19950106002941995010600294NE 1995 1 6 CKSA94353 219950103A7250516701 TUBINE BLADE DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE NR 3 ENGINE FAILED A CKSAE ENGINE SHUTDOWN JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 GL23812CK 45890 643333 KMCI - FLT 59901 - ON CLIMB-OUT, NR 3 ENGINE HAD A SUDDEN DROP IN EPR ACCOMPANIED BY SEVERE VIBRATION. ENGINE IMMEDIATELY SHUT DOWN. REMOVED AND REPLACED NR 3 IAW AIA DC-8 MIP-1 SECTION 9. C/W TRIM RUN ALL SYSTEMS. OPS CHECKS NORMAL IAW AIA MIP-1 SECTION 10, NO LEAKS NOTED. (X) 2L74 4F4 F 4A25 1E8 19950106003341995010600334EU 1995 1 6 9500013240 119950102A2926 HYD RESERVOIR AIRBUS320 A320211 3930320EU AFT FUSELAGE LOW FLUID A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01340NW 372 DURING TAKEOFF ROLL, RECEIVED "HYD B RSVR LO AIR PR" MESSAGE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE SERVICED THE BLUE HYDRAULIC SYSTEM RESERVOIR WITH APPROXIMATELY ONE GALLON OF FLUID. 2L72 4F RTA28NM 19950106003351995010600335NM 1995 1 6 9500022285 119950102A2760 HANDLE BOEING727 727251 138408HNM SPEED BRAKES NOT SEATED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01285US 21324 TAKEOFF WARNING HORN SOUNDED UPON APPLICATION OF DEPARTURE THRUST. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND AUTO SPEED BRAKES ON MEL REQUIRING THE HANDLE TO BE MANUALLY SEATED IN DETENT. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950106003361995010600336NM 1995 1 6 9500032702 119950101A2751 POSITION SWITCH BOEING727 727225 1384077NM TE FLAPS OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018877Z 21450 DURING 5 DEGREE FLAP TAKEOFF, AURAL WARNING HORN SOUNDED. ABORTED DEPARTURE. RECYCLED FLAPS AND SPEED BRAKES. SECOND DEPARTURE ATTEMPT WAS NORMAL. MAINTENANCE ADJUSTED FLAP POSITION SWITCH S196. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950106003371995010600337NM 1995 1 6 9500042202 119950103A274132EN144 POSITION SWITCH BOEING727 727251 138408HNM STABILIZER TRIM MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01202US 22155 DURING 5 DEGREE FLAP TAKEOFF AT 20 KNOTS, CENTRAL AURAL WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE UPPER STABILIZER TRIM POSITION WARNING SWITCH S532. OPERATIONAL CHECK NORMAL PER MM 31-26-24. 2L73 4F A3WE 19950106003381995010600338NM 1995 1 6 9500052290 119950103A2780BACB10EU08 BEARING BOEING727 727251 138408HNM NR 7 SLAT SEIZED A NWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL01290US 21378 DURING DEPARTURE CLIMB UPON FLAP RETRACTION (2 DEGREES TO UP), THE NR 7 LEADING EDGE SLAT REMAINED EXTENDED. RECYCLED FLAPS TO NO AVAIL. RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 7 LEADING EDGE SLAT INBOARD TRACK BEARING SEIZED. REPLACED BEARING. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950106003391995010600339NM 1995 1 6 95FDEA00001 119950104A2750 SPRING BOEING727 727233 138408ANM TE FLAPS FROZEN A FDEAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO04222FE 20933 AFTER TAKEOFF UPON FLAP RETRACTION, ASYMMETRIC OUTBOARD FLAPS, FLAPS IND DOESN'T MATCH DETENT, FLAP HANDLE IS DIFFICULT TO MOVE FROM 0 TO 2 DEGREES. FOUND LT OTBD FLAP TRANSMITTER RETRACT SPRING STIFF FROM COLD - FREED SPRING WITH HEAT - OPS CKS GOOD NOW. 2L73 4F RTA3WE 19950106003401995010600340NM 1995 1 6 95UAL727001 119950104A3350S109 BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE DOOR 1 L EEL DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297274U 21421 EMERGENCY EXIT LIGHT INOP DOOR 1 LT. REPLACED BATTERIES AND LIGHT ASSEMBLY. 2L73 4F4 F A3WE E2EA 19950106003411995010600341NM 1995 1 6 95UAL727002 119950104A3350S109 BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE DOOR 1 L/R DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297459U 21913 EMERGENCY EXIT LIGHT INOP DOOR 1 LT AND 1 RT. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19950106003421995010600342NM 1995 1 6 95UAL757001 119950104A2560 SLIDE AIRCRUISERS D31393110 BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT OFF WING DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29518UA 0307 24871 DURING OVERHAUL OF THE RIGHT OFF-WING SLIDE, THE WEBBING BETWEEN THE RAMP AND SLIDE PORTION OF THE UNDERSIDE DISBONDED FROM THE LOWER TRUNK TUBE. RE-ATTACHED DISBONDED WEBBING WITH ADHESIVE. 2L72 4F4 FRTA2NM E17NE 19950106003431995010600343EU 1995 1 6 95UALA32001 119950104A2130 PRESSURIZATION AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29419UA 487 AFTER TAKEOFF, RECEIVED AN ECAM CABIN PRESSURE SYSTEM NR 1 AND NR 2 FAULT. MANUAL MODE BACKUP WAS INOPERATIVE. RETURNED TO FIELD AND LANDED OVERWEIGHT. 2L72 4F RTA28NM E40NE 19950106003441995010600344WP 1995 1 6 95UALD10001 119950103A3397 WIRE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291856U 46975 EEL LIGHT ON RT AISLE B ZONE INOPERATIVE. REPLACED JUMPER CABLE. 2L73 4F4 F A22WE E23EA 19950106003451995010600345WP 1995 1 6 95UALD10002 119950103A3397 WIRE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291852U 47811 EEL STRIP LIGHT IN B ZONE LEFT AND RIGHT SIDE INOPERATIVE. REPLACED LEFT AND RIGHT SIDE JUMPER CABLE ASSEMBLIES. 2L73 4F4 F A22WE E23EA 19950106003471995010600347SW 1995 1 6 QXEA9500001 119950102A3260602EN16 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG INTERMITTENT A QXEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM0927186 AC707 HLN - NLG INTRANSIT LIGHT REMAINED ON AFTER LANDING GEAR SELECTED UP. FLIGHT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FERRIED TO PDX FOR REPAIRS. BOTH NLG UPLOCK SWITCHES WERE REPLACED AND ALL GROUND TESTS WERE NORMAL. AIRCRAFT RELEASED FOR SERVICE. 1L72 4T A8SW 19950106003481995010600348NM 1995 1 6 QXEA9500002 119950102A323310800113 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT MLG INTERMITTENT A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09841PH9643 082 PDX - LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. CREW SELECTED ALTERNATE EXTENSION AND GEAR CAME DOWN AND LOCKED. REPLACED LT MLG UPLOCK ACTUATOR AND ALL GROUND TESTS WERE NORMAL. AIRCRAFT RELEASED FOR SERVICE. 2H72 4T RTA13NM 19950106003491995010600349EU 1995 1 6 QXEA9500003 119950103A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 GEG - SEVERAL OVERHEAD EMERGENCY LIGHTS INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950113000691995011300069NM 1995 1 13 94UAL737281 119950104A4920 APU BOEING737 737* NM APU COMPT FOD A UALAF ACTIVATE FIRE EXT. CJ F.O.D. WARNING INDICATION TXTAXI/GRND HDL 1 WP29 95161 AT DEPARTURE, APU AUTO SHUTDOWN. WHEN RESTART WAS ATTEMPTED, THERE WAS A FIRE WARNING AND THE BOTTLE WAS DISCHARGED. APU INOPED AND EXTERNAL INSPECTION COMPLETED. APU WAS REPLACED. FOUND RAG IN THE INLET AND THE ROTATING GROUP HAD HIT THE STATIONARY GROUP CAUSING WHAT WE CALL METAL SPLATTER. THIS RESULTED IN DISASSEMBLY OF THE APU FOR FULL REBUILD. 2L72 4F RTA16WE 19950113000701995011300070 1995 1 13 94UAL737282 419950104A2565101658101 SLIDE BF GOODRIC BOEING737 737* NM TUBES FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29 DURING AIR RETENTION TEST OF AN AIRFORCE SLIDE, THE UNIT FAILED FOR POROSITY ALONG THE TUBES. SLIDE IS ON IT'S FIRST OVERHAUL. NOTIFIED THE AIRFORCE ABOUT THE FAILED UNIT. 2L72 4F RTA16WE 19950113000721995011300072NM 1995 1 13 94UAL747083 119950103A571165B082342 SPAR CHORD BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE BS 1000 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29154UA 20103 AT APPROXIMATELY, BS 1000, LBL 80 - 84, AN AREA OF CORROSION WAS DISCOVERED ON THE WING CENTER SECTION FRONT SPAR INSTALLATION. THE CORROSION (LEVEL 2) EXISTED ON LOWER CHORD (P/N 65B 08234-2) AND REQUIRED MATERIAL REMOVAL THAT EXCEEDED MAX ALLOWABLE LIMITATIONS. MAX MATERIAL REMOVED (APPROX 0.30 INCH DEEP) WAS IN THE OUTER FORWARD CORNER AREA. A NESTED ANGLE REPAIR WAS ACCOMPLISHED PER THE GUIDELINES OF THE 747 SRM 51-40-04 TO SUIT THIS PARTICULAR CONDITION. 2L74 4F4 F A20WE E20EA 19950113000731995011300073NM 1995 1 13 95FDEA00003 119950104A7931 BYPASS SWITCH BOEING727 727233 138408ANM NR 1 ENGINE MALFUNCTIONED A FDEAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO04274FE 22039 NR 1 ENG LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON AT APPROX 0450Z FL240 CRUISE. OIL PRESS WAS 47 PSI QUAN AND TEMP NORMAL RANGE RETARDED NR 1 THRUST LEVER TO IDLE LIGHT REMAINED ON SHUTDOWN NR 1 ENG IAW CHECK LIST. LIGHT STAYED ON ABOUT 4 MINS AFTER ENG START BEFORE LIGHT GOES OUT. REMOVED AND REPLACED NR 1 ENG LOW OIL PRESS FILTER BYPASS SW. LEAK AND OPS CK GOOD. RAN NR 1 ENG PER JRH OIL LOW PRESS/FILTER BYPASS LIGHT OPS CK'D NORMAL. 2L73 4F RTA3WE 19950113000741995011300074NM 1995 1 13 95FDEA00004 119950104A5610B275600102A WINDOW BOEING727 7272S2F 1384O81NM COCKPIT CRACKED A FDEAABI UNSCHED LANDING EMER. DESCENT CABIN DEPRESSURIZATION O OTHER CRCRUISE 1 SO04205FE 22927 R-2 WINDOW FAILED WHILE IN CRUISE AT FL 350 AND CABIN DIFF PRESS OF 8.4 PSI DESCENDED TO FL 240 AND REDUCED CABIN PRESS TO 5.0 PSI. APPEARS TO BE INNER PANE. REMOVED AND REPLACED NR 2 SLIDING WINDOW PER MM 56-12-11. 2L73 4F A3WE 19950113000761995011300076WP 1995 1 13 ABXA9500001 119950103A323056165545503ABX1 CYLINDER DOUG DC8 DC862 3021970WP LT MLG BOGIE BLOWN A ABXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23805AX 5299 45906 HYDRAULIC PRESSURE AND FLUID LOSS ON CLIMB-OUT. AIRCRAFT RETURNED TO ILN. FOUND LEFT MLG BOGIE TRIM CYLINDER BLOWN. REMOVED AND REPLACED CYLINDER IAW DC 8 MM CHAPTER 32. REMOVED AND REPLACED NR 2 AND NR 3 ENGINE HYDRAULIC PUMPS AND ASSOCIATED FILTERS. BLED HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK IAW DC 8 MM CHAPTER 29. 2L74 4F 4A25 19950113000771995011300077NE 1995 1 13 ABXA9500002 219950104A7200 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 2 FAILED A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23814AX 46041 671116 ON CLIMB-OUT OF ILN, NR 2 EPR DROPPED 1.75 TO 1.40. ALL OTHER ENGINE INDICATIONS DROPPED AT THE SAME TIME, ACCOMPANIED BY AN ENGINE VIBRATION. SHUT DOWN NR 2 ENGINE. AIRCRAFT CONTINUED TO ATL AND LANDED WITHOUT ANY FURTHER PROBLEMS. INSPECTED ENGINE ON GROUND AND NOTED TURBINE SECTION DAMAGE. INSPECTED, PREPARED, AND THREE-ENGINE FERRIED AIRCRAFT TO ILN. REMOVED AND REPLACED NR 2 ENGINE IAW DC 8 MM CHAPTER 72. 2L74 4F4 F 4A25 1E8 19950113000781995011300078 1995 1 13 COM11712 219950104A73203035817 FUEL HEATER EMB 120 EMB120RT SO LT ENGINE LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01254CA112481561 120233 LEFT ENGINE FUEL TO OIL HEAT EXCHANGER IS LEAKING FUEL. REPLACED HEAT EXCHANGER. 2L72 4T RTA31SO 19950113000791995011300079SO 1995 1 13 COM11713 119950101A3241426871 CONTROL BOX EMB 120 EMB120RT SO ANTI-SKID SYST DEFECTIVE A COMAO OTHER O OTHER LDLANDING 1 SO01256CA8968 767 120245 DURING LANDING ANTI-SKID FAILED. REPLACED THE ANTI-SKID CONTROL BOX. 2L72 4T RTA31SO 19950113000811995011300081SO 1995 1 13 COM11715 119950101A323020960 HOOK ASSY EMB 120 EMB120RT SO RT MLG LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01200CD13538 120200 RT MLG WILL NOT RETRACT. CLEANED AND LUBED RT MLG UPLOCK HOOK ASSY. FUNCTION CHECK OF LANDING GEAR SYSTEM SATISFACTORY. 2L72 4T RTA31SO 19950113000821995011300082SO 1995 1 13 COM11716 119950103A5246MS23085 SWITCH EMB 120 EMB120RT SO RT WING OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01254CA 120233 SERVICE DOOR WARNING LIGHT ILLUMINATED. ADJUSTED FUEL SERVICE DOOR MICROSWITCH. 2L72 4T RTA31SO 19950113000851995011300085SO 1995 1 13 COM11719 119950104A2910 HYD SYST EMB 120 EMB120RT SO LT NACELLE FROZEN A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01256CA 120245 GREEN SYSTEM HYDRAULIC RESEVOIR LOW PRESSURE INDICATOR ON. RESERVOIR PRESSURIZATION SYSTEM CONTAINED MOISTURE WHICH FROZE. PURGED MOISTURE FROM SYSTEM. 2L72 4T RTA31SO 19950113000871995011300087 1995 1 13 COM30990 319950103A61147503503AG O-RING SAAB SF340 SF340A 7850100EU LT PROP TWISTED A COMAK NONE O OTHER DEDESCENT 1 SO01344CA 340A025 LEFT PROPELLER FLUCTUATES 5 TO 10 RPM. REPLACED PROPELLER PISTON DOME O-RING. 2L72 4T RTA52EU 19950113000901995011300090EA 1995 1 13 COM60360 119950103A2430HA4A039 CONTACTOR CNDAIRCL600 CL6002B19 EA AVIONICS FAILED A COMAD RETURN TO BLOCK JH WARNING INDICATION ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 SO01914CA4128 7012 ESS TRU DROPS OFF LINE. REPLACED THE ESS POWER TRANSFER CONTACTOR. 2L72 4F RTA21EA 19950113000911995011300091EA 1995 1 13 COM60361 119950104A2750 RETRACT MECH CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 SO01915CA 7013 FLAPS FAIL MESSAGE ON EICAS. FLAPS STUCK AT ZERO DEGREES. COULD NOT DUPLICATE. CLEARED FAULTS FROM FLAP ELECTRONIC CONTROL UNIT AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950113000921995011300092 1995 1 13 COM60362 419950102A22106229968001 YAW DAMPER CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE JF WARNING INDICATION FLT CONT AFFECTED UKUNKNOWN 1 SO01918CA595 7018 YAW DAMPER NR 2 IS INOP. REPLACED THE YAW DAMPER. 2L72 4F RTA21EA 19950113000931995011300093EA 1995 1 13 COM60363 119950103A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01917CA1535 1108 7017 FLAPS FAILED WHEN SELECTED FOR TAKEOFF. REPLACED THE LEFT BRAKE AND POSITION SENSOR UNIT. 2L72 4F RTA21EA 19950113000941995011300094EA 1995 1 13 COM60364 119950101A2820B9738665 VALVE CNDAIRCL600 CL6002B19 EA WING INOP A COMAK NONE O OTHER UKUNKNOWN 1 SO01931CA2086 7037 GRAVITY FUEL CROSS FLOW VALVE IS INOP. REPLACED CROSS FLOW VALVE. 2L72 4F RTA21EA 19950113000981995011300098NM 1995 1 13 UPS201906 119950104A3350 EEL BATTERY BOEING727 727247 138408FNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01211UP 21700 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT ON OVERHEAD ON ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES. PERFORMED OPS CHECK. OP CHK GOOD ON GROUND. 2L73 4F A3WE 19950113000991995011300099NM 1995 1 13 UPS201909 119950102A3350 EEL BOEING727 72725C 138400HNM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01948UP 19357 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT INOP. INSTALLED SERVICEABLE EMERGENCY LIGHT ASSY. OPS CHECK GOOD. 2L73 4F A3WE 19950113001001995011300100NM 1995 1 13 UPS201910 119950105A3350 EEL BOEING727 727180C 138406GNM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01921UP 19874 MAINTENANCE REPORTED FWD ENTRY DOOR EMER LIGHT INOP. REMOVED EMER LIGHT UNIT. REPLACED WITH SERVICEABLE UNIT, BATT CHARGE DATE 8-94. OPS CHECK OK. PER AMM 33-40. 2L73 4F A3WE 19950113001011995011300101NM 1995 1 13 UPS201911 119950105A2612 CONNECTOR BOEING727 72725C 138400HNM NR 2 ENGINE LOOSE A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01950UP 19718 PILOT REPORTED NR 2 ENGINE FIRE DETECTION (GRD FAULT LIGHT) FLICKERS ENROUTE, LIGHT REMAINED OUT ON LANDING. CLEANED AND RESECURED LOOP CONNECTOR. GROUND CHECKS GOOD. 2L73 4F A3WE 19950113001031995011300103NM 1995 1 13 UPS401912 119950103A3350 EEL BOEING747 747123F NM FLIGHT DECK FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 PILOT REPORTED SEVERAL EMER LIGHTS UNDER INSTRUMENT GLARESHIELD ARE BURNED OUT. CENTER BULBS ON BOTH ENDS. F/O,FAR RIGHT BULB. RELAMPED EMERGENCY LIGHTING. OPS CHECK GOOD. 2L74 4F A20WE 19950113001041995011300104WP 1995 1 13 UPS801907 119950103A3260 PROX SWITCH DOUG DC8 DC871F 302199DWP RT MLG DOOR MALFUNCTION A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01708UP 46048 PILOT REPORTED DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH CHECK LIST AND CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED RT MLG DOOR PROX SWITCH WITH SERVICEABLE UNIT. PERFORMED OPS CHECK OK. 2L74 4F RT4A25 19950113001051995011300105WP 1995 1 13 UPS801908 119950104A3260 CONNECTOR DOUG DC8 DC871F 302199DWP LT MLG LOOSE A IPXAO OTHER N FALSE WARNING LDLANDING 1 SO01797UP 45897 PILOT REPORTED, LEFT MLG DOES NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN. CYCLED GEAR 3 TIMES. ERM CHECKLIST COMPLETED WITH REQUIRED VISUAL FLY BY (CHANGED BULBS-DID NOT WORK). FOUND PLUG P1-213 LOOSE AND CONTAMINATED. CLEANED AND SECURED PLUGS AND PINS ON SWITCH PS1-208 AND REINSTALLED PLUG. CKD INSTALLATION AT S1-208 MECH SWITCH PER M/M 32-60-00 PG 201. LEFT MAIN DOWN AND LOCKED INDICATON NOW NORMAL. 2L74 4F RT4A25 19950113002961995011300296WP 1995 1 13 9500199955 119950104A3260 UPLOCK SWITCH DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01922RW 47182 DURING APPROACH INTO MSP, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED FOR LANDING. PERFORMED GO-AROUND AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. REPLACED THE NOSE GEAR UPLOCK SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113002971995011300297EU 1995 1 13 9500233214 119950107A2750 RETRACT MECH AIRBUS320 A320211 3930320EU TE FLAPS MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01314US 160 DURING APPROACH INTO PHX RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT. ACCOMPLISHED A FLAPS LESS THAN ONE LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTION OF THE FLAP DRIVE MECHANISM REVEALED NO DISCREPANCY. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950113002981995011300298NE 1995 1 13 9500246304 219950108A7397 WIRE BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 3 ENGINE SHORTED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01664US 23819 717578 DURING INITIAL POWER APPLICATION FOR TAKEOFF (KIX), THE NR 3 ENGINE HAD NO RESPONSE AND THE TAKEOFF WAS ABORTED. A WIRE TO THE RESOLVER WAS FOUND RUBBING A STAND OFF AND WAS REPAIRED. A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 FRTA20WE E24NE 19950113002991995011300299NE 1995 1 13 9500256614 219950108A7230 COMPRESSOR BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 3 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK RMJPARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION TOTAKEOFF 1 GL01614US 20359 662502 DURING INITIAL POWER APPLICATION FOR TAKEOFF WITH 14-26 KT WIND, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE ENGINE AND MAGNETIC SUMP PLUGS WERE INSPECTED AND A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BORESCOPE IS SCHEDULED. 2L74 4F4 F A20WE E20EA 19950113003001995011300300EU 1995 1 13 9500263214 119950108A2750 FLAP DRIVE AIRBUS320 A320211 3930320EU LT TE FLAP OUT OF RIG A NWAAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 GL01314US 160 DURING APPROACH INTO SNA RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN SELECTING FLAPS 3. THE FLAPS WERE LOCKED AT ZERO. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE NR 1, 2, 3, AND 4 LEFT WING FLAP ACTUATORS. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950113003011995011300301EU 1995 1 13 9500273242 119950109A3610 DUCT AIRBUS320 A320211 3930320EU RT AC BAY LEAKING A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01342NW 381 DURING CLIMBOUT FROM DTW, RECEIVED 'AIR R WING LEAK' MESSAGE. ACCOMPLISHED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PNEUMATIC DUCT LEAKING FORWARD OF RIGHT PACK FLOW CONTROL VALVE. TIGHTENED CLAMP. LEAK CHECK OK. 2L72 4F RTA28NM 19950113003021995011300302NM 1995 1 13 9500282707 119950106A21507005 SWITCH BOEING727 727225 1384077NM ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TOTAKEOFF 1 GL01816EA 22553 DURING TAKEOFF, AUTO PACK TRIP SYSTEM DID NOT ARM. TAKEOFF WAS ABORTED. MAINTENANCE REPLACED S690, S691, AND S692 ENGINE PNEUMATIC PRESSURE SENSING SWITCHES. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950113003031995011300303WP 1995 1 13 9500299758 119950106A2420 AC GEN SYST DOUG DC9 DC941 302207NWP LEFT MALFUNCTIONED A NWAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION UKUNKNOWN 1 GL01758NW 47286 LOSS OF LEFT DC BUS AND TWO AC PHASE OCCURRED ENROUTE MDT-DTW. FLIGHT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AC POWER RELAY, VOLTAGE REGULATOR, GENERATOR CONTROL PANEL, AND LEFT ENGINE GENERATOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003041995011300304WP 1995 1 13 9500309930 119950107A3231 CONTROL CABLE DOUG DC9 DC931 3022065WP NLG DOOR BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL0189S 47042 EXCESSIVE VIBRATION WAS COMING FROM THE NOSE LANDING GEAR AREA AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSO AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND NOSE GEAR DOOR STOP CABLE BROKEN. REMOVED BROKEN CABLE; CLOSED AND SECURED NOSE GEAR DOORS. DEFERRED REPAIR PER MEL 32-7. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003051995011300305WP 1995 1 13 9500319102 119950106A7711 PT7 TUBE DOUG DC9 DC915 3022036WP PWA JT8 JT8D7 52053NE RT ENGINE BROKEN A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0192S 47063 657525 ON TAKEOFF, THE NR 2 EPR WAS .2 BELOW NR 1 WITH OTHER PARAMETERS MATCHED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. THE EPR TRANSMITTER WAS REPLACED. A BROKEN PT7 TUBE WAS FOUND BETWEEN THE 2 O'CLOCK AND 4 O'CLOCK PROBES. REPLACED THE PT7 TUBE. ENGINE RUN-UP CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950113003061995011300306WP 1995 1 13 9500329859 119950108A3260 UPLOCK MECH DOUG DC9 DC951 3022051WP LT MLG CONTAMINATED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01768NC 47729 LEFT MAIN LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. INSPECTED GEAR AND DOOR PROXIMITY SWITCHES AND TARGETS. CLEANED UPLOCK MECHANISM. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003071995011300307WP 1995 1 13 9500339876 119950109A3260 PROX CONTL BOX DOUG DC9 DC951 3022051WP NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01785NC 48110 NOSE LANDING GEAR RED UNSAFE LIGHT ILLUMINATED ON APPROACH INTO DTW. LIGHT EXTINGUISHED WHEN GEAR WAS EXTENDED. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION AND AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. REPLACED NOSE GEAR UPLOCK SENSOR AND PROXIMITY CONTROL BOX. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003081995011300308WP 1995 1 13 ABXA9500003 119950109A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC933F 302207AWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23935AX 3000 47413 COCKPIT EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES. OPS CHECKED GOOD IAW DC-9 M.M. 33-53-0. 2L72 4F A6WE 19950113003091995011300309 1995 1 13 COM11723 419950107A3197 SPLICE EMB 120 EMB120RT SO ELEVATOR DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01159A 533 533 120159 TAKEOFF TRIM AURAL WARNING ACTIVATED. REPAIRED DEFECTIVE WIRE SPLICES AT ELEVATOR TRIM PROXIMITY SENSORS. 2L72 4T RTA31SO 19950113003101995011300310SO 1995 1 13 COM11724 119950109A71701126005 EPA CHECK VALVE EMB 120 EMB120RT SO LT NACELLE LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01159A 120159 FUEL LEAK, LT NACELLE. REPLACED EPA SYSTEM CHECK VALVE. 2L72 4T RTA31SO 19950113003111995011300311EU 1995 1 13 COM30998 119950108A302032899541 AIR VALVE SAAB SF340 SF340A 7850100EU RT ENGINE DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01158CA164421095 340A158 RT ENGINE AIR VALVE WARNING LIGHT IS ON. REPLACED RT AIR VALVE. 2L72 4T RTA52EU 19950113003121995011300312 1995 1 13 COM30999 319950108A6114660712675 PISTON DOME SAAB SF340 SF340A 7850100EU LT PROP WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01344CA 3003 340A025 LT PROPELLER IS FLUCTUATING 50 RPM. REPLACED THE PROPELLER PISTON DOME. 2L72 4T RTA52EU 19950113003131995011300313EU 1995 1 13 COM31000 119950109A2730DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100EU LT PITCH TRIM DEFECTIVE A COMAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SO01359CA1563852 340A053 MAIN PITCH TRIM OPERATES WITH ONLY ONE-HALF OF SWITCH DEPRESSED. REPLACED LT PITCH TRIM ACTUATOR. 2L72 4T RTA52EU 19950113003141995011300314NE 1995 1 13 COM31001 219950108A7200 ENGINE ROTOL R3894123F SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01357CA 1636 876584 340A044 367209 LT PROPELLER RPM DROPS TO 1300 DURING APPROACH PHASE OF LANDING. REPLACED LT ENGINE. 2L72 4T4 TRTA52EU E8NE6 19950113003151995011300315WP 1995 1 13 MWEA95004 119950107A52105914121 DOOR PAN DOUG DC9 DC914 3022034WP FWD PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31800ME 45842 DURING "C" CHECK INSP, A 3 INCH CRACK WAS FOUND IN THE INNER PAN AFT SIDE NEAR THE LOWER STOP BRACKET OF THE MAIN FWD PASSENGER ENTRANCE DOOR. THE DOOR WAS REPAIRED BY SPLICING A NEW PAN SEGMENT INTO THE EXISTING PAN IAW SRM 51-30-02. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003161995011300316WP 1995 1 13 MWEA95005 119950110A53119912246 FRAME DOUG DC9 DC932 3022066WP FS 1038.868 CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 DURING SERVICE CHECK FOUND FWD SIDE WEB OF STA 1038.868 RIB CHAFED BY THE LEFT TEMP CONTROL VALVE. REPOSITIONED THE TEMP CONTROL VALVE. FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-01, FIG. 4. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950113003171995011300317NM 1995 1 13 SWAA950001 119950102A5320 WEB BOEING737 7375H4 138449DNM CARGO DOORWAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND AFT CARGO DOOR WEB CRACKED AND TORN AT AFT END OF DOORWAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950113003181995011300318NM 1995 1 13 SWAA950002 119950102A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 987 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, RBL 23, 28, 32, 36, 40, AND 43. REPAIRED PER SWA RA 1-553-1232. 2L72 4F RTA16WE 19950113003191995011300319NM 1995 1 13 SWAA950003 119950102A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 947, LBL 5, AND RBL 5. REPAIRED PER SWA RA 1-553-1229. 2L72 4F RTA16WE 19950113003201995011300320NM 1995 1 13 SWAA950004 119950102A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 987 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, LBL 35. REPAIRED PER SWA RA 1-553-1230. 2L72 4F RTA16WE 19950113003211995011300321NM 1995 1 13 SWAA950005 119950102A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 987 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, RBL 26. REPAIRED PER SWA RA 1-553-1231. 2L72 4F RTA16WE 19950113003221995011300322NM 1995 1 13 SWAA950006 119950102A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 987 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM FORWARD FLANGE SCREW HOLE CORROSION AT BS 987, LBL 15. REPAIRED PER SWA RA 1-553-1232. 2L72 4F RTA16WE 19950113003231995011300323NM 1995 1 13 SWAA950007 119950102A5320 ANGLE BOEING737 7375H4 138449DNM BS 294 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND FORWARD GALLEY RIGHT SIDE Z-ANGLE CORRODED BETWEEN BS 294 TO 312, BELOW THRESHOLD ATTACH POINTS. REPAIRED PER SWA RA 1-553-1228. 2L72 4F RTA16WE 19950113003241995011300324NM 1995 1 13 SWAA950008 119950107A5320 SKIN BOEING737 7372H4 138448CNM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947 AT STRINGER 24R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950113003251995011300325NM 1995 1 13 SWAA950009 119950107A5330 SKIN BOEING737 7373H4 1384600NM BS 812 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 2 INCH FUSELAGE SKIN CRACK AT BS 812, AT STRINGER 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950113003261995011300326NM 1995 1 13 SWAA950010 119950107A5330 SKIN BOEING737 7373H4 1384600NM AFT OF CARGO DR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07318SW 23339 DURING SCHEDULED SERVICE CHECK, FOUND 4 INCH FUSELAGE SKIN CRACK 24 INCHES AFT OF AFT CARGO DOOR. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950113004701995011300470WP 1995 1 13 9500349862 119950108A7330 FUEL TEMP SENSOR DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE RT ENGINE DEFECTIVE A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01771NC 47769 688231 AFTER DEPARTURE, THE NR 2 FUEL TEMPERATURE WAS FLUCTUATING FROM PLUS 30 TO MINUS 60 DEGREES. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND FUEL TEMPERATURE SENSOR DEFECTIVE. REPLACED SENSOR. ENGINE TUNE-UP CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950113004711995011300471NM 1995 1 13 9500356612 119950109A5315 FLOOR BEAM BOEING747 747251B 1384892NM FS 600 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, FOUND CORROSION ON CABIN FLOOR BEAM AT FS 600, RBL 23. REMOVED CORROSION, FABRICATED REPAIR, AND INSTALLED. 2L74 4F A20WE 19950113004721995011300472EU 1995 1 13 9500363213 119950110A213087292325V04 COMPUTER AIRBUS320 A320211 3930320EU E/E BAY FAILED A NWAAA UNSCHED LANDING JO WARNING INDICATION OTHER CLCLIMB 1 GL01313US4658 4658 153 DURING CLIMB-OUT FROM DTW, RECEIVED 'VENT SKIN VALVE' FAULT. UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950113004731995011300473EU 1995 1 13 9500373202 119950106A2130VFT300A1 VALVE AIRBUS320 A320211 3930320EU FUSELAGE SKIN MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01302US9040 5308 32 DURING CLIMB-OUT FROM MSP, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SKIN AIR EXTRACT VALVE. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950113004741995011300474EU 1995 1 13 9500383247 119950110A5270 HANDLE AIRBUS320 A320211 3930320EU AFT CARGO DOOR NOT STOWED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01347NW 408 DURING TAKEOFF ROLL, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE NOT FAIRED. STOWED HANDLE AND ALL INDICATIONS WERE NORMAL. 2L72 4F RTA28NM 19950113004751995011300475WP 1995 1 13 95FDEA00005 119950107A36101555M23601 DUCT DOUG DC10 DC1030F 3023504WP 14TH STAGE FAILED A FDEAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 SO04322FE 47908 ENG FIRE IN NR 2 ENG SHORTLY AFTER ROTATION. OBSERVED EGT REACHED 899 DEG. MEMORY ITEMS ACCOMP, CKLT PROCED COMPLIED WITH, RETURNED TO OAK FOR UNEVENTFUL LANDING (FIRE HANDLE PULLED, BOTTLE NOT DISCHARGED). REPLACED 14TH STAGE LWR CROSSOVER DUCT, LPT COOLING MANIFOLD RIGHT SIDE. REPLACED B, C AND D OIL SUMP SCAVENGE TUBES. REPLACED PYLON DRAW TUBES 3 FWD STRUTS AND 2 AFT STRUTS. 2L73 4F RTA22WE 19950113004761995011300476NM 1995 1 13 95FDEA00006 119950110A5210 DOOR BOEING727 727227 1384078NM FWD ENTRY REQ RIG A FDEAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO04481FE 21463 FWD ENTRY DOOR OPENED APPROX 3 0R 4 INCHES AFTER A/C WAS DEPRESSURIZED ON TAXI IN AT MEM. RIGGED DOOR IAW MM 52-11-01, PG 514 (3 A-D). REINSTALLED LINER AND SLIDE. 2L73 4F A3WE 19950113004851995011300485NM 1995 1 13 DL72L950040 119950102A5400 SKIN BOEING727 727232 1384082NM S DUCT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, NR 2 INLET SKIN IS DAMAGED INSIDE 'S' DUCT AT THE 1 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 13. 2L73 4F A3WE 19950113004861995011300486NM 1995 1 13 DL72L950053 119950102A5313 STRINGER BOEING727 727232 1384082NM STA 720C STR 15LCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, STRINGER 15L CRACKED AT STA 720C. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950113005001995011300500NM 1995 1 13 DL72S950033 119950103A5521 ANGLE BOEING727 727232 1384082NM LEFT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 DURING LETTER CHECK, THE LEFT ELEVATOR INTERNAL SUPPORT ANGLE INSIDE ACCESS PANEL 9307 WAS FOUND CRACKED. REPAIRED PER SRM 55-21-4 FIG 1. 2L73 4F A3WE 19950113005011995011300501NM 1995 1 13 DL72S950044 119950104A5720 STIFFENER ANGLE BOEING727 727232 1384082NM LEFT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING LETTER CHECK, A 3 INCH CRACK WAS FOUND IN THE VERTICAL STIFFENER ANGLE ON THE WING FRONT SPAR ON THE OUTBOARD SIDE OF NR 3 SLAT OUTBOARD TRACK ROLLER FITTING. REPAIRED PER MM 57-20-21 PG. 813. 2L73 4F A3WE 19950113005021995011300502NM 1995 1 13 DL72S950045 119950104A5414 SKIN BOEING727 727232 1384082NM RT SIDE S DUCT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING LETTER CHECK, THE NR 2 ENGINE S DUCT HOUSING RIGHT SIDE OUTER SKIN WAS FOUND WITH A 1.25 INCH CRACK EXTENDING UP FROM ACCESS PANEL 9524. REPAIRED PER MM 54-30-0 PG 803. 2L73 4F A3WE 19950113005031995011300503NM 1995 1 13 DL72S950046 119950104A5754 SLAT BOEING727 727232 1384082NM LEFT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING LETTER CHECK, LEFT WING NR 4 LEADING EDGE SLAT WAS FOUND WITH TWO .5 INCH CRACKS ON THE LOWER SKIN IN THE RADIUS OF THE INBOARD SLAT TRACK FAIRING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950113005051995011300505NM 1995 1 13 DL72S950048 119950104A5754 SLAT RIB BOEING727 727232 1384082NM LEFT WING NR 4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING LETTER CHECK, FOUND LEFT WING NR 4 LEADING EDGE SLAT WITH A .5 INCH CRACK IN THE NOSE RIB JUST OUTBOARD OF ACTUATOR ROD ATTACH FITTING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950113005061995011300506NM 1995 1 13 DL72S950066 119950106A5312 BULKHEAD BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING LETTER CHECK, FOUND A .75 INCH CRACK IN FS 1183 BULKHEAD WEB AT UPPER EDGE OF HORIZONTAL STIFFENER AT WL 168 AT RBL 25. REPAIRED PER SRM 53-10-9 FIG 6. 2L73 4F A3WE 19950113005071995011300507NM 1995 1 13 DL72S950082 119950106A2424939D1502 REGULATOR BOEING727 727232 1384082NM E/E COMPARTMENT FAULTY A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO11540DA 22386 DURING CRUISE, WITH NR 2 GENERATOR INOP NR 3 BUS-TIE BREAKER TRIPPED. DIVERTED FLIGTH TO DFW. FOUND NR 3 VOLTAGE REGULATOR FAULTY. REPLACED REGULATOR OPERATION NORMAL. 2L73 4F A3WE 19950113005111995011300511NM 1995 1 13 DL72W950079 119950107A3320036405 BALLAST BOEING727 727247 138408FNM CABIN SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO112807W 20579 DURING CRUISE, CABIN CEILING LIGHTS CIRCUIT BRAKER TRIPPED. HAD BURNING ODOR AT SEAT ROW 13. FOUND BALLAST FOR CEILING LIGHTS SHORTED. REPLACED BALLAST OPERATION NORMAL. 2L73 4F A3WE 19950113005291995011300529NM 1995 1 13 DL757950001 119950101A2530256001014 OVEN BOEING757 757232 1384965NM FWD GALLEY FAULTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11675DL 25980 DURING CRUISE, NOTICED ELECTRICAL BURNING ODOR IN FORWARD GALLEY. DEACTIVATED GALLEY EQUIPMENT ODOR DISSIPATED. FOUND ODOR COMING FROM FWD OVEN, REPLACED OVEN OPERATION NORMAL. 2L72 4F RTA2NM 19950113005341995011300534NM 1995 1 13 DL757950067 119950105A5753 FLAP BOEING757 757232 1384965NM RT WING GOUGED SKIN A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 DURING LETTER CHECK, RIGHT WING NR 4 AFT FLAP LOWER SKIN WAS FOUND GOUGED BETWEEN THE NR 7 AND NR 8 FLAP FAIRING. REPAIRED PER SMR 57-70-05. 2L72 4F RTA2NM 19950113005351995011300535NM 1995 1 13 DL757950081 119950106A4900380029815 APU BOEING757 757232 1384965NM APU COMPARTMENT LOOSE LINE A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO11676DL 25981 DURING CRUISE, HAD RIGHT ENGINE GENERATOR LIGHT, DISCONNECTED GENERATOR PER POM, APU FAILED TO START. DIVERTED TO MSP. SERVICED APU WITH 4 PINTS OF OIL, BITE CHECK, NORMAL. NEXT DAY APU AUTO SHUT DOWN AT FL 350. RT GENERATOR DEFFERRED, DIVERTED ATL. BITE CHECK SHOWED FAULT FAN ISOLATION VALVE. FOUND LINE LOOSE AND LEAKING ON FAN ISOLATION VALVE, SECURED LINE OPERATION NORMAL. 2L72 4F RTA2NM 19950113005381995011300538NE 1995 1 13 DL76L950083 219950107A7200PW4060 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE FAILED A DALAAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CLCLIMB 1 SO11179DN16001 25144 724314 DURING CLIMB-OUT AT FL 120, HAD VIOLENT VIBRATION ON RIGHT ENGINE. EGT SHOT UP TO 756 DEGREES. SHUT DOWN NR 2, RETURNED TO AMS. ENGINE WAS REPLACED AND ROUTED TO SHOP.SHUTDOWN 2L72 4F4 FRTA1NM E24NE 19950113005391995011300539NM 1995 1 13 DL76S950078 119950107A25301811150417 DISPENSER BOEING767 767332 1382001NM AFT GALLEY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11136DL 23146 DURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE AND BURNING ODOR FROM COFFEEMAKERS IN AFT GALLEY. REMOVED POWER, AND ODOR STOPPED. FOUND THE RIGHT REAR COFFEEMAKER SHORTED. REPLACED COFFEEMAKER OPERATION NORMAL. 2L72 4F RTA1NM 19950113005411995011300541WP 1995 1 13 DLL10950041 119950104A33408906K1665 SWITCH LKHEED1011 10113851 5265010WP COCKPIT BURNED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11720DA 193C1136 DURING DESCENT, CAPTAIN TURNED ON OVERHEAD PANEL AND EYE BROW PANEL LIGHTS AND A BURNING ODOR WAS NOTICED. AFTER LANDING INSPECTION, DISCOVERED THE RIGHT WING LANDING LIGHT SWITCH WITH EVIDENCE OF ARCING. REPLACED SWITCH AND TERMINALS, OPERATION NORMAL. 2L73 4F A23WE 19950113005431995011300543WP 1995 1 13 DLL13950080 119950105A36107724601 SENSOR LKHEED1011 10113851 5265010WP NR 3 PNEUMATICS FAULTY A DALAOH OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11788DL 193A1141 DURING DESCENT, HAD NR 3 ENGINE HP DUCT OVERHEAT WHEN USING AIRFOIL AND ENGINE ANTI-ICE. FOLLWED PROCEDURE PER PDM AND OVERHEAT REOCCURED. SHUTOFF BOTH ENGINE ISOLATION AND HIGH PRESSURE VALVE FOR NR 3 ENGINE, OVERHEAT WENT OUT THEN ENTIRE CABIN FILLED WITH SMOKE. LANDED SLC WITHOUT INCIDENT. TROUBLESHOOTING FOUND NR 3 AIR EJECTOR AIR TEMP SENSOR FAULTY. REPLACED SENSOR OPERATION NORMAL. 2L73 4F A23WE 19950113005451995011300545NM 1995 1 13 DLM88950028 119950102A71105930645505 COWL DOUG MD88 MD88 3023688NM ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11930DL 49717 DURING SHOP INSPECTION, FOUND DENTS AND GOUGE ON LEADING EDGE LIP AT 6,9,5,4 O'CLOCK POSITIONS OF ENGINE INTAKE COWL. REPAIRED DAMAGE PER SRM 54-04. 2L72 4F RTA6WE 19950113005481995011300548NE 1995 1 13 DLM88950077 219950107A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11955DL15846 49886 718177 DURING TAKEOFF, CABIN FILLED WITH SMOKE, RETURNED TO ATL. ENGINE RUN UP DISCOVERED NR 1 ENGINE PRODUCING SMOKE AT HIGH POWER SETTINGS. ENGINE WAS REPLACED AND ROUTED TO SHOP. 2L72 4F4 FRTA6WE E9NE 19950113005491995011300549NE 1995 1 13 SWAA950011 219950108A7250 ENGINE BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE NBR 1 OVERTEMP A SWAAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 SW07510SW 24187 725711 EXPERIENCED NUMBER 1 ENGINE FLAMEOUT. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND AFT TURBINE SECTION DAMAGE. REPLACED ENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F4 FRTA16WE E2GL 19950113007191995011300719NM 1995 1 13 9500405520 119950109A7930 INDICATION BOEING757 757251 1384970NM PWA 2037 PW2037 NE ENG OIL MALFUNCTION A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01520US 23208 716459 DURING CRUISE, RECEIVED 'L ENG OIL COOL' AND 'L ENG PRICONT' STATUS MESSAGE. THE EPR BLANKED OUT AT THE LOWER POWER SETTINGS BELOW 1.1 EPR. OIL TEMPERATURES REMAINED IN NORMAL POWER RANGES. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ELECTRONIC ENGINE CONTROL ALTERNATOR STATOR AND LEFT PROPULSION DISCRETE INTERFACE UNIT. SYSTEM CHECKED NORMAL ON GROUND RUN. 2L72 4F4 FRTA2NM E17NE 19950113007201995011300720EU 1995 1 13 9500413233 119950105A71202380210505 THRUST LINK AIRBUS320 A320211 3930320EU FWD ENG MOUNT WEAR MARKS A ANWAAK NONE O OTHER ININSP/MAINT 1 GL01333NW 329 DURING C-CHECK, FOUND THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE INBOARD AFT MOUNT LINK WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY RHOR CMM 71-22-07. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.0005 INCH TO 0.001 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-095310 AND 32-96330. 2L72 4F RTA28NM 19950113007211995011300721NM 1995 1 13 95FDEA00007 119950108A275196010212 TRANSMITTER DOUG MD11 MD11F 3023600NM LT WING FLAP MALFUNCTION A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO04611FE 48604 NRT - CONTINUOUS LANDING GEAR AURAL ALERT AT 1500 FT ON CLIMBOUT. GEAR UP INDICATIONS NORMAL, RECYCLED GEAR NO EFFECT, CONFIRMED GEAR/FLAPS UP ON CONFIG PAGE DURING GEAR RECYCLE AURAL WARNING STOPPED WHEN GEAR WAS DOWN AND LOCKED. FOUND WATER ACCUMLATION AT LEFT WING OUTBD FLAP XMTR, REPLACED FLAP XMTR AND CLEANED CONNECTOR. ALSO, REPLACED AURAL WARNING UNIT FOR PRECAUTIONARY. 2L73 4F RTA22WE 19950113007221995011300722NM 1995 1 13 95FDEA00008 119950108A275110573334195 CONNECTOR DOUG MD11 MD11F 3023600NM LT WING FLAP CONTAMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO04611FE 48604 NRT - LANDING GEAR AURAL WARNING CAME ON AT 1500 FT ON CLIMB-OUT GEAR AND FLAP POSITIONS CONFIRMED UP NORMAL WARNING OFF WHEN GEAR WAS LOWERED FOR LANDING. FOUND CONNECTOR P1-1111 PIN S HAD BAD INSULATION BY MEGER TESTER FOR LEFT OUTBD FLAP POS XMTR T2-5 ALSO WATER AND DE-ICE FLUID CONTAMINATION AT FLAP TRACK FAIRING. REPLACED CONNECTOR P1-1111 AND CLEANED WATER AND DE-ICE FLUID. LANDING GEAR AND CENTER AURAL WARNING F/O OK. 2L73 4F RTA22WE 19950113007231995011300723SO 1995 1 13 COM11725 119950105A301038E966A VALVE EMB 120 EMB120RT SO WING CENTER LEAKING A COMAK NONE MJ OVER TEMP WARNING INDICATION APAPPROACH 1 SO01152CA7350 2035 120152 RT DUCT LEAK WARNING LIGHT ILLUMINATED. REPLACED THE AIR FOIL DE-ICE REGULATING VALVE. 2L72 4T RTA31SO 19950113007241995011300724NE 1995 1 13 COM11726 219950109A7261310344601 SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO01137H 120137 115239 FLUID LEAKING FROM LEFT ENGINE. REPLACED THE CENTRIFUGAL BREATHER CARBON SEAL. 2L72 4T4 TRTA31SO E20NE 19950113007251995011300725 1995 1 13 COM20349 419950109A34205222644011 SLAVING ACCY SWRNGNSA227 SA227AC 8780603SW AVIONICS DEFECTIVE A COMAK NONE O OTHER NRNOT REPORTED 1 SO01459AM1357612807 AC700 PILOTS HSI HEADING IS OFF BY 20 DEGREES. REPLACED THE NR 1 SLAVING ACCY. 1L72 4T A8SW 19950113007261995011300726EU 1995 1 13 COM31002 119950111A26131734362450 DETECTOR SAAB SF340 SF340A 7850100EU RT EXHAUST DIRTY A COMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01370CA 340A010 RT 'TAILPIPE HOT' WARNING ILLUMINATED DURING FLIGHT. CLEANED WIRE CONNECTIONS AT TAILPIPE HEAT DETECTORS. 2L72 4T RTA52EU 19950113007271995011300727NE 1995 1 13 COM31003 219950111A73206055T19P14 HMU SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE DEFECTIVE A COMAK NONE O OTHER NRNOT REPORTED 1 SO01343CA9591 273 340A024 367200 COMPRESSOR STALLS AND TEMP RISE DURING LEFT ENGINE START. AUTO IGNITION COMES ON INTERMITTENTLY DURING FLIGHT. REPLACED THE HMU. 2L72 4T4 TRTA52EU E8NE6 19950113007281995011300728EA 1995 1 13 COM60367 119950110A2760 SPOILER CNDAIRCL600 CL6002B19 EA NR 1/NR 2 FAULT STATUS A COMAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 SO01914CA 7012 FLIGHT SPOILERS FAULT STATUS MESSAGE IS ACTIVE. RESET SECU NR 1 AND NR 2. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950113007291995011300729EA 1995 1 13 COM60368 119950111A323016600101 UPLOCK CNDAIRCL600 CL6002B19 EA NLG MALFUNCTION A COMAO OTHER O OTHER APAPPROACH 1 SO01920CA2611 7022 NLG DID NOT EXTEND. CYCLED LANDING GEAR TWICE AND NLG EXTENDED NORMALLY. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE NLG UPLOCK ACTUATOR FOR TROUBLESHOOTING. 2L72 4F RTA21EA 19950113007301995011300730 1995 1 13 COM60369 419950107A256245301502B ELT CNDAIRCL600 CL6002B19 EA AFT EQUIP BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2924 7027 C-CHECK INSPECTION, ELT AFT MOUNT CAP IS DAMAGED, ELT CASE IS BROKEN AND ELT IS INOP. INSTALLED NEW ELT ASSY. 2L72 4F RTA21EA 19950113007311995011300731EA 1995 1 13 COM60370 119950107A2612601R5790013 HARNESS CNDAIRCL600 CL6002B19 EA LT ENGINE BURNED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2924 7027 C-CHECK INSPECTION, LEFT ENGINE B LOOP FIRE DETECT HARNESS BURNED. REPLACED B LOOP HARNESS. 2L72 4F RTA21EA 19950113007321995011300732EA 1995 1 13 COM60371 119950107A2612601R5790011 HARNESS CNDAIRCL600 CL6002B19 EA RT ENGINE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2924 7027 C-CHECK INSPECTION, RT ENGINE A LOOP FIRE DETECT HARNESS FOUND DAMAGED. REPLACED FIRE LOOP A HARNESS. 2L72 4F RTA21EA 19950113007331995011300733EA 1995 1 13 COM60372 119950107A2750601R93106501 FLEX SHAFT CNDAIRCL600 CL6002B19 EA LT FLAP OUTB DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA 7027 TASK 12-680-100, LT FLAP OUTBD FLEX DRIVE SHAFT IS DAMAGED. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950113007341995011300734EA 1995 1 13 COM60373 119950107A2750601R93106103 FLEX SHAFT CNDAIRCL600 CL6002B19 EA LT FLAP INBD DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2940 7027 TASK 12-680-100, LT INBD FLAP FLEX DRIVE SHAFT IS DAMAGED. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950113007351995011300735EA 1995 1 13 COM60374 119950107A2750601R93106103 FLEX SHAFT CNDAIRCL600 CL6002B19 EA RT FLAP INBD DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2940 7027 TASK 12-680-100, RT INBD FLAP FLEX DRIVE SHAFT IS DAMAGED. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950113007361995011300736EA 1995 1 13 COM60375 119950107A2750601R93106501 FLEX SHAFT CNDAIRCL600 CL6002B19 EA RT FLAP OUTBD DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA 7027 TASK 12-680-100, RT OUT BD FLAP FLEX DRIVE SHAFT IS DAMAGED. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950113007371995011300737EA 1995 1 13 COM60376 119950107A2621897889 FIRE BOTTLE CNDAIRCL600 CL6002B19 EA APU EQUIP DEFECTIVE A COMAK NONE L NO TEST ININSP/MAINT 1 SO01926CA3481 7027 APU PUSH TO DISCHARGE DOES NOT ILLUMINATE DURING TEST. REPLACED APU FIRE BOTTLE. SWITCH CAN NOT BE REPLACED WITHOUT REPLACING THE FIRE BOTTLE. 2L72 4F RTA21EA 19950113007381995011300738EA 1995 1 13 COM60377 119950107A2730NAS6705DU16 BOLT 6001030056 CNDAIRCL600 CL6002B19 EA LT ELEV WORN A COMAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SO01926CA2924 7027 TASK NR 27-900-106, LT ELEVATOR SYSTEM NR 3 PCU BEARING FAILS THE BACKLASH CHECK. REPLACED WORN BUSHINGS AND BOLT AT ELEVATOR ATTACH POINT. 2L72 4F RTA21EA 19950113007391995011300739EA 1995 1 13 COM60378 119950107A5315 FLOOR BEAMS CNDAIRCL600 CL6002B19 EA FS280 - FS409 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA2924 7027 FLOOR BEAMS CORRODED FROM FS 280 TO FS 409 PLUS 80 ON LBL 9.0, LBL 27, RBL 9.0, RBL 27.0, PAX DOOR SILL ANGLE AND SERVICE DOOR SILL ON LBL 36 AND RBL 36. REPAIRED CORROSION IAW REO 601R-53-21-014. 2L72 4F RTA21EA 19950113007401995011300740EA 1995 1 13 COM60379 119950107A2910601R751511 VALVE CNDAIRCL600 CL6002B19 EA RT ENG HYD INOP A COMAK NONE O OTHER ININSP/MAINT 1 SO01926CA800 173 7027 TASK NR 002-05-900-991, RT ENGINE HYDRAULIC SHUT OFF VALVE DOES NOT CLOSE DURING RT FIREX PUSH TEST. REPLACED S.O.V. 2L72 4F RTA21EA 19950113007411995011300741EA 1995 1 13 COM60380 119950107A291673031 RESERVOIR CNDAIRCL600 CL6002B19 EA WING CENTER LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01926CA2924 7027 TASK NR 32-900-100, SYSTEM NR 3 RESERVOIR IS LEAKING. REPLACED CRACKED PISTON IN NR 3 RESERVOIR. 2L72 4F RTA21EA 19950113007421995011300742NM 1995 1 13 DL72L950096 119950102A5410 ANGLE BOEING727 727232 1384082NM NR2 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, NR 2 PYLON COWLING SUPPORT ANGLE WORN AT 6 O'CLOCK POSITION. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950113007451995011300745NM 1995 1 13 DL72W950095 119950108A5713 STRINGER BOEING727 727247 138408FNM LT WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, LEFT WING STA 686.5 STRINGER NR 2 WAS FOUND CRACKED REPAIRED STRINGER PER MM 57-13-0 PG 803. 2L73 4F A3WE 19950113007491995011300749 1995 1 13 DL767950116 419950110A2565BPS73 POWER SUPPLY BOEING767 767232 1385132NM RT OVERWING FAULTY A DALAK NONE L NO TEST ININSP/MAINT 1 SO11103DA 22215 DURING LAYOVER, RIGHT SIDE OVERWING EMERGENCY ESCAPE SLIDE SQUIB TEST 2 INOP. REPLACED RIGHT SQUIB POWER SUPPLY TEST NORMAL. 2L72 4F RTA1NM 19950113007501995011300750WP 1995 1 13 DLL10950084 119950102A5753529517113 FLAP VANE LKHEED1011 10113851 5265010WP NR3 LT WING CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 DURING SHOP INSPECTION, CRACKING WAS FOUND IN THE LEFT WING NR 3 FLAP VANE TOP SKIN DOUBLER AT 35 INCHES FROM THE INBOARD EDGE. INSTALLED SPLICED SKIN REPAIR PER SRM 57-53-00 FIG 805. 2L73 4F A23WE 19950113007511995011300751WP 1995 1 13 DLL13950117 119950111A2120 DUCT LKHEED1011 10113851 5265010WP AC COMPARTMENT SEPARATED A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO11788DL 193A1141 DURING CRUISE, A LOUD BANG WAS HEARD UNDERNEATH CABIN FLOOR AREA, AND AN IMMEDIATE 1000 FT/MIN CABIN ALTITUDE RISE. STARTED EMERGENCY DESCENT, REGAINED CABIN PRESSURE AT 15,000 FEET. RETURNED TO SJU. FOUND DUCT SEPARATED FROM NR 3 ACM. RESECURED DUCT OPERATION NORMAL. 2L73 4F A23WE 19950113007521995011300752WP 1995 1 13 DLL16950085 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 579/BL26L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FUSELAGE SKIN FAIL/SAFE TEAR STRAP WAS FOUND DISBONDED AT FS 579 AT STR 26L. REPAIRED PER SRM 53-31-00 PG806. 2L73 4F A23WE 19950113007531995011300753WP 1995 1 13 DLL16950086 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 639 BL 10R DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 639 AT BL 10R. REPAIRED PER SRM 553-31-00 PG. 810. 2L73 4F A23WE 19950113007541995011300754WP 1995 1 13 DLL16950087 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 659 BL10R DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 659 AT BL 10R. REPAIRED PER SRM 53-31-00 PG 816. 2L73 4F A23WE 19950113007551995011300755WP 1995 1 13 DLL16950088 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 659 BL6L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 659 AT BL 6L. REPAIRED PER SRM 53-31-00 PG 816. 2L73 4F A23WE 19950113007561995011300756WP 1995 1 13 DLL16950091 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 719/BL20L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 AT BL 20L. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950113007571995011300757WP 1995 1 13 DLL16950092 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 719/ BL36L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 AT BL36L. REPAIRED PER SRM 53-31-00 PG 816. 2L73 4F A23WE 19950113007581995011300758WP 1995 1 13 DLL16950093 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 719/BL12L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 BL 12L. REPAIRED PER SRM 53-31-00 PG 816. 2L73 4F A23WE 19950113007591995011300759WP 1995 1 13 DLL16950103 119950110A5330 DOUBLER LKHEED1011 10113853 5265020WP FS 1625 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN BONDED DOUBLER AT FS 1625 JUST OUTBOARD OF STRINGER 6 DISBONDED. REPAIRED PER SRM 53-31-00 PG 960. 2L73 4F A23WE 19950113007601995011300760WP 1995 1 13 DLL16950104 119950107A5340 P-DOME LKHEED1011 10113853 5265020WP P-DOME STR 43 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND AFT P-DOME CRACKED AFT OF STRINGER 43 ATTACH FITTING UNDER Z-ANGLE. REPAIRED PER SRM 53-11-00 PG 812, 813. 2L73 4F A23WE 19950113007611995011300761WP 1995 1 13 DLL16950105 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 679 BL 10R DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 AT BL 10R. REPAIRED PER SRM 53-31-00 PG 816. 2L73 4F A23WE 19950113007621995011300762WP 1995 1 13 DLL16950106 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 679 BL 12L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 BL 6R. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950113007631995011300763WP 1995 1 13 DLL16950107 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS BL 12L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679, BL 12L. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950113007641995011300764WP 1995 1 13 DLL16950108 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 679 BL 26L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 679 AT BL 26L. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950113007651995011300765WP 1995 1 13 DLL16950109 119950101A5330 SKIN LKHEED1011 10113853 5265020WP FS 679 BL 28R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND CORROSION DAMAGE TO FUSELAGE SKIN UNDER FAIL/SAFE STRAP AT FS 679 BL 28R. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950113007661995011300766WP 1995 1 13 DLL16950110 119950104A5330 SKIN LKHEED1011 10113853 5265020WP FS BL 22R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP CORRODED AT FS 679 AT BL 22R. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950113007671995011300767WP 1995 1 13 DLL16950111 119950104A5320 THRESHOLD LKHEED1011 10113853 5265020WP R1 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, THE R-1 DOOR THRESHOLD PANEL WAS FOUND WITH CORROSION DAMAGE AT THE FWD AND AFT DRAIN HOLES. REPAIRED PER SRM 53-15-00 PG 816-820. 2L73 4F A23WE 19950113007681995011300768WP 1995 1 13 DLL16950113 119950105A5320 THRESHOLD LKHEED1011 10113853 5265020WP R-1 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, CORROSION WAS FOUND ON BOTTOM SURFACE OF R-1 DOOR THRESHOLD PLATE AROUND DRAIN OPENINGS AND UNDER THE AFT GIRT BAR RECEPTACLE, FS 328 TO 369 WL 200. REPAIRED PER SRM 53-15-00 PG 816. 2L73 4F A23WE 19950113007691995011300769WP 1995 1 13 DLL16950114 119950105A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS619/BL12L DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED AT FS 619 AT BL 12L. NO CORROSION FOUND IN AREA, REPAIRED STRAP PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950113007701995011300770WP 1995 1 13 DLL16950115 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS719/BL44B DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 719 BL44R. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950113007711995011300771SW 1995 1 13 QXEA9500007 119950110A3260602EN6026 SWITCH SWRNGN SWRNGNSA227 SA227AC 8780603SW NLG RT INOP A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09382PH AC589 BOI - NOSE GEAR WOULDN'T STAY UP AND LOCKED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. REPLACED NOSE GEAR RIGHT HAND UPLOCK SWITCH IAW MAINT MANUAL NOSE GEAR. 1L72 4T A8SW 19950113007721995011300772EU 1995 1 13 QXEA9500008 119950110A3350MGG1055 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BURNED OUT A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09803PH 11017 PDX - FORWARD EMERGENCY LIGHTS IN CABIN INOP. REPLACED BULBS AND LIGHTS. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950113007731995011300773WP 1995 1 13 UP801915 119950105A5312 BEAM DOUG DC8 DC871F 302199DWP STA 1766 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 MAINTENANCE REPORTED APPROX 1.75 INCH CRACK AT BOTTOM RADIUS OF NR 3 ANGLE (BEAM) ON PRESSURE BULKHEAD AT CENTER. INSTALLED REPAIR IAW EO DC8-6310-6306A, TEMP REV 53-81, 53-7-0. 2L74 4F RT4A25 19950113007741995011300774 1995 1 13 UP801922 419950111A34166223975005 CONNECTOR DOUG DC8 DC873F 302199FWP FLIGHT DECK SHORTED A IPXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01818UP 46108 PILOT REPORTED, DESENDING THROUGH 18,000 FT, GOT RED FLAG ON FIRST OFFICER'S ALTIMETER, STARTED TO SMELL ELECTRICAL SMOKE. TURNED OFF RIGHT EFIS MASTER, SMOKED STOPPED. REMOVED CANNON PLUG AND CLEANED MOISTURE ON IT AND REMOVED AND REPLACED FIRST OFFICERS ALTIMETER. GROUND CK OK. 2L74 4F RT4A25 19950113007751995011300775WP 1995 1 13 UP801923 119950111A5230 DOOR DOUG DC8 DC873F 302199FWP NR 4 PIT DOOR CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 MAINTENANCE REPORTED,NR 4 PIT DOOR HAS CRACK IN LOWER AFT BOTTOM OF DOOR APPROX 1 INCH LONG. INSTALLED REPAIR IAW SRM 52-2-0. 2L74 4F RT4A25 19950113007761995011300776NM 1995 1 13 UPS201920 119950110A3260 WARN LIGHTS BOEING727 72730C 1384009NM FLIGHT DECK MALFUNCTION A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01918UP 19008 PILOT REPORTED LEFT MAIN GEAR DOOR INDICATED NOT UP AND LOCKED ON FLIGHT DECK GEAR PANEL. LIGHT EXTINGUISHED ON F/E PANEL. CHECKLIST WAS C/W AND THE GEAR WAS EXTENDED AND RETRACTED. BOTH LIGHTS DID NOT GO OUT. CLEANED LEFT GEAR DOOR SWITCH AND CHECKED SECURITY, FOUND OK. OPS CHECKED OK. 2L73 4F A3WE 19950113007771995011300777NM 1995 1 13 UPS201921 119950111A3260 SWITCH BOEING727 72725C 138400HNM RT MLG DOOR REQ ADJUST A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01933UP 19857 PILOT REPORTED, RT MLG DOOR UNSAFE AFTER RETRACTION WHEN HANDLE IN OFF POSITION. RECYCLED GEAR. OPS NORMAL. ADJUSTED RT MLG DOOR WARNING SWITCH PER MM 32-62-11. OPS CHECKED LANDING GEAR DOOR WARNING PER MM 32-62-11. CHECKS GOOD. 2L73 4F A3WE 19950113007791995011300779EU 1995 1 13 WWMA9500001 119950103A25301012030 HOT JUG SAAB SF340 340B 7860101EU GALLEY DEFECTIVE I WWMAO OTHER BW SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CRCRUISE 1 WP15358RZ 340B358 FLIGHT 7821 MAF/DFW, PILOT REPORTED THAT WHILE INFLIGHT NOXIOUS FUMES WERE SMELLED IN THE GALLEY AREA, NO VISIBLE SMOKE OBSERVED. AN EMERGENCY WAS DECLARED. HOWEVER, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THAT THE ELECTRICAL RECEPTACLE ON THE NR 2 HOT JUG HAD MELTED AND THAT THE PROBLEM STEMMED FROM AN ATR HOT JUG BEING INCORRECTLY INSTALLED IN THE AIRCRAFT. THE HOT JUG WAS REMOVED FROM THE AIRCRAFT AND MEL NR 010031 WAS ISSUED FOR THAT ITEM. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950113007801995011300780EU 1995 1 13 WWMA9500002 119950105A2120 AIR DIST BAG JETSTMJETSTM3201 1500217EU LT FLOW CONT CABIN SMOKE I WWMAOH OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15957AE 957 FLIGHT 5134 - SFO/MRY - PILOT REPORTED, THAT WHILE INFLIGHT A LARGE AMOUNT OF SMOKE DEVELOPED IN THE FLIGHT DECK AND CABIN AREA. THE LEFT FLOW CONTROL WAS TURNED OFF AT WHICH TIME THE SMOKE CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED LENGTHY RT AND LT ENGINE GROUND RUNS WITH LT AND RT ACMS OPERATING IN BOTH MANUAL AND AUTO MODES. OPERATIONAL CHECKS WERE NORMAL WITH NO SMOKE DETECTED, RESIDUAL OR OTHERWISE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA56EU 19950113007811995011300781EU 1995 1 13 WWMA9500003 119950106A261251224127 FIRE LOOP BAG JETSTMJETSTM3201 1500217EU ZONE 1 RH ENGINEDEFECTIVE I WWMAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 WP15967JS 967 FLIGHT 5213 - LAX/SBP - PILOT REPORTED, THAT WHILE TAXIING INTO THE RAMP AREA THE RT ENGINE FIRE LIGHT WITH BELL AND AURAL WARNINGS ACTIVATED. THE RIGHT ENGINE WAS SHUT DOWN IMMEDIATELY WITH NO FURTHER PROBLEMS DEVELOPING. MAINTENANCE PERSONNEL DETERMINED THAT A FAULTY FIRE DETECTION LOOP AT ZONE 1 IN THE RT ENGINE HAD CAUSED THE FALSE INDICATION. THE FIRE DETECTION LOOP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950113007821995011300782EU 1995 1 13 WWMA9500004 119950108A33206500006 LIGHT SOCKET SAAB SF340 340B 7860101EU SEAT 12A DEFECTIVE I WWMAO OTHER A FLAME/FIRE ININSP/MAINT 1 WP15359SB 340B359 FLIGHT 7819 - CLL-DFW - PILOT REPORTED, THAT DURING PREFLIGHT INSPECTION AND WHEN EXTERNAL POWER WAS APPLIED TO THE AIRCRAFT THE OVERHEAD FLOURESCENT LIGHT AT SEAT 12A BURST INTO FLAMES. THE POWER WAS REMOVED AND THE FLAMES EXTINGUISHED. MAINTENANCE PERSONNEL INSPECTED THE OVERHEAD LIGHTING AT SEAT 12A AND FOUND EVIDENCE OF BURNING AT THE LIGHT SOCKET AND THAT THE LIGHT BULB WAS NOT FULLY SEATED IN THE SOCKET. THE SOCKET WAS REPLACED, OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950113007831995011300783NE 1995 1 13 WWMA9500005 219950109A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENG MALFUNCTION I AWWMAAE UNSCHED LANDING ENGINE SHUTDOWN JR WARNING INDICATION PARTIAL RPM/PWR LOSS CLCLIMB 1 WP15283AE 340B283 FLIGHT 7752 - MAF-DFW - PILOT REPORTED THAT DURING TAKEOFF AND CLIMB AT APPROX 400 FEET, A SERIES OF LOUD BANGS WERE HEARD INDICATIVE OF A COMPRESSOR STALL ON THE RT ENG. THIS WAS ACCOMPANIED BY A MASTER WARNING, TRIPLE CHIME AND THE RT ENGINE OIL PRESS LIGHT ILLUMINATING AS WELL AS THE RT ENGINE GOING INTO AUTOCOARSEN. AN EMERGENCY WAS DECLARED, AN INFLIGHT SHUTDOWN WAS PERFORMED AND THE AIRCRAFT RETURNED TO MAF W/O INCIDENT. IT WAS DETERMINED THAT THE PILOT HAD LEFT THE CTOT TURNED ON. MX PERSONNEL PERFORMED A BORESCOPE CHECK AND ENGINE RUNS AND WERE UNABLE TO DUPLICATE THE PROBLEM. A TEST FLIGHT WAS PERFORMED WITH ALL OPERATIONAL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950120000011995012000001WP 1995 1 20 9500449947 119950107A5510 BRACKET DOUG DC9 DC931 3022065WP HORIZ STAB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018938E 47161 DURING PERIODIC CHECK, FOUND CORROSION IN BOTH LEFT AND RIGHT HORIZONTAL STABILIZER 'A' BRACKETS UPPER FASTENER BORES. OVERSIZED BORES AND INSTALLED BUSHINGS PER EA 99-094108 AND -094107 RESPECTIVELY. 2L72 4F A6WE 19950120000021995012000002WP 1995 1 20 9500459947 119950107A5320 FITTING DOUG DC9 DC931 3022065WP FS 607 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018938E 47161 DURING PERIODIC CHECK, FOUND CORROSION ON 'FISHTAIL' FITTING FS 604 AT LONGERON 28R. REPLACED FITTING PER SRM 51-01 AND DWG 5911418. 2L72 4F A6WE 19950120000031995012000003WP 1995 1 20 9500469945 119950107A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CRACKS IN ATTACH FITTINGS FS 996 AT LONGERONS 27R, 24L, AND AT INTERCOSTAL BETWEEN LONGERON 27L AND 28L. REPLACED ALL FITTINGS PER SRM 51-30. 2L72 4F A6WE 19950120000041995012000004WP 1995 1 20 9500479945 119950107A5511 SPAR CHORD DOUG DC9 DC931 3022065WP HORIZ STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CRACKS IN THE HORIZONTAL STABILIZER AFT SPAR 'T' CAPS LEFT SIDE LOWER (XHS 205-211) AND RIGHT SIDE UPPER (XHS 188). REPAIRED BOTH PER SRM 55-02. 2L72 4F A6WE 19950120000051995012000005WP 1995 1 20 9500489927 119950107A5511 SPAR CHORD DOUG DC9 DC931 3022065WP HORIZ STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING PERIODIC CHECK, FOUND CRACKS IN THE LEFT HORIZONTAL STABILIZER AFT SPAR UPPER 'T' CAP BETWEEN NR3 - NR4 HINGES AND LOWER 'T' CAP (OUTBOARD END). REPAIRED BOTH PER SRM 55-02. 2L72 4F A6WE 19950120000061995012000006WP 1995 1 20 9500499945 119950109A5314 KEEL BEAM DOUG DC9 DC931 3022065WP FS 604-637 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND 10 INCH CRACK AND CORROSION IN RIGHT SIDE KEEL BEAM FS 604 - 637 BETWEEN LONGERON 28R - 29R. REPLACED BEAM PER SRM 51-30-2. 2L72 4F A6WE 19950120000071995012000007WP 1995 1 20 9500509945 119950109A5720 FITTING DOUG DC9 DC931 3022065WP WS 0 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CRACK IN CENTER WING TANK FITTING XCW O, BETWEEN WING STRINGERS 17 - 18. REPLACED FITTING PER SRM 51-10-4. 2L72 4F A6WE 19950120000081995012000008WP 1995 1 20 9500519927 119950110A5320 FITTING DOUG DC9 DC931 3022065WP FS 676 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING PERIODIC CHECK, FOUND RADIUS CRACK IN BELT FRAME ATTACH FITTING FS 676 ABOVE LONGERON 29L. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950120000091995012000009WP 1995 1 20 9500529154 119950108A5230 FITTINGS DOUG DC9 DC914 3022034WP AFT CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018913E 45830 DURING PERIODIC CHECK, FOUND CRACKS IN AFT CARGO DOOR UPPER AND LOWER BEAM END FITTINGS. REPLACED FITTINGS PER SRM 51-30-5. 2L72 4F A6WE 19950120000101995012000010WP 1995 1 20 9500539872 119950110A5311 FRAME DOUG DC9 DC951 3022051WP FS 926-945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION ON LOWER FLANGES OF FS 926-945 FRAMES BETWEEN LONGERONS 28L - 28R. REPAIRED PER EA 98-093718 AND -093779 RESPECTIVELY. 2L72 4F A6WE 19950120000111995012000011WP 1995 1 20 9500549872 119950110A5744 HINGE DOUG DC9 DC951 3022051WP NR 2 FLAP CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION IN THE NR 2 FLAP HINGE SUPPORT FITTING BORE LEFT WING. REPAIRED PER EA 98-03773. 2L72 4F A6WE 19950120000121995012000012WP 1995 1 20 9500551162 119950111A5320 SUPPORT DOUG DC10 DC1040 3023508WP FS 1997-1969 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01162US 46771 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE GALLEY SUPPORT AT FS 1947 - 1969. LBL 55. REPAIRED PER EA 11-96398. 2L73 4F A22WE 19950120000131995012000013WP 1995 1 20 9500561162 119950111A5320 FLOOR SUPPORT DOUG DC10 DC1040 3023508WP FS 1970-1978 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01162US 46771 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE AFT GALLEY FLOOR SUPPORT AT FS 1970 - 1978, LBL 27. REPAIRED PER EA 11-96399. 2L73 4F A22WE 19950120000141995012000014NE 1995 1 20 9500571153 219950111A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 3 ENGINE STALLED A NWAAE ENGINE SHUTDOWN MR OVER TEMP PARTIAL RPM/PWR LOSS LDLANDING 1 GL01153US 46762 686171 DURING LANDING ROLLOUT IN REVERSE THRUST, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE ENGINE WAS INSPECTED AND THE RABS SOLENOID WAS REPLACED. A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BOROSCOPE IS SCHEDULED. 2L73 4F4 F A22WE E20EA 19950120000151995012000015WP 1995 1 20 9500589161 119950108A3260 TERMINAL STRIP DOUG DC9 DC914 3022034WP RT MLG WW CONTAMINATED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL018905E 8905E DURING CLIMB-OUT FROM CMH, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT AND CYCLED GEAR NUMEROUS TIMES. PROBLEM COULD NOT BE DUPLICATED. CLEANED TERMINAL STRIP IN AREA OF RIGHT WHEEL WELL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000161995012000016WP 1995 1 20 9500599156 119950110A3297 WIRE DOUG DC9 DC914 3022034WP LT MLG BROKEN A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018915E 45832 LEFT MAIN GEAR UNSAFE LIGHT DID NOT ILLUMINATE WHILE GEAR WAS INTRANSIT ON RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED BROKEN WIRE FROM LEFT WING ROOT TERMINAL STRIP TO LEFT GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000171995012000017WP 1995 1 20 9500609311 119950111A30409615059002 TEMP CONTROL DOUG DC9 DC982 3022082WP LT WINDSHIELD MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01314RC340801222 49110 CAPTAIN'S WINDSHIELD ANTI-ICE SYSTEM FAILED AFTER TAKEOFF FROM PHL. FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S WINDSHIELD TEMPERATURE CONTROLLER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000181995012000018WP 1995 1 20 9500619873 119950110A3231 RETRACT MECH DOUG DC9 DC951 3022051WP NLG DOOR ICE BUILD UP A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01782NC 48107 EXCESSIVE VIBRATION WAS COMING FROM THE NOSE GEAR AREA AFTER GEAR RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND LEFT NOSE GEAR DOOR OPEN. ALSO, ICE WAS NOTED IN NOSE WELL AND AROUND DOOR. SECURED DOOR AND REMOVED ICE ACCUMULATION. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000191995012000019WP 1995 1 20 9500629876 119950110A3260 WASHER DOUG DC9 DC951 3022051WP RT MLG STRIKER WORN A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01785NC 48110 DURING CLIMB-OUT FROM MCI, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. GEAR DOOR OPEN LIGHT WAS OUT. RECYCLED GEAR AND LIGHT STAYED ON. PERFORMED UPLATCH CHECK AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN GEAR UPLATCH STRIKER LEVER GUIDE WASHER WORN. REPLACED WASHER. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000201995012000020WP 1995 1 20 9500631146 119950112A5330 SKIN DOUG DC10 DC1040 3023508WP FS 515-560 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, NON-STANDARD REPAIR WAS FOUND AT FS 515 - 560, STR 24L - 23L. REMOVED DAMAGE AND INSTALLED DOUBLERS PER EA 11-96400. 2L73 4F A22WE 19950120000211995012000021WP 1995 1 20 9500649908 119950107A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01958N 47254 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED RELEASE MECHANISM. 2L72 4F A6WE 19950120000221995012000022NM 1995 1 20 9500652767 119950111A2613 SENSE LOOP BOEING727 7272M7 138407SNM PWA JT8 JT8D17 52049NE RT PYLON MALFUNCTIONED A NWAAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL01727RW 21656 696728 WHILE IN CRUISE FLIGHT, THE NR 3 STRUT OVERHEAT WARNING ILLUMINATED. PERFORMED PRECAUTIONARY SHUT DOWN OF THE NR 3 ENGINE. FOUND THE SENSE LOOP HAD FAILED. REPLACED THE LOOP AND TESTED THE SYSTEM. CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950120000231995012000023 1995 1 20 9500669979 419950111A34205223120004 INSTR AMPLIFIER DOUG DC9 DC931 3022065WP E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL019343 2224514334 47439 CAPTAIN'S GYRO FLAG APPEARED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S ATTITUDE DIRECTIONAL INDICATOR WITH NO HELP. REPLACED INSTRUMENT AMPLIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO GATE. 2L72 4F A6WE 19950120000241995012000024 1995 1 20 9500679750 419950112A342070515V3 STANDBY HORIZ DOUG DC9 DC941 302207NWP INSTR PANEL MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01750NW28232246 47114 STANDBY HORIZON GYRO FLAG APPEARED DURING CLIMB-OUT FROM HOU. PULLED AND RESET CIRCUIT BREAKER Z31 WITH THE SAME RESULTS. FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED STANDBY HORIZON AND POWER INVERTER. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000251995012000025 1995 1 20 9500689950 419950112A3416LK355 ALTIMETER DOUG DC9 DC932 3022066WP FIRST OFFICER'S MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL019346 172121889 47376 FIRST OFFICER'S ALTIMETER FAILED DURING CLIMB-OUT FROM GEG. FLIGHT DIVERTED TO RAP AND LANDED WITHOUT INCIDENT. REPLACED ALTIMETER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000261995012000026WP 1995 1 20 9500709996 119950113A3231 LATCH BOLTS DOUG DC9 DC931 3022065WP LT MLG DOOR LOOSE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL018932E 47141 DURING APPROACH INTO MSP, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. FOUND LEFT MAIN INBOARD GEAR DOOR LATCH ROLLER MOUNTING BOLTS LOOSE. TIGHTENED BOLTS. ALSO, REPLACED THE RIGHT INBOARD GEAR DOOR DUE TO DAMAGE SUFFERED ON LANDING. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950120000271995012000027NM 1995 1 20 9500715520 119950115A3240 CONTROL CABLE BOEING757 757251 1384970NM PARKING BRAKE LACK OF LUBE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01520US 23208 RECEIVED CONFIGURATION WARNING AFTER TAKEOFF THRUST AND EPR MODE WAS SET. ABORTED TAKEOFF. SET AND RELEASED THE PARKING BRAKE HANDLE AND THE LIGHT REMAINED OUT. CONTINUED TAKEOFF. LUBRICATED BRAKE CABLE ON ARRIVAL IN DCA. PARKING BRAKE RELEASE CHECKED NORMAL. 2L72 4F RTA2NM 19950120000281995012000028NE 1995 1 20 9500726739 219950114A7230 COMPRESSOR BOEING747 747251F 1384898NM PWA JT9 JT9D7R4G2 52054NE NR 3 ENGINE STALLED A NWAAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01639US 23887 715177 DURING CLIMB PASSING THROUGH FL 360, THE NR 3 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS AND RECOVERED. ENGINE OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. AN ENGINE INSPECTION AND BOROSCOPE CHECKED OK. THE LOWER 3.5 BLEED VALVE AND EVBC WERE REPLACED. THE ENGINE WAS PRECISION TRIMMED AND OPERATION CHECKED OK. 2L74 4F4 F A20WE E3NE 19950120000291995012000029 1995 1 20 95FDEA00009 219950111A7200 ENGINE BOEING727 727233 138408ANM NR 3 FLAMED OUT A FDEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 SO04254FE 20936 NR 3 ENG FLAMED OUT ON T/O PASSING 4000 FT AGL 220 KIAS. ATTEMPTED RESTART UNSUCCESSFUL, ENG SHUTDOWN CHECKLIST COMPLIED WITH. CHECKED NR 3 ENG, IGN SYS CK'D NORMAL, OPS CK'D NR 3 FUEL HEAT VALVE CK'D NORMAL. REPLACED NR 3 ENG MAIN FUEL FILTER. RAN ENG LEAK CK'D GOOD, INSPECTED MOISTURE TRAP AND CDP AIR LINE ALL CK'D GOOD. ENG INLET, AND EXHAUST VISUALLY INSPECTED GOOD. COMPLIED W/FLAME OUT TROUBLESHOOTING PER MM 72-00-07A, PWA AND SUMPED NR 3 MAIN FUEL TANK, NO WATER FOUND. RAN NR 2 ENG TO T/O PWR, CK'D NORMAL, OK TO CONTINUE. 2L73 4F RTA3WE 19950120000301995012000030NM 1995 1 20 95FDEA00010 119950112A3260656021132 ACCESSORY UNIT BOEING727 727277 138408SNM LT MLG FALSE WARNING A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO04240FE 20978 AFTER T/O FROM MEM AT GEAR RETRACTION, THE L/MAIN GEAR RED LIGHT WOULD NOT EXTINGUISH. CHECKLIST PROCEDURE ACCOMPLISHED. ALL GREEN ALL GEAR DOOR LIGHTS AND THE NOSE AND R/MAIN RED LIGHT EXTINGUISHED. THE L/MAIN RED LIGHT STILL WOULD NOT EXTINGUISH. FLT CONTINUED PER CHECKLIST PAGE 2-6-20. REPLACED LANDING GEAR ACCESSORY UNIT AND TESTED GOOD PER MM 32-09-121 PG 501. 2L73 4F RTA3WE 19950120000311995012000031NM 1995 1 20 95FDEA00011 119950111A53002024T3063 SKIN BOEING727 727233 138408ANM BS 1347 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04278FE 22345 CRACKED AND DENTED SKIN AT BS 1347, LBL 30, WL 200. REPAIRED DAMAGED SKIN AT BS 1347, LBL 30, WL 200 IAW FEDEX SRM 54-30-7. 2L73 4F RTA3WE 19950120000321995012000032NM 1995 1 20 95FDEA00012 119950109A57516519256 FITTING BOEING727 72725 1384006NM RT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 R/W O/B AILERON CENTER O/B HINGE FITTING NR 3 A/C SIDE IS CORRODED WHERE LOWER SURFACE PANEL ATTACHES. REMOVED AND REPLACED R/W O/B AILERON CENTER O/B HINGE FITTING NR 3. 2L73 4F A3WE 19950120000331995012000033NE 1995 1 20 95FDEA00013 219950110A7397 WIRE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE CHAFED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW99496FE 21670 NR 3 FUEL ICING LIGHT CAME ON AT LEVEL OFF. ABNORMAL PROCEDURES COMPLIED WITH HOWEVER THE LIGHT REMAINED ON. WE WERE BURNING FROM TANK NR 2 AT THE TIME. FOUND CHAFED WIRE GROUNDED TO ENG CASE NEAR FUEL FITLER PRESSURE SWITCH REPAIRED SAME. NR 3 ENG FUEL DE-ICING SYSTEM OPS CKS OK PER MM 73-14-0. 2L73 4F4 F A3WE E2EA 19950120000341995012000034EU 1995 1 20 95FDEA00014 119950114A5610NP17520 WINDOW AIRBUS310 A310203 EU RT COCKPIT CRACKED A FDEAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO04411FE 360 RIGHT FRONT WINDOW CRACKED, (FIRST OFFICER'S) OUTER PANE CRACKED. REMOVED AND REPLACED FIRST OFFICER WINDOW PER MM 56-11-11 UP TO 3 (8). COMPLETED INSTALLATION PER 56-11-11 PG 420 THROUGH STEP E. SEALANT APPLIED AT OPS CHECKED GOOD. 2L72 4F RTA35EU 19950120000351995012000035NM 1995 1 20 95UAL727003 119950111A3350S109 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT OVERWING DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297259U 21406 RIGHT AFT OVERWING EMERGENCY EXIT LIGHT IS DIM WITH SHIP'S POWER. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19950120000361995012000036NM 1995 1 20 95UAL727004 119950111A3350S109 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AFT GALLEY DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297259U 21406 EMERGENCY EXIT AISLE LIGHT BY AFT GALLEY INOP. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19950120000371995012000037NM 1995 1 20 95UAL727005 119950111A3350S109 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297289U 21567 FORWARD OVERHEAD EMERGENCY EXIT LIGHT DIM AND FLICKERING. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19950120000381995012000038NM 1995 1 20 95UAL727006 119950111A3350R70R600 EEL RELAY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE COCKPIT INTERMITTENT A UALAK NONE L NO TEST ININSP/MAINT 1 WP297260U 21407 EMERGENCY EXIT LIGHTS COME ON INTERMITTENTLY WITH COCKPIT SWITCH IN THE ARMED POSITION. REPLACED R70 AND R600 RELAYS. 2L73 4F4 F A3WE E2EA 19950120000391995012000039NM 1995 1 20 95UAL737001 119950104A2910 HYD FLUID BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE A HYD SYST LOW QTY A UALAK NONE JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP29341UA 24245 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ONE FOURTH FULL AFTER TAKEOFF. 'A' SYSTEM EMPTY, LOW PRESSURE LIGHTS ON. 2L72 4F4 FRTA16WE E2GL 19950120000401995012000040NM 1995 1 20 95UAL737002 119950104A2410735511A CSD BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 WP29328UA 24148 NUMBER ONE CONSTANT SPEED DRIVE LOW PRESSURE WARNING LIGHT CAME ON WHEN GENERATOR TRIPPED. DISCONNECTED CONSTANT SPEED DRIVE. ALL INDICATIONS SHOWED CONSTANT SPEED DRIVE DID NOT DISCONNECT. HAD RESIDUAL VOLTS AND OIL TEMPERATURE PEGGED. REPLACED CONSTANT SPEED DRIVE, GENERATOR AND OIL COOLER. CHECKS OK. SHOP FOUND THAT GOVERNOR SUPPORT FAILED WHICH CAUSED FAILURE OF THE HYDRAULIC LOG. 2L72 4F4 FRTA16WE E2GL 19950120000411995012000041 1995 1 20 95UAL747001 419950112A25657A123857 SLIDE BF GOODRICH BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE DOOR DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29161UA 21352 DURING INADVERTENT DEPLOYMENT TOP TUBE DID NOT INFLATE DUE TO MECHANIC ATTEMPTING TO CLOSE DOOR DURING DEPLOYMENT. SLIDE/RAFT WAS TRAPPED IN DOORWAY. REPLACED SLIDE/RAFT. SENT REMOVED SLIDE/RAFT TO VENDOR FOR REPAIR. 2L74 4F4 F A20WE E20EA 19950120000421995012000042NM 1995 1 20 95UAL747002 119950112A2612 DETECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 ENGINE ACTIVATED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29191UA 26880 727331 NR 2 ENGINE FIRE WARNING CAME ON WHILE CLIMBING THROUGH 2500 FEET. SHUT DOWN ENGINE FOUND EVIDENCE OF OVERHEAT AT UPPER AFT FIRE DETECTOR. CAUSED BY BURNED TAPE. CLEANED AREA AND ACCOMPLISHED FIRE DETECTION TEST. TESTED OK. 2L74 4F4 FRTA20WE E24NE 19950120000431995012000043WP 1995 1 20 95UALD10004 119950111A3350 EEL STRIPS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291836U 47968 SEVERAL ADJACENT EEL STRIPS INOPERATIVE ON BOTH SIDES OF THE AIRPLANE. REPLACED STRIPS AS NECESSARY. OPERATIONAL CHECK NORMAL. 2L73 4F4 F A22WE E23EA 19950120000441995012000044WP 1995 1 20 ABXA9500004 119950111A21215007025381 RECIRC FAN DOUG DC8 DC863 302198AWP LEFT ODOR A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23811AX 46113 EN ROUTE TO BOS, CREW REPORTED LEFT RECIRCULATING FAN CAUSED AN OILY SMELL IN THE COCKPIT. OPS CHECKED LEFT RECIRCULATING FAN AND ALL FOUR CTC'S IAW DC 8 MM CHAPTER 21. NO OILY SMELL OR ABNORMAL ODORS NOTICED. 2L74 4F 4A25 19950120000451995012000045SO 1995 1 20 COM11727 119950111A5720SEEABOVE SKIN SUPPORTS EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01263CA7834 120255 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651 01I AT RIBS NR 15 AND 16, LEFT AND RIGHT WINGS, P/N 120-17056-015, 120-17056-017, 120-17056-019, 120-17057-007, 120-17056-015, 120-17056-013, 120-17056-015; 120-17056-017, 120-17056-019, 120-17057-007, 120-17056-015. REPLACED A TOTAL OF 11 SKIN SUPPORTS IAW AERODESIGN E.O. NR 1327-2. 2L72 4T RTA31SO 19950120000461995012000046EU 1995 1 20 COM31004 119950112A61207503503AH O-RING SAAB SF340 SF340A 7850100EU LT PROP WORN A COMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01146CA 340A146 LEFT PROPELLER SLOW TO ACCELERATE AND MAX RPM WAS 1330. REPLACED THE PROPELLER PISTON O-RING. 2L72 4T RTA52EU 19950120000471995012000047EU 1995 1 20 COM31005 119950115A61208542M2 COMPUTER SAAB SF340 SF340A 7850100EU CABIN DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01361CA13682357 340A056 AUTO COARSEN SYSTEM DID NOT ARM DURING TAKE OFF. REPLACED THE AUTO COARSEN COMPUTER. 2L72 4T RTA52EU 19950120000481995012000048EU 1995 1 20 COM31006 119950114A61201103P0620 SWITCH 1103P2671 SAAB SF340 SF340A 7850100EU LT/RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01361CA1818 402 0312 340A056 AUTO COARSEN ARM INDICATOR DID NOT ILLUMINATE DURING TAKEOFF. REPLACED THE RT AND LT AUTO COARSEN P3 PRESSURE SWITCHES. 2L72 4T RTA52EU 19950120000491995012000049NE 1995 1 20 COM31007 219950113A7200CT75A2 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT FAILED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING MY OVER TEMP ENGINE STOPPAGE CLCLIMB 1 SO01340SF202075869 340A014 367197 RT ENGINE FAILED DURING CLIMB. REPLACED THE ENGINE ASSY. 2L72 4T4 TRTA52EU E8NE6 19950120000501995012000050EU 1995 1 20 COM31008 119950114A2613MS345OKT222S CONNECTOR SAAB SF340 SF340A 7850100EU RT NACELLE DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01341CA 340A021 RT TAIL PIPE HOT WARNING ACTIVATED DURING CLIMB. CLEANED WIRING CONNECTION FOR TAIL PIPE HEAT SENSORS AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950120000511995012000051EU 1995 1 20 COM31009 119950114A26131734362450 DETECTOR SAAB SF340 SF340A 7850100EU RT NACELLE DEFECTIVE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01370CA 340A010 RT ENGINE TAIL PIPE HOT WARNING ACTIVATED. REPLACED DEFECTIVE HEAT SENSOR ON RT EXHAUST DUCT. 2L72 4T RTA52EU 19950120000521995012000052NM 1995 1 20 DL72L950121 119950104A5210 SKIN BOEING727 727232 1384082NM L1 DOOR BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, SKIN IS BENT ON L-1 DOOR AT THE FWD LOWER ATTACH POINT AND UPPER AFT CORNER. REPAIED PER SRM 52-11-01 FIG 804. 2L73 4F A3WE 19950120000531995012000053NM 1995 1 20 DL72L950123 119950102A5313 STRINGER BOEING727 727232 1384082NM FS 1140-1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND STR 26 R CORRODED FROM FS 1140 - 1166. REPAIRED PER ERA 300913-14. 2L73 4F A3WE 19950120000541995012000054NM 1995 1 20 DL72L950124 119950103A5311 FRAME BOEING727 727232 1384082NM FS 804.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND FRAME 804.5 CRACKED. REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950120000551995012000055NM 1995 1 20 DL72L950125 119950107A5311 FRAME BOEING727 727232 1384082NM FS 804.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND FRAME 804.5 BETWEEN L/A O/W EXIT OPENINGS STR 14 FRAME CHORD CRACKED. REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950120000561995012000056NM 1995 1 20 DL72L950126 119950104A5755 TE SKIN BOEING727 727232 1384082NM NR 2 SPOILER DELAMINATING A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND NR 2 SPOILER TE DELAMINATING. REPAIRED PER SRM 51-40-6. 2L73 4F A3WE 19950120000691995012000069NM 1995 1 20 DL72L950167 119950113A5754 LE RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND RIB INSIDE NR 3 L/E SLAT CRACKED. REPAIRED PER SRM 57-50-3 FIG 9. 2L73 4F A3WE 19950120000701995012000070NM 1995 1 20 DL72L950168 119950106A5720 WEB BOEING727 727232 1384082NM LT WING LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND WEB CRACKED INSIDE LT WING L/E O/B OF NR 2 SLAT ACTUATOR. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950120000711995012000071NM 1995 1 20 DL72L950170 119950104A5712 RIB BOEING727 727232 1384082NM LT WING LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND NR 2 L/E SLAT ACTUATOR ATTACH RIBS CRACKED, REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950120000731995012000073NM 1995 1 20 DL72S950143 119950109A5320 WEB BOEING727 727232 1384082NM FS 1243 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 DURING LETTER CHECK, FOUND AFT FUSELAGE STAIRWELL RIGHT SIDE VERTICAL WEB CRACKED AT FS 1243 AT LIGHTENING HOLE. REPAIRED PER MM 53-11-0 PG 828. 2L73 4F A3WE 19950120000741995012000074NM 1995 1 20 DL72S950144 119950103A5522 SKIN BOEING727 727232 1384082NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 DURING LETTER CHECK, THE RIGHT ELEVATOR UPPER SKIN WAS FOUND WITH A SMALL HOLE JUST FWD OF TAB, DAMAGE WAS DUE TO LIGHTNING STRIKE. REPAIRED ELEVATOR SKIN PER SRM 52-20-3. 2L73 4F A3WE 19950120000771995012000077NM 1995 1 20 DL72W950149 119950105A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND STRINGER CRACKED FORWARD AND AFT OF RT LEADING EDGE FLOOD LIGHT AT STRINGER 15 STA 720 B AND 720 C, REPAIRED PER SRM 53-10-3 FIGURE 1 DETAILS 1 AND 2. 2L73 4F A3WE 19950120000781995012000078NM 1995 1 20 DL72W950152 119950104A5755 PANEL BOEING727 727247 138408FNM NR 7 SPOILER GOUGES A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV FOUND NR 7 SPOILER PANEL TO HAVE NUMEROUS HOLES AND DEEP GOUGES ON LOWER SURFACE. REPAIRED SKIN PER SRM 51-40-6. 2L73 4F A3WE 19950120000791995012000079NM 1995 1 20 DL72W950153 119950104A5755 BEAM BOEING727 727247 138408FNM LT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND SPOILER BEAM WEB CRACKED JUST OUTBOARD OF NR 7 SPOILER ACTUATOR ATTACH FITTING, REPAIRED PER M/M 57-55-00. 2L73 4F A3WE 19950120000801995012000080NM 1995 1 20 DL72W950154 119950106A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND IN THE VERTICAL STABILIZER INTERIOR AT STA 1303 WEB CRACKED ON LEFT SIDE ABOVE 'S' DUCT, REPAIRED PER SRM 53-10-4 FIGURE 12. 2L73 4F A3WE 19950120000811995012000081NM 1995 1 20 DL72W950155 119950106A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND IN THE VERTICAL STABILIZER INTERIOR AT STA 1303 WEB CRACKED ON RT SIDE ABOVE 'S' DUCT, REPAIRED PER SRM 53-10-4 FIGURE 12. 2L73 4F A3WE 19950120000821995012000082NM 1995 1 20 DL72W950162 119950106A5315 BEAM FLOOR BOEING727 727247 138408FNM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND FLOOR BEAM CORRODED AT FUSELAGE STATION 344 LBL 32 TO LBL 60, REPAIRED PER SRM 53-10-8 FIGURE 8. 2L73 4F A3WE 19950120000831995012000083NM 1995 1 20 DL72W950163 119950107A5315 BEAM FLOOR BOEING727 727247 138408FNM FS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND STATION 400 FLOOR BEAM BL 0 TO RBL 4 CORRODED, REPAIRED PER SRM 53-10-8 FIGURE 3. 2L73 4F A3WE 19950120000841995012000084NM 1995 1 20 DL72W950164 119950110A5720 UPLOCK FRAME BOEING727 727247 138408FNM WS 910/913 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND THE RT UPLOCK FRAMES AT STA 910 AND 913 HAVE TEMPORORARY REPAIRS, REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950120000851995012000085NM 1995 1 20 DL733950068 119950104A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 986.5 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 DURING HMV, CORROSION WAS FOUND ON FLOOR BEAM AT STA 986.5 AROUND FASTENER HOLES ON TOP FLANGE. REPAIRED PER SRM 53-00-51 PG 220. 2L72 4F RTA16WE 19950120000861995012000086NM 1995 1 20 DL733950069 119950105A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 DURING HMV, CORROSION WAS FOUND ON A FLOOR BEAM AT FS 328 AROUND FASTENER HOLES FROM LEFT TO RIGHT SIDE OF THE FUSELAGE. REPAIRS INVOLVED TREAT AND PAINT LBL49 PER PS 900-2 NR 5 AND REPAIR LBL 36 AND RT OUTBOARD END PER SRM 53-00-51 FIG 205. 2L72 4F RTA16WE 19950120000871995012000087NM 1995 1 20 DL733950071 119950103A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 312 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 DURING HMV, CORROSION WAS FOUND AT FS 312 FLOOR BEAM FASTENER HOLES AT LBL 6, CENTERLINE AND RBL 8. REPAIRED PER SRM 53-10-51 FIG 205. 2L72 4F RTA16WE 19950120000881995012000088NM 1995 1 20 DL733950072 119950103A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 294 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON FLOOR BEAM 'T' CAP SURFACE AT STA 294 BL0 TO OUTBOARD RBL AROUND FASTENER HOLES. REPAIRED PER ERA 300920-14. 2L72 4F RTA16WE 19950120000891995012000089NM 1995 1 20 DL733950073 119950103A5347 SEAT TRACK BOEING737 737347 1384647NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, FOUND CORROSION ON LEFT OUTBOARD SEAT TRACK AT FS 344. REPAIRED PER SRM 53-00-52 PG 202-205. 2L72 4F RTA16WE 19950120000901995012000090NM 1995 1 20 DL733950074 119950103A5347 FLOOR TRACK BOEING737 737347 1384647NM FS 328 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 ON RT SIDE AT CENTER FWD END. REPAIRED PER SRM 53-00-52 PG 202-205. 2L72 4F RTA16WE 19950120000911995012000091NM 1995 1 20 DL733950075 119950103A5347 FLOOR TRACK BOEING737 737347 1384647NM FS 328 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM STA 328 ON OUTBOARD TRACK RIGHT HAND SIDE AT FWD END. REPLACED SEAT TRACK PER SRM 51-00-00. 2L72 4F RTA16WE 19950120000921995012000092NM 1995 1 20 DL733950076 119950103A5347 FLOOR TRACK BOEING737 737347 1384647NM FS 328 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON GALLEY FLOOR TRACK AT FLOOR BEAM 328 RT SIDE ON THE FWD END OF INBOARD TRACK. REPAIRED PER SRM 53-00-52 PG 202-205. 2L72 4F RTA16WE 19950120000931995012000093NM 1995 1 20 DL733950097 119950104A5347 SEAT TRACK BOEING737 737347 1384647NM FS 960 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON SEAT TRACK UPPER SURFACES AT STA 960 ON THE OUTBOARD SIDE. REPAIRED PER SRM 53-00-52 FIG 204. 2L72 4F RTA16WE 19950120000941995012000094NM 1995 1 20 DL733950101 119950104A5320 FLOOR SUPPORT BOEING737 737347 1384647NM FS 960 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, FOUND FLOOR SUPPORT CORRODED AT STA 960 LBL 10-30. REMOVED OLD, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-00-00. 2L72 4F RTA16WE 19950120000951995012000095NM 1995 1 20 DL733950118 119950104A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 960-975 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON FLOOR BEAM CAPS SECTIONS AT STA 960 TO 975 RBL 30-40. REPAIRED PER SRM 53-00-51. 2L72 4F RTA16WE 19950120000961995012000096NM 1995 1 20 DL733950119 119950108A5347 SEAT TRACK BOEING737 737347 1384647NM FS 344 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, CORROSION WAS FOUND ON SEAT TRACK HORIZONTAL FLANGE AT STA 344 LBL 20. REMOVED OLD SECTION, FABRICATED NEW SEAT TRACK AND INSTALLED SEAT TRACK PER SRM53-00-52. 2L72 4F RTA16WE 19950120000971995012000097NM 1995 1 20 DL733950141 119950110A5247 APU DOOR BOEING737 737347 1384647NM APU COMPARTMENT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112310 23596 DURING LETTER CHECK, FOUND LOWER APU SHROUD RUBBING ON THE APU DOOR CAUSING DAMAGE WHICH REQUIRED REPAIRS PER SRM 52-40-01 FIG 204. 2L72 4F RTA16WE 19950120000981995012000098NM 1995 1 20 DL733950160 119950110A5743654988506 ATTACH FITTING BOEING737 737347 1384647NM RT MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 DURING ROUTINE INSPECTION AT HMV, THE RT WING O/B AFT SUPPORT FITTING FOR THE MAIN LANDING GEAR BEAM WAS FOUND CRACKED. THE CRACKED FITTING WILL REMAIN IN SERVICE PER S/B 737-57-1216 AND WILL BE REPAIRED PER S/B REQUIREMENTS. 2L72 4F RTA16WE 19950120000991995012000099NM 1995 1 20 DL757950134 119950110A2410729825G IDG BOEING757 757232 1384965NM NR 1 ENGINE FAILED A DALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11639DL 23993 DURING CLIMB-OUT, LEFT GENERATOR DRIVE LIGHT ILLUMINATED ACCOMPANIED WITH ENGINE VIBRATION, DISCONNECTED IDG, STARTED APU, 10 MINUTES LATER APU AUTO SHUTDOWN. RETURNED FLIGHT TO ATL. FOUND IDG FAILED. REPLACED IDG, TROUBLESHOOTING APU COULD NOT FIND ANY PROBLEMS RETURNED TO SERVICE. 2L72 4F RTA2NM 19950120001001995012000100NM 1995 1 20 DL757950142 119950111A5753 SKIN BOEING757 757232 1384965NM NR 3 FORE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 DURING LETTER CHECK, RIGHT WING NR 3 FWD FLAP WAS FOUND WITH A DENT IN THE LOWER SKIN AT STA 86. REPAIRED DAMAGE PER SRM 57-53-01. 2L72 4F RTA2NM 19950120001021995012000102NE 1995 1 20 DLL10950178 219950113A7200RB21122B02 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 BIRD STRIKE A DALAE ENGINE SHUTDOWN C F.O.D. TOTAKEOFF 1 SO11719DA40117 193C1135 010104 ON TAKEOFF, NR 3 ENGINE INGESTED A SEA GULL WITH RESULTING COMPRESSOR STALLS, FLIGHT RETURNED TO PDX AFTER NR 3 ENGINE WAS SHUT DOWN. ENGINE WAS REPLACED DUE TO COMPRESSOR DAMAGE. 2L73 4F4 F A23WE E12EU 19950120001031995012000103WP 1995 1 20 DLL16950128 119950109A5712 RIB LKHEED1011 10113853 5265020WP LT WS 293 MODIFIED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 REF EO 7-59089 IN COMPLIANCE OF VA 31733AT LEFT WING RIB CAP AT IWS 293, BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED, DUE TO INTERFERENCE FROM RIB CAP. CUT RIB CAP FOR TOOL CLEARANCE AND REPAIR PER SRM 57-12-00 PG805. 2L73 4F A23WE 19950120001041995012000104WP 1995 1 20 DLL16950129 119950109A5712 RIB LKHEED1011 10113853 5265020WP LT WS 319 MODIFIED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 REF EO 7-59089 AT LEFT WING IWS 319, BOTTOM HOLE ON VERICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE OF RIB CAP. CUT RIB FLANGE FOR TOOL CLEARENCE AND REPAIRED PER SRM 57-12-00 PG 805. 2L73 4F A23WE 19950120001051995012000105WP 1995 1 20 DLL16950130 119950109A5712 RIB LKHEED1011 10113853 5265020WP RT WS 293 MODIFIED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 REF EO 7-59089-3 IN COMPLIANCE OF VA 31733 AT RIGHT WING IWS293 BOTTOM HOLE ON VERTICAL RIB FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE TO RIB CAP. CUT RIB CAP FOR CLEARANCE AND REPAIRED PER SRM 57-12-00 P805. 2L73 4F A23WE 19950120001061995012000106WP 1995 1 20 DLL16950131 119950109A5712 RIB LKHEED1011 10113853 5265020WP RT WS 319 MODIFIED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 REF EO 7-59089-3 AT RIGHT WING IWS 319 RIB CAP BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE WITH THE RIB CAP. CUT RIB CAP AND REPAIRED PER SRM 57-12-00 PG 805. 2L73 4F A23WE 19950120001071995012000107WP 1995 1 20 DLL16950132 119950105A5330 TEARSTRAP LKHEED1011 10113853 5265020WP FS 865/883 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL, A TEARSTRAP BETWEEN FS 865 AND 883, BETWEEN STR 34 AND 35 WAS FOUND DELAMINATED. REPAIRED PER SRM 53-31-0 FIG 816. 2L73 4F A23WE 19950120001081995012000108WP 1995 1 20 DLL16950133 119950113A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1370 LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, A TEAR STRAP WAS FOUND LOOSE AT FS 1370 BETWEEN STR 33 AND 34. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950120001101995012000110NM 1995 1 20 DLM88950175 119950112A2421976J2526 GENERATOR DOUG MD88 MD88 3023688NM NR 1 ENGINE FAILED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO11914DL 49545 DURING CRUISE, LEFT GENERATOR WENT OFF LINE, STARTED APU HAD CROSS TIE LOCKOUT. DIVERTED CVG. RESET CROSSTIE OPERATION NORMAL, DEFERRED PER MEL NR 1 GEN. GENERATOR WAS REPLACED AND ROUTED TO SHOP, OPERATION NORMAL. 2L72 4F RTA6WE 19950120001111995012000111NM 1995 1 20 DLM88950177 119950112A2910AS153080200 HYD HOSE DOUG MD88 MD88 3023688NM TAIL COMP LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11908DL 49539 DURING CLIMBOUT, ON FLAP SLAT RETRACTION HAD TOTAL LOSS OF RIGHT SYSTEM HYDRAULIC PRESSURE AND FLUID. RETURNED TO DFW. FOUND LEAKING LINE AT RIGHT FWD FILTER MODULE IN TAIL COMAPARTMENT. REPLACED LINE OPERATION NORMAL. 2L72 4F RTA6WE 19950120001121995012000112WP 1995 1 20 MWEA95007 119950117A5532 SKIN DOUG DC9 DC932 3022066WP VERT STAB GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, FOUND LT VERTICAL STAB SKIN GOUGED UNDER HORIZONTAL TO VERTICAL STAB FAIRING. FABRICATED AND INSTALLED NEW SKIN SECTION IAW SRM 51-10-2A AND 51-01 PG 1. 2L72 4F A6WE 19950120001131995012000113WP 1995 1 20 MWEA95008 119950117A5230 BEAM DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, FOUND AFT CARGO DOOR NR 4 BEAM FWD END CRACKED. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 52-01. 2L72 4F A6WE 19950120001141995012000114 1995 1 20 MWEA95009 419950115A256513621225 EVAC SLIDE DOUG DC9 DC914 3022034WP TAIL COMPT LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 84 45711 DURING ROUTINE INSPECTION, THE TAIL EVACUATION SLIDE PRESSURE WAS FOUND TO BE LOW. REPLACED TAIL EVACUATION SLIDE, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950120001151995012000115EU 1995 1 20 QXEA9500009 119950112A3350MGG1055 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU GALLEY FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 GEG - GALLEY EMERGENCY LIGHT (3V) WON'T ILLUMINATE. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950120001161995012000116EU 1995 1 20 QXEA9500010 119950112A3350 EEL FOKKERF28 F28MK1000 4990808EU CABIN MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09466US 11075 GEG - FLOOR PROXIMITY LIGHT MISSING FROM SEAT 11A/B. PLACED ON MEL 33-13. 2L72 4F RTA20EU 19950120001171995012000117 1995 1 20 QXEA9500011 219950112A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW NR 1 POSITION MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09386PH AC597 PDX - VAPORIZED ENGINE OIL SMELL FROM NR 1 BLEED AIR. SYSTEM PLACED ON MEL 21-4. 1L72 4T A8SW 19950120001181995012000118NM 1995 1 20 QXEA9500014 119950113A326080053519 CAUTION PANEL DHAV DHC8 DHC8102 2809003NM CABIN MALFUNCTIONED A QXEAK NONE N FALSE WARNING APAPPROACH 1 NM09815PH 50 PDX - WOW CAUTION LIGHT ILLUMINATED TWICE ON FINAL APPROACH. NO FAULTS NOTED ON PSEU MEGGED WIRES FROM PSEU TO CAUTION PANEL, NO DEFECTS NOTED. REPLACED THE CAUTION PANEL. AIRCRAFT WAS TEST FLOWN SATISFACTORY AND RETURNED TO SERVICE. 2H72 4T RTA13NM 19950120001191995012000119NM 1995 1 20 QXEA9500015 119950115A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM LANDING GEAR DEFECTIVE A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09821PH 67169 104 PDX - THE LANDING GEAR INOP CAUTION LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED PSEU IAW, DEHAVILLAND -8 M.M. 32-61-50, PG. 201. OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950120001201995012000120 1995 1 20 QXEA9500017 219950113A7200 ENGINE DORNERDO32 DO328100 2996000NM NR 2 LOST POWER A QXEAO OTHER R PARTIAL RPM/PWR LOSS APAPPROACH 1 NM09332PH 3010 RDM - APPROCH INTO RDM, NR 2 ENG TORQUE DROPPED FROM APPROX 40 PERCENT TO 0 PERCENT, FOLLOWED BY YAWING OF A/C. ADVANCED NR 2 POWER LEVER, TORQUE WAS RESTORED. ALMOST IMMEDIATLY NR 1 TQ DROPPED FROM APPROX 40 PERCENT TO 0 PERCEN. ADVANCED PWR LEVER AND TQ WAS RESTORED. WEATHER WAS SNOWING, ALL ENG DEICE WAS ON. NO EVIDENCE OF ICE WAS ON THE A/C. A/C LANDED IN RDM W/O FURTHER INCIDENT. OPS CHECK OF NR 1/2 AIR INTAKE AND DEICE SYS PERFORMED, AIR INTAKE INSP PERFORMED, POWER ASSURANCE RUN ACCOMPLISHED ON NR 1/2 ENG, ALL CHECKS WERE NORMAL. REPLACED NR 1/2 FUEL FILTERS. FUEL SAMPLES TAKEN, WATER AMOUNT IN FUEL WAS ABOVE NORMAL BUT NOT ENOUGH TO CAUSE ENG POWER LOSS. FDR REMOVED FOR FURTHER ANALYSIS. 2H72 4T RTA45NM 19950120001211995012000121NM 1995 1 20 SWAA950012 119950109A5330 SKIN BOEING737 7373H4 1384600NM BS 935 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07301SW 22941 DURING SCHEDULED A2 CHECK, FOUND 2.275 INCH FUSELAGE SKIN CRACK AT BS 935, BETWEEN S24 AND 25R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950120001221995012000122NM 1995 1 20 SWAA950013 119950109A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07301SW 22941 DURING SCHEDULED A2 CHECK, FOUND 3 INCH FUSELAGE SKIN CRACK BELOW S12L AND FORWARD OF WINDOW NUMBER 12. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950120001231995012000123NM 1995 1 20 SWAA950014 119950111A5330 SKIN BOEING737 7372H4 138448CNM BS 937 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0720SW 21337 DURING SCHEDULED SPECIAL VISIT, SKIN LAP INSPECTION FOUND SKIN CRACK INDICATION AT BS 937, S4L. REPAIRED PER TRAMCO EWO 93-0003. 2L72 4F A16WE 19950120001241995012000124NM 1995 1 20 SWAA950015 119950111A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0720SW 21337 DURING SCHEDULED SPECIAL VISIT, SKIN LAP INSPECTION FOUND SKIN CRACK INDICATIONS AT BS 268, 328, 336, 343, 351, 480, 490, 510, 767, AND 977, S4R. REPAIRED PER TRAMCO EWO 95-0003. 2L72 4F A16WE 19950120001251995012000125NM 1995 1 20 SWAA950016 119950111A5330 SKIN BOEING737 7372H4 138448CNM BS 590 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0720SW 21337 DURING SCHEDULED SPECIAL VISIT, SKIN LAP INSPECTION FOUND SKIN CRACK INDICATION AT BS 590, S4L. REPAIRED PER TRAMCO EWO 95-0028. 2L72 4F A16WE 19950120001261995012000126NM 1995 1 20 SWAA950017 119950110A3412102AH2AG AIR TEMP PROBE BOEING737 7373H4 1384600NM CAPT INOP A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07387SW 26602 NUMBER 1 AIR TEMP PROBE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED TOTAL AIR TEMP PROBE PER BOEING M/M. 2L72 4F RTA16WE 19950120001271995012000127NM 1995 1 20 SWAA950018 119950112A5320 CLIP BOEING737 7373Y0 1384671NM BS 727D CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, RBL 8, WL 147. REPLACED STRINGER CLIP PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950120001281995012000128NM 1995 1 20 SWAA950019 119950112A5330 SKIN BOEING737 7373Y0 1384671NM BS 368/867 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 368, WL 205, LEFT SIDE AND A LONGITUDINAL CREASE AFT OF CARGO DOOR, BS 867, BETWEEN S22R AND 23R. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950120001291995012000129NM 1995 1 20 SWAA950020 119950112A5320 WEB BOEING737 7375H4 138449DNM AFT CARGO DR WAYCRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AND TORN OUT AT LOWER FWD END OF AFT CARGO DOORWAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950120001301995012000130NM 1995 1 20 UPS201925 119950112A3231 RETRACT MECH BOEING727 72725C 138400HNM RT MLG MALFUNCTION A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01932UP 19856 PILOT REPORTED, RT MLG DOOR FAILED TO CLOSE AFTER TAKEOFF, CYCLED GEAR, SECOND TIME DOOR CLOSED, BUT SLOWLY. TESTED RT MAIN GEAR DOOR PER MM 32-12-01, CHECKS GOOD. NO PROBLEMS NOTED. 2L73 4F A3WE 19950120001311995012000131NM 1995 1 20 UPS201934 119950109A5320 WEB BOEING727 727173C 1384059NM BS 1226 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 53-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950120001321995012000132NM 1995 1 20 UPS201935 119950109A5320 WEB BOEING727 727173C 1384059NM BS 1290 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1290 WL 180 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151. 2L73 4F A3WE 19950120001331995012000133NM 1995 1 20 UPS201937 119950116A5347 SEAT TRACK BOEING727 727185C 138406NNM FS 756-852 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK, MAINTENANCE FOUND SEAT TRACK HAS CORROSION AND PITTING STA 756-852, LB 25, WL 208. INSTALLED REPAIR IAW SRM 51-20-4 AND SRM 51-30-2. 2L73 4F A3WE 19950120001341995012000134NM 1995 1 20 UPS201938 119950116A5510 TE BEAM BOEING727 727185C 138406NNM HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON RT HORIZIZONTAL STAB UPPER T/E BEAM, LOWER SURFACE OF FWD FLANGE AT APPROX STAB STA 118.00. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950120001351995012000135NM 1995 1 20 UPS201939 119950116A5347 SEAT TRACK BOEING727 727185C 138406NNM FS 756-852 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 756-852, LBL 45, WL 208. INSTALLED REPAIR IAW SRM 51-10-2. 2L73 4F A3WE 19950120001361995012000136NM 1995 1 20 UPS201940 119950116A5751 CTR HINGE BOEING727 727185C 138406NNM RT AILERON CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK MAINTENANCE, FOUND CENTER HINGE FOR T/E PANEL ON RT I/B AILERON PITTED AND CORRODED. INSTALLED REPAIR IAW SRM 20-20-01. 2L73 4F A3WE 19950120001371995012000137NM 1995 1 20 UPS201941 119950116A5744 TRACK BOEING727 727185C 138406NNM NR 6 FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK MAINTENANCE, FOUND NR 6 FLAP TRACK HAS RUST EMITTING FROM SPOILER BEAM ATTACH POINT. INSTALLED REPAIR IAW OHM 57-40-01. 2L73 4F A3WE 19950120001381995012000138NM 1995 1 20 UPS201942 119950116A5320 EXPANSION LINK BOEING727 727185C 138406NNM FS 740-760 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK LBL 45, STA 740-760. INSTALLED REPAIR IAW SRM 51-10-01 AND 51-30-2. 2L73 4F A3WE 19950120001391995012000139NM 1995 1 20 UPS201943 119950116A5347 SEAT TRACK BOEING727 727185C 138406NNM FS 740-760 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK MAINTENANCE, FOUND SEAT TRACK AT LBL 45 STA 740-760 CORRODED. INSTALLED REPAIR IAW SRM 51-10-01, 51-30-2, 51-10-02 AND MM 51-20-151. 2L73 4F A3WE 19950120001401995012000140NM 1995 1 20 UPS201944 119950116A5320 ANGLE BOEING727 727185C 138406NNM FS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN C-CHECK, MAINTENANCE FOUND CORRODED ANGLE THAT ATTACHES DELTA BEAM AND BS 740 WEB, AFT SIDE OF WEB, LBL 9 TO RBL 9. INSTALLED REPAIR IAW SRM 51-30-2 AND MM 20-10-05. 2L73 4F A3WE 19950120001411995012000141NM 1995 1 20 UPS201953 119950113A2910 HYD SYST BOEING727 72730C 1384009NM LWR FUSELAGE OVERSERVICED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01906UP 19314 PILOT REPORTED, AIR CONDITIONING FUMES STILL EVIDENT ESPECIALLY AT HIGH POWER SETTING. FOUND HYDRAULIC SYSTEM OVERSERVICED. DRAINED HYD FLUID TO PROPER LEVEL. 2L73 4F A3WE 19950120001421995012000142NM 1995 1 20 UPS201954 119950113A2150 LT PACK BOEING727 72730C 1384009NM CABIN SMOKE A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO01906UP 19314 PILOT REPORTED, FUMES IN FLIGHT DECK AFTER T/O (SIMILAR TO PREVIOUS PROBLEM) LEFT PACK WAS SHUT OFF AND FUMES DIMINISHED. INSTALLED REPAIR. RAN PACKS, OPS CHECK GOOD. OK FOR SERVICE. 2L73 4F A3WE 19950120001431995012000143NM 1995 1 20 UPS201955 119950109A5320 WEB BOEING727 727173C 1384059NM BS 1226 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE REPORTED CRACK IN WEB AT BS 1226 WL 188 RBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND 51-20-151. 2L73 4F A3WE 19950120001441995012000144NM 1995 1 20 UPS501926 119950116A5320 FLOOR SUPPORT BOEING757 75724APF 1384969NM FS 1425 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01431UP 25462 WHILE IN 'C' CHECK, MAINTENANCE REPORTED FLOOR SUPPORT STA 1425 RBL 11 CRACKED AND DENTED IN AFT CARGO BAY. INSTALLED REPAIR IAW SRM 51-70-12. 2L72 4F RTA2NM 19950120001451995012000145WP 1995 1 20 UPS501933 119950111A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 100 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING A WALKAROUND, MAINTENANCE REPORTED CRACK IN LOWER SIDE WITH 1 EACH POPPED FASTENER HEAD (RIVET). CRACK IS OPEN WITH VISIBLE CORROSION. 2L74 4F RT4A25 19950120001461995012000146WP 1995 1 20 UPS801927 119950104A5320375922201 SPLICE DOUG DC8 DC873F 302199FWP FS 1260-1280 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED FS 1260-1280, LONG 36 SPLICE FITTING CRACKED 12 INCHES LONG. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950120001471995012000147WP 1995 1 20 UPS801928 119950105A53203750330505 SPLICE DOUG DC8 DC873F 302199FWP FS 440-480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED FS 440-460, LONG 27L SPLICE FITTING CRACKED 3 INCHES LONG. INSTALLED REPAIR IAW SRM 51-1-21D. 2L74 4F RT4A25 19950120001481995012000148WP 1995 1 20 UPS801929 119950103A57535651189 HINGE FITTING DOUG DC8 DC873F 302199FWP FS 409/339 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP HINGE SUPPORT FITTINGS CRACKED AT STA 409, INBOARD FITTING AND STA 339 OUTBOARD FITTING. INSTALLED REPAIR IAW DOUGLAS DRAWING 5751186. 2L74 4F RT4A25 19950120001501995012000150WP 1995 1 20 UPS801931 119950102A57125770123 LE RIBS DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING LEADING EDGE NR 11, NR 12, NR 13, NR 16, NR 17 RIBS CRACKED ON UPPER SIDE COUNTING OUTBOARD OF NR 1 PYLON. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801. 2L74 4F RT4A25 19950120001511995012000151WP 1995 1 20 UPS801932 119950102A57125770123 LE RIBS DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING OUTBOARD OF NR 1 PYLON NR 4, NR 5, NR 6, NR 9, NR 10 RIBS ON LEADING EDGE CRACKED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801. 2L74 4F RT4A25 19950120001521995012000152WP 1995 1 20 UPS801945 119950116A57555655169 SKIN DOUG DC8 DC873F 302199FWP NR 5 SPOILER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED NR 5 SPOILER LEFT WING DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-61-01. 2L74 4F RT4A25 19950120001531995012000153WP 1995 1 20 UPS801946 119950116A57301050707576 LE SKIN DOUG DC8 DC873F 302199FWP WS 310 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING L/E FASTENER HOLE 1 INCH CRACK AT STA XFS 310, UPPER SURFACE. INSTALLED REPAIR IAW SRM 57-2-0. 2L74 4F RT4A25 19950120001541995012000154WP 1995 1 20 UPS801947 119950116A57535652287 VANE DOUG DC8 DC873F 302199FWP NR 1 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 1 FLAP VANE DELAMINATED AT BOTH SURFACES. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950120001551995012000155WP 1995 1 20 UPS801948 119950116A57535701446 VANE DOUG DC8 DC873F 302199FWP NR 3 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 3 FLAP VANE DELAMINATED ON UPPER SIDE. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950120001561995012000156WP 1995 1 20 UPS801949 119950116A57535701152 VANE DOUG DC8 DC873F 302199FWP NR 4 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING NR 4 FLAP VANE DELAMINATED ON BOTH SURFACES. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950120001571995012000157WP 1995 1 20 UPS801950 119950116A5753 VANE DOUG DC8 DC873F 302199FWP NR 4 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP VANE NR 4 DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950120001581995012000158WP 1995 1 20 UPS801951 119950116A5753 VANE DOUG DC8 DC873F 302199FWP NR 3 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED RT WING FLAP VANE NR 3 DELAMINATED ON BOTH SIDES. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950120001591995012000159WP 1995 1 20 UPS801952 119950116A5330040707576 SKIN DOUBLER DOUG DC8 DC873F 302199FWP FS 190 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE REPORTED SKIN SPLICE DOUBLER HAS HEAVY INTERGRANULAR CORROSION AT FS 190, BETWEEN LONG 32L - 32R. INSTALLED REPAIR IAW SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 19950120001641995012000164WP 1995 1 20 ERA00014 119950117A2120 AIR DISTR CVAC 340 34031 2422704WP CABIN SMOKE A ERAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AL03568JA 57 SMOKE APPEARED IN CABIN. RAN AIRCRAFT FOR 30 MINUTES ON THE GROUND, OPERATED HEAT AND PRESSURIZATION IN ALL MODES, NO SMOKE NOTED. PERFORMED CHECK FLIGHT, COULD NOT DUPLICATE PROBLEM. 2L72 4R 6A6 19950120001651995012000165NM 1995 1 20 ERA00015 119950117A3350 EEL TRACK DHAV DHC8 DHC8103 1386005NM CABIN MALFUNCTIONED A ERAAK NONE L NO TEST ININSP/MAINT 1 AL03882EA 098 FLOOR TRACK EMERGENCY LIGHTS WON'T WORK FROM THE FLIGHT ATTENDANT STATION. REBOOTED ELECTRICAL SYSTEM, OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 19950120001711995012000171CE 1995 1 20 95ZZZX258 119950104A793199121782 TRANSMITTER CESSNA500 550 2076604CE LT ENG OIL FAILED A CWQAO OTHER O OTHER CRCRUISE 1 GL056862Q 5500265 LEFT ENGINE LOW OIL PRESSURE TRANSMITTER FAILED WHILE EN ROUTE. REPLACED TRANSMITTER. RETURNED TO SERVICE. 1L72 4F A22CE 19950120002321995012000232NM 1995 1 20 94UAL767043 119950116A492036111751 CARBON SEAL ALLIED SIGNA BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE APU CHIPPED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29609UA 21870 61458 FUMES IN COCKPIT WHEN APU SUPPLIED PACKS. REPLACED APU. SHOP FOUND CARBON SEAL CHIPPED. 2L72 4F4 FRTA1NM E3NE 19950120002331995012000233WP 1995 1 20 9500699872 119950112A5311 FRAME DOUG DC9 DC951 3022051WP FS 907 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION ON FS 907 FRAME LOWER FLANGE FROM LONGERON 29L - 29R. REPAIRED PER EA 98-093772. 2L72 4F A6WE 19950120002341995012000234WP 1995 1 20 9500739305 119950111A5350 RELEASE MECH DOUG DC9 DC982 3022082WP TAILCONE LACK OF LUBE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307RC 48086 DURING LINE CHECK, FOUND THAT THE TAILCONE FAILED TO RELEASE AND DROP. CHECKED RIGGING AND LUBRICATED THE RELEASE MECHANISM. CHECKED OK. 2L72 4F A6WE 19950120002351995012000235WP 1995 1 20 9500749997 119950112A2612 FIRE LOOP DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE RT ENGINE MALFUNCTIONED A NWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 GL018933E 47142 653617 INBOUND TO MSN, THE NR 2 FIRE WARNING ILLUMINATED. SYSTEM FAILED OPERATIONAL TEST OF THE SECONDARY LOOP. PULLED THE FIRE HANDLE SHUTTING DOWN NR 2 AND DISCHARGED BOTH FIRE BOTTLES. FOUND 'B' LOOP HAD MALFUNCTIONED. PLACED THE 'B' LOOP ON MEL. INSPECTED ENGINE FOR PNEUMATIC LEAKS. NONE FOUND. REPLACED THE FIRE BOTTLES. ENGINE RUN-UP AND SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950120002361995012000236WP 1995 1 20 9500759910 119950110A5320 FITTING DOUG DC9 DC931 3022065WP FS 908 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01960N 47256 DURING PERIODIC CHECK, FOUND CRACK IN FS 908 FRAME ATTACH FITTING AT FLOOR LEVEL. REPLACED PER SRM 51-30-5. 2L72 4F A6WE 19950120002371995012000237WP 1995 1 20 9500769910 119950110A5320 FITTING DOUG DC9 DC931 3022065WP FS 928 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01960N 47256 DURING PERIODIC CHECK, FOUND CORROSION IN FS 928 FRAME ATTACH FITTING AT FLOOR LEVEL. REPLACED PER SRM 51-30-5. 2L72 4F A6WE 19950120002381995012000238WP 1995 1 20 9500779927 119950111A5311 FRAME DOUG DC9 DC931 3022065WP FS 1132 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING PERIODIC CHECK, FOUND 12 INCH CRACK IN THE FS 1132 FRAME AT LONGERONS 17L - 19L. REPLACED LOWER FRAME PER DWG 9911877 AND SRM 51-30-2. 2L72 4F A6WE 19950120002391995012000239WP 1995 1 20 9500789856 119950111A5343 LUG DOUG DC9 DC951 3022051WP MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01765NC 47718 DURING PERIODIC CHECK, FOUND CORROSION IN LEFT MAIN LANDING GEAR FITTING SIDE BRACE LUG. REPAIRED PER EA 98-094270. 2L72 4F A6WE 19950120002401995012000240WP 1995 1 20 9500799154 119950111A5210 FITTING DOUG DC9 DC914 3022034WP MAIN CABIN DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018913E 45830 DURING PERIODIC CHECK, FOUND CRACK IN MAIN CABIN DOOR END FITTING NR 5 BEAM. REPLACED FITTING. 2L72 4F A6WE 19950120002411995012000241WP 1995 1 20 9500809856 119950111A5712 RIB DOUG DC9 DC951 3022051WP WS 485.5 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01765NC 47718 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT WING RIB, WS 485.5. REPAIRED PER EA 98-094922. 2L72 4F A6WE 19950120002421995012000242WP 1995 1 20 9500819872 119950111A5220 FRAME DOUG DC9 DC951 3022051WP EMERGENCY EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CRACK IN THE RIGHT AFT EMERGENCY EXIT FRAME AT NR 14 STOP. REPAIRED PER EA 98-96160. 2L72 4F A6WE 19950120002431995012000243WP 1995 1 20 9500829872 119950111A5313 LONGERON DOUG DC9 DC951 3022051WP FS 1055 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 30 AT FS 1055 FASTENER HOLE. REPAIRED PER EA 98-096168. 2L72 4F A6WE 19950120002441995012000244WP 1995 1 20 9500839872 119950111A5311 FRAME DOUG DC9 DC951 3022051WP FS 964 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION ON FS 964 FRAME LOWER FLANGE FROM LONGERON 28L - 29R. REPAIRED PER EA 98-093780. 2L72 4F A6WE 19950120002451995012000245WP 1995 1 20 9500849927 119950112A5320 CHORD DOUG DC9 DC931 3022065WP FS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING PERIODIC CHECK, FOUND CORROSION IN FS 110 LOWER CHORD ANGLE, NOSE WHEEL WELL RIGHT TUNNEL. REPAIRED PER EA X9-53-51. 2L72 4F A6WE 19950120002461995012000246WP 1995 1 20 9500859154 119950112A574439148382 FITTING DOUG DC9 DC914 3022034WP RT TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018913E 45830 DURING PERIODIC CHECK, FOUND TWO CRACKS IN THE RIGHT WING FLAP, NR 2 AFT HINGE OUTBOARD SUPPORT FITTING. REPLACED FITTING PER SRM 57-09, FIG 14, PG 56. 2L72 4F A6WE 19950120002471995012000247WP 1995 1 20 9500869945 119950112A5744 HINGE FITT DOUG DC9 DC931 3022065WP LT TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WING NR 2 FLAP HINGE FITTING OUTBOARD FASTENER BORES. REPAIRED PER XEA X9-9-27-9. 2L72 4F A6WE 19950120002481995012000248NE 1995 1 20 9500879915 219950116A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 FLAMED OUT A NWAACD ABORTED TAKEOFF RETURN TO BLOCK JX WARNING INDICATION ENGINE FLAMEOUT TOTAKEOFF 1 GL01965N 47417 666911 ON TAKEOFF ROLL, THE NR 2 ENGINE FLAMED OUT. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ENGINE WAS INSPECTED, NO TROUBLE FOUND. ENGINE RUN-UP PERFORMED AND SYSTEMS CHECKED OK. FLAMEOUT WAS ATTRIBUTED TO THE INGESTION OF HEAVY SNOW AND SLUSH ACCUMULATIONS FOUND ON THE RUNWAY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950120002491995012000249NE 1995 1 20 9500882294 219950112A7261 OIL RETURN TUBE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE STRIPPED A NWAAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL01294US 21505 700030 EN ROUTE TO DEN, THE NR 3 ENGINE LOW OIL PRESSURE WARNING INDICATION ILLUMINATED. OIL PRESSURE AND OIL QUANTITY INDICATED ZERO. ACCOMPLUSHED PRECAUTIONARY SHUTDOWN OF THE NR 3 ENGINE. MAINTENANCE FOUND THREADS DETERIORATED IN GEARBOX CASE ALLOWING OIL LEAKAGE AT RETURN TUBE. REPAIRED THREADS AND RESEALED TUBE. SERVICED ENGINE OIL. TESTED ENGINE PER MM. ENGINE CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950120002501995012000250NM 1995 1 20 9500896608 119950113A33506106765 EEL BATTERY PACK BOEING747 747151 1384891NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01608US 19785 DURING LINE CHECK, SEVERAL EMERGENCY LIGHTS AT CABIN DOORS WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AND PERFORMED FUNCTIONAL CHECK. UNITS TESTED NORMAL. 2L74 4F A20WE 19950120002511995012000251NM 1995 1 20 9500902705 119950115A32501692RA12 VALVE BOEING727 727225 1384077NM NLG STEERING MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01802EA6821 22433 DURING TAKEOFF, FULL RIGHT RUDDER REQUIRED TO MAINTAIN RUNWAY CENTER LINE. ABORTED TAKEOFF AT 60 KTS AND RETURNED TO GATE. MAINTENANCE DUPLICATED MALFUNCTION. REPLACED NOSE LANDING GEAR METERING VALVE, RUDDER PEDAL STEERING MECHANISM, AND RIGGED STEERING SYSTEM. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950120002521995012000252NM 1995 1 20 95UAL737003 119950113A3350 EEL STRIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29303UA 23644 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHT STRIP INOP. REPLACED LIGHT STRIP. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950120002531995012000253NM 1995 1 20 95UAL737004 119950113A2612 FIRE WARNING BOEING737 737291 138448WNM PWA JT8 JT8D9A 52048NE APU ACTIVATED A UALAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP29980UA 21545 DURING TAXI GOT APU FIRE WARNING. BOTTLE WAS DISCHARGED, BUT LIGHT REMAINED ON. FIRE TRUCKS ESCORTED AIRCRAFT BACK TO TERMINAL. 2L72 4F4 F A16WE E2EA 19950120002541995012000254NM 1995 1 20 95UAL757002 119950117A3350 EEL BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29527UA 24995 EMERGENCY EXIT SIGNS IN FIRST CLASS INOP. SIGNS POWERED BY SAME BATTERY. REPLACED BATTERY, OPS CKS OK. 2L72 4F4 FRTA2NM E17NE 19950120002551995012000255NM 1995 1 20 95UAL757003 119950117A3350 EEL POWER CABLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29509UA 24763 EEL INOP ROW 25C-32C. REPLACED POWER CABLE. OPS CKS OK. 2L72 4F4 FRTA2NM E17NE 19950120002561995012000256NM 1995 1 20 95UAL767001 119950117A3350 EEL CABLE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29611UA 21872 EEL INOP ROW 9-11. REPLACED FEEDER CABLE. OPS CKS OK. 2L72 4F4 FRTA1NM E3NE 19950120002571995012000257GL 1995 1 20 95UALD10005 219950112A7230 COMPRESSOR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 ENGINE STALLED A UALAK NONE R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 WP291846U 48262 451561 RETURNED TO GATE NR 1 ENGINE SHUTDOWN DUE TO APPARENT COMPRESSOR STALL. FLAMES REPORTED BY PASSENGERS ENGINE DISASSEMBLED IN SHOP. NO CAUSE FOR STALL WAS FOUND. UNRELATED DISCREPANCIES WERE FOUND AND CORRECTED. 2L73 4F4 F A22WE E23EA 19950120002581995012000258WP 1995 1 20 95UALD10006 119950112A4900381022MOD APU DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL APU COMPT FAILED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP291845U 48261 A PUNGENT ODOR WAS NOTICED IN AFT CABIN BY FLIGHT ATTENDANT. DURING CLIMB-OUT GOT STRONGER, WITH RECIRC FANS OFF AND ALL PACKS ON DISSAPATED TO A SLIGHT SMELL. FLIGHT ATTENDANT EYES WATERED. REPLACED APU. 2L73 4F4 F A22WE E23EA 19950120002591995012000259WP 1995 1 20 95UALD10007 119950112A217021D10C011 COALESCER BAGS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DIRTY A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 WP291846U 48262 CABIN HAS FAINT ODOR DURING TAKEOFF. CAUSED ILL PASSENGER. REPLACED DIRTY COALESCER BAGS. 2L73 4F4 F A22WE E23EA 19950120002601995012000260WP 1995 1 20 95UALD10008 119950112A2120 AIR DIST DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN SMOKING A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP291832U 46631 DIVERTED TO LAS WITH SMOKE IN CABIN. AIRPLANE CHANGED. 2L73 4F4 F A22WE E23EA 19950120002611995012000261NE 1995 1 20 95UALD10009 219950112A72309061M13G05 LP MANIFOLD DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE TURBINE CASE CRACKED A UALAK NONE O OTHER NRNOT REPORTED 1 WP291852U 47811 NR 1 ENGINE COWL BLOW OUT DOOR OPEN ON ARRIVAL. FOUND TURBINE CASE COOLING MANIFOLD SEPARATED AT TUBE SLEEVE OTBD SIDE OF TURBINE CASE. SEVERAL MANIFOLD SUPPORT BRACKETS ALSO BROKEN. LP MANIFOLD RUPTURED AND DAMAGED AN ADJACENT BRACKET(9044M606041). MANIFOLDS ROUTINELY CHECKED AT L-CHECK. FIRST REPORTED INCIDENT OF THIS P/N MANIFOLD CRACKING. ISOLATED CASE BUT WILL MONITOR. 2L73 4F4 F A22WE E23EA 19950120002621995012000262WP 1995 1 20 95UALD10010 119950116A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291817U 46616 EEL STRIP LIGHTING FROM SEAT 9B TO 18B LEFT SIDE CABIN INOPERATIVE. REPLACED POWER CABLE JUST AFT OF DOOR L-2 TO EEL LIGHT STRIP. 2L73 4F4 F A22WE E23EA 19950120002631995012000263WP 1995 1 20 95UALD10011 119950116A3350 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291812U 46611 GREEN LIGHT DOES NOT ILLUMINATE DURING EMERGENCY LIGHT BATTERY TEST. REPLACED BATTERY PACK AND CHARGERS. 2L73 4F4 F A22WE E23EA 19950120002641995012000264WP 1995 1 20 ABXA9500022 119950113A32600080004002 PROXIMITY BOX DOUG DC8 DC863 302198AWP LT MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING CRCRUISE 1 GL23823AX 46122 LEFT MAIN GEAR DOOR LATCH LIGHT ILLUMINATED. RECYCLED LANDING GEAR 3 TIMES, LIGHT REMAINED ILLUMINATED. AIRCRAFT REDUCED AIRSPEED AND CONTINUED TO ILN. REMOVED AND REPLACED FAULTY PROXIMITY CONTROL BOX. REPLACED BENT PROXIMITY SWITCH PADDLE FOR LEFT GEAR DOOR. SYSTEM OPS CHECKED GOOD IAW DC 8 MM CHAPTER 32. 2L74 4F 4A25 19950120002651995012000265SO 1995 1 20 COM11728 119950110A541112042266001 FRAME EMB 12001400013 EMB 120 EMB120RT SO NACELLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01161CA13965 120143 DURING INSPECTION FOUND THE FRAME 10 WEB IN LEFT NACELLE INBOARD SIDE TO HAVE AN APPROX .625 INCH CRACK RUNNING THROUGH THE FRAME FLANGE RADIUS JUST UNDER THE CUTOUT FOR THE STRINGER. STOP DRILLED THE CRACK AND ADDED A DOUBLER MADE OUT OF AN ORIGINAL FRAME 10 WEB OF SAME PART NR. ALL WORK WAS DONE IAW AERODESIGN REPORT NR 869-1, REV IR, 10-02-93 DATED 1-9-95. 2L72 4T RTA31SO 19950120002661995012000266SO 1995 1 20 COM11729 119950114A612078249012 PCU EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO011105G6416 668 120105 RT ENGINE NP FLUCTUATED BETWEEN 97 AND 102 PERCENT. ALL OTHER ENGINE PARAMETERS WERE NORMAL. REPLACED THE RT PROPELLER PITCH CONTROL UNIT. 2L72 4T RTA31SO 19950120002671995012000267SO 1995 1 20 COM11730 119950115A323012038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01179CA8093 3016 120179 LANDING GEAR INDICATION 'A' SYSTEM IS INOP AND CIRCUIT BREAKER IS TRIPPED. REPLACED THE LANDING GEAR CONTROL BOX ASSY. 2L72 4T RTA31SO 19950120002681995012000268SO 1995 1 20 COM11731 119950115A30607861442 DE-ICE LEAD EMB 120 EMB120RT SO RT PROP BROKEN A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01200CD 120200 RT PROPELLER DE-ICE FAILED. REPLACED BROKEN HEATER LEAD WIRE. 2L72 4T RTA31SO 19950120002691995012000269SW 1995 1 20 COM20350 119950116A32602755009 DOORS SWRNGNSA227 SA227AC 8780603SW NLG REQUIRED ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01704C 13795 AC704 NLG INTRANSIT INDICATOR REMAINED ON AFTER GEAR RETRACTION. ADJUSTED NLG DOORS. 1L72 4T A8SW 19950120002701995012000270EU 1995 1 20 COM31010 119950115A3350 EEL SAAB SF340 SF340A 7850100EU CABIN MALFUNCTIONED A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01380CA 340A012 EMERGENCY LIGHTING SYSTEM IS INTERMITTENT. COULD NOT DUPLICATE. EMERGENCY LIGHTING SYSTEM FUNCTIONS SATISFACTORY. 2L72 4T RTA52EU 19950120002711995012000271EU 1995 1 20 COM31011 119950115A2820AE7062172 FUEL HOSE SAAB SF340 SF340A 7850100EU RT NACELLE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01380CA 340A012 FUEL LEAK RT WHEEL WELL AREA. REPLACED FUEL INTERCONNECT TUBE IN RT NACELLE. 2L72 4T RTA52EU 19950120002721995012000272EU 1995 1 20 COM31012 119950116A76035308211 POWER LEVER SAAB SF340 SF340A 7850100EU COCKPIT DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01359CA15583240 340A053 THE POWER LEVERS CAN BE RETARDED BELOW THE FLIGHT IDLE GATE WITHOUT USING THE RELEASE TRIGGERS. REPLACED THE POWER LEVER QUADRANT ASSY. 2L72 4T RTA52EU 19950120002731995012000273EA 1995 1 20 COM60381 119950115A2741 TRIM IND CNDAIRCL600 CL6002B19 EA STAB TRIM MALFUNCTIONED A COMAK NONE O OTHER UKUNKNOWN 1 SO01914CA 7012 STABILIZER TRIM INDICATOR FLUCTUATES RAPIDLY BETWEEN 3 AND 0. COULD NOT DUPLICATE. NO FAULTS FOUND IN STABILIZER TRIM INDICATION. 2L72 4F RTA21EA 19950120002741995012000274EA 1995 1 20 COM60382 119950115A301014463101 DUCT CNDAIRCL600 CL6002B19 EA LT WING CRACKED A COMAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CRCRUISE 1 SO01924CA3261 7026 ANTI-ICE DUCT WARNING MESSAGE CAME ON DURING CLIMB. REPLACED THE LT WING OUTBD SECTION BLEED AIR ANTI-ICE DUCT, WHICH WAS FOUND CRACKED. 2L72 4F RTA21EA 19950120002751995012000275NM 1995 1 20 QXEA9500016 119950116A3260066401800 PSEU DHAV DHC8 DHC8102 2809003NM LANDING GEAR DEFECTIVE A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09815PH4349712283 50 BLI - THE WOW LIGHT ILLUMINATED IN FLIGHT AFTER GEAR EXTENSION AND THEN WENT OUT PRIOR TO TOUCH DOWN. PERFORMED PSEU TARGET TEST GOOD, INSPECTION PROX SENSOR GAPS AND WIRING IN ALL WHEEL WELLS. COMPLIED WITH RETRACTION AND EXTENSION TESTS AND COULD NOT DUPLICATE THE PROBLEM. REMOVED AND REPLACED THE PSEU AND COMPLIED WITH A BITE TEST. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950120002761995012000276NM 1995 1 20 QXEA9500018 119950116A3231 RETRACT MECH DHAV DHC8 DHC8102 2809003NM RT MLG DOOR OBSTRUCTED A QXEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09102AV 91 PDX - THE RT YELLOW MAIN GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED THE GEAR HANDLE DOWN LEFT MAIN AND NOSE GEAR WENT DOWN AND LOCKED. RT MAIN RED UNSAFE LIGHT REMAINED ILLUMINATED WITH NO GREEN DOWN AND LOCKED AND INDICATED UNSAFE BY ALTERNATE MEANS. REMOVED OBSTRUCTION FROM RT FORWARD GEAR DOOR HINGE ARM PATH. GEAR OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950120003061995012000306NM 1995 1 20 UPS201936 119950114A326063200036 DOOR SWITCH BOEING727 72725C 138400HNM RT MLG DOOR MALFUNCTION A IPXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01932UP 19857 PILOT REPORTED RT GEAR DOOR LIGHT ON WITH HANDLE IN OFF POSITION. CYCLED GEAR, NO HELP. REMOVED AND REPLACED MAIN GEAR DOOR WARNING SWITCH IAW MM 32-62-11, OPS CHECK NORMAL. 2L73 4F A3WE 19950120003071995012000307NM 1995 1 20 UPS201963 119950117A5330 SKIN BOEING727 727185C 138406NNM BS 475-480 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND FASTENERS AT BS 475-480 LEAKING AND SKIN PILLOWING BETWEEN STR 7 AND 6L. INSTALLED REPAIR IAW SRM 53-30-3, 51-30-2, 51-10-6, 51-10-2, AND MM 51-20-00. 2L73 4F A3WE 19950120003081995012000308NM 1995 1 20 UPS201964 119950117A5753 FOREFLAP BOEING727 727185C 138406NNM RT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND R/W O/B FOREFLAP I/B END HAS A PREVIOUS REPAIR DELAMINATING. INSTALLED REPAIR IAW SRM 51-40-06. 2L73 4F A3WE 19950120003091995012000309NM 1995 1 20 UPS201965 119950117A5543 TAB BOEING727 727185C 138406NNM RUDDER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND UPPER RUDDER TAB UPPER CLOSURE WEB DELAMINATED. INSTALLED REPAIR IAW SRM 51-40-9 AND 51-30-2. 2L73 4F A3WE 19950120003101995012000310NM 1995 1 20 UPS201966 119950117A53206518442 DOOR WAY BOEING727 727185C 138406NNM MID GALLEY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND MID GALLEY DOOR WAY, UPPER FORWARD CORNER REVEAL CRACKED OUT OF FASTENER HOLE. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, AND MM 51-20-151. 2L73 4F A3WE 19950120003111995012000311NM 1995 1 20 UPS201967 119950117A5210 LINER BOEING727 727185C 138406NNM FWD ENTRY DOOR CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND FORWARD ENTRY DOOR UPPER FORWARD LINER SUPPORT PAN L-ANGLE CRACKED. INSTALLED REPAIR IAW SRM 51-20-1, 51-10-2, 51-30-2. 2L73 4F A3WE 19950120003121995012000312NM 1995 1 20 UPS201968 119950117A523069191705 WEB BOEING727 727185C 138406NNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKED WEB ON AFT CARGO DOOR AT AFT HINGE ON BOTH FWD AND AFT SIDE OF HINGE ATTACHMENTS. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-4, 51-30-5, AND MM 51-20-21, 51-20-151. 2L73 4F A3WE 19950120003131995012000313NM 1995 1 20 UPS201969 119950117A523069191704 WEB BOEING727 727185C 138406NNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKED WEB ON AFT CARGO DOOR AT FWD HINGE ON FWD SIDE OF HINGE ATTACHMENT. INSTALLED REPAIR IAW SRM 51-30-5, 51-30-2 AND 51-20-4. 2L73 4F A3WE 19950120003141995012000314NM 1995 1 20 UPS201970 119950117A5320 LONG BEAM BOEING727 727185C 138406NNM FS 754-757 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AT STA 754-757 RBL 45.75 WL 203 ON LONGITUDINAL BEAM LOWER FLANGE. INSTALLED REPAIR IAW SRM 51-40-4, 51-30-2. 2L73 4F A3WE 19950120003151995012000315NM 1995 1 20 UPS201971 119950117A532069348161 EXPANSION LINK BOEING727 727185C 138406NNM FS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND FWD EXPANSION LINK ATTACH FITTING CORRODED STA 740 RBL 45 WL 207-201. 2L73 4F A3WE 19950120003161995012000316NM 1995 1 20 UPS201972 119950117A532065263074 TRANS BEAM BOEING727 727185C 138406NNM BS 1215 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND FWD CORROSION ON LOWER TRANSVERSE BEAM BS 1215 RBL 21 LBL 21 WL 174. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-2, 51-20-151. 2L73 4F A3WE 19950120003171995012000317NM 1995 1 20 UPS201973 119950117A5320 TRANS BEAM BOEING727 727185C 138406NNM BS 1215 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND O/B UPPER TRANSVERSE BEAM INSIDE TORQUE BOX TO BE CORRODED BS 1215 RBL23 WL 174. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-4. 2L73 4F A3WE 19950120003181995012000318NM 1995 1 20 UPS201974 119950117A5320 TRANS BEAM BOEING727 727185C 138406NNM BS 1215 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LEFT UPPER TRANSVERSE BEAM (O/B) BS 1215 WL 174 LBL 17. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950120003191995012000319NM 1995 1 20 UPS201975 119950117A5320 VERTICAL STIFF BOEING727 727185C 138406NNM BS 1215 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND VERTICAL STIFFENER AT BS 1215 RBL 21 WL 173-169 TO BE CORRODED. INSTALLED REPAIR IAW 51-30-2. 2L73 4F A3WE 19950120003201995012000320NM 1995 1 20 UPS201976 119950117A5320 TRANSVERSE BEAM BOEING727 727185C 138406NNM BS 1215 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LOWER TRANSVERSE BEAM BS 1215 RBL 21-23 WL 174. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-20-4, AND MM 51-20-151. 2L73 4F A3WE 19950120003211995012000321WP 1995 1 20 UPS801956 119950117A523037549301N FITTING DOUG DC8 DC873F 302199FWP SLIDE DOOR CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON C X-SLIDE DOOR NR 1 AND NR 4 LOWER T-BOLT BACK UP FITTINGS. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950120003221995012000322WP 1995 1 20 UPS801957 119950117A5347S295597812000 TIE DOWN TRACKS DOUG DC8 DC873F 302199FWP FS80-260 360-450CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LOWER CARGO TIE DOWN TRACKS AT FS 80-260, LBL 36 AND FS 360-450, RBL 36. INSTALLED REPAIR IAW SRM 51-3-0. 2L74 4F RT4A25 19950120003231995012000323WP 1995 1 20 UPS801958 119950117A53203755822505N FITTING DOUG DC8 DC873F 302199FWP FS 339 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION AT B/T FITTING FS 339 BETWEEN LONG 33L-34L. INSTALLED REPAIR IAW SRM 53-2-0, PAGE 13 AND 14. 2L74 4F RT4A25 19950120003241995012000324WP 1995 1 20 UPS801959 119950117A532037502571 SPLICE DOUG DC8 DC873F 302199FWP FS 600-620 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONG 31L SPLICE FITTING FS 600-620. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950120003251995012000325WP 1995 1 20 UPS801960 119950117A53203755822505N FITTING DOUG DC8 DC873F 302199FWP FS 301 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION ON B/T FITTING, FWD AND AFT SIDES BETWEEN LONG 28L-29L, FS 301. INSTALLED REPAIR IAW SRM 53-2-0, FIG. 2D. 2L74 4F RT4A25 19950120003261995012000326WP 1995 1 20 UPS801961 119950117A53200327075T6 FINGER DOUBLER DOUG DC8 DC873F 302199FWP FS 275 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER SECTION ABOVE LONG 30L, FS 275. INSTALLED REPAIR IAW SRM 53-2-0. 2L74 4F RT4A25 19950120003271995012000327WP 1995 1 20 UPS801962 119950117A57445751189 SUPPORT FITTING DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01851UP 46051 WHILE IN 'C' CHECK, MAINTENANCE FOUND LEFT WING FLAP HINGE SUPPORT FITTING CRACKED AT STA 409, INBD FITTING. INSTALLED REPAIR IAW DOUGLAS DRAWING B/P 5751189. 2L74 4F RT4A25 19950120003771995012000377WP 1995 1 20 9500919967 119950113A5744 FITTING DOUG DC9 DC931 3022065WP LT SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING LINE CHECK, FOUND CRACK IN INBOARD SPOILER FITTING LEFT WING. REPLACED FITTING. 2L72 4F A6WE 19950120003781995012000378WP 1995 1 20 9500929856 119950113A5330 SKIN DOUG DC9 DC951 3022051WP FS 1185 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01765NC 47718 DURING PERIODIC CHECK, FOUND OIL CANNING IN FUSELAGE SKIN FS 1185, LONGERONS 16L - 17L AND 17R - 18R. REPAIRED PER EA 98-094269. 2L72 4F A6WE 19950120003791995012000379WP 1995 1 20 9500939945 119950113A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CORROSION IN FS 110 BULKHEAD TUNNEL AT LONGERON 27R, 6 INCHES UP FROM BOTTOM CORNER. REPAIRED PER XEA X9-53-50. 2L72 4F A6WE 19950120003801995012000380WP 1995 1 20 9500949872 119950113A7120 FITTING DOUG DC9 DC951 3022051WP ENGINE SUPPORT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND RUST BLEEDING FROM BETWEEN PYLON SKIN AND FORWARD ENGINE MOUNT SUPPORT (BEAVERTAIL) FITTINGS, UPPER AND LOWER. REPLACED BOTH FITTINGS PER DWG 9958161. 2L72 4F A6WE 19950120003811995012000381WP 1995 1 20 9500959876 119950113A5400 WEB DOUG DC9 DC951 3022051WP LT PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01785NC 48110 DURING LINE CHECK, FOUND .75 INCH CRACK IN WEB JUST AFT OF FORWARD ENGINE MOUNT. REPAIRED PER EA 98-087982. 2L72 4F A6WE 19950120003821995012000382WP 1995 1 20 9500969872 119950116A5330 SKIN DOUG DC9 DC951 3022051WP FS 674-693 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 674 - 693, LONGERONS 29L - 28R. REPAIRED PER EA 98-096164. 2L72 4F A6WE 19950120003831995012000383NM 1995 1 20 9500975525 119950104A5330146N3511 SKIN BOEING757 757251 1384970NM FS 1300-1400 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01525US 25521 23619 DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN FROM FS 1300 - 1400, STR 26L TO 26R WAS FOUND WITH NICKS AND SCRATCHES CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER NWA EA 55-093699. 2L72 4F RTA2NM 19950120003841995012000384NM 1995 1 20 9500985525 119950104A5330 SKIN BOEING757 757251 1384970NM FS 1401-1430 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01525US 25521 23619 DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN FROM FS 1401 TO 1430, STR 27L TO 29L WAS FOUND WITH NICKS AND SCRATCHES CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER NWA EA 55-96317. 2L72 4F RTA2NM 19950120003851995012000385WP 1995 1 20 9500999856 119950113A5350 LATCH LEVER DOUG DC9 DC951 3022051WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01765NC 47718 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ALSO, FOUND THAT THE CLEVIS PIN HOLE WAS WORN IN THE UPPER LEFT LATCH LEVER. REPLACED THE LATCH LEVER AND RERIGGED THE RELEASE MECHANISM. 2L72 4F A6WE 19950120003861995012000386WP 1995 1 20 9501009959 119950116A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING LINE CHECK EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS. REMOVED PRIMER FROM THE BALL END OF THE CABLE AND ADJUSTED THE CLIPS. CHECKED OK. 2L72 4F A6WE 19950120003871995012000387NM 1995 1 20 9501012711 119950110A53306518420482 SKIN BOEING727 7272S7 138407ZNM FS 303 DENTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01715RC 22019 DURING PERIODIC CHECK, MAINTENANCE FOUND LARGE DENT FORWARD OF MAIN CABIN DOOR AT FS 303, STR 7L. REPAIRED PER NWA EA 27-096165. 2L73 4F A3WE 19950120003881995012000388EU 1995 1 20 9501023211 119950116A3260 INDICATION AIRBUS320 A320211 3930320EU LT MLG DOOR MALFUNCTION A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01311US 125 DURING CLIMB-OUT FROM MKE AFTER LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE FULLY CLOSED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED AND LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2L72 4F RTA28NM 19950120003891995012000389WP 1995 1 20 9501039154 119950117A5330 SKIN DOUG DC9 DC914 3022034WP FS 846-896 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018913E 45830 DURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN APPROXIMATELY 9 INCHES BELOW THE LEFT PYLON AT FS 846 AND FS 896. REPAIRED BOTH PER EA 91-094921. 2L72 4F A6WE 19950120003901995012000390WP 1995 1 20 9501049154 119950117A5350 CLIPS DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018913E 45830 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS. RERIGGED TAILCONE. CHECKED OK. 2L72 4F A6WE 19950120003911995012000391WP 1995 1 20 9501059156 119950117A5210 DOOR TRIM DOUG DC9 DC914 3022034WP MAIN CABIN DOOR INTERFERENCE A NWAAK NONE O OTHER ININSP/MAINT 1 GL018915E 45832 AFTER ARRIVAL ATL-DTW, THE MAIN CABIN DOOR WOULD NOT OPEN AT THE JETWAY WITHOUT EXTERNAL ASSISTANCE. FOUND DOOR TRIM INTERFERING WITH THE DOOR STOP. REPAIRED TRIM AND REMOVED BURR FROM THE DOOR STOP. CHECKED OK. 2L72 4F A6WE 19950120003921995012000392WP 1995 1 20 ABXA9500005 119950113A52805910557504 DOOR DOUG DC9 DC931 3022065WP RT MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEVEL I CORROSION ON THE INTERIOR FLANGES OF THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR. LINK AND ARM ASSEMBLIES HAD EXCESSIVE PLAY. REPLACED RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950120003931995012000393WP 1995 1 20 ABXA9500006 119950110A53125910163185 WEB DOUG DC9 DC932F 3022067WP FS 996 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND DENT IN LEFT P-DOME SKIN AT APPROXIMATELY THE 10:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10728-MR. 2L72 4F A6WE 19950120003941995012000394WP 1995 1 20 ABXA9500007 119950109A53125910163185 WEB DOUG DC9 DC932F 3022067WP FS 996 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 2:00 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR. 2L72 4F A6WE 19950120003951995012000395WP 1995 1 20 ABXA9500008 119950109A53125910163185 WEB DOUG DC9 DC932F 3022067WP FS 996 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND TWO DENTS IN RIGHT P-DOME SKIN BETWEEN THE 2:00 AND 3:00 O'CLOCK POSITIONS. REPAIRED DENTS IAW ABX REA D95310735-MR. 2L72 4F A6WE 19950120003961995012000396WP 1995 1 20 ABXA9500009 119950109A53125910163185 WEB DOUG DC9 DC932F 3022067WP FS 996 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND P-DOME DENTED AT APPROXIMATELY THE 12:30 O'CLOCK POSITION. REPAIRED DENT IAW ABX REA D953-10735-MR. 2L72 4F A6WE 19950120003971995012000397WP 1995 1 20 ABXA9500010 119950110A53125910163183 WEB DOUG DC9 DC932F 3022067WP FS 996 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK, INSPECTION FOUND DRILL STARTS IN LEFT P-DOME SKIN WEB. REPAIRED IAW ABX REA D953-10713-MR. 2L72 4F A6WE 19950120003981995012000398WP 1995 1 20 ABXA9500011 119950110A531159203401 FRAME DOUG DC9 DC932F 3022067WP FS 617 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND DRILL STARTS IN FRAME 617 BETWEEN LONGERONS 9L AND 10L. REPAIRED IAW ABX REA D953-10744-MR. 2L72 4F A6WE 19950120003991995012000399WP 1995 1 20 ABXA9500012 119950109A53115920340503 FRAME DOUG DC9 DC932F 3022067WP FS 658 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND DRILL START ON FRAME 658 AT LONGERON 7L. REPAIRED IAW ABX REA D953-10731-MR. 2L72 4F A6WE 19950120004051995012000405WP 1995 1 20 ABXA9500020 119950107A52805910557135 DOOR DOUG DC9 DC932F 3022067WP LT MLG DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR DELAMINATED. REPLACED OUTBOARD ARTICULATING DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6 AND DC-9 MM 32-12-1. 2L72 4F A6WE 19950120004061995012000406WP 1995 1 20 ABXA9500021 119950107A52805910557110 DOOR DOUG DC9 DC932F 3022067WP RT MLG DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED. REPLACED THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950120004071995012000407WP 1995 1 20 ABXA95013 119950111A53115920338503 FRAME DOUG DC9 DC932F 3022067WP FS 756 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND DRILL START IN FRAME 756 JUST ABOVE LONGERON 10R. REPAIRED IAW ABX REA D953-10729-MR. 2L72 4F A6WE 19950120004091995012000409NM 1995 1 20 DL72L950165 119950105A5330 SKIN BOEING727 727232 1384082NM FS 450-460 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 AT HMV, FOUND DENT IN FUSELAGE SKIN BETWEEN STA 450-460 AND STR 17R AND 18R. ROUTED OUT DAMAGE PER SRM 53-30-3. 2L73 4F A3WE 19950120004101995012000410NM 1995 1 20 DL72L950166 119950103A5311 FRAME BOEING727 727232 1384082NM FS 700 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 AT HMV, FOUND FRAME 700 CRACKED BETWEEN STR 22 AND 23 R. FABRICATED PARTS AND REPAIRED DAMAGE PER SRM 53-10-4. 2L73 4F A3WE 19950120004111995012000411NM 1995 1 20 DL72L950169 119950103A5713 LONGERON BOEING727 727232 1384082NM WS 868.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND RIGHT WING UPPER STRINGER NR 10 AT STA 686.5 CRACKED AT THE STRINGER TO RIB ATTACH FASTENER HOLE. REPAIRED PER MM 57-13-0. 2L73 4F A3WE 19950120004131995012000413NM 1995 1 20 DL72L950172 119950103A5713 LONGERON BOEING727 727232 1384082NM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND RIGHT WING UPPER STRINGER NR 13 WITH A CRACK AT FASTENER HOLE AT ATTACH POINT TO WING RIB AT WS 629. REPAIRED PER MM 57-13-0. 2L73 4F A3WE 19950120004141995012000414NM 1995 1 20 DL72L950173 119950103A5713 LONGERON BOEING727 727232 1384082NM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND RIGHT WING UPPER STRINGER CRACKED AT STRINGER TO RIB ATTACH HOLE AT WS 629. REPAIRED PER MM 57-13-0. 2L73 4F A3WE 19950120004151995012000415NM 1995 1 20 DL72L950174 119950102A5311 FRAME BOEING727 727232 1384082NM FS 1148 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND FRAME AND SKIN CLIPS CORRODED AT FS 1148 AT STR 28L-30. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950120004161995012000416NM 1995 1 20 DL72L950187 119950106A5320651751737 STIFFINERS BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING INSPECTION (L/C), THE RT TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS AT FS 1263. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4. 2L73 4F A3WE 19950120004171995012000417NM 1995 1 20 DL72L950192 119950104A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING HMV, FOUND NR 7 L/E SLAT ACT ATTACH RIBS CRACKED AT LWR FWD RADIUS. FABRICATED PART AND REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950120004181995012000418NM 1995 1 20 DL72L950205 119950108A57536521631326 LE SKIN BOEING727 727232 1384082NM NR 4 FORE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 AT HMV, SHOP INSPECTION THE RIGHT WING NR 4 FORE FLAP HAS FOUND WITH WEAR DAMAGE ON THE LEADING EDGE SKIN AT 29 INCHES FROM THE OUTBOARD END OF FLAP. REPAIRED DAMAGE PER SRM 57-50-4. 2L73 4F A3WE 19950120004191995012000419NM 1995 1 20 DL72L950206 119950108A57536521631326 LE SKIN BOEING727 727232 1384082NM NR 4 FORE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 AT HMV SHOP INSPECTION, THE RIGHT WING NR 4 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO THE LEADING EDGE SKIN AT 86 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 5750-4. 2L73 4F A3WE 19950120004201995012000420NM 1995 1 20 DL72S950190 119950105A5320 STIFFENERS BOEING727 727232 1384082NM FS 1263/1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS/BEAMS CRACKED AT BOTH FS 1263 AND FS 1273. THE DAMAGED PART WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129, REV 4. 2L73 4F A3WE 19950120004211995012000421NM 1995 1 20 DL72S950194 119950111A575465162255A KRUGER FLAP BOEING727 727232 1384082NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 DURING SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 KRUGER FLAP NEAR THE I/B HINGE. REPAIRED CRACK PER SRM 57-50-3. 2L73 4F A3WE 19950120004221995012000422NM 1995 1 20 DL72S950214 119950102A524165561502 CENTER FRAME BOEING727 727232 1384082NM GALLEY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11521DA 21472 DURING SHOP INSPECTION, THE AFT CENTER FRAME ON FWD GALLEY DOOR WAS FOUND CRACKED. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950120004231995012000423NM 1995 1 20 DL72S950215 119950104A711065196854539 NOSE COWL BOEING727 727232 1384082NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE AFT LIP WORN TO A KNIFE EDGE AT THE 6:30 TO 7:30 POSITION. REPAIRED PER SRM 54-10-3. 2L73 4F A3WE 19950120004241995012000424NM 1995 1 20 DL72S950216 119950110A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 DURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT WAS FOUND WITH INTERNAL SUPPORT RIBS NR 7 AND NR 9 CRACKED. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950120004251995012000425NM 1995 1 20 DL72W950182 119950104A57536521631273A FOREFLAP BOEING727 727247 138408FNM LEFT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 NR 1 LT OB FOREFLAP HAS WORN AREA 98 INCHES FROM OB END ON LEADING EDGE, FOUND THIS DURING HMV SHOP INSPECTION. REPAIRED PER SRM 57504. 2L73 4F A3WE 19950120004261995012000426NM 1995 1 20 DL72W950183 119950108A57536521631273A LE SKIN BOEING727 727247 138408FNM NR 1 FORE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 NR 1 LT OB FORE FLAP HAS CRACK JUST FORWARD OF OB CUP, FOUND THIS DURING HMV SHOP INSPECTION. REPAIRED PER SRM 57504. 2L73 4F A3WE 19950120004271995012000427NM 1995 1 20 DL72W950184 119950108A57536521631273A LE SKIN BOEING727 727247 138408FNM NR 1 FORE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 NR 1 LT OB FOREFLAP HAS WEAR ON LEADING EDGE 54 INCHES FROM OB END, FOUND THIS DURING HMV SHOP INSPECTION. REPAIRED PER SRM 57504. 2L73 4F A3WE 19950120004281995012000428NM 1995 1 20 DL72W950188 119950112A5320 MLG PRESS DECK BOEING727 727247 138408FNM FS 940-950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING ROUTINE INSPECTION AT HMV, THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL PRESSURE DECKS WERE FOUND TO HAVE APPROXIMATELY ONE INCH LONG CRACKS AT STATION 949 AND BL 60 (ONE CRACK ON EACH SIDE). THE CRACKS ARE ON THE AFT END OF THE BEADS BETWEEN STA 940 AND 950 IN EACH CASE. THE CRACKS WILL BE REPAIRED PER BACO MODIFICATION 65-89360-135. 2L73 4F A3WE 19950120004291995012000429NM 1995 1 20 DL72W950198 119950105A5311 FRAME BOEING727 727247 138408FNM FS 660 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AT HMV, FOUND FRAME FS 660 CRACKED ABOVE LT FIXED FLOOR. REPAIRED PER SRM 53-10-4, PG 21. 2L73 4F A3WE 19950120004311995012000431NM 1995 1 20 DL733950212 119950104A5754 LE SLAT BOEING737 737347 1384647NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 AT HMV, FOUND NR 5 LEADING EDGE SLAT CRACKED ON BOTTOM ALONG FASTENERS. REPAIRED PER SRM 57-43-01 FIG 205. 2L72 4F RTA16WE 19950120004321995012000432NM 1995 1 20 DL733950213 119950110A5522 SKIN BOEING737 737347 1384647NM LT ELEVATOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 DURING HMV, FOUNG SMALL PUNCTURE AND FIBER DAMAGE IN LEFT ELEVATOR UPPER SURFACE. LOCATED 3 FEET FROM INBOARD AND 7 INCHES FROM SPAR AFT. REPAIRED ELEVATOR PUNCTURE PER SRM 55-20-01 IN REF TO 51-70-17. 2L72 4F RTA16WE 19950120004331995012000433NM 1995 1 20 DL73S950161 119950113A3350BPS73 EEL RACK BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11311DL 23083 DURING INSPECTION, FOUND AFT CABIN FLOOR EMERGENCY TRACK LIGHTS INOP. REPLACED RACK M9222, OPERATION NORMAL. 2L72 4F RTA16WE 19950120004341995012000434NE 1995 1 20 DL757950191 219950116A72615007436C PUMP BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A DALAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SO11645DL 24216 716559 DURING CRUISE, NR 2 ENGINE OIL QUANTITY STEADILY DECREASED. INSPECTION OF NR 2 OIL SYSTEM FOUND THE ENGINE SCAVANGE OIL PUMP WITH A CRACKED PUMP CASE. REPLACED OIL PUMP, OPERATION NORMAL. 2L72 4F4 FRTA2NM E17NE 19950120004351995012000435NM 1995 1 20 DL757950197 119950112A5320 INTERCOSTAL BOEING757 757232 1384965NM FS 365 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 DURING LETTER CHECK K1, FOUND INTERCOSTAL STRAP CRACKED FS 365 IN E/E COMPT RT TUNNEL. REPAIRED PER M/M 53-01-04-8. 2L72 4F RTA2NM 19950120004361995012000436NM 1995 1 20 DL757950200 119950112A5320 INTERCOSTAL BOEING757 757232 1384965NM FS 365 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 DURING LETTER CHECK K1, FOUND INTERCOSTAL STRAP CRACKED FS 365 IN E/E COMPT LT TUNNEL. REPAIRED PER M/M 53-01-04-8. 2L72 4F RTA2NM 19950120004371995012000437NM 1995 1 20 DL757950202 119950112A5321 FLOOR PANEL BOEING757 757232 1384965NM MID GALLEY DEFECTIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 DURING LETTER CHECK K1, FOUND MID GALLEY FLOOR HAS SOFT SPOT LEFT CENTER BETWEEN OVENS. REPAIRED FLOOR PANEL PER SRM 53-00-50. 2L72 4F RTA2NM 19950120004381995012000438NM 1995 1 20 DL76L950195 119950114A2780849704 CARD BOEING767 767332 1382001NM PSEU FAULTY A DALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO11179DN 25144 ON APPLICATION OF TAKEOFF POWER HAD TAKEOFF WARNING, L/E SLAT ASSYMETRY. REJECTED TAKEOFF, RETURNED TO BLOCK. TROUBLESHOOTING FOUND PSEU HAS CARD 012 FAULT, TEST 503/507. REPLACED CARD OPERATION NORMAL WITH SYSTEMS CRITICAL TO ETOPS. 2L72 4F RTA1NM 19950120004391995012000439NE 1995 1 20 DL76L950219 219950114A7200PW4060 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO11178DN17410 25143 724149 ON PUSHBACK, DURING ENGINE START DID NOT HAVE N2 ROTATION. RETURNED TO BLOCK. STARTER AND TRANSMISSION TOWER SHAFT WAS REMOVED DURING TROUBLESHOOTING. DETERMINATION WAS MADE TO REPLACE ENGINE FOR RETURN TO SERVICE AND CONTINUE TROUBLESHOOTING STARTER AND TRANSMISSION PROBLEMS ON GROUND. 2L72 4F4 FRTA1NM E24NE 19950120004401995012000440NE 1995 1 20 DL76L950220 219950117A7230PW4060 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TOTAKEOFF 1 SO11178DN7500 25143 724686 DURING TEST FLIGHT FOR ETOPS ENGINE CHANGE ACCEPTANCE, NR 2 ENGINE HAD COMPRESSOR STALLS ON TAKEOFF. RETURNED CPH. ENGINE WAS REMOVED AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19950120004411995012000441WP 1995 1 20 DLL16950090 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1715 UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 1715 BETWEEN STRINGERS 44 AND 45. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950120004421995012000442WP 1995 1 20 DLL16950112 119950105A5320 THRESHOLD LKHEED1011 10113853 5265020WP R-2 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, THE R-2 DDOR THRESHOLD WAS FOUND CORRODED AT THE AREAS EXPOSED BY REMOVAL OF THE FWD AND AFT ATTACH FITTING. CHECKED LIMITS AND REPAIRED PER SRM 53-15-00 FIG 808. 2L73 4F A23WE 19950120004431995012000443WP 1995 1 20 DLL16950185 119950102A57531529112109 SKIN LKHEED1011 10113853 5265020WP LT FLAP VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 NR 1 LEFT FLAP VANE UPPER SKIN CRACKED IN TWO PLACES UNDER BOTH RUB STRIPS. REMOVED DAMAGED SKIN SECTION, MFG AND INSTALLED SPLICE REPAIR AND DOUBLERS PER SRM 57-53-00 FIG 815. DAMAGE FOUND AT HMV. 2L73 4F A23WE 19950120004441995012000444WP 1995 1 20 DLL16950186 119950105A5330 SKIN LKHEED1011 10113853 5265020WP FS 729-846 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRP DISBONDED AT FS 746 AND 846 BETWEEN STRINGERS 34 AND 36, ALSO AT FS 729 AND FS 846 BETWEEN STRINGERS 32-31. REPAIRED PER SRM 53-31-0 FIG 816 AND FIG 804. 2L73 4F A23WE 19950120004451995012000445WP 1995 1 20 DLL16950189 119950110A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND HORIZONAL TRUSS MEMBER AT LT FS 1103, CRACKED UPPER TAB. REPAIRED PER SRM 53-21-00 PAGES 853-855. 2L73 4F A23WE 19950120004461995012000446WP 1995 1 20 DLL16950196 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 699 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED AT FS 699 BL-36R. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950120004471995012000447WP 1995 1 20 DLL16950201 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 699 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND TEAR STRAP DISBONDED AT FS 699 BL-14L AND BL-6L. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950120004481995012000448WP 1995 1 20 DLL16950203 119950105A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 903/923 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND TEAR STRAP DELAMINATED BETWEEN FS 903 AND 923 BETWEEN STR 28 AND 29. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950120004491995012000449WP 1995 1 20 DLL16950204 119950105A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1675 UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND TEAR STRAP UNBONDED AT FS 1675 BETWEEN STR 44 AND 45. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950120004501995012000450NM 1995 1 20 DLM88950199 119950105A71105930645505 NOSE COWL DOUG MD88 MD88 3023688NM LT ENGINE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11906DE 53415 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE OUTER SKIN OF ACOUSTIC PANEL DELAMINATED OVER AN 8 INCH BY 20 INCH AREA AT THE 6 O'CLOCK POSITION. REPAIRED DAMAGE PER SRM 54-04. 2L72 4F RTA6WE 19950120004511995012000451SW 1995 1 20 QXEA9500019 119950117A2160BYLB504371 MIXING VALVE SWRNGNSA227 SA227AC 8780603SW NR 1 BLEED AIR MALFUNCTION A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM092727B10035 AC730 PDX - NR 1 BLEED AIR UNCONTROLLABLY HOT WITH SMOKE IN THE CABIN. REMOVED AND REPLACED THE LT MIXING VALVE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950120004521995012000452SW 1995 1 20 QXEA9500020 119950117A32302719248001 SPRING SWRNGNSA227 SA227AC 8780603SW LT MLG WORN A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09382PH AC589 SEA - LT GEAR INTRANSIT LIGHT REMAINED ON. 1L72 4T A8SW 19950120004951995012000495SO 1995 1 20 95ZZZX375 119950103A7170EU40744A3 LINE GULSTMG1159 G1159A 3970109SO RROYCESPEY SPEY5118 54523EU FUEL DRAIN LEAKING A IMKAK NONE K FLUID LOSS ININSP/MAINT 1 EA2582A 342 11097 DURING AN INSPECTION OF THE LT ENGINE, FOUND FUEL DRAIN LINE LEAKING. ORDERED NEW LINE FROM GULFSTREAM AEROSPACE. DURING THE RECEIVING INSPECTION, FOUND FLARED END OF LINE BY B-NUT CORRODED AND MISSING MATERIAL DUE TO PITTING. NOTE: THE LINE WAS A NEW UNIT MFG 11/89 AND RECEIVED 12/29/94 FROM GACSPARES. ANOTHER LINE WAS ORDERED AND RECEIVED WITH NO DISCREPANCIES. THE LINE WAS INSTALLED, ENGINE RUN AND LEAK CHECK WAS ACCOMPLISHED WITH NO DISCREPANCIES. ALL WORK ACCOMPLISHED PER MM. AIRCRAFT RETURNED TO SERVICE. OPER CONTROL NR 949069. 2L72 4F4 F A12EA E2EU 19950120005381995012000538EU 1995 1 20 VTZA95001 119950101A7603745162403 POWER CABLE JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILURE A VTZAO OTHER O OTHER CRCRUISE 1 EA27306UE 41020 DAY-IAD - FLT 6942 - DURING CRUISE, THE RT ENGINE TELEFLEX CABLE FROZE IN FLIGHT. UNABLE TO MOVE POWER LEVER. ACFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT POWER CABLE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950120005391995012000539EU 1995 1 20 VTZA95002 119950101A3310HWB111044INS CONNECTOR BAG JETSTMJETSTM3201 1500217EU COCKPIT LOOSE A VTZAO OTHER O OTHER CLCLIMB 1 EA27472UE 823 IAD-CLT - FLT 6297 - DURING CLIMB, THE LT SKIRT PANEL LIGHTS FLICKERED AND THEN EXTINGUISHED SHORTLY AFTER TAKEOFF. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENT. MAINTENANCE RESECURED ALL CONNECTORS ON SKIRT PANEL AND OPS CHECK GOOD. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950120005401995012000540EU 1995 1 20 VTZA95003 119950102A2130137307L483 STATIC LINE BAG JETSTMJETSTM3201 1500217EU FUSELAGE KINKED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27481UE 895 IAD-BUF - FLT 6314 - DURING FLIGHT, COULD NOT CONTROL PRESSURIZATION IN FLIGHT. ACFT DID AN EMERGENCY DESCENT DURING FLIGHT, AND RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED A KINKED STATIC LINE AT OUTFLOW CONTROL VALVE. ACFT WAS RELEASED AND APPROVED FOR SERVICE. (W) 2L72 4T RTA56EU 19950120005411995012000541EU 1995 1 20 VTZA95004 119950102A5270 DOOR WARNING JETAIRJETSTMJETSTM4101 1500501EU BAGG COMPT ILLUMINATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27303UE 41015 MHT-IAD - FLT 6226 - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 06261 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. (W) 2L72 4T RTA41NM 19950120005421995012000542EU 1995 1 20 VTZA95005 119950103A5270 DOOR WARNING JETAIRJETSTMJETSTM4101 1500501EU BAGG COMPT ILLUMINATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27314UE 41027 IAD-PVD - FLT 6215 - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING ILLUMINATING. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI 40020 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. (W) 2L72 4T RTA41NM 19950120005431995012000543EU 1995 1 20 95ZZZZ14 119950103A36106124200 DUCT ASSY SAAB SF340 340B 7860101EU LT NACELLE FAILED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23321TH4808 232 340B321 AIRCRAFT RETURNED TO FIELD DUE TO THE LEFT UPPER DUCT HEAT FAIL LIGHT ILLUMINATED. THROUGH TROUBLESHOOTING THE LEFT UPPER DUCT WAS DETERMINED TO BE THE PROBLEM. THE DUCT ASSEMBLY WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM WAS PERFORMED WITH ALL INDICATIONS NORMAL. (Z) 2L72 4T RTA52EU 19950120005581995012000558EU 1995 1 20 AWXA9500027 119950113A3220MS172271 WASHER AIRBUS320 A320231 3930325EU NLG FAILED A AAWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 DURING SCHEDULED INSPECTION, FOUND KEY WASHER TANGS TO BE PROPERLY SECURED BUT KEY PORTION OF LOCK WASHER DEFECTIVE ALLOWING ROTATION OF NUT ON NOSE LANDING GEAR DOOR ACTUATOR LOWER ATTACHMENT FITTING BOLT. THE KEY PORTION OF THE LOCK WASHER IS NOT VISABLE WITHOUT REMOVING THE NUT. REMOVED AND REPLACED LOCK WASHER PER AMM 32-32-16 PP 404-407. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA28NM 19950120005681995012000568NM 1995 1 20 CAL950001 119950101A291065445101152 HYD LINE BOEING737 737130 1384435NM RT MLG WW CHAFED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0944214 19031 FLT NR 1680 - ORD - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATION SLOWLY DROPPED TO ZERO WHILE EN ROUTE FROM MCI TO MKE. THE AIRCRAFT WAS DIVERTED TO ORD. THE 'A' SYSTEM LOW PRESSURE LIGHTS BEGAN TO FLICKER ON AND OFF WHILE ON FINAL APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CHAFED HYDRAULIC LINE IN THE RIGHT WHEEL WELL. THE HYDRAULIC LINE IN THE RIGHT WHEEL WELL. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (Z) 2L72 4F A16WE 19950120005691995012000569NM 1995 1 20 CAL950004 119950103A2782654465116 ACTUATOR BOEING737 737291 138448WNM NR 6 LE SLAT INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091025113965 20361 FLT NR 1639 - PHL - THE AIRCRAFT WAS RETURNED TO PHL AFTER THE NR 6 LEADING EDGE SLAT FAILED TO RETRACT. MAINTENANCE FOUND THE NR 6 SLAT ACTUATOR STUCK IN THE DOWN POSITION. THE ACTUATOR WAS REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (Z) 2L72 4F A16WE 19950120005701995012000570NE 1995 1 20 CAL950010 219950103A7200 ENGINE BOEING737 737219 1384469NM PWA JT8 JT8D9 52048NE NR 2 MALFUNCTIONED A CALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0910248 20344 655281 FLT NR 1629 - ATL - THE NR 2 ENGINE OIL TEMPERATURE REACHED RED LINE WHILE EN ROUTE TO MSY. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (Z) 2L72 4F4 F A16WE E2EA 19950120005891995012000589EU 1995 1 20 VTZA95007 119950104A326091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR DIRTY A VTZAO OTHER N FALSE WARNING LDLANDING 1 EA27472UE 823 IAD-ALB - FLT 6372 - DURING APPROACH, DECLARED AN EMERGENCY DUE TO NO DOWN AND LOCKED INDICATION AFTER GEAR EXTENSION. ACFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBED MICROSWITCHES. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950120005901995012000590EU 1995 1 20 VTZA95008 119950105A326091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR FAILED A VTZAK NONE N FALSE WARNING APAPPROACH 1 EA27496UE 900 CLE-IAD - FLT 6548 - DURING APPROACH, HAD TO RECYCLE GEAR TO GET NOSE GEAR GREEN DOWNLOCK INDICATION. ACFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NOSE DOWNLOCK MICROSWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950120006061995012000606EU 1995 1 20 WTAA950012 119950102A3297622800200 WIRE BAG JETSTMJETSTM3101 1500215EU NLG WW BROKEN A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17425UE 798 SEA - THE NLG INTRANSIT INDICATION LIGHT REPORTED INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE ON NLG UPLOCK MICROSWITCH. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950120006071995012000607SO 1995 1 20 WTAA950013 119950103A5270MS250851 SWITCH EMB 120 EMB120RT SO PAX DOOR OUT OF ADJUST A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17454UE 120155 SFO - THE FWD DOOR WARNING LIGHT FAILS TO EXTINGUISH. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. ACFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE CLEARED DMI BY ADJUSTING FWD DOOR WARNING MICROSWITCH. (W) 2L72 4T RTA31SO 19950120006181995012000618WP 1995 1 20 AALA950025 119950109A2197 WIRE DOUG DC9 DC982 3022082WP CABIN TEMP IND CHAFED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW077540A 49994 ORD - FLT 1333 - AFTER LANDING ORD DURING ROLL-OUT, ELECTRICAL ARC AND SMOKE NOTICED FROM COCKPIT OVERHEAD PANEL. AIRCRAFT TAXI TO GATE WITHOUT INCIDENT. REPAIRED CHAFED WIRES TO CABIN TEMPERATURE INDICATOR IN OVERHEAD PANEL. PRECAUTIONARY REPLACED CABIN TEMPERATURE INDICATOR AND CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. AAL INSPECTED APPROXIMATELY 18 OTHER AIRCRAFT AND FOUND 50 PERCENT OF THOSE WITH THE SAME WIRING CHAFED TO VARIOUS DEGREES. (X) 2L72 4F A6WE 19950120006211995012000621NE 1995 1 20 C2XA95CL001 219950104A73103035729 FILTER 3035715 EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 ENGINE CONTAMINATED A C2XACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0916710 120106 EWR-EWR - FLT 3698 - ON TAKEOFF ROLL WITH TORQUE THROUGH 55-60 PERCENT, RIGHT ENGINE FUEL FILTER LIGHT ON OVERHEAD AND MASTER CAUTION FUEL LIGHT ON M.A.P. ILLUMINATED. TAKEOFF WAS ABORTED. AS POWER LEVERS WERE RETARDED, WARNING EXTINGUISHED. MAINTENANCE INSPECTED FILTERS FOR CONTAMINATION, NO DEFECTS NOTED. PLACED ON MEL 73-33-1, CONTROL NR 769810. ON R.O.N. IN BTV, MAINTENANCE REMOVED AND REPLACED NR 2 FUEL HEATER FILTER. OPS CHECK GOOD. REMOVED FROM MEL AND AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950120006361995012000636EU 1995 1 20 VTZA95009 119950102A527091SE6 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE BAY OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27303UE 41015 MHT-IAD - FLT 6226 - DURING TAKEOFF ON 1-2-95 AT 1930 HOURS, ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 06261 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 06261 ON 1-6-95 BY ADJUSTING THE BAGGGAGE DOOR FORWARD MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950120006371995012000637EU 1995 1 20 VTZA95010 119950106A302031998061 ANTI-ICE VALVE BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILURE A VTZALA ABORTED APPROACH UNSCHED LANDING O OTHER APAPPROACH 1 EA27473UE 828 IAD-PHF - FLT 6243 - DURING APPROACH AT 1715 HOURS ON 1-6-95, ABORTED APPROACH DUE TO LT ENGINE ANTI-ICE FAILED IN-FLIGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LT ENGINE ANTI-ICE VALVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950120006381995012000638 1995 1 20 VTZA95011 419950109A3421H321ASM1 STANDBY ADI BAG JETSTMJETSTM3201 1500217EU COCKPIT FAILURE A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27495UE 818 IAD-ROC - FLT 6452 - DURING CRUISE AT 1355 HOURS ON 1-9-95, RETURNED TO IAD DUE TO THE STANDBY ADI FAILING IN-FLIGHT. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED STANDBY ADI. (X) 2L72 4T RTA56EU 19950120006391995012000639EU 1995 1 20 VTZA95012 119950109A30609005EN38 UPLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27488UE 907 PIT-IAD - FLT 6328 - DURING CRUISE ON 1-9-95 AT 1050 HOURS, RETURNED TO PIT DUE TO THE NOSE GEAR INTRANSIT LIGHT NOT EXTINGUISHING AFTER GEAR WAS RETRACTED. AN IN-FLIGHT EMERGENCY WAS DECLARED. FLIGHT CREW RE-EXTENDED THE GEAR AND LANDED AT PIT WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND LUBED NOSE GEAR UPLOCK MICROSWITCH. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950120006401995012000640EU 1995 1 20 VTZA95013 119950111A79311186107150614 OIL PRESS TRANS BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27485UE 901 IAD-ROC - FLT 6365 - DURING CLIMB-OUT AT 0015 HOURS ON 1-11-95, THE LT ENGINE OIL TEMP FLUCTUATED IN-FLIGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED OIL PRESSURE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950130000011995013000001EU 1995 1 30 9501063232 119950113A71202380210505 THRUST LINK AIRBUS320 A320211 3930320EU NR 1 ENGINE WORN A ANWAAK NONE O OTHER ININSP/MAINT 1 GL01332NW 319 DURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-22-07. THE MAXIMUM DEPTH OF THE DAMAGED AREAS WAS 0.002 INCH. REPAIRED PER NWA EA 32-96336. 2L72 4F RTA28NM 19950130000021995013000002NM 1995 1 30 9501072204 119950117A3250 APEX PIN BOEING727 727251 138408HNM NOSE GEAR MISSING A ANWAAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL01204US 22544 ON LANDING ROLLOUT AT 100 KTS, AIRCRAFT VEERED TO THE LEFT AND BEGAN TO SHUDDER. MAINTENANCE INSPECTED AIRCRAFT ON RUNWAY AND FOUND NOSE GEAR TORSION LINK APEX PIN MISSING. TOWED OFF RUNWAY AND REPLACED APEX PIN. OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950130000031995013000003WP 1995 1 30 9501089873 119950113A32225910448 STRUT DOUG DC9 DC951 3022051WP NLG REQUIRED SERVICEA NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01782NC 48107 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM MOT. PUSHED GEAR HANDLE RELEASE BUTTON IN AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO DESTINATION (MSP) WITHOUT FURTHER INCIDENT. JACKED AIRCRAFT AND PERFORMED GEAR EXTENSION AND RETRACTION CHECK. NO PROBLEMS WERE FOUND. IT IS SUSPECTED THAT WATER WAS MIXED IN WITH NOSE GEAR STRUT FLUID. DRAINED FLUID AND SERVICED NOSE STRUT TO PROPER LEVELS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130000041995013000004WP 1995 1 30 9501099919 119950116A3231 MLG DOOR DOUG DC9 DC932 3022066WP LT MLG OPEN A NWAAO OTHER J WARNING INDICATION LDLANDING 1 GL01941N 47450 LEFT MAIN GEAR DOOR WAS OPEN ON LANDING INTO TUS. REPLACED THE LEFT MAIN GEAR DOOR SEQUENCE VALVE AND ACTUATOR DUE TO DAMAGE INCURRED. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130000051995013000005WP 1995 1 30 9501109139 119950118A3260 UNSAFE LIGHT DOUG DC9 DC914 3022034WP TR MLG ILLUMINATED A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01948L 47049 DURING APPROACH INTO CID, THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED GEAR, WIRING, AND SWITCHES. NO DISCREPANCIES FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130000061995013000006WP 1995 1 30 9501119163 119950114A2424939D2171 VOLTAGE REG DOUG DC9 DC914 3022034WP LT ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL018906E3301518315 45747 LEFT ENGINE GENERATOR DROPPED OFF LINE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND VOLTAGE REGULATOR FAULT SET ON LEFT GENERATOR CONTROL UNIT. REPLACED THE LEFT VOLTAGE REGULATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130000071995013000007NE 1995 1 30 9501121161 219950117A7530 EVC DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 3 ENGINE MALFUNCTIONED A NWAACE ABORTED TAKEOFF ENGINE SHUTDOWN JMRWARNING INDICATION OVER TEMP PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01161US 46770 686138 DURING TAKEOFF ROLL (AMS), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND BOROSCOPED. THE EVC WAS REPLACED AND A PRECISION TRIM WAS ACCOMPLISHED. GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. 2L73 4F4 F A22WE E20EA 19950130000081995013000008 1995 1 30 9501133220 419950104A3414 AIR SPEED IND AIRBUS320 A320211 3930320EU NR 1 PRIMARY MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01320US 213 DURING TAKEOFF ROLL, CREW NOTICED NO AIRSPEED INFORMATION ON THE NR 1 PRIMARY FLIGHT DISPLAY. THERE WERE NO ASSOCIATED WARNINGS OR ECAM MESSAGES. THE TAKEOFF WAS ABORTED AT 100 KTS. DURING THE REJECTED TAKEOFF, THE AIRSPEED INDICATION ON THE NR 1 PRIMARY FLIGHT DISPLAY RETURNED AND MATCHED THAT OF THE NR 2 PRIMARY FLIGHT DISPLAY. CREW WAITED APPROXIMATELY 20 MINUTES TO COOL THE BRAKES AND THEIR SUBSEQUENT INVESTIGATION REVEALED NO FAULTS. THE FOLLOWING TAKEOFF WAS NORMAL. NO MAINTENANCE LOG WAS INITIATED. 2L72 4F RTA28NM 19950130000091995013000009NM 1995 1 30 95FDEA00018 119950116A5313 STRINGER BOEING727 72725 1384006NM BS 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 STR 21R IS CRACKED AT BS 600. REMOVED AND REPLACED STR SECTION FROM BS 595 TO 610 STR 21R IAW FEDEX SRM 53-10-03. 2L73 4F A3WE 19950130000101995013000010NM 1995 1 30 95FDEA00026 119950115A5320 STRUCTURE BOEING727 727233 138408ANM BS 738.95 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04278FE 22345 CRACK INDICATIONS NOTED IN HOLES 1-6 BELOW FLOOR AT BS 783.95 LT. REPAIRED HOLES 1-6 BELOW FLOOR AT BS 783.95 LT PER EA 7-5310-23485. 2L73 4F RTA3WE 19950130000111995013000011WP 1995 1 30 ABXA9500024 119950118A3260700001010 DNLOCK SWITCH DOUG DC8 DC862 3021970WP LT MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23805AX 45906 LEFT MAIN GEAR LIGHT FAILED TO COME ON WHEN THE GEAR WAS LOWERED DURING FINAL APPROACH INTO DFW. GEAR WAS RECYCLED AND LIGHT CAME ON NORMALLY WITH THE SECOND EXTENSION. DEFERRED IAW GMM, INSPECTED, AND FERRIED AIRCRAFT TO ILN. REMOVED AND REPLACED LEFT MAIN GEAR DOWN LIMIT SWITCH WIRING HARNESS DUE TO AGE DETERIORATION. ADJUSTED AND TESTED PROXIMITY SWITCH IAW ABX MAB 32-6. REPLACED LEFT MLG DOWNLOCK SWITCH AND LUBED GEAR. PERFORMED GEAR INDICATION AND SWING TEST IAW DC 8 MM CHAPTER 32. SYSTEM OPS CHECKED GOOD. CLEARED DEFERRAL. 2L74 4F 4A25 19950130000121995013000012WP 1995 1 30 ABXA9500025 119950113A3231S10266145002 SPACER DOUG DC9 DC931 3022065WP FS 111 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE ARM ASSEMBLY ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR TO HAVE EXCESSIVE PLAY. REPLACED DOOR ARM SPACER IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950130000131995013000013WP 1995 1 30 ABXA9500026 119950113A3231BLFR511272 BUSHING DOUG DC9 DC931 3022065WP FS 111 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE ROD END ASSEMBLY ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR TO HAVE EXCESSIVE PLAY. REPLACED ROD END BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950130000141995013000014WP 1995 1 30 ABXA9500027 119950113A3231BLFR4245T BEARING DOUG DC9 DC931 3022065WP FS 111 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR LINK ASSEMBLY HAD EXCESSIVE PLAY. REPLACED DOOR LINK BEARING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950130000181995013000018WP 1995 1 30 ABXA9500031 119950116A5330591142747 SKIN DOUG DC9 DC932F 3022067WP FS 955 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN CRACKED AT STA'S 945 THROUGH 965, JUST BELOW LONGERON 14L. REPAIRED SKIN IAW ABX REA D953-10758-MR. 2L72 4F A6WE 19950130000191995013000019WP 1995 1 30 ABXA9500032 119950117A532099194021 TRAP PANEL DOUG DC9 DC932F 3022067WP FS 58 ELONGATED HOLES A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 WHILE COMPLYING WITH SB 57-129R4, FOUND HOLES IN THE LEFT TRAPEZOID PANEL COMMON TO VERTICAL ATTACH FITTING, OUT OF ROUND AND THE SECOND HOLE FROM BOTTOM STEPPED INSIDE. REPAIRED HOLES IAW DC-9 SRM 51-30-5. STEPPED HOLE REPAIRED IAW ABX REA D957-10786. 2L72 4F A6WE 19950130000201995013000020WP 1995 1 30 ABXA9500033 119950113A533059525628 SKIN DOUG DC9 DC932F 3022067WP FS 990 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STA 990 AND LONGERON 14R. REPAIRED IAW ABX REA D953-10771-MR. 2L72 4F A6WE 19950130000211995013000021WP 1995 1 30 ABXA9500034 119950114A53115903371 FRAME DOUG DC9 DC932F 3022067WP FS 598 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK AND CORROSION INSPECTIONS, FOUND DRILL START IN EDGE OF FRAME 598 AT LONGERON 7R. REPAIRED IAW ABX REA D953-10764-MR, FIGURE 3. 2L72 4F A6WE 19950130000221995013000022WP 1995 1 30 ABXA9500035 119950113A53115920338501 FRAME DOUG DC9 DC932F 3022067WP FS 737 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK AND CORROSION INSPECTIONS, FOUND PREVIOUS BLENDOUT ON FRAME STA 737. REPAIRED IAW ABX REA D953-10759-MR. 2L72 4F A6WE 19950130000231995013000023WP 1995 1 30 ABXA9500036 119950114A531159203371 FRAME DOUG DC9 DC932F 3022067WP FS 598 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK AND CORROSION INSPECTIONS, FOUND FOUR DRILL STARTS IN FRAME 598 BETWEEN LONGERONS 8L AND 10L. REPAIRED PER ABX REA D953-10764-MR, FIGURE 1. 2L72 4F A6WE 19950130000241995013000024WP 1995 1 30 ABXA9500037 119950112A5315991154683 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 996 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING C-CHECK INSPECTION, A PRIOR REPAIR TO THE FLOOR BEAM AT STA 996, RBL35 WAS REMOVED TO REVEAL SEVERAL CUTOUTS IN THE UPPER FLANGE OF THE ANGLE. FLOOR BEAM WAS REPAIRED IAW ABX REA D953-10768-MR. 2L72 4F A6WE 19950130000251995013000025WP 1995 1 30 ABXA9500038 119950112A5320991224345 GUSSET DOUG DC9 DC932 3022066WP FS 965 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING C-CHECK INSPECTION, FOUND A GUSSET CHAFED AT STA 965, LONGERON 4R AND 4L. REPAIRED GUSSET IAW ABX REA D953-10730-MR. 2L72 4F A6WE 19950130000261995013000026WP 1995 1 30 ABXA9500039 119950113A53129912246115 BLKHD TEE DOUG DC9 DC932 3022066WP FS 1039 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON BULKHEAD TEE AT STA 1039 BETWEEN LONGERON 30 AND 26L. REPAIRED TEE IAW ABX REA D953-10761-MR. 2L72 4F A6WE 19950130000271995013000027WP 1995 1 30 ABXA9500040 119950113A5320591015837 JAMB DOUG DC9 DC932 3022066WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON THE AFT LOWER CARGO DOOR JAMB WEB. REPAIRED WEB IAW ABX REA D953-10732-MR. 2L72 4F A6WE 19950130000291995013000029NE 1995 1 30 DL31L950311 219950121A7230PW4152 COMPRESSOR AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 SO11836AB5650 660 724914 DURING CRUISE, NR 2 ENGINE HAD COMPRESSOR STALL WITH EGT AND VIBRATION RISING, SHUT DOWN ENGINE DIVERTED YYT. FOUND METAL IN TAILPIPE, REPLACED ENGINE FOR RETURN TO SERVICE, ROUTED FAILED ENGINE TO SHOP. 2L72 4F RTA35EU E24NE 19950130000301995013000030NM 1995 1 30 DL72L950264 119950104A5754 ANGLE BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 709169 DURING HMV, NR 5 SLAT CLOSEOUT ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950130000321995013000032NM 1995 1 30 DL72S950261 119950118A5754 ATTACH ANGLE BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 DURING LETTER CHECK, THE LEFT WING NR 4 LEADING EDGE SLAT LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND WITH A .5 INCH CRACK IN ITS RADIUS BEHIND THE INBOARD SLAT UPSTOP. REPAIRED PER MM 57-54-0 FIG 812. 2L73 4F A3WE 19950130000331995013000033NM 1995 1 30 DL72S950277 119950119A5330 SKIN DOUBLER BOEING727 727232 1384082NM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11531DA 21814 DURING B-1 LETTER CHECK, FOUND TWO RIVETS SHEARED IN FUSELAGE SKIN DOUBLER AND DOUBLER IS BULGED AFT OF FS 1010 AT STRINGER 29R. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950130000341995013000034NM 1995 1 30 DL72S950290 119950120A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 DURING E-2 L/C, FOUND ONE .25 INCH CRACK IN LWR SKIN OF LEFT ELEVATOR, 7 INCHES FROM I/B EDGE. REPAIRED PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950130000351995013000035NM 1995 1 30 DL72S950292 119950120A5210 SKIN BOEING727 727232 1384082NM FWD ENTRY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 DURING E-2 LETTER CHECK, FOUND MAIN ENTRY DOOR OUTER SKIN CRACKED .5 INCH AT LOWER HINGE CUTOUT LOWER AFT CORNER. REPAIRED PER B727MM 52-11-01 PG808. 2L73 4F A3WE 19950130000361995013000036NE 1995 1 30 DL72S950305 219950117A731437820113 FUEL PUMP BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 3 ENGINE SHEARED SHAFT A ADALAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 SO11532DA 22045 687530 DURING DESCENT, NR 3 ENGINE FLAMED OUT. UNABLE TO RESTART, LANDED ORD WITHOUT INCIDENT. REPLACED FUEL PUMP AND FUEL CONTROL, OPERATION NORMAL. SHOP INSPECTION FOUND FUEL PUMP SHAFT WAS SHEARED. 2L73 4F4 F A3WE E2EA 19950130000371995013000037NM 1995 1 30 DL72W950280 119950112A5711 FRAME BOEING727 727247 138408FNM WS 910/913 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND THE RT UPLOCK FRAMES AT STA 910 AND 913 HAVE TEMPORARY REPAIRS. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950130000381995013000038NM 1995 1 30 DL72W950281 119950105A5210 SKIN BOEING727 727247 138408FNM L-1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND THE L-1 DOOR LOWER FORWARD CORNER SKIN CRACKED VIEW INSIDE ACCESS HOLE, REPAIRED PER M/M 52-11-0 FIG 803. 2L73 4F A3WE 19950130000391995013000039NM 1995 1 30 DL72W950282 119950106A5210 WEB BOEING727 727247 138408FNM L-1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND WEB CRACKED INSIDE THE LOWER FWD CORNER OF L-1 DOOR, REPAIRED PER M/M 52-11-0 FIG 803 ON NR 429. 2L73 4F A3WE 19950130000401995013000040NM 1995 1 30 DL72W950283 119950105A5210 SKIN BOEING727 727247 138408FNM L 1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND THE L-1 DOOR AFT FRAME SKIN ON DOOR AT UPPER ROLLER GUIDE FITTING SKIN CRACKED. REPAIRED PER ERA 300996-14. 2L73 4F A3WE 19950130000411995013000041NM 1995 1 30 DL72W950284 119950119A5311 FRAME BOEING727 727247 138408FNM FS 600 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND THE FRAME CRACKED AT STA 600 BETWEEN STRINGER 25L THROUGH STRINGER 24 L, REPAIRED PER SRM 53-10-4 PG 87. 2L73 4F A3WE 19950130000421995013000042NM 1995 1 30 DL72W950285 119950115A5754 ANGLE BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND AN ANGLE CRACKED AT TAI CUTOUT ON THE NR 7 LEADING EDGE SLAT, REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950130000431995013000043NM 1995 1 30 DL72W950300 119950105A5313 STRINGER BOEING727 727247 138408FNM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AT HMV, FOUND CORROSION DAMAGE TO LOWER FUSELAGE STRINGER 27R AT FS 720F. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950130000441995013000044NM 1995 1 30 DL72W950301 119950105A5313 STRINGER BOEING727 727247 138408FNM FS 580-600 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AT HMV, FOUND CORROSION DAMAGE TO LOWER FUSELAGE STRINGER 28L AT FS 580 TO FS 600. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950130000451995013000045NM 1995 1 30 DL72W950303 119950107A5313 STRINGER BOEING727 727247 138408FNM FS 450-480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AT HMV, FOUND LOWER FUSELAGE STRINGER 28L CORRODED AT FS 450 TO FS 480. REPLACED STRINGER PER SRM 51-30-1 FIG 1. 2L73 4F A3WE 19950130000461995013000046NM 1995 1 30 DL72W950304 119950107A5313 STRINGER BOEING727 727247 138408FNM FS 450-480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AT HMV, FOUND LOWER FUSEALAGE STRINGER 28R CORRODED AT FS 450 TO FS 480. REPLACED STRINGER PER SRM 51-10-1 FIG 1. 2L73 4F A3WE 19950130000471995013000047NE 1995 1 30 DL73S950260 219950117A7220658536915 DOME BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE DISLODGED A DALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO11320DL 23092 709169 ON TAKEOFF NR 1 ENGINE HAD COMPRESSOR STALL, ABORTED TAKOFF. UPON RETURNING TO GATE FOUND INTAKE DOME ASSEMBLY DISLODGED, WITH DAMAGE TO N-1 ACCESSORY GEARCASE, AND 5 FAN BLADES. SUSPECT CAUSE OF COMPRESSOR STALL WAS WHEN THE DOME ASSEMBLY MOUNT FAILED AND DOME BECAME DISLOGED. REPLACED N1 GEARBOX, DOME AND DRESSED THE FAN BLADES. RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2EA 19950130000481995013000048NM 1995 1 30 DL73S950279 119950118A2520417N3100349A PSU BOEING737 737232 1384475NM CABIN FAULTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11324DL 23096 AFTER TAKEOFF FLIGHT ATTENDANTS REPORTED STRONG BURING ODOR IN MID CABIN AND AFT. NO SMOKE OR FIRE NOTED. RETURNED HSV. TRACED SOURCE OF ODOR TO PSU AT ROW 17ABC. REPLACED PSU OPERATION NORMAL. 2L72 4F RTA16WE 19950130000491995013000049NM 1995 1 30 DL757950293 119950119A5400311N300026SP STRUCTURE BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 DURING L/O, NR 2 ENG WAS REMOVED FOR SCHEDULED MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE INBOARD WEB OF PYLON STRUCTURE AT THE FWD INSPECTION HOLE. REPAIRED PER SRM 54-51-01 FIG 203. 2L72 4F RTA2NM 19950130000501995013000050WP 1995 1 30 DLL10950287 119950113A32331535927105 ACTUATOR LKHEED1011 10113851 5265010WP RT MLG CRACKED BODY A ADALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO11715DA 193C1092 DURING CLIMB-OUT, HEARD LOUD BANG AND NOTICED C SYSTEM HYDRAULIC FAILURE, MANUALLY EXTENDED LANDING GEAR, LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR RETRACT ACTUATOR WITH A CIRCUMFERENTIAL CRACK ON END OF CYLINDER AT ACTUATOR PISTON EXIT. REPLACED ACTUATOR OPERATION NORMAL. 2L73 4F A23WE 19950130000511995013000051WP 1995 1 30 DLL16950250 119950104A5312 STIFFENER LKHEED1011 10113853 5265020WP PRESS BLKHD CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL AFT P DOME STIFFENER IS CORRODED FROM WHERE IT TIES TO STR 41 TO HALF WAY UP STIFFENER. REMOVED CORRODED SECTION, INSTALLED STIFFENER SECTION AND SPLICE PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950130000521995013000052WP 1995 1 30 DLL16950254 119950105A5400 ANGLE LKHEED1011 10113853 5265020WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT OVERHAUL NR 2 ENG INLET, LEFT SIDE AT 3:00 POS- FS 1705, HORIZONTAL ANGLE IS CRACKED. REPLACED TEE AND SPACER SECTION IAW SRM 54-12-00 FIG 803. 2L73 4F A23WE 19950130000531995013000053WP 1995 1 30 DLL16950255 119950105A5400 ANGLE LKHEED1011 10113853 5265020WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL NR 2 ENG INLET DUCT, LT FS1705, 9:00 POS 'VIEWED THROUGH PANEL 311UL', BULKHEAD ANGLE CRACKED FABRICATED AND INSTALLED REPAIR TEE ANGLE AND SPACER PER SRM 54-12-00 FIG 803. 2L73 4F A23WE 19950130000541995013000054WP 1995 1 30 DLL16950257 119950105A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 1745 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL AT CABIN AFT GALLEY/SERVICE CTR, UNDER FLOOR AREA, TOP OF FS1745 FLOOR BEAM, CORROSION AROUND FASTENER HOLE AT RBL53. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-21-00 PG 865-868. 2L73 4F A23WE 19950130000551995013000055WP 1995 1 30 DLL16950259 119950104A5312 STIFFENER LKHEED1011 10113853 5265020WP PRESS BLKHD CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL AT AFT P-DOME, STIFFENER IS CORRODED ON LWR END WHERE IT TIES TO STR 25. REMOVED CORROSION AND INSTALLED STIFFENER AND SPLICE PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950130000561995013000056WP 1995 1 30 DLL16950263 119950105A5743 FITTING LKHEED1011 10113853 5265020WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND LMLG RETRACT ACT FITTING ATTACH STRUCTURE CORRODED IN UPPER MATING SURFACE AROUND BOLT HOLES. LOCAL BLENDED SURFACES TO REMOVE CORROSION, HFEC INSPECTED ALL SURFACES AND FOUND OK. REPAIRED PER SRM 57-14-00 PG 809. 2L73 4F A23WE 19950130000571995013000057WP 1995 1 30 DLL16950265 119950120A5743 TRUNNION FITTING LKHEED1011 10113853 5265020WP RT MLG RUSTY A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, THE RIGHT MAIN LANDING GEAR TRUNION FITTING BETWEEN LATERAL BRACE LUGS ARE RUSTY. REPAIRED PER SRM 57-14-00 FIG 804. 2L73 4F A23WE 19950130000581995013000058WP 1995 1 30 DLL16950266 119950120A5743 TRUNNION FITTING LKHEED1011 10113853 5265020WP RT MLG RUSTY A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 HMV, THE RIGHT MAIN LANDING GEAR TRUNNION FITTING WAS FOUND CORRORDED BETWEEN FWD TRUNNION LUGS. REMOVED CORROSION PER SRM 57-14-00 FIG 804. 2L73 4F A23WE 19950130000591995013000059WP 1995 1 30 DLL16950268 119950120A5313 STRINGER LKHEED1011 10113853 5265020WP FS 963 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, FOUND FUSELAGE STRINGER 32 INSIDE MESC WITH CORROSION DAMAGE JUST FORWARD OF FS 963. REPLACED DAMAGED SECTION OF STR BETWEEN STA 933-983 PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950130000601995013000060WP 1995 1 30 DLL16950269 119950120A5313 STRINGER LKHEED1011 10113853 5265020WP FS 963 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, FOUND STRINGER CORRODED INSIDE MESC FWD OF STA 963 S-34. REPLACED STRINGER SECTION PER SRM 53-13-00 PG 896. 2L73 4F A23WE 19950130000611995013000061WP 1995 1 30 DLL16950270 119950120A5330 SKIN LKHEED1011 10113853 5265020WP FS 1615 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, FOUND CORROSION ON FUSELAGE SKIN UNDER AND AROUND TEAR STAP AT FS 1615 BETWEEN STRINGERS 34-37. REMOVED LIGHT CORRROSION AND CHECKED WITHIN LIMITS PER SRM 53-31-00 FIG 801. REINSTALLED TEAR TRAP PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950130000621995013000062WP 1995 1 30 DLL16950271 119950120A5330 SKIN DOUBLER LKHEED1011 10113853 5265020WP FS 727 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, FOUND INTERIOR FUSELAGE SKIN DOUBLER FOR SKIN SPLICE AT FS 727 AT BL-0 CORRODED. REPAIRED PER SRM 53-31-00 FIG 836. 2L73 4F A23WE 19950130000631995013000063WP 1995 1 30 DLL16950272 119950120A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 729/846 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709169 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DELAMINATED BETWEEN FS 729 AND 846 BETWEEN STRINGERS 32-31. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950130000641995013000064WP 1995 1 30 DLL16950273 119950120A5743 TRUNION FITTING LKHEED1011 10113853 5265020WP RT MLG RUSTY A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, THE RIGHT MAIN LANDING GEAR FWD TRUNNION ATTACH FITTING WAS FOUND CORRODED AT THE FWD TRUNNION LUG AND IN AREA OF AFT LUG. REPAIRED PER SRM 57-14-00 FIG 804. 2L73 4F A23WE 19950130000651995013000065WP 1995 1 30 DLL16950275 119950120A5743 FITTING LKHEED1011 10113853 5265020WP RT MLG RUSTY A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, THE RIGHT MAIN GEAR FITTING AT UPPER LATERAL BRACE LUG WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER SRM 57-14-00 FIG 804. 2L73 4F A23WE 19950130000661995013000066WP 1995 1 30 DLL16950276 119950120A5270 HINGES LKHEED1011 10113853 5265020WP RT MLG DOOR RUSTY A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, HINGES AND BUSHINGS THAT ARE ATTACHED RT MAIN GEAR FITTING FOR UPPER HINGE DOOR WERE FOUND CORRODED. REPAIRED PER SRM 57-14-00 FIG 804. 2L73 4F A23WE 19950130000671995013000067WP 1995 1 30 DLL16950291 119950104A5313 STRINGER LKHEED1011 10113853 5265020WP FS 963 CORROSSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND STRINGER AND SKIN CORROSION AT FS 963 STR 32 AND 34 IN THE MESC. REPAIRED PER SRM 53-13-00 PAGE 806. 2L73 4F A23WE 19950130000681995013000068WP 1995 1 30 DLL16950294 119950115A5320 FLOOR SUPPORT LKHEED1011 10113853 5265020WP FS 888-901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND CABIN FLOOR SUPPORT AT FS 888-901 AT LBL 46.5 CORRODED. REPLACED SUPPORT PER SRM 51-10-05 PG.1. 2L73 4F A23WE 19950130000691995013000069WP 1995 1 30 DLL16950295 119950106A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 901-923 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND CABIN FLOOR SUPPORT CORRODED AT LBL 30 FS 901-923. FOUND CORROSION TO BE OUT OF LIMITS, REPLACED FLOOR SUPPORT PER SRM 51-10-00 PG 1. 2L73 4F A23WE 19950130000701995013000070WP 1995 1 30 DLL16950296 119950106A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 900 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND CABIN FLOOR SUPPORT CORRODED ON LOWER SURFACE APP FS 900 AT RBL 30. REPLACED FLOOR SUPPORT PER SRM 51-10-05. 2L73 4F A23WE 19950130000711995013000071WP 1995 1 30 DLL16950297 119950105A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 315 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND CABIN FLOOR BEAM CORRODED ON UPPER SURFACE AT FS 315 FROM CENTER LINE TO DOOR (L-1). FOUND TO BE OUT OF LIMITS PER SRM 53-21-00. REPAIRED PER SRM 53-21-00 PG 868. 2L73 4F A23WE 19950130000721995013000072WP 1995 1 30 DLL16950298 119950106A5347 SEAT TRACK LKHEED1011 10113853 5265020WP FS 1318 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FS 1318 CENTER INBOARD SEAT TRACK CORRODED AT FS 1318 AVBOVE HYDTRAULIC SERVICE CENTER. REPLACED TRACK PER SRM 53-21-00. 2L73 4F A23WE 19950130000731995013000073WP 1995 1 30 DLL16950299 119950120A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 923 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND TEAR STRAP AT FS 923 STR 21 AND 22 DISBONDED. REPAIRED PER SRM 53-30-00 PG 807. 2L73 4F A23WE 19950130000741995013000074WP 1995 1 30 MWEA95110 119950117A2560113313 EVAC SLIDE DOUG DC9 DC915 3022036WP PAX DOOR FELL OFF DOR A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING ROUTINE MAINTENANCE, THE PAX DOOR EMERGENCY SLIDE FELL OUT. RESECURED EMERGENCY SLIDE IN DOOR SLIDE HOLDER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950130000751995013000075NM 1995 1 30 SWAA950050 119950117A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21262 DURING SCHEDULED 1/4 D CHECK, FOUND SEVERALS CRACKS EXTENDING FROM UNDER RIVET HEADS AT FWD SIDE OF PRESSURE BULKHEAD AT BS 178, LBL 6 AND WL 183.0. REPAIRED PER SWA RA 1-253-1236. 2L72 4F A16WE 19950130000761995013000076NM 1995 1 30 SWAA950051 119950117A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21262 DURING SCHEDULED QUARTER D CHECK, FOUND MANY CRACKS EXTENDING FROM THE INBOARD VERTICAL ROW OF BULKHEAD FASTENER HOLES, LBL 5.25 AND WL 185.5. REPAIRED PER SWA RA 1-253-1236. 2L72 4F A16WE 19950130000771995013000077NM 1995 1 30 SWAA950052 119950117A5320 CLIP BOEING737 7373Q8 1384670NM BS 727D CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIP CORRODED AT BS 727D, RBL 16, WL 150. REPLACED PER BOEING STRUCTURAL REPAIR MANAUL. 2L72 4F RTA16WE 19950130000781995013000078NM 1995 1 30 SWAA950053 119950117A53302024T3 SKIN BOEING737 7373Q8 1384670NM BS 885 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 885, BETWEEN S19 AND 20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL. 2L72 4F RTA16WE 19950130000791995013000079NM 1995 1 30 SWAA950054 119950117A5315 FLOOR BEAM BOEING737 7373Q8 1384670NM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORROSION AT BS 294.5, LBL 11 TO RBL 45. REPAIRED PER SWA RA 1-353-418. 2L72 4F RTA16WE 19950130000801995013000080NM 1995 1 30 SWAA950055 119950117A5320693725404 ANGLE BOEING737 7373Q8 1384670NM BS 570 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND SKATE ANGLE CRACKED AT BS 570, WL 158, LBL 50. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130000811995013000081NM 1995 1 30 SWAA950056 119950117A5320 WEB BOEING737 7373Q8 1384670NM BS 726 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED MAINTENANCE CHECK, FOUND CRACK IN WEB AT BS 726, S18A, LEFT SIDE. REPAIRED PER SWA RA 1-553-1222. 2L72 4F RTA16WE 19950130000821995013000082NM 1995 1 30 SWAA950057 119950117A335020121 EEL BATT CHARGER BOEING737 7373H4 1384600NM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07366SW 25251 FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED FORWARD RIGHT BATTERY CHARGER PER BOEING M/M. 2L72 4F RTA16WE 19950130000831995013000083NM 1995 1 30 SWAA950058 119950117A5330 SKIN BOEING737 7373H4 1384600NM BS 380 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07370SW 26597 DURING SCHEDULED B1 CHECK, FOUND TWO GOUGES ON FUSELAGE SKIN AT BS 380, AT WL 208 AND 216. REPAIRED BOTH PER BOEING STRUCTURAL RPAIR MANUAL. 2L72 4F RTA16WE 19950130000841995013000084NM 1995 1 30 UPS202045 119950117A3260653756855U GEAR ASSY BOX BOEING727 72730C 1384009NM LANDING GEAR MALFUNCTION A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01919UP 19012 (SUPPLEMENTAL MRR) PILOT REPORTED LEFT MAIN GEAR LIGHT WOULD NOT INDICATE GREEN WHEELS. RECYCLED THEN BOTH LEFT AND RIGHT MAIN GEAR WOULD NOT INDICATE GREEN WHEELS. ON THE THIRD RECYCLE BOTH LEFT AND RIGHT MAIN GEAR GREEN LIGHTS INDICATED SAFE CONDITION. REPLACED GEAR ASSY BOX IAW MM 32-09-11. SYS CHECKS GOOD. 2L73 4F A3WE 19950130000851995013000085NM 1995 1 30 UPS202048 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7208 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7208. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000861995013000086NM 1995 1 30 UPS202049 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7210 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7210. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000871995013000087NM 1995 1 30 UPS202050 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7606 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7606. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000881995013000088NM 1995 1 30 UPS202051 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7610 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7610. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000891995013000089NM 1995 1 30 UPS202052 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7608 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7608. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000901995013000090NM 1995 1 30 UPS202053 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7603 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7603. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000911995013000091NM 1995 1 30 UPS202054 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7602 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7602. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000921995013000092NM 1995 1 30 UPS202055 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7207 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7207. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000931995013000093NM 1995 1 30 UPS202056 119950120A5730 SKIN BOEING727 727185C 138406NNM PANEL 7204 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FUEL CELL ACCESS CUT OUT FOR PANEL 7204. REPAIRED PER UPS ENGINEERING FILE NUMBER 727-57-1068, 727-57-1074. 2L73 4F A3WE 19950130000941995013000094NM 1995 1 30 UPS202058 119950120A5347 SEAT TRACK BOEING727 727185C 138406NNM FS 756-852 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 756-852, LBL 65. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-2, 51-20-4. 2L73 4F A3WE 19950130000951995013000095NM 1995 1 30 UPS202059 119950120A5347 SEAT TRACK BOEING727 727185C 138406NNM FS 780-820 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AT STA 780-820, RBL 45, WL 208. REPLACED SEAT TRACK PER SRM 51-30-02, 51-10-1. 2L73 4F A3WE 19950130000961995013000096NM 1995 1 30 UPS202060 119950120A5320 FLOOR SUPPORT BOEING727 727185C 138406NNM FS 756 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 756, LBL 45-60. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2. 2L73 4F A3WE 19950130000971995013000097NM 1995 1 30 UPS202061 119950120A5320 FLOOR SUPPORT BOEING727 727185C 138406NNM FS 848 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT NUT PLATE AT STA 848, LBL 40, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, 51-10-1. 2L73 4F A3WE 19950130000981995013000098NM 1995 1 30 UPS202062 119950120A53302024T3050 SKIN BOEING727 727185C 138406NNM FS 1155 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND SKIN CRACKED AT STA 1155 BETWEEN STR 20-21L. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-30-8, 53-30-3. 2L73 4F A3WE 19950130000991995013000099NM 1995 1 30 UPS202063 119950120A5311 FRAME BOEING727 727185C 138406NNM FS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT STA 760, LBL 65-70, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-10-6, 51-30-2, AND UPS ENGINEERING FILE NUMBER 727-53-1456. 2L73 4F A3WE 19950130001001995013000100NM 1995 1 30 UPS202064 119950120A5311 FRAME BOEING727 727173C 1384059NM FS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND FLOURESCENT LIQUID PENETRANT INSPECTION OF FASTENER HOLES ON BS 660 FRAME AT OR NEAR STRINGER 19R EXHIBIT A CRACK INDICATION FROM SCREW HOLE TO FASTENER HOLE. INSTALLED REPAIR IAW SRM 51-40-3, 51-30-2, AND 51-10-2. 2L73 4F A3WE 19950130001011995013000101NM 1995 1 30 UPS202065 119950120A5753 SKIN BOEING727 727173C 1384059NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS AREA OF DELAMINATION ON I/B T/E CORNER LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND MM 51-20-151. 2L73 4F A3WE 19950130001021995013000102NM 1995 1 30 UPS202066 119950120A5753 SKIN BOEING727 727173C 1384059NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B FORE FLAP HAS DENT WITH DELAMINATION 12 INCHES FROM O/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6 AND 51-20-151. 2L73 4F A3WE 19950130001031995013000103NM 1995 1 30 UPS202067 119950120A5753 SKIN BOEING727 727173C 1384059NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 60 INCHES FROM I/B END UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6. 2L73 4F A3WE 19950130001041995013000104NM 1995 1 30 UPS202068 119950120A5753 SKIN BOEING727 727173C 1384059NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 86 INCHES FROM O/B END LOWER SURFACE. INSTALLED REPAIR IAW SRM 51-40-6. 2L73 4F A3WE 19950130001051995013000105NM 1995 1 30 UPS202069 119950120A5753 SKIN BOEING727 727173C 1384059NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND LEFT WING O/B AFT FLAP T/E HAS EDGE DELAMINATION AT O/B CORNER. INSTALLED REPAIR IAW SRM 51-40-6. 2L73 4F A3WE 19950130001061995013000106NM 1995 1 30 UPS202070 119950120A57516593155437 HINGE BOEING727 727173C 1384059NM LT AILERON CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND L/W, O/B AILERON, AFT I/B HINGE HALF IS CORRODED. INSTALLED REPAIR IAW MM 27-10-41. 2L73 4F A3WE 19950130001071995013000107NM 1995 1 30 UPS202072 119950120A5753651920115 SUPPORT ROLLER BOEING727 727173C 1384059NM NR 5 TE FLAP PITTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND R/W O/B FLAP I/B CARRIAGE (NR 5) AFT SUPPORT ROLLER IS PITTED. INSTALLED REPAIR IAW 51-10-6. 2L73 4F A3WE 19950130001081995013000108NM 1995 1 30 UPS202073 119950120A5712 RIB BOEING727 727173C 1384059NM WS 629 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND R/W RIB CHORD IS CRACKED AT WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5. 2L73 4F A3WE 19950130001091995013000109NM 1995 1 30 UPS202074 119950120A5712 RIB BOEING727 727173C 1384059NM WS 629 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND L/W RIB CHORD IS CRACKED WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5. 2L73 4F A3WE 19950130001101995013000110NM 1995 1 30 UPS202075 119950120A5510 WEB BOEING727 727173C 1384059NM RT HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION IN WEB AT STA 68.92 INSIDE RT HORIZONTAL STAB. INSTALLED REPAIR IAW SRM 55-10-2, 55-10-1, AND 51-30-2. 2L73 4F A3WE 19950130001111995013000111NM 1995 1 30 UPS202076 119950120A5330 SKIN BOEING727 727173C 1384059NM FS 1020 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AT SKIN LAP AT BS 1020, WL 188, RBL 55. INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F A3WE 19950130001401995013000140WP 1995 1 30 9501141146 119950119A5312 BULKHEAD SUPPORT DOUG DC10 DC1040 3023508WP CENTER WW CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL AT LBL 19-29. INSTALLED REPAIR ANGLE PER EA 11-93766. 2L73 4F A22WE 19950130001411995013000141NE 1995 1 30 9501151156 219950119A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 3 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01156US 46765 686173 DURING TAKEOFF (CDG), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL AT 48 KNOTS AND THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BORESCOPE HAS BEEN SCHEDULED. 2L73 4F4 F A22WE E20EA 19950130001421995013000142WP 1995 1 30 9501161150 119950118A5610 WINDOW DOUG DC10 DC1040 3023508WP RT COCKPIT NOT LATCHED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01150US 46759 DURING TAKEOFF, THE FIRST OFFICER'S WINDOW CAME OPEN, ABORTED TAKEOFF. RESEATED AND LOCKED WINDOW. OPERATIONAL CHECK AND SECURITY CHECK OK. 2L73 4F A22WE 19950130001431995013000143WP 1995 1 30 9501179139 119950118A3260 DNLOCK SWITCH DOUG DC9 DC914 3022034WP RT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01948L 47049 DURING APPROACH INTO MEM, THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130001441995013000144WP 1995 1 30 9501189876 119950119A3230 SPRING DOUG DC9 DC951 3022051WP GEAR BYPASS HNDLWEAK A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01785NC 48110 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO MEM, AND LANDED WITH MAIN GEAR DOORS DOWN. FOUND BYPASS HANDLE SPRINGS WEAK. REPLACED SPRINGS, AND REPLACED THE LEFT AND RIGHT MAIN GEAR DOORS DUE TO DAMAGE INCURRED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130001451995013000145WP 1995 1 30 9501199754 119950119A2170 CLAMP DOUG DC9 DC941 302207NWP WATER SEP DUCT WORN A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL01754NW 47178 ENROUTE DTW-CLT, CABIN PRESSURE WARNING AND MASTER WARNING LIGHTS ILLUMINATED AT 33,000 FEET. ACCOMPLISHED DESCENT TO 15,000 FEET AND CABIN PRESSURE WAS REGAINED. FLIGHT CONTINUED TO DESTINATION, AND LANDED WITHOUT INCIDENT. FOUND CLAMP LOOSE, AND DUCT DISCONNECTED AT MOISTURE SEPARATOR. INSTALLED NEW CLAMP, AND RECONNECTED DUCT. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130001461995013000146NM 1995 1 30 9501206303 119950122A3241 CAUTION LIGHT BOEING747 747451 1384940NM ANTI-SKID SYST ILLUMINATED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01663US 23818 DURING CRUISE, ANTI-SKID CAUTION LIGHT APPEARED. FLIGHT DIVERTED TO JFK DUE TO RUNWAY CONDITIONS AT DTW. DEACTIVATED THE NR 2 AND NR 4 BRAKES AND DEFERRED. 2L74 4F RTA20WE 19950130001471995013000147NM 1995 1 30 9501212711 119950116A53306517556132 SKIN BOEING727 7272S7 138407ZNM FS 1343 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01715RC 22019 DURING PERIODIC CHECK, MAINTENANCE FOUND 2 CRACKS EMITTING FROM FASTENER HOLE AT FS 1343, WL 257. REPAIRED PER NWA EA 27-93776. 2L73 4F A3WE 19950130001481995013000148SO 1995 1 30 COM11734 119950118A27306225734002 SERVO EMB 120 EMB120RT SO PITCH TRIM DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01256CA8847 120245 ELECRIC TRIM IS INOP, AND MANUAL TRIM FEELS ROUGH. REPLACED THE PITCH TRIM SERVO. 2L72 4T RTA31SO 19950130001491995013000149SO 1995 1 30 COM11735 119950120A3230 RETRACT MECH EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01243CA 120212 LANDING GEAR WOULD NOT RETRACT. COULD NOT BE DUPLICATE. LANDING GEAR RETRACTION CHECKS NORMAL. 2L72 4T RTA31SO 19950130001501995013000150SO 1995 1 30 COM11736 119950121A32301959500007 RETRACT MECH EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01261CA7854 120254 LT MLG INTRANSIT INDICATOR REMAINED ON AFTER GEAR RETRACTION. ADJUSTED RETRACT ACTUATOR FOR PROPER UPLOCK HOOK ENGAGEMENT. 2L72 4T RTA31SO 19950130001511995013000151NE 1995 1 30 COM20351 319950119A6110 PROPELLER SWRNGNSA227 SA227AC 8780603SW MCAULY4HFR344HFR34C652 NE LT ENGINE LEAKING A COMAK NONE KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 SO01458AM 800 AC699 881162 LT PROPELLER LEAKING OIL AT BLADE HUBS. REPLACED PROPELLER. 1L72 4T A8SW 6 C3PNE 19950130001521995013000152EU 1995 1 30 COM31016 119950122A33506104781 BATTERY SAAB SF340 SF340A 7850100EU CABIN EEL DISCHARGED A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01342CA 340A023 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY PACKS. 2L72 4T RTA52EU 19950130001531995013000153EU 1995 1 30 COM31017 119950121A61205308211 QUADRANT SAAB SF340 SF340A 7850100EU COCKPIT DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01361CA161585259 340A056 AUTO COARSEN SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED CONTROL QUADRANT. 2L72 4T RTA52EU 19950130001541995013000154 1995 1 30 COM31018 419950118A34256626190113 COMPUTER SAAB SF340 SF340A 7850100EU AVIONICS DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01358CA14157559 340A047 NR 1 AHRS HEADING WAS OFF BY 25 DEGREES. REPLACED THE NR 1 AHC-85. 2L72 4T RTA52EU 19950130001551995013000155EU 1995 1 30 COM31019 119950119A3297 WIRE SAAB SF340 SF340A 7850100EU LT ANTI SKID BROKEN A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01370CA2357123571 340A010 ANTI-SKID CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. REPAIRED BROKEN WIRE IN AFT LT WHEEL WELL. 2L72 4T RTA52EU 19950130001561995013000156EA 1995 1 30 COM60388 119950119A2760270003 PCU CNDAIRCL600 CL6002B19 EA RT SPOILERON DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01918CA3662 7018 SPOILERON FAULT MESSAGE ON EICAS. REPLACED RT OUTBD SPOILERON PCU 2L72 4F RTA21EA 19950130001581995013000158NM 1995 1 30 UPS202077 119950123A5320 FAILSAFE STRAP BOEING727 727185C 138406NNM BS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AND O/B FAILSAFE STRAPS TO BE CRACKED AT BS 294, WL 215 APPROX. LBL 50. INSTALLED REPAIR IAW UPS FILE NR 727-53-1459. 2L73 4F A3WE 19950130001591995013000159NM 1995 1 30 UPS202078 119950123A5330 BUTT JOINT BOEING727 727173C 1384059NM FS 441 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND STA 441, STR 6L TO 10L CORROSION EMANATING FROM FWD SIDE OF BUTT JOINT. INSTALLED REPAIR IAW EO B727-5310-1371E, APP. 8.5. 2L73 4F A3WE 19950130001601995013000160NM 1995 1 30 UPS202079 119950123A5753 FLAP BOEING727 727173C 1384059NM RT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 57 INCHES FROM I/B END. INSTALLED REPAIR IAW ARM 51-40-06. 2L73 4F A3WE 19950130001611995013000161NM 1995 1 30 UPS202080 119950123A5753 FLAP BOEING727 727173C 1384059NM RT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING I/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 31 INCHES FROM I/B END LOWER SURFACE. INSTALLED REPAIR IAW ARM 51-40-06. 2L73 4F A3WE 19950130001621995013000162NM 1995 1 30 UPS202081 119950123A5753 FLAP BOEING727 727173C 1384059NM RT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON T/E 72 INCHES FROM O/B END ON T/E. INSTALLED REPAIR IAW ARM 51-40-06. 2L73 4F A3WE 19950130001631995013000163NM 1995 1 30 UPS202082 119950123A5712 RIB BOEING727 727173C 1384059NM WS 656.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING RIB CHORD WAS CRACKED AT WING STA 656.5, LOWER CHORD S-8. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-2, 51-20-1, 51-30-2. 2L73 4F A3WE 19950130001641995013000164NM 1995 1 30 UPS402020 119950123A5320 WEB BOEING747 747121 1384871NM FS 1840-1860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 WHILE IN 'C' CHECK IN AMSTERDAM, MAINTENANCE FOUND CORROSION ON WEB FROM BEAM AT BS 1840-1860, STR 33L IN THE AFT CARGO COMP. INSTALLED REPAIR IAW SRM 51-40-02. 2L74 4F A20WE 19950130001651995013000165NM 1995 1 30 UPS402021 119950123A5311 FRAME BOEING747 747121 1384871NM FS 2040 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01681UP 19661 WHILE IN 'C' CHECK IN AMSTERDAM, MAINTENANCE FOUND BULK CARGO COMP FRAME AT STA 2040 STR 29L CRACKED. INSTALLED REPAIR IAW SRM 53-10-04, FIG 39. 2L74 4F A20WE 19950130001661995013000166NM 1995 1 30 UPS402089 119950121A3260NAS5137 WARNING IND BOEING747 747121 1384871NM NLG MALFUNCTION A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01691UP 19641 PILOT REPORTED ON GEAR EXTENTION WITH PRIMARY NOSE GEAR SENSOR INOP. THE GEAR INDICATES UNSAFE ON THE PILOT'S PANEL, AND THE LANDING GEAR WARNING HORN WILL NOT SILENCE UNTIL BREAKER IS PULLED. ALT SENSOR INDICATES SAFE IN F/E PANEL. INSTALLED REPAIR IAW MM 32-61-15, P/N 69B47531-3, P/N 69B47530-7. 2L74 4F A20WE 19950130001671995013000167WP 1995 1 30 UPS802085 119950120A2560 ESCAPE SLIDE DOUG DC8 DC873F 302199FWP FLIGHT DECK REQD REPACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 MAINTENANCE REPORTED EMERGENCY EXIT SLIDE NEEDS REPACK. REINSTALLATION OF SLIDE INTO SLIDE HOLDER ON ENTRANCE DOOR. 2L74 4F RT4A25 19950130001681995013000168 1995 1 30 UPS802086 419950122A2565515610010 ESCAPE SLIDE DOUG DC8 DC871F 302199DWP FLIGHT DECK LOW PRESSURE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01713UP 46014 MAINTENANCE REPORTED EVACUATION SLIDE BELOW LIMITS. REMOVED AND REPLACED EVAC SLIDE IAW 25-60-01. 2L74 4F RT4A25 19950130001691995013000169WP 1995 1 30 UPS802087 119950121A3260 WARNING LIGHT DOUG DC8 DC873F 302199FWP LANDING GEAR MALFUNCTION A IPXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01840UP 46140 WHILE A/C WAS IN COLOGNE, MAINTENANCE REPORTED UPLATCH CHECK DOOR NOT LATCHED LIGHT ILLUMINATED AND NOSE GEAR EXTENDED. 2L74 4F RT4A25 19950130001701995013000170WP 1995 1 30 UPS802088 119950121A3231NAS5137 UPLATCH MECH DOUG DC8 DC873F 302199FWP LT MLG DOOR OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO01819UP 46019 PILOT REPORTED DURING DEPARTURE FROM DFW, THE GEAR NOT LATCHED LIGHT ILLUMINATED. THE ALTERNATE GEAR/DOOR WARNING SYSTEM INDICATED THE MAIN GEAR DOOR CLOSED. PERFORMED THE 'GEAR/DOOR NOT LATCHED LIGHT ILLUMINATED' CHECKLIST, AND HAD TO CYCLE THE GEAR 2 TIMES BEFORE SUCCESSFUL UPLATCH CHECK. FOUND LOCKING TAB SHEARED AND LOCKING NUT LOOSE, NOT SAFTIED ON LEFT GEAR DOOR UPLATCH CYL. FOUND LEFT GEAR DOOR UPLATCH MECHANISM OUT OF RIG. ALSO, RT GEAR DOOR UPLATCH PROX SWITCHES LOOSE. COMPLETED MM PROCEDURE 32-31-04. OPS CHECK NORMAL. 2L74 4F RT4A25 19950130001711995013000171EU 1995 1 30 95ZZZX418 119950105A341113730296K402 PITOT HEAD BAG JETSTMJETSTM3101 1500215EU LT FWD FUSELAGE INOPERATIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07845JS 769 FLT 4076 - DURING TAKEOFF ROLL, CAPTAIN NOTICED AIR SPEED INDICATOR REMAINED AT ZERO, TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO GATE. OUT STATION MAINTENANCE PREHEATED PITOT/STATIC SYSTEM TO MELT ANY POSSIBLE ICE ACCUMULATION IN PITOT HEAD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950130001771995013000177WP 1995 1 30 HAL95001 119950103A57535912150505 BRACKET DOUG DC9 DC951 3022051WP TE FLAP CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13672MC 47661 HNL - ITEM FROM M-71, NR 138547-1. DURING SERVICE CHECK, FOUND A CRACK IN INBOARD FLAP HINGE (BRACKET ASSY) ON THE RIGHT WING. VERIFIED CRACK WITH EDDY CURRENT. FOUND SMALL CRACK INDICATION AT THE LUG ON THE CASTING THAT IS THE ATTACH POINT FOR THE RETRACT CYLINDER. REMOVED AND REPLACED BRACKET ASSY AND TORQUED PER DC-9 OVERHAUL MANUAL 27-50-1. PART RECEIVED FROM DACO. RECONNECTED FLAP ACTUATOR PER MM AND THE OPERATIONAL CHECK WAS OKAY. (X) 2L72 4F A6WE 19950130001781995013000178WP 1995 1 30 HAL95002 119950103A5330 SKIN DOUG DC9 DC951 3022051WP FS 1209 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA38387 47689 HNL - ITEM FROM FORM 46 NR 138535 DURING SERVICE CHECK. RIGHT FUSELAGE SKIN CRACKED APPROXIMATELY .75 INCH AT STA 1209 APPROXIMATELY 13 INCHES ABOVE RIGHT ENGINE PYLON. REPAIRED MADE PER HAL AIRCRAFT REPAIR AUTHORIZATION FORM M105 FILE NR 71035. (CUT-OUT DAMAGE AND INSTALL FILLER AND DOUBLER.) (X) 2L72 4F A6WE 19950130001791995013000179WP 1995 1 30 HAL95003 119950103A5330 SKIN DOUG DC9 DC951 3022051WP FS 1209 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA38387 47689 HNL - ITEM FROM FORM 46 NR 138536 DURING SERVICE CHECK. LEFT FUSELAGE SKIN CRACKED APPROXIMATELY .6250 INCH AT STA 1209 APPROXIMATELY 9 INCHES ABOVE LEFT ENGINE PYLON. (X) 2L72 4F A6WE 19950130001801995013000180WP 1995 1 30 HAL95004 119950105A33501001191 EEL DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A HALAK NONE L NO TEST ININSP/MAINT 1 WP13601AP 1797 47658 HNL - ITEM FROM M-71, LOG PAGE NR 138673. THE EMERGENCY LIGHT AT THE ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS OKAY. (X) 2L72 4F A6WE 19950130001831995013000183SW 1995 1 30 LOSA9501 119950103A612031039391 ELBOW WOODWARD 8974106 FRCHLDSA227 SA227DC 3377521SW NR 2 ENGINE CRACKED A LOSAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP23451LA1372 2490726 DC849B PHX - NR 2 OIL PRESSURE FLICKERED AND THEN DROPPED TO ZERO. EXECUTED EMERGENCY ENGINE SHUT DONW. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 PROP GOVERNOR OIL LINE ELBOW CRACKED. REPLACED ELBOW ASSEMBLY PER MM 61-20-20. OPERATIONAL CHECKS AND LEAK CHECKS NORMAL. (X) 1L72 4T RTA18SW 19950130001841995013000184SW 1995 1 30 LOSA9502 119950103A3230ML1092 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG SHORTED A LOSAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23165SW24416 AC514 BFL - AFTER TAKEOFF, GEAR WOULD NOT RETRACT. LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO ONT FOR MAINTENANCE. MAINTENANCE FOUND NOSE GEAR UPLOCK SWITCH SHORTED. REMOVED AND REPLACED SWITCH ASSEMBLY PER MM 32-60-30. (X) 1L72 4T A8SW 19950130001851995013000185SW 1995 1 30 LOSA9503 119950109A2435 BEARING LUCAS 2307010 FRCHLDSA227 SA227DC 3377521SW RT STARTER/GEN SEIZED A LOSAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CLCLIMB 1 WP23451LA396 94103 DC849B LAX - ON TAKEOFF, RT GENERATOR FAIL LIGHT ILLUMINATED IN-FLIGHT. UNABLE TO RESET. AIR TURN BACK AND LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO ONT FOR MAINTENANCE. RT STARTER/GENERATOR FORWARD BEARING SEIZED. BAND RECEIVER SEVERED BEFORE SPLINE SHAFT COULD SHEAR OFF. REMOVED AND REPLACED RT STARTER/GENERATOR. INSPECTED GEAR BOX DRIVE PAD PRIOR TO INSTALLATION. PERFORMED ENGINE RUN-UP AND GENERATOR OPERATION CHECKED OKAY. (X) 1L72 4T RTA18SW 19950130001941995013000194NM 1995 1 30 TSAA9553001 119950103A5312 BULKHEAD BOEING737 737297 1384480NM BS 1016 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13728AL 22629 DURING SCHEDULED INSPECTION OF AFT PRESSURE BULKHEAD AT BS 1016, (AD 84-20-03), FOUND .75 INCH EXPOSED CRACK AT RIVET, LOCATED AT AFT CENTER PRESSURE BULKHEAD WEB AT 7 O'CLOCK POSITION. REPAIRED PER ECO 2544. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 26853:30. CYCLES: 65359. (X) 2L72 4F A16WE 19950130001951995013000195NM 1995 1 30 TSAA9553002 119950103A5330 SKIN BOEING737 7373Y0 1384671NM BS 357 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING SCHEDULED INSPECTION OF FUSELAGE SKIN AND FASTENER IN THE AREA OF THE 9.0 G NET ATTACHMENT, FOUND SKIN CRACK APPROXIMATELY .25 INCH AT BS 357 APPROXIMATELY 3 INCHES BELOW STR 8R. REPAIRED PER ECO 2517. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 22242:06. CYCLES: 25822. (X) 2L72 4F RTA16WE 19950130001961995013000196NM 1995 1 30 TSAA9553020 119950106A5312 BULKHEAD CHORD BOEING737 7372Q9 138448MNM BS 727 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13804AL 21719 DURING HEAVY MAINTENANCE VISIT, FOUND BS 727 BULKHEAD OUTER CHORD CRACKED BETWEEN S22L AND 23L, 5.25 INCHES LONG. STOP DRILLED PER SRM 51-10-01 IAW BOEING MESSAGE ALO-HNL 94-0388RR DATED 29 DECEMBER 94 AND REPAIRED PER ECO 1325. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950130001971995013000197NM 1995 1 30 WRLA94029 119950108A33500105606 EEL WIRE DOUG MD11 MD11 3023602NM CABIN FAILED A WRLAK NONE L NO TEST ININSP/MAINT 1 EA27271WA 48518 EMERGENCY LIGHT BATTERY NR 3 INDICATED LOW DURING PRE-FLIGHT CHECK. FOUND WIRE BARE AND SHORTED AT ROW 14 FLOOR TRACK ON RIGHT SIDE OF AIRCRAFT. REPLACED WIRE AND RE-TESTED EMERGENCY LIGHTS. EMERGENCY LIGHT TEST PASSED. (X) 2L73 4F RTA22WE 19950130002471995013000247NM 1995 1 30 9501225533 119950116A5313146N5444 LONGERON BOEING757 757251 1384970NM FS 1510 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01533US 24264 24264 DURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORTS AT FS 1510, RBL 3, LBL 3, AND LBL 7 WERE FOUND CORRODED. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-60-53, AND NWA EA 55-93708. 2L72 4F RTA2NM 19950130002481995013000248NE 1995 1 30 9501232717 219950123A7260 THREADS BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 GEAR BOX DAMAGED A NWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01721RC 22492 707907 IN CRUISE FLIGHT, NR 2 ENGINE OIL QUANTITY STARTED RAPIDLY DECREASING. A PRECAUTIONARY SHUTDOWN OF THE NR 2 ENGINE WAS PERFORMED A .8 GALLONS INDICATED OIL QUANTITY. FOUND THREADS IN THE GEARBOX CASE FOR THE LP6 FITTING PULLED OUT. THREADS WERE REPAIRED AND THE FITTING WAS REPLACED. SERVICED ENGINE OIL AND PERFORMED ENGINE RUNUP. SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950130002491995013000249WP 1995 1 30 9501249908 119950119A301039244421 REG VALVE DOUG DC9 DC931 3022065WP AFT ACCESS COMP MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01958N 33065274 47254 DURING CLIMB-OUT FROM MSN, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY OPERATING PROCEDURES AND DETERMINED LOSS OF WING AND TAIL ICE PROTECTION. FLIGHT DIVERTED TO MSP, AND LANDED WITHOUT INCIDENT. REPLACED ICE PROTECTION REGULATOR VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130002501995013000250 1995 1 30 9501259961 419950119A3454 NAV RECEIVERS DOUG DC9 DC931 3022065WP NR 1/2 MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER APAPPROACH 1 GL01924RW 47185 LOSS OF NR 1 VHF NAV OCCURRED ON APPROACH INTO BIS. CIRCUIT BREAKER POPPED AND WOULD NOT RESET. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RADIO NAV SWITCHING UNIT AND BOTH NR 1 AND NR 2 NAV RECEIVERS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130002511995013000251WP 1995 1 30 9501261146 119950123A5742 BOLT DOUG DC10 DC1040 3023508WP WING/PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, CRACK INDICATIONS WERE FOUND ON THE WING PYLON TO FRONT SPAR FITTING ATTACH NR 2 LOWER BOLT. REPLACED NR 2 AND NR 4 LOWER BOLTS. 2L73 4F A22WE 19950130002521995013000252WP 1995 1 30 9501271146 119950123A5330 SKIN DOUG DC10 DC1040 3023508WP LWR FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE MOUNTING RINGS UNDER THE FOUR RADIO ALTIMETER ANTENNAS. INSTALLED TITANIUM DOUBLERS PER EA 11-96572. 2L73 4F A22WE 19950130002531995013000253WP 1995 1 30 9501281146 119950123A5312 BULKHEAD ANGLE DOUG DC10 DC1040 3023508WP CTR WHEEL WELL CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SUPPORT ANGLE OF THE FORWARD BULKHEAD IN THE CENTER WHEEL WELL, AT RBL 10-29. INSTALLED REPAIR ANGLE PER EA 11-93766. 2L73 4F A22WE 19950130002541995013000254NM 1995 1 30 9501296612 119950118A5313 LONGERON BOEING747 747251B 1384892NM FS 520-740 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, FOUND SKIN PANEL CORRODED BETWEEN OUTER SKIN AND TEAR STRAPS IN NUMEROUS AREAS, FS 520 TO 740, STR 39R-44R. FABRICATED SKIN AND INSTALLED REPAIR. 2L74 4F A20WE 19950130002551995013000255WP 1995 1 30 9501301146 119950112A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1801-1815 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC INSPECTION, CORROSION WAS FOUND IN THE AFT CARGO COMPARTMENT AT FS 1801-1815, STR 44R. REPLACED LONGERON PER EA 11-96636. 2L73 4F A22WE 19950130002561995013000256NM 1995 1 30 9501316612 119950111A5230 STIFFENER BOEING747 747251B 1384892NM CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, FOUND THE FORWARD CARGO DOOR ANGLE STIFFENER TO DOOR SKIN ABOVE FORWARD OPENING ARM FITTING WITH A 2 INCH CRACK. FABRICATED NEW PART FROM .063 INCH 7075-0 AND INSTALLED REPAIR. 2L74 4F A20WE 19950130002571995013000257EU 1995 1 30 9501323205 419950120A3417HG1150AC05 ADC AIRBUS320 A320211 3930320EU AVIONICS COMPT MALFUNCTIONED A ANWAAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL01305US9444 9444 41 DURING APPROACH INTO BOS, RECEIVED 'F/CTL ADR DISAGREE' MESSAGE. DUE TO SEVERE WEATHER IN THE APPROACH PATH INTO BOS, CREW ELECTED TO DIVERT TO PHL. AN EMERGENCY WAS DECLARED, AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA INERTIAL REFERENCE UNIT COMPUTER, AND THE NR 2 SPOILER ELEVATOR COMPUTER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950130002581995013000258WP 1995 1 30 ABXA9500042 119950113A32313923167505 ARM DOUG DC9 DC932F 3022067WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR FLYING DOOR ARM WORN. REPLACED ROD END IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950130002611995013000261WP 1995 1 30 ABXA9500045 119950117A5320591015835 DOOR JAMB DOUG DC9 DC932F 3022067WP FS 917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND AFT LOWER CARGO DOOR JAMB WEB HAD LEVEL I CORROSION. REPAIRED IAW ABX REA D953-10762-MR. 2L72 4F A6WE 19950130002621995013000262WP 1995 1 30 ABXA9500046 119950117A5320591015837 DOOR JAMB DOUG DC9 DC932F 3022067WP FS 917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND AFT LOWER CARGO DOOR JAMB WEB HAD LEVEL I CORROSION. REPAIRED WEB IAW ABX REA D953-10762-MR. 2L72 4F A6WE 19950130002631995013000263WP 1995 1 30 ABXA9500047 119950121A531199211793 FRAME DOUG DC9 DC932F 3022067WP FS 446 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND FRAME STA 446 GOUGE BLEND OUT IN OUTSIDE RADIUS ADJACENT TO LONGERON 8L. REPAIRED GOUGE BLEND OUT PER ABX REA D953-10779-MR. 2L72 4F A6WE 19950130002641995013000264WP 1995 1 30 ABXA9500048 119950118A5312991855335 BLKHD TEE DOUG DC9 DC932F 3022067WP FS 965 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND BULKHEAD STA 965 INBOARD T-CAP HAD GOUGES AND DRILL STARTS FROM LONGERON 18L TO 18R, FORWARD AND AFT EDGES. REPAIRED IAW DC-9 SRM 53-01 FIGURE 1 SHEET 3 AND ABX REA D953-10788-MR. 2L72 4F A6WE 19950130002651995013000265WP 1995 1 30 ABXA9500049 119950118A531159203371 FRAME DOUG DC9 DC932F 3022067WP FS 598 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION, FOUND HOLE IN FRAME 598 AT LONGERON 10L. REPAIRED FRAME IAW DC-9 SRM 51-30-2 AND ABX REA D953-10764-MR. 2L72 4F A6WE 19950130002661995013000266WP 1995 1 30 ABXA9500050 119950117A32313923159507 LINK DOUG DC9 DC932F 3022067WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR FLYING DOOR LINK HAD EXCESSIVE PLAY. REPLACED LINK ASSEMBLY IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950130002671995013000267WP 1995 1 30 ABXA9500051 119950117A3231DREMS5085 ROD ASSEMBLY DOUG DC9 DC932F 3022067WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR FLYING DOOR ROD ASSEMBLY HAD EXCESSIVE PLAY. REPLACED ROD ASSEMBLY IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950130002681995013000268 1995 1 30 ABXA9500052 419950121A3454066106001 RECEIVER DOUG DC9 DC941 302207NWP NR 1 DEFECTIVE A AABXAB EMER. DESCENT O OTHER APAPPROACH 1 GL23969AX 4773 47464 DURING APPROACH, ALL NAVIGATIONAL RADIOS LOST. AIRCRAFT HAD MODERATE ICING AT THE TIME. CDI NEEDLES WERE ERRATIC DURING PREVIOUS HOLDING PATTERN. CHECKED NAV ANTENNA SYSTEM FOR CONTINUITY AND SYSTEM CHECKED GOOD. CHECKED NAV ANTENNA COAXIAL CONNECTIONS IN AFT BAG BIN FEED THROUGH. CLEANED COAXIAL CONNECTIONS AT NAV ANTENNA ON VERTICAL STABILIZER. CHECKED GOOD, REPLACED NR 1 AND NR 2 NAV RECEIVERS. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 34-32. 2L72 4F A6WE 19950130002691995013000269 1995 1 30 ABXA9500053 419950121A3454066106000 RECEIVER DOUG DC9 DC941 302207NWP NR 2 DEFECTIVE A AABXAB EMER. DESCENT O OTHER APAPPROACH 1 GL23969AX4 4 47464 DURING APPROACH ALL NAVIGATIONAL RADIOS LOST. AIRCRAFT HAD MODERATE ICING AT THE TIME. CDI NEEDLES WERE ERRATIC DURING PREVIOUS HOLDING PATTERN. CHECKED NAV ANTENNA SYSTEM FOR CONTINUITY AND SYSTEM CHECKED GOOD. CHECKED NAV ANTENNA COAXIAL CONNECTIONS IN AFT BAG BIN FEED THROUGH. CLEANED COAXIAL CONNECTIONS AT NAV ANTENNA ON VERTICAL STABILIZER. CHECKED GOOD. REPLACED NR 1 AND NR 2 NAV RECEIVERS. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 34-32. 2L72 4F A6WE 19950130002701995013000270WP 1995 1 30 ABXA9500054 119950119A25105641031519 SEAT DOUG DC8 DC861 3021952WP LT COCKPIT WON'T LOCK A ABXAK NONE O OTHER CRCRUISE 1 GL23842AX 46015 CAPTAIN'S SEAT DOES NOT LOCK IN THE FORE AND AFT POSITION. PIN DOES NOT ENGAGE IN RAIL. REMOVED AND REPLACED CAPTAIN'S SEAT AFTER RETURN FLIGHT TO ILN. SEAT OPS CHECKED GOOD, IAW DC8 MM CHAPTER 25. 2L74 4F 4A25 19950130002711995013000271SO 1995 1 30 COM11737 119950122A79303022375 SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMAK NONE O OTHER CRCRUISE 1 SO01168CA 120168 115249 RT ENGINE OIL PRESSURE FLUCTUATING. REPLACED THE CENTRIFUGAL AIR/OIL SEPARATOR SEAL. 2L72 4T4 TRTA31SO E20NE 19950130002721995013000272SO 1995 1 30 COM11738 119950123A3260922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01255CA 120238 LT MLG GREEN SAFE LIGHT IS INOP, AND RED INTRANSIT LIGHT IS ILLUMINATED. REPLACED THE DOWN LOCK PROXIMITY SENSOR. 2L72 4T RTA31SO 19950130002731995013000273NE 1995 1 30 COM11739 219950123A73103035729 FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DIRTY A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO011117H 120117 115574 THE RT ENGINE FUEL FILTER WARNING LIGHT ILLUMINATED. REPLACED FUEL FILTER. 2L72 4T4 TRTA31SO E20NE 19950130002741995013000274SO 1995 1 30 COM11740 119950122A323012043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01243CA9998 2159 120212 LANDING GEAR WOULD NOT RETRACT. CONTROL HANDLE COULD BE SELECTED UP. REPLACED THE LANDING GEAR RELAY BOX. 2L72 4T RTA31SO 19950130002751995013000275EA 1995 1 30 COM60390 119950123A3240 BRAKES CNDAIRCL600 CL6002B19 EA MAIN GEAR CONTAMINATED A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO01933CA 7040 TOWER PERSONNEL REPORTED HEAVY SMOKE COMING FROM MLG. FOUND SMOKE TO BE CAUSED BY DE-ICING GLYCOL ON BRAKES. CLEANED BRAKE ASSY, AND AIRCRAFT CONTINUED SERVICE. 2L72 4F RTA21EA 19950130002761995013000276EA 1995 1 30 COM60391 119950123A3230 UPLOCKS CNDAIRCL600 CL6002B19 EA LANDING GEAR DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01936CA 7043 THE MLG WOULD NOT FULLY RETRACT. GEAR DISAGREE MESSAGE ON EICAS. CLEANED ICE AND GRIT FROM UPLOCKS. GEAR RETRACT CHECK NORMAL. 2L72 4F RTA21EA 19950130002791995013000279NM 1995 1 30 DL72L950326 119950122A2730401602783 SWITCH BOEING727 727232 1384082NM ELEVATOR SYSTEM FAULTY A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11514DA 21430 DURING CLIMB THROUGH 12,000 FEET ELEVATOR FEEL DIFF, PRESSURE LIGHT ILLUMINATED. PERFORMED PROCEDURES IAW POM, FOUND NO OTHER DISCREPANCIES. AFTER ONE HOUR AT CRUISE, LIGHT EXTINGUISHED FOR 5 MINUTES THEN ILLUMINATED, THEN LIGHT EXTINGUISHED IN DESCENT. LANDED IN ATL. REPLACED ELEVATOR FEEL COMPUTER DIFFERENTIAL PRESSURE SWITCH. OPS CHECK NORMAL. 2L73 4F A3WE 19950130002801995013000280NM 1995 1 30 DL72S950288 119950102A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11524DA 21584 DURING SHOP INSPECTION, LEFT WING NR 3 SLAT WAS FOUND WITH NR 3, NR 7, NR 9 AND NR 10 RIBS CRACKED. REPAIRED PER SRM 57-50-3 AND SRM 57-54-0 FIG 804. 2L73 4F A3WE 19950130002811995013000281NM 1995 1 30 DL72S950313 119950121A213065602413 DUCT BOEING727 727232 1384082NM AC COMPARTMENT BROKEN A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11490DA 21020 DURING CLIMB-OUT, AIRCRAFT WOULD NOT HOLD PRESSURE, SELECTED ALTERNATE BLEED WITH NO HELP. DIVERTED TO MCO. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY LEAKING AIR. ALSO, FOUND DUCT FROM MIX VALVE TO SEPARATOR ASSEMBLY BROKEN IN SEVERAL PLACES. REPLACED DUCT OPERATION NORMAL. 2L73 4F A3WE 19950130002831995013000283NM 1995 1 30 DL73E950289 119950108A52476550904271 SKIN BOEING737 737247 138448DNM APU DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11377DL 23604 DURING SHOP INSPCTION, APU COMPARTMENT DOOR WAS FOUND WITH THE OUTER SKIN GOUGED THROUGH, AT 31.5 INCHES FROM THE AFT END OF DOOR. REPAIRED PER SRM 52-00-3. 2L72 4F A16WE 19950130002841995013000284NM 1995 1 30 DL757950328 119950122A2421729825G IDG BOEING757 757232 1384965NM NR 2 ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO11642DL 23996 DURING CRUISE, RIGHT GENERATOR DRIVE LIGHT COME ON. DISCONNECTED GENERATOR PER POM. APU FAILED REPEATED START ATTEMPTS, DIVERTED MCO. REPLACED RT IDG, AND APU FUEL CONTROL AND FLOW DIVIDER. OPERATION NORMAL. 2L72 4F RTA2NM 19950130002851995013000285NM 1995 1 30 DL76S950302 119950122A2121 COOLING FAN 732591D BOEING767 767332 1382001NM FWD CARGO MALFUNCTIONED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11135DL 25145 JUST PRIOR TO DESCENT, HEAVY SMELL OF ELECTICAL WIRE HEATING. FOUND 6H21 EXHAUST FAN C/B OUT. SELECTED OVERIDE ON EQUIPMENT COOLING, AND SMELL WENT AWAY. FWD TO MCO AND PLACARD MEL 21-58-04B C/B COLLARD. REPLACED FWD EQUIPMENT COOLING FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19950130002861995013000286NE 1995 1 30 DLL10950327 219950122A7310RB21122B02 FUEL LINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 1 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11714DA43004 193C1090 010616 DURING CRUISE, NR 1 FUEL PRESSURE LIGHT ILLUMINATED. OBSERVED LOOSING FUEL FROM AREA UNDERNEATH NR 1 ENGINE POD. SHUTDOWN NR 1 ENGINE RETURNED TO HNL. FOUND MISALIGNED FUEL LINE TO FUEL/OIL HEAT EXCHANGER AND CUT SEALS. REPLACED SEALS AND REALIGNED FUEL LINE. LEAK CHECK OK, RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 19950130002871995013000287 1995 1 30 DLL14950312 419950120A34174031800902 ADC LKHEED1011 1011385115 5265015WP E/E COMPARTMENT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11737D 193C1228 DURING CRUISE, F/O INSTRUMENT WARNING FLAGS APPEARED INTERMITENTLY, ADC INSTRUMENTS FLUCTUATE. DIVERTED TO LAX. REPLACED AIR DATA COMPUTER. LEAK CHECK OK, RETURNED TO SERVICE. 2L73 4F A23WE 19950130002881995013000288WP 1995 1 30 DLL16950306 119950105A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 281 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL, CORROSION WAS FOUND ON FLOOR BEAM AT FS 281 LT SIDE ALONG TOP SURFACE FROM DOOR TO AFT CENTERLINE. REMOVED DAMAGED SECTION AND INSTALLED NEW T-SECTION PER SRM 53-21-00 PG 849-852 2L73 4F A23WE 19950130002891995013000289WP 1995 1 30 DLL16950307 119950106A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL, CABIN FLOOR BEAM CAP FROM RBL 42.5 TO RBL 74.5 WAS FOUND CORRODED. ALSO, CORROSION ON UNDERSIDE AT FASTENER HOLES FS 901. REMOVED CAP, INSTALLED REPAIR PER SRM 53-21-00 PG 849-852. 2L73 4F A23WE 19950130002901995013000290WP 1995 1 30 DLL16950308 119950106A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 1763 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURRING OVERHAUL FOUND, FLOOR BEAM UPPER FLANGE TOP SURFACE CORRODED AT STA 1763, LBL 36 TO LBL 54. ALSO, SEVERAL PLACES ON LWR SURFACE AT SAME CLIP NUT HOLES. INSTALLED NEW SECTION OF T-CAP PER SRM 53-21-00 PG 849-852. 2L73 4F A23WE 19950130002911995013000291WP 1995 1 30 DLL16950309 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 933 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL, FOUND TEAR STRAP DISBONDED BETWEEN STA 943-923, BETWEEN STR 35 & 36. CUT TEAR STRAP, CLEANED CORROSION AND REPAIRED PER SRM 53-31-00 PG 801. 2L73 4F A23WE 19950130002921995013000292WP 1995 1 30 DLL16950310 119950105A5320 ANGLE LKHEED1011 10113853 5265020WP FS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING OVERHAUL, FOUND ANGLE AT STA 1103 RT SIDE, AT AFT SIDE OF FRAME AT FLOOR LINE CRACKED. REMOVED ANGLE, REPAIRED FRAME ATTACH TAB ON OUTBOARD END OF STA 1103, FRAME TO SEAT T-RACK TENSION TIE FITTING PER SRM 53-21-00 PG 853. 2L73 4F A23WE 19950130002931995013000293WP 1995 1 30 DLL16950320 119950122A5320 INTERCOSTAL LKHEED1011 10113853 5265020WP FS 1778-1792 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND THE INTERCOSTAL CAP CRACKED BETWEEN FS 1778 TO FS 1792, AT LBL 40. REPLACED CAP PER SRM 51-10-05. 2L73 4F A23WE 19950130002941995013000294WP 1995 1 30 DLL16950321 119950105A5320 FORMER LKHEED1011 10113853 5265020WP FS 267 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FORMER WAS FOUND CORRODED AT FS 267, BELOW STR 21 JUST OUTBOARD OF NR 3 RAM AIR INLET SCOOP (AFT SIDE). REMOVED DAMAGED SECTION OF FRAME ANGLE, AND INSTALLED REPAIR PER SRM 53-12-00 FIG 805. 2L73 4F A23WE 19950130002951995013000295WP 1995 1 30 DLL16950322 119950104A5313 STRINGER LKHEED1011 10113853 5265020WP FS 963-983 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND STRINGER 33 WITH CORROSION DAMAGE AT FS 983 AND 963. ALSO, LIGHT CORROSION ON FS 963 FRAME, JUST INBOARD OF STRINGER 34. REPAIRED PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950130002961995013000296WP 1995 1 30 DLL16950323 119950118A5330 SKIN LKHEED1011 10113853 5265020WP FS 933 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, THE 0.020 INCH BONDED INTERNAL SKIN WAS FOUND CORRODED AT FS 933, BETWEEN STRINGERS 30 AND 31. REPAIRED PER SRM 53-31-00 FIG 836. 2L73 4F A23WE 19950130002971995013000297WP 1995 1 30 DLL16950324 119950106A5320 PRESSURE DECK LKHEED1011 10113853 5265020WP FS 349 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND PRESSURE DECK CORRODED AFT OF STIFFENER AT FS 349, AND OUTBOARD OF BL 0 UNDER THE RT FWD LAV. REPAIRED PER SRM 53-11-00 PG 922. 2L73 4F A23WE 19950130002981995013000298NM 1995 1 30 UPS202091 119950124A5313 STRINGER BOEING727 727185C 138406NNM BS 294.5 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINT FOUND STR 15 AT BS 294.5 LEFT SIDE HAS A CRACK AT THE UPPER FLANGE ATTACH POINT LEFT SIDE. X-RAY NR 14-15 LEFT. INSTALLED REPAIR IAW EO 727-5310-1259F. 2L73 4F A3WE 19950130008461995013000846NM 1995 1 30 95ZZZX426 119950105A3231661516624 CONTROL CABLE BOEING727 727224 1384076NM NLG DOOR CORRODED A CALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0979746 22449 EWR - FLT 0232 - NOSE GEAR DOOR OPEN LIGHT ON FORWARD PANEL AND SECOND OFFICER'S PANEL REMAINED ILLUMINATED AFTER RAISING THE LANDING GEAR ON TAKEOFF FROM EWR. CYCLING GEAR DID NOT HELP. CREW CONFIRMED DOOR WAS OPEN BY VISUAL INSPECTION THROUGH THE VIEW PORT. AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOOR CABLES WITH ZERO TENSION AND BOTH CABLES STRETCHED AND CORRODED. CABLE PIVOT QUADRANT WAS WORN IN CABLE GROOVE AND CORRODED. CABLES AND QUADRANT WERE REMOVED AND REPLACED. AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 32-22-1, PAGE 501. NOSE GEAR WAS SWUNG SEVERAL TIMES WITH ALL OPERATION AND INDICATIONS CHECKING GOOD. REF CONTL NR CAL95-0013. 2L73 4F A3WE 19950130008471995013000847EU 1995 1 30 C2XA25IA002 119950113A2730S27381953200 BEARING AEROSPATR42 ATR42320 8680930EU ELEVATOR RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914834 193 IAH - DURING C-CHECK INSPECTION, FOUND ELEVATOR TORQUE TUBE, LT OUTER PITCH UNCOUPLING MECHANISM BEARING RUSTED. MAINTENANCE REMOVED AND REPLACED THE BEARING IAW ATR 42 MM 27-31-42 RAI-10000-005. A/C TT 9,267.5. CYC. 11,818. (X) 2H72 4T RTA53EU 19950130008481995013000848SO 1995 1 30 C2XA95CL002 119950103A3242214791 BRAKE EMB 120 EMB120RT SO RT MLG LOCKED A C2XAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW09167248151 0566 120171 EWR/BGM - FLT 3453 - RIGHT OUTBOARD BRAKE LOCKED UP DURING TAXI IN EWR. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED NR 4 BRAKE ASSY. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950130008491995013000849 1995 1 30 C2XA95CL003 419950114A61137847841 SPINNER BULKHEADHAMSTD EMB 120 EMB120RT SO RT PROPELLER LOOSE A AC2XAO OTHER J WARNING INDICATION ININSP/MAINT 1 SW09347125106 219 120111 RIC/CLE - FLT 3273 - FLIGHT CREW REPORTED RIGHT PROP DE-ICE AND PROP SYNC INOPERATIVE AFTER LANDING IN CLE. UPON INSPECTION, MAINTENANCE FOUND NR 2 PROP SPINNER BULKHEAD HAD 2 SHEARED BOLTS AND 2 BOLTS BACKED OUT. DAMAGE HAD OCCURRED TO THE PROP ASSY DUE TO THE LOOSE SPINNER BULKHEAD. MAINTENANCE REMOVED AND REPLACED THE RIGHT PROPELLER ASSY IAW HAMSTD MM 61-10-00. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950130008501995013000850EU 1995 1 30 C2XA95IA001 119950112A5320MS204704 RIVET AEROSPATR42 ATR42320 8680930EU FRAME 22 MISSING A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914834 193 IAH - DURING C-CHECK INSPECTION, FOUND ONE MISSING RIVET ON STR 18, RT SIDE, JUST BELOW FRAME 22. MAINTENANCE PERFORMED AN INTERIM REPAIR BY PROTECTING AND SEALING VACANT HOLE PER CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5330-01073. TT 9,267.5. CYC. - 11,818. (X). 2H72 4T RTA53EU 19950130008521995013000852NE 1995 1 30 CAL950011 219950104A7261 OIL PRESS TUBE BOEING727 727224 1384076NM PWA JT8 JT8D9 52048NE NR 6 BEARING BROKEN A CALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0966734 20663 666322 GSO - FLT 0383 - THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM EWR TO RSW. THE OIL PRESSURE DECREASED TO THE YELLOW ARC. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 6 BEARING OIL PRESSURE TUBE FOR ENGINE NR 1 BROKEN. THE NR 6 BEARING OIL PRESSURE TUBE WAS REMOVED AND REPLACED. THE NR 1 ENGINE WAS RUN AND NO LEAKS WERE NOTED. (X) 2L73 4F4 F A3WE E2EA 19950130008531995013000853NM 1995 1 30 CAL950013 119950105A3231661516623 CONTROL CABLE BOEING727 727224 1384076NM NLG DOOR CORRODED A CALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW0979746 22449 EWR - FLT 0232 - NOSE GEAR DOOR OPEN LIGHT ON FORWARD PANEL AND SECOND OFFICER'S PANEL REMAINED ILLUMINATED AFTER RAISING THE LANDING GEAR ON TAKEOFF FROM EWR. CYCLING GEAR DID NOT HELP. CREW CONFIRMED DOOR WAS OPEN BY VISUAL INSPECTION THROUGH THE VIEW PORT. AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOOR CABLES WITH ZERO TENSION AND BOTH CABLES STRETCHED AND CORRODED. CABLE PIVOT QUADRANT WAS WORN IN CABLE GROOVE AND CORRODED. CABLES AND QUADRANT WERE REMOVED AND REPLACED. AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 32-22-1, PAGE 501. NOSE GEAR WAS SWUNG SEVERAL TIMES WITH ALL OPERATION AND INDICATIONS CHECKING GOOD. REF CONTL NR 95ZZZX426. (X) 2L73 4F A3WE 19950130008621995013000862NM 1995 1 30 CAL950028 119950110A2750652661465 TRANSMISSION BOEING727 727227 1384078NM LT TE FLAP BINDING A ACALAO OTHER J WARNING INDICATION CLCLIMB 1 SW09107569807 5413 21042 IAH - FLT 0407 - THE INBOARD FLAPS FAILED TO RETRACT INITIALLY DURING FLAP RETRACTION AFTER TAKEOFF. THE FLAPS RETRACTED USING ALTERNATE FLAP RETRACTION PROCEDURES. THE INBOARD FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES DURING LANDING. THE INBOARD FLAPS HAD A HISTORY OF BINDING BOTH ON THE GROUND AND IN-FLIGHT. MAINTENANCE FOUND THE NR 4 FLAP TRANSMISSION BINDING. THE NR 4 FLAP TRANSMISSION WAS REMOVED AND REPLACED. OPERATION OF THE FLAPS CHECKED GOOD. (X) 2L73 4F A3WE 19950130008631995013000863NM 1995 1 30 CAL950029 119950108A2750652355936 TRANSMISSION BOEING727 727224 1384076NM RT TE FLAP INOPERATIVE A ACALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09697353896915060 20664 IAH - FLT 0414 - THE OUTBOARD FLAPS HAD A HISTORY OF NOT EXTENDING BOTH ON THE GROUND AND IN-FLIGHT. MAINTENANCE FOUND EXCESSIVE SHAFT PLAY IN THE NR 8 FLAP TRANSMISSION. THE NR 8 FLAP TRANSMISSION WAS REMOVED AND REPLACED. THE FLAPS WERE OPERATED ELECTRICALLY AND HYDRAULICALLY AND ALL CHECKED NORMAL. THE AIRCRAFT HAS COMPLETED AT LEAST FOUR FLIGHTS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED, AND THERE HAVE BEEN NO REPEATS OF FLAP BINDING PROBLEMS. (X) 2L73 4F A3WE 19950130008641995013000864NM 1995 1 30 CAL950030 119950107A29136506501 HYDRAULIC PUMP BOEING727 727225 1384077NM NR 2 ENGINE CASE SPLIT A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW098885Z15371 21854 PTY - FLT 0770 - THE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT FLICKERED ON AND OFF AFTER TAKEOFF AND WAS FOLLOWED BY LOSS OF THE A-SYSTEM HYDRAULIC QUANTITY. THE AIRCRAFT WAS RETURNED TO PTY WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PUMP CASE SPLIT. THE NR 2 HYDRAULIC PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 ENGINE HYDRAULIC PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE. OPERATIONAL AND LEAK CHECKS AFTER HYDRAULIC SYSTEM SERVICING WERE GOOD. (X) 2L73 4F A3WE 19950130008661995013000866WP 1995 1 30 95112 119950122A53205912528501 DOOR JAMB SILL DOUG DC9 DC915 3022036WP AFT CARGO COMPT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 DURING INSP OF AFT CARGO COMPARTMENT DOOR JAMB SILL AREA, CORROSION WAS FOUND ON ATTACHING INTERCOSTAL WEB 2 GUSSETS, AND 2 CLIPS, THAT ATTACH DOOR JAMB SILL AT STA 758.00 LONGERON 29 RIGHT. REMOVED CORRODED PARTS, FABRICATED NEW AND INSTALLED CLIPS, GUSSETS, AND WEB IAW 51-30-5. REMOVED CORRODED INTERCOSTAL AND FABRICATED NEW IAW 51-10-2A AND INSTALLED IAW 51-30-5. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130008671995013000867NM 1995 1 30 95FDEA00064 119950121A5320651841568 STIFFENER BOEING727 72725 1384006NM BS 327 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION ON VERTICAL STIFFENER BS 327, RBL 14, WL 182. REMOVED AND REPLACED STIFFENER AT BS 327, RBL 14, WL 182. 2L73 4F A3WE 19950130008681995013000868NM 1995 1 30 95FDEA00065 119950122A5313BAC498142 STRINGER BOEING727 72725 1384006NM BS 486 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 BS 486, STR 21L, WL 175 CRACKED. REPAIRED CRACKED STR AT BS 486, STR 21L, WL 175 PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950130008691995013000869NM 1995 1 30 95FDEA00066 119950122A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 520-580 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION AT (71C209-02) BS 534-541, WL 156, LBL 18 ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK BS 520-580, LB 18 WL 156. 2L73 4F A3WE 19950130008701995013000870NM 1995 1 30 95FDEA00067 119950122A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 1090 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION (71C709-02) AT BS 1090 PLUS 7, WL 148, RBL 15 UNDER NUTPLATES. REMOVED AND REPLACED WITH NEW CARGO SEAT TRACK BS 1130-1010, RBL 15, WL 148. 2L73 4F A3WE 19950130008711995013000871NM 1995 1 30 95FDEA00068 119950122A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 1110 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION (71C709-02) AT BS 1110-8, WL 149, RBL 13 ON SPLICE PLATE. REMOVED AND REPLACED CARGO SEAT TRACK FROM BS 1130-1010, RBL 15, WL 148. 2L73 4F A3WE 19950130008721995013000872NM 1995 1 30 95FDEA00069 119950122A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 1030 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION (71C709-02) ON FLOOR TRACK AND SPLICE PLATE AT BS 1030-6, STR 28R, RBL 12, WL 147. REMOVED AND REPLACED CARGO SEAT TRACK FROM BS 1130-1010, RBL 15, WL 148. 2L73 4F A3WE 19950130008731995013000873NM 1995 1 30 95FDEA00070 119950121A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 1050-1070 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION (71C709-02) UNDER NUTPLATES FROM BS 1050-1070, STR 28R, RBL 15. REMOVED AND REPLACED SEAT TRACK BS 1130-1010, RBL 15, WL 148. ALL WORK DONE IAW SRM 53-10-5. 2L73 4F A3WE 19950130008741995013000874NM 1995 1 30 95FDEA00071 119950121A5320651627910 BEAM BOEING727 72725 1384006NM BS 805 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION ON UPPER CHORD OF LONGITUDINAL BEAM BS 805 PLUS 14 INCHES, RBL 45, WL 208. REMOVED AND REPLACED UPPER CHORD OF LONGITUDINAL BEAM FROM BS 740-850, RBL 45, WL 208. 2L73 4F A3WE 19950130008751995013000875NM 1995 1 30 95FDEA00072 119950121A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 900 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 DAMAGE ON SEAT TRACK BS 900, RBL 25, WL 208. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM BS 850-950, RBL 25, WL 208. ALL WORK DONE IAW SRM 53-10-5. 2L73 4F A3WE 19950130008761995013000876NM 1995 1 30 95FDEA00073 119950121A5320651627910 BEAM BOEING727 72725 1384006NM BS 760-810 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION ON INBOARD FLANGE BS 810-760, RBL 25, WL 208 ON LONGITUDINAL BEAM. REMOVED AND REPLACED UPPER CHORD OF LONGITUDINAL BEAM FROM BS 740-850, RBL 25, WL 208. ALL WORK DONE IAW SR 53-10-2. 2L73 4F A3WE 19950130008771995013000877NM 1995 1 30 95FDEA00074 119950123A5320BAC1510190 SUPPORT BOEING727 72721C 138400MNM BS 320 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04103FE 19136 2 CORRODED FASTENERS RBL 40, BS 320, WL 208 UNDERSIDE OF BEAM AND CHORD. ALSO, FOUND FLOOR SUPPORT CORRODED. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT PER BOEING DRAWING 65-26173, FEDEX SRM 51-10-02, 51-30-2 AND MM 51-20-21. 2L73 4F A3WE 19950130008781995013000878NM 1995 1 30 95FDEA00075 119950111A5347BAC15201432 SEAT TRACK BOEING727 72721C 138400MNM FS 870-1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 SEAT TRACK CORRODED WL 208, LBL 25, STA 870-1070. REMOVED AND REPLACED NEW SEAT TRACK BS 870-1070, LBL 25, WL 208 IAW FEDEX 727 SRM 53-10-5. 2L73 4F A3WE 19950130008791995013000879NM 1995 1 30 95FDEA00076 119950123A532069246212 EXPANSION LINK BOEING727 72721C 138400MNM FS 848 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 EXPANSION LINK BETWEEN STA 848-87, LBL 25, WL 208 IS CORRODED BEYOND LIMITS. REMOVED CORROSION, TREATED AND PRIMED ALL PER SRM 51-10-6, 53-10-1 AND FEDEX EA 7-5310-23666. 2L73 4F A3WE 19950130008801995013000880NM 1995 1 30 95FDEA00077 119950113A5320M400956 BRACKET BOEING727 72721C 138400MNM BS 303 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 WHILE WORKING CARD NR 0278 FOUND BRACKET STA 303, LBL 32 CRACKED WL 208. REMOVED AND REPLACED BRACKET PER SRM 51-20-1. 2L73 4F A3WE 19950130008811995013000881NM 1995 1 30 95FDEA00078 119950123A5347 SEAT TRACK BOEING727 72725 1384006NM BS 540 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION (71C209-02) BS 540, STR 27, WL 156 UNDER NUTPLATE ON SEAT TRACK. REMOVED AND REPLACED SEAT TRACK FROM BS 520-560. ALL WORK DONE PER IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950130008821995013000882NM 1995 1 30 95FDEA00079 119950123A5320 TERMINAL CHORD BOEING727 72725 1384006NM BS 879 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 DURING UT INSPECTION OF BS 879 TERMINAL FITTING OUTER CHORD, FOUND 1 INCH LONG CRACK LOCATED 1 INCH BELOW STR 9L CENTERLINE. REPAIRED CRACK IN BS 870 TERMINAL FITTING 1 INCH BELOW STR 9L, IAW BOEING SB 727-53-0194 AND FEDEX EA 7-5310-23663. 2L73 4F A3WE 19950130008831995013000883NM 1995 1 30 95FDEA00080 119950123A5330M374323 SKIN BOEING727 72721C 138400MNM BS 1345 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 18136 GOUGE IN SKIN BS 1345 STR 11L. CUT OUT DAMAGE AT BS 1345, STR 11L. FABRICATED, INSTALLED DOUBLER AND FILLER PER FEDEX SRM 54-30-3. 2L73 4F A3WE 19950130008841995013000884NM 1995 1 30 95FDEA00081 119950123A5313TPN1 STRINGER BOEING727 72721C 138400MNM BS 441.5 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 TOOLING MARKS BS 441.5, STR NR 1 LT AND RT. REMOVED SECTION OF STR, AND CUT OUT A REPLACEMENT SECTION. FABRICATED AND SPLICED IN PER SRM FEDEX 53-10-3 AT STR NR 1 STA 430-450. 2L73 4F A3WE 19950130008851995013000885NM 1995 1 30 95FDEA00082 119950123A53302024T3 SKIN BOEING727 7272S2F 1384O81NM BS 1284 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04205FE 22927 DENT WITH GOUGE 1 INCH W BY 1.5 INCH L BY .075 INCH D, BS 1284, JUST ABOVE STR 22R FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE AREA IN ACCORDANCE WITH FEDEX SRM 53-30-3 FIG 1 AT BS 1284 STR 22R. 2L73 4F A3WE 19950130008861995013000886NM 1995 1 30 95FDEA00083 119950124A53117075T6 FRAME BOEING727 72721C 138400MNM BS 1110 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 CORROSION AT BS 1110, WL 154, RBL 25 UNDER TOP FLANGE OF FRAME. REPAIRED FLANGE OF FRAME PER FEDEX SRM 51-40-3 FIG 1 AND 3. 2L73 4F A3WE 19950130008871995013000887NM 1995 1 30 95FDEA00084 119950117A5320M374333 ANGLE BOEING727 72721C 138400MNM BS 294-312 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 WEB AT LBL 42 BETWEEN BS 294 AND 312 HAS CRACK ON EXISTING REPAIR ANGLE, WL 207. REMOVED WEB, FABRICATED, ALODINED, PRIMED AND PAINTED. INSTALLED FABRICATED WEB AT LBL 42 BETWEEN BS 294 AND 312, WL 207 PER FEDEX SRM 51-20-1 AND PER FEDEX MM 51-20-2. 2L73 4F A3WE 19950130008881995013000888NM 1995 1 30 95UAL727007 119950119A3350S109 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT OVERWING DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297297U 21892 RIGHT EXTERIOR OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950130008891995013000889NM 1995 1 30 95UAL727008 119950119A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP297297U 21892 CENTER OVERHEAD EMERGENCY LIGHT INOP. REPLACED FIXTURE. 2L73 4F4 F A3WE E2EA 19950130008901995013000890NM 1995 1 30 95UAL727009 119950119A335010604503 EEL RELAY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297446U 21900 EMERGENCY EXIT LIGHTS ON AIRCRAFT INOP. REPLACED RELAY. 2L73 4F4 F A3WE E2EA 19950130008911995013000891NM 1995 1 30 95UAL727010 119950124A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297454U 21908 AFT LIGHT CENTER AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950130008921995013000892NM 1995 1 30 95UAL767002 119950124A2913 HYD PUMP ABEX 6506606 BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE RIGHT FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29602UA 21863 RIGHT HYDRAULIC SYSTEM FAILED. AIRCRAFT RETURNED TO FIELD. ENGINE DRIVEN PUMP REPLACED. AIRCRAFT DISPATCHED WITH NO FURTHER FAULTS. 2L72 4F4 FRTA1NM E3NE 19950130008931995013000893WP 1995 1 30 ABXA9500055 119950124A56105613217507 WINDOW DOUG DC9 DC931 3022065WP RT COCKPIT OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 DURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS IAW DC-9 MM 56-10. OPS CHECKED GOOD. 2L72 4F A6WE 19950130008941995013000894WP 1995 1 30 ABXA9500056 119950124A56105613217508 WINDOW DOUG DC9 DC931 3022065WP LT COCKPIT OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23938AX 47009 DURING PREFLIGHT, BOTH CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS LOCKING MECHANISM LOCATED ON THE TOP FORWARD PART OF THE WINDOW, INTERMITTENTLY WILL NOT RELEASE. THIS RESULTING IN THE WINDOW NOT OPENING. ADJUSTED CAPTAIN'S AND FIRST OFFICER'S SLIDING WINDOWS IAW DC-9 MM 56-10. OPS CHECKED GOOD. 2L72 4F A6WE 19950130008951995013000895WP 1995 1 30 MWEA95111 119950122A52305910141 OUTER PAN DOUG DC9 DC915 3022036WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 DURING INSP OF AFT CARGO DOOR, A 2 INCH CRACK WAS FOUND IN THE OUTER PAN RADIUS IN THE UPPER FWD CORNER OF THE AFT DOOR. THE CRACK WAS STOP DRILLED, AND AN EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03 FIG 8. AREA WAS TREATED IAW SRM 51-10-3. OPERATIONAL CHECK AND PRESSURE CHECK GOOD. A/C RETURNED TO SERVICE. 2L72 4F A6WE 19950130008961995013000896NM 1995 1 30 MWEA95113 119950123A25603952273502 GIRTH BAR LATCH DOUG MD88 MD88 3023688NM AFT GALLEY DOOR LACK OF LUBE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31601ME 49762 THE REAR GALLEY SERVICE DOOR SLIDE GIRTH BAR WAS FOUND HARD TO LATCH AND UNLATCH. GIRTH BAR LATCHES WERE FOUND DIRTY AND REQUIRING LUBRICATION. THE GIRTH BAR LATCHES WERE CLEANED AND LUBRICATED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 19950130008971995013000897WP 1995 1 30 MWEA95114 119950124A33506011777 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP RT NACELLE INOPERATIVE A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31204ME 47680 DURING A SERVICE CHECK, THE RIGHT SIDE NACELLE EMERGENCY LIGHT WAS FOUND INOP. REPLACED BATTERY POWER SUPPLY FOR THE RIGHT NACELLE LIGHT. OPERATIONAL CHECK WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950130008981995013000898EU 1995 1 30 QXEA9500025 119950123A3350 EEL BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 111096 PDX - THE EMERGENCY LIGHT AT THE FWD GALLEY DOOR IS INOP. REPLACED DEFECTIVE BULB, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950130008991995013000899EU 1995 1 30 QXEA9500026 119950123A3350 EEL BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 PDX - THE CENTER AISLE OVERHEAD EXIT SIGN HAS SEVERAL EMERGENCY LIGHT BULBS INOP. REBULBED LIGHTS, AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950130009001995013000900NM 1995 1 30 SWAA950059 119950119A278265446519 ACTUATOR BOEING737 7372H4 138448CNM NR 5 SLAT FAILED A ASWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0763SW 22061 DURING CLIMB, NUMBER 5 SLAT WOULD NOT FULLY RETRACT. RECYCLED SLATS WITH NO HELP. AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 5 SLAT ACTUATOR AND OPERATION CHECK PER BOEING MM. 2L72 4F A16WE 19950130009011995013000901NM 1995 1 30 SWAA950060 119950119A278265446519 ACTUATOR BOEING737 7372H4 138448CNM NR 6 SLAT INOP A ASWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0780SW 22675 DURING CLIMB, NUMBER 6 L/E SLAT TRANSIT LIGHT REMAINED ILLUMINATED. RECYCLED SLATS WITH NO HELP. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 6 SLAT ACTUATOR AND OPERATION CHECK PER BOEING MM. 2L72 4F A16WE 19950130009021995013000902NM 1995 1 30 SWAA950061 119950120A33506104791 EEL CHARGER BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED A-CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING MM. 2L72 4F A16WE 19950130009031995013000903NM 1995 1 30 SWAA950062 119950120A33501000679 EEL BOEING737 7372H4 138448CNM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0786SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING MM. 2L72 4F A16WE 19950130009041995013000904NM 1995 1 30 SWAA950063 119950120A33506040681 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0792SW 22964 DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SERVICE AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND CHARGER PER BOEING MM. 2L72 4F A16WE 19950130009051995013000905NM 1995 1 30 SWAA950064 119950120A53302024T3 SKIN BOEING737 7373H4 1384600NM BS 951 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07315 23337 DURING SCHEDULED MAINT CHECK, FOUND A 3 INCH CRACK IN FUSELAGE SKIN IN LOWER SECTION 46, BS 951, FWD OF POTABLE WATER SERVICE PANEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130009061995013000906NM 1995 1 30 SWAA950065 119950120A53302024T3 SKIN BOEING737 7373H4 1384600NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07315SW 23337 DURING SCHEDULED MAINT CHECK, FOUND A 2 INCH CRACK IN LOWER LEFT FUSELAGE SECTION 46, BS 727E, AFT OF LOWER EMERGENCY EXIT LIGHT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130009071995013000907NM 1995 1 30 SWAA950066 119950118A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 761 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING WALKAROUND CHECK, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950130009081995013000908NM 1995 1 30 SWAA950067 119950118A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 814 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING WALKAROUND CHECK, FOUND A 2.25 INCH FUSELAGE SKIN CRACK AT BS 814, AT S16L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950130009091995013000909NM 1995 1 30 SWAA950068 119950118A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 831 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING WALKAROUND CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 831, 2 INCHES ABOVE S25R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950130009101995013000910NM 1995 1 30 SWAA950069 119950118A3350202121 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07349SW 24408 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REPLACED AFT BATTERY PACK PER BOEING MM. 2L72 4F RTA16WE 19950130009111995013000911NM 1995 1 30 SWAA950070 119950118A3350202121 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND SECTION OF CABIN EMERGENCY FLOOR LIGHTING INOP. REPLACED AFT BATTERY PACK PER BOEING MM. 2L72 4F RTA16WE 19950130009121995013000912NM 1995 1 30 SWAA950071 119950118A3350BSP73 EEL BATTERY BOEING737 7373H4 1384600NM RT OVER WING DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07361SW 26572 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK PER BOEING MM. 2L72 4F RTA16WE 19950130009131995013000913NM 1995 1 30 SWAA950072 119950118A335020121 EEL CHARGER BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07366SW 26577 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING MM. 2L72 4F RTA16WE 19950130009141995013000914NM 1995 1 30 SWAA950073 119950121A335020131 EEL BATTERY BOEING737 7375H4 138449DNM L1 DOOR DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07519SW 25318 DURING SCHEDULED SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT SIGN LIGHT INOP. REPLACED BATTERY PACK PER BOEING MM. 2L72 4F RTA16WE 19950130009151995013000915NM 1995 1 30 SWAA950074 119950117A53302024T3 SKIN BOEING737 7373H4 1384600NM LT FUS CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07301SW 22941 DURING SCHEDULED A-CHECK, FOUND FUSELAGE SKIN CRACK BETWEEN PASSENGER WINDOWS 11 AND 12. THE CRACK MEASURED 3 INCHES IN LENGTH AND APPROX CENTERED IN THE SKIN PANEL BETWEEN WINDOWS JUST BELOW S12L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130009161995013000916NM 1995 1 30 SWAA950075 119950117A5711 SPAR BOEING737 7373Y0 1384671NM WS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND RIGHT WING SPAR UPPER SURFACE AT WS 500 JUST AFT OF FRONT SPAR CORRODED. REPAIRED PER TRAMCO EWO 95-0051. 2L72 4F RTA16WE 19950130009171995013000917NM 1995 1 30 SWAA950076 119950117A5320 INTERCOSTAL BOEING737 7373Y0 1384671NM BS 767-787 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORROSION AT BS 767-787, RBL 22, WL 150 AND AT BS 344, BL 0, WL 208. FABRICATED AND REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130009181995013000918NM 1995 1 30 SWAA950077 119950119A5330 SKIN BOEING737 7373H4 1384600NM AFT FUS DAMAGED A SWAAK NONE O OTHER TOTAKEOFF 1 SW07367SW 26578 ON TAKEOFF, AIRCRAFT EXPERIENCED SLIGHT TAIL DRAG. INSPECTED AREA PER BOEING STRUCTURAL REPAIR MANUAL. PERFORMED MAINT FERRY FLIGHT TO DAL FOR REPAIRS. FABRICATED DOUBLER AND REPAIRED DAMAGED AREA PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950130009191995013000919NM 1995 1 30 UPS202101 119950125A5320 FRAME BOEING727 727185C 138406NNM GALLEY DOORWAY CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01940UP 19826 WHILE IN 'C' CHECK, MAINTENANCE FOUND MID GALLEY DOORWAY FORWARD UPPER FRAME SEGMENT CRACKED TOP I/B CORNER STA 636. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950130009201995013000920EU 1995 1 30 WWMA9500006 119950111A3260622800200 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG DEFECTIVE I WWMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP15959AE 959 FLT 5246 - MRY-LAX - PILOT REPORTED THAT AFTER DEPARTURE, AND AFTER RETRACTING THE LANDING GEAR THE NOSE GEAR DOWN LIGHT WOULD NOT EXTINGUISH. THE GEAR WAS RECYCLED WITH THE SAME RESULT. THE AIRCRAFT RETURNED TO MRY. MAINTENANCE PERSONNEL DETERMINED THE PROBLEM TO BE A FAULTY NOSE GEAR DOWNLOCK SWITCH. THE SWITCH WAS REPLACED, OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950130009211995013000921EU 1995 1 30 WWMA9500007 119950114A3230 RELEASE VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR POPPED I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15961AE 961 FLT 5011 (LAX/CLD), PILOT REPORTED AFTER TAKEOFF THAT THE GEAR WOULD NOT RETRACT, AND RECEIVED THREE RED INTRANSIT LIGHTS. PILOT RECYCLED TWICE WITH SAME RESULTS. MAINTENANCE DETERMINED EMERGENCY EXTENSION LANDING GEAR RELEASE VALVE POPPED. MAINTENANCE RESET VALVE, SERVICED HYDRAULIC ACCUMULATOR RESERVOIR AND PERFORMED REQUIRED GEAR SWINGS. FUNCTION CHECKS WERE GOOD IAW JS 3201 MM CHAPTER 29-00 AND 32-00. THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA56EU 19950130009221995013000922EU 1995 1 30 WWMA9500008 119950116A2150 PACK BAG JETSTMJETSTM3201 1500217EU LEFT ODOR I WWMAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15968AE 968 FLT 5118 - SAN-LAX - PILOT REPORTED THAT THE LT BLEED HAD A STRONG OILY SMELL WHEN USED. MAINTENANCE PERSONNEL DETERMINED THAT THE PROBLEM ASSOCIATED WITH THE LT BLEED CAME WITHIN THE PARAMETERS OF MEL REFERENCE 21-01 (AIR CONDITIONING PACKS) AND IT WAS DEFERRED NR 010070. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA56EU 19950130009231995013000923EU 1995 1 30 WWMA9500009 119950117A3222107A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NOSE GEAR FAILED I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15958AE 958 FLT 5026 SMX-LAX, PILOT REPORTED THAT AFTER TAKEOFF THE NOSE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE PERSONNEL DETERMINED THAT THE NLG WAS NOT EXTENDING FULLY AND FAILED TO COMPLETE A CIRCUIT WITH THE SQUAT SWITCH. THE NOSE LANDING GEAR STRUT ASSEMBLY WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED WITH SATISFACTORY RESULTS, AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA56EU 19950130009241995013000924EU 1995 1 30 WWMA9500010 119950118A3040PC1993 HEAT INVERTER BAG JETSTMJETSTM3201 1500217EU RT WINDSHIELD DEFECTIVE I WWMAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP15968AE 968 FLT 7794 TRAINING FLIGHT SBP-SBP. PILOT REPORTED THAT UPON LANDING, AND WHEN REVERSE WAS USED A STRONG SMELL OF SMOKE WAS NOTICED IN THE COCKPIT. MAINTENANCE PERSONNEL DETERMINED THE PROBLEM TO BE A FAULTY RT WINDSHIELD HEAT INVERTER. THE INVERTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950130009251995013000925EU 1995 1 30 WWMA9500011 119950119A3520K386371 O2 BOX COVER BAG JETSTMJETSTM3201 1500217EU CABIN FELL DOWN I WWMAK NONE O OTHER CRCRUISE 1 WP15964AE 964 FLT 5027 - SAN-LAX - PILOT REPORTED THAT DURING FLIGHT THE O2 MASK COVER AT SEAT 2B/C FELL DOWN EXPOSING THE MASKS. MAINTENANCE PERSONNEL RESTOWED THE MASKS, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950130009261995013000926EU 1995 1 30 WWMA9500012 119950122A3230HTE4878 IN-OUT VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR DEFECTIVE I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15961AE 961 FLIGHT NR 5060 (LAX/IYK) PILOT REPORTED AFTER TAKEOFF THAT THE MAIN AND NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE FOUND THE EMERGENCY RELEASE PIN POPPED. THEY REMOVED AND REPLACED THE INWARD-OUTWARD VALVE AND PERFORMED A GEAR SWING. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950130009271995013000927WP 1995 1 30 WWMA9500013 219950119A7210331124HFR34C653 GEARBOX BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE DEFECTIVE I WWMAO OTHER KT FLUID LOSS ENGINE CASE PENETRATION CRCRUISE 1 WP15961AE 961 FLIGHT NR 5069 (LAX/FAT) PILOT REPORTED RIGHT HAND ENGINE SHUT ITSELF DOWN INFLIGHT. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN FAT WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THAT THE GEARBOX HAD FAILED AND PART OF THE BULLRING WAS LAYING IN THE BOTTOM OF THE ENGINE COWLING. MAINTENANCE REPLACED THE RIGHT ENGINE, RIGHT PROP AND OIL COOLER. ALL OIL LINES WERE FLUSHED. ALL NECESSARY RUNS WERE PERFORMED AND THE ACFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA56EU E4WE 19950130009321995013000932NE 1995 1 30 ASOA95001 219950102A73145009984 FUEL PUMP EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENG FAILED A AASOAE ENGINE SHUTDOWN YJ ENGINE STOPPAGE WARNING INDICATION DEDESCENT 1 SO11282AS162596706 120226 115511 FLT NR 7527 - EN ROUTE, FROM ATL-GPT, RIGHT ENGINE FAILED DESCENDING OUT OF 8,000 FEET. FOLLOWED POH PROCEDURES, DIVERTED FLIGHT TO MOB WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL PUMP AND HMU. FOUND THE FUEL PUMP SHAFT SHEARED. ALL LEAK AND OPERATIONAL CHECKS GOOD. (W) 2L72 4T4 TRTA31SO E20NE 19950130009461995013000946SW 1995 1 30 MALA954219 119950101A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15426MA AC645 FLT 3447 - ON APPROACH TO MSP, THE NOSE GEAR HAD TO BE CYCLED FOUR TIMES BEFORE A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE NOSE GEAR DOWN LIMIT SWITCHES. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950130009481995013000948SW 1995 1 30 MALA954221 119950101A2697 WIRE SWRNGNSA227 SA227AC 8780603SW LT ENGINE CHAFED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15428MA AC646 FLT 3014 - IN CRUISE FLIGHT FROM DTW, THE LEFT ENGINE FIRE LIGHT FLASHED MOMENTARILY IN FLIGHT. THE AIRCRAFT RETURNED DTW. MAINTENANCE REPAIRED CHAFED WIRES 393005B-22 AND 393005E-22. SYSTEM OPERATED SATISFACTORILY. THE FIRE EXTINGUISHER LOGIC MODULE WAS ALSO REPLACED FOR PRECAUTIONARY MEASURES. (W) 2L72 4T RTA8SW 19950130009491995013000949SW 1995 1 30 MALA954222 119950102A2120 AIR DISTR SWRNGNSA227 SA227AC 8780603SW CABIN SMOKING A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15428MA AC646 DTW - DURING A MAINTENANCE TEST FLIGHT, THE CREW NOTED SMOKE IN THE COCKPIT AND CABIN ON SHORT FINAL. THE CREW SHUT OFF THE BLEEDS AND RETURNED TO DTW. MAINTENANCE GROUND RAN THE ACFT. ALL SYSTEMS OPERATED SATISFACTORILY. NO SMOKE NOTED. (W) 1L72 4T A8SW 19950130009501995013000950NM 1995 1 30 MALA954223 119950102A33506004781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN EEL DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15826MA 330 MLI - FLT 3285 - DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950130009511995013000951SW 1995 1 30 MALA954224 119950104A572027311108023 CHANNEL SWRNGNSA227 SA227AC 8780603SW WING/FUS CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 MSP - DURING SCHEDULED MAINTENANCE, THE LOWER WING SKIN FAIRING TO FUSELAGE ATTACHMENT CHANNEL (P/N 27-31110-8023), WAS FOUND TO BE CRACKED AT BL 0.00. REPAIRS WERE COMPLETED THROUGH INSTALLATION OF A CHANNEL STIFFENER IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950203000011995020300001WP 1995 2 3 9501339311 119950118A5270 WARNING LIGHT DOUG DC9 DC982 3022082WP CARGO DOOR ILLUMINATED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01314RC 49110 DURING TAKEOFF ROLL DEN-MSP (BELOW 60 KNOTS), FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT FURTHER INCIDENT. NO TROUBLE FOUND WITH DOOR, TARGET, OR SENSOR. 2L72 4F A6WE 19950203000021995020300002NM 1995 2 3 9501396718 119950124A7830 TR UNIT BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE MALFUNCTIONED A ANWAAE ENGINE SHUTDOWN J WARNING INDICATION LDLANDING 1 GL01618US 21121 689654 DURING LANDING, THE NR 1 ENGINE REVERSER WOULD NOT COME OUT OF FULL REVERSE TO THE STOWED POSITION AND THE ENGINE WAS SHUT DOWN WHILE ON THE RUNWAY. A GROUND RUN-UP WAS ACCOMPLISHED AND PROPER REVERSER OPERATION WAS CONFIRMED BY ITS OPERATION THROUGH SEVERAL REVERSING CYCLES. 2L74 4F4 F A20WE E20EA 19950203000031995020300003NM 1995 2 3 9501402289 119950126A3350 EEL BATTERY BOEING727 727251 138408HNM GALLEY DOOR DISCHARGED A NWAAK NONE L NO TEST UKUNKNOWN 1 GL01289US 21377 RIGHT FORWARD GALLEY DOOR EMERGENCY EVACUATION CHUTE LIGHT INOPERATIVE. REPLACED BATTERY AND LIGHT BULBS. 2L73 4F A3WE 19950203000041995020300004NM 1995 2 3 9501412711 119950125A3150 TO WARNING BOEING727 7272S7 138407ZNM COCKPIT SOUNDED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01716RC 22019 DURING APPLICATION OF TAKEOFF THRUST WITH FLAPS 15 SELECTED, AURAL WARNING HORN SOUNDED. ABORTED TAKEOFF. MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM TEST. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950203000051995020300005NM 1995 2 3 95FDEA00085 119950126A2751656048815 TRANSMITTER BOEING727 727233 138408ANM LT TE FLAP FAILED A AFDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25222FE 20933 DURING FLAP RETRACTION ON T/O O/B FLAPS SHOWED AS ASYMMETRICAL. O/B FLAPS WERE LOCKED OUT. COMPLIED WITH EMERGENCY PROCEDURES AND RETURNED TO AIRPORT. LANDED WITH NO OTHER PROBLEMS. REPLACED LEFT O/B FLAP POSITION TRANSMITTER ASYMMETRICAL. CHECKS OK PER MM 27-52-13. 2L73 4F RTA3WE 19950203000061995020300006NM 1995 2 3 95FDEA00086 119950126A2751106081917 SWITCH BOEING727 727232 1384082NM NR 1 LE FLAP FAILED A FDEAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SO04499FE 21018 AFTER T/O, DURING FLAP RETRACTION, GOT STEADY AMBER LEADING EDGE FLAP LIGHT AT 2 DEG. CHECKED S/O PANEL, IT SHOWED NR 1 FLAP STILL EXTENDED CYCLED FLAPS, NO HELP. RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. REPLACED NR 1 L/E FLAP SWITCH. CHECKS OK PER MM 27-82-404. 2L73 4F A3WE 19950203000071995020300007NM 1995 2 3 95FDEA00087 119950125A5320 ANGLE BOEING727 72721C 138400MNM BS 258 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 CORROSION ON L ANGLE AT BS 259 WL 150 RBL 20. REMOVED AND REPLACED ANGLE AT BS 259 WL 150 RBL 20 PER FEDEX SRM 51-40-1. 2L73 4F A3WE 19950203000081995020300008NM 1995 2 3 95FDEA00088 119950125A53207075T6 THRESHOLD BOEING727 72721C 138400MNM BS 1057-1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 CORROSION (71C708-02) BS 1057-1110, WL 148, RBL 25 ON SUBTHRESHOLD PLATE. REMOVED AND REPLACED SUBTHRESHOLD PLATE. 2L73 4F A3WE 19950203000091995020300009NM 1995 2 3 95FDEA00089 119950125A532065196721 STRAP BOEING727 72721C 138400MNM BS 1057-1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 CORROSION (71C708-02) BS 1057-1110, WL 149, RBL 20 ON SCUFF PLATE T-STRAP. REMOVED AND REPLACED T-STRAP PER DRAW NR 65-20732-4. 2L73 4F A3WE 19950203000101995020300010NM 1995 2 3 95FDEA00090 119950126A53206524546 CHORD BOEING727 72721C 138400MNM BS 761 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 CORROSION ON STUB BEAM LOWER ANGLE AT BS 761 WL 204 RBL 60. REMOVED AND REPLACED LOWER CHORD PER FEDEX SRM 51-10-1. 2L73 4F A3WE 19950203000111995020300011NM 1995 2 3 95FDEA00091 119950127A53207075T6 STRAP BOEING727 72721C 138400MNM BS 760 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 FRAME STRAP HAS CORROSION AT BS 760, RBL 65, WL 205. REPAIRED PER FEDEX EA 7-5310-7-23668. 2L73 4F A3WE 19950203000121995020300012NM 1995 2 3 95FDEA00092 119950127A53117075T6 WEB BOEING727 72721C 138400MNM BS 760 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25143FE 19136 CORROSION ON FRAME WEB BS 760 RBL 65-70 WL 204-208. REPAIRED PER FEDEX EA 7-5310-7-23668. 2L73 4F A3WE 19950203000131995020300013WP 1995 2 3 ABXA9500058 119950124A32313649239509 CONTROL CABLE DOUG DC8 DC863 302198AWP RT MLG OUT OF ADJ A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23811AX 46113 UPON CLIMB-OUT OF ILN RIGHT MAIN GEAR DOOR 'UNLATCHED' LIGHT ILLUMINATED. RECYCLED GEAR AND HAD SAME INDICATION. REDUCED AIRSPEED AND CONTINUED TO EWR. PERFORMED MAIN GEAR DOOR CLOSED PROXIMITY SWITCH TEST. RIGHT MAIN LANDING GEAR DOOR 'UNLATCHED' LIGHT REMAINED ON. REPLACED RIGHT PROXIMITY SWITCH STRIKER AND SPRING. ADJUSTED MAIN LANDING GEAR DOOR FOLLOW-UP CABLE. PERFORMED GEAR RETRACTION TEST, AND OPS CHECKED GOOD IAW DC-8 MM CHAPTER 32. 2L74 4F 4A25 19950203000141995020300014WP 1995 2 3 ABXA9500059 119950124A32604649164 INDICATOR ASSY DOUG DC8 DC861 3021952WP LT/RT MLG DIRTY A ABXAO OTHER O OTHER CRCRUISE 1 GL23851AX 45940 ON TEST FLIGHT OUT OF GSO, THE LEFT AND RIGHT GEAR VISUAL DOWNLOCK INDICATORS SHOWED DOWN AND LOCKED WITH GEAR RETRACTED. RECYCLED GEAR AND HAD SAME INDICATION. REMOVED AND REINSTALLED LEFT AND RIGHT GEAR VISUAL DOWNLOCK INDICATORS IAW DC-8 MM CHAPTER 32. SYSTEM OPS CHECKED GOOD ON GEAR SWING IAW DC-8 MM CHAPTER 32. 2L74 4F 4A25 19950203000151995020300015EA 1995 2 3 BIER9501A 219950127A7414 MAGNETO SLICK 6355 PIPER PA32 PA32260 7103206SO LYC O540 O540E4B5 41532EA LEFT MALFUNCTIONED B BIEAK NONE O OTHER ININSP/MAINT 1 EA2133058 94080004 327500012 L1943840 AT 100 HR INSP NOTICED LEFT MAG TIMEING INCORRECT. AFTER DISSASEMBLY FOUND PT.S COATED AND IMPULSE COUPLING PAST 500 HR LIMITS, VARIOUS OTHER PARTS WERE WORN WORSE THAN THE ENG REBUILDER'S CLAIMED TIME IN SERVICE OF MAG WOULD DICTATE (350 HR.S SINCE NEW). BOTH MAGS WERE REPLACED AS A PRECAUTION. STRESS THE IMPORTANCE OF A 500 HR MAG INSPECTION. 1L71 3O3 O A3SO E295 19950203000161995020300016NM 1995 2 3 DL72L950369 119950112A5330 SKIN BOEING727 727232 1384082NM FS 990 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 BELLY SKIN AT STR 28R, STA 990 FOUND CORRODED. A 2.5 INCH BY 2.5 INCH SECTION WAS CUT OUT TO REMOVE CORROSION. A 0.040 INCH TI-6AL-4V DOUBLER, AND A 0.063 INCH TI-6AL-4V TRIPLER WILL BE INSTALLED OVER CUTOUT. 2L73 4F A3WE 19950203000171995020300017NM 1995 2 3 DL72S950350 119950125A5240 SKIN BOEING727 727232 1384082NM R/H SVC DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 FOUND DURING B-2 LETTER CHECK TPA, OUTER SKIN BROKEN OUT FWD RT SVC DOOR LOWER HINGE. INSTALLED DOUBLER REPAIR PER SRM 52-40-2. 2L73 4F A3WE 19950203000181995020300018NM 1995 2 3 DL72S950370 119950110A575465162249092 SKIN BOEING727 727232 1384082NM NR 8 SLAT LE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING SHOP INSPECTION, RIGHT WING NR 8 SLAT WAS FOUND WITH THE LEADING EDGE SKIN DENTED AT 51 INCHES TO 57 INCHES FROM THE I/B END OF SLAT. REPAIRED PER SRM 57-50-3 FIG 1. 2L73 4F A3WE 19950203000201995020300020NM 1995 2 3 DLM88950346 119950125A5210 SKIN DOUG MD88 MD88 3023688NM FWD PAX DOOR CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11996DL 53363 DURING INSPECTION FOUND .5 INCH CRACK IN THE FWD ENTRY DOOR UPPER AFT CORNER. THE CRACK WAS REPAIRED PER SRM 52-05 FIG 32. 2L72 4F RTA6WE 19950203000211995020300021WP 1995 2 3 UPS802104 119950125A5312 SUPPORTS DOUG DC8 DC873F 302199FWP AFT PRES BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN 'B' CHECK MAINTENANCE, FOUND 3RD AND 4TH HORIZONTAL SUPPORTS ABOVE NR 60, DOOR CRACKED ON AFT PRESSURE BULKHEAD. REPAIRED PER UPS EO DC8-5310-6570 AND DC8-5310-6605A. 2L74 4F RT4A25 19950203000221995020300022WP 1995 2 3 UPS802105 119950125A3260 BULB SOCKETS DOUG DC8 DC873F 302199FWP RT MLG FAILED A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01803UP 46073 PILOT REPORTED ON APPROACH AFTER LOWERING L/G, DID NOT GET ANY LIGHTS. RESET L/G AND WARNING INTERLOCK C/B AFTER IT POPPED. LOWERED GEAR AGAIN, GOT 3 GREEN SAFE INDICATORS. REPAIRED UPPER BULB SOCKET OF RIGHT L/G LIGHT ASSY. OPS CHECK SYSTEM NORMAL IAW 32-60-00. 2L74 4F RT4A25 19950203000231995020300023WP 1995 2 3 UPS802106 119950121A3231 UPLOCK MECH DOUG DC8 DC873F 302199FWP LT MLG DOOR OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01819UP 46019 PILOT REPORTED DURING DEPARTURE FROM DFW, THE 'GEAR NOT LATCHED' LIGHT ILLUMINATED. THE ALTERNATE GEAR/DOOR WARNING SYSTEM INDICATED THE MAIN GEAR DOOR CLOSED. WE PERFORMED THE 'GEAR/DOOR NOT LATCHED LIGHT' ILLUMINATED CHECKLIST AND HAD TO CYCLE THE GEAR 2 TIMES BEFORE SUCCESSFUL UPLATCH CHECK. FOUND LOCKING TAB SHEARED AND LOCKING NUT LOOSE AND NOT SAFETIED ON LEFT GEAR DOOR UPLATCH CYL. FOUND LEFT GEAR DOOR UPLATCH MECHANISM OUT OF RIGG. ALSO, RT GEAR DOOR UPLATCH PROX SWITCH WAS LOOSE. COMPLETED MM PROCEDURE 32-31-04. OPS NORMAL (P/N 4648615-5503, NAS513-7). 2L74 4F RT4A25 19950203000241995020300024WP 1995 2 3 UPS802107 119950127A572036429742 SUPPORT FITTING DOUG DC8 DC871F 302199DWP FS 680-687 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950203000251995020300025WP 1995 2 3 UPS802108 119950127A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1152 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950203000261995020300026WP 1995 2 3 UPS802109 119950127A53110807075T6 FRAME DOUG DC8 DC871F 302199DWP FS 20 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK, MAINTENANCE FOUND DURING A CORROSION BULGE INSPECTION, FRAME HEAVILY CORRODED ON OPEN UP AT FS 20, LONGERON 33R. INSTALLED REPAIR IAW SRM 53-2-0. 2L74 4F RT4A25 19950203000271995020300027WP 1995 2 3 9501429872 119950118A5347 TIE DOWN TRACK DOUG DC9 DC951 3022051WP FS 855-1030 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01781NC 48121 DURING PERIODIC CHECK, FOUND CORROSION IN AFT CARGO TIE-DOWN TRACK FS 855-1030. REPLACED TRACK PER EA 98-93787. 2L72 4F A6WE 19950203000281995020300028WP 1995 2 3 9501439927 119950118A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN AFT CARGO DOOR FRAME END FITTING UPPER FORWARD CORNER. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950203000291995020300029WP 1995 2 3 9501449927 119950118A5320 FITTING DOUG DC9 DC931 3022065WP FS 658 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN BELT FRAME ATTACH FITTING FS 658 ABOVE LONGERON 29L. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950203000301995020300030WP 1995 2 3 9501459927 119950119A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP FS 965 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN FLOOR BEAM FS 965, RBL 19-25. REPAIRED PER XEA X9-53-99. 2L72 4F A6WE 19950203000311995020300031WP 1995 2 3 9501469990 119950121A53203916209501N FITTING DOUG DC9 DC931 3022065WP FS 680 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN SEAT TRACK SUPPORT FITTING FS 680, LBL 44. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950203000321995020300032WP 1995 2 3 9501479988 119950122A5313 LONGERON DOUG DC9 DC931 3022065WP FS 950 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 23R END FITTING AT FS 950. REPLACED PER SRM 51-30-2. 2L72 4F A6WE 19950203000331995020300033WP 1995 2 3 9501489988 119950122A5313 LONGERON DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 27R END FITTING FS 996. REPLACED PER SRM 51-30-5. 2L72 4F A6WE 19950203000341995020300034WP 1995 2 3 9501499947 119950122A5720 TRAP PANEL DOUG DC9 DC931 3022065WP LT/RT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018938E 47161 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN LEFT AND RIGHT TRAPEZOIDAL PANEL INBOARD FITTINGS AT FASTENER HOLES. REPLACED BOTH PER BULLETIN 53-115, AC54284. 2L72 4F A6WE 19950203000351995020300035WP 1995 2 3 9501509956 119950128A7930 O-RING DOUG DC9 DC931 3022065WP PWA JT8 JT8D15 52051NE LT ENG GEARBOX DETERIORATED A NWAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 GL01923RW 47183 657142 EN ROUTE TO MSP, THE NR 1 ENGINE OIL QUANTITY BEGAN DECREASING. FLIGHT DIVERTED TO DTW AS A PRECAUTION. FOUND THE LP6 FITTING LEAKING. RESEALED FITTING, SERVICED ENGINE, RAN ENGINE, AND CHECKED FOR LEAKS. THE LP6 FITTING LEAK CHECK OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950203000361995020300036WP 1995 2 3 9501511221 119950128A3620 MANIFOLD LIGHT DOUG DC10 DC1030 3023501WP NR 3 ILLUMINATED A NWAAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 GL01221NW 46579 DURING CLIMB, THE NR 3 MANIFOLD FAIL LIGHT ILLUMINATED, AND THE PNEUMATIC PRESSURE ROSE TO 20 PSI. DUMPED 18,000 POUNDS OF FUEL AND RETURNED TO HNL. MANUALLY SHUT OFF THE PRESSURE REGULATOR VALVE AND DEFERRED THE NR 3 MANIFOLD SYSTEM PER MEL 36-1F. 2L73 4F A22WE 19950203000371995020300037NM 1995 2 3 9501522706 119950129A2913323636 HYDRAULIC PUMP BOEING727 727225 1384077NM B HYD SYST LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01815EA1189786 22552 ON FINAL APPROACH TO MEM, THE AIRCRAFT EXPERIENCED A 'B' HYDRAULIC SYSTEM FAILURE. AIRCRAFT LANDED NORMALLY, CLEARED RUNWAY, AND WAS TOWED TO THE GATE. FOUND BOTH 'B' PUMPS LEAKING AT THE CASE. REPLACED BOTH 'B' SYSTEM PUMPS. SYSTEM CHECKED NORMAL. 2L73 4F A3WE 19950203000381995020300038NM 1995 2 3 95UAL747004 119950130A3300 BATTERY PACK BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CABIN EEL DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP294719U 19880 DOOR 5 L-EMERGENCY EXIT LIGHT REMAINS ON AT ALL TIMES. REPLACED BATTERY PACK. 2L74 4F4 F A20WE E20EA 19950203000391995020300039NM 1995 2 3 95UAL767003 119950130A3350 LAMP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT EXT EEL MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29658UA 27113 LEFT EXTERIOR EMERGENCY LIGHTS WON'T TEST. REPLACED LAMPS. 2L72 4F4 FRTA1NM E24NE 19950203000401995020300040NE 1995 2 3 95UAL767004 219950130A7320 PS4 LINE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 ENGINE LOOSE A UALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29602UA 21863 709611 ABORTED TAKEOFF AT 110 KNOTS, DUE TO LOSS OF POWER IN NUMBER ONE ENGINE. REPLACED FUEL CONTROL, STATOR VANE ACTUATOR, FUEL PUMP, AND TT2 SENSOR. UNITS OP CHECKED GOOD IN SHOP. ALSO, RESECURED LOOSE PS4 LINE, WHICH WAS FOUND LOOSE AFTER ABORTED TAKEOFF. SUSPECT PS4 LINE AT FAULT. 2L72 4F4 FRTA1NM E3NE 19950203000411995020300041WP 1995 2 3 95UALD10014 119950130A3350 EEL GROUND DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291817U 46616 EMERGENCY LIGHT INOPERATIVE AT DOOR 1R. REPAIRED GROUND, CHECKS OKAY. 2L73 4F4 F A22WE E23EA 19950203000421995020300042SO 1995 2 3 COM11753 119950126A3260922FS2A6NZ735 WOW SENSOR EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01243CA 120212 LANDING GEAR CONTROL CANNOT BE SELECTED TO THE RETRACT POSITION. COULD NOT DUPLICATE THE DISCREPANCY. ALL THREE 'WEIGHT ON WHEELS' PROXIMITY SENSORS WERE REPLACED FOR TROUBLESHOOTING. 2L72 4T RTA31SO 19950203000431995020300043EU 1995 2 3 COM31021 119950126A61208210153 PCU SAAB SF340 SF340A 7850100EU RT PROP DEFECTIVE A COMAK NONE O OTHER LDLANDING 1 SO01342CA18274225 340A023 RT PROPELLER RPM DECAYS DURING LANDING FLARE. REPLACED THE PROPELLER PITCH CONTROL UNIT. 2L72 4T RTA52EU 19950203000441995020300044EU 1995 2 3 COM31022 119950126A27708618M1 ACTUATOR SAAB SF340 SF340A 7850100EU RUDDER DEFECTIVE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01146CA14393 340A146 RUDDER GUST LOCK CIRCUIT BREAKER TRIPPED. REPLACED GUST LOCK ACTUATOR. 2L72 4T RTA52EU 19950203000451995020300045EA 1995 2 3 COM60395 119950129A2820B9731653 VALVE CNDAIRCL600 CL6002B19 EA LT ENG SOV FAILED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA2758 2758 7031 LEFT ENGINE FUEL SHUT OFF VALVE FAIL MESSAGE ON EICAS. REPLACED LT SOV. 2L72 4F RTA21EA 19950203000461995020300046EA 1995 2 3 COM60396 119950125A274070621 MOTOR CONTL UNIT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01937CA1023 7044 STABILIZER TRIM CHANNEL 1 IS INOP. REPLACED THE MOTOR CONTROL UNIT. 2L72 4F RTA21EA 19950203000471995020300047NM 1995 2 3 DL72W950374 119950123A5713 STRINGER BOEING727 727247 138408FNM WS 656 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 709217 DURING HMV, STRINGER MARKED NR 6 CRACKED AT WS 656.5. THE CRACK ORIGINATES AT HOLE AND RUNS O/B APPROX .5 INCH. REPAIR PER MM 57-13-0. 2L73 4F A3WE 19950203000491995020300049NM 1995 2 3 DL72W950376 119950125A5320 WEB BOEING727 727247 138408FNM VENTRAL STAIR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 709217 DURING HMV, RT VENTRAL STAIR LOWER BOX WEB CRACK. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950203000501995020300050WP 1995 2 3 DLL16950381 119950105A5347 SEAT TRACK LKHEED1011 10113853 5265020WP FS 1665-1745 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING OVERHAUL THE SEAT TRACK THAT RUNS FROM FS 1665 FS 1745 AT RBL 22 WAS FOUND CORRODED. REPLACED SECTION OF TRACK PER SRM 53-21-00 PG 836. 2L73 4F A23WE 19950203000511995020300051WP 1995 2 3 DLL16950382 119950106A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 884 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING OVERHAUL THE CABIN FLOOR BEAM LOWER SURFACE OF UPPER CAP WAS CORRODED AT SEVERAL FASTENER HOLES FS 884 RBL10. MANUFACTURED AND INSTALLED REPAIR PARTS PER SRM 53-21-00 PG 849-852 2L73 4F A23WE 19950203000521995020300052WP 1995 2 3 DLL16950383 119950106A5315 FLOOR BEAM CAP LKHEED1011 10113853 5265020WP FS 1763 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING OVERHAUL AT STA 1763 THE FLOOR BEAM UPPER FLANGE TOP SURFACE HAD DEEP CORROSION SEVERAL PLACES LB 62 LBL 88. REMOVED AND INSTALLED T-CAP PER SRM 53-21-00 PG 849-852. 2L73 4F A23WE 19950203000531995020300053NM 1995 2 3 DLM88950389 119950125A2410696233B CSD DOUG MD88 MD88 3023688NM NR 1 ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11916DL 49591 DURING CLIMB-OUT, THE LEFT CSD OVERHEATED. DISCONNECTED PER POM, BECAUSE RIGHT GENERATOR WAS ON MCO. RETURNED TO IAD. REPLACED CSD AND GENERATOR. 2L72 4F RTA6WE 19950203000541995020300054WP 1995 2 3 ERA00001 119950125A33501104411 BATTERY PACK GRIMES 1102833 CVAC 340 34031 2422704WP ALLSN 501D 501D13H 03004GL CABIN EEL DISCHARGED A ERAAK NONE L NO TEST ININSP/MAINT 1 AL03569JA 69 INTERIOR EMERGENCY EXIT LIGHT ON RT SIDE ROW 3 INOP. REPLACED BATTERY PACK. 2L72 4R4 T 6A6 E282 19950203000551995020300055NM 1995 2 3 SWAA950078 119950124A5320 ANGLE BOEING737 7373Y0 1384671NM BS 832 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND AFT CARGO DOOR L ANGLE CORRODED AT BS 832 RBL 32 WL 158. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950203000561995020300056NM 1995 2 3 SWAA950079 119950124A53302024T3 SKIN BOEING737 7373Y0 1384671NM BS 767 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED, AND A PREVIOUS REPAIR AT BS 767, BETWEEN S20 AND 21R. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950203000571995020300057NM 1995 2 3 SWAA950080 119950124A53206545884252 STIFFENER BOEING737 7373Y0 1384671NM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM STIFFENER CORRODED AT BS 294.5 AND 312, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950203000581995020300058NM 1995 2 3 SWAA950081 119950124A32414271901 CONTROL UNIT BOEING737 7373H4 1384600NM ANTI-SKID SYST MALFUNCTION A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07301SW 22941 AFTER TAKEOFF, MAIN GEAR BRAKE ANTI-SKID INOP LIGHT FLICKERED MOMENTARILY, THEN REMAINED ILLUMINATED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED ANTI-SKID CONTROL UNIT PER BOEING MM. 2L72 4F RTA16WE 19950203000591995020300059NM 1995 2 3 SWAA950082 119950124A53302024T3 SKIN BOEING737 7372H4 138448CNM RT FUS CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07103SW 23109 DURING WALKAROUND INSPECTION , FOUND A 4 INCH SKIN CRACK ON RIGHT SIDE FUSELAGE, JUST AFT OF T/E FLAPS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950203000601995020300060NM 1995 2 3 SWAA950083 119950125A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 890 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21339 DURING SCHEDULED C3 CHECK, FOUND 3 INCH SKIN CRACK AT BS 890, AT S24R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950203000611995020300061NM 1995 2 3 SWAA950084 119950125A57302024T3 SKIN BOEING737 7372H4 138448CNM RT WING LE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21339 DURING SCHEDULED C3 CHECK, FOUND RIGHT WING FIXED L/E CRACKS AT NUMBER 4 AND 5 AUX TRACK CUTOUTS. REPAIRED PER SWA RA 1-257-264/65. 2L72 4F A16WE 19950203000621995020300062NM 1995 2 3 SWAA950085 119950125A53122024T3 BULKHEAD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21339 DURING SCHEDULED C3 CHECK, FOUND PRESSURE BULKHEAD CRACKED IN RADIUS OF FWD VERTICAL FLANGE OF T-SUPPORT AT BS 178 LBL 5.5 WL 183.0. REPAIRED PER SWA RA 1-253-1239. 2L72 4F A16WE 19950203000631995020300063NM 1995 2 3 SWAA950086 119950125A5320 STRAP BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21339 DURING SCHEDULED C3 CHECK, FOUND SEVERAL CRACKS UNDER VERTICAL STRAP AT BS 178, LBL 5.7. REPAIRED PER SWA RA 1-253-1240. 2L72 4F A16WE 19950203000641995020300064NM 1995 2 3 SWAA950087 119950125A5720 ANGLE BOEING737 7372H4 138448CNM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED C-2 CHECK, FOUND SUPPORT ANGLE CRACKED AT WING TO FUSELAGE TRANSITION PANEL INBOARD OF GROUND SPOILER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950203000651995020300065NM 1995 2 3 SWAA950088 119950125A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING WALKAROUND INSPECTION, FOUND A 2 INCH FUSELAGE SKIN CRACK AT BS 761, 1 INCH ABOVE S17L. A 2.25 INCH CRACK AT BS 814 S16L, AND A 2.75 INCH CRACK AT BS 831, 2 INCHES ABOVE S25R. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950203000661995020300066NM 1995 2 3 SWAA950089 119950126A5313 STRINGER BOEING737 7373Y0 1384671NM BS 727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CORROSION AROUND FASTENERS AT BS 727D TO 767, S26R, AND AT BS 767 TO 807, S26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950203000671995020300067NM 1995 2 3 SWAA950090 119950126A5313 STRINGER BOEING737 7373Y0 1384671NM BS 1116-1127 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND APU COMPARTMENT BULKHEAD AIR INLET CUTOUT WITH CORROSION ON UPPER AND LOWER STRINGERS AND STIFFENERS FROM BS 1116 TO 1127. REPLACED PARTS PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950203000681995020300068NM 1995 2 3 SWAA950091 119950127A5220BACB30FP6 CHORD BOEING737 7375H4 138449DNM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED MAINT CHECK, FOUND FORWARD GALLEY DOORWAY INNER CHORD CRACKED AT BS 294. REPAIRED PER SWA RA 1-553-1228. 2L72 4F RTA16WE 19950203000691995020300069NM 1995 2 3 SWAA950092 119950127A53206974544 WEB BOEING737 7375H4 138449DNM BS 726 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED MAINT CHECK, FOUND WEB CRACKED AT BS 726 STRINGER 18A, RIGHT SIDE. REPAIRED PER SWA RA 1-553-1233. 2L72 4F RTA16WE 19950203000701995020300070NM 1995 2 3 SWAA950093 119950127A5320 WEB BOEING737 7375H4 138449DNM BS 1088 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07505SW 24182 DURING SCHEDULED MAINT CHECK, FOUND WEB HOLE CRACK AT BS 1088 BULKHEAD. REPAIRED PER SWA RA 1-553-1234. 2L72 4F RTA16WE 19950203000711995020300071NM 1995 2 3 SWAA950094 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED FROM BS 480 TO 500B, 808, 858, STRINGER 10R. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000721995020300072NM 1995 2 3 SWAA950095 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 380, 381, 400 TO 431, 450 TO 461, 490, 500, 500 PLUS 1, AND 500A TO 500B, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000731995020300073NM 1995 2 3 SWAA950096 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 400, 410, 420, 430, 440, 461 TO 500A, 500B, 500B PLUS 10, 586, 587, 605, 626, 705, 727A, 777, 778, 818, 838, 848, 868, 878, 888, 898, 925, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000741995020300074NM 1995 2 3 SWAA950097 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 379 TO 399, 479 TO 500, 500 PLUS 9, 500A, 500A PLUS 9, 500A PLUS 10, 500B PLUS 1, 588, 628, 684 TO 706, 746, 747, 777, 816, 817, 846, 847, 886, 887, 916, 945, 965 TO 995, STRINGER 4R. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000751995020300075NM 1995 2 3 SWAA950098 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM FS 520/521 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACK INDICATIONS AT THE FOLLOWING LOCATION: BS 520 AND 521, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000761995020300076NM 1995 2 3 SWAA950099 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 413 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN DENTED AT BS 413, BETWEEN S5 AND 6R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950203000771995020300077NM 1995 2 3 SWAA950100 119950127A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 380, S14R. REPAIRED PER TRAMCO EWO 95-0058. 2L72 4F A16WE 19950203000781995020300078NM 1995 2 3 UPS202111 119950127A3260 CONNECTOR BOEING727 72725C 138400HNM NLG DIRTY A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01948UP 19357 PILOT REPORTED ON APPROACH INTO ELP WHEN GEAR WAS EXTENDED, THE GREEN NOSE GEAR DOWN AND LOCK LIGHT WAS BEARLY VISIBLE. FLIGHT TEST PERFORMED, OPS GOOD. CYCLED L/G AFTER GO AROUND ONCE, GEAR CYCLED. LIGHT DIM THEN AFTER TEN SECONDS, FULL BRIGHT. A/C LANDED WITHOUT INCIDENT. INSPECTED NLG, FOUND DOWNLOCK SWITCHES CANNON PLUGS DIRTY. CLEANED CONNECTORS AND INSURE PROPER BULBS INSTALLED IN ANNUNCIATOR PANEL. N/G LIGHTS OPERATE NORMAL. 2L73 4F A3WE 19950203000791995020300079NM 1995 2 3 UPS202112 119950130A5230 TRANSVERSE BEAM BOEING727 727173C 1384059NM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR HAS 2 CRACKS ON THE NR 3 TRANSVERSE BEAM AND WEB. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950203000801995020300080NM 1995 2 3 UPS202113 119950130A5230 TRANSVERSE BEAM BOEING727 727173C 1384059NM AFT CARGO DOOR CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND AFT CARGO DOOR NR 1 TRANSVERSE BEAM CORRODED. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950203000811995020300081NM 1995 2 3 UPS202114 119950130A5210 UPPER GATE BOEING727 727173C 1384059NM FWD ENTRY DOOR CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON FORWARD ENTRY DOOR UPPER GATE. INSTALLED REPAIR IAW SRM 51-10-2, 51-30-2, 51-30-8 AND MM 51-20-151. 2L73 4F A3WE 19950203000821995020300082NM 1995 2 3 UPS202115 119950130A5313 STRINGER BOEING727 727173C 1384059NM BS 410 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON STR NR 23R BS 410 WL 164 RBL 42. INSTALLED REPAIR IAW SRM 53-10-3. 2L73 4F A3WE 19950203000831995020300083NM 1995 2 3 UPS202116 119950130A5330 SKIN LAP BOEING727 727173C 1384059NM BS 927/940 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON SKIN LAP STR 4 LT AT STA 927, 940. INCLUDED STA 954-958 AT STR 4 LT. 2L73 4F A3WE 19950203000841995020300084NM 1995 2 3 UPS202117 119950130A5753 SUPPORT BLOCK BOEING727 727173C 1384059NM LT WING CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND CORROSION O/B FLAP O/B AFT SUPPORT BLOCK CORRODED AND WORN ON LEFT WING. INSTALLED REPAIR IAW MM 27-51-13. 2L73 4F A3WE 19950203000851995020300085NM 1995 2 3 UPS202118 119950130A5753 SUPPORT BLOCK BOEING727 727173C 1384059NM LT WING CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND CORROSION ON LT WING O/B FLAP, I/B AFT SUPPORT BLOCK. INSTALLED REPAIR IAW MM 27-51-13. 2L73 4F A3WE 19950203000861995020300086NM 1995 2 3 UPS202119 119950130A5712 RIB MOUNT TAB BOEING727 727173C 1384059NM WS 656.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINT FOUND VENT BOX STR 12 RIB MOUNT TAB CRACKED AT WS 656.5 (KIT P/N 65C26139-16), LT WING. INSTALLED REPAIR IAW SRM 57-10-4 AND SB 57A159. 2L73 4F A3WE 19950203000871995020300087WP 1995 2 3 UPS802110 119950129A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP FLIGHT DECK EEL DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01744UP 45944 MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS FAILED OPS TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. 2L74 4F RT4A25 19950203000881995020300088WP 1995 2 3 UPS802121 119950128A3350 LAMP DOUG DC8 DC873F 302199FWP FLIGHT DECK EEL FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01808UP 46008 MAINTENANCE REPORTED FLIGHT DECK EMERGENCY LIGHT INOP (DOME LIGHT). RELAMPED, OPS CHECK NORMAL. 2L74 4F RT4A25 19950203001011995020300101WP 1995 2 3 CAL950003 119950103A2150 DUCT DOUG DC9 DC982 3022082WP LT A/C SYSTEM BLOWN A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW0914890 49114 SAT - FLT 0437 - A STRONG BURNING ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON FINAL APPROACH TO SAT WITH THE ICE PROTECTION ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LT AIR CONDITIONING SYSTEM DUCT BLOWN IN THE TAIL COMPARTMENT AFT OF WATER SEPARATOR AND LOOSE INSULATION. THE DUCT WAS REMOVED AND REPLACED AND THE INSULATION WAS REMOVED. NO ODOR WAS OBSERVED WHILE PACKS WERE OPERATED WITH THE ICE PROTECTION ON. (X) 2L72 4F A6WE 19950203001021995020300102WP 1995 2 3 CAL950005 119950103A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916895 49394 IAH- FLT 0133 - A SECTION OF CABIN AISLE PATH EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE REPLACED SOME FAULTY DIODES, BUT THE PROBLEM WAS REPEATED. A BROKEN WIRE WAS FOUND BY ROW 5. THE WIRE WAS REPAIRED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X) 2L72 4F A6WE 19950203001031995020300103NM 1995 2 3 CAL95002 119950101A335010604503 EEL RELAY BOEING727 727224 1384076NM LT OVERHEAD PNL INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0966734 20663 IAH - FLT 1076 - CABIN EMERGENCY AISLE PATH LIGHTING WOULD NOT COME ON AUTOMATICALLY WHEN SWITCHED TO STANDBY POWER DURING A PREFLIGHT CHECK. THE EMERGENCY POWER LIGHT RELAY WAS REMOVED AND REPLACED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X) 2L73 4F A3WE 19950203001041995020300104WP 1995 2 3 CAL950027 119950108A5350 LATCHES DOUG DC9 DC982 3022082WP TAIL CONE LACK OF LUBE A CALAK NONE O OTHER ININSP/MAINT 1 SW0916894 49393 HOU - THE TAIL CONE INTERIOR RELEASE HANDLE PULL FORCE WAS EXCESSIVE. THE TAIL CONE LATCHES WERE LUBRICATED AND THE INTERIOR RELEASE HANDLE PULL FORCE CHECKED GOOD PER MM 53-50-00. (X) 2L72 4F A6WE 19950203001051995020300105EU 1995 2 3 CAL950031 119950111A2750CHA1057006B TRANSMISSION AIRBUS300 A300B4203 3930306EU NR 3 TE FLAPS INOPERATIVE A ACALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW091596717679786 121 EWR - FLT 0614 - THE FLAPS WOULD NOT EXTEND ON APPROACH TO EWR. A NO FLAPS LANDING WAS MADE WITHOUT INCIDENT. MAINTENANCE FOUND THE LT WING NR 3 FLAP TRANSMISSION AT FAULT. THE NR 3 FLAP TRANSMISSION WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD PER MM 27-51-28. (X) 2L72 4F A35EU 19950203001061995020300106NM 1995 2 3 CAL950032 119950103A3350 EEL BATT CHARGER BOEING737 7373T0 1384582NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917316 23367 BFM - INSPECTION FOUND AN AFT SECTION OF EMERGENCY LIGHT TRACK INOPERATIVE. THE AFT BATTERY CHARGER WAS REPLACED AND OPERATION OF THE EMERGENCY TRACK LIGHT WAS RESTORED. (X) 2L72 4F RTA16WE 19950203001071995020300107NM 1995 2 3 CAL950033 119950103A335020121 EEL POWER SUPPLY BOEING737 7373T0 1384582NM FS 960 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917316 23367 BFM - INSPECTION FOUND THE L-2 EXTERIOR DOOR LOCATOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY AT STA 960L WAS REMOVED AND REPLACED AND OPERATION OF THE DOOR LOCATOR EMERGENCY LIGHT CHECKED GOOD. )X) 2L72 4F RTA16WE 19950203001081995020300108NM 1995 2 3 CAL950034 119950113A25301430E OVEN BOEING727 727227 1384078NM FWD GALLEY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09147604867 21118 TPA - FLT 0591 - SMOKE BEGAN COMING FROM VENTS ABOVE AND ON SIDE OF OVEN IN THE FORWARD GALLEY WHILE IN FLIGHT. CIRCUIT BREAKERS WERE PULLED AND THE SMOKE CEASED. THE LT FORWARD GALLEY OVEN WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. THE RT FORWARD GALLEY OVEN WAS CHECKED AND FOUND GOOD. (X) 2L73 4F A3WE 19950203001091995020300109EU 1995 2 3 CAL950035 119950113A2750CHA1059008B TRANSMISSION AIRBUS300 A300B4203 3930306EU NR 5 TE FLAP INOPERATIVE A ACALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW091596724294 121 EWR - FLT 0529 - THE FLAPS WOULD NOT EXTEND ON APPROACH TO EWR. THE SLATS WENT TO 16 DEGREES NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT NR 5 FLAP TRANSMISSION WAS REMOVED AND REPLACED. THE FLAPS WERE CYCLED SEVERAL TIMES AND OPERATION CHECKED GOOD WITH NO DEFECTS NOTED. (X) 2L72 4F A35EU 19950203001101995020300110EU 1995 2 3 CAL950037 119950115A278274789212 ACTUATOR AIRBUS300 A300B4103 3930104EU LT LE FLAP LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914980 086 FLL - FLT 0249 - THE GREEN SYSTEM HYDRAULIC QUANTITY DROPPED TO WITHIN ONE-EIGHTH OF RED DOT ON GAUGE WHILE EN ROUTE TO FLL. MAINTENANCE FOUND THE LT KRUGER FLAP NOTCH LEAKING. THE LT SLOT FLAP ACTUATOR WAS REMOVED AND REPLACED. THE GREEN HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A35EU 19950203001111995020300111EU 1995 2 3 CAL950039 119950116A2910S00134160290 HYD LINE AIRBUS300 A300B4203 3930306EU BLUE HYD SYS LEAKING A CALAOH OTHER DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914973 211 EWR - FLT 0398 - THE BLUE SYSTEM HYDRAULIC QUANTITY DECREASED TO TOP OF YELLOW ARC WHILE IN FLIGHT. THE SERVOS WERE TURNED OFF PER THE 'ABNORMAL' CHECK LIST AND THE HYDRAULIC FLUID LOSS CEASED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BLUE SYSTEM FIRE RESISTANT HYDRAULIC LINE LEAKING AT THE COUPLING. THE PRESSURE LINE WAS REPLACED. LEAK CHECK DURING ENGINE RUN WAS GOOD. (X) 2L72 4F A35EU 19950203001121995020300112NM 1995 2 3 CAL950041 119950116A3234 GEAR HANDLE BOEING737 7373T0 1384582NM COCKPIT DIRTY A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW0912322 23373 IAH - FLT 1485 - WHEN THROTTLES WERE RETARDED WITH FLAPS EXTENDED, THE HORN WOULD NOT SILENCE. THE LANDING GEAR WAS LOWERED WITH 3 GREEN AND 3 RED GEAR LIGHTS ILLUMINATING. A 'TOO LOW' GEAR ALERT WAS ALSO RECEIVED. THE GEAR WAS CYCLED AND INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DEBRIS STICKING IN GEAR HANDLE. THE GEAR HANDLE WAS CLEANED AND LUBRICATED AND OPERATION CHECKED GOOD. (X) 2L72 4F RTA16WE 19950203001131995020300113NE 1995 2 3 CAL950043 219950117A7260 GEARBOX BOEING727 727243 138408DNM PWA JT8 JT8D9 52048NE NR 1 ENGINE LEAKING A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW0917407 21270 665844 THE NR 1 ENGINE OIL PRESSURE BEGAN TO DECREASE AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 ENGINE LOW OIL PRESSURE LIGHT WHILE EN ROUTE. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* THE GEARBOX WAS REMOVED AND REPLACED ON LINE. SHOP FINDINGS REPORTED NO TROUBLE FOUND DURING ENGINE TEST CELL RUN. 2L73 4F4 FRTA3WE E2EA 19950203001281995020300128NE 1995 2 3 95ZZZZ31 219950106A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT FAILURE A NVEAE ENGINE SHUTDOWN Y ENGINE STOPPAGE APAPPROACH 1 SO03201AE 340B201 785446 JAN - FLT NR 4431 - RT ENGINE FAILURE INBOUND TO JAN, 25 MILES FROM JAN. ENGINE AUTOFEATHERED, AND CREW ISOLATED ENGINE. SAFE LANDING OCURRED, NO INJURIES. INSPECTION ON THE GROUND REVEALED THE RIGHT GEARBOX FAILED. REPLACED RIGHT ENGINE AND PROPELLER. 2L72 4T4 TRTA52EU E8NE 19950203001291995020300129EU 1995 2 3 95ZZZZ32 119950111A3310E035801 LIGHT ASSY AEROSPATR42 ATR42300 8680920EU OVERHEAD LIGHT ARCED A NVEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO03143DD 056 MIA - FLT NR 5817 - PILOT REPORT CAPTAIN OVERHEAD READING LIGHT ARCED AND A SMELL OF BURNT WIRES WAS DETECTED. THE CIRCUIT BREAKER POPPED AND THE ARCIING AND SMELL WENT AWAY LANDED IN MAI WITHOUT INCIDENT. FOUND THE OVERHEAD READING LIGHT SHORTED, REPLACED LIGHT ASSY AND OPS CHECK WAS GOOD. 2H72 4T RTA53EU 19950203001311995020300131EU 1995 2 3 95ZZZZ34 119950106A3260 CONNECTOR SAAB SF340 340B 7860101EU LT MLG DIRTY A CHQAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA23224TH 340B224 PILOT REPORTED, WHILE ON APPROACH, THE LEFT MAIN GEAR WOULD NOT ILLUMINATE DOWN AND LOCKED. UPON LANDING WITHOUT INCIDENT, MAINTENACNE INSPECTED LANDING GEAR. THE CANNON PLUGS IN THE LEFT GEAR WELL WERE CLEANED ALONG WITH THE SQUAT SWITCHES. A FUNCTIONAL CHECK OF THE SYSTEM WAS PERFORMED WITH ALL INDICATIONS NORMAL. 2L72 4T RTA52EU 19950203001411995020300141NM 1995 2 3 MZZA9501 119950109A2750BACB10A836 BEARING 652661437 BOEING727 727232 1384082NM NR 4 FLAP LT SEIZED A MZZAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP1315781 0007 20636 FLT 821 - GUM - AIRCRAFT AIR RETURNED AFTER TAKEOFF CREW ADVISED THAT DURING FLAP RETRACTION, INBOARD FLAPS STUCK BETWEEN 2 AND 5 DEGREES. FOUND LEFT FLAP THRUST BEARING FROZEN. REPLACED THRUST BEARING AND SYSTEM OPERATIONAL CHECKED SATISFACTORY. (Z) 2L73 4F A3WE 19950203001421995020300142NM 1995 2 3 MZZA9502 119950113A3260189929 SENSOR BOEING727 727227 1384078NM LT UPLOCK FAILURE A MZZAO OTHER N FALSE WARNING CLCLIMB 1 WP1386426 21364 FLT NR 963 - GUM - LEFT GEAR UP LIGHT DID NOT EXTINGUISH ON RETRACTION. ALL GEAR DOORS DID CLOSE. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE FOUND LEFT GEAR UPLOCK SENSOR AT FAULT DURING GEAR UP SIMULATION OF PROX SENSORS. REPLACED SENSOR, PERFORMED GEAR SWING, OPERATION AND INDICATION NOW NORMAL. (Z) 2L73 4F A3WE 19950203001441995020300144NM 1995 2 3 TSAA9557022 119950110A5711 SPAR WEB BOEING737 7372Q9 138448MNM FSS 433 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13804AL 21719 DURING HEAVY MAINTENANCE VISIT, CORROSION FOUND UNDER NR 5 SLAT ACTUATOR ATTACH FITTING FRONT SPAR WEB AT FSS 433. REPAIRED PER ECO 2132R2. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950203001451995020300145 1995 2 3 WTAA950017 419950103A3414A3615710260 INDICATOR BAG JETSTMJETSTM3101 1500215EU COCKPIT A/S FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17402UE 734 YKM - CAPTAINS AIRSPEED INDICATOR REPORTED INOPERATIVE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SEA FOR MAINTENANCE. REPLACED CAPTAINS AIRSPEED INDICATOR. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950203001461995020300146 1995 2 3 WTAA950018 419950104A3418C771076 TRANSDUCER BAG JETSTMJETSTM3101 1500215EU LT AND RT WING REQ'D ADJ A WTAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP17331CA 793 FAT - EN ROUTE SFO TO VIS AT 12,000 FEET, STALL IDENT LIGHT ILLUMINATED FOLLOWED BY STICK SHAKER AND STALL WARNING HORN ACTIVATION. AIRCRAFT DIVERTED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT AND RT STALL SYSTEM LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL CHECK NORMAL ON GROUND AND DURING SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950203001471995020300147SO 1995 2 3 WTAA950021 119950105A2720 RUDDER EMB 120 EMB120RT SO RUDDER RT MALFUNCTION A AWTAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP17120AM 120012 SFO - AFTER DEPARTURE, LIMITED RIGHT RUDDER TRAVEL REPORTED. NO ASSOCIATED FAULTS LIGHTS NOTED ON RUDDER PANEL. CREW DECLARED AND EMERGENCY AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED RUDDER SYSTEM WITH NO DEFECTS NOTED. RUDDER SYSTEM ANDYAW SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RELEASED FOR FERRY FLIGHT TO SCHEDULED HEAVY CHECK IN (FAT). NO FLIGHT CONTROL DISCREPANCIES REPORTED DURING FERRY FLIGHT. AIRCRAFT REMAINS IN MAINTENANCE. (Z) 2L72 4T RTA31SO 19950203001481995020300148GL 1995 2 3 WTAA950022 319950109A6112660716276 DE-ICE BOOT BAG JETSTMJETSTM3101 1500215EU ROTOL R333 R333482F12 GL LT PROP MISSING A WTAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 WP17103XV 747 DRG54788 EUG - EN ROUTE PDX TO MFR, CREW REPORTED LEFT PROPELLER VIBRATION. AIRCRAFT DIVERTED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE DISCOVERED ONE PROPELLER BLADE DE-CE BOOT MISSING. REPLACED LEFT PROPELLER ASSEMBLY WITH SERVICEABLE UNIT. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 6 CP61GL 19950203001491995020300149SO 1995 2 3 WTAA950023 119950104A5270JS5 SWITCH EMB 120 EMB120RT SO PASSENGER DOOR WORN A WTAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP17281UE 120092 LAX - FORWARD DOOR WARNING LIGHT ACTIVATED DURING TAXI OUT. AIRCRAFT RETURNED TO GATE. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE CLEARED DMI BY REPLACING AND ADJUSTING FORWARD DOOR WARNING MICROSWITCH ROLLER. (Z) 2L72 4T RTA31SO 19950203001501995020300150 1995 2 3 WTAA950024 419950104A3418C771076 TRANSDUCER BAG JETSTMJETSTM3101 1500215EU RT WING MALFUNCTION A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17331CA 793 SFO - RT STALL IDENT LIGHT ILLUMINATED AND STICK SHAKER ACTIVATION REPORTED AT 150 KTS. MAINTENANCE ADJUSTED REPLACED AND ADJUSTED RIGHT STALL SYSTEM LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950203001511995020300151SO 1995 2 3 WTAA950025 119950109A5210JS5 SWITCH ROLLER EMB 120 EMB120RT SO PAX DOOR OUT OF ADJUST A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17216YV 120216 FAT - FORWARD DOOR WARNING LIGHT ACTIVATED IN FLIGHT WITH INTERMITTENT. AURAL WARNING INDICATIONS. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL WITH THE ADJUSTMENT OF THE PASSENGER DOOR MICROSWITCH ROLLERS. (M) 2L72 4T RTA31SO 19950203001521995020300152SO 1995 2 3 WTAA950026 119950109A5270 DOOR WARN EMB 120 EMB120RT SO FWD DOOR MALFUNCTION A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17269UE 120194 SFO - FORWARD DOOR WARNING LIGHT FAILS TO EXTINGUISH. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950203001531995020300153SO 1995 2 3 WTAA950027 119950109A5300 FUSELAGE EMB 120 EMB120RT SO AIR FRAME BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17278UE 120083 SFO - CREW REPORTED POSSIBLE BIRD STRIKE AT UNREPORTED AREA OF AIRCRAFT. MAINTENANCE INSPECTED AIRCRAFT IAW EMB1-120RT MM 5-50-08. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950203001541995020300154WP 1995 2 3 WTAA950028 219950109A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENG MALFUNCTION A WTAAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 WP17430UE 784 SFO - DURING ENGINE START, LEFT ENGINE OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY ENGINE SHUTDOWN. FLAMES REPORTED FROM ENGINE INTAKE AFTER ENGINE SHUT DOWN. CREW ACTIVATED ENGINE FIRE BOTTLE. FLAMES EXTINGUISHED. MAINTENANCE INSPECTED LEFT ENGINE. NO DEFECTS NOTED. DETERMINED ENGINE STOPPAGE AND SUBSEQUENT REPORTED INTAKE FIRE A RESULT OF HIGH WINDS BLOWING UP TAILPIPE. REPLACED LT ENIGNE NR 1 FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA21EU E4WE 19950203001551995020300155SO 1995 2 3 WTAA950030 119950109A2750 CONTROL EMB 120 EMB120RT SO FLAP FLAP WARN A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17281UE 120092 SFO - FLAP CONTROL FAULT REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE DISCREPANCY. FOR PRECAUTIONARY PURPOSES, CLEANED INBOARD FLAP ACTUATOR CANNON PLUGS, RERACKED FLAP COMPUTER AND FLAP ANNUNCIATOR PANEL. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950203001561995020300156NM 1995 2 3 95ZZZW27 119950110A30403212 HEAT CONTROLLER BOEING737 7373S3 1384711NM LT WINDSHIELD FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28313AW 3564 23712 PHX-SFO - FLT 604 - AIR TURNBACK DUE TO CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER PER AWA TASK CARD R1B56001, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. REF AWXA9500021. 2L72 4F RTA16WE 19950203001681995020300168NM 1995 2 3 AWXA9500001 119950102A561065C343481 WINDSHIELD BOEING737 737112 1384412NM NR 1 DELAMINATED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28708AW 2155 19771 STA LAS - FLT 886 - PHX-SJC - AIRCRAFT DIVERTED TO LAS DUE TO A CRACK IN CAPTAINS NR 1 WINDOW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE EVALUATED CRACK AND DETERMINED IT WAS A BUBBLE TRACK OR DELAMINATION IN THE VINYL MATTING GIVING THE APPEARANCE OF A CRACK. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950203001701995020300170NM 1995 2 3 AWXA9500005 119950105A2781189915 SENSOR BOEING737 737277 1384570NM NR 2 SLAT INOPERATIVE A AAWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28179AW 22646 PHX-ABQ - FLT 200 - THE NR 2 INTRANSIT SLAT LIGHT REMAINED ILLUMINATED. FLAPS WERE SELECTED ON APPROACH WITH NR 2 DEVICE ILLUMINATED ON OVERHEAD PANEL. ALL OTHER DEVICES INDICATED FLAPS WERE FULLY EXTENDED. EMERGENCY WAS DECLARED FOR THE NR 2 SLAT NOT FULLY EXTENDING. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX OPS CHECKED LE FLAPS AND SLATS PER BMM 27-810 PG 517. NO FAULTS NOTED. INDICATION SYSTEM PLACED ON UMSR 27-04 CONTROL NR 14315. INDICATION SYSTEM INOP. ACFT RETURNED TO SERVICE. PHX MX REPLACED NR 2 FULL EXTEND SENSOR. MEL REMOVED AND ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001711995020300171NM 1995 2 3 AWXA9500006 119950105A5320 INTERCOSTAL BOEING737 7373G7 1384595NM FS 380 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 PHX - FLT 485 - DURING SCHEDULED INSPECTION, FOUND CRACK IN INTERCOSTAL AFT OF STATION 380 BL 0. REMOVED, FABRICATED AND REPLACED ANGLE PER SRM 51-40-02. (W) 2L72 4F RTA16WE 19950203001721995020300172NM 1995 2 3 AWXA9500007 119950105A2742AR7077M2 MOTOR ACTUATOR BOEING737 7373G7 1384595NM STAB TRIM INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28157AW V0217 23779 LAX-LAS - FLT 74 - AIR TURNBACK, STABILIZER TRIM WAS INOPERATIVE WITH YOKE TRIM SWITCHES (BOTH CAPT AND F/O). ACFT RETURNED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. CONTRACT MX REPLACED STAB TRIM MOTOR ACTUATOR IAW AWA TASK CARD R6C27001, NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001731995020300173EU 1995 2 3 AWXA9500008 119950104A335032145L EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW 053 PHX - DURING ROUTINE MAINTENANCE CHECK, FORWARD BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950203001741995020300174EU 1995 2 3 AWXA9500009 119950105A3350321452 EEL POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304RX 304 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT AND RT FORWARD EMERGENCY EXIT LIGHT SIGNS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950203001751995020300175NM 1995 2 3 AWXA9500010 119950106A3350 EEL BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED LIGHTING AS REQUIRED, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001761995020300176NM 1995 2 3 AWXA9500011 119950108A3350 EEL WIRING BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 17-19. RECONNECTED AND SECURED WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001771995020300177NM 1995 2 3 AWXA9500012 119950109A5320 ANGLE BOEING737 7373G7 1384595NM FS 957 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 PHX - FLT 1600 - DURING SCHEDULED INSPECTION, FOUND FLOOR BOARD SUPPORT CORRODED BEYOND CLEAN UP LIMITS, STATION 957 LBL 18 TO LBL 40. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND 51-40-02. (W) 2L72 4F RTA16WE 19950203001781995020300178NM 1995 2 3 AWXA9500013 119950109A5320 ANGLE BOEING737 7373G7 1384595NM FS 957 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28158AW 23780 PHX - FLT 1600 - DURING SCHEDULED INSPECTION, FOUND FLOOR BOARD SUPPORT CORRODED BEYOND CLEAN UP LIMITS, STATION 957 RBL 10 TO RBL 18. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND 51-40-02. (W) 2L72 4F RTA16WE 19950203001791995020300179NM 1995 2 3 AWXA9500014 119950110A53106552878533 CHORD BOEING737 73733A 1384673NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 PHX - FLT 602 - DURING C-7 INSPECTION, FOUND UPPER SURFACE OF R2 DOOR INNER CHORD CORRODED BEYOND CLEAN UP LIMITS. REMOVED AND REPLACED INNER CHORD PER SRM 51-40-02 (W) 2L72 4F RTA16WE 19950203001801995020300180NM 1995 2 3 AWXA9500015 119950110A5320 CHANNEL BOEING737 73733A 1384673NM AFT LAV CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 DURING C-7 INSPECTION, FOUND AFT LAV FORWARD RT AND LT WALL SUPPORT HAT CHANNEL CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW WALL SUPPORT ANGLES PER SRM 51-10-02 AND 51-40-02. (W) 2L72 4F RTA16WE 19950203001811995020300181NM 1995 2 3 AWXA9500016 119950110A53206552878533 ANGLE BOEING737 73733A 1384673NM AFT LAV CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 PHX - FLT 602 - DURING C-7 INSPECTION, FOUND AFT LAV ANGLE SUPPORT BL 0 STATION 986 TO 1016 CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER SRM 51-40-02. (W) 2L72 4F RTA16WE 19950203001821995020300182NM 1995 2 3 AWXA9500017 119950110A5320 INTERCOSTAL BOEING737 73733A 1384673NM FS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 PHX - FLT 602 - DURING C-7 INSPECTION, FOUND INTERCOSTAL CORRODED BEYOND CLEAN UP LIMITS, STATION 986 TO 1006 BL 0 LBL 24. REMOVED, FABRICATED AND INSTALLED SECTION OF INTERCOSTAL PER SRM 51-10-02 AND 51-40-02. (W) 2L72 4F RTA16WE 19950203001831995020300183NM 1995 2 3 AWXA9500018 119950110A5320 ANGLE BOEING737 73733A 1384673NM FS 380 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28168AW 23629 PHX - FLT 602 - DURING C-7 INSPECTION, FOUND FORWARD BAG PIT CEILING FLOORBOARD SUPPORT INTERCOSTAL CRACKED IN SEVERAL PLACES, STATION 380 TO 400 BL 0. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-51 AND 51-40-02. (W) 2L72 4F RTA16WE 19950203001841995020300184NM 1995 2 3 AWXA9500019 119950109A5220BAC1521686 SEAL BOEING737 73733A 1384673NM EMER EXIT FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28168AW 23629 FLT 15 - PHX-LAX - AIR TURNBACK, ON CLIMB-OUT THROUGH FL 310 CABIN PRESSURE ALT WARNING LIGHT ILLUMINATED. CREW UNABLE TO PRESSURIZE AIRCRAFT IN MANUAL OR STANDBY MODE. AFTER LANDING, MAINTENANCE FOUND THE LT EMERGENCY EXIT HATCH LEAKING AROUND SEAL. MAINTENANCE REMOVED AND REPLACED HATCH SEAL WITH P/N 69418683 AND ADJUSTED THE HATCH STOPS. FIT AND RIG CHECK OK. AIRCRAFT PRESSURIZED ON GROUND WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001861995020300186NM 1995 2 3 AWXA9500020 119950110A213012924011 SENSOR BOEING737 737277 1384570NM NR 1 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28188AW 22655 ONT-PHX - FLT 439 - AIR TURNBACK, CREW UNABLE TO CONTROL PRESSURIZATION ON CLIMB THROUGH 2000 FEET, PRESSURIZATION FLUCTUATED 4000 FEET A MINUTE. CREW SWITCHED TO STANDBY MODE AND RETURNED TO GATE WITHOUT FURTHER PROBLEMS. CONTRACT MX PERFORMED OPS TEST OF PRESSURE CONTROL SYSTEM PER BMM 21-31-01 PG 201/204 AND BMM 21-31-0 PG 501/505 THROUGH STEP E. MX REMOVED AND REPLACED 490 DEGREE SENSOR, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001871995020300187NM 1995 2 3 AWXA9500021 119950110A30405893543095 WINDSHIELD BOEING737 7373S3 1384711NM LT COCKPIT BROKEN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28313AW 3564 23712 PHX-SFO - FLT 604 - AIR TURNBACK DUE TO CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. MX REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER PER AWA TASK CARD R1B56001, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. REF 95ZZZW 2L72 4F RTA16WE 19950203001881995020300188NM 1995 2 3 AWXA9500022 119950108A335020131A EEL BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEATS 13-18. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001891995020300189NM 1995 2 3 AWXA9500023 119950110A3350900835A EEL BATTERY PACK BOEING737 7372Q8 138448KNM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28137AW 23148 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH, ROWS 16-22. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001901995020300190NM 1995 2 3 AWXA9500024 119950110A3350 EEL CONNECTOR BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 7. RECONNECTED LOOSE CONNECTOR, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001911995020300191NM 1995 2 3 AWXA9500025 119950110A3350900835A EEL BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28182AW 22649 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001921995020300192NM 1995 2 3 AWXA9500026 119950110A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND THREE SECTIONS OF FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED WIRES AT ROWS 10, 15 AND 18. OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950203001931995020300193NM 1995 2 3 AWXA9500028 119950112A2720 PCU BOEING737 73733A 1384673NM RUDDER MALFUNCTIONED A AAWXAO OTHER O OTHER APAPPROACH 1 WP28164AW 23625 ONT-PHX - FLT 1530 - ON APPROACH, ACFT EXPERIENCED UNCOMMANDED SMALL RUDDER MOVEMENTS. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX PERFORMED RUDDER PCU INTERNAL LEAKAGE CHECK. ALL TESTS PASSED IAW AWA TASK CARD A8M27001. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001941995020300194NM 1995 2 3 AWXA9500029 119950113A3320059341 BALLAST BOEING737 73733A 1384673NM CABIN FAILED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP28168AW 2814 23629 ABQ-PHX - FLT 553 - SMOKE APPEARED TO BE EMANATING FROM SIDE RISES IN ROWS 16A THROUGH 17A. RECIRCULATING FAN TURNED OFF AND SMOKE STOPPED. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX FOUND ROW 16 ABC LIGHT BALLAST FRIED. MX REMOVED AND REPLACED LIGHT BALLAST, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950203001951995020300195WP 1995 2 3 9501531146 119950128A5330 DOUBLER DOUG DC10 DC1040 3023508WP FS 1156 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE INNER SKIN STIFFENER AT FS 1156, STR 50L AND 51L. INSTALLED NEW DOUBLER PER EA 11-96638. 2L73 4F A22WE 19950203001961995020300196WP 1995 2 3 9501541146 119950127A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1988-1990 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE END FITTING AT LONGERON 18R, FS 1988 AND LONGERON 19R, FS 1990. INSTALLED STRAP DOUBLERS PER EA 11-96271. 2L73 4F A22WE 19950203001971995020300197WP 1995 2 3 9501551146 119950127A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1581 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON AT STR 44L, FS 1581. INSTALLED REPAIR STRAP PER 11-96601. 2L73 4F A22WE 19950203001981995020300198WP 1995 2 3 9501569984 119950117A5541 RIB DOUG DC9 DC932 3022066WP RUDDER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING PERIODIC CHECK, FOUND APPROXIMATELY 70 WORKING RIVETS ON THE LEFT SIDE OF THE RUDDER. FURTHER X-RAY INVESTIGATION REVEALED CRACKS IN THE 2ND RIB BELOW THE SEAM. REPLACED RUDDER. 2L72 4F A6WE 19950203001991995020300199WP 1995 2 3 9501579952 119950128A5541 RIB DOUG DC9 DC931 3022065WP RUDDER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01916RW 47144 DURING PERIODIC CHECK, FOUND SKIN CRACKED IN THE RUDDER, RIGHT SIDE ZR40 AND ZR55. FURTHER INVESTIGATION ALSO, REVEALED A RIB CRACK AT ZR55. REPLACED RIB AND REPAIRED SKIN PER SRM 55-03. 2L72 4F A6WE 19950203002001995020300200WP 1995 2 3 9501589947 119950128A5743 FITTING DOUG DC9 DC931 3022065WP LT/RT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018938E 47161 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT AND RIGHT MAIN LANDING GEAR ATTACH FITTINGS AT THE FIXED STRUT. REPAIRED BOTH PER EA 99-095679. 2L72 4F A6WE 19950203002011995020300201WP 1995 2 3 9501599988 119950129A5230 FITTING DOUG DC9 DC931 3022065WP AFT CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND ONE INCH CRACK IN THE FORWARD CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950203002021995020300202NM 1995 2 3 9501606718 119950127A7830 TR UNIT BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE MALFUNCTIONED A ANWAAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP LDLANDING 1 GL01618US 21122 689564 DURING LANDING WHILE IN REVERSE THRUST, THE NR 1 ENGINE EXPERIENCED AN OVERTEMP OF 950 DEGREES FOR 20 SECONDS AND THE LOW OIL PRESSURE LIGHT CAME ON. THE REVERSER WOULD NOT STOW AND THE ENGINE WAS SHUTDOWN WHILE ON THE TAXIWAY. THE ENGINE WAS INSPECTED AND A GROUND RUNUP CONFIRMED PROPER OIL PRESSURE AND ENGINE AND REVERSER OPERATION. 2L74 4F4 F A20WE E20EA 19950203002031995020300203NM 1995 2 3 9501612277 119950127A7711 EPR TRANS BOEING727 7272S7 138407ZNM PWA JT8 JT8D15 52051NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01277US 21156 700419 THE NR 1 ENGINE EPR MALFUNCTIONED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR. THE NR 1 ENGINE WAS RUNUP, AND EPR SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950203002041995020300204WP 1995 2 3 9501629106 119950128A7711 EPR INDICATION DOUG DC9 DC915 3022036WP PWA JT8 JT8D7 52053NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL0196S 47206 645160 ON TAKEOFF ROLL, THE NR 2 ENGINE HAD NO EPR INDICATION. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. SYSTEM WAS INSPECTED AND THE INDICATORS WERE SWAPPED FOR TROUBLESHOOTING. THE PROBLEM COULD NOT BE DUPLICATED. SYSTEM FUNCTIONALLY TESTED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950203002051995020300205NM 1995 2 3 9501636304 119950128A261289873202 FIRE CARD BOEING747 747451 1384940NM APU FAILED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 GL01664US223072940 23819 DURING LANDING, THE APU FIRE WARNING ACTIVATED. THE FIRE BOTTLE WAS FIRED. INSPECTION REVEALED NO FIRE. REPLACED THE FIRE BOTTLE AND THE APU FIRE LOOP CARD. 2L74 4F RTA20WE 19950203002061995020300206NM 1995 2 3 9501646304 119950127A2612 FIRE LOOP BOEING747 747451 1384940NM APU FAILED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 GL01644US 23819 DURING LANDING, THE APU FIRE WARNING ACTIVATED. THE FIRE BOTTLE WAS FIRED. INSPECTION REVEALED NO FIRE. REPLACED BOTTLE AND BOTH FIRE LOOPS. 2L74 4F RTA20WE 19950203002071995020300207 1995 2 3 9501651221 219950128A7532 BLEED VALVE DOUG DC10 DC1030 3023501WP NR 3 ENGINE MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL01221NW 46579 DURING TAKEOFF, THE NR 3 PNEUMATIC PRESSURE INDICATOR ROSE TO 25 PSI. THE SYSTEM WAS SHUT-OFF PER MEL 36-1F. REDUCING THE ENGINE POWER, THE PRESSURE WOULD DECREASE. REPLACED THE PRSOV (898626-3 S.N 55114), AND THE HIGH STAGE BLEED VALVE (9786980-8 S/N 01088). 2L73 4F A22WE 19950203002081995020300208WP 1995 2 3 9501669860 119950125A5753 SKIN DOUG DC9 DC951 3022051WP RT TE FLAP SPLIT A NWAAK NONE O OTHER ININSP/MAINT 1 GL01769NC 47757 DURING LINE CHECK, FOUND THAT THE RIGHT OUTBOARD FLAP TRAILING EDGE WAS SPLIT 3.5 INCHES. REPAIRED PER EA 98-96604. 2L72 4F A6WE 19950203002091995020300209WP 1995 2 3 ABXA9500060 119950126A3231 LINK ASSY DOUG DC8 DC862 3021970WP NOSE GEAR MALFUNCTIONED A ABXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23802AX 46134 AFTER TAKEOFF AND GEAR RETRACTION, CREW HEARD A LOUD 'BANG' ACCOMPANIED BY AN EXTREME VIBRATION IN THE NOSE GEAR AREA. AIRCRAFT RETURNED TO DFW. RAN ALL FOUR TURBO COMPRESSORS, AND CHECKED DUCTING IN NOSE GEAR AREA. NO DISCREPANCIES WERE NOTED. JACKED NOSE GEAR AND CHECKED LT AND RT NOSE TIRES FOR LOOSENESS. ALL CHECKED NORMAL. THE SAME DISCREPANCY OCCURRED ON 1/30/95. FOUND RT NOSE GEAR DOOR LINK ASSY MALFUNCTIONING. 2L74 4F 4A25 19950203002101995020300210WP 1995 2 3 ABXA9500061 119950127A326032802651 TARGET DOUG DC8 DC863 302198AWP RT MLG DOOR LOOSE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23811AX 46113 AFTER TAKEOFF AND GEAR RETRACTION, GEAR 'UNSAFE' LIGHT STAYED ON. SELECTOR INDICATED THAT THE RIGHT MLG DOOR WAS NOT LATCHED. ON THE THIRD GEAR RECYCLE 'UNSAFE' LIGHT EXTINGUISHED AND GEAR DOOR INDICATED UP AND LOCKED. FOUND LOOSE STRIKER PLATE AT RIGHT MLG DOOR PROXIMITY SWITCH. TIGHTENED STRIKER. MLG GEAR UPLATCH AND DOOR CLOSED PROXIMITY SWITCH TEST OPS CHECKED GOOD IAW DC 8 MM CHAPTER 32. 2L74 4F 4A25 19950203002111995020300211WP 1995 2 3 ABXA9500062 119950130A3231510361 LINK ASSY DOUG DC8 DC862 3021970WP RT NOSE DOOR DEFECTIVE A ABXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23802AX 46134 LOUD 'BANG' EXPERIENCED AFTER GEAR RETRACTION. ONCE GEAR WAS SAFELY UP, NOISE AND VIBRATION WAS NOTICED. AIRCRAFT RETURNED TO SAN. INSPECTED AND FERRIED AIRCRAFT TO ONT. JACKED AIRCRAFT, FOUND RT NOSE GEAR DOOR FORWARD LINK UNLATCHING. REMOVED AND REPLACED LINK ASSY, AND PERFORMED RETRACTION CHECK IAW DC 8 MM CHAPTER 32. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950203002121995020300212SO 1995 2 3 COM11754 119950127A291012041043001 TUBE ASSY EMB 120 EMB120RT SO NLG LEAKING A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO011117H 120117 HYDRAULIC FLUID LEAK IN NLG AREA. REPLACED NLG UPLOCK HOOK HYDRAULIC TUBING. 2L72 4T RTA31SO 19950203002131995020300213EU 1995 2 3 COM31023 119950128A36107275031503 TUBE ASSY SAAB SF340 SF340A 7850100EU RT NACELLE BROKEN A COMAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01342CA 340A023 THE RT ENGINE ITT ROSE VERY QUICKLY DURING TAKEOFF. REPLACED BROKEN HIGH PRESSURE BLEED AIR TUBE. 2L72 4T RTA52EU 19950203002141995020300214EU 1995 2 3 COM31024 119950128A2750HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100EU TE FLAPS DEFECTIVE A COMAK NONE JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO01140N 199744608 340A140 FLAPS FAILED DURING LANDING. REPLACED FLAP CONTROL VALVE. 2L72 4T RTA52EU 19950203002151995020300215EU 1995 2 3 COM31025 119950127A33506104781 EEL BATTERIES SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST UKUNKNOWN 1 SO01342CA 340A023 EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES. 2L72 4T RTA52EU 19950203002161995020300216EA 1995 2 3 COM60398 119950129A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 1 SPOILER FAILED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01936CA1378 7043 OUTBD GROUND SPOILERS FAULT MESSAGE ON EICAS. REPLACED THE NR 1 SPOILER ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950203002171995020300217EA 1995 2 3 COM60399 119950125A352011508201 OXY MODULE CNDAIRCL600 CL6002B19 EA CABIN DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01916CA4214 7014 ROUTINE CHECK INSPECTION, FOUND SEAT 9A OXYGEN MASK WILL NOT DEPLOY. REPLACED THE EMERGENCY O2 MODULE. 2L72 4F RTA21EA 19950203002181995020300218EA 1995 2 3 COM60400 119950125A2820B9731651 VALVE CNDAIRCL600 CL6002B19 EA RT ENGINE INOP A COMAK NONE O OTHER ININSP/MAINT 1 SO01916CA4214 7014 RT ENGINE FUEL SHUTOFF VALVE WILL NOT CLOSE WHEN FIRE PUSH SWITCH IS ACTIVATED. REPLACED FUEL SOV. 2L72 4F RTA21EA 19950203002191995020300219NM 1995 2 3 DL72E950390 119950116A711065196854540 NOSE COWL BOEING727 727247 138408FNM NR 3 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112826W 21331 709217 DURING INITIAL INSPECTION, A 4 INCH CRACK WAS FOUND IN THE OUTER SKIN AT APROXIMATELY THE 11 O/C POSITION. THE CRACK WAS REPAIRED PER SRM 54-30-3 FIG 3A, WHICH REQUIRES A MRR, REF NR 5987. 2L73 4F A3WE 19950203002201995020300220NM 1995 2 3 DL72L950420 119950105A5754 SKIN BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKED LOWER SKIN AT INBD TRACK FAIRING. REPAIRED PER MM 57-54-0 FIG 15. 2L73 4F A3WE 19950203002211995020300221NM 1995 2 3 DL72L950421 119950105A5754651622173 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH THE RIB CHORD CRACKED AT THE O/B END, AND WORN AT THE I/B TRACK. REPAIRED PER MM 57-54-0 FIG 812. 2L73 4F A3WE 19950203002221995020300222NM 1995 2 3 DL72L950422 119950105A5754651622172 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950203002231995020300223NM 1995 2 3 DL72L950423 119950105A5754651622173 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP INSPECTION, FOUND LEFT WING NR 4 SLAT WITH RIB NR 12 AND NR 18 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950203002241995020300224NM 1995 2 3 DL72L950424 119950105A5754 SKIN BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP ISNPECTION, LEFT WING NR 4 SLAT UPPER SKIN WAS WORN AT FENCE. ALSO, A TIME LIMITED REPAIR WAS FOUND ON LOWER SKIN AT FENCE AREA. REPAIRED PER MM 57-54-0 FIG 813 AND SRM 57-50-3 FIG 1. 2L73 4F A3WE 19950203002251995020300225NM 1995 2 3 DL72S950371 119950126A5320 WEB BOEING727 727232 1384082NM LT NLG WW CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 CORROSION WAS FOUND ON THE SKIN CLIP AND WEB JUST O/B OF THE LT NOSE CHORD AT STA 303.9. THE DAMAGE WAS REPAIRED PER MM 53-30-0 FIG 806. DAMAGE FOUND DURING SPECIAL INSPECTION. 2L73 4F A3WE 19950203002261995020300226NM 1995 2 3 DL72S950377 119950126A5754651622296 ANGLE BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 709217 DURING CORROSION ISNPECTION, FOUND NR 6 SLAT WITH A .5 INCH CRACK IN ATTACH ANGLE BELOW ANTI-ICE DUCT TEE. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950203002271995020300227NM 1995 2 3 DL72S950378 119950126A5754651622296 SKIN BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 709217 DURING CORROSION INSPECTION, RT WING NR 6 SLAT WAS FOUND WITH A 2.25 INCH CRACK IN LOWER AFT SKIN. REPAIRED PER MM 57-54-0 PG 801. 2L73 4F A3WE 19950203002281995020300228NM 1995 2 3 DL72S950379 119950126A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 709217 DURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A 1 INCH CRACK IN L/E RIB, JUST OUTBOARD OF INBOARD SLAT TRACK. REPAIRED PER MM 57-54-0 PG 815-815A. 2L73 4F A3WE 19950203002291995020300229NM 1995 2 3 DL72S950380 119950126A5754651622296 ANGLE BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 709217 DURING CORROSION INSPECTION, RIGHT WING NR 6 SLAT WAS FOUND WITH A .5 INCH CRACK IN O/B ATTACH ANGLE, JUST I/B OF O/B STOP. REPAIRED PER MM 57-54-0 PG 816. 2L73 4F A3WE 19950203002301995020300230NM 1995 2 3 DL72S950403 119950127A3230 UPLOCK FRAME BOEING727 727232 1384082NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11403DA 21147 DURING E-1 LETTER CHECK, FOUND RT MLG UPLOCK FRAME CRACKED AT FS 913.5, ABOVE RADIUS BLOCK. REPAIRED PER MM 53-11-0 PG 834-837. 2L73 4F A3WE 19950203002311995020300231NM 1995 2 3 DL72S950438 119950126A5350 FAIRING BOEING727 727232 1384082NM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING INSPECTION, FOUND FUSELAGE TO WING BODY FAIRING RIGHT SIDE WITH A 7 INCH CRACK FS 720E PLUS 12 INCHES. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950203002321995020300232NM 1995 2 3 DL72W950406 119950129A5754651622295 RIB BOEING727 727247 138408FNM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 DURING SHOP INSPECTION, FOUND NR 6 RIB FOR NR 3 SLAT CRACKED. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950203002331995020300233NM 1995 2 3 DL72W950407 119950104A5753652163253A SPAR BOEING727 727247 138408FNM NR 2 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, A NR 2 MIDFLAP WAS ROUTED TO SHOP FOR RESTORATION. SHOP INSPECTION FOUND THE AFT SPAR RAIL CRACKED 41 INCHES TO 55 INCHES FROM I/B END. DAMAGE WAS REPAIRED PER M/M 57-52-0 PG.807 2L73 4F A3WE 19950203002341995020300234NM 1995 2 3 DL72W950408 119950104A5753652163253A SPAR BOEING727 727247 138408FNM NR 2 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, A NR 2 MID FLAP BN 186 WAS ROUTED TO THE SHOP FOR RESTORATION. SHOP INSPECTION FOUND THE AFT SPAR RAIL TO BE CRACKED AT THE AFT DRIVE ROD CUT. DAMAGE WAS REPAIRED PER MM 57-52-0 PG 807. 2L73 4F A3WE 19950203002351995020300235NM 1995 2 3 DL72W950415 119950123A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 STA 1303 INSIDE VERT STAB WEB CRACKED AT BOTH O/B ENDS AT FLOORLINE. FABRICATED RT AND LT DOUBLERS 2024T3 .040 AS PER SRM 53-10-4 PG 45. DAMAGE FOUND AT HMV. 2L73 4F A3WE 19950203002361995020300236NM 1995 2 3 DL72W950417 119950121A5753652163262 RAIL BOEING727 727247 138408FNM NR 3 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 NR 3 MID FLAP WAS FOUND TO HAVE A CRACKED T/E LOWER RAIL 53 INCHES TO 57 INCHES FROM I/B END. REPAIRED PER MM 57-52-0. DAMAGE FOUND AT SHOP HMV VISIT. 2L73 4F A3WE 19950203002371995020300237NM 1995 2 3 DL72W950426 119950125A5754 RIB BOEING727 727247 138408FNM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 NR 2 SLAT RIB AND NR 3 CRACKED AT RADIUS FORM LWR RIB CAP. FABRICATED REPAIR PER MM 57-54-0 PG 806-807. FOUND DURING HMV. 2L73 4F A3WE 19950203002381995020300238NM 1995 2 3 DL72W950429 119950123A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND STR 15R CRACKED AT RT FUS WING L/E LT BOX AFT OF FS 720A. REPAIRED PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19950203002391995020300239NM 1995 2 3 DL72W950433 119950111A5320 ANGLE BOEING727 727247 138408FNM LWR FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND CORROSION DAMAGE ON T-ANGLE ANT HINGE ATTACH AREAS FOR LOWER FUSELAGE ACCESS PANEL 3448R. REPAIRED PER MM 53-30-1 PG 801. 2L73 4F A3WE 19950203002401995020300240NM 1995 2 3 DL72W950434 119950105A5240 SKIN BOEING727 727247 138408FNM SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, R-2 SERVICE DOOR WAS FOUND WITH SKIN CRACKED AT UPPER HINGE ARM CUTOUT. REPAIRED PER SRM 52-40-2 PG 15. 2L73 4F A3WE 19950203002411995020300241NM 1995 2 3 DL72W950435 119950105A5313 STRINGER BOEING727 727247 138408FNM FS 500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING HMV, FOUND LOWER FUSELAGE STRINGER 27L CORRODED AT FS 500 TO 520. REPAIRED PER SRM 53-10-3 PG 3. 2L73 4F A3WE 19950203002431995020300243NM 1995 2 3 DL733950388 119950112A57536546430132 SKIN BOEING737 737347 1384647NM NR 3 FORE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308WA 23441 709217 DURING HMV SHOP INSPECTION, RIGHT WING NR 3 FORE FLAP WAS FOUND WITH DENTED SKIN, LOWER LEADING EDGE JUST OUTBOARD OF INBOARD ATTACH POINT. REPAIRED PER SRM 57-53-01 FIG 201. 2L72 4F RTA16WE 19950203002441995020300244NM 1995 2 3 DL73S950373 119950126A3610655812310 DUCT BOEING737 737232 1384475NM NR 1 ENGINE CRACKED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11324DL 23096 DURING CLIMB-OUT, HAD NR 1 ENGINE OVERHEAT LIGHT. RETURNED SLC, AND FOUND CRACKED BLEED DUCT. REPLACED DUCT, OPERATION NORMAL. 2L72 4F RTA16WE 19950203002451995020300245NM 1995 2 3 DL73S950384 119950126A5542 SKIN BOEING737 737232 1384475NM RUDDER PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 709217 FOUND DURING LETTER CHECK, L2 SMALL HOLE IN RUDDER. APPROXIMATELY .5 INCHES DIAMETER, 7 FEET FROM TOP OF RUDDER, AND APPROXIMATELY 7 INCHES AFT OF HINGE LINE. REPAIRED PER SRM 55-40-5. 2L72 4F RTA16WE 19950203002461995020300246NM 1995 2 3 DL73S950385 119950126A5280 DOOR BOEING737 737232 1384475NM LT MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 709217 FOUND DURING LETTER CHECK, L2 MLG INNER DOOR CRACKED AT T/E. REPAIRED PER SRM 51-40-13. 2L72 4F RTA16WE 19950203002471995020300247NM 1995 2 3 DL73S950386 119950126A5330 SKIN BOEING737 737232 1384475NM FS 211-259 LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11328DL 23100 709217 FOUND DURING LETTER CHECK, L2 LIGHTNING STRIKES ON LEFT FWD FUSELAGE BETWEEN STA 211 TO 259. BLENDED AREAS PER SRM 53-30-3. DYE CHECK OK, TREATED AREA PER SRM 53-30-3 2L72 4F RTA16WE 19950203002481995020300248NM 1995 2 3 DL73S950395 119950121A5523 SKIN 65C2638425SPBOEING737 737232 1384475NM ELEV TAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11327DL DL4 23099 709217 DURING SHOP INSPECTION, FOUND LEFT ELEVATOR TAB WITH DAMAGE TO COMPOSITE SKIN AT TAB HINGE CUTOUTS. REPAIRED PER SRM 55-20-1. 2L72 4F RTA16WE 19950203002491995020300249 1995 2 3 DL757950409 419950129A2200W28112013R20 AUTOPILOT WIRE BOEING757 757232 1384965NM STAB ACCY COMPT BURNT A DALAK NONE O OTHER ININSP/MAINT 1 SO11660DL 24422 TROULBLESHOOTING FAULTY RT FCC. FOUND WIRES W2811-2013R AND W2811-2013B, SHORTED AND BURNED IN THE STABILIZER ACCESORY COMPARTMENT. THE WIRES HAD CHAFED AGAINST THE RIGHT STAB BUNGIE SUPPORT. REPAIRED WIRES, OPERATION NORMAL. 2L72 4F RTA2NM 19950203002501995020300250NM 1995 2 3 DL757950410 119950122A5753 SKIN BOEING757 757232 1384965NM NR 3 AFT FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 DURING HMV, #3 AFT FLAP LOWER SURFACE CRACKED AT CENTER OF FLAP. REPAIRED PER SRM 57-70-17. 2L72 4F RTA2NM 19950203002511995020300251NM 1995 2 3 DL757950411 119950126A5315 FLOORBEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 AT HMV, FLOORBEAM FS 324 WAS CORRODED AT RBL 0. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-08 PAGE 201. 2L72 4F RTA2NM 19950203002521995020300252NM 1995 2 3 DL757950412 119950126A5315 FLOOR BEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 AT HMV, CORROSION ON TOP FLANGE OF FLOORBEAM FS 324 RBL 50. CLEANED CORROSION AND REPAIRED PER SRM 53-10-08. 2L72 4F RTA2NM 19950203002531995020300253NM 1995 2 3 DL76S950387 119950126A5753 WEDGE BOEING767 767332 1382001NM NR 4 TE FLAP DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11119DL 23278 709217 FOUND DURING J-2 LETTER CHECK, DELAMINATION AREA ON LOWER SKIN OF NR 4 FLAP T/E WEDGE. REPAIRED PER SRM 51-70-07, AND PAINTED AREA. 2L72 4F RTA1NM 19950203002541995020300254WP 1995 2 3 DLL10950391 119950115A57531529112110AD VANE SKIN LKHEED1011 10113851 5265010WP NR 1 TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 709217 DURING SHOP ISNPECTION, FOUND 3 DENTS ON THE LOWER SKIN OF NR 1 RT FLAP VANE. A FLUSH REPAIR WAS INSTALLED PER SRM 57-53-00 FIG 806. 2L73 4F A23WE 19950203002551995020300255WP 1995 2 3 DLL10950392 119950115A57531529112110AD VANE SKIN LKHEED1011 10113851 5265010WP NR 1 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 709217 DURING SHOP INSPECTION, FOUND CRACK IN UPPER SKIN 39 INCHES FROM O/B EDGE ON NR 1 RT FLAP VANE. A FLUSH REPAIR WAS INSTALLED PER SRM 57-53-00 PG 811. 2L73 4F A23WE 19950203002561995020300256WP 1995 2 3 DLL10950393 119950115A57531529112110AD VANE SKIN LKHEED1011 10113851 5265010WP NR 1 TE FLAP GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 709217 DURING SHOP INSPECTION, A DEEP GOUGE ON UPPER SKIN AT THE I/B EDGE OF THE NR 1 RT FLAP VANE. AN EXTERNAL REPAIR WAS INSTALLED PER SRM 57-53-00 FIG 805. 2L73 4F A23WE 19950203002571995020300257WP 1995 2 3 DLL10950396 119950115A57531529112109 VANE SKIN LKHEED1011 10113851 5265010WP NR 1 TE FLAP GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 709217 DURING SHOP INSPECTION, FOUND GOUGE IN UPPER SKIN OF THE NR 1 RT FLAP VANE. AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 57-53-00 PG 810. 2L73 4F A23WE 19950203002581995020300258WP 1995 2 3 DLL15950431 119950128A253050226 OVEN LKHEED1011 10113853 5265020WP GALLEY FIRE A DALAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CRCRUISE 1 SO11754DL 193Y1181 DURING CRUISE, HAD DEBRIS IN GALLEY OVEN CATCH FIRE. EXTINGUISHED FIRE USING HALON BOTTLE. REPLACED OVEN AND FIRE BOTTLE. RETURNED TO SERVICE. 2L73 4F A23WE 19950203002591995020300259WP 1995 2 3 DLL16950394 119950105A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 1763 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING HMV, FOUND CABIN FLOOR BEAM CORRODED AFT GALLEY/SERVICE CENTER, FS 1763 FROM RBL37 TO THE R-3 DOOR THRESHOLD. 2L73 4F A23WE 19950203002601995020300260WP 1995 2 3 DLL16950398 119950105A5343 FITTING LKHEED1011 10113853 5265020WP RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING HMV, RT MLG RETRACT ACTUATOR FITTING FOUND TO HAVE CORROSION ON FWD AND AFT FACES AND HOLES 1, 2, AND 4. BURNISHED FITTING FACES AND MACHINED HOLES TO REMOVE CORROSION AS PER SRM 57-14-00. INSTALLED CAD PLATED BUSHINGS. 2L73 4F A23WE 19950203002611995020300261WP 1995 2 3 DLL16950399 119950106A5343 FITTING LKHEED1011 10113853 5265020WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 709217 DURING HMV, LT MLG RETRACT ACTUATOR FITTING HOLES 1, 2, 3, 4, 5, AND 6 FOUND TO HAVE CORROSION. REAMED HOLES 1 THROUGH 6 TO REMOVE CORROSION, AND INSTALLED BUSHINGS PER SRM 57-14-00 PGS 819 AND 820. 2L73 4F A23WE 19950203002621995020300262WP 1995 2 3 DLL16950401 119950112A5330 SKIN LKHEED1011 10113853 5265020WP FS 729-846 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND CORROSION ON FUSELAGE SKIN BETWEEN FS 729 AND FS 846, STRINGER 332 AND 33. ROUTED OUT INTERNAL BONDED DOUBLER, AND REMOVED CORROSION AS PER SRM 53-33-00 FIG 836. 2L73 4F A23WE 19950203002631995020300263WP 1995 2 3 DLL16950405 119950107A5343 FITTING LKHEED1011 10113853 5265020WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING HMV, FOUND LT MLG SUPPORT FITTING UPPER FLANGE HOLES 1, 2, 3, 4, 5, AND 6 WERE CORRODED. REAMED HOLES 1 THROUGH 6, AND REMOVED CORROSION PER SRM 57-14-00 PG 809-811. INSTALLED BUSHINGS, TREATED AND PAINTED. 2L73 4F A23WE 19950203002651995020300265NM 1995 2 3 DLM88950372 119950126A5230 PAN DOUG MD88 MD88 3023688NM AFT CARGO DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11994DL 53346 DURING C-2 LETTER CHECK, C-3 BAG BIN DOOR AFT PAN GOUGED AT HOLD OPEN. REPAIRED PER SRM 52-05 FIG 27 SH 1-3. 2L72 4F RTA6WE 19950203002661995020300266NM 1995 2 3 DLM88950419 119950124A5752 TAB SKIN DOUG MD88 MD88 3023688NM LT AILERON DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11932DL 49719 DURING SHOP INSPECTION, LEFT WING AILERON TAB INBD, OUTBD T/E CORNERS WERE FOUND TO BE DAMAGED. THESE DAMAGES WERE REPAIRABLE PER SRM 51-70-1A, REPAIR NR 18, PG 109. PATCHED BOTH CORNERS WITH A GRAPHITE PRECURED PATCH. 2L72 4F RTA6WE 19950203002671995020300267NM 1995 2 3 DLM88950430 119950127A332003980 BALLAST DOUG MD88 MD88 3023688NM CABIN LIGTS BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11951DL 49882 DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN OVERHEAD LIGHT AREA AT SEAT ROWS 28 TO 29AB. SHUT-OFF LIGHTS AND ODOR WAS LESS PRONOUNCED. REPLACED BALLAST B6-50 AT SEAT ROW 31AB. OPERATION NORMAL. 2L72 4F RTA6WE 19950203002681995020300268NM 1995 2 3 DLM88950432 119950128A3260HO5A00354 CAWS BOX DOUG MD88 MD88 3023688NM LANDING GEAR FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11939DL 49812 DURING CRUISE, ALL THREE UNSAFE LANDING GEAR LIGHTS ILLUMINATED AT 1 HOUR INTO FLIGHT. ALL OTHER INDICATIONS NORMAL. LANDED TPA WITHOUT INCIDENT. REPLACED CAWS BOX AND PROX BOX, AND SWUNG GEAR. OPERATION NORMAL. 2L72 4F RTA6WE 19950203002691995020300269WP 1995 2 3 MWEA95115 119950126A24201032200 SWITCH DOUG DC9 DC932 3022066WP COCKPIT MALFUNCTIONED A MWEAK NONE O OTHER UKUNKNOWN 1 GL31501ME 47132 CAPTAIN'S FLIGHT DIRECTOR INOP. FOUND THAT WHEN EMERGENCY POWER SWITCH IS CYCLED, ALL CONTACTS WOULD NOT TOGGLE BACK TO THE OFF POSITION. REPLACED SWITCH. 2L72 4F A6WE 19950203002701995020300270WP 1995 2 3 MWEA95116 119950127A3350100865 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP AFT LAV INOPERATIVE A MWEAK NONE L NO TEST CRCRUISE 1 GL31204ME 1008 47680 PILOT REPORTED AT CRUISE, THE LAST 5 LIGHTS ON THE EMERGENCY FLOOR TRACK LIGHTING CAME ON DIMLY. PILOT TESTED SYSTEM, AND RESET BREAKER. UPON RETURN TO MKE, MECHANICS REPLACED AFT FLOOR TRACK LIGHTING BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950203002711995020300271WP 1995 2 3 MWEA95117 119950127A2560113313 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER CRCRUISE 1 GL31302ME 47102 PILOT REPORTS WHILE EN ROUTE TO MKE, THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF. MECHANIC REINSTALLED SLIDE COVER, AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950203002721995020300272SW 1995 2 3 QXEA9500027 119950128A2150 AC PACK SWRNGNSA227 SA227AC 8780603SW NR 2 EXCESS OIL A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM0926932 AC660 BOI - WITH THE NR 2 BLEED SELECTED, THERE IS SOME SMOKE IN THE CABIN. INSPECTED THE NR 2 ENG INTAKE, NO OIL NOTED. REMOVED THE DRAIN PLUG ON THE NR 2 COOLING TURBINE AND DRAINED SOME EXCESS OIL. REINSTALLED THE PLUG. OPERATIONAL CHECK OF THE NR 2 BLEED AIR WAS NORMAL,AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA8SW 19950203002731995020300273EU 1995 2 3 QXEA9500028 119950128A3231 DOOR UPLOCK FOKKERF28 F28MK1000 4990808EU RT MLG OUT OF ADJUST A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09452US 11105 PDX - WITH THE GEAR RETRACTED THE RT MAIN GEAR RED LIGHT STAYED ON. ADJUSTED THE RT DOOR UPLOCK BRACKET AND STOP IAW MM 32-10-07 PG 203 B AND C. THE SYSTEM CHECKED GOOD DURING GEAR SWINGS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950203002741995020300274SW 1995 2 3 QXEA9500029 119950129A2150 PACK SWRNGNSA227 SA227AC 8780603SW RIGHT BLEED SMOKING A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM0926932 AC660 BOI - SMOKE IN THE CABIN FROM THE RIGHT BLEED WHEN THE ENGINE GOES INTO BETA RANGE. SYSTEM PLACED ON MEL, AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA8SW 19950203002751995020300275EU 1995 2 3 QXEA9500030 119950129A3230 UPLOCK ROLLERS FOKKERF28 F28MK1000 4990808EU RT MLG OUT OF ADJUST A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09452US 11105 PDX - THE RT MAIN GEAR UNLOCK RED LIGHT ILLUMINATES IN FLIGHT. ADJUSTED THE INBOARD UPLOCK ROLLER ASSY, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950203002761995020300276WP 1995 2 3 95ZZZW28 119950104A335020131A EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST TXTAXI/GRND HDL 1 NM01956AS 48079 PDX - PRIOR TO DEPARTURE OF FLIGHT NR 338, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AFT OF ROW 10 WITH EMERGENCY LIGHT ARMED OR OFF. REPLACED BATTERY CHARGER AND PACK, LIGHTS OPERATED NORMALLY. REFERENCE ASAA95008. 2L72 4F A6WE 19950203002871995020300287NM 1995 2 3 ASAA95001 119950101A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01756AS 25097 SEA - DURING MAINTENANCE CHECK, FIVE MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 15 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950203002881995020300288WP 1995 2 3 ASAA95002 119950102A5210591473027 LINKAGE DOUG DC9 DC983 3022083WP L-1 DOOR BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01972AS 53448 SEA - DURING MAINTENANCE CHECK, THE L-1 DOOR GUST LOCK WAS FOUND INOPERATIVE. REPLACED BROKEN GUST LOCK LINKAGE, ADJUSTED AND LOCK OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950203002891995020300289NM 1995 2 3 ASAA95003 119950101A3350654681530 EEL TRACK BOEING737 737290C 138448VNM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - DURING C-CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FLOOR TRACKS AND REWIRED TRACK SECTION, LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950203002901995020300290WP 1995 2 3 ASAA95004 119950102A335041B004AD07G3 EEL BATTERY DOUG DC9 DC982 3022082WP O/W EXIT LIGHTS DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950203002911995020300291WP 1995 2 3 ASAA95005 119950103A335060030431 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19 THROUGH 22. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950203002921995020300292WP 1995 2 3 ASAA95006 119950103A52103917973503 HANDLE DOUG DC9 DC982 3022082WP L-1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01956AS 48079 PDX - FLT 337 - CREW REPORTED THE L-1 DOOR HANDLE WAS DIFFICULT TO CLOSE. LUBED LOWER RIGHT LATCH AND DOOR OPERATED NORMALLY. (W) 2L72 4F A6WE 19950203002931995020300293WP 1995 2 3 ASAA95007 119950104A335020131A EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST DEDESCENT 1 NM01956AS 48079 OAK - FLT 436 - ON ARRIVAL, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AFT OF ROW 10 DURING DESCENT. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950203002941995020300294WP 1995 2 3 ASAA95008 119950104A3350RPS1B EEL BATT CHARGER DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST TXTAXI/GRND HDL 1 NM01956AS 48079 PDX - FLT 338 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AFT OF ROW 10 WITH EMERGENCY LIGHT ARMED OR OFF. REPLACED BATTERY CHARGER AND PACK, LIGHTS OPERATED NORMALLY. REFERENCE 95ZZZW28. 2L72 4F A6WE 19950203002951995020300295WP 1995 2 3 ASAA95009 119950105A3350 EEL SWITCH DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01930AS 49231 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FAILED TO TEST PROPERLY. SECURED LOOSE SWITCH AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950203002961995020300296NM 1995 2 3 ASAA95010 119950106A3350883200312 EEL TRANSMITTER BOEING737 737290C 138448VNM CABIN WEAK A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WOULD NOT ILLUMINATE. REPLACED AFT TRACK LIGHTING TRANSMITTER AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950203002971995020300297NM 1995 2 3 ASAA95011 119950107A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY (W) 2L72 4F RTA16WE 19950203002981995020300298WP 1995 2 3 ASAA95012 119950107A3350303 EEL LAMP DOUG DC9 DC983 3022083WP L1 DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01962AS 53076 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. RELAMPED AND LIGHT OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950203002991995020300299SO 1995 2 3 WTAA950031 119950106A5270JS5 ROLLER EMB 120 EMB120RT SO PAX DOOR LACK OF LUBE A WTAAK NONE N FALSE WARNING DEDESCENT 1 WP17454UE 120155 MRY - FORWARD DOOR WARNING LIGHT ACTIVATED DURING DESCENT. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE FOUND MICROSWITCH ROLLER STICKING. CLEANED AND LUBED MICROSWITCH ACTUATOR ROLLER. SYSTEM OPERATIONAL TEST NORMAL. (W) 2L72 4T RTA31SO 19950203003001995020300300SO 1995 2 3 WTAA950032 119950108A5270MS250851 SWITCH EMB 120 EMB120RT SO PAX DOOR BROKEN WIRE A WTAAK NONE P NO WARNING INDICATION TXTAXI/GRND HDL 1 WP17251YV 120251 SFO - FORWARD DOOR WARNING LIGHT FAILS TO ACTIVATE WITH DOOR OPEN ON GROUND. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE FOUND BROKEN WIRE AT PASSENGER DOOR MICROSWITCH. REPAIRED WIRE AT MICROSWITCH. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. 2L72 4T RTA31SO 19950203003021995020300302SO 1995 2 3 WTAA950035 119950109A2750 CONNECTOR EMB 120 EMB120RT SO LT TE FLAP DIRTY A AWTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17455UE 120163 ACV - FLAP ASYMMETRY REPORTED WITH FLAPS SET TO 15 DEGREES IN FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FLAP SYSTEM FOUND MOISTURE IN LEFT OUTBOARD FLAP ACTUATOR ELECTRICAL CONNECTORS. CLEANED AND RESECURED CONNECTOR. FLAP SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003031995020300303SO 1995 2 3 WTAA950038D 119950110A323012043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR SHORTED A WTAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP17451UE 120108 SFO - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL MODULE AND RELAY BOX. LANDING RETRACTION AND EXTENSION NORMAL DURING GROUND TEST AND SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003041995020300304SO 1995 2 3 WTAA950040 119950110A3240741VR0253C13ZBV LIGHT SOCKET EMB 120 EMB120RT SO PARKING BRAKE SHORTED A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17455UE 120163 SFO - PARK BRAKE INDICATION LIGHT ILLUMINATED DURING APPROACH TO LANDING. CREW RESET PARK BRAKE HANDLE, LIGHT REMAINED ILLUMINATED. CREW DECLARED AN EMERGENCY AND CONTINUED APPROACH. AIRCRAFT LANDED AT STATION WITHOUT INCIDENT. MAINTENANCE DISCOVERED SHORTED LIGHT SOCKET. REPAIRED SOCKET. PARK BRAKE LIGHT OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003051995020300305SO 1995 2 3 WTAA950044 119950115A2750MS3126P1210S CONNECTOR EMB 120 EMB120RT SO LT TE FLAP LOOSE A WTAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP17285UE 120153 RDM - FLAP DISAGREEMENT REPORTED WITH FLAPS SELECTED TO 15 DEGREES. FLAP ASYMMETRY REPORTED FOLLOWING RESET OF FLAPS. LEFT OUTBOARD FLAP SHOWING 3 BARS BEYOND SELECTED SETTING. AIRCRAFT FERRIED TO FAT FOR MAINTENANCE. MAINTENANCE FOUND LOOSE WIRES AT LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG. RESECURED WIRES. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003061995020300306SO 1995 2 3 WTAA950045 119950115A2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A WTAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP17281UE 120092 SFO - FLAP CONTROL FAULT REPORTED DURING TAKEOFF ROLL AT APPROXIMATELY 70 KNOTS. TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED FLAP SYSTEM. NO DEFECTS NOTED. CLEARED FLAP CONTROL UNIT AND FLAP ANNUNCIATOR FAULTS. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950203003071995020300307SO 1995 2 3 WTAA950046 119950115A5270 WARNING EMB 120 EMB120RT SO PAX DOOR ILLUMINATED A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17453UE 120148 REN-SFO - EN ROUTE, FORWRD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT CONTINUED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED PASSENGER DOOR AND DOOR WARNING SYSTEM. NO DEFECTS NOTED. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003081995020300308SO 1995 2 3 WTAA950047 119950115A5270JS5 ROLLER EMB 120 EMB120RT SO PAX DOOR OUT OF ADJUST A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17279UE 120085 SFO - FORWARD DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT CONTINUED TO STATION, LANDING WITHOUT INCIDENT. MAINTENANCE ADJUSTED PASSENGER DOOR MICROSWITCH ROLLER. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003091995020300309SO 1995 2 3 WTAA950048 119950115A5270JS5 ROLLER EMB 120 EMB120RT SO PAX DOOR OUT OF ADJUST A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17455UE 120163 SFO - FORWARD DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED PASSENGER DOOR MICROSWITCH ROLLER. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003101995020300310SO 1995 2 3 WTAA950050 119950115A2612MS3456KT14S5S CONNECTOR EMB 120 EMB120RT SO APU DIRTY A WTAAK NONE N FALSE WARNING LDLANDING 1 WP17120AM 120012 FAT - APU FIRE WARNING INDICATION DURING LANDING. MAINTENANCE DETERMINDED FIRE DETECTION SYSTEM WAS PREVIOUSLY DEFERRED AND APU WAS NOT IN USE AT TIME OF FALSE FIRE WARNING. SUBSEQUENTLY MAINTENANCE CLEARED DEFFERAL WITH THE REPLACEMENT OF THE APU FIRE DETECTOR CANNON PLUG. (W) 2L72 4T RTA31SO 19950203003111995020300311SO 1995 2 3 WTAA950052 119950116A2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A WTAAO OTHER J WARNING INDICATION LDLANDING 1 WP17284UE 120145 RNO - FLAP ASYMMETRY REPORTED ON SELECTION OF FLAPS TO 25 DEGREES DURING LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND INSPECTED FLAP SYSTEM. COULD NOT DUPLICATE DISCREPANCY. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003121995020300312SO 1995 2 3 WTAA950053 119950116A2750MS3126P1210S CONNECTOR EMB 120 EMB120RT SO RT TE FLAP MOISTURE CONTAM A AWTAAO OTHER J WARNING INDICATION LDLANDING 1 WP17284UE 120145 RNO - FLAP ASYMMETRY REPORTED ON SELECTION OF FLAPS TO 25 DEGREES DURING LANDING. RT OUTBOARD FLAP INDICATING 10 DEGREES LESS THAN OTHER FLAPS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND INSPECTED FLAP SYSTEM. DISCOVERED MOISTURE IN RT OUTBOARD FLAP ACTUATOR CANNON PLUG. REMOVED MOISTURE FROM CANNON PLUG AND APPLIED GELTEK PROTECTIVE TAPE TO CONNECTOR. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003131995020300313EU 1995 2 3 WTAA950054 119950116A527091SE13 SWITCH BAG JETSTMJETSTM3101 1500215EU PAX DOOR WORN A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17417UE 794 SEA - PASSENGER DOOR CAPTION REMAINS ILLUMINATED WITH DOOR CLOSED. DEFERRED DOOR WARNING SYSTEM PER MEL 52-2. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE REPLACED DOOR HANDLE MICROSWITCH. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. (W) 2L72 4T RTA21EU 19950203003141995020300314NE 1995 2 3 WTAA950055 219950117A7321 EEC WARNING EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE ACTIVATED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17282UE 120124 SFO - ELECTRIC ENGINE CONTROL (EEC) FAILURE AURAL WARNING INDICATION RECEIVED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESET EEC. SYSTEM OPERATIONAL CHECK NORMAL. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T4 TRTA31SO E20NE 19950203003151995020300315SO 1995 2 3 WTAA950056 119950117A3350036604001 EEL BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17251YV 120251 FAT -FORWARD CABIN EMERGENCY LIGHTS FAIL TO TEST. MAINTENANCE REMOVED AN REPLACED FORWARD CABIN EMERGENCY LIGHT BATTERY PACK. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203003451995020300345NE 1995 2 3 95ZZZX508 219950106A8530 EXHAUST VALVE BEECH 18 E18S 1151006CE PWA R985 R985AN14B 52008NE NR 5 CYL STICKING A VLLAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS DEDESCENT 1 GL058711H 932 BA87 21230 LEFT ENGINE STARTED RUNNING ROUGH ON DESCENT INTO LEX. FOUND NR 5 CYLINDER WITH ZERO COMPRESSION, IT APPEARED THE EXHAUST VALVE WAS STICKING IN THE VALVE GUIDE AND NOT CLOSING COMPLETELY ON THE VALVE SEAT. 1L72 3R3 R A765 5E1 19950203003551995020300355EU 1995 2 3 95ZZZX518 119950104A493028616 FEED LINE BRAERO1000 BAE1251000 1500287EU APU FUEL BURNED A DXTAK NONE O OTHER ININSP/MAINT 1 GL07520QS1013 NA1008 FOUND DURING PRE-FLIGHT. APU FUEL FEED HOSE WAS BURNED THROUGH THE PLASTIC SHIELD AND INTO THE HOSE INSULATION. BLEEDAIR FROM LEFT MIXER VALVE IS BURNING THE APU FUEL FEED LINE. NEED LINE ROUTED AWAY FROM BLEED AIR. 2L72 4F RTA3EU 19950203003651995020300365NM 1995 2 3 9501675508 119950130A5320146N852251 CHORD BOEING757 757251 1384970NM FS 1380-1442 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01508US 30360 23197 DURING PERIODIC CHECK, THE AFT CARGO LOWER DOOR SILL INNER CHORD WAS FOUND CORRODED. REMOVED CORROSION AND REPAIRED PER NWA EA 55-93722. 2L72 4F RTA2NM 19950203003661995020300366NM 1995 2 3 9501685508 119950128A5315146N5091 FLOOR BEAM BOEING757 757251 1384970NM FS 1681 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01508US 30360 23197 DURING PERIODIC CHECK, THE FLOOR BEAM UPPER CHORD WAS FOUND CORRODED AT FS 1681, LBL 4 TO LBL 21, AND AT RBL 14. REMOVED CORROSION AND REPAIRED PER NWA EA 55-93720 AND 55-93719. 2L72 4F RTA2NM 19950203003671995020300367NM 1995 2 3 9501692706 119950130A2722591005015 POWER PACK BOEING727 727225 1384077NM RUDDER LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01815EA7011 7011 22552 AFTER TAKEOFF, HYDRAULIC SYSTEM 'A' AND 'B' QUANTITY DECREASING SLOWLY. SYSTEM 'A' QUANTITY STOPPED AT 2.5 GALLONS WHILE 'B' SYSTEM CONTINUED TO DECREASE. ISOLATED HYDRAULIC FLUID LOSS TO SYSTEM 'B' RUDDER. FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 'B' SYSTEM RUDDER POWER PACKAGE. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950203003681995020300368NE 1995 2 3 9501706615 219950131A7530 EVCB 7724991 BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN RX PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT DEDESCENT 1 GL01615US 92397 20360 702451 DURING TOP OF DESCENT FL410, THE NR 4 ENGINE EXPERIENCED A SURGE AND FLAMED-OUT. A RESTART AT FL340 WAS SUCCESSFUL AND OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED, FUEL PRESSURES WERE CHECKED, AND A BORESCOPE WAS ACCOMPLISHED. THE EVBC WAS REPLACED, AND A PRECISION TRIM WAS ACCOMPLISHED. PROPER ENGINE OPERATION WAS CONFIRMED. 2L74 4F4 F A20WE E3NE 19950203003691995020300369NM 1995 2 3 95FDEA00093 119950125A5347BAC15201434 SEAT TRACK BOEING727 7272S2F 1384O81NM BS 523 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04205FE 22927 SEAT TRACK HAS MECHANICAL DAMAGE ON TOP SURFACE OF BS 523 RBL 45 WL 209. REMOVED FABRICATED AND INSTALLED SEAT TRACK IAW SRM 53-10-5. 2L73 4F A3WE 19950203003701995020300370NM 1995 2 3 95FDEA00094 119950125A5347BAC15201331 SEAT TRACK BOEING727 7272S2F 1384O81NM BS 517-523 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04205FE 22927 SEAT TRACK HAS MECHANCIAL DAMAGE ON TOP SURFACE BS 517-523, BL O, WL 209. BLENDED DAMAGE, IT WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK BS 360-550, BL O, WL 208 IAW SRM 53-10-2. 2L73 4F A3WE 19950203003711995020300371NM 1995 2 3 95FDEA00095 119950124A53112MM135844 FRAME BOEING727 72725 1384006NM BS 211.8 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 CORROSION ON FRAME BS 211.8, RBL 18, WL 168. REPAIRED FRAME AT BS 211.8, RBL 18 WL 168, AS PER FEDEX SRM 51-40-4. 2L73 4F A3WE 19950203003721995020300372NM 1995 2 3 95FDEA00096 119950124A53157075T6 FLOOR BEAM BOEING727 72725 1384006NM BS 312 CORRODED WEB A FDEAK NONE O OTHER ININSP/MAINT 1 SO25503FE 18273 CORROSION ON WEB OF FLOOR BEAM BS 312, LBL 57, WL 205. REMOVED AND REPLACED WEB PER FEDEX EA 7-5310-23657. 2L73 4F A3WE 19950203003731995020300373NM 1995 2 3 95FDEA00097 119950124A531165176641 FRAME BOEING727 72725 1384006NM BS 520 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04503FE 18273 FRAME AT BS 520, STR 22L IS CRACKED IN UPPER FLANGE OF FRAME. REMOVED AND REPLACED NEW FRAME. 2L73 4F A3WE 19950203003741995020300374NM 1995 2 3 95FDEA00099 119950124A5330202473 SKIN BOEING727 72721C 138400MNM BS 1342 DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 FASTENERS PULLED THROUGH SKIN AT BS 1342, STR 20R. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND FORMER SKIN REPAIR PER FEDEX SRM 53-30-3 AT BS 1342 STR 20R. 2L73 4F A3WE 19950203003751995020300375NM 1995 2 3 95FDEA00100 119950124A532065207323 SILL WEB BOEING727 72721C 138400MNM BS 1050-1057 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 IN AFT CARGO AT STA 1050-1057 WL 146, RBL 20 THE SILL WEB IS CRACKED. REMOVED CRACKED WEB, FABRICATED NEW WEB AND INSTALLED SILL WEB PER FEDEX SRM 51-20-1. 2L73 4F A3WE 19950203003761995020300376NM 1995 2 3 95FDEA00101 119950124A5320651841713 STIFFENER BOEING727 72721C 138400MNM BS 303 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04143FE 19136 STIFFENER ON TOP OF DOG HOUSE, AT BS 303, RBL 10, WL 181 HAS CORROSION. REMOVED AND REPLACED STIFFENER PER FEDEX SRM 53-10-01. 2L73 4F A3WE 19950203003771995020300377WP 1995 2 3 95FDEA00102 119950131A3230 RETRACT MECH DOUG DC10 DC1030F 3023504WP LANDING GEAR MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION LDLANDING 1 SO04321FE 47836 LANDING GEAR DIDN'T EXTEND WHEN LANDING GEAR HANDLE WAS PLACED IN DOWN POSITION. DOORS OPENED, BUT GEAR DIDN'T EXTEND. HYD PRESS WAS OK AND GEAR NOT DOWN CONFIRMED BY GEAR HORN ON STDY AT FLAPS 35 DEGREES. RECYCLED GEAR AND GEAR EXTNEDED ON SECOND ATTEMPT, SLOWLY. CHECKED L/GEAR RETRACTION AND EXTENSION COMPONENTS FOR FAULTS, NONE FOUND. PINNED GEAR AND OPERATED GEAR SELECTOR VALVE SEVERAL TIMES. OPS OK, AND A/C OK FOR SVC. PINS REMOVED. 2L73 4F RTA22WE 19950203003781995020300378NM 1995 2 3 95FDEA00103 119950129A5712BAC2506855 RIB BOEING727 7272S2F 1384O81NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04205FE 22927 HFECI OF FASTENER HOLES AT BS 760, RBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED THREE PLACES IN RIB CHORD, AND BOTTOM FWD HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760, RBL 70.5 PER FEDEX EA 7-5710-2368A. 2L73 4F A3WE 19950203003791995020300379NM 1995 2 3 95FDEA00104 119950129A5712BAC1506855 RIB BOEING727 7272S2F 1384O81NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04205FE 22927 HFECI OF FASTENER HOLES AT BS 760 LBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED IN RIB CHORD, AND BOTTOM HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760 LBL 70.5 PER FEDEX EA 7-5710-23684. 2L73 4F A3WE 19950203003801995020300380NM 1995 2 3 DL72S950180 119950116A711065196854539 COWL BOEING727 727232 1384082NM NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH LEADING EDGE LIP CRACKED. REPAIRED PER SRM 54-30-3. 2L73 4F A3WE 19950203003811995020300381NM 1995 2 3 DL72S950441 119950130A5754 SKIN BOEING727 727225 1384077NM NR 2/3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 FOUND DURING C-1 LETTER CHECK, 1.375 INCH CRACK ON I/B LWR CORNER OF NR 2 L/E FLAP. ALSO, .5 INCH CRACK AT I/B LWR CORNER OF NR 3 L/E FLAP. REPAIRED PER B727 M/M 57-53-0 PG 804. 2L73 4F A3WE 19950203003821995020300382NM 1995 2 3 DL72S950442 119950130A2780 ACT BRACKET BOEING727 727225 1384077NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 FOUND DURING C-1 LETTER CHECK, NR 5 L/E FLAP ACTUATOR BRACKET CRACKED ON O/B SIDE. REPAIRED PER B727 MM 57-20-21 FIG 807. 2L73 4F A3WE 19950203003831995020300383NM 1995 2 3 DL72W950427 119950126A7110 COWL BOEING727 727247 138408FNM NR 3 ENG NOSE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV, NR 3 ENGINE NOSE COWL RING WAS FOUND WORN AT 3 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950203003841995020300384NM 1995 2 3 DL73S950425 119950130A3350 EEL 3114981 BOEING737 737232 1384475NM R 2 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11318DL 23090 DURING SERVICE CHECK, THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOP. REPLACED REFLECTOR AND BULB OPERATION NORMAL. 2L72 4F RTA16WE 19950203003851995020300385NM 1995 2 3 DL73S950439 119950130A5210 AFT CLEVIS BOEING737 737232 1384475NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11325DL 23097 DURING LETTER CHECK M-1, FOUND L1 DOOR UPPER GATE AFT CLEVIS CRACKED. MANUFACTURED AND INSTALLED NEW ANGLE PER ERA 274058-14, REF SRM 52-10-2. 2L72 4F RTA16WE 19950203003861995020300386NM 1995 2 3 DL73S950440 119950130A5522 SKIN BOEING737 737232 1384475NM RT ELEVATOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11325DL 23097 DURING LETTER CHECK M-1, FOUND RT ELEVATOR HAS A HOLE IN LOWER SURFACE. REPAIRED AS PER SRM 51-40-13. 2L72 4F RTA16WE 19950203003871995020300387NM 1995 2 3 DL757950443 119950131A5754114N4004165A WEDGE BOEING757 757232 1384965NM NR 3LE SLAT TE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 DURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT T/E WEDGE WAS FOUND TO BE DELAMINATED. REPAIRED BY PLACING WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950203003881995020300388NM 1995 2 3 DL76L950444 119950130A2781851801 SENSOR BOEING767 767332 1382001NM LT LE SLAT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11178DN 25143 DURING CLIMB-OUT, HAD SLAT ASSYMETRY LIGHT VISUAL CHECK OK SLATS APPEARED UP. ACCOMPLISHED ABNORMAL PROCEDURES, RETURNED JFK. THE SLAT LIGHT CAME ON AT FLAPS 1 DEGREE TO FULL UP. INTERROGATED PSEU, HAD FAULT CODE 280, LEFT OUTER SLAT NR 5 SENSOR. REPLACED SENSOR OPERATION NORMAL. 2L72 4F RTA1NM 19950203003891995020300389NM 1995 2 3 DLM88950418 119950130A302013277505 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE CRACKED A DALAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11985DL 53312 725718 ON CLIMB-OUT, AT AVL WITH ENGINE ANTI-ICE ON, GOT LEFT ENGINE FIRE WARNING. FOLLOWED APPROPIRATE PROCEDURES, WARNING CEASED WHEN POWER WAS REDUCE. FOUND ENGINE NOSE COWL AFT ANTI-ICE AIR DUCT BROKEN. REPLACED DUCT, OPERATION NORMAL. 2L72 4F4 FRTA6WE E9NE 19950203003901995020300390WP 1995 2 3 MWEA95118 119950128A5320 INTERCOSTAL DOUG DC9 DC914 3022034WP FS 245 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 WHILE CHANGING NR 2 GALLEY, A FLANGE WAS FOUND CRACKED ON AN INTERCOSTAL UNDER THE NR 3 SEAT TRACK AT STA 245. THE FLANGE WAS REPAIRED IAW SRM 533-01 FIG 2, AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 19950203003911995020300391WP 1995 2 3 MWEA95119 119950128A53472914913 SEAT TRACK DOUG DC9 DC914 3022034WP FS 209-235 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING NR 2 GALLEY CHANGE, NR 3 SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS AT STA 209 AND 235. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 200 TO S65 IAW SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950203003941995020300394EA 1995 2 3 95ZZZZ36 219950120A73203032125 PY LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE LOOSE A GPPAE ENGINE SHUTDOWN O OTHER TOTAKEOFF 1 CE0917012 UC11 32038 FLT NR 2090 DEPARTED CDR, THE RIGHT ENGINE DECELERATED AND WENT INTO FEATHER (AUTO FEATHER ENGAGED) AFTER TAKEOFF. FLIGHT CREW SHUT DOWN ENGINE AND LANDED SAFELY BACK IN CDR. MAINTENANCE FOUND THE PY LINE LOOSE AT THE FIRESHIELD. 'B' NUT WAS TIGHTENED AND SYSTEM CHECKED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA24CE E4EA 19950203003961995020300396NM 1995 2 3 AWXA9500030 119950112A3350MS27212 EEL TERMINAL BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - ON ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 11-14. REPLACED LIGHT TERMINAL ENDS, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950203003971995020300397NM 1995 2 3 AWXA9500031 119950117A2130 PRESSURIZATION BOEING737 7373G7 1384595NM CABIN MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28322AW 25400 ABQ - FLT 864 - ABQ-PHX - AIR TURN BACK, CREW UNABLE TO PRESSURIZE AIRCRAFT IN AUTO, STANDBY OR MANUAL MODES. AIRCRAFT RETURNED TO ABQ AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE GROUND PRESSURIZED AIRCRAFT, CHECKED OUTFLOW VALVES, DOOR SEALS AND BY-PASS VALVE. ALL OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950203003981995020300398NM 1995 2 3 AWXA9500032 119950118A5330 SKIN BOEING737 737275 1384485NM FS 727B CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20958 PHX - DURING SCHEDULED INSPECTION, FOUND FUSELAGE SKIN CRACKED AT STATION 727B STRINGER 17R. REPAIRED DAMAGE PER SRM 53-30-3. (Z) 2L72 4F A16WE 19950203003991995020300399NM 1995 2 3 AWXA9500033 119950118A5330 SKIN BOEING737 737275 1384485NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20958 PHX - DURING LFEC INSPECTION OF LOWER SKIN LAPS, CRACKS WERE FOUND AT THE FOLLOWING LOCATIONS, STA 381 14R, STA 400 14L, STA 490 14L, STA 597 4L, STA 628 4L, STA 756 14R, STA 777 14L, STA 787 20L, STA 877 20L. ALL AREAS REPAIRED PER EO 53-30-16. (Z) 2L72 4F A16WE 19950203004001995020300400NM 1995 2 3 AWXA9500034 119950118A5330 SKIN BOEING737 737277 1384570NM BS 767 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED 2.25 INCH, STATION 767 STRINGER 19R. REPAIRED SKIN PER SRM 53-30-3, FIG 6. (Z) 2L72 4F RTA16WE 19950203004011995020300401NM 1995 2 3 AWXA9500035 119950118A5753654648146 FLAP CARRIAGE BOEING737 737277 1384570NM NR 7 TRACK FAILED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 750 22655 PHX - FLT 417 - DURING SCHEDULED MAINTENANCE, FOUND RT OUTBOARD MID FLAP INBOARD END BROKEN AWAY FROM NR 7 FLAP TRACK CARRIAGE. REMOVED AND REPLACED NR 7 MAIN TRACK CARRIAGE ASSEMBLY PER BMM 27-51-81. (Z) 2L72 4F RTA16WE 19950203004021995020300402SO 1995 2 3 C2XA95CL008 119950124A2820MS2778423 VALVE EMB 120 EMB120RT SO RT WING OPEN A AC2XAA UNSCHED LANDING FO FLT CONT AFFECTED OTHER TOTAKEOFF 1 SW0934712 120111 FLT 3288 - CLE-GSO - AFTER TAKEOFF, AIRCRAFT ROLLED TO THE LEFT. DISCOVERED A 2000 LBS FUEL IMBALANCE, WITH LEFT WING HEAVY. AIRCRAFT AIR RETURNED TO CLE. MAINTENANCE FOUND RIGHT FUEL TANK DEFUEL VALVE SWITCH IN THE OPEN POSITION. CLOSED SWITCH AND TRANSFERED FUEL FROM LEFT SIDE TO RIGHT. SAFTIED SWITCHES. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950203004031995020300403SO 1995 2 3 C2XA95IA004 119950116A323412038599001 CONTROL HANDLE EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SW0912709 120138 120101 IAH - FLT 7775 - PRIOR TO FLIGHT, THE CREW REPORTED THE NOSE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. MAINTENANCE INSPECTED AND FOUND THE 'A' SYSTEM UNLOCK LIGHT WAS INTERMITTENT. MAINTENANCE REMOVED AND REPLACED THE GEAR CONTROL HANDLE IAW EMB 120 MM 32-30-03. OPERATIONAL CHECK GOOD IAW EMB 120MM 32-30-00. AIRCRAFT WAS RELEASED FOR SERVICE. (Z) 2L72 4T RTA31SO 19950203004041995020300404SO 1995 2 3 C2XA95IA005 119950119A532012004449001 'T' PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND RT AFT 'T' PROFILE CORRODED AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004051995020300405SO 1995 2 3 C2XA95IA006 119950119A532012004170004 'T' PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND RT 'T' PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004061995020300406SO 1995 2 3 C2XA95IA007 119950119A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004071995020300407EU 1995 2 3 C2XA95IA008 119950121A57535751000502100 SKIN AEROSPATR42 ATR42320 8680930EU RT TE FLAP DELAMINATION A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914815 104 IAH - DURING A 4YR 12,000 CYCLE INSPECTION SSI 57-52-04 (PART 4), ULTRASONIC INSPECTION OF FLAP. THE RT INBOARD FLAP, ADJACENT TO RIB NR 5 FLAP ATTACH FITTING, (FWD FITTING INBD SIDE), FOUND A 1.5 INCH BY 1.5 INCH AREA OF DELAMINATION. MAINTENANCE REMOVED AND REPLACED FLAP (P/N 5751000502100) IAW ATR 42MM 57-52-00, OPERATIONAL CHECKS GOOD IAW ATR 42MM JIC 27-51-00 OPT 10000-001. (Z) 2H72 4T RTA53EU 19950203004081995020300408SO 1995 2 3 C2XA95IA011 119950119A532012004149001 'T' PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND RT OUTBOARD 'T' PROFILE CORRODED FRAME 36. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004091995020300409SO 1995 2 3 C2XA95IA012 119950119A532012027929001A BUTT STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND CENTER BUTT STRAP CORRODED FROM FRAME 37, TO 41. MAINTENANCE REMOVED CORROSION, AND INSTALLED NEW SECTION OF BUTT STRAP. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004101995020300410SO 1995 2 3 C2XA95IA013 119950119A532012027929001A BUTT STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND RT BUTT STRAP CORRODED BETWEEN FRAMES 34, AND 39. MAINTENANCE REMOVED CORROSION, AND INSTALLED NEW SECTION OF BUTTSTRAP. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 15,473. (Z) 2L72 4T RTA31SO 19950203004111995020300411WP 1995 2 3 HAL95007 119950114A335041B004A007G3 EEL BATTERIES DOUG DC9 DC951 3022051WP COCKPIT DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13669HA 47654 FOUND ON PREFLIGHT NO COCKPIT EMERGENCY LIGHTS. REPLACED THE BATTERIES IN THE BATTERY PACK B5-23. THE OPERATIONAL CHECK WAS GOOD. (Z) 2L72 4F A6WE 19950203004121995020300412WP 1995 2 3 HAL95009 119950117A3350P401005111 EEL MODULE DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 47662 HNL - THE EMERGENCY EXIT PLACARDED LIGHT AT 18 AB AFT LEFT EMERGENCY OVERWING EXIT BOTTOM IS INOPERATIVE. REMOVED AND REPLACED THE LIGHT CONTROL MODULE. THE OPERATIONAL CHECK WAS GOOD. (Z) 2L72 4F A6WE 19950203004131995020300413WP 1995 2 3 HAL95010 119950118A5330 SKIN DOUG DC9 DC951 3022051WP FS 1209 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 27180 47796 HNL - FOUND APPROX .25 INCH CRACK AT RIVET ON FUSELAGE SKIN STATION 1209 LEFT SIDE APPROXIMATELY 8 INCHES UP FROM ENGINE PYLON. MADE FILLER AND DOUBLER REPAIR PER HAL M105 FILE NR 61044. (Z) 2L72 4F A6WE 19950203004141995020300414WP 1995 2 3 HAL95011 119950117A5330 SKIN DOUG DC9 DC951 3022051WP FS 1247 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 27180 47796 HNL - DURING S-CHECK, FOUND APPROXIMATELY 1.0625 INCH CRACK BETWEEN LONGERON 3R AND LONGERON 4R AT FUSELAGE STATION 1247. MADE FILLER AND INTERNAL DOUBLER REPAIR PER HAL FORM M 105 FILE NR 61038. (Z) 2L72 4F A6WE 19950203004151995020300415EU 1995 2 3 SIMA950121 119950112A32465010488 WHEEL GOODYEAR 50092371 SAAB SF340 SF340A 7850100EU MLG CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21119AE4562 340A119 LAW - DURING INSPECTION OF WHEEL ASSEMBLY FOR TIRE CHANGE, FOUND A THREE INCH CRACK IN BEAD AREA OF HUB P/N 5009237-1, S/N NOV91-0174. HUB WAS REMOVED FROM SERVICE. (Z) 2L72 4T RTA52EU 19950203004161995020300416EU 1995 2 3 SIMA950151 119950115A33506013211 EEL POWER SUPPLY SAAB SF340 340B 7860101EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21593MA 18925 340B206 ORD - FLT 4245 - WHEN POWER IS TAKEN OFF THE AIRCRAFT, THE EMERGENCY LIGHT ILLUMINATES AND WILL NOT EXTINGUISH. RAI EMERGENCY LIGHT POWER SUPPLIES IAW CARD NR 1283. OPS CHECK GOOD, CHANGED ALL 5. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA52EU 19950203004171995020300417EU 1995 2 3 SIMA950171 119950117A3240 BRAKE AEROSPATR72 ATR72212 EU RT MLG FIRE A SIMAO OTHER AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 SW21408AT 408 AFTER LANDING THE ACFT DECELERATED QUICKLY AND PULLED SLIGHTLY TO THE RIGHT. PULLED ONTO RAMP AND HAD TO APPLY POWER FOR TAXI. BRAKE TEMP LIGHT ILLUMINATED AND THE ACFT SETTLED TO THE RT AND A PILOT BEHIND THEM NOTIFIED 408 THAT THEY HAD A FIRE IN THE RIGHT GEAR WELL. STOPPED THE ACFT AND EVACUATED ACFT ON THE LT SIDE. FIRE DAMAGE WAS EVALUATED AND ACFT WAS FERRIED TO DEE HOWARD FOR REPAIR. ALL REPAIRS WERE ACCOMPLISHED UNDER FAA 337 AND THE ATTACHED ATR DRAWINGS. THE ACFT HAD A GEAR RETRACTION CHECK IAW THE AMM AND ALL AFFECTED SYSTEMS WERE FUNCTIONALLY CHECKED SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950203004181995020300418EU 1995 2 3 VTZA95015 119950103A527091SE6 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27314UE 41027 DURING TAKEOFF, FLT NR 6215, FROM IAD TO PVD AT 1235 HRS, ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANFE OPENED DMI 40020 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI 40020 ON 01-06-95 BY ADJUSTING BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950203004191995020300419WP 1995 2 3 VTZA95016 219950111A73108975131 FUEL FILTER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE331* 01514WP RT ENGINE CLOGGED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27481UE 895 DURING CRUISE, FLIGHT NR 6940 FROM CLE TO AVP DIVERTED TO IAD AT 0600 HRS, DUE TO THE RT ENGINE FUEL FILTER BLOCKED CAP LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL FILTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T3 TRTA56EU E2WE 19950203004201995020300420EU 1995 2 3 VTZA95018 119950111A29321379049D HYD PRESS SWITCH BAG JETSTMJETSTM3201 1500217EU RT WING FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27486UE 905 FLT 6368 - CRW-IAD - DURING CLIMB-OUT RETURNED TO CRW DUE TO THE HYDRAULIC SYSTEM HIGH PRESSURE WARNING CAPTION ILLUMINATING IN FLIGHT. MAINTENANCE AT CRW DEFERRED THE INDICATION SYSTEM. WHEN AIRCRAFT ARRIVED AT IAD, MAINTENANCE REPLACED THE OVER PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950203004211995020300421EU 1995 2 3 VTZA95020 119950111A3040 WARNING LIGHT BAG JETSTMJETSTM3201 1500217EU LT WINDSCREEN ILLUMINATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27370MT 800 FLT 6348 - IAD-GSO - ABORTED TH TAKEOFF DUE TO THE CAPTAINS WINDSCREEN CAPTION ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950203004221995020300422EU 1995 2 3 VTZA95021 119950112A7712 SENSOR WIRE JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE BROKEN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27311UE 41029 FLT 6150 - IAD-EWR - ABORTED TAKEOFF DUE TO THE RT ENGINE IEC CAPTION ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENACNE REPAIRED A BROKEN WIRE TO THE TT2 SENSOR P/N 6945059010. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950203004231995020300423EU 1995 2 3 VTZA95022 119950114A2913PV304426 HYDRAULIC PUMP BAG JETSTMJETSTM3201 1500217EU LT/RT ENG FAILED A VTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27489UE 908 FLT NR 6278 - CMH-IAD - DURING CRUISE HAD A COMPLETE LOSS OF HYDRAULIC PRESSURE ON LEFT ENGINE FIRST, THEN RT PRESSURE FAILED. AIRCRAFT RETURNED TO CMH WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOTH HYDRAULIC PUMPS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950203004241995020300424EU 1995 2 3 VTZA95023 119950115A2612D2370120 FIRE LOOP BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 EA27496UE 900 DURING TAXI, THE LEFT ENGINE FIRE WARNING ACTIVATED ON REPOSITION TO THE GATE. CREW DISCHARGED BOTH BOTTLES. MAINTENANCE LATER INSPECTED, BUT FOUND NO VISIBLE SIGNS OF FIRE. MAINTENANCE REPLACED THE FIRE BOTTLES AND THE FIRE CONTROL UNIT. AIRCRAFT WAS RELEASED BUT ON TAXI OUT THE FIRE WARNING ILLUMINATED AGAIN. MAINTENANCE THEN REPLACED THE FIRE DETECTION LOOP. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950203004251995020300425GL 1995 2 3 VTZA95024 319950117A6110R333482F12 PROPELLER BAG JETSTMJETSTM3201 1500217EU ROTOL R333 R333482F12 GL LT ENGING WORN A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA27470UE 814 DRG552388 FLT 6499 - IAD-ROA - DURING CLIMB-OUT HAD SEVERE PROPELLER VIBRATION. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE THEN REPLACED THE PROPELLER ON THE LEFT ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 6 CP61GL 19950203004261995020300426EU 1995 2 3 VTZA95025 119950131A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU NR 1 ENGINE FAILURE A VTZAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27472UE 823 IAD/ISP - FLT 6300 - DURING CRUISE AT 1900 HRS ON 2-22-95, NR 1 STARTER FELL OFF LINE IN-FLIGHT AND WOULD NOT RESET. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950203004271995020300427EU 1995 2 3 VTZA95026 119950117A524014153133409 DOOR JETAIRJETSTMJETSTM4101 1500501EU LAV SERVICE MISSING A VTZAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 EA27313UE 41026 FLT NR 6547 - ROA-LYH - UPON ARRIVING AT THE HANGAR FOR NIGHT MAINTENANCE, THE LAVATORY SERVICE DOOR WAS DISCOVERED TO BE MISSING. MAINTENANCE OPENED DMI NR 40098 IAW MAL NR 52-40 ON THE LAV SERVICE DOOR. DMI WAS LATER CLEARED AT LYH 1-20-95 BY REPLACING LAV SERVICE DOOR. (Z) 2L72 4T RTA41NM 19950203004281995020300428NM 1995 2 3 VTZA95027 119950120A612078249017 PROP CNTL UNIT DHAV DHC8 DHC8102 2809003NM LT ENG FAILED A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27418AW 289 FLT 6532 - IAD-ORF - AT 1300 THE CREW SHUT THE LEFT ENGINE DOWN IN FLIGHT FOR LOW OIL PRESSURE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO RIC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT PROP CONTROL UNIT. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2H72 4T RTA13NM 19950203004291995020300429EU 1995 2 3 VTZA95029 119950131A7714AG34 TACH GENERATOR BAG JETSTMJETSTM3201 1500217EU RT ENG FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27481UE 895 FLT NR 6181 - IAD-BWI - ABORTED THE TAKEOFF, DUE TO THE RIGHT ENGINE RPM FLUCTUATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT TACH GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950203004301995020300430EU 1995 2 3 VTZA95030 119950121A6120 OIL LINE BAG JETSTMJETSTM3201 1500217EU LT ENGINE LOOSE A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27496UE 900 FLT 6180 - IAD-BGM - LEFT ENGINE OIL PRESSURE FLUX 20 PSI WITH OIL CAPTION ILLUMINATED. CREW SHUT DOWN ENGINE AND DIVERTED TO MDT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTEN OIL LINE TO PROP GOVERNOR P/N 31057165. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950203004311995020300431 1995 2 3 VTZA95031 319950121A6140310389813 BETA SWITCH JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27313UE 41026 FLT 6292 - IAD-DAY - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT BETA LIGHT ILLUMINATED ON TAKEOFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED LEFT BETA SWITCH. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950203004321995020300432EU 1995 2 3 VTZA95033 119950122A301029S7D525511 INBD DE-ICE BOOT BAG JETSTMJETSTM3201 1500217EU LT INBOARD WING FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27478UE 892 FLT 6256 - IAD-ALB - AT 1500 LEFT WING DE-ICE BOOT FAILED IN ICING CONDITIONS. AIRCRAFT DIVERTED TO SWF AND LANDED WITHOUT INCIDENT. MAINTENANACE REMOVED AND REPLACED LEFT INBOARD WING DE-ICE BOOT. OPS CHECK GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950203004351995020300435NM 1995 2 3 95ZZZX530 119950111A32601EN16RB1 SWITCH BOEING727 727228 NM RT MLG DOOR MALFUNCTIONED A DHLAA UNSCHED LANDING NE FALSE WARNING VIBRATION/BUFFET CLCLIMB 1 SO01724DH 19862 ON CLIMB AFTER MAIN LANDING GEAR RETRACTION, RED MAIN LANDING GEAR DOOR LIGHT ON FORWARD PANEL AND RIGHT DOOR UNSAFE LIGHT ON SECOND OFFICER'S PANEL WERE ON, AIRFRAME VIBRATION FELT. REPLACED RIGHT DOOR WARNING LIGHT SWITCH. MM 32-10. 2L73 4F A3WE 19950203004361995020300436WP 1995 2 3 95ZZZX531 119950110A2760 PUMP DOUG DC8 DC873 302199CWP SPOILER SYSTEM LOW A DHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01802DH 46076 SPOILER PUMP PRESSURE DROPPED TO 2450 PSI ON TAKEOFF ROLL. TAKEOFF REJECTED. SERVICED SPOILER RESERVOIR, SPOILER PUMP PRESSURE GOOD AT 3000 PSI. 2L74 4F RT4A25 19950203004371995020300437 1995 2 3 95ZZZX532 419950105A344421EN1076 SWITCH BOEING727 72722 1384002NM RT MLG DIRTY A DHLAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO01707DH 18321 CVG - AT 200 FEET AGL FINAL APPROACH, GPWS ACTIVATED WITH 'TOO LOW FLAPS' WARNING. FLAP POSITION WAS VERIFIED IN 30 DEGREE POSITION BY ALL THREE CREW MEMBERS. GO-AROUND WAS EXECUTED, NEXT APPROACH WAS UNEVENTFUL TO A NORMAL LANDING. CLEANED FLAP SWITCH. OPS CHECKS GOOD. PER MM 34-12-11. 2L73 4F A3WE 19950203004381995020300438 1995 2 3 95ZZZX533 419950110A3444 SWITCH BOEING727 72722C 138400FNM MLG DIRTY A DHLAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO01706DH 19192 AT 500 FEET ON FINAL APPROACH, GPWS WENT OFF AND SAID 'TOO LOW, GEAR'. EXECUTED GO-AROUND, ON SECOND APPROACH GPWS DID NOT GO OFF. CLEANED LANDING GEAR SWITCH. GROUND CHECKS NORMAL. PER MM 34-52-0. 2L73 4F A3WE 19950203004391995020300439NE 1995 2 3 95ZZZX534 219950116A7230 BEARING SEAL BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE FAILED A P5CAAEO UNSCHED LANDING ENGINE SHUTDOWN OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23735SJ458 19642 662581 NR 1 ENGINE OIL PRESSURE LIGHT ON MASTER CAUTION PANEL ON. FLUCTUATING OIL PRESSURE 10 TO 30 PSI AND LOSS OF OIL QUANTITY TO THREE-FOURTHS GALLON. BREATHER TEMPERATURE 230 DEGREES. ENGINE SHUT DOWN. LANDING IN MIA UNEVENTFUL. SERVICED ENGINE WITH 24 QUARTS OF OIL. PERFORMED LEAK CHECK AND RAN ENGINE AT POWER FOR FIVE MINUTES. NO LEAKS FOUND. SUSPECT CARBON SEAL FAILURE. AIRCRAFT SCHEDULED FOR THREE ENGINE FERRY FLIGHT TO JFK FOR UER NR 1. 2L74 4F4 F A20WE E20EA 19950203004431995020300443CE 1995 2 3 95ZZZX538 119950103A7110B140048 LATCH BEECH 1900 1900C 1154161CE LT UPPER COWL LOOSE A GPPAA UNSCHED LANDING O OTHER CLCLIMB 1 CE09120GP UC59 CLE - FLT 3223 - DEPARTING, HAD THE LT COWL OUTBOARD SIDE COME UNLATCHED. AIRCRAFT RETURNED TO CLE WHERE GPX MAINTENANCE INSPECTED THE COWL AND LATCH MECHANISM WITH NO DISCREPANCIES NOTED. COWL WAS SECURED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 19950203004441995020300444CE 1995 2 3 95ZZZX539 119950102A323211238992219 ACTUATOR BEECH 1900 1900C 1154161CE NLG MALFUNCTIONED A GPPAO OTHER J WARNING INDICATION APAPPROACH 1 CE0938011 UC9 DEN - FLT 2072 - FLIGHT INBOUND, WAS UNABLE TO OBTAIN A NLG DOWN AND LOCK LIGHT. GP EXPRESS MAINTENANCE CLEANED AND ADJUSTED THE DOWNLOCK SWITCH AND CYCLED THE GEAR SEVERAL TIMES WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. LATER THAT DAY, FLIGHT 2074 REPORTED THE SAME MALFUNCTION. GP EXPRESS MAINTENANCE REPLACED THE DOWNLOCK SWITCH AND CYCLES THE GEAR WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. ON 1-3-95, SAME DISCREPANCY OCCURRED INBOUND TO DEN ON FLIGHT 2078. GP EXPRESS MAINTENANCE REPLACED NLG ACTUATOR. SYSTEM GROUND CHECKED SATISFACTORY AND A/C RETURNED TO SERVICE. 2L72 4T RTA24CE 19950203004451995020300445EU 1995 2 3 95ZZZX540 119950103A2730 BOLTS SAAB SF340 340B 7860101EU ELEVATOR HINGE LOOSE A ANVEAK NONE O OTHER ININSP/MAINT 1 SO03273AE 340B273 DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR HINGE BOLTS LOOSE AND/OR NOT TORQUED PROPERLY. INSPECTORS ARE CHECKING FOR SIDE PLAY IN THE ELEVATOR BEARINGS AND FINDING THAT THE PLAY IS DUE TO LOOSE BOLTS; NOT WORN BEARINGS. THIS PROBLEM HAS BEEN FOUND ON SEVERAL AIRCRAFT PREVIOUSLY, WITH CORRECTIVE ACTION BEING RE-TORQUE OF ELEVATOR BOLT. THERE IS NOT A CURRENT SERVICE BULLETIN OR AIRWORTHINESS DIRECTIVE FOR THIS PROBLEM. 2L72 4T RTA52EU 19950203004461995020300446EU 1995 2 3 95ZZZX541 119950103A3210AIR123738 PIVOT PIN AIR8302212 SAAB SF340 SF340A 7850100EU MLG ASSY CRACKED B AAY55K NONE O OTHER ININSP/MAINT 1 SO03325PX PG561A312 340A051 DURING OVERHAUL OF MAIN LANDING GEAR ASSEMBLY, FOUND DRAG BRACE TO LANDING GEAR ATTACH PIVOT PIN CRACKED AT HEAD AROUND RADIUS OF PIN. THIS HAS BEEN NOTED ON PREVIOUS OVERHAUL OF LANDING GEAR ASSEMBLIES. THERE IS NO SERVICE BULLETIN OR AIRWORTHINESS DIRECTIVE THAT ADDRESSES THIS PROBLEM. 2L72 4T RTA52EU 19950203004491995020300449CE 1995 2 3 95ZZZX544 119950104A2910 HYD SYSTEM BEECH 99 C99 1154006CE LEFT REQUIRED SERVICEA GUUAO OTHER KP FLUID LOSS NO WARNING INDICATION NRNOT REPORTED 1 SO197209W U224 NAS/FLL - FLT 424 - PILOT REPORT: 1) HYDRAULIC FLUID LEAK LEFT SIDE. 2) LEFT MAIN GEAR DOWN LIGHT DOES NOT COME ON WITH GEAR EXTENDED. MAINTENANCE: FERRIED AIRCRAFT TO MIA. FOUND HYDRAULIC SYSTEM LOW ON FLUID, BLED HYDRAULIC SYSTEM, PERFORMED GEAR RETRACTION TESTS WITH SATISFACTORY RESULTS. AIRCRAFT RETURNED TO SERVICE. 1L72 3T A14CE 19950203004511995020300451NM 1995 2 3 95ZZZX546 119950103A5312 BULKHEAD BOEING727 727231 1384079NM RT MLG WW CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554332 20310 DURING CHECK C-2D, FOUND CRACK APPROXIMATELY TWO INCHES IN BULKHEAD BELOW APU FLOW CONTROL VALVE, IN RT MLG WHEELWELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TWA DWG C03242 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES. 2L73 4F A3WE 19950203004521995020300452NE 1995 2 3 95ZZZX547 219950113A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE LEFT FAILED A ATWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE05919TW 49368 JFK - FLT 481 - DURING CLIMB, SHUT DOWN LEFT ENGINE DUE TO LOUD BANG AND INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, SN 3218. GROUND RUN-UP AND OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 27,663 HOURS; 14,695 CYCLES. CHECK OP-16 - 8-17-94 - MCI. 2L72 4F4 F A6WE E9NE 19950203004581995020300458NE 1995 2 3 95ZZZX553 219950114A7314378200 FUEL PUMP BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE SHAFT SHEARED A AMYWACD ABORTED TAKEOFF RETURN TO BLOCK OY OTHER ENGINE STOPPAGE TOTAKEOFF 1 SO19887MA 1076 21857 UPON TAKEOFF ROLL, AT APPROXIMATELY 60 KNOTS, ENGINE NR 2 FAILED. ALL ENGINE NR 2 INDICATIONS WERE NORMAL AT TIME OF FAILURE. AOM PROCEDURES 2-E-2, 2-A-9-1, AND 2-A-6-2 WERE FOLLOWED. NR 2 ENGINE INOP, TRANSFERRED TO DMI, LOG SLIP NR 1690 IAW MEL 78-1. NR 2 T/R BLOCKED PER MM 78-30-00. INSTALLED PLACARD. GMM FORM M-14C FOLLOWED FOR FERRY FLIGHT PREPARATIONS. AT MIA, FOUND ENGINE DRIVEN FUEL PUMP FAILED. REPLACED THE FUEL PUMP AND THE FCU (AS PRECAUTIONARY). NOTE: MAINTENANCE DELAY: 2 HRS 53 MIN. 2L73 4F4 F A3WE E2EA 19950203004611995020300461CE 1995 2 3 95ZZZX556 119950106A2430 FIELD WIRE PRESTOLITE ALX9405 BEECH 36 A36 1151604CE ALTERNATOR BROKEN A AVRAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL21236CH 91000788 E502 INSPECTION OF THE AIRCRAFT'S ELECTRICAL SYSTEM FOUND A BROKEN FIELD WIRE AT THE TERMINAL END ATTACHMENT TO THE ALTERNATOR. THIS CAUSED A LOSS OF ELECTRICAL POWER AND DEAD BATTERY. PILOT PUT THE GEAR DOWN, GEAR ONLY WENT DOWN EST. 80 PERCENT, HOWEVER, LANDING WAS ATTEMPTED. THE PILOT TOOK OFF AGAIN WHEN HE HEARD A NOISE OF THE GEAR DOORS CONTACTING THE GROUND. THE A/C TOOK OFF AND RETURNED TO HOME BASE. UPON LANDING AND AT ROLL-OUT, THE RT LANDING GEAR COLLAPSED. 1L71 3O 3A15 19950203004621995020300462EU 1995 2 3 95ZZZX557 119950110A29109302631001 LINE AEROQUIP SAAB SF340 SF340A 7850100EU NOSE GEARWELL LEAKING A CHQAO OTHER JK WARNING INDICATION FLUID LOSS APAPPROACH 1 EA23128CH14777 340A128 PILOT REPORTED DURING GEAR EXTENSION, HYDRAULIC QUANTITY AND MAIN ACCUMULATOR PRESSURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE FROM THE PUMP TO THE FILTER LEAKING. THE LINE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS. 2L72 4T RTA52EU 19950203004631995020300463WP 1995 2 3 95ZZZX558 119950103A2410696233B CSD DOUG DC9 DC932 3022066WP NR 1 OVERHEAT A VJ6AA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO11904VJ 47377 ATL/TPA - FLT 531 - RETURNED TO ATL DUE TO A NR 1 CSD OVERHEAT AND THE CSD WOULD NOT DISCONNECT. REMOVED AND REPLACE NR 1 CSD. 2L72 4F A6WE 19950203004651995020300465NM 1995 2 3 95ZZZX560 119950110A5320 FRAME BOEING737 7373Y0 1384671NM BS 480 S21L CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13303AL 23499 DURING SCHEDULED INSPECTION OF MAIN CARGO DOOR LOWER SILL AREA FRAME (PEMCO AEROPLEX, INC. INSTALLATION), FOUND BS 440 AND BS 480 FRAME CRACKED AT S21L, AND BS 400 AND BS 420 REINFORCEMENT DOUBLER UNDER FRAME CRACKED AT RADIUS. REPAIRED PER ECO 3548, PART I AND II. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 21225.56 CYCLE: 24387. REF CONTROL NR TSAA953020, 95ZZZX561, AND 95ZZZX562. 2L72 4F RTA16WE 19950203004661995020300466NM 1995 2 3 95ZZZX561 119950110A5320 DOUBLER BOEING737 7373Y0 1384671NM BS 400 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13303AL 23499 DURING SCHEDULED INSPECTION OF MAIN CARGO DOOR LOWER SILL AREA FRAME (PEMCO AEROPLEX, INC. INSTALLATION), FOUND BS 440 AND BS 480 FRAME CRACKED AT S21L, AND BS 400 AND BS 420 REINFORCEMENT DOUBLER UNDER FRAME CRACKED AT RADIUS. REPAIRED PER ECO 3548, PART I AND II. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 21225.56 CYCLE: 24387. REF CONTROL NR TSAA953020, 95ZZZX560, AND 95ZZZX562. 2L72 4F RTA16WE 19950203004671995020300467NM 1995 2 3 95ZZZX562 119950110A5320 DOUBLER BOEING737 7373Y0 1384671NM BS 420 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13303AL 23499 DURING SCHEDULED INSPECTION OF MAIN CARGO DOOR LOWER SILL AREA FRAME (PEMCO AEROPLEX, INC. INSTALLATION), FOUND BS 440 AND BS 480 FRAME CRACKED AT S21L, AND BS 400 AND BS 420 REINFORCEMENT DOUBLER UNDER FRAME CRACKED AT RADIUS. REPAIRED PER ECO 3548, PART I AND II. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 21225.56 CYCLE: 24387. REF CONTROL NR TSAA953020, 95ZZZX560, AND 95ZZZX561. 2L72 4F RTA16WE 19950203004691995020300469EU 1995 2 3 AWXA9500051 119950115A3232MS172271 KEY WASHER AIRBUS320 A320231 3930325EU NLG DOOR ACT BROKEN TAB A AAWXAK NONE O OTHER ININSP/MAINT 1 WP28631AW 077 PHX - DURING FLEET INSPECTION, DUE TO OTHER FAILURES NOTED, FOUND KEY WASHER TANGS PROPERLY SECURED, BUT KEY PORTION OF LOCK WASHER DEFECTIVE ALLOWING ROTATION OF NUT ON NLG DOOR ACTUATOR LOWER ATTACHMENT FITTING BOLT. THE KEY PORTION OF THE LOCK WASHER IS NOT VISIBLE WITHOUT REMOVING THE NUT. REMOVED AND REPLACED LOCK WASHER PER AMM 32 32 16 PP 404 407. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950203004701995020300470EU 1995 2 3 AWXA9500052 119950115A3232MS172271 KEY WASHER AIRBUS320 A320231 3930325EU NLG DOOR ACT BROKEN TAB A AAWXAK NONE O OTHER ININSP/MAINT 1 WP28637AW 099 PHX - DURING FLEET INSPECTION, DUE TO OTHER FAILURES NOTED, FOUND KEY WASHER TANGS PROPERLY SECURED, BUT KEY PORTION OF LOCK WASHER DEFECTIVE ALLOWING ROTATION OF NUT ON NOSE LANDING GEAR DOOR ACTUATOR LOWER ATTACHMENT FITTING BOLT. THE KEY PORTION OF THE LOCK WASHER IS NOT VISIBLE WITHOUT REMOVING THE NUT. REMOVED AND REPLACED LOCK WASHER PER AMM 32 32 16 PP 404 407. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950203004711995020300471EU 1995 2 3 AWXA9500053 119950115A3232MS172271 KEY WASHER AIRBUS320 A320231 3930325EU NLG DOOR ACT BROKEN TAB A AAWXAK NONE O OTHER ININSP/MAINT 1 WP28624AW 55 PHX - DURING FLEET INSPECTION DUE TO OTHER FAILURES NOTED, FOUND KEY WASHER TANGS PROPERLY SECURED, BUT KEY PORTION OF LOCK WASHER DEFECTIVE ALLOWING ROTATION OF NUT ON NOSE LANDING GEAR DOOR ACTUATOR LOWER ATTACHMENT FITTING BOLT. THE KEY PORTION OF THE LOCK WASHER IS NOT VISIBLE WITHOUT REMOVING THE NUT. REMOVED AND REPLACED LOCK WASHER PER AMM 32 32 16 PP 404 407. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950203004721995020300472SO 1995 2 3 C2XA95CL004 119950116A323012038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916702608 120160 120078 CORRECTED SDR. DTW\CLE - FLT 3142 - ON CLIMB-OUT, SELECTED GEAR RETRACTION. SIX GREEN LIGHTS REMAIN ILLUMINATED ALONG WITH FIVE RED GEAR LIGHTS. LEFT 'B' RED GEAR LIGHT ONLY ONE NOT ILLUMINATED. GEAR DID NOT MOVE. MAINTENANCE SWAPPED LEFT GEAR 'A' AND 'B' UPLOCK CANNON PLUGS IAW SL 120-032-0015 AND PLACED 'B' INDICATION ON MEL 32-60-1, CONTROL NR 769898. ON 1-17-95, MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL BOX. OPS CHECK GOOD. REMOVED FROM MEL. (X) 2L72 4T RTA31SO 19950203004731995020300473SO 1995 2 3 C2XA95IA003 119950118A5320 OMEGA BEAM EMB 120 EMB120RT SO FWD CENTER CABINCORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 DURING C-CHECK INSPECTION, FOUND CORROSION ON AIRCRAFT CENTERLINE FLOOR SUPPORT OMEGA BEAM, BETWEEN FRAMES NR 14 AND NR 15. MAINTENANCE REPAIRED OMEGA BEAM BY INSTALLING A REINFORCEMENT DOUBLER, AND REMOVED ALL OTHER CORROSION BETWEEN FRAMES NR 14 AND NR 15. REPAIR ACCOMPLISHED PER ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01043 TT - 10984.6T. T CYL - 15473. (X) 2L72 4T RTA31SO 19950203004741995020300474NE 1995 2 3 EIAA9502 219950130A7261510393 CARBON SEAL DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 1 ENG LEAKING A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM09817EV 46022 671363 MZJ - ACCOMPLISHED PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY. OIL PRESSURE REMAINED AT 32 PSI INITIALLY THE FLUCTUATED 15-30 PSI. OIL QUANTITY WAS AT 1.75 GALLONS WHEN ENGINE SHUTDOWN. PRESSURE AND TEMPERATURES NORMAL. OIL QUANTITY CONTINUED TO DECREASE TO 0.0 INDICATION. TOTAL WINDMILL TIME, 4 HOURS 30 MINUTES. REMOVED AND REPLACED NR 1 ENGINE INLET CASE AND NR 1 BEARING CARBON SEAL PER ECRA 671363-72-005-1 REV A. LEAK CHECK GOOD AND ENGINE RUN WORK ACCOMPLISHED ON EAC WO NR 70-1415-04-0001 AND 70-1416-03-0001. RII ACCOMPLISHED. (M) 2L74 4F4 F 4A25 1E8 19950203004781995020300478WP 1995 2 3 ORJA95001 119950131A2131 CONTROLLERS DOUG DC9 DC982 3022082WP NR 1/2 MALFUNCTIONED A ORJAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP11822RA 49932 AT 26,000 FEET, NOTED CABIN ALTITUDE INCREASING, WHILE STILL CLIMBING TO ASSIGNED ALTITUDE. AIRCRAFT LEVELED AND DESCENT REQUESTED. RED CABIN LIGHT CAME ON AT 11M. CABIN ALTITUDE PRESSURE CONTROLLERS SWITCH, CABIN ALTITUDE KEPT INCREASING AND OXYGEN MASK DEPLOYED. AIRCRAFT WAS DESCENDED TO 11M. FLIGHT ATTENDANT REPORTED FUMES AND HAZE IN CABIN. REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE CONTROLLERS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19950203004791995020300479NM 1995 2 3 P2EA95002 119950105A2130 PRESSURIZATION BOEING737 737222 1384473NM CABIN MALFUNCTIONED A P2EAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE05208AU 19547 SLC - FLT 202 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF (AUTO, STANDBY, OR MANUAL). COULD NOT CONTROL OUTFLOW VALVE. RETURNED FOR LANDING AT DEN WITHOUT INCIDENT. PERFORMED SYSTEM TEST PER MM 21-31-0A. RAN ENGINES AND PRESSURIZED AIRCRAFT. OPERATION CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950203004801995020300480EU 1995 2 3 RAIA950103 119950102A3350311701 BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN EEL LOW VOLTS A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423AM3452 1262 858 STL - EMERGENCY LIGHTING IS INOPERATIVE. MAINTENANCE REPLACED EMRGENCY LIGHTING BATTERY. (X) 2L72 4T RTA56EU 19950203004811995020300481EU 1995 2 3 RAIA950108 119950108A21311379284L403 VALVE BAG JETSTMJETSTM3201 1500217EU LT NACELLE OUT OF ADJUST A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03423AM8832 858 STL - FLT 7420 - MANUAL PRESSURIZATION INOPERATIVE. MAINTENANCE RESECURED LEFT FLOW CONTROL VALVE. GROUND PRESSURIZATION CHECK NORMAL. (X) 2L72 4T RTA56EU 19950203004821995020300482EU 1995 2 3 RAIA950115 119950116A2710137320E408 CONTROL CABLE BAG JETSTMJETSTM3201 1500217EU AILERONS LOOSE A RAIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 CE03428AM8544 877 STL - ON APPROACH, WHEN FLAP SETTING IS SELECTED, AIRCRAFT ROLLS TO THE RIGHT. UPON INSPECTION, MAINTENANCE DISCOVERED AILERON CONTROL CABLE TENSION TO BE LOW. ADJUSTED CABLE TENSION PER J32 MM 271000. (X) 2L72 4T RTA56EU 19950203004831995020300483EU 1995 2 3 RAIA950116 119950116A2121 FAN AEROSPATR42 ATR42300 8680920EU GROUND COOL SMOKE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03423TE 119 STL - LEFT PACK EMITS SMOKE ON GROUND. MAINTENANCE DEFERRED LEFT GROUND COOLING FAN PER MEL 21513. (X) 2H72 4T RTA53EU 19950203004841995020300484 1995 2 3 RAIA950117 419950117A34257001676903 MODE SELECTOR BAG JETSTMJETSTM3201 1500217EU COCKPIT BURNED LIGHT A RAIAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03864AE8277 864 LAX - FLT 4750 - SMOKE BEING EMITTED FROM BEHIND THE CAPTION PANEL. MAINTENANCE REPLACED FLIGHT DIRECTOR MODE SELECTOR UNIT WHICH INDICATED BURNED LIGHTING. TEST OF SYSTEM REVEALED NORMAL, NO SMOKE NOTICED. (X) 2L72 4T RTA56EU 19950203004851995020300485SO 1995 2 3 RAIA950118 119950117A30103D237606 EJECTOR VALVE EMB 120 EMB120RT SO LT AFT FAULTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03126AM8366 120102 ALO - FLT 7455 - BOTH OUTBOARD HORIZONTAL AND VERTICAL STABILIZER DE-ICE BOOTS FAILED. MAINTENANCE REPLACED DE-ICE EJECTOR VALVE FOR HORIZONTAL AND VERTICAL STABILIZER DE-ICE BOOT, GROUND CHECK OKAY. (X)` 2L72 4T RTA31SO 19950203004861995020300486EU 1995 2 3 RAIA950121 119950116A33503012001 BATTERY PACK AEROSPATR72 ATR72202 8680940EU CABIN EEL LOW VOLTS A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE5899 789 283 STL - EMERGENCY LIGHTING IS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACK. (X) 2H72 4T RTA53EU 19950203004871995020300487NM 1995 2 3 TSAA953020 119950110A5320 FRAME BOEING737 7373Y0 1384671NM BS 440 S21L CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13303AL 23499 DURING SCHEDULED INSPECTION OF MAIN CARGO DOOR LOWER SILL AREA FRAME (PEMCO AEROPLEX, INC. INSTALLATION), FOUND BS 440 AND BS 480 FRAME CRACKED AT S21L, AND BS 400 AND BS 420 REINFORCEMENT DOUBLER UNDER FRAME CRACKED AT RADIUS. REPAIRED PER ECO 3548, PART I AND II. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 21225.56 CYCLE: 24387. REF CONTROL NR 95ZZZX560, 95ZZZX561, AND 95ZZZX562. (X) 2L72 4F RTA16WE 19950203004881995020300488EU 1995 2 3 UF6A950108 119950112A2611CG7PT2 SMOKE DETECTOR BAG ATP ATP EU AFT BAGGAGE DIRTY A UF6AO OTHER N FALSE WARNING CRCRUISE 1 CE03855AW7150 1388 490 2029 ORD - FLT 5018 - FALSE SMOKE WARNING FROM AFT BAGGAGE COMPARTMENT. MAINTENANCE CLEANED CANNON PLUG ON AFT BAGGAGE COMPARTMENT SMOKE DETECTOR. A/C TT 6999. (X) 2L72 4T RTA27NM 19950203004891995020300489EU 1995 2 3 UF6A950109 119950114A331010620BAC6 SWITCH BAG ATP ATP EU COCKPIT FAILED A UF6AK NONE O OTHER ININSP/MAINT 1 CE03851AW8351 2020 ORD - FLT 5007 - EMERGENCY LIGHT SWITCH STICKING IN COCKPIT. MAINTENANCE REPLACED EMERGENCY LIGHT CAP. (X) 2L72 4T RTA27NM 19950203004901995020300490EU 1995 2 3 UF6A950110 119950115A33506013211 POWER SUPPLY BAG ATP ATP EU AFT PAX CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03851AW6040 177 16395 2020 AZO - FLT 5002 - ONE SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 6 POWER SUPPLY. (X) 2L72 4T RTA27NM 19950203004911995020300491NE 1995 2 3 WTAA950029 219950109A7310 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE WARNING LIGHT A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17122AM 120013 LEFT ENGINE FUEL FILTER LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. REMOVED AND REPLACED LEFT ENGINE LOW AND HIGH PRESSURE FUEL FILTERS FOR PRECAUTIONARY PURPOSES. INSPECTED, REMOVED FILTERS. NO CONTAMINATION OR DEFECTS NOTED. SYSTEM OPERATIONAL AND LEAK CHECKED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950203004921995020300492SW 1995 2 3 QXEA9500031 119950201A32332751016003 ACTUATOR SWRNGNSA227 SA227AC 8780603SW LT MLG MALFUNCTIONED A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09382PH2320023200 AC589 PDX - LEFT WING FAILED TO INDICATE DOWN AND LOCKED CREW CYCLED GEAR 3 TIMES AND AFTER 4 MINUTES GEAR INDICATED DOWN. FLIGHT LANDED WITHOUT INCIDENT REPLACED LT, INBD GEAR ACTUATOR. REPLACED WORN BELLCRANK AND BUSHINGS AS PRECAUTION. GROUND TESTED AND RETURNED AIRCRAFT TO SERVICE. 2L72 4T RTA8SW 19950203004971995020300497SO 1995 2 3 RAAAE994036 119950131A3350821015 BATTERY PACK 8631003 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 FORWARD PASSENGER COMPARMTENT EGRESS TRANSMITTER FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19950203005221995020300522EU 1995 2 3 REXA95001 119950103A2121C209690C RECIRC FAN SAAB SF340 SF340A 7850100EU CABIN FAILED A REXAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO04321PX547 87 340A031 STRANGE ODOR IN CABIN, DISCOVERED FUEL IN LEFT WHEEL WELL, MAY BE RELATED. FLUID IN LEFT WHEEL WELL IS A MIX OF OIL AND WATER, MOSTLY WATER. SMELL APPEARS TO BE ELECTRICAL, PULLED FLOOR BOARD AND DETERMINED LEFT RECIRC TO BE THE CAUSE OF THE PROBELM. LEFT RECIRC FAN DEFERRED PER MEL 21-20-01 CAT C. CLEARED DEFER BY REMOVING AND REPLACING LEFT RECIRC FAN. OPS CHECKS GOOD. (W) 2L72 4T RTA52EU 19950203005261995020300526NM 1995 2 3 USAA950010 119950110A2410739515B IDG BOEING767 767201 1385125NM RIGHT LEAKING A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19650US 23902 PIT - FLT 816 - RETURNED TO FIELD DUE TO E/M 'GEN OFF'. ALSO, THE GENERATOR OFF LIGHT ILLUMINATED. MAINTENANCE REPLACED THE RT IDG. OPERATIONS AND LEAK CHECKED GOOD. (W) 2L72 4F RTA1NM 19950203005281995020300528SO 1995 2 3 WTAA950036 119950109A2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A WTAAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 WP17455UE 120163 SFO - NACELLE FLAP ASYMMETRY REPORTED ON GROUND. MAINTENANCE RESET AND INSPECTED FLAP SYSTEM, COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203005291995020300529SO 1995 2 3 WTAA950038A 119950110A323012038594001 CONTROL MODULE EMB 120 EMB120RT SO LANDING GEAR FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP17451UE 120108 SFO - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. REPLACED LANDING GEAR CONTROL MODULE AND RELAY BOX. LANDING RETRACTION AND EXTENSION NORMAL DURING GROUND TEST AND SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950203005301995020300530EU 1995 2 3 WTAA950041 119950110A77123107466 TQ COND SIG BAG JETSTMJETSTM3101 1500215EU RT ENGINE MALFUNCTIONED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17428UE 806 FAT - DURING CLIMB-OUT THROUGH 8,000 FEET, LEFT ENGINE TORQUE INDICATION WENT TO 104.5 PERCENT. TORQUE INDICATION REMAINED AT APPROXIMATELY 104.5 PERCENT AFTER POWER LEVER WAS RETARDED. ALL OTHER ENGINE PARAMETERS REPORTED NORMAL. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED ELECTRICAL CONNECTORS AT TORQUE SIGNAL CONDITIONER UNIT AND TORQUE RING. SWAPPED TO J2 BRIDGE. PROBELM CONTINUED. REPLACED LEFT ENGINE TORQUE SIGNAL CONDITIONER UNIT AND RETURNED TO BRIDGE J1. TORQUE INDICATIONS NORMAL DURING ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950203005311995020300531EU 1995 2 3 WTAA950043 119950113A5210JE5 ACTUATOR BAG JETSTMJETSTM3101 1500215EU PASSENGER DOOR OUT OF ADJUST A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17107XV 723 LAX - PASSENGER DOOR CAPTION REMAINS ILLUMINATED WITH DOOR CLOSED AND SHOOT BOLTS ENGAGED. DEFERRED DOOR WARNING SYSTEM PER MEL 52-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENLTY CLEARED DEFERRAL WITH THE ADJUSTMENT OF THE PASSENGER DOOR WARNING ACTUATOR. (M) 2L72 4T RTA21EU 19950203005321995020300532NM 1995 2 3 95FDEA00105 119950131A2910NAS1611119 O-RING DOUG MD11 MD11F 3023600NM NR 1 HYD SYST FAILED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO04614FE 48528 HYD NR 1 OFF ALERT AFTER 50 MINUTES OF FLIGHT AT FLT LEVEL 320. QUANTITY FELL TO 2.8, PRESS DROPPED TO 40 PSI, NR 2, NR 3 NORMAL. HYD TEMP NR 1 - 48C TEMP ROSE TO 92C, THEN CAME BACK DOWN. FOUND HYD LEAK FROM LINE FITTING ON FILTER HEAD TO NR 1L HYD PUMP PRESS LINE. REMOVED AND REPLACED PACKING AT PRESS FITTING. CHANGED ALL FOUR FILTER ELEMENTS PRECAUTIONARY. NO CONTAMINATION FOUND. SERVICED NR 2 HYD SYS. ENGINE RUN OK. HYD TEMP WITHIN LIMITS PER MM 29-10-00. 2L73 4F RTA22WE 19950203005331995020300533NM 1995 2 3 95FDEA00106 119950202A2910 HYD SYST DOUG MD11 MD11F 3023600NM NR 3 HYD SYST REQD SERVICE A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO04605FE 48514 TPE - LOST NR 3 HYDRO SYSTEM, FLUID QUANTITY WENT DOWN TO 2.8. SERVICED NR 3 HYDRO SYSTEM TO 8.5 GALLONS. TROUBLESHOT AND RAN ENGINES. NO LEAK NOTED. (SUSPECT AIR BLEED VALVE PLUNGER MAY HAVE STUCK OPEN.) EXCERISED PLUNGER AND OPS. CHECK NORMAL. 2L73 4F RTA22WE 19950203005341995020300534WP 1995 2 3 ABXA9500064 119950130A32607000010101 DN LOCK SW DOUG DC9 DC933F 302207AWP LT MLG CORROSION A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23930AX 47363 LEFT MAIN LANDING GEAR DOWN INDICATOR DID NOT ILLUMINATE ON INITIAL GEAR EXTENSION. CYCLED LANDING GEAR AND LIGHT ILLUMINATED. FOUND CORROSION IN THE LEFT GEAR DOWNLOCK SWITCH AND MOISTURE IN THE CANNON PLUG. CLEANED CORROSION FROM SWITCH AND REMOVED MOISTURE FROM THE CANNON PLUG. OPS CHECKED GOOD DURING GEAR SWING IAW DC-9 SUPPLEMENTAL M.M. 32-60-00. 2L72 4F A6WE 19950203005351995020300535WP 1995 2 3 ABXA9500066 119950201A323059104475041 RETRACT MECH DOUG DC9 DC941 302207NWP NLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23970AX 798 47494 NOSE WHEEL LANDING GEAR WOULD NOT EXTEND ON FIRST ATTEMPT, RECYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY. PERFORMED LANDING GEAR SWING IAW DC-9 M.M. 32-20-0. COULD NOT DUPLICATE MALFUNCTION. GEAR OPS CHECKED GOOD. LUBED NOSE GEAR. INSPECTED RETURN SPRING, NOSE GEAR LINKAGE, CABLES, UPLOCK RELEASE MECHANISM. NO DEFECTS NOTED. INSPECTED NOSE BUNGEE CYLINDER AND MAIN NOSE GEAR ACTUATOR. NO LEAKS OR DEFECTS NOTED. INSPECTED ALL OF NOSE GEAR WELL. NO DEFECTS NOTED. 2L72 4F A6WE 19950203005361995020300536SO 1995 2 3 COM11755 119950130A325078SF2B502 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING DEFECTIVE A ACOMAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO01137H 120137 COPILOTS NWS IS INOP. AIRCRAFT VEERS HARD LEFT. REPLACED THE NWS FEEDBACK POTENTIOMETER. 2L72 4T RTA31SO 19950203005371995020300537SO 1995 2 3 COM11756 119950201A7330725825 FILTER LIGHT EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE ILLUMINATED A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01258CA 120247 115374 RIGHT ENGINE FUEL FILTER WARNING LIGHTS ILLUMINATED DURING TAKEOFF. INSPECTED FILTER AND FOUND TO BE SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. COULD NOT DUPLICATE. 2L72 4T4 TRTA31SO E20NE 19950203005381995020300538SO 1995 2 3 COM11757 119950201A3030MS2740127 AOA HEAT RELAY EMB 120 EMB120RT SO LEFT DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01259CA 120252 LEFT A.O.A. VANE HEAT INOP WARNING ACTIVATED. REPLACED RELAY KO187, SYSTEM CHECK NORMAL. 2L72 4T RTA31SO 19950203005391995020300539SO 1995 2 3 COM11758 119950126A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01254CA9552 9552 120233 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT RIBS NR 15 AND NR 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN E.O. 1327-2. P/N: 120-17056-007, 3 EA; 120-17056-015, 4 EA; 120-17056-013, 1 EA; 120-17056-011, 1 EA; 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-17057-005, 1 EA. 2L72 4T RTA31SO 19950203005401995020300540SO 1995 2 3 COM11759 119950129A5720 SUPPORTS EMB 120 EMB120RT SO RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01258CA8512 8512 120247 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT WING RIBS 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-17056-015, 2 EA; 120-17057-006, 1 EA. 2L72 4T RTA31SO 19950203005411995020300541SW 1995 2 3 COM20353 119950131A32302752019001 UPLOCK ASSY SWRNGNSA227 SA227AC 8780603SW NLG LACK OF LUBE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01704C AC704 NLG INTRANSIT INDICATOR REMAINED ON AFTER GEAR RETRACTION. CLEANED AND LUBRICATED NLG UPLOCK ASSY. 1L72 4T A8SW 19950203005421995020300542EU 1995 2 3 COM31026 119950130A76005308211 QUADRANT SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A COMAK NONE O OTHER ININSP/MAINT 1 SO01341CA191061676 340A021 FRICTION LOCK ON CONTROLS QUADRANT IS NOT WORKING. REPLACED QUADRANT. 2L72 4T RTA52EU 19950203005431995020300543EA 1995 2 3 COM60401 119950130A2150 ACM CNDAIRCL600 CL6002B19 EA LEFT INOP A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01927CA 7031 RIGHT AIR CONDITIONING PACK HIGH PRESSURE CAUTION MESSAGE ON EICAS. FOUND NO FAULTS WITH ACM SYSTEM. HIGH PRESSURE CAUTION IS DUE TO LT ACM BEING INOP. 2L72 4F RTA21EA 19950203005441995020300544EA 1995 2 3 COM60402 119950131A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 2 DEFECTIVE A COMAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 SO01932CA3384 653 7038 SPOILER ON FAULT MESSAGE ON EICAS. REPLACED THE NR 2 SECU. 2L72 4F RTA21EA 19950203005451995020300545EA 1995 2 3 COM60403 119950131A2751855D1005 SENSOR CNDAIRCL600 CL6002B19 EA LT TE FLAP FAILED A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01931CA2297 7037 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE LT FLAP BRAKE AND POSITION SENSOR. 2L72 4F RTA21EA 19950203005461995020300546NM 1995 2 3 DL72P950447 119950118A533065545906 SKIN BOEING727 727225 1384077NM FS 680 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO118889Z 21858 DURING INSPECTION, THE FUSELAGE SKIN AT F.S. 680-686 WAS FOUND CORRODED AT STR. 28L AND WAS CUT OUT. A PRE-EXISTING REPAIR DOUBLER SPANNING THE AREA FROM F.S. 688-720A AND STR. 28L-28R WAS REMOVED AND EXTENDED TO INCLUDE THE NEW CUTOUT NOTED ABOVE. BOTH OF THESE REPAIRS WERE REPAIRED IN ACCORDANCE WITH THE SRM SKIN SPLICE FROM B727 SRM 53-30-3, FIG. 12. 2L73 4F A3WE 19950203005471995020300547NM 1995 2 3 DL72S950446 119950120A5310 TORQUE BOX BOEING727 727232 1384082NM FS 1253-1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11531DA 21814 DURING LETTER CHECK INSPECTION, THE UPPER CHORD AT RBL 20 RUNNING FORE/AFT IN THE AFT VENTRAL STAIRWAY TORQUE BOX WAS FOUND CRACKED AT STA. 1273. IN ORDER TO GAIN ACCESS FOR REPAIR OF THE CHORD, THE I/B WEB WAS CUT BETWEEN STA 1253 AND STA 1273. BOTH THE WEB AND THE CHORD WERE REPAIRED PER THE S/B 727-53-0129 REV.4. 2L73 4F A3WE 19950203005481995020300548NM 1995 2 3 DLM11950453 119950129A2120 AIR DISTR DOUG MD11 MD11 3023602NM CABIN ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11811DE 48566 DURING APPROACH, CABIN CREW REPORTED ELECTRICAL BURNING SMELL AND A LIGHT HAZE IN BUSINESS AND COACH CABINS. LANDED PDX CHECKED GALLEY EQUIPMENT OPERATION, LIGHT AND ENTERTAINMENT SYSTEM, COULD NOT DUPLICATE RETURNED TO SERVICE. 2L73 4F RTA22WE 19950203005491995020300549NM 1995 2 3 DLM88950452 119950130A30101173T0369 THERMAL SWITCH DOUG MD88 MD88 3023688NM TAIL COMP FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11910DL 49541 DURING APPROACH, HAD FUMES AND OR HOT SMELL IN CABIN AND COCKPIT WITH AIR FOIL ANTI-ICE SELECTED, SMELL GOT STRONGER WITH TAIL DE-ICE ON. LAVATORY SMOKE DETECTORS ACTIVATED. LANDED ATL. REPLACED TEMPERATURE SENSOR RAN ENGINES AND PACKS WITH ANTI-ICE ON OPERATION NORMAL. 2L72 4F RTA6WE 19950203005501995020300550WP 1995 2 3 MWEA95120 119950131A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31203ME 47673 PILOT REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED SLIDE COVER AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950203005511995020300551WP 1995 2 3 MWEA95121 119950131A25603952273501 GIRT BAR LATCH DOUG DC9 DC932 3022066WP GALLEY DOOR DIRTY A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31203ME 47673 PILOT REPORTS GIRT BAR ON GALLEY SERVICE DOOR SLIDE HARD TO OPERATE. CLEANED AND LUBED GIRT BAR RELEASE. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950203005521995020300552NM 1995 2 3 UPS202131 119950201A3260S96 UPLOCK SWITCH BOEING727 72762C 138402CNM NLG INOPERATIVE A IPXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01913UP 19245 PILOT REPORTED FORWARD PANEL NOSE GEAR RED LIGHT INOP WHEN GEAR RAISED AND LOWERED WITH EXCEPTION OF SLIGHT FLICKER, LIGHT CHECKS OK AND ILLUMINATES WHEN POWER LEVERS RETARDED IN FLIGHT. REPLACED NOSE GEAR LOCK SWITCH. TEST GOOD. 2L73 4F A3WE 19950203005531995020300553NM 1995 2 3 UPS202134 119950202A5322 SHEAR TIE BOEING727 727173C 1384059NM BS 1130 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SHEAR TIE AT BS 1130, WL 186, STRINGERS 19R AND 20R. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-02, 53-10-2. 2L73 4F A3WE 19950203005541995020300554NM 1995 2 3 UPS202135 119950202A5750 SUPPORT BOEING727 727173C 1384059NM TE MID FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON RT WING MID FLAP O/B FLAP CARRIAGE BEARING SUPPORT. INSTALLED REPAIR IAW MM 27-51-13. 2L73 4F A3WE 19950203005551995020300555NM 1995 2 3 UPS202136 119950202A5330 SKIN BOEING727 727173C 1384059NM FS 110 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON SKIN AT STR 4L STA 110. INSTALLED REPAIR IAW SRM 53-30-2, 53-30-1, 53-30-3. 2L73 4F A3WE 19950203005561995020300556NM 1995 2 3 UPS202137 119950202A5320 CLIP BOEING727 727173C 1384059NM BS 1166 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER CLIP AT BS 1166 STRINGER 18R. INSTALLED REPAIR IAW SRM 53-10-3, 51-10-02, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005571995020300557NM 1995 2 3 UPS202138 119950202A5330 SKIN LAP BOEING727 727173C 1384059NM BS 683-685 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INNER SKIN LAP BS 683-685 STRINGER 4 RT. INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F A3WE 19950203005581995020300558NM 1995 2 3 UPS202139 119950202A575465173194 RIB BOEING727 727173C 1384059NM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT FIRST RIB ON O/B END CRACKED. INSTALLED REPAIR IAW 51-10-1 AND DWG 65-16223. 2L73 4F A3WE 19950203005591995020300559NM 1995 2 3 UPS202140 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT NR 4 SLAT I/B END RIB CRACKED IN FWD RADIUS. INSTALLED REPAIR IAW SRM 51-30-02 AND OHM 57-51-61. 2L73 4F A3WE 19950203005601995020300560NM 1995 2 3 UPS202141 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT, 7TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01. 2L73 4F A3WE 19950203005611995020300561NM 1995 2 3 UPS202142 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 4 SLAT, 6TH RIB FROM O/B END (JUST I/B OF O/B TRACK) IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01. 2L73 4F A3WE 19950203005621995020300562NM 1995 2 3 UPS202143 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B END RIB IS CRACKED. INSTALLED REPAIR IAW SRM 51-10-1. 2L73 4F A3WE 19950203005631995020300563NM 1995 2 3 UPS202144 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 13TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3. 2L73 4F A3WE 19950203005641995020300564NM 1995 2 3 UPS202145 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 14TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3. 2L73 4F A3WE 19950203005651995020300565NM 1995 2 3 UPS202146 119950202A575465162211 SKIN BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND TAI SKIN CRACKED 1 INCH O/B OF O/B TRACK TO SLAT ATTACH POINT. INSTALLED REPAIR IAW EO 727-57-1080. 2L73 4F A3WE 19950203005661995020300566NM 1995 2 3 UPS202147 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 4TH FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3. 2L73 4F A3WE 19950203005671995020300567NM 1995 2 3 UPS202148 119950202A571265162232 RIB BOEING727 727173C 1384059NM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND I/B TRACK O/B RIB FLANGE CRACKED. INSTALLED REPAIR IAW EO727-57-1078. 2L73 4F A3WE 19950203005681995020300568NM 1995 2 3 UPS202149 119950202A575465162242 RIB BOEING727 727173C 1384059NM NR 8 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 1ST RIB FROM I/B IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2 AND DWG 65-16224. 2L73 4F A3WE 19950203005691995020300569NM 1995 2 3 UPS202150 119950202A575465162211 PANEL BOEING727 727173C 1384059NM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT COVE PANEL CRACKED AT O/B UP STOP. INSTALLED REPAIR IAW SRM 51-20-1 AND 51-30-02. 2L73 4F A3WE 19950203005701995020300570NM 1995 2 3 UPS202151 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT RT (I/B) ACTUATOR RIB CRACKED BETWEEN FLANGES COMMON TO SPAR AND UPPER SKIN. INSTALLED REPAIR IAW EO 727-57-1077. 2L73 4F A3WE 19950203005711995020300571NM 1995 2 3 UPS202152 119950202A575465162211 RIB BOEING727 727173C 1384059NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B RIB AT I/B TRACK IS CRACKED AT FLANGE COMMON TO COVE PANELS AND IS NOT CONTAINED BY PREVIOUS REPAIR. INSTALLED REPAIR IAW BSRM 57-50-3. 2L73 4F A3WE 19950203005721995020300572NM 1995 2 3 UPS202153 119950202A575465162241 ANGLES BOEING727 727173C 1384059NM NR 1 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 1 SLAT I/B AND O/B TRACK TO SKIN ANGLES ARE CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND IPC 57-50-1. 2L73 4F A3WE 19950203005731995020300573NM 1995 2 3 UPS202154 119950202A575465162222 RIB BOEING727 727173C 1384059NM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 13TH FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9. 2L73 4F A3WE 19950203005741995020300574NM 1995 2 3 UPS202155 119950202A575465162222 RIB BOEING727 727173C 1384059NM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 12TH FROM I/B END IS CORRODED. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-10-6 AND DWG 65-17296. 2L73 4F A3WE 19950203005751995020300575NM 1995 2 3 UPS202156 119950202A575465162232 RIB BOEING727 727173C 1384059NM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT 12TH RIB FROM I/B IS CRACKED COMMON TO LWR CHORD. INSTALLED REPAIR IAW SRM 57-50-3, PAGE 26, FIGURE 9. 2L73 4F A3WE 19950203005761995020300576NM 1995 2 3 UPS202157 119950202A5320 STIFFENER BOEING727 727173C 1384059NM BS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STIFFENER WL 182 LBL 14 TO LBL 10 BS 344. INSTALLED REPAIR IAW SRM 51-10-6 AND 51-30-2. 2L73 4F A3WE 19950203005771995020300577NM 1995 2 3 UPS202158 119950202A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM WEB, DOUBLER AND BONDED DOUBLER BS 344, WL 208, RBL 11 TO 27. INSTALLED REPAIR IAW SRM 51-40-2 AND EO 727-53-1463. 2L73 4F A3WE 19950203005781995020300578NM 1995 2 3 UPS202159 119950201A33507762 EEL BOEING727 727247 138408FNM EXIT DOOR INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01210UP 21699 MAINTENANCE REPORTED EXIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY. 2L73 4F A3WE 19950203005791995020300579NM 1995 2 3 UPS202160 119950202A5320 WEB BOEING727 727173C 1384059NM BS 1226 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1226 WL 188 LBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 53-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005801995020300580NM 1995 2 3 UPS202161 119950202A5320 WEB BOEING727 727173C 1384059NM BS 1290 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1290 LBL 21 WL 180. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005811995020300581NM 1995 2 3 UPS202162 119950202A5320 WEB BOEING727 727173C 1384059NM BS 1226 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1226 WL 188 RBL 21. INSTALLED REPAIR IAW SRM 51-20-2, 51-20-4, 51-30-2, 51-40-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005821995020300582NM 1995 2 3 UPS202163 119950202A5320 WEB BOEING727 727173C 1384059NM BS 1256 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN WEB AT BS 1256 WL 192 RBL 21. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-30-2, 51-40-2, 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005831995020300583NM 1995 2 3 UPS202164 119950202A5754 FLAP BOEING727 727173C 1384059NM NR 6 K FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 K FLAP CORRODED ON VERY INBD SIDE AT FASTENERS FOR END BULB SEAL. INSTALLED REPAIR IAW UPS EO B727-5740-3980. 2L73 4F A3WE 19950203005841995020300584NM 1995 2 3 UPS202165 119950202A5320 WEB BOEING727 727173C 1384059NM FS 251.6 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD AND AFT SIDE OF WEB STA 251.6 LBL 42 WL 218. INSTALLED REPAIR IAW SRM 53-10-2, 51-40-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005851995020300585NM 1995 2 3 UPS202166 119950202A523069241141 ANGLE BOEING727 727173C 1384059NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND MAIN CARGO DOOR HAS CRACKED L ANGLE AT BS 540 STR 4. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950203005861995020300586NM 1995 2 3 UPS202167 119950202A5230 TRANSVERSE BEAM BOEING727 727173C 1384059NM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 2 TRANSVERSE BEAM. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950203005871995020300587NM 1995 2 3 UPS202168 119950202A5313BAC1498147 STRINGER BOEING727 727173C 1384059NM FS 835 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER 16 RT AT STA 835. INSTALLED REPAIR IAW SRM 51-10-2, 51-30-2, 51-20-4 AND MM 51-20-151. 2L73 4F A3WE 19950203005881995020300588NM 1995 2 3 UPS202169 119950202A5315BAC1505101167 FLOOR BEAM BOEING727 727173C 1384059NM FS 480 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AND SEVERAL AREAS OF BARE METAL ON UPPER CHORD OF FLOOR BEAM AT BS 480 WL 208 FROM RBL 0-60. INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F A3WE 19950203005891995020300589NM 1995 2 3 UPS202170 119950202A5313 STRINGER BOEING727 727173C 1384059NM FS 1020 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER NR 2L ON UPPER FLANGE AT BS 1020. INSTALLED REPAIR IAW SRM 53-10-3. 2L73 4F A3WE 19950203005901995020300590NM 1995 2 3 UPS202171 119950202A5313 STRINGER BOEING727 727173C 1384059NM FS 540-560 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER NR 8R BS 540-560. INSTALLED REPAIR IAW SRM 53-10-1. 2L73 4F A3WE 19950203005911995020300591NM 1995 2 3 UPS202172 119950202A5511 SPAR CHORD BOEING727 727173C 1384059NM RT HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON RIGHT HAND STAB. LOWER REAR SPAR CHORD AT STAB. STA 212-223 AND STA 172-169. 2L73 4F A3WE 19950203005921995020300592NM 1995 2 3 UPS202173 119950202A575369807731 RIB BOEING727 727173C 1384059NM LT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP HAS CRACKED RIB IN T/E COVE 52 INCHES IN FROM INBOARD SIDE. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950203005931995020300593NM 1995 2 3 UPS202174 119950202A57534MM136613 RIB BOEING727 727173C 1384059NM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED RIB ON THE RT WING O/B MID FLAP 9 INCHES IN FROM THE O/B END IN THE TRAILING EDGE COVE. INSTALLED REPAIR IAW SRM 51-10-1, 51-10-2, 51-30-2, 51-30-5, 51-20-4 AND MM 51-20-151. 2L73 4F A3WE 19950203005941995020300594NM 1995 2 3 UPS202175 119950202A5712 RIB CHORD BOEING727 727173C 1384059NM WS 686.5 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND RIGHT WING RIB CHORD CRACKED AT WS 686.5 LOWER CHORD STRINGER 6. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-1, 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950203005951995020300595NM 1995 2 3 UPS202176 119950202A5753 WEDGE BOEING727 727173C 1384059NM LT TE MID FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP T/E WEDGE HAS NUMEROUS AREAS OF CORROSION. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950203005961995020300596NM 1995 2 3 UPS202177 119950202A5753 WEDGE BOEING727 727173C 1384059NM LT TE MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT WING I/B MID FLAP T/E WEDGE LOWER SKIN SUPPORT CHORD ANGLE CRACKED AT NR 2 AFT FLAP TRACK CUTOUT. INSTALLED REPAIR IAW SRM 51-40-4, 51-20-2 AND OHM 20-50-02. 2L73 4F A3WE 19950203005971995020300597NM 1995 2 3 UPS202178 119950202A5320 ANGLE BOEING727 727173C 1384059NM FS 825 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRUCTURE SUPPORT ANGLE ON FORWARD SIDE OF UPPER CORD STUB BEAM STA 825 RBL 55-62 WL 208. INSTALLED REPAIR IAW SRM 51-10-01, 51-20-04 AND 51-30-2. 2L73 4F A3WE 19950203005981995020300598NM 1995 2 3 UPS202179 119950202A5520 ANGLE BOEING727 727173C 1384059NM NR 7 ELEV HINGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SUPPORT ANGLE FOR NR 7 ELEVATOR HINGE RIB ON REAR SPAR CHORD WEB STAB STA 223.05 LT. INSTALLED REPAIR IAW SRM 51-30-2 AND DRAWING 65-16876. 2L73 4F A3WE 19950203005991995020300599NM 1995 2 3 UPS202180 119950202A5320 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 STIFFENER LBL 33. INSTALLED REPAIR IAW SRM 51-30-2, 51-30-5. 2L73 4F A3WE 19950203006001995020300600NM 1995 2 3 UPS202181 119950202A5320 STIFFENER BOEING727 727173C 1384059NM BS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL STIFFENER BS 740 WL 163 LBL 13. INSTALLED REPAIR IAW SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950203006011995020300601NM 1995 2 3 UPS402133 119950131A3350 EEL BOEING747 747123F NM FLIGHT DECK INOPERATIVE A IPXAK NONE L NO TEST UKUNKNOWN 1 SO01672UP 20324 PILOT REPORTED THAT IN HKG, SEVERAL EMERGENCY LIGHTS UNDER THE INST GLARESHIELD ARE BURNED OUT. FILAMENTS REPLACED. LIGHTING OK. 2L74 4F A20WE 19950203006021995020300602WP 1995 2 3 UPS802122 119950131A53301002024T3 SKIN DOUBLER DOUG DC8 DC871F 302199DWP FS 12 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND FUSELAGE SKIN DOUBLER HAS 1 INCH LONG CRACK. RT AND LT AFT HEAT EXCHANGER CUTOUT LOWER AFT CORNERS. INSTALLED REPAIR IAW UPS EO DC8-5330-4732D. 2L74 4F RT4A25 19950203006031995020300603WP 1995 2 3 UPS802123 119950131A5313AND101302006 LONGERON DOUG DC8 DC871F 302199DWP FS 260-265 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10. 2L74 4F RT4A25 19950203006041995020300604WP 1995 2 3 UPS802124 119950131A53130637075T6 LONGERON DOUG DC8 DC871F 302199DWP FS 260-265 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10. 2L74 4F RT4A25 19950203006051995020300605WP 1995 2 3 UPS802125 119950131A5712575720123 RIBS DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 17, 21, 24, AND 27 UPPER RIBS CRACKED IN UPPER SURFACES. INSTALLED REPAIRS IAW MM 27-00-00, FIG. 801. (P/N 5769589, 5720123). 2L74 4F RT4A25 19950203006061995020300606WP 1995 2 3 UPS802126 119950131A5712575720123 RIBS DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 9, 11, 12, 14, AND 16 UPPER RIBS CRACKED ON UPPER SURFACES. INSTALLED REPAIRS IAW MM 57-00-00, FIG. 801. (P/N 5769589, 5720123). 2L74 4F RT4A25 19950203006071995020300607WP 1995 2 3 UPS802127 119950202A57535701110 VANE DOUG DC8 DC871F 302199DWP NR 6 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NB 6 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950203006081995020300608WP 1995 2 3 UPS802128 119950202A57535701473 VANE DOUG DC8 DC871F 302199DWP NR 5 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NR 5 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950203006091995020300609WP 1995 2 3 UPS802129 119950202A57125770123 RIB DOUG DC8 DC871F 302199DWP WS 660 LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK MAINTENANCE FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STA XFS 660. REPAIRED RIB PER MM 57-00-00. 2L74 4F RT4A25 19950203006101995020300610WP 1995 2 3 UPS802130 119950202A57535652288 VANE DOUG DC8 DC871F 302199DWP NR 2 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 2 FLAP VANE DELAMINATED ON UPPER SURFACE. REPLACED VANE PER MM 27-51-14. 2L74 4F RT4A25 19950203006111995020300611WP 1995 2 3 UPS802132 119950131A2170 WATER SEPARATOR DOUG DC8 DC873F 302199FWP LT PACK SATURATED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01816UP 45990 PILOT REPORTED LEFT PACK EMITS CHEMICAL ODOR (STRONG CLEANING SOLVENT) CAUSES BURNING SENSATION IN THE EYES. REPLACED LEFT PACK WATER SEPARATOR, COALESER BAG. RAN LEFT AND RIGHT PACKS FOR OVER ONE HOUR. NO ODORS NOTED. CHECKS GOOD PER MM 21-55-03. 2L74 4F RT4A25 19950203006131995020300613SO 1995 2 3 C2XA95CL006 119950119A3230922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT MLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916702 120078 DAY\CLE - FLT 3285 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT AIR RETURNED TO DAY. MAINTENANCE SWAPPED LEFT UPLOCK 'A' AND 'B' SYSTEM CANNON PLUGS IAW SNL 120-032-0015. OPS CHECK GOOD. PLACED 'B' SYSTEM INDICATION ON MEL 32-60-01, CONTROL NR 769924. ON 1-21-95, MAINTENANCE REMOVED AND REPLACED LEFT 'A' UPLOCK PROX SENSOR, SWAPPED CONNECTORS BACK. OPS CHECK GOOD. REMOVED FROM MEL. (X) 2L72 4T RTA31SO 19950203006141995020300614SO 1995 2 3 C2XA95CL007 119950123A32332060500004 ACTUATOR EMB 120 EMB120RT SO NLG OUT OF ADJUST A C2XAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW09127033378 73 120084 CLE\ROC - FLT 3113 - AT GEAR RETRACTION, THE RED NOSE 'A' AND 'B' LIGHT ILLUMINATED, GEAR WAS RECYCLED WITH SAME RESULTS. AIRCRAFT RETURNED TO CLE. MAINTENANCE ADJUSTED THE NOSE GEAR ACTUATOR IAW EMB MM 32-32-11. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950203006151995020300615SO 1995 2 3 C2XA95IA009 119950119A532012004149002 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND LT OUTBOARD T-PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950203006161995020300616SO 1995 2 3 C2XA95IA010 119950119A532012005779001C T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND RT OUTBOARD T-PROFILE CORRODED AT FRAME 40. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 10,984.6. CYC. 15,473. (X) 2L72 4T RTA31SO 19950203006171995020300617SO 1995 2 3 C2XA95IA014 119950119A5320 OMEGA BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912715 120125 IAH - DURING C-CHECK INSPECTION, FOUND AFT CABIN CENTER OMEGA BEAM CORRODED BETWEEN FRAMES 38 AND 39. MAINTENANCE REMOVED CORROSION AND INSTALLED REINFORCEMENT DOUBLER. REPAIR ACCOMPLISHED PER CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01043. A/C TT 10,984.6. CYC. 15,473. (X) 2L72 4T RTA31SO 19950203006181995020300618SO 1995 2 3 C2XA95IA015 119950123A2612MS3456KT1455S CONNECTOR EMB 120 EMB120RT SO RT MLG WW MOISTURE CONTAM A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0916718 120136 IAH - FLT 2630 - CREW REPORTED RT ENGINE AND WHEELWELL FIRE DETECTION INOP LIGHT FLICKERED ON IN-FLIGHT. MAINTENANCE CLEANED MOISTURE FROM RT ENG AND WHEELWELL FIRE DETECTOR LOOP CANNON PLUG, OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE. (CANNON PLUG NR PO832). (X) 2L72 4T RTA31SO 19950203006191995020300619EU 1995 2 3 C2XA95IA016 119950124A5311S53672402200 FRAME AEROSPATR42 ATR42320 8680930EU AFT FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914815 104 IAH - DURING C-CHECK INSPECTION, FRAME NR 37 WAS FOUND CORRODED THROUGH THE METAL THICKNESS AT STR 14R. MAINTENANCE REMOVED THE AFFECTED MATERIAL AND APPLIED A DOUBLER TO THE AFFECTED AREA. (X) 2H72 4T RTA53EU 19950203006201995020300620EU 1995 2 3 C2XA95IA017 119950124A5751MS276434 BEARINGS AEROSPATR42 ATR42320 8680930EU LT/RT AILERONS RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914815 104 IAH - DURING C-CHECK INSPECTION, LT AND RT AILERON CONTROL ROD TO BELLCRANK BEARINGS FOUND RUSTED WITH LT BEARING HAVING A NOTED POPPING WHEN THE AILERON WAS MOVED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS AND THE AIRCRAFT WAS RELEASED TO SERVICE. AIRCRAFT TT 14901.8. T.C. 16928. (X) 2H72 4T RTA53EU 19950203006241995020300624NM 1995 2 3 TAOA019501 119950103A33501000677 EEL GRIMES BOEING727 727225 1384077NM L-2 DOOR INOPERABLE A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 3055 20445 L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR L-1 DOOR EMERGENCY EXIT LIGHT. (X) 2L73 4F A3WE 19950203006301995020300630NM 1995 2 3 TWRA9501 119950104A3350 EEL WIRING BOEING747 747136 1384883NM CABIN CUT A TWRAK NONE L NO TEST CRCRUISE 1 EA15606FF 20273 DURING FLIGHT, THE UPPER DECK FLOOR LIGHTS COME ON AND STAY ON AT ALL TIMES. REPAIRED CUT AND CHAFED WIRES AT POWER SUPPLY, OPS CHECK OKAY. (X) 2L74 4F A20WE 19950203006321995020300632NM 1995 2 3 TWRA9503 119950105A335058223 EEL BATTERY PACK BOEING747 747238B 1384828NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15614FF 20534 DURING PRE-FLIGHT, SOME EMERGENCY LIGHTS INOP IN 'D' ZONE. REPLACED BATTERIES IN CEILING, OPS CHECK OKAY. (X) 2L74 4F A20WE 19950203006331995020300633NM 1995 2 3 TWRA9504 119950131A2612895398 FIRE WARN BOEING747 747121 1384871NM NR 1 ENGINE MALFUNCTIONED A TWRAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 EA15617FF 19650 DURING CRUISE, NR 1 ENGINE FIRE WARNING LIGHT CAME ON CAUSED BY B-LOOP FIRE INDICATION. ENGINE WAS SHUT DOWN IAW FIRE CHECK LIST. 2211 FLT MANUAL, VOL I. BOTH FIRE BOTTLES DISCHARGED. THERE WAS NO VISUAL INDICATION OF FIRE. A-LOOP WAS PREVIOUSLY PLACARDED INOP OUT OF MIAMI. AFTER FURTHER TROUBLESHOOTING, MAINTENANCE REPLACED AFT FIRE WARNING DETECTOR. SYSTEM CHECK NORMAL PER MM 26-21-00. (X) 2L74 4F A20WE 19950203006341995020300634NM 1995 2 3 TWRA9505 119950110A3350601211 EEL BATTERY PACK BOEING747 747136 1384883NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15605FF 20271 DURING DAILY SERVICE, FOUND BOTH OVER-WING LIGHTS INOPERATIVE ON RIGHT SIDE FUSELAGE. REPLACED BATTERY AT R-3 MAIN ENTRY DOOR, OPS CHECK OKAY. (X) 2L74 4F A20WE 19950203006351995020300635NM 1995 2 3 TWRA9506 119950114A335060B40053 EEL BATTERY PACK BOEING747 747282B 1384860NM CABIN DISCHARGED A TWRAK NONE L NO TEST TXTAXI/GRND HDL 1 EA15610FF 20501 DURING LOADING OF A/C, COULD NOT EXTINGUISH EMERGENCY EXIT LIGHTS. RESEATED CANNON PLUG AT ALL EXIT LIGHTS, REPLACED BATTERY PACK AT L-5 MAIN ENTRY DOOR, REPAIRED GROUND PLUG R484. SYSTEM OPS CHECK OKAY. (X) 2L74 4F A20WE 19950203006381995020300638CE 1995 2 3 95ZZZW41 119950104A5753 SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143AM UC143 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE LT O/B FLAP (P/N 35165050258), REVEALED A 1.5 INCH CRACK IN THE UPPER SKIN, AND A 1 INCH CRACK IN THE LOWER SKIN ALONG THE TE BETWEEN THE FIRST AND SECOND RIB O/B FROM THE I/B END. THE CRACKS WERE REPAIRED BY STOP DRILLED AND INSTALLING DOUBLERS. 2L72 4T RTA24CE 19950203006401995020300640EU 1995 2 3 95ZZZW43 119950111A79311241013 OIL PRESS TRANS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT ENGINE FAILED A AVTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27477UE 890 P66187 IAD-ISP - FLT 6300 - DURING CRUISE, DIVERTED TO BWI DUE TO THE RT BETA LIGHT ILLUMINATING,WHICH WAS VERIFIED AS AN INDICATION PROBLEM. ALSO, THE RT OIL PRESSURE FAILED HIGH, AND RT FUEL PRESSURE FILED LOW. AN INFLIGHT EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN ENGINE AND DIVERTED TO BWI. MAINTENANCE REPLACED THE P3 LINE, THE OIL PRESSURE TRANSMITTER, THE FUEL PRESSURE TRANSMITTER AND THE BETA SWITCH. ACFT WAS RELEASED AND APPROVED FOR SERVICE. REF VTZA95019, REF 95ZZZW44, REF 95ZZZW45. 2L72 4T3 TRTA56EU E3WE 19950203006411995020300641EU 1995 2 3 95ZZZW44 119950111A73321241013 FUEL PRESS TRANS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT ENGINE FAILED A AVTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27477UE 890 P66187 IAD-ISP - FLT 6300 - DURING CRUISE, DIVERTED TO BWI DUE TO THE RT BETA LIGHT ILLUMINATING,WHICH WAS VERIFIED AS AN INDICATION PROBLEM. ALSO, THE RT OIL PRESSURE FAILED HIGH, AND RT FUEL PRESSURE FILED LOW. AN INFLIGHT EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN ENGINE AND DIVERTED TO BWI. MAINTENANCE REPLACED THE P3 LINE, THE OIL PRESSURE TRANSMITTER, THE FUEL PRESSURE TRANSMITTER AND THE BETA SWITCH. ACFT WAS RELEASED AND APPROVED FOR SERVICE. REF VTZA95019, REF 95ZZZW43, REF 95ZZZW45. 2L72 4T3 TRTA56EU E3WE 19950203006421995020300642 1995 2 3 95ZZZW45 319950111A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT ENGINE FAILED A AVTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27477UE 890 P66187 IAD-ISP - FLT 6300 - DURING CRUISE, DIVERTED TO BWI DUE TO THE RT BETA LIGHT ILLUMINATING,WHICH WAS VERIFIED AS AN INDICATION PROBLEM. ALSO, THE RT OIL PRESSURE FAILED HIGH, AND RT FUEL PRESSURE FILED LOW. AN INFLIGHT EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN ENGINE AND DIVERTED TO BWI. MAINTENANCE REPLACED THE P3 LINE, THE OIL PRESSURE TRANSMITTER, THE FUEL PRESSURE TRANSMITTER AND THE BETA SWITCH. ACFT WAS RELEASED AND APPROVED FOR SERVICE. REF VTZA95019, REF 95ZZZW43, REF 95ZZZW44. 2L72 4T3 TRTA56EU E3WE 19950203006441995020300644WP 1995 2 3 HAL95008 119950115A5330 SKIN DOUG DC9 DC951 3022051WP FS 1209 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13603DC 47784 HNL - DURING SERVICE CHECK FOUND SMALL CRACK AT RIVET ON THE RT SIDE OF THE FUSELAGE AT STA 1209 APPROXIMATELY 8 INCHES ABOVE THE RT ENG PYLON. MADE FILLER AND DOUBLER REPAIR PER SRM 53-04 PG 98A FIG 18. (W) 2L72 4F A6WE 19950203006451995020300645WP 1995 2 3 HAL95012 119950117A5330 SKIN DOUG DC9 DC951 3022051WP FS 1247 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 HNL - DURING S-CHECK, FOUND APPROXIMATELY 1.25 INCH CRACK BETWEEN LONGERON 3L AND LONGERON 4L AT FUSELAGE STA 1247. MADE FILLER AND INTERNAL DOUBLER REPAIR PER HAL FORM M 105 FILE NR 61037. (W) 2L72 4F A6WE 19950203006471995020300647NM 1995 2 3 TSAA9553025 119950124A5330 SKIN BOEING737 7372S2C 138448GNM BS 941 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13806AL 21927 DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 941 S24L. HFEC CONFIRMED CRACK LENGTH 2.9375 INCH (CRACK PARALLEL WITH STRINGER). REPAIRED PER SRM 53-30-3. ACFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950203006491995020300649WP 1995 2 3 USAA950005 119950105A335060030451LB EEL BATT PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19995VJ 47334 EWR - THE FLOOR LEVEL EMERGENCY LIGHTS PAST ROW 17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BAD SECTION OF WIRE AND REPLACED THE BATTERY PACK. (W) 2L72 4F A6WE 19950203006501995020300650NM 1995 2 3 USAA950012 119950108A2421948F4582 AC GENERATOR BOEING737 7373B7 1384580NM NR 1 ENGINE FAILED A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA19507AU 23382 PHL - FLT 1021 - AFTER TAKEOFF, LT GENERATOR FAILED, APU ON MEL. FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED NR1 ENGINE AC GENERATOR. (W) 2L72 4F RTA16WE 19950203006511995020300651NM 1995 2 3 USAA950015 119950110A3350 EEL BOEING737 7372Q9 138448MNM LT OVERWING INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19230AU 21975 DCA - THE LEFT EMERGENCY EXIT OVERWING LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY AT EMERGENCY EXIT ROW. (W) 2L72 4F A16WE 19950203006521995020300652WP 1995 2 3 VTZA95019 219950111A73201311543L401 P3 LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT ENGINE CRACKED A AVTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27477UE 890 P66187 IAD-ISP - FLT 6300 - DURING CRUISE, DIVERTED TO BWI DUE TO THE RT BETA LIGHT ILLUMINATING,WHICH WAS VERIFIED AS AN INDICATION PROBLEM. ALSO, THE RT OIL PRESSURE FAILED HIGH, AND RT FUEL PRESSURE FAILED LOW. AN INFLIGHT EMERGENCY WAS DECLARED AND THE CREW SHUTDOWN ENGINE AND DIVERTED TO BWI. MAINTENANCE REPLACED THE P3 LINE, THE OIL PRESSURE TRANSMITTER, THE FUEL PRESSURE TRANSMITTER AND THE BETA SWITCH. ACFT WAS RELEASED AND APPROVED FOR SERVICE. REF 95ZZZW43, REF 95ZZZW44, REF 95ZZZW45. 2L72 4T3 TRTA56EU E3WE 19950210000011995021000001NM 1995 2 10 9501716623 119950201A5315 FLOOR BEAM BOEING747 747251B 1384892NM FS 460 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623US 21705 DURING PERIODIC CHECK, FOUND THE FLOOR BEAM AT FS 460, LBL 25 - 35 CORRODED. REMOVED STIFFENER AND CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND INSTALLED REPAIR. 2L74 4F A20WE 19950210000021995021000002WP 1995 2 10 9501729930 119950123A2133 OUTFLOW VALVE DOUG DC9 DC931 3022065WP AFT FUSELAGE ICE CONTAMINANT A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL0189S 47042 DURING CLIMB-OUT FROM MDW, CABIN PRESSURE WARNING AND MASTER WARNING LIGHTS ILLUMINATED. PERFORMED MANUAL OPERATION BUT CONTROL WHEEL WAS HARD TO MOVE. WHEEL MOVEMENT EVENTUALLY LOOSENED AND NORMAL CABIN PRESSURE WAS ACHIEVED. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FOUND ICE ACCUMULATION ON OUTFLOW VALVE. REMOVED ICE DEBRIS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210000031995021000003WP 1995 2 10 9501739903 119950127A2160SYLZ9212 ELECT CONTL UNIT DOUG DC9 DC931 3022065WP LEFT MALFUNCTIONED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01853N 3331517822 47083 ON TAKEOFF AT 90 KTS, MASTER CAUTION AND AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHTS ILLUMINATED. ABORTED TAKEOFF AND CLEARED RUNWAY. SUCCESSFUL TAKEOFF WAS ACCOMPLISHED ON SECOND ATTEMPT. REPLACED THE LEFT ELECTRONIC THERMAL CONTROL UNIT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210000041995021000004WP 1995 2 10 9501749975 119950127A2410696233B CSD DOUG DC9 DC931 3022065WP RT ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019339 408685237 47382 RIGHT CSD TEMPERATURE ROSE ABOVE RED LINE DURING CLIMB-OUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE CSD AND GENERATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210000051995021000005WP 1995 2 10 ABXA9500065 119950201A7830AE24645E014D HOSE DOUG DC8 DC862 3021970WP TR UNIT LEAKING A ABXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL23804AX 45987 HYDRAULIC QUANTITY WENT TO STANDPIPE LEVEL ON APPROACH. REMOVED AND REPLACED THRUST REVERSER HYDRAULIC PUMP PRESSURE HOSE WHICH WAS LEAKING. SYSTEM OPS CHECKED GOOD IAW DC 8 MM CHAPTER 78. 2L74 4F 4A25 19950210000061995021000006NM 1995 2 10 BIER9502 119950203A322245050901 CENTERING CAM PIPER PA60 PA60700P 7106023NM NLG STRUT DENTED A ABIEAK NONE J WARNING INDICATION LDLANDING 1 EA216892Q1400 608423007 ON APPROACH NOSE GEAR DID NOT INDICATE DN LOCK, AFTER SEVERAL ATTEMPTS IT LOCKED. ON LANDING AIRCRAFT VEERED LEFT WHEN NOSE WHEEL TOUCHED DOWN. UPON TEARDOWN OF NOSE STRUT, FOUND THE CENTERING CAM HAD SERERAL DENTS IN THE CAMBER FACE WHICH ALLOWED THE CENTER PIN TO CATCH IT AND NOT CENTER. THIS CAUSED THE NOSE WHEEL TO HANG IN THE NOSE WELL AND ALSO TO COME DOWN SIDE WAYS WHEN EXTENDING GEAR. SUSPECT ROUGH PUSH BACKS CAUSED PROBLEM. ALSO, SUSPECT CENTER PIN HAD BEEN SHEARED EARLIER BUT THE CAM WAS NOT INSPECTED. SUGGEST INSPECTING CAM WHEN RESEALING STRUT OR IF CENTER PIN IS SHEARED. 1M72 3O RTA17WE 19950210000071995021000007NM 1995 2 10 SWAA950110 119950131A3350900835A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED A3 CHECK, FOUND FWD OVERHEAD EXIT SIGN INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950210000081995021000008NM 1995 2 10 SWAA950111 119950131A3350 EEL BATTERY BOEING737 7373A4 1384585NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07668SW 23060 DURING SCHEDULED CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT NOT TESTING. REPLACED BATTERY PER BOEING M/M. 2L72 4F RTA16WE 19950210000091995021000009NM 1995 2 10 SWAA950112 119950201A531365617777 STRINGER BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 360, S15L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000101995021000010NM 1995 2 10 SWAA950113 119950201A532065596644 SPLICE BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S4L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000111995021000011NM 1995 2 10 SWAA950114 119950201A5313BAC5602 STRINGER BOEING737 7373H4 1384600NM BS 501 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 501, S28R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000121995021000012NM 1995 2 10 SWAA950115 119950201A53206561777505 SPLICE BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, S14L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000131995021000013NM 1995 2 10 SWAA950116 119950201A5313BAC15171471 STRINGER BOEING737 7373H4 1384600NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 767, S11L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000141995021000014NM 1995 2 10 SWAA950117 119950201A5320 CLIP BOEING737 7373H4 1384600NM BS 727B BENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP BENT AND GOUGED AT BS 727B, S26R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000151995021000015NM 1995 2 10 SWAA950118 119950201A53206941372 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 927, S27R, AT BS 500A, S9R, AT BS 663, S10L, AT BS 663, S10R, AND AT BS 947, S25R. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000161995021000016NM 1995 2 10 SWAA950119 119950201A532065528948 SUPPORT BOEING737 7373H4 1384600NM BS 540 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, BL 0 TO RBL 25. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000171995021000017NM 1995 2 10 SWAA950120 119950201A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM FASTENER HOLE CORRODED AT BS 947, WL 208, RBL 5. REPAIRED PER SWA EWO 95-0086. 2L72 4F RTA16WE 19950210000181995021000018NM 1995 2 10 SWAA950121 119950201A532065529941 SUPPORT BOEING737 7373H4 1384600NM BS 540 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FLOOR BEAM SUPPORT CRACKED AT BS 540, WL 208, BL 0 TO LBL 25. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000191995021000019NM 1995 2 10 SWAA950122 119950201A53206546547576 VERTICAL BEAM BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D-CHECK, FOUND VERTICAL BEAM STANCHION CRACKED AT BS 747+4, RBL 11, WL 161. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000201995021000020NM 1995 2 10 SWAA950123 119950201A5315BAC1505100246 FLOOR BEAM BOEING737 7373H4 1384600NM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FLOOR BEAM NUTPLATE HOLES CORRODED AT BS 312, LBL 11 TO RBL 11, WL 208. REPLACED DAMAGED SECTION PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000211995021000021NM 1995 2 10 SWAA950124 119950201A5754 SKIN BOEING737 7373H4 1384600NM NR 2 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND NUMBER 2 SLAT SKIN CRACKED ADJACENT TO EXISTING REPAIR. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING 65C30133. 2L72 4F RTA16WE 19950210000221995021000022NM 1995 2 10 SWAA950125 119950201A5320 ANGLE BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND 'L' ANGLE CRACKED AT BS 616, WL 200. REPAIRED PER TRAMCO EWO 95-0066. 2L72 4F RTA16WE 19950210000231995021000023NM 1995 2 10 SWAA950126 119950201A5320655287897 MOP SILL BOEING737 7373H4 1384600NM BS 985 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR MOP SILL CORRODED AT BS 985, WL 208, S17R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000241995021000024NM 1995 2 10 SWAA950127 119950201A5210655287461 FRAME BOEING737 7373H4 1384600NM AFT PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOOR UPPER FORWARD FRAME CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000251995021000025NM 1995 2 10 SWAA950128 119950201A5314 KEEL BEAM BOEING737 7373H4 1384600NM BS 500 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND AC DISTRIBUTION BAY LEFT KEEL BEAM OUTBOARD FLANGE CORRODED AT BS 500D, WL 149, LBL 7. REPAIRED PER TRAMCO EWO 95-0073. 2L72 4F RTA16WE 19950210000261995021000026NM 1995 2 10 SWAA950129 119950201A5230 FRAME BOEING737 7373H4 1384600NM FWD CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME CRACKED IN FORWARD TOP RADIUS ABOVE NUMBER 5 STOP FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000271995021000027NM 1995 2 10 SWAA950130 119950201A5320 FRAME BOEING737 7373H4 1384600NM BS 500 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FORWARD CARGO AFT DOOR FRAME DENTED IN TOP FLANGE OF FRAME, BS 500, RBL 45, WL 165.75. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000281995021000028NM 1995 2 10 SWAA950131 119950201A5242 SKIN BOEING737 7373H4 1384600NM E/E DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND E/E DOOR OUTER SKIN GOUGED AND NICKED. REPAIRED DAMGED AREAS PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000291995021000029NM 1995 2 10 SWAA950132 119950201A53306545775126 SKIN BOEING737 7373H4 1384600NM BS 727-907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKS FROM BS 727 TO 907, S20 TO 25L AND R. REPLACED SKINS PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000301995021000030NM 1995 2 10 SWAA950133 119950201A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT: BS 916.5, 2 INCH ABOVE S25L, BS 807 TO 812, S27L TO 27R, AT BS 307, BETWEEN 21 AND 22R, AT BS 500A +6, BETWEEN S24 AND 24R, AT BS 311, BETWEEN S20 AND 21R, AT BS 1064, BETWEEN S20 AND 21R, AND FROM BS 849 TO 854, BL 0 TO RBL 15, WL 159. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000311995021000031NM 1995 2 10 SWAA950134 119950201A5330 SKIN BOEING737 7373H4 1384600NM BS 957 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 957, AT S19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000321995021000032NM 1995 2 10 SWAA950135 119950201A53206546561509 FRAME BOEING737 7373H4 1384600NM SERVICE DOORWAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOORWAY UPPER FORWARD FRAME CRACKED ON INBOARD RADIUS AT LATCH FITTING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000331995021000033NM 1995 2 10 SWAA950136 119950201A5330 SKIN BOEING737 7373H4 1384600NM BS 327 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 327, RBL 65, WL 210. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000341995021000034NM 1995 2 10 SWAA950137 119950201A53207075T6040 VERTICAL SUPPORT BOEING737 7373H4 1384600NM BS 500 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FORWARD FOUND VERTICAL SUPPORT WEB DENTED AT SIDEWALL SUPPORT PLATE ATTACH LOCATION BS 500+3, RBL 22.5, WL 156. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000351995021000035NM 1995 2 10 SWAA950138 119950201A532065458661211 STRESS PANEL BOEING737 7373H4 1384600NM BS 663-727 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND KEEL BEAM STRESS PANEL DAMAGED AT BS 663-727, BL 0, WL 148. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000361995021000036NM 1995 2 10 SWAA950139 119950201A53207075T6050 VERTICAL BEAM BOEING737 7373H4 1384600NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND WEB BETWEEN VERTICAL STANCHION BEAMS CRACKED AT BS 727, LBL 12-15, WL 170. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000371995021000037NM 1995 2 10 SWAA950140 119950201A532065C807351 MOP SILL BOEING737 7373H4 1384600NM SERVICE DOOR CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000381995021000038NM 1995 2 10 SWAA950141 119950201A5320 ANGLE BOEING737 7373H4 1384600NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND PRESSURE WEB ANGLE CRACKED AT BS 663, RBL 65, WL 203. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000391995021000039NM 1995 2 10 SWAA950142 119950201A53207075T6 PRESSURE DECK BOEING737 7373H4 1384600NM BS 665.75-672.75CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND WING CENTER SECTION PRESSURE DECK WEB CRACKS AT BS 665.75, RBL 39.25, WL 202.5 AND AT BS 672.75, RBL 42.5, WL 202.5. REPAIRED PER TRAMCO EWO 95-0065. 2L72 4F RTA16WE 19950210000401995021000040NM 1995 2 10 SWAA950143 119950201A52402024T3050 SKIN BOEING737 7373H4 1384600NM SERVICE DOOR GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND FORWARD SERVICE DOOR OUTER SKIN GOUGED ON FORWARD EDGE ABOVE LOWER HINGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000411995021000041NM 1995 2 10 SWAA950144 119950201A53302024T3036 SKIN BOEING737 7373H4 1384600NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07309SW 22948 DURING SCHEDULED D CHECK, FOUND LIGHTNING STRIKE DAMAGE AT THE FOLLOWING AREAS: BS 777, S9R, AT BS 727A+16 TO 18, S8R, AT BS 500D+1.5, S3R, AT BS 727E+10, S9R, AT BS 607.75, S5R, AT BS 441, S9L, AT 278.5, 3.75 INCH ABOVE S12L, AT BS 500A+11.25 AND +13.75, S6R, AT BS 748, S9R, AT BS 727E+1.25, S9R, AT BS 727C+7 TO 8, S9R, AT BS 749.5, S9R, AT BS 727A+2, S8R, AT BS 656, S5R, AT BS 582.5, S5R, AT BS 727C+1.25, S9R, AT BS 546.5, S5R, AT BS 500A+8, S8L, AT BS 540.5, S5R, AND AT BS 523.5, S5R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210000421995021000042 1995 2 10 WWMA9500014 219950125A721031070512 AIR OIL SEAL BAG JETSTMJETSTM3201 1500217EU LT GEAR CASE DEFECTIVE I WWMAK NONE O OTHER CRCRUISE 1 WP15959AE 959 FLIGHT NR 5240 (SAN/LAX) PILOT REPORTED, LEFT BLEED AIR SMELLING LIKE COMPRESSOR WASH AGENT. MAINTENANCE FOUND OIL LEAKING FROM LEFT HAND GEAR CASE CARBON SEAL INTO INTAKE. MAINTENANCE REMOVED AND REPLACED COMPRESSOR AIR OIL SEAL CARBON AND ROTOR. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000431995021000043EU 1995 2 10 WWMA9500015 119950125A32307445B HYD VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR DEFECTIVE I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15961AE 961 FLIGHT NR 5232 (OXR/LAX) PILOT REPORTED, THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. MAINTENANCE FOUND THE EMERGENCY RELEASE VALVE BYPASS PIN POPPED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC RELEASE VALVE. OPERATIONAL CHECKS WERE GOOD, NO LEAKS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000441995021000044EU 1995 2 10 WWMA9500016 119950126A3520 OXY MASKS BAG JETSTMJETSTM3201 1500217EU CABIN DEPLOYED I WWMAG O2 MASK DEPLOYED O OTHER LDLANDING 1 WP15963AE 963 FLIGHT NR 5244 (FAT/LAX) PILOT REPORTED SEAT 6A OXYGEN MASK DEPLOYED. MAINTENANCE RESECURED OXYGEN MASK AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000451995021000045NE 1995 2 10 WWMA9500017 219950125A7230 COMP BLADE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE DEFECTIVE I AWWMAAE UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP15283AE5977 340B283 FLIGHT NR 5320 (FSM/DFW) PILOT REPORTED THAT THE RIGHT ENGINE FLAMED OUT ON TAKEOFF. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE PERFORMED BORESCOPE ON THE RIGHT HAND ENGINE IAW CT7 MM 72-00. MAINTENANCE FOUND THE RIGHT HAND STAGE 3 COMPRESSOR BLADE TORN; BLADE IS NOT WITHIN LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW SAAB AMM 71-00. PERFORMED LEAK CHECK AND RUNS: CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950210000461995021000046EU 1995 2 10 WWMA9500018 119950207A261251224127 FIRE LOOP BAG JETSTMJETSTM3201 1500217EU LT ENGINE DAMAGED A WWMADF RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 WP15951AE 951 ON TAXI OUT, THE CREW REPORTED A FIRE INDICATION ON THE LEFT ENGINE. THE CREW FIRED BOTH ENGINE FIRE BOTTLES. UPON INVESTIGATION, MAINTENANCE FOUND NO EVIDENCE OF FIRE, BUT DID FIND A NICK ON THE LEFT ENGINE FORWARD FIRE LOOP. THE LOOP WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000471995021000047 1995 2 10 WWMA9500019 219950130A7200TPE33112U ENGINE BAG JETSTMJETSTM3201 1500217EU RIGHT FAILED I WWMAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 WP15952AE 952 FLIGHT 5028 - LAX/BFL - PILOT REPORTED THE RIGHT ENGINE FAILED IN FLIGHT AND THEY RETURNED TO LAX WITHOUT INCIDENT. MAINTENANCE FOUND THE CHIP DETECTOR TO HAVE METAL ON IT AND THE OIL FILTER WAS CONTAIMINATED WITH METAL. MAINTENANCE REPLACED THE ENGINE, PROPELLER, OIL COOLER, AND FLUSHED ALL ASSOCIATED LINES. ALL NECESSARY RUNS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000481995021000048EU 1995 2 10 WWMA9500020 119950131A3260615423 DNLOCK SPRING BAG JETSTMJETSTM3201 1500217EU RT MLG BROKEN I WWMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP15958AE 958 FLIGHT 5137 LAX/SBA - PILOT REPORTED, THAT THE RIGHT MAIN GEAR INTRANSIT LIGHT DID NOT INDICATE INTRANSIT. WHEN THE GEAR WAS CYCLED UP THE RIGHT MAIN GREEN LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK RETURN SPRING BROKEN CAUSING THE MICROSWITCH TO STAY IN THE GEAR DOWN MODE. MAINTENANCE REPLACED THE RETURN SPRING AND PERFORMED GEAR SWINGS. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950210000901995021000090WP 1995 2 10 95ZZZZ38 119950123A3350003PA54 TRACK EEL DOUG DC9 DC983 3022083WP CABIN INOP A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 PDX - FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. (Z) 2L72 4F RTA6WE 19950210000911995021000091NM 1995 2 10 ASAA95013 119950108A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 SEA - DURING MAINTENANCE CHECK THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950210000921995021000092WP 1995 2 10 ASAA95014 119950108A3350RPS1B EEL POWER SUPPLY DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 PDX - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950210000931995021000093NM 1995 2 10 ASAA95015 119950109A33508821004 EEL BATT PACK BOEING737 737290C 138448VNM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - FLT 51 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN 'OFF' ARM, OR 'ON' POSITIONS. REPLACED BATTERY PACK AT ROW 10 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950210000941995021000094NM 1995 2 10 ASAA95016 119950109A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 SEA - DURING MAINTENANCE CHECK THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950210000951995021000095WP 1995 2 10 ASAA95017 119950113A21701808492 COALESCERS DOUG DC9 DC983 3022083WP AIR COND SYS DIRTY A ASAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM01948AS 53021 SEA - FLT 99 - ON ARRIVAL, CREW REPORTED 'DIRTY SOCKS' ODOR IN CABIN OF 10,000 FEET DURING APPROACH. REPLACED COALESCERS AND NO ODORS WERE NOTED. COALESCERS LOOKED AND SMELLED CLEAN. (W) 2L72 4F RTA6WE 19950210000961995021000096WP 1995 2 10 ASAA95018 119950113A3350 EEL WIRING DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01969AS 53063 LAX - FLT 255 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT THE OVERWING EXIT AREA WERE INOPERATIVE. REPAIRED BROKEN WIRING IN FLOOR TRACK LIGHTS AT OVERWING EXIT AREA, AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950210000971995021000097NM 1995 2 10 ASAA95019 119950114A33508731002142 EEL ASSY BOEING737 7372X6C 1384552NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - FLT 65 - PRIOR TO DEPARTURE, CREW REPORTED THE FWD BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED 'EXIT TO REAR' LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950210000981995021000098NM 1995 2 10 ASAA95020 119950114A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 SEA - DURING MAINTENANCE CHECK THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950210000991995021000099WP 1995 2 10 ASAA95022 119950116A335060030431 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK THE AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950210001001995021000100WP 1995 2 10 ASAA95023 119950118A335041B004AD07G3 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS WERE FOUND INOPERATIVE. REPLACED PACK BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950210001011995021000101NM 1995 2 10 ASAA9524 119950119A33508821004 EEL BATTERY BOEING737 737290C 138448VNM AFT PALLET DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - CHECK, FOUND AFT PALLET TRACK LIGHTS DIMLY ILLUMINATED. MAINTENANCE REPLACED BATTERY PACK, OPS CHECKED NORMAL. (W) 2L72 4F A16WE 19950210001021995021000102WP 1995 2 10 ASAA9525 119950123A33500105601 EEL TRACK COVER DOUG DC9 DC983 3022083WP CABIN MISSING A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 PDX - CHECK, FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. REF 95ZZZW108. 2L72 4F RTA6WE 19950210001031995021000103NM 1995 2 10 ASAA9526 119950121A3350883200312 EEL RECEIVER BOEING737 737290C 138448VNM CABIN INOP A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA -CHECK, TRACK LIGHTS INOP AT ROW 11. MAINTENANCE REPLACED RECEIVER ASSY AT ROW 11. (W) 2L72 4F A16WE 19950210001041995021000104NM 1995 2 10 ASAA9527 119950121A335086210144 EEL BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - CHECK, SMOKE BARRIER EXIT LIGHTS INOP. MAINTENANCE REPLACED BATTERY. (W) 2L72 4F A16WE 19950210001051995021000105WP 1995 2 10 ASAA9528 119950121A335041BOO4AD07G3 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 SEA - CHECK, 3 CEILING LIGHTS INOP AT ROWS 24 AND 25. MAINTENANCE REPLACED BATTERIES AND SYSTEM OPS CHECKED NORMAL. (W) 2L72 4F RTA6WE 19950210001061995021000106WP 1995 2 10 ASAA9529 119950121A335010011901 EEL ASSEMBLY DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01963AS 53077 SFO - CHECK, FWD ENTRY DOOR L1 PORTABLE EMERGENCY LIGHT ON/OFF SWITCH INOP. LIGHT COULD NOT BE TURNED ON. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND OPS CHECK NORMAL. (W) 2L72 4F RTA6WE 19950210001071995021000107NM 1995 2 10 ASAA9531 119950121A3350 EEL WIRING BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 PDX - CHECK, FLOOR TRACK LIGHTS INOP AT ROWS 28-36. MAINTENANCE RECONNECTED LOOSE BUS WIRE IN TRACK. (W) 2L72 4F RTA16WE 19950210001331995021000133NM 1995 2 10 9501755520 119950205A2421729825E IDG BOEING757 757251 1384970NM LT ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01520US1852 23208 AT THE START OF TAKEOFF, THE LEFT GENERATOR DRIVE LIGHT FLICKERED AND THE LEFT GENERATOR CONTROL LIGHT ILLUMINATED; ABORTED TAKEOFF. PLACED THE LEFT IDG ON MEL 24-00-1. REPLACED THE LEFT INTEGRATED DRIVE GENERATOR AT MSP. SYSTEM CHECK ON RUN-UP WAS NORMAL. 2L72 4F RTA2NM 19950210001341995021000134NM 1995 2 10 9501765508 119950201A5313146N55416 STRINGER BOEING757 757251 1384970NM FS 1330 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01508US 30360 23197 DURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGER AT FS 1330, RBL 11 AND RBL 7 WAS FOUND CORRODED AT THE NUTPLATES. REMOVED CORROSION AND REPAIRED PER NWA EA 55-96620. 2L72 4F RTA2NM 19950210001351995021000135NM 1995 2 10 9501775508 119950201A5313146N5444 STRINGER BOEING757 757251 1384970NM FS 1510 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01508US 30360 23197 DURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGER AT FS 1510, RBL 11 AND RBL 7 WAS FOUND CORRODED AT THE NUTPLATES. REMOVED CORROSION AND REPAIRED PER NWA EA 55-93725 2L72 4F RTA2NM 19950210001361995021000136WP 1995 2 10 9501781146 119950202A5315 FLOOR BEAM DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FLOOR BEAM AT FS 879, RBL 29 - 37. REMOVED DAMAGE AND REPAIRED PER EA 11-96621. 2L73 4F A22WE 19950210001371995021000137WP 1995 2 10 9501791146 119950202A5320 INTERCOSTAL DOUG DC10 DC1040 3023508WP FS 445 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE FUSELAGE BELT FRAME TO INTERCOSTAL STRAP AT FS 445, LBL 25 TO THE ACCESS DOOR 115AZ. REPLACED STRAP. 2L73 4F A22WE 19950210001381995021000138SW 1995 2 10 COM20354 119950202A274027821087 CONTROL BOX SWRNGNSA227 SA227AC 8780603SW PITCH TRIM MALFUNCTIONED A COMAK NONE O OTHER UKUNKNOWN 1 SO01457AM8532 3632 AC694 PITCH TRIM OUT OF RANGE AURAL WARNING IS INOP. COULD NOT DUPLICATE DISCREPANCY. REPLACED PITCH TRIM CONTROL BOX FOR TROUBLESHOOTING. 1L72 4T A8SW 19950210001391995021000139EA 1995 2 10 COM60404 119950201A27706229968001 YAW DAMPER CNDAIRCL600 CL6002B19 EA RUDDER DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01934CA1455 7042 NR 1 YAW DAMPER DISCONNECTED IN FLIGHT. REPLACED YAW DAMPER. 2L72 4F RTA21EA 19950210001401995021000140NE 1995 2 10 DL31L950517 219950202A7250PW4152 STATOR VANE AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11835AB8100 650 724562 DURING INSPECTION, PERFORMING OPERATION 5163, BOROSCOPE INSPECTION 1ST AND 2ND STAGE HPT. FOUND 1ST STAGE STATOR VANES WITH CRACKING BEYOND LIMITS. ENGINE WAS REMOVED AND ROUTED TO SHOP, ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2L72 4F RTA35EU E24NE 19950210001411995021000141NM 1995 2 10 DL72E950491 119950202A5320 WEB BOEING727 727247 138408FNM FS 1240 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON C2 LETTER CHECK, TWO .25 INCH CRACKS UPPER LIGHTENING HOLE STA 1240R - AFT STAIRWELL AREA, REPAIRED PER 53-11-0 NR 15. 2L73 4F A3WE 19950210001421995021000142NM 1995 2 10 DL72E950492 119950202A5320 FORMER BOEING727 727247 138408FNM AFT FUS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON C2 LETTTR CHECK, FWD COWL TO FUSELAGE LIP DAMAGED AT 6 O'CLOCK POSITION, REPAIR AND REPLACED DOUBLER PER M/M 53-11-0 PG 801 2L73 4F A3WE 19950210001431995021000143NM 1995 2 10 DL72K950503 119950203A5320 STAIR WEB BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11479DA 20756 FOUND ON LETTER CHECK, A .875 INCH CRACK IN DOUBLER AT HORIZ STIFFENER STA 1263 BELOW VENTRAL STAIR ACT - 2. .75 INCH CRACK AT LIGHTENING HOLE UPPER STA 1266 BELOW VENTRAL STAIR ACT - REPAIR - 1. REPAIRED PER ERA 301128-14 CODE 4-53-10 - 2. REPAIRED PER M/M 53-11-0 P 832. 2L73 4F A3WE 19950210001441995021000144NM 1995 2 10 DL72L950479 119950119A575365192709 TRACK BOEING727 727232 1384082NM LT TE FLAPS INB CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING INSPECTION AT HMV, THE LEFT SIDE INBD TRACK FOR THE INBD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE FWD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBD AND OUTBD SIDES OF THE TRACK. THE HOLES WERE REPAIRED IN ACCORDANCE WITH FAA APPROVAL LETTER 95-120S-34. 2L73 4F A3WE 19950210001451995021000145NM 1995 2 10 DL72L950498 119950103A71105930645505 NOSE COWL BOEING727 727232 1384082NM ENGINE WORN AND BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 DURING SHOP INSPECTION, FOUND PREVIOUS REPAIR DAMAGED AT THE EIGHT O'CLOCK POSITION ON ENGINE NOSE COWL. REPAIRED DAMAGE AS PER SRM 54-10-3. 2L73 4F A3WE 19950210001461995021000146NM 1995 2 10 DL72L950511 119950202A711065196854539 SKIN BOEING727 727232 1384082NM NR 1 ENG COWL PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 651 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL OUTER SKIN WAS FOUND WITH PUNCTURE DAMAGE AT 7 O'CLOCK POSITION. REPAIRED PER SRM 54-30-3. 2L73 4F A3WE 19950210001491995021000149NM 1995 2 10 DL72S950449 119950201A5320 DOOR FRAME BOEING727 727232 1384082NM SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, .5 INCH CRACK EXTENDING FROM LOWER AFT STOP CASTING IN FWD SVC DOOR FRAME REPAIRED PER M/M 52-12-0. 2L73 4F A3WE 19950210001501995021000150NM 1995 2 10 DL72S950450 119950118A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 1050 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION ON BEAM TOP/BOTTOM AT STA 1050 BETWEEN LEFT INBOARD AND LEFT O/B SEAT TRACK REPAIRED PER M/M 53-20-11 PG 802. 2L73 4F A3WE 19950210001511995021000151NM 1995 2 10 DL72S950451 119950131A5720 STIFFENER BOEING727 727232 1384082NM FWD SPAR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 FOUND ON F1 LETTER CHECK, 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 6 SLAT OUTBD TRACK INBD ANGLE LOWER END, REPAIR. INSTALLED NEW ANGLE PER M/M 57-20-21 PG 813. 2L73 4F A3WE 19950210001521995021000152NM 1995 2 10 DL72S950455 119950131A5720 STIFFENER BOEING727 727232 1384082NM RT FWD SPAR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 FOUND ON F1 LETTER CHECK 1. 2 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK INBD ANGLE LOWER END 2. 1 .5 INCH CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NR 7 SLAT OUTBD TRACK OUTBD ANGLE LOWER END, REPAIR - 1. REPLACED STIFFENER PER M/M 57-20-21. 2L73 4F A3WE 19950210001531995021000153NM 1995 2 10 DL72S950459 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 1030-1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION ON LEFT O/B SEAT TRACK BETWEEN STA 1030 AND 1050 BOTH SIDES OF TRACK, REPAIR. REPLACED SEAT TRACK SECTION PER CVSRM 53-10-5. 2L73 4F A3WE 19950210001541995021000154NM 1995 2 10 DL72S950460 119950118A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION TOP OF FLOOR BEAM STA 1030 AT CENTER LINE, REPAIR. FABRICATED AND INSTALLED SEC OF T CAP PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950210001551995021000155NM 1995 2 10 DL72S950461 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 1110-1130 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION FOUND SEAT TRACK LOCATED AT LBL 25 BETWEEN 1130 AND 1110, REPAIR. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 3. 2L73 4F A3WE 19950210001561995021000156NM 1995 2 10 DL72S950462 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 1090-1036 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORRROSION FOUND SEAT TRACK RBL 45 BETWEEN 1090 AND 1136 TOP AND BOTTOM SIDES, REPAIR. REPLACED SEAT TRACK FROM 1110 TO 1136 PER SRM 53-10-3 FIG 7. 2L73 4F A3WE 19950210001571995021000157NM 1995 2 10 DL72S950463 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 380-480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION SEVERAL PLACES ON RT I/B SEAT TRACK RBL 23 FROM STA 380 - 480, REPAIR. REPLACED SEAT TRACK SECTION FROM STA 380 TO 440 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950210001581995021000158NM 1995 2 10 DL72S950469 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 420 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK O/B RT STA 420-445, REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950210001591995021000159NM 1995 2 10 DL72S950470 119950118A5347 SEAT TRACK BOEING727 727232 1384082NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK STA 344. REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950210001601995021000160NM 1995 2 10 DL72S950471 119950119A5311 FORMER BOEING727 727232 1384082NM FS 600 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK TPAMM, 1 INCH CRACK FORMER UP RADIUS STA 600, REPAIRED PER SRM 53-10-4 FIG 21. 2L73 4F A3WE 19950210001611995021000161NM 1995 2 10 DL72S950473 119950120A5347 SEAT TRACK BOEING727 727232 1384082NM BS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK TPAMM, CORROSION ON SEATTRACK BS 380 RBL48. REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950210001621995021000162NM 1995 2 10 DL72S950474 119950120A5347 SEAT TRACK BOEING727 727232 1384082NM FS 1033 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK TPAMM, LEFT INBD SEAT TRACK CRACKED STA 1033. REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950210001631995021000163NM 1995 2 10 DL72S950475 119950123A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK TPAMM, CORROSION ON FLOOR BEAM STA 1030. REPAIRED PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950210001641995021000164NM 1995 2 10 DL72S950476 119950123A5320 HORIZ WALKWAY BOEING727 727232 1384082NM FS 303.9 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 FOUND ON CV2 CHECK TPAMM, OUTBOARD LEG OF LEFT NLG HORIZONTAL WALKWAY CORRODED STA 303.9. REPAIRED PER SRM 53-10-4 AND ERA 303065-14. 2L73 4F A3WE 19950210001651995021000165NM 1995 2 10 DL72S950477 119950202A5320 CLIP BOEING727 727232 1384082NM FS 950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FS 950A FRAME TO SKIN SHEAR TIE CRACKED BETWEEN STRINGERS 28-27R. REPAIRED PER MM 53-11-0 FIG 815. 2L73 4F A3WE 19950210001661995021000166NM 1995 2 10 DL72S950478 119950202A5320 CLIP BOEING727 727232 1384082NM FS 980 BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FS 980 FRAME TO SKIN CLIP CRACKED BETWEEN STRINGERS 29R AND 30. REPAIRED PER MM 53-11-0 FIG 815. 2L73 4F A3WE 19950210001671995021000167NM 1995 2 10 DL72S950480 119950201A5320651751737 AFT TRNVRSE BEAM BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11539DA 22385 DURING ROUTINE INSPECTION AT LETTER CHECK, THE RT TORQUE BOX HAD STIFFENERS CRACKED AT FS 1263. IN ACCORDANCE WITH B727 S/B 53-0129, REV 4, THE PART WAS REPLACED. 2L73 4F A3WE 19950210001681995021000168NM 1995 2 10 DL72S950488 119950131A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND CRACK IN LOWER SKIN PANEL OF LEFT WING OUTBOARD AILERON. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950210001691995021000169NM 1995 2 10 DL72S950495 119950202A5320 CLIP BOEING727 727232 1384082NM FS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FS 950F FRAME TO SKIN SHEAR TIE CORRODED AT STRINGER 29R. REPAIRED PER MM 53-11-0 FIG 815. 2L73 4F A3WE 19950210001701995021000170NM 1995 2 10 DL72S950496 119950203A5320 WEB BOEING727 727232 1384082NM FS 1290-1330 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND ON LETTER CHECK, LIGHTNING HOLES DAMAGED LEFT AT STA 1290 1330 IN STAIR WELL VERTICAL WEB, REPAIR. INSTALLED DOUBLER AT STA 1330 PER M/M 53-11-0. 2L73 4F A3WE 19950210001711995021000171NM 1995 2 10 DL72S950497 119950203A5754 COVER BOEING727 727232 1384082NM LE SLAT TRACK CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND ON LETTER CK -1. .5 IN CRACK ON NR 5 L/E SLAT I/B TRACK COVER SKIN - 2. .5 IN CRACK ON NR 6 L/E SLAT I/B TRACK COVER SKIN - 1. AND 2. REPAIRED PER M/M 57-54-0 PG 820. 2L73 4F A3WE 19950210001721995021000172NM 1995 2 10 DL72S950499 119950201A5713 STRINGER BOEING727 727232 1384082NM WS 656 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND RT WING WS 656 STRINGER 11 ABOVE TANK PLATE CRACKED. REPAIRED PER M/M 57-13-0 FIG 804. 2L73 4F A3WE 19950210001731995021000173NM 1995 2 10 DL72S950500 119950131A5753 HINGE BUSHING BOEING727 727232 1384082NM NR 5 FLAP TRACK LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND NR 5 FLAP TRACK, FWD BUSHING HINGE FOR STRUT DOOR BUSHING IS LOOSE AND WORKING IN BORE, REPAIRED PER M/M 57-43-0 FIG 804. 2L73 4F A3WE 19950210001741995021000174NM 1995 2 10 DL72S950501 119950202A5320 CLIP BOEING727 727232 1384082NM FS 1050 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND SKIN CLIP CRACKED AT FS 1050 BETWEEN STR 30 AND 29L, REPAIRED PER M/M 53-11-0 FIG 815. 2L73 4F A3WE 19950210001751995021000175NM 1995 2 10 DL72S950502 119950203A5754 FLAP BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND ON LETTER CHECK, 1 IN CRACK I/B END OF NR 6 L/E FLAP, REPAIR. INSTALLED DOUBLER PER M/M 57-53-0 PG 804. 2L73 4F A3WE 19950210001761995021000176NM 1995 2 10 DL72W950464 119950201A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, STR 9 LEFT INSIDE VERT STAB AT FIN STA 110 CRACKED. REPAIRED PER MM 55-30-0 PG 803 FIG 803. 2L73 4F A3WE 19950210001771995021000177NM 1995 2 10 DL72W950465 119950201A5531 RIB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND RIB CHORD CRACKED AT FIN STA 110 AT STR 10 LEFT. REPAIRED PER MM 55-30-0 PG 802. 2L73 4F A3WE 19950210001781995021000178NM 1995 2 10 DL72W950482 119950124A5313 STRINGER BOEING727 727247 138408FNM FS 675 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV, FOUND CORROSION DAMAGE TO STRINGER 27R AT FS 675 TO FS 684. REMOVED SECTION OF DAMAGED STRINGER AND REPAIRED PER SRM 53-10-3 FIG 1. FUSELAGE SKIN WAS ALSO FOUND DAMAGED AT THIS LOCATION, CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A. 2L73 4F A3WE 19950210001791995021000179NM 1995 2 10 DL72W950483 119950125A5754 FITTING BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV, LEFT WING NR 4 SLAT WAS FOUND WITH THE INBOARD AND OUTBOARD SLAT ACTUATOR FITTING SUPPORT RIB DOUBLERS CRACKED AT THE LOWER FORWARD FLANGE RADIUS. REPAIRED BY INSTALLING NEW DOUBLERS PER MM 57-54-0 PG 805. 2L73 4F A3WE 19950210001801995021000180NM 1995 2 10 DL72W950494 119950124A5313 STRINGER BOEING727 727247 138408FNM FS 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND CORROSION ON STR 30 AFT OF STA 1166. REPAIRED STRINGER PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950210001811995021000181NM 1995 2 10 DL72W950504 119950122A57536521631274A SKIN BOEING727 727247 138408FNM NR 4 FORE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV SHOP INSPECTION, NR 4 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO LEADING EDGE SKIN AT 48 INCHES FROM OUTBOARD END OF FLAP. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950210001821995021000182NM 1995 2 10 DL733950457 119950128A5754 SKIN 65C26602108 BOEING737 737347 1384647NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11307WA 121 23440 AT HMV, NR 5 SLAT LOWER T/E SKIN WAS FOUND CRACKED AT RIVET HEADS ON BOTH SIDES OF SLAT ACTUATOR. REPAIRED PER SRM 57-43-01 FIG 205. 2L72 4F RTA16WE 19950210001831995021000183NM 1995 2 10 DL733950458 119950128A5330 SKIN BOEING737 737347 1384647NM FS 360 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11307WA NA 23440 AT HMV, FOUND FUSELAGE SKIN DENTED AT FS 360 ABOVE STRINGER 19R. REPAIRED PER SRM 53-00 -01 PG 312. 2L72 4F RTA16WE 19950210001841995021000184 1995 2 10 DL73S950489 419950201A3417HG480B42 AIR DATA COMP BOEING737 737232 1384475NM EE COMP FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11315DL 23087 DURING CLIMB-OUT AT 10,000 FT, 32 AIR DATA COMPUTER FAILED. RETURNED ATL. REPLACED ADC OPERATION NORMAL. 2L72 4F RTA16WE 19950210001851995021000185NM 1995 2 10 DL757950404 119950125A5400BACB30NX10K HI-LOCK BOEING757 757232 1384965NM NR 2 PYLON FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 3 FASTENERS LOOSE, 1 FASTENER HAS SHEARED HEAD IN NR 2 PYLON STRUCTURE STA 107.7 AT WL 139.909 (REF DWG 311N3110 SH 1 B-9). 2L72 4F RTA2NM 19950210001871995021000187NM 1995 2 10 DL757950490 119950202A7110 NOSE COWL BOEING757 757232 1384965NM NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11606DL 22813 DURING LETTER CHECK L-1, FOUND NR 1 ENG O/B NOSE COWL DAMAGED. REPAIRED NR 1 ENG O/B NOSE COWL PER SRM 51-70-12 AND PAINTED AREA. 2L72 4F RTA2NM 19950210001881995021000188NM 1995 2 10 DL757950507 119950204A2720 RATIO MODULE 285T0014104 BOEING757 757232 1384965NM RUDDER CONTROL FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11624DL D00199 22914 ON CLIMB-OUT RUDDER RATIO EICAS MSG AND RUDDER RATIO OVERHEAD LIGHT ILLUMINATED WITH UNCOMMANDED RUDDER MOVEMENT. FOUND PCA FAULT BALL SET ON RT RUDDER RATIO MODULE. REPLACED MODULE AND PERFORMED BITE. CKS GOOD. 2L72 4F RTA2NM 19950210001891995021000189NM 1995 2 10 DLM88950466 119950202A2910AS153080254 HOSE DOUG MD88 MD88 3023688NM RT HYD SYS LEAKING A DALAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11954DL 49885 SHORTLY AFTER TAKEOFF USING NORMAL POWER, THE FLIGHT ATTENDANTS REPORTED THE SMELL OF SMOKE THROUGHOUT THE CABIN. FOUND HYD LEAK IN RT SIDE TAIL COMPARTMENT. HOSE MFG NR AS153-08-0254. REPLACED HOSE RETURNED TO SERVICE. 2L72 4F RTA6WE 19950210001901995021000190NM 1995 2 10 DLM88950467 119950202A5311 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11962DL 49981 FOUND DURING E-2 LETTER CHECK, 2.5 INCH CRACK FWD UPPER LEFT WHEEL WELL FRAME. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950210001911995021000191NM 1995 2 10 DLM88950468 119950202A5311 FRAME DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11962DL 49981 FOUND DURING E-2 LETTER CHECK, 2 INCH CRACK IN RIGHT WHEEL WELL FORWARD UPPER FRAME. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950210001921995021000192NM 1995 2 10 DLM88950493 119950201A71105930645505 COWL DOUG MD88 MD88 3023688NM ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11969DL 53172 DURING INITIAL INSPECTION, A DENT WAS FOUND AT THE 9 O/C POSITION ON THE L/E LIP SKIN. THIS DENT WAS REPAIRED PER SRM 54-04A. 2L72 4F RTA6WE 19950210001931995021000193 1995 2 10 MWEA95122 419950204A256513621225 EVAC SLIDE DOUG DC9 DC914 3022034WP TAIL LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 183 45711 DURING INSPECTION, THE TAIL EVACUATION SLIDE PRESSURE WAS FOUND TO BE LOW. REPLACED TAIL EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950210001941995021000194NM 1995 2 10 SWAA950145 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 391, 421, 431, 441, 461, 500A, AND 500A+1, 500B, 500B+1, 530, AT STRINGER 10R. REPAIRED PER TRAMCO EWO 95-0115. 2L72 4F A16WE 19950210001951995021000195NM 1995 2 10 SWAA950146 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 389, 390, 399, 409, 410, 419, 500, 500+9, 500A+10, 500A+19, 500B, 500B+9, 500B+10, 520, 529, 460, 479, 480, 489, 817, 847, 857, 877, 897, 926, 936, 946, AND 956, AT STRINGER 4R. REPAIRED PER TRAMCO EWO 95-0115. 2L72 4F A16WE 19950210001961995021000196NM 1995 2 10 SWAA950147 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 276, 277, 286, 287, 380, 381, 400, 401, 410, 411, 420, 421, 430, 440, 441, 450, 460, 470, 471, 480, 491, 500, 500+10, 500+11, 500A, 500A+1, 500B, 500B+1, AND 510, AT STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0115. 2L72 4F A16WE 19950210001971995021000197NM 1995 2 10 SWAA950148 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM FS 469-500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 469, AND AT 500A+9, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0115. 2L72 4F A16WE 19950210001981995021000198NM 1995 2 10 SWAA950149 119950203A53122024T3 BULKHEAD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178, WL 184, LBL 5.7, PRESSURE BULKHEAD, AT FASTENER HOLES. REPAIRED PER TRAMCO EWO 95-0119. 2L72 4F A16WE 19950210001991995021000199NM 1995 2 10 SWAA950150 119950203A53207075T6511 STIFFENER BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, WL 181-184, LBL 8. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950210002001995021000200NM 1995 2 10 SWAA950151 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 381 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 351, AND 381, STRINGER 14R. REPAIRED PER TRAMCO EWO 95-0115. 2L72 4F A16WE 19950210002011995021000201NM 1995 2 10 SWAA950152 119950203A53302024T3 SKIN BOEING737 7372H4 138448CNM FS 267-328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS FROM BS 267 TO 328, STRINGER 24R, ON BACK SIDE OF EXISTING REPAIR. REMOVED EXISTING REPAIR AND REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950210002021995021000202NM 1995 2 10 UPS402186 119950203A3350 EEL BOEING747 747SR46 NM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS (INCANDESCENT LIGHTS) UNDER THE INST GLARESHIELD ARE BURNED OUT: CAPTAIN'S SIDE 2ND FROM LEFT, CENTER 2ND FROM LEFT, F/U SIDE LEFT MOST BULB. REPLACED BULBS. OPS CHECK GOOD. 2L74 4F A20WE 19950210002031995021000203WP 1995 2 10 UPS802182 119950206A53134645397501 LONGERON DOUG DC8 DC871F 302199DWP FS 1560 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION ON LONGERON 31L, FS 1560. INSTALLED REPAIR IAW UPS EO DC8-5310-6606-A. 2L74 4F RT4A25 19950210002041995021000204WP 1995 2 10 UPS802183 119950206A5330577331153 SKIN DOUBLER DOUG DC8 DC871F 302199DWP FS 1600 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK, MAINTENANCE FOUND SKIN DOUBLER HEAVY CORROSION UNDER SHEAR TIE, FS 1600, LONGERON 28R. INSTALLED REPAIR IAW UPS EO DC8-53-1310 (MINOR). 2L74 4F RT4A25 19950210002051995021000205WP 1995 2 10 UPS802184 119950206A53115772958 FRAME DOUG DC8 DC871F 302199DWP FS 1360-1340 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION ON FRAME, FS 1360-1340, BELOW LONGERON 21R. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2. 2L74 4F RT4A25 19950210002061995021000206WP 1995 2 10 UPS802185 119950206A532037502571 FITTING DOUG DC8 DC871F 302199DWP FS 610 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING 'C' CHECK, MAINTENANCE FOUND LONGERON SPLICE FITTINGS 2 EACH CRACKED AT FS 610, LONGERONS 31L AND 31R. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210002071995021000207WP 1995 2 10 UPS802187 119950204A3350 EEL DISARM DOUG DC8 DC871F 302199DWP FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01772UP 46072 DURING POST FLIGHT CHECK, MAINTENANCE FOUND EMER DISARM CHECK INOP. SECURED OVERHEAD PANEL CAMLOCS (2 EACH) EMER DISARM CHECK. CHECKS NORMAL. EMER LIGHTS, OPS CK NORMAL. 2L74 4F RT4A25 19950210002321995021000232CE 1995 2 10 BUHA95001 119950207A555351310244 FITTING CESSNA402 402C 207590RCE VERTICAL STAB CORRODED AS BUHAK NONE O OTHER ININSP/MAINT 1 GL23160PB 11858 402C0493 VERTICAL STABILIZER FORWARD SPAR ATTACH FITTING AT FUSELAGE, FOUND CORRODED. (X) 1L72 3O A7CE 19950210002931995021000293SO 1995 2 10 95ZZZX697 219950126A7414S6RN25 IMPULSE COUPLING CESSNA207 207A 2073604CE CONT O520 IO520F 17032SO RT MAG BROKEN A ABAJAK NONE ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS ININSP/MAINT 1 AL019942M 4021148 20700756 291045R DURING ENGINE RUN-UP, PILOT REPORTED EXCESSIVE RPM DROP OF RT MAGNETO AND ALSO NO VACUUM. AN INVESTIGATION REVEALED THE REAR MAGNETO BEARING FROZE AND THE IMPULSE COUPLING BROKE OFF AND DESTROYED DRIVE GEAR THAT RUNS THE VACUUM PUMP AND THE REAR ACCESSORY CASE WAS CRACKED. OUTSIDE AIR TEMP WAS MINUS 28 DEGREES CELCIUS AND FURTHER INVESTIGATION FOUND THE TANNIS ENGINE HEATER WAS NOT PLUGGED IN. 1H71 3O3 O A16CE E5CE 19950210002941995021000294EU 1995 2 10 95ZZZZ39 119950123A27307227279541 CABLES SAAB SF340 340B 7860101EU FS 389 CHAFED H AY55K NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FUSELAGE STATION 389.0. CABLE DIAMETER ORIGINALLY IS .163 INCH, MEASURED DIAMETER AT CHAFED AREA IS .140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950210002951995021000295EU 1995 2 10 95ZZZZ40 119950123A27307227279542 CABLES SAAB SF340 340B 7860101EU FS 389 CHAFED H AY55K NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FUSELAGE STATION 389.0. CABLE DIAMETER ORIGINALLY IS .163 INCH, MEASURED DIAMETER AT CHAFED AREA IS .140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950210002961995021000296SW 1995 2 10 95ZZZZ41 119950109A52102724004017 SHAFT SWRNGNSA227 SA227AC 8780603SW CABIN DOOR DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL152692P AC658B FLT 3032 - IN CRUISE FLIGHT FROM DTW, THE CABIN DOOR LIGHT ILLUMINATED IN FLIGHT. THE CREW REDUCED THE CABIN DIFFERENTIAL PRESSURE TO ZERO AND THE LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE PASSENGER DOOR HANDLE U-JOINT, P/N MS 20271B10, AND SHAFT, P/N 27-24004-017. SYSTEM OPERATED SATISFACTORILY. REFERENCE MALA954235. 1L72 4T A8SW 19950210002971995021000297SO 1995 2 10 95ZZZZ42 119950115A3246GY5187C35 BOLT GOODYEAR 95610619 GULSTMG1159 G1159 3953505SO NR 3 WHEEL BROKEN A AKKYAK NONE O OTHER ININSP/MAINT 1 NE03220FL APR81688 50 DURING POST FLIGHT INSPECTION, MAINTENANCE FOUND TWO BOLTS BROKEN ON THE RT INBOARD WHEEL. THE FLIGHT CREW INDICATED THAT ALL OPERATIONS HAD BEEN NORMAL. THESE BOLTS HAD 357 LANDING SINCE NDT. 2L72 4F RTA12EA 19950210002981995021000298WP 1995 2 10 95ZZZZ43 119950122A335020131A EEL BATT PACK DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19914VJ 47068 PIT - THE FLOOR LEVEL EMERGENCY EXIT LIGHTS FROM ROW C FORWARD DO NOT TEST. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK AND REPAIRED A BROKEN WIRE. OPERATIONS CHECKED GOOD. REFERENCE NR USAA950033. 2L72 4F A6WE 19950210003001995021000300NM 1995 2 10 AWXA9500043 219950120A7261AW7270007 INSERT BOEING737 737275 1384485NM PWA JT8 JT8D* NE NR 1 ENG GEAR BXWORN THREADS A AWXAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP282FOR 20922 LAS-ELP - FLT 976 - AIR TURNBACK - ON CLIMB-OUT AIRCRAFT LOST NR 1 ENGINE OIL PRESSURE. CREW SHUT ENGINE DOWN AND RETURNED TO LAS WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND STRIPPED THREADS ON BANJO FITTING OF GEAR BOX, JUST ABOVE THE MAIN OIL FILTER. MAINTENANCE REMOVED AND REPLACED FITTING LP5 BOSS AND BANJO FITTING. LEAK CHECK ON RUNUP NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F4 F A16WE E2EA 19950210003011995021000301NM 1995 2 10 AWXA9500044 119950124A53156546816 FLOOR BEAM BOEING737 7372M8 1384483NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28141AW 21955 PHX - DURING SCHEDULED INSPECTION, FOUND BS 967 RBL 27 BEAM UPPER CHORD LOWER SURFACE CORRODED BEYOND CLEAN UP LIMITS AT A PREVIOUSLY REPAIRED LOCATION. REMOVED UPPER CHORD REPAIR STRAP AND INTERCOSTAL, AND INSTALLED NEW FILLER AND STRAP PER SRM 53-10-9, FIG 2 AND BOEING TELEX AMW PHX 93-0275 RR AUTHORIZING ER 2-53-16-37A. (Z) 2L72 4F A16WE 19950210003021995021000302NM 1995 2 10 AWXA9500057 119950124A3350900835A EEL BATT PACK BOEING737 7372M8 1384483NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F A16WE 19950210003031995021000303EU 1995 2 10 AWXA9500058 119950127A3260848401 SENSOR AIRBUS320 A320231 3930325EU RT MLG DOOR INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28622AW 980 054 PHX-MKE - FLT 1956 - AIR TURNBACK - RIGHT MAIN GEAR DOOR DID NOT INDICATE UP AND LOCKED. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND RT GEAR DOOR PROXIMITY SENSOR '26GA' INTERMITTENT. MAINTENANCE REMOVED AND REPLACED NR 2 RT MLG DOOR UPLOCK PROXIMITY SWITCH PER MM 32-31-73. PERFORMED NR 1 AND NR 2 LGCIU BITE TEST, BOTH SYSTEMS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA28NM 19950210003041995021000304SW 1995 2 10 MALA954225 119950103A32301K5B373110B TQ TUBE BUSHING SWRNGNSA227 SA227AC 8780603SW NLG CORRODED A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15436MA AC719 FLT 3234 - IN CRUISE FLIGHT TO MSP, THE NOSE LANDING GEAR BEGAN TO CYCLE. THE CREW CYCLED THE GEAR BUT THE GEAR CONTINUED TO CYCLE. THE CREW CONTINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE REPLACED THE NLG UPLOCK TORQUE TUBE BUSHINGS. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003051995021000305SW 1995 2 10 MALA954226 119950105A32602752021003 SW ACTUATORS SWRNGNSA227 SA227AC 8780603SW NLG BENT A MALAK NONE N FALSE WARNING CRCRUISE 1 GL15436MA AC719 FLT 3306 - IN CRUISE FLIGHT TO MSP, THE NOSE GEAR BEGAN TO CYCLE. THE CREW CYCLED THE GEAR BUT THE GEAR CONTINUED TO CYCLE. THE AIRCRAFT CONTINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE REPLACED THE UPLOCK SWITCH ACTUATORS. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003061995021000306SW 1995 2 10 MALA954228 119950103A32601EN516 UPLOCK SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAK NONE N FALSE WARNING CLCLIMB 1 GL15422MA AC635 FLT NR 3038 - DURING CLIMB-OUT FROM CAK, THE NOSE GEAR BEGAN TO CYCLE. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK LIMIT AND POSITION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003071995021000307SW 1995 2 10 MALA954232 119950106A3411 PITOT SYSTEM SWRNGNSA227 SA227AC 8780603SW LT/RT REQ'D SERVICE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15434MA AC717 FLT NR 3094 - ON CLIMB-OUT FROM DTW, THE CAPTAINS AIRSPEED INDICATOR BEGAN TO DROP. DURING THE CLIMB THE FIRST OFFICERS AIRSPEED INDICATOR ALSO BEGAN TO DROP. THE CREW SELECTED PITOT HEAT ONLY ON BOTH SIDES AND BOTH AIRSPEEDS CAME BACK TO NORMAL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE EITHER DISCREPANCY. THE CAPTAINS AND FIRST OFFICERS PITOT/STATIC SYSTEMS WERE PURGED. SYSTEMS OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003081995021000308SW 1995 2 10 MALA954233 119950107A32601EN516 UPLOCK SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15423MA AC636 FLT NR 3496 - ON APPROACH TO MSP, THE NOSE GEAR INTRANSIT LIGHT AND DOWN AND LOCKED LIGHT WAS SLOW TO ILLUMINATE. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED THE NOSE GEARS LEFT UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003091995021000309SW 1995 2 10 MALA954234 119950110A3260JG2A LIGHT RELAY SWRNGNSA227 SA227AC 8780603SW LANDING GEAR INOP A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15425MA AC640 FLT 3074 - ON APPROACH TO MSP, THE GEAR DOOR POSITION LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS DOWN AND LOCKED. MAINTENANCE REPLACED A RELAY. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003101995021000310SW 1995 2 10 MALA954235 119950109A5210MS20271B10 U-JOINT SWRNGNSA227 SA227AC 8780603SW CABIN DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL152692P AC658B FLT 3032 - IN CRUISE FLIGHT FROM DTW, THE CABIN DOOR LIGHT ILLUMINATED IN FLIGHT. THE CREW REDUCED THE CABIN DIFFERENTIAL PRESSURE TO ZERO AND THE LIGHT EXTINGUISHED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE PASSENGER DOOR HANDLE U-JOINT, P/N MS 20271B10, AND SHAFT, P/N 27-24004-017. SYSTEM OPERATED SATISFACTORILY. REFERENCE 95ZZZZ41. 1L72 4T A8SW 19950210003111995021000311SW 1995 2 10 MALA954237 119950111A5753273114101 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, THE RIGHT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED IAW FAC MM PAGES 201-202. (Z) 1L72 4T A8SW 19950210003121995021000312SW 1995 2 10 MALA954238 119950111A5753273114101 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED THROUGH A PART FOR PART REPLACEMENT OF THE DOUBLER IAW FAC SRM 57-90-10 PAGES 45 AND 46 AND ARP 57-20-9424. (Z) 1L72 4T A8SW 19950210003131995021000313NM 1995 2 10 MALA954240 119950112A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15833MA 343 FLT 3033 - DURING THE POST FLIGHT IN DTW, THE COCKPIT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950210003141995021000314SW 1995 2 10 MALA954242 119950113A32601EN516 POSITION SWRNGNSA227 SA227AC 8780603SW NLG WW INTERNAL FAULT A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1527465 AC755B FLT 3495 - AFTER TAKEOFF FROM MSP, THE RED NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR RETRACTION. THE BULB TESTED GOOD. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NOSE LANDING GEAR POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003151995021000315SW 1995 2 10 MALA954244 119950116A32601EN516 DNLOCK SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15428MA AC646 FLT 3240 - ON APPROACH TO MSP, THE RIGHT GEAR DID NOT INDICATE DOWN AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR AND THE INDICATION LIGHT WAS SLOW TO ILLUMINATE. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MSP. MAINTENANCE REPLACED THE INBOARD DOWN AND LOCKED SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950210003161995021000316NM 1995 2 10 MALA954245 119950117A33506004781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15853MA 353 FLT 3051 - UPON POWER UP IN DAY FOR THE FIRST FLIGHT OF THE DAY, THE EMERGENCY LIGHTS WERE INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950210003311995021000331EU 1995 2 10 USAA950017 119950116A3260 DNLOCK SENSOR FOKKERF28 F28MK0100 4990807EU RT MLG INTERMITTENT A USAAK NONE N FALSE WARNING APAPPROACH 1 EA19885US 11345 CLT - FLT NR 1095 - ON FINAL APPROACH, CREW GOT 3 GREEN LIGHTS ON THE GEAR BUT ALSO GOT A LIGHT IN THE GEAR HANDLE AND RT MLG NOT LOCKED ON MULTI FUNCTION DISPLAY UNIT. CYCLED GEAR. ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED RT MLG PRIMARY DOWNLOCK SENSOR OVER-SENSING. REPLACED SENSOR IAW MM 32-61-03-400-814A AND CONFIRMED CORRECT ADJ PER MM 32-61-03-820-815A. LANDING GEAR POSITION INDICATION SYSTEM OPERATIONAL NORMAL. (Z) 2L72 4F RT 19950210003321995021000332NM 1995 2 10 USAA950018 119950115A3231 CONTROL CABLE BOEING727 727214 138407RNM LT NLG BROKEN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19750US 21512 SJU - FLT 0396 - DURING GEAR RETRACTION, A LOUD NOISE WAS HEARD FROM THE NOSE GEAR. THE NOSE GEAR DOOR L/E ANNUNCIATOR PANEL LIGHT REMAINED ILLUMINATED. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR CABLE BROKEN. THEY REPLACED BOTH GEAR DOOR CABLES. (Z) 2L73 4F A3WE 19950210003331995021000333WP 1995 2 10 USAA950019 119950112A3260 SWITCH DOUG DC9 DC931 3022065WP LT MLG OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19921VJ 48141 PHL - FLT 1735 - AFTER TAKEOFF, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE CREW DECIDED TO RETURN TO PHL. MAINTENANCE ADJUSTED THE NOSE GEAR UPLOCK PROXIMITY SWITCH. OPERATIONS CHECKED NORMAL. (Z) 2L72 4F A6WE 19950210003341995021000334WP 1995 2 10 USAA950020 119950111A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19822US 49139 LGA - FLT 2236 - THE CABIN FLOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONS CHECKED NORMAL. (Z) 2L72 4F A6WE 19950210003351995021000335EU 1995 2 10 USAA950021 119950116A3230201218005 DOWNLOCK ACT FOKKERF28 F28MK1000 4990808EU LT MLG MALFUNCTIONED A USAAK NONE J WARNING INDICATION APAPPROACH 1 EA19868US 11313 PHL - FLT NR 183 - ON FINAL APPROACH, CREW COULD NOT GET 3 GREEN LIGHTS ON THE GEAR. THE LEFT MAIN GEAR LIGHT TESTED BUT WOULD NOT ILLUMINATE. CYCLED GEAR, THEN AN INTERMITTENT LEFT LANDING GEAR DOWNLOCK SWITCH LIGHT ON MULTIFUNCTION DISPLAY UNIT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR DOWNLOCK ACTUATOR AND RIGGED PER MM. (Z) 2L72 4F RTA20EU 19950210003361995021000336NM 1995 2 10 USAA950026 119950113A335020121 EEL BATT CHARGER BOEING737 737301 1384611NM COCKPIT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19573US 23560 PHL - COCKPIT EMERGENCY EXIT DOES NOT LIGHT WHEN TESTED. MAINTENANCE REPLACED CHARGER ASSEMBLY. EMERGENCY LIGHTS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950210003371995021000337NM 1995 2 10 USAA950029 119950115A33501000679 EEL BOEING737 737201 1384454NM COCKPIT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19237US 22353 PHL - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (Z) 2L72 4F A16WE 19950210003381995021000338NM 1995 2 10 USAA950031 119950118A3350 EEL BOEING737 7373B7 1384580NM CABIN MISSING A USAAK NONE L NO TEST ININSP/MAINT 1 EA19525AU 23860 PHL - FLT 2338 - FLOOR EMERGENCY TRACK LIGHTING AT ROW 3 HAS LENS AND LIGHT MISSING. MAINTENANCE REPLACED LIGHT AND LENS. (Z) 2L72 4F RTA16WE 19950210003391995021000339NM 1995 2 10 USAA950032 119950122A2420948F4582 GCU BOEING737 737301 1384611NM NR 1 FAILED A USAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19563AU 23551 IND - FLIGHT EN ROUTE PIT TO PHX WHEN NR 1 GENERATOR DROPPED OFF LINE, FOLLOWED BY APU OPERATING INTERMITTENTLY THE SHUTTING DOWN. FLIGHT DIVERTED TO IND WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BENT PIN NR 2213 ON NR 1 ENGINE GCU. REPLACED GCU. (Z) 2L72 4F RTA16WE 19950210003401995021000340WP 1995 2 10 USAA950033 119950122A3350RPS1B EEL BATT CHARGER DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19914VJ 47068 PIT - THE FLOOR LEVEL EMERGENCY EXIT LIGHTS FROM ROW C FORWARD DO NOT TEST. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK AND REPAIRED A BROKEN WIRE. OPERATIONS CHECKED GOOD. REFERENCE NR 95ZZZZ43. 2L72 4F A6WE 19950210003411995021000341WP 1995 2 10 USAA950034 119950117A335060030451LB EEL BATT PACK DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19995VJ 47334 PIT - THE AFT CABIN EMERGENCY LIGHTS WRE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950210003421995021000342 1995 2 10 USAA950035 419950120A34546223255009 VOR RECEIVER DOUG DC9 DC931 3022065WP NR 1 INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19958VJ 47351 CLT - FLT 8028 - THE NR 1 NAV IS 45 PERCENT OFF. IT IS TO TTHE RIGHT OF THE NR 2 NAV. MAINTENANCE REPLACED THE VOR REC SYSTEM. OPERATIONS CHECK GOOD. (Z) 2L72 4F A6WE 19950210003431995021000343WP 1995 2 10 USAA950043 119950125A335020131A EEL BATT PACK DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19993VJ 47332 CLT - FLT 1004 - THE EMERGENCY EXIT LOW LEVEL FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT BATTERY PACK. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950210003441995021000344WP 1995 2 10 95ZZZW59 119950119A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION ON FUSELAGE RT SIDE EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. 2L74 4F 4A25 19950210003451995021000345WP 1995 2 10 95ZZZW60 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 849-869 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 31 HAS CORROSION FROM STA 849 TO 869. 2L73 4F A23WE 19950210003461995021000346WP 1995 2 10 95ZZZW61 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-933 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 32 HAS CORROSION FROM 901 TO 933. 2L73 4F A23WE 19950210003471995021000347WP 1995 2 10 95ZZZW62 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 869-901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 32 HAS CORROSION FROM STATION 869 TO 901. 2L73 4F A23WE 19950210003481995021000348WP 1995 2 10 95ZZZW63 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 943 TO 985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 32 HAS CORROSION FROM STATION 943 TO 985. 2L73 4F A23WE 19950210003491995021000349WP 1995 2 10 95ZZZW64 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-923 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL2 CORROSION - STRINGER NR 33 HAS CORROSION FROM STA 901 TO 923. 2L73 4F A23WE 19950210003501995021000350WP 1995 2 10 95ZZZW65 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 869-901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 34 HAS CORROSION FROM STA 869 TO 901. 2L73 4F A23WE 19950210003511995021000351WP 1995 2 10 95ZZZW66 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 943-985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 34 HAS CORROSION FROM STA 943 TO 985. 2L73 4F A23WE 19950210003521995021000352WP 1995 2 10 95ZZZW67 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 923-985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 33 HAS CORROSION FROM 923 TO 985. 2L73 4F A23WE 19950210003531995021000353WP 1995 2 10 95ZZZW68 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 809-849 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 34 HAS CORROSION FROM 809 TO 849. 2L73 4F A23WE 19950210003541995021000354WP 1995 2 10 95ZZZW69 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-943 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 34 HAS CORROSION FROM STA 901 TO 943. 2L73 4F A23WE 19950210003551995021000355WP 1995 2 10 95ZZZW70 119950119A5313 STRINGER LKHEED1011 10113851 5265010WP FS 960 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19762BE 193P1070 LEVEL 2 CORROSION - STA 960 LOWER AREA AT STRINGER 33 SEVERAL RIVET HEADS MISSING. 2L73 4F A23WE 19950210003561995021000356WP 1995 2 10 95ZZZW71 119950119A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - RT WING LEADING EDGE AT NR 3 AUX FUEL TANK HAS BULGING CORROSION. 2L74 4F 4A25 19950210003571995021000357WP 1995 2 10 95ZZZW72 119950119A5730 SKIN DOUG DC8 DC862 3021970WP WS 454-485 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - RT WING SKIN FROM STA 454 TO 485 HAS CORROSION. 2L74 4F 4A25 19950210003581995021000358WP 1995 2 10 95ZZZW74 119950119A5730 SKIN DOUG DC8 DC862 3021970WP WS 291.5-310.25 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - RT WING LE STA 291.5 TO 310.25 HAS BULGING CORROSION. 2L74 4F 4A25 19950210003591995021000359WP 1995 2 10 95ZZZW76 119950111A5711 SPAR DOUG DC8 DC862 3021970WP RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - ON RT WING NR 3 AUX TANK LOWER SURFACE FRONT SPAR ATTACH FLANGE HAS AREAS OF BULGING. 2L74 4F 4A25 19950210003601995021000360WP 1995 2 10 95ZZZW77 119950111A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORROSION A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - ON RT WING LE O/B OF NR 4 ENG BULGING CORROSION AROUND SCREW HEADS. 2L74 4F 4A25 19950210003611995021000361WP 1995 2 10 95ZZZW78 119950111A5730 PANEL DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - ON RT WING LE UPPER SURFACE PANEL AFT OF O/B END OF O/B SLOT HAS CORROSION AROUND SCREW HEADS. 2L74 4F 4A25 19950210003621995021000362WP 1995 2 10 95ZZZW79 119950111A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1340 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - IN AFT CARGO COMPARTMENT, CIRCUMFERENTIAL LOWER FLANGE AND VERTICAL SIDEWALL SUPPORT ARE CORRODED AT BS 1340R BETWEEN LONGERONS 27R AND 26R. 2L74 4F 4A25 19950210003641995021000364WP 1995 2 10 95ZZZW81 119950124A5313 STRINGER LKHEED1011 10113851 5265010WP FS 809-829 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 1004 LEVEL 2 CORROSION - STRINGER NR 32 HAS CORROSION BETWEEN STA 809 AND 829. 2L73 4F A23WE 19950210003661995021000366EU 1995 2 10 95ZZZW83 119950110A323071540 SEQUENCING VLV FOKKERF28 F28MK4000 4990810EU NLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19481US 11230 SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07. LEAK AND OPERATION CHECKS NORMAL. REF USAA950011. 2L72 4F RTA20EU 19950210003671995021000367WP 1995 2 10 95ZZZW84 119950101A5320 CIRCUMFERENTIAL DOUG DC8 DC862 3021970WP BS 1140 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - AFT CARGO COMPARTMENT AT BS 1140 LONGERON 33R CIRCUMFERENTIAL IS CORRODED AT CENTER OF DOORWAY. 2L74 4F 4A25 19950210003681995021000368NM 1995 2 10 IXKA9500002 119950119A3260 LIGHT SWITCH BOEING727 727230 1384080NM TAIL SKID DIRTY A IXKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25357KP 20675 EWR - FLT 4001 - AFTER TAKEOFF, THE TAIL SKID LIGHT REMAINED ON. RECYCLED GEARS, LIGHT STILL ON. RETURNED TO EWR. CLEANED MOISTURE, OIL AND CORROSION FROM SWITCHES. OPERATED TAIL SKID SEVERAL TIMES AND VERTIFIED OPERATION PER MM 32-61-01, NO DEFECTS NOTED. (W) 2L73 4F A3WE 19950210003691995021000369SW 1995 2 10 MALA954227 119950103A26121734361450 FIRE DETECTOR SWRNGNSA227 SA227AC 8780603SW LT ENGINE INTERMITTENT A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15428MA AC646 DTW - FLT 3341 - DURING CLIMBOUT, THE LT ENGINE FIRE LIGHT ILLUMINATED FOR 10 TO 15 SECONDS. ALL ENGINE PARAMETERS NORMAL. THE ACFT RETURNED TO DTW. MAINTENANCE REPLACED THE 450 DEGREES FIRE DETECTOR. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950210003701995021000370SW 1995 2 10 MALA954229 119950105A7714 RPM GAUGE SWRNGNSA227 SA227AC 8780603SW LT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15421MA AC634 LNK - FLT 3222 - IN CRUISE, THE LT RPM GAUGE BEGAN TO FLUCTUATE. NO OTHER ENGINE FLUCTUATIONS NOTED. THE ACFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950210003711995021000371NM 1995 2 10 MALA954230 119950104A335082410221011 EEL CONTL PANEL DHAV DHC8 DHC8102 2809003NM CABIN FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15817MA 249 DTW - DURING MAINTENANCE, THE EMERGENCY LIGHT SYSTEM WOULD NOT TEST FROM THE COCKPIT SWITCH. REPAIRS WERE COMPLETED BY REPLACING THE FLIGHT ATTENDANT'S CONTROL PANEL. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950210003721995021000372SW 1995 2 10 MALA954231 119950107A52302724050083 UPPER FRAME SWRNGNSA227 SA227AC 8780603SW CARGO DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421MA AC634 DURING ROUTINE MAINTENANCE IN MSP, MAINTENANCE FOUND THE CARGO DOOR UPPER FRAME DENTED. REMOVED FRAME AND INSTALLED NEW FRAME. WORK COMPLETED IAW FAIRCHILD SRM 51-00-00 PG 4 FOR PART REPLACEMENT. (W) 1L72 4T A8SW 19950210003731995021000373SW 1995 2 10 MALA954236 119950107A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG INTERNAL FAULT A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15436MA AC719 MSP - FLT 3219 - ON APPROACH, THE NOSE GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR WAS LOWERED. MAINTENANCE REPLACED THE LT UPPER NOSE GEAR SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950210003741995021000374SW 1995 2 10 MALA954239 119950107A53112722085013 FRAME SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B MSP - DURING ROUTINE MAINTENANCE, FOUND THE CARGO DOOR FRAME CRACKED AT FS 438.060. REPAIRED BY INSTALLING A REPAIR ANGLE AND FILLER PLATE IAW FAIRCHILD LAR 95-MALA-003 DATED 1/4/95. (W) 1L72 4T A8SW 19950210003751995021000375NM 1995 2 10 MALA954241 119950113A540085410025011 EXHAUST SHROUD DHAV DHC8 DHC8102 2809003NM NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15854MA 357 CKB - DURING SCHEDULED INSPECTION, MAINTENANCE NOTED THAT THE RT EXHAUST SHROUD, LT AND RT SIDE SKIN WAS CRACKED AND BUCKLED. REPAIRS WERE COMPLETED IAW WVAC EU-DH8-93-07 REVISION A. (W) 2H72 4T RTA13NM 19950210003761995021000376SW 1995 2 10 MALA954243 119950115A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW RT MLG SLOW A MALAK NONE J WARNING INDICATION APAPPROACH 1 GL15422MA AC635 MSP - FLT 3252 - ON APPROACH, THE RT MAIN GEAR WAS SLOW TO INDICATE DOWN AND LOCKED. THE ACFT LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950210003791995021000379EA 1995 2 10 PAYA95D7001 219950101A72603022375 CARBON SEAL DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA NR 4 ENGINE MISINSTALLED A PAYAE ENGINE SHUTDOWN WJ INADEQUATE Q C WARNING INDICATION APAPPROACH 1 EA17176RA 76 ORF-PNE - FLT 7570 - WHILE ON APPROACH, THE NR 4 ENGINE OIL PRESSURE CAUTION LIGHT ILLUMINATED. CREW SECURED THE ENGINE FOR LANDING. MAINTENANCE FREED AND RESEATED CARBON SEAL. PERFORMED ACTION IAW P AND W MM 72-05-00 PG 629. ENGINE WAS RUNUP FOR EXTENDED DURATION AND LEAK CHECKED GOOD. (W) 2H74 4T4 T A20EA E4EA 19950210003801995021000380EA 1995 2 10 PAYA95D7002 119950104A3230155505 UPLOCK ACT DHAV DHC7 DHC7102 2802708EA LT MLG STICKING A PAYAO OTHER O OTHER APAPPROACH 1 EA17175RA 56 BOX-JFK - FLT 7705 - THE LT MLG WAS SLOW TO EXTEND WITH RT MLG AND NOSE GEAR ALREADY DOWN AND LOCKED. MAINTENANCE REMOVED AND REPLACED THE LT MLG UPLOCK ACTUATOR AND C/W RET/EXT CHECKS IN BOTH NORMAL AND EMERGENCY MODE. CHECKS WERE SATISFACTORY. (W) 2H74 4T A20EA 19950210003811995021000381EU 1995 2 10 USAA950011 119950110A323071539 SELECTOR VLV FOKKERF28 F28MK4000 4990810EU NLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19481US 11230 SYR - FLT 1091 - AFTER GEAR RETRACTION THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR DOOR SELECTOR AND SEQUENCING VALVES PER MM 32-32-06 AND 07. LEAK AND OPERATION CHECKS NORMAL. REF 95ZZZW83. 2L72 4F RTA20EU 19950210003821995021000382WP 1995 2 10 95ZZZW47 119950113A53475277266013500 SEAT TRACK DOUG DC8 DC873F 302199FWP FS 1450 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURING C-CHECK, THE NR 2 SEAT TRACK HAS CORROSION AT STA 14550. REPLACED SEAT TRACK PER DOUGLAS SRM CHAPTER 53. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003831995021000383WP 1995 2 10 95ZZZW48 119950113A5347S27726601350 SEAT TRACK DOUG DC8 DC873F 302199FWP FS 1450-1570 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURING C-CHECK, THE NR 1 SEAT TRACK AT FS 1450-1570 HAS CORROSION. REPLACED SEAT TRACK PER DOUGLAS SRM CHAPTER 53. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003841995021000384WP 1995 2 10 95ZZZW49 119950113A574457568481 ATTACH FITTING DOUG DC8 DC873F 302199FWP TE LT FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURNG C-CHECK, LT WING I/B FLAP O/B ATTACH FITTING CRACK. REPLACED CRACKED ATTACH FITTING PER DOUGLAS SRM CHAPTER 57. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003851995021000385WP 1995 2 10 95ZZZW50 119950113A5744 ATTACH FITTING DOUG DC8 DC873F 302199FWP RT FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURING C-CHECK, I/B LEG OF RT I/B FLAP ATTACH FITTING CRACKED AT STA 97. REWORKED PER DOUGLAS DRAWING 5894377 AND RETURNED TO SERVICE. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003861995021000386WP 1995 2 10 95ZZZW51 119950113A574457511832 ATTACH FITTING DOUG DC8 DC873F 302199FWP RT FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURING C-CHECK, RT WING I/B FLAP O/B ATTACH FITTING CRACKED. REPLACED CRACKED ATTACH FITTING PER DOUGLAS SRM CHAPTER 57. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003871995021000387WP 1995 2 10 95ZZZW52 119950113A5312 HORIZ BEAM DOUG DC8 DC873F 302199FWP AFT PRESS BLKHD CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01805DH61354 46125 DURING C-CEHCK, AFT PRESSURE BULKHEAD THIRD HORIZONTAL BEAM FROM BOTTOM CRACKED AT BL '0' 3 INCHES. REPAIRED PER DOUGLAS SRM CHAPTER 53. TOTAL CYCLES 24057. 2L74 4F RT4A25 19950210003881995021000388NM 1995 2 10 95ZZZW53 119950118A291010605632 HYD HOSE BOEING727 727228 NM NR 1 ENG FAILED A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01722DH 19861 SLOW LEAK IN 'A' SYSTEM, HYD 1.5 GALLONS REMAIN IN RESERVOIR 'B' SYSTEM RESERVOIR FULL. ENGINE NR 2 HYDRAULIC LOW PRESS LIGHT CYCLES ON AND OFF APPROX 1 CYCLE PER MINUTE WITH ENGINE NR 1 'A' HYDRAULIC PUMP SWITCH ASSOCIATED FLUID SHUTOFF SWITCH CLOSED. STANDBY HYDRAULIC RESERVOIR READS EMPTY, STANDBY PUMP GREEN LIGHT OUT WITH STANDBY RUDDER SWITCH ON. REPLACED BLOWN HYDRAULIC PRESS LINE AND STANDBY PUMP/MOTOR ASSY. MM 29-10. 2L73 4F A3WE 19950210003891995021000389WP 1995 2 10 95ZZZW54 119950114A276057184705001 RESERVOIR DOUG DC8 DC873F 302199FWP SPOILER HYD SYS REQD FLUID A DHLACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO01804DH 46124 ON TAKEOFF, SPOILER HYDRAULIC PRESSURE ZERO, PULLING AND RESETTING THE SPOILER HYDRAULIC PUMP CONTROL CIRCUIT BREAKER RESTORED SPOILER HYDRAULIC PRESSURE TO NORMAL. SERVICED SPOILER RESERVOIR AND BLEED SPOILER RESERVOIR. OPS CHECK GOOD ON GROUND, MM 27-60. 2L74 4F RT4A25 19950210003901995021000390NM 1995 2 10 95ZZZW55 119950114A273065989005 RUB BLOCK BOEING727 72782C 1384026NM LT ELEVATOR OUT OF ADJUST A DHLAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01709DH 19968 DURING CONTROL CHECK, MOVING WHEEL FROM FULL FWD TO AFT, THERE IS A VIBRATION AND A FEEL OF BINDING IN ELEVATORS. CAN FEEL SHAKING THROUGH FLOOR OF ACFT. RETURNED TO BLOCKS. ADJUSTED RUB BLOCK ON LT ELEVATOR. IAW BOEING MM 27-30-1. OPS CHECK OK. 2L73 4F A3WE 19950210003911995021000391NM 1995 2 10 95ZZZW56 119950117A783062161 SWITCH BOEING727 72723 1384004NM NR 3 TR UNIT DIRTY A DHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01717DH 19389 THE NR 3 THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. AFTER CLEARING RUNWAY, CYCLED REVERSER. LIGHT WENT OUT. CLEANED CONNECTOR AND SWITCH AT THRUST REVERSER. ALSO, CHECKED THRUST REVERSER FOR DAMAGE. CHECKED GOOD. GROUND RAN, CHECK NORMAL. 2L73 4F A3WE 19950210003951995021000395WP 1995 2 10 BUFA9501 119950106A3231 RETRACT MECH DOUG DC8 DC861 3021952WP NLG DOOR OUT OF ADJUST A BUFAO OTHER E VIBRATION/BUFFET CRCRUISE 1 CE05161DB 45980 MQY - AIR RETURN, FLIGHT LEVEL 330, 0155Z. HEARD AND FELT VIBRATION IN COCKPIT, DESCENT TO FLIGHT LEVEL 190 AND 230 KNOTS, GEAR UP LATCH CHECK, SMALL CHANGE IN VIBRATION. NO WARNING LIGHTS ON, LANDING GEAR LEVER UP. JACKED ACFT AND ACCOMPLISHED NOSE GEAR RETRACTION. FOUND FWD DOOR LT ROD OUT OF ADJUSTMENT. ADJUSTED ROD IAW MM 32-22-1. OPS CHECK AND RII COMPLIED WITH. 2L74 4F 4A25 19950210004051995021000405WP 1995 2 10 USAA950004 119950103A32607000010101 DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP RT MLG INOPERATIVE A USAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 EA19967VJ 47375 ORF - FLT 956 - ON GEAR EXTENSION AT PHF, THE RT MAIN GEAR INDICATED UNSAFE. THE GEAR WAS RECYCLED AND THE INDICATION WAS STILL UNSAFE. THE CAPTAIN MADE A VISUAL INSPECTION WHICH SHOWED OK. THE FLIGHT DIVERTED TO ORF. WHILE MAKING A LOW PASS OVER THE RUNWAY, THE GEAR WAS CONFIRMED TO BE DOWN. MAINTENANCE REPLACED THE RT MAIN GEAR DOWNLOCK SWITCH AND CLEARED THE CONNECTOR. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950210004061995021000406WP 1995 2 10 USAA950006 119950104A2150BACC10DP300B CLAMP DOUG DC9 DC982 3022082WP RT PACK LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19817US 48097 MCO - FLT 2382 - AFTER DEPARTING MCO, CREW RECEIVED AND OVERHEAT INDICATION IN THE TAIL SECTION. THE CREW FOLLOWED EMERGENCY PROCEDURES TO ISOLATE THE PROBLEM. THE LT PACK WAS SHUTDOWN, BUT THE CABIN PRESSURE COULD NOT BE MAINTAINED ON THE RIGHT PACK. THE CREW DECIDED TO RETURN TO MCO. MAINTENANCE REPLACED THE CLAMP ON RT PACK AAV INLET. THE ACFT WAS PRESSURIZED WITH THE RT PACK. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950210004071995021000407WP 1995 2 10 USAA950007 119950103A2130 PRESSURIZATION DOUG DC9 DC982 3022082WP CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19816US 48096 PIT - FLT 431 - AFTER CLIMB TO 10,000 FEET, THE ACFT WOULD NOT PRESSURIZE. THE CREW DECIDED TO RETURN TO PIT. MAINTENANCE PERFORMED A BITE CHECK, INSPECTED THE OUTFLOW VALVE, ACCOMPLISHED AN AUTO PRESSURE CHECK. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950210004081995021000408EU 1995 2 10 USAA950008 119950106A301032899023 SHUT OFF VALVE FOKKERF28 F28MK0100 4990807EU RT WING FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19881US 11333 PIT - FLT 508 - 'THE WING ANTI-ICE CAPACITY' MESSAGE CAME ON WITH THE WING AN TAIL ANTI-ICE TURNED ON. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT HPSOV NOT OPENING COMPLETELY WHEN AIR IS ON. REPLACED THE RT HPSOV. OPERATION CHECKS NORMAL. (W) 2L72 4F RT 19950210004091995021000409NM 1995 2 10 USAA950014 119950108A5730 ACCESS PANEL BOEING737 7373B7 1384580NM NR 1 PYLON LEAKING A USAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 EA19523AU 23858 PIT - FLT 385 - FLIGHT EN ROUTE PHL TO DEN WHEN TOP LT WING OVAL PANEL, ABOVE ENGINE NACELLE SHOWED MINOR SEEPAGE. NO FUEL IMBALANCE NOTED. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED FUEL TANK ACCESS PANEL AFT OF NR 1 PYLON ON TOP OF WING. LEAK CHECK OK. (W) 2L72 4F RTA16WE 19950210004101995021000410NM 1995 2 10 USAA950016 119950110A2781 PROX SWITCH BOEING737 7373B7 1384580NM NR 5 SLAT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19502AU 23377 BWI - FLT 1795 - FLIGHT EN ROUTE, WHEN FWD AMBER LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED. THE NR 5 SLAT FULL EXTEND LIGHT ALSO ON. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 5 LEADING EDGE SLAT PROXIMITY SWITCH, S178. ALL INDICATIONS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950210004111995021000411CE 1995 2 10 95ZZZX664 119950112A2731NAS302661312 TRIM CABLE BEECH 1900 1900D 1154162CE ELEVATOR SEPARATED A GLBAK NONE F FLT CONT AFFECTED APAPPROACH 1 CE01118UX410 UE118 SUPPLEMENTAL SDR - 1-20-95. ISN - ON APPROACH, ELEVATOR TRIM CABLE SNAPPED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE IS INVESTIGATING THE FAULT. IN RE ELEVATOR TRIM TAB CABLE BREAK. MAINTENANCE INSPECTED ENTIRE CABLE RUN AND FOUND THE BROKEN CABLE HAD BEEN RUNNING OVER RATHER THAN UNDER A CABLE GUARD. A NEW CABLE WAS PROPERLY INSTALLED, SEVERAL PRECAUTIONARY INSPECTIONS WERE ACCOMPLIHSED, AND A TEST FLIGHT WAS SATISFACTORY. A SPECIAL INSPECTION OF OUR D-MODEL FLEET FOUND NO DEFECTS. NOTE: A SAFETY COMMINIQUE DATED 1-95 WAS ISSUED BY THE MANUFACTURER. AN AD HAD ALSO BEEN ISSUED CONCERNING THIS ISSUE. 2L72 4T RTA24CE 19950210004121995021000412EA 1995 2 10 95ZZZX665 219950111A7200 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA LEFT FAILED A AOQAO OTHER J WARNING INDICATION APAPPROACH 1 EA112025M 2762 BB384 PCE80823 ON 1-11-95 DURING APPROACH TO ISP, LT ENGINE CHIP DETECTOR WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED WTIHOUT FURTHER INCIDENT. INSPECTION OF CHIP DETECTOR REVEALED A PIECE OF METAL BRIDGED ACROSS CHIP DETECTOR CONTACTS. ENGINE REMOVED FROM SERVICE. TEAR DOWN REPORT WILL FOLLOW. 1L72 4T4 T A24CE E4EA 19950210004151995021000415EU 1995 2 10 95ZZZX668 119950103A3260622800100 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU NLG LACK OF LUB A SABAO OTHER N FALSE WARNING CRCRUISE 1 SO05190PC 750 AIRCRAFT WAS EN ROUTE FROM HUNTINGTON WEST VIRGINIA TO CHARLOTTE, NORTH CAROLINA, PILOT NOTICED A NOSE GEAR GREEN LIGHT INDICATION WITH GEAR IN THE UP AND LOCKED POSITION. PILOT CONTINUED TO DESTINATION AND DECLARED AN EMERGENCY, AIRCRAFT LANDED SAFELY. MAINTENANCE WAS DISPATCHED TO MEET THE AIRCRAFT THE THE TAXI RAMP WHERE THEY PROCEEDED TO PIN THE GEAR IN THE DOWN AND LOCKED POSITION. AFTER EVALUATION IT WAS DETERMINED THE NOSE GEAR SWITCH WAS FROZEN FROM WATER ACCUMULATION, CLEANED, AND LUBED SWITCH, OPS CHECK GOOD. 2L72 4T RTA21EU 19950210004161995021000416WP 1995 2 10 95ZZZX669 119950115A21701808492 COALESCERS DOUG DC9 DC982 3022082WP CABIN CONTAMINATED A ASAAAI UNSCHED LANDING CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01937AS6557 49364 PDX - FLT 506 - AIR TURN BACK. CREW REPORTED SMOKE ODOR IN COCKPIT SHORTLY AFTER TAKEOFF AND LAV SMOKE DETECTOR ACTIVATED. DEPRESSURIZED AIRCRAFT AT 500 FEET AND LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN-UP OF BOTH ENGINES FOR 5 MINUTES WITH BOTH PACKS ON IN ALL CONFIGURATIONS AND NO ODOR WAS DETECTED. HOWEVER, AT FULL HOT WITH APU ON, SMOKE ODOR FILLED THE CABIN. REPLACED COALESCERS AND RELEASED AIRCRAFT PER MD80 MEL 49-1. SUBSEQUENTLY, REPLACED APU IN SEA ON 1-17-95, AND REMOVED MEL PLACARD. REFERENCE CONTROL NR ASAA 95-021. 2L72 4F A6WE 19950210004211995021000421WP 1995 2 10 ASAA95021 119950115A4900GTCP8598DHF APU DOUG DC9 DC982 3022082WP AFT FUSELAGE DEFECTIVE A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01937AS17563 49364 PDX - FLT 506 - AIR TURN BACK. CREW REPORTED SMOKE ODOR IN COCKPIT SHORTLY AFTER TAKEOFF AND LAV SMOKE DETECTOR ACTIVATED. DEPRESSURIZED AIRCRAFT AT 500 FEET AND LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN-UP OF BOTH ENGINES FOR 5 MINUTES WITH BOTH PACKS ON IN ALL CONFIGURATIONS AND NO ODOR WAS DETECTED. HOWEVER, AT FULL HOT WITH APU ON, SMOKE ODOR FILLED THE CABIN. REPLACED COALESCERS AND RELEASED AIRCRAFT PER MD80 MEL 49-1. SUBSEQUENTLY, REPLACED APU IN SEA ON 1-17-95, AND REMOVED MEL PLACARD. REFERENCE CONTROL NR 95ZZZX669. (X) 2L72 4F A6WE 19950210004221995021000422NM 1995 2 10 CAL950009 119950103A77117898301 EPR TRANSMITTER BOEING757 757224 1384958NM NR 2 ENGINE INOPERATIVE A CALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0912109214 27299 IAH - FLT 0145 - THE AIRCRAFT WAS DIVERTED TO IAH WHILE EN ROUTE FROM EWR TO MEX, AFTER EXPERIENCING ENGINE PROBLEMS. THE POWER DIFFERENTIAL BETWEEN THE LT AND RT ENGINE WAS CAUSING THE THROTTLES TO BE DISPLACED 3-4 INCHES. THE NR 2 ENGINE EPR TRANSMITTER WAS REMOVED AND REPLACED. THE ENGINES WERE RUN AND ENGINE PERFORMANCE MATCHED. (X) 2L72 4F RTA2NM 19950210004241995021000424EU 1995 2 10 VTZA95017 119950111A5270 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR ILLUMINATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27304UE 41017 IAD/DAY - FLT 6290 - DURING TAKEOFF AT 1800 HOURS ON 1-11-95, ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950210004251995021000425 1995 2 10 9501849754 419950127A3421258733511 VERTICAL GYRO DOUG DC9 DC941 302207NWP NR 1 MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01754NW4101311693 47178 CAPTAIN'S VERTICAL GYRO FAILED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 VERTICAL GYRO AND ADI. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210004261995021000426WP 1995 2 10 9501859968 119950201A24336RW176YN3 RECTIFIER DOUG DC9 DC931 3022065WP RIGHT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019332 6953833369 47264 LOSS OF RIGHT TRANSFORMER RECTIFIER OCCURRED AFTER TAKEOFF. DC LOAD WAS INDICATING ZERO. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT TRANSFORMER RECTIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210004271995021000427 1995 2 10 9501869153 419950112A3454 NAV RECEIVER DOUG DC9 DC914 3022034WP NR 1 FAILED A NWAAA UNSCHED LANDING O OTHER APAPPROACH 1 GL018912E 45829 NR 1 VOR FAILED ON APPROACH INTO DTW. FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. REPLACED NR 1 NAV/COMM CONTROL PANEL AND NR 1 NAV RECEIVER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950210004281995021000428NE 1995 2 10 9501872289 219950204A7230 COMPRESSOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01289US 21377 685592 DURING TAKEOFF ROLL, TWO COMPRESSOR STALLS OCCURRED ON THE NR 2 ENGINE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. AIRCRAFT WAS FERRIED TO ORD WHERE THE NR 2 ENGINE WAS REPLACED AND RUN-UP CHECKED OK. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950210004291995021000429NM 1995 2 10 9501882284 119950201A53136556441 STRINGER BOEING727 727251 138408HNM FS 971-986 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND STR 29L BETWEEN FS 971 AND 986 CORRODED. REPAIRED PER NWA EA 22-093791. 2L73 4F A3WE 19950210004311995021000431NM 1995 2 10 95FDEA00112 119950207A3230 RETRACT MECH BOEING727 727233 138408ANM LANDING GEAR MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04270FE 22035 AFTER T/O GEAR HANDLE WOULD NOT GO ABOVE OFF POSITION. ACCOMPLISHED CKLIST, ELECTED TO RETURN TO MEM WITH GEAR DOWN. REMOVED AND REPLACED R-92 RELAY PRECAUTIONARY SWUNG GEARS SEVERAL TIMES, FOUND NO DEFECTS A/C OK FOR SERVICE AS PER MM 32-31-11. 2L73 4F RTA3WE 19950210004321995021000432NM 1995 2 10 95FDEA00113 119950208A2612 FIRE WARNING BOEING727 727232 1384082NM ENGINE ACTIVATED A FDEAK NONE N FALSE WARNING CLCLIMB 1 SO04498FE 20867 AFTER T/O FIREBELL RANG MOMENTARILY AND ONE RED LT FLASHED, WAS OVER BEFORE WE COULD DETERMINE SOURCE. TESTED ENG AND W/W FIRE WARNING. CKS NORMAL. NO HISTORY NOTED. SYSTEM OK FOR SERVICE. 2L73 4F A3WE 19950210004331995021000433WP 1995 2 10 ABXA9500067 119950203A33504TL1110B EEL SWITCH DOUG DC9 DC931 3022065WP CABIN INTERMITTENT A ABXAK NONE L NO TEST CRCRUISE 1 GL23947AX 47004 CABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY IN FLIGHT. REPLACED CABIN EMERGENCY LIGHT SWITCH PER DC-9 MM. OPS CHECKED NORMAL. 2L72 4F A6WE 19950210004341995021000434WP 1995 2 10 ABXA9500068 119950206A326032802651 DOOR TARGET DOUG DC8 DC862 3021970WP LT MLG LOOSE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23803AX 45917 UPON GEAR RETRACTION, CREW HAD AN UNSATISFACTORY GEAR UPLATCH INDICATION. RECYCLED GEAR THREE TIMES, LEFT GEAR DOOR LIGHT ILLUMINATED. COMPLIED WITH ALTERNATE PROCEDURE AND LIGHT WENT OUT. CLEANED AND LUBED LEFT MLG DOOR UPLATCH MECHANISM. PERFORMED OPERATIONAL CHECK OF UPLATCH MECHANISM AND DOOR LIGHT. SYSTEM OPS CHECKED GOOD IAW DC8 MM. THE LEFT MLG DOOR UPLATCH STRIKER TARGET WAS FOUND TO BE LOOSE AFTER THE NEXT FLIGHT. TIGHTENED AND PERFORMED MLG PROXIMITY TEST IAW DC 8 MM CHAPTER 32. 2L74 4F 4A25 19950210004351995021000435WP 1995 2 10 ABXA9500069 119950208A2910577412063004 HYD HOSE DOUG DC8 DC861 3021952WP RT MLG RUPTURED A ABXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL23841AX 45908 ON SHORT FINAL, THE HYDRAULIC FLUID QUANTITY LEVEL DROPPED TO THE STANDPIPE LEVEL AFTER GEAR AND FLAP EXTENSION. LEVEL REMAINED THERE AFTER LANDING. FOUND THE RIGHT GEAR UNLOCK BOGIE TRIM LINE RUPTURED. REMOVED AND REPLACED THE HYDRAULIC LINE IAW DC 8 MM CHAPTER 32. SYSTEM LEAK AND OPS CHECKED GOOD. 2L74 4F 4A25 19950210004361995021000436 1995 2 10 ABXA9500070 419950208A316036143091006 MFD DISPLAY UNIT DOUG DC8 DC861 3021952WP COCKPIT DEFECTIVE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23850AX2125 33 45894 DURING CRUISE, THE MULTIFUNCTION DISPLAY WENT BLACK AND MADE A 'GROWLING' NOISE. THERE WAS A SMELL OF SMOKE IN THE COCKPIT; CREW PULLED THE CIRCUIT BREAKER. REMOVED AND REPLACED THE MFD. SYSTEM OPS CHECKED GOOD IAW DC 8 MM CHAPTER 34. 2L74 4F 4A25 19950210004371995021000437WP 1995 2 10 ABXA9500071 119950208A25105641031515 SEAT ROLLERS DOUG DC8 DC863 302198AWP LT COCKPIT DIRTY A ABXAK NONE O OTHER CRCRUISE 1 GL23813AX 46136 CAPTAIN'S SEAT WILL NOT LOCK IN NUMEROUS POSITIONS. CLEANED AND LUBED FORE/AFT TRACKS AND ROLLERS. LUBED LOCKPINS AND LOCKPIN HOLES. SEAT OPERATED NORMALLY IAW DC 8 MM CHAPTER 25. 2L74 4F 4A25 19950210004391995021000439NM 1995 2 10 DL72S950508 119950201A5313695848826 STRINGER BOEING727 727232 1384082NM FS 950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11400DA 21144 DURING INSPECTION FOUND FUSELAGE STRINGER 18A LEFT SIDE, CRACKED ON HORIZONTAL FLANGE AT FS 950. REPAIRED PER MM 53-12 PG 818 ITED LEVEL 2 REPAIR. 2L73 4F A3WE 19950210004401995021000440NM 1995 2 10 DL72S950525 119950206A57536521631325K SKIN BOEING727 727232 1384082NM NR 1 FORE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 DURING SHOP INSPECTION THE LEFT WING NR 1 FORE FLAP WAS FOUND WITH THE LEADING EDGE SKIN DAMAGED AT 7 INCHES TO 12 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950210004411995021000441NM 1995 2 10 DL72S950532 119950111A57546516221100 RIB BOEING727 727232 1384082NM NR 5 SLAT LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11526DA 21586 ON NR 5 L/E SLAT DURING INSPECTION A CRACK WAS FOUND ON A RIB. A REPAIR DOUBLER WAS INSTALLED PER M/M 57-54-00 FIG 809. 2L73 4F A3WE 19950210004421995021000442NM 1995 2 10 DL72S950533 119950111A57546516221100 SKIN BOEING727 727232 1384082NM NR 5 LE SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11526DA 21586 DURING INSPECTION ON A B727 NR 5 L/E SLAT, A HOLE WAS FOUND TO BE ELONGATED UNDER WHERE THE FENCE IS MOUNTED. IN ADDITION, THE OUTER SKIN WAS FOUND TO BE WORN AT THE SAME LOCATION. AN EXTERNAL DOUBLER WAS INSTALLED PER THE M/M 57-54-00 PG 817. 2L73 4F A3WE 19950210004431995021000443NM 1995 2 10 DL72S950537 119950206A2720 PCU 591005017 BOEING727 727232 1384082NM RUDDER FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11546DA 504 22677 DURING CLIMB THROUGH 18,000 FEET BOTH 'A' SYSTEM HYDRAULIC PUMPS FAILED, LANDED LAX. FOUND LOWER RUDDER PCU FAILED, CAUSING A SYSTEM FAILURE. REPLACED PCU AND BOTH 'A' SYSTEM PUMPS AND FILTERS. 2L73 4F A3WE 19950210004441995021000444NM 1995 2 10 DL72W950484 119950125A5754 WEB BOEING727 727247 138408FNM NR 7 LE SLAT GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 FOUND DURING HMV, GOUGE IN WEB FWD OF ATTACH BOLT NR 7 SLAT O/B. REPAIRED PER M/M 57-54-0 PG 807. 2L73 4F A3WE 19950210004451995021000445NM 1995 2 10 DL72W950485 119950123A5320 DOOR FRAME BOEING727 727247 138408FNM DOOR CUT OUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 FOUND DURING HMV, RI1 DOOR OPENING FUSELAGE FRAME WAS FOUND CRACKED, LOWER END. REPAIRED PER SRM 53-10-4. 2L73 4F A3WE 19950210004461995021000446NM 1995 2 10 DL72W950486 119950130A5530 ATTACH ANGLES BOEING727 727247 138408FNM VERTICAL STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 FOUND DURING HMV, ATTACH ANGLE CRACKED AT NR 5 STR ABOVE NR 2 'S' DUCT INSIDE VERT STAB. REPAIRED PER SRM55-30-5 PG.1, FIG 1. 2L73 4F A3WE 19950210004471995021000447NM 1995 2 10 DL72W950487 119950130A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 FOUND DURING HMV, NR 5 STR CRACKED INSIDE VERT STAB AT STA 110.4. REPAIRED PER ERA 301113-14. 2L73 4F A3WE 19950210004491995021000449NM 1995 2 10 DL72W950528 119950127A5330 SKIN BOEING727 727247 138408FNM FS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND AFT B/B INNER SKIN BETWEEN STA 950/950A O/B OF STR 30 LFT CORRODED. REPAIRED PER ERA 301093-14. 2L73 4F A3WE 19950210004501995021000450NM 1995 2 10 DL733950523 119950128A5313 STRINGER BOEING737 737347 1384647NM FS 787 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11307WA 23440 DURING HMV, FOUND CARGO TIEDOWN STRINGER CRACKED IN AFT B/B RT CARGO TIEDOWN AT STA 787. REMOVED DAMAGED SECTION AND REPLACED PER SRM 53-00-53 PG 201-203, 206, 207. 2L72 4F RTA16WE 19950210004531995021000453NM 1995 2 10 DL757950515 119950206A5754114N4005157 SKIN BOEING757 757232 1384965NM NR 4 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11648DL 24372 DURING SHOP INSPECTION, NR 4 SLAT WAS FOUND WITH THE TRAILING EDGE WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02. 2L72 4F RTA2NM 19950210004541995021000454NM 1995 2 10 DL757950524 119950111A5754114N4003178A SKIN BOEING757 757232 1384965NM NR 9 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11635DL 23762 NR 9 LE SLAT, TRAILING EDGE WAS FOUND TO BE DELAMINATED WEDGE WAS REPLACED DURING SHOP 38O VISIT PER SRM 57-43-02 AND AD 90-23-06. 2L72 4F RTA2NM 19950210004551995021000455NM 1995 2 10 DL757950540 119950204A2410 GASKET BOEING757 757232 1384965NM NR 2 IDG LEAKING A DALAA UNSCHED LANDING HK ELECT. POWER LOSS-50 PC FLUID LOSS CRCRUISE 1 SO11620DL 22910 DURING CRUISE WITH NR 2 IDG ON MCO, APU FLAMED OUT, DIVERTED DFW. PEFORMED BITE CHECK ON APU CONTROLLER AND HAD SEVERAL SUCCESSFUL STARTS. NR 2 IDG HAD LEAKING GASKET, REPLACED GASKET, RETURNED TO SERVICE. 2L72 4F RTA2NM 19950210004561995021000456NM 1995 2 10 DL757950542 119950206A3350BPS73 POWER SUPPLY BOEING757 757232 1384965NM CABIN EEL FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11620DL 22910 DURING INSPECTION, FIRST CLASS FLOOR TRACK LIGHTS FAILED TO TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L72 4F RTA2NM 19950210004571995021000457NM 1995 2 10 DL76L950518 119950204A5753113T310078 FLAP BOEING767 767332 1382001NM RT TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11172DN 24775 AT HMV, RT WING OUTBOARD FLAP WAS FOUND WITH WEAR DAMAGE AT INBOARD FORWARD EDGE AND AT THE INBOARD ATTACH FITTING. REPAIRED PER SRM 57-53-01 PG 205 WITH REFERENCE TO SRM 51-70-17. 2L72 4F RTA1NM 19950210004581995021000458WP 1995 2 10 DLL16950472 119950201A53121505312101 FRAME SEGMENTS LKHEED1011 10113853 5265020WP AFT PRESS DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 DURING AIRCRAFT HMV IN ATL, THE FRAME SEGMENTS ON THE AFT PRESSURE DOME BETWEEN S23 AND S44 WERE FOUND WITH CRACK IN THE LOWER FLANGE RADII. THE DAMAGE WAS TRIMMED OUT, SPLICE STRAPS WERE ADDED, AND THE REPAIR AREA WAS TREATED FOR CORROSION. 2L73 4F A23WE 19950210004601995021000460NM 1995 2 10 DLM88950538 119950204A26218981501 FIRE BOTTLES DOUG MD88 MD88 3023688NM TAIL COMP FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11913DE 49956 DURING PNEUMATIC SYSTEM CHECKOUT, A LOUD NOISE WAS HEARD IN THE TAIL OF THE AIRCRAFT. ON INVESTIGATION, BOTH FIRE BOTTLES WERE FOUND RIPPED FROM THEIR MOUNTS AND DISCHARGED, CAUSING EXTENSIVE DAMAGE TO PNEUMATIC DUCTS, AFT PRESSURE DOME AND STRINGER 10 AT FS 1338. CAUSE OF DISCHARGE AND BOTTLE FAILURE IS UNDER INVESTIGATION. 2L72 4F RTA6WE 19950210004611995021000461WP 1995 2 10 MWEA95124 119950208A2560113313 EVAC SLIDE DOUG DC9 DC915 3022036WP PAX DOOR DETACHED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31900ME 45841 PILOT REPORTS MAIN ENTRANCE DOOR EVACUATION SLIDE FELL OFF. MECHANICS RESECURED EVACUATION SLIDE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950210004621995021000462NM 1995 2 10 SWAA950157 119950206A335020131A EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950210004631995021000463NM 1995 2 10 SWAA950158 119950205A335020131A EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07322SW 23343 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS LEFT AND RIGHT SIDES INOP. REPLACED BATTERY PACK AND BASE PER BOEING M/M. 2L72 4F RTA16WE 19950210004641995021000464NM 1995 2 10 SWAA950159 119950207A53206545834255 INTERCOSTAL BOEING737 737317 138447PNM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 294.5 AND 312. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004651995021000465NM 1995 2 10 SWAA950160 119950207A53302024T3 SKIN BOEING737 737317 138447PNM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT FOLLOWING LOCATIONS: BS 1020, BETWEEN S12 AND 13L, AT BS 1000, WL 220, LEFT SIDE BEHIND AFT ENTRY DOOR, AT BS 356, BETWEEN S18 AND 19R, AT BS 193, WL 192, LEFT SIDE, AT BS 1040, LBL 188, BS 972, BETWEEN S22 AND 23L, AND AT BS 1000, LBL 4, WL 185. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004661995021000466NM 1995 2 10 SWAA950161 119950207A5754 SKIN BOEING737 737317 138447PNM NR 6 LE SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND NUMBER 6 SLAT CRACKED AT LOWER L/E OF SLAT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004671995021000467NM 1995 2 10 SWAA950162 119950207A5315BAC1506626 FLOOR BEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM UPPER CHORD CORROSION AT BS 1112 TO 1121, RBL 22, WL 228, AT BS 986.5, LBL 55 TO RBL 55, WL 208 AND AT BS 1016, RBL 45 TO LBL 45, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004681995021000468NM 1995 2 10 SWAA950163 119950207A5315BAC1505100246 FLOOR BEAM BOEING737 737317 138447PNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM CORRODED BS 328, WL 208, RBL 7 TO 56, AT BS 312, WL 208, LBL 15, AND AT BS 344, WL 208, LBL 60. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004691995021000469NM 1995 2 10 SWAA950164 119950207A5315BAC1506626 FLOOR BEAM BOEING737 737317 138447PNM BS 1112-1121 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR BEAM LOWER HORIZONTAL CHORD CORRODED FROM BS 1112 TO 1121, RBL 22, WL 216. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004701995021000470NM 1995 2 10 SWAA950165 119950207A5321 FLOOR BOEING737 737317 138447PNM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND CRACK IN COCKPIT FLOOR AT BS 248, LBL 12, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004711995021000471NM 1995 2 10 SWAA950166 119950207A53302024T3040 SKIN BOEING737 737317 138447PNM BS 727 OIL CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING AT BS 727E+3, BETWEEN S22 AND 23L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004721995021000472NM 1995 2 10 SWAA950167 119950207A53117075T6063 FRAME BOEING737 737317 138447PNM BS 787 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME DAMAGE AT BS 787, RBL 22, WL 156. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004731995021000473NM 1995 2 10 SWAA950168 119950207A5241 DOOR BOEING737 737317 138447PNM BS 298 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND CRACK ON FWD UPPER CORNER OF FWD GALLEY DOOR AT FASTENER HOLE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210004741995021000474EA 1995 2 10 COM60394 119950127A274070623 MOTOR CONTL UNIT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 SO01920CA1691 63 7022 STABILIZER TRIM CHANNEL 2 IS INOP. REPLACED THE STABILIZERMOTOR CONTROL UNIT. 2L72 4F RTA21EA 19950210004751995021000475EA 1995 2 10 COM60397 119950124A5755 SPOILER CNDAIRCL600 CL6002B19 EA RIGHT DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA 7031 HOLE FOUND IN RT INBD GROUND SPOILER. C/W TEMPORARY REPAIRAND TRANSFERED TO DEFERRED MAINTENANCE LIST, PER DER REPORTAND CANADAIR REO 601R-57-71-001. 2L72 4F RTA21EA 19950210004761995021000476NM 1995 2 10 9501802296 119950203A3260H1010154 SWITCH BOEING727 727251 138408HNM NLG FAILED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01296US 21788 DURING APPROACH UPON LANDING GEAR EXTENSION, NOSE GEAR UNSAFE INDICATION REMAINED ILLUMINATED. RECYCLED LANDING TO NO AVAIL. NOSE LANDING GEAR SAFE INDICATION STARTED TO SLOWLY FLASH. VERIFIED NOSE LANDING GEAR POSITION THROUGH VIEWING PORT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED S-93 AND S-96 (P/N'S H10-1015-4 AND -3) POSITION SWITCHES. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950210004771995021000477NM 1995 2 10 9501812703 119950203A275118157013 TRANSMITTER BOEING727 727225 1384077NM TE FLAP FAILED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL018878Z6883 6883 21451 DURING APPROACH UPON FLAP EXTENSION, TRAILING EDGE INBOARD FLAPS INDICATED AN ASYMMETRICAL CONDITION. COMPLETED ABNORMAL PROCEDURE AND DECLARED AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT INBOARD FLAP POSITION DRIVE UNIT AND TRANSMITTER. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950210004781995021000478 1995 2 10 9501823241 419950205A34446228701002 ANTENNA AIRBUS320 A320211 3930320EU RADIO ALT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01341NW7001 7001 380 DURING CRUISE, RECEIVED 'NAV RA 2' FAULT. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 RADIO ALTIMETER TRANSMISSION ANTENNA (6SA2). OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950210004791995021000479EU 1995 2 10 9501833204 219950203A7321 ECU AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 ENGINE MALFUNCTIONED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL01304US165877119 307 731363 DURING CLIMB, THE NR 1 ENGINE EXPERIENCED TWO OR THREE POWER SURGES. NUMEROUS 'A' AND 'B' FADEC MESSAGES WERE OBSERVED. ENGINE THRUST WAS REDUCED TO IDLE AND ENGINE WAS EVENTUALLY SHUT DOWN DUE TO FAILURE DURING RETURN TO MEM. THE ENGINE CONTROL UNIT AND ENGINE CONTROL ALTERNATOR WERE REPLACED. CHECKED OK FOR SERVICE. 2L72 4F4 FRTA28NM 19950210004801995021000480NM 1995 2 10 95UAL727011 119950201A3350 EEL BATTERIES BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297275U 21422 FOUR EMERGENCY LIGHTS LOCATED THROUGOUT AFT CABIN INOPERATIVE. REPLACED BATTERIES. CHECKS OKAY. 2L73 4F4 F A3WE E2EA 19950210004811995021000481NM 1995 2 10 95UAL737006 119950124A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29335UA 24230 RIGHT REAR DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004821995021000482NM 1995 2 10 95UAL737007 119950124A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29335UA 24230 LEFT REAR DOOR INTERIOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004831995021000483NM 1995 2 10 95UAL737008 119950126A523065558786 SEAL BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CARGO DOOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP299032U 19070 LEVELED OFF AT 23,000 FEET, HEARD LOUD RUMBLE SOUND, FOLLOWED BY STANDBY FAIL LIGHT AND OXYGEN LIGHT. DESCENDED AND RETURNED TO ORD. FOUND FORWARD CARGO SEAL BLOWN OUT OF CHANNEL, DUE TO LOWER DOOR THRESHOLD SILL NOT PROPERLY ADJUSTED. REPLACED DOOR SEAL AND ADJUSTED THRESHOLD PLATE. 2L72 4F4 F A16WE E2EA 19950210004841995021000484NM 1995 2 10 95UAL737009 119950130A3260 BULB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT MLG FAILED A UALAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 WP29316UA 23948 ON FINAL, WITH LANDING GEAR LEVER DOWN, RIGHT GEAR GREEN LIGHT DID NOT ILLUMINATE. DID TOWER FLY BY AND CONFIRMED GEAR DOWN. REPLACED LIGHT BULB. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004851995021000485NM 1995 2 10 95UAL737010 119950130A3350 EEL CABLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29374UA 24639 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 THROUGH ROW 16. REPLACED EMERGENCY ESCAPE PATH LIGHT POWER CABLE. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004861995021000486NM 1995 2 10 95UAL737011 119950203A2612 FIRE LIGHT BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE ILLUMINATED A UALAF ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 WP299069U 19950 CREW REPORTS THAT DURING FLIGHT, NUMBER TWO ENGINE FIRE WARNING SOUNDED FOR TWO SECONDS AND WENT OFF. SOUNDED A SECOND TIME, SHUT DOWN ENGINE AND DISCHARGED THE BOTTLE. LANDED UNDER AMBER ALERT. 2L72 4F4 F A16WE E2EA 19950210004871995021000487NM 1995 2 10 95UAL737012 119950203A3350 EEL CABLE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29923UA 26643 EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT 2 A AND B. REPLACED EMERGENCY ESCAPE PATH FEEDER CABLE AT SEAT 2 A AND B. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004881995021000488NM 1995 2 10 95UAL737013 119950206A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29369UA 24538 FLOOR EMERGENCY ESCAPE PATH LIGHTING INOP ROWS 10 THROUGH 15. REPLACED BATTERY AT LEFT HAND MID POSITION. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004891995021000489NM 1995 2 10 95UAL737014 119950206A2440WH941D3352MOD CONTACTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 EXT POWER FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29306UA 23667 NUMBER ONE GENERATOR HARD TO PUT ON LINE. PRIOR TO TAKEOFF NUMBER ONE AND TWO ENGINES VARIED RPM AT IDLE, AND AT 100 KNOTS STICK SHAKER ACTIVATED. ABORTED TAKEOFF. REPLACED NUMBER ONE EXTERNAL POWER CONTACTOR AND R348 RELAY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950210004901995021000490NM 1995 2 10 95UAL747005 119950206A3350 EEL WIRE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 EMERGENCY EXIT SIGNS AT DOOR 4 LEFT REMAIN ON AFTER TEST. RESPLICED WIRE BUNDLE. 2L74 4F4 FRTA20WE E24NE 19950210004911995021000491EU 1995 2 10 95UALA32005 119950120A3350 EEL AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29403UA 442 INTERIOR EMERGENCY EXIT LIGHTS OUT AT DOOR 1 LEFT AND 1 RIGHT. 2L72 4F RTA28NM E40NE 19950210004921995021000492EU 1995 2 10 95UALA32007 119950127A2430 DC ELECTRICAL AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE NR 2 MALFUNCTIONED A UALAO OTHER L NO TEST ININSP/MAINT 1 WP29412UA 465 WHEN ACCOMPLISHING THE DC EMERGENCY GENERATION CHECK, TEST FAILS NO ELECTRICAL PARAMETERS. NR 2 ENGINE PARAMETERS APPEAR AND UPPER ECAM SCREEN BLANKS AND SWITCHES TO LOWER SCREEN. 2L72 4F RTA28NM E40NE 19950210004931995021000493EU 1995 2 10 95UALA32008 119950201A2560D31516109 RELEASE CABLE AIRCRUISERS MR25613 AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE L 1 DOOR SLIDE TANGLED A UALAK NONE O OTHER ININSP/MAINT 1 WP29401UA1070 435 DURING SCHEDULED SLIDE DEPLOYMENT AT C-CHECK, SLIDE AT DOOR 1 LEFT DID NOT DEPLOY. SLIDE RELEASE CABLE WAS FOUND WRAPPED AROUND VALVE BODY PREVENTING SLIDE FROM DEPLOYING. AIRCRUISERS HAS CREATED A SERVICE BULLETIN TO ENSURE PROPER PACKING OF SLIDES. UNITED WILL ACCOMPLISH A FLEET CAMPAIGN TO REMOVE E ALL POTENTIALLY AFFECTED SLIDE RAFTS. 2L72 4F RTA28NM E40NE 19950210004941995021000494EU 1995 2 10 95UALA32009 119950206A270131073065 SERVO CONTROL LUCAS 31073065 AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE RT AILERON LEAKING A UALAK NONE L NO TEST ININSP/MAINT 1 WP29412UA2273 1903 465 HYDRAULIC MOTOR GENERATOR FAILS TEST. TRIES TO COME UP TO SPEED AND THEN SHUTS OFF. REPLACED RIGHT HAND OUTBOARD AILERON SERVO CONTROL DUE TO HIGH INTERNAL LEAKAGE. 2L72 4F RTA28NM E40NE 19950210004951995021000495SO 1995 2 10 COM11760 119950206A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01162CA4064 2568 120150 FLAP CONTROL FAULT WARNING WILL NOT RESET. REPLACED RT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950210004961995021000496SO 1995 2 10 COM11761 119950205A324012028972009 LINE ASSY EMB 120 EMB120RT SO PARKING BRAKE CHAFED A COMAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01130G 14619 120130 RT HYDRAULIC SYSTEM LOST ALL PRESSURE AND QUANTITY. REPLACED THE PARKING BRAKE ACCUMULATOR PRESSURE SUPPLY LINE, DUE TO CHAF DAMAGE. 2L72 4T RTA31SO 19950210004971995021000497 1995 2 10 COM11762 419950205A612278249012 PCU EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO011117H11601425 120117 RT ENGINE NP FLUCTUATES 1.5 PERCENT. REPLACED RT PCU. 2L72 4T RTA31SO 19950210004981995021000498SO 1995 2 10 COM11763 119950205A5753PE610261 ROLLERS EMB 120 EMB120RT SO LT TE FLAP WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01244CA 120217 FLAP DISAGREEMENT WARNING, WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED THE LEFT OUTBD FLAP ROLLERS. 2L72 4T RTA31SO 19950210004991995021000499SO 1995 2 10 COM11764 119950204A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION LDLANDING 1 SO011117H9622 136 120117 OUTBD FLAPS COULD NOT BE RAISED FROM THE EXTENDED POSITION. REPLACED THE RT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950210005001995021000500EU 1995 2 10 COM31027 119950204A243523080031 START GEN SAAB SF340 SF340A 7850100EU RT ENGINE FAILED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01344CA19666691 340A025 RT ENGINE WILL NOT START. REPLACED THE STARTER/GEN. 2L72 4T RTA52EU 19950210005011995021000501EA 1995 2 10 COM60405 119950205A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA RT TE FLAP DEFECTIVE A COMAO OTHER N FALSE WARNING LDLANDING 1 SO01940CA799 7048 FLAPS FAIL MESSAGE ON EICAS WHEN FLAPS SELECTED DOWN FOR LANDING. REPLACED THE RT FLAP BRAKE AND POSITION SENSOR UNIT. 2L72 4F RTA21EA 19950210005021995021000502EA 1995 2 10 COM60406 119950205A3230864806 PSEU CNDAIRCL600 CL6002B19 EA LANDING GEAR DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01916CA3376 2548 7014 LANDING GEAR DID NOT RETRACT. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19950210005031995021000503EA 1995 2 10 COM60407 119950203A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 1 SPOILER DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01912CA3757 586 7011 SECU UNSAFE MESSAGE ON EICAS. REPLACED THE NR 1 SECU. 2L72 4F RTA21EA 19950210005041995021000504EA 1995 2 10 COM60408 119950203A2750860D10016 FECU CNDAIRCL600 CL6002B19 EA ET FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01941CA7 7050 FLAP OVERSPEED WARNING OCCURS WHEN FLAPS SELECTED TO 20 DEG. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950210005051995021000505EA 1995 2 10 COM60409 119950203A322016400103 DRAG BRACE CNDAIRCL600 CL6002B19 EA NLG LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01916CA2014 7014 NLG WILL NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY. 2L72 4F RTA21EA 19950210005061995021000506WP 1995 2 10 MWEA95123 119950206A3800 WATER LINE DOUG DC9 DC932 3022066WP CARGO COMPT RUPTURED A MWEAO OTHER K FLUID LOSS APAPPROACH 1 GL31401ME 47133 DURING APPROACH TO MKE, PILOT WAS UNABLE TO MOVE GEAR HANDLE TO DOWN POSITION. HE EXTENDED GEAR USING EMERGENCY GEAR EXTENSION HANDLE AND PROCEDURES. GEAR EXTENDED, VERIFIED 3 GREEN. AFTER THE GEAR WAS EXTENDED THE FLAP HANDLE MOVED STIFFLY TO 15 POSITION WITHOUT FLAP ACTUATION. SLATS EXTENDED NORMALLY. AIRCRAFT LANDED WITHOUT INCIDENT. MECHANICS FOUND BROKEN WATER SUPPLY LINE IN FWD BAGGAGE COMPT. WHICH LEAKED INTO GEAR WELL CAUSING LANDING GEAR CONTROL VALVE TO FREEZE. THAWED ICE FROM WHEEL WELL. REPAIRED WATER LINE. PERFORMED GEAR EXTENSION AND RETRACTION TEST. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950210005071995021000507EU 1995 2 10 QXEA9500033 119950204A491038075412 APU FOKKERF28 F28MK1000 4990808EU CABIN MALFUNCTIONED A QXEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM09803PH103674105 11017 SEA - OIL SMELL COMING FROM AIR VENTS. AIRCRAFT WAS ON DESCENT INTO SEA WITH ENGINES AT IDLE POWER FOR 10 MIN. CREW DETERMINED SMELL WAS FROM THE APU. REPLACED APU IAW MM. APU OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950210005081995021000508EU 1995 2 10 QXEA9500034 119950205A33501312 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 PDX - EXIT LIGHT IN CABIN CEILING ABOVE ROW 8 INOP. REPLACED BULBS AND LIGHT OPS CHEKCED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950210005091995021000509NM 1995 2 10 QXEA9500035 119950205A33506104781 EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09826PH 163 12580 SEA - LEFT HAND AFT OUTSIDE AND AFT OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND POWER SUPPLY AND LIGHT OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950210005101995021000510NM 1995 2 10 QXEA9500036 119950205A33506038441 EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09823PH 110 PDX - THE TWO FORWARD EMERGENCY LIGHTS IN THE STRIP LIGHTING ARE INOP. REPLACED BATTERY POWER SUPPLY AT SEAT 1DE AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950210005111995021000511EU 1995 2 10 QXEA9500037 119950206A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 SEA - EMERGENCY EXIT SIGN IN OP AT COCKPIT DOOR. REPLACED BULBS AS REQUIRED AND SING OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950210005121995021000512NM 1995 2 10 SWAA950153 119950204A7110314A101010 COWL BOEING737 7373H4 1384600NM NR 1 ENGINE DENTED A SWAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW07300SW 22940 EXPERIENCED BIRDSTRIKE TO NUMBER 2 ENGINE. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION AND NOTED DAMAGE TO ENGINE INLET COWL. NO DAMAGE TO ENGINE INTERNALLY. PERFORMED TEMP REPAIR AND MAINTENANCE FERRIED AIRCRAFT TO DAL FOR REPAIRS. REPLACED ENGINE INLET COWL PER BOEING M/M. 2L72 4F RTA16WE 19950210005131995021000513NM 1995 2 10 SWAA950154 119950204A5330 SKIN BOEING737 7372K6 NM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH CRACK IN LEFT FUSELAGE SKIN JUST AFT OF FILLET FAIRING AT BS 767. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950210005141995021000514NM 1995 2 10 SWAA950155 119950204A53206546547 CHORD BOEING737 7373Y0 1384671NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND COMPRESSION CHORD CRACKED AT BS 727, WL 199, RBL 13 TO 15. REPAIRED PER TRAMCO EWO 95-0076. 2L72 4F RTA16WE 19950210005151995021000515NM 1995 2 10 SWAA950156 119950204A5330 SKIN BOEING737 7373Y0 1384671NM BS 727-747 OIL CANNING A SWAAK NONE O OTHER ININSP/MAINT 1 SW07699SW 23826 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN OIL CANNING FROM BS 727D TO 747, STRINGER 22L TO 24L. REPAIRED PER TRAMCO EWO 95-0082. 2L72 4F RTA16WE 19950210005161995021000516NM 1995 2 10 UPS202202 119950202A3350 EEL BATTERIES BOEING727 72727C 138400JNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01912UP 19244 DURING PREDEPARTURE CHECK, EMERGENCY EXIT SIGN DIM AT FORWARD ENTRY DOOR. REPALCED BATTERIES, CHECKS OK. MFG P/N 5106. 2L73 4F A3WE 19950210005181995021000518NM 1995 2 10 95ZZZW85 119950121A3260H146 SWITCH BOEING727 72729 1384007NM NLG DIRTY A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01712DH 19401 NOSE GEAR DOOR LIGHT DOES NO ILLUMINATE DURING GEAR EXTENSION (ON S/O PANEL). CLEANED AND LUBED NOSE GEAR DOOR SWITCH PLUNGERS LIGHTS AND SWITCHES, OPS CKS GOOD. 2L73 4F A3WE 19950210005191995021000519NM 1995 2 10 95ZZZW86 119950121A322265727628 STRUT ASSY BOEING727 72730C 1384009NM NLG REQD SERVICE A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01701DH 19011 UPON LANDING GEAR RETRACTION ON CLIMB, RED GEAR DOOR LIGHT ON, AND AMBER NOSE GEAR LIGHT ON SECOND OFFICER PANEL ON. SERVICED NOSE GEAR STRUT WITH NITROGEN AND FLUID. JACKED NOSE GEAR AND PERFORMED GEAR SWING. OPS CHECKS OK. MM 32-20. 2L73 4F A3WE 19950210005381995021000538NM 1995 2 10 AALA950010 119950104A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739365 24046 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT AFT GALLEY PARTITION A6 LAVATORY, AND FWD OF A6 LAVATORY INOPERATIVE. RECONNECTED CONNECTOR AT 41HJ. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950210005391995021000539EU 1995 2 10 AALA950022 119950106A3350A3060719103 EEL STRIP FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071438H 11428 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN HAD THREE LIGHTS INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RT 19950210005401995021000540NM 1995 2 10 AALA950024 119950108A3350 EEL WIRE BOEING767 767223 1385123NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT ROWS 7H AND 8H INOPERATIVE. REPAIRED DEFECTIVE WIRE SPLICE BY PAX SEAT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950210005411995021000541NM 1995 2 10 AALA950055 119950111A3350A3060719101 STRIP BOEING757 757223 1384957NM CABIN EEL DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07662AA 25296 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA2NM 19950210005421995021000542WP 1995 2 10 AALA950064 119950115A3350 EEL DOUG DC10 DC1010 3022110WP CABIN MALFUNCTIONED A AALAK NONE O OTHER DEDESCENT 1 SW07135AA 47830 SFO - FLT 177 - DURING DESCENT, EMERGENCY FLOOR LIGHTS THROUGHOUT CABIN ILLUMINATED AND EXTINGUISHED PRIOR TO LANDING. ACFT LANDED SFO WITHOUT INCIDENT. ACCOMPLISHED EMERGENCY FLOOR LIGHT SYSTEM CHECK AND POWER SUPPLY CHECK WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE INCIDENT AND ACFT RETURNED TO SERVICE. (W) 2L73 4F A22WE 19950210005431995021000543EU 1995 2 10 AALA950102 119950123A3150350B53004308 COMPUTER AIRBUS300 A300B4605R 3930308EU E/E COMPT DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW077076A 610 MIA - FLT 2110 - DURING CLIMBOUT, BEGAN RECEIVING ECAM FAILURE MESSAGES WITH NO OTHER ABNORMAL INDICATIONS. UNABLE TO EXTINGUISH ANY OF THE FAILURE MESSAGES. ACFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 FLIGHT WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950210005441995021000544WP 1995 2 10 CKSA95004 119950125A5330 SKIN DOUG DC8 DC861 3021952WP FS 140 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23816CK 45892 YIP - DURING B-CHECK, INSPECTION FOUND EVIDENCE OF SKIN CORROSION AT STA 140 BETWEEN STRINGERS 26 AND 27R. REMOVED CORROSION AND INSTALLED REPAIR PER DC-8 SRM 53-2-1. (W) 2L74 4F 4A25 19950210005451995021000545NM 1995 2 10 CKSA95005 119950130A21707405992 COALESCER BAG BOEING747 747146 NM AIR COND SYST DIRTY A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23701CK 19725 JFK-YIP - FLT 61444 - ON DESCENT, SMOKE BECAME EVIDENT IN THE COCKPIT. PERFORMED COCKPIT SMOKE REMOVAL CHECK LIST. SHUT OFF UPPER DECK ELECTRIC HEATERS, SMOKE DISSIPATED. INSPECTED ENVIRONMENTAL COALESCER BAG AND FOUND DIRTY. REMOVED AND REPLACED COALESCER BAG. OPS CHECKS GOOD. (W) 2L74 4F A20WE 19950210005461995021000546NM 1995 2 10 TAOA019505 119950123A3350OL3071BPEGPL EEL LAMP BOEING727 727254 138408LNM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15912TS 20438 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950210005471995021000547NM 1995 2 10 TAOA019506 119950125A335010000677 EEL BOEING727 727254 138408LNM CABIN INOPERATIVE A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15912TS 20438 THE FWD GALLEY EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950210005481995021000548NM 1995 2 10 TAOA019508 119950121A335010000677 EEL BOEING727 727254 138408LNM CABIN INOP A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15914TS 20251 THE RT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950210005491995021000549NE 1995 2 10 9501892291 219950205A7230 COMPRESSOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01291US 21379 SUSPECTED COMPRESSOR STALL (POSITION UNKNOWN) OCCURRED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ALL ENGINES WERE INSPECTED FOR DAMAGE AND DISCREPANCIES. NONE NOTED. STRONG CROSSWINDS ARE BELIEVED TO BE THE CAUSE OF THIS COMPRESSOR STALL. WIND AT THE TIME WAS REPORTED AS 270 TO 280 DEGREES. AT 20-25 PEAK GUST 38, RUNWAYS IN USE 35 OR 36. 2L73 4F4 F A3WE E2EA 19950210005501995021000550EU 1995 2 10 9501903211 119950206A5230 HANDLE AIRBUS320 A320211 3930320EU AFT CARGO DOOR NOT SECURE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01311US 125 DURING TAKEOFF ROLL, THE AFT CARGO DOOR INDICATED OPEN. THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE POPPED OUT 0.5 INCH. SECURED DOOR HANDLE AND ALL INDICATIONS AND OPERATION NORMAL. 2L72 4F RTA28NM 19950210005511995021000551WP 1995 2 10 9501919106 119950206A7711 PT7 LINE DOUG DC9 DC915 3022036WP PWA JT8 JT8D7 52053NE NR 2 ENGINE FROZEN A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL0196S 47206 654160 NR 2 ENGINE EPR INDICATOR DID NOT GIVE ACCEPTABLE READINGS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. FOUND FROZEN MOISTURE IN THE PT7 LINE. REMOVED LINE, CLEARED BLOCKAGE, AND REINSTALLED LINE. RAN ENGINE. SYSTEM OPERATION WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950210005521995021000552NM 1995 2 10 95FDEA00114 119950206A5313BAC1498740 STRINGER BOEING727 72725 1384006NM BS 435-440 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION (NRO246) FOUND ON STR 19R FROM BS 435-440 RBL 65. REMOVED AND REPLACED STR 19R FROM BS 410.5 - 441 IAW FEDEX SRM 53-10-3 FIG 1 DETAIL II. 2L73 4F A3WE 19950210005531995021000553WP 1995 2 10 ABXA9500072 119950120A53203912073501 FITTING DOUG DC9 DC931 3022065WP LT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING COMPLIANCE OF A.D. 90-18-03; S.B. 57-129, REV. 3, THE LEFT TRAPEZOIDAL PANEL VERTICAL ATTACH FITTING SHOWED A CRACK INDICATION DURING ULTRASONIC INSPECTION. REPLACED ATTACH FITTING IAW E.A. NR AD 57-03213-MA. 2L72 4F A6WE 19950210005541995021000554WP 1995 2 10 ABXA9500073 119950107A5312591036749 FRAME DOUG DC9 DC933F 302207AWP AFT PRESS BLKHD GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING COMPLIANCE OF A.D. 79-24-01; S.B. 53-127, FOUND GOUGE AT 10 O'CLOCK POSITION ON PLUG DOOR STOP. BLENDED OUT GOUGE AT 10 O'CLOCK POSITION IAW DC-9 SRM 51-01. 2L72 4F A6WE 19950210005551995021000555WP 1995 2 10 ABXA9500074 119950123A5320992151029 INTERCOSTAL DOUG DC9 DC932F 3022067WP FS 446 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION FOUND INTERCOSTAL AT LONGERON 8L, STA. 446, ON AFT SIDE OF CARGO DOOR FRAME HAD A HOLE DRILLED IN RADIUS. REPAIRED IAW ABX REA D953-10779-MR. 2L72 4F A6WE 19950210005561995021000556WP 1995 2 10 ABXA9500075 119950124A5320991154623 ANGLE DOUG DC9 DC932F 3022067WP FS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH S.B. 53-241 FOUND LEVEL I CORROSION ON ANGLE FROM LONGERON 25R TO 27L, STA. 996. REPAIRED IAW ABX REA D953-10786-MR. 2L72 4F A6WE 19950210005571995021000557WP 1995 2 10 ABXA9500076 119950124A532099115468 WEB DOUG DC9 DC932F 3022067WP FS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH S.B. 53-241, FOUND LEVEL I CORROSION ON WEB AT LONGERONS 29L AND 27R, STA. 996. REPAIRED IAW ABX REA D953-10786-MR. 2L72 4F A6WE 19950210005581995021000558WP 1995 2 10 ABXA9500077 119950207A25105925379523ABX1 SEAT DOUG DC9 DC941 302207NWP LT COCKPIT LACK OF LUBE A ABXAK NONE O OTHER CRCRUISE 1 GL23967AX 47509 CAPTAIN'S SEAT WILL NOT LOCK IN THE VERTICAL MODE. PERIODICALLY DURING FLIGHT IT SETTLED LOWER. LUBED CAPTAIN'S SEAT AS REQUIRED. COULD NOT DUPLICATE MALFUNCTION. SEAT OPS CHECKED GOOD IN ALL VERTICAL POSITIONS. 2L72 4F A6WE 19950210005591995021000559WP 1995 2 10 ABXA9500078 119950208A3260 WIRE DOUG DC9 DC933F 302207AWP RT MLG OPEN A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23933AX 47291 WHEN LANDING GEAR EXTENDED, RIGHT GEAR UNSAFE AND RIGHT LANDING GEAR LIGHTS DID NOT ILLUMINATE. RECYCLED GEAR. RIGHT LANDING GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RIGHT LANDING GEAR LIGHT ILLUMINATED. REPAIRED WIRE NR 2G206E24 NEAR TERMINAL BOARD S3-66 PER STANDARD PROCEDURES AND PRINT NR 32-61-00. CYCLED GEAR. OPS CHECKED GOOD. 2L72 4F A6WE 19950210005601995021000560SO 1995 2 10 COM11765 119950208A5753PE610261 ROLLERS EMB 120 EMB120RT SO LT TE FLAP WORN A COMAK NONE S AFFECT SYSTEMS UKUNKNOWN 1 SO011117H 120117 FLAP DISAGREEMENT WARNING. REPLACED LT OUTBD FLAP ROLLERS. 2L72 4T RTA31SO 19950210005611995021000561SO 1995 2 10 COM11766 119950206A5753 BONDING STRAP EMB 120 EMB120RT SO TE FLAPS BINDING A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01267CA 120259 FLAP DISAGREE WARNING WHENS FLAPS SELECTED UP. FLAP BONDING STRAP WAS INTERFERRING WITH INBD LT FLAP. REPLACED BONDING STRAP. 2L72 4T RTA31SO 19950210005621995021000562SO 1995 2 10 COM11767 119950206A27523203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION LDLANDING 1 SO01161CA135214773 120143 OUTBD FLAP ASYMMETRY WARNING AFTER LANDING. REPLACED LT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950210005631995021000563SO 1995 2 10 COM11768 119950207A27503471001001 FLAP ANNUNCIATOR EMB 120 EMB120RT SO INST PANEL DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01269CA5350 120263 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. REPLACED THE FLAP ANNUNCIATOR UNIT. 2L72 4T RTA31SO 19950210005641995021000564SO 1995 2 10 COM11769 119950207A5753PE610261 ROLLER EMB 120 EMB120RT SO LT/RT TE FLAPS WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01269CA 120263 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. REPLACED THE LT AND RT OUTBD FLAP ROLLERS. 2L72 4T RTA31SO 19950210005651995021000565EU 1995 2 10 COM31028 119950206A2450A2042C PDU SAAB SF340 SF340A 7850100EU LEFT DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01320CA8326 637 340A064 EMERGENCY BUS IS ACTIVATED WHEN ALL POWER IS OFF. REPLACED THE LT POWER DISTRIBUTION UNIT. 2L72 4T RTA52EU 19950210005661995021000566EU 1995 2 10 COM31029 119950206A2720MS3116F84P CONNECTOR SAAB SF340 SF340A 7850100EU RUDDER DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01340SF 340A014 RUDDER LIMITER WARNING ACTIVATED. REPLACED DEFECTIVE WIRING CONNECTOR ON RUDDER LIMITER OVERRIDE ACTUATOR. 2L72 4T RTA52EU 19950210005671995021000567EU 1995 2 10 COM31030 119950206A7603 CABLE ASSY SAAB SF340 SF340A 7850100EU LT/RT BINDING A COMAK NONE O OTHER UKUNKNOWN 1 SO01358CA 340A047 POWER LEVERS ARE DIFFICULT TO MOVE. REPLACED DEFECTIVE SECTIONS OF LT AND RT POWER CONTROL CABLES. LT P/N: C82180-3; RT P/N: C82224-7; RT P/N: C82146-3. 2L72 4T RTA52EU 19950210005681995021000568EU 1995 2 10 COM31031 119950206A32465009237 BEARING RACE 510488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA10218516 920174 340A064 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL SUB-ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR BUSHING REPAIR. 2L72 4T RTA52EU 19950210005691995021000569EA 1995 2 10 COM60410 119950206A2720601R152261 TRIM CONTL PANEL CNDAIRCL600 CL6002B19 EA RUDDER DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01924CA 7026 RUDDER TRIM IS INOP. REPLACED TRIM CONTROL PANEL. 2L72 4F RTA21EA 19950210005701995021000570NM 1995 2 10 UP202206 119950208A575465162261 FLAP BOEING727 727173C 1384059NM NR 2 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND DAMAGE DUE TO EXCESSIVE CORROSION, REMOVED AND REPLACED NR 2 K-FLAP. INSTALLED REPAIR IAW MM 27-81-1. 2L73 4F A3WE 19950210005711995021000571NM 1995 2 10 UP202207 119950208A575465162251 FLAP BOEING727 727173C 1384059NM NR 3 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP I/B LOWER BONDING JUMPER UPPER AND LOWER ATTACH POINTS. INSTALLED REPAIR IAW SRM 57-50-1. 2L73 4F A3WE 19950210005721995021000572NM 1995 2 10 UP202208 119950208A575465162271 FLAP BOEING727 727173C 1384059NM NR 6 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP O/B UPPER ATTACH LUG I/B SIDE AROUND FASTENERS. INSTALLED REPAIR IAW SRM 57-50-1. 2L73 4F A3WE 19950210005731995021000573NM 1995 2 10 UP202209 119950208A5753651859933 FLAP BOEING727 727173C 1384059NM NR 7 TE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 7 FLAP CARRIAGE SPINDLE AND YOKE. INSTALLED REPAIR IAW MM 27-51-13. 2L73 4F A3WE 19950210005741995021000574NM 1995 2 10 UP202210 119950208A5320651759359 DOOR THRESHOLD BOEING727 727173C 1384059NM FS 304 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLIGHT DECK DOOR THRESHOLD SILL AROUND NUTPLATES AT STA 304, WL 208, RBL 12, LBL 8. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2 AND 51-10-6. 2L73 4F A3WE 19950210005751995021000575NM 1995 2 10 UP202211 119950208A5320651986219 CHORD BOEING727 727173C 1384059NM FS 344-351 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK IN HORIZONTAL FLANGE OF UPPER LEFT HAND NOSE CHORD FROM BS 344-351, LBL 15, WL 169; CRACK RUNS TO A PREVIOUS REPAIR AT BS 340. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-1, 51-20-4 AND 51-30-2. 2L73 4F A3WE 19950210005761995021000576NM 1995 2 10 UP202212 119950208A5320 ANGLE BOEING727 727173C 1384059NM FS 350 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON ANGLE BS 350 WL 170-174 LBL 15. INSTALLED REPAIR IAW SRM 51-10-2, 51-20-4, 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950210005771995021000577NM 1995 2 10 UP202213 119950208A5755 SKIN BOEING727 727173C 1384059NM NR 14 SPOILER DISBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 14 SPOILER HAS AN AREA OF DISBOND ON I/B FORWARD CORNER UPPER SURFACE. INSTALLED REPAIR IAW SRM 51-20-151. 2L73 4F A3WE 19950210005781995021000578NM 1995 2 10 UP202214 119950208A53206518415111 STIFFENER BOEING727 727173C 1384059NM FS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND STIFFENER CORRODED BEYOND LIMITS AT BS 344 LBL 15 WL 169. INSTALLED REPAIR IAW SRM 51-20-4, 51-10-1, 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950210005791995021000579NM 1995 2 10 UP202215 119950208A5344 HINGE FITTING BOEING727 727173C 1384059NM MID GALLEY DOOR CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND MID GALLEY DOORWAY UPPER HINGE CUTOUT CASTING TO BE CORRODED. INSTALLED REPAIRS IAW SRM 51-30-2, 51-10-2, 51-30-5, 51-20-4, 51-30-8 AND OHM 20-41-02. (PART NUMBERS - 65-18252-3 AND 65-16722-58). 2L73 4F A3WE 19950210005801995021000580NM 1995 2 10 UP202216 119950208A5330 SKIN BOEING727 727173C 1384059NM BS 860-870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND UPPER FUEL CELL SKIN CORRODED AT BS 860-870, LBL 60-70. INSTALLED REPAIR IAW UPS EO 727-57-1081. 2L73 4F A3WE 19950210005811995021000581NM 1995 2 10 UP202217 119950208A551165382051 SPAR BOEING727 727173C 1384059NM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND LT FRONT STAB STA 124 HAS CRACK IN UPPER SPAR IN STAB, UPPER FLANGE WHERE SPAR HAS BEEN PREVIOSLY BLENDED. (CORROSION ALSO FOUND). INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2, 55-10-2, AND 65-20661. 2L73 4F A3WE 19950210005821995021000582NM 1995 2 10 UP202218 119950208A5520 STIFFENER BOEING727 727173C 1384059NM ELEV STA 167 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND BEAD STIFFENER CRACKED AT APROX. R.E.S. 167 APPROX. 3075 INCH FROM TRAILING EDGE. INSTALLED REPAIR IAW SRM 55-20-3. 2L73 4F A3WE 19950210005831995021000583NM 1995 2 10 UP202220 119950208A5320655343314 FITTING BOEING727 727173C 1384059NM CARGO DOORWAY CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND AFT CARGO DOORWAY STOP PAD FITTING ON AFT DOORWAY AT STR 25 TO BE CORRODED. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950210005841995021000584NM 1995 2 10 UP202221 119950208A5311 FRAME BOEING727 727173C 1384059NM BS 580 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND FASTENER HOLES ON THE BS 580 FRAME AT OR NEAR STR 19R TO 22R EXHIBITS CORROSION INDICATION. INSTALLED REPAIR IAW SRM 51-40-3. 2L73 4F A3WE 19950210005851995021000585NM 1995 2 10 UP202222 119950208A575465162242 RIB BOEING727 727173C 1384059NM NR 8 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 2ND RIB IN FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND DWG 65-16224. 2L73 4F A3WE 19950210005861995021000586NM 1995 2 10 UP202223 119950208A575465162212 RIB BOEING727 727173C 1384059NM NR 5 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT THIRD RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9. 2L73 4F A3WE 19950210005871995021000587NM 1995 2 10 UP202224 119950208A575465162212 RIB BOEING727 727173C 1384059NM NR 5 LE FLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT 2ND RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9. 2L73 4F A3WE 19950210005881995021000588NM 1995 2 10 UP202225 119950208A575465162212 RIB BOEING727 727173C 1384059NM NR 5 LE FLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT 4TH RIB IN FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9. 2L73 4F A3WE 19950210005891995021000589NM 1995 2 10 UP202226 119950208A575465162222 RIB BOEING727 727173C 1384059NM NR 6 LE FLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT 3RD RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9. 2L73 4F A3WE 19950210005901995021000590NM 1995 2 10 UP202227 119950208A5510 BEAM BOEING727 727173C 1384059NM LT HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LT HORIZ. STAB. LOWER T/E BEAM AT ELEVATOR STA 169-157, STA 142 AND STA 125-121. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950210005911995021000591NM 1995 2 10 UP202228 119950208A575465162261 ATTACH LUG BOEING727 727173C 1384059NM NR 2 TE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP O/B BULLNOSE ATTACH POINT LUG UPPER SURFACE AROUND FASTENERS. INSTALLED REPAIR IAW MM 27-81-1. 2L73 4F A3WE 19950210005921995021000592NM 1995 2 10 UP202230 119950208A5320 EXPANSION LINK BOEING727 727173C 1384059NM FS 740-760 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON EXPANSION LINK AROUND NUTPLATES STA 740-760, RBL 25, WL 208. SEAT TRACK ALSO FOUND OUT OF LIMITS. INSTALLED REPAIR IAW OHM 20-50-03 AND 20-50-01, 51-10-1, 51-10-2, 51-10-6, 51-20-4, 51-30-2 AND MM 51-20-151. (P/N 69-24621-3 AND 65-34144-23). 2L73 4F A3WE 19950210005931995021000593NM 1995 2 10 UP202231 119950208A5320655343321 DOORWAY STOP BOEING727 727173C 1384059NM FS 740-760 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON AFT CARGO DOORWAY STOP PAD FITTING ON AFT DOORWAY AT STR 24. INSTALLED REPAIR IAW SRM 51-30-2 AND 51-10-2. 2L73 4F A3WE 19950210005941995021000594NM 1995 2 10 UP202232 119950208A575465162221 RIB BOEING727 727173C 1384059NM NR 3 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT 9TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3. 2L73 4F A3WE 19950210005951995021000595NM 1995 2 10 UP202233 119950208A575465162222 RIB BOEING727 727173C 1384059NM NR 6 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT 3RD RIB OUT FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9. 2L73 4F A3WE 19950210005961995021000596NM 1995 2 10 UP202234 119950208A575465162222 RIB BOEING727 727173C 1384059NM NR 6 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RT (O/B) ACTUATOR ATTACH POINT RIB FLANGE IS CRACKED COMMON TO COVE PANEL LOWER ATTACHMENT STRINGER. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9. 2L73 4F A3WE 19950210005971995021000597NM 1995 2 10 UP202235 119950208A575465162242 TRACK BOEING727 727173C 1384059NM NR 8 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT I/B AND O/B TRACK COMMON TO SKIN ANGLES ARE CRACKED. INSTALLED REPAIR IAW UPS OHM 57-51-31, SRM 51-30-2 AND IPC 57-50-1-1. 2L73 4F A3WE 19950210005981995021000598NM 1995 2 10 UP202236 119950208A5330 SKIN BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LOWER SIDE OF UPPER FUEL SKIN BS 870, LBL 65 AND RBL 65. INSTALLED REPAIR IAW SRM 51-30-2 AND UPS EO 727-57-1081. 2L73 4F A3WE 19950210005991995021000599NM 1995 2 10 UP202237 119950208A5320651620254 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON WEB STIFFENER BS 870 RBL 24.5. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950210006001995021000600NM 1995 2 10 UP202238 119950208A5320651620216 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON WEB STIFFENER BS 870 RBL 51. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950210006011995021000601NM 1995 2 10 UP202239 119950208A5320651620215 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB WL 171 STIFFENER AT LBL 50.5. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950210006021995021000602NM 1995 2 10 UP202240 119950208A5312 BULKHEAD BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD SIDE OF 870 BULKHEAD WEB AT TEARSTRAP ON MAIN LANDING GEAR BULKHEAD FROM, LBL 20 RBL 30 WL 160. INSTALLED REPAIR IAW SRM 53-10-9, 51-30-2 AND UPS EO 727-53-1462. 2L73 4F A3WE 19950210006031995021000603NM 1995 2 10 UP202241 119950208A5320BAC1503100024 BEAM BOEING727 727173C 1384059NM BS 745 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LOWER LONGITUDINAL BEAM CHORD, RBL 13 WL 157 BS 745. INSTALLED REPAIR AIW SRM 51-10-2, 51-30-2 AND 51-40-4. 2L73 4F A3WE 19950210006041995021000604NM 1995 2 10 UP202242 119950209A5320652617314 INTERCOSTAL BOEING727 727173C 1384059NM BS 326-344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INTERCOSTAL IN SEVERAL AREAS BS 326-344, LBL 30, WL 208. INSTALLED REPAIR IAW SRM 51-10-1AND 51-30-2. 2L73 4F A3WE 19950210006051995021000605WP 1995 2 10 UPS802188 119950202A5320 DOOR JAMB DOUG DC8 DC871F 302199DWP FS 1660 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN 'B' CHECK MAINTENANCE REPORTED LT AFT SERVICE DOOR AFT UPPER CORNER OF FUSELAGE CUTOUT STA 1660-6 CRACKS COMING FROM FASTENER HOLES. REPAIRED PER EO DC8-5330-4067-A. DOOR JAMB CORNER DAMAGE - TEMP REPAIR. 2L74 4F RT4A25 19950210006061995021000606WP 1995 2 10 UPS802189 119950207A532097549453 WEBBING DOUG DC8 DC871F 302199DWP FS 1180 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON WEBBING, FS 1180 LONGERON 34R-35R. INSTALLED REPAIR IAW UPS EO DC8-5310-6599-A. 2L74 4F RT4A25 19950210006071995021000607WP 1995 2 10 UPS802190 119950207A5313S264571612000 LONGERON DOUG DC8 DC871F 302199DWP FS 380-400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 35L, FS 380-400. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006081995021000608WP 1995 2 10 UPS802191 119950207A532003270755T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 320-405 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON INNER DOUBLER, FS 320-405, LONGERON 35L-34R. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006091995021000609WP 1995 2 10 UPS802192 119950207A53200637075T6 SHEAR TIE DOUG DC8 DC871F 302199DWP FS 1240 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON SHEAR TIE, LONGERON 35L-36, FS 1240. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006101995021000610WP 1995 2 10 UPS802193 119950207A53113614944509 BELTFRAME DOUG DC8 DC871F 302199DWP FS 1360 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON BELTFRAME, FS 1360, LONGERON 34L-33R. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2. 2L74 4F RT4A25 19950210006111995021000611WP 1995 2 10 UPS802194 119950207A53204640162IN END FITTING DOUG DC8 DC871F 302199DWP FS 1400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON FS 1400, END FITTING, LONGERON 21L. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006121995021000612WP 1995 2 10 UPS802195 119950207A53203755845 FITTING DOUG DC8 DC871F 302199DWP FS 1180 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND MODERATE CORROSION ON B/T FITTING, FS 1180, LONGERON 35R-36. INSTALLED REPAIR IAW SRM 53-2-0, FIGURE 2D. 2L74 4F RT4A25 19950210006131995021000613WP 1995 2 10 UPS802196 119950207A5320 FITTING DOUG DC8 DC871F 302199DWP FS 280 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON B/T FITTING LONGERON 33R-34R, FS 280. INSTALLED REPAIR IAW SRM 53-2-0. 2L74 4F RT4A25 19950210006141995021000614WP 1995 2 10 UPS802197 119950207A532037558441 FITTING DOUG DC8 DC871F 302199DWP FS 1153 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON B/T FITTING, FS 1153, LONGERONS 30L-31L. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006151995021000615WP 1995 2 10 UPS802198 119950207A532037558421 FITTING DOUG DC8 DC871F 302199DWP FS 1153 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING, FS 1153, LONGERONS 27L-28L. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006161995021000616WP 1995 2 10 UPS802199 119950207A53134617670501 LONGERON DOUG DC8 DC871F 302199DWP FS 110 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 25R SPLICE FITTING, FS 110. INSTALLED REPAIR IAW SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 19950210006171995021000617WP 1995 2 10 UPS802200 119950207A5320564619318 ANGLE DOUG DC8 DC871F 302199DWP FS 810 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON FLOOR WEB ANGLE, LONGERON 21R, F.S. 810. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950210006181995021000618WP 1995 2 10 UPS802201 119950207A53209754003505 DOUBLER DOUG DC8 DC871F 302199DWP FS 267-273 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION AT DOUBLER, FS 267 TO 273, LONGERON 35L. INSTALLED REPAIR IAW UPS EO DC8-5310-6602. 2L74 4F RT4A25 19950210006191995021000619WP 1995 2 10 UPS802203 119950207A5312564091549 BULKHEAD WEB DOUG DC8 DC871F 302199DWP FS 980 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND 1 INCH LONG CRACK ON PRESSURE BULKHEAD WEB AT FS 980, RBL 2.65. INSTALLED REPAIR IAW UPS EO DC8-53-1308. 2L74 4F RT4A25 19950210006201995021000620WP 1995 2 10 UPS802204 119950207A53200907075T6 JAMB DOUBLER DOUG DC8 DC871F 302199DWP FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND EXTERNAL SKIN DOUBLER HAS SEVERAL CRACKS ON FORWARD CARGO DOOR JAMB CUTOUT. LOWER FWD CORNER. INSTALLED REPAIR IAW UPS EO DC8-5310-6566-B. 2L74 4F RT4A25 19950210006211995021000621WP 1995 2 10 UPS802205 119950207A52309754100125 BEAM DOUG DC8 DC871F 302199DWP CARGO SLIDE DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 WHILE IN 'C' CHECK MAINTENANCE FOUND CARGO SLIDE DOOR NR 5 BEAM INBOARD CHANNEL CRACKED IN TWO LOCATIONS. INSTALLED REPAIR IAW UPS EO DC8-5230-6564-A. 2L74 4F RT4A25 19950210006221995021000622NE 1995 2 10 95ZZZX698 219950128A7310 FUEL FILTER BOEING747 747124 1384874NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE CLOGGED A P5CAO OTHER O OTHER DEDESCENT 1 WP23630SJ 19733 663048 ON DESCENT INTO HKG, NR 4 ENGINE STAYED IN IDLE WITH NO THROTTLE RESPONSE. APPLIED FUEL HEAT WITH NO HELP. ATTEMPTED RESTART TO RESCHEDULE FUEL. STILL NO RESPONSE. LANDED WITHOUT INCIDENT. MAIN FUEL FILTER CHECKED AND REPLACED IAW MM 73-11-00. ENGINE RUN CARRIED OUT. ALL INDICATIONS NORMAL. THROTTLE CYCLING RESPONSE NORMAL. AIRCRAFT DISPATCHED. NO FURTHER DISCREPANCY NOTED. 2L74 4F4 F A20WE E20EA 19950210006241995021000624NM 1995 2 10 95ZZZX701 119950119A24332421F10 FUSE DHAV DHC8 DHC8102 2809003NM RIGHT BLOWN A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15846MA 344 MSP - FLT 3209 - ON CLIMB-OUT, THE RIGHT TRU CIRCUIT BREAKER TRIPPED. THE CREW RESET THE CIRCUIT BREAKER AND IT TRIPPED AGAIN. THE AIRCAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT TRU, PN 28VS200Y4D, AND A BLOWN AC GENERATOR LIMITED FUSE, PN 2421-F10. SYSTEM OPERATED SATISFACTORILY. REFERENCE CONTROL NR MALA954248. (X) 2H72 4T RTA13NM 19950210006251995021000625SW 1995 2 10 LOSA9507 119950128A3213MS28775142 PACKING SWRNGNSA227 SA227AC 8780603SW RT MLG STRUT WORN A LOSAK NONE K FLUID LOSS ININSP/MAINT 1 WP23165SW24554 AC514 LAS - RIGHT MAIN GEAR OLEO STRUT LEAKING. HYDRAULIC FLUID LEAKING ABOUT 1 DROP PER 4-5 SECONDS. RIGHT MAIN GEAR STRUT REPACKED IAW SA-227 MM CHAPTER 32-10-10. OPERATIONAL CHECKS AND LEAK CHECK PERFORMED. RESULTS: SATISFACTORY. (X) 1L72 4T A8SW 19950210006281995021000628SW 1995 2 10 MALA95249 119950119A5730 SKIN SWRNGNSA227 SA227AC 8780603SW RT WING DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER WING SKIN SCRATCHED AND DENTED. REPAIRS COMPLETED IAW FAC LAR 95-MALA-026 AND SRM 57-90-20 REPAIR NR 10. (X) 1L72 4T A8SW 19950210006301995021000630NM 1995 2 10 MALA954248 119950119A243328VS200Y4D TRU DHAV DHC8 DHC8102 2809003NM RIGHT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15846MA 344 MSP - FLT 3209 - ON CLIMB-OUT, THE RIGHT TRU CIRCUIT BREAKER TRIPPED. THE CREW RESET THE CIRCUIT BREAKER AND IT TRIPPED AGAIN. THE AIRCAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT TRU, PN 28VS200Y4D, AND A BLOWN AC GENERATOR LIMITED FUSE, PN 2421-F10. SYSTEM OPERATED SATISFACTORILY. REFERENCE CONTROL NR 95ZZZX701. (X) 2H72 4T RTA13NM 19950210006311995021000631SW 1995 2 10 MALA954250 119950119A2720 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER BENT A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE BENT. REPAIRS COMPLETED BY REPLACING TORQUE TUBE IAW FAC 27-20-20, 27-00-00, AND SRM 51-00-00, PAGE 3. (X) 1L72 4T A8SW 19950210006321995021000632SW 1995 2 10 MALA954251 119950119A53202722093106 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 174 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER INTERCOSTAL, PN 27-22093-106, AT FS 174, CRACKED. REPAIRS COMPLETED TO THE RT INTERCOSTAL IAW FAC SRM. (X) 1L72 4T A8SW 19950210006331995021000633SW 1995 2 10 MALA954252 119950119A5320 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 133 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEUDLED INSPECTION, MAINTENANCE FOUND RT INTERCOSTAL CRACKED AT FS 133 AT THE RELIEF RADIUS CUT-OUT. REPAIRS COMPLETED IAW FAC ARP 53-20-9148 AND SRM. (X) 1L72 4T A8SW 19950210006341995021000634SW 1995 2 10 MALA954253 119950119A57532731141001 SUPPORT DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT FLAP WALKING BEAM ROLLER BEARING SUPPORT DOUBLER, PN 27-31141-001, WORN. REPAIRS COMPLETED THROUGH A PART-FOR-PART REPLACEMENT IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950210006351995021000635SW 1995 2 10 MALA954254 119950119A53202722104031 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 212 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT INTERCOSTAL, PN 27-22104-031, AT FS 212, CRACKED AT THE CORNER RELIEF RADIUS. REPAIRS COMPLETED IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950210006361995021000636SW 1995 2 10 MALA954255 119950119A53112722125021 BELT FRAME SWRNGNSA227 SA227AC 8780603SW FS 133 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22125-021, CRACKED AT THE UPPER OUTBOARD RELIEF RADIUS. REPAIRS COMPLETED AT FS 133 IAW FAIRCHILD ARP 53-20-9029 AND THE SRM. (X) 1L72 4T A8SW 19950210006371995021000637SW 1995 2 10 MALA954256 119950119A53202722093107 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 174 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND LT LOWER INTERCOSTAL, PN 27-22093-107, AT FS 174, CRACKED AT THE RELIEF RADIUS. REPAIRS COMPLETED TO THE LT LOWER INTERCOSTAL AT FS 174 IAW FAIRCHILD ARP 53-20-9148 AND SRM. (X) 1L72 4T A8SW 19950210006381995021000638SW 1995 2 10 MALA954257 119950119A53112722093146 BELT FRAME SWRNGNSA227 SA227AC 8780603SW FS 145 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-146, AT FS 145, CRACKED AT THE UPPER OUTBOARD RELIEF RADIUS. REPAIRS COMPLETED IAW FAIRCHILD ARP 53-20-9029 AND THE SRM. (X) 1L72 4T A8SW 19950210006391995021000639SW 1995 2 10 MALA954258 119950119A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW WS 27.103 WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT FLAP WALKING BEAM ROLLER BEARING DOUBLER AT STA 27.103, PN 27-31141-001, WORN. REPAIRS COMPLETED THROUGH A PART-FOR-PART REPLACEMENT OF THE ROLLER DOUBLER IAW FAC SRM. (X) 1L72 4T A8SW 19950210006401995021000640SW 1995 2 10 MALA954259 119950119A53112722104035 BELT FRAME SWRNGNSA227 SA227AC 8780603SW FS 212 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSO - DURING SCHEDULED INSPECTION - MAINTENANCE FOUND LOWER BELT FRAME, PN 27-22104-035, AT FS 212, CRACKED AT THE UPPER, OUTBOARD RELIEF RADIUS. REPAIRS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAIRCHILD ARP 53-20-9029 AND THE SRM. (X) 1L72 4T A8SW 19950210006411995021000641SW 1995 2 10 MALA954260 119950119A53472721052035 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 107.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND PILOT'S SEAT TRACK ATTACHMENT NUT PLATES ON FS 107.060 CRACKED. A REPAIR ANGLE DOUBLER WAS ATTACHED TO THE FRAME, PN 27-21052-035 IAW FAIRCHILD ARP 53-10-8913, REVISION A AND THE SRM (X) 1L72 4T A8SW 19950210006421995021000642SW 1995 2 10 MALA954261 119950119A53472721052035 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 107.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND COPILOT'S SEAT TRACK ATTACHMENT NUT PLATES ON FS 107.060 CRACKED. REPAIRS WERE COMPLETED TO THE FRAME, PN 27-21052-035, IAW FAIRCHILD ARP 53-10-8913, REVISION A AND THE SRM. (X) 1L72 4T A8SW 19950210006431995021000643SW 1995 2 10 MALA954262 119950119A53202725006001 BRACKET SWRNGNSA227 SA227AC 8780603SW COCKPIT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FORWARD, OUTBOARD PILOT'S SEAT TRACK SUPPORT BRACKET CRACKED AT THE TRACK ATTACHMENT NUT PLATES. REPAIRS COMPLETED TO THE BRACKET, PN 27-25006-001, BY INSTALLING A DOUBLER IAW FAIRCHILD ARP 53-10-9322 AND THE SRM. (X) 1L72 4T A8SW 19950210006441995021000644SW 1995 2 10 MALA954263 119950119A53202725008001 BRACKET SWRNGNSA227 SA227AC 8780603SW COCKPIT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FORWARD, INBOARD PILOT'S SIDE SEAT TRACK SUPPORT BRACKET, PN 27-25008-001, CRACKED AT THE TRACK ATTACHMENT NUT PLATES. REPAIRS WERE COMPLETED TO THE SEAT TRACK BY INSTALLING A REPAIR DOUBLER IAW FAIRCHILD ARP 53-10-9322 AND SRM. (X) 1L72 4T A8SW 19950210006451995021000645SW 1995 2 10 MALA954271 119950122A77222719149003 EGT GAUGE SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15436MA AC719 MSP - FLT 3231 - ON CLIMB-OUT, RIGHT ENGINE EGT DROPPED TO 250 DEGREES WITH ALL OTHER ENGINE GAUGES WORKING NORMALLY. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE EGT GAUGE. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950210006461995021000646WP 1995 2 10 MALA954272 219950122A720031025408 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15428MA AC646 P44412C FLT 3185 - ON CLIMB-OUT FROM DTW, THE CREW RECEIVED A LEFT ENGINE FIRE WARNING LIGHT AND THE LEFT SUB PANEL FIRE LIGHT. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT ENGINE. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T4 T A8SW E4WE 19950210006471995021000647SW 1995 2 10 MALA954274 119950125A2913PVC0442C HYDRAULIC PUMP SWRNGNSA227 SA227AC 8780603SW LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL152693C AC659B MSP - FLT 3327 - IN CRUISE FLIGHT, LEFT HYDRAULIC PRESSURE ANNUNCIATOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LEFT ENGINE HYDRAULIC PUMP AND PRESSURE SWITCH. SYSTEM OPERATED SATISFACTORILY. SWITCH, PN SS1012-7. (X) 1L72 4T A8SW 19950210006501995021000650WP 1995 2 10 MGMA950018 119950108A3350 CONNECTOR DOUG DC8 DC862 3021970WP CABIN EEL LOOSE A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23802MG 46098 EMERGENCY LIGHT OVER SEAT 21C IN THE AISLE IS INOP. REPAIRED LOOSE CONNECTION TO LIGHT. OPS CHECKED NORMAL. TOTAL CYCLES 12,975. (Z) 2L74 4F 4A25 19950210006511995021000651WP 1995 2 10 MGMA950028 119950108A335020191A BATTERY PACK GRIMES 20131A DOUG DC8 DC862 3021970WP CABIN EEL DISCHARGED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23802MG 30342 46098 EMERGENCY LIGHT OVER L-1 INOP. REPLACED BATTERY PACK. OPS CHECKED NORMAL. TOTAL CYCLES 12,975. (Z) 2L74 4F 4A25 19950210006521995021000652WP 1995 2 10 ORJA95002 119950114A3350 EEL DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11840RA 49424 EMPENNAGE EMERGENCY LIGHTS INOP. RESET BATTERY. SYSTEM CHECKS GOOD. (X) 2L72 4F A6WE 19950210006531995021000653WP 1995 2 10 ORJA95003 119950117A3350 EEL DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11822RA 49932 EMERGENCY FLOOR LIGHTS INOP AT 6 AND 7 DEF. REPLAMPED AND RESECURED FLOOR TRACK LIGHTING. OPS CHECK OKAY. (X) 2L72 4F A6WE 19950210006541995021000654WP 1995 2 10 ORJA95006 119950125A3350EA1D131D3 EEL BATTERY NICAD DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11841RA 49421 ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY, OPS CHECKED GOOD. (X) 2L72 4F A6WE 19950210006621995021000662EA 1995 2 10 95ZZZW94 119950104A323062380 SEQUENCE VALVE DHAV DHC7 DHC7102 2802708EA NLG WW FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07903HA8322 061 ORF-DCA - FLT 3003 - NOSE GEAR UNSAFE LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACT SELECTED ON CLIMB-OUT. ACFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED UPPER NOSE LANDING GEAR SEQUENCE VALVE. 2H74 4T A20EA 19950210006711995021000671NM 1995 2 10 AALA950001 119950102A2612FBD1542503 FIRE LOOP BOEING767 767323 1385205NM NR 1 ENG DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07372AA 25199 JFK - FLT 59 - DURING CLIMB-OUT, BOTH A AND B ENGINE FIRE WARNING LOOPS ON NR 1 ENGINE ILLUMINATED. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED BOTH FIRE WARNING LOOP DETECTORS. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950210006721995021000672EU 1995 2 10 AALA950002 119950102A3231 BUMPER FOKKERF28 F28MK0100 4990807EU LT MLG OUT OF ADJUST A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071416A 11395 RDU - FLT 1721 - AFTER TAKEOFF, THE LT MLG WARNING LIGHT ILLUMINATED. CYCLED GEAR WITH SAME RESULTS. RETURNED TO RDU AND LANDED WITHOUT INCIDENT. ADJUSTED LT MLG DOOR BUMPER STOP JAM AND PROPERLY SAFETY WIRED. (W) 2L72 4F RT 19950210006731995021000673NM 1995 2 10 AALA950012 119950105A3350A3060819104 EEL STRIP DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071753 48487 JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEAT 5A AND L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L73 4F RTA22WE 19950210006741995021000674WP 1995 2 10 AALA950057 119950112A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07221AA 49172 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT CABIN UNDER EXIT DECAL INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN UNDER EXIT DECAL. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F A6WE 19950210006801995021000680WP 1995 2 10 CAL950048 119950111A5350 CLIP DOUG DC9 DC982 3022082WP TAIL CONE BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW0918835 49439 HOU - THE FORCE REQUIRED TO PULL HANDLE FROM CLIPS WAS TOO LOW DURING TAIL CONE DROP TEST. REMOVED AND REPLACED BROKEN CLIP. (W) 2L72 4F A6WE 19950210006811995021000681SO 1995 2 10 WTAA950037 119950108A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A AWTAAO OTHER J WARNING INDICATION LDLANDING 1 WP17285UE 120153 SFO - ACFT REPORTED TO ROLL AFTER TAKEOFF WITH FLAPS IN TAKEOFF CONFIGURATION. NO ASSOCIATED FLAP WARNING INDICATION REPORTED. ACFT ROLL TENDENCY RESOLVED AFTER CREW RETRACTED FLAPS. PROBLEM REOCCURRED ON LANDING WITH FLAPS SELECTED TO 25 DEGREES. FLAP DISAGREEMENT WARNING ASSOCIATED WITH SECOND EVENT. MAINTENANCE FOUND RT O/B FLAP ACTUATOR FAILS TO EXTEND PAST 25 DEGREES. REPLACED FLAP ACTUATOR. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950210006821995021000682SO 1995 2 10 WTAA950039 119950110A5610 SEAL EMB 120 EMB120RT SO LT WINDSHIELD LOOSE A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17274UE 120054 SFO - UNIDENTIFIED NOISE REPORTED IN COCKPIT DURING CLIMB. ACFT RETURNED TO STA WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT TO LOCATE SOURCE OF NOISE. FOUND 6 INCH PORTION OF 'PRC' SEAL LOOSE AT TOP OF CAPTAIN'S WINDSHIELD. REMOVED EXCESS MATERIAL. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950210006831995021000683SO 1995 2 10 WTAA950042 119950111A4920 APU EMB 120 EMB120RT SO AFT FUSELAGE MALFUNCTIONED A WTAAK NONE A FLAME/FIRE TXTAXI/GRND HDL 1 WP17201YW 120201 RDM - FLAMES REPORTED FROM APU EXHAUST DURING APU SHUTDOWN ON GROUND. NO ACTION REQUIRED BY FLIGHT OR GROUND CREW TO EXTINGUISH FIRE. FLAMES IMMEDIATELY SUBSIDED FOLLOWING SHUTDOWN. MAINTENANCE INSPECTED APU AND TAILCONE. MINOR PAINT DAMAGE TO TAILCONE NOTED. NO DAMAGE TO APU OR APU EXHAUST REPORTED. PERFORMED OPERATIONAL CHECK OF APU ON GROUND, AND WAS UNABLE TO DUPLICATE DISCREPANCY. PROBABLE CAUSE OF FLAMES WERE EXCESSIVE SURFACE WINDS BLOWING IN APU TAILPIPE. (W) 2L72 4T RTA31SO 19950210006841995021000684SO 1995 2 10 WTAA950049 119950115A27305299 ACTUATORS EMB 120 EMB120RT SO LT/RT HORIZ STABLACK OF LUBE A AWTAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 WP17455UE 120163 SFO-PSP - EN ROUTE, DURING TRANSITION FROM FL 250 TO FL 270, ELECTRIC ELEVATOR TRIM REPORTED STUCK IN NOSE UP POSITION. CREW UNABLE TO ADJUST ELEVATOR TRIM ELECTRICALLY OR MANUALLY. LEVEL FLIGHT ATTITUDE MAINTAINED BY ADDITIONAL APPLICATION OF FWD PRESSURE ON CONTROL YOKE. ACFT CONTINUED TO STA. ELEVATOR TRIM BEGAN TO OPERATE NORMALLY UPON DESCENT AS ACFT PASSED THROUGH 16,00 FEET. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ELEVATOR TRIM SYSTEM. NO DEFECTS NOTED. LUBED ELEVTOR TRIM TAB ACTUATORS. UNABLE TO DUPLICATE DISCREPANCY ON GROUND. ELEVATOR TRIM SYSTEM OPERATIONAL CHECK NORMAL. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950210006851995021000685SO 1995 2 10 WTAA950057 119950116A523012023272001 CARGO DOOR EMB 120 EMB120RT SO AFT FUSELAGE UNSECURED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17286UE 120175 SFO - ACFT FAILED TO PRESSURIZE AFTER DEPARTURE. ACFT RETURNED TO STA WITHOUT INCIDENT. UPON INSPECTION OF ACFT AT GATE, CARGO DOOR HANDLE DISCOVERED UNSECURED. MAINTENANCE INSPECTED CARGO DOOR AND HANDLE, AND NO DEFECTS NOTED. CARGO DOOR OPERATION NORMAL (CARGO DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL 52-70-1). PRESSURIZATION SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950210006861995021000686SO 1995 2 10 WTAA950058 119950118A5270 WARNING LIGHT EMB 120 EMB120ER 3260203SO PAX DOOR ILLUMINATED A WTAAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 WP17275UE 120058 SEA - PASSENGER DOOR WARNING LIGHT REMAINS ILLUMINATED WITH DOOR CLOSED. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950210006871995021000687SO 1995 2 10 WTAA950059 119950117A5270 WARNING LIGHT EMB 120 EMB120RT SO PAX DOOR ILLUMINATED A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17454UE 120155 FAT - PASSENGER DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950217000011995021700001WP 1995 2 17 95ZZZW100 119950111A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6AG O2 MASK DEPLOYED O OTHER CLCLIMB 1 SO11907VJ 47444 ATL-IAD - FLT 192 - DURING CLIMB-OUT, AUTO PRESSURIZATION WENT INOP AND ACFT DEPRESSURIZED AT APPROXIMATELY 10,000 FEET. OXYGEN MASKS IN CABIN DEPLOYED AND CREW PRESSURIZED ACFT MANUALLY. UPON ARRIVAL IN IAD, OXYGEN MASKS WERE STOWED AND AUTO PRESSURIZATION PLACED ON MEL. 2L72 4F A6WE 19950217000021995021700002NE 1995 2 17 95ZZZW101 219950107A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LT FAILED A ANVEAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO03282AT 282 MIA - FLT 5728 - SHORTLY AFTER TO, CREW NOTICED A DROP IN LT ENGINE TQ. WHILE DISCUSSING IT, THEY HEARD A POPPING NOISE AND THE LT TQ DROPPED RAPIDLY. SMOKE WAS PRESENT IN THE COCKPIT AND CABIN. THEY DECLARED AN EMERGENCY AND RETURNED TO MIA. BOTH FIRE BOTTLES WERE DISCHARGED. THE ACFT WAS EVACUATED WITHOUT FURTHER INCIDENT. FOUND METAL IN CHIP DETECTORS AND OIL FILTERS. PROP WAS LOCKED-UP. ENGINE CHANGE WAS COMPLIED WITH. 2H72 4T4 TRTA53EU E20NE 19950217000031995021700003NE 1995 2 17 95ZZZW102 219950112A7261J221P906 PACKING GE 4068T53G01 SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE DISPLACED A NVEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO03203NE1000810008 340B203 JFK - FLT 4942 - CREW SHUTDOWN LT ENGINE IN CRUISE DUE TO LOW OIL PRESSURE. LANDED SAFELY IN JFK. INSPECTION REVEALED OIL LEAKING FROM B-SUMP OIL SCREEN HOUSING. REPLACED O-RINGS ON B-SUMP OIL SCREEN HOUSING, CMM 79-00-00 PG 406. 2L72 4T4 TRTA52EU E8NE 19950217000041995021700004NM 1995 2 17 95ZZZW103 119950124A7933162BL704C OIL TEMP IND BOEING727 727228 NM NR 3 ENGINE MALFUNCTIONED A DHLAO OTHER N FALSE WARNING DEDESCENT 1 SO01727DH 20404 THE NR 3 ENGINE OIL TEMP GAUGE CLIMBED TO PAST RED LINE AND FLICKERED AS MUCH AS 50 DEGREES CELSIUS DURING DESCENT. ACCOMPLISHED ALTERNATE PROCEDURE AOM 5.174 PG 8, 9. CHECKED CONNECTOR AT TEMP BULB AND CLEANED SAME ON ENGINE. SWAPPED INDICATORS FOR TROUBLESHOOTING 2 AND 3. GROUND CHECKS GOOD. 2L73 4F A3WE 19950217000051995021700005WP 1995 2 17 95ZZZW95 119950113A213453895811 PRESS SENSOR DOUG DC9 DC932 3022066WP CABIN FAILED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO111269L 47285 ON CLIMB-OUT, PRESSURIZATION UNCONTROLLABLE IN AUTO AND MANUAL. AUTO PILOT PREVIOUSLY ON MEL. FLIGHT RETURNED TO ATL. REPLACED CABIN PRESSURE DIFFERENTIAL SENSOR. 2L72 4F A6WE 19950217000061995021700006WP 1995 2 17 95ZZZW96 119950116A2450914F5654 BUS PROCT PNL DOUG DC9 DC932 3022066WP ELECT SYST FAILED A VJ6AA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO11908VJ 47321 ATL-MEM - FLT 520 - REPORTED NUMEROUS CIRCUIT BREAKERS WERE POPPING IN COCKPIT. CAPTAIN DECLARED AN EMERGENCY. FLIGHT RETURNED TO ATL. REMOVED AND REPLACED BUS CONT PANEL, OPS CHECK GOOD PER MM 24-52. 2L72 4F A6WE 19950217000071995021700007WP 1995 2 17 95ZZZW97 119950120A2913AS66411L3666 HYD PUMP DOUG DC9 DC932 3022066WP NR 1 ENGINE FAILED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11904VJ 47377 IAD-ATL - FLT 175 - FLIGHT EXPERIENCED A LT SYSTEM HYDRAULIC LOW PRESSURE LIGHT, 300 PSI AFTER PERFORMING THE GEAR UPLATCH CHECK. FLIGHT RETURNED TO IAD FOR REPAIRS. REMOVED AND REPLACED HYDRAULIC PUMP NR 1 ENGINE. 2L72 4F A6WE 19950217000081995021700008WP 1995 2 17 95ZZZW98 119950120A3610D17D87 CLAMP DOUG DC9 DC932 3022066WP LT ENGINE BROKEN A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO111269L 47285 MDW-ATL - FLT 245 - DURING CLIMB-OUT, THE LT ENGINE FIRE WARNING CAME ON, RETARDED POWER LEVER, LIGHT WENT OUT. RETURNED TO MDW. FOUND 13TH STAGE BLANKING CAP OFF, BROKEN CLAMP. REPLACED CAP AND CLAMP, ENGINE OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19950217000091995021700009WP 1995 2 17 95ZZZW99 119950112A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6AG O2 MASK DEPLOYED O OTHER CRCRUISE 1 SO11907VJ 47444 ATL-PHL - FLT 534 - EN ROUTE, OXYGEN MASKS DEPLOYED AUTOMATICALLY DUE TO USE OF AUTO PRESSURIZATION SYSTEM PREVIOUSLY PLACED ON MEL AS INOP. RETURNED TO MANUAL PRESSURIZATION CONTROL AND REGAINED CONTROL. MASK PANELS AT SEAT 4 AB ROW 6 AND 7 AB AND 11 AB DID NOT DEPLOY. PLACED ON MEL 35-2-2 PAR F, G AND H. 2L72 4F A6WE 19950217000101995021700010NM 1995 2 17 CAL950044 119950117A2420BACC18AE35 CIRCUIT BREAKER BOEING737 7373T0 1384582NM NR 1 TRANS BUS FAILED A CALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW0917309 23360 CLE - FLT 1835 - THE ACFT EXPERIENCED AN ELECTRICAL FAILURE WHILE EN ROUTE TO MDW. THE APU WAS STARTED, BUT IT WOULD ONLY POWER THE LT SIDE. THE TRANSFER BUS OFF LIGHT ON THE RT SIDE WAS ON. THE RT SIDE INSTRUMENTS WERE ALL WORKING. THE CREW ELECTED TO DIVERT TO CLE. WHILE EN ROUTE TO CLE THE NR 1 TRANSFER BUS CIRCUIT BREAKER WAS RESET AND ALL ELECTRICAL POWER WAS RESTORED. THE REST OF THE FLIGHT WAS UNEVENTFUL. MAINTENANCE FOUND THE NR 1 TRANSFER BUS CIRCUIT BREAKER INTERNALLY FAILED. THE CIRCUIT BREAKER WAS REMOVED AND REPLACED. THE R3 TRANSFER RELAY WAS ALSO REPLACED AS A PRECAUTIONARY MEASURE AND OPERATION CHECKED GOOD. (W) 2L72 4F RTA16WE 19950217000111995021700011NM 1995 2 17 CAL950055 119950121A3230 RETRACT MECH BOEING727 727243 138408DNM LANDING GEAR LACK OF LUBE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW0958414 22166 LAX - FLT 497 - WHEN THE LANDING GEAR WAS EXTENDED ON APPROACH TO LAX THE THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WITH NO GREEN. THE MLG EXTENDED ON ITS OWN APPROXIMATELY FIVE SECONDS LATER WITH THE NOSE GEAR COMING DOWN WITHIN ANOTHER FIVE SECONDS. THE ACFT LANDED SAFELY WITH ALL THREE GREEN LIGHTS INDICATED AND NO RED. MAINTENANCE PERFORMED A FULL GEAR EXTENSION/RETRACTION PER MM 32-30-00 AND NO DISCREPANCIES WERE FOUND. ALL THREE LANDING GEAR WERE LUBRICATED. THE GEAR WERE RESWUNG AND ALL OPERATION CHECKED GOOD. (W) 2L73 4F RTA3WE 19950217000121995021700012SW 1995 2 17 LOSA9504 119950118A29102718009015 HYD POWER PACK FRCHLDSA227 SA227DC 3377521SW RT HYD SYST MALFUNCTIONED A LOSAE ENGINE SHUTDOWN K FLUID LOSS TXTAXI/GRND HDL 1 WP23454LA DC855B LAS - CREW RPORTED RT ENGINE HYDRAULIC LIGHT REMAINED LIT, AFTER START-UP AND RT HYDRAULIC PRESSURE GAUGE INDICATED ZERO. MAINTENANCE FOUND HYDRAULIC PRESSURE NORMAL AFTER BYPASSING FLAP SYSTEM BY PULLING 'FLAP CONTROL' C/B. RT ENGINE HYDRAULIC PUMP AND FILTER WAS REPLACED PER MM. FLAP CONTROL VALVE WAS CHANGED DUE TO LEAKING AND HYDRAULIC POWER PACK CHANGED TO CORRECT LOW PRESSURE. ACFT RELEASED FOR SERVICE. (W) 1L72 4T RTA18SW 19950217000131995021700013SW 1995 2 17 LOSA9505 119950123A2840CLF540031 FLOAT SWITCH FRCHLDSA227 SA227DC 3377521SW RT WING FUEL TANSTICKING A LOSAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP23452LA DL848B PHX - THE RT FUEL PUMP TRANSFER LIGHT WILL NOT EXTINGUISH. ACFT FERRIED TO MAINTENANCE. REPLACED RT SIDE TRANSFER LIGHT FLOAT SWITCH PER MM. PERFORMED FUNCTIONAL AND LEAK CHECKS. (W) 1L72 4T RTA18SW 19950217000141995021700014SW 1995 2 17 LOSA9506 119950123A7933MS3126E12108 CONNECTOR SWRNGNSA227 SA227AC 8780603SW LT ENGINE CORRODED A LOSAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 WP23165SW AC514 LAX - THE LT ENGINE OIL TEMP GAUGE EXCEEDED RED ARC WHEN SPEED LEVERS BROUGHT TO HIGH. PRESSURE REMAINED IN GREEN ARC, SHUTDOWN LT ENGINE. PERFORMED ENGINE RUNUP AND CHECKED THE OIL TEMP INSIDE OF OIL TANK. CHECKED TEMP TO BE 84 DEGREES CELSIUS. CLEANED AND RESEATED CANNON PLUG ON LT ENGINE TEMP GAUGE PER MAINTENANCE CONTROL. POWER RUN BOTH RT AND LT ENGINES AND TEMP GAUGES CHECKED NORMAL. ACFT RELEASED FOR SERVICE. (W) 1L72 4T A8SW 19950217000151995021700015EU 1995 2 17 RAIA950122 119950119A3110D46302001 CAPTION PANEL BAG JETSTMJETSTM3201 1500217EU COCKPIT FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03867AE8174 867 THE ATTENTION GETTERS WENT OFF ON CAPTION PANEL, WOULD NOT RESET. MAINTENANCE REPLACED CAPTION PANEL. TESTS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950217000161995021700016 1995 2 17 RAIA950124 419950119A612278249024 PCU EMB 120 EMB120RT SO RT ENG LEAKING A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03131AM8990 120158 SBN - FLT 7515 - THE RT ENGINE LOW OIL PRESSURE, CREW DIVERTED TO SBN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT PROPELLER CONTROL UNIT. GROUND CHECK REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (W) 2L72 4T RTA31SO 19950217000171995021700017EU 1995 2 17 RAIA950125 119950119A521091SE13 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03343TE5299 955 FWA - FLT 7513 - THE PAX DOOR CAPTION ILLUMINATED. MAINTENANCE ADJUSTED PAX DOOR HANDLE MICROSWITCH. TEST OF SYSTEM REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950217000181995021700018EU 1995 2 17 RAIA950126 119950117A33503011151 EEL POWER PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03426TE8584 228 STL - FLT 7176 - SEVERAL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED FWD EMERGENCY LIGHTING POWER PACK. (W) 2H72 4T RTA53EU 19950217000191995021700019EU 1995 2 17 RAIA950127 119950118A5753MS2764821 BEARING BAG JETSTMJETSTM3201 1500217EU RT TE FLAP WORN A ARAIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 CE03428AM8551 877 STL - FLT 7307 - ACFT ROLLS TO THE RT WHEN FLAPS SELECTED TO 35 DEGREES. MAINTENANCE DISCOVERED RT CENTER FLAP HINGE BEARING TO BE WORN. MAINTENANCE REPLACED RT CENTER FLAP HINGE BEARING AND ADJUSTED RIGGING. GROUND TEST OF FLAP SYSTEM CHECK GOOD. (W) 2L72 4T RTA56EU 19950217000201995021700020EU 1995 2 17 RAIA950130 119950122A521091SE13 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR HDL OUT OF ADJUST A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03339TE 935 STL - FLT 7492 - PAX DOOR LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED DOOR HANDLE MICROSWITCH. SYSTEM TEST REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950217000211995021700021EU 1995 2 17 RAIA950131 119950123A33503011151 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE13380 119 STL - EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING POWER SUPPLY. (W) 2H72 4T RTA53EU 19950217000221995021700022EU 1995 2 17 RAIA950132 119950124A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU STA 130 DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03426AM5967 874 STL - SEVERAL EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (W) 2L72 4T RTA56EU 19950217000231995021700023EU 1995 2 17 RAIA950133 119950124A3350OL60423P EEL BULB AEROSPATR72 ATR72202 8680940EU RT EXTERIOR FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE5952 283 STL - THE RT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED BULB IN RT FWD EXTERIOR EMERGENCY EXIT LIGHT. (W) 2H72 4T RTA53EU 19950217000241995021700024EU 1995 2 17 UF6A950112 119950117A61208022631 O-RING BAG ATP ATP EU LT ENGINE LEAK A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 CE03856AW6961 2032 ORD - FLT 5020 - THE NR 1 ENGINE NP ACCELERATED TO 80 PERCENT, THEN DROPPED TO 40 PERCENT ON TAXI. MAINTENANCE REPLACED THE BETA TUBE O-RINGS, OPS CHECK GOOD. (W) 2L72 4T RTA27NM 19950217000251995021700025EU 1995 2 17 UF6A950113 119950119A3240201045717 BRAKE LINE BAG ATP ATP EU RT MLG LEAKING A UF6AD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CE03860AW 2037 ORD - FLT 5049 - ON TAXI, THE LT HYDRAULIC PRESSURE WENT TO ZERO. MAINTENANCE REPLACED RT I/B BRAKE LINE LEAK. OPS CHECK GOOD. (W) 2L72 4T RTA27NM 19950217000261995021700026EU 1995 2 17 UF6A950114 119950119A33506013211 EEL POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03851AW1698 2020 ORD - FLT 5020 - EMERGENCY FLOOR TRACK LIGHTING ROW 13 IS INOP. MAINTENANCE REPLACED THE POWER SUPPLY. OPS CHECK GOOD. (W) 2L72 4T RTA27NM 19950217000271995021700027EU 1995 2 17 UF6A950115 119950118A3350S5310009N EEL CONNECTOR BAG ATP ATP EU CABIN DIRTY A UF6AK NONE L NO TEST TXTAXI/GRND HDL 1 CE03856AW6923 2032 ORD - FLT 5069 - OVERWING EXIT LIGHT CWP ILLUMINATED ON TAXI. MAINTENANCE CLEANED CONNECTOR ON EXIT LIGHT PLUG. OPS CHECK GOOD. (W) 2L72 4T RTA27NM 19950217000281995021700028EU 1995 2 17 UF6A950116 119950120A2910 HYD FLUID BAG ATP ATP EU HYD SYST REQD SERVICE A UF6AK NONE J WARNING INDICATION ININSP/MAINT 1 CE03860AW5212 2037 ORD - FLT 5106 - LOW HYDRAULIC LEVEL LIGHT ILLUMINATED. MAINTENANCE SERVICED HYDRAULIC SYSTEM WITH FLUID. (W) 2L72 4T RTA27NM 19950217000291995021700029EU 1995 2 17 UF6A950117 119950120A3350362624 EEL STRIP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03857AW6401 2034 ORD - FLT 5042 - FLOOR TRACK LIGHTING INOP. MAINTENANCE REPLACED LIGHT STRIP. (W) 2L72 4T RTA27NM 19950217000301995021700030WP 1995 2 17 VTZA95028 219950121A72003103380 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT BIRD STRIKE A VTZAK NONE C F.O.D. LDLANDING 1 EA27471UE 821 MDT-IAD - FLT 6571 - AT 1930 THE RT ENGINE HAD A BIRD STRIKE TO THE INTAKE ON LANDING. THE BIRD WAS INGESTED AND IMPELLER RECEIVED FOD. ACFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE. OPS CHECKED GOOD. ACFT WAS THEN APPROVED FOR RETURN TO SERVICE. ACFT WAS RELEASED ON 1-26-95. (W) 2L72 4T3 TRTA56EU E3WE 19950217000311995021700031EU 1995 2 17 VTZA95035 119950126A243051539019E GCU JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 IAD-TYS - FLT 6353 - DURING CLIMB-OUT, THE LT ENGINE STARTER/GENERATOR FELL OFF LINE. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED GCU. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950217000321995021700032EU 1995 2 17 VTZA95038 119950128A760021188405 IEC JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27311UE 41029 TYS-IAD - FLT 6182 - DURING TAXI, THE IEC FAILED ON TAXI OUT. ACFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE RESET THE IEC. OPS CHECK GOOD. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950217000331995021700033NM 1995 2 17 WRLA95002 119950118A3230ACG72371 LOWER LOCK LINK DOUG MD11 MD11F 3023600NM NLG CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 EA27274WA 48633 THE INITIAL EXPANDED EDDY CURRENT INSPECTION, PERFORMED IAW AD 94-18-07 PAR B-2-II AND MD-11 ALERT SERVICE BULLETIN A32-47, REVEALED A CRACK INDICATION IN THE UPPER SURFACE OF THE LINK, APPROXIMATELY 15 MILLIMETERS IN LENGTH. REWORK OF THE LINK TO THE LIMITS ALLOWED BY SERVICE BULLETIN FAILED TO REMOVE THE CRACK INDICATION. REMOVED AND REPLACED LINK (P/N ACG7237-1), (S/N AP166 WITH NEW LINK (P/N ACG 7237-1), (S/N AP177). 2L73 4F RTA22WE 19950217000341995021700034SO 1995 2 17 WTAA950062 119950122A30402SC1160A CURRENT SENSOR EMB 120 EMB120RT SO RT WINDSHIELD SHORTED A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP17120AM 120012 SFO - ELECTRICAL BURNING ODOR REPORTED IN COCKPIT WITH RT WINDSHIELD HEAT ON. MAINTENANCE REPLACED RT WINDSHIELD HEAT CURRENT SENSOR. SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000351995021700035SO 1995 2 17 WTAA950063 119950128A79201593731 HOSE EMB 120 EMB120RT SO LT ENGINE LEAKING A WTAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP17122AM 120013 FAT-SFO - EN ROUTE, LOSS OF LT ENGINE OIL PRESSURE REPORTED. CREW ACCOMPLISHED SHUTDOWN OF LT ENGINE AND DECLARED AND EMERGENCY. ACFT LANDED AT STA WITHOUT INCIDENT. MAINTENANCE DISCOVERED OIL COOLER CROSSOVER HOSE LEAKING. REPLACED HOSE AND SERVICED ENGINE WITH OIL. ACCOMPLISHED ENGINE RUN AND LEAK CHECKED HOSE. NO LEAKS OR DEFECTS NOTED. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000361995021700036WP 1995 2 17 95ZZZW108 119950123A3350003PA54 EEL TRACK COVER DOUG DC9 DC983 3022083WP CABIN MISSING A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 PDX - CHECK, FIRST CLASS EMERGENCY TRACK LIGHTING INOP. MAINTENANCE FOUND TRACK COVER MISSING AND LIGHT ASSEMBLY UNPLUGGED. RECONNECTED PLUG AND REPLACED MISSING TRACK COVER. REF ASAA9525. 2L72 4F RTA6WE 19950217000381995021700038NM 1995 2 17 ASAA9530 119950121A5210507945178 DOOR BOEING737 7374Q8 NM FWD CABIN LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01754AS8031 25095 ANC - CHECK, L1 DOOR HARD TO SHUT. MAINTENANCE INSPECTED AND LUBRICATED DOOR. OPS CHECKED NORMAL. (W) 2L72 4F RTA16WE 19950217000391995021700039NM 1995 2 17 ASAA9535 119950125A52416545871521 GALLEY DOOR BOEING737 7374Q8 NM FWD CABIN LACK OF LUBE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01779AS 25111 JNU - CHECK, R1 FWD DOOR DOOR DIFFICULT TO OPEN. MAINTENANCE LUBED HINGES AND CAM ROLLER BEARINGS. (W) 2L72 4F RTA16WE 19950217000401995021700040NM 1995 2 17 ASAA9539 119950126A3244419K622 TIRE BOEING737 7374Q8 NM LT MLG FAILED A ASAAA UNSCHED LANDING O OTHER CLCLIMB 1 NM01775AS 25108 SEA - FLT 67 - ON DEPARTURE, THE NR 1 MLG TIRE TREAD SEPARATED FROM ITS CASING CAUSING DAMAGED TO THE LT GEAR DOORS, LT I/B MID-FLAP, LT I/B TRAILING EDGE FLAP, LT LOWER WING SKIN, LT I/B THRUST REVERSER COWLING AND THE LT HORIZONTAL STABILIZER. MAINTENANCE REPLACED NR 1 MLG WHEEL ASSEMBLY AND REPLACED OR REPAIRED CONSEQUENTIAL DAMAGE AS REQUIRED. THE NR 2 MLG WHEEL ASSEMBLY WAS REPLACED AS A PRECAUTION. (W) 2L72 4F RTA16WE 19950217000431995021700043SO 1995 2 17 RAAAE895001 119950107A2140172194 ELEMENT LKHEED188 188C 5262604SO HEATER OVERHEATED A RAAAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03178RV 188C2010 ANC-SDP - IN FLIGHT, COCKPIT FILLED WITH SMOKE. PERFORMED ELECTRICAL FIRE PROCEDURES AND COCKPIT SMOKE REMOVAL CHECKLIST. PERFORMED EMERGENCY DESCENT AND DIVERTED TO CDB. REPLACED 10 HEAT ELEMENTS DUE TO OVERHEAT. (W) 2L74 4T 4A22 19950217000441995021700044NE 1995 2 17 95ZZZW110 219950202A7230 BEARING SEAL BOEING747 747124 1384874NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE FAILED A P5CAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP23630SJ 19733 662388 ORD - ON CLIMB-OUT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT CAME ON, FOLLOWED BY A LOSS OF OIL QUANTITY AND A RISE IN OIL TEMPERATURE. ENGINE SHUTDOWN, FUEL DUMP AND ACFT RETURNED TO ORD. POST FLIGHT INSPECTION OF ENGINE SHOWED NO EXTERNAL LEAKS. ENGINE MAIN OIL FILTER WAS FOUND FULL OF THICK BLACK OIL. SUSPECT NR 4 BEARING CARBON SEAL FAILURE. ACFT WAS FERRIED TO MAINTENANCE BASE FOR ENGINE CHANGE. 2L74 4F4 F A20WE E20EA 19950217000451995021700045NM 1995 2 17 95ZZZW111 119950112A5313 STRINGER BOEING727 727254 138408LNM BS 475 CORRODED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 WHILE PERFORMING LAP JOINT MODIFICATION PER AD 91-06-06, 2 INCH BY 6 INCH CORROSION WAS FOUND ON PRODUCTION STRAP AT BS 440 BETWEEN S-19R AND S-20R. REPAIRED DOUBLER PER BOEING DRAWING 65054572 AND ENGINEERING AUTHORIZATION EA S1387. A 2 INCH BY 7 INCH AREA OF CORROSION WAS FOUND ON STRINGER 19R AT BS 475. INSTALLED STRINGER SPLICE PER SRM 53-10-3 AND SRM 51-40-3. FOUND .6 INCH CRACK ON S-18L AT BS 500. REPLACED CRACKED SECTION PER SRM 53-0-3 FIG 1 DETAIL 1. ALSO, FOUND 1.2 INCH CRACK ON THE FUSELAGE SKIN ON S-18L AT BS 456. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3. REF TAOA029501. REF 95ZZZW112. REF 95ZZZW113. 2L73 4F A3WE 19950217000461995021700046NM 1995 2 17 95ZZZW112 119950112A5313 STRINGER BOEING727 727254 138408LNM BS 500 CRACKED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 WHILE PERFORMING LAP JOINT MODIFICATION PER AD 91-06-06, 2 INCH BY 6 INCH CORROSION WAS FOUND ON PRODUCTION STRAP AT BS 440 BETWEEN S-19R AND S-20R. REPAIRED DOUBLER PER BOEING DRAWING 65054572 AND ENGINEERING AUTHORIZATION EA S1387. A 2 INCH BY 7 INCH AREA OF CORROSION WAS FOUND ON STRINGER 19R AT BS 475. INSTALLED STRINGER SPLICE PER SRM 53-10-3 AND SRM 51-40-3. FOUND .6 INCH CRACK ON S-18L AT BS 500. REPLACED CRACKED SECTION PER SRM 53-0-3 FIG 1 DETAIL 1. ALSO, FOUND 1.2 INCH CRACK ON THE FUSELAGE SKIN ON S-18L AT BS 456. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3. REF TAOA029501. REF 95ZZZW111. REF 95ZZZW113. 2L73 4F A3WE 19950217000471995021700047NM 1995 2 17 95ZZZW113 119950112A5330 SKIN BOEING727 727254 138408LNM BS 456 CRACKED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 WHILE PERFORMING LAP JOINT MODIFICATION PER AD 91-06-06, 2 INCH BY 6 INCH CORROSION WAS FOUND ON PRODUCTION STRAP AT BS 440 BETWEEN S-19R AND S-20R. REPAIRED DOUBLER PER BOEING DRAWING 65054572 AND ENGINEERING AUTHORIZATION EA S1387. A 2 INCH BY 7 INCH AREA OF CORROSION WAS FOUND ON STRINGER 19R AT BS 475. INSTALLED STRINGER SPLICE PER SRM 53-10-3 AND SRM 51-40-3. FOUND .6 INCH CRACK ON S-18L AT BS 500. REPLACED CRACKED SECTION PER SRM 53-0-3 FIG 1 DETAIL 1. ALSO, FOUND 1.2 INCH CRACK ON THE FUSELAGE SKIN ON S-18L AT BS 456. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3. REF TAOA029501. REF 95ZZZW111. REF 95ZZZW112. 2L73 4F A3WE 19950217000481995021700048SO 1995 2 17 95ZZZW114 119950114A2612 CONNECTOR GULSTMG1159 G1159 3953505SO RT ENG FIRE LOOPFAILED A WICAO OTHER N FALSE WARNING CRCRUISE 1 AL03666JT 162 TEB-BDL - EN ROUTE, INTERMITTENT FLASHING OF RT ENGINE FIRE WARNING LIGHT WITH THE BELL OCCURRED. SEVERAL REOCCURANCES DURING FLIGHT FOLLOWED. PROBLEM WAS ALLEVIATED WHEN THROTTLE WAS RETARDED. AFTER LANDING AT BDL WITHOUT INCIDENT, THE ITEM WAS TROUBLESHOT AS BARE WIRE GOING INTO THE CONNECTOR TO THE LOWER FIRE LOOP. CONNECTOR WAS REPLACED AND WIRES WERE REPAIRED. OPS CHECKS OK. 2L72 4F RTA12EA 19950217000491995021700049WP 1995 2 17 95ZZZW115 119950127A4900GTCP8598D APU DOUG DC9 DC932 3022066WP FUSELAGE MALFUNCTIONED A VJ6AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11915VV 47443 IAD - FLT 469 - WHILE AT THE GATE, EXPERIENCED FUMES AND SMOKE TO A MARGINAL DEGREE DUE TO THE APU. PLACED APU ON MEL 49-1. 2L72 4F A6WE 19950217000501995021700050NE 1995 2 17 95ZZZW116 219950127A73101320115 ANTI-ICE VALVE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7 52053NE RT FUEL HEAT MALFUNCTIONED A VJ6AA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO11901VJ 47275 ATL-IAD - FLT 368 - FLIGHT RETURNED TO ATL DUE TO RT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED LIMITS PER MM 71-00. REMOVED AND REPLACED NR 2 FUEL ANTI-ICE VALVE. 2L72 4F4 F A6WE E2EA 19950217000511995021700051WP 1995 2 17 95ZZZW117 119950202A5320991183877 STIFFENER DOUG DC9 DC951 3022051WP FS 1217 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 HNL - TWO STIFFENERS (T ANGLE) WERE FOUND SEVERELY CRACKED AND CORRODED AT THE CANTED BULKHEAD FWD FACE FS 1217. REPLACED STIFFENERS. REF HAL95016. 2L72 4F A6WE 19950217000521995021700052WP 1995 2 17 BUFA9502 119950205A2910 LINE DOUG DC8 DC8F54 3021926WP HYD SYST LOOSE A BUFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE057046G 45885 MIA - ON CLIMB, THE HYDRAULIC FLUID LOSS TO STANDPIPE. RETURNED TO MIA, NO EMERGENCY DECLARED, AND HAD UNEVENTFUL LANDING. FOUND LOOSE LINE AT CASE DRAIN. TIGHTENED 'B' NUT, RAN ENGINE AND PERFORMED OPERATION AND LEAK CHECK. CHECK OK PER MM. (W) 2L74 4F 4A25 19950217000531995021700053WP 1995 2 17 BUFA9503 119950206A57535751184504 FITTING DOUG DC8 DC863 302198AWP WS 219 CRACKED A BUFAK NONE O OTHER ININSP/MAINT 1 CE05781AL 45926 WHILE ACCOMPLISHING B-CHECK WORK CARD NR 605001, FOUND RT FLAP HORN O/B STA 219 CRACKED APPROXIMATELY 5 INCHES VERTICALLY. TYPICAL CRACK FWD OF AFT ATTACHMENT AT 1, PG 11 OF S/B 27-249. FLAP REMOVED AND FITTING REPLACED IAW SRM 51-3-0 AND 51-1-21. FLAP REINSTALLED IAW MM 27-51-2. ACFT RETURNED TO SERVICE. (W) 2L74 4F 4A25 19950217000571995021700057EU 1995 2 17 CAL950063 119950123A2760 INPUT ROD AIRBUS300 A300B4103 3930104EU LT SPEEDBRAKE OUT OF ADJUST A CALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0911985 119 SDQ - FLT 702 - TAKEOFF WAS ABORTED AT LESS THAN 50 KNOTS DUE TO THE TAKEOFF WARNING HORN COMING ON, ACCOMPANIED BY AN INTERMITTENT CONFIGURATION LIGHT AND SPEEDBRAKE LIGHT. MAINTENANCE FOUND THAT THE LT WING O/B SPEEDBRAKE WOULD NOT FULLY STOW. THE INPUT ROD WAS ADJUSTED PER A300 MM 27-62-15 AND OPERATION OF THE SPEEDBRAKES CHECKED GOOD. (W) 2L72 4F A35EU 19950217000591995021700059NM 1995 2 17 CAL950065 119950118A5320 INTERCOSTAL BOEING727 727227 1384078NM BS 400-420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097975444031 21363 GSO - INSPECTION FOUND A .5 INCH CRACK IN CABIN FLOOR INTERCOSTAL AT STA 400-420, BL 0. REMOVED CRACKED INTERCOSTAL TOP ANGLE AND INSTALLED NEW ANGLE IAW SRM 53-10-2, 51-10-1, 51-30-2, AND 51-10-2. (W) 2L73 4F A3WE 19950217000601995021700060NM 1995 2 17 CAL950066 119950118A5315 FLOORBEAM BOEING727 727227 1384078NM BS 1090 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097975444031 21363 GSO - INSPECTION FOUND LT END OF FLOORBEAM AT STA 1090 CORRODED. THE CORROSION WAS REMOVED AND DOUBLER AND FILLER WERE INSTALLED IAW EC 5310-01102. (W) 2L73 4F A3WE 19950217000611995021700061NM 1995 2 17 CAL950067 119950118A5320 FLOOR SUPPORT BOEING727 727227 1384078NM FS 1070 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097975444031 21363 GSO - INSPECTION FOUND THE FLOOR SUPPORT ANGLE CORRODED AT STA 1070, RBL 30-45. THE CORRODED SECTION OF THE FLOOR SUPPORT ANGLE WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2. (W) 2L73 4F A3WE 19950217000621995021700062NM 1995 2 17 CAL950068 119950118A5320 SUPPORT BOEING727 727227 1384078NM FS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0979754 21363 GSO - INSPECTION FOUND THE FWD LAVATORY AFT WALL I/B CORNER FLOOR SUPPORT STRUCTURE CORRODED AT STA 344, RBL 17. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-10-2. (W) 2L73 4F A3WE 19950217000631995021700063NM 1995 2 17 CAL950069 119950118A5312 BLKHD SUPPORT BOEING727 727227 1384078NM RT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0979754 21363 GSO - INSPECTION FOUND THE RT AFT LAVATORY FWD BULKHEAD SUPPORT CORRODED. THE CORRODED SUPPORT ANGLE WAS REMOVED, AND A NEW ONE WAS INSTALLED IAW SRM 53-10-2, 51-30-2, AND 51-10-1. (W) 2L73 4F A3WE 19950217000641995021700064NM 1995 2 17 CAL950070 119950118A5320 PRESSURE WEB BOEING727 727227 1384078NM RT AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097975444031 21363 GSO - INSPECTION FOUND THE RT AFT LAVATORY FLOOR PRESSURE WEB CORRODED. THE FLOOR PRESSURE WEB WAS REMOVED, AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-2, 51-30-2 AND 51-10-2. (W) 2L73 4F A3WE 19950217000651995021700065EU 1995 2 17 CAL950071 119950125A2750 FLAP TRANS AIRBUS300 A300B4103 3930104EU TE FLAPS INOPERATIVE A ACALAO OTHER J WARNING INDICATION APAPPROACH 1 SW0916982 091 MCO - FLT 117 - THE FLAPS WOULD NOT EXTEND ON APPROACH. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 AND NR 6 FLAP TRANSMISSIONS AT FAULT. BOTH THE NR 1 AND NR 6 RT FLAP TRANSMISSIONS WERE REMOVED AND REPLACED. IN ADDITION, ALL FLAP TRANSMISSIONS AND DOWNDRIVE GEARBOXES WERE DRAINED AND SERVICED. THE FLAPS WERE CYCLED SEVERAL TIMES AND ALL OPERATION CHECKED GOOD. (W) 2L72 4F A35EU 19950217000661995021700066NM 1995 2 17 CAL950072 119950127A3260 DNLOCK SENSOR BOEING737 737130 1384435NM RT MLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0914206 19023 EWR - FLT 1881 - THE RT MLG GREEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GREEN LIGHT WOULD EXTINGUISH BY MOVING THE GEAR HANDLE TO UP, BUT WOULD COME BACK ON WITH THE GEAR HANDLE IN OFF. THE ACFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE ACFT HAD A HISTORY OF THIS PROBLEM. MAINTENANCE FOUND THE S73 RT MLG DOWNLOCK SENSOR AT FAULT. THE SENSOR WAS REMOVED AND REPLACED AND GEAR INDICATIONS CHECKED GOOD. THE ACFT HAS FLOWN OVER 15 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (W) 2L72 4F A16WE 19950217000671995021700067NM 1995 2 17 CAL950073 119950127A29106517844335 HYD LINE BOEING727 727232 1384082NM NR 1 ENG LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0927783 20638 MIA - FLT 334 - THE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO .1250 GALLON WHILE IN FLIGHT. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE ACFT WAS DIVERTED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE LEAKING. THE LINE WAS REMOVED AND REPLACED. LEAK AND PRESSURE CHECKS AFTER HYDRAULIC SYSTEM SERVICING WERE GOOD. (W) 2L73 4F A3WE 19950217000681995021700068NM 1995 2 17 CAL950074 119950128A29106517844299 HYD LINE BOEING727 727227 1384078NM NR 2 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0979771 20840 EWR - FLT 518 - THE ACFT LOST 'A' SYSTEM HYDRAULICS ON APPROACH WITH THE NR 1 PUMP LOW PRESSURE LIGHT FLICKERING ON AND OFF. THE GEAR AND FLAPS WERE EXTENDED USING ALTERNATE MEANS AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE LINE AT 'A' SYSTEM MODULE LEAKING. THE HYDRAULIC PRESSURE LINE WAS REPLACED AND LEAK CHECK WAS GOOD. (W) 2L73 4F A3WE 19950217000691995021700069NE 1995 2 17 CAL950075 219950128A7261 O-RING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0916804 49246 IAH - FLT 464 - THE NR 1 ENGINE LOST OIL QUANTITY IN FLIGHT. THE OIL PRESSURE GRADUALLY DROPPED TO 20 PSI. THE ACFT WAS DIVERTED TO BNA AS A PRECAUTIONARY MEASURE. MAINTNANCE FOUND O-RING ON HIGH PRESSURE SHAFT OF NR 1 ENGINE LEAKING. THE O-RING WAS REPLACED. THE NR 1 ENGINE WAS RUN AND OPERATION CHECKED GOOD WITH NO LEAKS NOTED. (W) 2L72 4F4 F A6WE E9NE 19950217000701995021700070WP 1995 2 17 HAL95015 119950203A57433912765504 SPAR CAP FITTING DOUG DC9 DC951 3022051WP RT MLG CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13709HA 47764 HNL - DURING ACCOMPLISHMENT OF AD 84-26-01, AMENDMENT 39-4971 (VISUAL INSP MLG ATTACH FITTING) A CRACK WAS FOUND IN AN ADJACENT UPPER AUXILIARY SPAR CAP FITTING, ATTACHED TO THE RT MLG ATTACH FITTING. REPLACED RT AUXILIARY SPAR CAP FITTING. (W) 2L72 4F A6WE 19950217000711995021700071WP 1995 2 17 HAL95016 119950202A5320991183875 STIFFENER DOUG DC9 DC951 3022051WP FS 1217 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 HNL - TWO STIFFENERS (T ANGLE) WERE FOUND SEVERELY CRACKED AND CORRODED AT THE CANTED BULKHEAD FWD FACE FS 1217. REPLACED STIFFENERS. REF 95ZZZW117. 2L72 4F A6WE 19950217000721995021700072WP 1995 2 17 HAL95017 119950202A555359201032 ATTACH FITTING DOUG DC9 DC951 3022051WP VERT STAB LE CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 HNL - VERTICAL STABILIZER LEADING EDGE, RT FRONT SPAR ATTACH FITTING WAS FOUND CRACKED WHILE ACCOMPLISHING NON-ROUTINE MAINTENANCE. REPLACED FITTING. (W) 2L72 4F A6WE 19950217000731995021700073WP 1995 2 17 HAL95018 119950208A2730 ROD END DOUG DC9 DC951 3022051WP RT ELEVATOR LOOSE A AHALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP132FOR 47742 OGG - FLT 258 - VIBRATION FELT INFLIGHT THROUGH WHOLE AIRPLANE BUT, MOSTLY THROUGH CONTROL YOKE. PITCH TRIM SEEMED TO CHANGE CONSTANTLY. STABILIZER TRIM SYSTEM WORKED FINE, MADE AIR TURNBACK. FOUND RT ELEVATOR BOOST CYLINDER AFT ROD-END NUT BACKED OFF. REPLACED EYE BOLT ASSEMBLY PER MM FOR PRECAUTION. LT ELEVATOR BOOST CYLINDER CONDITION AND SECURITY CHECK OKAY. ELEVATOR OPERATION CHECK OKAY. RT ELEVATOR ROD-END RETAINER TO BE REPLACED AFTER ACFT FERRIED TO HNL. (W) 2L72 4F A6WE 19950217000741995021700074SW 1995 2 17 LOSA9508 119950203A3250791010BA22 WIRE FRCHLDSA227 SA227DC 3377521SW NLG STEERING BROKEN A LOSAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23451LA DC849B CREW REPORTED THAT SPEED LEVERS HIGH NOSE WHEELSTEERING INOPERTIVE. MAINTENANCE REPLACED DEFECTIVE WIRE (791010BA22) IN PEDESTAL. ALL REQUIRED CHECKS NORMAL. ACFT RELEASED FOR SERVICE. (W) 1L72 4T RTA18SW 19950217000751995021700075NM 1995 2 17 TAOA029501 119950112A5320 STRAP BOEING727 727254 138408LNM BS 440 CORRODED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 WHILE PERFORMING LAP JOINT MODIFICATION PER AD 91-06-06, 2 INCH BY 6 INCH CORROSION WAS FOUND ON PRODUCTION STRAP AT BS 440 BETWEEN S-19R AND S-20R. REPAIRED DOUBLER PER BOEING DRAWING 65054572 AND ENGINEERING AUTHORIZATION EA S1387. A 2 INCH BY 7 INCH AREA OF CORROSION WAS FOUND ON STRINGER 19R AT BS 475. INSTALLED STRINGER SPLICE PER SRM 53-10-3 AND SRM 51-40-3. FOUND .6 INCH CRACK ON S-18L AT BS 500. REPLACED CRACKED SECTION PER SRM 53-0-3 FIG 1 DETAIL 1. ALSO, FOUND 1.2 INCH CRACK ON THE FUSELAGE SKIN ON S-18L AT BS 456. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 3. REF 95ZZZW111. REF 95ZZZW112. REF 95ZZZW113. 2L73 4F A3WE 19950217000761995021700076NM 1995 2 17 TWRA9507 119950122A335060B40053 EEL BATT PACK BOEING747 747282B 1384860NM MAIN ENTRY DOOR INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15610FF 20501 DURING DAILY SERVICE, EMERGENCY LIGHTS AT R1 MAIN ENTRY DOOR CAME ON AND OFF. REPLACED BATTERY PACK AT R1 MED, AND REPLACED LIGHT ASSEMBLY. OPS CHECK OK. (W) 2L74 4F A20WE 19950217000771995021700077EU 1995 2 17 VTZA95040 119950202A32348662C SELECTOR VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR MALFUNCTIONED A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27496UE 900 IAD-SYR - FLT 6338 - DURING APPROACH, THE NOSE GEAR INTRANSIT LIGHT ILLUMINATED AFTER GEAR EXTENSION WITH NO DOWNLOCK INDICATION. DOWNLOCK INDICATION ILLUMINATED SEVERAL MINUTES LATER PRIOR TO LANDING. ACFT LANDED WITH NO FURTHER INCIDENTS. ACFT WAS THEN FERRIED TO IAD, WHERE MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950217000781995021700078NM 1995 2 17 95ZZZW119 119950110A7712SELOC2N TQ INDICATOR DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE MALFUNCTIONED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA07981HA1955 374 378 TYS-DCA - FLT 3341 - ON TAKEOFF ROLL, NR 2 TORQUE INDICATOR FLUXED FULL SCALE. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. CLEANED CANNON PLUG ON TORQUE SENSOR CONTROL UNIT AND TORQUE INDICATOR, RUNUP CHECK GOOD. REMOVED AND REPLACED NR 2 TORQUE INDICATOR IN DCA AS A PRECAUTION. 2H72 4T RTA13NM 19950217000791995021700079NM 1995 2 17 95ZZZW120 119950101A2731 TRIM DHAV DHC8 DHC8102 2809003NM ELEVATOR OUT OF POSITION A HNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA07926HA 114 JAX-TPA - FLT 3048 - ON TAKEOFF ROLL, THE TAKEOFF WARNING HORN SOUNDED. THE TAKEOFF WAS ABORTED AND AFTER CLEARING THE RUNWAY, ALL ITEMS WERE RECHECKED AND FOUND TO BE IN THE PROPER POSITION. HOWEVER, THE CREW NOTED THE ELEVATOR TRIM WAS AT THE REAR LIMIT OF THE TAKEOFF RANGE. THE ELEVATOR TRIM WAS REPOSITIONED SLIGHTLY INTO THE TAKEOFF RANGE AND NO FURTHER EVIDENCE OF HORN SOUNDING WAS NOTED. THE ACFT THEN PROCEEDED WITH A NORMAL TAKEOFF WITHOUT FURTHER INCIDENT. 2H72 4T RTA13NM 19950217000801995021700080NM 1995 2 17 95ZZZW121 119950114A6123 SWITCH DHAV DHC8 DHC8102 2809003NM AUTOFEATHER SYS DIRTY A HNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA07941HA 161 CHO-SBY - FLT 3354 - ON TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. CLEANED AUTOFEATHER MICROSWITCH CONTACTS. OPERATIONAL CHECK GOOD. 2H72 4T RTA13NM 19950217000811995021700081NM 1995 2 17 95ZZZW122 119950124A3260841101 WOW SENSOR DHAV DHC8 DHC8102 2809003NM NR 2 MLG FAILED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07938HA 152 SBY-CHO - FLT 3156 - WEIGHT ON WHEELS CAUTION LIGHT CAME ON DURING TAKEOFF. ACFT TURNED BACK AND LANDED IN SBY WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 MLG I/B WEIGHT ON WHEELS SENSOR. 2H72 4T RTA13NM 19950217000821995021700082NM 1995 2 17 AWXA9500055 119950124A27526544569 ACTUATOR BOEING737 7373G7 1384595NM NR 6 SPOILER FAILED A AAWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28155AW 4676 23777 LAS - FLT 959 - AT TAKEOFF, CREW ENCOUNTERED A MODERATE ROLL TO THE RT. APPROXIMATELY 50 PERCENT YOKE DEFLECTION WAS REQUIRED TO MAINTAIN THE WINGS LEVEL. ACFT CONTINUED TO LAS WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED RT O/B FLAPS TOGGLE. FLAPS OPS CHECKED, NO FAULTS NOTED. RUDDER PCU TEST C/W, NO MALFUNCTIONS NOTED. TEST FLIGHT COMPLIED WITH, ACFT STILL ROLLS TO RT ON ROTATION. MX REMOVED AND REPLACED NR 6 FLIGHT SPOILER HYDRAULIC ACTUATOR PER AWA TASK CARD R3M27021. CHECKED TRAVEL ON ALL FLT SPOILERS PER SAME TASK CARD. NO FURTHER DISCREPANCIES WERE NOTED. ACFT OK FOR SERVICE. TEST FLIGHT COMPLETED AND NO UNUSUAL ROLL NOTED AT ANYTIME. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950217000831995021700083NM 1995 2 17 AWXA9500056 119950125A572069607919 STRUT ASSY BOEING737 7373G7 1384595NM RT WING BROKEN A AWXAO OTHER F FLT CONT AFFECTED CLCLIMB 1 WP28155AW25234 23777 RNO-PHX - FLT 460 - ON TAKEOFF AND INITIAL CLIMB, ACFT EXPERIENCED ROLL TO RT TENDENCY, 20 DEGREES LT AILERON WAS REQUIRED TO COUNTER UNTIL APPROXIMATELY 170/180 KIAS. ACFT CONTINUED TO PHX WITHOUT FURTHER PROBLEMS. MX FOUND STRUT ASSEMBLY FOR RT WING UPPER FIX PANEL BROKEN (PANEL NEXT TO AND I/B OF NR 6 FLT SPOILER). MX REPLACED STRUT ASSY AND FAIRED PANEL TO WING AND NR 6 SPOILER. ACFT OK FOR TEST FLIGHT. PERFORMED THREE TAKEOFFS AND LANDINGS, NO ABNORMAL ROLL TENDENCIES NOTED. ACFT RETURNED TO SERVICE. TOTAL CYCLES 19935. (W) 2L72 4F RTA16WE 19950217000841995021700084NM 1995 2 17 AWXA9500070 119950131A275110619264 INDICATOR BOEING737 737277 1384570NM TE FLAPS FAILED A AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28187AW 176 22654 CMH-BOS - FLT 1620 - DURING LANDING PROCEDURE, FLAPS STUCK AT POSITION 1 WITH NO LEADING EDGE INDICATION. WHILE ACCOMPLISHING QRH PROCEDURES, THE FLAPS STARTED MOVING AND CREW RECEIVED PROPER LANDING CONFIGURATION. DURING FLAP RETRACTION AFTER LANDING, FLAPS STUCK AT 25 DEGREE POSITION. CONTRACT MX FOUND FLAP POSITON INDICATOR FAILED. CONTRACT MX REPLACED INDICATOR, OPERATION CHECK NORMAL. ACFT RELEASED TO SERVICE. FLAP OPERATION REINSPECTED UPON ARRIVAL AT CMH, NO DEFECTS NOTED. (W) 2L72 4F RTA16WE 19950217000851995021700085NM 1995 2 17 AWXA9500074 119950130A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 5 THROUGH 7 AND ROW 33 TO AFT. RECONNECTED WIRING AND RESECURED LIGHTS AS REQUIRED, OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950217000861995021700086SO 1995 2 17 C2XA95CL009 119950129A27503075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO AVIONICS BAY MALFUNCTIONED A AC2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0915713607 120114 CLE-CVG - FLT 3263 - RECEIVED FLAP DISAGREEMENT ON DEPARTURE, COULD NOT RESET. ACFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT. OPS CHECK GOOD IAW EMB MM 27-50-00. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000871995021700087SO 1995 2 17 C2XA95CL010 119950129A5753PE610261 ROLLER'S EMB 120 EMB120RT SO RT TE FLAP BINDING A C2XAO OTHER J WARNING INDICATION LDLANDING 1 SW0915713 120114 DTW-CLE - FLT 3142 - FLAP DISAGREEMENT LANDING IN CLE. MAINTENANCE REMOVED AND REPLACED RT O/B FLAP ROLLER'S WITH NEW STYLE IAW EMB MM 27-50-12 AND EA 2750-01007. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000881995021700088SO 1995 2 17 C2XA95CL011 119950129A5753PE610261 ROLLER'S EMB 120 EMB120RT SO LT TE FLAP BINDING A C2XAK NONE FJ FLT CONT AFFECTED WARNING INDICATION LDLANDING 1 SW0915713 120114 PIT-CLE - FLT 3331 - FLAP ASSYMETRY O/B LT SIDE. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ROLLERS WITH NEW STYLE IAW EMB MM 27-50-12 AND EA275001007. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000891995021700089SO 1995 2 17 C2XA95CL012 119950127A2750MS3126P1210S CONNECTOR EMB 120 EMB120RT SO RT TE FLAP SHORTED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0934712 120111 CLE-GRR - FLT 3373 - FLAP DISAGREEMENT AFTER TAKEOFF. ACFT AIR RETURN TO CLE. MAINTENANCE REMOVED AND REPLACED RT O/B ACTUATOR CANNON PLUG. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000901995021700090EU 1995 2 17 C2XA95CL013 119950128A3234F96GA0102 GEAR CONTROL AEROSPATR42 ATR42320 8680930EU COCKPIT FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0911835 194 EWR-BTV - FLT 3664 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO EWR. MAINTENANCE PLACED GEAR ON MEL 32-31-3 CONTROL NR 769998. DURING RON IN BTV ON 01/28/95 MAINTENANCE REMOVED AND REPLACED GEAR CONTROL LEVER. OPS CHECK GOOD. REMOVED MEL AND RETURNED ACFT TO SERVICE. (W) 2H72 4T RTA53EU 19950217000911995021700091SO 1995 2 17 C2XA95CL014 119950205A3260922AA2Y6PZ722 PROX SENSOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING EN VIBRATION/BUFFET FALSE WARNING CLCLIMB 1 SW0934712 120111 CLE-ROC - FLT 3115 - AFTER TAKEOFF, RT RED 'A' SYSTEM LIGHT ON AFTER GEAR RETRACTION, CYCLED GEAR AND LIGHT STILL ON. NOISES AND VIBRATION AS IF GEAR DOORS WERE OPEN. ACFT AIR RETURNED TO CLE. MAINTENANCE ADJUSTED RT GEAR UPLOCK TARGETS IAW EMB MM 32-60-01. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000921995021700092SO 1995 2 17 C2XA95CL015 119950202A32301959500007 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091571310640 120114 SYR-CLE - FLT 3189 - THE RT MAIN GEAR WOULD NOT RETRACT. FERRIED ACFT TO CLE. MAINTENANCE ADJUSTED RT MAIN GEAR ACTUATOR AND OPS CHECK GOOD. IAW EMB MM 32-30-00. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000931995021700093SO 1995 2 17 C2XA95CL017 119950206A5753KRP138112VT ROLLER'S EMB 120 EMB120RT SO LT TE FLAP BINDING A C2XAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW0916729 120185 CLE-DTW - FLT 3141 - AIR RETURN, O/B FLAP DISAGREEMENT. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ACTUATOR IAW EMB MM 27-50-09. OPS CHECK GOOD. ACFT SENT ON TEST FLIGHT, TEST FLIGHT FAILED. MAINTENANCE REMOVED AND REPLACED LT O/B FLAP ROLLER'S IAW EMB MM 27-50-12. OPS CHECK GOOD. ACFT SENT ON TEST FLIGHT, TEST FLIGHT WAS SATISFACTORY. ACFT RETURNED TO SERVICE 02/07/95. (W) 2L72 4T RTA31SO 19950217000941995021700094SO 1995 2 17 C2XA95CL018 119950207A2913PV302229 HYD PUMP EMB 120 EMB120RT SO LT ENGINE FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW09167029347 120078 CLE-DAY - FLT 3223 - THE LT MAIN HYDRAULIC PUMP FAILED IN FLIGHT. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED LT ENGINE HYDRAULIC PUMP IAW EMB MM 29-10-03. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000951995021700095SO 1995 2 17 C2XA95CL020 119950206A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTIONED A AC2XAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW09157219847 120160 CLE- FLT 3276 - FLAP DISAGREEMENT AFTER TAKEOFF. ACFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED THE LT I/B FLAP ACTUATOR IAW EMB MM 27-50-07. OPERATIONAL CHECKS WERE GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950217000961995021700096EU 1995 2 17 USAA950022 119950122A326020111251225 SENSOR FOKKERF28 F28MK0100 4990807EU LT MLG FAULTED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19864US 11306 MCO - FLT 8004 - ON TAKEOFF, LIFT DUMPER FAULTED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE L3 SENSOR ON LT GEAR MM 32-63-03 PG 401. RAN BITE TEST. NO FAULT ON LIFT DUMPERS, OPERATIONS CHECK NORMAL. (W) 2L72 4F RT 19950217000971995021700097EU 1995 2 17 USAA950023 119950117A5210D26245403 SEAL FOKKERF28 F28MK0100 4990807EU CABIN DOOR WORN A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19864US 11306 PIT - FLT 114 - RUSHNG AIR SOUND WAS HEARD COMING FROM THE MED BY F/A. CABIN BEGAN TO CLIMB. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR SEAL. PRESSURIZED AND OPERATIONS CHECK OK. (W) 2L72 4F RT 19950217000981995021700098EU 1995 2 17 USAA950024 119950119A2910 NUT FOKKERF28 F28MK0100 4990807EU HYD PUMP LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19886US 11346 PIT - FLT 1025 - AFTER TAKEOFF, THE CREW GOT A 'HYD SYS 2 LO QTY' ALERT. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PRESSURE LINE 'B' NUT ON UPPER PUMP LOOSE AT QUICK DISCONNECT. MAINTENANCE TIGHTENED FITTING. SERVICED, RAN ENGINE, ALL OPERATIONS NORMAL. (W) 2L72 4F RT 19950217000991995021700099NM 1995 2 17 USAA950025 119950111A2130 PRESSURIZATION BOEING737 7374B7 1384702NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19436US 24558 ORF - FLT 124 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES. OPS CHECK NORMAL. SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES. OPS CHECK NORMAL. SWAPPED UNITS BACK TO ORIGNAL CONFIGURATION, BITE TEST OF TEMP CONTROL UNITS OK. (W) 2L72 4F RTA16WE 19950217001001995021700100NM 1995 2 17 USAA950028 119950114A5242 DOOR BOEING737 737301 1384611NM E/E BAY NOT LOCKED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19334US 23231 MCO - FLT 682 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FOUND FWD ELECTRICS BY DOOR UNLATCHED. CLOSED AND SECURED DOOR. SYSTEM CHECKS NORMAL. (W) 2L72 4F RTA16WE 19950217001011995021700101NM 1995 2 17 USAA950038 119950125A7920 LINE BOEING737 7374B7 1384702NM NR 2 ENGINE CRACKED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19427US 24549 MCO - FLT 350 - EN ROUTE, THE NR 2 ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE BEGAN TO DROP AND OIL TEMPERATURE REMAINED NORMAL. FLIGHT CREW IDLED ENGINE AND DIVERTED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FOUND OIL LINE FROM GEAR BOX TO OIL PRESSURE SWITCH CRACKED. REPLACED LINE AND ADDED 16 QUARTS OF OIL. RAN ENGINE, CHECKED CHIP DETECTORS, ALL CLEAN. OIL PRESSURE OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950217001021995021700102EU 1995 2 17 USAA950039 119950123A3230 RETRACT MECH FOKKERF28 F28MK0100 4990807EU RT MLG ICED UP A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19869US 11314 PIT - FLT 977 - ON TAKEOFF, THE CREW GOT A RT MAIN LANDING GEAR WARNING ON THE MFDU. GEAR WAS RECYCLED BUT THE WARNING REMAINED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A LARGE AMOUNT OF ICE AND SAND FROM THE MLG. OPERATION CHECKS NORMAL. (W) 2L72 4F RT 19950217001031995021700103NM 1995 2 17 9501925525 119950107A5400311N3510152 WEB BOEING757 757251 1384970NM NAC STA 102 WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01525US 25520 23619 DURING PERIODIC CHECK, THE NR 2 ENGINE PYLON FAN COWL SUPPORT BEAM WEB WAS FOUND WORN AT APPROXIMATELY NAC RBL 11, NAC STA 102. INSTALLED REPAIR DOUBLER PER SRM 51-70-13, FIG.1 AND NWA EA 55-93697. 2L72 4F RTA2NM 19950217001041995021700104WP 1995 2 17 9501939754 119950205A7711 EPR INDICATION DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01754NW 47178 676245 AS THROTTLES WERE ADVANCED FOR TAKEOFF, THE NR 2 ENGINE EPR INDICATOR HUNG AT 1.5. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE CREW PERFORMED A GROUND RUN-UP ON BOTH ENGINES. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950217001051995021700105NM 1995 2 17 95FDEA00115 119950207A3310 LIGHT BOEING727 7272S2F 1384O81NM FE TABLE SMOKING A FDEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO04201FE 22924 SMOKE WAS COMING FROM FLUORESCENT LIGHT AND RIGHT TABLE LIGHT AREA. PULLED C/B FOR F/E TABLE FLUORESCENT LIGHT FIXTURE. NO FURTHER SMOKE, TIGHTENED LOOSE WIRE. 2L73 4F A3WE 19950217001061995021700106NM 1995 2 17 95FDEA00116 119950204A532065453136 CLIP BOEING727 72725 1384006NM BS 4OO DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 MECHANICAL DAMAGE FOUND ON STR CLIP AT BS 400 STR 6L. REMOVED AND REPLACED STR CLIP AT BS 400 STR 6L. 2L73 4F A3WE 19950217001071995021700107NM 1995 2 17 95FDEA00117 119950205A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 600-720 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 MECHANICAL DAMAGE ON SEAT TRACK AT BS 600 PLUS 16 INCHES - 620 PLUS 3, BL 0, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM BS 600 - 720, BL 0, WL 208.5. 2L73 4F A3WE 19950217001081995021700108NM 1995 2 17 95FDEA00118 119950207A521050794516 BEAM BOEING727 72725 1384006NM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FWD ENTRY DOOR LOWER GATE BEAM HAS A 1.5 INCHES CRACK ON FWD SIDE. REMOVED AND REPLACED FWD ENTRY DOOR LWR GATE BEAM. 2L73 4F A3WE 19950217001091995021700109NM 1995 2 17 95FDEA00119 119950207A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 620-627 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON SEAT TRACK FLANGE BS 620-627, LBL 45, WL 208.5 IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT BS 590 - 650, LBL 45, WL 208. 2L73 4F A3WE 19950217001101995021700110NM 1995 2 17 95FDEA00120 119950207A5347 SEAT TRACK BOEING727 72725 1384006NM BS 480-483 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON SEAT TRACK FLANGE BS 480-483 LBL 46 WL 208.5. REMOVED AND REPLACED SEAT TRACK AT BS 480-590 LBL 46 WL 208.5 PER FEDEX SRM 53-10-5. 2L73 4F A3WE 19950217001111995021700111NM 1995 2 17 95FDEA00121 119950207A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 344-347 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON SEAT TRACK FLANGE AT BS 344-347, LBL 42, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 344-400, LBL 45, WL 208. 2L73 4F A3WE 19950217001121995021700112NM 1995 2 17 95FDEA00122 119950207A575465162276 SKIN BOEING727 72725 1384006NM NR 6 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION (76C002-00) NR 6 K-FLAP DATAPLATE. REMOVED DAMAGE AROUND DATAPLATE, REPAIRED K-FLAP WEB AND RELOCATED DATAPLATE IAW SRM 5250-3, DWG SR 27-57-010 REV B. 2L73 4F A3WE 19950217001131995021700113NM 1995 2 17 95FDEA00123 119950209A53122024T3 BLKHD WEB BOEING727 72725 1384006NM BS 950 CRACK A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 POSSIBLE CRACK AT BS 950 BULKHEAD LBL 40 WL 185. REPAIRED CRACK IS 950 BULKHEAD AT LBL 40 WL 185 PER FEDEX SRM 53-10-9 FIG 2. 2L73 4F A3WE 19950217001141995021700114NM 1995 2 17 95FDEA00124 119950208A5330 SKIN BOEING727 72725 1384006NM BS 367 OIL CANNING A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 SKIN IS OIL CANNING BS 367 BETWEEN STR 22 AND 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950217001151995021700115NM 1995 2 17 95FDEA00125 119950209A53117075T6 FRAME BOEING727 72725 1384006NM BS 520 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION IS FWD CARGO BAY ON FRAME AT BS 520 STR 26 LBL 25. REMOVED CORROSION FROM FRAME OUT OF LIMITS PER SRM REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950217001161995021700116NM 1995 2 17 95FDEA00126 119950204A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 490/540/640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON SEAT TRACK FLANGE BS 490-540, 570 AND 640, RBL 25, WL 208.5. REMOVED AND REPLACED TRACK FROM BS 480-740 IAW FEDEX SRM 53-10-1. 2L73 4F A3WE 19950217001171995021700117NM 1995 2 17 95FDEA00127 119950209A5320651627910 BEAM BOEING727 72725 1384006NM BS 760-840 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION FOUND ON TOP AND BOTTOM SIDE OF LONGITUDINAL BEAM IS SEVERAL AREAS FROM BS 760-840 WL 208 LBL 25. REMOVED AND REPLACED LONGITUDINAL BEAM IAW 53-10-2. 2L73 4F A3WE 19950217001181995021700118NM 1995 2 17 95FDEA00128 119950209A5754M33692420240 SKIN BOEING727 72725 1384006NM NR 4 LE FLAP GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FIXED L/E GOUGED ON LOWER SURFACE AT NR 4 SLAT I/B TRACK. REMOVED EXISTING REPAIR AND FABRICATED AND INSTALLED NEW REPAIR PER FEDEX SRM 5730-2. 2L73 4F A3WE 19950217001191995021700119NM 1995 2 17 95FDEA00129 119950208A53202024T3 DOUBLER BOEING727 72725 1384006NM BS 415-457 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 BS 451-457 BETWEEN STR 18-19R RBL 65 INTERNAL DOUBLER ON E-BAY EXHAUST HAS SIGNS OF CORROSION. REMOVED OLD DOUBLER BS 451-457 STR 18 AND 19R RBL 65 AND INSTALLED NEW DOUBLER. 2L73 4F A3WE 19950217001201995021700120NM 1995 2 17 95FDEA00130 119950206A5330M392346 SKIN BOEING727 727233 138408ANM BS 1095 OIL CAN A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22321 DENT IN SKIN OUT OF LIMITS 1 INCHE WIDE BY 7 INCHES LONG BY .080 DEEP AT BS 1095 WL 134.5 LBL 24. REWORKED DENT AT BS 1095 WL 134.5 LBL 24 TO WITHIN LIMITS FOUND SKIN TO OIL CAN. REMOVED DAMAGE FABRICATED PARTS AND INSTALLED ON A/C ALL WORK DONE IAW SRM 53-30-3. 2L73 4F RTA3WE 19950217001211995021700121NM 1995 2 17 95FDEA00131 119950207A53302024T3M409741 SKIN BOEING727 727233 138408ANM BS 187 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 DENT IN SKIN OUT OF LIMITS 2 INCHES WIDE BY 3 INCHES BY .085 DEEP AT BS 187 WL 160 RBL 12. REPAIRED DAMAGED AREA BS 187 WL 160 RBL 12 PER FEDEX SRM 53-30-3. 2L73 4F RTA3WE 19950217001221995021700122NM 1995 2 17 95FDEA00132 119950207A575365265423 FITTING BOEING727 727233 138408ANM LT TE MID FLAP DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 WHILE WORKING FEDEX CARD 75C051-00 FOUND I/B DRUM SUPPORT BACKUP FITTING HEAVILY GOUGED. REMOVED GOUGED FITTING IN L/W I/B MIDFLAP LOCATED AND DRILLED AND INSTALLED NEW FITTING. 2L73 4F RTA3WE 19950217001231995021700123NM 1995 2 17 95FDEA00133 119950209A55002024T3050 WEB BOEING727 727233 138408ANM BS 1303 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 BS 1303 WEB IS CRACKED LWR LEFT CORNER (MARKED). REPAIRED CRACK LWR LEFT CORNER BS 1303 IAW FEDEX DRAWING SR 27-53-015. 2L73 4F RTA3WE 19950217001241995021700124NM 1995 2 17 95FDEA00134 119950210A33103285 LIGHT BOEING727 7272S2F 1384O81NM FE PANEL FAILED A FDEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO04201FE 22924 SMOKE COMING FROM ENGINEERS FLUORESCENT LIGHT, THIS IS A REPEAT WRITE UP. FOUND FLT ENGINEER'S RT AFT TABLE LIGHT BAD, WITH A BURNT ODOR FROM LIGHT. REMOVED AND REPLACED SAME. OPS CHECKS NORMAL AS PER MM 33-10. 2L73 4F A3WE 19950217001251995021700125NM 1995 2 17 95UAL727012 119950206A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE EXTERIOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297452U 21906 BOTH LEFT AND RIGHT AFT EXTERIOR EMERGENCY SLIDE LIGHTS INOPERATIVE. REPLACED M983 BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950217001261995021700126NM 1995 2 17 95UAL727013 119950206A2120 AIR DISTR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN ODOR A UALAK NONE L NO TEST NRNOT REPORTED 1 WP297265U 21412 ELECTRICAL SMELL NEAR ROW 10. SMELL EXTENDED THROUGHOUT CABIN. 2L73 4F4 F A3WE E2EA 19950217001271995021700127 1995 2 17 95UAL747006 419950208A25657A1323107 SLIDE BOEING747 747422 1384935NM PWA 4056 PW4056 NE MULTIPLE AREAS FAILED TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 SLIDE FAILED AIR RETENTION SHOP TEST DUE TO POROSITY. ADDITIONALLY HOSES FROM CYLINDER TO SLIDE INCORRECTLY POSITIONED. SLIDE SCRAPPED. 2L74 4F4 FRTA20WE E24NE 19950217001281995021700128NE 1995 2 17 95UAL747007 219950209A75307479558 VANE CONTROL BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE NR 4 ENGINE WORN A UALAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 WP29160UA 1174 21237 686035 NR 4 ENGINE FLAMEOUT AT TOP OF DESCENT ENGINE REPLACED. INVESTIGATION REVEALED WEAR OF INTERNAL EVC COMPONENTS CAUSED THE IMPROPER POSITIONING OF THE COMPRESSOR VANES. THE CORRELATION BETWEEN THE RAPID COMPONENT DEGRADATION AND THE NEW PRATT AND WHITNEY VANE SCHEDULE, WHICH WAS INCORPORATED INTO THIS UNIT, IS BEING INVESTIGATED. 2L74 4F4 F A20WE E20EA 19950217001291995021700129WP 1995 2 17 95UALD10015 119950206A217021D10C011 COALESCER BAGS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN CONTAMINATED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP291828U 46627 FUMES IN CABIN DURING PREFLIGHT FROM LIGHT TO STRONG. APU SUPPLYING PACKS WITH STRONG TAIL WIND. DURING TAXI AND CLIMB FUMES STRONG CAUSING EYES AND NOSES TO WATER AND BURN. FUMES DISSIPATED WITH NR 2 ENGINE PNEU SUPPLY OFF. ACCOMPLISHED PACK BURN OUT AND REPLACED THE THREE COALESCER BAGS. 2L73 4F4 F A22WE E23EA 19950217001301995021700130 1995 2 17 95UALD10016 419950206A2310 HF RADIOS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL LT/RT MALFUNCTIONED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP291846U 48262 MADE A HNL STOP DUE TO HF RADIOS WOULD NOT TRANSMIT AT CAPT, F/O OR S/O POSITIONS ON ANY FREQUENCY. 2L73 4F4 F A22WE E23EA 19950217001311995021700131WP 1995 2 17 95UALD10017 119950206A2730AJH7000 LOAD FEEL DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE ELEV SYS MIS-INDEXED A AUALAO OTHER P NO WARNING INDICATION CLCLIMB 1 WP291852U50898 47811 DURING CLIMB, RT WING HEAVY ELEVATOR INDICATION SPLIT. SIX DEG AILERON TRIM. NO HORIZONTAL STAB TRIM. ALL HYD PRESSURE OKAY. NO WARNING LIGHTS. FOUND ELEV LOAD FEEL UNIT INSTALLED 120 DEGREES OFF INDEX WHICH DISPLACED THE NEUTRAL OF THE ELEVATORS. CHAIN DRIVE UNIT FUSE FOUND SHEARED. DISCREPANCIES CORRECTED AND SYSTEMS CHECKED EXTENSIVELY. AIRCRAFT TEST FLOWN. 2L73 4F4 F A22WE E23EA 19950217001321995021700132WP 1995 2 17 ABXA9500079 119950209A25105925379523ABX1 SEAT DOUG DC9 DC941 302207NWP COCKPIT DEFECTIVE A ABXAK NONE O OTHER CRCRUISE 1 GL23967AX 47509 DURING CRUISE FLIGHT CAPTAIN'S SEAT DROPPED TO THE FLOOR. VERTICAL ADJUST DOESN'T SEEM TO BE LOCKING. INSPECTED, LUBED CAPTAIN'S SEAT ASSEMBLY UP AND DOWN LOCKING PINS AND LINKAGE CONTROL CABLE. OPS CHECKED GOOD. SEAT WAS REPLACED AS A PRECAUTIONARY MEASURE AT ILN IAW DC-9 MM 25-10. SEAT OPS CHECKED GOOD. 2L72 4F A6WE 19950217001331995021700133WP 1995 2 17 ABXA9500080 119950124A532099115467 WEB DOUG DC9 DC932F 3022067WP BS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK, INSPECTION WHILE COMPLYING WITH SB 53-241, FOUND LEVEL I CORROSION ON WEB AT LONGERONS 29L AND 27R, STA 996. REPAIRED IAW REA D953-10787-MR. 2L72 4F A6WE 19950217001341995021700134WP 1995 2 17 ABXA9500081 119950205A3231BLFR4245T2 BUSHING DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR SECONDARY LINKAGE FORK WORN AT THE DRIVE ROD. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950217001351995021700135WP 1995 2 17 ABXA9500082 119950205A52805913433503 HINGE DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON OUTBOARD MAIN LANDING GEAR DOOR FOR WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950217001361995021700136WP 1995 2 17 ABXA9500083 119950128A57133911238516 STRINGER DOUG DC9 DC931 3022065WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03, S.B. 57-98, FOUND GOUGES IN STRINGER NR 11 BARREL NUT HOLE IN RIGHT WING. REMOVED GOUGES IN STRINGER NR 11 BARREL NUT HOLE IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950217001371995021700137WP 1995 2 17 ABXA9500084 119950128A57133911236504 STRINGER DOUG DC9 DC931 3022065WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D.90-18-03, S.B. 57-98, FOUND GOUGES ON TOP OF STRINGER NR 13 NEAR BARREL NUT HOLE. REMOVED GOUGES ON TOP OF STRINGER NR 13 IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950217001381995021700138WP 1995 2 17 ABXA9500085 119950131A78305958782503 TR LINK DOUG DC9 DC931 3022065WP NR 2 ENGINE NICKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 75-14-06, A.D.90-18-03, S.B.'S 78-36, 78-38, 78-40, 78-66, FOUND BY EDDY CURRENT INSPECTION TWO EACH CRACK INDICATIONS ON THE INBOARD LOWER THRUST REVERSER LINK ON THE NR 2 ENGINE. BLENDED NICKS ON THRUST REVERSER DRIVE LINK IAW DC-9 OVERHAUL MANUAL, CHAPTER 78-30-1. 2L72 4F A6WE 19950217001391995021700139WP 1995 2 17 MWEA95125 119950209A2750 CONTROL CABLE DOUG DC9 DC932 3022066WP TE FLAPS CORRODED A AMWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 PILOT REPORTS ROLL TENDANCY WHEN FLAPS ARE SELECTED TO 15 DEGREES. MECHANIC FOUND BROKEN FLAP BUS CABLE. FABRICATED NEW CABLE, INSTALLED AND RIGGED. OPS CHECK GOOD. RETURNED A/C TO SERVICE. CABLE WAS OF THE TYPE THAT HAS A CLEAR NYLON COATING. CABLE GETS DIRTY, NYLON CRACKS, CABLE CORRODES. CANNONT ADEQUATELY INSPECT CABLE WITH NYLON ON IT. 2L72 4F A6WE 19950217001401995021700140NM 1995 2 17 MWEA95126 119950209A25603952273501 GIRT BAR DOUG MD88 MD88 3023688NM AFT GALLEY DOOR OUT OF ADJUST A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 PILOT REPORTS AFT GALLEY SERVICE DOOR EVAC SLIDE GIRT BAR HARD TO REMOVE. MECHANIC ADJUSTED GIRT BAR LATCHES. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950217001411995021700141SW 1995 2 17 QXEA9500038 119950207A323027520001078 RETRACT MECH OZONE 0A555001 SWRNGNSA227 SA227AC 8780603SW NLG WORN A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09386PH AC597 GEG - NOSE GEAR SLOW (30 SECONDS) TO INDICATE GREEN ON GEAR EXTENSION. GEAR WARNING HORN SOUNDED WITH POWER LEVER REDUCTION FOR APPROX 30 SECONDS THEN INDICATION AND HORN OPERATED NORMALLY. INTRANSIT LIGHT ILLUMINATED WHILE GEAR WAS INTRANSIT BUT REMAINED OUT WHEN PROBLEMS WERE NOTED. AIRCRAFT FERRIED TO PDX FOR REPAIR. REPLACED BOTH CAMS BELL CRANK SPRINGS, PIVOT PINS, EMERGENCY SIDE ACTUATOR. GEAR OPS CHECK GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950217001421995021700142SW 1995 2 17 QXEA9500039 119950208A32302752003 BELLCRANKS SWRNGNSA227 SA227AC 8780603SW NLG REQ'D SHIMMING A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09386PH AC597 PDX - NLG WOULDN'T STAY IN THE WHEELWELL, GEAR CYCLES CONTINUALLY. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. RESHIMMED BOTH ACTUATOR BELLCRANKS AND ADJUSTED UPLIMIT SWITCH. NOSE GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950217001431995021700143NM 1995 2 17 QXEA9500040 119950207A32608700030012 PSEU ELDEC DORNERDO32 DO328100 2996000NM LANDING GEAR MALFUNCTIONING A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09329PH2868 531 3007 PDX - WOW LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT LANDED IN PDX WITHOUT FURTHER PROBLEMS. REPLACED PSEU AND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950217001441995021700144NM 1995 2 17 QXEA9500041 119950209A335010126291 EEL SIGN DHAV DHAV DHC8 DHC8102 2809003NM CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09821PH 104 SEA - EXIT SIGN AT 4A BROKEN. REPLACED SIGN AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950217001451995021700145WP 1995 2 17 9501949971 119950202A2780 T DUCT DOUG DC9 DC931 3022065WP LEFT SLAT BINDING A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL019335 47337 SLAT DISAGREEMENT LIGHT ILLUMINATED WHEN SLATS WERE SELECTED FOR LANDING INTO SRQ. AIRCRAFT EXPERIENCED A ROLL TO THE RIGHT. RECYCLED HANDLE THREE TIMES BEFORE LIGHT EXTENDED. NORMAL LANDING WAS ACCOMPLISHED. FOUND LEFT SLAT 'T' DUCT BINDING. ADJUSTED GUIDE BLOCKS AND LUBED. CYCLED SLATS NUMEROUS TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001461995021700146 1995 2 17 9501959754 419950207A3418 STALL TRANSDUCER DOUG DC9 DC941 302207NWP RIGHT FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01754NW 47178 STALL INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF WHEN FLAPS AND SLATS WERE RETRACTED. PERFORMED PRECAUTIONARY FLIGHT PROCEDURES AND NR 2 SYSTEM TESTED BAD. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT STALL WARNING TRANSDUCER AND TONE GENERATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001471995021700147WP 1995 2 17 9501969925 119950208A5246 FUEL DOOR DOUG DC9 DC932 3022066WP RT WING JAMMED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01925US 47472 SLATS WOULD NOT RETRACT FULLY AFTER TAKEOFF AND SLAT DISAGREEMENT LIGHT ILLUMINATED. RECYCLED SLATS TWICE WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING FUELING PANEL DOOR JAMMED INTO SLAT. REPLACED DAMAGED LATCH ON FUEL PANEL AND SECURED DOOR. SLATS RETRACTED NORMALLY ON OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001481995021700148NE 1995 2 17 9501979997 219950208A7532 PRBC VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL018933E 47142 656025 ON TAKEOFF, A COMPRESSOR STALL OCCURRED ON NR 1 ENGINE. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ENGINE WAS INSPECTED FOR DAMAGE, NON FOUND. MAINTENANCE REPLACED THE PRBC AND P/D VALVES. ENGINE WAS RUN UP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950217001491995021700149WP 1995 2 17 9501989863 119950204A5350 LOCK ARM DOUG DC9 DC951 3022051WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01772NC 47774 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE UPPER LEFT LOCK ARM WORN. ADJUSTED HANDLE AND REPLACED/RE-RIGGED THE LOCK ARM. CHECKED OK. 2L72 4F A6WE 19950217001501995021700150NE 1995 2 17 9501996615 219950207A7200 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 1 FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 GL01615US 20360 702147 DURING CRUISE, A MIST WAS NOTED COMING FROM THE UNDERSIDE OF THE NR 1 ENGINE. THE AIRCRAFT RETURNED TO NRT. THE ENGINE WAS SHUT DOWN 15 MINUTES BEFORE LANDING. NO FUEL WAS DUMPED. THE GEARBOX SCAVENGE PUMP WAS REPLACED AND A RUN-UP SHOWED NO EVIDENCE OF ANY LEAKAGE. THE AIRCRAFT WAS POSITION FERRIED TO KIX AND AGAIN EXPERIENCED THE MIST. THE AIRCRAFT WAS FERRIED BACK TO NRT WHERE THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E3NE 19950217001511995021700151WP 1995 2 17 9502009918 119950209A3260 UPLATCH MECH DOUG DC9 DC932 3022066WP LT MLG DOOR OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01940N 47572 DURING CLIMB-OUT FROM MCI, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME INDICATIONS. FLIGHT CONTINUED TO DESTINATION (MSP) AND NORMAL LANDING WAS ACCOMPLISHED. FOUND THE LEFT GEAR DOOR UPLATCH MECHANISM OUT OF ADJUSTMENT. ADJUSTED PER MM 32-31-4. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001521995021700152WP 1995 2 17 9502019918 119950209A3260 UPLOCK CONNECTOR DOUG DC9 DC932 3022066WP LT MLG DIRTY A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01940N 47572 DURING CLIMB-OUT FROM RST, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH SAME INDICATIONS. FLIGHT CONTINUED TO DESTINATION (MSP) AND NORMAL LANDING WAS ACCOMPLISHED. ADJUSTED THE LEFT MAIN GEAR DOOR ACTUATOR AND CLEANED CANNON PLUG TO THE LEFT MAIN GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001531995021700153WP 1995 2 17 9502029930 119950209A3010 SLIP JOINT DOUG DC9 DC931 3022065WP WING DE-ICE OUT OF POSITION A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL0189S 47042 AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH WING AIRFOIL SYSTEM ANTI-ICE ACTIVATED. LIGHT EXTINGUISHED WITH TAIL ANTI-ICE ACTIVATED. AFTER CYCLE OF TAIL SYSTEM, THE LIGHT REILLUMINATED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED FORWARD ICE PROTECTION PRESSURE ABNORMAL SWITCH AND SUPPLY PRESSURE REGULATOR. ALSO, FOUND SLIP JOINT BETWEEN FIRST AND SECOND RIGHT WING SLATS OUT OF POSITION. RESECURED SLIP JOINT. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950217001541995021700154NE 1995 2 17 9502039909 219950211A7230 COMPRESSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE NR 2 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 GL01959N 47255 657274 AS POWER WAS BROUGHT UP FOR TAKEOFF, COMPRESSOR STALLS OCCURRED ON NR 2 ENGINE APPROXIMATELY 85 PERCENT N2. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED A SMALL PIECE OF CARDBOARD FROM THE INLET AND INSPECTED FOR DAMAGE, NONE FOUND. THE ENGINE WAS RUN UP AND FOUND OK FOR CONTINUED SERVICE. 2L72 4F4 F A6WE E2EA 19950217001551995021700155NM 1995 2 17 9502046626 119950209A2612895312 FIRE LOOP BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE APU MALFUNCTIONED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 GL01626US 21708 702041 DURING FINAL APPROACH, THE APU FIRE LIGHT ILLUMINATED AND BELL SOUNDED. THE FIRE BOTTLE WAS DISCHARGED. INSPECTION FOUND NO SIGN OF FIRE AND THE BOTTLE WAS REPLACED. TROUBLESHOOTING FOUND THE FIRE WARNING LOOP 'A' TO BE AT FAULT. THE ELEMENT WAS REPLACED AND OPERATIONAL CHECK OF THE APU AND FIRE WARNING SYSTEM CHECKED OK. 2L74 4F4 F A20WE E3NE 19950217001561995021700156WP 1995 2 17 9502059756 119950209A5350 LATCHES DOUG DC9 DC941 302207NWP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE LATCHES. CHECKED OK. 2L72 4F A6WE 19950217001571995021700157WP 1995 2 17 ABXA9500086 119950210A335060030431 EEL POWER SUPPLY DOUG DC9 DC931 3022065WP CABIN DEFECTIVE A ABXAK NONE L NO TEST CRCRUISE 1 GL23947AX 3349 47004 COCKPIT EMERGENCY LIGHTS INTERMITTENTLY GO DIM TO BRIGHT. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-9 MM 33-53-0. 2L72 4F A6WE 19950217001581995021700158SO 1995 2 17 COM11770 119950211A541112039739002 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01137H 14481 120137 DURING INSPECTION FOUND RIGHT NACELLE OUTBOARD HALF FRAME P/N 120-39739-002 TO BE CRACKED. REMOVED FRAME AND INSTALLED SERVICEABLE HALF FRAME P/N 120-48439-002. ORIGINAL FRAME THICKNESS 15.032 INCH NEW FRAME 15.040 INCH INSTALLED AS PER EMB 120 SRM AND AERODESIGN REPORT NR 661-13. 2L72 4T RTA31SO 19950217001591995021700159SO 1995 2 17 COM11771 119950212A541112007881004 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01137H 14481 120137 DURING INSPECTION, FOUND RIGHT NACELLE HALF FRAME P/N 120-07881-004 TO BE CRACKED. REPAIRED PER EMB SRM. INSTALLED PER AERODESIGN REPORT NR 661-13 DATED 2-12-95. 2L72 4T RTA31SO 19950217001601995021700160SO 1995 2 17 COM11772 119950207A5753PE610261 ROLLER EMB 120 EMB120RT SO TE FLAPS WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254CA 120233 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. REPLACED THE OUTBD FLAP ROLLERS. 2L72 4T RTA31SO 19950217001611995021700161SO 1995 2 17 COM11773 119950203A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01261CA7919 120254 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSP TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1387.2. P/N 120-17056-015 4 EA; 120-17057-008 2 EA; 120-17056-007 1 EA; 120-17057-015 1 EA; 120-17056-013 1 EA; 120-17056-017 2 EA; 120-17056-019 2 EA. 2L72 4T RTA31SO 19950217001621995021700162SO 1995 2 17 COM11774 119950205A5720 SUPPORTS EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01259CA 120252 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1387-2. P/N 120-17056-019 2 EA; 120-17056-017 2 EA; 120-17056-015 1 EA; 120-17056-013 1 EA; 120-17057-005 1 EA; 120-17057-007 1 EA; 120-17057-006 1 EA. 2L72 4T RTA31SO 19950217001631995021700163SO 1995 2 17 COM11775 119950209A492038003761 APU EMB 120 EMB120RT SO AFT FUSELAGE FAILED A COMAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE TXTAXI/GRND HDL 1 SO01243CA3039 120212 APU TEMP REACHED 680 DEG DURING START. RAMP PERSONNEL SAW FLAMES 3 MINUTES AFTER ABORT. REPLACED APU. 2L72 4T RTA31SO 19950217001641995021700164SO 1995 2 17 COM11776 119950209A31508005579 WARNING UNIT EMB 120 EMB120RT SO E/E BAY DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01261CA115216926 120254 TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED THE AURAL WARNING UNIT. 2L72 4T RTA31SO 19950217001651995021700165EU 1995 2 17 COM31032 119950209A27207253899420 LEVER SAAB SF340 SF340A 7850100EU RUDDER WORN A COMAK NONE O OTHER CRCRUISE 1 SO01370CA 340A010 MODERATE YAWING OSCILATION DURING CRUISE AND DESCENT. REPLACED WORN RUDDER TRIM TAB BEARINGS AND WORN DAMPER YAW LEVER. BEARINGS P/N MS28912-6C, 7255439-007. 2L72 4T RTA52EU 19950217001661995021700166EA 1995 2 17 COM60411 119950207A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT/RT TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01940CA169 8 7048 FLAPS FAILED WHILE ATTEMPTING TO EXTEND FOR DE-ICE. REPLACED THE LT AND RT BPSU. 2L72 4F RTA21EA 19950217001671995021700167EA 1995 2 17 COM60412 119950210A274283962 TRIM ACTUATOR CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01941CA667 7050 STABILIZER TRIM CHANNEL 2 WILL NOT ENGAGE. REPLACED THE HORIZONTAL STAB TRIM ACTUATOR. 2L72 4F RTA21EA 19950217001681995021700168EU 1995 2 17 DL31L950576 119950208A2530 COFFEE MAKER AIRBUS310 A310324 3930206EU FWD GALLEY BURNING ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11835AB 650 DURING CRUISE, HAD BURNING ODOR IN FORWARD GALLEY AREA AT COFFEE MAKERS, REMOVED COFFEE MAKER POWER ODOR DISSIPATED. REMOVED COFFEE MAKERS, INSPECTED WIRING THEN CYCLED MAKERS, COULD NOT DUPLICATE, RETURNED TO SERVICE. 2L72 4F RTA35EU 19950217001691995021700169NM 1995 2 17 DL72W950577 119950205A261365349203 DETECTOR UNIT BOEING727 727247 138408FNM NR 1 ENGINE FAILED A DALAE ENGINE SHUTDOWN M OVER TEMP CLCLIMB 1 SO112822W 21327 ON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED, UNABLE TO EXTINGUISH, SHUT DOWN NR 1 ENGINE. REPLACED DETECTOR UNIT, SECURED DUCT CLAMP AT 13TH STAGE VALVE, RETURNED TO SERVICE. 2L73 4F A3WE 19950217001701995021700170NM 1995 2 17 DL757950506 119950204A5330 SKIN BOEING757 757232 1384965NM FS 465 PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 RT SIDE OF FUSELAGE SKIN HAS A 3 INCH DIAMETER HOLE PUNCTURED AT FS STA 465 AT STR 20RT. REPAIRED PER SRM 53-00-01 FIG 205 PAGE 212-215 AND ERA 301133-14 FOR FASTENER SUBSTITUTION DAMAGE OCCURED AND REPAIRED DURING HMV, VISIT. 2L72 4F RTA2NM 19950217001711995021700171WP 1995 2 17 DLL10950575 119950208A55101524940294 FAIRING LKHEED1011 10113851 5265010WP RT STABILIZER CRACKED A DALAK NONE E VIBRATION/BUFFET CLCLIMB 1 SO11712DA 193C1088 ON CLIMB-OUT, HEARD UNUSUAL RUMBLE AS AIRCRAFT ACCELERATED, RUMBLE INCREASED WITH SPEED. FOUND RIGHT LOWER STAB TO FUSELAGE FAIRING LEADING EDGE UNFAIRED WITH SUBSTRUCTURE CRACKED. REPLACED FAIRING PER MM 55-16-00. 2L73 4F A23WE 19950217001721995021700172WP 1995 2 17 DLL16950089 119950104A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 639 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11763DL 193Y1197 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 639 AT BL 31R. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950217001731995021700173NM 1995 2 17 DLM88950574 119950207A21216054577 FAN DOUG MD88 MD88 3023688NM FLIGHT DECK FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11916DL 49591 ON APPROACH TO DFW, ENCOUNTERED STRONG ACRID BURNING ODOR IN CABIN AND FLIGHT DECK. PERFORMED SMOKE AND FUME CHECKLIST, LANDED WITHOUT INCIDENT. FOUND CABIN RECIRCULATION FAN SHORTED, REPLACED FAN OPERATION NORMAL. 2L72 4F RTA6WE 19950217001741995021700174WP 1995 2 17 MWEA95127 119950212A523059101419 DOOR PAN DOUG DC9 DC914 3022034WP FWD CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING ROUTINE INSPECTION OF CARGO DOORS, THE FWD CARGO DOOR PAN WAS FOUND TO BE CRACKED IN RADIUS APPROX 1.25 INCH IN LENGTH. REPAIRED DOOR PAN IAW SRM 52-03, FIG 8. REINSTALLED DOOR. PERFORMED LEAK AND OPS CHECK. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950217001751995021700175WP 1995 2 17 MWEA95128 119950212A38107914210538 WATER LINE DOUG DC9 DC932 3022066WP RT MLG WW LEAKING A MWEAK NONE O OTHER LDLANDING 1 GL31501ME 47132 PILOT REPORTS LANDING GEAR HANDLE TOOK MORE THAN NORMAL FORCE TO PUT IN DOWN POSITION PRIOR TO LANDING. ALSO, PILOT REPORTED DURING LANDING AS BRAKES WERE APPLIED THERE WAS LITTLE BRAKING AND THE PEDAL PRESSURE FELT ERRATIC. PEDAL PRESSURE FELT ERRATIC DURING BRAKE RELEASE ALSO. MECHANICS FOUND ICE ON CABLES FOR LANDING GEAR AND ON BRAKE CABLES DUE TO POTABLE WATER LINE LEAK ABOVE RT WHEEL WELL. REPAIRED WATER LINE. REMOVED ICE FROM CABLES. PERFORMED OPS CHECK. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950217001761995021700176WP 1995 2 17 MWEA95129 119950212A38107914210536 WATER LINE DOUG DC9 DC915 3022036WP FWD BAG COMPT DISCONNECTED A MWEAK NONE O OTHER CRCRUISE 1 GL31900ME 45841 PILOT REPORTED STIFF AILERONS IN FLIGHT. MECHANICS FOUND LINE FOR WATER SYSTEM DISCONNECTED WHICH CAUSED WATER TO DRAIN INTO WHEEL WELLS FORMING ICE ON AILERON PULLEY CLUSTERS. REMOVED ICE FROM PULLEYS. INSPECTED CABLES AND PERFOMRED OPS CHECK. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950217001771995021700177EU 1995 2 17 QXEA9500042 119950210A33501012721 EEL FOKKER FOKKERF28 F28MK1000 4990808EU CABIN LOOSE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 BOI - EMERGENCY EXIT LIGHT AT SEAT 12B FELL OFF. RESECURED LIGHT AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950217001781995021700178EU 1995 2 17 QXEA9500043 119950210A33501012721 EEL FOKKER FOKKERF28 F28MK1000 4990808EU CABIN MISSING A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - FLOOR PROXIMITY LIGHT MISSING FROM SEAT 2AB. REPLACED LIGHT AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950217001791995021700179NM 1995 2 17 QXEA9500044 119950210A335010005511 EEL DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09830PH 314 PDX - COCKPIT EMER LIGHT INOP. REPLACED LIGHT ASSY AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950217001801995021700180NM 1995 2 17 QXEA9500045 119950210A335010005511 EEL DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09830PH 314 GEG - COCKPIT EMER LIGHT INOP. REPLACED LIGHT ASSY AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950217001811995021700181EU 1995 2 17 QXEA9500046 119950211A2560S80227 BOTTLE SWITLIK S130508 FOKKERF28 F28MK1000 4990808EU GALLEY LOW PRESSURE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09468US 598 11095 GEG - ESCAPE SLIDE BOTTLE PRESSURE IS IN RED ARC. SERVICED BOTTLE TO 3200PSI IAW MAINT MANUAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950217001821995021700182SW 1995 2 17 QXEA9500047 119950212A3310 PANEL SWRNGN SWRNGNSA227 SA227AC 8780603SW COCKPIT SHORTED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09380PH AC582 PDX - STRONG ELECTRICAL SMELL IN COCKPIT. REPLACED RIGHT HAND FORWARD CONSOLE LIGHTING PANEL. LIGHT PANEL OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950217001831995021700183NM 1995 2 17 SWAA950169 119950203A5312BACB30FP6A BLKHD WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0728SW 21339 DURING SCHEDULED CHECK, FOUND CRACKS IN THE FWD PRESSURE BULKHEAD WEB BETWEEN WL 184 TO 207, BS 178. REPAIRED PER SWA RA 1-253-1240. 2L72 4F A16WE 19950217001841995021700184NM 1995 2 17 SWAA950170 119950203A5312BAC1505100361 BLKHD TEE BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0728SW 21339 DURING SCHEDULED C3 CHECK, FOUND TWO CRACKS IN THE I/B AND O/B FWD TEE CHORDS AT BS 178 PRESSURE BULKHEAD, LBL 5.7. REPAIRED PER SWA RA 1-253-1240. 2L72 4F A16WE 19950217001851995021700185NM 1995 2 17 UPS202243 119950208A32601000679 EEL BOEING727 72730C 1384009NM FLIGHT DECK INOP A IPXAK NONE L NO TEST UKUNKNOWN 1 SO01906UP 19314 PILOT REPORTED EMERGENCY EXIT UNARMED. INDICATOR LIGHT WILL NOT TEST OR ILLUMINATE WHEN DISARMED. CHANGED LIGHT BULB, NO HELP. RELAMPED, OPS CHECKED OK. 2L73 4F A3WE 19950217001861995021700186NM 1995 2 17 UPS202244 119950208A33501000679 EEL BOEING727 72731C 1384011NM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01922UP 19231 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT OVER MAIN CABIN DOOR INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKED GOOD. 2L73 4F A3WE 19950217001871995021700187NM 1995 2 17 UPS202246 119950209A33501000679 EEL BOEING727 72762C 138402CNM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01912UP 19244 (SUPPLEMENTAL MRR) FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMER. EXIT LIGHT ASSY AS PER MM 33-50-01. OPS CHECKED GOOD. 2L73 4F A3WE 19950217001881995021700188NM 1995 2 17 UPS202247 119950213A532065225513 CHANNEL BOEING727 727172C 1384058NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 DURING 'C' CHECK IN NAPLES, MAINTENANCE FOUND CHANNEL CORRODED BEYOND LIMITS AT STA 1342, WL 259. REPLACED CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950217001891995021700189NM 1995 2 17 UPS202249 119950213A5711 SPAR CHORD BOEING727 72725C 138400HNM FS 1342 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND REAR SPAR BULKHEAD CHORD HAS A CRACKED ANGLE ON THE RT SIDE AT F/S 1342, RBL 16. REPLACED ANGLE PER BOEING DRAWING 65-19104 AND SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950217001901995021700190NM 1995 2 17 UPS202250 119950213A5311 FRAME BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT LOWER FRAME CHORD CORRODED AT RBL 24, WL 220. REPLACED LOWER CHORD PER SRM 51-30-2, AND UPS EO B727-5530-4001. 2L73 4F A3WE 19950217001911995021700191NM 1995 2 17 UPS202251 119950213A5320 CHORD BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT O/B CHORD AT RBL 30, WL 250 IS CORRODED. REPLACED CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950217001921995021700192NM 1995 2 17 UPS202252 119950213A53206593155677 CHANNEL BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT AFT CHANNEL CORRODED AT RBL 18, WL 247. REPLACED CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950217001931995021700193NM 1995 2 17 UPS202253 119950213A532065225517 CHANNEL BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 CENTER CHANNEL CORRODED AT WL 247. REPLACED CENTER CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950217001941995021700194NM 1995 2 17 UPS202254 119950213A5311 FRAME BOEING727 72725C 138400HNM STA 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT FRAME CHORD CORRODED AT RBL 20, WL 238. REPLACED CHORD PER UPS EO B727-5530-4601B. 2L73 4F A3WE 19950217001951995021700195NM 1995 2 17 UPS202255 119950213A5311 FRAME BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT LOWER FRAME CHORD CORRODED AT LBL 24, WL 220. REPLACED CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950217001961995021700196NM 1995 2 17 UPS202256 119950213A5320 CHORD BOEING727 72725C 138400HNM STA 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT O/B CHORD CORRODED AT LBL 30, WL 250. REPLACED CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950217001971995021700197NM 1995 2 17 UPS202257 119950213A5320 CHORD BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 FWD CHORD CORRODED. REPLACED FWD CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950217001981995021700198NM 1995 2 17 UPS202258 119950213A5311 FRAME BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT FRAME CHORD CORRODED AT LBL 20, WL 228. REPLACED CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950217001991995021700199NM 1995 2 17 UPS202259 119950213A5320 CHANNEL BOEING727 72725C 138400HNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 LEFT CHANNEL CORRODED AT LBL 18, WL 247. REPLACED CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950217002001995021700200NM 1995 2 17 UPS202260 119950213A5530 CHORD BOEING727 72725C 138400HNM FIN STA 22.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND RT INNER CHORD FIN CRACKED AND CORRODED AT FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER BOEING DRAWING 65C20296 AND 65C20381. 2L73 4F A3WE 19950217002011995021700201NM 1995 2 17 UPS202261 119950213A5530 ANGLE BOEING727 72725C 138400HNM FS 1345 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND RT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-3. 2L73 4F A3WE 19950217002021995021700202NM 1995 2 17 UPS202262 119950213A5530 ANGLE BOEING727 72725C 138400HNM FS 1345 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND LEFT SKIN SUPPORT ANGLE CRACKED AT FS 1345, FIN STA 22.5. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950217002031995021700203NM 1995 2 17 UPS202263 119950213A5330 SKIN BOEING727 72725C 138400HNM FS 1283-1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING 'C' CHECK, MAINTENANCE FOUND SKIN LAP AT STR 14L FROM STA 1283-1342 IS CORRODED. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950217002041995021700204NM 1995 2 17 UPS202264 119950210A531169154054 FRAME BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND RT FRAME CHORD FS 1342, RBL 20, WL 238 IS CORRODED. INSTALLED REPAIR IAW BOEING DWG 69-15405 AND SRM 51-30-2. 2L73 4F A3WE 19950217002051995021700205NM 1995 2 17 UPS202265 119950210A531165175086 FRAME BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND RT FRAME LWR CHORD RBL 24, WL 220, FS 1342 IS CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-17508 AND SRM 51-30-2. 2L73 4F A3WE 19950217002061995021700206NM 1995 2 17 UPS202266 119950210A531165175085 FRAME BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND RT FRAME LWR CHORD LBL 24, WL 220, FS 1342 IS CORRODED. INSTALLED REPAIR IAW EO B727-5530-4601. 2L73 4F A3WE 19950217002071995021700207NM 1995 2 17 UPS202267 119950210A532065225513 CHANNEL BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER CHANNEL IS CORRODED FS 1342, WL 242. INSTALLED REPAIR IAW EO B727-5530-4601. 2L73 4F A3WE 19950217002081995021700208NM 1995 2 17 UPS202268 119950210A532065225512 CHANNEL BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 RT CHANNEL WL 247, RBL 18 CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-93155 AND SRM 51-30-2. 2L73 4F A3WE 19950217002091995021700209NM 1995 2 17 UPS202269 119950210A532065225511 CHANNEL BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FS 1342 LEFT CHANNEL WL 247, LBL 18 CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-93155 AND SRM 51-30-2. 2L73 4F A3WE 19950217002101995021700210NM 1995 2 17 UPS202270 119950210A532065195322 CHORD BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND RT OUTBOARD CHORD FS 1342, RBL 30, WL 250 CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-19532 AND SRM 51-30-2. 2L73 4F A3WE 19950217002111995021700211NM 1995 2 17 UPS202271 119950210A532065195321 CHORD BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND LEFT OUTBOARD CHORD FS 1342 LBL 30, WL 250 CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-19532 AND SRM 51-30-2. 2L73 4F A3WE 19950217002121995021700212NM 1995 2 17 UPS202272 119950210A532065209812 CHORD BOEING727 72727C 138400JNM FS 1342 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND STA 1342 FWD CHORD CRACKED AND CORRODED. INSTALLED REPAIR IAW BOEING DWG 65-20981 AND SRM 51-30-2. 2L73 4F A3WE 19950217002131995021700213NM 1995 2 17 UPS202273 119950210A531169154053 FRAME BOEING727 72727C 138400JNM FS 1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND LEFT FRAME CHORD STA 1342, LBL 20, WL 228 CORRODED. INSTALLED REPAIR IAW BOEING DWG 69-15405 AND SRM 51-30-2. 2L73 4F A3WE 19950217002141995021700214NM 1995 2 17 UPS202274 119950210A5330 DOUBLER BOEING727 72727C 138400JNM FS 1323-1342 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND AT FS 1323-1342 STR 9L-10L LIGHT CORROSION BETWEEN INNER DOUBLER AND SKIN. INSTALLED REPAIR IAW SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950217002151995021700215NM 1995 2 17 UPS202275 119950210A5330 SKIN BOEING727 72727C 138400JNM FS 1325 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FUSELAGE UPPER SKIN LAP CORRODED BEYOND LIMITS AT STRINGER 10L BS 1325. INSTALLED REPAIR IAW 53-30-3, FIGURE 14. 2L73 4F A3WE 19950217002161995021700216NM 1995 2 17 UPS202276 119950210A5320 DOUBLER BOEING727 72727C 138400JNM FS 1183-1203 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FS 1183-1203 BETWEEN STR 9L-10L LIGHT CORROSION BETWEEN INNER DOUBLER AND SKIN. INSTALLED REPAIR IAW SEM 51-30-2. 2L73 4F A3WE 19950217002171995021700217NM 1995 2 17 UPS202277 119950210A5330 SKIN BOEING727 72727C 138400JNM FS 1183-1203 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FUSELAGE UPPER SKIN CORRODED BEYOND LIMITS AT STR 10L FROM FS 1183-1203. INSTALLED REPAIR IAW SRM 53-30-3. 2L73 4F A3WE 19950217002181995021700218NM 1995 2 17 UPS202278 119950210A52109078136 DOOR STOP FITT BOEING727 72727C 138400JNM FS 348 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FS 348 MAIN ENTRY DOOR STOP FITTING IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217002191995021700219NM 1995 2 17 UPS202279 119950210A5320 SHEAR TIES BOEING727 72727C 138400JNM FS 303.9 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FS 303.9 STR 26R/L TO TEE CHORD AFTER FASTENER AND CORROSION REMOVAL, SHEAR TIES CRACKED. INSTALLED REPAIR IAW SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19950217002201995021700220NM 1995 2 17 UPS202280 119950210A5730 SKIN BOEING727 72727C 138400JNM LBL 42 RBL 13 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND WING CENTER SECTION LOWER SKIN AT FRONT SPAR BETWEEN LBL 42 AND RBL 13 CORRODED. INSTALLED REPAIR IAW EO B727-5710-6575A AND DHC 915-561 REV B. 2L73 4F A3WE 19950217002211995021700221NM 1995 2 17 UPS202281 119950210A5730 SKIN BOEING727 72727C 138400JNM FS 825 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER WING BOX UPPER SKIN FS 825, RBL 55-46 COMMON TO STRINGER 9 AFTER EXISTING CORRODED DOUBLER WAS REMOVED, SKIN WAS FOUND TO BE BEYOND LIMITS. INSTALLED REPAIR IAW DHC SK915-577 AND UPS ENGINE. FILE NR 727-57-1071. 2L73 4F A3WE 19950217002221995021700222NM 1995 2 17 UPS202282 119950210A5730 SKIN BOEING727 72727C 138400JNM RBL 45-50 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER WING BOX UPPER SKIN RBL 45-50 BETWEEN STR 4 AND 7 AFTER FASTENER REMOVAL, SKIN WAS FOUND TO BE BEYOND LIMITS. INSTALLED REPAIR IAW DHC SK 915-577 AND ENGINE FILE NR 727-57-1071. 2L73 4F A3WE 19950217002231995021700223NM 1995 2 17 UPS202283 119950210A5320651768856 CHORD BOEING727 72727C 138400JNM FS 320 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FS 320 LBL 208, WL 208 MAIN ENTRY DOOR SILL SUPPORT CHORD SEVERLY CORRODED. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217002241995021700224NM 1995 2 17 UPS202284 119950210A532065317873 ANGLE BOEING727 72727C 138400JNM ENTRY DOOR SILL CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND FWD ENTRY DOOR SILL INBD SUPPORT ANGLE CORRODED. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217002251995021700225NM 1995 2 17 UPS202285 119950210A5730 SKIN BOEING727 72727C 138400JNM BL 0 RBL 24.5 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER WING BOX UPPER SKIN BETWEEN BL 0 AND RBL 24.5 AND STR 18-21 CORRODED. INSTALLED REPAIR IAW DHC SK 915-577 AND ENG FILE NR 727-57-1071. 2L73 4F A3WE 19950217002261995021700226NM 1995 2 17 UPS202286 119950210A5730 SKIN BOEING727 72727C 138400JNM RBL 24.5-45 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER WING BOX UPPER SKIN RBL 24.5 - RBL 45 HAS 5 AREAS OF CORROSION. INSTALLED REPAIR IAW DHC SK 915-577, ENG FILE NR 72 7-57-1071, EO B727-5710-6584A AND DHC SK 915-586. 2L73 4F A3WE 19950217002271995021700227NM 1995 2 17 UPS202287 119950210A5730 SKIN BOEING727 72727C 138400JNM RBL 64 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 DURING 'C' CHECK, MAINTENANCE FOUND CENTER WING BOX UPPER SKIN CORRODED BEYOND LIMITS FORWARD AND AFT OF FRAME 783 RBL 64 BETWEEN STR 15 AND 17. INSTALLED REPAIR IAW DHC 915-577 AND ENG, FILE NR 727-57-1071. 2L73 4F A3WE 19950217002281995021700228NM 1995 2 17 UPS202298 119950213A5230 ANGLE BOEING727 72725C 138400HNM NR 3 CARGO DR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND AFT CARGO DOOR NR 13 O/B L ANGLE CRACKED IN RADIUS AT AFT VERTICAL TIE. REPLACED ANGLE ON AFT VERTICAL TIE PER SRM 51-30-2. 2L73 4F A3WE 19950217002291995021700229NM 1995 2 17 UPS202299 119950213A5313 STRINGER BOEING727 72725C 138400HNM FS 509.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 22L AT BS 509.5, LBL 52. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2, 53-10-3, 53-10-1. 2L73 4F A3WE 19950217002301995021700230NM 1995 2 17 UPS202300 119950213A5313 STRINGER BOEING727 72725C 138400HNM FS 538 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 23, BS 538, LBL 46 OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950217002311995021700231NM 1995 2 17 UPS202301 119950213A5320 CLIP BOEING727 72725C 138400HNM FS 380 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND STRINGER 26L CLIP CRACKED AT BS 380. REPLACED CLIP PER SRM 51-20-4. 2L73 4F A3WE 19950217002321995021700232NM 1995 2 17 UPS202302 119950213A5320 INTERCOSTAL BOEING727 72725C 138400HNM FS 211.8-218.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 211.8-218.8, RBL 25, WL 193. REPLACED INTERCOSTAL PER SRM 51-20-1, 51-20-21, 51-30-2, 53-10-1. 2L73 4F A3WE 19950217002331995021700233NM 1995 2 17 UPS202303 119950213A5320 INTERCOSTAL BOEING727 72725C 138400HNM FS 500 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT BS 500, LBL 52, WL 172. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-30-2, 51-20-1, 53-10-2. 2L73 4F A3WE 19950217002341995021700234NM 1995 2 17 UPS202304 119950213A5313 STRINGER BOEING727 72725C 138400HNM FS 740-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 1 AT STA 740-870, BL 0. REPLACED STRINGER PSR SRM 53-10-3, 53-10-4, 53-10-4. 2L73 4F A3WE 19950217002351995021700235NM 1995 2 17 UPS202305 119950213A5320 CLIP BOEING727 72725C 138400HNM FS 990 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CRACKED STR CLIP AT STA 990, STR 8R, WL 278. REPLACED CLIP PER SRM 51-30-2. 2L73 4F A3WE 19950217002361995021700236NM 1995 2 17 UPS202306 119950213A5320 CLIP BOEING727 72725C 138400HNM FS 970 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CRACKED STR CLIP AT STA 970, STR9R, WL 270. REPLACED CLIP PER SRM 51-30-2. 2L73 4F A3WE 19950217002371995021700237NM 1995 2 17 UPS202307 119950213A5330 SKIN BOEING727 72725C 138400HNM FS 1078/1080 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT STA 1078 AND STRAP STA 1080 ABOVE STR 10R, WL 262. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3. 2L73 4F A3WE 19950217002381995021700238NM 1995 2 17 UPS202308 119950213A5320 CHANNEL BOEING727 72725C 138400HNM FS 1140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL AT STA 1140, LBL 25-65, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1, 51-30-5, 51-30-2. 2L73 4F A3WE 19950217002391995021700239NM 1995 2 17 UPS202309 119950213A5320 ANGLE BOEING727 72725C 138400HNM FS 342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND SCREW HOLES IN L ANGLE ON TOP OF HAT CHANNEL AT STA 342, RBL 25-45, RBL 25-45, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1, 51-20-1, 51-10-2, 51-10-2, 51-10-6, 53-10-1. 2L73 4F A3WE 19950217002401995021700240NM 1995 2 17 UPS202310 119950213A5753 SKIN BOEING727 72725C 138400HNM RT TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND RT WING I/B AFT FLAP I/B 75 INCHES HAS CORROSION ON SKIN. REPAIRED AREA PER SRM 51-40-6. 2L73 4F A3WE 19950217002411995021700241NM 1995 2 17 UPS202311 119950213A5313 STRINGER BOEING727 72725C 138400HNM FS 297 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STR 3L AT STA 297. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-2, 53-10-3. 2L73 4F A3WE 19950217002421995021700242NM 1995 2 17 UPS202312 119950213A5754 LUG BOEING727 72725C 138400HNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP I/B LUG CORRODED. REPLACED NR 6 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19950217002431995021700243NM 1995 2 17 UPS202313 119950213A5311 FRAME BOEING727 72725C 138400HNM FS 804 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CRACK IN STA 804 FRAME CHORD AT STR 13R. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-3, 51-10-2. 2L73 4F A3WE 19950217002441995021700244NM 1995 2 17 UPS202314 119950213A5320 INTERCOSTAL BOEING727 72725C 138400HNM FS 211.8-218.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 211.8-218.8, LBL 25, WL 193. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2. 2L73 4F A3WE 19950217002451995021700245NM 1995 2 17 UPS202315 119950213A5754 FLAP BOEING727 72725C 138400HNM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP O/B LOWER BONDING JUMPER ATTACH POINT. REPLACED K-FLAP PER MM 51-30-8. 2L73 4F A3WE 19950217002461995021700246WP 1995 2 17 UPS802245 119950209A32462601475J WHEEL DOUG DC8 DC873F 302199FWP LT MLG FAILED A IPXAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01813UP 46059 PILOT REPORTED LEFT MAIN GEAR DOOR LIGHT ON AFTER GEAR RETRACTION. RAN CHECKLIST, NO HELP. FLEW AT REDUCED AIRSPEED. NR 1 WHEEL RIM FAILURE. CHANGED NR 1 AND NR 2 TIRE ASSY. CYCLED GEAR DOORS. DOOR LIGHTS CHECKED OK IAW 32-40-01. 2L74 4F RT4A25 19950217002471995021700247WP 1995 2 17 UPS802288 119950213A53203779659501 FITTING DOUG DC8 DC871F 302199DWP FS 902 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LONGERON END FITTING CRACKED AT FS 902, LONG 16L. REPLACED FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950217002481995021700248WP 1995 2 17 UPS802289 119950213A575556551662 SKIN DOUG DC8 DC871F 302199DWP RT NR 2 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND RT WING NR 2 SPOILER DELAMINATED ON UPPER SURFACE. REPLACED SPOILER PANEL PER MM 27-60-01. 2L74 4F RT4A25 19950217002491995021700249WP 1995 2 17 UPS802290 119950213A53132597242 LONGERON DOUG DC8 DC871F 302199DWP FS 75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 32R CRACKED AT FS 75. REPAIRED LONGERON PER SRM 53-2-2. 2L74 4F RT4A25 19950217002501995021700250WP 1995 2 17 UPS802291 119950213A532057550583 FITTING DOUG DC8 DC871F 302199DWP FS 781 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 34L END FITTING CRACKED AT FS 781. REPLACED FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950217002511995021700251WP 1995 2 17 UPS802292 119950213A5330807075T6 SKIN DOUG DC8 DC871F 302199DWP FS 380 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND SKIN CRACKED AT FASTENER HOLE AT FS 380, BETWEEN LONGERONS 30L-29R. REPAIRED SKIN PER SRM 53-2-1. 2L74 4F RT4A25 19950217002521995021700252WP 1995 2 17 UPS802294 119950213A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 32 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND RT AND LT HEAT EXCHANGER DOUBLER CUT OUT CRACKED ON AFT CORNER AT FS -32. REPAIRED PER UPS EO DC8-5330-4732. 2L74 4F RT4A25 19950217002531995021700253WP 1995 2 17 UPS802295 119950213A57125770123 RIBS DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LEFT WING LEADING EDGE RIBS CRACKED AT STATIONS XFS 313, 369, 622, 672, 790, 796 UPPER, AND XFS 790 LOWER. REPAIRED RIBS PER MM 57-00-00. 2L74 4F RT4A25 19950217002541995021700254WP 1995 2 17 UPS802296 119950213A55115770123 RIB DOUG DC8 DC871F 302199DWP LT HORIZ STAB LECRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LEFT HORIZONTAL STAB I/B LEADING EDGE RIBS CRACKED, 1ST, 2ND, AND 3RD RIBS FROM INBOARD END. REPAIRED RIBS PER SRM 55-2-0. 2L74 4F RT4A25 19950217002551995021700255WP 1995 2 17 UPS802297 119950213A531397549332 LONGERON DOUG DC8 DC871F 302199DWP FS 190 LON 35L CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE FOUND LONGERON 35L HAS 3 CRACKS AT O/B ENDS BETWEEN STA 190-390. REPLACED LONGERON PER SRM 51-1-20. 2L74 4F RT4A25 19950217002571995021700257WP 1995 2 17 9502069984 119950131A5230 FITTING DOUG DC9 DC932 3022066WP FWD CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO DOOR NR 5 BEAM END FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950217002581995021700258WP 1995 2 17 9502079984 119950131A5313 LONGERON DOUG DC9 DC932 3022066WP FS 522 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 29L AT FS 522. REPLACED LONGERON PER EA 99-096876. 2L72 4F A6WE 19950217002591995021700259WP 1995 2 17 9502089981 119950201A5312 BLKHD WEB DOUG DC9 DC931 3022065WP LT LAVATORY OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01994Z 47097 DURING PERIODIC CHECK, FOUND OIL CANNING IN THE LEFT LAVATORY BULKHEAD WEB AT THE INBOARD LIGHTENING HOLE. REPAIRED PER EA 99-096894. 2L72 4F A6WE 19950217002601995021700260WP 1995 2 17 9502099863 119950201A5743 FITTING DOUG DC9 DC951 3022051WP LT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01772NC 47774 DURING PERIODIC CHECK, FOUND CORROSION ON LEFT MAIN LANDING GEAR SIDE BRACE ATTACH FITTING LUG. REPAIRED PER EA 98-094923. 2L72 4F A6WE 19950217002611995021700261WP 1995 2 17 9502109984 119950201A5320 FITTING DOUG DC9 DC932 3022066WP CARGO DOOR JAMB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING PERIODIC CHECK, FOUND CORROSION IN AFT CARGO DOOR JAMB LOWER VERTICAL ATTACH FITTING, FS 945. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950217002621995021700262WP 1995 2 17 9502119945 119950202A57535919217501 HINGE DOUG DC9 DC931 3022065WP WS 251 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 49980 45840 DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE MOUNTING HOLES, WS 251. REPLACED HINGE FITTING PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950217002631995021700263WP 1995 2 17 9502129756 119950202A5210 FRAME DOUG DC9 DC941 302207NWP MAIN CABIN DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CRACK IN MAIN CABIN DOOR NR 7 BEAM AFT END IN THE RADIUS. REPLACED END FITTING AND REPAIRED THE BEAM PER SRM 52-05, FIG.31. 2L72 4F A6WE 19950217002641995021700264WP 1995 2 17 9502139756 119950202A5220 FRAME DOUG DC9 DC941 302207NWP EMER EXIT DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT FORWARD EMERGENCY EXIT DOOR PAN AT THE NR 14 STOP FITTING. REPAIRED PAN PER EA 97-093728. 2L72 4F A6WE 19950217002651995021700265WP 1995 2 17 9502149756 119950203A5415 FITTING DOUG DC9 DC941 302207NWP RT PYLON RUSTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND RUST ON THE UPPER SURFACE OF THE UPPER 'BEAVER TAIL' FITTING AND THE LOWER SURFACE OF THE LOWER 'BEAVER TAIL' FITTING RIGHT PYLON FORWARD SPAR. REPLACED BOTH FITTINGS PER DWG 9958161. 2L72 4F A6WE 19950217002661995021700266WP 1995 2 17 9502159951 119950204A5330 SKIN DOUG DC9 DC932 3022066WP FS 1002 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019347 45827 DURING PERIODIC CHECK, FOUND OIL CANNING IN FUSELAGE SKIN BETWEEN LOWER LEFT PYLON ATTACH ANGLE AND LONGERON 17L AT FS 1002 AND BETWEEN LONGERONS 17L - 18L AT FS 1015. REPAIRED BOTH PER EA 99-096893. 2L72 4F A6WE 19950217002671995021700267WP 1995 2 17 9502169988 119950205A5330 SKIN DOUG DC9 DC931 3022065WP FS 897-917 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON INNER FUSELAGE SKIN FS 897 - 917 BETWEEN LONGERONS 22L - 23L. REPAIRED PER XEA X9-53-57. 2L72 4F A6WE 19950217002681995021700268WP 1995 2 17 9502179988 119950206A5313 LONGERON DOUG DC9 DC931 3022065WP FS 229 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 18L LOWER SPLICE FITTING AT FS 229. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950217002691995021700269WP 1995 2 17 9502189992 119950206A5320 FITTING DOUG DC9 DC931 3022065WP FS 639 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FS 639 FRAME FITTING 'DINOSAUR RIB', LEFT SIDE JUST ABOVE CENTER TANK. REPAIRED PER EA 99-093477. 2L72 4F A6WE 19950217002701995021700270WP 1995 2 17 9502199992 119950206A5320 FRAME DOUG DC9 DC931 3022065WP FS 884-903 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND PIT MARKS IN THE RIGHT SIDE WINDOW CUTOUTS AT FS 884 AND FS 903. REPAIRED PER EA 99-95751. 2L72 4F A6WE 19950217002711995021700271WP 1995 2 17 9502209756 119950206A5415 FITTING DOUG DC9 DC941 302207NWP PYLON RUSTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND RUST ON THE LOWER SURFACE OF THE LOWER 'BEAVER TAIL' FITTING AND UPPER AND LOWER SURFACES OF THE UPPER 'BEAVER TAIL' FITTING. REPLACED BOTH FITTINGS PER SRM 51-01. 2L72 4F A6WE 19950217002721995021700272WP 1995 2 17 9502219951 119950207A5313 LONGERON DOUG DC9 DC932 3022066WP FS 389-435 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019347 45827 DURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 17R AT FS 389 AND FS 408 AND IN LONGERON 17L AT FS 435. REPAIRED ALL THREE LOCATIONS PER EA 99-096899. 2L72 4F A6WE 19950217002731995021700273WP 1995 2 17 9502229138 119950207A57535912596502 STUDS DOUG DC9 DC915 3022036WP NR 4 FLAP HINGE BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL019348 59857 45787 DURING LINE CHECK, FOUND BROKEN ATTACH STUDS AT THE RIGHT WING NR 4 FLAP HINGE. REPLACED 4 STUDS AND THE HINGE PER CITEXT 09-5740-1-0004. 2L72 4F A6WE 19950217002741995021700274WP 1995 2 17 9502239756 119950207A5320 FRAME DOUG DC9 DC941 302207NWP WINDOW CUTOUT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CORROSION ON WINDOW CUTOUT 25L. REPAIRED PER EA 97-72509. 2L72 4F A6WE 19950217002751995021700275WP 1995 2 17 9502249945 119950208A5753 STUDS DOUG DC9 DC931 3022065WP NR 2 FLAP HINGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CORROSION ON NR 2 FLAP HINGE ATTACH STUDS. REPAIRED PER XEA X9-27-9. 2L72 4F A6WE 19950217002761995021700276WP 1995 2 17 9502259756 119950208A5312 FITTING DOUG DC9 DC941 302207NWP AFT PRESS BLKHD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD VAULT DOOR UPPER RIGHT STOP FITTING AND SILL. ALSO, FOUND A CRACK IN THE SILL AT THE UPPER LEFT DOOR STOP FITTING. REPLACED THE STOP FITTING AND REPAIRED THE SILL CRACKS PER SRM 53-05, FIG.30 A. 2L72 4F A6WE 19950217002771995021700277WP 1995 2 17 9502269951 119950209A5330 SKIN DOUG DC9 DC932 3022066WP FS 1056-1080 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019347 45827 DURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1056 - 1080 BETWEEN LONGERONS 17R - 18R. REPAIRED PER EA 99-096893. 2L72 4F A6WE 19950217002781995021700278NM 1995 2 17 9502276308 119950208A5347 SEAT TRACK BOEING747 747451 1384940NM FS 1622-1656 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01668US 24223 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1622 - 1656, RBL 75.92R - 78R. REPAIRED PER EA 63-96585, SEC.1. 2L74 4F RTA20WE 19950217002791995021700279NM 1995 2 17 9502286308 119950208A5320 BEAM BOEING747 747451 1384940NM FS 1702-1733 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01668US 24223 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FLOOR BOARD SUPPORT BEAM AT FS 1702 - 1733, RBL 42. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 63-96584. 2L74 4F RTA20WE 19950217002801995021700280NE 1995 2 17 9502296614 219950212A7230 COMPRESSOR BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 3 ENGINE STALLED A NWAADEF RETURN TO BLOCK ENGINE SHUTDOWN ACTIVATE FIRE EXT. BJMSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OVER TEMP TXTAXI/GRND HDL 1 GL01614US 20359 662502 DURING TAXIOUT (AMS), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH HIGH EGT, LOSS OF OIL PRESSURE, AND SMOKE WAS REPORTED COMING FROM THE TAILPIPE. THE FIRE HANDLE WAS PULLED AND THE BOTTLES WERE DISCHARGED. A BOROSCOPE AND INSPECTION OF THE ENGINE CHECKED OK. THE FIRE BOTTLES WERE REPLACED AND A FULL POWER RUN-UP CONFIRMED PROPER ENGINE OPERATION. THE ENGINE IS SCHEDULED FOR REPLACEMENT. 2L74 4F4 F A20WE E20EA 19950217002811995021700281 1995 2 17 9502306719 419950211A34417883450041A COMPUTER BOEING747 747251F 1384898NM E/E BAY MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01619US 21321 EN ROUTE NRT-TPE, THE NR 2 AND NR 3 INS EXPERIENCED OVERHEAT PROBLEMS. THE INS RED WARNING LIGHT WOULD NOT CLEAR. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND RETURNED TO NRT. REPLACED THE NR 2 AND NR 3 INS COMPUTERS. PERFORMED CHECK AND UNITS TESTED NORMAL. 2L74 4F A20WE 19950217002821995021700282NM 1995 2 17 9502312292 119950210A2910 HYD FLUID BOEING727 727251 138408HNM A HYD SYST LOW QTY A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01292US 21503 DURING CRUISE, 'A' SYSTEM HYDRAULIC QUANTITY LOW. DURING FLAP EXTENSION QUANTITY DECREASED TO 2.0 GALLONS, UPON GEAR EXTENSION QUANTITY RETURNED TO NORMAL. CLOSED 'A' SYSTEM HYDRAULIC FLUID SHUTOFF VALVES AND CALLED OUT EMERGENCY EQUIPMENT AS A PRECAUTION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED 'A' HYDRAULIC SYSTEM AND INSPECTED FOR LEAKS. NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950217002831995021700283 1995 2 17 95FDEA00135 219950210A7200 ENGINE BOEING727 727227 1384078NM NR 2 FAILED A FDEAAE UNSCHED LANDING ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CLCLIMB 1 SO04495FE 21669 CGN - ENG NR 2 FAILED JUST AFTER LIFT OFF CGN; FLAPS 15 DEG A/C VIBRATION, WITH NR 2 ENG N1, N2 DROPPING, FUEL FLOW DROPPING, OIL QTY AND PRESS NORMAL. ENG SHUTDOWN WITH APPROPRIATE CHECKLIST ACCOMPLISHED. 2L73 4F A3WE 19950217002841995021700284SO 1995 2 17 COM11777 119950212A32402025000002 SWIVEL EMB 120 EMB120RT SO LT MLG BRAKE LEAKING A COMAK NONE KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 SO01255CA 120238 HYDRAULIC LEAK, LEFT MLG. REPLACED LEAKING BRAKE LINE SWIVEL. 2L72 4T RTA31SO 19950217002851995021700285SO 1995 2 17 COM11778 119950210A7603584502 CONTROL CABLE EMB 120 EMB120RT 3260202SO RT ENGINE BINDING A COMAK NONE O OTHER ININSP/MAINT 1 SO01261CA 120254 RT POWER LEVER IS BINDING. REPLACED TELEFLEX CABLE ASSY. 2L72 4T RTA31SO 19950217002861995021700286SO 1995 2 17 COM11779 119950211A3260922FS2A6NZ735 SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01244CA 120217 LANDING GEAR CONTROL COULD NOT BE SELECTED TO UP UNTIL OVERRIDE RELEASE WAS USED. REPLACED THE LEFT MLG WEIGHT ON WHEELS PROXIMITY SENSOR. 2L72 4T RTA31SO 19950217002871995021700287SO 1995 2 17 COM11780 119950211A3260 UNSAFE IND EMB 120 EMB120RT SO NLG ACTIVATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01200CD 120200 NLG INDICATED UNSAFE AFTER LANDING GEAR RETRACTED. COULD NOT DUPLICATE NLG DISCREPANCY. 2L72 4T RTA31SO 19950217002881995021700288SO 1995 2 17 COM11781 119950212A32331959510006 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01200CD2 2 120200 AFTER LANDING GEAR RETRACITON, NLG AND LEFT MLG INTRANSIT LIGHTS REMAINED ON. ADJSUTED LEFT MLG RETRACT ACTUATOR AND ADJUSTED NLG PROXIMITY SENSORS. 2L72 4T RTA31SO 19950217002891995021700289SO 1995 2 17 COM11782 119950212A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01200CD11065 120200 LEFT MLG INTRANSIT LIGHTS REMAINED ON AFTER RETRACTION. REPLACED THE LEFT MLG RETRACT ACTUATOR. 2L72 4T RTA31SO 19950217002901995021700290SO 1995 2 17 COM11783 119950212A32302025000002 SWIVEL EMB 120 EMB120RT SO LT MLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01255CA 120238 HYDRAULIC LEAK, LEFT MLG. TIGHTENED FITTINGS ON HYDRAULIC SWIVEL. 2L72 4T RTA31SO 19950217002911995021700291 1995 2 17 COM31033 419950210A61228210153 PCU SAAB SF340 SF340A 7850100EU RT PROP DEFECTIVE A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01347CA8242 613 340A028 RT PROPELLER RPM IS LAGGING AT LOW POWER SETTINGS. REPLACED THE PROPELLER PITCH CONTROL UNIT. 2L72 4T RTA52EU 19950217002921995021700292EA 1995 2 17 COM60413 119950213A78301217542 FLEX SHAFT CNDAIRCL600 CL6002B19 EA RT ENGINE SEPARATING A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA2842 7031 RT ENGINE THRUST REVERSER FLEX SHAFT AT 9 O'CLOCK POSITION IS SEPARATING. C-CHECK INSPECTION TASK NR 12-440-100. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950217002931995021700293EA 1995 2 17 COM60414 119950213A78301217542 FLEX SHAFT CNDAIRCL600 CL6002B19 EA LT ENGINE SEPERATED A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA2842 7031 LEFT ENGINE THRUST REVERSER FLEX SHAFT AT 9 O'CLOCK POSITION IS SEPERATING. C-CHECKED INSPECTION TASK NR 12-430-100. REPLACED FLEX SHAFT. 2L72 4F RTA21EA 19950217002941995021700294EA 1995 2 17 COM60415 119950213A552060010300 BUSHINGS CNDAIRCL600 CL6002B19 EA LT ELEVATOR WORN A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA2842 7031 LEFT SYSTEM NR 3 ELEVATOR PCU FAILS THE BACKLASH TEST. C-CHECK INSPECTION TASK NR 002-27-900-106. REPLACED WORN BUSHINGS AT ELEVATOR ATTACH POINT. 2L72 4F RTA21EA 19950217002951995021700295EA 1995 2 17 COM60416 119950213A5520NAS6705DU16 BOLTS CNDAIRCL600 CL6002B19 EA LT ELEVATOR LOOSE A COMAK NONE O OTHER ININSP/MAINT 1 SO01927CA2842 7031 LEFT SYSTEM NR 1 AND 2 ELEVATOR PCU FAILS BEARING BACKLASH TEST. C-CHECK INSPECTION TASK 002-27-900-106. BOLTS AT PCU TO ELEVATOR ATTACH POINT FOUND LOOSE. TORQUED VOLTS TO PROPER VALVE AND BACKLASH CHECK SATISFACTORY. 2L72 4F RTA21EA 19950217002961995021700296EA 1995 2 17 COM60417 119950212A2820B9738663 VALVE CNDAIRCL600 CL6002B19 EA WING CENTER DEFECTIVE A COMAK NONE S AFFECT SYSTEMS UKUNKNOWN 1 SO01938CA996 7046 GRAVITY FUEL CROSS FLOW VALVE IS INOP. REPLACED CROSS FLOW VALVE. 2L72 4F RTA21EA 19950217002971995021700297EU 1995 2 17 DL31L950602 119950209A2133 OUTFLOW VALVE AIRBUS310 A310324 3930206EU CABIN INOP A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11835AB 650 AFTER TAKEOFF, FORWARD OUTFLOW VALVE FAILED IN FULL OPEN POSITION. CABIN ALTITUDE FOLLOWED, UNABLE TO PRESSURIZE, RETURNED CVG. RESEATED C/P ON OUTFLOW VALVE, CLEANED VALVE, PERFORMED BITE ON CONTROLLER, OPERATED SEVERAL TIMES, ALL NORMAL, RETURNED TO SERVICE. 2L72 4F RTA35EU 19950217002981995021700298NM 1995 2 17 DL72E950529 119950207A5320 ANGLE 651751738 BOEING727 727247 138408FNM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 THERE IS A 1 INCH CRACK IN THE ANGLE OF THE FORWARD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER S/B 53-0129. DAMAGE FOUND AT LETTER CHECK. 2L73 4F A3WE 19950217002991995021700299NM 1995 2 17 DL72L950605 119950211A3020320115 ANTI-ICE VALVE BOEING727 727232 1384082NM NR 3 ENGINE LEAKING A DALAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO11510DA 21312 DURING CLIMB, HAD NR 3 STRUT OVERHEAT LIGHT ON, LIGHT WENT OUT WITH REDUCTION OF POWER. RETURNED ATL. REPLACED NR 3 ENGINE ANTI-ICE VALVE AND UPPER ANTI-ICE DUCT ASSEMBLY AT VALVE, LEAK CHECK OK. 2L73 4F A3WE 19950217003001995021700300NM 1995 2 17 DL72S950512 119950131A5730 SKIN BOEING727 727232 1384082NM LT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 HOLE IN LOWER SKIN PANEL 9 IN FROM O/B END OF LT AILERON. ITEM FOUND DURING INSPECTION AT HMV2 IN ATL. ITEM REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950217003011995021700301NM 1995 2 17 DL72S950519 119950206A575465162221 RIB BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11475DA 20752 DURING SHOP INSPECTION, FOUND LEFT WING NR 3 SLAT WITH THE LOWER CHORD DAMAGED OUBOARD OF THE INBOARD UP STOP FITTING AND RIB NR 10 CRACKED AT ITS LOWER END, OUTBOARD OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950217003021995021700302NM 1995 2 17 DL72S950526 119950119A57536521631325K FOREFLAP BOEING727 727232 1384082NM NR 1 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 DURING SHOP INSP NR 1 FORE FLAP WAS FOUND WITH WEAR DAMAGE AT 108 INCHES FROM THE INBOARD END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950217003031995021700303NM 1995 2 17 DL72S950534 119950207A5320 WEB BOEING727 727232 1384082NM FS 1276 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11420DA 21273 DURING LETTER CHECK, FOUND A .4375 INCH LONG CRACK IN VERTICAL WEB AFT STAIRWELL AREA LEFT SIDE FS 1276. REPAIRED PER SRM 53-11-0 PG 832. 2L73 4F A3WE 19950217003041995021700304NM 1995 2 17 DL72S950535 119950207A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11420DA 21273 FOUND ON LTR CK, .4375 INCH BY .25 INCH SECTION OF FUSELAGE SKIN ROUTED OUT AT AFT CORNER OF ACCESS PLATE 3903. REPAIRED PER M/M 53-30-0 PG 804. 2L73 4F A3WE 19950217003051995021700305NM 1995 2 17 DL72S950550 119950202A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FS 1070 CABIN FLOOR SUPPORT BEAM UPPER CAP CORRODED, OUTBOARD OF RT OUTBOARD SEAT TRACK. REPAIRED PER MM 53-20-11 FIG 804 A. 2L73 4F A3WE 19950217003061995021700306NM 1995 2 17 DL72S950551 119950202A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FS 400 CABIN FLOOR BEAM UPPER CAP WITH CORROSION DAMAGE ALONG ITS LENGTH. REPAIRED PER SRM 53-10-8 FIG 3 AT RBL 10 TO LBL 10 AND SRM 53-20-11. 2L73 4F A3WE 19950217003071995021700307NM 1995 2 17 DL72S950552 119950207A5330 SKIN BOEING727 727232 1384082NM FS 380 SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING INSPECTION, FOUND OUTER FUSELAGE SKIN SCRATCHED BEYOND LIMITS AFT OF FORWARD ENTRY DOOR JUST BELOW FLOOR LINE AT FS 380. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950217003081995021700308NM 1995 2 17 DL72S950585 119950201A5712 RIB BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND RIB CRACKED ON O/B SIDE OF NR 6 L/E SLAT TAI DUCT AND A RIB CRACKED NEXT RIB O/B OF ITEM NR 1, REPAIRED BYSTOP DRILLING CRACK AND FABRICATING REPAIR DOUBLER PER SRM 57-50-3 PG 25, INSTALLED REPAIR PER SRM 57-50-3 PG 25. 2L73 4F A3WE 19950217003091995021700309NE 1995 2 17 DL72S950607 219950209A7200JT8D15A ENGINE BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 3 FLAMED OUT A DALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO11532DA57339 22045 687530 DURING DESCENT, NR 3 ENGINE FLAMED OUT UPON RETARD OF THROTTLES AT FL370. FUEL HEAT AND IGNITION ON AT THE TIME. HAD SUCCESSFUL AIR RESTART. INSPECTED AND REPLACED FUEL AND OIL FILTERS FOUND OK, RAN ENGINE PER PFHB, NO PROBLEMS FOUND, RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950217003101995021700310NM 1995 2 17 DL72W950527 119950207A5753651622296 SKIN BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 DURING SHOP INSPECTION RIGHT WING NR 6 SLAT WAS FOUND WITH A CRACK IN THE LOWER SKIN AT 19 INCH FROM THE INBOARD END OF SLAT AND 13 INCH FROM THE OUTBOARD END OF SLAT. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950217003111995021700311NM 1995 2 17 DL72W950539 119950125A5315 FLOOR BEAM BOEING727 727247 138408FNM FS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND FLOOR BEAM CORRODED AT STA 1070 RT SIDE. REPAIRED PER SRM 53-10-8 PG 2A. 2L73 4F A3WE 19950217003121995021700312NM 1995 2 17 DL72W950541 119950125A5313 LONGERON BOEING727 727247 138408FNM FS 580 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND STR 28R CORRODED AT STA 580-600. REPAIRED PER SRM 53-10-3 PG 4. 2L73 4F A3WE 19950217003131995021700313NM 1995 2 17 DL72W950543 119950125A5313 LONGERON BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND SPLICE CORRODED ON STR 28R AND STR 30 AT STA 1010. REPAIRED PER SRM 53-10-11 FIG 3. 2L73 4F A3WE 19950217003141995021700314NM 1995 2 17 DL72W950544 119950124A5320 CLIP BOEING727 727247 138408FNM FS 1148 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND SKIN CLIP CORRODED AT STA 1148 STR 29R-30. REPAIRED PER M/M 53-11-0 PG 8. 2L73 4F A3WE 19950217003151995021700315NM 1995 2 17 DL72W950545 119950124A5320 CLIP BOEING727 727247 138408FNM FS 1148 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, FOUND SKIN CLIP CORRODED STA 1148 STR 30. REPAIRED PER M/M 53-10-0 PG 825. 2L73 4F A3WE 19950217003161995021700316NM 1995 2 17 DL72W950564 119950124A5312 SUPPORT BOEING727 727247 138408FNM FS 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, CORROSION ON TOP HORIZ SUPPORT STA 1166 BULKHEAD AT CENTER CEILING SUPPORT STRAP. REPAIRED PER SRM 51-40-4 FIG 3. 2L73 4F A3WE 19950217003171995021700317NM 1995 2 17 DL72W950565 119950125A5320 INTERCOSTAL BOEING727 727247 138408FNM FS 600 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING HMV, INTERCOSTAL STA 600 CORRODED. REPAIRED PER SRM 51-10-4. 2L73 4F A3WE 19950217003181995021700318NM 1995 2 17 DL757950581 119950206A5315 FLOOR BEAM BOEING757 757232 1384965NM FS 365 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11667DN 25035 DURING HMV CABIN FLOOR BEAM UPPER CAP WAS FOUND TO BE CORRODED AT STA 365 BETWEEN RBL29 AND RBL47. REPAIRED PER SRM 53-00-51 PG 201. 2L72 4F RTA2NM 19950217003191995021700319NM 1995 2 17 DL76L950549 119950108A5542173T200123 SKIN BOEING767 767332 1382001NM RUDDER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11171DN 24759 INITIAL SHOP INSP OF 767 RUDDER FOUND 1 AREA OF DAMAGE CONSISTING OF A CRACK AND DELAMINATION, DAMAGE WAS LIMITED TO EXT SKIN PANEL ONLY. DAMAGE LOCATION WAS ON LOWER LEFT SIDE OF SKIN PANEL APPROX 9 FEET FROM THE BOTTEM OF THE RUDDER APPROX SIZE OF DAMAGE WAS 12 INCHES BY 8 INCHES THIS DAMAGE WAS REPAIRED IN ACCORDANCED WITH SRM 55-40-01. 2L72 4F RTA1NM 19950217003201995021700320NM 1995 2 17 DL76L950553 119950204A5753 WEDGE BOEING767 767332 1382001NM RT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11172DN 24775 DURING HMV, FOUND RIGHT WING OUTBOARD FLAP TRAILING EDGE WEDGE WITH DELAMINATION AT 2 FEET OUTBOARD OF THE INB FLAP TRACK. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950217003211995021700321NM 1995 2 17 DL76S950546 119950207A5751 AILERON BOEING767 767332 1382001NM LT WING LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11137DL 25306 DURING LETTER CHECK INSP, FOUND L/WING ODBD AILERON EVIDENCE OF LIGHTNING STRIKE INSTALLED PERMANENT REPAIR AS PER SRM 57-60-02 FIG 201, BALANCE NOT CHANGED REF 51-60-01, PAINTED REPAIR ON LEFT AILERON. 2L72 4F RTA1NM 19950217003221995021700322NM 1995 2 17 DL76S950547 119950207A5330 SKIN BOEING767 767332 1382001NM FWD FUS LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11137DL 25306 FOUND DURING LETTER CHECK INSP, LIGHTNING STRIKE FOREWARD OF RIGHT LOWER PITOT TUBE ON FUSE SKIN BLENDED DAMAGE PER SRM 53-00-01 DYE CHK OK, TREATED AREA AND REPAINTED. 2L72 4F RTA1NM 19950217003231995021700323NM 1995 2 17 DL76S950548 119950207A5330 SKIN BOEING767 767332 1382001NM FWD FUS LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11137DL 25306 DURING LETTER CHECK INSP, FOUND 10 LIGHTNING STRIKES ON A/C BELLY (STARTING JUST AFT OF NOSE GEAR TO SECOND BODY DRAIN AFT OF E AND E COMPT AT 6 O'CLOCK POS) FUSELAGE SKIN BLENDED DAMAGE PER SRM 53-00-01, DYE CHECK OK. TREATED AREAS W/ALODINE. 2L72 4F RTA1NM 19950217003241995021700324WP 1995 2 17 DLL10950531 119950207A2120 AIR DISTR LKHEED1011 10113851 5265010WP CABIN ODOR A DALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DEDESCENT 1 SO111732D 193C1213 ALL AFT SMOKE DETECTORS SOUNDED WITH HAZE IN CABIN OF AIRCRAFT. HAZE APPEARED AFTER THROTTLES PULLED TO IDLE AT TOP OF DESCENT. IRRITATING FUMES IN AFT. CHECKED OPERATION OF ALL PACKS, COULD NOT DUPLICATED, RETURNED TO SERVICE. 2L73 4F A23WE 19950217003251995021700325WP 1995 2 17 DLL17950604 119950210A242051511003 GEN CONTL UNIT LKHEED1011 10113853 5265020WP MID E/E COMP LIGHTNING DAMAGEA DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO11766DA 193H1207 DURING CLIMB-OUT LIGHTNING STRUCK AIRCRAFT, HAD NR 3 DIFFERENTIAL FAULT ON GENERATOR WITH ACCOMPANING LOSS OF NR 3 FLIGHT STATION BUS. RETURNED ATL, REPLACED NR 3 GENERATOR CONTROL UNIT, OPERATION NORMAL. 2L73 4F A23WE 19950217003261995021700326NM 1995 2 17 DLM88950563 119950208A5230 DOOR DOUG MD88 MD88 3023688NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11945DL 49818 FOUND DURING LETTER CHECK, AFT CARGO DOOR HANDLE CUTOUT CRACKED REPAIRED DOOR HANDLE PER SRM 52-05. 2L72 4F RTA6WE 19950217003271995021700327NM 1995 2 17 DLM88950579 119950210A2120 AIR DISTR DOUG MD88 MD88 3023688NM CABIN ODOR A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11911DL 49542 ON TAKEOFF AND APP HAD SMOKE/FUMES IN CABIN. RAN PACKS, ENGINES AND APU COULD NOT DUPLICATE, PERFORMED DUCT BURNOUT, RETURNED TO SERVICE. 2L72 4F RTA6WE 19950217003281995021700328 1995 2 17 DLM88950603 419950209A34254608000307 AHRS DOUG MD88 MD88 3023688NM NR 1 INOP A DALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO11963DL 49982 ON TAKEOFF ROLL AT 100 KNOTS, BOTH AHRS FAILED. FAILURE OCCURRED AFTER HITTING A BUMP ON RUNWAY. ABORTED TAKEOFF. REPLACED NR 1 AHRS AND RESEATED NR 1 AHRS. CHECKED SECURITY OF CADC, SYMBOL GENERATOR AND DFGC NR 1 AND NR 2, OPERATION NORMAL. 2L72 4F RTA6WE 19950217003291995021700329NM 1995 2 17 DLM88950606 119950210A2170 COALESCER BAG DOUG MD88 MD88 3023688NM CABIN DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11913DL 49544 AFTER TAKEOFF, HAD STRONG ODOR OF SMOKE FILL THE CABIN AND FLIGHT DECK, THIS OCCURRED AFTER FULL POWER APPLICATION, AFTER WIND SHEAR ALERT. RETURNED ATL. RAN ENGINES AT T/O POWER, NO SMOKE OR ODOR NOTED. PERFORMED DUCT BURNOUT, AND CHANGED WATER SEPARATOR BAGS. 2L72 4F RTA6WE 19950217003301995021700330NE 1995 2 17 DLM88950608 219950130A7310JT8D219 BRACKET DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED A DALAK NONE O OTHER LDLANDING 1 SO11910DL15355 49541 718216 ON LANDING HAD EXCESSIVE SMOKE COMING FROM NR 2 ENGINE. AIRCRAFT WAS EVACUATED. FOUND FUEL LEAK AT NOZZLE AREA OF ENGINE, ENGINE WAS REPLACED AND ROUTED TO SHOP FOR INVESTIGATION. UPON SHOP DISASSEMBLY OF ENGINE IT WAS FOUND THAT BRACKETPART NR 773243 HAD BROKEN AND A PIECE OF THE BRACKET HAD WEDGED BETWEEN THE FUEL MANIFOLD P/N 806266 AND CHAFED A HOLE IN THE MANIFOLD CAUSING THE FUEL LEAK. 2L72 4F4 FRTA6WE E9NE 19950217003311995021700331WP 1995 2 17 UPS802357 119950209A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1220-1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 DURING 'B' CHECK, MAINTENANCE FOUND FUSELAGE SKIN BULGED AND PULLING RIVET 6 O'CLOCK POSITION BETWEEN 1ST AND 2ND CIRCUMFERENTIAL AFT OF NR 3 PIT DOOR STATION 1220-1240. FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330-6670A. 2L74 4F RT4A25 19950217003321995021700332WP 1995 2 17 UPS802358 119950210A5312 WEB DOUG DC8 DC873F 302199FWP PRESS BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 DURING 'B' CHECK, MAINTENANCE FOUND 3.5 INCH CRACK IN LOWER LEG OF J3 WEB OF AIRPLANE AFT PRESSURE BULKHEAD COMPARTMENT 60. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR. 2L74 4F RT4A25 19950217003331995021700333NM 1995 2 17 95FDEA00136 119950210A5320 SHEAR TIE BOEING727 727233 138408ANM BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 CORROSION ON SHEAR TIE IN AFT BAY ON AFT SIDE OF FRAME BS 1166, LBL 1-4, WL 152. CORRODED SHEAR TIE FOUND TO BE OUT OF LIMITS. REMOVED OLD SHEAR TIE, FABRICATED INSTALLED NEW SHEAR TIE. 2L73 4F RTA3WE 19950217003341995021700334NM 1995 2 17 95FDEA00137 119950210A57207075T6 AUX SPAR BOEING727 727233 138408ANM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 LEFT WING AUXILIARY SPAR LOWER CHORD CRACKED AT INBD FWD (FWD OF NR 7 SPOILER FITTING). CUTOUT CRACKED LW-AUX-SPAR LWR CHORD. FABRICATED NEW CHORD AND REPAIR ANGLES AND INSTALLED PER FEDEX EA 75810-23728. 2L73 4F RTA3WE 19950217003351995021700335NM 1995 2 17 95FDEA00138 119950211A5311 FRAME BOEING727 72725 1384006NM BS 500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FOUND CORROSION UNDER NUTPLATE ON FRAME STA 500 LBL 53 WL 175. CUT OUT DAMAGED AREA ON FRAME BS 500 LBL 53 WL 175 AREA OF 1 INCH BY .75 INCH FABRICATED FILLER-DOUBLER AND INSTALLED PER SRM 51-40-3. 2L73 4F A3WE 19950217003361995021700336NM 1995 2 17 95FDEA00139 119950210A53117075T6050 FRAME BOEING727 72725 1384006NM FS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FOUND CORROSION UNDERNEATH NUTPLATE ON FRAME STA 560 LBL 48 WL 170. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F A3WE 19950217003371995021700337NM 1995 2 17 95FDEA00140 119950211A5320651627910 BEAM BOEING727 72725 1384006NM BS 758 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CRACK FOUND ON LONGITUDINAL BEAM AT BS 758 RBL 45 WL 208. REMOVED AND REPLACED LONGITUDINAL BEAM AT STA 758 RBL 45 WL 208. 2L73 4F A3WE 19950217003381995021700338NM 1995 2 17 95FDEA00141 119950210A5751651926012 HINGE FITTING BOEING727 72725 1384006NM RT AILERON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 RIGHT O/B AILERON 2ND HINGE FITTING FROM I/B END HAS CORROSION. REMOVED AND REPLACED NEW AILERON HINGE FITTING. 2L73 4F A3WE 19950217003391995021700339NM 1995 2 17 95FDEA00142 119950212A53117075T6 FRAME BOEING727 72725 1384006NM FS 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 WHILE ACCESSING FOR FUSELAGE 00124, FOUND FRAME CRACKED AT STA 500 RBL 24 WL 158. CUT OUT DAMAGE FRAME AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. 2L73 4F A3WE 19950217003401995021700340NM 1995 2 17 DL72S950556 119950208A5320 SKIN CLIP BOEING727 727232 1384082NM FS 1090 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 DURRING LETTER CHECK, FOUND FS 1090 FRAME TO SKIN SHEAR TIE CORRODED ON ITS FWD SIDE AT STRINGERS 29R AND 28R. REPAIRED PER M/M 53-11-0 FIG 815. 2L73 4F A3WE 19950217003411995021700341NM 1995 2 17 DL72S950557 119950208A5320 BLKHD BEAM BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 DURING LETTER CHECK, FOUND FS 1183 BULKHEAD VERTICAL BEAM AT RBL 8 WITH A 1 INCH CRACK. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950217003421995021700342NM 1995 2 17 DL72S950566 119950130A5753652163586A LE SKIN BOEING727 727232 1384082NM NR 4 TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV SHOP INSPECTION, THE RIGHT WING NR 4 AFT FLAP LEADING EDGE SKIN WAS FOUND DENTED AT 64 INCHES FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950217003431995021700343NM 1995 2 17 DL72S950572 119950201A5311 FRAME BOEING727 727232 1384082NM FS 312 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 FUSELAGE FRAME CRACKED AT TWO FASTENER HOLES STA 312 AT STR 13R. FABRICATED REPAIR ANGLES PER SRM 53-10-4. INSTALLED REPAIR PER SRM 53-10-4. ITEM FOUND DURING INSPECTION AT HMV 2. 2L73 4F A3WE 19950217003441995021700344NM 1995 2 17 DL72S950573 119950201A5347 SEAT TRACK BOEING727 727232 1384082NM FS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 FWD SUPPORT LUG OF SEAT TRACK CRACKED, LOC STA760 RT O/B SEAT TRACK. REPAIRED PER SRM 53-10-8 PG 47-49 FIG 11. THIS ITEM WAS FOUND DURING INSPECTION AT HMV2. 2L73 4F A3WE 19950217003451995021700345NM 1995 2 17 DL72S950586 119950201A5754 LE RIB BOEING727 727232 1384082NM NR 7LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND RIB CRACKED ON INBD SIDE OF INBD TRACK ON NR 7 L/E SLAT AND A RIB CRACKED ON OUTBD SIDE OF INBD TRACK NR 7 SLAT, REPAIRED PER MM 57-54-0 PG 805 ON INBD SIDE AND OUTBD SIDE PER MM 57-57-0 PG 805. 2L73 4F A3WE 19950217003461995021700346NM 1995 2 17 DL72S950587 119950131A5713 STRINGER BOEING727 727232 1384082NM WS 338.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND FUEL TANK UPPER STRINGER NR 17 CRACKED AT WS 338.50, REPAIRED PER SRM 57-10-4 FIG 6 AND ERA 301143-14 REV A. 2L73 4F A3WE 19950217003471995021700347NM 1995 2 17 DL72S950588 119950201A5313 STRINGER BOEING727 727232 1384082NM FS 380 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND STRINGER 15 LEFT CRACKED AT LOWER RIVET STA 380, REPAIRED PER 53-10-3 FIG 1. 2L73 4F A3WE 19950217003481995021700348NM 1995 2 17 DL72S950589 119950204A5230 SKIN BOEING727 727232 1384082NM C-2 CARGO DOOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND C-2 DOOR HAS HOLE PUNCHED IN IT ABOVE AFT LOWER CORNER, REPAIRED PER SRM 52-00-3 FIG 3. 2L73 4F A3WE 19950217003491995021700349NM 1995 2 17 DL72S950591 119950201A5754 RIB BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 RIB CRACKED, 2ND RIB FROM OUTBOARD END OF NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER M/M 57-54-0 PG 819. 2L73 4F A3WE 19950217003501995021700350NM 1995 2 17 DL72S950592 119950201A5754 STOPS BOEING727 727232 1384082NM NR 5 LE SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 INBOARD AND OUTBOARD STOP WORN ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED STOPS PER MM27-81-11 PG 803. 2L73 4F A3WE 19950217003511995021700351NM 1995 2 17 DL72S950593 119950201A5754 RIB BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 OUTBOARD RIB CRACKED ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950217003521995021700352NM 1995 2 17 DL72S950594 119950201A5530 STRINGER BOEING727 727232 1384082NM FS 133.800 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 STRINGER CRACKED AT FS 133.800, STR 9L CRACKED AT RIB. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19950217003531995021700353NM 1995 2 17 DL72S950595 119950201A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 LOWER CHORD ANGLE CRACKED AT 2ND RIB O/B OF ACTUATOR FITTING ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 816. 2L73 4F A3WE 19950217003541995021700354NM 1995 2 17 DL72S950596 119950201A5754 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 RIB CRACKED, 3RD RIB OUTBOARD OF ACTUATOR MOUNT ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950217003551995021700355NM 1995 2 17 DL72S950611 119950208A5754651622171 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 DURING INSPECTION OF THE NR 4 LEADING EDGE SLAT, RIB MARKED NR 18 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0 FIG 805. 2L73 4F A3WE 19950217003561995021700356NM 1995 2 17 DL72S950622 119950201A5313 STRINGER BOEING727 727232 1384082NM FS 560 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND FUSELAGE STRINGER 7R, CRACKED FORWARD OF FS 560, REPAIRED PER SRM 51-10-3. 2L73 4F A3WE 19950217003571995021700357NM 1995 2 17 DL72W950567 119950122A57536521631273A SKIN BOEING727 727247 138408FNM NR 1 FORE FLAP WORN/HOLE A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV SHOP INSPECTION, LEFT WING NR 1 FORE FLAP WAS REPAIRED FOR DAMAGE TO THE L/E SKIN AT 11 INCHES FROM THE INBOARD END OF FLAP AND A TIME LIMITED REPAIR WAS REPLACED AT 46 INCHES FROM THE OUTBOARD END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950217003581995021700358NM 1995 2 17 DL72W950568 119950122A57536521631273A LE SKIN BOEING727 727247 138408FNM NR 1 FOFE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 AT HMV SHOP INSPECTION, LEFT WING NR 1 FORE FLAP WAS FOUND WITH WEAR DAMAGE TO THE LEADING EDGE SKIN AT 64 INCHES FROM THE I/B END OF FLAP AND 26 INCHES TO 29 INCHES FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950217003591995021700359NM 1995 2 17 DL72W950623 119950123A5753652163388A SUPPORT FITTING BOEING727 727247 138408FNM NR 4 MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING SHOP INSPECTION, NR 4 MID FLAP O/B SUPPORT FITTING THRUST BOREFLANGE PITTED WITH CORROSION. FLANGE WAS MACHINED PER SRM 57504 TO REMOVE PITS, NO BUSHING WAS REQUIRED, FITTING PN 65-19248-4. 2L73 4F A3WE 19950217003601995021700360NM 1995 2 17 DL73S950555 119950208A7110657377391 COWL BOEING737 737232 1384475NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 DURING A ROUTINE INSPECTION A 3 INCH BY 4 INCH DENT WAS FOUND ON THE NR 1 ENGINE SIDE COWL NEXT TO THE OIL ACCESS DOOR. THE DENT WAS CUT OUT AND AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 54-10-3. THE AUTHORITY USED TO REPLACE THE FLUSH REPAIR WITH AN EXTERNAL ONE WAS FOUND AT SRM CHAP 51. 2L72 4F RTA16WE 19950217003611995021700361NM 1995 2 17 DL757950629 119950202A4940211734218 CONTROLLER BOEING757 757232 1384965NM APU FAULTY A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO11642DL 23996 DURING CRUISE, HAD RIGHT GENERATOR AND DRIVE LIGHT, APU FAILED TO START, DIVERTED DFW. REPLACED APU BATTERY, CONTROLLER, AND IGNITION PLUG, OPERATION NORMAL. CONTROLLER HAD HISTORY OF NO FLAME FAULT. 2L72 4F RTA2NM 19950217003621995021700362NE 1995 2 17 DL76L950627 219950213A7261PW4060 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 HIGH OIL CONSUMPA DALAK NONE O OTHER ININSP/MAINT 1 SO11173DN16562 24800 724139 AFTER REVIEWING OIL CONSUMPTION HISTORY, IT WAS DETERMINED CONSUMPTION RATE WAS BEYOND LIMITS, ENGINE WAS REMOVED AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19950217003631995021700363NM 1995 2 17 DLM88950580 119950127A55435955545503 TE SKIN DOUG MD88 MD88 3023688NM RUDDER TAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11994DL 53346 DURING SHOP INSPECTION, RUDDER TAB WAS FOUND WITH 2 CRACKS ON THE TRAILING EDGE. ONE WAS 7 INCHES LONG AT 30 INCHES FROM THE TOP, THE OTHER WAS 2 INCHES LONG AT 3 INCHES FROM THE BOTTOM. REPAIRED CRACKS PER SRM 51-70-1A, NR 18 1A NR 18. 2L72 4F RTA6WE 19950217003641995021700364NM 1995 2 17 DLM88950628 119950213A36105910244125 DUCT DOUG MD88 MD88 3023688NM TAIL COMP BLOWN A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11901DL 49532 ON CLIMB-OUT PASSING 14,000 FT TAIL COMPARTMENT TEMP HIGH WARNING LIGHT CAME ON. RETURNED DFW. FOUND PNEUMATIC DUCT BLOWN RIGHT SIDE TAIL COMPARTMENT. REPLACED DUCT. 2L72 4F RTA6WE 19950217003651995021700365NM 1995 2 17 MWEA95130 119950214A25605917689103 SLIDE COVER DOUG MD88 MD88 3023688NM MAIN CABIN DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31701ME 49760 PILOT REPORT, CLIP WHICH HOLDS EVACUATION SLIDE COVER ON MAIN CABIN DOOR FELL OFF. MECHANIC REINSTALLED CLIP AND SLIDE COVER. RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA6WE 19950217003661995021700366WP 1995 2 17 ABXA9500087 119950201A552359104141 SKIN DOUG DC9 DC932 3022066WP LT ELEV TAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING OFF WING INSPECTION PROCEDURES FOUND LEVEL II CORROSION ON THE LEFT ELEVATOR TAB INBOARD LOWER SKIN. REPAIRED IAW DC-9 SRM 57. 2L72 4F A6WE 19950217003671995021700367WP 1995 2 17 ABXA9500088 119950106A53425939711501 ANGLE DOUG DC9 DC931 3022065WP FS 1087 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND LEFT DORSAL FIN ATTACH ANGLE HAD ONE FASTENER HEAD MISSING AND SEVERAL FASTENERS NOT PORPERLY SEATED. REPLACED FASTENERS IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950217003681995021700368WP 1995 2 17 ABXA9500089 119950110A53425939711502 ANGLE DOUG DC9 DC931 3022065WP FS 1087 FAILED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 89-08-10 AND S.B.'S A53-154 AND A53-223, FOUND RIGHT DORSAL FIN ATTACH ANGLE BUCKLED AND FASTENERS PULLED. REPLACED RIGHT DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 53-05, FIGURE 23 AND SB'S A53-154 AND A53-223. 2L72 4F A6WE 19950217003691995021700369WP 1995 2 17 ABXA9500090 119950205A52805913433503 HINGE DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON THE OUTBOARD MAIN LANDING GEAR DOOR FOR THE WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950217003701995021700370WP 1995 2 17 ABXA9500091 119950111A532099100733 PANEL DOUG DC9 DC931 3022065WP FS 83 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR UPPER WHEEL WELL PRESSURE PANEL WAS FOUND CRACKED AT STA 83. REPAIRED PANEL IAW SB 53-187. 2L72 4F A6WE 19950217003711995021700371WP 1995 2 17 ABXA9500092 119950201A53123913926 FITTING DOUG DC9 DC931 3022065WP AFT PLUG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23924AX 47403 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 80-02-16, THE AFT PRESSURE DOME PLUG DOOR LUG SHOWED A CRACK INDICATION ON THE X-RAY. FITTING WAS REPLACED IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950217003721995021700372WP 1995 2 17 ABXA9500093 119950214A33505708458503 EEL PWR PACK DOUG DC8 DC863 302198AWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23820AX 46155 EMERGENCY LIGHTS WEAK. REPLACED EMERGENCY LIGHTS POWER PACK IAW DC-8 MM CHAPTER 33. OPS CHECKED GOOD. 2L74 4F 4A25 19950217003731995021700373SO 1995 2 17 COM11784 119950215A32402025000002 SWIVEL EMB 120 EMB120RT SO LT MLG BRAKE DEFECTIVE A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO011117H 120117 LEFT BRAKE TEST FUNCTION IS INOP. REPLACED LT MLG BRAKE SWIVEL. 2L72 4T RTA31SO 19950217003741995021700374SO 1995 2 17 COM11785 119950210A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01268CA7425 7425 120262 THE FOLLOWING WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERO DESIGN REPORT NR 1387-2, AT WING RIBS 15, 16 AND 18. P/N 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 3 EA; 120-17056-013, 2 EA; 120-17057-006, 1 EA; 120-17057-005, 1 EA; 120-17057-007, 1 EA; 120-17056-011, 1 EA; 120-17059-015, 1 EA. 2L72 4T RTA31SO 19950217003751995021700375 1995 2 17 COM11786 419950212A3418C818061 STALL COMPUTER EMB 120 EMB120RT SO AVIONICS DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01179CA12347 120179 DURING TAKEOFF, STALL AURAL WARNING, STICK SHAKER AND STICK PUSHER ACTIVATED. REPLACED THE STALL COMPUTER. 2L72 4T RTA31SO 19950217003761995021700376SO 1995 2 17 COM11787 119950214A612330005000052 SIGNAL COND EMB 120 EMB120RT SO LT ENG DEFECTIVE A COMAK NONE O OTHER CLCLIMB 1 SO01267CA6464 987 120259 AUTO FEATHER WARNING CAME ON AFTER TAKEOFF. REPLACED THE LT TORQUE SIGNAL CONDITIONER. 2L72 4T RTA31SO 19950217003771995021700377EU 1995 2 17 COM31034 119950208A3230L38710SA SWIVEL SAAB SF340 SF340A 7850100EU LT MLG BROKEN A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01140N 340A140 LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. HYDRAULIC LEAK NOTICED ON LT MLG. REPLACED LT MLG DOWNLOCK SWIVEL FITTING. 2L72 4T RTA52EU 19950217003781995021700378EU 1995 2 17 COM31035 119950214A33506013211 EEL POWER SUPPLY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST UKUNKNOWN 1 SO01358CA15372324 340A047 EMERGENCY LIGHTING ABOVE FWD RT EMERGENCY EXIT IS INOP. REPLACED BATTERY PACK. 2L72 4T RTA52EU 19950217003791995021700379EA 1995 2 17 COM60418 119950213A27604916403 SECU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO01917CA4216 3418 7017 SPOILER ON FAULT MESSAGE ON EICAS. REPLACED SPOILER ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950217003841995021700384SW 1995 2 17 MEJA9501001 119950105A7712310703411 TORQUE RING SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE3311U 01514WP RT ENGINE MALFUNCTIONED A MEJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW17376PH1953 1953 AC573 44267 AFTER TAKEOFF IN CLIMB RIGHT ENGINE TORQUE INDICATION BEGAN TO FLUCTUATE PLUS OR MINUS 10 PERCENT. AIRCRAFT RETURNED TO SAT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT DISCREPANCY AND FOUND A DEFECTIVE TORQUE RING. REMOVED AND REPLACED TORQUE RING IN ACCORDANCE WITH THE GARRETT MAINTENANCE MANUAL. PERFORMED RUN UP AND LEAK CHECK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T3 T A8SW E3WE 19950217003851995021700385SW 1995 2 17 MEJA9501002 119950106A2613MS3126E2461P CONNECTOR SWRNGNSA227 SA227AT 8780610SW RT WING ROOT WET A MEJAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW17560UP9938 9938 AT560 ON FLIGHT 1851 IN CRUISE THE RIGHT WING OVERHEAT LIGHT CAME ON. AIRCRAFT TURNED BACK AND RETURNED TO MFE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND MOISTURE IN THE WING ROOT CONNECTOR FOR THE WING OVERHEAT LIGHT SYSTEM. CLEANED AND DRIED THE CONNECTOR. PERFORMED SYSTEM FUNCTIONAL CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950217003861995021700386SW 1995 2 17 MEJA9502003 119950203A243051509002B GEN CONTROL UNIT SWRNGNSA227 SA227AT 8780610SW RT NACELLE FAILED A MEJACD ABORTED TAKEOFF RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SW17570UP 338 AT570 ON TAKEOFF ROLL, RIGHT GENERATOR FAILED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND AIRCRAFT WAS FERRIED TO PHL FOR MAINTENANCE. TROUBLESHOT SYSTEM AND FOUND DEFECTIVE GENERATOR CONTROL UNIT (GCU). REMOVED AND REPLACED GCU IN ACCORDANCE WITH FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL 24-30-25. SYSTEM FUNCTIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950217003871995021700387SW 1995 2 17 QXEA9500048 119950213A3260602EN16 UPLOCK SW SWRNGNSA227 SA227AC 8780603SW NLG INTERMITTENT A QXEAK NONE N FALSE WARNING APAPPROACH 1 NM0926959 AC662 BZN - NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEAR FUNCTIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO BOI WHERE LT UPLOCK SWITCH ASSY WAS REPLACED. GROUND TESTS PERFORMED SATISFACTORY AND AIRCRAFT RELEASED FOR SERVICE. 1L72 4T A8SW 19950217003881995021700388SW 1995 2 17 QXEA9500049 119950213A29102781006019 HYD LINE SWRNGNSA227 SA227AC 8780603SW LT MLG WW LEAKING A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09383PH24048 AC590 FCA - LOST HYDRAULIC PRESSURE, NOSE GEAR UNSAFE LIGHT ILLUMINATED, CREW PERFORMED EMERGENCY GEAR EXTENSION AND RETURNED TO FIELD. FOUND HYDRAULIC LINE IN LEFT WHEEL WELL LEAKING. REPLACED LINE, AND NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS. SERVICED RESERVOIR. GROUND TESTING SATISFACTORY. AIRCRAFT WAS RELEASED FOR SERVICE. 1L72 4T A8SW 19950217003891995021700389SW 1995 2 17 QXEA9500050 119950213A3260602EN16 UPLOCK SW SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A QXEAK NONE N FALSE WARNING CLCLIMB 1 NM09384PH AC592 GEG - DURING GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON. FLIGHT CONTINUED TO PDX WITHOUT INCIDENT. REPLACED NLG UPLIMIT SWITCH. GROUND TESTS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 1L72 4T A8SW 19950217003901995021700390NM 1995 2 17 SWAA950171 119950213A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0786SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED JUST ABOVE POTABLE WATER SERVICE PANEL AT S25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950217003911995021700391NM 1995 2 17 SWAA950172 119950213A3350 EEL BATTERY BOEING737 7372T4 1384492NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07722WN 22698 AT GATE, FOUND EMERGENCY FLASHLIGHT NOT TESTING. REPLACED FLASHLIGHT PER BOEING M/M. 2L72 4F A16WE 19950217003921995021700392NM 1995 2 17 SWAA950173 119950213A5210 SEALS BOEING737 7373H4 1384600NM PAX DOOR MISALIGNED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07336SW 23940 DURING CLIMBOUT, NOTED PRESSURIZATION LEAKAGE AT FORWARD ENTRY DOOR, LOWER HINGE SEAL. UNABLE TO MAINTAIN PRESSURE. AIRCRAFT RETURNED TO SJC AND MADE AN UNEVENTFUL LANDING. FOUND LOWER HINGE SEAL NOT SEATING PROPERLY. REPOSITIONED SEAL PER BOEING M/M, NO HELP. REPLACED UPPER AND LOWER HINGE SEAL COVERS. 2L72 4F RTA16WE 19950217003931995021700393NM 1995 2 17 SWAA950174 119950214A5330 SKIN BOEING737 7373G7 1384595NM L2 DOOR CUTOUT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07683SW 24008 DURING SCHEDULED 1/2 D CHECK, FOUND CRACK IN UPPER CORNER OF LOWER HINGE SKIN CUTOUT AT FWD SERVICE DOOR. REPAIRED PER SWA ACO 3189-52. 2L72 4F RTA16WE 19950217003941995021700394NM 1995 2 17 SWAA950175 119950214A5320 DOOR FRAME BOEING737 7373A4 1384585NM FS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07678AA 23290 DURING SCHEDULED B1 CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT BS 787. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950217003951995021700395NM 1995 2 17 SWAA950176 119950214A5330 SKIN BOEING737 737317 138447PNM BS 328 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07693SW 23174 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 328, S21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950217003961995021700396NM 1995 2 17 SWAA950177 119950214A5330 SKIN BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, BETWEEN S17L AND 17R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950217003971995021700397NM 1995 2 17 SWAA950178 119950211A33506104781 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED A2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950217003981995021700398NM 1995 2 17 SWAA950179 119950212A3350 EEL BOEING737 7372H4 138448CNM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0782SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2L72 4F A16WE 19950217003991995021700399NM 1995 2 17 SWAA950180 119950210A33506104789 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR AND FWD ENTRY EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950217004001995021700400NM 1995 2 17 UPS202316 119950214A5320 STRAP BOEING727 727173C 1384059NM FS 970-1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATES BS 970-1050 LBL 2-RBL 2 ON CEILING STABILIZER STRAP. INSTALLED REPAIR IAW SRM 51-10-1, 51-30-2, 51-10-2 AND MM 51-20-31. 2L73 4F A3WE 19950217004011995021700401NM 1995 2 17 UPS202317 119950214A5315BAC150510042 FLOOR BEAM BOEING727 727173C 1384059NM FS 1030 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND AND UNDER BOLTS AT BS 1030 RBL 56-63 WL 201 ON LOWER FLANGE OF FLOOR BEAM. INSTALLED REPAIR IAW B727-5310-6627A. 2L73 4F A3WE 19950217004021995021700402NM 1995 2 17 UPS202318 119950214A5320 CHANNEL BOEING727 727173C 1384059NM FS 227 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S FORWARD SEAT PEDESTAL, AFT INTERCOSTAL STA 227 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 51-30-2, 51-20-1, 53-10-1 AND 51-10-2. 2L73 4F A3WE 19950217004031995021700403NM 1995 2 17 UPS202319 119950214A5320 CHANNEL BOEING727 727173C 1384059NM FS 230 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S AFT SEAT PEDESTAL FORWARD INTERCOSTAL AT STA 230 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 53-10-1, 51-20-1 AND 51-10-2. 2L73 4F A3WE 19950217004041995021700404NM 1995 2 17 UPS202320 119950214A5347 SEAT PEDESTAL BOEING727 727173C 1384059NM FS 246 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CAPTAIN'S AFT SEAT PEDESTAL AFT INTERCOSTAL AROUND BOLT HOLES THROUGH FLOOR AT STA 246 WL 208 LBL 12-30. INSTALLED REPAIR IAW SRM 51-20-1, 51-30-2 AND 53-10-1. 2L73 4F A3WE 19950217004051995021700405NM 1995 2 17 UPS202321 119950214A5320 HAT CHANNEL BOEING727 727173C 1384059NM FS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION THROUGHOUT HAT CHANNEL BOTH TOP AND BOTTOM SIDES AT BS 344 WL 208 RBL 17-61. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950217004061995021700406NM 1995 2 17 UPS202322 119950214A532065261737 INTERCOSTAL BOEING727 727173C 1384059NM FS 326-344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON INTERCOSTAL FROM BS 326-344 WL 208 RBL 42. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004071995021700407NM 1995 2 17 UPS202323 119950214A5315 FLOOR BEAM BOEING727 727173C 1384059NM FS 312 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 312 WL 208 FROM RBL 14 TO LBL 55. INSTALLED REPAIR IAW UPS EO NR B727-5310-6624. 2L73 4F A3WE 19950217004081995021700408NM 1995 2 17 UPS202324 119950214A5315 FLOOR BEAM BOEING727 727173C 1384059NM FS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 344 WL 208 FROM RBL 65 TO LBL 65. INSTALLED REPAIR IAW UPS EO NR B727-5310-6623A AND SRM 51-30-2. 2L73 4F A3WE 19950217004091995021700409NM 1995 2 17 UPS202325 119950214A5315 FLOOR BEAM BOEING727 727173C 1384059NM FS 540 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 540 UNDER NUTPLATE LBL 41-55 WL 208. INSTALLED REPAIR IAW UPS EO B 727-5310-6647. 2L73 4F A3WE 19950217004101995021700410NM 1995 2 17 UPS202326 119950215A53216518745113 FLOOR BOEING727 727173C 1384059NM FS 950 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FASTENERS THROUGH PRESSURE FLOOR STA 950 LBL 28 WL 201. INSTALLED REPAIR IAW SRM 51-30-02 AND 51-20-04. 2L73 4F A3WE 19950217004111995021700411NM 1995 2 17 UPS202327 119950215A5320 BUTT JOINT BOEING727 727173C 1384059NM FS 479 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FORWARD SIDE OF BUTT JOINT STA 479 BETWEEN STR 9 AND 10. INSTALLED REPAIR IAW EO 727-5310-1371 APPEN. 8.5, BOEING DWG 69-62161 AND SRM'S 51-10-02 AND 51-30-02. 2L73 4F A3WE 19950217004121995021700412NM 1995 2 17 UPS202328 119950215A5313 STRINGER BOEING727 727173C 1384059NM FS 520-540 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STRINGER STA 520-540 STR 3 RT SIDE. INSTALLED REPAIR IAW SRM 53-10-3. 2L73 4F A3WE 19950217004131995021700413NM 1995 2 17 UPS202330 119950215A551165382035 SPAR CHORD BOEING727 727173C 1384059NM LT HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON LT HORIZONTAL STAB LOWER REAR SPAR CHORD AT STAB. STA 223 STA 194-200 AND STA 186. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004141995021700414NM 1995 2 17 UPS202331 119950215A5753 RIB BOEING727 727173C 1384059NM RT TE MID-FLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND R/W O/B MID-FLAP I/B FOREFLAP SUPPORT RIB IS CRACKED ON FLANGE BETWEEN FASTENERS ON I/B SIDE. INSTALLED REPAIR IAW SRM 51-30-2 AND 57-50-4. 2L73 4F A3WE 19950217004151995021700415NM 1995 2 17 UPS202332 119950215A5753 CARRIAGE BOEING727 727173C 1384059NM NR 5 TE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 5 FLAP CARRIAGE SPINDLE. INSTALLED REPAIR IAW MM 27-51-03. 2L73 4F A3WE 19950217004161995021700416NM 1995 2 17 UPS202333 119950215A2510 SEAT PEDESTAL BOEING727 727173C 1384059NM BS 228-245 CRACKS A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKS ON BOTH UPPER AND LOWER AFT FLANGES OF INBOARD AFT CAPT'S SEAT PEDESTAL AT LBL 12 WL 208 BS 228-245. INSTALLED REPAIR IAW SRM 51-20-1 AND 51-30-2. 2L73 4F A3WE 19950217004171995021700417NM 1995 2 17 UPS202334 119950215A5313 STRINGER BOEING727 727173C 1384059NM FS 710-714 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AT STA 710-714 STRINGER 21L. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004181995021700418NM 1995 2 17 UPS202335 119950215A5320 ANGLE BOEING727 727173C 1384059NM FS 545-556 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON CARGO DOOR THRESHOLD ANGLE BS 545-556 RBL 28 WL 154. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004191995021700419NM 1995 2 17 UPS202336 119950215A53207075T6 SHEAR TIE BOEING727 727173C 1384059NM BS 1030 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED SHEAR TIE AT BS 1030 WL 185 RBL 55 (BETWEEN STR 19R-20R). INSTALLED REPAIR IAW SRM 51-40-3 AND 53-10-2. 2L73 4F A3WE 19950217004201995021700420NM 1995 2 17 UPS202338 119950215A5347 SEAT TRACK BOEING727 727173C 1384059NM BS 344-360 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND SEAT TRACK STA 344-360 LBL 60 WL 208 TO HAVE CORROSION IN FASTENERS HOLES. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004211995021700421NM 1995 2 17 UPS202339 119950215A5320651620255 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND BS 870 WEB STIFFENER AT LBL 45 CORRODED OUT OF LIMITS. INSTALLED REPAIR IAW SRM 51-10-2. 2L73 4F A3WE 19950217004221995021700422NM 1995 2 17 UPS202340 119950215A5320651620218 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB STIFFENER AT RBL 57 OUT OF LIMITS. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004231995021700423NM 1995 2 17 UPS202341 119950215A53132024T3 STRINGER BOEING727 727173C 1384059NM FS 360-380 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 3 STRINGER LT; FLANGES STA 360-380. INSTALLED REPAIR IAW SRM 53-10-1, 53-10-3, 51-10-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950217004241995021700424NM 1995 2 17 UPS202342 119950215A5313BAC1493513 STRINGER BOEING727 727173C 1384059NM BS 480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKED STRINGER BS 480 STR 25 RT RBL 31 WL 154. INSTALLED REPAIR IAW SRM 51-30-2, 51-10-2 AND 51-10-3. 2L73 4F A3WE 19950217004251995021700425NM 1995 2 17 UPS202343 119950215A5313 STRINGER BOEING727 727173C 1384059NM FS 259-277 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STR 2R FROM STA 259-277 AROUND NUTPLATES. INSTALLED REPAIR IAW SRM 51-30-2, 53-10-1 AND MM 20-43-01. 2L73 4F A3WE 19950217004261995021700426NM 1995 2 17 UPS202344 119950215A5330 SKIN BOEING727 727173C 1384059NM BS 754-773 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION BS 754-773 UPPER FUEL CELL SKIN RBL 25-44 WL 205. INSTALLED REPAIR IAW UPS EO 727-57-1075. 2L73 4F A3WE 19950217004271995021700427NM 1995 2 17 UPS202345 119950215A5511 SPAR CHORD BOEING727 727173C 1384059NM RT HORIZ STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND RT HORIZONTAL STAB. CLOSURE RIB UPPER CHORD IS CORRODED ON BOTTOM SIDE OF FLANGE AND CRACKS RUNNING FROM FASTENER TO FASTENER. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004281995021700428NM 1995 2 17 UPS202346 119950215A5330 SKIN BOEING727 727173C 1384059NM FS 740-758 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION UPPER FUEL CELL SKIN STA 740-758 RBL 25-62. INSTALLED REPAIR IAW SRM 51-10-2, 51-10-6, 57-30-2 AND OHM 20-10-03. 2L73 4F A3WE 19950217004291995021700429NM 1995 2 17 UPS202347 119950215A5753 SKIN BOEING727 727173C 1384059NM TE MID FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND WINGS 321 I/B MIDFLAP LOWER AFT SKIN CRACKED AT AFT EDGE BEHIND NR 4 CARRIAGE. INSTALLED REPAIR IAW SRM 57-50-4. 2L73 4F A3WE 19950217004301995021700430NM 1995 2 17 UPS202359 119950215A5320 WEB BOEING727 727173C 1384059NM BS 311 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL WEB DOUBLER RBL 15 WL 175 BS 311. INSTALLED REPAIR IAW SRM 53-10-2 AND SRM 51-30-2. 2L73 4F A3WE 19950217004311995021700431NM 1995 2 17 UPS202360 119950215A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 720 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES BS 720 RBL 45-62 WL 208. INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F A3WE 19950217004321995021700432NM 1995 2 17 UPS202361 119950215A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 326 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM AT BS 326 WL 208 RBL 14-LBL 55. INSTALLED REPAIR IAW UPS EO B727-5310-6625. 2L73 4F A3WE 19950217004331995021700433NM 1995 2 17 UPS202362 119950215A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 680 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM BS 680 RBL 15-45 WL 208. INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F A3WE 19950217004341995021700434NM 1995 2 17 UPS202363 119950215A5315BAC1505101167 FLOOR BEAM BOEING727 727173C 1384059NM BS 600 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 600 TOP CHORD RBL 48-61 WL 208. INSTALLED REPAIR IAW 53-10-8. 2L73 4F A3WE 19950217004351995021700435NM 1995 2 17 UPS202364 119950215A5313 STRINGER BOEING727 727173C 1384059NM BS 360-400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION AT NR 2 STR LT STA 360-400; ON FLANGES/SIDES. INSTALLED REPAIR IAW SRM 53-10-3, 51-30-2 AND 53-10-4. 2L73 4F A3WE 19950217004361995021700436NM 1995 2 17 UPS202365 119950215A553069177774 STIFFENER BOEING727 727173C 1384059NM FIN STA 233.746 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL FIN INTERSPAR SKIN STIFFENER RT SIDE AT VERTICAL FIN STA 233.746 INSIDE VERTICAL FIN. INSTALLED REPAIR IAW 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950217004371995021700437NM 1995 2 17 UPS202366 119950215A5315 FLOOR BEAM BOEING727 727173C 1384059NM FS 294 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON STA 294 FLOOR BEAM AROUND NUTPLATES WL 208 LBL 30 TO RBL 10. INSTALLED REPAIR IAW UPS EO 727-53-1461. 2L73 4F A3WE 19950217004381995021700438NM 1995 2 17 UPS202367 119950215A5313 STRINGER BOEING727 727173C 1384059NM BS 1080-1088 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BACKSIDE OF STRINGER AT BS 1080-1088 STRINGER 20L. INSTALLED REPAIR IAW SRM 53-10-3, 51-70-2. 2L73 4F A3WE 19950217004391995021700439NM 1995 2 17 UPS202368 119950215A5315 FLOOR BEAM BOEING727 727173C 1384059NM FS 1110 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON FLOOR BEAM STA 1110 LBL 60 AND LBL 43-3 WL 208. INSTALLED REPAIR IAW SRM 53-10-8. 2L73 4F A3WE 19950217004401995021700440NM 1995 2 17 UPS202369 119950215A5320651620217 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION BS 870 WEB STIFFENER AT LBL 57.5. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004411995021700441NM 1995 2 17 UPS202370 119950215A5320651620253 STIFFENER BOEING727 727173C 1384059NM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 870 WEB STIFFENER AT LBL 28. INSTALLED REPAIR IAW SRM 51-30-2. 2L73 4F A3WE 19950217004421995021700442NM 1995 2 17 UPS202378 119950215A5270 FWD ENTRY DOOR BOEING727 72727C 138400JNM FLIGHT DECK UNLATCHED A IPXAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01915UP 19533 PILOT REPORTED UPON TAXI IN, FORWARD ENTRY DOOR LIGHT ILLUMINATED. FRONT ENTRY DOOR INSIDE LATCH FOUND UNLATCHED. CHECKED DOOR RIG AND ADJUSTED AS REQUIRED PER MM 52-11-00 ADJUSTMENT/TEST INSTRUCTIONS. DOOR OPERATION CHECKS OK. 2L73 4F A3WE 19950217004431995021700443NM 1995 2 17 UPS202388 119950215A3260 UPLOCK SWITCH BOEING727 72725C 138400HNM NLG MALFUNCTION A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01948UP 19357 PILOT REPORTED WHEN HE EXTENDED THE GEAR THE FIRST TIME, THE TWO MAIN GEAR INDICATED DOWN WITH GREEN LIGHTS, BUT NOSE DIDN'T. RECYCLED THE GEAR AND SAME THING HAPPENED. THE NOSE GEAR VISUAL HOLE CONFIRMED NOSE GEAR DOWN (STRIPES ALIGNED). WHEN NOSE GEAR TOUCHED DOWN ON LANDING, NOSE GEAR GREEN LIGHT CAME ON. DETERMINED THAT THE NOSE GEAR LOCK SWITCH BAD. WHILE TAPPING ON SWITCH, LIGHT WOULD FLICKER. REMOVED AND REPLACED SWITCH PER 32-64-01, GROUND TEST GOOD. 2L73 4F A3WE 19950217004441995021700444WP 1995 2 17 UPS802348 119950213A53135649327 LONGERON DOUG DC8 DC871F 302199DWP FS 1750 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 13 RT, FS 1750 HAS 1.5 INCH CRACK. INSTALLED REPAIR IAW SRM 53-2-2. 2L74 4F RT4A25 19950217004451995021700445WP 1995 2 17 UPS802349 119950213A53132597242212000 LONGERON DOUG DC8 DC871F 302199DWP FS 25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 12R AT FS 25 HAS 1 INCH CRACK. INSTALLED REPAIR IAW SRM 53-2-2. 2L74 4F RT4A25 19950217004461995021700446WP 1995 2 17 UPS802350 119950213A5313032174PH LONGERON DOUG DC8 DC871F 302199DWP FS 85-95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 21L, STA 85-95 LIGHTENING HOLES 3 EACH WITH CRACKS ON WEB. INSTALLED REPAIR IAW SRM 51-1-21. 2L74 4F RT4A25 19950217004471995021700447WP 1995 2 17 UPS802351 119950213A57535702446 VANE DOUG DC8 DC871F 302199DWP NR 3 TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 3 FLAP VANE DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-51-14. 2L74 4F RT4A25 19950217004481995021700448WP 1995 2 17 UPS802352 119950213A57535652287506 VANE DOUG DC8 DC871F 302199DWP NR 1 TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND RT WING NR 1 FLAP VANE DELAMINATED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 27-61-01. 2L74 4F RT4A25 19950217004491995021700449WP 1995 2 17 UPS802353 119950213A57510502024T3 SKIN DOUG DC8 DC871F 302199DWP RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND RT I/B AILERON LOWER SKIN HAS 2 EACH .25 INCH LONG CRACKS AT INBOARD EDGE. INSTALLED REPAIR IAW SRM 57-2-0. 2L74 4F RT4A25 19950217004501995021700450WP 1995 2 17 UPS802354 119950213A57130502024T3 LONGERON DOUG DC8 DC871F 302199DWP FS 130-390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 35L AND 34R CRACKED AT FS 190-390. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950217004511995021700451WP 1995 2 17 UPS802355 119950213A57139754913 LONGERON DOUG DC8 DC871F 302199DWP FS 220-255 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 36 I/B SIDE CRACKED AT FS 220-255 AND FS 220-360. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950217004521995021700452WP 1995 2 17 UPS802356 119950213A5312 BEAM DOUG DC8 DC873F 302199FWP COMPT. 60 CRACK A IPXAO OTHER O OTHER ININSP/MAINT 1 SO01812UP 46112 DURING 'B' CHECK MAINTENANCE FOUND AFT BULKHEAD CRACKED AT HORIZONTAL "J" BEAM SUPPORT, 3RD SUPPORT FROM BOTTOM. INSTALLED REPAIR IAW EO DC8-5310-6669A. 2L74 4F RT4A25 19950217004531995021700453WP 1995 2 17 UPS802371 119950215A5313975491335 LONGERON DOUG DC8 DC871F 302199DWP FS 220 CRACK A IPXAO OTHER O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND LONGERON 35R I/B SIDE CRACKED AT FS 220. INSTALLED REPAIR IAW SRM 53-2-2. 2L74 4F RT4A25 19950217004541995021700454WP 1995 2 17 UPS802372 119950215A53134750419 LONGERON DOUG DC8 DC871F 302199DWP FS 1227 CRACK A IPXAO OTHER O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND FS 1227, LONGERON 19R END FITTING CRACKED 1/2 INCH LONG. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950217004551995021700455WP 1995 2 17 UPS802373 119950215A52300632024T3 FRAME DOUG DC8 DC871F 302199DWP A X-SLIDE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND "A" X-SLIDE FLOOR FRAME CRACKED 2 EACH PLACES INSIDE UPPER LIGHTING HOLE BETWEEN 5 AND 6 T-HOOKS. INSTALLED REPAIR IAW SRM 52-2-2, FIGURE 2. 2L74 4F RT4A25 19950217004561995021700456WP 1995 2 17 UPS802374 119950215A53115772958 BELTFRAME DOUG DC8 DC871F 302199DWP FS 1580 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND FS 1580 LONGERON 21R BELTFRAME CRACKED. INSTALLED REPAIR IAW SRM 53-2-0, FIG. 3. 2L74 4F RT4A25 19950217004571995021700457WP 1995 2 17 UPS802375 119950215A532036169481 END FITTING DOUG DC8 DC871F 302199DWP FS 700 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND BELTFRAME END FITTING CRACKED 1 INCH LONG AT FS 700 LONGERON 21L. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950217004581995021700458WP 1995 2 17 UPS802376 119950215A2510 INSULATION DOUG DC8 DC871F 302199DWP PRESS BULKHEAD BINDING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01707UP 45907 DURING TEST OPS AND TAKEOFF, THE GEAR LEVER WAS HARD TO RAISE INTO UP AND LOCKED POSITION, CYCLED GEAR AND LEVER MOVED OK INTO UP AND LOCKED. FOUND INSULATION ON FWD PRESSURE BULKHEAD FOULING CONTROL CABLES. INSTALLED INSULATION PROPERLY AND GEAR OPS CHECKED GOOD PER MM 32-30-00. 2L74 4F RT4A25 19950217004591995021700459WP 1995 2 17 UPS802377 119950214A3260H141003 DN LOCK SWITCH DOUG DC8 DC873F 302199FWP LT MLG MALFUNCTION A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01815UP 46002 PILOT REPORTED LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE ON INITIAL DOWN SELECTION. AFTER CYCLING GEAR AFTER GO-AROUND, LIGHT SHOWED NORMAL DOWN AND LOCKED INDICATION. LANDED NORMALLY. INSTALLED NEW LANDING GEAR DOWNLOCK SWITCH AND CANNON PLUG PER MM 32-60-00. 2L74 4F RT4A25 19950217004601995021700460WP 1995 2 17 UPS802379 119950215A53115772958 FRAME DOUG DC8 DC871F 302199DWP FS 1580 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND BELT FRAME HAS 2 INCH LONG CRACK AT FS 1580, LONGERON 21L. INSTALLED REPAIR IAW SRM 53-2-0. 2L74 4F RT4A25 19950217004611995021700461WP 1995 2 17 UPS802380 119950215A54005804007509 ANGLE DOUG DC8 DC871F 302199DWP NR 1 PYLON CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND NR 1 PYLON OUTBOARD ATTACHMENT ANGLE CRACKED. INSTALLED REPAIR IAW SRM 51-1-20D. 2L74 4F RT4A25 19950217004621995021700462WP 1995 2 17 UPS802381 119950215A57300637075T6 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND 3 INCH LONG CRACK ON RT WING LEADING EDGE SKIN AT STA XFS 182.5 LOWER SURFACE. INSTALLED REPAIR IAW SRM 57-2-0. 2L74 4F RT4A25 19950217004631995021700463WP 1995 2 17 UPS802382 119950215A531156121613 FRAME DOUG DC8 DC871F 302199DWP FS 1890 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON AFT SIDE OF FRAME WEB, LONGERON 36, FS 1890. INSTALLED REPAIR IAW UPS EO DC8-53-1320. 2L74 4F RT4A25 19950217004641995021700464WP 1995 2 17 UPS802383 119950215A53200407075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 20 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND FLIGHT DECK SUBFLOOR FINGER DOUBLER HAS MODERATE CORROSION AT FS 20, LBL 62. INSTALLED REPAIR IAW SRM 51-1-21. 2L74 4F RT4A25 19950217004651995021700465WP 1995 2 17 UPS802384 119950215A5320BAC150643 ANGLE DOUG DC8 DC871F 302199DWP FS 70 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND A/C COMPT. FS 70, LONGERON 31L ATTACH ANGLE HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-21. 2L74 4F RT4A25 19950217004661995021700466WP 1995 2 17 UPS802385 119950215A575337759061 TRACKS DOUG DC8 DC871F 302199DWP RT TE FLAPS CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 340. INSTALLED REPAIR IAW MM 27-51-03. 2L74 4F RT4A25 19950217004671995021700467WP 1995 2 17 UPS802386 119950215A575337759071 TRACKS DOUG DC8 DC871F 302199DWP RT TE FLAPS CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 410. INSTALLED REPAIR IAW MM 27-51-03. 2L74 4F RT4A25 19950217004681995021700468WP 1995 2 17 UPS802387 119950215A575337759032 TRACKS DOUG DC8 DC871F 302199DWP RT TE FLAPS CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK MAINTENANCE FOUND HEAVY CORROSION ON RT FLAP TRACKS STA XRS 3. INSTALLED REPAIR IAW MM 27-51-03. 2L74 4F RT4A25 19950217004691995021700469NE 1995 2 17 UPS802389 219950213A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE NR 1 FLAME OUT A IPXAO OTHER X ENGINE FLAMEOUT NRNOT REPORTED 1 SO01729UP 46029 PILOT REPORTED NR 1 ENGINE FLAMED OUT AT F/L .350 OAT -59 DEGREES CELSIUS, DURING CYCLING OF NR 1 CROSSFEED. ACCOMPLISHED FUEL TANK TRANSFER CHECKS - ALL NORMAL. INSPECTED INLET/TAIL PIPE NR 1 ENGINE - NO DAMAGE NOTED. REPLACED NR 1 ENGINE FUEL FILTER PRECAUTIONARY - NO FOREIGN MATERIAL. RAN ENGINE - NO LEAKS. NORMAL OPERATION. 2L74 4F4 FRT4A25 E2GL 19950217004711995021700471CE 1995 2 17 95ZZZZ45 119950121A3260444EN496 SQUAT SWITCH BEECH 1900 1900C 1154161CE RT MLG INOP A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0187GL UC87 GRI - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURN BACK. PILOT REPORTED THAT WITH GEAR RETRACTED, THE GEAR HANDLE LIGHT STAYED ON AND THE WARNING HORN WILL NOT SILENCE. MAINTENANCE REPLACED THE RT MLG SQUAT SWITCH. THE GEAR WARNING SYSTEMS WORKED SATISFACTORILY DURING SEVERAL GEAR SWINGS. (Z) 2L72 4T RTA24CE 19950217004721995021700472CE 1995 2 17 95ZZZZ46 119950118A32301013841377 GEAR CONTROL BEECH 1900 1900C 1154161CE C/P CONSOLE INOP A GLBAK NONE P NO WARNING INDICATION TOTAKEOFF 1 CE0198GL 1760 UC98 MSP - PILOT REPORTED THAT THE LANDING GEAR UNSAFE LIGHTS DO NOT LIGHT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL. A GEAR SWING WAS SUCCESSFUL. (Z) 2L72 4T RTA24CE 19950217004741995021700474CE 1995 2 17 95ZZZZ48 119950120A712012991003279 ENGINE TRUSS BEECH 1900 1900C 1154161CE INBD TUBE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0167UE 2797 300 UC67 ESC - DURING SCHEDULED TRUSS INSPECTION, THE RT TRUSS WAS FOUND CHAFED BEYOND LIMITS IN THE AREA OF THE FREON COMPRESSOR. THE TRUSS WAS REPLACED WITH SERVICEABLE TRUSS. (Z) 2L72 4T RTA24CE 19950217004751995021700475CE 1995 2 17 95ZZZZ49 119950120A712012991003279 ENGINE TRUSS BEECH 1900 1900C 1154161CE INBD TUBE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0167UE 2797 300 UC67 ESC - DURING SCHEDULED TRUSS INSPECTION, THE RT TRUSS WAS FOUND CHAFED BEYOND LIMITS IN THE AREA OF THE FREON COMPRESSOR. THE TRUSS WAS REPLACED WITH SERVICEABLE TRUSS. (Z) 2L72 4T RTA24CE 19950217004761995021700476EU 1995 2 17 95ZZZZ51 119950122A28201379305A150 FUEL LINE BAG JETSTMJETSTM3201 1500217EU RT FUEL CELL DAMAGED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN PX NO WARNING INDICATION ENGINE FLAMEOUT CRCRUISE 1 SO03943AE 943 FLT 4409 - BNA - PILOT REPORT AT 17,000 FEET DURING CRUISE THE RT ENIGNE SHUT ITSELF DOWN WITH NO WARNINGS. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. AN INSPECTION OF THE RT FUEL SYSTEM REVEALED THAT THERE WAS NO CONTAMINATION. THE FUEL LINE FROM THE BOOST PUMP TO THE ISOLATION VALVE WAS FOUND TO BE PARTIALLY COLLAPSED. AS A PRECAUTION THE FUEL SHUT OFF AND ISOLATION VALVES WERE ALSO CHANGED. (Z) 2L72 4T RTA56EU 19950217004771995021700477WP 1995 2 17 95ZZZZ52 219950114A73208691691 P2-T2 SENSOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENG FAILED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO03940AE 940 P66148C FLT 4580 - BNA - ON CLIMB-OUT THE LEFT ENGINE TQ AND FUEL FLOW SURGED. THE LEFT ENGINE WAS SHUT DOWN, THE CREW DECLARED AND EMERGENCY AND LANDED BACK AT BNA WITHOUT INCIDENT. REPLACED LEFT ENGINE P2-T2 SENSOR. (Z) 2L72 4T4 TRTA56EU E4WE 19950217004781995021700478WP 1995 2 17 95ZZZZ53 119950118A3610 CLAMP DOUG DC8 DC8F54 3021926WP NR 3 ENGINE LOOSE A TC8AO OTHER N FALSE WARNING CLCLIMB 1 GL23802CK 45679 FALSE FIRE WARNING NR 3 ENGINE DURING CLIMB WARNING CEASED WHEN ENGINE BLEED AIR TURNED OFF ALL OTHER PARAMETERS NORMAL. RETORQUED CLAMPS ON REGULATOR VALVE DUCTING. CHECKS GOOD ON ENGINE RUN UP. FIRE WARNING SYSTEM INTEGRITY OK. 2L74 4F 4A25 19950217004791995021700479WP 1995 2 17 95ZZZZ54 119950117A32461542511 MAIN WHEEL BENDIX DOUG DC8 DC8F55 3021928WP LT MLG BROKEN A TC8AO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 GL23808CK771 H2732 45817 NR 2 MAIN TIRE MISSING AFTER LANDING YIP. FOUND OUTBOARD FLANGE BROKEN OFF. REPLACED NR 2 AND NR 1 MAIN WHEEL ASSY. 2L74 4F 4A25 19950217004801995021700480NM 1995 2 17 95ZZZZ55 119950127A3350900835A EEL BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19324AS 20264 AFT CABIN EMERGENCY EXIT LIGHT SIGN OVER AFT STAIR DOOR BLINKING. REPLACED BATTERY PACK IAW MM 33-50. 2L73 4F A3WE 19950217004811995021700481EA 1995 2 17 95ZZZZ56 219950126A7260 CHIP LIGHT BEECH 99 C99 1154006CE PWA PT6 PT6A27 52043EA RT ENGINE ILLUMINATED A GUUAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19130GP U222 FLT 473 - MIA-GHB - NORTH OF BIMINI, RIGHT CHIP DETECTOR LIGHT ILLUMINATED, PERFORMED PRECAUTIONARY ENGINE SHUTDOWN, DECLARED AN EMERGENCY AND RETURNED TO MIA. INSPECTED NR 1 CHIP DETECTOR FOUND ONE SMALL SLIVER, CLEANED CHIP DETECTOR. INSPECTED NR 1 OIL FILTER NO DEFICIENCIES NOTE, CHANGED OIL FILTER. RAN AIRCRAFT FOR 20 MINUTES NO CHIP DETECTOR ANNUNCIATION AIRCRAFT RELEASED. (Z) 1L72 3T4 T A14CE E4EA 19950217004821995021700482CE 1995 2 17 95ZZZZ57 119950123A3260 SWITCH BEECH 99 C99 1154006CE LANDING GEAR OUT OF ADJUST A GUUAK NONE N FALSE WARNING DEDESCENT 1 SO19131GP U225 FLT 5325 - PBI-MIA - GEAR WARNING HORN SOUNDS TOO HIGH. ADJUSTED POWER LEVER SWITCH. AIRCRAFT TEST FLOWN TO MARK PEDESTAL FOR SWITCH ADJUSTMENT. PERFORMED GEAR RETRACTION TEST WITH SATISFACTORY RESULTS. AIRCRAFT RETURNED TO SERVICE. (Z) 1L72 3T A14CE 19950217004831995021700483CE 1995 2 17 95ZZZZ58 119950117A3260 WARNING LIGHT BEECH 99 C99 1154006CE LANDING GEAR MALFUNCTIONED A GUUAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO19131GP U225 FLT NR 492 - DAB-MIA - NO GEAR WARNING RED LIGHT WHEN TORQUE REDUCED TO ZERO. PERFORMED GEAR RETRACTION TEST AFTER ADJUSTING BOTH THROTTLE SWITCHES WITH SATISFACTORY RESULTS. AIRCRAFT RETURNED TO SERVICE. (Z) 1L72 3T A14CE 19950217004841995021700484EA 1995 2 17 95ZZZZ59 219950126A72003037347CL14 SHROUD SEGMENT PWA 3040361 BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE BROKEN A GPPAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. AY FLAME/FIRE ENGINE STOPPAGE DEDESCENT 1 CE09170123065 UC11 32038 GJT TRAINING FLIGHT, WHILE ADVANCING THE POWER LEVERS DURING STALL RECOVERY NOTICED FLAMES EMITTING FROM THE RT ENGINE EXHAUST STACKS. ENGINE WAS SHUTDOWN, PROP WAS FEATHERED ANDFIRE BOTTLE WAS DISCHARGED. AIRCRAFT LANDED SAFELY IN GJT. INITIAL INSPECTION BY GP EXPRESS MAINTENANCE INDICATES THAT A SHROUD SEGMENT DISLODGED INTO THE CT DISK ASSY, CAUSING BLADE FAILURE WITH CONSQUENT DAMAGE DOWN STREAM TO THE PT DISKS THEREFORE EXITING THROUGH THE EXHAUST. CT BLADE FAILURECAUSED AN IMBALANCE WHICH ALSO DAMAGED THE NR 2 BRG ANDLABRYNTH SEAL. THE GAS GENERATOR, THE HOT SECTION AND THEPOWER SECTION WAS REPLACED WITH SERVICEABLE UNITS. ACFTWAS RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E4EA 19950217004881995021700488WP 1995 2 17 CAL950008 119950103A3222 STRUT DOUG DC9 DC932 3022066WP NOSE GEAR PRESSURE LOW A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0969523 47520 FLT NR 1708 - MDW - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT WAS RETURNED TO MDW. MAINTENANCE CHECKED THE GROUND/AIR SENSE RIG AND FOUND IT TO BE WITHIN LIMITS. THE NOSE GEAR STRUT PRESSURE WAS FOUND LOW. THE NOSE STRUT WAS SERVICED AND THE GEAR OPERATED NORMALLY DURING GEAR SWING. (Z) 2L72 4F A6WE 19950217004891995021700489WP 1995 2 17 CAL950014 119950106A3260MS250081 SWITCH DOUG DC9 DC982 3022082WP LANDING GEAR INOPERATIVE A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0983873 49121 FLT NR 0356 - EWR - ALL THREE GEAR RED UNSAFE LIGHTS WERE OBSERVED TO BE ILLUMINATED DURING CLIMB-OUT THROUGH 18,000 FEET. CYCLING THE GEAR DID NOT HELP. THE CREW VERIFIED THAT IT WAS AN INDICATION PROBLEM ONLY, AND THAT ALL GEAR WERE UP AND LOCKED. THE FLIGHT WAS CONTINUED AND WHEN GEAR WAS EXTENDED ON APPROACH TO EWR ALL GEAR DOWN INDICATIONS WERE NORMAL. MAINTENANCE FOUND THE LANDING GEAR HANDLE SWITCH AT FAULT. THE SWITCH WAS REMOVED AND REPLACED AND ALL INDICATIONS WERE NORMAL. (Z) 2L72 4F A6WE 19950217004901995021700490WP 1995 2 17 CAL950015 119950107A3230 GRD SHIFT MECH DOUG DC9 DC982 3022082WP NLG FROZEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914890 49114 FLT NR 0262 - CLE - THE THREE GEAR RED UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED LEAVING CLE. THE GEAR WAS EXTENDED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR AND GROUND SHIFT MECHANISM FROZEN WITH ICE. THE FROZEN AREA WAS DE-ICED. THE GEAR OPERATED NORMALLY DURING A TEST FLIGHT. (Z) 2L72 4F A6WE 19950217004911995021700491 1995 2 17 CAL950038 419950116A2565113319DG SLIDE DOUG DC9 DC932 3022066WP GALLEY DOOR LOW PRESSURE A CALAK NONE O OTHER ININSP/MAINT 1 SW0912507217441783 47788 FLT NR 1524 - MSY - THE R-1 GALLEY DOOR SLIDE WAS FOUND WITH LOW PRESSURE DURING A PREFLIGHT CHECK. THE R-1 GALLEY DOOR SLIDE WAS REMOVED AND REPLACED. (Z) 2L72 4F A6WE 19950217004921995021700492WP 1995 2 17 CAL950042 119950116A215020495054 ACM DOUG DC9 DC982 3022082WP LEFT FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW0914840189642057 49580 FLT NR 0206 - CLE - A FLIGHT ATTENDANT NOTICED HAZE IN THE CABIN ON APPROACH TO CLE JUST BEFORE TOUCHDOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT AIR CYCLE MACHINE BLOWING OIL. THE LEFT AIR CYCLE MACHINE WAS REMOVED AND REPLACED AND THE WATER SEPARATOR BAG WAS REPLACED. THE APU WAS RUN WITH PACK OPERATING AND OPERATION CHECKED GOOD WITH NO HAZE OBSERVED. (Z) 2L72 4F A6WE 19950217004931995021700493WP 1995 2 17 CAL950047 119950111A5350 CABLES DOUG DC9 DC982 3022082WP TAIL CONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0918835 49439 HOU - THE TAILCONE RELEASE PULL TEST FAILED AT ALL THREE POSITIONS. THE TAILCONE RELEASE CABLES WERE RIGGED PER MM 53-53-00, PARAGRAPH 3A, PAGE 502, CONFIGURATION 1. (Z) 2L72 4F A6WE 19950217004941995021700494NM 1995 2 17 CAL950049 119950118A2820 CIRCUIT BREAKER BOEING727 727232 1384082NM NR 1 FUEL SYSTEMTRIPPED A CALAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 SW0917789 20643 FLT NR 1911 - IAH - THE AIRCRAFT WAS RETURNED TO IAH AFTER TAKEOFF DUE TO UNEVEN FUEL BURN FROM FUEL TANKS. THE NR 1 TANK WAS BURNING FASTER THAN OTHERS. FUEL WAS DUMPED TO CONTROL BALANCE. MAINTENANCE FOUND THAT THE NR 1 FUEL TRANSFER VALVE WAS NOT WORKING DUE TO A POPPED CIRCUIT BREAKER. THE CIRCUIT BREAKER WAS RESET. THE ENGINES WERE RUN FOR SEVERAL MINUTES AND FUEL BURN WAS NORMAL. (Z) 2L73 4F A3WE 19950217004951995021700495NE 1995 2 17 CAL950053 219950120A7230K102G07 COMPRESSOR VANE AIRBUS300 A300B4203 3930306EU GE CF6 CF650* 30018NE NR 1 ENGINE WORN A CALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW091496622240 117 528204 FLT NR 0648 - IAH - TAKEOFF WAS ABORTED AT APPROXIMATELY 80 KNOTS AFTER THE NR 1 ENGINE STALLED, ACCOMPANIED BY A LOUD BANG. THE NR 1 ENGINE WAS REMOVED AND REPLACED. S/D THE PRIMARY CAUSE OF FAILURE WAS DUE TO A HIGH PRESSURE COMPRESSOR STAGE 8 VANE LIBERATION, PROBABLY CAUSED BY WEAR OF THE AFT DOVETAIL LIP. (M) 2L72 4F4 F A35EU E23EA 19950217004961995021700496NE 1995 2 17 CAL950058 219950121A7200 ENGINE BOEING747 747243B 1384830NM PWA JT9 JT9D7A 52054NE NR 1 FAILED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW093302147584 20520 685815 FLT NR 0907 - HNL - THE AIRCRAFT WAS RETURNED TO HNL WITH THE NR 1 ENGINE SHUT DOWN. THE NR 1 ENGINE WILL BE REMOVED AND REPLACED. (Z) 2L74 4F4 F A20WE E20EA 19950217004971995021700497WP 1995 2 17 HAL95014 119950127A2421976J2526 GENERATOR DOUG DC9 DC951 3022051WP NR 1 ENG FAILED A HALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 WP13603DC PM915 47784 FLT NR 526 - CREW REPORTED LOSS OF LEFT AC BUS AND CABIN PRESSURE CONTROLLER. CABIN RATE INDICATOR ALWAYS SHOWED CLIMB 1,500 FEET PLUS. ALSO, LEFT GENERATOR WOULD NOT RESET. REMOVED AND REPLACED LEFT GENERATOR. SECURITY AND OPERATION CHECK GOOD. (Z) 2L72 4F A6WE 19950217004981995021700498NE 1995 2 17 IXKA9500001 219950117A732060136921 NUT BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 3 ENG MISSING A AIXKAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 EA25354PA 20624 FLT 11, INBOUND TO ATL, NR 3 ENGINE WAS SHUTDOWN IN FLIGHT, WOULD NOT RESPOND TO THROTTLE MOVEMENT, WENT TO MAX POWER INDICATIONS. REMOVED AND REPLACED NR 3 ENGINE FUEL CONT PER MM 73-21-2, WHEN RIGGING FOUND NUT MISSING AND CRANK OFF SHAFT AT PYLON CONNECTION POINT. REINSTALLED CRANK AND INSTALLED NUT. TRIMMED NR 3 ENGINE IAW 71-00. OPS CHECKED OK. LEAK CHECK OK. (Z) 2L73 4F4 F A3WE E2EA 19950217004991995021700499NM 1995 2 17 IXKA9500003 119950118A5210MS166241037 RETAINER RING BOEING727 727225 1384077NM FWD ENTRY DOOR MISSING A IXKAK NONE O OTHER TXTAXI/GRND HDL 1 EA258883Z 21580 AT ARRIVAL IN TPA, FLT 59, UNABLE TO OPEN L1 FWD ENTRY DOOR. FOUND RETAINER RING MISSING ON UPPER DOOR GUIDE ARM LOCK PIN REINSTALLED UPPER DOOR GUIDE ARM LOCK PIN AND RING RETAINER PER MM 52-10. OPS CHECKED OK. (Z) 2L73 4F A3WE 19950217005011995021700501NE 1995 2 17 IXXA199504 219950125A7200 ENGINE DOUG DC8 DC871 302199AWP GE CFM56 CFM562C1 13802NE NR 4 MALFUNCTIONED A IXXAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 GL23823BX 46064 692195 AT 25,000 FEET, DURING DESCENT INTO OAK, THE NR 4 ENGINE THROTTLE WAS ADVANCED FROM IDLE TO 2500 PPH FUEL FLOW, AND THE ENGINE FLAMED OUT. THE ENGINE SPONTANEOUSLY RELIT AND MAINTAINED STEADY OPERATION FOR A SHORT PERIOD OF TIME. EGT AND FUEL FLOW THEN BEGAN TO FLUCTUATE. THE ENGINE WAS THEN PRECAUTIONARILY SHUT DOWN. INSPECTION ON THE GROUND IN OAK REVEALED NO ABNORMALITIES. THE MAIN FUEL FILTER WAS PRECAUTIONARILY CHANGED AND THE ENGINE OPERATIONALLY CHECKED IAW THE ATI JRH. ENGINE OPERATION WAS NORMAL. THE MAIN FUEL FILTER WAS NOT FOUND TO BE CONTAMINATED. (Z) 2L74 4F4 F 4A25 E2GL 19950217005021995021700502 1995 2 17 TSAA9534026 419950129A34217926357002 ADI BOEING737 7372M6C 1384708NM NR 2 FAILED A TSAAO OTHER O OTHER CLCLIMB 1 WP13805AL 21809 FLT 201 - HNL-LIH - FIRST OFFICER ATTITUDE FAILED JUST AFTER TAKEOFF. RETURN TO HNL. REMOVED AND REPLACED NR 2 ADI. GROUND OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950217005031995021700503EU 1995 2 17 VTZA95039 119950201A24221B3501B13 INVERTER BAG JETSTMJETSTM3201 1500217EU FUSELAGE FAILED A VTZAK NONE H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27475UE 850 FLT NR 6381 - DURING CRUISE FROM IAD TO CMH AT 1330 HOURS ON 2-01-95, THE INVERTER FAILED IN FLIGHT. AIRCRAFT LANDED AT CMH WITH NO FURTHER INCIDENTS. CONTRACT MAINTENANCE REPLACED THE INVERTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950217005041995021700504SO 1995 2 17 WTAA950061 119950121A3350101103 EEL WIRE EMB 120 EMB120RT SO CABIN BROKEN A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17281UE 120092 SFO - ROW 8 EMERGENCY EXIT LIGHT P/N 1011103 FAILS TO ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE AT LIGHT ASSEMBLY. EMERGENCY EXIT LIGHT OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950217005051995021700505SO 1995 2 17 WTAA950064 119950129A2120 AIR DISTR EMB 120 EMB120RT SO COCKPIT ODOR A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP17284UE 120145 RNO - ELECTRICAL BURNING ODOR REPORTED IN COCKPIT. MAINTENANCE INSPECTED ELECTRICAL PANELS IN COCKPIT AND AVIONICS AND SERVICE BAYS. NO DEFECTS NOTED. UNABLE TO DUPLICATE ELECTRICAL BURNING ODOR. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950217005061995021700506SO 1995 2 17 WTAA950067 119950130A3260922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A WTAAK NONE N FALSE WARNING CLCLIMB 1 WP17284UE 120145 SFO - RIGHT MAIN LANDING GEAR RED INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACTION. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE ADJUSTED RT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR. LANDING GEAR OPERATION AND POSITION INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950217005071995021700507EU 1995 2 17 95ZZZX733 119950112A3411 PITOT TUBE ISRAEL1121 1121B 0142010EU RT SYSTEM PLUGGED A UBIAK NONE O OTHER NRNOT REPORTED 1 SW09122ST 122 COPILOT EXPERIENCED ERRONEOUS AIRSPEED INDICATION. RIGHT PITOT SYSTEM CHECKED, FOUND RESTRICTION. PURGED SYSTEM WITH DRY COMPRESSED AIR. FOREIGN SUBSTANCE EXITED PITOT TUBE. SUBSTANCE WAS WHITE AND POWDERY. POSSIBLY WAX OR POLISH. 2M72 4J A2SW 19950217005091995021700509CE 1995 2 17 95ZZZX735 119950119A29101240016C40734 LINE BEECH 99 99 1154002CE NLG RETRACT LEAK A ATIMAO OTHER K FLUID LOSS CRCRUISE 1 NM07299GL U102 AT AROUND 8:20 A.M. FLIGHT 296 FROM BILLINGS TO MISSOULA, HYDRAULIC POWER PACK CIRCUIT BREAKER TRIPPED AND LANDING GEAR EXTENDED PREMATURELY. THE PILOT USED HIS HAND PUMP TO LOCK THE GEAR DOWN AND DECLARED AN EMERGENCY LANDING. THE PLANE LANDED WITHOUT INCIDENT AT MISSOULA MT AIRPORT. THE HYDRAULIC LANDING GEAR SYSTEM WAS INSPECTED AND A LEAK IN THE NOSE GEAR RETRACT LINE WAS FOUND. THIS LEAK CAUSED THE HYDRAULIC POWER PACK TO RUN CONTINUOUSLY TO HOLD THE GEAR IN THE UP POSITION. WHEN THE PUMP OVERHEATED IT CAUSED THE CIRCUIT BREAKER TO TRIP AND THE GEAR TO FREE FALL. THE HYDRAULIC LINE WAS REPLACED AND THE GEAR CYCLED. NO OTHER DEFECTS NOTED. 1L72 3T A14CE 19950217005141995021700514CE 1995 2 17 95ZZZX740 119950130A275050000084 CONTROL CABLE CESSNA402 402B 207590PCE LT FLAP FRAYED A OEZAK NONE O OTHER ININSP/MAINT 1 WP19154TT 402B0314 DURING RIGGING CHECK OF FLAP SYSTEM, MECHANIC FOUND RIGHT FLAP CABLE FRAYED. UPON FURTHER INSPECTION, LEFT CABLE FOUND FRAYED ALSO, BUT COULD NOT BE FOUND FRAYED WHILE CABLE WAS INSTALLED. 1L72 3O A7CE 19950217005151995021700515CE 1995 2 17 95ZZZX741 119950130A275050000083 CONTROL CABLE CESSNA402 402B 207590PCE RT FLAP FRAYED A OEZAK NONE O OTHER ININSP/MAINT 1 WP19154TT 402B0314 DURING RIGGING CHECK OF FLAP SYSTEM, MECHANIC FOUND RIGHT FLAP CABLE FRAYED. UPON FURTHER INSPECTION, LEFT CABLE FOUND FRAYED ALSO, BUT COULD NOT BE FOUND FRAYED WHILE CABLE WAS INSTALLED. 1L72 3O A7CE 19950217005251995021700525EA 1995 2 17 95ZZZX751 219950111A7314025323101 PUMP BEECH 90 B90 1152912CE PWA PT6 PT6A20 52043EA ENGINE FUEL FAILED A DBQAO OTHER Y ENGINE STOPPAGE APAPPROACH 1 GL1314VK 1748 3812 LJ365 PCE21630 DURING APROACH TO LANDING, RIGHT ENGINE LOST POWER. INSPECTION AND REMOVAL OF THE FUEL PUMP REVEALED A FAILURE OCCURRED INTERNALLY IN THE FUEL PUMP ASSY. THIS ALSO CAUSED THE ENGINE-TO-PUMP DRIVE COUPLING TO FAIL. FAILURE OF THE ENGINE DRIVEN PUMP AND DRIVE DISABLED THE FUEL CONTROL UNIT. THIS CAUSED THE ENGINE TO FLAME OUT. 1L72 3T3 T 3A20 E4EA 19950217005281995021700528EU 1995 2 17 95ZZZX754 119950104A493028616 LINE BRAERO1000 BAE1251000 1500287EU APU FUEL BURNED A DXTAK NONE O OTHER ININSP/MAINT 1 GL07541QS151 259041 FOUND DURING PRE-FLIGHT - APU HOSE (FUEL FEED) WAS BURNED THROUGH THE PLASTIC SHIELD, AND THROUGH THE RUBBER INSULATION HALF WAY. CAUSE: LEFT ENGINE BLEED AIR AT MIXER VALVE IS BURNING THROUGH THE APU FUEL FEED LINE. NEED LINE ROUTED TO A DIFFERENT PATH. 2L72 4F RTA3EU 19950217005291995021700529EU 1995 2 17 95ZZZX755 119950109A493028616 LINE BRAERO1000 BAE1251000 1500287EU APU FUEL BURNED A DXTAK NONE O OTHER ININSP/MAINT 1 GL07539QS728 259039 APU FUEL FEED LINE FOUND BURNED ON INSPECTION. OUTSIDE FUEL SLEEVEING HAD A HOLE BURNED THROUGH. FIRE RETARDANT SLEEVE HAD A HOLE BURNED INTO THE RED RUBBER COVERING. WAS NOT BURNED TO FUEL HOSE AT THIS TIME. 2L72 4F RTA3EU 19950217005301995021700530EU 1995 2 17 95ZZZX756 119950109A493028616 HOSE BRAERO1000 BAE1251000 1500287EU APU FUEL BURNED A DXTAK NONE O OTHER ININSP/MAINT 1 GL07535QS938 259035 FUEL FEED LINE FOR APU FOUND DURING INSPECTION. OUTSIDE FUEL SLEEVEING HAD 2 HOLES BURNED THROUGH. FIRE RETARDANT SLEEVE HAD ONE HOLE BURNED IN RED RUBBER COVERING. WAS NOT BURNED TO HOSE AT THIS TIME. 2L72 4F RTA3EU 19950217005521995021700552SW 1995 2 17 95ZZZX777 119950127A7714AG34 TACH GENERATOR SWRNGNSA226 SA226TC 8780404SW LT ENGINE LOOSE DRIVE A BDHAK NONE O OTHER ININSP/MAINT 1 GL15229AM 224 036825 TC305 CREW REPORTED LEFT ENGINE WOULD NOT START. NO RPM INDICATION, IGNITION, OR FUEL FLOW WAS OBSERVED ON START. INSPECTION OF THE SYSTEM FOUND THE TACH GENERATOR SHAFT DISENGAGED FROM THE WINDINGS. THE TACH GENERATOR WAS REPLACED AND THE AIRCRAFT WAS RELEASED. 2L72 4T RTA8SW 19950217005531995021700553 1995 2 17 95ZZZX778 419950117A3425066304600 HSI SWRNGNSA226 SA226TC 8780404SW LT COCKPIT INOPERATIVE A BDHAO OTHER O OTHER NRNOT REPORTED 1 GL15328BA 11161 TC253 CAPTAIN'S COMPASS SYTEM SHOWED HEADING FLAG IN-FLIGHT AND STOPPED TURNING. INSPECTED COMPASS SYSTEM AND FOUND HEADING INDICATOR INOP. REMOVED AND REPLACED HEADING INDICATOR AND SWING COMPASS, CHECKED OKAY, AIRCRAFT RELEASED. 1L72 4T A8SW 19950217005541995021700554SW 1995 2 17 95ZZZX779 119950110A79311105122N OIL PRESS WIRE SWRNGNSA226 SA226TC 8780404SW LT ENGINE BROKEN A BDHAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15327BA TC249 CREW REPORTED THE LEFT OIL PRESSURE INDICATOR WENT TO ZERO WITH ALL OTHER INDICATIONS NORMAL. INSPECTION OF THE SYSTEM FOUND A BROKEN WIRE AT THE OIL PRESSURE TRANSMITTER CONNECTOR. THE WIRE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED. 1L72 4T A8SW 19950217005551995021700555SW 1995 2 17 95ZZZX780 119950106A2613 OVERHEAT WIRE SWRNGNSA226 SA226TC 8780404SW LT WING CHAFED A BDHAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 GL15327BA TC249 LEFT WING OVERHEAT ANNUNCIATOR LIGHT FLICKERED AFTER TAKEOFF. LEFT ENGINE BLEED, GENERATOR WAS SHUT OFF, AND AIRCRAFT RETURNED TO AIRPORT IAW AFM. SYSTEM WAS INSPECTED AND FOUND WIRE NR 6801DD-22 CHAFED. REPLACED WIRE AND PERFORMED OPERATIONAL CHECK OKAY. 1L72 4T A8SW 19950217005581995021700558SW 1995 2 17 95ZZZX783 119950131A612031039391 ELBOW SWRNGNSA227 SA227AC 8780603SW LT PROP GOV CRACKED A CHQAOE OTHER ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 EA233115K AC586 CMH - PILOT REPORTED WHILE ON FINAL APPROACH TO CMH, LEFT ENGINE LOW OIL PRESSURE LGHT ILLUMINATED ALONG WITH A LOSS OF OIL PRESSURE ON LEFT GAUGE. THE LEFT ENGINE WAS SHUT DOWN. UPON INSPECTION BY MAINTENANCE, THE 90 DEGREE ELBOW ON THE LEFT PROP GOVERNOR WAS FOUND CRACKED IN HALF. THE ELBOW WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. 1L72 4T A8SW 19950217005591995021700559 1995 2 17 95ZZZX784 419950130A22104030952902 YAW DAMP COUPLER BOEING737 737201 1384454NM AUTOPILOT MALFUNCTIONED A F3LAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED APAPPROACH 1 NM03207AU61488 86082422 19423 BZN - UPON APPROACH, AIRCRAFT STARTED TO YAW LEFT AND RIGHT AFTER SELECTING 40 DEGREE FLAP SETTING. PILOT TURNED OFF YAW DAMPER AND YAW PROBLEM WAS CORRECTED. PLACARDED PER MEL 22-3. ON JANUARY 31, 1995, MAINTENANCE REPLACED YAW DAMPER COUPLER AND THE RUDDER PCU. SYSTEM CHECKED OKAY. REFERENCE CONTROL NR F3LA95004. 2L72 4F A16WE 19950217005601995021700560NM 1995 2 17 95ZZZX785 119950125A33506013211 EEL BATT CHARGER BOEING737 737201 1384454NM CABIN INOPERATIVE A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03217US58742 20215 OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR F3LA95002. 2L72 4F A16WE 19950217005611995021700561SO 1995 2 17 ASOA95002 119950121A3230 PROX SWITCH EMB 120 EMB120RT SO RT MLG FAILED A ASOAO OTHER J WARNING INDICATION APAPPROACH 1 SO11215AS 120010 ATL/LYH - FLT 7248 - UPON SELECTING GEAR DOWN TO LAND, LANDING GEAR WOULD NOT EXTEND. HAD TO USE ELECTRIC OVERRIDE TO EXTEND GEAR SUCCESSFULLY. CONTINUED APPROACH AND LANDED SAFELY AND WITHOUT INCIDENT. A/C WAS FERRIED LYH-ATL GEAR DOWN. IN ATL, REPLACED RIGHT MAIN A-DOWNLOCK PROXIMITY SWITCH. (X) 2L72 4T RTA31SO 19950217005621995021700562EU 1995 2 17 ASOA95003 119950123A77143039242 NH SENSOR AEROSPATR72 ATR72212 EU RIGHT ENGINE DEFECTIVE A AASOAO OTHER N FALSE WARNING CLCLIMB 1 SO11636AS 375 DFW/HOU - FLT 7719 - DURING CLIMB PASSING THROUGH 4500 FEET, THE NR 2 ENGINE SURGED WITH TORQUE SHOWING IN EXCESS OF 110 PERCENT THEN DROPPING TO 10 PERCENT WITH POWER LEVER IN NOTCH CLIMB MODE. NP NOTED AT 86 PERCENT. RETURNED FLIGHT TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. DOWN-LOADED FDAU AND FOUND THE EXCEEDENCES CALLED FOR A MANDATORY BORESCOPE OF THE ENGINE WITHIN THE NEXT TEN FLIGHT HOURS. ALSO REPLACED THE NR 1 NH SENSOR DUE TO FAULT CODES THAT WERE FOUND. OPERATIONAL CHECKS GOOD ON GROUND RUN. THE BORESCOPE WAS PERFORMED ON THE ENGINE IN TXK THE EVENING OF JANUARY 24, 1995, AND NO DEFECTS WERE NOTED. (X) 2H72 4T RTA53EU 19950217005631995021700563SO 1995 2 17 C2XA95IA023 119950207A553012015374002 ANGLE EMB 120 EMB120RT SO FIN TO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0957734 120199 IAH - DURING C-CHECK INSPECTION, FOUND RT FIN TO FUSELAGE ATTACH (DRAG) ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED RT ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 8,443.7. CYCLES - 12,794. (X) 2L72 4T RTA31SO 19950217005641995021700564NM 1995 2 17 F3LA95002 119950125A33506104781 EEL BATTERY PACK BOEING737 737201 1384454NM CABIN INOPERATIVE A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03217US58742 20215 OMA - DURING AN FAA RAMP AUDIT, FAA REPORTED RT WING INTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BOTH LAMPS, BATTERY PACK AND BATTERY CHARGER AND CHECKED OKAY. REFERENCE CONTROL NR 95ZZZX785. (X) 2L72 4F A16WE 19950217005651995021700565NM 1995 2 17 F3LA95003 119950130A3350 EEL CONNECTOR BOEING737 737201 1384454NM CABIN BROKEN A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03217US58776 20215 FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. PLACARDED PER MEL 33-14. UPON ARRIVAL IN DEN, MAINTENANCE REPAIRED CANNON PLUG AND CHECKED OKAY. (X) 2L72 4F A16WE 19950217005661995021700566NM 1995 2 17 F3LA95004 119950130A272065448614 PCU BOEING737 737201 1384454NM RUDDER MALFUNCTIONED A AF3LAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED APAPPROACH 1 NM03207AU61488 1076A 19423 BZN - UPON APPROACH, AIRCRAFT STARTED TO YAW LEFT AND RIGHT AFTER SELECTING 40 DEGREE FLAP SETTING. PILOT TURNED OFF YAW DAMPER AND YAW PROBLEM WAS CORRECTED. PLACARDED PER MEL 22-3. ON JANUARY 31, 1995, MAINTENANCE REPLACED YAW DAMPER COUPLER AND THE RUDDER PCU. SYSTEM CHECKED OKAY. REFERENCE CONTROL NR 95ZZZX784. (X) 2L72 4F A16WE 19950217005671995021700567NM 1995 2 17 F3LA95005 119950206A33506104781 EEL BATTERY PACK BOEING737 737201 1384454NM CABIN DISCHARGED A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03207AU61530 19423 DEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LT AFT BATTERY PACK AND CHECKED OKAY. (X) 2L72 4F A16WE 19950217005681995021700568SW 1995 2 17 LOSA9509 119950202A29132781009015 HYD POWER PACK AIRIGHT 188005 FRCHLDSA227 SA227DC 3377521SW WHEELWELL INOPERATIVE A LOSAO OTHER J WARNING INDICATION CRCRUISE 1 WP23453LA1383 1159 DC852B CREW REPORTED THAT WITH AIRCRAFT IN CRUISE FLIGHT, HYDRAULIC PRESSURE INDICATED 2350 PSI (ABOVE RED LINE). AIRCRAFT LANDED LAS WITHOUT INCIDENT. AIRCRAFT FERRIED TO ONT FOR MAINTENANCE. MAINTENANCE REPLACED HYDRAULIC POWER PACK DUE TO A PRESSURE RELIEF FUNCTION INOPERATIVE PER MM 29-10-10. ALL FUNCTIONAL AND LEAK CHECKS NORMAL. AIRCRAFT WAS TEST FLOWN. RESULTS: SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 1L72 4T RTA18SW 19950217005761995021700576WP 1995 2 17 95ZZZX793 219950209A7261 ENGINE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP RT ENG LOST OIL PRESS A CWQAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL05886CS10174757 35023 74191 ENGINE LOST OIL PRESSURE, SECURED ENGINE AND RETURNED TO BUR. MAINTENANCE FOUND OIL FILTER BYPASS BUTTON DEPLOYED. APPROXIMATELY 1 PINT OF OIL AND METAL DRAINED FROM RESERVOIR, UNDER INVESTIGATION. 2L72 4F4 F A10CE E6WE 19950217005781995021700578SW 1995 2 17 95ZZZX795 119950123A3213 STRUT SWRNGNSA226 SA226TC 8780404SW RT MLG REQUIRED SERVICEA BDHAO OTHER J WARNING INDICATION APAPPROACH 1 GL15329BA TC238 RIGHT MLG WOULD NOT EXTEND. THE AIRCRAFT MADE AN EMERGENCY LANDING WITH GEAR UP PROCEDURES. RIGHT MAIN STRUT SLIGHTLY COMPRESSED WHEN THE LANDING GEAR WAS RETRACTED. THIS, IN TURN, CAUSED THE AFT GEAR DOOR STOPS (MOUNTED ON THE GEAR SCISSORS) TO SLIP OFF GEAR DOOR STOP BLOCKS BINDING THE GEAR WHEN SELECTED DOWN. 1L72 4T A8SW 19950217005991995021700599SW 1995 2 17 95ZZZX702 119950118A32305439331 UPLOCK SHAFT SWRNGNSA227 SA227AC 8780603SW NLG BINDING A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15426MA AC645 DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR MALA954247, AND CONTROL NR 95ZZZX703. (X) 1L72 4T A8SW 19950217006001995021700600SW 1995 2 17 95ZZZX703 119950118A32302752000087 PICK-UP ROLLER SWRNGNSA227 SA227AC 8780603SW NLG BINDING A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15426MA AC645 DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR MALA954247, AND CONTROL NR 95ZZZX702. (X) 1L72 4T A8SW 19950217006011995021700601NM 1995 2 17 95ZZZX704 119950120A323082410315001 LIGHT SOCKET DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15817MA 249 MSP - FLT 3318 - ON APPROACH, LT MAIN GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. ALSO, THE ALTERNATE NOSE GEAR GREEN LIGHT WAS INOP. MAINTENANCE REPLACED LT UPLOCK ACTUATOR, PN 10800-113, WHICH HAD AN INTERNAL FAULT, AND THE LANDING GEAR EMERGENCY DOWNLOCK INDICATOR LIGHT SOCKET, PN 82410315-001, THAT HAD AN INTERNAL FAULT WITH THE SOCKET. SYSTEMS OPERATED SATISFACTORILY DURING A TEST FLIGHT. REFERENCE CONTROL NR MALA954267. 2H72 4T RTA13NM 19950217006021995021700602CE 1995 2 17 95ZZZX705 119950122A261017AS1015 ROTARY SWITCH BEECH 1900 1900C 1154161CE RT SUB-PANEL DIRTY A GPPAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 CE09125GP UB6 CDR - FLT 2092 - DEPARTING, HAD THE RT FIRE T-HANDLE ILLUMINATE. FLIGHT CREW SHUT DOWN AND FEATHERED THE ENGINE AND DISCHARGED THE FIRE BOTTLE. AIRCRAFT RETURNED SAFELY TO CDR. MAINTENANCE INSPECTED ENGINE AND NO SIGN OF FIRE WAS NOTED. ENGINE WAS CLEARED AND AIRCRAFT WAS FERRIED TO DEN. IN DEN, GP EXPRESS MAINTENANCE TIGHTENED AND CLEANED THE CONTACTS ON THE FIRE DETECTION ROTARY TEST SWITCH. SYSTEM WAS CHECKED WITH NO DISCREPANCIES NOTED. ENGINE FIRE BOTTLE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 19950217006031995021700603EU 1995 2 17 95ZZZX706 119950111A242131342001 AC GENERATOR SAAB SF340 340B 7860101EU RT PGB FAILED A PLGAAE UNSCHED LANDING ENGINE SHUTDOWN JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NE05354BE1755 1348 340B246 JFK - AFTER DEPARTURE, RT A/C GENERATOR FAILURE LIGHT ILLUMINATED WITH A SHOWER OF SPARKS EMANATING FROM THE RT A/C GENERATOR EXHAUST DUCT. THE CREW SECURED THE ENGINE AND RETURNED TO JFK, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE GENERATOR, QED PAD AND MOUNT CLAMP. VISUALLY INSPECTED NACELLE WITH NO DEFECTS FOUND. PERFORMED REQUIRED GROUND RUNS AND RETURNED A/C TO SERVICE. 2L72 4T RTA52EU 19950217006041995021700604EU 1995 2 17 95ZZZX707 119950121A242131342001 AC GENERATOR LUCAS SAAB SF340 SF340A 7850100EU RT ENGINE FAILED A CHQAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA23125CH 1815 92054 340A125 AIRCRAFT RETURNED TO AIRPORT DUE TO THE FAILURE OF THE RIGHT A.C. GENERATOR. THE RIGHT A.C. GENERATOR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. 2L72 4T RTA52EU 19950217006051995021700605SW 1995 2 17 95ZZZX708 119950119A30603E20421 BRUSH BLOCK BFGOODRICH SWRNGNSA227 SA227AC 8780603SW LT PROP WORN A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA233115M AC588 AIRCRAFT RETURNED TO AIRPORT DUE TO LT PROP HEAT WENT INOPERATIVE. MAINTENANCE INSPECTED AND FOUND RT BRUSH BLOCK AT FAULT. THE BRUSH BLOCK WAS REPLACED AND A FUNCTION CHECK OF THE SYSTEM WAS PERFORMED WTIH ALL INDICATIONS NORMAL. 1L72 4T A8SW 19950217006061995021700606EU 1995 2 17 95ZZZX709 119950120A243523080031 STARTER/GEN LUCAS SAAB SF340 340B 7860101EU LT ENGINE FAILED A CHQAO OTHER O OTHER ININSP/MAINT 1 EA23252CH 1143 4673 340B252 THE LEFT ENGINE WAS REPORTED THAT IT WOULD NOT ROTATE ON START ATTEMPT. MAINTENANCE REPLACED LEFT STARTER/GENERATOR AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. 2L72 4T RTA52EU 19950217006071995021700607EU 1995 2 17 95ZZZX710 119950123A36107769022 TEMP CONTROL VLV SAAB SF340 340B 7860101EU LEFT FAILED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23224TH 860743 340B224 AFTER TAKEOFF, LEFT DUCT OVER-TEMP LIGHT CAME ON. THE AIRCRAFT RETURNED TO FIELD. THROUGH TROUBLESHOOTING, DETERMINED LEFT DUAL TEMP CONTROL VALVE WAS THE PROBLEM. THE VALVE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. 2L72 4T RTA52EU 19950217006081995021700608NM 1995 2 17 95ZZZX711 119950106A5241 SKIN BOEING727 727231 1384079NM FWD GALLEY DOOR CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0512304 19561 MCI - DURING CHECK 'C', FOUND .3750 INCH CRACK IN FORWARD GALLEY DOOR OUTER SKIN, FROM FASTENER TO EDGE OF DOOR CUT-OUT, LOWER AFT CORNER. INSTALLED REPAIR PER SSRM 53-30-206, PAGE 201 AND PAGE 204. AIRCRAFT TOTAL TIME: 66,258 HOURS; 45,561 CYCLES. 2L73 4F A3WE 19950217006091995021700609NM 1995 2 17 95ZZZX712 119950105A7120 CASTING BOEING727 727231 1384079NM NR 1 ENG MT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554332 20310 MCI - DURING CHECK C-2D, FOUND .75 INCH CRACK IN TOP INBOARD CORNER OF NR 1 ENGINE AFT ENGINE MOUNT CASTING. REPAIRED BY INSTALLING DOUBLERS PER BOEING DWG 65C34994. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES. 2L73 4F A3WE 19950217006111995021700611WP 1995 2 17 95ZZZX714 119950129A3260 CONNECTOR DOUG DC9 DC931 3022065WP LT MLG DOWNLOCKDIRTY A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05992Z 47095 CVG - FLT 698 - DURING APPROACH, LT MLG UNSAFE LIGHT REMAINED ON AFTER LANDING GEAR EXTENSION. CYCLED LANDING GEAR AND VISUALLY CHECKED LOCK. CLEANED ELECTRICAL CONNECTOR ON DOWNLOCK SWITCH. LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL. CHECK OP-15 - 4-17-94 - MCI. 2L72 4F A6WE 19950217006121995021700612WP 1995 2 17 95ZZZX715 119950128A3260H146 SWITCH DOUG DC9 DC931 3022065WP LT MLG UPLOCK MALFUNCTION A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05992Z 47095 STL - FLT 106 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LT MLG UNSAFE LIGHT REMAINED ON. RECYCLED LANDING GEAR AND VISUALLY CHECKED LOCK. REPLACED LT MLG UPLOCK SWITCH, MFG P/N H14-6. LANDING GEAR POSITION AND WARNING SYTEM CHECKED NORMAL. CHECK OP-15 - 4-17-94 - MCI. 2L72 4F A6WE 19950217006131995021700613WP 1995 2 17 95ZZZX716 119950127A3020 ANTI-ICE DOUG DC9 DC982 3022082WP ENGINE CABIN SMOKE A TWAAOH OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE05905TW 49157 STL - FLT 269 - DURING APPROACH WITH ANTI-ICE ON, A LIGHT SMOKE APPEARED IN CABIN. TURNED ANTI-ICE OFF, SMOKE DISSIPATED. PERFORMED ENGINE HIGH POWER RUN, NO SMOKE OR ODOR DETECTED, AND LEAK CHECKED DUCTING. CHECK C-1D - 9-14-94 - MCI. 2L72 4F A6WE 19950217006141995021700614WP 1995 2 17 95ZZZX717 119950110A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1665-1685 LT CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0541016 193B1060 DURING CHECK C-6C, FOUND CORROSION AT STR 44, STA 1665 TO STA 1685, LEFT SIDE FUSELAGE. INSTALLED STRINGER SPLICE PER SRM 53-13-00, PAGE 806E, 201. AIRCRAFT TOTAL TIME: 58,443 HOURS; 21,909 CYCLES. 2L73 4F A23WE 19950217006151995021700615WP 1995 2 17 95ZZZX718 119950110A5330 SKIN LKHEED1011 10113851 5265010WP FS 679 STR 37-38CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0541016 193B1060 DURING CHECK C-6C, FOUND CORROSION CRACK ON LEFT SIDE OF FUSELAGE STA 679, BETWEEN STR 37 AND STR 38. INSTALLED REPAIR DOUBLER PER SSRM 53-30-02, PAGE 201. AIRCRAFT TOTAL TIME: 58,443 HOURS; 21,909 CYCLES. 2L73 4F A23WE 19950217006161995021700616EU 1995 2 17 C2XA95IA019 119950131A7120S5421020001100 MOUNT AEROSPATR42 ATR42320 8680930EU LT NACELLE CHAFED A AC2XAK NONE O OTHER ININSP/MAINT 1 SW0931807 078 IAH - DURING C-CHECK INSPECTION, LEFT ENGINE NACELLE AFT INBOARD TRUSS MOUNT MIDDLE TUBE WAS FOUND CHAFED BEYOND LIMITS. MAINTEANACE REMOVED AND REPLACED AFFECTED MOUNT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. REF ATR 42 NTM SSI NR 54-11-11. (TT 13791.2). (TC 18138). (X) 2H72 4T RTA53EU 19950217006171995021700617EU 1995 2 17 C2XA95IA020 119950131A5320S5337122925000 SUPPORT AEROSPATR42 ATR42320 8680930EU FWD FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0931807 078 IAH- DURING C-CHECK INSPECTION, FRAME SUPPORT FOR THE MAIN CARGO DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TT 13791.2). (TC 18138). (X) 2H72 4T RTA53EU 19950217006181995021700618EU 1995 2 17 C2XA95IA021 119950131A2710MS276434 BEARING AEROSPATR42 ATR42320 8680930EU RIGHT WING RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0931807 078 IAH - DURING C-CHECK INSPECTION, RT AILERON CONTROL BEARING FOUND BLEEDING RUST. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING AND AIRCRAFT WAS RETURNED TO SERVICE. (TT 13791.1) (TC 18138). (X) 2H72 4T RTA53EU 19950217006191995021700619SW 1995 2 17 MALA954247 119950118A323054530321 UPLOCK ROLLER SWRNGNSA227 SA227AC 8780603SW NLG BINDING A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15426MA AC645 DTW - FLT 3149 - ON APPROACH, NOSE GEAR WOULD NOT EXTEND. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ROLLER, PN 5453032-1, UPLOCK ROLLER SHAFT, PN 543033-1, AND THE NOSE LANDING GEAR DOOR PICK-UP ROLLER, PN 27-52000-087, THAT WERE FOUND BINDING. SYSTEM OPERATED SATISFACTORILY. (REFERENCE CONTROL NR 95ZZZX702, AND CONTROL NR 95ZZZX703. (X) 1L72 4T A8SW 19950217006201995021700620NM 1995 2 17 MALA954264 119950120A30607826893 BRUSH BLOCK DHAV DHC8 DHC8102 2809003NM RIGHT PROP WORN A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15846MA 344 MSP - FLT 3116 - AFTER TAKEOFF, RT TRU CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RT PROP DE-ICE BRUSH BLOCK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950217006211995021700621EU 1995 2 17 MALA954265 119950120A2824911433M4 CROSS-FLOW VALVE FOKKERF27 F27MK200 4990620EU RIGHT FAILED A AMALAK NONE O OTHER CRCRUISE 1 GL15278MA 10280 MSP - FLT 3283 - IN CRUISE FLIGHT, CROSS-FEED BINDS WHEN MOVED FROM OFF TO OPEN. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED RT CROSS-FLOW VALVE. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T A817 19950217006221995021700622SW 1995 2 17 MALA954266 119950119A32303219014001 BELLCRANK SPRING SWRNGNSA227 SA227AC 8780603SW RT MLG WEAK A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15446MA AC693 DTW - FLT 3445 - ON APPROACH, RT MAIN GEAR DID NOT EXTEND. THE CREW CYCLED GEAR AND PROBLEM REMAINED. THE CREW PERFORMED AN EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED RT MLG BELLCRANK SPRING. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950217006231995021700623NM 1995 2 17 MALA954267 119950120A323010800113 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15817MA 249 MSP - FLT 3318 - ON APPROACH, LT MAIN GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. ALSO, THE ALTERNATE NOSE GEAR GREEN LIGHT WAS INOP. MAINTENANCE REPLACED LT UPLOCK ACTUATOR, PN 10800-113, WHICH HAD AN INTERNAL FAULT, AND THE LANDING GEAR EMERGENCY DOWNLOCK INDICATOR LIGHT SOCKET, PN 82410315-001, THAT HAD AN INTERNAL FAULT WITH THE SOCKET. SYSTEMS OPERATED SATISFACTORILY DURING A TEST FLIGHT. REFERENCE CONTROL NR 95ZZZX704. (X) 2H72 4T RTA13NM 19950217006241995021700624SW 1995 2 17 MALA954268 119950118A26122719301001 TADPOLE SEAL SWRNGNSA227 SA227AC 8780603SW LEFT ENGINE WORN A MALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15428MA AC646 YNG - FLT 3055 - ON CLIMB-OUT, LT ENGINE FIRE ANNUNCIATOR PANEL LIGHT, AND LT ENGINE SUB-PANEL FIRE LIGHT ILLUMINATED. THE CREW SHUT DOWN THE LT ENGINE AND DIVERTED TO CLE. MAINTENANCE REPLACED TADPOLE SEAL. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950217006251995021700625EU 1995 2 17 MALA954269 119950120A2824 CROSS-FEED VALVE FOKKERF27 F27MK200 4990620EU FUEL SYSTEM MALFUNCTIONED A MALAK NONE O OTHER CRCRUISE 1 GL15278MA 10280 MSP - FLT 3246 - IN CRUISE FLIGHT, THE CROSS-FEED VALVE WAS STUCK IN THE OFF POSITION. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE INSPECTED THE CROSS-FLOW VALVES AND PULLEYS. NO DEFECTS WERE NOTED. (X) 2H72 4T A817 19950217006261995021700626WP 1995 2 17 MALA954270 219950121A723031070511 COMPRESSOR SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE LEAKING A MALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15434MA AC717 MSP - FLT 3306 - IN CRUISE FLIGHT, CREW NOTED AN UNPLEASANT SMELL WHILE THE AIRCRAFT WAS PRESSURIZED. THE AIRCRAFT CONTINUED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE COMPRESSOR SEAL. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T4 T A8SW E4WE 19950217006271995021700627NM 1995 2 17 MALA954273 119950125A3260 LIGHT BULBS DHAV DHC8 DHC8102 2809003NM NLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15859MA 361 DTW - FLT 3131 - ON APPROACH, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE DURING GEAR EXTENSION. THE GEAR WAS VERIFIED TO BE DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED BOTH NOSE GEAR DOWN LIGHT BULBS. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950217006281995021700628SW 1995 2 17 MALA954275 119950125A5270MS250081 SWITCH SWRNGNSA227 SA227AC 8780603SW CARGO DOOR OUT OF ADJUST A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15158MC AC762B MSP - FLT 3292 - IN CRUISE FLGIHT, CARGO DOOR WARNING AND FO'S SIDE PANEL LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE ADJUSTED LOWER AFT WARNING SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950217006291995021700629SW 1995 2 17 MALA954276 119950126A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15439MA AC722 DTW - FLT 3182 - ON APPROACH, LT MAIN INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED GEAR AND THE PROBLEM RECURRED. BOTH TIMES THE DOWN AND LOCKED INDICATION WAS RECEIVED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED AND LUBED GEAR SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950217006301995021700630WP 1995 2 17 ORJA95005 119950106A335000105606003 EEL WIRE HARNESS DOUG DC9 DC983 3022083WP CABIN FAILED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 EMERGENCY FLOOR EXIT LIGHTING INOP ON RIGHT SIDE ROWS 11-15. FOUND BAD WIRE HARNESS. INSTALLED NEW HARNESS, OPS GOOD. (X) 2L72 4F RTA6WE 19950217006321995021700632NM 1995 2 17 95ZZZX720 119950108A7711611429 PT7 TUBE BOEING737 7372P6 NM NR 2 ENGINE FRACTURED A A6XAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO132FOR 21612 NR 2 ENGINE EPR INDICATION APPEARS LOW DURING GROUND RUN-UP. INVESTIGATION FOUND PT7 TUBE ASSEMBLY WAS BROKEN ON B-NUT. REPLACED TUBE ASSEMBLY PER PRATT AND WHITNEY MM 78-22-00. 2L72 4F RTA16WE 19950217006331995021700633NM 1995 2 17 95ZZZX721 119950119A5713 STRINGER BOEING727 727212 138407GNM LT WS 629 S9 CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13296AS 21459 TNN - DURING 1/4D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACKS WERE FOUND ON OUTER WING UPPER Z-STRINGER AT RIB ATTACHMENT HOLE IN THE FOLLOWING LOCATIONS. (A) RT WING S-9 AND WS 629. (B) LT WING S-9 AND WS 629. (C) LT WING S-10 AND WS 629. THE CRACKS WERE STOP DRILLED AND REPAIRED PER EA5762-01050, PART 3, FIGURE B. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0724683, 0724684, AND 0724698 (SEQ. NR. 06048, 05053, AND 05054). REF CONTROL MZZA9505, AND NR 94ZZZX722. 2L73 4F A3WE 19950217006341995021700634NM 1995 2 17 95ZZZX722 119950119A5713 STRINGER BOEING727 727212 138407GNM LT WS 629 S10 CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13296AS 21459 TNN - DURING 1/4D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACKS WERE FOUND ON OUTER WING UPPER Z-STRINGER AT RIB ATTACHMENT HOLE IN THE FOLLOWING LOCATIONS. (A) RT WING S-9 AND WS 629. (B) LT WING S-9 AND WS 629. (C) LT WING S-10 AND WS 629. THE CRACKS WERE STOP DRILLED AND REPAIRED PER EA5762-01050, PART 3, FIGURE B. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0724683, 0724684, AND 0724698 (SEQ. NR. 06048, 05053, AND 05054). REF CONTROL MZZA9505, AND NR 94ZZZX721. 2L73 4F A3WE 19950217006351995021700635EU 1995 2 17 95ZZZX723 119950123A27307227279541 ELEV CONTL CABLE SAAB SF340 340B 7860101EU FS 389.0 CHAFED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 BNA - DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY WAS 0.163, MEASURED DIAMETER AT CHAFED AREA IS 0.140. REMOVED AND REPLACED BOTH PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950217006361995021700636EU 1995 2 17 95ZZZX724 119950123A27307227279542 ELEV CONTL CABLE SAAB SF340 340B 7860101EU FS 389.0 CHAFED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 BNA - DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY WAS 0.163, MEASURED DIAMETER AT CHAFED AREA IS 0.140. REMOVED AND REPLACED BOTH PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950217006371995021700637EU 1995 2 17 95ZZZX725 119950103A2730 BOLTS SAAB SF340 340B 7860101EU ELEVATOR LOOSE A NVEAK NONE O OTHER ININSP/MAINT 1 SO03273AE 340B273 BNA - DURING ROUTINE C-CHECK INSPECTION AT OUR CONTRACT MX FACILITY IN BNA, THE ELEVATOR HINGE BOLTS WERE FOUND LOOSE, AND/OR NOT TORQUED PROPERLY. SIDE PLAY IN THE BEARINGS WERE INVESTIGATED, AND LOOSE BOLTS WERE FOUND TO BE THE CAUSE, NOT THE BEARINGS THEMSELVES. THIS PROBLEM HAS BEEN FOUND ON SEVERAL ACFT PREVIOUSLY, WITH CORRECTIVE ACTIONS BEING RETORQUE OF THE ELEVATOR BOLTS. PRESENTLY, THERE ARE NO CURRENT SERVICE BULLETINS OR AD'S FOR THIS PROBLEM. 2L72 4T RTA52EU 19950217006441995021700644CE 1995 2 17 95ZZZX732 119950118A2751MS252531 LIMIT SWITCH BEECH 1900 1900D 1154162CE CONSOLE OUT OF ADJUST A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0196UX 1414 UE96 ISN - AFTER DEPARTURE, CREW ELECTED AN AIR TURN-BACK WHEN THE GEAR HORN WOULD NOT SILENCE WITH GEAR IN UP POSITION. MAINTENANCE ADJUSTED THE FLAP LIMIT SWITCH. THE OPS CHECK WAS GOOD. 2L72 4T RTA24CE 19950217006471995021700647NM 1995 2 17 AALA950023 119950107A3350 EEL WIRE BOEING757 757223 1384957NM R2 DOOR PINCHED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07696AN 26976 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT EXIT MARKER AT R2 DOOR INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHT WIRE FOUND PINCHED AT R2 DOOR EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATIONAL. (X) 2L72 4F RTA2NM 19950217006501995021700650NM 1995 2 17 CKSA95001 119950110A5320 ANGLE BOEING727 727223 1384074NM FS 870 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL236816 19491 OSC - CRACK IN ANGLE AND WEB FORWARD OF APU LT GEAR WELL, FORWARD OF APU. REPLACED ANGLE AND REPAIRED WEB IAW 727 SRM CHAPTER 51, FIGURE 51-40-2, FIGURE 1. REPLACED APU FORWARD WEB VERTICAL STIFFENER, STA 870, LT GEAR WELL, FORWARD OF APU. (X) 2L73 4F A3WE 19950217006511995021700651WP 1995 2 17 CKSA95003 119950118A323045973405503 UPLATCH DOUG DC8 DC8F55 3021928WP LT MLG OUT OF ADJUST A CKSAO OTHER J WARNING INDICATION CLCLIMB 1 GL2329549 45803 KPHL/KYIP - FLT 61605 - RED LANDING GEAR UNSAFE LIGHT COMES ON DURING UPLATCH CHECK. RE-CYCLE OF GEAR NO HELP. WARNING TEST SWITCH ON F/E PANEL IDENTIFIES LIGHT SOURCE AS LT MAIN GEAR. LT DOOR OKAY. RIGGED MAIN LANDING UPLATCH MECHANISM IAW DC-8 MM, CHAPTER 32-6-2, PERFORMED LANDING GEAR EXTENSION AND RETRACTION TEST IAW DC-8 MM 32-3-0. OPS NORMAL AT THIS TIME. (X) 2L74 4F 4A25 19950217006521995021700652WP 1995 2 17 HAL95013 119950122A3350P4020049 BATTERY SUPPLY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 47662 HNL - ITEM FROM M-71 LOG PAGE NR 140721-1, THE AFT EMERGENCY FLOOR LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BOTH BATTERY PACKS. THE OPERATIONAL CHECK WAS GOOD. (X) 2L72 4F A6WE 19950217006531995021700653NE 1995 2 17 M3HA95001 219950111A7320 ECU LIGHT AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 ENGINE ILLUMINATED A M3HACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP13983MA 308 HNL - FLT 221 - ECU1 FAULT LIGHT ILLUMINATED ONCE DURING TO POWER ADDITION AND ONCE FOLLOWING ENGINE START. REST OKAY ON BOTH OCCASIONS. CHECKED ELECTRICAL CONNECTORS TO ECU1. CHECKED GOOD. ENGINE RAN OKAY AT IDLE AND POWER RUN FOR TAKEOFF. FOUND TO BE GOOD IAW JIC 72-00-00-ERU-10040-001. (X) 2H72 4T4 TRTA53EU E20NE 19950217006541995021700654EU 1995 2 17 M3HA95002 119950114A33503011206 EEL AEROSPATR42 ATR42320 8680930EU CABIN FAILED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13984MA495 757 337 HNL - DURING 'EXTERIOR LIGHT CHECKS', A MECHANIC NOTICED THE RIGHT FORWARD EXTERIOR EMERGENCY FLOOD LIGHT WOULD NOT TEST. IT WAS DETERMINED THERE WAS A SHORT CIRCUIT WITHIN THE LIGHT ASSEMBLY WHICH ALSO CAUSED THE POWER SUPPLY TO FAULT. REPLACED EMERGENCY SUPPLY UNIT (FIN10WL) WITH SERVICEABLE POWER UNIT AND REPLACED EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD IAW JIC 33-51-24-RAI-10000-001 AND JIC 33-50-00-OPT-10000-001. PART TOTAL CYCLES 831 HOURS. (X) 2H72 4T RTA53EU 19950217006551995021700655EU 1995 2 17 M3HA95003 119950115A33503011185 EEL POWER SUPPLY AEROSPATR42 ATR42320 8680930EU CABIN MALFUNCTIONED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13984MA7 337 HNL - DURING 'EXTERIOR LIGHT CHECKS, THE RIGHT FORWARD EXTERIOR EMERGENCY FLOOD LIGHT DID NOT ILLUMINATE WITHOUT AIRCRAFT POWER. IT WAS DETERMINED THE ORIGINAL 'FACTORY INSTALLED' POWER SUPPLY UNIT WAS OF THE WRONG PART NUMBER. REPLACED EMERGENCY POWER SUPPLY UNIT (FIN10WL) WITH SERVICEABLE EMERGENCY SUPPLY POWER UNIT IAW JIC 33-51-21-RAI-10000-002. OPERATIONALLY CHECKS GOOD JIC 33-50-00-OPT-10000-001. PART TOTAL CYCLES, 9 HOURS. (X) 2H72 4T RTA53EU 19950217006571995021700657NM 1995 2 17 MZZA9503 119950121A3297 WIRE BOEING727 727212 138407GNM NLG FAILED A MZZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13309AS 21947 SPN - FLT 921 - AIR RETURNED TO SPN DUE TO NOSE GEAR RED LIGHT WOULD NOT GO OUT. FOUND PIN AND WIRE SPLICE BAD. REPINNED AND SPLICED IN NEW WIRE ON C/P OF UPPER NOSE GEAR CONTROL SWITCH. OPS CHECK NORMAL. (X) 2L73 4F A3WE 19950217006581995021700658NM 1995 2 17 MZZA9504 119950119A5713 STRINGER BOEING727 727212 138407GNM WS 656.5 CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13296AS 21459 TNN- DURING 1/4D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON LT OUTER WING UPPER VENT STRINGER AT RIB ATTACHMENT HOLE, S-13 AND WS 656.5. THE CRACK WAS STOP DRILLED AND REPAIRED PER EA5762-01050, PART 3, FIGURE 3. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0724682 (SEQ NR 05052). (X) 2L73 4F A3WE 19950217006591995021700659NM 1995 2 17 MZZA9505 119950119A5713 STRINGER BOEING727 727212 138407GNM RT WS 629 CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13296AS 21459 TNN - DURING 1/4D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACKS WERE FOUND ON OUTER WING UPPER Z-STRINGER AT RIB ATTACHMENT HOLE IN THE FOLLOWING LOCATIONS. (A) RT WING S-9 AND WS 629. (B) LT WING S-9 AND WS 629. (C) LT WING S-10 AND WS 629. THE CRACKS WERE STOP DRILLED AND REPAIRED PER EA5762-01050, PART 3, FIGURE B. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0724683, 0724684, AND 0724698 (SEQ. NR. 06048, 05053, AND 05054). REF CONTROL NR 94ZZZX721, AND NR 94ZZZX722. (X) 2L73 4F A3WE 19950217006601995021700660WP 1995 2 17 ORJA95004 119950108A3350 EEL DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11750RA 49777 EMEREGENCY LIGHT FIXTURE AFT STAIRWELL MIDDLE INOP. RELAMPED. OPS CHECK NORMAL. (X) 2L72 4F RTA6WE 19950217006611995021700661WP 1995 2 17 95ZZZZ60 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-933 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 32 HAS CORROSION FROM STATION 901 TO 933. REMOVED AND REPLACED STRINGER SECTION IAW 51-10-05. (Z) 2L73 4F A23WE 19950217006621995021700662WP 1995 2 17 95ZZZZ61 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 869-901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 32 HAS CORROSION FROM STATION 869 TO 901. REMOVED AND REPLACED STRINGER SECTION IAW 51-10-05. 2L73 4F A23WE 19950217006631995021700663WP 1995 2 17 95ZZZZ62 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 849-869 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL CORROSION, STRINGER NR 31 HAS CORROSION FROM STATION 849 TO 869. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05. 2L73 4F A23WE 19950217006641995021700664WP 1995 2 17 95ZZZZ63 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 943-985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 32 HAS CORROSION FROM STATION 943 TO 985. REMOVED AND REPLACED STRINGER SECTION IAW 51-10-05 AND INSTALLED SPLICE PLATES IAW SRM 51-13-00. 2L73 4F A23WE 19950217006651995021700665WP 1995 2 17 95ZZZZ64 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-923 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 33 HAS CORROSION FROM STATION 901 TO 923. REMOVED AND REPLACED STRINGER SECITON IAW SRM 51-10-05. 2L73 4F A23WE 19950217006661995021700666WP 1995 2 17 95ZZZZ65 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 869-901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER 34 HAS CORROSION FROM STATION 869 TO 901. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05 AND INSTALLED SPLICE PLATES IAW SRM 51-13-00. 2L73 4F A23WE 19950217006671995021700667WP 1995 2 17 95ZZZZ66 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 901-943 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 34 HAS CORROSION FROM STATION 901 TO 943. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05. 2L73 4F A23WE 19950217006681995021700668WP 1995 2 17 95ZZZZ67 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 809-849 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 34 HAS CORROSION FROM STATION 809 TO 849. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-15. 2L73 4F A23WE 19950217006691995021700669WP 1995 2 17 95ZZZZ68 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 923-985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 33 HAS CORROSION FROM STATION 923 TO 985. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05. 2L73 4F A23WE 19950217006701995021700670WP 1995 2 17 95ZZZZ69 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 943-985 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 34 HAS CORROSION FROM STATION 943 TO 985. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05. 2L73 4F A23WE 19950217006711995021700671WP 1995 2 17 95ZZZZ70 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 849-869 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 32 HAS CORROSION FROM STATION 849 TO 869. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05. 2L73 4F A23WE 19950217006721995021700672WP 1995 2 17 95ZZZZ71 119950202A5313 STRINGER LKHEED1011 10113851 5265010WP FS 809-829 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, STRINGER NR 32 HAS CORROSION FROM STATION 809 TO 829. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-10-05 AND INSTALLED SPLICE PLATES IAW SRM 51-13-00. 2L73 4F A23WE 19950217006731995021700673WP 1995 2 17 95ZZZZ72 119950201A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING L/E UPPER SURFACE PANEL AFT OF INBOARD SLOT HAS BULGING CORROSION AND CRACKS AROUND FASTENER HEADS. REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950217006741995021700674WP 1995 2 17 95ZZZZ73 119950202A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING L/E UPPER SURFACE PANEL AFT OF OUTBOARD SLOT HAS CORROSION AROUND SCREW HEADS. REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950217006751995021700675WP 1995 2 17 95ZZZZ74 119950201A5730 SKIN DOUG DC8 DC862 3021970WP WS 223.5-257.5 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING LEADING EDGE STATION 223.5 TO 257.5 HAS BULGING CORROSION. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950217006761995021700676WP 1995 2 17 95ZZZZ75 119950201A5730 SKIN DOUG DC8 DC862 3021970WP RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING NR 3 AUX FUEL TANK HAS BULGING CORROSION AROUND SCREW HEADS. REMOVED CORRODED SECTION AND REPAIRED PER SRM 57-2-1. 2L74 4F 4A25 19950217006771995021700677WP 1995 2 17 95ZZZZ76 119950201A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING L/E UPPER SURFACE PANEL OUTBOARD OF NR 4 PYLON HAS CORROSION AROUND SCREW HEADS. REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-1-20. 2L74 4F 4A25 19950217006781995021700678WP 1995 2 17 95ZZZZ77 119950201A5320 CIRCUMFERENTIAL DOUG DC8 DC862 3021970WP FS 1240 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT AT STATION 1240 CIRCUMFERENTIAL HAS CORROSION ON UPPER AND LOWER FLANGES FROM LONG 35 LT TO 34 RT. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0. 2L74 4F 4A25 19950217006791995021700679WP 1995 2 17 95ZZZZ78 119950202A5730 SKIN DOUG DC8 DC862 3021970WP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING L/E JUST OUTBOARD OF NR 4 ENGINE PYLON HAS BULGING CORROSION AROUND SCREW HEADS AND SKIN CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950217006801995021700680WP 1995 2 17 95ZZZZ79 119950202A5320 CIRCUMFERENTIAL DOUG DC8 DC862 3021970WP FS 1340 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT CIRCUMFERENTIAL LOWER FLANGE AND VERTICAL SIDEWALL SUPPORT ARE CORRODED AT STATION 1340 BETWEEN LONGERONS 27R AND 26L. REMOVED CORRODED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 54-4-20. 2L74 4F 4A25 19950217006811995021700681WP 1995 2 17 95ZZZZ80 119950202A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2. 2L74 4F 4A25 19950217006821995021700682WP 1995 2 17 95ZZZZ81 119950202A5320 CIRCUMFERENTIAL DOUG DC8 DC862 3021970WP FS 1140 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT CIRCUMFERRENTIAL END IS CORRODED AT STA 1140, LONGERON 33 CENTER OF DOORWAY. CLEANED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-8. 2L74 4F 4A25 19950217006831995021700683WP 1995 2 17 95ZZZZ82 119950202A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE SKIN ABOVE WINDOW 19L HAS CORROSION AROUND FASTENER HEAD. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-1-8 AND RIAA DRAWING NR RCH D85310-5015. 2L74 4F 4A25 19950217006841995021700684WP 1995 2 17 95ZZZZ83 119950202A5753 SKIN DOUG DC8 DC862 3021970WP TE FLAP SLOT CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LEADING EDGE PANEL FOR SLOT DOORS NR 2, NR 3 AND NR 4 HAS INTERGRANULAR CORROSION AT INBD END. REMOVED CORROSION FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-1. 2L74 4F 4A25 19950217006851995021700685WP 1995 2 17 95ZZZZ84 119950131A335060030431 EEL PWR SUPPLY DOUG DC9 DC915F 3022037WP CABIN FAILED A RYNAK NONE L NO TEST ININSP/MAINT 1 CE07567PC 47153 DURING PRE-FLIGHT IN BHM, FOUND THE EMERGENCY EXIT LIGHTS TO BE INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY. 2L72 4F A6WE 19950217006861995021700686NM 1995 2 17 95ZZZZ85 119950118A783065578183 TR SWITCH BOEING727 72723 1384004NM NR 3 ENG INOP A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01717DH 19389 NR 3 THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL, APPROXIMATELY 1.6 EPR. TAKEOFF REJECTED. REMOVED AND REPLACED NR 3 THRUST REVERSER SWITCH. GROUND RAN TO 1.93 EPR. OPS CHECKS GOOD IAW DHL B727 M 78-30-91. 2L73 4F A3WE 19950217006871995021700687WP 1995 2 17 95ZZZZ86 119950125A3244 TIRE DOUG DC8 DC873F 302199FWP NR 1 MLG BLOWN A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH 888 2304 46125 NR 1 TIRE BLEW ON LANDING. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY, P/N 2614112. 2L74 4F RT4A25 19950217006881995021700688WP 1995 2 17 95ZZZZ87 119950125A3244 TIRE DOUG DC8 DC873F 302199FWP NR 2 MLG BLOWN A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH 46125 NR 2 TIRE BLEW ON LANDING. REMOVED AND REPLACED MAIN WHEEL ASSY, P/N 26014112, IAW MM 32-40-1. OPS CHECK OK. 2L74 4F RT4A25 19950217006901995021700690SO 1995 2 17 RAAAE995001 119950113A33508621014 EEL BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (Z) 2L74 4T 4A22 19950217006911995021700691SO 1995 2 17 RAAAE995002 119950113A33508621014 EEL BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 RT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (Z) 2L74 4T 4A22 19950217006921995021700692SO 1995 2 17 RAAAE995003 119950113A3350862114 EEL BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (Z) 2L74 4T 4A22 19950217006931995021700693 1995 2 17 TWRA9508 419950128A22102590624 AP MODE SELECTOR BOEING747 747131 1384881NM COCKPIT MALFUNCTIONED A ATWRAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 EA15608FF 19672 DURING FLIGHT A/C BANKED RIGHT THEN HARD LEFT, AUTOPILOT DISENGAGED THEN REENGAGED SEVERAL MINUTES LATER AND AIRCRAFT FLEW NORMAL. PERFORMED CABLE RUN INSPECTION FROM CONTROL COLUMN TO INBOARD AILERON, CHECKED CABLE TENSIONS, FOUND CABLE AA PULLEY FROM LEFT CENTRAL CONTROL ACTUATOR WITH WORN BEARING. PRESSURIZED AIRCRAFT ADDED WATER TO CANTED BULKHEAD AT STATION 1241 FOUND WATER DRAINING OUT OF BULKHEAD NEAR DRAIN. REMOVED P-10 PANEL SENT OUT FOR REPAIR. REPAIRED AND INSTALLED UNIT, OPS CHECK OK. (Z) 2L74 4F A20WE 19950217006941995021700694NM 1995 2 17 TWRA9509 119950204A3350 EEL BATTERY PACK BOEING747 747131 1384881NM CABIN UNSEATED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15608FF 19672 DURING PREFLIGHT FOUND HALF OF 'E' ZONE EMERGENCY LIGHTING FLICKERING. RESEATED BATTERY PACK, OPS CHECK OK. (Z) 2L74 4F A20WE 19950217006951995021700695NM 1995 2 17 TWRA9510 119950206A2560 GIRT BAR TRACK BOEING747 747136 1384883NM PAX DOOR DIRTY A TWRAK NONE O OTHER ININSP/MAINT 1 EA15606FF 20273 DURING DEPARTURE CHECKS 1L AND 1R MAIN ENTRY DOORS WOULD NOT GO INTO AUTOMATIC. MAINTENANCE CLEANED SLIDER TRACKS FOR BOTH DOORS, OPS CHECK OK. (Z) 2L74 4F A20WE 19950217006961995021700696NM 1995 2 17 VTZA95041 119950201A276082440060003 PROX SWITCH DHAV DHC8 DHC8102 2809003NM RT SPOILER BROKEN A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27419AW 297 FLT NR 6429 - IAD-JFK - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE SPOILER ADVISOR LIGHT ILLUMINATING. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 07697 IAW MEL 27-9-3 ON THE SPOILER ADVISORY SYSTEM. MAINTENANCE LATER CLEARED DMI NR 07697 ON 02-04-95 BY REPAIRING THE SPLICE ON THE RT OUTBOARD GROUND SPOILER PANEL PROXIMITY SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2H72 4T RTA13NM 19950217006971995021700697EU 1995 2 17 VTZA95042 119950205A32609EN1C11HBB2 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR WIRES BROKEN A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27494UE 810 FLT 6453 - SYR-IAD - DURING APPROACH THERE WAS NO NOSE GEAR DOWN AND LOCKED INDICATION. CREW CYCLED GEAR AND PERFORMED AN EMERGENCY GEAR EXTENSION WITH NO POSITIVE RESULTS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED BROKEN WIRES AT DOWNLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950217006981995021700698EA 1995 2 17 VTZA95043 119950203A2913PV30323 HYDRAULIC PUMP DHAV DHC8 DHC8311 1386006EA RT ENGINE FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27430AW 279 FLT NR 6943 - SWF-IAD - DURING CLIMB-OUT DIVERTED TO SWF DUE TO THE NR 2 ENGINE HYDRAULIC PUMP ILLUMINATING UPON GEAR RETRACTION/EXTENSION. AN EMERGENCY WAS DECLARED, BUT AIRCRAFT RETURNED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP. PERFORMED GEAR SWING, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2H72 4T RTA13NM 19950217006991995021700699EU 1995 2 17 VTZA95044 119950205A32609EN1C11HBB2 SWITCH BAG JETSTMJETSTM3201 1500217EU RT MAIN GEAR DIRTY A VTZAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA27493UE 805 FLT 6424 - IAD-BUF - DURING APPROACH THE RT MAIN GEAR WOULD NOT INDICATE SAFE. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTNENANCE CLEANED AND LUBED DOWNLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950217007001995021700700WP 1995 2 17 VTZA95045 219950204A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT DAMAGED A VTZAK NONE C F.O.D. TXTAXI/GRND HDL 1 EA27497UE 904 P66020 SWF-IAD - FLT 6585 - DURING TAXI OUT, THE CREW TAXIED RT ENGINE INTO A SNOW BANK. CREW SHUTDOWN ENGINE AND RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED RT ENGINE AND PROPELLER DUE TO SUDDEN STOPPAGE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T3 TRTA56EU E3WE 19950221000011995022100001WP 1995 2 21 95ZZZZ35 119950110A242451202011 VOLTAGE REG DOUG DC8 DC8F54 3021926WP NR 2 SYSTEM OVERHEATED A RRXAH DEACTIVATE SYST/CIRCUITS JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15991CF 45801 FLT 228 - KDAY-KMCO - DURING CRUISE NR 2 GENERATOR UNPARALLELED LIGHT CAME ON. FREQS NORMAL, VOLTS ERRATIC. TURNED GENERATOR OFF. DISCONNECTED GENERATOR AFTER ELECTRICAL SMOKE FILLED COCKPIT. MAINTENANCE FOUND VOLTAGE REGULATOR BAD. SMOKE CAUSED BY OVERHEATING. DEFERRED NR 2 GENERATOR SYSTEM PER MEL 24-1. VOLTAGE REGULATOR REPLACED UPON ARRIVAL AT KDAY. SYSTEM OPS CHECKED GOOD AND DMI WAS CLEARED. 2L74 4F 4A25 19950221000031995022100003NM 1995 2 21 DL72S950454 119950131A5711 STIFFENER BOEING727 727232 1384082NM RT FWD SPAR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 FOUND ON F1 LETTER CHECK, 1. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR 7 SLAT INBD TRACK INBD ANGLE LOWER END 2. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR7 SLAT INBD TRACK OUTBD ANGLE LOWER END, REPAIRED PER MM 57-20-21 PG 813. 2L73 4F A3WE 19950221000041995022100004NM 1995 2 21 DL73S950481 119950201A53156545410223 FLOOR BEAM BOEING737 737232 1384475NM FS 657 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11319DL 23091 DURING ROUTINE INSPECTION, THE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 657. THE UPPER CAP WAS COMPLETELY CRACKED, BUT NO CRACKS WERE FOUND IN THE WEB. PER B737 S/B 737-57-1210, THE CAP WILL BE REPAIRED. 2L72 4F RTA16WE 19950221000101995022100010WP 1995 2 21 95ZZZW73 119950119A5730 SKIN DOUG DC8 DC862 3021970WP WS 223.5-257.5 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION - RT WING LE STA 223.5 BULGING CORROSION. 2L74 4F 4A25 19950224000161995022400016 1995 2 24 95ZZZX832 419950104A2211112884141 COMPUTER BOLKMS117 BK117A4 5626017EU YAW CSAS DEFECTIVE A DYRAA UNSCHED LANDING F FLT CONT AFFECTED NRNOT REPORTED 1 NM07586BH 018702051 7129 THE COMPUTER CAUSED THE T/R TO OSCILLATE FORCING THE PILOT TO RETURN TO BASE FOR TROUBLESHOOTING AND REPAIRS WHICH CONSISTED OF REPLACING THE YAW CSAS COMPUTER. 1G72 3U H13EU 19950224000231995022400023NM 1995 2 24 9502322284 119950214A5743656233513 BEAM BOEING727 727251 138408HNM LT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT MAIN LANDING GEAR BEAM BORE CORRODED. REPAIRED PER NWA EA 22-093796. 2L73 4F A3WE 19950224000241995022400024NM 1995 2 24 9502332284 119950214A5741651852214 CHORD BOEING727 727251 138408HNM FS 760 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND WING TO BODY UPPER RIB CHORD AT FS 760, RBL 70.5 DAMAGED. REPAIRED PER NWA EA 22-093804. 2L73 4F A3WE 19950224000251995022400025NM 1995 2 24 9502342284 119950212A53126516350288 BLKHD BEAM BOEING727 727251 138408HNM FS 1183 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND FS 1183 BULKHEAD VERTICAL BEAM AT RBL 36.83 CRACKED IN RADIUS. REPAIRED PER NWA EA 22-096683. 2L73 4F A3WE 19950224000261995022400026NM 1995 2 24 9502352284 119950208A5753 RIB BOEING727 727251 138408HNM TE MID FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT/RIGHT MID FLAP INBOARD RIB CRACKED. REPAIRED PER NWA EA 22-090163. 2L73 4F A3WE 19950224000271995022400027NM 1995 2 24 9502362284 119950208A5315 FLOOR BEAM BOEING727 727251 138408HNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, MAINTENANCE FOUND FS 1130 FLOOR BEAM FORWARD LOWER CHORD, LBL 38 - RBL 51 CORRODED. REPAIRED PER NWA EA 22-093814. 2L73 4F A3WE 19950224000281995022400028NM 1995 2 24 9502372284 119950208A5743 ATT FITTING BOEING727 727251 138408HNM RT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01284US 21323 DURING PERIODIC CHECK, FOUND RIGHT MAIN LANGING GEAR BEAM OUTBOARD END REAR SPAR ATTACH FITTINGS CORRODED. REPAIRED PER NWA EA 22-093797. 2L73 4F A3WE 19950224000291995022400029NM 1995 2 24 9502382293 119950212A4900 APU BOEING727 727251 138408HNM AFT FUS FIRE A NWAAF ACTIVATE FIRE EXT. J WARNING INDICATION ININSP/MAINT 1 GL01293US 21504 DURING DE-ICING AT GATE, EXPERIENCED AN APU FIRE WARNING IN THE COCKPIT. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED. EVIDENCE OF FIRE WAS FOUND, THE FIRE BOTTLE WAS REPLACED AND THE APU WAS PLACED ON MEL. THE APU WAS LATER REPLACED. 2L73 4F A3WE 19950224000301995022400030NM 1995 2 24 9502396612 119950105A5230 FRAME WEB BOEING747 747251B 1384892NM CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, THE FORWARD LOWER CARGO DOOR LOWER FRAME WEB WAS FOUND CORRODED AT ELECTRICAL SWITCH HOLE. THE FRAME WEB (65B04697-601) IS MADE FROM 0.125 INCH 7075-T6 ALUMINUM. MADE REPAIR PER EA 66-93685. 2L74 4F A20WE 19950224000311995022400031NM 1995 2 24 9502406612 119950105A5313 STRINGER BOEING747 747251B 1384892NM FS 730-740 DENTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, THE FUSELAGE STR 18L WAS FOUND WITH A DENT BETWEEN FS 730 AND 740. STRINGER MATERIAL IS .040 INCH 7075-T8 ALUMINUM PER BAC 1498-140. MADE REPAIR PER EA 66-93737. 2L74 4F A20WE 19950224000321995022400032WP 1995 2 24 9502411162 119950109A5320AGA7086501 SUPPORT DOUG DC10 DC1040 3023508WP AFT LT GALLEY CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01162US 46771 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER SIDE OF THE LEFT OUTBOARD AFT GALLEY SUPPORT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER EA 11-96398. 2L73 4F A22WE 19950224000331995022400033WP 1995 2 24 9502421151 119950215A5320 WINDOW REVEAL DOUG DC10 DC1040 3023508WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01151US 46760 DURING PERIODIC CHECK, CRACKS WERE FOUND ON THE WINDOW REVEALS AT WINDOWS 1, 13, 23, AND 26. INSTALLED DOUBLERS PER EA 11-93858. 2L73 4F A22WE 19950224000341995022400034WP 1995 2 24 9502439856 119950106A5744 FITTING DOUG DC9 DC951 3022051WP NR 3 TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01765NC 47718 DURING PERIODIC CHECK, FOUND 1 .5 INCH CRACK IN NR 3 FLAP HINGE ATTACH FITTING INTERIOR RIGHT SIDE FLAP. REPLACED FITTING PER SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950224000351995022400035WP 1995 2 24 9502449945 119950111A5753 HINGE DOUG DC9 DC931 3022065WP NR 3 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-12. 2L72 4F A6WE 19950224000361995022400036WP 1995 2 24 9502459927 119950113A5753 HINGE DOUG DC9 DC931 3022065WP NR 3 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN NR 3 FORWARD FLAP HINGE FASTENER BORES WS 251. REPAIRED PER XEA X9-27-11. 2L72 4F A6WE 19950224000371995022400037WP 1995 2 24 9502469756 119950210A5313 STRINGER DOUG DC9 DC941 302207NWP FS 370-408 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 16R, PARTIAL CRACK AT FS 370 AND CRACKED COMPLETELY THROUGH AT FS 389 AND FS 408. REPAIRED PER EA 97-093818. 2L72 4F A6WE 19950224000381995022400038WP 1995 2 24 9502479756 119950210A5330 SKIN DOUG DC9 DC941 302207NWP FS 401-406 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CORROSION AT THE SKIN BUTT JOINT FS 401 - 406 AT THE FORWARD CARGO DOOR LOWER FLANGE. REPAIRED PER EA 97-096671. 2L72 4F A6WE 19950224000391995022400039WP 1995 2 24 9502489756 119950210A5320 JAMB DOUG DC9 DC941 302207NWP FWD CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CORROSION IN FORWARD CARGO DOOR JAMB PAN AFT SIDE. REPAIRED PER EA 97-096686. 2L72 4F A6WE 19950224000401995022400040WP 1995 2 24 9502499756 119950210A53475922359 TRACK DOUG DC9 DC941 302207NWP AFT CARGO COMPT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01756NW 47180 DURING PERIODIC CHECK, FOUND CORROSION ON RIGHT CARGO TRACK UPPER SURFACE IN THE AFT CARGO COMPARTMENT. REPLACED TRACK PER EA 97-096677. 2L72 4F A6WE 19950224000411995022400041WP 1995 2 24 9502509928 119950211A5531 RIB DOUG DC9 DC931 3022065WP VERT STAB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON VERTICAL STABILIZER RIB ZRS 19. REPAIRED PER EA 99-092433. 2L72 4F A6WE 19950224000421995022400042WP 1995 2 24 9502519928 119950211A5531 BEAM DOUG DC9 DC931 3022065WP VERT STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION IN VERTICAL STABILIZER BEAM ACROSS THE LOWER RUDDER 'A' BRACKET. REPAIRED SPAR ASSEMBLY PER EA 99-0924422. 2L72 4F A6WE 19950224000431995022400043WP 1995 2 24 9502529928 119950211A5312 WEB DOUG DC9 DC931 3022065WP AFT PRESS BLKHD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .5 INCH CRACK IN THE AFT PRESSURE BULKHEAD WEB, LEFT SIDE. REPAIRED PER EA 99-093485 AND EO 5310-01130. 2L72 4F A6WE 19950224000441995022400044WP 1995 2 24 9502539988 119950212A5313 STRINGER DOUG DC9 DC931 3022065WP FS 925 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, CORROSION ON LONGERON 30 SPLICE FITTING AT FS 925. REPLACED FITTING PER SRM 53-02. 2L72 4F A6WE 19950224000451995022400045WP 1995 2 24 9502549988 119950212A5753 HINGE DOUG DC9 DC931 3022065WP NR 2 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT WING NR 2 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-14. 2L72 4F A6WE 19950224000461995022400046WP 1995 2 24 9502559988 119950212A5753 HINGE DOUG DC9 DC931 3022065WP NR 2 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORRROSION IN RIGHT WING NR 2 FLAP HINGE FASTENER BORES. REPAIRED PER XEA X9-27-17. 2L72 4F A6WE 19950224000471995022400047WP 1995 2 24 9502569957 119950213A5320 FITTING DOUG DC9 DC931 3022065WP FS 1087-1121 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01915RW 47139 DURING PERIODIC CHECK, FOUND CRACK IN TAIL FITTING FS 1087 - 1121 AT LONGERON 30. REPLACED FITTING PER DWG 88277 AND SRM 51-30-5. 2L72 4F A6WE 19950224000481995022400048WP 1995 2 24 9502579957 119950214A5320 FITTING DOUG DC9 DC931 3022065WP FS 617 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01915RW 47139 DURING PERIODIC CHECK, FOUND CRACK IN FITTING FS 617 AT LONGERON 29R. REPLACED PER SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950224000491995022400049NM 1995 2 24 9502582293 119950214A3260H1010154 POSITION SW BOEING727 727251 138408HNM NLG FAILED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01293US 21504 DURING APPROACH UPON LANDING GEAR EXTENSION, NOSE GEAR SAFE (GREEN) INDICATION DID NOT ILLUMINATE WHILE UNSAFE (RED) INDICATION REMAINED ILLUMINATED. CREW RECYCLED LANDING GEAR TO NO AVAIL. VERIFIED NOSE LANDING GEAR WAS DOWN AND LOCKED THROUGH VIEWING PORT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR POSITION SWITCH. OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950224000501995022400050WP 1995 2 24 9502599981 119950213A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01994Z 47097 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ADJUSTED THE INTERIOR AND EXTERIOR CLIPS. 2L72 4F A6WE 19950224000511995022400051WP 1995 2 24 9502609951 119950212A5350 CABLE DOUG DC9 DC932 3022066WP TAILCONE FRAYED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019347 45827 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE TAILCONE CABLE FRAYED BETWEEN THE RIGHT SIDE LATCHES AT THE LOWER PULLEY. REPLACED THE CABLE AND RERIGGED THE TAILCONE. 2L72 4F A6WE 19950224000521995022400052NM 1995 2 24 9502612769 119950213A2612 FIRE LOOP BOEING727 7272M7 138407SNM PWA JT8 JT8D17R 52049NE NR 2 ENGINE MALFUNCTIONED A NWAAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL01729RW 21742 689872 IN CRUISE FLIGHT, THE NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED. THE ENGINE WAS SHUT DOWN AND ONE FIRE BOTTLE WAS DISCHARGED. NO SECONDARY INDICATION OF FIRE WAS NOTED. THE FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. A FAULT WAS LOCATED IN THE NR 2 ENGINE FIRE LOOP. THE LOOP AND FIRE BOTTLE WERE REPLACED. THE SYSTEM TESTED OK. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950224000531995022400053NM 1995 2 24 9502622715 119950215A27821U1110 ACTUATOR BOEING727 7272S7 138407ZNM LE FLAP FAILED A NWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL01719RC4462417183 22490 DURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 1 LEADING EDGE FLAP REMAINED EXTENDED. RECYCLED FLAPS TO NO AVAIL, RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 LEADING EDGE FLAP ACTUATOR AND PERFORMED LEAK AND OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 19950224000541995022400054WP 1995 2 24 9502631151 119950216A5311 FRAME DOUG DC10 DC1040 3023508WP FS 979 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01151US 46760 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FRAME TEE AT FS 979, STR 44L - 45L IN FORWARD CARGO COMPARTMENT. REMOVED CORROSION AND REPAIRED PER EA 11-9385. 2L73 4F A22WE 19950224000551995022400055WP 1995 2 24 9502651157 119950216A7830DC10407 AIR DUCT DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 ENGINE REV RUPTURED A ANWAAEA ENGINE SHUTDOWN UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL01157US 46766 686135 DURING INITIAL CLIMB, THE NR 1 ENGINE EXPERIENCED THE REVERSER UNLOCK LIGHT ILLUMINATE THEN GO OUT FOLLOWED BY THE FIRE LIGHT AND BELL COMING ON. POWER WAS REDUCED TO IDLE AND THE LIGHTS EXTINGUISHED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO SEA WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. THE FIRE BOTTLE WAS NOT DISCHARGED AND NO FUEL WAS DUMPED. THE 'S' DUCT AT THE PLUSSEY UNIT WAS FOUND RUPTURED. THE DUCT, RIGHT FAN COWL, VENT VALVE, AND THE REVERSER DIVE UNIT WERE REPLACED. THE SYSTEM CHECKED OK. 2L73 4F4 F A22WE E20EA 19950224000561995022400056WP 1995 2 24 9502669105 119950211A3260 DNLOCK SW DOUG DC9 DC915 3022036WP LT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL0195S 47205 DURING APPROACH INTO MSP, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON GEAR EXTENSION. CONFIRMED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000571995022400057WP 1995 2 24 9502679154 119950214A2421 GENERATOR DOUG DC9 DC914 3022034WP LT ENGINE FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018913E 45830 AC EMERGENCY BUS OFF LIGHT ILLUMINATED AFTER TAKEOFF. THIS PROBLEM AFFECTED MULTIPLE COCKPIT INSTRUMENTS. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AC GENERATOR AND GENERATOR CONTROL PANEL. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000581995022400058WP 1995 2 24 9502689154 119950215A2420 RELAY DOUG DC9 DC914 3022034WP AC SYST FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018913E 45830 AC EMERGENCY BUS OFF LIGHT ILLUMINATED AFTER TAKEOFF. THIS PROBLEM AFFECTED MULTIPLE COCKPIT INSTRUMENTS. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE AC EMERGENCY TRANSFER RELAY R2-47, CIRCUIT BREAKER B1-185, AND 'A' PHASE CIRCUIT BREAKER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000591995022400059 1995 2 24 9502699155 419950211A3418 STICK SHAKER DOUG DC9 DC914 3022034WP COCKPIT MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL018914E 45831 STALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED ON FINAL APPROACH INTO DTW. PERFORMED STALL RECOVERY AND ACCOMPLISHED GO-AROUND PROCEDURES. NORMAL INDICATIONS WERE ACHIEVED ON SECOND APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000601995022400060 1995 2 24 9502709753 419950214A3418 STALL COMPUTER DOUG DC9 DC941 302207NWP NR 1/2 MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01753NW 47117 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER FLAP RETRACTION ON TAKEOFF AND REMAINED ON AT SPEEDS UP TO 340 KTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. REPLACED BOTH NR 1 AND NR 2 STALL WARNING COMPUTERS AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000611995022400061WP 1995 2 24 9502719760 119950210A3231 RETRACT MECH DOUG DC9 DC941 302207NWP NLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 GL01760NW 47288 A LOUD 'BANG' WAS HEARD ON INITIAL GEAR RETRACTION AFTER TAKEOFF. NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND VIBRATION WAS EXPERIENCED. FLIGHT RETURNED TO DTW AND SUCCESSFUL OVERWEIGHT LANDING WAS ACCOMPLISHED. PERFORMED OVERWEIGHT LANDING INSPECTION PER MM 05-51-00, CODE 10. REPLACED DAMAGED LEFT FORWARD NOSE GEAR DOOR, DOOR STOP CABLE, AND FORWARD DOOR RETRACT LINK. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224000621995022400062WP 1995 2 24 9502729944 119950208A2410B18D18 CSD OIL COOLER DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE RUPTURED A NWAADE RETURN TO BLOCK ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS TXTAXI/GRND HDL 1 GL011309T405394735 47376 667012 TAXIING FOR TAKEOFF, THE NR 2 ENGINE CSD OIL PRESSURE LOW LIGHT STARTED FLICKERING. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND THE CSD OIL COOLER RUPTURED. THE COOLER WAS REPLACED AND THE OIL WAS SERVICED. ACCOMPLISHED ENGINE RUN-UP AND SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950224000631995022400063NM 1995 2 24 9502732298 119950216A7711JG298A4 INDICATOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01298US2608511622 22152 696617 AS THROTTLES WERE ADVANCED FOR TAKEOFF, THE NR 1 ENGINE EPR FAILED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE EPR INDICATOR WAS REPLACED. SYSTEM FUNCTIONAL TEST WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950224000641995022400064NM 1995 2 24 95FDEA00146 119950213A5347BAC152079 SEAT TRACK BOEING727 727233 138408ANM BS 1128 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 SEAT TRACK IS CRACKED AT BS 1128 LBL 625 WL 208. REMOVED SEAT TRACK, INSTALLED FABRICATED TRACK BACK DRILLED, COUNTER SUNK HOLES, ALODINED AND PRIMED TRACK, INSTALLED FASTENERS. 2L73 4F RTA3WE 19950224000651995022400065NM 1995 2 24 95FDEA00147 119950212A5315BA15057075T FLOOR BEAM BOEING727 727233 138408ANM BS 1110 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 TRAMCO RESPONSIBILITY 9502-30. MISDRILLED HOLE IN FLOOR BEAM AT BS 1110 LBL 25 WL 208. REPAIRED FLOOR BEAM AT BS 1110 LBL 25 WL 208 PER FEDEX SRM 53-10-8. 2L73 4F RTA3WE 19950224000661995022400066NM 1995 2 24 95FDEA00148 119950213A5315BAC1505100617 FLOOR BEAM BOEING727 72725 1384006NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION FLOOR BEAM UPPER CHORD BS 680 LBL 36 WL 208. REMOVED CORRODED CHORD, FABRICATED AND INSTALLED REPLACEMENT CHORD AT BS 680 LBL 36 TO RBL 14 WL 208 PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19950224000671995022400067NM 1995 2 24 95FDEA00149 119950215A5315BAC150529222 FLOOR BEAM BOEING727 72725 1384006NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON TOP AND BOTTOM OF TOP CHORD OF FLOORBEAM AT BS 344 RBL 17 - LBL 61 WL 208. REPLACED TOP CHORD FROM LBL 707 - RBL 70. IAW FEDEX DRAWING NUMBER SR 27 53-007. 2L73 4F A3WE 19950224000681995022400068NM 1995 2 24 95FDEA00150 119950213A5320M362260 SHEAR TIE BOEING727 72725 1384006NM FS 441 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FOUND SHEAR TIE CRACKED AT AFT SIDE STA 441 RT BETWEEN STR 18 AND 19, RBL 65. REMOVED CRACKED SHEAR TIE STA 441 RT STR 18 AND 19 (AFT SIDE) RBL 65 AND REPLACED WITH FABRICATED SHEAR TIE. 2L73 4F A3WE 19950224000691995022400069 1995 2 24 95FDEA00151 419950216A3442 RADAR BOEING727 727233 138408ANM FWD FUS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04276FE 22041 RADAR FAILURE WARNING ON CLIMB-OUT ANTENNA FAIL, (QUIT SWEEPING). REMOVED AND REPLACED RADAR INDICATOR, RADAR ANTENNA AND RADAR RT UNIT. SYS OPS CK GOOD. 2L73 4F RTA3WE 19950224000701995022400070NM 1995 2 24 95FDEA00152 119950216A5610 WINDOW BOEING727 727233 138408ANM FLIGHT DECK CRACKED A FDEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO04220FE 20934 DURING CLIMB-OUT, R-1 WINDOW BEGAN ARCING FOLLOWED BY CRACKING OF THE OUTER PANE OF THE R-1 WINDOW. REMOVED R-1 WINDOW AND TAGGED PARTS, INSTALLED R-1 WINDOW PER MM 56-11-11. CHECK FOR CORRECT R-1 TERMINAL AND R-1 WINDOW CONTROL TO BE REPLACED. TERMINAL CK OK. REMOVED AND REPLACED WINDOW HEAT CONTROL. 2L73 4F RTA3WE 19950224000711995022400071 1995 2 24 95FDEA00153 419950217A3442 RADAR BOEING727 727233 138408ANM FWD FUS FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04276FE 22041 RADAR FAILURE WARNING ON CLIMB-OUT ANTENNA FAIL QUIT SWEEPING. CHECKED ALL WIRING FROM ANT TO R/T, BOTH POINT TO POINT, WIRE AND TO GND. ALL CKS GOOD, R/T MESSAGE ANNUNCIATED BRIEFLY. REMOVED AND REPLACED R/T FOUND ANTENNA WAVE GUIDE O-RING DETERIORATED REPLACED SAME. FOUND INDICATOR LEFT BUTTON INOP. REMOVED AND REPLACED IND A/C CLEARED FOR TEST FLIGHT PER MOCC. 2L73 4F RTA3WE 19950224000721995022400072NM 1995 2 24 95UAL727016 119950213A3350 EEL POWER PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297261U 21408 RIGHT 0VERWING EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED POWER PACK. 2L73 4F4 F A3WE E2EA 19950224000731995022400073NM 1995 2 24 95UAL737015 119950213A2612896768 DETECTOR BOEING737 737291 138448WNM PWA JT8 JT8D9A 52048NE APU SHORTED A UALAAF UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP29980UA 21545 RECEIVED APU FIRE WARNING IN FLIGHT. FIRE BOTTLE WAS DISCHARGED. FOUND OVERHEAT DETECTOR LOOP IN TAILPIPE SHORTED TO GROUND. REPLACED LOOP DETECTOR AND CONNECTOR. CHECKS OK. 2L72 4F4 F A16WE E2EA 19950224000741995022400074NM 1995 2 24 95UAL737016 119950213A3350 EEL STRIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29203UA 24718 EMERGENCY ESCAPE PATH LIGHT STRIP INOP AT ROW 13. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950224000751995022400075NM 1995 2 24 95UAL737017 119950213A2120 INSTRUMENT PANEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLIGHT COMPT VIBRATION A UALAK NONE E VIBRATION/BUFFET CLCLIMB 1 WP29354UA 24360 AFTER TAKEOFF, HEARD AND FELT LOUD RAPID VIBRATION COMING FROM BEHIND INSTRUMENT PANEL. VIBRATION QUIT AT ABOUT 300 FEET. LANDED UNDER AMBER ALERT. 2L72 4F4 FRTA16WE E2GL 19950224000761995022400076NM 1995 2 24 95UAL737018 119950213A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29393UA 24668 RIGHT OVER WING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950224000771995022400077NM 1995 2 24 95UAL737019 119950213A7931 OIL PRESS IND BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE NR 1 ENGINE MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29992UA 22089 ON TAKEOFF, NR 1 ENGINE INDICATED LOSS OF OIL PRESSURE. ABORTED TAKEOFF. 2L72 4F4 F A16WE E2EA 19950224000781995022400078NM 1995 2 24 95UAL737021 119950216A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29362UA 24455 EMERGENCY ESCAPE PATH LIGHT INOP AT ROW 12. REPLACED LIGHT STRIP. 2L72 4F4 FRTA16WE E2GL 19950224000791995022400079NM 1995 2 24 95UAL737022 119950220A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29333UA 24228 FIRST CLASS EMERGENCY ESCAPE PATH LIGHT STRIP INOP. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950224000801995022400080NM 1995 2 24 95UAL747009 119950213A2910 HYD SYST BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE NR 1 SYST FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29158UA 21054 NR 1 HYDRAULIC SYSTEM FAILED DURING FLAP RETRACTION. 2L74 4F4 F A20WE E20EA 19950224000811995022400081NM 1995 2 24 95UAL747010 119950213A3350 EEL CONNECTOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29191UA 26880 ALL EMERGENCY CEILING LIGHTS INOP IN E ZONE. SECURED CONNECTOR D11700J. SYSTEM GROUND CHECKED OK. 2L74 4F4 FRTA20WE E24NE 19950224000821995022400082NM 1995 2 24 95UAL747011 119950213A5270 DOOR POWER LIGHT BOEING747 747451 1384940NM PWA 4056 PW4056 NE UPPER DECK DOOR FAILED TEST A UALAK NONE L NO TEST ININSP/MAINT 1 WP29105UA 26473 LEFT STRETCHED UPPER DECK DOOR POWER LIGHT FAILED TEST. REPLACED BATTERY PACK AND ANNUNCIATOR MODULE. 2L74 4F4 FRTA20WE E24NE 19950224000831995022400083NM 1995 2 24 95UAL747012 119950215A3350 EEL BOEING747 747222B 1384904NM PWA JT9 JT9D7R4G2 52054NE CABIN MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29151UA 23736 DOOR 4 RIGHT EMERGENCY LIGHT STAYS ON DIM. REPLACED LIGHT ASSY. 2L74 4F4 FRTA20WE E3NE 19950224000841995022400084NE 1995 2 24 95UAL757004 219950217A7200 ENGINE JFC104 BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ENG MALFUNCTION A UALAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 WP29560UA F24196 26660 726648 RIGHT ENGINE MADE UNCOMMANDED INCREASE TO MAX POWER. SHUTDOWN ENGINE. DISASSEMBLY SHOWED SIGNS OF METAL SLIVERS ON THE LOW SIDE OF THE PRESSURE RELIEF VALVE WHICH CAUSED THE VALVE TO MALFUNCTION. 2L72 4F4 FRTA2NM E17NE 19950224000851995022400085NM 1995 2 24 95UAL757005 119950220A3350 EEL BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29539UA 25223 EEL LIGHTS INOP ROWS 24 TO 32. REPLACED BATTERY PACK M735. 2L72 4F4 FRTA2NM E17NE 19950224000861995022400086NM 1995 2 24 95UAL767005 119950217A3244 TIRE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LANDING GEAR FAILED A UALAO OTHER O OTHER LDLANDING 1 WP29620UA 21880 LANDED UNDER AMBER ALERT DUE TO LOSS OF TIRE. 2L72 4F4 FRTA1NM E3NE 19950224000871995022400087NE 1995 2 24 95UAL767006 219950217A7230 COMPRESSOR BLADEPWA 51H38701 BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT ENGINE FAILED A UALAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 WP29649UA 25286 SHUTDOWN LEFT ENGINE DUE TO COMPRESSOR STALLS AND LANDED UNDER AMBER ALERT. EIGHTH STAGE BLADE FAILED, DUE TO SEVENTH STAGE INNER SHROUD DOWL PIN LIBERATION. 2L72 4F4 FRTA1NM E24NE 19950224000881995022400088NM 1995 2 24 95UAL767007 119950217A8012 VALVE ALLIED SIGNA9798582 BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE STARTER MALFUNCTION A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29652UA 597C 25390 STARTER VALVE, AND STARTER SEQUENCE LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO FIELD. UNABLE TO FIND FAULT WITH VALVE. OVERHAULED IT AS A PRECAUTION AND RETURNED TO STOCK. 2L72 4F4 FRTA1NM E24NE 19950224000891995022400089NM 1995 2 24 95UAL767008 119950220A2450 CIRCUIT BREAKER BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE AC ELECT SYST TRIPPED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29648UA 25285 THE C327 CIRCUIT BREAKER TRIPPED IN FLIGHT, CAUSING THE LOSS OF THE RIGHT 115 VOLT A/C TRANSFER BUSS. 2L72 4F4 FRTA1NM E24NE 19950224000901995022400090EU 1995 2 24 95UALA32010 119950215A3350 EEL AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29413UA 470 EEL LIGHT OUT AT SEAT 2B. REPLACED LIGHT ASSEMBLY AND OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA28NM E40NE 19950224000911995022400091WP 1995 2 24 95UALD10003 119950110A4900 APU DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL AFT FUS INOPERATIVE A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291836U 47968 DEN - PUNGENT ODOR SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. LAX - CABIN SMELLED OF OIL AFTER AIR CONDITIONING PUT ON WITH APU FOR AIR SOURCE. APU INOP. COMPLIED WITH MEL 49-A. CONTAMINANTS IN SYSTEM. ACCOMPLISHED PACK BURN OUT. 2L73 4F4 F A22WE E23EA 19950224000921995022400092WP 1995 2 24 95UALD10018 119950213A3350 EEL STRIP DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN MALFUNCTIONED A UALAK NONE L NO TEST DEDESCENT 1 WP291859U 47819 FIRST CLASS RIGHT AISLE EMERGENCY FLOOR STRIP LIGHTS CAME ON DURING DESCENT. WENT OFF JUST BEFORE LANDING. REPLACED POWER SUPPLY. 2L73 4F4 F A22WE E23EA 19950224000931995022400093GL 1995 2 24 95UALD10019 219950216A7320 MEC WOODWARD GOV8062111 DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 ENG SEAL WORN A UALAO OTHER Y ENGINE STOPPAGE TOTAKEOFF 1 WP291824U 11646 46623 451347 LOST NR 3 ENGINE ON TAKEOFF. AFTER LIFT OFF NR 3 SPOOLED TO 0 N1, THEN SPOOLED UP AND DOWN AGAIN. CDP SENSOR CHECKED OK. MEC BENCH CHECKED AND FUEL FLOW AND VSV WITHIN LIMITS. DISASSEMBLY OF MEC REVELED MAIN DRIVE SHAFT SEAL BADLY WORN WHICH MAY HAVE CAUSED EXCESSIVE LEAKAGE WITHIN THE MEC. 2L73 4F4 F A22WE E23EA 19950224000941995022400094WP 1995 2 24 95UALD10020 119950216A2120 AIR DISTR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN ODOR A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291849U 46939 PUNGENT ODOR(SMOKE) IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. SMELL OCCURS WITH TRIM AIR VALVE AT MID POSITION. 2L73 4F4 F A22WE E23EA 19950224000951995022400095WP 1995 2 24 95UALD10021 119950220A3350EMBS1392 EEL BATTERY PACK EMSE299 DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291825U 46624 EMERGENCY LIGHTING DOES NOT TEST FROM OVERHEAD PANEL BITE TEST FROM ENGINEERS PANEL FAULTS MID FWD POWER SUPPLY. REPLACED BATTERY PACK AND POWER SUPPLY. 2L73 4F4 F A22WE E23EA 19950224000961995022400096SO 1995 2 24 COM11788 119950216A27503472001001 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAK NONE O OTHER APAPPROACH 1 SO01247CA2637 1885 120225 CONTROL FAULT WARNING WHEN FLAPS SELECTED FOR APPROACH. REPLACED FLAP CONTROL UNIT. 2L72 4T RTA31SO 19950224000971995022400097SO 1995 2 24 COM11789 119950216A7603 CONTROL CABLE EMB 120 EMB120RT SO LT PWR LEVER BROKEN A COMAO OTHER O OTHER NRNOT REPORTED 1 SO01241CA 120211 GO AROUND BUTTON ON LEFT POWER LEVER IS INOPERATIVE. REPAIRED BROKEN WIRE IN POWER LEVER QUADRANT. 2L72 4T RTA31SO 19950224000981995022400098SO 1995 2 24 COM11790 119950215A306078614423 LEAD EMB 120 EMB120RT SO RT PROP BROKEN A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01244CA 120217 RT PROPELLER ANTI-ICE IS INOP. REPLACED BROKEN DE-ICE LEAD. 2L72 4T RTA31SO 19950224000991995022400099SW 1995 2 24 COM20355 119950216A29102781032 HYD LINE SWRNGNSA227 SA227AC 8780603SW LT NACELLE LEAKING A COMAK NONE KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 SO01704C AC704 SEVERE HYDRAULIC LEAK, LEFT LANDING GEAR AREA. REPLACED EMERGENCY GEAR DOWN HYDRAULIC LINE. 1L72 4T A8SW 19950224001001995022400100 1995 2 24 COM31036 319950217A6110 PROP SAAB SF340 SF340A 7850100EU LEFT DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01158CA 1474 340A158 LEFT PROPELLER HAS BLADE TIP DAMAGE. REPLACED PROPELLER. 2L72 4T RTA52EU 19950224001011995022400101EA 1995 2 24 COM60419 119950218A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT/RT WING DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01917CA3029 339 7017 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE LEFT AND RT BPSU. 2L72 4F RTA21EA 19950224001021995022400102EA 1995 2 24 COM60420 119950217A3412102AH2AG TAT PROBE CNDAIRCL600 CL6002B19 EA FUSELAGE DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA2281 1771 7017 TAT PROBE HEAT MESSAGE ON EICAS. REPLACED TAT PROBE. 2L72 4F RTA21EA 19950224001031995022400103EA 1995 2 24 COM60421 119950216A3230617501 SELECTOR VALVE CNDAIRCL600 CL6002B19 EA WING CENTER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01936CA1503 7043 LANDING GEAR DISAGREE MESSAGE ON EICAS. LEFT MLG DOES NOT INDICATE UP. DISCREPANCY CANNOT BE DUPLICATED, REPLACED MLG SELECTOR VALVE FOR TROUBLESHOOTING. 2L72 4F RTA21EA 19950224001041995022400104NM 1995 2 24 DL72E950610 119950213A5754651622373 RIB BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND CRACKED RIB UPON INSPECTION ON NR 2 SLAT. REPAIRED RIB PER MM 57-54-00. 2L73 4F A3WE 19950224001051995022400105NM 1995 2 24 DL72K950616 119950214A711065196854141 NOSE COWL BOEING727 727232 1384082NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 DURING ROUTINE SHOP INSPECTION THE AFT LANDING STRIP BETWEEN 8-9 0'CLOCK POSITION WAS FOUND TO BE WORN. ON NR 1 ENGINE NOSE COWL, REPAIRED PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950224001101995022400110NM 1995 2 24 DL72L950625 119950214A5754 NOSE RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND DURING C-2 LETTER CHECK, NR 7 SLAT I/B ACTUATOR NOSE RIB CRACKED .1250 INCH. REPAIRED PER B727 MM 57-54-0 PG 803. 2L73 4F A3WE 19950224001111995022400111NM 1995 2 24 DL72S950571 119950209A5530 SKIN BOEING727 727232 1384082NM LT VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11409DA 21153 DURING LETTER CHECK, FOUND 2 CRACKS IN PANEL FWD OF SADDLE PLATE LEFT SIDE VERTICAL STABILIZER. REPAIRED PER MM 54-30-0 PG 801-802. 2L73 4F A3WE 19950224001121995022400112NM 1995 2 24 DL72S950584 119950210A5330 SKIN BOEING727 727232 1384082NM PAX DOOR CUT OUTCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 FOUND DURING A-2 LETTER CHECK, 2 INCH VISIBLE CRACK AT LWR HINGE CUTOUT OF MAIN ENTRY DOOR ON FUSELAGE. REPAIRED PER MM 53-30-0 PG 820-836 PART 2. 2L73 4F A3WE 19950224001131995022400113NM 1995 2 24 DL72S950630 119950212A5313 STRINGER BOEING727 727232 1384082NM 15R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 FOUND AT HMV RT WING L/E LT BOX FWD SIDE HAS CRACK IN STR 15R. FABRICATED REPAIR PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19950224001141995022400114NM 1995 2 24 DL72S950631 119950210A5740 BRACKET BOEING727 727232 1384082NM NR 1 LE FLAP ACTCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 FOUND AT HMV IB/OB AT NR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED. REPAIRED BRACKETS PER M/M 57-20-21 FIG 807. 2L73 4F A3WE 19950224001151995022400115NM 1995 2 24 DL72S950656 119950214A2197D870 WIRE BOEING727 727232 1384082NM RT PACK LOOSE A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO11409DA 21153 DURING CRUISE, UNABLE TO MAINTAIN CABIN PRESSURE, INITIATED EMERGENCY DESCENT. REGAINED CONTROL AT FL 180 IN MANUAL MODE. FOUND INTERMITTENT WIRES AT RIGHT PACK FLOW CONTROL AND SHUT OFF VALVE. REPLACED 3 WIRES AT CANNON PLUG D870, WDM 21-61-02 PG.4. OPERATION NORMAL. 2L73 4F A3WE 19950224001161995022400116NM 1995 2 24 DL72W950617 119950214A5754651622193 TE FAIRING BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 DURING SHOP INSPECTION, FOUND NR 4 SLAT WITH THE I/B AND O/B TRACK FAIRINGS CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950224001171995022400117NM 1995 2 24 DL72W950618 119950214A5754651622193 SKIN BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 DURING SHOP INSPECTION, FOUND NR 4 SLAT SKIN CRACKED AT MOUNT HOLE FOR THE WING FENCE. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950224001181995022400118NM 1995 2 24 DL72W950620 119950214A5754 ANGLE BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112816W 20872 FOUND DURING D-2 LETTER CHECK, COVE SKIN ATTACH ANGLE CRACKED 2 INCH AT O/B STOP FITTING NR 6 SLAT. REPAIRED PER MM 57-54-0 PG 816. 2L73 4F A3WE 19950224001191995022400119NM 1995 2 24 DL733950578 119950210A5230 SKIN BOEING737 737347 1384647NM BAGG DOOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11307WA 23440 DURING HMV, FOUND A DEEP GOUGE IN THE C-1 B/B DOOR IN MID-SECTION OF EXTERNAL SKIN 9 INCHES FROM AFT END. CUT OUT DAMAGE AND REPAIRED PER SRM 52-00-01. 2L72 4F RTA16WE 19950224001221995022400122NM 1995 2 24 DL757950636 119950206A5755113N460123 SKIN BOEING757 757232 1384965NM SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11667DN 25035 DURING SHOP INSPECTION, FOUND 3 PUNCTURES IN BOTTOM SKIN OF SPOILER PANEL. REPAIRED PER SRM 57-70-01. 2L72 4F RTA2NM 19950224001231995022400123NM 1995 2 24 DL76L950658 119950215A79316228303104 TRANSMITTER BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENG OIL MALFUNCTION A DALAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO11171DN 24759 724138 DURING CLIMBOUT, HAD NO OIL PRESSURE INDICATION ON NR 2 ENGINE, SHUT ENGINE DOWN, RETURNED JFK. FOUND FAULTY OIL PRESSURE TRANSMITTER, REPLACED SAME, OPERATION NORMAL. SUPPLEMENT 1: SHOP EVALUATION OF TRANSMITTER DID NOT FIND ANY FAULT. DUE TO LOW OIL PRESSURE INDICATION HISTORY, THE LEFT EICAS COMPUTER WAS REMOVED. DL SHOP EVALUATION COULD NOT FIND ANY FAULT. COMPUTER WAS SENT TO COLLINS, THEIR SHOP EVALUATION COULD NOT FIND ANY FAULT. AS A PRECAUTION, THE CIRCUIT BOARD FOR THE AFFECTED FUNCTIONS WAS REPLACED, UNIT WAS RETURNED TO STOCK. 2L72 4F4 FRTA1NM E24NE 19950224001241995022400124NM 1995 2 24 DL76S950657 119950215A2121605457 FAN BOEING767 767332 1382001NM AC BAY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11116DL 23275 DURING CRUISE, FLIGHT ATTENDANT REPORTED BURNING SMELL FROM OVERHEAD GASPER FAN VENTS. DEACTIVATED FAN, ODOR STOPPED. REPLACED GASPER FAN OPERATION NORMAL. 2L72 4F RTA1NM 19950224001251995022400125WP 1995 2 24 DLL10950619 119950214A5753 SKIN 1529112110ADLKHEED1011 10113851 5265010WP NR 1 TE VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA DL2 193C1096 DURING SHOP INSPECTION TWO CRACKS WERE FOUND IN THE UPPER SKIN OF RT WING NR 1 FLAP VANE, REPLACED SKIN PER SR 57-53-00. 2L73 4F A23WE 19950224001261995022400126NM 1995 2 24 DLM88950558 119950208A5230 DOOR FRAME DOUG MD88 MD88 3023688NM CARGO DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11916DE 53421 DURING LETTER CHECK, FWD CARGO DOOR PAN WAS FOUND DAMAGED AT HOLD OPEN AFT SIDE. REPAIRED PER SRM 52-05 FIG 27. 2L72 4F RTA6WE 19950224001271995022400127NM 1995 2 24 DLM88950559 119950208A5230 DOOR PAN DOUG MD88 MD88 3023688NM CARGO DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11916DE 53421 DURING LETTER CHECK, CENTER CARGO DOOR PAN WAS FOUND DAMAGED AT HOLD OPEN FORWARD SIDE, REPAIRED PER SRM 52-05 FIG 27. 2L72 4F RTA6WE 19950224001281995022400128NM 1995 2 24 DLM88950582 119950210A7110 NOSE COWL DOUG MD88 MD88 3023688NM NR 1 ENG DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11984DL 53311 FOUND DURING D-1 LETTER CHECK, SOUND SUPPRESSION SCREEN DELAMINATED AT 0300 POSITION INSIDE NOSE COWL. REPAIRED PER SRM 54-04A. 2L72 4F RTA6WE 19950224001291995022400129NM 1995 2 24 DLM88950583 119950210A3230 STRIKER ANGLE DOUG MD88 MD88 3023688NM LT MLG W.W. CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11984DL 53311 ITEM DEFERRED FROM C-2 CHECK 07/25/94, TIME LIMITED REPAIR INSTALLED AT LEFT MLG WHEEL WELL AFT O/B STRIKER ANGLE PER SRM 53-05 FIG 81A. INSTALLED PERMANENT REPAIR PER SRM 53-05 FIG 81A. 2L72 4F RTA6WE 19950224001301995022400130NM 1995 2 24 DLM88950590 119950211A5230 DOOR DOUG MD88 MD88 3023688NM CARGO COMPT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11926DL 49713 TRANSFERRED FROM A/C LOG BOOK Z272827. FOUND UPON ARRIVAL IN ATL, FWD B/B DOOR DAMAGED LWR EDGE. REPAIRED DAMAGED AREA PER SRM 52-05 FIG 4. 2L72 4F RTA6WE 19950224001311995022400131WP 1995 2 24 MWEA95131 119950218A52803913433503 HINGE DOUG DC9 DC932 3022066WP LT MLG CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 47673 DURING C-CHECK INSP, ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE, FOUND 1 HINGE LOBE CRACKED. REPLACED HINGE PER DAC SB 32-244 AND SRM 51-30. A/C RETURNED TO SERVICE. 2L72 4F A6WE 19950224001321995022400132WP 1995 2 24 MWEA95132 119950220A5230 SKIN DOUG DC9 DC932 3022066WP AFT CARGO DOOR PUNCTURED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING ROUTINE MAINTENANCE, FOUND 1 INCH BY .75 INCH PUNCTURE IN AFT CARGO DOOR OUTER SKIN. REMOVED DAMAGED AREA, INSTALLED DOUBLER IAW DAC SRM 52-01, FIG 2, SHEET 3. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224001331995022400133WP 1995 2 24 MWEA95133 119950211A5230 PAN DOUG DC9 DC915 3022036WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING INSPECTION PER DAC SB52-125, FOUND FORWARD CARGO DOOR HAD A .25 INCH CRACK IN THE OUTER PAN RADIUS. REPIARED IAW DAC SRM 52-03, FIG 8 (DOUBLER INSTALLATION). 2L72 4F A6WE 19950224001341995022400134 1995 2 24 MWEA95134 419950217A2565136212 EVAC SLIDE DOUG DC9 DC932 3022066WP AFT ACCESSORY SLOW TO INFLATE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 4597 47102 DURING A TIME CHANGE FOR A TAIL SLIDE (3 YR INTERVAL), A FUNCTIONAL TEST OF THE SLIDE REVEALED A 20 SECOND HESITATION BEFORE THE SLIDE STARTED TO INFLATE. SLIDE SENT TO VENDOR FOR BENCH CHECK. 2L72 4F A6WE 19950224001351995022400135NM 1995 2 24 QXEA9500051 119950216A3350 EEL DORNERDO32 DO328100 2996000NM CABIN MALFUNCTIONED A QXEAK NONE L NO TEST APAPPROACH 1 NM09335PH 3013 GEG - WHEN CREW SELECTED DOUBLE CHIME TO SIGNAL PASSING 10,000 FEET THE EMERGENCY LIGHTS ACTIVATED AND COULD NOT BE TURNED OFF. FLIGHT LANDED WITHOUT INCIDENT. FOUND WIRE BUNDLE AT 15VEA PINCHED. REPOSITION BUNDLE SYSTEM OPERATED NORMAL. AIRCRAFT RELEASED FOR SERVICE. 2H72 4T RTA45NM 19950224001361995022400136NM 1995 2 24 UPS202390 119950220A5311 FRAME BOEING727 727173C 1384059NM BS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT BS 560, STR 22L-24L. REPAIRED FRAME PER SRM 51-40-03. 2L73 4F A3WE 19950224001371995022400137NM 1995 2 24 UPS202391 119950220A5320652355520 STIFFENER BOEING727 727173C 1384059NM BS 770 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON DELTA BEAM WEB AT BS 770, LBL 5, WL 148. REPLACED STIFFENER PER SRM 51-10-1, 51-30-2, 51-20-4. 2L73 4F A3WE 19950224001381995022400138NM 1995 2 24 UPS202392 119950220A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 580, RBL 47-59, WL 201. REPAIRED FLOOR BEAM PER UPS EO FILE NUMBER 727-53-1482. 2L73 4F A3WE 19950224001391995022400139NM 1995 2 24 UPS202393 119950220A5315BAC1505101167 FLOOR BEAM BOEING727 727173C 1384059NM BS 1030 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FLOOR BEAM AT STA 1030, RBL 41, WL 208. REPAIRED FLOOR BEAM PER SRM 53-10-8. 2L73 4F A3WE 19950224001401995022400140NM 1995 2 24 UPS202394 119950220A5320651841730 STIFFENER BOEING727 727173C 1384059NM BS 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON HORIZONTAL STIFFENER AT BS 300, RBL 15, WL 208. REPAIRED STIFFENER PER SRM 53-10-1, 51-30-2, 51-20-4, 51-10-1. 2L73 4F A3WE 19950224001411995022400141NM 1995 2 24 UPS202395 119950220A5311651766424 FRAME BOEING727 727173C 1384059NM BS 620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK, MAINTENANCE REPORTED CORROSION ON FRAME AT BS 620, STR 19R-23R. REPLACED FRAME AT BS 620, STR 19R-23R PER SRM 51-30-2. 2L73 4F A3WE 19950224001421995022400142NM 1995 2 24 UPS202402 119950216A53200807075O CHANNEL BOEING727 72727C 138400JNM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED LEFT MAIN ENTRY DOOR UPPER SIDE OF LOWER 'U' CHANNEL CORRODED. FABRICATED REPAIR PER SRM 51-40-1, 51-10-2, 51-20-4. 2L73 4F A3WE 19950224001431995022400143NM 1995 2 24 UPS202403 119950216A534715201257 SEAT TRACK BOEING727 72727C 138400JNM BS 740-820 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED SEAT TRACK CORRODED AT FS 740-820. FABRICATED AND INSTALLED SEAT TRACK PER SRM 53-10-5, 51-30-2, 53-10-2. 2L73 4F A3WE 19950224001441995022400144NM 1995 2 24 UPS202404 119950216A5720 ANGLE BOEING727 72727C 138400JNM BS 744 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED ATTACH ANGLES CRACKED AT WING CENTER SECTION LEFT SIDE AT STA 744. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2. 2L73 4F A3WE 19950224001451995022400145NM 1995 2 24 UPS202405 119950216A5330 SKIN BOEING727 72727C 138400JNM BS 259.7-277 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED FASTENER HOLES CRACKED AT BS 259.7-277, RT SIDE AT STR 9. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3, 51-30-2. 2L73 4F A3WE 19950224001461995022400146NM 1995 2 24 UPS202406 119950216A5743651929614 FITTING BOEING727 72727C 138400JNM LT/RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) CRACKED AND CORRODED, LEFT AND RIGHT MLG. REPLACED FITTING PER SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950224001471995022400147NM 1995 2 24 UPS202407 119950216A5743651929613 FITTING BOEING727 72727C 138400JNM LT/RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01907UP 19118 DURING 'C' CHECK, MAINTENANCE REPORTED FORWARD SUPPORT ATTACH FITTING (WING ATTACH) IS CRACKED. REPLACED FITTING PER SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950224001481995022400148NM 1995 2 24 UPS402408 119950214A575412634411 PDU BOEING747 747121 1384871NM NR 4 LE FLAP MALFUNCTION A IPXAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SO01691UP 19641 (SUPPLEMENTAL MRR) PILOT REPORTED THAT RIGHT NR 4 LEADING EDGE FLAP DID NOT EXTEND PNEUMATICALLY DURING APPROACH. EXTENDED FLAP ELECTRICALLY PER PROCEDURE. REPLACED NR 4 RT L/E FLAP PDU PER MM 27-81-03. 2L74 4F A20WE 19950224001491995022400149NM 1995 2 24 UPS402423 119950215A335033510301 EEL BOEING747 747123F NM UPPER DECK BROKEN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 DURING 'DAILY' CHECK, MAINTENANCE REPORTED UPPER DECK EMERGENCY LIGHT ASSY BROKEN. REPLACED LIGHT ASSY. 2L74 4F A20WE 19950224001501995022400150NM 1995 2 24 UPS502412 119950219A7120310N30241 MOUNT BOLTS BOEING757 75724APF 1384969NM RT ENGINE MOUNT LOOSE A AIPXAK NONE O OTHER ININSP/MAINT 1 SO01417UP 23904 DURING 'WEEKEND' CHECK, MAINTENANCE REPORTED RT ENGINE FORWARD MOUNT BOLTS FOUND BACKED OUT DURING INSPECTION. RESULTANT GAP BETWEEN ENGINE MOUNT SURFACES WAS .125 ALONG FWD PORTION, REDUCING TO .067 AT AFT PORTION. FORWARD MOUNT BOLTS AND BARREL NUTS WERE REPLACED AND TORQUED TO LIMITS PER UPS EO B757-7121-5743A. BOLT P/N: 310N3024-1. NUT P/N: VB13027-12. 2L72 4F RTA2NM 19950224001511995022400151WP 1995 2 24 UPS802396 119950220A53200502024T3 DOUBLER DOUG DC8 DC871F 302199DWP FS 960-980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED DOUBLER CORRODED AT FS 960-980, UPPER SURFACE OF WHEEL WELL, RBL 69. REPLACED DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950224001521995022400152WP 1995 2 24 UPS802397 119950220A53200507075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 857-879 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON DOUBLER AT FS 857-879, LBL 5, RBL 5. REPLACED DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950224001531995022400153WP 1995 2 24 UPS802398 119950220A53133141599712000 LONGERON DOUG DC8 DC871F 302199DWP FS 1698 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON LONGERON 30L, FS 1698. REPAIRED LONGERON PER SRM 51-1-20, 53-2-0. 2L74 4F RT4A25 19950224001541995022400154WP 1995 2 24 UPS802399 119950220A531557550327 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 1725 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION AT FLOOR BEAM AT FS 1725, RBL 24. REPAIRED BEAM PER UPS EO DC8-5310-6604A. 2L74 4F RT4A25 19950224001551995022400155WP 1995 2 24 UPS802400 119950220A5347527726604500 SEAT TRACK DOUG DC8 DC871F 302199DWP FS 1685-1700 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON NR 5 SEAT TRACK AT FS 1685-1700. REPLACED SEAT TRACK PER SRM 53-2-3. 2L74 4F RT4A25 19950224001561995022400156WP 1995 2 24 UPS802401 119950220A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 1660-1680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON INNER SKIN DOUBLER AT FS 1660-1680, LONGERON 27L-28L. REPAIRED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950224001571995022400157WP 1995 2 24 UPS802409 119950215A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1270-1275 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 DURING 'SPECIAL VISIT', MAINTENANCE REPORTED LONGERON 36 CRACKED FROM STA 1270-1275. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F RT4A25 19950224001581995022400158WP 1995 2 24 UPS802410 119950220A5312 J-BEAM DOUG DC8 DC873F 302199FWP AFT PRES BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 DURING B CHECK, MAINTENANCE REPORTED NR 3 AND NR 4 J-BEAM AT AFT PRESSURE BULKHEAD CRACKED. INSTALLED REPAIR PER UPS EO DC8-5310-6715A. 2L74 4F RT4A25 19950224001591995022400159WP 1995 2 24 UPS802411 119950217A5312 J BEAM DOUG DC8 DC871F 302199DWP AFT PRESS BULKHDCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 DURING 'B' CHECK, MAINTENANCE REPORTED AFT PRESSURE BULKHEAD 'J' BEAM CRACKED 4TH BEAM UP FROM BOTTOM. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6694. 2L74 4F RT4A25 19950224001601995022400160WP 1995 2 24 UPS802413 119950220A53200637075T6 STIFFENER DOUG DC8 DC871F 302199DWP FS 120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON RT VERTICAL STIFFENER AT STA 120, LONGERON 22R-27R. REPLACED STIFFENER PER SRM 51-1-20. 2L74 4F RT4A25 19950224001611995022400161WP 1995 2 24 UPS802414 119950220A53200327075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 220-260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON INNER DOUBLER AT FS 220-260, LONGERON 35L-30R. REPLACED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950224001621995022400162WP 1995 2 24 UPS802415 119950220A531157556005 FRAME DOUG DC8 DC871F 302199DWP FS 1140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON BELTFRAME CAP AT FS 1140, LONGERON 31R-31L. REPLACED CAP PER SRM 51-1-21. 2L74 4F RT4A25 19950224001631995022400163WP 1995 2 24 UPS802416 119950220A53115754671502 FRAME DOUG DC8 DC871F 302199DWP FS 1140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON BELTFRAME AT FS 1140, LONGERON 33L-35R. REPLACED FRAME PER SRM 51-1-20. 2L74 4F RT4A25 19950224001641995022400164WP 1995 2 24 UPS802417 119950220A53200717075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 1332-1335 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED CORROSION ON GUSSET DOUBLER AT FS 1332-1335, LONGERON 33R. REPLACED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950224001651995022400165WP 1995 2 24 UPS802418 119950220A532037592221 FITTING DOUG DC8 DC871F 302199DWP FS 1265 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 36 SPLICE FITTING CORRODED AT FS 1265. REPLACED FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950224001661995022400166WP 1995 2 24 UPS802419 119950220A53133648359 LONGERON DOUG DC8 DC871F 302199DWP FS 1360-1380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 36 CORRODED AT FS 1360-1380. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6637A. 2L74 4F RT4A25 19950224001671995022400167WP 1995 2 24 UPS802420 119950220A53203643759501 FITTING DOUG DC8 DC871F 302199DWP FS 920 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED VERTICAL ATTACH FITTING CORRODED AT STA 920, LBL 1. REPLACED FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950224001681995022400168WP 1995 2 24 UPS802421 119950220A531597746061 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 55 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED FLOOR BEAM CORRODED AT FS 55, RBL 12. REPAIRED PER UPS EO DC8-5310-6638A. 2L74 4F RT4A25 19950224001691995022400169WP 1995 2 24 UPS802422 119950220A531397746061 LONGERON DOUG DC8 DC871F 302199DWP FS 55 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED LONGERON 24L CRACKED AT FS 865 AND AT FS 895. REPLACED LONGERON PER SRM 51-1-20D. 2L74 4F RT4A25 19950224001701995022400170WP 1995 2 24 UPS802424 119950220A53135750198 LONGERON DOUG DC8 DC871F 302199DWP FS 860-880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 DURING 'C' CHECK, MAINTENANCE REPORTED RT WHEEL WELL LONGERON 24R CRACKED AT FS 860-880. REPAIRED PER UPS EO DC8-5310-6636A. 2L74 4F RT4A25 19950224001711995022400171WP 1995 2 24 UPS802425 119950218A3350 EEL CONNECTOR DOUG DC8 DC871F 302199DWP CABIN BROKEN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01705UP 45949 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT INTERMITTENT. REPLACED CONNECTOR AT TERMINAL BLOCK, CHECKS OK. 2L74 4F RT4A25 19950224001721995022400172WP 1995 2 24 UPS802426 119950218A3350 EEL WIRE DOUG DC8 DC871F 302199DWP CABIN BROKEN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01705UP 45949 MAINTENANCE REPORTED CABIN DOOR EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT BATTERY TERMINAL BLOCK. OPS CK OK. 2L74 4F RT4A25 19950224001731995022400173WP 1995 2 24 UPS802427 119950217A33505708458501 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01905UP 45949 MAINTENANCE REPORTED EMER EXIT LIGHTS INOP. REPLACED BATTERY PACK. OPS CK OK. 2L74 4F RT4A25 19950224001741995022400174NM 1995 2 24 95ZZZW123 119950130A5330 SKIN BOEING727 727231 1384079NM FS 490 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432761898 20234 MCI - DURING SPECIAL CHECK, FOUND CRACK IN LT LOWER LAP FUSELAGE SKIN, STA 490, LT STRINGER LAP 26L. CUT OUT CRACK AND CORROSION PER SRM 53-30-03 AND REPAIRED PER SRM 53-30-3 FIG 14. TOTAL CYCLES 42,197. 2L73 4F A3WE 19950224001751995022400175EU 1995 2 24 95ZZZW124 119950115A29101379305A77 HYDRAULIC LINE BAG JETSTMJETSTM3101 1500215EU RT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL07837JS 736 FLT 4133 - DURING CRUISE, 11,000 MSL FLIGHT CREW HEARD AN UNUSUAL NOISE FROM THE ENGINE NACELLES. BOTH HYDRAULIC PRESSURE GAUGES WERE AT NEAR '0' PSI INDICATION. ACFT DIVERTED TO HARRISBURG, PA WHERE IT MADE AN EMERGENCY LANDING WITHOUT INCIDENT. MAINTENANCE PERSONNEL DISCOVERED A BROKEN HIGH PRESSURE LINE IN RT ENGINE COMPARTMENT. LINE WAS REPLACED AND ACFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950224001761995022400176 1995 2 24 95ZZZW125 419950115A34256628196001 AHRS COMPUTER EMB 120 EMB120RT SO E/E BAY MALFUNCTIONED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07331JS 120035 FLT 4170 - SHORTLY AFTER TAKEOFF, THE CREW REPORTED A LOSS OF HSI AND RMI INDICATION. ACFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE REINITIALIZED BOTH AHRS COMPUTERS. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950224001771995022400177 1995 2 24 95ZZZW126 419950105A34148040B567N AIRSPEED IND BAG JETSTMJETSTM3101 1500215EU LT COCKPIT DEFECTIVE A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07851JS 834 FLT 4008 - SHORTLY AFTER TAKEOFF, FLIGHT CREW NOTICED A 100 KNOT DISCREPANCY BETWEEN CAPTAIN'S AND F/O'S AIRSPEED INDICATORS. CREW WAS ADVISED TO RETURN TO FIELD. PIT MAINTENANCE REPLACED CAPTAIN'S SIDE AIRSPEED INDICATOR. ACFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950224001781995022400178 1995 2 24 95ZZZW127 419950105A3414 AIRSPEED IND BAG JETSTMJETSTM3101 1500215EU LT COCKPIT MALFUNCTIONED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07839JS 748 FLT 4196 - SHORTLY AFTER TAKEOFF, THE CAPTAIN NOTICED HIS AIRSPEED INDICATOR WAS NOT OPERATING PROPERLY, HE ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. PIT MAINTENANCE PERSONNEL INSPECTED ACFT, CONDUCTED PITOT/STATIC AIRSPEED CHECK, COULD NOT DUPLICATE DISCREPANCY. ACFT RETURNED TO SERVICE WITH NO FURTHER INCIDENT. 2L72 4T RTA21EU 19950224001791995022400179NM 1995 2 24 95ZZZW128 119950207A3260 UNSAFE LIGHT BOEING727 727155C 138404ZNM LT MLG ILLUMINATED A DHLAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO01715DH 19618 DURING GEAR EXTENSION, LT MAIN RED UNSAFE LIGHT ON, GREEN LIGHT OUT. FOLLOWING MANUAL GEAR EXTENSION PROCEDURE, CRANK WOULD NOT MOVE. APPLYING PRESSURE EXTINGUISHED LIGHT AND ILLUMINATED GREEN LIGHT. MANUAL GEAR INDICATOR SHOWED GEAR DOWN. COLD WEATHER SENSOR PROBLEM SUSPECTED. PERFORMED GO AROUND, AND LANDED WITHOUT INCIDENT. OPS CHECK INDICATING SYSTEM, IAW BOEING MM 32-61-21 PG 501 AND 502. NO DEFECTS FOUND. 2L73 4F A3WE 19950224001801995022400180NM 1995 2 24 AWXA9500037 119950115A3350900835A EEL BATT PACK BOEING737 737112 1384412NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28708AW 19771 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT AFT EXTERIOR WING EMERGENCY EXIT LIGHT AND THE AFT CENTER AISLE INTERIOR EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F A16WE 19950224001811995022400181NM 1995 2 24 AWXA9500038 119950116A3350 EEL TERMINALS BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 7 AND 8. RESECURED LOOSE TERMINALS, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224001821995022400182NM 1995 2 24 AWXA9500039 119950116A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 10 THROUGH 14. REPAIRED LIGHT WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224001831995022400183NM 1995 2 24 AWXA9500040 119950117A3350 EEL ASSY BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTING INOPERATIVE. RESEATED PINS IN AFT ROW LIGHT ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224001841995022400184NM 1995 2 24 AWXA9500041 119950117A3350900835A EEL BATT PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224001851995022400185NM 1995 2 24 AWXA9500042 119950117A3350 EEL ASSEMBLY BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LAST THREE FLOOR PATH EMERGENCY EXIT LIGHTS IN AFT CABIN INOPERATIVE. RECONNECTED AND RESECURED LIGHT ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224001861995022400186NM 1995 2 24 AWXA9500046 119950125A5343 FITTING BOEING737 737222 1384473NM LT MLG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - FLT 31 - DURING C-8 INSPECTION, FOUND A .400 INCH CRACK IN LT MLG TRUNNION SUPPORT FITTING AT STA 706. BLEND REPAIR ACCOMPISHED IAW EO 53-46-06. (W) 2L72 4F A16WE 19950224001871995022400187NM 1995 2 24 AWXA9500047 119950125A5320 ANGLE BOEING737 737222 1384473NM FS 328 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - FLT 31 - DURING C-8 INSPECTION, FOUND INTERCOSTAL SUPPORT ANGLE CRACKED AT STA 328 RBL 35. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-1. (W) 2L72 4F A16WE 19950224001881995022400188NM 1995 2 24 AWXA9500048 119950125A5312 BLKHD ANGLE BOEING737 737222 1384473NM BS 294.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - FLT 31 - DURING C-8 INSPECTION, FOUND 7 CRACKS IN NOSE WHEEL WELL AFT VERTICAL BULKHEAD, STA 294.5 RBL 75, LOCATION 5TH FROM TOP TO 12TH. CRACKS WERE VERIFIED BY EDDY CURRENT. REPAIRED PER AWA EO 53-11-08 PART II. (W) 2L72 4F A16WE 19950224001891995022400189NM 1995 2 24 AWXA9500049 119950125A5312 INTERCOSTAL BOEING737 737222 1384473NM FS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - FLT 31 - DURING C-8 INSPECTION, FOUND INTERCOSTAL ON BULKHEAD 727 CRACKED BETWEEN LT VERTICAL FRAMES 4 AND 5. REPAIRED PER SRM 51-30-2 AND 53-10-02. (W) 2L72 4F A16WE 19950224001901995022400190NM 1995 2 24 AWXA9500083 119950205A335020131A EEL BATT CHARGER BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28154AW 23776 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LT BATTERY CHARGER ASSEMBLY, OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950224001911995022400191NM 1995 2 24 IXKA9500004 119950202A27511812993 POS INDICATOR BOEING727 727225 1384077NM TE FLAPS MALFUNCTIONED A IXKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25354PA 20624 ATL - FLT 73 - ON TAKEOFF, SPLIT FLAP CONDITION (I/B FLAPS WOULD NOT RETRACT BEYOND 5 DEGREES) USED ALTERNATED FLAP EXTENSION TO LOWER FLAPS. FLIGHT RETURNED TO ATL. REMOVED AND REPLACED I/B FLAP POSITION INDICATOR PER MM 27-51-00. OPS CHECK OK. (W) 2L73 4F A3WE 19950224001921995022400192WP 1995 2 24 USAA950009 119950101A2130 LINES DOUG DC9 DC982 3022082WP PRESS SYST LOOSE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19817US 48097 CLT - FLT 1133 - A VIBRATION WAS REPORTED IN THE FLOOR OF THE ACFT AND AFT JUMPSEAT AREA. THE CREW DECIDED TO DIVERT TO CLT. FOUND SENSE LINES TO LT AUGMENTATION VALVE AND PILOT PRESSURE REGULATORS LOOSE. TIGHTENED LINES. (W) 2L72 4F A6WE 19950224001931995022400193EU 1995 2 24 USAA950045 119950127A3230MS203922C11 PIN FOKKERF28 F28MK0100 4990807EU RT MLG SHEARED A USAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA19867US 11312 CLT - FLT 685 - AFTER TAKEOFF, BOTH MLG WOULD NOT RETRACT WHEN SELECTED UP. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT GEAR SEQUENCE VALVE BRACKET LEVER ATTACH PIN. CHECKS OK ON GEAR RETRACTION. (W) 2L72 4F RT 19950224001941995022400194 1995 2 24 USAA950048 419950123A2565D31873101 SLIDE FOKKERF28 F28MK0100 4990807EU EMRG EXIT DOOR FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19883US 11337 IND - ACCOMPLISHMENT OF JOB CARD J525-60-10 CALLS FOR SLIDE DEPLOYMENT. UPON DEPLOYMENT, SLIDE MOUNTED LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED SERVICE DOOR EVACUATION SLIDE. (W) 2L72 4F RT 19950224001951995022400195NM 1995 2 24 USAA950050 119950104A5320 FITTING BOEING737 7373B7 1384580NM BS 947.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA BS 947.5 RBL 48 INCHES SEAT TRACK ATTACH ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224001961995022400196NM 1995 2 24 USAA950051 119950103A533065479573 SKIN BOEING737 7373B7 1384580NM CARGO DR CUTOUT CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 SPOTS OF CORROSION 6 INCH BY 6 INCH AND 2 INCHES IN DIAMETER, 6 INCH BY 6 INCH AT FWD CORNER AND 2 INCHES IN DIAMETER AT AFT CORNER OF AFT CARGO DOOR CUTOUT. REPAIRED PER SRM 51-10-2 AND SRM 51-40-02. CORROSION TASK NR C53-100-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224001971995022400197NM 1995 2 24 USAA950052 119950104A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL OF FLOORBEAM, INSPECTION FOUND TOTAL OF 8 INCHES IN VARIOUS LOCATIONS CORROSION BS 328 BETWEEN BL 0 AND RBL 56. REPAIRED PER TR 53-107-12. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. 2L72 4F RTA16WE 19950224001981995022400198NM 1995 2 24 USAA950054 119950104A5320655287897 ANGLE BOEING737 7373B7 1384580NM BS 947-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 80 INCH CORRODED AREA BS 947 TO BS 1016 LT SIDE 'Z' ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224001991995022400199NM 1995 2 24 USAA950055 119950104A5320654587545 Z ANGLE BOEING737 7373B7 1384580NM BS 294.5-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA APPROX 46 INCHES BY 2 INCHES 'Z' ANGLE I/B OF GALLEY SERVICE DOOR WL 207.5 FROM BS 294.5 TO BS 328. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002001995022400200NM 1995 2 24 USAA950056 119950109A53201123845 'Z' ANGLE BOEING737 7373B7 1384580NM FS 310-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 34 INCHES CORRODED AREA 'Z' ANGLE AT FWD ENTRY DOOR STA. 310 TO 344. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002011995022400201NM 1995 2 24 USAA950057 119950109A532065C161219 ATTACH FITTINGS BOEING737 7373B7 1384580NM LT DR GIRT BAR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AREA ON LT ENTRY DOOR GIRT BAR ATTACH FITTINGS BOTH FRONT AND AFT. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002021995022400202NM 1995 2 24 USAA950058 119950104A5347 SEAT TRACK BOEING737 7373B7 1384580NM BS 270-294.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND THREE AREAS, 1 INCH BY .250 INCH, .500 INCH BY .250 INCH, 1 INCH BY 1.25 INCH CORRODED, FWD OF GALLEY SERVICE DOOR BS 270 TO BS 294.5 - 42.0 O/B OF BBL 0. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002031995022400203NM 1995 2 24 USAA950059 119950104A5347 SEAT TRACK BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION OF SEAT TRACKS, FOUND CORRODED AREA APPROXIMATELY 29.0 INCHES BY 1.25 INCHES, BS 328 - 10 INCHES AFT OF BS 359.96 APPROX 20 INCHES O/B OF BBL 0. REPAIRED PER SRM 53-00-52. CORRODED TASK NR C3-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002041995022400204NM 1995 2 24 USAA950060 119950123A532065C10592154 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION OF INTERCOSTAL, FOUND 1 INCH BY 6 INCH CORRODED AREA, BS 947 THROUGH BS 967 LBL 48 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002051995022400205NM 1995 2 24 USAA950061 119950104A5320 BEAM BOEING737 7373B7 1384580NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL NUT PLATE HOLES .25 INCH BY .25 INCH AREA CORRODED, BS 986 'T' CAP CLIP NUT HOLES. REPAIRED PER TR 53-15-01A. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950224002061995022400206EU 1995 2 24 USAA950086 119950203A3030853BRM0D2 PITOT FOKKERF28 F28MK0100 4990807EU FWD RT FUS INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19888AU 11357 CLT - FLT 460 - DURING FLIGHT THE NR 2 PITOT HEAT FAULTED. C/B WAS NOT POPPED. RECYCLED AND FAULTED AGAIN. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 PITOT HEAD. PITOT AND HEAT CHECK NORMAL. (W) 2L72 4F RT 19950224002071995022400207EU 1995 2 24 USAA950088 119950205A33506104781 EEL BATT PACK FOKKERF28 F28MK0100 4990807EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19894US 11379 PIT - FLT 883 - DURING PREFLIGHT, FOUND FLT DECK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATION CHECKS NORMAL. (W) 2L72 4F RT 19950224002081995022400208NM 1995 2 24 USAA950089 119950102A32201H32345221 LEG ASSEMBLY BOEING737 7373B7 1384580NM NLG SHEARED OFF A USAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA19525AU 23860 PHL - FLT 2394 - ON TAXI IN, LT NOSE WHEEL SHEARED OFF. MAINTENANCE PINNED GEAR AND TOWED ACFT TO GATE. MAINTENANCE REPLACED NOSE LANDING GEAR LOWER LEG ASSEMBLY. (W) 2L72 4F RTA16WE 19950224002091995022400209EU 1995 2 24 VTZA95046 119950207A32609EN1C11HBB2 DNLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NLG BROKEN A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27478UE 892 IAD-SYR - FLT 6338 - DURING APPROACH, DECLARED AN EMERGENCY DUE TO CREW HAVING TO CYCLE THE NOSE GEAR TWICE TO GET A NOSE GEAR DOWN AND LOCKED INDICATION. ACFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE ON THE NOSE GEAR DOWNLOCK MICROSWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950224002101995022400210EU 1995 2 24 VTZA95047 119950205A3222105A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NLG FAILED A AVTZAG O2 MASK DEPLOYED O OTHER CRCRUISE 1 EA27480UE 894 ROC-IAD - FLT 6336 - DURING CRUISE, THERE WAS A RAPID CABIN DECOMPRESSION AT 17,000 FEET. IT TOOK APPROXIMATELY 30 SECONDS TO REACH 0 PSI. THERE WERE NO STRUCTURAL OR WINDOW DEFECTS NOTED BY THE FLIGHT CREW. ACFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 20008 ON 02-08-95 BY REPACKING THE NOSE STRUT. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950224002111995022400211EU 1995 2 24 VTZA95048 119950205A32609EN1C11HBB2 DNLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NLG BROKEN A VTZAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA27494UE 810 IAD-FLT 6596 - DURING THE APPROACH PORTION OF THE MAINTENANCE ACCEPTANCE FLIGHT, THE NOSE GEAR WOULD NOT INDICATE DOWN AND LOCKED. AN EMERGENCY WAS DECLARED AND ACFT LANDED IN IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED BROKEN WIRES AT DOWNLOCK MICROSWITCH. PERFORMED GEAR SWING, OPS CHECK GOOD. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950224002581995022400258SO 1995 2 24 95ZZZZ88 119950130A2613 CONNECTOR LKHEED382 382G 526414USO NR 2 NACELLE LOOSE A SRAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO19920SJ 4561 DURING TAXI OUT FOR FLIGHT NR ADT 3 FROM MHZ, NR 2 NACELLE OVERHEAT LIGHT CAME ON. FOUND NR 2 NACELLE OVERHEAT PROBE CONNECTION LOOSE AND NR 2 MISG PLUG WET DUE TO DE-ICING, DRIED CANNON PLUG AND TIGHTEN CONNECTIONS, OPS CHECKED GOOD. 2H74 4T A1SO 19950224002591995022400259WP 1995 2 24 95ZZZZ89 119950131A7722CALL503 EGT HARNESS DOUG DC8 DC873F 302199FWP LT/RT ENG FAILED A SRAAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19874SJ 46149 AFTER TAKEOFF ON FLIGHT NR 197 FROM DUBAI, NR 1 ENGINE EGT WENT OFF SCALE HIGH, SHUT DOWN ENGINE AND DUMPED FUEL TO LANDING WEIGHT AND PERFORMED AIR TURN BACK TO DUBAI. INSPECTED ENGINE AND FOUND NO OBVIOUS DEFECTS, SUSPECT EGT HARNESS, REPLACED LEFT AND RIGHT EGT HARNESS, OPS CHECKED GOOD. (Z) 2L74 4F RT4A25 19950224002601995022400260SO 1995 2 24 95ZZZZ90 119950121A3231 ROD LKHEED382 382B 5264104SO LT MLG DOOR LOOSE A SRAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO19916SJ 4134 DURING FLIGHT NR ADT4, CREW FELT VIBRATION FROM LEFT WHEEL WELL, REDUCED AIRSPEED AND ALTITUDE THEN DIVERT TO AVB. FOUND OUTER DOOR ACTUATION ROD NOT SECURED TO DOOR, SECURED ROD AND PERFORMED VISUAL INSPECTION OF WHEEL WELL, NO DEFECTS FOUND. 2H74 4T A1SO 19950224002611995022400261NM 1995 2 24 AWXA9500075 119950130A3350900835A EEL POWER SUPPLY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28181AW 22648 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 16 AND 17 SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT 18 LT, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950224002621995022400262NM 1995 2 24 AWXA9500076 119950101A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 7 THROUGH 9. REPAIRED WIRES, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950224002631995022400263NM 1995 2 24 AWXA9500077 119950131A335020131A EEL BATT CHARGER BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 18 TO 21. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950224002641995022400264 1995 2 24 AWXA9500078 419950202A3416B180081103 ALTIMETER BOEING737 737112 1384412NM LT COCKPIT INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28708AW N0031 19771 PHX - FLT 574 - PHX-OAK - AIR TURNBACK - AFTER TAKEOFF, THE CAPTAINS ELECTRIC ALTIMETER STAYED IN ONE POSITION. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS ELECTRIC ALTIMETER. OPS CHECK NORMAL PER MM 34-12-00. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950224002651995022400265NM 1995 2 24 AWXA9500079 119950207A5320 ANGLE BOEING737 737277 1384570NM FS 520 BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 PHX - FLT 1590 - DURING C8 INSPECTION, FOUND WIRE HARNESS SUPPORT ANGLE BRACKET FORWARD ATTACH POINT BROKEN BETWEEN STATION 520 AND 540 RBL 45. WIRES CHAFING ENGINE CONTROLS. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2. INSPECTED AND FOUND NO DAMAGE TO WIRES OR CONTROLS. (Z) 2L72 4F RTA16WE 19950224002661995022400266NM 1995 2 24 AWXA9500080 119950207A5315 FLOOR BEAM WEB BOEING737 737277 1384570NM FS 520 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 PHX - FLT 1590 - DURING C8 INSPECTION, FOUND INTERCOSTAL WEB CRACKED, FORWARD SIDE OF STATION 520 FLOOR BEAM AT RBL 24.75 LBL 24.75 AND LBL 45.5. INSTALLED NEW WEB AND ANGLE PER SRM 51-30-2 AND 51-10-1. (Z) 2L72 4F RTA16WE 19950224002671995022400267NM 1995 2 24 AWXA9500081 119950207A53206546575517 SHEAR TIE BOEING737 737277 1384570NM FS 1138 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28186AW 22653 PHX - FLT 1590 - DURING C8 INSPECTION, FOUND CRACK IN FRAME AT BS 1138, STRINGER 5L AND 12L. REPAIRED BY INSTALLATION OF NEW SHEAR TIE AND STRAP PER SRM 51-30-2. (Z) 2L72 4F RTA16WE 19950224002681995022400268NM 1995 2 24 MGMA950037 119950107A3350900835A EEL BATTERY PACKGRIMES BOEING727 727191 1384063NM CABIN DISCHARGED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23504MG 24649 19395 CENTER OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CHECKED NORMAL. TOTAL CYCLES 42,010. (Z) 2L73 4F A3WE 19950224002691995022400269WP 1995 2 24 MGMA950048 119950117A3350307 EEL LAMP GRIMES DOUG DC8 DC862 3021970WP CABIN FAILED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23803MG 45910 EMERGENCY FLOOR TRACK LIGHTS INOP SEATS 7 THROUGH 10. RELAMPED, OPS CHECK OK, TOTAL CYCLES 12,451. (Z) 2L74 4F 4A25 19950224002701995022400270WP 1995 2 24 MGMA950058 119950117A3350307 EEL LAMP DOUG DC8 DC862 3021970WP CABIN FAILED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23803MG43161 45910 EMERGENCY FLOOR TRACK LIGHTS INOP SEATS 20 THROUGH 23. RELAMPED, OPS CHECK OK. TOTAL CYCLE 12,451. (Z) 2L74 4F 4A25 19950224002711995022400271WP 1995 2 24 MGMA950068 119950117A3350307 EEL LAMP GRIMES DOUG DC8 DC862 3021970WP CABIN FAILED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23803MG 45910 EMERGENCY FLOOR TRACK LIGHTS INOP SEAT 3. RELAMPED, OPS CHECK OK. TOTAL CYCLES 12,451. (Z) 2L74 4F 4A25 19950224002721995022400272WP 1995 2 24 MGMA950078 119950117A35306350A33UUUC OXY BOTTLE DOUG DC8 DC862 3021970WP COCKPIT EMPTY A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23801MG44681 45986 EMERGENCY OXYGEN BOTTLE EMPTY. REPLACED OXYGEN BOTTLE. LEAK CHECK NORMAL. TOTAL CYCLES 14,724. (Z) 2L74 4F 4A25 19950224002731995022400273WP 1995 2 24 MGMA950088 119950117A3350307 EEL LAMP DOUG DC8 DC862 3021970WP CABIN INOP A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23801MG44681 45986 EMERGENCY FLOOR TRACK LIGHTS INOP SEAT 6A. RELAMPED, OPS CHECK OK. TOTAL CYCLES 14,724. (Z) 2L74 4F 4A25 19950224002741995022400274WP 1995 2 24 MGMA950098 119950117A3350307 EEL LAMP DOUG DC8 DC862 3021970WP CABIN INOP A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23801MG44681 45986 EMERGENCY FLOOR TRACK LIGHTS INOP SEAT 20A. RELAMPED, OPS CHECK OK. TOTAL CYCLES 14,724. (Z) 2L74 4F 4A25 19950224002751995022400275WP 1995 2 24 MGMA950108 119950117A3350307 EEL LAMP DOUG DC8 DC862 3021970WP CABIN FAILED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23801MG44681 45986 EMERGENCY FLOOR TRACK LIGHTS MISSING LENS, SEAT 7A AND 8A. REPLACED LENS AND LAMP. OPS CHECK OK. TOTAL CYCLES 14,724. (Z) 2L74 4F 4A25 19950224002761995022400276WP 1995 2 24 MGMA950118 119950117A3350307 EEL LAMP DOUG DC8 DC862 3021970WP CABIN FAILED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23801MG44681 45986 EMERGENCY FLOOR TRACK LIGHTS INOP SEAT 2A. RELAMPED, OPS CHECK OK. TOTAL CYCLES 14,724. (Z) 2L74 4F 4A25 19950224002771995022400277NM 1995 2 24 RAAAB195001 119950105A5320 ANGLE BOEING727 72722C 138400FNM BS 5940 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV53454 19093 LEFT STRINGER 18 SILL ANGLE CHORD CRACKED AT BS 950. REMOVED CRACKED ANGLE CHORD AT BS 940-950 WEB MATERIAL. INSTALLED REPAIR PER SB 727-53-140 FIG 1 AND 2. (Z) 2L73 4F A3WE 19950224002781995022400278NM 1995 2 24 RAAAB195002 119950105A5320 ANGLE BOEING727 72722C 138400FNM BS 5940 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV53454 19093 RT STRINGER 18 SILL ANGLE CHORD CRACKED AT BS 950. REMOVED CRACKED ANGLE CHORD AT BS 940-950 WEB MATERIAL, INSTALLED REPAIR PER SB 727-53-140 FIG 1 AND 2. (Z) 2L73 4F A3WE 19950224002791995022400279NM 1995 2 24 RAAAB195004 119950112A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 1070 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING PERFORMANCE OF 3 YEAR CPCP INSPECTION PER CARD S3-54102, FOUND FLOOR BEAM CRACKED AT FASTENER HOLE BS 1070 RBL 3. REPAIRED PER SRM 51-40-4 FIG 1. 2L73 4F A3WE 19950224002801995022400280NM 1995 2 24 RAAAB195005 119950112A5311 CIRCUMFERENTIAL BOEING727 72722C 138400FNM BS 990 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING PERFORMANCE OF 3 YEAR CPCP INSPECTION PER CARD S3-54102, FOUND CORROSION ON FWD FACE OF CIRCUMFERENTIAL BS 990 INBD OF STRINGER 29R AT FUSELAGE ATTACH RIVETS. REPAIRED PER SRM 53-10-4 FIG 11, SHEET 2 AND 3. (Z) 2L73 4F A3WE 19950224002811995022400281NM 1995 2 24 RAAAB195006 119950112A5313 STRINGER BOEING727 72722C 138400FNM BS 1110 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING PERFORMANCE OF 3 YEAR CPCP INSPECTION PER CARD S3-54102, FOUND CORROSION IN STRINGER 29R AT BS 1110. REPAIRED PER SRM 53-10-3 FIG 1, SHEET 4, DETAIL I. (Z) 2L73 4F A3WE 19950224002821995022400282NM 1995 2 24 RAAAB195007 119950112A5322 SHEAR TIE BOEING727 72722C 138400FNM B S 600 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING PERFORMANCE OF 3 YEAR CPCP INSPECTION PER CARD S3-52102, FOUND CRACKED SHEAR TIE BETWEEN STRINGERS 26R AND 25R B-5-600. REPAIRED PER SRM 53-10-2 SECTION 43, FIG 3. (Z) 2L73 4F A3WE 19950224002831995022400283EU 1995 2 24 WTAA950065A 119950127A261260261210SN CONNECTOR BAG JETSTMJETSTM3101 1500215EU FS 187.15 MOISTURE A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17107XV 723 SFO - RT ENGINE FIRE BELL, CAPTION LIGHT AND FIRE LIGHT ACTIVATED WHEN ELECTRICAL BUS IS POWERED. MAINTENACNE CLEANED MOISTURE FROM FIRE CONTROL UNIT CONNECTORS AND ZONE II FIRE WIRE ASSEMBLY. RIGHT ENGINE FIRE WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950224002841995022400284EU 1995 2 24 WTAA950065B 119950127A2612D2370120 FIRE WIRE BAG JETSTMJETSTM3101 1500215EU RT ENGINE MOISTURE A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17107XV 723 SFO - RIGHT ENGINE FIRE BELL, CAPTION LIGHT AND FIRE LIGHT ACTIVATED WHEN ELECTRICAL BUS IS POWERED. MAINTENANCE CLEANED MOISTURE FROM FIRE CONTROL UNIT CONNECTORS AND ZONE II FIRE WIRE ASSEMBLY. RIGHT ENGINE FIRE WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950224002851995022400285EU 1995 2 24 WTAA950066 119950127A261251224127 FIRE LOOP BAG JETSTMJETSTM3101 1500215EU RT ENGINE SHORTED A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17107XV 723 MOD - RIGHT ENGINE FIRE BELL, CAPTION LIGHT AND FIRE LIGHT ACTIVATED IN FLIGHT. NO SMOKE OR FIRE VISABLE. MAINTENANCE DETERMINED INDICATION TO BE FALSE FOLLOWING INSPECTION OF RT ENGINE AND FIRE WARNING SYSTEM. REPLACED RIGHT ENGINE FORWARD FIRE LOOP. FIRE WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950224002861995022400286SO 1995 2 24 WTAA950068 119950130A524612016900010 FUEL DOOR EMB 120 EMB120RT SO RT WING NOT LATCHED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17451UE 120108 FAT - SERVICE DOOR WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESECURED OUTBOARD FUEL SERVICE DOOR LATCH. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950224002871995022400287SO 1995 2 24 WTAA950076 119950207A3350D36604001 EEL BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17284UE 120145 RDM - CABIN EMERGENCY LIGHTS FAIL TO TEST. MAINTENANCE REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY PACK AT ROW 6. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950224002881995022400288NE 1995 2 24 WTAA950077 219950209A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A AWTAAE ENGINE SHUTDOWN BJMSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OVER TEMP CRCRUISE 1 WP17122AM 120013 115028 SFO - EN ROUTE FAT TO SFO, LEFT ENGINE RISE IN T6 INDICATION TO 850 DEGREES REPORTED FOLLOWED BY POPPING NOISE, VIBRATION AND POWER SURGE FROM ENGINE. CREW ACCOMPLISHED SHUT DOWN OF LEFT ENGINE AND DECLARED AND EMERGENCY. AIRCRAFT LANDED AT STATION WITHOUT INCIDENT. CREW SUBSEQUENTLY REPORTED SMOKE ODOR IN CABIN FROM NR 1 PACK FOLLOWING ABOVE ENGINE OCCURRENCE. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. AIRCRAFT RETURNED TO SERVICE. AWAITING ENGINE TEARDOWN EVALUATION TO DETERMINE CAUSE. (Z) 2L72 4T4 TRTA31SO E20NE 19950224002891995022400289NM 1995 2 24 95UAL727014 119950209A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297287U 21565 EMERGENCY EXIT LIGHT ABOVE AIRSTAIRS STAYS ON. REPLACED BATTERY PACK AND BASE. 2L73 4F4 F A3WE E2EA 19950224002901995022400290NM 1995 2 24 95UAL727015 119950209A3350 EEL STRIP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297457U 21911 EMERGENCY EXIT LIGHTS LEFT FLOOR STRIP LOOSE AND BUCKLING, REPAIRED. 2L73 4F4 F A3WE E2EA 19950224002911995022400291NE 1995 2 24 95ZZZX839 219950206A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RIGHT FAILED A TWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE05904TW 49156 MCI - FLT 119 - DURING CLIMB, RIGHT ENGINE LOST POWER. SHUT DOWN ENGINE. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE SN 3257. ENGINE TOTAL TIME: 19,850 HOURS; 10,375 CYCLES. CHECK C-2D - 1-13-94 - MCI. 2L72 4F4 F A6WE E9NE 19950224002921995022400292WP 1995 2 24 95ZZZX840 119950126A5330 SKIN LKHEED1011 1011385115 5265015WP FS 760 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND SKIN CRACK ON LEFT SIDE OF FUSELAGE BETWEEN STR 39 AND STR 40, STA 760. INSTALLED DOUBLER REPAIR PER SRM 53-30-02, FIGURE 201. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224002931995022400293WP 1995 2 24 95ZZZX841 119950126A5312 WEB LKHEED1011 1011385115 5265015WP AFT PRESS BLKHD CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND A ONE INCH CRACK IN AFT PRESSURE BULKHEAD WEB. INSTALLED REPAIR PER SRM 53-11-00, PAGE 808, FIGURE 805. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224002941995022400294WP 1995 2 24 95ZZZX842 119950126A5312 RIVETS LKHEED1011 1011385115 5265015WP PRESS BLKHD MISSING A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND TWO RIVETS MISSING FROM AFTER PRESSURE BULKHEAD AND AREA BULGE AT SIX O'CLOCK POSITION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-11-00, PAGE 808. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224002951995022400295WP 1995 2 24 95ZZZX843 119950126A5330 SKIN LKHEED1011 1011385115 5265015WP FS 585 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND SKIN CRACK ON RIGHT SIDE OF FUSELAGE OUT OF RIVET HOLE, STA 585, STR 30. REPAIRED BY INSTALLING DOUBLER PER SRM 53-31-00, PAGE 828. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224002961995022400296WP 1995 2 24 95ZZZX844 119950126A5312 FORMER RING LKHEED1011 1011385115 5265015WP BLKHD CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND CORROSION ON FORMER RING AT SIX O'CLOCK POSITION IN AREA OF DRAIN HOLES, FORWARD SIDE OF PRESSURE BULKHEAD AFT OF LAVATORY TANK. REMOVED CORROSION SECTION OF FORMER RING AND SPLICED IN NEW SECTION PER SRM 53-11-00, PAGE 815. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224002971995022400297WP 1995 2 24 95ZZZX845 119950126A5753 TE WEDGE LKHEED1011 1011385115 5265015WP TE FLAP DAMAGED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND CRUSHED TRAILING EDGE OF NR 2 TRAILING EDGE FLAP, OUTBOARD END. REMOVED DAMAGED WEDGE AND INSTALLED NEW SECTION PER SRM 57-54-00, PAGE 12. AIRCRAFT TOTAL TIME: 63,846 HOURS; 31,029 CYCLES. 2L73 4F A23WE 19950224002981995022400298WP 1995 2 24 95ZZZX846 119950126A5312 BULKHEAD LKHEED1011 1011385115 5265015WP FS 1809 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND CORROSION AT SIX O'CLOCK POSITION OF DRAIN HOLES FORWARD OF PRESSURE BULKHEAD STA 1809. REMOVED DOUBLER, REPAIRED FRAME PER SRM 51-50-03, AND REINSTALLED ORIGINAL DOUBLER. AIRCRAFT TOTAL TIME: 63,846 HOURS; 31,029 CYCLES. 2L73 4F A23WE 19950224002991995022400299WP 1995 2 24 95ZZZX847 119950120A5713 STRINGER LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK, FOUND 1.50 INCH CRACK AT RIGHT WING F/T, STA 555 CASTELLATION, UPPER STR 14. INSTALLED NEW CHORD ANGLE PER DWG 1647070. AIRCRAFT TOTAL TIME: 59,628 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224003001995022400300WP 1995 2 24 95ZZZX848 119950125A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK, FOUND A 1 INCH CRACK IN IWS 555 RIB UPPER CAP CASTELLATION, AT 14 STRINGERS FORWARD OF REAR SPAR ABOVE RIB CUT OUT, LT WING. REPAIRED UPPER RIB CAP AT IWS 555 ST STR 18 AND STR 19, PER ARA 867. AIRCRAFT TOTAL TIME: 59,628 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224003011995022400301WP 1995 2 24 95ZZZX849 119950120A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK - FOUND .75 INCH CRACK IN RT WING INTERNAL UPPER RIB CAP, IN AFT RADIUS, IWS 555, OUTBOARD SIDE, SIXTH STRINGER FROM AFT STR 13. INSTALLED UPPER CHORD ANGLE PER DWG. NR. 1647070. AIRCRAFT TOTAL TIME 59,628 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224003021995022400302NM 1995 2 24 95ZZZX850 119950120A5313 STRINGER BOEING727 727231 1384079NM BS 990 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554351 21983 MCI - DURING CHECK C-2D, FOUND A 6 INCH CRACK AT STR 29R, BS 990, OUTBOARD SIDE OF BOTTOM RADIUS. STOP DRILLED CRACK PER SRM 51-10-1, PAGE 6A, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440. ACFT TOTAL TIME: 37,342 HOURS; 24,204 CYCLES. 2L73 4F A3WE 19950224003031995022400303WP 1995 2 24 95ZZZX851 119950201A3260H146 DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP RT MLG FAILED A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05980Z 47344 STL - FLT 641 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR. REPLACED RIGHT MLG DOWNLOCK SWITCH, MFG PN H14-6. LANDING GEAR OPERATION AND POSITION AND WARNING SYSTEM CHECKED NORMAL. CHECK C - 1-28-94 - MCI. 2L72 4F A6WE 19950224003041995022400304NM 1995 2 24 95ZZZX852 119950120A5320 TIE BOEING727 727231 1384079NM STR 29R CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554351 21983 MCI - DURING CHECK C-2D, FOUND CORROSION AT END OF LONGERON TIE TO STR 29R. REMOVED CORROSION PER SRM 51-10-6, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440. AIRCRAFT TOTAL TIME: 37,342 HOURS; 24,204 CYCLES. 2L73 4F A3WE 19950224003051995022400305WP 1995 2 24 95ZZZX853 119950126A5330 SKIN LKHEED1011 1011385115 5265015WP FS 1512 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 JFK - DURING CHECK C-3B, FOUND CORROSION ON INNER SKIN AT STA 1512, BETWEEN STR 32 AND STR 33 UNDER CARGO COMPARTMENT FLOOR. REMOVED CORROSION AND INSTALLED TEAR STRAP DOUBLER AND REPAIR DOUBLER PER SRM 53-31-00, PAGE 829, FIGURE 815. AIRCRAFT TOTAL TIME: 63,846 HOURS; 17,917 CYCLES. 2L73 4F A23WE 19950224003061995022400306NM 1995 2 24 95ZZZX854 119950125A5330 SKIN BOEING727 727231 1384079NM FS 1110-1120 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0584357 21989 DURING OP-17, FOUND FUSELAGE TOP SKIN AT STA 1110 TO STA 1120 DENTED LEFT AND RIGHT OF BL 0. REPAIRED PER SRM 53-30-3, FIGURE 3. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES. 2L73 4F A3WE 19950224003071995022400307WP 1995 2 24 95ZZZX855 119950205A49903812761 APU DOUG DC9 DC982 3022082WP AFT FUSELAGE OIL LEAK A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05916TW 49187 STL - FLT 409 - AFTER TAKEOFF, A NOTICEABLE SMOKE AND ODOR APPEARED IN CABIN, DISSIPATED DURING CLIMB. FOUND APU, MFG PN 381276-1, LEAKING OIL INTO AIR CONDITIONING SYSTEM. PLACARDED APU INOPERATIVE. PER THE MINIMUM EQUIPMENT AND DISPATCH PROCEDURES MANUAL, 49-1. CHECK C-1D - 1-395 - MCI. 2L72 4F A6WE 19950224003081995022400308WP 1995 2 24 95ZZZX856 119950120A5311 FRAME DOUG DC9 DC932 3022066WP RIGHT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05996Z 47028 STL - DURING OP-15, FOUND A ONE INCH CRACK IN RT MAIN FRAME, COMING FROM AFT LOWER HOLE ATTACHED TO TRAPEZOID PANEL. REPAIRED PER SSRM 53-60-102. AIRCRAFT TOTAL TIME: 70,380 HOURS: 78,720 CYCLES. 2L72 4F A6WE 19950224003091995022400309NM 1995 2 24 95ZZZX857 119950205A3232731414 ACTUATOR BOEING727 727231 1384079NM RT MLG DOOR MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0552310 19829 STL - FLT 297 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN WHEELWELL DOOR LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR. FOUND DOOR HYDRAULIC ACTUATOR, MFG 7-3141-4, BYPASSING. REPLACED RIGHT MLG DOOR ACTUATOR. LANDING GEAR DOOR AND DOOR INDICATION SYSTEM OPERATION CHECKED NORMAL. CHECK C-2 - 8-19-94 - MCI. 2L73 4F A3WE 19950224003101995022400310WP 1995 2 24 95ZZZX858 119950124A5313 LONGERON DOUG DC9 DC932 3022066WP FS 718 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05996Z 47028 STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 8L, STA 718. REPAIRED PER SRM 53-02, FIGURE 2, PAGE 2A. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES. 2L72 4F A6WE 19950224003111995022400311WP 1995 2 24 95ZZZX859 119950124A5313 SPLICE DOUG DC9 DC932 3022066WP FS 414 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05996Z 47028 STL - DURING OP-15, FOUND .25 INCH CRACK IN FORWARD CARGO BIN LONGERON 30 AND IN LONGERON SPLICE, STA 414. INSTALLED NEW SECTION OF LONGERON AND REPLACED SPLICE PLATE. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES. 2L72 4F A6WE 19950224003121995022400312WP 1995 2 24 95ZZZX860 119950120A5530 ATTACH ANGLE DOUG DC9 DC951 3022051WP VERTICAL STAB CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05409EA 47728 STL - DURING CHECK C, FOUND A .25 INCH CRACK IN VERTICAL STABILIZER RIGHT DORSAL FIN ATTACH ANGLE, FROM FASTENER HOLE TO EDGE. REPAIRED PER SRM 51-30 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 38,864 HOURS; 35,359 CYCLES. 2L72 4F A6WE 19950224003131995022400313WP 1995 2 24 95ZZZX861 119950123A5313 LONGERON DOUG DC9 DC932 3022066WP FS 639/658 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05996Z 47028 STL - DURING OP-15, FOUND CRACK IN LONGERON 6R, STA 639 AND STA 658, APPROXIMATELY .1250 INCH TO .50 INCH. REPAIRED PER SRM 53-02 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 70,380 HOURS; 78,720 CYCLES. 2L72 4F A6WE 19950224003141995022400314NE 1995 2 24 95ZZZX862 219950110A7321 FUEL CONTROL CESSNA500 560CESSNA 2076750CE PWA JT15 JT15D5 52112NE LT ENGINE MALFUNCTIONED A WJCAO OTHER X ENGINE FLAMEOUT LDLANDING 1 EA11147VC 5600105 PCE108222 ON 1-10-95, AIRCRAFT WAS ON LANDING ROLL INTO LUNKIN FIELD (LUK), OHIO WHEN THE LEFT ENGINE FLAMED OUT. THE ACFT TAXIED INTO LOCAL F80 ON ONE ENGINE WITH NO OTHER COMPLICATIONS. THE ACFT WAS EVALUATED FOR CAUSE OF THE FLAME OUT AT EXECUTIVE JET MANAGEMENT AT LUK. NO OBVIOUS REASON WAS FOUND. AFTER COMMUNCIATIONS WITH PRATT & WHITNEY AS TO THE SAFETY OF OPERATIONS K-C AVIATION DECIDED TO MOVE ACFT TO CESSNA FACILITY IN GREENSBORO, N.C. ON A FERRY AUTHORIZATION. WHILE THERE, THE RIGGING WAS ADJUSTED, THE FLOW DIVIDER WAS REPLACED AND A FUEL CONTROL UNIT WAS INSTALLED. OPS CHECK OKAY. RTS 1-13-95. 2L72 4F4 FRTA22CE E25EA 19950224003151995022400315NM 1995 2 24 95ZZZX863 119950129A243223013 BATTERY CHARGER BOEING737 737247 138448DNM A E COMPT FAILED A A6XAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO134515W 19612 BATTERY CHARGER SYSTEM CIRCUIT BREAKER TRIPPED FOLLOWED BY SMOKE IN THE COCKPIT. INTERNAL SHORTED BATTERY CHARGER FOUND AT FAULT. 2L72 4F A16WE 19950224003161995022400316WP 1995 2 24 95ZZZX864 119950110A5330 SKIN DOUG DC9 DC932 3022066WP FS 110-150 DAMAGED A VJ6AD RETURN TO BLOCK C F.O.D. TXTAXI/GRND HDL 1 SO11922VV 47489 MEM/ATL - FLT 147 - AIRCRAFT RETURNED TO GATE TO GET MORE PASSENGERS. WITH ENGINES RUNNING TOW BAR BROKE AND TUG JACKKNIFED, CAUSING DAMAGE TO BELLY SKIN FROM STA 110 TO STA 150. REPAIR TO BE MADE BY DOUGLAS AIRCRAFT CORPORATION. 2L72 4F A6WE 19950224003171995022400317WP 1995 2 24 95ZZZX865 119950120A213339271411 PRESS REG VALVE DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11922VV 47489 ATL/MDW - FLT 240 - RETURNED TO ATL DUE TO FLIGHT CREW COULD NOT PRESSURIZE AIRCRAFT IN AUTO OR MANUAL. REPLACED PRESSURIZED REGULATION VALVE FOR LEFT AIR CONDITIONING PACK AND SEGMENT. 2L72 4F A6WE 19950224003181995022400318 1995 2 24 95ZZZX866 419950115A3421258733511 VERTICAL GYRO DOUG DC9 DC932 3022066WP NR 2 FAILED A VJ6AA UNSCHED LANDING JI WARNING INDICATION FLT. ATTITUDE INST. CLCLIMB 1 SO11523MD 47320 ATL/BNA - FLT 558 - RETURNED TO ATL DUE TO FIRST OFFICER'S ADI FAILING DURING CLIMB-OUT. REMOVED AND REPLACED NR 2 VERTICAL GYRO. OPS CHECK GOOD PER MM 34. 2L72 4F A6WE 19950224003191995022400319 1995 2 24 95ZZZX867 419950116A3421258733511 VERTICAL GYRO DOUG DC9 DC932 3022066WP NR 2 FAILED A VJ6AA UNSCHED LANDING IJ FLT. ATTITUDE INST. WARNING INDICATION CLCLIMB 1 SO11523MD 47320 ATL/MIA - FLT 595 - RETURNED TO ATL DUE TO FIRST OFFICER'S GYRO WENT INOP ON CLIMB-OUT. REMOVE AND REPLACE NR 2 GYRO AND REMOVE AND REPLACE INSTRUMENT AMP PER MM 34-00, OPS CHECK NORMAL. 2L72 4F A6WE 19950224003201995022400320 1995 2 24 95ZZZX868 419950116A340011493751 INSTRUMENT AMP DOUG DC9 DC932 3022066WP NR 2 FAILED A VJ6AA UNSCHED LANDING IJ FLT. ATTITUDE INST. WARNING INDICATION CLCLIMB 1 SO11523MD 47320 ATL/MIA - FLT 595 - RETURNED TO ATL DUE TO FIRST OFFICER'S GYRO WENT INOP ON CLIMB-OUT. REMOVE AND REPLACE NR 2 GYRO AND REMOVE AND REPLACE INSTRUMENT AMP PER MM 34-00, OPS CHECK NORMAL. 2L72 4F A6WE 19950224003241995022400324NE 1995 2 24 C2XA95IA022 319950207A6111RFC11N16 BLADE EMB 120 EMB120RT SO HAMSTD14RF 14RF9 NE NR 1 PROP CRACKED A AC2XAK NONE O OTHER ININSP/MAINT 1 SW09577347140 1936 120199 866754 IAH - DURING C-CHECK INSPECTION, THE NR 1 PROPELLER, NR 1 BLADE WAS FOUND TO HAVE A LIFTING AND TORN EROSION SHEATH. UPON REMOVAL OF THE SHEATH. THE BLADE LEADING EDGE BELOW THE SHEATH, WAS FOUND CRACKED THROUGH THE RESIN INTO THE HEATING ELEMENT IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE AND THE AIRCRAFT RETURNED TO SERVICE. A/C TT 8443.7. CYCLES 12,794. (X) 2L72 4T RTA31SO 6 CP11NE 19950224003261995022400326NE 1995 2 24 VTZA95037 219950126A72605725109162 CHIP DETECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAILURE A VTZAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27317UE 41031 P76007 IAD/RDU - FLT 6576 - DURING TAXI AND GROUND RUN-UP ON 1-26-94, THE LT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED AT THE RUN-UP BLOCK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE CHIP DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950224003271995022400327NE 1995 2 24 95ZZZX699 219950121A7321 FUEL CONTROL BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE LEAKING A P5CAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23741SJ4356 19648 662552 EN ROUTE TO SEOUL, KOREA, FLIGHT CREW REPORTED A FIRE WARNING ON NR 4 ENGINE. ENGINE SHUT DOWN USING ENGINE FIRE CHECKLIST. CREW DECLARED AN EMERGENCY AND LANDED AT PUSAN WITHOUT INCIDENT. BOTH FIRE BOTTLES DISCHARGED. CREW REPORTED NR 2 FIRE BOTTLE DISCHARGED AFTER NUMEROUS ATTEMPTS. MAINTENANCE FOUND EVIDENCE OF A FIRE IN AREA OF FUEL CONTROL UNIT. ENGINE REMOVED FOR REPAIRS. BOTH FIRE BOTTLES REPLACED AND FUNCTIONAL CHECK NORMAL. AIRCRAFT RELEASED FOR SERVICE. 2L74 4F4 F A20WE E20EA 19950224003281995022400328WP 1995 2 24 9501799953 119950215A2820 WING DOUG DC9 DC931 3022065WP LEFT FUEL LEAK A NWAAO OTHER K FLUID LOSS UKUNKNOWN 1 GL01918RW 47158 FUEL BEGAN LEAKING FROM LEFT WING EN ROUTE HPN-MSP. FUEL WAS VENTING FROM RIGHT TANK AT A RATE OF 800 LBS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBLEMS WERE NOTED ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003291995022400329NM 1995 2 24 9502746612 119950111A5320 LOWER BEAM BOEING747 747251B 1384892NM FS 1840-1860 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612US 20357 DURING PERIODIC CHECK, FOUND THE AFT CARGO LOWER BEAM CORRODED AT FS 1840 TO 1860. THE LOWER BEAM WEB (65B04721-1) IS MADE FROM 0.125 INCH 7075-T6 ALUMINUM. MADE REPAIR PER EA 66-93767. 2L74 4F A20WE 19950224003301995022400330NE 1995 2 24 9502769997 219950217A7510 FUEL HEAT VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL019343 47439 653954 ON DESCENT INTO MCI, OIL AND FUEL TEMPERATURES FOR NR 2 ENGINE EXCEEDED NORMAL OPERATING PARAMETERS. A PRECAUTIONARY SHUTDOWN WAS PERFORMED AND THE FLIGHT WAS CONCLUDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE. AN ENGINE RUN-UP WAS PERFORMED, THE SYSTEM CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950224003311995022400331WP 1995 2 24 9502779874 119950213A32225910448563 STRUT DOUG DC9 DC951 3022051WP NLG UNDERSERVICED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01783NC 48108 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RED UNSAFE LIGHT WAS ALSO ILLUMINATED AND LOUD RUMBLE WAS HEARD. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT UNDERSERVICED. SERVICED STRUT TO PROPER LIMITS. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003321995022400332WP 1995 2 24 9502789914 119950209A3260 SWITCH WIRES DOUG DC9 DC931 3022065WP NLG BROKEN A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01964N 47416 NOSE GEAR UNSAFE LIGHT FLICKERED ON AND OFF DURING GEAR EXTENSION. PERFORMED GO-AROUND OF TOWER AND LIGHT EXTINGUISHED DURING SECOND APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BAD WIRING IN NOSE GEAR DOWNLOCK SWITCH. REPAIRED BROKEN WIRES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003331995022400333 1995 2 24 9502803213 419950219A2213K217AAM8 FLT CONTL UNIT AIRBUS320 A320211 3930320EU COCKPIT INOPERATIVE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01313US8754 13 153 DURING CLIMB-OUT, FLIGHT CONTROL UNITS NR 1 AND NR 2 FAILED. RESET CIRCUIT BREAKERS, NO HELP. DECISION WAS MADE TO RETURN TO MSP. REPLACED FLIGHT CONTROL UNIT. SYSTEM TESTS WERE NORMAL. 2L72 4F RTA28NM 19950224003341995022400334WP 1995 2 24 9502819953 119950216A2810 FUEL TANK DOUG DC9 DC931 3022065WP RT MAIN TANK VENTING A NWAAO OTHER K FLUID LOSS UKUNKNOWN 1 GL01918RW 47158 FUEL BEGAN VENTING FROM THE RIGHT MAIN TANK EN ROUTE MSP-HPN. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. PERFORMED BACKFLUSH PROCEDURE PER MM 28-20-0. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003351995022400335WP 1995 2 24 9502829980 119950214A2820 FUEL DOUG DC9 DC931 3022065WP RT TANK TRANSFERING A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL019344 47440 UPON LEVEL OFF AT CRUISE FLIGHT, FUEL WAS TRANSFERRED FROM RIGHT TANK TO CENTER TANK AT RATE OF 50 LBS PER MINUTE. TRANSFER STOPPED WITH APPLICATION OF CENTER TANK PUMPS. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003361995022400336WP 1995 2 24 9502839985 119950214A2913AS66411LS661 HYD PUMP DOUG DC9 DC932 3022066WP LT ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01985US 47479 LOSS OF LEFT HYDRAULIC SYSTEM PRESSURE OCCURRED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003371995022400337WP 1995 2 24 9502849997 119950211A2420976J2544 GEN CONTL PANEL DOUG DC9 DC931 3022065WP LT ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018933E362274241 47142 AC CROSSTIE LOCKOUT LIGHT ILLUMINATED ON ROTATION WITH NR 1 CSD DISCONNECTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED AC CROSSTIE RELAY, RIGHT GENERATOR RELAY, AND RIGHT GENERATOR CONTROL PANEL WITH NO HELP. REPLACED LEFT ENGINE GENERATOR CONTROL UNIT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003381995022400338WP 1995 2 24 9502859984 119950218A2150 DUCT DOUG DC9 DC932 3022066WP AIR COND SYST TORN A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01984US 47383 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN DURING CLIMB-OUT THROUGH 12,000 FEET. AIRFLOW WAS VERY LOW AND TEMPERATURES IN COCKPIT AND CABIN WERE HIGH. MIX VALVE ON LEFT SIDE WAS NOTED AS BEING FULL COLD. SELECTED MANUAL POSITION AND MOVED IT SLIGHTLY TOWARD HOT. AIRFLOW INCREASED AND SMOKE DISSIPATED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND AIR CONDITIONING DUCT TORN AND CLAMP BROKEN. REPLACED DUCT AND CLAMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003391995022400339WP 1995 2 24 9502869968 119950219A213094840213 PRESS AMPLIFIER DOUG DC9 DC931 3022065WP E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL019332 3660419648 47264 AUTO CABIN PRESSURIZATION FAILED AFTER TAKEOFF. CABIN PRESSURE WENT TO FULL INCREASE RELIEVING PRESSURE AT 8.06 PSI AND SHOWING NEGATIVE CABIN ALTITUDE. NORMAL CABIN PRESSURE WAS REGAINED USING MANUAL CONTROL BUT VERY DIFFICULT TO MAINTAIN. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE AMPLIFIER. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950224003401995022400340NM 1995 2 24 9502876740 119950219A8000R41013 START SYST BOEING747 747251F 1384898NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING ININSP/MAINT 1 GL01640US22792438 23888 702210 DURING START OF THE NR 4 ENGINE, THE NR 1 START SYSTEM FAILED TO START ENGINE. WHEN CREW ATTEMPTED TO SWITCH TO SYSTEM 2, THE ENGINE FOGGED AND A HOT START OCCURRED INCLUDING MAX EGT. SUBSEQUENTLY CREW PULLED THE FIRE HANDLE AND BOTTLE WAS DISCHARGED. REPLACED THE NR 1 AND NR 2 IGNITION PLUGS, CONDITION MOTOR, AND FIRE BOTTLES. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 F A20WE E3NE 19950224003411995022400341NM 1995 2 24 9502886309 119950220A5412 BULKHEAD BOEING747 747451 1384940NM FS 378.43 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01669US 24224 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE NR 3 PYLON AFT BULKHEAD 378.43. REMOVED DAMAGE AND REPAIRED PER EA 63-096770. 2L74 4F RTA20WE 19950224003421995022400342SO 1995 2 24 COM11791 119950218A325012022546001 WIRING ASSY EMB 120 EMB120RT SO NLG STEERING DAMAGED A ACOMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01268CA 120262 UNCOMMANDED NOSE WHEEL STEERING. REPLACED FEED BACK POT WIRING HARNESS. 2L72 4T RTA31SO 19950224003431995022400343 1995 2 24 COM11792 219950217A73207863904 HMU EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01247CA10753397 120225 RT ENGINE WILL NOT START. REPLACED THE HMU. 2L72 4T RTA31SO 19950224003441995022400344 1995 2 24 COM31037 419950220A61228210163 GOVERNOR SAAB SF340 SF340A 7850100EU LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01347CA4459 1152 340A028 LEFT ENGINE PROPELLER OVERSPEED TEST DOES NOT FUNCTION. REPLACED THE OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950224003451995022400345EA 1995 2 24 COM60422 119950220A274070604 HSTCU CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01916CA2712 89 7014 MACH TRIM INOP WARNING MESSAGE ON EICAS. REPLACED THE HORIZONTAL STAB TRIM CONTROL UNIT. 2L72 4F RTA21EA 19950224003461995022400346EA 1995 2 24 COM60423 119950219A274070623 MCU CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01941CA1521 61 7050 STABILIZER CHANNEL 1 FAIL MESSAGE. REPLACED THE STABILIZER MOTOR CONTROL UNIT. 2L72 4F RTA21EA 19950224003471995022400347EA 1995 2 24 COM60424 119950217A2760 ECU CNDAIRCL600 CL6002B19 EA SPOILER SYST MALFUNCTIONED A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01932CA 7038 SPOILERON CAUTION MESSAGE ON EICAS. RESET SPOILER ELECTRONIC CONTROL UNITS. SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950224003481995022400348EA 1995 2 24 COM60425 119950217A325017300233 SBW HARNESS CNDAIRCL600 CL6002B19 EA NLG STEERING DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01929CA2619 7035 NOSE WHEEL STEERING IS INOP. REPLACED THE SBW HARNESS ON NLG. 2L72 4F RTA21EA 19950224003501995022400350NM 1995 2 24 DL72P950726 119950217A3350900542 EEL PACK BOEING727 727225 1384077NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO118889Z 21858 DURING INSPECTION, RIGHT SIDE EMERGENCEY EXIT LIGHTS FAILED TO TEST. REPLACED BATTERY ASSEMBLY OPERATION NORMAL. 2L73 4F A3WE 19950224003511995022400351NM 1995 2 24 DL72S950644 119950216A5755651734781A PANEL BOEING727 727232 1384082NM NR 12 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 DURING HMV, FOUND NR 12 SPOILER PANEL DELAMINATED AT THE TRAILING EDGE, REPAIRED PER B-727 SRM 51-40-6. 2L73 4F A3WE 19950224003521995022400352NM 1995 2 24 DL72S950648 119950215A2780 BRACKET BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, NR 6 LEADING EDGE FLAP ACTUATOR SUPPORT BRACKETS WERE FOUND CRACKED. REPAIRED THE BRACKETS PER MAINTENANCE MANUAL 57-20-21. 2L73 4F A3WE 19950224003531995022400353NM 1995 2 24 DL72S950651 119950216A5754 LE RIB BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 NBR 5 SLAT I/B L/E RIB AT ACTUATOR CRACKED .1250 INCH AT L/E. STOPPED DRILLED PER M/M57-54-0 PG 803. DAMAGE FOUND AT LETTER CHECK. 2L73 4F A3WE 19950224003541995022400354NM 1995 2 24 DL72S950652 119950216A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 NR 7 SLAT LWR SKIN ATTACH ANGLE CRACKED .25 INCH AT 2 PLACES AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0 PG 807. DAMAGE FOUND AT LETTER CHECK. 2L73 4F A3WE 19950224003551995022400355NM 1995 2 24 DL72S950654 119950216A5320 WEB BOEING727 727232 1384082NM AFT STAIRWELL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING LETTER CHECK, FOUND .625 INCH AND 1 INCH CRACKS AT LIGHTNING HOLE AFT STAIRWELL TORQUE BOX STRUCTURE RT LOWER WEB. REPAIRED PER MM 53-11-00. 2L73 4F A3WE 19950224003561995022400356NM 1995 2 24 DL72S950655 119950216A5522 SKIN BOEING727 727232 1384082NM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING LETTER CHECK, FOUND .75 INCH CRACK ON EXISTING REPAIR DOUBLER ON RIGHT ELEVATOR LOWER SKIN JUST OUTBOARD OF TAB. REPLACED DOUBLER PER SRM 53-20-3. 2L73 4F A3WE 19950224003571995022400357NM 1995 2 24 DL72S950660 119950217A57556517348108A TE PANEL BOEING727 727232 1384082NM RT SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 DURING SHOP INSPECTION, FOUND RIGHT WING SPOILER PANEL TRAILING EDGE DELAMINATED. REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950224003581995022400358NM 1995 2 24 DL72S950662 119950216A5754 ANGLE BOEING727 727232 1384082NM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING LETTER CHECK, FOUND NR 1 L/E SLAT WITH SLAT ACTUATOR I/B ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21 PG 812. 2L73 4F A3WE 19950224003591995022400359NM 1995 2 24 DL72S950663 119950216A5311 FRAME BOEING727 727232 1384082NM FS 913.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 FOUND ON LETTER CK, STA 913.5 CRACKED BEHIND RADIUS BLOCK FUS FRAME AT MLG UPLOCK ASSY. REPAIRED, INSTALLED DOUBLER PER M/M 53-11-0 PG 834 - 837. 2L73 4F A3WE 19950224003601995022400360NM 1995 2 24 DL72S950670 119950208A5751652176519 SKIN BOEING727 727232 1384082NM LT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND LEFT INBOARD AILERON WITH A DENT ON THE UPPER SKIN. THE DENT WAS REPAIRED BY INSTALLING A FLUSH REPAIR PER SRM 57-50-5 FIG 1. 2L73 4F A3WE 19950224003611995022400361NM 1995 2 24 DL72S950674 119950130A57536521631273A LE SKIN BOEING727 727232 1384082NM NR 1 FORE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV SHOP INSPECTION, NR 1 FORE FLAP L/E SKIN WAS FOUND CRACKED AT O/B CUT OUT PAN. REPAIRED PER SRM 57-50-04. 2L73 4F A3WE 19950224003621995022400362NM 1995 2 24 DL72S950679 119950120A5754651622370 SKIN BOEING727 727232 1384082NM NR 7 LE SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 UPON INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A TEMPORARY REPAIR FOUND ON THE OUTER SKIN 45 INCHES FROM THE OUTBOARD END. THE DAMAGE WAS REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19950224003631995022400363NM 1995 2 24 DL72S950680 119950120A5754651622370 SLAT BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 DURING THE INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THERE WAS A CRACK FOUND THE UPPER I/B CORNER OF THE 'T' DUCT OPENING. THE CRACK WAS REPAIRED PER MM 57-54-0 PG 802A. 2L73 4F A3WE 19950224003641995022400364NM 1995 2 24 DL72S950682 119950120A5754651622370 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 DURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, RIB MARKED NR 11 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950224003651995022400365NM 1995 2 24 DL72S950696 119950201A5311 FRAME BOEING727 727232 1384082NM FS 600 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 FWD B/B STA 600 FRAME CRACKED AT STR CLIPS STR 23 AND 24 LEFT. REPAIRED PER SRM 53-10-4 PG 88-90. DAMAGE FOUND AND REPAIRED AT HMV VISIT. 2L73 4F A3WE 19950224003661995022400366NM 1995 2 24 DL72S950707 119950210A5755 SKIN BOEING727 727232 1384082NM NR 12 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 12 SPOILER DELAMINATED. MADE BONDED NOTE PER SRM 51-50-6. 2L73 4F A3WE 19950224003671995022400367NM 1995 2 24 DL72S950708 119950214A5755 SKIN BOEING727 727232 1384082NM NR 14 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 14 SPOILER DELAMINATED. REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950224003681995022400368NM 1995 2 24 DL72S950712 119950211A5755 SKIN BOEING727 727232 1384082NM NR 11 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 11 SPOILER PANEL DELAMINATED AT T/E. REPAIRED AS PER SRM 57-50-06. 2L73 4F A3WE 19950224003691995022400369NM 1995 2 24 DL72S950713 119950213A5754 RIB BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 3 SLAT CLOSE OUT ATTACH RIBS NR 5 AND NR 17 CRACKED IN RADIUS. FABRICATED REPAIR PER MM 57-54-0. 2L73 4F A3WE 19950224003701995022400370NM 1995 2 24 DL72S950714 119950213A5754 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 2 SLAT RIB MKD NR 2 CRACKED AT LWR T/E RADIUS. FABRICATED AND INSTALLED NEW REPAIR PER M/M 57-54-0 PG 819. 2L73 4F A3WE 19950224003711995022400371NM 1995 2 24 DL72S950715 119950210A5754 BRACKET BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 2 L/E FLAP ACT. BRACKET L/E CRACKED IB AND OB. FABRICATED AND INSTALLED NEW DOUBLER PER M/M 57-20-21. 2L73 4F A3WE 19950224003721995022400372NM 1995 2 24 DL72S950716 119950209A5755 PANEL BOEING727 727232 1384082NM NR 7 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 7 SPOILER PANEL HAS BOTTOM SURFACE TEMPORARY. REPAIRED PER B727 SRM 51-40-6 FIG 35. 2L73 4F A3WE 19950224003731995022400373NM 1995 2 24 DL72S950717 119950210A5755 SKIN BOEING727 727232 1384082NM NR 9 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 9 SPOILER DELAMINATED. BONDED REPAIR PER SRM 57-60-6. 2L73 4F A3WE 19950224003741995022400374NM 1995 2 24 DL72S950718 119950215A5754 SUPPORT BRACKET BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND NR 5 KRGR FLAP ACT SUPPORT BRACKET CRACKED AT LWR OB LEG. FABRICATED AND INSTALLED NEW DOUBLER PER M/M 57-20-21. 2L73 4F A3WE 19950224003751995022400375NM 1995 2 24 DL72S950719 119950212A5313 STRINGER BOEING727 727232 1384082NM LT BOX CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND L/WING L/E LT BOX CRACK IN STR 15L FWD AND AFT OF BOX. DRILLED AND INSTALLED NEW REPAIR PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950224003761995022400376NM 1995 2 24 DL72S950720 119950212A5310 LT BOX BOEING727 727232 1384082NM RT WING LE CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV, FOUND CORROSION UNDER SEALANT AT RW L/E LT BOX AT STR 15R CABIN. FABRICATED REPAIR PER SRM 53-30-3. 2L73 4F A3WE 19950224003771995022400377NM 1995 2 24 DL72S950721 119950203A5347 SEAT TRACK BOEING727 727232 1384082NM CABIN CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING HMV, FOUND SEAT TRACK CORROSION AT STA 344 LEFT I/B TRACK, REPAIRED BY REPLACING SEAT TRACK LT I/B FROM STA 380 FWD PER MM 53-20-11 FIG 802. 2L73 4F A3WE 19950224003781995022400378NM 1995 2 24 DL72W950413 119950129A5754 PANEL 651622498 BOEING727 727247 138408FNM RT LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA BN390 22111 DURING SHOP INSPECTION, RT WING SLAT PANEL WAS FOUND WITH DENTED UPPER SKIN. REPAIRED PER SRM 57-50-3 FIG 1. 2L73 4F A3WE 19950224003791995022400379NM 1995 2 24 DL72W950641 119950126A5330 SKIN BOEING727 727247 138408FNM FS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 BELLY SKIN INBD OF STR 29L FS 950 CORRODED. 2.8 BY 4.0 CUTOUT TO REMOVE CORROSION. A 0.040 TI-6AL-4V DOUBLER AND A 0.063 TI-6AL-4V TRIPLER INSTALLED OVER CUTOUT. 2L73 4F A3WE 19950224003801995022400380NM 1995 2 24 DL72W950643 119950207A53126516350344 BULKHEAD WEB BOEING727 727247 138408FNM BS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112815W 20871 BS 1183 BULKHEAD WEB CRACKED IN 4 PLACES AT RBL18. 1.0 INCH CRACK AT WL173, 0.5 INCH CRACK AT WL175, 1.25 INCH CRACK AT WL177, AND 1.0 INCH CRACK AT WL 179. CRACKS STOP DRILLED AND REPAIR DOUBLER INSTALLED. DAMAGE FOUND DURING LETTER CHECK, REPAIRED PER EAR 259480-14RVC. 2L73 4F A3WE 19950224003811995022400381NM 1995 2 24 DL72W950659 119950217A57556517348108A PANEL BOEING727 727247 138408FNM RT SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO112816W 20872 DURING LETTER CHECK, FOUND RT WING SPOILER PANEL WITH DELAMINATION DAMAGE, REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950224003821995022400382NM 1995 2 24 DL72W950686 119950123A5753652163388A SUPPORT FITTING BOEING727 727247 138408FNM NR 4 MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 NR 4 MID FLAP I/B CARRIAGE SUPPORT FITTING, UPPER I/B AND O/B THRUST BEARING RETAINER BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG 14. INSTALLED BUSHINGS. DAMAGE REPAIRED DURING SHOP VISIT. 2L73 4F A3WE 19950224003831995022400383NM 1995 2 24 DL72W950687 119950123A5753652163388A SUPPORT FITTING BOEING727 727247 138408FNM NR 4 MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 NR 4 MID FLAP O/B CARRIAGE SUPPORT FITTING UPPER I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14. INSTALLED BUSHING. DAMAGE REPAIRED DURING SHOP VISIT. 2L73 4F A3WE 19950224003841995022400384NM 1995 2 24 DL72W950688 119950123A5753652163388A RIB BOEING727 727247 138408FNM NR 4 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 NR 4 MID FLAP I/B AFT RIB CRACKED AT LOWER AFT CORNER. REPAIRED PER M/M 575200 FIG 808 PAGE 817. DAMAGE REPAIRED DURING SHOP VISIT. 2L73 4F A3WE 19950224003851995022400385NM 1995 2 24 DL733950711 119950216A5315 FLOOR BEAM BOEING737 737347 1384647NM FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 FOUND AT HMV, FLOOR BEAM CORRODED AT FS 328. CORROSION AT BL 0 AND RIGHT OF BL. REPAIRED PER SRM 53-00-51 FIG 205. 2L72 4F RTA16WE 19950224003861995022400386NE 1995 2 24 DL73E950727 219950216A7260737GRBXASSY GEARBOX BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11238WA 23186 709163 DURING CLIMB-OUT FROM ATL, HAD LOSS OF NR 2 ENGINE OIL QUANTITY AND PRESSURE, SHUT DOWN NR 2 ENGINE RETURNED ATLANTA. FOUND OIL FILTER CAP AND STUDS BLOWN LOOSE FROM N-2 GEARBOX. UNABLE TO REPAIR, REPLACED GEARBOX ASSEMBLY, RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 19950224003871995022400387NM 1995 2 24 DL73S950642 119950204A5320 SKIN BOEING737 737232 1384475NM R-1 DOOR CUT OUTCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309DL 23081 DURING LETTER CHECK, THE R-1 DOORWAY FRAME WAS FOUND CRACKED AT LOWER AFT CORNER APPROXIMATELY 1.75 INCH. THE CRACK ENDS IN A NUTPLATE HOLE. REPAIRED PER ERA, 301125-14. 2L72 4F RTA16WE 19950224003881995022400388NM 1995 2 24 DL757950671 119950110A5743114N4003178A WEDGE BOEING757 757232 1384965NM NR 9 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11660DL 24422 DURING OVERHAUL, DELAMINATION WAS DISCOVERED ON THE NR 9 SLAT WEDGE THE WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950224003891995022400389NM 1995 2 24 DL757950684 119950202A5350655446565 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11675DL 25980 NOSE OF RADOME WAS DELAMINATED AND EXCEEDED MOISTURE LIMITS. REMOVED AND REPLACED INNER SKIN AS PER B-757 SRM 53-10-72. DAMAGE WAS REPAIRED DURING SHOP VISIT. 2L72 4F RTA2NM 19950224003901995022400390NM 1995 2 24 DL757950724 119950214A5754 TE WEDGE 114N4002148ABOEING757 757232 1384965NM NR 10 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11640DL A20175 23994 DURING INITAL INSP THE TRAILING EDGE WEDGE WAS FOUND TO BE DELAMINATED. A NEW TRAILING EDGE WEDGE WAS INSTALLED IAW SRM 57-43-02, AND E/A NR 274662-14AD FOT THE RIGHT WING NR 10 L/E SLAT. 2L72 4F RTA2NM 19950224003911995022400391NM 1995 2 24 DL767950664 119950216A5230 DOOR BOEING767 767232 1385132NM FWD CARGO COMPT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11105DA 22217 DURING LETTER CHECK INSP, FOUND FWD CARGO DOOR HAS TWO AREAS OF DAMAGE ON SUPPORT STRUCTURE FOR LOWER HOOKS MARKED BETWEEN FWD AND MID HOOK AND BETWEEN MID AND AFT HOOK BURNISHED AND DYE CHECKED FWD AREA DYE CHECKED OK. REMOVED DAMAGE FROM AFT AREA IAW SRM 51-70-11 FABRICATED DOUBLER AND INSTALLED. 2L72 4F RTA1NM 19950224003921995022400392NM 1995 2 24 DL767950665 119950216A5330 SKIN BOEING767 767232 1385132NM FUSELAGE LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11105DA 22217 DURING LETTER CHECK, FOUND LIGHTNING STRIKES TOP OF FUSELAGE LOCATED FWD AND AFT OF PRODUCTION SPLICE FWD OF VERTICAL STABLIZER 3 FWD AND 3 AFT, BURNISHED OUT AND REMOVED RIVETS EDDY CURRENT. CHECKED OK INSTALLED RIVETS PER SRM 53-00-01 2L72 4F RTA1NM 19950224003931995022400393WP 1995 2 24 DLL10950729 119950114A5411 FRAME LKHEED1011 10113851 5265010WP NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 DURING LETTER CHECK, FOUND NR 1 PYLON WITH 2 INCH CRACK IF FORWARD END OF PYLON, JUST FWD OF HYDRAULIC SUPPLY LINE INSIDE PANEL 451TZ. REPAIRED PER SRM 54-11-00 PG 812. 2L73 4F A23WE 19950224003941995022400394WP 1995 2 24 DLL16950666 119950212A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 619 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 TEAR STRAP AT FS 619 BETWEEN STR 29-30 IS DISBONDED. REPAIRED PER SRM 53-31-00 FIG 804. DAMAGE FOUND AT HMV. 2L73 4F A23WE 19950224003951995022400395WP 1995 2 24 DLL16950667 119950212A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 619 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 TEAR STRAP AT FS 619 BETWEEN STR 31-32 IS DISBONDED. REPAIRED PER SRM 53-31-00 FIG 804. DAMAGE FOUND AT HMV. 2L73 4F A23WE 19950224003961995022400396WP 1995 2 24 DLL16950668 119950212A5751 BUSHING LKHEED1011 10113853 5265020WP RT AILERON MIGRATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND RT WING O/B AILERON, O/B PCA ATTACH POINT TO AILERON BUSHING IS MIGRATED. REPAIRED WORN LUGS AND REPLACED BUSHINGS PER SRM 57-55-00. 2L73 4F A23WE 19950224003971995022400397WP 1995 2 24 DLL16950669 119950217A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 860 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 FS 860 TEAR STRAP DISBONDED BETWEEN STR 27-29 AND STR 35-36. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950224003981995022400398WP 1995 2 24 DLL16950701 119950213A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 860 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 C1 BB FAIL STRAP DELAMINATED AT STRINGER 23, 26 AND 28, FS 860. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950224003991995022400399WP 1995 2 24 DLL16950703 119950213A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1585-1605 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED IN C-2 STA 1585-1605, STR 35-37. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950224004001995022400400WP 1995 2 24 DLL16950704 119950213A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1585-1605 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT C-2 STA 1585-1605 STR 32-33. REPAIRED PER SRM 53-31-00 PG 801. 2L73 4F A23WE 19950224004011995022400401WP 1995 2 24 DLL16950705 119950213A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1565-1585 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN TEAR STRAP DISBONDED WITH CORROSION BETWEEN 1565-1585, AT STRINGERS 31-32. CLEANED CORROSION AND REPAIRED PER SRM 53-31-00 FIG 801. 2L73 4F A23WE 19950224004021995022400402WP 1995 2 24 DLL17950728 119950122A5521 SPAR LKHEED1011 10113853 5265020WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11767DA 193H1209 DURING LETTER CHECK, FOUND RIGHT ELEVATOR, SPAR WEB CRACKED AT LIGHTENING HOLE JUST INBOARED OF THE OUTBOARD ATTACH FITTING. REPAIRED PER SRM 55-21-00. 2L73 4F A23WE 19950224004031995022400403NM 1995 2 24 DLM88950640 119950215A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO11948DL 49879 DURING LETTER CHECK, FOUND FUSELAGE SKIN WITH A DEEP SCRATCH BELOW NR 2 ENGINE PYLON, JUST FWD OF AFT CARGO DOOR. REPAIRED PER SRM 53-04. 2L72 4F RTA6WE 19950224004041995022400404NM 1995 2 24 DLM88950645 119950214A5230 SKIN DOUG MD88 MD88 3023688NM C 2 DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 C2 DOOR HANDLE CUTOUT SKIN IS DENTED AND GOUGED. INSTALLED REPAIR DOUBLER PER SRM 52-05 FIG 30. 2L72 4F RTA6WE 19950224004051995022400405NM 1995 2 24 DLM88950653 119950216A5400 ANGLE DOUG MD88 MD88 3023688NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11960DL 49979 DURING LETTER CHECK, FOUND NR 2 PYLON WEDGE, UPPER SURFACE TO FUSELAGE ATTACH ANGLE CRACKED, REPAIRED PER SRM 54-04 FIG 4. 2L72 4F RTA6WE 19950224004061995022400406NM 1995 2 24 DLM88950672 119950214A5330 SKIN DOUG MD88 MD88 3023688NM FS 218 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 FUSELAGE DENTED JUST AFT OF L1 DOOR ABOVE THE FLOOR LINE AT STA 218. INSTALLED REPAIR PER SRM 53-04 FIG 12B. FOUND AT HMV. 2L72 4F RTA6WE 19950224004071995022400407NM 1995 2 24 DLM88950673 119950214A5730 PANEL DOUG MD88 MD88 3023688NM UPR WING TE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 DURING HMV, FOUND PANEL CRACKED WITH SMALL DENT IN UPPER WING T/E PANEL 10 INCHES OB OF OB END OF OB SPOILER. REPAIRED PER SRM 57-04 FIG 3 PAGE 7 AND 8. 2L72 4F RTA6WE 19950224004081995022400408NM 1995 2 24 DLM88950676 119950217A5311 FRAME DOUG MD88 MD88 3023688NM LT MLG W/W CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11996DL 53363 DURING LETTER CHECK, FOUND A 1 INCH CRACK IN THE 0/B END OF THE LEFT MLG WHEEL WELL OPENING AFT JAMB, LOWER TEE STRIKER ANGLE. REPAIRED PER SRM 53-05 FIG 81A. 2L72 4F RTA6WE 19950224004091995022400409NM 1995 2 24 DLM88950681 119950215A5313 STRINGER DOUG MD88 MD88 3023688NM FS 1418 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, FOUND AFT UPPER FUSELAGE STRINGER 2R CRACKED AT FS 1418. REPAIRED PER SRM 53-02 PG 6 FIG 5. 2L72 4F RTA6WE 19950224004101995022400410NM 1995 2 24 DLM88950683 119950215A5313 STRINGER DOUG MD88 MD88 3023688NM FS 1418 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, FOUND AFT UPPER FUSELAGE STRINGER 2L CRACKED AT FS 1418. REPAIRED PER SRM 53-02 PG 6 FIG 5. 2L72 4F RTA6WE 19950224004111995022400411NM 1995 2 24 DLM88950685 119950212A5753 SKIN 5930495504 DOUG MD88 MD88 3023688NM TE FLAP VANE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 2698 49723 I/B FLAP O/B VANE HAD SHARP DENT ON LOWER I/B SIDE AT MOUNT POINT. MADE BONDED REPAIR PER MD 88 SRM 57-04, DAMAGE FOUND AT HMV. 2L72 4F RTA6WE 19950224004121995022400412NM 1995 2 24 DLM88950699 119950215A5347 SEAT TRACK DOUG MD88 MD88 3023688NM FS 1190 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, LT INBD SEAT TRACK AT FS 1190 IS CORRODED AFT GALLEY INBD AFT MOUNT. CLEANED CORROSION, CUT OUT CORRODED SEAT TRACK FABRICATED REPAIR SPLICE AND ANGLES AND INST NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. 2L72 4F RTA6WE 19950224004131995022400413NM 1995 2 24 DLM88950731 119950214A71105930645501 NOSE COWL DOUG MD88 MD88 3023688NM NR 2 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 DURING SHOP INSPECTION, NR 2 ENGINE NOSE COWL WAS REPAIRED FOR A DENT IN THE LEADING EDGE LIP. REPAIRED DENT PER SRM 54-04A. 2L72 4F RTA6WE 19950224004141995022400414NM 1995 2 24 QXEA9500052 119950217A3350 EEL DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09828PH 287 PDX - THE EMERGENCY EXIT LIGHT AT SEAT 4E HAS BEEN KICKED OFF THE WALL. RESECURED LIGHT ASSEMBLY TO THE WALL AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950224004151995022400415 1995 2 24 QXEA9500053 219950218A7200 ENGINE DORNERDO32 DO328100 2996000NM NR 2 MALFUNCTIONED A AQXEAK NONE X ENGINE FLAMEOUT APAPPROACH 1 NM09337PH 3020 SEA - DURING DESCENT NR 2 ENGINE TORQUE DROPPED FROM 30 PERCENT TO 0 PERCENT. AIRCRAFT YAWED TO THE RIGHT, AFTER APPROXIMATELY 5 SECONDS TORQUE WAS RESTORED. COMPLIED WITH A COMPLETE ENGINE OPERATIONAL TEST IAW AMM JIC ,71-00-00. STEP SPECIFIED PER FAX FROM DORNIER DATED 2-20-95. NO DEFECTS NOTED. REPLACED NR 2 ENGINE INTAKE ASSY WITH MOD 2 INTAKE BOOTS PER DORNIER ASB, 328-71-00. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19950224004161995022400416NM 1995 2 24 QXEA9500054 119950220A3350 EEL LENS DHAV DHC8 DHC8102 2809003NM CABIN MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV 91 PDX - THE EMERGENCY LIGHT AT THE MAIN CABIN DOOR IS MISSING A LENS. INSTALLED A REPLACEMENT LENS COVER. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950224004171995022400417NM 1995 2 24 UP802469 119950218A5753 SKIN BOEING747 747123F NM LT MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 MAINTENANCE REPORTED LEFT O/B MID FLAP PANEL CRACKED ACROSS FITTING AT ABOUT CENTER OF PANEL. REPAIRED PER SRM 51-40-09. 2L74 4F A20WE 19950224004181995022400418NM 1995 2 24 UP802470 119950219A7110 NOSE COWL BOEING747 747123F NM NR 4 ENGINE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 MAINTENANCE REPORTED NR 4 NOSE COWL DELAMINATED AT 6 O'CLOCK. REPAIRED PER SRM 51-40-9. 2L74 4F A20WE 19950224004191995022400419WP 1995 2 24 UP802471 119950220A33506012235 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01819UP 45990 MAINTENANCE REPORTED EMER EXIT LIGHTS INOP. REPLACED BATTERY PACK. 2L74 4F RT4A25 19950224004201995022400420NM 1995 2 24 UPS202445 119950221A5313 STRINGER BOEING727 72725C 138400HNM BS 673 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 18R, BS 673 ON STR SPLICE. INSTALLED REPAIR PER SRM 53-10-1, 53-10-2, 53-10-3, 51-10-2, 51-30-2, 51-20-151. 2L73 4F A3WE 19950224004211995022400421NM 1995 2 24 UPS202446 119950221A5313 STRINGER BOEING727 72725C 138400HNM BS 370 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 22L, BS 370. INSTALLED REPAIR PER SRM 53-10-3, 51-40-3. 2L73 4F A3WE 19950224004221995022400422NM 1995 2 24 UPS202447 119950221A5313 STRINGER BOEING727 72725C 138400HNM BS 620-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 6L, BS 620-740. INSTALLED REPAIR PER SRM 53-10-3, 51-10-4. 2L73 4F A3WE 19950224004231995022400423NM 1995 2 24 UPS202448 119950221A5320 WEB BOEING727 72725C 138400HNM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON AFT DOOR CUT OUT FRAME WEB AT BS 1110, RBL 22. INSTALLED REPAIR PER SRM 51-40-2, 53-10-1, 51-30-2, 51-10-2, 51-20-4. 2L73 4F A3WE 19950224004241995022400424NM 1995 2 24 UPS202449 119950221A5320 ANGLE BOEING727 72725C 138400HNM BS 748-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON ANGLE AT BS 748-760, RBL 63, WL 203. INSTALLED REPAIR PER SRM 51-10-6, 51-30-2, 51-10-1, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950224004251995022400425NM 1995 2 24 UPS202450 119950221A5313 STRINGER BOEING727 72725C 138400HNM BS 630 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR UNDER STR CLIP, DIRECTLY UNDER STAND OFF ON STR 20R, BS 360, RBL 58. INSTALLED REPAIR PER SRM 51-20-4, 51-30-2. 2L73 4F A3WE 19950224004261995022400426NM 1995 2 24 UPS202451 119950221A5311 FRAME BOEING727 72725C 138400HNM BS 440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON FRAME BS 440, LBL 14-20, WL 155. INSTALLED REPAIR PER SRM 53-40-3, 51-20-21, 51-20-151. 2L73 4F A3WE 19950224004271995022400427NM 1995 2 24 UPS202452 119950221A5730 SKIN BOEING727 72725C 138400HNM BS 758 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 758, RBL 66, WL 202. REPAIRED PER UPS EO 727-57-1089. 2L73 4F A3WE 19950224004281995022400428NM 1995 2 24 UPS202453 119950221A5730 SKIN BOEING727 72725C 138400HNM BS 745 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 745, RBL 35, WL 208. REPAIRED PER UPS EO 727-57-1089. 2L73 4F A3WE 19950224004291995022400429NM 1995 2 24 UPS202454 119950221A5730 SKIN BOEING727 72725C 138400HNM BS 7817 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON TOP SURFACE OF TOP SKIN OF CENTER FUEL CELL, STA 817, LBL 50, WL 198. REPAIRED PER UPS EO 727-57-1089. 2L73 4F A3WE 19950224004301995022400430NM 1995 2 24 UPS202455 119950221A5313 STRINGER BOEING727 72725C 138400HNM BS 380-460 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON STR 2R, BS 380-460. INSTALLED REPAIR PER SRM 53-10-3, 53-10-4, 51-30-2, 52-13-95. 2L73 4F A3WE 19950224004311995022400431NM 1995 2 24 UPS202456 119950221A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 847 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON SEAT TRACK FLANGE LBL 46, STA 847. INSTALLED REPAIR PER SRM 51-30-8. 2L73 4F A3WE 19950224004321995022400432NM 1995 2 24 UPS202457 119950221A5754 RIB BOEING727 72725C 138400HNM NR 2 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 2 SLAT RIB IN FOOT RADIUS ON O/B SIDE OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1. 2L73 4F A3WE 19950224004331995022400433NM 1995 2 24 UPS202458 119950221A5754 RIB BOEING727 72725C 138400HNM NR 7 LE SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT I/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1. 2L73 4F A3WE 19950224004341995022400434NM 1995 2 24 UPS202459 119950221A5754 RIB BOEING727 72725C 138400HNM NR 7 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT O/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1 AND UPS EO 727-57-1083. 2L73 4F A3WE 19950224004351995022400435NM 1995 2 24 UPS202460 119950221A5754 RIB BOEING727 72725C 138400HNM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT I/B RIB OF I/B TRACK. INSTALLED REPAIR PER SRM 57-50-3, 51-10-1 AND UPS EO 727-57-1083. 2L73 4F A3WE 19950224004361995022400436NM 1995 2 24 UPS202461 119950221A5754 RIB BOEING727 72725C 138400HNM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT RIB, O/B SIDE OF I/B TRACK. INSTALLED REPAIR PER UPS EO 727-57-1083. 2L73 4F A3WE 19950224004371995022400437NM 1995 2 24 UPS202462 119950221A5752 TRIM TAB BOEING727 72725C 138400HNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON R/W, I/B AILERON TRIM TAB FWD O/B HINGE FITTING. REPAIRED PER SRM 51-30-2. 2L73 4F A3WE 19950224004381995022400438NM 1995 2 24 UPS202463 119950221A5754 RIB BOEING727 72725C 138400HNM NR 1 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 1 SLAT 3RD RIB FROM I/B END AT UPPER FWD FLANGE, COMMON TO UPPER SKIN. REPAIRED PER UPS EO 727-57-1083. 2L73 4F A3WE 19950224004391995022400439NM 1995 2 24 UPS202464 119950221A5754 RIB BOEING727 72725C 138400HNM NR 1 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON NR 1 SLAT 4TH RIB FROM I/B END AT UPPER FWD FLANGE, COMMON TO UPPER SKIN. REPAIRED PER UPS EO 727-57-1083. 2L73 4F A3WE 19950224004401995022400440NM 1995 2 24 UPS202465 119950221A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 259.5-277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR ON INTERCOSTAL AROUND NUTPLATE HOLES BS 259.5-277, LBL13-15, WL208. REPAIRED PER SRM 53-10-01. 2L73 4F A3WE 19950224004411995022400441NM 1995 2 24 UPS202466 119950221A5230 FRAME BOEING727 72725C 138400HNM FWD CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON FWD CARGO DOOR, LWR FWD CORNER OF FRAME AT FWD CENTER GUIDE ROLLER BRACKET. REPAIRED PER SRM 51-10-01, 51-30-02. 2L73 4F A3WE 19950224004421995022400442NM 1995 2 24 UPS202467 119950221A5320 CLIP BOEING727 72725C 138400HNM BS 1148 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON STRINGER CLIP AT BS 1148, RBL 48, WL 173. REPAIRED PER SRM. 2L73 4F A3WE 19950224004431995022400443NM 1995 2 24 UPS202468 119950221A5320 CHORD BOEING727 72725C 138400HNM BS 219-227 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORR STA 219-227, LBL 44, WL236, O/B CHORD. REPAIRED PER SRM 51-10-03, 51-30-02, MM 51-20-151. 2L73 4F A3WE 19950224004441995022400444NM 1995 2 24 95ZZZW118 119950107A3040SYLZ50970 HEAT CONTROLLER DHAV DHC8 DHC8102 2809003NM LT WINDSHIELD FAILED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07940HA10203 639C 156 CLT-HHH - FLT 3377 - DURING TAKEOFF ROLL, LT WINDSHIELD HOT CAUTION LIGHT ILLUMINATED. ACFT ABORTED TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER. 2H72 4T RTA13NM 19950224004451995022400445NM 1995 2 24 95ZZZW107 119950126A323065446916 LANDINIG GEAR MO BOEING737 7372Q8C 138448SNM NLG MALFUNCTIONED A ASAAO OTHER J WARNING INDICATION APAPPROACH 1 NM01741AS23907 21959 ANC - FLT 145 - DURING APPROACH ON GEAR EXTENSION THE NOSE GEAR REMAINED UP. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR HYDRAULIC MODULE AND THE NOSE GEAR LOCK ACTUATOR. NOSE GEAR RETRACTED AND EXTENDED NORMALLY ON GEAR SWING PER BOEING MM. REF ASAA9537. 2L72 4F A16WE 19950224004461995022400446NM 1995 2 24 ASAA9537 119950126A3233651781914 LOCK ACTUATOR BOEING737 7372Q8C 138448SNM NLG MALFUNCTIONED A ASAAO OTHER J WARNING INDICATION APAPPROACH 1 NM01741AS23907 21959 ANC - FLT 145 - DURING APPROACH ON GEAR EXTENSION THE NOSE GEAR REMAINED UP. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR HYDRAULIC MODULE AND THE NOSE GEAR LOCK ACTUATOR. NOSE GEAR RETRACTED AND EXTENDED NORMALLY ON GEAR SWING PER BOEING MM. REF 95ZZZW107. 2L72 4F A16WE 19950224004471995022400447EU 1995 2 24 RAIA950129 119950122A326091SE16 UPLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU RT MLG OUT OF ADJUST A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03422AM12630 856 STL - FLT 7466 - THE RT MAIN GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH WHEN GEAR SELECTED UP. MAINTENANCE ADJUSTED RT MAIN GEAR UPLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950224004481995022400448WP 1995 2 24 9502751148 119950220A771460B901034 TRANSMITTER DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01148US5471 5471 46757 686157 DURING TAKEOFF, THE NR 1 ENGINE FAIL LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. REPLACED THE NR 1 ENGINE N1 TRANSMITTER. 2L73 4F4 F A22WE E20EA 19950224004491995022400449WP 1995 2 24 9502899923 119950208A5320 PAN DOUG DC9 DC932 3022066WP CARGO DR CUTOUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01927RC 47469 DURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO CUTOUT PAN AT THE LOWER FORWARD CORNER. REPAIRED PER EA 99-93849. 2L72 4F A6WE 19950224004501995022400450WP 1995 2 24 9502909981 119950216A5320 FITTING DOUG DC9 DC931 3022065WP FS 980 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01994Z 47097 DURING PERIODIC CHECK, FOUND TWO .5 INCH CRACK IN THE 'SHOVEL' FITTING FS 980 AT LONGERON 30. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950224004511995022400451WP 1995 2 24 9502919968 119950218A5330 SKIN DOUG DC9 DC931 3022065WP FS 427-446 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019332 47264 DURING LINE CHECK, FOUND ONE INCH CRACK IN FUSELAGE SKIN BETWEEN FS 427 - 446 AND LONGERONS 29R - 30. REPAIRED PER SRM 53-04, FIG 12B. 2L72 4F A6WE 19950224004521995022400452WP 1995 2 24 9502929105 119950218A5320 INTERCOSTAL DOUG DC9 DC915 3022036WP FS 351 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0195S 47205 DURING LINE CHECK, FOUND ONE .5 INCH CRACK IN VERTICAL INTERCOSTAL, FORWARD CARGO DOOR JAMB FS 351. REPLACED INTERCOSTAL PER EA 91-096933. 2L72 4F A6WE 19950224004531995022400453WP 1995 2 24 9502939992 119950218A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 1038 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN BULKHEAD FS 1038 JUST ABOVE INTERCOSTAL AT LONGERON 13R. REPAIRED PER EA 99-093501. 2L72 4F A6WE 19950224004541995022400454WP 1995 2 24 9502949992 119950218A5320 FITTING DOUG DC9 DC931 3022065WP FS 617 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN BOTH FUSELAGE FRAME FITTINGS (DINOSAUR RIBS) AT FS 617 LEFT AND RIGHT SIDES. REPAIRED PER EA 99-093476 AND 99-093478 RESPECTIVELY. 2L72 4F A6WE 19950224004551995022400455WP 1995 2 24 9502959992 119950219A5320 FITTING DOUG DC9 DC931 3022065WP FS 606-615 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 26R END FITTING FS 605 - 615. REPLACED FITTING PER SRM 51-01 AND DWG 3915129-501. 2L72 4F A6WE 19950224004561995022400456WP 1995 2 24 9502969992 119950219A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 83 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018960E 45869 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN UPPER HORIZONTAL PRESSURE PANEL IN THE NOSE LANDING GEAR WHEEL WELL FS 83, LBL 36. REPAIRED PER EA 99-093492. 2L72 4F A6WE 19950224004571995022400457WP 1995 2 24 9502979928 119950220A5320 SUB FLOOR DOUG DC9 DC931 3022065WP FS 148 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FLIGHT DECK SUB FLOOR FS 148 AT RBL 12. REPAIRED PER EA 99-093499. 2L72 4F A6WE 19950224004581995022400458WP 1995 2 24 9502989957 119950221A5320 BRACKET DOUG DC9 DC931 3022065WP FS 1097 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01915RW 47139 DURING PERIODIC CHECK, FOUND ONE .25 INCH CRACK IN VERTICAL ATTACH ANGLE FS 1097 LEFT SIDE. REPAIRED PER EA 99-094929. 2L72 4F A6WE 19950224004591995022400459NM 1995 2 24 9502992711 119950218A2730680005007 PCU BOEING727 7272S7 138407ZNM ELEVATOR LEAKAGE A NWAAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01715RC42300186 22019 DURING DEPARTURE CLIMB AFTER GEAR RETRACTION, HYDRAULIC SYSTEM 'B' QUANTITY DECREASED TO ZERO AND LOW PRESSURE INDICATION ILLUMINATED. FLIGHT DUMPED 6,000 LBS OF FUEL AND INITIATED RETURN TO MIA. ON APPROACH THE 'A' SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.9 GALLONS ALTHOUGH PRESSURE REMAINED IN GREEN BAND. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LEAK AT RIGHT ELEVATOR POWER CONTROL UNIT. REPLACED ELEVATOR PCU AND 'B' SYSTEM PUMPS AND FILTERS. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950224004601995022400460WP 1995 2 24 ABXA9500095 119950221A2750015525331 SPRING NIHON YS11 YS11A500 6310416WP LT TE FLAP DEFECTIVE A AABXAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED TOTAKEOFF 1 GL23919AX 2113 FLAP ASYMMETRY LIGHT ILLUMINATED DURING RETRACTION AFTER TAKEOFF. FLAP MOVEMENT STOPPED AT EIGHT DEGREES. ACCOMPLISHED ABNORMAL CHECKLIST AND RETURNED TO LAND. FOUND ASYMMETRY RETURN SPRING NOT FULLY RETURNING. CLEANED AND LUBRICATED LEFT FLAP ASYMMETRY SPRING. FLAPS OPS CHECKED NUMEROUS TIMES. OPS CHECKED GOOD IAW YS-11 M.M. 27-55-0. ALSO, REPLACED THE LEFT FLAP ASYMMETRY SWITCH DRUM AT ILN, AFTER NEXT FLIGHT, IAW YS-11 MM CHAPTER 27. OPS CHECKED GOOD. 2L72 4T A1PC 19950224004611995022400461WP 1995 2 24 ABXA9500096 119950221A2120 AIR DISTR NIHON YS11 YS11A500 6310416WP COCKPIT ODOR A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23917AX 2077 SMELLED SMOKE IN FLIGHT. SHUT DOWN AUTOPILOT AND SWITCHED INVERTER. NOT SURE WHICH CAUSED SMELL. CHECKED AUTOPILOT SYSTEM IAW YS-11 MM PROCEDURES. AUTOPILOT CHECKED GOOD. NO SMOKE OR BLOWN FUSES. 2L72 4T A1PC 19950224004621995022400462SO 1995 2 24 BIER950005 119950222A5741 ATTACH FITTING PIPER PA32 PA32300 7103212SO LEFT WING CORRODED A BIEAK NONE O OTHER ININSP/MAINT 1 EA213073W7441 7441 327940081 AT COMPLIANCE WITH PIPERS SB 977, FOUND WING REAR ATTACH FITTING, LEFT, FLAKING AT POINT WHERE BRACKET PASSES THROUGH AIRCRAFT SKIN. REMOVED FITTING AND REPLACED WITH NEW PIPER PART. 1L71 3O A3SO 19950224004631995022400463NM 1995 2 24 DL72K950760 119950204A5320651751738 ANGLE BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11479DA 20756 DURING INSPECTION, A .875 INCH CRACK WAS FOUND IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263 IN ACCORDANCE WITH B727 S/B 53-0129, REV. 4, THE BEAM WILL BE REPLACED. 2L73 4F A3WE 19950224004641995022400464NM 1995 2 24 DL72L950756 119950220A323365404676 ACTUATOR BOEING727 727232 1384082NM NOSE GEAR CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO11510DA 21312 ON LANDING GEAR EXTENSION, LOST ALL A SYSTEM HYDRAULIC FLUID, LANDED SAN WITHOUT INCIDENT, FOUND NOSE LANDING GEAR DOWN LOCK ACTUATOR CRACKED. REPLACED ACTUATOR OPERATION NORMAL. 2L73 4F A3WE 19950224004651995022400465NM 1995 2 24 DL72S950694 119950201A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND NR 3 L/E SLAT WITH RIBS NR 1 AND NR 2 CRACKED. REPAIRED PER SRM 57-50-3 FIG 9 AND MM 57-54-0 PG 819. 2L73 4F A3WE 19950224004661995022400466NM 1995 2 24 DL72S950695 119950201A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIBS JUST INBOARD OF THE INBOARD SLAT TRACK AND OUTBOARD OF TAI DUCT. REPAIRED PER MM 57-54-0 PG 807. 2L73 4F A3WE 19950224004671995022400467NM 1995 2 24 DL72S950732 119950131A5330 SKIN BOEING727 727232 1384082NM FS 480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 SKIN CORRODED BETWEEN STR 27 AND 28 RIGHT AFT OF STA 480 FWD BB REMOVED CORROSION, FABRICATED DOUBLER PER SRM 53-30-3. REPAIRED PER ERA 301155-14, FOUND AND REPAIRED AT HMV. 2L73 4F A3WE 19950224004681995022400468NM 1995 2 24 DL72S950748 119950131A5330 SKIN BOEING727 727232 1384082NM FS 480 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 SEVERAL AREAS OF LT CORR BET STR 27 AND 28 RT JUST AFT OF STA 480 FRAME FWD B/B FOUND AT HMV. CUT OUT CORR AREA FAB REPAIR DOUBLER PER SRM 53-30-3 INSTALLED REPAIR PER ERA 301155-14 2L73 4F A3WE 19950224004691995022400469NM 1995 2 24 DL72S950749 119950131A5330 SKIN BOEING727 727232 1384082NM FS 480 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 LEVELING COMPOUND DISBONDED AND LIFTING O/B STR 27R AFT STA 480 FOUND AT HMV. CUT OUT DAMAGE AND REPAIRED PER SRM 53-30-3 FIG 3A. 2L73 4F A3WE 19950224004701995022400470NM 1995 2 24 DL72S950750 119950219A5313 STRINGER BOEING727 727232 1384082NM FS 550 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 STR 27L HAS SEVERAL AREAS OF CORROSION AROUND FASTENERS FROM STA 550 TO 590 FOUND AT HMV. REPAIRED PER SRM 53-10-3 2L73 4F A3WE 19950224004711995022400471NM 1995 2 24 DL72S950751 119950202A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 360 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 STA 360 FLOOR BEAM NUT CLIP HOLES CORRODED MANY PLACES FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 1. 2L73 4F A3WE 19950224004721995022400472NM 1995 2 24 DL72S950761 119950208A5320651841483 WEB BOEING727 727232 1384082NM FS 285 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145. 2L73 4F A3WE 19950224004731995022400473NM 1995 2 24 DL72S950763 119950204A5521 REAR SPAR BOEING727 727232 1384082NM RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 DURING INSPECTION, THE RT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .25 INCH FROM INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM OUTBD TAB HINGE FITTING-TO-REAR SPAR ATTACHMENT. IN ACCORDANCE WITH B727 S/B 55-0087, THE CRACK WAS STOP DRILLED AND SET UP FOR REPETITIVE INSPECTION UNTIL PERMANENT REPAIR. 2L73 4F A3WE 19950224004741995022400474NM 1995 2 24 DL733950730 119950128A575365C263202 SKIN BOEING737 737347 1384647NM NR 4 MID FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11307WA 23440 TOP SIDE OF LOWER SKIN WAS FOUND WORN AT SECOND FROM I/B AFT TRACK CUTOUT, OF NR 4 MID FLAP. REPAIRED PER SRM 57-53-01 WITH REF TO 51-70-10. 2L72 4F RTA16WE 19950224004761995022400476NM 1995 2 24 DL73S950757 119950219A32405059 VALVE BOEING737 737232 1384475NM LT MLG WW LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO11310DA 23082 ON TAXI OUT LOST ALL HYDRAULIC FLUID. FOUND BRAKE SHUTTLE VALVE LEAKING. REPLACED VALVE, OPERATION NORMAL. 2L72 4F RTA16WE 19950224004771995022400477NM 1995 2 24 DL76S950698 119950219A5330 SKIN BOEING767 767332 1382001NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11123DN 23437 DURING LETTER CHECK, FOUND SEVERAL LIGHTNING STIKES TO FUSELAGE SKIN. RT SIDE REPAIRED PER SRM 53-00-01 ITEM 3. 2L72 4F RTA1NM 19950224004781995022400478WP 1995 2 24 DLL10950600 119950125A57551529102178 SKIN LKHEED1011 10113851 5265010WP SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO111731D 193C1200 ON INITIAL SHOP INSPECTION, SPOILER PANEL WAS FOUND WITH 4 AREAS OF DELAMINATION ON THE LOWER SKIN. AT 48 INCHES, AND 4 INCHES FROM THE OUTBOARD END OF SLAT ON THE TRAILING EDGE, ALSO AT THE INBOARD TRAILING EDGE AND 24 INCHES FROM THE INBOARD END AT THE T/E OF SLAT, REPAIRED PER SRM 57-52-00. 2L73 4F A23WE 19950224004791995022400479WP 1995 2 24 DLL10950700 119950213A57531529112109 SKIN LKHEED1011 10113851 5265010WP LT TE FLAP VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 DURING SHOP INSPECTION, LEFT WING FLAP VANE WAS FOUND WITH CRACKED SKIN AT P/B WEAR STRIP. REPAIR WAS PERFORMED PER SRM 57-53-00 FIG 806. 2L73 4F A23WE 19950224004801995022400480WP 1995 2 24 DLL16950733 119950212A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 579 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN FAIL/SAFE TEAR STRAP DISBONDED AT FS 579 BETWEEN STRINGER 29 AND 30. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950224004811995022400481NM 1995 2 24 DLM11950706 119950219A2497604414 WIRE DOUG MD11 MD11 3023602NM G-8 GALLEY ARCED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11801DE 48472 DURING INSPECTION, CONDUCTING REPAIRS FOR L-3 DOOR FOUND GALLEY POWER FEEDER WIRE WITH SIGNS OF ARCING TO BUMPER STOP FOR L-3 DOOR. WIRE NUMBER 6044-1-4 (AL). THIS WAS LOCATED BETWEEN TERMINAL BLOCKS S3-914 AND S3-675. THE FAULTY ROUTING OF WIRE IS BELEIVED TO HAVE BEEN DONE AT THE FACTORY. WIRE WAS REPAIRED. 2L73 4F RTA22WE 19950224004821995022400482NM 1995 2 24 DLM88950675 119950217A5230 DOOR DOUG MD88 MD88 3023688NM NR 2 CARGO DOOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11996DL 53363 DURING LETTER CHECK, FOUND C-2 CARGO DOOR DOOR PAN/FRAME WITH GOUGE DAMAGE. REPAIRED PER SRM 52-05 FIG 27. 2L72 4F RTA6WE 19950224004831995022400483NM 1995 2 24 DLM88950677 119950217A5755 SKIN DOUG MD88 MD88 3023688NM NR 1 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11996DL 53363 DURING LETTER CHECK, FOUND EXISTING FILLER MATERIAL FOR DENT TO NR 1 SLAT COMING LOOSE AND CHIPPED. CHECKED PER SRM 53-07 AND REPAIRED PER SRM 57-03 FIG 18A. 2L72 4F RTA6WE 19950224004841995022400484NM 1995 2 24 DLM88950740 119950214A5320 DOOR FRAME DOUG MD88 MD88 3023688NM CARGO DR AREA CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, AFT B/B FUSELAGE LOWER DOOR FRAME CORRODED 6 INCHES FROM FWD LOWER CORNER TO 37 INCHES AFT JUST FWD OF 2ND LOWER DOOR STOP. CLEANED CORROSION FOUND OUT OF LIMITS PER SRM 53-05 PAGE 173. INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 63. 2L72 4F RTA6WE 19950224004851995022400485NM 1995 2 24 DLM88950747 119950213A5347 SEAT TRACK DOUG MD88 MD88 3023688NM FWD COAT CLOSET CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, SEAT TRACK IS CORRODED AT FWD COAT CLOSET AFT OUT BD MOUNT. REPAIRED PER ERA 270258-14. 2L72 4F RTA6WE 19950224004861995022400486NM 1995 2 24 SWAA950181 119950215A4900 APU BOEING737 7373H4 1384600NM CABIN SMOKING A SWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07376SW 26584 AT GATE, SLIGHT SMOKE NOTED IN CABIN AREA. INSPECTED AND DETERMINED THE SMOKE WAS FROM APU. APU WAS DEACTIVATED PER MEL 49-1. OPERATED AC PACKS TO DISSAPATE SMOKE. 2L72 4F RTA16WE 19950224004871995022400487NM 1995 2 24 SWAA950182 119950215A213039606411 CONTROL VALVE BOEING737 7372H4 138448CNM RT PACK FAILED A SWAAGA O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0724SW 20925 AFTER LEVELING AT 28,000, CABIN PRESSURE WARNING HORN SOUNDED. CABIN ALTITUDE CONTINUED TO CLIMB. USING STANDBY OR MANUAL SYSTEM, NO HELP. CREW INITIATED DESCENT. OXYGEN MASKS WERE DEPLOYED. CREW REGAINED CABIN PRESSURE USING APU AND LEFT PACK. AIRCRAFT DIVERTED TO BNA AND MADE AN UNEVENTFUL LANDING. REPLACED RIGHT PACK CONTROL AND SHUTOFF VALVE. PERFORMED CABIN DEPRESSURIZATION INSPECTION PER M/M. OPERATION TESTED BOTH AC PACKS, OK. PERFORMED CABIN PRESSURIZATION SYSTEM TEST OK. CLEANED AND RESTOWED CABIN OXYGEN MASKS, AND REPLACED OXYGEN BOTTLE. 2L72 4F A16WE 19950224004881995022400488NM 1995 2 24 SWAA950183 119950214A5320 ACCESS PANEL BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0794SW 23053 DURING SCHEDULED CHECK, FOUND NOSE WHEEL WELL CEILING LEFT PRESSURE ACCESS PANEL CRACKED AT AFT I/B RADIUS. REPAIRED PER SWA RA 1-253-1249. 2L72 4F A16WE 19950224004891995022400489NM 1995 2 24 SWAA950184 119950215A2782654465117 ACTUATOR BOEING737 7372H4 138448CNM NR 6 LE FLAP FAILED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0762SW 22060 AFTER TAKEOFF, NUMBER 6 L/E SLAT WOULD NOT PROPERLY RETRACT. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 6 SLAT ACTUATOR PER BOEING M/M. 2L72 4F A16WE 19950224004901995022400490NM 1995 2 24 SWAA950185 119950217A3260 UPLOCK SENSOR BOEING737 7375H4 138449DNM LT MLG MALFUNCTION A SWAAO OTHER N FALSE WARNING TOTAKEOFF 1 SW07503SW 24180 AFTER TAKEOFF, LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED, TIGHTENED RED LIGHT BASE, AND OPERATION CHECKED PER BOEING M/M. ON NEXT FLIGHT EXPERIENCED RED LIGHT FLICKERING IN FLIGHT. REPLACED LEFT MAIN GEAR UPLOCK SENSOR PER BOEING M/M. 2L72 4F RTA16WE 19950224004911995022400491WP 1995 2 24 95ZZZX870 119950203A217021D001 SEPARATOR BAGS DOUG DC9 DC932 3022066WP CABIN DIRTY A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11923VV 47488 ATL/DFW - FLT 231 - AIRCRAFT RETURNED TO ATL DUE TO UNABLE TO PRESSURIZE IN AUTO OR IN MANUAL. REMOVE AND REPLACE WATER SEPARATOR BAGS AFTER T/S AND FINDING BAGS CLOGGED WITH ICE. 2L72 4F A6WE 19950224004921995022400492CE 1995 2 24 95ZZZX871 119950209A3040MS24166D1 RELAY BEECH 1900 1900C 1154161CE WINDOW DEICE FAILED A VALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP233172912755 UC54 PSP/LAX - EN ROUTE, CREW SMELLED SMOKE AND NOTICED LIGHT HAZE IN COCKPIT AREA. THEY CLEARED SMOKE WITH VENT AND MADE PRECAUTIONARY LANDING AT ONT. BEECH DEALER RAN SYSTEMS CHECKS AND FOUND NO MALFUNCTION. AIRCRAFT FERRIED TO HOMEBASE AND FURTHER INSPECTION FOUND BURNED LOW HEAT WINDOW DEICE RELAY. RELAY WAS REPLACED, NO OTHER DAMAGE WAS FOUND. A SMALL FOIL WRAPPED CANDY BAR WAS FOUND ON THE RELAY. IT APPEARS THAT IT FELL THROUGH FROM SUN SHADE ABOVE INSTALLATION PANEL AND SHORTED RELAY. 2L72 4T RTA24CE 19950224004931995022400493EU 1995 2 24 95ZZZX872 119950123A27307227279541 CONTROL CABLE SAAB SF340 340B 7860101EU FS 389.0 CHAFED H AY55K NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY IS 0.163 INCH, MEASURED DIAMETER AT CHAFED AREA IS 0.140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950224004941995022400494EU 1995 2 24 95ZZZX873 119950123A27307227279542 CONTROL CABLE SAAB SF340 340B 7860101EU FS 389.0 CHAFED B AY55K NONE O OTHER ININSP/MAINT 1 SO03202KD9670 340B202 DURING ROUTINE C-CHECK INSPECTION, FOUND ELEVATOR PRIMARY FLIGHT CONTROL CABLES CHAFED BY FAIRLEADS AT FS 389.0. CABLE DIAMETER ORIGINALLY IS 0.163 INCH, MEASURED DIAMETER AT CHAFED AREA IS 0.140 INCH. REMOVED AND REPLACED BOTH ELEVATOR PRIMARY FLIGHT CONTROL CABLES. 2L72 4T RTA52EU 19950224004951995022400495EU 1995 2 24 95ZZZX874 119950131A6120SD3476014XA RPM CABLE STBROSSD3 SD360 8100606EU LT PROP BROKEN A NVEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO03164DD SH3734 JFK - FLT 4843 - PILOT REPORT NO CONTROL OF LT PROP RPM. RPM STAYS AT 1720 RPM. MAINTENANCE FOUND AND REPLACED A BROKEN PROP RPM CABLE. 2H72 4T A41EU 19950224004961995022400496CE 1995 2 24 95ZZZX875 119950202A3297 WIRE BEECH 1900 1900C 1154161CE NLG FAILED A PLGAO OTHER P NO WARNING INDICATION APAPPROACH 1 NE05815BE UB54 MHT - AFTER THE LANDING GEAR WAS CYCLED DOWN, THE NOSE GEAR GREEN DID NOT INDICATE DOWN AND LOCKED. FLIGHT CREW PERFORMED ABNORMAL CHECK. LIST VERIFIED GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. ACFT WAS INSPECTED AND FOUND SAFE FOR FERRY TO PSM FOR REPAIRS. UPON ARRIVAL, MAINTENANCE FOUND WIRES TO BE AT FAULT BETWEEN THE NOSE GEAR DOWN AND LOCK SWITCH AND CANNON PLUG P162. REMOVED AND REPLACED WIRING AND OPS CHECKED IAW BEECH MM. OPERATIONS CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 19950224004971995022400497NM 1995 2 24 95ZZZX876 119950205A7920 OIL RETURN LINE BOEING747 747122 1384872NM NR 1 ENGINE LOOSE A P5CAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP234710U 19755 HNL - AT 1815Z, EN ROUTE, ENGINE OIL QUANTITY DROPPED TO ZERO AND OIL PRESSURE STARTED TO FLUCTUATE. OIL TEMPERATURE AT 100 DEGREES. SIMULTANEOUSLY, NR 1 ENGINE OIL PRESSURE LIGHT STARTED BLINKING. ENGINE SHUT-DOWN AT 1816Z. LANDED IN HNL UNEVENTFUL. MAINTENANCE FOUND A LOOSE LINE CONNECTION AT BACKGEAR BOX RETURN LINE. RETORQUED LINE CONNECTION. PERFORMED ENGINE LEAK CHECK. RESULTS: SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. 2L74 4F A20WE 19950224004981995022400498NM 1995 2 24 AALA950081 119950117A3350 EEL WIRE BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE IN BUSINESS CLASS AND MAIN CABIN FOUND INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHT WIRE SPLICES IN BUSINESS CLASS AND MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224004991995022400499NM 1995 2 24 AALA950083 119950118A3350 EEL WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07360AA 24041 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEATS 2B THROUGH 12B, INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT WIRING FOUND LOOSE BY PASSENGER SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005001995022400500NM 1995 2 24 AALA950087 119950120A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07320AA 22321 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE FROM PASSENGER SEAT 23B AFT FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005011995022400501EU 1995 2 24 AALA950091 119950121A3260 LOCK PIN FOKKERF28 F28MK0100 4990807EU LT MLG DOOR WORN A AALAO OTHER N FALSE WARNING CLCLIMB 1 SW071416A 11395 DFW - FLT 1412 - AFTER TAKEOFF CRP WITH LANDING GEAR RETRACTED, LT MLG DOOR LOCK LIGHT ILLUMINATED. NO OTHER ABNORMAL INDICATIONS & ACFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. BITE CHECK OF LANDING GEAR PROXIMITY UNIT WITH NO DEFECTS FOUND. ACFT DEPARTED DFW AS T1412/21 & AFTER TAKEOFF WITH LANDING GEAR RETRACTED, LT MLG WARNING LIGHT ILLUMINATED. ABNORMAL PROCEDURES CHK LIST & MASTER CAUTION PROCEDURE WITH SAME RESULTS. ACFT RETURNED TO DFW & LANDED WITHOUT INCIDENT. GROUND CHK REVEALED LT MLG DOOR BUMPER STOP BACKED OFF. REPLACED WORN LOCKING PIN & ADJUSTED LT MLG DOOR BUMPER. LANDING GEAR RETRACTION CHK WITH NO DEFECTS FOUND. FUNCTIONAL CHK FLT, NO DEFECTS FND. SYS OPER CHK NORM. (X) 2L72 4F RT 19950224005021995022400502NM 1995 2 24 AALA950108 119950124A33508100022601 EEL BOEING767 767323 1385205NM CABIN INTERMITTENT A AALAK NONE L NO TEST ININSP/MAINT 1 SW07387AM 27184 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 16B FOUND INTERMITTENT. REPLACED EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 16B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005031995022400503NM 1995 2 24 AALA950110 119950124A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07387AM 27184 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT ROW 39H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PASSENGER SEAT ROW 39H. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005041995022400504NM 1995 2 24 AALA950126 119950126A33508100022601 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07361AA 24042 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEAT 15B FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT ASSEMBLY AT PASSENGER SEAT 15B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005051995022400505NM 1995 2 24 AALA950128 119950124A3350 EEL WIRE BOEING767 767223 1385123NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07320AA 22321 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LOWER FORWARD AND AFT OPENING OF L2 DOOR FOUND INOPERATIVE. REPLACED SHORTED WIRES FOR LOWER FORWARD AND AFT L2 DOOR EMERGENCY EXIT LIGHTS LOCATED IN CONDUIT L9008. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005061995022400506NM 1995 2 24 AALA950130 119950127A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07354AA 24035 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT AFT FLIGHT ATTENDANT POSITION FOUND INTERMITTENT. RESECURED EMERGENCY FLOOR LIGHT CONNECTOR AT AFT FLIGHT ATTENDANT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005071995022400507NM 1995 2 24 AALA950132 119950120A3350A3060719101 EEL STRIP BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07353AA 24034 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE OF BUSINESS CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT LT AISLE OF BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005081995022400508NM 1995 2 24 AALA950161 119950130A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07363AA 24044 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FOUND INOPERATIVE AT MID-GALLEY, AFT OF SEAT ROW 42H AND AFT GALLEY BELOW MID-JUMP SEATS. SECURED CONNECTORS AT SAME LOCATIONS. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005091995022400509NM 1995 2 24 AALA950168 119950201A3350 EEL WIRE BOEING767 767323 1385205NM CABIN DISCONNECTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07378AN 25447 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN SEATS 7H AND 21H FOUND INOPERATIVE. SECURED DISCONNECTED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005101995022400510NM 1995 2 24 AALA950192 119950202A3350 EEL WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739367 25194 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 7B FOUND INOPERATIVE. RESECURED LOOSE WIRE TO EMERGENCY FLOOR LIGHT AT PASSENGER SEAT 7B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005111995022400511 1995 2 24 AALA950196 419950202A256531073105 SLIDE AIRCRUISERS BOEING727 727223 1384074NM CABIN DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07709AA A2655 22466 ORD - DURING SHOP VISIT, EMERGENCY EVACUATION SLIDE GIRT FOUND UNGLUED APPROXIMATELY 1.0 INCH AT MATING SURFACE. SLIDE INTRODUCED TO SHOP FOR REPAIR. (X) 2L73 4F A3WE 19950224005121995022400512NM 1995 2 24 AALA950198 119950201A3350A3060719103 EEL STRIP BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07357AA 24038 ORD - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT FIRST CLASS GALLEY RT AISLE FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT AT FIRST CLASS GALLEY RT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950224005131995022400513WP 1995 2 24 IXXA199507 119950205A53305613861509 SKIN DOUG DC8 DC871 302199AWP FS8 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23823BX715692917 46064 DURING ROUTINE C-CHECK MAINTENANCE, A CRACK WAS NOTED IN THE EXTERIOR SKIN AT FS 8 RT AND LONGERON 27. THE CRACK ORIGINATED IN THE NOSE LANDING GEAR DOOR CUT-OUT. REPAIR OF THE AFFECTED AREA WAS ACCOMPLISHED BY CUTTING OUT THE DAMAGED AREA, INSTALLATION OF A FILLER, AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-132, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-123. (X) 2L74 4F 4A25 19950224005141995022400514WP 1995 2 24 IXXA199508 119950205A53112537716 BELT FRAME DOUG DC8 DC871 302199AWP FS 520 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23823BX715692917 46064 DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION REMOVAL WAS BEYOND SRM LIMITS. DAMAGE WAS LIMITED TO LONGERON 34 RT AND 36.5 OF THE BELT FRAME AT FS 520. REPAIR OF THE AFFECTED AREA WAS ACCOMPLISHED BY REMOVAL OF THE CORRODED SECTION AND SPLICING IN A NEW SECTION. THE WORK WAS ACCOMPLISHED IAW DRAWING HSE27-53-130, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-124. (X) 2L74 4F 4A25 19950224005151995022400515WP 1995 2 24 IXXA199509 119950205A53305779934501 SKIN DOUG DC8 DC871 302199AWP FS 330 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23823BX715692917 46064 DURING ROUTINE C-CHECK INSPECTION, THE EXTERNAL SKIN SURROUNDING THE 'A' PIT DOOR WAS FOUND DAMAGED AT THE AFT EDGE OF THE DOOR CUT OUT. THE REPAIR OF THE AREA REMOVED THE DAMAGED AREA, INSTALLED A FILLER, INSTALLED AN INTERNAL AS WELL AS TWO EXTERNAL REPAIR DOUBLERS. THE REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-131, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-125. (X) 2L74 4F 4A25 19950224005161995022400516WP 1995 2 24 IXXA199510 119950205A57303757851 SKIN DOUG DC8 DC862 3021970WP WS 410-425 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE 'C' CHECK INSPECTION, UPPER LEFT WING SKIN CORROSION WAS FOUND. CORROSION REMOVAL WENT BEYOND LIMITS OF THE DOUGLAS SRM. REPAIR WAS ACCOMPLISHED AFTER REMOVAL OF ALL CORROSION IAW SKETCH SKA95002-2, AND E.O. 57-DC8-126. AFFECTED AREA WAS STR 9 AND STR 10 AT WS XRS 410 TO XRS 425. (X) 2L74 4F 4A25 19950224005171995022400517WP 1995 2 24 IXXA199511 119950205A53132641455 LONGERON DOUG DC8 DC862 3021970WP FS 973R CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON LONGERON 32 RT FS 973. CORROSION BLEND OUT OF THE LONGERON WENT BEYOND SRM LIMITS. REPAIR OF THE LONGERON WAS ACCOMPLISHED BY INSTALLING REPAIR DOUBLERS IAW SKA93002-3, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-127. (X) 2L74 4F 4A25 19950224005181995022400518WP 1995 2 24 IXXA199512 119950205A53132611062 LONGERON DOUG DC8 DC862 3021970WP FS 587-592 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION REMOVAL IN A LOCALIZED AREA IN THE RADIUS OF LONGERON 35 RT, STA 587-STA 592 WAS BLENDED BEYOND SRM LIMITS. REPAIR OF THE LONGERON WAS ACCOMPLISHED IAW SKETCH SKA95002-5, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-130. (X) 2L74 4F 4A25 19950224005191995022400519WP 1995 2 24 IXXA199513 119950205A53302014T6AL SKIN DOUG DC8 DC862 3021970WP FS 980-1090 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS NOTED BETWEEN LONGERONS 34.5 LT TO 34.5 RT, BETWEEN FS 980 AND FS 1087. CORROSION REMOVAL ON THE INTERNAL SKIN WENT BEYOND SRM LIMITS. REPAIR OF THE ARA WAS ACCOMPLISHED IAW SKETCH SKA 95002-7, AND E.O. 53-DC8-131. REPAIR WAS ACCOMPLISHED BY ADDING AN INTERNAL DOUBLER, AND EXTERNAL SPLICE DOUBLER, REPLACING LONGERON SECTIONS AND ATTACH ANGLES. (X) 2L74 4F 4A25 19950224005201995022400520WP 1995 2 24 IXXA199514 119950205A5320 FRAME DOUG DC8 DC862 3021970WP FS 930 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND AT FS 930 WINDOW FRAME LEFT SIDE. THE CORROSION WAS REMOVED AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SKETCH SKA95002-8, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-132. (X) 2L74 4F 4A25 19950224005211995022400521WP 1995 2 24 IXXA199515 119950205A53432641877 FITTING DOUG DC8 DC862 3021970WP FS 905 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG TORQUE TUBE SUPPORT FITTING CRACKED BEYOND REPAIRABLE LIMITS. THE FITTING WAS REMOVED AND REPLACED IAW DOUGLAS SRM AND SB 53-61. (X) 2L74 4F 4A25 19950224005221995022400522WP 1995 2 24 IXXA199516 119950205A57303757851 SKIN DOUG DC8 DC862 3021970WP LT WING CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23728PL6788817349 45918 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND OUTBOARD OF THE NR 1 ENGINE, UPPER PLATING OF THE WING AT XS-00. THE AREA CORROSION WAS BLENDED BEYOND SRM LIMITS AND REQUIRED REPAIR. REPAIR WAS ACCOMPLISHED IAW SKETCH SKA 95002-2, WHICH WAS FAA DER APPROVED, AND E.O. 57-DC8-128. REPAIR DOUBLER WAS INSTALLED. (X) 2L74 4F 4A25 19950224005231995022400523WP 1995 2 24 IXXA199517 119950207A3260 WARNING LIGHT DOUG DC8 DC871 302199AWP MLG DOOR MALFUNCTIONED A IXXAO OTHER N FALSE WARNING CLCLIMB 1 GL23823BX 46064 MCO - ON TAKEOFF, MLG DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE LANDING GEAR WAS CYCLED, AND THE LIGHT EXTINGUISHED. FOLLOWING LANDING IN MCN, LANDING GEAR WAS OPERATIONALLY CHECKED IAW THE DC-8 MM. THE PROBLEM COULD NOT BE DUPLICATED DURING MULTIPLE CYCLES OF THE LANDING GEAR. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950224005241995022400524SW 1995 2 24 LOSA9511 119950207A3250791010BA22 WIRE FRCHLDSA227 SA227DC 3377521SW NLG STEERING BROKEN A LOSAO OTHER O OTHER TXTAXI/GRND HDL 1 WP23452LA1602 DC848B STP - CREW REPORTED NOSE WHEEL STEERING DOES NOT OPERATE WHEN POWER BUTTON IS PRESSED. OPERATES NORMALLY WITH RIGHT SPEED LEVER IN 'LOW' POSITION. MAINTENANCE FOUND BROKEN WIRE IN PEDESTAL AREA - NEAR END OF TUBE CONDUIT. (X) 2L72 4T RTA18SW 19950224005251995022400525EU 1995 2 24 VTZA95014 119950111A3010BFG74451C BOOT PATCH BAG JETSTMJETSTM3201 1500217EU LT WING FAILED A AVTZAA UNSCHED LANDING Z SIGNIFICANT FAILURE REPORT CRCRUISE 1 EA27494UE 810 IAD/ALB - FLT 6155 - DIVERTED TO SWF ON 1-11-95 AT 0855 HRS DUE TO THE AIRFRAME DEICING FAILING IN-FLIGHT. AIRCRAFT LANDED AT SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED BOOT PATCHES AND DRAINED WATER FROM BOOT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950224005261995022400526CE 1995 2 24 95ZZZZ100 119950204A5520101610000613 ELEVATOR BEECH 1900 1900C 1154161CE LT HORIZ STAB DAMAGE A GLBAK NONE C F.O.D. TXTAXI/GRND HDL 1 CE01104GL9762 UC104 RHI - DURING DE-ICING OPERATIONS, THE DE-ICE TOWER CONTACTED THE LEFT ELEVATOR RESULTING IN DAMAGE BEYOND LIMITS. MAINTENANCE REMOVED THE DAMAGE ELEVATOR, INSPECTED THE AREA FOR DAMAGE, AND INSTALLED A SERVICEABLE ELEVATOR. 2L72 4T RTA24CE 19950224005271995022400527EA 1995 2 24 95ZZZZ101 219950131A7261 SEALS BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE LEAKING A GLBAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 CE0198GL 9836 UC98 PCE32601 OTW - UPON ARRIVAL OTW, THE CREW REPORTED LEFT ENGINE LOW OIL PRESSURE. INSPECTION REVEALED INTERNAL SEEPAGE ALLOWING OIL LEAKS AT THE COMPRESSOR. MAINTENANCE REMOVED THE ACCESSORY GEARBOX AND REPLACED PERFORMED PACKINGS, SEALS, AND GASKETS. THE NR 2 BEARING OIL SCAVANGE SCREEN WAS CLEANED. 2L72 4T4 TRTA24CE E4EA 19950224005281995022400528CE 1995 2 24 95ZZZZ102 119950203A53201144200365 FRAME BEECH 1900 1900C 1154161CE DOORWAY CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01174GL7843 UC174 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE ENTRANCE DOORWAY FUSELAGE BULKHEAD CRACKED AT THE POINT WHERE THE AIRSTAIR DOOR DAMPNER BRACKET ATTACHES. REPAIRED BY INSTALLING AN ANGLE REINFORCEMENT INSIDE THE BULKHEAD IAW BEECH SRM 53-90-00 PGS 24 AND 25. 2L72 4T RTA24CE 19950224005291995022400529CE 1995 2 24 95ZZZZ103 119950130A5730 RIVETS BEECH 1900 1900C 1154161CE RT WING LOOSE A GLBAK NONE K FLUID LOSS ININSP/MAINT 1 CE0145GL 14410 UC45 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RIGHT WING SEEPING FUEL OUTBOARD OF THE NACELLE ALONG THE SPAR. SEVERAL RIVETS WERE REPLACED AND THE AREA WAS SEALED WITH MIL-S-8802F SEALANT. 2L72 4T RTA24CE 19950224005301995022400530EU 1995 2 24 95ZZZZ104 119950204A33503011151 EEL PWR SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21424MQ 2865 045 MIA - FLT 3589 - FORWARD SECTION OF THE EMERGENCY LIGHTS INOP WITH BATTERY POWER. MAINTENANCE RAI POWER SUPPLIES AT STATION 29W AND 3WL IAW 33-51-21. SYSTEM CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA950351. 2H72 4T RTA53EU 19950224005311995022400531 1995 2 24 95ZZZZ91 419950124A34164016341905 ALTIMETER HONEYWELL DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A HNAAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 EA07911HA145867918 8707495 034 FLT 3306 - CLT-CAK - NR 1 ALTIMETER FLAGGED ON CLIMB-OUT AT 8000 FEET, AIRCRAFT TURNED BACK AND LANDED IN CLT WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ALTIMETER. PROBLEM RETURNED LATER IN THE DAY. FOUND WIRES CHAFED AT RNAV COMPUTER 3461-1-P3-1. CAPPED AND STOWED WIRING, MEL'D RNAV COMPUTER. 2H72 4T RTA13NM 19950224005321995022400532EA 1995 2 24 95ZZZZ92 119950205A3260 UNSAFE LIGHT DHAV DHC7 DHC7102 2802708EA NLG ILLUMINATED A HNAAO OTHER N FALSE WARNING APAPPROACH 1 EA07905HA 070 FLT 3102 - HPN TO DCA - UPON GEAR EXTENSION, A NOSE GEAR UNSAFE CONDITION RED LIGHT WAS OBSERVED. CREW CYCLED GEAR AND STILL OBSERVED THE UNSAFE GEAR LIGHT. ACTIVATED HAND PUMP TO OBTAIN GREEN CONDITON. INSPECTED NOSE GEAR, NO DISCREPANCIES NOTED. CYCLED NOSE GEAR ON GROUND. TEST FLIGHT SATISFACTORY. (Z) 2H74 4T A20EA 19950224005331995022400533NE 1995 2 24 95ZZZZ93 219950120A72612380 OIL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 2 ENG REQ'D SERVICE A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07927HA 117 FLT 3264 - EWN-CLT - NR 2 ENGINE OIL PRESSURE CAUTION LIGHT AND ENGINE OIL PRESSURE GAUGE ILLUMINATED AFTER TAKEOFF. AIRCRAFT TURNED BACK AND LANDED IN EWN WITHOUT INCIDENT. CHECKED NR 2 ENGINE FOR OIL LEAKS, NO LEAKS FOUND. SERVICED WITH 2 QUARTS OF OIL. OPERATIONAL CHECK GOOD. (Z) 2H72 4T4 TRTA13NM E20NE 19950224005341995022400534NE 1995 2 24 95ZZZZ94 319950122A6110 PROP DHAV DHC8 DHC8102 2809003NM HAMSTD14RF 14RF9 NE NR 1 OUT OF BALANCE A HNAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA07927HA 117 FLT 72 - ORF-PHF - AIRCRAFT HAS VIBRATION ABOVE 180 KNOTS. AIRCRAFT TURNED BACK TO ORF AND LANDED WITHOUT INCIDENT. PERFORMED PROP BALANCE AND ADJUSTED PROP BALANCE WEIGHTS ON NR 1 PROP. 2H72 4T RTA13NM 6 CP11NE 19950224005351995022400535NM 1995 2 24 95ZZZZ95 119950119A2910 B-NUTS DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYST LOOSE A HNAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA07935HA 142 FLT 3057 - BWI-HPN - NR 1 HYDRAULIC SYSTEMS CONTENTS WENT TO ZERO IN FLIGHT. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. RETORQUED SEVERAL 'B' NUTS ON HYDRAULIC LINES TOP OF NR 1 NACELLE ABOVE JET PIPE. SERVICED SYSTEM AND BLED, PERFORMED SEVERAL LEAK CHECKS. NO LEAKS NOTED AT THIS TIME. 2H72 4T RTA13NM 19950224005361995022400536NM 1995 2 24 95ZZZZ96 119950114A27505906989101 DRIVE CABLE DHAV DHC8 DHC8102 2809003NM TE FLAPS BROKEN A HNAAK NONE J WARNING INDICATION LDLANDING 1 EA07907HA25830 011 FLT EN01 - ROA-ORF - FLAP DRIVE CAUTION LIGHT ILLUMINATED WHEN RAISING FLAPS AFTER LANDING. FOUND LEFT INBOARD SECONDARY FLAP DRIVE CABLE BROKEN. REMOVED AND REPLACED INBOARD SECONDARY FLAP DRIVE CABLE. 2H72 4T RTA13NM 19950224005371995022400537NM 1995 2 24 95ZZZZ97 119950119A33506104791X EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07910HA24234 PS107 022 FLT 3205 - HHH-CLT - EMERGENCY EXIT SIGN OVER FORWARD RIGHT EMERGENCY EXIT DOOR AND FORWARD OVERHEAD EMERGENCY FLOOR LIGHT DOES NOT TEST DURING PREFLIGHT CHECK. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IN 3351P2 POSITION. REFERENCE NR 95ZZZZ98. 2H72 4T RTA13NM 19950224005381995022400538NM 1995 2 24 95ZZZZ98 119950119A33506013211X EEL BATTERY PACKGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07910HA3712 ORF77 022 FLT 3205 - HHH-CLT - EMERGENCY EXIT SIGN OVER FORWARD RIGHT EMERGENCY EXIT DOOR AND FORWARD OVERHEAD EMERGENCY FLOOR LIGHT DOES NOT TEST DURING PREFLIGHT CHECK. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK IN 3351P2 POSITION. REFERENCE NR 95ZZZZ97. 2H72 4T RTA13NM 19950224005391995022400539CE 1995 2 24 95ZZZZ99 119950204A27501015210577 SPLIT FLAP CAM BEECH 1900 1900C 1154161CE RT TE FLAP FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0186UE 11587 UC86 CIU - AFTER TAKEOFF THE CREW ELECTED AN AIR TURN BACK BECAUSE THE FLAPS WERE STUCK IN THE TAKEOFF POSITION. AFTER AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RT SPLIT FLAP CAM AND RE-RIGGED THE SWITCH. 2L72 4T RTA24CE 19950224005411995022400541SO 1995 2 24 ASOA95004 119950201A302044E202A WATER SEPARATOR EMB 120 EMB120RT SO RT WING DEFECTIVE A ASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11236AS 120049 AFTER TAKEOFF FROM ATL-MCN, THE RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED. FOLLOWED POH PROCEDURES AND SHUTDOWN RIGHT ENGINE. FLIGHT RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED WATER SEPARATOR AND PRESSURE REGULATOR. ALSO, REPAIRED BLEED LINE IN RIGHT LEADING EDGE. OPERATIONAL AND LEAK CHECK GOOD. PRESSURE REGULATOR P/N 38E96-6A. (Z) 2L72 4T RTA31SO 19950224005421995022400542NM 1995 2 24 RAAAB195003 119950112A5320 CLIP BOEING727 72722C 138400FNM BS 1070 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING PERFORMANCE OF 3 YEAR CPCP INSPECTION PER CARD S3-54102, FOUND BEAM CLIP CRACKED AT BS-1070 RBL 3. STOP DRILLED CRACK REPAIRED PER SRM 51-40-3 PG 4, FIG 1 SHEET 4. (Z) 2L73 4F A3WE 19950224005431995022400543NM 1995 2 24 RAAAB295001 119950109A3350873100212 EEL BOEING727 72722C 138400FNM CABIN INOP A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 MID CABIN DOOR EXIT IDENTIFIER LIGHT INOP AT GATE. RESEATED IN CONNECTOR. (Z) 2L73 4F A3WE 19950224005441995022400544WP 1995 2 24 RAAAE495001 119950119A33508621006 EEL BATTERY PACK 873100212 LKHEED188 188A 5262602WP CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL039744C 188A1140 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (Z) 2L74 4T RT4A22 19950224005451995022400545EU 1995 2 24 SIMA950241 119950124A5240 DOOR HANDLE AEROSPATR42 ATR42300 8680920EU SERVICE DOOR LOOSE A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21429MQ 0135 DURING TAKEOFF AIRCRAFT SERVICE DOOR OPENED, VISUALLY CONFIRMED BY FLIGHT ATTENDANT. SECURED LOOSE BOLT ON DOOR HANDLE AND OPS CHECK GOOD, IAW MM 52-42-00. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950224005461995022400546EU 1995 2 24 SIMA950351 119950204A33503011151 EEL PWR SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21424MQ 2851 045 MIA - FLT 3589 - FORWARD SECTION OF THE EMERGENCY LIGHTS INOP WITH BATTERY POWER. MAINTENANCE RAI POWER SUPPLIES AT STATION 29W AND 3WL IAW 33-51-21. SYSTEM CHECK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE 95ZZZZ104. 2H72 4T RTA53EU 19950224005471995022400547EU 1995 2 24 SIMA950391 119950208A33503012000 EEL POWER SUPPLY AEROSPATR72 ATR72212 EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21320AT 209 320 DFW - DURING LINE CHECK, MAINTENANCE FOUND SEVERAL AFT EMERGENCY LIGHTS FLASHING. EMERGENCY LIGHT POWER SUPPLY WAS REMOVED AND REPLACED ALONG WITH BATTERY PACK. OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950224005481995022400548NM 1995 2 24 USAA950013 119950108A2910 HYD LINE BOEING737 7372H5 138448ENM LT MLG WW FAILED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19220US 20453 CLT - FLT 1243 - FLIGHT EN ROUTE PHL TO ATL WHEN 'A' SYSTEM HYDRAULIC QUANTITY INDICATED ZERO. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE ABOVE LEFT MAIN GEAR AND 'A' SYSTEM PRESSURE FILTERS AND BOTH CASE DRAIN FILTERS. CHECKED GOOD. (Z) 2L72 4F A16WE 19950224005491995022400549WP 1995 2 24 USAA950041 119950124A3222 STRUT DOUG DC9 DC931 3022065WP NOSE GEAR FLAT A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19914VJ 47068 PIT FLT 107 - ON TAKEOFF AFTER GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. THE GEAR WOULD NOT PRESSURIZE AND THE STALL INDICATION FAILURE LIGHT ILLUMINATED. FLIGHT RETURNED TO PIT. MAINTENANCE FOUND THE NLG STRUT FLAT AND REPLACED THE STRUT. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950224005501995022400550WP 1995 2 24 USAA950042 119950125A3222MS288892 SCHADER VLV DOUG DC9 DC931 3022065WP NLG STRUT LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19933VJ 47216 SWF - FLT 1522 - ON TAKEOFF, THE NLG WOULD NOT RETRACT. FLIGHT RETURNED TO SWF. MAINTENANCE FOUND THE NLG STRUT FLAT, AND SERVICED THE STRUT WITH NITROGEN. THE SCHRADER VALVE WAS REPLACED. LEAK CHECKED GOOD. (W) 2L72 4F A6WE 19950224005511995022400551EU 1995 2 24 USAA950049 119950130A301012292411 VALVE FOKKERF28 F28MK4000 4990810EU CENTER WING INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19484US 11234 PIT - FLIGHT NR 1141 - ON CLIMB-OUT FROM CVG, THE WING ANTI-ICE MODULATING VALVE WOULD NOT OPEN. NO HEATING OBSERVED ON TEMP GAUGE. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WING-ICE MODULATING VALVE PER MM 30-10-02. OPERATION CHECKS NORMAL. (Z) 2L72 4F RTA20EU 19950224005521995022400552WP 1995 2 24 USAA950062 119950129A532099579073 INTERCOSTAL DOUG DC9 DC931 3022065WP FS 389 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19930VJ70647 45868 IND - ACCOMPLISHED SCHEDULED SID INSPECTION PSE 53.09.001A FORWARD CARGO DOOR JAMB AREA. FOUND 1.25 INCH CRACK IN FRAME STATION 389 LONGERON 18R (VISUAL INSPECTION). REMOVED AND REPLACED INTERCOSTAL. (Z) 2L72 4F A6WE 19950224005531995022400553EU 1995 2 24 USAA950063 119950125A5312 BLKHD FOKKERF28 F28MK4000 4990810EU AFT PRESS BLKHD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19496US27986 11169 PIT - DURING SCHEDULED SIP VISIT FOUND A 2.5 INCH CRACK IN THE REAR PRESSURE BULKHEAD BEAM NR 3 AT BODY LINE 750 RT. REF - INSPECTION SIP 53-10-03 LFEC PROCEDURE. INSTALLED WEB REPAIR PATCH AND NEW REAR FACE DOUBLER AND TWO 92. REPAIR ANGLES PER USAIR EA 29285A. (Z) 2L72 4F RTA20EU 19950224005541995022400554WP 1995 2 24 USAA950084 119950123A5210H2024B SWITCH DOUG DC9 DC931 3022065WP PAX DOOR INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19980VJ 48156 PIT - FLT 0521 - THE CAPTAIN REPORTED A LOUD POPPING OR SNAPPING NOISE ON CLIMB-OUT. AT THE SAME TIME THE MAIN DOOR ANNUNCIATOR LIGHT ILLUMINATED. CAPTAIN DECIDED TO RETURN TO PIT. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR SWITCH. OPERATIONS CHECKED NORMAL. (Z) 2L72 4F A6WE 19950224005551995022400555EU 1995 2 24 USAA950087 119950204A33505515800106 EEL HOLDER FOKKERF28 F28MK4000 4990810EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19498US 11181 PIT - FLT NR 231 - DURING PREFLIGHT THE FLIGHT ATTENDANT FOUND EMERGENCY EXIT OVERHEAD LIGHTS INOPERATIVE. MAINTENANCE REPLACED LIGHT PLATE ASSEMBLY TO THE EMERGENCY EXIT LIGHTS ON CENTER CABIN PER WING EXIT. OPERATION CHECKS NORMAL. (Z) 2L72 4F RTA20EU 19950224005561995022400556NM 1995 2 24 AWXA9500045 119950125A5315 FLOORBEAM BOEING737 737222 1384473NM FS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - FLT 32 - DURING C-8 INSPECTION, FOUND FLOORBEAM UPPER CAP CORRODED AT FASTENER HOLE, STA 312 BL 0. INSTALLED REPAIR ANGLE IAW SRM 51-40-04. (W) 2L72 4F A16WE 19950224005571995022400557NM 1995 2 24 AWXA9500050 119950124A3230 RETRACT MECH BOEING757 7572S7 1384962NM LANDING GEAR MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28905AW 23567 JFK - FLT 11 - AIR TURNBACK, CREW UNABLE TO RETRACT LANDING GEAR. LEVER WOULDN'T GO PAST THE 'OFF' POSITION. GEAR OVER RIDE WAS NOT ATTEMPTED, AND THERE WERE NO ASSOCIATED EICAS MESSAGES. A/C RETURNED TO GATE. MX PERFORMED VISUAL INSPECTION OF GEAR, AND NO DEFECTS WERE FOUND. MX PERFORMED BITE CHECK ON PSEU, NO ABNORMALITIES NOTED. MX PINNED GEAR AND VERIFIED OVER RIDE FUNCTION OPERATES NORMALLY. UNMANNED STATION RELEASE ISSUED PER MEL 32-31-01. ON DEPARTURE, GEAR SELECTED UP AND RETRACTED. ON ARRIVAL, MX PERFORMED PSEU BITE CHECK, ALL SYSTEMS CHECK NORMAL PER FIM 32-61-00. SYSTEM RESET AND PERFORMED VISUAL INSPECTION OF ALL GEAR SENSORS, NO DEFECTS NOTED. A/C RELEASED TO SERVICE. (W) 2L72 4F RTA2NM 19950224005581995022400558NM 1995 2 24 AWXA9500054 119950126A276165445616 ACTUATOR BOEING737 7373G7 1384595NM NR 6 SPOILER INOPERATIVE A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28154AW 4312 23776 PHX - FLT 460 - OAK-LAS - A VIBRATION WAS FELT DURING CLIMB, CRUISE AND DESCENT. THE VIBRATION SEEMED LIKE AIRFRAME, CREW TRIED INCREASING AND DECREASING ACFT AND ENGINE SPEED, BUT UNABLE TO DETERMINE. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX REPLACED NR 6 SPOILER ACTUATOR PER AWA TASK CARD R3M27021. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950224005591995022400559NM 1995 2 24 AWXA9500059 119950130A5320 TEE ANGLE BOEING737 7372A6 138448BNM RT WING/BODY CHAFED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND RT WING TO BODY SUPPORT STRUCTURE FWD END ATTACH POINT TEE ANGLE CHAFED. REPAIRED BY FABRICATION OF NEW ANGLE PER SRM 51-40-4. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005601995022400560NM 1995 2 24 AWXA9500060 119950130A5320 ANGLE BOEING737 7372A6 138448BNM E/E COMPT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND CRACK IN ANGLE SUPPORTING AFT CHANNEL OF BATTERY SHELF IN E AND E COMPARTMENT. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2 AND 51-10-1. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005611995022400561NM 1995 2 24 AWXA9500061 119950130A5313 STRINGER BOEING737 7372A6 138448BNM FS 1103 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND THREE CRACKS ON STR 12R STA 1103 UNDER VORTEX GENERATOR. REPAIRED PER SRM 53-10-3. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005621995022400562NM 1995 2 24 AWXA9500062 119950130A5330 SKIN BOEING737 7372A6 138448BNM FS 727 WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND SEVERAL PULLING THROUGH PANEL SKIN AT STA 727 BL 0. REPLACED FASTENERS PER SRM 51-30-2. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005631995022400563NM 1995 2 24 AWXA9500063 119950130A5347 SEAT TRACK BOEING737 7372A6 138448BNM BS 747 WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND SEAT TRACK WORN BEYOND LIMITS, BS 747 RBL 24. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005641995022400564NM 1995 2 24 AWXA9500064 119950130A5311 FRAME BOEING737 7372A6 138448BNM FS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28145AW30161 20194 PHX - FLT 1202 - DURING C-11 INSPECTION, FOUND CRACK ON FRAME OF AIRSTAIRS DOOR CUTOUT, STA 360 BETWEEN STR 20 AND 21L. STOP DRILLED CRACK PER SRM 51-10-1 AND REPAIRED PER EO 53-11-04. TOTAL CYCLES 28453. (W) 2L72 4F A16WE 19950224005651995022400565NM 1995 2 24 AWXA9500066 119950125A3350 EEL WIRING BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28905AW 23567 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, LAST ROW IN AFT. REPAIRED WIRING TO LIGHTS, OPS CHECK NORMAL. (W) 2L72 4F RTA2NM 19950224005661995022400566NM 1995 2 24 AWXA9500067 119950125A335010617837 EEL ASSEMBLY BOEING737 737277 1384570NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28185AW 22652 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LIGHT BROKEN ON RT EMERGENCY EXIT DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224005671995022400567NM 1995 2 24 AWXA9500069 119950126A335020131A EEL BATTERY BOEING737 7373Y0 1384671NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 23747 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND GALLEY EMERGENCY BATTERY PACK AT FAULT. REMOVED AND REPLACED BATTERY ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950224005681995022400568NE 1995 2 24 AWXA9500072 219950201A7311457311261 OIL COOLER BOEING757 7572G7 1384963NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE INOPERATIVE A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28909AW FC22243 24522 PHX-JFK - FLT 294 - AIR TURNBACK DURING TAKEOFF, CABIN AND COCKPIT HAD A STRONG OIL SMELL WITH SMOKE IN CABIN. THE NR 1 ENGINE WAS REDUCED TO IDLE FOR LANDING. THE NR 1 ENGINE OIL TEMP ROSE TO 174 DEGREES FOR 5 TO 8 SECONDS. ON GROUND THE NR 1 ENGINE OIL PRESSURE WAS 26 PSI. A/C LANDED AND RETURNED TO GATE WITHOUT FURTHER PROBLEMS. MX TROUBLESHOT PER FIM 79-34-00, PG 105 BLK 1 AND 22. OIL QUANTITY WAS 21 QTS AND HAD SMELL OF FUEL. DRAINED OIL SYSTEM AND RESERVICED. REMOVED AND REPLACED NR 1 ENGINE FCOC PER BMM 79-21-01. RAN NR 1 ENGINE, LEAK CHECK GOOD PER MM 71-00-00. CHECKED CHIP DETECTOR AFTER ENGINE RUNS, NO METAL NOTED AT THIS TIME. A/C RETURNED TO SERVICE. (W) 2L72 4F4 FRTA2NM E12EU 19950224005691995022400569NM 1995 2 24 AWXA9500082 119950206A274032EN614 SWITCH BOEING737 7372E3 NM STAB TRIM FAILED A AWXAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP28138AW 22792 CMH-MDW - FLT 1492 - AIR TURNBACK, MAIN ELECTRIC HORIZONTAL STABILIZER TRIM SYSTEM INOPERATIVE IN THE NOSE DOWN POSITION. ACFT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STAB TRIM LIMITS SWITCH PER MM 27-41-101. GROUND OPS CHECK NORMAL IN BOTH NOSE UP AND NOSE DOWN MODES. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950224005951995022400595NM 1995 2 24 9503006601 119950221A7830 TR UNIT BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE INOPERATIVE A NWAAE ENGINE SHUTDOWN MRJOVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION LDLANDING 1 GL01601US 19778 662454 DURING LANDING ROLLOUT, THE NR 4 ENGINE REMAINED IN REVERSE RESULTING IN A COMPRESSOR STALL AND OVERTEMP. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT TAXIED TO THE GATE. FOUND NR 4 THRUST REVERSER DRIVE UNIT INOPERATIVE. LOCKED OUT NR 4 THRUST REVERSER, BORESCOPED NR 4 ENGINE, AND PERFORMED ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 F A20WE E20EA 19950224005961995022400596WP 1995 2 24 MWEA95135 119950221A531239145061 LATCH FITTING DOUG DC9 DC915 3022036WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 DURING SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD PLUG DOOR LOWER LATCH FITTING BROKEN. REMOVED DAMAGED FITTING, INSTALLED NEW FITTING. A/C RETURNED TO SERVICE. 2L72 4F A6WE 19950224005971995022400597NM 1995 2 24 95ZZZX877 119950209A3260835107 A5 CARD BOEING767 767231 1385131NM LANDING GEAR FAILED A TWAAO OTHER N FALSE WARNING DEDESCENT 1 CE05610TW 22573 LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION. FOUND A-5 CARD, MFG PN 8-351-07, IN ELECTRONIC PROXIMITY SWITCH BOX. LANDING GEAR POSITION AND WARNING SYSTEM CHECKED AND B.I.T.E. CHECKED NORMAL. CHECK C-4A - 1 -19-95 - JFK. 2L72 4F RTA1NM 19950224005981995022400598NM 1995 2 24 95ZZZX878 119950204A5754 SKIN BOEING727 727231 1384079NM NR 5 LE SLAT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554350 21969 JFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES. 2L73 4F A3WE 19950224005991995022400599NM 1995 2 24 95ZZZX879 119950202A2810 FUEL TANK BOEING727 727231 1384079NM WS 656.50 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0584357 21989 MCI - DURING OP-17, FOUND CRACK IN LT WING FUEL TANK IN TOP AFT NR 3 STRINGER, WS 656.50, AT RIB NR 6 ATTACH POINT. REPAIRED PER SSRM 57-20-201, PAGE 215, FIGURE 207. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES. 2L73 4F A3WE 19950224006001995022400600WP 1995 2 24 95ZZZX880 119950208A4900 APU DOUG DC9 DC982 3022082WP AFT FUSELAGE OIL LEAK A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE05916TW 49187 JFK - DURING TAKEOFF, HAD SMOKE IN CABIN. TURNED OFF HIGH PRESSURE BLEED AIR. FOUND APU LEAKING OIL. REPLACED APU, MFG PN 381276-1. APU OPERATION AND LEAK CHECKED NORMAL. CHECK C-1D - 1-30-95 - MCI. 2L72 4F A6WE 19950224006021995022400602WP 1995 2 24 95ZZZX882 119950131A5720 CASTELLATION LKHEED1011 10113851 5265010WP FS 503 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK, FOUND 1.1250 INCH CRACK IN RT WING FT CASTELLATION, STA 503, FORWARD OF STR 13. REPAIRED PER SB 093-57-207 AND REPLACED CHORD PER DWG. NR 1647070. AIRCRAFT TOTAL TIME: 59,528 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224006031995022400603WP 1995 2 24 95ZZZX883 119950131A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK FOUND A 1.25 INCH CRACK IN RT WING INTERNAL/LOWER RIB CAP AT AFT RADIUS, IWS 555, OUTBOARD SIDE, 6TH STRINGER FROM AFT. REMOVED AND REPLACED LOWER FORWARD RIB CHORD PER SB 093-57-207, AND DWG. NR 1647070. AIRCRAFT TOTAL TIME: 59,528 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224006041995022400604WP 1995 2 24 95ZZZX884 119950201A5312 BLKHD SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 DURING CHECK C-9B, FOUND .25 INCH CRACK IN AFT BULKHEAD SKIN, STA 1363, ON OUTBOARD RIVET HOLE BETWEEN STIFFENER 15 AND 16; FOUND 4 INCH CRACK AT OUTBOARD FRAME, LT WHEELWELL, AT NR 16 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLERS PER SRM 53-11-00, FIGURE 850. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006051995022400605WP 1995 2 24 95ZZZX885 119950201A5312 INTERCOSTAL LKHEED1011 10113851 5265010WP FS 1363 BROKEN A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND FORWARD END OF INTERCOSTAL, AFT BULKHEAD STA 1363, BROKEN AWAY FROM BULKHEAD BETWEEN STRINGERS 41L AND 42L, WHEELWELL. INSTALLED CLIP ANGLE PER SRM 53-12-00. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006061995022400606WP 1995 2 24 95ZZZX886 119950201A5312 BULKHEAD LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND A 28 INCH VERTICAL CRACK IN AFT BULKHEAD, STA 1363, THROUGH 8 STIFFENERS, WITH 7 STIFFENERS SHEARED. STOP DRILLED CRACKS AND REPAIR PER SRM 53-11-00, FIGURE 851. AIRCRAFT TOTAL TIME 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006071995022400607WP 1995 2 24 95ZZZX887 119950131A5320 TIE CLIP LKHEED1011 10113851 5265010WP FS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511004 193B1016 MCI - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN RT WING FT RADIUS, NR 3 STRINGER FROM LOWER REAR SPAR TIE CLIP, STA 555. AIRCRAFT TOTAL TIME: 59,528 HOURS; 23,327 CYCLES. 2L73 4F A23WE 19950224006081995022400608WP 1995 2 24 95ZZZX888 119950201A5312 BLKHD ANGLE LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND A 3 INCH CRACK IN AFT BULKHEAD OUTBOARD CORD ANGLE, THROUGH BOTH LEGS AT WL 160, STA 1363, AND FOUND EXTERIOR CORD ANGLE CRACKED. REPAIRED PER SRM 53-11-00, FIGURE 842. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006091995022400609WP 1995 2 24 95ZZZX889 119950202A5744 ATTACH FITTING LKHEED1011 1011385115 5265015WP AILERON CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531031 193B1115 JFK - DURING CHECK C-9C, FOUND CRACK IN OUTBOARD AILERON DAMPER ATTACH FITTING REAR SPAR OF LT WING INBOARD EAR. REMOVED AND REPLACED FITTING PER SRM 51-10-01, PARAGRAPH D. AIRCRAFT TOTAL TIME: 65,236 HOURS; 17,223 CYCLES. 2L73 4F A23WE 19950224006101995022400610WP 1995 2 24 95ZZZX890 119950201A5330 SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006111995022400611WP 1995 2 24 95ZZZX891 119950201A5312 BLKHD SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006121995022400612WP 1995 2 24 95ZZZX892 119950201A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1363 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511003 193B1015 JFK - DURING CHECK C-9B, FOUND FUSELAGE SKIN, AFT BULKHEAD SKIN, CRACKED AT OUTBOARD NR 7 STIFFENER, STA 1363, AND FOUND A 1.50 INCH CRACK AT OUTBOARD END OF NR 9 STIFFENER. STOP DRILLED CRACKS AND REPAIRED WITH DOUBLER PER SRM 53-11-00, FIGURE 850. AIRCRAFT TOTAL TIME: 60,716 HOURS; 22,699 CYCLES. 2L73 4F A23WE 19950224006131995022400613NE 1995 2 24 95ZZZX893 219950209A7230795075 RETAINING NUT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE LT ENG NR 3 BRG NOT TIGHT A TWAAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05916TW 49187 STL - FLT 223 - DURING CLIMB, HAD SMOKE IN CABIN. SELECTED FULL RATE CABIN PRESSURE AND FULL COLD, AND CABIN CLEARED. FOUND OIL IN 8TH STAGE AIR DUCT OF LT ENGINE, SN 1215. REPLACED LT ENGINE. ENGINE TOTAL TIME: 18,588 HOURS; 9,630 CYCLES, CHECK C-1D - 1-30-95 - MCI. INVESTIGATION INTO SMOKE IN THE CABIN, REVEALED OIL IN THE 8TH STAGE DUCT OF ENGINE 1215 CAME FROM THE NR 3 BEARING, MFG PN 795075, RETAINING NUT BEING LESS TIGHT THAN NORMAL. ENGINE SN 1215 WAS REPAIRED AND RETURNED TO SERVICE. (X) 2L72 4F4 F A6WE E9NE 19950224006141995022400614WP 1995 2 24 95ZZZX894 119950210A2120 AIR DISTRIBUTION DOUG DC9 DC982 3022082WP COCKPIT ODOR A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05950U 49230 OMA - FLT 142 - DURING CRUISE, HAD ODOR AND SMOKE IN COCKPIT. ELECTRICAL SYTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL. CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND. CHECK C-2D - 1-13-94 - MCI. 2L72 4F A6WE 19950224006151995022400615NE 1995 2 24 95ZZZX895 219950206A7250800892 TURBINE VANE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT ENGINE SHIFTED A TWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE05904TW 49156 MCI - FLT 119 - DURING CLIMB, RT ENGINE LOST POWER. SHUT DOWN ENGINE. FOUND METAL PARTICLES IN TAIL PIPE. REPLACED ENGINE, SN 3257. ENGINE TOTAL TIME: 19,850 HOURS; 10,375 CYCLES. CHECK C-2D - 1-13-94 - MRI. INVESTIGATION INTO ENGINE, SN 3257, LOSS OF POWER DURING CLIMB, REVEALED LOW PRESSURE TURBINE 2 VANE, MFG. PN 800892, SHIFTED AFT CONTACTING LOW PRESSURE TURBINE 2 BLADE, CAUSING BLADE FRACTURE. ENGINE, SN 3257, WAS REPAIRED AND RETURNED TO SERVICE. (X) 2L72 4F4 F A6WE E9NE 19950224006161995022400616WP 1995 2 24 IXXA199505 119950205A5330 SKIN DOUG DC8 DC871 302199AWP CARGO DR CUTOUT DAMAGED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23823BX715692917 46064 DURING C-CHECK, THE EDGE OF THE SKIN AT THE 'D' LOWER CARGO COMPARTMENT DOOR CUT OUT WAS FOUND MISSING A SMALL AMOUNT OF MATERIAL DUE TO PHYSICAL DAMAGE. THE DAMAGED AREA WAS CUT OUT, A FILLER INSTALLED, AND AN EXTERNAL DOUBLER AND SPLICE DOUBLER INSTALLED. THE REPAIR WAS ACCOMPLISHED IAW DRAWING HSE-27-129. WHICH WAS FAA DER APPROVED, AND ATI EO 53-DC8-121. (X) 2L74 4F 4A25 19950224006171995022400617WP 1995 2 24 IXXA199506 119950205A53305613861509 SKIN DOUG DC8 DC871 302199AWP NLG WELL CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23823BX715692917 46064 DURING ROUTINE C-CHECK INSPECTION, AN EXTERIOR SKIN CRACK WAS NOTED. THE CRACK WAS NOTED AT THE NOSE WHEELWELL AFT LT OUTBOARD CORNER OF THE DOOR CUT OUT. THE CRACK, .0250 INCH IN LENGTH, TERMINATED IN A FASTENER HOLE. AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW DRAWING HSE27-53-133, WHICH WAS FAA DER APPROVED, AND E.O. 53-DC8-122. (X) 2L74 4F 4A25 19950224006181995022400618EU 1995 2 24 RAIA950134 119950128A5270WN53 WIRE BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR CHAFED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03434AM8420 887 STL - FLT 7508 - PASSENGER DOOR LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPAIRED CHAFED WIRE AT PASSENGER DOOR. TEST REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950224006191995022400619EU 1995 2 24 RAIA950135 119950128A5270WN53 WIRE BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR PINCHED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03434AM8420 887 STL - FLT 7508 - PASSENGER DOOR LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE DISCOVERED PINCHED WIRING AT PASSENGER DOOR HANDRAIL. MAINTENANCE REPLACED PINCHED SECTION OF THE WIRING. SYSTEM TEST GOOD. (X) 2L72 4T RTA56EU 19950224006201995022400620SW 1995 2 24 RAIA950136 119950127A2913PV300426 HYD PUMP SWRNGNSA226 SA226TC 8780404SW RT ENGINE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03603AS171025357 TC239 SPI - FLT 7194 - RT HYDRAULIC PRESSURE LIGHT FLICKERED ON AND OFF. MAINTENANCE REPLACED RT HYDRAULIC PUMP. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (X) 1L72 4T A8SW 19950224006211995022400621SO 1995 2 24 RAIA950137 119950127A3000D55201001 DEICE MONITOR EMB 120 EMB120RT SO AVIONICS BAY FAILED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03128AM14371 120109 STL - FLT 7459 - DE-ICE MONITOR FAILED. MAINTENANCE RESET DE-ICE TIMER UNIT. TEST OF DE-ICING SYSTEM REVEALED NORMAL OPERATION. (X) 2L72 4T RTA31SO 19950224006221995022400622EU 1995 2 24 RAIA950138 119950129A261251224090 LOOP CONNECTOR AEROSPATR42 ATR42300 8680920EU RT ENGINE MOISTURE A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03425TE11370 125 STL - FLT 7124 - RT ENGINE FIRE LOOP A & B LOOP FAULTED, WOULD NOT RESET. MAINTENANCE CLEANED RT FIRE LOOP CONNECTIONS. SYSTEM TEST GOOD. (X) 2H72 4T RTA53EU 19950224006231995022400623EU 1995 2 24 RAIA950139 119950129A261251224090 FIRE LOOP AEROSPATR42 ATR42300 8680920EU RT ENGINE FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03425TE11370 125 STL - FLT 7124 - RT ENGINE FIRE DETECTION WENT OFF AFTER TAKEOFF. NO ACTUAL FIRE WAS NOTED. MAINTENANCE REPLACED RT ENGINE FIRE LOOP. SYSTEM TEST REVEALED NORMAL OPERATION. (X) 2H72 4T RTA53EU 19950224006241995022400624EU 1995 2 24 RAIA950140 119950127A33503011151 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03426TE8661 746 228 STL - EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING POWER SUPPLY. (X) 2H72 4T RTA53EU 19950224006251995022400625EU 1995 2 24 RAIA950143 119950129A33503012000 EEL POWER SUPPLY AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE5971 1425 283 STL - MAINTENANCE - EMERGENCY PATH LIGHTING WILL NOT TURN OFF AT MIDDLE SECTION. MAINTENANCE REPLACED POWER SUPPLY. (X) 2H72 4T RTA53EU 19950224006261995022400626EU 1995 2 24 RAIA950144 119950131A75008961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENG FAILED A RAIAO OTHER JR WARNING INDICATION PARTIAL RPM/PWR LOSS CLCLIMB 1 CE03973JX3211 973 66334 STL - FLT 4728 - RT ENGINE TORQUE DROPPED RAPIDLY. MAINTENANCE REPLACED RT ENGINE BLEED AIR GASKETS. POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T4 TRTA56EU E4WE 19950224006271995022400627EU 1995 2 24 RAIA950201 119950203A2422559012A INVERTER AEROSPATR42 ATR42300 8680920EU NR 2 FAILED A RAIAO OTHER J WARNING INDICATION CRCRUISE 1 CE032FOR 11578 176 STL - FLT 7146 - NR 2 INVERTER FAULTED. MAINTENANCE REPLACED NR 2 INVERTER. OPERATIONAL CHECK GOOD. (X) 2H72 4T RTA53EU 19950224006281995022400628EU 1995 2 24 RAIA950202 119950205A32601849D SWITCH BAG JETSTMJETSTM3201 1500217EU RT MLG DIRTY A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03339TE8891 935 STL - FLT 7308 - RT MAIN GEAR UNLOCK LIGHT STAYS ON WITH GEAR SELECTED UP. MAINTENANCE CLEANED RT MAIN GEAR UPLOCK AND DOWNLOCK SWITCHES. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950224006291995022400629GL 1995 2 24 RAIA950203 319950203A6112 DEICE BAG JETSTMJETSTM3201 1500217EU ROTOL R333 R333482F12 GL RIGHT ENGINE FAILED A RAIAO OTHER O OTHER CRCRUISE 1 CE03430AM7786 1840 880 DRG89 STL - 7512 - RT PROPELLER DE-ICE INOPERATIVE. MAINTENANCE REPLACED RT PROPELLER ASSEMBLY. DE-ICE SYSTEM CHECK NORMAL. (X) 2L72 4T RTA56EU 6 CP61GL 19950224006301995022400630EU 1995 2 24 RAIA950204 119950203A32609EN1C11HB2BB2 DOWNLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NLG FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03337TE9305 885 929 STL - FLT 7332 - NOSE GEAR INDICATES IN THE DOWN POSITION WITH GEAR SELECT HANDLE IN THE UP POSITION. MAINTENANCE REPLACED NOSE GEAR DOWNLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950224006311995022400631SW 1995 2 24 RAIA950205 119950203A2435230790001 STARTER\GEN SWRNGNSA226 SA226TC 8780404SW LT ENGINE FAILED A RAIAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 CE03603AS22352798 TC239 SP - FLT 7190 - LEFT GENERATOR FELL OFF LINE. MAINTENANCE REPLACED LEFT STARTER GENERATOR, OPERATIONAL CHECK GOOD. (X) 1L72 4T A8SW 19950224006321995022400632SW 1995 2 24 RAIA950206 119950203A2430230790001 GEN CONTL UNIT SWRNGNSA226 SA226TC 8780404SW LT ENGINE FAILED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03603AS236914365 TC239 SPI - FLT 7198 - LEFT GENERATOR FELL OFF LINE. MAINTENANCE REPLACED LEFT GENERATOR CONTROL UNIT. (X) 1L72 4T A8SW 19950224006331995022400633SO 1995 2 24 RAIA950207 119950206A30607861442 DEICE LEAD EMB 120 EMB120RT SO RT PROPELLER FAILED A RAIAO OTHER J WARNING INDICATION CRCRUISE 1 CE03125AM126063106 120017 STL - FLT 7452 - RT PROPELLER DE-ICE FAULTED. MAINTENANCE REPLACED RT PROPELLER DE-ICE LEAD. SYSTEM CHECK GOOD. (X) 2L72 4T RTA31SO 19950224006341995022400634EU 1995 2 24 RAIA950208 119950206A3060660716235 DEICE LEAD BAG JETSTMJETSTM3201 1500217EU LT PROPELLER BROKEN A RAIAO OTHER O OTHER CRCRUISE 1 CE03423AM7488 2988 858 STL - FLT 7308 - LT PROPELLER HEAT INOPERATIVE. MAINTENANCE REPLACED LT PROPELLER BROKEN DE-ICE LEAD. SYSTEM CHECK GOOD. (X) 2L72 4T RTA56EU 19950224006351995022400635WP 1995 2 24 RAIA950209 219950208A73218977801 FCU BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03433AM754722013 885 66146 RIGHT ENGINE FAILED TO MAKE TARGET TORQUE. MAINTENANCE REPLACED RT FUEL CONTROL UNIT. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T4 TRTA56EU E4WE 19950224006361995022400636SO 1995 2 24 RAIA950210 119950208A27503472001001 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03128AM5899 120109 STL - FLT 7495 - FLAP DISAGREEMENT WAS EXPERIENCED AFTER TAKEOFF. MAINTENANCE RERACKED FLAP CONTROL UNIT. SYSTEM TEST GOOD. (X) 2L72 4T RTA31SO 19950224006371995022400637EU 1995 2 24 RAIA950211 119950203A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR OUT OF ADJUST A RAIAO OTHER N FALSE WARNING NRNOT REPORTED 1 CE03342TE5587 954 STL - FLT 7035 - PASSENGER DOOR LIGHT ILLUMINATED EN ROUTE TO STL. MAINTENANCE CLEANED AND ADJUSTED PASSENGER DOOR MICROSWITCH. SYSTEM OPERATION CHECK GOOD. (X) 2L72 4T RTA56EU 19950224006381995022400638NE 1995 2 24 UF6A950201 319950131A6110 PROP ABA811011A BAG ATP ATP EU HAMSTD5500 65500F1 NE NR 1 ENGINE DAMAGED A UF6AK NONE C F.O.D. TXTAXI/GRND HDL 1 CE03857AW6473 4A424891 2034 GRB - FLT 5069 - NR 1 PROP STRUCK STAND ON SHUT DOWN AT THE GATE. MAINTENANCE REPLACED NR 1 PROP ASSEMBLY, TOOK OIL SAMPLE AND INSPECTED CHIP DETECTOR. OPS CHECK GOOD. (X) 2L72 4T RTA27NM 6 CP13NE 19950224006391995022400639EU 1995 2 24 UF6A950202 119950203A3350HWBON11462BAU2 EEL CONNECTOR BAG ATP ATP EU CABIN LOOSE A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03855AW7080 2029 GRB - FLT 5089 - THREE EMERGENCY LIGHT STRIPS INOPERATIVE. MAINTENANCE RESECURED LOOSE CONNECTOR. (X) 2L72 4T RTA27NM 19950224006401995022400640EU 1995 2 24 UF6A950203 119950204A7931648846062 OIL PRESS GAUGE BAG ATP ATP EU RT ENGINE FAILED A UF6AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03859AW3941 2036 ORD - FLT 5027 - RIGHT OIL PRESSURE FLUCTUATING IN-FLIGHT. MAINTENANCE REPLACED RIGHT OIL PRESSURE GAUGE. (X) 2L72 4T RTA27NM 19950224006411995022400641EU 1995 2 24 UF6A950204 119950205A33506013211 EEL CONNECTOR BAG ATP ATP EU CABIN LOOSE A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03860AW5302 2037 GRB - FLT 5062 - EMERGENCY LIGHT INOPERATIVE AT ROWS 6 AND 7, ROWS 13 AND 14. MAINTENANCE RESECURED LOOSE CONNECTION ON POWER SUPPLY. (X)` 2L72 4T RTA27NM 19950224006421995022400642EU 1995 2 24 UF6A950205 119950207A27501ENN14 SWITCH BAG ATP ATP EU TE FLAPS FAILED A UF6AO OTHER N FALSE WARNING ININSP/MAINT 1 CE03859AW6320 2036 PIA - FLT 5090 - FLAPS FAILED AT ZERO DEGREES. MAINTENANCE REPLACED THE DOWN MICROSWITCH (CG18). (X) 2L72 4T RTA27NM 19950224006431995022400643WP 1995 2 24 AALA950085 119950119A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07447AA 49473 SWF - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 22 TO 24 INOPERATIVE. ACFT MAINTENANCE FERRY SWF/DFW. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950224006441995022400644NM 1995 2 24 AALA950089 119950121A3350S283T0231 EEL INVERTER BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN MID-GALLEY INOPERATIVE. REPLACED INVERTER FOR EMERGENCY FLOOR LIGHTS IN MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950224006451995022400645 1995 2 24 AALA950162 419950131A2565CBB3334B SLIDE BOEING727 727223 1384074NM PAX DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07872AA 21384 ORD - DURING SHOP VISIT, FOUND 6 INCH SEAM SEPARATION AT GIRT BAR END OF EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W) 2L73 4F A3WE 19950224006461995022400646 1995 2 24 AALA950164 419950130A2565CBB3334B SLIDE BOEING727 727223 1384074NM PAX DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07868AA 21373 ODR - DURING SHOP VISIT, FOUND 3 INCH SEAM SEPARATION AT BOTTOM LT CENTER OF EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W) 2L73 4F A3WE 19950224006471995022400647 1995 2 24 AALA950165 419950130A2565CBB3334B SLIDE BOEING727 727223 1384074NM PAX DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW076803 19478 ORD - DURING SHOP VISIT, FOUND GIRT COMING UNGLUED ON EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W) 2L73 4F A3WE 19950224006481995022400648 1995 2 24 AALA950166 419950130A2565CBB1683A SLIDE BOEING727 727227 1384078NM PAX DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07731AA 20738 ORD - DURING SHOP VISIT, FOUND GIRT COMING UNPLUGGED AT MATING SURFACE, ALSO HAD RUNWAY SEAM SEPARATION ON EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (W) 2L73 4F A3WE 19950224006591995022400659NM 1995 2 24 MRKA9514 119950117A3350862100601 EEL BATT PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03674MA 23292 THE FLOOR PROXIMITY LIGHTS AT ROWS 8, AND 19 FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED OK. (W) 2L72 4F RTA16WE 19950224006601995022400660NM 1995 2 24 MRKA9515 119950117A3350873100252 EEL ASSY BOEING737 7372X6C 1384552NM CABIN INOP A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03674MA 23292 THE LT OVERWING EXIT IDENTIFIER LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. (W) 2L72 4F RTA16WE 19950224006761995022400676WP 1995 2 24 USAA950036 119950122A2130 PRESSURIZATION DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19925VJ 48145 PIT - FLT 358 - ON CLIMB-OUT, THE ACFT WOULD NOT PRESSURIZE IN EITHER THE AUTO OR MANUAL MODE. CREW DECIDED TO DIVERT TO PIT. MAINTENANCE INSPECTED THE OUTFLOW VALVE, ALL DUCTING, DOORS, AND FRAMES. NO ABNORMALITIES WERE FOUND. THE ACFT WAS PRESSURIZED TO 7.5 PSI. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950224006771995022400677WP 1995 2 24 USAA950037 119950122A56105912290502 WINDSHIELD DOUG DC9 DC931 3022065WP COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19946VJ 47026 DCA - FLT 545 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD HAD AN ELECTRICAL ARCING WHICH IMMEDIATELY CAUSED APPROXIMATELY TWENTY CRACKS IN THE OUTSIDE WINDOW. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DCA. MAINTENANCE REPLACED THE WINDSHIELD. AN OPERATIONAL CHECK OF THE WINDSHIELD ANTI-ICING AND ANTI-FOGGING SYSTEMS WERE CHECKED. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950224006781995022400678WP 1995 2 24 USAA950040 119950121A2913AS66411LS666 PUMP DOUG DC9 DC931 3022065WP NR 2 ENGINE SHEARED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19930VJ 45868 CLT - FLT 2350 - ON CLIMB-OUT, THE RT ENGINE HYDRAULIC PUMP FAILED. CREW DECIDED TO RETURN TO CLT. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAULIC PUMP. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950224006791995022400679WP 1995 2 24 USAA950044 119950120A30101059842 ANTI-ICE VALVE DOUG DC9 DC931 3022065WP TAIL INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19959VJ 47352 CLT - FLT 1531 - ON CLIMB-OUT, THE CAPTAIN ADVISED THAT HE LOST ANTI-ICE CAPABILITIES. FLIGHT DIVERTED TO CLT. MAINTENANCE REPLACED THE ANTI-ICE TAIL VALVE. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950224006801995022400680WP 1995 2 24 USAA950085 119950130A3230 RETRACT MECH DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19920VJ 48140 PIT - FLT 1005 - AFTER TAKEOFF, THE CAPTAIN RAISED THE GEAR, BUT GOT AN UNSAFE NOSE GEAR INDICATION LIGHT. THE GEAR WAS LOWERED, BUT THE UNSAFE NOSE GEAR LIGHT REMAINED. THE CAPTAIN THEN USED ABNORMAL PROCEDURES TO LOWER THE NOSE GEAR, AND RECEIVED A GREEN LIGHT FOR NOSE GEAR DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO GATE. MX INSPECTED THE LANDING GEAR AND ALL COMPONENTS. NO ABNORMAL CONDITIONS WERE NOTED. A GEAR SWING WAS PERFORMED, ALL OPERATING PARAMETERS WERE WITHIN LIMITS. NO OTHER DISCREPANCIES WERE NOTED. (W) 2L72 4F A6WE 19950303000011995030300001WP 1995 3 3 9502799953 119950215A2810 FUEL SYS DOUG DC9 DC931 3022065WP RT TANK VENTING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 GL01918RW 47158 FUEL BEGAN LEAKING FROM LEFT WING ENROUTE HPN-MSP. FUEL WAS VENTING FROM THE RIGHT TANK AT A RATE OF 800 POUNDS PER HOUR. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED FUEL TANK BACKFLUSH PROCEDURE PER MAINTENANCE MANUAL. NO TRANSFER PROBLEMS WERE NOTED ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303000021995030300002 1995 3 3 9503016635 419950224A341737571832 COMPUTER BOEING747 747227B 1384888NM E/E COMPARTMENT INOPERATIVE A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01635US2719018 21682 DURING CRUISE, THE CAPTAIN'S MACH INDICATOR, VSI, TAS INDICATOR, AND EPRL BEGAN TO FLUCTUATE. THE NR 1 AUTO-PILOT AND AUTO-THROTTLES BECAME INOPERATIVE. THE AIRCRAFT DIVERTED TO HNL AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 CENTRAL AIR DATA COMPUTER. OPERATIONAL CHECK OK. 2L74 4F A20WE 19950303000031995030300003NM 1995 3 3 95FDEA00163 119950216A5313 STRINGER BOEING727 727233 138408ANM BS 460 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04284FE 22621 WHILE WORKING NR 0335, DISCOVERED STR 1 CRACKED AT BS 460. CUT FRAME TO FACILITATE STR REMOVAL, REMOVED PORTION OF DAMAGED STR, REPAIRED STR AND FRAME PER SRM 53-10-4, 57-40-5, 53-10-3. 2L73 4F RTA3WE 19950303000041995030300004NM 1995 3 3 95FDEA00164 119950220A5720651620053 STIFFENER BOEING727 727277 138408SNM FSS 260 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04241FE 20979 MCM - LT WING FRONT SPAR STIFFENER CORRODED AND EXFOLIATED UNDER HYD LINE CLAMP STANDOFFS. LOCATED JUST OUTBD OF BOOST PUMP PRESSURE SWITCHES APPROX. FRONT SPAR STA 260. REMOVED HYD LINES LT WING F.O.M. INSTALLED SPAR STIFFENER REF EA 7-5710-3813 REV A. CLOSED FUEL TANK, LEAK CK OK. 2L73 4F RTA3WE 19950303000051995030300005NM 1995 3 3 95FDEA00165 119950218A5210 SEAL BOEING727 72724C 1384005NM FWD ENTRY DOOR CRACKED A FDEAK NONE O OTHER CLCLIMB 1 SO04114FE 19527 FWD ENTRY DIFFICULT TO CLOSE AND OPEN. UPON CLOSER INSP FOUND A CRACKED SEAL AROUND UPR ROLLER ASSY AT REAR. UNABLE TO CLOSE DOOR COMPLETELY. (UPR AND LWR AFT ROLLER AREAS CRACKED.) REPAIRED DAMAGED FRAME PER EA 7-5210-23817. FWD ENTRY DOOR INSTALLED AND ADJUSTMENT/TEST C/W IAW MM 52-11-01. OK FOR SERVICE. 2L73 4F A3WE 19950303000061995030300006NM 1995 3 3 95FDEA00166 119950224A2120 AIR DISTR BOEING727 727233 138408ANM FLIGHT DECK ODOR A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO04178FE 22345 DURING CLIMB THROUGH APPROX 20,000 AN ACRID ODOR BECAME EVIDENT IN THE COCKPIT. ODOR DISSIPATED WHEN PACKS SECURED ON LANDING. REMOVED AND REPLACED LEFT AND RIGHT CONDENSOR BAG & LEAK CHECKED GOOD. CHECKED ALL PNUEMATICS DUCTS LEAKAGE, NO LEAKS. 2L73 4F RTA3WE 19950303000071995030300007WP 1995 3 3 ABXA9500097 119950222A52803923159505 ARM DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARM ASSEMBLY WORN. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000081995030300008WP 1995 3 3 ABXA9500098 119950222A52803923166501 FITTING DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244 FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR FITTING WORN. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000091995030300009WP 1995 3 3 ABXA9500100 119950222A52803923159505 ARM DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR ARM ASSEMBLY WORN. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000101995030300010WP 1995 3 3 ABXA9500101 119950222A528029244721 PIN DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR TO WING HINGE PINS WORN. REPLACED HINGE PINS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000111995030300011WP 1995 3 3 ABXA9500102 119950220A524099115827N BEAM DOUG DC9 DC931 3022065WP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING COMPLIANCE OF AD 81-10-10, SBR 52-125 AND 52-127, FOUND HORIZONTAL BEAM CRACKED AT HINGE ATTACH STA Z30,187 BETWEEN Y 170 AND Y176.5. REPLACED SERVICE DOOR ASSEMBLY IAW DC-9 MM 52-41-0. 2L72 4F A6WE 19950303000121995030300012WP 1995 3 3 ABXA9500103 119950220A524099115827N BEAM DOUG DC9 DC931 3022065WP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING COMPLIANCE OF AD 81-10-10, SB 52-125 AND 52-127, FOUND HORIZONTAL BEAM CRACKED AT HINGE ATTACH STA. Z11.063 BETWEEN Y170 AND Y176.5. REPLACED SERVICE DOOR ASSEMBLY IAW DC-9 MM 52-41-0. 2L72 4F A6WE 19950303000131995030300013WP 1995 3 3 ABXA9500105 119950220A5280S2210370P4101 BUSHING DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY ON LEFT MAIN GEAR OUBOARD DRIVE ROD IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19950303000141995030300014WP 1995 3 3 ABXA9500108 119950220A3231NAS110520D BOLT DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19950303000151995030300015WP 1995 3 3 ABXA9500109 119950205A52805913433503 HINGE DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR ARTICULATING DOOR BUSHING WORN ON OUTBOARD MAIN LANDING GEAR DOOR FOR WING MOUNTED HINGE. REPLACED HINGE IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000161995030300016NE 1995 3 3 ABXA9500110 219950210A7240541992 DRAIN BOSS PWA JT8D7B DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 657552 47552 657552 DURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY ASB 5676, FOUND CRACK INDICATION ON FORWARD LOWER COMBUSTION CHAMBER OUTER CASE DRAIN BOSS. REPLACED ENGINE IAW ABX WORKCARD RJT 7001. 2L72 4F4 F A6WE E2EA 19950303000171995030300017NE 1995 3 3 ABXA9500111 219950220A7240541992 DRAIN BOSS PWA JT8D7B DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 657399 47072 657399 DURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY SB 5676, FOUND PS4 AND LOWER AFT DRAIN BOSS ON OUTER CASE OF COMBUSTION CHAMBER HAD CRACK INDICATIONS. REPLACED NR 1 ENGINE IAW ABX WORKCARD RTJ 7001. 2L72 4F4 F A6WE E2EA 19950303000181995030300018WP 1995 3 3 ABXA95099 119950222A5280HB218600 BUSHING DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23967AX 47509 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR DOOR TO WING HINGE BUSHINGS WORN. REPLACED HINGE BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950303000191995030300019WP 1995 3 3 ABXA95104 119950220A3231NAS110520D BOLT DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19950303000201995030300020WP 1995 3 3 ABXA95106 119950220A32313923159501 ROD END DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD END WORN. REPLACED ROD END ARM ASSEMBLY IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19950303000211995030300021WP 1995 3 3 ABXA95107 119950222A5280S2210370P4101 BUSHING DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19950303000221995030300022NM 1995 3 3 DL72E950758 119950203A5521 SPAR BOEING727 727247 138408FNM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 DURING INSPECTION, THE RIGHT ELEVATOR REAR SPAR WAS FOUND TO HAVE A CRACK EMANATING .1250 INCH FROM THE INBD SIDE OF THE SHEAR PLATE AT THE SECOND FROM THE OUTBD TAB HINGE FITTING TO REAR SPAR ATTACHMENT. THE CRACK WAS STOP DRILLED IN ACCORDANCE WITH B727 S/B 55-087, THE CRACK WAS STOP DRILLED AND SET UP FOR REPETITIVE INSPECTION AND PERMANENT REPAIR. 2L73 4F A3WE 19950303000231995030300023NM 1995 3 3 DL72K950820 119950222A3350 EEL BULB BOEING727 727232 1384082NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11413DA 21233 DURIING PREFLIGHT FOUND SEVERAL LIGHTS OUT IN FLOOR ESCAPE PATH TRACK LIGHTS, RELAMPED, OPERATION NORMAL. 2L73 4F A3WE 19950303000241995030300024NM 1995 3 3 DL72L950778 119950222A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 FOUND DURING C-1 LETTER CHECK - 1 INCH CRACKED VERTICAL STAB, OUTER SKIN AT STR 10. REPAIRED PER MM 55-30-0 PG 801. 2L73 4F A3WE 19950303000251995030300025NM 1995 3 3 DL72L950779 119950222A5754 SLAT BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 FOUND DURING C-1 LETTER CHECK - .25 INCH CRACK AT NR 3 L/E SLAT BELOW TAI TELESCOPING ROD. REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950303000271995030300027NM 1995 3 3 DL72L950782 119950222A5754 SLAT BOEING727 727232 1384082NM NR 6 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 NR 6 SLAT CRACKED AT ACT. MOUNT BOLT I/B SIDE (.50 INCH). FOUND DURING C-1 LETTER CHECK TPAMM. REPAIRED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950303000281995030300028NM 1995 3 3 DL72S950742 119950119A5753652163261 MIDFLAP BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING SHOP INSPECTION A CRACK WAS FOUND IN AFT LOWER CHORD 12 INCHES AFT OF IB CARRIAGE SUPPORT. THE CHORD WAS REPAIRED PER MM 57-52-0. THIS DAMAGE WAS IN NR 2 MID FLAP. 2L73 4F A3WE 19950303000291995030300029NM 1995 3 3 DL72S950743 119950119A5753652163261 MIDFLAP BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING SHOP INSP. CRACK AT IB ACTUATOR CUT-OUT WAS REPAIRED PER MM 57-52-0, DAMAGE FOUND IN NR 2 MID FLAP. 2L73 4F A3WE 19950303000301995030300030NM 1995 3 3 DL72S950744 119950119A575365216321 MIDFLAP BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING SHOP INSPECTION A CRACK WAS FOUND AT THE 2ND FROM IB AFT FLAP TRACK CUT-OUT IN AFT LOWER CHORD OF NR 2 MID FLAP. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950303000311995030300031NM 1995 3 3 DL72S950745 119950119A5753652163261 MIDFLAP BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING SHOP VISIT AFT LOWER CHORD WAS FOUND CRACKED 15 INCHES AND 29 INCHES FROM IB END, OF NR 2 MID FLAP. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950303000321995030300032NM 1995 3 3 DL72S950746 119950119A5753652163261 MIDFLAP BOEING727 727232 1384082NM NR 2 TE MIDFLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING SHOP VISIT THE OB CARRIAGE SUPPORT FITTING WAS FOUND TO HAVE THE TWO IB THRUST BEARING RETAINER BOLT HOLES CORRODED, IN NR 2 MID FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950303000331995030300033NM 1995 3 3 DL72S950752 119950221A5320 WEB BOEING727 727232 1384082NM FS 1218 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 .25 INCH CRACK IN VERT. WEB RT SIDE OF STAIRWAY STA 1218 PROTRUDING FROM 1ST RIVET IN UPPER ROW. DAMAGE FOUND AT LETTER CHECK, REPAIRED PER MM 53-11-00 PG 832-833. 2L73 4F A3WE 19950303000341995030300034NM 1995 3 3 DL72S950753 119950221A5330 SKIN BOEING727 727232 1384082NM FWD ENT CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 1.1250 INCH CRACK ON LWR HINGE CUT-OUT FWD ENTRY DOOR AT FUSELAGE SKIN. DAMAGE FOUND AT LETTER CHECK. REPAIRED PER PER M/M 53-30-0. 2L73 4F A3WE 19950303000351995030300035NM 1995 3 3 DL72S950754 119950221A5320 BEAM BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 DURING LETTER CHECK, FOUND CRACK IN VERTICAL BEAM AT FS 1183 AT RBL 8. REPAIRED PER MM 53-11-0 FIG 809. 2L73 4F A3WE 19950303000361995030300036NM 1995 3 3 DL72S950773 119950207A5320 FLOOR SUPPORT BOEING727 727232 1384082NM FS 950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 FOUND ON LTR CK - 1 INCH CRACK THROUGH MOUNT BOLT HOLE FLOOR PANEL SUPPORT CHANNEL FWD SIDE STA 950C BL 18R - REPAIR - REPAIRED PER SRM 53-10-5 AND I.D. PER P.S. 900-5-1 NR 4. 2L73 4F A3WE 19950303000371995030300037NM 1995 3 3 DL72S950785 119950206A5347 SEAT TRACK BOEING727 727232 1384082NM FS 480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 480 LBL 22 - REPAIR - REPLACED DAMAGED SEAT TRACK FROM 440-480 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950303000381995030300038NM 1995 3 3 DL72S950786 119950206A5347 SEAT TRACK BOEING727 727232 1384082NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 344 TO 360 AT LBL 22 - REPAIR - REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950303000391995030300039NM 1995 3 3 DL72S950787 119950206A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION AT FLOOR BEAM TOP SIDE AND BOTTOM WHERE CLIP NUTS ATTACH STATION 380 RBL 12 TO 63 - REPAIR - REPLACED TEE CAP PER SRM 53-10-8. 2L73 4F A3WE 19950303000401995030300040NM 1995 3 3 DL72S950788 119950206A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 1110 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION AT FLOOR BEAM AT BL 0 TO LBL 16 STA 1110 - REPAIR - INSTALLED REPAIR ANGLE PER MM 53-20-11 FIG 804A. 2L73 4F A3WE 19950303000411995030300041NM 1995 3 3 DL72S950789 119950206A5320 CLIP BOEING727 727232 1384082NM FS 303 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION AT LOWER FWD FUSELAGE SKIN CLIP STA 303 AT NOSE W/W CHORD - REPAIR - REPAIRED PER SRM 51-40-3 FIG 1. 2L73 4F A3WE 19950303000421995030300042 1995 3 3 DL72S950791 419950221A3160694849824 PANEL BOEING727 727232 1384082NM FLIGHT DECK SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11402DA 21146 DURING CRUISE, HAD ELECTRICAL BURNING SMELL AND SMOKE COMING FROM FLIGHT ENGINEERS PANEL THROUGH GASPER FAN SWITCH HOLE. DEACTIVATED CIRCUITS, ODOR CEASED. FOUND P4-22 PANEL SHORTED TO GROUND. REPLACED PANEL, OPERATION NORMAL. 2L73 4F A3WE 19950303000431995030300043NM 1995 3 3 DL72S950793 119950206A5313 STRINGER BOEING727 727232 1384082NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 0 FOUND ON CV2 CK - CORROSION INSIDE STRINGER 27L FWD STA 720F - REPAIR - REPLACED SECTION OF STRINGER PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950303000441995030300044NM 1995 3 3 DL72S950795 119950222A5754651622296 SKIN BOEING727 727232 1384082NM NR 6 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11485DA 20865 0 DURING INSPECTION, FOUND NR 6 SLAT WITH CRACKED L-ANGLE UNDER UP-STOP. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950303000451995030300045NM 1995 3 3 DL72W950759 119950202A5530 STRINGER BOEING727 727247 138408FNM FIN STA 110.4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING INSPECTION AT OVERHAUL, STRINGER 7R OF THE VERTICAL STABILIZER WAS FOUND CRACKED AT THE FIN STA 110.4 RIB ATTACHMENT TAB. IN ACCORDANCE WITH B727 S/B 55-0075, A REPAIR ANGLE WAS INSTALLED. 2L73 4F A3WE 19950303000461995030300046NM 1995 3 3 DL733950764 119950216A5347 SEAT TRACK BOEING737 737347 1384647NM FS 947 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 LT I/B SEAT TRACK CORRODED AT F.S. 947. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52. 2L72 4F RTA16WE 19950303000471995030300047NM 1995 3 3 DL733950765 119950220A5347 SEAT TRACK BOEING737 737347 1384647NM FS 328-344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 FOUND AT H.M.V. RT CTR SEAT TRACK CORRODED BETWEEN STA 328 AND 344. REPAIRED PER SRM 53-00-52 PG 202. 2L72 4F RTA16WE 19950303000481995030300048NM 1995 3 3 DL733950766 119950220A5347 SEAT TRACK BOEING737 737347 1384647NM FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 FOUND AT H.M.V. RT I/B SEAT TRACK CORRODED AT FS 328. REPAIRED PER SRM 53-00-52 PG 202. 2L72 4F RTA16WE 19950303000491995030300049NM 1995 3 3 DL733950767 119950216A5320 FLOOR SUPPORT BOEING737 737347 1384647NM FS 947-967 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 FLOOR SUPPORT CORRODED LBL 25 FS 947-967. FOUND AT H.M.V. REPAIRED PER SRM 53-00-52 FIG 204. 2L72 4F RTA16WE 19950303000501995030300050NM 1995 3 3 DL733950768 119950216A5522 TE SKIN 65C2574683A BOEING737 737347 1384647NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 8430F 23442 LT ELEVATOR HAS INBOARD TRAILING EDGE DAMAGED. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01. PART DAMAGED DURING ROUTING. 2L72 4F RTA16WE 19950303000511995030300051NM 1995 3 3 DL733950769 119950216A5522 SKIN 65C2574684 BOEING737 737347 1384647NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 8433F 23442 FOUND AT H.M.V. RT ELEVATOR HAS SCAB PATCH ON BOTTOM SURFACE OF COMPOSITE. REPAIRED PER SRM 51-70-17. 2L72 4F RTA16WE 19950303000521995030300052NM 1995 3 3 DL733950770 119950217A5522 SKIN 65C2638411A BOEING737 737347 1384647NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 9998V 23442 LT ELEVATOR TAB HINGE OPENINGS CRACKED SEVERAL PLACES. FOUND AT H.M.V. REPAIRED PER SRM 55-20-01. 2L72 4F RTA16WE 19950303000531995030300053NM 1995 3 3 DL733950772 119950216A5522 SKIN 65C2638411A BOEING737 737347 1384647NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 4920L 23442 RT ELEVATOR TAB HAS COMPOSITE BROKEN OUT AT HINGE OPENINGS. FOUND AT H.M.V. REPAIRED PER SRM 51-40-15. 2L72 4F RTA16WE 19950303000541995030300054NM 1995 3 3 DL73E950771 119950125A52306546921528 FRAME BOEING737 7372J8 1384489NM FWD CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11235WA 22859 DURING SHOP INSPECTION, A 0.70 INCH CRACK WAS FOUND IN THE INNER RADIUS OF THE FORWARD CARGO DOOR FRAME. THE CRACK IS LOCATED ON THE FORWARD EDGE OF THE DOOR BETWEEN DOOR STOP NR 4 & NR 5. REPAIRED PER ERA 270046-14AD. 2L72 4F RTA16WE 19950303000561995030300056NM 1995 3 3 DL76L950774 119950221A5753 SKIN BOEING767 767332 1382001NM RT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11181DN 25986 DURING LETTER CHECK INSP. FOUND AREA OF DAMAGE ON LOWER SURFACE OF T/E FORE FLAP MARKED IN LINE WITH NR 8 TIRE, RT WING. INSTALLED PERMANENT REPAIR PER SRM 57-53-01 FIG 201. 2L72 4F RTA1NM 19950303000591995030300059WP 1995 3 3 DLL10950739 119950208A7110LJ21744 NOSE COWL LKHEED1011 10113851 5265010WP 1/3 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO111731D 193C1200 DURINE A ROUTINE SHOP INSPECTION, NR 1 ENGINE NOSE COWL, FOUND CRACKED AT FORWARD BULKHEAD OUTER ANGLE OF NOSE COWL. THE CRACK WAS REPAIRED PER SRM 54-21-00. 2L73 4F A23WE 19950303000601995030300060WP 1995 3 3 DLL10950741 119950222A57531529113111 VANE LKHEED1011 10113851 5265010WP LT TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 DURING SHOP INSPECTION, LEFT WING FLAP VANE WAS FOUND WITH TWO CRACKS IN THE UPPER SKIN. REPAIRED PER SRM 57-53-00. 2L73 4F A23WE 19950303000611995030300061WP 1995 3 3 DLL15950794 119950220A5755 HINGE LUGS LKHEED1011 10113853 5265020WP LT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11756DR 193Y1185 0 E.O. 7-68609-12 OPN. 103 FOUND CRACKED INBETWEEN I/B SPOILER HINGE LUGS OF NR 2 SPOILER. DAMAGE FOUND AT LETTER CHECK. REPAIRED PER SRM 57-22-00 FIG 806. 2L73 4F A23WE 19950303000621995030300062WP 1995 3 3 DLL16950735 119950217A5330 STRAP LKHEED1011 10113853 5265020WP C-1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 C-1 B/B FAILSAFE STRAP DELAMINATED, F/S 749-769, STRINGERS 30 AND 34. ACTUAL LOCATION F/S 860, STRINGERS 30 AND 34. DAMAGE FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950303000631995030300063WP 1995 3 3 DLL16950736 119950214A5330 STRAP LKHEED1011 10113853 5265020WP C-2 COMPT DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 TEAR STRAP DISBONDED - C-2 F/S 1735 BETWEEN STR 34 AND 35. REPAIRED PER SRM 53-31-00 PAGE 830. DAMAGE FOUND AT HMV. 2L73 4F A23WE 19950303000641995030300064WP 1995 3 3 DLL16950737 119950212A57531529112109 SKIN LKHEED1011 10113853 5265020WP LT TE FLAP VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HVM, FOUND LEFT WING FLAP VANE WITH CRACK IN UPPER SKIN. DAMAGED WAS REMOVED AND REPAIRED PER SRM 57-53-00 FIG 806. 2L73 4F A23WE 19950303000651995030300065WP 1995 3 3 DLL16950738 119950212A5330 SKIN LKHEED1011 10113853 5265020WP FS 182 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 FUSELAGE SKIN GOUGED STA 182 BELOW L-2 COCKPIT WINDOW. FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 811. DAMAGE FOUND AT HMV. 2L73 4F A23WE 19950303000661995030300066WP 1995 3 3 DLL16950755 119950213A5330 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP C-1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 ITEM NR 1 C1 B/B-FAILSAFE STRAP DELAMINATED-F.S.729-749, STRINGERS NR 37 AND NR 34. ITEM NR 2 SAME AREA AT STRINGERS NR 31 AND NR 32, N.R. 484, CONT. ON N.R. 1514. CORRECTION: REMOVED CORROSION AT STRINGERS NR 32 AND NR 31 F.S. 729-749. THICKNESS OF STRINGERS NR 31 AND NR 32 STA. 749, .062 INCH, REMOVED EXPOSED ADHESIVE AT STR. 34, CUT STRAP AT STR 37, FABRICATED SPLICE. PAINTED ALL AREAS, DRILLED ATTACH PATTERN IN TEAR STRIP AT STR. 31-32. INSTALLED REPAIR AT STR. 37. INST. TACT PAT. AT STR 31-32 & INSTALLED SPLICE AT STR. 34 PER SRM 53-31-00 PG. 830. 2L73 4F A23WE 19950303000671995030300067WP 1995 3 3 DLL16950796 119950224A5712 RIB CAPS LKHEED1011 10113853 5265020WP WS 293.38/319.83CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, RIB CAPS AT IWS 293.38 AND 319.83 WERE CUT TO FACILITATE REMOVAL AND COLD WORK OF FASTENERS IN REAR SPAR REWORK. REF EO 7-59089-3. REPAIRED RIBS PER SRM 57-12-00. 2L73 4F A23WE 19950303000681995030300068WP 1995 3 3 DLL16950797 119950224A5330 SKIN LKHEED1011 10113853 5265020WP FS 220 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN DENTED AT FS 220 BETWEEN STRINGERS 3 AND 4. REPAIRED PER SRM 53-31-0. 2L73 4F A23WE 19950303000691995030300069WP 1995 3 3 DLL16950798 119950224A5347 SEAT TRACK LKHEED1011 10113853 5265020WP FS 1705/1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND CABIN SEAT TRACK AT FS 1705 AND 1725, 4TH FROM LEFT SIDE, CORRODED. REPLACED TRACK, PER SRM 53-21-00. 2L73 4F A23WE 19950303000701995030300070WP 1995 3 3 DLL16950799 119950224A53131550247103 LONGERON LKHEED1011 10113853 5265020WP FS 983 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND LONGERON AT FS 983 BETWEEN STRINGERS 45 AND 46 CRACKED. REPLACED LONGERON. 2L73 4F A23WE 19950303000711995030300071WP 1995 3 3 DLL16950800 119950224A5330 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP C-1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED IN FWD CARGO AREA, FS 886-901 AT STRINGER 23, 30, AND 34. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303000721995030300072WP 1995 3 3 DLL16950801 119950224A5320 STRAP LKHEED1011 10113853 5265020WP C-2 COMPT CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, C-2 STRAP COMMON TO STRINGER 33 IS CORRODED ON LEFT SIDE OF THE STRINGER, JUST AFT OF TEAR STRAP AT FS 1695. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950303000731995030300073WP 1995 3 3 DLL16950802 119950224A5330 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP C-1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND C-1 FUSEALGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 889-869 BETWEEN STRINGERS 37 AND 30. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950303000741995030300074WP 1995 3 3 DLL16950803 119950222A5313 STRINGER LKHEED1011 10113853 5265020WP FS 953 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 0 AT OVERHAUL STRINGER 32 AT LOWER SIDE OF SKIN ATTACH FLANGE (FS 953) WAS FOUND CORRODED. INSTALLED NEW SECTION OF STRINGER WITH SPLICE REPAIR PER SRM 53-13-00, FIG. 804. 2L73 4F A23WE 19950303000751995030300075WP 1995 3 3 DLL16950804 119950213A5330 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP FS 729-849 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 0 AT OVERHAUL FOUND C-1 BAG BIN FAIL SAFE STRAP DELAMINATED AT FS 729-849, STR 37 AND 34 (SAME CONDITION AT STR 31-32). REMOVED CORROSION AND FABRICATED NEW SPLICE PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303000761995030300076WP 1995 3 3 DLL16950805 119950224A5320 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP C-1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 0 AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DELAMINATED AT FS 709-729 ABOVE STRINGER 40. REPAIRED PER SRM 53-31-00, PG 830. 2L73 4F A23WE 19950303000771995030300077WP 1995 3 3 DLL16950806 119950213A5330 FAIL SAFE STRAP LKHEED1011 10113853 5265020WP C1 COMPT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 0 AT HMV, FOUND FUSELAGE SKIN FAILSAFE TEAR STRAP DELAMINATED AT FS 809-829 AT STRINGERS 27, 31, AND 23. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303000781995030300078NM 1995 3 3 DLM11950734 119950220A5754 CHAFE STRAP DOUG MD11 MD11 3023602NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11801DE 48472 DURING D-3 LETTER CHECK IN ATL, FOUND A .50 INCH CRACK PAST STOP DRILL ON OUTBOARD SIDE OF NR 2 SLAT AT TOP SIDE OF CHAFE STRIP. REPAIRED PER SRM 57-10-00 PG 30. 2L73 4F RTA22WE 19950303000791995030300079NM 1995 3 3 DLM88950777 119950222A5311 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11938DL 49811 TWO INCH CRACK ON LEFT W/W CUT-OUT ON GL OUTBOARD END LEFT WING. ITEM FOUND DURING F-1 LETTER CHECK. REPAIRED PER SRM 53-05-FIG 81A. 2L72 4F RTA6WE 19950303000801995030300080NM 1995 3 3 DLM88950781 119950213A5330 SKIN DOUG MD88 MD88 3023688NM FUS BELLEY DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 DURING HMV FOUND SKIN DENTED APPROX 12 INCHES LONG AT LOWER BELLY SKIN JUST BELOW C-1 DOOR CUT-OUT. REPAIRED PER ERA 270282-14. 2L72 4F RTA6WE 19950303000811995030300081NM 1995 3 3 DLM88950784 119950222A5230 HANDLE CUTOUT DOUG MD88 MD88 3023688NM C-1 DOOR WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 0 DURING HMV FOUND C-1 DOOR HANDLE CUT-OUT WORN AND BENT ALONG EDGE. REPAIRED PER SRM 52-05 FIG 30. 2L72 4F RTA6WE 19950303000821995030300082NE 1995 3 3 DLM88950790 219950217A7200JT8D219 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 BIRD STRIKE A DALAEA ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CLCLIMB 1 SO11901DL13329 49532 725552 ON TAKOFF, TOOK NUMEROUS BIRD STRIKES, NR 1 ENGINE WAS SHUT DOWN, RETURNED MSP. REPLACED ENGINE AND NOSE COWL FOR RETURN TO SERVICE. 2L72 4F4 FRTA6WE E9NE 19950303000831995030300083NM 1995 3 3 DLM88950792 119950221A56105912290505 WINDSHIELD DOUG MD88 MD88 3023688NM FLIGHT DECK CRACKED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11982DL 53273 DURING CRUISE, CAPTAIN'S L-1 WINDSHIELD OVERHEATED AND CRACKED. LANDED BOS. REPLACED WINDSHIELD AND CONTROLLER OPERATION NORMAL. 2L72 4F RTA6WE 19950303000841995030300084NM 1995 3 3 MWEA95136 119950223A25603952273501 GIRT BAR LATCH DOUG MD88 MD88 3023688NM AFT SERVICE DOORLACK OF LUBE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 F/A REPORTS AFT SERVICE DOOR GIRT BAR IS DIFFICULT TO INSTALL. MECHANIC LUBED GIRT BAR LATCHES, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950303000851995030300085NE 1995 3 3 MWEA95137 219950219A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE LEFT FAILED A AMWEAO OTHER JR WARNING INDICATION PARTIAL RPM/PWR LOSS CRCRUISE 1 GL31204ME414182304 47680 665799 PILOT REPORTS WITH CLIMB POWER THE EPR AND N1 ON LEFT ENGINE DROPPED SIGNIFICANTLY. ALL OTHER INDICATIONS ON LEFT ENGINE NORMAL AND EQUAL TO RIGHT ENGINE. ADVANCING LEFT THROTTLE CLIMB POWER ON EPR GAUGE INCREASED LT ENGINE EGT & N2 TO NEAR LIMITS. IN CRUISE AT 10,000 FEET, WITH EPR'S AND N1'S EVEN, LEFT THROTTLE WAS 1 KNOB AHEAD OF RIGHT AND LEFT EGT AND N2 AND FUEL FLOW WERE SIGNIFICANTLY HIGHER. LANDED WITHOUT INCIDENT. BORESCOPE INSPECTION REVEALED LT COMBUSTION CHAMBER EXIT DUCT SEAL HAD LIBERATED AFT OF NR 1 COMB CAN AND FWD OF TURBINE NOZZLE GUIDE VANE (2 SECTIONS). REPLACED ENGINE AND RETURNED A/C TO SERVICE. OPEN PENDING FURTHER INVESTIGATION. 2L72 4F4 F A6WE E2EA 19950303000861995030300086NM 1995 3 3 MWEA95138 119950223A25603552273502 GIRT BAR LATCH DOUG MD88 MD88 3023688NM AFT GALLEY DOOR LACK OF LUBE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 PILOT REPORTS AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR VERY HARD TO DISARM. MECHANIC CLEANED AND LUBED GIRT BAR LATCHES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 19950303000871995030300087WP 1995 3 3 MWEA95139 119950223A2560113313 EVAC SLIDE DOUG DC9 DC915 3022036WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER DEDESCENT 1 GL31300ME 45718 PILOT REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF DURING DESCENT. MECHANIC REINSTALLED GALLEY DOOR EVACUATION SLIDE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950303000881995030300088NM 1995 3 3 QXEA9500055 119950221A33503280034 EEL DORNERDO32 DO328100 2996000NM CABIN MALFUNCTIONED A QXEAK NONE L NO TEST APAPPROACH 1 NM09335PH 3013 SEA - EMERGENCY LIGHTING FLICKERED ON FINAL THEN WENT OFF AFTER LANDING. UNABLE TO DUPLICATE ON GROUND. FLIGHT CONTINUED TO PDX WHERE PROBLEM RECURRED. PDX MAINTENANCE REPLACED PANEL 15VE. GROUND TESTED AND A/C RELEASED FOR SERVICE. 2H72 4T RTA45NM 19950303000891995030300089EU 1995 3 3 QXEA9500056 119950222A33501012721 EEL ASSY FOKKERF28 F28MK1000 4990808EU CABIN MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 GEG - DURING MAINTENANCE FOUND EMERGENCY EVAL LIGHT ON SEAT 10 A/B INOP. RELAMPED FIXTURE, OPERATIONALLY TESTED. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950303000901995030300090EU 1995 3 3 QXEA9500057 119950223A33501312 EEL LAMP FOKKERF28 F28MK1000 4990808EU LT OVERWING FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 GEG - DURING MAINTENANCE FOUND LEFT OVERWING 3V EXIT LIGHT INOP. RELAMPED FIXTURE OPERATIONALLY TESTED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950303000911995030300091EU 1995 3 3 QXEA9500058 119950223A33501820 EEL LAMP FOKKERF28 F28MK1000 4990808EU RT OVERWING FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09803PH 11031 GEG - RIGHT OVERWING EMERGENCY EXIT FOUND INOP DURING MAINTENANCE. RE-BULBED FIXTURE, OPERATIONALLY TESTED. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950303000921995030300092NM 1995 3 3 UPS202428 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 308 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 20R, BS 308, WL 189. REPAIRED PER SRM 53-10-03, 51-30-02, MM 51-31-0, 51-20-21, 51-20-31. 2L73 4F A3WE 19950303000931995030300093NM 1995 3 3 UPS202429 119950222A5311 FRAME BOEING727 727173C 1384059NM BS 480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR AND A CRACK ON FRAME BS 480, STR 23-25R. REPAIRED PER SRM 51-40-03. 2L73 4F A3WE 19950303000941995030300094NM 1995 3 3 UPS202430 119950222A5311 FRAME BOEING727 727173C 1384059NM BS 520 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON FRAME BS 520, STR 20-24L. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950303000951995030300095NM 1995 3 3 UPS202431 119950222A5320 SILL BOEING727 727173C 1384059NM FWD ENTRY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON FWD ENTRY DOOR SILL BS 297-360, WL 208, LBL 57. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303000961995030300096NM 1995 3 3 UPS202432 119950222A5320 STIFFENERS BOEING727 727173C 1384059NM BS 312-344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON FWD ENTRY DOOR SILL LWR STIFFENERS AT NUT PLATE HOLES BS 312-344, WL 208, LBL 58 AND 61. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303000971995030300097NM 1995 3 3 UPS202433 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 304-440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 2R, BS 304-440, ON FLANGES AND SIDES. REPAIRED PER SRM 53-10-03, 51-30-02. 2L73 4F A3WE 19950303000981995030300098NM 1995 3 3 UPS202434 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 304-440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 3R, BS 304-328, 360-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04. 2L73 4F A3WE 19950303000991995030300099NM 1995 3 3 UPS202435 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 304-440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 5R, BS 304-328, 344-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04. 2L73 4F A3WE 19950303001001995030300100NM 1995 3 3 UPS202436 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 304-440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 4R, BS 304-328, 344-360, 360-400, AND 420-440 ON FLANGES AND SIDES. REPAIRED SRM 53-10-03, 51-30-02, 53-10-04. 2L73 4F A3WE 19950303001011995030300101NM 1995 3 3 UPS202437 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 721-736 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 25L, STA 721-736. REPAIRED PER SRM 53-10-03. 2L73 4F A3WE 19950303001021995030300102NM 1995 3 3 UPS202438 119950222A5311 FRAME BOEING727 727173C 1384059NM BS 572 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR AND CRACK ON FWD CARGO DOOR AFT A/C FRAME, BS 572, STR 25 AND 26R. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303001031995030300103NM 1995 3 3 UPS202439 119950222A5320 WEB BOEING727 727173C 1384059NM BS 785-805 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON WEB STA 785-805, RBL 62-70, WL 208. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303001041995030300104NM 1995 3 3 UPS202440 119950222A5320 TIE BOEING727 727173C 1384059NM BS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CRACK ON STRINGER 7R TIE, FWD SIDE OF BS 740. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303001051995030300105NM 1995 3 3 UPS202441 119950222A5754 CHORD BOEING727 727173C 1384059NM NR 6 SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON NR 6 SLAT LWR CHORD AT ROD END CUT OUT. REPAIRED PER SRM 57-50-02. 2L73 4F A3WE 19950303001061995030300106NM 1995 3 3 UPS202442 119950222A5511 RIB BOEING727 727173C 1384059NM LT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON LT HORIZ STAB UPPER CLOSURE RIB CHORD, I/B END. REPAIRED PER SRM 51-30-2. 2L73 4F A3WE 19950303001071995030300107NM 1995 3 3 UPS202443 119950222A5311 FRAME BOEING727 727173C 1384059NM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON FRAME BS 600, STR 17-28R. REPAIRED PER SRM 51-30-02. 2L73 4F A3WE 19950303001081995030300108NM 1995 3 3 UPS202444 119950222A5313 STRINGER BOEING727 727173C 1384059NM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 22R, BS 360, WL 140, RBL 45. REPAIRED PER SRM 53-10-03, MM 53-11-00. 2L73 4F A3WE 19950303001091995030300109NM 1995 3 3 UPS202472 119950222A5230 BEAM BOEING727 72725C 138400HNM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 4 TRANSVERSE BEAM IN O/B RADIUS. REPAIRED PER SRM 51-10-01, 51-30-02, AND MM 52-31-53. 2L73 4F A3WE 19950303001101995030300110NM 1995 3 3 UPS202473 119950222A5512 SKIN BOEING727 72725C 138400HNM RT HORIZ STAB TECORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR. ON RT HORIZONTAL STAB UPPER T/E IN BAY NR 5 NEAR O/B END. REPLACED PER SRM 51-30-2, 55-10-06. 2L73 4F A3WE 19950303001111995030300111NM 1995 3 3 UPS202474 119950222A5541 RIB BOEING727 72725C 138400HNM RUDDER WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND LOWER RUDDER, LOWER BULLNOSE CLOSURE RIB, WEB IS WORN THROUGH. REPLACED WEB PER SRM 55-10-01. 2L73 4F A3WE 19950303001121995030300112NM 1995 3 3 UPS202475 119950222A5531 SPAR BOEING727 72725C 138400HNM VERT FIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON LT VERT. FIN MID SPAR AT AFT ATTACH POINT FOR ACCESS PNL 9601 PANEL SUPPORT. REPAIRED PER UPS EO 727-55-0276. 2L73 4F A3WE 19950303001131995030300113NM 1995 3 3 UPS202476 119950222A5531 SPAR BOEING727 72725C 138400HNM VERT FIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON VERTICAL FIN, RT SIDE, MID SPAR CORRODED AND CHAFED AT AFT ATTACH POINT FOR ACCESS PNL 9602. INSTALLED REPAIR PER UPS EO 727-55-0277. 2L73 4F A3WE 19950303001141995030300114NM 1995 3 3 UPS202477 119950222A5753 FITTING BOEING727 72725C 138400HNM LT TE MID FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR. ON LT I/B MID FLAP I/B CARRIAGE FITTING BORE. REPLACED PER SRM 51-10-01. 2L73 4F A3WE 19950303001151995030300115NM 1995 3 3 UPS202478 119950222A5753 FITTING BOEING727 72725C 138400HNM RT TE MID FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR. ON RT I/B MID FLAP I/B CARRIAGE FITTING BORE. REPLACED PER SRM 51-10-01. 2L73 4F A3WE 19950303001161995030300116NM 1995 3 3 UPS202479 119950222A5753 SKIN BOEING727 72725C 138400HNM LT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND DELAMINATION ON LT I/B FORE FLAP 36 INCHES TO 54 INCHES FROM I/B END. REPLACED PER SRM 51-40-06, AND BOEING OHM 57-52-01. 2L73 4F A3WE 19950303001171995030300117NM 1995 3 3 UPS202483 119950222A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 219-227 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 219-227, RBL 240-243.5, WL 227. REPLACED PER MM 51-20-151, SRM 51-30-02, 51-10-02. 2L73 4F A3WE 19950303001181995030300118NM 1995 3 3 UPS202484 119950222A5313 STRINGER BOEING727 72725C 138400HNM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON STR 6L, STA 277-294, UPPER AND LWR FLANGE. REPLACED PER SRM 51-30-02, 51-10-02. 2L73 4F A3WE 19950303001191995030300119NM 1995 3 3 UPS202485 119950222A5320 G BEAM BOEING727 72725C 138400HNM BS 256 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON G-BEAM STA 256, LBL 13, RBL 25, WL 208. REPLACED PER SRM 51-30-02, 51-10-01. 2L73 4F A3WE 19950303001201995030300120NM 1995 3 3 UPS202486 119950222A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 259.5-277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON INTERCOSTAL STA 259.5-277, LBL 13-15, WL 208. REPLACED PER SRM 51-10-20, MM 51-20-151. 2L73 4F A3WE 19950303001211995030300121NM 1995 3 3 UPS202487 119950222A5311 FRAME BOEING727 72725C 138400HNM BS 294.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CRACK ON FRAME AT STA 294.5 WL 255 AT STR 10L. REPLACED PER SRM 51-10-01, 51-30-2. 2L73 4F A3WE 19950303001221995030300122NM 1995 3 3 UPS202488 119950222A5313 STRINGERS BOEING727 72725C 138400HNM BS 294.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CRACKS ON STRINGERS 14 AND 15 LEFT AT BS 294.5. REPAIRED PER UPS EO 8727-5310-1259-F. 2L73 4F A3WE 19950303001231995030300123NM 1995 3 3 UPS202489 119950222A5320 FORGING BOEING727 72725C 138400HNM BS 738 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND 3 EACH CRACKS EXTENDING FROM PREVIOUS STOP DRILLS ON 740 FORGING BS 738, BELOW STR 20L ON FORGING FOOT. NDI FOUND 4 CRACKS AND REPAIRED PER SRM 51-10-1. 2L73 4F A3WE 19950303001241995030300124NM 1995 3 3 UPS202490 119950222A5313 STRINGER BOEING727 72725C 138400HNM BS 680-700 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON STRINGER 9R, STA 680-700. REPAIRED PER SRM 51-30-2, 53-10-3. 2L73 4F A3WE 19950303001251995030300125NM 1995 3 3 UPS202491 119950222A5315 FLOOR BEAM BOEING727 72725C 138400HNM FS 500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR AROUND FLOOR BOARD HOLES IN FLOOR BEAM STA 500, RBL 10-45, WL 208. REPAIRED PER UPS ENGINEERING FILE 727-53-1490. 2L73 4F A3WE 19950303001261995030300126NM 1995 3 3 UPS202492 119950222A5347 SEAT TRACK BOEING727 72725C 138400HNM FS 414-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING "C" CHECK MAINTENANCE FOUND CORR ON SEAT TRACK FLANGE LBL 44, WL 208, STA 414-480, BOTTOM SIDE. REPAIRED PER SRM 51-30-2, 53-10-5, 51-10-2. 2L73 4F A3WE 19950303001271995030300127WP 1995 3 3 UPS802514 119950222A3260 SWITCH DOUG DC8 DC871F 302199DWP RT MLG MALFUNCTIONED A IPXAO OTHER N FALSE WARNING DEDESCENT 1 SO01715UP 45915 PILOT REPORTED RT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED, BOTH GEAR NOT LATCHED AND DOOR NOT LATCHED LIGHTS REMAINED ILLUMINATED, RECYCLED GEAR, ALL INDICATIONS NORMAL. REPLACED RT MAIN GEAR DOWNLOCK SWITCH - PERFORMED GEAR SWING, ALL INDICATIONS NORMAL. 2L74 4F RT4A25 19950303001281995030300128WP 1995 3 3 UPS802515 119950221A3230 LOCK ACT DOUG DC8 DC871F 302199DWP LT MLG MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION DEDESCENT 1 SO01919UP 45915 (SUPPLEMENTAL MRR) PILOT REPORTED WHEN LOWERED LANDING GEAR, NO LEFT MAIN GEAR CAME DOWN, CYCLED GEAR 3-4 TIMES, NO LEFT MAIN LANDING GEAR. ATTEMPT TO LOWER LT MAIN GEAR MANUALLY AND DID NOT WORK PROPERLY. TURNED HANDLE C/W 2-3 TURNS AND GOT DOOR LIGHT, WAIT 5 SECONDS AND TRIED TO CONTINUE TURN TO STOP, BUT HANDLE WOULD NOT MOVE. IT FELT BOUND. FINALLY, FORCED HANDLE UNTIL HEARD A CABLE BREAK. LEFT GEAR CAME DOWN AT THAT TIME. CHECK LEFT MANUAL EXTENSION FOR BROKEN CABLE OR SOMETHING. REPLACED LT MAIN GEAR LOCK ACTUATOR PER MM 32-30-00. REPLACED MLG CABLES PER 32-34-41. REPLACED MANUAL EXTENSION DRUM PER 32-34-71. 2L74 4F RT4A25 19950303001471995030300147CE 1995 3 3 95ZZZX914 119950207A3240 LINE CESSNA402 402B 207590PCE PARKING BRAKE CRACKED A OEZAK NONE O OTHER ININSP/MAINT 1 WP19971588856 402B0544 BRAKE LINE CRACKED WHERE IT FASTENED TO THE PARKING BRAKE VALVE. SUBMITTER SUGGESTS FATIGUE WAS THE CAUSE. 1L72 3O A7CE 19950303001521995030300152CE 1995 3 3 95ZZZX919 119950206A3240 LINE CESSNA207 T207A 2073614CE RT BRAKE HOLE CHAFED A OEZAK NONE K FLUID LOSS ININSP/MAINT 1 WP19101EN6261 20700666 LOSS OF BRAKE PRESSURE ON RT SIDE. FOUND HOLE WORN THROUGH BRAKE LINE UNDER LANDING GEAR FAIRING. SUSPECTED LINE WAS PUSHED DOWN BY PERSONNEL CAUSING CONTACT WITH SCREW THAT SECURES FAIRING. 1H71 3O A16CE 19950303001531995030300153CE 1995 3 3 95ZZZX920 119950210A324299103933 CALIPER PARKERHANFIN CESSNA402 402B 207590PCE BRAKE PINS WORN A OEZAK NONE O OTHER ININSP/MAINT 1 WP198049Q 402B0401 BRAKE WAS STICKING DURING APPLICATION. FOUND ANCHOR PINS WORN CAUSING BRAKE TO COCK AND BIND UP. SUBMITTER RECOMMENDS THESE PINS BE CLEANED, INSPECTED, AND LUBED EVERY 100 HOURS. 1L72 3O A7CE 19950303001731995030300173WP 1995 3 3 9503029914 119950221A2130 PRESSURIZATION DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01964N 47416 CABIN WOULD NOT PRESSURIZE IN EITHER AUTO OR MANUAL AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSPECTED ALL DOOR SEALS, OUTFLOW VALVE, AND PRESSURIZED AIRCRAFT WITH BOTH ENGINES RUNNING. ALL CHECKED OK WITH NO PROBLEMS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303001741995030300174WP 1995 3 3 9503039304 119950222A213121171801 PRESS CONTROL DOUG DC9 DC982 3022082WP E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01931MC1731578 48057 AIRCRAFT WOULD NOT PRESSURIZE WITH PRIMARY SYSTEM AFTER TAKEOFF. SWITCHED TO STANDBY AND SYSTEM WORKED NORMALLY. TRANSFER LOCKOUT AND STANDBY ON LIGHTS ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE PRIMARY CABIN PRESSURE CONTROLLER. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303001751995030300175WP 1995 3 3 9503049180 119950215A5270 SWITCH DOUG DC9 DC914 3022034WP CARGO DOOR DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL013312L 45707 DURING DTW-PIT TAKEOFF ROLL, FORWARD CARGO DOOR WARNING ILLUMINATED AT APPROXIMATELY 20 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. THE SWITCH WAS CLEANED AND THE DOOR CYCLED. CHECKED OK. 2L72 4F A6WE 19950303001761995030300176NM 1995 3 3 9503055527 119950224A212173176 COOLING FAN BOEING757 757251 1384970NM FWD E/E BAY FAILED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL01527US2505625056 23842 A STRONG ELECTRICAL BURNING SMELL WAS NOTICED IN THE COCKPIT. FOLLOWED COCKPIT OPERATING PROCEDURE AND SMELL WAS EVACUATED, SOURCE WAS UNKNOWN. FOUND THE FORWARD EQUIPMENT COOLING SUPPLY FAN CIRCUIT BREAKER POPPED, AND WAS UNABLE TO RESET. REPLACED FORWARD EQUIPMENT COOLING FAN. SYSTEM CHECKED NORMAL. 2L72 4F RTA2NM 19950303001771995030300177NM 1995 3 3 95FDEA00167 119950224A2720 TAB HINGES BOEING727 727227 1384078NM RUDDER BROKEN A FDEAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO04482FE 21464 A/C HAS A HEAVY YAW VIBRATION AND FLOOR VIBRATION ABOVE .72M AT FL 350. AT FL 280 VIBRATION STARTS AT .62M SPEEDBRAKES, CLIMB, DESCENTS AND TURNS HAVE NO EFFECT ON VIBRATION OR YAW. AIRCRAFT WAS FLOWN AT 62M AND FL280 FROM DAY-MEM. REMOVED LOWER TAB. FOUND BROKE TAB HINGES AND ATTACH HARDWARE WORN AND BROKEN. REPLACED LOWER TAB HINGES IAW MM 27-20-11. REPLACED LOWER TAB IAW MM 27-20-11 AND 27-20-00. OPS CHECK GOOD. 2L73 4F A3WE 19950303001781995030300178NM 1995 3 3 95UAL747008 119950213A5312 BLKHD CAP 65B018945 BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE BS 1350 CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29155UA 20104 LEVEL 2 CORROSION FOUND IN BS 1350 BULKHEAD LOWER CAP PLATE ASSY AND FITTINGS AT BOTH LBL AND RBL 127, WL 160. REPAIRED CAP PLATE ASSEMBLY AND REPLACED FITTINGS. 2L74 4F4 F A20WE E20EA 19950303001791995030300179NM 1995 3 3 95UAL747014 119950223A3350 EEL CABLE BOEING747 747451 1384940NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29106UA 26474 UPPER DECK EEL STRIP INOP. REPLACED INTERCONNECT CABLE. 2L74 4F4 FRTA20WE E24NE 19950303001801995030300180SO 1995 3 3 COM11793 119950219A5753PE610261 ROLLERS EMB 120 EMB120RT SO LT TE FLAP WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO011110J 120110 INBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF. REPLACED ROLLERS ON LT INBOARD FLAP. 2L72 4T RTA31SO 19950303001811995030300181NE 1995 3 3 COM11794 219950221A7320MS33201 CIRCUIT BREAKER EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT TRIPPED A COMAK NONE O OTHER UKUNKNOWN 1 SO011117H 120117 FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET CIRCUIT BREAKERS AND SYSTEM TEST NORMAL. 2L72 4T4 TRTA31SO E20NE 19950303001821995030300182SO 1995 3 3 COM11795 119950224A53301201923001 SKIN EMB 120 EMB120RT SO FS 6842.6 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01152CA13885 120152 DURING EXTERNAL INSPECTION LOWER FUSELAGE STA FS 6842.6 SHOWED SIGNS OF CORROSION. FURTHER INSPECTION, REVEALED FUSELAGE SKIN (P/N 120-19230-001), TO HAVE CORROSION BETWEEN SKIN AND TITANIUM STRAP (P/N 120-22409-001). AIRCRAFT WAS REPAIRED IN ACCORDANCE WITH EMBRAER REPAIR EST-061/95 AND AERODESIGN AIRCRAFT ENGINEERING REPORT 1437-1. 2L72 4T RTA31SO 19950303001831995030300183SO 1995 3 3 COM11796 119950217A533012019230001 SKIN EMB 120 EMB120RT SO FS 6842.6 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO011117H15241 120117 DURING MAINTENANCE SERVICE CHECK, RIVETS WERE FOUND TO HAVE BROKEN OR MISSING HEADS AT LOWER FUSELAGE CENTER LINE, FRAME 21 STA FS 6842.6. FURTHER INSPECTION REVEALED FUSELAGE SKIN (P/N 120-92030-001), TO HAVE CORROSION BETWEEN SKIN AND TITANIUM REINFORCING STRAP (P/N 120-22409-001). AIRCRAFT WAS REPAIRED IN ACCORDANCE WITH EMB REPAIR EST-061/95 AND AERODESIGN AIRCRAFT ENGINEERING REPORT 1437-7. CORROSION AREA APPROX 1.0 INCH BY 1.5 INCH, 30 PERCENT OF THICKNESS. 2L72 4T RTA31SO 19950303001841995030300184SO 1995 3 3 COM11797 119950226A532012010087001 DOUBLER EMB 120 EMB120RT SO FS 4214.0 CORRODED A COMAK NONE O OTHER UKUNKNOWN 1 SO011110J15606 120110 DURING INSPECTION OF UNDER FLOOR LAVATORY AREA, THE DOUBLER FOR THE OAT SENSOR WAS FOUND TO HAVE CORROSION. THE DOUBLER WAS REPLACED BY A FABRICATED DOUBLER AND INSTALLED IN ACCORDANCE WITH AERODESIGN AIRCRAFT ENGINEERING REPORT 1452-1. 2L72 4T RTA31SO 19950303001851995030300185SO 1995 3 3 COM11798 119950223A553012015374002 ANGLE EMB 120 EMB120RT SO VERT STAB CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01255CA9514 120238 DURING INSPECTION TASK 5530-324-03I AND 5530-324-02I, VERTICAL STABILIZER TO FUSELAGE ANGLE WAS FOUND TO BE CRACKED. REPLACED ANGLE IAW AERODESIGN REPORT 1446-1 AND EMB SRM. 2L72 4T RTA31SO 19950303001861995030300186SO 1995 3 3 COM11799 119950223A524612016900008 FUEL DOOR EMB 120 EMB120RT SO RT WING NOT SECURE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01268CA 120262 SERVICE DOOR WARNING ACTIVATED DURING TAKEOFF. SECURED FUEL SERVICE DOOR AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950303001871995030300187SO 1995 3 3 COM11800 119950219A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01267CA7540 7540 120259 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-O1I AT WING RIBS 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT 1327-2, 120-17056-019 (2 EA), 120-17056-017 (2 EA), 120-17056-015 (4 EA), 120-17056-013, 120-17057-006, 120-17057-005, 120-17057-007, 120-17056-011. 2L72 4T RTA31SO 19950303001881995030300188EA 1995 3 3 COM60427 119950226A2760 SPOILER IND CNDAIRCL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO01917CA 7017 FLIGHT SPOILERS AND GROUND SPOILERS FAULT MESSAGE ON EICAS. MAINTENANCE COULD NOT DUPLICATE. SYSTEM TEST NORMAL, NO FAULT CODES. 2L72 4F RTA21EA 19950303001891995030300189EA 1995 3 3 COM60428 119950223A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 1 DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01918CA913 201 7018 SPOILERON AND FLIGHT SPOILER FAULT MESSAGE ON EICAS. REPLACED THE NR 1 SECU. 2L72 4F RTA21EA 19950303001901995030300190EA 1995 3 3 COM60429 119950223A5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA RT COCKPIT CRACKED A COMAK NONE O OTHER UKUNKNOWN 1 SO01926CA3233 7027 CO-PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 19950303001911995030300191NM 1995 3 3 DL72K950823 119950224A5320 WEB BOEING727 727232 1384082NM FS 1233 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11413DA 21233 1 INCH CRACK AT LIGHTNING HOLE CUTOUT FLANGE STA 1233L. CRACK WAS FOUND DURING A-2 LETTER CK. INSTALLED DOUBLER PER MM 53-11-0 PG 828. 2L73 4F A3WE 19950303001921995030300192NM 1995 3 3 DL72K950824 119950224A5330 SKIN BOEING727 727232 1384082NM PAX DR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11413DA 21233 MAIN ENTRY DOOR LWR HINGE CUTOUT AT FUSELAGE SKIN CRACKED 1.5 INCH. CRACK WAS FOUND DURING A-2 LETTER CHECK. REPAIRED PER MM 53-30-0 PG 821. 2L73 4F A3WE 19950303001931995030300193NM 1995 3 3 DL72K950826 119950224A5320 ANGLE BOEING727 727232 1384082NM NR 2 ENG CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11413DA 21233 DURING A-2 LETTER CHECK, FOUND ANGLE DAMAGED AT FWD LWR NR 2 ENG CUTOUT. REPAIRED PER MM 53-11-0 PG 801. 2L73 4F A3WE 19950303001941995030300194NM 1995 3 3 DL72P950842 119950224A3350900542 EEL RACK BOEING727 727225 1384077NM CABIN FAULTY A DALAK NONE L NO TEST ININSP/MAINT 1 SO118889Z 21858 DURING INSPECTION, ALL 3 RT WING EMERGENCY LIGHTS, AND CENTER CABIN OVERWING EMERGENCY EXIT LIGHT WERE INOP. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A3WE 19950303001951995030300195NM 1995 3 3 DL72S950813 119950216A532069678811 ANGLE BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4. 2L73 4F A3WE 19950303001961995030300196NM 1995 3 3 DL72S950814 119950211A5320651751737 STIFFENER BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 DURING INSPECTION, THE RT UPPER TORQUE BOX WAS FOUND TO HAVE CRACKED STIFFENERS LOCATED AT F61273. THE STIFFENERS WILL BE REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4. 2L73 4F A3WE 19950303001971995030300197NM 1995 3 3 DL72S950815 119950209A5320651751738 BEAM BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING INSPECTION, THE FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED IN THE ANGLE. THE BEAM WILL BE REPLACED IN ACCORDANCE WITH B727 S 53-0129 REV 4. 2L73 4F A3WE 19950303001981995030300198NM 1995 3 3 DL72S950816 119950208A5313 STRINGER BOEING727 727232 1384082NM FS 520 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND CORROSION AT STR 23R JUST FWD OF STA 520. REPAIRED PER SRM 53-10-3 ID PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950303001991995030300199NM 1995 3 3 DL72S950817 119950202A5754 RIB BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9. 2L73 4F A3WE 19950303002001995030300200NM 1995 3 3 DL72S950818 119950206A5720 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813. 2L73 4F A3WE 19950303002011995030300201NM 1995 3 3 DL72S950819 119950206A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813. 2L73 4F A3WE 19950303002021995030300202NM 1995 3 3 DL72S950821 119950206A5720 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER. 2L73 4F A3WE 19950303002031995030300203NM 1995 3 3 DL72S950822 119950215A5330 SKIN BOEING727 727232 1384082NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING CV-2 CK, FOUND FUSELAGE SKIN DAMAGED BETWEEN STA 720E AND 720F AT STR 27L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950303002041995030300204NM 1995 3 3 DL72S950827 119950131A57536521630187 SKIN BOEING727 727232 1384082NM NR 2 FORE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, NR 2 FORE FLAP WAS FOUND WITH TOP SKIN DELAMINATED AT 44 INCHES FROM THE I/B END. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-06. 2L73 4F A3WE 19950303002051995030300205NM 1995 3 3 DL72W950812 119950214A532069678811 ANGLE BOEING727 727247 138408FNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112816W 20872 DURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WILL BE REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4. 2L73 4F A3WE 19950303002061995030300206NM 1995 3 3 DL733950783 119950215A57536546486129 WEDGE BOEING737 737347 1384647NM TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 AT HMV, FOUND FLAP TRAILING EDGE WEDGE DELAMINATED AT ITS OUTBOARD END. REPAIRED PER SRM 57-53-02. 2L72 4F RTA16WE 19950303002071995030300207NM 1995 3 3 DL733950825 119950220A5320 FLOOR SUPPORT BOEING737 737347 1384647NM FS 727 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 AT HMV, FOUND AFT B/B FLOOR SUPPORT CRACKED AT TIE DOWN FITTING STA 727B LT AND 727D RT. REPAIRED PER SRM 53-00-53 FIG 202. 2L72 4F RTA16WE 19950303002081995030300208NM 1995 3 3 DL76S950828 119950223A5413314T1210431 LONGERON BOEING767 767332 1382001NM NR 1 NACELLE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11134DL 25123 000247 DURING SHOP INSPECTION, NR 1 ENGINE CORE COWL LOWER LONGERON WAS FOUND WORN AT THE AFT HINGE FITTING. REPAIRED PER SRM 54-41-02 FIG 207. 2L72 4F RTA1NM 19950303002091995030300209WP 1995 3 3 DLL10950829 119950103A57551529102177 SPAR LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11716DA 193C1095 000247 NDT INSPECTION, REVEALED A CRACK ON SPAR BEHIND NR 2 ATTACH FITTING. DURING INITIAL SHOP INSPECTION UPPER AND LOWER SKIN WERE FOUND TO BE DELAMINATED. THIS L-1011 NR 2 LT SPOILER WAS RECONDITION PER CMM 1529102 WITH REF TO SRM 57-52-00. 2L73 4F A23WE 19950303002101995030300210WP 1995 3 3 DLL16950807 119950213A5330 TEARSRTAP LKHEED1011 10113853 5265020WP FS 1585-1605 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING OVERHAUL, FOUND TEARSTRAP DISBONDED AT STA 1585-1605 BETWEEN STR 29-31. REPAIRED SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950303002111995030300211WP 1995 3 3 DLL16950808 119950214A5315 FLOORBEAM LKHEED1011 10113853 5265020WP BS 1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING OVERHAUL, FOUND FLOORBEAM CORRODED AT STA 1725, LBL 34-58. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950303002121995030300212WP 1995 3 3 DLL16950809 119950213A5330 TEARSTRIP LKHEED1011 10113853 5265020WP FS 1605/809 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1605-1625 STR 32-33, FS 1605-1625 STR 33-34, FS 809-829 STR 31. 2L73 4F A23WE 19950303002131995030300213WP 1995 3 3 DLL16950810 119950214A5330 TEARSTRIP LKHEED1011 10113853 5265020WP FS 1695/1635 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1695 STR 30-29, FS 1635 STR 38-39, FS 1635 STR 40-41. 2L73 4F A23WE 19950303002141995030300214WP 1995 3 3 DLL16950811 119950214A5330 TEARSTRIP LKHEED1011 10113853 5265020WP FS 1735 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING OVERHAUL, FOUND TEARSTRIP DISBONDED AT FS 1735 STR 29-31. REPAIR PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950303002151995030300215WP 1995 3 3 DLL16950831 119950221A5347 SEAT TRACK LKHEED1011 10113853 5265020WP FS 1665-1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING HMV, FOUND CABIN SEAT ATTACH TRACK CORRODED AT FS 1665 TO 1725 AT RBL 42. REPLACED TRACK PER SRM 53-21-00 FIG 820. 2L73 4F A23WE 19950303002161995030300216WP 1995 3 3 DLL16950832 119950212A5330 FAILSAFE STRAP LKHEED1011 10113853 5265020WP FS 639/689 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 639 AND 689 BETWEEN STRINGERS 29, 30 AND 31 TO 35. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303002171995030300217WP 1995 3 3 DLL16950833 119950213A5330 FAILSAFE STRAP LKHEED1011 10113853 5265020WP FS 1545-1565 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1545 TO FS 565 BETWEEN STRINGERS 30 TO 37. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303002181995030300218WP 1995 3 3 DLL16950834 119950213A5330 FAILSAFE STRAP LKHEED1011 10113853 5265020WP FS 1443/1535 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND FUSELAGE SKIN FAILSAFE TEARSTRAP DISBONDED AT FS 1443 BETWEEN STRINGESR 30 AND 31, AND FS 1535 BETWEEN STRINGERS 33-34. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950303002191995030300219WP 1995 3 3 DLL16950835 119950214A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 281 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND CABIN FLOOR SUPPORT BEAM AT FS 281 WITH CORROSION DAMAGE AT LBL 74 TO RBL 74. REPAIRED PER SRM 53-21-00 PG 823-824. 2L73 4F A23WE 19950303002201995030300220WP 1995 3 3 DLL16950836 119950214A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 901/923 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND CABIN FLOORBEAM AT FS 923 CORRODED AT LBL 31. REPAIRED PER SRM 53-21-00 PG 866-868,_AND FLOORBEAM AT FS 901 CORRODED AT LBL 42 AND 47. REPAIRED PER SRM 53-21-00 PG 849-852. 2L73 4F A23WE 19950303002211995030300221WP 1995 3 3 DLL16950837 119950221A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 886 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND CORROSION ON CABIN FLOORBEAM FS 886 RBL 30. REPAIRED PER SRM 53-21-00 PG 866-868. 2L73 4F A23WE 19950303002221995030300222WP 1995 3 3 DLL16950838 119950221A5330 SKIN LKHEED1011 10113853 5265020WP FS 629-649 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND LOWER FUSELAGE SKIN CORRODED AT FS 629-649 BETWEEN STRINGER 32 AND 34. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 FIG 825. 2L73 4F A23WE 19950303002231995030300223WP 1995 3 3 DLL16950839 119950213A5400 ANGLE LKHEED1011 10113853 5265020WP NR 2 NACELLE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS 2 INCHES. CRACK LOCATED INSIDE ACCESS PANEL 311UR, AT NR 2 ENGINE INTAKE. REPAIRED PER SRM 54-12-00 PG 808. 2L73 4F A23WE 19950303002241995030300224WP 1995 3 3 DLL16950840 119950213A5400 ANGLE LKHEED1011 10113853 5265020WP NR 2 NACELLE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 000247 DURING HMV, FOUND STIFFENER ANGLE CRACKED FROM EDGE TO RADIUS, APPROX 2 INCHES INSIDE ACCESS PANEL 311UL OF NR 2 ENGINE INTAKE (LEFT SIDE OF S DUCT LOOKING UP AND AFT). REPAIRED PER SRM 54-12-00 FIG 803. 2L73 4F A23WE 19950303002251995030300225NM 1995 3 3 DLM88950843 119950224A21505910244125 DUCT DOUG MD88 MD88 3023688NM RT PACK CRACKED A DALAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11924DL 49711 DURING CLIMBOUT, HAD TAIL COMPARTMENT OVERHEAT. ISOLATED PROBLEM TO RIGHT PACK, SHUT PACK DOWN, LIGHT OUT, AND CONTINUED FLIGHT. FOUND CRACKED DUCT AT RIGHT PACK. REPLACED DUCT OPERATION NORMAL. 2L72 4F RTA6WE 19950303002261995030300226NM 1995 3 3 UPS202248 119950225A5530 CHORD BOEING727 72725C 138400HNM VERT FIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 DURING C-CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN TORQUE BOX RT HORIZONTAL CHORD, RBL 19 FIN STA 0. INSTALLED REPAIR PER UPS ENGINEERING FILE NR 727-55-0273. 2L73 4F A3WE 19950303002271995030300227NM 1995 3 3 UPS202493 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 682 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 26L BS 682, LBL 23. INSTALLED REPAIR PER SRM 53-10-01, 53-10-2. 2L73 4F A3WE 19950303002281995030300228NM 1995 3 3 UPS202494 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 673 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 19R, BS 673, ON STRINGER SPLICE. INSTALLED REPAIR PER SRM 53-10-01, 53-10-2, 51-10-06, 51-01-02, 51-30-02, 53-10-03, MM 51-20-151. 2L73 4F A3WE 19950303002291995030300229NM 1995 3 3 UPS202495 119950224A5320 STIFFENER BOEING727 72725C 138400HNM BS 747 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BREATHER WEB AND STIFFENER ABOVE DELTA BEAM BL 0, WL165, BS 747. INSTALLED REPAIR PER SRM 51-40-02, 51-30-02, MM 20-10-05. 2L73 4F A3WE 19950303002301995030300230NM 1995 3 3 UPS202496 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 670-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3L, STA 670-740. INSTALLED REPAIR PER SRM 53-10-03, 51-30-02. 2L73 4F A3WE 19950303002311995030300231NM 1995 3 3 UPS202497 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 996-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6L, STA 996-1130. INSTALLED REPAIR PER SRM 53-10-03, 53-10-01, 51-10-02, 51-20-151, 53-10-04. 2L73 4F A3WE 19950303002321995030300232NM 1995 3 3 UPS202498 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 970-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3L, STA 970-1130. INSTALLED REPAIR PER SRM 51-10-06, 51-30-02, 51-10-02, 51-40-05, 53-10-01, 53-10-04. 2L73 4F A3WE 19950303002331995030300233NM 1995 3 3 UPS202499 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 970-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2R, STA 500-520, 580-740. INSTALLED REPAIR PER SRM 51-10-06, 51-30-02, 51-10-02, 51-40-05, 53-10-01, 53-10-04, AND MM 51-20-151. 2L73 4F A3WE 19950303002341995030300234NM 1995 3 3 UPS202500 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 921 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM BOTTOM CHORD AFT SIDE STA 921, WL 201. INSTALLED REPAIR PER UPS EO B727-5310-6692. 2L73 4F A3WE 19950303002351995030300235NM 1995 3 3 UPS202501 119950224A5320 EXPANSION LINK BOEING727 72725C 138400HNM BS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AROUND BUSHINGS AT STA 860, LBL 25, WL 207. INSTALLED REPAIR PER SRM 51-10-01, 51-10-02, MM 51-20-151. 2L73 4F A3WE 19950303002361995030300236NM 1995 3 3 UPS202502 119950224A5320 EXPANSION LINK BOEING727 72725C 138400HNM BS 750 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK UNDER NUTPLATES AT STA 750, BL 0, WL 207.5. INSTALLED REPAIR PER SRM 51-30-02, 53-10-01. 2L73 4F A3WE 19950303002371995030300237NM 1995 3 3 UPS202503 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES IN FLOORBEAM STA 328, LBL 23 AND 48, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6666A. 2L73 4F A3WE 19950303002381995030300238NM 1995 3 3 UPS202504 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES IN FLOORBEAM STA 312, LBL 2, 18, AND 43, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6693A. 2L73 4F A3WE 19950303002391995030300239NM 1995 3 3 UPS202505 119950224A5320 HAT CHANNEL BOEING727 72725C 138400HNM BS 304-344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON END OF HAT CHANNEL STA 304-344, RBL 13, WL 208. INSTALLED REPAIR PER SRM 51-30-02, 51-01-02, 51-10-06, 51-20-01, MM 51-20-31. 2L73 4F A3WE 19950303002401995030300240NM 1995 3 3 UPS202506 119950224A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 314 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON AFT FLANGE OF INTERCOSTAL STA 314, RBL 17 TO 40, WL 208. INSTALLED REPAIR PER SRM 51-10-01, 51-10-02, 51-30-01, MM 51-20-151. 2L73 4F A3WE 19950303002411995030300241NM 1995 3 3 UPS202507 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION AROUND FLOOR BOARD HOLES IN FLOORBEAM STA 560, RBL 45-65, LBL 0-25, LBL 57-63, ON BOTTOM SIDE OF TOP CHORD. INSTALLED REPAIR PER SRM 53-10-08. 2L73 4F A3WE 19950303002421995030300242NM 1995 3 3 UPS202508 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 485 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK SPLICE, STA 485, LBL 44, WL 208. INSTALLED REPAIR PER SRM 51-30-02, 51-10-02. 2L73 4F A3WE 19950303002431995030300243NM 1995 3 3 UPS202509 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 990 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK COUNTER SINKS, STA 990, LBL 45, WL 208. INSTALLED REPAIR PER SRM 51-30-08, 51-10-02, 53-10-05. 2L73 4F A3WE 19950303002441995030300244NM 1995 3 3 UPS202510 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 953-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGES STA 953 TO 1130 RBL 61, WL 208. INSTALLED REPAIR PER SRM 53-10-01, 53-10-05, 51-30-02, 51-10-02, MM 51-20-151. 2L73 4F A3WE 19950303002451995030300245NM 1995 3 3 UPS202511 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 620-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 620 TO 740 RBL 25, WL 208. INSTALLED REPAIR PER SRM 53-10-05, 51-30-02. 2L73 4F A3WE 19950303002461995030300246NM 1995 3 3 UPS202512 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 620-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT STA 299 LBL 0 TO 12, WL 208. INSTALLED REPAIR PER SRM 51-30-02. 2L73 4F A3WE 19950303002471995030300247NM 1995 3 3 UPS202513 119950224A5320 WINDOW POST BOEING727 72725C 138400HNM FLIGHT DECK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK UNDER REPAIR IN E TO F WINDOW POST. THE RIGHT SIDE, IS NOT CONTAINED BY STOP DRILL OR RIVET HOLE. CRACK IS BETWEEN THE 1ST AND 2ND SCREW FROM THE BOTTOM OF THE NR 3 WINDOW. REPAIRED PER UPS EO B727-5310-0012. 2L73 4F A3WE 19950303002481995030300248NM 1995 3 3 UPS202521 119950224A5313 STRINGER BOEING727 72725C 138400HNM BS 743 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON STRINGER 17R BS 743, RBL 70.5. INSTALLED REPAIR PER SRM 51-40-04. 2L73 4F A3WE 19950303002491995030300249NM 1995 3 3 UPS202522 119950224A5311 FRAME BOEING727 72725C 138400HNM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FRAME IN BOLT HOLES BETWEEN STRINGERS 21L AND 21R, BS 360. INSTALLED REPAIR PER UPS EO B727-5310-6725. 2L73 4F A3WE 19950303002501995030300250NM 1995 3 3 UPS202523 119950224A5320 SHEAR TIE BOEING727 72725C 138400HNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE AND FAIL-SAFE STRAP BS 680, STR 19R. INSTALLED REPAIR PER SRM 51-10-02, 51-30-05, 51-20-04. 2L73 4F A3WE 19950303002511995030300251NM 1995 3 3 UPS202524 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 1030 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1030 RBL 0-65 LBL 0-65, WL 208. INSTALLED REPAIR PER UPS EO B272-5310-6711. 2L73 4F A3WE 19950303002521995030300252NM 1995 3 3 UPS202525 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1110 RBL 0-65 LBL 0-65, WL 208. INSTALLED REPAIR PER UPS EO B272-5310-6728. 2L73 4F A3WE 19950303002531995030300253NM 1995 3 3 UPS202526 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 1090 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AROUND NUTPLATES AT STA 1090 LBL 45-65 WL 208. INSTALLED REPAIR PER UPS ENGINEERING FILE NR B727-53-1484. 2L73 4F A3WE 19950303002541995030300254NM 1995 3 3 UPS202527 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 680 LBL 38-51 RBL 45-65, WL 208. INSTALLED REPAIR PER SRM 53-10-08. 2L73 4F A3WE 19950303002551995030300255NM 1995 3 3 UPS202528 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 640 RBL 60-63 LBL 45 RBL 25, LBL 48 ON BOTTOM OF UPPER CHORD. INSTALLED REPAIR PER UPS EO B727-5310-6712A. 2L73 4F A3WE 19950303002561995030300256NM 1995 3 3 UPS202529 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 540 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 540 RBL 10 LBL 7, WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6726A. 2L73 4F A3WE 19950303002571995030300257NM 1995 3 3 UPS202530 119950224A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES AT STA 600 RBL 45-65 LBL 10-56 WL 208. INSTALLED REPAIR PER UPS EO B727-5310-6714A. 2L73 4F A3WE 19950303002581995030300258NM 1995 3 3 UPS202531 119950224A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGES STA 740, AND BARE ALUMINUM ON FLANGES STA 420-480 AND 500-540 LBL 25 WL 208. INSTALLED REPAIR PER SRM 53-10-01. 2L73 4F A3WE 19950303002591995030300259NM 1995 3 3 UPS202532 119950224A5730 SKIN BOEING727 72725C 138400HNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7606 RIGHT WING. INSTALLED REPAIR PER SRM 57-30-03, AND UPS ENGINEERING FILE NR 727-57-1091. 2L73 4F A3WE 19950303002601995030300260NM 1995 3 3 UPS202533 119950224A5730 SKIN BOEING727 72725C 138400HNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7607 RIGHT WING. INSTALLED REPAIR PER SRM 57-30-03. 2L73 4F A3WE 19950303002611995030300261NM 1995 3 3 UPS202534 119950224A5730 SKIN BOEING727 72725C 138400HNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT 7608 RIGHT WING. INSTALLED REPAIR PER UPS ENGINEERING FILE 727-57-1091. 2L73 4F A3WE 19950303002621995030300262NM 1995 3 3 UPS202535 119950224A5210 GATE BEAM BOEING727 72725C 138400HNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 DURING D-CHECK, MAINTENANCE FOUND CRACK ON FWD ENTRY DOOR LWR GATE BEAM CRACKED LWR FWD CORNER IN RADIUS. INSTALLED REPAIR PER SRM 51-10-01, 51-30-02. 2L73 4F A3WE 19950303002631995030300263NM 1995 3 3 UPS502516 119950223A2612 FIRE CARD BOEING757 75724APF 1384969NM AFT EQUIP BAY MALFUNCTIONED A IPXAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SO01440UP 25471 PILOT REPORTED, THAT ON LANDING AT RSW AN AFT FIRE EICAS MESSAGE APPEARED ALONG WITH A FIRE BELL AND MASTER CAUTION WARNING, AN AFT EQUIPMENT OVERHEAT MESSAGE. ALL 3 FIRE BOTTLES WERE FIRED. REPLACED FIRE BOTTLES, A FOLTS CARD AND SMOKE DETECTORS AS PRECAUTIONARY. NO TROUBLE FOUND. 2L72 4F RTA2NM 19950303002641995030300264NM 1995 3 3 UPS502520 119950223A5754114N4004145 WEDGE BOEING757 75724APF 1384969NM NR 3 LE SLAT DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01406UP 23728 DURING C-CHECK, MAINTENANCE FOUND NR 3 SLAT T/E WEDGE IS DELAMINATED AND EXCEEDS ALLOWABLE LIMITS. REPLACED SLAT PER MM 27-81-02. 2L72 4F RTA2NM 19950303002651995030300265WP 1995 3 3 UPS802517 119950222A5312 BEAM DOUG DC8 DC873F 302199FWP AFT BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 DURING B-CHECK, MAINTENANCE FOUND NR 3 AND 4 'J' BEAM CRACKED AT AFT BULKHEAD. REPAIRED PER UPS EO DC8-5310-6715A. 2L74 4F RT4A25 19950303002661995030300266WP 1995 3 3 UPS802518 119950223A5312 BEAM DOUG DC8 DC871F 302199DWP AFT BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 (SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD TOP SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A. 2L74 4F RT4A25 19950303002671995030300267WP 1995 3 3 UPS802519 119950223A5312 BEAM DOUG DC8 DC871F 302199DWP AFT BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 (SUPPLEMENTAL MRR) DURING 'B' CHECK, MAINTENANCE FOUND AFT BULKHEAD BOTTOM SIDE OF J4 BEAM CRACKED. STOP DRILLED CRACK, FABRICATED DOUBLER AND CLIPS AND INSTALLED PER UPS EO DC8-5310-6735-A. 2L74 4F RT4A25 19950303002681995030300268CE 1995 3 3 95ZZZX922 119950126A27501013800006 CONTROL CABLE BEECH 1900 1900C 1154161CE RT TE FLAPS BINDING A AHERAO OTHER F FLT CONT AFFECTED DEDESCENT 1 AL035632C UC81 KSM - FLT 5691 - ON DESCENT, THE WING FLAPS BECAME STUCK IN THE APPROACH POSITION. A LANDING WAS MADE WITHOUT INCIDENCE. THE AIRCRAFT WAS THEN REPOSITIONED TO ANC ON A SPECIAL FLIGHT PERMIT. AFTER TROUBLESHOOTING THE WING FLAP SYSTEM, MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD AND THE RIGHT OUTBOARD FLAP DRIVE CABLES. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL NR HERA9504. 2L72 4T RTA24CE 19950303002691995030300269CE 1995 3 3 95ZZZX923 119950131A27501185210552 SWITCH BEECH 1900 1900C 1154161CE RT TE FLAPS DIRTY A AHERAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 AL0380346 UC94 ANC - FLT 1481 - AIR RETURN DUE WING FLAPS WOULD NOT RETRACT PAST THE TAKEOFF POSITION AFTER TAKEOFF. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED AND LUBED THE LEFT AND RIGHT FLAP SAFETY SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE FLAP SYSTEM WORKING NORMALLY, THE AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE CONTROL NR HERA9505. 2L72 4T RTA24CE 19950303002701995030300270CE 1995 3 3 95ZZZX924 119950117A27501185210552 SWITCH BEECH 1900 1900C 1154161CE RT TE FLAPS DIRTY A AHERAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 AL0355456 UC165 ANC - FLT 1495 - AIR RETURN DUE WING FLAPS STUCK IN THE TAKEOFF POSITION AFTER DEPARTURE. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED THE LEFT AND RIGHT FLAP SAFETY SWITCHES AND CHECKED THE RIGGING OF THE SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE FLAP SYSTEM WORKING NORMALLY, THE AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE CONTROL NR HERA9501. 2L72 4T RTA24CE 19950303002721995030300272EU 1995 3 3 AALA950253 119950210A3200 LEVELING BAR FOKKERF28 F28MK0100 4990807EU NLG STILL ATTACHED A AAALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW071403M 11354 DFW - FLT 1412 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, EXPERIENCED LOUD THUMP IN NOSE LANDING GEAR AREA AND NOSE GEAR CAUTION LIGHT ILLUMINATED. RECYCLED LANDING GEAR AND CAUTION LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REMOVED LEVELING BAR FOUND STILL ATTACHED TO NOSE LANDING GEAR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. AIRCRAFT MAINTENANCE FERRY DFW/TUL. INSTALLED DOUBLER ON NOSE LANDING GEAR FORWARD BULKHEAD AT UPPER RT CORNER. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RT 19950303002731995030300273NM 1995 3 3 CAL950101 119950208A243223013 BATTERY CHARGER BOEING737 737130 1384435NM E/E BAY INOPERATIVE A CALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW09442141848915963 19031 TPA - FLT 1790 - THE FLIGHT ATTENDANT REPORTED A SMOKY ODOR IN CABIN DURING CLIMB-OUT. THE BATTERY CHARGER CIRCUIT BREAKER WAS PULLED AND THE ODOR SUBSIDED. THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE BATTERY CHARGER AT FAULT AND THE BATTERY WAS HOT. BOTH THE CHARGER AND BATTERY WERE REMOVED AND REPLACED. ALL CIRCUIT BREAKERS WERE RESET AND THE SYSTEM TESTED GOOD PER MM 24-31-21, PAGE 501. (X) 2L72 4F A16WE 19950303002741995030300274NM 1995 3 3 CAL950104 119950208A3350 EEL WIRING BOEING727 727224 1384076NM CABIN CUT A CALAK NONE L NO TEST ININSP/MAINT 1 SW0979749 22451 EWR - FLT 0397 - EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE IN FIRST CLASS SECTION OF CABIN DURING A PRE-FLIGHT CHECK. MAINTENANCE FOUND WIRING TO BATTERY PACK CUT UNDER LT FIRST CLASS SEATS AND 3 BLOWN FUSES. THE WIRING WAS REPAIRED AND THE THREE FUSES WERE REPLACED. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN WAS RESTORED. (X) 2L73 4F A3WE 19950303002751995030300275WP 1995 3 3 CAL950105 119950207A7603 LINKAGE DOUG DC10 DC1030 3023501WP NR 2 ENGINE BINDING A ACALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW0987070 48292 EWR - FLT 0063 - TAKEOFF WAS ABORTED AT 110 KNOTS WHEN THE NR 2 ENGINE THROTTLE WOULD NOT MOVE PAST THE 25 DEGREE ANGLE POSITION. MAINTENANCE FOUND THE NR 2 ENGINE THROTTLE BINDING. THE POWER LEVER LINKAGE WAS MISALIGNED AT THE QUADRANT CONNECTION AND AN ADDITIONAL LINKAGE WAS FOUND OBSTRUCTED BY DEBRIS. THE DEBRIS WAS REMOVED. THE NR 2 ENGINE WAS RUN TO 90 PERCENT N1 WITH NO BINDING NOTED. IN ADDITION, THE NR 2 ENGINE THROTTLE TELEFLEX CABLE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. AN ADJUSTMENT AND TEST WAS PERFORMED IAW MM 76-11-01, PAGE 201 AND OPERATION OF THE NR 2 ENGINE THROTTLE CHECKED GOOD WITH NO DEFECTS NOTED. (X) 2L73 4F A22WE 19950303002761995030300276NM 1995 3 3 CAL950112 119950208A3260 WIRE BRACKET BOEING727 727243 138408DNM NLG BROKEN A ACALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0917410 21663 CLE - FLT 0422 - THE AIRCRAFT HAD A HISTORY OF THE NOSE GEAR DOOR WARNING LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. WHILE TROUBLESHOOTING IN CLE, MAINTENANCE FOUND THE NOSE GEAR WIRE HARNESS WAS HANGING LOW WHICH RESULTED IN THE HARNESS BEING CAUGHT IN-BETWEEN THE FORWARD NOSE GEAR DOORS. THE HARNESS BRACKET WAS FOUND BROKEN. THE BRACKET WAS REMOVED AND REPLACED. A FUNCTIONAL CHECK WAS PERFORMED WITH GEAR DOOR RETRACTION, HARNESS CLEARANCE, AND INDICATIONS CHECKING GOOD. THE AIRCRAFT HAS FLOWN AT LEAST SEVEN FLIGHTS WITHOUT A REPEAT OF NOSE GEAR DOOR WARNING PROBLEMS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (X) 2L73 4F RTA3WE 19950303002771995030300277NM 1995 3 3 CAL950115 119950210A2910651782111 HYD MODULE BOEING737 737291 138448WNM A-HYD SYSTEM LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW091725247710750 20362 CLE - FLT 1255 - THE 'A' HYDRAULIC SYSTEM WAS LOST AFTER DEPARTING LGA. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND PLUG BROKEN ON 'A' SYSTEM HYDRAULIC MODULE. THE 'A' SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED AND LEAK CHECKS WERE GOOD. IN ADDITION, BOTH THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED DUE TO THE 'A' HYDRAULIC SYSTEM FAILURE. (X) 2L72 4F A16WE 19950303002781995030300278NM 1995 3 3 CAL950117 119950111A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096130430739 23355 BFM - INSPECTION FOUND FLOORBEAM CORRODED ON TOP CAP AND LOWER SURFACE AT STA 986.5. THE FLOORBEAM WAS REPAIRED IAW EC 5310-01102. (X) 2L72 4F RTA16WE 19950303002791995030300279NM 1995 3 3 CAL950118 119950113A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096130430739 23355 BFM - INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT BS 328, RBL 42. THE FLOORBEAM WAS REPAIRED IAW EC 5363-01007. (X) 2L72 4F RTA16WE 19950303002801995030300280NM 1995 3 3 CAL950120 119950213A291065449912 HYD VALVE BOEING737 737217 1384464NM A-HYD SYSTEM LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0916232 19886 BWI - FLT 1555 - THE AIRCRAFT LOST THE 'A' SYSTEM HYDRAULIC QUANTITY SHORTLY AFTER TAKEOFF FROM BWI. THE AIRCRAFT WAS RETURNED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MANUAL SHUT-OFF VALVE IN THE TAIL COMPARTMENT LEAKING. THE VALVE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A16WE 19950303002811995030300281WP 1995 3 3 CAL950122 119950207A5320 SUPPORT DOUG DC10 DC1030 3023501WP FS 1887 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091406281963 47863 BFM - A MAIN CABIN FLOOR SUPPORT WAS FOUND CORRODED AT STA 1887 FROM LBL 30 TO LBL 48. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-01. (X) 2L73 4F A22WE 19950303002821995030300282WP 1995 3 3 CAL950123 119950207A5312 BULKHEAD DOUG DC10 DC1030 3023501WP CTR MLG WW CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091406281963 47863 BFM - INSPECTION FOUND CENTER MLG WHEELWELL AFT BULKHEAD CORRODED FROM LBL 31 TO RBL 31. THE BULKHEAD WAS REPAIRED IAW SRM 51-00. (X) 2L73 4F A22WE 19950303002831995030300283EU 1995 3 3 CAL950125 119950213A7330AC9227F1740 CLOG LIGHT AIRBUS300 A300B4103 3930104EU GE CF6 CF650C2 30018NE NR 1 ENGINE FUELILLUMINATED A CALAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 SW0911984 108 455845 EWR - FLT 0701 - THE NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED ON CLIMB-OUT OF EWR. FUEL WAS DUMPED AND AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE FUEL FILTER WAS REMOVED AND INSPECTED. NO CONTAMINATION OR DEFECTS WERE FOUND. THE NR 1 ENGINE FUEL FILTER WAS REPLACED AS A PRECAUTIONARY MEASURE. THE NR 1 ENGINE WAS RUN AT ALL POWER SETTINGS AND THE FUEL FILTER CLOG LIGHT DID NOT ILLUMINATE. THE FUEL FILTER WAS REMOVED AND REPLACED AFTER THE ENGINE RUN. THE REMOVED FILTER WAS INSPECTED AND NO CONTAMINATION WAS FOUND. (X) 2L72 4F4 F A35EU E23EA 19950303002861995030300286CE 1995 3 3 HERA9501 119950117A27501185210551 SWITCH BEECH 1900 1900C 1154161CE RT TE FLAPS DIRTY A AHERAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 AL0355456 UC165 ANC - FLT 1495 - AIR RETURN DUE WING FLAPS STUCK IN THE TAKEOFF POSITION AFTER DEPARTURE. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED THE LEFT AND RIGHT FLAP SAFETY SWITCHES AND CHECKED THE RIGGING OF THE SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE FLAP SYSTEM WORKING NORMALLY, THE AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX924. (X) 2L72 4T RTA24CE 19950303002871995030300287CE 1995 3 3 HERA9503 119950119A3610 BLEED AIR BEECH 1900 1900C 1154161CE LT/RT FAILED A HERAO OTHER O OTHER CRCRUISE 1 AL0355456 UC165 SDP/ANC - FLT 1476 - AIRCRAFT EXPERIENCED A DUAL BLEED AIR FAILURE. TOTAL TIME OF FAILURE WAS APPROXIMATELY 10 SECONDS. THE FAILURES OCCURRED WHILE DESCENDING THROUGH 15,000 FEET IN CLEAR WEATHER AND MINUS 20 DEGREES CELSIUS OAT. CONDITIONS PRIOR TO THE FAILURES WERE AS FOLLOWS: ALTITUDE - FL210 FOR 2 HOURS IN CLEAR WEATHER AND MINUS 33 DEGREES CELSIUS OAT. MAINTENANCE COULD NOT FIND A REASON FOR THE FAILURES AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T RTA24CE 19950303002881995030300288CE 1995 3 3 HERA9504 119950126A27501013800001 CONTROL CABLE BEECH 1900 1900C 1154161CE LT TE FLAPS BINDING A AHERAO OTHER F FLT CONT AFFECTED DEDESCENT 1 AL035632C UC81 KSM - FLT 5691 - ON DESCENT, THE WING FLAPS BECAME STUCK IN THE APPROACH POSITION. A LANDING WAS MADE WITHOUT INCIDENCE. THE AIRCRAFT WAS THEN REPOSITIONED TO ANC ON A SPECIAL FLIGHT PERMIT. AFTER TROUBLESHOOTING THE WING FLAP SYSTEM, MAINTENANCE REMOVED AND REPLACED THE LEFT INBOARD AND THE RIGHT OUTBOARD FLAP DRIVE CABLES. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX922. (X) 2L72 4T RTA24CE 19950303002891995030300289CE 1995 3 3 HERA9505 119950131A27501185210551 SWITCH BEECH 1900 1900C 1154161CE LT TE FLAPS DIRTY A AHERAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 AL0380346 UC94 ANC - FLT 1481 - AIR RETURN DUE WING FLAPS WOULD NOT RETRACT PAST THE TAKEOFF POSITION AFTER TAKEOFF. A LANDING WAS MADE AT ANC WITHOUT INCIDENCE. MAINTENANCE CLEANED AND LUBED THE LEFT AND RIGHT FLAP SAFETY SWITCHES. AFTER OPERATIONAL CHECKS CONFIRMED THE FLAP SYSTEM WORKING NORMALLY, THE AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX923. (X) 2L72 4T RTA24CE 19950303003191995030300319NE 1995 3 3 PAYA95A4001 219950123A73207863924 HMU AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 2 ENGINE SURGING A PAYAO OTHER O OTHER APAPPROACH 1 EA174201G 048 120423 JFK-PNE - NR 2 ENGINE SURGING AT ALL POWER SETTINGS. REMOVED AND REPLACED NR 2 HMU. PERFORMED GROUND AND TEST FLIGHT OPS CHECKS. BOTH OPS CHECKS WERE SATISFACTORY. (X) 2H72 4T4 TRTA53EU E20NE 19950303003201995030300320EU 1995 3 3 PAYA95A4002 119950208A5313 STRINGER AEROSPATR42 ATR42300 8680920EU FUSELAGE CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174211G10961 178 DURING C-CHECK, DISCOVERED SURFACE CORROSION ON STR 16R BETWEEN FRAMES 28 AND 31. REMOVED CORROSION AND TREATED AREA. (X) 2H72 4T RTA53EU 19950303003211995030300321EU 1995 3 3 PAYA95A4003 119950208A5313 STRINGER AEROSPATR42 ATR42300 8680920EU FUSELAGE CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174211G10961 178 DURING C-CHECK, DISCOVERED SURFACE CORROSION ON STR 16R BETWEEN FRAMES 34 AND 35. REPLACED DAMAGED SECTION OF STRINGER. (X) 2H72 4T RTA53EU 19950303003221995030300322EU 1995 3 3 PAYA95A4004 119950208A5260 AIRSTAIR DOOR AEROSPATR42 ATR42300 8680920EU CABIN CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174211G10961 178 DURING C-CHECK, DISCOVERED SURFACE CORROSION ON AIRSTAIR DOOR INTERIOR NEAR HINGE POINTS. REPAIRED EFFECTED AREA. (X) 2H72 4T RTA53EU 19950303003231995030300323EU 1995 3 3 PAYA95A4005 119950208A5260 AIRSTAIR DOOR AEROSPATR42 ATR42300 8680920EU CABIN CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174211G10961 178 DURING C-CHECK, DISCOVERED CRACK IN PATCH OF A PREVIOUS REPAIR, LOWER FORWARD AIRSTAIR DOOR. REPLACED PATCH. (X) 2H72 4T RTA53EU 19950303003241995030300324EA 1995 3 3 PAYA95D7003 119950123A3230 RETRACT MECH DHAV DHC7 DHC7102 2802708EA LT MLG MALFUNCTIONED A PAYAO OTHER J WARNING INDICATION APAPPROACH 1 EA17177RA 85 PHL-JFK - FLT 7707 - THE LT MAIN GEAR FAILED TO EXTEND NORMALLY. EMERGENCY GEAR EXTENSION PERFORMED NORMAL. JACKED ACFT AND CYCLED GEAR 20 TIMES WITH NO DEFECTS NOTED. RELEASED ACFT FOR TEST FLIGHT AND CYCLED GEAR AT ALTITUDE. NO DEFECTS NOTED. (W) 2H74 4T A20EA 19950303003251995030300325EA 1995 3 3 PAYA95D7004 119950122A3230 RETRACT MECH DHAV DHC7 DHC7102 2802708EA RT MLG MALFUNCTIONED A PAYAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA17176RA 76 JFK-PNE - FLT 176 - THE RT MLG FAILED TO EXTEND NORMALLY, EMERGENCY EXTENSION PERFORMED, NO TRANSIENT LIGHT ILLUMINATED DURING EXTENSION. GREASED RT MLG, FUNCTIONALLY CHECKED EXTENSION AND RETRACTION THROUGH TEN CYCLES WITH NO DEFECTS NOTED. (W) 2H74 4T A20EA 19950303003261995030300326NM 1995 3 3 TSAA9552030 119950203A5230 SKIN BOEING737 737297 1384480NM CARGO DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND AFT CARGO DOOR EXTERIOR SKIN CRACKED AT LOWER AFT CORNER. REPAIRED PER ECO 2003R2. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003271995030300327NM 1995 3 3 TSAA9552032 119950203A5240 HINGE GATE BOEING737 737297 1384480NM SERVICE DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND AFT SERVICE DOOR TOP HINGE GATE CRACKED. REPLACED TOP GATE HINGE PER ECO 1593R2. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003281995030300328NM 1995 3 3 TSAA9553029 119950203A5311 FRAME BOEING737 737297 1384480NM FS 578 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND BS 578, LT FRAME INBD FLANGE CRACKED BETWEEN S-16L AND S-17L. REPAIRED PER ECO 1567 DEV. HR 1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003291995030300329NM 1995 3 3 TSAA9553031 119950203A5312 BULKHEAD FITTING BOEING737 737297 1384480NM BS 757 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND BULKHEAD-TO-FLOOR BEAM FITTING AT BBL '0' AND BS 727 CRACKED HORIZONTALLY ACROSS RADIUS OF FORWARD FLANGE, .75 INCH LONG. REPAIRED PER ECO 2331 PART I AND IV. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003301995030300330NM 1995 3 3 TSAA9553033 119950203A5312 BULKHEAD WEB BOEING737 737297 1384480NM BS 178 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND CRACK IN BULKHEAD WEB AT BS 178, WL 1850, LT LOWER NOSE COMPARTMENT. REPAIRED PER ECO 2518R1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003311995030300331NM 1995 3 3 TSAA9553034 119950203A5312 BULKHEAD WEB BOEING737 737297 1384480NM BS 178 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND CRACK IN BULKHEAD WEB, DT 178, WL 185.0, RT LOWER NOSE COMPARTMENT. REPAIRED PER ECO 2518R1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003321995030300332NM 1995 3 3 TSAA9553035 119950203A5311 FRAME BOEING737 737297 1384480NM BS 597 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND BS 597, LT FRAME INBD FLANGE FOUND CRACKED BETWEEN S-16L AND S-17L. REPAIRED PER ECO 1567, DEV. 6, OPTION 2. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003331995030300333NM 1995 3 3 TSAA9553036 119950203A5320 ANGLE BOEING737 737297 1384480NM BS 578 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, CABIN - BS 578 LT STUB OTBD ATTACH ANGLE FOUND CRACKED AT LOWER EDGE TO RIVET HOLE. REPAIRED PER ECO 1567 DEV. H R1, OPTION 1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003341995030300334NM 1995 3 3 TSAA9553037 119950203A5313 STRINGER BOEING737 737297 1384480NM AFT FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, FOUND STRINGER ABOVE APU INLET - EXFOLIATION CORROSION. REPLACED STRINGER PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003351995030300335NM 1995 3 3 TSAA9555038 119950203A5510 BEAM BOEING737 737297 1384480NM LT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, LT HORIZONTAL STABILIZER LOWER T/E BEAM - CORROSION AT ES 50.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003361995030300336NM 1995 3 3 TSAA9555039 119950203A5510 BEAM BOEING737 737297 1384480NM LT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, LT HORIZONTAL STABILIZER LOWER T/E BEAM - SURFACE CORROSION AT ES 195.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003371995030300337NM 1995 3 3 TSAA9555040 119950203A5510 BEAM BOEING737 737297 1384480NM RT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, RT HORIZONTAL STABILIZER UPPER T/E BEAM - SURFACE CORROSION AT ES 195.0. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003381995030300338NM 1995 3 3 TSAA9555041 119950203A5510 BEAM BOEING737 737297 1384480NM RT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, RT HORIZONTAL STABILIZER UPPER T/E BEAM - SURFACE CORROSION AT ES 213. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003391995030300339NM 1995 3 3 TSAA9557027 119950203A5730 SKIN BOEING737 737297 1384480NM WS 484 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT LEFT WING SKIN, WS 484, CORROSION NOTED. REPAIRED PER ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003401995030300340NM 1995 3 3 TSAA9557028 119950203A5730 SKIN BOEING737 737297 1384480NM WS 474 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING HEAVY MAINTENANCE VISIT, LEFT WING SKIN, WS 474, CORROSION NOTED. REPAIRED PER ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950303003411995030300341NM 1995 3 3 YAUA9501 119950120A5320 WINDOW POST BOEING727 727231 1384079NM COCKPIT CRACKED A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 TYPE SERVICE '2B' CHECK. X-RAY OF WINDOW POST N-F, AD 93-05-17, REF. SB 737-53-0086. FOUND CRACK AT 6TH FASTENER DOWN TO EDGE OF POST N-F, RIGHT HAND. EDDY CURRENT USED TO VERIFY CRACK. MODIFICATION/REPAIR DONE IAW SB 727-53-0086, REV 2, PART II, PAGE 24, USING BOEING KIT 65C35282-8, REF. CARD CCR 590-193 AND NON-ROUTINE CARD NR 26. (X) 2L73 4F A3WE 19950303003421995030300342WP 1995 3 3 9503069106 119950225A5270 SWITCH DOUG DC9 DC915 3022036WP CABIN DOOR MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL0196S 47206 DURING START OF TAKEOFF ROLL MEM-IND, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND THE AIRCRAFT RETURNED TO THE GATE. REPLACED THE DOOR WARNING SWITCH. CHECKED OK. 2L72 4F A6WE 19950303003431995030300343WP 1995 3 3 9503079760 119950223A5220 RELEASE MECH DOUG DC9 DC941 302207NWP LT EMER EXIT OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01760NW 47288 DURING PERIODIC CHECK, FOUND THAT THE LEFT AFT EMERGENCY OVERWING EXIT WOULD NOT OPEN FROM THE OUTSIDE. ADJUSTED THE OUTER HANDLE RELEASE MECHANISM PER MM 52-21-0. 2L72 4F A6WE 19950303003441995030300344WP 1995 3 3 9503089923 119950226A5350 CLIPS DOUG DC9 DC932 3022066WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01927RC 47469 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ADJUSTED THE CLIPS. CHECKED OK. 2L72 4F A6WE 19950303003451995030300345WP 1995 3 3 9503099852 119950223A5320 FITTING DOUG DC9 DC951 3022051WP FS 636 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01761NC 47709 DURING PERIODIC CHECK, FOUND CORROSION ON FRAME SUPPORT FITTINGS FS 636 AT LONGERONS 29B LEFT AND RIGHT. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950303003461995030300346WP 1995 3 3 9503109957 119950223A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP FS 258 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01915RW 47139 DURING PERIODIC CHECK, FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM FASTENER HOLES AT FLOOR PANELS NR 28 AND NR 29, FS 258. REPAIRED PER EA 99-096929. 2L72 4F A6WE 19950303003471995030300347WP 1995 3 3 9503119101 119950224A5313 LONGERON DOUG DC9 DC915 3022036WP FS 370 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0191S 47063 DURING LINE CHECK, FOUND .5 INCH CRACK IN LONGERON 16R THROUGH LOWER LEG AT FS 370. REPAIRED PER EA 91-094932. 2L72 4F A6WE 19950303003481995030300348WP 1995 3 3 9503129979 119950225A5753 SKIN DOUG DC9 DC931 3022065WP RT TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING LINE CHECK, FOUND 10 INCH CRACK IN THE RIGHT TRAILING EDGE FLAP, 53 INCHES INBOARD FROM THE OUTBOARD END. REPAIRED PER EA 98-091929, SEC.1. 2L72 4F A6WE 19950303003491995030300349WP 1995 3 3 9503139928 119950225A5320 CHORD DOUG DC9 DC931 3022065WP FS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER 'T' CAPS IN THE LEFT AND RIGHT NOSE LANDING GEAR TUNNELS FS 110. REPAIRED BOTH PER EA 99-093494. 2L72 4F A6WE 19950303003501995030300350WP 1995 3 3 9503149912 119950226A2120 DUCT DOUG DC9 DC931 3022065WP ACM LEAKING A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01962N 47406 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FOLLOWED PRECAUTIONARY FLIGHT PROCEDURES AND LIGHT REMAINED ON. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND DUCT LEAK AT HOT SIDE OF ACM. REPAIRED LEAK. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303003511995030300351 1995 3 3 9503159978 419950224A22162587788901 SERVO DOUG DC9 DC931 3022065WP AUTO PILOT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL019342 65732474 47391 AUTO-PILOT FAILED EN ROUTE DTW-HOU, FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED AUTO-PILOT ELEVATOR SERVO. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303003521995030300352 1995 3 3 9503169882 419950226A3421258733511 VERTICAL GYRO DOUG DC9 DC951 3022051WP LEFT MALFUNCTIONED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01670MC351845913 47659 CAPTAIN'S VERTICAL GYRO FAILED DURING TAKEOFF ROLL AT DTW. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED CAPTAIN'S VERTICAL GYRO. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303003531995030300353WP 1995 3 3 9503179945 119950226A32225910448 STRUT DOUG DC9 DC932 3022066WP NLG DEFLATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018925E 45840 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED GROUND SHIFT LINKAGE AND CABLES WITH NO PROBLEMS FOUND. PERFORMED FULL SERVICE OF NOSE LANDING GEAR STRUT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303003541995030300354NM 1995 3 3 95FDEA00168 119950221A532065453182 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04485FE 18871 CRACK FOUND IN STR CLIP BS 440 STR 2R. REMOVED FASTENERS FROM CRACKED STR CLIP AT BS 440 STR 2R. THEN INSTALLED NEW STR CLIP IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950303003551995030300355NM 1995 3 3 95FDEA00169 119950221A5330040T3 SKIN BOEING727 72722 1384002NM BS 390 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE IN EXTERNAL SKIN STA 390, STR 7 AND 8 SKIN THICKNESS .040 GOUGE .012, GOUGE OUT OF LIMITS AS PER FEDEX SRM 53-30-1. REPAIRED GOUGE WITH SKIN FLUSH REPAIR AT STA 390 STR 7 AND 8 PER FEDEX SRM 53-30-3 FIG 13. 2L73 4F A3WE 19950303003561995030300356NM 1995 3 3 95FDEA00170 119950222A53206526176X3 INTERCOSTAL BOEING727 72722 1384002NM BS 322 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON FLOOR SUPPORT BS 322, LBL 30, WL 208. REMOVED CORRODED FLOOR SUPPORT THEN INSTALLED A NEW FLOOR SUPPORT AT BS 322, LBL 30, WL 208. 2L73 4F A3WE 19950303003571995030300357NM 1995 3 3 95FDEA00171 119950222A5320652617314 SUPPORT BOEING727 72722 1384002NM BS 334 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON FLOOR SUPPORT BS 334, LBL 30, WL 208. REMOVED CORRODED FLOOR SUPPORT THEN INSTALLED A NEW FLOOR SUPORT BS 334, LBL 30, WL 208. 2L73 4F A3WE 19950303003581995030300358NM 1995 3 3 95FDEA00172 119950222A5320707ST6050 CLIP BOEING727 72727C 138400JNM BS 970 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04145FE 19109 CORROSION IN AFT CARGO BAY THERE IS CORROSION ON STR CLIP AT BS 970, STR 30. REMOVED AND FABRICATED STR CLIP 7076T6-050 AND INSTALLED STR CLIP. 2L73 4F A3WE 19950303003591995030300359NM 1995 3 3 95FDEA00173 119950216A53157075TL FLOORBEAM BOEING727 72725 1384006NM BS 1110 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION (72C237-02) UNDER TOP CHORD OF FLOORBEAM AT NUTPLATES HOLES BS 1110, RBL 10-50, WL 208. REPAIRED FLOORBEAM BS 1110, RBL 10-50, WL 208 PER FEDEX EA 7-5310-23793. 2L73 4F A3WE 19950303003601995030300360NM 1995 3 3 95FDEA00174 119950217A531170750063 FRAME BOEING727 72725 1384006NM BS 600 DOUBLE DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO04507FE 18278 DOUBLE HOLE IN FRAME BS 600, STR 4R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 51-40-3. 2L73 4F A3WE 19950303003611995030300361NM 1995 3 3 95FDEA00175 119950216A53157075T6 FLOORBEAM BOEING727 72725 1384006NM BS 560 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 FOUND CORROSION ON FLOORBEAM STA 560, RBL 16, WL 198. REMOVED CORROSION AND REPAIRED FLOORBEAM AT BS 560, RBL 16, WL 198 PER FEDEX EA 7-5310-23795. 2L73 4F A3WE 19950303003621995030300362NM 1995 3 3 95FDEA00176 119950216A53157075T6 FLOORBEAM BOEING727 72725 1384006NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION ON TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208. REPAIRED TOP AND BOTTOM OF FLOORBEAM AT BS 312, LBL 45, WL 208 IAW EA 7-5310-23790. 2L73 4F A3WE 19950303003631995030300363NM 1995 3 3 95FDEA00177 119950216A53157075T6 FLOORBEAM BOEING727 72725 1384006NM BS 276 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04507FE 18278 CORROSION FOUND ON TOP CHORD OF FLOORBEAM BS 276, RBL 12, WL 208. REPAIRED TOP CHORD FLOORBEAM IAW 727 SRM 51-40-04, 51-20-01. 2L73 4F A3WE 19950303003641995030300364EU 1995 3 3 95FDEA00178 119950226A3260BDM3003 PROX DET UNIT AIRBUS300 A300F4605R 3930327EU E/E BAY MALFUNCTIONED A FDEAA UNSCHED LANDING I FLT. ATTITUDE INST. CLCLIMB 1 SO04654FE 738 T/O AUTO THROTTLES DROPPED OFF, REENGAGED AFTER T/O, DROPPED AGAIN, L/GEAR INTERLOCK SELECTED SYS 2. NR 1 A/P AND PITCH TRIM TRIPPED OFF. F/O'S PITOT HEAT O/H ON, WHEN A/P REENGAGED. SELECTED NR 2 A/P, O/H LT OUT, BACK ON. TURNED OFF PER ECAM. CAPTS FLT DIRECTOR DISAPPEARED-CYCLE ON/OFF, CAME ON W/N OPS PROPERLY. SPEED PROTECTOR BARS FAULTED. SELECTED CAPTS ADC ON 2 SPEED BARS BACK ON. GOT NR 1 PRESS FAULT ON ECAM. SELECTED 2 RETURN TO PHX. FOUND PROX DET UNIT FAILED AND REVEALED CODES. REPLACED PROX SENSOR 64GB AND PROX DET UNIT PER MM 32-31-71. ALL CK GOOD. 2L72 4F RTA35EU 19950303003651995030300365NM 1995 3 3 95FDEA00179 119950223A5313BAC1498138 STRINGER BOEING727 72722 1384002NM BS 440 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE IN STR BS 440, STR 7L. ACCOMPLISHED STR REPAIR BS 440, STR 7L PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950303003661995030300366NM 1995 3 3 95FDEA00180 119950224A532065453132 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 STR CLIP DAMAGED BS 440 STR 8L. REMOVED DAMAGED STR CLIP AND INSTALLED NEW CLIP IAW SRM 51-30-2. 2L73 4F A3WE 19950303003671995030300367NM 1995 3 3 95FDEA00181 119950225A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 440-482 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON THE SEAT TRACK BS 480-482 WL 208 LBL 23.5. REMOVED CORRODED SEAT TRACK SECTION. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION USING EXISTING AS TEMPLATE. 2L73 4F A3WE 19950303003681995030300368NM 1995 3 3 95FDEA00182 119950223A53202024T3 WEB BOEING727 72722 1384002NM BS 310 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 SEVERAL HOLES IN THE WEB DAMAGED WHILE REMOVING A STIFFENER AT BS 310, LBL 12 - RBL 12, WL 180. REMOVED DAMAGED AREA IN WEB BS 310, LBL12-RBL 12, WL 180. FABRICATED DOUBLER AND FILLERS, SCOTCH BRITED, ALODINED, PRIMED, INSTALLED AS PER FEDEX SRM 53-10-9. 2L73 4F A3WE 19950303003691995030300369NM 1995 3 3 95FDEA00183 119950224A5320BAC14902785 ANGLE BOEING727 72722 1384002NM BS 960 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION IN AFT CARGO BAY BS 960, RBL 20, WL 144 ON L-ANGLE STIFFENER (HORIZONTAL) FOR BULKHEAD. CORROSION OUT OF LIMIT PER FEDEX SRM 53-10-01 CUT OUT DAMGED. FABRICATED PARTS, REPAIRED PER FEDEX SRM 51-40-04. 2L73 4F A3WE 19950303003701995030300370NM 1995 3 3 95FDEA00184 119950227A532069144691 CLIP BOEING727 72722 1384002NM BS 870 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 NOTED CRACK AND/OR HOLE DAMAGE IN LT BS 870 TERMINAL FITTING ROW 1, HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP. 2L73 4F A3WE 19950303003711995030300371NM 1995 3 3 95FDEA00185 119950225A53302024T3 SKIN BOEING727 72727C 138400JNM BS 128 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04145FE 19109 GOUGE IN SKIN BS 1280 JUST ABOUT STR 21R .020 D OUT OF LIMITS PER SRM. REPAIRED PER FEDEX SRM 53-30-2. 2L73 4F A3WE 19950303003721995030300372NM 1995 3 3 95FDEA00186 119950225A53302024T3 SKIN BOEING727 72727C 138400JNM BS 1280 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04145FE 19109 SKIN BULGE AND RIVETS HEADS POPPING AT SKIN LAP BS 1280, STR 10L. REPAIRED SKIN LAP STA 1280, STR 19L PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950303003731995030300373NM 1995 3 3 95UAL757006 119950228A2750 RSTRACT MECH BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 WP29547UA 25368 DURING APPROACH THE FLIGHT CREW WAS UNABLE TO EXTEND FLAPS FULLY. OP CHECKED FLAPS, BITE CHECKED FLAP SLAT ELECTRONIC UNIT, AND VISUALLY INSPECTED FLAPS. NO DEFECTS FOUND. 2L72 4F4 FRTA2NM E17NE 19950303003741995030300374NE 1995 3 3 95UAL767009 219950228A7530 BLEED CONTROL 7765555 BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 2 ENGINE FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29605UA 799A 21866 709678 ON TAKEOFF ROLL NR 2 ENGINE WOULD NOT PRODUCE FULL POWER. REPLACED ENGINE VANE AND BLEED CONTROL. 2L72 4F4 FRTA1NM E3NE 19950303003751995030300375EU 1995 3 3 95UALA32011 119950228A5610 WINDOW AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE RT COCKPIT LOOSE A UALAK NONE O OTHER LDLANDING 1 WP29421UA 500 CABIN DEPRESSURIZED DURING LANDING. FIRST OFFICERS WINDOW WAS THE SOURCE OF AIR LOSS. WINDOW IS LOOSE. WINDOW STARTED LEAKING ON DESCENT AND MOVED INWARD RELEASING CABIN PRESSURE ON TOUCH DOWN. 2L72 4F RTA28NM E40NE 19950303003761995030300376EU 1995 3 3 95UALA32012 119950228A2700 FLIGHT CONTROLS AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CONTROL SYST MALFUNCTIONED A AUALAO OTHER O OTHER CRCRUISE 1 WP29417UA 483 CREW REPORTED THAT AFTER TAKEOFF, AIRCRAFT WANTED TO FLY RIGHT WING DOWN, NOT STRAIGHT. AFTER ALTITUDE WAS REACHED, PROBLEM WENT AWAY. AFTER REACHING AN ALTITUDE OF 12788 CREW STATED THAT IN CLIMB AIRCRAFT TENDED TO FAVOR LT WING LOW AND AT HIGHER THAN NORMAL CRUISE FAVORED RT WING LOW CREW HAD NO ECAM MESSAGES AND NO MESSAGES ON POST FLIGHT REPORT. 2L72 4F RTA28NM E40NE 19950303003771995030300377SO 1995 3 3 COM11801 119950226A5720 SKIN SUPPORTS EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01269CA7633 7633 120263 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AT RIBS 15 AND 16. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17057-005, 2 EA; 120-17057-007, 1 EA; 120-17056-011, 1 EA. 2L72 4T RTA31SO 19950303003781995030300378SO 1995 3 3 COM11802 119950223A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01159A 6090 120159 CONROL FAULT WARNING WHEN FLAPS SELECTED TO 15 DEGREES. REPLACED LEFT INBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950303003791995030300379SW 1995 3 3 COM20356 119950228A272027420519011 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01704C 288 AC704 RUDDER TORQUE TUBE WAS FOUND TO BE BENT. THE TORQUE TUBE WAS REPLACED WITH NEW PART (SUBSTITUTE PART NUMBER 27-42051-8037) PER FAIRCHILD MAINTENANCE MANUAL 27-20-04, PPG 201-204 AND AEROTECH REPORT NR 1210, REV IR DATED 9-21-92. 1L72 4T A8SW 19950303003801995030300380EA 1995 3 3 COM60430 119950225A2740601R5170G1 SWITCH PANEL CNDAIRCL600 CL6002B19 EA COCKPIT DIRTY A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01926CA3247 7027 STABILIZER TRIM, CHANNEL 1 DISENGAGES WHEN AUTOPILOT IS ENGAGED. CLEANED STABILIZER SWITCH PANEL, SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950303003811995030300381EA 1995 3 3 COM60431 119950227A3040NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 EA LT WINDSHIELD FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01938CA1089 1089 7046 LEFT WINDSHIELD HEAT FAILED. SWAPPED OVERTEMP SENSOR LEADS TO SPARE SENSOR. 2L72 4F RTA21EA 19950303003821995030300382NM 1995 3 3 DL72L950848 119950222A532069678811 GUSSET BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 THE RT TORQUE BOX HORIZONTAL BEAM GUSSET AT FS 1273 WAS FOUND CRACKED. THE GUSSET WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129 REV. 4. 2L73 4F A3WE 19950303003831995030300383NM 1995 3 3 DL72S950849 119950211A5320 FORMER BOEING727 727232 1384082NM FS 540 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV FOUND HOLE IN FORMER STA 540 STR 24L. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 26. 2L73 4F A3WE 19950303003841995030300384NM 1995 3 3 DL72S950850 119950212A5320 WEB BOEING727 727232 1384082NM FS 357 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV FOUND SUPPORT WEB CRACKED AT STA 357 STR 16 L AIR DUCT CUTOUT. FABRICATED DOUBLER PER ERA 301217-4. INSTALLED PER SRM 53-10-4. 2L73 4F A3WE 19950303003851995030300385NM 1995 3 3 DL72S950851 119950210A5510 SUPPORT BOEING727 727232 1384082NM HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV FOUND SUPPORT STRIP CRACKED ON T/E OF STAB BELOW O/B ELEV ATTCH HNGE POINT. INSTALLED NEW T/E BEAM. 2L73 4F A3WE 19950303003861995030300386NM 1995 3 3 DL72S950852 119950211A5313 STRINGER BOEING727 727232 1384082NM FS 580 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT HMV FOUND HOLE IN STR 25L AT STA 580. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950303003871995030300387NE 1995 3 3 DL72S950853 219950223A731437820113 FUEL PUMP BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING X ENGINE FLAMEOUT TOTAKEOFF 1 SO11495DA 21075 687376 ON TAKOFF NR 1 ENGINE FLAMED OUT. RETURNED PHX LANDED WITHOUT INCIDENT. REPLACED FUEL CONTROL AND PUMP. SHOP INSPECTION FOUND FUEL PUMP DRIVE SHAFT SHEARED. 2L73 4F4 F A3WE E2EA 19950303003881995030300388NM 1995 3 3 DL72S950857 119950105A5754651622295 SKIN BOEING727 727225 1384077NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 UPON INSPECTION OF THE NR 3 SLAT, THE SKIN WAS FOUND TO BE CRACKED AT THE ACTUATOR. A REPAIR WAS PERFORMED PER THE SRM 57-50-3, FIGURE 1. 2L73 4F A3WE 19950303003891995030300389NE 1995 3 3 DL73S950870 219950226A7200JT8D15A ENGINE BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 FAILED A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO11303DL29726 23075 709114 AFTER TAKOFF, RDU NR 1 ENGINE FLAMED-OUT AT TOP OF CLIMB. OFF LANDED GSO. FOUND METAL ON CHIP DETECTOR AND OIL SCREEN, N1 FAN BINDING AND UNABLE TO TURN N2. REPLACED ENGINE AND ROUTED TO SHOP FOR REPAIRS (SUPPLEMENT 5-18-95). UPON DISASSEMBLY IN SHOP, FOUND NR 3 BEARING STACK FAILURE. NR 3 BEARING STACK HAS SPUN, FUSING SEVERAL PARTS TOGETHER DL EO 42-61043, WHICH PREVENTS THIS FAILURE, HAD NOT YET BEEN INCORPORATED. 2L72 4F4 FRTA16WE E2EA 19950303003901995030300390NM 1995 3 3 DL757950871 119950223A3397W1 HARNESS BOEING757 757232 1384965NM FLIGHT DECK CHAFED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11627DL 22917 DURING CRUISE HAD 4 FLIGHT DECK PANEL LIGHTING CIRCUIT BREAKERS POP. REMOVED CAPTAINS P1-3 INSTRUMENT PANEL, FOUND W-1 WIRE BUNDLE WITH BURNED WIRES. THE CAUSE WAS FROM THE WIRE BUNDLE CHAFING ON THE CAPTAINS WINDOW DEFROSTER AIR HOSE. A TOTAL OF 17 WIRES WERE REPAIRED AND WIRE BUNDLE WAS PROTECTED WITH ANTI-CHAF MATERIAL. A FLEET INSPECTION WAS INITIATED ONE ADDITIONAL AIRCRAFT WAS FOUND WITH CHAFED WIRES. 2L72 4F RTA2NM 19950303003911995030300391NM 1995 3 3 DL76L950597 119950211A5321453T193683 FLOOR PANEL BOEING767 767332 1382001NM C-1 CARGO DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11172DN 24775 C-1 CARGO COMPARTMENT FLOOR PANEL 4R IS DENTED IN CENTER OF PANEL. FOUND AND REPAIRED PER HMV, PER SRM 53-00-50. 2L72 4F RTA1NM 19950303003921995030300392NM 1995 3 3 QXEA9500059 119950227A3350 EEL BREAKER DORNERDO32 DO328100 2996000NM CABIN TRIPPED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09335PH 3013 PDX - THE EMERGENCY ESCAPE LIGHTS CIRCUIT BREAKER WAS FOUND POPPED ON THE GROUND. RESET CIRCUIT BREAKER OPERATIONAL CHECK GOOD. NO DEFECTS NOTED AND A/C WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19950303004431995030300443NM 1995 3 3 AALA950160 119950130A3350A3060722 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07885AA 21524 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS UNDER EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L73 4F A3WE 19950303004441995030300444 1995 3 3 AALA950171 419950201A256531073105 SLIDE BOEING727 727223 1384074NM PAX DOOR SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07872AA 21384 ORD - DURING SLIDE SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE SEAM AT GIRT TUBE FAILED. SCRAPPED EMERGENCY EVACUATION SLIDE. (W) 2L73 4F A3WE 19950303004451995030300445 1995 3 3 AALA950173 419950201A256531073105 SLIDE BOEING727 727223 1384074NM CABIN DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW076804 19479 ORD - DURING SLIDE SHOP VISIT, DETACHABLE GIRT ASSEMBLY ONEMERGENCY EVACUATION SLIDE FOUND DETERIORIATED. SLIDE PROCESSED THROUGH SHIP FOR OVERHAUL, INCLUDING REPLACEMENT OF DETACHABLE GIRT ASSEMBLY. (W) 2L73 4F A3WE 19950303004461995030300446EU 1995 3 3 AALA950194 119950201A3350 FLAT WIRE AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770054 461 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 21AB TO 23AB INOPERATIVE. REPLACED SIDEWALL RIBBON WIRE TO EMERGENCY FLOOR LIGHT CONNECTION AT PAX SEAT 21AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950303004471995030300447WP 1995 3 3 AALA950201 119950204A3350A3030398101 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE CONNECTIONA AALAK NONE L NO TEST ININSP/MAINT 1 SW07241AA 49254 OKC - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. TIGHTENED LOOSE EMERGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTOR AT FIRST CLASS BULKHEAD. SYSTEM CHECKS NORMAL OPERATION. (W) 2L72 4F A6WE 19950303004481995030300448NM 1995 3 3 AALA950202 119950205A3230 SENSOR BOEING767 767223 1385123NM LT MLG DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW07320AA 22321 MIA-DFW - FLT 457 - AFTER TAKEOFF, GEAR FAILED TO RETRACT. ON FOURTH ATTEMPT, GEAR RETRACTED AND LOCKED. LANDED DFW WITHOUT INCIDENT. REPLACED LT TILT SENSOR AND ADJUSTED BOTH LT MLG SENSORS. ACCOMPLISHED GEAR SWING, SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950303004491995030300449EU 1995 3 3 AALA950214 119950206A3350A3030398101 EEL CONNECTOR FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071404D 11355 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT FRONT OF COACH INOPERATIVE. REPAIRED BROKEN CONNECTOR. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RT 19950303004501995030300450NM 1995 3 3 AALA950216 119950206A3350A3060722 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07892AA 22008 LGA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE IN COACH. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L73 4F A3WE 19950303004511995030300451NM 1995 3 3 AALA950220 119950206A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07892AA 22008 LGA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT AFT GALLEY AND REAR DOOR. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR AT AFT GALLEY. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L73 4F A3WE 19950303004521995030300452WP 1995 3 3 AALA950232 119950207A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07442AA 49468 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 21 AFT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIPS FROM PAX SEAT ROW 21 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950303004531995030300453 1995 3 3 AALA950237 419950206A256531073105 SLIDE BOEING727 727223 1384074NM CABIN DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07868AA 21373 ORD - DURING SHOP VISIT, FOUND HOLE IN EMERGENCY EVACUATION SLIDE AT LT BOTTOM CENTER AIR TUBE. SLIDE INTRODUCED TO SHOP FOR REPAIR. (W) 2L73 4F A3WE 19950303004541995030300454NM 1995 3 3 AALA950238 119950208A2120 AIR DISTR BOEING727 727223 1384074NM CABIN SMOKING A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07703AA 22461 SJC-CCS - FLT 2141 - DURING CRUISE PASSENGERS AND FLIGHT ATTENDANTS REPORTED SMELLING SMOKE IN MID SECTION OF ACFT. SMELL DISSIPATED, PRECAUTIONARY TESTED AFT BODY OVERHEAT CIRCUIT. LANDED CCS WITHOUT INCIDENT. COULD NOT DUPLICATE ON GROUND, SYSTEM GROUND CHECKED NORMAL OPERATION. ACFT RETURNED TO SERVICE. (W) 2L73 4F A3WE 19950303004551995030300455EU 1995 3 3 AALA950251 119950209A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW0714065 508 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT DOOR 3L REMAINED ILLUMINATED. REPAIRED TWO WIRES FOUND SHORTED AT DOOR 3L. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950303004561995030300456NE 1995 3 3 AWXA9400550 219950217A7261570023 NR 5 CARBON SEAL BOEING737 737222 1384473NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE DETERIORATED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28144AW 19074 687840 PHX - FLT 45 - CORRECTION TO SUPPLEMENTAL/CLOSED SDR DATED 95-02-09; ORIGINAL SDR DATED 94-08-24. LAS/LAX - ON CLIMB-OUT, NR 1 ENGINE HIGH OIL TEMP AND APU GENERATOR WENT OFF LINE. NR 1 GENERATOR PLACARDED INOPERATIVE. ACFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX COMPLIED WITH NR 1 ENGINE CHANGE. ENGINE WAS DISASSEMBLED AND ANALYZED AT GTC IN EAST GRANDBY, CT. DUE TO ENGINE'S HIGH TIME SINCE OVERHAUL AND NORMAL DETERIORATION OF BEARING CARBON SEALS (TSO 18315, CSO 16693), HOT COMPRESSED AIR USED TO PRESSURIZE THE CARBON SEALS 'LEAKS' THROUGH TO THE OILED BEARING AREA RESULTING IN THE OIL BEING HEATED. THE RESULT IS HIGH BREATHER PRESSURE AND HIGH OIL TEMPERATURE. (X) 2L72 4F4 F A16WE E2EA 19950303004571995030300457NE 1995 3 3 AWXA9500071 219950201A732179830014045 EEC AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE INOPERATIVE A AAWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28626AW 65 LAS-PHL - FLT 1787 - EN ROUTE, AFTER TWO HOURS THE CREW OBSERVED ECAM 'ENGINE STALL ALERT' AND NOTED FLUCTUATION OF NR 2 ENGINE EPR. THIRTY MINUTES LATER CREW RECEIVED ECAM NR 2 'SENSOR FAULT AVOID RAPID THRUST CHANGES' MESSAGE. ACFT DIVERTED TO CMH WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED NR 2 ENGINE EEC IAW AWA TASK CARD R5M73302. PERFORMED TASK PER AMM 71-00-00 710 022. OPS CHECK NORMAL, NO FAULTS OR MESSAGES. ACFT RETURNED TO SERVICE. (W) 2L72 4F4 FRTA28NM E311NE 19950303004581995030300458NM 1995 3 3 AWXA9500084 119950213A534465528643 HINGE CASTING BOEING737 73733A 1384673NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW 23627 DURING C-6 INSPECTION, FOUND L2 DOOR UPPER HINGE ARM LOWER CASTING CRACKED AT FUSELAGE SIDE. REMOVED AND REPLACED L2 DOOR HINGE CASTING PER SRM 51-10-02. TOTAL CYCLES 21092. (W) 2L72 4F RTA16WE 19950303004591995030300459NM 1995 3 3 AWXA9500085 119950213A5320 WEB BOEING737 73733A 1384673NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW27436 23627 PHX - DURING C-6 INSPECTION, FOUND L2 DOORWAY FWD FRAME INTERNAL WEB FINGER UNDER REINFORCEMENT STRAP CRACKED AT UPPER HINGE CASTING. INSTALLED REPAIR PER ER 3-53-19 21A. TOTAL CYCLES 21092. (W) 2L72 4F RTA16WE 19950303004601995030300460NM 1995 3 3 AWXA9500086 119950213A5320 CHORD BOEING737 73733A 1384673NM L2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW27436 23627 PHX - DURING C-6 INSPECTION, FOUND L2 DOOR CHORD CORRODED BEYOND CLEAN UP LIMITS. REMOVED AND REPLACED CHORD PER SRM 51-10-02 AND SRM 51-40-02. TOTAL CYCLES 21092. (W) 2L72 4F RTA16WE 19950303004611995030300461NM 1995 3 3 AWXA9500087 119950213A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28166AW27436 23627 PHX - DURING C-6 INSPECTION, FOUND STA 986 FLOORBEAM TOP CAP CORRODED AT NUTPLATE HOLES, ENTIRE LENGTH. REPAIRED DAMAGE PER ER 3 53 16 20A. TOTAL CYCLES 21092. (W) 2L72 4F RTA16WE 19950303004621995030300462NM 1995 3 3 AWXA9500088 119950207A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 17 THROUGH 21. RECONNECTED WIRE TO LIGHT ASSEMBLY AT ROW 19. OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950303004631995030300463NM 1995 3 3 AWXA9500089 119950209A3350 EEL PINS BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 7 THROUGH 9. RECONNECTED PINS ON LIGHT ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950303004641995030300464NM 1995 3 3 AWXA9500090 119950211A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 14 THROUGH 19. REPAIRED WIRE AT ROW 14, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950303004691995030300469NM 1995 3 3 BJNA951001 119950213A33503114981 EEL REFLECTOR BOEING737 7372H4 138448CNM CABIN CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM 20336 THE RT FWD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD EXTERIOR EMERGENCY LIGHT REFLECTOR ASSY AND LAMP. OPS CHECKS NORMAL. (W) 2L72 4F A16WE 19950303004701995030300470NM 1995 3 3 BJNA951002 119950213A33503114981 EEL REFLECTOR BOEING737 7372H4 138448CNM CABIN CORRODED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EXTERIOR EMERGENCY EXIT LIGHT REFLECTOR ASSY AND LAMP. OPS CHECKS NORMAL. (W) 2L72 4F A16WE 19950303004711995030300471NM 1995 3 3 BJNA952001 119950131A3350 EEL BULB BOEING737 7372H4 138448CNM CABIN FAILED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 THE FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULBS L1, R1 DOOR LIGHTS EXTERIOR IAW 33-51-21. (W) 2L72 4F A16WE 19950303004731995030300473NM 1995 3 3 MRKA9510 119950113A3222654620035 STRUT BOEING737 7372T4C 1384501NM NLG LEAKING A MRKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03675MA 23065 AIR RETURN DUE TO NLG WOULD NOT LOCK IN THE UP POSITION. INSPECTION FOUND STRUT TO BE UNDER SERVICED. SERVICED STRUT WITH AIR AND OIL. AFTER SERIES OF FLIGHTS THE STRUT ASSEMBLY WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950303004741995030300474NM 1995 3 3 MRKA953 119950107A21502760000101 VALVE BOEING737 737317 138447PNM LT PACK INOP A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL032FOR 23173 FLIGHT RETURNED TO GATE, DUE TO RT AIR CONDITIONING PACK DEFERRED AND LT AIR CONDITIONING PACK OVERHEAT TRIPPED AND WOULD NOT RESET. REMOVED AND REPLACED WING ISOLATION VALVE DUE TO STUCK OPEN. OPS CHECK OK. (W) 2L72 4F RTA16WE 19950303004751995030300475NM 1995 3 3 MRKA956 119950110A2120 AIR DISTR BOEING737 7372X6C 1384552NM CABIN ODOR A MRKAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03673MA 23124 AIR CONDITIONING SYSTEM SMELLS LIKE OIL AT HIGH POWER SETTINGS. RAN PACKS ON GROUND, COULD NOT DUPLICATE. OK FOR CONTINUED SERVICE. (W) 2L72 4F RTA16WE 19950303004761995030300476NM 1995 3 3 PCAA9500190 119950130A3350 EEL COVER DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A PCAAK NONE O OTHER ININSP/MAINT 1 EA13821EX 173 PLASTIC COVER TO EMERGENCY FLOOR LIGHTS IS COMING UP. RESECURED LIGHT COVER. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950303004771995030300477NM 1995 3 3 TAOA029507 119950210A53126960242 ANGLE BOEING727 727254 138408LNM 1183 BULKHEAD CORRODED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15913TS 20250 DURING C-CHECK, BLKHD ANGLE AT BS 1183, LBRL 26.9 AND WL 207 WAS FOUND CORRODED ON THE I/B SIDE. FABRICATED NEW TENSION ANGLE PER BAC DRAWING 69-60242 AND INSTALLED PER BAC DRAWING 65-19606. (W) 2L73 4F A3WE 19950303004781995030300478NM 1995 3 3 95FDEA00187 119950227A5320TPN7 DOUBLERS BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 AFT CARGO BAY BS 1050 RBL 3-9 WL 146. THE FRAME IS CRACKED. REMOVED DAMAGED AREAS RBL 3-9. FABRICATED DOUBLER AND TWO FILLERS AND INSTALLED PER FEDEX SRM 51-40-3 AT STA 1050. 2L73 4F A3WE 19950303004791995030300479NM 1995 3 3 95FDEA00188 119950227A5320405469 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK FOUND IN STR CLIP BS 440 STR 16L. REMOVED STR CLIP AT BS 440 STR 16L THEN INSTALLED A STR CLIP. 2L73 4F A3WE 19950303004801995030300480NM 1995 3 3 95FDEA00189 119950228A53117075T6 FRAME BOEING727 72722 1384002NM BS 520 DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 520 BELOW STR 9R. ACCOMPLISHED FRAME REPAIR AT BS 520, STR 9R IAW PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950303004811995030300481NM 1995 3 3 95FDEA00190 119950228A53117075T6 FRAME BOEING727 72722 1384002NM BS 540 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R. REMOVED MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R AND REPAIRED IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19950303004821995030300482NM 1995 3 3 95FDEA00191 119950227A5347MM139622NPN SEAT TRACK BOEING727 72722 1384002NM BS 600-650 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION FOUND ON SEAT TRACK BS 600-650 BL 0 WL 208. REMOVED CORRODED SEAT TRACK, INSTALLED FABRICATED SEAT TRACK BS 600-650 BL 0 WL 208 IAW FEDEX SRM 53-10-5 SEAT TRACK EXTRUSION REPAIR. 2L73 4F A3WE 19950303004831995030300483NM 1995 3 3 95FDEA00192 119950228A53117075T6 FRAME BOEING727 72722 1384002NM BS 660 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE FOUND ON FRAME BS 660 BETWEEN STR 8 AND 9L WL 271. ACCOMPLISHED FRAME REPAIR BS 660 BETWEEN STR 8 AND 9L WL 271 PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950303004841995030300484NM 1995 3 3 95FDEA00193 119950228A53207075T6180 VERTCAL BEAM BOEING727 72727C 138400JNM BS 1178 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04145FE 19109 WHILE WORKING EO 7-5310-7-23550 FOUND EXTRA HOLE DRILLED IN VERTICAL BEAM AT RBL 46 WL 243 BS 1178. BLENDED DAMAGE AT RBL 46 WL 243 BS 1178. SUBMIT TO ENGINEERING FABRICATED REPAIR PARTS IAW FEDEX SRM 51-40-4 AND 53-10-2. INSTALLED WET WITH SEALANT AND INSTALLED FASTENERS. 2L73 4F A3WE 19950303004851995030300485NM 1995 3 3 95FDEA00195 119950225A53117075T6 FRAME BOEING727 72722 1384002NM BS 680 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 GOUGE ON FRAME AT BS 680 STR 14L. REMOVED DAMAGED AREA, REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950303004861995030300486NM 1995 3 3 95FDEA00196 119950301A21317909601 PRESS CONTROLLER BOEING727 727232 1384082NM E/E COMPT FAILED A FDEAA UNSCHED LANDING O OTHER CRCRUISE 1 SO04498FE 20867 LOSS OF PRESSURIZATION AT FL 310. UNABLE TO MAINTAIN CABIN PRESS IN AUTO, MANUAL, OR STANDBY MODE. REMOVED AND REPLACED CABIN PRESS CONTROLLER PER MM 21-31-0. CABIN PRESSURE FUNCTION TEST NORMAL PER JRH 7-23. 2L73 4F A3WE 19950303004871995030300487WP 1995 3 3 ABXA9500120 119950227A304030631 SENSOR DOUG DC8 DC863 302198AWP CAPT WINDOW DIRTY A ABXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23821AX 46116 AT TOP OF DESCENT, AFTER ANTI-FOG C/B WAS CLOSED, A STRONG ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT. NO SMOKE WAS DETECTED. C/B WAS OPENED AND SMELL DISAPPEARED. DEFERRED IAW DC-8 MEL 30-5B.DI NR 821184. DEN: CLEARED. FOUND CAPTAIN'S CLEARVIEW WINDOW WARMER THAN OTHERS. CLEANED SENSOR AND INSTALLED HEAT SINK COMPOUND. SYSTEM OPS CHECKED GOOD IAW DC-8 MM CH 30. 2L74 4F 4A25 19950303004881995030300488WP 1995 3 3 ABXA9500121 119950228A56105644324502 RETAINER DOUG DC9 DC932 3022066WP FS 120 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 56-11 REV 3, FOUND THE RIGHT CLEARVIEW WINDOW FRAME CRACKED IN THE UPPER AFT CORNER. REPLACED DOUBLER IAW DC-9 SRM 56-01 AND ABX REA D956-13036-SB. 2L72 4F A6WE 19950303004891995030300489EU 1995 3 3 QXEA9500060 119950227A4900 APU FOKKERF28 F28MK1000 4990808EU CABIN ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09469US 11096 PDX - STRONG OIL SMELL IN COCKPIT AND CABIN WHEN USING APU. NO VISIBLE SMOKE. CLEARS UP AFTER APU SHUT DOWN. PLACED APU ON MEL. 2L72 4F RTA20EU 19950303004901995030300490EU 1995 3 3 95ZZZX976 119950211A5610NP1588011 WINDSHIELD AEROSPATR42 ATR42300 8680920EU LT FWD CRACKED A NVEAAB UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO03242AT 242 PBI - STA 5681 - EN ROUTE FROM JAX TO MIA AT CRUISE FLIGHT, THE CAPTAIN'S FWD WINDSHIELD HEAT SHORTED INTERNALLY AND ARCED. SOON AFTER, THE OUTER PANE CRACKED RESEMBLING A SPIDER WEB. CAPTAIN'S VISIBILITY WAS NEAR ZERO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PBI WITHOUT INCIDENT. C/A - REPLACED CAPT'S FWD W/S. 2H72 4T RTA53EU 19950303004911995030300491NE 1995 3 3 95ZZZX977 219950204A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FLAMED OUT A NVEAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SO03211NE 340B211 785314 BNA - FLT 4562 - RIGHT ENGINE FLAMED-OUT ON APPROACH TO BNA. THE CREW WAS ABLE TO RESTART ENGINE AND LANDED SAFELY. COULD NOT DUPLICATE. VISUAL CHECKS AND ENGINE RUNS REVEALED NOTHING. ACFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950303004921995030300492NM 1995 3 3 95ZZZX978 119950210A326066191631 UPLOCK SWITCH BOEING727 727155C 138404ZNM LT MLG OUT OF ADJUST A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01715DH 19618 DURING GEAR RETRACTION, LT MLG GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR DOWN. IAW AOM ALTERNATE OPERATION. PERFORMED AIR TURNBACK, LANDED WITOUT INCIDENT. ADJUSTED UPLOCK SWITCH LINKAGE. IAW B727M/M 32-61-21. OPS CHECKS NORMAL. 2L73 4F A3WE 19950303004931995030300493NM 1995 3 3 95ZZZX979 119950209A3260H1010261 DNLOCK SWITCH BOEING727 727155C 138404ZNM LT MLG MALFUNCTIONED A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01715DH 19618 DURING INITIAL GEAR EXTENSION, GREEN LMG DOWNLOCK LIGHT DID NOT ILLUMINATE WITH RED UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE OPERATION, CH 5.144, PAGE 5, SUCCESSFULLY. DURING BOTH CYCLES, THE S/O DOOR ANNUNCIATOR LIGHTS SEQUENCED NORMALLY. TESTED UPLOCK AND DOWNLOCK SWITCHES IAW B MM 32-61-21, PAGES 501 AND 502. OPS CHECKS GOOD. 2L73 4F A3WE 19950303004941995030300494EU 1995 3 3 AALA950176 119950202A5322 SHEAR TIE FOKKERF28 F28MK0100 4990807EU FS 28026 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071415K6112 11385 SHEAR TIE CRACKED AT OBLIQUE FRAME 32-2, BETWEEN STR 54 - STR 55. REMOVED DAMAGED SHEAR TIE. MANUFACTURED AND INSTALLED NEW SHEAR TIE ANGLE PER F-100 SRM 53-00-02, REPAIR NR 2. CYCLES, 5,215. (X) 2L72 4F RT 19950303004951995030300495EU 1995 3 3 AALA950180 119950202A5322 SHEAR TIE FOKKERF28 F28MK0100 4990807EU AFT FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071415K6112 11385 SHEAR TIE CRACKED, TOP, LEFT OF CENTER ON 2ND ANGLED OBLIQUE FRAME. CUT OUT DAMAGE, MANUFACTURED DOUBLER, DRILLED AND INSTALLED PER SRM 53-00-02, REPAIR NR 2. CYCLES 5,215. (X) 2L72 4F RT 19950303004961995030300496EU 1995 3 3 AALA950184 119950202A5320 SHEAR TIE FOKKERF28 F28MK0100 4990807EU AFT FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071415K6112 11385 SHEAR TIE CRACKED, TOP LEFT OF CENTER ON 4TH ANGLED OBLIQUE FRAME. CUT OUT DAMAGE, MANUFACTURED DOUBLER, DRILLED AND INSTALLED PER SRM 53-00-02, REPAIR 2. CYCLES 5,215. (X) 2L72 4F RT 19950303004971995030300497EU 1995 3 3 AALA950188 119950202A5322 SHEAR TIE FOKKERF28 F28MK0100 4990807EU FS 30244 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071415K6112 11385 SHEAR TIES CRACKED BETWEEN STR 36 AND STR 37, AT OBLIQUE FRAME 58.5-2, STA 30.244. INSTALLED REPAIR ANGLES PER SRM 53-00-02, PART 2, P. 201-203. CYCLES 5,215. (X) 2L72 4F RT 19950303004981995030300498WP 1995 3 3 CAL950080 119950130A2612AUL71221 FIRE LOOP DOUG DC10 DC1030 3023501WP NR 1 ENGINE INOPERATIVE A CALAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SW0976073 46940 HNL - FLT 0906 - THE NR 1 ENGINE FIRE WARNING 'B' LOOP LIGHT BEGAN TO FLICKER ON AND OFF AND EVENTUALLY ILLUMINATED STEADILY WHILE ON DESCENT INTO HNL. THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND THE PYLON FORWARD 'B' LOOP AT FAULT. THE PYLON FORWARD 'B' LOOP WAS REMOVED AND REPLACED. IN ADDITION, THE PYLON AFT LOOP A AND B ASSEMBLY WAS REPLACED. OPERATION OF THE 'B' FIRE DETECTION LOOP CHECKED GOOD. (X) 2L73 4F A22WE 19950303004991995030300499EU 1995 3 3 CAL950083 119950131A3213 AXLE AIRBUS300 A300B4103 3930104EU LT MLG DAMAGED A CALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW0929981115651115 87 FLT NR 0117 - EWR - THE AIRCRAFT WAS RETURNED TO THE GATE AFTER THE NR 1 MLG BRAKE LOCKED UP. THE AIRCRAFT WAS TAKEN OUT OF SERVICE. INITIAL INSPECTION FOUND THE LEFT MLG FORWARD AXLE DAMAGED. S/D - INVESTIGATION REVEALED THAT DAMAGE TO THE BRAKE WAS A SECONDARY FAILURE DUE TO EXCESSIVE HEAT. PROBABLE CAUSE OF THE EXCESSIVE HEAT WAS ATTRIBUTED TO THE WHEEL BEARING RETAINING RING BECOMING ENTANGLED IN THE BRAKE FAN, WHICH KEPT THE FAN FROM ROTATING TO COOL THE BRAKE. THE ALLIED SIGNAL BRAKE ASSEMBLY AFFECTED WAS P/N 2606802-5, S/N B0968. (W) 2L72 4F A35EU 19950303005001995030300500EU 1995 3 3 CAL950084 119950202A2910SC663100332 HYD LINE AIRBUS300 A300B4203 3930306EU LT MLG WW LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0915967 121 FLL - FLT 0164 - THE AIRCRAFT LOST GREEN SYSTEM HYDRAULIC FLUID QUANTITY AFTER TAKEOFF FROM FLL. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC LOW LEVEL LIGHT AND LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO FLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE ON GEAR ACTUATOR IN LT WHEELWELL LEAKING. THE HYDRAULIC LINE WAS REPLACED. OPERATIONAL AND LEAK CHECKS AFTER HYDRAULIC SYSTEM SERVICING WERE GOOD. (X) 2L72 4F A35EU 19950303005011995030300501WP 1995 3 3 CAL950086 119950204A2612AUL7128501 FIRE LOOP DOUG DC10 DC1010 3022110WP NR 3 ENGINE CRUSHED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SW0968046 47800 GUM - FLT 0973 - THE NR 3 ENGINE 'B' LOOP FIRE WARNING LIGHT ILLUMINATED WHILE IN-FLIGHT. THE CREW WENT TO 'A' LOOP AND TEST FAILED ON 'A'. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE NR 3 ENGINE HAD A HISTORY OF FALSE FIRE WARNINGS. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGINE AFT PYLON 'B' FIRE LOOP DETECTOR WAS FOUND CRUSHED. THE DETECTOR WAS REPLACED. IN ADDITION, THE LOWER FORWARD 'A' LOOP WAS FOUND BENT. THE 'A' LOOP WAS SECURED IN PROPER POSITION AND CHAFED WIRES AT UPPER AFT SECTION WERE REPAIRED. AN OPERATIONAL TEST OF BOTH LOOPS CHECKED NORMAL. (X) 2L73 4F A22WE 19950303005021995030300502EU 1995 3 3 CAL950087 119950205A3230C23005305 PITCH DAMPER AIRBUS300 A300B4103 3930104EU LT MLG INOPERATIVE A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW09729909111 259 EWR - FLT 0288 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF USING EITHER SYSTEMS 1 OR 2. THE AIRCRAFT WAS RETURNED TO WHERE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT PITCH DAMPER INDICATOR TRIPPED. THE LT MAIN GEAR PITCH DAMPER WAS REMOVED AND REPLACED. THE LT MAIN GEAR PITCH DAMPER WAS SERVICED IAW MM 12-12-32 AND OPERATION CHECKED GOOD. (X) 2L72 4F A35EU 19950303005031995030300503NM 1995 3 3 CAL950091 119950201A5320 INTERCOSTAL BOEING737 737217 1384464NM BS 508 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT BS 508 BETWEEN STR 28L AND STR 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950303005041995030300504NM 1995 3 3 CAL950092 119950201A5220 FRAME BOEING737 737217 1384464NM PAX DR CUTOUT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A .25 INCH CRACK IN FORWARD ENTRY DOOR FORWARD FRAME CUT OUT AT UPPER HINGE ARM. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 51-10-2, AND SRM 51-30-2. (X) 2L72 4F A16WE 19950303005051995030300505NM 1995 3 3 CAL950093 119950201A5315 FLOORBEAM BOEING737 737217 1384464NM FS 639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN STA 639 LT SIDE FLOORBEAM WEB CABLE CUTOUT. THE FLOORBEAM WEB WAS REPAIRED IAW BOEING DRAWING 65C25211. (X) 2L72 4F A16WE 19950303005061995030300506NM 1995 3 3 CAL950094 119950201A5321 FLOOR PANEL BOEING737 737217 1384464NM FS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND THE NR 6 FLOOR PANEL SUPPORT CORRODED AT STA 312. THE PANEL SUPPORT WAS REPAIRED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950303005071995030300507NM 1995 3 3 CAL950095 119950201A5320 CHORD BOEING737 737217 1384464NM FS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A .50 INCH CRACK IN RT STA 727 OUTBOARD CHORD AT STR 18A. THE CRACKED CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW BOEING DRAWING 65C33722. (X) 2L72 4F A16WE 19950303005081995030300508NM 1995 3 3 CAL950096 119950201A5313 STRINGER BOEING737 737217 1384464NM FS 685 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN STR 5R AT STA 685. THE CRACK WAS STOP DRILLED AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-10-3. (X) 2L72 4F A16WE 19950303005091995030300509NM 1995 3 3 CAL950097 119950201A5311 FRAME BOEING737 737217 1384464NM FS 578 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A .50 INCH CRACK IN STA 578 MAIN CABIN FRAME AT STR 16 - STR 17L. THE FRAME WAS REPAIRED IAW SRM 51-40-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950303005101995030300510NM 1995 3 3 CAL950098 119950201A5311 BELT FRAME BOEING737 737217 1384464NM BS 420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 2 INCH CRACK IN BELT FRAME AT BS 420, STR 22L. THE CRACK WAS REPAIRED IAW BOEING DRAWING 65C25113. (X) 2L72 4F A16WE 19950303005111995030300511NM 1995 3 3 CAL950099 119950201A5311 FRAME BOEING737 737217 1384464NM BS 500A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500A BETWEEN STR 21L AND STR 20L. THE CRACKED FRAME WAS CUT OUT IAW BOEING DRAWING 65C225113 AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X) 2L72 4F A16WE 19950303005121995030300512NM 1995 3 3 CAL950100 119950201A5311 FRAME BOEING737 737217 1384464NM BS 480 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A .50 INCH CRACK IN BELT FRAME AT BS 480 BETWEEN STR 21L AND STR 20L. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-30-0. (X) 2L72 4F A16WE 19950303005131995030300513EU 1995 3 3 CAL950102 119950208A2910 HYD LINE AIRBUS300 A300B4103 3930104EU GREEN HYD SYST LOOSE A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0929981 87 EWR - FLT 0261 - THE GREEN SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO 1.3 GALLONS WHILE IN-FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF WARNING LIGHT. THE HYDRAULIC LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FLAP INSTRUMENTATION UNIT TIMING VALVE HYDRAULIC LINE LOOSE AT THE B-NUT. THE B-NUT WAS TIGHTENED AND THE GREEN HYDRAULIC SYSTEM WAS SERVICED. THE NR 2 ENGINE WAS RUN AND ALL FLIGHT CONTROLS WERE CYCLED WITH NO LEAKS NOTED. (X) 2L72 4F A35EU 19950303005141995030300514NM 1995 3 3 CAL950103 119950208A5750 TOGGLES BOEING737 7373T0 1384582NM LT TE FLAP BROKEN A CALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0960312 23363 DEN - FLT 1431 - THREE TO FOUR UNITS OF RIGHT WING DOWN AILERON WERE REQUIRED TO KEEP WINGS LEVEL WITH FLAPS SET AT 15-25 DEGREES ON APPROACH TO DEN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LT OUTBOARD FLAP TOGGLES BROKEN. BOTH TOGGLES WERE REPLACED AND FLAP OPERATION CHECKED GOOD. (X) 2L72 4F RTA16WE 19950303005151995030300515NM 1995 3 3 CAL950106 119950201A5311 FRAME BOEING737 737217 1384464NM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT BS 500 BETWEEN STR 21L AND STR 20L. THE CRACKED BELT FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950303005161995030300516NM 1995 3 3 CAL950107 119950201A5320 INTERCOSTAL BOEING737 737217 1384464NM E & E BAY CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL BEHIND AFT FORMER IN E AND E BAY. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-30-2. (X) 2L72 4F A16WE 19950303005171995030300517NM 1995 3 3 CAL950108 119950201A5512 SKIN BOEING737 737217 1384464NM LT HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND A .50 INCH CRACK IN THE LT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN AT STA 66. THE CRACK WAS STOP DRILLED AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 55-10-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950303005181995030300518NM 1995 3 3 CAL950109 119950201A5330 SKIN BOEING737 737217 1384464NM FS 727 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND CORROSION ON RT EXTERNAL SKIN AND DOUBLER AT STA 727 BETWEEN STR 17R AND STR 18R. THE CORROSION WAS REMOVED AND A DOUBLER IN INSTALLED IAW EC 5330-02227. (X) 2L72 4F A16WE 19950303005191995030300519NM 1995 3 3 CAL950110 119950201A5330 SKIN BOEING737 737217 1384464NM BS 188-251.6 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES BETWEEN BS 188 AND BS 251.6 ON THE LT SIDE OF FUSELAGE. ALL CRACKS WERE APPROXIMTELY .25 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X) 2L72 4F A16WE 19950303005201995030300520NM 1995 3 3 CAL950111 119950201A5330 SKIN BOEING737 737217 1384464NM BS 188-251.6 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423371921 19887 GSO - INSPECTION FOUND SKIN CRACKED AT SEVERAL FASTENER HOLES ON RT SIDE OF FUSELAGE BETWEEN BS 188 AND BS 251.6. ALL CRACKS WERE APPROXIMATELY 1 INCH LONG. THE CRACKS WERE REPAIRED IAW EA 5310-01188, PART 3. (X) 2L72 4F A16WE 19950303005211995030300521CE 1995 3 3 HERA9502 119950117A56101143840202 WINDSHIELD BEECH 1900 1900C 1154161CE RT FORWARD CRACKED A HERAO OTHER O OTHER CRCRUISE 1 AL03554567922 UC165 BET - FLT 1495 - EN ROUTE AT FL220, THE OUTSIDE LAYER OF THE RT FORWARD WINDSHIELD CRACKED. THE OUTSIDE AIR TEMPERATURE WAS MINUS 34 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS ON AT THE TIME. THE AIRCRAFT CONTINUED ON TO BET AND A LANDING WAS MADE WITHOUT INCIDENCE. MIANTENANCE REMOVED AND REPLACED THE CRACKED WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T RTA24CE 19950303005221995030300522NM 1995 3 3 MRKA959 119950113A3350862101401 EEL BATTERY PACK BOEING737 7372T4C 1384501NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03675MA 23065 FLOOR PROXIMITY LIGHT AT RIGHT OVERWING EXIT FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS OKAY. (X) 2L72 4F RTA16WE 19950303005231995030300523EA 1995 3 3 VTZA95050 119950204A2930 WARNING LIGHT DHAV DHC8 DHC8311 1386006EA NR 2 HYD SYSTEM ILLUMINATED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27430AW 279 IAD/JFK - FLT 6485 - DURING CLIMB AT 1500 HRS ON 2-4-95, THE NR 2 HYDRAULIC CAUTION LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 05245 IAW MEL 29-3 ON THE HYDRAULIC WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 05245 ON 2-8-95 BY BLEEDING THE NR 2 HYDRAULIC SYSTEM. GROUND AND AIR OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA13NM 19950303005241995030300524EU 1995 3 3 VTZA95053 119950208A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 EA27477UE 890 IAD/AVP - FLT 6592 - DURING CLIMB-OUT AT 0910 ON 2-8-95, LT STARTER/GENERATOR FELL OFF LINE AND WOULD NOT RESET. AIRCRAFT RETURNED TO IAD IWTH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950303005251995030300525EU 1995 3 3 VTZA95054 119950210A524014153133409 DOOR JETAIRJETSTMJETSTM4101 1500501EU LAV SERVICE MISSING A VTZAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 EA27315UE 41033 IAD/PVD - FLT 6219 - DURING PRE-FLIGHT AT 2200 HOURS ON 2-6-95, CREW NOTICED THE LAV SERVICE DOOR MISSING. MAINTENANCE OPENED DMI NR 17216 IAW CDL 52-40. MAINTENANCE LATER CLEARED DMI NR 17216 BY REPLACING THE LAV SERVICE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950303005261995030300526EU 1995 3 3 VTZA95056 119950211A243523095002 STARTER/GEN JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILED A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 EA27311UE 41029 PWM/IAD - FLT 6500 - DURING CRUISE ON 2-11-95 AT 1030 HRS, THE RT START/GENERATOR CAPTION ILLUMINATED IN-FLIGHT, APPROXMATELY 30 MINUTES LATER THE RT ENGINE BEGAN TO VIBRATE. CREW SHUT DOWN ENGINE IN-FLIGHT AND DECLARED AN EMERGENCY. FLIGHT DIVERTED TO PVD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT START/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950303005271995030300527 1995 3 3 VTZA95057 319950211A61401417701 BETA PRESS SW JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE DIRTY A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA27311UE 41029 PVD/IAD - FLT 6943 - DURING TAKEOFF ROLL, AT 2115 HRS ON 2-11-95, THE RT ENGINE RED BETA LIGHT ILLUMINATED AFTER ROTATION. THE CREW SECURED THE ENGINE IN-FLIGHT AND RETURNED TO PVD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE ZONAL CANNON PLUG AND THE BETA PRESSURE SWITCH. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950303005281995030300528EU 1995 3 3 VTZA95058 119950214A77228974696 CONNECTOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE LOOSE A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27483UE 898 IAD/MDT - FLT 6496 - DURING CRUISE AT 1420 HRS ON 2-14-95, RT ENGINE EGT GAUGE FAILED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE BACKSHELL TO THE SOFT HARNESS, PN 8974696, CANNON PLUG LOOSE. TIGHTENED BACKSHELL AND OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950303005291995030300529EU 1995 3 3 VTZA95059 119950216A32301849E UPLOCK ASSY BAG JETSTMJETSTM3201 1500217EU NLG FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27370MT 800 LYN/RIC - FLT 6908 - DURING APPROACH ON 2-16-95 AT 0630 HRS, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. CREW SAID GEAR REMAINED IN WHEELWELL. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO LYH. LYH MAINTENANCE REPLACED THE UPLOCK ASSY, OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950303005311995030300531WP 1995 3 3 9503181146 119950125A5313AFA71601 LONGERON DOUG DC10 DC1040 3023508WP FS 1581 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE LONGERON 44L, FS 1581. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-96601. 2L73 4F A22WE 19950303005321995030300532WP 1995 3 3 9503191162 119950119A5330ABA70493 SKIN DOUG DC10 DC1040 3023508WP FS 275-343 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01162US 46771 DURING PERIODIC CHECK, DAMAGE WAS FOUND ON THE LEFT FUSELAGE NOSE SKIN AT FS 275 - 343, Z-2.90 TO Z-20.15. INSTALLED REPAIR DOUBLERS PER EA 11-96599. 2L73 4F A22WE 19950303005331995030300533NM 1995 3 3 9503206614 119950223A5330 SKIN BOEING747 747251B 1384892NM FS 1964 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, THE LOWER EXTERIOR SKIN AT FS 1964, STR 42L WAS FOUND CORRODED. REMOVED DAMAGED AREA AND INSTALLED STRINGER SPLICE AND SKIN PER EA 66-82020. 2L74 4F A20WE 19950303005341995030300534WP 1995 3 3 9503211149 119950223A7603 PWR LEVER CABLE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 2 ENGINE LACK OF LUBE A NWAAE ENGINE SHUTDOWN O OTHER LDLANDING 1 GL01148US 46758 686112 DURING LANDING (AMS), THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE POWER LEVER CABLE WAS CLEANED, LUBRICATED, AND OPERATION CHECKED OK. 2L73 4F4 F A22WE E20EA 19950303005351995030300535WP 1995 3 3 9503221149 119950224A7603 POWER CABLES DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN O OTHER LDLANDING 1 GL01149US 46758 686112 DURING LANDING THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE THROTTLE BOOT WAS CLEANED, DRIED WITH ALCOHOL, AND THE OPERATION CHECKED OK. LATER AT MSP, THE LONG AND SHORT ENGINE PUSH/PULL CABLES WERE REPLACED AND THE AFT PRESSURE BULKHEAD SEALS WERE CLEANED AND RELUBED. 2L73 4F4 F A22WE E20EA 19950303005361995030300536WP 1995 3 3 9503239961 119950227A3231 DR STOP CABLE DOUG DC9 DC931 3022065WP NLG BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01924RW 47185 A LOUD "BANG" FOLLOWED BY A STRONG VIBRATION OCCURRED ON ROTATION DURING TAKEOFF. FLIGHT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOOR STOP CABLE BROKEN. DEFERRED CABLE ASSEMBLY PER MEL 32-7 AND CHECKED FOR DOOR SECURITY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950303005371995030300537NM 1995 3 3 9503245507 119950227A7603 CIRCUIT BREAKER BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR1 THRUST LEVERTRIPPED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01507US 23196 716455 DURING TAKEOFF AS TAKEOFF POWER WAS APPLIED, THE NR 1 THRUST LEVER WAS UNABLE TO REACH FULL TAKEOFF. THE TAKEOFF WAS ABORTED. THE LEFT REVERSER INTERLOCK CIRCUIT BREAKER WAS RESET AND THE SYSTEM CHECKED OK. 2L72 4F4 FRTA2NM E17NE 19950303005381995030300538WP 1995 3 3 9503259990 119950228A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE FORWARD CARGO DOOR HORIZONTAL ANGLE BRACE FITTING. REPLACED FITTING PER SRM 51-10-2 AND 51-30-3. 2L72 4F A6WE 19950303005391995030300539WP 1995 3 3 9503269758 119950228A5312 BULKHEAD DOUG DC9 DC941 302207NWP FS 729 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01758NW 47286 DURING LINE CHECK, FOUND CORROSION ON THE CANTED BULKHEAD FS 729 AT LBL 40 BETWEEN THE LOWER CHORD AND WEB. REPAIRED PER EA 97-096744. 2L72 4F A6WE 19950303005401995030300540EU 1995 3 3 9503273226 119950226A2750 RETRACT MECH AIRBUS320 A320211 3930320EU TE FLAPS MALFUNCTIONED A ANWAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 GL01326US 282 DURING APPROACH INTO SAN, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN FLAP 3 WAS SELECTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DESCREPANCIES. 2L72 4F RTA28NM 19950303005411995030300541WP 1995 3 3 9503289857 119950302A5610 WINDOW SEAL DOUG DC9 DC951 3022051WP LT EYEBROW LOOSE A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01766NC 47739 DURING CLIMB JAX-MEM THE FLIGHT CREW HEARD A LOUD FLAPPING NOISE NEAR THE CAPTAIN'S EYEBROW WINDOW. MAINTENANCE CONTROL WAS NOTIFIED AND THE AIRCRAFT RETURNED TO JAX WITHOUT FURTHER INCIDENT. FOUND LOOSE SEALANT AT THE AFT SIDE OF THE CAPTAIN'S EYEBROW WINDOW. TRIMMED SEALANT AND DEFERRED REPAIR. INSPECTED THE NR 1 ENGINE INLET. CHECKED OK. 2L72 4F A6WE 19950303005421995030300542WP 1995 3 3 95UALD10022 119950301A2721 CABLES DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL RUDDER TRIM LACK OF LUBE A AUALAO OTHER O OTHER DEDESCENT 1 WP291833U 47965 RUDDER AND RUDDER TRIM FROZE ON DESCENT. RUDDER WAS BROKEN LOOSE WITH HEAVY PRESSURE AND TRIM BECAME FREE DURING TAXIING IN HEAVY RAIN IN HNL. REPLACE RUDDER TRIM PUSH\PULL CABLE. INSPECTED AND LUBED AFT RUDDER QUADRANTS. CHECKED RUDDER PER MMOV. 2L73 4F4 F A22WE E23EA 19950303005431995030300543WP 1995 3 3 95UALD10023 119950301A4900 APU DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL APU BAY MALFUNCTIONED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291849U 46939 PUNGENT ODOR (SMOKE) IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. REPLACED APU AND ACCOMPLISHED BURNOUT. ALSO REPLACED APU FORWARD MOUNT ACCOUNT RUBBER INSULATOR SPLIT AND HANGING OUT OF MOUNT. 2L73 4F4 F A22WE E23EA 19950303005441995030300544SO 1995 3 3 COM11803 119950228A3230922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01267CA 120259 LANDING GEAR WILL NOT RETRACT. REPLACED DEFECTIVE PROXIMITY SENSOR ON LT MLG UPLOCK. 2L72 4T RTA31SO 19950303005451995030300545SO 1995 3 3 COM11804 119950228A2731ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01463CA1173 1173 120267 TAKEOFF TRIM WARNING, TRIM WAS CONFIRMED TO BE IN THE TAKEOFF RANGE. REPLACED THE ELEVATOR TRIM PROXIMITY SENSORS. 2L72 4T RTA31SO 19950303005461995030300546NE 1995 3 3 COM11805 219950226A73103035729 FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE SUSPECT A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01200CD 120200 LEFT ENGINE FUEL FILTER WARNING CAME ON DURING FLIGHT. THE PROBLEMS CANNOT BE DUPLICATED AND VISUAL INSPECTION OF FILTERS INDICATED NO UNUSUAL DEBRIS. REPLACED THE FUEL FILTERS AND FUEL PRESSURE SWITCHES FOR TROUBLESHOOTING. 2L72 4T4 TRTA31SO E20NE 19950303005471995030300547SW 1995 3 3 COM20357 119950228A272027420519011 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER BENT A COMAK NONE O OTHER ININSP/MAINT 1 SO01704C 288 AC704 RUDDER TORQUE TUBE WAS FOUND TO BE BENT. THE TORQUE TUBE WAS REPLACED WITH NEW PART (SUBSTITUTE PN 27-42051-8037) PER FAIRCHILD MAINTENANCE MANUAL 27-20-04, PG. 201-204 AND AEROTECH REPORT NR 1210, REV. IR, DATED 9-21-92. 1L72 4T A8SW 19950303005481995030300548EA 1995 3 3 COM60432 119950228A301014463101 DUCT ASSY CNDAIRCL600 CL6002B19 EA LT OUTBD WING CRACKED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01912CA 7011 ANTI-ICE DUCT WARNING MESSAGE WHEN WING A/I SELECTED ON. REPLACED THE LEFT WING OUTBD DEICE DUCT ASSY. 2L72 4F RTA21EA 19950303005491995030300549NM 1995 3 3 SWAA950186 119950224A33501000679 EEL BATTERY BOEING737 7372T4 1384492NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07722WN 22698 FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT AND BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950303005501995030300550NM 1995 3 3 SWAA950187 119950226A335020131A EEL BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING AND RIGHT AFT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950303005511995030300551NM 1995 3 3 SWAA950188 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 480 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0724SW 20925 DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT FUSELAGE SKIN LAP, BS 480, S10L, AT BS 500B+10, S14L AND AT BS 530, S10R. REPAIRED PER SWA RA 1-253-1251 AND SI 8615-53. 2L72 4F A16WE 19950303005521995030300552NM 1995 3 3 SWAA950189 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0724SW 20925 DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION NEAR SEVERAL FASTENERS IN PRESSURE WEB AT I/B SIDE OF STRAP, BS 178, LBL 5.7, FROM WL 205 TO 186. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950303005531995030300553NM 1995 3 3 SWAA950190 119950228A5312 BLKHD ANGLE BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0724SW 20925 DURING SCHEDULED A1 CHECK, FOUND CRACK INDICATION AT BS 178 PRESSURE BULKHEAD VERTICAL T-ANGLE AT LBL 5.7 AT WL 184, IN THE I/B AND O/B FLANGE RADIUS. REPAIRED PER SWA RA 1-253-1250. 2L72 4F A16WE 19950303005541995030300554NM 1995 3 3 SWAA950191 119950228A5330 SKIN BOEING737 7373H4 1384600NM SERV DOOR CUTOUTCRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07315SW 23339 DURING SCHEDULED B2 CHECK, FOUND FORWARD SERVICE DOOR CUTOUT CRACKED 1 INCH AT AFT LOWER RADIUS. REPAIRED PER SWA RA 1-353-1252. 2L72 4F RTA16WE 19950303005551995030300555NM 1995 3 3 SWAA950192 119950228A5210 SKIN BOEING737 7373H4 1384600NM AFT ENTRY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07315SW 23339 DURING SCHEDULED B2 CHECK, FOUND AFT ENTRY DOOR UPPER RADIUS HINGE CUTOUT CRACKED .3750 INCH. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950303005561995030300556NM 1995 3 3 SWAA950193 119950228A5320 STRAP BOEING737 7373A4 1384585NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07674AA 23252 DURING SCHEDULED C1 CHECK, FOUND TIE STRAP CRACKED AT BS 328, LOWER E & E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950303005571995030300557NM 1995 3 3 UPS202537 119950301A5311 FRAME BOEING727 727173C 1384059NM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 600 FRAME, STR 22-23L. REPAIRED FRAME PER SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950303005581995030300558NM 1995 3 3 UPS202538 119950301A5311 FRAME BOEING727 727173C 1384059NM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND FRAME CORRODED AT BS 640, STR 20L, 22L, 23L, 25L. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 19950303005591995030300559NM 1995 3 3 UPS202539 119950301A5347 SEAT TRACK BOEING727 727173C 1384059NM BS 858 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK AT BS 858, RBL 1, WL 208. REPLACED SEAT TRACK PER SRM 51-30-2. 2L73 4F A3WE 19950303005601995030300560NM 1995 3 3 UPS202540 119950301A5347 SEAT TRACK BOEING727 727173C 1384059NM FS 848-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION IN WELL OF SEAT TRACK ON EXPANSION LINK AT STA 848-870. REPLACED SEAT TRACK PER SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950303005611995030300561NM 1995 3 3 UPS202542 119950301A5313 STRINGER BOEING727 727173C 1384059NM FS 294.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CRACKS IN STRINGERS 14L, 15L, 16L AT STA 294.5. REPAIRED PER UPS EO B727-5310-1259F. 2L73 4F A3WE 19950303005621995030300562NM 1995 3 3 UPS202543 119950301A5320 STIFFENER BOEING727 727173C 1384059NM BS 870-880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON PRESSURE WEB STIFFENER AT RBL 45, WL 202, BS 879. REPLACED STIFFENER PER SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950303005631995030300563NM 1995 3 3 UPS202544 119950301A5313 STRINGER BOEING727 727173C 1384059NM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND STRINGER 4L CORRODED AT BS 1110. REPAIRED STRINGER PER SRM 53-10-3. 2L73 4F A3WE 19950303005641995030300564NM 1995 3 3 UPS202545 119950301A5320 EXPANSION LINK BOEING727 727173C 1384059NM BS 850-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 850-870, RBL 45, WL 207. REPLACED LINK PER SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950303005651995030300565NM 1995 3 3 UPS202546 119950301A5320 WEB BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON VERTICAL WEB AT STA 870, LBL 10-25, WL 200. REPLACED WEB PER SRM 51-20-4, 51-30-2. 2L73 4F A3WE 19950303005661995030300566NM 1995 3 3 UPS202548 119950301A5312 BLKHD STIFFENER BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CORROSION ON BS 740 BULKHEAD STIFFENER AT RBL 14. REPAIRED PER SRM 51-10-2, 51-30-2. 2L73 4F A3WE 19950303005671995030300567NM 1995 3 3 UPS202549 119950301A5313 STRINGER BOEING727 727173C 1384059NM BS 352.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE FOUND CRACK AT STA 352.5, STR 20, WL 120. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950303005681995030300568NM 1995 3 3 UPS202550 119950302A5320 STIFFENER BOEING727 727173C 1384059NM BS 294-300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE REPORTED HORIZONTAL STIFFENER CORRODED AT BS 294-300, RBL 15, WL 178. REPLACED STIFFENER PER SRM 51-30-5, 51-10-1, 51-30-1. 2L73 4F A3WE 19950303005691995030300569NM 1995 3 3 UPS202551 119950302A5312651594024 BLKHD ANGLE BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE REPORTED CORROSION ON ANGLE ON PRESSURE BULKHEAD AT BS 740, WL 170. REPLACED ANGLE AND SIDE LOAD BEAM PER SRM 51-10-1, 51-10-2, 51-20-1. 2L73 4F A3WE 19950303005701995030300570NM 1995 3 3 UPS202552 119950302A5314651628038 STIFFENER BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE REPORTED CORROSION ON VERTICAL STIFFENER CONNECTING UPPER AND LOWER KEEL BEAM AT BS 740, RBL 13, WL 163. REPLACED STIFFENER PER SRM 51-30-2. 2L73 4F A3WE 19950303005711995030300571NM 1995 3 3 UPS202553 119950302A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 870 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE REPORTED CRACK IN FLOOR BEAM AT STA 870. REPLACED FLOOR BEAM PER SRM 51-10-1. 2L73 4F A3WE 19950303005721995030300572NM 1995 3 3 UPS202554 119950302A5320 EXPANSION LINK BOEING727 727173C 1384059NM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 DURING 'D' CHECK MAINTENANCE REPORTED EXPANSION LINK CORRODED AT BS 740-760, RBL 45, WL 207. REPLACED LINK PER SRM 51-30-2, 53-10-1. 2L73 4F A3WE 19950303005731995030300573NM 1995 3 3 UPS202578 119950301A33501060091101 EEL BATTERY BOEING727 72727C 138400JNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01939UP 19532 MAINTENANCE REPORTED EMERGENCY LIGHT BATTERY LOW. REPLACED BATTERY. 2L73 4F A3WE 19950303005741995030300574NM 1995 3 3 UPS202580 119950301A3350 EEL BATTERY PACK BOEING727 72727C 138400JNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01939UP 19532 MAINTENANCE REPORTED EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS. CHECK OK. 2L73 4F A3WE 19950303005751995030300575NM 1995 3 3 UPS202581 119950228A553065175086 CHORD BOEING727 72727C 138400JNM FIN STA 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON LWR. CHORD VERT FIN STA. 1342 RT. REPLACED CHORD PER UPS EO B727-5530-4601B. 2L73 4F A3WE 19950303005761995030300576NM 1995 3 3 UPS202582 119950228A553065175086 CHORD BOEING727 72727C 138400JNM FIN STA 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON LWR. CHORD VERT FIN STA. 1342 LT. REPLACED CHORD PER UPS EO B727-5530-4601B. 2L73 4F A3WE 19950303005771995030300577NM 1995 3 3 UPS202583 119950228A553065225512 CHORD BOEING727 72727C 138400JNM FIN STA 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANEL CHORD VERT FIN STA. 1342 RT. REPLACED CHANNEL CHORD PER UPS EO B727-5530-4601B. 2L73 4F A3WE 19950303005781995030300578NM 1995 3 3 UPS202584 119950228A5330 SKIN BOEING727 72727C 138400JNM FIN STA 360 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN SKIN STA 360 STRINGER 24L. INSTALLED REPAIR PER UPS EO B727-5330-0509Q. 2L73 4F A3WE 19950303005791995030300579NM 1995 3 3 UPS202585 119950228A5720 CHORD BOEING727 72727C 138400JNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN FASTENER HOLE IN CHORD RT WING (MRR FILED OPEN). 2L73 4F A3WE 19950303005801995030300580NM 1995 3 3 UPS202586 119950228A5330 SKIN BOEING727 72727C 138400JNM BS 306 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON EXTERNAL SKIN STA 306 STRINGER 26L. INSTALLED REPAIR PER UPS EO B727-5330-0509Q. 2L73 4F A3WE 19950303005811995030300581NM 1995 3 3 UPS202587 119950228A5320 WEB BOEING727 72727C 138400JNM BS 1352 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON RING CHORD WEB STA 1352. REPAIRED PER UPS EO B727-7100-2729C. 2L73 4F A3WE 19950303005821995030300582NM 1995 3 3 UPS202588 119950228A5320 CHORD BOEING727 72727C 138400JNM BS 1352 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON RING CHORD STA 1352. REPAIRED PER UPS EO B727-7100-2729C. 2L73 4F A3WE 19950303005831995030300583NM 1995 3 3 UPS202589 119950228A5343 TRUNNION FTGS BOEING727 72727C 138400JNM NLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON NLG TRUNNION FITTINGS LT AND RT. REPAIRED PER UPS EO 53-60-1. 2L73 4F A3WE 19950303005841995030300584NM 1995 3 3 UPS202590 119950228A5753 FLAP TRACK BOEING727 72727C 138400JNM RT TE FLAPS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT INBD FLAP TRACK. REWORKED PER UPS EO B727-5740-6668. 2L73 4F A3WE 19950303005851995030300585NM 1995 3 3 UPS202591 119950228A5753 FLAP TRACK BOEING727 72727C 138400JNM LT TE FLAPS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON L INBD FLAP TRACK. REWORKED PER UPS EO B727-5740-6668. 2L73 4F A3WE 19950303005861995030300586NM 1995 3 3 UPS202592 119950228A5720 DOUBLER BOEING727 72727C 138400JNM WS 187 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON WING DOUBLER WS 187 LT. INSTALLED REPAIR PER SRM 57-10-1, 57-10-2, 51-30-00, OHM 20-10-03. 2L73 4F A3WE 19950303005871995030300587NM 1995 3 3 UPS402563 119950227A5347 SEAT TRACK BOEING747 747123F NM BS 615 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 MAINTENANCE REPORTED SEAT TRACK CORRODED BENEATH PALLET LOCK LOCATED AT RT SIDE O/B POS NR 1 CLOSEST TO CARGO DOOR IN FWD BELLY SECTION. REPLACED SEAT TRACK AS REQUIRED. 2L74 4F A20WE 19950303005881995030300588NM 1995 3 3 UPS402579 119950301A3350 EEL PANEL BOEING747 747121 1384871NM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01691UP 19641 MAINTENANCE REPORTED EMERGENCY LIGHT CONTROL PANEL SHOWS UNARMED IN ARM POSITION. REPLACED EMER EXIT LIGHT CONTROL PANEL. OPS CK NORMAL. 2L74 4F A20WE 19950303005891995030300589WP 1995 3 3 UPS802536 119950228A2930 HYD PRESS IND DOUG DC8 DC873F 302199FWP COCKPIT MALFUNCTIONED A IPXAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01806UP 46006 WHILE EN ROUTE TO TPE, PILOT NOTED PRESSURE DROP TO 1000 PSI (HYD. SYS. PRESS.) ON UPLATCH CHECK. CYCLED GEAR; PRESSURE RETURNED TO NORMAL. SYSTEM LEAK CHECKED, NO EVIDENCE OF HYD. LEAK. ACCUMULATOR PRESSURE CHECKED SATIS. HYD QTY. CHECKED, SYSTEM FULL. HYD. SYS. PRESSURE CHECKED, SATIS. 2L74 4F RT4A25 19950303005901995030300590WP 1995 3 3 UPS802562 119950227A5312 J ANGLE DOUG DC8 DC873F 302199FWP AFT PRESS BULKHDCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 MAINTENANCE REPORTED 'J' ANGLE CRACKED ON AFT PRESS BULKHEAD. REPAIRED PER UPS EO DC8-5310-6746. 2L74 4F RT4A25 19950303005911995030300591CE 1995 3 3 95ZZZX980 119950213A5540573301413 BRACKET CESSNA441 441 2076020CE RUD BAL WEIGHT CRACKED A AWTXAK NONE O OTHER ININSP/MAINT 1 NM07140MP1000 4410165 WHILE DOING PHASE 5 INSPECTION, FOUND A 5 INCH CRACK IN LT SIDE OF THE RUDDER BALANCE WEIGHT BRACKET. THE BRACKET WAS THE NEW, IMPROVED STYLE INSTALLED PER CQB86-9. SUBMITTER SUGGESTS NEW BRACKET IS TOO WIDE AND HAS TO BE SQUEEZED IN TO FIT SHAPE OF RUDDER BEFORE RIVETING. CESSNA NEEDS TO REDESIGN SIZE OF BRACKET. 1L72 3T RTA28CE 19950303005951995030300595SO 1995 3 3 95ZZZX984 119950224A792275944 VALVE PIPER PA31 PA31350 7103110SO RT THERMO VALVE CRIMP NUT LOOSE A AGSUAK NONE O OTHER ININSP/MAINT 1 WP1966883948 317405184 WHILE COMPLYING WITH LYCOMING MANDATORY SB NR 518A, THE FOLLOWING DISCREPANCIES WERE NOTED ON BOTH LEFT AND RIGHT THERMOSTATIC BYPASS VALVES. INSUFFICIENT CRIMP DEPTH ON CRIMP NUT. CRIMP NUT WAS LOOSE ON SHAFT. EXCESSIVE WEAR NOTED ON BOTH VALVE SEATS. 1L72 3O A20SO 19950303005961995030300596SO 1995 3 3 95ZZZX985 119950224A792275944 VALVE 2102160901 PIPER PA31 PA31350 7103110SO LT THERMO VALVE CRIMP NUT LOOSE A GSUAK NONE O OTHER ININSP/MAINT 1 WP1966883948 317405184 WHILE COMPLYING WITH LYCOMING MANDATORY SB 518A, THE FOLLOWING DISCREPANCIES WERE NOTED ON BOTH LEFT AND RIGHT THERMOSTATIC BYPASS VALVES. INSUFFICIENT CRIMP DEPTH ON CRIMP NUT. CRIMP NUT WAS LOOSE ON SHAFT. EXCESSIVE WEAR NOTED ON BOTH VALVE SEATS. 1L72 3O A20SO 19950310000011995031000001WP 1995 3 10 6203339962 119950301A3260 SWITCH DOUG DC9 DC931 3022065WP LT MLG DOWNLOCK MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01914RW 47362 LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION IN MSP. EXECUTED MISSED APPROACH PROCEDURES AND VISUALLY CONFIRMED THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310000061995031000006EU 1995 3 10 9503293227 119950101A71202380210505 THRUST LINKS AIRBUS320 A320211 3930320EU FWD ENG MOUNT WEAR MARKS A NWAAK NONE O OTHER ININSP/MAINT 1 GL01327NW 297 DURING OVERNIGHT MAINTENANCE, THE NR 1 ENGINE INBOARD AND OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.003 INCH TO 0.005 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-095306 AND EA 32-095307. 2L72 4F RTA28NM 19950310000071995031000007EU 1995 3 10 9503303202 119950102A71202380210505 THRUST LINKS AIRBUS320 A320211 3930320EU FWD ENG MOUNT WEAR MARKS A NWAAK NONE O OTHER ININSP/MAINT 1 GL01302US 32 DURING OVERNIGHT MAINTENANCE, THE NR 1 AND NR 2 ENGINES INBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS DID NOT EXCEED 0.002 INCH DEEP. REPAIRS ACCOMPLISHED PER NEA EA 32-095308 AND EA 32-095309. 2L72 4F RTA28NM 19950310000081995031000008EU 1995 3 10 9503313232 119950112A71202380210505 THRUST LINK AIRBUS320 A320211 3930320EU FWD ENG MOUNT WEAR MARKS A NWAAK NONE O OTHER ININSP/MAINT 1 GL01332NW 319 DURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE FORWARD INBOARD THRUST LINK WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREAS AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.001 INCH TO 0.002 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-96336 AND EA 32-96337. 2L72 4F RTA28NM 19950310000091995031000009WP 1995 3 10 9503329963 119950301A2820 COUPLING DOUG DC9 DC931 3022065WP FUEL VENT TUBE LOOSE A NWAAA UNSCHED LANDING K FLUID LOSS UKUNKNOWN 1 GL01913RW 47171 FUEL BEGAN VENTING FROM RIGHT WING EN ROUTE MSP-BIL. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND FUEL VENT TUBE COUPLING LOOSE ON OUTBOARD SECTION OF LEFT WING TANK. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310000101995031000010WP 1995 3 10 9503349962 119950301A3260 DNLOCK SWITCH DOUG DC9 DC932 3022066WP LT MLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL01914RW 47362 LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION IN DSM. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310000111995031000011NM 1995 3 10 95FDEA00194 119950227A5320 CLIP BOEING727 72722 1384002NM BS 870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 NOTED CRACK AND/OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. INVESTIGATED DAMAGE. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP. 2L73 4F A3WE 19950310000121995031000012WP 1995 3 10 ABXA9500122 119950216A5320991015423 WEB DOUG DC9 DC931 3022065WP BS 756 TORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION AND COMPLIANCE OF E.A. FS-53-03689, FOUND CUSP WEB TORN AT FS 756, LEFT SIDE. REPLACED CUSP WEB IAW DC-9 SRM 51-30-2 AND ABX REA D953-10965-MR. 2L72 4F A6WE 19950310000131995031000013WP 1995 3 10 ABXA9500123 119950218A5312991150883 BLKHD WEB DOUG DC9 DC931 3022065WP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND BULKHEAD WEB AT STA 110 HAD LEVEL I CORROSION AT LONGERON 27R AT THE LOWER T-CAP. REPAIRED WEB IAW ABX REA D953-10960-MR. 2L72 4F A6WE 19950310000141995031000014WP 1995 3 10 ABXA9500124 119950215A533059114065 SKIN DOUG DC9 DC931 3022065WP BS 160 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DAMAGED AT TOP FORWARD CORNER OF MAIN ENTRY DOOR CUT OUT. REPAIRED IAW ABX REA D953-10962-MR. 2L72 4F A6WE 19950310000151995031000015WP 1995 3 10 ABXA9500125 119950222A5330591140021 SKIN DOUG DC9 DC931 3022065WP BS 83 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND INTERIOR SKIN GOUGED AND SCRATCHED AT STA 83, FLOOR LINE, RIGHT SIDE. REPAIRED IAW ABX REA-D953-11019-MR. 2L72 4F A6WE 19950310000161995031000016WP 1995 3 10 ABXA9500126 119950223A5312991150985 BLKHD T-CAP DOUG DC9 DC931 3022065WP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ON STA 110 BULKHEAD IN NOSE WHEEL WELL RIGHT TUNNEL. REPAIRED STA 110 BULKHEAD IAW ABX REA D953-10960-MR. 2L72 4F A6WE 19950310000171995031000017WP 1995 3 10 ABXA9500127 119950221A5330592032339 SKIN DOUG DC9 DC931 3022065WP BS 440 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND TEMPORARY REPAIR FORWARD OF STATIC PORT AT FS 440, LONGERON 23R. PERMANENT REPAIR NEEDED. REPAIRED IAW ABX REA D9536-10908-MR. 2L72 4F A6WE 19950310000181995031000018WP 1995 3 10 ABXA9500128 119950220A5330591140021 SKIN DOUG DC9 DC931 3022065WP BS 83-110 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND THREE DENTS ADJACENT TO REPAIR AT LONGERON 18 R, FROM STA 83 THROUGH 110. REPAIRED SKIN IAW ABX REA D953-11019-MR. 2L72 4F A6WE 19950310000191995031000019WP 1995 3 10 ABXA9500129 119950224A532099105035 WEB DOUG DC9 DC931 3022065WP BS 946-965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND LEFT CUSP WEB CRACKED AT LIGHTENING HOLE AT STA 946 THROUGH 965. REPAIRED WEB IAW ABX REA D953-11017-MR. 2L72 4F A6WE 19950310000201995031000020WP 1995 3 10 ABXA9500130 119950209A5320D0489826 WEB DOUG DC9 DC931 3022065WP BS 669-737 DEFORMED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05 AND S.B. 53-131, FOUND RIGHT CUSP WEB OVER FRAMES 669, 718 AND 737 DEFORMED AND MISSING PARTS. REPLACED CUSP WEB IAW E.A. NR FS-53-03689-MA. 2L72 4F A6WE 19950310000211995031000021WP 1995 3 10 ABXA9500131 119950209A5320D0489825 WEB DOUG DC9 DC931 3022065WP BS 699-737 DEFORMED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05 AND S.B. 53-131, FOUND LEFT CUSP WEB OVER FRAMES 699, 718 AND 737 DEFORMED AND PARTS MISSING. REPLACED CUSP WEB IAW E.A. NR FS-53-03689-MA. 2L72 4F A6WE 19950310000221995031000022WP 1995 3 10 ABXA9500132 119950209A5320591008543 SEAL DEPRESSOR DOUG DC9 DC931 3022065WP BS 200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND AFT LOWER SERVICE DOOR SEAL DEPRESSOR GOUGED AND BENT. BLENDED AND STRAIGHTENED SEAL DEPRESSOR IAW DC-9 SRM 53-01 AND 51-410-3. 2L72 4F A6WE 19950310000231995031000023WP 1995 3 10 ABXA9500133 119950209A5320591008523 SEAL DEPRESSOR DOUG DC9 DC931 3022065WP BS 160 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FORWARD LOWER SERVICE DOOR SEAL DEPRESSOR GOUGED AND BENT. BLENDED AND STRAIGHTENED SEAL DEPRESSOR IAW DC-9 SRM 53-01 AND 51-10-3. 2L72 4F A6WE 19950310000241995031000024WP 1995 3 10 ABXA9500134 119950210A5340S2923978516 STOP BOLT DOUG DC9 DC931 3022065WP BS 200 DEFORMED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FORWARD SERVICE DOOR AFT UPPER STOP BOLT DEFORMED. REPLACED DOOR STOP IAW DC-9 M.M. 20-16-0. 2L72 4F A6WE 19950310000251995031000025WP 1995 3 10 ABXA9500135 119950221A532059124921 DOOR JAMB DOUG DC9 DC931 3022065WP BS 200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FORWARD SERVICE DOOR JAMB HAD LEVEL I CORROSION AT FORWARD AND AFT LOWER CORNERS. REPLACED LOWER SECTION OF DOOR JAMB IAW DC-9 SRM 53-05, FIG. 55. 2L72 4F A6WE 19950310000261995031000026WP 1995 3 10 ABXA9500136 119950209A571339112362 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 12, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B. 2L72 4F A6WE 19950310000271995031000027WP 1995 3 10 ABXA9500137 119950209A57133911236504 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 13, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B. 2L72 4F A6WE 19950310000281995031000028WP 1995 3 10 ABXA9500138 119950209A57133911236502 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 15, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B. 2L72 4F A6WE 19950310000291995031000029WP 1995 3 10 ABXA9500139 119950209A57133911240504 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 17, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B. 2L72 4F A6WE 19950310000301995031000030WP 1995 3 10 ABXA9500140 119950209A57133911238510 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 19, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B 2L72 4F A6WE 19950310000311995031000031WP 1995 3 10 ABXA9500141 119950213A532099582424 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 699-718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING C-CHECK INSPECTION, FOUND INTERCOSTAL ON LONGERON 6R, BETWEEN FRAMES 699 - 718, CRACKED. FABRICATED INTERCOSTAL PER ABX PFEA NR PFE-D953-09408 AND INSTALLED IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950310000321995031000032EU 1995 3 10 QXEA9500061 119950302A33501315 EEL LAMP FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 BOI - DURING MAINTENANCE RT EMERGENCY EXIT 5V LIGHT FOUND INOP. RELAMPED FIXTURE. TESTED OK. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950310000331995031000033EU 1995 3 10 QXEA9500062 119950302A351010032N PBE FOKKERF28 F28MK1000 4990808EU COCKPIT DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09803PH11190 11031 BOI - DURING MAINTENANCE FOUND COCKPIT PBE WITH RED INDICATOR POPPED. REPLACED PBE. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950310000341995031000034NM 1995 3 10 SWAA950194 119950228A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD PRESSURE WEB FROM BL 0 TO RBL 17, WL 184 TO 230, UNDER STRAPS AND ANGLES. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950310000351995031000035NM 1995 3 10 SWAA950195 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 818-828 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 818 TO 828, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200. 2L72 4F A16WE 19950310000361995031000036NM 1995 3 10 SWAA950196 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 867-888 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 867, 860, 870, 887, 888, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200. 2L72 4F A16WE 19950310000371995031000037NM 1995 3 10 SWAA950197 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 767, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0200. 2L72 4F A16WE 19950310000381995031000038NM 1995 3 10 SWAA950198 119950228A5330 SKIN BOEING737 7372H4 138448CNM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 768, AT STRINGER 4R. REPAIRED PER TRAMCO EWO 95-0200. 2L72 4F A16WE 19950310000391995031000039EU 1995 3 10 RAIA950123 119950119A5260S5217640300860 STEP AEROSPATR42 ATR42300 8680920EU PAX DOOR CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE032FOR 199 MAINTENANCE DISCOVERED SURFACE CORROSION ON PAX DOOR STEP BOX. CORROSION DEFINED AS FILIFORM TYPE. MAINTENANCE CLEANED AND TREATED AREAS OF CORROSION IAW ATR42 SRM 51-21-42 FOR PAINTING AND CORROSION PREVENTION AND INSPECTION MM 52-10-00. (W) 2H72 4T RTA53EU 19950310000401995031000040WP 1995 3 10 PJXA951 119950109A32462606225 WHEEL BEARING DOUG DC9 DC983 3022083WP NR 3 MLG FAILED A PJXAO OTHER O OTHER LDLANDING 1 SO112FOR 49668 THE NR 3 O/B BEARING FAILED ON LANDING IN CANCUN. REPLACED LOWER STRUT, WHEELS AND NR 3 BRAKES. (W) 2L72 4F RTA6WE 19950310000511995031000051NE 1995 3 10 95ZZZX1011 219950111A7200 ENGINE AMD FALC20FALCON20C5 2730107EU GE CF700 CF7002D2 30010NE INTERNAL FLAME OUT A AGXPAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 GL23179GA 100 222J040 ENGINE FLAMED OUT TWICE DURING HIGH ALTITUDE FLAME OUT CHECK. SUSPECT CAUSE AS INTERNAL ENGINE FAILURE. RECOMMEND TEAR DOWN ENGINE FOR INSPECTION. 2L72 4F4 FRTA7EU E7EA 19950310000521995031000052NE 1995 3 10 95ZZZX1012 219950110A732150D1T39G29 FUEL CONTROL AMD FALC20FALCON20C5 2730107EU GE CF700 CF7002D2 30010NE NR 1 ENGINE MALFUNCTION A AGXPAO OTHER X ENGINE FLAMEOUT CLCLIMB 1 GL23179GA GAT6A56 100 222J040 LEFT ENGINE FLAMED OUT TWICE (ONCE AT CLIMB-OUT THROUGH 33,000 FEET, RE-LIGHT AT 24,000 FEET), FLAMED OUT AGAIN AT 30,000 FEET. SUSPECT CAUSE AS MALFUNCTION OF ENGINE FUEL CONTROL UNIT. RECOMMEND REPLACING FUEL CONTROL UNIT AND PERFORM A HIGH ALTITUDE FLAME OUT CHECK. 2L72 4F4 FRTA7EU E7EA 19950310000611995031000061NE 1995 3 10 95ZZZX1021 219950213A7321216381019 FUEL CONTROL CNDAIRCL600 CL6001A11 1900302EA LYC ALF502ALF502L2 41580NE NR 2 ENGINE FAILED A ANVIAOA OTHER UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SW05600TE3179 1056 3179 ENGINE FLAME-OUT AT FL370, ENGINE FAILED TO RESTART ON SUBSEQUENT ATTEMPTS. AIRCRAFT MADE A SAFE LANDING AT GULPORT, MS. INVESTIGATION REVEALED INTERNAL FAILURE OF FUEL CONTROL UNIT. REMOVED DEFECTIVE COMPONENT AND INSTALLED REPAIRED REPLACEMENT. PERFORMED GROUND LEAK AND OPS CHECKS, AND ADJUSTED AS REQUIRED IAW MM SPECS. 2L72 4F4 FRTA21EA E6NE 19950310000621995031000062 1995 3 10 95ZZZX1022 419950203A237089094005211 CVR BDINST HWKSLYDH125 DH1253ARA 423013PEU COCKPIT FAIL TEST A MDGAK NONE L NO TEST ININSP/MAINT 1 SO0925MJ A01208 705 UNIT FAILED PUSH-TO-TEST. COCKPIT TEST ON PRE-FLIGHT. UNIT HAS 361 HOURS SINCE REPAIR. HIGH FAILURE RATE. 2L72 4J A3EU 19950310000691995031000069EU 1995 3 10 95ZZZX1029 119950124A2434 ALTERNATOR HAMFLUHFB320HFB320 4071204EU RT ENGINE MISWIRED A GXPAK NONE HBWELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C NRNOT REPORTED 1 GL23171GA 139 WHEN TURNING ON EITHER AIRFRAME ANTI-ICE OR DE-ICE, BOTH ALTERNATORS FELL OFF LINE. INTERIOR OF AIRCRAFT FILLED WITH SMOKE. ALTERNATORS WERE WIRED INCORRECTLY TO THE AIRCRAFT. SMOKE CAUSED BY ALTERNATOR PHASE BEING OUT. RECOMMENDATION: PROPER TRAINING ON REMOVAL AND INSTALLATION PROCEDURES. 2L72 4J A14EU 19950310000701995031000070 1995 3 10 95ZZZX1030 419950124A3457TNL2000T GPS HAMFLUHFB320HFB320 4071204EU COCKPIT FAILED A GXPAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23171GA 139 GPS LOST POWER AND SPARKED IN AREA OF CAPTAIN'S LEFT KNEE. BROKEN WIRE GOING TO GPS WIRE WAS NOT PROPERLY SECURED. 2L72 4J A14EU 19950310000731995031000073CE 1995 3 10 95ZZZX1033 119950206A212119A608 FAN CESSNA500 500CESSNA 2076602CE AIR DIST BEARING FAILED A MDGAK NONE O OTHER ININSP/MAINT 1 SO0910UH 84 5000304 INSPECTION FOUND BEARING IN FAN FAILED AFTER ONLY 84 HOURS SINCE NEW. 1L72 4F A22CE 19950310000751995031000075CE 1995 3 10 95ZZZX1035 119950210A27102300003272 CONTROL CABLE LEAR 35 35LEAR 5170600CE AILERON DAMAGED A SN7AK NONE O OTHER ININSP/MAINT 1 EA2131FN 2383 033 DURING A 2400-HOUR INSPECTION (CABLE CHANGE), THE CABLES LISTED UNDER SECTION 5 WERE FOUND TO HAVE NUMEROUS BROKEN STRANDS -- MORE THAN NORMALLY FOUND DURING A CABLE CHANGE. 2L72 4F A10CE 19950310000761995031000076CE 1995 3 10 95ZZZX1036 119950210A2710230000246 CONTROL CABLE LEAR 35 35LEAR 5170600CE AILERON DAMAGED A SN7AK NONE O OTHER ININSP/MAINT 1 EA2131FN 2383 033 DURING A 2400-HOUR INSPECTION (CABLE CHANGE), THE CABLES LISTED UNDER SECTION 5 WERE FOUND TO HAVE NUMEROUS BROKEN STRANDS -- MORE THAN NORMALLY FOUND DURING A CABLE CHANGE. 2L72 4F A10CE 19950310000771995031000077CE 1995 3 10 95ZZZX1037 119950210A27102300003078 CONTROL CABLE LEAR 35 35LEAR 5170600CE AILERON DAMAGED A SN7AK NONE O OTHER ININSP/MAINT 1 EA2131FN 2383 033 DURING A 2400-HOUR INSPECTION (CABLE CHANGE), THE CABLES LISTED UNDER SECTION 5 WERE FOUND TO HAVE NUMEROUS BROKEN STRANDS -- MORE THAN NORMALLY FOUND DURING A CABLE CHANGE. 2L72 4F A10CE 19950310000951995031000095NM 1995 3 10 ASAA9568 119950213A5210507945178 DOOR MECHANISM BOEING737 7374Q8 NM FWD CABIN LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01764AS7253 25101 SEA - L1 DOOR BINDS ON CLOSING. MAINTENANCE LUBED TOP HINGE AND OPS CHECKED NORMAL. (Z) 2L72 4F RTA16WE 19950310000961995031000096EU 1995 3 10 AWXA9500073 119950203A2910MR29104 MANIFOLD AIRBUS320 A320231 3930325EU NR 1 LEAKS A AWXAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 WP28620AW 0197 052 ATL - FLT 19 - ATL-PHX - AFTER NR 1 ENGINE START, GROUND CREW NOTICED LARGE HYDRAULIC LEAK ASSOCIATED WITH YELLOW HYDRAULIC LOW LEVEL. LEAK NOTED AT YELLOW HYDRAULIC RESERVOIR DOOR. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER PROBLEMS. CONTRACT MAINTENANCE REPLACED GROUND SERVICE MANIFOLD, REF MM 29-19-41, PAGES 427/437. NO LEAKS NOTED UNDER PRESSURE. SYSTEM SERVICED TO FULL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA28NM 19950310000971995031000097NM 1995 3 10 AWXA9500091 119950214A2530416100123 COFFEEMAKER BOEING737 7372A6 138448BNM AFT GALLEY SHORTED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28145AW 0431 20194 FLT 1911 - LAS-OAK - AIR TURNBACK, CREW DECLARED AND EMERGENCY DUE TO AN ELECTRICAL SMELL IN AFT GALLEY. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AFT INBOARD COFFEEMAKER HAD BURNT WIRES. INSTALLED NEW COFFEEMAKER AND SMELL CLEARED. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950310000981995031000098NM 1995 3 10 AWXA9500092 119950301A5230 DOOR FRAME BOEING737 737277 1384570NM CARGO DOOR CRACKED A AAWXAO OTHER OJ OTHER WARNING INDICATION DEDESCENT 1 WP28182AW 22649 LAS - FLT 134 - CABIN PRESSURE, AC REQUIRED 53 PERCENT N1 TO MAINTAIN CABIN DURING DESCENT. AC LANDED IN LAS WITHOUT FURTHER PROBLEMS. MX FOUND AFT CARGO DOOR LOWER FWD DOOR FRAME INNER STRUCTURE CRACKED. MX INSPECTED AC AND FOUND THE AC SAFE FOR ONE TIME PRESSURIZED FERRY FLIGHT TO PHX FOR CARGO DOOR FRAME REPAIR. DURING C-13 INSPECTION, REPAIRED DOOR LOWER BEAM WEB AND OUTER CHORD CRACK AT LOWER FWD END. REMOVED AND REPLACED T-CHORD AND WEB PER SRM 51-10-02, REF PRINT NR 55C25180. (Z) 2L72 4F RTA16WE 19950310000991995031000099NM 1995 3 10 AWXA9500094 119950214A3350900835A EEL BATTERY PACK BOEING737 7372A6 138448BNM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28145AW 20194 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT GALLEY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R2 DOOR, OPS CHECK GOOD. (Z) 2L72 4F A16WE 19950310001001995031000100NM 1995 3 10 AWXA9500095 119950221A5320 ANGLE BOEING737 7373G7 1384595NM FS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND SUPPORT BRACKET CRACKED ON AFT FLANGE, STATION 540 BETWEEN BL 0 AND LBL 24. REPAIRED ANGLE PER SRM 51-70-11. (Z) 2L72 4F RTA16WE 19950310001011995031000101NM 1995 3 10 AWXA9500096 119950221A540067737596 FORMER BOEING737 7373G7 1384595NM NR 2 ENG PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND NR 2 ENGINE PYLON FAIRING FORMER CRACKED AT UPPER END IN RADIUS. REMOVED AND REPLACED CRACKED FORMER PER SRM 51-10-02 AND SRM 51-40-02. (Z) 2L72 4F RTA16WE 19950310001021995031000102NM 1995 3 10 AWXA9500097 119950221A5315 FLOORBEAM BOEING737 7373G7 1384595NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND FLOORBEAM CORRODED BEYOND LIMITS AROUND SCREW HOLES, STATION 967 LBL 48. REPAIRED DAMAGED AREA PER ER 3-53-16-23. (Z) 2L72 4F RTA16WE 19950310001031995031000103NM 1995 3 10 AWXA9500098 119950221A5320 INTERCOSTAL BOEING737 7373G7 1384595NM FS 986-1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND ANGLE INTERCOSTAL CORRODED BEYOND LIMITS AT SCREW HOLES, BS 986 TO 1006 LBL 18. FABRICATED AND INSTALLED INTERCOSTAL PER ER 53-10-01B. (Z) 2L72 4F RTA16WE 19950310001041995031000104NM 1995 3 10 AWXA9500099 119950221A5320 INTERCOSTAL BOEING737 7373G7 1384595NM FS 967/986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND INTERCOSTAL BETWEEN BS 967 AND 986 RBL 20 CORRODED BEYOND CLEAN UP LIMITS AROUND SCREW HOLES. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-1 AND SRM 51-30-02. (Z) 2L72 4F RTA16WE 19950310001051995031000105NM 1995 3 10 AWXA9500100 119950221A5312 CHORD BOEING737 7373G7 1384595NM LAV BLKHD CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND CORROSION ON INNER CHORD AT RT AFT LAV FORWARD BULKHEAD R2 DOOR AREA. REMOVED AND REPLACED CHORD PER SRM 51-10-02 AND 51-40-02. (Z) 2L72 4F RTA16WE 19950310001061995031000106NM 1995 3 10 AWXA9500101 119950221A5315 FLOOR BEAM BOEING737 7373G7 1384595NM FS 947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND TOP CAP OF FLOOR BEAM CORRODED AROUND SCREW HOLES, STATION 947 LBL 12 TO RBL 8. REPAIRED DAMAGED AREA PER ER-53-16-24. (Z) 2L72 4F RTA16WE 19950310001071995031000107NM 1995 3 10 AWXA9500102 119950221A5315 FLOORBEAM BOEING737 7373G7 1384595NM FS 986 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28303AW 24010 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND FLOOR BEAM SCREW HOLES CORRODED, STATION 986 FROM L2 TO R2. INSTALLED REPLACEMENT UPPER T-CAP AND REPAIR SPLICE PER ER 3-53-16-22. (Z) 2L72 4F RTA16WE 19950310001081995031000108SW 1995 3 10 MALA954278 119950129A32601EN516 DNLOCK SW SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAK NONE N FALSE WARNING APAPPROACH 1 GL1527465 AC755B FLT 3198 - ON CLIMB-OUT FROM DSM, THE RIGHT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON RETRACTION. ALL OTHER GEAR INDICATIONS WERE NORMAL. ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT ALSO FAILED TO ILLUMINATE DURING GEAR EXTENSION. MAINTENANCE REPLACED THE RIGHT INBOARD DOWNLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310001091995031000109SW 1995 3 10 MALA954279 119950127A32601EN516 DNLOCK SW SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAK NONE N FALSE WARNING APAPPROACH 1 GL15424MA AC639 FLT 3494 - ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT DOESN'T ILLUMINATE DURING THE GEAR EXTENSION. MAINTENANCE REPLACED THE RIGHT INBOARD DOWN SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310001101995031000110 1995 3 10 MALA954280 419950127A23126226520008 COMM CONTROL PNL SWRNGNSA227 SA227AC 8780603SW COCKPIT INTERNAL FAULT A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15159MC AC728 FLT 3352 - IN CRUISE FLIGHT FROM MSP, THE NR 1 COMM DISPLAY BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 1 COMM CONTROL PANEL. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310001111995031000111SW 1995 3 10 MALA954281 119950130A57532736003002 RIB SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP INBOARD END RIB TO HAVE CHAFING DAMAGE FROM CONTACT WITH THE SWING LINK BRACKET. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT FLAP INBOARD END RIB. (Z) 1L72 4T A8SW 19950310001121995031000112NM 1995 3 10 MALA954282 119950130A27317003032612 ELEV TRIM SERVO DHAV DHC8 DHC8102 2809003NM ELEV TRIM FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15828MA 333 FLT 3109 - DURING THE PREFLIGHT IN MSP, THE CREW NOTED THAT THE ELEVATOR TRIM DOESN'T ALWAYS RELEASE WHEN THE AUTO PILOT IS DISENGAGED. MAINTENANCE REPLACED THE ELEVATOR TRIM SERVO ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001131995031000113NM 1995 3 10 MALA954283 119950106A3350 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15828MA 333 FLT 3061 - DURING THE POST FLIGHT IN DTW, THE COCKPIT OVERHEAD EMERGENCY LIGHT FAILED TO TEST. MAINTENANCE RESECURED A LOOSE BRACKET. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001141995031000114NM 1995 3 10 MALA954284 119950112A335010005511 EEL LAMP DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST CRCRUISE 1 GL15833MA 343 FLT 3033 - IN CRUISE FLIGHT TO DTW, THE COCKPIT CEILING EMERGENCY LIGHT WOULD INTERMITTENTLY GO TO BRIGHT. MAINTENANCE REPLACED THE EMERGENCY EXIT LAMP ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001151995031000115 1995 3 10 MALA954285 419950202A3440 RT UNIT DHAV DHC8 DHC8102 2809003NM RADAR ALT FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15832MA 341 FLT 3216 - IN CRUISE FLIGHT TO LSE, THE GPWS, TCAS AND RADAR ALTIMETER SYSTEMS FAILED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE RADAR ALTIMETER R/T WAS REPLACED AS A PRECAUTION. (Z) 2H72 4T RTA13NM 19950310001161995031000116EU 1995 3 10 MALA954286 119950204A33506008905 EEL BATTERY PACK FOKKERF27 F27MK200 4990620EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15278MA 10280 DURING SCHEDULED MAINTENANCE IN CWA, THE FORWARD CARGO AND FORWARD CABIN EVACUATION LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT 3C AND 3D. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T A817 19950310001171995031000117SW 1995 3 10 MALA954287 119950205A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FUSELAGE CARGO DOOR FRAME CRACKED AT THE GAS SPRING BOLT MOUNTING HOLE. REPAIRS WERE COMPLETED THROUGH INSTALLATION OF A REPAIR DOUBLER IAW FAC LAR 95-MALA-042 AND FAC 51-00-00 STANDARD PRACTICES. (Z) 1L72 4T A8SW 19950310001181995031000118NM 1995 3 10 MALA954288 119950204A5542 SKIN DHAV DHC8 DHC8102 2809003NM RUDDER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15822MA 326 DURING MAINTENANCE IN MSP, A CRACK WAS NOTED TO THE RIGHT SIDE OF THE UPPER FORE RUDDER AT STATION X877.123. REPAIRS WERE COMPLETED IAW DEHAVILLAND RD8-55-226 FOR THE STIFFENER REPAIR AND SRM 51-40-11 AND 55-40-28 FOR REPLACEMENT OF 9 INCHES OF THE UPPER RUDDER SKIN. (Z) 2H72 4T RTA13NM 19950310001191995031000119SW 1995 3 10 MALA954295 119950207A53112722104047 FRAME SWRNGNSA227 SA227AC 8780603SW FS 212.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT LOWER BELT FRAME CRACKED AT FS 212.27. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW SRM 53-90-20. (Z) 1L72 4T A8SW 19950310001201995031000120SW 1995 3 10 MALA954296 119950207A53112722100035 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT LOWER BELT FRAME AT FS 242.27 IS CRACKED AT RADIUS .125. REPAIRS WERE COMPLETED IAW WITH FAC SRM 53-90-20. (Z) 1L72 4T A8SW 19950310001211995031000121SW 1995 3 10 MALA954297 119950207A5753 RIB SWRNGNSA227 SA227AC 8780603SW LT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP END RIB CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE END RIB, P/N 27-36015-007, IAW FAC SRM 51-30-03, 51-40-01, 51-40-02, AND 51-00-00. (Z) 1L72 4T A8SW 19950310001221995031000122SW 1995 3 10 MALA954298 119950207A57532736015008 RIB SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP END RIB CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE END RIB, P/N 27-36015-008, IAW FAC SRM 51-30-03, 51-40-01, 51-40-02 AND 51-00-00. (Z) 1L72 4T A8SW 19950310001231995031000123SW 1995 3 10 MALA954299 119950207A3297 WIRE SWRNGNSA227 SA227AC 8780603SW NLG STEERING DEFECTIVE A MALAO OTHER O OTHER LDLANDING 1 GL15421MA AC634 FLT 3065 - DURING THE LANDING ROLL IN DTW, AT APPROXIMATELY 40 KNOTS, THE AIRCRAFT VEERED TO THE RIGHT WITH THE NOSE WHEEL STEERING BUTTON PUSHED. THE AIRCRAFT CONTINUED TO THE GATE. MAINTENANCE REPAIRED A DEFECTIVE WIRING SECTION. SYSTEM OPERATED SATISFACTORILY. (Z) 2L72 4T RTA8SW 19950310001241995031000124SW 1995 3 10 MALA954305 119950210A3260 POSITION SW SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15433MA AC714 FLT 3214 - ON APPROACH TO MSP, THE NOSE GEAR RED INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, MAINTENANCE REPLACED THE LEFT UP POSITION SWITCH AND REPLACED A TERMINAL STRIP. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310001251995031000125SW 1995 3 10 MALA954306 119950211A53202720085 CARGO DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 491.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING SCHEDULED MAINTENANCE IN MSP, A CRACK WAS FOUND AT THE AFT CARGO DOOR FRAME, GAS SPRING STRUT MOUNT AREA. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED AREA, AND FABRICATING AND INSTALLING A REPAIR ANGLE, REPAIR PLATE AND FILLER IAW FAC LAR-95-MALA-048 AND SRM 51-30-02 AND 51-30-04. (Z) 1L72 4T A8SW 19950310001261995031000126EU 1995 3 10 MALA954308 119950211A3230 RETRACT MECH FOKKERF27 F27MK200 4990620EU NLG LACK OF LUBE A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15278MA 10280 FLT 3261 - ON APPROACH TO MSP, THE NOSE GEAR DOWN AND LOCKED LIGHT WAS SLOW TO ILLUMINATE. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE CLEANED AND LUBED THE NOSE GEAR. SYSTEM OPERATED SATSIFACTORILY. (Z) 2H72 4T A817 19950310001271995031000127NM 1995 3 10 MALA954313 119950211A324021565 BRAKES DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15822MA 326 WHILE TAXIING IN DTW, AN EXCESSIVE AMOUNT OF POWER IS NEEDED TO REACH NORMAL TAXI SPEED. MAINTENANCE REPLACED THE RIGHT OUTBOARD AND INBOARD BRAKE ASSEMBLIES. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001281995031000128NM 1995 3 10 MALA954314 119950211A324058570 BRAKE VALVE DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15822MA 326 WHILE TAXIING IN DTW, THE CREW NOTED THAT MORE THAN NORMAL PRESSURE NEEDS TO BE APPLIED TO THE BRAKES TO STOP THE AIRCRAFT. MAINTENANCE REPLACED THE STANDBY BRAKE VALVE. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001291995031000129NM 1995 3 10 MALA954315 119950211A324021565 BRAKE DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15822MA 326 FLT 3001 - WHILE TAXIING IN DTW, THE CREW NOTED THAT THE BRAKES WERE GRABBING WHILE TAXIING. MAINTENANCE REPLACED THE LEFT INBOARD AND OUTBOARD BRAKE ASSEMBLIES. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310001301995031000130SW 1995 3 10 MALA954316 119950212A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15438MA AC721 FLT 3256 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE RESHIMMED THE BELLCRANKS. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (Z) 1L72 4T A8SW 19950310001311995031000131SW 1995 3 10 MALA954320 119950214A5230 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 438.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, THE AFT CARGO DOOR FRAME WAS CRACKED AT FS 438.06. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED AREA, INSTALLING A REPAIR DOUBLER IAW FAC LAR-95-MALA-052. (Z) 1L72 4T A8SW 19950310001341995031000134NM 1995 3 10 TAOA029503 119950203A33506012541 EEL BATTERY PACKGRIMES BOEING727 727254 138408LNM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15914TS 3182 20251 LEFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK OK. (Z) 2L73 4F A3WE 19950310001351995031000135NM 1995 3 10 TAOA029504 119950205A3350900835A EEL BATTERY PACKBELL BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS B3426 22043 LEFT EXTERNAL EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK ASSEMBLY. OPERATIONAL CHECK OK (Z) 0 4 A3WE 19950310001361995031000136NM 1995 3 10 TAOA029505 119950205A3350DMA17023 EEL BATTERY PACKGRIMES BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 22043 RED EPL LIGHT SOCKET MISSING AND WIRES BROKEN AT ROW 2D. REPLACED SOCKET ASSEMBLY AND REPAIRED WIRES. OPERATIONAL CHECK OK. (Z) 0 4 A3WE 19950310001371995031000137NM 1995 3 10 TAOA029506 119950208A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 6759 20441 OVERHEAD EMERGENCY EXIT SIGN AT ROW 16 INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (Z) 2L73 4F A3WE 19950310001381995031000138NM 1995 3 10 TAOA029510 119950212A33501315 EEL LAMP BOEING727 727254 138408LNM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15915TS 20252 EMERGENCY EXIT LIGHT AT ROW 18F INOPERABLE. RELAMPED. OPERATIONAL CHECK OK. (Z) 2L73 4F A3WE 19950310001391995031000139NM 1995 3 10 TWRA9511 119950212A335060B40053 EEL BATTERY PACK BOEING747 747131 1384881NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15608FF 19672 DURING PREFLIGHT INSPECTION, FOUND 'E' ZONE EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (Z) 2L74 4F A20WE 19950310001401995031000140EU 1995 3 10 VTZA95051 119950208A2912QA03061 HYD FILTER BAG JETSTMJETSTM3201 1500217EU FUSELAGE CLOGGED A VTZAO OTHER O OTHER APAPPROACH 1 EA27496UE 900 DURING APPROACH TO LANDING AN IN FLT EMERGENCY WAS DECLARED ON FLT NR 6296, DUE TO N/G DOWNLOCK INDICATION. THE RED INTRANSIT LIGHT STAYED ILLUMINATED. A/C LANDED AT SYR. A/C FERRIED TO IAD WHERE MX REPLACED THE DOWNLOCK MICROSWITCH BRACKET AND READJUSTED THE DOWNLOCK MICROSWITCH. OPS CHECK GOOD. A/C WAS RETURNED TO SERVICE. S/D - FLT NR 6240 FROM IAD TO ROA ON APPROACH, THE LANDING GEAR INDICATED 2 GREEN, THE NOSE INDICATION LAGGED. UPON LANDING/TAXI NOSE INITIALLY FLICKERED RE/GREEN THEN INDICATED ALL 3 GREEN DOWN AND LOCKED. A/C WAS FERRIED TO LYH WHERE MX CLEANED THE HYD RETURN FILTER AND COMPLIED WITH MX ACCEPTANCE FLT. OPS CHECK GOOD. BRACKET P/N 1371166K11, SWITCH P/N 9EN1C11HBB2. (Z) 2L72 4T RTA56EU 19950310001411995031000141NM 1995 3 10 95ZZZW129 119950212A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07922HA 312 094 HPN-PHL - FLT 3108 - ON APPROACH, LANDING GEAR DID NOT EXTEND ON NORMAL GEAR EXTENSION. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE. 2H72 4T RTA13NM 19950310001421995031000142NM 1995 3 10 95ZZZW130 119950210A3240 BRAKE SYST DHAV DHC8 DHC8102 2809003NM MLG REQD SERVICE A HNAAO OTHER O OTHER LDLANDING 1 EA07924HA 105 PHF-PHL - FLT 3091 - AFTER LANDING ROLLOUT, CREW REPORTED MOMENTARY LOSS OF BRAKES WHEN TURNING. FOUND AIR IN BRAKE SYSTEM, BLED AS REQUIRED. 2H72 4T RTA13NM 19950310001431995031000143 1995 3 10 95ZZZW131 419950208A612278249028 PROP CONTL UNIT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE FAILED A HNAAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION APAPPROACH 1 EA07926HA12122 114 GSO-DCA - FLT 3269 - ON FINAL APPROACH, THE NR 1 PROP RPM DECAYED TO 780, COULD NOT CONTROL WITH CONDITION LEVER OR POWER LEVER. CAPTAIN SHUT ENGINE DOWN AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 PROP CONTROL UNIT. 2H72 4T RTA13NM 19950310001441995031000144NM 1995 3 10 95ZZZW132 119950208A3350 EEL CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN BENT A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07941HA 161 EWR-BWI - FLT 3266 - DURING FLIGHT CREW PREFLIGHT, FOUND FIRST TWO EMERGENCY FLOOR LIGHTS INOP. REPLACED PIN 6 ON PS2 BATTERY POWER SUPPLY CONNECTOR. 2H72 4T RTA13NM 19950310001451995031000145NM 1995 3 10 95ZZZW133 119950219A26123001146100040011FIRE LOOP DHAV DHC8 DHC8102 2809003NM APU CHAFING A HNAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA07908HA25532 5850 015 CLT-EWN - FLT 3220 - THE FIRE DETECTION WARNING LIGHT AND APU FIRE FAULT ADVISORY LIGHT ILLUMINATED DURING FLIGHT. ACFT TURNED BACK AND LANDED IN CLT WITHOUT INCIDENT. REMOVED AND REPLACED APU FIRE LOOP FOR CHAFING. 2H72 4T RTA13NM 19950310001461995031000146NM 1995 3 10 ASAA95067 119950213A33506013211 EEL BATT PACK BOEING737 737298C 1384490NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE FWD EMERGENCY EVACUATION SLIDE EXTERIOR LIGHTS WERE FOUND INOPERATIVE. REPLACED FWD EVACUATION SLIDE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950310001471995031000147WP 1995 3 10 ASAA9541 119950129A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, THE FLOOR EMERGENCY EXIT LIGHTS FROM ROW 27 AFT WERE FOUND INOPERATIVE. REPAIRED WIRING AT SIDEWALL AND REPLACED PICO FUSE AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950310001481995031000148NM 1995 3 10 ASAA9542 119950202A33503071BPEGPL EEL LAMP BOEING737 7374Q8 NM CABIN INOP A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 LAX - DURING CHECK, THE EMERGENCY TRACK LIGHTS INTERMITTENTLY INOP. MAINTENANCE RELAMPED LIGHT AT ROW 2. (W) 2L72 4F RTA16WE 19950310001491995031000149WP 1995 3 10 ASAA9546 119950206A3350S103 EEL BATT PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950310001501995031000150NM 1995 3 10 ASAA9547 119950208A5315 FLOORBEAM BOEING737 737210C 1384459NM BS 500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, CORROSION WAS FOUND ON FLOORBEAM AT BS 500B. MAINTENANCE ACCOMPLISHED REPAIR PER SRM 51-10-6 AND EA 5310-01324. (W) 2L72 4F A16WE 19950310001511995031000151NM 1995 3 10 ASAA9548 119950208A5315 FLOORBEAM BOEING737 737210C 1384459NM FS 520 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, FOUND CRACKS IN STA 520 FLOOR SUPPORT BEAM AT THE FOLLOWING LOCATIONS, LBL 45, RBL 24.5 AND RBL 45. MAINTENANCE REPAIRED CRACKS USING EA 5310-01318, EA 5310-01319 AND EA 5310-01320. (W) 2L72 4F A16WE 19950310001521995031000152NM 1995 3 10 ASAA9549 119950207A3350 EEL WIRING BOEING737 737490 1384715NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - DURING CHECK, EMERGENCY FLOOR LIGHTS INOP AT ROWS 15 AND 16. MAINTENANCE REPAIRED LOOSE WIRING. (W) 2L72 4F RTA16WE 19950310001531995031000153NM 1995 3 10 ASAA9550 119950207A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 SEA - DURING CHECK, THREE AFT MOST EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED WIRING. (W) 2L72 4F RTA16WE 19950310001541995031000154NM 1995 3 10 ASAA9560 119950209A3350S283T0143 EEL BATT PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING CHECK, THE L2 AND R2 EXTERIOR EMERGENCY LIGHTS OUT. MAINTENANCE REPLACED BATTERY PACK ASSY. (W) 2L72 4F A16WE 19950310001551995031000155NM 1995 3 10 ASAA9561 119950209A5210507945178 DOOR HANDLE BOEING737 7372X6C 1384552NM FWD CABIN STIFF A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 ANC - DURING CHECK, THE LT FWD ENTRY DOOR HARD TO LATCH. MAINTENANCE ADJUSTED DOOR UPPER GUIDE ARM. (W) 2L72 4F RTA16WE 19950310001561995031000156WP 1995 3 10 ASAA9562 119950211A3350S103 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE THREE OVERHEAD EMERGENCY LIGHTS FROM ROW 6 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950310001571995031000157WP 1995 3 10 ASAA9563 119950212A33501001191 PORT EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01950AS 53023 PDX - DURING MAINTENANCE CHECK, THE FWD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950310001581995031000158NM 1995 3 10 ASAA9564 119950212A323065737625 RETRACT MECH BOEING737 737290C 138448VNM NLG FAILED A ASAAK NONE O OTHER LDLANDING 1 NM01742AS 23136 ANC - FLT 145 - ON ARRIVAL, THE CREW REPORTED THE NLG FAILED TO EXTEND WHEN LANDING GEAR HANDLE WAS PLACED TO DOWN. PERFORMED MANUAL EXTENSION AND LANDED WITHOUT INCIDENT. CLEANED AND INSPECTED NLG, NO DEFECTS NOTED. PERFORMED EXTENSION AND RETRACTION TEST, NO DISCREPANCIES NOTED. (W) 2L72 4F A16WE 19950310001591995031000159WP 1995 3 10 ASAA9565 119950213A3350 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 ONT - FLT 531 - PRIOR TO DEPARTURE, CREW REPORTED ROW 13 EMERGENCY EXIT FLOOR TRACK LIGHTS WILL NOT TEST. RESEATED BATTERY IN PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950310001601995031000160WP 1995 3 10 ASAA9566 119950214A3350101191 PORT EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS 53449 PDX - DURING MAINTENANCE CHECK, THE FWD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950310001611995031000161WP 1995 3 10 ORJA95007 119950105A335041B004AD073 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11841RA 49421 AFT OVERHEAD COCKPIT EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN EMERGENCY LIGHT BATTERY PACK 85-23 ALL EMERGENCY LIGHTS OPS CHECKED GOOD. (W) 2L72 4F A6WE 19950310001621995031000162WP 1995 3 10 ORJA95008 119950107A33500105606003 EEL DOUG DC9 DC982 3022082WP CABIN INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11840RA 49424 EMERGENCY FLOOR TRACK LIGHTING INOP AT MID SECTION. REMOVED AND REPLACED MID SECTION RIBBON FROM SIDEWALL TO FLOOR LIGHTS, CHECKS GOOD. (W) 2L72 4F A6WE 19950310001631995031000163WP 1995 3 10 ORJA95009 119950107A335041B004AD073 EEL BATTERY DOUG DC9 DC982 3022082WP COCKPIT DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11840RA 49424 FIRST CLASS EMERGENCY CEILING LAMPS INOP. CHANGED BATTERIES, OPS CHECKED GOOD. (W) 2L72 4F A6WE 19950310001641995031000164WP 1995 3 10 ORJA95010 119950208A2720MS20470AD810 RIVETS DOUG DC9 DC983 3022083WP RUDDER DAMPERS BROKEN A ORJAO OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 WP11876RA 53183 RNO - DURING TAXI OUT WITH RUDDER POWERED, LARGE VIBRATION FELT IN RUDDER PEDALS. VIBRATION STOPS WHEN RUDDER IS UNPOWERED. REPLACED SHEAR RIVETS ON BOTH UPPER AND LOWER RUDDER DAMPERS. CYCLED RUDDER, OPS NORMAL. (W) 2L72 4F RTA6WE 19950310001651995031000165WP 1995 3 10 ORJA95011 119950209A3260 PROX SWITCH DOUG DC9 DC982 3022082WP NLG DIRTY A ORJAO OTHER N FALSE WARNING CLCLIMB 1 WP11842RA 49604 SJC - ON DEPARTURE, GEAR RETRACTED, NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. COMPLIED WITH ABNORMAL AOM PROCEDURED LIGHT WENT OUT. CLEANED SURFACE OF PROX SWITCH, RETRACTED GEAR SEVERAL TIMES, NO ABNORMALITIES PER MM 32-20-00. (W) 2L72 4F A6WE 19950310001661995031000166WP 1995 3 10 ORJA95012 119950215A335041B004AD073 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11876RA 53183 EMERGENCY OVERHEAD LIGHTS INOP AT ROW 29, LT AND RT SIDES. REMOVED AND REPLACED BATTERIES. (W) 2L72 4F RTA6WE 19950310001671995031000167NM 1995 3 10 PCAA9500183 119950103A3350 EEL DHAV DHC8 DHC8102 2809003NM CABIN INOP A PCAAK NONE L NO TEST ININSP/MAINT 1 EA132FOR 215 THE FLOOR LEVEL EMERGENCY LIGHTS AND MID CABIN EXIT SIGNS INOP. FERRIED ACFT TO LGA FOR REPAIR. CREW REPORTS CONDITION NO LONGER EXITS. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001681995031000168NM 1995 3 10 PCAA9500184 119950104A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LT MLG LACK OF LUBE A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13810EX 308 UPON SELECTION OF GEAR DOWN, LT MAIN DID NOT EXTEND FOR ABOUT 20 SECONDS. GEAR THEN WENT DOWN AND LOCKED, GOT THREE GREEN LIGHTS. LUBED GEAR ACTUATORS AND UPLOCK INSPECTED GEAR, PERFORMED SATISFACTORY TEST FLIGHT. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001691995031000169NE 1995 3 10 PCAA9500185 219950108A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 FAILED A PCAAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 EA13821EX13230 173 120939 THE NR 1 ENGINE SHUTDOWN IN FLIGHT. INSPECTED AND FOUND ACCESSORY GEAR DRIVE SHIFTED AND OIL COMTAMINATED WITH METAL. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY AND OIL COOLER. LEAK AND OPERATIONALLY CHECKED GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA13NM E20NE 19950310001701995031000170NM 1995 3 10 PCAA9500187 119950109A3350 EEL WIRE DHAV DHC8 DHC8102 2809003NM CABIN BROKEN A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13805EX 228 THE THIRD AND FOURTH EMERGENCY ESCAPE PATH LIGHTS INOP. ALSO, THE EXTERIOR EMERGENCY LIGHT INOP. REPLACED BROKEN WIRE AND REPAIRED BROKEN WIRE IN CABIN FLOOR. OP CHECKS GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001711995031000171NM 1995 3 10 PCAA9500188 119950118A3260855401 PROX SW DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A PCAAO OTHER N FALSE WARNING CLCLIMB 1 EA13816EX 329 WHEN GEAR WAS SELECTED UP, THE RT MAIN DID NOT RETRACT. THE LT AND NOSE GEAR INDICATED RETRACTED. THE RT GEAR HAD A RED INTRANSIT LIGHT WITH NO GEAR DOOR INDICATION. FOUND THE RT UPLOCK PROXIMITY SENSOR BAD. REMOVED AND REPLACED SENSOR, SWUNG GEAR AND BLED SYSTEM. SYSTEM CHECKS GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001721995031000172NM 1995 3 10 PCAA9500189 119950125A2913 HYD PUMP DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13806EX 263 THE NR 2 HYDRAULIC PUMP FAILED WHEN LANDING GEAR WAS EXTENDED. SUSPECT AIR WAS DRAWN INTO HYDRAULIC SYSTEM BY BACKWARDS WINDMILLING PROP. BLED SYSTEM OF AIR. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP DUE TO HAVING OPERATED WHILE CAVITATED. GROUND CHECK OK. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001731995031000173NM 1995 3 10 PCAA9500191 119950130A335010005511 EEL DHAV DHC8 DHC8102 2809003NM CABIN FAILED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13805EX3163 228 THE FLIGHT COMPARTMENT OVERHEAD EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT. OPS CHECK OK. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950310001841995031000184EU 1995 3 10 USAA950090 119950206A2150 PACK FOKKERF28 F28MK0100 4990807EU NR 1 MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19867US 11312 LGA - FLT 1156 - DURING FLIGHT THERE WAS DEPRESSURIZATION. THE NR 1 PACK FAULTED. CAPTAIN GOT THE CABIN PRESSURE UNDER CONTROL. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED NR 1 PACK WITH ENGINE BLEED AND APU AIR. CHECKS SATISFACTORY. NO FAULT PRESENT. (W) 2L72 4F RT 19950310002571995031000257NM 1995 3 10 95013392284 119950228A27821U109592 ACTUATOR BOEING727 727251 138408HNM NR 8 LE SLAT FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL01284US2437855 21323 DURING FLIGHT, THE NR 8 LEADING EDGE SLAT INTRANSIT INDICATION ILLUMINATED. SLAT POSITION CONFIRMED UP VISUALLY. DIVERTED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 8 LEADING EDGE SLAT ACTUATOR. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950310002581995031000258EU 1995 3 10 9503353202 119950131A71102380302509 SKIN AIRBUS320 A320211 3930320EU NR 1/2 ENG COWL DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01302US 32 DURING C-CHECK, FOUND THE NR 1 AND NR 2 ENGINE FAN COWLS RIGHT SIDE WITH 22 INCH BY 28 INCH AND 20 INCH BY 28 INCH AREA OF DELAMINATION RESPECTIVELY. REPAIRS ACCOMPLISHED PER NWA EA 32-96350 AND EA 32-96349. 2L72 4F RTA28NM 19950310002591995031000259WP 1995 3 10 9503369970 119950301A2421976J2526 AC GENERATOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN EHTVIBRATION/BUFFET ELECT. POWER LOSS-50 PC ENGINE CASE PENETRATION CLCLIMB 1 GL019334 348468075 47247 657499 EN ROUTE DTW-ROC, THE NR 2 GENERATOR EXPERIENCED AN UNCONTAINED FAILURE. THE GENERATOR FAILURE PENETRATED THE ENGINE FAN CASE CAUSING NR 2 ENGINE TO VIBRATE. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO BUF LANDING WITHOUT INCIDENT. THE ENGINE WAS REPLACED, RUN-UP, AND TESTED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950310002601995031000260WP 1995 3 10 9503379152 119950228A793141800044 TRANSMITTER DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL018911E497 497 45825 657550 THE NR 2 ENGINE OIL PRESSURE INDICATOR EXCEEDED NORMAL LIMITS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 80 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER. THE SYSTEM CHECKED OK AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950310002611995031000261NE 1995 3 10 9503389302 219950228A7230 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE STALLED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CLCLIMB 1 GL01302RC 48055 708431 CLIMBING OUT OF PHL, THE NR 1 ENGINE N1 WAS NEAR THE YELLOW ARC AND EPR WAS LOW. AT APPROXIMATELY FL300, A COMPRESSOR STALL AND VIBRATION OCCURRED IN THE NR 1 ENGINE. THE ENGINE WAS SHUT DOWN. THE FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. THE ENGINE WAS REPLACED, RUN-UP, AND CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E9NE 19950310002621995031000262NM 1995 3 10 9503392284 119950228A27821U109592 ACTUATOR BOEING727 727251 138408HNM NR 8 LE SLAT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL01284US2437855 21323 DURING FLIGHT, THE NR 8 LEADING EDGE SLAT INTRANSIT INDICATION ILLUMINATED. SLAT POSITION CONFIRMED UP VISUALLY. DIVERTED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 8 LEADING EDGE SLAT ACTUATOR. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950310002631995031000263WP 1995 3 10 9503401226 119950228A5330 SKIN DOUG DC10 DC1030 3023501WP FS 1880 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE BELLY SKIN AT FS 1880, BL 0. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 12-96763. 2L73 4F A22WE 19950310002641995031000264WP 1995 3 10 9503411227 119950304A2781806125 PROX UNIT DOUG DC10 DC1030 3023501WP LE FLAPS FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01227NW1068310683 46969 DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED AND THE SLAT DISAGREEMENT LIGHT ILLUMINATED. ABORTED TAKEOFF. REPLACED THE ELECTRONIC PROXIMITY UNIT. OPERATIONAL CHECK OK. 2L73 4F A22WE 19950310002661995031000266EU 1995 3 10 COM31038 119950301A6120 AUTO COARSEN SAAB SF340 SF340A 7850100EU ENGINE INOP A COMACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01344CA 340A025 AUTO COARSEN IS INOP. COULD NOT DUPLICATE. AUTO COARSEN SYSTEM TEST NORMAL. 2L72 4T RTA52EU 19950310002671995031000267 1995 3 10 COM31039 419950301A23404970114010 PA CRADLE ASSY SAAB SF340 SF340A 7850100EU COCKPIT ODOR A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01358CA218699702 340A047 TOXIC SMELL IN COCKPIT. REPLACED THE CABIN PA SYSTEM CRADLE ASSY. 2L72 4T RTA52EU 19950310002681995031000268WP 1995 3 10 MWEA95140 119950304A523059101577N DOOR PAN DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE INSP THE AFT CARGO DOOR PAN WAS FOUND TO BE CRACKED AT A PREVIOUS REPAIR ON FWD LOWER SIDE. REPAIRED AFT CARGO DOOR IAW SRM 52-05, FIG 50. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950310002691995031000269WP 1995 3 10 MWEA95141 119950304A5320 DOOR JAMB DOUG DC9 DC915 3022036WP FWD ENT DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING ROUTINE INSPECTION IT WAS FOUND THAT FWD PAX ENTRANCE DOOR JAMB HAD A 1.25 INCH CRACK AT UPPER FWD CORNER. REPAIRED DOOR JAMB IAW SRM 53-05, FIG, 26. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950310002701995031000270EU 1995 3 10 QXEA9500064 119950304A3350 EEL FOKKERF28 F28MK1000 4990808EU CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 THE EMERGENCY EXIT HANDLE LIGHT ON THE LEFT SIDE ROW 8 IS INOPERATIVE. REMOVED AND REPLACED THE LAMP, OPERATIONAL CHECKS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950310002711995031000271EU 1995 3 10 QXEA9500065 119950304A3350 EEL BULB FOKKERF28 F28MK1000 4990808EU COCKPIT FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09802PH 11017 THE EMERGENCY EXIT SIGNS ABOVE THE COCKPIT DOOR AND ENTRANCE TO THE CABIN ARE INOPERATIVE. RELAMPED THE LIGHTS AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950310002721995031000272SW 1995 3 10 QXEA9500066 119950306A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NOSE GEAR BROKEN A QXEAK NONE P NO WARNING INDICATION APAPPROACH 1 NM092734X AC738 THE NOSE GEAR INTRANSIT LIGHT IS INOPERATIVE WHEN PUTTING THE GEAR DOWN, THE GEAR OPERATES NORMALY WHEN RETRACTED. REPLACED THE LEFT UP POSITION SWITCH PER THE WIRING MANUAL 32-60-02 P 1A SHEET 1, OPERATIONAL CHECKED GOOD IAW M.M. 32-00-00 PG 201-203 AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T A8SW 19950310002731995031000273NM 1995 3 10 UPS202555 119950303A5320 EXPANSION LINK BOEING727 727173C 1384059NM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK BOLT ATTACH POINTS BS740-760, LBL 25, WL 207. INSTALLED REPAIR PER SRM 51-10-6, 51-10-1, 51-10-2, 51-20-4, 51-30-2, OHM 20-50-3, MM51-20-151. 2L73 4F A3WE 19950310002741995031000274NM 1995 3 10 UPS202556 119950303A5320 SPLICE PLATE BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON UPPER SPLICE PLATE BS 870, RBL 65-70. REPLACED PER SRM 51-10-1, 51-30-2, 51-20-4. 2L73 4F A3WE 19950310002751995031000275NM 1995 3 10 UPS202557 119950303A5313 STRINGER BOEING727 727173C 1384059NM BS 510 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 21L AT BS 510. INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950310002761995031000276NM 1995 3 10 UPS202558 119950303A5341 BODY FORGING BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STA 870 BODY FORGING, WL 90, RBL 65-70. INSTALLED REPAIR PER SRM 51-10-6, 51-10-2, 51-30-10, OHM 20-10-3, MM 51-20-00. 2L73 4F A3WE 19950310002771995031000277NM 1995 3 10 UPS202559 119950303A5313 STRINGER BOEING727 727173C 1384059NM BS 1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON AFT UPPER AND LWR SIDES OF STR 20R, BS 1050, RBL 60, WL 180. INSTALLED REPAIR PER SRM 53-10-3, 51-30-2,51-20-21. 2L73 4F A3WE 19950310002781995031000278NM 1995 3 10 UPS202560 119950303A5311 FRAME BOEING727 727173C 1384059NM BS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 660 BETWEEN STR 22-23L, AND FRAME CRACKED AT STR 25L. INSTALLED REPAIR PER SRM 51-40-3. 2L73 4F A3WE 19950310002791995031000279NM 1995 3 10 UPS202561 119950303A5754 SKIN BOEING727 727173C 1384059NM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED PER MM 27-81-00, 27-81-01. 2L73 4F A3WE 19950310002801995031000280NM 1995 3 10 UPS202564 119950303A5311 FRAME BOEING727 727173C 1384059NM BS 1090 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT BS 1090, RBL 70.5, WL 202. REPLACED PER SRM 51-30-2, 51-10-1, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950310002811995031000281NM 1995 3 10 UPS202565 119950303A5320 STIFFENER BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, RBL 8.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1. 2L73 4F A3WE 19950310002821995031000282NM 1995 3 10 UPS202566 119950303A5320 STIFFENER BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, RBL 16.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1. 2L73 4F A3WE 19950310002831995031000283NM 1995 3 10 UPS202567 119950303A5320 STIFFENER BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STIFFENER STA 870, LBL 8.0, WL 180. REPLACED PER SRM 51-30-2, 51-30-5, 51-10-1. 2L73 4F A3WE 19950310002841995031000284NM 1995 3 10 UPS202568 119950303A5347 SEAT TRACK BOEING727 727173C 1384059NM BS 570-640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION IN FWD CARGO BAY IN 'WELL' OF FLOOR TRACK AT STA 570-640, LBL 18, WL 155. INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, 51-10-02. 2L73 4F A3WE 19950310002851995031000285NM 1995 3 10 UPS202569 119950303A5320 ANGLE BOEING727 727173C 1384059NM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON ANGLE AT BS 760 LBL 62 WL 205 ATTACHED TO FUSELAGE FRAME. INSTALLED REPAIR PER SRM 51-30-2, 51-20-4, 51-10-2, 51-20-1. 2L73 4F A3WE 19950310002861995031000286NM 1995 3 10 UPS202570 119950303A5311 FRAME BOEING727 727173C 1384059NM BS 500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 500, NEAR STR 20-24L. INSTALLED REPAIR PER SRM 53-10-2, 51-40-3, 51-30-2. 2L73 4F A3WE 19950310002871995031000287NM 1995 3 10 UPS202571 119950303A5347 SEAT TRACK LINK BOEING727 727173C 1384059NM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK EXPANSION LINK FROM BS 740-760, LBL 45, WL 208. INSTALLED REPAIR PER SRM 53-10-1, 51-30-2, OHM 20-50-03. 2L73 4F A3WE 19950310002881995031000288NM 1995 3 10 UPS202572 119950303A5347 SEAT TRACK BOEING727 727173C 1384059NM BS 960-1176 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON FLANGES OF SEAT TRACK STA 960-1176, BL 0, WL 208. INSTALLED REPAIR PER SRM 53-10-1, 51-10-1, 51-30-2. 2L73 4F A3WE 19950310002891995031000289NM 1995 3 10 UPS202573 119950303A5755 NR 3 SPOILER BOEING727 727173C 1384059NM LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE AND CONTAMINATION ON NR 3 SPOILER. REPLACED PER MM 27-61-01. 2L73 4F A3WE 19950310002901995031000290NM 1995 3 10 UPS202574 119950306A5755 NR 4 SPOILER BOEING727 727173C 1384059NM LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE ON NR 4 SPOILER. REPLACED PER MM 27-61-01. 2L73 4F A3WE 19950310002911995031000291NM 1995 3 10 UPS202575 119950306A5755 NR 5 SPOILER BOEING727 727173C 1384059NM LT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 5 SPOILER. INSATLLED REPAIR PER SRM 51-40-6, 57-50-6. 2L73 4F A3WE 19950310002921995031000292NM 1995 3 10 UPS202576 119950306A5320 WEB BOEING727 727173C 1384059NM BS 1110-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON WEB STA 1110-1130, RBL 60-65, WL 208. INSTALLED REPAIR PER SRM 51-10-6, 51-40-0. 2L73 4F A3WE 19950310002931995031000293NM 1995 3 10 UPS202577 119950306A5320 WEB BOEING727 727173C 1384059NM BS 1110-1130 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON WEB AROUND FASTENER HOLES, STA 1110-1130, RBL 26, WL 208. INSTALLED REPAIR PER SRM 51-10-1, 51-10-2, 51-30-2. 2L73 4F A3WE 19950310002941995031000294NM 1995 3 10 UPS202593 119950306A5720 CHORD BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FLANGE OF THE 740 CHORD RBL 10-45. INSTALLED REPAIR PER UPS EO B727-5710-6628A AND B727-5710-6763. 2L73 4F A3WE 19950310002951995031000295NM 1995 3 10 UPS202594 119950306A5311 FRAME BOEING727 727173C 1384059NM BS 500 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FRAME AROUND FASTENER HOLES AT BS 500 AT OR NEAR STRINGER 21-26R. STRINGER 19R HAS CRACK AT SAME LOCATION. INSTALLED REPAIR PER SRM 51-10-2, 51-40-5, 51-40-3, 51-30-2. 2L73 4F A3WE 19950310002961995031000296NM 1995 3 10 UPS202595 119950306A5743 FWD TRUNNION BOEING727 727173C 1384059NM RT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON RT MLG RT FWD TRUNNION FITTING INNER FACES AROUND BUSHING BORES. REPLACED PER SRM 51-30-2. 2L73 4F A3WE 19950310002971995031000297NM 1995 3 10 UPS202596 119950306A5315 FLOOR BEAM BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON LWR FLANGE OF FLOOR BEAM BS 740, WL 199, RBL 4-LBL 4. INSTALLED REPAIR PER UPS EO B727-5310-6752A. 2L73 4F A3WE 19950310002981995031000298NM 1995 3 10 UPS202598 119950306A5712 RIB CHORD BOEING727 727173C 1384059NM WING/BODY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON UPPER VERTICAL FLANGE OF THE WING TO BODY RIB UPPER CHORDS AT BS 760, RBL 70.5, AND LBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-1271F. 2L73 4F A3WE 19950310002991995031000299NM 1995 3 10 UPS202599 119950306A5330 SKIN BOEING727 727173C 1384059NM BS 850-863 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON INTERNAL SKIN AT STA 850-863, WL 192, RBL 70. INSTALLED REPAIR PER UPS EO B727-5310-6754A. 2L73 4F A3WE 19950310003001995031000300NM 1995 3 10 UPS202600 119950306A5320 FORGING BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 870 BODY FORGING, FWD SIDE, WL 190, LBL 65-70. INSTALLED REPAIR PER UPS EO B727-5310-6769. 2L73 4F A3WE 19950310003011995031000301NM 1995 3 10 UPS202601 119950306A5330 SKIN BOEING727 727173C 1384059NM BS 870-855 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON INTERNAL SKIN BS 870-855, WL 192, LBL 70. INSTALLED REPAIR PER UPS EO B727-5310-6754. 2L73 4F A3WE 19950310003021995031000302NM 1995 3 10 UPS202602 119950306A5320 FORGING BOEING727 727173C 1384059NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 870 BODY FORGING WL 208.1, RBL 59-64, UNDER FLOOR BEAM. INSTALLED REPAIR PER UPS EO B727-5310-6771A. 2L73 4F A3WE 19950310003031995031000303NM 1995 3 10 UPS202603 119950306A5320 FORGING BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 740 BODY FORGING WL 206-209, RBL 65. INSTALLED REPAIR PER UPS EO B727-5310-6770A. 2L73 4F A3WE 19950310003041995031000304NM 1995 3 10 UPS202604 119950306A5320 FORGING BOEING727 727173C 1384059NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON 740 BODY FORGING WL 206-208, LBL 65. INSTALLED REPAIR PER UPS EO B727-5310-6770A. 2L73 4F A3WE 19950310003051995031000305NM 1995 3 10 UPS202605 119950306A5320 FORGING BOEING727 727173C 1384059NM BS 870 CORR/CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACKS AND CORROSION ON 870 BODY FORGING FLANGES WL 207-205, LBL 58-LBL 64. INSTALLED REPAIR PER UPS EO B727-5310-6771A. 2L73 4F A3WE 19950310003061995031000306NM 1995 3 10 UPS202606 119950306A5311 FRAME BOEING727 727173C 1384059NM BS 480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND TWO CRACKS ON FRAME AT BS 480, BETWEEN STRINGERS 22L AND 23L. INSTALLED REPAIR PER UPS EO B727-5310-6760A. 2L73 4F A3WE 19950310003071995031000307NM 1995 3 10 UPS202607 119950306A5754 NR 3 LE FLAP BOEING727 727173C 1384059NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950310003081995031000308WP 1995 3 10 UPS802608 119950306A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BULKHEAD AT STA 683 BETWEEN STRINGERS 30R-31R. INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F RT4A25 19950310003091995031000309WP 1995 3 10 UPS802609 119950306A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BULKHEAD AT STA 683 BETWEEN STRINGERS 30L-31L. INSTALLED REPAIR UPS EO DC8-5310-6755A. 2L74 4F RT4A25 19950310003101995031000310WP 1995 3 10 UPS802610 119950306A5522 SKIN DOUG DC8 DC873F 302199FWP LT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LEFT ELEVATOR TOP SKIN O/B OF NR 3 HINGE, 8 INCHES AFT OF T-CAP. REPLACED PER SRM 55-2-1. 2L74 4F RT4A25 19950310003111995031000311WP 1995 3 10 UPS802611 119950306A5311 BELTFRAME DOUG DC8 DC873F 302199FWP BS 240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON BELTFRAME STA 240, LONGERON 34-35L. INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950310003121995031000312WP 1995 3 10 UPS802612 119950306A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 340 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LONGERON 21L FWD SIDE OF STA 340. INSTALLED REPAIR PER UPS EO DC8-5310-6682A. 2L74 4F RT4A25 19950310003131995031000313WP 1995 3 10 UPS802613 119950306A5320 ANGLE DOUG DC8 DC873F 302199FWP NR 1 PIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 46140 WHILE IN 'B' CHECK, MAINTENANCE FOUND A CRACK IN FWD VERTICAL 'V' ANGLE NR 1 PIT, LWR SECTION BETWEEN BOLT HOLES. REPAIRED PER UPS EO DC8-5310-6773A. 2L74 4F RT4A25 19950310003141995031000314WP 1995 3 10 UPS802614 119950306A5330 SKIN DOUG DC8 DC873F 302199FWP NLG WW CUTOUT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 46140 WHILE IN 'B' CHECK, MAINTENANCE FOUND A CRACK IN FUS SKIN AFT LEFT CORNER OF NOSE WHEEL WELL CUT OUT. REPAIRED PER UPS EO DC8-5330-4154A. 2L74 4F RT4A25 19950310003151995031000315SW 1995 3 10 MALA954300 119950206A3260 INTRANSIT LIGHT SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15424MA AC639 FLT 3455 - ON APPROACH TO DTW, THE NOSE GEAR RED INTRANSIT LIGHT FAILED TO ILLUMINATE DURING THE GEAR EXTENSION. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310003161995031000316 1995 3 10 MALA954301 419950209A34215040030911 ATTITUDE SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15428MA AC646 FLT 3467 - UPON DEPARTURE FROM DTW, THE ARTIFICIAL HORIZON TUMBLED DURING ROTATION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 ATTITUDE GYRO. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310003171995031000317NM 1995 3 10 MALA954302 119950208A3230101655 UPLOCK ROLLER DHAV DHC8 DHC8102 2809003NM RT MLG FROZEN A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15826MA 330 FLT 3336 - ON APPROACH TO CMX, THE RIGHT GEAR DIDN'T INDICATE DOWN AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ROLLER. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310003181995031000318NM 1995 3 10 MALA954303 119950208A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15829MA 335 FLT 3125 - ON APPROACH TO ESC, THE LEFT UNSAFE GEAR DOWN INDICATION LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE CREW PERFORMED THE ALTERNATE GEAR EXTENSION PROCEDURES. ALL GEAR EXTENDED NORMALLY. THE AIRCRAFT CONTINUED TO ESC. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310003191995031000319 1995 3 10 MALA954304 419950210A3416 ALTIMETER SWRNGNSA227 SA227AC 8780603SW NR 1 MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15446MA AC693 FLT 3144 - AFTER TAKEOFF FROM DTW, THE NR 1 ALTIMETER AND ALTITUDE ALERTER FLAGGED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE NR 1 ALTIMETER WAS REPLACED. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310003201995031000320SW 1995 3 10 MALA954307 119950211A32301EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF RIG A MALAO OTHER O OTHER CLCLIMB 1 GL15438MA AC721 FLT 3447 - DURING THE CLIMB-OUT FROM TVF, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND THE PROBLEM CONTINUED. THE AIRCRAFT CONTINUED TO MSP WITH THE GEAR DOWN. MAINTENANCE RERIGGED THE UPLIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310003211995031000321SW 1995 3 10 MALA954309 119950210A5270V31 DOOR SWITCH SWRNGNSA227 SA227AC 8780603SW CARGO DOOR OUT OF RIG A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15159MC AC728 FLT 3222 - IN CRUISE FLIGHT, THE CARGO DOOR UNSAFE LIGHTS ILLUMINATED. THE CREW REDUCED THE PRESSURE DIFFERENTIAL TO ZERO AND THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE ADJUSTED THE CARGO HANDLE MICROSWITCH. SYSTEM OPERATED SATISFACTORILY. (Z) 1L72 4T A8SW 19950310003221995031000322NM 1995 3 10 MALA954317 119950213A2611 SMOKE LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15833MA 343 FLT 3022 - IN CRUISE FLIGHT TO CWA, THE 'SMOKE' LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDURES. THE CREW DIDN'T NOTE ANY EVIDENCE OF SMOKE OR FIRE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE SMOKE DETECTOR CONTROL AMPLIFIER WAS REPLACED. SYSTEM OPERATED SATISFACTORILY. (Z) 2H72 4T RTA13NM 19950310003681995031000368NM 1995 3 10 SCNA95001 119950101A2612894120 FIRE DET BOEING727 7272A1 138407FNM NR 3 ENGINE FAULTY A SCNAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 GL15287SC 2717 21345 MSP - FLT 688 THE NR 3 ENGINE FIRE LOOP GROUND CIRCUIT DETECTOR LOOP FLICKERED ON BUMPS DURING TAXI. REMOVED AND REPLACED NR 3 ENGINE FIRE DETECTOR LOOP M447 IAW 26-11-12. PERFORMED ADJUSTMENT TEST 26-11-01. OPS CHECK GOOD DURING ENGINE RUN AND TAXI TO GATE. (W) 2L73 4F A3WE 19950310003691995031000369NM 1995 3 10 SCNA95002 119950102A3350 EEL LAMPS BOEING727 7272A1 138407FNM L1 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 MSP - THE L1 DOOR EMERGENCY OUTSIDE LIGHT INOPERATIVE. RELAMPED L1 DOOR OUTSIDE EMERGENCY LIGHT PER 33-50-11. OPS CHECKS GOOD. (W) 2L73 4F A3WE 19950310003701995031000370NM 1995 3 10 SCNA95005 119950103A33501000677 EEL ASSY BOEING727 727282 2F0R NM COCKPIT FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 2976 21949 MSP - EMERGENCY LIGHT OVER COCKPIT DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER COCKPIT DOOR. OPERATIONAL CHECK GOOD PER 33-50-00. (W) 2L73 4F RTA3WE 19950310003711995031000371WP 1995 3 10 SCNA95006 119950103A3350 EEL TRACK DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15572SC 46977 MSP - THE FWD CABIN, LT AFT EMERGENCY TRACK LIGHTING IS INOPERATIVE. REPAIRED BROKEN WIRE AT 6 G, TRACK LIGHTING CHECKED GOOD PER 33-50-00. (W) 2L73 4F A22WE 19950310003721995031000372NM 1995 3 10 SCNA95009 119950113A335010617844 EEL BATTERIES BOEING727 7272A1 138407FNM AFT AIRSTAIR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15286SC 21601 MSP - AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK PER B727 MM 33-50-00. (W) 2L73 4F A3WE 19950310003731995031000373WP 1995 3 10 SCNA95010 119950120A2611DDK1060 SMOKE DET DOUG DC10 DC1010 3022110WP FWD DIRTY A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15573SC 46905 MSP - THE FWD GALLEY SMOKE DETECTOR BEEPS INTERMITTENTLY. UNABLE TO DUPLICATE PROBLEM, BLEW DUST OUT OF ALL LAV SMOKE DETECTORS PRECAUTIONARY AND OPERATIONAL CHECKED GOOD. (W) 2L73 4F A22WE 19950310003741995031000374NM 1995 3 10 SCNA95012 119950123A3243AV24E1144 VALVE BOEING727 7272J4 1384006NM PARKING BRAKE LEAKS A SCNAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15288SC H37097 20765 MSP - ACFT RETURNED TO GATE, CREW REPORTED SMOKE IN CABIN AND COCKPIT. FOUND THE PARKING BRAKE VALVE LEAKING SKYDROL INTO APU INTAKE. REPLACED VALVE AND OPERATIONS CHECKED NORMAL. (W) 2L73 4F RTA3WE 19950310003751995031000375NM 1995 3 10 SCNA95013 119950125A2611 SMOKE DET BOEING727 7272J4 1384006NM AFT LAV DISCHARGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15288SC 20765 MSP - AFT LAVATORY SMOKE DETECTOR INOPERATIVE. INSTALLED NEW BATTERY AND TESTED GOOD. (W) 2L73 4F RTA3WE 19950310003761995031000376NM 1995 3 10 SCNA95014 119950125A3350 EEL TRACK BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 21438 MSP - FOUND EMERGENCY TRACK LIGHTING IN REAR HALF OF ACFT INOPERATIVE. ALLOWED EMERGENCY TRACK LIGHTING TO CHARGE ON APU POWER AND OPERATIONS CHECKED GOOD. (W) 2L73 4F RTA3WE 19950310003771995031000377NM 1995 3 10 SCNA95016 119950127A3350900835A EEL BATT PACK BOEING727 7272A1 138407FNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 12884 21345 MSP - L-1 DOOR CENTER AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED GOOD. (W) 2L73 4F A3WE 19950310003781995031000378NM 1995 3 10 SCNA95020 119950207A33506013211 EEL POWER SUPPLY BOEING727 727282 2F0R NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 8703 21949 MSP - THE L1 AND R1 EMERGENCY ESCAPE SLIDE LIGTHS INOPERATIVE. REMOVED AND REPLACED ESCAPE SLIDE LIGHT POWER SUPPLY M982. (W) 2L73 4F RTA3WE 19950310003791995031000379WP 1995 3 10 SCNA95022 119950209A261172130000010 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 1 LAV DIRTY A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15573SC 3375 46905 MSP - THE FWD NR 1 LAV SMOKE DETECTOR GOES OFF FOR NO APPARENT REASON. CLEANED SMOKE DETECTOR AND RESEATED CANNON PLUG. SMOKE DETECTOR CHECKED GOOD. (W) 2L73 4F A22WE 19950310003801995031000380WP 1995 3 10 SCNA95023 119950210A261172130000010 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 1 LAV FAULTY A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15573SC 3375 46905 MSP - THE NR 1 LAV SMOKE DETECTOR RINGING IN OVERHEAD PANEL. REMOVED AND REPLACED SMOKE DETECTOR, OPERATION CHECK GOOD. (W) 2L73 4F A22WE 19950310003811995031000381NM 1995 3 10 SCNA95024 119950218A33501001143 EEL POWER PACK BOEING727 7272A1 138407FNM AFT AIRSTAIR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15286SC 21601 MSP - DURING LINE CHECK FOUND AFT AIRSTAIR EMERGENCY OVERHEAD LIGHT INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY LIGHT POWER PACK, IAW MM 33-50-61 AND OPS CHECKED GOOD. (W) 2L73 4F A3WE 19950310003821995031000382WP 1995 3 10 9502641162 119950120A5315AFA00433 FLOOR BEAM DOUG DC10 DC1040 3023508WP FS 1701 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01162US 46771 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE CENTER CARGO FLOOR BEAM AT FS 1701, RBL 33. REMOVED DAMAGE AND INSTALLED DOUBLERS PER EA 11-93754. 2L73 4F A22WE 19950310003831995031000383NM 1995 3 10 USAA950053 119950104A5320 INTERCOSTAL BOEING737 7373B7 1384580NM FS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19533AU18842 24515 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREWHOLE 1 INCH BY 1 INCH INTERCOSTAL AT RBL 10 BETWEEN 312 AND 328. REPAIRED PER TR 51-70-12 SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310003841995031000384NE 1995 3 10 9503431151 219950304A7261 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01151US 46760 686144 DURING INITIAL CLIMB, THE NR 1 ENGINE EXPERIENCED LOSS OF OIL QUANTITY AND PRESSURE AND WAS SHUT DOWN. 70,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO SFO WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED. BLACK OIL WAS FOUND AND THE AIRCRAFT WAS FERRIED TO MSP FOR AN ENGINE CHANGE. 2L73 4F4 F A22WE E20EA 19950310003851995031000385 1995 3 10 9503446601 419950304A341719039253 CADC BOEING747 747151 1384891NM E/E BAY MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL01601US4140211311 19778 AFTER TAKEOFF, THE NR 1 AND NR 3 INS FAILED. CREW FOLLOWED COCKPIT OPERATING MANUAL AND RETURNED TO NRT. MAINTENANCE REPLACED NR 1 CADC AND PERFORMED BITE AND LEAK CHECK. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19950310003861995031000386NM 1995 3 10 9503456730 119950303A561060B10028102 WINDOW BOEING747 7472J9F 1384806NM NR 1 RIGHT CRACKED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01630US1901619016 21668 EN ROUTE SFO-ANC, FLIGHT DIVERTED TO SEA DUE TO WINDOW 1R CRACKED. MAINTENANCE REPLACED THE WINDOW AND THE AIRCRAFT RETURNED TO SERVICE. 2L74 4F RTA20WE 19950310003871995031000387NM 1995 3 10 9503462715 119950227A5311 FRAME BOEING727 7272S7 138407ZNM FS 783 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01719RC 22490 DURING PERIODIC CHECK, MAINTENANCE FOUND FS 783 FRAME CRACKED ON INBOARD FLANGE WL 203, LEFT HAND SIDE. REPAIRED PER NWA EA 27-096692. 2L73 4F A3WE 19950310003881995031000388NM 1995 3 10 9503472705 119950301A5753 RIB BOEING727 727225 1384077NM TE MID FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 22433 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT WING OUTBOARD MID FLAP CLOSURE RIB CRACKED. REPAIRED PER NWA EA 27-090164. 2L73 4F A3WE 19950310003891995031000389WP 1995 3 10 ABXA9500144 119950303A5510NAS5786B RETAINER DOUG DC9 DC915 3022036WP HORIZ STAB LOOSE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RETAINER LOOSE. SECURED BARREL NUT RETAINER AS REQUIRED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950310003901995031000390WP 1995 3 10 ABXA9500145 119950303A5510LH7456T080 BARREL NUT DOUG DC9 DC915 3022036WP HORIZ STAB RUSTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RUSTED. CLEANED AND TREATED BARREL NUT IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950310003911995031000391WP 1995 3 10 ABXA9500146 119950302A528029242891 BUSHING DOUG DC9 DC932 3022066WP RT MLG DOOR MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47392 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING MISSING IN RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950310003921995031000392SO 1995 3 10 COM11806 119950303A528012019414001 ANGLE EMB 120 EMB120RT SO LT MLG DOOR CRACKED A COMAK NONE O OTHER UKUNKNOWN 1 SO01265CA 120257 LEFT MLG DOOR OPENED IN FLIGHT. REPLACED CRACKED AFT HINGE BRACKET ON MLG DOOR. 2L72 4T RTA31SO 19950310003931995031000393SO 1995 3 10 COM11807 119950303A323018190003 VALVE EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01200CD12141397 120200 LEFT MLG DID NOT FULLY RETRACT, RED INTRANSIT LIGHTS REMAINED ON. REPLACED THE LANDING GEAR SOLENOID VALVE. 2L72 4T RTA31SO 19950310003941995031000394EU 1995 3 10 COM31040 119950302A5270MS213211 SWITCH SAAB SF340 SF340A 7850100EU CABIN DOOR LACK OF LUBE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01342CA 340A023 CABIN DOOR HANDLE WARNING CAME ON DURING CLIMB. CLEANED AND LUBED STICKING DOOR HANDLE MICRO SWITCH. 2L72 4T RTA52EU 19950310003951995031000395EA 1995 3 10 COM60433 119950302A2750855S1005 BPSU CNDAIRCL600 CL6002B19 EA RT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01920CA3599 3410 7022 FLAP FAIL MESSAGE ON EICAS. FLAPS STUCK AT 3 DEGREES. REPLACED THE RT BPSU. 2L72 4F RTA21EA 19950310003961995031000396NM 1995 3 10 DL72E950892 119950227A711065196854141 NOSE COWL BOEING727 727247 138408FNM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 871 NOSE COWL, FLANGE WORN, NR 1 ENG NOSE COWL AFT FLANGE IS WORN TO RAZOR EDGE AT 7:00 POSITION. INSTALLED DOUBLER PER SRM 54-10-3. NR 290. 2L73 4F A3WE 19950310003971995031000397NM 1995 3 10 DL72E950894 119950222A711065196854141 NOSE COWL BOEING727 727247 138408FNM NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 871 TWO TEMP REPAIRS LOCATED AT THE 5:00 AND 6:00 POSITIONS IN THE NOSE COWL LIP SKIN. C/W ERA 258540-14 BY INSTALLING DOUBLER PER SRM 54-30-3 FIGURE 2. N/R'S 202 AND 5. 2L73 4F A3WE 19950310003981995031000398NM 1995 3 10 DL72S950598 119950201A5530 STRINGER BOEING727 727232 1384082NM LT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND STRINGER 4 LT. CRACKED AT 5TH BULKHEAD FROM ACCESS PANEL IN VERTICAL STABILIZER. REPAIRED PER SRM 55. 2L73 4F A3WE 19950310003991995031000399NM 1995 3 10 DL72S950599 119950201A5530 STRINGER BOEING727 727232 1384082NM LT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND STRINGER 9 LT CRACKED AT 3RD BULHEAD UP FROM ACCESS PANEL INSIDE VERTICAL STABILIZER. REPAIRED PER SRM 55. 2L73 4F A3WE 19950310004001995031000400NM 1995 3 10 DL72S950689 119950202A5754 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND NR 2 LEADING EDGE SLAT WITH CRACKED RIB AT 2ND LOCATION FROM THE OUTBD END OF SLAT. REPAIRED PER SRM 57-54-0 PG 819. 2L73 4F A3WE 19950310004011995031000401NM 1995 3 10 DL72S950690 119950201A5754 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 AT HMV, FOUND RT WING NR 6 SLAT WITH THE 2ND RIB FROM THE INBOARD END CRACKED AND 2 CRACKS IN RIB ON THE OUTBARD SIDE OF THE INBOARD TRACK. REPAIRED PER SRM 57-50-3 PG 25. 2L73 4F A3WE 19950310004021995031000402NM 1995 3 10 DL72S950691 119950201A5312 CHANNELS BOEING727 727232 1384082NM FWD BB AFT BLKHDWORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 CHANNELS WORN FWD B/B AFT BULKHEAD TWO VERTICAL SUPPORT CHANNELS ARE WORN (LOC OVER STG 26L AND 26R) AT FLEX JOINTS. ALSO, RIVETS SHEARED LEFT SUPPORT AT CEILING. FOUND AT HMV, REPAIRED PER SRM 53-10-9 FIG 8, REPLACED RIVETS 2L73 4F A3WE 19950310004031995031000403NM 1995 3 10 DL72S950875 119950129A5753 SKIN 6521630188 BOEING727 727232 1384082NM RT TE FORE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 684 21061 DURING INSPECTION TOP SKIN FOUND DENTED AT 46 INCHES AND 60 INCHES FROM I/B END. RT WING NR 3 FORE FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950310004041995031000404NM 1995 3 10 DL72S950876 119950131A57536521630188 LE SKIN BOEING727 727232 1384082NM NR 3 FORE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING SHOP VISIT LE WAS FOUND WORN 17 INCHES AND 22 INCHES FROM IB END. A REPAIR DOUBLER WAS INSTALLED PER SRM 57504 AFTER IT WAS DETERMINED THAT WEAR EXCEEDED ALLOWABLE DAMAGE LIMITS OF SRM 57-50-01 FOR NR 3 FORE FLAP. 2L73 4F A3WE 19950310004051995031000405NM 1995 3 10 DL72S950895 119950130A5753652163361 RETAINER BOEING727 727232 1384082NM NR 1 TE MID FLAPCORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 871 NR 1 MID FLAP, I/B CARRIAGE SUPPORT FITTING, THRUST BEARING RETAINER UPPER BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG. 14, OVERSIZED HOLES AND INSTALLED BUSHINGS. 2L73 4F A3WE 19950310004061995031000406NM 1995 3 10 DL72S950896 119950130A5753652163361 SUPPORT BOEING727 727232 1384082NM NR 1 MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 871 NR 1 MID FLAP, O/B CARRIAGE SUPPORT FITTING, THURST BEARING RETAINER UPPER I/B AND O/B BOLT HOLES CORRODED ALSO LOWER I/B BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14. OVERSIZED HOLES AND INSTALLED BUSHINGS. 2L73 4F A3WE 19950310004071995031000407NM 1995 3 10 DL72S950897 119950130A5753652163361 THRUST BEARING BOEING727 727232 1384082NM NR 1 TE MID FLAPCORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 871 NR 1 MID FLAP, O/B THRUST BEARING BORE CORRODED. REPAIRED PER SRM 575004 FIG 15. MACHINED OVERSIZE AND INSTALLED BUSHING. 2L73 4F A3WE 19950310004081995031000408NM 1995 3 10 DL72S950898 119950130A5753652163361 RIB BOEING727 727232 1384082NM NR 1 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 871 NR 1 MID FLAP, I/B AFT RIB CRACKED. REPAIRED PER SRM 575200 INSTALLED DOUBLER. 2L73 4F A3WE 19950310004091995031000409NM 1995 3 10 DL72W950883 119950104A5753 SKIN 6521631262 BOEING727 727247 138408FNM RT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA BN394 22109 DURING SHOP INSPECTION, DELAMINATION FOUND LOWER SKIN 25 IN FROM O/B END. RIGHT WING FLAP PANEL, REPAIRED PER SRM 57-50-1 WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950310004101995031000410NM 1995 3 10 DL72W950884 119950104A5753 SKIN 6521631262 BOEING727 727247 138408FNM RT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA BN394 22109 DURING SHOP INSPECTION, FOUND TO BE DELAMINATED AT LOWER SKIN I/B TRAILING EDGE. RIGHT WING FLAP PANEL, REPAIRED PER SRM 57-50-1 WITH REF TO 51-40-6. 2L73 4F A3WE 19950310004111995031000411NM 1995 3 10 DL72W950886 119950104A5753 SKIN 6521631262 BOEING727 727247 138408FNM RT TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA BN394 22109 DURING SHOP INSPECTION, FOUND CRACK IN L/E SKIN AT 153 IN FROM O/B END. RIGHT WING FLAP PANEL. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950310004121995031000412NM 1995 3 10 DL733950893 119950218A5755 SKIN 65C2524216A BOEING737 737347 1384647NM INBD SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA MA2354 23442 871 DURING ROUTINE INSPECTION, SEVERAL SMALL DENTS AND ONE SKIN PUNCTURE WERE FOUND ON INSIDE SKIN OF I/B SPOILER. DAMAGE WAS CAUSED FROM DEBRIS THROWN FROM THE MAIN LANDING GEAR. REPAIRED THE DAMAGE PER SRM 57-50-5. 2L72 4F RTA16WE 19950310004131995031000413NM 1995 3 10 DL757950891 119950302A2420FRF6365501747 CONNECTOR BOEING757 757232 1384965NM NR 2 ENGINE FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11684DA 27104 RIGHT ENGINE GENERATOR HAS HISTORY OF DROPPING OF LINE ON CLIMB-OUT AND CRUISE FOUND PLUG AND RECEPTABLE DAMAGED AND ARCED TOGETHER RIGHT ENG GENERATOR OFF LIT ILLUMINATED PIN B ON CONNECTOR WAS OPEN. CONNECTOR D01292J MFG PN FRF0-36-5P03-747 AND D1092P. REPLACED CONNECTOR AND REPAIRED DAMAGED WIRING OPERATION NORMAL. 2L72 4F RTA2NM 19950310004141995031000414WP 1995 3 10 DLL10950854 119950227A5743 TRUNNION FITTING LKHEED1011 10113851 5265010WP MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11725DA 193C1162 PAINT PEELING AND RUST ON O/B SURFACE OF MLG TRUNNION FITTING. CLEAN CORROSION PER SRM 57-14-00 FIG 804 DAMAGE FOUND AT LETTER CHECK. 2L73 4F A23WE 19950310004151995031000415WP 1995 3 10 DLL10950855 119950226A3211 FITTING LKHEED1011 10113851 5265010WP MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11725DA 193C1162 REF TASK NR 32-730-01 MLG FITTING HAS LARGE AREAS OF RUST ON IB SIDE OF FITTING. REPAIR PER SRM 57-14-00 FIG 804. FOUND AT LETTER CHECK. 2L73 4F A23WE 19950310004161995031000416WP 1995 3 10 DLL10950856 119950225A3211 GEAR FITTING LKHEED1011 10113851 5265010WP RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11725DA 193C1162 REF TASK C-32-730-01 RT MLG I/B SIDE OF GEAR FITTING BETWEEN FWD AND AFT FITTINGS PAINT IS PEELED AND LARGE AREAS OF RUST. FOUND AT LETTER CHECK, REPAIRED PER 57-14-00 FIG 804. 2L73 4F A23WE 19950310004171995031000417WP 1995 3 10 DLL10950885 119950222A57531529113111 SKIN LKHEED1011 10113851 5265010WP LT TE FLAP VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 DURING SHOP INSPECTION, LEFT WING FLAP VANE WAS FOUND WITH TWO CRACKS IN THE UPPER SKIN. REPAIRED PER SRM 57-53-00. 2L73 4F A23WE 19950310004181995031000418WP 1995 3 10 DLL15950858 119950227A5522 PANEL LKHEED1011 10113853 5265020WP RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11756DR 193Y1185 RT ELEVATOR OUTBD LIP PNL CRACKED PASSED STOP DRILL HOLE JUST INBD OF OUTBD STATIC WICK UPPER SURFACE. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 55-22-00 FIG 802. DAMAGE FOUND AT LETTER CHECK. 2L73 4F A23WE 19950310004191995031000419NM 1995 3 10 DLM11950830 119950226A5730 SKIN DOUG MD11 MD11 3023602NM WING LE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11808DE 48479 DURING INSPECTION, FOUND WEAR DAMAGE TO WING LEADING EDGE AT THE INTERSECTION OF NR 1 AND NR 2 LEADING EDGE SLATS. REPAIRED PER SRM 57-10-00 PG 63. 2L73 4F RTA22WE 19950310004201995031000420NM 1995 3 10 DLM88950930 119950304A323139567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR FAILED A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11977DL 53258 AFTER TAKEOFF, HEARD LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA AFTER GEAR RETRACTION. RETURNED TPA, FOUND RT NOSE GEAR DOOR OPEN. REPLACED RIGHT DOOR LINK DUE TO NOT LOCKING. 2L72 4F RTA6WE 19950310004211995031000421NM 1995 3 10 DLM88950939 119950222A71105930645501 NOSE COWL DOUG MD88 MD88 3023688NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11901DL 49532 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS REPAIRED FOR GROUND DAMAGE TO THE INTAKE LIP AT THE 4 O'CLOCK POSITION. REPAIRED PER SRM 54-04A FIG 1. 2L72 4F RTA6WE 19950310004221995031000422 1995 3 10 DLM88950941 419950306A3441HG1103BA01 IRU DOUG MD88 MD88 3023688NM E/E COMP FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11991DL 53343 AFTER TAKEOFF, NR 1 INERTIAL REFERENCE UNIT FAILED, WITH ASSOCIATED SYSTEM FAILURES. DIVERTED CVG. REPLACED IRU, OPERATION NORMAL. 2L72 4F RTA6WE 19950310004231995031000423NM 1995 3 10 QXEA9500067 119950306A30202955D5240211 DE-ICE BOOT DORNER 1A716E100004DORNERDO32 DO328100 2996000NM NR 1 ENGINE DEBONDED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09328PH103 1020 3006 PDX - NUMBER ONE ENGINE INLET DE-ICE BOOT P/N 295-5D5240-211 FOUND DEBONDED AT LEFT HAND FORWARD SIDE OF BOOT. DEBOND WAS APPROX 12 SQ IN IN SIZE. REPLACED INLET ASSY I/A/W MAINT MANUAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950310004241995031000424NM 1995 3 10 SCNA95028 119950301A261265378993 OVERHEAT LINE BOEING727 7272J4 1384006NM APU BROKEN A SCNAF ACTIVATE FIRE EXT. N FALSE WARNING ININSP/MAINT 1 GL15288SC 20765 AFTER SHUT DOWN OF APU HAD FIRE INDICATION OF RED LIGHT IN FIRE SWITCH WITH EGT OF 550 DEGREES. PULLED FIRE SWITCH AND DISCHARGED BOTTLE. FIRE INDICATIONS WENT OUT AFTER THAT. VISUALLY INSPECTED APU AND NO EVIDENCE OF FIRE FOUND. REMOVED AND REPLACED APU FIRE BOTTLE PER MM 26-23-1. FOUND APU OVERHEAT DISCHARGE LINE BROKEN. REPLACED APU OVERHEAT DISCHARGE LINE. SYSTEM OPERATIONS CHECK GOOD. 2L73 4F RTA3WE 19950310004251995031000425NM 1995 3 10 SCNA95029 119950303A3350900835A EEL BATTERY PACK BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 FORWARD AISLE EMERGENCY EXIT SIGN IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT FORWARD AISLE EXIT SIGN. OPERATIONS CHECK GOOD. 2L73 4F RTA3WE 19950310004261995031000426NM 1995 3 10 95ZZZX1042 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 2 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 2 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR YAUA9502 AND 95ZZZX1043 THROUGH 95ZZZX1046. 2L73 4F A3WE 19950310004271995031000427NM 1995 3 10 95ZZZX1043 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 3 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 3 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR YAUA9502 AND 95ZZZX1044 THROUGH 95ZZZX1046, AND 95ZZZX1042. 2L73 4F A3WE 19950310004281995031000428NM 1995 3 10 95ZZZX1044 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 4 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 4 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR YAUA9502 AND 95ZZZX1045, 95ZZZX1046, AND, 95ZZZX951042 AND 95ZZZX1043. 2L73 4F A3WE 19950310004291995031000429NM 1995 3 10 95ZZZX1045 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 5 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 5 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR YAUA9502 AND 95ZZZX1042 THROUGH 95ZZZX1044, AND 95ZZZX1046. 2L73 4F A3WE 19950310004301995031000430NM 1995 3 10 95ZZZX1046 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 8 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 8 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR YAUA9502 AND 95ZZZX1042 THROUGH 95ZZZX1045. 2L73 4F A3WE 19950310004321995031000432EU 1995 3 10 95ZZZX1048 119950201A2612 DETECTOR BOLKMS117 BK117A4 5626017EU FIRE DETECTOR WIRE BROKEN A HDNAO OTHER N FALSE WARNING CRCRUISE 1 SW039024Z 7134 AIRCRAFT EXPERIENCED A FALSE FIRE WARNING IN-FLIGHT CAUSED BY A BROKEN WIRE ON FIRE DETECTOR. 1G72 3U H13EU 19950310004371995031000437SW 1995 3 10 95ZZZX1053 119950127A6410206010765001 BEARING BELL 206 206B 1181511SW T/R CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11125NH586 52099 MECHANIC NOTED A CRACKED FEATHERING BEARING ON TAIL ROTOR BLADE DURING POST-FLIGHT INSPECTION. REPLACED BEARING AND SLEEVE, PN 206-010-765-001 AND PN 206-010-733-003, IAW WITH BHT C.R. & O. MM. 1G71 3U H2SW 19950310004381995031000438SW 1995 3 10 95ZZZX1054 119950126A6300206010335001 LEVER ASSEMBLY 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032758L 309 45266 BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 2 EACH, PN 206-010-338-001 SPACERS, 4 EACH, PN 206-010-337-001 BEARINGS, 2 EACH, PN NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, AND BOLTS TT 309.1. 1G71 3U H2SW 19950310004391995031000439SW 1995 3 10 95ZZZX1055 119950126A6230206010336005 LINK 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032758L 309 45266 BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 2 EACH, PN 206-010-338-001 SPACERS, 4 EACH, PN 206-010-337-001 BEARINGS, 2 EACH, PN NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, AND BOLTS TT 309.1. 1G71 3U H2SW 19950310004441995031000444GL 1995 3 10 95ZZZX1060 219950123A7210MS2740113 RELAY SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL NR 2 CHIP LIGHT MALFUNCTION A ALGAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW031547K 760085 NR 2 ENGINE CHIP LIGHT ILLUMINATED. REPLACED NR 2 ENGINE CHIP RELAY (K8). SYSTEM CHECKED AND FOUND TO OPERATE NORMALLY. 1G72 3U3 U H1NE E1GL 19950310004451995031000445SW 1995 3 10 95ZZZX1061 119950201A7714206375200103 TACH GENERATOR BELL 206 206L4 1182110SW ENGINE N1 FAILED A ALGAO OTHER N FALSE WARNING CRCRUISE 1 SW03173AL1308 243833 52066 DURING LEVEL FLIGHT, N1 GAUGE FELL TO ZERO, ENGINE OUT LIGHT ILLUMINATED, AND AUDIO ENGINE OUT CAME ON. CROSS-CHECK OF INDICATORS NOTED NO OTHER DEFECTS. 1G71 3U NCH2SW 19950310004461995031000446 1995 3 10 95ZZZX1062 419950131A3422 WIRE BELL 206 206L1 1182107SW PANEL GYRO CHAFED A AALGAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW031068S 45436 WHILE AT CRUISE FLIGHT, SPARKS WERE EMITTED FROM RIGHT SIDE OF CONSOLE JUST UNDER PILOT'S VENT HANDLE. GYRO SWITCH WENT TO 'OFF' POSITION AND FUEL FILTER CAUTION LIGHT FLICKERED DIM THEN NORMAL, THEN EXTINGUISHED. GENERATOR WAS TURNED OFF. DURING TROUBLESHOOTING, FOUND GYRO WIRES CHAFED TO INSTRUMENT PANEL WHICH CAUSED OTHER WIRES TO SHORT IN SAME WIRE BUNDLE. REPAIRED WIRE AS REQUIRED. FUNCTIONAL CHECKED AFFECTED SYSTEM AND FOUND OKAY. 1G71 3U H2SW 19950310004471995031000447NM 1995 3 10 95ZZZX1063 119950225A29106517844238 HYDRAULIC LINE BOEING727 727151C 138404VNM A-HYD SYSTEM CHAFED A RYNAO OTHER K FLUID LOSS DEDESCENT 1 CE07432EX 19867 EMERGENCY LANDING MADE DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID AND PRESSURE ON INBOUND INTO INDIANAPOLIS. REPAIRED NR 1 ENGINE A-SYSTEM PUMP, PRESSURE LINE. 2L73 4F A3WE 19950310004631995031000463WP 1995 3 10 95ZZZX1079 219950130A73211390136 DIAPHRAGM WOODWARD 89737515 SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT FUEL CONTROL DEFECTIVE A EQGAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SW19360AE 5921 1708962 AC675 JLN - ON FINAL APPROACH, RIGHT ENGINE BEGAN SURGING. PILOT MADE A PRECAUTIONARY SHUT DOWN ON THE RIGHT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED FOR A FERRY FLIGHT TO HOT. AFTER ARRIVING IN HOT, IT WAS DETERMINED THE P3 ROLLING DIAPHRAGM WAS DEFECTIVE IN THE RIGHT ENGINE FUEL CONTROL. 1L72 4T4 T A8SW E4WE 19950310004651995031000465NM 1995 3 10 MRKA951 119950103A5240 DOOR BOEING737 73725A 1384481NM NOSE COMPT NOT LATCHED A MRKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03685MA 23791 AIR RETURN TO LAS DUE AIRCRAFT WOULD NOT PRESSURIZE. INSPECTION FOUND LOWER NOSE COMPARTMENT DOOR NOT PROPERLY LATCHED. SECURED DOOR AND RETURNED AIRCRAFT TO SERVICE. (X) 2L72 4F RTA16WE 19950310004661995031000466NM 1995 3 10 MRKA9513 119950117A3350862101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03674MA 23292 FLOOR PROXIMITY LIGHT AT RIGHT OVERWING EXIT FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECKED OKAY. (X) 2L72 4F RTA16WE 19950310004681995031000468SO 1995 3 10 WTAA950078 119950209A261212048732001 FIRE LOOP EMB 120 EMB120RT SO LT ENGINE FAILED A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17288UE 120184 SFO - LEFT FIRE PANEL 'DET INOP ENG/WW' LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FIRE DETECTOR LOOP ASSEMBLY. FIRE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950310004691995031000469EU 1995 3 10 WTAA950085 119950214A771432005028 TACH GENERATOR BAG JETSTMJETSTM3101 1500215EU LT ENGINE FAILED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17422UE 782 LAX - LEFT ENGINE RPM INDICATOR REPORTED INOPERATIVE AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR. ENGINE RPM INDICATIONS NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950310004701995031000470SO 1995 3 10 WTAA950087 119950125A2121EVAC523C2 FAN EMB 120 EMB120RT SO BS 11150.0 FAILED A WTAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP17278UE 120083 LAX - CREW REPORTED BURNING SMELL IN CABIN FROM RIGHT RECIRCULATION FAN. SMELL DISAPPEARED WITH FAN OFF. MAINTENANCE DEFERRED RT RECIRCULATION FAN PER M.E.L. 21-25-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED RIGHT RECIRCULATION FAN. SYSTEM OPERATIONAL CHECK NORMAL. CLEARED D.M.I. AIRCRAFT, RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950310004711995031000471SO 1995 3 10 WTAA950088 119950216A2731922AA24A6PZ722A PROX SENSOR EMB 120 EMB120RT SO LT ELEV TRIM FALSE SIGNAL A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17268UE 120207 RDM - ON APPLICATION OF TAKEOFF POWER, CREW RECEIVED 'TAKEOFF TRIM' AURAL WARNING. TAKEOFF WAS ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LT ELEVATOR TRIM PROXIMITY SENSOR. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950310004721995031000472SO 1995 3 10 WTAA950089 119950217A2612 FIRE DETECTOR EMB 120 EMB120RT SO LT ENGINE SHORTED A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17288UE 120184 SFO - LEFT FIRE PANEL 'DET INOP ENG/WW' LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FIRE DETECTOR. FIRE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. MFG PART NUMBER 3601-75-450/160C-5.8M. (X) 2L72 4T RTA31SO 19950310004731995031000473EU 1995 3 10 WTAA950090 119950217A77148DJ31WDJ4 RPM GAUGE BAG JETSTMJETSTM3101 1500215EU COCKPIT FAILED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17107XV 723 SFO - RIGHT ENGINE RPM GAUGE FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE RPM GAUGE. ENGINE RPM INDICATIONS NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950310004741995031000474EU 1995 3 10 WTAA950091 119950217A3350311701 EEL BATTERY PACK BAG JETSTMJETSTM3101 1500215EU CABIN DISCHARGED A WTAAK NONE L NO TEST NRNOT REPORTED 1 WP17428UE 806 SFO - EMERGENCY LIGHTING REPORTED DIM. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACKS (4 EACH). SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950310004751995031000475NE 1995 3 10 WTAA950092 219950219A73103033355 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE CLOGGED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17454UE 120155 FAT - LEFT ENGINE FUEL FILTER INDICATION LIGHT ILLUMINATED DURING CLIMB AT 11,000 FEET. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE HIGH PRESSURE FUEL FILTER. PERFORMED ENGINE GROUND RUN. ENGINE OPERATION NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950310004761995031000476SO 1995 3 10 WTAA950093 119950220A524012016900010 SERVICE DOOR EMB 120 EMB120RT SO RT WING UNSECURED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17269UE 120194 FAT - SERVICE DOOR WARNING INDICATION RECEIVED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESECURED CAMLOCK ON FUEL SERVICE DOOR. DOOR WARNING SYSTEM OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950310004771995031000477 1995 3 10 WTAA950094 419950219A3418C771076 TRANSDUCER BAG JETSTMJETSTM3101 1500215EU LT WING MALFUNCTIONED A WTAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP17423UE 799 EUG - LEFT STALL PROTECTION SHAKER AND HORN ACTIVATES WHEN STALL SYSTEM TURNED ON. MAINTENANCE REPLACED LEFT LIFT TRANSDUCER. STALL SYSTEM OPERATIONAL, CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950310004781995031000478NM 1995 3 10 YAUA9502 119950125A5754 BOLTS BOEING727 727231 1384079NM NR 1 LE SLAT LOOSE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA57431 20098 COMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 1 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KIT NR 65-92682-1. REF PSA WORK CARDS NR 46-51 W/O 950113-08. REF CONTROL NR 95ZZZX1042 THROUGH 95ZZZX1046. (X) 2L73 4F A3WE 19950310004791995031000479SW 1995 3 10 95ZZZZ118 119950210A27202742051037 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER CHAFED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE RUDDER TORQUE TUBE P/N 27-42051-037 TO BE CHAFED AT PHENOLIC PRESSURE SEAL CONTACT AREA. COMPLETED REPAIR TO THE RUDDER BY THE REPLACEMENT OF THE TORQUE TUBE IAW THE FAIRCHILD SRM. (Z) 1L72 4T A8SW 19950310004801995031000480SW 1995 3 10 95ZZZZ119 119950210A5712278401005 RIB SWRNGNSA227 SA227AC 8780603SW LT WING ELONGATED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT WING RIB P/N 27-84010-005 TO HAVE ELONGATED HOLE AT HYDRAULIC LINE PASS THROUGH, FORWARD OF MAIN SPAR. COMPLETED REPAIR TO LEFT WING RIB IAW FAIRCHILD ARP 57-20-9313 AND SRM. (Z) 1L72 4T A8SW 19950310004811995031000481SW 1995 3 10 95ZZZZ120 119950210A53202731110033 SUPPORT SWRNGNSA227 SA227AC 8780603SW LWR FUSELAGE CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD BELLY SUPPORT CHANNEL P/N 27-31110-033 AT BL 0.00 TO BE CRACKED AT THE PLUMBING PASS THROUGHS. COMPLETED REPAIR TO THE FORWARD BELLY SUPPORT CHANNEL BY REPLACEMENT OF THE CHANNEL AND INSTALLATION OF CHANNEL SUPPORT STIFFENERS IAW THE FAIRCHILD SRM 57-90-30 REPAIRS NR 1 AND NR 2. (Z) 1L72 4T A8SW 19950310004821995031000482SW 1995 3 10 95ZZZZ121 119950210A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.24 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT LOWER FLANGE OF CONSTANT FRAME P/N 27-22093-146 AT FS 174.24 TO BE CRACKED AT THE FLANGE BEND RADIUS. COMPLETED REPAIRS TO THE FRAME FLANGE IAW FAIRCHEILD ARP 53-20-9148 REV A. (Z) 1L72 4T A8SW 19950310004831995031000483SW 1995 3 10 95ZZZZ122 119950210A57532736069004 SKIN SWRNGNSA227 SA227AC 8780603SW RT TE FLAP DAMAGED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, COMPLETED REWORK OR PREVIOUSLY ACCOMPLISHED REPAIRS TO THE RT FLAP UPPER SKIN (P/N 27-36069-004) AT FLAP TRAILING EDGE AND WS 90.3. REPAIR WAS COMPLETED BY REMOVAL OF EXISTING REPAIR AND THE FABRICATION AND INSTALLATION OF A REPAIR PATCH AND INTERNAL DOUBLER IAW FAIRCHILD SRM 51-90-04 PGS 17 AND 18. (Z) 1L72 4T A8SW 19950310004841995031000484SW 1995 3 10 95ZZZZ123 119950210A57532736069004 SKIN SWRNGNSA227 SA227AC 8780603SW RT TE FLAP DAMAGED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, COMPLETED REWORK OF PREVIOUSLY ACCOMPLISHED REPAIR TO THE RT FLAP UPPER SKIN (P/N 27-36069-004) JUST INBOARD OF WS 90.3 4.5 INCHES FORWARD OF TRAILING EDGE. REPAIR WAS ACCOMPLISHED BY REMOVAL OF EXISTING REPAIR AND THE FABRICATION AND INSTALLATION OF A REPAIR PATCH AND INTERNAL DOUBLER IAW FAIRCHILD SR. (Z) 1L72 4T A8SW 19950310004851995031000485SW 1995 3 10 95ZZZZ124 119950210A53112722093145 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.24 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT LOWER BELT FRAME P/N 27-22093-145 AT FS 159.24 TO BE CRACKED AT THE LOWER CORNER CUTOUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM AND FAIRCHILD ARP 53-20-9148 REV A. (Z) 1L72 4T A8SW 19950310004861995031000486SW 1995 3 10 95ZZZZ125 119950210A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B DURING A MAINTENANCE INSPECTION IN MSP, FOUND THE RT LOWER BELT FRAME P/N 27-22100-035 AT FS 242 TO BE CRACKED AT THE LOWER CORNER CUTOUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM 53-90-20, REPAIR NR 19. (Z) 1L72 4T A8SW 19950310004871995031000487NM 1995 3 10 ASAA95074 119950214A5315 FLOOR BEAM BOEING737 737210C 1384459NM BS 727B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD FLANGES OF THE FLOOR BEAM AT BS 727B. REPAIRED PER EA 53-10-01323 AND BOEING TELEX ASA SEA-95-0095RR. (Z) 2L72 4F A16WE 19950310004881995031000488WP 1995 3 10 ASAA9552 119950208A53202024T40025 MOPSILL DOUG DC9 DC982 3022082WP R1 DOOR CORROSION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PAE - DURING 30K CHECK CORROSION WAS FOUND ALONG MOPSILL AT R1 DOOR. REMOVED CORODED MOPSILL WEB Y160 TO Y184, X-53 TO X-57.5, Z PLUS 1. FABRICATED NEW WEB. ALODINED, PRIMED, PAINTED AND INSTALLED IAW SRM 51-30-01, 51-30-02, 53-01 AND 53-20-01. (Z) 2L72 4F A6WE 19950310004891995031000489WP 1995 3 10 ASAA9553 119950208A5347ACA74143 SEAT TRACK DOUG DC9 DC982 3022082WP CABIN CORROSION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PAE - DURING 30K CHECK CORROSION WAS FOUND ON SEAT TRACK FROM Y201 TO Y225, X PLUS 22, Z PLUS 1. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-20-00, PGS 1-15, 51-30-01, PGS 1-8, 51-30-05, PGS 1-10, AND 53-03, PG 10. (Z) 2L72 4F A6WE 19950310004901995031000490WP 1995 3 10 ASAA9554 119950208A53473932140 SEAT TRACK DOUG DC9 DC982 3022082WP CABIN CORROSION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PAE - DURING 30K CHECK CORROSION WAS FOUND ON SEAT TRACK FROM Y1098 TO Y1212, X-0, Z-0. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW SRM 51-10-03, 51-10-04, 51-20-00, 51-30-01, 51-30-02 AND 53-14-03. (Z) 2L72 4F A6WE 19950310004911995031000491NE 1995 3 10 ASAA9570 219950214A7230 COMPRESSOR DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE NR 2 ENGINE FOD DAMAGE A ASAACD ABORTED TAKEOFF RETURN TO BLOCK ED VIBRATION/BUFFET INFLIGHT SEPARATION TOTAKEOFF 1 NM01964AS8282 8282 53078 SEA - NR 2 ENGINE HAD COMPRESSOR STALL DURING TAKEOFF ROLL. MAINTENANCE FOUND FOD DAMAGE TO C1 BLADES. REPLACED ENGINE. (Z) 2L72 4F4 FRTA6WE E9NE 19950310004921995031000492WP 1995 3 10 ASAA9577 119950216A52105910081135 DOOR DOUG DC9 DC982 3022082WP L1 DOOR DIFF TO CLOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED DOOR AND OPERATED NORMALLY. (Z) 2L72 4F A6WE 19950310004931995031000493NM 1995 3 10 AWXA9500112 119950227A5330 SKIN BOEING737 737277 1384570NM BS 707 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - DURING C6 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT KEEL BEAM AREA, STA 707 LBL 6. STOP DRILLED CRACKS AND REPAIRED DAMAGED PER ER 2 53 15 26. (W) 2L72 4F RTA16WE 19950310004941995031000494NM 1995 3 10 AWXA9500113 119950227A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 520 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - DURING C6 INSPECTION, FOUND FLOOR BEAM CRACKED ON FORWARD SIDE OF WEB BEHIND PREVIOUSLY INSTALLED DOUBLER, STATION 520 RBL 24. REPAIRED DAMAGE PER EO 53-14-12. (Z) 2L72 4F RTA16WE 19950310004951995031000495NM 1995 3 10 AWXA9500114 119950227A21401828202 HEAT EXCHANGER BOEING737 7373G7 1384595NM RIGHT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28305AW 24012 PHX - FLT 1530 - DURING C7 INSPECTION, FOUND CRACK IN RT PACK BAY PRIMARY HEAT EXCHANGER AT LOWER FORWARD END ON WELD. REMOVED AND REPLACED RT HEAT EXCHANGER PER AWA TASK CARD R2C21004. (Z) 2L72 4F RTA16WE 19950310004961995031000496NM 1995 3 10 CKSA95007 119950210A53137075T6 STRINGER BOEING727 72735 1384012NM FS 740 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23728CK55189 18847 YIP - DURING B-CHECK FOUND STRINGER 21R FWD OF STATION 740 CORRODED. REPAIRED STRINGER BY REMOVING CORRODED SECTION AND INSTALLING FILLER AND DOUBLER IAW 727 SRM 53-10-3. (Z) 2L73 4F A3WE 19950310004971995031000497EU 1995 3 10 RAIA950216 119950212A7722 SRL BAG JETSTMJETSTM3201 1500217EU RT ENG MALFUNCTIONED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03864AE 864 LAX - FLT 4734 - RT ENGINE ONLY ACHIEVED 80 PERCENT TORQUE. MAINTENANCE DEFERRED RT SRL AND TEMP LIMITER PER MEL 76-1 AND 76-2, CAT C. (Z) 2L72 4T RTA56EU 19950310004981995031000498SO 1995 3 10 RAIA950217 119950214A77123037603 SENSOR EMB 120 EMB120RT SO RT ENG FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03131AM13399 120158 STL - FLT 7484 - POWER LEVER SPLIT. MAINTENANCE REPLACED RT ENGINE T1.8 SENSOR. GROUND POWER RUNS REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA31SO 19950310004991995031000499EU 1995 3 10 RAIA950218 119950213A33500L60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 10087 199 STL - FLT 7126 - FORWARD RT EMERGENCY LIGHT OVER THE EMERGENCY HATCH IN THE CABIN IS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (Z) 2H72 4T RTA53EU 19950310005001995031000500SO 1995 3 10 RAIA950219 119950213A33503071BPE EEL BULB EMB 120 EMB120RT SO CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03125AM18861 120017 STL - ONE RED LIGHT OUT IN ESCAPE PATH LIGHTING. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (Z) 2L72 4T RTA31SO 19950310005011995031000501EU 1995 3 10 RAIA950220 119950213A33503012001 EEL BATTERY AEROSPATR72 ATR72202 8680940EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03721TE8038 217 STL - EMERGENCY LIGHT INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY. (Z) 2H72 4T RTA53EU 19950310005021995031000502EU 1995 3 10 RAIA950221 119950216A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03430AM8632 880 STL - FLT 7498 - PAX DOOR LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO SPI AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND ADJUSTED PAX DOOR MICROSWITCH. SYSTEM TEST REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA56EU 19950310005031995031000503 1995 3 10 RAIA950222 419950216A34256226190204 COMPUTER EMB 120 EMB120RT SO AVIONICS BAY MALFUNCTIONED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03126AM12086 120102 BHM - FLT 7461 - BOTH CAPTAINS AND FIRST OFFICERS EFIS SCREENS WENT BLANK. MAINTENANCE RE-INITIALIZED AHRS COMPUTER. SYSTEM TEST REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA31SO 19950310005041995031000504EU 1995 3 10 RAIA950223 119950217A71201379080H401 TRUSS TUBE BAG JETSTMJETSTM3201 1500217EU LT ENG CHAFED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03434AM8511 887 STL - LEFT ENGINE LOWER INBOARD FWD ENGINE TRUSS TUBE IS CHAFED. MX REPLACED LEFT ENGINE LOWER INBOARD FWD ENGINE TRUSS TUBE. (Z) 2L72 4T RTA56EU 19950310005051995031000505SO 1995 3 10 RAIA950224 119950214A3350D36604001 EEL BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03127AM148852154 120103 STL - SEVERAL AFT EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED AFT EMERGENCY LIGHTING BATTERY. (Z) 2L72 4T RTA31SO 19950310005061995031000506EU 1995 3 10 RAIA950225 119950215A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE135211439 119 STL - EMERGENCY LIGHTING INOP AT ROW 5CD. MAINTENANCE REPLACED BATTERY AT ROW 5CD. (Z) 2H72 4T RTA53EU 19950310005071995031000507SO 1995 3 10 RAIA950226 119950217A495012044167001 BLEED EMB 120 EMB120RT SO APU LEAKING A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03127AM14909 120103 STL - APU HAS SMOKE COMING FROM COMPARTMENT AND BLEED LINE UNDER BELLY. MAINTENANCE REPLACED DUCT SECTION UNDER BELLY. GROUND RUNS REVEALED NORMAL. (Z) 2L72 4T RTA31SO 19950310005081995031000508NE 1995 3 10 RAIA950227 219950219A72603022383 SEAL AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RT ENGINE LEAKING A RAIAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03421TE9543 102 120934 STL - FLT 7180 - RIGHT ENGINE OIL PRESSURE FLUCTUATION. MAINTENANCE REPLACED RT ENGINE AC GENERATOR GARLOCK SEAL. REPLENISHED OIL AND PERFORMED GROUND RUNS. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (Z) 2H72 4T4 TRTA53EU E20NE 19950310005091995031000509 1995 3 10 RAIA950228 419950217A3454313202 CONNECTOR EMB 120 EMB120RT SO VOR ANTENNA BAD PIN A RAIAO OTHER O OTHER CLCLIMB 1 CE03127AM14909 120103 STL - FLT 7458 - PILOT REPORTED BOTH VORS WILL NOT RECEIVE. MAINTENANCE REPAIRED COAX CONNECTOR TO ANTENNA PHASE COUPLER. SYSTEM CHECK OK. (Z) 2L72 4T RTA31SO 19950310005101995031000510EU 1995 3 10 RAIA950229 119950217A32609EN1C111HB2BB2 DNLOCK SW BAG JETSTMJETSTM3201 1500217EU RT GEAR FAILED A RAIAO OTHER N FALSE WARNING LDLANDING 1 CE03431AM12209 881 BRL - FLT 7051 - RT MAIN GEAR DOES NOT SHOW DOWN AND LOCK. NO EMERGENCY DECLARED CREW LANDED SAFELY. MAINTENANCE REPLACED RT MAIN GEAR DOWNLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA56EU 19950310005111995031000511EU 1995 3 10 RAIA950230 119950217A3234F96GA0102 GEAR HANDLE AEROSPATR72 ATR72202 8680940EU COCKPIT FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03721TE8051 217 STL - FLT 7010 - LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. MAINTENANCE REPLACED LANDING GEAR SELECTOR LEVER. GEAR SWINGS REVEALED NORMAL OPERATION. (Z) 2H72 4T RTA53EU 19950310005121995031000512EU 1995 3 10 RAIA950231 119950216A3240ACM26810 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU COCKPIT REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03426AM8791 874 STL - FLT 7437 - LEFT BRAKE VERY WEAK, PEDAL GOES FURTHER THAN RT BEFORE BRAKE REACHES EFFECTIVENESS. MAINTENANCE SERVICED LEFT BRAKE MASTER CYLINDER (P/N ACM26810). TAXI CHECK OK. LEAK CHECK OK. (Z) 2L72 4T RTA56EU 19950310005131995031000513WP 1995 3 10 RAIA950232 219950220A7320A218C14 'X' SCREW BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENG OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03431AM7306 206 881 66178 STL - FLT 7535 - RT RPM DROPPED TO 97 PERCENT ON CLIMB. MAINTENANCE ADJUSTED RT ENGINE RPM SCREW 'X'. GROUND POWER RUNS REVEALED NORMAL OPERATION. (Z) 2L72 4T4 TRTA56EU E4WE 19950310005141995031000514 1995 3 10 UF6A950210 419950211A25652077001 ESCAPE SLIDE BAG ATP ATP EU AFT BAG DOOR LOW PRESS A UF6AK NONE O OTHER ININSP/MAINT 1 CE03854AW6511 110 2028 ORD - FLT 5104 - RT REAR ESCAPE SLIDE HAS LOW PRESSURE. MAINTENANCE REPLACED ESCAPE SLIDE. (Z) 2L72 4T RTA27NM 19950310005151995031000515 1995 3 10 UF6A950211 419950212A34449650576020 GPWS COMPUTER BAG ATP ATP EU AVIONICS BAY FAILED A UF6AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03858AW4037 2035 SBN - FLT 5104 - AFTER TAKEOFF 'TAKEOFF CONFIGURATION' WARNING SOUNDED. MAINTENANCE REPLACED GPWS COMPUTER. (Z) 2L72 4T RTA27NM 19950310005161995031000516EU 1995 3 10 UF6A950212 119950213A3350363624 EEL STRIP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03855AW7124 2029 ORD - FLT 5005 - TWO STRIP LIGHTS INOP, RIGHT FRONT OF A/C. MAINTENANCE REPLACED ONE STRIP LIGHT. (Z) 2L72 4T RTA27NM 19950310005171995031000517EU 1995 3 10 UF6A950213 119950214A335058674 EEL INVERTER BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03855AW7129 2029 SBN - FLT 5102 - EMERGENCY LIGHTS INOP. FORWARD TWO STRIPS. MAINTENANCE REPLACED EMERGENCY LIGHT INVERTER. (Z) 2L72 4T RTA27NM 19950310005211995031000521CE 1995 3 10 95ZZZW147 119950112A5730 SKIN CESSNA402 402C 207590RCE WS 119,29 CORRODED A ATWAK NONE O OTHER ININSP/MAINT 1 WP1526548 402C0347 CORROSION ON SKIN UNDER AND AFT OF EXHAUST PIPE RT WING. CORROSION UNDER EXHAUST PIPE LT WING. SKIN WAS REPLACED AT WS 119.29. 1L72 3O A7CE 19950310005221995031000522CE 1995 3 10 95ZZZW148 119950130A5730 LE SKIN CESSNA402 402C 207590RCE WS 119.29-229.71CORRODED A ATWAK NONE O OTHER ININSP/MAINT 1 WP1536911 402C0314 CORROSION LEADING EDGE TO FRONT SPAR RT WING TOP AND BOTTOM AT WS 119.29 THROUGH 229.71. (W) 1L72 3O A7CE 19950310005231995031000523CE 1995 3 10 95ZZZW149 119950210A5730 LE SKIN CESSNA402 402C 207590RCE WS 19.29-229.71 CORRODED A ATWAK NONE O OTHER ININSP/MAINT 1 WP156789X 402C0440 TOP AND BOTTOM OF BOTH RT AND LT WINGS HAVE SEVERE CORROSION AT LEADING EDGE TO FRONT SPAR AT WS 119.29 THROUGH 229.71. CORROSION AND POPPED RIVETS JUST AFT OF EXHAUST PIPE RT AND LT WINGS AT WS 119.29. DER APPROVABLE AT WS 119.29 THROUGH 229.71 337 AND 8110-3. 1L72 3O A7CE 19950310005241995031000524CE 1995 3 10 95ZZZW150 119950130A5730 LE SKIN CESSNA402 402C 207590RCE WS 119.29-229.7 CORRODED A ATWAK NONE O OTHER ININSP/MAINT 1 WP1536911 402C0314 CORROSION ON LEADING EDGE OF WING AT TOP AND BOTTOM OF FRONT SPAR AT WS 119.29 THROUGH 229.7. CORROSION AT BOTTOM OF WING JUST AFT OF EXHAUST PIPE ON LEFT AND RIGHT WINGS AT WS 119.29. (W) 1L72 3O A7CE 19950310005281995031000528WP 1995 3 10 95ZZZW155 119950210A2120 AIR DISTR DOUG DC9 DC982 3022082WP COCKPIT ODOR A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05950U 49230 OMA - FLT 142 - DURING CRUISE HAD ODOR AND SMOKE IN COCKPIT. ELECTRICAL SYSTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL. CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND. CHECK C-2D - 1-13-93 - MCI. 2L72 4F A6WE 19950310005421995031000542NM 1995 3 10 MZZA9507 119950208A3350 EEL SIGN COVER BOEING727 7272F9 138407DNM R1 GALLEY DOOR CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13299AS 21427 TNN - DURING S-CHECK INSPECTION ON ACFT AT AIR ASIA, CRACK WAS FOUND ON R1 GALLEY SERVICE DOOR EXIT SIGN COVER. THE DAMAGED EXIT SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH (P/N BR9279-106), ASSEMBLY PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. (W) 2L73 4F RTA3WE 19950310005431995031000543NM 1995 3 10 MZZA9508 119950208A256065C1990119 LATCH CABLE BOEING727 7272F9 138407DNM L1 ENTRY DOOR BROKEN A MZZAK NONE O OTHER ININSP/MAINT 1 WP13299AS 21427 TNN - DURING S-CHECK INSPECTION ON ACFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON L1 ENTRY DOOR ESCAPE SLIDE LATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 25-60-15. (W) 2L73 4F RTA3WE 19950310005461995031000546GL 1995 3 10 SCNA95018 219950204A7321665032062127 MAIN ENG CONTL DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL NR 1 ENGINE FAULTY A ASCNAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 GL15571SC 46645 SJC - FLT 39 - DURING INITIAL POWER REDUCTION AT 33,000 FEET, THE NR 1 ENGINE COMPRESSOR STALLED. AT 20,000 FEET UPON INCREASE IN POWER, NR 1 ENGINE STALLED AGAIN. POWER WAS REDUCED TO IDLE, MAX TEMP DURING STALL WAS 800 DEGREES. PERFORMED BORESCOPE OF LPT, HPT. AND HIGH STAGE COMPRESSOR. FOUND TO BE OK. REPLACED CIT SENSOR. REMOVED AND REPLACED MEC AND RIGGED VARIABLE STATOR VANE SYSTEM IAW 73-20-01. OPERATED ENGINE IAW 71-00-TO 100 PERCENT POWER ASSURANCE AND ALL PARAMETERS WITHIN LIMITS. (W) 2L73 4F4 F A22WE E23EA 19950310005471995031000547GL 1995 3 10 SCNA95019 219950208A72619043M37G01 SUMP LINE DOUG DC10 DC1010 3022110WP GE CF6 CF6* 30020GL NR 2 ENGINE LEAKS A SCNAD RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 GL15573SC 46905 MSP - FLT 67 - THE NR 2 ENGINE OIL PRESSURE DROPPED BELOW THE RED LINE, OIL QUANTITY DROPPED TO 3 QUARTS, PRECAUTIONARY SHUTDOWN OF NR 2 ACCORDING TO PROCEDURES, ALSO HAD LOW ENGINE OIL PRESSURE LIGHT. FOUND OIL PRESSURE LINE AND C SUMP SCAVENGE RETURN LINE CHAFING AGAINST EACH OTHER. REPLACED BOTH LINES, SERVICED NR 2 ENGINE OIL, AND RAN NR 2 ENGINE, NO LEAKS NOTED. (W) 2L73 4F4 F A22WE E23EA 19950310005481995031000548EU 1995 3 10 SIMA950441 119950213A7602S761808600800 CONTROL CABLE AEROSPATR42 ATR42300 8680920EU NR 2 ENGINE MISROUTED A SIMAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW21243AT7118 0243 DURNG BRIDGE INSPECTION, MAINTENANCE FOUND THE NR 2 ENGINE CONDITION LEVER CABLE MISROUTED AND CHAFING INTO A SUPPORT BRACKET AT 90VU, BETWEEN FRAME 12 AND 13. SUPPORT BRACKET WAS REPAIRED BY INSTALLING A PIECE OF .071 ALUMINUM OVER DAMAGE IAW SRM 53-00-00. CABLE WAS REMOVED, INSPECTED, AND PROPERLY ROUTED. TENSION WAS ADJUSTED IAW JIC 61-21-21. ACFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950310005491995031000549EU 1995 3 10 VTZA95062 119950217A261172111211000 SMOKE DETECTOR JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE POD FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27304UE 41017 IAD-BOS - FLT 6481 - DURING CLIMB-OUT, THE POD SMOKE LIGHT ILLUMINATED. AN INFLIGHT EMERGENCY WAS DECLARED AND ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 21787 IAW MEL 26-3 ON THE FIRE DETECTION SYSTEM. MAINTENANCE LATER CLEARED DMI NR 21787 ON 02-18-95 BY REPLACING THE SMOKE DETECTOR. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950310005501995031000550NE 1995 3 10 VTZA95063 219950215A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT FLAME-OUT A VTZAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27315UE 41033 P75045 RIC-IAD - FLT 6277 - DURING POST-LANDING ROLLOUT, THE LT ENGINE FLAMED OUT AFTER LANDING ON TAXI TO GATE. ACFT ARRIVED AT GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE DECELERATION SCHEDULE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA41NM E18NE 19950310005511995031000551NE 1995 3 10 VTZA95064 219950215A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT FLAMED OUT A VTZAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27317UE 41031 P75044 PWM-IAD - FLT 6500 - DURING THE POST-LANDING ROLLOUT, THE LT ENGINE FLAMED OUT ON TAXI TO GATE. ACFT ARRIVED AT GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE DECELERATION SCHEDULE. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA41NM E18NE 19950310005521995031000552WP 1995 3 10 9503489751 119950306A3260 UPLIMIT SWITCH DOUG DC9 DC941 302207NWP NLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01751NW 47115 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DURING CLIMB-OUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR UPLIMIT SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005531995031000553WP 1995 3 10 9503499882 119950304A3260 RELAY DOUG DC9 DC951 3022051WP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01670MC 47659 ALL LANDING GEAR RED UNSAFE LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED DURING CLIMB-OUT. RECYCLED GEAR WITH SAME RESULTS. FOLLOWED PRECAUTIONARY OPERATING PROCEDURES AND FLIGHT CONTINUED TO DESTINATION (MIA). AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED R2-28 LANDING GEAR LEVER RELAY. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005541995031000554 1995 3 10 9503509937 419950305A342152237000004 ATTITUDE IND DOUG DC9 DC931 3022065WP INST PANEL MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01908H 323562237 47517 CAPTAIN'S VERTICAL GYRO FAILED ON ROTATION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 VERTICAL GYRO WITH NO HELP. REPLACED NR 1 ATTITUDE DIRECTIONAL INDICATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005551995031000555WP 1995 3 10 9503519940 119950306A2613 WIRE DOUG DC9 DC932 3022066WP AFT FUSELAGE CHAFED A NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL013322L 47031 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CRUISE FLIGHT AT 33,000 FEET. FLIGHT DIVERTED TO BIS AND LANDED WITHOUT INCIDENT. FOUND WIRING TO RIGHT TEMPERATURE SENSOR CHAFED AND GROUNDING ON TUBING. REPLACED THE RIGHT TEMPERATURE SENSOR AND INSTALLED HEAT SHRINK ON WIRING. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005561995031000556WP 1995 3 10 9503529970 119950304A3610 SEALS DOUG DC9 DC931 3022065WP SUPPLY DUCT FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019334 47247 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CLIMB-OUT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED PERI SEALS ON SUPPLY DUCT GOING TO WING ANTI-ICE. ALSO, REPLACED BAD NUT AND SECURED CLAMP ON UPSTREAM SIDE OF AUGMENTATION VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005571995031000557WP 1995 3 10 9503539874 119950307A2781 RETRACT SWITCHES DOUG DC9 DC951 3022051WP LE FLAP SYST FAILED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01783NC 48108 ON APPROACH INTO DTW, SLAT DISAGREEMENT LIGHT REMAINED ON AFTER SLATS WERE EXTENDED FOR LANDING. NO ABNORMAL ROLL WAS NOTICED. CAPTAIN DECLARED AN EMERGENCY AND ACCOMPLISHED A SUCCESSFUL 'FLAP ONLY' LANDING. REPLACED THE SLAT RETRACT SWITCHES AND SLAT CONTROL LEVER SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310005581995031000558WP 1995 3 10 9503549852 119950302A5350 RELEASE MECH DOUG DC9 DC951 3022051WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01761NC 47709 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. ALSO, FOUND A WORN CABLE SLIDER BLOCK AND LATCH LOCK ARM. REPLACED THE BLOCK AND ARM AND RERIGGED THE TAILCONE. CHECKED OK. 2L72 4F A6WE 19950310005591995031000559NE 1995 3 10 9503551153 219950306A7230JT9D20 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 2 ENGINE STALLED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01153US483731187 46762 686136 DURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. DUMPED 43,000 LBS OF FUEL AND RETURNED TO LAX. FERRIED AIRCRAFT TO MSP AND REPLACED THE NR 2 ENGINE. 2L73 4F4 F A22WE E20EA 19950310005601995031000560NM 1995 3 10 95UAL727020 119950306A3350 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297254U 21401 RIGHT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY. 2L73 4F4 F A3WE E2EA 19950310005611995031000561NM 1995 3 10 95UAL727021 119950306A3350 EEL BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297261U 21408 RIGHT AFT OVER WING EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950310005621995031000562NM 1995 3 10 95UAL727022 119950306A3520 MASK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE PASSENGER MALFUNCTION A UALAK NONE L NO TEST ININSP/MAINT 1 WP297271U 21418 DURING O2 SYSTEM TROUBLESHOOTING FOR LEAKS PASSENGER MASKS WERE DROPPED INADVERTENTLY. NOT ALL DROPPED AS REQUIRED. ALL LAV AND FLIGHT ATTENDANT PANELS ARE PAINTED SHUT AND NUMEROUS PASSENGER PANELS DID NOT OPEN. FLIGHT ATTENDANT LAV PSU DOORS ON FLEET CHECKED. 20 HAD OVERSPRAY THAT AFFECTED DEPLOYMENT. ALL FREED AND CLEANED. C-CK AND HMV J/C'S REVISED TO CK FOR OVERSPRAY. NON DEPLOYMENTS ATTRIBUTED TO MIS-PACKED O2 MASKS AND HOSES BY HMV CONTRACTOR. THE OTHER 11 PLANES WORKED BY SAME CONTRACTOR ARE BEING CHECKED. 2L73 4F4 F A3WE E2EA 19950310005631995031000563NM 1995 3 10 95UAL727023 119950306A361066OR69 DUCT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AFT AIRSTAIR RUPTURED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP297253U 21400 CREW REPORTED LOUD BANG IN AFT AIRSTAIR AREA. BODY OVERHEAT AND TAILSKID LIGHT ON. AIRPLANE RETURNED TO ORD. REPLACED NR 3 ENGINE TAI PNEUMATIC DUCT AT RIGHT AFT AIRSTAIR. 2L73 4F4 F A3WE E2EA 19950310005641995031000564WP 1995 3 10 ERA00002 119950216A323024085571016 UPLOCK LEVER CVAC 340 34031 2422704WP ALLSN 501D 501D13H 03004GL NLG CRACKED A ERAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 AL03569JA 69 NOSE LANDING GEAR WOULD NOT RETRACT. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE. 2L72 4R4 T 6A6 E282 19950310005651995031000565WP 1995 3 10 ERA00003 119950216A323024085571016 UPLOCK LEVER CVAC 340 34031 2422704WP ALLSN 501D 501D13H 03004GL NLG CRACKED A AERAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 AL03569JA 69 GEAR UNLOCK LIGHT WOULD NOT GO OUT AFTER DEPARTURE. FOUND LEVER P/N 240-8557101-6 CRACKED. THIS CRACKED LEVER WOULD NOT ALLOW THE NLG UPLOCK TO ACTUATE. RE-RIGGED NOSE LANDING GEAR AND PERFORMED RETRACT TEST. 2L72 4R4 T 6A6 E282 19950310005661995031000566WP 1995 3 10 ERA00004 119950224A2497P107 WIRE CVAC 440 440 2422902WP EXT PWR RECPT FAILED A ERAAA UNSCHED LANDING GB MULTIPLE FAILURE SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03566EA 381 LEFT DC GENERATOR WENT OFF LINE ON APPROACH. COMPLETE DC POWER FAILURE AFTER LANDING. SMOKE SMELL IN COCKPIT. BATTERY POWER COULD ONLY BE DISCONNECTED BY REMOVING BATTERIES. WIRE NR P107 FROM A2 TERMINAL OF DC EXTERNAL PWR CONTROL (CHANGEOVER) RELAY SHORTED TO PWR TERMINAL A2 OF BATTERY RELAY. WIRE EITHER TOO LONG OR NOT PROPERLY TIE-WRAPPED TO KEEP FROM CHAFING. WIRE BURNED AND MELTED FROM CHAGE OVER RELAY TO COCKPIT EXTERNAL BATTERY SWITCH. MANY OTHER WIRES MELTED THAT WERE CONTAINED IN THE SAME WIRE BUNDLES. 2L72 4R 6A6 19950310005671995031000567WP 1995 3 10 SCNA95030 119950303A3350A3060719103 EEL TRACK DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 EMERGENCY FLOOR TRACK LIGHTING IN FORWARD CABIN, LEFT SIDE INOPERATIVE. REPAIRED WIRE AT L1 PORTION OF FLOOR TRACK LIGHTING AND OPS CHECK GOOD. 2L73 4F A22WE 19950310005681995031000568NM 1995 3 10 SCNA95031 119950303A3350900542 EEL BATT CHARGER BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 L-2 DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED BATTERY CHARGER AT L-2 DOOR, M1092. ALSO, REMOVED AND REPLACED L-2 DOOR BATTERY PACK. OPS CHECK GOOD. 2L73 4F RTA3WE 19950310005691995031000569NM 1995 3 10 SCNA95032 119950306A33501102832 EEL BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 FORWARD OVERHEAD SELF-CONTAINED EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT AND OPS CHECK GOOD PER MM 33-50-81. 2L73 4F RTA3WE 19950310005701995031000570NM 1995 3 10 SCNA95033 119950303A335037067001 EEL BATTERIES BOEING727 7272A1 138407FNM AFT AIRSTAIRS DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 AFT AIRSTAIRS EMERGENCY OVERHEAD LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERIES AND OPERATIONS CHECKED GOOD. 2L73 4F A3WE 19950310005961995031000596CE 1995 3 10 95ZZZX1105 119950210A3230504501018 TORQUE TUBE CESSNA310 310R 2074245CE MLG RETRACT CRACKED A AAHTAK NONE O OTHER ININSP/MAINT 1 GL11988485930 310R0614 DURING AN ANNUAL INSPECTION, RT MLG TORQUE TUBE FOUND CRACKED. THE CRACK IS APPROXIMATELY .50 INCH LONG AND IS LOCATED ON THE WELD AT THE BOSS FOR THE FORK BOLT. THE CRACK WAS DETECTED BY A VISIBLE LINE IN THE PAINT ON THE PART, BUT WHEN THE PAINT WAS REMOVED FOR A MORE THOROUGH INSPECTION, CRACK WAS OBVIOUS ONLY WHEN LIQUID PENETRANT INSPECTION WAS UTILIZED. 1L72 3O 3A10 19950310006471995031000647WP 1995 3 10 9503569990 119950304A5320 SPLICE FITTING DOUG DC9 DC931 3022065WP FS 851-870 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 22L SPLICE FITTING AT FS 851 - 870. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950310006481995031000648WP 1995 3 10 9503579926 119950305A57555910055516 LE SPAR DOUG DC9 DC932 3022066WP RT SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 4456 47425 DURING "A" CHECK, FOUND 9.5 INCH CRACK IN THE RIGHT INBOARD FLIGHT SPOILER LEADING EDGE SPAR. REPLACED SPOILER PER CITEXT 90-2760-1-9901. 2L72 4F A6WE 19950310006491995031000649WP 1995 3 10 9503589960 119950303A53203916209501N SUPPORT FITTING DOUG DC9 DC931 3022065WP FS 680 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01920RW 47163 DURING PERIODIC CHECK, FOUND CRACK IN VERTICAL SUPPORT FITTING FS 680 AT THE LEFT OUTBOARD SEAT TRACK. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950310006501995031000650NM 1995 3 10 9503602278 119950308A3260 DOOR SWITCHES BOEING727 727251 138408HNM NLG DIRTY A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01278US 21157 DURING APPROACH UPON LANDING GEAR EXTENSION, NOSE GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH PROPER INDICATIONS. MAINTENANCE FOUND THE NOSE LANDING GEAR WITH SWITCHES AND AREA CONTAMINATED. CLEANED SWITCHES AND DOOR AREA, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950310006511995031000651NM 1995 3 10 9503612705 119950302A5712651852214 RIB CHORD BOEING727 727225 1384077NM FS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 22433 DURING PCK, MAINTENANCE FOUND WING TO BODY UPPER RIB CHORD, FS 760, RBL 70.5 CRACKED. REPAIRED PER NWA EA 27-096690. 2L73 4F A3WE 19950310006521995031000652NM 1995 3 10 95UAL747016 119950309A3350 EEL BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29181UA 25278 EEL IS INOP FROM ROW 35 TO ROW 45 ON RIGHT SIDE OF AIRCRAFT. FEEDER STRIP REINSTALLED PER WIRING DIAGRAM. 2L74 4F4 FRTA20WE E24NE 19950310006531995031000653WP 1995 3 10 95UALD10026 119950309A3350 EEL BATTERY DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291814U 46613 EMERGENCY LIGHTING BATTERY CHECK FAILED. REPLACED BATTERY PACK FOR THE MID AFT POWER SUPPLY. 2L73 4F4 F A22WE E23EA 19950310006541995031000654 1995 3 10 COM11808 419950307A34216226342022 EADI EMB 120 EMB120RT SO COCKPIT FAILED A COMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO01268CA1363080 120262 DURING DESCENT CREW NOTED BURNING ELECTRICAL SMELL IN COCKPIT. COPILOT'S EADI FAILED. REPLACED COPILOT'S EADI. 2L72 4T RTA31SO 19950310006551995031000655SO 1995 3 10 COM11809 119950306A5720 SUPPORTS EMB 120 EMB120RT SO LT/RT WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01247CA1029810298 120225 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01i AND 5720-552/652-01I AT WING RIBS NR 15, 16, AND 18. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17056-007, 2 EA; 120-17057-005, 1 EA; 120-17057-007, 2 EA; 120-17059-015, 2 EA; 120-17057-006, 1 EA. THE SKIN SUPPORTS WERE REPLACED IAW AERO DESIGN REPORT NR 1327-2. 2L72 4T RTA31SO 19950310006561995031000656SO 1995 3 10 COM11810 119950305A61208022483 PUMP EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01264CA8803 950 120256 LEFT PROPELLER AUXILIARY PUMP TEST FAILED. REPLACED PUMP. 2L72 4T RTA31SO 19950310006571995031000657SO 1995 3 10 COM11811 119950305A243051539014A GCU EMB 120 EMB120RT SO ELEC BAY DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01256CA8668 2190 120245 RIGHT ENGINE STARTER DOES NOT TERMINATE START SEQUENCE AT 50 PERCENT. REPLACED THE GCU. 2L72 4T RTA31SO 19950310006581995031000658SO 1995 3 10 COM11812 119950308A3260922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT MLG BROKEN A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01462CA 120264 LEFT MLG GREEN "A" SYSTEM LIGHT FLICKERS ON AND OFF DURING FLIGHT WITH GEAR RETRACTED. REPLACED BROKEN DOWNLOCK PROXIMITY SENSOR. 2L72 4T RTA31SO 19950310006591995031000659SO 1995 3 10 COM11813 119950308A3260922AA2YA6PZ72 PROX SWITCH EMB 120 EMB120RT SO LT MLG REQUIRE ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01200CD 120200 LEFT MAIN LANDING GEAR INTRANSIT LIGHTS REMAIN ON AFTER RETRACTION. ADJUSTED THE LEFT MLG UPLOCK PROXIMITY SWITCHES. 2L72 4T RTA31SO 19950310006601995031000660 1995 3 10 COM11814 419950307A3418C818061 COMPUTER EMB 120 EMB120RT SO NR 2 STALL WARN DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01179CA12521 120179 NR 2 STALL WARNING SYSTEM RED LIGHT IS ON. REPLACED THE NR 2 STALL COMPUTER. 2L72 4T RTA31SO 19950310006611995031000661EA 1995 3 10 COM60434 119950306A3010124112450 SWITCH CNDAIRCL600 CL6002B19 EA LT WING DEFECTIVE A COMAK NONE N FALSE WARNING CLCLIMB 1 SO01932CA 7038 ANTI ICE DUCT MESSAGE ON EICAS. REPLACED 3 DEFECTIVE THERMAL SWITCHES IN LT WING LEADING EDGE. 2L72 4F RTA21EA 19950310006621995031000662WP 1995 3 10 SCNA95034 119950308A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15151SY 48295 FORWARD CABIN EMERGENCY LIGHTS FAIL TEST. REPLACED FORWARD CABIN EMERGENCY LIGHTS POWER SUPPLY AND OPS CHECK GOOD. 2L73 4F A22WE 19950310006631995031000663NM 1995 3 10 SCNA95035 119950305A56105893543129 L-1 WINDOW BOEING727 727225 1384077NM COCKPIT FAULTY A SCNAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL15283SC 22559 WINDOW HEAT CONDUCTOR, UPPER LEFT L-1 WINDOW, ARCHING AND SMOKE NOTED. TURNED OFF L-1 AND L-2 WINDOW HEAT, CONDITION STOPPED. REPLACED L-1 WINDOW PER MM 56-11-11, PRESSURIZED WINDOW AS PER MM 36-00, OPS CHECKED WINDOW HEAT AS PER MM 30-45-02. NO LEAKS NOTED ON PRESSURIZATION AND WINDOW HEAT OPS CHECKED GOOD. 2L73 4F A3WE 19950310006641995031000664NM 1995 3 10 SWAA950199 119950302A5315 FLOOR BEAM STRAP BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07324SW 23414 DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT CENTERLINE, AT 31.75 INCHES TO RIGHT OF CENTERLINE, AND AT 11.25 INCHES TO THE LEFT OF CENTERLINE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950310006651995031000665NM 1995 3 10 SWAA950200 119950303A5311 BELTFRAME BOEING737 7372H4 138448CNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0794SW 23053 DURING SCHEDULED 1/4 D-CHECK, FOUND BELTFRAME CRACKED AT BS 360, S26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950310006661995031000666NM 1995 3 10 SWAA950201 119950303A5330 SKIN BOEING737 7373H4 1384600NM PAX DOOR AREA CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07315SW 23337 DURING SCHEDULED B2 CHECK, FOUND A .3750 INCH CRACK AT UPPER RADIUS OF HINGE CUTOUT ON FUSELAGE AFT ENTRY DOOR CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950310006671995031000667NM 1995 3 10 SWAA950202 119950303A335090083 EEL BATTERY BOEING737 7372H4 138448CNM COCKPIT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0723SW 21338 DURING SCHEDULED C3 CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT DIM. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950310006681995031000668NM 1995 3 10 SWAA950203 119950304A3350900835A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0773SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950310006691995031000669NM 1995 3 10 SWAA950204 119950304A3350900835A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0773SW 22673 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950310006701995031000670NM 1995 3 10 SWAA950205 119950304A335020131A EEL BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN FLOOR TRACK LIGHTS AND RIGHT AFT EXTERIOR EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950310006711995031000671NM 1995 3 10 UPS202615 119950306A5754 NR 6 KFLAP BOEING727 727173C 1384059NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950310006721995031000672NM 1995 3 10 UPS202616 119950306A5754 NR 1 KFLAP BOEING727 727173C 1384059NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950310006731995031000673NM 1995 3 10 UPS202617 119950306A5720 CHORD BOEING727 727173C 1384059NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER CHORD LEFT WING STA 656.5, S-8 VENT BOX, FWD. INSTALLED REPAIR PER SB 727-57-0127. 2L73 4F A3WE 19950310006741995031000674NM 1995 3 10 UPS202618 119950306A5711 SPAR CHORD BOEING727 727173C 1384059NM WS 71-73 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER SPAR CHORD RT WING BS 870, WS 71-73. INSTALLED REPAIR PER UPS EO B727-5710-6737A, B727-5710-6722A. 2L73 4F A3WE 19950310006751995031000675NM 1995 3 10 UPS202619 119950306A5313 STRINGER BOEING727 727173C 1384059NM BS 464 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON STRINGER 24R AT BS 464. INSTALLED REPAIR PER SRM 51-20-1, 51-30-23. 2L73 4F A3WE 19950310006761995031000676NM 1995 3 10 UPS202620 119950306A5320 INTERCOSTAL BOEING727 727173C 1384059NM BS 1050 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 1050, RBL 60, WL 180. INSTALLED REPAIR PER SRM 53-10-1, 51-30-00, 51-10-2, 51-30-2, AND MM 51-20-151. 2L73 4F A3WE 19950310006771995031000677NM 1995 3 10 UPS202621 119950306A5730 FUEL CELL CUTOUT BOEING727 727173C 1384059NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON LWR SURFACE OF RT WING FUEL CELL CUT OUT 7606. INSTALLED REPAIR PER UPS EO FILE NR B727-57-1088. 2L73 4F A3WE 19950310006781995031000678NM 1995 3 10 UPS202622 119950306A5711 SPAR CHORD BOEING727 727173C 1384059NM WS 102-114 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON RT WING LWR AFT SPAR CHORD BS 870, RT WING STA 102-114. INSTALLED REPAIR PER SRM 51-30-2. 2L73 4F A3WE 19950310006791995031000679NM 1995 3 10 UPS202623 119950306A5320 FWD FLANGE BOEING727 727173C 1384059NM BS 950 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON THE FWD FLANGE BS 950, RBL 58, WL 208. REPAIRED PER UPS EO FILE NR B272-53-1528. 2L73 4F A3WE 19950310006801995031000680NM 1995 3 10 UPS202624 119950306A5730 CENTER TANK SKIN BOEING727 727173C 1384059NM BS 763 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE IN "D" CHECK MAINTENANCE FOUND CRACKS EMANATING FROM FASTENER HOLES AFT ON SKIN LWR SURFACE CENTER TANK AT BS 763, RBL 70 WL 201. REPAIRED PER UPS EO B727-5710-6738A. 2L73 4F A3WE 19950310006811995031000681NM 1995 3 10 UPS402629 119950308A2612 FIRE LOOP BOEING747 747123F NM NR 4 A DIRTY A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01671UP 20323 PILOT REPORTED THAT ON CLIMBOUT, FIRE DETECTION LIGHT ILLUMINATED WITH A FAULT INDICATION. THE NR 4 A-LOOP INDICATED A SHORT. AFTER 15 MINUTES, SHORT CORRECTED ITSELF. CLEANED CONTACT ON NR 4 A-LOOP, NR 4 A-CARD, OPS CHECK OK. 2L74 4F A20WE 19950310006821995031000682WP 1995 3 10 UPS802625 119950306A3260 PROX SENSOR DOUG DC8 DC873F 302199FWP LT MLG INOP A IPXAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01840UP 46140 PILOT REPORTED DURING UPLATCH CHECK GEAR NOT LATCHED LIGHT ILLUMINATED, CYCLED GEAR, 2ND UPLATCH CHECK SAME RESULT, CYCLED GEAR 3RD TIME, GEAR UPLATCH CHECK NOSE GEAR CAME DOWN. FOURTH TIME, GEAR UPLATCH CHECK GEAR NOT LATCHED LIGHT AND DOORS LATCHED LIGHT ILLUMINATED, CYCLED GEAR 5TH TIME, UPLATCH CHECK GEAR NOT LATCHED LIGHT ILLUMINATED NOSE GEAR DID NOT FALL OUT. REPLACED LT MLG GEAR PROXIMITY SENSOR SWITCH PER DC8 MM 32-60-00. PERFORMED GEAR SWING, OPS CK NORMAL (UPLOCK PROXIMITY SENSOR). 2L74 4F RT4A25 19950310006831995031000683WP 1995 3 10 UPS802626 119950306A5312 BEAM DOUG DC8 DC873F 302199FWP AFT BULKHEAD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN "B" CHECK MAINTENANCE FOUND CRACK ON AFT BULKHEAD LATERAL STRUCTURE, 4TH BEAM (J-BEAM) FROM THE BOTTOM, ON LWR LEG OF BEAM. REPAIRED PER UPS EO DC8-5310-6598. 2L74 4F RT4A25 19950310006841995031000684WP 1995 3 10 UPS802627 119950306A3231 RETRACT MECH DOUG DC8 DC873F 302199FWP LT MLG DOOR OUT OF ADJ A IPXAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01804UP 46004 PILOT REPORTED DOORS NOT LATCHED LIGHT REMAINED ON THROUGHOUT FLIGHT; CHECKLIST COMPLIED WITH; LT ALTERNATE MAIN GEAR DOOR WARNING LIGHT ILLUMINATED. ADJUSTED LEFT MAIN GEAR DOOR PRELOAD PER MM 32-31-05, STEP 32. 2L74 4F RT4A25 19950310006851995031000685NM 1995 3 10 UPS802628 119950307A3260 ANNUN PANEL BOEING727 72725C 138400HNM LANDING GEAR INOP A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01933UP 19857 PILOT REPORTED THAT ON INITIAL GEAR EXTENTION NLG GREEN LIGHT DID NOT ILLUMINATE, RECYCLED GEAR AND DID NOT GET GREEN NLG LIGHT (RED UNSAFE LIGHT WAS OUT). ON SUBSEQUENT APPROACH, GEAR WAS LOWERED AND NLG GREEN LIGHT DID NOT ILLUMINATE. VISUALLY CHECKED AND VERIFIED NOSE GEAR. REPLACED LANDING GEAR ANNUNCIATOR PANEL. OPS CHECK OK. 2L73 4F A3WE 19950310006861995031000686SW 1995 3 10 95ZZZX1130 119950208A6720206928110 PIN ASSY BELL 206 206L4 1182110SW T/R PEDAL DEFECTIVE A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH1801 52076 WHILE DISENGAGING THE TAIL ROTOR LOCKOUTS, THE PINS WOULD NOT RELEASE FORM THE LINK ASSY (PN 206-001-701-001). SUBSTANTIAL FORCE WAS REQUIRED TO REMOVE THE EXPANDABLE PINS. THE MECHANIC NOTED THE EXPANDABLE RINGS USE TO SECURE THE PINS WITHIN THE LINKS WOULD NOT RETRACT TO ITS ORIGINAL SIZE. REPLACED EXPANDABLE PIN ASSEMBLY IAW AERONAUTICAL ACCESSORIES, INC. STC SR00513AT, REPORT NR AA-94051, REV. A. 1G71 3U NCH2SW 19950310006871995031000687WP 1995 3 10 95ZZZX1131 119950218A213121171801 PRESS CONTROL DOUG DC9 DC931 3022065WP CABIN ERRATIC A A4JAG O2 MASK DEPLOYED J WARNING INDICATION DEDESCENT 1 SO158931E 47140 FLT 1818 - 33,000 FEET ON DESCENT, EXPERIENCED RAPID PRESSURE LOSS IN AIRCRAFT, UNDER CONTROL BY 10,000 FEET CABIN ALTITUDE. PASSENGER OXYGEN MASKS DEPLOYED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT PIE. REPLACED CABIN PRESSURE CONTROL PANEL AND CABIN PRESSURE CONTROLLER. ALL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310006881995031000688WP 1995 3 10 95ZZZX1132 119950218A213010256852 PRESS SELECTOR DOUG DC9 DC931 3022065WP CABIN ERRATIC A A4JAG O2 MASK DEPLOYED J WARNING INDICATION DEDESCENT 1 SO158931E 47140 FLT 1818 - 33,000 FEET ON DESCENT, EXPERIENCED RAPID PRESSURE LOSS IN AIRCRAFT, UNDER CONTROL BY 10,000 FEET CABIN ALTITUDE. PASSENGER OXYGEN MASKS DEPLOYED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT PIE. REPLACED CABIN PRESSURE CONTROL PANEL AND CABIN PRESSURE CONTROLLER. ALL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950310006891995031000689NM 1995 3 10 BJNA952002 119950215A3350 EEL BOEING737 7372H4 138448CNM L1 DOOR LOOSE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 FORWARD EXTERIOR EMERGENCY EXIT LIGHTS INOP. ACFT RELEASED PER MEL 33-14 DMI NR 024, ITEM TRANSFERRED TO CEX FORM 4001 AND PLACARDED, DAY OPERATIONS ONLY. REFER TO MEL 33-14 DMI NR 024 EXTERIOR EMERGENCY LIGHT SYSTEMS INOP. FOUND L1 DOOR RETRACTABLE EXIT LIGHT DISLODGED, RESECURED. OPS CHECKS GOOD AT THIS TIME IAW 33-51-0. (X) 2L72 4F A16WE 19950310006901995031000690WP 1995 3 10 BUFA9504 119950214A2910 HYD FITTING DOUG DC8 DC862 3021970WP LT MLG LEAKING A BUFAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE05922BV 45925 DURING FINAL APROACH, ACFT HYDRAULIC PRESSURE DROPPED DOWN TO 500-600. FOUND HYDRUALIC LINE FITINGS AT LT MLG RETRACT ACTUATOR, PN 57740355507, LEAKING. REPLACED PACKING AT SAME FITTINGS. LEAK CHECK C/W IWA MM 29-01. AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950310006911995031000691WP 1995 3 10 BUFA9505 119950215A8012642810 START VALVE DOUG DC8 DC862 3021970WP NR 2 ENGINE FAILED A BUFAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE05922BV 45925 DURING CLIMB THROUGH FL 260, PRECAUTIONARY ENGINE SHUT DOWN DUE TO NR 2 START VALVE OPEN. FOUND PRESSURE RELIEF CONTROL VALVE FAILED NR 2 ENGINE. REPLACED PRESSURE RELIEF CONTROL VALVE. OPS CHECK GOOD IAW MM 36-12-2. AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950310006921995031000692NE 1995 3 10 CAL950090 219950205A75301555M23G01 DUCT ASSY AIRBUS300 A300B4103 3930104EU GE CF6 CF650C2 30018NE NR 1 ENGINE RUPTURED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0911984362438970 108 455938 FLT 288 - EWR - THE NR 1 ENGINE HAD A FIRE WARNING ON TAKEOFF. THE A/C WAS RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE 14TH STAGE DUCT ON THE NR 1 ENG WAS FOUND BLOWN. IN ADDITION, A THRUST REVERSER HALF AND COWLING HAD SUSTAINED SOME DAMAGE. THE FAILURE WAS DUE TO HIGH VIBRATORY STRESSES IN THE 14TH STAGE CDP AIR TUBE RESULTING FROM THE 14TH STAGE AIR BLEED TUBE. THE CF6-50 FLEET HAS BEEN MODIFIED BY REMOVING THE 14TH STAGE AIR BLEED TUBE PER GE SERVICE BULLETIN 75-071. (M) 2L72 4F4 F A35EU E23EA 19950310006931995031000693NM 1995 3 10 CAL950131 119950214A3260 WARNING LIGHT BOEING727 727227 1384078NM NLG ILLUMINATED A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0910756 21042 EWR - FLT 0894 - THE RED NOSE GEAR WARNING LIGHT REMAINED ILLUMINATED WITH NO NOSE GEAR GREEN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. ALL INDICATIONS WERE NORMAL WITH 3 GREEN AFTER THE GEAR WAS CYCLED. A NOSE GEAR RETRACTION AND EXTENSION TEST WERE PERFORMED SEVERAL TIMES AND ALL NOSE GEAR INDICATIONS WERE NORMAL. THE PROBLEM COULD NOT BE DUPLICATED AND NO TROUBLE WAS FOUND. THE AIRCRAFT HAS SUBSEQUENTLY COMPLETED SEVERAL FLIGHTS WITHOUT A REPEAT OF RED NOSE GEAR WARNING INDICATION PROBLEM. (X) 2L73 4F A3WE 19950310006941995031000694NM 1995 3 10 CAL950133 119950216A2910 O-RING BOEING737 7373T0 1384582NM A-HYD SYST LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914307 23358 IAH - FLT 1638 - THE A-HYDRAULIC SYSTEM QUANTITY BEGAN TO DECRASE IN FLIGHT. THE LEAKAGE STOPPED WHEN THE A-SYSTEM WAS ISOLATED BY TURNING THE SYSTEM-1 FLIGHT CONTROL TO STANDBY RUDDER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE O-RING AT THE ACCUMULATOR FITTING OF A-SYSTEM HYDRAULIC ELECTRIC PUMP LEAKING. THE O-RING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECK WAS GOOD. (X) 2L72 4F RTA16WE 19950310006951995031000695NM 1995 3 10 CAL950134 119950216A3211 TRUNNION BOEING727 727243 138408DNM RT MLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0917406 21269 FLT NR 667 - DEN - THE CREW HEARD A BUMP SOUND AND FELT A JOLT ABOUT 1000 FEET AFTER TOUCHDOWN. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG HAD FAILED JUST FORWARD OF THE AFT TRUNNION AREA CAUSING AFT TOP OF GEAR TO MOVE IN AN UPWARD DIRECTION AND THE SIDE STRUT TO JAM IN RIGHT INBOARD MID FLAP AREA. S/D - INVESTIGATION REVEALED THAT THE CAUSE OF LANDING GEAR FAILURE WAS DUE TO A CRACKED OUTER CYLINDER AFT TRUNNION JOURNAL. THE CRACK WAS A RESULT OF CORROSION. (M) 2L73 4F RTA3WE 19950310006961995031000696EU 1995 3 10 CAL950135 119950216A291340157 HYD PUMP AIRBUS300 A300B4203 3930306EU LT HYD SYST LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09149699737 1554 207 EWR - FLT 0292 - THE GREEN SYSTEM HYDRAULIC QUANTITY FELL TO THE RED DOT ACCOMPANIED BY ILLUMINATION OF THE LEVEL LOW LIGHT AND MWP HYDRAULIC LIGHTS WHILE EN ROUTE TO EWR. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND LT GREEN ELEC HYDRAULIC PUMP LEAKING. THE PUMP REMOVED AND REPLACED. THE GREEN HYDRAULIC SYSTEM WAS SERVICED TO FULL AND NO LEAKS WERE NOTED WITH BOTH ENGINES OPERATION. (X) 2L72 4F A35EU 19950310006971995031000697NM 1995 3 10 CAL950137 119950218A2910 HYD LINE BOEING737 737130 1384435NM A-HYD SYST LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0914209 19026 CLE - FLT 1475 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY BEGAN TO DECREASE AFTER TAKEOFF FROM CLE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE A-HYDRAULIC SYSTEM PRESSURE LINE UNION IN THE RT WHEELWELL LEAKING. THE UNION WAS TIGHTENED AND LEAK CHECK WAS GOOD DURING AN ENGINE RUN. (X) 2L72 4F A16WE 19950310006981995031000698EU 1995 3 10 CAL950138 119950218A2750 TRANSMISSION AIRBUS300 A300B4103 3930104EU LT/RT TE FLAPS LACK OF LUBE A ACALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0916982 091 EWR - FLT 0750 - WHEN FLAP HANDLE MOVED TO 8 DEGREES ON APPROACH TO EWR, FLAPS WOULD NOT EXTEND. CYCLING FLAP HANDLE HAD NO EFFECT. 'ABNORMAL' RPOCEDURES WERE C/W & ACFT LANDED WITH SLATS AT 16 DEGREES & FLAPS AT ZERO DEGREES. MX COULD NOT DUPLICATE PROBLEM & NO DEFECTS FOUND. FLAP CONTROL UNIT WAS SERVICED & FLAP TRANSMISSIONS LUBRICATED AS A PRECAUTIONARY MEASURE. OPERATION OF FLAPS CHECKED GOOD. ACFT HAS COMPLETED OVER 10 FLIGHTS WITHOUT A REPEAT OF FLAP PROBLEMS SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (X) 2L72 4F A35EU 19950310006991995031000699NM 1995 3 10 CAL950139 119950219A291355097 HYD PUMP BOEING727 727224 1384076NM NR 1 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0993738141059772 20666 EWR - FLT 0376 - AIRCRAFT LOST A-SYSTEM HYDRUALIC QUANTITY WHILE EN ROUTE TO EWR. AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A-SYSTEM NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950310007001995031000700NE 1995 3 10 CAL950140 219950220A75301555M23G01 DUCT AIRBUS300 A300B4103 3930104EU GE CF6 CF650C2 30018NE NR 1 ENG RUPTURED A CALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0911985322906957 119 528129 FLT NR 288 - EWR - TAKEOFF WAS ABORTED AT 60 KNOTS AFTER THE NR 1 ENGINE N1 DROPPED AND THE EGT ROSE TO 950 DEGREES. MAINTENANCE FOUND THE NR 1 ENGINE 14TH STAGE DUCT BLOWN. THE 14TH STAGE DUCT WAS REMOVED AND REPLACED. THE NR 1 ENGINE WAS RUN AT HIGH POWER WITH ALL PARAMETERS AND INDICATIONS CHECKING NORMAL. S/D - THE FAILURE WAS DUE TO HIGH VIBRATORY STRESSES IN THE 14TH STAGE CDP AIR TUBE RESULTING FROM THE 14TH STAGE AIR BLEED TUBE. THE CF6-50 FLEET HAS BEEN MODIFIED BY REMOVING THE 14TH STAGE AIR BLEED TUBE PER GE SERVICE BULLETIN 75-071. (M) 2L72 4F4 F A35EU E23EA 19950310007011995031000701WP 1995 3 10 GRAA9528 119950130A2913AS66411LS666 HYD PUMP DOUG DC9 DC915 3022036WP RT ENGINE FAILED A GRAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP111064T 45778 UPON DESCENDING INTO MISSOULA, MONTANA, ACFT N NR 1064T LOST ALL HYDRAULIC FLUID FROM THE RT SYSTEM. THE LANDING GEAR WAS EXTENDED BY USING THE FREE-FALL METHOD. THE AIRCRAFT LANDED AT MISSOULA AIRPORT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RT ENGINE DRIVEN HYDRAULIC PUMP HAD THE SEALS RUPTURED IN IT. MAINTENANCE REMOVED THE DEFECTIVE PUMP AND REPLACED WITH A SERVICEABLE UNIT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK AND A LEAK CHECK. THE UNIT OPERATIONALLY CHECKED NORMAL AND NO LEAKS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950310007021995031000702WP 1995 3 10 GRAA9529 119950221A335060030451 POWER SUPPLY DOUG DC9 DC987 3022087WP CABIN FAILED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111074T 49727 WHILE PERFORMING A LINE INSPECTION, MAINTENANCE DISCOVERED THE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE GALLEY AND COCKPIT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND POWER SUPPLY INOPERATIVE IN THE FORWARD AND AFT POSITIONS. OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F RTA6WE 19950310007031995031000703 1995 3 10 GRAA9530 419950221A344420676315112 RADIO ALT IND DOUG DC9 DC915 3022036WP COCKPIT FAILED A GRAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP111068T 45782 RENO, NEVADA - UPON TAXI OUT FROM GATE B-10, AIRCRAFT N1068T HAD A RADIO ALTIMETER FAIL FLAG IN BOTH RADIO ALTIMETERS. THE AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE CAPTAIN'S RADIO ALTIMETER INDICATOR AND THE SYSTEM CONTINUED TO FAIL. MAINTENANCE DEFERRED THE SYSTEM IAW MEL: 34-23. MAINTENANCE INSTALLED ANOTHER RADIO ALTIMETER INDICATOR IN THE CAPTAIN'S POSITION. OPERATIONAL CHECKED NORMAL. NO DEFECTS NOTED. CLEARED THE DEFERRAL. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950310007041995031000704SW 1995 3 10 MALA954289 119950206A52302724107053 HANDLE ASSY SWRNGNSA227 SA227AC 8780603SW CARGO DOOR DAMAGED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15159MC AC728 DTW - FLT 3395 - ON CLIMB-OUT, CARGO DOOR WARNING LIGHT ILLUMINATED AT 4.5 PSI DIFFERENTAIL. THE CREW REDUCED THE CABIN DIFFERENTIAL AND RETURNED TO DTW. MAINTENANCE REPLACED THE CARGO DOOR HANDLE ASSY. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950310007051995031000705NM 1995 3 10 MALA954290 119950206A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15832MA 341 DTW - FLT 3085 - DURING PRE-FLIGHT, THE FA REPORTED THE SECOND OVERHEAD EMERGENCY LIGHT WOULD INTERMITTENTLY ILLUMINATE. MAINTENANCE REPLACED BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950310007061995031000706SW 1995 3 10 MALA954291 119950206A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 491.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 MSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE NOTED A CRACK AT THE AFT FUSELAGE FRAME FS 491.060. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC LAR 95-MALA-042 AND SRM 51-00-00 STANDARD PRACTICES. (X) 1L72 4T A8SW 19950310007071995031000707SW 1995 3 10 MALA954292 119950207A57202731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW WS 27.103 WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT AND RT FLAP WALKING BEAM ROLLER DOUBLER WORN AT STATION WS 27.103. MAINTENANCE REPLACED LT AND RT AFT RIB DOUBLERS. (X) 1L72 4T A8SW 19950310007081995031000708SW 1995 3 10 MALA954293 119950207A53202731110033 CHANNEL SWRNGNSA227 SA227AC 8780603SW BL 0.00 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND FORWARD FAIRING CENTER ATTACH CHANNEL CRACKED AT THE HYDRAULIC LINE PASS-THROUGH. REPAIRS WERE COMPLETED BY INSTALLING REPAIR DOUBLERS IAW FAC SRM 57-90-30. (X) 1L72 4T A8SW 19950310007091995031000709SW 1995 3 10 MALA954294 119950207A53112722093145 FRAME SWRNGNSA227 SA227AC 8780603SW FS 189.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LT LOWER BELT FRAME CRACKED AT FS 189.06. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (X) 1L72 4T A8SW 19950310007101995031000710SW 1995 3 10 MALA954310 119950211A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1563NE AC763B MSP - FLT 3213 - DURING CLIMB-OUT, NOSE GEAR INTRANSIT LIGHT DID NOT GO OUT AFTER TAKEOFF. THE CREW CYCLED THE GEAR AND THE PROBLEM CONTINUED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE RERIGGED THE UP LIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950310007111995031000711SW 1995 3 10 MALA954311 119950212A32222752500001 STRUT SWRNGNSA227 SA227AC 8780603SW NLG LOW PRESSURE A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL1563NE AC763B MSP - FLT 3084 - ON CLIMB-OUT, NOSE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER RETRACTING GEAR. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE SERVICED THE NOSE GEAR STRUT. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950310007121995031000712NM 1995 3 10 MALA954312 119950212A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL15819MA 251 DTW - FLT 3187 - ON APPROACH, RIGHT GEAR HUNG UP FOR 15 SECONDS UPON GEAR EXTENSION. THE CREW PERFORMED A GO-AROUND AND THE GEAR EXTENDED NORMALLY ON THE SECOND ATTEMPT. MAINTENANCE REPLACED UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950310007131995031000713NM 1995 3 10 MALA954319 119950214A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15824MA 327 CMX - FLT 3125 - ON APPROACH, LT GEAR DID NOT EXTEND UPON GEAR EXTENSION. THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION AND THE GEAR EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT IN CMX. MAINTENANCE REPLACED THE UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950310007141995031000714SO 1995 3 10 RAIA950212 119950207A3350MS346L1210S EEL CONNECTOR EMB 120 EMB120RT SO CABIN MOISTURE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03129AM13872 120119 STL - AFT HALF OF THE FLOOR EMERGENCY ESCAPE PATH LIGHTING INOP. MAINTENANCE CLEANED CANNON PLUG ON POWER SUPPLY. SYSTEM CHECK GOOD. (X) 2L72 4T RTA31SO 19950310007151995031000715EU 1995 3 10 RAIA950213 119950208A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE14127 106 STL - EMERGENCY EXIT SIGNS BELOW EXITS INOP. MAINTENANCE RESEATED EMERGENCY BATTERY IN POWER SUPPLY. (X) 2H72 4T RTA53EU 19950310007161995031000716EU 1995 3 10 RAIA950214 119950210A33503012001 EEL BATTERY AEROSPATR72 ATR72202 8680940EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE6030 1845 283 MX - EMERGENCY LIGHT BATTERY DEAD AT ROW 3A AND ROW 3B. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY. (X) 2H72 4T RTA53EU 19950310007171995031000717 1995 3 10 RAIA950215 419950211A34257003110912 EHSI TUBE AEROSPATR42 ATR42300 8680920EU COCKPIT FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03423TE13501 119 STL - FLT 7142 - NR 1 EHSI FAILED. MAINTENANCE REPLACED NR 1 EHSI. (X) 2H72 4T RTA53EU 19950310007191995031000719NM 1995 3 10 TAOA019509 119950131A3350900835A EEL BATTERY PACKGRIMES BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 9455 20441 CEILING EMERGENCY EXIT LIGHT AT OVERWING EXIT INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OKAY. (X) 2L73 4F A3WE 19950310007201995031000720NM 1995 3 10 TAOA019510 119950131A3350900835A EEL BATTERY PACKGRIMES BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 22465 20441 EMERGENCY EXIT LIGHT AT FORWARD LIFE RAFT COMPARTMENT INOPERABLE. REPLACED BATTERY PACK - OPERATIONAL CHECK OKAY. (X) 2L73 4F A3WE 19950310007211995031000721EU 1995 3 10 UF6A950206 119950208A33506013211 EEL POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6AK NONE O OTHER ININSP/MAINT 1 CE03854AW6157 84 2028 ORD - FLT 5065 - EMERGENCY FLOOR PROXIMITY LIGHT STRIP INOP AT 7 C AND 7 D. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (X) 2L72 4T RTA27NM 19950310007221995031000722EU 1995 3 10 UF6A950207 119950209A3350363624 EEL STRIP BAG ATP ATP EU 243AS CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03851AW8481 2020 ORD - FLT 5049 - AFT FLOOR STRIP LIGHT INOP. MAINTENANCE REPLACED STRIP LIGHT. (X) 2L72 4T RTA27NM 19950310007231995031000723EU 1995 3 10 UF6A950208 119950210A3246L814794024 BEARING ROTOL 201045004 BAG ATP ATP EU LT MLG FAILED A UF6AO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 CE03854AW7563 1 DRG529188 2028 ORD - FLT 5101 - POST-FLIGHT INSPECTION FOUND NR 1 TIRE MISSING. MAINTENANCE REPLACED LT MLG ASSY. (X) 2L72 4T RTA27NM 19950310007241995031000724EU 1995 3 10 UF6A950209 119950210A3350HWBON11462BAU2 EEL CONNECTOR BAG ATP ATP EU CABIN DIRTY A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03855AW7109 2029 ORD - FLT 5033 - EMERGENCY FLOOR STRIP LIGHT INOP. MAINTENANCE CLEANED CONNECTOR. (X) 2L72 4T RTA27NM 19950310007251995031000725NM 1995 3 10 WRLA95004 119950220A2910BKJ12F123SDY175 CONNECTOR DOUG MD11 MD11 3023602NM NR 1 HYD PUMP LOOSE A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27271WA 48518 WHILE ON TAXI, FLIGHT CREW OBSERVED NR 1 ENGINE PUMP HYDRAULIC OFF LIGHT WOULD NOT EXTINGUISH. CREW SWITCHED HYD SYSTEM CONTROLLER FROM 'AUTO' TO 'MANUAL' AND THEN BACK TO 'AUTO'. HOWEVER, NR 1 ENGINE LT HYD PUMP WOULD NOT TURN OFF. CREW ELECTED TO RETURN TO GATE FOR REPAIRS. LINE MAINTENANCE FOUND CANNON PLUGS ON BOTH RT AND LT LOW PRESSURE HYD SWITCHES LOOSE AND DIRTY. CLEANED CANNON PLUG ON BOTH RT AND LT LOW PRESSURE SWITCHES AND RECONNECTED. IN ADDITION, REMOVED DEPRESSURIATION SOLENOID SWITCH, CLEANED AND RECONNECTED. HYDRAULIC SYSTEM CHECKED NORMAL ON ENGINE RUN. AIRCRAFT RETURNED TO SERVICE. THESE SPECIFIC CANNON PLUGS ARE LOOSENING ON A REPETITIVE BASIS. (X) 2L73 4F RTA22WE 19950310007261995031000726NM 1995 3 10 WRLA95005 119950217A2710B11005 CIRCUIT BREAKER DOUG MD11 MD11F 3023600NM AILERON CONTROL PULLED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27274WA 48633 DURING TAXI AND 'FLIGHT CONTROL CHECK', CREW UNABLE TO RECEIVE PROPER FLT CONTROL POSITION INDICATION FOR AILERONS. CREW ELECTED TO RETURN TO GATE FOR TROUBLESHOOTING. ACFT RETURNED TO GATE WITHOUT INCIDENT. UPON TROUBLESHOOTING, NOTED 'DEFLECTED AILERON' CIRCUIT BREAKER WAS PUSHED IN. SYSTEM DEACTIVATED PRIOR TO DELIVERY TO WO. FURTHER INVEST CONFIRMED C/B MISTAKENLY REACTIVATED BY REMOVING LOCKING COLLAR & RESETTING BY MX DURING LAST MX ACTIVITY. C/B PULLED & COLLARED, & FLT CONTROL TEST SUCCESSFULLY PERFORMED. ACFT RETURNED TO SERVICE. A 'SPECIAL MAINTENANCE' TASK CARD HAS BEEN DEVELOPED TO REMOVE & STOW WIRING THAT SUPPLIED POWER TO C/B, & A 'DEACTIVATED' PLACARD WILL BE PLACED OVER C/B LEGEND. (X)2L73 4F RTA22WE 19950310007271995031000727NM 1995 3 10 95ZZZW195 119950118A532065C10592142 INTERCOSTAL BOEING737 737301 1384611NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18 TO RBL 24 TO RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REF USAA950126. 2L72 4F RTA16WE 19950310007281995031000728NM 1995 3 10 95ZZZW196 119950215A323065404674 LOCK ACTUATOR BOEING727 72777C 1380420NM NLG INTERNAL FAILUREA RYNAO OTHER O OTHER LDLANDING 1 CE07526PC 20370 SEA - UPON LANDING, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED, HAD TO EXTEND NOSE GEAR MANUALLY. REMOVED AND REPLACED THE NLG LOCK ACTUATOR. 2L73 4F A3WE 19950310007291995031000729NM 1995 3 10 95ZZZW197 119950217A5330 SKIN BOEING737 737275 1384485NM BS 510 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ACCOMPLISHMENT OF LOWER LAP SKIN INSPECTION PER BSB 737 53A1177, SKIN CRACKS WERE IDENTIFIED AT BS 510 STR 10L, .200 INCHES IN LENGTH. ALL AREAS WERE REPAIRED IAW AWA EO 53-30-16 AND ER 2-53-33-08. REF 95ZZZW198, 95ZZZW199, 95ZZZW200, AWXA9500093. 2L72 4F A16WE 19950310007301995031000730NM 1995 3 10 95ZZZW198 119950217A5330 SKIN BOEING737 737275 1384485NM BS 845 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ACCOMPLISHMENT OF LOWER LAP SKIN INSPECTION PER BSB 737 53A1177, SKIN CRACKS WERE IDENTIFIED AT BS 845 STR 4L, .125 INCHES IN LENGTH. ALL AREAS WERE REPAIRED IAW AWA EO 53-30-16 AND ER 2-53-33-08. REF 95ZZZW197, 95ZZZW199, 95ZZZW200, AWXA9500093. 2L72 4F A16WE 19950310007311995031000731NM 1995 3 10 95ZZZW199 119950217A5330 SKIN BOEING737 737275 1384485NM BS 909 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ACCOMPLISHMENT OF LOWER LAP SKIN INSPECTION PER BSB 737 53A1177, SKIN CRACKS WERE IDENTIFIED AT BS 909 STR 20R, REMOVED WITH .0625 INCH OVERSIZE. ALL AREAS WERE REPAIRED IAW AWA EO 53-30-16 AND ER 2-53-33-08. REF 95ZZZW197, 95ZZZW198, 95ZZZW200, AWXA9500093. 2L72 4F A16WE 19950310007321995031000732NM 1995 3 10 95ZZZW200 119950217A5330 SKIN BOEING737 737275 1384485NM BS 953 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ACCOMPLISHMENT OF LOWER LAP SKIN INSPECTION PER BSB 737 53A1177, SKIN CRACKS WERE IDENTIFIED AT BS 953 STR 10R, REMOVED WITH .0625 INCH OVERSIZE. ALL AREAS WERE REPAIRED IAW AWA EO 53-30-16 AND ER 2-53-33-08. REF 95ZZZW197, 95ZZZW198, 95ZZZW199, AWXA9500093. 2L72 4F A16WE 19950310007331995031000733NM 1995 3 10 AWXA9500093 119950217A5330 SKIN BOEING737 737275 1384485NM BS 492 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ACCOMPLISHMENT OF LOWER LAP SKIN INSPECTION PER BSB 737 53A1177, SKIN CRACKS WERE IDENTIFIED AT BS 492 STR 10L, .125 INCHES IN LENGTH. ALL AREAS WERE REPAIRED IAW AWA EO 53-30-16 AND ER 2-53-33-08. REF 95ZZZW197, 95ZZZW198, 95ZZZW199, 95ZZZW200. 2L72 4F A16WE 19950310007341995031000734EU 1995 3 10 SIMA950552 119950224A5280S5287900100066 DOOR ASSY AEROSPATR72 ATR72212 EU LT MLG DEPARTED ACFT A ASIMAK NONE D INFLIGHT SEPARATION CRCRUISE 1 SW21410AT1634 410 DURING FLIGHT 3806, THE LT MLG BI-FOLD FOLLOW UP BLEW OFF. IT WAS NOTICED MISSING DURING PRE-FLIGHT WALK AROUND FOR NEXT FLIGHT SEGMENT. (W) 2H72 4T RTA53EU 19950310007351995031000735NM 1995 3 10 USAA950091 119950131A5350 FAIRING BOEING737 7374B7 1384702NM WING LOOSE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19441US 24812 CLT - FLT 2442 - ON CLIMB, AIRFRAME VIBRATION AT HGH POWER SETTNGS. NO VIBRATION AT IDLE POWER DESCENT OR LOW POWER SETTING. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE RUN AT ALL POWER SETTINGS. VIBRATION INDICATION NEVER EXCEEDED .5. PERFORMED AVM SIGNAL CHECK, BITE CHECKED OK. FOUND WING TO BODY FAIRING SEAL LOOSE. SEALED WING TO BODY FAIRINGS. OK FOR SERVICE. (W) 2L72 4F RTA16WE 19950310007361995031000736NM 1995 3 10 USAA950095 119950204A2750 BELLCRANK BOEING737 737401 1384701NM TE FLAPS WORN A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19411US 23880 MLB - FLT 1926 - DURING MISSED APPROACH AT MCO. FLAPS WOULD NOT RETRACT. FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL FLAP ASSEMBLYS, JACKSCREWS, AND CARRIAGES. COULD NOT DUPLICATE ANY FAULTS. FOUND RT O/B TRAILING EDGE FLAP 'A' ARM BELLCRANKS VERY WORN AT ROD END ATTACHMENT. REPLACED SAME, OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950310007371995031000737NM 1995 3 10 USAA950099 119950212A216039811611 MIX VALVE BOEING737 737301 1384611NM RIGHT PACK FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19560AU 23514 PIT - FLT 576 - ON CLIMB-OUT, CREW HAD NO CONTROL OVER RT AIR MIX VALVE. VALVE WENT FULL COLD AND WAS NOT CONTROLLABLE IN MANUAL OR AUTO. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED RT PACK AIR MIX VALVE. OPS CHECK, LEAK CHECK GOOD. (W) 2L72 4F RTA16WE 19950310007381995031000738WP 1995 3 10 USAA950106 119950208A3230 RETRACT MECH DOUG DC9 DC982 3022082WP NLG MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19824US 49143 MKE - FLT 293 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO MKE WITHOUT INCIDENT. INSPECTED NOSE GEAR RETRACT AND EXTEND MECH. NO DEFECTS NOTED. SERVICED NOSE GEAR STRUT, IAW DOUGLAS MM 32-21-02. GEAR SWING CHECKS GOOD. (W) 2L72 4F A6WE 19950310007391995031000739NM 1995 3 10 USAA950108 119950124A3010 TAI VALVE BOEING767 767201 1385125NM RT ENGINE INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19647US 23899 BWI - FLT 198 - FLIGHT DIVERTED TO BWI DUE TO E/M 'R ENG TAI VALVE'. PERFORMED MAINTENANCE PER FIMR PROCEDURES. VALVE CHECKS GOOD. (W) 2L72 4F RTA1NM 19950310007401995031000740NM 1995 3 10 USAA950109 119950201A2560 SLIDER SQUIB BOEING767 767201 1385125NM LEFT DIRTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19645US 23897 PIT - THE LT EMERGENCY SLIDER SQUIB DOES NOT TEST IN NR 1 POSITION, AND THE RT SLIDER SQUIB DOES NOT TEST IN THE NR 2 POSITION. MAINTENANCE CLEANED THE SWITCHES AND RELAYS. (W) 2L72 4F RTA1NM 19950310007411995031000741 1995 3 10 USAA950110 419950209A34256225048344 EFIS CONTL PANEL BOEING767 7672B7 1385107NM LEFT INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19654US 25225 BWI - FLT 194 - AFTER TAKEOFF, THE CAPTAIN'S ADI DISPLAY FAILED. FLIGHT RETURNED TO BWI. MAINTENANCE REPLACED THE CAPTAIN'S EFIS CONTROL PANEL. OPERATIONS CHECKED GOOD. (W) 2L72 4F RTA1NM 19950310007421995031000742NM 1995 3 10 USAA950115 119950119A53201136043 GIRT BRACKET BOEING737 737301 1384611NM BS 312/344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORRODED AREAS ON GIRT BRACKETS 2 PLACES. FWD ENTRY STA 312 AND STA 244. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007431995031000743NM 1995 3 10 USAA950117 119950111A5320 FLOOR SUPPORT BOEING737 737301 1384611NM STA 807-907 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION OF FLOOR SUPPORT, FOUND SURFACE CORROSION AROUND NUTPLATES 1 INCH BY 1 INCH SEVERAL PLACES 20 INCHES RBL BETWEEN STA 807 AND STA 907. REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007441995031000744NM 1995 3 10 USAA950118 119950119A5347 SEAT TRACK BOEING737 737301 1384611NM STA 887 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND .25 INCH BY .5 INCH GOUGE STA 887 LBL 25. REPAIRED PER SRM 53-00-52 FIG 204. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007451995031000745NM 1995 3 10 USAA950119 119950123A5320 SUPPORT ANGLE BOEING737 737301 1384611NM BS 727 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION , FOUND .75 INCH BY .75 INCH 6 AREAS CORROSION 4 INCHES AFT OF BS 727 D FROM BL 0 TO S-28 L BL 0 TO S-28 R UNDERSIDE OF ANGLES WHERE NUTPLATE ATTACHES. REPLACED PER T/R 53-10-06, SRM 53-00-53, AND BAC DRW. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007461995031000746NM 1995 3 10 USAA950120 119950111A5347 SEAT TRACK BOEING737 737301 1384611NM BS 294.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION OF SEAT TRACK, FOUND TWO CORROSION AREAS 1.0 INCH BY 1.0 INCH AND .500 BY 1.0 INCH, BETWEEN FWD GALLEY BULKHEAD AND BS 294.5, 42.0 INCHES FROM BBL 0. REPAIRED PER BOEING DRAWING 69-40352-6. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007471995031000747NM 1995 3 10 USAA950121 119950124A5315 FLOORBEAM BOEING737 737301 1384611NM BS 1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION WIDTH OF FLOORBEAM, FLOORBEAM HOLES CORRODE AT BS 1016. REPAIRED PER TYPICAL REPAIR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007481995031000748NM 1995 3 10 USAA950122 119950111A5315 FLOORBEAM BOEING737 737301 1384611NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORROSION ON FLOORBEAM AT BS 344 FROM BL 0 TO LBL 24 INCHES. REPAIRED PER TR 53-10-03. CORROSION TASK NR. C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007491995031000749NM 1995 3 10 USAA950123 119950111A5315 FLOORBEAM BOEING737 737301 1384611NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 31.0 INCH BY 2 INCH BS 328 FLOORBEAM T-CAP. REPAIRED PER SRM 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007501995031000750NM 1995 3 10 USAA950124 119950119A53206546812169 INTERCOSTAL BOEING737 737301 1384611NM BS 967-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 19 INCH CORRODED AREA ON INTERCOSTAL AT BS 967 TO BS 986 RBL 18 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007511995031000751NM 1995 3 10 USAA950125 119950118A532065C10592155 INTERCOSTAL BOEING737 737301 1384611NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 20 INCH CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007521995031000752NM 1995 3 10 USAA950126 119950118A532065C10592156 INTERCOSTAL BOEING737 737301 1384611NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 22 INCH CORRODED AREA ON INTERCOSTAL, BS 947 TO BS 967 RBL 18 TO RBL 24 TO RBL 40. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REF 95ZZZW195. 2L72 4F RTA16WE 19950310007531995031000753NM 1995 3 10 USAA950127 119950124A5320 CAP STRIP BOEING737 737301 1384611NM BS 1006-1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24.6 INCH BY 1.3 INCH CORROSION BS 1006 TO BS 1016 LBL 28 INCHES. REPAIRED PER SRM 51-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007541995031000754NM 1995 3 10 USAA950128 119950124A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 1006-1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 24 INCH BY 1.3 INCH CORROSION ON INTERCOSTAL BS 1006 TO BS 1016 RBL 18 INCHES. REPAIRED PER SRM 51-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007551995031000755NM 1995 3 10 USAA950129 119950117A532065C10592155 INTERCOSTAL BOEING737 737301 1384611NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES CORROSION ON INTERCOSTAL AT BS 947 TO BS 967 AT LBL 30. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007561995031000756NM 1995 3 10 USAA950130 119950111A53206545834260 INTERCOSTAL BOEING737 737301 1384611NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORROSION ON INTERCOSTAL AT BS 312 TO BS 328 AT LBL 12 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007571995031000757NM 1995 3 10 USAA950131 119950111A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .500 INCH CORROSION ON INTERCOSTAL BETWEEN BS 328 AND BS 344, 25 FROM BBL 0. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007581995031000758NM 1995 3 10 USAA950132 119950111A53206545834260 INTERCOSTAL BOEING737 737301 1384611NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUMEROUS SCREW HOLES .500 INCH BY 500 INCH, INTERCOSTAL BETWEEN BS 312 AND BS 328, 11.5 INCHES FROM BBL 0. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007591995031000759NM 1995 3 10 USAA950133 119950126A53121716748 HAT CHANNEL BOEING737 737301 1384611NM FWD BULKHEAD CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 30 INCH CORRODED AREA LT LAVATORY AFT FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007601995031000760NM 1995 3 10 USAA950134 119950119A53121716748 HAT CHANNEL BOEING737 737301 1384611NM FWD BULKHEAD CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 30 INCH CORRODED AREA RT AFT LAVATORY FWD BULKHEAD. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007611995031000761NM 1995 3 10 USAA950135 119950119A5320 ANGLE BOEING737 737301 1384611NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 VISUAL INSPECTION, FOUND 3 INCH BY 59 INCH CORRODED AREA, BS 947 TO 1006 LT SIDE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-2. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007621995031000762NM 1995 3 10 USAA950136 119950119A5320 ANGLE BOEING737 737301 1384611NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 5 SQUARE INCHES OF CORROSION BS 947 TO BS 1006. REPAIRED PER SRM 51-10-2 AND SRM 51-10-11. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007631995031000763NM 1995 3 10 USAA950140 119950119A5313 STRINGER BOEING737 737301 1384611NM BS 350-360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 R. REPAIRED PER SRM 53-00-03. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007641995031000764NM 1995 3 10 USAA950141 119950119A5313 STRINGER BOEING737 737301 1384611NM BS 350-360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER BENEATH PAINT 1 INCH BY 10 INCH BS 350 TO 360 S-25 L. REPAIRED PER SRM 53-00-03. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950310007651995031000765NE 1995 3 10 USAA950156 219950210A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE NR 1 FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CRCRUISE 1 EA19827US 48049 JAX - FLT 7004 - AT FL 310, THE CREW EXPERIENCED ACFT VIBRATION AND SURGE IN THE LT ENGINE EPR. THE CREW SET THE LT ENGINE BACK TO IDLE THEN SHUTDOWN THE ENGINE. THE ACFT WAS SLOWED DOWN TO 180 KNOTS AND HAD A SMOOTH RIDE TO JAX. THE SINGLE ENGINE TIME WAS APPROXIMATELY 12 TO 15 MINUTES. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT ENGINE. OPERATIONS CHECKED GOOD. SUSPECT ICE INGESTION IN REMOVED ENGINE. (W) 2L72 4F4 F A6WE E9NE 19950310007661995031000766NM 1995 3 10 USAA950157 119950223A32309527M99P11 FAN BLADES BOEING737 737301 1384611NM NR 2 ENGINE BIRD STRIKE A USAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 EA19589US 23934 LGA - FLT 488 - AT 500 FEET ON CLIMB-OUT, HAD A SUDDEN LOUD RUMBLE AND HIGH VIBRATION IN NR 2 ENGINE. WHEN POWER HAS REDUCED AT LEVEL OFF, NOISE DECREASED AND VIBRATION DECREASED TO NORMAL LEVELS. SUSPECTED BIRDSTRIKE. FLIGHT RETURNED TO LGA WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED FAN BLADES NR 21, 4, 23, 5, 24, 6, 25, AND 2, DUE TO BIRD INGESTION FOD. (W) 2L72 4F RTA16WE 19950320000011995032000001NE 1995 3 20 9503596611 219950306A7261 OIL FILTER BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 2 ENGINE CLOGGED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01611US 20356 662311 DURING CRUISE NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED TO ANC WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE. NO FUEL WAS DUMPED. DEBRIS WAS FOUND IN THE MAIN OIL FILTER. THE FILTER WAS REPLACED AND CHECKED OK AFTER ENGINE RUNUP. THE FILTER WAS STILL CLEAN WHEN REPLACED LATER AT MSP. 2L74 4F4 F A20WE E20EA 19950320000021995032000002EU 1995 3 20 9503623232 119950110A5350D53371604001 ANGLE AIRBUS320 A320211 3930320EU BELLY FAIRING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01332NW 319 DURING 'C' CHECK, FOUND THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B CRACKED. THE CRACK, EMINATES FROM THE FORWARD MOST EDGE TO THE 3RD FASTENER HOLE APPROXIMATELY 6 INCHES AFT OF THE FORWARD EDGE. THE ANGLE IS ATTACHED TO THE LEFT OVERWING EMERGENCY SLIDE PACK. REPAIRED PER NWA EA 32-095314. 2L72 4F RTA28NM 19950320000031995032000003WP 1995 3 20 MWEA95142 119950308A71105910298521 NOSE COWL DOUG DC9 DC932 3022066WP LT ENGINE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 2650 47133 DURING ROUTINE INSPECTION, THE LEFT ENGINE NOSE COWL WAS FOUND TO HAVE A 2 INCH CRACK ON LIP OF INLET BETWEEN TWO FASTENERS AT THE 4 O'CLOCK POSITION. REMOVED AND REPLACED WITH SERVICEABLE NOSE COWL. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950320000041995032000004WP 1995 3 20 MWEA95143 119950309A3350S103 EEL BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST CRCRUISE 1 GL31204ME 47680 CREW REPORTS THE LAST 4 TO 6 EMERGENCY FLOOR TRACK LIGHTS IN CABIN BLINKED ON IN CRUISE. PERFORMED OPS CHECK IAW MM 33-50-00. REPLACED D-CELL NICAD BATTERY IN AFT PACK AS PRECAUTION. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950320000051995032000005NM 1995 3 20 QXEA9500068 119950307A3350P4010021 BATTERY DHAV DHC8 DHC8102 2809003NM COCKPIT LIGHT DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09102AV 91 DURING MAINTENANCE COCKPIT EMERGENCY FLASHLIGHT WAS FOUND TO HAVE DEPLETED BATTERIES. BATTERIES REPLACED AND AIRCRAFT RELEASED FOR SERVICE. 2H72 4T RTA13NM 19950320000061995032000006NM 1995 3 20 QXEA9500070 119950307A353010042N PBE DHAV DHC8 DHC8102 2809003NM COCKPIT DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09828PH9869 287 DURING MAINTENANCE, FOUND COCKPIT PBE RED INDICATOR SHOWING. REPLACED PBE AND RELEASED AIRCRAFT FOR SERVICE. 2H72 4T RTA13NM 19950320000071995032000007EU 1995 3 20 QXEA9500073 119950310A33501820 EEL LAMP FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 DURING MAINTENANCE, FOUND CEILING EMERGENCY LIGHT FILLAMENTS INOP AT ROWS 1 AND 6. RELAMPED FIXTURES AND RELEASED AIRCRAFT FOR SERVICE. 2L72 4F RTA20EU 19950320000081995032000008NM 1995 3 20 QXEA9600069 119950317A27318409 TRIM ACTUATORS DORNER DORNERDO32 DO328100 2996000NM ELEVATOR MALFUNCTIONING A QXEAK NONE J WARNING INDICATION DEDESCENT 1 NM09330PH 3008 PDX - AT FL 260 ON DESCENT, MESSAGE ELEVATOR MISTRIM NOSE ON. AFTER AUTOPILOT DISCONNECT THE ELEVATOR TRIM WOULD NOT FUNCTION, THE TRIM WAS STUCK. FLIGHT CREW SELECTED STANDBY TRIM, BUT TRIM DIDN'T FUNCTION WITH CONTINUED FORWARD PRESSURE TO MAINTAIN FLIGHT PATH. AT LOWER ALTITUDE WITH AIRSPEED BELOW 200 KTS TRIM SPEED FAST ACTIVATED AND TRIM BEGAN TO FUNCTION NORMALLY FROM LEFT AND RIGHT SIDE. AIRCRAFT ACCELERATED TO 210 KTS AND TRIM FUNCTIONED NORMALLY, LEFT, RIGHT AND STANDBY. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. LEFT AND RIGHT TRIM ACTUATORS REPLACED IAW MAINT MANUAL. TRIM SYS OPS CHECKED GOOD. 2H72 4T RTA45NM 19950320000091995032000009EU 1995 3 20 QXEA9600071 119950317A33501315 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 OVERHEAD EVAC LIGHT IN CEILING IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. 2L72 4F RTA20EU 19950320000101995032000010EU 1995 3 20 QXEA9600072 119950317A3350608905 POWER SUPPLY FOKKER FOKKERF28 F28MK1000 4990808EU CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 ENTRYWAY EXIT LIGHT IS INOP ALONG WITH FORWARD CABIN EXIT SIGN AND FORWARD FLOOR PROXIMITY LIGHTS. NUMBER 2 AND 3 POWER SUPPLY REPLACED AND LIGHTS OPS CHECKED GOOD. 2L72 4F RTA20EU 19950320000111995032000011SW 1995 3 20 95ZZZZ126 119950210A56102621126006 WINDSCREEN SWRNGNSA227 SA227AC 8780603SW RT COCKPIT HEATING INOP A CHQAO OTHER O OTHER NRNOT REPORTED 1 EA233115K AC586 PILOT REPORTED THE RIGHT WINDSHIELD HEAT IS INOP. THE SYSTEM WAS TROUBLESHOT AND THE RIGHT WINDSCREEN WAS DETERMINED TO BE THE PROBLEM. THE RIGHT WINDSCREEN WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (Z) 1L72 4T A8SW 19950320000121995032000012SW 1995 3 20 95ZZZZ127 119950211A772231039201 TEMP SENSOR GARRTT SWRNGNSA227 SA227AC 8780603SW RT ENGINE FAILED A CHQAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 EA23359AE 0387 AC674 PILOT RETURNED TO FIELD DUE TO RT EGT INDICATION WENT TO ZERO. MAINTENANCE TROUBLESHOT SYSTEM AND DETERMINDED THAT THE RIGHT ENGINE TEMPERATURE SENSOR HAD FAILED. THE SENSOR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (Z) 1L72 4T A8SW 19950320000131995032000013EU 1995 3 20 95ZZZZ128 119950215A3010 DE-ICE BOOT SAAB SF340 340B 7860101EU RT HORIZ STAB LOOSE A CHQAK NONE O OTHER ININSP/MAINT 1 EA23252CH 340B252 AIRCRAFT RETURNED TO FIELD DUE TO VIBRATION. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE TOP TRAILING EDGE OF RT HORIZONTAL STABILIZER DE-ICE BOOT HAD COME LOOSE. THE BOOT WAS RESECURED AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL. (Z) 2L72 4T RTA52EU 19950320000141995032000014NE 1995 3 20 95ZZZZ129 319950220A6111 PROP BLADE SWRNGNSA227 SA227AC 8780603SW MCAULY4HFR344HFR34C652 NE RT ENGINE LEAKING A CHQAO OTHER K FLUID LOSS NRNOT REPORTED 1 EA23359AE 254 AC674 890509 PILOT REPORTED OIL LEAKING FROM RIGHT PROPELLER. MAINTENANCE INSPECTED AND DETERMINED THE NR 4 BLADE WAS LEAKING AT THE BLADE ROOT. THE PROPELLER WAS REPLACED AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. 1L72 4T A8SW 6 C3PNE 19950320000151995032000015EU 1995 3 20 95ZZZZ130 119950219A3230HP848930621 VALVE SAAB SF340 340B 7860101EU LANDING GEAR FAILED A CHQAO OTHER O OTHER ININSP/MAINT 1 EA23224TH 1018 340B224 MAINTENANCE NOTED THAT WHEN BATTERIES WERE TURNED ON THAT THE HYDRAULIC PUMP STARTED TO CYCLE EVERY 10-15 SECONDS. FURTHER TROUBLESHOOTING REVEALED THAT THE LANDING GEAR CONTROL VALVE HAD FAILED INTERNALLY. THE VALVE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. (Z) 2L72 4T RTA52EU 19950320000161995032000016WP 1995 3 20 95ZZZZ131 119950216A2120 AIR DISTR DOUG DC9 DC932 3022066WP CABIN ODOR A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11914VV 47486 FLT 462 - TPA-IAD - FLIGHT ATTENDANT REPORTED FAINT SMELL OF SMOKE IN CABIN ON APPROACH AT 8000 FEET. PRESSURE DUMPED AT SAME TIME. BOTH AIRFOIL AND ENGINE ANTI-ICE WERE ON. DUCT TEMP AND DUCT PRESSURE WERE OK. NO AIRFOIL TEMP HIGH LIGHTS ON. OPERATIONS CHECKED BOTH AIR CONDITIONING SYSTEMS PER MM 21-00 AND COULD NOT DUPLICATE. PRESSURE TO 20 IN HG. AIR CONDITION PRESSURE OK. CAPTAIN ON BOARD DURING OPS CHECK AND AGREED SYSTEM OK. CAPTAIN AND FIRST OFFICER BOTH REPORTED SMELLING NO SMOKE, ONLY 1 FLT ATTENDANT REPORTED FAINT SMELL. (Z) 2L72 4F A6WE 19950320000171995032000017EU 1995 3 20 95ZZZZ132 119950222A57127257001506 RIB SAAB SF340 SF340A 7850100EU WS 42.3 CORRODED H AY55K NONE O OTHER ININSP/MAINT 1 SO03360CA22761 006 340A006 DURING THE COURSE OF AN 8000 HOUR INSPECTION, FOUND LOWER WING RIB AT WS 42.3 HAD EXFOLATION IN THE FUEL TANK AREA UNDER PANEL 521AT. THIS AREA IS NORMALLY COVERED BY SEALANT AND IS NOT READILY AVAILABLE FOR INSPECTION. AREA WAS CLEANED AND FOUND CORROSION DEPTHS OF 100 PERCENT IN CERTAIN AREAS. CORROSION WAS REMOVED AND AREA REPAIRED IN ACCORDANCE WITH SAAB REPAIR SCHEME 72YFS0792. THIS IS THE FIRST OCCURANCE OF THIS TYPE DAMAGE FOUND AT THIS REPAIR STATIONS. 2L72 4T RTA52EU 19950320000181995032000018NM 1995 3 20 95ZZZZ133 119950215A323065404674 LOCK ACTUATOR BOEING727 72777C 1380420NM NLG FAILED A RYNAO OTHER O OTHER LDLANDING 1 CE07526PC 20370 UPON LANDING AT SEA THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED, HAD TO EXTEND NOSE GEAR MANUALLY. REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR. (Z) 2L73 4F A3WE 19950320000191995032000019NE 1995 3 20 C2XA95CL022 219950206A72613037223 CARBON SEAL AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE RT ENGINE NICKED A C2XAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SW0999838 259 120779 FLT NR 3565 - EWR-PHL - RIGHT ENGINE OIL PRESSURE WARNING WHEN RIGHT ENGINE WAS FEATHERED AT GATE. CONTRACT MAINTENANCE SERVICED ENGINE OIL AND GROUND RAN ENGINE. NO LEAKS WERE NOTED. AIRCRAFT WAS DETERMINED TO BE SAFE FOR A FERRY FLIGHT FROM PHL TO EWR. EWR MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE BREATHER TUBE CARBON SEAL IAW PWA MM 72-20-00. OPERATIONAL AND LEAK CHECKS WERE NOTED. AIRCRAFT WAS DETERMINED TO BE SAFE FOR A FERRY FLIGHT FROM PHL TO EWR. EWR MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE BREATHER TUBE CARBON SEAL IAW PWA MM 72-20-00. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2H72 4T4 TRTA53EU E20NE 19950320000201995032000020SO 1995 3 20 C2XA95CL025 119950211A5753KRP138112VT ROLLERS EMB 120 EMB120RT SO LT TE FLAP BINDING A C2XAO OTHER J WARNING INDICATION DEDESCENT 1 SW0916702 120078 FLT NR 3337 - PIT-CLE - FLAP DISAGREEMENT AFTER TAKEOFF, 1 MINUTE LATER CLEARED ITSELF. AFTER LANDING IN CLE MAINTENANCE CLEANED FLAP TRACKS AND ROLLERS. AIRCRAFT WAS SENT ON A TEST FLIGHT. TEST FLIGHT WAS UNSATISFACTORY. MAINTENANCE REMOVED AND REPLACED LEFT OUTBOARD FLAP ROLLERS AND SENT AIRCRAFT ON ANOTHER TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000211995032000021SO 1995 3 20 C2XA95CL028 119950211A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP INTERMITTENT A C2XAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 SW09347129505 120111 FLT NR 3287 - DAY-CLE - RECEIVED FLAP DISAGREEMENT ON WAY IN TO CLE. MAINTENANCE REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW EMB MM 27-50-07. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000221995032000022SO 1995 3 20 C2XA95CL029 119950211A27503075001007 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW09157217961 0137 120160 FLT NR 3182 - CLE-SYR - FLAP DISAGREEMENT AFTER TAKEOFF. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB MM 27-50-06. OPS CHECK GOOD. SENT AIRCRAFT ON TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000231995032000023SO 1995 3 20 C2XA95CL030 119950211A27523203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP INTERMITTENT A AC2XAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SW09197048487 0872 120086 FLT 3304 - TOL-CLE - FLAP DISAGREEMENT, LEFT AND RIGHT INBOARD SHOWING 10 DEGREES. MAINTENANCE REMOVED AND REPLACED OUTBOARD TRACKS ON INBOARD FLAPS. OPS CHECK GOOD. ON PREFLIGHT POWER UP RECEIVED FLAP CONTROL FAULT, WOULD NOT RESET. INBOARD SHOWED 10 DEGREES. MAINTENANCE REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR. OPS CHECK GOOD. PRIOR TO TEST FLIGHT RECEIVED CONTROL FAULT AND ASYMMETRY ON INBOARD FLAPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. SENT ON TEST FLIGHT. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE ON 2/13/95. (Z) 2L72 4T RTA31SO 19950320000241995032000024SO 1995 3 20 C2XA95CL031 119950211A5753KRP138112VT ROLLERS EMB 120 EMB120RT SO TE FLAPS BINDING A C2XAK NONE J WARNING INDICATION TOTAKEOFF 1 SW0917728 120182 FLT NR 3350 - CMH-CLE - AFTER TAKEOFF RECEIVED FLAP DISAGREEMENT, AFTER A MINUTE CLEARED ITSELF. UPON LANDING IN CLE MAINTENANCE CLEANED ALL FLAP TRACKS. AIRCRAFT SENT ON TEST FLIGHT. TEST FLIGHT WAS UNSATISFACTORY. MAINTENANCE THEN REMOVED AND REPLACED RIGHT HYDRAULIC RESERVOIR. SENT ON TEST FLIGHT. TEST FLIGHT UNSATISFOCTORY AGAIN. MAINTENANCE REMOVED AND REPLACED ALL OUTBOARD FLAP ROLLERS. SENT ON TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE ON 2/13/95. (Z) 2L72 4T RTA31SO 19950320000251995032000025NE 1995 3 20 C2XA95CL032 219950206A73103035317 FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DIRTY A C2XACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0917728 120182 FLT NR 3357 - CLE-MKE - RIGHT FUEL FILTER LIGHT CAME ON DURING TAKEOFF. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE LOW PRESSURE FILTER IAW EMB MM 73-13-03 AND 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA31SO E20NE 19950320000261995032000026NE 1995 3 20 C2XA95CL033 219950213A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT FAILED A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN JY WARNING INDICATION ENGINE STOPPAGE CLCLIMB 1 SW09157138310 115400 120114 115400 FLT NR 3183 - CLE-CLE - SHORTLY AFTER TAKEOFF THE LEFT ENGINE OIL PRESSURE DROPPED TO ZERO FOLLOWED BY A LOUD BANG. THE FLIGHT CREW SECURED THE LEFT ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-120 MM MAINTENANCE DIRECTIVES NR 7 AND NR 8, AND NR 9. ALL OPERATIONAL AND LEAKED CHECKS WERE GOOD IAW EMB-120 MM 61-00-00 AND 71-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA31SO E20NE 19950320000271995032000027SO 1995 3 20 C2XA95CL035 119950211A5753KRP138112VT ROLLERS EMB 120 EMB120RT SO LT TE FLAP BINDING A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0931711 120107 FLT NR 3183 - CLE-CLE - AFTER TAKEOFF, UPON FLAP RETRACTION, GOT DISAGREEMENT WARNING. OUTBOARD AND INBOARD FLAPS STAYED DOWN TWO LIGHT BARS. MAINTENANCE CLEANED ALL FLAP TRACK AND INSPECTED THE ROLLERS. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR A TEST FLIGHT, WAS UNSATISFACTORY. MAINTENANCE REMOVED AND REPLACED THE FLAP ROLLERS ON THE LEFT OUTBOARD FLAP IAW EMB-120 MM 27-50-12. OPERATIONAL CHECKS WERE GOOD EMB-120 MM 27-50-00. AIRCRAFT WAS AGAIN RELEASED FOR A TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000281995032000028SO 1995 3 20 C2XA95CL038 119950218A27523203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTION A AC2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09277169135 0796 120128 FLT - 3287 - GSO - ON FLAP RETRACTION A DISAGREEMENT OCCURRED. AFTER LANDING FLAPS CLEARED THEMSELVES. OUT STATION MAINTENANCE INSPECTED AND DETERMINED AIRCRAFT WAS SAFE FOR A FERRY FLIGHT FROM GSO TO CLE. CLE MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-09. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000291995032000029SO 1995 3 20 C2XA95IA026 119950216A3000PE4200732 LINE EMB 120 EMB120RT SO CENTER WING MISALIGNED A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW0912709 120101 LRD - FLT NR 2584 - UPON CLIMB, THE RIGHT DUCT LEAK LIGHT ILLUMINATED. THE PILOT REPORTED THAT THE LIGHT WOULD NOT EXTINGUISH UNITL THE RIGHT ENGINE WAS SHUTDOWN. THE CREW RETURNED TO THE FIELD, AFTER SHUTTING THE RIGHT ENGINE DOWN, WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT DE-ICE REGULATOR VALVE OVERBOARD VENT LINE NOT TO BE IN ALIGNMENT WITH OVERBOARD VENT HOLE IN THE ASSOCIATED ACCESS PANEL. MAINTENANCE REPOSITONED THE LINE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950320000301995032000030EU 1995 3 20 C2XA95IA027 119950219A5330S53371229258 PLATE AEROSPATR42 ATR42320 8680930EU FWD FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947801 60 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR ACTUATOR, FUSELAGE SIDE, ATTACHMENT PLATE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PLATE, AND THE AIRCRAFT WAS RELEASED TO SERVICE. (Z) 2H72 4T RTA53EU 19950320000311995032000031EU 1995 3 20 C2XA95IA028 119950219A7120S54210200000500 MOUNT AEROSPATR42 ATR42320 8680930EU LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947801 60 IAH - DURING C-CHECK INSPECTION, THE NR 1 ENGINE, INBOARD AFT, TRUSS MOUNT WAS FOUND TO BE CHAFED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MOUNT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. REF ATR NTM 54-21-21. (Z) 2H72 4T RTA53EU 19950320000321995032000032EU 1995 3 20 SIMA950411 119950210A2910MS27371G0143 HYD LINE AEROSPATR42 ATR42300 8680920EU HYD BAY CHAFED A SIMAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW21430MQ12088 0136 RSW - FLT 3525 - IN-FLIGHT FROM MIA TO RSW, BLUE SYSTEM HYDRAULIC LOW LEVEL INDICATION CAME ON FOLLOWED BY BLUE PUMP LOW PRESS AND LOSS OF BLUE HYD SYSTEM. AIRCRAFT DECLARED EMERGENCY AND MADE ZERO DEGREE FLAP LANDING AT RSW. EMERGENCY EVACUATION WAS NOT REQUIRED, LANDED WITHOUT INCIDENT. MTX INSPECTED AND FOUND PRESSURE LINE FROM BLUE HYD PUMP CHAFED. REPLACED LINE, PERFORMED NECESSARY LEAK CHECKS AND RETURNED AIRCRAFT TO SERVICE. PART TOTAL CYCLES, 15,980. (X) 2H72 4T RTA53EU 19950320000331995032000033WP 1995 3 20 USAA950064 119950105A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1388 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 1388 RT SIDE OF VERTICAL STAB ATTACH ANGLE. STOP DRILLED AND INSTALLED REPAIR ANGLES PER SRM 53-05 FIG 84 AND USAIR EA NR 29735. (Z) 2L72 4F A6WE 19950320000341995032000034WP 1995 3 20 USAA950065 119950105A5313 LONGERON DOUG DC9 DC981 3022081WP BS 28 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND SEVERAL CRACKS IN LONGERON 17L AT STATION 280. REPLACED LONGERON AND SPLICED PER SRM 53-02 FIG 2 AND USAIR EA NR 2893. (Z) 2L72 4F A6WE 19950320000351995032000035WP 1995 3 20 USAA950066 119950105A5313 LONGERONS DOUG DC9 DC981 3022081WP BS 1452 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND .5 INCH AND .75 INCH CRACK IN STATION 1452 LONGERONS 3R AND 3L. MANUAL NEW CLIP AND REPAIRED PER SRM 53-03. (Z) 2L72 4F A6WE 19950320000361995032000036WP 1995 3 20 USAA950067 119950105A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1388 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT STRINGER 1388 AFT SIDE OF CANTED BELT FRAME RT SIDE ATTACH ANGLE. INSTALLED ATTACH ANGLE STRAP REPAIR PER SRM 55-02 FIG 26. (Z) 2L72 4F A6WE 19950320000381995032000038WP 1995 3 20 USAA950069 119950109A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 885 CUSP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND A 3 INCH CRACK AT STATION 885 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND 2. (Z) 2L72 4F A6WE 19950320000391995032000039WP 1995 3 20 USAA950070 119950109A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 906 CUSP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.25 INCH CRACK AT STATION 906 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2. (Z) 2L72 4F A6WE 19950320000401995032000040WP 1995 3 20 USAA950071 119950110A5320 CLIPS DOUG DC9 DC981 3022081WP FWD CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19807US37207 48039 PIT - DURING Q-3 CHECK INSPECTION ACCOMPLISHED CORROSION CONTROL TASK ITEM NR C51-53300 AND FOUND LEVEL II CORROSION AT THE FORWARD CARGO DOOR HINGE ATTACH FLANGE CLIPS. MANU NEW CLIPS AND INSTALLED PER SRM 53-11-2. (Z) 2L72 4F A6WE 19950320000411995032000041NM 1995 3 20 USAA950096 119950207A56105893543109 WINDSHIELD BOEING737 7373B7 1384580NM L1 CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19526AU7353 23861 BWI - FLT EN ROUTE DCA TO CMH WHEN CAPTAINS OUTER WINDSHIELD PANE CRACKED. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED CAPTAINS L1 WINDSHIELD. (Z) 2L72 4F RTA16WE 19950320000421995032000042WP 1995 3 20 USAA950107 119950208A7920 OIL LINE DOUG DC9 DC981 3022081WP LT ENGINE INOPERATIVE A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19802US 48036 CLT - FLT 1133 - THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO, AND THE OIL PRESSURE ALSO DROPPED. THE ENGINE WAS SHUTDOWN AND FLIGHT DIVERTED TO CLT. MAINTENANCE REPLACED THE OIL LINE TO THE OIL PRESSURE SWITCH AND THE FILTERS. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950320000431995032000043WP 1995 3 20 USAA950111 119950211A26131173T0640 TEMP SENSOR DOUG DC9 DC931 3022065WP LT/RT TAIL INOPERATIVE A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19936VJ 48116 PIT - FLT 1560 - AFTER CLIMB AND ENTERING CRUISE, THE TAIL COMPARTMENT TEMPERATURE LIGHT ILLUMINATED. THE CREW DECIDED TO RETURN TO PIT. MAINTENANCE REPLACED BOTH LEFT AND RIGHT TAIL TEMPERATURE SENSORS. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950320000441995032000044NE 1995 3 20 USAA950112 219950210A7230 COMPRESSOR DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE RT ENGINE STALLS A AUSAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19828US 48028 708426 ROC - FLT 1890 - ON TAKEOFF, CREW HEARD A BANG. THE FIRST OFFICER CALLED FOR CONTINUOUS MAXIMUM POWER. CREW HEARD SEVERAL MORE COMPRESSOR STALLS. CAPTAIN NOTICED THAT THE EPR HAD ROLLED BACK TO 1.0 TO 1.2 POWR WAS PULLED BACK AND ALL ENGINE INDICATIONS APPEARED NORMAL. CAPTAIN DECLARED AND EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. OPERATIONS CHECKED GOOD. (Z) 2L72 4F4 F A6WE E9NE 19950320000451995032000045WP 1995 3 20 USAA950114 119950213A531159114471 FRAME DOUG DC9 DC931 3022065WP BS 389 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19997VJ67355 47336 IND - DURING CX-5 CHECK INSPECTION ACCOMPLISHED SID INSPECTION PSE 53.09.001A, FOUND .5 INCH CRACK AT STATION 389 LONGERON 17R. (VISUAL INSPECTION). CUT OUT DAMAGED AREA, INSTALLED FILLER/DOUBLER TYPE REPAIR PER DAC SRM 53-04 FIG 35 AND USAIR EA 29574. (Z) 2L72 4F A6WE 19950320000461995032000046WP 1995 3 20 USAA950150 119950109A5330 SKIN DOUG DC9 DC931 3022065WP STA 101 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK INSPECTION, FOUND A .75 INCH CRACK AT STATION 101 BETWEEN LONGERON 27R AND 28R SKIN. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-01 FIG 2 SHEET 3. (Z) 2L72 4F A6WE 19950320000471995032000047WP 1995 3 20 USAA950153 119950218A2424939D2171 REGULATOR DOUG DC9 DC931 3022065WP RT INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19995VJ 47334 RDU - FLT 0103 - THE RIGHT GENERATOR TRIPPED OFF LINE DURING FLIGHT. THERE WAS NO CROSS TIE LOCKOUT. THE FLIGHT DIVERTED TO RDU. MAINTENANCE REPLACED THE RIGHT VOLTAGE REGULATOR. OPERATIONS CHECKED NORMAL. (Z) 2L72 4F A6WE 19950320000481995032000048WP 1995 3 20 USAA950154 119950219A3260 SWITCH DOUG DC9 DC931 3022065WP NOSE GEAR DIRTY A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19939VJ 48120 CLT - FLT 1857 - THE NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE CREW DECIDED TO RETURN TO CLT. MAINTENANCE CLEANED THE NOSE GEAR UP PROXIMITY SWITCH. THE GEAR WAS CYCLED THREE TIMES WITH NO PROBLEMS. (Z) 2L72 4F A6WE 19950320000491995032000049WP 1995 3 20 USAA950155 119950216A3260 HARNESS DOUG DC9 DC982 3022082WP RT MLG MISALIGNED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19823US 49142 PIT - FLIGHT 1181 - AFTER TAKEOFF, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR AND GOT THREE GREEN LIGHTS. AFTER THE SECOND RETRACTION THE UNSAFE LIGHT STILL REMAINED ILLUMINATED. ON FINAL APPROACH JUST BEFORE GEAR EXTENSION, THE RED LIGHT WENT OUT GIVING NORMAL GEAR UP INDICATION. MAINTENANCE REPOSITIONED THE HARNESS LANDING GEAR. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950320000501995032000050NM 1995 3 20 USAA950158 119950226A2550 CARGO STRAP BOEING737 7374B7 1384702NM AFT CARGO DOOR JAMMED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19431US 24553 MIA - FLT 2240 - AFT CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF. FLIGHT RETURNED TO MIA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CARGO STRAP WEDGED BETWEEN ROLLER AND CAM. REMOVED STRAP AND CHECKED OPERATION OF DOOR WARNING SYSTEM. OPS CHECK NORMAL (Z) 2L72 4F RTA16WE 19950320000551995032000055CE 1995 3 20 95ZZZX1137 119950216A28221C73 PUMP AIRBORNE CESSNA501 501 2076603CE RT BOOST FAILED A ISYAK NONE O OTHER ININSP/MAINT 1 GL2568EA 2010 1D1 5010068 DURING POST-FLIGHT INSPECTION, A FUEL LOAD MISBALANCE WAS NOTED. ACTIVATED CROSS-FEED SYSTEM TO BALANCE LOAD. RIGHT BOOST PUMP RAN, BUT LOW FUEL WARNING. NO EVIDENCE OF CROSS-FEED WAS NOTED. TROUBLESHOOTING REVEALED RIGHT PUMP RUNNING, BUT NO FUEL FLOW. REPLACED RIGHT BOOST PUMP. 1L72 4F A27CE 19950320000911995032000091EU 1995 3 20 95ZZZX1173 119950124A2421 ALTERNATOR HAMFLUHFB320HFB320 4071204EU DC SYSTEM MISWIRED A GXPAK NONE BHWSMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC INADEQUATE Q C ININSP/MAINT 1 GL23171GA 1039 OPERATOR CONTROL NR GXPA543E. WHEN TURNING ON EITHER AIRFRAME ANTI-ICE OR DE-ICE, BOTH ALTERNATORS FELL OFF-LINE. INTERIOR OF ACFT FILLED WITH SMOKE. ALTERNATOR WAS WIRED INCORRECTLY TO THE AIRCRAFT. SMOKE WAS CAUSED BY ALTERNATOR PHASES BEING OUT OF SYNC. SUBMITTER RECOMMENDS PROPER TRAINING OR REMOVAL/INSTALLATION PROCEDURES. 2L72 4J A14EU 19950320000931995032000093CE 1995 3 20 95ZZZX1175 119950216A3244184F081 TIRE GOODYEARAERO CESSNA500 550 2076604CE BALANCE PATCH DEFECTIVE A ISYAK NONE O OTHER ININSP/MAINT 1 GL2584EA 414 32040910 5500484 WHILE MOVING AIRCRAFT INTO HANGAR, NOSE TIRE MADE ODD NOISE. DISASSEMBLY REVEALED BALANCE PATCH INSIDE TIRE HAD COME LOOSE. PATCH WAS FREE TO CHANGE POSITION. SUBMITTER SUSPECTS POOR QUALITY OF ADHESIVE. MANUFACTURER WAS NOTIFIED OF PROBLEM. LANDINGS, 41. 1L72 4F A22CE 19950320000941995032000094EU 1995 3 20 USAA950113 119950218A3230 RETRACT MECH FOKKERF28 F28MK0100 4990807EU NLG MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA19851US 11278 GSO - FLT 884 - AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT. RECYCLED GEAR. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE NLG DISCREPANCY. ALL INDICATIONS NORMAL. (W) 2L72 4F RT 19950320000951995032000095NM 1995 3 20 USAA950116 119950110A5311 FRAME BOEING737 737301 1384611NM BS 500 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND 4 INCH BY 2 INCH CORRODED AREA STA 500 D STR 27 LT. REPAIRED PER SRM 53-00-07 FIG 204. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950320000961995032000096NM 1995 3 20 USAA950137 119950126A5320 ANGLE BOEING737 737301 1384611NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 20 INCH IN LENGTH CORROSION SEVERAL AREAS, BS 947 TO BS 1006 'Z' ANGLE RT AFT SERVICE DOOR. REPAIRED PER SRM 51-70-11. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950320000971995032000097NM 1995 3 20 USAA950138 119950111A5320 ANGLE BOEING737 737301 1384611NM BS 294.5-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL, INSPECTION FOUND CORROSION TWO AREAS 2 INCH BY 2 INCH, 54.0 INCH BY 1 INCH 'Z' ANGLE FWD GALLEY SERVICE DOOR BS 294.5 TO BS 344. REPAIRED PER BOEING DRAWING 65-45875 AND SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950320000981995032000098NM 1995 3 20 USAA950139 119950120A5210 ANGLE BOEING737 737301 1384611NM FWD ENTRY DOOR CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19301AU27938 23229 INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND 8 SQUARE INCHES OF CORROSION 'Z' ANGLE FWD ENTRY DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950320000991995032000099NM 1995 3 20 USAA950145 119950215A21337110033 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19518AU31336 23704 BOS - FLT 83 - UNABLE TO PRESSURIZE ACFT ON CLIMB-OUT. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FWD OUTFLOW VALVE FOR DEFECTIVE SWITCH OPERATION. ALL CHECKS NORMAL. (W) 2L72 4F RTA16WE 19950320001001995032000100NM 1995 3 20 USAA950146 119950214A2150655281050 PACK BOEING737 7373B7 1384580NM RIGHT FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19520AU186 23706 PHL - FLT 1926 - UNABLE TO PRESSURIZE ACFT ON CLIMB. FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT INCIDENT. MAINTENACNE FOUND RT PACK NOT ABLE TO SUPPLY SUFFICIENT AIRFLOW. RELEASED ON MEL 21-1. REPLACED AIR CONDITIONING ACCESSORY UNIT M324. OPS CHECK NORMAL. CLEARED MEL. (W) 2L72 4F RTA16WE 19950320001011995032000101NM 1995 3 20 USAA950147 119950214A5753 ROLLERS BOEING737 737401 1384701NM TE FOREFLAP LOOSE A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19418US 23985 FLL - FLT 44 - DURING CLIMB AT APPROX 1,000 FEET FLAPS SET, ACFT EXPERIENCED VIBRATION WHICH INCREASED WITH AIRSPEED. FLIGHT RETURNED TO FLL WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FERRIED ACFT TO CLT. TIGHTENED ROLLERS ON BOTH I/B ENDS AND ON BOTH I/B FOREFLAP TOGGLES. CYCLED FLAPS, NO FURTHER DEFECTS NOTED ON TEST. (W) 2L72 4F RTA16WE 19950320001021995032000102NM 1995 3 20 USAA950148 119950214A5270 WIRE BOEING737 7374B7 1384702NM AFT CARGO BROKEN A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19781AU 25020 PHL - FLT 63 - AFT CARGO DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED 3 BROKEN WIRES AT AFT CARGO DOOR SWITCH. OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950320001031995032000103EU 1995 3 20 USAA950149 119950220A2133566920 VALVE FOKKERF28 F28MK0100 4990807EU AC BAY STICKING A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19856US 11286 PIT - FLT 428 - AT FL 330 GOT EXCESSIVE CABIN ALTITUDE MESSAGE. CABIN WAS APPROACHING 11,000 FEET. CREW DID EMERGENCY DESCENT IAW PROCEDURES. ALSO, TRIED MANUAL PRESSURIZATION BUT HAD NO RESPONSE. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PRESSURIZED ACFT. LEAK DOWN RATE WITHIN LIMITS. FOUND COOLING OUTFLOW VALVE STICKING. REPLACED VALVE, TEST OK. (W) 2L72 4F RT 19950320001041995032000104WP 1995 3 20 USAA950159 119950209A5347 TIE DN TRACK DOUG DC9 DC981 3022081WP BS 541/634 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 541 AND 634, LT SIDE TIE DOWN TRACK. INSTALLED REPAIR ANGLES PER TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950320001051995032000105WP 1995 3 20 USAA950160 119950209A5311 BELTFRAME DOUG DC9 DC981 3022081WP BS 1418 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK INSPECTION, FOUND TWO EACH CRACKS BOTH .5 INCH, STA 1418 LONGERON 2 LT BELTFRAME. CUT OUT DAMAGE AREA AND INSTALLED FILLER, DOUBLERS PER SRM 53-03 FIG 32 SHT 4 PG 135. (W) 2L72 4F A6WE 19950320001061995032000106WP 1995 3 20 USAA950161 119950125A5330 SKIN DOUG DC9 DC981 3022081WP BS 345 DENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND DENT BEYOND LIMITS .065 INCH DEEP FUSELAGE STA 345 LONGERON 20 RT. CUT OUT DAMAGED SKIN AND INSTALLED PLUG FILLER AND INTERNAL DOUBLER PER SRM 53-04 FIG 38 AND EA 26628 REV B. (W) 2L72 4F A6WE 19950320001071995032000107WP 1995 3 20 USAA950162 119950124A5330 SKIN DOUG DC9 DC981 3022081WP BS 229 DENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 DURING Q-4 CHECK, INSPECTION FOUND DENTS BOTH .063 INCH DEEP STA 229, LONGERONS 22 TO 26 LT, IN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED FLUSH REPAIR WITH INTERNAL FINGER DOUBLER. PER SRM 53-04 FIG 26. (W) 2L72 4F A6WE 19950320001081995032000108WP 1995 3 20 USAA950163 119950131A5330 SKIN DOUG DC9 DC981 3022081WP BS 823 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 823 LONGERON 29 RT, IN SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W) 2L72 4F A6WE 19950320001091995032000109WP 1995 3 20 USAA950164 119950131A5330 SKIN DOUG DC9 DC981 3022081WP BS 800 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I STA 800 BETWEEN LONGERONS 28 RT AND 29 RT SKIN. CORROSION TASK NR C22-57301. INSTALLED DOUBLER PER SRM 53-04 FIG 53. (W) 2L72 4F A6WE 19950320001101995032000110WP 1995 3 20 USAA950165 119950131A5320 STIFFENER DOUG DC9 DC981 3022081WP BS 1338 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND 1 INCH CRACK STA 1338 CENTER TOP OF AFT PASS DOCK IN STIFFENER. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2 SHEET 4. (W) 2L72 4F A6WE 19950320001111995032000111WP 1995 3 20 USAA950166 119950207A5330 SKIN DOUG DC9 DC981 3022081WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND .52 INCH CRACK STA 1437 BETWEEN LONGERON 2 AND 3 LT, IN SKIN. CUT OUT DAMAGE AND INSTALLED PLUG REPAIR DOUBLER PER SRM 53-04 FIG 38. (W) 2L72 4F A6WE 19950320001121995032000112WP 1995 3 20 USAA950167 119950207A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1412 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH STA 1418 LONGERON 2RT. SPLICED IN NEW SECTION OF LONGERON, PER SRM 53-02 FIG 5. (W) 2L72 4F A6WE 19950320001131995032000113WP 1995 3 20 USAA950168 119950207A5730 SKIN DOUG DC9 DC981 3022081WP RT WING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACKS 2 EACH .25 INCH BY .1250 INCH RT WING FUEL PANELS ACCESS DOOR AREA, LEADING EDGE SKIN. STOP DRILLED CRACKS, MFG DOUBLERS AND INSTALLED REPAIR PER SRM 57-06B PAGE 9 FIG 3. (W) 2L72 4F A6WE 19950320001141995032000114WP 1995 3 20 USAA950169 119950131A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1309 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND .75 INCH CRACK STA 1309 LONGERON 12 FEET. INSTALLED LONGERON AND SPLICE PER SRM USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950320001151995032000115WP 1995 3 20 USAA950170 119950131A5330 SKIN DOUG DC9 DC981 3022081WP BS 1172 LIGHTNING STRIKEA USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND LIGHTNING STRIKE .375 INCH BY .035 INCH DEEP STA 1172 LONGERON 30 IN SKIN. INSTALLED EXTERNAL DOUBLER, DAMAGE WAS BLENDED. PER SRM 53-04 FIG 38 VIEW G USAIR EA 29390. (W) 2L72 4F A6WE 19950320001161995032000116WP 1995 3 20 USAA950171 119950131A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 541 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 541 RT SIDE TIE DOWN TRACK. REMOVED CORROSION, CLEANED, ALODINE, PRIMED, INSTALLED 'L' ANGLES, PER USAIR TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950320001171995032000117WP 1995 3 20 USAA950172 119950131A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 693 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION STA 693 LT SIDE TIE DOWN TRACK. REMOVED CORROSION AND INSTALLED REPAIR STRAPS PER USAIR TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950320001181995032000118WP 1995 3 20 USAA950173 119950131A5347 SEAT TRACK DOUG DC9 DC981 3022081WP STA 332 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION BETWEEN STA 332 AND 389 RT I/B SEAT TRACK. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W) 2L72 4F A6WE 19950320001191995032000119WP 1995 3 20 USAA950174 119950124A5330 SKIN DOUG DC9 DC981 3022081WP BS 229 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND GOUGE .022 INCH IN FUSELAGE LT SIDE STA 229 BETWEEN LONGERON 18L AND 19L SKIN. BLENDED DAMAGED SKIN AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38. (W) 2L72 4F A6WE 19950320001201995032000120WP 1995 3 20 USAA950175 119950131A5347 SEAT TRACK DOUG DC9 DC981 3022081WP COCKPIT WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND COCKPIT AND CO-PILOTS AFT SEAT TRACKS WEAR BEYOND LIMITS. REMOVED AND INSTALLED REPAIR KIT PER TYPICAL REPAIR 53-20-06. (W) 2L72 4F A6WE 19950320001211995032000121WP 1995 3 20 USAA950176 119950206A5315991556171 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1338 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1338 RT LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. REPLACED TOP ANGLE AND INSTALLED DOUBLER REPAIRS, WEB AND FITTING TYPICAL REPAIR 53-10-14 AND SRM 53-05 FIG 72. (W) 2L72 4F A6WE 19950320001221995032000122WP 1995 3 20 USAA950177 119950206A5315 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1332 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED STA 1322 RT SIDE LAV AREA FLOORBEAM. CORROSION TASK NR C58-53300. CUT OUT DAMAGED AREA, INSTALLED FILLER, REPAIR ANGLES AND DOUBLER. PE SRM 53-05 TYPICAL REPAIR 53-10-19 EA 29461. (W) 2L72 4F A6WE 19950320001231995032000123WP 1995 3 20 USAA950178 119950203A5320 ATTACH ANGLE DOUG DC9 DC981 3022081WP BS 1338 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CORROSION LEVEL I AREA PREVIOUSLY REWORKED AFT PAC DOOR LOWER THRESHOLD ATTACH ANGLE STA 1338 AT FLOOR PANEL NR 101 ATTACH ANGLE. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 34 EA 29474. (W) 2L72 4F A6WE 19950320001241995032000124WP 1995 3 20 USAA950179 119950206A53111195132 BELTFRAME DOUG DC9 DC981 3022081WP BS 446 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .25 INCH STA 446 LONGERON 30 BELTFRAME. INSTALLED REPAIR 'J' ANGLE PLATES PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950320001251995032000125WP 1995 3 20 USAA950180 119950209A5532 SKIN DOUG DC9 DC981 3022081WP BS 1408/1429 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19806US36862 48038 PIT - DURING Q-4 CHECK, INSPECTION FOUND CRACK .5 INCH AT STA 1408 AND 1429 LT SIDE LONGERON 2 LT DORSAL FIN SKIN. CUT OUT DAMAGE SKIN AND INSTALLED SKIN SPLICE REPAIR PER DACO PER SKETCH 3413J AND EA 29421 AND EO 5388X223. (W) 2L72 4F A6WE 19950320001261995032000126EU 1995 3 20 C2XA95CL036 119950211A315045150560 ALPHA PROBE AEROSPATR42 ATR42320 8680930EU FWD FUSELAGE FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0923802 593 064 FLT 3248 - GSO- ENROUTE, CAPTAIN ALPHA PROBE FAULTED. FOUND ALPHA PROBE CIRCUIT BREAKER OUT. RETURNED TO GSO AND REMAINED IN VISUAL NON-ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED THE LEFT ALPHA PROBE IAW ATR JIC 31-53-11-RAI-10000-003. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950320001271995032000127EU 1995 3 20 C2XA95IA025 119950216A5330S53572601202 SKIN STRAP AEROSPATR42 ATR42320 8680930EU FS 11660 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0918814 103 IAH - DURING A SCHEDULED ACCOMPLISHMENT OF SSI 53-51-26, THE LEFT MAIN LANDING GEAR WHEEL WELL SKIN STRAP AT STATION 11660/FRAME 25, BETWEEN STRINGERS 15 AND 16, WAS FOUND TO BE CRACKED. THE AFFECTED AREA WAS REPAIRED BY BLENDING THE CRACKED MATERIAL, AND INSTALLING A DOUBLER. ALL WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION NR EC5310-01067, AND ATR DRAWING NR 15S53R0045. (W) 2H72 4T RTA53EU 19950320001281995032000128WP 1995 3 20 HAL95021 119950220A3231188001 CONTROL CABLE DOUG DC9 DC951 3022051WP RT MLG DOOR BROKEN A HALAO OTHER O OTHER LDLANDING 1 WP132FOR 47742 HNL - FLT 127 - CORRECTED SDR TO REFLECT CORRECT FLT NR. RIGHT MAIN GEAR DOOR CAME DOWN DURING LANDING ROLL AT 80 TO 90 KNOTS. ALL CONDITIONS NORMAL DURING TOUCH DOWN AND DURING GEAR DOWN CHECK, NO GEAR DOOR OPEN LIGHT SEEN UNTIL SCRAPING SOUND AS AIRCRAFT DECELERATED. FOUND RT GEAR DOOR POSITION SEQUENCE CABLE TUBE ASSY SPOT WELD BROKEN AND SHIFTED TO THE RIGHT APPROXIMATELY 2 INCHES. REMOVED DOOR AND INSPECTED HINGE. NO DEFECTS NOTED. INSTALLED SERVICEABLE DOOR PER MM 32-12-1. INSTALLED MLG PUSH/PULL CABLE PER MM 32-31-0. ADJUSTMENT/TEST PER MM 32-31-0. GEAR SWING AND FREE-FALL CHECK OKAY. INSPECTED NR 2 ENGINE INLET FOR FOD AND NO DAMAGE NOTED. (X) 2L72 4F RTA6WE 19950320001291995032000129 1995 3 20 HAL95022 419950218A34215223700004 ADI DOUG DC9 DC951 3022051WP LT COCKPIT FAILED A HALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13420EA 132 47689 FLT NR 172 - HNL - CAPTAINS ADI GYRO FLAG ON ADI STUCK ON 12 DEGREES NOSE-UP. MADE AIR TURN BACK TO HNL. REMOVED AND REPLACED THE CAPTAINS ADI AND THE GROUND OPERATIONAL CHECK WAS OK. (W) 2L72 4F A6WE 19950320001301995032000130NM 1995 3 20 IXKA9500009 119950223A2750696670833 CONTROL CABLE BOEING727 727251 138408HNM RT TE FLAP BROKEN A IXKAK NONE O OTHER ININSP/MAINT 1 EA25264US 19983 AT EWR, ON POST FLIGHT INSPECTION FOUND RIGHT INBOARD FLAP CABLE FOR FOLLOW UP DRUM BROKEN. REMOVED AND REPLACED RT INBOARD AFT FLAP CABLE PER MM 27-51-05. OPS CHECK OK. (W) 2L73 4F A3WE 19950320001311995032000131NM 1995 3 20 IXKA9500010 119950225A5210 DOOR BOEING727 727225 1384077NM L2 DOOR NOT CLOSED A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA258880Z 21453 AFTER TAKEOFF, FLT NR 52, PBI TO EWR, UNABLE TO PRESSURIZE AIRCRAFT DUE TO AIR LEAK AT L2 DOOR. SECOND OFFICERS ANNUNCIATOR SHOWED ALL DOOR CLOSED. DIVERTED TO ATL. FOUND L2 DOOR NOT FULLY CLOSED. CHECKED DOOR STOPS AND HINGES, CHECKED OK. (W) 2L73 4F A3WE 19950320001321995032000132NM 1995 3 20 MZZA9509 119950223A21505727561 TEMP SWITCH BOEING727 727212 138407GNM RT PACK FAILED A MZZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13296AS 21459 FLT 925 - GUM - AFTER TAKEOFF RIGHT AIR CONDITIONING PACK TRIPPED OFF. CREW PERFORMED ABNORMAL CHECK LIST AND COULD NOT RESET PACK. AIRCRAFT RETURNED BACK TO GUM. MAINTENANCE FOUND RIGHT PACK 190 DEGREES TEMP SWITCH AT FAULT. REMOVED AND REPLACED TEMP SWITCH ASSY, RIGHT PACK OPERATION CHECK GOOD. (W) 2L73 4F A3WE 19950320001331995032000133WP 1995 3 20 USAA950072 119950118A5753 SPAR CAP DOUG DC9 DC931 3022065WP RT FLAP STATION CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN RT FLAP LOWER SPAR CAP STATION XFIS 304.031. SPLICED IN NEW SECTION OF SPAR CAP PER DAC REPAIR DWB J060179 AND USAIR EA 29245. (W) 2L72 4F A6WE 19950320001341995032000134WP 1995 3 20 USAA950073 119950105A5320 CUSP MEMBRANE DOUG DC9 DC931 3022065WP BS 598 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK AT CUSP MEMBRANE AT STATION 598 RIGHT. SPLICED IN SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96. (W) 2L72 4F A6WE 19950320001351995032000135WP 1995 3 20 USAA950074 119950112A5320 CUSP MEMBRANE DOUG DC9 DC931 3022065WP BS 598 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION, FOUND .75 INCH CRACK IN CUSP MEMBRANE AT STATION 598 LEFT. SPLICED IN SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 96. (W) 2L72 4F A6WE 19950320001361995032000136WP 1995 3 20 USAA950075 119950106A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK NR C58-53300 ON THE RT LAV FLOOR BEAM STATION 990 GROUND LEVEL I CORROSION (PREVIOUSLY REWORKED). INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 20A. (W) 2L72 4F A6WE 19950320001371995032000137WP 1995 3 20 USAA950076 119950112A5320 FLOOR SUPPORT DOUG DC9 DC931 3022065WP STA 965 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C58-5330 ON FLOOR SUPPORT AT STATION 965 RT LAV PREVIOUSLY REWORKED, LEVEL I. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-10-14. (W) 2L72 4F A6WE 19950320001381995032000138WP 1995 3 20 USAA950077 119950109A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 465 GROOVED/WORK A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION FOUND DEEP GROOVES IN FLOOR BEAM STATION 465 CAUSED BY FLOORBOARD. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 20/20A. (Z) 2L72 4F A6WE 19950320001391995032000139WP 1995 3 20 USAA950078 119950109A5321 FLOOR SKIN DOUG DC9 DC931 3022065WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C46-53303 INSIDE OF SERVICE DOOR STATION 200 FOUND LEVEL I CORROSION ON SUBFLOOR. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFLOOR PER SRM 53-01 FIG 2. (Z) 2L72 4F A6WE 19950320001401995032000140WP 1995 3 20 USAA950079 119950109A5321 FLOOR SKIN DOUG DC9 DC931 3022065WP BS 160-200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION ACCOMPLISHED CORROSION TASK C45-53301 AND C46-53303 FOUND LEVEL I CORROSION ON SUBFLOOR SKIN UNDER THRESHOLD AT STATION 160-200. AREA WAS PREVIOUSLY 6 INCH BY 14 INCH. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SUBFLOOR PER SRM 53-01 FIG 2. (W) 2L72 4F A6WE 19950320001411995032000141WP 1995 3 20 USAA950080 119950106A5313 LONGERON DOUG DC9 DC931 3022065WP BS 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19977VJ32293 48155 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT STATION 200, LONGERON 15L INNER SKIN WEB AT RIVET. INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2. (W) 2L72 4F A6WE 19950320001451995032000145WP 1995 3 20 USAA950100 119950209A3222 NLG STRUT DOUG DC9 DC931 3022065WP NLG FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19920VJ 48140 PIT - FLT 1297 - ON CLIMB-OUT, THE CAPTAIN PULLED THE GEAR HANDLE BUT IT WOULD NOT GO INTO THE 'UP' POSITION. CREW DECIDED TO RETURN TO PIT. MAINTENANCE DRAINED FLUID FROM THE NOSE LANDING GEAR LOWER LEG, REINSTALLED THE LOWER LEG AND SERVICED. NUMEROUS GEAR SWINGS WERE PERFORMED. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950320001461995032000146WP 1995 3 20 USAA950101 119950208A216032185831 TEMP CONTL VLV DOUG DC9 DC931 3022065WP LT PACK STUCK A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19986VJ 47209 CLT - FLT 0881 - DURING CLIMB, BOTH PACKS FAILED. THE RIGHT PACK RETURNED FOR 15 SECONDS THEN FAILED AGAIN. CREW RETURNED CLT. MAINTENANCE FOUND THE LEFT TEMPERATURE CONTROL VALVE STUCK OPEN CAUSING THERMOL TRIP ON LEFT PACK. THE LEFT PACK TEMPERATURE CONTROL VALVE WAS REPLACED. OPERATIONS CHECKED NORMAL. (W) 2L72 4F A6WE 19950320001471995032000147WP 1995 3 20 USAA950102 119950207A3222 STRUT DOUG DC9 DC931 3022065WP NOSE GEAR INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19965VJ 47374 SYR - FLT 0545 - AFTER TAKEOFF, CREW RECEIVED A NOSE GEAR UNSAFE LIGHT. THE GEAR WAS CYCLED TWO MORE TIMES AND THE LIGHT REMAINED ON. THE FLIGHT DIVERETED TO SYR AND LANDED SAFELY. MAINTENANCE SERVICED THE NOSE STRUT. A GEAR SWING WAS PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT OK FOR SERVICE. (W) 2L72 4F A6WE 19950320001481995032000148WP 1995 3 20 USAA950103 119950107A32607000010101 SWITCH DOUG DC9 DC931 3022065WP NOSE GEAR FAULTY A USAAO OTHER P NO WARNING INDICATION DEDESCENT 1 EA19943VJ 47058 PIT - FLIGHT 0310 - CREW COULD NOT GET A GREEN LIGHT ON THE NOSE GEAR. THE GEAR WAS RECYCLED AND THE NOSE GEAR GREEN DOWNLOCK LIGHT CAME ON. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH. (W) 2L72 4F A6WE 19950320001491995032000149WP 1995 3 20 USAA950104 119950206A3222 STRUT DOUG DC9 DC931 3022065WP NOSE GEAR FLAT A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19941VJ 47054 PIT - FLT NR 1576 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM PIT. MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT ON ARRIVAL AT THE GATE. THE STRUT WAS SERVICED WITH NITROGEN AND THE STRUT INFLATED TO THE PROPER HEIGHT. (W) 2L72 4F A6WE 19950320001501995032000150WP 1995 3 20 USAA950105 119950203A3230 UPLATCH ROLLER DOUG DC9 DC931 3022065WP RT MLG LOOSE A USAAO OTHER O OTHER DEDESCENT 1 EA19927VJ 48154 CAE - FLT 0253 - ON LANDING IN CAE, THE GEAR DOOR OPEN LIGHT WOULD NOT GO OUT. THE GEAR WAS RECYCLED THREE TIMES BUT THE LIGHT REMAINED ON. MAINTENANCE SECURED A LOOSE ROLLER ON THE RIGHT MAIN LANDING GEAR UPLATCH. CHECKED OTHER PORTIONS OF THE DOOR INDICATION SYSTEM. NO DEFECTS WERE NOTED. GEAR WAS SWUNG SEVERAL TIMES. ALL INDICATIONS WERE NORMAL. (W) 2L72 4F A6WE 19950320001511995032000151NE 1995 3 20 VTZA95079 219950225A731030356811 FUEL FILTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 2 ENG DIRTY A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27417AW 285 FLT NR 6529 - IAD-LGA - THE NR 2 FUEL FILTER BYPASS CONTAMINATION LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT RETURNED TO IAD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE HIGH PRESSURE FUEL FILTER. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (W) 2H72 4T4 TRTA13NM E20NE 19950320001521995032000152EU 1995 3 20 VTZA95080 119950207A7603 SPEED LEVER JETAIRJETSTMJETSTM4101 1500501EU NR 1 ENG OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27317UE 41031 DURING TAKEOFF, FLT NR 6319, IAD TO CLE, ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 89 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT.S MAINTENANCE RERIGGED NR 1 ENGINE SPEED LEVER. GROUND RUNS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950320001531995032000153EU 1995 3 20 VTZA95081 119950227A3060B40610 DE-ICE LEAD JETAIRJETSTMJETSTM4101 1500501EU RT PROP BROKEN A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27306UE 41020 DURING TAXI FOR TAKEOFF, FLT NR 6210, PVD-IAD, RETURNED TO GATE DUE TO THE RT PROP HEAT INDICATING INOP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 3 BLADE DE-ICE LEAD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950320001541995032000154WP 1995 3 20 9503639928 119950307A5241 FITTING DOUG DC9 DC931 3022065WP GALLEY DOWN CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018921E 45836 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE FOUND GALLEY DOOR STOP FITTINGS WORN AND CORRODED. REPAIRED FITTINGS PER EA 99-092285. 2L72 4F A6WE 19950320001551995032000155WP 1995 3 20 9503649996 119950308A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK, FOUND CRACKED FITTING AT FS 604 AT LONGERON 24R. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950320001561995032000156NE 1995 3 20 9503656636 219950310A7200 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 1 FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01636US 23547 715250 DURING CRUISE, THE NR 1 ENGINE LOST OIL PRESSURE AND WAS SHUTDOWN, 70,000 LBS FUEL WAS DUMPED. THE AIRCRAFT DIVERTED TO NRT WHERE AN UNEVENTFUL THREE LANDING WAS MADE. THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E3NE 19950320001571995032000157WP 1995 3 20 9503669760 119950307A5350 RELEASE MECH DOUG DC9 DC941 302207NWP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01760NW 47288 DURING PERIODIC CHECK, FOUND THE TAILCONE RELEASE MECHANISM OUT OF RIG. RE-RIGGED TAILCONE, CHECKED OK. 2L72 4F A6WE 19950320001581995032000158WP 1995 3 20 9503679927 119950308A5220 DOOR MECHANISM DOUG DC9 DC931 3022065WP RT EMER EXIT WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING PERIODIC CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO LATCH THE FORWARD RIGHT OVERWING EMERGENCY EXIT HANDLE. REPLACED THE DOOR, CHECKED OK. 2L72 4F A6WE 19950320001591995032000159 1995 3 20 9503683214 419950309A31609615325021 DMC AIRBUS320 A320211 3930320EU NR 1 SYST FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01314US196167257 160 DURING TAKEOFF ROLL, THE CAPTAIN'S PRIMARY FLIGHT DISPLAY, NAVIGATION DISPLAY AND UPPER ENGINE DISPLAY FAILED. THE TAKEOFF WAS ABORTED AT 60 KNOTS. ECAM FAULTED EIS DMC NR 1. PLACED NR 1 DISPLAY MANAGEMENT COMPUTER ON MEL 31-63-01 AND LATER REPLACED. OPS CHECKED OK. 2L72 4F RTA28NM 19950320001601995032000160WP 1995 3 20 9503691144 119950312A5311 FRAME DOUG DC10 DC1040 3023508WP FS 1099 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LOWER CHORD OF FRAME AT FS 1099, STRINGER 51R AND 52R. REMOVED DAMAGED AREA AND INSTALLED SPLICES PER EA 11-97861. 2L73 4F A22WE 19950320001611995032000161WP 1995 3 20 9503701144 119950312A5730 SKIN DOUG DC10 DC1040 3023508WP LT WING LE CRACK A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LEADING EDGE SKIN AT THE FORWARD INBOARD CORNER OF FUELING ACCESS DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 11-89870. 2L73 4F A22WE 19950320001621995032000162WP 1995 3 20 9503711144 119950309A5315 FLOORBEAM DOUG DC10 DC1040 3023508WP FS 939 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE FLOORBEAM AT FS 939 IN FORWARD CARGO COMPARTMENT. 2L73 4F A22WE 19950320001631995032000163WP 1995 3 20 9503721144 119950311A5311 FRAME DOUG DC10 DC1040 3023508WP FS 1902/1997 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON FRAME AT FS 1902 LONGERON 51R TO 50L AND FS 1997 LONGERON 51L TO 48R. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-97827. 2L73 4F A22WE 19950320001641995032000164NM 1995 3 20 9503735514 119950310A3260 INDICATOR BULB BOEING757 757251 1384970NM RT MLG FAILED A NWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL01514US 23202 EXECUTED A GO-AROUND AT MSP DUE TO THE RIGHT MAIN GEAR GREEN LIGHT WOULD NOT COME ON. ACFT LANDED WITHOUT INCIDENT. REPLACED INDICATOR BULB, SYSTEM CHECKED NORMAL. 2L72 4F RTA2NM 19950320001651995032000165EU 1995 3 20 9503743214 119950312A5246 HYD DOOR AIRBUS320 A320211 3930320EU AFT FUSELAGE LOOSE A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01314US 160 DURING CLIMB-OUT FROM DTW, EXPERIENCED MEDIUM FREQUENCY AIRFRAME VIBRATION AT 310 KNOTS. LEVELED OFF AT FL230 AND REDUCED SPEED TO 290 KNOTS AND VIBRATION STOPPED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED YELLOW HYDRAULIC SYSTEM ACCESS DOOR WITH SLIGHT AMOUNT OF LOOSENESS. REPOSITIONED LATCH, OPS CHECKED OK. 2L72 4F RTA28NM 19950320001661995032000166NM 1995 3 20 95UAL727024 119950313A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297269U 21416 TWO CEILING EMERGENCY LIGHTS IN COACH CABIN WILL NOT TEST. REPLACED BATTERY PACKS. 2L73 4F4 F A3WE E2EA 19950320001671995032000167NM 1995 3 20 95UAL737005 119950118A38001060871383 FILL LINE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LAVATORY LEAKING A UALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP29374UA 24639 726449 DURING STEADY CRUISE FLIGHT LEVEL 350, HEARD LOUD BANG AND FELT YAW TO RIGHT. NR 2 ENGINE INDICATED FLAME-OUT. SHUTDOWN ENGINE AND PULLED FIRE HANDLE. FOUND EVIDENCE OF BLUE ICE INGESTION. BORESCOPED ENGINE AND ACCOMPLISHED A POWER ASSURANCE RUN, CHECKED OK. THE LAVATORY FILL LINE WAS FOUND LEAKING, AND WAS REPLACED. 2L72 4F4 FRTA16WE E2GL 19950320001681995032000168NM 1995 3 20 95UAL737023 119950307A2910654468311 HYD MODULE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE WHEEL WELL CRACKED A UALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP299072U 19953 AFTER TAKEOFF WITH GEAR AND FLAPS UP, FLIGHT CONTROL WARNING LIGHT AND STANDBY HYDRAULIC SYSTEM LOW QUANTITY LIGHT CAME ON. 'A' SYSTEM QUANTITY READ ONE GALLON. REPLACED HYDRAULIC STANDBY MODULAR PACKAGE DUE TO A CRACKED HOUSING. ALSO, REPLACED STANDBY PUMP AND CASE DRAIN FILTER. SERVICED SYSTEM AND CHECKED OK. 2L72 4F4 F A16WE E2EA 19950320001691995032000169NM 1995 3 20 95UAL737026 119950308A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29302UA 23643 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS 11,13,17,18 AND EMERGENCY EXIT LIGHT AT DOOR TWO LEFT. REPLACED BATTERY PACK AND CHARGER ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 19950320001701995032000170NM 1995 3 20 95UAL737027 119950308A335060243 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN SHORTED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29349UA 24253 FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING INOP. FOUND EMERGENCY ESCAPE PATH LIGHT STRIP SHORTED BY FORWARD GALLEY. REPLACED LIGHT ASSEMBLY, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950320001711995032000171NE 1995 3 20 95UAL737028 219950308A7200 ENGINES BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1/2 BIRD STRIKE A UALACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 WP29946UA 26687 CREW REPORTS, ABORTED TAKEOFF BECAUSE THEY STRUCK A FLOCK OF SEAGULLS. ACCOMPLISHED BIRD STRIKE INSPECTION PER MM 05-51-37 AND VISUALLY CHECKED AIRCRAFT FOR AREA OF IMPACT. CHECKED NR 1 AND NR 2 ENGINES, FLIGHT CONTROLS AND WINGS. NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 19950320001721995032000172NM 1995 3 20 95UAL737029 119950308A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29382UA 24657 EMERGENCY LIGHTS ARE INOP AT THE FOLLOWING LOCATIONS, EXIT LIGHT AT FORWARD LAVATORY AND DOOR ONE LEFT, SLIDE LIGHT AT DOOR ONE RIGHT AND AISLE LIGHTS AT ROWS TWO AND THREE. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950320001731995032000173NE 1995 3 20 95UAL757007 219950310A72301B6521 FAN BLADE BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ENGINE BENT A UALAO OTHER CE F.O.D. VIBRATION/BUFFET TOTAKEOFF 1 WP29528UA 25018 ON TAKEOFF FROM SMF, INGESTED ONE BIRD IN THE RIGHT ENGINE. DAMAGE DONE TO AT LEAST TWO BLADES. ODOR IN CABIN. INITIAL VIB 22. VIBRATION NOTED AT ALL POWER SETTINGS. PEEK VIBRATION EPR 1.05. BIRD INGESTION REQUIRED REPLACEMENT OF TWO FAN BLADE PAIRS. 2L72 4F4 FRTA2NM E17NE 19950320001741995032000174NE 1995 3 20 95UAL767010 219950308A7320 METERING UNIT HAMILTON STA8010002 BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT ENGINE MALFUNCTION A UALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 WP29645UA F26940 25280 724407 LEFT ENGINE CAUGHT FIRE DURING START. NO COCKPIT INDICATION OF FIRE. BOTTLES DISCHARGED FIRE EXTINGUISHED. NO PIMU FAULTS. REPLACED FUEL METERING UNIT AS A PRECAUTION. 2L72 4F4 FRTA1NM E24NE 19950320001751995032000175NM 1995 3 20 95UAL767011 119950310A3350 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN EEL DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29643UA 25093 EMERGENCY EXIT LIGHTS DAMAGED. REPLACED LIGHT STRIP AT 1E. REPLACED FORWARD GALLEY CROSS AISLE LIGHT STRIP AND FEEDER CABLE. 2L72 4F4 FRTA1NM E24NE 19950320001761995032000176WP 1995 3 20 95UALD10027 119950313A3350 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291844U 48260 EMERGENCY EXIT LIGHTS BY DOOR 2R CAME ON AFTER LANDING. REPLACED MID BATTERY PACK, U17100. 2L73 4F4 F A22WE E23EA 19950320001771995032000177WP 1995 3 20 ABXA9500147 119950308A32600080004003 PROX SW BOX DOUG DC9 DC941 302207NWP ONLG DEFECTIVE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23954AX 47612 NOSE GEAR UNSAFE LIGHT STAYED ON AFTER TAKEOFF OUT OF ELP. RECYCLED GEAR AND WENT THROUGH ABNORMAL, LIGHT STAYED ON. REPLACED PROXIMITY SWITCH BOX. PERFORMED SYSTEM CHECK. SYSTEM CHECKED NORMAL IAW DC-9 MM 32-60-01 PAGE 214 STEP 5A. 2L72 4F A6WE 19950320001781995032000178SO 1995 3 20 COM11815 119950311A5753PE610261 ROLLER EMB 120 EMB120RT SO LT FLAP DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01162CA 120150 FLAP DISAGREEMENT WARNING, FLAPS STUCK AT 15 DEGREES. REPLACED DEFECTIVE ROLLER ON LT OUTBD FLAP. 2L72 4T RTA31SO 19950320001791995032000179SO 1995 3 20 COM11816 119950312A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01162CA135 120150 FLAP DISAGREEMENT WARNING, FLAPS WOULD NOT RETRACT. REPLACED THE RT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950320001801995032000180 1995 3 20 COM31041 419950309A61228210163 GOVERNOR SAAB SF340 SF340A 7850100EU RT ENGINE DEFECTIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01347CA18530795 340A028 THE RT PROPELLER OVERSPEED SYSTEM WILL NOT TEST. REPLACED OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950320001811995032000181 1995 3 20 COM31042 419950309A61228210163C GOVERNOR SAAB SF340 SF340A 7850100EU LT ENGINE DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01359CA218 340A053 THE LT PROPELLER RPM WOULD NOT EXCEED 1100 RPM. REPLACED DEFECTIVE PROPELLER OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950320001821995032000182EU 1995 3 20 COM31043 119950312A61201103P0620 PRESS SWITCH SAAB SF340 SF340A 7850100EU LT/RT ENG DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01358CA2935 449 340A047 RECEIVED AUTO COARSEN WARNING DURING TAKEOFF. REPLACED THE P3 PRESSURE SWITCHES. 2L72 4T RTA52EU 19950320001831995032000183EA 1995 3 20 COM60435 119950310A28202261141 BOOST PUMP CNDAIRCL600 CL6002B19 EA LT WING FAILED A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01920CA3782 7022 THE LT FUEL BOOST PUMP IS INOP. REPLACED BOOST PUMP. 2L72 4F RTA21EA 19950320001841995032000184EA 1995 3 20 COM60436 119950309A2750855D1004 BRAKE SENSOR CNDAIRCL600 CL6002B19 EA LT/RT TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01924CA3030 3030 7026 THE FLAPS WILL NOT RETRACT. REPLACED THE LT AND RT BRAKE AND POSITION SENSORS. 2L72 4F RTA21EA 19950320001851995032000185 1995 3 20 COM60437 219950308A73218062385 FUEL CONTROL CNDAIRCL600 CL6002B19 EA RT ENGINE DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01920CA2504 7022 THE RT ENGINE WILL NOT START. REPLACED RT FUEL CONTROL. 2L72 4F RTA21EA 19950320001861995032000186EA 1995 3 20 COM60438 119950309A322016400103 DRAG BRACE CNDAIRCL600 CL6002B19 EA NLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01920CA2344 7022 THE NLG IS LEAKING HYDRAULIC FLUID. REPLACED THE NLG DRAG BRACE ASSY. 2L72 4F RTA21EA 19950320001871995032000187NM 1995 3 20 DL72E950899 119950227A5713 STRINGER BOEING727 727247 138408FNM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, AFT SIDE OF FORWARD VENT BOX STRINGER CRACKED AT RIB ATTACH, WS 686.5, LT WING. REPAIRED PER MM 57-13-0 PG 808. 2L73 4F A3WE 19950320001881995032000188NM 1995 3 20 DL72E950902 119950228A5320 UPLOCK SUPPORT BOEING727 727247 138408FNM WS 913 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, LEFT MLG UPLOCK SUPPORT FRAME AT FS 913 WAS FOUND WITH TIME LIMITED REPAIR. INSTALLED PERMANENT REPAIR PER MM 53-11-0 PG 815. 2L73 4F A3WE 19950320001891995032000189NM 1995 3 20 DL72E950903 119950228A5311 FRAME BOEING727 727247 138408FNM FS 804.95 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND FS 804.95 FRAME CRACKED, RT SIDE JUST BELOW WINDOW FRAME. REPAIRED PER SRM 53-10-4 FIG 22. 2L73 4F A3WE 19950320001901995032000190NM 1995 3 20 DL72E950913 119950305A5751 SKIN 657273411W BOEING727 727247 138408FNM LT AILERON PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 77 21328 DURING HMV, FOUND HOLE PUNCTURED IN LOWER SKIN, I/B END 727 O/B AILERON. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950320001911995032000191NM 1995 3 20 DL72E950914 119950305A5751 BONDNG WIRE HOLE 657273411W BOEING727 727247 138408FNM LT AILERON ELONGATED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 77 21328 DURING HMV, FOUND 727 O/B AILERON BONDING WIRE ATTACH HOLE ELONGATED. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950320001921995032000192NM 1995 3 20 DL72E950915 119950228A5751 BONDNG WIRE HOLE BOEING727 727247 138408FNM LT AILERON ELONGATED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND O/B LT WG AILERON BONDING WIRE ATTACH HOLE IS ELONGATED AT O/B TAB CUTOUT AREA. RPAIRED PER SRM 57-50-5 FIG 3. 2L73 4F A3WE 19950320001931995032000193NM 1995 3 20 DL72E950916 119950228A5751 SKIN BOEING727 727247 138408FNM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND L/W OB AILERON HOLE NEXT TO WT AND BALANCE PLACARD ON I/B UNDERSIDE. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950320001941995032000194NM 1995 3 20 DL72E950917 119950301A5330 SKIN BOEING727 727247 138408FNM FS 1052 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 1052 OUTBOARD OF STRINGER 28L. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950320001951995032000195NM 1995 3 20 DL72E950932 119950228A5320 SUPPORT BOEING727 727247 138408FNM NR 2 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 THE NR 2 FWD COWL MATING SUPPORT RING FOUND WORN AT HMV. INSTALLED SPLICES AND REPAIR ANGLE PER MM 53-11-0. 2L73 4F A3WE 19950320001961995032000196NM 1995 3 20 DL72E950935 119950227A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND STRINGER 15R CRACKED AT ITS ENDS AT WING ICE LIGHT HOUSING FS 720C. REPAIRED PER SRM 53-1-03. 2L73 4F A3WE 19950320001971995032000197NM 1995 3 20 DL72E950981 119950227A5754 RIB BOEING727 727247 138408FNM LT LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND NR 1 LEADING EDGE SLAT RIB MARKED NR 4 HAS CRACKED ATTACH ANGLE. REPAIRED BY REPLACING ANGLE. 2L73 4F A3WE 19950320001981995032000198NM 1995 3 20 DL72E950982 119950227A5754 RIB BOEING727 727247 138408FNM RT LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND NR 6 LEADING EDGE SLAT TAI 'T' DUCT HAS EXCESSIVE PLAY AT 'T' JOINT. THE ADJACENT O/B RIB TO ABOVE BAY IS CRACKED AT FWD CLOSURE CHORD. REPAIRED PER MM 57-54-0 PG 806. 2L73 4F A3WE 19950320001991995032000199NM 1995 3 20 DL72E950983 119950227A5754 RIB BOEING727 727247 138408FNM RT LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND NR 6 LEADING EDGE SLAT RIB MARKED '11' IS CRACKED BEHIND CLOSURE CHORD. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950320002001995032000200NM 1995 3 20 DL72K950908 119950118A711065196854141 NOSE COWL BOEING727 727232 1384082NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11481DA 20861 790 DURING SHOP VISIT, FOUND WORN AREAS ON AFT LANDING EDGE BETWEEN 6 AND 9 O'CLOCK POSITION ON NOSE COWL. REPAIRED AS PER 727 SRM 54-10-3. 2L73 4F A3WE 19950320002011995032000201NM 1995 3 20 DL72L950911 119950225A711065196854539 NOSE COWL BOEING727 727232 1384082NM ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 DURING SHOP INSPECTION, A CRACK WAS FOUND ON OUTER ANGLE AT FORWARD BULKHEAD 6 O'CLOCK POSITION, ON ENGINE NOSE COWL. REPAIRED DAMAGE PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950320002021995032000202NM 1995 3 20 DL72L950912 119950225A711065196854539 NOSE COWL BOEING727 727232 1384082NM ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 DURING SHOP INSPECTION, A CRACK WAS FOUND IN THE WEB AT NAC STA 77.50 AT 7 O'CLOCK POSITON OF ENGINE NOSE COWL. REPAIRED SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950320002031995032000203NM 1995 3 20 DL72S950901 119950302A5754 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 NOSE RIB CRACKED .25 INCH I/B SIDE NR 6 SLAT AT ACT ATTACH. CRACK WAS FOUND DURING C-2 LETTER CHECK TPAMM 3-2-95. STOPPED DRILLED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950320002041995032000204NM 1995 3 20 DL72S950905 119950302A5754 CHORD BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 FOUND ON C2 LTR CK, LOWER CHORD CRACKED BELOW TAI DUCT NR 7 SLAT. REPAIRED AND INSTALLED DOUBLER PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950320002051995032000205NM 1995 3 20 DL72S950918 119950208A57536521631274A SKIN BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 THE LT SKIN WAS WORN AT APPROX 7.5 INCHES AND 10.5 INCHES FROM THE I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950320002061995032000206NM 1995 3 20 DL72S950919 119950208A57536521631274A SKIN BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 A TEMP REPAIR WAS FOUND 74 INCHES FROM THE O/B END ON L/E SKIN OF NR 4 FOREFLAP. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER SRM 57 50 4 FIG 1. 2L73 4F A3WE 19950320002071995032000207NM 1995 3 20 DL72S950920 119950208A57536521631274A SKIN BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 THE L/E WAS WORN 52.5 INCHES FROM THE O/B END OF NR 4 FOREFLAP. THE AREA WAS CLEANED UP AND AN EXTERNAL DOUBLER INSTALLED PER SRM 57 50 4 FIG 1. 2L73 4F A3WE 19950320002081995032000208NM 1995 3 20 DL72S950921 119950208A57536521631274A SKIN BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 A TEMP REPAIR WAS FOUND 47 INCHES FROM THE OB END. AN AREA WAS WORN THROUGH BOTH THE REPAIR AND THE LE SKIN OF NR 4 FOREFLAP. CLEANED UP DAMAGE AND INSTALLED DOUBLER PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950320002091995032000209NM 1995 3 20 DL72S950931 119950306A5754 FAIRING BOEING727 727232 1384082NM RT LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FOUND ON F-1 LETTER CHECK, CRACK AT NR 5 SLAT INBD TRACK FAIRING. REPAIRED PER MM 57-40-0 PG 820-821. 2L73 4F A3WE 19950320002101995032000210NM 1995 3 20 DL72S950938 119950306A5320 WEB BOEING727 727232 1384082NM FS 1227 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FOUND DURING F-1 LETTER CHECK, .75 INCH CRACK IN LT TORQUE BOX WEB FROM FWD LWR LIGHTENING HOLE STA 1227. REPAIRED PER MM 53-11-0 PG 828. 2L73 4F A3WE 19950320002111995032000211NM 1995 3 20 DL72S950942 119950306A5720 STIFFENER BOEING727 727232 1384082NM RT WING CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FOUND DURING F-1 LETTER CHECK, NR 6 L/E SLAT O/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED. REPLACED STIFFENERS PER MM 57-20-21 PG 813. 2L73 4F A3WE 19950320002121995032000212NM 1995 3 20 DL72S950943 119950306A5720 SPAR STIFFENER BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FOUND DURING F-1 LETTER CHECK, NR 6 SLAT I/B TRACK I/B AND O/B SPAR STIFFENER ANGLES CRACKED 2 INCHES. REPLACED STIFFENERS PER MM 57-20-21 PG 813. 2L73 4F A3WE 19950320002131995032000213NM 1995 3 20 DL72S950946 119950225A5753652163395A SKIN BOEING727 727232 1384082NM NR 1 TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 DURING SHOP VISIT, FOUND THE NR 1 MIDFLAP LEADING EDGE SKIN DENTED I/B OF F/F TRACK CUTOUT 98 INCHES FROM I/B END. CUT OUT DAMAGE AND INSTALLED DOUBLER PER MM 57-50-0 FIG 803 PG 808. 2L73 4F A3WE 19950320002141995032000214NM 1995 3 20 DL72S950957 119950208A5753 SKIN 6521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 47 22392 DURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 19 INCHES FROM I/B END, RT WING NR 4 FOREFLAP. REPAIRED PER SRM 57-40-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002151995032000215NM 1995 3 20 DL72S950958 119950208A57536521631274 SKIN BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 DURING SHOP INSPECTION, BOTTOM SKIN FOUND DELAMINATED 19 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002161995032000216NM 1995 3 20 DL72S950959 119950208A5753 SKIN 6521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA BN47 22392 DURING SHOP INSPECTION, BOTTOM SKIN DELAMINATED 15 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002171995032000217NM 1995 3 20 DL72S950960 119950208A5753 SKIN 6521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA BN47 22392 DURING SHOP INSPECTION, FOUND TOP SKIN DENTED 89 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002181995032000218NM 1995 3 20 DL72S950961 119950208A5753 SKIN 0521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA BN47 22392 DURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 21.5 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002191995032000219NM 1995 3 20 DL72S950962 119950208A5753 SKIN 6521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA BN47 22392 DURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 46 TO 59 INCHES FROM O/B END OF NR 4 FOREFLAP. REPAIRED PER SRM 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002201995032000220NM 1995 3 20 DL72S950963 119950208A5753 SKIN 6521631274 BOEING727 727232 1384082NM RT TE FOREFLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA BN47 22392 DURING SHOP INSPECTION, TOP SKIN FOUND DELAMINATED 46 INCHES FROM I/B END OF NR 4 FOREFLAP. REPAIRED PER SMR 57-50-4, WITH REF TO SRM 51-40-6. 2L73 4F A3WE 19950320002211995032000221NM 1995 3 20 DL72S950970 119950308A5320 TORQUE BOX WEB BOEING727 727232 1384082NM RT HAND CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON LTR CK, RIGHT FWD TORQUE BOX WEB CRACKED ALONG CHORD ANGLE RIVET ROW CRACK LENGTH 1.75 INCHES TO 2.25 INCHES. CRACK AT FWD LOWER TORQUE BOX WEB EXTENDING FROM LIGHTNING HOLE. REPAIRED PER MM 53-11-0 PG 833 AND 828. 2L73 4F A3WE 19950320002221995032000222NM 1995 3 20 DL72S950971 119950308A5311 FRAME BOEING727 727232 1384082NM FS 913.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON LTR CK, FRAME CRACKED STA 913.5 IN WW. REPAIRED PER MM 53-11-0 PG 834. 2L73 4F A3WE 19950320002231995032000223NM 1995 3 20 DL72S950972 119950227A5210 SKIN BOEING727 727232 1384082NM L-1 DOOR SCRAPED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, PER OMI PERMANENT REPAIR OF L-1 DOOR AFT END LWR RT CORNER SCRAPE. INSTALLED DOUBLER PER ERA 301277-14 CODE 4-53-31-20. 2L73 4F A3WE 19950320002241995032000224NM 1995 3 20 DL72S950973 119950228A5320 ANGLE BOEING727 727232 1384082NM FS 1067 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION ON FLOOR SUPPORT ANGLE STA 1067 LBL 27 TO 45. REPLACED FLOOR ANGLE. 2L73 4F A3WE 19950320002251995032000225NM 1995 3 20 DL72S950974 119950228A5347 SEAT TRACK BOEING727 727232 1384082NM FS 344-400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION AT TOP AND UNDERSIDE OF SEAT TRACK AT CLIPNUT HOLES BETWEEN STA 380 AND STA 400 RBL 44. REPLACED SEAT TRACK SECTION FROM 344 TO 400 AT VRBL 64 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950320002261995032000226NM 1995 3 20 DL72S950975 119950228A5347 SEAT TRACK BOEING727 727232 1384082NM FS 344-440 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION AT SEAT TRACK FROM STA 344 TO STA 440BL 24R. REPLACED TRACK SECTION BS 344 TO 400 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950320002271995032000227NM 1995 3 20 DL72S950976 119950228A5347 SEAT TRACK BOEING727 727232 1384082NM BS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION AT LEFT O/B SEAT TRACK BS 1010. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950320002281995032000228NM 1995 3 20 DL72S950977 119950228A5347 SEAT TRACK BOEING727 727232 1384082NM BS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION AT GALLEY SUPPORT TRACK BS 1070 PLUS 6. REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950320002291995032000229NM 1995 3 20 DL72S950978 119950228A5313 STRINGER BOEING727 727232 1384082NM FS 540 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CK, CORROSION BOTTOM SIDE OF O/B LEG UNDER NUTPLATE STR 28R FWD OF STA 540. REPAIRED PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19950320002301995032000230NM 1995 3 20 DL72W950907 119950219A5753652163261 SPAR BOEING727 727247 138408FNM TE MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING SHOP INSPECTION, FOUND NR 2 MIDFLAP AFT LOWER SPAR WITH 2 CRACKS AT 53 INCHES AND 56 INCHES FROM INBD END OF FLAP. REPAIRED PER MM 57-52-20 PG 807. 2L73 4F A3WE 19950320002311995032000231NM 1995 3 20 DL72W950947 119950104A57536521630187A SKIN BOEING727 727247 138408FNM LT TE FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 DURING SHOP VISIT, FOUND THE NR 2 FOREFLAP HAS APPROX .5 INCH WORN AREA APPROX 2 INCHES FROM O/B END. THE DAMAGE IS LOCATED ON LEADING EDGE OF FLAP. INSTALLED EXTERNAL DOUBLER PER 727 SRM 57-50-4. 2L73 4F A3WE 19950320002321995032000232NM 1995 3 20 DL72W951038 119950307A3350900835A EEL BATT PACK BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112814W 20870 DURING PREFLIGHT, LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19950320002331995032000233NM 1995 3 20 DL72W951039 119950306A282065235281 TUBE BOEING727 727247 138408FNM RT WING CRACKED A ADALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SO112819W 21057 DURING CRUISE, NR 3 FUEL QTY WAS DROPPING AT 2,500 LBS PER HOUR WITHOUT BURNING FROM THAT TANK. VISUALLY CHECKED NR 3 AT CRUISE ALTITUDE AND COULD SEE A STREAM OF FUEL VAPORS OFF THE RIGHT WING. LANDED DFW. FOUND CRACKED FUEL TUBE. REPLACED TUBE AND RETURNED TO SERVICE. 2L73 4F A3WE 19950320002341995032000234NM 1995 3 20 DL72W951040 119950307A3350S106 EEL BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112814W 20870 DURING PREFLIGHT, AFT STAIRWELL EMERGENCY LIGHTS INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950320002351995032000235NM 1995 3 20 DL73S951035 119950309A25305374AD COFFEE MAKER BOEING737 737232 1384475NM FWD GALLEY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11313DL 23085 DURING CLIMB-OUT, HAD SMOKE AND FUMES COMING FROM FORWARD GALLEY. ALSO, WATER LEAKING AT COFFEE MAKER. DEACTIVATED POWER AND RETURNED ICT. FOUND COFFEE MAKER DRAIN VALVE STUCK OPEN. REPLACED MAKER OPERATION NORMAL. 2L72 4F RTA16WE 19950320002361995032000236NM 1995 3 20 DL757950904 119950302A7110 NOSE COWL BOEING757 757232 1384965NM NR 2 ENG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11677DL 25982 DURING LETTER CHECK INSP, FOUND L/E OF NOSE COWL AT 3.0 POS ERODING. REPAIRED PER SRM 54-11-01 NR 2 NOSE COWL. 2L72 4F RTA2NM 19950320002371995032000237NM 1995 3 20 DL757950929 119950203A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11606DL 22813 INITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 LARGE AREAS OF DELAMINATION AT THE 7 O'CLOCK POSITION. ALL REPAIRS WERE ACCOMPLISHED AS PER SRM 53-10-72. INTERIOR SKIN AND ALL HONEYCOMB CORE WERE REPLACED DURING REPAIR PROCEDURES. UPON REPAIR BEING COMPLETED RADOME EROISION AND PAINT WERE REAPPLIED PER PS 900-9-1-11 NR 05. 2L72 4F RTA2NM 19950320002381995032000238NM 1995 3 20 DL757950954 119950302A5754114N4002132 WEDGE BOEING757 757232 1384965NM RT LE SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 DURING HMV, NR CARD 125 WAS WRITTEN FOR HAIL DAMAGE ON THE T/E WEDGE OF THE NR 10 L/E SLAT. THE WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950320002391995032000239NM 1995 3 20 DL757950967 119950307A5754114N4002131 WEDGE BOEING757 757232 1384965NM NR 1 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 AT HMV, LEFT WING NR 1 SLAT WAS FOUND WITH DELAMINATION ON THE TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950320002401995032000240NM 1995 3 20 DL757950968 119950302A5754114N4003147 WEDGE BOEING757 757232 1384965NM LT LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 DURING INSPECTION, HAIL DAMAGE WAS FOUND ON NR 2 L/E SLAT WEDGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950320002411995032000241NM 1995 3 20 DL757950969 119950302A5754114N4003148 WEDGE BOEING757 757232 1384965NM RT LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 THE NUMBER NINE LEADING EDGE SLAT WAS FOUND TO HAVE HAIL DAMAGE DURING INSECTION AT HMV. NRC 124. REPAIRED BY REPLACING TRAILING EDGE WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950320002421995032000242NE 1995 3 20 DL757951037 219950308A75303800035114 ACTUATOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FAULTY A DALAA UNSCHED LANDING JX WARNING INDICATION ENGINE FLAMEOUT CRCRUISE 1 SO11632DL 23613 716348 DURING CRUISE, HAD SVA FAILSAFE MSG, NR 2 ENGINE FLAMED-OUT. LANDED RDU. RAN ENGINE PER PFHB TEST 14 SVA, TEST NORMAL. FERRIED AC TO ATL. REPLACED STATOR VANE ACTUATOR, RETURNED TO SERVICE. 2L72 4F4 FRTA2NM E17NE 19950320002431995032000243NE 1995 3 20 DL757951041 219950310A7200PW2037 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11650DL19279 24390 716509 DURING CLIMB-OUT, HAD OIL TEMP ENTER YELLOW BAND, THEN HAD SMELL OF OIL IN CABIN AND FLT DECK, ALONG WITH LOSS OF OIL QTY. RETURNED TPA. REPLACED NR 1 ENGINE FOR RETURN TO SERVICE. ROUTED ENGINE TO SHOP. 2L72 4F4 FRTA2NM E17NE 19950320002441995032000244WP 1995 3 20 DLL13951036 119950308A29133508807 PUMP LKHEED1011 10113851 5265010WP C HYD SYS CRACKED A DALAO OTHER K FLUID LOSS APAPPROACH 1 SO11783DL 193A1009 ON APPROACH, 'C' SYSTEM HYDRAULIC QTY DROPPED BELOW HALF FULL. FOUND 'C' SYSTEM ENGINE DRIVEN PUMP WITH A CRACK AT PUMP OUTLET. REPLACED PUMP, OPERATION NORMAL. 2L73 4F A23WE 19950320002451995032000245WP 1995 3 20 DLL16950923 119950213A5330 TEAR STRAP LKHEED1011 10113853 5265020WP FS 1605-1625 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND TEAR STRAP DISBONDED C2 BIN BETWEEN 1605 TO 1625, STRINGER 29 AND 30. LIFTED TEAR STRAP AND REMOVED CORROSION, TREATED AND PAINTED AREA. FABRICATED AND INSTALLED REPAIR SPLICES PER SRM 53-31-00. 2L73 4F A23WE 19950320002461995032000246 1995 3 20 DLL16950924 419950215A2360 STATIC WICK LKHEED1011 10113853 5265020WP BASES 34/43 FAILED CHECK A DALAK NONE L NO TEST ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND STATIC WICK BASES 34 AND 43 FAILED MEG CHECK. REPLACED STATIC WICK BASES 34 AND 43. REQ PANELS INSTALLED ON AC STATIC ARRESTER BASES. 2L73 4F A23WE 19950320002471995032000247WP 1995 3 20 DLL16950926 119950219A5743 ACT FITTING LKHEED1011 10113853 5265020WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND HOLES CORRODED HOLES 1, 2, 4, 6, IN LMLG ACTUATOR FITTING CORRODED. REF TASK C-32-730-01. REAMED HOLES 1, 2, 4, 5 AND 6 TP .688. REMOVED DAMAGE AND TO FACILATATE MAINT ON HOLE NR 5, REAMED NR 3 .719 TO REMOVE DAMAGE. CORROSION REMOVED, ALL REMAINING WORK DONE ON JPC 031255. 2L73 4F A23WE 19950320002481995032000248WP 1995 3 20 DLL16950927 119950219A5743 ACT FITTING LKHEED1011 10113853 5265020WP LT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND HOLES DAMAGED IN LMLG ACTUATOR FITTING. DRILLED HOLES 17 THROUGH 20 TO .628 TO REMOVE DAMAGE. CORROSION REMOVED. ALL REMAINING WORK DONE ON JPC 031255. 2L73 4F A23WE 19950320002491995032000249WP 1995 3 20 DLL16950928 119950301A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 930 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV,FOUND TEAR STRAP DISBONDED, STA 930 BETWEEN STRINGER 31 AND 32. PEELED TEAR STRAP BACK, NO CORROSION FOUND. INSTALLED REPAIR PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950320002501995032000250WP 1995 3 20 DLL16950948 119950301A5330 STRAP LKHEED1011 10113853 5265020WP FS 930 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HVM, FOUND TEAR STRAP DISBONDED AT FS 930 BETWEEN STR 31 AND 32. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950320002511995032000251WP 1995 3 20 DLL16950949 119950213A5330 STRAP LKHEED1011 10113853 5265020WP BS 1605-1625 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 AT HMV, FOUND TEAR STRAP DISBONDED AT FS 1605 AND 1625 BETWEEN STRINGER 29 AND 30. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950320002521995032000252WP 1995 3 20 DLL16950950 119950223A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 1823-1842 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 FLOORBEAM STA 1823 TO 1842 LBL 71 LBL 44 CORRODED AT FLOOR PANEL ATTACH HOLES, TWO PLACES. DAMAGE FOUND AT HMV. REPAIRED PER SRM 53-21-00 PAGES 866 TO 868. 2L73 4F A23WE 19950320002531995032000253NM 1995 3 20 DLM88950900 119950302A5230 BRACKETS DOUG MD88 MD88 3023688NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11950DL 49881 OUTER DOOR WILL NOT LATCH IN UPLOCK POS, BOTH BRACKETS DAMAGED AND CRACKED. CRACK ALSO, IN AFT EDGE OF DOOR BELOW AFT HANGER. FOUND DURING F-1 LETTER CK TPAMM 3/2/95. REPAIRED FIRST ITEM BY SRM 52-05 FIG 27, REPAIRED 2ND ITEM BY SRM 52-05 FIG 26A. 2L72 4F RTA6WE 19950320002551995032000255NM 1995 3 20 DLM88950955 119950307A5347 SEAT TRACK DOUG MD88 MD88 3023688NM FS 220 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 AT HMV, SEAT TRACK CORRODED UNDER FWD LAV LT INBD SECTION AT APPROX FS 220. MFG AND INSTALLED REPAIR PER SRM 53-05 PAGE 10G. 2L72 4F RTA6WE 19950320002561995032000256NM 1995 3 20 DLM88950956 119950306A5754 FITTING DOUG MD88 MD88 3023688NM NR 1 LE SLAT GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 AT HMV, LT WING NR 1 L/E SLAT INBD TRACK FITTING (ON SLAT) IS GOUGED IN THE RADIUS. BLENDED GOUGE WITHIN ACCEPTABLE LIMITS PER SRM 57-02 PAGE 7, TREATED AND PAINTED. 2L72 4F RTA6WE 19950320002571995032000257NM 1995 3 20 DLM88950964 119950308A5320 ANGLE DOUG MD88 MD88 3023688NM AFT KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11949DL 49880 FOUND ON D-1 LETTER CHECK, CROSSOVER ANGLE CRACKED BOTH LT AND RT CORNERS AFT OF KEEL BEAM. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950320002581995032000258NM 1995 3 20 DLM88950965 119950306A7110 COWL DOUG MD88 MD88 3023688NM NR 2 ENG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 AT HMV, NR 2 ENG LOWER AFT COWL IS DAMAGED AT FWD END. REPAIRED PER SRM 54-06. 2L72 4F RTA6WE 19950320002591995032000259WP 1995 3 20 MWEA95144 119950310A335060030431 EEL BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31301ME 47190 DURING ROUTINE INSPECTION, FOUND THAT THE EMERGENCY LIGHTS IN TAIL COMPARTMENT WOULD NOT EXTINGUISH. REPLACED EMERGENCY LIGHT BATTERY PACK. 2L72 4F A6WE 19950320002601995032000260WP 1995 3 20 MWEA95145 119950311A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31203ME 47673 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER CAME OFF. REINSTALLED GALLEY DOOR EVACUATION SLIDE COVER AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950320002611995032000261WP 1995 3 20 MWEA95146 119950311A5400 ANGLE DOUG DC9 DC914 3022034WP RT PYLON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING ROUTINE INSP, THE ANGLE WHICH SUPPORTS SERVICE PANEL 8105 ON RT PYLON LOWER SURFACE WAS CRACKED APPROX 1.5 INCHES. REPAIRED ANGLE IAW 54-01 FIG 2. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950320002621995032000262WP 1995 3 20 MWEA95147 119950311A521059141215 DOOR PAN DOUG DC9 DC914 3022034WP FWD PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING ROUTINE INSPECTION, THE FWD PASSENGER ENTRANCE DOOR WAS FOUND TO BE CRACKED ON FWD UPPER CORNER AT 2.5 INCHES IN LENGTH ON DOOR PAN. REPAIRED FWD ENTRY DOOR IAW SRM 52-05 FIG 18A. 2L72 4F A6WE 19950320002631995032000263WP 1995 3 20 MWEA95148 119950311A54005913262 ANGLE DOUG DC9 DC914 3022034WP LT PYLON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING ROUTINE INSPECTION, THE LEFT PYLON UPPER SURFACE TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED APPROX .25 INCH IN LENGTH. REPAIRED ATTACH ANGLE IAW SRM 54-05 FIG 10. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950320002641995032000264NM 1995 3 20 SWAA950206 119950307A5340 STRINGER CLIP BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND STRINGER CLIPS CRACKED AT BS 400, S27L, AND 28L, AT BS 747, S10R, AT BS 500D, S3R AND 19R/L, AT BS 406, S3R, AT BS 380, S7L, AT BS 500A, S1, AT BS 727B, S14L, AT BS 663, S10R AND L, AND AT BS 727A, S16R. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002651995032000265NM 1995 3 20 SWAA950207 119950307A5315 FLOORBEAM BOEING737 7373A4 1384585NM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, TOP AND BOTTOM OF UPPER T-CHORD FROM LBL 10 TO RBL 49. REPAIRED PER TRAMCO EWO 95-0172. 2L72 4F RTA16WE 19950320002661995032000266NM 1995 3 20 SWAA950208 119950307A5315BAC1490 FLOORBEAM BOEING737 7373A4 1384585NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, AT BL 0 AND LBL 12, WL 208, AND AT BS 360, LBL 10 AND RBL 1, WL 208, AND AT BS 344, LBL 10 AND RBL 10. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002671995032000267NM 1995 3 20 SWAA950209 119950307A5330 SKIN BOEING737 7373A4 1384585NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT BS 312, BETWEEN 18 AND 19R, AT BS 320, BETWEEN S20 AND 21R, FROM BS 363 TO 364, S5L, AND AT BS 1128, BETWEEN S14 AND 15R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002681995032000268NM 1995 3 20 SWAA950210 119950307A5330 SKIN BOEING737 7373A4 1384585NM BS 328 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH AT FORWARD GALLEY DOORWAY LOWER AFT CORNER, BS 328, RBL 65, WL 211. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002691995032000269NM 1995 3 20 SWAA950211 119950307A5730 SKIN BOEING737 7373A4 1384585NM LT WING LE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND LEFT WING L/E DENTED 15 INCHES OUTBOARD OF NUMBER 1 ENGINE, MEASURING 1.5 INCHES BY .5 INCH BY .012 INCH DEEP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002701995032000270NM 1995 3 20 SWAA950212 119950307A5240 SKIN BOEING737 7373A4 1384585NM AFT SERV DOOR BENT A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND AFT SERVICE DOOR EXTERNAL SKIN BENT AT UPPER OUTER EDGE LOWER HINGE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002711995032000271NM 1995 3 20 SWAA950213 119950307A5311 FRAME BOEING737 7373A4 1384585NM BS 492 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME FLANGE CRACKED AT BS 492, S24R. REPAIRED PER TRAMCO EWO 95-0194. 2L72 4F RTA16WE 19950320002721995032000272NM 1995 3 20 SWAA950214 119950307A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 986.5/344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, RBL 45 TO LBL 45, AT BS 344, LBL 25 TO BL 0, WL 208. REPAIRED PER SWA RA 1-353-542 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002731995032000273NM 1995 3 20 SWAA950215 119950307A5320 ANGLE BOEING737 7373T0 1384582NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND L-ANGLE CRACKED AT BS 294, RBL 30, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002741995032000274NM 1995 3 20 SWAA950216 119950307A5311 FRAME BOEING737 7373T0 1384582NM BS 947 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME DENTED AND GOUGED AT UPPER FASTENER HOLE OF STRINGER CLIP BS 947, S26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002751995032000275NM 1995 3 20 SWAA950217 119950307A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTS AT BS 314, S18R, AT BS 916, S21 TO 22L, AND AT BS 424, BETWEEN S21 AND 22R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002761995032000276NM 1995 3 20 SWAA950218 119950307A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 880 TO 890, BETWEEN S25 AND 26L, AT BS 990, BETWEEN S14 AND 15L, AT BS 670, BETWEEN S2 AND 3R, AND AT BS 390, BETWEEN S16 AND 17L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002771995032000277NM 1995 3 20 SWAA950219 119950307A5330 SKIN BOEING737 7373T0 1384582NM BS 960 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGES IN FUSELAGE SKIN AT BS 960, BETWEEN S20 TO 21L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002781995032000278NM 1995 3 20 SWAA950220 119950307A5330 SKIN BOEING737 7373T0 1384582NM BS 807 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07697SW 23838 DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO BAY SHEAR TIE CRUSHED AND SKIN DENTED AT BS 807, RBL 6 TO LBL 6, WL 151.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950320002791995032000279NM 1995 3 20 SWAA950221 119950308A33506013121 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0791SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND FORWARD SECTION OF CABIN EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING MM. 2L72 4F A16WE 19950320002801995032000280NM 1995 3 20 UPS202630 119950313A5320 MOP SILL BOEING727 72727C 138400JNM BS 294-304 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON MOP SILL AT STA 294 TO 304, LBL 45, WL 208. REPLACED PER SRM 51-10-01, 51-10-2, 51-30-2. 2L73 4F A3WE 19950320002811995032000281NM 1995 3 20 UPS202631 119950313A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 1183, RBL 62, WL 256. INSTALLED REPAIR PER SRM 53-10-2, 51-20-1, 51-30-2. 2L73 4F A3WE 19950320002821995032000282NM 1995 3 20 UPS202632 119950313A5311 FRAME BOEING727 72727C 138400JNM BS 1203 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FRAME WEB BS 1203, LBL 60, WL 220. INSTALLED REPAIR PER SRM 51-10-1, 51-40-2, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950320002831995032000283NM 1995 3 20 UPS202633 119950313A5754 SKIN BOEING727 72727C 138400JNM LT LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND DATA PLATE ON NR 1 K-FLAP. INSTALLED REPAIR PER SRM 57-10-1, 57-50-3. 2L73 4F A3WE 19950320002841995032000284NM 1995 3 20 UPS202634 119950313A5311 FRAME BOEING727 72727C 138400JNM BS 720 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON FRAME AT BS 720, LBL 10, WL 153. INSTALLED REPAIR PER SRM 51-30-2, 53-10-1, 51-40-2, MM 51-20-151. 2L73 4F A3WE 19950320002851995032000285NM 1995 3 20 UPS202635 119950313A5312 BULKHEAD ANGLE BOEING727 72727C 138400JNM BS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON BULKHEAD ANGLE AT BS 480, RBL 3, AND LBL 10, WL 155. INSTALLED REPAIR PER SRM 53-10-1. 2L73 4F A3WE 19950320002861995032000286NM 1995 3 20 UPS202636 119950313A5210 FRAME BOEING727 72727C 138400JNM FWD ENTRY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FWD ENTRY DOOR AFT FRAME AT LWR AFT STOP PIN FITTING. REPLACED PER SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950320002871995032000287NM 1995 3 20 UPS202637 119950313A5330 DOUBLER BOEING727 72727C 138400JNM BS 949 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON DOUBLER JUST FWD OF 950 FRAME, STA 949, RBL 70, WL 201. INSTALLED REPAIR PER SRM 51-20-1. 2L73 4F A3WE 19950320002881995032000288NM 1995 3 20 UPS202638 119950313A5320 PRESSURE BOX BOEING727 72727C 138400JNM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD RT PRESSURE BOX STA 740 TO 760, RBL 63 TO 70, WL 207. INSTALLED REPAIR PER UPS EO B727-5710-1271F. 2L73 4F A3WE 19950320002891995032000289NM 1995 3 20 UPS202639 119950313A5320 PRESSURE BOX BOEING727 72727C 138400JNM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD LT PRESSURE BOX STA 740 TO 760, LBL 63 TO 70, WL 208. INSTALLED REPAIR PER UPS EO B727-5710-1271F. 2L73 4F A3WE 19950320002901995032000290NM 1995 3 20 UPS202640 119950313A5320 CREASE BEAM BOEING727 72727C 138400JNM BS 302-366 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM STA 302 TO 366 RBL 60, WL 208. INSTALLED REPAIR PER SRM 51-40-3. 2L73 4F A3WE 19950320002911995032000291NM 1995 3 20 UPS202641 119950313A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 851 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AROUND NUTPLATES BS 851, RBL 25 TO 0, WL 208. INSTALLED REPAIR PER SRM 51-10-1. 2L73 4F A3WE 19950320002921995032000292NM 1995 3 20 UPS202642 119950313A5753 FLAP BOEING727 72727C 138400JNM RT TE FOREFLAP DETERIORATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND DETERIORATING PREVIOUS REPAIR ON RT WING I/B FOREFLAP, NEAR I/B TRACK FAIRING. INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950320002931995032000293NM 1995 3 20 UPS202643 119950313A5754 SKIN BOEING727 72727C 138400JNM RT LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT SKIN NEAR GUIDE HOOK UPPER FASTENER. INSTALLED REPAIR PER SRM 57-50-3. 2L73 4F A3WE 19950320002941995032000294NM 1995 3 20 UPS202644 119950313A5754 RIB BOEING727 72727C 138400JNM RT LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON NR 5 SLAT RIB I/B SIDE OF ACTUATOR. INSTALLED REPAIR PER SRM 57-50-3. 2L73 4F A3WE 19950320002951995032000295NM 1995 3 20 UPS202645 119950313A5753 SKIN BOEING727 72727C 138400JNM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND DELAMINATION RT WING I/B FOREFLAP, AFT I/B CORNER. INSTALLED REPAIR PER SRM 51-40-06. 2L73 4F A3WE 19950320002961995032000296NM 1995 3 20 UPS202646 119950313A5753 SKIN BOEING727 72727C 138400JNM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND DELAMINATION RT WING I/B MID FLAP, AFT I/B CORNER OF TRAILING EDGE. INSTALLED REPAIR PER SRM 51-40-06. 2L73 4F A3WE 19950320002971995032000297NM 1995 3 20 UPS202647 119950313A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 1090 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE BS 1090, STR 30 TO 29R, WL 142. INSTALLED REPAIR PER SRM 53-10-4, 51-10-2, 51-20-4, 51-30-2, MM 51-20-151. 2L73 4F A3WE 19950320002981995032000298NM 1995 3 20 UPS202648 119950313A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE STA 1110, STR 30 TO 29L, WL 142. INSTALLED REPAIR PER SRM 53-20-4, 51-10-6, 51-30-2, 53-10-1. 2L73 4F A3WE 19950320002991995032000299NM 1995 3 20 UPS202649 119950313A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON INTERCOSTAL AT BS 1183, RBL 62, WL 224. REPLACED PER SRM 51-30-2. 2L73 4F A3WE 19950320003001995032000300NM 1995 3 20 UPS202650 119950313A5311 FRAME BOEING727 72727C 138400JNM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FRAME WEB AT BS 760, LBL 68, WL204. INSTALLED REPAIR PER SRM 53-10-1, 51-20-01, 51-30-2. 2L73 4F A3WE 19950320003011995032000301NM 1995 3 20 UPS202651 119950313A5330 SKIN BOEING727 72727C 138400JNM BS 294-328 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKS AND DELAMINATION ON LT DOG HOUSE STA 294 TO 328, LBL 25, WL 150. INSTALLED REPAIR PER SRM 51-30-2, 51-20-1, MM 51-20-151. 2L73 4F A3WE 19950320003021995032000302WP 1995 3 20 UPS802652 119950311A2611 SMOKE DET DOUG DC8 DC871F 302199DWP NR 2 INOPERATIVE A IPXAO OTHER L NO TEST ININSP/MAINT 1 SO01797UP 45897 MAINTENANCE REPORTED DURING SMOKE DETECTOR TEST, WARNING LIGHT REMAINED ON. RECYCLED SELECTOR SWITCH AND FOUND NR 2 SMOKE DETECTOR WOULD NOT TEST. DEFERRED NR 2 SMOKE DETECTOR PER MEL 26-6-1. CONTROL M90343 ASSIGNED. 2L74 4F RT4A25 19950320003031995032000303SO 1995 3 20 95ZZZX1176 119950201A2842200250000101 FUEL QTY SENSOR SIMMONDS EMB 120 EMB120RT SO RT WING MALFUNCTIONED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07332JS 120038 FLT 4158 - SHORTLY AFTER TAKEOFF, FLIGHT CREW REPORTED THE RT FUEL QUANTITY INDICATOR DROPPED FROM 1500 TO 500 POUNDS, CREW ELECTED TO RETURN TO THE FIELD. MAINTENANCE INSPECTED AIRCRAFT, DEFERRED RT FUEL QUANTITY INDICATION SYSTEM. AIRCRAFT RETURNED TO SERVICE. OVERNIGHT MAINTENANCE REPLACED RT FUEL TANK, UNITS CLEARED DEFERRED ITEM. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320003041995032000304EU 1995 3 20 95ZZZX1177 119950123A34114000007 PITOT BAG JETSTMJETSTM3101 1500215EU LEFT OBSTRUCTED LINE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07842JS 753 FLT 4134, DURING TAKEOFF ROLL, CREW REPORTED LT AIRSPEED INDICATOR FAILED TO RESPOND NORMALLY. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. INSPECTED LEFT PITOT SYSTEM, TURNED ON PITOT HEAT AND DRAINED SYSTEM. PERFORMED OPERATIONAL CHECK IAW BAE MM 34-11-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003051995032000305 1995 3 20 95ZZZX1178 419950122A3425066031160003 EHSI BENDIX ED102E EMB 120 EMB120RT SO RT INSTR PANEL DEFECTIVE A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL07332JS 1220 120038 WHEN ACTIVATING MASTER AVIONICS SWITCH, MAINTENANCE PERSONNEL REPORTED SPARKS AND SMOKE FROM RT SIDE OF COCKPIT INSTRUMENT PANEL. REPLACED RT EHSI, OPERATIONAL CHECK GOOD. SERVICE INVESTIGATION REVEALED AN INTERNAL PROBLEM WITH HIGH VOLTAGE POWER SUPPLY, BENDIX/KING IS CURRENTLY EVALUATING THE PROBLEM. 2L72 4T RTA31SO 19950320003061995032000306NE 1995 3 20 95ZZZX1179 219950125A7261 OIL SYSTEM EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE REQUIRED SERVICEA VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07331JS 120035 FLT 4023 - SHORTLY AFTER TAKEOFF, CAPTAIN NOTICED RT ENGINE OIL PRESSURE FLUCTUATION ASSOCIATED WITH AURAL WARNING AND MASTER WARNING PANEL INDICATION. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED RIGHT ENGINE OIL LEVEL, CONDUCTED ENGINE GROUND RUN. ALL ITEMS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA31SO E20NE 19950320003071995032000307SO 1995 3 20 95ZZZX1180 119950213A29110884230011 ACCUMULATOR EMB 120 EMB120RT SO HYD SYST DEFECTIVE A VNAAO OTHER O OTHER CLCLIMB 1 GL07335JS 120059 FLT 4262 - CREW NOTED ON TAKEOFF, LANDING GEAR TOOK 45 SECONDS TO FULLY RETRACT. AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENANCE REPLACED LANDING GEAR SYSTEM ACCUMULATOR - 32-50-00. CONDUCTED GEAR SWING, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320003081995032000308EU 1995 3 20 95ZZZX1181 119950207A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG DEFECTIVE A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL07855JS 739 FLT 4002 - WHEN SELECTING 'GEAR DOWN' IN PREPARATION FOR LANDING, CREW WAS UNABLE TO OBTAIN A SAFE NOSE LANDING GEAR INDICATION. AN EMERGENCY WAS DECLARED. EMERGENCY EQUIPMENT ON STANDBY, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED NOSE LANDING GEAR DOWNLOCK MICROSWITCH IAW MM 32-50-00. CONDUCTED LANDING GEAR SWING, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003091995032000309EU 1995 3 20 95ZZZX1182 119950204A3260622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG DEFECTIVE A VNAAO OTHER N FALSE WARNING APAPPROACH 1 GL07845JS 769 FLT 4019 - DURING APPROACH AND PREPARATION FOR LANDING WHEN SELECTING GEAR DOWN, CREW NOTICED AN UNSAFE GEAR INDICATION ALL 3 LANDING GEAR LEGS. F/O VISUALLY CONFIRMED MAIN LANDING GEARS WERE DOWN AND LOCKED. NO EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND A DEFECTIVE DOWNLOCK MICROSWITCH RT MLG - REMOVED AND REPLACED DEFECTIVE COMPONENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003101995032000310EU 1995 3 20 95ZZZX1183 119950205A3260622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU NLG MALFUNCTIONED A VNAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL07842JS 753 FLT 4110 - WHEN SELECTING GEAR DOWN ON APPROACH TO A00, CREW UNABLE TO GET GEAR SAFE LIGHT NLG. CYCLED GEAR SEVERAL TIMES, STILL UNABLE TO GET SAFE LIGHT NLG. CREW ELECTED TO RETURN TO PIT, UNABLE TO VERIFY NLG DOWN, CREW DECLARED AN EMERGENCY. AFTER DECLARING AN EMERGENCY, NLG GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT DIFFICULTY. EMERGENCY EVACUATION NORMAL. MAINTENANCE INSPECTED AND CLEANED NLG DOWNLOCK MICROSWITCH, CONDUCTED LANDING GEAR SERVICING. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003111995032000311EU 1995 3 20 95ZZZX1184 119950206A3260622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU NLG DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL07842JS 753 JST - FLT 4088 - ON APPROACH, SELECTED GEAR DOWN, NO SAFE GEAR INDICATION - NLG - CYCLED GEAR HANDLE 4 TIMES, STILL NO INDICATION. RETURNED TO PIT, DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NLG DOWNLOCK MICROSWITCH. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003121995032000312SO 1995 3 20 95ZZZX1185 119950123A27503472001001 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07331JS 120035 FLT 4172 - SHORTLY AFTER TAKEOFF, CREW SELECTED FLAPS UP. FLAP WARNING (AURAL) WAS HEARD BY THE CREW. AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320003131995032000313 1995 3 20 95ZZZX1186 319950123A6140 BETA CAPTION BAG JETSTMJETSTM3101 1500215EU LT ENGINE ILLUMINATED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07843JS 757 FLT 4098 - DURING TAKEOFF ROLL, CREW REPORTED THE LEFT 'BETA' CAPTION ILLUMINATED, TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. INSPECTED LEFT ENGINE BETA INDICATION SYSTEM AND ENGINE, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003141995032000314SO 1995 3 20 95ZZZX1187 119950123A27503472001001 FLAP CONTL EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07340JS 120172 FLT 4005 - SHORTLY AFTER TAKEOFF, CREW REPORTED A FLAP DISAGREEMENT INDICATION, AIRCRAFT RETURNED TO LAND WITHOUT FURTHER INCIDENT. TROUBLESHOT AND CORRECTED PROBLEM BY REPLACING THE FLAP CONTROL UNIT IAW EMB MM 27-50-06. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320003151995032000315EU 1995 3 20 95ZZZX1188 119950125A341113730296K402 PITOT TUBE BAG JETSTMJETSTM3101 1500215EU LEFT ICED UP A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07852JS 724 FLT 4197 - DURING TAKEOFF, THE CAPTAIN NOTICED HIS AIRSPEED INDICATOR WAS NOT FUNCTIONING PROPERLY. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE APPLIED PITOT HEAT TO SYSTEM, OPERATIONAL CHECK OF SYSTEM AFTER BEING HEATED WAS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003161995032000316EU 1995 3 20 95ZZZX1189 119950213A3411 PITOT TUBE BAG JETSTMJETSTM3101 1500215EU LEFT ICED UP A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07845JS 769 FLT 4094 - DURING TAKEOFF ROLL, CAPTAIN'S AIRSPEED INDICATOR STOPPED AT 68 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED ICE ACCUMULATION IN CAPTAIN'S PITOT TUBE, THEY THEN ACTIVATED PITOT HEATER SYSTEM TO THAW ICE FROM SYSTEM. CONDUCTED HIGH SPEED TAXI, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950320003171995032000317SO 1995 3 20 95ZZZX1190 119950213A793138760016 OIL PRESS TRANS ITT EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07335JS 120059 FLT 4262 - AFTER TAKEOFF, CREW RECEIVED LOW OIL PRESSURE WARNING, BOTH AURAL AND VISUAL NR 2 ENGINE. AIRCRAFT RETURNED TO GATE, OUTSIDE MAINTENANCE INSPECTED NR 2 ENGINE, SERVICED OIL LEVEL. AIRCRAFT WAS FERRIED TO CAK WHERE MAINTENANCE REPLACED OIL PRESSURE TRANSMITTER, GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320003181995032000318NM 1995 3 20 95ZZZX1191 119950118A36103620076 PRECOOLER VALVE BOEING757 7572Q8 1384972NM PNEUMATIC DIST FAILED A AMTACD ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11755AT 633 24965 MDW - FLT 575 - AT BEGINNING OF TAKEOFF ROLL WHEN POWER APPLIED, COCKPIT FILLED WITH HEAVY SMOKE. TAKEOFF ABORTED, RETURNED TO GATE FOR MX ACTION. REMOVED AND REPLACED FAN MOD. VALVE IAW MM 36-11-16, PERFORMED OPERATIONAL CHECK TO THE AIR SUPPLY DISTRIBUTION SYSTEM IAW 36-11-00. RAN BOTH ENGINES TO TAKEOFF POWER. OPS CHECK GOOD, NO SMOKE NOTED. 2L72 4F RTA2NM 19950320003191995032000319NE 1995 3 20 95ZZZX1192 219950214A7230 BEARING BOEING757 7572Q8 1384972NM PWA 2037 PW2040 NE NR 2 ENG NR 1 OIL LEAK A AMTAA UNSCHED LANDING BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CLCLIMB 1 GL11755AT 24965 716313 PHOG - FLT 578 - DURING CLIMB, COCKPIT FILLED WITH SMOKE. PERFORMED AIR TURN-BACK. PERFORMED INSPECTION OF PACK SYSTEMS, INSPECTED ENGINES FOR LEAKS, NO EICAS MESSAGES. AIRPLANE WAS INSPECTED AND FOUND TO BE SAFE FOR A NON-REVENUE FLIGHT BACK TO MAINLAND U. S. FOR MAINTENANCE. NOTE: AT IND, NR 2 ENGINE WAS REMOVED. REASONS: OIL LEAKAGE COMING FROM NOSE CONE BEARING FORWARD OF FAN. 2L72 4F4 FRTA2NM E17NE 19950320003201995032000320 1995 3 20 95ZZZX1193 419950306A2565D31393110 ESCAPE SLIDE BOEING757 757212 NM RT OVERWING FAIL TEST A AAMTAK NONE L NO TEST ININSP/MAINT 1 GL11752AT 0201RP 23128 IND - DURING ROUTINE ESCAPE SLIDE OPERATIONAL CHECK, THE RT OVERWING SLIDE REMAINED ON TOP OF WING, ALL SECTIONS INFLATED, DOOR OPENED PROPERLY. SECTION OF VELCRO STRAPPING DID NOT LET LOOSE PREVENTING 3 BOTTOM SAETY WIRES (FUSE) FROM BREAKING. LARGE VELCRO STRAP, 6 FEET, DID NOT RELEASE. EVALUATION FOUND WHAT APPEARS TO BE A TEMPORARY TIE AROUND SLIDE RESTRICTING SLIDE TO BRAKE THE FRANGIBLE LINKS. ADDITIONALLY, LACING COVERS (2 EACH) WERE TORN ALONG LOWER SEAM. A FLEET CAMPAIGN WAS SCHEDULED BY VENDOR. REPLACED ESCAPE SLIDE. 2L72 4F RTA2NM 19950320003211995032000321WP 1995 3 20 95ZZZX1194 119950213A3231 RETRACT MECH LKHEED1011 10113851 5265010WP RT MLG DOOR FAILED A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11195AT 193P1041 MKE - FLT 55 - DURING TAKEOFF AND CLIMB, RT GEAR OR DOOR INTRANSIT FAILED TO COME UP. AIR TURN-BACK. SWAPPED RT AND LT PRESS. CONT. CHECK VALVES PER MM 32-33-04, RT DOOR OPS CHECK NORMAL. LEAK CK GOOD. 2L73 4F A23WE 19950320003221995032000322SO 1995 3 20 95ZZZX1195 119950205A2612700120 FIRE LOOP LKHEED382 382G 526414USO NR 2 ENGINE DAMAGED A SRAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SO19920SJ 4561 FLT 2001 - NR 1 ENGINE FIRE WARNING CAME ON, SHUT DOWN NR 2 ENGINE, AND DISCHARGED FIRE BOTTLE. AIRCRAFT LANDED WITHOUT INCIDENTS. ON GROUND, INSPECTED ENGINE AND FOUND NO FIRE OCCURRED. FOUND FIRE LOOP DAMAGED, REPLACED FIRE LOOP AND FIRE EXTINGUISHING BOTTLE AND SQUIB, OPS CHECKED GOOD. 2H74 4T A1SO 19950320003231995032000323SO 1995 3 20 95ZZZX1196 119950209A6120582855 VALVE HOUSING LKHEED382 382B 5264104SO NR 3 FAILED A SRAAO OTHER JR WARNING INDICATION PARTIAL RPM/PWR LOSS CRCRUISE 1 SO19916SJ 4134 LUTTON - FLT 597F - DURING FLIGHT, NR 3 PROP RPM WENT DOWN TO 95 PERCENT. REDUCED POWER AND LANDED. FOUND NR 3 VALVE HOUSING FAULTY. REPLACED NR 3 VALVE HOUSING, RIGGED PROP, AND PERFORMED ENGINE RUN, OPS CHECKED GOOD. 2H74 4T A1SO 19950320003241995032000324WP 1995 3 20 95ZZZX1197 119950215A32414205301B CONTROL BOX DOUG DC8 DC873F 302199FWP ANTI-SKID SYST INOP A DHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01804DH 559C 46124 ON TAKEOFF, ANTI-SKID INOP LIGHT CAME ON DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED. OPENED AND CLOSED ANTI-SKID CONTROL CIRCUIT BREAKERS, ARMED ANTI-SKID AND LIGHT WENT OUT. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECKS OKAY. MM 32-40-04. 2L74 4F RT4A25 19950320003251995032000325SO 1995 3 20 C2XA95CL039 119950224A27503075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW09267147008 0305 120118 CLE/GRR - FLT 3373 - FLAPS WOULD NOT RETRACT AFTER TAKEOFF (CONTROL FAULT). RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW 27-50-06, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003261995032000326SO 1995 3 20 C2XA95IA029 119950224A323012032943001 SEQUENCE VALVE EMB 120 EMB120RT SO LT MLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0912705 120089 IAH - FLT 2697 - DURING CLIMB, PILOT REPORTED LT GEAR DID NOT RETRACT WHEN GEAR WAS SELECTED TO THE 'UP' POSITION. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LT MLG SEQUENCE VALVE. THE OPERATIONAL CHECK OF THE GEAR PROVED SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003271995032000327SO 1995 3 20 C2XA95IA030 119950224A271012012637001 BEARING ASSY EMB 120 EMB120RT SO LT AILERON WORN A C2XAK NONE E VIBRATION/BUFFET CRCRUISE 1 SW0912715 120125 IAH - FLT 2577 - DURING CRUISE, PILOT REPORTED A STRANGE VIBRATION WAS FELT THROUGHOUT AIRCRAFT DURING FLIGHT WITH VISUAL VIBRATION ON RT ENGINE INTERMITTENTLY WITH NP FLUCTUATION. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRFRAME AND RT ENGINE. NO DEFECTS WERE NOTED ON THE RT ENGINE, THE LT AILERON WAS FOUND TO HAVE A WORN OUTBOARD BEARING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING. THE AIRCRAFT WAS SATISFACTORILY TEST FLOWN, AND RELEASED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003281995032000328EU 1995 3 20 C2XA95IA031 119950302A53476022457 SEAT TRACK AEROSPATR42 ATR42320 8680930EU CABIN LT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919812 99 IAH - DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE LT FLIGHT ATTENDANT SEAT TRACK. THE CORROSION WAS DETERMINED TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT SEAT TRACK IAW CONTINENTAL EXPRESS EC 5340-01004. TT, 15,473.0. TOTAL CYCLES, 16,718. (X) 2H72 4T RTA53EU 19950320003291995032000329EU 1995 3 20 C2XA95IA033 119950301A2721S2728176000200 BELLCRANK AEROSPATR42 ATR42320 8680930EU RUDDER TAB RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0976803 066 IAH - DURING C-CHECK INSPECTION, RUDDER TRIM TAB CONTROL BELLCRANK WAS FOUND TO HAVE RUSTED BEARINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARINGS. THE AIRCRAFT WAS RETURNED TO SERVICE. TT, 13,346.8. TOTAL CYCLES, 19,110. (X) 2H72 4T RTA53EU 19950320003301995032000330EU 1995 3 20 C2XA95IA034 119950301A5320S52376105208 FRAME AEROSPATR42 ATR42320 8680930EU FS 6174 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0976803 066 IAH - DURING C-CHECK INSPECTION, CARGO DOOR FRAME AT STA 6174 WAS FOUND CRACKED AT THE UPPER EXTREMITY OF THE FRAME. MAINTENANCE PERFORMED AN INTERIM REPAIR BY STOP DRILLING THE CRACK AND APPLYING A DOUBLER. ALL WORK WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5230-01038, ORIG. TOTAL CYCLES, 19,110. AIRCRAFT TT, 13,346.8. (X) 2H72 4T RTA53EU 19950320003311995032000331EU 1995 3 20 CX2A95IA032 119950302A53476022457 SEAT TRACK AEROSPATR42 ATR42320 8680930EU CABIN RT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919812 99 IAH - DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE RT FLIGHT ATTENDANT'S SEAT TRACK. THE CORROSION WAS DETERMINED TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT SEAT TRACK IAW CONTINENTAL EXPRESS EC 5340-01004. TT, 15,473.0. TOTAL CYCLES, 16,718. (X) 2H72 4T RTA53EU 19950320003321995032000332NM 1995 3 20 IXKA9500005 119950208A73318TJ95GAB POWER SUPPLY AMETEK 8TJ95GAB BOEING727 727225 1384077NM FUEL FLOW FAILED A IXKAA UNSCHED LANDING O OTHER CLCLIMB 1 EA25354PA R0208 20624 EWR - FLT 29 - AFTER TAKEOFF, ALL FUEL FLOW WENT TO ZERO, RETURNED TO EWR. FOUND SHORTED NR 5 PIN ON FUEL FLOW POWER SUPPLY AND CHAFED WIRE TO POWER SUPPLY 8 TO 10 INCHES BEHIND S/O PANEL. REPAIRED CHAFED WIRE AND REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER MM 73-30. OPS CHECK OKAY. (X) 2L73 4F A3WE 19950320003331995032000333WP 1995 3 20 IXXA199518 119950214A5270 WIRE DOUG DC8 DC863F 302198FWP CARGO DOOR BROKEN A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23786AL 46121 PIA - ON DEPARTURE, THE MAIN CARGO DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO PIA FOR MAINTENANCE. INSPECTION OF THE DOOR ON THE GROUND SHOWED IT TO BE PROPERLY LOCKED. A WIRE WAS REPAIRED IN THE WARNING LIGHT CIRCUIT. THE AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950320003341995032000334SO 1995 3 20 WTAA950069 119950201A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120ER 3260203SO COCKPIT TRIPPED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17275UE 120058 FAT - AURAL WARNING SYSTEM ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESET AURAL WARNING SYSTEM CIRCUIT BREAKER. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003351995032000335EU 1995 3 20 WTAA950070 119950126A3350311701 EEL BATTERY PACK BAG JETSTMJETSTM3101 1500215EU CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17418UE 780 LAX - CABIN EMERGENCY LIGHTING SYSTEM FAILS TO ILLUMINATE DURING GROUND TEST. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT SYSTEM BATTERY PACKS. SYSTEM OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320003361995032000336 1995 3 20 WTAA950071 419950201A3414A3615710260 AIRSPEED IND BAG JETSTMJETSTM3101 1500215EU LEFT FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17425UE 798 SEA - CAPTAIN'S AIRSPEED INDICATOR REPORTED INOPERATIVE ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. REPLACED CAPTAIN'S AIRSPEED INDICATOR. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320003371995032000337EU 1995 3 20 WTAA950072 119950205A7712 TQ INDICATOR BAG JETSTMJETSTM3101 1500215EU LT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17418UE 780 FAT - LT ENGINE TORQUE INDICATION DROPPED FROM 104.5 PERCENT TO 80 PERCENT DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED TORQUE INDICATION SYSTEM AND PERFORMED ENGINE GROUND RUNS. UNABLE TO DUPLICATE DISCREPANCY. NO DEFECTS WITH SYSTEM NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320003381995032000338EU 1995 3 20 WTAA950073A 119950206A7712TUS06RF1135S CONNECTOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE CONTAMINATED A WTAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP17401UE 729 LMT - RT ENGINE TORQUE INDICATION DROPPED TO 60 PERCENT DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRED TORQUE AND TEMPERATURE LIMITING (TTL) SYSTEM PER MEL 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEANED AND REINSTALLED ELECTRICAL CONNECTORS AT RT ENGINE TORQUE RING AND FUEL LIMITER BYPASS VALVE. TTL SYSTEM OPERATIONAL CHECK NORMAL. (X) 2L72 4T RTA21EU 19950320003391995032000339EU 1995 3 20 WTAA950073B 119950206A7712KPT06F84S CONNECTOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE CONTAMINATED A WTAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP17401UE 729 LMT - RT ENGINE TORQUE INDICATION DROPPED TO 60 PERCENT DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRRED TORQUE AND TEMPERATURE LIMITING (TTL) SYSTEM PER MEL 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEANED AND REINSTALLED ELECTRICAL CONNECTORS AT RT ENGINE TORQUE RING AND FUEL LIMITER BYPASS VALVE. TTL SYSTEM OPERATIONAL CHECK NORMAL. (X) 2L72 4T RTA21EU 19950320003401995032000340EU 1995 3 20 WTAA950074 119950206A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17107XV 723 SFO - CREW REPORTED BIRD STRIKE TO AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AIRCRAFT. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320003411995032000341WP 1995 3 20 WTAA950075 219950207A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LEFT BIRD STRIKE A WTAAK NONE C F.O.D. TOTAKEOFF 1 WP17419UE 779 SEA - CREW REPORTED BIRD STRIKE TO AIRCRAFT AT LEFT ENGINE PROPELLER AND LANDING GEAR AREA. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AIRCRAFT. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19950320003421995032000342SO 1995 3 20 WTAA950079 119950210A5101 STRUCTURE EMB 120 EMB120RT SO AIRFRAME BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17279UE 120085 FAT - CREW REPORTED BIRD STRIKE TO AIRCRAFT. NO DAMAGE NOTED FOLLOWING INSPECTION OF AIRCRAFT ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003431995032000343EU 1995 3 20 WTAA950080 119950210A523031518224 LATCH ASSY BAG JETSTMJETSTM3101 1500215EU BAGGGAGE LOOSE A WTAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP17428UE 806 MOD - EN ROUTE VIS TO SFO - POD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO STATION WITHOUT INCIDENT. POD DOOR DISCOVERED OPEN UPON INSPECTION AT GATE. ON CALL MAINTENANCE FOUND POD DOOR LATCH ASSY TO NOT POSITIVELY SECURE DOOR IN CLOSED POSITION. MAINTENANCE ORIGINATED A NON-AIRWORTHINESS DEFERRAL OF POD DOOR AND SECURED DOOR CLOSED USING HIGH SPEED ALUMINUM TAPE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY TIGHTENING RETENTION NUT ON LATCH ROTATION BOLT. POD DOOR LATCH ASSEMBLY OPERATION NORMAL. (X) 2L72 4T RTA21EU 19950320003441995032000344EU 1995 3 20 WTAA950081 119950212A5730 SKIN BAG JETSTMJETSTM3101 1500215EU RT WING LE BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17421UE 804 MRY - CREW REPORTED BIRD STRIKE TO AIRCRAFT AT RIGHT WING LEADING EDGE BETWEEN LANDING LIGHT LENS AND ENGINE NACELLE. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION. FOUND MINOR DENT IN WING LEADING EDGE. REPAIRED DAMAGE IAW JTSTM-3101 SRM 51-40-00. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320003451995032000345SO 1995 3 20 WTAA950082 119950213A2731 ELEVATOR TRIM EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A AWTAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 WP17201YW 120201 SMF - EN ROUTE, RDD TO SFO, CREW REPORTED UNCOMMANDED PITCH UP TENDENCY WITH AUTOPILOT ENGAGED DURING CLIMB-OUT. CREW DISENGAGED AUTOPILOT AT 12,000 FEET ALTITUDE. CREW REPORTED STIFF ELEVATOR MOVEMENT CONTINUED FOLLOWING DISENGAGEMENT OF AUTOPILOT. CREW DECLARED EMERGENCY AND DIVERTED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED ELEVATOR AND ELEVATOR TRIM SYSTEM. NO DEFECTS NOTED DURING INSPECTION, UNABLE TO DUPLICATE REPORTED DISCREPANCY ON SUBSEQUENT TEST FLIGHT. LUBRICATION OF ELEVATOR TRIM ACTUATION SYSTEM ACCOMPLISHED AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003461995032000346SO 1995 3 20 WTAA950083 119950214A7331 INDICATOR EMB 120 EMB120RT SO RT ENG FF MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17286UE 120175 ACV - RIGHT FUEL FLOW GAUGE REPORTED INOPERATIVE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRED RIGHT FUEL FLOW INDICATOR PER MEL 73-32-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY INSPECTED AND OPERATIONALLY TESTED FUEL FLOW INDICATION SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. NO DEFECTS NOTED. (X) 2L72 4T RTA31SO 19950320003471995032000347SO 1995 3 20 WTAA950084 119950214A325013BF7184 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING FAILED A WTAAO OTHER J WARNING INDICATION LDLANDING 1 WP17201YW 120201 SFO - NOSE WHEEL PULLED TO RIGHT ON LANDING FOLLOWED BY PEDAL STEERING INOP LIGHT ILLUMINATION AND PEDAL STEERING FAILURE. AIRCRAFT COMPLETED LANDING ROLL WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR STEERING FEED BACK POTENTIOMETER. SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003481995032000348SO 1995 3 20 WTAA950086 119950215A7931M8372386R1005N CONNECTOR EMB 120 EMB120RT SO LT ENGINE DIRTY A WTAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 WP17269UE 120194 FAT - AFTER TAKEOFF, LEFT ENGINE OIL LOW PRESSURE AURAL WARNING ACTIVATED WITH REPORTED FLUCTUATION OF LEFT ENGINE OIL PRESSURE INDICATION OF FROM 30 PSI TO 60 PSI. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED OIL PRESSURE INDICATION SYSTEM, CLEANED ELECTRICAL CONNECTOR AT LEFT ENGINE OIL PRESSURE TRANSMITTER AND SERVICED ENGINE WITH OIL (1 QUART). PERFORMED ENGINE GROUND RUN. OIL PRESSURE INDICATION NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320003491995032000349NM 1995 3 20 DL73S950844 119950126A53156545515 FLOORBEAM BOEING737 737232 1384475NM FS 663 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11312DL 23084 THE BL 0.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STA 663, AND THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED. THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 4 INCHES AT THE SAME LOCATION. THE CRACKS ARE TYPICAL PER BOEING SERVICE BULLETIN REPAIR FOR THIS CONDITION. THE 65C34537-11 REINFORCING ANGLE COULD NOT BE INSTALLED PER THE SERVICEBULLETIN, SO THE ORIGINAL REINFORCEMENT ANGLE WILL BE REINSTALLED. 2L72 4F RTA16WE 19950320003501995032000350NM 1995 3 20 DL73S950846 119950220A5315654510515 FLOOR BEAM BOEING737 737232 1384475NM FS 663 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11322DL 23094 THE BL 0.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STATION 663. THE UPPER CAP OF THE BEAM IS CRACKED ON THE RIGHT HAND FLANGE ONLY, STARTING FROM AN EXISTING FASTENER HOLE. NO CRACKS WERE FOUND ON THE WEB. THE PANEL ATTACH HOLE WAS ALSO FOUND CRACKED AFTER HFEC INSPECTION. THE AREAWILL BE TRIMMED OUT AND REPAIRED. 2L72 4F RTA16WE 19950320003511995032000351NE 1995 3 20 9506596611 219950306A7261 OIL FILTER BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 2 ENGINE DIRTY A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01611US 20356 662311 DURING CRUISE, NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED TO ANCWHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE. NO FUELWAS DUMPED. DEBRIS WAS FOUND IN THE MAIN OIL FILTER. THE FILTER WAS REPLACED AND CHECKED OK AFTER ENGINE RUNUP. THE FILTER WAS STILL CLEAN WHEN REPLACED LATER AT MSP. 2L74 4F4 F A20WE E20EA 19950320003531995032000353EU 1995 3 20 9503753207 119950310A5347 SEAT TRACK AIRBUS320 A320211 3930320EU FS 7599 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307US 106 DURING INTERMEDIATE LAYOVER CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE SEAT TRACK AT Y = +765, FRAME 18. CORROSION WAS AT A NUT CLIP LOCATION. REPAIRED PER NWA EA 32-96360. 2L72 4F RTA28NM 19950320003541995032000354 1995 3 20 9503769953 419950309A3421 VERT GYRO DOUG DC9 DC931 3022065WP LT COCKPIT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01918RW 47158 CAPTAIN'S ATTITUDE INDICATOR GYRO FLAG APPEARED DURING CLIMB-OUT. PITCH WENT TO 15 DEGREES AND LOCKED. FLIGHT RETURNED TO GTF AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S VERTICAL GYRO AND ADI. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950320003551995032000355WP 1995 3 20 9503779983 119950309A3260 DNLOCK SWITCH DOUG DC9 DC932 3022066WP LT MLG FAILED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01983US 47282 DURING CLIMB-OUT FROM MSP, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (ORD) AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950320003561995032000356WP 1995 3 20 9503789906 119950309A2420 GENERATORS DOUG DC9 DC931 3022065WP LT/RT ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01956N 47252 LEFT AND RIGHT GENERATORS DROPPED OFF LINE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. RAN OPERATIONAL CHECK WITH NO PROBLEMS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950320003571995032000357NM 1995 3 20 9503792276 119950311A3260 SWITCH BOEING727 727251 138408HNM NLG FAILED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01276US 21155 DURING APPROACH UPON LANDING GEAR EXTENSION, NOSE GEAR UNSAFE INDICATION REMAINED ILLUMINATED. RECYCLED LANDING GEAR TO NO AVAIL. PRIOR TO PERFORMING ALTERNATE EXTENSION, NOSE GEAR SAFE INDICATION ILLUMINATED. VERIFIED INDICATION THROUGH VIEWING PORT AND LANDING GEAR AURAL WARNING HORN. MAINTENANCE REPLACED NOSE GEAR UP AND DOWN INDICATION SWITCHES. GEAR SWING CHECK NORMAL. 2L73 4F A3WE 19950320003581995032000358NM 1995 3 20 95FDEA00215 119950310A36103964401 FLOW CONTL VALVE BOEING727 727233 138408ANM AFT BODY LEAKING A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO04220FE 20934 LWR AFT BODY HEAT CAME ON DURING CLIMB-OUT PASSING THROUGH FL 320. NR 2 LEFT AND NR 3 BLEEDS OPEN BOTH PACKS ON, WENT THROUGH THE EMERGENCY PROCEDURE. THE LIGHT WENT OUT WHEN WE TURNED LEFT PACK OFF. CHECKED DUCTS AND CLAMPS IN AFT STAIRS WELL AREA FOUND OK. FOUND LEFT FLOW CONTROL VALVE WEEP HOLE BLOWING A HIGH PRESSURE STREAM OF AIR IN DETECTOR AREA. REMOVED AND REPLACED VALVE CABIN AIR FLOW AS PER MM 36-12 PRESSURE CHECKED AND GROUND CHECKED GOOD. 2L73 4F RTA3WE 19950320003591995032000359NM 1995 3 20 95FDEA00216 119950310A3260 DNLOCK SWITCH BOEING727 72725 1384006NM LT MLG FAILED A FDEAA UNSCHED LANDING CN F.O.D. FALSE WARNING APAPPROACH 1 SO04152FE 18285 ON GEAR EXTENSION LEFT MAIN GEAR INDICATED UNSAFE (RED) NOTED A BIRD STRIKE ON LEFT SIDE PRIOR TO GEAR EXTENSION. FOUND LEFT MLG DOWNLOCK SW INOP. REMOVED AND REPLACED LEFT MLG DOWNLOCK SW PER MM 32-61-21 AND 32-61-0 A/C JACKED, GEAR OPS CHECKED NORMAL PER MM 32-61-0. FOUND NO DAMAGE FROM BIRD STRIKE. 2L73 4F A3WE 19950320003601995032000360NM 1995 3 20 95FDEA00217 119950310A53157075T6100 FLOORBEAM BOEING727 72722 1384002NM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (71C209-02) BS 640 WL 200 RBL 6-13 IN NUTPLATE HOLES ON LOWER FLANGE OF FLOORBEAM. BLENDED OUT CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM STA 640 IAW FEDEX EA 7-5310-23908. 2L73 4F A3WE 19950320003611995032000361NM 1995 3 20 95FDEA00218 119950310A53157075T6100 FLOORBEAM BOEING727 72722 1384002NM BS 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 DOUBLE HOLE IN LOWER FLANGE OF FLOORBEAM BS 600 RBL 62 WL 208. REPAIRED LOWER FLANGE OF BS 600 FLOORBEAM RBL 62 PER FEDEX EA 7-5310-23941. 2L73 4F A3WE 19950320003621995032000362NM 1995 3 20 95FDEA00219 119950310A53157075T6 FLOORBEAM BOEING727 72722 1384002NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (71C709-02) IN NUTPLATE HOLES ON LOWER FLANGE OF FLOORBEAM AT BS 1110 RBL 3-47 WL 200. REPAIRED BS 1110 FLOORBEAM RBL 3-47 WL 200 AS PER FEDEX EA 7-5310-23951. 2L73 4F A3WE 19950320003631995032000363NM 1995 3 20 95FDEA00220 119950310A53137075T6040 STRINGER BOEING727 72722 1384002NM BS 400 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 STR 21R IS CRACKED AT BS 400. REPAIRED STR 21R AT BS 400 IAW FEDEX SRM 53-10-01. 2L73 4F A3WE 19950320003641995032000364NM 1995 3 20 95FDEA00221 119950310A5313BAC1498144 STRINGER BOEING727 72722 1384002NM BS 802 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 MECHANICAL DAMAGE ON STR 8L BS 802. REMOVED DAMAGED .5 INCH SECTION OF STR 8L FROM BS 802, FABRICATED AND INSTALLED PART PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950320003651995032000365NM 1995 3 20 95FDEA00222 119950310A53206920365 STIFFENER BOEING727 72722 1384002NM BS 300 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION IN E/E BAY ON FRAME STIFFENER AT BS 300 LBL 38 WL 169. PART OUT OF LIMIT REMOVED .070 BY .1250 BY .5 INCH CORROSION, REMOVED AND REPLACED STIFFENER STRAP. 2L73 4F A3WE 19950320003661995032000366NM 1995 3 20 95FDEA00223 119950310A53302024T4063 SKIN BOEING727 72722 1384002NM FWD FUS GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 GOUGES IN SKIN AT F/O'S WINDSHIELD WIPER MOUNT AND JUST BELOW O/B SIDE OF NR 1 WINDOW. BLENDED GOUGE AT SKIN BELOW F/O'S WINDSHIELD WIPER. INSTALLED DOUBLER PER FEDEX EA NR 7-5330-23942. 2L73 4F A3WE 19950320003671995032000367NM 1995 3 20 95FDEA00224 119950310A53302024T3 SKIN BOEING727 72722 1384002NM BS 441 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 GREATER THAN 10 PERCENT MATERIAL LOSS INDICATION NOTED AT BS 441 CIRCUMFERENTIAL SPLICE FWD SKIN PANEL BETWEEN STR 1920R. REPAIRED AFT UPR SKIN STA 440 STR 19 IAW FEDEX SRM 53-30-3 AND INITATED PART 5 OF 7-5330-7-2319G FOR BS 441 BETWEEN STR 19-20 FWD SKIN. 2L73 4F A3WE 19950320003681995032000368NM 1995 3 20 95FDEA00225 119950310A5320 FITTING BOEING727 72722 1384002NM BS 870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 BS 870 TERMINAL FITTING ROW 2 HOLES NR 3 AND NR 4 HAVE CRACK INDICATION NOTED RT SIDE. REPAIRED CRACK BETWEEN HOLES 3 AND 4, ROW 2 IN BS 870 TERMINAL FITTING RT SIDE IAW FEDEX EA 7-5310-23954. 2L73 4F A3WE 19950320003691995032000369NM 1995 3 20 95FDEA00226 119950310A55122024T3050 SKIN BOEING727 72722 1384002NM HORIZ STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 9503-11 LEFT HORIZONTAL STABILIZER INTERSPAR SKIN (LWR SURFACE) IS DAMAGED BETWEEN STAB STA 151.81 AND STAB 169.81. REPAIRED DAMAGED AREA ON LEFT HORIZONTAIL STAB LOWER SKIN IAW FEDEX SRM 55-10-3. 2L73 4F A3WE 19950320003701995032000370NM 1995 3 20 95FDEA00227 119950311A5300 AIRFRAME BOEING727 727233 138408ANM FWD FUS VIBRATION A FDEAH DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET UKUNKNOWN 1 SO04264FE 21626 INFO ONLY, AT 8,000, 220 KIAS, NOTICEABLE VIBRATION BEGAN UNDERNEATH THE COCKPIT, PRESS NORMAL WITH NR 2 PACKS IN OPERATION, CYCLED GEAR, VIBRATION REMAINED, SELECT MANUAL AC AT OPENED OUTFLOW VLV, AS CABIN PASSED THROUGH 6500, SELECTED AUTO, VIBRATION STOPPED AS PRESS CONTROLLER PUT BACK IN AUTO, AIRSPEED WAS 290 KIAS AT 16000. INSPECTED OUTFLOW VLV BOTH AC AND DC SYS TESTED NORMAL. INSPECTED A/C FOR ANY LOOSE PANELS OR SURFACE DEFECTS, NONE FOUND. A/C OK FOR SERVICE. 2L73 4F RTA3WE 19950320003711995032000371NM 1995 3 20 95FDEA00228 119950311A2916AYG70725023 RESERVOIR DOUG MD11 MD11F 3023600NM NR 3 HYD SYST FAILED A FDEAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO04605FE 48514 LOST NR 3 HYDRO SYS FLUID QTY, THE SYS WENT DOWN TO EMPTY AFTER GEAR RETRACTION. REMOVED AND REPLACED NR 3 SYS HYD RESERVOIR. RAN HYDRO PRESS AND CHECKED FOR LEAKS. OPS CKD GOOD, OK FOR SERVICE. 2L73 4F RTA22WE 19950320003721995032000372WP 1995 3 20 ABXA9500148 119950112A533059114063 SKIN DOUG DC9 DC932 3022066WP FS 150 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE SKIN GOUGED AT THE ENTRY DOOR FORWARD JAMB, SECOND PRESSURE STOP FROM BOTTOM. REPAIRED SKIN IAW ABX REA D953-10696-MR. 2L72 4F A6WE 19950320003741995032000374WP 1995 3 20 ABXA9500150 119950213A53205912350 DOUBLER DOUG DC9 DC932 3022066WP FS 83 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE STEEL PLATE ALONG THE CENTER WINDSHIELD LOWER FRAME RUSTED AND HAD POPPED RIVETS. CLEANED AND TREATED PLATE IAW DC-9 SRM CHAPTER 51-10-3 AND REPLACED FASTENERS IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND ABX REA D953-10945. 2L72 4F A6WE 19950320003751995032000375WP 1995 3 20 ABXA9500151 119950131A53120252024T3 BULKHEAD SKIN DOUG DC9 DC932 3022066WP FS 996 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DENT AND PUNCTURE IN AFT PRESSURE BULKHEAD SKIN, FORWARD FACE, BETWEEN LONGERON 29R AND 30R APPROXIMATELY EIGHT INCHES UP FROM TEE CAP. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 1, SHEET 2. 2L72 4F A6WE 19950320003761995032000376WP 1995 3 20 ABXA9500152 119950216A5320991245550 DOUBLER DOUG DC9 DC932 3022066WP FS 408 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE INNER DOUBLER CUT OUT AT BOTTOM OF LOWER CARGO DOOR JAMB AT FS 408. REPAIRED INNER DOUBLER IAW ABX REA D953-10895-MR. 2L72 4F A6WE 19950320003771995032000377WP 1995 3 20 ABXA9500153 119950213A52605915066501 DOOR DOUG DC9 DC932 3022066WP FS 160 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD AIRSTAIR DOOR HAD A REPAIR ON A CRACK AT THE INNER RIB THAT WAS NOT IAW THE SRM. REPAIRED IAW ABX REA D952-10953-MR. 2L72 4F A6WE 19950320003811995032000381WP 1995 3 20 ABXA9500157 119950207A5320591046423 ANGLE DOUG DC9 DC932 3022066WP FS 650 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A L ANGLE CRACKED ABOVE THE CENTER WING TANK AT FS 650 AND LBL 44. REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003831995032000383WP 1995 3 20 ABXA9500159 119950210A531199124512 FRAME DOUG DC9 DC932 3022066WP FS 362 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME GOUGED AT FS 362, BETWEEN LONGERON 29 AND 30R. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10947-MR. 2L72 4F A6WE 19950320003841995032000384WP 1995 3 20 ABXA9500160 119950211A57115911301502 SPAR DOUG DC9 DC932 3022066WP XRS 164 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WING REAR SPAR CRACKED AT INBOARD LOWER HOLE FOR INBOARD FLAP HINGE. REPAIRED ANGLE IAW ABX REA D957-10642-SB. 2L72 4F A6WE 19950320003861995032000386WP 1995 3 20 ABXA9500162 119950209A531359203192 LONGERON DOUG DC9 DC932 3022066WP FS 237 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 FROM FS 237 TO FS 579, IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003871995032000387WP 1995 3 20 ABXA9500163 119950126A5311991187721 FRAME DOUG DC9 DC932 3022066WP FS 1132 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME 1132, LEFT SIDE BELOW CATWALK. REPLACED FRAME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003881995032000388WP 1995 3 20 ABXA9500164 119950203A53203957175501 FITTING DOUG DC9 DC932 3022066WP FS 1121 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE FRAME FITTING CRACKED AT FS 1121. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND 51-30-3. 2L72 4F A6WE 19950320003891995032000389WP 1995 3 20 ABXA9500165 119950118A532056443242 RETAINER DOUG DC9 DC932 3022066WP FS 120 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV 3 X-RAY INSPECTION OF THE RIGHT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239. 2L72 4F A6WE 19950320003911995032000391WP 1995 3 20 ABXA9500167 119950118A532056443241 RETAINER DOUG DC9 DC932 3022066WP FS 120 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; SB 56-11, REV 3 X-RAY INSPECTION OF LEFT COCKPIT EYEBROW WINDOW RETAINER, FOUND A CRACK INDICATION. REPAIRED CRACK IAW ABX REA D956-10760 AND EA NR AD-56-3239. 2L72 4F A6WE 19950320003931995032000393WP 1995 3 20 ABXA9500169 119950131A5330592032393 SKIN DOUG DC9 DC932 3022066WP FS 229-512 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER FUSELAGE SKIN FROM FS 229 TO FS 512, FROM LONGERON 18R TO 26R, HAD NUMEROUS AREAS OF CORROSION AND PREVIOUS REPAIRS. REPLACED SKIN FROM FS 229 TO FS 512 IAW ABX REA D953-10751-MR AND DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003951995032000395WP 1995 3 20 ABXA9500171 119950116A53305911418111 SKIN DOUG DC9 DC932 3022066WP FS 588-669 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FUSELAGE EXTERIOR SKIN FROM FS 588 SPLICE TO FS 669 SPLICE AT LONGERON 26 LEFT TO 26 RIGHT. REPLACED SKIN IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003961995032000396WP 1995 3 20 ABXA9500172 119950124A533059197073 SKIN DOUG DC9 DC932 3022066WP FS 802-996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON AFT FUSELAGE LOWER SKIN FROM FS 802 TO FS 996, BETWEEN LONGERON 26 RIGHT TO 26 LEFT. REPLACE LOWER SKIN FROM FS 802 TO FS 996 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320003981995032000398WP 1995 3 20 ABXA9500174 119950206A5400995815958 RIB CAP DOUG DC9 DC932 3022066WP YN 170 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK ON THE NR 2 ENGINE PYLON RIB CAP AT STATION YN 170. REPAIRED RIB CAP IAW ABX REA D954-10691-MR. 2L72 4F A6WE 19950320003991995032000399WP 1995 3 20 ABXA9500175 119950211A53415913055504AX FITTING DOUG DC9 DC932 3022066WP FS 604 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON WING TO FUSELAGE FITTING ON TOP OF CENTER WING SECTION, RIGHT SIDE, AT STATION XCW 58 AND FS 604. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-5 AND 51-20-0. 2L72 4F A6WE 19950320004001995032000400WP 1995 3 20 ABXA9500176 119950112A57115911301501 SPAR DOUG DC9 DC932 3022066WP XRS 385-390 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP BETWEEN XRS 385 AND XRS 390. REPAIRED LEFT WING LOWER REAR SPAR CAP IAW ABX REA D957-10773-MR. 2L72 4F A6WE 19950320004011995032000401WP 1995 3 20 ABXA9500177 119950123A57115911301502 SPAR DOUG DC9 DC932 3022066WP XRS 488-560 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING C-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LOWER FLANGE OF THE RIGHT WING LOWER REAR SPAR FROM XRS 488 TO XRS 560. REPAIRED RIGHT WING LOWER REAR SPAR IAW ABX REA D957-10795-MR. 2L72 4F A6WE 19950320004021995032000402WP 1995 3 20 ABXA9500178 119950118A5730591216147 PANEL DOUG DC9 DC932 3022066WP XRS 69 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING UPPER BONDED PANEL INBOARD OF THE GEAR TRUNNION. REPLACED UPPER BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2L72 4F A6WE 19950320004031995032000403WP 1995 3 20 ABXA9500179 119950131A573059127352 PANEL DOUG DC9 DC932 3022066WP XRS 509 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING OUTBOARD TRAILING EDGE PANEL JUST FORWARD OF THE AILERON. REPLACED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2L72 4F A6WE 19950320004041995032000404WP 1995 3 20 ABXA9500180 119950202A53302024T3 SKIN DOUG DC9 DC932 3022066WP FS 889 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN IMPROPER REPAIR ON THE FUSELAGE EXTERIOR SKIN AT FS 889 AND LONGERON 21 RIGHT. REPAIRED SKIN IAW ABX REA D953-10806-MR. 2L72 4F A6WE 19950320004051995032000405SO 1995 3 20 COM11817 119950313A573012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A ACOMAK NONE O OTHER ININSP/MAINT 1 SO01162CA14139 120150 FUEL WAS FOUND LEAKING FROM THE LEFT WING UPPER SKIN. TWO RIVET HEADS WERE FOUND BROKEN AT RIB NR 20 BETWEEN STRINGERS NR 2 AND NR 3. INTERNAL INSPECTION REVEALED THE SKIN SUPPORT BRACKET CRACKED AT THAT LOCATION. THE SKIN SUPPORT WAS REPLACED PER AERODESIGN REPORT NR 1327-2, REVIR, DATED 11-30-94. 2L72 4T RTA31SO 19950320004061995032000406SO 1995 3 20 COM11818 119950303A5730 SKIN SUPPORT EMB 120 EMB120RT SO WING RIBS CRACKED A ACOMAK NONE O OTHER ININSP/MAINT 1 SO01462CA7015 120264 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE CRACKED SKIN SUPPORTS WERE REPLACED IAW AERO DESIGN REPORT NR 1327-2. P/N 120-17056-007, 6 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17056-011, 1 EA; 120-17057-006, 1 EA; 120-17057-007, 2 EA; 120-17057-005, 1 EA; 120-17056-019, 1 EA; 120-17062-011, 1 EA; 120-17060-011, 1 EA. 2L72 4T RTA31SO 19950320004071995032000407SO 1995 3 20 COM11819 119950313A5270 WARNING LIGHT EMB 120 EMB120RT SO CARGO DOOR ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01254CA 120233 CARGO DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. DEFERRED DOOR WARNING SYSTEM AND AIRCRAFT CONTINUED SERVICE. 2L72 4T RTA31SO 19950320004081995032000408SO 1995 3 20 COM11820 119950312A29321206P011401 PRESS SWITCH EMB 120 EMB120RT SO RUDDER DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01156CA 120156 RUDDER, GREEN HYDRAULIC SYSTEM FAIL WARNING, DOES NOT FUNCTION. REPLACED RUDDER SYSTEM PRESSURE SWITCH. 2L72 4T RTA31SO 19950320004091995032000409SW 1995 3 20 COM20358 119950311A5210272404410 FRAME SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01702M AC702 FOUND PASSENGER DOOR UPPER FORWARD CORNER FRAME TO BE CRACKED. FIRST NOTICED CORNER DOUBLER (COVER) TO BE CRACKED. WHEN DOUBLER WAS REMOVED FOUND FRAME TO ALSO BE CRACKED. BOTH PARTS CRACKED AT APEX OF CORNER RADIUS. INSTALLED SERVICEABLE PARTS AND RETURNED TO SERVICE. WORK PERFORMED I/A/W AERODESIGN ENGINEERING REPORT NR 1469-1 DATED 3-11-95. 1L72 4T A8SW 19950320004101995032000410SW 1995 3 20 COM20359 119950311A52102724181086 DOUBLER SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01702M AC702 FOUND PAX DOOR UPPER FORWARD CORNER FRAME DOUBLER TO BE CRACKED. FURTHER INSPECTION REVEALED UPPER FORWARD CORNER FRAME ALSO TO BE CRACKED. REPLACED PARTS WITH SERVICEABLE LIKE PARTS AND RETURNED TO SERVICE. CRACKS ARE AT THE APEX OF THE RADIUS ON THE FRAME AND DOUBLER. REPAIR DONE IN ACCORDANCE WITH AERODESIGN AIRCRAFT ENGINEERING REPORT NR 1469-1 DATED 3-11-95. 1L72 4T A8SW 19950320004111995032000411EU 1995 3 20 COM31044 119950313A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01340SF9840 560 JAN920185 340A014 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950320004121995032000412EU 1995 3 20 COM31045 119950313A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01340SF4727 560 NOV920499 340A014 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950320004131995032000413EU 1995 3 20 COM31046 119950312A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01357CA10807488 OCT910075 340A044 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950320004141995032000414EU 1995 3 20 COM31048 119950314A5343AIR835625 TRUNNION BEARING SAAB SF340 SF340A 7850100EU NLG DIRTY A COMAK NONE O OTHER CLCLIMB 1 SO01358CA140912230 340A047 LOUD SQUEAL FROM NLG DURING EXTENSION OR RETRACTION. CLEANED NLG TRUNNION BEARINGS AND SQUEALING NOISE STOPPED. 2L72 4T RTA52EU 19950320004151995032000415EA 1995 3 20 COM60439 119950313A3260864806 PSEU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01915CA3527 2278 7013 WOW INPUT MESSAGE ON EICAS. PROXIMITY SYSTEM FAULT ON STATUS PAGE. REPLACED THE PSEU. 2L72 4F RTA21EA 19950320004161995032000416 1995 3 20 MWEA95149 419950313A256511331DC EVAC SLIDE DOUG DC9 DC914 3022034WP GALLEY DOOR LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31800ME 861 45842 DURING ROUTINE DAILY INSPECTION THE GALLEY SERVICE DOOR EVACUATION SLIDE PRESSURE WAS FOUND TO BE LOW. REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950320004171995032000417NM 1995 3 20 SWAA950222 119950309A5330 SKIN BOEING737 7372H4 138448CNM BS 470-490 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 470, 471, AND 490, STRINGER 10L. REPAIRED PER TRAMCO EWO 95-0203. 2L72 4F A16WE 19950320004181995032000418NM 1995 3 20 SWAA950223 119950309A5330 SKIN BOEING737 7372H4 138448CNM BS 727-578 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 727+11, 757, AND 758, STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0203. 2L72 4F A16WE 19950320004191995032000419NM 1995 3 20 SWAA950224 119950309A5330 SKIN BOEING737 7372H4 138448CNM BS 391 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT BS 391, STRINGER 14L. REPAIRED PER TRAMCO EWO 95-0203 AND 95-0205. 2L72 4F A16WE 19950320004201995032000420NM 1995 3 20 SWAA950225 119950309A5320 STIFFENER BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT VERTICAL STIFFENER, BS 178, LBL 6, WL 184. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004211995032000421NM 1995 3 20 SWAA950226 119950309A5312 BULKHEAD SKIN BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004221995032000422NM 1995 3 20 SWAA950227 119950309A5320 STIFFENER BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT VERTICAL STIFFENER, BS 178, RBL 6, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004231995032000423NM 1995 3 20 SWAA950228 119950309A5330 SKIN BOEING737 7372H4 138448CNM BS 986.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0754SW 21535 DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATION AT AFT ENTRY DOOR UPPER AFT CORNER, BS 986.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004241995032000424NM 1995 3 20 SWAA950229 119950309A5311 BELTFRAME BOEING737 7372H4 138448CNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0794SW 23053 DURING SCHEDULED QUARTER D CHECK, FOUND BELTFRAME CRACKED AT BS 360, STRINGER 26L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004251995032000425NM 1995 3 20 SWAA950230 119950309A5320 WEB BOEING737 7372H4 138448CNM LT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0794SW 23053 DURING SCHEDULED QUARTER D CHECK, FOUND WEB CRACKED 1 INCH AT I/B RADIUS ABOVE RAM AIR DUCT AT FWD END ATTACH POINT, LEFT AC BAY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950320004581995032000458EU 1995 3 20 95ZZZW201 119950228A7712 SIG CONDITIONER BAG JETSTMJETSTM3201 1500217EU RT ENGINE MALFUNCTIONED A NVEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO03940AE 940 BNA - FLT 4686 - PILOT RT ENGINE FAILED TO RESPOND TO POWER LEVER MOVEMENTS. RT ENGINE WAS SHUTDOWN, AC RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND TORQUE INDICATOR CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER SYSTEM OPERATIONAL CHECKED NORMAL. REPLACED TORQUE SIGNAL CONDITIONER AS A PRECAUTION. 2L72 4T RTA56EU 19950320004591995032000459EU 1995 3 20 95ZZZW202 119950227A261251653152 FIRE CONTL UNIT AEROSPATR42 ATR42300 8680920EU RT ENGINE FAILED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO03144DD 74 MIA - FLT 5740 - CREW REPORTS, RT ENGINE FIRE WARNING INDICATION ON TAKEOFF. NO FIRE OR SMOKE NOTED. FEATHERED AND SHUTDOWN THE ENGINE AND RETURNED TO MIA. CFR WAS NOTIFIED. ACFT LANDED WITHOUT INCIDENT. REPLACED FIRE CONTROL UNIT AND OPS CHECK GOOD. 2H72 4T RTA53EU 19950320004601995032000460EU 1995 3 20 95ZZZW203 119950214A32301859 DNLOCK ACTUATOR BAG JETSTMJETSTM3201 1500217EU NLG CONTAMINATED A NVEAL ABORTED APPROACH OP OTHER NO WARNING INDICATION APAPPROACH 1 SO03936AE4368 936 BNA - FLT - 4569 - ON APPROACH, WHEN GEAR WAS EXTENDED WITH NO NOSE GEAR GREEN LIGHT INDICATION AND NO TAXI LIGHT. ACFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. PURGE WATER OUT OF DOWNLOCK ACTUATOR BY SERVICING ACTUATOR WITH GREASE. ALSO, CLEANED DOWNLOCK SWITCH AS PRECAUTIONARY MEASURES. 2L72 4T RTA56EU 19950320004611995032000461EU 1995 3 20 95ZZZW204 119950213A325061823 JACK ASSY BAG JETSTMJETSTM3201 1500217EU NLG STEERING BROKEN A NVEAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO03934AE6716 934 PIA - FLT 4786 - ON TAXI FOR TAKEOFF, CREW HEARD LOUD POP FROM NOSE AREA OF ACFT. THE ACFT WOULD ONLY TURN IN ONE DIRECTION. CREW RETURNED ACFT TO BLOCK. FOUND THAT STEERING JACK BROKE. REMOVED AND REPLACED STEERING JACK. 2L72 4T RTA56EU 19950320004621995032000462NM 1995 3 20 95ZZZW205 119950227A3230 PIN BOEING727 727247 138408FNM NLG NO INSTALLED A AARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19326AS 20268 MIA - AFTER TAKEOFF, THE NLG AND DOOR LIGHT REMAINED ON WITH AIRFRAME VIBRATION AND AIR NOISE FROM GEAR AREA. RETURNED TO MIA. FOUND NOSE GEAR SENSOR LINK PIN NOT INSTALLED. REINSTALLED PIN. REPLACED LT AND RT NLG WHEELS. INSPECTED AREA, ACFT DEPARTED TO PAP. 2L73 4F A3WE 19950320004631995032000463WP 1995 3 20 95ZZZW206 119950227A2612D5020 FIRE LOOP DOUG DC8 DC862 3021970WP NR 2 ENGINE FAILED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1966656 45953 DURING POST FILGHT, NR 2 ENGINE FIRE WARNING TEST FOUND INOP. REMOVED AND REPLACED LOWER FIRE LOOP ASSY IAW MM 28-10. OPS CHECK GOOD. 2L74 4F 4A25 19950320004641995032000464WP 1995 3 20 95ZZZW207 119950216A5711 SPAR DOUG DC8 DC862 3021970WP FS 857 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 CENTER TANK (WING) TOP AFT SPAR FLANGE (CAP) HAS LEVEL II CORROSION ON TOP OF HORIZONTAL FLANGE AROUND FASTENER HEADS AT BL 23L FS 857 REF N/R NR 5086. 2L74 4F 4A25 19950320004651995032000465WP 1995 3 20 95ZZZW208 119950220A5720 SUPPORT PLATE DOUG DC8 DC862 3021970WP WS 341.5 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 L/E BETWEEN NR 3 AND 4 ENGINE AT XFS341.500 RIB LOWER SUPPORT PLATE HAS TWO CRACKS EMANATING FROM FASTENER HOLES. REF N/R 1101 WO NR 950007. 2L74 4F 4A25 19950320004661995032000466WP 1995 3 20 95ZZZW209 119950220A5730 SKIN DOUG DC8 DC862 3021970WP WS 304-416 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 L/E BETWEEN NR 3 AND 4 ENGINE HAS CORROSION LEVEL II AND DELAMINATION OF FASTENER HOLES (UPPER) XFS 304 TO XFS 416. REF N/R 1102 W/O NR 950007. 2L74 4F 4A25 19950320004671995032000467WP 1995 3 20 95ZZZW210 119950218A3350501107503 EEL PWR SUPPLY DOUG DC8 DC862 3021970WP CABIN INOPERATIVE A ARWAK NONE L NO TEST ININSP/MAINT 1 SO19810BN 45905 DURING ROUTINE MAINTENANCE CHECK, FOUND BATTERY PACK FOR EMERGENCY LIGHTS DEAD. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD IAW MM 33-10. 2L74 4F 4A25 19950320004681995032000468WP 1995 3 20 95ZZZW211 119950217A33505708458405 EEL BATTERY PACK DOUG DC8 DC862 3021970WP CABIN DISCHARGED A ARWAK NONE L NO TEST ININSP/MAINT 1 SO19810BN 45905 BATTERY PACK FOR EMERGENCY LIGHTS IS DEAD. REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMAL IAW DC8MM 33-10-00/33-50-00. 2L74 4F 4A25 19950320004691995032000469WP 1995 3 20 95ZZZW212 119950228A575457695832 SLOT DOOR DOUG DC8 DC862 3021970WP LE FLAP CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 RT WING OUTBOARD SLOT DOOR HAS CORROSION LEVEL II AT L/E. REF N/R 1117 WO 950015. 2L74 4F 4A25 19950320004701995032000470WP 1995 3 20 95ZZZW213 119950201A573057583874 SKIN DOUG DC8 DC863 302198AWP WS 454 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 LOWER WING PANEL HAS 3 INCH CRACK ON RT WING AT XW 454. ACCOMPLISHED REPAIRS PER DOUG ROD SKETCH NR 94-11-18-006 WORK DOCUMENTED IN ARROW AIR W/O 950034. 2L74 4F 4A25 19950320004711995032000471NM 1995 3 20 95ZZZW214 119950224A3350079123 EEL LENS BOEING727 727247 138408FNM CABIN MISSING A ARWAK NONE O OTHER ININSP/MAINT 1 SO19326AS 20268 RED LENS MISSING FROM EMERGNECY PATH LIGHTING. REPLACED MISSING LENS FOR EMERGENCY PATH LIGHTING. OPS NORMAL. 2L73 4F A3WE 19950320004721995032000472NM 1995 3 20 95ZZZW215 119950226A2432061513 BATTERY CHARGER BOEING747 747122 1384872NM COCKPIT OVERHEATED A P5CAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP234712U 19757 CREW REPORTED SMOKE COMING FROM FEO'S PANEL JUST FORWARD OF RIGHT UPPER DECK DOOR. SMOKE DISSIPATED AFTER 2 MINUTES. POST FLIGHT INSPECTION BY MAINTENANCE REVEALED BATTERY CHARGER CAUSING OVERHEAT OF SHIP BATTERY. REMOVED AND REPLACED BATTERY CHARGER AND SHIP BATTERY PER MM 24-31-01. OPERATIONAL CHECKS NORMAL. INSPECTED ASSOCIATED WIRING, FOUND OK. AIRCRAFT RELEASE FOR SERVICE. 2L74 4F A20WE 19950320004731995032000473NM 1995 3 20 95ZZZW216 119950216A5320 RING BOEING727 727231 1384079NM FS 520 BENT A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736842 21989 MCI - DURING OP-17, FOUND FORMER RING BENT BETWEEN STRINGERS 23L AND 24L, FS 520. REPAIRED PER ARA 9106. TOTAL CYCLES 22,210. 2L73 4F A3WE 19950320004741995032000474WP 1995 3 20 95ZZZW217 119950127A5311 FRAME DOUG DC9 DC932 3022066WP BS 680 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05996Z 47028 STL - DURING OP-15, FOUND ONE INCH CRACK IN MAIN FRAME RIGHT SIDE, STATION 680, ABOVE STRINGER 15R. REPAIRED PER EMLR 65330. TOTAL CYCLES 78,720. 2L72 4F A6WE 19950320004751995032000475NM 1995 3 20 95ZZZW218 119950210A5230 SKIN BOEING727 727231 1384079NM CARGO DOOR CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554340 20845 MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN EXTERIOR SKIN AT TOP AFT CORNER OF FORWARD ENTRY DOOR. CUT OUT CRACKED AND DAMAGED AREA, REPAIRED PER SRM 5-30-03. TOTAL CYCLES 33,173. 2L73 4F A3WE 19950320004761995032000476NM 1995 3 20 95ZZZW219 119950216A5313 STRINGER BOEING727 727231 1384079NM FS 1000-1010 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736843 21989 MCI - DURING OP-17 FOUND A 6 INCH CRACK AT AFT CARGO STRINGER 29, IN RT VERTICAL LEG INBOARD SIDE, FS 1000 TO FS 1010. REPAIRED PER ARA 8682 AND STANDARD PRACTICES. TOTAL CYCLES 22,210. 2L73 4F A3WE 19950320004771995032000477NM 1995 3 20 95ZZZW220 119950213A5330 SKIN BOEING727 727231 1384079NM FWD FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055434439682 21631 MCI - DURING CHECK C-1D, FOUND A 1.5 INCH CRACK IN FORWARD FUSELAGE, RUNNING FORWARD TO FASTENER HOLE UPPER HINGE CUTOUT, FORWARD ENTRY DOOR. REPAIRED BY INSTALLING DOUBLER PER S/B 727-53-0198. TOTAL CYCLES 25,548. 2L73 4F A3WE 19950320004781995032000478WP 1995 3 20 95ZZZW221 119950228A2120 AIR DIST DOUG DC9 DC982 3022082WP CABIN ODOR A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE05904TW 49156 STL - DURING DESCENT, SMOKE APPEARED IN CABIN WITH A HOT ODOR. TURNED OFF AIRFOIL ANTI-ICE AND SMOKE AND ODOR DISSIPATED. ACCOMPLISHED AIR CONDITIONING DUCT OIL CONTAMINATION CHECKS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-2D. 2L72 4F A6WE 19950320004791995032000479WP 1995 3 20 95ZZZW222 119950203A5312 DOOR JAMB DOUG DC9 DC934 302207EWP AFT PRESS BLKHD CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05936L 39992 47711 STL - DURING C-CHECK, FOND A .875 INCH CRACK IN UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD PASSENGER DOOR JAMB. STOP DRILLED CRACK AND REPAIRED PER S/B 53-137. TOTAL CYCLES 29,619. 2L72 4F RTA6WE 19950320004801995032000480WP 1995 3 20 95ZZZW223 119950213A5720 CASTELLATION LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE053100859861 193B1028 MCI - DURING SPECIAL CHECK, FOUND CRACK IN CASTELLATION, EMANATING UNDER UPPER RIB, OUTBOARD SIDE IWS 555.00, AT STRINGER 18, 19 AND 20, RESPECTIVELY. REPAIRED PER DRAWING 1647070 AND TWA STANDARD PRACTICES. TOTAL CYCLES 23,012. 2L73 4F A23WE 19950320004811995032000481WP 1995 3 20 95ZZZW224 119950213A5330 SKIN LKHEED1011 10113851 5265010WP BS 649 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE051501757754 193B1063 MCI - DURING CHECK C-6C, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN, WITH AREA BULGED OUTWARD AND WITH RIVET HEAD MISSING, STATION 649, STRINGER 36-37. REPAIRED PER SRM 53-31-00, FIGURE 815. TOTAL CYCLES 22,020. 2L73 4F A23WE 19950320004821995032000482NM 1995 3 20 95ZZZW225 119950216A5320 STIFFENER BOEING747 747131 1384881NM BS 1301 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059310996368 19675 JFK - DURING SPECIAL CHECK, FOUND TWO CRACKS AT BOTTOM OF STIFFENER, STATION 1301. REPAIRED PER SRM 53-10-09. TOTAL CYCLES 17,680. 2L74 4F A20WE 19950320004831995032000483WP 1995 3 20 95ZZZW226 119950221A3230PN2T205 CIRCUIT BREAKER LKHEED1011 1011385115 5265015WP LANDING GEAR TRIPPED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0531031 193B1115 JFK - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. FOUND NO ELECTRICAL POWER TO LANDING GEAR TRUCK LEVEL SENSORS. REPLACED 2F16 CIRCUIT BREAKER, MFG P/N 2T20-5. LANDING GEAR SYSTEM CHECKED NORMAL. CHECK C-9C. 2L73 4F A23WE 19950320004841995032000484WP 1995 3 20 95ZZZW227 119950213A5712 RIB LKHEED1011 10113851 5265010WP WS 503 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE051100459668 193B1016 MCI - DURING SPECIAL CHECK, FOUND CRACKS IN UPPER RIB CAP IWS 503, IN CASTELLATION AT FORWARD SIDE OF STRINGERS 13, 24 AND 25, 1.1250 INCH, 1.25 INCH AND ONE INCH, RESPECTIVELY, INTO AND THROUGH RADIUS. REPAIRED BY INSTALLATION OF NEW SECTION OF RIB CAP PER DRAWING NR 1647070. TOTAL CYCLES 23,342. 2L73 4F A23WE 19950320004851995032000485WP 1995 3 20 95ZZZW228 119950301A2530 CONNECTOR DOUG DC9 DC932 3022066WP NR 2 COFFEE POT SHORTED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05929L 47174 STL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT. SHUT OFF ELECTRICAL POWER TO GALLEY. FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED. REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS, MFG P/N WK-236318. OPERATION OF NR 2 COFFEEMAKER CHECKED NORMAL. CHECK OP-16. 2L72 4F A6WE 19950320004861995032000486WP 1995 3 20 95ZZZW229 119950301A32301506362101 SUPPORT LKHEED1011 10113851 5265010WP NLG UPLOCK BROKEN A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0531014 193B1036 JFK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE INTRANSIT LIGHT REMAINED ON AND NOSE LANDING GEAR DOOR LIGHT WOULD ILLUMINATE WHEN LANDING GEAR SELECTOR PLACED IN NEUTRAL. FOUND NOSE LANDING GEAR UPLOCK SUPPORT BROKEN, MFG P/N 1506362-101. REPLACED NOSE LANDING GEAR UPLOCK ASSEMBLY, MFG P/N 1606361-105. NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL. CHECK C-7C. 2L73 4F A23WE 19950320004871995032000487WP 1995 3 20 ASAA9580005 119950217A5753 FAIRING DOUG DC9 DC982 3022082WP LT TE FLAP OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 SEA - DURING SERVICE CHECK, THE LEFT INBOARD FLAP FAIRING WAS FOUND TO BE OUT OF ADJUSTMENT. WITH THE FLAPS RETRACTED, THE LEFT MLG DOOR WOULD NOT OPEN DUE TO INTERFERENCE FROM FLAP FAIRING. ADJUSTED THE FLAP FAIRING PER MM 27-51-0 AND MLG DOOR OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320004881995032000488NE 1995 3 20 ASAA9580007 219950217A7250 TURBINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE FAILED A ASAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NM01938AS 49365 P717325D OAK - FLT 439 - CREW REPORTED NR 1 ENGINE FAILED AFTER TAKEOFF, NR 1 ENGINE SHUTDOWN AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE DUE TO TURBINE FAILURE. VENDOR TEARDOWN REVEALED 8TH STAGE STATOR SUPPORT FLANGE FAILED. (W) 2L72 4F4 F A6WE E9NE 19950320004891995032000489WP 1995 3 20 ASAA9580017 119950224A5347TMS6019943 SEAT TRACK DOUG DC9 DC982 3022082WP BS 210 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS28294 49232 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK Y210, X-45, Z PLUS 1. REMOVED CORRODED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05 PG 10, 51-10-03 PG 18, 51-10-04 PG 16, 51-20-00 PGS 1 AND 7, 51-30-01 PGS 1 AND 4, 51-30-02 PG 1, 51-30-05 PGS 1, 4, 4A 6 AND 7. (W) 2L72 4F A6WE 19950320004901995032000490WP 1995 3 20 ASAA9580018 119950224A53112777930 FRAME DOUG DC9 DC982 3022082WP BS 1233 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS28294 49232 PAE - DURING 30 K CHECK, CORROSION WAS FOUND ON FRAME AT Y1233, X PLUS 12 TO X-8 AND AFT SIDE OF FRAME. REMOVED CORROSION, FRAME OUT OF LIMITS. REMOVED DAMAGED SECTION AND REPAIRED FRAME IAW DC-9 SRM 53-03, 53-01, 53-14-03, 51-30-05. (W) 2L72 4F A6WE 19950320004911995032000491WP 1995 3 20 ASAA9580019 119950224A5311 FRAME DOUG DC9 DC982 3022082WP BS 1311 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS28294 49232 PAE - DURING 30 K CHECK, CORROSION WAS FOUND ON FRAME AT Y1311, Z-43, X PLUS 0. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 53-14-03 PGS 24-26, 51-10-01 PG 50, 53-03 PG 1, 51-10-03 PGS 15 AND 18. (W) 2L72 4F A6WE 19950320004921995032000492WP 1995 3 20 ASAA9580021 119950224A5320993061269 MEMBRANE DOUG DC9 DC982 3022082WP BS 1142 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PAE - DURING 30K CHECK CORROSION WAS FOUND ON CEILING WEB IN LEFT TUNNEL OF AFT CARGO COMPARTMENT AT Y1142, Z PLUS 52, Z PLUS 0. REMOVED MEMBRANE. INSTALLED NEW MEMBRANE WET WITH SEAL AT FUS STATION 984-1338, X PLUS 52, Z PLUS 0 IAW DOUGLAS AIRCRAFT DRAWING NR 9930612. (W) 2L72 4F A6WE 19950320004931995032000493WP 1995 3 20 ASAA9580023 119950224A5347TMS6019609 CARGO TRACK DOUG DC9 DC982 3022082WP BS 218-370 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK CORROSION WAS FOUND AROUND FASTENER HOLES IN CARGO TRACK AT Y300-Y350, X-22, Z-44. REMOVED CORRODED CARGO TRACK. INSTALLED NEW CARGO TRACK IAW DC-9 SRM 53-05, 51-10-03, 51-30-02, 51-30-05. TOTAL CYCLES 20,062. (W) 2L72 4F A6WE 19950320004941995032000494WP 1995 3 20 ASAA9580024 119950317A52105910081167 MECHANISM DOUG DC9 DC982 3022082WP L-1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01935AS 49236 SEA - FLT 477 - CREW REPORTED L-1 DOOR DIFFICULT TO OPEN. ADJUSTED DOOR PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950320004951995032000495WP 1995 3 20 ASAA9580025 119950224A533029129003 SKIN DOUBLER DOUG DC9 DC982 3022082WP BS 212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK CORROSION WAS FOUND ON SKIN DOUBLER AT Y12, X-1, Z-50. REMOVED CORRODED DOUBLER. INSTALLED NEW FINGER DOUBLER LONGERON IAW DC-9 SRM 53-02, 53-14-01, 51-10-03, 51-01, 51-30-02, 51-30-01, 53-34-00. TOTAL CYCLES 20,062. (W) 2L72 4F A6WE 19950320004961995032000496NE 1995 3 20 IXXA199519 219950306A7200 ENGINE DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 1 BIRD STIKE A IXXAA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL2341CX 46129 671275 ON DEPARTURE OUT OF DIEGO GARCIA, A SEA BIRD WAS OBSERVED TO ENTER THE NR 1 ENGINE, CAUSING SUBSTANTIAL FOREIGN OBJECT DAMAGE TO THE ENGINE GAS PATH. INGESTION OF THE SEA BIRD ALSO CAUSED DAMAGE TO THE NOSE COWL, BULLET, AND FAN DUCTS. THE AIRCRAFT RETURNED TO DIEGO GARCIA FOR MAINTENANCE, WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. ARRANGEMENTS WERE MADE TO REPLACE THE ENGINE AT THE LOCATION. 2L74 4F4 F 4A25 1E8 19950320004971995032000497WP 1995 3 20 WRLA95007 119950303A2430BD63 QUICK DISCONNECT DOUG DC10 DC1030F 3023504WP LT BATTERY LOOSE A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27107WA 46836 DURING CLIMB, CREW NOTICED THAT ALL CLOCKS STOPPED. INSPECTION OF BATTERY INDICATION BY THE FLIGHT CREW REVEALED NO VOLTS AND AMPS. THE PILOT IN COMMAND PULLED AND RESET BATTERY CHARGER CIRCUIT BREAKER AND VOLTS WENT TO 35 VOLTS AND NO AMPS, BUT THEN RETURNED TO ZERO VOLTS. THE ACFT DIVERTED TO AN ALTERNATE. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE DISCOVERED LT BATTERY DISCONNECT LOOSE. THE QUICK DISCONNECT WAS RESECURED AND SAFETIED. ALL CLOCKS WERE RESET, ALL OPS OK. ACFT RETURNED TO SERVICE. THIS INCIDENT IS UNDER INVESTIGATION. (W) 2L73 4F RTA22WE 19950320004981995032000498NM 1995 3 20 9503802705 119950310A5320 SHEAR TIE BOEING727 727225 1384077NM FS 950 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 22433 DURING PCK, MAINTENACE FOUND AFT CARGO BILGE FS 950B, BETWEEN STR 29L - 29R STEAR TIE CORRODED. REPAIRED PER SRM 53-10-4 PG 43 AND NWA EA 27-096481. 2L73 4F A3WE 19950320004991995032000499NM 1995 3 20 9503812705 119950310A5530 LONGERON BOEING727 727225 1384077NM VERT STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 22433 DURING PCK, MAINTENANCE FOUND VERTICAL STABILIZER, FIN STA 157.2, STR 7 LEFT CRACKED. REPAIRED PER NWA EA 27096482. 2L73 4F A3WE 19950320005001995032000500NM 1995 3 20 9503822705 119950215A524165569923 FRAME BOEING727 727225 1384077NM LT SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 3803 22433 DURING PCK, REMOVED AFT LEFT SERVICE DOOR FOR RESTORATION. SHOP FOUND FORWARD FRAME CRACKED AT UPPER HINGE CUT-OUT. REPAIRED PER COMPONENT MAINTENANCE MANUAL AND NWA EA 27-096700. 2L73 4F A3WE 19950320005011995032000501NM 1995 3 20 9503832705 119950215A524165569924 FRAME BOEING727 727225 1384077NM RT SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 4024 22433 DURING PCK, REMOVED AFT RIGHT SERVICE DOOR FOR RESTORATION. SHOP FOUND FORWARD FRAME CRACKED. REPAIRED PER SHOP COMPONENT MAINTENANCE MANUAL AND NWA EA 27-096699. 2L73 4F A3WE 19950320005021995032000502NM 1995 3 20 9503842285 119950313A2932ST7R TRANSMITTER BOEING727 727251 138408HNM A HYD SYST LEAKING A NWAAH DEACTIVATE SYST/CIRCUITS JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL01285US3688 820 21324 DURING FLIGHT, 'A' SYSTEM HYDRAULIC QUANTITY DECREASING. ONCE QUANTITY DECREASED TO 2.5 GALS, 'A' SYSTEM PUMPS DEACTIVATED, FLUID SHUTOFF VALVES CLOSED AND AFFECTED FLIGHT CONTROL SYSTEM SWITCHES TURNED OFF. QUANTITY STABILIZED AT 2.2 GALS. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 'A' SYSTEM HYDRAULIC PRESSURE TRANSMITTER. OPERATIONAL AND LEAK CHECK NORMAL. 2L73 4F A3WE 19950320005031995032000503NM 1995 3 20 95FDEA00229 119950310A5313BAC1493412 STRINGER BOEING727 72722 1384002NM BS 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 BS 500 WL 190 STR 19R STR IS GOUGED ON LOWER SIDE CHANNEL. REMOVED GOUGED STR 19 BS 500 WL 190 AND INSTALLED NEW STR PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950320005041995032000504NM 1995 3 20 95FDEA00230 119950312A53117075T6 FRAME BOEING727 72722 1384002NM BS 970 DOUBLE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 AT BS 970 STR 27R WL 157 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 970 STR 27R WL 157 PER FEDEX 51-40-3. 2L73 4F A3WE 19950320005051995032000505NM 1995 3 20 95FDEA00231 119950310A53117075T6 FRAME BOEING727 72722 1384002NM BS 990 DOUBLE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 AT BS 990 STR 27R WL 148 THERE IS A DOUBLE HOLE IN THE FRAME. REPAIRED FRAME AT BS 990 STR 27R WL 157 PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950320005061995032000506NM 1995 3 20 95FDEA00232 119950310A534710309430 SEAT TRACK BOEING727 72722 1384002NM COCKPIT WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 F/E'S AFT SEAT TRACK IS WORN. REMOVED AND REPLACED F/E'S AFT SEAT TRACK. 2L73 4F A3WE 19950320005071995032000507NM 1995 3 20 95FDEA00233 119950310A532069144691 CLIP BOEING727 72722 1384002NM BS 870 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CRACK AND OR HOLE DAMAGE IN LEFT BS 870 TERMINAL FITTING ROW 1 HOLE NR 1. DETERMINED BY HFEC THAT DAMAGE TO FRAME TO STRINGER CLIP TO BE MECHANICAL TOOLING DAMAGE. REMOVED AND REPLACED CLIP. 2L73 4F A3WE 19950320005081995032000508NM 1995 3 20 95FDEA00234 119950310A53122024T3080 BULKHEAD BOEING727 72722 1384002NM BS 950 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 DENT IN PRESSURE BULKHEAD BS 950 RBL 23 WL 153. REPAIRED DENT IN BS 950 CENTER BULKHEAD AT RBL 23 WL 153 PER FEDEX SRM 53-10-9 FIG 4. 2L73 4F A3WE 19950320005091995032000509NM 1995 3 20 95FDEA00235 119950310A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 870 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION ON SEAT TRACK BS 870 RBL 25 WL 208 OUT OF LIMITS PER SRM 51-10-01 1 INCH BY 1 INCH BY .035 ORIGINAL THICKNESS .090. REMOVED AND REPLACED SEAT TRACK BS 870-960 RBL 25 WL 208, EXISTING FACTORY SPLICE BS 870-960 RBL 25 WL 208. 2L73 4F A3WE 19950320005101995032000510NM 1995 3 20 95FDEA00236 119950310A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 344-350 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (72C235-02) ON SEAT TRACK BS 344-350 RBL 25. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-1. 2L73 4F A3WE 19950320005111995032000511NM 1995 3 20 95FDEA00237 119950310A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 470-484 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION ON SEAT TRACK BS 470-484 LBL 45 WL 208. REPLACED SEAT TRACK FROM BS 480-510 LBL 45 WL 208 AND CLEANED CORROSION ON TRACK FLANGE AT BS 470 PER FEDEX SRM 53-10-5. 2L73 4F A3WE 19950320005121995032000512NM 1995 3 20 95FDEA00238 119950310A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION ON SEAT TRACK BS 480 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480-510 RBL 25 WL 208. 2L73 4F A3WE 19950320005131995032000513NM 1995 3 20 95FDEA00239 119950310A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (72C235-02) ON SEAT TRACK BS 740 LBL 25. CORROSION FOUND TO BE OUT OT LIMITS, REMOVED AND REPLACED SEAT TRACK FROM BS 710-740 IAW SRM 53-10-5. 2L73 4F A3WE 19950320005141995032000514NM 1995 3 20 95FDEA00240 119950310A5315 FLOOR BEAM BOEING727 72722 1384002NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (72C235-2) ON 344 FLOOR BEAM RBL 15 WL 208 UNDER NUTPLATE HOLE. CORROSION PERMIATED THROUGH BEAM AND HAT CHANNEL OUT OF LIMITS PER FEDEX SRM 53-10-1 REMOVED, FABRICATED AND INSTALLED TOP CHORD OF FLOORBEAM BS 344 BLO TO RBL 60 IN IAW FEDEX SR 27-53-007. REMOVED AND REPLACED HAT CHANNEL UNDER LAV WALL. 2L73 4F A3WE 19950320005151995032000515NM 1995 3 20 95FDEA00241 119950310A53137075T6040 STRINGER BOEING727 72722 1384002NM BS 420 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 STR 25R IS CRACKED AT BS 420. REPAIRED STR 25R AT BS 420 IAW SRM 53-10-3 FIG 1 DETAIL II. 2L73 4F A3WE 19950320005161995032000516NM 1995 3 20 95FDEA00242 119950310A5313BAC1498141 STRINGER BOEING727 72722 1384002NM BS 1150-1160 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 CORROSION (72C237-02) ON STRINGER AT BS 1150-1160 STR 7L. FOUND CORROSION TO BE OUT OF LIMITS. REPAIRED STR AT BS 1150-1160 IAW SRM 53-10-3 AND 51-40-3. 2L73 4F A3WE 19950320005171995032000517NM 1995 3 20 95FDEA00243 119950310A531369163831 STRINGER TIE BOEING727 72722 1384002NM BS 680 CRACKED A FDEAO OTHER O OTHER ININSP/MAINT 1 SO25190FE 19083 FRAME TO STRINGER TIE CRACKED AT BS 680 STR 11L. REMOVED, FABRICATED AND REPLACED STR TIE AT BS 680 STR 11L. 2L73 4F A3WE 19950320005181995032000518NM 1995 3 20 95FDEA00244 119950310A53117075T6 FRAME BOEING727 72722 1384002NM BS 680 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 GOUGE ON FRAME AT BS 680 STR 14L. REMOVED AND REPLACED DAMAGED AREA PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950320005191995032000519NM 1995 3 20 95FDEA00245 119950310A5543651648210 FITTING BOEING727 72722 1384002NM RUDDER TAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04190FE 19083 UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED CRACKED UPPER RUDDER TAB ACTUATING ROD SUPPORT FITTING. 2L73 4F A3WE 19950320005201995032000520NM 1995 3 20 95FDEA00246 119950315A793356B17C OIL TEMP BULB BOEING727 7272S2F 1384O81NM NR 2 ENG FAILED A FDEAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO04206FE 22928 NR 2 ENG OIL TEMP IND 150 AFTER TAKEOFF WE REDUCED PWR TO 1.43 75 PERCENT N1, 350 EGT 82 N2. AFTER 15 MIN ENG OIL TEMP 140. ENG SHUTDOWN WAS ACCOMPLISHED IAW. CHECKLIST. AFTER PWR REDUCTION CSD TEMP DECREASED FROM 118 TO 80 DEG CELSIUS. REMOVED AND REPLACED NR 2 ENG OIL TEMP BULB AS PER MM 79-34-21. RAN NR 2 ENG AS PER JRH OPS CK GOOD. ALSO, SERVICED NR 2 CSD AND NR 2 ENG OIL. 2L73 4F A3WE 19950320005211995032000521WP 1995 3 20 ABXA9500181 119950116A561056441611 RETAINER DOUG DC9 DC932 3022066WP FS 120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE CAPTAIN'S CLEARVIEW WINDOW RETAINER. REPAIRED RETAINER IAW ABX REA D953-10757-MR. 2L72 4F A6WE 19950320005221995032000522WP 1995 3 20 ABXA9500182 119950103A5315991556141 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH EA FS533747, FOUND A FLOOR BEAM UPPER CAP AND WEB CORRODED AT FS 996 BETWEEN RBL 47 AND LBL 47. REPLACED UPPER FRAME CAP AND REPAIRED WEB IAW ABX REA D953-10666-MR. 2L72 4F A6WE 19950320005231995032000523WP 1995 3 20 ABXA9500183 119950210A53305911407503 SKIN DOUG DC9 DC932 3022066WP FS 218-256 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FORWARD FUSELAGE SKIN HAD CORROSION AND A PREVIOUS REPAIR THAT WAS NOT IAW THE SRM, FROM FS 218 TO 256 AND BETWEEN LONGERON'S 14 AND 16 RIGHT. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10849-MR. 2L72 4F A6WE 19950320005241995032000524WP 1995 3 20 ABXA9500184 119950130A573059127371 PANEL DOUG DC9 DC932 3022066WP WS 414 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION AND DELAMINATION ON THE LEFT WING TRAILING EDGE BONDED PANEL JUST FORWARD OF LEFT AILERON. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 19950320005251995032000525WP 1995 3 20 ABXA9500185 119950130A57115900301501 SPAR CAP DOUG DC9 DC932 3022066WP WS 509-563 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER TEE CAP FROM XRS 509 TO XRS 563. REPAIRED RIGHT WING REAR SPAR IAW ABX REA D957-10641-MR. 2L72 4F A6WE 19950320005261995032000526WP 1995 3 20 ABXA9500186 119950207A5311991184157 FRAME DOUG DC9 DC932 3022066WP FS 1089 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME TEE AT FS 1089 BETWEEN LONGERON 11 AND 12 LEFT. REPAIRED TEE IAW ABX REA D953-10888-MR. 2L72 4F A6WE 19950320005271995032000527WP 1995 3 20 ABXA9500187 119950204A5311991960317 FRAME DOUG DC9 DC932 3022066WP FS 1121 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT FS 1121, UPPER PORTION OF -17 FRAME BETWEEN LONGERON 29 LEFT TO 29 RIGHT. REPAIRED FUSELAGE FRAME IAW ABX REA D953-10916-MR. 2L72 4F A6WE 19950320005281995032000528WP 1995 3 20 ABXA9500188 119950105A57115911300501 SPAR CAP DOUG DC9 DC932 3022066WP WS 515 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION BLEND OUT THAT EXCEEDED THE SRM LIMITS. LEFT WING REAR SPAR AT APPROXIMATELY WING STATION XRS 515. REPAIRED LEFT WING REAR SPAR TEE CAP IAW ABX REA D957-10701-MR. 2L72 4F A6WE 19950320005291995032000529WP 1995 3 20 ABXA9500189 119950130A57115911301501 SPAR CAP DOUG DC9 DC932 3022066WP WS 494.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR TEE CAP AT STATION XRS 494.5. REPAIRED LEFT WING LOWER SPAR CAP IAW ABX REA D957-10793-MR. 2L72 4F A6WE 19950320005301995032000530WP 1995 3 20 ABXA9500190 119950110A53205911418122 ANGLE DOUG DC9 DC932 3022066WP FS 604 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD END OF THE CANTED KEEL ATTACH ANGLE HAD CORROSION REMOVAL THROUGH TWO FASTENER HOLES. REPAIRED CANTED KEEL ATTACH ANGLE IAW ABX REA D953-10752-MR. 2L72 4F A6WE 19950320005331995032000533WP 1995 3 20 ABXA9500193 119950128A5315991224359 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 965 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FLOOR BEAM AT FS 965 AT RBL 22. REPAIRED FLOOR BEAM IAW ABX REA D953-10811-MR. 2L72 4F A6WE 19950320005361995032000536WP 1995 3 20 ABXA9500196 119950118A57115911301502 SPAR CAP DOUG DC9 DC932 3022066WP WS 387-395 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP BETWEEN XRS 387 AND XRS 395. REPAIRED RIGHT WING REAR LOWER SPAR CAP IAW ABX REA D957-10715-MR. 2L72 4F A6WE 19950320005371995032000537WP 1995 3 20 ABXA9500197 119950126A5310591142841 SKIN DOUG DC9 DC932 3022066WP FS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON A SKIN REPAIR ON AFT FUSELAGE SKIN FROM FS 996 TO FS 1034 AT LONGERON 23 LEFT. REPAIRED AFT FUSELAGE SKIN IAW ABX REA D953-10834-MR. 2L72 4F A6WE 19950320005381995032000538WP 1995 3 20 ABXA9500198 119950201A575559205212 PANEL DOUG DC9 DC932 3022066WP WS 164 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND DELAMINATION ON THE RIGHT WING INBOARD GROUND SPOILER PANEL. REPLACED PANEL IAW DC-9 M.M. 27-62-1. 2L72 4F A6WE 19950320005391995032000539WP 1995 3 20 ABXA9500199 119950113A57115911301501 SPAR DOUG DC9 DC932 3022066WP WS 488-520 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR FROM STATION XRS 488 TO XRS 520. REPAIRED LEFT WING LOWER REAR SPAR IAW ABX REA D957-10692-MR. 2L72 4F A6WE 19950320005401995032000540 1995 3 20 ABXA9500200 419950315A342136143091006 DISPLAY UNIT DOUG DC8 DC863 302198AWP LT COCKPIT FAILED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23824AX2531 697 46141 DURING PREFLIGHT, FOUND THE CAPTAINS DU NR 2 DISPLAYING THE SG FLAG AND EMITTING A BURNING ODOR. NOT VERIFIED. REMOVED AND REPLACED THE CAPTAINS NR 2 DU AS A PRECAUTIONARY MEASURE. SYSTEMS OPS CHECKED GOOD IAW SUPP MM CHAPTER 34. 2L74 4F 4A25 19950320005411995032000541WP 1995 3 20 ABXA9500201 119950123A53302024T42 SKIN DOUG DC9 DC932 3022066WP FS 120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON FUSELAGE SKIN FORWARD OF E AND E COMPARTMENT ENTRY DOOR BETWEEN LONGERON 28 RIGHT AND 29 RIGHT. REPAIRED IAW DC-9 SRM CHAPTER 53-01, FIGURE 4, SHEET 3. 2L72 4F A6WE 19950320005421995032000542WP 1995 3 20 ABXA9500202 119950202A531327779223 LONGERON DOUG DC9 DC932 3022066WP FS 333 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 27, RIGHT LOWER SURFACE, AFT OF FS 333. REPLACED LONGERON 27 RIGHT IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320005431995032000543WP 1995 3 20 ABXA9500203 119950216A532099196503 DOOR JAMB DOUG DC9 DC932 3022066WP FS 370-427 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FORWARD LOWER CARGO COMPARTMENT DOOR JAMB AT LONGERON 29R FS 370 TO FS 427. REPLACED DOOR JAMB AND U-CHANNEL IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19950320005441995032000544WP 1995 3 20 ABXA9500204 119950127A53135920319501 LONGERON DOUG DC9 DC932 3022066WP FS 256-351 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29L CRACKED AFT OF STATION 256 AND 351. REPLACED LONGERON 29L FROM FS 237 TO FS 522 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950320005451995032000545WP 1995 3 20 ABXA9500205 119950207A531227779224 STIFFENER DOUG DC9 DC932 3022066WP FS 1089 BLKHD CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 11 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19950320005461995032000546WP 1995 3 20 ABXA9500206 119950207A53121475407 STIFFENER DOUG DC9 DC932 3022066WP FS 1089 BLKHD CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 8 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19950320005471995032000547WP 1995 3 20 ABXA9500207 119950207A531227779224 STIFFENER DOUG DC9 DC932 3022066WP FS 1089 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47084 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LEVEL II CORROSION ON STIFFENER ON AFT FACE OF CANTED BULKHEAD 1089 AT LONGERON 6 LEFT. REPLACED STIFFENER IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19950320005491995032000549SO 1995 3 20 BIER950006 119950227A2434401424 BOLT PIPER PA28 PA28236 7102815SO LYC O540 O540* 41532EA ALTERNATOR MOUNTWORN A BIEAK NONE P NO WARNING INDICATION ININSP/MAINT 1 EA21435951100 288411018 L23759 DURING MAINTENANCE FOR UNRELATED ALTERNATOR PROBLEM, FOUND TOP ALTERNATOR BOLT (PN 401 424) WORN APPROX 20 PERCENT THROUGH. HAVE SEEN THIS NUMEROUS TIMES BEFORE AND BELIEVE THIS TO BE CAUSED BY THE FRONT AND/OR REAR BUSHING(S) (PN 753 380) BECOMING LOOSE AND VIBRATING CAUSING THIS WEAR. BUSHING LOOSENESS COULD BE ATTRIBUTED TO IMPROPER INSTALLATION OF ALT IE, IMPROPER INSTALLATION OF WASHERS FOR SPACING. SUGGEST CLOSE INSP OF ALT INSTALL AND ATTACH HARDWARE AT NEXT INSP. 1L71 3O3 O 2A13 E295 19950320005501995032000550NE 1995 3 20 DL72E951053 219950308A7200JT8D15A ENGINE BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 3 FLAME OUT A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO11283WA49009 21485 695370 ON CLIMB THROUGH FL230 NR 3 ENGINE FLAMED OUT. OIL PRESSURE WENT TO ZERO. DID NOT ATTEMPT RESTART. REMOVED ENGINE ROUTED TO SHOP. INITIAL INDICATIONS SHOW ENGINE SEIZED, UNABLE TO ROTATE. 2L73 4F4 F A3WE E2EA 19950320005511995032000551NM 1995 3 20 DL73S951091 119950313A56105893543110RPR WINDSHIELD BOEING737 737232 1384475NM FLIGHT DECK R-1 FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11332DL 23104 DURING CRUISE, HEARD BURNING NOISE AND HAS ACRID SMELL IN FLT DECK, THEN HAD SMOKE AT R-1 WINDOW TERMINAL BLOCK, LANDED BNA, FOUND R-1 WINDOW TERMINAL BURNED. RELACED R-1 WINDOW, CONTROLLER AND CIRCUIT BREAKER. OPERATION NORMAL. 2L72 4F RTA16WE 19950320005521995032000552NM 1995 3 20 DL757951093 119950313A3610 PNEUMATIC SYSTEM BOEING757 757232 1384965NM AC COMP CONTANIMATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11636DL 23763 SHORTLY AFTER TAKEOFF HAD SMOKE AND ODOR ENTER CABIN. RETURNED ATL. FOUND PNEUMATIC SYSTEM CONTANIMATED. A WATER BASED SOLUTION WAS DRAINED FROM GROUND AIR CONNECTION. RAN BOTH ENGINES AND PACKS AFTER 1 HOUR HAD NO ODOR. RETURNED TO SERVICE. 2L72 4F RTA2NM 19950320005531995032000553WP 1995 3 20 DLL14951052 119950312A2750472086119 TRANSDUCER LKHEED1011 1011385115 5265015WP LEFT WING FAILED A DALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SO11737D 193C1228 ON APPROACH AT FLAP EXTENSION. GOT A FLAP/SLAT LOCK LIGHT. HAD FULL SLATS AND LESS THAT 4 DEGREES OF FLAPS. FOUND LEFT FLAP TRANSDUCER FAULTY. REPLACED TRANSDUCER OPERATION NORMAL. 2L73 4F A23WE 19950320005541995032000554NM 1995 3 20 DLM88951051 119950312A2910AE7055381 HYD LINE DOUG MD88 MD88 3023688NM RT FIREWALL LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11971DL 53214 DURING CLIMB THROUGH FL270 LOST RIGHT SYSTEM FLUID AND PRESSURE. LANDED ATL. FOUND RIGHT ENGINE PRESSURE LINE THROUGH FIRE WALL LEAKING. REPLACED LINE OPERATION NORMAL. 2L72 4F RTA6WE 19950320005551995032000555NM 1995 3 20 QXEA9500074 119950313A3350 COVER DHAV DHC8 DHC8102 2809003NM CABIN FLASHLIGHTBROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09831PH 328 THE FLIGHT ATTENDANT EMERGENCY FLASH LIGHT, EMERGENCY USE ONLY COVER IS BROKEN. REPLACED THE COVER ON THE FLASHLIGHT AND THE A/C WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950320005561995032000556SW 1995 3 20 QXEA9500075 119950313A326027520200003 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG BROKEN A QXEAK NONE P NO WARNING INDICATION APAPPROACH 1 NM093116Z AC598 THE NOSE GEAR RED INTRANSIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE NOSE GEAR UP POSITION SWITCH. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T A8SW 19950320005571995032000557NM 1995 3 20 QXEA9500076 119950313A2120 CIRCUIT BREAKER DORNERDO32 DO328100 2996000NM COCKPIT TRIPPED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09335PH 3013 THE HX FAN CIRCUIT BREAKER TRIPPED WITH SMOKE IN THE COCKPIT. RESET THE HX CIRCUIT BREAKER AND THE FAN OPERATIONAL CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19950320005581995032000558NM 1995 3 20 SCNA95036 119950313A5241 R2 DOOR BOEING727 727259 138408JNM AFT GALLEY OUT OF RIG A SCNAD RETURN TO BLOCK O OTHER CLCLIMB 1 GL15289SC 22475 AFTER DEPARTING LAS A SUBSTANTIAL AIR LEAK IN RIGHT AFT GALLEY DOOR WAS DETECTED, AND AIRCRAFT WOULD NOT PRESSURIZE PROPERLY ON CLIMB-OUT. FOUND R2 DOOR NOT CLOSED PROPERLY, FORWARD LOBE NOT IN TRACK. RECLOSED DOOR AND OPS CHECKED GOOD. 2L73 4F A3WE 19950320005591995032000559NM 1995 3 20 SCNA95037 119950314A33501102833 EEL BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 AFT OVERHEAD SELF-CONTAINED EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD IAW 33-50-01. 2L73 4F RTA3WE 19950320005611995032000561EU 1995 3 20 95ZZZX1230 119950211A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU AVIONICS BAY DIRTY A NVEAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO03253AE 340B253 PIT - FLT 4914 - CREW REPORT AVIONICS SMOKE LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT LANDED AND RETURNED TO ITS GATE WITHOUT FURTHER INCIDENT. INSPECTED AVIONICS BAY AND FOUND NO EVIDENCE OF A FIRE. CLEANED SMOKE DETECTOR AND RETURNED TO SERVICE. 2L72 4T RTA52EU 19950320005621995032000562WP 1995 3 20 95ZZZX1231 119950104A5320 BELT RING DOUG DC9 DC951 3022051WP FS 1212.809 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05410EA 47731 STL - DURING CHECK-C, FOUND .25 INCH CRACK IN BELT RING, IN TAIL COMPARTMENT, STA 1212.809, LONGERON 6L, 6R, 5R, 5L, 4R, AND 4L. REPLACED BELT RING PER SRM 51-10-4 AND SRM 51-30-0. AIRCRAFT TOTAL TIME: 38,988 HOURS, 35,341 CYCLES. 2L72 4F A6WE 19950320005631995032000563NE 1995 3 20 95ZZZX1233 219950210A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 FLAMED OUT A P5CAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 WP23853FT 19753 685903 JUST PRIOR TO DESCENT INTO MIA AT FL 390, THE NR 4 ENGINE FLAMED OUT. THE ENGINE SHUT-DOWN CHECK LIST WAS COMPLETED AND THE IN-FLIGHT ENGINE START CHECK LIST WAS COMPLETED. THE FUEL FLOW INDICATED 3-400 POUNDS PER HOUR. ON THE FIRST TWO ATTEMPTS, THE FUEL FLOW DID NOT INCREASE, BUT EGT INCREASED WITH NO INCREASE IN N1 OR N2. ON THE THIRD ATTEMPT, AT APPROXIMATELY FL 320 AND 280 KNOTS, ENGINE RESTARTED. A NORMAL DESCENT AND APPROACH WAS MADE AT MIA. REPLACED NR 4 ENGINE FUEL FILTER, BOTH IGNITERS AND SUMPED ALL FUEL TANKS. ENGINE R/U NORMAL. 2L74 4F4 F A20WE E20EA 19950320005661995032000566EU 1995 3 20 95ZZZX1236 119950218A3213200920004 SHOCK ABSORBER ROTOL STBROSSD3 SD360 8100606EU RT MLG BROKEN A ATRBAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO21376MQ21551 DRG330085 SH3685 DURING LANDING, NO GEAR INDICATION FOR RT MLG, LOW PASS C/W OVER TOWER FOUND THAT GEARS WERE DOWN. NORMAL LANDING PROCEDURE WAS CARRIED OUT. DURING TOUCH-DOWN ON RUNWAY, RT GEAR COLLAPSED. FOUND SHOCK ABSORBER BROKE THE RETAINING JAM NUT CAUSING CYLINDER TO SEPARATE FROM THE BODY. AIRCRAFT SUFFERED MINOR DAMAGE, WHEEL AND BRAKE WERE REPLACED. SHOCK ABSORBER WAS REMOVED AND REPLACED. TO BE SENT FOR METAL TEST EVALUATION. 2H72 4T A41EU 19950320005671995032000567WP 1995 3 20 95ZZZX1237 119950216A21701808492 COALESCER BAG DOUG DC9 DC951 3022051WP LEFT PACK DIRTY A A4JAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO15919PJ 47663 FLT 807 - LEFT PACK TRIPPED IN FLIGHT AND CABIN ATTENDANT REPORTED SMOKE IN CABIN. SMOKE WAS ALSO EVIDENT IN COCKPIT. LEFT PACK WAS TURNED OFF AND SMOKE DECREASED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT ILG (DIVERTED). INSPECTED TAIL COMPARTMENT FOR EVIDENCE OF HEAT DAMAGE. NONE FOUND. REPLACED WATER SEPARATOR BAG. OPERATION OF PACK NORMAL AND ACFT RETURNED TO SERVICE. 2L72 4F A6WE 19950320005681995032000568NM 1995 3 20 95ZZZX1238 119950130A3020 PRESSURE SWITCH 851003B DORNERDO32 DO328100 2996000NM LT ENGINE FAILED A EQGAK NONE N FALSE WARNING CRCRUISE 1 SW19328LS 0322 3025 LEFT INTAKE DEICE BOOT FAILURE APPEARED ON THE ANNUNCIATOR. HOWEVER, ALL BOOTS FUNCTIONED PROPERLY. AFTER TROUBLESHOOTING, DETERMINED THAT AN INTERNAL PRESSURE SENSING SWITCH FAILED CAUSING ERRONOUS READING. REPLACED EJECTOR FLOW CONTROL VALVE. 2H72 4T RTA45NM 19950320005721995032000572SW 1995 3 20 95ZZZX1242 119950119A243503601014 BEARING 23079010 FRCHLDSA227 SA227DC 3377521SW STARTER/GEN FAILED A EQGAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW193025B721 676 92200 DC850B BEARING/ PN 03-6010-14, FAILED. GENERATOR FELL OFF LINE IN FLIGHT AND WOULD NOT RESET. 1L72 4T RTA18SW 19950320005781995032000578CE 1995 3 20 95ZZZX1248 119950114A5711 SPAR CESSNA402 402B 207590PCE WS 119.29-133.29CORROSION A FAHAK NONE O OTHER ININSP/MAINT 1 SO193945C 402B0822 SEVERE CORROSION ON REAR SPAR RT WING AT AFT END OF NACELLE. THIS REPAIR REQUIRED A DER AND 337 FOR MAJOR REPAIR AT WS 119.29 - WS 133.29 AND 8110-3. 1L72 3O A7CE 19950320005801995032000580NM 1995 3 20 AALA950124 119950126A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07695AN 26975 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 5 AND 17 FOUND INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT AT ROW 5. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950320005811995032000581EU 1995 3 20 AALA950135 119950130A5330 SKIN FOKKERF28 F28MK0100 4990807EU FS 22706 DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW071458H 11478 TULE - LIGHTING BURN AND MISDRILLED HOLE IN FUSELAGE SKIN STA 22706 AT STR 2. INSTALLED DOUBLER ON FUSELAGE SKIN PER SRM 53-00-02, FIGURE 203, AND ON STRINGER PER ESO 51000 DATED 1-26-95. CYCLES, 2193, T.S.T. 2964. (X) 2L72 4F RT 19950320005821995032000582EU 1995 3 20 AALA950139 119950130A5753 SKIN FOKKERF28 F28MK0100 4990807EU TE FLAP VANE GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW071458H 11478 TULE - DEEP GOUGE IN TOP SKIN OF INBOARD LT FLAP VANE OUTBOARD OF INBOARD ACCESS COVER. REPAIRED DAMAGE BY BLENDING GOUGED AREA AND INSTALLATION DOUBLER PER ESO 51000, DATED 1-26-95. (X) 2L72 4F RT 19950320005831995032000583NM 1995 3 20 AALA950169 119950201A3350 EEL WIRE BOEING757 757223 1384957NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07686AA 25343 DFW - DURING OVERNIGHT, MAINTENANCE FOUND EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FIRST CLASS COFFEE BAR INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950320005841995032000584NM 1995 3 20 AWXA9500068 119950126A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 15. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950320005851995032000585NM 1995 3 20 CAL950088 119950205A3230 CIRCUIT BREAKER BOEING737 737524 1384721NM LANDING GEAR TRIPPED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0917619 27332 ELP - FLT 1684 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO ELP. MAINTENANCE FOUND THE LANDING GEAR LEVER LATCH AND PRESSURE WARNING CIRCUIT BREAKER TRIPPED. THE CIRCUIT BREAKER AS RESET. OPERATION OF THE LANDING GEAR HANDLE CHECKED NORMAL IAW MM 32-31-00, PAGE 501. (X) 2L72 4F RTA16WE 19950320005861995032000586NM 1995 3 20 PCAA9500192 119950126A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13827EX 390 AFTER TAKEOFF, GEAR DID NOT RETRACT. INSPECTED AIRCRAFT, FOUND ALTERNATE RELEASE DOOR OPEN. RESET DOOR. OPS CHECK GOOD ON FLIGHT TEST. ACFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 559, AIRCRAFT TOTAL TIME 473. (X) 2H72 4T RTA13NM 19950320005911995032000591WP 1995 3 20 SCNA95003 119950101A3350110049 POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN EEL FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 2360 46946 MSP - AFT CABIN EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED AFT CABIN EMERGENCY FLOOR TRACK LIGHTING POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD PER MM. (X) 2L73 4F A22WE 19950320005921995032000592NM 1995 3 20 SCNA95004 119950103A3350 EEL TRACK BOEING727 727259 138408JNM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 MSP - AFT ONE-THIRD OF FLOOR TRACK LIGHTING (EMERGENCY) IS INOPERATIVE. FOUND FOURTH FROM THE AFT EMERGENCY LAMP SEGMENT SHORTED. REMOVED AND REPLACED SEGMENT AND TRACK COVERING. OPS CHECK GOOD PER MM 33-50-00. (X) 2L73 4F A3WE 19950320005931995032000593WP 1995 3 20 SCNA95007 119950105A3250ACG70111 COLLAR DOUG DC10 DC1010 3022110WP NLG STEERING DAMAGED A ASCNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15907WA ABS369 46946 MSP - FLT 29 - NOSE GEAR WOULD NOT RETRACT. AFTER LANDING, AIRCRAFT WAS DIFFICULT TO STEER LEFT. FOUND STEERING COLLAR, COLLAR, CYLINDER, AND CYLINDER ATTACH HARDWARE DAMAGED DUE TO 'EXCEEDING THE TOW LIMITS'. REPLACED STEERING COLLAR, COLLAR, BOTH STEERING CYLINDERS, ATTACH HARDWARE (INSPECTED CENTERING CAMS) AND PERFORMED STEERING FUNCTIONAL TEST AND GEAR SWING. (X) 2L73 4F A22WE 19950320005941995032000594WP 1995 3 20 SCNA95008 119950105A3397 WIRE DOUG DC10 DC1010 3022110WP L4 DOOR EEL BROKEN A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 MSP - DURING LINE CHECK, FOUND EMERGENCY LIGHT AT L4 DOOR BULKHEAD INOPERATIVE. CONFIRMED BROKEN WIRE UNDER STORAGE BIN AREA, REPOSITIONED WIRE, SPLICED WIRE CONNECTOR IN, OPERATION CHECK GOOD. (X) 2L73 4F A22WE 19950320005951995032000595NM 1995 3 20 SCNA95011 119950120A213039854021 AIR VALVE BOEING727 727259 138408JNM RIGHT PACK FAULTY A SCNAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15289SC P3678 22475 SLC - FLT 865 - ON CLIMB-OUT, FLIGHT ENGINEER UNABLE TO CONTROL CABIN IN AUTO, STANDBY, OR MANUAL (OUTFLOW VALVE IN FULL CLOSED POSITION WITH CABIN CLIMBING). FOUND RIGHT FORWARD PACK VALVE INOPERATIVE. REPLACED RIGHT FORWARD PACK VALVE AND RAN RIGHT PACK, OPERATIONS CHECKED NORMAL. ALSO PRESSURIZED AIRCRAFT ON GROUND AND FOUND NO AIR LEAKS. AIRCRAFT PRESSURIZED NORMALLY. (X) 2L73 4F A3WE 19950320005961995032000596WP 1995 3 20 SCNA95015 119950122A2920AJK7054521 HYD LINE DOUG DC10 DC1015 3022118WP NR 2 ENGINE LEAKING A SCNAK NONE K FLUID LOSS ININSP/MAINT 1 GL15151SY 48295 MSP - NR 2 HYDRAULIC SYSTEM PRESSURE LINE CHAFING WITH STANDBY RUDDER PRESSURE LINE CAUSING A LEAK BELOW NR 2 INLET DUCT. REPLACED BOTH LINES AND LEAK CHECKED GOOD. (X) 2L73 4F A22WE 19950320005971995032000597WP 1995 3 20 SCNA95017 119950201A3350EMB1392 POWER SUPPLY DOUG DC10 DC1010 3022110WP COCKPIT EEL FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 43611 46946 MSP - COCKPIT EMERGENCY LIGHT TEST FAILS. REMOVED AND REPLACED FORWARD CABIN OVERHEAD EMERGENCY LIGHT POWER SUPPLY AND SYSTEM PASSED TEST. (X) 2L73 4F A22WE 19950320005981995032000598WP 1995 3 20 SCNA95021 119950211A3350110049 EEL POWER PACK DOUG DC10 DC1015 3022118WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15151SY 9755 48295 MSP - FORWARD CABIN EMERGENCY TRACK LIGHTING INOPERATIVE IN BOTH AISLES. REMOVED AND REPLACED FORWARD SECTION BATTERY POWER PACK, SPLICED BROKEN WIRES, EMERGENCY FLOOR TRACK LIGHTING OPS CHECKED GOOD. (X) 2L73 4F A22WE 19950320005991995032000599EU 1995 3 20 SIMA950554 119950224A3350301210 EEL AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR INOP A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21428MQ 525 0128 MQT - DURING PS-2 CHECK, MAINTENANCE REPORTED THE EMERGENCY LIGHT IN THE PASSENGER/CREW DOOR WAS INOPERATIVE. EMERGENCY LIGHT ASSY WAS RAI'D AND AN OPERATIONAL CHECK WAS PERFORMED IAW ATR-42 J/C 33-50-00 OPT10000-002. ACFT WAS THEN RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950320006001995032000600 1995 3 20 SIMA950602 419950301A34177000700959 AIR DATA COMP AEROSPATR42 ATR42300 8680920EU LT COCKPIT FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21425MQ2306 87 047 MIA - FLT 3537 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. ACFT RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. MTX - REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. OPS CHECK GOOD AND ACFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES 2,402. (X) 2H72 4T RTA53EU 19950320006011995032000601EU 1995 3 20 VTZA95049 119950202A524614153133409 DOOR JETAIRJETSTMJETSTM4101 1500501EU LAV SERVICE FAILURE A AVTZAK NONE D INFLIGHT SEPARATION TOTAKEOFF 1 EA27317UE 41031 CHS/IAD - FLT 6417 - DURING TAKEOFF AT 1430 HRS ON 2-2-95, THE LAVATORY SERVICE DOOR SEPARATED FROM THE AIRCRAFT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17279 IAW CDL-52-40 ON THE LAV SERVICE DOOR. (X) 2L72 4T RTA41NM 19950320006021995032000602EU 1995 3 20 VTZA95052 119950210A524014153133409 DOOR JETAIRJETSTMJETSTM4101 1500501EU LAV SERVICE MISSING A VTZAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 EA27301UE 41012 BOS/IAD - FLT 6232 - UPON LANDING AT 1400 HRS ON 2-7-95, CREW NOTICED THE LAVATORY SERVICE DOOR WAS MISSING. MAINTENANCE OPENED DMI NR 02807 ON 2-7-95 IAW CDL 52-40 ON THE LAV SERVICE DOOR. MAINTENANCE LATER CLEARED DMI NR 02807 BY REPLACING THE LAV SERVICE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950320006031995032000603NE 1995 3 20 VTZA95055 219950210A72605725109162 CHIP DETECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE CONTAMINATED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27318UE 41041 P76062 IAD/MHT - FLT 6203 - DURING CLIMB AT 1245 HRS ON 2-10-95, RT ENGINE OIL CONTAMINATION CAPTION ILLUMINATED ON CLIMB-OUT, AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PULLED THE RT CHIP DETECTOR AND FOUND IT TO HAVE FLAKES OF METAL. CLEANED DETECTOR AND RAN ENGINE FOR 30 MINUTES. FIVE MINUTES AT 100 PERCENT, 25 MINUTES AT 80 PERCENT. TOOK SOAP SAMPLE, REPLACED OIL FILTER AND RAN AGAIN FOR 30 MINUTES. NO OIL CONTAMINATION LIGHT. PULLED AND INSPECTED RT CHIP DETECTOR, NO METAL FOUND. AIRCRAFT OKAY FOR CONTINUED SERVICE PER ALLIED SIGNAL SOAP SAMPLE RESULTS. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950320006041995032000604EU 1995 3 20 VTZA95060 119950215A261251653151 FIRE DET BAG JETSTMJETSTM3201 1500217EU LT ENGINE DIRTY A VTZAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27497UE 904 HPN/IAD - FLT 6946 - DURING TAXI AT 2100 HRS ON 2-15-95, LEFT ENGINE FIRE DETECT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE CANNON PLUG ON THE FIRE DETECTION BOX. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950320006051995032000605SO 1995 3 20 WTAA950095 119950223A3350D36604001 EEL BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAAK NONE L NO TEST NRNOT REPORTED 1 WP17279UE 120085 MRY - CREW REPORTED CABIN EMERGENCY LIGHTING PARTIALLY INOPERATIVE. DEFERRED CABIN EMERGENCY LIGHTING SYSTEM PER MEL 33-50-1. AIRCRAFT RESTRICTED TO DAY OPERATION ONLY. MAINTENANCE SUBSEQUENTLY REPLACED CENTER CABIN EMERGENCY LIGHT BATTERY PACK. CABIN EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006061995032000606SO 1995 3 20 WTAA950096 119950223A3260922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17280UE 120090 SFO - LT MLG RED INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED AND ADJUSTED LT MLG UPLOCK PROXIMITY SENSOR. LANDING GEAR OPERATION AND POSITION INDICATIONS NORMAL ON GROUND AND DURING SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006071995032000607SO 1995 3 20 WTAA950099 119950224A291012040345001 HYDRAULIC LINE EMB 120 EMB120RT SO NLG ACTUATOR LEAKING A WTAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP17122AM 120013 SFO - LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE REPORTED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE ON NOSE GEAR ACTUATOR LEAKING. REPLACED HYDRAULIC LINE. HYDRAULIC SYSTEM OPERATIONAL CHECK AND LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006081995032000608EU 1995 3 20 WTAA950100 119950224A3411AN8275D FITTING BAG JETSTMJETSTM3101 1500215EU COCKPIT LOOSE A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17429UE 807 SFO - AT 7,000 FEET, F/O'S ALTIMETER INDICATES 440 FEET LOWER THAN CAPTAIN'S ALTIMETER AND F/O'S AIRSPEED INDICATOR SHOWS 12 KIAS LESS THAN CAPTAIN'S INDICATOR. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND AIR LEAK IN STATIC SYSTEM. TIGHTENED B-NUT ON LINE CROSS FITTING BEHIND F/O'S INSTRUMENT PANEL. OPERATION CHECK AND LEAK CHECK OF NR 2 PITOT/STATIC SYSTEM SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320006091995032000609NE 1995 3 20 WTAA950101 219950225A7261 OIL SYSTEM EMB 120 EMB120RT SO PWA PW121 PW121 52124NE RT ENGINE REQ'D SERVICE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17285UE 120153 RDD - RIGHT ENGINE OIL PRESSURE REPORTED AT 50 PSI AFTER APPLICATION OF TAKEOFF POWER. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE AND DISCOVERED ENGINE OIL LEVEL LOW. SERVICED RIGHT ENGINE WITH OIL (7 QUARTS). PERFORMED ENGINE GROUND RUN. OIL PRESSURE INDICATION NORMAL. NO OIL LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950320006101995032000610NE 1995 3 20 WTAA950102 219950226A7261 OIL SYSTEM EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE REQ'D SERVICE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17276UE 120067 RDM - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE AND SERVICED WITH OIL (1 QUART). PERFORMED ENGINE GROUND RUN. OIL PRESSURE INDICATION NORMAL. NO OIL LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950320006111995032000611SO 1995 3 20 WTAA950103 119950227A2930MS3476L10SW CONNECTOR EMB 120 EMB120RT SO BLUE HYD SYST CONTAMINATED A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17451UE 120108 RDM - AFTER TAKEOFF, CREW REPORTED BLUE HYDRAULIC SYSTEM QUANTITY INDICATION FLUCTUATING. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLUE SYSTEM HYDRAULIC QUANTITY INDICATION SYSTEM. CLEANED CONNECTOR ON BLUE SYSTEM HYDRAULIC QUANTITY SENDING UNIT. QUANTITY INDICATION SYSTEM INDICATES NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006121995032000612NE 1995 3 20 WTAA950104 219950225A7310AS3209009 O-RINGS EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A AWTAACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 WP17201YW 120201 SBP - RT ENGINE AUTOFEATHER SYSTEM ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. FOLLOWING ABORTED TAKEOFF, RT ENGINE LOW OIL PRESSURE INDICATION RECEIVED. CREW SECURED RT ENGINE. MAINTENANCE INSPECTED RT ENGINE AND FOUND FUEL LEAK AT FUEL TRANSFER TUBE O-RINGS TO BE CAUSE OF ENGINE LOSS OF POWER. REPLACED RT ENGINE FUEL TRANSFER TUBE O-RINGS. PERFORMED ENGINE GROUND RUNS. ENGINE OPERATION AND OIL PRESSURE INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950320006131995032000613SO 1995 3 20 WTAA950105 119950226A3350D36604001 EEL BATTERY PACK EMB 120 EMB120RT SO FWD CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17455UE 120163 FAT - FORWARD CABIN FLOOR TRACK EMERGENCY EXIT LIGHTS REPORTED INOPERATIVE DURING GROUND TEST MAINTENANCE REPLACED FORWARD EMERGENCY LIGHTING SYSTEM BATTERY PACK. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006141995032000614SO 1995 3 20 WTAA950106 119950226A528012012347001 HANDLE ASSY EMB 120 EMB120RT SO LT MLG DOOR WORN A WTAAK NONE J WARNING INDICATION TOTAKEOFF 1 WP17268UE 120207 RNO - LEFT MLG DOOR WILL NOT CLOSE DURING GEAR RETRACTION. MAINTENANCE REMOVED AND REPLACED LT MLG OUTBOARD DOOR HANDLE ASSY. GEAR DOOR OPERATION NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006151995032000615SO 1995 3 20 WTAA950107 119950228A2422 INVERTER EMB 120 EMB120RT SO AC GEN SYST MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17286UE 120175 SFO - LEFT INVERTER FELL OFF LINE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE CYCLED INVERTER OFF AND ON NUMEROUS TIMES. UNABLE TO DUPLICATE DISCREPANCY. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950320006161995032000616EU 1995 3 20 WTAA950109 119950302A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 WP17417UE 794 STS - CREW REPORTED BIRD STRIKE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AREA. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950320006181995032000618NM 1995 3 20 ASAA9510004 119950224A5511 SPAR BOEING737 737210C 1384459NM LT HORIZ STAB CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, THE LEFT HORIZONTAL STABILIZER REAR SPAR UPPER LUG WAS FOUND CORRODED AND A CRACK WAS DETECTED IN THE BORE OF THE UPPER LUG. REPAIRED PER EA 5510-01026 AND BOEING TELEX ASA-SEA-950082RR. (Z) 2L72 4F A16WE 19950320006191995032000619NM 1995 3 20 ASAA9510005 119950224A5315 FLOOR BEAM BOEING737 737210C 1384459NM BS 685 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, THE LONGITUDINAL FLOOR BEAM AT RBL 45.5 BETWEEN BS 670 AND 690 AND WAS FOUND CORRODED IN SEVERAL LOCATIONS. REPAIRED PER EA 5310-01329 AND BOEING TELEX ASA-SEA-95-0094RR. (Z) 2L72 4F A16WE 19950320006201995032000620NM 1995 3 20 ASAA9510006 119950224A5312 BULKHEAD BOEING737 737210C 1384459NM BS 727 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, THE LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, LBL 27 AND 38 WAS FOUND CRACKED. REPAIRED PER EA 5310-01325 AND BOEING TELEX ASA-SEA-95-0111RR. (Z) 2L72 4F A16WE 19950320006211995032000621NM 1995 3 20 ASAA9510007 119950224A5312 BULKHEAD BOEING737 737210C 1384459NM BS 727 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, LOWER OUTBOARD CHORD OF BS 727 BULKHEAD, RBL 38 AND 27 WAS FOUND CRACKED. REPAIRED PER EA 5310-01326 AND BOEING TELEX ASA-SEA-95-0111RR. (Z) 2L72 4F A16WE 19950320006221995032000622NM 1995 3 20 ASAA9510008 119950224A5315 FLOOR BEAM BOEING737 737210C 1384459NM BS 727B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, FLOOR BEAM AT BS 727B WAS FOUND TO BE CORRODED ON THE UPPER CHORD FLANGES. REPAIRED PER EA 5310-01323 AND BOEING TELEX ASA-SEA-95-0098RR. (Z) 2L72 4F A16WE 19950320006231995032000623WP 1995 3 20 ASAA9580002 119950217A5210 DOOR HANDLE DOUG DC9 DC982 3022082WP FWD ENTRY DOOR OUT OF SEQUENCE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01931AS 49232 ONT - PRIOR TO DEPARTURE OF FLIGHT 383 CREW REPORTED THE FORWARD ENTRY DOOR WOULD NOT LATCH PROPERLY. CYCLED DOOR HANDLE AND OPERATED NORMALLY. (Z) 2L72 4F A6WE 19950320006241995032000624WP 1995 3 20 ASAA9580004 119950217A5210 DOOR DOUG DC9 DC982 3022082WP FWD ENTRY DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PDX - DURING MAINTENANCE, THE FORWARD ENTRY DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. ADJUSTED THE HORIZONTAL RIG AND DOOR OPERATED NORMALLY. (Z) 2L72 4F A6WE 19950320006251995032000625NM 1995 3 20 AWXA9500106 119950221A3350900835A EEL BATTERY PACK BOEING737 7372Q8 138448KNM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28137AW 23148 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT OVERWING CEILING LOCATION, OPS CHECK NORMAL. (Z) 2L72 4F RTA16WE 19950320006261995032000626NM 1995 3 20 AWXA9500107 119950221A335020131A EEL BATTERY BOEING737 7373S3 1384711NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT SECTION. REMOVED AND REPLACED BATTERY ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950320006271995032000627NM 1995 3 20 AWXA9500111 119950227A5330 SKIN BOEING737 737277 1384570NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - DURING C6 INSPECTION, FOUND FUSELAGE SKIN CRACKED AND TORN AT AFT UPPER EDGE OF RADOME, LBL 6. ROUTED OUT DAMAGE AND REPAIRED AREA PER ER 2-53-31-10. (Z) 2L72 4F RTA16WE 19950320006281995032000628NM 1995 3 20 AWXA9500115 119950223A3350 EEL WIRES BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28168AW 23629 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 1 THROUGH 4, 13 AND 14. RECONNECTED WIRES AS REQUIRED, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950320006291995032000629NM 1995 3 20 AWXA9500116 119950223A335020131A EEL BATT CHARGER BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 TO REAR OF AIRCRAFT. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950320006301995032000630NM 1995 3 20 AWXA9500117 119950224A3350 EEL CONNNECTOR BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28306AW 24633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 18 THROUGH 20. REPAIRED CONNECTOR AT ROW 20, OPS CHECK NORMAL. (Z) 2L72 4F RTA16WE 19950320006311995032000631NM 1995 3 20 AWXA9500118 119950225A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 25 THROUGH 27. REPINNED WIRE AT ROW 25, OPS CHECK GOOD. (Z) 2L72 4F RTA2NM 19950320006321995032000632NM 1995 3 20 AWXA9500129 119950226A33505106 EEL BATTERIES BOEING737 737297 1384480NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28147AW 22630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR OVERHEAD/PORTABLE EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (Z) 2L72 4F A16WE 19950320006331995032000633NM 1995 3 20 AWXA9500130 119950227A335020131A EEL BATT CHARGER BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN AFT AND REAR SECTIONS OF AIRCRAFT INOPERATIVE. REMOVED AND REPLACED RT AND LT AFT BATTERY CHARGER ASSEMBLIES, OPS CHECK NORMAL. (Z) 2L72 4F RTA16WE 19950320006341995032000634NM 1995 3 20 AWXA9500131 119950301A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304AW 24011 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED MID CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED WIRES, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950320006351995032000635NM 1995 3 20 AWXA9500132 119950301A3350 EEL BOEING737 73733A 1384673NM CABIN INOP A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28167AW 23628 PHX - ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE IN REAR SECTION. REPAIRED AS REQUIRED, OPS CHECK OK. (Z) 2L72 4F RTA16WE 19950320006361995032000636NM 1995 3 20 AWXA9500133 119950303A3350 EEL BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 21 THROUGH 23. REPINNED AT ROW 21, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950320006371995032000637NM 1995 3 20 USAA950027 119950114A2910 HYD FITTING BOEING737 737201 1384454NM LT MLG LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19244US 22752 PHL - FLT 8610 - FLIGHT EN ROUTE BUT TO ACY WHEN AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. FLIGHT DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED BROKEN FITTING AT LEFT MAIN GEAR DOWN LINE RESTRICTOR. ALSO, REPLACED NR 1 AND NR 2 ENGINE 'A' SYSTEM HYDRAULIC PUMPS, PRECAUTIONARY. (Z) 2L72 4F A16WE 19950320006381995032000638NM 1995 3 20 USAA950030 119950118A3234A42006028305 SOLENOID BOEING737 737201 1384454NM LDG GEAR LEVER FAILED A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19245US 22751 ROC - FLT 1670 - UNABLE TO RAISE GEAR HANDLE ON TAKEOFF. CREW PERFORMED CHECKLIST, DETERMINED THAT LANDING GEAR LEVER LATCH SOLENOID FAILED. OVER RIDE LEVER PULLED AND GEAR RETRACTED NORMALLY PER CHECK LIST. FLIGHT PROCEEDED ON TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LOCK SOLENOID. (Z) 2L72 4F A16WE 19950320006391995032000639EU 1995 3 20 USAA950046 219950126A7261 FILTER BOEING737 7372B7 1384560NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE CONTAMINATED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19285AU 23132 TYS - 1192 - ON CLIMB, NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. FLIGHT RETURNED TO TYS WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL FILTER CONTAMINATED WITH CARBON. REPLACED MAIN OIL FILTER. RAN ENGINE, CHECKED FOR LEAKS, NO LEAKS NOTED. OIL FILTER BYPASS LIGHT DID NOT ILLUMINATE AT RUN UP. (Z) 2L72 4F4 F A16WE E21EU 19950320006401995032000640NM 1995 3 20 USAA950047 119950128A3610 DUCT BOEING737 737201 1384454NM NR 1 ENG LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19239US 22354 MCO - ON CLIMB, LEFT ENGINE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO MCO WHERE AN OVERWEIGHT LANDING WAS MADE. REPEAT EVENT, ON CLIMB, LEFT ENGINE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO MCO WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND GASKET FAN TSO THERMOSTAT IN PNEUMATIC LINE RUPTURED. REPLACED GASKET. ACOMPLISHED OVERWEIGH LANDING INSPECTION. FOUND 13TH STAGE ANIT-ICE DUCT LEAKING AT EXPANSION JOINT 12 O'CLOCK POSTION UNDER ENGINE FIXED COWL. REPLACED RIGID LINE. (Z) 2L72 4F A16WE 19950320006411995032000641NM 1995 3 20 USAA950092 119950204A3350 EEL BATTERY PACK BOEING737 737201 1384454NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19257AU 22799 PHL - 159 - FORWARD EXTERIOR EMERGENCY EXIT LIGHTS AND AFT CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK FOR FORWARD EMERGENCY EXIT LIGHTS. REPLACED AFT OVERHEAD EMERGENCY LIGHT POWER SUPPLY. OPS CHECK NORMAL. (Z) 2L72 4F A16WE 19950320006421995032000642NM 1995 3 20 USAA950093 119950204A27511817392 TRANSMITTER BOEING737 737201 1384454NM TE FLAP FAILED A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19227AU 21816 EWR - 44 - DURING APPROACH FOR LANDING LGA, TRAILING EDGE FLAP INDICATION BETWEEN 1 DEGREE AND 2 DEGREE. FLIGHT DIVERTED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FLAP POSITION. (Z) 2L72 4F A16WE 19950320006431995032000643NM 1995 3 20 USAA950094 119950204A3030 PITOT WIRING BOEING737 7372B7 1384560NM RT ELEV FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19270AU 22882 IND - FLT 1860 - EN ROUTE TO PIT, FLIGHT LOST ELEVATOR FEEL PITOT HEAT. FLIGHT DIVERTED TO IND, DUE TO ICING SITUATION AT PIT. LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED WIRE IN CONNECTOR AT RIGHT ELEVATOR PITOT PROBE. HEAT TEST CHECKS GOOD. (Z) 2L72 4F A16WE 19950320006441995032000644NM 1995 3 20 USAA950098 119950208A27502061141 INDICATOR BOEING737 737201 1384454NM FLAP SYSTEM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA19265AU26799 22962 JFK - FLT 2689 - ON APPROACH LGA, WHEN FLAPS WERE SET TO 5, FLAPS FROZE IN THE 1 POSITION. FLIGHT DIVERTED TO JFK WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND INDICATOR SPLIT CAUSING FLAP SYSTEM TO BE LOCKED OUT. REPLACED INDICATOR. SYSTEMS OPS NORMAL. (Z) 2L72 4F A16WE 19950320006451995032000645NM 1995 3 20 USAA950181 119950201A5312 BULKHEAD SKIN BOEING737 737301 1384611NM BS 178 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US2695126951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .375 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN (BS 178) BS 178, LBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z) 2L72 4F RTA16WE 19950320006461995032000646NM 1995 3 20 USAA950182 119950201A5312651630049 BULKHEAD SKIN BOEING737 737301 1384611NM BS 178 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US2695126951 23232 INT -DURING Q-4 CHECK VISUAL INSPECTION, FOUND .75 INCH VERTICAL CRACK IN FORWARD PRESSURE BULKHEAD SKIN BS 178, BS 178 RBL 5, WL 200. REPAIRED PER T/R 53-10-07. (Z) 2L72 4F RTA16WE 19950320006471995032000647NM 1995 3 20 USAA950183 119950210A5330 SKIN BOEING737 737301 1384611NM BS 867 TO 887 CHAF WEAR A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND APPROX .5 INCH BY 4 INCH LONG CHAF WEAR DEEP INTO FUSELAGE SKIN, BETWEEN STRINGER 1 AND 2 LEFT AT STATION 867 TO 887. REPAIRED PER SRM 53-00-01 AND TR 53-30-01 AND TR 53-30-03 AND EA 38864. (Z) 2L72 4F RTA16WE 19950320006481995032000648NM 1995 3 20 USAA950184 119950203A5320 BEAM BOEING737 737301 1384611NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 31 INCH BY 2 INCH CORRODED AREA ON BEAM AT BS 986.5. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-00-51. CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950320006491995032000649NM 1995 3 20 USAA950185 119950208A5313 STRINGER BOEING737 737301 1384611NM BS 775 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON AFT CARGO FLOOR STRINGERS, BS 775 AT LBL 2, 7, AND 12 RBL 2, 7, (5 PLACES). REPAIRED PER TR 53-10-06. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950320006501995032000650NM 1995 3 20 USAA950186 119950220A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 847-787.7 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .625 INCH BY 10 INCH TOTAL CORROSION IN SEVERAL PLACES, ON FLOOR BEAM AT BS 847 THROUGH BS 787.7. REPAIRED PER SRM 53-00-53 FIG 202. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950320006511995032000651NE 1995 3 20 USAA950191 219950225A7261 GARLOCK SEAL BOEING737 7372B7 1384560NM PWA JT8 JT8D15A 52051NE NR 1 ENG LEAKING A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA19280AU 22892 709002 CLT - 1838 - ON CLIMB LOW OIL PRESSURE LIGHT FOR NR 1 ENGINE ILLUMINATED ALONG WITH OIL QUANTITY INDICATING NEAR ZERO. CREW SHUT DOWN NR 1 ENGINE AND FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 GARLOCK SEAL. LEAK CHECK GOOD. (Z) 2L72 4F4 F A16WE E2EA 19950320006521995032000652WP 1995 3 20 95ZZZW230 119950223A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE053101357748 193B1035 MCI - DURING SPECIAL CHECK, FOUND CRACKS AT STA 555 UPPER RIB CAP AS FOLLOWS, .75 INCH O/B OF STRINGER 18, 1 INCH IN STRINGER 18 CASTELLATION, .6250 INCH STRINGER 19, 1 INCH I/B SIDE OF STRINGER 19, AND .0625 INCH AT STRINGER 21. REPAIRED SECTIONS OF CAP PER DRAWING 1647070. TOTAL CYCLES 21031. 2L73 4F A23WE 19950320006531995032000653NM 1995 3 20 95ZZZW231 119950228A5532 SKIN BOEING727 727231 1384079NM FS 1333 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736843 21989 MCI - DURING OP-17, FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER SKIN FUSELAGE, STA 1333. REPAIRED PER ARA 9113. TOTAL CYCLES 22210. 2L73 4F A3WE 19950320006541995032000654NM 1995 3 20 95ZZZW232 119950216A5313 STRINGER BOEING727 727231 1384079NM FS 990 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736842 21989 MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO STRINGER/STRINGER SPLICE 29R AND 29L, FS 990. REMOVED CORROSION PER SRM 51-10-6 AND REPAIRED PER ARA 8682 AND STANDARD PRACTICES. TOTAL CYCLES 22210. 2L73 4F A3WE 19950320006551995032000655WP 1995 3 20 95ZZZW233 119950222A5320 FITTING DOUG DC8 DC862 3021970WP BS 1606 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 30 RT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950320006561995032000656WP 1995 3 20 95ZZZW234 119950222A5315 FLOORBEAM DOUG DC8 DC862 3021970WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP IS CORRODED AT BS 1440 FROM 45 INCHES LBL TO 45 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950320006571995032000657WP 1995 3 20 95ZZZW235 119950222A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1606-1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 32 RT IS CORRODED BETWEEN BS 1606 AND 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F 4A25 19950320006581995032000658WP 1995 3 20 95ZZZW236 119950222A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1606-1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 36 IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F 4A25 19950320006591995032000659WP 1995 3 20 95ZZZW237 119950222A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 36 IS CORRODED 6 INCHES FWD AND AFT OF BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F 4A25 19950320006601995032000660WP 1995 3 20 95ZZZW238 119950222A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1550 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 36 IS CORRODED AT BS 1550. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI ER SRM 53-2-2. 2L74 4F 4A25 19950320006611995032000661WP 1995 3 20 95ZZZW239 119950222A5315 FLOORBEAM DOUG DC8 DC862 3021970WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FLOORBEAM CAP AT BS 1574 IS CORRODED FROM 36 INCHES LBL TO 36 INCHES RBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950320006621995032000662WP 1995 3 20 95ZZZW240 119950222A5311 FRAME DOUG DC8 DC862 3021970WP BS 1586 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN LOWER CIRCUMFERRENTIAL FRAME 'J' FLANGES ARE CORRODED, UPPER AND LOWER AT BS 1586 FROM LONGERON 24L TO 24R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19950320006631995032000663WP 1995 3 20 95ZZZW241 119950222A5320 FITTING DOUG DC8 DC862 3021970WP BS 1606 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 30 LT END BATHTUB FITTING IS CORRODED AT BS 1606L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950320006641995032000664WP 1995 3 20 95ZZZW242 119950222A5311 FRAME DOUG DC8 DC862 3021970WP BS 1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, CIRCUMFERRENTIAL FRAME IS CORRODED AT BS 1574 BETWEEN LONGERON 24 RT AND 26 RT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19950320006651995032000665NE 1995 3 20 95ZZZW243 219950218A7230 C1 BLADE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 1 ENGINE LOCKED UP A RIAAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SO19300AW 193P1134 10626 DURING CRUSIE, HIGH VIBRATION ON NR 1 ENGINE WAS NOTICED. ENGINE WAS SHUTDOWN AT 0133. UPON INSPECTION FOUND C1 BLADES LOCKED UP. PERFORMED MTC MNL PROCEDURE 72-31-05 TO UNLOCK BLADES. ENGINE WAS RAN AND VIBRATION LIMITS WERE WITHIN ACCEPTABLE LIMITS. 2L73 4F4 F A23WE A12EU 19950320006661995032000666NE 1995 3 20 95ZZZW244 219950219A7261 FILTER LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 ENGINE DIRTY A RIAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO19319EA 193A1040 10063 LAS - DURING CLIMB AND CRUSIE, NR 2 ENGINE FILTER PRESSURE LIGHT WAS FLICKERING AND SLIGHT OIL QTY LOSS WAS INDICTED. ENGINE WAS SHUTDOWN AT 1700 AND FLIGHT WAS DIVERTED TO KORD. UPON LANDING AT 1727 FILTERS WERE REPLACED AND CHIP DETECTORS WHERE INSPECTED AND FOUND OK. FIVE QTS OF OIL WAS ADDED. ENGINE RUNUP CHECKED OK. 2L73 4F4 F A23WE A12EU 19950320006671995032000667WP 1995 3 20 95ZZZW245 119950203A5320 FITTING DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 26 RT END FITTING IS CORRODED AT STA 1530. REMOVED AND REPLACED DAMAGED SECTION OF LONGERON PER SRM 51-1-0. 2L74 4F 4A25 19950320006681995032000668WP 1995 3 20 95ZZZW246 119950203A5730 SKIN DOUG DC8 DC862 3021970WP RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING L/E O/B SLOT CUTOUT FWD SKIN HAS SURFACE CORROSION I/B SIDE. CUT OUT CORROSION AND INSTALLED DOUBLER PER SRM 51-2-1. 2L74 4F 4A25 19950320006691995032000669WP 1995 3 20 95ZZZW247 119950210A5320 SUPPORT LKHEED1011 10113851 5265010WP BS 297 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL CORROSION 2, MAIN CABIN FWD BAR FLR AREA STA 297 LT SIDE O/B OF 4TH SEAT TRACK FLR SUPPORT HAS CORROSION. REMOVED CORROSION, FABRICATION TREATED, PRIMED AND INSTALLED ANGLE REPAIR AS PER SRM 51-21-01 AND 53-21-01. 2L73 4F A23WE 19950320006701995032000670WP 1995 3 20 95ZZZW248 119950210A5320 WALL LKHEED1011 10113851 5265010WP HEAT EXCHANGER CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, FUSELAGE RT SIDE NR 3 HEAT EXCHANGE AREA FWD I/B WALL HAS CORROSION DOT 829. REMOVED CORROSION, FABRICATED REPAIRS, TREATED AND PRIMED AREA AND INSTALLED REPAIRS AS PER SRM 51-21-01 AND DRAWING RCH, L15310-5013. 2L73 4F A23WE 19950320006711995032000671WP 1995 3 20 95ZZZW249 119950210A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 22 RT END FITTING CORRODED AT BS 1530 RT. REMOVED CORRODED END FITTING, TREATED NEW FITTING AND INSTALLED AS PER SRM 51-1-8 AND 51-1-00. 2L74 4F 4A25 19950320006721995032000672WP 1995 3 20 95ZZZW250 119950210A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 28 LT END FITTING IS CORRODED AT BS 1530 LT. REMOVED 'L' AND REMOVED CORROSION, FABRICATED REPAIR AND INSTALLED REPAIR AS PER SRM 51-1-8 AND 53-2-8. 2L74 4F 4A25 19950320006731995032000673WP 1995 3 20 95ZZZW251 119950210A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE RT EXTERIOR SKIN AT WINDOW NR 14R HAS CORROSION AROUND FASTENERS. REMOVED WINDOW, REMOVED CORROSION, FABRICATED REPAIR, TREATED, PRIMED AND INSTALLED REPAIR AND WINDOW AS PER SRM 51-1-8, DRAWING RCH D85310-5015 AND MM 56-20-00. 2L74 4F 4A25 19950320006741995032000674WP 1995 3 20 95ZZZW252 119950210A5347 SEAT TRACK DOUG DC8 DC862 3021970WP BS 1500-1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 1500 RT TO BS 1540 RT 25 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-1-8 AND 51-10-0. 2L74 4F 4A25 19950320006751995032000675WP 1995 3 20 95ZZZW253 119950210A5347 SEAT TRACK DOUG DC8 DC862 3021970WP BS 1500-1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 150 RT TO BS 1540 RT, 39 INCHES RBL. REMOVED DAMAGED TRACK, FABRICATED REPAIR, CLEANED AREA, TREATED, PRIMED AND INSTALLED REPAIR AS PER SRM 51-10-00 AND 51-1-8. 2L74 4F 4A25 19950320006761995032000676WP 1995 3 20 95ZZZW254 119950210A5347 SEAT TRACK LKHEED1011 10113851 5265010WP BS 297 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FWD BAR FLOOR AREA STA 297 BET LT SIDE 4TH SEAT TRACK AND RT SIDE 4TH SEAT TRACK FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION, TREATED, AND PRIMED AS PER SRM 51-20-01. 2L73 4F A23WE 19950320006771995032000677WP 1995 3 20 95ZZZW255 119950201A5711 SPAR FLANGE DOUG DC8 DC862 3021970WP WING TANK 3 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RTT WING NR 3 AUX TANK LOWER SURFACE FRONT SPAR ATTACH FLANGE HAS AREAS OF BULGING CORROSION. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950320006781995032000678WP 1995 3 20 95ZZZW256 119950201A5320 BRACKET DOUG DC8 DC862 3021970WP BS 1500 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT PASSENGER DOOR AFT SIDE, FRAME CUTOUT BRACKET HAS CORROSION STA 1500. REMOVED AND REPLACED 'T' BRACKET IAW SRM 53-1-0. 2L74 4F 4A25 19950320006791995032000679WP 1995 3 20 ASAA9580008 119950218A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 18 TO 21 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006801995032000680WP 1995 3 20 ASAA9580009 119950218A3350 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 10 WERE FOUND INOPERATIVE. RESET CONNECTOR TO BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006811995032000681WP 1995 3 20 ASAA9580010 119950220A5210 INTERLOCK DOUG DC9 DC982 3022082WP FWD ENTRY DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 LAX - DURING MAINTENANCE THE FWD ENTRY DOOR WOULD NOT LATCH PROPERLY. ADJUSTED DOOR INTERLOCK MECHANISM AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006821995032000682WP 1995 3 20 ASAA9580011 119950221A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01938AS 49365 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006831995032000683WP 1995 3 20 ASAA9580012 119950221A33506011779 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950320006841995032000684WP 1995 3 20 ASAA9580013 119950221A3350600344 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 REMAINED ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950320006851995032000685WP 1995 3 20 ASAA9580014 119950220A4900GTCP8598DHF AUX POWER UNIT DOUG DC9 DC983 3022083WP AFT FUSELAGE SEAL LEAKING A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM01942AS11587 53052 PHX - FLT 706 - UPON ARRIVAL, CREW REPORTED CABIN FILLED WITH SMOKE, SHUTDOWN APU AND SMOKE DISSIPATED. INSPECTED APU, FOUND INLET SHAFT SEAL LEAKING. RELEASED ACFT PER MD80 MEL 49-1. SUBSEQUENTLY REPLACED APU. (W) 2L72 4F RTA6WE 19950320006861995032000686WP 1995 3 20 ASAA9580015 119950218A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 9 WERE FOUND INOPERATIVE. REPAIRED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006871995032000687WP 1995 3 20 ASAA9580016 119950222A335060030431 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950320006881995032000688WP 1995 3 20 ASAA9580020 119950224A5311 FRAME DOUG DC9 DC982 3022082WP BS 1326 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS20228 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1326, Z-42, X PLUS 0. FABRICATED REPAIR SPLICES AND FRAME. CLEANED, TREATED. ALODINED AND PRIMED. INSTALLED REPAIR PARTS AND FASTENERS IAW DC-9 SRM 53-03 FIG 2A 51-30-05 PG 8A, 51-10-03 PG 14, 18A AND 21, 51-30-01 PG 8 AND 14, 51-30-02 PG 1. TOTAL CYCLES 28294. (W) 2L72 4F A6WE 19950320006891995032000689WP 1995 3 20 ASAA9580030 119950225A33501001191 EEL DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01930AS 49231 SEA - DURING MAINTENANCE CHECK, THE FWD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950320006901995032000690WP 1995 3 20 ASAA9580031 119950225A335060030431 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950320006911995032000691NM 1995 3 20 MZZA9506 119950208A3350 EEL SIGN COVER BOEING727 7272F9 138407DNM L2 GALLEY DOOR CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP13299AS 21427 TNN - DURING S-CHECK INSPECTION, CRACK WAS FOUND ON L2 GALLEY SERVICE DOOR EXIT SIGN COVER. THE DAMAGED EXIT SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH (P/N BR727-105) ASSEMBLY PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON ROUTINE REPAIR ITEM CARD NR 0725422 (SEQ NR 02078). (W) 2L73 4F RTA3WE 19950320006921995032000692WP 1995 3 20 9503851226 119950227A5754ARB24301 RIB DOUG DC10 DC1030 3023501WP XDLE =309 WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 DURING PERIODIC CHECK, THE LHS DROOPED LEADING EDGE INBOARD RIB AT STA XDLE =309 WAS FOUND WORN. BLENDED DAMAGE AREA AND INSTALLED REPAIR ANGLE PER EA 12-96666. 2L73 4F A22WE 19950320006931995032000693NM 1995 3 20 9503866614 119950303A5720 CHORD BOEING747 747251B 1384892NM WNG 837 840 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, THE RIGHT WING LOWER SURFACE MID-SPAR CHORD (STRINGER 10) FORWARD ATTACH FLANGE WAS FOUND CORRODED AT WBL 837-840, JUST OUTBOARD OF THE NR 4 PYLON. STRINGER IS MACHINED FROM 2024-T3511 EXTRUSION PER BAC 1506-2562. MADE REPAIR PER EA 66-93966. 2L74 4F A20WE 19950320006941995032000694NM 1995 3 20 9503876614 119950301A5320 WEB BOEING747 747251B 1384892NM FS 1301-1306 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE LOWER SURFACE OF THE PRESSURE DECK WEB BETWEEN BS 1301-1306 RBL 110-127. DISCREPANT PRESSURE DECK WEB IS MADE FROM L071 INCH 7075-T6 ALUMINUM. MADE REPAIR PER EA 66-80199. 2L74 4F A20WE 19950320006951995032000695NM 1995 3 20 9503886632 119950301A5321 FLOOR BOEING747 747251B 1384892NM FS 490 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 23112 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CABIN FLOOR, RIGHT SIDE WALL HORIZONTAL FLANGE BS 490. AFT SIDE OF NR 1 RIGHT ENTRY DOOR. FLANGE IS MADE FROM 7075-16 ALUMINUM FORMED SECTION. MADE REPAIR PER EA 66-97860. 2L74 4F A20WE 19950320006961995032000696WP 1995 3 20 9503899305 119950310A5754 SKIN DOUG DC9 DC982 3022082WP NR 5 SLAT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307RC 48086 DURING PERIODIC CHECK FOUND CRACK AND MISSING FASTENERS IN NR 5 SLAT INBOARD SIDE SKIN. REPAIRED PER EA 93-96479 SECT 1. 2L72 4F A6WE 19950320006971995032000697WP 1995 3 20 9503909180 119950310A5320 FITTING DOUG DC9 DC914 3022034WP FS 766 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013312L 45707 DURING PERIODIC CHECK FOUND CORROSION IN THE LONGERON 26R FRAME ATTACH FITTING AT FS 766. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950320006981995032000698WP 1995 3 20 9503919996 119950310A5320 FITTING DOUG DC9 DC931 3022065WP FS 984 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CRACK IN LONGERON 28R END FITTING AT FS 984. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950320006991995032000699WP 1995 3 20 9503929996 119950310A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CRACK IN FLOOR SUPPORT FITTING, LONGERON 28R AT FS 996. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950320007001995032000700WP 1995 3 20 9503939996 119950313A5320 FITTING DOUG DC9 DC931 3022065WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CORROSION IN THE RIGHT SIDE KEEL FITTING AT FS 756. REPLACED FITTING PER 51-30-0 AND SB 53-75. 2L72 4F A6WE 19950320007011995032000701WP 1995 3 20 9503949305 119950314A5220 FRAME DOUG DC9 DC982 3022082WP EMER EXIT DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307RC 48086 DURING PERIODIC CHECK FOUND CRACKS IN BOTH RIGHT OVERWING EMERGENCY EXIT DOOR FRAMES AT THE NR 14 STOP. REPAIRED PER EA 93-096707 AND -096708. 2L72 4F A6WE 19950320007021995032000702WP 1995 3 20 9503959996 119950314A5320 FITTING DOUG DC9 DC931 3022065WP FS 579 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CRACK IN LONGERON 27L END FITTING AT FS 579. REPLACED PER SRM 51-30-0. 2L72 4F A6WE 19950320007031995032000703WP 1995 3 20 9503969996 119950314A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CORROSION IN LONGERON 29R END FITTING AT FS 604. REPLACED PER SRM 51-30-3. 2L72 4F A6WE 19950320007041995032000704WP 1995 3 20 9503979996 119950314A5320 FITTING DOUG DC9 DC931 3022065WP FS 598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND CORROSION IN LONGERON 30 END FITTING AT FS 598. REPLACED PER SRM 51-30-0. 2L72 4F A6WE 19950320007051995032000705NM 1995 3 20 9503982284 119950303A7711LG14C14 EPR TRANSMITTER BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01284US4681723229 21323 700220 ON TAKEOFF, NR 1 ENGINE EPR INDICATION WAS UNACCEPTABLE, TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND PERFORMED ENGINE RUNUP. SYSTEM CHECKED 'OK'. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950320007061995032000706NM 1995 3 20 9503995504 119950314A21506806403 ACM BOEING757 757251 1384970NM AFT FUSELAGE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01504US32290 23193 TAKEOFF WAS ABORTED AT 50 KTS DUE TO LOUD WHINE IN THE COCKPIT. COCKPIT TEMPERATURE WAS 85 DEGREES, WITH LEFT AIR CYCLE MACHINE MALFUNCTION. PLACARDED LEFT PACK INOPERABLE PER MEL 21-51-1. REPAIRED LEFT AIR CYCLE MACHINE PER MM 21-51-03, P. 201 IN BOS, SYSTEM CHECKED NORMAL. 2L72 4F RTA2NM 19950320007071995032000707NM 1995 3 20 9504002295 119950314A2923323636 HYD PUMP BOEING727 727251 138408HNM HYD BAY FAILED A ANWAAAJ UNSCHED LANDING DUMP FUEL JK WARNING INDICATION FLUID LOSS UKUNKNOWN 1 GL01295US360174745 21506 DURING FLIGHT, 'B' SYSTEM HYDRAULIC PUMP NR 2 PRESSURE INDICATION FLICKERING FOLLOWED BY DECREASE IN 'B' SYSTEM QUANTITY. CREW DECLARED AN EMERGENCY AND PERFORMED HYDRAULIC FLUID/SYSTEM LOSS CHECKLIST. JETTISONED 6900 POUNDS OF FUEL AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINES 155 AND 160 IN THE ILLUSTRATED PARTS CATALOG REFERENCE 29-14-00 FIGURE 6 AND 'B' SYSTEM PUMP AND FILTERS. OPERATIONAL AND LEAK CHECK NORMAL. 2L73 4F A3WE 19950320007081995032000708NE 1995 3 20 9504012293 219950304A73217436024 FUEL CONTROL BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL01293US8531 8531 21504 696472 WHEN POWER WAS REDUCED FOR DESCENT, NR 2 ENGINE OIL PRESSURE DECREASED TO 10 PSI FOLLOWED BY ILLUMINATION OF THE LOW OIL PRESSURE WARNING. A PRECAUTIONARY SHUTDOWN WAS PERFORMED AND THE FLIGHT WAS CONCLUDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THAT THE ENGINE WAS SPOOLING DOWN WHEN THE THROTTLE WAS RETARDED. MAINTENANCE REPLACED THE FUEL CONTROL UNIT AND PERFORMED AN ENGINE RUNUP. THE SYSTEM CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVICE. THIS FUEL CONTROL ASSY CONSISTS OF THE FOLLOWING COMPONENTS: PUMP, P/N 378201-5, HEATER, P/N 522649, AND THE FUEL CONTROL, P/N 743602-4. 2L73 4F4 F A3WE E2EA 19950320007091995032000709WP 1995 3 20 9504029996 119950314A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK FOUND THAT INADEQUATE FORCE WAS REQUIRED TO RELEASE THE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ADJUSTED THE LATCHES AND THE CLIPS. CHECKED OK. 2L72 4F A6WE 19950320007101995032000710WP 1995 3 20 9504039998 119950311A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018943E 47143 DURING LINE CHECK FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED AND LUBRICATED THE CLIPS. CHECKED OK. 2L72 4F A6WE 19950320007111995032000711NM 1995 3 20 95FDEA00205 119950228A5320ANB73871 DOOR FRAME DOUG MD11 MD11 3023602NM LT MLG CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO04601FE 48401 THE LEFT HAND CENTERLINE LANDING GEAR DOOR FRAME IS CRACKED ALONG THE FWD, INBOARD CORNER, CRACK IS APPOX 3.5 INCHES LONG C-CK N/R 7004. REMOVED LT FWD CENTERLINE DOOR AND INSTALLED NEW FRAME. P/N ANB 7387-1 PER SRM 53-00-01. 2L73 4F RTA22WE 19950320007121995032000712 1995 3 20 95FDEA00206 419950307A3417HG480B13 CADC BOEING727 727233 138408ANM LEFT MALFUNCTIONED A AFDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04257FE 20939 AFTER TAKEOFF, THE CAPTAIN'S AIRSPEED AND ALT FLAGS CAME IN VIEW. PROBABLE CASE FAILURE. THE AIR DATA CMPTR CB WAS POPPED AND WOULD NOT RESET. REMOVED AND REPLACED AIR DATA COMPUTER PER MM 34-12-01. OPS CHECK GOOD, NEEDS PITOT STATIC CK. A/C DOWNGRADED TO NOT CAT 2, CKA AND CKB W. NOLTE 16114 PERFORM PITOT STATIC CHECK. IAW MM 34-11, OPS CK NORMAL NOTE INITIAL ROOT CAUSE WET E & E COMPARTMENT SR 13661. 2L73 4F RTA3WE 19950320007131995032000713NM 1995 3 20 95FDEA00207 119950305A3230 RETRACT MECH BOEING727 727225 1384077NM NLG LACK OF LUBE A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO04469FE 21581 ON FINAL APPROACH, NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS LOWERED, GEAR WAS RAISED AND WHEN EXTENDED AGAIN, ALL GEAR LOCKED DOWN NORMALLY. INSPECTED NOSE GEAR COMPONENTS NO DAMAGE, FOUND WATER AND ICE IN KNUCKLE, LUBED KNUCKLE, OK FOR SERVICE. 2L73 4F A3WE 19950320007141995032000714 1995 3 20 95FDEA00208 419950307A3417HG480B13 CADC BOEING727 727233 138408ANM LEFT MALFUNCTIONED A AFDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04271FE 22036 CAPTAIN'S AIRSPEED FAILED AND ALTITUDE FAILED ON TAKEOFF ROLL-CYCLED C.B. FOR ADC, MACH, AIRSPEED-NO HELP, ALT WARNING SYSTEM INOP ALSO. (RAIN DURING LOADING WATER IN E & E). FOUND WATER IN E & E COMPARTMENT (HEAVY RAINS DURING LOADING) REMOVED AND REPLACED AIR DATA COMPUTER PER MM 34-12-11. PERFORMED PITOT/STATIC TEST IAW 34-11-0 OPS CHECKED NORMAL, A/C DOWNGRADED TO NOT CAT II, CK A CK B, MOCC NOTIFIED. 2L73 4F RTA3WE 19950320007151995032000715NM 1995 3 20 95FDEA00212 119950310A2910 AIR BLEED VALVE DOUG MD11 MD11 3023602NM NR 3 HYD SYST MALFUNCTIONED A FDEAO OTHER FJKFLT CONT AFFECTED WARNING INDICATION FLUID LOSS CLCLIMB 1 SO04605FE 48514 SIN: LOST NR 3 HYD SYSTEM FLUID QTY. THE SYSTEM WENT DOWN TO EMPTY AFTER GEAR RETRACTION. SERVICED NR 3 HYD SYSTEM TO 8.5 GAL, TROUBLESHOT AND RAN HYD SYSTEM AND LEAK CHECKED, NO LEAKS NOTED (SUSPECT AIR BLEED VALVE PLUNGER MAY HAVE STUCK DOWN), ALSO, RAN NR 3 ENGINE TO CHECK FOR LEAKS NOTED. EXCERISED PLUNGER AND OPS CHECKS GOOD. OK FOR SERVICE. 2L73 4F RTA22WE 19950320007161995032000716NM 1995 3 20 95FDEA00213 119950316A5320 WINDOW POST BOEING727 727233 138408ANM FLIGHT DECK CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04221FE 20932 NDT PLEASE C/W E.O. 7-5330-7-3354 ( AD 93-05-17) X-RAY INSPECTION THE E-N WINDOW POST. E.O. 7-5330-7-3354 PART II X-RAY INSP E-N WINDOW POST RT HAND. PILOTS SLIDING WINDOW CRACK INDICATION APPX 1.125 INCH LONG. ENGINEERING NOTIFIED. REFERENCE PART 4 AND PART 5 FOR E.O. 7-5330-7-3354 FOR REPAIRS. 2L73 4F RTA3WE 19950320007171995032000717NM 1995 3 20 95FDEA00279 119950315A3610 COUPLING BOEING727 727232 1384082NM NR 1 BLEED LEAKING A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO04498FE 20867 YMX: AFTER ABOUT 1 HR INTO FLT, LWR AFT BODY OVERHEAT LIGHT CAME ON PERFORMED ABNORMAL CHECKLIST, LIGHT WENT OUT. PROCEDURE STATED LEAK IS BETWEEN BLEED VALVE AND PACK VALVE. (PROBLEM NR 1 BLEED). REMOVED AND REPLACED COUPLING ASSY (ON LINE GOING TO PURGE VALVE) ON LT AIR CLEANER DUE TO LEAKING. LEAK CHECK C/O AND SYSTEM FOUND SERVICEABLE. 2L73 4F A3WE 19950320007181995032000718SO 1995 3 20 COM11821 119950307A32463006031 WHEEL HALF 314461 EMB 120 EMB120RT SO RT MLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01268CA12229517 120262 WHEEL S/N 1625 WAS REMOVED FROM AIRCRAFT 268CA, TIRE WAS WORN TO LIMITS. UPON CLEANING THE OUTER WHEEL HALF, FOUND AN AREA THAT LOOKED PITTED AND SOME CORROSION. THE PAINT WAS REMOVED FROM THE AREA IN QUESTION AND CHECKED BY EDDY CURRENT METHOD, THIS VERIFIED THE CRACK. REMOVED WHEEL OUT OF SERVICE AND SENT TO CVG TIRE SHOP FOR DETAIL INSPECTION OF AREA. 2L72 4T RTA31SO 19950320007191995032000719SO 1995 3 20 COM11823 119950312A323112012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMAK NONE O OTHER UKUNKNOWN 1 SO01462CA 120264 LEFT MLG OUTBD DOOR IS HANGING OPEN. REPLACED BROKEN LATCH ASSY ON GEAR DOOR. 2L72 4T RTA31SO 19950320007201995032000720SO 1995 3 20 COM11824 119950315A291012039828 HYD LINE EMB 120 EMB120RT SO RT NACELLE DAMAGED A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01267CA7707 120259 HYDRAULIC LEAK, RT ENGINE NACELLE. ENGINE DRIVEN PUMP SUCTION LINE WAS DAMAGED BY CHAFING. C/W A TEMPORARY REPAIR BY SUBSTITUTION OF A FLEX LINE ASSY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950320007211995032000721EA 1995 3 20 COM60440 119950314A326017300123 HARNESS CNDAIRCL600 CL6002B19 EA LT MLG DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01915CA 7013 WOW INPUT MESSAGE ON EICAS. PROXIMITY SYSTEM FAULT CAUTION ON STATUS PAGE. REPLACED THE LT MLG ELECTRICAL HARNESS. 2L72 4F RTA21EA 19950320007221995032000722EA 1995 3 20 COM60441 119950314A5610NP1393221 WINDOW CNDAIRCL600 CL6002B19 EA LT COCKPIT LEAKING A COMAK NONE O OTHER CLCLIMB 1 SO01920CA2 2 7022 LT COCKPIT WINDOW LEAKED PRESSURIZATION AT 15,000 FEET CAUSING LOUD WIND NOISE. RESEALED THE LT SIDE COCKPIT WINDOW IAW M/M PROCEDURES AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950320007231995032000723NM 1995 3 20 UPS202660 119950315A5720 CLIP BOEING727 72727C 138400JNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON T-CLIP BS 760, LBL 70.5, WL 204. INSTALLED REPAIR PER UPS EO B727-5710-121F. 2L73 4F A3WE 19950320007241995032000724NM 1995 3 20 UPS202661 119950315A5712 RIB BOEING727 72727C 138400JNM BS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'D' CHECK MAINTENANCE FOUND 3 CRACKS AROUND HOLES IN RIB CHORD BS 760, LBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-1271. 2L73 4F A3WE 19950320007251995032000725NM 1995 3 20 UPS202662 119950315A5712 RIB BOEING727 72727C 138400JNM BS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01911UP 19119 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACKS IN RIB CHORD AT TWO FASTENER HOLES, BS 760, RBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-6789A. 2L73 4F A3WE 19950320007261995032000726NM 1995 3 20 UPS402664 119950315A3350 EEL BOEING747 747123F NM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 MAINTENANCE REPORTED ONE EMERGENCY LIGHT OVER THE CREW SERVICE DOOR IS INOPERATIVE. DEFERRED CREW EMERGENCY EXIT (1) ONE LIGHT INOP PER MEL 33-13. 2L74 4F A20WE 19950320007271995032000727NM 1995 3 20 UPS502663 119950315A3234257T110314 LDG LEVER MODULE BOEING757 75724APF 1384969NM FLIGHT DECK MALFUNCTIONED A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01436UP 25467 PILOT REPORTED, PUT GEAR DOWN TO LAND IN ONT. NO RT GEAR DOWN INDICATION LIGHT. PRESS TO TEST AT BULB, WOULD NOT WORK. TEST SWITCH ON OVERHEAD PANEL WAS PUSHED. DID GO AROUND. CYCLED GEAR 4 TO 5 TIMES. DID NOT HELP. DID EMER GEAR CHECK LIST. DID NOT HELP. CYCLED GEAR 1 MORE TIME, GOT RT MLG DOWN AND LOCK INDICATION. NORMAL LANDING. REPLACED LANDING GEAR LEVER MODULE. 2L72 4F RTA2NM 19950320007281995032000728WP 1995 3 20 UPS802653 119950314A5530 ANGLE DOUG DC8 DC873F 302199FWP FS 1766 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON RT VERT. STAB. TO FUSELAGE ATTACH ANGLE, FS 1766. INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F RT4A25 19950320007291995032000729WP 1995 3 20 UPS802654 119950314A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON LT WING L/E, LWR SKIN SCREW HOLE ON I/B END. INSTALLED REPAIR PER SRM 57-2-0. 2L74 4F RT4A25 19950320007301995032000730WP 1995 3 20 UPS802655 119950314A5400 STIFFENER DOUG DC8 DC873F 302199FWP NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON NR 1 PYLON HORIZONTAL STIFFENER AT STA 364-942. REPAIRED PER UPS EO FILE NR DC8-54-0029. 2L74 4F RT4A25 19950320007311995032000731WP 1995 3 20 UPS802656 119950314A5312 BULKHEAD BEAM DOUG DC8 DC873F 302199FWP FS 1766 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON AFT PRESSURE BULKHEAD, 'J' BEAM, THIRD FROM TOP AT FS 1766, RBL 1, THRU ACCESS HOLE 60. REPAIRED PER SRM 53-2-0. 2L74 4F RT4A25 19950320007321995032000732WP 1995 3 20 UPS802657 119950314A5712 RIBS DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACKS ON LT WING, LWR SURFACE, UPPER RIBS 13, 29, 24, AND 14. REPAIRED PER MM 57-00-00. 2L74 4F RT4A25 19950320007331995032000733WP 1995 3 20 UPS802658 119950314A5720 DOUBLER DOUG DC8 DC873F 302199FWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01813UP 46059 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON RT WING L/E LWR SURFACE DOOR DOUBLER AT STA XFS 360-366. REPAIRED PER UPS EO FILE NR DC8-57-0539. 2L74 4F RT4A25 19950320007341995032000734WP 1995 3 20 UPS802659 119950313A33505208458503 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01894UP 46094 MAINTENANCE REPORTED EMER. EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. 2L74 4F RT4A25 19950320007461995032000746CE 1995 3 20 95ZZZX1261 119950309A323323941047 ACTUATOR LEAR 35 35A 5170602CE MLG DEFECTIVE A NVIAO OTHER J WARNING INDICATION APAPPROACH 1 SW051110S 875 3228 306 PILOT REPORTED RIGHT LANDING GEAR DID NOT INDICATE DOWN AND LOCKED. ON THE THIRD ATTEMPT, WHILE THE AIRCRAFT WAS IN A LEFT BANK, THE LANDING GEAR SHOWED ALL THREE DOWN AND LOCKED. THE CREW EXECUTED A NORMAL LANDING. THE AIRCRAFT WAS PLACED ON JACKS AND THE LANDING GEAR CYCLED, WHERE IT WAS DISCOVERED THE RIGHT MAIN GEAR ACTUATOR WAS SLOW TO LOCK IN THE DOWN POSITION. INSPECTION THROUGH THE POSITION INDICATOR SWITCH PORT REVEALED AN INTERNAL DEFECT. THE ACTUATOR WAS REPLACED. 2L72 4F A10CE 19950320007581995032000758EA 1995 3 20 95ZZZX1274 219950208A8500 ENGINE PIPER PA60 PA60601 7106010NM LYC O540 IO540S1A5 41532EA LT ENGINE FAILED A BSYAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 GL078248J 6527962140 L1527248A LEFT ENGINE SHUT DOWN IN-FLIGHT, ACFT LANDED. REMOVED AND REPLACED ENGINE, CAUSE FOR FAILURE UNKNOWN AT THIS TIME. 1M72 3O3 ORTA17WE 1E4 19950324000011995032400001NM 1995 3 24 9504046304 119950125A5414 SKIN BOEING747 747451 1384940NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01664US 23819 DURING OVERNIGHT INSPECTION, A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON SKIN AT THE NR 452 ER CUTOUT. STOP DRILLED CRACK AND INSTALLED DOUBLERS PER EA 63-96605. 2L74 4F RTA20WE 19950324000021995032400002WP 1995 3 24 9504051151 119950210A5320AEA01121 INTERCOSTAL DOUG DC10 DC1040 3023508WP FS 1310 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01151US 46760 DURING PERIODIC CHECK, A CRACK WAS FOUND IN THE INTERCOSTAL WEB OF THE LEFT CENTER FUSELAGE DOOR JAMB AT STA 1310. 2L73 4F A22WE 19950324000031995032400003WP 1995 3 24 9504069927 119950307A5755 HINGE DOUG DC9 DC931 3022065WP FLIGHT SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN RIGHT OUTBOARD FLIGHT SPOILER INNER HINGE. REPLACED HINGE PER SRM 51-30-1. 2L72 4F A6WE 19950324000041995032400004WP 1995 3 24 9504079927 119950307A5311 FRAME DOUG DC9 DC931 3022065WP FS 756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FS 756 BELTFRAME AT LONGERON 10L. REPAIRED PER XEA X9-53-47. 2L72 4F A6WE 19950324000051995032400005WP 1995 3 24 9504089945 119950310A5530 BRACKET DOUG DC9 DC931 3022065WP VERTICAL STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018925E 45840 DURING LINE CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR, RIGHT SIDE ABOVE THE RUDDER LEADING EDGE. REPAIRED PER XEA X9-53-82. 2L72 4F A6WE 19950324000061995032400006WP 1995 3 24 9504099936 119950314A5542 SKIN DOUG DC9 DC931 3022065WP RUDDER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011799U 47370 DURING LINE CHECK, FOUND CRACKS AND LOOSE RIVETS IN THE LEFT SIDE RUDDER SKIN. REPLACED RUDDER PER CITEXT 90-2720-1-9801. 2L72 4F A6WE 19950324000071995032400007WP 1995 3 24 9504109180 119950315A5320 STRAP DOUG DC9 DC914 3022034WP CARGO DOOR JAMB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013312L 45707 DURING PERIODIC CHECK FOUND CORROSION IN THE AFT CARGO DOOR JAMB 'BEAR' STRAP. REPAIRED PER EA 99-094798. 2L72 4F A6WE 19950324000081995032400008WP 1995 3 24 9504119908 119950315A5320 FITTING DOUG DC9 DC931 3022065WP FS 585 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01958N 47254 DURING LINE CHECK FOUND 3 INCH CRACK IN LONGERON 20L END FITTING AT FS 585. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950324000091995032400009NM 1995 3 24 9504122294 119950315A3244657276187 TIRE BOEING727 727251 138408HNM MLG FAILED A NWAAK NONE O OTHER TOTAKEOFF 1 GL01294US 384 21505 AFTER TAKEOFF, CLE CENTER CONTACTED FLT 478 ADVISING THAT TIRE DEBRIS WAS FOUND ON DEPARTURE RUNWAY. FLIGHT CONTINUED AND DISPATCH CONTACTED TPA TOWER TO HAVE EMERGENCY EQUIPMENT STANDING BY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 TIRE CAP SEPARATED AND REPLACED NR 1 AND NR 2 WHEEL ASSEMBLY. NO OTHER DAMAGED NOTED. 2L73 4F A3WE 19950324000101995032400010NM 1995 3 24 9504132705 119950313A53156517588 FLOOR BEAM BOEING727 727225 1384077NM FS 267 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01802EA 22433 DURING PCK, MAINTENANCE FOUND FLIGHT DECK FLOOR BEAM BS 267, LBL 4 CORRODED. REPAIRED PER NWA EA 27-96484. 2L73 4F A3WE 19950324000111995032400011NE 1995 3 24 9504142281 219950308A7230 COMPRESSOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01281US 21160 ENGINE FAIL WARNING ILLUMINATED ON TAKEOFF ROLL. A COMPRESSOR STALL WAS SUSPECTED (ENGINE POSITION UNDETERMINED). THE TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINES, NO DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950324000121995032400012WP 1995 3 24 95FDEA00214 119950310A2612 FIRE WARNING DOUG DC10 DC1030F 3023504WP APU MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO04322FE 47908 THE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, REMOVED AND REPLACED LIGHT ASSY. OPS CKD GOOD. 2L73 4F RTA22WE 19950324000131995032400013NM 1995 3 24 95FDEA00280 119950316A26117740 DECTECTOR BOEING727 727225 1384077NM E/E COMPT FALSE WARNING A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO04469FE 21581 DURING FLT AT FL290 THE NR 2 MAIN CARGO SMOKE INDICATOR ILLUMINATED. COMPLIED WITH ALL APPLICABLE CHECKLIST AND THE LIGHT WENT OUT. FOUND SMOKE DECTECTOR TO BE BAD. REMOVED BAD REPLACED DETECTOR, GROUND OPS CK GOOD. 2L73 4F A3WE 19950324000141995032400014NM 1995 3 24 95FDEA00281 119950316A5311TPN7 FRAME BOEING727 72722 1384002NM FUSELAGE GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 MCD FWD AND AFT SIDE FRAMES ARE GOUGED 52 INCHES UP FROM THE BOTTOM OF DOOR. REPAIRED MCD FWD AND AFT FRAMES 52 INCHES UP FRONT BOTTOM OF DOOR. ALL WORK DONE IAW FEDEX DRAWING NR SR 27-52-009. 2L73 4F A3WE 19950324000151995032400015NM 1995 3 24 95FDEA00282 119950316A5320BAC1510335 HAT CHANNEL BOEING727 72722 1384002NM BS 324-339 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON HAT CHANNEL AT BS 324-339 RBL 16.5 WL 208. REPLACED HAT CHANNEL AT BS 324-339 RBL 16.5 WL 208 WITH FABRICATED PART AND INSTALLED IAW FEDEX SRM 51-10-01. 2L73 4F A3WE 19950324000161995032400016NM 1995 3 24 95FDEA00284 119950316A5330040T3 SKIN BOEING727 72722 1384002NM BS 390 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE IN EXTERNAL SKIN STA 390 STR 7-8 SKIN THICKNESS .040 GOUGE .012, GOUGE OUT OF LIMITS AS PER FEDEX SRM 53-30-1. REPAIRED GOUGE WITH SKIN FLUSH REPAIR AT STA 390 STR 7-8 PER FEDEX SRM 53-30-3 FIG 13. 2L73 4F A3WE 19950324000171995032400017NM 1995 3 24 95FDEA00285 119950316A53207075T6040 WEB BOEING727 72722 1384002NM BS 358 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK IN WEB BS 358 STR 16L WL 216 LBL 60. REPAIRED CRACK IN WEB AT BS 358 STR 16L WL 200 LBL 60 IAW FEDEX SRM 51-40-2. 2L73 4F A3WE 19950324000181995032400018NM 1995 3 24 95FDEA00286 119950316A5313BAC1495138 STRINGER BOEING727 72722 1384002NM BS 440 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE IN STR BS 440 STR 7L. ACCOMPLISHED STR REPAIR BS 440 STR 7L PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950324000191995032400019NM 1995 3 24 95FDEA00287 119950316A57206595600762 STIFFENER BOEING727 72722 1384002NM BS 870 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON 870 LOWER CENTER WING CHORD, LBL 6 ON VERTICAL FLANGE. ACCOMPLISHED REPAIR AT BS 870 LWR CHORD PER FEDEX EA 7-5710-23931 AND FEDEX EA 7-5710-23944. 2L73 4F A3WE 19950324000201995032400020NM 1995 3 24 95FDEA00288 119950316A5320651986220 CHORD BOEING727 72722 1384002NM BS 317 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION (C-BAY) ON UPR R/NOSE CHORD AT BS 317 RBL 13 WL 169 (ACCESS IS REQUIRED) REMOVAL OF INBOARD AND CTR FLOOR WEBS. ACCESSED BY REMOVING FLOOR WEBS AND NOSE GEAR ASSEMBLY AND STRUCT DOORS (L/R) AFT. REMOVED AND REPLACED NOSE CHORD AT BS 317 RBL 13 WL 169 REINSTALLED FLOOR WEBS, NOSE GEAR ASSEMBLY AND GEAR STRUCT DOORS AFT L/R AND HINGES ASSEMBLY ON STRUCT DOOR LEFT. FUNCTIONAL TESTED NOSE GEAR ASSEMBLY AND STEERING PER FEDEX MM 32-22-12, 32-21-0, 32-33-1, 32-51-11, 32-51-0, 32-33-0, 32-51-1. 2L73 4F A3WE 19950324000211995032400021NM 1995 3 24 95FDEA00289 119950316A5347BAC1520843AL FLOOR TRACK BOEING727 72722 1384002NM BS 990 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 IN THE AFT CARGO BAY BS 990 LBL 23 WL 146 THE FLOOR TRACK IS CRACKED. CUT OUT DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIR SECTION OF SEAT TRACK AND STRAPS IAW FEDEX SRM 53-10-5 AREA REMOVED BS 959-990 LBL 23 WL 146. 2L73 4F A3WE 19950324000221995032400022NM 1995 3 24 95FDEA00290 119950316A5311TPN7 FRAME BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 AFT CARGO BAY BS 1050 RBL 3-9 WL 146 THE FRAME IS CRACKED. REMOVED DAMAGED AREAS RBL 3-9. FABRICATED DOUBLER AND TWO FILLERS AND INSTALLED PER FEDEX SRM 51-40-3 AT STA 1050. 2L73 4F A3WE 19950324000231995032400023NM 1995 3 24 95FDEA00291 119950316A532065453135 STR CLIP BOEING727 72722 1384002NM BS 440 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 STR CLIP DAMAGED BS 440 STR 7L. REMOVED DAMAGED STR CLIP AT BS 440 STR 7L THEN INSTALLED A NEW STR CLIP. 2L73 4F A3WE 19950324000241995032400024NM 1995 3 24 95FDEA00292 119950316A532065453132 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 STR CLIP DAMAGED BS 440 STR 8L. REMOVED DAMAGED STR CLIP & INSTALLED NEW CLIP IAW SRM 51-30-2. 2L73 4F A3WE 19950324000251995032400025NM 1995 3 24 95FDEA00293 119950316A5320405469 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK FOUND IN STR CLIP BS 440 STR 16L. REMOVED STR CLIP AT BS 440 STR 16L THEN INSTALLED ON STR CLIP. 2L73 4F A3WE 19950324000261995032400026NM 1995 3 24 95FDEA00294 119950316A53117075T6 FRAME BOEING727 72722 1384002NM BS 520 DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 520 BELOW STR 9R. ACCOMPLISHED FRAME REPAIR AT BS 520 STR 9R IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19950324000271995032400027NM 1995 3 24 95FDEA00295 119950316A53117075T6 FRAME BOEING727 72722 1384002NM BS 540 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R. REMOVED MECHANICAL DAMAGE ON FWD SIDE OF FRAME BS 540 BELOW STR 9R AND REPAIRED IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19950324000281995032400028NM 1995 3 24 95FDEA00296 119950316A5347MM137622NPN SEAT TRACK BOEING727 72722 1384002NM BS 600-650 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION FOUND ON SEAT TRACK BS 600-650 BL 0 WL 208. REMOVED CORRODED SEAT TRACK, INSTALLED FABRICATED SEAT TRACK BS 600-650 BL 0 WL 208 IAW FEDEX SRM 53-10-5 SEAT TRACK EXTRUSION REPAIR. 2L73 4F A3WE 19950324000291995032400029NM 1995 3 24 95FDEA00297 119950316A53117075T6 FRAME BOEING727 72722 1384002NM BS 660 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 GOUGE FOUND ON FRAME BS 660 BETWEEN STR 8-9L WL 271. ACCOMPLISHED FRAME REPAIR BS 660 STR 8-9L WL 271. PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950324000301995032400030NM 1995 3 24 95FDEA00298 119950316A5320652617813 INTERCOSTAL BOEING727 72722 1384002NM BS 320 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON FLOOR SUPPORT BS 322 LBL 30 WL 208. REMOVED CORRODED FLOOR SUPPORT THEN INSTALLED A NEW FLOOR SUPPORT AT BS 322 LBL 30 WL 208. 2L73 4F A3WE 19950324000311995032400031NM 1995 3 24 95FDEA00300 119950316A5315BAC1505100246 FLOOR BEAM BOEING727 72722 1384002NM BS 344 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION FOUND ON UPPER FLANGE OF FLOORBEAM BS 344 LBL 22, 42 AND 55 WL 208. REMOVED DAMAGED FLOORBEAM AND INSTALLED NEW FLOORBEAM AT BS 344 LBL 65-RBL 65 PER FEDEX DRW NR SR 27-53-007. 2L73 4F A3WE 19950324000321995032400032NM 1995 3 24 95FDEA00301 119950316A532065453132 CLIP BOEING727 72722 1384002NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK FOUND IN STR CLIP BS 440 STR 2R. REMOVED FASTENERS FROM CRACKED STR CLIP AT BS 440 STR 2R. THEN INSTALLED NEW STR CLIP IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950324000331995032400033NM 1995 3 24 95FDEA00302 119950316A5320TPN7 DOUBLER BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK IN THE 1050 BS FRAME S 26L PASSING THROUGH JIG HOLE. REMOVED CRACK 1050 BS S26L FABRICATED ANGLE BACK DRILLED HOLE, DEBURRED, ALODINED, PRIMERED AND FASTENED INTO PLACE. ALL WORK ACCOMPLISHED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950324000341995032400034NM 1995 3 24 95FDEA00303 119950316A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 344-346 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON SEAT TRACK BS 344-346 WL 208 RBL 22. REMOVED, FABRICATED AND INSTALLED SEAT TRACK BS 344-399 WL 208 RBL 22 IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950324000351995032400035NM 1995 3 24 95FDEA00304 119950316A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 425-480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON SEAT TRACK AROUND NUT CLIP HOLE AT VARIOUS AREAS BETWEEN BS 425-480 BL 0 WL 208. REMOVED DAMAGE SEAT TRACK, INSTALLED, FABRICATED SEAT TRACK BS 425-480 BL 0 WL 208 IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950324000361995032400036NM 1995 3 24 95FDEA00305 119950316A5320 TEAR STRAP BOEING727 72722 1384002NM BS 380 STR 4L DISBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 TEAR STRAP BS 380 DISBONDED BETWEEN STR 4-10L. NO MATERIAL LOSS NOTED. TEAR STRAP BS 380 STR 4-10L. REPAIRED PER FEDEX SRM 53-30-4. 2L73 4F A3WE 19950324000371995032400037NM 1995 3 24 95FDEA00306 119950316A5320 WEB BOEING727 72722 1384002NM BS 310 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 SEVERAL HOLES IN THE WEB DAMAGED WHILE REMOVAL A STIFFENER AT BS 310 LBL 12-RBL 12 WL 180. REMOVED DAMAGED AREA IN WEB BS 310 LBL 12-RBL 12 WL 180. FABRICATED DOUBLER AND FILLERS, SCOTCH BRITED, ALODINDED, PRIMED, INSTALLED AS PER FEDEX SRM 53-10-9. MFG NR 354351 2026T3 AND 382391 2024-T3. 2L73 4F A3WE 19950324000381995032400038NM 1995 3 24 95FDEA00307 119950316A5320BAC15062530 STIFFENER BOEING727 72722 1384002NM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION OF STIFFENER AT BS 879 RBL 46 WL 201. REMOVED CORRODED STIFFENER, INSTALLED FABRICATED STIFFENER IAW FEDEX EA 7-5310-23953. 2L73 4F A3WE 19950324000391995032400039NM 1995 3 24 95FDEA00308 119950316A5320BAC14902785 ANGLE BOEING727 72722 1384002NM BS 960 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION IN AFT CARGO BAY BS 960 RBL 20 WL 144 ON L-ANGLE STIFFENER (HORIZONTAL) FOR BULKHEAD. CORROSION OUT OF LIMIT PER FEDEX SRM 53-10-01 CUT OUT DAMAGED, FABRICATED PARTS, REPAIRED PER FEDEX SRM 51-40-04. 2L73 4F A3WE 19950324000401995032400040NM 1995 3 24 95FDEA00309 119950316A5320TPN111 WEB BOEING727 72722 1384002NM BS 870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CRACK IN WEB AT BS 874 RBL 8 WL 146 JUST BELOW APU FLOW CONTROL VALVE. ACCESSED AREA BY REMOVING APU DUCT AND APU. STOP DRILLED CRACK AT BS 874 RBL 8 WL 146 AND REPAIRED PER FEDEX SRM 53-10-9 AT BS 874 RBL 8 WL 146. REINSTALLED APU DUCTS AND APU TO INSTALLED ON CUST CARD NR 71C301-02 WORK DONE PER FEDEX MM 49-10-0. 2L73 4F A3WE 19950324000411995032400041NM 1995 3 24 95FDEA00311 119950316A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 480-482 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION ON THE SEAT TRACK BS 480-482 WL 208 LBL 23.5. REMOVED CORRODED SEAT TRACK SECTION. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION USING EXISTING AS TEMPLATE. 2L73 4F A3WE 19950324000421995032400042NM 1995 3 24 95FDEA00312 119950316A5347BAC1520792 SEAT TRACK BOEING727 72722 1384002NM BS 480-600 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION AROUND NUTCLIP HOLES IN SEAT TRACK NUMEROUS AREAS BETWEEN BS 480-600 WL 208 BL O. REMOVED DAMAGED SEAT TRACK, INSTALLED FABRICATED SEAT TRACK BS 480-600 WL 208 BL 0 IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950324000431995032400043NM 1995 3 24 95FDES00283 119950316A523065163526 FRAME BOEING727 72722 1384002NM CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 FWD CARGO DOOR AFT HINGE FWD HINGE FRAME ON A/C IS CRACKED. REMOVED AND REPLACED FWD CARGO DOOR AFT HINGE, FWD HINGE FRAME. ALL WORK DONE IAW FEDEX SRM 51-30-2, 51-30-5, 51-30-8 AND FEDEX MM 52-31-0, FUNCTIONAL TESTED FWD CARGO DOOR IAW FEDEX MM 52-30-0. 2L73 4F A3WE 19950324000441995032400044NM 1995 3 24 95UAL747017 119950315A2612 FIRE WARNING BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE ACTIVATED A UALAAFE UNSCHED LANDING ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP294727U 19883 NR 1 ENGINE FIRE WARNING SOUNDED AFTER LIFT OFF. PULLED FIRE HANDLE, SHUT DOWN ENGINE. FIRE WARNING LIGHT WENT OUT. 2L74 4F4 F A20WE E20EA 19950324000451995032400045WP 1995 3 24 ABXA9500209 119950307A53305911401117 SKIN DOUG DC9 DC933F 302207AWP BS 209 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT LONGERON 19R AT STA 207. REPAIRED IAW ABX REA D953-11089-MR. 2L72 4F A6WE 19950324000461995032400046WP 1995 3 24 ABXA9500210 119950204A57115911301505 SPAR CAP DOUG DC9 DC933F 302207AWP XRS 563 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR LOWER T-CAP HAD LEVEL II CORROSION AT WING TIP. REPAIRED IAW ABX REA D957-11076-MR. 2L72 4F A6WE 19950324000471995032400047WP 1995 3 24 ABXA9500211 119950228A531199196171 FRAME DOUG DC9 DC933F 302207AWP BS 699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05, S.B. 53-131 FOUND FRAME STA 699 RIGHT, CRACKED ON THE FORWARD LOWER FLANGE. CRACK IS WITHIN LIMITS OF DC-9 S.B. 53-131. 2L72 4F A6WE 19950324000481995032400048WP 1995 3 24 ABXA9500212 119950301A53209957913501 INTERCOSTAL DOUG DC9 DC933F 302207AWP BS 415 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND CORROSION ON UPPER DOOR JAMB AT AFT CORNER. REMOVED CORROSION, TREATED AND PRIMED AREA IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950324000491995032400049WP 1995 3 24 ABXA9500213 119950228A5312591013013 BLKHD JAMB DOUG DC9 DC933F 302207AWP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 85-01-02, S.B. 53-137 FOUND THE AFT PRESSURE BULKHEAD UPPER DOOR JAMB LEFT AND RIGHT CORNERS HAVE BEND RADIUS CRACKS IN THE FORWARD FLANGE WHICH EXTEND BEYOND THE STOP DRILLS. REPAIRS ARE ACCEPTABLE AS IS PER SERVICE REWORK DRAWING J060097, GENERAL NOTE NR 28. CRACKS UNDER REPAIR ANGLE ARE STILL ACCEPTABLE PER GENERAL NOTE NR 34 OF SERVICE REWORK DRAWING J060097. 2L72 4F A6WE 19950324000501995032400050WP 1995 3 24 ABXA9500214 119950309A5320575468828 DOUBLER DOUG DC9 DC933F 302207AWP BS 130 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND SMALL CRACKS AROUND FASTENERS ON DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19950324000511995032400051WP 1995 3 24 ABXA9500215 119950306A53119919649501 FRAME DOUG DC9 DC933F 302207AWP BS 756 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23934AX 47462 DURING C-CHECK INSPECTION, FOUND DRILL HOLE IN FUSELAGE FRAME STA 756 BETWEEN LONGERONS 7L AND 8L. REPAIRED IAW ABX REA D953-11085-MR. 2L72 4F A6WE 19950324000521995032400052NM 1995 3 24 DL76L951143 119950314A2934019012002 QTY TRANSMITTER BOEING767 767332 1382001NM CENTER HYD RES MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11178DN 25143 DURING CRUISE FL 290, CENTER HYDRAULIC QUANTITY LIGHT CAME ON WITH DROP IN BRAKE PRESSURE. ALSO, HAD RESERVE BRAKES AND STEERING LIGHT COME ON AND OFF. THEN QTY INDICATION FLUCTUATIONS. DIVERTED JFK, LANDED WITHOUT INCIDENT. VERIFIED HYDRAULIC QTY FULL, REPLACED CENTER SYSTEM QTY TRANSMITTER. OPERATION NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK 2L72 4F RTA1NM 19950324000531995032400053NM 1995 3 24 DL76S951144 119950314A2611 SMOKE ALARM BOEING767 767332 1382001NM LAVATORY ACTIVATED A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO11134DL 25123 DURING CRUISE, HAD FOUR LAVATORY SMOKE ALARMS SOUND. WITH NO VISIBLE SMOKE ONLY SLIGHT ELECTRICAL SMELL. SMELL DISSIPATED QUICKLY. AFTER LANDING, REACTIVATIED SMOKE, ALARMS, RAN PACKS, RECIC. FAN AND ALL GALLEY EQUIPMENT, NO TROUBLE FOUND RETURNED TO SERVICE. 2L72 4F RTA1NM 19950324000541995032400054WP 1995 3 24 MWEA95150 119950315A2560113313 EVAC SLIDE DOUG DC9 DC932 3022066WP FWD ENTRY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31302ME 47102 PILOT REPORTS MAIN CABIN DOOR EVACUATION SLIDE FELL OFF DOOR. RESECURED SLIDE, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950324000551995032400055NM 1995 3 24 QXEA9500078 119950316A35104566M37B042NM PBE DORNERDO32 DO328100 2996000NM COCKPIT CONTAMINATED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09332PH317 3010 DURING ROUTINE MAINTENANCE, FOUND COCKPIT PBE CONTAMINATED. REPLACED PBE AND RETURNED AIRCRAFT TO SERVICE. 2H72 4T RTA45NM 19950324000621995032400062CE 1995 3 24 95ZZZX1306 119950227A8120 MOUNT ARM CESSNA207 T207 2073612CE TURBO MOUNT FAILED A OEZAK NONE O OTHER ININSP/MAINT 1 WP191526U760 20700162 FOUND TURBOCHARGER MOUNT EAR CRACKED IN TWO PIECES. SUBMITTER SUSPECTS THE MOUNTING ARMS WERE IMPROPERLY INSTALLED AND HARDWARE WAS OVERTORQUED. SUBMITTER SUGGESTS MECHANICS MUST TAKE EXTRA CARE TO INSURE PROPER ALIGNMENT OF MOUNTS TO PRECLUDE THIS TYPE OF FAILURE. 1H71 3O A16CE 19950324000731995032400073GL 1995 3 24 95ZZZX1317 219950201A726055337 GEARBOX CESSNA525 525 2076601CE WILINTFJ44 FJ44 66000GL LT ENGINE SEAL FAILED A IMJAK NONE O OTHER NRNOT REPORTED 1 EA25800HS WL1149 5250051 1127 LEFT ENGINE LOSS OF OIL PRESSURE, 135 OPERATOR - IMJA. OIL SEAL INSTALLED DURING COURSE OF SB71-05 9-18-94. TIME IN SERVICE, 22.0 HOURS, 12 CYCLES. 1L72 4F4 FRTA1WI E3GL 19950324000821995032400082WP 1995 3 24 9504201144 119950311A5730 SKIN DOUG DC10 DC1040 3023508WP RT WING LE DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE RIGHT DROOPED LEADING EDGE. REMOVED DAMAGE AND REPAIRED PER EA 11-96662. 2L73 4F A22WE 19950324000831995032400083WP 1995 3 24 9504221144 119950307A5312 BULKHEAD DOUG DC10 DC1040 3023508WP BS 1159 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT AND RIGHT SIDE FUEL TANK BULKHEAD TEE AT FS 1159, X = 50. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-97796. 2L73 4F A22WE 19950324000841995032400084WP 1995 3 24 9504231144 119950306A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1486-1523 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE CENTER FUSELAGE EXTERNAL LONGERONS 30L-32L, FS 1386-1523. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-96668. 2L73 4F A22WE 19950324000851995032400085NE 1995 3 24 9504249902 219950313A7320 MOSTURE TRAP DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE CONTAMINATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01952N 47073 666810 CLIMBING OUT OF MEM, THE CREW NOTED SMALL FLUCTUATIONS IN NR 2 ENGINE INDICATOR. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. UPON INSPECTION, WATER WAS FOUND IN THE FCU MOISTURE TRAP. THE TRAP AND DRAIN HOLE WERE CLEANED. ENGINE RUNUP WAS PERFORMED AND SYSTEM CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950324000861995032400086NE 1995 3 24 9504252713 219950310A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01716RC 22021 SUSPECTED COMPRESSOR STALL OCCURRED ON TAKEOFF (ENGINE POSITION UNDETERMINED). THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE CREW NOTED GUSTING CROSSWINDS AT THE TIME OF DEPARTURE. THE ENGINES WERE INSPECTED, RUNUP, AND CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950324000871995032400087NE 1995 3 24 9504269752 219950310A7532 PRBC VALVE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 1 ENGINE FAILED A NWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01754NW 47116 676209 DEPARTING FROM MSP, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AT APPROXIMATELY 3,000 FEET. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ENGINE WAS INSPECTED, NO DAMAGE NOTED. MAINTENANCE REPLACED THE PRBC AND P AND D VALVE. THE ENGINE WAS RUNUP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950324000881995032400088WP 1995 3 24 9504279866 119950308A276159139005517 ACTUATOR DOUG DC9 DC951 3022051WP RT SPOILER MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL01775NC4063440634 47785 AIRCRAFT ROLLED LEFT AFTER SPEED BRAKES WERE DEPLOYED DURING DESCENT. REPLACED THE RIGHT SPOILER ACTUATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000891995032400089WP 1995 3 24 9504289971 119950310A2780 SLATS MECH DOUG DC9 DC931 3022065WP LT WING LACK OF LUBE A NWAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED UKUNKNOWN 1 GL019335 47337 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH SLATS EXTENDED, FLAPS AT 5 DEGREES, AND SPEED AT 220 KNOTS. RETRACTED SLATS AND AIRCRAFT ROLLED TO THE RIGHT. EXTENDED SLATS AGAIN WITH FLAPS SET AT 15 DEGREES. NORMAL SLAT CONFIGURATION WAS ACHIEVED. INSPECTED AND FOUND LEFT SLATS BINDING DURING EXTENSION. LUBED LEFT WING SLATS AND ROLLERS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000901995032400090WP 1995 3 24 9504299958 119950312A3260 SWITCH DOUG DC9 DC931 3022065WP LT MLG DOOR BROKEN A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01917RW 47145 GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED ON APPROACH. ACCOMPLISHED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT GEAR DOOR SWITCH ARM BROKEN. REPLACED SWITCH, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000911995032400091WP 1995 3 24 9504309754 119950313A3150 TO WARNING DOUG DC9 DC941 302207NWP COCKPIT SOUNDED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01754NW 47178 TAKEOFF WARNING HORN SOUNDED DURING TAKEOFF ROLL AT DTW. ABORTED TAKEOFF AND RETURNED TO GATE. DISCREPANCY COULD NOT BE DUPLICATED DURING OPERATIONAL CHECK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000921995032400092WP 1995 3 24 9504319852 119950313A32600351881027 SOCKET DOUG DC9 DC951 3022051WP COCKPIT PANEL SHORTED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01761NC 47709 DURING UPLATCH CHECK, GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE. REPLACED BULB, THEN ALL THREE RED UNSAFE LIGHTS ILLUMINATED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. NO GREEN LIGHTS ILLUMINATED DURING GEAR EXTENSION FOR LANDING. GEAR WAS VISUALLY CONFIRMED TO BE DOWN AND LOCKED THROUGH PERISCOPE. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION. INSPECTED AND FOUND L2-265 SOCKET TO GEAR DOOR OPEN LIGHT SHORTED. REPLACED SOCKET, CIRCUIT BREAKER U-21 FOR GEAR PROXIMITY BOX, WHICH DID NOT TRIP. REPLACED PROXIMITY BOX. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000931995032400093WP 1995 3 24 9504329751 119950315A2780 SWITCHES DOUG DC9 DC941 302207NWP SLATS MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01751NW 47115 STALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED DURING SLAT RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED SLAT EXTEND SWITCHES. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324000941995032400094NM 1995 3 24 95FDEA00310 119950316A571465185385 CHORD BOEING727 72722 1384002NM BS 870 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO04185FE 18871 CORROSION FOUND ON CENTER WING UPPER 870 CHORD VERTICAL FLANGE BETWEEN CHORD AND WEB RBL 39-43. ACCOMPLISHED REPAIR AT BS 870 UPPER CHORD PER EA 7-5710-23944 (P/N AND STIFFENER NR 651620213). 2L73 4F A3WE 19950324000951995032400095NM 1995 3 24 95FDEA00313 119950317A2782651781823 ACTUATOR BOEING727 72725 1384006NM NR 2 LE SLAT FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO04508FE 18279 AFTER T/O NR 2 SLAT INDICATOR FAILED TO RETRACT. COMPLIED WITH CHECKLIST RETURNED AND LANDED. REPLACED NR 2 L/E SLAT ACTUATOR IAW MM 27-81-32 PG 401-409. SYS OPS NORMAL RII COMPLIED WITH. 2L73 4F A3WE 19950324000961995032400096NM 1995 3 24 95FDEA00314 119950318A5610 SLIDING WINDOW BOEING727 72722 1384002NM LT COCKPIT CAME OPEN A FDEAA UNSCHED LANDING O OTHER ININSP/MAINT 1 SO04195FE 19144 ON ROTATION L/H SLIDING WINDOW CAME OPEN. TESTED CAPTS L2 WINDOW (SLIDING WINDOW) PER 727 MM 56-12-11 PG 505 PARA A, NO DEFECT NOTED. INSPECTED ENGINE INLETS AND EXHAUSTS, NO DEFECTS NOTED. 2L73 4F A3WE 19950324000971995032400097SO 1995 3 24 COM11825 119950317A61207902013 ACTUATOR EMB 120 EMB120RT SO HAMSTD14RF 14RF9 NE LT LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01265CA7958 139 120257 891014 LEFT ENGINE LEAKING OIL FROM THE PROPELLER AREA. REPLACED THE PROPELLER ACTUATOR ASSY. 2L72 4T RTA31SO 6 CP11NE 19950324000981995032400098SO 1995 3 24 COM11826 119950317A3230MS3476L106P CONNECTOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01259CA 120252 LANDING GEAR WOULD NOT RETRACT. REPLACED THE WOW PROXIMITY SENSOR WIRING CONNECTOR ON THE RT MLG. 2L72 4T RTA31SO 19950324000991995032400099SO 1995 3 24 COM11827 119950318A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01257CA8654 8654 120248 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I, AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT NR 1327-2. P/N 120-17056-013, 120-17056-015 (4 EA), 120-17056-017 (2 EA), 120-17056-007 (8 EA), 120-17057-005 (2 EA), 120-17057-007, 120-17056-019. 2L72 4T RTA31SO 19950324001001995032400100EA 1995 3 24 COM60442 119950316A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 EA PILOTS SHATTERED A COMAK NONE O OTHER UKUNKNOWN 1 SO01916CA4566 7014 PILOTS FRONT WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 19950324001011995032400101NM 1995 3 24 SCNA95038 119950315A335090052 EEL POWER SUPPLY BOEING727 7272A1 138407FNM RT OVERWING FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 RIGHT CENTER OVERWING EMERGENCY LAMP INOPERATIVE. REMOVED AND REPLACED EMERGENCY LAMP POWER SUPPLY. LAMP OPS CHECKED GOOD. 2L73 4F A3WE 19950324001021995032400102NM 1995 3 24 SCNA95039 119950315A524165569924 R2 DOOR BOEING727 727259 138408JNM AFT GALLEY NOT LATCHED A ASCNAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15289SC 22475 CABIN BEGAN RAPID CLIMB WITH AIRCRAFT CLIMBING THROUGH 18,OOO FEET. AN ON BOARD MECHANIC NOTED AIR LEAK AT AFT GALLEY DOOR. FOUND DOOR NOT FULLY LATCHED AT BOTTOM. DOOR WAS INSPECTED INSIDE AND OUT FOR DAMAGE AND LEAKS, NONE FOUND. OPERATIONAL CHECK AND INDICATIONS ALL NORMAL, OK FOR SERVICE. 2L73 4F A3WE 19950324001031995032400103NM 1995 3 24 SCNA95040 119950317A3350900542 EEL BATT CHARGER BOEING727 7272J4 1384006NM L-2 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 L-2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER M1092, AND BATTERY PACK AT L-2 DOOR. OPS CHECK GOOD. 2L73 4F RTA3WE 19950324001041995032400104NM 1995 3 24 UPS202665 119950315A3260 SWITCH BOEING727 72731C 1384011NM RT MLG FAILED A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01924UP 19234 PILOT REPORTED RIGHT MAIN GEAR NO GREEN LIGHT. CYCLED GEAR, STILL NO LIGHT (GOOD TEST), 25 FLAPS, HORN (WARNING), RECEIVED GREEN LIGHT 25 SECONDS AFTER HANDLE WAS DOWN. MX REPLACED DOWNLOCK POSTION SWITCH IAW MM 32-61-22 AND REPLACED LANDING GEAR ELECTICAL MODULE IAW MM 32-09-111. PERFORMED GEAR SWING IAW MM 07-11-00, NO DEFECTS NOTED. 2L73 4F A3WE 19950324001051995032400105NM 1995 3 24 UPS202666 119950316A2751 TORQUE TUBE BOEING727 72762C 138402CNM TE FLAPS DISCONNECTED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01913UP 19245 SUPPLEMENTAL MRR - PILOT REPORTED WHEN RETRACTING FLAPS AFTER TAKEOFF, THE INBOARD TRAILING EDGE ASYMMETRY FLAPS STOPPED AT 5 DEGREES. THE LEFT FLAPS READ 2 DEGREES, RIGHT READ 5 DEGREES. FLIGHT CREW DECLARED EMERGENCY AND RETURNED TO DSM. FOUND TORQUE TUBE DISCONNECTED. RECONNECTED TORQUE TUBE AND RIGGED FLAP PER MM 27-51-00. 2L73 4F A3WE 19950324001061995032400106NM 1995 3 24 UPS202676 119950320A5754 SKIN BOEING727 72751C 1384015NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LEADING EDGE SKIN OF NR 6 SLAT 20 INCHES DOWN AND 50 INCHES OUTBOARD OF INBOARD END AT A FASTENER. MX REMOVED DAMAGE AND REPAIRED PER SRM 57-50-1, 57-50-3 AND INSTALLED PER SRM 51-30-2. 2L73 4F A3WE 19950324001071995032400107NM 1995 3 24 UPS202677 119950320A5320 SUPPORT BOEING727 72751C 1384015NM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND SUPPORT TO BE CORRODED BEYOND LIMITS AT STA 740-760, LBL 62, WL 208. MX REPLACED SUPPORT IAW SRM 51-10-1. 2L73 4F A3WE 19950324001081995032400108NM 1995 3 24 UPS202678 119950320A5320 CLIP BOEING727 72751C 1384015NM BS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND UPPER T-CLIP CRACKED IN RADIUS AT STA 740, RBL 25, WL 201. MX REPLACED T-CLIP IAW SRM 51-10-1, 51-10-2, 51-20-1, 51-20-4 AND 51-30-2. 2L73 4F A3WE 19950324001091995032400109NM 1995 3 24 UPS202679 119950320A3221 BEAM BOEING727 72751C 1384015NM NLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK INDICATIONS IN THE NLG BEAM FWD OUTBOARD FLANGE. MX REPAIRED IAW SRM 51-30-2, 51-10-2, MM 51-20-151 AND UPS EO B727-5310-0543. 2L73 4F A3WE 19950324001101995032400110NM 1995 3 24 UPS202680 119950320A5712 RIB BOEING727 72751C 1384015NM BS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK INDICATIONS IN THE FWD 2 HOLES IN RIB CHORD AT STA 760, LBL 70.5. MX REPAIRED IAW UPS EO B727-5710-1271-F, APPENDIX F. 2L73 4F A3WE 19950324001111995032400111NM 1995 3 24 UPS202681 119950320A5250 GATE BOEING727 72751C 1384015NM MID GALLEY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON MID GALLEY DOOR LOWER HORIZONTAL GATE BEAM UNDER NUTPLATES. MX REPLACED LOWER GATE IAW SRM 51-30-2, 51-30-5 AND 51-10-2. 2L73 4F A3WE 19950324001121995032400112WP 1995 3 24 UPS802667 119950320A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND 2 SHEAR TIES CRACKED AT STA 640, AFT AND FWD OF LONGERON 27L. MX REPAIRED SHEAR TIES PER SRM 53-2-0 FIGURE 2A. 2L74 4F RT4A25 19950324001131995032400113WP 1995 3 24 UPS802668 119950320A5320 FITTING DOUG DC8 DC871F 302199DWP BS 781 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND 2 FLOOR BEAM FITTINGS CRACKED AT STA 781, RBL 48 AND LBL 48. MX REPLACED FITTINGS PER SRM 51-1-20D. 2L74 4F RT4A25 19950324001141995032400114WP 1995 3 24 UPS802669 119950320A5320 FITTING DOUG DC8 DC871F 302199DWP BS 759 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND FLOOR BEAM FITTING CRACKED AT STA 759, LBL 48. MX REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950324001151995032400115WP 1995 3 24 UPS802670 119950320A5753 VANE DOUG DC8 DC871F 302199DWP LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND LEFT WING NR 5 FLAP VANE DELAMINATED AT LOWER SURFACE. MX REPLACED VANE PER MM 27-51-14. 2L74 4F RT4A25 19950324001161995032400116WP 1995 3 24 UPS802671 119950320A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND FUSELAGE FRAME FITTING CRACKED JUST FWD AND BELOW LIMIT SWITCH, STA 1240, LONGERON 25R. MX REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950324001171995032400117WP 1995 3 24 UPS802672 119950320A5753 VANE DOUG DC8 DC871F 302199DWP RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND RIGHT WING NR 5 FLAP VANE DELAMINATED. MX REPLACED VANE PER MM 27-51-14. 2L74 4F RT4A25 19950324001181995032400118WP 1995 3 24 UPS802673 119950320A5755 SKIN DOUG DC8 DC871F 302199DWP NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 1 SPOILER UPPER SURFACE DELAMINATED ON LEFT WING. MX REPLACED SPOILER ASSY PER MM 27-61-01. 2L74 4F RT4A25 19950324001191995032400119WP 1995 3 24 UPS802674 119950320A5311 BELTFRAME DOUG DC8 DC871F 302199DWP BS 1040 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND BELTFRAME WITH 2 INCH CRACK AT STA 1040 BETWEEN LONGERON 20R AND 21R. MX REPLACED FRAME SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950324001201995032400120WP 1995 3 24 UPS802675 119950320A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 1600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND SHEAR TIE CRACKED 2 INCHES AT STA 1600, LONGERON 23L. MX REPLACED SHEAR TIE PER SRM 53-2-0. 2L74 4F RT4A25 19950324001421995032400142NM 1995 3 24 AALA950249 119950212A3350 EEL WIRE BOEING767 767323 1385205NM CABIN NEED RESECURING A AALAK NONE L NO TEST ININSP/MAINT 1 SW07384AA 26996 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE MID-GALLEY BY PASSENGER SEAT 19EF FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT WIRE AT RT AISLE BY PASSENGER SEAT 19EF. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950324001431995032400143NM 1995 3 24 AALA950266 119950213A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN NEED RESECURING A AALAK NONE L NO TEST ININSP/MAINT 1 SW07358AA 24039 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PASSENGER SEATS 7AB, 12AB, 34AB, TO AFT LAVATORY, AND 40HJ FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHTS CONNECTORS AT PASSENGER SEATS 7AB AND 34AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950324001441995032400144NM 1995 3 24 AALA950268 119950213A33500L3071BPEGL EEL LAMP BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07321AA 22322 SFO - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT SEATS 8B AND 9B FOUND INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT SEATS 8B AND 9B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950324001451995032400145NM 1995 3 24 AALA950281 119950219A3350 EEL WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 26AB AND 33AB FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT 26AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950324001461995032400146 1995 3 24 AALA950317 419950223A2565CBB3335 SLIDE BOEING727 727227 1384078NM PASSENGER DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07725AA A2590 20732 ORD - DURING SHOP VISIT FOUND 2 RUNWAY SEAM SEPARATIONS OF 8 INCHES AND A FRAYED LATCH ASSEMBLY ON THE EMERGENCY EVACUATION SLIDE. ROUTED FOR REPAIR. (X) 2L73 4F A3WE 19950324001471995032400147NM 1995 3 24 AALA950332 119950225A300065222723 DUCT BOEING727 727223 1384074NM NR 2 ENGINE CRACKED A AALAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 SW07871AA 21383 JFK - FLT 1251 - AFTER TAKEOFF EWR DURING CLIMB-OUT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED WHEN NR 2 POWER LEVER WAS RETARDED TO IDLE. JETTISONED FUEL AND AIRCRAFT DIVERTED TO JFK, LANDING WITHOUT INCIDENT. REPAIRED NR 2 ENGINE FIREWALL THERMO ANTI-ICE DUCT FOUND CRACKED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950324001481995032400148SO 1995 3 24 ASOA95005 119950205A5210 WARNING EMB 120 EMB120RT SO PASSENGER DOOR ACTIVATED A ASOAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO11233AS 120031 ATL/MYR - FLT 7385 - EN ROUTE AT 23,000 FEET, CREW HEARD A POP FROM BEHIND LEFT SEAT. AT THE SAME TIME, RECEIVED FORWARD DOOR WARNING. DECIDED TO DIVERT FLIGHT TO AGS WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. CHECKED ALIGNMENT MARKS AND DISCUSSED PROBLEM WITH MAINTENANCE CONTROL. ALL CHECKS WERE GOOD AND NO DEFECTS OR ABNORMALITIES WERE NOTED. CONTINUED FLIGHT TO MYR. TAT 21506.67. (X) 2L72 4T RTA31SO 19950324001491995032400149SO 1995 3 24 ASOA95006 119950207A2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A AASOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11239AS 120057 CRW/ATL - FLT 7060 - AFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT. DUE TO RUNWAY CONDITIONS AT CRW, DIVERTED FLIGHT TO TRI WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. OPERATED FLAPS ON GROUND FROM 0-45 DEGREES SEVERAL TIMES WITH NO DEFECTS NOTED. PULLED FLAP CONTROL UNIT AND RERACKED WITH NO DEFECTS NOTED. CYCLED FLAPS AGAIN, OPERATIONAL CHECK GOOD. CONTINUED FLIGHT TO ATL. TAT 20590.36. (X) 2L72 4T RTA31SO 19950324001501995032400150NE 1995 3 24 ASOA95007 219950208A7261 SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 ENGINE FAILED A ASOAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO11223AS 120021 115059 ATL/GNV - FLT 7180 - NR 2 ENGINE INDICATED LOW OIL PRESSURE AND WARNING UPON ARRIVAL INTO ATL FROM GNV. REDUCED POWER BELOW 75 PERCENT NH AND OBSERVED PSID IN YELLOW ARC (AROUND 50 PERCENT PSID). CONTINUED APPROACH AND LANDED WITHOUT INCIDENT. AFTER LANDING, SHUT DOWN RIGHT ENGINE TO PRECLUDE ENGINE DAMAGE. REMOVED AND REPLACED RIGHT ENGINE CENTRIFUGAL BREATHER CARBON SEAL. LEAK AND OPERATIONAL CHECK GOOD. TAT 21460.1. (X) 2L72 4T4 TRTA31SO E20NE 19950324001511995032400151SO 1995 3 24 ASOA95008 119950210A2910 HYDRAULIC LINE EMB 120 EMB120RT SO LANDING GEAR FAILED A ASOAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11230AS 120032 ATL/ABY - FLT 7002 - EN ROUTE, BLUE HYDRAULIC SYSTEM FAILED. ON FINAL APPROACH TO ATL, GEAR WOULD NOT COME DOWN. EXECUTED FREE FALL OF GEAR AND GEAR EXTENDED. LANDED IN ATL SAFELY AND WITHOUT INCIDENT. REPLACED HYDRAULIC LINE ON RIGHT HYDRAULIC RESERVOIR. OPERATIONAL AND LEAK CHECK GOOD. GEAR SWING COMPLIED WITH DUE TO FREE FALL PROCEDURE. GEAR OPERATIONAL CHECK GOOD. TAT 20684.62. (X) 2L72 4T RTA31SO 19950324001521995032400152SO 1995 3 24 ASOA95009 119950220A7931310573501 VALVE EMB 120 EMB120RT SO NR 1 ENGINE DEFECTIVE A ASOAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 SO11240AS 120060 ATL/ILM - FLT 7503 - EN ROUTE, THE NR 1 ENGINE OIL PRESSURE WENT BELOW 40 PSI. SHUT DOWN NR 1 ENGINE AND DIVERTED FLIGHT TO AGS WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE OIL PRESSURE REGULATOR VALVE. OPERATIONAL AND LEAK CHECKS GOOD. TAT 19719.97. (X) 2L72 4T RTA31SO 19950324001531995032400153SO 1995 3 24 ASOA95010 119950223A2750 CONNECTOR EMB 120 EMB120RT SO TE FLAPS DIRTY A ASOAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SO11269AS 120210 LYH/ATL - FLT 7247 - AFTER TAKEOFF, RECEIVED A FLAP ASSYMETRY ON OUTBOARD PAIR WITH ROLL TENDENCY. DECLARED AN EMERGENCY AND RETURNED FLIGHT LYH WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. CLEANED CANNON PLUGS AND RECEPTACLES AT OUTBOARD ACTUATORS. DROVE ALL FLAP PAIRS TO ZERO AND THE AIRCRAFT WAS FERRIED FROM LYH TO ATL. INSPECTED ENTIRE FLAP SYSTEM WITH NO DEFECTS NOTED. SUBSEQUENT MAINTENANCE ACTION - REPLACED FLAP ROLLERS AND RIGHT OUTBOARD FLAP. TAT 11255.2. (X) 2L72 4T RTA31SO 19950324001541995032400154NE 1995 3 24 CAL950143 219950222A75301555M23G01 DUCT ASSY AIRBUS300 A300B4103 3930104EU GE CF6 CF650C2 30018NE NR 1 ENG RUPTURED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0913983334523102 92 517709 FLT NR 668 - MCO - THE NR 1 ENG EXPERIENCED BLEED LOSS AND FIRE WARNING AFTER TAKEOFF. THE EGT ROSE TO 955 DEGREES. THE NR 1 ENGINE THRUST WAS REDUCED AND THE FIRE WARNING CEASED. THE A/C WAS RETURNED TO MSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENG 14TH STAGE DUCT RUPTURED WHICH RESULTED IN DAMAGE TO OTHER DUCTS, LINES, AND THE THRUST REVERSER. S/D - THE FAILURE WAS DUE TO HIGH VIBRATORY STRESSES IN THE 14TH STAGE CDP AIR TUBE RESULTING FROM THE 14THE STAGE AIR BLEED TUBE. THE CF6-50 FLEET HAS BEEN MODIFIED BY REMOVING THE 14TH STAGE AIR BLEED TUBE PER GE SB 75-071 (M) 2L72 4F4 F A35EU E23EA 19950324001551995032400155EU 1995 3 24 CAL950149 119950225A2750CHA1058008B TRANSMISSION AIRBUS300 A300B4203 3930306EU NR 4 TE FLAP BINDING A ACALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW091497610662 271 LAX - FLT 0199 - THE FLAPS WOULD NOT EXTEND FOR LANDING ON APPROACH TO LAX. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH, BUT THE FLAPS WOULD NOT EXTEND. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 4 RT FLAP TRANSMISSION JAMMED. THE NR 4 FLAP TRANSMISSION WAS REMOVED AND REPLACED. IN ADDITION, BOTH WING FLAP SYSTEMS WERE RERIGGED IAW MM 27-51-00. THE FLAPS WERE EXTENDED AND RETRACTED SEVERAL TIMES AND OPERATION CHECKED GOOD. (X) 2L72 4F A35EU 19950324001561995032400156NM 1995 3 24 CAL950154 119950215A5320 SUPPORT BOEING727 727232 1384082NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778063832 20635 DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 312, RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X) 2L73 4F A3WE 19950324001571995032400157NM 1995 3 24 CAL950155 119950215A5320 SUPPORT BOEING727 727232 1384082NM BS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778063832 20635 DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 344, BBL ZERO TO RBBL 48.75. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X) 2L73 4F A3WE 19950324001581995032400158NM 1995 3 24 CAL950156 119950215A5320 SUPPORT BOEING727 727232 1384082NM BS 320 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778063832 20635 DEN - INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 320, RBBL 12. THE CORRODED SECTION OF FLOOR SUPPORT WAS REMOVED AND A NEW SECTION WAS INSTALLED PER SRM 53-10-8. (X) 2L73 4F A3WE 19950324001591995032400159NM 1995 3 24 CAL950163 119950215A5320 ANGLE BOEING727 727243 138408DNM BS 700 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A 2 INCH CRACK AT BOTH ENDS OF BOTTOM CENTER ANGLE AT FS 700. THE ANGLE WAS REMOVED AND THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1 AND SRM 51-30-2. REPAIRS WERE INSTALLED IAW SRM 51-30-2. (X) 2L73 4F RTA3WE 19950324001601995032400160NM 1995 3 24 CAL950164 119950215A5315 FLOOR BEAM BOEING727 727243 138408DNM BS 344 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A 1.25 INCH CRACK IN STRAP AT LOWER SIDE OF FLOOR BEAM, BS 344. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19950324001611995032400161NM 1995 3 24 CAL950165 119950215A5311 FRAME BOEING727 727243 138408DNM BS 760.95 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A 1 INCH CRACK IN WEB AT RT STA 760.95 OVERWING EXIT FRAME. THE CRACK WAS LOCATED AT THE FIRST HOLE UNDER FLOOR LINE. THE CRACK WAS REPAIRED BY INSTALLING A REPAIR ANGLE, FILLER, SHIMS, AND SILL SPLICE IAW BOEING DRAWING 65C36279-2. (X) 2L73 4F RTA3WE 19950324001621995032400162NM 1995 3 24 CAL950166 119950215A5320 STIFFENER BOEING727 727243 138408DNM BS 308 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND CORRODED STIFFENER ON TOP OF DOG HOUSE AT BS 308. THE STIFFENER WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-20-4. (X) 2L73 4F RTA3WE 19950324001631995032400163NM 1995 3 24 CAL950167 119950215A5743 BRACKET BOEING727 727243 138408DNM RT LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A .75 INCH CRACK IN RT WING, NR 5 LEADING EDGE SLAT ACTUATOR ATTACH BOLT BRACKET. A REPAIR WAS PERFORMED IAW SRM 51-30-2 AND BOEING DRAWING 65-17276. (X) 2L73 4F RTA3WE 19950324001641995032400164NM 1995 3 24 CAL950168 119950228A5230 SEALANT BOEING727 727227 1384078NM CARGO DOOR MISSING A CALAAG UNSCHED LANDING O2 MASK DEPLOYED O OTHER CRCRUISE 1 SW0916758 21043 JAX - FLT 0364 - CABIN PRESSURE WAS LOST AT FL290 & OXYGEN MASKS DEPLOYED. CREW SWITCHED FROM AUTO TO STANDBY TO MANUAL, BUT CABIN PRESS COULD NOT BE CONTROLLED. BLEEDS WERE SWITCHED, BUT CABIN STILL WOULD NOT PRESS. ACFT DIVERTED TO JAX. MX FOUND AFT CARGO DOOR SEALANT MISSING BETWEEN SEAL CHANNEL & FUSELAGE AT LOWER FWD & AFT SECTION OF DOOR FRAME. AREA RESEALED USING AERODYNAMIC SEALANT, DECAY CHECK PEFORMED PER MM 5-51-101 & SYSTEM CHECKS GOOD. IN ADDITION, CABIN PRESS CONTROLLER REMOVED & REPLACED AS A PRECAUTIONARY MEASURE. MX FOUND ALL OXYGEN MASKS HAD DROPPED FROM THEIR PSU'S. ALL OXYGEN MASKS WERE CLEANED & STOWED. (X) 2L73 4F A3WE 19950324001651995032400165NM 1995 3 24 CAL950169 119950302A2750 TOGGLES BOEING737 7373T0 1384582NM LT TE FOREFLAP BENT A CALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 SW0969351 23589 CLE - FLT 0150 - AIRCRAFT BEGAN TO ROLL WHEN FLAPS WERE EXTENDED ON FINAL APPROACH TO CLE. FOUR UNITS OF RIGHT AILERON WITH RUDDER TRIM AT ONE UNIT RIGHT WAS REQUIRED TO MAINTAIN CONTROL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT OUTBOARD FOREFLAP TOGGLES BENT. BOTH THE INBOARD AND OUTBOARD TOGGLES WERE REPLACED PER MM 27-51-47. THE FLAPS WERE CYCLED THROUGH FULL RANGE AND ALL OPERATION WAS NORMAL. (X) 2L72 4F RTA16WE 19950324001661995032400166NM 1995 3 24 IXKA9500007 119950223A7331 CONNECTOR AMETEK 8TJ95GAB4 BOEING727 727225 1384077NM NR 1 FUEL FLOW DIRTY A IXKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25354PA 00001 20624 AFTER TAKEOFF, FLT NR 9003 RETURNED TO EWR AFTER ALL F/F INDICATORS FAILED. REMOVED AND REPLACED FUEL FLOW POWER SUPPLY PER MM 73-31-12. OPS OK. FURTHER INVESTIGATION DETERMINED WIRE NR 198-14 SHORTED TO LFT ANTI-ICE VALVE C/P. REPAIRED WIRE AND REPLACED P90 PLUG OF NR 1 F/F TRANSMITTER DUE SATURATION, PER 73-30. OP CHECK OK. AFTER BENCH CHECK OF F/F POWER SUPPLY BY AMETEK THERE WAS NO FAULT FOUND WITH UNIT. (W) 2L73 4F A3WE 19950324001671995032400167NM 1995 3 24 IXKA9500008 119950223A7331 CONNECTOR BOEING727 727225 1384077NM NR 1 FUEL FLOW DIRTY A IXKAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA25354PA 20624 AFTER TAKEOFF EWR, FLT NR 9003, RETURNED TO EWR FOR SECOND TIME. AFTER ALL FUEL FLOW INDICATORS FAILED. FOUND WIRE NR 198-014-18 SHORTED TO LEFT ANTI-ICE VALVE C/P. REPAIRED WIRE AND REPLACED P90 PLUG OF NR 1 FUEL FLOW TRANSMITTER DUE SATURATION. (W) 2L73 4F A3WE 19950324001681995032400168SW 1995 3 24 MALA954318 119950213A52302724050113 PIN SWRNGNSA227 SA227AC 8780603SW CARGO DOOR BENT A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL1563NE AC763B MSP - FLT 3295 - IN CRUISE FLIGHT, THE CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT AT A 4.0 DIFFERENTIAL. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED A BENT BAYONET PIN. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950324001691995032400169SW 1995 3 24 MALA954321 119950214A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 441.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 MSP - DURING SCHEDULED INSPECITON, AFT CARGO DOOR FRAME FOUND CRACKED AT FS 441.06. REPAIRS WERE COMPLETED BY REPLACING DAMAGED AREA WITH A REPAIR DOUBLER IAW FAC LAR-95-MALA-052. (X) 1L72 4T A8SW 19950324001701995032400170NM 1995 3 24 MALA954322 119950216A573085520057104 SKIN DHAV DHC8 DHC8102 2809003NM RT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15861MA 362 CKB - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND TRAILING EDGE ON THE RIGHT INBOARD UPPER SKIN CRACKED AND TWO LOOSE ATTACHING RIVETS NEAR THE STATIC WICK. MAINTENANCE FABRICATED AND INSTALLED A NEW SECTION IAW DHC-8 SRM 51-23-00. SKIN, 85520057-104. (X) 2H72 4T RTA13NM 19950324001711995032400171SW 1995 3 24 MALA954323 119950216A32301EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER O OTHER CLCLIMB 1 GL15422MA AC635 YNG - FLT 3147 - ON CLIMB-OUT, NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND THE PROBLEM WAS CORRECTED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950324001721995032400172SW 1995 3 24 MALA954326 119950221A57532731141001 ROLLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND LEFT FLAP TRACK ROLLER DOUBLER, PN 27-31141-001, WORN AT WS 27.103. REPAIRS WERE COMPLETED THROUGH A PART FOR PART REPLACEMENT IAW FAC SRM 51-00-00, PAGE 4, FAC ARP 57-20-9424, AND FAC LAR 95-MALA-056 AND STANDARD PRACTICES. (X) 1L72 4T A8SW 19950324001731995032400173NM 1995 3 24 MALA954330 119950222A323010800113 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15822MA 326 DTW - FLT 3120 - ON APPROACH, RT MAIN GEAR FAILED TO EXTEND. THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION AND THE GEAR WENT TO THE DOWN AND LOCKED POSITION. MAINTENANCE REPLACED RT MLG UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001741995032400174NM 1995 3 24 MALA954332 119950221A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15854MA 357 DURING A MAINTENANCE GATE WALK-AROUND, THE COCKPIT OVERHEAD EMERGENCY LIGHT ABOVE THE JUMP SEAT WAS FOUND INOPERATIVE. MECHANICS REPLACED THE HAND HELD EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001751995032400175SW 1995 3 24 MALA954333 119950223A53112722104047 FRAME SWRNGNSA227 SA227AC 8780603SW FS 212.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22104-047 AT FS 212.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001761995032400176SW 1995 3 24 MALA954334 119950223A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 144.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-146 AT FS 144.24, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001771995032400177SW 1995 3 24 MALA954335 119950223A53112722093153 FRAME SWRNGNSA227 SA227AC 8780603SW FS 197.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LT LOWER BELT FRAME, PN 27-22093-153 AT FS 197.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001781995032400178SW 1995 3 24 MALA954336 119950223A53112122093155 FRAME SWRNGNSA227 SA227AC 8780603SW FS 227.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MAINTENANCE FOUND THE LT LOWER BELT FRAME, PN 27-22093-155 AT FS 227.27, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001791995032400179SW 1995 3 24 MALA954337 119950223A53112722093145 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.060 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING SCHEDULED MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-145 AT FS 174.060, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001801995032400180SW 1995 3 24 MALA954338 119950223A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.247 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RT LOWER BELT FRAME, PN 27-22093-146 AT FS 159.247, CRACKED AT THE UPPER OUTBOARD FLANGE RELIEF RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001811995032400181SW 1995 3 24 MALA954339 119950223A5753 DOUBLER SWRNGNSA227 SA227AC 8780603SW WS 27.103 WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING SCHEDULED INSPECTION - MAINTENANCE FOUND THE SUPPORT DOUBLER, PN 27-31141-001, FOR THE LT FLAP WALKING BEAM ROLLER BEARING AT WS 27.103 WORN. COMPLETED REPAIR BY THE PART FOR PART REPLACEMENT OF THE DOUBLER IAW THE FAIRCHILD SRM AND ARP 57-20-9424. (X) 1L72 4T A8SW 19950324001821995032400182SW 1995 3 24 MALA954340 119950223A57202735112026 ANGLE SWRNGNSA227 SA227AC 8780603SW LT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE INBOARD, UPPER WING SKIN TO NACELLE ATTACH ANGLE, PN 27-35112-026, CRACKED AT LT NACELLE. COMPLETED REPAIR TO THE ATTACH ANGLE IAW FAIRCHILD ARP 54-20-9101, REV B AND THE SRM. (X) 1L72 4T A8SW 19950324001831995032400183NM 1995 3 24 MALA954341 119950224A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15831MA 339 DTW - FLT 3043 - DURING POST-FLIGHT INSPECTION, MAIN CABIN DOOR EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE UPPER WARDROBE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001841995032400184SW 1995 3 24 MALA954342 119950227A2730 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RT ELEVATOR ELONGATED HOLES A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 MSP - DURING SCHEDULED MAINTENANCE, MAINTENANCE FOUND THE ATTACHMENT BOLT HOLES OF THE RT ELEVATOR TORQUE TUBE, PN 27-44026-003, ELONGATED. COMPLETED REPAIR TO THE RT ELEVATOR BY REPLACEMENT OF THE TORQUE TUBE IAW FAIRCHILD MM AND SRM. (X) 1L72 4T A8SW 19950324001851995032400185SW 1995 3 24 MALA954343 119950227A53202720085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW CARGO DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND FORWARD FUSELAGE MOUNTED CARGO DOOR FRAME, PN 27-20085, CRACKED AT THE GAS STRUT MOUNT HOLE. COMPLETED REPAIR TO THE FRAME MEMBER IAW FAIRCHILD LAR 94-MALA-224 AND SRM. (X) 1L72 4T A8SW 19950324001861995032400186SW 1995 3 24 MALA954344 119950224A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15438MA AC721 DTW - FLT 3071 - ON APPROACH, NOSE GEAR DOWN AND LOCKED LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED AND LUBED THE GEAR INDICATION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950324001871995032400187SW 1995 3 24 MALA954345 119950227A575327311141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE RT SUPPORT DOUBLER (PN 27-31141-001) FOR THE FLAP WALKING BEAM ROLLER BEARING WORN. COMPLETED REPAIR BY REPLACEMENT OF THE SUPPORT DOUBLER IAW FAIRCHILD SRM AND ARP 57-20-9424. (X) 1L72 4T A8SW 19950324001881995032400188NM 1995 3 24 MALA954346 119950226A2150782709010 ACM DHAV DHC8 DHC8102 2809003NM AFT EQUIP BAY FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15865MA 364 CMI - FLT 3107 - ON APPROACH, CREW NOTED AN ELECTRICAL SMELL IN THE COCKPIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR CYCLE MACHINE. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001891995032400189SW 1995 3 24 MALA954347 119950228A53202722081 DOOR SILL SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND AFT CARGO DOOR SILL (PN 27-22081) CRACKED AT THE CUT-OUT RADIUS FOR FUSELAGE FRAME AT FS 438. COMPLETED REPAIR TO THE CARGO DOOR SILL IAW FAIRCHILD LAR 95-MALA-062 AND SRM. (X) 1L72 4T A8SW 19950324001901995032400190SW 1995 3 24 MALA954348 119950228A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG OUT OF ADJUST A MALAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL1526906 AC654B MSP - FLT 3209 - ON CLIMB-OUT, RT GEAR DID NOT INDICATE UP AND LOCKED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO MSP. MAINTENANCE RERIGGED THE UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950324001911995032400191SW 1995 3 24 MALA954349 119950228A57122731241076 RIB SWRNGNSA227 SA227AC 8780603SW WS 66.58 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND TRAILING EDGE OF RT WING RIB (PN 27-31241-076) AT WS 66.58, CRACKED. COMPLETED REPAIR TO THE TRAILING EDGE OF THE RT WING RIB IAW FAIRCHILD LAR 95-MALA-064 AND SRM. (X) 1L72 4T A8SW 19950324001921995032400192SW 1995 3 24 MALA954350 119950228A53302723000011 SKIN SWRNGNSA227 SA227AC 8780603SW FS 530.81-548.81DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND LOWER AFT FUSELAGE SKIN PANEL (PN 27-23000-011) DENTED BETWEEN STA NR 530.810 AND STA NR 548.810. COMPLETED REPAIR TO THE LOWER AFT SKIN PANEL IAW THE FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001931995032400193SW 1995 3 24 MALA954351 119950228A25712782366904 TRAY SWRNGNSA227 SA227AC 8780603SW RT BATTERY CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND RT BATTERY SUPPORT TRAY ASSEMBLY (PN 27-82366-904) CRACKED. COMPLETED REPAIR BY THE PART FOR PART REPLACEMENT OF THE BATTERY SUPPORT TRAY ASSEMBLY IAW THE FAIRCHILD SRM. (X) 1L72 4T A8SW 19950324001941995032400194SW 1995 3 24 MALA954352 119950227A3260 POSITION IND SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15438MA AC721B MSP - FLT 3270 - ON APPROACH, NOSE GEAR INTRANSIT LIGHT WAS INTERMITTENT DURING GEAR EXTENSION. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, LANDING GEAR POSITION INDICATOR WAS REPLACED. THE SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950324001951995032400195NM 1995 3 24 MALA954353 119950302A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LT MLG MALFUNCTIONED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15830MA 337 MSP - FLT 3203 - ON APPROACH, LEFT MAIN GEAR TOOK 30 SECONDS LONGER THAN THE RIGHT TO INDICATE DOWN AND LOCKED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001961995032400196SW 1995 3 24 MALA954354 119950302A32301EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG OUT OF ADJUST A MALAO OTHER O OTHER CLCLIMB 1 GL15428MA AC646 TOL - FLT 3393 - ON CLIMB-OUT, LEFT GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED GEAR AND THE PROBLEM RECURRED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT GEAR 'UP' POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950324001971995032400197NM 1995 3 24 MALA954355 119950302A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LT MLG LACK OF LUBE A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15831MA 339 DTW - FLT 3118 - ON APPROACH, LEFT GEAR UNSAFE LIGHT TOOK THIRTY SECONDS LONGER TO EXTINGUISH THAN THE RIGHT. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE UPLOCK ROLLER WAS CLEANED AND LUBED. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950324001981995032400198EU 1995 3 24 SIMA950601 119950301A2710S2711009700101 LINK ASSY AEROSPATR42 ATR42300 8680920EU LT AILERON CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21432MQ11106 144 MQT - DURING (IMBV) INTERMEDIATE MAIN BASE VISIT, MAINTENANCE FOUND THE LEFT AILERON TRIM TAB ACTUATOR LINK ASSEMBLY CORRODED. THE LINK ASSEMBLY WAS R&R IAW J1C 271172 - RAI - 10000-002. AILERON SYSTEM FUNCTIONALLY TESTED GOOD IAW JIC 271000-FUT-10000. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 15,290. (X) 2H72 4T RTA53EU 19950324001991995032400199NE 1995 3 24 VTZA95097 219950306A7320 WIRE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT FUEL CONTROL BROKEN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27308UE 41023 P75009 IAD/JFK - FLT 6305 - DURING TAKEOFF AT 1255 HOURS ON 3-6-95, ABORTED THE TAKEOFF DUE TO LT IEC FAILING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED BROKEN WIRING AT FUEL ENRICHMENT TORQUE MOTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950324002001995032400200EU 1995 3 24 VTZA95098 119950306A3246AH52688 TIRE ASSY BAG JETSTMJETSTM3201 1500217EU NOSE GEAR WORN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27473UE 828 IAD/ALB - FLT 6458 - DURING TAKEOFF AT 1700 HOURS ON 3-6-95, ABORTED TAKEOFF DUE TO THE CREW BEING UNABLE TO MAINTAIN DIRECTIONAL CONTROL DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED BOTH NOSE TIRE ASSYS. PERFORMED TAXI CHECKS AT 70 PLUS KNOTS WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324002011995032400201EU 1995 3 24 VTZA95099 119950306A77122236629820 TORQUE RING CONN BAG JETSTMJETSTM3201 1500217EU LT ENGINE DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27484UE 899 CLE/IAD - FLT 6548 - DURING TAKEOFF AT 0630 HOURS ON 3-6-95, ABORTED THE TAKEOFF DUE TO THE LT ENGINE TORQUE FLUCTUATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE TORQUE RING CANNON PLUG AT THE GEAR CASE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324002021995032400202NM 1995 3 24 95ZZZW257 119950217A3350900542 EEL BATT CHARGER BOEING737 737298C 1384490NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, THE AFT CENTER EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH AFTER RECON EMERGENCY LIGHT TEST. REPLACED BATTERY PACK AND CHARGER, LIGHTS OPERATED NORMALLY. REF ASAA9510001. 2L72 4F RTA16WE 19950324002031995032400203NM 1995 3 24 ASAA9510001 119950217A3350900835A EEL BATT PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, THE AFT CENTER EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH AFTER RECON EMERGENCY LIGHT TEST. REPLACED BATTERY PACK AND CHARGER, LIGHTS OPERATED NORMALLY. REF 95ZZZW257. 2L72 4F RTA16WE 19950324002041995032400204NM 1995 3 24 ASAA9510002 119950220A33508731002142 EEL ASSEMBLY BOEING737 737298C 1384490NM WINDSCREEN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE WINDSCREEN EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED 'EXIT TO REAR' LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950324002051995032400205NM 1995 3 24 ASAA9510003 119950224A33506013211 EEL BATT PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE AFT EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT THE L2 AND R2 DOORS. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950324002061995032400206NM 1995 3 24 ASAA9540004 119950227A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01764AS 25101 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING IN AFT CABIN AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950324002071995032400207WP 1995 3 24 ASAA9556 119950208A335060030451 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 PDX - DURING MAINTENANCE CHECK, THE FWD RT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002081995032400208WP 1995 3 24 ASAA9557 119950208A335060030451 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 1 TO 3 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002091995032400209WP 1995 3 24 ASAA9558 119950208A335060030451 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM 16 TO 20 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002101995032400210WP 1995 3 24 ASAA9559 119950209A3350S103 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROW 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002111995032400211NM 1995 3 24 ASAA9569 119950213A3350S417N5048 EEL TRACK BOEING737 7374Q8 NM CABIN DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - PILOT REPORTED, LAST 5 EMERGENCY TRACK LIGHTS DO NOT ILLUMINATE. REPLACED LIGHT SECTION AT ROW 26 AND SECURED LIGHT LENS. (W) 2L72 4F RTA16WE 19950324002121995032400212WP 1995 3 24 ASAA9571 119950215A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING CHECK, CEILING EMERGENCY LIGHTS AT ROWS 6 TO 9, 15 TO 18 AND 26 TO 29 INOP. MAINTENANCE ATTACHED LOOSE GROUND WIRES TO GROUND STUDS. OPS CHECKED NORMAL. (W) 2L72 4F A6WE 19950324002131995032400213WP 1995 3 24 ASAA9572 119950215A3350S283T014X EEL BATTERY PACK DOUG DC9 DC982 3022082WP EXTERIOR DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING CHECK, EXTERIOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK. (W) 2L72 4F A6WE 19950324002141995032400214WP 1995 3 24 ASAA9573 119950215A335041B004AD07G3 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01950AS 53023 SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9 TO 12. REPLACED BATTERIES IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002151995032400215NM 1995 3 24 ASAA9575 119950216A5210507945155 HANDLE BOEING737 7372X6C 1384552NM L1 DOOR FROZEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE L1 DOOR EXTERIOR HANDLE WOULD NOT OPEN DOOR. HEATED AND LUBRICATED DOOR HANDLE, OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950324002161995032400216NM 1995 3 24 ASAA9576 119950216A5210507945178 HINGES BOEING737 7374Q8 NM L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01779AS 25111 SEA - FLT 489 - CREW REPORTED, L1 DOOR HARD TO CLOSE AND MAKES BINDING NOISE. LUBED DOOR HINGES AND GUST LOCK, DOOR OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950324002171995032400217WP 1995 3 24 ASAA9580001 119950217A335060030451 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 SEA - DURING MAINTENANCE CHECK, THE FWD OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPAIRED WIRING, REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002181995032400218WP 1995 3 24 ASAA9580006 119950217A3350P4010014110 EEL BATT PACK DOUG DC9 DC983 3022083WP L2 DOOR DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 SEA - DURING SHOP INSPECTION OF L2 DOOR EMERGENCY EVACUATION SLIDE (REMOVED DUE TO TIME LIMIT) THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE WHEN SLIDE WAS DEPLOYED. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950324002191995032400219WP 1995 3 24 ASAA9580022 119950224A5347TMS6019943 SEAT TRACK DOUG DC9 DC982 3022082WP BS 231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y231, X-45, Z PLUS 0. REMOVED CORRODED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05 PG 8R, 9, 10G AND 10P, 51-10-03 PG 15, 18 AND 21, 51-10-04 PG 1 AND 16, 51-20-00 PG 4A, 7 AND 8, 51-30-01 PG 1 AND 4, 51-30-05 PG 2 AND 7. (W) 2L72 4F A6WE 19950324002201995032400220WP 1995 3 24 ASAA9580026 119950224A5311 FRAME DOUG DC9 DC982 3022082WP BS 636 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND IN FASTENER HOLE AT FRAME AT Y636, X-18, Z-44. REPAIRED FRAME IAW DC-9 SRM 53-01 FIG 2, 51-10-03 PG 15, 51-30-05 PG 1, 2, AND 2A, 51-10-03 PG 3. (W) 2L72 4F A6WE 19950324002211995032400221WP 1995 3 24 ASAA9580027 119950224A5311 FRAME DOUG DC9 DC982 3022082WP BS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1155 BETWEEN LONGERON 29L AND 28R. REPLACED FRAME IAW DC-9 SRM 53-14-03, 51-14-03, 51-30-05, 51-10-02, 51-30-02. (W) 2L72 4F A6WE 19950324002221995032400222WP 1995 3 24 ASAA9580028 119950224A5311 FRAME DOUG DC9 DC982 3022082WP BS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1231 BETWEEN LONGERON 26L AND 29R. REPAIRED FRAME IAW DC-9 SRM 53-03, 51-10-03, 53-01, 53-30-20. (W) 2L72 4F A6WE 19950324002231995032400223WP 1995 3 24 ASAA9580029 119950224A532099360737 ANGLE DOUG DC9 DC982 3022082WP BS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME TO SKIN SUPPORT ANGLE ON FRAME Y1155, X-6, Z-45. REMOVED DAMAGED SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE IAW DC-9 SRM 51-30-05, 51-30-02. (W) 2L72 4F A6WE 19950324002241995032400224WP 1995 3 24 ASAA9580032 119950227A5311 FRAME DOUG DC9 DC982 3022082WP BS 1271 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1271 BETWEEN LONGERON 25L AND 27R. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 51-20-00, 51-30-05, 51-10-03, 53-03. (W) 2L72 4F A6WE 19950324002251995032400225WP 1995 3 24 ASAA9580033 119950227A5311 FRAME DOUG DC9 DC982 3022082WP BS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS27894 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1250 BETWEEN LONGERON 26L AND 29R. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 51-10-03, 51-30-00, 51-30-01, 51-30-02, 51-30-05, 51-30-08, 51-10-03. (W) 2L72 4F A6WE 19950324002261995032400226WP 1995 3 24 ASAA9580034 119950301A5347TMS6019609 CARGO TRACK DOUG DC9 DC983 3022083WP BS 1153 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS12810 53019 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1154, X-14, Z-45. REMOVED CORRODED CARGO TRACK. INSTALLED NEW CARGO TRACK IAW DC-9 SRM 51-01 PG 1, 51-10-03 PG 8 AND 21. (W) 2L72 4F RTA6WE 19950324002271995032400227WP 1995 3 24 ASAA9580035 119950301A5320993607317NC ANGLE DOUG DC9 DC983 3022083WP BS 1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME TO SKIN ATTACH ANGLE AT Y1212, X-5, Z-50. REMOVED CORRODED ATTACH ANGLE. INSTALLED NEW ATTACH ANGLE IAW DC-9 SRM 51-00, 51-30-02 PG 1 AND 8, 51-30-05 PG 12. (W) 2L72 4F RTA6WE 19950324002281995032400228WP 1995 3 24 ASAA9580036 119950301A5311 FRAME DOUG DC9 DC983 3022083WP BY 1309 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1309, X PLUS 7 TO X-5, Z-48. REMOVED CORRODED SECTION OF FRAME. INSTALLED NEW FRAME IAW DC-9 SRM 53-03 FIG 2A, 51-10-03 PG 1, 3 AND 8. (W) 2L72 4F RTA6WE 19950324002291995032400229WP 1995 3 24 ASAA9580037 119950301A5320993061245 MOPSILL DOUG DC9 DC982 3022082WP L2 DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON L2 DOOR MOPSILL BETWEEN GIRT BARS AND FUSELAGE. REMOVED CORRODED MOPSILL CUSP MEMBRANE. INSTALLED NEW MEMBRANE IAW DC-9 SRM 53-05, 51-30-00, 51-30-01, 51-30-02, 51-10-03, TRAMCO EWO 95-8022. (W) 2L72 4F A6WE 19950324002301995032400230NM 1995 3 24 9504155532 119950313A5330 SKIN BOEING757 757251 1384970NM FS 660-670 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01532US 21409 24263 DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 660 - 670 AROUND STRINGER 27R WAS FOUND WITH TYPICAL NICK AND GOUGE DAMAGE CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 AND NWA EA 55-93840. 2L72 4F RTA2NM 19950324002311995032400231NM 1995 3 24 9504165532 119950210A5330 SKIN BOEING757 757251 1384970NM FS 1340-1360 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01532US 21409 24263 DURING PERIODIC CHECK, NUMEROUS NICKS AND SCRATCHES WERE FOUND ON THE FUSELAGE BELLY SKIN BETWEEN FS 1340 - 1360, STR 26R. DAMAGE WAS CAUSED BY CARGO NETS. INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 204 AND NWA EA 55-93835. 2L72 4F RTA2NM 19950324002321995032400232NM 1995 3 24 9504175532 119950214A5330146N3330 SKIN BOEING757 757251 1384970NM FS 1355-1410 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01532US 21409 24263 DURING PERIODIC CHECK, THE FUSELAGE BELLY SKIN BETWEEN FS 1355 - 1410, STR 24L - 26L WAS FOUND WITH NICKS AND GOUGES CAUSED BY CARGO NETS. REMOVED DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-00-01, FIG 205 AND NWA EA 55-93836. 2L72 4F RTA2NM 19950324002331995032400233NM 1995 3 24 9504185515 119950313A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 28929 23203 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE LATERAL FLOOR BEAM UPPER CHORD AT FS 365, LBL 24.75. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-096485. 2L72 4F RTA2NM 19950324002341995032400234NM 1995 3 24 9504195515 119950307A5313146N5416 LONGERON BOEING757 757251 1384970NM FS 1330-1510 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 28929 23203 DURING PERIODIC CHECK, THE AFT CARGO COMPARTMENT FLOOR STRINGERS AT BS 1510 AND 1330 WERE FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIRS PER NWA EA 55-96724 AND 55-96725. 2L72 4F RTA2NM 19950324002351995032400235NM 1995 3 24 9504215515 119950310A5320146N852251 DOOR SILL BOEING757 757251 1384970NM FS 1410 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 28929 23203 DURING PERIODIC CHECK, THE AFT CARGO DOOR LOWER SILL INNER CHORD WAS FOUND CORRODED ON THE TOP AND BOTTOM SIDES AROUND THE NUTPLATE HOLES. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97802. 2L72 4F RTA2NM 19950324002361995032400236NM 1995 3 24 9504332294 119950316A3260 WIRE BOEING727 727251 138408HNM RT MLG BROKEN A NWAAO OTHER P NO WARNING INDICATION UKUNKNOWN 1 GL01294US 21505 DURING LANDING GEAR RETRACTION/EXTENSION, RIGHT GEAR DOOR INDICATION REMAINS EXTINGUISHED. RECYCLED LANDING GEAR WITH SAME RESULTS. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE BEHIND THE RIGHT DOOR SWITCH CANNON PLUG. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950324002371995032400237NM 1995 3 24 9504342705 119950316A3230656021132 LANDING ACC UNIT BOEING727 727225 1384077NM E/E COMPARTMENT FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01802EA7004 22433 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950324002381995032400238NM 1995 3 24 9504352252 119950317A3260 SWITCH BOEING727 727251 138408HNM LANDING GEAR LACK OF LUBE A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01252US 19971 DURING APPROACH UPON LANDING GEAR EXTENSION, ALL GEAR UNSAFE (RED), SAFE (GREEN), AND TAILSKID INDICATIONS REMAINED ILLUMINATED. RECYCLED GEAR WITH PROPER INDICATIONS. MAINTENANCE FOUND THE LANDING GEAR HANDLE DOWN SWITCH STICKING. LUBRICATED SWITCH. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950324002391995032400239NM 1995 3 24 9504366622 119950316A2410 CSD 705117A BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JM WARNING INDICATION OVER TEMP CRCRUISE 1 GL01622US 1913 21704 702055 DURING CRUISE, THE NR 2 ENGINE CSD OIL WARNING LIGHT ILLUMINATED FOLLOWED BY THE GENERATOR OFF AND FIELD OPEN LIGHTS. THE CSD WAS DISCONNECTED AND THE OIL TEMPERATURE CONTINUED TO RISE. THE ENGINE WAS SHUT DOWN, 35,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO NRT WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. THE CSD AND THE OIL TEMPERATURE INDICATOR WERE REPLACED AND A GROUND RUN-UP CONFIRMED PROPER SYSTEM OPERATION. 2L74 4F4 F A20WE E3NE 19950324002401995032400240NM 1995 3 24 9504376614 119950317A7930 OIL BYPASS LIGHT BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 3 ENGINE ILLUMINATED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01614US 20359 662472 DURING CRUISE, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. POWER WAS REDUCED TO FLIGHT IDLE AND THE LIGHT EXTINGUISHED. 2,000 LBS OF FUEL WAS DUMPED AND THE AIRCAFT DIVERTED TO ANC WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. NO CONTAMINATION WAS FOUND IN THE FILTER AND THE FILTER AND PRESSURE SWITCH WERE REPLACED. ENGINE OPERATIONAL CHECK OK ON RUN-UP. 2L74 4F4 F A20WE E20EA 19950324002411995032400241NM 1995 3 24 9504382767 119950318A2910AE7039222 HYD HOSE BOEING727 7272M7 138407SNM A HYD SYST LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 GL010484 21656 EN ROUTE TO CUN, SYSTEM 'A' HYDRAULIC FLUID QUANTITY DECREASED TO LESS THAN ONE GALLON. CREW DECLARED AN EMERGENCY AND PERFORMED ABNORMAL PROCEDURES. FLIGHT RETURNED TO TPA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC PRESSURE HOSE LEAKING AT ENGINE PUMP. REPLACED HOSE, FILTERS, AND CASE. OPERATIONAL CEHCK NORMAL. 2L73 4F A3WE 19950324002421995032400242NM 1995 3 24 9504396614 119950306A5320 DOUBLER BOEING747 747251B 1384892NM FWD LAV CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE DOUBLER FOR THE FORWARD LAV PAN. THE DOUBLER, P/N 65B07388-1 IS .050 INCH 7075-T6. MADE REPAIR PER EA 66-97771. 2L74 4F A20WE 19950324002431995032400243NM 1995 3 24 95FDEA00315 119950319A3620 OVERHEAT LIGHT BOEING727 727227 1384078NM NR 1 ENGINE ILLUMINATED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO04496FE 21670 NR 1 ENG STRUT OVERHEAT LIGHT CAME ON PASSING 10,000 FEET CLIMBING OUT. ENG ANTI-ICE HAD JUST BEEN SHUTOFF, BOTH PACS ON, BLEEDS OPEN ON NR 1 AND NR 3. ABNORMAL PROCEDURES IN RED TABS COMPLIED WITH/ACCOMPLISHED. LIGHT STAYED OUT AS NR 1 THROTTLE READVANCED TO CLIMB SETTING. IAW CHECKLIST NR 1 BLEED AND PAC SHUTDOWN. INSPECTED NR 1 ENG STRUT AREA FOR PNEU LEAKS AND RUBBING OF SENSING ELEMENT. OK FOR SERVICE. 2L73 4F A3WE 19950324002441995032400244WP 1995 3 24 ABXA9500216 119950316A2420 WIRE DOUG DC9 DC941 302207NWP AC GEN SYST BURNED A ABXAO OTHER HB ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23954AX 47612 RIGHT GENERATOR DROPPED OFF LINE WITH CROSS-TIE LOCKOUT. SMOKE IN THE COCKPIT REPORTED. FOUND GENERATOR FEEDER CABLES OVERHEATED BEHIND THE GENERATOR CONTROL PANEL. REPLACED TERMINAL ON MAIN FEEDER CABLE. REPLACED CABLE FROM TERMINAL STRIP TO GENERATOR RELAY. OPS CHECKED GOOD IAW DC-9 M.M. CHAPTER 24. 2L72 4F A6WE 19950324002451995032400245SO 1995 3 24 COM11828 119950320A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO011117H8701 300 120117 DISAGREEMENT WARNING WHEN ATTEMPTING TO RETRACT FLAPS DURING CLIMB. REPLACED RT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950324002461995032400246SO 1995 3 24 COM11829 119950319A7331923111 FUEL FLOW TRANS EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01137H 6823 928 120137 RT ENGINE FUEL FLOW INDICATION FAILED DURING TAKEOFF. REPLACED FUEL FLOW TRANSMITTER. 2L72 4T RTA31SO 19950324002471995032400247SO 1995 3 24 COM11830 119950319A27523203001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION LDLANDING 1 SO01189CA108212660 120189 FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED UP AFTER LANDING. REPLACED THE LEFT OUTBD FLAP HYDRAULIC ACTUATOR. 2L72 4T RTA31SO 19950324002481995032400248NE 1995 3 24 COM11831 219950318A7200PW118 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A COMAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO01159A 116221911 120159 115412 RT ENGINE OIL PRESSURE DROPPED TO 45 PSI. GRINDING NOISE NOTICED. REPLACED ENGINE. 2L72 4T4 TRTA31SO E20NE 19950324002491995032400249SO 1995 3 24 COM11832 119950310A5720 SKIN SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01463CA6615 120267 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 2 EA; 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17057-006, 1 EA; 120-17057-005, 1 EA; 120-17056-013, 1 EA. 2L72 4T RTA31SO 19950324002501995032400250SO 1995 3 24 COM11833 119950317A3230MS3476L106P CONNECTOR EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01168CA 120168 LANDING GEAR CONTROL CANNOT BE SELECTED TO UP POSITION. REPLACED DEFECTIVE WOW PROXIMITY SENSOR WIRING CONNECTOR AT RT MLG. 2L72 4T RTA31SO 19950324002511995032400251SO 1995 3 24 COM11834 119950321A541112009639001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01156CA13938 120156 INSPECTION REVEALED THE LEFT NACELLE OUTBOARD BACK-UP FRAME, ON THE FWD SIDE OF THE HYDRAULIC BAY FIREWALL, TO BE CRACKED. THE BACK-UP FRAME WAS REPAIRED PER AERODESIGN REPORT NR 658-3, REV IR DATED 2-9-94. 2L72 4T RTA31SO 19950324002521995032400252EU 1995 3 24 QXEA9500079 119950318A3350 EEL FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - THE 3 VOLT EVACUATION LIGHT AT THE RT EMERGENCY EXIT IN THE CABIN IS INOPERATIVE. RELAMPED AND OPERATIONAL COMPLIED WITH. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950324002531995032400253EU 1995 3 24 QXEA9500080 119950318A3350 EEL FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - THE 28 VOLT EMERGENCY LIGHT AT THE LEFT CABIN EMERGENCY EXIT IS INOPERATIVE. RELAMPED THE LIGHT ASSEMBLY OPERATIONAL CHECKED GOOD AND A/C WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950324002541995032400254EU 1995 3 24 QXEA9500081 119950318A3350 EEL POWER SUPPLY FOKKERF28 F28MK1000 4990808EU CABIN MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 GEG - THE SERVICE DOOR UPPER EMERGENCY EVACUATION LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW MM 33-50-01, PG. 401, 2A/B. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950324002551995032400255EU 1995 3 24 QXEA9500082 119950318A3350 EEL FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 BOI - FOUND ROW 1 EMERGENCY LIGHT TO BE INOPERATIVE. RELAMPED THE LIGHT ASSEMBLY AND OPERATIONAL CHECK COMPLIED WITH. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950324002561995032400256SW 1995 3 24 QXEA9500084 119950320A7500 BLEED AIR SWRNGNSA227 SA227AC 8780603SW NR 1 ODOR A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM092734X 738 GEG - OIL SMELL IN CABIN, ISOLATED TO THE NR 1 BLEED AIR SYSTEM. NR 1 BLEED PLACED ON MEL 21-4. 1L72 4T A8SW 19950324002571995032400257NM 1995 3 24 QXEA9500085 119950320A302029S505420211 DE-ICE BOOT DORNER 001A716E1000DORNERDO32 DO328100 2996000NM NR 1 ENGINE DEBONDED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09337PH 174 1042 3020 PDX - DE-ICE BOOT IN NR 1 ENGINE IN LEFT COWL FOUND DEBONDED JUST INSIDE LIP FOR AN AREA OF APPROX 144 SQ IN. REPLACED INLET AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950324002581995032400258NM 1995 3 24 QXEA9500086 119950320A302029S505420011 DE-ICE BOOTS DORNER DO1A716E1000DORNERDO32 DO328100 2996000NM NR 1/2 ENGINES DEBONDED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09329PH 10661061 3007 PDX - NR 1 AND NR 2 ENGINE INLETS FOUND WITH DEBONDED DE-ICE BOOTS. REPLACED INLETS AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950324002591995032400259EU 1995 3 24 QXEA9500087 119950320A3350MGG1055 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 PDX - SEVERAL BULBS ARE OUT IN EACH CABIN EXIT SIGN. REPLACED BULBS AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950324002601995032400260NM 1995 3 24 SWAA950231 119950309A33506013211 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0791SW 22963 DURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION, EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950324002611995032400261NM 1995 3 24 SWAA950232 119950314A3260655825029 PC CARD BOEING737 7373H4 1384600NM NLG INOP A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07379SW 26586 IN FLIGHT, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLING GEAR, NO HELP. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFULL LANDING. TROUBLESHOT AND FOUND M983 PC CARD FAULT. REPLACED AND OPERATIONAL CHECKED PER BOEING M/M. 2L72 4F RTA16WE 19950324002621995032400262NM 1995 3 24 SWAA950233 119950314A5311 FRAME BOEING737 7372H4 138448CNM BS 663.75 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0760SW 21812 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STRINGER 3R. REPAIRED PER SWA RA 1-253-1260. 2L72 4F A16WE 19950324002631995032400263NM 1995 3 24 SWAA950234 119950314A5320 CHORD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0774SW 22674 DURING SCHEDULED MAINT CHECK, FOUND BS 178, LBL 5.7, FORWARD CHORD CRACKED. REPAIRED PER SWA RA 1-253-1255. 2L72 4F A16WE 19950324002641995032400264NM 1995 3 24 SWAA950235 119950314A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 308 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0774SW 22674 DURING SCHEDULED MAINT CHECK, FOUND BS 308, LBL 20, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1257. 2L72 4F A16WE 19950324002651995032400265NM 1995 3 24 SWAA950236 119950314A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0774SW 22674 DURING SCHEDULED MAINT CHECK, FOUND BS 360, BL 0, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1258. 2L72 4F A16WE 19950324002661995032400266NM 1995 3 24 SWAA950237 119950314A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0774SW 22674 DURING SCHEDULED MAINT CHECK, FOUND BS 328, RBL 22 TO RBL 48, FORWARD FLANGE, FLOOR BEAM CORRODED. REPAIRED PER SWA RA 1-253-1256. 2L72 4F A16WE 19950324002671995032400267NM 1995 3 24 SWAA950238 119950314A5320 SPLICE BOEING737 7372H4 138448CNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0774SW 22674 DURING SCHEDULED MAINT CHECK, FOUND BS 312, FLOOR BEAM UPPER SPLICE CORRODED. REPAIRED PER SWA RA 1-253-420. 2L72 4F A16WE 19950324002781995032400278SW 1995 3 24 95ZZZX1344 119950220A6410206010765001 BEARING 206011810141BELL 206 206L4 1182110SW ROOT OF BLADE WORN A ALGAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 SW03173AL1295 HB391 52066 TAIL ROTOR PEDALS BINDING. FOUND BLADE BEARING WORN BEYOND LIMITS. SUBMITTER SUGGESTION, CAUSED BY INFERIOR QUALITY BEARINGS. 1G71 3U NCH2SW 19950324002791995032400279GL 1995 3 24 95ZZZX1345 219950210A732323001986 TUBE ASSY BELL 206 206L1 1182107SW ALLSN 250C 250C28B 03013GL ENGINE BROKEN A ALGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0327483 45230 CAE860124 ON TAKEOFF, NOTED THAT N2 RPM DROPPED TO 98 PERCENT AND DID NOT RECOVER. UPON LANDING, RPM RECOVERED TO 100 PERCENT. 1G71 3U3 U H2SW E1GL 19950324002801995032400280NE 1995 3 24 95ZZZX1346 119950210A2910SS48C2C163000 HOSE SKRSKYS76 S76A 8143006NE XMSN AREA LEAKING A ALGAK NONE K FLUID LOSS ININSP/MAINT 1 SW03708AL 760277 AFTER LANDING, COPILOT NOTED HYDRAULIC FLUID COMING FROM LEFT SIDE OF ENGINE INLET COWLING. HOSE ASSY FOUND LEAKING. REPLACE HOSE ASSY. 1G72 3U H1NE 19950324002811995032400281SW 1995 3 24 95ZZZX1347 119950307A24353143503600913 BEARING BELL 206 206L1 1182107SW ARMATURE SHAFT ROUGH A ALGAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW0327545796 45234 ON RUN-UP, FOUND ENGINE MAXIMUM ATTAINABLE N2 RPM WAS 95 PERCENT, ALSO, TORQUE WAS FLUCTUATING. VIBRATION OF STARTER/GENERATOR WAS HARMONICAL WITH THE FUEL CONTROL RPM CAUSING FLUCTUATION. ON DISASSEMBLY OF THE STARTER/GENRATOR, THE BEARING WAS FOUND ROUGH AND GREASE WAS DRY. LUBRICANT IN BEARING APPEARS TO BE THE ABSOLUTE MINIMUM QUANTITY. 1G71 3U H2SW 19950324002881995032400288CE 1995 3 24 95ZZZX1354 119950307A5311 FRAME CESSNA402 402CESSNA 207590KCE NLG BRG BLOCK DAMAGED A OEZAK NONE O OTHER ININSP/MAINT 1 WP193500T11000 4020113 DURING RUN-UP, PILOT REPORTED NOSE GEAR LIGHT WENT OUT. INVESTIGATION REVEALED THE RIB AND FRAME WERE DESTROYED WHERE THE BEARING BLOCK FOR THE NOSE GEAR RETRACTION TORQUE TUBE MEETS WITH THE TRANSMISSION PUSH/PULL TUBE. THE AIRCRAFT HAS FLOWN APPROXIMATELY 200 HOURS SINCE MAJOR REPAIR WAS DONE DUE TO A NOSE GEAR FAILURE. FOUND A LOOSE SCREW ON THE LIMIT SWITCH WIRE TERMINAL AND SUSPECT THIS MAY HAVE CAUSED THE GEAR TO GO FAR AND, THUS, BREAK THE STRUCTURE, BUT AT PRESENT, CANNOT BE SURE. 1L72 3O A7CE 19950324002951995032400295WP 1995 3 24 95ZZZZ134 119950208A792186745 OIL COOLER R2800CB3 DOUG DC6 DC6A 3021706WP NR 3 ENGINE LEAKING A NACAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 AL0399330 2578 31426 43576 FLT NR 431 - SHUTDOWN NR 3 ENGINE DUE TO LOSS OF OIL AT 1907Z. REPLACED OIL COOLER DUE TO LEAKING. (Z) 2L74 4R 6A3 19950324002961995032400296WP 1995 3 24 95ZZZZ135 119950211A32301330046 UPLATCH PIN 5248876 DOUG DC6 DC6A 3021706WP NOSE GEAR SHEARED A NACAK NONE J WARNING INDICATION CLCLIMB 1 AL0399330 43576 NOSE GEAR EXTENDS IN FLIGHT WHEN GEAR HANDLE IS PLACED IN THE NEUTRAL POSITION. REPLACED NOSE GEAR UPLATCH PIN AND SPACER ASSY. (Z) 2L74 4R 6A3 19950324002971995032400297NE 1995 3 24 95ZZZZ136 219950211A8530327628 CYLINDER HEAD DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 4 ENGINE CRACKED A NACAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 AL034206L 2185 43709 35498 FLT 701 - SHUT DOWN NR 4 ENGINE DUE TO BACKFIRING AT 2358Z. REPLACED NR 1 CYLINDER. (Z) 2L74 4R4 R 6A3 E264 19950324002981995032400298NE 1995 3 24 95ZZZZ137 219950207A7320361158 CONTROL LEVER BENDIX PR58E5 DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 CARBURETOR WORN TEETH A NACAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 AL031027N 140 742535 43580 36781 FLT 32 SHUT DOWN NR 4 ENGINE AT 0603Z DUE TO LOSS OF FUEL FLOW AND BMEP. REPLACED MANUAL MIXTURE CONTROL LEVER AND HOUSING ASSY. (Z) 2L74 4R4 R 6A3 E264 19950324002991995032400299CE 1995 3 24 95ZZZZ138 119950205A712011891002537 TRUSS BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GPPAK NONE O OTHER ININSP/MAINT 1 CE0938015 UC14 WHILE COMPLIED WITH AD 92-06-09 A CRACK WAS FOUND IN AREA A OF THE LT TRUSS (RT SIDE). TRUSS WAS REPLACED WITH A NEW 'D' STYLE TRUSS, PN 129-910032-79. AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA24CE 19950324003001995032400300 1995 3 24 95ZZZZ139 419950213A34255222638006 HSI BEECH 1900 1900C 1154161CE LT INST PANEL FAILED A GPPAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE09317BH UB32 FLT NR 2099 - AFTER DEPARTURE FROM DEN, THE CAPTAINS HSI WENT INOP. AIRCRAFT RETURNED TO DEN WHERE GP EXPRESS MAINTENANCE REPLACED THIS HSI WITH A SERVICEABLE UNIT. SYSTEM GROUND CHECKED SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA24CE 19950324003011995032400301NE 1995 3 24 95ZZZZ140 219950302A7261 OIL FILTER DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 ENG CONTAMINATED A Y2PAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23197US 47154 P654600 YIP - RETURNED TO POINT OF DEPARTURE (YIP), NR 1 ENGINE OIL CLOGGED LIGHT ILLUMINATED (ENGINE S/N P-654600). REMOVED OIL FILTER, FOUND CARBON FILTER, DRAINED AND RESERVICED OIL TANK. REPLACED FILTER. (Z) 2L72 4F4 F A6WE E2EA 19950324003021995032400302NM 1995 3 24 95ZZZZ141 119950224A801138322211 STARTER BOEING727 727225 1384077NM NR 3 ENGINE FAILED A TAOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15920TS 20448 DURING CLIMB NR 3 START VALVE LIGHT ILLUMINATED. RETURNED TO BOSTON. REPLACED NR 3 START VALVE, P/N97907021 S/N P1714 AND STARTER P/N 38322211, S/N P63264 ENGINE. RUN UP OK. REFERENCE NR TAOA029514 2L73 4F A3WE 19950324003031995032400303WP 1995 3 24 95ZZZZ142 119950217A5240CFH58S CAM FOLLOWER DOUG DC9 DC982 3022082WP L2 DOOR DEFECTIVE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01931AS 49232 PDX - DURING SERVICING THE L2 SERVICE DOOR WOULD NOT LOCK OPEN OR CLOSE NORMALLY. REPLACED THE DOOR INTERLOCK SPRING AND CAM FOLLOWER AND DOOR OPERATED NORMALLY. REFERENCE ASAA9580003. 2L72 4F A6WE 19950324003041995032400304EU 1995 3 24 95ZZZZ143 119950303A277014191003801 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GUST LOCK OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27306UE 41020 FLT NR 6444 - BDL-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO TAKEOFF WARNING. MAINTENANCE INSPECTED AIRCRAFT AND RELEASED FOR FERRY FLIGHT TO LYH. AIRCRAFT LANDED AT LYH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE MICRO-SWITCH AND ADJUSTED GUST LOCK MICRO SWITCH. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA95093. 2L72 4T RTA41NM 19950324003051995032400305WP 1995 3 24 95ZZZZ144 119950222A5320 ANGLE DOUG DC8 DC862 3021970WP BS 1520 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT ANGLE AT BS 1520 IS CORRODED FROM 12 INCHES RBL TO 45 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003061995032400306WP 1995 3 24 95ZZZZ145 119950222A5320 FLOOR SUPPORT DOUG DC8 DC862 3021970WP BS 1460-1500 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT OVERHEAD FLOOR SUPPORT CORRODED BETWEEN BS 1460 AND BS 1500, 12 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003071995032400307WP 1995 3 24 95ZZZZ146 119950222A5320 WEB DOUG DC8 DC862 3021970WP BS 1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CARGO COMPARTMENT CIRCUMFERRENTIAL WEB CORRODED AT BS 1540 FROM 34L TO 34R. REMOVED CORROSION AND REPLACED SPLICE PLATE PER SRM 51-1-0. 2L74 4F 4A25 19950324003081995032400308WP 1995 3 24 95ZZZZ147 119950222A5620 WINDOW DOUG DC8 DC862 3021970WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/MAIN CABIN WINDOW NR 18R HAS CORROSION ON INSIDE SURFACE OF FRAME. FABRICATED AND INSTALLED REPAIR PER RICH REPAIR SKETCH 5164-6. 2L74 4F 4A25 19950324003091995032400309WP 1995 3 24 95ZZZZ148 119950222A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1586-1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CABIN SQUARE FLOOR SUPPORT FRAME IS CORRODED BETWEEN BS 1586 AND BS 1574. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003101995032400310WP 1995 3 24 95ZZZZ149 119950222A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1606-1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 22 INCHES RBL. REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003111995032400311WP 1995 3 24 95ZZZZ150 119950222A5320 FITTING DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/LONGERON 30 RIGHT END FITTING IS CORRODED AT BS 1530 RIGHT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003121995032400312WP 1995 3 24 95ZZZZ151 119950222A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1480 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1480L AND BS 1520L, 15 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003131995032400313WP 1995 3 24 95ZZZZ152 119950222A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/LONGERON 26 LEFT END FITTING IS CORRODED AT BS 1530 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003141995032400314WP 1995 3 24 95ZZZZ153 119950222A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 9 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950324003151995032400315WP 1995 3 24 ASAA9580003 119950217A524049543411 INTERLOCK SPRING DOUG DC9 DC982 3022082WP L2 DOOR BROKEN A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01931AS 49232 PDX - DURING SERVICING THE L2 SERVICE DOOR WOULD NOT LOCK OPEN OR CLOSED NORMALLY. REPLACED THE DOOR INTERLOCK SPRING AND CAM FOLLOWER AND DOOR OPERATED NORMALLY. (Z) 2L72 4F A6WE 19950324003161995032400316WP 1995 3 24 ORJA9513 119950214A38309041873 DRAIN DISK DOUG DC9 DC983 3022083WP FWD GALLEY MISSING A ORJAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 WP11836RA 53046 RETURN TO SJC, LOUD SQUEALING NOISE STILL PRESENT IN FWD GALLEY AREA. FOUND RESTRICTOR (AIR) MISSING IN FWD GALLEY WATER DRAIN LINES. INSTALLED RESTRICTOR. PRESSURIZED AIRCRAFT TO 4BSID. NO MORE SQUEAL. AIRCRAFT OK TO CONTINUE. (Z) 2L72 4F RTA6WE 19950324003171995032400317WP 1995 3 24 ORJA9514 119950301A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11845RA 49380 ROW 14 OVERHEAD EMERGENCY LIGHTS 3 INOP. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL. (Z) 2L72 4F A6WE 19950324003181995032400318NM 1995 3 24 TAOA029514 119950224A801297907021 START VALVE BOEING727 727225 1384077NM NR 3 ENGINE FAILED A TAOAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15920TS 20448 DURING CLIMB NR 3 START VALVE LIGHT ILLUMINATED. RETURNED TO BOSTON. REPLACED NR 3 START VALVE, P/N97907021 S/N P1714 AND STARTER P/N 38322211, S/N P63264 ENGINE. RUN UP OK. (Z) 2L73 4F A3WE 19950324003191995032400319NM 1995 3 24 TAOA029515 119950226A2120R101AKE5001FC RELAY LEACH BOEING727 727225 1384077NM CABIN FAILED A TAOAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15923TS 20441 RIGHT PACK WENT TO 110 DEGREES AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED SMOKE IN COCKPIT. REPLACED RIGHT FAN DOOR RELAY. OPERATIONAL CHECK OF BOTH PACKS OK. (Z) 2L73 4F A3WE 19950324003201995032400320NM 1995 3 24 USAA950187 119950220A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 986.5-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 10 INCH TOTAL OF CORRODED AREA ON INTERCOSTAL AT BS 986.5 THROUGH BS 1016. REPAIRED PER SRM 53-60-51 AND SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950324003211995032400321NM 1995 3 24 USAA950188 119950206A5320 ANGLE BOEING737 737301 1384611NM BS 727-947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 200 INCH CORRODED AREA STATION 727 TO 767 AND 847 TO 947 RIGHT ANGLE IN AFT CARGO. REPAIRED PER SRM 51-10-02 AND 51-40-02. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950324003221995032400322NM 1995 3 24 USAA950189 119950206A5312 BLKHD ANGLE BOEING737 737301 1384611NM BS 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 36 INCH CORRODED AREA, STATION 947 BULKHEAD LOWER ATTACH ANGLE S-26 R TO S-26L. REPAIRED PER BOEING DRAWING NR PL 65-49616 REV LTR AND SHT 13 OF 73 ID NR 12. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950324003231995032400323NM 1995 3 24 USAA950190 119950207A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19335US26951 23232 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH BY .028 INCH SPOT OF CORROSION BS 1006 RBL 10. REPAIRED PER EA 38836. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (Z) 2L72 4F RTA16WE 19950324003241995032400324EU 1995 3 24 VTZA95084 119950228A7931 OIL PRESS LIGHT JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE ILLUMINATED A VTZAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 EA27306UE 41020 IAD/BOS - FLT 6418 - DURING TAXI AFTER LANDING AT 1320 HRS ON 2-28-95, THE RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE COCKPIT WINDOWS FOGGED FROM HOT AIR ENTERING THE COCKPIT. AIRCRAFT ARRIVED AT GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED GROUND POWER RUNS AND INSPECTED ACM, BUT COULD NOT DUPLICATE DISCREPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR 95ZZZX1392. (X) 2L72 4T RTA41NM 19950324003251995032400325EU 1995 3 24 VTZA95086 119950303A3150 TAKEOFF WARNING JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ACTIVATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27309UE 41022 FLT NR 6517 - IAD-BDL - AIRCRAFT ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING, CREW VERIFIED ALL CONTROLS WERE PROPERLY SET. MAINTENANCE OPS CHECKED TAKEOFF CONFIGURATION WARNING OPS CHECKED GOOD, NO DEFECTS NOTED. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950324003261995032400326EU 1995 3 24 VTZA95087 119950226A21332097J011000 OUTFLOW VALVE JETAIRJETSTMJETSTM4101 1500501EU CABIN CONTAMINATED A VTZAA UNSCHED LANDING GM MULTIPLE FAILURE OVER TEMP CLCLIMB 1 EA27304UE 41017 FLT 6506 - IAD-BOS - RETURNED TO IAD DUE TO PRESSURIZATION INOP IN AUTO MANUAL, CABIN HIGH ALTITUDE AND CABIN OXYGEN LIGHT ILLUMINATED, LEFT AND RIGHT O/T DUCT LIGHT ILLUMINATED AND NO CONTROL OVER CABIN TEMP IN AUTO. MAINTENANCE FROM 1 AND 2 ABOVE OPENED DMI NR 21790 IAW MEL 21-2 ON THE PRESSURIZATION SYSTEM. DMI NR 21790 WAS LATER CLEARED AT LYH BY CLEANING OUTFLOW VALVES SCREEN FILTERS, OPS CHECKED GOOD, CAN NOT DUPLICATE ON GROUND. FOR 3 AND 4 ABOVE PERFORMED OPS CHECK IN BOTH AUTO AND MANUAL WITH BOTH BLEEDS ON FULL BUT COULD FIND NO DEFECTS. (Z) 2L72 4T RTA41NM 19950324003271995032400327EU 1995 3 24 VTZA95088 119950303A52101415201613 SEAL JETAIRJETSTMJETSTM4101 1500501EU PAX DOOR FAILED A VTZAD RETURN TO BLOCK O OTHER CLCLIMB 1 EA27309UE 41022 FLT NR 6411 - IAD-BDL - AIRCRAFT RETURNED TO IAD DUE TO CREW COMPLAINED OF DOOR SEAL LEAK. MAINTENANCE FOUND THAT THE DOOR WAS DEFERRED ALREADY AT TIME OF RETURN. THE DMI NR WAS 02672 IAW MEL 52-6 AND WAS CLEARED 3-5-95 AT IAD. (Z) 2L72 4T RTA41NM 19950324003281995032400328EU 1995 3 24 VTZA95090 119950304A7921HTE860028 WIRE BAG JETSTMJETSTM3201 1500217EU LT OIL COOLER BROKEN WIRE A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27491UE 911 FLT NR 6221 - SWF-IAD - AIRCRAFT RETURNED TO SWF DUE TO OIL COOLER DOOR WOULD NOT INDICATE CLOSED INFLIGHT. MAINTENANCE FOUND BROKEN WIRE AT ACTUATOR, P/N HTE860028. THE WIRE WAS REPAIRED AND OPS CHECKED GOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950324003291995032400329EU 1995 3 24 VTZA95091 119950304A7921SYLC522454 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU LT OIL COOLER FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27310UE 41028 FLT 6305 - IAD-JFK - AIRCRAFT RETURNED IAD DUE TO LEFT OIL COOLER FLAP WOULD NOT CLOSE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE LEFT OIL COOLER ACTUATOR. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950324003301995032400330EU 1995 3 24 VTZA95093 119950303A324091SE16 PARKING BRAKE SW JETAIRJETSTMJETSTM4101 1500501EU MLG FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27306UE 41020 FLT NR 6444 - BDL-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO TAKEOFF WARNING. MAINTENANCE INSPECTED AIRCRAFT AND RELEASED FOR FERRY FLIGHT TO LYH. AIRCRAFT LANDED AT LYH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PARKING BRAKE MICRO-SWITCH AND ADJUSTED GUST LOCK MICRO SWITCH. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950324003311995032400331EU 1995 3 24 VTZA95094 119950309A3230 RETRACT MECH JETAIRJETSTMJETSTM4101 1500501EU RT MLG ICED UP A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27303UE 41015 FLT 6547 - IAD TO LYH - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE RT MAIN INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND GEAR ICED UP. MAINTENANCE DE-ICED LANDING GEAR AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA41NM 19950324003321995032400332EU 1995 3 24 VTZA95095 119950309A3230 RETRACT MECH BAG JETSTMJETSTM3201 1500217EU RT MLG ICED UP A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27474UE 849 FLT 6206 - IAD-CMH - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE RT MAIN INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND GEAR ICED UP. MAINTENANCE DE-ICED LANDING GEAR AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950324003331995032400333EU 1995 3 24 VTZA95096 119950309A3230 RETRACT MECH BAG JETSTMJETSTM3201 1500217EU RT MLG ICED UP A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27483UE 898 FLT 6536 - IAD-LYH - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE RT MAIN INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND GEAR ICED UP. MAINTENANCE DE-ICED LANDING GEAR AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950324003341995032400334WP 1995 3 24 AALA950275 119950218A3350A3030398101 CONNECTOR DOUG DC10 DC1010 3022110WP CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07162AA 46943 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT DOOR 2L INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT CONNECTOR AT DOOR 2L. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950324003351995032400335EU 1995 3 24 AALA950277 119950219A3350A3060819104 EEL STRIP AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0777080 626 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEATS 24B AND 25B INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEATS 24B AND 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950324003361995032400336EU 1995 3 24 AALA950279 119950219A3350A3030398101 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0777080 626 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BY SEAT ROW 27 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT CROSS AISLE BY SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950324003371995032400337EU 1995 3 24 AALA950280 119950218A3350A3060819104 EEL STRIP AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0790070 513 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT 12H AND 15H INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEATS 12H AND 15H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950324003381995032400338WP 1995 3 24 AALA950298 119950220A3350 EEL WIRES DOUG DC10 DC1030 3023501WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07163AA 46914 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT COCKPIT THRESHOLD INOPERATIVE. REPAIRED DAMAGED/BROKEN EMERGENCY FLOOR LIGHT WIRING AT COCKPIT THRESHOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950324003391995032400339NM 1995 3 24 AALA950299 119950216A3350A3060720101 EEL CONDUCTOR BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07694AN 26974 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED FLAT CONDUCTOR WIRES AT FRONT AND BACK OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA2NM 19950324003401995032400340NM 1995 3 24 AALA950301 119950216A3350 EEL BOEING767 767223 1385123NM CABIN MALFUNCTIONED A AALAK NONE O OTHER CRCRUISE 1 SW07334AA 22332 MIA-SFO - FLT 357 - DURING CRUISE, EMERGENCY FLOOR LIGHTS ILLUMINATED THROUGHOUT CABIN FOR APPROXIMATELY 3 MINUTES AND THEN EXTINGUISHED. ACFT PROCEEDED TO SFO WITH NO FURTHER ILLUMINATIONS. ACCOMPLISHED CHECK OF EMERGENCY FLOOR LIGHT SYSTEM WITH NO DEFECTS FOUND. UNABLE TO DUPLICATE PROBLEM. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA1NM 19950324003411995032400341NM 1995 3 24 AALA950305 119950221A3350A3060819104 EEL STRIP DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071755 48490 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTS STRIP AT RT AISLE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F RTA22WE 19950324003421995032400342NM 1995 3 24 AALA950310 119950220A3397 WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07896AA 22012 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT SECTION OF MAIN CABIN INOPERATIVE. REPAIRED BROKEN/SHORTED WIRING AT AFT CABIN EMERGENCY FLOOR LIGHT CONTROLLER. REPLACED EMERGENCY FLOOR LIGHT BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950324003431995032400343 1995 3 24 AALA950322 419950222A2565CBB3335 SLIDE BOEING727 727223 1384074NM RT AFT DOOR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07878AA 21390 ORD - DURING SHOP VISIT, EMERGENCY EVACUATION SLIDE GIRT BAR FOUND DETERIORIATED. EMERGENCY EVACUATION SLIDE INTRODUCED TO SHOP FOR REPAIR AND REPLACEMENT OF GIRT BAR. (W) 2L73 4F A3WE 19950324003441995032400344NM 1995 3 24 AALA950334 119950225A3350LP8095001 EEL LAMP BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07316AA 22318 SFO - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY FLOOR LIGHTS AT PAX SEATS 3B, 4H, 22B AND 33B INOPERATIVE. REPLACED SEAT MOUNTED EMERGENCY FLOOR LIGHT LAMP ASSEMBLIES AT PAX SEATS 3B, 4H, 22B AND 33B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003451995032400345WP 1995 3 24 AALA950337 119950226A3350 EEL WIRE DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07154AA 46709 SFO - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY FLOOR LIGHT CROSS AISLE MARKER AT LOWER RT IN SERVICE CENTER INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT WIRE FOR CROSS AISLE MARKER A LOWER RT IN SERVICE CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950324003461995032400346NM 1995 3 24 AALA950370 119950228A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07379AA 25448 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7H AND 21H INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003471995032400347NM 1995 3 24 AALA950371 119950228A3350LP8095001 EEL BOEING767 767223 1385123NM CABIN MISSING A AALAK NONE L NO TEST ININSP/MAINT 1 SW07329AA 22329 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT ASSEMBLY AT PAX SEAT 3H MISSING. REPLACED MISSING EMERGENCY FLOOR LIGHT ASSEMBLY AT PAX SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003481995032400348NM 1995 3 24 AALA950374 119950227A2530AAP2954 COFFEE MAKER BOEING767 767323 1385205NM GALLEY DEFECTIVE A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07359AA 24040 ORY-ORD - FLT 41 - DURING CRUISE, ELECTRICAL BURNING SMELL AND SMOKE NOTED FROM BEHIND COFFEE MAKERS NR 1 AND 2 IN FIRST CLASS GALLEY. SHUT-OFF ELECTRICAL POWER TO NR 1 AND 2 COFFEE MAKERS AND ACFT PROCEEDED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NR 1 AND 2 COFFEE MAKERS IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003491995032400349NM 1995 3 24 AALA950376 119950302A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 JFK - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTING AT 26AB THROUGH 39AB INOPERATIVE. REPLACED LOOSE CONNECTOR AT 39AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003501995032400350NM 1995 3 24 AALA950377 119950302A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07324AA 22325 SFO - DURING OVERNIGHT EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 8H THROUGH 11H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324003511995032400351WP 1995 3 24 AALA950380 119950304A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07481AA 49656 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 22 AND AFT LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950324003521995032400352NM 1995 3 24 AALA950411 119950308A3620131962 SENSE LINE BOEING727 727223 1384074NM NR 3 ENGINE BROKEN A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07880AA 21519 SJC - FLT 2143 - EN ROUTE MIA-CCS DURING CRUISE, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND LIGHT EXTINGUISHED. ACFT DIVERTED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 3 ENGINE MODULATING VALVE SENSE LINE. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950324003531995032400353WP 1995 3 24 AALA950415 119950307A3350 EEL WIRE DOUG DC10 DC1010 3022110WP CABIN BROKEN A AALAK NONE L NO TEST APAPPROACH 1 SW07166AA 46908 JFK - FLT 678 - DURING APPROACH, EMERGENCY FLOOR LIGHTS AT RT BETWEEN R1 AND R3 DOORS ILLUMINATED. ACFT LANDED JFK WITHOUT INCIDENT. REPAIRED BROKEN/SHORTED WIRING FROM AM1 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950324003541995032400354 1995 3 24 CAL950113 419950209A344220412153112 RADAR IND DOUG DC9 DC932 3022066WP COCKPIT INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09195041222 47638 OKC - FLT 1468 - THE RADAR WENT INOPERATIVE AND WAS ACCOMPANIED BY A BURNING ODOR WHILE EN ROUTE TO OKC. THE RADAR WAS TURNED OFF AND THE ODOR SUBSIDED. THE FLIGHT WAS CONTINUED AND THE ACFT LANDED AT OKC WITHOUT INCIDENT. MAINTENANCE FOUND THE RADAR INDICATOR AT FAULT. THE RADAR INDICATOR WAS REPLACED AND RADAR OPERATION CHECKED GOOD. (W) 2L72 4F A6WE 19950324003551995032400355NM 1995 3 24 CAL950129 119950213A2612 FIRE WARNING BOEING737 7372C0 1384488NM APU ACTIVATED A CALAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW0973243 20072 EWR - FLT 1452 - WHEN THE APU WAS STARTED ON APPROACH, THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. THE APU WAS SHUTDOWN, THE APU FIRE BOTTLE WAS DISCHARGED AND THE FIRE WARNING CEASED. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU AND APU FIRE DETECTION SYSTEM WERE PLACARDED INOPERATIVE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING CORRECTIVE ACTION. THE WIRING AND CONNECTORS ON APU FIRE DETECTION SYSTEM CHECKED GOOD. NO DEFECTS WERE FOUND. OPERATION OF THE FIRE DETECTION SYSTEM AND APU CHECKED GOOD. THE APU FIRE BOTTLE WAS REPLACED AND THE PLACARD WAS REMOVED. (W) 2L72 4F A16WE 19950324003561995032400356NM 1995 3 24 CAL950130 119950214A2612896768 FIRE LOOP BOEING737 737247 138448DNM APU INOPERATIVE A CALAAF UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW0914246 20129 DAB - FLT 1867 - DURING CRUISE, THE APU NOT OPERATING, APU FIRE WARNING LIGHT AND BELL ACTIVATED. THE FIRE BOTTLE WAS DISCHARGED, BUT THE APU FIRE WARNING CONTINUED TO ACTIVATE INTERMITTENTLY. THE ACFT DIVERTED TO DAB, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU AND THE APU FIRE WARNING SYSTEM WERE PLACARDED INOPERATIVE. THE FIRE BOTTLE WAS REPLACED. THE SDR WILL REMAIN OPEN PENDING CORRECTIVE ACTION. THE APU TAILPIPE FIRE DETECTION LOOP WAS REPLACED. BATTERY REPLACEMENT WAS REQUIRED TO START THE APU. THE APU WAS STARTED WITH NO INDICATION OF APU FIRE WARNING. THE APU FIRE DETECTION SYSTEM TESTED GOOD AND BOTH PLACARDS WERE REMOVED. (W) 2L72 4F A16WE 19950324003571995032400357NM 1995 3 24 CAL950159 119950223A5330 SKIN BOEING737 737130 1384435NM BS 940-950 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420664598 19023 GSO - INSPECTION FOUND THE SKIN BULGED AT LAP JOINT STRINGER 19L STA 940 TO 950. THE DAMAGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-6, 53-30-3 AND 51-30-2. (W) 2L72 4F A16WE 19950324003581995032400358NM 1995 3 24 CAL950160 119950223A5712 RIB BOEING737 737130 1384435NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420664598 19023 GSO - INSPECTION FOUND A .5 INCH CRACK IN O/B RIB AT RT WING NR 4 SLAT O/B TRACK. THE CRACK WAS STOP DRILLED AND REPAIR FITTINGS WERE INSTALLED IAW EC 5710-01660. (W) 2L72 4F A16WE 19950324003591995032400359NM 1995 3 24 CAL950171 119950303A3260 SWITCH BOEING727 727232 1384082NM RT MLG DOOR CRACKED A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0933785 20640 IAH - FLT 148 - THE RT MLG DOOR DID NOT INDICATE UP AND LOCKED DURING GEAR RETRACTION AFTER TAKEOFF FROM IAD. THE GEAR WAS CYCLED AND THE RT MLG DOOR INDICATED UP AND LOCKED. MAINTENANCE FOUND THE S399 RT GEAR DOOR SWITCH CRACKED. THE GEAR DOOR SWITCH WAS REMOVED AND REPLACED. GEAR OPERATION AND INDICATIONS CHECKED GOOD. (W) 2L73 4F A3WE 19950324003601995032400360NM 1995 3 24 CALA950158 119950223A5330 SKIN BOEING737 737130 1384435NM BS 970 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420664598 19023 GSO - INSPECTION FOUND THE FUSELAGE SKIN BULGED OVER STRINGER 20L AT STA 970, BELOW REAR ENTRY. THE DAMAGED AREA WAS CUT OUT AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-2 FIG 15 SRM 51-20-4 AND SRM 51-30-2. (W) 2L72 4F A16WE 19950324003611995032400361WP 1995 3 24 USAA950196 119950117A5330 SKIN DOUG DC9 DC931 3022065WP BS 198 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK, INSPECTION FOUND .3750 INCH CRACK AT STA 198 BETWEEN LONGERON 20L AND 21L IN SKIN. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-05 FIG 57A. (W) 2L72 4F A6WE 19950324003621995032400362WP 1995 3 24 USAA950197 119950113A5330 SKIN DOUG DC9 DC931 3022065WP BS 37 TORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK, INSPECTION FOUND SMALL SECTION OF SKIN TORN AT STA 37 LT RADOME HINGE CUTOUT. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 77. (W) 2L72 4F A6WE 19950324003631995032400363WP 1995 3 24 USAA950198 119950111A5220 DOOR PAN DOUG DC9 DC931 3022065WP EMERGENCY EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK, INSPECTION FOUND .25 INCH CRACK AT RT FWD EMERGENCY EXIT DOOR AT UPPER AFT CORNER STOP 14 PAN AREA. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (W) 2L72 4F A6WE 19950324003641995032400364WP 1995 3 24 USAA950199 119950116A5311 FRAME DOUG DC9 DC931 3022065WP BS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK, INSPECTION FOUND .5 INCH CRACK IN STA 980 FRAME AT LONG 17L. ACCOMPLISHED SPLICE REPAIR PER SRM 53-03 FIG 32. (W) 2L72 4F A6WE 19950324003651995032400365WP 1995 3 24 USAA950200 119950112A5330 SKIN DOUG DC9 DC931 3022065WP BS 996 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19929VJ37531 48118 PIT - DURING Q-1 CHECK, INSPECTION FOUND 3 SMALL CRACKS BETWEEN .0625 INCH AND .25 INCH LONG AT RIVET HEAD BELOW LONGERON 15L AND JUST FWD OF STA 996. INSTALLED DOUBLER REPAIR INTERNALLY PER SRM 53-04 FIG 49. (W) 2L72 4F A6WE 19950324003661995032400366NE 1995 3 24 USAA950203 219950301A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE LEFT OVERTEMP A USAAAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 EA19962VJ 47507 657295 CLT - FLT 441 - AT CRUISE, HAD LT ENGINE OVERTHRUST. CREW SHUTDOWN LT ENGINE. SINGLE ENGINE TIME APPROXIMATELY 20 MINUTES. MAINTENANCE REPLACED THE LT ENGINE DUE TO OVERTEMP CONDITION. OPERATIONS CHECKED NORMAL. (W) 2L72 4F4 F A6WE E2EA 19950324003671995032400367WP 1995 3 24 USAA950204 119950226A3350 EEL SWITCH DOUG DC9 DC931 3022065WP COCKPIT INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19963VJ 47508 BOS - THE EMERGENCY LIGHTS POP CIRCUIT BREAKER. MAINTENANCE REPLACED THE LIGHT SWITCH IN THE COCKPIT OVERHEAD PANEL. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950324003681995032400368WP 1995 3 24 USAA950205 119950304A3350 EEL ASSEMBLY DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19982VJ 48158 CLT - THE EMERGENCY LIGHT AT THE PASSENGER ENTRY DOOR IS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (W) 2L72 4F A6WE 19950324003691995032400369EU 1995 3 24 USAA950208 119950305A5230 DOOR FOKKERF28 F28MK4000 4990810EU CARGO COMPT NOT LATCHED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19475AU 11222 LIT - FLT 374 - ON ROTATION, THE 'CARGO DOORS' LIGHT ILLUMINATED. CREW RETURNED TO LIT WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL DOOR LATCHES, HOOKS AND PRESSURIZED ACFT TO 3 PSI. NO PROBLEMS FOUND. (W) 2L72 4F RTA20EU 19950324003701995032400370EU 1995 3 24 USAA950215 119950226A2910A71281429 HYD LINE FOKKERF28 F28MK4000 4990810EU LANDING GEAR CRACKED A USAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 EA19479AU 11228 CLT - FLT 1250 - THE NR 1 HYDRAULIC SYSTEM QUANITY AND PRESSURE WENT TO ZERO IMMEDIATELY AFTER FLAP RETRACTION AFTER TAKEOFF. CREW RETURNED TO CLT. MAINTENANCE REPLACED THE SUPPLY LINE ON THE LANDING GEAR SELECTOR VALVE. LEAK CHECKED GOOD. (W) 2L72 4F RTA20EU 19950324003711995032400371EU 1995 3 24 USAA950216 119950226A3231 BOLT FOKKERF28 F28MK4000 4990810EU RT MLG DR ACT MISSING A USAAO OTHER J WARNING INDICATION APAPPROACH 1 EA19486US 11237 PIT - FLT 1197 - THE RT MLG GAVE AN USAFE INDICATION UPON LOWERING. CREW RECYCLED THE GEAR AND RECEIVED THREE GREEN LIGHTS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A MISSING BOLT IN THE RT FWD MAIN GEAR DOOR ACTUATOR. OPERATIONS CHECKED GOOD. (W) 2L72 4F RTA20EU 19950324003721995032400372WP 1995 3 24 USAA950220 119950308A3222 STRUT DOUG DC9 DC931 3022065WP NLG REQ SERVICE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19989VJ 47212 BDL - FLT 972 - THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER THE GEAR HANDLE WAS SELECTED UP AN UNLATCH CHECK PERFORMED. THERE WAS CONTINUOUS NOISE WITH THE GEAR HANDLE UP AND THE UNSAFE LIGHT ON. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT. OPERATIOINS CHECKED GOOD. (W) 2L72 4F A6WE 19950324003731995032400373WP 1995 3 24 USAA950223 119950307A2120 AIR DIST DOUG DC9 DC931 3022065WP CABIN ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19987VJ 47210 CAE - FLT 849 - AFTER TAKEOFF, CREW SMELLED TOXIC FUMES THROUGHOUT THE COCKPIT AND CABIN. FLIGHT RETURNED TO CAE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE INTAKES, FLUID QUANTITIES, CARGO BINS AND E AND E COMPARTMENT. WATER SEPARATORS WERE DRAINED FOR CONTAMINATION. ALL CHECKED GOOD. (W) 2L72 4F A6WE 19950324003741995032400374NM 1995 3 24 9504406623 119950202A5314 KEEL BEAM BOEING747 747251B 1384892NM FS 1466 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623US 21705 DURING PERIODIC CHECK, THE KEEL BEAM LOWER CHORD WAS FOUND CORRODED AT FS 1466, LBL 7. CORROSION IN ON THE UPPER HORIZONTAL FLANGE AND IS 0.152 INCHES DEEP. CHORD IS MADE FROM BAC1520-1680 7075-T6511 ALUMINUM EXTRUSION. MADE REPAIR PER EA 66-96581. 2L74 4F A20WE 19950324003751995032400375NM 1995 3 24 9504416623 119950201A5320 DOUBLER BOEING747 747251B 1384892NM FWD LAVATORY CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623US 21705 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE DOUBLER FOR THE FORWARD LAV PAN. THE DOUBLER P/N 65B07388-1 IS 0.50 INCH 7075-T6. MADE REPAIR PER EA 66-93819. 2L74 4F A20WE 19950324003761995032400376NM 1995 3 24 9504426623 119950201A5414 SKIN BOEING747 747251B 1384892NM NR 4 PYLON WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623US 21705 DURING PERIODIC CHECK, THE NR 4 PYLON RIGHT SKIN PANEL AND UPPER CAP SKIN WAS FOUND WORN ADJACENT TO THE WING TO PYLON FAIRING ATTACH ANGLE. PYLON SKIN AND UPPER CAP SKIN ARE MADE FROM .063 INCHES 2024-T3 AND .025: DOUBLER PLUS .032 INCH TRIPLER. MADE REPAIR PER EA 66-96610. 2L74 4F A20WE 19950324003771995032400377NM 1995 3 24 9504432702 119950312A5330 SKIN BOEING727 727225 1384077NM FS 1124 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING THROUGH FLIGHT INSPECTION, MAINTENANCE FOUND AFT FUSELAGE BELLY SKIN CORRODED AT FS 1124, STR 27L AND 28R AND CORROSION AND CRACKS AT 29L. REPAIRED PER SRM 53-30-03, FIG.3. 2L73 4F A3WE 19950324003781995032400378NM 1995 3 24 9504442702 119950312A5330 SKIN BOEING727 727225 1384077NM FS 1010 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING THROUGH FLIGHT INSPECTION, MAINTENANCE FOUND AFT FUSELAGE BELLY SKIN CORRODED AT FS 1010 4 INCHES AFT AND 2 INCHES LEFT OF STR 30. REPAIRED PER NWA EA 27-093693. 2L73 4F A3WE 19950324003791995032400379WP 1995 3 24 9504459978 119950320A27805919526 T DUCTS DOUG DC9 DC931 3022065WP LE FLAPS LACK OF LUBE A NWAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED UKUNKNOWN 1 GL019342 47391 SLAT DISAGREEMENT LIGHT ILLUMINATED DURING SLAT EXTENSION. AIRCRAFT ROLLED SLIGHTLY TO THE LEFT. VISUAL INSPECTION INDICATED LEFT SLAT TO BE FULLY EXTENDED AND RIGHT SLAT APPROXIMATELY .75 EXTENDED. INDICATED AIRSPEED WAS 200-220 KNOTS. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. LUBED SLAT TELESCOPING DUCTS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324003801995032400380WP 1995 3 24 9504469180 119950320A301039244421 VALVE DOUG DC9 DC914 3022034WP AIRFOIL ANTI-ICEMALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL013312L3443423 45707 AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED DURING CRUISE. PERFORMED PRECAUTIONARY COCKPIT OPERATING PROCEDURES AND DIVERTED TO CLE. REPLACED AIRFOIL ANTI-ICE PRESSURE REGULATOR AND SHUTOFF VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950324003811995032400381WP 1995 3 24 9504471152 119950321A5320 ROLLER TRAY DOUG DC10 DC1040 3023508WP FS 759 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE ROLLER TRAY IN THE FORWARD CARGO COMPARTMENT AT FS 759, RBL 28. REMOVED CORROSION AND INSTALLED DOUBLER AND FILLER PER EA 11-97896. 2L73 4F A22WE 19950324003821995032400382WP 1995 3 24 9504481152 119950321A5521 RIB DOUG DC10 DC1040 3023508WP XE 67.226 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, FOUND THE RIGHT DETACHABLE ELEVATOR RIB DAMAGED AT FS XE =67.226, 49.5 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 55-20-00. 2L73 4F A22WE 19950324003831995032400383NM 1995 3 24 9504496615 119950321A5313 LONGERON BOEING747 747251B 1384892NM FS 460 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01615US 20360 DURING PERIODIC CHECK, FOUND A CRACK IN SECTION 41 LOWER LOBE. CRACK IS LOCATED AT STR 28R, FS 460. REMOVED DAMAGED FLANGE, FABRICATED REPAIR, AND INSTALLED. 2L74 4F A20WE 19950324003841995032400384WP 1995 3 24 95FDEA00316 119950313A5280ANB73872 FRAME DOUG DC10 DC1030 3023501WP CTR GEAR DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04307FE 48291 CENTER LANDING GEAR RT W/W DOOR CRACKED AT FWD I/B CORNER REF N/R 7002. REMOVED CRACKED FRAME, INSTALLED NEW DOOR FRAME AND INSPECTION PLATES PER DOUGLAS SRM 51-00-00. RE-INSTALLED DOOR PER M/M 32-14-03 REF C-CK-05 N/R 7002. 2L73 4F A22WE 19950324003851995032400385SO 1995 3 24 SWIA95519 119950204A5242 DOOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AVIONICS BAY NOT CLOSED A SWIAO OTHER J WARNING INDICATION TOTAKEOFF 1 NM07190SW 120050 SERVICE DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TO. RETURNED TO GATE. FOUND SERVICE DOOR NOT FULLY CLOSED. RESECURED AVIONICS BAY SERVICE DOOR. LIGHT EXTINGUISHED. OPS CHECKS GOOD. SEE FL 75608. 2L72 4T4 TRTA31SO E20NE 19950324003861995032400386SO 1995 3 24 SWIA95520 119950207A7712 SIG COND EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 NM07190SW 120050 ABORTED TAKEOFF. FLIGHT 242 LAX. TORQUE ON RIGHT ENGINE WENT TO 107 PERCENT AND NP DROPPED TO 17.1 PERCENT ON APPLICATION OF TAKEOFF POWER. REPLACED RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUN AND OPS CKS GOOD. SEE FL 75611 FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003881995032400388SO 1995 3 24 SWIA95522 119950208A3246 WHEEL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE MLG CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07207SW 120266 NR 1 MAIN WHEEL CRACKED. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY. SEE FL 73942 FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003891995032400389SO 1995 3 24 SWIA95525 119950214A2750 RETRACT MECH EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS LACK OF LUBE A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07212SW 120276 AFTER TAKEOFF FLAPS WOULD NOT RETRACT. THERE WAS A DISAGREEMENT BETWEEN OUTBD NACELLE AND INBOARD FLAPS. FAULT CLEARED AFTER LANDING. INSPECTED OUTBD FLAPS. CLEANED AND LUBRICATED ROLLERS. CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD. SEE FL 75711 FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003901995032400390EA 1995 3 24 SWIA95526 119950214A3260 UPLOCK CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT MLG ICED UP A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07403SW 7028 UNABLE TO GET RIGHT MAIN GEAR TO GIVE AN UP AND LOCKED INDICATION. CYCLED GEAR SEVERAL TIME THEN GOT A GEAR DISAGREE WARNING IN RETRACT POSITION. AFTER DE-ICING MAIN ENG GEAR, INSPECTED GEAR AND PERFORMED A GEAR SWING. NO PROBLEMS FOUND. SUSPECT LARGE AMOUNT OF ICE ON UPLOCK POST. OPS CHECKS GOOD AT THIS TIME. SEE FL 5054 FOR MECH SIGN OFF. 2L72 4F4 FRTA21EA E15NE 19950324003911995032400391SO 1995 3 24 SWIA95528 119950214A2752 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07195SW 120127 FLAP MAP LIGHTS ILLUMINATED AND CONTROL FAULT WOULD NOT CLEAR. CLEANED CANNON PLUGS ON FLAP ACTUATORS OF BOTH LEFT AND RIGHT INBOARD AND OUTBOARD FLAPS. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950324003921995032400392SO 1995 3 24 SWIA95529 119950215A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT TE FLAP CONTAMINATED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07186SW 120034 RECEIVED A FLAP ASYMMETRY WARNING ON TAXI OUT. RETURNED TO GATE. FOUND WATER AND ICE IN RIGHT IB FLAP ACTUATOR CANNON PLUG. CLEANED WATER OUT AND IT FIXED PROBLEM. FLAPS OPERATED NORMAL FOR 15 CYCLES. SEE FL 73291 FOR SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003931995032400393NE 1995 3 24 SWIA95530 219950217A7321 FUEL CONTROL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07193SW 120088 RIGHT EEC CAUSES POWER SURGES ON THE RIGHT ENGINE. DEFERRED PER MEL 73-21-1. RAN THE RIGHT ENGINE, CND. PERFORMED HMU SOL TEST IAW MM OK. CHECKED EEC HARNESS AND INPUTS IAW SL 120-072-0001 EMB EEC TS GUIDE. NO DISCREPANCIES NOTED. SWAPPED LEFT AND RIGHT NH SENSORS FOR TS. RAN ENGINES. OPS CHECKS GOOD AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 19950324003941995032400394SO 1995 3 24 SWIA95531 119950217A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAK NONE J WARNING INDICATION CLCLIMB 1 NM07213SW 120277 OB FLAP DISAGREED AFTER LANDING AND FLAPS WERE SELECTED UP. CLEANED CANNON PLUGS ON OB ACTUATORS. COULD NOT DUPLICATE PROBLEM. FLAPS OPERATED NORMALLY. SEE FL FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003951995032400395SO 1995 3 24 SWIA95532 119950219A2750 ROLLERS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS LACK OF LUBE A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07213SW 120277 AFTER TAKEOFF, SELECTED FLAPS UP. GOT A DISAGREEMENT INDICATION. SHOWED OB FLAPS NOT RETRACTING. CLEANED AND LUBED FLAP ROLLERS. CLEANED MOISTURE FROM CANNON PLUGS. CYCLED FLAPS MANY TIMES. CHECKS GOOD. SEE FL FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324003961995032400396SO 1995 3 24 SWIA95533 119950218A323012041124001 HARNESS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07221SW 120290 LANDING GEAR WILL NOT COME UP. REMOVED AND REPLACED NOSE GEAR A SYSTEM UP HARNESS. CYCLED GEAR. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950324003971995032400397EA 1995 3 24 SWIA95534 119950219A2750 FECU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAPS FAILED A SWIAO OTHER J WARNING INDICATION APAPPROACH 1 NM07409SW 7056 FLAPS FAILED ON APPROACH. REMOVED AND REPLACED FECU. FLAP OPS CHECK OK. SEE FL 5129 FOR MECH SIGN OFF. 2L72 4F4 FRTA21EA E15NE 19950324003981995032400398NE 1995 3 24 SWIA95535 219950226A7530 FLOW VALVE LINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE LOOSE A SWIAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 NM07212SW 120276 3 MIN AFTER TO, RIGHT DUCT LEAK WARNING CAME ON. DECREASED POWER AND LIGHT STAYED ON. SHUT DOWN THE RIGHT ENGINE AND RETURNED TO FIELD. LIGHT STAYED ON FOR FOUR MINUTES AFTER ENGINE SHUT DOWN. TIGHTENED LOOSE LINE ON FLOW VALUE. OPS CHECKS GOOD. SEE FL 75723. 2L72 4T4 TRTA31SO E20NE 19950324003991995032400399SO 1995 3 24 SWIA95536 119950228A2731 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ELEV TRIM FAILED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 NM07194SW 120120 TAKEOFF AURAL TRIM AURAL WARNING WITH TRIM IN THE GREEN ARC. FOUND LEFT ELEVATOR TRIM TAB PROX SENSOR INTERNALLY SHORTING AND CAUSING AURAL WARNING UNIT CB TO TRIP. REPLACED LEFT ELEVATOR TRIM TAB PROX SENSOR IAW MM 27-32-05. OPS CKS GOOD. SEE FL 75461. 2L72 4T4 TRTA31SO E20NE 19950324004001995032400400EA 1995 3 24 SWIA95538 119950302A5101 STRUCTURE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE AIRFRAME VIBRATION A ASWIAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM07406SW 7030 DURING CLIMB AS AIRSPEED APPROACHED 280 KTS, AIRPLANE BEGAN TO VIBRATE (LIKE OUT OF BAL NOSEWHEEL). IT ALSO YAWED LEFT (ABOUT 1/2 BALL OUT OF TRIM) AIRSPEED CHANGES OF 100 PLUS KNOTS HAD NO EFFECT ON VIBRATION OR YAW. THE SAME RUDDER TRIM KEPT EVERYTHING CENTERED FROM 310 KNOTS. PERFORMED GEAR SWING. CHECKED CONDITION AND SECURITY OF ALL ACCESS PANELS. INSPECTED ALL FLIGHT CONTROL SURFACES FOR CONDITION AND SECURITY. FOUND NO DISCREPANCIES. SEE FL 5164 FOR MECH SIGN OFF. 2L72 4F4 FRTA21EA E15NE 19950324004011995032400401 1995 3 24 SWIA95539 319950302A6140 RELAY EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTO FEATHER SYSFAILED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 NM07196SW 120151 ON TAKEOFF ROLL, PILOT REPORTED NO AUTO FEATHER ARM LIGHT. LIGHTS ALL TEST GOOD ON MAP. REPLACED AUTO FEATHER ARM LIGHT RELAY. OPS CHECKS GOOD. SEE FL FOR MECH SIGN OFF. 2L72 4T4 TRTA31SO E20NE 19950324004021995032400402EA 1995 3 24 SWIA95541 119950306A30106243843 SENSOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT WING MALFUNCTIONED A SWIAK NONE N FALSE WARNING CRCRUISE 1 NM07403SW 7028 WING ANTI-ICE SENSOR CAUTION MESSAGE COMES ON WITH WING ANTI-ICE ON IN NORMAL. IN STANDBY, CHECKS OK. REPLACED LEFT WING CONTROL SENSOR AND OVERHEAT SENSOR. OPS CHECKS GOOD. SEE FL 5073 FOR MECH SIGN OFF. 2L72 4F4 FRTA21EA E15NE 19950324004031995032400403SO 1995 3 24 SWIA95543 119950305A2750 CONNECTORS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07195SW 120127 INBD FLAP CONTROL FAULT WHEN FLAPS ARE EXTENDED BEYOND 15 DEG. CLEANED FLAP TRACKS. ALSO REMOVED, CLEANED AND REINSTALLED FLAP ACTUATOR CANNON PLUGS. OPS CHECKS GOOD AT THIS TIME. SEE FL 73078. 2L72 4T4 TRTA31SO E20NE 19950324004261995032400426CE 1995 3 24 95ZZZX1383 119950221A324306111800 CYL O-RING CESSNA208 208B 2073701CE RT BRAKE FAILED A AWHAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP17891FE2286 208B0221 PILOT REPORTED UPON TURNING OFF TAXIWAY, RT BRAKE FAILURE. TOWED AIRCRAFT INTO PARKING POSITION. INSPECTION OF RT BRAKE ASSY SHOWED SIGNS OF BRAKE FLUID LEAKING FROM LOWER PISTON ASSY. REMOVED BRAKE ASSY AND REPLACED DEFECTIVE O-RING. REINSTALLED BRAKE ASSY, BLED BRAKE SYSTEM. FUNCTIONAL CHECK NORMAL. 1H71 3T A37CE 19950324004291995032400429NM 1995 3 24 AWXA9500120 119950320A2612831557 FIRE LOOP BOEING737 73733A 1384673NM APU SHORTED A AWXAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 WP28164AW 23625 LAX-LAS - FLT NR 78 - EN ROUTE TO LAS, THE APU FIRE LIGHT AND BELL CAME ON. PULLED AND ROTATED FIRE HANDLE AND EXTINGUISHER FIRED. APU WAS INSPECTED AND NO EVIDENCE OF DAMAGE NOTED. APU PLACED ON MEL 49-01. TROUBLESHOOTING OF FIRE DETECTION SYSTEM REVEALED THE LOWER LOOP M334 TO HAVE .41 MEG RESISTANCE. REMOVED AND REPLACED FIRE LOOP PER BMM, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950324004301995032400430NM 1995 3 24 EISA95018 119950220A3610655881313 DUCT BOEING727 727221 1384071NM AFT BAGGAGE PIT RUPTURED A EISAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW07367PA 22539 DURING PREFLIGHT, FOUND SMOKE IN REAR OF CABIN (AFT GALLEY AREA). REMOVED AND REPLACED RUPTURED DUCT IN AFT BAGGAGE PIT, OPS AND LEAK CHECK GOOD. (Z) 2L73 4F A3WE 19950324004311995032400431WP 1995 3 24 EISA95019 119950223A3350 EEL CONNECTOR DOUG DC9 DC931 3022065WP CABIN CORRODED A EISAK NONE L NO TEST ININSP/MAINT 1 SW07977ML 47329 DURING PREFLIGHT AT MCO, FOUND OVERWING EMERGENCY EXIT LIGHTS TOO DIM. BATTERIES CHECKED GOOD, FOUND CORROSION ON LIGHT ASSEMBLIES CONNECTION, CLEANED CORRODED AREAS, LIGHTS CHECKED GOOD. (Z) 2L72 4F A6WE 19950324004321995032400432NM 1995 3 24 EISA95021 119950306A5311 BELTFRAME BOEING727 727221 1384071NM BS 344 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE FRAME, BS 344 AT STRINGER 23R. REPAIRED PER SRM 53-10-4, FIGURE 1. (Z) 2L73 4F A3WE 19950324004331995032400433NM 1995 3 24 EISA95022 119950306A5230 SKIN BOEING727 727221 1384071NM CARGO DOOR DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT DOOR FRAME AND SKIN DAMAGED, LOWER AFT CORNER. REPAIRED PER SRM 52-00-3 FIGURE 1. (Z) 2L73 4F A3WE 19950324004341995032400434NM 1995 3 24 EISA95023 119950306A5320 ANGLE BOEING727 727221 1384071NM BS 410 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND FLOOR SUPPORT ANGLE CRACKED, BS 410 WL 166.1, RBL 38 INCHES. REPAIRED PER SRM 51-40-4. (Z) 2L73 4F A3WE 19950324004351995032400435NM 1995 3 24 EISA95024 119950306A5320 ANGLES BOEING727 727221 1384071NM BS 560-580 DENTED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT ANGLES DENTED FROM BS 560 TO 580, STRINGER 29L TO 29R. REPAIRED PER SRM 51-40-1, FIGURE 1. (Z) 2L73 4F A3WE 19950324004361995032400436NM 1995 3 24 EISA95025 119950306A5320 ANGLE BOEING727 727221 1384071NM BS 950-970 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT RIB REINFORCEMENT SECTION CRACKED BETWEEN BS 950 F TO 970, STRINGER 30. REPAIRED PER SRM 51-10-1, PARAGRAPH AA, PAGE 4. (Z) 2L73 4F A3WE 19950324004371995032400437NM 1995 3 24 EISA95026 119950306A5313 LONGERON BOEING727 727221 1384071NM BS 950-970 BENT A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT LONGERONS BENT BETWEEN BS 950F TO BS 970, STRINGER 29L TO 30. REPAIRED PER SRM 53-10-5 FIGURE 6, PAGE 17 (Z) 2L73 4F A3WE 19950324004381995032400438NM 1995 3 24 EISA95027 119950306A5313 STRINGER BOEING727 727221 1384071NM BS 950D-950E CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AT BS 950D TO 950E. REPAIRED PER BOEING FAX, C00 SJO-95-0037RR. (Z) 2L73 4F A3WE 19950324004391995032400439NM 1995 3 24 EISA95028 119950306A5320 CHANNEL BOEING727 727221 1384071NM BS 990-1010 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION BULGE FROM BS 990 TO BS 1010, STRINGER 27R. REPAIRED PER SRM 51-10-1. (Z) 2L73 4F A3WE 19950324004401995032400440NM 1995 3 24 EISA95029 119950306A5313 LONGERON BOEING727 727221 1384071NM BS 970-990 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND A CRACK IN LONGERON, BS 970 TO BS 990, STRINGER 29R. REPAIRED PER SRM 53-10-8. (Z) 2L73 4F A3WE 19950324004411995032400441NM 1995 3 24 EISA95030 119950306A5311 FRAME BOEING727 727221 1384071NM BS 990 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND A HOLE IN THE AFT CARGO COMPARTMENT DOOR FRAME, BS 990, STRINGER 24R. REPAIRED PER SRM 51-40-7 FIGURE 3. (Z) 2L73 4F A3WE 19950324004421995032400442NM 1995 3 24 EISA95031 119950306A5320 INTERCOSTAL BOEING727 727221 1384071NM BS 1050-1090 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL BETWEEN BS 1050 AND 1090, LBL 24 INCHES, WL 20 INCHES. REPLACED PER SRM 51-10-1, PAGE 4. (Z) 2L73 4F A3WE 19950324004431995032400443NM 1995 3 24 EISA95032 119950306A5320 END FITTING BOEING727 727221 1384071NM BS 1183 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER END FITTING, STRINGER 28R, BS 1183. REPLACED PER SRM 51-10-1 PAGE 4. (Z) 2L73 4F A3WE 19950324004441995032400444NM 1995 3 24 EISA95033 119950306A5330 SKIN BOEING727 727221 1384071NM BS 484 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FUSELAGE SKIN, BS 484 BETWEEN STRINGER 28L AND 28R. REPAIRED PER DRAWING HSE 2-53-153. (Z) 2L73 4F A3WE 19950324004451995032400445NM 1995 3 24 EISA95034 119950306A5320 ANGLE BOEING727 727221 1384071NM BS 312-344 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BETWEEN BS 312 AND BS 344, WL 208.1, LBL 62 INCHES. REPAIRED PER SRM 51-40-3. (Z) 2L73 4F A3WE 19950324004461995032400446NM 1995 3 24 EISA95035 119950306A5320 CHORD BOEING727 727221 1384071NM BS 1176.9 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON CHORD AT BS 1176.9, WL 208.1 LBL 58 INCHES. REPAIRED PER BOEING SB 727-53-0184 AND DRAWING HSE2-53-149. (Z) 2L73 4F A3WE 19950324004471995032400447NM 1995 3 24 EISA95036 119950306A5320 SUPPORT BOEING727 727221 1384071NM BS 760.95 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND A CRACK IN THE FLOOR ANGLE SUPPORT, BS 760.95, WL 208.1, LBL 5. REPAIRED PER SRM 51-40-3, FIGURE 1, SHEET 4. (Z) 2L73 4F A3WE 19950324004481995032400448NM 1995 3 24 EISA95037 119950306A5315 FLOOR BEAM BOEING727 727221 1384071NM BS 1110 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1110, WL 208.1. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z) 2L73 4F A3WE 19950324004491995032400449NM 1995 3 24 EISA95038 119950306A5320 SUPPORT BOEING727 727221 1384071NM BS 1110-1130 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BS 1110 TO 1130, LBL 12, WL 208.1. REPAIRED PER SRM 51-10-1. (Z) 2L73 4F A3WE 19950324004501995032400450NM 1995 3 24 EISA95039 119950306A5320 ANGLE BOEING727 727221 1384071NM BS 1138-1158 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 1138 TO BS 1158, WL 208.1. REPAIRED PER SRM 51-10-1. (Z) 2L73 4F A3WE 19950324004511995032400451NM 1995 3 24 EISA95040 119950306A5347 TRACK BOEING727 727221 1384071NM BS 1090-1140 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BSL 1090 TO BS 1140, WL 208.1, LBL 45.5. REPLACED PER SRM 53-10-5, FIGURE 7. (Z) 2L73 4F A3WE 19950324004521995032400452NM 1995 3 24 EISA95041 119950306A5347 SEAT TRACK BOEING727 727221 1384071NM BS 1090-1140 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1090 TO BS 1140, WL 208.1, LBL 24.75. REPLACED PER SRM 51-10-1. (Z) 2L73 4F A3WE 19950324004531995032400453NM 1995 3 24 EISA95042 119950306A5347 SEAT TRACK BOEING727 727221 1384071NM BS 1070 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON SEAT TRACK, BS 1070 TO BS 1140, WL 208.1, LBL 55 INCHES. REPAIRED PER SRM 51-10-1 PAGE 4. (Z) 2L73 4F A3WE 19950324004541995032400454NM 1995 3 24 EISA95043 119950306A5320 SUPPORT BOEING727 727221 1384071NM BS 1050 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT BS 1050 TO 1070, LBL 22. REPLACED PER SRM 51-30-2. (Z) 2L73 4F A3WE 19950324004551995032400455NM 1995 3 24 EISA95044 119950306A5320 SUPPORT BOEING727 727221 1384071NM BS 1030 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT, BSL 1110 TO BS 1030, LBL 12 INCH. REPLACED PER SRM 51-10-1 PARAGRAPH 4A, FIGURE 4. (Z) 2L73 4F A3WE 19950324004561995032400456NM 1995 3 24 EISA95045 119950306A5320 INTERCOSTAL BOEING727 727221 1384071NM BS 1110 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON INTERCOSTAL, BS 1110 TO BS 1130, BL '0'. REPAIRED PER SRM 51-10-1. (Z) 2L73 4F A3WE 19950324004571995032400457NM 1995 3 24 EISA95046 119950306A5315 FLOOR BEAM BOEING727 727221 1384071NM BS 1030 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1030, WL 208.1, LBL 1 INCH. REPAIRED PER SRM 53-10-8, FIGURE 3. (Z) 2L73 4F A3WE 19950324004581995032400458NM 1995 3 24 EISA95047 119950306A5320 ANGLE BOEING727 727221 1384071NM BS 970-990 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, BS 970 TO BS 990, BL '0'. REPLACED PER SRM 51-10-1, PARA 4A, PAGE 4. (Z) 2L73 4F A3WE 19950324004591995032400459NM 1995 3 24 EISA95048 119950306A5511 SPAR BOEING727 727221 1384071NM HORIZ STAB CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, STATION 223.05. REPAIRED PER DRAWING HSE2-55-146. (Z) 2L73 4F A3WE 19950324004601995032400460NM 1995 3 24 EISA95049 119950306A5330 SKIN BOEING727 727221 1384071NM AFT LAV CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION BULGES AT AFT LAVATORY SERVICE PANEL. REPAIRED PER SRM 51-10-1 PAGE 4. (Z) 2L73 4F A3WE 19950324004611995032400461NM 1995 3 24 EISA95050 119950306A5313 STRINGER BOEING727 727221 1384071NM BS 990-1010 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON STRINGER 29R AND 30, BETWEEN BS 990 AND 1010. REPAIRED PER DRAWING HSE2-53-147 AND BOEING FAX C00-SJ0-95-0037RR. (Z) 2L73 4F A3WE 19950324004621995032400462NM 1995 3 24 EISA95051 119950306A5320 BEAM BOEING727 727221 1384071NM BS 1183 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON BS 1183 VERTICAL BEAM AT BL '0', WL 148. REPAIRED PER DRAWING HSE2-53-154 AND HSE2-53-150. (Z) 2L73 4F A3WE 19950324004631995032400463NM 1995 3 24 EISA95052 119950306A5315 FLOOR BEAM BOEING727 727221 1384071NM BS 1130 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07367PA 22539 DURING A SCHEDULED C-CHECK, FOUND CORROSION ON FLOOR BEAM, BS 1130, LBL 10 INCHES, WL 208.1. REPAIRED PER DRAWING HSE-53-151. (Z) 2L73 4F A3WE 19950324004641995032400464WP 1995 3 24 EISA95053 119950313A3610598765503 DUCT DOUG DC9 DC932 3022066WP NR 1 ENGINE RUPTURED A EISAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07945ML 47168 DURING CLIMB-OUT FROM HSA GOT FIRE INDICATION ON LEFT ENGINE, DIVERTED TO GPT. FOUND 13TH STAGE BLEED AIR DUCT RUPTURED, REPLACED DUCT. (Z) 2L72 4F A6WE 19950324004651995032400465WP 1995 3 24 EISA95054 119950315A335060030431 EEL POWRE SUPPLY DOUG DC9 DC931 3022065WP CABIN INOP A EISAK NONE L NO TEST UKUNKNOWN 1 SW07928ML 47326 FORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT POWER SUPPLY. (Z) 2L72 4F A6WE 19950324004661995032400466 1995 3 24 RAIA950233 419950221A3444959960712326 ANTENNA AEROSPATR72 ATR72202 8680940EU FWD FUSELAGE FAULTY A RAIAO OTHER O OTHER CRCRUISE 1 CE03721TE8064 217 STL - FLT 7144 - STICK SHAKER, STICK PUSHER FAULT. MAINTENANCE REPLACED RADIO ALTIMETER ANTENNAS. GROUND TEST REVEALED NORMAL OPERATION. (Z) 2H72 4T RTA53EU 19950324004671995032400467SW 1995 3 24 RAIA950234 119950220A29327G284 SWITCH SWRNGNSA226 SA226TC 8780404SW RT MLG WW FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03603AS23937 TC239 STL - FLT 7543 - THE RT HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. MAINTENANCE REPLACED RT HYDRAULIC LOW PRESSURE SWITCH. SYSTEM AND LEAK CHECK GOOD. (W) 1L72 4T A8SW 19950324004681995032400468EU 1995 3 24 UF6A950214 119950221A212175MA1571 COOLING FAN BAG ATP ATP EU AVIONICS COMPT FAILED A UF6AA UNSCHED LANDING O OTHER CRCRUISE 1 CE03854AW4714 4413945 2028 ORD - FLT 5015 - FORWARD AVIONICS COOLING FAN FAILED IN FLIGHT. MAINTENANCE REPLACED AVIONICS COOLING FAN. OPS CHECK GOOD. (Z) 2L72 4T RTA27NM 19950324004691995032400469WP 1995 3 24 95ZZZW258 119950301A2530WK6236318 HARNESS DOUG DC9 DC932 3022066WP COFFEE MAKER SHORTED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05929L 47174 STL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT. SHUT-OFF ELECTRICAL POWER TO GALLEY. FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED. REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS (P/N WK6-236318). OPERATION OF NR 2 COFFEMAKER CHECKED NORMAL. CHECK OP-16 1-12-94 - STL. 2L72 4F A6WE 19950324004701995032400470WP 1995 3 24 95ZZZW259 119950302A5330 SKIN LKHEED1011 10113851 5265010WP FS 668 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE051100661753 193B1018 JFK - DURING C-CHECK, FOUND A FUSELAGE SKIN CRACK AT STA 668, STRINGER 36L. REPAIRED PER SRM 53-31-00 PG 828 FIG 815. TOTAL CYCLES 22734. 2L73 4F A23WE 19950324004711995032400471WP 1995 3 24 95ZZZW260 119950228A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE053101336843 193B1035 MCI - DURING OP-17, FOUND STA 555 UPPER RIB CRACKED O/B SIDE OF STRINGER 18 AND FOUND A .5 INCH CRACK AT STRINGER 19. INSTALLED NEW SECTION OF UPPER CAP FROM STRING 19 FWD PER DWG NR 1647070. TOTAL CYCLES 22210. 2L73 4F A23WE 19950324004721995032400472WP 1995 3 24 95ZZZW261 119950228A5712 RIB LKHEED1011 10113851 5265010WP WS 503.76 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE053101336843 193B1035 MCI - DURING OP-17, FOUND A ONE INCH CRACK IN UPPER RIB CAP I/B SIDE AT STRINGERS 21 AND 24, STA 503.76. REPAIRED UPPER RIB CAP PER DWG. NR 1647070 AND INSTALLED NEW SPLICE PER VIEW K. TOTAL CYCLES 22210. 2L73 4F A23WE 19950324004731995032400473WP 1995 3 24 95ZZZW262 119950228A5713 STRINGER LKHEED1011 10113851 5265010WP WS 529.4 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE053101336843 193B1035 MCI - DURING OP-17, FOUND .75 INCH CRACK AT STRINGER 19, RT WING STA 529.40 UPPER RIB CAP O/B SIDE. CUTOUT DAMAGED RIB CAP AND SPLICED PER DWG NR 1647070, VIEW V. TOTAL CYCLES 22210. 2L73 4F A23WE 19950324004741995032400474NM 1995 3 24 95ZZZW263 119950305A3610652244143 DUCT BOEING727 727231 1384079NM NR 3 ENGINE RUPTURED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0554341 21628 STL - DURING CLIMB, NR 3 ENGINE FIREWARNING SOUNDED. REDUCED POWER ON THE NR 3 ENGINE AND FIREWARNING CEASED. FOUND 13TH STAGE DUCT AND PERFORMED A HIGH POWER LEAK CHECK. CHECKED NORMAL. CHECK C-1 11-21-94 - MCI. 2L73 4F A3WE 19950324004751995032400475WP 1995 3 24 95ZZZW264 119950301A53201506362101 SUPPORT LKHEED1011 10113851 5265010WP NLG UPLOCK BROKEN A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0531014 193B1036 JFK - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE INTRANSIT LIGHT REMAINED ON AND NOSE GEAR DOOR LIGHT WOULD ILLUMINATE WHEN LANDING GEAR SELECTOR PLACED IN NEUTRAL. FOUND NOSE LANDING GEAR UPLOCK SUPPORT BROKEN, (P/N 1506362-101). REPLACED NOSE LANDING GEAR UPLOCK ASSEMBLY, (P/N1606361-105). NOSE LANDING GEAR OPERATION AND INDICATION CHECKED NORMAL. CHECK C-7C - 11-21-94 - JFK. 2L73 4F A23WE 19950324004761995032400476NM 1995 3 24 95ZZZW265 119950309A21331032801 OUTFLOW VALVE BOEING727 727231 1384079NM CABIN MALFUNCTIONED A TWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 CE0554336 20490 STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1). OPS CHECKS NORMAL. CHECK C-1 - 10-18-94 - MCI. REF 95ZZZW266, 95ZZZW267, 95ZZZW268. 2L73 4F A3WE 19950324004771995032400477NM 1995 3 24 95ZZZW266 119950309A21331032805 OUTFLOW VALVE BOEING727 727231 1384079NM CABIN MALFUNCTIONED A TWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 CE0554336 20490 STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1). OPS CHECKS NORMAL. CHECK C-1 - 10-18-94 - MCI. REF 95ZZZW265, 95ZZZW267, 95ZZZW268. 2L73 4F A3WE 19950324004781995032400478NM 1995 3 24 95ZZZW267 119950309A21317638101 CONTROLLER BOEING727 727231 1384079NM CABIN MALFUNCTIONED A TWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 CE0554336 20490 STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1). OPS CHECKS NORMAL. CHECK C-1 - 10-18-94 - MCI. REF 95ZZZW265, 95ZZZW266, 95ZZZW268. 2L73 4F A3WE 19950324004791995032400479NM 1995 3 24 95ZZZW268 119950309A21311310461 CONTROLLER BOEING727 727231 1384079NM CABIN MALFUNCTIONED A TWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 CE0554336 20490 STL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PRESSURE CONTROLLER, (P/N 131046-1). OPS CHECKS NORMAL. CHECK C-1 - 10-18-94 - MCI. REF 95ZZZW265, 95ZZZW266, 95ZZZW267. 2L73 4F A3WE 19950324004801995032400480WP 1995 3 24 95ZZZW269 119950307A30207958591501 DUCT DOUG DC9 DC932 3022066WP NR 1 ENGINE FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05998R 47030 STL - FLT 658 - DURING CLIMB, THE NR 1 ENGINE (S/N 2107) WAS SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION AND A DECREASE IN OIL QUANTITY. FOUND NOSE COWL ANTI-ICE DUCT, (P/N 7958591-501), RUPTURED, BLOWING HOT AIR ON BYPASS LIGHT SWITCH, MELTING SOLDER JOINTS OF SWITCH BODY. REPLACED ANTI-ICE DUCT, REPLACED BYPASS SWITCH, (P/N 42D109-1A) AND REPLENISHED OIL QUANTITY. ENGINE OPERATION AND LEAK CHECKS NORMAL. CHECK C-1 - 1-12-94 - STL. 2L72 4F A6WE 19950324004811995032400481WP 1995 3 24 95ZZZW270 119950302A32105937042501 DEFLECTOR DOUG DC9 DC982 3022082WP LT MLG DAMAGED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05957U 49702 LAX - FLT - 210 - ON TAKEOFF, WHEN LANDING GEAR WAS RETRACTED, LT MLG RED LIGHT AND DOOR LIGHT REMAINED ILLUMINATED. FOLLOWED FLIGHT HANDBOOK PROCEDURES AND LIGHTS REMAINED ILLUMINATED. FOUND DEFLECTOR ASSEMBLY (P/N 5937042-501) BENT AND CONTACTING HYDRAULIC RESERVOIR. REPLACED DEFLECTOR ASSEMBLY AND LANDING GEAR OPERATION CHECKED NORMAL. CHECK C-1D - 1-13-94 - MCI. 2L72 4F A6WE 19950324004821995032400482EU 1995 3 24 95ZZZW271 119950226A3350A3030398101 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770054 461 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FRONT OF RT AISLE IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950324004831995032400483SO 1995 3 24 95ZZZW272 119950222A32331959500007 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03131AM10793 120158 STL - FLT 7061 - THE RT MAIN GEAR DOORS WOULD NOT CLOSE AFTER TAKEOFF. MAINTENANCE ADJUSTED RT MAIN GEAR ACTUATOR. GEAR SWINGS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA31SO 19950324004841995032400484NM 1995 3 24 AALA950335 119950224A3350 CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07339AA 22336 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT 17AB INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 17AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950324004851995032400485NM 1995 3 24 AALA950353 119950227A3260 SPLICE BOEING727 727223 1384074NM NLG BROKEN A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW07701AA 22459 MIA - FLT 651 - DURING APPROACH WITH LANDING GEAR EXTENDED, NLG UNSAFE LIGHT ILLUMINATED AND AURAL WARNING HORN SOUNDED. ACCOMPLISHED GO-AROUND AND RECYCLED LANDING GEAR WITH ALL INDICATIONS RETURNING TO NORMAL. ACFT LANDED MIA WITHOUT INCIDENT. REPAIRED BROKEN WIRE SPLICE TO NOSE LANDING GEAR DOWNLOCK SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950324004861995032400486NM 1995 3 24 AALA950375 119950302A361069316941 DUCT BOEING727 727223 1384074NM NR 2 ENGINE BLOWN A AALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07870AA 21382 JFK-MIA - FLT 743 - AFTER TAKEOFF, THE LOWER BODY OVERHEAT LIGHT ILLUMINATED AND A LOUD THUD HEARD BY FLIGHT ATTENDANTS. PULLED NR 2 ENGINE TO IDLE TO EXTINGUISH LIGHT. LIGHT CAME BACK ON WHEN THROTTLE ADVANCED. THE LT NR 2 ENGINE AT IDLE, DIVERTED AND LANDED JFK WITHOUT INCIDENT. REPLACED BLOWN SECTION OF THERMAL ANTI-ICE DUCTING, SHUT-OFF VALVE, ANTI-ICE VALVE AND THERMO SENSOR. ACCOMPLISHED ENGINE RUNUP, SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950324004871995032400487NE 1995 3 24 PAYA95A4006 219950216A7260 GEAR BOX AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 1 ENGINE FAILED A PAYAO OTHER J WARNING INDICATION CLCLIMB 1 EA174202G 050 FLT 7707 - THE NR 1 ENGINE SHUTDOWN IN FLIGHT WITH AN ACCOMPANIED LOSS OF OIL AND FUEL PRESSURE. ACCESSORY GEAR BOX FUEL PUMP DRIVE GEAR FAILED RESULTING IN TOTAL LOSS OF FUEL AND OIL PRESSURE. THE NR 1 FIRE HANDLE PULLED TO SECURE ENGINE AND FEATHER PROP. ATB ACCOMPLISHED AND LANDING WAS UNEVENTFUL. REMOVED AND REPLACED NR 1 ENGINE. (W) 2H72 4T4 TRTA53EU E20NE 19950324004881995032400488NE 1995 3 24 PAYA95A4007 219950222A7321 ECU AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 2 FAILED A PAYAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA174211G 178 FLT 7658 - THE NR 2 ECU FAULTED AND WHEN NR 2 PROP WAS FEATHERED CREW REPORTED SMOKE CAUTION ILLUMINATED ON CAP. CREW FURTHER REPORTED VISUAL INDICATION OF SMOKE IN CABIN AND COCKPIT. MAINTENANCE RAN ACFT FOR 30 MINUTES AND NOTED NO INDICATION OR VISUAL CONFIRMATION OF SMOKE ANYWHERE THROUGHOUT ACFT CABIN OR COCKPIT. (W) 2H72 4T4 TRTA53EU E20NE 19950324004891995032400489EU 1995 3 24 PAYA95A4008 119950301A5313 STRINGER AEROSPATR42 ATR42300 8680920EU FS 173 CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174207G 083 THE CORROSION ON STRINGER NR 11 AT STA 173. REPLACED DAMAGED SECTION OF STRINGER. (W) 2H72 4T RTA53EU 19950324004901995032400490EU 1995 3 24 PAYA95A4009 119950301A5347 SEAT TRACK AEROSPATR42 ATR42300 8680920EU CABIN CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174207G 083 CORROSION ON FLIGHT ATTENDANTS RT SEAT TRACK. REPLACED SEAT TRACK SECTION. (W) 2H72 4T RTA53EU 19950324004911995032400491EU 1995 3 24 PAYA95A4010 119950301A3340 BRACKET AEROSPATR42 ATR42300 8680920EU LT STROBE LIGHT CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174207G 083 CRACK IN LT WING TIP STROBE LENSE ATTACH BRACKET. REPLACED BRACKET. (W) 2H72 4T RTA53EU 19950324004921995032400492EU 1995 3 24 PAYA95A4011 119950301A5260 FRAME AEROSPATR42 ATR42300 8680920EU BOTTOM STEP CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174207G 083 CRACK IN BOTH SIDES OF BOTTOM STEP FRAME. REPAIRED CRACK. (W) 2H72 4T RTA53EU 19950324004931995032400493EU 1995 3 24 PAYA95A4012 119950301A5210 FRAME AEROSPATR42 ATR42300 8680920EU PAX DOOR CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174207G 083 PASSENGER DOOR BOTTOM AFT 'L' FRAME CORRODED. REPLACED FRAME. (W) 2H72 4T RTA53EU 19950324004941995032400494EU 1995 3 24 PAYA95A4013 119950301A3234F96GA0102 GEAR SELECTOR AEROSPATR42 ATR42300 8680920EU LANDING GEAR MALFUNCTIONED A PAYAO OTHER J WARNING INDICATION CLCLIMB 1 EA174209G 129 BDL-JFK - FLT 7651 - CREW REPORTED LANDING GEAR SELECTOR HANDLE STICKING DURING UP SELECTION. REPLACED GEAR SELECTOR. (W) 2H72 4T RTA53EU 19950324004951995032400495SO 1995 3 24 RAIA950235 119950222A324114004114 TRANSDUCER EMB 120 EMB120RT SO MLG MOISTURE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03128AM14537 120109 STL - FLT 7458 - BRAKES ARE EXTREMELY WEAK EXCEPT AT VERY LOW SPEEDS, OK WITH ANTI-SKID OFF. MAINTENANCE CLEANED ALL FOUR ANTI-SKID TRANSDUCERS. TAXI CHECK REVEALED NORMAL OPERATION. (W) 2L72 4T RTA31SO 19950324004961995032400496 1995 3 24 UF6A950215 419950221A3417 FITTING BAG ATP ATP EU NR 2 ADC LOOSE A UF6AA UNSCHED LANDING O OTHER CRCRUISE 1 CE03860AW5368 2037 ORD - FLT 5033 - THE NR 2 EFIS AIRSPEED INCORRECT. MECHANIC TIGHTENED LOOSE FITTING ON NR 2 ADC. OPS CHECK GOOD. LEAK CHECK GOOD. (W) 2L72 4T RTA27NM 19950324004971995032400497WP 1995 3 24 9504509996 119950310A5320 DOUBLER DOUG DC9 DC931 3022065WP FS 1084 BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK, FOUND BROKEN DOUBLER AT FS 1084, LONGERON 18L. REPAIRED PER EA 99-097155. 2L72 4F A6WE 19950324004981995032400498WP 1995 3 24 9504519996 119950316A5342 ANGLE DOUG DC9 DC931 3022065WP FS 1096 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1096 RIGHT SIDE. REPAIRED PER EA 99-097062, FIG.1. 2L72 4F A6WE 19950324004991995032400499WP 1995 3 24 9504529960 119950316A57445919217502 HINGE DOUG DC9 DC931 3022065WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01920RW 28668 47163 DURING PERIODIC CHECK, FOUND CORROSION IN RIGHT NR 3 FLAP HINGE FORWARD SIDE FASTENER HOLES. REPLACED HINGE PER CITEXT 09-5740-9-9800. 2L72 4F A6WE 19950324005001995032400500WP 1995 3 24 9504539854 119950317A5320 FITTING DOUG DC9 DC951 3022051WP FS 775 BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01763NC 47716 DURING PERIODIC CHECK, FOUND BROKEN FLANGE ON THE CENTER TANG TO RIGHT OUTBOARD SEAT TRACK SUPPORT FITTING FS 775. REPLACED FITTING. 2L72 4F A6WE 19950324005011995032400501WP 1995 3 24 9504549960 119950317A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP FS 980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01920RW 47163 DURING PERIODIC CHECK, FOUND CORROSION ON AFT CARGO FLOOR BEAM FS 980 INBOARD OF VERTICAL SIDE PANELS. REPAIRED PER EA 99-097152. 2L72 4F A6WE 19950324005021995032400502WP 1995 3 24 9504559908 119950318A5330 SKIN DOUG DC9 DC931 3022065WP FS 451 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01958N 47254 DURING LINE CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 451 BETWEEN LONGERONS 29R - 30. REPAIRED PER EA 99-097065. 2L72 4F A6WE 19950324005031995032400503WP 1995 3 24 9504569759 119950318A5330 SKIN DOUG DC9 DC941 302207NWP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING LINE CHECK, FOUND TWO 1.50 INCH CRACKS IN THE RIGHT FUSELAGE SKIN AFT OF ELEVATOR ACCUMULATOR SERVICE DOOR. REPAIRED PER EA 97-096492. 2L72 4F A6WE 19950324005041995032400504WP 1995 3 24 9504579854 119950320A5330 SKIN DOUG DC9 DC951 3022051WP FS 880 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01763NC 47716 DURING PERIODIC CHECK, FOUND CORROSION ON FUSEALGE SKIN STRAP FS 880 JUST BELOW LONGERON 26L. REPAIRED PER EA 98-097063. 2L72 4F A6WE 19950324005051995032400505WP 1995 3 24 9504589960 119950320A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01920RW 47163 DURING PERIODIC CHECK, FOUND CORROSION ON AFT CARGO FS 996 FLOOR BEAM RIGHT SIDE INBOARD OF VERTICAL SIDE PANELS. REPAIRED PER EA 99-097166. 2L72 4F A6WE 19950324005061995032400506WP 1995 3 24 9504599960 119950320A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01920RW 47163 DURING PERIODIC CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN BELOW THE ELEVATOR HYDRAULIC ACCUMULATOR ACCESS DOOR. REPAIRED PER EA 99-097154. 2L72 4F A6WE 19950324005071995032400507NM 1995 3 24 9504606305 119950218A5414322U411020 SKIN BOEING747 747451 1384940NM NR 1 ENG PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING OVERNIGHT LINE CHECK, A CRACK WAS FOUND ON THE NR 1 ENGINE PYLON INBOARD SKIN AT THE FORWARD UPPER CORNER OF THE NR 452 PANEL CUTOUT. STOP DRILLED CRACK AND REPAIRED PER EA 63-96730. 2L74 4F RTA20WE 19950324005081995032400508WP 1995 3 24 9504619956 119950316A57445919218506 HINGE DOUG DC9 DC931 3022065WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01923RW 26597 47183 DURING PERIODIC CHECK, FOUND CORROSION IN RIGHT WING NR 2 FLAP HINGE FORWARD UPPER BORES. REPLACED FITTING PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950324005091995032400509WP 1995 3 24 9504629156 119950321A5542 SKIN DOUG DC9 DC914 3022034WP RUDDER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018915E 45832 DURING LINE CHECK, FOUND .50 INCH CRACK IN THE RUDDER SKIN RIGHT SIDE STA 154. CRACK IS LOCATED APPROXIMATELY 3 INCHES AFT OF REPAIR WITH SEVERAL LOOSE RIVETS. REPLACED RUDDER. 2L72 4F A6WE 19950324005101995032400510NM 1995 3 24 9504636305 119950323A5720 SUPPORT BOEING747 747451 1384940NM LEFT WING LE DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING LINE CHECK (KIX), DAMAGE WAS FOUND ON THE LEFT WING LEADING EDGE LOWER PANEL SUPPORT AT WS 838 AND THE OUTBOARD FUELING DOOR. REPLACED DOOR AND SUPPORT. 2L74 4F RTA20WE 19950324005111995032400511WP 1995 3 24 9504641144 119950302A5313ARC3017541 LONGERON DOUG DC10 DC1040 3023508WP FS 514 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01144JC 46753 DURING PERIODIC INSPECTION, CRACKS WERE FOUND ON LONGERON 28L AT FS 514. LONGERON IS MADE FROM .050 INCH THICK 7075-T6 ALUMINUM. TRIMMED LONGERON AND INSTALLED DOUBLER PER EA11-96648. 2L73 4F A22WE 19950324005121995032400512WP 1995 3 24 9504651226 119950302A5753NRC6062501 VANE DOUG DC10 DC1030 3023501WP LT TE FLAP WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 DURING PERIODIC CHECK, WEAR WAS FOUND ON THE LEFT INBOARD FLAP VANE. SMOOTHED AREA AND INSTALLED DOUBLER PER EA 12-93867. 2L73 4F A22WE 19950324005131995032400513WP 1995 3 24 9504661226 119950227A5751NRC6043501 SKIN DOUG DC10 DC1030 3023501WP LT AILERON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01226NW 46583 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT INBOARD AILERON LOWER SKIN 8 INCHES FROM INBOARD END AND 20 INCHES FROM FORWARD EDGE. REPAIRED PER EA 12-93869. 2L73 4F A22WE 19950324005141995032400514WP 1995 3 24 95FDEA00317 119950314A5280NNB60869 CORNER DOUG DC10 DC1030 3023501WP LT MLG DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04307FE 48291 LEFT MAIN LANDING GEAR DOOR - CRACKED AT FWD I/B CORNER. REMOVED AND REPLACED CORNER. REF: SRM 53-00-01. 2L73 4F A22WE 19950324005151995032400515WP 1995 3 24 95FDEA00318 119950314A5280ANB73871 DOOR FRAME DOUG DC10 DC1030 3023501WP LT CTR GEAR DOORCRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO04307FE 48291 CENTER LANDING GEAR LT W/W DOOR CRACKED AT FWD I/B CORNER. REF N/R 7003. REMOVED CRACKED FRAME, INSTALLED NEW DOOR FRAME AND INSPECTION PLATES PER DOUGLAS SRM 51-00-00. REINSTALLED DOOR PER MM 32-14-03. 2L73 4F A22WE 19950324005161995032400516NM 1995 3 24 95FDEA00319 119950322A3610 DUCT BOEING727 727233 138408ANM AFT FUS LEAKING A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO04281FE 22348 LOWER AFT BODY O/H LIGHT CAME ON DURING FLIGHT AT FL310. COMPLETED 'LWR AFT BODY O/H LIGHT ON' ABNORMAL/EMERG CKLIST. LIGHT REMAINED ON. DIVERTED TO FLL. ON LONG FINAL APPROACH W/ALL ENG AT IDLE FOR DESCENT, LIGHT WENT OUT. CKD KEEL BEAM LOOP M-367, AFT CARGO COMP LOOPS M-366, M-767 AND M323. NO LEAKS FOUND OR DISCREP IN LOOP/WIRING, CKD AFT AIRSTAIRS LOOP M-365 RT CKS GOOD. FOUND AIR LEAK NEAR LOOP M-322 LT AIRSTAIRS. TIGHTENED CLAMP ON AIR CLEANER OVERBOARD LINE. RAN ALL 3 ENG AT T/O PWR AND PART PWR FOR A FEW MINUTES. NO WARNING LIGHT CAME ON. OK FOR SVC. 2L73 4F RTA3WE 19950324005171995032400517NM 1995 3 24 95FDEA00320 119950321A7312 HEAT VALVE BOEING727 7272S2F 1384O81NM NR 2 ENGINE FAILED A FDEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO04206FE 22928 GDL - NR 2 FUEL HEAT VALVE STUCK OPEN. FOLLOWED PROCEDURE, SHUT NR 2 ENG DOWN. REMOVED AND REPLACED FUEL HEAT ANTI-ICE VALVE, PER MM 73-14-11 PG 401, OPS CHECKED GOOD, OK FOR SERVICE. A/C DIVERTED TO GDL DUE PRECAUTIONARY NR 2 ENG SHUTDOWN. 2L73 4F A3WE 19950324005181995032400518WP 1995 3 24 ABXA9500219 119950202A55235910414504 TAB DOUG DC9 DC932 3022066WP RT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT ELEVATOR GEAR TAB. REPLACED TAB IAW DC-9 M.M. 27-30-4. 2L72 4F A6WE 19950324005191995032400519WP 1995 3 24 ABXA9500220 119950209A5320992368734 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 560-579 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE INTERCOSTALS BETWEEN STA 560 AND STA 579, BETWEEN LONGERONS 27 AND 28. REPAIRED INTERCOSTALS IAW ABX REA D953-10925-MR. 2L72 4F A6WE 19950324005201995032400520WP 1995 3 24 ABXA9500221 119950209A532099234883 DOUBLER DOUG DC9 DC932 3022066WP BS 585 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON AN INTERNAL DOUBLER UNDER LONGERON 26L AT STA 585. REPAIRED DOUBLER IAW ABX REA D953-10868-MR. 2L72 4F A6WE 19950324005211995032400521WP 1995 3 24 ABXA9500222 119950215A531599581861 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 935 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE L0WER FLANGE OF THE FLOOR BEAM AT STA 935, RBL 15. REPAIRED FLOOR BEAM IAW ABX REA D953-10973-MR. 2L72 4F A6WE 19950324005221995032400522WP 1995 3 24 ABXA9500223 119950126A5320SR0953013711 SPLICE DOUG DC9 DC932 3022066WP FWD LWR CARGO CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON LONGERON 30 SPLICE, FORWARD OF STA 560. REPLACED LONGERON 30 SPLICE IAW DC-9 SRM 53-02, FIGURE 14. 2L72 4F A6WE 19950324005231995032400523WP 1995 3 24 ABXA9500224 119950203A5330591970731 SKIN DOUG DC9 DC932 3022066WP FS 917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE SKIN IN THE AREA OF THE NR 1 DOOR STOP OF THE AFT LOWER CARGO DOOR. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10873-MR. 2L72 4F A6WE 19950324005241995032400524WP 1995 3 24 ABXA9500225 119950127A531599581841 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 897.0 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FLOOR BEAM AT STA 897.0 AND RBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10844-MR. 2L72 4F A6WE 19950324005251995032400525WP 1995 3 24 ABXA9500226 119950127A5315995821421 FITTING DOUG DC9 DC932 3022066WP FS 897.0 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND A DOUBLE DRILLED HOLE IN THE FITTING AT STA 897.0 AND RBL 54.5. REPAIRED FITTING IAW ABX REA D953-10844-MR. 2L72 4F A6WE 19950324005261995032400526WP 1995 3 24 ABXA9500227 119950201A5330591140659 SKIN DOUG DC9 DC932 3022066WP FS 218.0 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND A DENT ON THE FUSELAGE SKIN AT STA 218, LONGERON 17L. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10854-MR. 2L72 4F A6WE 19950324005271995032400527WP 1995 3 24 ABXA9500228 119950124A53159915527508 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 680 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND A FLOOR BEAM CRACKED WITH DOUBLE DRILLED HOLES AT STA 680, LBL 54.5. REPAIRED FLOOR BEAM IAW ABX REA D953-10828-MR. 2L72 4F A6WE 19950324005281995032400528WP 1995 3 24 ABXA9500229 119950124A531199196182N FRAME DOUG DC9 DC932 3022066WP FS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, THE RIGHT FUSELAGE MAIN FRAME AT STA 718 WAS FOUND CRACKED IN THE RIGHT WHEELWELL. REPLACED RIGHT MAIN FRAME IAW SERVICE BULLETIN 53-131. 2L72 4F A6WE 19950324005291995032400529WP 1995 3 24 ABXA9500230 119950120A575399576007 BRACKET DOUG DC9 DC932 3022066WP LT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, THE LEFT FLAP OUTBOARD HINGE ATTACH BRACKETS WERE FOUND CRACKED. REPLACED BRACKETS IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950324005301995032400530WP 1995 3 24 ABXA9500231 119950130A53209919402506 TRAP PANEL DOUG DC9 DC932 3022066WP CENTER FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, THE RIGHT TRAPEZOIDAL PANEL WAS FOUND CRACKED BETWEEN THREE EACH BOLTS ON THE HORIZONTAL FLANGE JUST FORWARD OF THE FIXED SIDE BRACE ATTACH POINT. REPLACED PANEL IAW DC-9 SERVICE BULLETIN 53-182. 2L72 4F A6WE 19950324005311995032400531WP 1995 3 24 ABXA9500232 119950202A533059114004 SKIN DOUG DC9 DC932 3022066WP FS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 FUSELAGE SKIN. REPAIRED FUSELAGE SKIN IAW ABX REA D953-10867-MR. 2L72 4F A6WE 19950324005321995032400532WP 1995 3 24 ABXA9500233 119950202A5312991150985 BLKHD TEE DOUG DC9 DC932 3022066WP FS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE STA 110 BULKHEAD LOWER TEE CAP. TEE CAP WAS REPAIRED IAW ABX REA D953-10867-MR. 2L72 4F A6WE 19950324005331995032400533WP 1995 3 24 ABXA9500234 119950309A57535912168503 VANE DOUG DC9 DC932 3022066WP LT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING UPPER MOVEABLE VANE. REPLACED VANE IAW DC-9 M.M. 27-51-2. 2L72 4F A6WE 19950324005341995032400534WP 1995 3 24 ABXA9500235 119950306A57535910042503 VANE DOUG DC9 DC932 3022066WP LT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND THE LEFT WING CENTER FIXED VANE CRACKED AT THE CENTER SUPPORT. REPLACED VANE IAW DC-9 M.M. 27-51-3. 2L72 4F A6WE 19950324005351995032400535WP 1995 3 24 ABXA9500236 119950306A57535910043509 VANE DOUG DC9 DC932 3022066WP LT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING OUTBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3. 2L72 4F A6WE 19950324005361995032400536WP 1995 3 24 ABXA9500237 119950306A57535910041509 VANE DOUG DC9 DC932 3022066WP LT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING INBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3. 2L72 4F A6WE 19950324005371995032400537WP 1995 3 24 ABXA9500238 119950202A57209919369502 TEE CAP DOUG DC9 DC932 3022066WP XCW 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER TEE CAP AT STA XCW 58.5. RIGHT WING TEE CAP WAS ALSO REPLACED DUE TO DISCREPANCIES NOTED ON THE LEFT TEE CAP IAW EA AD-57-03766-MR. 2L72 4F A6WE 19950324005381995032400538WP 1995 3 24 ABXA9500239 119950202A57209919369501 TEE CAP DOUG DC9 DC932 3022066WP XCW 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 57-98, FOUND A CRACK AND CORROSION ON THE LEFT WING LOWER STA 58.5 TEE CAP. REPLACED TEE CAP IAW EA AD-57-03766-MR. 2L72 4F A6WE 19950324005391995032400539WP 1995 3 24 ABXA9500240 119950319A32313927498503 ROD END DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR ATTACH ROD END LOOSE IN ATTACH ROD. REPLACED ROD ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950324005401995032400540WP 1995 3 24 ABXA9500241 119950318A528052210370P4101 BUSHING DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND WORN BUSHING IN ARM ASSEMBLY ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950324005411995032400541WP 1995 3 24 ABXA9500242 119950319A528052210370P4109 BUSHING DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING FOR ATTACH ROD TO FOLLOW UP ROD WORN ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950324005421995032400542WP 1995 3 24 ABXA9500243 119950319A528052210370P4109 BUSHING DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23956AX 47620 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING WORN IN THE ARM ASSEMBLY ON THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950324005431995032400543WP 1995 3 24 ABXA9500244 119950118A57555910053501 SPOILER DOUG DC9 DC932F 3022067WP LT WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING C-CHECK INSPECTION FOUND LEVEL II CORROSION, EXFOLIATION AND SEVERAL POPPED RIVETS ON THE SPOILER PANEL LOWER SURFACE. REPLACED SPOILER PANEL IAW DC-9 M.M. 27-62-1. 2L72 4F A6WE 19950324005441995032400544WP 1995 3 24 BAXA9500218 119950203A5330591141927 SKIN DOUG DC9 DC932 3022066WP BS 813 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C-CHECK INSPECTION FOUND CORROSION IN THE FUSELAGE SKIN LAP AT STA 813, LONGERON 26L FUSELAGE SKIN REPAIRED IAW ABX REA D953-10877-MR. 2L72 4F A6WE 19950324005451995032400545SO 1995 3 24 COM11835 119950321A5720 SUPPORTS EMB 120 EMB120RT SO RIBS 15/16 CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01266CA7874 7874 120258 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AT WING RIBS NR 15 AND NR 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2. P/N 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 3 EA; 120-17056-013, 1 EA; 120-17056-007, 1 EA; 120-17056-006, 1 EA; 120-17057-005, 1 EA. 2L72 4T RTA31SO 19950324005461995032400546EU 1995 3 24 COM31049 119950322A2450A2042C PDU SAAB SF340 SF340A 7850100EU LEFT DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01344CA2777 2712 340A025 LEFT DC GENERATOR DROPPED OFF LINE AND WILL NOT RESET. REPLACED THE LT POWER DISTRIBUTION UNIT. 2L72 4T RTA52EU 19950324005471995032400547 1995 3 24 COM60443 419950320A34183995100106 COMPUTER CNDAIRCL600 CL6002B19 EA STALL WARNING DEFECTIVE A COMAK NONE F FLT CONT AFFECTED APAPPROACH 1 SO01912CA3396 791 7011 THE STICK SHAKERS ACTIVATED DURING FINAL APPROACH. REPLACED THE STALL WARNING COMPUTER. 2L72 4F RTA21EA 19950324005481995032400548EA 1995 3 24 COM60444 119950321A2740601R92301951 HSTCU CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01926CA1151 501 7027 STABILIZER CHANNEL 1 STATUS MESSAGE. REPLACED THE HSTCU. 2L72 4F RTA21EA 19950324005491995032400549EA 1995 3 24 COM60445 119950321A2150 PACK CNDAIRCL600 CL6002B19 EA CABIN MALFUNCTIONED A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SO01917CA 7017 SMOKE IN COCKPIT AND CABIN WHEN USING LEFT AIR CONDITIONING PACK. DEFERRED LT ACM AND AIRCRAFT CONTINUED SERVICE. 2L72 4F RTA21EA 19950324005501995032400550WP 1995 3 24 SCNA95041 119950320A2910NAS59324 B-NUT DOUG DC10 DC1010 3022110WP NR 2 HYD SYS UNSECURE A SCNAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL15571SC 46645 ONE HOUR INTO FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY WENT TO .5 GALLON WITH ALL OTHER INDICATIONS NORMAL. DURING FLAP EXTENSION FROM 15 TO 22 DEGREES, NR 2 HYDRAULIC QUANTITY DROPPED TO NEAR ZERO, AND BOTH LOW PRESSURE LIGHTS ILLUMINATED. FOUND NR 2 HYDRAULIC SUPPLY LINE LEAKING AT FIRE SHUTOFF VALVE. RESECURED B-NUT, RESERVICED SYSTEM, AND LEAK CHECKED GOOD. 2L73 4F A22WE 19950324005511995032400551NM 1995 3 24 UPS202682 119950321A5755 SKIN BOEING727 72731C 1384011NM NR 9 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND NR 9 SPOILER DELAMINATED ON LOWER SURFACE OUTBOARD FWD CORNER. MAINTENANCE REPAIRED IAW SRM 57-50-6 AND 51-40-6. 2L73 4F A3WE 19950324005521995032400552NM 1995 3 24 UPS202683 119950321A5753 SKIN BOEING727 72731C 1384011NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD AFT FLAP HAS A PREVIOUS REPAIR THAT IS DELAMINATING ON UPPER SURFACE. MAINTENANCE REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950324005531995032400553NM 1995 3 24 UPS202684 119950321A5753 TE SKIN BOEING727 72731C 1384011NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE DELAMINATED 12 INCHES OUTBOARD OF INBOARD END. MAINTENANCE REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950324005541995032400554NM 1995 3 24 UPS202685 119950321A5752 TRIM TAB BOEING727 72731C 1384011NM LT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND OUTBOARD AILERON TRIM TRAILING EDGE DELAMINATED IN 2 AREAS ON LEFT WING. MAINTENANCE REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950324005551995032400555NM 1995 3 24 UPS202686 119950321A5753 TE SKIN BOEING727 72731C 1384011NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND RIGHT WING INBOARD MID FLAP TRAILING EDGE LOWER SURFACE DELAMINATED 63 INCHES FROM OUTBOARD END AND 18 INCHES FROM INBOARD END AROUND AFT FLAP TRACK CUTOUTS. MAINTENANCE REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950324005561995032400556NM 1995 3 24 UPS202687 119950321A5754 SLAT BOEING727 72731C 1384011NM NR 6 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT INBOARD END CRACKED. MAINTENANCE REPAIRED IAW SRM 51-30-2 AND 57-50-3. 2L73 4F A3WE 19950324005571995032400557NM 1995 3 24 UPS202688 119950321A5754 RIB BOEING727 72731C 1384011NM NR 4 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND NR 4 SLAT HAS CRACKED RIB AT SS 112 LOWER AFT CORNER. MAINTENANCE REPAIRED IAW SRM 57-50-3. 2L73 4F A3WE 19950324005581995032400558NM 1995 3 24 UPS202689 119950321A5754 RIB BOEING727 72731C 1384011NM NR 6 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN "D" CHECK, MAINTENANCE FOUND NR 6 SLAT HAS CRACKED RIB AT SS 225 AT AFT CORNER WHERE LOWER CHORD ATTACHES TO RIB. MAINTENANCE REPAIRED IAW SRM 57-50-3 AND 51-30-2. 2L73 4F A3WE 19950324005591995032400559NM 1995 3 24 UPS202690 119950321A5347 SEAT TRACK BOEING727 72751C 1384015NM BS 1166 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN "C" CHECK, MAINTENANCE FOUND CORROSION IN WELL OF SEAT TRACK AT STA 1166, RBL 45, WL 208. MAINTENANCE REPLACED SEAT TRACK IAW SRM 53-10-1, 51-10-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950324005601995032400560NM 1995 3 24 UPS202691 119950321A5754 CHORD BOEING727 72751C 1384015NM NR 3 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN "C" CHECK, MAINTENANCE FOUND NR 3 SLAT CHORD CRACKED AT TAI DUCT CUTOUT. MAINTENANCE REPAIRED IAW SRM 51-40-4. 2L73 4F A3WE 19950324005611995032400561NM 1995 3 24 UPS202692 119950321A5520 DOUBLER BOEING727 72751C 1384015NM RT ELEV CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN "C" CHECK, MAINTENANCE FOUND CORROSION ON RIGHT BALANCE PANEL WHERE BALANCE WEIGHT ATTACHES. MAINTENANCE FABRICATED NEW DOUBLER. 2L73 4F A3WE 19950324005621995032400562WP 1995 3 24 UPS802693 119950322A5320 FITTING DOUG DC8 DC871F 302199DWP BS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN "C" CHECK, MAINTENANCE FOUND STA 660 BELTFRAME DOOR FITTING CRACKED AT LONGERON 36. MAINTENANCE REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950324005631995032400563WP 1995 3 24 UPS802694 119950322A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1270 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN "C" CHECK, MAINTENANCE FOUND LONGERON 36 HAS 1.8 INCH CRACK ON AFT END AT STA 1270. MAINTENANCE REPAIRED IAW UPS EO DC8-5310-6795-A. 2L74 4F RT4A25 19950324005641995032400564WP 1995 3 24 UPS802695 119950322A3260 DOOR LIGHT DOUG DC8 DC871F 302199DWP RT MLG ILLUMINATED A IPXAO OTHER N FALSE WARNING DEDESCENT 1 SO01744UP 45994 PILOT REPORTED EXTENDED GEAR FOR EARLY DESCENT. GEAR RETRACTED DUE TO ATC. AFTER RETRACTION, RED 'DOOR NOT LATCHED' LIGHT REMAINED ILLUMINATED WITH RIGHT 'ALT GEAR DOOR' LIGHT ILLUMINATED. RECYCLED GEAR WITH SAME INDICATIONS. MAINTENANCE CHECKED RIGHT GEAR AND DOOR AREA. NO DEFECTS NOTED. TESTED RIGHT MAIN GEAR DOOR UPLATCH IAW MM 32-31-04, PAGE 503. CHECKS OK. LUBED GEAR. OK FOR SERVICE. 2L74 4F RT4A25 19950324005651995032400565NM 1995 3 24 UPS802696 119950323A5522 SKIN BOEING757 75724APF 1384969NM LT ELEV DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01408UP 23730 DURING SEGMENT 2 CHECK, MAINTENANCE FOUND LEFT ELEVATOR UPPER TRAILING EDGE DELAMINATED AT INBOARD PCU AT ELEVATOR STATION 100. MAINTENANCE REPAIRED IAW SRM 51-70-4 AND MM 51-21-10. 2L72 4F RTA2NM 19950324005661995032400566CE 1995 3 24 95ZZZX1386 119950209A2710MS202201 PULLEY BEECH 1900 1900C 1154161CE AILERON CONTL JAMMED A AXZWAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP0711ZR UB11 CEN/TUS - EN ROUTE - PILOT EXPERIENCED LEFT FLUTTER AND BUFFETING DURING PITCH OR ACFT ATTITUDE CHANGES. SUSPECTED CONTROL SURFACE PROBLEM ON THE GROUND, DURING AILERON MOVEMENT WITH THE YOKE AND HAND MOVEMENT ON THE CONTROL SURFACE, FELT SLIGHT BINDING. INSPECTED CABLE ROUTING OF ALL FLIGHT CONTROL SURFACES FROM COMPONENTS TO COCKPIT CONTROLS. FOUND RIVET HEAD JAMMED IN CABLE PULLEY (AILERON) BL 27. REMOVED RIVET HEAD FROM PULLEY. INSPECTED PULLEY FOR DAMAGE. NONE NOTED. INSPECTED ALL CABLE ROUTES FOR DEBRIS. NO OTHER DEBRIS NOTED. TEST FLEW AIRCRAFT. NO PROBLEMS NOTED ON TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 19950324005671995032400567CE 1995 3 24 95ZZZX1387 119950207A5230 CLOSE OUT PANELS BEECH 1900 1900C 1154161CE CARGO DOOR MISSING A AXZWAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 WP0711ZR 18400 UB11 HMO/TUS - EN ROUTE, CARGO DOOR, PN 1144301093, (AFT CABIN DOOR), OPENED IN-FLIGHT. PERFORMED FULL FUNCTIONAL, OPS CHECK AND RIG CHECK OF CARGO DOOR SYSTEM AND WARNING SYSTEM. ALL FUNCTIONS CHECK NORMAL. NO DEFECTS FOUND. INSPECTED AIRFRAME AND CARGO DOOR FOR STRUCTURAL DAMAGE IAW BEECH MM 52-30-00. NO DAMAGE NOTED ON DOOR STRUCTURE OR AIRFRAME STRUCTURE OR COMPONENTS. THREE CLOSE-OUT PANELS WERE FOUND MISSING ON INNER DOOR LINER. CLOSE OUT PANELS DEPARTED AIRCRAFT WHEN DOOR OPENED IN-FLIGHT. REPLACED CLOSE OUT PANELS. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 19950324005701995032400570NM 1995 3 24 95ZZZX1390 119950226A3260 CONNECTOR BOEING727 727151C 138404VNM NLG LOOSE A RYNAO OTHER N FALSE WARNING LDLANDING 1 CE07432EX 19867 UPON GEAR EXTENSION, 'UNSAFE' LIGHT (NOSE GEAR) CAME ON. PRIOR TO LANDING, NORMAL 'GEAR DOWN' LIGHT CAME ON; VISUAL INSPECTION WAS PERFORMED AND A NORMAL LANDING WAS MADE. TIGHTENED LOOSE CONNECTOR ON DOWNLOCK SWITCH. PERFORMED FULL GEAR SWING. ALL INDICATIONS NORMAL. 2L73 4F A3WE 19950324005711995032400571SW 1995 3 24 95ZZZX1391 119950216A612031024111 TUBE ASSY SWRNGNSA227 SA227AC 8780603SW LT ENGINE CRACKED A LVRAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW19343AE4874 AC554 APPROXIMATELY 20 MINUTES INTO CRUISE FLIGHT, LEFT ENGINE OIL PRESSURE STARTED DROPPING. THE PILOT MADE A PRECAUTIONARY SHUT DOWN AND RETURNED TO HOT. THE LOW PRESSURE OIL LINE GOING FROM THE PROP PITCH CONTROL TO THE GOVERNOR WAS FOUND LEAKING. THE LINE WAS REPLACED AND GROUND RUNS CHECKED NORMAL. 1L72 4T A8SW 19950324005721995032400572EU 1995 3 24 95ZZZX1392 119950228A2150 ACM JETAIRJETSTMJETSTM4101 1500501EU COCKPIT MALFUNCTIONED A VTZAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 EA27306UE 41020 IAD/BOS - FLT 6418 - DURING TAXI AFTER LANDING AT 1320 HRS ON 2-28-95, THE RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE COCKPIT WINDOWS FOGGED FROM HOT AIR ENTERING THE COCKPIT. AIRCRAFT ARRIVED AT GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED GROUND POWER RUNS AND INSPECTED ACM, BUT COULD NOT DUPLICATE DISCREPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95084. 2L72 4T RTA41NM 19950324005731995032400573NE 1995 3 24 95ZZZX1393 219950215A73207863916 HMU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE RT ENGINE DIRTY A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27418AW 289 PCE121104 LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1394. AND NR 95ZZZX1395. 2H72 4T4 TRTA13NM E20NE 19950324005741995032400574NE 1995 3 24 95ZZZX1394 219950215A73217836633005LS ECU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE RT ENGINE DIRTY A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27418AW 289 PCE121104 LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1393. AND NR 95ZZZX1395. 2H72 4T4 TRTA13NM E20NE 19950324005751995032400575NM 1995 3 24 95ZZZX1395 119950215A771210005000006 TORQUE SIGN COND DHAV DHC8 DHC8102 2809003NM RT ENGINE DIRTY A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27418AW 289 LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR VTZA95061, NR 95ZZZX1393. AND NR 95ZZZX1394. 2H72 4T RTA13NM 19950324005761995032400576NM 1995 3 24 95ZZZX1396 119950209A3260 GEAR LIGHT BOEING767 767231 1385131NM RT MLG MALFUNCTIONED A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE05610TW 22573 LAX - FLT 721 - ON DESCENT WHEN LANDING GEAR WAS EXTENDED, RT MLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND ALTERNATE LANDING GEAR EXTENSION. FOUND A-5 CARD, MFG PN 8-351-07, IN ELECTRONIC PROXIMITY SWITCH BOX. LANDING GEAR POSITION AND WARNING SYSTEM CHECKED AND B.I.T.E. CHECKED NORMAL. CHECK C-4A - 1-19-95 - JFK. 2L72 4F RTA1NM 19950324005771995032400577NE 1995 3 24 95ZZZX1397 219950206A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RIGHT FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE05904TW 49156 MCI - FLT 119 - DURING CLIMB, RT ENGINE LOST POWER. SHUT DOWN ENGINE. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE SN 3257. ENGINE TOTAL TIME: 19,850 HOURS, 10,375 CYCLES. CHECK C-2D - 1 13-94 - MCI. 2L72 4F4 F A6WE E9NE 19950324005781995032400578NM 1995 3 24 95ZZZX1398 119950202A5713 STRINGER BOEING727 727231 1384079NM WS 656.50 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0584357 21989 MCI - DURING OP-17, FOUND CRACK IN LT WING FUEL TANK IN TOP AFT NR 3 STRINGER, WS 656.50, AT RIB NR 6 ATTACH POINT. REPAIRED PER SSRM 57-20-201, PAGE 215, FIGURE 207. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES. 2L73 4F A3WE 19950324005791995032400579NM 1995 3 24 95ZZZX1399 119950204A5754 SKIN BOEING727 727231 1384079NM NR 5 LE SLAT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554350 21969 JFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES. 2L73 4F A3WE 19950324005801995032400580NE 1995 3 24 95ZZZX1400 219950209A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE LEFT FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05916TW 49187 STL - FLT 223 - DURING CLIMB, HAD SMOKE IN CABIN. SELECTED FULL RATE CABIN PRESSURE AND FULL COLD, AND CABIN CLEARED. FOUND OIL IN 8TH STAGE AIR DUCT OF LEFT ENGINE SN 1215. REPLACED LEFT ENGINE. ENGINE TOTAL TIME: 18,588 HOURS; 9,630 CYCLES. CHECK C-1D - 1-30-95 - MCI. 2L72 4F4 F A6WE E9NE 19950324005811995032400581SW 1995 3 24 95ZZZX1401 119950210A53112722125021 FRAME SWRNGNSA227 SA227AC 8780603SW FS 133.87 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22125-021 AT FS 133.87 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950324005821995032400582SW 1995 3 24 95ZZZX1402 119950210A53112722100035 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING MAINTENANCE INSPECTION, FOUND LT LOWER BELT FRAME PN 27-22100-035 AT FS 242 CRACKED AT LOWER CORNER CUT OUT RADIUS. COMPLETE REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. 1L72 4T A8SW 19950324005831995032400583SW 1995 3 24 95ZZZX1403 119950210A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.24 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND INNER RT FLANGE OF CONSTANT FRAME PN 27-22093-146 AT FS 174.24 CRACKED AT FLANGE BEND RADIUS. COMPLETED REPAIR TO THE FRAME FLANGE IAW FAIRCHILD SRM REPAIR SCHEME NR 20. 1L72 4T A8SW 19950324005841995032400584SW 1995 3 24 95ZZZX1404 119950210A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.24 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING AMAINTENANCE INSPECTION, FOUND UPPER LT FLANGE OF CONSTANT FRAME PN 27-22093-146 AT FS 174.24 CRACKED AT THE FLANGE BEND RADIUS. COMPLETED REPAIRS TO THE FRAME FLANGE IAW FAIRCHILD SRM 53-90-20 REPAIR NR 19. 1L72 4T A8SW 19950324005851995032400585SW 1995 3 24 95ZZZX1405 119950210A53112722093145 FRAME SWRNGNSA227 SA227AC 8780603SW FS 145.95 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22093-145 AT FS 145.95 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950324005861995032400586SW 1995 3 24 95ZZZX1406 119950210A53112722104047 FRAME SWRNGNSA227 SA227AC 8780603SW FS 212.27 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22104-047 AT FS 212.27 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950324005871995032400587SW 1995 3 24 95ZZZX1407 119950210A5330 SKIN SWRNGNSA227 SA227AC 8780603SW FS 461-487 DAMAGED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND RT AFT EXTERNAL SKIN BETWEEN FS 461 AND FS 487 CREASED. COMPLETED REPAIR TO FUSELAGE EXTERIOR SKIN PANEL IAW FAIRCHILD SRM. 1L72 4T A8SW 19950324005881995032400588SW 1995 3 24 95ZZZX1408 119950210A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND LT FLAP WALKING BEAM ROLLER BEARING SUPPORT DOUBLER PN 27-31141-001 WORN. COMPLETED REPAIR BY THE PART-FOR-PART REPLACEMENT OF THE ROLLER BEARING SUPPORT DOUBLER IAW FAIRCHILD SRM. 1L72 4T A8SW 19950324005891995032400589SW 1995 3 24 95ZZZX1409 119950210A52302724050083 FRAME SWRNGNSA227 SA227AC 8780603SW CARGO DOOR DENTED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND LOWER FRAME MEMBER OF THE AFT CARGO DOOR PN 27-24050-083 DENTED. COMPLETED REPAIR TO THE AFT CARGO DOOR BY THE PART-FOR-PART REPLACEMENT IAW THE FAIRCHILD SRM. 1L72 4T A8SW 19950324005901995032400590SW 1995 3 24 95ZZZX1410 119950210A53112722093145 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.24 CRACKED A VFSAK NONE O OTHER ININSP/MAINT 1 NE0563NE AC763B MSP - DURING A MAINTENANCE INSPECTION, FOUND RT LOWER BELT FRAME PN 27-22093-145 AT FS 159.24 CRACKED AT THE UPPER CORNER CUT OUT RADIUS. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW FAIRCHILD SRM. 1L72 4T A8SW 19950324005911995032400591WP 1995 3 24 ASAA9540 119950127A32605758405401 THROTTLE SWITCH DOUG DC9 DC983 3022083WP COCKPIT DEFECTIVE A ASAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM01968AS 53016 SEA - FLT 574 - AIR TURN-BACK. CREW REPORTED ALL 3 GEAR RED LIGHTS ON AND GEAR WARNING HORN SOUNDED AFTER GEAR RETRACTED. CYCLED GEAR AND CONDITION REPEATED. REMOVED AND REPLACED THE LEFT THROTTLE SWITCH ASSEMBLY S319 AND OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19950324005921995032400592WP 1995 3 24 ASAA9551 119950208A52302024T3 SKIN DOUG DC9 DC982 3022082WP MID CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01931AS 49232 PAE - DURING 30K CHECK, A DENT WAS FOUND IN MID-CARGO COMPARTMENT DOOR. REMOVED DAMAGED AREA. FABRICATED DOUBLER, FILLER AND SHIMS. INSTALLED REPAIR WITH SEALANT AND SECURED WITH FASTENERS IAW SRM 52-05, FIGURE 3 AND 5-10-03, PGS 15 AND 18. (X) 2L72 4F A6WE 19950324005931995032400593EU 1995 3 24 AWXA9500103 119950222A3260 SENSORS AIRBUS320 A320231 3930325EU RT MLG DOOR DIRTY A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28621AW 053 LAS/RNO - FLT 523 - AIR TURNBACK. RT MAIN GEAR DOOR WOULD NOT INDICATE CLOSED UPON GEAR RETRACTION. AIRCRAFT RETURNED TO LAS WITH NR 2 MAIN GEAR DOOR INDICATING UNLOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MX PERFORMED RIG CHECK ON UNLOCK AND GROUND OPENING SYSTEM, AND CLEANED UPLOCK MECHANISM AND SENSORS. PERFORMED FUNCTIONAL TEST OF LANDING GEAR DOOR CLOSED DETECTORS PER SIL 32 067. RIG CHECK PERFORMED PER AMM 32 31 33 AND AMM 32 12 00, OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950324005941995032400594NM 1995 3 24 AWXA9500105 119950220A3350 EEL CONNECTOR BOEING757 7572G7 1384963NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 15 THROUGH 18. RECONNECTED EMERGENCY LIGHTS AT ROW 16, OPS CHECK GOOD. (X) 2L72 4F RTA2NM 19950324005951995032400595NM 1995 3 24 AWXA9500109 119950227A5320 ANGLE BOEING737 737277 1384570NM BS 328 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - DURING C6 INSPECTION, FOUND CRACK IN INTERCOSTAL TO FLOOR BEAM TIE ANGLE, FORWARD SIDE OF STA 328 AT LBL 45. INSTALLED NEW TIE ANGLE PER SRM 53 10 2 AND SRM 51 30 2. (X) 2L72 4F RTA16WE 19950324005961995032400596NM 1995 3 24 AWXA9500110 119950227A5260 DRIP PAN BOEING737 737277 1384570NM AIR STAIRS CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28187AW 22654 PHX - DURING C6 INSPECTION, FOUND 12 INCH CRACK IN OUTBOARD CORNER OF AIR STAIR DRIP PAN. REPAIRED CRACK PER SRM 51 40 9, PARAGRAPH 7. (X) 2L72 4F RTA16WE 19950324005971995032400597SW 1995 3 24 LOSA9513 119950223A2910 HYDRAULIC LINE SWRNGNSA227 SA227AC 8780603SW LEFT WING CRACKED A LOSAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23165SW AC514 CREW REPORTED THAT RIGHT AND LEFT HYDRAULIC PRESSURE LIGHTS CAME ON IN-FLIGHT FLUCTUATING AND ZERO PSI HYDRAULIC PRESSURE, FLEW APPROXIMATELY 25 MINUTES IN THIS CONDITION. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CRACKED HYDRAULIC LINE IN LEFT WING STUB ROOT ABOVE ACM. REPLACED LINE AND SERVICED HYDRAULIC SYSTEM. PERFORMED ENGINE RUN-UPS AND LEAK CHECK SYSTEM. RESULTS: SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 1L72 4T A8SW 19950324005981995032400598WP 1995 3 24 LOSA9514 219950221A7321895D935 DIAPHRAGM WOODWARD 8973515 SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT FUEL CONTROL LEAKING A LOSAO OTHER K FLUID LOSS TOTAKEOFF 1 WP23165SW2931 1821504 AC514 P44415 CREW REPORTED RIGHT ENGINE WAS UNABLE TO OBTAIN CHARTED TAKEOFF POWER, WITH RIGHT POWER LEVER FULL FORWARD. EGT WAS 600 DEGREES AND TORQUE 76 PERCENT AT 100.5 PERCENT RPM. CHARTED TORQUE WAS 84 PERCENT. MAINTENANCE REPLACED P2T2 SENSOR AND FUEL CONTROL PS3 ROLLING DIAPHRAGM. ADJUSTED MAX FUEL FLOW PER GARRTT MM 72-00-00. ENGINE RUN-UP SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 1L72 4T4 T A8SW E4WE 19950324005991995032400599SW 1995 3 24 SWHA95002 119950222A32302752004045 UPLOCK HOOK SWRNGNSA227 SA227AC 8780603SW NLG WORN A SWHAO OTHER J WARNING INDICATION APAPPROACH 1 SW17373PH AC538 BPT/AUS - ON SCHEDULED FLIGHT, LANDING APPROACH AT AUS, NOSE LANDING GEAR FAILED TO EXTEND NORMALLY. THE GEAR WAS EXTENDED BY EMERGENCY PROCEDURES, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED NOSE GEAR UPLOCK HOOK ASSEMBLY TO BE EITHER WORN AND OUT OF ADJUSTMENT OR POSSIBLY MISDRILLED DURING EARLIER INSTALLATION. THE NOSE UPLOCK HOOK ASSY WAS REMOVED AND REPLACED WITH ASSY PN 27 52019-8001, RIGGED AND FUNCTIONALLY TESTED AND RETURNED TO SERVICE. (X) 1L72 4T A8SW 19950324006001995032400600NM 1995 3 24 TAOA029516 119950227A2910AE2460010H0360 HYDRAULIC HOSE BOEING727 727254 138408LNM RT MLG LEAKING A TAOAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15914TS 20251 LGA/DCA - FLT 6541 - LOST A-SYSTEM HYDRAULIC PRESSURE DURING GEAR RETRACTION. AIRCRAFT DIVERTED TO EWR. REPLACED RT MLG DOWN HOSE. REPLACED A-SYSTEM HYDRAULIC FILTERS SERVICED, BLED AND PERFORMED OPERATIONAL CHECK OF SYSTEM. (X) 2L73 4F A3WE 19950324006011995032400601NM 1995 3 24 TWRA9512 119950224A534065B09641 SUPPORT FITTING BOEING747 747121 1384871NM CABIN DOOR CORRODED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15609FF 20354 DURING B-SERVICE, WHILE INSPECTING 2L M.E.D. GIRT BAR FITTING, FOUND TWO STEEL PINS (HIGH LOCK FASTENERS) CORRODED. REPLACED FITTING AND ATTACHING HARDWARE. INSPECTED PER SB 747-53A2378. (X) 2L74 4F A20WE 19950324006021995032400602NM 1995 3 24 TWRA9513 119950224A534065B09641 SUPPORT FITTING BOEING747 747121 1384871NM CABIN DOOR CORRODED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15609FF 20354 DURING B-SERVICE WHILE INSPECTING 5L MAIN ENTRY DOOR FITTING, FOUND AFT GIRT BAR FITTING CORRODED. REPLACED FITTING AND ATTACHING HARDWARE. INSPECTED PER SB 747-53A2378. (X) 2L74 4F A20WE 19950324006031995032400603NM 1995 3 24 VTZA95061 119950215A301085720015004 LE BOOT DHAV DHC8 DHC8102 2809003NM RT WING FAILED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27418AW 289 LGA/IAD - FLT 6322 - DURING CRUISE AT 910 HOURS ON 2-15-95, RT WING BOOT NR 2 SECTION WILL NOT INFLATE, AND RT TORQUE FLUCTUATED 10 PERCENT. AIRCRAFT DIVERTED TO SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEADING EDGE ASSEMBLY AND CLEANED THE RT ENGINE ECU, HMU, AND TSCU CONNECTORS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: CONTROL NR 95ZZZX1393, NR 95ZZZX1394. AND NR 95ZZZX1395. (X) 2H72 4T RTA13NM 19950324006041995032400604NE 1995 3 24 VTZA95065 219950216A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27318UE147 41041 P76062 IAD/TYS - FLT 6355 - DURING CLIMB ON 2-16-95 AT 1830 HRS, THE RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE CLEANED CHIP DETECTOR PER ALLIED SIGNAL. ENGINE IS SET FOR RESAMPLE AT 25 HRS PER ALLIED SIGNAL. AIRCRAFT WAS THEN FERRIED TO LYH PER ALLIED SIGNAL SERVICE LETTER. LYH MAINTENANCE REPLACED ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950324006051995032400605EU 1995 3 24 VTZA95066 119950220A5270MS161065 SWITCH BAG JETSTMJETSTM3201 1500217EU BAGGAGE COMPT OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27492UE 790 HPN/IAD - FLT 6161 - DURING CLIMB-OUT AT 1810 HRS ON 2-20-95, POD DOOR LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO HPN WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03180 IAW MEL 52-1 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 03180 BY ADJUSTING THE POD DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324006061995032400606EU 1995 3 24 VTZA95067 119950216A32301849E UPLOCK ASSY BAG JETSTMJETSTM3201 1500217EU NLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27370MT 800 LYN/RIC - FLT 6908 - DURING APPROACH ON 2-16-95 AT 0630 HRS, THE NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. CREW SAID GEAR REMAINED IN WHEELWELL. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO LYH. LYN MAINTENANCE REPLACED THE UPLOCK ASSY, OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324006071995032400607NE 1995 3 24 VTZA95068 219950214A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27309UE2543 41022 P75008 IAD/RIC - FLT 6537 - DURING CLIMB-OUT ON 2-14-95 AT 1445 HRS, THE LEFT OIL CONTAMINATION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED THE CHIP DETECTOR AND PERFORMED A SOAP SAMPLE. AIRCRAFT HAS BEEN FERRIED TO LYH FOR FURTHER GEARBOX INSPECTION. UPON FURTHER INSPECTION, MAINTENANCE REPLACED THE LEFT ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950324006081995032400608EU 1995 3 24 VTZA95069 119950217A261172111211000 SMOKE DETECTOR JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE COMPT FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27304UE 41017 IAD/BOS - FLT 6481 - DURING CLIMB-OUT ON 2-17-95 AT 1000 HRS, THE POD SMOKE LIGHT ILLUMINATED. AN IN-FLIGHT EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 21787 IAW MEL 26-3 ON THE FIRE DETECTION SYSTEM. MAINTENANCE LATER CLEARED DMI NR 21787 ON 2-18-95 BY REPLACING THE SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950324006091995032400609EU 1995 3 24 VTZA95070 119950222A3231137121C DOOR BAG JETSTMJETSTM3201 1500217EU NOSE GEAR OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27475UE 850 IAD/EWR - FLT 6433 - AFTER TAKEOFF AT 2100 HRS ON 2-22-95, NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH WHEN GEAR WAS RETRACTED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND NOSE GEAR DOOR OUT OF ADJUSTMENT. READJUSTED DOOR, AND OPS CHECK GOOD. (X) 2L72 4T RTA56EU 19950324006101995032400610WP 1995 3 24 VTZA95071 219950220A732189778025 FUEL CONTL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27471UE 821 PHF/IAD - FLT 6240 - DURING TAKEOFF AT 1040 HRS ON 2-20-95, TAKEOFF WAS ABORTED DUE TO THE LEFT ENGINE TORQUE DROPPING TO 60 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA56EU E4WE 19950324006111995032400611EU 1995 3 24 VTZA95072 119950221A243051539019E GCU JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27317UE 41031 IAD/CLE - FLT 6319 - DURING CLIMBOUT AT 0839 HRS ON 2-21-95, THE LEFT GENERATOR CAME OFF LINE AND WOULD NOT RESET. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE GCU. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950324006121995032400612EU 1995 3 24 VTZA95073 119950221A243523095002 STARTER/GEN JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 EA27317UE 41031 IAD/CLE - FLT 6319 - DURING TAKEOFF AT 0957 HRS ON 2-21-95, ABORTED TAKEOFF DUE TO LT GENERATOR COMING OFF LINE DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950324006131995032400613EU 1995 3 24 VTZA95074 119950222A7931 OIL PRESS IND BAG JETSTMJETSTM3201 1500217EU LT ENGINE MALFUNCTIONED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27484UE 899 ALB/IAD - FLT 6156 - DURING TAKEOFF AT 1930 HRS ON 2-22-95, ABORTED TAKEOFF DUE TO THE LEFT ENGINE OIL PRESSURE INDICATION MOMENTARILY PEGGING TO THE HIGH SIDE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM DURING POWER RUNS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324006141995032400614WP 1995 3 24 VTZA95076 219950223A7320 GOVERNOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33110U 01514WP RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27313UE 41026 IAD/EWR - FLT 6278 - DURING TAKEOFF ROLL AT 1515 HRS ON 2-23-95, FLIGHT CREW ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE OVERSPEED GOVERNOR IDLE SETTING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E4WE 19950324006151995032400615EU 1995 3 24 VTZA95077 119950223A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR FAILED A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27494UE 810 EWR/SWF - FLT 6504 - DURING APPROACH, AT 1330 HRS ON 2-23-95, AN IN-FLIGHT EMERGENCY WAS DECLARED DUE TO THE NOSE GEAR DOWN AND LOCKED LIGHT AND THE INTRANSIT LIGHT ILLUMINATING SIMULTANEOUSLY. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS AT SWF. MAINTENANCE REPLACED THE DOWNLOCK SWITCH. ACFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324006161995032400616EU 1995 3 24 VTZA95078 119950223A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27370MT 800 IAD/SCE - FLT 6475 - DURING CRUISE AT 1800 HRS ON 2-23-95, AN IN-FLIGHT EMERGENCY WAS DECLARED DUE TO THE NOSE GEAR DOWN AND LOCKED LIGHT NOT ILLUMINATING. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DOWNLOCK MICROSWITCH AND REPAIRED WIRE NR F47. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950324006171995032400617EU 1995 3 24 VTZA95082 219950228A73208974575 BYPASS VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG FUEL FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27477UE 890 IAD/LGA - DURING TAKEOFF AT 0915 HRS ON 2-28-95, ABORTED THE TAKEOFF DUE TO THE LT ENGINE ONLY MAKING 92 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED TTL BYPASS VALVE. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA56EU E4WE 19950324006181995032400618EU 1995 3 24 VTZA95083 119950301A243523079009 STARTER GEN BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A VTZAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27488UE 907 FLT NR 6172 - IAD-LYH - DURING CRUISE AN EMERGENCY WAS DECLARED DUE TO THE RT GENERATOR FAILING IN FLIGHT. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950331000011995033100001EU 1995 3 31 950467SHOP 119950217A71202380204501 CROSS BEAM AIRBUS320 A320211 3930320EU FWD ENG MOUNT WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01 DURING ENGINE SHOP OVERHAUL, SEVERAL FORWARD ENGINE MOUNT CROSS BEAMS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG.803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.002 INCH TO 0.011 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-095124A. 2L72 4F RTA28NM 19950331000021995033100002EU 1995 3 31 9504683207 119950217A5320D53480043203 SILL AIRBUS320 A320211 3930320EU FS 32571 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307US 106 DURING INTERMEDIATE LAYOVER VISIT, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT CABIN DOOR LOWER SILL. CORROSION WAS FOUND AROUND EXISTING NUT PLATES. REPAIR ACCOMPLISHED PER NWA EA 32-96362. 2L72 4F RTA28NM 19950331000031995033100003EU 1995 3 31 9504693207 119950317A5320D53472189200 FLOOR SUPPORT AIRBUS320 A320211 3930320EU FS 32571-33096 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01307US 106 DURING THE INTERMEDIATE LAYOVER VISIT, THE AFT GALLEY FLOOR SUPPORT AT Y=1165 BETWEEN FRAME 68 AND 69 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE UPPER FLANGE. CORROSION IN LOCALIZED AROUND ONE FASTENER ATTACH HOLE FOR FLOOR BOARDS AT APPROXIMATELY X=3942. REPAIR ACCOMPLISHED PER NWA EA 32-97830. 2L72 4F RTA28NM 19950331000041995033100004NE 1995 3 31 9504702290 219950320A7260 GEARBOX BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE DAMAGED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL01290US 21378 696275 NR 2 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED WHILE CRUISING AT FL330. INDICATED OIL PRESSURE WAS 15 PSI. A PRECAUTIONARY SHUTDOWN WAS PERFORMED. THE FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE THREADS FOR THE MAIN OIL FILTER ATTACH STUDS PULLED OUT OF THE GEARBOX. THE GEARBOX WAS REPLACED. THE ENGINE WAS RUN-UP AND CHECKED OK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950331000051995033100005NE 1995 3 31 9504719972 219950221A7261 OIL CAP DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE NOT SECURE A NWAAA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 GL019336 47338 666789 NR 1 ENGINE OIL QUANTITY DECREASED TO 7 QUARTS ON TAKEOFF. REPORTS FROM THE TOWER INDICATED FLUID LEAKING FROM THE LEFT ENGINE. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OIL TANK CAP UNSECURED. THE OIL WAS SERVICED AND THE CAP WAS SECURED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950331000061995033100006NM 1995 3 31 QXEA9500088 119950323A3350P4010021 BATTERY DHAV DHC8 DHC8102 2809003NM CABIN FLASHLIGHTDISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09102AV 91 DURING PREFLIGHT, FOUND FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT INOP. BATTERY REPLACED AND LIGHT FUNCTION TESTED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2H72 4T RTA13NM 19950331000071995033100007NM 1995 3 31 SWAA950248 119950321A33506013211 EEL BATTERY BOEING737 7372H4 138448CNM LT OVERWING DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LEFT OVERWING LIGHT BATTERY PER BOEING M/M. 2L72 4F A16WE 19950331000081995033100008NM 1995 3 31 SWAA950249 119950319A33507003661 EEL BALLAST BOEING737 7373H4 1384600NM RT OVERWING INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED LIGHT BALLAST ASSEMBLY PER BOEING M/M. 2L72 4F RTA16WE 19950331000091995033100009NM 1995 3 31 SWAA950250 119950319A33506104781 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07354SW 25219 DURING OVERNIGHT CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP. REPLACED TWO FLOOR TRACK BATTERY PACKS PER BOEING M/M. 2L72 4F RTA16WE 19950331000101995033100010NM 1995 3 31 SWAA950251 119950321A335020131A EEL BATTERY BOEING737 7373H4 1384600NM L2 DOOR DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07355SW 25250 DURING SCHEDULED SERVICE CHECK, FOUND LEFT AFT ENTRY DOOR EMERGENCY LIGHTING INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950331000111995033100011NM 1995 3 31 SWAA950252 119950321A3350110049 EEL BATT HOUSING BOEING737 7373T0 1384582NM CABIN FAILED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07684WN 23941 DURING SCHEDULED SERVICE CHECK, FOUND CABIN FORWARD SECTION OF FLOOR TRACK LIGHTING INOP. REPLACED BATTERY CHARGER HOUSING PER BOEING M/M. 2L72 4F RTA16WE 19950331000121995033100012NM 1995 3 31 SWAA950253 119950320A335020131A EEL BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07522SW 26564 DURING SCHEDULED SERVICE CHECK, FOUND A CABIN EMERGENCY LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950331000131995033100013NM 1995 3 31 SWAA950254 119950323A5330 SKIN BOEING737 7372H4 138448CNM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0796SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACK AT BS 767, 11 INCHES ABOVE SKIN LAP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331000141995033100014EU 1995 3 31 95ZZZZ154 119950223A5230 SEALS FOKKERF28 F28MK0100 4990807EU CARGO DOOR LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19856US 11286 CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THE LEFT ENGINE CHANGE OVER SWITCH. OPERATIONS CHECKED NORMAL. REFERENCE NR USAA950218. 2L72 4F RT 19950331000151995033100015EU 1995 3 31 95ZZZZ155 119950301A21303965161 VALVE FOKKERF28 F28MK0100 4990807EU RIGHT INOPERATIVE A USAAO OTHER O OTHER CRCRUISE 1 EA19856US 11286 PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE. OPERATIONS CHECKED GOOD. REFERENCE USAA950201. 2L72 4F RT 19950331000161995033100016NE 1995 3 31 95ZZZZ156 319950228A6114 PROPELLER HUB BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RT ENGINE LEAKING OIL A JJBAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA01836CA2603 UE32 AIRCRAFT WAS EN ROUTE FROM BUF TO ALBANY NY, PILOT OBSERVED OIL PRESSURE DROPPING ON RIGHT ENGINE. THE AIRCRAFT DIVERTED TO SYR NY AND LANDED UNEVENTFUL. INVESTIGATION OF LOW OIL PRESSURE REVEALED OIL LEAKING FROM PROP. PROP REMOVED AND REPLACED AND UNIT RETURNED TO HARTZELL FOR INVESTIGATION. (Z) 2L72 4T RTA24CE 5 CP10NE 19950331000171995033100017WP 1995 3 31 95ZZZZ157 119950219A217017946081 WATER SEPARATOR DOUG DC9 DC951 3022051WP AFT FUSELAGE FAILED A HALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13679HA 452915 47662 HNL - FLT 504 - WITH THE LEFT PACK ON, THE CABIN FILLED WITH SMOKE. IN AUTO MODE DUCT TEMP WENT TO MAXIMUM HOT. PACK DID NOT SHUT DOWN. REPLACED THE LEFT AND RIGHT WATER SEPARATORS. LEAK CHECK IN SERVICE OK. REPLACED THE LEFT TURBINE COOLING ASSY, LEAK CHECK AND OPS CHECK OK. REMOVED AND REPLACED THE RT TURBINE COOLING ASSY. THE LEAK CHECK AND OPS CHECK OK. RAN PACKS FOR 20 MINUTES WITH APU AND 15 MINUTES WITH ENGINE AND NO SMOKE. REFERENCE 95ZZZZ158 AND 159 AND HAL95020. 2L72 4F A6WE 19950331000181995033100018WP 1995 3 31 95ZZZZ158 119950219A21502049505 COOLING TURBINE DOUG DC9 DC951 3022051WP AFT FUSELAGE FAILED A HALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13679HA 421351 47662 HNL - FLT 504 - WITH THE LEFT PACK ON, THE CABIN FILLED WITH SMOKE. IN AUTO MODE DUCT TEMP WENT TO MAXIMUM HOT. PACK DID NOT SHUT DOWN. REPLACED THE LEFT AND RIGHT WATER SEPARATORS. LEAK CHECK IN SERVICE OK. REPLACED THE LEFT TURBINE COOLING ASSY, LEAK CHECK AND OPS CHECK OK. REMOVED AND REPLACED THE RT TURBINE COOLING ASSY. THE LEAK CHECK AND OPS CHECK OK. RAN PACKS FOR 20 MINUTES WITH APU AND 15 MINUTES WITH ENGINE AND NO SMOKE. REFERENCE 95ZZZZ157, 159 AND HAL95020. 2L72 4F A6WE 19950331000191995033100019WP 1995 3 31 95ZZZZ159 119950219A21502049505 COOLING TURBINE DOUG DC9 DC951 3022051WP AFT FUSELAGE FAILED A HALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13679HA 161784 47662 HNL - FLT 504 - WITH THE LEFT PACK ON, THE CABIN FILLED WITH SMOKE. IN AUTO MODE DUCT TEMP WENT TO MAXIMUM HOT. PACK DID NOT SHUT DOWN. REPLACED THE LEFT AND RIGHT WATER SEPARATORS. LEAK CHECK IN SERVICE OK. REPLACED THE LEFT TURBINE COOLING ASSY, LEAK CHECK AND OPS CHECK OK. REMOVED AND REPLACED THE RT TURBINE COOLING ASSY. THE LEAK CHECK AND OPS CHECK OK. RAN PACKS FOR 20 MINUTES WITH APU AND 15 MINUTES WITH ENGINE AND NO SMOKE. REFERENCE 95ZZZZ157, 158 AND HAL95020. 2L72 4F A6WE 19950331000201995033100020WP 1995 3 31 HAL95020 119950219A217017946081 WATER SEPARATOR DOUG DC9 DC951 3022051WP AFT FUSELAGE FAILED A HALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13679HA 262045 47662 HNL - FLT 504 - WITH THE LEFT PACK ON, THE CABIN FILLED WITH SMOKE. IN AUTO MODE DUCT TEMP WENT TO MAXIMUM HOT. PACK DID NOT SHUT DOWN. REPLACED THE LEFT AND RIGHT WATER SEPARATORS. LEAK CHECK IN SERVICE OK. REPLACED THE LEFT TURBINE COOLING ASSY, LEAK CHECK AND OPS CHECK OK. REMOVED AND REPLACED THE RT TURBINE COOLING ASSY. THE LEAK CHECK AND OPS CHECK OK. RAN PACKS FOR 20 MINUTES WITH APU AND 15 MINUTES WITH ENGINE AND NO SMOKE. REFERENCE 95ZZZZ157, 158, 159. 2L72 4F A6WE 19950331000211995033100021WP 1995 3 31 HAL95023 119950303A335060030431 EEL POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 14146 47796 HNL - THE EMERGENCY CEILING LIGHT AT ROWS 16-18 WILL NOT COME ON. REPLACED THE BATTERIES IN THE EMERGENCY PACK AND IT WAS NO HELP. REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND THE OPERATIONAL CHECK WAS GOOD. (Z) 2L72 4F A6WE 19950331000221995033100022WP 1995 3 31 HAL95024 119950305A335041B004A007G3 EEL BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 47654 HNL - THE EMERGENCY EXIT LIGHT AT BOTH AFT OVERWING EXITS (ROW 18) IS OUT. REPLACED THE EMERGENCY POWER SUPPLY BATTERIES ABOVE THE OVERWING EXITS. THE OPERATIONAL CHECK WAS GOOD. (Z) 2L72 4F A6WE 19950331000231995033100023NM 1995 3 31 TSAA9527044 119950303A5513 SKIN BOEING737 7373Y0 1384671NM RT ELEV TAB CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING HEAVY MAINTENANCE VISIT, FOUND RT ELEVATOR TAB SKIN CRACKED AT NR 2 HINGE TOP SIDE. REPAIRED PER ECO 2560. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950331000241995033100024NM 1995 3 31 TSAA9527045 119950303A5513 SKIN BOEING737 7373Y0 1384671NM LT ELEV TAB DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING HEAVY MAINTENANCE VISIT, FOUND LEFT ELEVATOR TAB WITH TEAR IN SKIN AT INBOARD BEARING. REPAIRED PER ECO 2560. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950331000251995033100025NM 1995 3 31 TSAA9527047 119950303A5754 SKIN BOEING737 7373Y0 1384671NM NR 3 LE SLAT CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING HEAVY MAINTENANCE VISIT, FOUND NR 3 LEADING EDGE SLAT LOWER SKIN SURFACE STARTING TO CORRODE AROUND FASTENER HEADS, TWO EACH. REPAIRED PER ECO 2562 PART I. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950331000261995033100026NM 1995 3 31 TSAA9527048 119950303A5754 SKIN BOEING737 7373Y0 1384671NM NR 3 LE SLAT CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING HEAVY MAINTENANCE VISIT, FOUND SEVERAL BULGE SPOTS AROUND FASTENER HEAD ON NR 3 LE SLAT LOWER SKIN SURFACE. REPAIRED PER ECO 2562 PART I. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950331000271995033100027NM 1995 3 31 TSAA9532049 119950306A2910 HYD LINE BOEING737 7372T4 1384492NM NLG FAILED A TSAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13808AL 23445 PILOT REPORT FLT 97 - HNL-LIH - NOSE GEAR WOULD NOT COME UP AFTER TAKEOFF. RETURNED TO HNL. FOUND RUPTURED LINE ON DOWNLOCK ACTUATOR. REPLACED LINE. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SREVICE. (Z) 2L72 4F A16WE 19950331000281995033100028NM 1995 3 31 TSAA9552042 119950224A5270 SWITCH BOEING737 737297 1384480NM EQUIPMENT DOOR LACK OF LUBE A TSAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP1370724 21740 FLT NR 210 - HNL-OGG - EQUIPMENT DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. REJECTED TAKEOFF. LUBRICATED WARNING SWITCH AND CYCLED EQUIPMENT DOOR. OPERATIONAL CHECK OKAY, AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950331000291995033100029NM 1995 3 31 TSAA9555046 119950303A5510 BEAM BOEING737 7373Y0 1384671NM HORIZ STAB TE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13304AL 23500 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION ON RT HORIZONTAL STABILIZER T/E BEAM UPPER CAP AT SS70 AND SS166. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950331000301995033100030NM 1995 3 31 TSAA9580043 119950228A80122730426 START VALVE BOEING737 737297 1384480NM NR 2 ENGINE MALFUNCTIONED A TSAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP1370724 21740 FLT 285 - KOA-HNL - NR 2 ENGINE START VALVE OPEN LIGHT CAME ON INFLIGHT. WHEN POWER WAS RETARDED LIGHT WENT OUT. PRECAUTIONARY LANDING (KOA) WAS ACCOMPLISHED. REPLACED NR 2 ENGINE START VALVE. REPLACED STARTER, GARLOCK SEAL, AND SPLINE AS A PRECAUTION. FUNCTIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950331000321995033100032NM 1995 3 31 USAA950097 119950206A5230 STOPS BOEING737 737201 1384454NM FWD CARGO DOOR OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19227AU 21816 CLT - FLT 435 - ON CLIMB-OUT THROUGH 8000 FEET, FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED ON MEL 52-3. REPLACED OVERHEAD ANNUNCIATOR MODULE PRECAUTIONARY, FOUND FWD CARGO DOOR STOP PINS BACKED OUT AROUND PROX SWITCH. ADJUSTED ALL FWD CARGO DOOR STOPS AS PER B737 MM, CLEARED MEL. (Z) 2L72 4F A16WE 19950331000331995033100033NM 1995 3 31 USAA950151 119950130A335020121 EEL BATT CHARGER BOEING767 7672B7 1385107NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19651US 24764 PHL - THE CROSS AISLE FLOOR LEVEL EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. OPERATIONS CHECKED GOOD. (Z) 2L72 4F RTA1NM 19950331000341995033100034NM 1995 3 31 USAA950152 119950222A3260 UPLOCK SENSOR BOEING727 727214 138407RNM RT GEAR DIRTY A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19754US 21958 CLT - FLT 0791 - JUST AFTER TAKEOFF CREW RECEIVED A RIGHT GEAR UNSAFE LIGHT FOR THE SECOND TIME REQUIRING FLIGHT TO RETURN TO CLT. MAINTENANCE CLEANED THE RIGHT GEAR UPLOCK SENSOR. OPERATIONS CHECKED GOOD. (Z) 2L73 4F A3WE 19950331000351995033100035NM 1995 3 31 USAA950195 119950301A3260 GEAR LIGHTS BOEING757 7572B7 1384964NM COCKPIT MALFUNCTIONED A USAAL ABORTED APPROACH N FALSE WARNING DEDESCENT 1 EA19611AU 27123 PHL - FLT 0676 - THE CAPTAIN LOWERED THE LANDING GEAR AND RECEIVED ONE GREEN LIGHT ON THE LEFT MAIN GEAR ONLY. AFTER RECYCLING THE GEAR, THE LIGHT STILL REMAINED. THE CAPTAIN DID A FLYBY AND THE TOWER STATED THAT THE GEAR APPEARED TO BE DOWN. THE CAPTIAN RESET THE LIGHT SOCKETS ON THE INDICATORS AND ALL THREE GREEN LIGHTS APPEARED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE SECURITY OF THE INDICATOR SOCKETS AND PERFORMED A BITE CHECK OF THE PROXIMITY BOX. ALL CHECKED NORMAL. (Z) 2L72 4F RTA2NM 19950331000361995033100036EU 1995 3 31 USAA950201 119950301A21303925308 PRSOV FOKKERF28 F28MK0100 4990807EU RIGHT MALFUNCTIONED A USAAO OTHER O OTHER CRCRUISE 1 EA19856US 11286 PHL - FLT 0244 - CABIN PRESSURE CONTINUED TO CLIMB AT FL 330. CREW DECLARED AN EMERGENCY TO GET LOWER PRESSURE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TO RIGHT PRSOV AND THE RIGHT PACK FLOW VALVE. OPERATIONS CHECKED GOOD. REFERENCE 95ZZZZ155. 2L72 4F RT 19950331000371995033100037EU 1995 3 31 USAA950202 119950228A3010 CONNECTOR FOKKERF28 F28MK0100 4990807EU WING ANTI-ICE NOT SEATED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19861US 11297 PIT - FLT 1842 - UPON TURNING WING ANTI-ICE ON, CREW RECEIVED A WING ANTI-ICE FAULT. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. MAINTENANCE SEATED PIN HH IN CONNECTOR AND CHECKED LOCKING. ALL CHECKED GOOD. (Z) 2L72 4F RT 19950331000381995033100038NM 1995 3 31 USAA950209 119950129A335020121 EEL BATT CHARGER BOEING767 7672B7 1385107NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19651US 24764 PHL - THE CROSS AISLE FLOOR LEVEL EMERGENCY LIGHTS FAILED TO TEST. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER. OPERATIONS CHECKED GOOD. (Z) 2L72 4F RTA1NM 19950331000391995033100039EU 1995 3 31 USAA950210 119950304A3350 EEL WIRING FOKKERF28 F28MK0100 4990807EU CABIN LOOSE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19850US 11276 PIT - THE EMERGENCY CENTER CABIN OVERWING STANDBY LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A LOOSE CONNECTION ON WIRING TO THE LIGHT. OPERATIONS CHECKED GOOD. (Z) 2L72 4F RT 19950331000401995033100040EU 1995 3 31 USAA950211 119950226A323171543 VALVE FOKKERF28 F28MK0100 4990807EU RT MLG DOOR INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19856US 11286 TPA - FLT 8003 - THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW TRIED TO RECYCLE GEAR. GEAR REMAINED EXTENDED AND CREW RETURNED TO TPA. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR VALVE. (Z) 2L72 4F RT 19950331000411995033100041NM 1995 3 31 USAA950212 119950305A33501000679 EEL ASSEMBLY BOEING737 737201 1384454NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19225US 21667 GSO - EMERGENCY LIGHT OVER DOOR 2L INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (Z) 2L72 4F A16WE 19950331000421995033100042NM 1995 3 31 USAA950213 119950304A28206937335123 MODULE BOEING737 7373B7 1384580NM P-5 PANEL FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19384US 22957 PIT - FLT 852 - FLIGHT EN ROUTE PHL TO MCI WHEN CIRCUIT BREAKER FOR NR 1 FORWARD BOOST PUMP, NR 2 AFT BOOST PUMP, AND CENTER BOOST PUMP POPPED. RESET UNSUCCESSFUL. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CIRCUIT BREAKER C65 AND OVERHEAD FUEL SYSTEM MODULE. OPERATION OF ALL BOOST PUMPS NORMAL. (Z) 2L72 4F RTA16WE 19950331000431995033100043NM 1995 3 31 USAA950214 119950306A7933 BULB BOEING737 737301 1384611NM NR 2 ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA19353US 23556 IAH - FLT 1439 - FLIGHT EN ROUTE SAT TO PIT WHEN NR 2 ENGINE OIL TEMPERATURE EXCEEDED RED LINE. CREW SHUT DOWN ENGINE AND DIVERTED TO IAH WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE OIL TEMPERATURE BULB. (Z) 2L72 4F RTA16WE 19950331000441995033100044EU 1995 3 31 USAA950217 119950226A2810 FUEL SYS FOKKERF28 F28MK0100 4990807EU LT/RT WING VENTING A USAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 EA19850US 11276 CLT - FLT NR 0330 - ON TAKEOFF, THE LEFT AND RIGHT WINGS WERE OBSERVED TO HAVE FUEL VENTING FROM THEM. FLIGHT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED AN OPERATIONAL TEST OF THE FUEL AUTO FEED SYSTEM. OPERATIONS CHECKED GOOD. (Z) 2L72 4F RT 19950331000451995033100045EU 1995 3 31 USAA950218 119950223A2130 SWITCH FOKKERF28 F28MK0100 4990807EU RIGHT INTERMITTENT A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19856US 11286 CLT - FLT 2188 - AIRCRAFT LOST PRESSURIZATION AT FL 330 AND CABIN ALTITUDE WAS INCREASING. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE CHANGE OVER SWITCH AND CARGO DOOR SEALS AND ADJUSTED THE LEFT ENGINE CHANGE OVER SWITCH. OPERATIONS CHECKED NORMAL. REFERENCE NR 95ZZZZ154. 2L72 4F RT 19950331000461995033100046EU 1995 3 31 USAA950224 119950224A3260 UNSAFE LIGHT FOKKERF28 F28MK0100 4990807EU RT MLG ILLUMINATED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19869US 11314 BUF - FLT 0873 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN THE GEAR WAS RETRACTED. THE GEAR WAS RECYCLED TWICE WITH THE SAME RESULTS. CREW RETURNED TO BUF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND FOUND HEAVY ICE. THE GEAR WAS DE-ICED. BITE CHECK OF THE PROX BOX WAS ACCOMPLISHED. ALL CHECKED GOOD. (Z) 2L72 4F RT 19950331000471995033100047SO 1995 3 31 WTAA950097 119950224A3350 EEL EMB 120 EMB120RT SO CABIN MALFUNCTIONED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17281UE 120092 SBP - FORWARD OVERWING AND INTERIOR TRACK EMERGENCY EXIT LIGHTS REPORTED INOPERATIVE. DEFERRED EMERGENCY LIGHTING PER MEL 33-50-1. SUBSEQUENTLY MAINTENANCE INSPECTED AND OPERATIONALLY TESTED EMERGENCY LIGHTING SYSTEM. NO DEFECTS NOTED. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000481995033100048SO 1995 3 31 WTAA950098 119950225A3350D36604001 EEL BATT PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17281UE 120092 SBP - FORWARD OVERWING AND INTERIOR TRACK EMERGENCY EXIT LIGHTS REPORTED INOPERATIVE. DEFERRED EMERGENCY LIGHTING PER MEL 33-50-1. SUBSEQUENTLY MAINTENANCE REPLACED FORWARD EMERGENCY LIGHTING SYSTEM BATTERY PACK. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000491995033100049SO 1995 3 31 WTAA950108 119950302A3350D36604001 EEL BATT PACK EMB 120 EMB120RT SO CABIN DISCHARGED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17281UE 120092 FAT - FORWARD EMERGENCY FLOOR TRACK LIGHTING REPORTED INOPERATIVE. MAINTENANCE REPLACED FORWARD EMERGENCY LIGHTING SYSTEM BATTERY PACK. EMERGENCY LIGHTING SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000501995033100050SO 1995 3 31 WTAA950110 119950302A30402SC1160A CURRENT SENSOR EMB 120 EMB120RT SO LT WINDSHIELD SHORTED A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP17281UE 120092 SFO - CREW REPORTED ELECTRICAL ODOR IN COCKPIT WITH LEFT WINDSHIELD HEAT ON. MAINTENANCE REPLACED LEFT WINDSHIELD HEAT CURRENT SENSOR. WINDSHIELD HEAT OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000511995033100051SO 1995 3 31 WTAA950111 119950303A5270MS250851 SWITCH EMB 120 EMB120RT SO PASSENGER DOOR LOOSE WIRE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17276UE 120067 SEA - DOOR WARNING INDICATIONS DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY FOUND LOOSE WIRES AT PASSENGER DOOR MICROSWITCH. REPAIRED WIRING. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000521995033100052EU 1995 3 31 WTAA950112 119950305A2150 RT PACK BAG JETSTMJETSTM3101 1500215EU CABIN SMOKING A WTAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP17430UE 784 SAN - SMOKE IN CABIN REPORTED DURING TAXI OUT WITH RIGHT AIR CONDITIONING PACK ON. AIRCRAFT RETURNED TO GATE. MAINTENANCE DEFERRED RIGHT PACK PER MEL 21-1. PERFORMED AIRCRAFT GROUND RUN. NO EVIDENCE OF SMOKE IN CABIN WITH RIGHT PACK OFF. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA21EU 19950331000531995033100053SO 1995 3 31 WTAA950113 119950306A3260MS3470L833S CONNECTOR EMB 120 EMB120RT SO LT MLG WW FAILED A WTAAA UNSCHED LANDING JO WARNING INDICATION OTHER TOTAKEOFF 1 WP17454UE 120155 SFO - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR ELECTRICAL CONNECTOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK ON GROUND. LANDING GEAR OPERATION AND POSITION INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000541995033100054SO 1995 3 31 WTAA950114 119950308A27223081401003 ACTUATOR EMB 120 EMB120RT SO RUDDER MALFUNCTIONED A WTAAK NONE F FLT CONT AFFECTED CRCRUISE 1 WP17120AM 120012 FAT - NO HYDRAULIC ASSIST ON RIGHT RUDDER ABOVE 120 KNOTS. AIRCRAFT LANDED IN FAT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BLUE SYSTEM RUDDER ACTUATOR PER EMB-120 MM. OPERATIONAL CHECK AND LEAK CHECK GOOD. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331000551995033100055SO 1995 3 31 COM11822 119950315A5753PE610261 ROLLER EMB 120 EMB120RT SO RT TE FLAP BINDING A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01162CA 120150 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP DURING CLIMB. REPLACED ROLLERS ON RT OUTBD FLAP. 2L72 4T RTA31SO 19950331000561995033100056NM 1995 3 31 95ZZZW273 119950207A323169210 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13820EX 019 THE LT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF, ACFT RETURNED TO FIELD. REMOVED AND REPLACED LT AFT GEAR DOOR ACTUATOR, AND MECHANICAL SEQUENCE VALVE IAW MM OPERATIONAL CHECKED GOOD. ACFT RETURNED TO SERVICE. REF PCAA9500195. 2H72 4T RTA13NM 19950331000571995033100057CE 1995 3 31 95ZZZW274 119950306A3230HMX5F6 ROD END BEECH 36 36BEECH 1151602CE NLG BROKEN A AJZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP197488N E38 SHORTLY AFTER TAKEOFF, PILOT WAS ADVISED THAT THE NOSE GEAR DID NOT FULLY RETRACT, WHILE THE MAINS DID. ATTEMPTS TO 'SHAKE' THE GEAR DOWN AND LOCKED FAILED. ACFT LANDED WITH NOSE GEAR COLLAPSED. ACFT SUFFERED DAMAGE TO GEAR DOORS, NOSE COWL AND PROP. 1L71 3O 3A15 19950331000581995033100058EU 1995 3 31 95ZZZW276 119950306A3020NH24668081 INTAKE DUCT SAAB SF340 340B 7860101EU RT ENG INLET FAILED A NVEAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE DEDESCENT 1 SO03194AE 340B194 THE RT INTAKE HT CYCLING TO OVERTEMP CONDITION. INTAKE MAT CAUGHT ON FIRE, CREW SHOT FIRE BOTTLE THEN SHUTDOWN THE ENGINE. FIRE WENT OUT SHORTLY AFTER ENGINE WAS SHUTDOWN. CFR MET ACFT AND TAXIED TO TERMINAL. LANDED WITHOUT FURTHER INCIDENT. REPLACED LOWER DUCT ASSY OPS CHECK GOOD. ALSO, REPLACED ENGINE FIRE BOTTLE. 2L72 4T RTA52EU 19950331000591995033100059NM 1995 3 31 AWXA9500121 119950228A2410 CSD BOEING737 737277 1384570NM NR 2 ENGINE OVERSERVICED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28187AW 22654 COS-PHX - FLT 550 - ACFT DIVERTED TO ABQ DUE TO NR 2 CSD OIL TEMP REACHING 150 DEGREES. CREW DECLARED AN EMERGENCY AND DIVERTED TO ABQ. APU ON MEL 49 01 INOP FOR BLEED LEAK. CREW WAS CONCERNED ABOUT A SINGLE SOURCE OF ELECTRICAL POWER. ACFT LANDED WITHOUT FURTHER INCIDENT. MX FOUND NR 2 ENGINE CSD OVER SERVICED WITH OIL, AND DRAINED CSD OIL TO PROPER LEVEL. MX RAN ENGINE WITHOUT ABNORMAL INDICATIONS. ACFT RELEASED FOR SERVICE. (W) 2L72 4F RTA16WE 19950331000601995033100060NM 1995 3 31 AWXA9500122 119950303A5315 FLOORBEAM BOEING737 737277 1384570NM BS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28182AW38430 22649 PHX - FLT 3797 - DURING C13 INSPECTION, FOUND CORROSION BEYOND CLEAN UP LIMITS, TOP AND BOTTOM OF CHORD AT FLOOR BEAM BS 967 RBL 23 TO RBL 43. REPAIR ANGLE FABRICATED AND INSTALLED PER SRM 51 40 4 AND SRM 51 30 2. TOTAL CYCLES 33914. (W) 2L72 4F RTA16WE 19950331000611995033100061NM 1995 3 31 AWXA9500123 119950303A5320 BRACKET BOEING737 7373G7 1384595NM BS 787 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW15224 24711 PHX - FLT 1267 - DURING C6 INSPECTION, FOUND AFT CARGO BAY FRAME ATTACH BRACKET CRACKED AT FLOOR SUPPORT ON RT SIDE, STA 787. REMOVED, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-02 AND SRM 51-40-02. TOTAL CYCLES 12211. (W) 2L72 4F RTA16WE 19950331000621995033100062NM 1995 3 31 AWXA9500124 119950303A5320 BRACKET BOEING737 7373G7 1384595NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28309AW15224 24711 PHX - FLT 1267 - DURING C6 INSPECTION, FOUND A 1 INCH CRACK IN RAM AIR INLET SUPPORT STRUCTURE 'L' ANGLE JUST BELOW DRAG ANGLE IN RADIUS. REPAIRED PER ER 1 53 20 02 AND ER 1 53 20 02B. TOTAL CYCLES 12211. (W) 2L72 4F RTA16WE 19950331000631995033100063EU 1995 3 31 AWXA9500126 119950302A2720 RUDDER PEDALS AIRBUS320 A320231 3930325EU RT COCKPIT STIFF A AWXAO OTHER O OTHER DEDESCENT 1 WP28624AW 55 ORD - FLT 701 - AFTER A/P DISCONNECT AT 1000 FEET ON DESCENT, THE FO'S RUDDER PEDAL INPUT REQUIRED EXCESSIVE FORCE. NO RUDDER PEDAL INPUT DEFECTS FROM CAPT'S SIDE. ACFT LANDED WITHOUT INCIDENT. MX COMPLIED WITH ER 32 27 21 02, INSTALLATION OF NEW LEVER IN THE RUDDER ARTIFICIAL FEEL AND TRIM UNIT. OPS CHECK OK. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA28NM 19950331000641995033100064NM 1995 3 31 AWXA9500127 119950303A5730 DOOR BOEING737 7373S3 1384711NM RT WING LOOSE A AWXAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP28316AW26854 23713 LAS-MDW - FLT 692 - ACFT DIVERTED INTO DENVER DUE TO SUSPECTED FUEL LEAK ON THE RT WING IN AREA OF NR 2 PYLON. CONTRACT MX INSPECTED AND RETORQUED FUEL TANK ACCESS DOOR ASSEMBLY AT WBR 227. NO FURTHER LEAKS REPORTED AT THIS TIME. ACFT RETURNED TO SERVICE. TOTAL CYCLES 16547. (W) 2L72 4F RTA16WE 19950331000651995033100065EU 1995 3 31 AWXA9500128 119950305A5610STA320241 WINDSHIELD AIRBUS320 A320231 3930325EU RT COCKPIT CRACKED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28633AW 566 082 ORD- LAS - FLT 777 - DURING CRUISE, CREW NOTICED A BURNING SMELL FROM THE FO'S WINDOW. A SHORT TIME LATER THE WINDOW OUTER PANE SHATTERED. ACFT DIVERTED TO DSM AND LANDED WITHOUT INCIDENT. CONTRACT MX INSPECTED WINDOW AND VERIFIED ONLY OUTER PANE CRACKED. ACFT MAINTENANCE FERRIED TO PHX. MX REPLACED FO'S WINDSHIELD. (W) 2L72 4F RTA28NM 19950331000661995033100066NM 1995 3 31 AWXA9500134 119950306A272065C370523 PCU BOEING737 7372A6 138448BNM RUDDER SHUDDERS A AWXAO OTHER J WARNING INDICATION ININSP/MAINT 1 WP28145AW 316SS 20194 LAS - FLT 3 - DURING RUDDER PCU TEST, FEEL DIFF LIGHT AND MASTER CAUTION FLIGHT CONTROL LIGHT ILLUMINATED. PERFORMED TEST ON RUDDER PCU PER AWA TASK CARD A8M27001. NO FAULTS NOTED PER BMM 27 21 0 PG 501. MX REMOVED AND REPLACED RUDDER PCU IAW AWA TASK CARD R6B27003 AND TESTED PER AWA TASK CARD F6B27001. ACFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950331000671995033100067EU 1995 3 31 AWXA9500135 119950309A2910NAS161210 O-RING AIRBUS320 A320231 3930325EU GREEN BRAKE MOD FAILED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP28625AW 064 PHL-CMH - FLT 265 - EMERGENCY LANDING DECLARED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM AFTER THIRTY MINUTES INTO FLIGHT. AFTER GEAR EXTENSION BY MANUAL SYSTEM, PRESSURE CAME BACK TO 3100 PSI, BUT QUANTITY JUST ABOVE AMBER. CREW HAD NO NOSE GEAR STEERING AFTER LANDING. NO OTHER PROBLEMS WERE NOTED. ACFT TOWED TO GATE. MX REPLACED O RING ON GREEN BRAKE MODULE IN CENTER WHEEL WELL. OPS NORMAL, NO LEAKS NOTED. PERFORMED AMM 32-00-00 TO RETURN LANDING GEAR SYSTEM BACK TO NORMAL AFTER FREE FALL. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA28NM 19950331000681995033100068NM 1995 3 31 AWXA9500136 119950308A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 7 THROUGH 10. RECONNECTED LOOSE WIRES AT ROW 10, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950331000691995033100069WP 1995 3 31 BDHA9500001 219950220A7240310166812 PLENUM SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110U 01514WP RT ENGINE CRACKED A BDHAK NONE O OTHER ININSP/MAINT 1 GL15328BA TC253 RAP - FLT 435 - DURING A ROUTINE RT ENGINE INSPECTION, MAINTENANCE FOUND A CRACK AROUND THE P3 AIR SUPPORT BOSS ON THE ENGINE PLENUM. ENGINE REMOVED AND PLENUM REPLACED, COMPLETED ENGINE RUNS AND ACFT RELEASED FOR SERVICE. (W) 1L72 4T4 T A8SW E4WE 19950331000701995033100070SW 1995 3 31 BDHA9500002 119950210A8012MS2456801 RELAY SWRNGNSA226 SA226TC 8780404SW LT ENGINE FAILED A BDHAO OTHER L NO TEST ININSP/MAINT 1 GL15229AM TC305 RAP - FLT 476 - THE LT ENGINE WOULD NOT START, NO FUEL FLOW OR IGNITION. INSPECTED AND FOUND NR 2 START CONTROL RELAY OPEN. REMOVED AND REPLACED NR 2 START CONTROL RELAY, AND ENGINE START COMPLETED SUCCESSFULLY. ACFT RELEASED FOR FLIGHT. (W) 1L72 4T A8SW 19950331000711995033100071 1995 3 31 BDHA9500004 419950206A3420727421 CIRCUIT BREAKER SWRNGNSA226 SA226TC 8780404SW LT BUSS MALFUNCTIONED A BDHAO OTHER I FLT. ATTITUDE INST. TOTAKEOFF 1 GL15327BA TC249 MSP - FLT 447 - CREW REPORTED THE LT ARTIFICAL HORIZON WOULD NOT PULL THE FLAG ON PREFLIGHT CHECK. THE CIRCUIT BREAKER WAS CYCLED AND ALL INDICATIONS WERE NORMAL. THE CIRCUIT BREAKER WAS REPLACED AND ACFT WAS RELEASED. (W) 1L72 4T A8SW 19950331000721995033100072WP 1995 3 31 BUFA 9506 119950228A7110 COWLING DOUG DC8 DC861 3021952WP NR 3 ENGINE MISSING A BUFAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 CE05161DB 45980 IAH-BNA - FLT 127 - THE NR 3 ENGINE, AFT COWLING MISSING ON POST FLIGHT WALK AROUND. ACFT INSPECTED WITH REFERENCE TO ACMM PROCEDURES AND DETERMINED IN SAFE AND AIRWORTHY CONDITION FOR MAINTNENANCE FERRY FLIGHT TO MQY. REPAIRED PYLON APRON PER DC-8 SRM 54-2-0 AND REPLACED AFT LT AND RT COWLING PER MM 71-10-3. (W) 2L74 4F 4A25 19950331000731995033100073WP 1995 3 31 BUFA9507 119950306A29107761892658 HYD LINE DOUG DC8 DC862 3021970WP NR 2 PYLON LEAKING A BUFAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE05922BV 45925 ON CLIMB, LOST HYDRAULIC FLUID. FOUND LOOSE HYDRAULIC SLOT LEADING EDGE LINE IN NR 2 ENGINE PYLON. TIGHTENED AND LEAKED CHECKED SAME IAW DC8-MM 29-01. ACFT RETURNED TO SERVICE. (W) 2L74 4F 4A25 19950331000741995033100074NM 1995 3 31 PCAA9500193 119950202A5610NP1579019 WINDSHIELD DHAV DHC8 DHC8102 2809003NM LT COCKPIT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13814EX7172 318 SMOKE EMANATING FROM CAPT'S WINDSHIELD. REMOVED AND REPLACED CAPT'S WINDSHIELD DUE TO ARCING OF TERMINAL LEADS. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000751995033100075NM 1995 3 31 PCAA9500194 119950207A2431522487 TEMP MONT DHAV DHC8 DHC8102 2809003NM BATT COMPT FAILED A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA132FOR 10077 215 MAIN BATTERY HOT AND AUX BATTERY HOT LIGHTS ILLUMINATED, ALSO NO TEMP INDICATION. REMOVED AND REPLACED BATTERY TEMP MONITOR OP CHECKS GOOD. INSPECTED BATTERIES FOUND TO BE COOL. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000761995033100076NM 1995 3 31 PCAA9500195 119950207A323282970014009 DOOR ACT DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13820EX 019 THE LT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF, ACFT RETURNED TO FIELD. REMOVED AND REPLACED LT AFT GEAR DOOR ACTUATOR, AND MECHANICAL SEQUENCE VALVE IAW MM OPERATIONAL CHECKED GOOD. ACFT RETURNED TO SERVICE. REF 95ZZZW273. (W) 2H72 4T RTA13NM 19950331000771995033100077NM 1995 3 31 PCAA9500196 119950208A3260841005 PROX CONT BOX DHAV DHC8 DHC8102 2809003NM LT MLG DOOR FAILED A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13801MX3769 008 THE LT DOOR OPEN ADVISORY LIGHT ILLUMINATED IN FLIGHT. CREW VERIFIED DOOR IS CLOSED. REMOVED AND REPLACED LT FWD GEAR DOOR ACTUATOR AND PSEU IAW MM, OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000781995033100078NM 1995 3 31 PCAA9500197 119950209A2431522487 TEMP MONT DHAV DHC8 DHC8102 2809003NM BATTERY COMPT FAILED A PCAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 EA13815EX7394 321 MAIN AND AUX BATT HOT MASTER WARNING LIGHTS ILLUMINATED. ACFT DIVERTED INTO MDT. REMOVED AND REPLACED BATTERY TEMP MONITOR OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000791995033100079NM 1995 3 31 PCAA9500198 119950219A2530180140 HOT JUG DHAV DHC8 DHC8102 2809003NM GALLEY SHORTED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13812EX 312 A VERY STRONG ELECTRICAL SMELL IN GALLEY AREA, NO VISIBLE SMOKE OBSERVED. INSPECTED GALLEY AREA AND FOUND CONNECTOR ON NR 2 HOT JUG SHORTED. REMOVED NR 2 HOT JUG. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000801995033100080NM 1995 3 31 PCAA9500199 119950220A291082970010477 HYD LINE DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYS CRACKED A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA13825EX 388 THE NR 2 HYDRAULIC SYSTEM LOST QUANTITY. FOUND HYDRAULIC LINE CRACKED AT FLARE. REPLACED RIGID LINE WITH FLEX LINE AS PER DASH-8 MM 20-50-52. SERVICED HYDRAULICS, BLED SYSTEM, LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000811995033100081NM 1995 3 31 PCAA9500200 119950226A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13820EX15260 019 WHILE SELECTING GEAR DOWN, NR 2 MAN HYDRAULIC PRESSURE WENT TO ZERO, NO GEAR EXTENDED AT THAT POINT. LOUD GRINDING NOISE WAS HEARD AFTER GEAR SELECTED DOWN, PERFORMED ALTERNATE EXTENSION. JACKED ACFT, CHECKED ENG DRIVE HYD PUMP FOR AIR LEAKS, BLED SYSTEM, AND CYCLED GEAR SEVERAL TIMES. REMOVED AND REPLACED PSEU FOR TROUBLESHOOTING, OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950331000821995033100082NE 1995 3 31 SCNA95025 219950223A732065C129333 APR MODULE BOEING727 727259 138408JNM PWA JT8 JT8D17 52049NE AFT FUSELAGE FAILED A SCNACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL15289SC 22475 CMI - FLT 687 - ON POWER UP FOR TAKEOFF, APR FAILED TO ARM. ABORTED BELOW 60 KNOTS, RESET, RETESTED SYSTEM AND OPERATIONS CHECKED NORMAL. PERFORMED GROUND CHECK PER MM 73-22-00 PG 502 SYSTEM OPERATIONS NORMAL. (W) 2L73 4F4 F A3WE E2EA 19950331000831995033100083SO 1995 3 31 COM11836 119950324A32602054000100 SWITCH EMB 120 EMB120RT SO NLG DEFECTIVE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01161CA 120143 AFTER TAKEOFF THE LANDING GEAR CONTROL HANDLE COULD NOT BE MOVED TO RETRACT THE GEAR. REPLACED NLG PROXIMITY WOW SWITCH AND HARNESS ASSY. 2L72 4T RTA31SO 19950331000841995033100084NM 1995 3 31 DL72E950998 119950227A5754 RIBS BOEING727 727247 138408FNM RT LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 DURING HMV FOUND NR 4 SLAT ACTUATOR RIB MARKED NR 12 CRACKED 3 PLACES AND RIB MKD NR 11 CRACKED IN FWD LOWER RADIUS, REPAIRED PER M/M 57-54-0 PG 805. 2L73 4F A3WE 19950331000851995033100085NM 1995 3 31 DL72E950999 119950227A5754 RIBS BOEING727 727247 138408FNM RT LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 DURING HMV FOUND NR 4 LEADING EDGE SLAT RIB MARKED NR 21 CRACKED AT FWD CLOSURE CHORD, REPAIRED PER M/M 57-54-0 PG 806. 2L73 4F A3WE 19950331000861995033100086NM 1995 3 31 DL72E951000 119950227A5313 STRINGER BOEING727 727247 138408FNM CABIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 DURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-3 FIG 1 DETAIL II FOR FWD AND AFT. 2L73 4F A3WE 19950331000871995033100087NM 1995 3 31 DL72E951013 119950301A5347 SEAT TRACK BOEING727 727247 138408FNM BS 1110-1130 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 DURING HMV FOUND LT SEAT TRACKS WORN AT SEVERAL SEAT LOCATIONS BETWEEN 950F AND 1138, REPAIRED BY REMOVING CORROSION PER SRM 51-10-6, TREATED AND PAINTED STA 950F THROUGH 1110, SPLICED IN NEW SECTION OF TRACK FROM STA 1110 TO 1130 LT OUTBOARD SPLICED IN NEW SECTION OF TRACK FROM STA 1110 TO 1130 LT INBOARD PER SRM 53-20-11 PG 803. 2L73 4F A3WE 19950331000881995033100088NM 1995 3 31 DL72E951014 119950309A5320 LIGHT BOX BOEING727 727247 138408FNM CABIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 DURING HMV FOUND L/W L/E LIGHT BOX, STR 15L IS CRACKED ON FWD AND AFT SIDES OF LIGHT BOX, REPAIRED PER SRM 53-10-1 FIG 1. 2L73 4F A3WE 19950331000891995033100089NM 1995 3 31 DL72E951021 119950227A5754 SKIN BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 746 NR 6 LE SLAT INTERIOR SKIN CRACKED, LOCATED IN BAY IB OF ACTUATOR RIBS. REPAIRED PER MM 57-54-0 PG 804. FOUND AT HMV. 2L73 4F A3WE 19950331000901995033100090NM 1995 3 31 DL72L950985 119950225A711065196854356 NOSE COWL BOEING727 727232 1384082NM NR 1 ENGINE GOUGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 002 GOUGE IN NOSE LIP SKIN OF NR 1 ENGINE NOSE COWL, AT 1:30 POSITION. REPAIRED PER SRM 54-30-3. 2L73 4F A3WE 19950331000911995033100091NM 1995 3 31 DL72L950987 119950301A711065196854539 COWL BOEING727 727232 1384082NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 746 DURING INITIAL INSPECTION OF NR 1 ENGINE NOSE COWL. FOUND FORWARD BULKHEAD OUTER ANGLE AT THE 9 O'CLOCK POSITION WITH ELONGATED BOLT HOLES. REPAIRED PER SRM 54-10-3 FIG. 3. 2L73 4F A3WE 19950331000921995033100092NM 1995 3 31 DL72L951011 119950225A711065196854539 NOSE COWL BOEING727 727232 1384082NM ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 746 DURING SHOP INSPECTION, FOUND KNIFE EDGE DAMAGE TO TRAILING EDGE LANDING AREA TO BE WORN AT, STATION 99.25 OF NOSE COWL. REPAIRED DAMAGE PER, SRM 54-10-3 FIG NR 3. 2L73 4F A3WE 19950331000931995033100093NM 1995 3 31 DL72L951016 119950129A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 746 NR 6 SLAT, SECOND RIB FROM I/B END CRACKED AT LOWER END. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. DAMAGE FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950331000941995033100094NM 1995 3 31 DL72L951017 119950129A5754651622296 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 746 NR 6 SLAT, ITEM NR 1, INNER CLOSE OUT PANEL LOWER ATTACH ANGLE HAS ELONGATED HOLE 4.5 INCHES FROM I/B END. ITEM NR 2, REPAIR INSUFFICIENT AT LOWER ATTACH ANGLE T-DUCT CUTOUT. REPAIRED BOTH ITEMS PER SRM 57-54-0 FIG 805A. 2L73 4F A3WE 19950331000951995033100095NM 1995 3 31 DL72L951042 119950310A5754 RIB 651622296 BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA BN898 21309 746 UPPER CORNER OF BOTH ACTUATOR RIBS ON NR 6 SLAT WERE FOUND CRACKED. REPAIRS WERE COMPLETED PER THE MM 57-54-0. FOUND AT SHOP VISIT. 2L73 4F A3WE 19950331000961995033100096NM 1995 3 31 DL72S950990 119950227A5414 SKIN BOEING727 727232 1384082NM PNL 9501 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 746 FOUND ON CV2 CHECK .25 INCH CRACKS IN SKIN AT FASTNER HOLES (4 PLACES) RT SIDE ABOVE FWD VERTICAL SPAR AND FWD OF PANEL 95012) FASTNERS LOOSE FWD OF PANEL 9501 REPAIR-1) REPAIR PER MM 54-30-0 PG801/FIG801 2). 2L73 4F A3WE 19950331000971995033100097NM 1995 3 31 DL72S950991 119950227A5753 ANGLE BOEING727 727232 1384082NM NR 6 FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 746 FOUND ON CV2 CHECK .25 INCH CRACK NR 6 FLAP ACTUATOR ATTACH ANGLE LOWER OUTBOARD SIDE REPAIR. REPAIRED PER MM 57-20-21 PG 811. 2L73 4F A3WE 19950331000981995033100098NM 1995 3 31 DL72S951003 119950112A57546516221100 SLAT BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11526DA 21586 746 DURING INSPECTION OF NR 5 L/E SLAT, N/R CARD WAS WRITTEN TO COMPLY WITH EO NR 4-55122-3AD. THIS EO WAS COMPLIED WITH AND N/R CARD SIGNED OFF. 2L73 4F A3WE 19950331000991995033100099NM 1995 3 31 DL72S951005 119950130A5753652163361 MID FLAP BOEING727 727232 1384082NM NR 4 TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 746 NR 4 MID FLAP, I/B AND O/B THRUST BEARING BORES CORRODED. REPAIRED PER SRM 575004, MACHINED THRUST BORES AND INSTALLED BUSHINGS. 2L73 4F A3WE 19950331001001995033100100NM 1995 3 31 DL72S951047 119950221A5754651622162 RIB BOEING727 727232 1384082NM NR 5 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 746 AT SHOP INSPECTION FOUND RT WING NR 5 SLAT WITH CRACKED RIB AT INBOARD TRACK ATTACH FITTING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950331001011995033100101NM 1995 3 31 DL72S951048 119950221A5754651622162 RIBS BOEING727 727232 1384082NM NR 5 LE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 746 AT SHOP INSPECTION RT WING NR 5 SLAT WEB, FORWARD OF ACTUATOR RIBS WAS FOUND WITH ENLARGED HOLES AT RIB ATTACH POINT. REPAIRED PER SRM 57-50-3 FIG 4. 2L73 4F A3WE 19950331001021995033100102NM 1995 3 31 DL72S951054 119950227A5711 SPAR STIFNER BOEING727 727232 1384082NM NR 7 SLAT TRACK CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 746 FOUND ON CV 2 CHECK 1 INCH CRACK IN LEADING EDGE SPAR STIFFENER AT NR 7 SLAT O/B TRACK O/B ANGLE. REPAIRED AND REPLACED STIFFNER PER M/M 57-20-21 PG 813. 2L73 4F A3WE 19950331001031995033100103NM 1995 3 31 DL72S951055 119950307A5330 SKIN BOEING727 727232 1384082NM BS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 746 FOUND ON CV2 CHECK, SKIN DAMAGED AT STR 27L BETWEEN 720A AND 720B. REPAIRED PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950331001041995033100104NM 1995 3 31 DL72W950988 119950302A5755 DOUBLER 651734874 BOEING727 727247 138408FNM TE SPOILER WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 5068J 20869 746 SMALL HOLE WORN IN 3 IN DOUBLER ON BOTTOM T/E OF SPOILER, MADE BONDED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950331001051995033100105NM 1995 3 31 DL72W950995 119950302A5755 SKIN 651734874 BOEING727 727247 138408FNM NR 8 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 5062J 20869 746 DURING INSPECTION, NR 8 SPOILER PANEL WAS FOUND DENTED AND DELAMINATED ON LOWER SKIN. MADE BONDED REPAIR PER SRM 57-40-6 WITH REF TO 51-40-6. 2L73 4F A3WE 19950331001061995033100106NM 1995 3 31 DL72W951002 119950308A5754651622291 RIBS BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 A NR 4 SLAT WAS SENT TO SHOP WITH NR 1174 FOR 2 CRACKS ON NR 2 AND NR 4 RIBS FROM I/B END. BOTH RIBS WERE REPAIRED PER SRM 57-54-0 FIG 814. 2L73 4F A3WE 19950331001071995033100107NM 1995 3 31 DL72W951018 119950310A5754 RIB 651622291 BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W BN1047 20869 746 AT HMV, FOUND LEFT WING NR 4 SLAT WITH RIB NR 7 CRACKED. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950331001081995033100108NM 1995 3 31 DL72W951019 119950304A5755 SPOILER BOEING727 727247 138408FNM LEFT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 DURING HMV FOUND NR 7 SPOILER HAS A HOLE IN IT AND IB BOTTOM END IS WORN DOWN. MADE BONDED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950331001091995033100109NM 1995 3 31 DL72W951020 119950308A5741 FITTING BOEING727 727247 138408FNM LT BOTTLE PIN CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 DURING HMV, FOUND LEFT REAR BOTTLE PIN FITTING INDICATING CRACK AT 10 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7. 2L73 4F A3WE 19950331001101995033100110NM 1995 3 31 DL72W951022 119950304A5210 ANGLE BOEING727 727247 138408FNM AFT ENTRY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 DURING HMV FOUND AFT ENTRY DOOR BOTTOM ANGLE CRACKED. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950331001111995033100111NM 1995 3 31 DL72W951023 119950303A5751 SKIN BOEING727 727247 138408FNM RT OUTBD AILERONDAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 DURING HMV, FOUND OUTBD AILERON OUTBD TAB ROD END LOOSE. REPLACED TAB ROD END AND REPLACED SECTION OF UPPER SKIN PER SRM 57-50-5 FIG 3. 2L73 4F A3WE 19950331001121995033100112NM 1995 3 31 DL72W951057 119950304A5311 FRAME BOEING727 727247 138408FNM BS 910 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 746 DURING HMV, FOUND FORMER AT STA 910 LT SIDE CRACKED. REPAIRED PER SRM 53-10-4, FIG 22 PG 87-89 2L73 4F A3WE 19950331001131995033100113NM 1995 3 31 DL76S951280 119950317A32462606735 WHEEL BOEING767 767332 1382001NM NOSE GEAR FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO11121DE 23435 ON TAXI OUT FELT AND HEARD LOUD BANG AT NOSE AREA. RETURNED TO GATE, FOUND RT NOSE WHEEL RIM BROKEN AND LEFT WHEEL DAMAGED FROM THE EXPLOSION. INITIAL INSPECTION, INDICATES FAILURE OF WHEEL AT BEAD AREA. 2L72 4F RTA1NM 19950331001141995033100114 1995 3 31 DLL12951278 419950324A2330RDAX5341 DECODER LKHEED1011 1011385115 5265015WP CABIN FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11724DA 193C1151 ON CLIMB-OUT, HAD STRONG ELECTRICAL BURNING SMELL IN MID GALLEY AREA. RETURNED ATL. FOUND DECODER UNIT AT SEAT ROW 20AB BURNED. REPLACED SAME OPERATION NORMAL. 2L73 4F A23WE 19950331001151995033100115WP 1995 3 31 DLL16951029 119950214A5312 BLKHD FRAME LKHEED1011 10113853 5265020WP PRESS DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 746 AT HMV, FOUND P-DOME FRAME CORRODED AT LOWER END OVER A 2FT SECTION. AT THE FORWARD SIDE OF P-DOME LEFT SIDE JUST AFT OF AFT CARGO AREA STRINGER 41. REPAIRED PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950331001161995033100116WP 1995 3 31 DLL16951030 119950214A5312 BLKHD FRAME LKHEED1011 10113853 5265020WP PRESS DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 746 AT HMV, FOUND FRAME CORRODED ON P-DOME LOWER INBOARD SIDE JUST AFT OF WHERE STRINGER 25 ENDS. REPAIRED PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950331001171995033100117WP 1995 3 31 DLL16951031 119950228A5330 SKIN LKHEED1011 10113853 5265020WP BS 1605-1625 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 746 AT HMV, FOUND FUSELAGE SKIN CORRODED UNDER TEARSTRAP BETWEEN STA 1605 AND 1625 AT STRINGER 29. REPAIRED PER SRM 53-31-00 PG 965. 2L73 4F A23WE 19950331001181995033100118WP 1995 3 31 DLL16951032 119950214A5320 DECK LKHEED1011 10113853 5265020WP BS 359 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 746 AT HMV, FOUND CORROSION DAMAGE ON PRESSURE DECK AT FS 359 LEFT OF FORWARD LAV 18 INCHES. REPAIRED PER SRM 53-11-00 FIG 840. 2L73 4F A23WE 19950331001191995033100119WP 1995 3 31 DLL16951034 119950303A5330 STRAP LKHEED1011 10113853 5265020WP BS 910 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 746 AT HMV, FOUND CENTER STRAP TO BE CORRODED. INTERNAL CENTER STRAP AT STA 910 STR 33. REPAIRED PER SRM 53-31-00 FIG 825. 2L73 4F A23WE 19950331001201995033100120NM 1995 3 31 DLM88951001 119950307A5313 STRINGER DOUG MD88 MD88 3023688NM BS 1418 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 DURING HMV, FOUND R-1 STRINGER CRACKED AT ST 1418. REPAIRED PER SRM 53-02 P1, 2 AND 3. 2L72 4F RTA6WE 19950331001211995033100121NM 1995 3 31 DLM88951010 119950306A552249801 SKIN DOUG MD88 MD88 3023688NM RT ELEV LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 AT HMV, FOUND RIGHT ELEVATOR OUTBOARD LOWER SKIN WITH BURN MARKS. LIGHTNING DAMAGE, AT 8 INCHES FROM TIP 4 INCHES FROM T/E. REPAIRED PER SRM 55-03. 2L72 4F RTA6WE 19950331001221995033100122NM 1995 3 31 DLM88951024 119950307A5347 SEAT TRACK DOUG MD88 MD88 3023688NM CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 DURING HMV, FOUND SEAT TRACK CORRODED 2ND FROM LEFT SIDE FROM THE FORWARD SIDE OF THE L2 DOOR TO THE AFT SIDE OF THE L2 DOOR. REPAIRED PER SRM 53-05 FIG 4F. 2L72 4F RTA6WE 19950331001231995033100123NM 1995 3 31 DLM88951025 119950306A5330 SKIN DOUG MD88 MD88 3023688NM FS 484-503 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 DENT IN FUSELAGE NEEDS TO BE CHECKED MARKED TPA 10-18-94 NR 106 AT FS 484-503, RT SIDE OF FUSELAGE. SUPPLEMENT. DENT FOUND WITHIN SRM LIMITS, DYE CHECK, NO CRACKS FOUND. 2L72 4F RTA6WE 19950331001241995033100124NM 1995 3 31 DLM88951027 119950306A5330 SKIN DOUG MD88 MD88 3023688NM NLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 DURING HMV NR CARD 47, SKIN CRACKED ABOVE RT NLG AFT STRUT DOOR AFT ATTACH ARM. REPAIRED PER SRM 53-05 FIG 62. 2L72 4F RTA6WE 19950331001251995033100125NM 1995 3 31 DLM88951028 119950306A5320 LOUVERS DOUG MD88 MD88 3023688NM BS1497 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 DURING HMV NR CARD 62 AIR LOUVERS CRACKED AT FWD END OF 2ND AND 3RD LOUVERS O/B FROM I/B END ON SUPPORT VERTICAL LEGS RT SIDE FS CANT 1497. REPAIRED PER SRM 53-05 FIG 16. 2L72 4F RTA6WE 19950331001261995033100126NM 1995 3 31 DLM88951043 119950313A5230 DOOR DOUG MD88 MD88 3023688NM MID CARGO COMPT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 AT HMV, MID CARGO DOOR EDGE WORN AT FWD AND AFT EDGES AT HOOK LOCK AREA. STRAIGHTENED EDGE AND DYE CHECKED FOR CRACKS AT FWD EDGE NO CRACKS FOUND MFG AND INSTALLED DOUBLER AT AFT EDGE PER SRM 52-05 PAGE 110A FIG 26A. 2L72 4F RTA6WE 19950331001271995033100127NM 1995 3 31 DLM88951044 119950311A5320 DOOR JAMB DOUG MD88 MD88 3023688NM FWD BAG BIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 AT HMV, FWD B/B LWR DOOR JAMB CORRODED SEVERAL PLACE. REMOVED DAMAGED AREA, GROUND AREA AT ENDS OF REPAIR FOUND TO BE WITHIN LIMITS PER SRM 53-01, INSTALLED NEW SECTION OF DOOR JAMB AND DOUBLERS PER SRM 53-05 FIG 44 (REF NR'S 482, 583, 485). 2L72 4F RTA6WE 19950331001281995033100128NM 1995 3 31 DLM88951045 119950311A5347 SEAT TRACK DOUG MD88 MD88 3023688NM FS 1127-1202 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 746 AT HMV, 3RD TRACK FROM LT SIDE IN LINE WITH FWD EDGE OF L-2 DOOR IS CORRODED. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. 2L72 4F RTA6WE 19950331001291995033100129NM 1995 3 31 DLM88951277 119950322A29107952176535 HYD LINE DOUG MD88 MD88 3023688NM TAIL COMP FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11968DL 53161 DURING CRUISE, LOST ALL RIGHT HYDRAULIC QTY AND PRESSURE, LANDED ATL. REPLACED HYD LINE ON PRESSURE SIDE OF ENGINE FILTER MODULE. 2L72 4F RTA6WE 19950331001301995033100130NM 1995 3 31 DLM88951279 119950325A323139567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11910DL 49541 AFTER TAKEOFF HAD LOUD NOISE COMING FROM NOSE GEAR AREA, AFTER GEAR RETRACTION. RETURNED OAK. FOUND RT NLG DOOR OPEN. REPLACED DOOR ACTUATOR LINK, CYCLED GEAR RETRUNED TO SERVICE. 2L72 4F RTA6WE 19950331001311995033100131WP 1995 3 31 MWEA95151 119950325A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP FWD ENT DOOR FELL OFF A MWEAK NONE O OTHER UKUNKNOWN 1 GL31302ME 47102 PILOT REPORTS EVACUATION SLIDE COVER ON FWD ENTRANCE DOOR FELL OFF AT MKE GATE. 2L72 4F A6WE 19950331001321995033100132NM 1995 3 31 UPS202697 119950324A5230 FRAME BOEING727 72751C 1384015NM MAIN CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON FRAME, MAINCARGO DOOR LWR BEAM AT STA 560. INSTALLED REPAIR PER UPS EO B727-5210-6802B. 2L73 4F A3WE 19950331001331995033100133NM 1995 3 31 UPS202698 119950324A5313 STRINGER BOEING727 72751C 1384015NM BS 847-861 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON UPPER AND LOWER SURFACE S18A, RBL 70, BS 847-861. INSTALLED REPAIR PER UPS EO B727-5310-6801A. 2L73 4F A3WE 19950331001341995033100134NM 1995 3 31 UPS202699 119950324A5320 FLANGE BOEING727 72751C 1384015NM BS 870 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS ON FLANGE RUNNING ALONG THE ROW OF THREE FASTENERS BS 870, LT SIDE, WL 201, LBL60. INSTALLED REPAIR PER UPS EO B727-5310-6813A. 2L73 4F A3WE 19950331001351995033100135NM 1995 3 31 UPS202700 119950324A5343 SUPPORT BEAM BOEING727 72751C 1384015NM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NLG DRAG BRACE SUPPORT BEAM. INSTALLED REPAIR PER UPS EO B727-5310-6825A. 2L73 4F A3WE 19950331001361995033100136WP 1995 3 31 UPS802701 119950327A5320 DOUBLER DOUG DC8 DC871F 302199DWP AFT HEAT EX DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON DOUBLER LT AFT HEAT EXCHANGER DOOR CUT OUT. INSTALLED REPAIR PER UPS EO DC8-5330-4732D. 2L74 4F RT4A25 19950331001371995033100137WP 1995 3 31 UPS802702 119950324A5330 SKIN DOUG DC8 DC871F 302199DWP SERV DOOR CUTOUTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN B-CHECK, MAINTENANCE FOUND CRACKS ON LT AFT SERVICE DOOR, AFT UPPER CORNER OF FUSELAGE CUT OUT EXTENDING FROM TWO RIVETS. INSTALLED REPAIR PER UPS EO DC8-5330-4067A. 2L74 4F RT4A25 19950331001381995033100138NM 1995 3 31 UPS802703 119950327A5321 FLOOR BOEING727 72722C 138400FNM BS 294.5-312 DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON WALKWAY PANEL AT STA 294.5-312, RBL 25, WL 169. REPLACED PER SRM 51-40-2, 53-10-2, 51-10-2, MM 51-20-151, AND 51-30-2. 2L73 4F A3WE 19950331001391995033100139NM 1995 3 31 UPS802704 119950327A5752 SKIN BOEING727 72722C 138400FNM RT AILERON TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT I/B AILERON TAB, T/E LWR SURFACE. INSTALLED REPAIR PER SRM 51-40-6, 51-80-3. 2L73 4F A3WE 19950331001401995033100140NM 1995 3 31 UPS802705 119950327A5753 SKIN BOEING727 72722C 138400FNM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, AFT FLAP TRAILING EDGE. NORDERED NEW FLAP ASSY. 2L73 4F A3WE 19950331001411995033100141NM 1995 3 31 UPS802706 119950327A5753 WEDGE BOEING727 72722C 138400FNM LT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B, MID FLAP TRAILING EDGE WEDGE, I/B END, UPPER SURFACE. INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950331001421995033100142NM 1995 3 31 UPS802707 119950327A5752 SKIN BOEING727 72722C 138400FNM LT AILERON TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON LT I/B AILERON TAB, TRAILING EDGE. INSTALLED REPAIR PER SRM 51-80-3 AND 51-40-6. 2L73 4F A3WE 19950331001441995033100144NE 1995 3 31 95ZZZW134 219950111A8500 ENGINE BEECH 18 E18S 1151006CE PWA R985 R985* 52008NE LT ENG MALFUNCTIONED A GGPAEA ENGINE SHUTDOWN UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 NM0142D 8213 8213 BA117 9817 BFI-MSO - ABOUT 40 MINUTES INTO FLIGHT, THE LT ENGINE STARTED TO RUN ROUGH, A LOSS OF POWER WAS NOTICED AND PILOT SHUTDOWN AND FEATHERED THE LT ENGINE AND LANDED AT ELM. 1L72 3R3 R A765 5E1 19950331001451995033100145NM 1995 3 31 MRKA952 119950105A79203352610030 LUBE UNIT BOEING737 7374Y0 1384705NM NR 2 ENGINE FAILED A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL032FOR 24911 FLIGHT RETURNED TO GATE, DUE TO NR 2 ENGINE OIL PRESSURE AND TEMPERATURE NOT WITH IN LIMITS. REMOVED AND REPLACED NR 2 ENGINE LUBRICATION UNIT IAW MM 79-21-01. OPS CHECKED OK. (W) 2L72 4F RTA16WE 19950331001461995033100146NM 1995 3 31 MRKA955 119950108A2613 OVERHEAT LIGHT BOEING737 7374Y0 1384705NM RT WING ILLUMINATED A MRKAO OTHER N FALSE WARNING CRCRUISE 1 AL032FOR 24345 THE RT WING BODY OVERHEAT LIGHT INTERMITTENT IN FLIGHT. OPERATED RT PACK WITH NO FAULTS NOTED. SYSTEM CHECKED NORMAL. OK FOR CONTINUED SERVICE. (W) 2L72 4F RTA16WE 19950331001471995033100147NM 1995 3 31 MRKA957 119950110A2613 CONNECTOR BOEING737 7374Y0 1384705NM RT WING LOOSE A MRKAO OTHER N FALSE WARNING CRCRUISE 1 AL032FOR 24345 THE RT WING BODY OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. FOUND LOOSE CANNON PLUG ON THERMAL ANTI-ICE SENSOR, AND RT WING LOOP RUBBING ON FLUID LINE UNDER WING LEADING EDGE. SECURED CANNON PLUG AND REPOSITIONED OVERHEAT WARNING DETECTOR. RAN ENGINE AND WING ANTI-ICE SYSTEM. OPS CHECKED NORMAL. (W) 2L72 4F RTA16WE 19950331001481995033100148NM 1995 3 31 MRKA958 119950111A2613 DETECTOR BOEING737 7374Y0 1384705NM RT WING LOOSE A MRKAO OTHER N FALSE WARNING CRCRUISE 1 AL032FOR 24345 THE RT WING BODY OVERHEAT LIGHT FLICKERED SEVERAL TIMES, THEN STAYED ON STEADY IN FLIGHT. CHECKED RESISTANCE AT D742, AND REPOSITIONED OVERHEAT DETECTOR DUE TO PULLED FROM SUPPORT. OPERATIONAL CHECKED OK FOR CONTINUED SERVICE. (W) 2L72 4F RTA16WE 19950331002261995033100226WP 1995 3 31 CAL950085 119950203A3350 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0935888 49117 FLT NR 0751 - EWR - THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (Z) 2L72 4F A6WE 19950331002271995033100227WP 1995 3 31 CAL950089 119950205A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09477AC 48062 FLT NR 0151 - SFO - SEVERAL EMERGENCY AISLE PATH LIGHTS WERE FOUND INOPERATIVE IN THE FIRST CLASS CABIN. MAINTENANCE FOUND BROKEN WIRING UNDER FORWARD CABIN FLOOR TRACK. THE WIRING WAS REPAIRED AND OPERATION OF AISLE PATH LIGHTING WAS RESTORED. (Z) 2L72 4F A6WE 19950331002281995033100228WP 1995 3 31 CAL950114 119950210A2450 CIRCUIT BREAKER DOUG DC9 DC982 3022082WP LT GEN PANEL FAILED A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0933805 49249 FLT NR 0246 - IAH - SEVERAL LEFT AC BUS CIRCUIT BREAKERS BEGAN POPPING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE B1-743 TO AMP 'C' PHASE CIRCUIT BREAKER ON LEFT GENERATOR PANEL AT FAULT. THE B1-743 CIRCUIT BREAKER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (Z) 2L72 4F A6WE 19950331002291995033100229WP 1995 3 31 CAL950119 119950212A29107912641658 HYD LINE DOUG DC9 DC932 3022066WP RT TR UNIT LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0912514 48113 FLT NR 1688 - JAX - THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO JAX. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED IN JAX WITHOUT INCIDENT. MAINTENANCE FOUND THE ELECTRIC PUMP HYDRAULIC PRESSURE LINE TO FILTER LINE LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACED THE FLEX LINE WITHIN 500 CYCLES OR 1200 FLIGHT HOURS, WHICHEVER COMES FIRST. IN ADDITION, A PIN HOLE LEAK WAS FOUND IN THE RT THRUST REVERSER BYPASS VALVE PRESSURE LINE. THE LINE WAS CAPPED INOPERATIVE. (Z) 2L72 4F A6WE 19950331002301995033100230WP 1995 3 31 CAL950124 119950128A5350 CABLES DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0916895 49394 HOU - THE EXTERIOR TAILCONE RELEASE HANDLE REQUIRED LESS THAN 25 POUNDS PULL TO RELEASE THE TAILCONE. THE TAILCONE RELEASE CABLES WERE RIGGED IAW MM 53-53-00, SO THAT HANDLE PULL WAS WITHIN SPECIFICATION. (Z) 2L72 4F A6WE 19950331002311995033100231NE 1995 3 31 CAL950126 219950214A7250 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE FATIGUED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW09728252984610433 49485 709742 FLT NR 0690 - IAH - THE NR 2 ENGINE LOST POWER AT FL260 ON CLIMB-OUT FROM IAH. THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. S/D - INVESTIGATION REVEALED THAT A THIRD STAGE TURBINE BLADE HAD FAILED IN HIGH CYCLE FATIGUE. (W) 2L72 4F4 F A6WE E9NE 19950331002321995033100232WP 1995 3 31 CAL950127 119950215A3000 SENSOR DOUG DC9 DC982 3022082WP LT WW SHORTED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0993875 49125 FLT NR 0683 - IAH - WHEN WING ANTI-ICE SYSTEM WAS TURNED ON THE PRESSURE ABNORMAL LIGHT ILLUMINATED STEADILY AND THE PROTECTION TEMP LOW LIGHTS REMAINED ON. THE AIR CONDITIONING AIR BEGAN TO SMELL HOT AND SMOKE ENTERED THE CABIN. THE AIRCRAFT LANDED SAFELY AT IAH. MAINTENANCE FOUND THE 180 DEGREE DUCT BLOWN SENSOR SHORTED IN THE LEFT WHEEL WELL. THE SENSOR WAS REPLACED AND OPERATION CHECKED GOOD WITH NO SMOKE DETECTED. (Z) 2L72 4F A6WE 19950331002331995033100233WP 1995 3 31 CAL950128 119950215A2910NAS16128 O-RING DOUG DC9 DC981 3022081WP LT MLG BRAKE RUPTURED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0916884 48074 FLT NR 0318 - EWR - THE LEFT HYDRAULIC SYSTEM FLUID QUANTITY BEGAN TO DECREASE WHILE IN FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED O-RING ON THE CAPPED END OF VALVE ASSEMBLY LEADING TO LEFT BRAKE PRESSURE TRANSMITTER. THE O-RING WAS REPLACED AND THE LEFT HYDRAULIC SYSTEM WAS SERVICED. THE LEFT ENGINE WAS RUN AND ALL HYDRAULIC FLIGHT CONTROLS WERE CYCLED WITH NO LEAKAGE NOTED. (Z) 2L72 4F A6WE 19950331002341995033100234WP 1995 3 31 CAL950132 119950215A3260 SENSOR DOUG DC9 DC982 3022082WP NLG DIRTY A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0914810 49264 FLT NR 0310 - EWR - THE RED NOSE GEAR WARNING LIGHT REMAINED ILLUMINATED WITH NO GREEN INDICATION WHEN LANDING GEAR WAS EXTENDED ON APPRAOCH TO EWR. THE GEAR WAS CYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE CLEANED DIRT AND GREASE FROM NOSE GEAR SENSOR. THE NOSE GEAR WAS SWUNG PER MM 32-30-00 PAGES 201-206 AND INDICATIONS CHECKED GOOD. THE AIRCRAFT HAS COMPLETED OVER 10 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (Z) 2L72 4F A6WE 19950331002351995033100235 1995 3 31 CAL950136 419950217A3120 ACCELEROMETER DOUG DC10 DC1030 3023501WP NR 2 INOPERATIVE A CALAO OTHER O OTHER CLCLIMB 1 SW0914062 47863 FLT NR 0500 - FRA - THE STALL WARNING ACTIVATED MOMENTARILY DURING CLIMB-OUT WITH AUTO SLAT DEPLOYMENT. MAINTENANCE FOUND THE NR 2 LINEAR ACCELERAOMETER UNIT AT FAULT. THE ACCELEROMETER UNIT WAS REPLACED AND A BITE TEST WAS SUCCESSFULLY ACCOMPLISHED. (Z) 2L73 4F A22WE 19950331002361995033100236WP 1995 3 31 CAL950142 119950221A2150 SEALS DOUG DC9 DC982 3022082WP RT ACM LEAKING A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW0914839 49635 FLT NR 0297 - IAH - A HOT OILY ODOR WAS OBSERVED IN THE CABIN WITH THE AIRFOIL ANTI-ICE ON, DURING TAKEOFF, APPROACH, AND LANDING PHASES OF FLIGHT. MAINTENANCE REPLACED THE PERI SEALS ON THE RT AIR CYCLE MACHINE OUT DUCT AND OPERATIONAL CHECKS WERE GOOD. (Z) 2L72 4F A6WE 19950331002371995033100237WP 1995 3 31 CAL950144 119950221A215097968011 VALVE DOUG DC9 DC982 3022082WP RT PACK FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW09938751484811684 49125 FLT NR 5392 - BOS - SMOKE APPEARED IN THE CABIN ON APPROACH TO BOS WITH THE ENGINE AND AIRFOIL ANTI-ICE ON. THE SAME PROBLEM HAD OCCURRED ON THE PREVIOUS FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED DIAPHRAGM IN THE RT WATER SEPARATOR TEMPERATURE CONTROL VALVE. THE CONTROL VALVE WAS REMOVED AND REPLACED. IN ADDITION, THE RT ACM WAS REPLACED AS A PRECAUTIONARY MEASURE, AND THE RT COALESCER BAG WAS REPLACED. A FUNCTIONAL CHECK WAS PERFORMED AND NO LEAKAGE WAS PRESENT IN THE RT PACK SYSTEM. BURNOUT PROCEDURES WERE COMPLETED IAW MM 21-20-02, PAGE 209, PARAGRPAH C AND NO FURTHER SMOKE OR ODORS WERE PRESENT. (Z) 2L72 4F A6WE 19950331002381995033100238NM 1995 3 31 CAL950145 119950222A2612380678111 FIRE LIGHT BOEING727 727243 138408DNM APU ILLUMINATED A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW09174102903 527 21663 FLT NR 0225 - CLE - THE APU FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM CLE. THE APU WAS SHUT DOWN AND THE LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE APU WAS INSPECTED AND NO DEFECTS WERE FOUND. THE APU WAS RUN WITH PACKS OPERATING AND OPERATION CHECKED GOOD WITH NO DISCREPANCIES. (Z) 2L73 4F RTA3WE 19950331002391995033100239NM 1995 3 31 CAL950146 119950223A3232731413 ACTUATOR BOEING727 727243 138408DNM LT MLG DOOR LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SW09174022389415146 21265 FLT NR 0748 - IAH - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULICS AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG DOOR ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (Z) 2L73 4F RTA3WE 19950331002401995033100240NM 1995 3 31 CAL950147 119950223A3251651781412 CYLINDER BOEING727 727243 138408DNM NLG STEERING LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW0917407 21270 FLT NR 0783 - EWR - EXCESSIVE NOSE WHEEL SHIMMY AND A SIGNIFICANT LOSS OF STEERING WAS OBSERVED AS THE NOSE GEAR TOUCHED DOWN DURING LANDING AT EWR. THE 'A' SYSTEM HYDRAULIC QUANTITY WAS NOTED AT ZERO AFTER THE AIRCRAFT STOPPED. MAINTENANCE FOUND THE NLG LEFT STEERING CYLINDER LEAKING. THE STEERING CYLINDER WAS REMOVED AND REPLACED. IN ADDITION, THE STEERING METERING VALVE WAS REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. (Z) 2L73 4F RTA3WE 19950331002411995033100241NM 1995 3 31 CAL950150 119950204A3260 WARNING LIGHT BOEING727 727227 1384078NM RT MLG ILLUMINATED A CALAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CRCRUISE 1 SW0914760 21118 FLT NR 0603 - EWR - THE RT MLG RED UNSAFE LIGHT AND RT GEAR DOOR LIGHTS ILLUMINATED IN FLIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PEFORMED EXTENSION AND RETRACTION OF THE LANDING GEAR AND NO DEFECTS WERE NOTED. THE PROBLEM COULD NOT BE DUPLICATED. (Z) 2L73 4F A3WE 19950331002421995033100242WP 1995 3 31 CAL950151 119950224A3260 SWITCH DOUG DC9 DC982 3022082WP LANDING GEAR FAILED A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0914890 49114 FLT NR 0132 - EWR - ALL THREE GEAR INDICATORS REMAINED RED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND ONLY THE NOSE GEAR LIGHT AND DOOR LIGHT REMAINED ON. THE GEAR WAS CYCLED A SECOND TIME AND ALL INDICATIONS WERE NORMAL. THE THREE GEAR INDICATORS WENT RED AGAIN WHILE AT FL 330, BUT ALL THREE EXTINGUISHED WITHIN A FEW MINUTES, WITHOUT CREW INTERVENTION. MAINTENANCE REMOVED AND REPLACED THE GEAR LEVER CONTROL HANDLE SWITCH. THE GEAR WAS CYCLED SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. (Z) 2L72 4F A6WE 19950331002431995033100243NM 1995 3 31 CAL950152 119950226A2910 HYD LINE BOEING737 737130 1384435NM 'A' HYD SYST CHAFED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0959207 19024 FLT NR 1484 - EWR - THE 'A' HYDRAULIC SYSTEM WAS LOST APPROXIMATELY 20 MINUTES BEFORE ARRIVING IN EWR. THE HYDRAULIC QUANTITY INDICATED ZERO. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM AILERON PCU HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE PRESSURE LINE WAS REMOVED AND REPLACED. IN ADDITON, BOTH ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. (Z) 2L72 4F A16WE 19950331002441995033100244WP 1995 3 31 CAL950153 119950226A323039140165507 BUNGEE CYL DOUG DC9 DC932 3022066WP LT MLG INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091452420774 47539 FLT NR 1647 - CLE - THE LEFT MLG RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND BOTH RED LIGHTS EXTINGUISHED WITH THREE GREEN GEAR LIGHTS INDICATED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG BUNGEE CYLINDER AT FAULT. THE LEFT MLG BUNGEE CYLINDER WAS REMOVED AND REPLACED. GEAR OPERATION AND INDICATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950331002451995033100245WP 1995 3 31 CAL950157 119950221A5320 PRESS PANEL DOUG DC9 DC932 3022066WP BS 83.55 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091351242711 48111 HOU - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEEL WELL UPPER PRESSURE PANEL AT STATION 83.55. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03031. (Z) 2L72 4F A6WE 19950331002461995033100246SW 1995 3 31 BDHA9500003 119950217A324021203 BRAKE VALVE SWRNGNSA226 SA226TC 8780404SW LT MLG STUCK A BDHAO OTHER L NO TEST LDLANDING 1 GL15327BA 4496 TC249 MSP - FLT 447 - CAPTAIN REPORTED LT BRAKE PEDAL SOFT AND FO REPORTED HIS LT PEDAL INOP. INSPECTED AND FOUND BRAKE SHUTTLE VALVE STUCK AND LT I/B BRAKE OUT OF ADJUSTMENT. REPLACED LT I/B BRAKE ASSY AND RESET SHUTTLE VALVE AND BLED BRAKE SYSTEM. ACFT RELEASED FOR FLIGHT. (W) 1L72 4T A8SW 19950331002471995033100247 1995 3 31 RAIA950236 419950221A3197FF342 WIRE BAG JETSTMJETSTM3201 1500217EU FLT DIR PANEL SHORTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03341TE5663 950 STL - FLT 7507 - SMOKE WAS BEING EMITTED FROM FLIGHT DIRECTOR PANEL. MAINTENANCE REPAIRED SHORTED WIRE BEHIND FLIGHT DIRECTOR SELECTOR PANEL. SYSTEM TEST REVEALED NO SMOKE OPS CHECK OK. (W) 2L72 4T RTA56EU 19950331002481995033100248EU 1995 3 31 RAIA950237 119950222A5210137968C121 ROD END BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAO OTHER J WARNING INDICATION CRCRUISE 1 CE03429AM8620 879 STL - FLT 7442 - THE PAX DOOR LIGHT ILLUMINATED. MAINTENANCE ADJUSTED ROD END ON PAX DOOR HANDLE. SYSTEM TEST REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950331002491995033100249SO 1995 3 31 RAIA950239 119950222A3260922AA2YA6PZ722 SWITCH EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03131AM 120158 STL - FLT 7460 - THE RT GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED RT MAIN GEAR UPLOCK PROXIMITY SWITCH. GEAR SWINGS AND TEST FLIGHT REVEALED NORMAL OPERATION. (W) 2L72 4T RTA31SO 19950331002501995033100250SO 1995 3 31 RAIA950240 119950222A3350D36604001 EEL BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03128AM13865 120109 STL - EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (W) 2L72 4T RTA31SO 19950331002511995033100251EU 1995 3 31 RAIA950241 119950224A52101371376C401 SHOOT BOLT BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03430AM8687 880 JLN - FLT 7077 - THE PAX DOOR ILLUMINATED. MAINTENANCE ADJUSTED CABIN DOOR SHOOT BOLTS. SYSTEM TEST GOOD. (W) 2L72 4T RTA56EU 19950331002521995033100252SO 1995 3 31 RAIA950242 119950223A27503075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A ARAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03130AM11058 120134 BHM - FLT 7461 - THE FLAP ASSYMETRY OCCURRED, RT FLAP WENT UP AND DOWN. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM TEST GOOD. (W) 2L72 4T RTA31SO 19950331002531995033100253EU 1995 3 31 RAIA950243 119950226A771231024766 SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03339TE6154 935 STL - FLT 7086 - THE LT ENGINE TORQUE ONLY MADE 95 PERCENT. MAINTENANCE ADJUSTED LT ENGINE TORQUE SIGNAL CONDITIONER. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950331002541995033100254EU 1995 3 31 RAIA950244 119950225A3350OL60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 11271 176 STL - THE RT FWD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED RT FWD EMERGENCY LIGHT BULB. (W) 2H72 4T RTA53EU 19950331002551995033100255SO 1995 3 31 RAIA950245 119950227A30103D237606 EJECTOR VALVE EMB 120 EMB120RT SO DE-ICE BOOTS STICKY A RAIAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 CE03130AM11299 120134 STL - FLT 7502 - THE LT AND RT WING I/B DE-ICE BOOT FAULTED ALONG WITH LT AND RT HORIZONTAL STAB. THE I/B DE-ICE BOOTS. MAINTENANCE CLEANED DE-ICE EJECTOR VALVES. OPERATION CHECK GOOD. (W) 2L72 4T RTA31SO 19950331002561995033100256EU 1995 3 31 RAIA950246 119950225A2910137311D1619 HYD LINE BAG JETSTMJETSTM3201 1500217EU RT HYD BAY BROKEN A RAIAB EMER. DESCENT K FLUID LOSS DEDESCENT 1 CE03434AM 887 ALO - FLT 7454 - THE CREW NOTICED HYDRAULIC PUMP PRESSURE ZERO ON BOTH SIDES. CREW PERFORMED EMERGENCY CHECKLIST AND LANDED ACFT. MAINTENANCE DISCOVERED BROKEN HYDRAULIC LINE AT THE MAIN HYD FILTER. REPLACED LINE, AND LEAK CHECK GOOD ON GROUND RUN. (W) 2L72 4T RTA56EU 19950331002571995033100257WP 1995 3 31 RAIA950248 219950227A7320A218C14 SCREW X BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03864AE6206 864 66126 LAX - FLT 4757 - THE RT ENGINE ON TAKEOFF ROLL PRODUCING ONLY 97 PERCENT RPM. MAINTENANCE ADJUSTED RT ENGINE 'X' SCREW. GROUND POWER RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T4 TRTA56EU E4WE 19950331002581995033100258EU 1995 3 31 RAIA950249 119950227A3310OL8552BPE BULB BAG JETSTMJETSTM3201 1500217EU INST PANEL FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03435AM8476 889 STL - FLT 7409 - THE FO'S INSTRUMENT LIGHTS (PANEL MASTER) FLICKERED AND WENT OFF SOON AFTER A STRONG ELECTRIC SMELL OCCURRED. MAINTENANCE RE-BULBED INSTRUMENT LIGTHS (PANEL MASTER). OPS CHECK GOOD. (W) 2L72 4T RTA56EU 19950331002591995033100259EU 1995 3 31 RAIA950250 119950227A21701947801 SOCK AEROSPATR72 ATR72202 8680940EU LT PACK DIRTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE 283 STL - THE LT PACK EMITTED ODOR OF BURNING SMELL. MAINTENANCE CLEANED WATER SEPARATOR SOCK. GROUND TEST GOOD, NO ODOR NOTED. (W) 2H72 4T RTA53EU 19950331002601995033100260EU 1995 3 31 RAIA950301 119950301A61208954815 PITCH CONTROL BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03431AM7348 881 STL - FLT 7464 - THE RT BETA LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED RT PROPELLER PITCH CONTROL UNIT. SYSTEM AND LEAK CHECK GOOD ON GROUND RUN. (W) 2L72 4T RTA56EU 19950331002611995033100261NE 1995 3 31 RAIA950302 219950302A73203032475 CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE NR 2 EEC DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03131AM 120158 115251 LEX - FLT 7476 - DURING CLIMB, THE NR 2 ENGINE TORQUE DROPPED OFF. TURNING ON AUTO IGNITION RESTORED TORQUE. MAINTENANCE CLEANED THE EEC AND SCU CONNECTORS, PERFORMED GROUND RUN AT VARIOUS POWER SETTINGS AND SYSTEM CHECKED NORMAL. (W) 2L72 4T4 TRTA31SO E20NE 19950331002621995033100262EU 1995 3 31 RAIA950303 119950302A7712305969 SENSOR AEROSPATR42 ATR42300 8680920EU NR 1 ENG INOP A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE032FOR 199 MEM - FLT 7146 - ON CLIMB, THE NR 1 ENGINE WOULD NOT MAKE TORQUE. MAINTENANCE REPLACED THE LT ENG OIL IMMERSED THERMAL SENSOR. (W) 2H72 4T RTA53EU 19950331002631995033100263EU 1995 3 31 RAIA950304 119950302A77129495411 TQ TEMP LIMITER BAG JETSTMJETSTM3201 1500217EU NR 2 ENGINE INTERMIT A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03864AE 864 LAX - FLT 4706 - IN FLIGHT NR 2 ENG EGT AND TORQUE FLUCTUATES. MAINTENANCE DETERMINED TORQUE/TEMP LIMITER CAUSING FAULT. SYSTEM DEFERRED PER J32 MEL. (W) 2L72 4T RTA56EU 19950331002641995033100264WP 1995 3 31 RAIA950305 219950304A75302558A000 VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT NAC INOP A RAIAO OTHER O OTHER CLCLIMB 1 CE03436AM 891 THE ACFT WOULD NOT PRESSURIZE ABOVE 8500 FEET OR 3.3 PSI DIFF. MAINTENANCE REPLACED THE BLEED AIR SHUT OFF. (W) 2L72 4T4 TRTA56EU E4WE 19950331002651995033100265EU 1995 3 31 RAIA950306 119950307A26122TP17 SWITCH BAG JETSTMJETSTM3201 1500217EU COCKPIT FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03428AM 877 STL - FLT 7305 - THE LT ENGINE FIRE WARNING SOUNDED. MAINTENANCE REPLACED THE FIRE DETECTION PRESS TO TEST SWITCH. (W) 2L72 4T RTA56EU 19950331002661995033100266EU 1995 3 31 RAIA950315 119950313A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03424AM 865 STL - FLT 7508 - THE PAX DOOR CAPTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED PAX DOOR MICRO-SWITCH. SYSTEM TEST GOOD. (W) 2L72 4T RTA56EU 19950331002671995033100267EU 1995 3 31 RAIA950316 119950313A771231024766 SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03424AM 865 STL - FLT 7088 - THE LT ENGINE ONLY ACHIEVED 82 PERCENT TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER FOR LT ENGINE. GROUND POWER RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950331002681995033100268SO 1995 3 31 RAIA95128 119950224A304025C1160A CURRENT LIMITOR EMB 120 EMB120RT SO RT WINDSHIELD BURNT A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03128AM 120109 STL - FLT 7151 - INSULATION BURNING TYPE SMELL WHEN RT WINDSHIELD HEAT IS TURNED ON. MAINTENANCE REPLACED WIRE AND WINDSHIELD HEAT CURRENT LIMITOR. (W) 2L72 4T RTA31SO 19950331002691995033100269WP 1995 3 31 SCNA95026 119950220A3350A3060719103 EEL TRACK DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 MSP - EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE IN FWD CABIN, LT AND RT SIDES. ON LT SIDE OF FWD CABIN, REPAIRED BROKEN WIRE, REPLACED FLOOR TRACK COVER AND SECURED. ON RT SIDE OF FWD CABIN, REPLACED TWO SECTIONS OF TRACKLIGHTING. FLOOR TRACK LIGHTING OPS CHECKED GOOD PER DC-10 MM 33-50-01. (W) 2L73 4F A22WE 19950331002701995033100270EU 1995 3 31 VTZA95100 119950309A2751TY176004A POTENTIOMETER JETAIRJETSTMJETSTM4101 1500501EU FLAPS DIRTY A VTZAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA27308UE 41023 IAD-RDU - FLT 6576 - DURING APPROACH, ABORTED THE APPROACH DUE TO FLAP ASYMMETRY CAPTION ILLUMINATING WHEN FLAPS SELECTED TO 9 DEGREES. AN EMERGENCY WAS DECLARED AND THE ACFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED EXCESSIVE GLYCOL FROM FLAP POSITION POTENTIOMETERS. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950331002711995033100271EU 1995 3 31 VTZA95101 119950309A3260622800200 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27477UE 890 IAD-RDU - FLT 6598 - DURING CLIMBOUT, THE NOSE AND LT MAIN LANDING GEAR INDICATED UNLOCKED WITH THE GEAR HANDLE SELECTED UP. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE NOSE UPLOCK MICROSWITCH AND LUBED THE LT MAIN LANDING GEAR UPLOCK MICROSWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950331002721995033100272EU 1995 3 31 VTZA95102 119950309A32301849D UPLOCK ASSY BAG JETSTMJETSTM3201 1500217EU RT MLG DIRTY A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27497UE 904 IAD-CRW - FLT 6375 - DURING CLIMBOUT, THE RT MLG UNLOCKED LIGHT WOULD NOT EXTINGUISH AFTER GEAR SELECTED UP. RECYCLED GEAR, STILL WOULD NOT EXTINGUISH. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED GEAR LEG FREE OF SNOW AND ICE, CLEANED UPLOCK AND PERFORMED GEAR SWING. OPERATES NORMALLY. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950331002731995033100273EU 1995 3 31 VTZA95103 119950310A2751TY176004A POTENTIOMETER JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27306UE 41020 IAD-BDL - FLT 6521 - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE TAKEOFF WARNING SOUNDING ON THE TAKEOFF ROLL. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE NR 1 AND NR 2 FLAP POSITION POTENTIOMETERS TO ZERO. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950331002741995033100274EU 1995 3 31 VTZA95104 119950310A29101379305A77 HYD PRESS HOSE BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27486UE 905 IAD-HPN - FLT 6281 - FLIGHT DIVERTED TO SWF, DUE TO THE LOSS OF HYDRAULIC PRESSURE IN THE LT AND RT PUMPS. AN EMERGENCY WAS DECLARED AND ACFT LANDED AT SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE HYDRAULIC LINE RUNNING FROM THE PUMP TO THE BULKHEAD. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950331002751995033100275 1995 3 31 VTZA95105 419950312A31607011672111 SYMBOL GEN JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27307UE 41021 IAD-CHS - FLT 6366 - DURING CLIMBOUT, THE RT SYMBOL GENERATOR FAILED. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE SYMBOL GENERATOR. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950331002761995033100276EU 1995 3 31 VTZA95106 119950312A2160218D4 DUCT CONTL UNIT BAG JETSTMJETSTM3201 1500217EU LT NACELLE FAILED A VTZAA UNSCHED LANDING MN OVER TEMP FALSE WARNING CLCLIMB 1 EA27491UE 911 IAD-SCE - FLT 6326 - DURING CLIMBOUT, THE DUCT OVERTEMP LIGHT ILLUMINATED IN FLIGHT AND WOULD NOT EXTINGUISH WITH FLOWS SHUT OFF. ACFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DUCT CONTROL UNIT. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950331002771995033100277 1995 3 31 VTZA95107 319950313A6140310389813 BETA SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27311UE 41029 IAD-RDU - FLT 6579 - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE RT ENGINE RED BETA LIGHT ILLUMINATED. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE BETA PRESSURE SWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950331002781995033100278NM 1995 3 31 9504725515 119950314A5315141N5113 FLOOR BEAM BOEING757 757251 1384970NM FS 377.7 GOUGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01515US 28929 23203 DURING PERIODIC CHECK, THE FLOOR BEAM AT FS 377.7, RBL 4 WAS DAMAGED AND WAS REPAIRED PER SRM 53-00-51, FIG 201 AND NWA EA 55-97863. 2L72 4F RTA2NM 19950331002791995033100279WP 1995 3 31 9504731152 119950325A5320 ANGLE DOUG DC10 DC1040 3023508WP FS 1781 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE 'J' ANGLE AT FS 1781, RBL 20 - LBL 15 BELOW THE SUMP FLOOR. REMOVED CORROSION AND INSTALLED DOUBLER. 2L73 4F A22WE 19950331002801995033100280WP 1995 3 31 9504741152 119950324A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1139-1156 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON 52 AT FS 1139 - 1156 IN CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97898. 2L73 4F A22WE 19950331002811995033100281WP 1995 3 31 9504751152 119950324A5312 BULKHEAD DOUG DC10 DC1040 3023508WP FS 1157 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE BULKHEAD AT FS 1157, STR 51R AND 50R IN THE CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND FILLERS PER EA 11-97898. 2L73 4F A22WE 19950331002821995033100282WP 1995 3 31 9504769982 119950218A5542 SKIN DOUG DC9 DC932 3022066WP RUDDER LOOSE FASTENERS A NWAAK NONE O OTHER ININSP/MAINT 1 GL01982US 47590 DURING LINE CHECK, FOUND APPROXIMATELY 40 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS. 2L72 4F A6WE 19950331002831995033100283WP 1995 3 31 9504779956 119950324A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01923RW 47183 DURING PERIODIC CHECK, FOUND CRACK IN FORWARD CARGO DOOR END FITTING VISIBLE THROUGH OPENING NR 21. REPLACED FITTING. 2L72 4F A6WE 19950331002841995033100284WP 1995 3 31 9504789762 119950325A5320 FITTING DOUG DC9 DC941 302207NWP FS 642 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NW 47395 DURING LINE CHECK, FOUND CRACK IN LONGERON 30 END FITTING AT FS 642. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950331002851995033100285WP 1995 3 31 9504799105 119950326A5542 SKIN DOUG DC9 DC915 3022036WP RUDDER LOOSE FASTENERS A NWAAK NONE O OTHER ININSP/MAINT 1 GL0195S 47205 DURING LINE CHECK, FOUND APPROXIMATELY 40 - 50 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS. 2L72 4F A6WE 19950331002861995033100286NE 1995 3 31 9504801150 219950323A7200 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 3 FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01150US 46759 686145 DURING CLIMB, THE NR 3 ENGINE OIL QUANTITY BEGAN TO DECREASE, THE OIL STRAINER LIGHT ILLUMINATED, AND THE ENGINE WAS SHUT DOWN. 30,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO HNL WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. METAL AND BLACK OIL WERE FOUND. THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19950331002871995033100287WP 1995 3 31 9504819986 119950324A5270 SWITCH DOUG DC9 DC932 3022066WP CARGO DOOR INOPERATIVE A NWAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 GL01986US 47480 DURING CLIMB DTW-HPN, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. FOUND THAT BOTH THE INNER AND OUTER AFT CARGO DOORS WERE LATCHED IN THE OPEN POSITION. ALSO, FOUND THAT THE DOOR WARNING SYSTEM WAS INOPERATIVE. REPLACED THE AFT CARGO DOOR WARNING SWITCH. 2L72 4F A6WE 19950331002881995033100288NM 1995 3 31 9504826615 119950324A5313 LONGERON BOEING747 747251B 1384892NM FS 1365-1458.5 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 20360 DURING PERIODIC CHECK, FOUND SEVERAL CRACKS ON FUSELAGE INTERIOR STRINGER AT FS 1438, 1412, 1452, 1365, 1382.5, 1401.5, 1443, 1444, 1446, AND 1452.5. MADE REPAIRS PER SRM 51-10-01, PAR.0. 2L74 4F A20WE 19950331002891995033100289NM 1995 3 31 9504836614 119950227A5320 MOP SILL BOEING747 747251B 1384892NM FS 862 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, THE MOP SILL INSTALLATION UPPER AND LOWER CHORDS AT RBL 117 WERE FOUND CORRODED AT FS 862. DISCREPANT CHORDS WERE MADE FROM 7075-T6511 EXTRUSION. MADE REPAIR PER EA 66-93963. 2L74 4F A20WE 19950331002901995033100290NM 1995 3 31 9504846615 119950324A5313 STRINGER BOEING747 747251B 1384892NM FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 20360 DURING PERIODIC CHECK, FOUND CRACK EMANATING FROM STR 12L WEB BUT OUT IN FRAME 240L. STOP DRILLED CRACK TO .257 AND INSTALLED 2024-T3 .063 INCH DOUBLER PER SRM 51-40-02. 2L74 4F A20WE 19950331002911995033100291NM 1995 3 31 9504856614 119950222A5320 STRAP BOEING747 747251B 1384892NM NR 3 PAX DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE BEAR STRAP THAT SURROUNDS THE NR 3 LEFT MAIN ENTRY DOOR. CORROSION IS ON THE UPPER AFT CORNER OF THE DOORWAY. BEAR STRAP IS MADE FROM 0.300 INCH 2024.T351 ALUMINUM PLATE. MADE REPAIR PER EA 66-96589. 2L74 4F A20WE 19950331002921995033100292 1995 3 31 9504869959 419950321A3418 STALL WARNING DOUG DC9 DC931 3022065WP COCKPIT MALFUNCTIONED A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01919RW 47162 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED UPON APPLICATION OF TAKEOFF POWER. TAKEOFF WAS ABORTED. A SUCCESSFUL TAKEOFF WAS ACCOMPLISHED ON SECOND ATTEMPT. RECYCLED SYSTEM ON GROUND. ALL CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950331002931995033100293 1995 3 31 9504879959 419950320A3442 RADAR DOUG DC9 DC931 3022065WP COCKPIT FAILED A NWAAA UNSCHED LANDING O OTHER UKUNKNOWN 1 GL01919RW 47162 RADAR BEGAN SPOKING ON LOWER RIGHT SIDE OF SCREEN EN ROUTE DTW-BNA. THIS CAUSED ERRONEOUS DISPLAY OF KNOWN WEATHER. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR INDICATOR AND TRANSCEIVER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950331002941995033100294NM 1995 3 31 9504882707 119950325A215039854021 VALVE BOEING727 727225 1384077NM RT PACK FAILED A NWAAB EMER. DESCENT O OTHER CLCLIMB 1 GL01816EA7288 7288 22553 CLIMBING THROUGH FL 320, CABIN RATE OF CLIMB CONTINUED TO INCREASE AND CABIN ALTITUDE EXCEEDED 10,000 FT. DECLARED AN EMERGENCY AND DESCENDED TO FL100. CABIN STABILIZED AT 7400 FT. FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NO AIRFLOW FROM RIGHT PACK. REPLACED RIGHT PACK FORWARD SHUTOFF VALVE. OPERATIONAL CHECK OK. 2L73 4F A3WE 19950331002951995033100295WP 1995 3 31 9504891152 119950321A5312 BULKHEAD DOUG DC10 DC1040 3023508WP CNTR ACCESS COMPCORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER WING PRESSURE BULKHEAD AND LONGERON 52 IN THE CENTER ACCESSORY COMPARTMENT. REPAIRED BULKHEAD PER EA N11-97898. 2L73 4F A22WE 19950331002961995033100296SO 1995 3 31 COM11837 119950327A3241M610627023 RELAY EMB 120 EMB120RT SO ANTI-SKID SYST DEFECTIVE A COMAK NONE O OTHER CLCLIMB 1 SO01249CA 120230 ANTI SKID WARNING LIGHT ILLUMINATES WHEN LANDING GEAR RETRACTED. REPLACED RELAY K0021, SYSTEM TEST NORMAL. 2L72 4T RTA31SO 19950331002971995033100297SO 1995 3 31 COM11838 119950327A3260922ZZ2YA6PZ722 SENSOR EMB 120 EMB120RT SO NLG DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01205CA 120205 NLG A SYSTEM INTRANSIT LIGHT IS ILLUMINATING INTERMITTENTLY. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR. 2L72 4T RTA31SO 19950331002981995033100298SO 1995 3 31 COM11839 119950327A5720 SUPPORTS EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01265CA8105 120257 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION ASK NR 5720-551/651-01I AT WING RIBS NR 15 AND 16. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2 AND EMB SRM P/N: 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17057-006, 1 EA; 120-17057-005, 1 EA. 2L72 4T RTA31SO 19950331002991995033100299EU 1995 3 31 COM31050 119950326A32509302533001 U-JOINT SAAB SF340 SF340A 7850100EU NLG STEERING BROKEN A COMAO OTHER O OTHER LDLANDING 1 SO01361CA 340A056 NOSE WHEEL STEERING FAILED DURING LANDING. REPLACED BROKEN UNIVERSAL JOINT ON STEERING TILLER LINKAGE. 2L72 4T RTA52EU 19950331003001995033100300EU 1995 3 31 COM31051 119950323A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01146CA11119516 JUL880556 340A146 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERIVCE AND SENT TO ABS FOR BUSHING REPAIR. 2L72 4T RTA52EU 19950331003011995033100301EU 1995 3 31 COM31052 119950325A243651539007A GCU SAAB SF340 SF340A 7850100EU LT DC GEN DEFECTIVE A COMAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO01344CA19313194 340A025 LEFT DC GENERATOR FAILED IN FLIGHT. REPLACED THE LEFT GCU AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950331003021995033100302WP 1995 3 31 MWEA95152 119950327A33506011777 EEL BATTERY PACK DOUG DC9 DC914 3022034WP AFT BAG PIT TERMINALS DIRTY A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31600ME 45725 DURING ROUTINE INSPECTION, THE LEFT EMERGENCY NACELLE LIGHT WAS FOUND TO BE INOP. MECHANIC CLEANED AND SECURED BATTERY TERMINALS. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950331003031995033100303 1995 3 31 MWEA95153 419950328A256513621284 EVAC SLIDE DOUG DC9 DC914 3022034WP TAIL LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 DURING ROUTINE INSPECTION THE TAIL EVACUATION SLIDE PRESSURE WAS FOUND TO BE LOW. REMOVED AND REPLACED TAIL EVACUATION SLIDE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950331003041995033100304SW 1995 3 31 QXEA9500090 119950324A32347092011 SELECTOR SWRNGN SWRNGNSA227 SA227AC 8780603SW LANDING GEAR MALFUNCTIONING A QXEAO OTHER O OTHER CLCLIMB 1 NM09269592498812195 AC662 PDX - MUST USE OVERRIDE TO RETRACT LANDING GEAR. REPLACED LANDING GEAR CONTROL AND GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950331003051995033100305EU 1995 3 31 QXEA9500091 119950325A3350MGG1055 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 PDX - SEVERAL BULB OUT IN EMERGENCY SIGNS AT OVERWING EXIT AND COCKPIT DOOR. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950331003061995033100306EU 1995 3 31 QXEA9500092 119950327A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 PDX - EMERGENCY EXIT LIGHT RIGHT SIDE INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950331003071995033100307NM 1995 3 31 SCNA95042 119950322A335037067001 EEL BATTERIES BOEING727 7272A1 138407FNM AFT AIRSTAIR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 AFT AIRSTAIR SELF CONTAINED EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES, AFT AIRSTAIR EMERGENCY LIGHTS OPS CHECK GOOD. 2L73 4F A3WE 19950331003081995033100308WP 1995 3 31 SCNA95043 119950322A242197751504 GENERATOR DOUG DC10 DC1010 3022110WP NR 3 FAILED A SCNAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL15572SC 46977 NUMBER 3 GENERATOR DROPPED OFFLINE IN CRUISE, COULD NOT BE RESET. GENERATOR FAIL NR 3 LIGHT CAME ON 25 MINUTES LATER. CSD WAS DISCONNECTED PER COM. CONTINUED TO DESTINATION WITH NR 3 DISCONNECTED. FOUND FAILED GENERATOR, REMOVED AND REPLACED GENERATOR IAW DC-10 MM 24-21-04, RAN ENGINE, OPS CHECK GOOD, LEAK CHECK GOOD. 2L73 4F A22WE 19950331003091995033100309WP 1995 3 31 SCNA95044 119950323A2910AJK7004655 HYD LINE DOUG DC10 DC1010 3022110WP NR 2 HYD CHAFED A SCNAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15571SC 46645 NUMBER 2 HYDRAULIC SYSTEM WENT TO '0' QUANTITY DURING FLIGHT. FOUND PRESSURE BOOTSTRAP LINE CHAFED IN MAINTENANCE BAY FORWARD OF APU DOOR, PANEL NR 311AB. TEMPORARILY REPAIRED BY INSTALLING FLEX LINE IAW BMM 6-15-10 SECURED LINE, RAN A/C PUMPS AND PRESSURIZED NR 2 SYSTEM USING ENGINE PUMPS, NO LEAKS NOTED. SERVICED TO 8 GALLONS PRIOR TO RUN. CHECKED ALL FILTER DELTA PINS, NO DEFECTS NOTED. 2L73 4F A22WE 19950331003101995033100310NM 1995 3 31 SCNA95045 119950324A561057176241 L-2 WINDOW BOEING727 7272J4 1384006NM COCKPIT NOT CLOSED A SCNAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15285SC 21676 ON INITIAL ACCELERATION AT HUX, L-2 WINDOW CAME OPEN. ABORTED TAKEOFF, RESHUT WINDOW, AND ALL INDICATION WERE NORMAL ON SECOND TAKEOFF (PACKS OFF TAKE-OFF). OPENED L-2 WINDOW AND INSPECTED TRACK AND LOCKING MECHANISM, CYCLED WINDOW SEVERAL TIMES AND FOUND IT TO LOCK NORMALLY. NO OTHER DEFECTS NOTED. OK FOR SERVICE. 2L73 4F RTA3WE 19950331003111995033100311NE 1995 3 31 95ZZZZ160 219950301A7313378200 FUEL PUMP BOEING737 7372U9 1384498NM PWA JT8 JT8D15 52051NE LT ENG MALFUNCTIONED A AWXAO OTHER O OTHER APAPPROACH 1 WP28149AW 2003 22575 DEN - FLT NR 494 - ON APPROACH INTO DENVER, AT APPROX 12,000 MSL, THE LT ENGINE WOULD NOT SPOOL ABOVE IDLE. EPR 1.07, N1 20 PERCENT, N2 35 PERCENT, EGT 320 DEGREES, FUEL FLOW .5. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED ENG FUEL CONTROL AND ENG FUEL PUMP PER R5M73009 AND R5M73007. CLEANED PS3 FILTER PER BMM 72-00, FIG 106. RAN ENGINES, OPS NORMAL. PERFORMED TRIM PER AWA CARD F5M71002. AIRCRAFT RELEASED FOR SERVICE. REFERENCE AWXA9500125. 2L72 4F4 FRTA16WE E2EA 19950331003121995033100312NM 1995 3 31 95ZZZZ161 119950221A2710654476122 PCU BOEING737 7374Q8 NM B AIL SYSTEM MALFUNCTIONED A AASAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM01783AS761 25114 LAX - FLT 533 - DURING CLIMB-OUT FROM SNA, THE AIRCRAFT DID NOT RESPOND WELL TO ROLL CONTROL. IT WAS VERY SLOW TO RESPOND TO ROLL INPUT. BETWEEN 0 AND 60 YOKE DEFLECTION THERE WAS A CONSIDERABLE DEAD SPOT NOTED. AS AIRSPEED INCREASED THE ROLL RATE IMPROVED BUT WAS NOT NORMAL UP TO 280 KTS AND MACH .74 AT 28,000 FEET. FLIGHT WAS DIVERTED TO LAX AND ROLL CONTROL WAS VERY LIMITED DURING LANDING. INSPECTED SPOILER AND AILERON SYSTEMS AND CHECKED OPERATION OF SAME. NO FAULTS WERE FOUND. REPLACED 'A' AND 'B' SYSTEM AILERON POWER CONTROL UNITS AS A PRECAUTIONARY MEASURE. ACCOMPLISHED FULL FLIGHT CONTROL CHECK ON TEST FLIGHT AND SYSTEM OPERATED NORMALLY. REFERENCE ASAA954002. 2L72 4F RTA16WE 19950331003131995033100313NE 1995 3 31 95ZZZZ162 219950302A72617578679 OIL FILTER DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 ENG DIRTY A Y2PAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23197US 47154 P654600 RETURNED TO YIP, NR 1 ENGINE OIL CLOGGED LIGHT ILLUMINATED. REMOVED OIL FILTER, FOUND CARBON IN FILTER, DRAINED AND RESERVICED OIL TANK. REPLACED FILTER. ENGINE 18.8 HOURS SINCE SHOP VISIT. (Z) 2L72 4F4 F A6WE E2EA 19950331003141995033100314WP 1995 3 31 95ZZZZ163 119950115A7110236004550101 NOSE COWL DOUG DC8 DC863F 302198FWP STA YN86.9 CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND TRAILING EDGE OF NR 1 ENGINE COWL CRACKED AT 2 O'CLOCK POSITION BY ANTI-ICE TUBE. FABRICATED AND INSTALLED REPAIR IAW SRM 71-5-2 PG 314 AND DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-1. 2L74 4F 4A25 19950331003151995033100315NM 1995 3 31 95ZZZZ164 119950228A5242 BRACKET BOEING727 7272Q9 138448MNM E/E COMPT DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, E/E COMPARTMENT DOOR SKIN GOUGED AND BULGED AT FWD END AND AFT END. REPLACED DAMAGED BRACKET ASSEMBLY AT FWD END PER SRM 51-10-1 PG 4. CUT OUT DAMAGED AFT END RT SIDE PER SRM 51-10-1. INSTALLED ANGLE REPAIR PER SRM 51-40-3. INSTALLED OUTER SKIN IAW SRM 51-30-2. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003161995033100316NM 1995 3 31 95ZZZZ165 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 700 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FWD CARGO STATION 700 STR 28L-28R, SKIN CORROSION AT DOME NUTS. REPLACED SKIN FROM STATION 681 TO 725 STRINGER 26L AND 26R PER SRM 53-30-3. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003171995033100317NM 1995 3 31 95ZZZZ166 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 685 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FWD CARGO COMPARTMENT SKIN CORROISON STATION 685 STRINGER 28R. REPLACED SKIN FROM STATION 681-725 BETWEEN STRINGER 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003181995033100318NM 1995 3 31 95ZZZZ167 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 680 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FWD CARGO SKIN CORROSION STATION 680 STRINGER 28L-28R. REPLACED SKIN FROM STATION 680 TO 725 BETWEEN STRINGER 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003191995033100319NM 1995 3 31 95ZZZZ168 119950228A5320 FLOOR SUPPORT BOEING727 7272Q9 138448MNM BS 640 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FLOOR SUPPORT 'Z' ANGLE JUST AFT OF STATION 640 HAS CORROSION RBL 15 TO LBL 15. REMOVED COROSION PER SRM 51-10-6. CUT OUT DAMAGE 2 CHANNELS 15 LBL AND 15 RBL. INSTALLED ANGLE REPAIRS PER SRM 51-40-3 8 INCHES BY 1 INCH BY 1 INCH .050 5 EACH. INSTALL SPLICE PLATE WITH ANCHOR NUTS. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003201995033100320NM 1995 3 31 95ZZZZ169 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM BS 680 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, STRINGER 26L JUST ABOVE THROUGH RIVETS HAS EVIDENCE OF CRACK AND HAS CORROSION STATION 620 TO JUST AFT OF STATION 680. REPLACED STRINGER 26L FROM STATION 500 TO 680 IAW SRM 53-10-3. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003211995033100321NM 1995 3 31 95ZZZZ170 119950228A5320 FLOOR SUPPORT BOEING727 7272Q9 138448MNM BS 600 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DRUING D-CHECK, FLOOR SUPPORT 'Z' ANGLE RBL 14 FWD OF STATION 600, AFT SIDE OF REPAIR DOUBLER, INNERSIDE OF TOP FLANGE DOES NOT EXTEND PAST AFT STOP DRILL, CHECK REPAIR COMFORMITY TO SRM. FABRICATED REPAIR IAW SRM 51-40-3. CRACK STOPS AT ORIGINAL STOP HOLE 12 INCH AND 2 INCH ANGLE .071 2024-T3, REPAIR ANGLE INSTALLED PER SRM 51-40-3. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003221995033100322NM 1995 3 31 95ZZZZ171 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 620-560 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, STRINGER 26L BETWEEN STATION 620 TO 560 IN CTR OF STRINGER ABOVE OR OUTBOARD OF RIVETS HAS EVIDENCE OF CRACK AND HAS CORROSION. REPLACED STRINGER 26L FROM STATION 500 TO 680 IAW SRM 53-10-3 FIG 1. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003231995033100323NM 1995 3 31 95ZZZZ172 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FWD PASS DOOR CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FWD PASSENGER DOOR, FUSELAGE SKIN ABOVE TOP HINGE CUT OUT HAS GRIND OUT TO RIVET WITH NO EDGE DISTANCE. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1 DIM, 6 INCHES BY 3 INCHES 2024-T3 .125. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003241995033100324NM 1995 3 31 95ZZZZ173 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 1380 DENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FUSELAGE EXTERIOR, DENT IN FUSELAGE SKIN AT FS 1380 APPROX AT STRINGER 5R AREA. CUT OUT DAMAGED AREA AS PER SRM 53-30-3. INSTALLED REPAIR DOUBLER AS PER SRM 53-30-3 7 INCHES BY 8 INCHES .063 7075-T6. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003251995033100325NM 1995 3 31 95ZZZZ174 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 1090-1136 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, SEAT TRACK NR 3 HAS MANY SPOTS CORRODED STATION 1090 TO 1136. REPLACED SEAT TRACK PER SRM 51-10-1 PG 4 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003261995033100326NM 1995 3 31 95ZZZZ175 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 344-480 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FABRICATE NEW SEAT TRACKS FROM BLANK STOCK BACB 20-792 AT RBL 45.50 BS 344 TO BS 480 DUE TO PITCH MISMATCH AND CORROSION BEYOND LIMITS. REPLACED TRACK IAW 51-10-1 PAR 4. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003271995033100327NM 1995 3 31 95ZZZZ176 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 1000-1030 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, SEAT TRACK NR 3 CORRODED FROM STATION 1000 TO 1030. REPLACED SEAT TRACK PER SRM 51-10-1 PG 4 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003281995033100328NM 1995 3 31 95ZZZZ177 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 960 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, SEAT TRACK NR 3 CORRODED AT STATION 960. REPLACED SEAT TRACK TRACK PER SRM 51-10-1 FROM STATION 960 TO 1136. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003291995033100329NM 1995 3 31 95ZZZZ178 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 980-1130 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, SEAT TRACK NR 5 HAS MANY SPOTS CORRODED STATION 980 TO 1130. REMOVED CORROSION (.002) PER SRM 51-10-06 AND CUT OUT AND INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 1030 TO 1130 PER SRM 51-10-01. ALODINE AND PRIMED FROM STATION 980 TO 1030 PER SRM 51-10-02. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003301995033100330NM 1995 3 31 95ZZZZ179 119950228A5315 FLOOR BEAM BOEING727 7272Q9 138448MNM BS 440 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, CORROSION OF FLOOR BEAM UPPER FLANGE FROM RBL 24 TO BLO BS 440. PERFORMED REPAIR AS PER SRM 53-10-8 FROM LBL 24 TO LBL 0 STATION 440. MATERIAL REPAIR BAC1505-100617. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003311995033100331NM 1995 3 31 95ZZZZ180 119950228A5414 SKIN BOEING727 7272Q9 138448MNM 'S' DUCT CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 20 BLR 3 INCH. REMOVED CORROSION APPROX 3 INCH BY 3 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 54-10-3, DOUBLER APPROX 6 INCHES BY 10 INCHES 7075-T6. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003321995033100332NM 1995 3 31 95ZZZZ181 119950228A5414 SKIN BOEING727 7272Q9 138448MNM 'S' DUCT CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, CORROSION IN 'S' DUCT ON SKIN INT AT RIB 27 BLR 3 INCHES. INSTALLED REPAIR 7075-T6 .080 INCH 4 INCHES BY 7 INCHES AS PER SRM 54-10-3. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003331995033100333NM 1995 3 31 95ZZZZ182 119950228A5311 FRAME BOEING727 7272Q9 138448MNM BS 1090 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FRAME UPPER FLANGE HAS DAMAGE AT BS 1090 STRINGER 25L. REMOVED PAINT, STOP DRILLED PER SRM 51-10-1, STRAIGHTENED DENTED FRAME PER SRM 51-40-1, INSTALLED FRAME REPAIR PER SRM 53-10-4. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003341995033100334NM 1995 3 31 95ZZZZ183 119950228A5720 ANGLE BOEING727 7272Q9 138448MNM WS 193 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, CORROSION ON R/W FRONT SPAR LONGITUDINAL STIFFENER ANGLE JUST BELOW FUEL TANK ACCESS PLATE WS 193.0. REMOVED AND DISCARDED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003351995033100335NM 1995 3 31 95ZZZZ184 119950228A5320 SHEAR WEB BOEING727 7272Q9 138448MNM BS 1137 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, CORROSION NUMEROUS AREAS MARKED ON SHEAR WEBB TO SURFACE FROM BS 1137 AFT TO CHORD ANGLE RBL 24 TO RBL 48. INSTALLED NEW SHEAR WEBB PER SRM 51-10-1 AND 51-30-2. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003361995033100336NM 1995 3 31 95ZZZZ185 119950228A5230 SKIN BOEING727 7272Q9 138448MNM FWD BAG DOOR ERODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FORWARD BAG DOOR, AFT LOWER EDGE SKIN ERODED AND FAIRING MATERIAL MISSING. REMOVED FASTENERS AS PER SRM 51-30-2. CUT OUT DAMAGED AREA AS PER SRM 51-10-1. TREATED AND PRIMED AREA AS PER SRM 51-10-3. MANUFACTURED DOUBLER 6 INCHES BY 8 INCHES .080 2024-T3 AND INSTALLED PER SRM 52-30-3. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003371995033100337NM 1995 3 31 95ZZZZ186 119950228A5311 FRAME BOEING727 7272Q9 138448MNM FS 1148 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO COMPARTMENT STATION 1148 AT STRINGER 27R CORROSION ON FRAME UPPER AND LOWER FLANGES. REMOVED AND REPLACED LOWER CLIP AT STATION 1148 STRINGER 27R. INSTALLED FRAME REPAIR ON UPPER FLANGE AS PER SRM 53-10-4 5 INCHES BY 2 INCHES BY 1 INCH .050. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003381995033100338NM 1995 3 31 95ZZZZ187 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1176 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT BAG BIN STRINGER 27L HAS HEAVY CORROSION AT STATION 1176. REMOVED AND REPLACED STRINGER 27L FROM STATION 1183 TO 1166 AS PER SRM 51-10-1 PARA 4. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3 APPROX 54 INCHES BY 12 INCHES. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950331003391995033100339NM 1995 3 31 ASAA954002 119950221A2710 CONTROL MECH BOEING737 7374Q8 NM AILERONS BINDING A ASAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NM01783AS963 25114 LAX - FLT 533 - DURING CLIMB-OUT, THE A/C DID NOT RESPOND WELL TO ROLL CNTRL. IT WAS SLOW TO RESPOND TO ROLL INPUT. BETWEEN 0 AND 60 YOKE DEFLECTION THERE WAS A DEAD SPOT NOTED. AS AIRSPEED INCREASED THE ROLL RATE IMPROVED BUT WAS NOT NORMAL UP TO 280 KTS AND MACH .74 AT 28,000 FT. FLT WAS DIVERTED TO LAX. REPLACED 'A' AND 'B' SYS AILERON PWR CNTRL UNITS AS A PRECAUTIONARY MEASURE. ACCOMPLISHED FULL FLT CONTROL CHECK ON TEST FLT AND SYS OP NORMALLY. MX REPLACED THE AILERON TRIM ACT FOR T/S. MX REPLACED THE AILERON TWR SHAFT ASSY (AILERON CENTERING MECH P/N 657596025) AND THE LOST MOTION DEVICE ASSY (AILERON TRANSFER MECH P/N 655420016) AS FINAL CORRECTIVE ACTION. (W) 2L72 4F RTA16WE 19950331003401995033100340NE 1995 3 31 AWXA9500125 219950301A73217436025 FUEL CONTROL BOEING737 7372U9 1384498NM PWA JT8 JT8D15 52051NE LT ENG MALFUNCTIONED A AAWXAO OTHER O OTHER APAPPROACH 1 WP28149AW JFC602 22575 DEN - FLT NR 494 - ON APPROACH INTO DENVER, AT APPROX 12,000 MSL, THE LT ENGINE WOULD NOT SPOOL ABOVE IDLE. EPR 1.07, N1 20 PERCENT, N2 35 PERCENT, EGT 320 DEGREES, FUEL FLOW .5. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED ENG FUEL CONTROL AND ENG FUEL PUMP PER R5M73009 AND R5M73007. CLEANED PS3 FILTER PER BMM 72-00, FIG 106. RAN ENGINES, OPS NORMAL. PERFORMED TRIM PER AWA CARD F5M71002. AIRCRAFT RELEASED FOR SERVICE. REFERENCED 95ZZZZ160. 2L72 4F4 FRTA16WE E2EA 19950331003411995033100341SO 1995 3 31 C2XA95CL040 119950303A32502050000002 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING MALFUNCTIONED A AC2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091572110001 442 120160 FLT NR 3135 - CLE-CLE - NOSE WHEEL MADE LOUD BANG WHEN WEIGHT WAS REMOVED FROM NOSE WHEEL PEDAL STEER INOP LIGHT ON MAP ILLUMINATED. GEAR WOULD NOT RETRACT UNTIL PASSING 2000 FEET. MAINTENANCE REMOVED AND REPLACED FEEDBACK POTENTIOMETER. PERFORMED OPS CHECK OF SYSTEM, FOUND GOOD IAW EMB MM 32-50-05 AND 32-50-00. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331003421995033100342SO 1995 3 31 C2XA95CL041 119950301A315080055811 COMPUTER EMB 120 EMB120RT SO AVIONICS BAY MALFUNCTIONED A C2XACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW09157307677 0319 120187 CLE-CLE - ABORTED TAKEOFF FOR TRIM OUT OF LIMITS WARNING. MAINTENANCE CLEANED AND RESEATED THE AURAL WARNING COMPUTER AND OPS CHECK GOOD IAW EMB MM 31-53-00. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950331003431995033100343 1995 3 31 CAL950054 419950120A223019543554 A/T PANEL DOUG DC10 DC1010 3022110WP COCKPIT FAILED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09680426537962987 46901 FLT NR 0009 - HNL - SMOKE APPEARED IN THE COCKPIT WHILE IN FLIGHT. THE BATTERY BUS FEEDS WERE PULLED PER EMERGENCY CHECK LIST AND THE SMOKE CEASED. MAINTENANCE FOUND THE AUTO THROTTLE PANEL AT FAULT. THE AUTO THROTTLE PANEL WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (Z) 2L73 4F A22WE 19950331003441995033100344WP 1995 3 31 CAL950076 119950129A3350 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0913881 48045 FLT NR 0327 - EWR - THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS SECTION OF CABIN WOULD NOT ILLUMINATE WHEN TESTED DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (Z) 2L72 4F A6WE 19950331003451995033100345WP 1995 3 31 CAL950116 119950123A3350 EEL WIRING DOUG DC10 DC1010 3022110WP CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0968041 46900 KUL - INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT ROW 1-3. MAINTENANCE FOUND AND OPEN CIRCUIT IN THE WIRING AND THREE BLOWN FUSES IN THE POWER PACK ASSEMBLY. THE WIRING WAS SPLICED AND THE FUSES WERE REPLACED. OPERATION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS RESTORED. (Z) 2L73 4F A22WE 19950331003461995033100346NM 1995 3 31 CAL950161 119950215A5720 SUPPORT BOEING727 727243 138408DNM WS 521 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 521. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236. (Z) 2L73 4F RTA3WE 19950331003471995033100347NM 1995 3 31 CAL950162 119950215A5720 SUPPORT BOEING727 727243 138408DNM WS 469 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09571PE44093 21264 GSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LOWER TRAILING EDGE SUPPORT CHANNEL AT STATION 469. THE SUPPORT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW EX 5720C01236 AND CAL DRAWING 5720 DC8908. (Z) 2L73 4F RTA3WE 19950331003481995033100348NM 1995 3 31 CAL950172 119950303A3231 DOOR BOEING727 727232 1384082NM RT NLG OUT OF ADJUST A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09523PE 20646 FLT NR 0702 - EWR - THE NLG WOULD NOT EXTEND WHEN GEAR WAS LOWERED FOR LANDING ON APPROACH TO EWR. THE NOSE GEAR DOOR LIGHT DID NOT INDICATE OPEN AND THE NOSE GEAR DOWN AND LOCKED INDICATION DID NOT ILLUMINATE. THE GEAR WAS CYCLED AND THE NOSE GEAR EXTENDED NORMALLY. MAINTENANCE FOUND THE RT NOSE GEAR DOOR OUT OF ADJUSTMENT. THE RT NOSE GEAR DOOR ROD ASSEMBLY AND SAFETY WERE ADJUSTED PER MM 32-22-1. THE NOSE GEAR WAS SWUNG SEVERAL TIMES AND ALL OPERATION CHECKED GOOD. (Z) 2L73 4F A3WE 19950331003491995033100349NE 1995 3 31 WRLA95008 219950305A7200 ENGINE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 3 LPC DAMAGE A AWRLAECD ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK A FLAME/FIRE TOTAKEOFF 1 EA27273WA 48519 DURING T/O, AT APPROX 80 KTS, CREW HEARD A LOUD 'BANG' FROM NR 3 ENG. A/C BEGAN VEERING TO RT. CREW CORRECTED DIRECTIONAL PATH AND ABORTED T/O. OBSERVED FLAME AND SMOKE FROM NR 3 ENG. CREW SHUTDOWN NR 3 ENG, AND AS A PRECAUTION DISCHARGED THE NR 1 FIRE EXTINGUISHER BOTTLE (NO FIRE INDICATION NOTED IN COCKPIT). A/C CLEARED RUNWAY WITHOUT FURTHER INCIDENT. A/C RETURNED TO GATE. INITIAL INVESTIGATION BY MX PERSONNEL VERIFIED NO EVIDENCE OF FIRE OR FIRE DAMAGE TO A/C OR ENGINE. FURTHER VISUAL INVESTIGATION COULD NOT FIND DAMAGE TO EITHER FAN OR TURBINE BLADES. HOWEVER, METAL DEBRIS WAS FOUND IN 2.9 BLEED AIR SCREENS. SUSPECT COMPRESSOR BLADE FAILURE. A/C TO BE TWO ENG FERRIED FOR ENGINE CHANGE. (Z) 2L73 4F4 FRTA22WE E24NE 19950331003501995033100350NM 1995 3 31 DL733950621 119950204A2612899323 DETECTOR BOEING737 737347 1384647NM GE CFM56 CFM56* 13802NE NR2 ENGINE FAULTY A DALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SO113301 23181 721213 DURING APPROACH HAD NR 2 ENGINE OVERHEAT/FIRE INDICATION NR 2 WAS SHUT DOWN, BOTTLE DISCHARGED. NO EVIDENCE OF FIRE WAS FOUND. SUBSEQUENT TROUBLESOOTING REPLACED LOOP DETECTOR. 2L72 4F4 FRTA16WE E2GL 19950331003511995033100351NE 1995 3 31 DLL14951145 219950314A7260M06592AA GEARBOX LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SO11737D 193C1228 014709 DURING CRUISE NR 1 ENGINE FLAMED OUT WITHOUT ANY WARNING, HAD NO OIL PRESSURE INDICATION AFTER FLAME OUT. FOUND ACCESSORY GEARBOX FAILED. REPLACED GEARBOX OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19950331003521995033100352WP 1995 3 31 DLL17950632 119950211A73338T5100GBD7 TRANSMITTER LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 2 ENG FF FAULTY A DALAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO11769DL 193H1218 014629 DURING CRUISE, NR 2 ENGINE WAS SHUT DOWN DUE TO HIGH FUEL FLOW DIVERTED JFK. FOUND FUEL LEAK AT TURBINE CASE DRAIN. AS PRECAUTION FUEL NOZZLES WERE REPLACED, AND FOUND FUEL LINE AT FLOAT EJECTOR VALVE NOT SAFTIED. REPLACED VALVE AND SAFTIED LINE. HIGH FUEL FLOW INDICATION WAS FOUND TO BE FAULTY FUEL FLOW TRANSMITTER. REPLACED TRANSMITTER. 2L73 4F4 F A23WE E12EU 19950331003541995033100354SW 1995 3 31 SWIA95523 119950207A261230300020 FIRE DET PROBE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE MALFUNCTIONED A SWIAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 NM072730P AC736 EN ROUTE TO PHX, BOTH LEFT FIRE LIGHTS ILLUMINATED. SHUT DOWN ENGINE AND SECURED AS PER EMERGENCY CHECK LIST. FOUND LEFT OIL COOLER FIRE DETECTION PROBE TO BE ACTIVATING AT TOO LOW A TEMP, GIVING A FALSE FIRE INDICATION. REPLACED FAULTY PROBE AND FIRE BOTTLE ASSY WITH SERVICEABLE UNITS. OPS CHECKS GOOD ON THE GROUND. 1L72 4T4 T A8SW E4WE 19950331003551995033100355SW 1995 3 31 SWIA95524 119950208A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT MLG MALFUNCTIONED A SWIAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 NM07686AV AC686 WITH 1/2 FLAPS, LEFT MAIN GEAR WOULD NOT COME DOWN. CYCLED GEAR 4 TIMES. FLAPS NEVER RETRACTED TO 1/4. LEFT MAIN CAME DOWN WITH A GREEN INDICATION. PERFORMED GEAR SWINGS. COULD NOT DUPLICATE WITH FLAPS IN ANY POSITION. AIRCRAFT RETURNED TO SERVICE. SEE FL 3392 FOR MECH SIGN OFF. 1L72 4T4 T A8SW E4WE 19950331003561995033100356SW 1995 3 31 SWIA95527 119950212A2430 LEAD SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT GENERATOR DAMAGED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM0727297 AC735 RIGHT GENERATOR TRIPPED OFF LINE AS POWER WAS ADVANCED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPAIRED C LEAD ON RIGHT GENERATOR TERMINAL BLOCK. RAN RIGHT ENGINE. LOADED GENERATOR TO 250 AMPS. OPS CHECKS GOOD AT LOW SPEED SETTINGS ON GROUND RUN. SEE FL 10682. 2L72 4T4 TRTA8SW E4WE 19950331003571995033100357WP 1995 3 31 SWIA95537 219950305A7320 BYPASS VALVE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NR 2 ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 NM07176SW AC591 NR 2 ENG BYPASSED AT 610 TEMP ON TO. AFTER ABORTING, RAN UP THE ENGINE TO DUPLICATE AND COULD NOT. DECIDED TO TRY TO POWER TO 615 ON NEXT TO AND UNTIL ABOUT 800 FT DID IT BYPASS FUEL AGAIN, HOWEVER, THE BYPASS VALUE WAS STUCK OPEN AND WOULD NOT STOP THE BYPASSING. RAN RIGHT ENG FOR BY PASS PROBLEM. ENG BYPASSES AT 650 DEG WITH SRL ON PERFORMED CHECK SEVERAL TIMES, NO DEFECTS NOTED. LEFT AND RIGHT FF THE SAME ON BOTH SIDES. INSPECTED RIGHT BY PASS VALUE AND WIRES. NO DEFECTED NOTED. COULD NOT DUPLICATE ON THE GROUND. 1L72 4T4 T A8SW E4WE 19950331003581995033100358SW 1995 3 31 SWIA95540 119950307A5210 AIR TUBE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP CABIN DOOR OUT OF POSITION A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07175SW AC621 EXPERIENCED RAPID DEPRESSURIZATION AT 15000 FEET. UNABLE TO CONTROL PRESSURIZATION IN EITHER NORMAL OR AUTO MODES. RAN NR 2 ENGINE. CHECKED CABIN AND CARGO DOOR SEALS. REPOSITIONED AIR TUBE FOR CABIN DOOR. CLEANED SQUAT SWITCH ON LANDING. OPS CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950331003591995033100359WP 1995 3 31 SWIA95542 219950304A732189737515 FUEL CONTROL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE MALFUNCTIONED A ASWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM072720B AC715 ON TAKEOFF, UNABLE TO ACHIEVE TARGET TORQUE OF 81 PERCENT WITH RIGHT ENGINE. OBTAINED WITH RIGHT POWER LEVER FULL FORWARD ONLY 76 PERCENT. ABORTED TAKEOFF. FOUND RIGHT FF AT 440 PPH AT TARGET. PUMP OUTPUT CHECKS GOOD. REPLACED RIGHT FUEL CONTROL AND REINSTALLED FUEL PUMP. ALL IAW MM 73-20-00. SEE FL 189039. 1L72 4T4 T A8SW E4WE 19950331003601995033100360WP 1995 3 31 SWIA95544 219950305A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LEFT MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM072699Y AC666 LEFT ENGINE DOES NOT MAKE POWER. PERFORMED COMPLETE GROUND RUN ON LEFT AND RIGHT ENGINES. LEFT ENGINE MADE TARGET TORQUE (90 PERCENT AT 19 DEG OAT/500 PA) WITH P/L TRAVEL AND POWER TO SPARE. SEE FL 09643. 1L72 4T4 T A8SW E4WE 19950331003611995033100361WP 1995 3 31 SWIA95545 219950307A7320 FUEL CONTROL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE OUT OF ADJUST A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07184SW AC647 ABORTED TAKEOFF. LEFT ENGINE AT 100 PERCENT ONLY PRODUCED 38 PERCENT TORQUE. WITH SPEEDS LOW, LEFT ENGINE ONLY PRODUCED 95 PERCENT. PERFORMED ENGINE RUN SHEET AND FOUND LEFT ENGINE RPM'S AT 103 PERCENT. ADJ ADJUSTED SCREW BY 1.5 TURNS CCW. THE ENGINE MADE TARGET TORQUE OF 91.7 PERCENT WITH ROOM TO SPARE. SEE FL 187746. 1L72 4T4 T A8SW E4WE 19950331003621995033100362SW 1995 3 31 SWIA95546 119950307A2120 AIR DIST SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP COCKPIT ODOR A SWIAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM07174SW AC620 STRONG BURNING INSULATION SMELL OCCURRED ON DESCENT AND LANDING. INSPECTED COCKPIT WIRING BEHIND INSTRUMENT PANEL, LEFT AND RIGHT SIDE PANELS AND J BOX. FOUND NO DEFECTS. INSPECT FWD CARGO COMPARTMENT FOR BURNT WIRES. NO DEFECTS NOTED. RAN ENGINES TO CHECK FLAP AND AIR COND SYSTEM. NO DEFECTS NOTED. INSTRUMENT PANEL LIGHTS AND BACK LIGHTING WORKS NORMAL. COULD NOT DUPLICATE ON THE GROUND. OPS CHECKS OK. 1L72 4T4 T A8SW E4WE 19950331003631995033100363SW 1995 3 31 SWIA95547 119950309A5210 SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP CABIN DOOR FAILED A SWIAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NM0727297 AC735 WHILE AT CRUISE ALT OVER STOCKTON 10,000 FEET ALTITUDE, CABIN DEPRESSURIZED THROUGH CABIN DOOR SEAL. REPLACED MAIN DOOR SEAL. PRESSURIZED AIRCRAFT. OPS CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950331003641995033100364WP 1995 3 31 95ZZZW277 119950225A261205020 FIRE LOOP DOUG DC8 DC863F 302198FWP NR 2 ENGINE GROUNDED A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15921R 46145 ON CLIMBOUT, THE NR 2 ENGINE GOT A FIRE WARNING. REDUCED POWER AND FIRE WENT OUT, FIRE WARNING DID RESET. MAINTENANCE AT CYYZ FOUND NR 2 FIRE LOOP GROUNDED OUT. REMOVED AND REPLACED LOWER FIRE WARNING HARNESS. SYSTEM OPS CHECKED GOOD. (W) 2L74 4F 4A25 19950331003651995033100365EU 1995 3 31 RAIA950307 119950308A3411 PITOT BAG JETSTMJETSTM3201 1500217EU NOSE MOISTURE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03422AM9123 856 STL - FLT 7425 - ON TAKEOFF ROLL, CAPTAINS AIRSPEED INDICATOR INOP. MAINTENANCE DRAINED PITOT LINES AND PERFORMED A PITOT TEST, SYSTEM CHECKED NORMAL. (W) 2L72 4T RTA56EU 19950331003661995033100366EU 1995 3 31 RAIA950308 119950308A213013788L SAFETY VALVE BAG JETSTMJETSTM3201 1500217EU CABIN DIRTY A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03422AM9123 856 ALO - FLT 7465 CABIN DEPRESSURIZED IN FLIGHT. MAINTENANCE CLEANED THE SAFETY VALVE SCREEN AND SEAT. (W) 2L72 4T RTA56EU 19950331003671995033100367SO 1995 3 31 RAIA950309 119950308A27523203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP INOPERATIVE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03125AM10494 120017 SUX - FLT 7210 - THE RT NACELLE FLAP WOULD NOT RETRACT. MAINTENANCE REPLACED THE NACELLE FLAP ACTUATOR. (W) 2L72 4T RTA31SO 19950331003681995033100368EU 1995 3 31 RAIA950310 119950310A3250AIR86002 STEERING CONTROL BAG JETSTMJETSTM3201 1500217EU NOSE GEAR OUT OF RIG A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03340TE6136 939 STL - FLT 7038 - THE ACFT IS NOT STEERABLE, BRAKING AND POWER NOT EFFECTIVE, STEERING HANDLE NOT EFFECTIVE. MAINTENANCE REINDEXED AND RIGGED STEERING CONTROL VALVE TO AIRFRAME STEERING LINKAGE. GROUND TAXI CHECK GOOD. (W) 2L72 4T RTA56EU 19950331003691995033100369WP 1995 3 31 RAIA950311 219950311A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE WORN A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03431AM7391 881 66178 STL - FLT 7094 - THE RT TORQUE LOW, ENGINE BYPASS AT 98 PERCENT. MAINTENANCE REPLACED RT ENGINE BLEED AIR GASKETS. (W) 2L72 4T4 TRTA56EU E4WE 19950331003701995033100370EU 1995 3 31 RAIA950312 119950309A575385613 EROSION TAPE BAG JETSTMJETSTM3201 1500217EU RT TE FLAP LOOSE A RAIAO OTHER O OTHER CRCRUISE 1 CE03429AM8690 879 ALO - FLT 7475 - DURING FLIGHT CREW HEARD UNUSUAL NOISE. AFTER LANDING THE LEFT WING FLAP EROSION TAPE WAS DISCOVERED TO BE LOOSE. MAINTENANCE REMOVED EXCESS AND SECURED EROSION TAPE, (W) 2L72 4T RTA56EU 19950331003711995033100371EU 1995 3 31 RAIA950313 119950112A771231024762 SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03431AM8735 881 STL - FLT 7330 - THE RT ENGINE MADE TARGET TORQUE, BUT GOT AN EGT SPIKE OF 700 DEG. MAINTENANCE ADJUSTED RT ENGINE TORQUE SIGNAL CONDITIONER. GROUND POWER RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950331003721995033100372 1995 3 31 RAIA950314 319950309A614031024762 MONOPOLE BAG JETSTMJETSTM3201 1500217EU RT PROP GOV FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03432AM5080 883 STL - FLT 7043 - THE RT SRL LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED AND ADJUSTED RT ENGINE PROPELLER GOVERNOR MONOPOLE. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950331003731995033100373NM 1995 3 31 TAOA039501 119950302A33506012541 EEL BATT PACK GRIMES BOEING727 727254 138408LNM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15915TS 3478 20252 THE LT EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950331003741995033100374NM 1995 3 31 TAOA039502 119950304A3350900835A EEL BATT PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 20445 THE FWD ENTRY EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950331003751995033100375NM 1995 3 31 TAOA039503 119950304A3350900835A EEL BATT PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 20445 THE RT OVERWING EMERGENCY EXIT SIGN INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950331003761995033100376NM 1995 3 31 TAOA039505 119950310A3350900835A EEL BATT PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 22043 THE EXTERIOR EMERGENCY LIGHTS, LT AFT AND CENTER INOPERABLE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (W) 0 4 A3WE 19950331003771995033100377EU 1995 3 31 UF6A950301 119950312A6123S5600075N CONNECTOR BAG ATP ATP EU NR 1 ENGINE DIRTY A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03854AW7685 2028 ORD - FLT 5069 - THE NR 1 AUTOFEATHER UNIT WILL NOT ARM. MAINTENANCE CLEANED CANNON PLUG 'C'. (X) 2L72 4T RTA27NM 19950331003891995033100389CE 1995 3 31 95ZZZX1422 119950307A3233508202085 ACTUATOR BEECH 200 200BEECH 1152920CE NLG OVERHEATED A AGONAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW01130PA 94B254 BB330 WHILE RIGGING GEAR, SUBMITTER NOTICED NOSE ACTUATOR WAS HOT TO TOUCH. CALLED BEECH SERVICE REP. THEY ADVISED TO REMOVE AND REPLACE ACTUATOR. HOT ACTUATOR WAS YELLOW TAGGED FROM BEECH. SECOND NEW ACTUATOR OPERATED PERFECTLY, WAS NOT HOT TO TOUCH. 1L72 4T A24CE 19950331004271995033100427NM 1995 3 31 AWXA9500119 119950227A21603981161 AIR MIX VALVE BOEING737 737275 1384485NM LEFT STUCK A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 20922 PHX\LAS - FLT 2807 - AIR TURNBACK, DUAL DUCT OVERHEAT DURING TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MX FOUND LEFT AIR MIX VALVE STUCK IN MID-POSITION, NOT MOVING IN MANUAL OR AUTO. MX REMOVED AND REPLACED LT AIR MIX VALVE, OPERATION CHECK NORMAL IAW AWA CARD R2C21003. REPLACED CABIN TEMP REGULATOR PN 548376, SN 076C2423, AS PRECAUTIONARY, OPERATIONAL CHECK NORMAL PER BMM 21 61 00. ACFT RETURNED TO SERVICE. AIR MIX VALVE, MFG PN 3981161 1, SN 38 3985. CONDITION STUCK OPEN, LOCATION ONLY. (X) 2L72 4F A16WE 19950331004291995033100429NE 1995 3 31 9503426603 219950326A7320 ENGINE BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE NR 2 FLAME OUT A NWAAO OTHER RX PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CRCRUISE 1 GL01603US 19780 662490 DURING CRUISE, THE NR 2 ENGINE EXPERIENCED A ROLLBACK OF ALL ENGINE INDICATIONS AND FLAMED OUT. RESTARTED ON FIRST ATTEMPT AND OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. FUEL TANKS WERE SUMPED, FUEL FILTER WAS REPLACED, FUEL PRESSURE WAS CHECKED, AND A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E20EA 19950331004301995033100430NM 1995 3 31 9504902277 119950322A575165217097 FITTING BOEING727 727251 138408HNM AILERON CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01277US 21156 DURING PERIODIC CHECK, FOUND INBOARD AILERON LEFT QUADRANT SUPPORT FITTING CORRODED. REPAIRED PER NWA EA 22-96488. 2L73 4F A3WE 19950331004311995033100431NM 1995 3 31 9504912277 119950320A522065021082 FRAME BOEING727 727251 138408HNM EMERG. EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01277US 21156 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEMENT. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS. 2L73 4F A3WE 19950331004321995033100432NM 1995 3 31 9504922277 119950320A522065021082 FRAME BOEING727 727251 138408HNM EMERG. EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01277US 21156 DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEMENT. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS. 2L73 4F A3WE 19950331004331995033100433NM 1995 3 31 9504932277 119950320A522065021082 FRAME BOEING727 727251 138408HNM EMERG. EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01277US 21156 DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT AFT EMERGENCY EXIT DOOR OUTSIDE HANDLE OPENING FRAME CRACKED. REPLACED CASTINGS PER BOEING SRM. REPLACED MAGNESIUM HOUSING WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS. 2L73 4F A3WE 19950331004341995033100434NM 1995 3 31 9504942706 119950325A5313655623632 STRINGER BOEING727 727225 1384077NM FS 488 STR 28L CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND FS 488, STR 28L CORRODED. REPIARED PER NWA EA 27-096496. 2L73 4F A3WE 19950331004351995033100435NM 1995 3 31 9504955534 119950325A5320146N5447 FLOOR SUPPORT BOEING757 757251 1384970NM FS 1445 1500 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01534US 21522 24265 DURING PERIODIC CHECK, THE AFT CARGO FLOOR SUPPORT STRINGERS WERE FOUND CORRODED AROUND NUTPLATES BETWEEN FS 1445 AND 1500, LBL 11 AND RBL 3. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97818. 2L72 4F RTA2NM 19950331004361995033100436NE 1995 3 31 9504961153 219950326A7200 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 2 FLAME OUT A NWAAE ENGINE SHUTDOWN XJMENGINE FLAMEOUT WARNING INDICATION OVER TEMP TXTAXI/GRND HDL 1 GL01153US 46762 686147 DURING TAXI OUT, THE NR 2 ENGINE EXPERIENCED A SURGE AND FLAMED OUT WITH THE EGT GOING TO MAX FOR THREE SECONDS. TAIL WIND GUSTS TO 25 KTS WERE BEING EXPERIENCED. THE ENGINE WAS INSPECTED AND BOROSCOPE WAS ACCOMPLISHED. AN ENGINE CHANGE HAS BEEN SCHEDULED. 2L73 4F4 F A22WE E20EA 19950331004371995033100437NM 1995 3 31 9504976632 119950314A5320 CHORD BOEING747 747251B 1384892NM FUS 400 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 23112 DURING PERIODIC CHECK, THE CREW ENTRY DOOR SILL CHORD AT RBL 80 AND FS 400 WERE FOUND WITH TYPICAL CRACKING. CRACK WAS ALSO FOUND IN FS 400 SHEAR TIE WEB DISCREPANT CHORD IS MADE FROM1036 - 2401 EXTRUSION AND MATERIAL IS 7075-T6511 ALUMINUM. MADE REPAIR PER EA 66-97778. 2L74 4F A20WE 19950331004381995033100438NM 1995 3 31 95UAL727025 119950316A7931761392 OIL PRESS TUBE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 2 ENGINE CRACKED A UALAE ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 WP297276U412987823 21423 700132 THE NR 2 ENGINE OIL PRESSURE AND QUANTITY DROPPING, LOW OIL PRESS LIGHT ON. THE ENGINE WAS SHUTDOWN. A BRAZE IN NR 6 OIL TUBE WAS CRACKED. ENGINE RECEIVED A FULL REPAIR AND ALL MODULES EXCEPT THE N1 COMPRESSOR WERE ROUTED. A FULL MIS CLEAN WAS ACCOMPLISHED. ALL MAIN LINE BEARINGS WERE OH INSPECTED. 2L73 4F4 F A3WE E2EA 19950331004391995033100439NM 1995 3 31 95UAL727026 119950316A291059110 HYDRAULICS BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE A SYSTEM FAILED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP297273U 21420 RETURNED TO LGA DUE TO LOSS OF A-SYSTEM HYDRAULICS. FLIGHT CANCELLED. REPLACED RIGHT HAND ELEVATOR POWER CONTROL UNIT. 2L73 4F4 F A3WE E2EA 19950331004401995033100440NM 1995 3 31 95UAL727027 119950321A3350 EEL LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN ROW 8 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297448U 21902 OVERHEAD EMERGENCY LIGHT ROW 8 INOPERATIVE. REPLACED BATTERY. CHECKS OKAY. 2L73 4F4 F A3WE E2EA 19950331004411995033100441NM 1995 3 31 95UAL727028 119950327A3350 EEL LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE LT BODY FAIRING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297457U 21911 EMERGENCY LIGHT ON LEFT WING TO BODY FAIRING INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950331004421995033100442NM 1995 3 31 95UAL727029 119950327A3350 EEL LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AFT AIRSTAIR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297287U 21565 AFT AIRSTAIR AREA EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES IN PACK. 2L73 4F4 F A3WE E2EA 19950331004431995033100443NM 1995 3 31 95UAL727030 119950327A2133 OUTFLOW VALVE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN PRESS MALFUNCTION A UALAB EMER. DESCENT O OTHER CRCRUISE 1 WP297266U 21413 UNABLE TO CONTROL CABIN PRESSURE IN STANDBY OR MANUAL. MADE EMERGENCY DESCENT TO 10,000 FEET AND GOT PRESSURE TO STABILIZE. UNABLE TO CONTROL OUTFLOW VALVE. CABIN WILL RISE BUT WILL NOT DESCEND. 2L73 4F4 F A3WE E2EA 19950331004441995033100444NM 1995 3 31 95UAL727031 119950327A3350 EEL LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE LT OVERWING INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297461U 21915 LEFT INTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. 2L73 4F4 F A3WE E2EA 19950331004451995033100445NM 1995 3 31 95UAL737030 119950317A2910 SEAL PLATE BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE RUDDER VALVE FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29995UA 22399 B-SYSTEM HYDRAULIC LOW QUANTITY LIGHT CAME ON AND A SYSTEM QUANTITY DROPPED TO 1.25 GALLONS. B-SYSTEM LOW PRESSURE LIGHT DID NOT COME ON, BUT AUTO PILOT WOULD NOT LIGHT. REPLACED FAILED SEAL PLATE ON RUDDER SOLENOID VALVE. CHECKS OK. 2L72 4F4 F A16WE E2EA 19950331004461995033100446NM 1995 3 31 95UAL737031 119950317A3350M1132 BATTERY PACK BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN EEL DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29909UA 25009 EMERGENCY ESCAPE PATH LIGHTS INOP AT DOORS 1 RIGHT AND 1 LEFT AND EMERGENCY EXIT SIGN OVER DOOR 1 LEFT INOP. REPLACED BATTERY PACK. LIGHTS CHECK OK. 2L72 4F4 FRTA16WE E2GL 19950331004471995033100447NM 1995 3 31 95UAL737032 119950317A3350 LIGHT STRIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN EEL DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29946UA 26687 EMERGENCY ESCAPE PATH LIGHTING INOP IN FIRST CLASS AND FORWARD GALLEY. REPLACED GALLEY FLOOR LIGHT STRIP. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950331004481995033100448NM 1995 3 31 95UAL737033 119950317A3397 WIRE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29947UA 26688 EMERGENCY ESCAPE PATH LIGHTING STRIP INOP IN FIRST CLASS ROWS ONE AND TWO, AND AT FORWARD GALLEY. REPLACED EMERGENCY ESCAPE PATH LIGHT POWER CABLE. GROUND CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950331004491995033100449WP 1995 3 31 95UALD10025 119950307A3260001801 PROX SENSOR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NLG WW FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP291844U 48260 AFTER TAKEOFF AT IAD GEAR RED LIGHT STAYED ON WHEN HANDLE WAS PLACED IN UP POSITION. GEAR WAS RETURNED TO DOWN AND LOCKED. RETURNED TO IAD. REPLACED BENT GROUND SENSING CONTROL ROD AND SERVICED NLG STRUT. OPS CK OK. THREE DAYS LATER SAME PROBLEM REOCCURRED. NLG DOWN POS SENSOR RPL. NO FURTHER INCIDENT. 2L73 4F4 F A22WE E23EA 19950331004501995033100450WP 1995 3 31 95UALD10028 119950320A3350 EEL LIGHT DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL A ZONE MID LAV DEFECTIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291833U 47965 A ZONE RT EEL STRIP LIGHT FAILED OPERATIONAL CHECK. REPLACED EEL STRIP IN FRONT OF RT MID LAV. 2L73 4F4 F A22WE E23EA 19950331004511995033100451WP 1995 3 31 ABXA9500245 119950324A2910NAS161220 O-RING DOUG DC8 DC862 3021970WP NR 2 HYD PUMP DEFECTIVE A ABXAO OTHER K FLUID LOSS APAPPROACH 1 GL23805AX 45906 DURING APPROACH AFTER THE FLAPS WERE SELECTED TO 35 DEGREES, THE HYDRAULIC FLUID LEVEL IN THE MAIN RESERVOIR WENT TO STANDPIPE LEVEL. FOUND DEFECTIVE O-RING AT THE NR 3 ENGINE HYDRAULIC PUMP INLET ELBOW. REPLACED O-RING. SERVICED, LEAK, AND OPS CHECKED SYSTEM IAW DC 8 MM CHAPTER 29. 2L74 4F 4A25 19950331004521995033100452WP 1995 3 31 ABXA9500246 119950326A32305774035508 CYLINDER DOUG DC8 DC863 302198AWP MLG SHEARED PIN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23811AX466594765 46113 UPON CLIMB-OUT OF PDX GEAR UNSAFE LIGHT, RIGHT MLG DOOR, AND RIGHT MLG UNSAFE LIGHTS ILLUMINATED. RECYCLED GEAR SEVERAL TIMES. DURING UPLATCH CHECK, THE LIGHT STAYED ON. PERFORMED ABNORMAL PROCEDURES AND UPLATCH CHECK DOOR LIGHT WENT OUT; GEAR UNLATCHED AND UNSAFE LIGHT STAYED ON. CONTINUED AT REDUCED AIRSPEED TO ILN. FOUND MLG ACTUATOR ATTACH PIN TO GEAR SHEARED AT THE STRUT. REMOVED AND REPLACED THE ATTACH PIN IAW REA0832-11273-MR AND DC 8 OVH MANUAL CHAPTER 32. REMOVED AND REPLACED THE RIGHT MLG ACTUATOR AS PRECAUTIONARY IAW DC 8 MM CHAPTER 32. GEAR INDICATION AND OPERATIONS CHECKED GOOD. 2L74 4F 4A25 19950331004531995033100453NM 1995 3 31 DL72E950989 119950309A5320 WEB BOEING727 727247 138408FNM AIR STAIR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 FOUND ON LETTER CHECK STA 1235 LT LIGHTENING HOLE DAMAGED AT 7:00 POSITION AIR STAIR VERTICAL WEB. REPAIR INSTALLED DOUBLER PER MM 53-11-0 PG 828. 2L73 4F A3WE 19950331004541995033100454NM 1995 3 31 DL72E950992 119950309A5753 FLAP BOEING727 727247 138408FNM NR 4 FORE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 FOUND ON LETTER CHECK NR 4 FORE FLAP L/E CRACKED .25 INCH ABOVE NR 7 FLAP TRACK. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950331004551995033100455NM 1995 3 31 DL72E950994 119950310A57536521634150K FLAP BOEING727 727247 138408FNM NR 3 FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 LEADING EDGE WORN 52 INCHES FROM I/B END OF RT WING NR 3 AFT FLAP. REPAIRED PER SRM 575004 FIG 9. 2L73 4F A3WE 19950331004561995033100456NM 1995 3 31 DL72E951059 119950225A5753652163234 FLAP BOEING727 727247 138408FNM NR 3 MID CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION I/B CARRIAGE FITTING IN THE I/B THRUST BEARING RETAINER BOLT HOLE CORROSION WAS REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950331004571995033100457NM 1995 3 31 DL72E951060 119950225A5753652163234 FLAP BOEING727 727247 138408FNM NR 3 MID CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 3MID FLAP DURING HMV INSP WAS FOUND TO HAVE CORROSION IN THREE THRUST BEARING RETAINER BOLT HOLES. 2L73 4F A3WE 19950331004581995033100458NM 1995 3 31 DL72E951061 119950227A5330 SKIN BOEING727 727247 138408FNM STA 700 STR 26L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND FUSELAGE SKIN CRACKED AT FS 700 AT STR 26L. REMOVED DAMAGED AREA, REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950331004591995033100459NM 1995 3 31 DL72E951062 119950225A5753652163234 FLAP DOUBLER BOEING727 727247 138408FNM NR 3 MID MIS INSTALLED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE AN IMPROPERLY INSTALLED DOUBLER ON THE AFT LOWER SPAR AT I/B QUADRENT PUSH ROD CUTOUT. 2L73 4F A3WE 19950331004601995033100460NM 1995 3 31 DL72E951063 119950227A5330 SKIN BOEING727 727247 138408FNM STA 1065 STR 28LCORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND AFT B/B FUSELAGE SKIN WITH CORROSION DAMAGE UNDER A PREVIOUS REPAIR AT FS 1065 AT STR 28L. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950331004611995033100461NM 1995 3 31 DL72E951064 119950227A5313 STRINGER BOEING727 727247 138408FNM STA 1050 STR 28RCORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND STR 28R CORRODED AT SPLICE AT FS 1050. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950331004621995033100462NM 1995 3 31 DL72E951065 119950228A5313 STRINGER BOEING727 727247 138408FNM STA 1050 STR 28LCORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AFT B/B CORROSION ON O/B SIDE OF STR 28L FS 1050-1070 NEAR JUNCTURE WITH FUS SKIN. FOUND AND REPAIRED AT HMV. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950331004631995033100463NM 1995 3 31 DL72E951066 119950228A5320 DOUBLER BOEING727 727247 138408FNM STA 1060 REQ REPLACEMENT A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV FOUND TIME LIMITED REPAIR AT FS1060 BETWEEN STR 21 AND 22L. INSTALLED PERMANENT REPAIR PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 19950331004641995033100464NM 1995 3 31 DL72E951067 119950301A5347 SEAT TRACK BOEING727 727247 138408FNM STA 420-380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND SEAT TRACK CORRODED AT FS 420 - 380 AT RBL 24 SPLICED IN SECTION FROM 400 TO 344 PER MM 53-20-11 FIG 802. SPLICED SEAT TRACK SECTION FROM 400-440 PER MM 53-20-11. 2L73 4F A3WE 19950331004651995033100465NM 1995 3 31 DL72E951069 119950225A5753652163234 SPAR BOEING727 727247 138408FNM NR 3 MID FLAP CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE A CRACKED AFT LOWER SPAR 55 INCHES FROM I/B END. 2L73 4F A3WE 19950331004661995033100466NM 1995 3 31 DL72E951070 119950301A5315 FLOOR BEAM BOEING727 727247 138408FNM STA 380 RBL 60 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND FS 380 CABIN FLOOR BEAM CORRODED AT RBL 60. REPAIRED PER SRM 53-10-8 FIG 1. 2L73 4F A3WE 19950331004671995033100467NM 1995 3 31 DL72E951071 119950225A5753652163234 DOUBLER BOEING727 727247 138408FNM NR 3 MID FLAP MIS INSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112823W 21328 NR 3 MID FLAP DURING HMV INSP WAS FOUND TO HAVE IMPROPERLY INSTALLED DOUBLER ON AFT LOWER SPAR AT QUADRANT PUSH ROD CUTOUT I/B END. THIS IS A REWRITE FROM CARD NR 4974. 2L73 4F A3WE 19950331004681995033100468NM 1995 3 31 DL72E951099 119950225A57536521631273A FLAP BOEING727 727247 138408FNM NR 1 FORE LE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 1 FORE FLAP, TEMP REPAIR INSTALLED ON LEADING EDGE, 48 INCHES FROM O/B END. FOUND AT HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG. 1 2L73 4F A3WE 19950331004691995033100469NM 1995 3 31 DL72E951101 119950225A57536521631273A FLAP BOEING727 727247 138408FNM NR 1 FORE LE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 1 FORE FLAP, TWO TEMP REPAIRS ON LEADING EDGE NEAR I/B END ON UPPER SIDE OF FLAP. FOUND DURING HMV, SHOP INSP. REPLACED TEMP REPAIRS WITH PERM REPAIR AS PER 57-50-4, FIG 1. 2L73 4F A3WE 19950331004701995033100470NM 1995 3 31 DL72E951102 119950225A57536521631273A FLAP BOEING727 727247 138408FNM NR 1 FORE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 1 FORE FLAP, LEADING EDGE WORN 12 INCHES FROM I/B END LOWERSIDE. FOUND DURING HMV, SHOP INSPECTION. REPAIRED PER SRM 57-50-4, FIG 1. 2L73 4F A3WE 19950331004711995033100471NM 1995 3 31 DL72E951103 119950315A5753 FLAP 6521631326K BOEING727 727247 138408FNM NR 4 FORE LE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 221 21328 AT HMV SHOP INSPECTION NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT 54 INCHES FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950331004721995033100472NM 1995 3 31 DL72E951110 119950302A5530 STRINGER BOEING727 727247 138408FNM STR 1L CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV INSPECTION PER EO 4-59253-3AD, FOUR DIFFERENT VERTICAL STABILIZER STRINGERS WERE FOUND CRACKED. THE CRACK LOCATIONS ARE STR8L AT STA 180.6, STR 9L AT STA 133.8, STR 7R AT STA 133.8, AND STR 1L AT STA 39.809. IN ACCORDANCE WITH M/M 55-30-0, PG. 803, AND S/B 727-55-0075, REV 2, THE STRINGERS WERE REPAIRED. 2L73 4F A3WE 19950331004731995033100473NM 1995 3 31 DL72E951122 119950228A5532 SKIN BOEING727 727247 138408FNM VERTICAL STAB. STOP DRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND VERTICAL STABILIZER EXTERIOR SKIN HAS A STOP DRILL ON RT SIDE 20 INCHES FWD OF REAR SPAR AT FUSELAGE, REPAIRED PER FABRICATING DOUBLER PER MM 55-30-0 PG 801 CRACK PREVIOUSLY STOP DRILLED, DYE CHECKED CRACK AND NO FURTHER DAMAGE. INSTALLED DOUBLER PER MM 55-30-0 PG 801. 2L73 4F A3WE 19950331004741995033100474NM 1995 3 31 DL72E951123 119950227A5311 FRAME BOEING727 727247 138408FNM AFT BAG BIN BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND AFT BAG BIN FRAME BROKEN AT STA 970 ABOVE STRINGER 23 L, REPAIRED BY CUTTING OUT DAMAGE DYE CHECKED PER 900-6-3 NR 1, NO CRACK FOUND. FABRICATED DOUBLER AND FILLER INSTALLED REPAIR PER SRM 53-10-4. 2L73 4F A3WE 19950331004751995033100475NM 1995 3 31 DL72E951126 119950301A5315 FLOOR BEAM BOEING727 727247 138408FNM STA 420 RBL 56 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 FLOOR BEAM CORRODED AT STA 42O, RBL 56 INCHES. O/B SEATTRACK RIGHT SIDE CORRODED SAME LOC AS ITEM 1. REPAIRED PER SRM 53-10-8 FIG 1. FOUND AT HMV. 2L73 4F A3WE 19950331004761995033100476NM 1995 3 31 DL72E951127 119950301A5320 FLOOR SUPPORT BOEING727 727247 138408FNM STA 418 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 FLOOR SUPPORT CORRODED AT STA 418 RBL 12 INCHES TO Z ANGLE AT AFT SIDE OF FWD SVC DOOR. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV. 2L73 4F A3WE 19950331004771995033100477NM 1995 3 31 DL72E951128 119950301A5315 FLOOR BEAM BOEING727 727247 138408FNM FUS. STA 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 FLOOR BEAM CORRODED AT FS 400 FROM LBL 12 TO RBL 12. SPLICED IN NEW SECTION OF BEAM PER SRM 53-10-8 FIG 3. FOUND AT HMV. 2L73 4F A3WE 19950331004781995033100478NM 1995 3 31 DL72E951129 119950314A5347 SEAT TRACK BOEING727 727247 138408FNM STA 800 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 SEAT TRACK RT I/B HAS TOOLING DAMAGE ON O/B FLANGE STA 800. REPAIRED PER SRM 53-10-5 PG27. FOUND AT HMV. 2L73 4F A3WE 19950331004791995033100479NM 1995 3 31 DL72E951130 119950311A5313 STRINGER BOEING727 727247 138408FNM STA 700 STR 28L CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 FWD B/B CORROSION ON STR 28L AT STA 700. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV. 2L73 4F A3WE 19950331004801995033100480NM 1995 3 31 DL72E951131 119950311A5347 SEAT TRACKS BOEING727 727247 138408FNM RH STA1010-1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 RT I/B AND RT O/B SEAT TRACKS CORRODED STA 1010-1050. REPAIRED PER MM 53-20-11 FIG 804. FOUND AT HMV. 2L73 4F A3WE 19950331004811995033100481NM 1995 3 31 DL72E951132 119950301A5320 BEAM BOEING727 727247 138408FNM STA 720D WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 BEAM WORN C1 AFT BULKHEAD WALL SUPPORT BEAM AT STA 720D, BELOW RT I/B SEAT TRACK IS WORN AT WASHERS. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV. 2L73 4F A3WE 19950331004821995033100482NM 1995 3 31 DL72E951133 119950301A5320 SUPPORT BOEING727 727247 138408FNM AC BAY STA 720D WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 SUPPORT WORN AC DISTRIBUTION BAY BULKHEAD SUPPORT WORN AT UPPER ATTACH POINT, FS 720D ABOVE STR26L. REPAIRED PER SRM 53-10-9 FIG 8. FOUND AT HMV. 2L73 4F A3WE 19950331004831995033100483NM 1995 3 31 DL72E951135 119950225A5753652163233 FLAP BOEING727 727247 138408FNM NR 2 MID CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 NR 2 MID FLAP, CRACK IN LOWER AFT SPAR CHORD AT 41 INCHES FROM O/B END OF FLAP AND ONE AT 18 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M 575200 PG 807, INSTALLED DOUBLER. FOUND AT HMV SHOP INSPECTION. 2L73 4F A3WE 19950331004841995033100484NM 1995 3 31 DL72E951155 119950228A5330 SKIN BOEING727 727247 138408FNM STA 1125 STR 27RCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 SKIN BULGED AND CRACKED STA 1125 STR 27 RT. FOUND AT HMV. REPAIRED PER SRM 53-30-3 FIG. 2L73 4F A3WE 19950331004851995033100485NM 1995 3 31 DL72E951156 119950301A5320 CHORD BOEING727 727247 138408FNM FS950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 CHORD CORRDED, CORROSION ON CHORD OB OF RT KEEL BEAM EXTENSION FS950, FOUND AT HMV. REPAIRED PER SRM 53-10-9 FIG 11. 2L73 4F A3WE 19950331004861995033100486NM 1995 3 31 DL72E951158 119950303A5321 FLOOR BOEING727 727247 138408FNM STA 1167 LBL44-4CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 STA 1167 FLOOR AT LBL 44 TO LBL 49 CORRODED. FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 10. 2L73 4F A3WE 19950331004871995033100487NM 1995 3 31 DL72E951166 119950301A5315 BEAM BOEING727 727247 138408FNM STA 1110 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 CORROSION FLOOR BEAM STA 1110, TOP OF BEAM ALL THE WAY ACROSS. REPAIRED AT RBL 18 TO RBL 33 PER SRM 53-10-8. 2L73 4F A3WE 19950331004881995033100488NM 1995 3 31 DL72E951171 119950301A5320 ANGLE BOEING727 727247 138408FNM FS312-344 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 ANGLE CORRODED FLOOR SUPPORT ANGLES CORRODED FROM FS 312 TO FS 344 LBL28. REPLACED SUPPORT AT FS 312 TO 328 AND CLEANED CORROSION PER SRM 51-10-6. 2L73 4F A3WE 19950331004891995033100489NM 1995 3 31 DL72E951172 119950206A5320 TEE BOEING727 727247 138408FNM PANEL 3348 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND CORROSION AT LOWER FUSELAGE HINGED PANEL 3348 FRAME WHERE HINGES ATTACH, IN THE RADIUS OF FRAME BEAM. REPAIRED ATTACH 'T' PER M/M 53-30-1, REPAIRED FORMED SECTION PER SRM 51-40-3 FIG 1. 2L73 4F A3WE 19950331004901995033100490NE 1995 3 31 DL72E951297 219950326A731437820113 PUMP BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE SHEARED SHAFT A DALAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 SO112826W 21331 687493 NR 2 ENGINE FLAMED OUT AT BEGINNING OF DESCENT WHEN THROTTLE WAS RETARDED. DID NOT RESTART. LANDED SLC. REPLACED FUEL PUMP AND CONTROL OPERATION NORMAL. 2L73 4F4 F A3WE E2EA 19950331004911995033100491NM 1995 3 31 DL72L951004 119950225A711065196854539 NOSE COWL BOEING727 727232 1384082NM PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 DURING SHOP INSPECTION, FOUND KNIFE EDGE DAMAGE TO THE FRAME AREA AT STATION 99.25 OF ENGINE INTAKE COWL. REPAIRED DAMAGE PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950331004921995033100492NM 1995 3 31 DL72L951072 119950225A7110 COWL 65196854539 BOEING727 727232 1384082NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 746 21308 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH WEAR DAMAGE TO AFT FRAME AT THE 4 AND 9 O'CLOCK POSITIONS. REPAIRED PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950331004931995033100493NM 1995 3 31 DL72L951076 119950309A5754 RIB 651622162 BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA BN939 21308 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH CRACKED RIBS AT LOCATIONS NR 17, 18, 19. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950331004941995033100494NM 1995 3 31 DL72S950997 119950310A3211 BEARING MOUNT BOEING727 727232 1384082NM L/H MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 LT MLG FWD TRUNNION BEARING MOUNT CORRODED ON INBD FACES AND ALL FOUR BORES. 2L73 4F A3WE 19950331004951995033100495NM 1995 3 31 DL72S951046 119950313A5210 SKIN BOEING727 727232 1384082NM MAIN ENTRY CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FOUND ON F-1 LETTER CHECK, .375 INCH CRACK MAIN ENTRY DOOR SKIN. INSTALLED REPAIR PER MM 52-11-01 FIG 806. 2L73 4F A3WE 19950331004961995033100496NM 1995 3 31 DL72S951049 119950313A5754 SKIN BOEING727 727232 1384082NM NBR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FOUND DURING F-1 LETTER CHECK, CRACK AT NBR 7 SLAT BELOW TAI TELESCOPING TUBE. REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950331004971995033100497NM 1995 3 31 DL72S951050 119950313A5400 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FOUND DURING F-1 LETTER CHECK, CENTER ENG INLET DUCT OUTER SKIN CRACKED .25 INCH RT SIDE FWD OF PNL 9501. REPAIRED PER M/M 54-30-0 FIG 801. 2L73 4F A3WE 19950331004981995033100498NM 1995 3 31 DL72S951078 119950308A5754651622296 RIB BOEING727 727232 1384082NM NR6 SLAT R/H LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE 2ND RIB FROM THE O/B END OF SLAT CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950331004991995033100499NM 1995 3 31 DL72S951080 119950308A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIB NR 4 CRACKED. (I/B RIB OF THE O/B TRACK). REPAIRED PER MM 57-54-0 PG. 813. 2L73 4F A3WE 19950331005001995033100500NM 1995 3 31 DL72S951082 119950308A5754651622296 RIB BOEING727 727232 1384082NM NR6 SLAT R/H LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING SHOP INSPECTION, FOUND NR 6 L/E SLAT WITH L/E RIBS NR 7 AND NR 12 CRACKED. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950331005011995033100501NM 1995 3 31 DL72S951083 119950308A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING SHOP INSPECTION NR 6 L/E SLAT WAS FOUND WITH L/E RIB NR 10 CRACKED. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950331005021995033100502NM 1995 3 31 DL72S951088 119950227A5343 BRACKET BOEING727 727232 1384082NM STA 910 R/H CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND DURING CV-2/ LO CHECK, .25 INCH VISIBLE CRACK AT STA 910 ANGLE ABOVE H BRACKET. RIGHT L/G UPLOCK ATTACH STRUCTURE. REPAIRED PER MM 53-11-0 PG 834. 2L73 4F A3WE 19950331005031995033100503NM 1995 3 31 DL72S951089 119950227A5343 ANGLE BOEING727 727232 1384082NM STA 913 R/H CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND DURING CV-2 L/O CHK, .25 INCH CRACK AT STA 913 SUPPORT ANGLE ABOVE H BRACKET RT SIDE. LANDING GEAR UPLOCK ATTACH STRUCTURE. REPAIRED PER MM 53-11-0 PG 834. 2L73 4F A3WE 19950331005041995033100504NM 1995 3 31 DL72S951094 119950310A5330 SKIN BOEING727 727232 1384082NM FS 480 STR 28L CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CHECK, CORROSION ON SKIN O/B SIDE STR 28L UNDER INNER COSTAL AFT OF STA 480. REPAIRED PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 19950331005051995033100505NM 1995 3 31 DL72S951095 119950228A5313 STRINGER BOEING727 727232 1384082NM FS 720D STR 27L CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CHECK, STR 27L AT STA 720D TO FWD OF STA 720C, WITH CORROSION DAMAGE, REPAIRED PER ERA 30133744. 2L73 4F A3WE 19950331005061995033100506NM 1995 3 31 DL72S951096 119950228A5320 FLOOR SUPPORT BOEING727 727232 1384082NM FS 620 STR 27R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CHECK, FLOOR SUPPORT 'Z' CHANNEL CORRODED AT FASTNER HOLES ABOVE STR 27R STA 620-640. REPAIRED PER ERA 301345-14 CODE 4-53-21-04. 2L73 4F A3WE 19950331005071995033100507NM 1995 3 31 DL72S951097 119950228A5320 Z ANGLE BOEING727 727232 1384082NM FS 620 STR 27R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CHECK, CORROSION FOUND ON 'Z' ANGLE ABOVE STR 27R JUST FWD OF STA 620. REPAIRED PER ERA 301345-14 CODE 4-53-21-04. 2L73 4F A3WE 19950331005081995033100508NM 1995 3 31 DL72S951098 119950228A5330 SKIN BOEING727 727232 1384082NM FS 480 STR 28L CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND ON CV2 CHECK, CORROSION LEFT SIDE OF STRINGER SPLICE STR 28L STA 480. REPAIRED SKIN PER SRM 53-30-3 FIG 3. REPLACED FACTORY SPLICE WITH SAME. 2L73 4F A3WE 19950331005091995033100509NM 1995 3 31 DL72S951111 119950212A531165C2030313 WEB BOEING727 727232 1384082NM WL 216 L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11407DA 21151 DURING SERVICE CHECK INSPECTION, THE REPLACEMENT WEB PREVIOUSLY INSTALLED AS PART OF THE FRAME REPAIR KIT WAS FOUND CRACKED AT WL 216. IN ACCORDANCE WITH BAC S/B 727-53-0153, R.6., THE EXISTING WEB WAS REPLACED. 2L73 4F A3WE 19950331005101995033100510NM 1995 3 31 DL72S951112 119950303A5320651841483 PLATE WEB BOEING727 727232 1384082NM BS 270 RH SIDE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 DURING INSPECTION AT CV-2, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 270. IN ACCORDANCE WITH BAC S/B 727-53-145, THE DAMAGED PORTION OF THE WEB WAS TRIMMED OUT, AND A DOUBLER AND 4 REPAIR STRAPS WERE INSTALLED. 2L73 4F A3WE 19950331005111995033100511NM 1995 3 31 DL72S951113 119950304A5320651751724 TRANSVERSE BEAM BOEING727 727232 1384082NM FS 1263 RH TORQ CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11485DA 20865 DURING LETTER CHECK INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED. PER THE B727 S/B 53-0129, REV 4, THE PART WILL BE REPLACED. 2L73 4F A3WE 19950331005121995033100512NM 1995 3 31 DL72S951117 119950315A5412 ANGLE BOEING727 727232 1384082NM NR 2 FIREWALL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11469DA 20746 FWD LEFT COWL LIP ON FIREWALL DAMAGED 8:00 POSITION. NBR 2 ENG. FOUND DURING B-2 LETTER CHECK. 2L73 4F A3WE 19950331005131995033100513NM 1995 3 31 DL72S951118 119950315A5754651622295 SLAT BOEING727 727232 1384082NM NR 3 LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 INNER SKIN CRACKED AT RIVET, O/B OF O/B ACTUATOR RIB. REPAIRED PER M/M 57-54-0 FIG 803A BY INSTALLING DOUBLER. NR 3 L/E SLAT, DAMAGE FOUND AT SHOP INSPECTION. 2L73 4F A3WE 19950331005141995033100514NM 1995 3 31 DL72S951121 119950315A5312 STIFFENER BOEING727 727232 1384082NM 1183 BULKHEAD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11469DA 20746 FOUND DURING B-2 LETTER CHECK, 1 INCH CRACK AT VERTICAL STIFFENER ON 1183 BULKHED LWR RADIUS BLOCK. INSTALLED DOUBLER PER N.N. 53-11-0 PG 811. 2L73 4F A3WE 19950331005151995033100515NM 1995 3 31 DL72S951124 119950221A5754651622195 SLAT BOEING727 727232 1384082NM NR 4 LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 INSPECTION FOUND NUMEROUS CRACKS AROUND MOUNT HOLES FOR FENCE IN THE NR 4 LE ADING EDGE SLAT. REPAIRED HOLES PER MM 57-54-0. 2L73 4F A3WE 19950331005161995033100516NM 1995 3 31 DL72S951134 119950311A5754651622295 SLAT BOEING727 727232 1384082NM NR 3 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 NR 3 SLAT, CRACK IN UPPER CORNER OF OPENING IN SPAR FOR TEE DUCT. INSTALLED DOUBLER PER M/M 57-54-0 FIG 810. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950331005171995033100517NM 1995 3 31 DL72S951137 119950316A5754 SLAT BOEING727 727232 1384082NM NR 2 LE CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11402DA 21146 FOUND DURING E-1 LETTER CHECK, 2 INCH BY .25 INCH CRACKS BELOW ANTI-ICE TUBE ON NBR 2 L/E SLAT. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950331005181995033100518NM 1995 3 31 DL72S951138 119950316A5320 WEB BOEING727 727232 1384082NM FS 1223/1323 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11404DA 21148 FOUND DURING E-1 LETTER CHECK, 3 LIGHTNING HOLES CRACKED VERTICAL WEB LT TORQUE BOX STA 1223, 1 EA LIGHTNING HOLE CRACKED VERTICL WEB RT TORQUE BOX 48 SEC STA 1323. REPAIRED PER M/M 53 -11 - 0 PG 828. 2L73 4F A3WE 19950331005191995033100519NM 1995 3 31 DL72S951139 119950316A5530 SKIN BOEING727 727232 1384082NM VERT STAB CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11402DA 21146 FOUND DURING E-1 LETTER CHECK, SKIN CRACKED .5 INCH VERTICAL STAB LT SIDE BELOW ACCESS PNL 9501. REPAIRED PER SRM 55-30-3 FIG 1. 2L73 4F A3WE 19950331005201995033100520NM 1995 3 31 DL72S951140 119950202A5755 PANEL 651734781A BOEING727 727232 1384082NM SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 727 20747 LARGE DELAMINATION LOWER SKIN, ON WING SPOILER PANEL. MADE BONDED REPAIR PER 727 SRM 57-50-6 DAMAGE FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950331005211995033100521NM 1995 3 31 DL72S951146 119950114A5754 RIB 65162295 BOEING727 727232 1384082NM LT NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA BN380 21433 DURING SHOP INSPECTION, RIB AT ACTUATOR FITTING WAS FOUND CRACKED ON L/WING NR 3 L/E SLAT. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950331005221995033100522NM 1995 3 31 DL72S951147 119950314A5240 DOOR BOEING727 727232 1384082NM FWD SVC DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 FOUND DURING CV-2 L/O CHK, .5 INCH CRACK IN FWD SVC DOOR FWD UPPER CORNER. REPAIRED PER MM 52-12-0 PG 808. 2L73 4F A3WE 19950331005231995033100523NM 1995 3 31 DL72W950996 119950309A5754 SLAT 651622291 BOEING727 727247 138408FNM NR 4 LT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W BN1047 20869 DURING INSPECTION, LEFT WING NR 4 SLAT WAS FOUND WITH CRACKING IN SUPPORT WEB FOR SPADE FITTINGS. 2L73 4F A3WE 19950331005241995033100524NM 1995 3 31 DL72W951007 119950310A5754 SLAT BOEING727 727247 138408FNM NR 4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 2 INCH SPIDER CRACK ON IB LWR CORNER OF NR 4 LE FLAP. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 57-53-0 PG 804. 2L73 4F A3WE 19950331005251995033100525NM 1995 3 31 DL72W951008 119950310A5753 FOREFLAP BOEING727 727247 138408FNM NR 4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 1 INCH CRACK ON NR 4 FOREFLAP ABOVE NR 8 FLAP TRACK. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 57-50-4 FIG 1. 2L73 4F A3WE 19950331005261995033100526NM 1995 3 31 DL72W951009 119950310A5320 WEB BOEING727 727247 138408FNM 48 SEC R/H SIDE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 2 LIGHTNING HOLES HAVE .25 INCH CRACKS IN FLANGE AT VERT WEB BELOW AIRSTAIR ACT. FOUND DURING B-1 LETTER CHECK TPAMM. REPAIRED PER MM 53-11-0 PG 828. 2L73 4F A3WE 19950331005271995033100527NM 1995 3 31 DL72W951015 119950310A5754 SLAT ANGLE BOEING727 727247 138408FNM NR 6 O/B CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 FOUND ON LTR CK, NR 6 POS L/E SLAT S/N BN105 HAS A 2 INCH CRACK AT O/B STOP PAD LWR COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0 PG 816. 2L73 4F A3WE 19950331005281995033100528NM 1995 3 31 DL72W951086 119950306A5315 BEAM BOEING727 727247 138408FNM STA 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 DURING HMV, FOUND FLOOR BEAM AT STA 400 CORRODED. REPAIRED PER SRM 53-10-8 PG 24 FIG 1. 2L73 4F A3WE 19950331005291995033100529NM 1995 3 31 DL72W951090 119950306A5313 STRINGER BOEING727 727247 138408FNM STA 680-700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 DURING HMV FOUND STR SPLICE CORRODED STR 26L, STA 680-700. REPLACED SPLICE PER SRM 53-10-3. 2L73 4F A3WE 19950331005301995033100530NM 1995 3 31 DL72W951092 119950308A5315 FLOOR BEAM BOEING727 727247 138408FNM STA 344/1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 DURING HMV, FOUND FLOOR BEAMS CORRODED AT STA 344 AND 1030. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950331005311995033100531NM 1995 3 31 DL72W951105 119950310A5320655612573 WEB BOEING727 727247 138408FNM FS 950E S26R CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 DURING INSPECTION AT HMV, THE C-2 DOOR CUTOUT FRAME AT FS 950E WAS FOUND CRACKED IN BOTH THE WEB AND THE INBD CHORD ABOVE S26R. THE CRACK ON THE CHORD IS IN THE RADIUS OF THE CHORD AND IS APPROX .375 INCH LONG RUNNING FWD AND AFT. ALSO, THERE WAS A WORN AREA AT THE CRACK LOCATION OF THE INBD CHORD. IN ACCORDANCE WITH BAC S/B 727-53A0199 REV 1, THE CHORD WAS SPLICED AND REPAIRED. THE WEB WAS REPAIRED PER E.O. 4-61247-12. 2L73 4F A3WE 19950331005321995033100532NM 1995 3 31 DL72W951106 119950310A5311655612671 FRAME BOEING727 727247 138408FNM FS 990 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 DURING INSPECTION AT HMV, THE FRAME AT STATION 990 WAS FOUND TO HAVE BOTH CORROSION ON BOTH THE VERTICAL AND HORIZONTAL FLANGES OF THE INBD CHORD BETWEEN S-27R AND S-26R. THE CORROSION EXTENDS OVER APPROXIMATELY 3 INCHES ON THE HORIZONTAL FLANGE. IN ACCORDANCE WITH BAC S/B 727-53A0199, REV 1, THE DAMAGE WAS CUT OUT AND SPLICED, PER ERA 301310-14AD. 2L73 4F A3WE 19950331005331995033100533NM 1995 3 31 DL72W951107 119950311A5330 SKIN BOEING727 727247 138408FNM FS 680 STR 27R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 DURING INSPECTION AT LETTER CHECK, CORROSION WAS FOUND ON THE SKIN AND STRINGER AT STATION 680, STR 27R. AN EXISTING REPAIR DOUBLER WAS ALSO REMOVED FROM THE SKIN AT STR 28R. THE SKIN CUTOUT AT STR 27R IS APPROXIMATELY 4.375 INCH BY 1.75 INCH AND THE CUTOUT AT STR28 R IS 2 INCHES BY 1.375 INCH. PER B727 SRM 53-10-3, FIG. 1, THE EXISTING REPAIR WAS REPLACED WITH A LARGER REPAIR TO COVER BOTH DAMAGED AREAS. 2L73 4F A3WE 19950331005341995033100534NM 1995 3 31 DL72W951108 119950311A532069678811 BEAM BOEING727 727247 138408FNM FS 1273 RT TORQ CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 DURING LETTER CHECK INSPECTION, THE RT UPPER TORQUE BOX UPPER AFT TRANSVERSE BEAM AND GUSSET ANGLE AT FS 1273 WERE FOUND CRACKED. PER BAC S/B 727-53-0129, REV A, BOTH THE BEAM AND GUSSET ANGLE WERE REPLACED. 2L73 4F A3WE 19950331005351995033100535NM 1995 3 31 DL72W951141 119950121A5753 SKIN 6521630251K BOEING727 727247 138408FNM NR 2 FORE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA BN15 22111 HOLE IN LOWER SKIN, SEVERAL AREAS IN UPPER AND LOWER SKIN T/E ARE DELAMINATED. NR 2 FORE FLAP AT SHOP INSPECTION. MADE BONDED REPAIR PER 727 SRM 57-50-4. 2L73 4F A3WE 19950331005361995033100536NM 1995 3 31 DL72W951157 119950314A5713 FLANGE BOEING727 727247 138408FNM RT WING STA 656 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND FLANGE CRACKED AT RT WS 656.5 AT UPPER STR 4. REPAIRED ANGLES AND PARTS PER MM 57-13-0 FIG 804. 2L73 4F A3WE 19950331005371995033100537NM 1995 3 31 DL72W951159 119950306A5313 STRINGER BOEING727 727247 138408FNM STR 27 R FS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND STR 27R CORRODED AT STA 740 AFT BB. FABRICATED AND INSTALLED PART PER SRM 53-10-3. 2L73 4F A3WE 19950331005381995033100538NM 1995 3 31 DL72W951160 119950306A5315 CAP BOEING727 727247 138408FNM FS 420 FLR BEAM CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV, FOUND LWR SURFACE OF UPPER CAP CORRODED AT FS 420 FLOOR BEAM. DRILLED AND REPLACED SECTION PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950331005391995033100539NM 1995 3 31 DL72W951161 119950304A5313 STRINGER BOEING727 727247 138408FNM STA 720 B-C CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND STA 720 B-C STR TIPS CRACKED LEFT SIDE. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950331005401995033100540NM 1995 3 31 DL72W951162 119950304A5313 STRINGER BOEING727 727247 138408FNM STA 720 B-C CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND STRINGER CRACKED AT FS 720 WING LT BOX. FABRICATED SPLICE PER SRM 53-10-3. 2L73 4F A3WE 19950331005411995033100541NM 1995 3 31 DL72W951163 119950314A5751 AILERON BOEING727 727247 138408FNM LT WING INBD GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND LWR SKIN GOUGED/DENTED LT WING INBD AILERON. REMOVED DAMAGE AND FABRICATED REPAIR PER SRM 57-50-5. 2L73 4F A3WE 19950331005421995033100542NM 1995 3 31 DL72W951165 119950308A5754 RIB BOEING727 727247 138408FNM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND NR 1 SLAT NR 1 RIB CRACKED AT LWR CLOSEOUT ANGLE. REMOVED AND INSTALLED PER MM 57-54-0. 2L73 4F A3WE 19950331005431995033100543NM 1995 3 31 DL72W951167 119950308A5754 RIB BOEING727 727247 138408FNM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND NR 1 SLAT, NR 2 RIB CRACKED AT LWR CLOSEOUT ATTACH ANGLE. REMOVED DAMAGED AREA AND MANUFACTURE REPAIR PER MM 57-40-0 PG810. 2L73 4F A3WE 19950331005441995033100544NM 1995 3 31 DL72W951168 119950308A5754 RIB BOEING727 727247 138408FNM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND NR 1 SLAT, NR 2 RIB CRACKED AT UPPER RADIUS. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER MM 57-54-00. 2L73 4F A3WE 19950331005451995033100545NM 1995 3 31 DL72W951169 119950305A5713 STRINGER BOEING727 727247 138408FNM RT WING STA 656 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND WING STA 656.5 STR FLANGE CRACKED ON OB END. DRILLED REPAIR AND INSTALLED REPAIR PER MM 57-13-0 PG 801. 2L73 4F A3WE 19950331005461995033100546NM 1995 3 31 DL72W951170 119950314A5313 STRINGER BOEING727 727247 138408FNM 26RT STA 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV FOUND CORROSION ON STR 26R AT STA 740 FWD BB. TRIMMED AND DRILLED UP STR SPLICE PER SRM 53-10-3. 2L73 4F A3WE 19950331005471995033100547NM 1995 3 31 DL73E951125 119950228A71106585378395 NOSE COWL BOEING737 737247 138448DNM NR 2 ENG WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11382DL 23609 AFT BULKHEAD DOOR FRAME LIP WORN AT 7 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3. FOR NR 2 ENGINE INTAKE COWL, DAMAGE FOUND AT SHOP INSPECTION. 2L72 4F A16WE 19950331005481995033100548NM 1995 3 31 DL73S951104 119950312A5320651841483 WEB BOEING737 737232 1384475NM NOSE W/W FS270 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11311DL 23083 DURING INSPECTION, A 6 INCH CRACK WAS FOUND AT THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL AT STATION 270. IN ACCORDANCE WITH S/B 727-53-145, THE WEB WAS TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED. 2L72 4F RTA16WE 19950331005491995033100549NM 1995 3 31 DL73S951109 119950222A5330 SKIN BOEING737 737232 1384475NM FS 480,STR 26R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11310DA 23082 DURING HMV INSPECTION, THE SKIN AT STA 480 WAS FOUND CORRODED IN TWO LOCATIONS BETWEEN STR 26R-28R. THE DAMAGE CONSISTED OF A 1.125 INCH CUTOUT NEAR STR 27R AND A 3.25 INCH BY 2.5 INCH CUTOUT AT THE STA 480 BUTT SPLICE. IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 3A AND DER APPROVAL, AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLED. 2L72 4F RTA16WE 19950331005501995033100550NM 1995 3 31 DL757951073 119950305A5730 PLATE OPENINGS BOEING757 757232 1384965NM RT WING LWR SKINCORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 AT HMV, FOUND ALL TANK PLATE OPENINGS IN RT WING LOWER SKIN TO HAVE FRETTING WEAR AND CORROSION. REMOVED CORROSION AND FRETTING DAMAGE PER SRM 57-20-01. ROTO PEENED TANK PLATE OPENINGS PER SRM 57-20-01. DYE CHECKED PER SRM 57-20-01. NO CRACKS FOUND. 2L72 4F RTA2NM 19950331005511995033100551NM 1995 3 31 DL757951075 119950305A5330 SKIN BOEING757 757232 1384965NM STA 520 S-10L LIGHTNING DAMAGEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11610DL 22817 DURING HMV, INSPECTION FOUND UPPER FUSELAGE SKIN AREA AT STATION 520 STRINGER 10L TO BE BURNISHED BEYOND LIMITS, .25 INCH LIGHTNING STRIKE. REPAIRED PER SRM 53-00-01. 2L72 4F RTA2NM 19950331005521995033100552NM 1995 3 31 DL757951100 119950314A5320 INTERCOSTAL BOEING757 757232 1384965NM FS 365 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11659DL 24421 FOUND ON F-1 LETTER CHECK, INTERCOASTAL STRAP CRACKED BELOW FLOOR BEAMS FS 365 LEFT TUNNEL INSIDE E/E COMPT. REPAIRED PER SRM 53-10-51. 2L72 4F RTA2NM 19950331005531995033100553NM 1995 3 31 DL757951150 119950316A5330 SKIN BOEING757 757232 1384965NM UPPER FUSELAGE LIGHTING STRIKE A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11666DN 25034 FOUND DURING LETTER CHECK, SEVERAL LIGHTNING STRIKES UPPER FUSELAGE BELOW SKY RADIO ANTENNA AND ALONG STRINGER 3L. REPAIRED PER SRM 53-00-01 FIG 207. 2L72 4F RTA2NM 19950331005541995033100554NM 1995 3 31 DL757951152 119950316A5330 SKIN BOEING757 757232 1384965NM UPPER FUSELAGE LIGHTING STRIKESA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11666DN 25034 FOUND DURING LETTER CHECK INSPECTION SEVERAL LIGHTNING STRIKES UPPER FUSELAGE IN AREA OF UPPER ANTI-COLLISON LIGHT FS 420 FS 580 FS 620 FS 690 REPAIRED FS 580 620 690 PER SRM 53-00-01 PERMANENT REPAIR FS 420 HAS TEMP REPAIR OF BLIND FASTENER PER SRM 53-00-01. 2L72 4F RTA2NM 19950331005551995033100555NM 1995 3 31 DL757951154 119950308A5315 FLOOR BEAM BOEING757 757232 1384965NM STA 377 LBL54 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 DURING HMV, INSPECTION FOUND FLOOR BEAM CORRODED AT STA 377 LBL 54 AT FASTENER HOLES. REPAIRED PER SRM 53-10-51. 2L72 4F RTA2NM 19950331005561995033100556NM 1995 3 31 DL767951148 119950314A5753113T131606 FLAP BOEING767 767232 1385132NM O/B FLAP LE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11110DL 22222 NR 7 INTERM REPAIR TO L/E OF O/B FLAP JUST I/B OF THE NBR 8 FLAP DRIVE IS DELAMINATED. 2L72 4F RTA1NM 19950331005571995033100557NM 1995 3 31 DL767951153 119950317A5753 FLAP BOEING767 767232 1385132NM NBR 1 LE CAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11102DA 22214 FOUND DURING O-2 CHECK, NR 1 FLAP L/E CAP DAMAGED 2 PLACES. INSTALLED PERMANENT REPAIR AS PER SRM 51-70-03 FIG 201. 2L72 4F RTA1NM 19950331005581995033100558WP 1995 3 31 DLL10950993 119950309A5720 ANGLE LKHEED1011 10113851 5265010WP LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11730DA 193C1199 LEFT T/E BAT STRUCTURE LWR CAP AT ITES 275.00 APPROX 13 INCHES OUTBD OF OUTBD HINGE FITTING NBR 2 SPOILER LWR CAP HAS A 2 INCH CRACK GOING THROUGH FASTENER HOLE. 2L73 4F A23WE 19950331005591995033100559WP 1995 3 31 DLL10951058 119950313A7110 COWL DOUBLER LKHEED1011 10113851 5265010WP NR 2 ENGINE LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11712DA 193C1088 FLUSH PATCH REPAIR COMING LOOSE ON OUTER SKIN OF TRANSLATING COWL AT 4 O'CLOCK POSITION. ON NR 2 ENGINE. FOUND AT LETTER CHECK, REPAIRED PER SRM 54-37-00 FIG 802. 2L73 4F A23WE 19950331005601995033100560WP 1995 3 31 DLL10951120 119950313A5313 STRINGER LKHEED1011 10113851 5265010WP STR 29 STA 1625 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11712DA 193C1088 STR 29 CRACKED OUT OF DRAIN HOLE UNDER SPLICE DOUBLER BETWEEN STA 1625-1645, FOUND DURING LETTER CHECK. REMOVED CRACKED SECTION AND FABRICATED NEW STRG SECTION AND SPLICE DOUBLERS AS PER SRM 53-13-00 FIG 804. OK TO INSTALL STRINGER REPLACEMENT. INSTALLED STRINGER AND SPLICE DOUBLERS. 2L73 4F A23WE 19950331005611995033100561WP 1995 3 31 DLL10951142 119950313A5280 DOOR LKHEED1011 10113851 5265010WP LT MLG STRUT CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11712DA 193C1088 LEFT MLG STRUT DOOR LOWER DOOR, CRACKED AT LOWER AFT SIDE. REPAIRED PER SRM 52-81-00 PG 811, FOUND AT LETTER CHECK. 2L73 4F A23WE 19950331005621995033100562NM 1995 3 31 DLM88951006 119950310A5311 FRAME DOUG MD88 MD88 3023688NM L/H W/W CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11967DL 53116 CRACK IN W/W AFT JAMB AFT ANGLE. FOUND DURING E-1 LETTER CHECK. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950331005631995033100563NM 1995 3 31 DLM88951079 119950314A5330 SKIN DOUG MD88 MD88 3023688NM R/H NLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11976DL 53257 FOUND ON D-2 LETTER CHECK, .375 INCH CRACK AT RT NLG WHEEL WELL AFT DOOR HINGE CUTOUT. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950331005641995033100564NM 1995 3 31 DLM88951081 119950314A5415 ATTACH ANGLE. DOUG MD88 MD88 3023688NM LT ENG PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11976DL 53257 FOUND ON D-2 LETTER CHECK, CRACK AT LEFT ENG PYLON TO FUSELAGE ATTACH ANGLE. REPAIRED PER SRM 54-04A FIG 4. 2L72 4F RTA6WE 19950331005651995033100565NM 1995 3 31 DLM88951085 119950307A5210 HORIZ BEAM DOUG MD88 MD88 3023688NM R-1 DR FWD EDGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 DURING HMV, FOUND R-1 DOOR HORIZONTAL BEAM CRACKED. AT FWD EDGE LWR HINGE PIVOT FITTINGS NEXT TO EXTERIOR SKIN. VISIBLE THROUGH LOWER FWD CORNER LIGHTENING HOLE. REPAIRED PER SRM 52-05. 2L72 4F RTA6WE 19950331005661995033100566NM 1995 3 31 DLM88951114 119950314A5754 RIB 5922532505 DOUG MD88 MD88 3023688NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 ON THE NR 2 SLAT 37, THE LOWER SKIN HAD TO BE REMOVED TO GAIN ACCESS TO A DAMAGED RIB. A SKIN SPLICE WAS COMPLETED PER THE SRM 57-09 TO REINSTALL THE LOWER SKIN. 2L72 4F RTA6WE 19950331005671995033100567NM 1995 3 31 DLM88951116 119950315A5320 FRAME DOUG MD88 MD88 3023688NM LT WHEEL WELL CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11911DL 49542 FOUND ON B-1 LETTER CHECK, CRACK AT OUTBD FWD WHEEL WELL FRAME. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950331005681995033100568NM 1995 3 31 DLM88951136 119950316A5320 RIB DOUG MD88 MD88 3023688NM RT WHEEL WELL CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11997DL 53364 FOUND DURING C-2 LETTER CHECK, CRACK IN CROSSOVER RIB AT AFT I/B CORNER OF RT WHEEL WELL CUTOUT. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950331005691995033100569WP 1995 3 31 SCNA95046 119950326A7603C803833 CONTROL CABLE DOUG DC10 DC1010 3022110WP NR 2 ENG THROTT BINDING A SCNAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 GL15SEDHT 47833 AIRCRAFT WAS CRUISING AT FLIGHT LEVEL 370 WHEN DESCENDING POWER ON NR 2 ENGINE WOULD NOT RETARD BELOW 93 PERCEHT N1, 89 PERCENT N2, FF 5200. NR 2 WOULD NOT ADVANCE OR RETARD. CONTINUED TO TRY TO MOVE THROTTLE UNTIL FL 180. SECURED NR 2 ENGINE AT FL 180, COMPLIED WITH EMERGENCY AND COM CHECK LISTS. FOUND NR 2 ENGINE THROTTLE CABLE TELEFLEX PORTION BINDING. CLEANED AND LUBED TELEFLEX AT ENGINE END AND AT THROTTLE DRUM END. OPERATIONAL CHECK GOOD THROUGH SEVERAL TIMES, NO BINDING NOTED AT THIS TIME. WORK ACCOMPLISHED PER DC10 MM 76-11-01. 2L73 4F A22WE 19950331005701995033100570WP 1995 3 31 SCNA95047 119950327A217020D103 COALESCER BAG DOUG DC10 DC1010 3022110WP NR 1 PACK FAULTY A SCNAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15571SC 46645 ON THE GROUND IN DFW, WHEN NR 1 PACK WAS TURNED ON USING ONLY THE APU, A VISIBLE HAZE AND FUMES WERE NOTICED IN THE COCKPIT AND LOWER GALLEY. REMOVED AND REPLACED COALESCER BAG IAW MM 21-54. RAN PACKS FOR 30 MINUTES AT VARIOUS TEMP SETTINGS, NO ODOR OR FUMES NOTED. 2L73 4F A22WE 19950331005711995033100571NM 1995 3 31 SCNA95048 119950326A326065253981 WARNING SWITCH BOEING727 7272A1 138407FNM NOSE GEAR DOORS INTERMITTENT A SCNAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15286SC 21601 NOSE GEAR DOOR LIGHT STAYED ON AFTER TAKEOFF. DUMPED 17, 500 LBS OF FUEL AND RETURNED TO ORD. FOUND INTERMITTENT NOSE GEAR DOOR WARNING SWITCH. REMOVED AND REPLACED NOSE GEAR DOOR WARNING SWITCHES. GEAR DOOR WARNING SYSTEM OPS CHECK GOOD IAW 727 MM 32-62-11. 2L73 4F A3WE 19950331005721995033100572 1995 3 31 LOSA9512 419950213A3418543026 STALL COMPUTER FRCHLDSA227 SA227CC SW LEFT MALFUNCTIONED A LOSAO OTHER N FALSE WARNING CRCRUISE 1 WP233022R1909 CC841B PILOT REPORTED STICKSHAKER BRIEFLY ENGAGED IN FLIGHT ABOVE 200 KNOTS AND ALSO ENGAGED BRIEFLY DURING FLIGHT ABOVE STALL SPEED. MAINTENANCE REPLACED LEFT STALL VANE ASSY FOR EXCESSIVE UNADJUSTABLE VOLTAGE, REPLACED SAS CONTROL BOX AND LT SAS COMPUTER. OPERATIONAL CHECKS NORMAL PER MM 27-30-30. AIRCRAFT HAS TEST FLIGHT AFTER MAINTENANCE. RESULTS SATISFACTORY, AIRCRAFT RELEASE FOR SERVICE. (Z) 1L72 4T RTA18SW 19950331005751995033100575NM 1995 3 31 ASAA9510009 119950305A521065298251 ROD BOEING737 737290C 138448VNM L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01730AS 22577 SEA - FLT 61 - PRIOR TO DEPARTURE, THE CREW REPORTED L1 DOOR WAS DIFFICULT TO CLOSE. ADJUSTED UPPER DOOR HINGE ROD AND DOOR OPERATED NORMALLY. (W) 2L72 4F A16WE 19950331005761995033100576NM 1995 3 31 ASAA9510010 119950306A33501060091101 EEL ASSY BOEING737 737210C 1384459NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT OVER THE L2 AIRSTAIR DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F A16WE 19950331005771995033100577NM 1995 3 31 ASAA9510011 119950309A3350RPS1B EEL BATT CHARGER BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - DURING MAINTENANCE CHECK, THE R-2 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A16WE 19950331005781995033100578NM 1995 3 31 ASAA9540003 119950226A3230BACC2C4C00996EG CONTROL CABLE BOEING737 7374Q8 NM LANDING GEAR OUT OF ADJ A ASAAO OTHER J WARNING INDICATION LDLANDING 1 NM01773AS 25106 LAX - FLT 88 - ON ARRIVAL, CREW REPORTED ALL THREE RED INTRANSIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR EXTENSION DURING APPROACH. RECYCLED GEAR AND RED LIGHTS EXTINGUISHED NORMALLY WHEN GEAR WAS EXTENDED. LANDED WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL CABLES OUT OF TOLERANCE. RERIGGED PER THE MM AND OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950331005791995033100579NM 1995 3 31 ASAA9540006 119950303A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01780AS 25112 SEA - DURING CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 22 TO 26. MAINTENANCE SECURED LOOSE CONNECTION AT ROW 26. (W) 2L72 4F RTA16WE 19950331005801995033100580NM 1995 3 31 ASAA9540007 119950308A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 SEA - DURING CHECK, FOUND LAST 5 FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED LOOSE WIRING AND FUNCTION CHECKED NORMAL. (W) 2L72 4F RTA16WE 19950331005811995033100581WP 1995 3 31 ASAA9580038 119950302A5347TMS6019943 SEAT TRACK DOUG DC9 DC983 3022083WP BS 261 GOUGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01944AS 53019 PAE - DURING 15K CHECK, GOUGE WAS FOUND ON SEAT TRACK AT Y261, X-46, Z-0. REMOVED GOUGED SEAT TRACK. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05. (W) 2L72 4F RTA6WE 19950331005821995033100582WP 1995 3 31 ASAA9580039 119950304A3350S103 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950331005831995033100583WP 1995 3 31 ASAA9580040 119950305A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01934AS 49235 SEA - DURING MAINTENANCE CHECK, BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950331005841995033100584WP 1995 3 31 ASAA9580041 119950305A3350081691 EEL SOCKET DOUG DC9 DC983 3022083WP CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE FWD 3 EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BROKEN LIGHT SOCKET AND STRIP. LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950331005851995033100585WP 1995 3 31 ASAA9580042 119950306A323059164605509 CNTL VALVE DOUG DC9 DC983 3022083WP LANDING GEAR DEFECTIVE A ASAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 NM01946AS 49658 PDX - FLT 561 - ON ARRIVAL, THE CREW REPORTED THE LANDING GEAR DID NOT EXTEND DURING APPROACH, ALL GEAR POSITION LIGHTS WERE RED AND GEAR WARNING HORN ON. ACCOMPLISHED GO-AROUND AND LANDING GEAR EXTENDED NORMALLY ON SECOND APPROACH. REPLACED THE LANDING GEAR CONTROL VALVE AND ACCOMPLISHED GEAR SWING, LANDING GEAR OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950331005861995033100586WP 1995 3 31 ASAA9580043 119950307A335060030431 EEL BATT PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS 49104 OAK - DURING MAINTENANCE CHEK, THE AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950331005871995033100587WP 1995 3 31 ASAA9580044 119950308A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT AT ROW 14 WAS FOUND INOPERATIVE. SECURED LOOSE GROUND WIRE AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A6WE 19950331005881995033100588WP 1995 3 31 ASAA9580045 119950309A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK THE L-2 DOOR EXIT IDENTIFIER LIGHT WAS FOUND INOPERATIVE. SECURED LOOSE GROUND WIRE AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A6WE 19950331005891995033100589WP 1995 3 31 ASAA9580049 119950314A5320 SHEAR TIE DOUG DC9 DC983 3022083WP BS 1174 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01942AS 53052 PAE - DURING 15K CHECK, CORROSION WAS ON SHEAR TIE AT Y1174, X PLUS 11 TO X-3, Z-49 FROM LONGERON 29L TO 30, AND ON FRAME X PLUS 34, Z-40. REMOVED CORRODED SHEAR TIE. FABRICATED AND INSTALLED NEW PIECES IAW DC-9 SRM 51-01 PG 1 AND 2, 51-10-04 PG 1, 51-10-03 PG 15 TO 23, 51-30-02 PG 1 AND 2, 51-30-05 PG 1-2A, 53-01 PG 3 TO 5. (W) 2L72 4F RTA6WE 19950331005901995033100590WP 1995 3 31 ASAA9580050 119950314A5311 FRAME DOUG DC9 DC983 3022083WP BS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01942AS 53052 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1231, X PLUS 15 TO X-14, Z-48 AND ON STRAP ON TOP OF THE FRAME. REPAIRED FRAME, FABRICATED AND INSTALLED FRAME STRAP IAW DC-9 SRM 53-03 PG 2A, 51-30-05 PG 1 TO 3, 51-10-04 PG 1 TO 3, 51-30-05 PG 1 TO 3. (W) 2L72 4F RTA6WE 19950331005911995033100591WP 1995 3 31 ASAA9580051 119950314A5311 FRAME DOUG DC9 DC983 3022083WP BS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01942AS 53052 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1250, X-15, Z-47 AND ON STRAP ON TOP OF THE FRAME AT X PLUS 7, Z-47. REMOVED CORRODED SECTION OF FRAME. FABRICATED AND INSTALLED NEW PIECES IAW DC-9 SRM 53-03 PG 1-4J, 53-14-03 PG 24H-26, 51-10-03 PG 15 AND 51. (W) 2L72 4F RTA6WE 19950331006171995033100617 1995 3 31 95ZZZX1486 419950222A237089094003211 CVR BDINST LKHEED1329 132923E 5263116SO COCKPIT FAIL-TO-TEST A MDGAK NONE L NO TEST ININSP/MAINT 1 SO0926MJ A01508 5101 CVR TOTAL TIME ON UNIT SINCE LAST REPAIR IS 358 FLIGHT TIME. UNIT FAILS PUSH-TO-TEST FUNCTION. 2L74 4J 2A15 19950331006221995033100622SW 1995 3 31 95ZZZX1491 119950307A3231016A39291 BOLT 010A3913131 MTSBSIMU2 MU2B20 5780407SW NLG DOOR SHEARED A KKFAO OTHER O OTHER CLCLIMB 1 GL2366CL A1055 135 NOSE GEAR DOORS FAILED TO OPEN ON GEAR RETRACTION. THE NOSE GEAR DOORS WERE CRUSHED AND THE GEAR DOWNLOCK MECHANISM WAS DAMAGED. THE NOSE GEAR COLLAPSED ON LANDING ROLL-OUT. THE TWO BOLTS THAT OPERATE THE NOSE GEAR DOORS IN CONJUNCTION WITH GEAR RETRACTION HAD SHEARED DUE TO THE DOORS BINDING, POSSIBLY FROM SNOW AND SLUSH. 1H72 3T A2PC 19950331006281995033100628SW 1995 3 31 95ZZZX1497 119950304A6720206001713001 SUPPORT BELL 206 206L 1181522SW T/R PEDAL CORRODED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11 20249 WHILE REFURBISHING TWO BELL 206L AIRCRAFT, EACH WITH 20248.9 AND 21315,2 AIRCRAFT TT, IT WAS NOTED THAT THE T/R PEDAL SUPPORTS WERE CORRODED. THIS CORROSION WAS ALONG THE ENTIRE MATING SURFACE AND AROUND THE BOLT ATTACHMENT EARS OF EACH SUPPORT. SOME CORROSION WAS ALSO NOTED ON THE AIRFRAME MATING SURFACE. NEW YORK HELICOPTER BELIEVES THE CORROSION NOTED ON THE SUPPORTS AND AIRFRAME SURFACES WAS DUE TO MOISTURE AND THE LONG PERIOD OF TIME THE SUPPORTS HAVE BEEN IN SERVICE, THE SUPPORTS ARE ORIGINAL TO THE AIRCRAFT. REPLACED LEFT AND RIGHT PEDAL SUPPORTS IAW BELL 206-L MM. 1G71 3U H2SW 19950331006291995033100629SW 1995 3 31 95ZZZX1498 119950304A6720206001713001 SUPPORT BELL 206 206L 1181522SW T/R PEDAL CORRODED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11 21315 WHILE REFURBISHING TWO BELL 206L AIRCRAFT, EACH WITH 20248.9 AND 21315,2 AIRCRAFT TT, IT WAS NOTED THAT THE T/R PEDAL SUPPORTS WERE CORRODED. THIS CORROSION WAS ALONG THE ENTIRE MATING SURFACE AND AROUND THE BOLT ATTACHMENT EARS OF EACH SUPPORT. SOME CORROSION WAS ALSO NOTED ON THE AIRFRAME MATING SURFACE. NEW YORK HELICOPTER BELIEVES THE CORROSION NOTED ON THE SUPPORTS AND AIRFRAME SURFACES WAS DUE TO MOISTURE AND THE LONG PERIOD OF TIME THE SUPPORTS HAVE BEEN IN SERVICE, THE SUPPORTS ARE ORIGINAL TO THE AIRCRAFT. REPLACED LEFT AND RIGHT PEDAL SUPPORTS IAW BELL 206-L MM. 1G71 3U H2SW 19950331006371995033100637WP 1995 3 31 9504989914 119950328A5744 FITTING DOUG DC9 DC931 3022065WP FLAP HINGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01964N 47416 DURING PERIODIC CHECK, FOUND CORROSION ON THE NR 3 RIGHT FORWARD FLAP HINGE FITTING. REPLACED FITTING PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950331006381995033100638WP 1995 3 31 9504999914 119950328A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE DEFECTIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01964N 47416 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. REPLACED TAILCONE. CHECKED OK. 2L72 4F A6WE 19950331006391995033100639WP 1995 3 31 9505009760 119950325A7711 LINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 1 ENG PT7 CRACKED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01760NW 47288 676179 NR 1 ENGINE EPR INDICATION WAS LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED A CRACKED PT7 LINE. THE SYSTEM CHECKED OK ON RUN-UP. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950331006401995033100640NM 1995 3 31 9505016615 119950324A5320 STIFFENER BOEING747 747251B 1384892NM FUS 1241 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 20360 DURING PERIODIC CHECK, THE LEFT WHEELWELL VERTICAL STIFFENER AT FS 1241 BULKHEAD WAS FOUND CRACKED. FABRICATED REPAIR AND INSTALLED. 2L74 4F A20WE 19950331006411995033100641NM 1995 3 31 9505026631 119950324A5315 CHORD BOEING747 747251B 1384892NM FUS 460 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01631US 23111 DURING PERIODIC CHECK, THE MAIN DECK UPPER FLOOR BEAM WAS FOUND DAMAGED IN THE UPPER SURFACE OF UPPER CHORD FS 460, RBL 59. FLOOR BEAM IS MADE OF 2024-T3511 ALUMINUM. MADE REPAIR PER EA 66-97922. 2L74 4F A20WE 19950331006421995033100642NM 1995 3 31 9505035534 119950324A5755113N5502 SKIN BOEING757 757251 1384970NM SPOILERS DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01534US 24265 DURING PERIODIC CHECK, THE NR 1, NR 2, NR 10, NR 11, AND NR 12 SPOILER UPPER SKIN PANELS WERE FOUND WITH NUMEROUS AREAS OF DAMAGE AND DELAMINATION (2 INCH DIAMETER TYPICAL). INSTALLED REPAIRS PER SRM 57-70-01, FIG. 201 AND NWA EA 55-97817. 2L72 4F RTA2NM 19950331006431995033100643NM 1995 3 31 9505046603 119950329A7722 INDICATOR 38140041 BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE COCKPIT EGT DEFECTIVE A NWAAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL01603US 7103101 18780 662693 DURING CLIMB, THE NR 1 ENGINE EXPERIENCED THE EGT RUNNING INTO THE RED CAUTION AREA AND THE AIRCRAFT RETURNED TO NRT WHERE AN UNEVENTFUL LANDING WAS MADE. NO FUEL WAS DUMPED. THE INDICATOR WAS FOUND TO BE READING HIGH STATICALLY AND WAS REPLACED. A GROUND RUN-UP CONFIRMED PROPER SYSTEM OPERATION. 2L74 4F4 F A20WE E20EA 19950331006441995033100644NE 1995 3 31 95UAL757009 219950328A72301B5179 BEARING BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 SPALLED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29588UA 26717 726725 AIRCRAFT DIVERTED AND LANDED UNDER AMBER ALERT DUE TO AN OIL FILTER BYPASS LIGHT ON. THE NR 1 BEARING FAILED. FOUND HEAVY SPALLING OF THE OUTER RACE. APPEARS TO BE AN ISOLATED INCIDENT. 2L72 4F4 FRTA2NM E17NE 19950331006451995033100645NM 1995 3 31 95UAL767014 119950329A2130 PRESSURIZATION BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE COCKPIT SQUEAL NOISE A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP29661UA 27158 LOUD SQUEALING NOISE IN COCKPIT CAUSED DIVERSION. 2L72 4F4 FRTA1NM E24NE 19950331006461995033100646WP 1995 3 31 ABXA9500247 119950325A323139231583501 LINK DOUG DC9 DC932 3022066WP LT MLG O/B DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23901AX 47381 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR LINK TO HAVE EXCESSIVE PLAY. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950331006471995033100647WP 1995 3 31 ABXA9500248 119950325A3231DREMS5085 ROD END DOUG DC9 DC932 3022066WP LT MLG O/B DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23901AX 47381 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR, DOOR TO GEAR LINKAGE INBOARD ROD END WORN. REPLACED ROD END IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950331006481995033100648WP 1995 3 31 ABXA9500249 119950318A5320595603347 CHANNEL DOUG DC9 DC931 3022065WP STA. 897 - 937 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON A FLOOR SUPPORT BETWEEN STA.'S 897 THROUGH 937. REPAIRED IAW ABX REA D953-11215. 2L72 4F A6WE 19950331006491995033100649WP 1995 3 31 ABXA9500250 119950313A532049125401A FITTING DOUG DC9 DC931 3022065WP STA. 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, A VERTICAL CABIN FLOOR SUPPORT FITTING WAS FOUND CRACKED AT STA. 965, LBL 34. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 19950331006501995033100650WP 1995 3 31 ABXA9500251 119950314A531339146771 SPLICE DOUG DC9 DC931 3022065WP STA. 955 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, LONGERON 30 SPLICE WAS FOUND CRACKED AT STA. 955. REPLACED SPLICE IAW DC-9 SRM 53-02-147. 2L72 4F A6WE 19950331006511995033100651WP 1995 3 31 ABXA9500252 119950317A532099105034 CUSP DOUG DC9 DC931 3022065WP STA. 994 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, THE RIGHT CUSP TEE WAS FOUND CRACKED AT STA. 994. REPAIRED IAW ABX REA D953-11118-MR. 2L72 4F A6WE 19950331006521995033100652WP 1995 3 31 ABXA9500253 119950314A5320D0489841 WEB DOUG DC9 DC931 3022065WP STA. 960 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, RBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950331006531995033100653WP 1995 3 31 ABXA9500254 119950314A5320D0489835 WEB DOUG DC9 DC931 3022065WP STA. 960 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, LBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950331006541995033100654WP 1995 3 31 ABXA9500255 119950316A53205644324501 RETAINER DOUG DC9 DC931 3022065WP COCKPIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE LEFT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3. 2L72 4F A6WE 19950331006551995033100655WP 1995 3 31 ABXA9500256 119950315A5322DWG53AA30STC019 SUPPORT DOUG DC9 DC931 3022065WP STA. 160 - 200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND THE FLOOR PANEL SUPPORT TO HAVE A HOLE WITH SHORT EDGE DISTANCE, A DOUBLE DRILLED HOLE AND TWO HOLES WITH SHORT EDGE DISTANCE BETWEEN THEM, STA. 160 THROUGH 200, RBL 44. REPAIRED IAW ABX REA D953-11137-MR. 2L72 4F A6WE 19950331006561995033100656WP 1995 3 31 ABXA9500257 119950316A53205644324502 RETAINER DOUG DC9 DC931 3022065WP COCKPIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE RIGHT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3. 2L72 4F A6WE 19950331006571995033100657WP 1995 3 31 ABXA9500258 119950307A5280S2431215 BUSHING DOUG DC9 DC931 3022065WP RT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, THE RIGHT MAIN LANDING GEAR FLYING DOOR WAS FOUND WITH SEVERAL BUSHINGS WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950331006581995033100658WP 1995 3 31 ABXA9500259 119950307A53135920319513 LONGERON DOUG DC9 DC931 3022065WP STA. 579 - 584 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, LONGERON 29L WAS FOUND TO BE CRACKED BETWEEN STA. 579 AND 584. REPAIRED IAW ABX REA D953-11090-MR. 2L72 4F A6WE 19950331006591995033100659WP 1995 3 31 ABXA9500260 119950315A53305911407117 SKIN DOUG DC9 DC931 3022065WP STA. 209 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STA. 209 BELOW LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR. 2L72 4F A6WE 19950331006601995033100660WP 1995 3 31 ABXA9500261 119950315A5330591140733 SKIN DOUG DC9 DC931 3022065WP STA. 209 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STATION 209 ABOVE LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR. 2L72 4F A6WE 19950331006611995033100661WP 1995 3 31 ABXA9500262 119950318A5413995815957 CAP DOUG DC9 DC931 3022065WP STA YN-174 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, FOUND THE NR 1 ENGINE PYLON CLOSING RIB CAP CRACKED AT STA. YN-174. REPAIRED IAW ABX REA D954-11218-MR. 2L72 4F A6WE 19950331006621995033100662WP 1995 3 31 ABXA9500263 119950314A553059113849 CAP DOUG DC9 DC931 3022065WP VERT STABILIZER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 47552 DURING C-CHECK INSPECTION, A PREVIOUS REPAIR TO THE LEFT VERTICAL STABILIZER WAS FOUND WITH LEVEL I CORROSION. REMOVAL OF THE REPAIR REVEALED THE REAR SPAR CAP HAD BEEN SPLICED. REPAIRED IAW ABX REA D955-1116-MR. 2L72 4F A6WE 19950331006631995033100663NM 1995 3 31 DL72E951173 119950309A5320 TEE BOEING727 727247 138408FNM STA 742 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND LOWER FUSELAGE STRUCTURE TEE ANGLE CORRODED AT FORWARD HINGE AREA OF PANEL 3448 AT FS 742. REPAIRED PER MM 53-30-1 FIG 804. 2L73 4F A3WE 19950331006641995033100664NM 1995 3 31 DL72E951174 119950317A5311 FRAME BOEING727 727247 138408FNM FS 580 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND FUSELAGE FS 580 FRAME CRACKED AT STR 25L. CRACK IS IN DOUBLER ON TOP OF FRAME UPPER FLANGE. REPAIRED PER SRM 53-10-4 PG 106. 2L73 4F A3WE 19950331006651995033100665NM 1995 3 31 DL72E951176 119950301A5313 STRINGER BOEING727 727247 138408FNM FS 1154 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, STRINGER 22L WAS FOUND CORRODED AT FS 1154 ON IB FLANGE AND A SPLICE BELOW LAV DUMP CHUTE. DAMAGED AREA WAS REMOVED AND NEW SECTION WAS MFG PER SRM 53-10-3 AND INSTALLED. 2L73 4F A3WE 19950331006661995033100666NM 1995 3 31 DL72E951190 119950228A5320 WEB BOEING727 727247 138408FNM STA 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV THE WEB INSIDE VERT STAB JUST ABOVE S-DUCT WAS CRACKED AT THE LT LOWER CORNER. STOP DRILLED THE CRACK AND FABRICATED REPAIR PER SRM 53-10-4. INSTALLED REPAIR. 2L73 4F A3WE 19950331006671995033100667NM 1995 3 31 DL72E951191 119950228A5320 WEB BOEING727 727247 138408FNM STA 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV THE WEB INSIDE VERT STAB HAD 2 CRACKS IN RT LOWER CORNER AT STA 1303. STOP DRILLED CRACK AND REPAIRED PER SRM 53-10-4. 2L73 4F A3WE 19950331006681995033100668NM 1995 3 31 DL72E951192 119950317A5320 ANGLES BOEING727 727247 138408FNM STA 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THE ANGLES WERE REPAIRED PER SRM 53-10-5 FIG 10. 2L73 4F A3WE 19950331006691995033100669NM 1995 3 31 DL72E951204 119950310A5313 STRINGER BOEING727 727247 138408FNM STA 740 27R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND STRINER 27R, CORRODED AT FS 740. REPAIRED PER SRM 53-10-3 FIG. 1. 2L73 4F A3WE 19950331006701995033100670NM 1995 3 31 DL72E951207 119950321A5313 STRINGER BOEING727 727247 138408FNM STR 25R STA 1148CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND STRINGER 25 CORRODED AT FS 1148. REMOVED DAMAGED SECTION REPAIRED PER SRM53-10-3 FIG 1. 2L73 4F A3WE 19950331006711995033100671NM 1995 3 31 DL72E951208 119950227A5320 SKIN CLIP BOEING727 727247 138408FNM STA 970 IB 29R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AFT BB SKIN CLIP CORRODED STA 970 LOWER LEG OF FRAME AFT SIDE BETWEEN 30 AND 29R. REPAIRED PER MM 53-11-0 FIG 815. 2L73 4F A3WE 19950331006721995033100672NM 1995 3 31 DL72E951209 119950227A5320 SKIN CLIP BOEING727 727247 138408FNM STA 970 IB 28R CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AFT BB SKIN CLIP CORRODED STA 970 AFT SIDE BETWEEN STR 29R AND 28R. FOUND AND REPAIRED AT HMV, PER MM 53-11-0 PG 815. 2L73 4F A3WE 19950331006731995033100673NM 1995 3 31 DL72E951210 119950227A5313 STRINGER BOEING727 727247 138408FNM FS 970-990 29L CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND AFT CARGO STRINGER 29L CORRODED BETWEEN STA 970 AND 990. REPAIRED PER DL ERA 301274-14. 2L73 4F A3WE 19950331006741995033100674NM 1995 3 31 DL72L951321 119950316A2910651784983 TUBE BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11509DA 21311 DURING CRUISE, B-SYSTEM HYDRAULIC QTY WENT TO 0. FOLLOWED ABNORMAL PROCEDURES LANDED SEA. FOUND LINE FROM NR 2 CASE DRAIN AT TEMP SWITCH CRACKED. INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE THEN SCHEDULED INSTALLATION OF REPLACEMENT LINE. 2L73 4F A3WE 19950331006751995033100675NM 1995 3 31 DL72S951177 119950320A5320 SKIN BOEING727 727232 1384082NM FUSELAGE SEC 48 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11538DA 22076 FOUND DURING A-1 LETTER CHECK - 48 SEC TORQUE BOX SKIN CRACKED .3750 INCH AT A LIGHTNING HOLE RT SIDE STA 1323. INSTALLED DOUBLER PER M/M 53-11-0. 2L73 4F A3WE 19950331006761995033100676NM 1995 3 31 DL72S951179 119950320A5754 STIFFENER BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11538DA 22076 FOUND DURING A-1 LETTER CHECK - .50 INCH CRACK AT NR 6 SLAT STIFFENER AT COVE PANEL BELOW ANTI-ICE T-DUCT. REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950331006771995033100677NM 1995 3 31 DL72S951182 119950222A5754651622199 SLAT BOEING727 727232 1384082NM NR 4 LT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 UPON INITIAL INSPECTION FOUND NR 6, NR 11, AND NR 18 RIBS CRACKED. RIBS REPAIRED PER 727 M/M CH 57-54-0 BY STOP DRILLING CRACKS AND INSTALLING REPAIR DOUBLERS ON LEFT WING NR 4 L/E SLAT. 2L73 4F A3WE 19950331006781995033100678NM 1995 3 31 DL72S951199 119950208A5753652163261X FLAP BOEING727 727232 1384082NM LT I/B MID CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 NR 2 FLAP DURING HMV SHOP INSP WAS FOUND TO HAVE A CRACK IN DOULBER ON AFT SPAR 36 INCHES FROM I/B END. DOUBLER WAS REPLACED PER SMR 57-52-0 PAGE 807. 2L73 4F A3WE 19950331006791995033100679NM 1995 3 31 DL72S951200 119950208A5753652163261X FLAP BOEING727 727232 1384082NM LT I/B MID FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 NR 2 MID FLAP DURING HMV WAS FOUND TO HAVE CORROSION IN ALL FOUR O/B THRUST BEARING RETAINER BOLT HOLES. THE HOLES WERE REPAIRED PER SRM 57-50-4 PAGE 34. 2L73 4F A3WE 19950331006801995033100680NM 1995 3 31 DL72S951201 119950208A5753652163261X FLAP BOEING727 727232 1384082NM LT I/B MID FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 NR 2 MID FLAP DURING HMV WAS FOUND TO HAVE CORROSION IN ALL FOUR I/B THRUST BEARING RETAINER BOLT HOLES. THE HOLES WERE REPAIRED PER SRM 57-50-4 PAGE 34. 2L73 4F A3WE 19950331006811995033100681NE 1995 3 31 DL757951324 219950324A7321651784983 CONTROL BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE FAULTY A ADALAO OTHER Z SIGNIFICANT FAILURE REPORT LDLANDING 1 SO11655DL 24395 ON LANDING WITH SPOILERS UNARMED AND THROTTLES AT REVERSE, HAD RIGHT ROLLING MOVEMENT ON ROLLOUT. TROUBLESHOT SPOILER SYSTEM COULD NOT FIND PROBLEMS. FLIGHT DATA RECORDED SHOWED LEFT ENGINE REVERSER DEPLOYED 5 SECONDS AFTER THE RIGHT REVERSER DEPLOYED, THIS CAUSED THE RIGHT ROLLING MOVEMENT. THE LEFT EEC WAS REPLACED, REVERSER DEPLOYMENT NORMAL. 2L72 4F4 FRTA2NM E17NE 19950331006821995033100682NM 1995 3 31 DL767951203 119950320A5753 FLAP BOEING767 767232 1385132NM LT WING AFT HOLE IN SKIN A DALAK NONE O OTHER ININSP/MAINT 1 SO11108DL 22220 FOUND DURING LETTER CHECK, HOLE IN BOTTOM OF NR 2 AFT FLAP I/B. REPAIRED PER SRM 51-70-10 AND 57-53-01. 2L72 4F RTA1NM 19950331006831995033100683NM 1995 3 31 DL76S951187 119950222A7110314T1210431 COWLING BOEING767 767332 1382001NM LT ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11134DL 25123 DURING SHOP INSP THE AFT LOWER LONGERON OF THE LEFT ENGINE SIDE COWL WAS FOUND TO BE WORN AT THE HINGE FITTING AND THE HINGE FITTING WAS WORN AND BENT. A NEW SECTION WAS SPLICED IN PER SRM 54-41-02, AND THE HINGE FITTING WAS BLENDED TO ALLOWABLE LIMITS OF SRM 54-41-90. 2L72 4F RTA1NM 19950331006841995033100684WP 1995 3 31 DLL10951323 119950326A2910 HYD SYS LKHEED1011 10113851 5265010WP TAIL OVER SERVICED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11735D 193C1226 AFTER TAKOFF, HAD STRONG ODOR THROUGHOUT CABIN, ACCOMPANIED BY SMOKE ALARMS IN AFT LAVATORIES. FOUND D-SYSTEM HYDRAULIC SYSTEM OVER SERVICED CAUSING APU INTAKE AIR CONTAMIMATION. RESERVICED D-SYSTEM RETURNED TO SERVICE. 2L73 4F A23WE 19950331006851995033100685NM 1995 3 31 DLM11951178 119950318A5753 FLAP DOUG MD11 MD11 3023602NM RT T/E FLAP REQ REPAIR A DALAK NONE O OTHER ININSP/MAINT 1 SO11809DE 48480 DURING LETTER CHECK, THE RIGHT WING INBOARD TRAILING EDGE WEDGE WAS FOUND WITH TIME LIMITED REPAIR FOR DELAMINATION DAMAGE. INSTALLED PERMANENT REPAIRS PER DALA ERA 270180-14. 2L73 4F RTA22WE 19950331006861995033100686NM 1995 3 31 DLM88951184 119950321A5340 ANGLE DOUG MD88 MD88 3023688NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11929DL 49716 FOUND DURING A-1 LETTER CHECK - NR 2 PYLON UPPER SKIN TO FUSELAGE SKIN, ATTACH ANGLE WAS FOUND WITH A .75 INCH CRACK. REPAIRED PER SRM 54-04 A, FIG 4. 2L72 4F RTA6WE 19950331006871995033100687NM 1995 3 31 DLM88951185 119950321A5320 CHANNEL DOUG MD88 MD88 3023688NM RT WHEELWELL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11929DL 49716 RT MLG W/W DOOR JAMB FWD CHANNEL CRACKED AT UPPER RADIUS APPROX 2.25 INCHES. REPAIRED PER SRM 53-05, FIG 78. 2L72 4F RTA6WE 19950331006881995033100688NM 1995 3 31 DLM88951320 119950326A2910AE7055371 LINE DOUG MD88 MD88 3023688NM RT PYLON RUPTURED A DALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO11929DL 49716 ON CLIMBOUT FROM ATL FOLLOWING SLAT RETRACTION, RT HYDRAULIC QTY AND PRESSURE WENT TO ZERO. RETURNED ATL. FOUND RT ENGINE HYDRAULIC PUMP PRESSURE LINE RUPTURED IN PYLON JUST BEFORE IT ENTERS THE FUSELAGE. REPLACED LINE RETURNED TO SERVICE. 2L72 4F RTA6WE 19950331006891995033100689WP 1995 3 31 MWEA95154 119950327A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A MWEABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 GL31501ME 47132 PILOT REPORTS ON CLIMB-OUT OF MKE, CABIN ALTITUDE CLIMBING. LEVELED OFF AT 29,000 FT, CABIN ALTITUDE STILL CLIMBING. TRIED CLOSING OUTFLOW VALVE MANUALLY. OXYGEN MASKS DEPLOYED. PERFORMED EMERGENCY DESCENT. RETURNED TO MKE. TROUBLESHOT SYSTEM, SERVICED WATER SEPARATORS, LEAK CHECKED DUCTS, OUTFLOW VALVE OPS CK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950331006901995033100690WP 1995 3 31 MWEA95155 119950327A2130 ROD END DOUG DC9 DC932 3022066WP OUTFLOW VALVE BINDING A MWEAB EMER. DESCENT O OTHER CLCLIMB 1 GL31501ME 47132 PILOT REPORTS AGAIN AT 23,000 FT, CABIN ALTITUDE CLIMBING. O2 MASKS DEPLOYED. PERFORMED EMERGENCY DESCENT INTO GRR. FERRIED BACK TO MKE. TROUBLESHOT SYSTEM. PERFORMED TWO TEST FLIGHTS. FOUND OUTFLOW CONTROL ROD NOT CLOSING VALVE IN FLIGHT BUT WORKING PROPERLY ON GROUND TESTS. CONTROL ROD END TOO TIGHT AT AFT END. LOOSENED ROD END BOLT. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950331006911995033100691EU 1995 3 31 QXEA9500093 119950329A3231NAS5593 PIN FOKKER A11345403 FOKKERF28 F28MK1000 4990808EU MLG DOOR STOP SHEARED OFF A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09803PH 11017 SEA - AFTER GEAR RETRACTION, LEFT MLG DOOR LIGHT REMAINED ON. FLIGHT CONTINUED TO PDX WHERE LIGHT EXTINGUISHED WHEN GEAR COMPLETED EXTENSION CYCLE. FLIGHT LANDED WITHOUT INCIDENT. FOUND NR 1 MLG DOOR UPSTOP BACKED OUT BECAUSE RETAINING PIN HAD BROKEN. RE-RIGGED STOP AND INSTALLED NEW PIN. GROUND TESTS COMPLETED AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950331006921995033100692NM 1995 3 31 SWAA95255 119950326A5320 STRAP BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07331SW 23695 DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZING STRAP CRACKED AT E/E COMPARTMENT, BS 312, BOTTOM OF FLOOR BEAM BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950331006931995033100693NM 1995 3 31 SWAA95256 119950327A53122024T3 WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 184 TO 207, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006941995033100694NM 1995 3 31 SWAA95257 119950327A53122024T3 WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE BULKHEAD WEB CRACKS AT BS 178, WL 209, AND 218, RBL 11.7 TO 13.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006951995033100695NM 1995 3 31 SWAA95258 119950327A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 361 DAMAGE A SWAAK NONE C F.O.D. ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LIGHTNING STRIKE DAMAGE AT BS 361, BETWEEN S2R AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006961995033100696NM 1995 3 31 SWAA95259 119950327A53302024T3 SKIN BOEING737 7372H4 138448CNM BS 987 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND SKIN CRACK AT BS 987, AT STRINGER 4L. REPAIRED PER TRAMCO EWO 95-0241 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006971995033100697NM 1995 3 31 SWAA95260 119950327A5320BAC14902734 BEAM BOEING737 7372H4 138448CNM BS 178 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 7, WL 203. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006981995033100698NM 1995 3 31 SWAA95261 119950327A5320 WEB BOEING737 7372H4 138448CNM BS 178 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 5.7, WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331006991995033100699NM 1995 3 31 SWAA95262 119950327A53202024T3 WEB BOEING737 7372H4 138448CNM BS 178 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 5.7, WL 184 TO 207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331007001995033100700NM 1995 3 31 SWAA95263 119950327A53202024T3 WEB BOEING737 7372H4 138448CNM BS 178 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, RBL 7.7 TO 14.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331007011995033100701NM 1995 3 31 SWAA95264 119950327A53202024T3 WEB BOEING737 7372H4 138448CNM BS 178 CRACK A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND PRESSURE WEB CRACKED AT BS 178, LBL 10.5 TO 12.7, WL 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950331007021995033100702NM 1995 3 31 SWAA95265 119950327A33506013211 PWR SUPPLY BOEING737 7372H4 138448CNM LT O/W EEL INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED SPECIAL VISIT FOR SKIN LAP INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT POWER SUPPLY PER BOEING M/M. 2L72 4F A16WE 19950331007031995033100703NM 1995 3 31 UPS202708 119950328A5320 SHEAR TIE BOEING727 72731C 1384011NM STA 1148 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT STA 1148, BETWEEN STRINGER 25 AND 16L. REPLACED PER DRM 53-10-4, 51-20-4, 51-30-1, 51-20-1. 2L73 4F A3WE 19950331007041995033100704NM 1995 3 31 UPS202709 119950328A5330 SKIN BOEING727 72731C 1384011NM STA 690-700 OIL CANNED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK MAINTENANCE FOUND OIL CANNED FUSELAGE SKIN AT BS 690-700, STRINGER 20-21R. INSTALLED REPAIR PER SRM 51-20-4, 51-30-2. 2L73 4F A3WE 19950331007051995033100705NM 1995 3 31 UPS202710 119950328A5320 STRINGER CLIP BOEING727 72731C 1384011NM STA 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER CLIP STA 328, STRINGER 21R. REPLACED PER SRM 51-20-1, 51-30-2, MM 51-20-21. 2L73 4F A3WE 19950331007061995033100706NM 1995 3 31 UPS202711 119950328A5313 STRINGER BOEING727 72731C 1384011NM STA 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L, STA 950-1183. INSTALLED REPLACEMENT AND REPAIR PER SRM 53-10-1, 53-10-3. 2L73 4F A3WE 19950331007071995033100707NM 1995 3 31 UPS202713 119950328A5313 STRINGER BOEING727 72731C 1384011NM STA 360-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L, STA 360-480. INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950331007081995033100708NM 1995 3 31 UPS202714 119950328A5753 FLAP BOEING727 72731C 1384011NM RT WING FORE DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON RT O/B FOREFLAP, T/E UPPER AND LWR SURFACE, ON PREVIOUS REPAIR. INSTALLED REPAIR PER SRM 51-40-06. 2L73 4F A3WE 19950331007091995033100709NM 1995 3 31 UPS202715 119950328A5755 SPOILER BOEING727 72731C 1384011NM LT WING NR 1 DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 1 SPOILER UPPER SURFACE I/B FWD CORNER. INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950331007101995033100710NM 1995 3 31 UPS202716 119950328A5755 SPOILER BOEING727 72731C 1384011NM LT WING NR 4 DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON NR 4 SPOILER LWR SURFACE O/B FWD CORNER. INSTALLED REPAIR PER SRM 51-40-6 AND 57-50-6. 2L73 4F A3WE 19950331007111995033100711NM 1995 3 31 UPS202717 119950328A5543 TAB BOEING727 72731C 1384011NM UPPER RUDDER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB, UPPER LT SIDE. INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950331007121995033100712NM 1995 3 31 UPS202718 119950328A5543 TAB BOEING727 72731C 1384011NM LOWER RUDDER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON LWR RUDDER TAB T/E. INSTALLED REPAIR PER SRM 51-40-9. 2L73 4F A3WE 19950331007131995033100713NM 1995 3 31 UPS202719 119950328A5542 SKIN BOEING727 72731C 1384011NM LOWER RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON LWR RUDDER BOTTOM SKIN. REPLACED SKIN PER SRM 51-30-2, 51-10-2, 51-10-1, MM 51-20-71. 2L73 4F A3WE 19950331007141995033100714NM 1995 3 31 UPS202720 119950328A5730 SLAT CUT OUT BOEING727 72731C 1384011NM NR 7 SLAT SHEARED FASTENERA IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND SHEARED FASTENERS ON NR 7 SLAT HOOK I/B CUT OUT ON UPPER AFT SIDE. INSTALLED REPAIR PER SRM 57-30-4. 2L73 4F A3WE 19950331007151995033100715NM 1995 3 31 UPS202721 119950328A5753 RIB BOEING727 72731C 1384011NM RT O/B MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK MAINTENANCE FOUND CRACK ON RT WING O/B MID FLAP, O/B AFT END RIB, AT LWR CORNER. REPLACED RIB PER SRM 51-30-2, 51-10-1, 51-10-2. 2L73 4F A3WE 19950331007161995033100716NM 1995 3 31 UPS202722 119950328A5753 RIB BOEING727 72731C 1384011NM RT I/B MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON RT WING I/B MID FLAP, RIB, IN LEADING EDGE, JUST I/B OF FOREFLAP CENTER TRACK CUT OUT. REPLACED RIB PER SRM 51-30-2. 2L73 4F A3WE 19950331007171995033100717NM 1995 3 31 UPS202723 119950328A5754 FLAP BOEING727 72731C 1384011NM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP, O/B BULLNOSE, UPPER HINGE LUG ATTACH FRAME, UPPER SURFACE ON BOTH NUTS. REPLACED K-FLAP PER SRM 57-50-01, OHM 57-51-21, MM 27-81-01. 2L73 4F A3WE 19950331007181995033100718NM 1995 3 31 UPS202725 119950328A5754 RIB BOEING727 72731C 1384011NM NR 3 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 3 SLAT RIB, LWR AFT CORNER WHERE RIB AND LWR CHORD ATTACH. INSTALLED REPAIR PER SRM 51-30-2, 57-50-3. 2L73 4F A3WE 19950331007191995033100719NM 1995 3 31 UPS202726 119950328A5751 SPAR CHORD BOEING727 72731C 1384011NM LT O/B AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CRACK ON LT WING O/B AILERON, UPPER FWD SPAR CHORD. INSTALLED REPAIR PER SRM 51-40-4, 51-10-2, 51-30-2, MM 51-20-00. 2L73 4F A3WE 19950331007201995033100720NM 1995 3 31 UPS202727 119950328A5753 FLAP BOEING727 72731C 1384011NM RT I/B AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON RT I/B AFT FLAP, UPPER SIDE, FWD I/B CORNER. INSTALLED REPAIR PER SRM 51-40-06. 2L73 4F A3WE 19950331007211995033100721NM 1995 3 31 UPS202728 119950328A5755 SPOILER BOEING727 72731C 1384011NM NR 12 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND NR 12 SPOILER CORE TO BE DELAMINATED. INSTALLED REPAIR PER SRM 57-50-6. 2L73 4F A3WE 19950331007221995033100722NM 1995 3 31 UPS202757 119950329A53302024T3071 SKIN BOEING727 72722C 138400FNM BS 259.7-277 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL SKIN AT BS 259.7-277. FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3, 51-30-5, 51-20-21, 51-30-2. 2L73 4F A3WE 19950331007231995033100723NM 1995 3 31 UPS202758 119950329A575465162276 FLAP BOEING727 72722C 138400FNM NR 6 K-FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK MAINTENANCE FOUND NR 6 K-FLAP O/B HINGE LUG ATTACH POINT HAS CORROSION UNDER TOP BOLT O/B SIDE. REPLACED K-FLAP PER SRM 57-51-1 AND MM 27-81-01. 2L73 4F A3WE 19950331007241995033100724NM 1995 3 31 UPS202759 119950329A575465162255A FLAP BOEING727 72722C 138400FNM NR 3 K-FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK MAINTENANCE FOUND NR 3 K-FLAP O/B HINGE O/B LUG UPPER AND LOWER BOLT HOLES HAVE PITTING AROUND O/B SIDE. REPLACED K-FLAP PER MM 27-81-00. 2L73 4F A3WE 19950331007251995033100725NM 1995 3 31 UPS202760 119950330A5753 WEDGE BOEING727 72722C 138400FNM RT MID FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK, MAINTENANCE FOUND TRAILING EDGE WEDGE ON RT I/B MID FLAP CORRODED. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2 AND OHM 20-50-01. 2L73 4F A3WE 19950331007261995033100726NM 1995 3 31 UPS202761 119950330A575165217651 AILERON BOEING727 72722C 138400FNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK, MAINTENANCE FOUND I/B AILERON CONTROL ROD FITTING CORRODED AROUND BOLT HOLE. REPLACED AILERON PER MM 27-10-11. 2L73 4F A3WE 19950331007271995033100727NM 1995 3 31 UPS202762 119950328A3260 WARNING LIGHT BOEING727 72727C 138400JNM TAIL SKID MALFUNCTIONED A IPXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01907UP 19118 (SUPPLEMENTAL MRR) PILOT REPORTED THAT AFTER TAKEOFF, RED GEAR LIGHTS REMAINED ON WITH GEAR HANDLE UP, TAIL SKID LIGHT REMAINED ON. RECYCLED HANDLE, ALL GREEN POS LIGHTS WORKED NORMALLY AND DOOR LIGHTS WORKED NORMALLY. RED LIGHTS REMAINED ON AFTER RECYCLE ON TAIL SKID LIGHT. PULLED ACTUATOR CIRCUIT BREAKER. TESTED TAIL SKID PER MM 32-71-01 WITH NO FAULTS FOUND. DMI CLEARED. 2L73 4F A3WE 19950331007281995033100728NM 1995 3 31 UPS202763 119950329A3350 BATTERIES BOEING727 72725C 138400HNM FLIGHT DECK EEL INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01951UP 19850 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT ABOVE MAIN DOOR INOP. REPLACED EMER EXIT LIGHT BATTERIES. OPS CK GOOD. 2L73 4F A3WE 19950331007291995033100729NM 1995 3 31 UPS202764 119950327A3350 LIGHT ASSY BOEING727 72727C 138400JNM FLIGHT DECK EEL INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01908UP 19114 MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE IN THE ON POSITION OR WHEN POWER WAS REMOVED FROM THE A/C IN THE ARM POSITION. INSTALLED 2 EA NEW LIGHT ASSY. OPS CK NORMAL. 2L73 4F A3WE 19950331007301995033100730NM 1995 3 31 UPS402746 119950329A5330 SKIN BOEING747 747123F NM BS 2020-2040 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON LAP SPLICE BETWEEN BS 2020 AND BS 2040, STR 19L. FABRICATED AND INSTALLED REPAIR PER UPS EO B747-5330-1053E. 2L74 4F A20WE 19950331007311995033100731NM 1995 3 31 UPS402747 119950329A5410 RIB BOEING747 747123F NM NAC STA 163 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND NR 4 PYLON RIB CRACKED AT NAC STA 163 O/B SIDE. REPLACED RIB PER SRM 51-30-2. 2L74 4F A20WE 19950331007321995033100732NM 1995 3 31 UPS402748 119950329A5414 SKIN BOEING747 747123F NM NAC STA 221 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND NR 4 PYLON OUTER SKIN CRACKED AT NAC STA 221. FABRICATED AND INSTALLED REPAIR PER SRM 54-30-03. 2L74 4F A20WE 19950331007331995033100733NM 1995 3 31 UPS402749 119950329A5313 STRINGER BOEING747 747123F NM BS 970 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND VERTICAL FLANGE CRACKED ON STR 3A RT AT BS 970. REPLACED STRINGER PER SRM 51-10-3. 2L74 4F A20WE 19950331007341995033100734NM 1995 3 31 UPS402750 119950329A5313 STRINGER BOEING747 747123F NM BS 1225 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND STRINGER 4L CRACKED AT BS 1225. REPLACED STRINGER PER SRM 51-10-3. 2L74 4F A20WE 19950331007351995033100735NM 1995 3 31 UPS402751 119950329A5315 FLOOR BEAM BOEING747 747123F NM BS 1660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT BS 1660. REPLACED UPPER CHORD PER SRM 51-30-2. 2L74 4F A20WE 19950331007361995033100736NM 1995 3 31 UPS402752 119950329A5315 FLOOR BEAM BOEING747 747123F NM BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT BS 1580. REPLACED UPPER CHORD PER SRM 51-30-2. 2L74 4F A20WE 19950331007371995033100737NM 1995 3 31 UPS402753 119950329A5711 WEB BOEING747 747123F NM STA 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CORROSION ON SPAR WEB AT STA 1000. FABRICATED AND INSTALLED REPAIR PER UPS EO B747-5710-6859A. 2L74 4F A20WE 19950331007381995033100738NM 1995 3 31 UPS402754 119950329A5315 FLOOR BEAM BOEING747 747123F NM STA 1760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD FLOOR BEAM AT BS 1760, RBL 25-40. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. 2L74 4F A20WE 19950331007391995033100739NM 1995 3 31 UPS402755 119950329A5311 FRAME BOEING747 747123F NM STA 1600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND CRACKED FRAME AT BS 1600, RBL 62. FABRICATED AND INSTALLED REPAIR PER UPS EO FILE NUMBER 747-53-0710. 2L74 4F A20WE 19950331007401995033100740NM 1995 3 31 UPS402756 119950329A5311 FRAME BOEING747 747123F NM STA 1700 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FRAME AT STA 1700, STR 48R, LBL 25. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4, 51-30-2. 2L74 4F A20WE 19950331007411995033100741WP 1995 3 31 UPS802712 119950327A5230 SKIN DOUG DC8 DC871F 302199DWP FWD X-SLIDE DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON FWD CROSS SLIDE DOOR SKIN (OUTER), FS 310, LONGERON 25R. INSTALLED REPAIR PER SRM 52-2-3. 2L74 4F RT4A25 19950331007421995033100742WP 1995 3 31 UPS802729 119950327A57307075T6063 SKIN DOUG DC8 DC871F 302199DWP RT WING XFS 416 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND RT WING LEADING EDGE UPPER SURFACE HAS CORROSION BULGE AT STA XFS 416. REPAIRED SKIN PER SRM 57-2-0. 2L74 4F RT4A25 19950331007431995033100743WP 1995 3 31 UPS802730 119950327A5347S2892072C38400 SPLICE SUPPORT DOUG DC8 DC871F 302199DWP FS 1640-1655 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AT SEAT TRACK SPLICE SUPPORT, NR 8 TRACK, FS 1640-1655, RBL 36. REPLACED SPLICE SUPPORT PER SRM 53-2-3 AND MM 53-40-02. 2L74 4F RT4A25 19950331007441995033100744WP 1995 3 31 UPS802731 119950327A53223773479516 FITTING DOUG DC8 DC871F 302199DWP FS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND FLOOR SUPPORT FITTING CORRODED AT FS 1580, LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950331007451995033100745WP 1995 3 31 UPS802732 119950327A53159887426502 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 1640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION AT FLOOR BEAM AT FS 1640, RBL 30-40. REPAIRED PER UPS EO DC8-5310-6793A. 2L74 4F RT4A25 19950331007461995033100746WP 1995 3 31 UPS802733 119950327A53159758924501 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM AT FS 140, RBL 65. REPAIRED PER UPS EO DC8-5310-6794A. 2L74 4F RT4A25 19950331007471995033100747WP 1995 3 31 UPS802734 119950327A53207075T6040 WEB DOUG DC8 DC871F 302199DWP FS 140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND WEB ON TOP OF FLOOR BEAM CORRODED AT FS 140, RBL 65. REPAIRED PER SRM 53-2-0. 2L74 4F RT4A25 19950331007481995033100748WP 1995 3 31 UPS802735 119950327A533057549923 SKIN DOUG DC8 DC871F 302199DWP FS 621 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INNER SKIN AND DOUBLER AT FS 621, LONGERON 34L. REPAIRED PER UPS EO DC8-5330-6792A. 2L74 4F RT4A25 19950331007491995033100749WP 1995 3 31 UPS802736 119950327A532037592221 FITTING DOUG DC8 DC871F 302199DWP FS 1260-1280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACKED SPLICE FITTING AT FS 1260-1280, LONGERON 36. REPLACED FITTING PER SRM 51-3-0, 51-1-20D. 2L74 4F RT4A25 19950331007501995033100750WP 1995 3 31 UPS802737 119950327A53204640162 FITTINGS DOUG DC8 DC871F 302199DWP FS 1540, 1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME END FITTINGS AT FS 1540 AND 1560, LONGERON 21R. REPLACED FITTINGS PER SRM 51-1-20D. 2L74 4F RT4A25 19950331007511995033100751WP 1995 3 31 UPS802738 119950327A53139755803 LONGERON DOUG DC8 DC871F 302199DWP FS 60-80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION ON LONGERON 21R, FS 60-80. REPAIRED LONGERON PER SRM 53-2-5. 2L74 4F RT4A25 19950331007521995033100752WP 1995 3 31 UPS802739 119950327A534752772660 SEAT TRACK DOUG DC8 DC871F 302199DWP FS 55-280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 9 SEAT TRACK AT FS 55-280. REPLACED SEAT TRACK PER SRM 53-2-3. 2L74 4F RT4A25 19950331007531995033100753WP 1995 3 31 UPS802740 119950327A5311 BELTFRAME DOUG DC8 DC871F 302199DWP FS 1060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME AT FS 1060, LONGERON 29-30L. FABRICATED AND INSTALLED REPAIR PER SRM 51-1-20D, 51-1-8. 2L74 4F RT4A25 19950331007541995033100754WP 1995 3 31 UPS802741 119950327A53203755822506 FITTING DOUG DC8 DC871F 302199DWP FS 350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTING AT FS 350, LONGERON 28L. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950331007551995033100755WP 1995 3 31 UPS802742 119950329A53204611422 FITTINGS DOUG DC8 DC873F 302199FWP FS 902, 940 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON 2 EA VERTICAL FLOOR BEAM STIFFENER FITTINGS AT FS 902 AND 940, BL 0. REPLACED FITTINGS PER SRM 51-1-20D. 2L74 4F RT4A25 19950331007561995033100756WP 1995 3 31 UPS802743 119950329A53207075T6050 DOUBLER DOUG DC8 DC873F 302199FWP FS 902-920 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER DOUBLER AT FS 902-920, BL 0, AT UPPER MAIN GEAR WHEELWELL PRESSURE DECK SURFACE. REPLACED DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19950331007571995033100757WP 1995 3 31 UPS802744 119950329A573097510822 SKIN DOUG DC8 DC873F 302199FWP RT XFS 29.6-33.3CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 WHILE IN 'C' CHECK MAINTENANCE FOUND CORROSION BULGE AROUND RT AUX TANK UPPER ATTACH ANGLE SCREW ON SKIN AT STA XFS 29.6-33.35. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-57-0542. 2L74 4F RT4A25 19950331007581995033100758WP 1995 3 31 UPS802745 119950329A57303646959 PANEL DOUG DC8 DC873F 302199FWP RT PANEL 519A CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT WING LEADING EDGE LOWER SURFACE PANEL 519A. REPLACED PANEL PER DRAWING NR 3646959. 2L74 4F RT4A25 19950331007591995033100759NM 1995 3 31 95ZZZW279 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1010 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO AREA OF SURFACE CORROSION IN STR 29R CHANNEL AND ON STR SPLICE APPROX 6 INCHES AFT OF FS 1010 FRAME. REMOVED FASTENERS AND FABRICATED SPLICE PLATE. REPLACED SPLICE AS PER SRM 51-10-1 PAR 4. INSTALLED FASTENERS PER SRM 51-30-2. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007601995033100760NM 1995 3 31 95ZZZW280 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 970-990 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO HAS SEVERAL AREAS OF SURFACE CORROSION AROUND FASTENERS AT O/B SIDE OF STR 29L BETWEEN FS 970 AND FS 990. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4 12 INCHES BY 1 INCH .100. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007611995033100761NM 1995 3 31 95ZZZW281 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 950 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO HAD CORROSION ALONG O/B ROW OF FASTENERS ON STR 29L BETWEEN FS 950E AND FS 950F. REMOVED CORROSION PER SRM 51-10-6, TREATED ALODINE AND PRIMED PER SRM 51-10-2, BEYOND LIMITS, INSTALLED ANGLE REPAIR PER SRM 51-40-4 12 INCHES BY 1 INCH .100 ON STR 29L STA 950E AND 950F MATERIAL REMOVED .032. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007621995033100762NM 1995 3 31 95ZZZW282 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 950 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO HAD CORROSION ON O/B SIDE OF STR 29R AROUND FASTENERS BETWEEN FS 950D AND FS 950E. REMOVED CORROSION PER SRM 51-10-6, CORROSION OUT OF LIMIT. FABRICATED EXIT STRAP AND INSTALLED PER SRM 51-40-4 9.5 INCHES BY 4 INCHES .125 2024-T3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007631995033100763NM 1995 3 31 95ZZZW283 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 950 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO HAD EVIDENCE OF CORROSION AROUND FASTENERS AT O/B SIDE OF STR 29L BETWEEN FS 950D AND FS 950E. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4, 2 INCHES BY 2 INCHES .100, FS 950D IS WITHIN LIMITS, INSTALLED FASTENERS PER SRM 51-30-2. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007641995033100764NM 1995 3 31 95ZZZW284 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 950 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO HAD EVIDENCE OF SURFACE CORROSION ALONG O/B EDGE OF STR 29L BETWEEN FS 950 AND FS 950A. REMOVED CORROSION IAW SRM 51-10-6, BEYOND LIMITS, INSTALLED REPAIR IAW SRM 51-40-4, ALODINE PRIMER PER SRM 51-10-2 2024-T3, .100 10.5 BY 6.25. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007651995033100765NM 1995 3 31 95ZZZW285 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FS 480 CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND NR 5 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC SA 17750 AND SRM 51-10-1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007661995033100766NM 1995 3 31 95ZZZW286 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FS 480 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND NR 3 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC - S4179750 AND SRM 51-10-1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007671995033100767NM 1995 3 31 95ZZZW287 119950228A5347 SEAT TRACK BOEING727 7272Q9 138448MNM FS 480 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND NR 2 SEAT TRACK CORRODED FROM STA 480 TO FWD END. REPLACED SEAT TRACK AS PER MODIFICATION STC SA 179750 AND SRM 51-10-1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007681995033100768NM 1995 3 31 95ZZZW288 119950228A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM FS 312 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND CORROSION ON INTERCOSTAL RBL 12 JUST FWD OF STA 312 FLOORBEAM. REPLACED DAMAGED INTERCOSTAL AS PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007691995033100769NM 1995 3 31 95ZZZW289 119950228A5320 SUPPORT BOEING727 7272Q9 138448MNM FS 312 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND CORROSION ON 'T' ANGLE FLOOR SUPPORT RBL 41 JUST FWD OF STA 312 FLOORBEAM. REPLACED ANGLE AND INSTALLED PER SRM 51-10-1 PG 4 AND 5, 51-30-2. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007701995033100770NM 1995 3 31 95ZZZW290 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 1085 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR - FUS SKIN BULGE AT EXTERNAL DOUBLER AT FS 1085 STR 30. CUT OUT DAMAGED SKIN BULGE PER SRM 53-30-3 AND INSTALLED DOUBLER SKIN REPAIR IAW SRM 53-30-3 9 INCHES BY 18 INCHES .071. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007711995033100771NM 1995 3 31 95ZZZW291 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 950B CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR GOUGE IN FUS SKIN EXTERIOR STR FS 950B AT STR 24L ('B' SYSTEM HYDRAULIC AREA). BURNISHED AREA PER SRM 51-10-1, NO CRACK NOTED, NDT TERMINATION BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 18 INCHES BY 10 INCHES .071. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007721995033100772NM 1995 3 31 95ZZZW292 119950228A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FS 1110 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND CORROSION ON FLOORBEAM FS 1110 FROM LBL 24 TO LBL 45 UPPER FLANGE. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-8. TREATED AND PRIMED AREA BEFORE INSTALLATION. FLANGE REPAIR 35 INCHES AND 2.5 INCHES - STRAPS 7085-T6. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007731995033100773NM 1995 3 31 95ZZZW293 119950228A5320 SUPPORT BOEING727 7272Q9 138448MNM FS 314 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, STA 314 FLOOR SUPPORT IS CORRODED FROM RBL 15 TO RBL 42. INSTALLED NEW SUPPORT ANGLE AS PER SRM 57-10-1 PAR 4 AND SRM 51-30-2 FROM RBL 15 - RBL 42 7075-T73 STA 314. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007741995033100774NM 1995 3 31 95ZZZW294 119950228A5315 FLOORBEAM BOEING727 7272Q9 138448MNM FS 344 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, STA 344 UPPER FLOORBEAM CAP CORRODED FROM LBL 60 TO RBL 60. REMOVED OLD BAD BEAM CP. CLEANED AREA REMOVED SOME MILD CORROSION FROM WEB AS PER SRM 51-10-6. INSTALLED NEW CAP AS PER SRM 51-10-1 PAR 4 , 51-30-2 7075-T3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007751995033100775NM 1995 3 31 95ZZZW295 119950228A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 400 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FLOORBEAM SUPPORT FROM BS 400 TO BS 420 RBL 55 UPPER ANGLE CORRODED AND HOLES DRILLED ON RADIUS. REPLACEMENT OF ANGLE AS PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007761995033100776NM 1995 3 31 95ZZZW296 119950228A5311 FRAME BOEING727 7272Q9 138448MNM BS 380 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D CHECK, FOUND CORROSION OF FRAME BS 380 FROM BL 0 TO RBL 24 UPPER FLANGE. REMOVED BAD SECTION. REPAIRED AS PER SRM 53-10-8 AND SRM 51-30-2. STA 380 FROM BL 0 TO RBL 24 7075-T73. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007771995033100777NM 1995 3 31 95ZZZW297 119950228A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 400 / 420 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND CORROSION ON UPPER FLANGES OF FLOORBEAMS BS 400 AND BS 420 BETWEEN RBL 24 AND LBL 24. STA 420 - REMOVED CORROSION AS PER SRM 51-10-6 - MIN THICKNESS REMAINING .114 WITHIN LIMITS PER SRM 53-10-1 FIG 4. STA 400 - REMOVED CORROSION PER SRM 51-10-6 - MIN THICKNESS REMAINING .088 OUT OF LIMITS PER SRM 53-10-1 FIG 4 RBL 21. STA 420 TO 400 ALODINED AND PRIMED PER SRM 51-10-2. CUT OUT BAD AREA STA 400 FROM RBL 6 TO 28 RBL AS PER SRM 53-10-8 28 INCHES BY 2 INCHES BY 2 INCHES 7075-T6. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007781995033100778NM 1995 3 31 95ZZZW298 119950228A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 400 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D CHECK, FOUND FLOORBEAM UPPER FLANGE BS 400 BETWEEN RBL 24 AND RBL 45 HAS CORROSION. ACCOMPLISHED REPAIR IAW SRM 51-10-6 AND SRM 53-10-8. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007791995033100779NM 1995 3 31 95ZZZW299 119950228A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 380 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D CHECK, FLOORBEAM UPPER FLANGE HAS CORROSION BS 380 BETWEEN RBL 24 AND RBL 45. REMOVED BAD SECTION, ACCOMPLISHED REPAIR AS PER SRM 53-10-8 AND SRM 51-30-2 ON STA 380 BETWEEN RBL 24 AND RBL 45 7075-T3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007801995033100780NM 1995 3 31 95ZZZW300 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1183-1166 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, BETWEEN STA 1183 AND 1166 STR 22L WAS CRACKED AND EXPLODED CORROSION. CUT OUT DAMAGED STR IAW SRM 53-10-3. INSTALLED NEW SECTION AND SPLICED STR REPAIR PER SRM 53-10-3 FROM STA 1183 TO 1154. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007811995033100781NM 1995 3 31 95ZZZW301 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1050 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR - FUS SKIN BULGED AND LOOSE RIVETS AT FS 1050 AT STR 26L AND STR 28L. REMOVED DAMAGED PORTION OF STR 27L THAT WAS CAUSING SKIN BULGE. REINSTALLED STRINGER SPLICE AS PER SRM 53-10-3. STRINGER SPLICE APPROX 10 INCHES. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007821995033100782NM 1995 3 31 95ZZZW302 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 328 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, UPPER EXT FUS BS 328 BETWEEN STR 1 AND 3L, DEEP DENT AND SCRATCHES. CUT OUT DAMAGED AREA PER SRM 53-30-3. INSTALLED EXTERNAL REPAIR AS PER SRM 53-30-3 FIG 3 AND FIG 14, 24 INCHES BY 30 INCHES 2024-T3 .070. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007831995033100783NM 1995 3 31 95ZZZW303 119950228A5230 SKIN BOEING727 7272Q9 138448MNM AFT CARGO DOOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, AFT CARGO DOOR FWD LOWER CORNER IS CHAPPED, ERODED AND CORRODED. INSTALLED DOUBLER SKIN REPAIR IAW SRM 52-00-3 8 INCHES BY 2 INCHES .063. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007841995033100784NM 1995 3 31 95ZZZW304 119950228A5311 FRAME BOEING727 7272Q9 138448MNM BS 1148 CORRODED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FRAME HAD SEVERAL AREAS OF CORROSION BS 1148 BETWEEN STR 22L TO STR 27L ON TOP AND BOTTOM OF UPPER FLANGE. REMOVED CORROSION, MATERIAL REMOVED AT FRAME, NUTPLATE HOLE EXCESSIVE, OUT OF LIMITS. INSTALLED FRAME REPAIR AS PER SRM 51-10-6 AND 51-10-4 FIG 1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007851995033100785NM 1995 3 31 95ZZZW305 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 700-720 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FOUND CORROSION AND BULGE IN FUS SKIN BETWEEN FS 700 AND FS 720 APPROX BELOW STR 28L. REPLACED SKIN FROM STA 681 TO 725 BETWEEN STR 26L AND 26R PER SRM 53-30-3 IAW SB 727-53-A203 AND AD 91-09-09. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007861995033100786NM 1995 3 31 95ZZZW306 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 700-720 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR HAD SEVERAL AREAS OF SURFACE CORROSION AROUND NUTPLATES AT FUS FAIRING SKIN MATING AREAS BETWEEN STR 26L AND STR 26R, BETWEEN FS 700 AND FS 720. REPLACED SKIN FROM STA 681 TO 725 BETWEEN SRM 26L AND 26R PER SRM 53-30-3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007871995033100787NM 1995 3 31 95ZZZW307 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 950-1010 GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D CHECK, FUS SKIN EXTERIOR SURFACE GOUGED AND LIGHTLY CORRODED ALONG LOWER EDGE OF LT FUS BODY FAIRING MATING SURFACE FROM FS 950C TO FS 1010 BETWEEN STR 27L AND STR 20L. REPAIRED GOUGED WITH DOUBLER 17 INCHES BY 11 INCHES 2024-T3 PER SRM 53-30-3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007881995033100788NM 1995 3 31 95ZZZW308 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 1090 GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR HAD DEEP GOUGE IN FUS SKIN AT FS 1090 STR 18L. BURNISHED GOUGE BEYOND LIMITS PER SRM 51-10-1. CUT OUT DAMAGE PER SRM 53-30-3. FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3 19 INCHES BY 12 INCHES 2024-T3 .063. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007891995033100789NM 1995 3 31 95ZZZW309 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 1183 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR HAD MANY SCRATCHES AND GOUGES IN FUS SKIN EXTERIOR SURFACE BETWEEN NEGATIVE PRESSURE RELIEF DOOR AND FS 1183 BETWEEN STR 18L AND STR 26L. REPAIRED GOUGES AT STA 1183 BETWEEN STA 18L AND STR 26L AS PER SRM 53-19-3, 19 INCHES BY 12 INCHES 2024-T3 .063. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007901995033100790NM 1995 3 31 95ZZZW310 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1150 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR HAD SKIN BULGE AT FS 1150 AT STR 23R. REMOVED STRINGER AND FASTENER AS PER SRM 53-10-3. REMOVED SURFACE CORROSION ON SKIN IN SECTION AS PER SRM 51-10-6 LESS THAN .003. ALODINE AND PRIMED AS PER SRM 51-10-2. INSTALLED STR 23R BETWEEN STA 1130 TO 1170 AS PER SRM 53-10-3. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007911995033100791NM 1995 3 31 95ZZZW311 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 1010 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR HOLE CORRODED IN FUS SKIN AT FS STR 30. CUT OUT DAMAGED AREA PER SRM 53-30-3 AND INSTALLED REPAIR .71 7075-T6 6 INCHES BY 8 INCHES. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007921995033100792NM 1995 3 31 95ZZZW312 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 324 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, UPPER EXT FUS APPROX BS 324 BETWEEN STR 3L AND 4L, DENT APPROX 1 INCH BY 2 INCH. CUT OUT OVERLAPPING SKIN PER SRM 53-30-3. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3, 24 INCHES BY 30 INCHES 2024-T3 .070. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007931995033100793NM 1995 3 31 95ZZZW313 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 333 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, UPPER EXT FUS APPROX BS 333 JUST ABOVE AND ON STR 4L, DENT AND SCRATCH APPROX 3 INCHES L. CUT OUT DAMAGE SKIN PER SRM 53-30-3. INSTALLED EXTERNAL REPAIR AS PER SRM 53-30-3 FIG 3, 24 INCHES BY 30 INCHES 2024-T3 .070 IAW SRM 53-30-3 FIG 14. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007941995033100794NM 1995 3 31 95ZZZW314 119950228A5330 SKIN BOEING727 7272Q9 138448MNM BS 950B BURNED A DHLAK NONE C F.O.D. ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, EXT FUS AT APPROX BS 950B STR 3L LIGHTENING STRIKE. REPAIRED LIGHTENING STRIKE AREA AS PER SRM 53-30-3. INSTALLATION OF DOUBLER 7 INCHES BY 12.5 INCHES 2024-T3 .090. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007951995033100795NM 1995 3 31 95ZZZW315 119950228A5711 SPAR CHORD BOEING727 7272Q9 138448MNM WS 360-383 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, R/W FRONT SPAR LOWER CHORD CORRODED AT WS 383.0. REMOVED CORROSION PER SRM 51-10-6. CORROSION OUT OF LIMITS .093 REMOVAL PER SRM 51-20-1 FIG E. CUT OUT SPAR CHORD FROM WS 386 PER SRM 51-10-1, SPLICED IN NEW SECTION 24 INCHES PER SRM 51-40-4. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007961995033100796NM 1995 3 31 95ZZZW316 119950228A5711 SPAR CAP BOEING727 7272Q9 138448MNM LT WING CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, LT WING LE LOWER SPAR CAP LOWER SURFACE HAS EXFOLIATED CORROSION AFT OF NR 3 LE SLAT ACTUATOR AT 6 INCHES I/B OF ACTUATOR MOUNT BRACKET. REMOVED DAMAGED SECTION, FABRICATED NEW SPAR CAP, INSTALLED NEW SECTION PER SRM 51-40-4 AND 51-10-1, MATERIAL OF STRAP REPAIR 2024-T3 .350 THICK 3 INCHES BY 11 INCHES. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950331007971995033100797NM 1995 3 31 ASAA9540005 119950303A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING CHECK, THE LAST 2 EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRING AND OPS CHECKED NORMAL. (W) 2L72 4F RTA16WE 19950331007991995033100799CE 1995 3 31 95ZZZX1506 119950317A57533316503030 BRACKET BEECH 1900 1900C 1154161CE LT TE FLAP FAILED A AVALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP231568W UC64 AIRCRAFT EXPERIENCED ASYMMETRICAL FLAP CONDITION DURING APPROACH AFTER FLAPS WERE EXTENDED TO 35 DEGREES. REQUIRED FULL RIGHT AILERON USING EXTREME FORCE WITH BOTH HANDS TO REGAIN LEVEL FLIGHT. FOUND AFT FLAP BEARING OUTER RACE FLANGE OF THE LEFT OTUBOARD FLAP WORN THROUGH FLAP HINGE BRACKET. REF. IPC 57-50-10, ITEMS 5 AND 21. NO SPECIFIC INSPECTION CALLED FOR IN CONTINUOUS INSPECTION PROGRAM FOR FLAP BEARING SUPPORT AREAS. 2L72 4T RTA24CE 19950331008001995033100800CE 1995 3 31 95ZZZX1507 119950313A321313889 BEARING BEECH 1900 1900D 1154162CE RT MLG FAILED A JJBAK NONE D INFLIGHT SEPARATION TOTAKEOFF 1 EA01841CA679 1018 UE40 ON ARRIVAL ALB, PIC NOTICED RIGHT INBOARD TIRE AND WHEEL, PN 40273A, ASSEMBLY MISSING. SUBJECT WHEEL ASSEMBLY WAS LATER FOUND AT ROC, THE LAST AIRPORT OF DEPARTURE. IT APPEARS OUTBOARD AND INBOARD BEARINGS FAILED. RETAINING NUT AND COTTER PIN WERE FOUND STILL ON AXLE. WHEEL, BRAKE, AND LANDING GEAR WERE REPLACED. 2L72 4T RTA24CE 19950331008011995033100801NE 1995 3 31 95ZZZX1508 219950313A73103035318 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE CLOGGED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17451UE 120108 FAT - LEFT ENGINE FUEL FILTER INDICATION LIGHT ILLUMINATED DURING CLIMB. TORQUE DROPPED 50 PERCENT. NORMAL OPS. AFTER EEC SELECTED OFF, AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE HIGH PRESSURE AND LOW PRESSURE FUEL FILTERS. PERFORMED ENGINE GROUND RUN. ENGINE OPERATION NORMAL. AIRCRAFT RETURNED TO SERVICE. REF. CONTROL NR WTAA950123. (X) 2L72 4T4 TRTA31SO E20NE 19950331008021995033100802WP 1995 3 31 95ZZZX1509 119950225A3240 BRAKES DOUG DC8 DC871 302199AWP MLG MALFUNCTIONED A RRXAO OTHER O OTHER LDLANDING 1 WP158087U 45977 MTPP - ON LANDING BRAKES WERE TOTALLY INOPERATIVE. USED EMERGENCY BRAKES TO STOP AIRCRAFT. (HYDRAULIC QUANTITY AND PRESSURE NORMAL). MAINTENANCE CHECKED LANDING GEAR AREA AND BLED ALL BRAKES. CHECKED ANTI-SKID SYSTEM. NO DEFECTS WERE FOUND. REPLACED NR 1 AND NR 5 MLG TIRES DUE TO FLAY SPOTS IAW MM 32-4-10. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 19950331008031995033100803WP 1995 3 31 95ZZZX1510 119950224A275037185095501 SLOT CONTL VALVE DOUG DC8 DC862F 3021972WP TE FLAP LEAKING A RRXAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP15997CF 46154 KAUS/KDAY - FLT 107 - IN-FLIGHT LOST ALL HYDRAULIC PRESSURE AND QUANTITY DOWN TO AUX MARK ON QUANTITY INDICATOR. MAINTENANCE FOUND SLOT CONTROL VALVE LEAKING. REMOVED AND REPLACED SLOT CONTROL VALVE IAW MM 27-80-4. HYDRAULIC SYSTEM SERVICED. LEAK AND OPS CHECK WAS GOOD. 2L74 4F 4A25 19950331008041995033100804WP 1995 3 31 95ZZZX1511 119950115A53202537717 CUSP DOUG DC8 DC863F 302198FWP FS 1365 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND CORROSION BETWEEN RT LOWER CUSP AND WEB F/S 1365 RT. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-8. 2L74 4F 4A25 19950331008051995033100805WP 1995 3 31 95ZZZX1512 119950115A5320 DOUBLERS DOUG DC8 DC863F 302198FWP FS 380-400 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND CORROSION ON AND UNDER INTERNAL DOUBLER AT FS 380 TO FS 400 AT LONGERONS 35 LEFT TO 36. CUT AND REMOVED SECTION OF INTERNAL DOUBLER. REMOVED CORROSION AND TREATED AREA. FABRICATED NEW SECTION OF INTERNAL DOUBLERS AND EXTERNAL DOUBLER. INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-7. 2L74 4F 4A25 19950331008061995033100806WP 1995 3 31 95ZZZX1513 119950115A53112537716 FRAME DOUG DC8 DC863F 302198FWP FS 1560 MISDRILLED A RRXAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND FRAME FITTING SHIM AT CUSP HAD COROSION. FRAME HAD SURFACE CORROSION AND HOLE DRILLED IN RADIUS FS 1560 RIGHT. REMOVED CORROSION. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED FRAME REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-4. 2L74 4F 4A25 19950331008071995033100807WP 1995 3 31 95ZZZX1514 119950115A53131290340 LONGERON DOUG DC8 DC863F 302198FWP FS 680 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND CORROSION ON LONGERON 31 LEFT FS 680 IN MID-SHIP ACCESSORY COMPT. REMOVED DAMAGED AREA OF LONGERON, FABRICATED REPAIR AND SPLICES. INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-5. 2L74 4F 4A25 19950331008081995033100808WP 1995 3 31 95ZZZX1515 119950115A5320 DOUBLER DOUG DC8 DC863F 302198FWP BS 80-95 CUT A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND CORROSION UNDER FINGER DOUBLER FS 80 TO FS 95 AT LONGERON 31 RIGHT. EXISTING REPAIR STRAP HAD TO BE CUT FOR ACCESS. CUT STRAP AND PEELED BACK FUSELAGE SKIN. REMOVED CORROSION UNDER FINGER DOUBLER. TREATED AND PRIMED AREA. REINSTALLED SKIN AND STRAP WITH SPLICE DOUBLER IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-6. 2L74 4F 4A25 19950331008091995033100809WP 1995 3 31 95ZZZX1516 119950115A53474889036 FLOOR TRACK DOUG DC8 DC863F 302198FWP CARGO COMPT WORN A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND FLOOR TRACK WORN AFT COMP 3 BL 45.500 RIGHT 2 EA PLACES. CUT OUT DAMAGED TRACK. FABRICATED NEW TRACK SECTION IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-10 AND INSTALLED IAW SRM 53-2-3. 2L74 4F 4A25 19950331008101995033100810WP 1995 3 31 95ZZZX1517 119950115A53112357716 FRAME DOUG DC8 DC863F 302198FWP FS 540 MISDRILLED A RRXAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND A HOLE DRILLED IN FRAME RADIUS AT CUSP ATTACH FITTING FS 540 RT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-4. 2L74 4F 4A25 19950331008111995033100811WP 1995 3 31 95ZZZX1518 119950115A53112537716 FRAME DOUG DC8 DC863F 302198FWP FS 1240 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND FRAME CORRODED FS 1240 LONGERON 34 LEFT TO 31 RIGHT. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW DER APRROVED ENGINEERING SKETCH SKA 94190-3. (X) 2L74 4F 4A25 19950331008121995033100812WP 1995 3 31 95ZZZX1519 119950115A53152652479 FLOOR BEAM DOUG DC8 DC863F 302198FWP FS 1702 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND FLOOR BEAM SUPPORT CORRODED BEYOND LIMITS, COMPARTMENT 18 BL 24.750 RIGHT FS 1702. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-2. 2L74 4F 4A25 19950331008131995033100813WP 1995 3 31 95ZZZX1520 119950115A5330 PLATING DOUG DC8 DC863F 302198FWP FS 1220-1240 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15921R 46145 DURING C-CHECK, FOUND INNER SKIN CORRODED IN C-PIT, FS 1220 TO FS 1240 AT LONGERONS 31 RIGHT TO 35 LEFT. OUTER FUSELAGE SKIN HAD TO BE CUT FOR ACCESS TO CORROSION. REMOVED CORROSION. FABRICATED STRAPS, FILLERS, AND DOUBLERS. INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH SKA 94190-9. 2L74 4F 4A25 19950331008141995033100814SO 1995 3 31 C2XA95IA024 119950208A281012036525001 PANEL EMB 120 EMB120RT SO LT WING LEAKING A C2XAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW0916724 120171 IAH - FLT 2871 - PILOT REPORTED WHILE EN ROUTE, AN IMBALANCE OF LEFT AND RIGHT FUEL LOADS WAS NOTICED. THE CREW MADE AN UNSCHEDULED LANDING AT MLU IWTHOUT FURTHER INCIDENT. ON THE GROUND, THE CREW NOTED FUEL LEAKING OUT OF THE LEFT WING AT ONE OF THE ACCESS PANELS. PANEL 522DB WAS FOUND TO HAVE BEEN LEAKING, WITH SOME SCREWS THAT HAD WORKED LOOSE NOTED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE PANEL AND LEAK CHECKED THE PANEL AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T RTA31SO 19950331008151995033100815WP 1995 3 31 CKSA95009 119950226A326032802501 SW LEVER ASSY DOUG DC8 DC863 302198AWP LANDING GEAR DIRTY A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23868BX55138 46034 KLAX - FLT 62063 - LANDING GEAR WARNING HORN REMAINED ON WHEN GEAR HANDLE WAS MOVED TO UP POSITION. RECYCLE OF GEAR - NO HELP AND LANDING GEAR UPLATCH CHECK NORMAL AND FLAPS RETRACTED. FOUND DIRT IN SECONDARY LANDING GEAR WARNING SWITCH LEVER ASSY CAUSING SWITCH TO STICK. CLEANED AS REQUIRED AND OPS TESTED WARNING SYSTEM OKAY PER 27-52-2 AND 32-20-0. (X) 2L74 4F 4A25 19950331008161995033100816 1995 3 31 CKSA95010 419950302A2210MF00569A CIRCUIT BREAKER DOUG DC8 DC863F 302198FWP AFT EQUIP PANEL FAILED A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23815CK32313 46151 YIP - FLT 62152 - ON TAKEOFF AT GEAR RETRACTION - HORN SOUNDED AND GEAR AND DOOR LIGHT REMAIN ON. RECYCLED GEAR, GEAR LIGHT WENT OUT. LIGHT REMAINED ON AND HORN SOUNDED. REMOVED AND REPLACED A/P OFF WARN CIRCUIT BREAKER. HORN CHECKS GOOD ON GROUND. (X) 2L74 4F 4A25 19950331008171995033100817WP 1995 3 31 GAIA9503 119950216A32345955996501 GEAR SELECTOR DOUG DC9 DC915F 3022037WP INST PANEL MALFUNCTIONED A GAIAO OTHER O OTHER APAPPROACH 1 SW07563PC46806 47055 YIP/OKC - FLT 511 - DURING APPROACH TO OKC, FLIGHT CREW DISCOVERED LANDING GEAR SELECTOR WOULD NOT MOVE DOWN. ABNORMAL LANDING GEAR EXTENSION PROCEDURES WERE FOLLOWED AND THE GEAR WAS EXTENDED. PRIOR TO CROSSING THE OUTER MARKER, THE LANDING GEAR SELECTOR WAS TRIED AGAIN AND MOVED TO THE DOWN POSITION. AN UNEVENTFUL LANDING WAS MADE. THE LANDING GEAR SELECTOR WAS LUBRICATED AND A DRAIN LINE WAS REPOSITIONED, THE GEAR SELECTOR WAS OPERATED SEVERAL TIMES WITH NO BINDING. THE AIRCRAFT WAS NON-REVENUE FERRIED TO DFW AND A RETRACTION TEST WAS PERFORMED WITH NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950331008181995033100818NM 1995 3 31 MGMA950127 119950218A32602314143 SWITCH BOEING727 727191 1384063NM RT MLG DOOR OUT OF ADJUST A MGMAO OTHER N FALSE WARNING CLCLIMB 1 WP23504MG 19395 AFTER GEAR RETRACTION, RED DOOR LIGHT IN FORWARD PANEL AND AMBER LIGHT ON F/E PANEL ILLUMINATED AS SOON AS GEAR HANDLE SELECTED FROM UP TO OFF. PUT THE GEAR HANDLE TO THE UP POSITION, BOTH LIGHTS WENT OFF. WAITED A FEW MINUTES, THEN PUT HANDLE IN OFF POSITION AND BOTH LIGHTS CAME ON. LEFT THE HANDLE IN UP POSITION FOR REST OF FLIGHT. ADJUSTED RT MLG DOOR SWITCH PER MM 32-62-11 AND LIGHTS OPS CHECK NORMAL. TOTAL TIME: 53675.8 HOURS. TOTAL CYCLERS: 42020. (X) 2L73 4F A3WE 19950331008191995033100819NE 1995 3 31 MGMA950138 219950309A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 1 STALLED A MGMACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP23803MG 45910 REJECTED TAKEOFF IN YIP DUE TO NR 1 ENGINE STALL. RAN UP ENGINE WITH NO OTHER INDICATIONS. TAKEOFF THEN NORMAL. INSPECTED INLET AND TAILPIPE ON NR 1 ENGINE. CHECKED BLEED VALVE SCHEDULING. ALL INDICATIONS NORMAL. TOTAL TIME: 43248.1 HOURS. TOTAL CYCLES: 12471. (X) 2L74 4F4 F 4A25 1E8 19950331008201995033100820NE 1995 3 31 MZZA9510 219950308A7200 ENGINE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 3 FAILED A MZZAEAJ ENGINE SHUTDOWN UNSCHED LANDING DUMP FUEL KJEFLUID LOSS WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 WP1379743 22252 A325 GUM - FLT 956 - DURING CLIMB PASSING 5,000 FEET, NR 3 ENGINE OIL QUANTITY DECREASING THROUGH 2.5 GALLONS, OIL PRESSURE AT 57 PSI, OIL TEMP 120 DEGREES CENTIGRADE. AT 1.6 GALLONS, AIRCRAFT SHUDDERED MODERATELY. NR 3 THROTTLE RETARDED TO CLOSED POSITION WHICH DECREASED VIBRATION. ENGINE FAILURE/FIRE CHECK LIST PERFORMED AND AIRCRAFT RETURNED BACK TO GUAM. ENGINE WINDMILL TIME APPROXIMATELY 12 MINUTES. (X) 2L73 4F4 F A3WE E2EA 19950331008211995033100821NM 1995 3 31 MZZA9511 119950221A522069459345 CABLE BOEING727 727224 1384076NM EMER EXIT STEP BROKEN A MZZAK NONE O OTHER ININSP/MAINT 1 WP1379744 22253 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON RT/LT AFT OVERWING EMERGENCY ESCAPE HATCH STEP FORWARD CABLES. THE DAMAGED CABLE ASSEMBLIES WERE REMOVED AND REPLACED PER B727 MM 52-21-0. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0721100 AND NR 0721101 (SEQ. NR. 02100 AND NR 02101). (X) 2L73 4F A3WE 19950331008221995033100822EU 1995 3 31 VTZA95108 119950313A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU BAGGAGE DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27483UE 898 IAD/MDT - FLT 6496 - DURING TAKEOFF AT 1515 HRS ON 3-13-95, ABORTED TAKEOFF DUE TO POD DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 08515 IAW MEL 52-1 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 08515 BY ADJUSTING THE POD DOOR MICROSWITCH ON 3-15-95. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950331008231995033100823WP 1995 3 31 WTAA950115 219950309A732189737526 FUEL CONTROL BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE OUT OF ADJUST A WTAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP17402UE 734 SFO - LT ENGINE WOULD NOT MAKE FULL POWER DURING CLIMB. COULD NOT REACH MAXIMUM EGT LIMIT. RETURNED TO SFO WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT ENGINE FUEL CONTROL MAXIMUM FUEL FLOW ADJUSTMENT. PERFORMED ENGINE GROUND RUN. MAXIMUM POWER AND EGT LIMITS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19950331008241995033100824SO 1995 3 31 WTAA950118 119950310A3230 RETRACT MECH EMB 120 EMB120RT SO NLG MALFUNCTIONED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17280UE 120090 RDD - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT. MAINTENANCE SERVICED NOSE LANDING GEAR, PW 1973000011, IAW MM 32-21-01. ACCOMPLISHED LANDING GEAR RETRACTION CHECK ON GROUND. LANDING GEAR OPERATION AND POSITION INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950331008251995033100825SO 1995 3 31 WTAA950119 119950310A301029S7D513531 DE-ICE BOOT EMB 120 EMB120RT SO HORIZ STAB WORN A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17451UE 120108 SNA - LEFT INBOARD STABILIZER DE-ICE INOPERATIVE IN-FLIGHT. RETURNED TO STATION WIHTOUT INCIDENT. MAINTENANCE REPLACED LEFT INBOARD STABILIZER DE-ICE BOOT AND PERFORMED OPERATIONAL CHECK OF SYSTEM. AIRFRAME DE-ICE SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950331008261995033100826SO 1995 3 31 WTAA950120 119950312A273112038650001 ACTUATOR EMB 120 EMB120ER 3260203SO HORIZ STAB TRIM LACK OF LUBE A WTAAK NONE J WARNING INDICATION DEDESCENT 1 WP17275UE 120058 LAX - ELEVATOR TRIM STICKING ON DESCENT. LANDED IN LAX WITHOUT INCIDENT. MAINTENANCE INSPECTED AND LUBED BOTH ELEVATOR TRIM ACTUATORS. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. TEST FLIGHT ACCOMPLISHED AND WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950331008271995033100827 1995 3 31 WTAA950122 319950313A6140 WARNING EMB 120 EMB120RT SO AUTOFEATHER SYS ACTIVATED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17268UE 120207 FAT - AUTOFEATHER WARNING DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUN AND OPERATIONAL CHECK OF AUTOFEATHER WARNING SYSTEM. AUTOFEATHER WARNING SYSTEM OPERATIONAL CHECK GOOD. NO SYSTEM FAILURE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950331008281995033100828NE 1995 3 31 WTAA950123 219950313A73103033355 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE CLOGGED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17451UE 120108 FAT - LEFT ENGINE FUEL FILTER INDICATION LIGHT ILLUMINATED DURING CLIMB. TORQUE DROPPED 50 PERCENT. NORMAL OPS. AFTER EEC SELECTED OFF, AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE HIGH PRESSURE AND LOW PRESSURE FUEL FILTERS. PERFORMED ENGINE GROUND RUN. ENGINE OPERATION NORMAL. AIRCRAFT RETURNED TO SERVICE. REF CONTROL NR 95ZZZX1508. (X) 2L72 4T4 TRTA31SO E20NE 19950331008291995033100829WP 1995 3 31 Y2PA95004 119950328A2130 VENT DOOR DOUG DC9 DC915F 3022037WP CABIN OPEN A Y2PAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23196US 47155 MMX - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO MMX. FOUND 'VENT DOOR' IN MAIN CABIN TO BE IN THE OPEN PSOITION. CLOSED THE 'VENT DOOR'. (M) 2L72 4F A6WE 19950407000011995040700001NM 1995 4 7 9505052706 119950327A5313655623620 LONGERON BOEING727 727225 1384077NM FS 688 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND FORWARD CARGO STR 27R AT FS 688 CORRODED. REPAIRED PER NWA EA 27-096506. 2L73 4F A3WE 19950407000021995040700002NM 1995 4 7 9505062706 119950328A5753652163395A RIB BOEING727 727225 1384077NM RT TE MID FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT WING OUTBOARD MID FLAP INBOARD RIB CRACKED. REPAIRED PER NWA EA 27-033511. 2L73 4F A3WE 19950407000031995040700003NM 1995 4 7 9505072706 119950327A5313655623620 LONGERON BOEING727 727225 1384077NM FS 690 CARGO A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND FORWARD CARGO STR 27L AT FS 690 CORRODED. REPAIRED PER NWA EA 27-096504. 2L73 4F A3WE 19950407000041995040700004NM 1995 4 7 9505082277 119950325A5320655612910 SILL BOEING727 727251 138408HNM NR 2 CARGO CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01277US 21156 DURING PERIODIC CHECK, MAINTENANCE FOUND THE NR 2 CARGO DOOR LOWER MAIN SILL OUTBOARD CHORD CORRODED. REPAIRED PER NWA EA 22-096505. 2L73 4F A3WE 19950407000051995040700005NM 1995 4 7 9505092275 119950328A5330 SKIN BOEING727 727251 138408HNM FS 305 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01275US 21154 DURING PERIODIC CHECK, MAINTENANCE FOUND FUSELAGE SKIN AT FS 305 ADJACENT TO NOSE LANDING GEAR WHEEL WELL CORRODED. REPAIRED PER EA 22-96706. 2L73 4F A3WE 19950407000061995040700006NM 1995 4 7 9505102706 119950327A575165217095 FITTING BOEING727 727225 1384077NM INBD AILERON CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND LEFT INBOARD AILERON QUADRANT SUPPORT FITTING CORRODED. REPAIRED PER NWA EA 27-096497. 2L73 4F A3WE 19950407000071995040700007NM 1995 4 7 9505112281 119950328A3350S106 EEL BATTERY BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01281US 21160 DURING THROUGH FLIGHT, FIRST CLASS EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950407000081995040700008NE 1995 4 7 9505122289 219950329A7321 FUEL CONTROL BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN JX WARNING INDICATION ENGINE FLAMEOUT DEDESCENT 1 GL01289US 21377 695258 AS AIRCRAFT STARTED TO DESCEND FROM FL370, THE NR 2 ENGINE FLAMED OUT. THE CREW NOTED '0' FUEL FLOW ON TWO RESTART ATTEMPTS. THE ENGINE WINDMILLED FOR APPROXIMATELY 30 MINUTES WITH AN INDICATED OIL PRESSURE OF 15 PSI. MAINTENANCE REPLACED THE FUEL CONTROL AND PUMP ASSEMBLY. ENGINE CHECKED OK ON RUN-UP. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950407000091995040700009NM 1995 4 7 9505132704 119950330A3260 GEAR LIGHT BOEING727 727225 1384077NM NLG MALFUNCTIONED A NWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL01801EA 22432 DURING APPROACH UPON LANDING GEAR EXTENSION, NOSE GEAR SAFE INDICATION WOULD NOT ILLUMINATE. RECYCLED LANDING GEAR MULTIPLE TIMES TO NO AVAIL. COULD NOT VERIFY NOSE LANDING GEAR POSITION THROUGH VIEWING PORT. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PINNED THE NOSE LANDING GEAR ON THE RUNWAY. FERRIED AIRCRAFT TO MSP. WORK IN PROGRESS. 2L73 4F A3WE 19950407000101995040700010NM 1995 4 7 95UAL737038 119950330A7830 TR LIGHT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT ENGINE ILLUMINATED A UALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP29389UA 24664 RIGHT ENGINE REVERSER LIGHT ON OVERHEAD PANEL CAME ON AT 95 KNOTS ON TAKEOFF. 2L72 4F4 FRTA16WE E2GL 19950407000111995040700011WP 1995 4 7 MEJA9502004 219950314A7320S9412021 PACKING GARRTT 8691691 SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP RH FUEL CONTROL CUT E AMEJAE ENGINE SHUTDOWN M OVER TEMP CRCRUISE 1 SW174206M 2334953 TC230 P54168 FLIGHT 6692, MTY TO SAT, RIGHT ENGINE EGT BEGAN TO RISE. REDUCED POWER AND EGT STARTED TO DECREASE. ADVANCED POWER AND EGT/TORQUE BEGAN TO SURGE. SHUTDOWN ENGINE AND PROCEEDED TO SAT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENCE. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND LEAK ON THE P2 SENSOR. REPLACED O-RING IN ACCORDANCE WITH THE GARRETT MAINTENANCE MANUAL. OPERATIONAL CHECK GOOD. FUNCTIONAL FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19950407000121995040700012SW 1995 4 7 MEJA9502005 119950315A55112743057005 SPAR SPLICE SWRNGNSA227 SA227AC 8780603SW HORIZ STAB CRACKED E AMEJAK NONE O OTHER ININSP/MAINT 1 SW173108X18643 AC517 DURING INSPECTION, MAINTENANCE FOUND THE HORIZONTAL STABILIZER SPAR SPLICE STRAP CRACKED. REMOVED AND REPLACED STRAP IN ACCORDANCE WITH FAIRCHILD AIRCRAFT INCORPORATED APPROVED REPAIR PROCEDURE (ARP) 55-10-9320 REV A. PERFORMED OPERATIONAL CHECK OF THE STABILIZER. NO DEFECTS NOTED. PERFORMED FUNCTIONAL CHECK FLIGHT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950407000131995040700013NM 1995 4 7 MWEA95156 119950329A2560 GIRT BAR DOUG MD88 MD88 3023688NM AFT GALLEY DOOR JAMMED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49782 CREW REPORTS AFT GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR VERY DIFFICULT TO INSTALL AND REMOVE FROM LATCHES. FABRIC FROM THE SLIDE WAS OBSTRUCTING GIRT BAR WHILE ARMING AND DISARMING SLIDE. CLEARED FABRIC. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950407000141995040700014EU 1995 4 7 QXEA9500094 119950330A33501820 EEL LAMP FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 3 AFT EVACUATION LIGHTS IN PASSENGER COMPARTMENT CEILING WERE FOUND INOP. RELAMPED FIXTURES AND AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA20EU 19950407000151995040700015NM 1995 4 7 QXEA9500095 119950330A335082410162007 EEL CONTROL BOX DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTION A QXEAK NONE L NO TEST CRCRUISE 1 NM09827PH 275 EMERGENCY LIGHTING ILLUMINATED IN FLIGHT. CREW RECYCLED BUT PROBLEM REOCCURED WITHIN A FEW MINUTES. REPLACED EMERGENCY LIGHT CONTROL BOX, GROUND TESTED AND RELEASED AIRCRAFT FOR SERVICE. 2H72 4T RTA13NM 19950407000161995040700016EU 1995 4 7 WWMA9500021 119950203A2150 OIL SYST BAG JETSTMJETSTM3201 1500217EU ACM OVER SERVICED I WWMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP15958AE 958 FLIGHT NR 5040 (SBP/LAX) PILOT REPORTED THAT THE LEFT BLEED CAUSED AN OIL SMELL IN CABIN. MAINTENANCE FOUND ACM OVERSERVICED. DESERVICED EXCESSIVE OIL. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000171995040700017EU 1995 4 7 WWMA9500022 119950205A3234137908D401 SELECTOR VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR DEFECTIVE I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15961AE 961 FLIGHT NR 5207 (LAX/SMX) PILOT REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE THREE GREEN GEAR INDICATIONS AND THE HYDRAULIC FLUID PRESSURE WERE NORMAL. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE FOUND THE EMERGENCY GEAR RELEASE VALVE RESET PIN POPPED. MAINTENANCE REPLACED THE SELECTOR VALVE. THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000181995040700018EU 1995 4 7 WWMA9500023 119950214A26122TP17 FIRE SWITCH BAG JETSTMJETSTM3201 1500217EU INSTR PANEL DEFECTIVE I WWMAO OTHER N FALSE WARNING CRCRUISE 1 WP15957AE 957 FLIGHT NR 5084 (SBP/LAX) PILOT REPORTED THAT AFTER 30 MINUTES OF FLIGHT AT 11,000 FEET THE LEFT ENGINE FIRE LIGHT ILLUMINATED. ALL ENGINE INSTRUMENTS INDICATED NORMAL. NO FIRE WAS PRESENT. MAINTENANCE INPECTED THE LEFT ENGINE FIRE SENSOR AND FOUND NO FAULTS. WHILE TESTING THE SYSTEM MAINTENANCE FOUND THE LEFT TEST SWITCH TO BE STICKY. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FIRE WARNING TEST SWITCH. ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000191995040700019EU 1995 4 7 WWMA9500024 119950222A2121 AC FAN BAG JETSTMJETSTM3201 1500217EU CABIN FAILED I WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP15951AE 951 FLIGHT NR 5164 (SFO/MRY) PILOT REPORTED THAT THE AC FAN, WHEN ON HAD A STRONG SMELL OF SOMETHING ELECTRICAL BURNING. WHEN SYSTEM WAS TURNED OFF THE SMELL WENT AWAY. THE AIRCRAFT WAS DEFERRED PER FLIGHT CREW, MEL ITEM 21-13. MAINTENANCE COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000201995040700020NE 1995 4 7 WWMA9500025 219950224A7200CT79B ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED I WWMACD ABORTED TAKEOFF RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP15341SB10923 340B341 GEE785119 FLIGHT NR 5378 (FMN/LBB/DFW), PILOT REPORTED AFTER MAXIMUM POWER TAKEOFF,F HE CALLED FOR CLIMB POWER AND CLIMB CHECKS AT ACCELERATION ALTITUDE. THE FIRST OFFICER ROTATED CTOT KNOB AND THE RIGHT ENGINE BEGAN TO COMPRESSOR STALL. THE OVERTEMP LIGHT ILLUMINATED AND THE FIRST OFFICER STATED THAT THE RIGHT ENGINE HAD SHUTDOWN. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND THE HOT SECTION SHOWED SIGNS OF DISTRESS. MAINTENANCE REPLACED THE RIGHT ENGINE AND PERFORMED ALL ASSOCIATED CHECKS. THE AIRCRAFT WAS RELEASE TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950407000211995040700021EU 1995 4 7 WWMA9500026 119950306A21507769105 ACM SAAB SF340 340B 7860101EU RT WING FAILED A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15256AE4188 340B256 FLIGHT 5124 - ABI/DFW - PILOT REPORTED A SLIGHT SMELL OF SMOKE AND THE RIGHT BLEED FAULT LIGHT ILLUMINATED. MAINTENANCE FOUND THE RIGHT ACM HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950407000221995040700022EU 1995 4 7 WWMA9500027 119950308A2121EVCTA465A RECIRC FAN SAAB SF340 340B 7860101EU CABIN FAILED I WWMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP15348SB 340B348 FLIGHT 5183 DFW/TXK, PILOT REPORTED THAT DURING PREFLIGHT INSPECTION HE BECAME AWARE OF A SMELL OF SMOKE IN THE CABIN AREA. MAINTENANCE PERSONNEL WERE SUMMONED AND DETERMINED THE PROBLEM TO BE A FAULTY RT COCKPIT RECIRCULATION FAN. THE FAN WAS REPLACED, OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA52EU 19950407000231995040700023EU 1995 4 7 WWMA9500028 119950309A3260 DOWNLOCK SWITCH SAAB SF340 340B 7860101EU LANDING GEAR OUT OF ADJUST I WWMAO OTHER N FALSE WARNING CLCLIMB 1 WP15247AE 340B247 FLIGHT 5106 MKE/ORD, PILOT REPORTED THAT AFTER TAKING OFF AND UPON RETRACTING THE GEAR THE LANDING GEAR INTRANSIT LIGHT FAILED TO EXTINGUISH. THE AIRCRAFT LANDED IN ORD WITHOUT INCIDENT. MAINTENANCE PERSONNEL CORRECTED THE PROBLEM BY ADJUSTING THE DOWNLOCK SWITCH AND THE RIGGING OF THE GEAR DOORS. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950407000241995040700024EU 1995 4 7 WWMA9500029 119950311A29101379305A155 FLEX HOSE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR BROKEN I WWMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP15958AE 958 FLIGHT NR 3372 (LAX/OXR), PILOT REPORTED DURING FLIGHT THE HYDRAULIC GAUGES WENT TO ZERO AND WAS CONFIRMED WHEN THE GEAR OR FLAP EXTENDED. THE MAIN BRAKE PRESSURE WAS AROUND 600 PSI AND THE EMERGENCY WAS 2000 PSI. THE GEAR WAS PUMPED DOWN USING THE EMERGENCY EQUIPMENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE RIGHT MAIN GEAR UPLINE BROKEN. MAINTENANCE REMOVED AND REPLACED MLG UPLINE IAW AMM 32-10-31 AND PERFORMED GEAR RETRACTION CHECK. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000251995040700025EU 1995 4 7 WWMA9500030 119950312A2120 AIR DISTR SAAB SF340 340B 7860101EU COCKPIT ODOR I WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP15338SB 340B338 FLIGHT 5382 (ABI/DFW), PILOT REPORTED SMELLING A BURNING OIL ODOR COMING FROM THE BLEED AIR SYSTEM. MAINTENANCE RAN THE RIGHT AND LEFT ENGINES FOR 30 MINUTES WITH ACMS ON AND THE BLEED VALVES OPEN. NO ODOR NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950407000261995040700026EU 1995 4 7 WWMA9500031 119950312A3234AIR873601 SELECTOR VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR DEFECTIVE I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15952AE 952 FLIGHT NR 3241 (LAX/CLD), PILOT REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. THE AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACED THE NON RETURN VALVE AND THE EMERGENCY HYDRAULIC SELECTOR VALVE IAW JSM 29-00. MAINTENA NCE PERFORMED MULTIPLE GEAR SWINGS IAW JS32 MM. THEY COULD NOT DUPLICATE THE PROBLEM; OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. P/N CHANGED AIR873601 & 7448. 2L72 4T RTA56EU 19950407000271995040700027EU 1995 4 7 WWMA9500032 119950315A32309902A SHUTTLE VALVE BAG JETSTMJETSTM3201 1500217EU LT MLG DEFECTIVE I WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15952AE 952 FLIGHT 3348 SBP/LAX, PILOT REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THAT THE LEFT MAIN LANDING GEAR RADIUS ROD SHUTTLE VALVE HAD FAILED. THE VALVE WAS REPLACED, GEAR SWINGS WERE PERFORMED AND OPERATIONAL CHECKS OF THE SYSTEM WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950407000281995040700028EU 1995 4 7 WWMA9500033 119950329A2930 INDICATION SAAB SF340 340B 7860101EU HYD SYST MALFUNCTIONED I WWMAO OTHER N FALSE WARNING APAPPROACH 1 WP15352SB 340B352 FLT 5201 - DFW-CLL - PILOT REPORTED THAT WHILE ON APPROACH, INSTRUMENT INDICATIONS SHOWED A COMPLETE LOSS OF HYDRAULIC PRESSURE. THE LANDING GEAR EMERGENCY EXTENTION HANDLE WAS PULLED AND THE SEPARATION BOLTS ACTIVATED, MOVING THE GEAR INTO DOWN AND LOCKED POSITION. MAINTENANCE PERSONNEL INSPECTED THE HYDRAULIC SYSTEM INCLUDING PUMP AND RESERVOIR, AND FOUND NO EVIDENCE OF LEAKS. THE RESERVOIR WAS FULL AND THE SYSTEM WORKED PROPERLY. THE LANDING GEAR WAS CYCLED IN EXCESS OF TWENTY TIMES WITH NO PROBLEMS OR MALFUNCTIONS NOTED. ALL OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950407000291995040700029NM 1995 4 7 95ZZZZ188 119950228A5311 FRAME BOEING727 7272Q9 138448MNM FS 300-320 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, INSIDE STATION 300-320, CHORD BELOW STRINGER 26R, SHOWS CORROSION AT AND UNDER LEVELING COMPOUND. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. CUT OUT DAMAGED SECTION OF CHORD AND REPAIRED PER SRM 51-40-4. DIM 16 INCHES BY 4 INCHES BY 4 INCHES 7075-T6 .125 CUT FRAME FOR ACCESS AND REPAIRED PER SRM 53-10-4, FRAME REPAIR DIM 12 INCHES BY 4 INCHES BY 1 INCH 7075-T6 .063. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000301995040700030NM 1995 4 7 95ZZZZ189 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1176 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT BAG BIN STRINGER 27R HAS HEAVY CORROSION AT STATION 1176 APPROXIMATELY. REMOVED AND REPLACED STRINGER 27R FROM STATION 1183 TO 1144 AS PER SRM 51-10-1 PAR 4. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3 APPROX 54 INCHES BY 12 INCHES. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000311995040700031NM 1995 4 7 95ZZZZ190 119950228A5315 FLOOR BEAM BOEING727 7272Q9 138448MNM BS 1130 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, FOUND CORROSION ON FLOOR BEAM RT BS 1130 BL 0 TO RBL 64 AND ON LEFT SIDE BS 1130 BL 0 TO LBL 26. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS. TREATED AND PRIMED AREA PER SRM 51-10-2. FABRICATED AND INSTALLED REPAIR AT RBL 27 AND LBL 28 AND 33 PER SRM 51-40-4. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000321995040700032NM 1995 4 7 95ZZZZ191 119950228A5315 FLOOR BEAM BOEING727 7272Q9 138448MNM FS 1030 HOLE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, STATION 1030 FLOOR BEAM TOP FLANGE HAS DRILLED HOLE AT CENTER OF FLANGE 'T' HOLE CONTINUES DOWN LOWER LEG OR WEB OF BEAM APPROXIMATELY .75 OF AN INCH. FABRICATED REPAIR PARTS PER SRM 53-10-8 AND 51-40-2. INSTALLED PARTS PER SRM 53-10-8. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407000331995040700033NM 1995 4 7 95ZZZZ192 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1183 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO FUSELAGE STATION 1183 CIRCUMFERENTIAL 'T' FITTING AND STRINGER BADLY CORRODED AT STRINGER 29L. REMOVED CORROSION ON FS 1183, OUT OF LIMTS (APPROX .080). INSTALLED CHORD ANGLE REPAIR AS PER (A/E NR LBN-MLB DRAWING). REMOVED AND REPLACED STRINGER 'T' FITTING AS PER SRM 51-10-1 PAR 4. INSTALLED STRINGER SPLICE (APPROX 10 INCHES) AS PER SRM 53-10-3 THICKNESS .090. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000341995040700034NM 1995 4 7 95ZZZZ193 119950228A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM FS 1150-1170 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO, SURFACE CORROSION ON INTERCOSTAL LOWER FLANGE BETWEEN STRINGER 29R AND STRINGER 28R BETWEEN FS 1150 AND FS 1170. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED WEB REPAIR AT PREVIOUS CRACK PER SRM 51040-2, INSTALLED INTERCOSTAL PER SRM 51-30-2. TOTAL CYCLES 29,577 2L73 4F RTA3WE 19950407000351995040700035NM 1995 4 7 95ZZZZ194 119950228A5320 FLOOR SUPPORT BOEING727 7272Q9 138448MNM FS 1170 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO, SURFACE CORROSION AROUND NUT PLATES AT LOWER SURFACE OF FLOOR SUPPORT ANGLES AT FS 1170 LBL 5 AND RBL 8. REMOVED CORROSION PER SRM 51-10-6 AND FOUND OUT OF LIMITS. INSTALLED ANGLE REPAIR PER SRM 51-40-4, MAT USED .050 2 INCHES BY 8 INCHES RBL 8 (.004 REMOVED LBL 5). TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000361995040700036NM 1995 4 7 95ZZZZ195 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1070-1090 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO, STRINGER 30 IS CORODED AND CRACKED INSIDE STRINGER CHANNEL BETWEEN FS 1070 AND FS 1090. CORROSION FOUND OVERLIMIT. REMOVED FASTENERS FOR REPAIR STRINGER. CUT OUT STRINGER DAMAGE AREA AND FABRICATED PART PER SRM 53-10-3, 20 INCHES 1498-131 .090 7075-T62 13 INCHES 1498-145 .071 7075-T62. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000371995040700037NM 1995 4 7 95ZZZZ196 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1050-1070 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO, CORROSION AT SEVERAL AREAS IN STRINGER 30 CHANNEL BETWEEN FS 1050 AND FS 1070. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA AND FABRICATED PART PER SRM 53-10-3 2 INCHES .71 7075-T62 AND 12 INCHES .90 7075-T62, TREATED AND PRIMED PER SRM 51-10-2. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000381995040700038NM 1995 4 7 95ZZZZ197 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1030-1050 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO CORROSION INSIDE STRINGER AT STRINGER 30 BETWEEN FS 1030 AND FS 1050. CUT OUT STRINGER DAMAGED AREA AND FABRICATED PART IAW SRM 53-10-3 AND INSTALLED 20 INCHES STRINGER BAC 1498-131 .71 7075-T6. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000391995040700039NM 1995 4 7 95ZZZZ198 119950228A5313 STRINGER BOEING727 7272Q9 138448MNM FS 1010 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32255 21930 DURING D-CHECK, AFT CARGO HEAVY CORROSION IN STRINGER CHANNEL AND STRINGER CRACKED BELOW FUSELAGE FRAME 1010 AT STRINGER 29L. REMOVED SPLICE PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS .002, TREATED ALODINE AND PRIMED PER SRM 51-10-2. INSTALLED SPLICE AND FASTENERS PER SRM 53-10-4. TOTAL CYCLES 29,577. 2L73 4F RTA3WE 19950407000401995040700040WP 1995 4 7 95ZZZZ199 119950315A57111528363250 SPAR WEB LKHEED1011 10113851 5265010WP WS 325-346 CRACKED A WRNAK NONE K FLUID LOSS ININSP/MAINT 1 SO05311EA 193A1012 DURING FUELING AIRCRAFT IN BQN, FUEL WAS NOTICED LEAKING FROM RT MLG TRUNNION AREA. INSPECT AREA AND FOUND APPROX 20 INCH CRACK FROM THE UPPER SPAR CAP AT APPROX WING STATION 325 TO THE MLG FORGING AT APPROX WING STATION 346 ON THE REAR SPAR WEB. AIRCRAFT DEFUELED AND FUEL CELL ENTRY MADE TO PERFORM NDT INSPECTIONS REQUIRED BY LOCKHEED. TEMPORARY REPAIR ENGINEERED BY LOCKHEED BEING INSTALLED FOR FERRY FLIGHT TO DELTA AIR LINES IN ATLANTA, GA. 2L73 4F A23WE 19950407000411995040700041WP 1995 4 7 95ZZZZ200 219950216A726131024111 TUBE ASSY SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE CRACKED A EQGAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW19343AE4874 AC554 P44370 APPROXIMATELY 20 MINUTES INTO CRUISE FLIGHT THE LEFT ENGINE OIL PRESSURE STARTED DROPPING. THE PILOT MADE A PRECAUTIONARY SHUTDOWN AND RETURNED TO HOT. THE LOW PRESSURE OIL LINE GOING FROM THE PROP PITCH CONTROL TO THE GOVERNOR WAS FOUND TO BE LEAKING. THE LINE WAS REPLACED AND GROUND RUNS CHECKED NORMAL. (Z) 1L72 4T4 T A8SW E4WE 19950407000421995040700042NM 1995 4 7 95ZZZZ201 119950201A2720 CONTROL BOEING757 7572Q8 1384972NM RUDDER MALFUNCTION A AAMTAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL11755AT 24965 MDW - CLIMBING OUT OF 30,000 FEET. AIRCRAFT ATTEMPTED TO ROLL RIGHT, RUDDER RATIO FLICKERED, THUMPING FELT IN RUDDER PEDALS AND FLIGHT ATTENDANT HEARD LOUD NOISE IN TAIL SECTION. FLT CONTINUED TO FLL. PERFORMED BITE CHECK OF RUDDER RATIO PER FIN 27-09-00 FIG 103 BLOCK I, SYSTEM CHECKS NORMAL. (Z) 2L72 4F RTA2NM 19950407000431995040700043 1995 4 7 C2XA95CL043 419950307A34426222504001 ANTENNA EMB 120 EMB120RT SO NOSE INOPERATIVE A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW092770712006 1227 120095 FLT NR 3223 - CLE-CLE - RADAR INOP. TILT DOESN'T WORK AND STABILIZATION APPEARS NOT TO WORK. WON'T PAINT ANY WEATHER. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR ANTENNA. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950407000441995040700044EU 1995 4 7 C2XA95CL044 119950311A28202402823 FLOW VALVE AEROSPATR42 ATR42300 8680920EU NR 2 FUEL TANK MALFUNCTION A AC2XAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SW0916824 166 FLT NR 3468 - ALB-EWR - ON DESCENT INTO EWR THE NR 2 ENGINE FAILED. THIS TOOK PLACE SHORTLY AFTER TERMINATING A FUEL CROSSFEED OPERATION. EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE FUEL FILTERS AND MOTIVE FLOW VALVE. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT WAS THEN RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950407000451995040700045SO 1995 4 7 C2XA95CL045 119950311A575112008080001 AILERON EMB 120 EMB120RT SO LT AILERON HOLE IN SKIN A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 FLT NR 3362 - CLE IND - ON POST FLIGHT WALKAROUND FOUND HOLE IN LEFT AILERON. FERRIED AIRCRAFT TO CLE. MAINTENANCE REMOVED AND REPLACED THE LEFT AILERON IAW EMB MM 27-11-02. RELEASED AIRCRAFT FOR TEST FLIGHT. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950407000461995040700046NE 1995 4 7 C2XA95CL046 219950312A73217863927 FUEL CONTROL AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 2 ENGINE MALFUNCTION A AC2XAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 SW09318078531 6015 F2540 078 120516 FLT NR 3470 - ALB-ALB - NR 2 ENGINE FAILED AFTER TAKEOFF. FIRST PARTIAL POWER LOSS, THEN FULL POWER SURGED BACK, THEN TOTAL POWER LOSS, NO COCKPIT FIRE INDICATIONS. MAINTENANCE REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT AND FUEL PUMP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2H72 4T4 TRTA53EU E20NE 19950407000471995040700047NE 1995 4 7 C2XA95CL047 219950312A73145009986C FUEL PUMP AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 2 ENGINE MALFUNCTION A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT TOTAKEOFF 1 SW09318078257 2071 1857 078 120516 FLT NR 3470 - ALB-ALB - NR 2 ENGINE FAILED AFTER TAKEOFF. FIRST PARTIAL POWER LOSS, THEN FULL POWER SURGED BACK, THEN TOTAL POWER LOSS, NO COCKPIT FIRE INDICATIONS. MAINTENANCE REMOVED AND REPLACED NR 2 FUEL CONTROL UNIT AND FUEL PUMP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2H72 4T4 TRTA53EU E20NE 19950407000481995040700048EU 1995 4 7 C2XA95CL048 119950317A7500 BLEED SYS AEROSPATR42 ATR42320 8680930EU RIGHT ENG MALFUNCTION A C2XAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW0925811134169187 094 FLT NR 3944 - EWR-EWR - ON TAXI OUT RECEIVED ELECTRIC SMOKE WARNING. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND RIGHT BLEED SYSTEM CAUSING ELECTRIC SMOKE WARNING. PLACED ON MEL 36-11-2 PLACARD NR 782526. DURING OVERNIGHT MAINTENANCE IN BTV ON 03/17/95, MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPS AND LEAK CHECKS GOOD. MEL 36-11-2 WAS REMOVED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950407000491995040700049SO 1995 4 7 C2XA95CL049 119950322A7931APT79100080D TRANSDUCER EMB 120 EMB120RT SO LT ENGINE BROKEN A C2XAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SW091572110091 282111328 120160 FLT NR 3362 - CLE-CLE - DURING CLIMB, LEFT ENGINE OIL PRESSURE PEGGED AT 80 PSI. RETARDED THROTTLE TO REDUCE BELOW TO 70 PSI. AIRCRAFT RETURNED TO CLE. MAINTENANCE INSPECTED AND FOUND THE OIL PRESSURE TRANSDUCER BROKEN. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE TRANSDUCER IAW EMB120 MM 79-31-10. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950407000501995040700050SO 1995 4 7 C2XA95CL050 119950322A323012038594001 CONTROL HANDLE EMB 120 EMB120RT SO COCKPIT MALFUNCTION A C2XAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SW09127159597 120125 FLT NR 3142 - DTW-CLE - AFTER COMPLETION OF PARKING CHECKLIST GEAR HANDLE RETRACTED ON ITS OWN. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW EMB-120 MM 32-31-03. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950407000511995040700051EU 1995 4 7 C2XA95IA035 119950311A5410S5421020001100 MOUNT AEROSPATR42 ATR42320 8680930EU LT NACELLE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917831 185 IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE INBOARD TRUSS MOUNT MIDDLE TUBE WAS FOUND TO BE CHAFED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MOUNT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. REF ATR MM 54-21-61-DVI. (Z) 2H72 4T RTA53EU 19950407000521995040700052EU 1995 4 7 C2XA95IA036 119950309A271182363 ACTUATOR AEROSPATR42 ATR42320 8680930EU LT WING AIL WORN A C2XAK NONE O OTHER ININSP/MAINT 1 SW09978415609 280 IAH - DURING INSPECTION CHECK '3C' ZONAL INSPECTION OF LEFT AILERON TRIM TAB, FOUND ABNORMAL WEAR AT TRIM ACTUATOR FORWARD ATTACHMENT. DISASSEMBLED CLEANED AND INSPECTED, FOUND ACTUATOR FORWARD ATTACHMENT FITTING HOLES ELONGATED. REPLACED TRIM ACTUATOR AND ATTACHMENT HARDWARE, PERFORMED OPERATIONAL CHECKS. WORK PERFORMED IAW ATR 42 MM JIC 27-12-71. TOTAL CYCLES 6,468. 2H72 4T RTA53EU 19950407000531995040700053EU 1995 4 7 C2XA95IA037 119950309A53476022457 SEAT TRACK AEROSPATR42 ATR42320 8680930EU FA SEAT LT CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0997841 280 IAH - DURING INSPECTION CHECK '3C', FOUND FLIGHT ATTENDANT SEAT LEFT ATTACHMENT TRACK CORRODED. INSPECTED AND FOUND CORROSION PITTING TO BE BEYOND LIMITS. REPLACED SEAT TRACK IN ACCORDANCE WITH COEX EX NR 5340-01004. (Z) 2H72 4T RTA53EU 19950407000541995040700054EU 1995 4 7 C2XA95IA038 119950308A5330S53171501203 SKIN AEROSPATR42 ATR42320 8680930EU FWD FUSELAGE DENTED A C2XAK NONE C F.O.D. APAPPROACH 1 SW0915823 165 PUD - FLT NR 3533 - PILOT REPORTED THAT UPON APPROACH, THE AIRCRAFT SUFFERED BIRD STIKES. THE AIRCRAFT LANDED AT THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A BIRD STRIKE INSPECTION AND FOUND THE RIGHT FORWARD LATERAL FUSELAGE SKIN DAMAGED. THE AIRCRAFT WAS FERRIED TO IAH. IAH MAINTENANCE PERFORMED A REPAIR BY APPLYING AN INTERNAL DOUBLER TO THE AFFECTED SKIN. THE REPAIR IS CONSIDERED INTERIM UNITL NEXT C-CHECK. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH CONTINENTAL EXPRESS EC 5330-01075, ORIG. (Z) 2H72 4T RTA53EU 19950407000551995040700055SO 1995 4 7 C2XA95IA040 119950321A323112012347001 LATCH EMB 120 EMB120RT SO LT GEAR DOOR BROKEN A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0915725 120173 IAH - FLT 2522 - PILOT REPORTED THAT WHEN THE GEAR WAS RETRACTED, THE LEFT MAIN GEAR DOOR REMAINED OPEN. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR FORWARD INBOARD DOOR LATCH. THE GEAR DOOR WAS SATISFACTORILY OPERATIONAL TESTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950407000561995040700056WP 1995 4 7 IXXA199520 119950318A3310BA171 BALLAST DOUG DC8 DC863 302198AWP COCKPIT LIGHTS FAILED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL23788AL 45999 ON TAXI OUT AT DIA, THE COCKPIT FLOURSCENT LIGHTING BECAME INOPERATIVE, FOLLOWED BY THE SMELL OF AN OVERHEATED BALLAST IN THE COCKPIT. MAINTENANCE IN DIA DETERMINED THAT A LIGHTING BALLAST HAD FAILED. THE FLOURSCENT LIGHT WAS DEFERRED, AND THE AIRCRAFT RETURNED TO SERVICE. (Z) 2L74 4F 4A25 19950407000571995040700057NM 1995 4 7 USAA950143 119950216A3397 WIRE BOEING737 737201 1384454NM EMERG LIGHT SYS BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19232US 22018 LGA - EMERGENCY EXIT LIGHTING AT SEATS REMAIN ON WHENEVER SWITCH IS PLACED IN ARM POSITION. MAINTENANCE FOUND CHARGE/ON WIRE BROKEN. SPLICED IN NEW WIRE. OPS CHECKS OK. (Z) 2L72 4F A16WE 19950407000581995040700058EU 1995 4 7 USAA950207 119950304A3213200633202 TORQUE LINK ROTOL 200739003 FOKKERF28 F28MK4000 4990810EU LT UPPER BROKEN A USAAO OTHER O OTHER LDLANDING 1 EA19479AU XC90171 11228 HTS - FLT 1028 - ON TOUCHDOWN, AIRCRAFT VEERED TO THE LEFT AND BOTH LEFT MAIN TIRES CAME OFF. AN EMEGENCY EVACUATION WAS NOT NECESSARY. NO INJURIES WERE REPORTED. MAINTENANCE REPLACED THE LEFT UPPER TORQUE LINK. (Z) 2L72 4F RTA20EU 19950407000591995040700059EU 1995 4 7 USAA950226 119950125A5320 SKIN FOKKERF28 F28MK4000 4990810EU STA 2422-2650 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19499US28785 11182 PIT - DURING SCHEDULED STRUCTURES VISIT FOUND MULTIPLE SMALL CRACKS TOTALING 3 INCHES IN THE NOSE GEAR BAY TOP COVER STATION 2422 TO 2650. REF SIP 53-10-10 (EDDY CURRENT). STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-02-18. (Z) 2L72 4F RTA20EU 19950407000601995040700060EU 1995 4 7 USAA950227 119950218A5312 BEAM FOKKERF28 F28MK4000 4990810EU AFT PRESS BLKHD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU21583 11222 PIT - DURING SCHEDULED STRUCTURES VISIT (SIP), FOUND 2 INCH CRACK IN AFT PRESSURE BULKHEAD HORIZONTAL BEAM III LOWER RADIUS AT CENTER OF BEAM. EDDY CURRENT REF SIP 53-10-03. STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PATCH, REPAIR ANGLES (2EACH) AND REAR FACE STRIP PER USAIR EA 29615. (Z) 2L72 4F RTA20EU 19950407000611995040700061EU 1995 4 7 USAA950228 119950213A5320 ANGLE FOKKERF28 F28MK4000 4990810EU FRAME 1550 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU21538 11222 PIT - DURING SCHEDULED STRUCTURES VISIT (SIP), FOUND A 5 INCH CRACK IN THE FWD PRESSURE BULKHEAD LOWER CONNECTION ANGLE AT FRAME 1550 BETWEEN STA 72 AND 73. (REF SIP 53-10-06). STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER SRM 53-11-00 AND USAIR EA 29585. (Z) 2L72 4F RTA20EU 19950407000621995040700062EU 1995 4 7 USAA950229 119950216A5330 SKIN FOKKERF28 F28MK4000 4990810EU SED UPPER FWD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU21538 11222 PIT - DURING RESCHEDULED STRUCTURES VISIT (SIP), FOUND A .375 INCH CRACK IN THE SE DOOR OPERATURE IN THE UPPER FWD CORNER. (REF SIP 53-10-20) EDDY CURRENT INSPECTION. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-02-16 AND USAIR EA NR 29601. (Z) 2L72 4F RTA20EU 19950407000631995040700063EU 1995 4 7 USAA950230 119950120A5340 ANGLE FOKKERF28 F28MK4000 4990810EU RT VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19481US18603 11230 PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 55-30-01 AND FOUND 2 .5 INCH CRACKS IN RT SIDE CONNECTION ANGLE AT VERTICAL STABILIZER TO FUSELAGE AT 50 PERCENT SPAR. CUT OUT CRACK SECTION OF ANGLE AND ACCOMPLISHED SPLICE REPAIR PER SRM 55-31-00. (Z) 2L72 4F RTA20EU 19950407000641995040700064EU 1995 4 7 USAA950231 119950120A5320 CLIP FOKKERF28 F28MK4000 4990810EU FRAME 3450 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19481US18603 11230 PIT - DURING FC-5 CHECK INSPECTION ACCOMPLISHED SIP 53-10-09 AND FOUND ONE .5 INCH CRACK RT AISLE OF MAIN FRAME CLIP 3450 40 INCHES ABOVE FLOOR LEVEL. REMOVED AND REPLACED CLIP PER SRM 53-02-12 FIG 6 AND USAIR EO 5391L681. (Z) 2L72 4F RTA20EU 19950407000651995040700065EU 1995 4 7 USAA950234 119950311A3350900835A BATTERY PACK FOKKERF28 F28MK4000 4990810EU ROWS 1, 2, 3 INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19494US 11167 PIT - FLT 0680 - THE EMERGENCY STRIP LIGHTS AT ROWS 1, 2 AND 3 WAS INTERMITTENT. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (Z) 2L72 4F RTA20EU 19950407000661995040700066NM 1995 4 7 VTZA95109 119950319A32605352011 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM COCKPIT OUT OF ADJUST A VTZAL ABORTED APPROACH O OTHER APAPPROACH 1 EA27417AW 285 FLT NR 6345 - IAD-LGA - ABORTED THE APPROACH DUE TO THE LEFT MAIN GREEN PRIMARY INDICATION NOT ILLUMINATING. SECONDARY INDICATION CHECKED GOOD. AIRCRAFT LANDED WITH NO FURTHER INCIDENCE. MAINTENANCE FOUND THE LIGHT LENS ASSEMBLY INTERFERING WITH THE LAMP. (Z) 2H72 4T RTA13NM 19950407000671995040700067WP 1995 4 7 VTZA95110 219950321A732021188407 IEC CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33110U 01514WP RT ENGINE DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27312UE 41025 FLT NR 6319 - IAD-CLE - ABORTED TAKEOFF DUE TO THE IEC LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE MOISTURE FROM THE ENRICH TORQUE MOTOR CANNON PLUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T4 TRTA41NM E4WE 19950407000681995040700068EU 1995 4 7 95ZZZX1521 219950221A7530JR21959 STRAP GULSTMG1159 G1159 3953505SO RROYCESPEY SPEY5118 54523EU BLEED VALVE FRACTURED A BQVACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA0158JF 13679 65 8655 ENGINE WOULD NOT DEVELOP TAKEOFF THRUST. BLEED VALVE STRAP FOUND FRACTURED. AN EVALUATION (CONDITION REPORT) INDICATES FAILURE DUE TO FLUTTER AND HIGH-CYCLE FATIGUE BROUGHT ABOUT BY EXCESSIVE LOADING OF ONE OR MORE BLEED VALVE SPHERICAL BEARINGS. THIS APPEARS TO BE AN ISOLATED INCIDENT. IMPROPER ADJUSTMENT DURING OVERHAUL MAY HAVE BEEN A FACTOR. 2L72 4F4 FRTA12EA E2EU 19950407000691995040700069SO 1995 4 7 95ZZZX1522 119950208A54001159B2190120 ANGLE GULSTMG1159 G1159A 3970109SO LT PYLON CRACKED A KKYAK NONE O OTHER ININSP/MAINT 1 NE03270MC2798 374 DURING AN INSPECTION OF THE LEFT PYLON, A .50 INCH CRACK WAS DISCOVERED IN THE PYLON LEADING EDGE ATTACHMENT ANGLE (PN 1159 B21901-20). THE ANGLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A12EA 19950407000701995040700070WP 1995 4 7 95ZZZX1523 119950207A3240305323001 MANIFOLD DOUG DC8 DC873F 302199FWP BRAKE SYSTEM CRACKED A SRAAK NONE JK WARNING INDICATION FLUID LOSS LDLANDING 1 SO19875SJ 46063 SEATTLE - FLT 808 - ON LANDING, AIRCRAFT HAD NO BRAKE PRESSURE ON RT MLG. COMPLETE LANDING WITH LEFT BRAKE AND REVERSE THRUST. FOUND BRAKE POWER VALVE MANIFOLD CRACKED. REPLACED UNIT AND REPLENISHED FLUID, SYSTEM OPS CHECKED GOOD. 2L74 4F RT4A25 19950407000711995040700071NM 1995 4 7 95ZZZX1524 119950302A575565B0225041 SPOILER BOEING747 747122 1384872NM NR 2 POSITION DAMAGED A AP5CAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP23853FT 19753 JFK - ON CLIMB-OUT, SIGNIFICANT FLUTTER WAS FELT AND HEARD DURING LEFT AND RIGHT TURNS. THIS HAPPENED AFTER FLAP RETRACTED. APPEARED OKAY ON DESCENT. AT LAX, CHECKED FLIGHT CONTROLS FOR CORRECT FAIR POSITION AND OPERATION, CHECKED AUXILIARY STRUCTURE AND DOORS. CHECKED CORRECT OPERATION OF AILERON LOCKOUT SYSTEM, ALL CHECKED NORMAL. DURING FOLLOW-UP POST FLIGHT INSPECTION AT HNL, FOUND NR 2 SPOILER PANEL DAMAGED AND DAMAGE TO TRAILING EDGE FLAPS. REPLACED SPOILER AND ACCOMPLISHED INTERM REPAIRS TO LT OUTBOARD FLAP ASSY. 2L74 4F A20WE 19950407000731995040700073NE 1995 4 7 95ZZZX1526 119950131A261230326E7 AMPLIFIER SKRSKYS76 S76 8143010NE FIRE DETECTOR MALFUNCTION A ALGAO OTHER N FALSE WARNING APAPPROACH 1 SW035446E20256 760175 DURING APPROACH, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. NO OTHER INDICATIONS OF FIRE WERE NOTED. THE AIRCRAFT MADE AN UNEVENTFUL LANDING AND WAS SHUT DOWN. NR 1 ENGINE FIRE DETECTOR AMP WAS FOUND BAD. REPLACED AMP. GROUND CHECK, OKAY. 1G72 3U H1NE 19950407000741995040700074NE 1995 4 7 95ZZZX1527 119950120A26126555004023103 AMPLIFIER SKRSKYS76 S76 8143010NE FIRE DETECTOR MALFUNCTION A ALGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW035446E 2453 760175 AFTER DEPARTURE, NR 2 ENGINE FIRE LIGHT ILLUMINATED. THERE WAS NO SMOKE VISIBLE, NO SMELL, AND NO ERRATIC ENGINE INDICATIONS. ACFT RETURNED FOR UNEVENTFUL LANDING. FIRE DETECTOR AMPLIFIER WAS REPLACED. SYSTEM OPS CHECK AND TEST OKAY. AWAITING DETAILS FROM REPAIR FACILITY ON AMPLIFIER DEFECTS. 1G72 3U H1NE 19950407000751995040700075EU 1995 4 7 95ZZZX1528 119950216A7110 COWL LATCH SAAB SF340 340B 7860101EU LT FORWARD LOOSE A PLGAA UNSCHED LANDING O OTHER CRCRUISE 1 NE05350BE 340B197 BOS/ROC, FLT 4915 - DURING FLIGHT, FLIGHT CREW NOTICED LEFT INBOARD FORWARD COWL LATCH WAS LOOSE AND COWLING WAS OPEN ABOUT 1 INCH. AIRCRAFT DIVERTED TO MHT AND COWLING WAS RELATCHED WITHOUT INCIDENT. AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T RTA52EU 19950407000761995040700076 1995 4 7 95ZZZX1529 319950211A6112660714247 PROP LEAD SAAB SF340 340B 7860101EU NR 3 BLADE FAILED A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05358BE 340B279 PQI - FLT 4599 - RT PROP DEICE FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO PQI LANDING WITHOUT INCIDENT. MEL'D PROP DEICE SYSTEM AND REPOSITIONED THE AIRCRAFT TO BOS. BOS MAINTENANCE REPLACED A DEFECTIVE PROP LEAD ON THE NR 3 BLADE AND RETURNED THE AIRCRAFT TO SERVICE FOLLOWING A SATISFACTORY GROUND RUN. 2L72 4T RTA52EU 19950407000771995040700077EU 1995 4 7 95ZZZX1530 119950222A32465010488 MAIN WHEEL SAAB SF340 SF340A 7850100EU BEAD SEAT CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05744BA NOV910187 340A105 DURING EDDY CURRENT INSPECTION, INBOARD MAIN WHEEL HALF WAS FOUND WITH A 2 INCH CRACK IN THE BEAD SEAT AREA. THE WHEEL HALF WAS REMOVED FROM SERVICE, DEFACED AND DISCARDED. 2L72 4T RTA52EU 19950407000781995040700078EU 1995 4 7 95ZZZX1531 119950210A32465010488 MAIN WHEEL SAAB SF340 340B 7860101EU INBD BEAD SEAT CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05360BE JUL931403 340B287 DURING EDDY CURRENT INSPECTION OF A SAAB MAIN WHEEL, A CRACK WAS DETECTED ON THE INBOARD BEAD SEAT AREA APPROXIMATELY 2 INCHES LONG. WHEEL WAS REMOVED FROM SERVICE AND SCRAPPED. 2L72 4T RTA52EU 19950407000791995040700079EU 1995 4 7 95ZZZX1532 119950208A362051533172 LOOP SAAB SF340 SF340A 7850100EU RT BLEED FAULTY A PLGAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NE05741BA 340A090 BWI - EN ROUTE IAD/BOS, RIGHT BLEED AIR FAULT LIGHT ILLUMINATED. FLIGHT CREW PERFORMED ABNORMAL CHECK LIST. SECURED RIGHT ENGINE AND LANDED IN BWI WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND IT SAFE FOR FERRY FLIGHT TO PSM FOR REPAIR. UPON ARRIVAL, MAINTENANCE FOUND RT SENSOR LOOP TO BE AT FAULT. REMOVED AND REPLACED SENSOR LOOP IAW SAAB AMM. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950407000801995040700080CE 1995 4 7 95ZZZX1533 119950205A7120114903635 TRUSS KIT BEECH 1900 1900C 1154161CE LEFT ENGINE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05807BE 348 UB44 DURING C/W AD 92-06-09 AMENDMENT 39-8189, LT ENGINE TRUSS WAS FOUND WITH A .1250 INCH CRACK IN AREA 'A' AT THE UPPER FORWARD GUSSET ON THE RIGHT INBOARD SIDE OF THE CLUSTER. REPAIRED THE TRUSS IAW BEECH SB 2255, REV 6, AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTA24CE 19950407000811995040700081CE 1995 4 7 95ZZZX1534 119950210A32601143610441 SWITCH BEECH 1900 1900 1154160CE RT MLG OUT OF ADJUST A PLGAO OTHER J WARNING INDICATION APAPPROACH 1 NE05806BE UB41 BOS - FLT 4607 - ON INITIAL EXTENSION OF LANDING GEAR, THE RT MLG WOULD NOT ILLUMINATE. LANDING GEAR CYCLED TWICE TO OBTAIN 3 GREEN DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE INSPECTED ACFT AND FOUND IT SAFE FOR FERRY FLIGHT TO PSM FOR REPAIRS. UPON ARRIVAL, MAINTENANCE CLEANED AND LUBED RT DRAG BRACE SWITCH, WHEELWELL CONNECTORS, AND ADJUSTED DRAG BRACE SWITCH. PERFORMED RETRACTION TEST. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 19950407000821995040700082NE 1995 4 7 95ZZZX1535 219950223A8530327627 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 ENG NR 16 FAILED A NACAE ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 AL031027N 978 995221 43580 36630 FLT 60 - SHUT DOWN NR 3 ENGINE DUE TO BACKFIRING AT 1930Z. REPLACED NR 16 CYLINDER. 2L74 4R4 R 6A3 E264 19950407000831995040700083NE 1995 4 7 95ZZZX1536 219950310A7322391548 MIXTURE CONTROL BENDIX PR58E5 DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 1 ENGINE DEFECTIVE A NACAE ENGINE SHUTDOWN RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CRCRUISE 1 AL031036F 1595 761229 43581 33029 FLT 690 - SHUT DOWN NR 1 ENGINE DUE TO BACKFIRING AT 0100Z. REPLACED NR 1 AMC. 2L74 4R4 R 6A3 E264 19950407000841995040700084NE 1995 4 7 95ZZZX1537 219950203A8520 CAM DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 1 ENGINE FAILURE A NACAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 AL031027N 1775 43580 37244 FLT 60 - SHUT DOWN NR 1 ENGINE DUE TO LOSS OF BMEP AT 2330Z. REPLACED NR 1 ENGINE. 2L74 4R4 R 6A3 E264 19950407000851995040700085EU 1995 4 7 95ZZZX1538 119950309A3260622800200 SWITCH BAG JETSTMJETSTM3101 1500215EU LT MLG DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07834JS 726 FLT 4097 - UNABLE TO EXTINGUISH 'RED' INTRANSIT LIGHT AFTER TAKEOFF/GEAR RETRACTION, RETURNED TO FIELD WITHOUT INCIDENT. PIT MAINTENANCE REPLACED LT MLG UPLOCK MICROSWITCH IAW MM 32-60-05. GEAR SWING CONDUCTED IAW MM 32-60-07. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950407000861995040700086 1995 4 7 95ZZZX1539 419950302A34256226190204 AHRS COMPUTER COLLINS AHC85 EMB 120 EMB120RT SO AVIONICS COMP MALFUNCTION A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07335JS 120059 PIT - FLT 4162 - DURING CLIMB-OUT PHASE OF FLIGHT, CAPTAIN NOTICED A DISCREPANCY IN HEADING INDICATION. AIRCRAFT RETURNED TO PIT GATE, WHERE MAINTENANCE RE-RACKED AND INITIALIZED BOTH NR 1 AND NR 2 AHRS COMPUTERS IAW MM 34-21-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950407000871995040700087WP 1995 4 7 95ZZZX1540 219950307A732013711543L401 BLEED LINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENG P3 DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL07856JS 744 PIT - FLT 4054 - UNABLE TO ACHIEVE TARGET TORQUE, ABORTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT, DISCOVERED A BROKEN P3 BLEED AIR LINE, LT ENGINE, REPLACED DEFECTIVE PART IAW GMM 71-00-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19950407000881995040700088 1995 4 7 95ZZZX1541 419950302A3414A3615710260 INDICATOR KOLLSMAN BAG JETSTMJETSTM3101 1500215EU PANEL AIRSPEED DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07851JS 2494 834 FLT 4111 - DURING TAKEOFF, CAPTAIN NOTICED A ZERO KNOTS INDICATION ON AIRSPEED INDICATOR, TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLACED CAPTAIN'S AIRSPEED INDICATOR IAW MM 34-00-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950407000891995040700089SO 1995 4 7 95ZZZX1542 119950226A3230922FSA6NZ735A PROXIMITY SENSORHONEYWELL EMB 120 EMB120RT SO RT MAIN GEAR DEFECTIVE A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07334JS 120056 FLT 4248 - UNABLE TO RETRACT LANDING GEAR AFTER TAKOFF, RETURNED TO GATE. AIRCRAFT LATER FERRIED TO CAK WHERE MAINTENANCE PERSONNEL REPLACED RT MLG WEIGHT-ON-WHEELS PROXIMITY SENSOR. 2L72 4T RTA31SO 19950407000901995040700090WP 1995 4 7 95ZZZX1543 219950227A726131036471 LINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE DEFECTIVE A VNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL07846JS 771 FLT 4138 - SHORTLY AFTER TAKEOFF, LT ENGINE OIL LIGHT ILLUMINATED, ENGINE SHUT DOWN. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. PIT MAINTENANCE PERSONNEL INSPECTED AND FOUND A BROKEN PROPELLER PITCH CONTROL OIL LINE, REPLACED LINE AND CONDUCTED ENGINE OIL FILTER CHECK AND ENGINE GROUND RUN IAW GMM 71-00-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19950407000911995040700091SO 1995 4 7 95ZZZX1544 119950228A5230 SEAL EMB 120 EMB120RT SO CARGO DOOR FAILED A VNAAGBA O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07340JS 120172 FLT 4248 - CRUISE CONFIGURATION AT F. L. 20, AIRCRAFT LOST PRESSURIZATION. OXYGEN MASKS DEPLOYED, CREW CONDUCTED EMERGENCY DESCENT PROCEDURES. AIRCRAFT RETURNED TO FNT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED CARGO DOOR SEAL FAILED. NO PARTS AVAILABLE FOR REPAIR. PRESSURIZATION WAS DEFERRED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950407000921995040700092EU 1995 4 7 95ZZZX1545 119950217A3260622800200 DOWNLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU NOSE LANDING GR DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07851JS 834 FLT 4198 - AFTER TAKEOFF WITH LANDING GEAR DOWN AND LOCKED, FLIGHT CREW NOTICED A NOSE LANDING GEAR IN-TRANSIT LIGHT AND RETURNED TO THE FIELD. AIRCRAFT LATER WAS FERRIED TO PIT WHERE MAINTENANCE REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH, SWUNG GEAR, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950407000931995040700093WP 1995 4 7 AALA950378 119950303A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07556AA 53086 DFW - FLT 0360 - EMERGENCY EXIT FLOOR PATH LIGHT STRIP TORN LOOSE AT ROW 31. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F A6WE 19950407000941995040700094EU 1995 4 7 C2XA95CL037 119950213A2731E006C6S4BJ0A SWITCH AEROSPATR42 ATR42320 8680930EU PITCH TRIM FAILED A C2XAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW0914832 187 ROC/EWR - FLT 3633 - MOMENTARY ELEVATOR NOSE DOWN TRIM RUN-AWAY. MAINTENANCE FOUND THE STANDBY PITCH TRIM STICKS IN THE NOSE DOWN POSITION. MAINTENANCE REMOVED AND REPLACED SWITCH 18CG IN REFERENCE TO ATR WIRING MANUAL CH 20. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950407000951995040700095WP 1995 4 7 ORJA9516 119950303A3350 FLASHLIGHT DOUG DC9 DC982 3022082WP FWD EMERG WEAK A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11841RA 49421 FORWARD EMERGENCY FLASHLIGHT IS WEAK. REPLACED BATTERY IN FORWARD EMERGENCY FLASHLIGHT. (X) 2L72 4F A6WE 19950407000961995040700096WP 1995 4 7 ORJA9517 119950306A3350 FLASHLIGHT DOUG DC9 DC982 3022082WP FWD EMERG INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11841RA 49421 FWD EMERGENCY FLASHLIGHT INOP. REPLACED FWD EMERGENCY FLASHLIGHT WITH A SERVICEABLE UNIT. OPS CHECKED NORMAL. (X) 2L72 4F A6WE 19950407000971995040700097WP 1995 4 7 ORJA9518 119950304A335041B004AD073 BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP RT OVERHEAD EEL INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11845RA 49380 RIGHT OVERHEAD EMERGENCY LIGHTS OUT ON SEATS 10/12. REPLACED BATTERY PACKS, LIGHTS TESTED OKAY. (X) 2L72 4F A6WE 19950407000981995040700098WP 1995 4 7 RAIA950320 219950314A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE BLOWN A RAIACD ABORTED TAKEOFF RETURN TO BLOCK OR OTHER PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03343TE7645 545 955 66163 STL - FLT 7308 - LEFT ENGINE FAILED TO ACHIEVE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE BLEED AIR GASKETS. GROUND POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T4 TRTA56EU E4WE 19950407000991995040700099SO 1995 4 7 RAIA950322 119950314A2150MS35206212 DOOR SCREW EMB 120 EMB120RT SO LEFT PACK LOOSE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03127AM15066 120103 STL - FLT 7151 - NORMAL FLIGHT LEFT PACK SMELLS BAD. MAINTENANCE REPAIRED LEFT RAM AIR DOOR. GROUND TEST OF LEFT PACK REVEALED NORMAL OPERATION AND NOTED NO SMELL. (X) 2L72 4T RTA31SO 19950407001001995040700100EU 1995 4 7 RAIA950323 119950314A21708323715 SOCK BAG JETSTMJETSTM3201 1500217EU AIR COND PACK DIRTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03422AM9150 450 856 STL - FLT 7058 - BLEEDS SMELL. MAINTENANCE REPLACED LT AND RT AIR CONDITIONING WATER SOCKS. (X) 2L72 4T RTA56EU 19950407001011995040700101SO 1995 4 7 RAIA950324 119950315A29127588717 FILTER EMB 120 EMB120RT SO LT HYD BAY DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03126AM149713577 120102 STL - FLT 7478 - LT HYDRAULIC FILTER LIGHT ILLUMINATED. MAINTENACE REPLACED LEFT HYDRAULIC FILTER. GROUND RUN REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (X) 2L72 4T RTA31SO 19950407001021995040700102EU 1995 4 7 RAIA950328 119950316A77228974764 COMPENSATOR BAG JETSTMJETSTM3201 1500217EU LT ENG, STA C FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03340TE6151 939 STL - FLT 7390 - SUPPLEMENT - LEFT EGT FLUCTUATES FROM 550 DEGREES TO 200 DEGREES. MAINTENANCE REPLACED LEFT EGT COMPENSATOR. SET COMPENSATOR TO GARRETT DSC SETTINGS. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950407001031995040700103SO 1995 4 7 RAIA950329 119950314A33503071BPE BULB EMB 120 EMB120RT SO EXT FUSE EEL BURNED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03131AM12571 120158 STL - EXTERIOR RT EMERGENCY LIGHT FOUND INOP. MAINTENANCE REPLACED LIGHT BULB. (X) 2L72 4T RTA31SO 19950407001041995040700104SO 1995 4 7 RAIA950330 119950319A326020224 STRIKER ARM EMB 120 EMB120RT SO RT GEAR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03127AM15110 120103 MSN - FLT 7171 - RT MAIN INTRANSIT LIGHTS ON BOTH CHANNELS WOULD NOT EXTINGUISH WHEN GEAR WAS SELECTED UP. MAINTENANCE CLEANED UPLOCK SENSOR BOX AND ADJUSTED RT MAIN GEAR UPLOCK SENSOR STRIKER ARM. GEAR SWINGS REVEALED NORMAL. (X) 2L72 4T RTA31SO 19950407001051995040700105EU 1995 4 7 RAIA950331 119950320A7722MS948906 LUG BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03423AM9171 858 STL - FLT 7334 - RT ENGINE TAKEOFF RPM 98 PERCENT AND RT EGT JUMPED FROM 620 DEGREES TO 730 DEGREES. MAINTENANCE REPLACED RT ENGINE EGT HARNESS TERMINAL LUG. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950407001061995040700106EU 1995 4 7 RAIA950333 119950321A3320E033601 SOCKET AEROSPATR72 ATR72202 8680940EU ROWS 11-12B SHORTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE03722TE8004 220 STL - FLT 7160 - ELECTRICAL SMOKE AND SMELL IN COCKPIT AND CABIN. UPON INVESTIGATION MAINTENANCE DISCOVERED LIGHT SOCKET AT ROWS 11 AND 12B SHORTED. REPLACED LIGHT SOCKET. OPERATIONAL CHECK GOOD, NO SMOKE NOTED. (X) 2H72 4T RTA53EU 19950407001071995040700107EU 1995 4 7 RAIA950334 119950321A771231024766 SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENG STA C OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03436AM8567 891 STL - FLT 7308 - LT ENGINE TORQUE DROPPED OFF LESS THAN 50 PERCENT TORQUE. MAINTENANCE RESET EGT COMPENSATOR AND ADJUSTED LT ENGINE TORQUE SIGNAL CONDITIONER. GROUND POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950407001081995040700108EU 1995 4 7 RAIA950335 119950320A3350311701 BATTERY PACK BAG JETSTMJETSTM3201 1500217EU FWD CABIN EEL LOW VOLTS A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03431AM5688 307 881 STL - FLT 7390 - EMERGENCY LIGHTS AT OVERHEAD AND EXIT LIGHT AT RT WING IS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK. (X) 2L72 4T RTA56EU 19950407001091995040700109EU 1995 4 7 RAIA950336 119950319A21501531D000 COOLING TURBINE BAG JETSTMJETSTM3201 1500217EU RT PACK FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03866AE991 866 FAT - SMOKE SMELL IN A/C. MAINTENANCE REPLACED RT COOLING TURBINE. (X) 2L72 4T RTA56EU 19950407001101995040700110EU 1995 4 7 RAIA950337 119950323A7722HTMAS0F2821PW CONNECTOR BAG JETSTMJETSTM3201 1500217EU RT ENG EGT LOOSE A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03340TE6180 939 STL - FLT 7088 - LT EGT FLUX, PLUS OR MINUS 100 DEGREES TO 150 DESGREES. MAINTENANCE TIGHTENED LT ENGINE FIREWALL CANNON PLUG. GROUND POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950407001111995040700111EU 1995 4 7 SIMA950641 119950305A2710 CONTROLS AEROSPATR42 ATR42300 8680920EU WINGS ICED UP A ASIMAK NONE EF VIBRATION/BUFFET FLT CONT AFFECTED DEDESCENT 1 SW21266AT 266 DFW - FLT 3947 - ON DESCENT FROM 17,000 MSL, DEVELOPED MODERATE ICE AT 15,500, SPEED 230 KNOTS. AS THE ICE WAS DETECTED, AIRCRAFT STARTED TO VIBRATE IN THE CONTROLS. AT THIS TIME, ACFT THEN PROCEEDED TO ROLL LEFT THEN RIGHT BEFORE COMING ACK TO NORMAL. CREW REPORTED ACFT WAS IN A CLEAN CONFIGURATION, BUT THE CONTROLS WERE FEELING VERY STIFF AND HARD TO MANEUVER. THE ICE DEPARTED ACFT SURFACES AND FLIGHT CONTROLS RETURNED TO NORMAL. THIS WAS AT ARRROX 8,000 MSL. MTX PERFORMED TURBULENCE INSPECTION AND OPERATIONAL TEST OF DE-ICE SYSTEM. NO FAULTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE. (X) 2H72 4T RTA53EU 19950407001121995040700112EU 1995 4 7 SIMA950731 119950314A3230L38710SA SWIVEL SAAB SF340 SF340A 7850100EU RT MLG DNLOCK CRACKED A SIMAA UNSCHED LANDING OJKOTHER WARNING INDICATION FLUID LOSS CLCLIMB 1 SW2189MQ 340A089 AFTER TAKEOFF, CREW NOTICED HYDRAULIC PUMP GRINDING AND RT MAIN GEAR NEVER UNLOCKED. HYDRAULIC SYSTEM PRESSURE WENT TO ZERO, SO CREW PERFORMED AN EMERGENCY EXTENSION OF LT MAIN AND NOSE GEARS. THE CREW RETURNED TO CID AND LANDED WITHOUT INCIDENT. AFTER INSPECTION OF THE RT WHEELWELL, MAINTENANCE FOUND RT DOWNLOCK SWIVEL CRACKED. (X) 2L72 4T RTA52EU 19950407001131995040700113EU 1995 4 7 SIMA950751 119950316A2710S2711009100000 BELLCRANK AEROSPATR42 ATR42300 8680920EU LEFT AILERON CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21428MQ 0128 MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND LT AILERON INBOARD BELLCRANK TO HAVE A CORRODED BEARING. BELLCRANK WAS REMOVED AND REPLACED AND FUNCTIONAL TEST OF AILERON CONTROL SYSTEM WAS SATISFACTORY IAW ATR 42 J/C 27-10-00 FUT 10005-007. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950407001141995040700114EU 1995 4 7 UF6A950303 119950315A6123S5600075N CONNECTOR BAG ATP ATP EU NR 1 ENGINE DIRTY A UF6AK NONE L NO TEST TXTAXI/GRND HDL 1 CE03854AW7693 2028 CAK - FLT 5018 - THE NR 1 AUTOFEATHER UNIT WILL NOT ARM. MAINTENANCE CLEANED CANNON PLUG 'C'. (X) 2L72 4T RTA27NM 19950407001151995040700115EU 1995 4 7 UF6A950304 119950316A6123S5600075N CONNECTOR BAG ATP ATP EU NR 1 ENG FAILED A UF6AK NONE L NO TEST TXTAXI/GRND HDL 1 CE03854AW7694 2028 SBN - FLT 5108 - THE NR 1 AUTOFEATHER UNIT WOULD NOT TEST. MAINTENANCE REPLACED CANNON PLUG C. (X) 2L72 4T RTA27NM 19950407001161995040700116NE 1995 4 7 Y2PA95002 219950213A7200 ENGINE DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 WORN A Y2PAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL23197US 47154 657238 ELP - DURING CRUISE AT 34,000 FEET, THE CREW ENCOUNTERED A LOUD RUMBLING. ALL SYSTEMS INDICATIONS WERE NORMAL. FURTHER INVESTIGATION REVEALED VIBRATION FROM NR 1 ENGINE WHENEVER POWER WAS ABOVE 1.78 EPR. S/D THE ENGINE WAS REMOVED AND SENT TO BOUNTY MAINTENANCE SERVICES (B4MR567J) FOR TEARDOWN EVALUATION. EXTENSIVE TEARDOWN INSPECTION, AND REPAIR WAS ACCOMPLISHED. NO ITEMS WERE IDENTIFIED THAT WOULD SPECIFICALLY ACCOUNT FOR THE ENGINE VIBRATION, HOWEVER, EXCESSIVE PLAY WAS FOUND IN THE C-1 DISK BLADE AREA, AND TWO WORN BEARINGS WERE NOTED. THE ENGINE WAS RETURNED TO SERVICE AND REINSTALLED ON THIS AIRCRAFT JUNE 23, 1995. (M) 2L72 4F4 F A6WE E2EA 19950407001171995040700117NE 1995 4 7 9505141141 219950330A7200 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 1 MALFUNCTIONED A NWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL01141US 46750 686121 DURING DESCENT FL280 AT IDLE POWER, THE NR 1 ENGINE ENCOUNTERED WAKE TURBULENCE AND A SURGE FOLLOWED BY RISING EGT. THE ENGINE WAS SHUTDOWN, AND A RELIGHT WAS SUCCESSFUL. OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND A BORESCOPE CHECKED OK. 2L73 4F4 F A22WE E20EA 19950407001181995040700118WP 1995 4 7 9505159992 119950327A3230 RETRACT MECH DOUG DC9 DC931 3022065WP LANDING GEAR LACK OF LUBE A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL018960E 45869 LANDING GEAR WAS SLOW TO RETRACT DURING CLIMBOUT FROM MEM VIBRATION WAS ALSO EXPERIENCED. RECYCLED GEAR AND ALL ACTIONS WERE EXTREMELY SLOW. FLIGHT CONTINUED TO DESTINATION DCA AND LANDED WITHOUT INCIDENT. CHECKED RIGGING AT LANDING GEAR CONTROL VALVE. FREED CABLE AT BYPASS VALVE AND GREASED BOTH MAIN AND NOSE GEARS. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950407001191995040700119WP 1995 4 7 9505169861 119950331A3010 CONTROL UNIT DOUG DC9 DC951 3022051WP RIGHT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01770NC 47758 RIGHT ICE PROTECTION TEMPERATURE LOW LIGHT REMAINED ON AFTER TAKEOFF. LIGHT EXTINGUISHED AFTER WORKING WITH CROSSFEED. LEFT SUPPLY TEMPERATURE HIGH LIGHT THEN ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT THERMAL CONTROL UNIT AND RIGHT LOW TEMPERATURE SENSOR. OPERATIONAL CHECK OK, AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950407001201995040700120EU 1995 4 7 9505173248 119950401A3260 DOOR LIGHT AIRBUS320 A320211 3930320EU LT MLG ILLUMINATED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01348NW 410 DURING APPROACH INTO SFO AFTER THE LANDING GEAR WAS EXTENDED, THE LEFT MAIN LANDING GEAR DOOR WARNING LIGHT ILLUMINATED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TEST OF NR 1 AND NR 2 LANDING GEAR CONTROL INTERFACE UNITS REVEALED NO FAULTS. CLEANED ASSOCIATED GEAR DOOR INDICATION SWITCHES. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950407001211995040700121NM 1995 4 7 95UAL747015 119950302A25308055010000 OVEN BOEING747 747422 1384935NM PWA 4056 PW4056 NE GALLEY DIRTY A UALAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 WP29178UA 24385 AIRCRAFT RETURNED TO GATE WITH AN OVEN FIRE. REPLACED OVEN. REMOVED OVEN WAS DISASSEMBLED AND A SMALL DEPOSIT OF SOLIDIFIED PLASTIC WAS FOUND ADHERING TO UPPER SURFACE OF OVEN UPPER INTERNAL BAFFLE PLATE CLOSEST TO FAN MOTOR AND BURNER ELEMENTS. IDENTIFICATION OF SOURCE OF PLASTIC IS UNKNOWN. NO DEFECTS IN OVEN PROPER. 2L74 4F4 FRTA20WE E24NE 19950407001221995040700122 1995 4 7 95UAL747019 419950327A2565 SLIDE BF GOODRICH 7A1323107 BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN MALFUNCTIONED A UALAK NONE O OTHER ININSP/MAINT 1 WP29179UA G426 25158 DURING INADVERTENT DEPLOYMENT, THE SUD SLIDE DID NOT FULLY INFLATE. REPLACED SLIDE. FLAPPER VALVE PIN WAS FOUND BROKEN. ADDITIONALLY, THE 410 POUND MECHANICAL RESTRAINT DID NOT SEPARATE. UNIT RETURNED TO VENDOR FOR REVIEW. 2L74 4F4 FRTA20WE E24NE 19950407001231995040700123NM 1995 4 7 95UAL747020 119950331A2612 FIRE WARNING BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO COMPT ACTIVATED A UALAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 WP29190UA 26879 ON FINAL APPROACH AT APPROXIMATELY 1500 FEET THE AFT CARGO FIRE WARNING SYSTEM ACTIVATED. DISCHARGED BOTTLE ON LANDING, NO DEFECT FOUND. FALSE WARNING CAUSED BY HIGH MOISTURE CONTENT FRUIT BEING TRANSPORTED IN AFT CARGO COMPARTMENT WHICH CAUSED FALSE FIRE WARNING. 2L74 4F4 FRTA20WE E24NE 19950407001241995040700124NE 1995 4 7 95UAL757008 219950329A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A UALAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 WP29539UA 25223 726555 NR 1 ENGINE SHUTDOWN PRIOR TO TOP OF DESCENT. NO PRIOR THROTTLE MOVEMENT OR CHANGE IN FUEL CONFIGURATION. A/C DESCENDED TO 16,000 FEET WHERE ENGINE WAS RESTARTED, A/C CONTINUED WITHOUT FURTHER INCIDENT. THE FUEL CONTROL UNIT WAS REMOVED AND ROUTED TO HAMILTON STANDARD FOR ANALYSIS, NO MECHANICAL CAUSE FOR SHUTDOWN FOUND. ENGINE REMAINED ON WING WITHOUT FURTHER INCIDENT. 2L72 4F4 FRTA2NM E17NE 19950407001251995040700125WP 1995 4 7 ABXA9500288 119950401A335060030431 EEL PWR SUPPLY DOUG DC9 DC932 3022066WP CABIN DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 EMERGENCY LIGHTS WOULD NOT GO OUT IN THE OFF POSITION. REPLACED THE EMERGENCY LIGHT POWER SUPPLY PACK IAW DC-9 MM CHAPTER 33-53-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950407001261995040700126SO 1995 4 7 COM11840 119950328A323112012347001 LATCH ASSY EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01258CA 120247 LEFT MAIN LANDING GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN LATCH ASSY. 2L72 4T RTA31SO 19950407001271995040700127SO 1995 4 7 COM11841 119950329A5720 SKIN SUPPORT EMB 120 EMB120RT SO WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01200CD1136111361 120200 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I AT WING RIBS NR 15, 16, 18 AND 21. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17062-005, 2 EA; 120-17056-015, 4 EA; 120-17057-006, 2 EA; 120-17056-007, 12 EA; 120-17057-015, 1 EA; 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-013, 2 EA; 120-17057-006, 1 EA. 2L72 4T RTA31SO 19950407001281995040700128SO 1995 4 7 COM11842 119950331A325012037995001 TILLER EMB 120 EMB120RT SO NLG STEERING DEFECTIVE A COMAO OTHER O OTHER UKUNKNOWN 1 SO01248CA 120228 NOSE WHEEL STEERING PULLS HARD TOWARDS RIGHT. REPLACED NOSE WHEEL STEERING TILLER. 2L72 4T RTA31SO 19950407001291995040700129SO 1995 4 7 COM11843 119950330A5720 SKIN SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01205CA1154311543 120205 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-013, 1 EA; 120-17057-005, 1 EA; 120-17059-017, 1 EA; 120-17059-015, 2 EA; 120-17059-019, 1 EA; 120-17063-009, 2 EA; 120-17057-006, 1 EA; 120-17062-005, 1 EA. 2L72 4T RTA31SO 19950407001301995040700130NE 1995 4 7 COM31053 219950330A73217086M60G11 ECU SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE DEFECTIVE A COMAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01361CA9759 460 340A056 367262 WHEN CONDITION LEVER ADVANCED TO MAX, THE PROPELLER UNIT WENT TO AN OVERSPEED CONDITION. REPLACED THE ENGINE ELECTRONIC CONTROL UNIT. 2L72 4T4 TRTA52EU E8NE6 19950407001311995040700131NE 1995 4 7 COM60446 219950328A73204096T76G01 CONTROL AMP CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT ENGINE DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01916CA4657 7014 807031 LEFT ENGINE ROLLED BACK TO 60 PERCENT N1. REPLACED THE LEFT ENGINE N1 CONTROL AMPLIFIER. 2L72 4F4 FRTA21EA E15NE 19950407001321995040700132EA 1995 4 7 COM60447 119950329A27603G5209A LEVER CNDAIRCL600 CL6002B19 EA COCKPIT DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01917CA4414 7017 FLIGHT SPOILER FAIL MESSAGE ON EICAS. REPLACED THE FLIGHT SPOILER SELECTOR LEVER. 2L72 4F RTA21EA 19950407001331995040700133NM 1995 4 7 DL72E951193 119950317A5320 ANGLE BOEING727 727247 138408FNM BS 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, THE FLOOR SUPPORT ANGLES AT STA 1166 WERE FOUND TO BE CORRODED. THESE WERE REPAIRED PER SRM 53-10-3 FIG 10. 2L73 4F A3WE 19950407001341995040700134NM 1995 4 7 DL72E951206 119950311A5313 STRINGER BOEING727 727247 138408FNM BS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 STRINGER 27R CORRODED INSIDE STRINGER STA 740 AFT OF SPLICE STRINGER SLICE PER SRM 53-10-3 PG 3. FOUND AT HMV. 2L73 4F A3WE 19950407001351995040700135NM 1995 4 7 DL72E951211 119950227A5313 STRINGER BOEING727 727247 138408FNM BS 1183 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AFT BB STRINGER END IS CORRODED, NR 29R AT STA 1183. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV. 2L73 4F A3WE 19950407001361995040700136NM 1995 4 7 DL72E951212 119950227A5311 FRAME BOEING727 727247 138408FNM BS 1130 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AFT BB FRAME CORRODED, STA 1130 BETWEEN STR 28R AND 29R. REPAIRED PER 53-11-0 PAGE 825. FOUND AT HMV. 2L73 4F A3WE 19950407001371995040700137NM 1995 4 7 DL72E951219 119950304A5313 STRINGER BOEING727 727247 138408FNM BS 990-1000 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING HMV, FOUND STRINGER CRACKED NR 29L CRACKED IN LOWER RADIUS FROM FS 990 - 1000. REPAIRED PER ERA 301274-14 REV B. FOUND AT HMV. 2L73 4F A3WE 19950407001381995040700138NM 1995 4 7 DL72L951216 119950309A5754651622162 SKIN BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 BAY NR 6 INNER SKIN, CRACKED AROUND RIVET. REPAIRED PER MM 57-54-0 FIG 803A. BAY NR 14 DOUBLER CRACKED .5 INCH LONG FWD TOP CORNER (MKD). REPAIRED PER MM 57-54-0 FIG 804 SLAT NR 5. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950407001391995040700139NM 1995 4 7 DL72S951214 119950221A5754651622195 SKIN BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 DURING SHOP INSPECTION, FOUND NR 4 L/E SLAT WITH CRACKED SKIN AT MOUNT AREA FOR WING FENCE. REPAIRED PER SRM 57-54-0 PG 817. 2L73 4F A3WE 19950407001401995040700140NM 1995 4 7 DL72S951215 119950221A5754651622195 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH RIB NR 6 CRACKED. REPAIRED PER MM 57-54-0 PG 807. 2L73 4F A3WE 19950407001411995040700141NM 1995 4 7 DL733951175 119950313A5542 SKIN BOEING737 737347 1384647NM RUDDER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313WA 23599 DURING INSPECTION, FOUND RUDDER WITH NUMEROUS AREAS OF DELAMINATION ON OUTER SKIN. REPAIRED PER SRM 55-40-01. 2L72 4F RTA16WE 19950407001431995040700143NM 1995 4 7 DL757951222 119950321A5321 FLOOR PANEL BOEING757 757232 1384965NM CARGO COMPT CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11621DL 22911 DURING LETTER CHECK INSP, CORROSION FOUND AFT CARGO FLOOR LEFT SIDE AFT OF CARGO DOOR. REMOVED FLOOR PANEL AND CANTED WALL PANEL. REMOVED CORRODED AREA, MANUFACTURED REPLACEMENT SECTION. STARTED INSTALLATION OF REPLACEMENT SECTION, INSTALLED DOUBLER, INSTALLED FLOOR PANEL AND CANTED WALL PANEL REF SRM 53-60-53. 2L72 4F RTA2NM 19950407001441995040700144NM 1995 4 7 DLM88951217 119950321A5320 SUB FLOOR DOUG MD88 MD88 3023688NM RT AFT FUS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING HMV, FOUND AFT RT SUBFLOOR CRACKED FWD OF PYLON BULKHEAD. REPLACED SUBFLOOR PER SRM 53-5 FIG 97. 2L72 4F RTA6WE 19950407001451995040700145NM 1995 4 7 DLM88951218 119950322A7110 NOSE COWL DOUG MD88 MD88 3023688NM NR 1 ENG DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11978DL 53259 1 INCH BY 1 INCH DENT IN NOSE COWL AT 1200 POS. REPAIRED INSP PER SRM 54-04 FIG 9. FOUND AT LETTER CHECK. 2L72 4F RTA6WE 19950407001461995040700146WP 1995 4 7 MWEA95157 119950403A335060030431 EEL BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31203ME 47673 CREW REPORTS COCKPIT AND GALLEY CEILING EMERGENCY LIGHTS REMAIN ON WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED BATTERY POWER PACK NR 1. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950407001471995040700147NM 1995 4 7 UPS202705 119950331A5753652163449 SKIN BOEING727 72722C 138400FNM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK MAINTENANCE FOUND LT I/B AFT FLAP TRAILING EDGE IS DELAMINATED ON TRAILING EDGE. REPLACED FLAP PER MM 27-51-02. 2L73 4F A3WE 19950407001481995040700148NM 1995 4 7 UPS202765 119950331A532065198613 ANGLE BOEING727 72722C 138400FNM NLG COMPT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND NOSE LANDING GEAR LOWER LT ANGLE CORRODED. REPLACED CHORD PER SRM 51-30-2, 51-50-1, 51-40-2. 2L73 4F A3WE 19950407001491995040700149NM 1995 4 7 UPS202766 119950331A5754 ATTACH POINTS BOEING727 72722C 138400FNM NR 6 K-FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND NR 6 K-FLAP ATTACH POINTS CORRODED ON K-FLAP SIDE. REPLACED FLAP PER MM 27-81-01. 2L73 4F A3WE 19950407001501995040700150NM 1995 4 7 UPS202767 119950331A5754 RIB BOEING727 72722C 138400FNM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND NR 5 SLAT RIB CRACKED. FABRICATED AND INSTALLED REPAIR PER SRM 57-50-3. 2L73 4F A3WE 19950407001511995040700151NM 1995 4 7 UPS202769 119950331A5753652163480 CORE BOEING727 72722C 138400FNM RT TE FLAP DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND RT WING I/B AFT FLAP CORE WATER DAMAGED. REPLACED FLAP PER MM 27-51-02. 2L73 4F A3WE 19950407001521995040700152NM 1995 4 7 UPS202770 119950331A5320 DOOR FRAME BOEING727 72722C 138400FNM MAIN CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR AFT SIDE FRAME CRACKED AT DRIFT PIN RECEPTACLE AT I/B RADIUS. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-40-2, 51-40-3, 51-10-2. 2L73 4F A3WE 19950407001531995040700153NM 1995 4 7 UPS202771 119950331A532065931157 FITTING BOEING727 72722C 138400FNM BS 500 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND MAIN CARGO DOOR LATCH SUPPORT FITTINGS IN THE FUSELAGE STRUCTURE CRACKED AT BS 500. REPLACED FITTING PER UPS EO B727-5310-0437. 2L73 4F A3WE 19950407001541995040700154NM 1995 4 7 UPS202787 119950331A5751652172512 WEDGE BOEING727 72722C 138400FNM LT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 DURING 'C' CHECK, MAINTENANCE FOUND LT AILERON O/B TRAILING EDGE WEDGE IS DELAMINATED. REPLACED WEDGE PER SRM 51-80-6, 51-10-2, 51-30-2, MM 27-10-41. 2L73 4F A3WE 19950407001551995040700155NM 1995 4 7 UPS202788 119950403A5320 INTERCOSTAL BOEING727 72731C 1384011NM BS 600-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL IN FWD CARGO BAY STA 600-680, RBL 65. REPLACED INTERCOSTAL PER SRM 51-10-2, 51-20-1, 51-30-2. 2L73 4F A3WE 19950407001561995040700156NM 1995 4 7 UPS202789 119950403A5230 BEAM BOEING727 72731C 1384011NM AFT CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CRACK ON AFT CARGO DOOR NR 4 HORIZONTAL BEAM AT BS 1084. REPLACED BEAM PER SRM 51-30-05, 51-30-02, 51-10-1. 2L73 4F A3WE 19950407001571995040700157NM 1995 4 7 UPS202790 119950403A5311 FRAME BOEING727 72731C 1384011NM BS 950 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BS 950 FRAME FORGING AROUND NUT HEAD ON BOTTOM OF FWD FORGING EAR WL 207, RBL 64. INSTALLED REPAIR PER SRM 51-10-6. 2L73 4F A3WE 19950407001581995040700158NM 1995 4 7 UPS202791 119950403A5320 INTERCOSTAL BOEING727 72731C 1384011NM BS 854 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATES AND CRACKS AROUND ATTACH POINTS OF INTERCOSTAL STA 854, LBL 25-45, WL 206. REPLACED PER SRM 51-30-2. 2L73 4F A3WE 19950407001591995040700159NM 1995 4 7 UPS202792 119950403A5320 STRINGER SPLICE BOEING727 72731C 1384011NM BS 950 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICES FWD SIDE STA 950, STRINGERS 2, 4, 6, 7, 8, 9 L. REPLACED STRINGERS SPLICES 2L AND 7L, BLENDED REMAINING STRINGER SPLICES. ALL WORK ACCOMPLISHED PER SRM 51-10-6, 51-30-2, 51-20-4, MM 51-20-151. 2L73 4F A3WE 19950407001601995040700160NM 1995 4 7 UPS202793 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 4L STA 950-1183. REPLACED STRINGER PER SRM 51-30-2, 53-10-3. 2L73 4F A3WE 19950407001611995040700161NM 1995 4 7 UPS202794 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8L STA 950-1183. REPLACED STRINGER AND SPLICES PER SRM 51-30-2, 53-10-3, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950407001621995040700162NM 1995 4 7 UPS202795 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8R STA 950-1183. REPLACED STRINGER PER SRM 51-30-2, 51-40-5, 53-10-4, 53-40-4. 2L73 4F A3WE 19950407001631995040700163NM 1995 4 7 UPS202796 119950403A5754 SKIN BOEING727 72731C 1384011NM NR 7 SLAT DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND NR 7 SLAT TRAILING EDGE SKIN AT I/B SLAT HOOK IS DAMAGED FROM LOOSE FASTENERS. INSTALLED REPAIR PER UPS ENGINEERING FILE NR B272-57-1339. 2L73 4F A3WE 19950407001641995040700164NM 1995 4 7 UPS202797 119950403A5720 FORGING BOEING727 72731C 1384011NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION IN LT FWD BOTTLE PIN FORGING AND FITTING 740. REPLACED BUSHINGS PER UPS EO FILE NR B727-53-1548. 2L73 4F A3WE 19950407001651995040700165NM 1995 4 7 UPS202798 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 480-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 2R, BS 480-740. INSTALLED REPAIR AND REPLACED SECTIONS OF STRINGER PER SRM 53-10-3. 2L73 4F A3WE 19950407001661995040700166NM 1995 4 7 UPS202799 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 480-620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 7R STA 480-620. REPLACED PER SRM 53-30-2. 2L73 4F A3WE 19950407001671995040700167NM 1995 4 7 UPS202800 119950403A5313 STRINGER BOEING727 72731C 1384011NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICE ENDS AND ON TERMINATION ENDS ON STRINGERS NR 2 THROUGH NR 9R ON FWD SIDE OF BS 740 FRAME (PRODUCTION JOINT). FITTINGS AT STRINGERS 3, 5, 8, 9, WERE REPLACED. STRINGER FITTINGS AT STRINGERS 2, 4, 6, 7, FOUND TO BE WITHIN LIMITS. ALL WORK DONE IN ACCORDANCE WITH SRM 51-10-6, 51-10-2, 51-20-4, 51-30-21, MM 51-20-151, AND 53-11-40-00. 2L73 4F A3WE 19950407001681995040700168NM 1995 4 7 UPS202801 119950403A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 950-970 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK I/B FLANGE STA 950-970, LBL 62.0. REPLACED SEAT TRACK PER SRM 53-10-1, 53-10-05. 2L73 4F A3WE 19950407001691995040700169NM 1995 4 7 UPS202802 119950403A5315 FLOOR BEAM BOEING727 72731C 1384011NM BS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLE UPPER FLANGE OF FLOORBEAM AT STA 312, LBL 45, WL 208. REPLACED PER UPS EO B727-5310-6838A. 2L73 4F A3WE 19950407001701995040700170NM 1995 4 7 UPS202803 119950403A5320 HAT CHANNEL BOEING727 72731C 1384011NM BS 315 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES IN UPPER FLANGE OF HAT CHANNEL AT STA 315, RBL 12. WL 208. REPLACED PER SRM 51-10-02, 51-30-2, 51-10-6, AND MM 51-20-151. 2L73 4F A3WE 19950407001711995040700171NM 1995 4 7 UPS202804 119950403A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 344-360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 344-360, LBL 61. REPLACED PER SRM 51-30-2, 51-10-1, 57-30-8. 2L73 4F A3WE 19950407001721995040700172NM 1995 4 7 UPS202807 119950403A5753 SKIN BOEING727 72731C 1384011NM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'C' CHECK, MAINTENANCE FOUND DELAMINATION ON LWR SKIN OF RT I/B MID FLAP. INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950407001731995040700173NM 1995 4 7 UPS402809 119950402A3350900835A EEL BATTERY PACK BOEING747 747123F NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 MAINTENANCE REPORTED, EMERGENCY BATTERY PACK FAILED, LOCATED OVER C/P EMER EXIT. REPLACED BATTERY PACK. 2L74 4F A20WE 19950407001741995040700174NM 1995 4 7 UPS402810 119950329A3350 EEL BOEING747 747123F NM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 MAINTENANCE REPORTED, UPPER RT PASSENGER CABIN EMER LIGHT INOP. REPLACED LIGHT, OPS CK GOOD. 2L74 4F A20WE 19950407001751995040700175WP 1995 4 7 UPS802772 119950331A5313975803 LONGERON DOUG DC8 DC873F 302199FWP FS 395-415 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON LONGERON 21L AT FS 395-415. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F RT4A25 19950407001761995040700176WP 1995 4 7 UPS802773 119950331A532046401622 FITTING DOUG DC8 DC873F 302199FWP BS 1400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME END FITTING AT FS 1400, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950407001771995040700177WP 1995 4 7 UPS802774 119950331A53119772958 FRAME DOUG DC8 DC873F 302199FWP FS 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON BELTFRAME AT FS 200, LONGERON 29R. REPAIRED FRAME PER SRM 53-2-3. 2L74 4F RT4A25 19950407001781995040700178WP 1995 4 7 UPS802775 119950331A53203758841 FITTINGS DOUG DC8 DC873F 302199FWP FS 1200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1200 BETWEEN LONGERON 33-34R AND 33-34L. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 19950407001791995040700179WP 1995 4 7 UPS802776 119950331A53203755840 FITTINGS DOUG DC8 DC873F 302199FWP FS 1180/1220 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTINGS AT FS 1180, LONGERON 33-34R AND FS 1220, LONGERON 33R. REPLACED FITTINGS PER SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 19950407001801995040700180WP 1995 4 7 UPS802777 119950331A53203755840 FITTING DOUG DC8 DC873F 302199FWP FS 1060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON B/T FITTING AT FS 1060, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 19950407001811995040700181WP 1995 4 7 UPS802778 119950331A53115772958 FRAME DOUG DC8 DC873F 302199FWP FS 1320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT FS 1320, LONGERONS 34-35R. REPAIRED FRAME PER SRM 53-2-0. 2L74 4F RT4A25 19950407001821995040700182WP 1995 4 7 UPS802779 119950331A533057799253N SKIN DOUG DC8 DC873F 302199FWP BS 70 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND CRACK IN FWD JACK POINT AT STA 70, LOWER BELLY SKIN. REPLACED SKIN PER UPS EO DC8-5330-6471. 2L74 4F RT4A25 19950407001831995040700183WP 1995 4 7 UPS802780 119950331A575556551661 SKIN DOUG DC8 DC873F 302199FWP NR 2 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND LT WING NR 2 SPOILER DELAMINATED TOP AND BOTTOM SIDES AT I/B TRAILING EDGE. REPLACED SPOILER PANEL PER MM 27-61-1. 2L74 4F RT4A25 19950407001841995040700184WP 1995 4 7 UPS802781 119950331A57535701473 SKIN DOUG DC8 DC873F 302199FWP NR 5 VANE ASSY DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON UPPER SURFACE NR 5 VANE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950407001851995040700185WP 1995 4 7 UPS802782 119950331A57535701446 SKIN DOUG DC8 DC873F 302199FWP NR 3 VANE ASSY DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 3 VANE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950407001861995040700186WP 1995 4 7 UPS802783 119950331A57535652288 SKIN DOUG DC8 DC873F 302199FWP NR 2 VANE ASSY DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND RT WING FLAP VANE DELAMINATED ON LOWER SURFACE NR 2 VANE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950407001871995040700187WP 1995 4 7 UPS802784 119950331A57307075T6090 SKIN DOUG DC8 DC873F 302199FWP WS 703 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND RT WING LEADING EDGE LOWER SURFACE ATTACH HOLE SKIN CRACKED AT STA XFS 703. REPAIRED SKIN PER SRM 57-2-0. 2L74 4F RT4A25 19950407001881995040700188WP 1995 4 7 UPS802785 119950331A57207075T6063 FRAME DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND RT WHEELWELL DOOR CUTOUT FRAME CRACKED ON FWD I/B CORNER. REPAIRED FRAME PER SRM 57-2-0. 2L74 4F RT4A25 19950407001891995040700189WP 1995 4 7 UPS802786 119950331A523098907103 DOOR TRACK DOUG DC8 DC873F 302199FWP FS 1160 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 DURING 'C' CHECK, MAINTENANCE FOUND FWD DOOR TRACK CRACKED AT FS 1160, LONGERONS 24R AND 29R. REPAIRED TRACKS PER UPS EO DC8-53-1351. 2L74 4F RT4A25 19950407001901995040700190WP 1995 4 7 UPS802808 119950401A5312 J BEAM DOUG DC8 DC873F 302199FWP AFT PRESS BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 DURING B-CHECK, MAINTENANCE REPORTED TOP J-BEAM ON AFT PRESS BULKHEAD LT O/B END HAS CRACK ON TOP FLANGE AND LOWER FLANGE. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5310-6598B. 2L74 4F RT4A25 19950407001921995040700192CE 1995 4 7 95ZZZX1585 119950316A324640172 WHEEL HALF PARKERHANFIN BEECH 99 99 1154002CE BOLT PAD HOLES CRACKED A BEMAK NONE O OTHER ININSP/MAINT 1 GL15139BA 152412 U76 CRACKS WERE FOUND IN THE WHEEL HALF AROUND THE BOLT HOLES ON TWO WHEEL HALVES OF SIMILAR VINTAGE AND TYPE. THEY WERE CAUSE FOR REPLACEMENT OF THE WHEEL HALF. RECOMMEND THE BOLT HOLES BE VISUALLY INSPECTED OR ZYGLOED AT EACH TIRE CHANGE TO PREVENT FAILURE OF THE WHEEL HALF. 1L72 3T A14CE 19950407002071995040700207CE 1995 4 7 95ZZZX1600 119950320A5711 SPAR CESSNA402 402C 207590RCE CARRY-THROUGH CRACKED A AOEZAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP193208G10574 402C00497 ON 11-24-89, CESSNA ME84-12 WAS C/W ON LT WING SPAR CARRY-THROUGH. IT WAS DONE IMPROPERLY AND HAS NOW CRACKED FURTHER THAN ALLOWED. AT SOME POINT, THE CRACKS WERE STOP DRILLED CAUSING DAMAGE TO THE CARRY-THROUGH CASTING. SUBMITTER RECOMMENDS WHEN C/W ME84-12, THAT BASIC SHEET METAL PRACTICES SHOULD BE FOLLOWED. IT IS SUBMITTER'S FIRM BELIEF THAT THIS DAMAGE WAS DONE BY IMPROPER PRACTICES USED. TIME SINCE MR84-12 IS 3,582.8 HOURS. 1L72 3O A7CE 19950407002261995040700226NE 1995 4 7 RAIA950332 219950321A7261 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RTG ENGINE REQ SERVICING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE032FOR 11230 199 120838 SGF - FLT 7020 - RT ENGINE OIL PRESSURE DROPPED TO 40 PSI. MAINTENANCE SERVICED RT ENGINE WITH OIL. GROUND RUNS REVEALED NO LEAKS. ENGINE PLACED AN OIL CONSUMPTION WATCH. (X) 2H72 4T4 TRTA53EU E20NE 19950407002271995040700227NM 1995 4 7 95ZZZW317 119950228A5711 SPAR BOEING727 7272Q9 138448MNM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, LT WING LE LOWER SPAR CAP HAS CORROSION UPPER AND LOWER SURFACE 53 INCHES TO 60 INCHES O/B OF I/B END (JUST O/B OF NR 3 LE FLAP ACUTATOR MOUNT AND PREVIOUS GRIND OUT). REMOVED FASTENERS PER SRM 51-30-2, REMOVED CORROSION PER SRM 51-10-6 AT 43 INCHES AND 53 INCHES AND FOUND OUT OF LIMITS, AND AT 60 INCHES IS WITHIN LIMITS PER SRM 57-20-1 PG 1. INSTALLED .301 .5H SS .10 IAW AVITAS ENGINEER NR 94PMSI .042D-1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407002281995040700228NM 1995 4 7 95ZZZW318 119950228A5711 SPAR BOEING727 7272Q9 138448MNM LT WING CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, LT WING LOWER LE SPAR HAS EXFOLIATED CORROSION LOWER SURFACE 15 INCHES O/B OF NR 1 LE SLAT ACTUATOR. REMOVED CORROSION PER SRM 51-10-6 MAX DEPTH REMOVED .070 OUT OF LIMITS. ALODINE AND PRIMED AREA PER SRM 51-10-2 AND INSTALLED REPAIR 7075-T6 .125 THICK 3 INCHES BY 13 INCHES PER SRM 51-40-4. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407002291995040700229NM 1995 4 7 95ZZZW319 119950228A5711 SPAR CAP BOEING727 7272Q9 138448MNM LT WING CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, LT WING LOWER LE SPAR CAP HAS CORROSION UPPER SURFACE 10 INCHES AND 30 INCHES O/B OF NR 3 LE SLAT ACTUATOR IN TWO PLACES. REMOVED CORROSION IAW SRM 51-10-6, MATERIAL LOSS .040 AND .050. CORROSION GRIND OUT ON UPPER SURFACE IS WITHIN LIMITS PER SRM 57-20-1. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 51-40-4. MATERIAL OF REPAIR STRAP 2024-T3 3 INCHES BY 11 INCHES. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407002301995040700230NM 1995 4 7 95ZZZW320 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 348.2 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR SKIN BULGE AT FWD SIDE OF FUS FWD JACK PAD AT FS 348.2 AT STR 21R. CUT OUT DAMAGED SECTION OF SKIN AND REMOVED CORROSION FROM UNDERLYING SURFACES PER SRM 51-10-6. INSTALLED DOUBLER REPAIR 12 INCHES BY 20 INCHES .050 2024-T3 PER SRM 53-30-3 FIG 1. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407002311995040700231NM 1995 4 7 95ZZZW321 119950228A5330 SKIN BOEING727 7272Q9 138448MNM FS 350 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01740DH32254 21930 DURING D-CHECK, FUS EXTERIOR BULGE IN FUS SKIN AT FS 350, BETWEEN STR 26R AND STR 27R, O/B OF ACCESS PANEL. CUT OUT DAMAGED SECTION OF SKIN PER SRM 51-10-6. REMOVED CORROSION FROM LOWER SURFACE OF CHORD ANGLE PER SRM 51-10-6. INSTALLED SKIN REPAIR 16 INCHES BY 11 INCHES .080 2024-T3 AND CHORD ANGLE REPAIR 16 INCHES BY 8 INCHES .100 7075-T6 PER SRM 53-30-3 AND 51-40-4. TOTAL CYCLES 29577. 2L73 4F RTA3WE 19950407002321995040700232NE 1995 4 7 95ZZZW322 219950317A7200 ENGINE BOEING757 757212 NM PWA 2037 PW2037 NE LT ENGINE FLAMEOUT A AMTAK NONE X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 GL11757AT 23127 716327 MDW - WHILE ON MAINTENANCE REPOSITIONING THE LEFT ENGINE FLAMED OUT. (MAINTENANCE TAXIING AIRCRAFT TO OTHER GATE). AFTER TROUBLESHOOTING PER THE F/M, THE LEFT ENGINE FUEL FILTER WAS REMOVED AND REPLACED PER MM. PERFORMED RUN UP PER 71-05-00 IN F/M. OPS CHECK GOOD. TORQUED EEC CONNECTORS PER 73-21-04 IN MM. NO EPCS/EICAS SYSTEM LATCH. 2L72 4F4 FRTA2NM E17NE 19950407002331995040700233WP 1995 4 7 95ZZZW323 119950221A261224490222 CONNECTOR DOUG DC8 DC862 3021970WP NR 2 ENG LOOSE A ARWAK NONE L NO TEST ININSP/MAINT 1 SO1966656 45953 DURING PREFLIGHT FOUND NR 2 ENGINE FIRE WARNING SYSTEM INOP. RESET CANNON PLUG, NR 2 ENGINE FIRE WARNING SYSTEM OK, CHECKED GOOD IAW MM 26-10. 2L74 4F 4A25 19950407002341995040700234WP 1995 4 7 95ZZZW324 119950221A33506012235 BATTERY PACK DOUG DC8 DC863F 302198FWP EEL LIGHTS WEAK A ARWAK NONE L NO TEST ININSP/MAINT 1 SO19661AV 742 45969 DURING PREFLIGHT BY CREW, FOUND EMERGENCY LIGHTS DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD IAW MM 33-50. 2L74 4F 4A25 19950407002351995040700235NM 1995 4 7 95ZZZW325 119950306A7722 EGT SYS BOEING757 757212 NM RT ENG MALFUNCTION A AMTAK NONE M OVER TEMP TOTAKEOFF 1 GL11750AT 23126 ATL - FLT 400 - RT ENG EGT INCREASED TO 649 DEGREES CELSIUS FOR 2 SECONDS, ON TAKEOFF FROM HOWARD AFB, PANAMA. NO SURGE ASSOCIATED. NO OTHER PARAMETERS EXCEEDED, OAT PLUS 35. INSPECTED ENGINE PER MM 72-00-00 P615, NO DAMAGE NOTED. EICAS RT ENG 649 DEGREES CELSIUS AT, 07 SECONDS. ON 3/8/95 REMOVED AND REPLACED ENGINE RT POS. 2L72 4F RTA2NM 19950407002361995040700236 1995 4 7 95ZZZW326 419950312A2565 SLIDE BOEING727 727264 138408MNM FWD ENTRY DETACHED A AMTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL11764AT 22984 IND - FLT NR 975 - FORWARD ENTRY DOOR CHUTE FELL OUT OF ITS CASE AFTER PUSH OUT. REINSTALLED FORWARD CHUTE INTO CASE, SECURED NOW AND CHECKED OK. 2L73 4F A3WE 19950407002371995040700237NM 1995 4 7 95ZZZW327 119950301A32603210278 UPLOCK SWITCH BOEING727 727227 1384078NM NLG MALFUNCTION A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11766AT 21999 STL - FLT 491 - AFTER TAKEOFF UPON GEAR RETRACTION HAD NOSE GEAR UNSAFE INDICATION. RECYCLED GEAR, NO HELP. RAN ABNORMAL PROCEDURES, INDICATION REMAINED. REPLACED NOSE LANDING GEAR UPLOCK SWITCH. PIN WAS STUCK IN GROUND POSITION, PERFORMED REMOVAL/INSTALLATION AND ADJ AND TEST PER MM 32-61-71 PG 402-502, OPS CHECK GOOD. 2L73 4F A3WE 19950407002381995040700238NM 1995 4 7 95ZZZW328 119950309A3350 STRIP BOEING727 7272B7 138407LNM CABIN FELL BROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11762AT 22162 ORD - FLT 298 - EGRESS LIGHTING STRIP BROKEN AT ROW 2. REPAIRED EGRESS LIGHT STRIP, OPS CHECKED GOOD. 2L73 4F A3WE 19950407002391995040700239WP 1995 4 7 95ZZZW329 119950302A7722 CONNECTOR DOUG DC8 DC873F 302199FWP NR 3 EGT LOOSE A SRAAJA DUMP FUEL UNSCHED LANDING O OTHER CLCLIMB 1 SO19873SJ 46091 DURING FLT NR 3571, NR 3 ENGINE EGT DROPPED TO ZERO, RETARDED THROTTLES, NR 3 EGT STABILIZED AT 200 DEGREES THEN BECAME ERRATIC, DUMPED FUEL AND COMPLETED AIR TURN BACK. FOUND LOOSE CONNECTION ON TERMINAL 'D' AT CPC JUNCTION, TIGHTEN CONNECTION, PERFORMED ENGINE GROUND RUN, OPS CHECKED GOOD. 2L74 4F RT4A25 19950407002401995040700240CE 1995 4 7 95ZZZW330 119950209A5753351650505258 FLAP BEECH 1900 1900C 1154161CE LT WING CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV11374 UC119 DURING SCHEDULED MAINTENANCE AN INSPECTION OF THE LEFT OUTBOARD FLAP REVEALED A 1.5 INCH CRACK IN THE UPPER SKIN ALONG THE TRAILING EDGE LOCATED BETWEEN THE FIRST AND SECOND RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER. 2L72 4T RTA24CE 19950407002411995040700241CE 1995 4 7 95ZZZW331 119950209A575310116000144 FLAP BEECH 1900 1900C 1154161CE RT WING CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV11374 UC119 DURING SCHEDULED MAINTENANCE AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 1 INCH CRACK IN THE LOWER SKIN ALONG THE TRAILING EDGE LOCATED BETWEEN THE THIRD AND FOURTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER. (W) 2L72 4T RTA24CE 19950407002421995040700242CE 1995 4 7 95ZZZW332 119950220A7120118910025121 MOUNT TRUSS BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV3661 UC134 DURING A SCHEDULED AD92-06-09 AREA 'A' INSPECTION OF THE LEFT ENGINE MOUNT TRUSS ASSEMBLY REVEALED A .300 INCH CRACK IN THE TOP OF THE OUTBOARD FORWARD UPPER COWL ATTACH BRACKET. THE CRACK WAS REPAIRED BY WELDING. 2L72 4T RTA24CE 19950407002441995040700244CE 1995 4 7 95ZZZW334 119950306A32601003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NOSE DRAG LEG INTERMITTENT A AMWAK NONE N FALSE WARNING APAPPROACH 1 CE0762YV 134 UC62 FLT NR 5682 - ON APPROACH TO MCI WITH THE LANDING GEAR DOWN, WHEN THE FLAPS WERE EXTENDED FULL, THE GEAR INTRANSIT LIGHT ILLUMINATED AND THE GEAR WARNING HORN SOUNDED INTERMITTENTLY. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FERRIED TO ICT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SWITCH WORKING INTERMITTENTLY. REMOVED AND REPLACED NOSE DOWNLOCK SWITCH, GEAR WARNING SYSTEM OPS CHECKED NORMAL. 2L72 4T RTA24CE 19950407002451995040700245CE 1995 4 7 95ZZZW335 119950307A32601003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NOSE DRAG LEG INTERMITTENT A AMWAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 CE0780ZR 3073 UC80 DURING TAXI FROM GATE ON ORIGINATING FLIGHT FROM DSM, THE LANDING GEAR INTRANSIT LIGHT ILLUMINATED AND WARNING HORN SOUNDED INTERMTTENTLY. LOCAL FBO COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS FERRIED TO ICT WHERE MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SWITCH INTERMITTENT. REMOVED AND REPLACED THE NOSE GEAR DOWNLOCK SWITCH, LANDING GEAR WARNING SYSTEM OPS CHECKED NORMAL. 2L72 4T RTA24CE 19950407002461995040700246CE 1995 4 7 95ZZZW336 119950223A7120118910025121 MOUNT TRUSS BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV10397 UC134 DURING A SCHEDULED ENGINE CHANGE AN INSPECTION OF THE LEFT ENGINE MOUNT TRUSS REVEALED A .500 INCH CRACK IN THE UPPER INBOARD FORWARD TUBE AT THE UPPER INBOARD FORWARD TUBE INTERSECTION WELD. THE CRACK WAS REPAIRED BY WELDING. 2L72 4T RTA24CE 19950407002471995040700247NM 1995 4 7 95ZZZW337 119950318A3230257T110315 MODULE BOEING767 767231 1385131NM MLG LEVER STICKING A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE05608TW 22571 LAX - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND INDICATION WAS NORMAL. FOUND LANDING GEAR MODULE, MFG P/N 257T1103-15, EXTEND/RETRACT LEVER STICKING. CLEANED AND LUBRICATED LANDING GEAR MODULE EXTEND/RETRACT LEVER. LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL. CHECK C-4A. 2L72 4F RTA1NM 19950407002481995040700248WP 1995 4 7 95ZZZW338 119950318A323039140165503 CYLINDER DOUG DC9 DC931 3022065WP LT MLG BUNGEE CRACKED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05989Z 47135 STL - AFTER TAKEOFF LEFT MAIN LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION. FOUND LEFT MAIN LANDING GEAR BUNGEE CYLINDER, MFG P/N 3914016-5503 CRACKED. REPLACED LEFT MAIN LANDING GEAR BUNGEE CYLINDER. LANDING GEAR OPERATION AND LIGHT SYSTEMS CHECKED NORMAL. 2L72 4F A6WE 19950407002491995040700249WP 1995 4 7 95ZZZW339 119950320A3230 RETRACT SYS DOUG DC9 DC982 3022082WP NLG REQ'D LUBE A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05914TW 49185 BOS - AFTER TAKEOFF NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR, AND NOSE LANDING GEAR RETRACTED. INSPECTED NOSE LANDING GEAR AND LUBRICATED. JACKED NOSE LANDING GEAR AND OPERATED NOSE LANDING GEAR SEVERAL TIMES AND ALL OPERATIONS WERE NORMAL. 2L72 4F A6WE 19950407002501995040700250NE 1995 4 7 95ZZZW340 219950315A7230739483 BEARING DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE LT ENGINE FAILED A TWAAAE UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 CE059302B 49528 MCI - MADE UNSCHEDULED LANDING ON ACCOUNT THAT THE LEFT ENGINE SHUT DOWN DUE TO POWER LOSS. FOUND METAL IN TAIL PIPE. REPLACED ENGINE S/N 3214. INVESTIGATION INTO LEFT ENGINE SHUT DOWN DUE TO LOSS OF POWER REVEALED NR 3 BEARING MFG P/N 739483 FAILED, DISENGAGING ACCESSORY GEARBOX DRIVE. ENGINE S/N 3214 WAS REPAIRED AND RETURNED TO SERVICE. ENGINE TOTAL TIME 32,672. ENGINE TOTAL TIME 17,193. (W) 2L72 4F4 FRTA6WE E9NE 19950407002511995040700251EU 1995 4 7 AWXA9500138 119950304A5230A22994K2882 CASTING AIRBUS320 A320231 3930325EU CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28620AW 052 PHX - FLT 0031 - DURING ROUTINE MAINTENANCE CHECK, FOUND THE FORWARD CARGO DOOR HANDLE SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 51-72-18 AND COMPLIED WITH ADJUSTMENT CHECK PER AMM 52-31-21, PG 408. NO ADJUSTMENT REQUIRED. (W) 2L72 4F RTA28NM 19950407002521995040700252NM 1995 4 7 AWXA9500140 119950312A3350 CONNECTOR BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 7 THROUGH 11. REATTACHED LOOSE CONNECTOR, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407002531995040700253NM 1995 4 7 AWXA9500141 119950313A3350900835A BATTERY PACK BOEING737 737277 1384570NM CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 DURING ROUTINE MAINTENANCE CHECK, FOUND R1 DOOR AND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED R1 AND R2 OVERHEAD BATTERY PACKS. OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407002541995040700254NM 1995 4 7 AWXA9500149 119950316A3350 CONNECTOR BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 19 THROUGH 23. RESECURED LOOSE CONNECTOR, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407002551995040700255NM 1995 4 7 AWXA9500150 119950317A3350 TERMINALS BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 7 THROUGH 12. RECONNECTED LOOSE TERMINALS, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407002561995040700256NM 1995 4 7 AWXA9500151 119950318A3397 WIRE BOEING737 7373G7 1384595NM CABIN EEL DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 12 TO 14. RECONNECTED WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407002571995040700257EU 1995 4 7 AWXA9500152 119950319A213087292325V04 AEVC AIRBUS320 A320231 3930325EU CABIN MALFUNCTION A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28622AW 054 AIR TURNBACK, ON CLIMB-OUT RECEIVED ECAM MESSAGE 'VENT SKIN VALVE FAULT'. CREW COULD NOT MAINTAIN CABIN PRESSURE. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND 'AVNC VENT' CNT CIRCUIT BREAKER OUT. RESET CIRCUIT BREAKER D7. SYSTEM TEST WAS OK. REPLACED AEVC AS PRECAUTIONARY PER AMM 21-26-34. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA28NM 19950407002581995040700258EU 1995 4 7 AWXA9500158 119950322A5320D5367200400000 PANEL AIRBUS320 A320231 3930325EU FWD PIT DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28621AW 053 PHX - FLT 1274 -DURING C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT THRESHOLD PLATE BENT AND DISTORTED. REMOVED AND REPLACED THRESHOLD PANEL PER SRM 51-72-00. (W) 2L72 4F RTA28NM 19950407002601995040700260WP 1995 4 7 CAL950079 119950130A2420120006650 CIRCUIT BREAKER DOUG DC9 DC982 3022082WP AC BUS 'A' PHASEFAILED A CALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0916802 49222 FLT NR 0461 - EWR - THE AIRCRAFT WAS RETURNED TO EWR AFTER SEVERAL CIRCUIT BREAKERS POPPED IN FLIGHT. RESETTING THE CIRCUIT BREAKERS DID NOT HELP. THE CARGO COMPARTMENT HEATER FAN B AND C, FORWARD RIGHT FUEL BOOST PUMP B AND C, FORWARD CENTER FUEL TANK BOOST PUMP B AND C, AFT FUEL TANK B AND C, AND LEFT AC BUS SYSTEM 'A' ALL POPPED. MX RESET ALL CIRCUIT BREAKERS AND INSPECTED THE LEFT ENGINE CSD, GENERATOR AND FEEDERS WITH NO DEFECTS NOTED. THE LEFT ENGINE WAS RUN AND MAINTENANCE WAS UNABLE TO DUPLICATE THE FAILURE. THE LT AC BUS 'A' PHASE CIRCUIT BREAKER B1-741 WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (W) 2L72 4F A6WE 19950407002611995040700261WP 1995 4 7 CAL950141 119950220A7722 EGT WIRE DOUG DC10 DC1010 3022110WP NR 2 ENG CHAFED A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0968046 47800 FLT NR 0963 - GUM - THE NR 2 ENGINE EGT CIRCUIT BREAKER POPPED IN FLIGHT. WHEN THE CIRCUIT BREAKER WAS RESET, THE LEFT EMERGENCY BUS WAS LOST. APPROPRIATE CHECKLIST PROCEDURES WERE COMPLIED WITH, AND THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRE TO PIN 'J' OF THE EGT INDICATOR CHAFED AND IN CONTACT WITH THE INDICATOR CAUSING A SHORT. THE WIRE WAS INSULATED WITH SHRINK TUBING AND OPERATION CHECKED GOOD. (W) 2L73 4F A22WE 19950407002621995040700262WP 1995 4 7 CAL950148 119950223A3350 EEL BATT DOUG DC9 DC932 3022066WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914524 47539 JAX - FLT 1521 - THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE FWD OVERWING EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (W) 2L72 4F A6WE 19950407002631995040700263WP 1995 4 7 CAL950170 119950302A335041B004AD0763 EEL BATT PACK DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916883 48073 FLT NR 0342 - EWR - ALL THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS SECTION OF CABIN WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT OVERHEAD AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN WAS RESTORED. (W) 2L72 4F A6WE 19950407002641995040700264EU 1995 4 7 CAL950173 119950303A2910NAS161212 O-RING AIRBUS300 A300B4203 3930306EU GREEN HYD SYST LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0913971 262 MCO - FLT 751 - THE GREEN SYSTEM HYDRAULIC QUANTITY LEVEL LOW LIGHT ILLUMINATED WITH THE MWP HYDRAULIC LIGHT AND SSC DURING CRUISE EN ROUTE TO MCO. THE HYDRAULIC PUMPS WERE DUMPED AND THE GREEN SERVO CONTROL WAS SHUT OFF. THE PUMPS WERE TURNED ON AND THE QUANTITY CONTINUED TO DROP. THE PUMPS WERE DUMPED AND 'ABNORMAL' PROCEDURES WERE COMPLIED WITH FOR A SAFE LANDING AT MCO. MAINTENANCE FOUND THE REDUCER FITTING ON RT SIDE OF GREEN SYSTEM HYDRAULIC PRESSURE MANIFOLD LEAKING. THE O-RING ON THE FITTING WAS REPLACED. THE GREEN HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (W) 2L72 4F A35EU 19950407002651995040700265EU 1995 4 7 CAL950174 119950302A2750CHA1171006B GEARBOX AIRBUS300 A300B4103 3930104EU TE FLAPS BINDING A CALAO OTHER O OTHER APAPPROACH 1 SW0916982 091 EWR - FLT 668 - THE ACFT HAD A HISTORY OF THE FLAPS NOT EXTENDING FOR LANDING. THE 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT SIMPLEX BEVEL GEARBOX IN THE NR 6 POSITION BINDING. THE NR 6 RT SIMPLEX BEVEL GEARBOX WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 AND NR 2 RT FLAP TRANSMISSIONS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE DUE TO THE HISTORY OF FLAPS LOCKING OUT. A FUNCTIONAL RIG CHECK OF THE RT FLAP SYSTEM WAS PERFORMED PER MM 27-51-00 AND ALL OPERATION CHECKED GOOD. (W) 2L72 4F A35EU 19950407002661995040700266NE 1995 4 7 CAL950175 219950305A7200 ENGINE BOEING747 747230B 1384889NM PWA JT9 JT9D7A 52054NE NR 1 FAILED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW0978019 20527 662579 HNL - FLT 907 - THE NR 1 ENGINE MADE A LOUD BOOM AFTER ABOUT TWO HOURS OF FLIGHT. THE NOISE WAS ACCOMPANIED BY A RISE IN EGT AND A DECREASE IN EPR AND N1. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO HNL, WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. (W) 2L74 4F4 F A20WE E20EA 19950407002671995040700267NM 1995 4 7 CAL950177 119950306A3350 EEL WIRING BOEING737 737217 1384464NM CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912230 19884 FLT NR 1828 - EWR - A PREFLIGHT CHECK FOUND THE EMERGENCY AISLE PATH LIGHTING FROM ROWS 7-12 INOPERATIVE. MAINTENANCE FOUND WIRING BROKEN ON TRACK LIGHTING AT ROW 12. THE WIRING WAS SPLICED AND THE FUSE ON FORWARD BATTERY PACK WAS REPLACED. OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. (W) 2L72 4F A16WE 19950407002681995040700268WP 1995 4 7 CAL950178 119950306A3350 EEL BATT DOUG DC9 DC932 3022066WP COCKPIT DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912514 48113 IAH - FLT 1859 - BOTH COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERIES IN THE BATTERY PACK FOR THE COCKPIT EMERGENCY LIGHTS WERE REPLACED. OPERATION OF THE COCKPIT EMERGENCY LIGHTS WERE RESTORED. (W) 2L72 4F A6WE 19950407002691995040700269NM 1995 4 7 CAL950182 119950301A5320 SUPPORT BOEING727 727227 1384078NM BS 1030 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW099976349749 20772 GSO - INSPECTION FOUND A .75 INCH CRACK IN FLOOR SUPPORT ANGLE U-CHANNEL AT BS 1030 ABOVE STRINGER 29R. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2. (W) 2L73 4F A3WE 19950407002701995040700270NM 1995 4 7 CAL950183 119950301A335020131A EEL BATTERY PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912327 23457 DHN - THE EMERGENCY EXIT LIGHT BATTERY PACK AT OVERHEAD CABIN STATION STA 630 FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. (W) 2L72 4F RTA16WE 19950407002711995040700271NM 1995 4 7 CAL950184 119950301A335020131A EEL BATT PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912327 23457 DHN - THE EMERGENCY EXIT LIGHT BATTERY PACK IN THE OVERHEAD AFT GALLEY AREA AT STATION 970 FAILED CAPACITY TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00. (W) 2L72 4F RTA16WE 19950407002721995040700272NM 1995 4 7 CAL950186 119950309A323069141065 HYD TRANS CYL BOEING727 727232 1384082NM NLG INOPERATIVE A CALAO OTHER O OTHER APAPPROACH 1 SW09523PE16999 20646 FLT NR 0777 - IAH - THE NLG TOOK APPROXIMATELY 10 SECONDS LONGER TO EXTEND THAN THE MLG, ON APPROACH TO IAH. WHEN THE NOSE GEAR DID EXTEND IT WAS ACCOMPANIED BY A BANG. MAINTENANCE FOUND THE NLG HYDRAULIC TRANSFER CYLINDER AT FAULT. THE TRANFER CYLINDER WAS REMOVED AND REPLACED. IN ADDITION, THE DRAG BRACE WAS LUBRICATED. OPERATION OF THE NLG CHECKED GOOD. (W) 2L73 4F A3WE 19950407002731995040700273NM 1995 4 7 CAL950191 119950305A335020131A EEL BATT PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959302 23353 BFM - INSPECTION FOUND THE EMERGENCY LIGHT ABOVE ROW 22 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950407002741995040700274NM 1995 4 7 CAL950192 119950305A3350 EEL BATTERY PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959302 23353 BFM - INSPECTION FOUND THE EMERGENCY LIGHT ABOVE ROW 2D INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950407002751995040700275NM 1995 4 7 CAL950193 119950305A335020131A EEL BATTERY PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959302 23353 BFM - INSPECTION FOUND THE EMERGENCY LIGHT ABOVE ROW 16 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950407002761995040700276NM 1995 4 7 CAL950194 119950305A335020131A EEL BATT PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959302 23353 BFM - INSPECTION FOUND THE EMERGENCY LIGHT ABOVE ROW 14 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950407002771995040700277NM 1995 4 7 CAL950195 119950305A335020131A EEL BATT PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959302 23353 BFM - INSPECTION FOUND EMERGENCY LIGHT ABOVE ROW 23 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F RTA16WE 19950407002781995040700278NM 1995 4 7 CKSA95011 119950308A261260B0002389 FIRE LOOP BOEING747 747146 NM NR 2 ENGINE DEFECTIVE A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23702CK78110 20332 DURING CLIMB-OUT AT 1000 FEET NR 2 ENGINE 'A' LOOP FAULT LT ILLUMINATED. REMOVED AND REPLACED NR 2 ENGINE 'A' FIRE LOOP DETECTOR. OPS CHECK GOOD IAW MM 26-10-00. (W) 2L74 4F A20WE 19950407002791995040700279NM 1995 4 7 CKSA95012 119950313A261260B002385 'A' LOOP BOEING747 747146 NM NR 1 ENGINE SHORTED OUT A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23702CK78163 20332 ENGINE FIRE LIGHT (AMBER) CAME ON IN FLIGHT, (ALSO FAULT LIGHT NR 1 ENGINE 'A' LOOP FULL SCALE DEFLECTION). REMOVED AND REPLACED NR 1 ENGINE 'A' LOOP. OPS CHECKS GOOD. (W) 2L74 4F A20WE 19950407002801995040700280WP 1995 4 7 MGMA950148 119950316A793142D491C SWITCH DOUG DC8 DC862 3021970WP NR 3 ENGINE FAILED A MGMAO OTHER N FALSE WARNING CLCLIMB 1 WP23802MG 3096 46098 NR 3 ENGINE OIL PRESSURE LIGHT CAME ON WITH OIL PRESSURE TEMPERATURE NORMAL. ABNORMAL CHECKLIST PERFORMED, LIGHT STILL STAYED ON. DURING APPROACH INTO EWR, LIGHT WENT OFF. CLEANED OIL FILTER AND REMOVED AND REPLACED DIFFERENTIAL OIL PRESSURE SWITCH. RAN ENGINE SYSTEM. GROUND OPERATIONAL CHECKS NORMAL PER MAINTENANCE MANUAL. TOTAL CYCLES 13,001. 2L74 4F 4A25 19950407002811995040700281NE 1995 4 7 MGMA950158 219950319A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 1 FAILED A MGMAFEA ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23801MG301696289 45986 669787 PRIOR TO SETTING THE EPR BEFORE 80 KTS HEARD A LOUD BANG AND NR 1 ENGINE INDICATIONS READS AS FOLLOWS, EGT EQUALS 600, N2 EQUALS 0, FF EQUALS 0, N1 EQUALS 0, OIL PRESSURE EQUALS 0 AND OIL TEMP EQUALS 75, AND OIL QUANTITY READ 5.0 GALLONS. WE WERE ADVISED OF BALLS OF SMOKE COMING OUT OF THE ENGINE AND EGT KEPT CLIMBING. ON CAPTAINS COMMAND, BLEW FORWARD AGENT AFTER COMPLETING ENGINE FIRE FAILURE CHECKLIST. MAINTENANCE FERRIED AIRCRAFT TO OSCODA FOR ENGINE CHANGE. TOTAL CYCLES 14,739. 2L74 4F4 F 4A25 1E8 19950407002821995040700282NM 1995 4 7 MGMA950167 119950319A2750 LINKAGE BOEING727 727191 1384063NM MLG WW BINDING A MGMAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP23503MG 19392 WHEN SELECTING FLAPS 5 DEGREES, OUTBOARD FLAPS STUCK AT 2 DEGREES. FOLLOWED GRAND AIR ABNORMAL CHECKLIST. LANDED NORMAL FLAPS AND SLATS. AFTER LANDING, CYCLED FLAP, OPERATED NORMAL. FOUND OUTBOARD FLAP SELECTOR VALVE LINKAGE BINDING, LUBRICATED SAME, CYCLED FLAPS SEVERAL TIMES. GROUND OPS CHECK NORMAL PER MM 27-51-51. (W) 2L73 4F A3WE 19950407002831995040700283WP 1995 4 7 RAIA950317 219950313A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE WORN A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03424AM5326 865 66322 STL - FLT 7088 - RT ENGINE ONLY ACHIEVED 82 PERCENT TORQUE. MAINTENANCE REPLACED BLEED AIR GASKETS ON THE RIGHT ENGINE. GROUND POWER RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T4 TRTA56EU E4WE 19950407002841995040700284EU 1995 4 7 RAIA950318 119950313A21501379239L402 DUCT BAG JETSTMJETSTM3201 1500217EU RT PACK CRACKED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03436AM8528 891 STL - FLT 7496 - DUCT LIGHT ILLUMINATED ON THE RIGHT SIDE. MAINTENANCE REPLACED RIGHT HEAT EXCHANGER DUCT ASSEMBLY. (W) 2L72 4T RTA56EU 19950407002851995040700285EU 1995 4 7 RAIA950319 119950312A33501317 EEL AEROSPATR42 ATR42300 8680920EU CABIN MISSING A RAIAK NONE O OTHER ININSP/MAINT 1 CE032FOR 10288 199 STL - ESCAPE PATH LIGHTING MISSING. MAINTENANCE REPLACED ESCAPE PATH LIGHTING. (W) 2H72 4T RTA53EU 19950407002861995040700286 1995 4 7 RAIA950325 419950315A3444 WARNING AEROSPATR42 ATR42300 8680920EU GPWS ACTIVATED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03424TE 124 STL - 7180 - GPWS WARNING GOES ON CONTINUOUSLY, WILL NOT STOP. MAINTENANCE DEFERRED GPWS SYSTEM AS PER MEL 34-48-1 CAT A. (W) 2H72 4T RTA53EU 19950407002871995040700287EU 1995 4 7 RAIA950326 119950313A3350OL60423P EEL BULBS AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03723TE6200 283 STL - FLT 7160 - TWO EMERGENCY FLOOR LIGHTS IN THE CABIN ARE INOP. MAINTENANCE REPLACED LIGHT BULBS FOR EMERGENCY LIGHTS IN CABIN. (W) 2H72 4T RTA53EU 19950407002881995040700288NE 1995 4 7 RAIA950327 219950316A7260NSA8203210 O-RING AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RT ENG CUT A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03424TE12177 124 1200661 STL - FLT 7150 - RIGHT ENG OIL PRESSURE FLUX. CREW DIVERTED TO CGI AND LANDED SAFELY. MAINTENANCE REPLACED RT ENGINE AIRCRAFT UNREGULATED GENERATOR O-RING. GROUND RUN AND LEAK CHECK GOOD. 2H72 4T4 TRTA53EU E20NE 19950407002891995040700289EU 1995 4 7 UF6A950302 119950313A6123S5600075N CONNECTOR BAG ATP ATP EU RT ENGINE DIRTY A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03854AW7686 7686 2028 ORD - FLT 5020 - THE NR ONE AUTO FEATHER UNIT WILL NOT ARM. MAINTENANCE CLEANED CANNON PLUG 'C'. (W) 2L72 4T RTA27NM 19950407002901995040700290WP 1995 4 7 USAA950238 119950312A213054447222 ACTUATOR DOUG DC9 DC931 3022065WP AFT FUSELAGE INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19993VJ30788 47332 PIT - FLT 0757 - FLIGHT DIVERTED TO PIT DUE TO A PRESSURIZATION PROBLEM. MAINTENANCE REPLACED THE OUTFLOW DOOR AFT MOTOR AND GEAR BOX. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950407002911995040700291WP 1995 4 7 USAA950239 119950312A3350 EEL LIGHTS DOUG DC9 DC931 3022065WP CABIN MALFUNCTION A USAAK NONE L NO TEST ININSP/MAINT 1 EA19991VJ 47310 CLT - FLT 0845 - THE FLOOR TRACK LIGHTING MALFUNCTION AT DEPARTURE TIME. (W) 2L72 4F A6WE 19950407002921995040700292WP 1995 4 7 95ZZZX1622 119950204A32600080004004 PROXIMITY SWITCH DOUG DC9 DC932 3022066WP RT MLG DEFECTIVE A VJ6AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11914VV 47486 ATL/TPA - FLT 101 - RETURNED TO ATL DUE TO UPON RAISING LANDING GEAR, NOSE GEAR UNSAFE LIGHT REMAINED ON. RIGHT GEAR UNSAFE LIGHT REMAINED ON ALSO. REMOVED AND REPLACED PROXIMITY SWITCH BOX, PN 008-0004-004, SN OFF 254, SN ON 263. OPERATION SELF-TEST IAW VALUEJET MM 32-00. AIRCRAFT WAS TEST FLOWN, OPS CHECK OKAY. 2L72 4F A6WE 19950407002931995040700293WP 1995 4 7 95ZZZX1623 119950204A575359121542 FLAP DOUG DC9 DC932 3022066WP RT FLAP TE DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11523MD 47320 AIRCRAFT WAS PORTED ON THE RAMP, CUSTOMERS WERE LOADING ONTO THE AIRCRAFT WHEN THE RIGHT TRAILING EDGE OF THE FLAP WAS STRUCK BY A BAGGAGE CART. APPROXIMATELY 20 INCHES OF THE TRAILING EDGE WAS BROKEN OFF. 2L72 4F A6WE 19950407002941995040700294NE 1995 4 7 95ZZZX1624 219950215A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 2 POWER LOSS A VJ6ACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO11923VV 47488 674194 IAD/PBI - FLIGHT 477 - RUNWAY CONDITIONS, STANDING SLUSH. DURING TAKEOFF, NR 2 ENGINE EXPERIENCED A LOUD BANG ACCOMPANIED BY DECAYING OF THE NR 2 ENGINE INSTRUMENTS. INITIATED A REJECTED TAKEOFF AT 110 KNOTS. ACCOMPLISHED A VISUAL INSPECTION OF NR 2 ENGINE INLET AND EXHAUST, THEN PERFORMED A POWER ASSURANCE RUN TO TAKEOFF POWER. ALSO, PERFORMED REJECTED TAKEOFF WORK CARDS NR 0027. OPS CHECKED GOOD PER MM 71-00, PAGE 537. 2L72 4F4 F A6WE E2EA 19950407002951995040700295WP 1995 4 7 95ZZZX1625 119950215A32607000010101 POSITION SWITCH DOUG DC9 DC932 3022066WP LT MLG DOWNLOCK MALFUNCTION A VJ6AL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO11901VJ 47275 ATL - FLT 134 - DURING APPROACH, LEFT GEAR UNSAFE LIGHT INITIATED A GO-AROUND. LANDED IN ATL, NO TROUBLE REPORTED. REMOVED AND REPLACED THE LEFT GEAR DOWNLOCK SWITCH AND CONNECTOR. 2L72 4F A6WE 19950407002961995040700296WP 1995 4 7 95ZZZX1626 119950127A7312320115 ANTI-ICE VALVE DOUG DC9 DC932 3022066WP RT FUEL HEAT MALFUNCTION A VJ6AA UNSCHED LANDING M OVER TEMP CRCRUISE 1 SO11901VJ 47275 ATL/IAD - FLT 368 - AIRCRAFT RETURNED TO ATL DUE TO RIGHT FUEL HEAT STAYED ON CAUSING OIL TEMP TO EXCEED 120 DEGREES CENTIGRADE. REMOVED AND REPLACED NR 2 ANTI-ICE VALVE. 2L72 4F A6WE 19950407002971995040700297WP 1995 4 7 95ZZZX1627 119950313A2410106855MA696233B CSD DOUG DC9 DC932 3022066WP NR 2 ENGINE FAILED A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 SO11905VJ 47378 IAD/ATL - FLT 173 - EXPERIENCED NR 2 ENGINE CSD OVERTEMP AND FOUND THE CSD WOULD NOT DISCONNECT. CREW WAS INFORMED TO SHUT DOWN NR 2 ENGINE AND AIR TURNED BACK TO IAD. CREW DECLARED AN EMERGENCY AND LANDED WITH NO OTHER PROBLEMS. 2L72 4F A6WE 19950407002981995040700298WP 1995 4 7 95ZZZX1628 119950314A3231 DOOR DOUG DC9 DC932 3022066WP NLG MALFUNCTION A VJ6AA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11923VV 47488 DTW/ATL - FLT 441 - RETURNED TO DTW DUE TO A VIBRATION FROM NOSE GEAR WHEELWELL AREA AFTER GEAR RETRACTION. FOUND NOSE GEAR DOORS OPEN. CLOSED DOORS AND INSPECTED NOSE GEAR AREA PER MM 32. 2L72 4F A6WE 19950407002991995040700299WP 1995 4 7 95ZZZX1629 119950320A2530 COFEEMAKER DOUG DC9 DC932 3022066WP GALLEY OVERHEAT A VJ6AAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO111269L 47285 ATL/PBI - FLT 501 - RETURNED TO ATL BECAUSE ON CLIMB-OUT CAPTAIN REPORTED SMOKE IN THE COCKPIT COMING FROM THE GALLEY AREA BEHIND THE FIRST OFFICER'S SEAT, AND DECLARED AN IN-FLIGHT EMERGENCY. ON FINAL APPROACH, CAPTAIN PULLED FORWARD GALLEY CIRCUIT BREAKER AND SMOKE STOPPED. AN OVERWEIGHT LANDING WAS MADE AT 101,000 POUNDS. PERFORMED OVERWEIGHT LANDING INSPECTION. REMOVED COFFEEMAKER AND PLACED ON MEL. 2L72 4F A6WE 19950407003001995040700300EU 1995 4 7 95ZZZX1630 119950220A2612CA3106KE2821P CONNECTOR BRAERODH125 HS125700A 4230170EU RT PYLON CORRODED A AJCAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING NRNOT REPORTED 1 EA2567PW 8538 NA0303 CREW EXPERIENCED NR 2 ENGINE FIRE WARNING. SHUT DOWN ENGINE AND DISCHARGED NR 1 AND NR 2 FIRE EXTINGUISHERS. FIRE WARNING REMAINED ON. LANDED AT CPR, INVESTIGATED AND FOUND NO EVIDENCE OF FIRE, OVERHEAT, OR BLEED AIR LEAK. FURTHER INVESTIGATION FOUND CORRODED PYLON CANNON PLUG SHORTED, GIVING FALSE FIRE WARNING INDICATION. REPLACED CANNON PLUG. OPS CHECK NORMAL. RECOMMEND INSPECTION OF TB1 CANNON PLUG IN LT AND RT PYLONS FOR CORROSION. REPLACE IF NECESSARY. 2L72 4F A3EU 19950407003011995040700301NM 1995 4 7 95ZZZX1631 119950315A3260 WIRE BOEING727 727231 1384079NM DOWNLOCK SENSOR BROKEN A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE0554325 20232 STL - FLT 246 - RT MAIN GEAR UNSAFE WARNING LIGHT REMAINED ON WHEN LANDING GEAR WAS EXTENDED. CYCLED LANDING GEAR WITH SAME RESULTS. FOUND BROKEN WIRE APPROXIMATELY TWELVE INCHES FROM THE DOWNLOCK PROXIMITY SENSOR. SPLICED BROKEN WIRE. OP CHECKS NORMAL. CHECK C-2 - 3-22-94 - MCI. 2L73 4F A3WE 19950407003021995040700302NM 1995 4 7 95ZZZX1632 119950308A2530 SERVING CART BOEING747 747257B 1384853NM CABIN FAILED A TWAAOH OTHER DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05303TW 1374 20116 JFK - FLT 885 - DURING CRUISE, SINGLE SERVICE CART POSITION D5A, OVERHEATED AND EMITTED SMOKE. CIRCUIT BREAKER TRIPPED. DISCONNECTED SERVING CART. REPLACED SINGLE SERVICE CART, SN 1374. SINGLE SERVICE CART POSITION OPERTION CHECKED NORMAL. CHECK C-2 - 4-3-94 - MCI. 2L74 4F A20WE 19950407003031995040700303NE 1995 4 7 95ZZZX1633 219950315A7320 PS4 LINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE LEAKING A P5CAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 WP23854FT 19754 662462 VCP/JFK - EN ROUTE AT FL 350 IN CRUISE, NR 1 ENGINE LOST POWER, N1, N2, EPR, AND FUEL FLOW DECREASED AND EGT INCREASED. RE-START ATTEMPTED, BUT WAS UNSUCCESSFUL. DESCENDED TO FL 310 AND WAS ABLE TO RE-START ENGINE USING GROUND START PROCEDURE. REST OF FLIGHT UNEVENTFUL. POST-FLIGHT BORESCOPE INSPECTION FOUND NO DISCREPANCIES. ADDITIONAL INSPECTION FOUND A LEAK AT A B-NUT ON THE PS4 LINE. TIGHTENED B-NUT. ENGINE RUN-UP PERFORMED IAW MM. ALL PARAMETERS NORMAL. 2L74 4F4 F A20WE E20EA 19950407003041995040700304WP 1995 4 7 CAL950188 119950312A3350 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916815 49113 EWR - FLT 0443 - SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 5-8. THE EMERGENCY LIGHT BATTERY PACK AT STA 427R WAS FOUND INOPERATIVE. THE BATTERIES FOR THE BATTERY PACK WERE REMOVED AND REPLACED. OPERATION OF THE OVERHEAD EMERGENCY LIGHTS AT ROWS 5-8 WAS RESTORED. (X) 2L72 4F A6WE 19950407003051995040700305NM 1995 4 7 CKSA95006 119950125A3234366103 SELECTOR VALVE BOEING747 747132 1384882NM LANDING GEAR BYPASSING A CKSAO OTHER J WARNING INDICATION APAPPROACH 1 GL23625PL7256372563 20247 SAEZ - FLT 61331 - ON APPROACH, BOTH BODY GEARS AND NOSE GEAR DID NOT EXTEND, WING GEAR OPERATION NORMAL. TRIED MANUAL EXTENSION WITH GEAR HANDLE OFF WITH NO CHANGE. TRIED MANUAL GEAR EXTENSION WITH GEAR HANDLE DOWN AND ALL GEAR OPERATED NORMALLY. REPLACED BODY AND NOSE GEAR SELECTOR VALVE, RIGGED BOTH SELECTOR VALVE QUADRANTS PER MM 32-31-0. GROUND CHECKS NORMAL. (X) 2L74 4F A20WE 19950407003061995040700306EU 1995 4 7 GAIA954 219950221A7200 ENGINE CVAC 240 240D 2422660WP RROYCEDART DART54210 54522EU LEFT FLAMED OUT A GAIAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 SW0794205 10 40033 YIP/CLE - FLT 205 - 25 MILES OUT IN HEAVY ICING CONDITIONS ON DESCENT INTO CLEVLEAND, OHIO, (THE ANTI-ICE SYSTEM HAD PREVIOUSLY BEEN ACTIVATED) THE LT ENGINE AUTOFEATHERED DUE TO AN ENGINE FLAME-OUT. THE FLIGHT CREW DECLARED AN EMERGENCY. THE AIRCRAFT MADE AN UNEVENTFUL LANDING AND WAS TOWED TO MAINTENANCE AREA. THE AIRCRAFT ENGINE WAS INSPECTED AND OPERATIONAL CHECKED IAW KHAC CV-600 MAINTENANCE CHECK LIST FOR ENGINE GROUND RUN CHECKS. NO DEFECTS WERE NOTED DURING GROUND CHECKS OF ENGINE, AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4R4 TRTA793 E5EU 19950407003081995040700308EU 1995 4 7 RAIA950321 119950314A3231S5287670800000 PIN AEROSPATR72 ATR72202 8680940EU NOSE GEAR LOOSE A RAIAA UNSCHED LANDING OE OTHER VIBRATION/BUFFET CLCLIMB 1 CE03722TE7959 220 STL - FLT 7010 - VIBRATION DETECTED AFTER RETRACTION OF GEAR. SUSPECT GEAR DOOR. UPON INSPECTION, MAINTENANCE DISCOVERED FORWARD MANUAL RELEASEABLE DOOR LOCK PIN LOOSE. MAINTENANCE RESECURED LOCK PIN. (X) 2H72 4T RTA53EU 19950407003091995040700309SW 1995 4 7 SWHA95003 119950306A56202790609007 SEAL 2790609003 SWRNGNSA227 SA227AC 8780603SW WINDOW REVEAL RUSTY A ASWHAK NONE O OTHER ININSP/MAINT 1 SW17789C AC540 WHILE PERFORMING AN UNSCHEDULED INSPECTION FOR SUSPECTED CORROSION, THE FOLLOWING CONDITION WAS DISCOVERED. AT EACH CABIN WINDOW, THE ACRYLIC PANE ATTACHMENT HARDWARE WAS FOUND CORRODED (RANGING FROM LIGHT TO VERY HEAVY) IN APPROXIMATELY 35 OUT OF THE 52 LOCATIONS. INVESTIGATION REVEALED THAT AT EACH CORRODED SCREW/NUT THERE WAS A CORRESPONDING INDENTION AND RUST STAIN AT EACH WINDOW TRIM ASSEMBLY SEAL (PN 27-90609-007). IT APPEARS THIS SEAL CHAFES THE HARDWARE ERODING THE PROTECTIVE COATING AND HOLDING MOISTURE. (X) 1L72 4T A8SW 19950407003101995040700310EU 1995 4 7 UF6A950305 119950317A612330048000014 AUTOFEATHER UNIT BAG ATP ATP EU LT ENGINE FAILED A UF6AO OTHER L NO TEST TXTAXI/GRND HDL 1 CE03854AW5652 2028 PIA - FLT 5096 - LEFT ENGINE AUTOFEATHER UNIT WILL NOT ARM. REMOVED AND REPLACED THE LEFT AUTOFEATHER UNIT. (X) 2L72 4T RTA27NM 19950407003111995040700311NM 1995 4 7 USAA950144 119950215A3350 FLOOR LIGHTS BOEING737 7372B7 1384560NM CABIN EEL MALFUNCTION A USAAK NONE L NO TEST ININSP/MAINT 1 EA19283AU 23116 PHL - EMERGENCY EXIT LIGHTS ILLUMINATE ABOUT EVERY 45 MINUTES, THEN SLOWLY FADE BACK TO OFF. MAINTENANCE FOUND FLOOR LIGHTS ON CONSTANTLY IN ARM. DISCONNECTED PLUG D4049F TO CHECK POWER. POWER CHECKED GOOD. WHEN RECONNECTED, PROBLEM DID NOT OCCUR. OPS CHECK NORMAL. (X) 2L72 4F A16WE 19950407003121995040700312NM 1995 4 7 USAA950192 119950227A3350MCR5 FUSE BOEING737 7374B7 1384702NM EMERG LIGHT SYS INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19447US 24874 CLT - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RPELACED FUSE ON M1479 EMERGENCY LIGHT BATTERY PACK AND RESAFTIED AFT FLIGHT ATTENDANT EMERGENCY EXIT LIGHT SWITCH. (X) 2L72 4F RTA16WE 19950407003131995040700313NM 1995 4 7 USAA950193 119950228A3350 BATTERY PACK BOEING737 737201 1384454NM EMERG LIGHT SYS INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19241US 22443 LGA - EMERGENCY EXIT LIGHTS FLASHING ROWS 8 THROUGH 15. MAINTENANCE REPLACED BATTERY PACK AT POWER SUPPLY ON SEAT 11A. (X) 2L72 4F A16WE 19950407003141995040700314 1995 4 7 USAA950219 419950308A3441HG1050AD05 IRU FOKKERF28 F28MK0100 4990807EU NR 1 FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19891US22510 11366 CLT - FLT 1112 - FLIGHT RETURNED TO GATE WITH A COMPASS PROBLEM WHICH MAINTENANCE FIXED. FLIGHT PROCEEDED AGAIN AND AFTER TAKEOFF, THE NR 1 UNIT FAILED AGAIN. CREW DECIDED TO RETURN TO CLT. MAINTENANCE REPLACED THE NR 1 IRU. OPERATIONS CHECKED GOOD. (X) 2L72 4F RT 19950407003151995040700315EU 1995 4 7 USAA950221 119950307A2916 RESERVOIR FOKKERF28 F28MK4000 4990810EU HYD SYSTEM LOW PRESSURE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19486US 11237 CLT - FLT 0366 - AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT. CAPTAIN WENT THROUGH PROPER PROCEDURES AND RECEIVED THREE GREEN DOWNLOCK LIGHTS. CREW DECIDED TO RETURN TO CLT. MAINTENANCE RECHARGED THE HYDRAULIC RESERVOIR PRESSURE. HYDRAULIC SYSTEM AND LANDING GEAR OPERATIONS CHECKED GOOD. (X) 2L72 4F RTA20EU 19950407003161995040700316EU 1995 4 7 USAA950225 119950125A5312 BULKHEAD FOKKERF28 F28MK4000 4990810EU FWD PRESS CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19499US28785 11182 PIT - DURING SCHEDULED STRUCTURES VISIT, FOUND 7.5 INCH CRACK IN AFT SIDE OF FORWARD PRESSURE BULKHEAD BETWEEN STA 72 AND STA 73. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PLATE PER SRM 53-11-00, PAGE 2. (X) 2L72 4F RTA20EU 19950407003171995040700317EU 1995 4 7 USAA950232 119950313A2822229432 PUMP FOKKERF28 F28MK0100 4990807EU R1, R2 INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19897US 11392 PIT - FLT 0141 - THE R1 FUEL BOOST PUMP FAULT LIGHT ILLUMINATED IN-FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTEANCE REPLACED THE R1 AND R2 BOOST PUMPS AND COCKPIT OVERHEAD PANEL. OPERATIONS CHECKED GOOD. (X) 2L72 4F RT 19950407003181995040700318WP 1995 4 7 USAA950235 119950310A323139567851 LINK DOUG DC9 DC931 3022065WP NLG LT FWD DAMAGED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19926VJ 48146 PIT - FLT 0590 - UPON GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE GEAR. THE RED UNSAFE LIGHT ILLUMINATED. THE GEAR WAS PUT DOWN, BUT THE LIGHT REMAINED. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT NOSE GEAR FORWARD LINK DUE TO DAMAGE. THE EXTENSION/RETRACTION AND FREE FALL ALL GOOD. (X) 2L72 4F A6WE 19950407003191995040700319WP 1995 4 7 USAA950236 119950311A2751ST12BD TRANSMITTER DOUG DC9 DC931 3022065WP RIGHT FLAP OUT OF LIMITS A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19929VJ 48118 CLT - FLT 8027 - AFTER TAKEOFF, THE STALL INDICATION FAIL AND WINDSHEAR WARNING LIGHTS ILLUMINATED. FLIGHT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT FLAP TRANSMITTER. OPERATIONS CHECKED GOOD. (X) 2L72 4F A6WE 19950407003201995040700320WP 1995 4 7 USAA950237 119950309A3230 CONTROL CABLE DOUG DC9 DC931 3022065WP RT MLG WW FROZEN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19933VJ 47216 DTW - FLT 1698 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR CONTROL CABLE IN THE RIGHT WHEEL WELL FROZEN. THE OBSTRUCTION WAS CLEANED. AIRCRAFT OKAY FOR SERVICE. (X) 2L72 4F A6WE 19950407003211995040700321NM 1995 4 7 WRLA95010 119950319A7400 IGNITION DOUG MD11 MD11 3023602NM NR 3 ENG A FAIL LIGHT A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27275WA 48631 AFTER PUSHBACK, NR 3 ENGINE 'A' IGNITION FAIL ILLUMINATED. CREW ELECTED TO RETURN TO GATE. GROUND CREW ASSIGNED DMI M74MR19-15 TO NR 3 ENGINE 'A' IGNITION. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950407003431995040700343 1995 4 7 95ZZZW341 419950307A3442M15851622 INDICATOR BOEING727 727228 NM RADAR FAILED A DHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01720DH 1430 19544 DURING CLIMB, RADAR INTERMITTENTLY INOP. ANNUNCIATES 'ANTENNA' IN BOTH 'TEST' AND 'WX' MODES. PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RADAR INDICATOR. OPS CHECK GOOD PER BOEING MM 34-41-0. 2L73 4F A3WE 19950407003441995040700344WP 1995 4 7 95ZZZW342 119950311A326056487405507 UPLOCK LINKAGE DOUG DC8 DC873F 302199FWP RT MLG DIRTY A DHLAO OTHER N FALSE WARNING CLCLIMB 1 SO01801DH 46033 DURING CLIMB-OUT OF CVG, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. LIGHT REMAINED ILLUMINATED AFTER 3 GEAR RECYCLES. SELECTED GEAR HANDLE TO UP POSITION, AND LEFT IT UP, LIGHT WENT OUT. CLEANED DEBRIS FROM RIGHT MAIN LANDING GEAR UPLATCH SWITCH. LUBED RIGHT UPLATCH OVERCENTER LINKAGE. PERFORMED UPLATCH CHECK IAW MM 32-32-5 PAGE 203. NO DISCREPANCIES NOTED. 2L74 4F RT4A25 19950407003451995040700345WP 1995 4 7 95ZZZW343 119950308A324626014112A WHEEL ASSY DOUG DC8 DC873F 302199FWP NR 1 MLG NR 2 FAILED A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH H1188 46125 DURING LANDING, HEARD A THUMPING NOISE AND WAS UNABLE TO TAXI CLEAR OF RUNWAY. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRE/WHEEL ASSY, PER DC8 MM 32-40-00. REFERENCE NR 95ZZZW344. 2L74 4F RT4A25 19950407003461995040700346WP 1995 4 7 95ZZZW344 119950308A324626014112A WHEEL ASSY DOUG DC8 DC873F 302199FWP NR 1 MLG FAILED A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH 2053 46125 DURING LANDING, HEARD A THUMPING NOISE AND WAS UNABLE TO TAXI CLEAR OF RUNWAY. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRE/WHEEL ASSY, PER DC8 MM 32-40-00. REFERENCE NR 95ZZZW343. 2L74 4F RT4A25 19950407003471995040700347NM 1995 4 7 95ZZZW345 119950318A783062162 SWITCH BOEING727 727228 NM NR 2 TR UNIT FAILED A DHLAO OTHER N FALSE WARNING LDLANDING 1 SO01727DH 20404 ENGINE NR 2 REVERSER OPERATING LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED NR 2 ENGINE REVERSER LIGHT SWITCH. OPS CHECKS NORMAL, MM 78-00. 2L73 4F A3WE 19950407003481995040700348NM 1995 4 7 95ZZZW346 119950324A33501619 EEL BULB BOEING737 7372P6 NM LT FWD DOOR FAILED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO132FOR 21356 LEFT FORWARD ENTRY DOOR (EXTERIOR) EMERGENCY SLIDE LIGHT INOP. RELAMPED BURNED OUT BULB, OPS CHECK NORMAL IAW MM 33-51-11 AND 33-51-21. (W) 2L72 4F RTA16WE 19950407003491995040700349NM 1995 4 7 95ZZZW347 119950305A3230651781910 ACTUATOR BOEING737 7372P6 NM NLG DOWNLOCK BROKEN A A6XAK NONE O OTHER DEDESCENT 1 SO132FOR 35615 21612 NOSE GEAR DOWNLOCK ACTUATOR UPPER ATTACH FITTING BROKEN. REMOVED AND REPLACED DOWNLOCK ACTUATOR IAW MM 32-33-21. (W) 2L72 4F RTA16WE 19950407003501995040700350NM 1995 4 7 95ZZZW348 119950102A33500L3071BPEGPL EEL BULB BOEING737 7372P6 NM CABIN FAILED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO132FOR 21612 LAST AFT RED SECTION OF FLOOR PROXIMITY LIGHTING INOP. RELAMPED BURNED OUT BULB. OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950407003511995040700351NM 1995 4 7 95ZZZW349 119950111A33500L3071BPEGPL EEL BULB BOEING737 737247 138448DNM CABIN FAILED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO134515W 19612 ESCAPE PATH LIGHT INOP AT SEAT ON ROW 5. RELAMPED BURNED OUT BULB. OPS CHECK NORMAL. (W) 2L72 4F A16WE 19950407003521995040700352NM 1995 4 7 95ZZZW350 119950111A33501619 EEL BULB BOEING737 737247 138448DNM CABIN FAILED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO134515W 19612 L-2 DOOR EXTERIOR ESCAPE PATH LIGHT INOP. RELAMPED BURNED OUT BULB. OPS CHECK NORMAL. (W) 2L72 4F A16WE 19950407003531995040700353NM 1995 4 7 95ZZZW351 119950111A3350BR9279110 EEL BULB BOEING737 737247 138448DNM CABIN FAILED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO134515W 19612 LEFT WING OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED BURNED OUT BULB. OPS CHECK NORMAL. (W) 2L72 4F A16WE 19950407003541995040700354NM 1995 4 7 95ZZZW352 119950317A2150 PACK BOEING727 727225 1384077NM RT MALFUNCTIONED A TAOAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15923TS 20441 RIGHT PACK OVERHEATED AFTER TAKEOFF. PACK WENT TO 160 CELSIUS. CREW REPORTED SMOKE IN CABIN. PACK SHUTOFF. CHECKED ALL RT PACK DUCTS, FLOW CONTROL VALVES AND SENSE LINES FOR LEAK AND SECURITY, ALL OK. CHECKED RAM AIR INLETS AND INLET DOOR, FOUND OK. LUBED RAM AIR DOORS, CLEANED ELECTRICAL CONNECTORS AT RT MIX VALVE AND ACM OVERHEAT SWITCHES, AND RE-TORQUED SENSOR LINES PRECAUTIONARY. OPERATED PACKS WITH LEVER LATCH CIRCUIT BREAKER PULLED, FLAPS 15. SYSTEM CHECKED OK PER MM 21-55-0. (W) 2L73 4F A3WE 19950407003551995040700355NM 1995 4 7 95ZZZW353 119950220A5510 CHORD BOEING727 7272Q9 138448MNM LT STABILIZER CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION AT UPPER T/E CHORD LOWER SIDE OUTBOARD END (LT STABILIZER). REMOVED CORROSION PER SRM 51-10-06, ALODINE AND PRIMED PER SRM 51-10-2, CORROSION OUT OF LIMITS, INSTALLED DOUBLER REPAIR PER SRM 5-10-6, REPAIR 2 INCHES BY 33 INCHES 2024-T3 .125. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407003561995040700356NM 1995 4 7 95ZZZW354 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 950 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON STRINGER 29R AFT OF BS 950E. REMOVED CORROSION AS PER SRM 51-10-6. FOUND CORROSION CRACK, STOP DRILLED AS PER SRM 51-10-1. ALODINED AND PRIMED AS PER SRM 51-10-2. INSTALLED REPAIR AS PER SRM 51-40-4 2 INCHES BY 2 INCHES 14 INCHES 7075-T6 .100 (2 EACH). TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407003571995040700357NM 1995 4 7 95ZZZW355 119950220A5315 FLOOR BEAM BOEING727 7272Q9 138448MNM BS 1130 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FLOOR BEAM UPPER FLANGE CORRODED BS 1130 LBL 24. CORROSION CLEANED, FOUND OUT OF LIMITS, REPAIRED AS PER SRM 51-40-4 1 INCH BY 1 INCH BY 12 INCH 7075-T6 .125. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407003581995040700358NM 1995 4 7 95ZZZW356 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM BS 350 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, RT CHORD ANGLE BULGING AT STATION 350 NOSE W/W AREA. REMOVED CHORD ANGLE AND CLEAN AREA PER SRM 51-50-1, TREATED AREA PER SRM 51-10-2, INSTALLED CHORD ANGLE PER SRM 51-10-1. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407003591995040700359NM 1995 4 7 95ZZZW357 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 328 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, LOWER NOSE COMP STATION 328 STRINGER 22R CORROSION AND CRACK ON STRINGER. CUT DAMAGE AREA AND REPAIRED WITH SPLICE REPAIR AS PER SRM 53-10-3. REPLACED 14.5 INCHES OF STRINGER WITH TWO SPLICES OF 10 INCHES EACH. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407003601995040700360NM 1995 4 7 95ZZZW358 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 480 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON FORWARD SIDE OF FRAME BS 480 BETWEEN STRINGER 28L AND 29L. REMOVED CORROSION PER SRM 51-10-06, OUT OF LIMITS. REMOVED DAMAGE AREA AS PER SRM 51-40-3. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 INCH BY 1 INCH BY 6 INCHES 2024-T3 .050. ALODINED AND PRIMED PER SRM 51-10-2. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003611995040700361NM 1995 4 7 95ZZZW359 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 950 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON DOOR CUTOUT SUPPORT JUST AFT OF BS 950E BETWEEN STRINGER 30 AND 27R. REMOVED FASTENERS FOR ACCESS, REMOVED CORROSION AS PER SRM 51-10-6, BEYOND LIMITS, CUT OUT DAMAGE AREA AS PER SRM 53-10-4 AND INSTALLED REPAIR 3 INCH BY 5 INCH AS PER SRM 51-10-4. INSTALLED FASTENERS AS PER SRM 51-30-2. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003621995040700362NM 1995 4 7 95ZZZW360 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 970 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION FOUND ON FORWARD SIDE OF FRAME AND LOWER FLANGE FROM STRINGER 27L TO STRINGER 28R BS 970. REMOVED FASTENERS FROM STRINGER 27L TO STRINGER 28R BS 970 PER SRM 51-30-2. REMOVED CORROSION AS PER SRM 51-10-6, OUT OF LIMITS, CLIP FROM STRINGER 27R TO STRINGER 28R, TREATED AND PRIMED AS PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 51-40-3, INSTALLED FRAME LOWER FLANGE PER SRM 51-30-2. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003631995040700363NM 1995 4 7 95ZZZW361 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 990 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON FRAME BS 990 LOWER FLANGE AND AFT SIDE SHEER CLIPS. ALSO, STRINGERS BETWEEN 30 AND 28L. INSTALLED BETWEEN STRINGER 28L AND 30L ANGLE REPAIR AS PER SRM 51-40-3 2024-T3 .071 7.5 INCHES BY 3.5 INCHES. REPLACED CLIPS PER SRM 51-30-2. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003641995040700364NM 1995 4 7 95ZZZW362 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 1030/1050 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING D-CHECK, CORROSION ON STRINGER 30 BETWEEN BS 1030 AND BS 1050, ALSO SKIN SURFACE ADJACENT TO STRINGER. REMOVED FASTENERS PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED PER SRM 51-10-2. REPLACED PARTS (FAB) PER SRM 51-10-1, SEALED AREA PER SRM 51-20-4, INSTALLED FASTENERS AND PARTS PER SRM 51-30-2, MATERIAL 2.5 INCHES BY 9 INCHES 2024-T3 .063. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003651995040700365NM 1995 4 7 95ZZZW363 119950220A5320 BEAM BOEING727 7272Q9 138448MNM BS 294-328 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURNG D-CHECK, NOSE COMP RT HORIZONTAL WALKWAY BEAM CHORD HAS CORROSION STATION 294-328 RT. CLEANED CORROSION PER SRM 51-10-6. FOUND OUT OF LIMITS STATION 294 TO 299. FABRICATED REPAIR PARTS PER SRM 51-40-4, .125 INCH BY 9 INCH BY 4 INCH, 7075-T6, TREATED WITH ALODINE AND PRIMED PER SRM 51-10-2. REPAIR PER SRM 51-10-4. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003661995040700366NM 1995 4 7 95ZZZW364 119950220A5320 INTERCOSTAL BOEING727 7272Q9 138448MNM BS 1030-1050 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, AFT CARGO RT STATION 1030-1050 STRINGER 25R INTERCOSTAL IS BENT AND CRACKED. STOP DRILLED CRACK AS PER SRM 51-10-1, INSTALLED DOUBLER AS PER SRM 51-40-2 2024-T3 .050 4.5 INCH BY 5.5 INCH. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003671995040700367NM 1995 4 7 95ZZZW365 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 1175 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, AFT CARGO STATION 1175 STRINGER 22L, CORROSION ON STRINGER. REMOVED FASTENERS, REMOVED STRINGER, REMOVED CORROSION. ALODINE AND PRIMED AND INSTALLED STRINGER NEW 30.5 INCH, INSTALLED FASTENERS, PER SRM 51-30-2, 53-10-1, 51-10-6, 51-10-2, 53-10-3 AND 51-30-2. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003681995040700368NM 1995 4 7 95ZZZW366 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 1183 CORROSION A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, VERTICAL SUPPORT BEAM FORWARD OF BS 1183 CORROSION STRESS CRACK AT BOTTOM ATTACHMENT LUG JUST INBOARD OF STRINGER 26L. REPAIR INSTALLED PER SRM 727-53-0181 AND DRAWING NR 65C33724. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003691995040700369NM 1995 4 7 95ZZZW367 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 1166 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION FRAME LOWER FLANGE BS 1166 BETWEEN STRINGER 29L AND 27L. REMOVED CORROSION FOUND OUT OF LIMITS, REMOVED CLIP AND INSTALLED NEW CLIP AS PER SRM 51-10-1 PART 4. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003701995040700370NM 1995 4 7 95ZZZW368 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM BS 620 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO DOOR CUT OUT, AFT BOTTOM CORNER 'L' ANGLE HAS CORROSION, LOCATED JUST ABOVE TIE DOWN STATION 620 STRINGER 26R. FABRICATED NEW 'L' ANGLE PER SRM 51-10-5 .063 2024-T3 2 INCH BY 1 INCH BY 2 INCH. TREATED AND PRIMED PER SRM 51-10-2 AND INSTALLED PER SRM 51-40-3. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003711995040700371NM 1995 4 7 95ZZZW369 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM BS 590 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO DOOR CUT OUT STATION 590 STRINGER 26 RT SUPPORT AND 'L' ANGLE ARE BENT. DAMAGED ANGLES REMOVED PER SRM 51-10-1, FABRICATED ANGLES PER SRM 51-40-4, TREATED AND PRIMED PER SRM 51-10-2, INSTALLED ANGLES PER SRM 51-10-1 4 INCHES BY 4 INCHES 2024-T3. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003721995040700372NM 1995 4 7 95ZZZW370 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 360 MATERIAL LOSS A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, 10 PERCENT SKIN LOSS NOTED BS 360 RT AFT ROW OF FASTENERS BETWEEN STRINGER 4 AND STRINGER 5. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER REPAIR PER SRM 43-30-3. DOUBLER SIZE 7 INCHES BY 15 INCHES 2024-T3 .071. TOTAL CYCLES 29,235. (W) 2L73 4F RTA3WE 19950407003731995040700373NM 1995 4 7 AWXA9500137 119950312A3230BACR13CG2A RELAY BOEING737 737275 1384485NM L/G MODULE INOP A AWXAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 20958 PHX - FLT 445 - AFTER TAKEOFF AND DURING CLIMB, THE LANDING GEAR CONTROL LEVER WOULD NOT RAISE PAST THE OFF DETENT TO RETRACT THE GEAR. CREW MADE NO ATTEMPT TO OVERRIDE THE LOCKOUT AND ELECTED TO RETURN TO PHOENIX. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE K3 RELAY, OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950407003741995040700374NM 1995 4 7 AWXA9500139 119950314A2130 PRESSURIZATION BOEING737 737277 1384570NM CABIN MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28185AW 22652 IAH - FLT 887 - AIR TURNBACK, IAH TO PHX, AFTER TAKEOFF, CREW REPORTED THAT THEY WERE UNABLE TO PRESSURIZE THE AIRCRAFT IN ANY MODE. BOTH OUTFLOW VALVES SHOWED FULL CLOSED AND THE PNEUMATIC DUCT PRESSURE WAS NORMAL. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT DOOR SEAL AND FOUND NO DEFECTS. PRESSURIZED THE AIRCRAFT WITH FIRST THE APU, THEN THE ENGINES. OPERATIONAL CHECKS WERE NORMAL. AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER PROBLEMS. INBOUND CREW REPORTED NO FAULTS AND THE AIRCRAFT REMAINS IN SERVICE. (W) 2L72 4F RTA16WE 19950407003751995040700375NM 1995 4 7 AWXA9500142 119950303A5330 SKIN BOEING737 737297 1384480NM FS 525 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING LANDING LIGHT REPLACEMENT, FOUND A 3.5 INCH CRACK IN FUSELAGE SKIN AT STATION 525 STRINGER 16L. REPAIRED CRACK IAW SRM 53-30-3, FIGURE 6. (W) 2L72 4F A16WE 19950407003761995040700376NM 1995 4 7 AWXA9500143 119950303A5313 STRINGER BOEING737 737297 1384480NM FS 520 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING REPAIR OF FUSELAGE SKIN CRACK, STRINGER 16L FOUND CRACKED APPROXIMATELY .5 INCH AT AFT END OF WING SCAN LIGHT ASSEMBLY, APPROXIMATELY STATION 520. REPAIRED IAW SRM 53-10-3, DETAIL VI. (W) 2L72 4F A16WE 19950407003771995040700377NM 1995 4 7 AWXA9500144 119950303A5313 STRINGER BOEING737 737297 1384480NM FS 510 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING REPAIR OF FUSELAGE SKIN CRACK, STRINGER 16L FOUND CRACKED APPROXIMATELY .5 INCHES AT FWD END OF WING SCAN LIGHT ASSEMBLY, APPROXIMATELY STATION 510. REPAIRED IAW SRM 53-10-3, DETAIL VI. (W) 2L72 4F A16WE 19950407003781995040700378NM 1995 4 7 AWXA9500145 119950320A2910MS2878225 O-RING BOEING737 7373G7 1384595NM LT WHEEL WELL DAMAGED A AWXAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP28305AW 24012 FLT 510 - PHX-OMA - DURING CRUISE, AIRCRAFT LOST 'A' SYSTEM HYDRAULICS. AIRCRAFT CONTINUED TO OMA AND LANDED WITHOUT FURTHER PROBLEMS. CONTRACT MAINTENANCE FOUND O-RINGS SEAL LEAKING AT LT WHEEL WELL HYDRAULIC PRESSURE MODULE. MAINTENANCE REPLACED O-RING, LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003791995040700379NM 1995 4 7 AWXA9500146 119950320A3040 GROMMETS BOEING737 7373G7 1384595NM LT WINDSHIELD DAMAGED A AWXAO OTHER A FLAME/FIRE CRCRUISE 1 WP28158AW 23780 FLT 720 - LAS-ABQ - ENROUTE TO ABQ, CAPTAINS WINDOW WAS ARCING AND IGNITED RUBBER GROMMET, CAUSING FIRE AND SMOKE IN COCKPIT. FIRE WAS EXTINGUISHED, AND AIRCRAFT LANDED UNEVENTFULLY IN ABQ. CONTRACT MAINTENANCE FOUND THE CAPTAINS WINDOW THAT WAS ARCING, IN TURN CAUGHT ONE OF THE RUBBER GROMMETS ON FIRE. NO FURTHER DAMAGE WAS NOTED. WINDOW HEAT PLACED ON MEL 30-11. AN UMSR WAS ISSUED AND AIRCRAFT RETURNED TO SERVICE. FURTHER MAINTENANCE ACTION REPLACED TWO SILICONE GROMMETS. WINDSHIELD HEAT OPS CHECK OK PER BMM AN AWA TASK CARD R1B56001 MEL CLEARED, AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003801995040700380NM 1995 4 7 AWXA9500147 119950315A2761654485114MR27696ACTUATOR BOEING737 7372M8 1384483NM NR 4 SPOILER CRACKED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28141AW 2735 21955 STATION DEN - FLT 125 - LAS-OMA - CREW REPROTED THE 'A' HYDRAULIC SYSTEM QUANTITY WAS LOW IN FLIGHT. AIRCRAFT DIVERTED TO DEN, LANDING WITHOUT FURTHER PROBLEMS. CONTRACT MX FOUND THE NR 4 GROUND SPOILER ACTUATOR HOUSING CRACKED AND LEAKING. MAINTENANCE REMOVED AND REPLACED SPOILER ACTUATOR PER BMM 27-62-0. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950407003811995040700381NM 1995 4 7 AWXA9500148 119950318A27505702224 JACKSCREW BOEING737 7373G7 1384595NM NR 2 TE FLAP CORRODED A AAWXAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 WP28308AW 603 24710 STATION ORD - FLT 692 - LAS-MDW - FLAPS LOCKED AT 15 DEGREES, CREW UNABLE TO OBTAIN FLAP SELECTION GREATER THAN 15 DEGREES. FLAPS WERE RECYCLED WITH NO CHANGE. CIRCUIT BREAKERS CHECKED AND FOUND OK. AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT FURTHER PROBLEMS. AIRCRAFT WAS INSPECTED AND FOUND AIRWORTHY FOR FERRY FLIGHT TO CMH. CMH MAINTENANCE FOUND NR 2 JACKSCREW ASSEMBLY BAD. REMOVED AND REPLACED NR 2 JACKSCREW ASSEMBLY PER BMM 27-51-73, OPS CHECK GOOD. PERFORMED REQUIRED INSPECTION AND FOUND SYSTEM TO OPERATE NORMALLY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003821995040700382NM 1995 4 7 AWXA9500154 119950321A5330 SKIN BOEING737 73733A 1384673NM AFT FUS DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28169AW 23630 PHX - FLT 1530 - DURING OVERNIGHT INSPECTION, FOUND A LARGE DENT IN LOWER SKIN JUST BEHIND AFT CARGO PIT DOOR. AREA WAS INSPECTED AND DAMAGE FOUND LIMITED TO CRACKED SHEAR TIE, FRAME 807 BL 0. FASTENERS WERE REMOVED AND SKIN RETURNED TO NORMAL CONTOUR. MX REPAIRED CRACKED SHEAR TIE PER SRM 53-00-7, FIGURE 203. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003831995040700383NM 1995 4 7 AWXA9500164 119950320A21501828202 HEAT EXCHANGER BOEING737 737275 1384485NM LEFT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 535616 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND LT PRIMARY HEAT EXCHANGER CRACKED AT WELD IN AFT LOWER INBOARD CORNER. REMOVED AND REPLACED HEAT EXCHANGER PER AWA TASK CARD R2C21004. LEAK CHECK COMPLIED WITH. (W) 2L72 4F A16WE 19950407003841995040700384NM 1995 4 7 AWXA9500171 119950323A2910 FLUID BOEING737 7372Q8 138448KNM HYD SYST LEAKING A AWXAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP28137AW 23148 SLC - FLT 2808 - PHX-SLC - CREW DECLARED AN EMERGENCY DUE TO LOSS OF HYDRAULIC FLUID. 125 MILES FROM SLC THE HYDRAULIC FLUID QUANTITY DROPPED. AIRCRAFT LANDED WITHOUT INCIDENT. AFTER LANDING, THE INDICATOR CAME UP TO THE REFILL MARK ON GAUGE. CONTRACT MAINTENANCE AND FLIGHT CREW PERFORMED WALKAROUND AND WERE UNABLE TO LOCATE ANY SIGNS OF LEAK. MX ADDED SIX QUARTS TO SYSTEM. AIRCRAFT RELEASED FOR CONTINUATION TO MAINTENANCE BASE. (W) 2L72 4F RTA16WE 19950407003851995040700385NM 1995 4 7 AWXA9500172 119950320A3350 EEL CONNECTORS BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGNCY EXIT LIGHTS INOPERATIVE FROM MID CABIN TO AFT GALLEY. RESEATED CONNECTORS AT ROWS 13 AND 19, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950407003861995040700386NM 1995 4 7 AWXA9500173 119950321A335058783 EEL HARNESS BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS IN FORWARD CABIN INOPERATIVE. REMOVED AND REPLACED LIGHT HARNESS ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F A16WE 19950407003871995040700387NM 1995 4 7 AWXA9500175 119950324A274210620332 ACTUATOR BOEING737 73733A 1384673NM STAB TRIM MALFUNCTIONED A AAWXAK NONE O OTHER LDLANDING 1 WP28168AW 23629 LAS - FLT 043 - UPON LANDING ROLL OUT, THE STABILIZER TRIMMED FORWARD AND BACKWARD WITH NO INPUT. MAINTENANCE REMOVED AND REPLACED STABILIZER TRIM ACTUATOR PER AWA TASK CARD R6C27001. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003881995040700388NM 1995 4 7 AWXA9500176 119950324A2820 FUEL SYSTEM BOEING737 7373G7 1384595NM CTR TANK MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28304AW 24011 PHX - FLT 2172 - LAS-IAH - DURING CRUISE, THE CENTER FUEL TANK SEEMED TO CONSUME FUEL AT AN EXCESSIVE RATE, 3600 LBS TO LESS THAN 900 LBS IN APPROXIMATELY 20 MINUTES. DUE TO A POSSIBLE FUEL LEAK, CREW DIVERTED AIRCRAFT TO PHX AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE INSPECTED FUEL QUANTITY SYSTEM AND CHECKED FOR LEAKS ON CENTER TANK AND VENTS. NO DEFECTS WERE NOTED. COMPLIED WITH OVERWEIGHT INSPECTION. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950407003891995040700389NM 1995 4 7 AWXA9500177 119950325A335020131A EEL BATTERY PACK BOEING737 73733A 1384673NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LGHTS INOPERATIVE, ROWS 11 THROUGH 14. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY AT STATION 629R, OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950407003901995040700390NM 1995 4 7 AWXA9500178 119950327A53206547951 SCUFF PLATE BOEING737 737277 1384570NM CARGO COMPT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FORWARD CARGO DOORWAY THRESHOLD CRACKED IN TWO PLACES. REMOVED AND WELDED REPAIR PER ER 1-53-30-02D AND INSTALLED THRESHOLD. (W) 2L72 4F RTA16WE 19950407003911995040700391NM 1995 4 7 AWXA9500179 119950327A5320 SPLICE BOEING737 737277 1384570NM FS 907 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURING SCHEDULED C11 INSPECTION, FOUND STRINGER SPLICE AT FS 907 STRINGER 28R CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW STRINGER SPLICE PER SRM 51-32-2 AND SRM 51-10-1. (W) 2L72 4F RTA16WE 19950407003921995040700392NM 1995 4 7 AWXA9500180 119950327A5330 SKIN BOEING737 737277 1384570NM FS 960 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT FORWARD LOWER CORNER OF AFT ENTRY DOOR CUTOUT. REPAIRED DAMAGE WITH DOUBLER REPAIR PER SRM 53-30-3. (W) 2L72 4F RTA16WE 19950407003931995040700393NM 1995 4 7 AWXA9500181 119950327A5330 SKIN BOEING737 737277 1384570NM FS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED DAMAGE WITH DOUBLER REPAIR PER SRM 53-30-3. (W) 2L72 4F RTA16WE 19950407003941995040700394NM 1995 4 7 AWXA9500182 119950327A5320 THRESHOLD BOEING737 737277 1384570NM FS 947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURING SCHEDULED C11 INSPECTION, FOUND R2 DOOR THRESHOLD CHORD CORRODED FROM FS 947 TO FS 1006. REMOVED, FABRICATED AND INSTALLED NEW CHORD ANGLE PER SRM 51-10-1. (W) 2L72 4F RTA16WE 19950407003951995040700395NM 1995 4 7 AWXA9500183 119950327A5320 INTERCOSTAL BOEING737 737277 1384570NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 PHX - DURING SCHEDULED C11 INSPECTION, FOUND CORROSION ON NUT PLATE CLIP OF INTERCOSTAL BETWEEN FS 967 AND FS 986.5 RBL 18. REMOVED DAMAGED PARTS, FABRICATED SHIM AND REINSTALLED ON INTERCOSTAL PER SRM 51-10-1. (W) 2L72 4F RTA16WE 19950407003961995040700396NM 1995 4 7 AWXA9500184 119950327A5315 FLOOR BEAM BOEING737 737277 1384570NM FS 947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURNIG SCHEDULED C11 INSPECTION, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR BEAM AT FS 947, RBL 32 TO RBL 49. REMOVED DAMAGE AND INSTALLED ANGLE REPAIR PER SRM 53-10-1 AND SRM 51-40-4. (W) 2L72 4F RTA16WE 19950407003971995040700397NM 1995 4 7 AWXA9500185 119950327A5315 FLOOR BEAM BOEING737 737277 1384570NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 PHX - DURING SCHEDULED C11 INSPECTION, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR BEAM AT FS 967 RBL 12 TO RBL 24. REMOVED DAMAGED AND REPAIRED WITH TOP CAP SPLICE PER SRM 53-10-9. (W) 2L72 4F RTA16WE 19950407003981995040700398NM 1995 4 7 AWXA9500186 119950327A5320 INTERCOSTAL BOEING737 737277 1384570NM FS 1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28183AW 22650 DURING SCHEDULED C11 INSPECTION, FOUND LAV THRESHOLD SUPPORT INTERCOSTAL CORRODED FROM FS 1006 TO FS 1016 LBL 22. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-1. (W) 2L72 4F RTA16WE 19950407003991995040700399NM 1995 4 7 TWRA9514 119950307A5210 MAIN ENTRY DOOR BOEING747 747136 1384883NM CABIN JAMMED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15606FF 20273 DURING PREFLIGHT, 5R MAIN ENTRY DOOR WOULD NOT GO INTO AUTO. RECYCLED 5R MED, OPS CHECK OK. (W) 2L74 4F A20WE 19950407004001995040700400NE 1995 4 7 TWRA9516 219950312A7200 ENGINE BOEING747 747121 1384871NM PWA JT9 JT9D7AH 52054NE NR 2 MALFUNCTIONED A TWRACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA15604FF 19659 685870 ABORTED TAKEOFF DUE TO NR 2 ENGINE EXPERIENCED A DROP IN EPR AND N1 ALONG WITH A INCREASE IN EGT. FOLLOWING TROUBLESHOOTING, MAINTENANCE ELECTED TO FERRY AIRCRAFT TO JFK FOR REPAIR. (W) 2L74 4F4 F A20WE E20EA 19950407004011995040700401NM 1995 4 7 TWRA9517 119950319A33501317 EEL BULB BOEING747 747121 1384871NM CABIN FAILED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15609FF 20354 ON DAILY CHECK, FOUND LEFT SIDE C-ZONE NR 1 CEILING (EMERGENCY LIGHT) INOPERABLE. REPLACED LIGHT BULB, OPS CHECK OK. (W) 2L74 4F A20WE 19950407004021995040700402NM 1995 4 7 9505186615 119950327A5720 STIFFENER BOEING747 747251B 1384892NM LBL 86 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01632US 20360 DURING PERIODIC CHECK, THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL 86 WAS FOUND CORRODED. DISCREPANT STIFFENER P/N 65B10671-1 IS MADE FROM BAC 1517-1672 EXTRUSION AND MATERIAL IS 7178-T6511 ALUMINUM. MADE REPAIR PER EA 66-97876. 2L74 4F A20WE 19950407004031995040700403WP 1995 4 7 9505191152 119950323A5330AEA70791 SKIN DOUG DC10 DC1040 3023508WP FS 1509-1531 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01152US 46761 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AND BULKHEAD AFT OF CENTER LANDING GEAR AT FS 1509 - 1531, LONGERONS 50L AND 50R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97918. 2L73 4F A22WE 19950407004051995040700405NM 1995 4 7 9505212202 119950401A3260 SWITCH BOEING727 727251 138408HNM LT MLG DOOR OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01202US 22155 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, LEFT MAIN GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED GEAR WITH PROPER INDICATIONS. MAINTENANCE ADJUSTED RIGHT MAIN LANDING GEAR DOOR INDICATION SWITCH. GEAR SWING OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950407004061995040700406NM 1995 4 7 9505222712 119950401A3260 INDICATION BOEING727 7272S7 138407ZNM RT MLG DOOR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01712RC 22020 DURING DEPARTURE CLIMB UPON PLACING GEAR HANDLE IN 'OFF' POSITION, RIGHT MAIN LANDING GEAR DOOR WARNING INDICATION ILLUMINATED. RECYCLED GEAR HANDLE TO 'UP' AND THEN 'OFF' POSITION TO NO AVAIL. RECYCLED LANDING GEAR WITH PROPER INDICATIONS. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION. 2L73 4F A3WE 19950407004071995040700407NM 1995 4 7 9505232706 119950330A5320651751737 TORQUE BOX BOEING727 727225 1384077NM FS 1253-1283 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01815EA 22552 DURING PERIODIC CHECK, MAINTENANCE FOUND VENTRAL STAIRWELL TORQUE BOX RIGHT SIDE FS 1253 - 1283 CRACKED. REPAIRED PER NWA EA 27-096512. 2L73 4F A3WE 19950407004081995040700408NM 1995 4 7 95UAL737024 119950308A2133106200815 REGULATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 INOP A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29398UA 24673 ON TAKE OFF WITH LEFT PACK INOP, RIGHT PACK WOULD NOT MAINTAIN PRESSURIZATION. CABIN CLIMBED AT 2000 FEET PER MINUTE, REVERTED TO STANDBY MODE. STANDBY MODE WAS NO HELP, TURNED ON APU AND CABIN STILL CLIMBED. REPLACED NUMBER TWO HIGH STAGE REGULATOR. RAN ENGINE, CHECKED OK. 2L72 4F4 FRTA16WE E2GL 19950407004091995040700409WP 1995 4 7 ABXA9500264 119950316A57133911238508 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN RIGHT WING STRINGER NR 20. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004101995040700410WP 1995 4 7 ABXA9500265 119950316A57133911238502 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 23R. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01. 2L72 4F A6WE 19950407004111995040700411WP 1995 4 7 ABXA9500266 119950316A57133911238502 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 23R. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004121995040700412WP 1995 4 7 ABXA9500267 119950315A572099193692 CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, INSIDE BARREL NUT HOLES IN STRINGERS NR 12, 13, 14, 15, 16, 17, 18, 19 AND 21. BLENDED IAW DC-9 SRM 51-10-3 AND SB 57-98. 2L72 4F A6WE 19950407004131995040700413WP 1995 4 7 ABXA9500268 119950320A572099193692 CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 22-23. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407004141995040700414WP 1995 4 7 ABXA9500269 119950316A57133911238508 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING ON TOP OF STRINGER NR 20. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01. 2L72 4F A6WE 19950407004151995040700415WP 1995 4 7 ABXA9500270 119950316A57133911238512 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 18, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004161995040700416WP 1995 4 7 ABXA9500271 119950316A57133911240504 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004171995040700417WP 1995 4 7 ABXA9500272 119950316A57133911240504 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01. 2L72 4F A6WE 19950407004181995040700418WP 1995 4 7 ABXA9500273 119950316A57133911238514 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004191995040700419WP 1995 4 7 ABXA9500274 119950316A57133911238514 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01. 2L72 4F A6WE 19950407004201995040700420WP 1995 4 7 ABXA9500275 119950316A57133911236502 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 15, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004211995040700421WP 1995 4 7 ABXA9500276 119950316A57133911236504 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 14, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004221995040700422WP 1995 4 7 ABXA9500277 119950316A57133911236504 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004231995040700423WP 1995 4 7 ABXA9500278 119950316A57133911236504 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 51-00-1 AND 57-01. 2L72 4F A6WE 19950407004241995040700424WP 1995 4 7 ABXA9500279 119950316A571339112362 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004251995040700425WP 1995 4 7 ABXA9500280 119950316A571339112362 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01. 2L72 4F A6WE 19950407004261995040700426WP 1995 4 7 ABXA9500281 119950316A57133911238516 STRINGER DOUG DC9 DC932 3022066WP WS 58 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 11, RIGHT WING. BLENDED IAW DC-9 SRM 57-01. 2L72 4F A6WE 19950407004271995040700427WP 1995 4 7 ABXA9500282 119950316A57133911238516 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 11, RIGHT WING. BLENDED CORROSION IAW DC-9 SRM 51-22-1 AND 57-01. 2L72 4F A6WE 19950407004281995040700428WP 1995 4 7 ABXA9500283 119950315A572099193691 CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP HORIZONTAL FLANGE INSIDE BARREL NUT HOLES IN STRINGERS 11, 14, 16, 18, 20 AND 21. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407004291995040700429WP 1995 4 7 ABXA9500284 119950315A57133911238503 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 22, LOWER FORWARD LEG. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407004301995040700430WP 1995 4 7 ABXA9500285 119950316A572099193692 CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, BETWEEN STRINGERS 11-12. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407004311995040700431WP 1995 4 7 ABXA9500286 119950317A572099193692 CAP DOUG DC9 DC932 3022066WP WS 58 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND RIGHT WING LOWER T-CAP CRACKED IN THE RADIUS JUST AFT OF STRINGER NR 16. BLENDED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950407004321995040700432WP 1995 4 7 ABXA9500287 119950316A572099193692 CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, AFT OF STRINGER NR 11. BLENDED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950407004331995040700433WP 1995 4 7 ABXA9500301 119950403A326056487405501 UPLATCH ASSY DOUG DC8 DC863 302198AWP LT MLG LACK OF LUBE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23812AX 46126 UPON CLIMBOUT OF SJC, UNSAFE GEAR LIGHT ILLUMINATED DURING UPLATCH CHECK. LEFT LANDING GEAR NOT LATCHED WAS INDICATED. RECYCLED GEAR 3 TIMES, SAME RESULT. PERFORMED ALTERNATE UPLATCH CHECK AND ALL GEAR AND DOOR INDICATIONS SHOWED LATCHED. LUBED LEFT GEAR UPLATCH ASSY. SWUNG GEAR AND OPS CHECKED GOOD IAW DC 8 MM CHAPTER 32. 2L74 4F 4A25 19950407004341995040700434WP 1995 4 7 ABXA9500302 119950404A57535751152 LINK DOUG DC8 DC861 3021952WP RT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23843AX 46017 DURING COMPLIANCE OF A.D. 88-10-07, S.B. 27-246, A.S.B. 27-269 HAD CRACK INDICATION AT POINT J INBOARD SIDE RIGHT HAND FLAP LINK. REPLACED LINK IAW DC8 MM 27-51-4. 2L74 4F 4A25 19950407004351995040700435SO 1995 4 7 COM11844 119950401A3397 WIRE EMB 120 EMB120RT SO LT WING TIP DAMAGED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01156CA14028 120156 NAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. REPAIRED CHAFED WIRE IN LT WING TIP. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950407004361995040700436SO 1995 4 7 COM11845 119950331A27315299 TRIM ACTUATOR EMB 120 EMB120RT SO RT ELEV BINDING A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01255CA9769 120238 ELEVATOR TRIM IS BINDING. REPLACED THE RT ELEVATOR TRIM ACTUATOR. 2L72 4T RTA31SO 19950407004371995040700437SO 1995 4 7 COM11846 119950330A575312025206004 RIB EMB 120 EMB120RT SO RT TE FLAP CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01152CA14130 120152 DURING INSPECTION, FOUND RIGHT OUTBOARD FLAP END RIB TO HAVE A SMALL PART OF UPPER FRAME OF END RIB TO BE MISSING. REMOVE END RIB AND MANUFACTURED NEW END RIB OUT OF .040 202V. INSTALLED WITH CR 3212-4 FASTENERS. ALL WORK DONE IAW AERODESIGN REPORT NR 1490-1 DATED 3-30-95. 2L72 4T RTA31SO 19950407004381995040700438EU 1995 4 7 COM31054 119950403A7603 POWER LEVER SAAB SF340 SF340A 7850100EU RIGHT OUT OF ADJUST A COMAK NONE O OTHER ININSP/MAINT 1 SO01340SF 340A014 WHEN RT POWER LEVER IS ADVANCED ABOVE FLIGHT IDLE, ENGINE OVERSPEEDS. ADJUSTED POWER LEVER CONTROLS AIRFRAME RIGGING TO M/N SPECS. SYSTEM OPERATES NORMAL. 2L72 4T RTA52EU 19950407004391995040700439EU 1995 4 7 COM31055 119950401A3230J23060604146 HYD HOSE SAAB SF340 SF340A 7850100EU LT MLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01146CA 340A146 HYDRAULIC FLUID LEAK, LT NACELLE AREA. REPLACED THE LT MLG RETRACT ACTUATOR HYDRAULIC LINE. 2L72 4T RTA52EU 19950407004401995040700440EA 1995 4 7 COM60448 119950331A27604916403 SECU CNDAIRCL600 CL6002B19 EA SPOILER SYST DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01917CA63 38 7017 OUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE NR 1 AND NR 2 SECU. 2L72 4F RTA21EA 19950407004411995040700441EA 1995 4 7 COM60449 119950331A27604916403 SECU CNDAIRCL600 CL6002B19 EA SPOILER SYST DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01936CA966 53 7043 FLIGHT SPOILER CAUTION MESSAGE ON EICAS. REPLACED THE NR 1 SECU. 2L72 4F RTA21EA 19950407004421995040700442NM 1995 4 7 DL72E951287 119950327A5754 SLAT BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11283WA 21485 NUMBER 5 SLAT CRACKED AT NOSE RIBS WHERE ACT ROD END ATTACHES. FOUND DURING E-2 LETTER CHECK TPAMM 3/27/95. FOUND PREVIOUS DOUBLERS CRACKED. REPLACED SLAT ASSEMBLY. 2L73 4F A3WE 19950407004431995040700443NM 1995 4 7 DL72E951288 119950327A5522 SKIN BOEING727 727247 138408FNM LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11283WA 21485 ONE INCH CRACK IN LOWER LT ELEV SKIN AFT OF NR 4 BAL BOARD. FOUND DURING E-2 LTR CK TPAMM 3/27/95. INSTALLED DOUBLER PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950407004481995040700448NM 1995 4 7 DL72E951350 119950225A5753652163362 FLAP BOEING727 727247 138408FNM RT TE MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 14725 THE NR 4 MID FLAP, I/B AND O/B CARRIAGE SUPPORT HOUSING BOTTOM SURFACE EACH HAVE 5 BOLT HOLES CORRODED. REPAIRED PER SRM 57-50-04 REAMED AND BUSHED HOLES. ALSO, I/B HAS 2 DAMAGED SPRING ATTACH BOLT HOLES. REPAIRED PER SRM 57-50-04. REAMED AND BUSHED HOLES. FOUND AT HMV SHOP INSPECTION. 2L73 4F A3WE 19950407004491995040700449NM 1995 4 7 DL72E951351 119950225A5753652163362 FLAP BOEING727 727247 138408FNM RT TE MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 14725 THE NR 4 MID FLAP, I/B CARRIAGE THRUST BEARING RETAINER UPPER I/B AND O/B BOLT HOLES CORRODED. REPAIRED PER SRM 57-57-04, REAMED AND BUSHED HOLES. FOUND AT HMV SHOP INSPECTION. 2L73 4F A3WE 19950407004501995040700450NM 1995 4 7 DL72K951284 119950322A5754 RIB 651622196 BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11471DA BN1141 20748 DURING SHOP INSPECTION, ITEM NR 1 AND NR 2 CRACKS WERE FOUND IN RIBS OF NR 6 SLAT. REPAIRS WERE INSTALLED PER MM 57-54-0. 2L73 4F A3WE 19950407004511995040700451NM 1995 4 7 DL72K951304 119950322A5754 RIB 651622296 BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11471DA BN1141 20748 BN294 DURING SHOP INSPECTION, A RIB WAS FOUND TO BE CRACKED IN RT WING NR 6 L/E SLAT. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19950407004521995040700452NM 1995 4 7 DL72K951305 119950322A5754 RIB 651622296 BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11471DA BN1141 20748 BN294 DURING A SHOP INSPECTION, TWO RIBS WERE FOUND TO BE CRACKED. ITEM NR 1 RIB NR 16 RIB CRACKED, A REPAIR WAS INSTALLED PER SRM 57-50-3. ITEM NR 2 RIB NR 17 CRACKED. A REPAIR WAS INSTALLED PER 57-50-3. RT WING NR 6 L/E SLAT. 2L73 4F A3WE 19950407004531995040700453NM 1995 4 7 DL72K951306 119950322A5754 SKIN 651622296 BOEING727 727232 1384082NM NR 6 LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11471DA BN1141 20748 BN294 DURING A SHOP INSPECTION, A DENT IN THE LEADING EDGE WAS FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS. A REPAIR WAS INSTALLED PER SRM 57-50-3. RT WING NR 6 L/E SLAT. 2L73 4F A3WE 19950407004541995040700454NM 1995 4 7 DL72K951352 119950331A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 A .5 INCH CRACK RT SIDE OF VERT STAB BELOW PANEL 9501. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 55-30-3. 2L73 4F A3WE 19950407004551995040700455NM 1995 4 7 DL72K951353 119950331A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 A ONE INCH CRACK LT SIDE OF VERT STAB AT STR-6 APPROX FIN STA 160. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3. 2L73 4F A3WE 19950407004561995040700456NM 1995 4 7 DL72K951354 119950331A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 A .5 INCH CRACK RT SIDE OF VERT STAB BELOW AND AFT OF SADDLE PANEL 9501. FOUND AT B-1 LETTER CK. REPAIRED PER SRM 55-30-3. 2L73 4F A3WE 19950407004571995040700457NM 1995 4 7 DL72K951355 119950331A5320 WEB BOEING727 727232 1384082NM TORQ BX CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 A ONE INCH CRACK ON LIGHTENING HOLE RT SIDE OF TORQUE BOX IN 48 SEC. FOUND AT B-1 LETTER CK. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950407004581995040700458NM 1995 4 7 DL72K951356 119950331A5754 SLAT BOEING727 727232 1384082NM NR 2 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 CRACK BELOW ANTI-ICE TUBE NR 2 SLAT OPN 5535 AD. FOUND AT B-1 LETTER CHECK. REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950407004591995040700459NM 1995 4 7 DL72L951257 119950324A5754 SLAT BOEING727 727232 1384082NM NR 7 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 A .375 INCH CRACK EMANATING FROM I/B STOP PAD NR 7 SLAT. FOUND DURING C-1 LETTER CHECK, TPAMM 3-24-95. REPAIRED PER MM 57-54-0 PG 816. 2L73 4F A3WE 19950407004601995040700460NM 1995 4 7 DL72S951246 119950323A5320 WEB BOEING727 727232 1384082NM TORQUE BOX CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11535DA 22048 FOUND DURING A-2 LETTER CHECK, CRACK IN LT TORQUE BOX SKIN .5 INCH LONG AT UPPER RIVET ROW ABOVE FWD LIGHTENING HOLE. ALSO,A .125 INCH CRACK AT UPPER FWD LIGHTENING HOLE LT SIDE VERT STAIRWAY. REPAIRED PER B727 MM 53-11-0 PG 832. 2L73 4F A3WE 19950407004611995040700461NM 1995 4 7 DL72S951303 119950316A5754651622374 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 BN294 A CRACK IN NR 10 RIB LOWER AFT CORNER. REPAIRED PER MM 57-54-0. ALSO, A CRACK IN NR 11 RIB LOWER FWD CORNER. REPAIRED PER MM 57-54-0. DAMAGE FOUND AT SHOP INSPECTION, OF NR 7 SLAT. 2L73 4F A3WE 19950407004621995040700462NM 1995 4 7 DL72S951310 119950328A5754 SKIN BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11482DA 20862 FOUND DURING E-2 LETTER CHECK, BOLT SHEARED AND UPPER SKIN WEDGE CRACKD 1 INCH NR 6 SLAT I/B GUIDE HOOK. REPAIRED PER SRM 57-50-3 FIG 10. 2L73 4F A3WE 19950407004631995040700463NM 1995 4 7 DL72S951311 119950328A5522 SKIN BOEING727 727232 1384082NM LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11482DA 20862 A FIVE INCH CRACK AT LOWER SKIN OF LT ELEV SKIN O/B SIDE. FOUND DURING A-2 LTR CK, TPAMM 3/28/95. REPAIRED PER SRM 55-20-3 FIG 5. 2L73 4F A3WE 19950407004641995040700464NM 1995 4 7 DL72S951312 119950328A5754 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11482DA 20862 THE NR 4 L/E SLAT RIB CRACKED .5 INCHES O/B SIDE. FOUND DURING A-2 LTR CHECK. REPAIRED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950407004651995040700465NM 1995 4 7 DL72S951314 119950320A5754651622374 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 BN294 A CRACK IN RIB NR 13. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950407004661995040700466NM 1995 4 7 DL72S951315 119950320A5754651622374 SKIN BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 BN294 LOWER SKIN TO RIB ATTACH ANGLE CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED PER SRM 57-54-0. DURING SHOP INSPECTION, OF NR 7 L/E SLAT. 2L73 4F A3WE 19950407004671995040700467NM 1995 4 7 DL72S951319 119950222A711065196854540 NOSE COWL BOEING727 727232 1384082NM ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 BN294 DURING SHOP INSPECTION, FOUND AFT BULKHEAD TORN AND BENT AT STATION 99.25, OF NOSE COWL. REPAIRED DAMAGE PER SRM 54-10-3 FIG NR 3. 2L73 4F A3WE 19950407004681995040700468NM 1995 4 7 DL72S951322 119950322A57546516221100 ANGLE BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 BN294 DURING INITIAL INSPECTION, OF THE NR 5 LEADING EDGE SLAT, THE LOWER AFT ANGLE AT THE O/B END WAS FOUND TO HAVE A CRACK. THE CRACK WAS REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950407004691995040700469NM 1995 4 7 DL72S951326 119950328A5753652163264 SPAR BOEING727 727232 1384082NM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 BN294 THE NR 3 MID FLAP DAMAGED FROM BLOWN TIRE. AFT SPAR RAIL CRACKED IN TWO PLACES AT I/B QUADRANT CUTOUT. REPAIRED PER MM 57520 FIG 802. SPLICED IN NEW RAIL SECTION. 2L73 4F A3WE 19950407004701995040700470NM 1995 4 7 DL72S951333 119950330A5754651622285 SKIN BOEING727 727232 1384082NM LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LOWER LEADING EDGE SKIN DENTED 26 INCHES FROM INBORD END. REPAIED LEADING EDGE AS PER THE 727 SRM 57-50-3. FLUSH REPAIR FIGURE ONE. DURING SHOP INSPECTION OF SLAT PANEL. 2L73 4F A3WE 19950407004711995040700471NM 1995 4 7 DL72S951334 119950330A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 A 1.25 INCH CRACK IN VERT STAB SKIN RT SIDE AT CUTOUT FOR PANEL 9501 SADDLE PLATE. FOUND DURING E-2 LR CK. REPAIRED PER SRM 55-30-3 PAMM. 2L73 4F A3WE 19950407004721995040700472NM 1995 4 7 DL72S951335 119950330A5320 WEB BOEING727 727232 1384082NM BS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 VERT WEB CRACKED .625 INCH AT UPPER FASTENER ROW STA 1273, 48 SEC TORQUE BOX. FOUND AT E-2 LTR CK. 2L73 4F A3WE 19950407004731995040700473NM 1995 4 7 DL72S951337 119950321A5347 SEAT TRACK BOEING727 727232 1384082NM BS 360-460 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 BN294 FOUND DURING CV-2 CHECK, CORROSION AT GALLEY ATTACH TRACK BETWEEN STA 344 AND 460 RBL 44. REPLACED SEAT TRACK FROM STA 344 TO 360 AND STA 410 TO 460. FOUND WITHIN LIMITS FROM 360 TO 440 PER SRM 53-10-1. 2L73 4F A3WE 19950407004741995040700474NM 1995 4 7 DL72S951338 119950321A5347 SEAT TRACK BOEING727 727232 1384082NM BS 1090-1137 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 BN294 FOUND DURING CV-2 CHECK, CORROSION ON LT CENTER SEAT TRACK STA 1040 TO 1137. FOUND WITHIN LIMITS FROM 1190 TO 1137 PER SRM 53-10-1. REPLACED SEAT TRACK FROM 1030 TO 1090 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950407004751995040700475NM 1995 4 7 DL72S951339 119950324A5330 SKIN BOEING727 727232 1384082NM BS 580-600 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 BN294 FOUND DURING CV-2 CHECK, CORROSION ON BELLY SKIN FROM STA 580 TO 600 BETWEEN STR 8R AND O/B INTERCOSTAL. REPAIRED PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950407004761995040700476NM 1995 4 7 DL72S951357 119950322A57546516221100 SKIN BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 14725 DURING THE INITIAL INSPECTION, THE NR 5 LEADING EDGE SLAT, THE AFT HOLE ON THE OUTER SKIN WHERE THE FENCE IS MOUNTED WAS FOUND TO HAVE A .5 INCH LONG CRACK BESIDE IT. THE SKIN WAS REPAIRED PER MM 57-54-0 FIG 813. 2L73 4F A3WE 19950407004771995040700477NM 1995 4 7 DL72S951380 119950308A57546516221100 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 LOWER AFT ANGLE CRACKED 2 INCHES O/B OF O/B STOP. REPAIRED PER MM 57-54-0 FIG 812. DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2L73 4F A3WE 19950407004781995040700478NM 1995 4 7 DL72S951386 119950329A3350S106 EEL BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11418DA 21271 DURING PREFLIGHT INSP, EMERGENCY EXIT LIGHT AT AF AIRSTAIR INOP. REPLACED BATTERIES OPERATION NORMAL. 2L73 4F A3WE 19950407004791995040700479NM 1995 4 7 DL72W951299 119950325A5330 SKIN BOEING727 727247 138408FNM BS 1061 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV, FOUND FUS SKIN DENTED AT STA 1061 STR 21L. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER PER SRM 53-30-3 PG 12. 2L73 4F A3WE 19950407004801995040700480NM 1995 4 7 DL72W951300 119950310A5330 SKIN BOEING727 727247 138408FNM FS 328 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV, FOUND SKIN DAMAGED AT FS 328 RT SIDE OF NLG OPENING. REPAIRED PER ERA 301438-14. 2L73 4F A3WE 19950407004811995040700481NM 1995 4 7 DL72W951301 119950326A5754 DOUBLER BOEING727 727247 138408FNM NR 4 TE SLAT MISINSTALLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112813W 20869 AT HMV, FOUND DOUBLERS INSTALLED BACKWARDS ON UPPER T/E SKIN OF NR 4 SLAT, NOT AERODYNAMICALLY SMOOTH. INSTALLED DOUBLERS PER SRM 57-50-3 PG 27. 2L73 4F A3WE 19950407004821995040700482NM 1995 4 7 DL72W951316 119950314A5313 STRINGER BOEING727 727247 138408FNM BS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 BN294 DURING HMV, FOUND CORROSION ON STR 27L AND END FITTING AT STA 740. REPAIRED PER SRM 53-10-3 PG 3. 2L73 4F A3WE 19950407004831995040700483NM 1995 4 7 DL72W951318 119950306A5315 FLOORBEAM BOEING727 727247 138408FNM FS 360 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 BN294 DURING HMV, UPPER CAP OF CABIN FLOORBEAM FS 360 WAS FOUND CORRODED FROM LBL12 TO RBL 20. REPAIRED FLOORBEAM PER SRM 53-10-8 PG 18 FIG 3. 2L73 4F A3WE 19950407004841995040700484NM 1995 4 7 DL72W951331 119950303A5753652163361 RETAINER BOEING727 727247 138408FNM LT TE MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 BN294 THE O/B CARRIAGE THRUST BEARING RETAINER LOWER O/B HOLE CORRODED. ALSO, I/B CARRIAGE THRUST BEARING RETAINER LOWER O/B BOLT HOLE CORRODED. REPAIRED PER SRM 57-50-04 FIG 14. REAMED AND BUSHED HOLES. DURING HMV, FOR NR 1 MID FLAP. 2L73 4F A3WE 19950407004851995040700485NM 1995 4 7 DL72W951332 119950303A5753652163361 RIB BOEING727 727247 138408FNM LT TE MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 BN294 THE NR 1 MID FLAP I/B AFT RIB CRACKED. REPAIRED PER SRM 57-52-00 FIG-808. INSTALLED DOUBLER. FOUND AT HMV SHOP INSPECTION. 2L73 4F A3WE 19950407004861995040700486NM 1995 4 7 DL72W951358 119950330A5754 DOWNSTOP BOEING727 727247 138408FNM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 14725 FOUND AT HMV, NR 2 SLAT DOWNSTOP HAS CRACK WHERE DOWNSTOP CONTACTS. ADJACENT TO DOWNSTOP ON SLAT CORNER, AT UPSTOP. REPAIRED PER MM 57-54-0 PG 820 AND 821, REF NR CARD NR 1672. 2L73 4F A3WE 19950407004871995040700487NM 1995 4 7 DL72W951360 119950303A5753652163234 SPAR BOEING727 727247 138408FNM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 14725 THE NR 3 MID FLAP, LOWER AFT SPAR RAIL CRACKED 19 INCHES FROM I/B END OF FLAP. REPAIRED PER MM 57-52-00 PG 807. SPLICED IN NEW SECTION OF RAIL. DURING HMV SHOP INSPECTION. 2L73 4F A3WE 19950407004881995040700488NM 1995 4 7 DL733951249 119950322A7110 NOSE COWL BOEING737 737347 1384647NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO113301 23181 FOUND DURING LETTER CHECK, DENT INSIDE NOSE COWL, CUT OUT DAMAGED SKIN AND CORE INJECTED POTTING COMPOUND AND CURED PER SRM 54-10-01. 2L72 4F RTA16WE 19950407004891995040700489NM 1995 4 7 DL757951295 119950302A5755 SKIN 113N550140A BOEING757 757232 1384965NM LT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL DL31 22817 DURING SHOP INSPECTION, LEFT WING SPOILER PANEL WAS FOUND WITH 6 INCH CRACK ON LOWER SKIN AND A 2 INCH CRACK ON UPPER SKIN AT INBOARD END OF SPOILER. REPAIRED PER SRM 51-70-04. 2L72 4F RTA2NM 19950407004901995040700490NM 1995 4 7 DL757951298 119950302A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 INTERIOR AFT EDGE OF RADOME DELAMINATED AT 12 O'CLOCK POSTION. DAMAGE OCCURED WHILE INSTALLING RADOME IN HANGAR. REPAIRED AS PER SRM 53-10-72. REMOVED HINGES AND HINGE BRACKET, REPAIRED FIBERGLASS, INSTALLED BRACKET AND HINGES, AND PAINTED AS PER PS 900-9-1-11 NR 05. RETURNED RADOME TO A SERVICEABLE UNIT. 2L72 4F RTA2NM 19950407004911995040700491NM 1995 4 7 DL757951308 119950327A5247 DOOR BOEING757 757232 1384965NM APU CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 BN294 THE RT APU COWL DOOR SKIN CRACKED AROUND LATCH CUTOUT, LOCATED 2ND FROM THE AFT END NR 62. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER PER MM 52-48-05. 2L72 4F RTA2NM 19950407004921995040700492NM 1995 4 7 DL757951361 119950328A5313 STRINGER BOEING757 757232 1384965NM BS 540 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 AT HMV, STRINGER 23L WAS FOUND CRACKED JUST FORWARD OF THE STA 540 FRAME. THE DAMAGED PORTION WAS REMOVED AND A SPLICE FABRICATED AND INSTALLED PER SRM 53-00-03 FIG 201. 2L72 4F RTA2NM 19950407004931995040700493NM 1995 4 7 DL757951362 119950329A5315 FLOORBEAM BOEING757 757232 1384965NM BS 680 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 14725 AT HMV, THE STA 680 FLOORBEAM WAS FOUND TO BE CORRODED AROUND HOLES LBL TO RBL0. THE CORROSION WAS CLEANED AND IN LIMITS, EXCEPT BETWEEN RBL 3 THRU RBL 9. A REPAIR WAS FABRICATED FOR RBL 3 TO RBL 9 PER SRM 53-30-51 AND INSTALLED PER SAME. 2L72 4F RTA2NM 19950407004941995040700494NM 1995 4 7 DL757951363 119950330A5751 SKIN BOEING757 757232 1384965NM RT AILERON DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 14725 AT HMV, AN AREA OF DELAMINATION WAS FOUND AT LOWER I/B EDGE OF THE RT AILERON. THE AILERON WAS REPAIRED IN THE SHOP PER SRM 57-60-01. 2L72 4F RTA2NM 19950407004951995040700495NM 1995 4 7 DL76L951272 119950326A5522 SKIN 183T30018 BOEING767 767332 1382001NM RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11176DN 000355 25061 RT OUTBD ELEVATOR LOWER SKIN WAS CRACKED AND DENTED AT ELEVATOR, STA 246 AND 25 INCH AFT OF LEADING EDGE. DAMAGE WAS REPAIRED PER SRM 51-70-17. 2L72 4F RTA1NM 19950407004961995040700496WP 1995 4 7 DLL10951349 119950328A5312 BLKHD ANGLE LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO111734D 193C1225 14725 DURING LETTER CHECK, FOUND FS 1363 BULKHEAD LOWER CHORD ANGLE CRACKED BETWEEN STRINGER 18 AND STRINGER 19. REPAIRED PER SRM 53-11-00 PG 931. 2L73 4F A23WE 19950407004971995040700497WP 1995 4 7 DLL14951313 119950213A5755 SKIN 15291021788 LKHEED1011 1011385115 5265015WP RT SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO111738D HO258 193C1234 BN294 THE RT WING SPOILER PANEL WAS ROUTED TO SHOP FOR REFURBISHING. SKIN AND SPAR WERE REPLACED PER SRM 57-52-00. 2L73 4F A23WE 19950407004981995040700498WP 1995 4 7 DLL17951289 119950321A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 639 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND C1 B/B TEAR STRAP DISBONDED AT STR 34 TO 35 STA 639. CLEANED AREA, NO CORROSION FOUND. INSTALLED REPAIR PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950407004991995040700499WP 1995 4 7 DLL17951290 119950322A5315 FLOORBEAM LKHEED1011 10113853 5265020WP BS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND FLOORBEAM CORRODED FS 901 LBL 68 TO LBL 92 TASK NR C-53-100-02. REMOVED DAMAGED AREA PER SRM 53-21-00 PG 849 TO 852. DYE PENETRANT CHECKED, CUT AREA PER PS 900-6-3 NR 1. NO CRACKES FOUND ON DYE CHECK. FABRACATED NEW CAP, INSTALLED NEW T-CAP PER SRM 53-21-00 PG 849 TO 852. 2L73 4F A23WE 19950407005001995040700500WP 1995 4 7 DLL17951291 119950321A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND FLOORBEAM CORRODED, AT FS 901 RBL 65 TO 71, TASK NR C-53-100-02. TRIMMED FLOORBEAM UPPER FLANGE, INSTALLED REPAIR PER SRM 53-21-00 PG 849 TO 852. 2L73 4F A23WE 19950407005011995040700501WP 1995 4 7 DLL17951292 119950322A5320 CHANNEL LKHEED1011 10113853 5265020WP NR 4 AFT LAV CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND CHANNEL CORRODED, LOWER CHANNEL AT ENTRY TO NR 4 LAV, TASK NR C-53-100-02. REPLACED CHANNEL. 2L73 4F A23WE 19950407005021995040700502WP 1995 4 7 DLL17951293 119950322A5320 CHANNEL LKHEED1011 10113853 5265020WP NR 3 AFT LAV CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND CHANNEL CORRODED, LOWER CHANNEL AT AFT NR 3 AFT LAV TASK NR 53-100-02. INSTALLED NEW CHANNEL PER SRM 53-21-00 PG 859. 2L73 4F A23WE 19950407005031995040700503WP 1995 4 7 DLL17951294 119950323A5743 FITTING LKHEED1011 10113853 5265020WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND FITTING CORRODED, LEFT MLG UPPER HOLES AT NR 1 TO 6 ATTACH POINT FOR RETRACT ACT FITTING. REAMED HOLES TO REMOVE CORROSION. INSTALLED BUSHING, PER SRM 57-14-00. 2L73 4F A23WE 19950407005041995040700504WP 1995 4 7 DLL17951340 119950320A5753 SKIN LKHEED1011 10113853 5265020WP RT TE FLAP VANE CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 DURING HMV, CORROSION WAS FOUND ON NR 4 FLAP VANE UPPER SKIN. REMOVED CORROSION PER SRM 51-21-01 PAGE 61. 2L73 4F A23WE 19950407005051995040700505WP 1995 4 7 DLL17951342 119950322A5312 FORMER LKHEED1011 10113853 5265020WP PRESS DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 DURING HMV, FOUND P-DOME FORMER IN CENTER OF P-DOME CORRODED, AREA WHERE ATTACHES TO 1809 Z ANGLE. REMOVED CORRODED SECTION OF FORMER, FABRICATED NEW FORMER AND INSTALLED PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950407005061995040700506WP 1995 4 7 DLL17951343 119950322A5312 FORMER LKHEED1011 10113853 5265020WP PRESS DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 DURING HMV, FOUND P-DOME FORMER AFT OF STR 24 WHERE IT ATTACHES TO 1809 Z ANGLE TO BE CORRODED. REMOVED CORROSION , OUT OF LIMITS. REPAIRED AS PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950407005071995040700507WP 1995 4 7 DLL17951344 119950322A5312 CHANNEL LKHEED1011 10113853 5265020WP BS 1809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 DURING HMV, P-DOME Z CHANNEL AT STA 1809 STR 40 TO SPLICE AT STR 29 FOUND TO BE CORRODED. REMOVED Z ANGLE FROM STRINGER 22 TO 44, FABRICATED SPLICE DOUBLER AS PER SRM 53-11-00 PG 946, AND INSTALLED AS PER SRM 53-11-00 FIG 848. 2L73 4F A23WE 19950407005081995040700508WP 1995 4 7 DLL17951345 119950322A5312 CHANNEL LKHEED1011 10113853 5265020WP BS 1809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 DURING HMV, Z CHANNEL AT STA 1809 STR 24 FOUND TO BE CORRODED. REMOVED Z ANGLE FROM STR 44 TO 22, CUT AND DRILLED NEW Z ANGLE AND SPLICE DOUBLER, INSTALLED PER SRM 53-11-00 FIG 848. 2L73 4F A23WE 19950407005091995040700509WP 1995 4 7 DLL17951346 119950322A5312 FORMER LKHEED1011 10113853 5265020WP BS 1809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 BN294 P-DOME FORMER STA 1809 Z ANGLE AFT OF STR 42 CORRODED. REMOVED CORRODED SECTION OF FORMER, FABRICATED NEW FORMER SEGMENT DOUBLER AND INSTALLED PER SRM 53-11-00 FIG 809. 2L73 4F A23WE 19950407005101995040700510WP 1995 4 7 DLL17951347 119950323A5414 PANEL LKHEED1011 10113853 5265020WP NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 DURING HMV, FOUND PYLON STRUCTURE AT AFT O/B CORNER FASTENER FOR FWD PYLON PANEL 451TZ IS CRACKED. WELDED THE CRACK PER SRM 54-11-00 PG 812. 2L73 4F A23WE 19950407005111995040700511WP 1995 4 7 DLL17951348 119950323A5743 FITTING LKHEED1011 10113853 5265020WP LT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 DURING HMV, FOUND FITTING ON LT MLG DAMAGED AT LOWER HOLES 17 TO 20. REAMED HOLES TO .625 TO REMOVE DAMAGE. DID HFEC CHECK, PRIMED HOLES AND INSTALLED BUSHINGS AS PER SRM 57-11-00. 2L73 4F A23WE 19950407005121995040700512WP 1995 4 7 DLL17951368 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1765-1783 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1765 TO 1783. MFG NEW SPLICE DOUBLER, AND INSTALLED ON N/R 1391. PER SRM 53-31-00. 2L73 4F A23WE 19950407005131995040700513WP 1995 4 7 DLL17951369 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1745-1765 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND SPLICE DOUBLER CORRODED AT STA 1745 TO 1765, LT STRINGER 33. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 FIG 825 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005141995040700514WP 1995 4 7 DLL17951370 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1705-1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1705 THRU 1725. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005151995040700515WP 1995 4 7 DLL17951371 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1685-1705 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1685 THRU 1705. MFG NEW SLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005161995040700516WP 1995 4 7 DLL17951372 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1645-1665 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1645 TO 1665. MFG NEW SPLICE DOUBLER PER SRM 53-31-00, AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005171995040700517WP 1995 4 7 DLL17951373 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1625-1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED AT STA 1625 TO 1645. MFG NEW SPLICE DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005181995040700518WP 1995 4 7 DLL17951374 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1778-1792 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1778 TO 1792. MFG NEW DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005191995040700519WP 1995 4 7 DLL17951375 119950322A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1792-1801 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND INTERNAL SPLICE DOUBLER CORRODED, AT STA 1792 TO 1801. MFG NEW DOUBLER PER SRM 53-31-00 AND INSTALLED ON NR 1391. 2L73 4F A23WE 19950407005201995040700520WP 1995 4 7 DLL17951376 119950324A5400 BUSHING LKHEED1011 10113853 5265020WP NR 3 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND BUSHING WORN ON NR 3 PYLON O/B WING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00 HONED BUSHING TO 2.5005, SIZE OK. 2L73 4F A23WE 19950407005211995040700521WP 1995 4 7 DLL17951381 119950323A5330 DOUBLER LKHEED1011 10113853 5265020WP BS 1453-1625 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND CENTER STRAP CORRODED, AT C2 B/B STR NR 3, FROM FS 1453 TO FS 1625. REMOVED CENTER STRAP. MFG NEW SPLICE DOUBLER AS PER SRM 53-31-00 FIG 825. INSTALLED NEW STRAP ON NR 1391. 2L73 4F A23WE 19950407005221995040700522WP 1995 4 7 DLL17951382 119950324A5400 BUSHING LKHEED1011 10113853 5265020WP NR 3 PYLON GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 AT HMV, FOUND BEARING GOUGED, NR 3 PYLON MAIN ATTACH CENTER BEARING. REMOVED BUSHING AND CLEANED BORE. INSTALLED NEW BUSHING PER SRM 54-11-00. HONED BUSHING TO 2.5005, SIZE OK. 2L73 4F A23WE 19950407005231995040700523WP 1995 4 7 DLL17951383 119950327A5711 CAP LKHEED1011 10113853 5265020WP WS 293 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 DURING HMV, HAD TO CUT CAP AT IWS 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. CUT CAPS AS NECESSARY TO FACILITATE MAINTENANCE, TRIMMED AND DRILLED REPAIR DOUBLERS AS PER SRM 57-12-00 PG 805. INSTALLED REPAIR ANGLES PER SRM 57-12-00 PG 805. 2L73 4F A23WE 19950407005241995040700524WP 1995 4 7 DLL17951384 119950322A5313 STRINGER LKHEED1011 10113853 5265020WP BS 1625-1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 14725 DURING HMV, FOUND STRINGER 33 CORRODED BETWEEN STA 1625 AND 1645. REMOVED STRINGER SECTION, DRILLED UP NEW STRINGER SECTION AND INSTALLED STRINGER PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950407005261995040700526NM 1995 4 7 DLM88951198 119950321A5415 ANGLE DOUG MD88 MD88 3023688NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11929DL 49716 FOUND DURING LETTER CHECK, NR 2 PYLON UPPER SKIN TO FUSELAGE ATTACH ANGLE WITH A .75 INCH CRACK. REPAIRED PER SRM 54-04 A FIG 4. 2L72 4F RTA6WE 19950407005271995040700527NM 1995 4 7 DLM88951242 119950320A5330 SKIN DOUG MD88 MD88 3023688NM FS 450-655 LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11940DL 49813 AT HMV, LIGHTNING STRIKES ON UPPER FUS SKIN HAS MULTIPLE LIGHTNING STRIKES ON IT FROM FS 450, 463, 484, 530, 579, AND 655 LT SIDE AT 1000 POS AND FS 655, 674, 750 LT SIDE AT 1100 POSITION. REPAIRED DAMAGE PER SRM 53-04 FIG 38 SH 6. REMOVED DAMAGED RIVET AT FS 655, REMOVED AND INSTALLED RIVETS AT STA 655, 674, 750 AND TREATED BURNISHED AREAS. ALL WORK DONE ACCORDING TO SRM 53-04 FIG 38. 2L72 4F RTA6WE 19950407005281995040700528NM 1995 4 7 DLM88951274 119950326A5230 DOOR DOUG MD88 MD88 3023688NM MID CARGO COMPT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, MID CARGO DOOR HANDLE CUTOUT FLANGE IS WORN AND BENT. REPAIRED PER SRM 52-05 FIG 30 PG 159. 2L72 4F RTA6WE 19950407005291995040700529NM 1995 4 7 DLM88951281 119950327A5347 SEAT TRACK DOUG MD88 MD88 3023688NM BS 1089-1165 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, SEAT TRACK CORRODED INBD AND OUTBD SECTIONS JUST FWD OF AFT SERVICE DOOR. REPAIRED PER SRM 53-05 FIG 4F. 2L72 4F RTA6WE 19950407005301995040700530NM 1995 4 7 DLM88951282 119950327A7110 NOSE COWL DOUG MD88 MD88 3023688NM NR 2 ENG DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, NR 2 ENG NOSE COWL L/E DENTED AT 2 O'CLOCK POSITION. REPAIRED PER SRM 54-04 FIG 9. 2L72 4F RTA6WE 19950407005311995040700531NM 1995 4 7 DLM88951283 119950327A5347 SEAT TRACK DOUG MD88 MD88 3023688NM CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, SEAT TRACK ADJACENT TO AFT SERVICE DOOR AFT INBD SECTION CORRODED. REPAIRED PER SRM 53-05 FIG 4F. 2L72 4F RTA6WE 19950407005321995040700532NM 1995 4 7 DLM88951285 119950327A5415 ANGLE DOUG MD88 MD88 3023688NM LT PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11985DL 53312 FOUND DURING D-1 LETTER CHECK, .75 INCH CRACK UPPER AFT LT PYLON TO FUSELAGE SKIN ATTACH ANGLE. REPAIRED PER SRM 54-04A. 2L72 4F RTA6WE 19950407005331995040700533NM 1995 4 7 DLM88951309 119950328A5210 SKIN DOUG MD88 MD88 3023688NM MAIN ENTRY DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11920DL 49644 FOUND DURING A-2 LETTER CHECK, MAIN ENTRY DOOR OUTER SKIN GOUGED AT HOOK BOX CUTOUT. REPAIRED PER SRM 52-05 FIG 20A. 2L72 4F RTA6WE 19950407005341995040700534NM 1995 4 7 DLM88951317 119950329A5415 ANGLE DOUG MD88 MD88 3023688NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11900DE 53372 FOUND DURING C-2 LETTER CHECK, NR 1 ENG PYLON UPPER SKIN TO FUSELAGE SKIN ATTACH ANGLE WAS FOUND CRACKED .5 INCHES. INSTALLED REPAIR PER SRM 54-04A. 2L72 4F RTA6WE 19950407005351995040700535NM 1995 4 7 DLM88951325 119950328A2780S4913810JF17821 CONTROL CABLE DOUG MD88 MD88 3023688NM LT LE SLAT BROKEN A DALAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO11989DL 53341 LEFT 0 SLAT PARTIALLY DEPLOYED. FOUND LEFT 0 SLAT CABLE BROKEN, LEFT 0 SLAT RETRACT AND EXTEND PULLEY AND BRACKETS BROKEN. REPLACED LEFT 0 SLAT, EXTEND AND RETRACKT CABLES AND REPLACED BROKEN PULLEYS AND BRACKETS. RIGGED SLATS AS PER MM. 2L72 4F RTA6WE 19950407005361995040700536NM 1995 4 7 DLM88951341 119950331A5320 WEB DOUG MD88 MD88 3023688NM LT MLG WW DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 BN294 AT HMV, TEMPORARY REPAIR ON AFT O/B CORNER OF LT W/W. REMOVED TEMP REPAIR AND DYE CHECKED CRACK, 6.25 INCHES LONG. REMOVED VERT STIFFENER TO PICK UP 5TH HOLE FROM REPAIR ANGLE. FABR NEW REPAIR ANGLE AND SENT TO HEAT TREAT PER SRM 53-05 FIG 81A. RE-MEASURED CRACK FOUND TO BE UNDER 6 INCH IN LENGTH. INSTALLED DOUBLER. 2L72 4F RTA6WE 19950407005371995040700537WP 1995 4 7 MWEA95158 119950404A3350P4010021 EEL BATTERY DOUG DC9 DC915 3022036WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31300ME 45718 DURING ROUTINE INSPECTION, THE AFT CABIN EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950407005381995040700538NM 1995 4 7 UPS202811 119950328A534365961179 FITTING BOEING727 72751C 1384015NM NLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01903UP 18945 DURING 'C' CHECK, MAINTENANCE COMPLIED WITH UPS EO B727-5340-0167D. REPAIRED AND REPLACED DRAG BRACE FITTING NOSE LANDING GEAR (CUSTOMER REQUEST). REPLACED NOSE LANDING GEAR DRAG BRACE FITTING PER UPS EO B727-5340-0167D APPENDIX E. 2L73 4F A3WE 19950407005391995040700539NM 1995 4 7 UPS202812 119950404A5754 FLAP BOEING727 72751C 1384015NM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP JUST O/B OF THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR 727-57-1340. 2L73 4F A3WE 19950407005401995040700540NM 1995 4 7 UPS202813 119950404A553069154053 CHORD BOEING727 727180C 138406GNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, INNER UPPER CHORD, LT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950407005411995040700541NM 1995 4 7 UPS202814 119950404A553069154054 CHORD BOEING727 727180C 138406GNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, INNER UPPER CHORD, RT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950407005421995040700542NM 1995 4 7 UPS202815 119950404A553065175085 CHORD BOEING727 727180C 138406GNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, LWR OUTER CHORD, LT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950407005431995040700543NM 1995 4 7 UPS202816 119950404A553065175086 CHORD BOEING727 727180C 138406GNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON VERT STAB, LWR OUTER CHORD, RT SIDE, STA 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950407005441995040700544NM 1995 4 7 UPS202817 119950401A553165175086 RIB BOEING727 72722C 138400FNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01928UP 19091 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON RT UPPER RIB CHORD AT RBL 70.5, BS 760, FORWARD TWO FASTENER HOLES. INSTALLED REPAIR PER UPS EO B727-5710-1271F. 2L73 4F A3WE 19950407005451995040700545WP 1995 4 7 UPS802819 119950330A21215007025381 RECIRC FAN DOUG DC8 DC871F 302199DWP FLIGHT DECK FAILED A IPXAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01703UP 45939 (SUPPLEMENTAL MRR) PILOT REPORTED BURNING ELECTRICAL SMELL IN FLIGHT DECK. FLIGHT CREW DONNED OXYGEN MASK AND PERFORMED PACK SMOKE CHECK LIST. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MECHANIC INFORMED FLIGHT CREW THAT THE RECIRC FAN MOTOR WAS BURNING/SMOKING. REPLACED RECIRC FAN PER MM 21-21-0. OPS CK GOOD. 2L74 4F RT4A25 19950407005661995040700566EU 1995 4 7 9505243234 119950331A5350D53371881000 ANGLE AIRBUS320 A320211 3930320EU BELLY FAIRING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01334NW 339 DURING 'C' CHECK, THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B AND THE LEFT OVERWING SLIDE PACK WAS FOUND CRACKED. THE CRACK EMANATES FROM THE FORWARD MOST EDGE TO THE SECOND FASTENER HOLE APPROXIMATELY 4 INCHES AFT OF THE FORWARD EDGE. REPAIRED PER NWA EA 32-97835. 2L72 4F RTA28NM 19950407005671995040700567WP 1995 4 7 9505259988 119950201A5744 FITTING DOUG DC9 DC931 3022065WP NR 3 FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON RIGHT WING NR 3 FLAP HINGE FASTENER BORES. REPLACED HINGE FITTING PER MM 57-40-1. 2L72 4F A6WE 19950407005681995040700568WP 1995 4 7 9505269980 119950329A5744 FITTING DOUG DC9 DC931 3022065WP WS 154 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019344 47440 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING NR 2 FLAP HINGE FITTING WS 154. REPLACED FITTING PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950407005691995040700569WP 1995 4 7 9505279988 119950330A5311 FRAME DOUG DC9 DC931 3022065WP FS 658 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN MAIN FRAME FS 658 ABOVE LONGERON 19L. REPAIRED PER EA X9-53-75. 2L72 4F A6WE 19950407005701995040700570WP 1995 4 7 9505289990 119950330A5720 BRACKET DOUG DC9 DC931 3022065WP WS 118 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO INCH CRACK IN A PANEL ATTACH ANGLE RIGHT WING LEADING EDGE LOWER SURFACE WS 118. REPAIRED PER XEA X9-57-18. 2L72 4F A6WE 19950407005711995040700571WP 1995 4 7 9505299914 119950330A5320 SHROUD DOUG DC9 DC931 3022065WP APU CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01964N 47416 DURING PERIODIC CHECK, FOUND ONE INCH CRACK IN THE APU HOUSING SHROUD LEFT SIDE RADIUS. REPAIRED PER EA 99-097422. 2L72 4F A6WE 19950407005721995040700572WP 1995 4 7 9505309980 119950330A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019344 47440 DURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD CARGO DOOR BEAM END FITTING FORWARD END. REPLACED FITTING. 2L72 4F A6WE 19950407005731995040700573WP 1995 4 7 9505319963 119950331A5320 FITTING DOUG DC9 DC931 3022065WP FS 583 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01913RW 47171 DURING PERIODIC CHECK, FOUND CRACK IN THE LONGERON 29L END FITTING AT FS 583. REPLACED FITTING PER SRM 53-03 FIG 3. 2L72 4F A6WE 19950407005741995040700574WP 1995 4 7 9505329604 119950331A5320 FITTING DOUG DC9 DC932 3022066WP FS 937 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOOR STRAP FITTING FS 937 AT LBL 20. REPLACED FITTING. 2L72 4F A6WE 19950407005751995040700575WP 1995 4 7 9505339871 119950401A5522 SKIN DOUG DC9 DC951 3022051WP LT ELEVATOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01780NC 48102 DURING LINE CHECK, FOUND CRACK IN LEFT ELEVATOR LOWER SKIN XHS 35. REPAIRED PER EA 98-097070. 2L72 4F A6WE 19950407005761995040700576WP 1995 4 7 9505349948 119950401A5521 SPAR CAP DOUG DC9 DC931 3022065WP ELEVATOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018929E 45866 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 1.25 INCH CRACK IN THE LEFT ELEVATOR SPAR CAP STA 156 AND A .75 INCH CRACK IN THE RIGHT ELEVATOR SPAR CAP STA 74. OVERHAULED BOTH PER CMM 27-27-30. 2L72 4F A6WE 19950407005771995040700577NM 1995 4 7 9505355517 119950402A5315141N512 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 28357 23205 DURING PERIODIC CHECK, THE FS 365 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION AROUND THE NUTPLATE HOLES. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-97820. 2L72 4F RTA2NM 19950407005781995040700578 1995 4 7 95ZZZW154 419950124A3442 RADAR BOEING757 75723APF 1384966NM FWD FUS MALFUNCTIONED A CLCAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19571CA 24456 SBGR-SBEG - FLT 74 - ACFT DIVERTED TO SBPV DUE TO WEATHER AND RADAR FAILURE. PERFORMED BITE CHECK OF SYSTEM WITH NO FAULTS FOUND. RADAR SYSTEM TESTED IAW MM 34-41-00. ACFT RETURNED TO SERVICE. 2L72 4F RTA2NM 19950407005791995040700579 1995 4 7 95ZZZX1656 419950314A31407013348913 DATA ACQUISITIONHONEYWELL DORNERDO32 DO328100 2996000NM AVIONICS COMP MALFUNCTION A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07423JS 94100275 3032 FLT 4219 - DURING TAKEOFF, CREW ALERTED TO NR 1 PITOT HEAT FAIL - CAS MESSAGE, ABORTED TAKEOFF, RETURNED TO GATE. MAINTENANCE REPLACED NR 2 DATA ACQUISITION UNIT IAW MM 31-42-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407005801995040700580NM 1995 4 7 95ZZZX1657 119950309A323022831000001 ROLLER ERAM DORNERDO32 DO328100 2996000NM RT MLG CONTAMINATED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07423JS 3032 FLT 4003 - UNABLE TO EXTINGUISH 'RED' INTRANSIT LIGHT AFTER TAKEOFF WHEN GEAR WAS RETRACTED. RETURNED TO FIELD WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED ICE AND SAND CONTAMINATION IN RT MLG UPLOCK ROLLER. CLEANED AND LUBRICATED ROLLER, CONDUCTED A TEST FLIGHT, EVERYTHING OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407005811995040700581NM 1995 4 7 95ZZZX1658 119950313A2730 TRIM DORNERDO32 DO328100 2996000NM ELEVATOR OUT OF RIG A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07423JS 3032 FLT 4234 - CREW ABORTED TAKEOFF AFTER RECEIVING AN AUDIBLE TAKEOFF TRIM CONFIGURATION WARNING. AIRCRAFT RETURNED TO THE GATE, FLIGHT CREW ADJUSTED ELEVATOR TRIM. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407005821995040700582NM 1995 4 7 95ZZZX1659 119950309A323022831000001 ROLLER ERAM DORNERDO32 DO328100 2996000NM RT MLG DIRTY A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07424JS 3033 FLT 4175 - CREW SELECTED GEAR 'UP' DURING CLIMB-OUT, UNSAFE GEAR LIGHT REMAINED ILLUMINATED FOR BOTH LT AND RT MLG. CREW SELECTED GEAR DOWN AND RETURNED TO THE FIELD. PIT MAINTENANCE INSPECTED AIRCRAFT AND FOUND ICE AND SAND CONTAMINATION IN RT MLG UPLOCK ROLLER. CLEANED AND LUBRICATED ROLLER, CONDUCTED TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407005831995040700583NM 1995 4 7 95ZZZX1660 119950321A3260656021195 WARNING UNIT BOEING727 727231 1384079NM RT MLG MALFUNCTION A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE0584357 21989 STL - FLT 447 - AFTER TAKEOFF, RT MLG RED LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. CYCLED LANDING GEAR. REPLACED LANDING GEAR POSITION AND WARNING ACCESSORY UNIT MFG PN 65-60211-95. LANDING GEAR POSITION AND WARNING LIGHT SYSTEM CHECKED NORMAL. 2L73 4F A3WE 19950407005841995040700584WP 1995 4 7 95ZZZX1661 119950321A3260833703 SENSOR DOUG DC9 DC982 3022082WP NLG PROX FAILED A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05911TW 49182 BOS - FLT 184 - DURING CRUISE ONE HOUR AFTER TAKEOFF, NLG RED UNSAFE LIGHT ILLUMINATED. DURING APPROACH, RED UNSAFE LIGHT REMAINED ON. CYCLED LANDING GEAR AND LIGHT WENT OUT. FOUND NLG PROXIMITY SENSOR MFG PN 8-337-03 BAD. REPLACED NLG PROXMITY SENSOR. NOSE LANDING GEAR POSITION AND WARNING SYSTEM CHECKED NORMAL. CHECK C2D 9-14-94 MCI. 2L72 4F A6WE 19950407005851995040700585WP 1995 4 7 95ZZZX1662 119950309A2913AS664111S666 PUMP DOUG DC9 DC932 3022066WP RT ENG HYD FAILED A VJ6AO OTHER J WARNING INDICATION CRCRUISE 1 SO11930VV 47723 PHL/ATL - FLT 225 - EXPERIENCED A LOSS OF HYDRAULIC PUMP PRESSURE ON THE RIGHT ENGINE. CREW TURNED ON THE AUXILIARY HYDRAULIC PUMP AND HAD SUFFICIENT PUMP PRESSURE AND NO LOSS OF HYDRAULIC FLUID. PLACED RIGHT HYDRAULIC PUMP ON MEL 29-5. 2L72 4F A6WE 19950407005861995040700586WP 1995 4 7 95ZZZX1663 119950310A2150 PACK UNIT DOUG DC9 DC932 3022066WP LT A/C MALFUNCTION A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11924VV 47534 ATL/DFW - FLT 231 - RETURNED TO ATL DUE TO RT AND LT AIR CONDITIONING PACKS AIRFLOW WENT TO ZERO. RESET CIRCUIT BREAKER FOR GROUND COOLING FAN FOR RT AIR CONDITION PACK. ON LT AIR CONDITION PACK, FOUND DUCT TEMP INDICATOR STUCK AND PACK THERMAL TRIPPED. PACK COOLED AND RE-STARTED INBOUND TO ATL. GROUND CHECK OKAY. 2L72 4F A6WE 19950407005871995040700587NE 1995 4 7 95ZZZX1664 219950215A7532310082901 BLEED VALVE PIPER PA31T PA31T3 7103128SO PWA PT6 PT6A11 52043NE RT ENGINE DIRTY A SOCALEA ABORTED APPROACH ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS APAPPROACH 1 AL03314SC 31T8275007 PCE10408 ANC - DURING LANDING, RT ENGINE HAD AN INTERMITTENT COMPRESSOR STALL. THE LANDING WAS ABORTED DUE TO HIGH WINDS. THE PILOT SHUT DOWN RT ENGINE AND RETURNED TO ENA AND LANDED WITHOUT INCIDENT. ON INSPECTION OF THE RT ENGINE, THE BLEED VALVE WAS FOUND STUCK, WHICH CAUSED THE COMPRESSOR TO INTERMITTENTLY STALL. 1L72 3T3 T A8EA E4EA 19950407005881995040700588NM 1995 4 7 95ZZZX1665 119950224A7603250676 DRUM BOEING747 747246F NM NR 1 ENG QUAD CABLE BROKEN A SRAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO19740SJ 22477 FLT 201 - DURING TAKEOFF ROLL AT APPROX TAKEOFF KNOTS, NR 1 ENGINE HAD SUDDEN LOSS OF POWER WITH ALL PARAMETERS GOING TO ZERO (EGT, EPR, F/F) CREW REJECTED TAKEOFF AND REVERSED THRUST WAS USED. AT THIS TIME, NR 2 ENGINE HAD COMPRESSOR STALL. INSPECTED NR 1 ENGINE AND FOUND QUADRANT DRUM CONTROL CABLE IN PYLON BROKEN AT CABLE LEAD. REPLACED DRUM. 2L74 4F A20WE 19950407005891995040700589NM 1995 4 7 95ZZZX1666 119950316A3246 SPACER BOEING757 75723A 1384967NM NLG WHEEL MISSING A AMTAK NONE E VIBRATION/BUFFET TOTAKEOFF 1 GL11512AT 25493 IND - CREW REPORTS NOSE WHEEL VIBRATION ON TAKEOFF. CONTINUE FLIGHT. INSTALLED MISSING NLG WHEEL BEARING SPACER AND REMOVED RT NOSE TIRE/WHEEL ASSY PER MM 32-45-02, PRECAUTIONARY. 2L72 4F RTA2NM 19950407005901995040700590CE 1995 4 7 95ZZZX1667 119950309A2750 LIMIT SWITCHES BEECH 1900 1900C 1154161CE TE FLAPS OUT OF ADJUST A PLGAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NE05819BE UB62 LGA - FLT 4869 - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. FLAPS WERE BROUGHT UP TO ZERO AND MEL'D. UPON ARRIVAL PSM RE-RIGGED FLAP UP AND DOWN LIMIT SWITCHES. ALL CHECKS WERE SATISFACTORY. ALL WORK WAS DONE IAW BEECH MM. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA24CE 19950407005911995040700591NM 1995 4 7 95ZZZX1668 119950318A33503322037 BATTERY BOEING727 7272B7 138407LNM CABIN EEL WEAK A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11770AT 21953 ORD - ON D/S CHECK, FOUND AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS VERY DIM. REMOVED AND REPLACED BATTERY PACK. CHECKS GOOD. 2L73 4F A3WE 19950407005921995040700592NE 1995 4 7 95ZZZX1669 219950302A731470540137 FUEL PUMP BOEING747 747212B 1384886NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE FAILED A ASRAAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19745SJ 20888 HONG KONG/ANC - FLT SJM002 - DURING FLIGHT, NR 2 ENGINE EPR DROPPED DOWN TO 1.07 AT 790 DEGREES EGT, PUSHING THROTTLE UP ON NR 2 TO MATCH EPR THEN CAUSED EGT TO CLIMB UP TO 895 DEGREES CELSIUS, DIVERT AIRCRAFT TO NRT. FOUND LOW PRESSURE AT FP-12 FUEL PUMP ON NR 2 ENGINE WITH SOME METAL CONTAMINATION AT FUEL PUMP. REPLACED PUMP AND FUEL HEATER, FUEL FILTER, PERFORMED ENGINE RUN, OPS CHECKED GOOD. 2L74 4F4 F A20WE E20EA 19950407005931995040700593SW 1995 4 7 LOSA9515 119950312A291027810322684 TUBE ASSY FRCHLDSA227 SA227DC 3377521SW RT ENGINE CRACKED AS LOSAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 WP23454LA1261 DC855B HYDRAULIC LEAK RIGHT NACELLE (RESERVOIR EMPTY). REMOVED AND REPLACED RIGHT ENGINE INBOARD HIGH PRESSURE HARD LINE. NACELLE STATION 109.89. TOTAL CYCLES, 1,543. (X) 1L72 4T RTA18SW 19950407005941995040700594WP 1995 4 7 ORJA9515 119950305A3350 FLASHLIGHT DOUG DC9 DC987 3022087WP FWD EMERG INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11751RA 49779 FOUND INBD FWD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY, OPS CHECKED GOOD. (X) 2L72 4F RTA6WE 19950407005951995040700595EU 1995 4 7 SIMA950791 119950320A3610ASNA21414005 O-RING AEROSPATR72 ATR72212 EU RT BLEED LEAKING A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21420AT 420 DFW - FLT 3643 - AFTER TAKEOFF, RT BLEED LEAK LIGHT CAME ON. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REMOVED AND INSPECTED WING, BLEED LINE O-RING, GROUND RUN, NO BLEED LEAK NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950407005971995040700597EU 1995 4 7 VTZA95092 119950304A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU POD DOOR HANDLE OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27319UE 41042 IAD/CHS - FLT 6483 - AT 0800, ACFT DIVERTED TO GSO DUE TO BAGGAGE DOOR WARNING ILLUMINATED IN-FLIGHT. MAINTENANCE INSPECTED DOOR AND DEFERRED INDICATION. DMI NR 17503 MEL NR 52-4. DMI NR 17503 WAS LATER CLEARED AT IAD BY ADJUSTING POD DOOR HANDLE MICROSWITCH 3-4-95. OPS CHECKED GOOD. (X) 2L72 4T RTA41NM 19950407005981995040700598 1995 4 7 WTAA950116 419950310A3418C771076 STALL VANE BAG JETSTMJETSTM3101 1500215EU RT WING FAILED A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17420UE 788 SEA - RT STALL WARNING AND STICK SHAKER CAME ON IN-FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO EUG. MAINTENANCE RPELACED RT STALL VANE. STALL SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950407005991995040700599SO 1995 4 7 WTAA950117 119950310A2730MS3476L2039P CONNECTOR EMB 120 EMB120RT SO HORIZ STAB CORRODED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17454UE 120155 LAX - AURAL TRIM WARNING ON TAKEOFF. TRIM WHEEL IN GREEN BAND. ABORTED TAKEOFF WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT. MAINTENANCE INSPECTED TRIM WARNING PROXIMITY SENSORS AND FOUND TWO CONNECTORS CORRODED. REPLACED CONNECTORS. TAKEOFF TRIM WARNING OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950407006001995040700600NE 1995 4 7 Y2PA95005 219950404A7261MOBILE254 OIL DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE CONTAMINATED A Y2PACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL23197US 47154 P654600 DTW - RETURNED TO POINT OF DEPARTURE, DTW. NR 1 ENGINE OIL CLOGGED LIGHT ILLUMINATED (ENGINE SN P-654600). AIRCRAFT ABORTED ON TAKEOFF ROLL. REMOVED OIL FILTER, FOUND CARBON IN FILTER, DRAINED AND RESERVICED OIL TANK. REPLACED FILTER. ENGINE IS A LOANER ENGINE. SCHEDULED FOR REMOVAL ON 6-10-95. ENGINE OWNER NOTIFIED OF CONDITION. (X) 2L72 4F4 F A6WE E2EA 19950407006061995040700606SO 1995 4 7 95ZZZX1675 119950308A27101159C210075111 CONTROL CABLE GULSTMG1159 GIV 3980115SO AILERON FRAYED A VIB5K NONE O OTHER ININSP/MAINT 1 SO11712CC3212 1028 DURING INSPECTION, FOUND CABLE ASSEMBLIES, PN 1159C20075-13, 15, 109, 111 FRAYED AND FLAT SPOTTED, WHERE THEY PASS THROUGH FAIR LEADS AND PULLEYS. TOTAL, 8 CABLES LOCATED IN WING REAR BEAM (AILERON CONTROL) SUGGEST MORE FREQUENT INSPECTION AND/OR CHANGE FAIR LEAD MATERIAL TYPE. 2L72 4F RTA12EA 19950407006071995040700607SO 1995 4 7 95ZZZX1676 119950308A27101159C20075109 CONTROL CABLE GULSTMG1159 GIV 3980115SO AILERON FRAYED A VIB5K NONE O OTHER ININSP/MAINT 1 SO11712CC3212 1028 DURING INSPECTION, FOUND CABLE ASSEMBLIES, FRAYED AND FLAT SPOTTED, WHERE THEY PASS THROUGH FAIR LEADS AND PULLEYS. TOTAL, 8 CABLES LOCATED IN WING REAR BEAM (AILERON CONTROL) SUGGEST MORE FREQUENT INSPECTION AND/OR CHANGE FAIR LEAD MATERIAL TYPE. 2L72 4F RTA12EA 19950407006081995040700608SO 1995 4 7 95ZZZX1677 119950308A27101159C2007515 CONTROL CABLE GULSTMG1159 GIV 3980115SO AILERON FRAYED A VIB5K NONE O OTHER ININSP/MAINT 1 SO11712CC3212 1028 DURING INSPECTION, FOUND CABLE ASSEMBLIES, FRAYED AND FLAT SPOTTED, WHERE THEY PASS THROUGH FAIR LEADS AND PULLEYS. TOTAL, 8 CABLES LOCATED IN WING REAR BEAM (AILERON CONTROL) SUGGEST MORE FREQUENT INSPECTION AND/OR CHANGE FAIR LEAD MATERIAL TYPE. 2L72 4F RTA12EA 19950407006091995040700609SO 1995 4 7 95ZZZX1678 119950308A27101159C2007513 CONTROL CABLE GULSTMG1159 GIV 3980115SO AILERON FRAYED A VIB5K NONE O OTHER ININSP/MAINT 1 SO11712CC3212 1028 DURING INSPECTION, FOUND CABLE ASSEMBLIES, FRAYED AND FLAT SPOTTED, WHERE THEY PASS THROUGH FAIR LEADS AND PULLEYS. TOTAL, 8 CABLES LOCATED IN WING REAR BEAM (AILERON CONTROL) SUGGEST MORE FREQUENT INSPECTION AND/OR CHANGE FAIR LEAD MATERIAL TYPE. 2L72 4F RTA12EA 19950407006101995040700610EU 1995 4 7 95ZZZX1679 119950220A2612CA3106KE2821P CONNECTOR BRAERODH125 HS125700A 4230170EU NR 2 ENG PYLON SHORTED A AJCAA UNSCHED LANDING EFNVIBRATION/BUFFET FLT CONT AFFECTED FALSE WARNING CRCRUISE 1 EA2567PW 8528 NA0303 CREW EXPERIENCED NR 2 ENGINE FIRE WARNING. SHUT DOWN ENGINE AND DISCHARGED NR 1 AND NR 2 FIRE EXTINGUISHERS. FIRE WARNING REMAINED ON. LANDED AIRCRAFT AT CPR, INVESTIGATED AND FOUND NO EVIDENCE OF FIRE, OVERHEAT, OR BLEED AIR LEAK. FURTHER INVESTIGATION FOUND CORRODED PYLON CANNON PLUG SHORTED, GIVING FALSE FIRE WARNING INDICATION. REPLACED CANNON PLUG. OPS CHECK NORMAL. RECOMMEND INSPECTION OF TB1 CANNON PLUG IN LT AND RT PYLONS FOR CORROSION. REPLACE IF NECESSARY. 2L72 4F A3EU 19950407006121995040700612EU 1995 4 7 95ZZZX1681 119950310A2720137315E3 TORQUE TUBE BAG JETSTMJETSTM3101 1500215EU RUD PEDAL LOOSE RIVETS A VIB5K NONE O OTHER ININSP/MAINT 1 SO11643JX13060 643 FOUND LOOSE RIVETS AT BOTH ENDS OF PILOT AND CO-PILOT RUDDER PEDAL TORQUE TUBE. 2L72 4T RTA21EU 19950407006151995040700615NE 1995 4 7 95ZZZX1684 219950217A853033226 VALVE 116734 DOUG DC3 DC3A 3021433WP PWA R1830 R183090D 52020NE NR 9 CYL EXH FAILED A CHRAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 GL0312BA 947 10035 144618 EXHAUST VALVE IN THE NR 9 CYLINDER NR 2 ENGINE FAILED CAUSING ENGINE TO RUN ROUGH. FURTHER INVESTIGATION FOUND METAL CONTAMINATION IN THE OIL SUMPS. THESE METAL FRAGMENTS WERE DETERMINED TO BE FROM PIECES OF THE DAMAGED VALVE. IT WAS THEN DECIDED TO REMOVE THE ENGINE FOR FURTHER INSPECTION AND THEN REPAIR. 2L72 4R4 R A669 5E4 19950407006201995040700620NM 1995 4 7 95ZZZW371 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 700 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 700 BETWEEN STRINGER 29L AND 29R. STOP DRILLED CRACK PER SRM 51-10-1, FABRICATED REPAIR DOUBLER .063 7075-T6 PER SRM 51-40-3, TREATED AND PRIMED DOUBLER, WET PER SRM 51-40-3 AND SRM 51-20-4, SIZE 1 INCH BY 3 INCH BY 10 INCH. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006211995040700621NM 1995 4 7 95ZZZW372 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 660 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 660 ABOVE STRINGER 28R, ALSO GUSSET NOT ATTACHED TO 'Z' ANGLE. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER 7075-T6 .063 8 INCHES BY 4 INCHES. INSTALLED DOUBLER PER SRM 51-40-2 AND INSTALLED FASTENERS PER SRM 51-30-2. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006221995040700622NM 1995 4 7 95ZZZW373 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 620 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH29235 21931 DURING D-CHECK, FRAME UPPER FLANGE CRACKED BS 620 BETWEEN STRINGER 28L NUMEROUS AREAS. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA (3 PLACES) PER SRM 53-10-4 FIG 1. INSTALLED FRAME AND REPAIR AND PER SRM 53-10-4 FIG 1 AND SRM 51-30-2. SIZE 24 INCHES BY 3 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006231995040700623NM 1995 4 7 95ZZZW374 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 560 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FRAME UPPER FLANGE CRACKED TWO PLACES BS 560 BETWEEN STRINGER 29L TO OUTBOARD OF 29R. STOP DRILLED CRACKS AS PER SRM 51-10-1. REMOVED DAMAGED AREA AS PER SRM 53-10-4. FABRICATED FILLER 7075-T6 1 INCH BY 3 INCH BY 30 INCHES AS PER SRM 53-10-4. TREATED AND PRIMED PER SRM 51-10-2 AND INSTALLED AS PER SRM 51-30-2. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006241995040700624NM 1995 4 7 95ZZZW375 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 540 GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 540, DAMAGED TO STRINGER 21L, GOUGED. GOUGE STOP DRILLED PER SRM 51-10-1, FABRICATED REPAIR DOUBLER CHANNEL PER SRM 53-10-3 .063 7075-T6, TREATED AND PRIMED PER SRM 51-10-2, REPAIR DOUBLER INSTALLED PER SRM 53-10-3 1 INCH BY 1 INCH BY 10 INCH. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006251995040700625NM 1995 4 7 95ZZZW376 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 20L, STRINGER IS DAMAGED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006261995040700626NM 1995 4 7 95ZZZW377 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 21L, STRINGER IS CRACKED. REPLACED DAMAGE SECTION AS PER SRM 53-10-3. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006271995040700627NM 1995 4 7 95ZZZW378 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 24L, STRINGER IS CRACKED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006281995040700628NM 1995 4 7 95ZZZW379 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 25L, STRINGER IS DAMAGED AND CRACKED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006291995040700629NM 1995 4 7 95ZZZW380 119950220A5313 STRINGER BOEING727 7272Q9 138448MNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FORWARD CARGO COMPARTMENT STATION 500 STRINGER 23, STRINGER IS CRACKED AND DAMAGED. STOP DRILLED CRACK AS PER SRM 53-10-3 AND INSTALLED REPAIR AS PER SRM 53-10-3 12 INCHES BY 2 INCHES. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006301995040700630NM 1995 4 7 95ZZZW381 119950220A5241 SKIN BOEING727 7272Q9 138448MNM RT GALLEY DR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, RT GALLEY SERVICE DOOR FORWARD EXTERNAL DOUBLER REPAIR ON EXTERIOR SKIN AT LOWER HINGE CUTOUT, IS BROKEN AT FWD CORNER. INSTALLED DOUBLER AS PER SRM 51-10-1 4 INCHES BY 4 INCHES PER SRM 51-40-2. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006311995040700631NM 1995 4 7 95ZZZW382 119950220A5311 FRAME BOEING727 7272Q9 138448MNM FS 415 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, RT FORWARD GALLEY SERVICE DOOR FRAME, EXFOLIATED CORROSION ON STRINGER 17R AT AFT LOWER CORNER OF GALLEY DOOR CUTOUT AT FS 415 APPROXIMATELY. REMOVED ANGLE, FOUND OUT OF LIMTI CORROSION, FABRICATED NEW ANGLE 2024-T3.040 AS PER SRM 51-10-1 AND INSTALLED ANGLE AS PER SRM 51-10-1. NEW ANGLE INSTALLED BETWEEN STATION 360 AND STATION 445. TOTAL CYCLES 29,235. 2L73 4F RTA3WE 19950407006321995040700632NM 1995 4 7 95ZZZW383 119950220A5311 FRAME BOEING727 7272Q9 138448MNM FS 375 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, THE RT FWD GALLEY SERVICE DOOR FRAME HAS CORROSION ON FUS FRAME AT APPROX FS 375 AT I/B FLANGE, FWD AND AFT SIDES AT STR 17R. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 MAT 7075-T6 .071 5 INCHES BY 6 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006331995040700633NM 1995 4 7 95ZZZW384 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 330-350 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, AREA EXPOSED BY REMOVAL OF ACCESS PANEL 1104, APPROX BET BS 330 TO 350 FRAME AT APPROX BS 350 HAS EXFOLIATION OF FWD FRAME (APPROX BR 3 INCHES TO BLL 10 INCHES), CORROSION AROUND FASTENERS, CORROSION AT LONG FASTENERS (LT AND RT), CORROSION AT AND AROUND FASTENERS AND HORIZ PLATE. REMOVED CORROSION PER SRM 51-10-6, CUT OUT DAMAGED AREA BS 350 PER SRM 51-40-2, ALODINE AND PRIMED PER SRM 51-10-2, INSTALLED WEB REPAIR PER SRM 51-40-2 AND FASTENERS PER SRM 51-10-1. SIZE 4 INCHES BY 11 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006341995040700634NM 1995 4 7 95ZZZW385 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 690 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, APPROX BS 690 STR 30 FLUSH PATCH REPAIR APPEARS BULGED, CORROSION IND. REPLACED SECTION OF SKIN AS PER SRM 53-30-3 FIG 12. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006351995040700635NM 1995 4 7 95ZZZW386 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 950E CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, AFT CARGO HAS CORROSION ON AFT SIDE OF FUS FRAME 950E AT FWD LOWER CORNER OF DOOR FRAME AT APPROX STR 27R. REMOVED CORROSION PER SRM 51-10-6, CUT OUT DAMAGED SECTION OF WEB AND INSTALLED NEW SECTION PER SRM 51-40-2, 6 INCH BY 18 INCH 7075-T6 .090. INSTALLED SPLICE REPAIR PER SB 727-53-0199, 6 INCHES BY 14 INCHES 7075-T6 .090. TREATED AND PRIMED PER SRM 51-10-2. TOTAL CYCLES 32285. 2L73 4F RTA3WE 19950407006361995040700636NM 1995 4 7 95ZZZW387 119950220A5330 SKIN BOEING727 7272Q9 138448MNM FUSELAGE WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FUS SKIN AT EDGE OF ACCESS PANELS 3519, 3520, AND 3521, PANELS HAVE WORN INTO THE SKIN. BURNISHED WORN AREAS PER SRM 51-10-1, INSTALLED INTERNAL REPAIR PER SRM 53-30-3 FIG 4. INSTALLED EXTERNAL REPAIR PER SRM 53-30-3 FIG 5, ON AREA FOUND TO BE BEYOND LIMITS. DOUBLER SIZE 2 INCHES BY 1.5 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006371995040700637NM 1995 4 7 95ZZZW388 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 1183 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, SKIN AREA BS 1070 AND BS 1183 BETWEEN STR 17L AND STR 21L DENTED AND SCRATCHED. BURNISHED MINOR SCRATCHES PER SRM 51-10-1, CHECKED DEPTH TO LENGTH RATIO OF DENTS. DENTS WITHIN LIMITS PER SRM 53-30-1. REPAIRED DENT AT STA 1080 JUST ABOVE STR 18L PER SRM 53-30-3 2024-T3 .063 9 INCHES BY 12 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006381995040700638NM 1995 4 7 95ZZZW389 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 1030 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, EXT FUS SKIN AREA WITHIN BS 1030 AND BS 1183 BETWEEN STR 21R AND 17R HAS MULTIPLE DENTS AND SCRATCHES. BURNISHED AREA PER SRM 51-10-1, STRAIGHTENED DENTS PER SRM 51-40-1 AND CHECKED LIMITS OF DENTS PER SRM 53-30-1. ALSO, REPAIRED DENTS AT STR 19 STA 1112 PER SRM 53-30-3. MATERIAL 2024-T3 .O63 8 INCHES BY 11 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006391995040700639NM 1995 4 7 95ZZZW390 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 340 HOLE OVERSIZED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, UPPER LOBE RT STA 340 AT TOP OF FLOORBEAM RBL 33, BRACKET TOP AFT RIVET HOLE OVERSIZED. REPLACED FLOORBEAM AS PER SRM 51-10-1 PAR 4. UPPER CAP REPLACED ONLY. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006401995040700640NM 1995 4 7 95ZZZW391 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 360 MATERIAL LOSS A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FLOORBEAM STA 360 RBL 4, TOP FWD HAS A CUT OUT 'CHECK FOR SRM COMFORMANCE'. CUT OUT DAMAGED AREA, FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-8. REPLACED 34.5 INCHES OF UPPER CHORD SPLICE 12.5 INCHES BY 2 INCHES BY 1 INCH O/B END, AND 13 INCHES BY 2 INCHES BY 1 INCH 7075-T6. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006411995040700641NM 1995 4 7 95ZZZW392 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 320-340 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, UPPER LOBE R/B STA 320 TO 340 RBL 42, FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION FLOOR SUPPORT PER SRM 51-10-6, BEYOND LIMITS. REPLACED FLOOR SUPPORT STA 320 TO 340 RBL 42 PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006421995040700642NM 1995 4 7 95ZZZW393 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM STA 30 LBL 3 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FLOORBEAM STA 310 LBL 3 HAS CORROSION ON TOP UNDERSIDE. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA PER SRM 51040-4. INSTALLED ANGLE REPAIR AS PER SRM 51-40-4 9.5 INCHES BY 1 INCH BY 1 INCH. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006431995040700643NM 1995 4 7 95ZZZW394 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 304-380 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, UPPER LOBE RT STA 304 TO 380 RBL 57 HAS CORROSION FLOOR TO SIDE WALL SUPPORT ANGLE. REMOVED CORROSION IN AREA PER SRM 51-10-6 AND 51-10-2. REPLACED FLOOR SUPPORT ANGLE PER SRM 51-10-1. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006441995040700644NM 1995 4 7 95ZZZW395 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 1050 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN FLOORBEAM AT BS 1050 BLL 65. REMOVED CORROSION PER SRM 51-10-6. ALODINE AND PRIMED CUT OUT DAMAGED AREA PER SRM 51-40-4. FABRICATED ANGLE REPAIR PER SRM 53-10-8, ANGLE SIZE 15 INCHES BY .8750 INCH BY 2 INCHES 7075-T6 0.50 AND 0.80. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006451995040700645NM 1995 4 7 95ZZZW396 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 1070 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN FLOORBEAM AT BS 1070 BLL 24 TO BLL 65. REMOVED CORROSION PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. CUT OUT DAMAGED AREA PER SRM 53-10-8. FABRICATED ANGLE 12 INCHES BY 2 INCHES 7075-T6 0.80. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006461995040700646NM 1995 4 7 95ZZZW397 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 990-1130 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT BLR 12 STA 990 TO 1130. REMOVED CORROSION BLR 12 STA 990 TO 1130 PER SRM 51-10-6. MATERIAL REMOVED .003, ALODINE AND PRIMED PER SRM 51-10-2. REPLACED FLOOR SUPPORT FROM STA 1030 TO 1050 AND FROM STA 1050 TO 1070 PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006471995040700647NM 1995 4 7 95ZZZW398 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 1070-1090 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT RBL 12 BS 1070 TO BS 1090. INSTALLED ANGLE REPAIR PER SRM 51-40-4 FIG 3 16 INCHES .050 2024-T3. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006481995040700648NM 1995 4 7 95ZZZW399 119950202A5320 ANGLE BOEING727 7272Q9 138448MNM BS 380-420 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING D-CHECK, FLOOR BOARD ATTACHMENT ANGLE RBL 64 BS 380 TO BS 420 HAS CORROSION TOP AND BOTTOM SIDES. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MATERIAL LOSS 0.002, FABRICATED ANGLE PER SRM 51-10-1 2024-T3 .063. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006491995040700649NM 1995 4 7 95ZZZW400 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 380 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON FLOORBEAM BS 380 UPPER FLANGE TOP AND BOTTOM SIDES FROM BL 0 TO RBL 64. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-8 AT RBL 16 STA 380. ANGLE 1 INCH BY 2 INCH BY 15 INCH 7075-T6 .050 AND ANGLE 1 INCH BY 2 INCH BY 15 INCH 7075-T6 .080. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006501995040700650NM 1995 4 7 95ZZZW401 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 400 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON TOP AND BOTTOM SIDES OF FLOORBEAM UPPER FLANGE BS 400 FROM BL 0 TO RBL 64. CUT OUT DAMAGED AREA, FABRICATED PARTS AND INSTALLED REPAIR PER SRM 53-10-8. REPLACED 37 INCHES OF UPPER CHORD SPLICE OF 12 INCHES BY 2 INCHES BY 1 INCH I/B END. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006511995040700651NM 1995 4 7 95ZZZW402 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM BS 400-420 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FLOOR BOARD ATTACHMENT ANGLE RBL 64 FROM BS 400 TO BS 420 HAS CORROSION. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MATERIAL LOSS 0.002 FABRICATED ANGLE PER SRM 51-10-1. MATERIAL 1014-T3 .063 84 INCHES BY 6 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006521995040700652NM 1995 4 7 95ZZZW403 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 344/360 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH 21931 DURING D-CHECK, CORROSION OF FLOORBEAM SUPPORT BETWEEN BS 344 AND BS 360 TOP FLANGE RBL 12. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-1 PAR 4 AND INSTALLED PER SRM 51-30-2. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006531995040700653NM 1995 4 7 95ZZZW404 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 328 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION AROUND HOLES TOP FLANGE OF FLOORBEAM BS 328 AT LBL 20 AND LBL 46. REMOVED CORROSION PER SRM 51-10-6. CUT 0UT DAMAGED AREAS AND INSTALLED 2 EACH ANGLE REPAIRS 10 INCHES BY 1 INCH BY 1 INCH AT LBL 20 AND LBL 46, MATERIAL USED 7075-T6 .125. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006541995040700654NM 1995 4 7 95ZZZW405 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 1343 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, ON THE NR 2 ENG TORQUE BOX LT SIDE, SKIN HAS FILLER COVERING DAMAGE JUST AFT OF STA 1343 ABOVE RAIN GUTTER. REMOVED FILLER AND PAINT FROM SKIN AFT OF STA 1343, FAB REPAIR PLATE APPROX 12 INCHES BY 14 INCHES .063 2024-T3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED AND SEALED AS PER SRM 53-30-3. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006551995040700655NM 1995 4 7 95ZZZW406 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 720 WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, FUS SKIN EXT SURFACE WORN DOWN BY CHAFING, STA 720 AT STR 19L. REPAIRED AS PER SRM 53-30-3 DETAIL IV. INSTALLED DOUBLER .090 2024-T3 14 INCHES BY 10 INCHES AND FILLER 2024-T3 14 INCHES BY 5 INCHES .071. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006561995040700656NM 1995 4 7 95ZZZW407 119950220A5330 SKIN BOEING727 7272Q9 138448MNM LT AFT FUS CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, BARE METAL AND FRAT CORROSION LEFT AFT FUS FAIRING CONTACT AREA ON FUSELAGE. BURNISHED WORN AREA PER SRM 51-10-1, INSTALLED INTERNAL REPAIR PER SRM 53-30-3 FIG 4. ALSO, INSTALLED AN EXTERNAL REPAIR 2 INCHES BY 1 INCH AS PER SRM 53-30-3 FIG 5 ON AREAS FOUND TO BE BEYOND LIMITS. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006571995040700657NM 1995 4 7 95ZZZW408 119950220A5347 SEAT TRACK BOEING727 7272Q9 138448MNM BS 1020-1130 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN SEAT TRACK 48L STA 1020 TO STA 1130. INSTALLED SEAT TRACK AS PER SRM 53-1-5 STA 1030 TO STA 1130. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006581995040700658NM 1995 4 7 95ZZZW409 119950220A5347 TRACK BOEING727 7272Q9 138448MNM BS 1020-1130 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN SEAT TRACK 24L STA 1020 TO STA 1130. REMOVED AND REPLACED TRACK SECTION PER SRM 51-10-4 PAR 4 FROM STA 1030 TO STA 1130. REMOVED CORROSION AND TREATED FROM STA 1020 TO 1030 PER SRM 51-10-6. MAT REMOVED .003. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006591995040700659NM 1995 4 7 95ZZZW410 119950220A5320 SUPPORT BOEING727 7272Q9 138448MNM BS 1020-1070 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION ON CABIN FLOOR SUPPORT LBL 12 BS 1020 TO BS 1070. REPLACED FLOOR SUPPORTS LBL 12 FROM 1030 TO 1050 AND FROM 1050 TO 1070 PER SRM 51-10-1 PAR 4. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950407006601995040700660WP 1995 4 7 9505369103 119950404A5350 CLIPS DOUG DC9 DC915 3022036WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL0193S 47078 DURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED CLIPS, CHECKED OK. 2L72 4F A6WE 19950407006611995040700661WP 1995 4 7 9505379958 119950404A5320 FITTING DOUG DC9 DC931 3022065WP FS 590 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01917RW 47145 DURING PERIODIC CHECK, FOUND 4 TO 6 INCH CRACK IN LONGERON 26L END FITTING AT FS 590. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950407006621995040700662WP 1995 4 7 9505389161 119950404A5342 FITTING DOUG DC9 DC914 3022034WP VERTICAL STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018905E 45746 DURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER SPAR ATTACH FITTING, LOWER RIGHT SIDE. REPLACED FITTING PER SRM 51-30-2 AND 55-30-0 FIG 2. 2L72 4F A6WE 19950407006631995040700663WP 1995 4 7 9505399963 119950404A5320 SUB FLOOR DOUG DC9 DC931 3022065WP FS 75 229 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01913RW 47171 DURING PERIODIC CHECK, FOUND OIL CANNING IN THE GALLEY SUB FLOOR FS 75 TO 229, RIGHT SIDE. REPAIRED PER EA 99-097069. 2L72 4F A6WE 19950407006641995040700664NM 1995 4 7 9505406614 119950301A5320 PRESS DECK BOEING747 747251B 1384892NM FS 1301-1306 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01614US 20359 DURING PERIODIC CHECK, CORROSION WAS FOUND AT SEVERAL LOCATIONS ON THE LOWER SURFACE OF THE PRESSURE DECK WEB BETWEEN FS 1301 TO 1306, RBL 110 TO 127. DISCREPANT PRESSURE DECK WEB IS MADE FROM .071 INCH 7075-T6 ALUMINUM. REPAIR PER EA 66-80199. 2L74 4F A20WE 19950407006651995040700665NE 1995 4 7 9505412763 219950403A7200 ENGINE BOEING727 7272M7 138407SNM PWA JT8 JT8D17 52049NE NR 3 FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01723RW 21202 707902 ON TAKEOFF ROLL, THE NR 3 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE TAKEOFF WAS ABORTED AT 80 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND THE OIL FILTER AND OIL PRESSURE ORIFICE OBSTRUCTED WITH CARBON. THE ENGINE WAS REPLACED AND RUNUP CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950407006661995040700666 1995 4 7 95UAL747021 419950406A2565 BULKHEAD BFGOODRICH 7A14189 BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29171UA G481 24322 SLIDE RAMP FAILED DURING FLAT FIRE IN SHOP. INTERNAL BULKHEAD FAILURE THE ENTIRE LENGTH OF SLIDE RAMP. SCRAPPED SLIDE RAMP. 2L74 4F4 FRTA20WE E24NE 19950407006671995040700667WP 1995 4 7 ABXA9500289 119950327A533059114063 SKIN DOUG DC9 DC932 3022066WP FS 160 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND SKIN GOUGED IN TWO PLACES, 12 AND 18 INCHES FROM BOTTOM OF DOOR JAMB ON FORWARD SIDE. REPAIRED IAW ABX REA D953-11260-MR. 2L72 4F A6WE 19950407006681995040700668WP 1995 4 7 ABXA9500290 119950324A5311995791739 FRAME DOUG DC9 DC932 3022066WP FS 937 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND THREE HOLES DRILLED AT EDGE OF ALC DOOR JAMB AT STA 937. REPAIRED IAW ABX REA D953-11237-MR. 2L72 4F A6WE 19950407006691995040700669WP 1995 4 7 ABXA9500291 119950321A57133911240503 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING UPPER SURFACE OF STRINGER NR 17. BLENDED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950407006701995040700670WP 1995 4 7 ABXA9500292 119950321A572099193691 T CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 19 TO 20. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407006711995040700671WP 1995 4 7 ABXA9500293 119950321A572099193691 T CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LOWER T-CAP ON LEFT WING BETWEEN STRINGERS 20 TO 21. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407006721995040700672WP 1995 4 7 ABXA9500294 119950321A572099193691 T CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING T-CAP BETWEEN STRINGERS 21 TO 22. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407006731995040700673WP 1995 4 7 ABXA9500295 119950321A572099193691 T CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP AT FORWARD AND AFT FLANGES ON STRINGER NR 20. BLENDED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950407006741995040700674WP 1995 4 7 ABXA9500296 119950312A52805933787503 HINGE DOUG DC9 DC932 3022066WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE HAD EXCESSIVE PLAY. REPLACED HINGE IAW DC-9 SRM 51-30-2 AND DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950407006751995040700675WP 1995 4 7 ABXA9500297 119950313A52805910557503 DOOR DOUG DC9 DC932 3022066WP WS 111.5 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER DELAMINATED. SEALED LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER IAW DC-9 SRM 51-20-0. REPLACED RIVETS IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950407006761995040700676WP 1995 4 7 ABXA9500298 119950318A32313923159505 ROD END DOUG DC9 DC932 3022066WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD OUTBOARD END HAD EXCESSIVE PLAY. REPLACED ROD END IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950407006771995040700677WP 1995 4 7 ABXA9500299 119950314A52805913433501 HINGE DOUG DC9 DC932 3022066WP WS 111.5 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE DEEPLY GOUGED. REPLACE DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950407006781995040700678WP 1995 4 7 ABXA9500300 119950313A32103923159505 ARM ASSY DOUG DC9 DC932 3022066WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR FORWARD LINKAGE CONNECTING POINT HAD EXCESSIVE PLAY. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950407006791995040700679WP 1995 4 7 ABXA9500303 119950317A5712991932216 RIB DOUG DC9 DC932 3022066WP WS 123 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND DEEP GOUGE ON RIGHT WING ADJACENT TO TELESCOPIC SLAT BLEED AIR DUCT. REPAIRED IAW ABX REA D957-11203-MR. 2L72 4F A6WE 19950407006801995040700680WP 1995 4 7 ABXA9500304 119950320A5330591142459 SKIN DOUG DC9 DC932 3022066WP BS 937 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND LEVEL I CORROSION ON INSIDE OF OUTER SKIN, JUST AFT OF ALC DOOR JAMB AT STA 937. REPAIRED IAW ABX REA D953-11223-MR. 2L72 4F A6WE 19950407006811995040700681WP 1995 4 7 ABXA9500305 119950320A5311991150985 FRAME DOUG DC9 DC932 3022066WP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND LEVEL II CORROSION ON FUSELAGE FRAME AT STA 110, RIGHT NOSE WHEEL TUNNEL, LOWER AFT CORNER. REPAIRED FRAME IAW ABX REA D953-11209-MR. 2L72 4F A6WE 19950407006821995040700682WP 1995 4 7 ABXA9500306 119950322A5320591008529 JAMB DOUG DC9 DC932 3022066WP BS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, FOUND THE UPPER FORWARD CORNER OF SERVICE DOOR JAMB HAD A CRACK IN THE EXTERIOR SKIN AT RIVET STA 160. TO GAIN ACCESS TO REPAIR SKIN THE WEB WAS CUT AT STA 184.375. REPAIRED CRACKED SKIN IAW DC-9 SRM 53-05 FIGURE 38 AND 51-30-5. INSTALLED WEB SPLICE IAW ABX REA D953-11251-MR. 2L72 4F A6WE 19950407006831995040700683WP 1995 4 7 ABXA9500307 119950322A531599581871 FLOORBEAM DOUG DC9 DC932 3022066WP BS 945 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND FLOORBEAM AT STA 945 GOUGED ON FORWARD FACE, RBL 1. REPAIRED IAW ABX REA D953-11238-MR. 2L72 4F A6WE 19950407006841995040700684WP 1995 4 7 ABXA9500308 119950318A5330591140027 SKIN DOUG DC9 DC932 3022066WP BS 37 BUCKLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23980AX 47176 DURING C-CHECK, INSPECTION FOUND SKIN JUST ABOVE LEFT FORWARD CORNER OF FORWARD NOSE GEAR DOOR BUCKLED. REPAIRED SKIN IAW ABX REA D953-11207-MR. 2L72 4F A6WE 19950407006851995040700685WP 1995 4 7 ABXA9500309 119950405A33505D0015 EEL CIRCUIT BKR DOUG DC8 DC863 302198AWP CABIN DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23812AX 46126 THE EMERGENCY LIGHT ILLUMINATED WITHOUT ANY LOSS OF AIRCRAFT ELECTRICAL POWER. FOUND A DEFECTIVE EMERGENCY LIGHT CONTROL CIRCUIT BREAKER. REMOVED AND REPLACED CIRCUIT BREAKER. EMERGENCY EXIT LIGHT CONTROL SYSTEM OPS CHECKS GOOD, IAW DC-8 MM CHAPTER 33. 2L74 4F 4A25 19950407006861995040700686WP 1995 4 7 ABXA9500310 119950404A5610224504259 HINGE PINS DOUG DC8 DC861 3021952WP CO-PILOTS WINDOWLACK OF LUBE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 46032 THE FIRST OFFICER'S SLIDING WINDOW VERY DIFFICULT TO OPEN. CLEANED AND LUBED HINGE PINS AND LATCHING MECHANISM. WINDOW OPS CHECKED GOOD IAW DC-8 MM CHAPTER 56. 2L74 4F 4A25 19950407006871995040700687SO 1995 4 7 COM11847 119950405A5243H1653081562 LATCH EMB 120 EMB120RT SO RT NACELLE BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01256CA 120245 RIGHT HYDRAULIC PACK SERVICE DOOR HAS A BROKEN LATCH. REPLACED LATCH. 2L72 4T RTA31SO 19950407006881995040700688SO 1995 4 7 COM11848 119950405A5243H1653081562 LATCH EMB 120 EMB120RT SO RT NACELLE BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01189CA 120189 RIGHT HYDRAULIC PACK SERVICE DOOR FWD LATCH IS BROKEN. REPLACED LATCH. 2L72 4T RTA31SO 19950407006891995040700689SO 1995 4 7 COM11849 119950331A291012038646002 HYD LINE EMB 120 EMB120RT SO RT NACELLE CRACKED A COMAK NONE KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01258CA8937 120247 HYDRAULIC SYSTEM LOW LEVEL WARNING ILLUMINATED. POST FLIGHT INSPECTION, FOUND HYD LEAK RT ENGINE NACELLE. THE ENGINE FIRE DECK WAS FOUND CRACKED AND BROKEN, WHERE THE HYDRAULIC LINES ENTER THE ENGINE COMPARTMENT. THIS DAMAGE CAUSED MOVEMENT AND CHAFING OF THE HYDRAULIC LINES. THE FIRE DECK AND HYDRAULIC LINES WERE REPAIRED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950407006901995040700690SO 1995 4 7 COM11850 119950331A3240396512 CONTL VALVE EMB 120 EMB120RT SO ANTI-SKID SYST DEFECTIVE A COMAK NONE L NO TEST UKUNKNOWN 1 SO01241CA8869 4709 120211 ANTI-SKID SYSTEM DOES NOT TEST. REPLACED BRAKE ANTI-SKID CONTROL VALVE. 2L72 4T RTA31SO 19950407006911995040700691SO 1995 4 7 COM11851 119950401A7600MS33201 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A COMAK NONE O OTHER UKUNKNOWN 1 SO01267CA 120259 FLIGHT IDLE STOP LOCKOUT SOLENOID CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND SYSTEM TEST NORMAL. 2L72 4T RTA31SO 19950407006921995040700692SO 1995 4 7 COM11852 119950401A323012038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01267CA7086 4725 120259 LANDING GEAR SELECTOR CONTROL COULD NOT BE MOVED TO THE RETREAT POSITION. REPLACED THE LANDING GEAR CONTROL BOX. 2L72 4T RTA31SO 19950407006931995040700693WP 1995 4 7 MWEA95163 119950404A3397 WIRE DOUG DC9 DC914 3022034WP COCKPIT BROKEN A MWEAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31400ME 45727 PILOT REPORTS, WHITE SMOKE COMING FROM THE CAPTAINS SIDE BRIEFCASE LIGHT DIMMER SWITCH. MAINTENANCE REPAIRED BROKEN WIRE BEHIND CAPTAINS BRIEFCASE RHEOSTAT. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950407006941995040700694EU 1995 4 7 QXEA9500083 119950320A35304566M37B PBE WARNING FOKKERF28 F28MK1000 4990808EU COCKPIT PROTRUDING A QXEAK NONE J WARNING INDICATION ININSP/MAINT 1 NM09801PH78983 26742 GEG - THE COCKPIT ENTRANCE PBE IS SOFT AND HAS IT'S WARNING INDICATOR PROTRUDING. THE PBE WAS REPLACED WITH A SERVICEABLE UNIT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950407006951995040700695NM 1995 4 7 QXEA9500096 119950331A3530 PBE TIE DHAV DHC8 DHC8102 2809003NM PILOT MISSING A QXEAK NONE O OTHER ININSP/MAINT 1 NM09820PH 63 SEA - AFT CABIN PBE SECURITY TIE IS MISSING. INSTALLED A SERVICEABLE TIE AS NEEDED, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950407006961995040700696NM 1995 4 7 QXEA9500097 119950401A2120 AIR DISTR DORNERDO32 DO328100 2996000NM COCKPIT SMOKE A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09338PH 3029 BLEED AIR CAUSED SMOKE IN THE COCKPIT. SHUT-OFF NR 2 POCK AND SMOKE CLEARED. GROUND RAN ENGINES AT IDLE AND ABOVE TO CLEAN OIL FROM BLEED AIR SYSTEM. CHECKED THE HX FAN FOR OPERATION, NO SMOKE SMELL NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407006971995040700697EU 1995 4 7 QXEA9500098 119950402A3350 LIGHT FOKKERF28 F28MK1000 4990808EU CABIN EEL BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - EVACUATION LIGHT ON SEAT 1/B IS BROKEN. REPAIRED LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950407006981995040700698EU 1995 4 7 QXEA9500099 119950402A35304566M37B PBE WARNING FOKKERF28 F28MK1000 4990808EU CABIN PROTRUDING A QXEAK NONE J WARNING INDICATION ININSP/MAINT 1 NM09452US1141 11105 PDX - THE AFT PBE RED BUTTON IS STICKING OUT. REMOVED AND REPLACED PBE. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950407006991995040700699EU 1995 4 7 QXEA9500100 119950402A4900 APU FOKKERF28 F28MK1000 4990808EU CABIN SMOKING A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09452US 11105 SEE - THE APU SMOKES AND PUTS SMOKE IN THE CABIN. APU WAS PLACED ON MEL REF 49-1 CAT C. 2L72 4F RTA20EU 19950407007001995040700700EU 1995 4 7 QXEA9500101 119950402A3350 EEL WIRE FOKKERF28 F28MK1000 4990808EU CABIN DAMAGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 GEG - THE AFT SECTION OF FLOOR PROXIMITY LIGHTS WON'T ILLUMINATE. APPLIED INTERM REPAIR TO THE DAMAGED WIRE HARNESS AND RESCHEDULED CORRECTIVE ACTION ON AN MRSI. LIGHTS WORKED NORMALLY AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950407007011995040700701NM 1995 4 7 QXEA9500102 119950401A33506104781 EEL BATTERY BOX DHAV DHC8 DHC8102 2809003NM CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09815PH10967484 50 SEA - THE FWD TWO RED EMERGENCY EXIT LIGHTS ARE INOP. REPLACED THE BATTERY PACK AND EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950407007021995040700702EU 1995 4 7 QXEA9500103 119950405A3310561408B212 BALLAST FOKKER FOKKERF28 F28MK1000 4990808EU COCKPIT FAILED A QXEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09801PH 11097 PDX - ACRID SMELL IN COCKPIT, ON TAXI OUT. FLIGHT ATTENDANT ALSO COMPLAINED OF ACRID SMELL. AIRCRAFT RETURNED TO GATE. REPLACED COCKPIT LIGHT BALLAST. AIRCRAFT GROUND RUN, NO ACRID SMELL NOTED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950407007031995040700703NM 1995 4 7 QXEA9500104 119950405A3260 HARNESS DORNER DORNERDO32 DO328100 2996000NM LT MLG DEFECTIVE A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09334PH 3012 PDX - AFTER GEAR RETRACTION OR EXTENSION, A SINGLE CHIME SOUNDS WITH AN AMBER PROX SYSTEM CAS MESSAGE, FOLLOWED BY A BLUE HYDRAULIC QTY CAS MESSAGE. REPLACED LEFT AMIN GEAR DOWNLOCK FORWARD HARNESS I/A/W MM. GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950407007041995040700704SW 1995 4 7 QXEA9500105 119950405A32302752000057 RETRACT MECH SWRNGN SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A QXEAK NONE O OTHER CLCLIMB 1 NM09384PH AC592 PDX - NOSE GEAR COMPLETED RETRACTION CYCLE WITH AN ALARMING THUMP, VERY LOUD AND CLEAR IN THE COCKPIT. RESHIMMED ACTUATOR BELLCRANK STOPS AND REPLACED STRIKER LINK RODS I/A/W MM. GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950407007051995040700705NM 1995 4 7 UPS202821 119950405A531169154055 FRAME BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT FRAME CHORD, STA 1342, LBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007061995040700706NM 1995 4 7 UPS202822 119950405A531169154056 FRAME BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT FRAME CHORD, STA 1342, RBL 20, WL 238. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007071995040700707NM 1995 4 7 UPS202823 119950405A53206595326 CHORD BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT O/B CHORD, STA 1342, RBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007081995040700708NM 1995 4 7 UPS202824 119950405A532065195325 CHORD BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT O/B CHORD, STA 1342, LBL 30, WL 250. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007091995040700709NM 1995 4 7 UPS202825 119950405A532065225517 CHORD BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL, STA 1342. REPLACED PER UPS EO 727-5530-4601B. 2L73 4F A3WE 19950407007101995040700710NM 1995 4 7 UPS202826 119950405A532065209812 CHORD BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE 1342 CHORD FWD SIDE. REPLACED PER UPS EO 727-5530-4601B. 2L73 4F A3WE 19950407007111995040700711NM 1995 4 7 UPS202827 119950405A53116517508224 FRAME BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT LWR FRAME CHORD STA 1342, RBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007121995040700712NM 1995 4 7 UPS202828 119950405A53116517508223 FRAME BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT LWR FRAME CHORD STA 1342, LBL 24, WL 220. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007131995040700713NM 1995 4 7 UPS202829 119950405A53116693155567 FRAME BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT CHANNEL, AFT SIDE OF FRAME, STA 1342, WL 247, LBL 18. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007141995040700714NM 1995 4 7 UPS202830 119950405A53206693155677 CHANNEL BOEING727 72722C 138400FNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT CHANNEL STA 1342, WL 247, RBL 18. REPLACED PER UPS EO 727-5530-4601. 2L73 4F A3WE 19950407007151995040700715NM 1995 4 7 UPS202831 119950405A5320 SHEAR TIE BOEING727 72722C 138400FNM BS 1323 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON SHEAR TIE BS 1323, BETWEEN STRINGERS 17 AND 18L. REPLACED PER SRM 51-40-3 AND 53-10-2. 2L73 4F A3WE 19950407007161995040700716NM 1995 4 7 UPS202832 119950405A5412 WEB BOEING727 72722C 138400FNM BS 1342 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FIREWALL WEB AT BS 1342, LBL 24, WL 220. INSTALLED REPAIR PER SRM 51-40-2 AND 54-10-3. 2L73 4F A3WE 19950407007171995040700717NM 1995 4 7 UPS202833 119950405A5320 RIB BOEING727 72722C 138400FNM BS 1365 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, RT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 1-30-2. 2L73 4F A3WE 19950407007181995040700718NM 1995 4 7 UPS202834 119950405A5320 RIB BOEING727 72722C 138400FNM BS 1365 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON O/B RIB STA 1365, LT SIDE. INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19950407007191995040700719NM 1995 4 7 UPS202835 119950405A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR PANEL BEAM WEB, BS 760, LBL 48, BELOW FLOOR LEVEL AFT SIDE. INSTALLED REPAIR PER SRM 51-40-2. 2L73 4F A3WE 19950407007201995040700720NM 1995 4 7 UPS202836 119950405A5320 FITTING BOEING727 72722C 138400FNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM TO SEAT TRACK SUPPORT FITTING, BS 760, LBL 48. REPLACED PER SRM 51-40-4 AND 51-30-2. 2L73 4F A3WE 19950407007211995040700721NM 1995 4 7 UPS202837 119950405A5320 SILL BOEING727 72722C 138400FNM BS 580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL WEB, UNDER DOOR FITTING, STA 580. INSTALLED REPAIR PER USRM 51-40-2. 2L73 4F A3WE 19950407007221995040700722NM 1995 4 7 UPS202838 119950405A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK LWR FLANGE OF CHORD, STA 760, LBL 45. INSTALLED REPAIR PER SRM 53-10-2, 51-30-2, 51-10-6, AND BOEING DRWNG 65-34144-13. 2L73 4F A3WE 19950407007231995040700723NM 1995 4 7 UPS202839 119950405A5320 SHEAR WEB BOEING727 72722C 138400FNM BS 1140-1145 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01929UP 19092 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON TWO HOLES THROUGH LT SHEAR WEB AT BS 1140 TO 1145, LBL 30, AS SEEN FROM BELOW. INSTALLED REPAIR PER SRM 51-40-2 AND 51-30-2. 2L73 4F A3WE 19950407007241995040700724WP 1995 4 7 UPS802820 119950405A53425651927 ANGLE DOUG DC8 DC873F 302199FWP VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01814UP 46090 WHILE IN 'C' CHECK, MAINTENANCE FOUND A CRACK ON RT VERT STAB TO FUSELAGE ATTACH ANGLE. INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F RT4A25 19950407007261995040700726EU 1995 4 7 95ZZZX1690 119950322A6420109013105111 TRUNNION 109813102115AGUSTAA109 A109K2 0260502EU T/R HUB GALLED A AQKZAK NONE M OVER TEMP ININSP/MAINT 1 NM07911RX186 A40001 10017 ON PRE-FLIGHT, A BLUING (HEATED) AREA WAS FOUND ON THE T/R HUB AT THE BUSHING END, ONE SIDE. A TEAR DOWN REVEALED THE TRUNNION SLEEVE AND BUSHING HAD SEVERE GALLING AND HEAT DAMAGE. BOTH TRUNNION AND BUSHINGS WERE REPLACED. SUBMITTER SUGGESTS RE-DESIGN WITH DIFFERENT MATERIALS AND TOLERANCES MIGHT HELP EXTEND THE LIFE OF THESE PARTS. 1G72 3U RTH7EU 19950407007581995040700758EA 1995 4 7 95ZZZX1722 119950313A5521C2TE103AND RIB DHAV DHC2 DHC2MK1 2800102EA LT ELEV CORRODED AL ERHAK NONE O OTHER ININSP/MAINT 1 AL036808317485 1254 LEFT ELEVATOR TIP RIB WAS FOUND PERFORATED BY CORROSION UNDER MASS BALANCE WEIGHTS C2TE-113 AND DASH 115. ONLY ONE FASTENER WAS RETAINING THE WEIGHTS. THE LEAD WEIGHTS ARE ON BOTH SIDES OF THE ALUMINUM RIB AND ARE RETAINED BY STEEL SCREWS. THE CONDITIONS ARE PERFECT FOR CORROSION. 1H71 3R A806 19950414000011995041400001NM 1995 4 14 9505422286 119950405A3230 RETRACT MECH BOEING727 727251 138408HNM LANDING GEAR MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01286US 21325 DURING DEPARTURE CLIMB, UNABLE TO ACTUATE LANDING GEAR HANDLE FOR GEAR RETRACTION. UPON FLAP RETRACTION, TAKEOFF WARNING HORN SOUNDED. SUSPECTED AIR GROUND SENSING PROBLEM. FLIGHT DIVERTED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE SIMULATED IN-FLIGHT MODE AND COULD NOT DUPLICATE MALFUNCTION. CLEANED AIR GROUND SENSOR. PERFORMED OPERATIONAL CHECK OF TAKEOFF WARNING SYSTEM WITH NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950414000021995041400002NM 1995 4 14 95UAL727033 119950406A3350 EEL RECEPTACLE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297257U 21404 EEL STRIP BETWEEN ROWS 5 T0 13 IS INOPERATIVE. REPLACED POWER STRIP RECEPTACLE. 2L73 4F4 F A3WE E2EA 19950414000031995041400003NM 1995 4 14 95UAL737044 119950406A2742AR7077M2MOD8 ACTUATOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE HORIZ STAB MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK KF FLUID LOSS FLT CONT AFFECTED TOTAKEOFF 1 WP29363UA 2900 24532 ON TAKEOFF ROLL, SPEED TRIM STARTED TRIMMING AIRCRAFT AT APPROXIMATELY 100 KNOTS. CONTINUED FORWARD NOSE DOWN TRIMMING AND WOULD NOT STOP. ABORTED TAKEOFF AT 110 KNOTS. TRIMMED STABILIZER TO AFT LIMIT OF GREEN BAND. REPLACED ELECTRIC ACTUATOR. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950414000041995041400004WP 1995 4 14 95UALD10030 119950406A3350 EEL CONTACTS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN CORRODED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291845U 48261 EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPLACED CORRODED CONTACTS C AND D 0N CONNECTOR. 2L73 4F4 F A22WE E23EA 19950414000051995041400005NM 1995 4 14 DHL95724001 119950404A3260106122615 SENSOR BOEING727 727228 NM LT MLG DIRTY A TDHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01724DH 19862 ON CLIMB-OUT, LANDING GEAR LEVER WOULD NOT GO PAST OFF. MOVED LEVER TO UP USING OVERRIDE SWITCH. LEVER LATCH AND LIGHTS CIRCUIT BREAKER POPPED P6-3. RESTORED AIRCRAFT TO FLIGHT MODE PER ALTERNATE PROCEDURE. CLEANED LEFT MAIN GEAR AIR GROUND PROXIMITY SWITCHES. COULD NOT DUPLICATE ON GROUND PER MM 3230. 2L73 4F A3WE 19950414000061995041400006 1995 4 14 MWEA95164 419950406A2565136212251 EVAC SLIDE DOUG DC9 DC932 3022066WP AFT FUSELAGE LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31204ME 47680 DURING ROUTINE INSPECTION, FOUND TAIL EVACUATION SLIDE PRESSURE LOW. REPLACED TAIL EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950414000071995041400007WP 1995 4 14 MWEA95165 119950406A253062000111 OVEN DOUG DC9 DC914 3022034WP GALLEY SMOKING A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31800ME 45842 CREW REPORTS NR 1 OVEN IS SMOKING WHEN TURNED ON. REPLACED NR 1 OVEN. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950414000081995041400008NM 1995 4 14 SCNA95049 119950404A335065784591 EEL BATTERY PACK BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 21438 L2 AND R2 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONS CHECKED GOOD. 2L73 4F RTA3WE 19950414000091995041400009NM 1995 4 14 95ZZZW411 119950220A5315 FLOORBEAM BOEING727 7272Q9 138448MNM BS 344 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, HEAVY CORROSION CABIN FLOORBEAM BS 344. REMOVED OLD BAD UPPER CAP. CLEANED AREA WITH ALODINE AND PRIMED BARE PLACES AS PER SRM 51-10-6. INSTALLED NEW CAP AS PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000101995041400010NM 1995 4 14 95ZZZW412 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 700-720 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CORROSION STA 700 BETWEEN STA 700 TO 720 STR 26L TO 26R ON PNL ATTACH ANCHOR NUTS. REPLACED SECTION OF SKIN AS PER SRM 53-30-3 FIG 12. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000111995041400011NM 1995 4 14 95ZZZW413 119950220A5330 SKIN BOEING727 7272Q9 138448MNM BS 690-700 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CRACK ON FUS SKIN STA 690 AND 700 BETWEEN STR 27L TO 28L. REPLACED SECTION OF SKIN 35 INCH BY 50 INCH 2024-T3 .071 AS PER SRM 53-30-3 FIG 12, SPLICE 7 INCH BY 50.5 INCH 2024-T3 .080. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000121995041400012NM 1995 4 14 95ZZZW414 119950220A5311 FRAME BOEING727 7272Q9 138448MNM STA 804 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, UPPER LOBE STA 804 STR 14R, CRACK IN FRAME, STOP DRILLED PER SRM 51-10-1. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 SIZE 1 INCH BY 1 INCH BY 9 INCH MAT 7075-T6 .071. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000131995041400013NM 1995 4 14 95ZZZW415 119950220A5311 FRAME BOEING727 7272Q9 138448MNM BS 720 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, UPPER LOBE STA 720F STR 15F, CRACKED AT FRAME. STOP DRILLED PER SRM 51-10-1. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 7075-T6 .071 1 INCH BY 1 INCH BY 10 INCH. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000141995041400014NM 1995 4 14 95ZZZW416 119950220A5242 SKIN BOEING727 7272Q9 138448MNM E/E DOOR DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, E AND E DOOR EXTERIOR SKIN DENTED AT AFT CENTER EDGE. STRAIGHTEN SKIN PER SRM 51-40-1. DYE CHECK PER SRM 20-20-2. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR AS PER SRM 52-00-3. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000151995041400015NM 1995 4 14 95ZZZW417 119950202A5711 SPAR BOEING727 7272Q9 138448MNM FSS 188-203 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, THE LT WING SPAR LOWER CHORD CORRODED FROM FS 188 TO 203. REMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER REPAIR PER SRM 51-40-4 FIG 1. REPAIR SIZE 2 INCHES BY 14 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000161995041400016NM 1995 4 14 95ZZZW418 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM BS 1176.9 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, HEAVY CORROSION RIGHT O/B END OF BS 1176.9 CHORD. REMOVED CHORD ANGLE PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6 MAT LOSS .002 INCH. REPLACED CHORD ANGLE PER SRM 51-10-1 PAR 4 AND INSTALLED PER SRM 51-30-2. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000171995041400017NM 1995 4 14 95ZZZW419 119950220A5320 ANGLE BOEING727 7272Q9 138448MNM FS 370 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01741DH32285 21931 DURING D-CHECK, CABIN INTERIOR HAS SURFACE CORROSION ON I/B AND O/B SIDES OF CABIN FLOOR ANGLE AT FS 370, AT APPROX STR 17R. REMOVED ANGLE PER SRM 51-30-2. REMOVED CORROSION AROUND ANGLE AREA PER SRM 51-10-6. MAT LOSS 0.002, FABRICATED ANGLE PER SRM 51-10-1 MAT .2024-T3 .063 84 INCHES BY 63 INCHES. TOTAL CYCLES 29235. 2L73 4F RTA3WE 19950414000181995041400018NM 1995 4 14 95ZZZW420 119950309A21317638102 CONTROLLER BOEING737 7373B7 1384580NM CABIN FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19398US 23507 LAS - FLT 414 - EN ROUTE LAX TO MCI, CABIN PRESSURE BEGAN CLIMBING. DROPPED TO FL 290 AND CREW WAS ABLE TO CONTROL PRESSURE ON MANUAL. BOTH GENERATORS THEN DROPPED OFF LINE. CREW GOT THEM BAC ON LINE AND DIVERTED FLIGHT TO LAS WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. OPS CHECKED ENGINE GENERATORS, NO PROBLEMS NOTED. REFERENCE NR USAA950241. 2L72 4F RTA16WE 19950414000191995041400019NM 1995 4 14 95ZZZW421 119950316A21503964981 CONTROL VALVE BOEING737 7374B7 1384702NM RIGHT FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19448US 24892 PIT - FLT 670 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. RIGHT PACK ON MEL AND LEFT PACK VERY WEAK. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT TURBO FAN VALVE AND FLOW CONTROL VALVE. REFERENCE USAA950247. 2L72 4F RTA16WE 19950414000201995041400020NM 1995 4 14 95ZZZW422 119950317A2133 OUTFLOW VALVE BOEING737 7373B7 1384580NM CABIN LEAKING A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19520AU 23706 PIT - FLT 1406 - FLIGHT EN ROUTE CMH TO TPA WHEN CREW REPORTED A PRESSURIZATION PROBLEM. AIR LEAK AND LOUD AIR NOISE HEARD FROM FORWARD ENTRY DOOR. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED HINGE PIN IN UPPER HINGE COVER. FOUND AFT OUTFLOW VALVE NOT COMPLETELY CLOSING. REPLACED OUTFLOW VALVE AND CONTROLLER. RESEALED INNER AREA AROUND EXTERNAL POWER RECEPTACLE. REFERENCE USAA950248 . 2L72 4F RTA16WE 19950414000211995041400021NM 1995 4 14 ASAA95043 119950202A5315 FLOORBEAM BOEING737 737210C 1384459NM BS 547.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLANGE OF THE FLOORBEAM UPPER CHORD AT STA 547.5. REPAIRED CHORD PER EA 5310-01317 AND BOEING TELEX ASA-SEA-94-0310RR. (W) 2L72 4F A16WE 19950414000221995041400022NM 1995 4 14 ASAA95044 119950202A5314 KEEL BEAM BOEING737 737210C 1384459NM BS 540 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, A CRACK WAS FOUND ON THE HORIZONTAL FLANGE OF THE KEEL BEAM CHORD AT BS 540, LBL 6.30. THE CRACK WAS APPROXIMATELY 2 INCHES IN LENGTH AND APPEARS TO HAVE ORIGINATED AT THE AFT MACHINE STEP AND TRAVELED FORWARD. REPAIRED CRACK PER EA 5310-01315. (W) 2L72 4F A16WE 19950414000231995041400023NM 1995 4 14 ASAA95045 119950202A5314 KEEL BEAM BOEING737 737210C 1384459NM BS 647-727 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01744AS 21822 SEA - DURING D-CHECK, SURFACE CORROSION WAS FOUND AROUND THE FASTENER HOLES OF KEEL BEAM BS 647 TO 727, LBL 6.5. REPAIRED KEEL BEAM PER EA 5310-01321 AND BOEING TELEX ASA-SEA-95-0057RR. (W) 2L72 4F A16WE 19950414000241995041400024NM 1995 4 14 ASAA9510012 119950311A3350900835A EEL BATT PACK BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - DURING MAINTENANCE CHECK, THE NR 1 SEAT PALLET EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000251995041400025NM 1995 4 14 ASAA9510013 119950315A335010617838 EEL ASSY BOEING737 737290C 138448VNM BULKHEAD INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000261995041400026NM 1995 4 14 ASAA9510014 119950320A3350303 EEL LAMP BOEING737 7372Q8C 138448SNM CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS ON PALLET 7 TO 5 AND 8 TO 7 WERE FOUND INOPERATIVE. RELAMPED AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000271995041400027NM 1995 4 14 ASAA9510015 119950320A5210 COVER BOEING737 737210C 1384459NM L-1 DOOR HINGE LOOSE A ASAAO OTHER O OTHER TXTAXI/GRND HDL 1 NM01744AS 21822 JNU - FLT 65 - CREW REPORTED, THE L-1 DOOR WAS DIFFICULT TO CLOSE. REATTACHED LOOSE HINGE COVER TRIM ON L-1 DOOR AND OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000281995041400028NM 1995 4 14 ASAA9510016 119950321A5210 LOCK RING BOEING737 7372Q8C 138448SNM L-1 DOOR MISSING A ASAAO OTHER O OTHER TXTAXI/GRND HDL 1 NM01741AS 21959 OME - FLT 51 - CREW REPORTED, UNABLE TO OPEN L-1 DOOR. FOUND LOCK RING MISSING FROM UPPER GUIDE ARM. REPLACED RING AND DOOR OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000291995041400029NM 1995 4 14 ASAA9510017 119950321A335020131A EEL BATTERY BOEING737 737290C 138448VNM FIRST PALLET DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE ON THE FIRST PALLET. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950414000301995041400030WP 1995 4 14 ASAA9532 119950123A3350S103 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01963AS 53077 SEA - AT CHECK, ROW AND AFT PEEPLS LIGHTS INOP. MAINTENANCE REPLACED BATTERIES. (W) 2L72 4F RTA6WE 19950414000321995041400032WP 1995 4 14 ASAA9536 119950125A3350PR2 EEL LAMP DOUG DC9 DC982 3022082WP CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01953AS 49386 SEA - CHECK, L-1 DOOR PORTABLE EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED AND OPS CHECKED NORMAL. (W) 2L72 4F A6WE 19950414000331995041400033WP 1995 4 14 ASAA9538 119950126A335060030431 EEL BATT PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01953AS 49386 SEA - AT CHECK, 4 OVERHEAD EMERGENCY LIGHTS IN MID CABIN COME ON WHEN ACFT POWER IS TURNED OFF. MAINTENANCE REPLACED BATTERY PACK. (W) 2L72 4F A6WE 19950414000341995041400034NM 1995 4 14 ASAA9540008 119950310A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - AT CHECK, AFT 2 EMERGENCY TRACK LIGHTS INOP. MAINTENANCE SECURED LIGHT HARNESS TO LIGHT ASSY. (W) 2L72 4F RTA16WE 19950414000351995041400035NM 1995 4 14 ASAA9540009 119950316A3350 EEL WIRING BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 SEA - AT CHECK, EMERGENCY FLOOR LIGHTS INOP AT ROW 26 AFT. MAINTENANCE SECURED LOOSE CONNECTION IN WIRING. (W) 2L72 4F RTA16WE 19950414000361995041400036NM 1995 4 14 ASAA9540010 119950318A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 SEA - AT CHECK, THE AFT 2 RED PEEPLS LIGHTS ARE INOP. MAINTENANCE RECONNECTED WIRING AT THE FWD MOST OF THE AFT PEEPLS LIGHTS. (W) 2L72 4F RTA16WE 19950414000371995041400037NM 1995 4 14 ASAA9540011 119950319A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - AT CHECK, TRACK LIGHTS AT ROWS 14 TO 17 INOP. MAINTENANCE RECONNECTED WIRES. (W) 2L72 4F RTA16WE 19950414000381995041400038WP 1995 4 14 ASAA9580046 119950311A3350 EEL TERMINAL DOUG DC9 DC982 3022082WP TAILCONE MISSING A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01956AS 48079 SEA - DURING MAINTENANCE CHECK, AN OVERHEAD EMERGENCY LIGHT IN THE TAILCONE WAS FOUND INOPERATIVE. INSTALLED MISSING TERMINAL SCREW ON LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A6WE 19950414000391995041400039WP 1995 4 14 ASAA9580048 119950313A3350273005 EEL FUSE DOUG DC9 DC982 3022082WP CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 27 AFT WERE FOUND INOPERATIVE. REPLACED THE PICO FUSE IN THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950414000401995041400040WP 1995 4 14 ASAA9580052 119950316A335060030451 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 1 THROUGH 7 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950414000411995041400041WP 1995 4 14 ASAA9580053 119950321A335041B004AD07G3 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS 49364 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 14 THROUGH 17. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950414000421995041400042WP 1995 4 14 ORJA9519 119950317A335041B004AD073 EEL BATTERY EA1D1303 DOUG DC9 DC987 3022087WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11750RA 49777 DURING T/S INSPECTION, FOUND EMERGENCY TRACK LIGHTING INOP. REPLACED FLOOR TRACK LIGHTING BATTERY POWER SUPPLY. OPS CHECK NORMAL. (W) 2L72 4F RTA6WE 19950414000431995041400043WP 1995 4 14 ORJA9520 119950318A3260 GEAR WARNING DOUG DC9 DC987 3022087WP COCKPIT ACTIVATED A ORJAO OTHER N FALSE WARNING CLCLIMB 1 WP11750RA 49777 RNO - ON TAKEOFF, GEAR WARNING HORN AND RED GEAR UNSAFE LIGHTS CAME ON. HORN COULD BE SILENCED, RED LIGHTS ON UNTIL 210 IAS. PERFORMED PROX BOX BITE TEST. OPS CHECK NORMAL. (W) 2L72 4F RTA6WE 19950414000441995041400044WP 1995 4 14 ORJA9521 119950319A32605758405403 SWITCH DOUG DC9 DC987 3022087WP PEDESTAL FAILED A ORJAO OTHER N FALSE WARNING CLCLIMB 1 WP11750RA 49777 RNO - ON CLIMB-OUT FROM LAS, AFTER GEAR RETRACTED, GEAR HORN SOUNDED AND ALL RED GEAR LIGHTS WERE RED. AT LEVEL OFF, ALL RED LIGHTS WENT OUT. REMOVED AND REPLACED THROTTLE LIMIT SWITCH PER MM 76-10-00. (W) 2L72 4F RTA6WE 19950414000451995041400045WP 1995 4 14 ORJA9522 119950320A335041B004AD073 EEL BATTERY EA1D1303 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11821RA 49931 EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERIES ON AISLE 16-19. OPS CHECK GOOD. (W) 2L72 4F A6WE 19950414000461995041400046WP 1995 4 14 ORJA9524 119950327A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 EMERGENCY AISLE TRACK LIGHTING INOP AT ROW 3, 4, AND 5. REPAIRED WIRES AT ROW 3, 4, AND 5, OPS NORMAL. (W) 2L72 4F RTA6WE 19950414000471995041400047EU 1995 4 14 USAA950233 119950307A3260 BRACKET FOKKERF28 F28MK4000 4990810EU RT MLG CHAFING A USAAO OTHER N FALSE WARNING CLCLIMB 1 EA19478US 11227 BGM - FLT 0746 - THE RED LANDING GEAR DOOR LIGHT REMAINED ON AFTER TAKEOFF FROM BFM. THE GEAR WAS RECYCLED BUT THE LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED TO PIT WITH GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSTALLED THREE RIVETS, ADJUSTED STOPS AND REPLACED THE RIGHT MAIN LANDING GEAR DOOR SADDLE BRACKET. THE DOOR WAS RIGGED AND GEAR SWING PERFORMED. ALL INDICATIONS WERE NORMAL. (W) 2L72 4F RTA20EU 19950414000481995041400048NM 1995 4 14 USAA950241 119950309A21337110033 VALVE BOEING737 7373B7 1384580NM CABIN FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19398US 23507 LAS - FLT 414 - EN ROUTE LAX TO MCI, CABIN PRESSURE BEGAN CLIMBING. DROPPED TO FL 290 AND CREW WAS ABLE TO CONTROL PRESSURE ON MANUAL. BOTH GENERATORS THEN DROPPED OFF LINE. CREW GOT THEM BAC ON LINE AND DIVERTED FLIGHT TO LAS WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. OPS CHECKED ENGINE GENERATORS, NO PROBLEMS NOTED. REFERENCE NR 95ZZZW420. 2L72 4F RTA16WE 19950414000491995041400049NM 1995 4 14 USAA950243 119950312A33501012623 EEL BOEING737 737301 1384611NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19353US 23556 DCA - LEFT SEAT EMERGENCY LIGHT ON ROW 10 INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY. (W) 2L72 4F RTA16WE 19950414000501995041400050WP 1995 4 14 USAA950244 119950316A3350 EEL BATTERY PACK DOUG DC9 DC931 3022065WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19967VJ 47375 PIT - FLT 0541 - THE COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950414000511995041400051WP 1995 4 14 USAA950245 119950316A3350 EEL WIRE DOUG DC9 DC931 3022065WP CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19932VJ 47189 CLT - THE FLOOR LEVEL LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE FIRST SEGMENT OF FLOOR TRACK LIGHTING. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950414000521995041400052NM 1995 4 14 USAA950246 119950315A5240311A106595 DOOR BOEING737 737301 1384611NM LT ENG PYLON MISSING A AUSAAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 EA19563AU 23551 TPA - FLT 60 - ON CLIMB-OUT FROM TPA, LEFT ENGINE PYLON PANEL CAME OFF. FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED PANEL ON CDL 54-20-1 AND RELEASED AIRCRAFT. REPLACED NACELLE STRUT ACCESS DOOR ON LEFT ENGINE PYLON. (W) 2L72 4F RTA16WE 19950414000531995041400053NM 1995 4 14 USAA950247 119950316A215039267831 FAN BOEING737 7374B7 1384702NM RIGHT FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19448US 24892 PIT - FLT 670 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. RIGHT PACK ON MEL AND LEFT PACK VERY WEAK. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT TURBO FAN VALVE AND FLOW CONTROL VALVE. REFERENCE 95ZZZW421. 2L72 4F RTA16WE 19950414000541995041400054NM 1995 4 14 USAA950248 119950317A5210 PIN BOEING737 7373B7 1384580NM PAX DOOR OUT OF POSITION A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19520AU 23706 PIT - FLT 1406 - FLIGHT EN ROUTE CMH TO TPA WHEN CREW REPORTED A PRESSURIZATION PROBLEM. AIR LEAK AND LOUD AIR NOISE HEARD FROM FORWARD ENTRY DOOR. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED HINGE PIN IN UPPER HINGE COVER. FOUND AFT OUTFLOW VALVE NOT COMPLETELY CLOSING. REPLACED OUTFLOW VALVE AND CONTROLLER. RESEALED INNER AREA AROUND EXTERNAL POWER RECEPTACLE. REFERENCE 95ZZZW422. 2L72 4F RTA16WE 19950414000551995041400055EU 1995 4 14 USAA950251 219950319A7260 DRIVE PAD BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENG LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19436US26080 24558 721203 PIT - FLT 1797 - FLIGHT EN ROUTE MCI TO LGA WITH NR 2 ENGINE OIL QUANTITY DECREASING. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE BAGGED DRAINS AND RAN ENGINE AT TAKEOFF POWER. NO LEAKS FOUND, NO OIL IN INLET OR TAILPIPE. FERRIED AIRCRAFT TO GSO. FOUND CSD DRIVE PAD LEAK. REPLACED ENGINE. (W) 2L72 4F4 FRTA16WE E21EU 19950414000571995041400057WP 1995 4 14 CAL950189 119950312A4950109382171 VALVE DOUG DC9 DC982 3022082WP APU INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916893117304061 49392 IAH - FLT 0126 - THE APU AUTO SHUT-DOWN DURING CLIMB-OUT AT 27,000 FEET. APU RESTART WAS UNSUCCESSFUL. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND APU LOAD CONTROL VALVE PARTIALLY OPEN DURING START AND UNDER NO LOAD. WHEN LOAD WAS APPLIED, APU FREQUENCY WOULD DROP OFF LINE. THE LOAD CONTROL VALVE WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. )X) 2L72 4F A6WE 19950414000581995041400058NM 1995 4 14 CAL950196 119950203A5753 WEB BOEING737 737130 1384435NM LT TE FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620363935 19020 31J - CORROSION WAS FOUND ON THE LT OUTBOARD MID-FLAP WEB AND DOUBLER AT THE FOREFLAP ATTACH POINT. THE CORRODED AREA WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-10-6, 51-40-6, 51-10-3, AND 57-52-00. (X) 2L72 4F A16WE 19950414000591995041400059NM 1995 4 14 CAL950197 119950203A5220 SKIN BOEING737 737130 1384435NM LT EMER EXIT DR.CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620363935 19020 31J - A 1 INCH CRACK WAS FOUND ON THE OUTER SKIN OF THE LEFT FORWARD EMERGENCY EXIT DOOR. THE CRACK WAS STOP DRILLED, ROUGH EDGES WERE BLENDED OUT, AND A REPAIR WAS INSTALLED IAW SRM 52-00-2. (X) 2L72 4F A16WE 19950414000601995041400060NM 1995 4 14 CAL950198 119950203A5315 FLOOR BEAM BOEING737 737130 1384435NM BS 716.0 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620363935 19020 31J - A 2 INCH CRACK WAS FOUND IN THE FLOOR BEAM AND RUNNING UNDER THE RADIUS AT BS 716.0 AND BL 0. A REPAIR WAS FABRICATD AND INSTALLED IAW SRM 53-10-9. (X) 2L72 4F A16WE 19950414000611995041400061NM 1995 4 14 CAL950199 119950203A5754 SLAT BOEING737 737130 1384435NM LT NR 3 LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620363935 19020 31J - INSPECTION FOUND A 1 INCH CRACK IN THE LEFT LEADING EDGE NR 3 SLAT NR 1 HINGE DOOR AREA. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-4, AND 51-30-2. (X) 2L72 4F A16WE 19950414000621995041400062WP 1995 4 14 CAL950200 119950316A3222 STRUT DOUG DC9 DC982 3022082WP NLG FLAT A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0972824 49824 IAH - FLT 0605 - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE LIGHT DID NOT EXTINGUISH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NLG STRUT FLAT. THE NOSE STRUT WAS REPACKED PER MM 32-21-02, PAGE 401 - PAGE 405. THE GEAR WAS SWUNG FOUR TIMES AND OPERATION CHECKED GOOD. (X) 2L72 4F A6WE 19950414000631995041400063NM 1995 4 14 CAL950201 119950315A5315 FLOOR BEAM BOEING737 737291 138448WNM FS 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND MAIN CABIN FLOOR BEAM CORRODED AT FS 1006 BETWEEN LBL 10 TO RBL 10. THE FLOORBEAM WAS REMOVED AND A NEW FLOOR BEAM WAS INSTALLED IAW SRM 53-10-9. (X) 2L72 4F A16WE 19950414000641995041400064NM 1995 4 14 CAL950202 119950315A5315 FLOOR BEAM BOEING737 737291 138448WNM BS 700-717 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A 0.80 INCH CRACK IN WEB AT FASTENERS ON FLOOR BEAM BETWEEN BS 700-BS 717, BBL 0. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950414000651995041400065NM 1995 4 14 CAL950203 119950315A5320 FLOOR SUPPORT BOEING737 737291 138448WNM FS 312-344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09102516808868088 20361 GSO - INSPECTION FOUND A MAIN CABIN FLOOR PANEL SUPPORT CORRODED AT FS 312 - FS 344, LBL 12. THE CORRODED SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950414000661995041400066NM 1995 4 14 CAL950204 119950204A5315 FLOOR BEAM BOEING737 737291 138448WNM FS 294.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND FLOOR BEAM UPPER T-ANGLE CORRODED AT FS 294.5 FROM LBL 25 TO RIGHT CUSP. THE FLOOR BEAM WAS REPAIRED IAW ECRA 5310-01102. (X) 2L72 4F A16WE 19950414000671995041400067NM 1995 4 14 CAL950205 119950315A5311 FRAME BOEING737 737291 138448WNM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A 0.70 INCH CRACK IN FRAME AT BS 500, STR 22L. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950414000681995041400068NM 1995 4 14 CAL950206 119950315A5315 FLOOR BEAM BOEING737 737291 138448WNM FS 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND FLOOR BEAM CORRODED FROM LEFT CUSP TO RIGHT CUSP AT FS 947. THE CORRODED AREAS WERE REMOVED IAW SRM 53-10-9 AND BLENDED IAW SRM 53-10-1. REPAIRS WERE INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950414000691995041400069NM 1995 4 14 CAL950207 119950315A5315 FLOOR BEAM BOEING737 737291 138448WNM FS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND AFT GIRT BAR ATTACH FITTING BRACKET AND FLOOR BEAM CORRODED AT FS 344. THE CORROSION WAS REMOVED AND REPAIR PARTS WERE FABRICATED IAW SRM 51-40-2 AND ECRA 5310C01102. A REPAIR WAS INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950414000701995041400070NM 1995 4 14 CAL950208 119950315A5313 STRINGER BOEING737 737291 138448WNM BS 500A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A .50 INCH CRACK FROM FASTENER HOLE IN STR 19L AT STA 500A. REPAIR DOUBLERS WERE FABRICATED IAW SRM 53-10-3 AND INSTALLED IAW SRM 51-30-2 AND SRM 51-30-0. (X) 2L72 4F A16WE 19950414000711995041400071NM 1995 4 14 CAL950209 119950315A5311 FRAME BOEING737 737291 138448WNM BS 500B CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 500B, STR 22L. THE CRACKED FRAME WAS REMOVED AND REPLACED WITH REPAIR KIT IAW BOEING DRAWING 65C25113. (X) 2L72 4F A16WE 19950414000721995041400072NM 1995 4 14 CAL950210 119950315A5712 LE RIB BOEING737 737291 138448WNM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A 1.2 INCH CRACK IN RT WING LEADING EDGE RIB, JUST OUTBOARD OF NR 5 SLAT ACTUATOR. THE CRACKED SECTION WAS REMOVED IAW SRM 51-30-2 AND A REPAIR WAS INSTALLED IAW SRM 51-20-4 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950414000731995041400073NM 1995 4 14 CAL950211 119950315A5754 SLAT BOEING737 737291 138448WNM NR 2 LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A 1.1 INCH CRACK IN THE NR 2 SLAT INBOARD AUXILIARY TRACK CUT-OUT. THE CRACKED AREA WAS REMOVED IAW SRM 57-30-4 AND REPAIR FILLER AND DOUBLER WITH SOLID FASTENERS WERE INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19950414000741995041400074NM 1995 4 14 CAL950212 119950315A5230 DOOR BOEING737 737291 138448WNM AFT CARGO CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091025168088 20361 GSO - INSPECTION FOUND A 1.2 INCH CRACK IN AFT CARGO DOOR ON THE INSIDE RIGHT CORNER UNDER DOUBLER. THE CRACK WAS REPAIRED BY FABRICATING AND INSTALLING DOUBLER AND FILLER IAW SRM 51-40-3. (X) 2L72 4F A16WE 19950414000751995041400075WP 1995 4 14 CAL950216 119950319A3350 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0969803 49229 IAH - FLT 0138 - INSPECTION FOUND EMERGENCY EXIT LIGHTS SWITCH ON, RESULTING IN DEAD BATTERIES. THE BATTERIES FOR ALL INTERIOR EMERGENCY LIGHTS WERE REPLACED AND OPERATION CHECKED GOOD. (X) 2L72 4F A6WE 19950414000761995041400076WP 1995 4 14 CAL950217 119950319A3260833703 PROX SWITCH DOUG DC9 DC982 3022082WP RT MLG INOPERATIVE A CALAO OTHER N FALSE WARNING LDLANDING 1 SW0913891 49102 TPA - FLT 0365 - THE RT MLG RED UNSAFE LIGHT ILLUMINATED INTERMITTENTLY WITH THE GEAR HANDLE IN THE DOWN POSITION WHEN APPROACHING TPA. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE RED LIGHT CAME ON CONTINUOUSLY UPON LANDING, AND WAS ACCOMPANIED BY CAWS LANDING GEAR ANNUNCIATION. THE AIRCRAFT TAXIED TO THE GATE NORMALLY. MAINTENANCE FOUND RT MLG DOWNLOCK PROXIMITY SWITCH AT FAULT. THE PROXIMITY SWITCH WAS REMOVED AND REPLACED. THE PROXIMITY SWITCH TESTED GOOD. (X) 2L72 4F A6WE 19950414001231995041400123WP 1995 4 14 95ZZZX1723 119950314A322259104475045 STRUT DOUG DC9 DC981 3022081WP NOSE GEAR DEFLATED A A4JAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15817SJ 48051 FLL - FLT 307 - ON TAKEOFF, UNABLE TO GET NOSE GEAR UP INDICATION. NOSE GEAR DOOR APPEARED TO STAY DOWN OR IN TRANSIT. CYCLED GEAR DOWN, ALL INDICATIONS NORMAL. RAISED GEAR AGAIN AND HAD SAME UNSAFE INDICATION. AIRCRAFT MADE UNEVENTFUL LANDING AT FLL. INSPECTED NOSE GEAR AND FOUND STRUT DEFLATED. NO OTHER DAMAGE FOUND. SERVICED NOSE STRUT AND AIRCRAFT MADE MAINTENANCE FERRY FLIGHT TO MIA. NOSE STRUT OKAY AT MIA. FOUND NOSE UPLOCK SWITCH BAD. REPLACED SWITCH. LANDING GEAR RETRACTION TEST GOOD. CYCLES, 5,911. 2L72 4F A6WE 19950414001241995041400124WP 1995 4 14 95ZZZX1724 119950314A3260833702 UPLOCK SWITCH DOUG DC9 DC981 3022081WP NOSE GEAR INOPERATIVE A A4JAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO15817SJ 48051 FLL - FLT 307 - ON TAKEOFF, UNABLE TO GET NOSE GEAR UP INDICATION. NOSE GEAR DOOR APPEARED TO STAY DOWN OR IN TRANSIT. CYCLED GEAR DOWN, ALL INDICATIONS NORMAL. RAISED GEAR AGAIN AND HAD SAME UNSAFE INDICATION. AIRCRAFT MADE UNEVENTFUL LANDING AT FLL. INSPECTED NOSE GEAR AND FOUND STRUT DEFLATED. NO OTHER DAMAGE FOUND. SERVICED NOSE STRUT AND AIRCRAFT MADE MAINTENANCE FERRY FLIGHT TO MIA. NOSE STRUT OKAY AT MIA. FOUND NOSE UPLOCK SWITCH BAD. REPLACED SWITCH. LANDING GEAR RETRACTION TEST GOOD. CYCLES, 5,911. 2L72 4F A6WE 19950414001251995041400125NE 1995 4 14 95ZZZX1725 319950313A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE LEFT PROPELLER MISSING A AJJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01844CA176 UE45 HJ75 DE-ICE BOOTS NOT MAINTAINING BOND TO PROPELLER BLADES. TWO DE-ICE BOOTS DISCOVERED MISSING FROM SAME PROPELLER ON TWO DIFFERENT OCCASIONS. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INVESTIGATION, IT IS APPARENT THE PROBLEM LIES WITH THE PAINT THAT IS APPLIED PRIOR TO BOOT INSTALLATION. 2L72 4T RTA24CE 5 CP10NE 19950414001261995041400126NM 1995 4 14 95ZZZX1726 119950318A5230AE7271025100 DOOR MECH BOEING727 72721 1384003NM MAIN CARGO DOOR UNLATCHED A RYNAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE07356QS 19258 MAIN CARGO DOOR LIGHT CAME ON IN-FLIGHT; UNSCHEDULED LANDING MADE IN MEMPHIS. NR 4 MCD PIN BACKED OUT SLIGHTLY TO WHERE SWITCH WAS NOT ENGAGED. PERFORMED OPERATIONAL CHECK OF MAIN CARGO DOOR SIX TIMES; COULD NOT DUPLICATE PROBLEM. ALSO, CLOSED DOOR AND PRESSURIZED AIRCRAFT; OPS/SYS CHECKED NORMAL. 2L73 4F A3WE 19950414001281995041400128CE 1995 4 14 95ZZZX1728 119950223A575335165050259 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0780ZR 10951 UC80 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT OUTBOARD FLAP, PN 35165050259, REVEALED A CRACK IN THE UPPER SKIN APPROXIMATELY 3 INCHES OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A 1.5 INCH BY 6 INCH DOUBLER. 2L72 4T RTA24CE 19950414001291995041400129WP 1995 4 14 95ZZZX1729 119950326A3230 BYPASS VALVE DOUG DC9 DC982 3022082WP LANDING GEAR OUT OF POSITION A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05954U 49426 JFK - FLT 253 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT AND LANDING GEAR UNSAFE LIGHTS ILLUMINATED. PLACED LANDING GEAR SELECTOR TO DOWN AND ALL DOWN, AND LOCKED INDICATION ILLUMINATED. VERIFIED LANDING GEAR DOWN. FOUND LANDING GEAR BYPASS VALVE IN THE BYPASS POSITION. STOWED AND LATCHED LANDING GEAR BYPASS VALVE. GROUND CHECKS OF LANDING GEAR CHECKED NORMAL. CHECK C-1D - 11-14-94 - MCI. 2L72 4F A6WE 19950414001301995041400130WP 1995 4 14 95ZZZX1730 119950210A5330 SKIN DOUG DC9 DC931 3022065WP BS 68.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05983Z 47411 STL - DURING CHECK-C, FOUND A .50 INCH AND A .25 INCH LONG SKIN CRACK AT TWO FASTENERS, STA 68.5. REPAIRED PER ARA 8823, USING SRO 9530239. AIRCRAFT TOTAL TIME: 60,099 HOURS; 71,912 CYCLES. 2L72 4F A6WE 19950414001311995041400131WP 1995 4 14 CAL950179 119950305A3260 PROX SENSORS DOUG DC9 DC982 3022082WP MLG DOORS INOPERATIVE A CALAO OTHER N FALSE WARNING DEDESCENT 1 SW0969803 49229 CLE - FLT 1718 - MAIN LANDING GEAR DOORS WOULD NOT RETRACT AFTER GEAR EXTENDED FOR LANDING AT CLE. THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND CREW CONFIRMED THE DOORS WERE DOWN BY A VISUAL CHECK THROUGH THE VIEW PORTS. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITH GEAR DOORS DOWN. MAINTENANCE FOUND LT MLG DOOR DAMAGED. THE LT MLG DOOR WAS REMOVED AND REPLACED. BOTH MLG DOOR PROXIMITY SENSORS WERE REMOVED AND REPLACED. GEAR INDICATIONS AND OPERATION CHECKED GOOD. (X) 2L72 4F A6WE 19950414001321995041400132WP 1995 4 14 CAL950180 119950306A3222 STRUT DOUG DC9 DC982 3022082WP NLG LOW PRESSURE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0972824 49824 CLE - FLT 0752 - NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING TPA. THE GEAR WAS CYCLED, BUT HAD NO EFFECT ON LIGHT. THE RED LIGHT EXTINGUISHED APPROXIMATELY 15 MINUTES LATER WHILE PASSING THROUGH 28,000 FEET. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND NLG STRUT PRESSURE LOW. THE STRUT SERVICED TO THE PROPER PRESSURE AND X-DIMENSION PER MM 32-21-02. THE NOSE GEAR WAS SWUNG 5 TIMES AND ALL INDICATIONS NORMAL. NO OTHER DEFECTS NOTED. (X) 2L72 4F A6WE 19950414001331995041400133WP 1995 4 14 CAL950187 119950309A783041000740104 T/R CNTL VALVE DOUG DC9 DC982 3022082WP LT ENGINE RUPTURED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW093583626430 49441 SFO - FLT 0165 - THE MAIN CABIN BEGAN TO FILL WITH SMOKE DURING TAXI TO TERMINAL AFTER LANDING AT SFO. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY, THE L-1 DOOR AND TAIL CONE EMERGENCY SLIDES WERE DEPLOYED, AND THE PASSENGERS EVACUATED AS A PRECAUTIONARY MEASURE. MAINTENANCE FOUND LT THRUST REVERSER CONTROL VALVE RUPTURED. THIS PERMITTED HYDRAULIC LEAKAGE INTO THE APU AIR INLET RESULTING IN SMOKE. LT THRUST REVERSER CONTROL VALVE REMOVED AND REPLACED, OPERATIONAL AND LEAK CHECKS GOOD. BOTH L-1 DOOR AND TAIL CONE SLIDES REMOVED AND REPLACED AND TAIL CONE RESINSTALLED. ENGINES RUN TO PURGE SYSTEM OF FUMES. THE COALESCER BAGS WERE REPLACED. (X) 2L72 4F A6WE 19950414001341995041400134NE 1995 4 14 CAL950213 219950318A7250 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE 3RD STG TURBINE FAILED A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW09809NY328864389 49263 708465 MIA - FLT 0292 - A LOUD BANG WAS HEARD AND THE NR 1 ENGINE SPOOLED DOWN DURING A CLIMB OUT OF MIA AT 18,000 FEET. THE AIRCRAFT WAS RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO FAIILURE OF A THIRD STAGE TURBINE BLADE. (X) 2L72 4F4 F A6WE E9NE 19950414001351995041400135WP 1995 4 14 CAL950214 119950318A29107936907615 HYD LINE DOUG DC9 DC982 3022082WP LT PYLON RUPTURED A CALAOH OTHER DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0918835 49439 IAH - FLT 0459 - LT HYDRAULIC SYSTEM PRESSURE AND QUANTITY BEGAN TO DECREASE IN-FLIGHT. THE LT ENGINE HYDRAULIC PUMP WAS TURNED OFF AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE FROM LT PYLON FITTING TO ENGINE CASE DRAIN FILTER RUPTURED. THE HYDRAULIC LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACE FLEX LINE WITH A RIGID LINE WITHIN 1200 HOURS OR 500 FLIGHTS, WHICHEVER COMES FIRST. (X) 2L72 4F A6WE 19950414001361995041400136EU 1995 4 14 CAL950221 119950318A2912 O-RING AIRBUS300 A300B4103 3930104EU HYD FILTER LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0911984 108 EWR - FLT 0750 - THE GREEN SYSTEM HYDRAULIC FLUID DECREASED INTO THE YELLOW ARC ABOUT 2 HOURS AFTER TAKEOFF. TURNING BOTH ENGINE DRIVEN PUMPS TO 'DUMP' STOPPED THE DECREASE, BUT THE DECREASE STARTED AGAIN WITH EITHER PUMP RUNNING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND GREEN SERVO CONTROL ELECTRIC HYDRAULIC SELECTOR FILTER LEAKING. A NEW O-RING AND BACK-UP RING WERE INSTALLED ON THE BOWL AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A35EU 19950414001371995041400137NM 1995 4 14 CAL950224 119950321A2910 HYD COUPLING BOEING727 727232 1384082NM B-HYD SYS BROKEN A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09519PE 20642 IAH - FLT 0650 - BOTH B-HYDRAULIC SYSTEM PUMP LOW PRESSURE LIGHTS ILLUMINATED WITH A DROP IN HYDRAULIC QUANTITY WHILE IN-FLIGHT TO IAH. HYDRAULIC QUANTITY LOSS CHECK LIST WAS COMPLIED WITH AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND QUICK DISCONNECT COUPLING BROKEN AT THE B-SYSTEM RESERVOIR. THE QUICK DISCONNECT COUPLING WAS REMOVED AND REPLACED. BOTH B-SYSTEM HYDRAULIC PUMPS WERE RUN AND THE FLIGHT CONTROLS WERE OPERATED WITH ALL OPERATIONS CHECKING GOOD. (X) 2L73 4F A3WE 19950414001381995041400138NM 1995 4 14 CAL950226 119950320A52806521636185 DOOR HINGE BOEING727 727243 138408DNM LT MLG BROKEN A CALAK NONE O OTHER LDLANDING 1 SW095841416102 22166 EWR - FLT 0614 - SMOKE WAS SEEN COMING FROM LT MLG UPON LANDING AT IAH. AIRCRAFT WAS STOPPED ON THE TAXIWAY. MAINTENANCE FOUND LT MLG FLYING DOOR HINGE BROKEN AND DOOR WAS LAYING ON THE TIRE WHICH CAUSED THE SMOKE. THE DOOR WAS FOUND DAMAGED DUE TO THE IMPACT WITH THE TIRE. THE DOOR WAS REPAIRED IAW SRM 51-00, AND SRM 52-80-2, FIGURE 2. (X) 2L73 4F RTA3WE 19950414001391995041400139SW 1995 4 14 LOSA9510 119950207A27977710125 CONNECTOR FRCHLDSA227 SA227CC SW STABILIZER TRIM LOOSE A LOSAO OTHER H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 WP233022R CC841B FAT - CREW REPORTED COPILOT AND AUXILIARY STABILIZER TRIMS INOPERATIVE. MAINTENANCE FOUND LOOSE WIRE AT CIRCUIT BREAKER. SECURED WIRE AND OPERATIONAL CHECKS NORMAL. AIRCRAFT RELEASED FOR FLIGHT. (X) 2L72 4T RTA18SW 19950414001401995041400140WP 1995 4 14 ORJA9523 119950322A32303937060501 BOLT DOUG DC9 DC982 3022082WP LT MLG BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11821RA9339 49931 FOUND LT MLG RETRACT CYLINDER LOWER ATTACH LINK BOLT BROKEN. OUTBOARD BOLT WAS OKAY DURING PREFLIGHT CHECK. REPLACED LOWER RETRACTION LINK BOLT PER MM 32-00-00 LEFT GEAR. (X) 2L72 4F A6WE 19950414001411995041400141EU 1995 4 14 PAYA95A4014 119950313A2120 AIR DIST AEROSPATR42 ATR42300 8680920EU COCKPIT SMOKE A PAYAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA174211G 178 CREW REPORTED SMOKE SMELL IN COCKPIT WITH ELECTRICAL SMOKE CAP LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND THEN RAN AIRCRAFT FOR 30 MINUTES WITH NO DEFECTS NOTED. (X) 2H72 4T RTA53EU 19950414001421995041400142NM 1995 4 14 TSAA9529052 119950317A2932 HYD PRESS TRANS BOEING737 737297 1384480NM 'A' HYD SYSTEM FAILED A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13726AL 22426 HNL/LIH - FLT 404 - DURING CLIMB, PILOT REPORTED LOSS OF HYDRAULIC PRESSURE. WHEN AIRCRAFT WAS CONFIGURED FOR LANDING (GEAR EXTENDED), HYDRAULIC PRESSURE RETURNED TO NORMAL. AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 'A' SYSTEM HYDRAULIC PRESSURE INDICATOR. AIRCRAFT RETURNED TO SERVICE. DURING SUBSEQUENT FLIGHT IN CLIMB, THE PROBLEM REPEATED ITSELF; HOWEVER, THE PRESSURE DID NOT RETURN TO NORMAL AFTER GEAR EXTENSION. AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 'A' SYSTEM HYDRAULIC PRESSURE TRANSMITTER. LEAK AND OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950414001431995041400143NM 1995 4 14 TSAA9553053 119950322A5330 SKIN BOEING737 737297 1384480NM BS 217-243 DAMAGED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 FUSELAGE SECTION 41, EXTERIOR SKIN DAMAGED BY GROUND EQUIPMENT CONTACT FROM BS 217 - BS 243, 6 INCHES ABOVE SKIN LAP AT STR 24L. REPAIRED PER ECO 2569. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 33859:51, CYCLES, 63606. (X) 2L72 4F A16WE 19950414001441995041400144NM 1995 4 14 TSAA9580051 119950308A801297907071 STARTER VALVE BOEING737 737297 1384480NM NR 2 ENGINE OPEN A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP1370724 21740 KOA/HNL - FLT 81 - PILOT REPORTED NR 2 'START VALVE OPEN' LIGHT CAME ON IN-FLIGHT. LIGHT WENT OUT WHEN POWER RETARDED. PRECAUTIONARY LANDING MADE IN KOA. REPLACED STARTER SHUT-OFF VALVE. ALSO, REPLACED STARTER, START SWITCH, AND STARTER SPLINE AS PRECAUTIONARY. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950414001451995041400145EU 1995 4 14 VTZA95116 119950327A523091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27310UE 41028 IAD/CHS - FLT 6366 - DURING TAKEOFF ROLL AT 1710 HOURS ON 3-27-95, ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATING. IAD OPENED DMI NR 03333 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. IAD MAINTENANCE LATER CLEARED DMI NR 03333 BY CLEANING AND LUBING THE BAGGAGE DOOR MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950414001461995041400146 1995 4 14 VTZA95117 419950327A3418C771065 STALL WARNING BAG JETSTMJETSTM3201 1500217EU COCKPIT OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27489UE 908 IAD/CRW - FLT 6378 - DURING CLIMB-OUT AT 1830 HRS ON 3-27-95, THE STICK SHAKER ACTIVATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE STALL SIGNAL SUMMING UNITS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950414001471995041400147EU 1995 4 14 VTZA95118 119950324A5270T411AE1002C TIME DELAY RELAY JETAIRJETSTMJETSTM4101 1500501EU COCKPIT OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27315UE 41033 IAD/ORF - FLT 6534 - DURING TAKEOFF AT 2200 HRS ON 3-24-95, ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING ILLUMINATION ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RESET CIRCUIT BREAKER FOR TIME DELAY RELAY. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950414001481995041400148EU 1995 4 14 VTZA95119 119950323A3150 WARNING JETAIRJETSTMJETSTM4101 1500501EU COCKPIT SOUNDED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27312UE 41025 IAD/BOS - FLT 6508 - DURING TAKEOFF AT 1620 HRS ON 3-23-95, ABORTED TAKEOFF DUE TO CONFIGURATION WARNING SOUNDING DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950414001491995041400149NM 1995 4 14 9505432771 119950404A5347 SEAT TRACK BOEING727 7272M7 138407SNM FS 383 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01742RW 21952 DURING PERIODIC CHECK, MAINTENANCE FOUND SEAT TRACK AT FS 383, RBL 24 CORRODED ON OUTBOARD SIDE. REPAIRED PER SRM 53-10-5 FIG 9 AND NWA EA 27-96518. 2L73 4F A3WE 19950414001501995041400150 1995 4 14 9505442768 419950408A3416A4016910021 ALTIMETER BOEING727 7272M7 138407SNM FLIGHT DECK FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01728RW127252508 21741 DURING DEPARTURE CLIMB, CAPTAIN'S AIRSPEED, ALTIMETER AND STANDBY ALTIMETER WERE UNRELIABLE. FLIGHT DIVERTED TO DLH WITHOUT FURTHER INCIDENT. MAINTENANCE FERRIED AIRCRAFT TO MSP FOR REPAIR. MAINTENANCE FOUND A LEAK IN CAPTAIN'S STATIC SYSTEM AT STANDBY ALTIMETER. REPLACED THE STANDBY ALTIMETER AND DAMAGED FITTING. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950414001511995041400151NM 1995 4 14 9505455523 119950407A25301238 OVEN BOEING757 757251 1384970NM AFT GALLEY MALFUNCTIONED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL01523US 23617 ON TAKEOFF, THE FLIGHT ATTENDANT REPORTED SMOKE FROM THE AFT GALLEY CENTER OVEN. AIRCRAFT RETURNED TO MSP, NO EMERGENCY WAS DECLARED. CHECKED FOR EVIDENCE OF FOOD OR PAPER, NONE FOUND. PULLED AND COLLARED OVEN CIRCUIT BREAKERS. REPLACED OVEN IN DCA, OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA2NM 19950414001521995041400152NM 1995 4 14 9505466625 119950409A7603 CONTROL CABLE 250671 BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE DISCONNECTED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01625US 51085 21070 702173 DURING TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. THE CONTROL CABLE IN THE PYLON WAS FOUND TO HAVE DISCONNECTED AT THE PYLON DRUM. THE CABLE BOX IN THE PYLON WAS REPLACED AND THE SYSTEM OPERATION CHECKED OK. 2L74 4F4 F A20WE E3NE 19950414001531995041400153NM 1995 4 14 9505475517 119950406A5315141N29321 FLOORBEAM BOEING757 757251 1384970NM FS 324 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 28357 23205 DURING PERIODIC CHECK, THE FS 324 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION AT LBL 15, WL 208. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-97821. 2L72 4F RTA2NM 19950414001541995041400154NM 1995 4 14 9505485517 119950406A5315141N5111 FLOORBEAM BOEING757 757251 1384970NM FS 345 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 28357 23205 DURING PERIODIC CHECK, THE FS 345 FLOORBEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-97822. 2L72 4F RTA2NM 19950414001551995041400155 1995 4 14 COM11853 419950409A3420 WIRES EMB 120 EMB120RT SO FLUX DETECTOR LOOSE A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01264CA 120256 CAPTAIN HSI INDICATING 180 DEGREE ERROR IN HEADING WITH RED HDG INDICATION FIRST OFFICER RMI HAS RED FLAG. FOUND WIRES LOOSE FROM LEFT FLUX DETECTOR WIRING HARNESS AT LEFT WINGTIP. RESET PINS, OPERATIONAL CHECKED OF LEFT HEADING SYSTEM GOOD. 2L72 4T RTA31SO 19950414001561995041400156SO 1995 4 14 COM11854 119950407A32332060500005 ACTUATOR EMB 120 EMB120RT SO NLG LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01265CA938 120257 HYDRAULIC FLUID LEAKING FROM NOSE GEAR WHEEL WELL. FOUND NOSE GEAR ACTUATOR LEAKING. REMOVED AND REPLACED ACTUATOR WITH SERVICEABLE UNIT. 2L72 4T RTA31SO 19950414001571995041400157SO 1995 4 14 COM11855 119950410A5730 SKIN SUPPORTS EMB 120 EMB120RT SO WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01246CA1089010890 120223 THE FOLLOWING PART NUMBER WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASKS 5720-551/651-01I AND 5720-552/652-01I. THE CRACKED WING SKIN SUPPORTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NUMBER 1327-2. RIB SKIN SUPPORT PART NUMBERS 3 EA, 120-04350-017, 1 EA, 120-04352-017, 1 EA, 120-04356-007. 2L72 4T RTA31SO 19950414001581995041400158 1995 4 14 COM20360 419950408A341880032417 ANN PANEL SWRNGNSA227 SA227AC 8780603SW COCKPIT MALFUNCTIONED A COMAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO01458AM11729 AC699 SAS FAULT LIGHT FLICKERED IN FLIGHT. DISABLED SYSTEM PER CHECKLIST. REMOVED AND REPLACED MASTER ANNUNCIATOR PANEL WITH SERVICEABLE UNIT. 1L72 4T A8SW 19950414001591995041400159EU 1995 4 14 COM31056 119950406A324650092371 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN CAP A COMAK NONE O OTHER ININSP/MAINT 1 SO01340SF17606391 340A014 MECHANIC REMOVED WHEEL ASSEMBLY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR BUSHING REPAIR. 2L72 4T RTA52EU 19950414001601995041400160EU 1995 4 14 COM31057 119950409A2420 WIRE SAAB SF340 SF340A 7850100EU RIGHT SHORTED A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01359CA 340A053 RIGHT A/C GENERATOR AND RIGHT INTAKE HEAT FAIL LIGHTS ILLUMINATED. FOUND WIRE SHORTED IN RIGHT WING FLAP COVE, REPAIRED WIRE. 2L72 4T RTA52EU 19950414001611995041400161 1995 4 14 COM60450 419950409A3140864806 PSEU CNDAIRCL600 CL6002B19 EA AVIONICS RACK SHORTED A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01927CA2325 7031 EICAS MESSAGES WOW OUTPUT, WOW INPUT AND STALL FAIL. REMOVED AND REPLACED PSEU WITH SERVICEABLE UNIT. 2L72 4F RTA21EA 19950414001621995041400162NM 1995 4 14 DL72S951398 119950130A5753652163261X SKIN BOEING727 727232 1384082NM NR 2 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 THE NR 2 MID FLAP DURING HMV SHOP INSP, WAS FOUND TO HAVE A CRACKED COVE SKIN AT THE I/B DRIVE ROD CUT OUT. THIS CRACK WAS REPIRED PER MM 57-52-0 PG 819. 2L73 4F A3WE 19950414001631995041400163NM 1995 4 14 DL72S951399 119950130A5753652163261X SPAR RAIL BOEING727 727232 1384082NM NR 2 TE MID FLAPCARCKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 THE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND THAT THE AFT LOWER RAIL HAS TWO CRACKS I/B AFT FLAP DRIVE CUTOUT. THIS CRACKS WERE REPAIRDED PER MM 57-52-0 PG 807. 2L73 4F A3WE 19950414001641995041400164NM 1995 4 14 DL72S951400 119950130A5753652163261X SPAR RAIL BOEING727 727232 1384082NM NR 2 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 THE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND TO HAVE AN CRACKED AFT LOWER RAIL AT I/B AFT FLAP TRACK O/B CORNER. CRACK WAS REPAIRED PER MM 57-52-0 PG 807. 2L73 4F A3WE 19950414001651995041400165NM 1995 4 14 DL72S951401 119950130A5753652163261X SPAR RAIL BOEING727 727232 1384082NM NR 2 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 THE NR 2 MID FLAP DURING HMV TO SHOP, WAS FOUND TO HAVE A CRACKED AFT SPAR RAIL 41 INCHES FROM O/B END OF FLAP. CRACK WAS REPAIRED PER MM 57-52-0 PG 807. 2L73 4F A3WE 19950414001661995041400166NM 1995 4 14 DL72S951407 119950404A57546516221100 RIB BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 RIB NR 18 CRACKED NEXT TO NUTPLATE. INSTALLED DOUBLER PER MM 57-54-0 FIGURE 805. DURING SHOP INSPECTION OF RT WING NR 5 L/E SLAT. 2L73 4F A3WE 19950414001671995041400167NM 1995 4 14 DL72S951411 119950405A2780 ACTUATOR SUPPORT BOEING727 727232 1384082NM NR 1 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11477DA 20754 ACTUATOR SUPPORT BOX CRACKED I/B AND O/B SIDES AT NR 1 L/E FLAP. FOUND AT D-1 LTR CK. REPAIRED PER MM 57-20-21 PG 811. 2L73 4F A3WE 19950414001681995041400168NM 1995 4 14 DL72S951412 119950405A2760 ACTUATOR ANGLE BOEING727 727232 1384082NM NR 13 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11477DA 20754 THE NR 13 SPOILER OUTBD ACT ATTACH ANGLE CRACKED. FOUND AT D-1 LTR CK. INSTALLED TIME LIMITED REPAIR PER SRM 57-50-6 PG 57 TO 60. 2L73 4F A3WE 19950414001691995041400169NM 1995 4 14 DL72S951413 119950405A5754 RIB BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11477DA 20754 FOUND DURING D-1 LETTER CHECK, NR 5 O/B RIB FOR ACTUATOR ROD END CRACKED. REPAIRED PER MM 57-54-0 PG 3, FOR RT WING NR 5 L/E SLAT. 2L73 4F A3WE 19950414001701995041400170NM 1995 4 14 DL72S951421 119950311A5754 SKIN 651622295 BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA BN1001 21702 2540 THE NR 3 SLAT 727, FWD EDGE OF SKIN CRACKED AT NUTPLATES ON RIB 9 AND 10. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION. 2L73 4F A3WE 19950414001711995041400171NM 1995 4 14 DL72S951422 119950311A5754 SKIN 65162295 BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA BN1001 21702 2540 THE NR 3 SLAT 727, AFT LWR SKIN CRACKED 5 INCHES FROM O/B END. REPAIRED PER MM 57-54-0 FIG 801, DURING SHOP INSPECTION. 2L73 4F A3WE 19950414001721995041400172NM 1995 4 14 DL72S951423 119950407A5754 ANGLE BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 THE NR 8 L/E SLAT LWR FWD SKIN ATTACH ANGLE CRACKED AT ANTI-ICE AIR DUCT CUTOUT. REPAIRED PER SRM 57-54-0. FOUND DURING D-2 LTR CK TPAMM 4/6/95. 2L73 4F A3WE 19950414001731995041400173NM 1995 4 14 DL72S951424 119950406A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 A .25 INCH CRACK IN FUSELAGE SKIN JUST AFT OF R-3 WINDOW. FOUND AT D-2 LETTER CHECK. REPAIRED PER SRM 53-30-3 FIG 8. 2L73 4F A3WE 19950414001741995041400174NM 1995 4 14 DL72S951425 119950406A2780 ACTUATOR BRACKET BOEING727 727232 1384082NM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 A 2.5 INCH CRACK AT NR 1 SLAT ACTUATOR CASTING MOUNT BRACKET I/B SIDE. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-20-21 PG 812. 2L73 4F A3WE 19950414001751995041400175NM 1995 4 14 DL72S951426 119950406A5414 SKIN BOEING727 727232 1384082NM PANEL 9523 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 A .25 INCH CRACK AT PNL NR 9523 LT SIDE OF VERT STAB. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 54-30-0 PG 804. 2L73 4F A3WE 19950414001761995041400176NM 1995 4 14 DL72S951427 119950406A2780 BRACKET BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 A .375 INCH CRACK NR 3 L/E FLAP ACT I/B ATTACH ANGLE. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-20-21 PG 811. 2L73 4F A3WE 19950414001771995041400177NM 1995 4 14 DL72S951431 119950214A5753652163262 FITTING BOEING727 727232 1384082NM NR 3 MID FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT SHOP INSPECTION, NR 3 MID FLAP CARRIAGE SUPPORT FITTING INBOARD THRUST BEARING RETAINER BOLT HOLES ARE CORRODED. REAMED HOLE TO .312 TO REMOVE CORROSION HFEC, TREATED AND BUSH PER SRM 57-50-4. 2L73 4F A3WE 19950414001781995041400178NM 1995 4 14 DL72S951432 119950214A5753652163262 ANGLE BOEING727 727232 1384082NM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT SHOP INSPECTION, NR 3 MID FLAP WAS FOUND WITH CHORD ANGLE CRACKED AT I/B AFT FLAP TRACK CUTOUT. REPLACED CHORD PER SRM 57-52-0. 2L73 4F A3WE 19950414001791995041400179NM 1995 4 14 DL72S951433 119950214A5753652163262 ANGLE BOEING727 727232 1384082NM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 CHORD ANGLE REPAIR CRACKED AT I/B PUSH ROD CUTOUT NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0. 2L73 4F A3WE 19950414001801995041400180NM 1995 4 14 DL72S951434 119950214A5753652163262 SPAR BOEING727 727232 1384082NM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 BOTTOM REAR SPAR CHORD CRACKED 54 INCHES FROM I/B END OF NR 3 MID FLAP. REPLACED CHORD PER MM 57-52-0. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950414001811995041400181NM 1995 4 14 DL72S951435 119950214A5753652163262 REAR SPAR BOEING727 727232 1384082NM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 AT SHOP INSP, NR 3 MID FLAP WAS FOUND WITH BOTTOM REAR SPAR CRACKED AT 40 INCHES FROM I/B END. REPAIRED PER MM 57-52-0 PG 807. 2L73 4F A3WE 19950414001821995041400182NM 1995 4 14 DL72S951441 119950401A5347 SEAT TRACK BOEING727 727232 1384082NM BS 1070-1115 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, CORROSION AT O/B GALLEY ATTACH TRACK LBL 56 BETWEEN STA 1070 AND STA 1115. REPLACED SEAT TRACK FROM STA 1070 TO STA 1110 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950414001831995041400183NM 1995 4 14 DL72S951442 119950331A5347 SEAT TRACK BOEING727 727232 1384082NM BS 344-480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, CORROSION ON RT CENTER SEAT TRACK STA 344 TO 480. CLEANED TREATED AND PAINTED FROM STA 460 TO 480 PER SRM 53-10-1, FROM STA 344 TO 460 REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950414001841995041400184NM 1995 4 14 DL72S951443 119950331A5347 SEAT TRACK BOEING727 727232 1384082NM BS 380-480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, CORROSION ON RT INBD SEAT TRACK STA 380 TO 480. REPLACED SEAT TRACK SECTION PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950414001851995041400185NM 1995 4 14 DL72S951444 119950403A5330 SKIN BOEING727 727232 1384082NM BS 480-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, CORROSION ON SKIN BETWEEN STA 480 AND 500 AT BL 0. REPAIRED PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 19950414001861995041400186NM 1995 4 14 DL72S951445 119950402A5313 STRINGER BOEING727 727232 1384082NM BS 1030-1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STR 27L STA 1030 TO STA 1050. REPAIRED PER ERA 301506-14 CODE 4-53-14. 2L73 4F A3WE 19950414001871995041400187NM 1995 4 14 DL72S951446 119950331A5754 ANGLE BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 NR 8 SLAT ANGLE CRACKED UNDER TELESCOPING TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19950414001881995041400188NM 1995 4 14 DL72S951452 119950407A2782269002914 ACTUATOR BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11419DA 21272 ON APPROACH, LOST SYSTEM A HYDRAULICS. LANDED ATL AND FOUND NR 7 SLAT ACTUATOR CRACKED. REPLACED ACTUATOR, OPERATION NORMAL. 2L73 4F A3WE 19950414001891995041400189NM 1995 4 14 DL72W951403 119950330A5311 FRAME BOEING727 727247 138408FNM BS 913.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 DURING HMV, THE LT MLG UPLOCK ASSEMBLY ATTACH FRAME IN LT WHEEL WELL FS 913.5 HAD TIME LIMITED REPAIR. REPLACED WITH PERMANENT REPAIR PER MM 53-11-0 PG 814. 2L73 4F A3WE 19950414001901995041400190NM 1995 4 14 DL72W951406 119950401A5330 SKIN BOEING727 727247 138408FNM BS 1100 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 FUSELAGE SKIN CRACKED 1 INCH BOTH SIDES OF C/L AT STA 1100. CUT OUT DAMAGE PER SRM 53-30-3. INSP OF DAMAGED AREA STA 1100 LT AND RT SHOWED CRACKS REMOVED. INSTALLED REPAIR PER SRM 53-30-3. FOUND AT HMV. 2L73 4F A3WE 19950414001911995041400191NM 1995 4 14 DL72W951440 119950313A5753652163261X ANGLE BOEING727 727247 138408FNM NR 2 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 THE NR 2 MID FLAP WAS FOUND TO HAVE THE ATTACH ANGLE AT I/B AFT FLAP TRACK CUTOUT CRACKED. THIS DAMAGED WAS REPAIRED PER MM 57-52-0 PG 807 FIG 802. ALSO, THE THRUST BEARING RETAINER BOLT HOLE CORRODED AT BOTTOM O/B SIDE OF I/B CARRIAGE SUPPORT FITTING. THIS WAS REPAIRED PER SRM 57-50-4 FIG 14. FOUND AT HMV, SHOP INSP. 2L73 4F A3WE 19950414001921995041400192NM 1995 4 14 DL72W951453 119950407A2120 AIR DISTR BOEING727 7272Q8 138407WNM CABIN ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11831L 21826 ON APROACH, HAD UNKNOWN NOXIOUS FUMES IN AFT PASSENGER CABIN. MADE EMERGENCY DESCENT, LANDED AGS. VISUALLY INSPECTED CABIN AND CARGO BINS FOR SPILLS, RAN ENGINES AND PRESSURIZED CABIN DID NOT HAVE ANY ODOR. RETURNED TO SERVICE. 2L73 4F A3WE 19950414001931995041400193NM 1995 4 14 DL73E951419 119950317A71106585378395 NOSE COWL BOEING737 737247 138448DNM NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11376DL 23603 2540 DURING SHOP INSPECTION, FOUND NR 1 ENGINE NOSE COWL WITH CRACKED FRAME AT THE 9 O'CLOCK POSITION. REPAIRED PER SRM 54-1-3. 2L72 4F A16WE 19950414001941995041400194NM 1995 4 14 DL757951415 119950404A5330 SKIN BOEING757 757232 1384965NM BS 654 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 AT LETTER CHECK, DUE PERMANENT REPAIR PER SRM 53-31-001 STA 654 WL 214.0 LT SIDE FUSELAGE SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-00-1. 2L72 4F RTA2NM 19950414001951995041400195NM 1995 4 14 DL757951416 119950328A7110 SKIN BOEING757 757232 1384965NM NR 2 NOSE COWL DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 THE NR 2 ENGINE NOSE COWL, UPPER SECTION OF OUTER SKIN DELAMINATED. REPAIRED PER MM 54-11-01. FOUND AT LETTER CHECK. 2L72 4F RTA2NM 19950414001961995041400196NM 1995 4 14 DL757951417 119950328A7110 NOSE COWL BOEING757 757232 1384965NM NR 2 ENGINE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 AT HMV, INSPECTION FOUND THE UPPER SECTION OF OUTER SKIN OF NR 2 ENGINE NOSE COWL DELAMINATED. REPAIRED PER SRM 54-11-01. 2L72 4F RTA2NM 19950414001971995041400197NM 1995 4 14 DL76S951408 119950104A5753113T23017A SKIN BOEING767 767332 1382001NM LT TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11125DL 24075 DURING HMV, LT I/B T/E FLAP WAS FOUND TO HAVE TEMPORARY REPAIRS 12 INCHES TO 37 INCHES, AND 88 INCHES TO 94 INCHES FROM I/B END. MADE BONDED REPAIRS PER B767 SRM 57-53-01. 2L72 4F RTA1NM 19950414001981995041400198NM 1995 4 14 DL76S951428 119950406A5753 SKIN BOEING767 767332 1382001NM TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11122DL 23436 FOUND DURING LETTER CHECK INSP, DENT ON UNDERSIDE OF OUTBOARD FLAP OUTBOARD END RT WING. REMOVED DAMAGED AREA AND STARTED REPAIR PER SRM 57-53-01, OK TO PAINT FINISHED REPAIR PER SRM 57-53-01 AND PAINTED AREA. 2L72 4F RTA1NM 19950414001991995041400199NM 1995 4 14 DL76S951429 119950406A5753 SKIN BOEING767 767332 1382001NM TE FLAP PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11122DL 23436 FOUND DURING LETTER CHECK INSP, DENT AND PUNCTURE ON UNDERSIDE OF OUTBOARD AFT FLAP BEHIND NR 11 SPOILER R5T WING. REPAIRED PER SRM 57-53-01, PAINTED AREA. 2L72 4F RTA1NM 19950414002001995041400200WP 1995 4 14 DLL14951418 119950320A5755 SKIN 1529105176 LKHEED1011 1011385115 5265015WP RT NR 5 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO111739D 255 193C1237 DURING SHOP INSPECTION, RT NR 5 SPOILER WAS FOUND TO BE DELAMINATED ON BOTTOM SKIN T/E. REPAIRED PER SRM 57-52-00. 2L73 4F A23WE 19950414002011995041400201WP 1995 4 14 DLL14951420 119950320A5755 SKIN 1529105176 LKHEED1011 1011385115 5265015WP RT NR 5 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO111739D 255 193C1237 2540 DURING SHOP INSPECTION, RT NR 5 SPOILER WAS FOUND TO BE CRACKED AT I/B L/E. REPAIRED PER SRM 57-52-00. 2L73 4F A23WE 19950414002021995041400202WP 1995 4 14 DLL15951397 119950405A54001545466101 PAN LKHEED1011 10113853 5265020WP NR 3 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11754DL 193Y1181 CRACK IN NR 3 ENG PYLON BOX PAN FWD OF HYD SUPPLY LINE. REF SRM 54-11-00 ITEM 37. CRACK IS TO BE WELDED PER SRM 54-11-00 PG 812. 2L73 4F A23WE 19950414002031995041400203WP 1995 4 14 DLL16951404 119950301A5711 SPAR CAP LKHEED1011 10113853 5265020WP RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING HMV COMPLYING WITH AD 93-17-10 AND 94-05-01, CRACKS WERE FOUND IN THE RIGHT WING REAR SPAR UPPER CAP FASTENER HOLES AT IWS 293.58 AND IWS 346.109. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. REPAIR APPROVAL PER FAA AMC LETTER DATED 3/13/95. 2L73 4F A23WE 19950414002041995041400204NM 1995 4 14 DLM88951250 119950322A5230 FLANGE DOUG MD88 MD88 3023688NM C3 DOOR BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING OVERHAUL, FOUND THE FLANGE AROUND THE C-3 DOOR HANDLE BENT. REPAIRED PER SRM 52-05 FIG 30. 2L72 4F RTA6WE 19950414002051995041400205NM 1995 4 14 DLM88951256 119950322A5230 SKIN DOUG MD88 MD88 3023688NM BAGGAGE DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING OVERHAUL, FOUND C-1 B/B DOOR SKIN BENT AT DOOR HANDLE. REPAIRED PER SRM 52-05 FIG 30 PAGE 159. 2L72 4F RTA6WE 19950414002061995041400206NM 1995 4 14 DLM88951275 119950322A5313 LONGERON DOUG MD88 MD88 3023688NM BS 1418 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING OVERHAUL, FOUND LONGERON 2R CRACKED AFT OF FS 1418 FRAME. REPAIRED PER SRM 53-02 FIGURE 5. 2L72 4F RTA6WE 19950414002071995041400207NM 1995 4 14 DLM88951396 119950404A5330 SKIN DOUG MD88 MD88 3023688NM FWD FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11914DE 49957 A .5 INCH CRACK AT RT NLG DOOR AFT HINGE CUTOUT IN FUSELAGE SKIN FOUND AT B-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62. 2L72 4F RTA6WE 19950414002081995041400208NM 1995 4 14 DLM88951405 119950320A5330 SKIN DOUG MD88 MD88 3023688NM FS 225 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING HMV, FOUND SKIN DENTED GOUGED AT FS 225 LT SIDE AT 1000 POSITION. REPAIRED PER SRM 53-04 VIEW J FIG 38. 2L72 4F RTA6WE 19950414002091995041400209NM 1995 4 14 DLM88951409 119950406A5210 SKIN DOUG MD88 MD88 3023688NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11908DE 53417 FOUND DURING TRIP CHECK, L-1 DOOR HOLD OPEN WAS OUT OF ADJUSTMENT. FOUND SKIN CRACKED BELOW HOLD OPEN HOOK ON DOOR SKIN. REPAIRED PER SRM 52-05 FIG 20B. 2L72 4F RTA6WE 19950414002101995041400210NM 1995 4 14 DLM88951437 119950407A7120 MOUNT YOKE DOUG MD88 MD88 3023688NM NR 2 PYLON CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 AT HMV, NR 2 ENG FWD UPPER AND LWR MOUNTS ARE CORRODED. REPLACED ENG MOUNT YOKE PER MM 71-20-03. 2L72 4F RTA6WE 19950414002111995041400211NM 1995 4 14 DLM88951438 119950407A7120 MOUNT YOKE DOUG MD88 MD88 3023688NM NR 1 PYLON CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 AT HMV, NR 1 PYLON UPPER AND LOWER FWD ENG MOUNTS ARE CORRODED. REMOVED CORROSION PER SRM 54-04 FIG 6 CAD PLATED PER SRM 54-04 FIG 6. 2L72 4F RTA6WE 19950414002121995041400212NM 1995 4 14 DLM88951454 119950407A3231 BRACKET DOUG MD88 MD88 3023688NM RT MLG DOOR CRACKED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11970DL 43173 ON CLIMBOUT, HAD LANDING GEAR DOOR OPEN LIGHT. CYCLED GEAR, DID NOT GO OUT. RETURNED ATL. FOUND RIGHT MAIN LDG GEAR DOOR PROX SWITCH MOUNT BRACKET BROKEN. REPLACED BRACKET, OPERATION NORMAL. 2L72 4F RTA6WE 19950414002131995041400213WP 1995 4 14 MWEA95166 119950406A3350081691 EEL SOCKET DOUG DC9 DC914 3022034WP CABIN INOP A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31800ME 45842 EMERGENCY FLOOR MACH LIGHT INOP AT ROW 1C (DEFERRED). REMOVED AND REPLACED FLOOR TRACK LIGHT SOCKET. OPS CHECK GOOD. CLEARED DMI, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950414002141995041400214WP 1995 4 14 SCNA95050 119950404A3350337701962 EEL BATT DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15SEDHT 47833 FOUND LEFT HAND SIDE OF ZONE A FLOOR LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED ZONE A POWER SUPPLY PER MM 33-51-01. OPS CHECK GOOD. 2L73 4F A22WE 19950414002151995041400215 1995 4 14 SWAA95266 419950330A3417HG480B42 ADC BOEING737 7373H4 1384600NM RT FLIGHT DECK INOP A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07341SW 24091 ON TAKEOFF, FIRST OFFICER'S AIRSPEED AND ALTIMETER INDICATORS BECAME INOPERATIVE. BUFFET ALERT ON CDU, AND SPEED TRIM FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED FIRST OFFICER'S AIR DATA COMPUTER PER BOEING MM. 2L72 4F RTA16WE 19950414002161995041400216NM 1995 4 14 SWAA95267 119950330A5320 CLIPS BOEING737 7373Y0 1384671NM BS 440 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 480, S2L, S3L, AT BS 500D, S3L, AT BS 616, S3L, AND AT BS 440, S16L. REPLACED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002171995041400217NM 1995 4 14 SWAA95268 119950330A53302024T3 SKIN BOEING737 7373Y0 1384671NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTS AT BS 1012, AT S14-15L, AT BS 927 AND 947.5, BETWEEN S18 AND 19L, AT BS 887 AND 907, BETWEEN S17 AND 18L, AT BS 310 AND 326, S21 TO 22R, AT BS 1006, S12 TO 13L, AT 1004, S11 TO 12L, AT BS 351, BETWEEN S25 AND 26L, AT BS 366, AT S5L, AND AT BS 950, BL 0. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002181995041400218NM 1995 4 14 SWAA95269 119950330A5755654645165A SKIN BOEING737 7373Y0 1384671NM NR 1 SPOILER DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND NUMBER 1 SPOILER SKIN DENTED 2 PLACES ON UPPER SURFACE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002191995041400219NM 1995 4 14 SWAA95270 119950330A5754 SKIN BOEING737 7373Y0 1384671NM NR 3 LE SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT SKIN CRACKED AT T/E. REPAIRED PER BOEING DRAWING BAC 65C30133. 2L72 4F RTA16WE 19950414002201995041400220NM 1995 4 14 SWAA95271 119950330A53302024T3 SKIN BOEING737 7373Y0 1384671NM BS 1100 CREASED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CREASED AT BS 1100, AT S16L AND AT BS 1112, S17L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002211995041400221NM 1995 4 14 SWAA95272 119950330A5755 SKIN BOEING737 7373Y0 1384671NM NR 5 SPOILER DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND NUMBER 5 GROUND SPOILER DENTED 2 PLACES ON LOWER SURFACE. REPAIRED PER TRAMCO EWO 95-0222. 2L72 4F RTA16WE 19950414002221995041400222NM 1995 4 14 SWAA95273 119950330A5312BAC1505100361 BLKHD STIFFENER BOEING737 7373Y0 1384671NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND PRESSURE BULKHEAD VERTICAL STIFFENER CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002231995041400223NM 1995 4 14 SWAA95274 119950330A5320BAC1505 ANGLE BOEING737 7373Y0 1384671NM BS 1121 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SUPPORT ANGLE CORRODED AT BS 1121, RT SIDE, 10 INCHES ABOVE APU AIR INLET OPENING. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002241995041400224NM 1995 4 14 SWAA95275 119950330A5311 FRAME BOEING737 7373Y0 1384671NM BS 993 MECH DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME TO INTERCOSTAL STRAP AT BS 993, WL 247 DAMAGED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002251995041400225NM 1995 4 14 SWAA95276 119950330A5313M383042 STRINGER BOEING737 7373Y0 1384671NM BS 1088-1138 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED ON RIGHT SIDE OF APU TORQUE BOX FROM BS 1088 TO 1138, WL 230. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002261995041400226NM 1995 4 14 SWAA95277 119950330A5320 SHEAR WEB BOEING737 7373Y0 1384671NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND SHEAR WEB CRACKED AT BS 312, BL 0, WL 207. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002271995041400227NM 1995 4 14 SWAA95278 119950330A53206546561509 DOOR FRAME BOEING737 7373Y0 1384671NM AFT SERV DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR UPPER FRAME CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002281995041400228NM 1995 4 14 SWAA95279 119950330A5311 FRAME BOEING737 7373Y0 1384671NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 294, CRACKED AT RBL 54, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002291995041400229NM 1995 4 14 SWAA95280 119950330A5320655287461 DOOR FRAME BOEING737 7373Y0 1384671NM AFT ENTRY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FORWARD UPPER FRAME OF AFT ENTRY DOOR CRACKED. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002301995041400230NM 1995 4 14 SWAA95281 119950330A5315 FLOORBEAM BOEING737 7373Y0 1384671NM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT UPPER FLANGE, BS 947, BL 0 TO LBL 10. REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002311995041400231NM 1995 4 14 SWAA95282 119950330A5315AND101362404 FLOORBEAM BOEING737 7373Y0 1384671NM BS 294 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 18.5 TO 23.5, WL 208. REPAIRED PER TRAMCO EWO 95-0231 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002321995041400232NM 1995 4 14 SWAA95283 119950330A5315BAC1505100246 FLOORBEAM BOEING737 7373Y0 1384671NM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 1 TO RBL7, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002331995041400233NM 1995 4 14 SWAA95284 119950330A5241 DOOR SKIN BOEING737 7373Y0 1384671NM FWD GALLEY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND FORWARD GALLEY DOOR LOWER HINGE CUTOUT CRACKED 2 PLACES. REPAIRED PER SWA ACO 3189-52. 2L72 4F RTA16WE 19950414002341995041400234NM 1995 4 14 SWAA95285 119950330A5330 SKIN BOEING737 7373Y0 1384671NM FUSELAGE LIGHTNING STRIKEA SWAAK NONE C F.O.D. ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 500A PLUS 8, BETWEEN S21 AND 22L, AT BS 500, BETWEEN 23 AND 24L, AND AT BS 460, BETWEEN S23 AND 24L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414002351995041400235NM 1995 4 14 UPS202840 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 660/680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY STRINGER 23L AT STATION 660 AND 680. MAINTENANCE FABRICATED NEW STRINGER REPAIR SECTIONS PER SRM 51-30-5, 51-10-6 AND SRM 51-10-3. 2L73 4F A3WE 19950414002361995041400236NM 1995 4 14 UPS202841 119950405A5312 BLKHD SUPPORT BOEING727 72731C 1384011NM FWD CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON FORWARD CARGO BAY AFT BULKHEAD UPPER SUPPORT. MAINTENANCE FABRICATED NEW UPPER SUPPORT, PREPARED AND INSTALLED PER SRM 51-10-2, 51-20-151, AND SRM 51-30-2. 2L73 4F A3WE 19950414002371995041400237NM 1995 4 14 UPS202842 119950405A5320 LINK MOUNT BOEING727 72731C 1384011NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON TORSION LINK MOUNT AT STATION 740, RBL 36, WL 164 MARKED. MAINTENANCE REMOVED AND REPLACED THE CORRODED TORSION LINK MOUNT IAW SRM 51-30-2. 2L73 4F A3WE 19950414002381995041400238NM 1995 4 14 UPS202843 119950405A5320 LINK MOUNT BOEING727 72731C 1384011NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON TORSION LINK MOUNT AT STATION 740, RBL 13 AND WL 164. MAINTENANCE REMOVED THE CORRODED LINK AND LINK MOUNT AND INSTALLED NEW LINK AND LINK MOUNT IAW SRM 51-30-2. 2L73 4F A3WE 19950414002391995041400239NM 1995 4 14 UPS202844 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9R AT STATION 740 TO 870. MAINTENANCE REPLACED WITH NEW SECTION OF STRINGER IAW SRM 53-10-1, 53-10-2, 51-10-6, 51-10-02 AND MM 51-20-151. 2L73 4F A3WE 19950414002401995041400240NM 1995 4 14 UPS202845 119950405A5320 CLIP BOEING727 72731C 1384011NM BS 970 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE STRINGER CLIP AT STATION 970, STRINGER 9R. MAINTENANCE REMOVED AND REPLACED THE STRINGER CLIP PER 727 SRM. 2L73 4F A3WE 19950414002411995041400241NM 1995 4 14 UPS202846 119950405A5755 SKIN BOEING727 72731C 1384011NM NR 14 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 WHILE IN 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SURFACE OF THE NR 14 SPOILER. MAINTENANCE REMOVED THE DAMAGED AREA, FINAL REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950414002421995041400242NM 1995 4 14 UPS202847 119950405A5755 SKIN BOEING727 72731C 1384011NM NR 14 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON PREVIOUS REPAIRED NR 14 SPOILER HAD EXPOSED FIBERS ON THE LEADING EDGE AND OUTBOARD EDGE UPPER SURFACE. MAINTENANCE REMOVED THE PREVIOUS REPAIR AND DELAMINATION PER SRM 51-50-6, FINAL REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950414002431995041400243NM 1995 4 14 UPS202848 119950405A5752 TRIM TAB BOEING727 72731C 1384011NM RT INBD AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT HAND INBOARD AILERON TRIM TAB AT THE TRAILING EDGE. MAINTENANCE REMOVED THE DELAMINATION AND FINAL REPAIRS PER SRM 51-40-6 AND SRM 51-80-3. 2L73 4F A3WE 19950414002441995041400244NM 1995 4 14 UPS202849 119950405A5753 SKIN BOEING727 72731C 1384011NM RT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD FORE FLAP ON THE INBOARD END UPPER SURFACE. MAINTENANCE REPAIRED BY REMOVING DELAMINATION AND PRIOR REPAIR PER SRM 51-40-06 AND FINAL REPAIR PER SRM 51-40-00. 2L73 4F A3WE 19950414002451995041400245NM 1995 4 14 UPS202850 119950405A5753 RUB STRIP BOEING727 72731C 1384011NM TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATED STAINLESS STEEL RUB STRIP AND AREAS UNDER THE RUB STRIP. MAINTENANCE REPAIRED THE AREA PER 727 SRM 51-40-06. 2L73 4F A3WE 19950414002461995041400246NM 1995 4 14 UPS202851 119950405A5543 RUDDER TAB BOEING727 72731C 1384011NM RUDDER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND THE UPPER RUDDER TAB LOWER SURFACE TO BE DELAMINATED. MAINTENANCE REPAIRED PER SRM 51-40-6. 2L73 4F A3WE 19950414002471995041400247NM 1995 4 14 UPS202852 119950405A5754 SKIN BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT ATTACHING FASTENER BETWEEN SS 147 AND SS 154.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B. 2L73 4F A3WE 19950414002481995041400248NM 1995 4 14 UPS202853 119950405A5754 SKIN BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TPI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 176 AND SS 182. MAINTENANCE REPAIRED IAW EO B727-5750-3082B. 2L73 4F A3WE 19950414002491995041400249NM 1995 4 14 UPS202854 119950405A5754 SKIN BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT TAI SKIN AROUND AFT AND FORWARD FASTENERS BETWEEN SS 188.5 AND SS 195.5. MAINTENANCE REPAIRED IAW EO B727-5750-3082B. 2L73 4F A3WE 19950414002501995041400250NM 1995 4 14 UPS202855 119950405A5754 RIB BOEING727 72731C 1384011NM NR 3 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SLAT RIB AT SS 225 LOWER AFT CORNER. MAINTENANCE REPAIRED THE RIB USING DOUBLER PER 727 SRM 57-50-3. 2L73 4F A3WE 19950414002511995041400251NM 1995 4 14 UPS202856 119950405A5754 RIB BOEING727 72731C 1384011NM NR 4 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 4 SLAT END RIB AT SLAT STATION ZERO. MAINTENANCE REMOVED AND INSTALLED A NEW RIB ASSEMBLY PER SRM 51-10-1. 2L73 4F A3WE 19950414002521995041400252NM 1995 4 14 UPS202857 119950405A5320 JOINT BOEING727 72731C 1384011NM BS 855 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION JOINT AT STATION 855 TO 870, RBL 45, WL 203 AT AFT ATTACH POINT. MAINTENANCE REMOVED THE CORROSION FROM EXPANSION JOINT AND FOUND DAMAGE OUT OF LIMITS. REPLACED PART IAW SRM 53-10-1 AND 51-30-02. 2L73 4F A3WE 19950414002531995041400253NM 1995 4 14 UPS202858 119950405A5311 FRAME BOEING727 72731C 1384011NM BS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE FRAME AT STATION 660 AND STRINGER 26R. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-10-1, 51-30-2, 53-10-1, 53-10-4, 51-40-3, AND 51-40-4. 2L73 4F A3WE 19950414002541995041400254NM 1995 4 14 UPS202859 119950405A5311 FRAME BOEING727 72731C 1384011NM BS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE FRAME AT STATION 660 AND STRINGER 26L AROUND HOLE. MAINTENANCE FABRICATED REPAIR DOUBLER, VERIFIED, CRACK REMOVED, BY NDI. INSTALLED FABRICATED PARTS PER SRM 51-40-3, 51-30-2, 51-10-2, 51-20-4 AND 51-20-1. 2L73 4F A3WE 19950414002551995041400255NM 1995 4 14 UPS202860 119950405A5320 WEB BOEING727 72731C 1384011NM BS 203 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE WEB AT STATION 203 TO 204, LBL 34 TO 40 AND WL 208. MAINTENANCE REMOVED, FABRICATED REPAIR PART, INSTALLED PER SRM 51-10-6, 51-30-2 AND MM 51-20-15. 2L73 4F A3WE 19950414002561995041400256NM 1995 4 14 UPS202861 119950405A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP OF AND IN SEAT TRACK WELL AT STATION 380 TO 430 AND RBL 23. MAINTENANCE REMOVED SEAT TRACK AND REPLACED IT WITH NEW PER SRM 5-10-6. 2L73 4F A3WE 19950414002571995041400257NM 1995 4 14 UPS202862 119950405A5320 JOINT BOEING727 72731C 1384011NM BS 855 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION JOINT (LINK) AT STATION 855 TO 820, RBL 45. MAINTENANCE REMOVED AND REPLACED EXPANSION LINK PER SRM 51-10-1. 2L73 4F A3WE 19950414002581995041400258NM 1995 4 14 UPS202863 119950405A5320 BRACKET BOEING727 72731C 1384011NM BS 364 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON BRACKET BETWEEN STRINGERS S5L AND S6L AT STATION 364. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW SRM 51-30-2. 2L73 4F A3WE 19950414002591995041400259NM 1995 4 14 UPS202864 119950405A5320 TIE BOEING727 72731C 1384011NM BS 950 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TIE FORWARD SIDE AT STATION 950 AND STRINGER S2R. MAINTENANCE REMOVED THE CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED THE LOWER STRINGER S2R TIE IAW SRM 53-30-1 AND 51-30-02. 2L73 4F A3WE 19950414002601995041400260NM 1995 4 14 UPS202865 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2L AT STATION 740 TO 870. MAINTENANCE REMOVED THE CORROSION, CUT OUT DAMAGED AREA OF STRINGER, FABRICATED PANTS, AND INSTALLED REPAIR PARTS AND DOUBLERS IAW SRM 53-10-1, 51-10-6, 53-10-3, 51-20-1, 51-10-2, 51-30-2, 51-30-4 AND MM 51-20-15, 53-11-00. 2L73 4F A3WE 19950414002611995041400261NM 1995 4 14 UPS202866 119950405A5543 SKIN BOEING727 72731C 1384011NM RUDDER TAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE BULLNOSE SKIN AT THE UPPER RUDDER TAB, UPPER BULLNOSE ABOVE UPPER HINGE. SKIN WAS PULLED BACK. MAINTENANCE REMOVED THE NOSE SKIN, RECEIVED NEW END CAP AND FINAL INSTALLATION PER SRM 51-30-2 AND 51-20-151. 2L73 4F A3WE 19950414002621995041400262NM 1995 4 14 UPS202867 119950405A5753 CARRIAGE BOEING727 72731C 1384011NM NR 6 TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 6 FLAP CARRIAGE UNDER THE THRUST NUT. MAINTENANCE REMOVED AND REPLACED THE FLAP CARRIAGE PER MM 57-52-01. 2L73 4F A3WE 19950414002631995041400263NM 1995 4 14 UPS202868 119950405A5754 RIB BOEING727 72731C 1384011NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 112 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-2 AND 57-50-3. 2L73 4F A3WE 19950414002641995041400264NM 1995 4 14 UPS202869 119950405A5754 RIB BOEING727 72731C 1384011NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT SS 105 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER. FINAL INSTALLATION IAW SRM 51-30-02 AND 57-50-3. 2L73 4F A3WE 19950414002651995041400265NM 1995 4 14 UPS202870 119950405A5754 RIB BOEING727 72731C 1384011NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 5 SLAT RIB AT STATION 97.5 AFT CORNER WHERE SLAT LOWER CHORD AND RIB ATTACH. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED DOUBLER AND FINAL INSTALLATION IAW SRM 51-30-02 AND 51-50-3. 2L73 4F A3WE 19950414002661995041400266NM 1995 4 14 UPS202871 119950405A5754 SKIN BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE SKIN OF THE NR 6 SLAT BETWEEN STATION 166.5 AND STATION 161.5 AT FORWARD FASTENERS. MAINTENANCE REMOVED THE FASTENERS, STOP DRILLED, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-20-04, 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950414002671995041400267NM 1995 4 14 UPS202872 119950405A5753 CHORD BOEING727 72731C 1384011NM LT TE MID FLAP CRACKED A AIPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND TWO 20 PLUS INCH CRACKS IN THE LEFT WING INBOARD MID FLAP AFT LOWER CHORD. MAINTENANCE REMOVED THE LOWER CHORD IAW SRM 51-30-2, FABRICATED, NEW EXTRUSION A LOWER CHORD. FINAL INSTALLATION IAW SRM 51-10-2. 2L73 4F A3WE 19950414002681995041400268NM 1995 4 14 UPS202873 119950405A5754 RIB BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT MOST INBOARD RIB (SEAL RETAINER RIB AT SLAT STATION 120). MAINTENANCE REMOVED THE CRACKED RIB, INSTALLED NEW RIB AND FINAL INSTALLATION IAW SRM 51-30-2 AND 51-30-5. 2L73 4F A3WE 19950414002691995041400269NM 1995 4 14 UPS202874 119950405A5320 CHANNEL BOEING727 72731C 1384011NM PIE SECTION CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE END ENCLOSURE RIB CHANNEL, OUT BOARD END OF RIGHT PIE SECTION. MAINTENANCE REMOVED THE CRACKED CHORD, FABRICATED PER SRM 51-30-2 AND FINAL INSTALLATION IAW SRM 51-30-5. 2L73 4F A3WE 19950414002701995041400270NM 1995 4 14 UPS202875 119950405A5754 RIB BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE NR 6 SLAT RADIUS OF THE RIB AT SS 140 FORWARD END AT RIB, UPPER FLANGE RADIUS AREA. MAINTENANCE REMOVED THE RIB, FABRICATED NEW RIB AND FINAL INSTALLATION IAW SRM 51-10-2 AND 51-20-151. 2L73 4F A3WE 19950414002711995041400271NM 1995 4 14 UPS202876 119950405A5311 FRAME BOEING727 72731C 1384011NM BS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME ON TOP AND BOTTOM FLANGES BETWEEN STRINGERS 2L TO 5L AT STATION 312. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR CHANNEL PER SRM 53-10-4 AND FINAL INSTALLATION PER SRM 53-10-4. 2L73 4F A3WE 19950414002721995041400272NM 1995 4 14 UPS202877 119950405A5320 CLIP BOEING727 72731C 1384011NM BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER CLIP AT STATION 420, STRINGER 6L. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER CLIP PER SRM 51-30-2, 51-10-2. 2L73 4F A3WE 19950414002731995041400273NM 1995 4 14 UPS202878 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 360-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R AT STATION 360 TO 480. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-10-3 AND FINAL INSTALLATION IAW SRM 51-30-2. 2L73 4F A3WE 19950414002741995041400274NM 1995 4 14 UPS202879 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 620-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9L AT STATION 620 TO 740. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-3, 51-30-2 AND 51-10-3. 2L73 4F A3WE 19950414002751995041400275NM 1995 4 14 UPS202880 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6R AT STATION 480 TO 620. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-01 AND 53-10-3. 2L73 4F A3WE 19950414002761995041400276NM 1995 4 14 UPS202881 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8R AT STATION 480 TO 620. MAINTENANCE REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 51-30-2, 53-10-3 AND 51-20-4. 2L73 4F A3WE 19950414002771995041400277NM 1995 4 14 UPS202882 119950405A5330 SKIN BOEING727 72731C 1384011NM BS 760-785 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE INNER SKIN AT STATION 760 TO 785 BETWEEN STRINGERS S8R AND S10R. MAINTENANCE REMOVED THE CORROSION, HFEC INSPECTED AREA, FLAP PINNED AREA AND REINSTALLED SURFACE FINISH IAW EO 95-2345. 2L73 4F A3WE 19950414002781995041400278NM 1995 4 14 UPS202883 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 680-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 9R AT STATION 680 TO 740. MAINTENANCE CUT FRAME AT BS 720, STR 9R FOR ACCESS. FABRICATED FRAME REPAIR PARTS, INSTALLED STRINGER 9R AND FRAME REPAIR PARTS PER SRM 53-10-4, 51-30-2 MM 51-20-151. 2L73 4F A3WE 19950414002791995041400279NM 1995 4 14 UPS202884 119950405A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 948 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP CENTER OF SEAT TRACK AT STATION 948, BL 0. MAINTENANCE REPLACED THE SEAT TRACK FROM BS 870 TO 960, BL 0. ALL WORK DONE PER SRM 53-10-1, 51-10-2, 53-10-5 AND 51-30-2. 2L73 4F A3WE 19950414002801995041400280NM 1995 4 14 UPS202885 119950405A5315 FLOORBEAM BOEING727 72731C 1384011NM BS 660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON NUTPLATES AT BOTTOM OF FLANGE OF FLOORBEAM AT STATION 660, RBL 64 TO LBL 64, WL 208.1. MAINTENANCE REMOVED TOP OF FLOORBEAM FROM WEB RBL 17 OUTBOARD TO END OF BEAM, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8. 2L73 4F A3WE 19950414002811995041400281NM 1995 4 14 UPS202886 119950405A5315 FLOORBEAM BOEING727 72731C 1384011NM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON NUTPLATES AT BOTTOM OF FLANGE OF FLOORBEAM AT STATION 680 FROM LBL 64 TO RBL 64 AND WL 208.1. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-10-8. 2L73 4F A3WE 19950414002821995041400282NM 1995 4 14 UPS202887 119950405A5755 SPOILER BOEING727 72731C 1384011NM NR 10 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND DELAMINATION AND CONTAMINATION ON THE NR 10 SPOILER. MAINTENANCE REPLACED THE SPOILER IAW MM 27-61-01. 2L73 4F A3WE 19950414002831995041400283NM 1995 4 14 UPS202888 119950405A5320 FITTING BOEING727 72731C 1384011NM BS 704 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER FITTING NR 2R AT STATION 740 AFT SIDE. MAINTENANCE REMOVED THE CORROSION ON NR 2R STRINGER AT STATION 704 AFT SIDE, FOUND TO BE OUT OF LIMITS, WORK ACCOMPLISHED PER SRM 51-10-6, ORDERED NEW PART AND INSTALLED IAW SRM 51-30-2. 2L73 4F A3WE 19950414002841995041400284NM 1995 4 14 UPS202889 119950405A5312 BLKHD STRAP BOEING727 72731C 1384011NM BS 351 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRAP ON TOP OF 351 BULKHEAD AT WL 160, LBL 25 TO RBL 25. MAINTENANCE FABRICATED A NEW STRAP AND INSTALLED STRAP PER SRM 51-30-2. 2L73 4F A3WE 19950414002851995041400285NM 1995 4 14 UPS202890 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 1 AT STATION 950 TO 1183. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-1, 51-10-0, 51-10-02, 51-20-151, 51-30-2 AND 53-10-3. 2L73 4F A3WE 19950414002861995041400286NM 1995 4 14 UPS202891 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 2R AT STATION 950 TO 1183. MAINTENANCE SPLICED A NEW SECTION OF STRINGER FROM BS 950 TO 1036 IAW SRM 53-10-3. 2L73 4F A3WE 19950414002871995041400287NM 1995 4 14 UPS202892 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R AT STATION 950 TO 1183. MAINTENANCE FABRICATED 'J' ANGLE REPAIR PARTS AND INSTALLED PER EO 727-53-1570. 2L73 4F A3WE 19950414002881995041400288NM 1995 4 14 UPS202893 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND PITTING CORROSION ON THE NR 1 K-FLAP AT CENTER ATTACH LUG ON UPPER INBOARD, UPPER OUTBOARD AND LOWER INBOARD MOUNT BOLT AREAS. MAINTENANCE REPLACE THE NR 1 K-FLAP IAW MM 27-81-01. 2L73 4F A3WE 19950414002891995041400289NM 1995 4 14 UPS202894 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 2 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE AT BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW OHM 57-51-11 AND MM 27-81-01. 2L73 4F A3WE 19950414002901995041400290NM 1995 4 14 UPS202895 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 3 K-FLAP OUTBOARD HINGE LUG UPPER AND LOWER BOLTS ON OUTBOARD SIDE. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01. 2L73 4F A3WE 19950414002911995041400291NM 1995 4 14 UPS202896 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 4 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 4 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE BOTH MOUNT BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01. 2L73 4F A3WE 19950414002921995041400292NM 1995 4 14 UPS202897 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 5 K-FLAP OUTBOARD HINGE LUG OUTBOARD FACE UNDER BOTH BOLTS. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01. 2L73 4F A3WE 19950414002931995041400293NM 1995 4 14 UPS202898 119950405A5754 K-FLAP BOEING727 72731C 1384011NM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE NR 6 K-FLAP OUTBOARD HINGE LUG OUTBOARD SIDE UNDER THE UPPER LUG. MAINTENANCE REMOVED AND REPLACED THE K-FLAP IAW SRM 57-50-01, OHM 57-51-21 AND MM 27-81-01. 2L73 4F A3WE 19950414002941995041400294NM 1995 4 14 UPS202899 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 360-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER S5R FROM STATION 360 TO 480. MAINTENANCE FABRICATED REPAIR SECTION AND INSTALLED IAW SRM 53-10-3, 53-10-1, 51-10-2 AND 51-10-6. 2L73 4F A3WE 19950414002951995041400295NM 1995 4 14 UPS202900 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3R AT STATION 480 TO 740. MAINTENANCE REPLACED THE STRINGER IAW SRM 53-10-1, 51-10-0, 51-10-02, 51-20-151, 51-30-2 AND 53-10-3. 2L73 4F A3WE 19950414002961995041400296NM 1995 4 14 UPS202901 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 4R SIDE AT STATION 480 TO 740. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLATION PER EO 95-2388, SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950414002971995041400297NM 1995 4 14 UPS202902 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 5R SIDE AT STATION 480 TO 740. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLATION PER EO 95-2388, SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950414002981995041400298NM 1995 4 14 UPS202903 119950405A5320 STRINGER SPLICE BOEING727 72731C 1384011NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER SPLICE FORWARD ON TERMINATION ENDS OF STRINGER CENTER THROUGH 9L SIDE ON FORWARD SIDE FRAME STATION 740. MAINTENANCE REMOVED AND REINSTALLED NEW STRINGER SPLICES AT STRINGERS 1 AND 8 AT STATION 740 FRONT SIDE IAW SRM 51-10-2 AND 51-10-1. 2L73 4F A3WE 19950414002991995041400299NM 1995 4 14 UPS202904 119950405A5320 CHANNEL BOEING727 72731C 1384011NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER FLANGE OF THE CHANNEL AT STATION 344 FROM RBL 10 INCHES TO 60 INCHES AND WL 208. MAINTENANCE FABRICATED A NEW CHANNEL IAW SRM 51-10-1, 51-10-2, 51-30-2 AND MM 57-20-151. 2L73 4F A3WE 19950414003001995041400300NM 1995 4 14 UPS202905 119950405A5330 SKIN BOEING727 72731C 1384011NM BS 1148-1163 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER SKIN AT SKIN LAP AT STATION 1148 TO 1163, STRINGER 25L TO 26L, STRINGER FITTING ALSO, CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FITTING, THE CORRODED SKIN AND DOUBLER IAW SRM 51-30-2, SRM 53-30-3, SRM 51-30-4, SRM 51-20-4 AND UPS EO 727-53-1563. 2L73 4F A3WE 19950414003011995041400301NM 1995 4 14 UPS202906 119950405A5230 BEAM BOEING727 72731C 1384011NM BS 1096 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A 1 INCH CRACK IN THE AFT CARGO DOOR NR 2 HORIZONTAL BEAM AT STATION 1096. MAINTENANCE REMOVED AND REPLACED THE BEAM PER SRM 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950414003021995041400302NM 1995 4 14 UPS202907 119950405A5314 KEEL BEAM BOEING727 72731C 1384011NM BS 872 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A CRACK IN THE KEEL BEAM VERTICAL WEB JUST FORWARD OF APU CUTOUT AT STATION 872, RBL 5.5, WL 162 IN RIGHT HAND MAIN LANDING GEAR WHEEL WELL. MAINTENANCE REMOVED THE DAMAGED STRUCTURE PER UPS EO B727-5330-7995. 2L73 4F A3WE 19950414003031995041400303NM 1995 4 14 UPS202908 119950405A5230 ANGLE BOEING727 72731C 1384011NM BS 1084 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK IN THE AFT CARGO DOOR NR 3 HORIZONTAL BEAM UPPER OUTBOARD L-ANGLE AT STATION 1084. MAINTENANCE REMOVED AND REPLACED THE L-ANGLE, UPPER OUTBOARD HORIZONTAL BEAM IAW SRM 51-30-5, 51-30-2 AND 51-10-1. 2L73 4F A3WE 19950414003041995041400304NM 1995 4 14 UPS202909 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 870-950 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 6R AT STATION 870 TO 950. MAINTENANCE BLENDED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-2, 51-20-04, MM 51-20-151, AND UPS EO 727-53-1570. 2L73 4F A3WE 19950414003051995041400305NM 1995 4 14 UPS202910 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3R AT STATION 950 TO 1183. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED PER SRM 53-10-2. 2L73 4F A3WE 19950414003061995041400306NM 1995 4 14 UPS202911 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 950-1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 5R AT STATION 950 TO 1183. MAINTENANCE REMOVED CORROSION, FABRICATED NEW STRINGER, SENT OUT FOR HEAT TREATMENT AND INSTALLED IAW SRM 51-30-2, 51-10-6, 53-10-1, 53-10-3 AND MM 51-20-151. 2L73 4F A3WE 19950414003071995041400307NM 1995 4 14 UPS202912 119950405A5720 CELL CUTOUT BOEING727 72731C 1384011NM WINGS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7207 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER EO 727-57-1123. 2L73 4F A3WE 19950414003081995041400308NM 1995 4 14 UPS202913 119950405A5720 CELL CUTOUT BOEING727 72731C 1384011NM WINGS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7202 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123. 2L73 4F A3WE 19950414003091995041400309NM 1995 4 14 UPS202914 119950405A5720 CELL CUTOUT BOEING727 72731C 1384011NM WINGS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND FRETTING CORROSION OF FUEL CELL CUTOUT NR 7206 UPPER SURFACE AREA. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UPS EO 727-57-1123. 2L73 4F A3WE 19950414003101995041400310NM 1995 4 14 UPS202915 119950405A5720 CELL CUTOUT BOEING727 72731C 1384011NM WINGS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7606 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123. 2L73 4F A3WE 19950414003111995041400311NM 1995 4 14 UPS202916 119950405A5720 CELL CUTOUT BOEING727 72731C 1384011NM WINGS CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL CUTOUT NR 7607 UPPER SURFACE. MAINTENANCE BLENDED CORROSION, TREATED, FABRICATED AND INSTALLED RING FILLERS, ALL WORK DONE PER UP EO 727-57-1123. 2L73 4F A3WE 19950414003121995041400312NM 1995 4 14 UPS202917 119950405A5315 FLOORBEAM BOEING727 72731C 1384011NM BS 720 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE FLOORBEAM AT STATION 720, RBL 51 AND RBL 61, WL 208. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED ALL WORK DONE PER SRM 51-10-1, 51-10-6, 51-10-2, 51-30-2 AND UPS EO B727-5310-6839A. 2L73 4F A3WE 19950414003131995041400313NM 1995 4 14 UPS202918 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 480-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 1 AT STATION 480 TO 740. MAINTENANCE REMOVED THE DAMAGED SECTIONS OF STRINGER 1 FROM BS 480 TO 511, BS 620 TO 740, FABRICATED AND INSTALLED REPAIR SPLICES AND NEW SECTIONS OF STRINGER. ALL WORK DONE PER SRM 53-10-3 AND UPS EO B727-53-1570. 2L73 4F A3WE 19950414003141995041400314NM 1995 4 14 UPS202919 119950405A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 954-958 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON TOP CENTER AND BOTTOM OUTBOARD FLANGE OF SEAT TRACK AT STATION 954 TO 958, RBL 24.75. MAINTENANCE REMOVED THE DAMAGED SECTION OF SEAT TRACK, REPLACED PER SRM 51-10-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950414003151995041400315NM 1995 4 14 UPS202920 119950405A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 942 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM INBOARD FLANGE OF SEAT TRACK AROUND FASTENER HOLES AT STATION 942, LBL 45.5. MAINTENANCE FABRICATED NEW SECTION OF SEAT TRACK AND REPAIR SPLICES, INSTALLED, PER SRM 51-10-6, 53-10-1, 51-30-2, 51-10-1, 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950414003161995041400316NM 1995 4 14 UPS202921 119950405A5315 FLOORBEAM BOEING727 72731C 1384011NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES UPPER AND LOWER FLANGES OF FLOORBEAM AT STATION 344, RBL 11 TO RBL 20, WL 208.1. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW UPS EO B727-5310-6844A. 2L73 4F A3WE 19950414003171995041400317NM 1995 4 14 UPS202922 119950405A5714 RIB BOEING727 72731C 1384011NM BS 760.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS IN FORWARD TWO AND AFT UPPER HOLES AND RIB CHORD AT STATION 760.5 AND RBL 70.5. MAINTENANCE REMOVED AND REPLACED FAIL SAFE STRAP AND T-CLIP AND REPAIRED RIB CHORD PER UPS EO B727-5710-6847A AND UPS EO B727-57-1338. 2L73 4F A3WE 19950414003181995041400318NM 1995 4 14 UPS202923 119950405A5320 STRAP BOEING727 72731C 1384011NM BS 760.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION AND CRACKS IN FORWARD TWO AND AFT UPPER HOLES AND RIB CHORD AT STATION 760.5 AND LBL 70.5. MAINTENANCE REMOVED AND REPLACED FAIL SAFE STRAP AND T-CLIP AND REPAIRED RIB CHORD PER UPS EO B727-5710-6847A AND UPS EO B727-57-1338. 2L73 4F A3WE 19950414003191995041400319NM 1995 4 14 UPS202924 119950405A5311 FRAME BOEING727 72731C 1384011NM BS 351.2 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER CHORD AND STRAP AT STATION 351.2 BETWEEN STRINGERS 26L AND 25L. MAINTENANCE TRIMMED OUT FAIL SAFE CHORD FOR ACCESS, BLENDED OUT CORROSION, FREEZE PLUG DISCREPANT HOLES. FABRICATED NESTING REPAIR ANGLES, FILLER, AND TAPERED SHIMS AND INSTALL REPAIR PARTS. WORK IAW UPS EO B727-5310-6860A. 2L73 4F A3WE 19950414003201995041400320NM 1995 4 14 UPS202925 119950405A5313 STRINGER BOEING727 72731C 1384011NM BS 620-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7R STA 620 TO 680. REPLACED PER SRM 53-10-1. 2L73 4F A3WE 19950414003211995041400321NM 1995 4 14 UPS202926 119950405A5754 RIB BOEING727 72731C 1384011NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT AT RIB SS 182, AFT CORNER WHERE LWR CHORD ATTACHES TO RIB. REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19950414003221995041400322NM 1995 4 14 UPS202927 119950405A5754 RIB BOEING727 72731C 1384011NM NR 4 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT RIB AT SS 63, FWD UPPER CORNER. REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19950414003231995041400323NM 1995 4 14 UPS202928 119950405A5320 CLIP BOEING727 72731C 1384011NM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORROSION ON T-CLIP AT STA 760, WHILE ACCESSING FOR 70.5 INSP. REPLACED PER SRM 51-30-02, 51-30-05. 2L73 4F A3WE 19950414003241995041400324NM 1995 4 14 UPS202929 119950405A5320 WEB BOEING727 72731C 1384011NM BS 1243 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CRACK AT STA 1243, LBL 15, WL 180, ON VERTICAL WEB FOR LWR TORQUE BOX, AT 7 O'CLOCK POSITION OF LWR LIGHTENING HOLE. REPAIRED PER SRM 51-40-2, 51-10-1. 2L73 4F A3WE 19950414003251995041400325NM 1995 4 14 UPS202930 119950405A5347 SEAT TRACK BOEING727 72731C 1384011NM BS 600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON SEAT TRACK FLANGE STA 600, RBL 55. REPLACED PER SRM 51-10-1, 51-10-2, 51-30-2, MM 51-20-151. 2L73 4F A3WE 19950414003261995041400326NM 1995 4 14 UPS202931 119950405A5755 CORE BOEING727 72731C 1384011NM NR 5 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CORE DAMAGE AND CONTAMINATION ON PREVIOUS REPAIR AREA, NR 5 SPOILER. INSTALLED REPAIR PER SRM 57-50-6, MM 51-20-151. 2L73 4F A3WE 19950414003271995041400327NM 1995 4 14 UPS202932 119950405A5754 TE SKIN BOEING727 72731C 1384011NM NR 7 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01926UP 19233 DURING 'D' CHECK, MAINTENANCE FOUND CRACK ON NR 7 SLAT T/E. INSTALLED REPAIR PER SRM 51-40-2, 51-30-2, MM 51-20-21, 51-20-71. 2L73 4F A3WE 19950414003281995041400328WP 1995 4 14 UPS802933 119950407A3260 DOOR LIGHT DOUG DC8 DC871F 302199DWP LT MLG DOOR ILLUMINATED A IPXAL ABORTED APPROACH N FALSE WARNING CRCRUISE 1 SO01779UP 45979 PILOT REPORTED DURING GO AROUND, GEAR DOOR NOT LATCHED INDICATION, CYCLED GEAR. ALSO, ALT LEFT GEAR DOOR LIGHT ILLUMINATED. CHECKED SYSTEM PER MM 32-31-04. COULD NOT DUPLICATE PROBLEM. 2L74 4F RT4A25 19950414003291995041400329WP 1995 4 14 UPS802934 119950408A3231 UPLATCH MECH DOUG DC8 DC873F 302199FWP MLG DOORS OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01812UP 46118 PILOT REPORTED AFTER GO AROUND, GEAR DOOR NOT LATCHED LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR, LIGHT REMAINED ON. FOUND LT AND RT MLG DOOR UPLATCH MECHANISM HOOK TO ROLLER CLEARANCE NON-EXISTANT, ADJ MAIN GEAR DOOR UPLATCH MECHANISM PER MM 32-31-04. OPS CK OK. 2L74 4F RT4A25 19950414003301995041400330NM 1995 4 14 UPS802935 119950408A3350 EEL BOEING747 747SR46 NM CABIN INOPERATIVE A IPXAO OTHER L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED EMER EXIT LIGHTS INOP, BY FWD ENTRY DOOR AND AFT ENTRY DOOR 2 EA. 2L74 4F A20WE 19950414003311995041400331 1995 4 14 9505491145 419950409A221137570818 COMPUTER DOUG DC10 DC1040 3023508WP AUTO PILOT MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL01145US157158705 46754 DURING CRUISE WITH A BANK ANGLE OF 10 DEGREES, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO 30 DEGREES. ADDITIONALLY, DURING APPROACH WITH 20 DEGREES SELECTED, THE AIRCRAFT EXPERIENCED ANOTHER UNCOMMANDED ROLL TO 35 DEGREES. REPLACED THE AUTO-PILOT CONTROL PANEL AND AUTO-PILOT ROLL COMPUTER. 2L73 4F A22WE 19950414003321995041400332SO 1995 4 14 COM11856 119950410A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO011110J141956542 120110 FLAP ASSYMETRY WARNING. RT OUTBD FLAP INDICATES 25 DEGREES WHEN SELECTED 15 DEGREES. REPLACED RT OUTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19950414003331995041400333NE 1995 4 14 COM60451 219950410A7320J1175C0264AA FUEL LINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A 30015NE LT ENGINE LOOSE A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01926CA 7027 FUEL LEAKING FROM LT ENGINE. TIGHTENED I.G.V. ACTUATOR FUEL LINE FITTING. NO LEAKS NOTED. 2L72 4F4 FRTA21EA E15NE 19950414003341995041400334 1995 4 14 COM60452 419950405A3418501125904 ACTUATOR CNDAIRCL600 CL6002B19 EA STALL WARNING DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01926CA506 7027 SCRAPING NOISE HEARD WHEN CONTROL YOKE MOVED FORE AND AFT. STALL WARNING ACTIVATED. REPLACED THE STICK PUSHER ACTUATOR. 2L72 4F RTA21EA 19950414003351995041400335NM 1995 4 14 DL72S951447 119950331A5240 SKIN BOEING727 727232 1384082NM RT SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK RT FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED .50 INCH. REPAIR: REPAIRED PER M/M 52-11-0 PG 808. 2L73 4F A3WE 19950414003361995041400336NM 1995 4 14 DL72S951449 119950403A5320 WEB BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK .25 INCH CRACK LIGHTNING HOLE TORQUE BOX SIDE WEBB STA 1263 LT SIDE. REPAIR: ROUTE OUT DAMAGED AREA PER M/M 53-11-0. 2L73 4F A3WE 19950414003371995041400337NM 1995 4 14 DL72S951450 119950331A5755 ANGLE BOEING727 727232 1384082NM NR 7 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, ONE INCH CRACK IN ATTACH ANGLE LOWER END OF NR 7 SPOILER ACTUATOR ATTACH FITTING. REPAIR: REPAIRED PER M/M 57-20-22 PAR 10. 2L73 4F A3WE 19950414003381995041400338NM 1995 4 14 DL72S951451 119950402A5320 CLIP BOEING727 727232 1384082NM BS 990 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 FOUND ON CV2 CHECK, ONE INCH CRACK IN SKIN CLIP BETWEEN STR 28L AND 29L FWD SIDE STA 990. REPAIR: REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950414003391995041400339NM 1995 4 14 DL72S951455 119950406A2710DP21BFS464 BEARINGS BOEING727 727232 1384082NM RT AILERON WORN A ADALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO11542DA 22391 DURING CRUISE, LEFT INBOARD AILERON WAS STUCK DOWN. NEEDS 20 DEGREE RIGHT AILERON INPUT FOR WINGS LEVEL AND 1.5 DEGREE RT RUDDER TRIM. FOUND RIGHT INBOARD AILERON LOWER QUADRANT BEARINGS FAILED. REPLACED BOTH BEARINGS PER MM 27-10-11. OPERATION NORMAL. 2L73 4F A3WE 19950414003401995041400340WP 1995 4 14 DLL17951466 119950322A5320 CHANNEL LKHEED1011 10113853 5265020WP NR 5 LAV CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND CHANNEL CORRODED AT NR 5 LAV AT ENTRY. REPLACED HAT CHANNEL PER SRM 53-21-00 PG 859-860. 2L73 4F A23WE 19950414003411995041400341WP 1995 4 14 DLL17951467 119950321A5320 CHANNEL LKHEED1011 10113853 5265020WP NR 1 AFT LAV CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND CHANNEL CORRODED AT OPENING TO NR 1 AFT LAV. INSTALLED NEW HAT CHANNEL, PER SRM 53-21-00 PG 859-860. 2L73 4F A23WE 19950414003421995041400342WP 1995 4 14 DLL17951468 119950321A5320 CHANNEL LKHEED1011 10113853 5265020WP NR 2 AFT LAV CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND CHANNEL CORRODED AT BOTTOM OPENING OF NR 2 AFT LAV. INSTALLED NEW CHANNEL PER SRM 53-21-00. 2L73 4F A23WE 19950414003431995041400343NM 1995 4 14 DLM88951457 119950408A5530 SUPPORT DOUG MD88 MD88 3023688NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 49810 AT HMV, LOUVER SUPPORTS CRACKED ON LT SIDE OF VERTICAL STABILIZER. REPAIRED PER SRM 53-05 FIG 66. 2L72 4F RTA6WE 19950414003441995041400344NM 1995 4 14 DLM88951458 119950408A5530 SUPPORT DOUG MD88 MD88 3023688NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 49810 AT HMV, LOUVER SUPPORTS ARE CRACKED ON RT SIDE OF VERTICAL STABILIZER. REPAIRED PER SRM. 53-05 FIG 66. 2L72 4F RTA6WE 19950414003451995041400345NM 1995 4 14 DLM88951459 119950409A52805914984410 SKIN DOUG MD88 MD88 3023688NM NLG DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11908DE 53417 49810 DURING A ROUTINE SHOP INSPECTION, NR 6921 WAS WRITTEN ON LT NLG DOOR FOR DAMAGE ON INNER SKIN LOWER FLANGE 10 INCHES FROM FWD EDGE. INSTALLED DOUBLER PER SRM 52-02 FIG. 6. 2L72 4F RTA6WE 19950414003461995041400346WP 1995 4 14 MWEA95168 119950410A3350100865 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST CRCRUISE 1 GL31204ME 614 47680 PILOT REPORTS LAST SEVEN LIGHTS ON EMERGENCY FLOOR TRACK LIGHTING ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING POWER SUPPLY (AFT). OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950414003471995041400347WP 1995 4 14 MWEA95169 119950407A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31502ME 48132 CREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950414003481995041400348WP 1995 4 14 MWEA95197 119950411A532039164091 ANGLE DOUG DC9 DC914 3022034WP BS 586 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING ROUTINE INSPECTION FOUND ANGLE CORRODED SEVERELY IN LEFT WHEELWELL FWD OUTBD CORNER STA 586. REPLACED ANGLE WITH FACTORY PART IAW SRM 51-30-5. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950414003491995041400349NM 1995 4 14 QXEA9500107 119950407A3530 PBE UNIT DHAV DHC8 DHC8102 2809003NM CLOSET VACUUM LOSS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09841PH8717 82 BOI - THE P.B.E. IN THE CABIN STORAGE CLOSET IS FULL OF AIR. REPLACED P.B.E. WITH A SERVICEABLE UNIT. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19950414003501995041400350NM 1995 4 14 QXEA9500108 119950409A3530 PBE UNIT DHAV DHC8 DHC8102 2809003NM CABIN VACUUM LOSS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09841PH17 82 BOI - THE FLIGHT ATTENDANTS P.B.E. IS SOFT AND THE RED TAB IS EXTENDED. 2H72 4T RTA13NM 19950414003511995041400351EU 1995 4 14 QXEA9500109 119950408A3350P2070001201 FLASHLIGHT FOKKERF28 F28MK1000 4990808EU COCKPIT DISCHARGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09802PH 11017 PDX - THE COCKPIT FLASHLIGHT LITTLE RED LIGHT IS NOT FLASHING. REMOVED AND REPLACED THE FLASHLIGHT AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950414003521995041400352SW 1995 4 14 QXEA9500110 119950409A2150 PACK SWRNGNSA227 SA227AC 8780603SW CABIN ODOR A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM0927442 AC750 SEA - THE FLIGHT CREW SMELLS VAPORIZED TURBINE ENGINE OIL IN THE CABIN. THE COOLING TURBINE WAS PLACED ON MEL REF. 21-4. 1L72 4T A8SW 19950414003531995041400353EU 1995 4 14 QXEA9500111 119950408A3230125753 UPLOCK ACTUATOR FOKKERF28 F28MK1000 4990808EU RT MLG LEAKING A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09450US 11101 PDX - ON GEAR EXTENSION THE RT MLG SHOWED UNSAFE GEAR WAS CYCLED AGAIN AND RT MLG SHOWED UNSAFE INDICATION FOR 15 LONGER THAN THE MLG AND NOSE GEAR. REMOVED AND REPLACED THE RT MLG AFT UPLOCK ACTUATOR. A/C PASSED GEAR OPERATIONAL CHECKS. 2L72 4F RTA20EU 19950414003541995041400354EU 1995 4 14 QXEA9500112 119950410A35304566M37B042NM PBE UNIT FOKKERF28 F28MK1000 4990808EU CABIN DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09462AU4073 11054 BOI - THE AFT TOP P.B.E. MASK PACKING IS SOFT. REMOVED AND REPLACED THE P.B.E. UNIT WITH A SERVICEABLE UNIT. 2L72 4F RTA20EU 19950414003551995041400355WP 1995 4 14 QXEA9500113 219950410A723031011602 CARBON SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NR 1 ENGINE LEAKING A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM0931168 599 SEA - REPLACED NR 1 ENGINE FWD COMPRESSOR CARBON SEAL AND COOLING TURBINE MOISTURE SEPARATOR SOCK. OPERATIONAL CHECKS COMPLIED WITH AND AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19950414003561995041400356WP 1995 4 14 SCNA95051 119950406A3350EMB1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN MALFUNCTIONED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15152SY 48289 EMERGENCY LIGHTS HAVE FAULT INDICATOR LIGHT FOR OVERWING BATTERY PACK. REMOVED AND REPLACED POWER SUPPLY ABOVE DOOR L-3 AND TESTED GOOD PER MM 33-51-01. 2L73 4F A22WE 19950414003571995041400357WP 1995 4 14 SCNA95052 119950407A3350EMB1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN MALFUNCTIONED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15152SY 48289 OVERWING CABIN EMERGENCY LIGHT FAIL TEST. REPLACED OVERWING POWER SUPPLY. OPS CHECK GOOD. 2L73 4F A22WE 19950414003581995041400358EU 1995 4 14 95ZZZW423 119950326A2612004WS00 WEU SAAB SF340 340B 7860101EU LT ENGINE FAILED A NVEACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO03232AE 1157 340B232 FLT 4905 - JFK - LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED. NO VISIBLE SMOKE OF FIRE. REMOVED AND REPLACED WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19950414003591995041400359EU 1995 4 14 95ZZZW424 119950308A26131734362450 OVERHEAT SENSOR SAAB SF340 340B 7860101EU RT NACELLE MALFUNCTIONED A NVEAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO03202KD 340B202 FLT 4943 - DCA - RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED AFTER TAKEOFF AT 300 FEET. CREW FOLLOWED EMERGENCY CHECKLIST AND SHUT DOWN RIGHT ENGINE. WARNING PERSISTED. WARNINGS STOPPED AFTER BOTH FIRE BOTTLES WERE DISCHARGED. SYSTEM INSPECTIONS SATISFACTORY. RERACKED WEU. 30 MINUTE ENGINE RUN PERFORMED, OPS CHECKED GOOD. REPLACED 2 FIRE BOTTLES AND SQUIBBS. 2L72 4T RTA52EU 19950414003601995041400360NM 1995 4 14 95ZZZW425 119950323A7933162BL704G OIL TEMP IND BOEING727 727228 NM NR 2 ENGINE FAILED A DHLAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO01726DH A1735 20409 ON CLIMB NR 2 ENGINE OIL TEMP INDICATOR PEGGED OUT. NR 2 ENGINE SHUTDOWN AFTER 5 MINUTES AT IDLE THRUST. ENGINE WINDMILLED FOR 12 MINUTES BEFORE LANDING. REMOVED AND REPLACED NR 2 OIL TEMP INDICATOR. GROUND RAN OP CHECKED NORMAL, MM 79-30-0. 2L73 4F A3WE 19950414003611995041400361EU 1995 4 14 95ZZZW426 119950320A3246201072699 SPACER MESSIER 201072015 FOKKERF28 F28MK0100 4990807EU LT MLG MISSING A JBXAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 GL31103ML4560 GLG0113 11444 UPON LANDING IN RDU IT WAS NOTED THAT THE NR 2 MAIN TIRE AND WHEEL ASSEMBLY WAS MISSING FROM THE AIRCRAFT. AXLE NUT WAS ATTACHED TO THE AXLE AND THE BRAKE ASSEMBLY WAS IN PLACE. DURING A TIRE CHANGE THE PREVIOUS NIGHT, THE SPACER HAD BEEN OMITTED DURING REINSTALLATION. 2L72 4F RT 19950414003621995041400362NM 1995 4 14 95ZZZW427 119950328A3260327 BULB BOEING727 72782C 1384026NM RT MLG BURNED OUT A RYNAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 CE07528PC 19597 RIGHT MAIN LANDING GEAR UNSAFE WARNING LIGHT CAME ON DURING GEAR EXTENSION. AIRCRAFT LANDED IN STL WITHOUT FURTHER INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR DOWN AND LOCKED INDICATION BULB. ALL INDICATIONS CHECK NORMAL. (W) 2L73 4F A3WE 19950414003631995041400363WP 1995 4 14 95ZZZW428 119950315A27205914387507 ACT BELLOWS DOUG DC9 DC915F 3022037WP RUDDER LEAKING A Y2PAO OTHER O OTHER DEDESCENT 1 GL23197US 47154 YIP - RUDDER UNRESTRICTED ANNUNCIATOR LIGHT VERY SLOW TO COME ON BELOW 170 KNOTS. REMOVED AND REPLACED ACTUATOR BELLOWS (P/N 5914387507) AND 2 EACH ROD END BEARINGS (P/N REP3F4) AND 2 EACH ROD END BEARINGS (P/N 16393). RERIGGED SYSTEM IAW MM 27-20-6. (W) 2L72 4F A6WE 19950414003641995041400364EU 1995 4 14 95ZZZW429 119950404A3213200920604 GLAND NUT 200920003 STBROSSD3 SD360 8100606EU LANDING GEAR CRACKED A TRBAK NONE O OTHER ININSP/MAINT 1 SO21374MQ230948207 DRG155584 SH3683 DURING FLEET CAMPAIGN INSPECTION OF SHOCK ABSORBER GLAND NUT FOR CRACKS AND CORROSION, FOUND CRACK ON NUT LOWER SECTION .25 INCH FROM RADIOUS 1.5 INCH LONG. (PRC SEALANT WAS MISSING SINCE LAST OVH). NUT WAS REPLACED BY NEW ONE. (W) 2H72 4T A41EU 19950414003651995041400365WP 1995 4 14 95ZZZW430 119950328A3260H146 UPLATCH SWITCH DOUG DC9 DC915F 3022037WP RT MLG WORN A RYNAK NONE N FALSE WARNING CLCLIMB 1 CE07567PC 47153 RIGHT MAIN LANDING GEAR UNSAFE WARNING LIGHT CAME ON DURING GEAR RETRACTION, RECYCLED GEAR, INDICATIONS NORMAL. AIRCRAFT LANDED IN ROA WITHOUT FURTHER INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR UPLATCH SWITCH, OPS CHECKS NORMAL. (W) 2L72 4F A6WE 19950414003661995041400366WP 1995 4 14 95ZZZW431 119950331A323059100615046 RETRACT MECH DOUG DC9 DC915F 3022037WP RIGHT MLG DRY A RYNAK NONE J WARNING INDICATION CLCLIMB 1 CE07567PC 47153 AFTER TAKEOFF FROM BHM THE RIGHT GEAR UNSAFE LIGHT CAME ON. RECYCLED GEAR WITH NO CHANGE IN INDICATION, UPON LANDING IN DAY GEAR INDICATION WAS NORMAL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. LUBED THE RIGHT MAIN LANDING GEAR, (P/N 59100615046) CYCLED GEAR, ALL OPS CHECKED GOOD. (W) 2L72 4F A6WE 19950414003671995041400367WP 1995 4 14 ASAA9580057 119950324A3230 RETRACT MECH DOUG DC9 DC982 3022082WP LANDING GEAR MALFUNCTIONED A ASAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01951AS 49111 OAK - FLT NR 433, ON DEPARTURE UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. ACCOMPLISHED APPROPRIATE CHECKLIST AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A LANDING GEAR EXTENSION TEST, A POSITION AND WARNING INDICATING SYSTEM TEST AND A GEAR CONTROL LEVER AND ANTI-RETRACTION LATCH CHECK PER ASA WORK CARDS AND MANUFACTURERS MAINTENANCE MANUAL. ALSO, RESERVICED THE NOSE STRUT AND CHECKED THE GROUND SENSING SWITCHES ACTUATION. UNABLE TO DUPLICATE ANDY DISCREPANCY. (W) 2L72 4F A6WE 19950414003681995041400368NE 1995 4 14 C2XA95CL051 219950326A73103035681 FILTER AEROSPATR42 ATR42300 8680920EU PWA PW121 PW121 52124NE NR 1 ENGINE DIRTY A C2XACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0918809 090 120414 FLT 3569 - EWR - ABORTED TAKEOFF, FUEL CLOG LIGHT NR 1 ENGINE CAME ON WHEN POWER LEVERS WERE ADVANCED. MAINTENANCE REMOVED AND REPLACED FUEL FILTER IAW PWA MM 72-01-40. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950414003691995041400369SO 1995 4 14 C2XA95CL052 119950326A32414091115 CLIP EMB 120 EMB120RT SO NR 3 MAIN WHEEL SHEARED A C2XAK NONE Z SIGNIFICANT FAILURE REPORT TXTAXI/GRND HDL 1 SW0916702 120078 FLT 3232 - DAY-CLE - BRAKES FAILED WITH ANTI-SKID ON. MAINTENANCE REMOVED AND REPLACED NR 3 WHEEL SPEED TRANSDUCER CLIP. OPS CHECK GOOD IAW EMB-120 MM 32-42-00. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950414003701995041400370WP 1995 4 14 CKSA95008 119950224A57435611425501 TRUNNION DOUG DC8 DC8F55 3021928WP LT MLG CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL232954963096 45803 OSC - DURING D-CHECK, FOUND APPROX 2.75 INCH LONG CRACK, LEFT MLG SUPPORT ATTACHED FITTING. REF DOUG SB 57-94, FIG 1, VIEW FF LOCATION E. REMOVED AND REPLACED LEFT MLG FITTING IAW AD 89-10-04 AND SB 57-94 AND FAA LETTER DATED 11-4-94. (W) 2L74 4F 4A25 19950414003711995041400371NE 1995 4 14 CKSA95013 219950316A7240 DEFUSER CASE DOUG DC8 DC855 3021927WP PWA JT3D JT3D3B 52039NE NR 1 ENG CRACKED A CKSAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23801CK58391 45816 643960 MSLP-KMIA - NR 1 ENGINE SHUTDOWN AT 1742Z DUE TO FIRE WARNING. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED NR 1 ENGINE IAW DC-8 MIP-1, CHAPTER 9 DO TO DIFFUSER CASE CRACK. OPS AND LEAKS CHECK GOOD IAW AIA DC-8 MIP-1 CHAPTER 10. (W) 2L74 4F4 F 4A25 1E8 19950414003721995041400372WP 1995 4 14 HAL95025 119950316A3260008004003 PROX SW DOUG DC9 DC951 3022051WP RT MLG FAILED A HALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP132FOR 135 47742 HNL - FLT NR 508 - AFTER TAKEOFF, RIGHT GEAR UNSAFE LIGHT ON. NORMAL GEAR EXTENSION. ON RETURN TO HONOLULU GEAR DOOR OPEN LIGHT ON WHEN UPLATCH CHECK. CHECKED GEAR SWITCH WIRE AND FOUND OK. INSPECTED GEAR AND UPLOCK AND FOUND OK. REPLACED PROXIMITY BOX. GEAR SWING CHECKED OK. (W) 2L72 4F A6WE 19950414003731995041400373WP 1995 4 14 HAL95026 119950322A335060030431 EEL POWER PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 10753 47662 HNL - THE FORWARD FOUR EMERGENCY LIGHTS WOULD NOT COME ON. REMOVED AND REPLACED THE EMERGENCY LIGHTS BATTERY POWER PACK. THE OPERATIONAL CHECK WAS GOOD. (W) 2L72 4F A6WE 19950414003741995041400374WP 1995 4 14 HAL95027 119950322A3222 STRUT DOUG DC9 DC951 3022051WP NLG LEAKING A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13669HA 47654 FLT NR 517 - OGG-HNL - THE NOSE LANDING GEAR FAILED TO RETRACT ON TAKEOFF. NOSE GEAR STEERING WAS STEERABLE. LEFT ALL GEAR DOWN BECAUSE HANDLE WOULD NOT RETRACT/RAISE. REPACKED NOSE STRUT AS PER MM. SERVICED AND LEAK CHECKED GOOD. MADE GEAR SWING AND THE OPERATION WAS OK. (W) 2L72 4F A6WE 19950414003751995041400375WP 1995 4 14 IXXA199521 119950327A2130 CONNECTOR DOUG DC8 DC863F 302198FWP CABIN PRESS DIRTY A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23784AL 46135 DURING CLIMB-OUT OF GSO, THE CABIN PRESSURIZATION WAS UNCONTROLLABLE BY EITHER MANUAL OR AUTOMATIC SYSTEMS. THE CABIN PRESSURE WAS CYCLING BETWEEN CLIMB AND DESCENT. THE AIRCRAFT RETURNED TO GSO FOR MAINTENANCE. TROUBLESHOOTING REVEALED A DIRTY ELECTRICAL CONNECTOR ON THE CABIN PRESSURE RATION CONTROLLER. THE CONNECTOR WAS CLEANED AND RESECURED. THE AIRCRAFT WAS GROUND PRESSURIZED AND PRESSURIZATION CONTROL OPS CHECKED IAW THE DC-8 MM. CONTROL WAS NORMAL, AND THE AIRCRAFT WS RETURNED TO SERVICE. (W) 2L74 4F 4A25 19950414003771995041400377NE 1995 4 14 TSAA9573050 219950308A7314378200 FUEL PUMP BOEING737 7372Q9 138448MNM PWA JT8 JT8D15 52051NE NR 1 ENGINE SHAFT SHEARED A TSAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP13809AL 4876 21720 P600670 FLT NR 282 - HNL-KOA - DURING CLIMB UNABLE TO REDUCE EPR ON NR 1 ENGINE. NO RESPONSE TO THROTTLE. PRECAUTIONARY SHUTDOWN NR 1 ENGINE IN FLIGHT. RETURNED TO HNL. FOUND FUEL PUMP WITH SHEARED SHAFT. REPLACED NR 1 FCU (PRECAUTIONARY) AND FUEL PUMP IAW PWA MM 73-11-1 AND 73-21-2. JET CALIBRATED IAW FORM M-125. GROUND OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F4 F A16WE E2EA 19950414003781995041400378EU 1995 4 14 VTZA95111 119950314A332042704 LAMP HOLDER JETAIRJETSTMJETSTM4101 1500501EU CABIN FAILED A VTZAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA27302UE 41013 FLT 6444 - BDL-IAD - DURING TAXI THE CABIN WINDOW LIGHT AT SEAT 4A AND 5A WAS INOP AND SMOKING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED BULB AND SECURED SOCKET AND OPENED DMI NR 02333 IAW MEL 33-7 ON THE LIGHT ASSY. IAD LATER CLEARED DMI NR 2333, BY REMOVED AND REPLACED LAMP HOLDER AT SEAT 4A. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950414003791995041400379EU 1995 4 14 VTZA95112 119950320A2120CA06R10SL3SF80 PRESS SW CONNECT BAG JETSTMJETSTM3201 1500217EU LEFT FAILED A VTZAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27488UE 907 FLT 6281 - IAD-HPN - DURING TAXI FOR TAKEOFF, RETURNED TO GATE DUE TO THE LEFT AIR OFF LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 07767 IAW MEL 21-1. IAD LATER CLEARED DMI NR 07767, BY REMOVED AND REPLACED AIR OFF PRESSURE SWITCH CANNON PLUG. OPS CHECKED GOOD. AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950414003801995041400380EU 1995 4 14 VTZA95113 119950321A79211379139H ACTUATOR BAG JETSTMJETSTM3201 1500217EU LT OIL COOLER FAILED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27497UE 904 FLT NR 6592 - IAD-AVP - DURING CRUISE RETURNED TO THE IAD WITH NO FURTHER INCIDENTS, DUE TO THE LEFT OIL COOLER FLAP INDICATING OPEN IN FLIGHT. MAINTENANCE REPLACED THE OIL COOLER FLAP ACTUATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950414003811995041400381EU 1995 4 14 VTZA95114 219950321A73208691691 TT2 SENSOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENGINE DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27483UE 898 FLT 6186 - LYH-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE AND EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 08518 IAW MEL 76-2. MAINTENANCE LATER CLEARED DMI NR 08518 BY CLEANING THE TT2 SENSOR CANNON PLUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA56EU E4WE 19950414003821995041400382EU 1995 4 14 VTZA95115 119950327A5101 STRUCTURE BAG JETSTMJETSTM3201 1500217EU AIR FRAME BIRD STRIKE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 EA27475UE 850 FLT NR 6221 - SWF-IAD - ABORTED TAKEOFF DUE TO A BIRD STRIKE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION WITH NO DAMAGE NOTED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950414003841995041400384WP 1995 4 14 VTZA95121 219950329A732089737527 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE OUT OF ADJUST A VTZAO OTHER O OTHER CRCRUISE 1 EA27485UE 901 P66071 FLT 6941 - LYH-IAD - DURING CRUISE THERE WAS AN ERRATIC TORQUE FLUCTUATION IN THE LEFT ENGINE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE MAX FUEL FLOW DOWN 30 PPH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA56EU E4WE 19950414003931995041400393NE 1995 4 14 95ZZZX1739 219950316A853084088CP CYLINDER DOUG DC3 DC3 3021401WP PWA R1830 R183094 52020NE LT ENG NR 13 FAILED A DJSAEA ENGINE SHUTDOWN UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 GL239382 118 12331 P139763 NR 13 CYLINDER THERMAL SHOCKED APPROXIMATELY 20 MILES EAST OF MKE. LEFT ENGINE ROUGH AND BACKFIRING. SHUT ENGINE DOWN, RETURNED TO MKE. REPLACED NR 13 CYLINDER POWER AND LEAK CHECK SATISFCATORY. RETURNED AIRCRAFT TO SERVICE. 2L72 4R4 R A669 5E4 19950414003941995041400394NE 1995 4 14 95ZZZX1740 219950327A7414SF14LN3 MAGNETO DOUG DC3 DC3 3021401WP PWA R1830 R183092 52020NE RT ENG LT MAG FAILED A MCCAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 SW1124230 782 20197 BP458934 AFTER TAKEOFF, RIGHT ENGINE STARTED TO BACKFIRE AND RUN ROUGH. ENGINE WAS SHUT DOWN AS A PRECAUTIONARY METHOD. UPON TROUBLESHOOTING, FOUND LT MAG BAD. MAG WAS REPLACED WITH A YELLOW TAGGED UNIT. ENGINE WAS GROUND RUN, CHECKED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4R4 R A669 5E4 19950414003951995041400395NM 1995 4 14 95ZZZX1741 119950316A2720653708 PCU BOEING737 7372P6 NM RUDDER MALFUNCTIONED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO172FOR 21355 WITH REFERENCE TO AD T95-06-53. AIRTRAN AIRWAYS, INC., RECEIVED RUDDER PCU PN 65-44861-5, SN 855A OVERHAULED BY NORTEK REPAIR CENTER, INC., FAA. , REPAIR STATION NR YA4R667M. THE RUDDER PCU ON AIRCRAFT EI-CJW (TAT 36,134.6 AND TAC 44104) WAS REMOVED AND REPLACED WITH SERVICEABLE UNIT. ON 3-16-95, PERFORMED ADJUSTMENT TESTS AND LEAK CHECKED PER BOEING 737-200 MM CHAPTER 27-21-91. FUNCTIONAL CHECK FLIGHT ACCOMPLISHED, NO DISCREPANCIES NOTED. AIRCRAFT EI-CJW WAS RETURNED TO SERVICE. 2L72 4F RTA16WE 19950414004071995041400407WP 1995 4 14 9505509995 119950405A5320 FITTING DOUG DC9 DC931 3022065WP FS 718 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FLOORBEAM TO KEEL ATTACH FITTING FS 718. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950414004081995041400408WP 1995 4 14 9505519989 119950405A53204912515 FITTING DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 29R TIE FITTING AT FS 996. REPLACED FITTING PER SRM 51 TO 42. 2L72 4F A6WE 19950414004091995041400409WP 1995 4 14 9505529995 119950406A5320 FITTING DOUG DC9 DC931 3022065WP FS 965 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FLOORBEAM TO BULKHEAD ATTACH FITTING FS 965 AT RBL 44. REPLACED FITTING PER SRM 51 TO 01. 2L72 4F A6WE 19950414004101995041400410WP 1995 4 14 9505539927 119950405A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018920E 45835 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950414004111995041400411WP 1995 4 14 9505549980 119950406A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019344 47440 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ADJUSTED THE CLIPS AND RE-RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950414004121995041400412WP 1995 4 14 9505559955 119950405A7711 EPR INDICATOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01922RW 47182 657492 WHEN POWER LEVERS WERE ADVANCED FOR TAKEOFF, THE NR 2 EPR INDICATION DID NOT INCREASE. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND TRANSMITTER. SYSTEM FUNCTIONALLY TESTED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950414004131995041400413NM 1995 4 14 95UAL767015 119950410A3350 EEL BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29614UA 21875 EEL LIGHTS INOP ON RIGHT HAND SIDE OF BUSINESS CLASS. REPLACED POWER FEEDER, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19950414004141995041400414WP 1995 4 14 95UALD10029 119950406A335059192 EEL JUMPER DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291852U 47811 EEL STRIP ON LEFT OF GALLEY AT DOOR 2L INOPERATIVE. REPLACED EEL JUMPER. 2L73 4F4 F A22WE E23EA 19950414004151995041400415WP 1995 4 14 95UALD10032 119950411A3350 EEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN MALFUNCTIONED A UALAK NONE L NO TEST DEDESCENT 1 WP291845U 48261 RIGHT AFT FLOOR EMERGENCY LIGHTS CAME ON AND STAYED ON DURING FINAL APPROACH. CHECKED WIRING FROM S3-919 TO P1- 7248 AND FROM P1-7248 TO R5-7251. UNABLE TO DUPLICATE PROBLEM. REPLACED BATTERY PACKS U1-7107, U1-7108 AND U1-7105. EEL TESTS GOOD. 2L73 4F4 F A22WE E23EA 19950414004161995041400416NM 1995 4 14 DL72E951164 119950301A5320 SUPPORT BOEING727 727247 138408FNM BS 1130-1148 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 FLOOR SUPPORTS STA 1130 TO 1148 RBL12 AND SMALL CONNECTING STUB SUPPORT WERE FOUND CORRODED. CLEANED CORROSION PER SRM 51-10-6, WITHIN LIMITS 53-20-11 FIG 804, TREATED PER 51-10-2 PG 1. REPLACED STUB SUPPORT. 2L73 4F A3WE 19950414004171995041400417NM 1995 4 14 DL72E951205 119950311A5320 SUPPORT BOEING727 727247 138408FNM BS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 AT HMV, FOUND LOWER FUSELAGE SKIN SUPPORT ANGLE AT FS 720 WITH CORROSION DAMAGE. REPLACED ANGLE PER MM 53-11-10 PG 858 TO 859. 2L73 4F A3WE 19950414004181995041400418NM 1995 4 14 DL72S951084 119950306A57546516221100 SLAT BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 DURING SHOP INSPECTION, FOUND RT WING NR 5 SLAT WITH CRACKED PREVIOUSLY INSTALLED REPAIR DOUBLER. INSTALLED NEW REPAIR PER MM 57-54-0. 2L73 4F A3WE 19950414004191995041400419NM 1995 4 14 DL72S951259 119950324A575465162221100 DOUBLER BOEING727 727232 1384082NM LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 DURING SHOP INSPECTION, DOUBLER ON RIB NR 11 AND 12 WERE FOUND CRACKED INSIDE SLAT PANEL. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19950414004201995041400420NM 1995 4 14 DL72W951074 119950314A7110651968545 COWL BOEING727 727247 138408FNM NR 3 ENG GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV, NR 3 ENGINE NOSE COWL WAS FOUND WITH GOUGED L/E SKIN. REPAIRED PER SRM 54-30-3 FIG 2. 2L73 4F A3WE 19950414004211995041400421NM 1995 4 14 DL72W951202 119950305A5350 FILLET PNL BOEING727 727247 138408FNM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 AT HMV, FILLET PNL 3441 FOUND WITH TIME LIMITED REPAIR. CUT OUT DAMAGE MFG SPLICE REPLACEMENT SECTION AND DOUBLER AS PER SRM 53-30-3 FIG 2, PER 53-50-1 FIG 1. INSTALLED REPAIR PER SRM 53-30-3 FIG 2,PER 53-50-1 FIG 1. 2L73 4F A3WE 19950414004221995041400422NM 1995 4 14 DL72W951336 119950330A5754 RIB BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112825W 21330 A .5 INCH CRACK AT NR 6 SLAT O/B ACT ROD END SUPPORT RIB. FOUND DURING E-1 LTR CK. REPAIRED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950414004231995041400423NM 1995 4 14 DL72W951377 119950403A5754651622199 RIBS BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 DURING SHOP INSP, RIBS 2, 8, 9, 21 WERE FOUND TO BE CRACKED. REPAIRED RIBS PER SRM 57-54-0 FIG 814. DURING SHOP INSPECTION OF NR 4 L/E SLAT. 2L73 4F A3WE 19950414004241995041400424NM 1995 4 14 DL72W951378 119950403A5754651622199 RIB BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 DURING SHOP INSP, RIBS 12 WAS FOUND TO BE CRACKED. REPAIRED PER SRM 57-54-0 FIG 804, FOR LT WING NR 4 SLAT. 2L73 4F A3WE 19950414004251995041400425NM 1995 4 14 DL72W951379 119950403A5754651622199 RIB BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 DURING SHOP INSP, NR 18 RIB WAS FOUND CRACKED. REPAIRED PER SRM 57-50-3 FIG 9, FOR LEFT WING NR 4 L/E SLAT. 2L73 4F A3WE 19950414004261995041400426NM 1995 4 14 DL72W951393 119950401A5530 WEB BOEING727 727247 138408FNM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 WEB CRACKED, TWO 1 INCH CRACKS IN STA 1303 UPPER WEB ABOVE AND TO RT SIDE OF 'S' DUCT (MARKED). FABRICATED REPAIR PLATE PER SRM 51-40-2 FIG 1. 2L73 4F A3WE 19950414004271995041400427NM 1995 4 14 DL73S951251 119950324A57531529517102 VANE BOEING737 737232 1384475NM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11311DL 23083 DURING INSPECTION, RT WING NR 3 FLAP VANE WAS FOUND WITH CRACKED UPPER SKIN. REPAIRED PER SRM 57-53-00 FIG 806. 2L72 4F RTA16WE 19950414004281995041400428NM 1995 4 14 DL757951394 119950403A5315 FLOORBEAM BOEING757 757232 1384965NM BS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 AT HMV, FLOORBEAM AT STA 324 RBL 61 WAS FOUND TO BE CORRODED. THE DAMAGED AREA WAS BLENDED OUT AND REPAIR ANGLE WAS FABRICATED AND INSTALLED PER SRM 53-10-08 FIG 202. AREA WAS TREATED PER SRM 51-10-08. 2L72 4F RTA2NM 19950414004291995041400429NM 1995 4 14 DL757951395 119950327A5753 LE SKIN BOEING757 757232 1384965NM LT TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 AT HMV, THE I/B AFT FLAP LEADING EDGE WAS FOUND TO BE WORN AT O/B END UNDER FAIRING. THE DAMAGE WAS REPAIRED PER SRM 57-53-01. 2L72 4F RTA2NM 19950414004301995041400430NM 1995 4 14 DL757951402 119950402A2530811150417 COFFEE MAKER BOEING757 757232 1384965NM AFT GALLEY SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11658DL 24420 DURING CRUISE HAD BURING ODOR IF AFT GALLEY, DEACTIVATED POWER ODOR DISSIPATED. FOUND ODOR COMING FROM NR 2 AFT COFFEE MAKER. REPLACED DISPENSER, OPERATION NORMAL. 2L72 4F RTA2NM 19950414004311995041400431WP 1995 4 14 DLL17951387 119950329A5311 FRAME LKHEED1011 10113853 5265020WP FS 1063 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 DURING HMV IN ATLANTA, INSPECTION FOUND THE FUSELAGE FRAME CRACKED AT FS 1063 RBL116,BELOW FLOOR LINE AT BOTTOM HOLE. THIS WAS REPAIRED PER SRM 53-12-00. DRILLED REPAIR DOUBLER PER SRM 53-12-00 PG 809. INSTALLED DOUBLER PER SRM 53-12-00. 2L73 4F A23WE 19950414004321995041400432WP 1995 4 14 DLL17951388 119950321A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 875 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, INSPECTION FOUND A TEAR STRAP DISBONDED IN THE C-1 B/B BETWEEN STR 34 TO 35 STA875. INSTALLED REPAIR PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950414004331995041400433WP 1995 4 14 DLL17951389 119950321A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 699 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, INSPECTION FOUND TEAR STRAP DISBONDED IN C-1 B/B AT STA 699 BETWEEN STR 34 TO 35. INSTALLED REPAIR PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950414004341995041400434WP 1995 4 14 DLL17951390 119950321A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 894 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, INSPECTION FOUND TEAR STRAP DISBONDED IN C-1 B/B BETWEEN STR 34 TO 36 AT STA 894. INSTALLED REPAIR PER SRM 53-31-00. 2L73 4F A23WE 19950414004351995041400435WP 1995 4 14 DLL17951391 119950321A5330 TEAR STRAP LKHEED1011 10113853 5265020WP BS 911 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, INSPECTION FOUND A TEAR STRAP DISBONDED IN C-1 BAG BIN AT STA 911 BETWEEN STR 34 TO 35. CLEANED CORROSION AND INSTALLED REPAIR PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950414004361995041400436WP 1995 4 14 DLL17951392 119950327A5720 CAP DOUBLERS LKHEED1011 10113853 5265020WP WS 293/319 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, CUT EXISTING CAP AT IWS 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. UPPER RIB CAPS, APPROX 10 INCHES FROM REAR SPAR. REF VA31744 AND EO 7-59089-3. CUT CAP AT 293.58 AND 319.83 TO FACILITATE FASTENER REMOVAL. FABRICATED DOUBLERS AS PER SRM 57-12-00 PG 805, FOR STA 293.58 AND 319.83. INSTALLED DOUBLERS PER SRM 57-12-00 PG 805. 2L73 4F A23WE 19950414004371995041400437NM 1995 4 14 DLM88950723 119950215A5320 SUPPORT DOUG MD88 MD88 3023688NM BS 1510 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 AT HMV, FOUND LEFT AND RIGHT SIDE TAIL COMPARTMENT LOUVER VENT SUPPORT STRUCTRUE CRACKED AT APPROXIMATE FS 1510. REPAIRED PER SRM 53-05 FIG 66. 2L72 4F RTA6WE 19950414004381995041400438NM 1995 4 14 DLM88951254 119950322A5320 SUPPORT DOUG MD88 MD88 3023688NM TAIL VENT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DURING HMV, FOUND LOUVER SUPPORTS CRACKED LT EXTERIOR THE 2 LOWER SUPPORTS WERE CRACKED AT FWD END. REPAIRED PER SRM 53-05 PG 181, 183, AND 185. 2L72 4F RTA6WE 19950414004391995041400439NM 1995 4 14 DLM88951255 119950320A5330 SKIN DOUG MD88 MD88 3023688NM FS 225 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 DENT WITHIN LIMITS PER SRM 53-04 FIG 38. BLENDED GOUGE, FOUND TO BE OUT OF LIMITS PER SRM 53-04 FIG 38. TRIMED OUT DAMAGED AREA, BEGAN FABRICATING PARTS PER SRM 53-04 FIG 38, FINISHED FABRICATING PARTS PER SRM 53-04 FIG 38. INSTALLED DOUBLERS PER SRM 53-04 FIG 38. 2L72 4F RTA6WE 19950414004401995041400440NM 1995 4 14 DLM88951286 119950328A5240 HORIZ BEAM DOUG MD88 MD88 3023688NM FWD SERV DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, FWD SERVICE DOOR IS CRACKED ON HORIZONTAL BEAM BELOW HINGE ATTACH FITTING. REPAIRED PER SRM 52-05 FIG 25. 2L72 4F RTA6WE 19950414004411995041400441NM 1995 4 14 DLM88951307 119950328A5320 SUPPORT DOUG MD88 MD88 3023688NM AFT FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11940DL 49813 AT HMV, RT TAI AREA LOUVER 2 SUPPORTS CRACKED. REPAIRED PER SRM 53-05 PG 181, PG 183, PG 185. 2L72 4F RTA6WE 19950414004421995041400442NM 1995 4 14 SCNA95053 119950407A33501619 EEL BULB BOEING727 7272J4 1384006NM L 1 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 L-1 DOOR EMERGENCY EXTERIOR SLIDE LIGHT INOPERATIVE. RELAMPED L-1 SLIDE LIGHT. OPS CHECK GOOD. 2L73 4F RTA3WE 19950414004431995041400443WP 1995 4 14 SCNA95054 119950409A2611PU499R3 SMOKE DETECTOR DOUG DC10 DC1015 3022118WP LAVATORY J FAILED A SCNAK NONE N FALSE WARNING ININSP/MAINT 1 GL15151SY 48295 LAVATORY J SMOKE DETECTOR CONTINUOUSLY GOING OFF. REMOVED AND REPLACED SMOKE DETECTOR IN LAV J. OPS CHECKS GOOD IAW MM 26-29-00. 2L73 4F A22WE 19950414004441995041400444NM 1995 4 14 UPS502936 119950407A7120311N50671 FUSE PIN BOEING757 75724APF 1384969NM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01410UP 23732 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 ENGINE O/B FUSE PIN IS MIGRATING OUT, NUT BACKED OFF AND FUSE PIN IS CRACKED. REPLACED FUSE PIN PER UPS EO B757-5440-0431 AND MM 71-00-02. 2L72 4F RTA2NM 19950414004451995041400445NM 1995 4 14 95ZZZW432 119950327A276130186 ACTUATOR 83205501 BOEING747 747122 1384872NM NR 7 SPOILER CRACKED A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23853FT EA1923017 19753 HYDRAULIC FLUID LEAK, RIGHT WING. LEAK FOUND TO BE NR 7 SPOILER ACTUATOR END CAP. REPLACED CAP LEAK. CHECK OK. 2L74 4F A20WE 19950414004461995041400446NM 1995 4 14 95ZZZW433 119950328A2560BACB30P04P6 PIVOT BOLT BOEING757 75723A 1384967NM DOOR L4 MISSING A NOCAK NONE O OTHER ININSP/MAINT 1 EA15757NA 24567 JFK - L4 DOOR SLIDE POSITION RETRACTABLE DOOR INDICATOR FAILED TO EXTEND WHEN DOOR IN ENGAGED POSITION. REPLACED PIVOT BOLT ASSEMBLY PER MM. OPERATIONAL CHECK OK. 2L72 4F RTA2NM 19950414004471995041400447NM 1995 4 14 95ZZZW434 119950328A3350767 EEL BOEING757 75728A 1384976NM CABIN INOPERATIVE A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15750NA 26277 JFK - FOUND R1 DOOR ESCAPE SLIDE EXIT LIGHT INOPERABLE. RELAMPED CHECK OK. (W) 2L72 4F RTA2NM 19950414004481995041400448EU 1995 4 14 95ZZZW435 119950316A7712 TQ IND SAAB SF340 SF340A 7850100EU RT ENG MALFUNCTIONED A CHQACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA23125CH 340A125 PILOT ABORTED TAKEOFF DUE TO RIGHT ENGINE WENT TO 120 PLUS TORQUE. A GROUND RUN WAS PERFORMED WITH THE CTOT SELECTED ON AND OFF. NO DEFECTS WERE NOTED ALL SYSTEMS FUNCTIONAL CHECKED NORMAL. (W) 2L72 4T RTA52EU 19950414004491995041400449WP 1995 4 14 95ZZZW436 119950326A2621893244 CONNECTOR DOUG DC8 DC863F 302198FWP NR 1 FIRE EXT SHORTED A CKSAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23815CK32464 46151 KMIA - NR 1 ENGINE FIRE WARNING WENT OFF AT 0500Z. SECURED NR 1 ENGINE IAW CHECKLIST. FIRE WARNING REMAINED, DISCHARGED ONE FIRE BOTTLE. FIRE WARNING EXTINGUISHED, SYSTEM TEST IS GOOD. FOUND SHORTED CANNON PLUG AT LOWER FIRE LOOP, INBOARD SIDE. REPLACED PLUG SYSTEM, CHECKED NORMAL IAW 26-10-0. ALSO, REMOVED NR 1 FIRE BOTTLE, SERVICED, REINSTALLED IAW 36-20-0, VISUALLY INSPECTED PNEUMATICS AND ENGINE CASE, FOUND NO LEAKS. REFERENCE CKSA95014. 2L74 4F 4A25 19950414004501995041400450EU 1995 4 14 95ZZZW437 119950105A28201608565 VALVE 1608565 FOKKERF28 F28MK0100 4990807EU LT WING LEAKING ALAJBXAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL31108ML579 TR112AK 11484 DURING DEPARTURE (7,000 FEET) ATC CONTROLLER INFORMED CREW FUEL WAS OBSERVED DUMPING FROM THE LEFT WING. FUEL ASSEMETRY LIGHT CAME ON WITH A FUEL INBALANCE AT 700 LBS. AIRCRAFT RETURNED WITHOUT INCIDENT. FUEL STOPPED LEAKING EN ROUTE TO MDW. MAINTENANCE DISCOVERED LEFT WING FUEL OVERFLOW VALVE FAULTY. 2L72 4F RT 19950414004511995041400451NM 1995 4 14 95ZZZW438 119950130A335058791 EEL CONNECTOR BOEING737 737242 1384477NM CABIN BROKEN A A6XAK NONE L NO TEST ININSP/MAINT 1 SO13159PL 21186 ESCAPE PATH LIGHTING INOP FROM ROW 3-8. REPAIRED PIN AT CANNON PLUG AT WALL CONNECTION. OPS CHECK NORMAL. 2L72 4F A16WE 19950414004521995041400452NM 1995 4 14 95ZZZW439 119950324A33501000679 EEL BOEING737 737242 1384477NM CABIN OPEN A A6XAK NONE L NO TEST ININSP/MAINT 1 SO13159PL 21186 CONTROL CABIN EMERGENCY LIGHT WILL NOT TURN ON. REMOVED AND REPLACED CONTROL CABIN EMERGENCY LIGHT ASSY. OPS CHECK NORMAL IAW MM 33-51-11. 2L72 4F A16WE 19950414004531995041400453WP 1995 4 14 AALA950575 119950403A33207094 BALLAST DOUG DC9 DC982 3022082WP CABIN OVERHEATED A AAALAO OTHER AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW077531A 47284D 49923 LGA - FLT 0339 - AT THE GATE PRIOR TO PASSENGER BOARDING, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN AT PASSENGER SEAT 27AB NEAR OVERHEAD BIN. FIRE DEPARTMENT SUMMONED AND FIRE EXTINGUISHED. CHECK OF CABIN OVERHEAD REVEALED FLOURESCENT LIGHT BALLAST AT PASSENGER SEAT 27AB HAD FAILED RESULTING IN ELECTRICAL FIRE. AIRCRAFT MAINTENANCE FERRY LGA/TUL FOR REPAIRS TO LIGHT SYSTEM AND OTHER CONSEQUENTIAL DAMAGE TO CABIN INTERIOR AND FUSELAGE. (W) 2L72 4F A6WE 19950414004541995041400454WP 1995 4 14 ASAA9580047 119950313A33506011779 EEL BATTERY PACK DOUG DC9 DC983 3022083WP AFT CARGO COMPT DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 OAK - DURING MAINTENANCE CEHCK, THE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950414004551995041400455EU 1995 4 14 AWXA9500104 219950223A7320 PMC LINE BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM563B2 13802EU LT ENGINE LOOSE A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28323AW 23684 IND - FLT 280 - DURING CLIMB, THE LEFT ENGINE BEGAN SURGING ABOUT 5 TO 7 PERCENT N1. ENGINE SURGED AT HALF THROTTLE BUT NOT AT IDLE. ALL FOUR ENGINE GAUGES SURGED WITH ACCOMPANYING YAW PROBLEMS. ENGINE SURGED AGAIN DURING REVERSE ON LANDING ROLL, PMC'S ON. AUTO THROTTLE ON/OFF NO DIFFERENCE. A/C RETURNED TO IND WITHOUT FURTHER INCIDENT. MX INSPECTED NR 1 ENG INLET AND EXHAUST, NO DEFECTS NOTED. CLEANED CONNECTION AT PMC/MEC. FOUND PMC SENSE LINE LOOSE AT TOP COMP CASE. RETIGHTENED AND RESAFTIED LINE. GROUND RUN ENGINES TO TAKEOFF PWR, OPS CHECK OK. IDLE CHECK OPS OK. GRD RUN WITH ENG BLEEDS ON/OFF AND PMS'S ON/OFF, OPS OK. NO OTHER DEFECTS NOTED. A/C RETURNED TO SERVICE. (W) 2L72 4F4 FRTA16WE E21EU 19950414004561995041400456EU 1995 4 14 C2XA95IA039 119950321A3350167006 EEL LAMP AEROSPATR72 ATR72212 EU CABIN FAILED A C2XAK NONE L NO TEST TXTAXI/GRND HDL 1 SW0969902 385 IAH - FLT 2738 - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS NEAR THE LAST TWO ROWS OF SEATS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMPS, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950414004571995041400457WP 1995 4 14 CKSA95014 119950326A2612CA06KE10SL4S CONNECTOR DOUG DC8 DC863F 302198FWP NR 1 ENG SHORTED A CKSAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23815CK32464 46151 KMIA - NR 1 ENGINE FIRE WARNING WENT OFF AT 0500Z. SECURED NR 1 ENGINE IAW CHECKLIST. FIRE WARNING REMAINED, DISCHARGED ONE FIRE BOTTLE. FIRE WARNING EXTINGUISHED, SYSTEM TEST IS GOOD. FOUND SHORTED CANNON PLUG AT LOWER FIRE LOOP, INBOARD SIDE, REPLACED PLUG SYSTEM, CHECKED NORMAL IAW 26-10-0. ALSO REMOVED NR 1 FIRE BOTTLE, SERVICED, REINSTALLED IAW 36-10-0. ALSO, REMOVED NR 1 FIRE BOTTLE, SERVICED, REINSTALLED IAW 36-20-1, VISUALLY INSPECTED PNEUMATICS AND ENGINE CASE, FOUND NO LEAKS. REFERENCE 95ZZZW436. 2L74 4F 4A25 19950414004611995041400461NM 1995 4 14 TWRA9524 119950324A5210 HANDLE BOEING747 747121 1384871NM CREW DOOR JAMED A TWRAK NONE O OTHER TXTAXI/GRND HDL 1 EA15613FF 19647 CREW SERVICE DOOR BUTTERFLY HANDLE DOES NOT RETRACT CAUSING DOOR TO JAM ON DOOR FRAME, DOOR WOULD BE UNABLE TO OPEN DURING AN EMERGENCY. LUBRICATED ALL ASSOCIATED LINKAGES DOOR OPS CHECK OK (W) 2L74 4F A20WE 19950414004781995041400478WP 1995 4 14 95ZZZX1769 119950326A324441X15018 TIRE CAP 95608591 DOUG DC9 DC951 3022051WP MLG SEPARTED A A4JAO OTHER O OTHER CLCLIMB 1 SO15920PJ JAN76812 47677 EWR - FLT 220 - AFTER TAKEOFF, ADVISED BY ATC OF TIRE DEBRIS ON RUNWAY. LANDED AT TPA, FOUND BLOWN NR 4 TIRE, RIGHT AFT FLAP DAMAGE, RIGHT GEAR WING DOOR LINKAGES AND FITTINGS DAMAGED. REPLACED NR 3 AND NR 4 WHEEL ASSEMBLIES AND NR 4 BRAKE. REPLACED ALL MISSING/DAMAGED HARDWARE ON RT GEAR WING DOOR. REPAIRED RIGHT FLAP IAW DOUGLAS SRM 57-03. PERFORMED LANDING GEAR RETRACTION TEST. TEST NORMAL. RETURNED TO SERVICE. 2L72 4F A6WE 19950414004791995041400479 1995 4 14 95ZZZX1770 319950317A61124E30171 DEICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE RIGHT PROPELLER MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01854CA198 UE60 DE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 198 HOURS AGO AT WHICH TIME THE BOOT WAS INSTALLED. UPON INSPECTION OF BOOT REMOVED, DISCOVERED THE PAINT APPLIED TO THE BLADE WAS STUCK TO GLUE ON THE BOOT. 2L72 4T RTA24CE 19950414004801995041400480WP 1995 4 14 CAL950218 119950320A3350 EEL BATTERIES DOUG DC9 DC982 3022082WP CABINS DISCHARGED A VTZAK NONE L NO TEST ININSP/MAINT 1 EA2734838 49634 IAH - FLT 0403 - INSPECTION FOUND SEVERAL ROWS OF EMERGENCY LIGHTING INOP. (ROWS 6-10 AND 17-23). BATTERY PACKS REPLACED, OPS CHKS GOOD. (X) 2L72 4F A6WE 19950414004811995041400481NM 1995 4 14 CAL950222 119950318A253042500019 COFFEE MAKER BOEING727 727243 138408DNM FWD GALLEY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09174131185110778 22165 EWR - FLT 1406 - THE FORWARD GALLEY OUTBOARD COFFEE MAKER BEGAN TO SMOKE WHEN TURNED ON WHILE IN-FLIGHT. THE COFFEE MAKER CIRCUITS WERE DEACTIVATED AND THE SMOKE CEASED. THE FORWARD GALLEY OUTBOARD COFFEE MAKER WAS REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD. IN ADDITION, THE FORWARD GALLEY INBOARD COFFEE MAKER WAS INSPECTED AND NO DEFECTS WERE NOTED. (X) 2L73 4F RTA3WE 19950414004821995041400482NM 1995 4 14 CAL950232 119950326A29136507506 HYD PUMP BOEING737 7373Q8 1384670NM NR 2 ENGINE LEAKING A CALAOH OTHER DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW09143849579 26313 EWR - FLT 1416 - THE B-SYSTEM HYDRAULIC QUANTITY BEGAN TO DROP ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE HYDRAULIC LOW PRESSURE LIGHT WHILE ON APPROACH TO EWR. THE NR 2 ENGINE HYDRAULIC PUMP WAS TURNED OFF PER 'ABNORMAL' PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F RTA16WE 19950414004831995041400483WP 1995 4 14 95UALD10033 119950412A3350 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291845U 48261 EEL LIGHTS ON AFT LEFT SIDE BY 3L ARE ON. REPLACED BATTERY PACK. LIGHTS GROUND CHECK NORMAL. 2L73 4F4 F A22WE E23EA 19950414004841995041400484WP 1995 4 14 95UALD10034 119950412A3350 EEL WIRE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST DEDESCENT 1 WP291845U 48261 EMERGENCY FLOOR LIGHTS ROW 29 TO REAR OF CABIN ON BOTH SIDES CAME ON DURING DESCENT. REPAIRED PIGGY BACK WIRE FROM S3-919 PIN 26 TO S3-726 PIN 33X. 2L73 4F4 F A22WE E23EA 19950414004851995041400485SO 1995 4 14 COM11857 119950412A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01164D 1371913719 120164 DURING INSPECTION TASK 5720-551/650-01I AND 5720-552/652-01I THE FOLLOWING WING SKIN SUPPORTS WERE FOUND TO BE CRACKED. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N 120-17056-013, 2 EA, 120-17056-015, 4 EA, 120-17056-017, 2 EA, 120-17056-019, 2 EA, 120-17057-007, 1 EA, 120-17057-005, 1 EA, 120-17057-006, 1 EA, 120-17059-017, 1 EA. 2L72 4T RTA31SO 19950414004861995041400486NE 1995 4 14 COM11858 219950412A73207863904 HMU EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01244CA53 120217 115454 LEFT ENGINE STARTS, BUT WILL NOT ACCELERATE BEYOND MIN FLOW. REPLACED THE ENGINE HMU. 2L72 4T4 TRTA31SO E20NE 19950414004871995041400487SW 1995 4 14 COM20361 119950411A3260IEN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DEFECTIVE A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01459AM AC700 RT MLG IS CYCLING IN THE UP POSITION. REPLACED THE RT MLG UP LIMIT SWITCH. 1L72 4T A8SW 19950414004881995041400488 1995 4 14 COM20362 419950411A3418 SAS WIRE SWRNGNSA227 SA227AC 8780603SW GLARESHIELD CHAFED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01458AM AC699 SAS FAULT LIGHT FLASHING IN FLIGHT. REPAIRED CHAFED WIRE AT INSTRUMENT PANEL GLARE SHIELD. 1L72 4T A8SW 19950414004891995041400489EU 1995 4 14 COM31058 119950411A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA4656 401 NOV920500 340A064 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950414004901995041400490EU 1995 4 14 COM31059 119950411A324650092371 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA3545 393 MAY930529 340A064 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. 2L72 4T RTA52EU 19950414004911995041400491EU 1995 4 14 COM31060 119950411A26131734362450 HEAT DETECTOR SAAB SF340 SF340A 7850100EU RT NACELLE DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01370CA 340A010 RT TAILPIPE HOT WARNING ACTIVATED. REPLACED LOOSE SEALANT AT RT TAILPIPE HEAT DETECTOR. 2L72 4T RTA52EU 19950414004921995041400492SW 1995 4 14 MEJA9503001 119950328A71202762114003 TRUSS SWRNGNSA227 SA227AC 8780603SW NR 1 ENGINE CRACKED E AMEJAK NONE O OTHER ININSP/MAINT 1 SW17378PH AC575 DURING AN AIRCRAFT PHASE 3 INSPECTION, THE NUMBER ONE ENGINE TRUSS WAS FOUND TO BE CRACKED AT THE UPPER FORWARD FIREWALL ATTACH POINT. REPLACED TRUSS WITH NEW TRUSS IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL 71-20-20. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950414004931995041400493 1995 4 14 MWEA95170 419950411A3418 AOA TRANSDUCER TELEDYNESYST80098717 DOUG DC9 DC932 3022066WP LEFT MALFUNCTIONED A MWEAO OTHER N FALSE WARNING CLCLIMB 1 GL31301ME 0031 47190 PILOT REPORTS DURING CLIMB, STALL INDICATION FAIL AND WINDSHEAR INOP ANNUNCIATOR ILLUMINATED. STALL ANNUNCIATOR FINALLY WENT OUT WHEN FLAPS WENT TO 40 ON LANDING. WINDSHEAR STAYED ILLUMINATED. MAINTENANCE FOUND LT ANGLE OF ATTACK TRANSDUCER TESTING BAD. REMOVED AND REPLACED LT AOA TRANSDUCER. OPS CHECK GOOD IAW MM 34-14-00. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950414004941995041400494NM 1995 4 14 SWAA95286 119950406A2911623337 HYD PUMPS BOEING737 7372H4 138448CNM LT/RT ENGINE MALFUNCTIONED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0796SW 23055 IN FLIGHT, NUMBER 1 AND 2 ENGINE HYDRAULIC PUMPS INDICATED LOW PRESSURE, 'A' SYSTEM QUANTITY DISPLAYED ZERO. AIRCRAFT RETURNED TO SAT AND MADE AN UNEVENTFUL LANDING. AFTER LANDING, SYSTEM 'A' INDICATED 1.5 GAL AND BEFORE REACHING GATE, INDICATED 2.5 GAL. FOUND O-RING RUPTURED ON NR 2 'A' SYSTEM PRESSURE SWITCH. REMOVED AND REPLACED BOTH ENGINE DRIVEN PUMPS, LOW PRESSURE SWITCH, CASE DRAIN FILTERS, AND SYSTEM 'A' FILTER. OP/PRESSURE CHECKED SYSTEM PER BOEING MM, NR 1 PUMP S/N MX398721 AND NR 2, MX369280. 2L72 4F A16WE 19950414004951995041400495NM 1995 4 14 SWAA95287 119950410A7830693735732 TR MODULE BOEING737 7372H4 138448CNM LT/RT ENGINE MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0723SW 21338 AFTER DEPARTURE, THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH ISOLATION PRESSURE SWITCHES AND T/R ISOLATION MODULE. LEAK AND OPS CHECKED NORMAL PER BOEING MM. 2L72 4F A16WE 19950414004961995041400496NM 1995 4 14 SWAA95288 119950409A7933 CONNECTOR BOEING737 7372H4 138448CNM NR 1 ENGINE BROKEN A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0793SW 22965 DURING CLIMBOUT, NUMBER 1 ENGINE OIL TEMP INDICATOR ENTERED YELLOW RANGE FOR 14 MINUTES. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NR 1 ENGINE OIL TEMP SENSOR CANNON PLUG PIN B BROKEN. REPLACED PIN AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING MM. 2L72 4F A16WE 19950414004971995041400497NM 1995 4 14 SWAA95289 119950408A3350 EEL WIRE BOEING737 7373H4 1384600NM CABIN BROKEN A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07335SW 23939 FIFTEEN MINUTES BEFORE PUSHBACK, EMERGENCY LIGHTS ILLUMINATED WITH NORMAL AIRCRAFT POWER APPLIED AND SWITCH IN ARMED POSITION. INSPECTED AND REPAIRED WIRE ON AFT GALLEY EMERGENCY LIGHT SWITCH PER BOEING MM. 2L72 4F RTA16WE 19950414004981995041400498NM 1995 4 14 SWAA95290 119950408A5240 SKIN BOEING737 7373H4 1384600NM SERVICE DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07326SW 23690 DURING SCHEDULED B/C CHECK, FOUND FWD SERVICE DOOR UPPER HINGE CUTOUT CRACKED IN UPPER CORNER. REPAIRED PER SWA RA 1-252-207. 2L72 4F RTA16WE 19950414004991995041400499NM 1995 4 14 SWAA95291 119950408A5210 SKIN BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07326SW 23690 DURING SCHEDULED B/C CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED IN LOWER CORNER. REPAIRED PER SWA RA 1-352-206. 2L72 4F RTA16WE 19950414005001995041400500NM 1995 4 14 SWAA95292 119950408A5320 STRAP BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07331SW 23695 DURING SCHEDULED QUARTER D-CHECK, FOUND STABILIZING STRAP IN E/E COMPT CRACKED AT BS 312, AT BOTTOM OF FLOORBEAM, BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950414005011995041400501NM 1995 4 14 SWAA95293 119950408A5330 SKIN BOEING737 7372H4 138448CNM BS 767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0724SW 20925 DURING SCHEDULED B-CHECK, FOUND FUSELAGE SKIN CRACKED .75 INCH AT BS 767 AND STRINGER 19R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950414005021995041400502NM 1995 4 14 SWAA95294 119950408A5414 SKIN BOEING737 7373H4 1384600NM NR 2 ENG STRUT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07331SW 23695 DURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING. CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN. INSTALLED DOUBLER PER ACO 6135-54. 2L72 4F RTA16WE 19950414005031995041400503NM 1995 4 14 SWAA95295 119950408A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0796SW 23055 DURING SCHEDULED QUARTER D-CHECK, FOUND FUSELAGE SKIN CRACKED 1.2 INCH AT AC GROUND SERVICING CUTOUT, RBL 5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950414005041995041400504 1995 4 14 UPS202937 419950412A34426226342024 CRT BOEING727 727108C 1384039NM LT FLIGHT DECK FAILED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01936UP 19503 PILOT REPORTED, SMOKE IN FLIGHT DECK ON INBOUND LEG TO PHL. CAPT'S UPPER CRT IS SUSPECT DO TO SCREEN BLANKED AFTER FUMES AND SMOKE, NOTICED BY FLIGHT CREW. REPLACED CRT ON CAPTAIN'S SIDE. 2L73 4F A3WE 19950414005051995041400505NM 1995 4 14 UPS202938 119950411A3260 DN LOCK SWITCH BOEING727 72727C 138400JNM NLG DIRTY A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01914UP 19246 PILOT REPORTED, THE NOSE GEAR UNSAFE LIGHT REMAINED ON WHEN THE LANDING GEAR WAS LOWERED, TWO RECYCLES, BOTH PRODUCED SAFE INDICATIONS. INSPECTED NLG, NO DEFECTS FOUND. CLEANED AND RESECURED NLG LOCK SWITCH AND SWUNG GEAR SEVERAL TIMES PER MM 32-61-21. SYS OPS CK NORMAL. 2L73 4F A3WE 19950414005061995041400506NM 1995 4 14 UPS202940 119950412A3350 EEL BOEING727 72727C 138400JNM FLIGHT DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01911UP 19119 SUPPLEMENTAL MRR - MAINTENANCE REPORTED, COCKPIT EMERGENCY EXIT LIGHT WILL NOT OPERATE OFF ARM SWITCH. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSY (S/N 4062) OFF, (S/N 4108) ON AND OPS CKD GOOD. 2L73 4F A3WE 19950414005071995041400507NM 1995 4 14 UPS502937 119950412A5753 SKIN BOEING757 75724APF 1384969NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01427UP 25458 WHILE IN 'C' CHECK, MAINTENANCE FOUND DELAMINATION ON LT O/B AFT FLAP. INSTALLED REPAIR PER SRM 51-40-17. 2L72 4F RTA2NM 19950414005081995041400508NM 1995 4 14 ASAA9540001 119950221A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROWS 1 THROUGH 3. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (Z) 2L72 4F RTA16WE 19950414005091995041400509NM 1995 4 14 ASAA9555 119950208A3350 EEL WIRING BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01782AS 25113 SEA - CHECK -- AFT 3 EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED WIRING HARNESS. (X) 2L72 4F RTA16WE 19950414005331995041400533EA 1995 4 14 95ZZZX1794 119950404A5312C2F5533 BULKHEAD DHAV DHC2 DHC2* 2800108EA EMPENNAGE CORRODED A ERHAK NONE O OTHER ININSP/MAINT 1 AL032740X 579 AFTER REMOVING HORIZONTAL STABILIZER ATTACH BRACKET, C2FS543A, TO INCORPORATE MOD 2/1338, BULKHEAD FOUND PERFORATED BY CORROSION. DAMAGE WAS NOT APPARENT UNTIL FITTING WAS REMOVED. ALL AREAS ON TAIL WHERE STEEL FITTINGS ARE RIVETED TO ALUMINUM STRUCTURE SHOULD BE SUSPECT. AIRPLANE IS OPERATED AS A SEAPLANE AND IS OCCASIONALLY OPERATED IN SALT WATER. 1H71 3R A806 19950414005341995041400534EA 1995 4 14 95ZZZX1795 119950404A5511 SPAR DOUBLER DHAV DHC2 DHC2* 2800108EA HORIZ STAB CORRODED A ERHAK NONE O OTHER ININSP/MAINT 1 AL032740X 579 HORIZONTAL STABILIZER REAR SPAR DOUBLERS EXTENDING FROM STATION ZERO TO 40 ON UPPER AND LOWER FLANGES OF SPAR WERE FOUND CORRODED UNDER ELEVATOR HINGE BRACKETS AND REAR ATTACH FITTING. STEEL BRACKETS RIVETED TO ALUMINUM STRUCTURE ON SEAPLANES ARE SUBJECT TO CORROSION. DOUBLERS WERE REPLACED. ALL PARTS IPOXY PRIMED. 1H71 3R A806 19950414005491995041400549EU 1995 4 14 VTZA95108B 119950315A5270MS161065 SWITCH BAG JETSTMJETSTM3201 1500217EU BAGGAGE POD BROKEN WIRE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27483UE 898 IAD/HPN - FLT 6284 - DURING TAKEOFF AT 2145 HRS ON 3-15-95, ABORTED TAKEOFF DUE TO THE POD DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 08516 IAW MEL 52-1 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 08516 ON 3-18-95 BY REPAIRING A BROKEN WIRE ON THE POD DOOR WARNING SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950414005501995041400550WP 1995 4 14 95ZZZZ202 119950314A3350GE305 EEL BULB CVAC 440 440 2422902WP CABIN FAILED A FLTAK NONE L NO TEST ININSP/MAINT 1 WP09968N 462 FOUND THE NR 4 CABIN EMERGENCY LIGHT BULB BURNED OUT. REPLACED BULB, SYSTEM CHECKS GOOD. 2L72 4R 6A6 19950414005511995041400551NM 1995 4 14 95ZZZZ203 119950224A551165382057 SPAR BOEING727 727281 138408NNM HORIZ STAB CORRODED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07905PG44144 20571 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ALONG THE INSIDE OF THE FWD LOWER SPAR OF THE HORIZONTAL STABILIIZER. 2L73 4F A3WE 19950414005621995041400562CE 1995 4 14 95ZZZZ214 119950327A73311303800101 FUEL FLOW GAUGE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE COCKPIT INOPERATIVE A AMASAK NONE O OTHER TXTAXI/GRND HDL 1 SW01139ZV54 UE139 FUEL FLOW INDICATOR ON RT SIDE INOPERATIVE. SUGGEST IMPROVEMENT OF INTERNAL COMPONENTS TO INCREASE RELIABILITY. 2L72 4T4 TRTA24CE E26NE 19950414005631995041400563NM 1995 4 14 95ZZZZ215 119950331A793165B90115 OIL LINE BOEING747 747122 1384872NM NR 2 ENGINE DAMAGED A P5CAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23852FT 19757 ANC-ORD - EN ROUTE THE NR 2 ENGINE EXPERIENCED A GRADUAL LOSS OF OIL. WHEN OIL TEMPERATURE STARTED TO RISE AND LOW PRESSURE LIGHT STARTED TO FLICKER, THE ENGINE WAS SHUTDOWN USING ALTERNATE PROCEDURES. LANDED ORD WITHOUT INCIDENT. MAINTENANCE REPLACED OIL LINE TO DIFFERENTIAL PRESSURE TRANSMITTER DUE TO A PIN HOLE LEAK. SERVICED OIL RESERVOIR. LEAK CHECK NORMAL. REPLACED OIL FILTER AS REQUIRED PER MM. ACFT RELEASED FOR FLIGHT. 2L74 4F A20WE 19950414005641995041400564NM 1995 4 14 95ZZZZ216 119950330A80127265742 START VALVE BOEING747 747122 1384872NM NR 3 ENGINE FAILED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP23851FT 19756 VCP-CCS - EN ROUTE, THE NR 3 ENGINE START LIGHT CAME ON. ENGINE SHUTDOWN AND ACFT DIVERTED TO GIG. REMOVED AND REPLACED NR 3 ENGINE START VALVE IAW MM 80-10-00, AND CHANGED NR 3 ENGINE STARTER AS PRECAUTIONARY. OPERATIONAL CHECKS NORMAL. ACFT RELEASED FOR FLIGHT. 2L74 4F A20WE 19950414005651995041400565WP 1995 4 14 95ZZZZ217 119950329A5320 ANGLE LKHEED1011 10113851 5265010WP FS 328 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION MAIN CABIN FLOOR AREA FLOOR SUPPORT AT STA 328 RT SIDE AND AFT OF FLIGHT ATTENDANT SEAT HAS CORROSION. REMOVED CORRODED FLOOR SUPPORT CLEANED AND TREATED AREA FABRICATED AND INSTALLED ANGLE PER SRM 53-21-01. 2L73 4F A23WE 19950414005661995041400566WP 1995 4 14 95ZZZZ218 119950329A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 297-349 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FWD BAR FLOOR AREA STA 297 TO STA 349 RT SIDE 4TH SEAT TRACK HAS CORROSION. REMOVED SECTION OF SEAT TRACK CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-30-03. 2L73 4F A23WE 19950414005671995041400567WP 1995 4 14 95ZZZZ219 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 328 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FWD RT SIDE O/B OF 4TH SEAT TRACK BETWEEN STA 328 AND STA 297 FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-30-3. 2L73 4F A23WE 19950414005681995041400568WP 1995 4 14 95ZZZZ220 119950328A5751 SKIN DOUG DC8 DC862 3021970WP RT AILERON CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT WING O/B AILERON LOWER SURFACE SKIN AT I/B END HAS CORROSION BULGING AROUND RIVETS. REMOVED CORROSION, TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950414005691995041400569WP 1995 4 14 95ZZZZ221 119950328A5752 AILERON DOUG DC8 DC862 3021970WP LT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LT WING I/B AILERON O/B TAB HAS BULGING CORROSION AT FASTENERS AT I/B END LOWER SURFACE. REMOVED CORROSION AND TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 51-1-9. 2L74 4F 4A25 19950414005701995041400570WP 1995 4 14 95ZZZZ222 119950328A5320 DOUBLER DOUG DC8 DC862 3021970WP FS 225-235 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO191805 45899 LEVEL 2 CORROSION, RT SIDE FLOOR LEVEL FINGER DOUBLERS ATTACHED TO FRAME AT FS 225 TO 235 HAVE CORROSION. REMOVED DAMAGED AREA, CLEANED AND TREATED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-01-0. 2L74 4F 4A25 19950414005711995041400571NE 1995 4 14 95ZZZZ223 219950401A7230 FAN BLADES BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE DAMAGED A P5CAO OTHER C F.O.D. LDLANDING 1 WP23851FT 19756 662346 VCP - CREW FOUND 4 DAMAGED FAN BLADES IN NR 4 ENGINE. SUSPECT BIRD STRIKE. LANDING WAS MADE IN EXTREME WEATHER CONDITION. MAINTENANCE INSPECTED NR 4 ENGINE IAW MM 71-00-00. NO OTHER DEFECTS FOUND. FOUR SETS OF FAN BLADES WERE REPLACED PER MM 72-31-01. ACFT RELEASE FOR SERVICE. 2L74 4F4 F A20WE E20EA 19950414005721995041400572 1995 4 14 95ZZZZ224 319950330A61124E30171 DE-ICE BOOT BEECH 1900 1900D 1154162CE LT PROP MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01833CA UE24 DE-ICE BOOT SEPERATED FROM PROP DURING FLIGHT. PROBLEM APPEARS TO BE WITH ADHESION OF PAINT ON PROP BLADE. BOOT IS GLUED TO PAINTED SURFACE. 2L72 4T RTA24CE 19950414005731995041400573SO 1995 4 14 C2XA95CL056 119950403A3260MS34701106S CONNECTOR EMB 120 EMB120RT SO LT/RT MLG DIRTY A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0915713 120114 CLE-BUF - FLT 3216 - CREW HEARD CLICK, THEN NOTICED STRONG ELECTRICAL SMELL FOLLOWED BY STICK SHAKER/PUSHER ACTUATION WHILE PARKED AT GATE. MAINTENANCE CLEANED AND RESEATED PROX SENSOR CANNON PLUGS ON LEFT AND RIGHT MAIN GEARS. OP'S CHECKED STALL WARNING SYSTEM GOOD. ACFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950414005741995041400574SO 1995 4 14 C2XA95IA041 119950330A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. ACFT APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950414005751995041400575SO 1995 4 14 C2XA95IA042 119950330A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURNG C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. ACFT APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950414005761995041400576SO 1995 4 14 C2XA95IA047 119950331A3232WTC22461 ACTUATOR EMB 120 EMB120RT SO RT MLG DOOR OUT OF ADJUST A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916731 120190 PNS - DLT 2801 - AFTER TAKEOFF, THE RIGHT MLG WOULD NOT RETRACT, AND THE GREEN LIGHTS REMAINED ILLUMINATED. MAINTENANCE INSPECTED THE GEAR AND RESECURED AND ADJUSTED THE RIGHT INBOARD LANDING GEAR DOOR ACTUATOR ROD END IN REFERENCE TO EMB 120 MM 32-12-00. OPERATIONAL CHECKS GOOD, ACFT RELEASED FOR SERVICE. (Z) 2L72 4T RTA31SO 19950414005771995041400577NM 1995 4 14 HAC000002 119950208A531465564417 KEEL BEAM BOEING727 727281 138408NNM BS 950-1010 CORRODED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07905PG44144 20571 IN THE PROCESS OF COMPLYING WITH SB 53-0176, KEEL BEAM CHORD PIN 65-56441-7 WAS FOUND TO BE BADLY CORRODED AT STA 970. DURING INSPECTION OF THE PART THERE ARE INDICATIONS THAT IT WASN'T CORROSION TREATED PROPERLY. THERE COULD BE MOISTURE BUILD UP IF DRAIN HOLES ARE PLUGGED. (Z) 2L73 4F A3WE 19950414005781995041400578NM 1995 4 14 P2EA95003 119950404A793042D107A1 BYPASS SWITCH BOEING737 737247 138448DNM NR 2 ENGINE FAILED A P2EAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 CE05204AU 19603 MCI - FLT 102 - PRECAUTIONARY IN FLIGHT SHUTDOWN OF NR 2 ENGINE INBOUND TO MCI DUE TO FILTER BYPASS LIGHT. AN EMERGENCY WAS DECLARED BY FLIGHT CREW. ACFT LANDED WITHOUT REPORTED INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL FILTER BYPASS SWITCH. (Z) 2L72 4F A16WE 19950414005791995041400579NE 1995 4 14 VTZA95122 219950406A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT FAILED A VTZAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27309UE 41022 75015C PWM-IAD - FLT 6500 - DURING TAXI FOR TAKEOFF, RETURNED TO THE GATE DUE TO THE LT ENGINE FLAMING-OUT. ACFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. CONTRACT MAINTENANCE PERFORMED A DECELERATION CHECK WITH NO DEFECTS NOTED. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T4 TRTA41NM E18NE 19950421000011995042100001EU 1995 4 21 9505553242 119950410A2432350L5100508 LIMITER AIRBUS320 A320211 3930320EU NR 2 BATTERY MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01342NW6858 2071 381 AFTER TAKEOFF FROM MSP, THE EMERGENCY GENERATOR FAULT LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS LOWERED AND RETURNED WHEN THE GEAR WAS RAISED. FLIGHT CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 BATTERY CHARGE LIMITER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950421000021995042100002NE 1995 4 21 9505569762 219950411A7310 FUEL LINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 2 ENGINE LEAKING A NWAAE ENGINE SHUTDOWN RK PARTIAL RPM/PWR LOSS FLUID LOSS DEDESCENT 1 GL01762NW 47395 676154 ON DESCENT, NR 2 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT. FLIGHT LANDED IN PVD WITHOUT INCIDENT. THE ENGINE WAS SHUT DOWN WHILE TAXIING TO THE GATE. MAINTENANCE FOUND FUEL LEAKING FROM THE LINE CONNECTING THE P AND D VALVE TO THE FUEL OIL COOLER. THE LINE WAS RESEALED AND CHECKED FOR LEAKS. NONE FOUND. THE ENGINE WAS RUN-UP AND CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950421000031995042100003 1995 4 21 9505579151 419950413A34172587400176 ADC DOUG DC9 DC914 3022034WP E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018909E28151 45770 CAPTAIN'S ALTIMETER AND ALTITUDE ALERTER FLAGGED DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S AIR DATA COMPUTER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000041995042100004WP 1995 4 21 9505589305 119950412A213121171801 PRESS CONTROLLER DOUG DC9 DC982 3022082WP FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01307RC31718188 48086 AUTO PRESSURIZATION FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 PRESSURE CONTROLLER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000051995042100005WP 1995 4 21 9505599305 119950410A3260 PROX CONTL DOUG DC9 DC982 3022082WP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01307RC 48086 DURING CLIMBOUT FROM CMH, NOSE AND MAIN LANDING GEAR RED UNSAFE LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH NO HELP. APPROXIMATELY ONE HOUR INTO FLIGHT, A 'CLICK' WAS HEARD AND ALL THREE RED UNSAFE LIGHTS EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES. DISCREPANCY COULD NOT BE DUPLICATED. REPLACED PROXIMITY CONTROL UNIT AS A PRECAUTION. 2L72 4F A6WE 19950421000061995042100006WP 1995 4 21 9505609760 119950412A3231 LINK DOUG DC9 DC941 302207NWP RT NLG DOOR FAILED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01760NW 47288 LOUD NOISE AND VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND THE RIGHT NOSE GEAR DOOR OPEN. REPLACED DOOR LINK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000071995042100007WP 1995 4 21 9505619852 119950408A3260 DNLOCK SWITCH DOUG DC9 DC951 3022051WP RT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING UKUNKNOWN 1 GL01761NC 47709 RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. RECYCLED GEAR TWICE AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION (ATL) AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000081995042100008WP 1995 4 21 9505629942 119950409A528059149841 DOOR DOUG DC9 DC932 3022066WP LT NLG DOOR DAMAGED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 GL013991C 47175 VIBRATION AND A SMALL 'THUMP' WAS COMING FROM THE NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOOR BENT AND OUT OF RIG. REPLACED DOOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000091995042100009 1995 4 21 9505639952 419950409A3421258733511 VERT GYRO DOUG DC9 DC931 3022065WP FWD ACCESSORY MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01916RW318992762 47144 FIRST OFFICER'S GYRO FLAG WAS IN VIEW DURING TAKEOFF ROLL. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS AND RETURNED TO GATE. REPLACED THE NR 2 VERTICAL GYRO. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421000101995042100010NM 1995 4 21 9505642275 119950411A5610 SEAL BOEING727 727251 138408HNM LT WINDSHIELD LOOSE A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 GL01275US 21154 DURING CLIMB, CAPTAIN'S WINDSHIELD EMITTING LOUD NOISE. MAINTAINED FL 160 AND DIVERTED TOWARDS ATL. DUMPED 11,000 POUNDS OF FUEL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND WEATHER SEAL TORN LOOSE ON TOP HALF OF WINDSHIELD. REMOVED SEAL AND REAPPLIED. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950421000111995042100011WP 1995 4 21 ABXA9500311 119950323A52805910557109 DOOR DOUG DC9 DC931 3022065WP LT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23948AX 47065 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE HALF WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-10-0. 2L72 4F A6WE 19950421000121995042100012WP 1995 4 21 ABXA9500312 119950329A5400591326227 ANGLE DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND NR 1 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE TO BE CRACKED. REPAIRED IAW ABX REA D954-11280-MR. 2L72 4F A6WE 19950421000131995042100013WP 1995 4 21 ABXA9500313 119950329A540059132625 ANGLE DOUG DC9 DC941 302207NWP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 1 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR. 2L72 4F A6WE 19950421000141995042100014WP 1995 4 21 ABXA9500314 119950329A5400591326228 ANGLE DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-112080-MR. 2L72 4F A6WE 19950421000151995042100015WP 1995 4 21 ABXA9500315 119950329A540059132626 ANGLE DOUG DC9 DC941 302207NWP RT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR. 2L72 4F A6WE 19950421000161995042100016WP 1995 4 21 ABXA9500316 119950331A5330592032339 SKIN DOUG DC9 DC931 3022065WP FS 362 OIL CANNING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN TO BE OIL CANNING, 1 INCH DIAMETER AT FUSELAGE STATION 362, LONGERONS 21 AND 22R. REPAIRED SKIN IAW ABX REA D953-11287-MR. 2L72 4F A6WE 19950421000171995042100017WP 1995 4 21 ABXA9500317 119950331A531199196192 FRAME DOUG DC9 DC931 3022065WP FS 737 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05; S.B. 53-131, FOUND RIGHT MAIN FRAME AT STA 737 CRACKED IN FORWARD INBOARD WEB. REPLACED MAIN FRAME AT STA 737R IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950421000181995042100018WP 1995 4 21 ABXA9500318 119950403A52802923161503 DOOR DOUG DC9 DC931 3022065WP LT MLG DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR DELAMINATED, APPROXIMATELY 30 SQUARE INCHES. REPLACED LEFT OUTBOARD FLYING DOOR IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950421000191995042100019WP 1995 4 21 ABXA9500319 119950401A5320995765914 INTERCOSTAL DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION FOUND THE UPPER FLANGE OF AN INTERCOSTAL CRACKED. REPAIRED INTERCOSTAL IAW ABX REA D953-11304-MR. 2L72 4F A6WE 19950421000201995042100020WP 1995 4 21 ABXA9500320 119950330A53111387619 FRAME DOUG DC9 DC931 3022065WP FS 639 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FUSELAGE FRAME AT STA 639 CRACKED AT LONGERON 19R. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16. 2L72 4F A6WE 19950421000211995042100021WP 1995 4 21 ABXA9500321 119950330A53113914119 FRAME DOUG DC9 DC931 3022065WP FS 658 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23929AX 45874 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FUSELAGE FRAME AT STA 658 CRACKED AT LONGERON 19R. REPAIRED IAW DC-9 SRM 53-03, FIGURE 16. 2L72 4F A6WE 19950421000221995042100022WP 1995 4 21 ABXA9500322 119950215A554049139401 FITTING DOUG 5523AX501AX DOUG DC9 DC932 3022066WP RUDDER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX 47640 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 RUDDER OFF WING INSPECTION FOUND LEVEL II CORROSION ON FITTING. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 27-20-1. 2L72 4F A6WE 19950421000231995042100023WP 1995 4 21 ABXA9500323 119950201A57537075T6511125 SPAR DOUG 5910069559 DOUG DC9 DC932 3022066WP LT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX ABXG182 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON LOWER AFT SPAR. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 51-10-3. REPAIRED SPAR IAW DC-9 SRM 57-06. 2L72 4F A6WE 19950421000241995042100024WP 1995 4 21 ABXA9500324 119950201A57537075T6125 SPAR DOUG 5910039559 DOUG DC9 DC932 3022066WP LT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX ABXG182 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON LEFT FLAP, FOUND LEVEL II CORROSION ON UPPER AFT SPAR AT STA. FLS. 114. BLENDED AND TREATED FOR CORROSION PER DC-9 SRM 581-10-3. REPAIRED SPAR PER DC-9 SRM 57-06. 2L72 4F A6WE 19950421000251995042100025WP 1995 4 21 ABXA9500325 119950209A57534916865503 BASE DOUG 5910039559 DOUG DC9 DC932 3022066WP LT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX ABXG182 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON SPRING BASE. REPLACED IAW DC-9 OVERHAUL MANUAL 27-50-1. 2L72 4F A6WE 19950421000261995042100026WP 1995 4 21 ABXA9500326 119950125A57537075T6050 RIB DOUG 5910039559 DOUG DC9 DC932 3022066WP LT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX ABXG182 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON THE OUTBOARD END RIB. REPLACED IAW DC-9 SRM 57-50-9. 2L72 4F A6WE 19950421000271995042100027WP 1995 4 21 ABXA9500327 119950201A57537075T6071 CAP DOUG 5910039559 DOUG DC9 DC932 3022066WP LT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23988AX ABXG182 47084 DURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 FLAP OFF WING INSPECTION ON THE LEFT FLAP, FOUND LEVEL II CORROSION ON LEADING EDGE NOSE CAP AT STA. XFLS 176. REPLACED IAW DC-9 SRM 57-50-9. 2L72 4F A6WE 19950421000281995042100028WP 1995 4 21 ABXA9500328 119950328A57533915183502 CAP DOUG 5910411516 DOUG DC9 DC931 3022065WP RT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23942AX 529516 47552 DURING DC-9 ELEVATOR OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE INBOARD LEADING EDGE CAP OF THE RIGHT ELEVATOR. REPLACED WITH SERVICEABLE CAP IAW DC-9 SRM 27-30. 2L72 4F A6WE 19950421000291995042100029WP 1995 4 21 ABXA9500329 119950321A57535910040504 RIB DOUG 5910134522 DOUG DC9 DC941 302207NWP RT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 6 47493 DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT FLAP INBOARD RIB BEARING BORE. REPAIRED INBOARD RIB HOLE FOR BEARING IAW DC-9 SRM 57-02, FIGURE 7, PAGE 11. 2L72 4F A6WE 19950421000301995042100030WP 1995 4 21 ABXA9500330 119950307A57532024T3063 ANGLE DOUG 5910134522 DOUG DC9 DC941 302207NWP RT FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 6 47493 DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIB ANGLE. REPLACED RIB ANGLE IAW DC-9 SRM 57-50-9. 2L72 4F A6WE 19950421000311995042100031WP 1995 4 21 ABXA9500331 119950413A2612244854G9834 FIRE LOOP DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE NR 4 ENGINE LOOSE A ABXAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23847AX 46031 644309 DURING CRUISE, THE NR FOUR ENGINE FIRE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SECURED AND THE FIRE BOTTLES WERE DISCHARGED. LIGHT REMAINED ON. FLIGHT REROUTED TO DEN. LANDED WITHOUT INCIDENT. FOUND LOWER FIRE LOOP LOOSE AND CONNECTOR FULL OF OIL. SECURED FIRE LOOP, CLEANED CONNECTOR, REPLACED FIRE BOTTLES AND SQUIBS. SYSTEM OPS CHECKED GOOD IAW DC-8 M.M., CHAPTER 26. OVERWEIGHT LANDING INSPECTION COMPLIED WITH IAW ABX CARD DC-8-3A. NO DISCREPANCIES NOTED. 2L74 4F4 F 4A25 1E8 19950421000321995042100032WP 1995 4 21 ABXA9500332 119950412A25105641031501 SEAT DOUG DC8 DC863 302198AWP PILOT SEAT LACK OF LUBE A ABXAK NONE O OTHER CRCRUISE 1 GL23817AX 45928 DURING CRUISE, THE CAPTAIN'S SEAT BACK WOULD NOT LOCK IN PLACE. LUBED CAPTAIN'S SEAT BACK CABLE RELEASE ASSEMBLY. SEAT OPS CHECKED GOOD IAW DC-8 M.M., CHAPTER 25. 2L74 4F 4A25 19950421000331995042100033NM 1995 4 21 DHL95741001 119950411A27301864 LAMP BOEING727 7272Q9 138448MNM ELEV FEEL SYST FAILED A TDHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01741DH 21931 DURING CRUISE, ELEVATOR DIFFERENTIAL PRESSURE LIGHT ON INTERMITTENTLY FOR SEVERAL MINUTES. FOUND ELEVATOR FEEL LIGHT BULB SHORTING. RELAMPED. NO OTHER DEFECTS NOTED. 2L73 4F RTA3WE 19950421000341995042100034WP 1995 4 21 DHL95804001 119950411A3230 RETRACT MECH DOUG DC8 DC873F 302199FWP LANDING GEAR MALFUNCTIONED A TDHLAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01804DH 46124 ON APPROACH, LANDING GEAR DID NOT EXTEND WHEN GEAR LEVER PLACED IN DOWN POSITION. RECYCLED, WORKED NORMALLY. JACKED AIRCRAFT AND PERFORMED 3 GEAR SWINGS, SEVERAL CYCLES. INSPECTED GEAR, NO DEFECTS NOTED. ALL GEAR SWINGS SUCCESSUL. COULD NOT DUPLICATE MALFUNCTION. ALL WORK IAW MM 32-30. 2L74 4F RT4A25 19950421000351995042100035WP 1995 4 21 SCNA95055 119950410A33500816901 EEL MODULE DOUG DC10 DC1010 3022110WP CABIN MALFUNCTIONED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15571SC 46645 CENTER CABIN, LEFT FLOOR EMERGENCY LIGHTING TRACK MODULE INOPERATIVE. REPAIRED DAMAGED WIRE AT MODULE. OPS CHECK GOOD. 2L73 4F A22WE 19950421000361995042100036WP 1995 4 21 95ZZZW440 119950331A3230450100109 CONTROL SWITCH LKHEED1011 10113851 5265010WP LANDING GEAR MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0515017 193B1063 JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6. LANDING GEAR SYSTEM OPERATION CHECKED NORMAL. REFERENCE 95ZZZW441. 2L73 4F A23WE 19950421000371995042100037WP 1995 4 21 95ZZZW441 119950331A32302680262M6 CONTROL VALVE LKHEED1011 10113851 5265010WP LANDING GEAR MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0515017 193B1063 JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6. LANDING GEAR SYSTEM OPERATION CHECKED NORMAL. REFERENCE 95ZZZW440. 2L73 4F A23WE 19950421000381995042100038NM 1995 4 21 95ZZZW442 119950403A2410 IDG BOEING747 747284B 1384862NM NR 2 ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE05305TW 20742 FLT NR 5 - JFK - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO FIRE WARNING. DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. FOUND INTERGRATED DRIVE GENERATOR, MFG P/N 28B26313A, FAILURE AND OVERHEAT DAMAGE TO PLUMBING AND ELECTRICAL WIRING. REPLACED ENGINE S/N 4131. INVESTIGATION INTO NR 2 ENGINE SHUTDOWN DUE TO FIREWARNING, REVEALED INTEGRATED DRIVE GENERATOR FAILED DUE TO INSUFFICIENT LUBRICATION SUPPLY. ENGINE S/N 4131 WAS REPAIRED AND RETURNED TO SERVICE. (W) 2L74 4F RTA20WE 19950421000391995042100039WP 1995 4 21 95ZZZW443 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 328-349 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION/MAIN CABIN FLOOR AREA RT SIDE STATION 349 TO 328 INBOARD OF NR 3 SEAT TRACK FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION TREATED AND FABRICATED AND INSTALLED REPAIR PER SRM 53-21-01. 2L73 4F A23WE 19950421000401995042100040WP 1995 4 21 95ZZZW444 119950329A5320 DOOR FRAME LKHEED1011 10113851 5265010WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION/MAIN CABIN R1 DOOR FRAME FLOOR AFT GIRTH BAR FITTING AREA PANEL HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-20-01. 2L73 4F A23WE 19950421000411995042100041WP 1995 4 21 95ZZZW445 119950329A5320 PLENNUM LKHEED1011 10113851 5265010WP FS 369 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, BELOW CABIN FLOOR RIGHT SIDE AFT OF STATION 369 AND BELOW MOST INBOARD PACK DUCT PLENNUM HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH DRAWING L15310-5022 SHEETS 1, 2 AND 3. (W) 2L73 4F A23WE 19950421000421995042100042WP 1995 4 21 95ZZZW446 119950329A5320 PLENNUM LKHEED1011 10113851 5265010WP FS 369 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, BELOW CABIN FLOOR RIGHT SIDE AT STATION 369 PLENNUM HAS CORROSION BELOW 3RD SEAT TRACK. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00. (W) 2L73 4F A23WE 19950421000431995042100043WP 1995 4 21 95ZZZW447 119950329A5320 ANGLE LKHEED1011 10113851 5265010WP FS 328 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN STATION 328 RT SIDE PLENNUM AREA AND AFT OF MOST INBOARD PACK DUCT AREA HAS CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-10-5. 2L73 4F A23WE 19950421000441995042100044WP 1995 4 21 95ZZZW448 119950329A5320 TEE CAP LKHEED1011 10113851 5265010WP FS 328 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN UNDER FLOOR AREA STATION 328 RT SIDE AND UNDER MOST INBOARD PACK DUCT PLENNUM TEE CAP HAS CORROSION. REMOVED CORROSION TREATED AREA AND FABRICATED AND INSTALLED REPAIR PER RICH DRAWING L15310-5021. 2L73 4F A23WE 19950421000451995042100045WP 1995 4 21 95ZZZW449 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1778 CORRODED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR RT SIDE STATION 1778 FLOOR SUPPORT BEAM HAS CORROSION FWD OF RIGHT SIDE FLIGHT ATTENDANT SEAT. CUT OUT DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950421000461995042100046WP 1995 4 21 95ZZZW450 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP COCKPIT CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR SUPPORT BELOW COCKPIT DOOR HAS CORROSION LEFT TO RIGHT SIDES. REMOVED DAMAGED AREA CLEANED AND TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 51-50-04. 2L73 4F A23WE 19950421000471995042100047WP 1995 4 21 95ZZZW451 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1778 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR SUPPORT BELOW RT SIDE R-4 DOOR FLIGHT ATTENDANT SEAT AFT OF STATION 1778 HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 51-50-02. 2L73 4F A23WE 19950421000481995042100048WP 1995 4 21 95ZZZW452 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 297 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FLOOR AREA AFT OF RT SIDE FWD LAVATORY FWD OF STATION 297 FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-10-05. 2L73 4F A23WE 19950421000491995042100049WP 1995 4 21 95ZZZW453 119950329A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 297-349 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FORWARD BAR FLOOR AREA 4TH INBOARD SEAT TRACK ON LEFT SIDE HAS CORROSION FROM STATION 349 TO STATION 297. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 51-10-05. 2L73 4F A23WE 19950421000501995042100050WP 1995 4 21 95ZZZW454 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 328 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, MAIN CABIN FORWARD BAR FLOOR AREA STATION 328 FLOOR SUPPORT BETWEN 4TH LEFT SIDE AND 4TH RT SIDE SEAT TRACKS HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-04. 2L73 4F A23WE 19950421000511995042100051WP 1995 4 21 95ZZZW455 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1763-1778 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR RT SIDE FLOOR SUPPORT BEAM BETWEEN STATION 1763 AND STATION 1778 AFT OF 2ND SEAT TRACK HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-50-02. 2L73 4F A23WE 19950421000521995042100052WP 1995 4 21 95ZZZW456 119950329A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 1745-1763 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR RT SIDE 2ND SEAT TRACK STATION 1745 TO STATION 1763 HAS CORROSION. REMOVED DAMAGED AREA CLEANED AND TREATED AREA FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-21-00. (W) 2L73 4F A23WE 19950421000531995042100053WP 1995 4 21 95ZZZW457 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1763 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR RT SIDE STATION 1763 FLOOR SUPPORT BEAM HAS CORROSION BETWEEN 1ST AND 2ND SEAT TRACKS. REMOVED DAMAGED AREA CLEANED CORROSION AND TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950421000541995042100054WP 1995 4 21 95ZZZW458 119950329A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 281 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CABIN FLOOR LEFT SIDE AT STATION 281 AND BELOW LAVATORY FLOOR SUPPORT HAS CORROSION. REMOVED SUPPORT CLEANED AND TREATED AREA FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-50-04. 2L73 4F A23WE 19950421000551995042100055NM 1995 4 21 95ZZZW459 119950309A5210 SEAL BRACKET BOEING737 737201 1384454NM FWD ENTRY DOOR FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19245US 22751 BWI - FLT 2476 - ON CLIMB-OUT OF BWI, LOUD WHISTLING NOISE HEARD COMING FROM FORWARD ENTRY DOOR, FOLLOWED BY A LOUD BOOM. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED UPPER HINGE SEAL AND SEAL BRACKET. REFERENCE USAA950240. 2L72 4F A16WE 19950421000591995042100059SO 1995 4 21 95ZZZW463 119950115A5610NP1513111 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT FAILED A MASAA UNSCHED LANDING O OTHER CRCRUISE 1 SW01283UE 120139 AIRCRAFT DEPARTED FIELD AT CRUISE ALTITUDE CAPTAINS WINDSHIELD SHATTERED. AIRCRAFT DIVERTED TO ALTERNATE AIRPORT AFTER DECLARING AND EMERGENCY, CALLED MX. WINDSHIELD ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421000601995042100060 1995 4 21 95ZZZW464 319950311A61124E30171 DE-ICE BOOT BEECH 1900 1900D 1154162CE RT PROP SEPARATED A AMASAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SW01126YV457 HJ291 UE126 TWO PROP DE-ICE BOOTS SEPARATING FROM LEADING EDGE EROSION SHIELD. PAINT ON SHIELD SEPARATED FROM SHIELD. SUBMITTER SUGGEST IMPROVING PAINTING PROCEDURES ON PROP BLADES OR LEAVING PAINT OFF OR EROSION SHIELD. 2L72 4T RTA24CE 19950421000611995042100061CE 1995 4 21 95ZZZW465 119950204A564011443010921 WINDOW BEECH 1900 1900C 1154161CE AFT CARGO DOOR BROKEN A GPPAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE09124GP UB23 FLT NR 2375 - DEPARTING DEN WAS UNABLE TO PRESSURIZE. AIRCRAFT RETURNED TO DEN WHERE GP EXPRESS MAINTENANCE DEFERRED THE PRESSURIZATION SYSTEM. LATER THAT DAY GP EXPRESS MAINTENANCE FOUND THE INSPECTION WINDOW FOR THE AFT CARGO DOOR LOCK MECHANISM BROKEN. WINDOW WAS REPLACED AND SYSTEM CHECKED SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 19950421000621995042100062CE 1995 4 21 95ZZZW466 119950112A3260 SWITCH BEECH 1900 1900C 1154161CE NLG DIRTY A MASAO OTHER P NO WARNING INDICATION APAPPROACH 1 SW0177YV UC77 CREW REPORTED WHEN GEAR WAS SELECTED DOWN, THERE WAS NO NOSE GEAR DOWN AND LOCK INDICATION. MAINTENANCE INSPECTED NOSE DOWN AND LOCKED SWITCHES AND WIRING, CLEANED AND LUBED SWITCHES. FUNCTION CHECKED LANDING GEAR. RETURNED AIRCRFT TO SERVICE. 2L72 4T RTA24CE 19950421000631995042100063CE 1995 4 21 95ZZZW467 119950116A3260 SWITCH BEECH 1900 1900C 1154161CE NLG OUT OF ADJUST A MASAO OTHER P NO WARNING INDICATION APAPPROACH 1 SW0177YV UC77 WHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO DOWNLOCK NOSE INDICATION. MAINTENANCE ADJUSTED DOWNLOCK SWITCH. FUNCTION CHECKED LANDING GEAR AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950421000641995042100064EU 1995 4 21 95ZZZW468 119950121A3110 INSTR PNL STBROSSD3 SD360 8100606EU COCKPIT SHORTED A MASAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW01162CN SH3762 CREW REPORTED AFTER TAKEOFF, SMOKE COMING FROM DOOR WARNING PANEL NEXT TO CO-PILOT. MAINTENANCE INSPECTED BEHIND PANEL AND FOUND THAT DE-ICING FLUID HAD LEAKED ONTO PANEL. DRIED PANEL AND RESEALED. PERFORMED SYSTEMS CHECK AND RETURNED TO SERVICE. 2H72 4T A41EU 19950421000651995042100065WP 1995 4 21 HAL95028 119950324A212160529042 COOLING FAN DOUG DC9 DC951 3022051WP LT OVERHEATED A HALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP132FOR 1202535 47742 SMOKE COMING OUT OF GROUND COOL FAN INLETS. LEFT GROUND FAN SIDE OF 'Y' DUCT EXTREMELY HOT. SUSPECT ELECTRICAL SHORT AT FAN. REMOVED AND REPLACED THE LEFT GROUND COOLING FAN ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD AND THE LEAK CHECK GOOD. NO SMOKE NOTED ON OPS CHECK. SYTEM OPERATING NORMALLY. (W) 2L72 4F A6WE 19950421000661995042100066WP 1995 4 21 HAL95029 119950324A335060030431 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13669HA 47654 HNL - THE AFT OVERWING EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT BATTERY POWER PACK. THE AFT OVERWING EXIT EMERGENCY LIGHTS CHECKED GOOD. (W) 2L72 4F A6WE 19950421000671995042100067WP 1995 4 21 IXXA199522 119950308A3230EE822147501 ROD END DOUG DC8 DC871 302199AWP RT MLG FRACTURED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23820BX 46065 AFTER LANDING AT TOL, IT WAS NOTED THAT THE RT MLG ACTUATOR ROD END HAD FAILED DURING THE LAST LANDING GEAR EXTENSION. THE ROD END DID NOT, HOWEVER, FAIL IN THE THREADS. THE EYE ITSELF FRACTURED ADJACENT TO THE THREADED SHANK. A PREVIOUSLY EXISTING CRACK ORIGINATING IN THE TRANSITION AREA FROM THE EYE TO THE THREADED SHANK APPEARS TO HAVE BEEN THE ORIGIN OF THE FRACTURE. THE ROD END WAS REPLACED IAW THE DC-8 MM AND TR 32-121, AND THE AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 19950421000681995042100068WP 1995 4 21 IXXA199523 119950327A21301031549092 SAFETY VALVE DOUG DC8 DC863F 302198FWP AFT FUSELAGE MALFUNCTIONED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23784AL 7 46135 THE AIRCRAFT DEPARTED GSO AND EXPERIENCED FLUCTUATING CABIN PRESSURE THAT COULD NOT BE CONTROLLED EITHER BY THE MANUAL OR AUTOMATIC SYSTEMS. THE AIRCRAFT RETURNED TO GSO FOR MAINTENANCE. TROUBLESHOOTING AND GROUND PRESSURIZATION REVEALED THAT ONE OF THE SAFETY RELIEF VALVES WAS CYCLING ABOVE 6 PSID, INSTEAD OF RELIEVING AT ITS CORRECT SETTING. THE SAFETY VALVE WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE AFTER A FINAL PRESSURIZATION CHECK. (W) 2L74 4F 4A25 19950421000691995042100069NM 1995 4 21 USAA950240 119950309A5210 SEAL BOEING737 737201 1384454NM FWD ENTRY DOOR FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19245US 22751 BWI - FLT 2476 - ON CLIMB-OUT OF BWI, LOUD WHISTLING NOISE HEARD COMING FROM FORWARD ENTRY DOOR, FOLLOWED BY A LOUD BOOM. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED UPPER HINGE SEAL AND SEAL BRACKET. REFERENCE 95ZZZW459. 2L72 4F A16WE 19950421000701995042100070NM 1995 4 21 USAA950242 119950311A2910BACH8A06NN0263T LINE BOEING737 7372Q9 138448MNM NLG W/W LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19231US 21976 CLT - FLT 2188 - EN ROUTE TPA TO LGA, LOST 'A' SYSTEM HYDRUALIC QUANTITY, FOLLOWED BY LOW 'A' PRESSURE LIGHTS. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR ACTUATOR LINE LEAKING AT 'B' NUT. REPLACED LINE, BOTH 'A' SYSTEM PRESSURE FILTERS, AND BOTH ENGINE DRIVEN PUMPS CASE DRAIN FILTERS. (W) 2L72 4F A16WE 19950421000711995042100071WP 1995 4 21 USAA950249 119950319A2420 FEEDER CABLE DOUG DC9 DC981 3022081WP RT ENGINE CHAFED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19811US 48043 PIT - FLT 0992 - ON TAKEOFF, THE RIGHT GENERATOR OFF LIGHT ILLUMINATED FOLLOWED BY AC CROSSTIE LOCKOUT. CREW DECIDED TO RETURN TO PIT. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND STOWED LAV DUMP CABLE CHAFING ON GEN FEEDER CABLE. ACCOMPLISHED REPAIRS TO THE RIGHT ENGINE GENERATOR FEEDER CABLES. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950421000721995042100072WP 1995 4 21 USAA950250 119950318A2410696233B CSD DOUG DC9 DC981 3022081WP NR 2 ENG LEAKING A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19811US 48043 PIT - FLT 0239 - AIRCRAFT RETURNED TO PIT DUE TO A GENERATOR PROBLEM. MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND THE RIGHT ENGINE GENERATOR FOR TROUBLESHOOTING. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950421000731995042100073NM 1995 4 21 USAA950253 119950313A5313 STRINGER BOEING737 7373B7 1384580NM BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN STRINGER S-16 R BS 500 C PLUS 4 INCHES. REPAIRED PER EO 5393X228. (W) 2L72 4F RTA16WE 19950421000741995042100074WP 1995 4 21 USAA950254 119950317A5342 ANGLE DOUG DC9 DC981 3022081WP LT STAB ATTACH CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19802US37968 48036 IND - DURING SCHEDULED CX-2 INSPECTION, FOUND A 1 INCH CRACK EXTENDING FROM VERTICAL LEG INTO HORIZONTAL LEG OF STABILIZER TO FUSELAGE ATTACH ANGLE. CUT OUT DAMAGED SECTION AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-05 FIG NR 23A. (W) 2L72 4F A6WE 19950421000751995042100075WP 1995 4 21 USAA950255 119950213A531159114471 FRAME DOUG DC9 DC931 3022065WP BS 389 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19997VJ67355 47336 IND - DURING SCHEDULED CX-5 INSPECTION, FOUND .5 INCH CRACK IN FRAME AT STATION 389 AT LONGERON 17R. CUT OUT DAMAGED AREA, INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-04 FIG 35 AND USAIR EA 29574. (W) 2L72 4F A6WE 19950421000761995042100076WP 1995 4 21 USAA950257 119950308A5330 SKIN DOUG DC9 DC931 3022065WP BS 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19975VJ71117 47146 PIT - DURING MAINTENANCE WALK AROUND CHECK, FOUND .5 INCH CRACK IN INNER AND OUTER SKIN AT AFT CORNER OF AIR STAIR LOWER CORNER STATION 200. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-05 FIG 57A. (W) 2L72 4F A6WE 19950421000771995042100077NM 1995 4 21 USAA950261 119950323A2780655280739 SENSOR BOEING737 7374B7 1384702NM E/E COMPT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19426US16615 24548 CLT - FLT 2195 - FLIGHT EN ROUTE DCA TO MSY WITH NR 2 LEADING EDGE FLAP INTRANSIT LIGHT ILLUMINATED. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 LEADING EDGE FLAP DOWN SENSOR AND FLAP/SLAT POSITION MODULEIN E/E COMPARTMENT. OPS CHECK NORMAL (W) 2L72 4F RTA16WE 19950421000781995042100078NM 1995 4 21 USAA950262 119950323A5240 LATCH BOEING737 7374B7 1384702NM FWD LAV SERV DR OPEN A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19427US 24549 PIT - FLT NR 497 - LOUD VIBRATION ON FORWARD RIGHT PART OF AIRCRAFT. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE CLOSE FORWARD LAV SERVICE LATCH. NO OTHER FAULTS FOUND ON FORWARD FUSELAGE OF AIRCRAFT, OK FOR SERVICE. (W) 2L72 4F RTA16WE 19950421000791995042100079NM 1995 4 21 USAA950263 119950216A53151711392 FLOOR BEAM BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORRODED 2 INCH BY 72 INCH AREA (CLIP NUT HOLES) BS 328. REPAIRED PER SRM 51-70-12 AND TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000801995042100080NM 1995 4 21 USAA950264 119950214A53151711392 FLOOR BEAM BOEING737 7373B7 1384580NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM CORROSION AT CHIP NUT HOLES BS 312 RBBL 24 TO LBBL 30. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000811995042100081NM 1995 4 21 USAA950265 119950213A53471711394 SEAT TRACK BOEING737 7373B7 1384580NM BS 340 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION ,FOUND SEAT TRACK 1 INCH BY 8 INCH CORRODED AREA BS 340 RBL 44. REPAIRED PER SRM 52-00-52 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000821995042100082NM 1995 4 21 USAA950266 119950213A53471711394 SEAT TRACK BOEING737 7373B7 1384580NM BS 340-364 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 24 INCH CORRODED AREA BS 340-364 RBL 24. REPAIRED PER SRM 53-00-52 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000831995042100083NM 1995 4 21 USAA950267 119950213A53471711394 SEAT TRACK BOEING737 7373B7 1384580NM BS 277-294 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEAT TRACK 2 INCH BY 12 INCH CORRODED AREA BS 277-294 RBL 24 INBOARD SIDE OF NR 1 GALLEY. REPAIRED PER SRM 53-00-52 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000841995042100084NM 1995 4 21 USAA950268 119950222A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 60 INCH STATION 986.5 ENTIRE LENGTH. REPAIRED PER TR 53-10-5. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000851995042100085NM 1995 4 21 USAA950269 119950213A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FLOOR BEAM (2) 1 INCH BY 1 INCH CORRODED AREAS (ABOUT .060 INCH DEEP), LBL 6 AND RBL 6 AT BS 947. REPAIRED PER SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000861995042100086NM 1995 4 21 USAA950270 119950214A53206545834257 INTERCOSTAL BOEING737 7373B7 1384580NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 .5 INCH BY 1 INCH CORRODED AREAS (ABOUT .050 INCH DEEP), BS 328-344 RBBL 12 (CABIN FLOOR SUPPORT). REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000871995042100087NM 1995 4 21 USAA950271 119950214A53201136993 ANGLE BOEING737 7373B7 1384580NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, BS 312-328 LBBL 12. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000881995042100088NM 1995 4 21 USAA950272 119950214A53201123845 ANGLE BOEING737 7373B7 1384580NM BS 300-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION 1 INCH BY 15 INCH AND 1 INCH BY 3 INCH FOR TOTAL OF 1 INCH BY 18 INCH, BS 300 THROUGH BS 344 AT FORWARD CABIN (LEFT SIDE) ENTRY DOOR. REPAIRED PER SRM 51-10-4. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000891995042100089NM 1995 4 21 USAA950273 119950214A53201123129 ANGLE BOEING737 7373B7 1384580NM BS 277-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCH BY 1 INCH BY 6 INCH EQUALS 1 INCH BY 36 T, BS 277-BS 328 FORWARD SERVICE DOOR ANGLE. REPAIRED PER SRM 51-10-4. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000901995042100090NM 1995 4 21 USAA950274 119950214A53201136992 ANGLE BOEING737 7373B7 1384580NM BS 320-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION AT CLIP NUT HOLES BS 320-344 LBBL 12. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000911995042100091NM 1995 4 21 USAA950275 119950214A53206545834256 INTERCOSTAL BOEING737 7373B7 1384580NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH BY 1 INCH CORRODED AREA (ABOUT .050 INCH DEEP), BS 312-328 RBBL 12 (CABIN FLOOR SUPPORT). REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000921995042100092NM 1995 4 21 USAA950276 119950203A5320 ANGLE BOEING737 7373B7 1384580NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED SEVERAL NUT PLATES BS 947 BS 1006. REPAIRED PER SRM 51-10-02 PG 16. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950421000931995042100093NM 1995 4 21 USAA950301 119950325A2822568126713005 PUMP BOEING737 737301 1384611NM NR 2 MAIN TANK FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19577US 23742 CLT - FLT 731 - FLIGHT EN ROUTE PHL TO MSY WHEN FORWARD NR 2 MAIN TANK FUEL BOOST PUMP LOW PRESSURE LIGHT CAME ON. FLIGHT DIVERETED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 FORWARD BOOST PUMP PER MM 28-22-41. NO LEAKS NOTED, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950421000941995042100094WP 1995 4 21 USAA950302 119950401A3070 LINE DOUG DC9 DC931 3022065WP RT COCKPIT DIRTY A USAABG EMER. DESCENT O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19972VJ 47052 CLT - FLT NR 0275 - CREW REPORTED FUMES IN COCKPIT. OXYGEN MASKS WERE USED AND AN EMERGENCY WAS DECLARED. MAINTENANCE CLEANED THE ANTI-ICE FLUID LINE AND ELBOW AT SOLENOID, FIRST OFFICERS SIDES. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950421000951995042100095WP 1995 4 21 USAA950303 119950401A323339208025507 CYLINDER DOUG DC9 DC931 3022065WP LT MLG LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19977VJ 48155 CLT - FLT 0741 - ON CLIMB-OUT, THE RED GEAR UNSAFE LIGHT AND YELLOW GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN DECLARED AND EMERGENCY AND FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE LEFT MAIN GEAR ACTUATING CYCLINDER. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950421001351995042100135 1995 4 21 AALA950417 419950308A2565D20835103 SLIDE AIRCRUISERS BOEING727 727 1384001NM FWD ENTRY DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A2543 ORD - DURING SHOP VISIT OVERPRESSURE CHECK, EMERGENCY EVACUATION SLIDE SEAM SEPARATED UNDER RUNWAY AND RUNWAY UNGLUED ON BOTTOM SIDE. SCRAPPED EMERGENCY EVACUATION SLIDE. (X) 2L73 4F A3WE 19950421001361995042100136 1995 4 21 AALA950427 419950308A2564D23835201 RAFT AIRCRUISERS BOEING727 727 1384001NM CABIN CUT A AALAK NONE O OTHER ININSP/MAINT 1 SW07 812 LAX - DURING SHOP VISIT DEPLOYMENT, LIFE RAFT HAD SMALL CUT BELOW ASPIRATOR. LIFE RAFT ROUTED TO VENDOR FOR REPAIR. (X) 2L73 4F A3WE 19950421001371995042100137 1995 4 21 AALA950428 419950308A2564D23835201 RAFT AIRCRUISERS BOEING727 727 1384001NM CABIN DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07 809 LAX - DURING SHOP VISIT DEPLOYMENT, LIFE RAFT FOUND WITH HOLE IN UPPER TUBE BY ASPIRATOR. ROUTED LIFE RAFT TO VENDOR FOR REPAIR. (X) 2L73 4F A3WE 19950421001961995042100196CE 1995 4 21 95ZZZW469 119950314A3260R100381001 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG OUT OF ADJUST A HERAO OTHER N FALSE WARNING LDLANDING 1 AL0380532 UC95 FLT 1412 - LANDING ANC COULD NOT GET A SAFE NOSE GEAR DOWN INDICATION (GREEN LIGHT) WHEN THE LANDING GEAR WAS LOWERED. A MANUAL GEAR EXTENSION WAS PERFORMED WITH THE NOSE GEAR STILL SHOWING UNSAFE. A LANDING WAS MADE AT ANC WITHOUT INCIDENT. MAINTENANCE RIGGED THE NOSE GEAR DRAG BRACE SWITCH AND PERFORMED A RETRACTION TEST AND OBSERVED THE NORMAL OPERATION AND INDICATION. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 2L72 4T RTA24CE 19950421001971995042100197EA 1995 4 21 95ZZZW470 219950211A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RIGHT FAILED A MASAAE UNSCHED LANDING ENGINE SHUTDOWN JYEWARNING INDICATION ENGINE STOPPAGE VIBRATION/BUFFET CLCLIMB 1 SW01144YV115454118 UC144 32072GG ON DEPARTURE OUT OF CSP RIGHT ENGINE TORQUE SURGED. CREW NOTICED RT OIL PRESSURE DROPPED AND SECURED ENGINE AT WHICH TIME A SEVERE VIBRATION WAS NOTICED. RETURNED TO CSP WITHOUT FURTHER INCIDENT. UPON ARRIVAL NO OIL WAS PRESENT IN RT ENGINE, OR WAS A LEAK NOTED. ENGINE WAS REMOVED FOR FURTHER INSPECTION AND NEW RT ENGINE INSTALLED. AIRCRAFT WAS TEST FLOWN AND DISPATCHED WITHOUT FURTHER INCIDENT. (W) 2L72 4T4 TRTA24CE E4EA 19950421001981995042100198CE 1995 4 21 95ZZZW471 119950317A61209994000115 CABLE LOCKPLATE BEECH 1900 1900C 1154161CE PEDESTAL DETACHED A APLGAK NONE O OTHER ININSP/MAINT 1 NE05809BE UB40 DURING THE PREFLIGHT PROPELLER MANUAL FEATHER CHECK THE PROPELLERS WOULD NOT FEATHER, ALL OTHER PROPELLER FUNCTIONS OPERATED NORMALLY. THE PROPELLER CONTROL LEVER LINKAGES WERE INSPECTED. THE RIVETS SECURING THE PROPELLER CONTROL CABLE LOCKPLATE TO THE AIRFRAME WERE FOUND SHEARED. THIS CAUSED THE LOCKPLATE TO NOT SECURE THE PROPELLER CONTROL CABLE HOUSINGS RESULTING IN THE INABILITY TO MANUALLY FEATHER THE PROPELLERS. THE RIVETS WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T RTA24CE 19950421001991995042100199WP 1995 4 21 95ZZZW472 119950330A2530888011 SERVING CART LKHEED1011 10113851 5265010WP GALLEY OVERHEATED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531013 193B1035 STL - DURING CRUISE, SINGLE SERVE CART S/N 0458 OVERHEATED CAUSING SMOKE IN LOWER GALLEY. DISCONNECTED ELECTRICAL CABLE. REPLACED SINGLE SERVE CART MFG P/N 888011 AND OPERATION CHECKED NORMAL. 2L73 4F A23WE 19950421002011995042100201EU 1995 4 21 95ZZZW474 119950213A3520 HOSE BAG BAE146BAE146200A 1500266EU PAX 02 BOTTLE KINKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 OXYGEN PASSENGER BOTTLE S/N 101 (CONTROL HEAD S/N) HAS ITS MASK HOSE KINKED AND OXYGEN WILL NOT FLOW TO THE MASK. REMOVED AND REPLACED OXYGEN MASK ASSY. OPS CHECKED OK AT THIS TIME. (W) 2H74 4F RTA49EU 19950421002021995042100202EU 1995 4 21 95ZZZW475 119950118A5320 GUSSET BAG BAE146BAE146200A 1500266EU FLOOR BEAM CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 SEVERAL FLOOR BEAM GUSSETS CORRODED IN FWD VESTIBULE BETWEEN FRAME 15-18. REMOVED AND REPLACED SEVERAL FLOOR BEAM GUSSETS IN FWD VEST BETWEEN FRAME 15-18, PLACED AIRCRAFT INTERCOSTALS AND FRAME BETWEEN FRAME 15 TO 18. (W) 2H74 4F RTA49EU 19950421002031995042100203EU 1995 4 21 95ZZZW476 119950119A2710 CONTROL CABLE BAG BAE146BAE146200A 1500266EU AILERON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 AILERON INTERCONNECT CABLES APPEAR TO HAVE CORROSION AT PULLEYS UNDER BOTH WING ARMPITS. REMOVED AND REPLACED BOTH AILERON INTERCONNECT CABLE CENTER SECTIONS (62BC AND 63BC) IAW MM IAW MM 27-11-00. TRAVEL AND FUNCTIONAL CHECKS OK. (W) 2H74 4F RTA49EU 19950421002041995042100204EU 1995 4 21 95ZZZW477 119950120A5320 SILL PLATE BAG BAE146BAE146200A 1500266EU PAX DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 PASSENGER DOOR SILL PLATE HAS SOME CORROSION FWD VESTIBULE. REMOVED AND REPLACED PASSENGER DOOR (LEFT FWD) WITH NEW SILL PLATE PER SRM STANDARD PRACTICES CHAPTER 51. (W) 2H74 4F RTA49EU 19950421002051995042100205EU 1995 4 21 95ZZZW478 119950124A2731 CONTROL CABLE BAG BAE146BAE146200A 1500266EU ELEV TRIM CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 CORROSION NOTED ON ELEVATOR TRIM CONTROL CABLES (52AB) UNDER DOGHOUSE PANEL INTO HORIZ STABS (NEED FURTHER EXAMINATION). UPON FURTHER INSPECTION FOUND CORROSION ON INNER STRANDS OF ELEV INTERCONNECT. NO CORROSION ON OTHER CABLES. (W) 2H74 4F RTA49EU 19950421002061995042100206EU 1995 4 21 95ZZZW479 119950124A5320 DOUBLER BAG BAE146BAE146200A 1500266EU RAD ALT MOUNT CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 CORROSION FOUND BETWEEN SKIN DOUBLERS ON RADIO ALTIMETER MOUNT RING AND FUSELAGE BELLY SKIN. (W) 2H74 4F RTA49EU 19950421002071995042100207EU 1995 4 21 95ZZZW480 119950126A2620 PIPE BAG BAE146BAE146200A 1500266EU PANEL 441AL HOLE CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 NR 4 NOSE COWL, PANEL 441AL, PIPE FROM FIRE BOTTLE TO RELIEF INDICATOR HAS HOLE WORN THROUGH FROM SUPPORT CLAMP. RUBBER BAD ON CLAMP. INSTALLED NEW PIPE FOR NR 4 LT FIRE BOTTLE DISCHARGE INDICATOR LINE IAW BAE 146 MM. BOTTLE AND SQUIBB NOT DISTURBED. (W) 2H74 4F RTA49EU 19950421002081995042100208EU 1995 4 21 95ZZZW481 119950127A5753 PIVOT PIN BAG BAE146BAE146200A 1500266EU RT WING FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 RT WING NR 3 FLAP TRACK, PIVOT PINS INBOARD AND OUTBOARD AFT POINT ARM TO CARRIAGE BAD. NEW PINS INSTALLED IN BOTH POSTIONS. (W) 2H74 4F RTA49EU 19950421002091995042100209NE 1995 4 21 95ZZZW482 219950127A7310216362035 MANIFOLD BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NR 2 ENG FUEL CRACKED A A6WAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL31611AW E3120 NR 2 ENGINE FIRE LIGHT ILLUMINATED. ENGINE SECURED. FOUND THE RIGHT FUEL MANIFOLD CRACKED. REPLACING BOTH FUEL MANIFOLDS. (W) 2H74 4F4 FRTA49EU E6NE 19950421002101995042100210EU 1995 4 21 95ZZZW483 119950215A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE LT DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 DENT ON LEFT SIDE OF FUSELAGE ABOUT 1 FOOT ABOVE THE NUMERAL SIX. VISUAL INSPECTION OF SKIN, NO CRACKS NOTED, SEE LOG PG 21852 B LK 1 AND 2 FOR EDDY CURRENT INSPECTION, REF FAX DJR/RJ0221-95, DJR/RJ0222-95. AIRCRAFT OK TO CONTINUE IN SERVICE FOR 50 CYCL CURRENT 26947 CYC DUE AT 26997 CYC. 2H74 4F RTA49EU 19950421002111995042100211EU 1995 4 21 95ZZZW484 119950314A3230 HANDLE BAG BAE146BAE146100A 1500260EU EMERG GEAR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 EMERGENCY GEAR RELEASE HANDLE CORRODED AND REMOVED TRANSFERRED TO W/O BQ8970 FOR REPAIR, REF W/C NR 2250 FOR HANDLE INSTALLATION. 2H74 4F RTA49EU 19950421002121995042100212EU 1995 4 21 95ZZZW485 119950322A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE FWD LT DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 AIRCRAFT HAS DENT ON FWD LEFT FUSELAGE FWD OF FRAME P APPROXIMATELY 7 INCHES ABOVE SKIN LAP JOINT, COMPLIED WITH PERMENANT REPAIR WITHIN 400 CYCLES, CURRENT TC AT TIME OF DAMAGE WAS 22471 TC, DUE BY 22871 TOTAL CYCLES, REF AVRO FAX'S DJR/RJ0243-95 AND DJR/RJ0234-95. COMPLIED WITH REPAIR IAW REPAIR DRAWING HC537H9305 STEPS 1-14. 2H74 4F RTA49EU 19950421002131995042100213EU 1995 4 21 95ZZZW486 119950325A25604566M37B SMOKE HOOD BAG BAE146BAE146300A 1500267EU FWD FLT ATTEND MALFUNCTION A A6WAK NONE O OTHER TXTAXI/GRND HDL 1 GL31614AW E3132 FORWARD FLIGHT ATTENDANT SMOKE HOOD APPEARS TO BE ACTIVATED. REPLACED THE SMOKE HOOD. 2H74 4F RTA49EU 19950421002141995042100214CE 1995 4 21 HERA9506 119950210A7331C6620570103 FUEL FLOW IND CESSNA207 T207A 2073614CE INSTR PNL MALFUNCTIONED A HERAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AL031765U 20700365 FLT NR 1521 - AIR RETURN TO OTZ, DUE FUEL FLOW INDICATED 11 GALLONS PER HOUR (GPH) IN CRUISE FLIGHT. A LANDING WAS MADE AT OTZ WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW INDICATOR AND PERFORMED A FUEL FLOW TEST IAW THE CESSNA SERVICE MANUAL. GROUND RUN UP INDICATED FUEL FLOW WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 1H71 3O A16CE 19950421002151995042100215EA 1995 4 21 HERA9507 119950314A7712 SOLONOID WIRE DHAV DHC6 DHC6300 EA NR 1 ENG SHORTED A HERAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 AL03724CA 793 FLT 1124 - AIR RETURN ENA - THE NR 1 ENGINE HAD TO BE SHUT DOWN AND SECURED DUE TO LOSS OF TORQUE AND PROPELLER RPM. THE AIRCRAFT LANDED ENA WITHOUT INCIDENT. THE BETA BACKUP AND AUTOFEATHER SYSTEMS WERE DEFERRED AND THE AIRCRAFT WAS REPOSITIONED TO ANC ON A SPECIAL FLIGHT PERMIT. MAINTENANCE VERIFIED THE BETA BACKUP SYSTEM TO BE FUNCTIONING CORRECTLY BUT FOUND A WIRE ON THE AUTOFEATHER SOLONOID VALVE CHAFED AND SHORTED TO GROUND. THE CHAFED WIRE WAS REPAIRED AND GROUND RUNUP DETERMINED AUTOFEATHER OPERATING NORMALLY. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 1H72 3T A9EA 19950421002161995042100216EA 1995 4 21 HERA9509 219950330A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 2 FAILED A HERAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 AL035632C9843 UC81 PCE32436 FLT 1463 - AIR RETURN ANC, NR 2 ENGINE HAD TO BE SHUT DOWN DUE TO INTERNAL FAILURE. THE AIRCRAFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. (W) 2L72 4T4 TRTA24CE E4EA 19950421002171995042100217 1995 4 21 MRKA9517 419950201A34511673A LAMP BOEING737 73725A 1384481NM NR 1 DME FAILED A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL03685MA 23791 RETURN TO GATE DUE NR 1 DME INDICATOR ON CAPTAIN SIDE BLANK AND NR 2 DME DEFERRED. RELAMPED DME INDICATOR AND RETURNED AIRCRAFT TO SERVICE. (W) 2L72 4F RTA16WE 19950421002181995042100218NM 1995 4 21 MRKA9518 119950202A3260189915 SWITCH BOEING737 7374S3 1384711NM LT MLG OUT OF ADJUST A MRKAK NONE N FALSE WARNING CRCRUISE 1 AL03691MA 24166 LEFT MAIN LANDING GEAR RED LIGHT FLICKERS INTERMITTENTLY DURING FLIGHT. ADJUSTED PROXIMITY SWITCH AND OPS CHECKED PER MM. (W) 2L72 4F RTA16WE 19950421002191995042100219NM 1995 4 21 MRKA9519 119950127A3350P4010033210 EEL BATTERY BOEING737 7374S3 1384711NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03691MA 24166 DOOR 1R, 2L, AND 2R EVACUATION SLIDE BATTERIES FAILED FUNCTIONAL TEST. REMOVED AND REPLACED BATTERIES. (W) 2L72 4F RTA16WE 19950421002201995042100220NM 1995 4 21 MRKA9520 119950202A3260189915 UPLOCK SWITCH BOEING737 7374S3 1384711NM LT MLG FAILED A MRKAO OTHER N FALSE WARNING CRCRUISE 1 AL03691MA 24166 LEFT MAIN LANDING GEAR RED LIGHT INTERMITTENT ON IN FLIGHT. REMOVED AND REPLACED LEFT MAIL LANDING GEAR UPLOCK SENSOR PER MAINTENANCE MANUAL 32-32-31 AND PERFORMED EXTENSION AND RETRACTION PER MM 32-32-00. (W) 2L72 4F RTA16WE 19950421002211995042100221NM 1995 4 21 MRKA9521 119950207A35304566M37B042N PBE BOEING737 7373M8 1384615NM FLIGHT DECK DAMAGED A MRKAK NONE O OTHER ININSP/MAINT 1 AL03681MA 24376 CONTROL CABIN PBE RED INDICATOR MISSING. REMOVED AND REPLACED PBE. (W) 2L72 4F RTA16WE 19950421002221995042100222NM 1995 4 21 MRKA9522 119950213A35304566M37B042N PBE INDICATOR BOEING737 7373M8 1384615NM FLIGHT DECK PROTRUDING A MRKAK NONE O OTHER ININSP/MAINT 1 AL03681MA 24376 REMOVED AND REPLACED CONTROL CABIN PBE DUE INDICATOR BUTTON PROTRUDING. (W) 2L72 4F RTA16WE 19950421002231995042100223NM 1995 4 21 MRKA9523 119950215A335020121 EEL PWR SUPPLY BOEING737 7374S3 1384711NM CABIN INOP A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03691MA 24166 REMOVED AND REPLACED POWER SUPPLY DUE OVERWING EMERGENCY EXIT SIGN INOPERATIVE. (W) 2L72 4F RTA16WE 19950421002241995042100224NM 1995 4 21 MRKA9524 119950217A335020131A EEL BATTERY PACK BOEING737 73725A 1384481NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03685MA 23791 REMOVED AND REPLACED FORWARD RIGHT AND AFT LEFT EMERGENCY EXIT SIGN BATTERY PACKS DUE LOW CAPACITY. (W) 2L72 4F RTA16WE 19950421002251995042100225NM 1995 4 21 MRKA9525 119950222A3350862101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03674MA 23292 FLOOR PROXIMITY LIGHT AT DOOR 1L FAILED TEST. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECKED OK. (W) 2L72 4F RTA16WE 19950421002261995042100226 1995 4 21 MRKA9526 419950222A2565D31354433 EVAC SLIDE BOEING737 73725A 1384481NM DOOR 1R LOW PRESS A MRKAK NONE O OTHER ININSP/MAINT 1 AL03685MA 23791 REMOVED AND REPLACED EVACUATION SLIDE ON DOOR 1R DUE LOW PRESSURE. (W) 2L72 4F RTA16WE 19950421002271995042100227NM 1995 4 21 MRKA9527 119950222A335020131A EEL BATTERY BOEING737 7374S3 1384711NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03686MA 24795 REMOVED AND REPLACED RIGHT OVERWING EXIT SIGN BATTERY DUE LOW VOLTS. (W) 2L72 4F RTA16WE 19950421002281995042100228NM 1995 4 21 MRKA9528 119950223A335020131A EEL BATTERY BOEING737 7373M8 1384615NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03681MA 24376 AFT SECTION OF FLOOR PROXIMITY LIGHTING INOP. REMOVED AND REPLACED BATTERY. OPERATIONAL CHECKED OK. (W) 2L72 4F RTA16WE 19950421002291995042100229NM 1995 4 21 MRKA9529 119950228A335020131A20127 EEL BATT CHARGER BOEING737 7373M8 1384615NM CABIN FAILED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03681MA 24376 AISLE LIGHT AT ROW 17R INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AND CHARGER ASSEMBLY. (W) 2L72 4F RTA16WE 19950421002301995042100230NM 1995 4 21 MRKA9530 119950302A3350862101401 EEL BATTERY BOEING737 7372T4C 1384501NM CABIN FAILED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03675MA 23065 FLOOR PROXIMITY LIGHTS AT ROW ELEVEN AND RIGHT OVERWING EXIT FAILED TEST. REMOVED AND REPLACED BATTERY PACKS. OPERATIONAL CHECKED OK. (W) 2L72 4F RTA16WE 19950421002311995042100231NM 1995 4 21 MRKA9531 119950304A5230 DOOR BOEING737 7374Y0 1384705NM CARGO COMPT OBSTRUCTED A MRKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL032FOR 23981 AIR RETURN DUE AIRCRAFT WOULD NOT PRESSURIZE. INSPECTION FOUND CARGO NET P/N 657896640 OBSTRUCTING AFT CARGO DOOR PRESSURE SEAL. REMOVED OBSTRUCTION AND PRESSURIZED AIRCRAFT PER MM 21-21-00. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950421002321995042100232NM 1995 4 21 MRKA9532 119950305A801297925461 VALVE BOEING737 7372X6C 1384552NM NR 1 ENGINE FAILED A MRKAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AL03673MA 23124 RETURN TO GATE DUE TO NR 1 START VALVE LIGHT FLICKERING DURING TAXI. REMOVED AND REPLACED START VALVE. OPERATIONAL CHECKED AND RETURNED AIRCRAFT TO SERVICE. (W) 2L72 4F RTA16WE 19950421002331995042100233EU 1995 4 21 MRKA9533 219950308A7320BACC63BP10A5S6L CONNECTOR BOEING737 7374Y0 1384705NM CFMINTCFM56 CFM563B2 13802EU NR 2 ENG CORRODED A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL032FOR 24345 RETURN TO GATE DUE NR 2 ENGINE WOULD NOT ACCELERATE. CLEANED LOW IDLE CANNON PLUG ON MAIN ENGINE CONTROL. OPERATIONAL CHECKED OK. (W) 2L72 4F4 FRTA16WE E21EU 19950421002341995042100234NM 1995 4 21 MRKA9534 119950308A32414265101 SHIELD BOEING737 7372T4C 1384501NM ANTI-SKID SYSTEMFAILED A MRKAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AL03675MA 23065 RETURN TO GATE DUE OUTBOARD ANTI-SKID INOPERATIVE LIGHT ILLUMINATED DURING TAXI. REMOVED AND REPLACED ANTI-SKID SHIELD. OPERATIONAL CHECKED OK. (W) 2L72 4F RTA16WE 19950421002351995042100235NM 1995 4 21 MRKA9535 119950315A326065661227 SENSOR BOEING737 7372T4C 1384501NM RT MLG FAILED A MRKAO OTHER N FALSE WARNING CRCRUISE 1 AL03676MA 23066 GREEN RIGHT GEAR LIGHT ON INTERMITTENTLY IN FLIGHT. OVERHEAD LIGHT WORKS NORMAL. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SENSOR. OPERATIONAL CHECK PER MM AND RETURNED AIRCRAFT TO SERVICE. (W) 2L72 4F RTA16WE 19950421002361995042100236NM 1995 4 21 MRKA9536 119950318A21317638101 CONTROLLER BOEING737 7374S3 1384711NM CABIN INOP A MRKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03686MA 24795 AIR RETURN DUE AIRCRAFT WOULD NOT PRESSURIZE ON CLIMB-OUT FROM DEN. REMOVED AND REPLACED PRESSURE CONTROLLER AND OPERATIONAL CHECKED PER MM 21-31-00. (W) 2L72 4F RTA16WE 19950421002371995042100237NM 1995 4 21 MRKA9537 119950325A35304566M7B042N PBE SEAL BOEING737 7374S3 1384711NM FLIGHT DECK BROKEN A MRKAK NONE O OTHER ININSP/MAINT 1 AL03690MA 24165 REMOVED AND REPLACED PBE IN CONTROL CABIN DUE VACUUM SEAL BROKEN. (W) 2L72 4F RTA16WE 19950421002381995042100238NM 1995 4 21 MRKA9538 119950326A35304566M7B042N PBE SEAL BOEING737 7372T4C 1384501NM CABIN BROKEN A MRKAK NONE O OTHER ININSP/MAINT 1 AL03676MA 23066 REMOVED AND REPLACED PBE IN OVERHEAD EMERGENCY EQUIPMENT BAG. (W) 2L72 4F RTA16WE 19950421002391995042100239NM 1995 4 21 MRKA9539 119950326A3350862101401 EEL BATTERY PACK BOEING737 7372T4C 1384501NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03676MA 23066 REMOVED AND REPLACED LEFT OVERWING EXIT FLOOR PROXIMITY LIGHT BATTERY PACK DUE FAILED TEST. (W) 2L72 4F RTA16WE 19950421002401995042100240NM 1995 4 21 MRKA9540 119950321A555269560273 ATTACH PLATE BOEING737 7374Y0 1384705NM LT ELEVATOR LOOSE A MRKAK NONE O OTHER ININSP/MAINT 1 AL032FOR 24345 DURING C-INSPECTION, THE LEFT OUTBOARD ELEVATOR HINGE ATTACH PLATES WERE FOUND LOOSE AND FRETTING, WHERE THEY ATTACH TO THE AFT END OF THE STABILIZER RIB AT STATION 213.32. THE HINGE ATTACH PLATES WERE REPLACED AND THE RIB END FITTING REPAIRED PER S/B 737-55-1054. (W) 2L72 4F RTA16WE 19950421002411995042100241NM 1995 4 21 MRKA9541 119950317A32227437FT972P3 STRUT BOEING737 7372X6C 1384552NM NLG FLAT A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL03674MA 23292 RETURN TO GATE DUE NOSE STRUT FLAT WHEN TAXIING. SERVICED NOSE STRUT WITH OIL AND AIR. (W) 2L72 4F RTA16WE 19950421002421995042100242NM 1995 4 21 MRKA9542 119950331A801232896302 VALVE BOEING737 7373M8 1384615NM NR 2 ENGINE FAILED A MRKAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AL03681MA 24376 RETURN TO GATE WHEN NR 2 START VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED START CONTROL VALVE. (W) 2L72 4F RTA16WE 19950421002431995042100243CE 1995 4 21 PLGA325951 119950325A32302058393 CONNECTOR BEECH 1900 1900C 1154161CE GEAR HANDLE LOOSE A PLGAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NE053069K UB71 BOS - AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND INSPECTED IT FOR FERRY FLIGHT PSM. PSM MAINTENANCE FOUND POWER WIRE G6D22 HAD PUSHED OUT OF THE SOCKET (PIN 4) AT THE LANDING GEAR CONTROL HANDLE. MAINTENANCE REPLACED THE CONNECTOR AND OPERATIONAL CHECKED THE SYSTEM IAW THE BEECH MM. ALL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T RTA24CE 19950421002441995042100244CE 1995 4 21 PLGA327951 119950327A61209994000115 CABLE LOCKPLATE BEECH 1900 1900 1154160CE PEDESTAL LOOSE A APLGAK NONE O OTHER ININSP/MAINT 1 NE05805BE UB38 DURING COMPLIANCE OF FCD 76-7 THE RIVETS SECURING THE PROPELLER CONTROL CABLE LOCKPLATE TO THE AIRFRAME STRUCTURE WERE FOUND TO BE LOOSE. THIS RESULTED IN THE LOCKPLATE TO FLEX SIGNIFICANTLY AND NOT PROPERLY SECURE THE PROPELLER CONTROL CABLES WHEN THE PROPELLER CONTROL LEVERS WERE MOVED TO THE FEATHER POSITION. THE RIVETS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA24CE 19950421002451995042100245EU 1995 4 21 PLGA330952 119950330A5347 SEAT TRACK SAAB SF340 340B 7860101EU FS 630-668 CORRODED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05351BE 340B237 DURING C-CHECK INSPECTION, FOUND CORROSION AT LAVATORY SEAT TRACK BEAM BETWEEN STATIONS 630 AND 668. THE CORROSION HOLES WERE CLEANED, TREATED AND REPAIRED IAW SAAB STRUCTURAL REPAIR MANUAL 53-70-60 PAGES 206-207 REVISION DATE MAR 31/94. (W) 2L72 4T RTA52EU 19950421002461995042100246EU 1995 4 21 PLGA330953 119950330A5321 FLOOR SAAB SF340 340B 7860101EU FS 160.10 CORROSION A PLGAK NONE O OTHER ININSP/MAINT 1 NE05351BE8595 340B237 DURING C-CHECK INSPECTION, FOUND MINOR CORROSION ON COCKPIT FLOOR STATION 160.10 TO 176.10. REMOVED CORROSION IAW SAAB SRM CHAPTER 51-70-40, TREATED AREA IAW SAAB SRM CHAPTER 51-20-40 AND SEALED AREA IAW SAAB SRM CHAPTER 51-20-50. (W) 2L72 4T RTA52EU 19950421002471995042100247EU 1995 4 21 PLGA330954 119950330A5310 STRUCTURE SAAB SF340 340B 7860101EU FS 231-288 CORRODED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05351BE 340B237 DURING C-CHECK, INSPECTION FOUND STRUCTURE WITH MINOR CORROSION BETWEEN STATION 231 AND STATION 288. CLEANED CORRODED AREA IAW SAAB SRM CHAPTER 51-70-40 AND APPLIED PROTECTIVE TREATMENT IAW SAAB SRM CHAPTER 51-20-40. SEALED AREA IAW SAAB SRM CHAPTER 51-20-50. (W) 2L72 4T RTA52EU 19950421002481995042100248SO 1995 4 21 WTAA950125 119950320A27425299 TRIM ACTUATOR EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A WTAAK NONE F FLT CONT AFFECTED CRCRUISE 1 WP17276UE 120067 ACV - ELEVATOR TRIM FROZE DURING FLIGHT. AIRCRAFT LANDED IN ACV WITHOUT INCIDENT. MAINTENANCE INSPECTED AND LUBED BOTH ELEVATOR TRIM ACTUATORS. OPERATINAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002491995042100249 1995 4 21 WTAA950126 319950321A6140MS252531 SWITCH EMB 120 EMB120RT SO LT PROP DIRTY A WTAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP17120AM 120012 FAT - LEFT BETA LIGHT FLASHING AT ALL POWER LEVER SETTINGS BELOW FLIGHT IDLE ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE CLEANED AND LUBRICATED LOW PITCH STOP MICROSWITCH. PERFORMED OPERATIONAL CHECK OF SYSTEM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002501995042100250EU 1995 4 21 WTAA950127 119950321A27505148YMK85 FLAP SELECTOR BAG JETSTMJETSTM3101 1500215EU COCKPIT FAILED A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17331CA 793 RDD - GEAR HORN CAME ON IN FLIGHT AN UNABLE TO CANCEL UNTIL GEAR WAS EXTENDED. AIRCRAFT LANDED IN RDD WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP SELECTOR AND PERFORMED AND OPERATIONAL CHECK OF FLAP AND GEAR WARNING SYSTEM AND FOUND TO BE OPERATING NORMALLY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002511995042100251SO 1995 4 21 WTAA950128 119950321A27425299 TRIM ACTUATOR EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A WTAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 WP17276UE 120067 SMF - ELEVATOR TRIM FROZE ON LEVEL OFF AT 19,000 FEET WHILE EN ROUTE FROM RDD TO SFO. AIRCRAFT DIVERTED TO SMF WITHOUT INCIDENT. MAINTENANCE INSPECTED AND LUBED BOTH ELEVATOR TRIM ACTUATORS AND PERFORMED OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002521995042100252SO 1995 4 21 WTAA950129 119950321A27305299 TRIM ACTUATOR EMB 120 EMB120RT SO HORIZ STAB CONTAMINATION A WTAAK NONE F FLT CONT AFFECTED CRCRUISE 1 WP17276UE 120067 FAT - ELEVATOR TRIM FROZE AT ALTITUDE ON REPOSITION FLIGHT TO FAT. MAINTENANCE REPLACED BOTH ELEVATOR TRIM ACTUATORS AND PERFORMED OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. TEST FLIGHT ACCOMPLISHED AND FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002531995042100253SO 1995 4 21 WTAA950130 119950322A27523203001007 FLAP ACTUATOR EMB 120 EMB120RT SO LT TE FLAP FAILED A AWTAAO OTHER J WARNING INDICATION LDLANDING 1 WP17286UE 120175 SBA - FLAP CONTROL FAULT REPORTED ON FLAPS DURING LANDING. OUTBOARD PAIR WOULD NOT GO PAST 10 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT OUTBOARD FLAP ACTUATOR AND PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM AND FOUND SYSTEM TO CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002541995042100254EU 1995 4 21 WTAA950131 119950322A3260 GEAR WARNING BAG JETSTMJETSTM3101 1500215EU RT MLG ACTIVATED A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17430UE 784 SFO - RIGHT MAIN LANDING GEAR RED INTRANSIT LIGHT ILLUMINATED AND LANDING GEAR POSITION WARNING HORN ACTIVATED MOMENTARILY WITH LANDING GEAR IN DOWN POSITION ON FINAL APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR ASSEMBLY AND LANDING GEAR POSITION INDICATION SYSTEM. NO DEFECTS NOTED. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002551995042100255EU 1995 4 21 WTAA950132 119950323A3260DN1050ZMK2 INDICATOR BAG JETSTMJETSTM3101 1500215EU LT MLG LOOSE A WTAAO OTHER O OTHER APAPPROACH 1 WP17421UE 804 SFO - LEFT MAIN LANDING GEAR 'GREEN' POSITION LIGHT REPORTED INTERMITTENT WHEN GEAR SELECTED DOWN. MAINTENANCE FOUND GEAR INDICATION LIGHT SOCKET IN POSITION INDICATOR ASSEMBLY LOOSE. TIGHTENED SOCKET. NO OTHER DEFECTS NOTED WITH GEAR POSITION INDICATION SYSTEM. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002561995042100256SO 1995 4 21 WTAA950133 119950323A323020885 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP17268UE 120207 SFO - AFTER TAKEOFF LEFT MAIN LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR UPLOCK ACTUATOR. LANDING GEAR OPERATION NORMAL ON GEAR RETRACTION CHECK AND SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002571995042100257EU 1995 4 21 WTAA950134 119950323A3260 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU RT MLG BROKEN A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17430UE 784 ACV - RIGHT MAIN LANDING GEAR RED INTRANSIT LIGHT ILLUMINATED AND LANDING GEAR POSITION WARNING HORN ACTIVATED MOMENTARILY WITH LANDING GEAR IN DOWN POSITION ON FINAL APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR ASSEMBLY AND LANDING GEAR POSITION INDICATION SYSTEM. FOUND AND REPAIRED BROKEN WIRE AT RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH (P/N 622800200). GEAR POSITION INDICATION NORMAL. AIRCRAFT RETURNED TO SERVICE (W) 2L72 4T RTA21EU 19950421002581995042100258EU 1995 4 21 WTAA950135 119950323A26121379111H FIRE LOOP BAG JETSTMJETSTM3101 1500215EU LT ENGINE DIRTY A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17107XV 723 SBA - LEFT ENGINE FIRE WARNING AND DETECTION SYSTEM FAILS TO TEST. CLEANED MOISTURE FROM LEFT ENGINE FIRE WARNING SYSTEM ELECTRICAL CONNECTORS. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002591995042100259 1995 4 21 WTAA950137 319950326A6110 PROPELLER BAG JETSTMJETSTM3101 1500215EU RIGHT BIRD STRIKE A WTAAD RETURN TO BLOCK C F.O.D. TXTAXI/GRND HDL 1 WP17430UE 784 SJC - BIRD STRIKE REPORTED AT RIGHT PROPELLER DURING TAXI. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION IAW JETSTM-3101 MM 5-50-25. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002601995042100260SO 1995 4 21 WTAA950139 119950327A3260922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO LT MLG FAILED A WTAAO OTHER N FALSE WARNING DEDESCENT 1 WP17288UE 120184 SFO - LEFT MAIN LANDING GEAR 'B' SYSTEM GREEN INDICATION LIGHT ILLUMINATED IN FLIGHT DURING DESCENT. MAINTENANCE DEFERRED LANDING GEAR 'B' INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED LEFT MAIN LANDING GEAR 'B' SYSTEM DOWNLOCK PROXIMITY SENSOR. LANDING GEAR POSITION INDICATION SYSTEM OPERATIONAL CHECK NORMAL. (W) 2L72 4T RTA31SO 19950421002611995042100261EU 1995 4 21 WTAA950140 119950327A3260 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU NOSE GEAR BROKEN A WTAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 WP17424UE 796 LAX - NOSE GEAR POSITION INDICATION FAILED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE ON NOSE GEAR UPLOCK MICROSWITCH (P/N 9005EN38). LANDING GEAR POSITION INDICATIONS NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002621995042100262SO 1995 4 21 WTAA950143 119950329A2751 WARNING EMB 120 EMB120RT SO FLAP CONTROL ACTIVATED A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17286UE 120175 SFO - FLAP CONTROL FAULT REPORTED ON FLAPS AFTER FLAP RETRACTION. SECOND INBOARD FLAP ANNUNCIATOR PAIR FLASHING. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEARED FLAP FAULT ON COMPUTER. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM. UNABLE TO DUPLICATE DISCREPANCY. FLAP SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950421002631995042100263EU 1995 4 21 WTAA950144 119950324A3260622800100 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17430UE 784 MOD - LANDING GEAR INDICATION FAILED TO INDICATE GEAR EXTEND ON INITIAL ATTEMPT. GEAR OPERATION NORMAL ON SUBSEQUENT ATTEMPT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR RADIUS ROD MICROSWITCH. LANDING GEAR POSITION INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002641995042100264EU 1995 4 21 WTAA950145 119950330A335086H00247308 EEL LAMP BAG JETSTMJETSTM3101 1500215EU CABIN FAILED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17419UE 779 SCK - CREW REPORTED CABIN OVERHEAD EMERGNCY LIGHT INOPERATIVE. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LAMP. CABIN EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950421002651995042100265WP 1995 4 21 95005701146 119950412A2430 RCCB DOUG DC10 DC1040 3023508WP EMERGENCY POWER FAILED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01146US 46755 DURING PREFLIGHT CHECK, THE AIRCRAFT EMERGENCY POWER FAILED TO TEST. FOUND REMOTE CONTROL CIRCUIT BREAKER (RCCB) B1-189 STUCK OPEN. REPLACED RCCB, OPERATIONAL CHECK OK. 2L73 4F A22WE 19950421002661995042100266EU 1995 4 21 9505653242 119950410A2432350L5100508 LIMITER AIRBUS320 A320211 3930320EU NR 2 BATTERY MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01342NW6858 2071 381 AFTER TAKEOFF FROM MSP, THE EMERGENCY GENERATOR FAULT LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS LOWERED, AND RETURNED WHEN THE GEAR WAS RAISED. FLIGHT CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 BATTERY CHARGER LIMITER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950421002671995042100267NE 1995 4 21 9505665518 219950413A7321 EEC STATOR BOEING757 757251 1384970NM PWA 2037 PW2037 NE RT ENGINE FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01518US 23196 716473 DURING CRUISE, RECEIVED 'R ENG SEC CONT' MESSAGE AND LOST OIL TEMPERATURE INDICATIONS. AIRCRAFT DIVERTED TO DTW. RIGHT EEC STATOR WAS REPLACED AND THE AIRCRAFT CHECK OK FOR SERVICE. 2L72 4F4 FRTA2NM E17NE 19950421002681995042100268NM 1995 4 21 9505672704 119950410A73318TJ80GAA2 POWER SUPPLY BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE FUEL FLOW SYST MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01801EA23289397 21451 ON CLIMBOUT FROM MEM, ALL THREE FUEL FLOW INDICATORS WERE ERRATIC. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW SYSTEM POWER SUPPLY. SYSTEM OPERATION CHECKED OK, AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950421002691995042100269NE 1995 4 21 9505681145 219950413A7200 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 MALFUNCTIONED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL01145US 46754 686128 DURING CLIMB, THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO LAX WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. NO FUEL WAS DUMPED. BLACK OIL WAS FOUND AND THE AIRCRAFT WAS FERRIED TO MSP WHERE THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19950421002701995042100270WP 1995 4 21 9505691221 119950412A3350 EEL WIRE DOUG DC10 DC1040 3023508WP CABIN BROKEN A NWAAK NONE L NO TEST CRCRUISE 1 GL01221NW 46579 DURING CRUISE, ALL EMERGENCY LIGHTS ILLUMINATED. PULLED CIRCUIT BREAKER AND LIGHTS EXTINGUISHED. AIRCRAFT CONTINUED TO DESTINATION. REPAIRED WIRE ON CANNON PLUG P1-1789. OPERATIONAL CHECK OK. 2L73 4F A22WE 19950421002711995042100271NE 1995 4 21 9505719878 219950415A7321 FUEL CONTROL DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01787NC 48149 688777 ON TAKEOFF, THE NR 1 ENGINE EPR AND N1 ROLLED BACK TO IDLE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL UNIT AND THE ENGINE WAS RUNUP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950421002721995042100272WP 1995 4 21 9505721153 119950413A5320 ANGLE DOUG DC10 DC1040 3023508WP FS 1162 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01153US 46762 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE 'TEE' ANGLE AT FS 1162, RBL 47 ABOVE ACCESS 142AZ. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 11-97997. 2L73 4F A22WE 19950421002731995042100273WP 1995 4 21 9505731153 119950413A5320 BRACKET DOUG DC10 DC1040 3023508WP FS 1761-1782 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01153US 46762 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SHEAR TIE AT FS 1761 TO 1782, STR 45R AND 46R. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 11-97995. 2L73 4F A22WE 19950421002741995042100274WP 1995 4 21 9505749863 119950414A7711JG298H1 EPR TRANSMITTER DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE AFT EQUIP BAY MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01772NC3043937 47774 696729 ON TAKEOFF, THE NR 2 ENGINE EPR INDICATION HUNG AT 1.4. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. A SERVICEABLE EPR TRANSMITTER WAS INSTALLED AND TESTED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950421002751995042100275NM 1995 4 21 9505752275 119950414A274132EN144 SWITCH BOEING727 727251 138408HNM STAB TRIM WARN INOPERATIVE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01275US 21154 DURING APPLICATION OF TAKEOFF POWER, INTERMITTENT WARNING HORN SOUNDED. ABORTED TAKEOFF, RECYCLED FLAP AND SPEED BRAKE CONTROLS. ON SECOND DEPARTURE ATTEMPT, SAME RESULTS OCCURRED. RETURNED TO THE GATE AND DEPLANED AIRCRAFT. MAINTENANCE FOUND S532 UPPER STABILIZER TRIM WARNING SWITCH INOPERATIVE. REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK, NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950421002761995042100276NM 1995 4 21 95UAL757010 119950417A2780 SENSOR BENDIX 18196915 BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 LE SLAT FAILED A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29511UA 24799 LANDED UNDER AMBER ALERT, BECAUSE THE LEADING EDGE DEVICES WOULD NOT EXTEND. REPLACED THE NR 1 SLAT POSITION SENSOR. SYSTEM OP CHECKED OK. 2L72 4F4 FRTA2NM E17NE 19950421002771995042100277WP 1995 4 21 ABXA9500333 119950414A26125777574501 FIRE ELEMENT DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE NR 4 ENG DEFECTIVE A ABXAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL23847AX 46031 644309 DURING CRUISE, THE NUMBER FOUR ENGINE FIRE LIGHT ILLUMINATED AND THE FIRE BELL SOUNDED. THE ENGINE WAS SECURED AND A FIRE BOTTLE WAS DISCHARGED. DURING THE WINDMILLING PROCEDURE, THE FIRE LIGHT FLICKERED MOMENTARILY. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT TO ILN. FOUND THE FORWARD UPPER FIRE DETECTOR ELEMENT DEFECTIVE. REMOVED AND REPLACED THE NUMBER FOUR ENGINE FIRE DETECTOR ELEMENT. SYSTEM OPERATIONAL CHECKED GOOD IAW DC-8 MM CHAPTER 26. 2L74 4F4 F 4A25 1E8 19950421002781995042100278NE 1995 4 21 COM11859 219950413A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CLCLIMB 1 SO01205CA132382276 120205 115345 LEFT ENGINE FAILED ABRUPTLY IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE. 2L72 4T4 TRTA31SO E20NE 19950421002791995042100279SO 1995 4 21 COM11860 119950416A5230 DOOR EMB 120 EMB120RT SO CARGO COMPT NOT LATCHED A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO011117H 120117 CARGO DOOR WARNING ACTIVATED DURING TAKEOFF. CLOSED AND LATCHED DOOR, PROBLEM DID NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950421002801995042100280NE 1995 4 21 COM11861 219950416A7200PW118 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT VIBRATION A COMADE RETURN TO BLOCK ENGINE SHUTDOWN E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01249CA119362207 120230 115348 UNUSUAL NOISE AND VIBRATION FROM RT ENGINE DURING TAXI. REPLACED RT ENGINE. 2L72 4T4 TRTA31SO E20NE 19950421002811995042100281SO 1995 4 21 COM11862 119950413A73123035817 FUEL HEATER EMB 120 EMB120RT SO RT ENGINE LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01267CA1176054 120259 FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE ENGINE FUEL TO OIL HEAT EXCHANGER. 2L72 4T RTA31SO 19950421002821995042100282SO 1995 4 21 COM11863 119950414A27203211001003 PCU EMB 120 EMB120RT SO RUDDER LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO011110J1375311852 120110 HYDRAULIC FLUID LEAK AT VERTICAL STABILIZER. REPLACED THE RUDDER POWER CONTROL UNIT. 2L72 4T RTA31SO 19950421002831995042100283EU 1995 4 21 COM31061 119950412A324650092371 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01370CA3637 603 APR930525 340A010 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950421002841995042100284EU 1995 4 21 COM31062 119950413A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01341CA2702 346 AUG930547 340A021 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO THE WORN LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950421002851995042100285EA 1995 4 21 COM60453 119950413A52103HT1 SWITCH CNDAIRCL600 CL6002B19 EA CABIN DOOR OUT OF ADJUST A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01931CA 7037 OVERBOARD COOL MESSAGE ON EICAS. AIRCRAFT WOULD NOT PRESSURIZE. ADJUSTED THE COOLING VALVES SWITCH ON CABIN DOOR HANDLE. 2L72 4F RTA21EA 19950421002861995042100286NM 1995 4 21 DL72W951461 119950411A5754 RIB BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 RIB CRACKED NR 2 L/E SLAT NR 4 RIB CRACKED (MARKED). STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 57-50-3 FIG 9. 2L73 4F A3WE 19950421002871995042100287NM 1995 4 21 DL72W951462 119950411A5754 RIB BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 RIB CRACKED NR 2 L/E SLAT NR 3 RIB CRACKED (MARKED). STOP DRILLED CRACK AS PER SRM 57-50-3. FABRICATED DOUBLER AS PER SRM 57-50-3 FIG 9 SHEET 1 AND 2. 2L73 4F A3WE 19950421002881995042100288NM 1995 4 21 DL72W951463 119950410A5754 RIB BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 RIB CRACKED NR 2 L/E SLAT NR 5 RIB FROM INBD END CRACKED FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-3 FIG 9. FOUND AT HMV. 2L73 4F A3WE 19950421002891995042100289NM 1995 4 21 DL72W951474 119950402A5754 RIB BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 NR 3 SLAT RIB CRACKED IB RIB AT ACT ATTACH POINT IS CRACKED AFT LOWER CORNER. REPAIRED PER MM 57-54-00 PG 806-807. 2L73 4F A3WE 19950421002901995042100290NM 1995 4 21 DL72W951475 119950402A5754 ANGLE BOEING727 727247 138408FNM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 NR 8 SLAT ANGLE CRACKED, ANGLE IS CRACKED UNDER IB UPSTOP FITTING NR 8 SLAT. REPAIRED PER MM 57-54-0 FIG 812. FOUND AT HMV, INSPECTION. 2L73 4F A3WE 19950421002911995042100291NM 1995 4 21 DL72W951477 119950330A5313 STRINGER BOEING727 727247 138408FNM FS 490-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND STRINGER 28L CORRODED AT FS 490 TO 500. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950421002921995042100292NM 1995 4 21 DL72W951478 119950402A5754 RIB BOEING727 727247 138408FNM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 RIB CRACKED NR 5 SLAT, FWD TOP CORNER OF RIB MARKED 119IB RIB AT ACT IS CRACKED. REPAIRED PER MM 57-54-0 PG 815 TO 815A. FOUND AT HMV. 2L73 4F A3WE 19950421002931995042100293NM 1995 4 21 DL72W951479 119950402A5754 RIB BOEING727 727247 138408FNM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 NR 5 SLAT RIB CRACKED, OB RIB OF OB TRACK ATTACH POINT IS CRACKED AT SCREW HOLE 2 INCHES UP FROM LOWER SKIN. REPAIRED PER SRM 57-50-3 FIG 9. 2L73 4F A3WE 19950421002941995042100294NM 1995 4 21 DL72W951480 119950409A5743 FITTING BOEING727 727247 138408FNM LT WING CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 LMG SUPPORT BEAM OB FITTING AT REAR SPAR HAS CORROSION IN BORE OF FWD SUPPORT FITTING. REPAIRED PER SRM 57-40-00 FIG 1. FOUND AT HMV. 2L73 4F A3WE 19950421002951995042100295WP 1995 4 21 DLL17951469 119950323A5743 HOLE LKHEED1011 10113853 5265020WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND HOLE CORRODED/PITTED. FITTING FOR RT MLG ACT. REAMED HOLE TO .690, TURNED BUSHING TO SIZE AND CAD PLATED PER PS 900-3-9, PRIMED HOLE PER PS 900-3-6, INSTALLED BUSHING PER SRM 57-14-00. 2L73 4F A23WE 19950421002961995042100296WP 1995 4 21 DLL17951470 119950410A5313 STRINGER LKHEED1011 10113853 5265020WP FS 297 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND STRINGER CRACKED, STR 37 LOWER RADIUS AT FS 297. FABRICATED SPLICE PER SRM 53-13-00 PG 806 FIG 804, TREATED AND PAINTED AREA, INSTALLED SPLICE. 2L73 4F A23WE 19950421002971995042100297WP 1995 4 21 DLL17951471 119950408A3020 INLET RING LKHEED1011 10113853 5265020WP NR 2 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND RING CRACKED, ON ANTI-ICE RING ON NR 2 ENG. REMOVED DAMAGED SECTION OF RING, FABRICATED REPAIR DOUBLER PER SRM 54-34-00 PG 804. INSTALLED DOUBLER PER SRM 54-34-00. 2L73 4F A23WE 19950421002981995042100298WP 1995 4 21 DLL17951473 119950408A3020 INLET RING LKHEED1011 10113853 5265020WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND RING CRACKED, INSIDE PANEL 311 DR. DRILLED TACK PATTEN FOR LOWER RIVET CRACK. INSTALLED UPPER REPAIR DOUBLER. REPAIRED CRACK PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950421002991995042100299WP 1995 4 21 MWEA95171 119950414A3350DCELL EEL BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31204ME 47680 DURING C-CHECK, MAINTENANCE REPORTS EMERGENCY LIGHTS IN FWD ENTRANCE AND COCKPIT WENT OUT 5 MINUTES INTO THE 10 MINUTE BURN TEST. REPLACED BATTERIES IN TWO FWD BATTERY PACKS. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950421003001995042100300WP 1995 4 21 MWEA95172 119950415A3350 EEL GROUND WIRE DOUG DC9 DC932 3022066WP CABIN BROKEN A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31204ME 47680 DURING C-CHECK, THE EMERGENCY FLOOR TRACK LIGHTING FROM ROW 18 TO REAR OF A/C WERE ON DIMLY WITH SWITCH TURNED OFF. REPAIRED GROUND WIRE AT BATTERY PACK FOR AFFECTED SEGMENT OF LIGHTS. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950421003011995042100301WP 1995 4 21 MWEA95173 119950415A5542 SKIN DOUG DC9 DC932 3022066WP RUDDER CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31204ME 47680 DURING C-CHECK, THE RUDDER SKIN WAS FOUND CRACKED APPROX 1 INCH ON RIGHT SIDE 4TH RIB FROM TOP. REPAIRED RUDDER SKIN IAW SRM 55-03 FIG 11. RECALCULATED BALANCE, AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950421003021995042100302EU 1995 4 21 QXEA9500114 119950415A3231A78722001 UPLOCK SPRING FOKKER FOKKERF28 F28MK1000 4990808EU LT MLG DOOR BROKEN A QXEAO OTHER J WARNING INDICATION CLCLIMB 1 NM09457US 11036 GEG - LEFT GEAR RED LIGHT REMAINS ILLUMINATED AFTER GEAR DOWN OR UP SELECTION. REPLACED BROKEN RETURN SPRING IN AFT GEAR DOOR UPLOCK ASSY. GEAR INDICATION OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003031995042100303EU 1995 4 21 QXEA9500115 119950415A33501012721 EEL FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 BOI - EMERGENCY EXIT LIGHT AT ROW 11A BROKEN. REPLACED LIGHT ASSY AND LIGHT OP. 2L72 4F RTA20EU 19950421003041995042100304EU 1995 4 21 QXEA9500116 119950415A3260602EN166 SWITCH WIRE FOKKER FOKKERF28 F28MK1000 4990808EU RT WING BROKEN A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09462AU 11054 PDX - RIGHT MAIN GEAR RED AND AMBER LIGHTS SLOW TO EXTINGUISH AFTER GEAR EXTENSION. REPLACED RIGHT HAND AFT MAIN GEAR DOOR SWITCH. INDICATION OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003051995042100305EU 1995 4 21 QXEA9500117 119950415A33501012721 EEL SIGN FOKKER FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 PDX - ROW 12A/B EXIT SIGN WON'T ILLUMINATE. REPLACED EXIT SIGN AT 12A/B AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003061995042100306 1995 4 21 QXEA9500118 419950416A2565S130508 SLIDE FOKKERF28 F28MK1000 4990808EU CABIN LOW PRESS A QXEAK NONE O OTHER ININSP/MAINT 1 NM09803PH 11031 PDX - EVACUATION SLIDE HAS LOW PRESSURE. REPLACED SLIDE ASSY AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003071995042100307EU 1995 4 21 QXEA9500119 119950416A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - SEVERAL OVERHEAD EMERGENCY EXIT LIGHTS INOP. REPLACED BULBS AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003081995042100308EU 1995 4 21 QXEA9500120 119950416A3350MGG1055 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 BOI - EXIT SIGN ABOVE COCKPIT DOOR WON'T ILLUMINATE. REPAIRED TWO BAD WIRES AND REPLACED SEVERAL BULBS. SIGN OPS CHECKED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950421003091995042100309NM 1995 4 21 QXEA9500121 119950416A335010005511 EEL DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT LOOSE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09828PH 287 GEG - OVERHEAD LIGHT IN COCKPIT AND CABIN FLOOR LIGHTS FLASH INTERMITTENTLY. RESET OVERHEAD LIGHT IN COCKPIT AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950421003101995042100310SW 1995 4 21 QXEA9500122 119950416A27202742025007 LINK ROD SWRNGN SWRNGNSA227 SA227AC 8780603SW RUDDER BROKEN A QXEAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NM09385PH AC595 PSC - RUDDER VIBRATION AFTER ROTATION. VIBRATION CONTINUED IN FLIGHT, AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER PROBLEM. RUDDER TRIM TAB TO TAB ACTUATOR ROD WAS BROKEN. REPLACED ROD AND RIGGED TRIM TAB I/A/W MM. THE ROD BROKE BECAUSE THE TAB ACTUATOR FORK END WAS 90 DEGRESS OUT OF POSITION. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950421003111995042100311NM 1995 4 21 UPS202941 119950413A3350 EEL BATTERY PACK BOEING727 727185C 138406NNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01940UP 19826 MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS INOP IN FLIGHT DECK. REPLACED BATTERY PACK PER MM 33-50-101. OPS CHECK OK. 2L73 4F A3WE 19950421003121995042100312NM 1995 4 21 UPS202942 119950413A3350 EEL BULB BOEING727 72725C 138400HNM FLIGHT DECK FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01931UP 19858 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT (UNARMED) ON PILOT'S OVERHEAD INOP. RELAMPED EMER EXIT LIGHTS. OPS CHECK GOOD PER MM 33-50. 2L73 4F A3WE 19950421003131995042100313NM 1995 4 21 UPS402943 119950413A2822705501373634 FUEL PUMP BOEING747 747SR46 NM NR 3 ENG MALFUNCTIONED A IPXAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 SO01689UP 20133 PILOT REPORTED, ENGINE FLAME-OUT AT FL 350. **S/D** REPLACED FUEL PUMP PER EO J T9D 7100-3426 AND TEST 3, 5 MM 71-00-00. LEAK AND OPERATIONAL CHECK OK. 2L74 4F A20WE 19950421003141995042100314WP 1995 4 21 UPS802944 119950414A3260 STRIKER PLATE DOUG DC8 DC871F 302199DWP RT MLG BROKEN A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01702UP 45902 PILOT REPORTED, RIGHT MAIN GEAR ALTERNATE DOOR LIGHT ILLUMINATED AND STAYED ON IN FLIGHT. PERFORMED SECOND UPLATCH CHECK SUCCESSFULLY WITH NO MAIN GEAR DOOR NOT LATCHED ILLUMINATING, APPEARS TO BE ALT SWITCH. FOUND RT SWITCH STRIKER PLATE BROKEN ON RT MAIN GEAR DOOR. REPLACED STRIKER, A/C OK FOR SERVICE. 2L74 4F RT4A25 19950421003171995042100317SW 1995 4 21 95ZZZX1851 119950327A282220506060603 BOOST PUMP BELL 412 412 1182202SW RT FUEL TANK FAILED A ALGAO OTHER J WARNING INDICATION CRCRUISE 1 SW03397AL2656 R3351 36012 DURING CRUISE FLIGHT NR 2, ENGINE FUEL BOOST PUMP PRESSURE FLUCTUATED AND THEN PRESSURE WENT TO ZERO. REPLACED BOOST PUMP. CAUSE UNKNOWN. 1G72 4U H4SW 19950421003181995042100318SW 1995 4 21 95ZZZX1852 119950327A5320206033663118 WINDOW 206033663103BELL 206 206L3 1182108SW RT PAX WINDOWS DEPARTED A ALGAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SW03347AL4742 51381 DURING FLIGHT, THE RIGHT REAR SLIDER WINDOW DEPARTED AIRCRAFT. INSPECTED AIRCRAFT FOR EXTERNAL DAMAGE. NO DEFECTS NOTED. INSTALLED WINDOW. POSSIBLE PASSENGER PUSHED ON WINDOW. 1G71 3U H2SW 19950421003201995042100320NE 1995 4 21 95ZZZX1854 119950315A632076450178118 TRANSMITTER SKRSKYS76 S76A 8143006NE TRANSMISSION FAILED A ALGAK NONE O OTHER ININSP/MAINT 1 SW03376AL 41953161 760002 AFTER LANDING, NOTICED THE TRANSMISSION OIL PRESSURE HAD DROPPED OUT OF THE GREEN AND THEN DROPPED TO ZERO PSI. REPLACED TRANSMISSION OIL PRESSURE TRANSMITTER. 1G72 3U H1NE 19950421003211995042100321EU 1995 4 21 95ZZZX1855 119950315A2930ZE3276 GUIDE SWITCH BOLKMS105 BO105S 5626006EU HYD PACK FAULTY A ALGAO OTHER J WARNING INDICATION CRCRUISE 1 SW032785R S642 HYDRAULIC BLOCK LIGHT ILLUMINATED DURING FLIGHT. SYSTEM SHIFTED TO NR 2. HYD ENGAGED. CONTINUED FLIGHT AND LANDED AS SOON AS PRACTICAL. DRIED OUT GUIDE ASSEMBLY MICROSWITCH. OPERATIONAL CHECKED OKAY. 1G72 3U H3EU 19950421003221995042100322NE 1995 4 21 95ZZZX1856 219950330A73217436024 CONTROL UNIT DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE RIGHT MALFUNCTIONED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA19979VJ 47372 PIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT. FLIGHT RETURNED TO PIT. SINGLE ENGINE TIME WAS TWELVE MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. THE RIGHT ENGINE FUEL CONTROL UNIT WAS ALSO REPLACED AS A PRECAUTION. OPERATIONS CHECKED GOOD. REFERENCE CONTROL USAA950304. (X) 2L72 4F4 F A6WE E2EA 19950421003231995042100323WP 1995 4 21 95ZZZX1857 119950402A2612 CONNECTOR DOUG DC8 DC873F 302199FWP NR 2 ENGINE LOOSE A RRXAO OTHER N FALSE WARNING DEDESCENT 1 WP15870TV 46086 TTPP - ON DESCENT, NR 2 ENGINE HAD INTERMITTENT FIRE WARNING WITH SHORT CIRCUIT GROUND LIGHT. MAINTENANCE INSPECTED ENGINE AND FOUND LOOSE CANNON PLUG ON LOWER FIRE LOOP. TIGHTENED CANNON PLUG AND SYSTEM CHECKED NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2L74 4F RT4A25 19950421003241995042100324WP 1995 4 21 95ZZZX1858 119950329A3230 UPLATCH DOUG DC8 DC863 302198AWP RT MLG DOOR LACK OF LUBE A RRXAON OTHER X ENGINE FLAMEOUT CLCLIMB 1 WP15797AL 46163 KBDL/KDAY - FLT 111 - ON CLIMB-OUT FROM KBDL, GEAR UPLATCH CHECK FAILED. DOORS NOT LATCHED LIGHT REMAINED ON. CYCLED GEAR SEVERAL TIMES AND THE LIGHT EXTINGUISHED. MAINTENANCE CLEANED AND LUBED THE RT GEAR DOOR FLIGHT LOCK AND GEAR UPLATCH. ALL GEAR INDICATIONS WERE NORMAL ON GEAR SWING IAW MM 32-8-2. N797AL RETURNED TO SERVICE. 2L74 4F 4A25 19950421003251995042100325WP 1995 4 21 95ZZZX1859 119950327A2612390D FIRE WARNING DOUG DC8 DC863F 302198FWP NR 2 ENGINE DEFECTIVE A RRXAO OTHER N FALSE WARNING CRCRUISE 1 WP15921R 46145 EINN/KORD - FLT 9123 - HAD INTERMITTENT FIRE WARNING ON NR 2 ENGINE DURING CRUISE. KORD MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FIRE WARNING AMPLIFIER, REPLACED WIRES FROM AMPLIFIER TO NR 2 ENGINE PYLON BOX. SYSTEM OPS CHECKED GOOD. (X) 2L74 4F 4A25 19950421003261995042100326GL 1995 4 21 95ZZZX1860 319950314A6110C2858 RETAINER BEECH 1900 1900C 1154161CE HARTZLHCB4M HCB4M GL LT PROPELLER FAILED A APLGAK NONE O OTHER ININSP/MAINT 1 NE05817BE169754476 UB52 FW309 DURING A SCHEDULED OIL FILTER INSPECTION, FINE METAL DEBRIS WAS FOUND IN THE LEFT ENGINE OIL FILTER. DUE TO PRIOR OPERATING EXPERIENCE, AN INTERNAL BORESCOPE OF THE PROPELLER WAS PERFORMED. THE BORESCOPE INSPECTION REVEALED DISTRESS TO THE FEATHERING SPRING RETAINING CUP WHICH WAS INSTALLED IAW HARTZELL SB 173 ON JUNE 23, 1992 AT LAST OVERHAUL. THE PROPELLER WAS REMOVED FOR INVESTIGATION AND OVERHAUL. SUBSEQUENT GROUND RUN OF THE AIRCRAFT FOUND NO FURTHER METAL DEBRIS GENERATION. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 6 CP56GL 19950421003271995042100327EU 1995 4 21 95ZZZX1861 119950317A5347 SEAT TRACK SAAB SF340 340B 7860101EU FS 630-668 CORRODED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05352BE 340B239 DURING C-CHECK INSPECTION FOUND SEVERAL CORROSION HOLES IN LAVATORY SEAT TRACK BETWEEN STA 630 - STA 668. THE FORWARD HOLE WAS 2 INCHES LONG BY 1 INCH HIGH. THE MIDDLE HOLE WAS 4 INCHES LONG BY 2 INCHES HIGH AND THE AFT HOLE WAS 2 INCHES LONG BY 1 INCH HIGH. THE AREA WAS CLEANED, TREATED AND REPAIRED IAW THE SAAB SRM 53-70-60, PAGE 206, DATED MARCH 31, 1994. 2L72 4T RTA52EU 19950421003281995042100328CE 1995 4 21 95ZZZX1862 119950317A2120 AIR DISTR BEECH 1900 1900C 1154161CE COCKPIT SMOKING A PLGAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NE05818BE UB61 BOS - WHILE ON THE GROUND WITH EXTERNAL POWER CONNECTED AND SELECTED ON, JUST PRIOR TO FIRST ENGINE START, THE CREW EXPERIENCED SMOKE IN THE COCKPIT. THE AIRCRAFT WAS SHUT DOWN, DEPLANED, AND MAINTENANCE NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE INSPECTED THE COCKPIT WITH NO FAULTS FOUND. MAINTENANCE GROUND RAN AIRCRAFT AND CHECKED ALL SYSTEMS WITH NO DEFECTS OR SMOKE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 19950421003291995042100329EU 1995 4 21 95ZZZX1863 119950401A2612899253 FIRE LOOP SAAB SF340 340B 7860101EU LT ENGINE SHORTED A NVEAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 SO03284AE 340B284 BNA - FLT 4590 - LEFT ENGINE FIRE DETECT LIGHT CAME ON. SHUT DOWN ENGINE. LIGHT WAS STILL ON. SHOT NR 1 FIRE BOTTLE. LIGHT WENT OUT. FIRE LOOP UNDER THE POWER TURBINE SHORTED INTERNALLY. REPLACED THE FIRE LOOP. 2L72 4T RTA52EU 19950421003301995042100330WP 1995 4 21 BUFA9508 119950330A3230 RETRACT MECH DOUG DC8 DC861 3021952WP LANDING GEAR LACK OF LUBE A BUFAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 CE05161DB 45980 MBJ/MIA - FLT AJM9037 - LANDING GEAR HANDLE DOWN, ALL UNSAFE LIGHTS ON F/E PANEL ON, HYDRAULIC PRESSURE AND QUANTITY NORMAL, NO GREEN LIGHTS, HAD TO GO AROUND, GEAR HANDLE UP, RED LIGHTS OUT, GEAR HANDLE DOWN, RED, THEN 3 GREEN, HYDRAULIC NORMAL. INSPECTED LANDING GEARS, ELECTRICAL WIRING AND CLEANED CONNECTORS. LUBRICATED GEARS AND PERFORMED GEAR SWING PER MM 32-10-0, PAGES 1-2, FIGURE 15. OPS CHECK NORMAL. (X) 2L74 4F 4A25 19950421003311995042100331WP 1995 4 21 HAL95030 119950326A3246 WHEEL DOUG DC9 DC951 3022051WP RT MLG POPPING A HALAK NONE O OTHER TXTAXI/GRND HDL 1 WP13699HA 47763 HNL - FLT 529 - ITEM FROM M-71 LOG PAGE NR 141600-1. A PASSENGER SITTING ON THE RIGHT SIDE AT THE EMERGENCY EXIT ROW REPORTED 'THUMPING' OR 'POPPING' SOUNDS WHILE TAXIING, PARTICULARLY IN TURNS. PROBABLY FROM THE MAIN GEAR. RETURNED TO RAMP. REPLACED THE NR 3 BRAKE ASSEMBLY, SN OFF NOV. 92-0340 AND SN ON SEP. 78-672. REPLACED THE NR 3 TIRE/WHEEL ASSY., SN OFF SEP. 92-1968 AND SN ON OCT. 94-2026. THE OPERATIONAL CHECK WAS OKAY. (X) 2L72 4F A6WE 19950421003321995042100332WP 1995 4 21 HAL95031 119950328A33506011775 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 1146 47764 HNL - FLT 561 - ITEM FROM M-71 LOG PAGE NR 141739-3. THE LEFT OVER-WING EMERGENCY LIGHT (OUTSIDE) IS INOPERATIVE. REMOVED AND REPLACED THE LEFT OVER-WING EMERGENCY BATTERY PACK. THE OPERATIONAL CHECK WAS OKAY. (X) 2L72 4F A6WE 19950421003331995042100333NE 1995 4 21 IXXA199524 219950331A72613053183050U1 OIL CAP DOUG DC8 DC871 302199AWP GE CFM56 CFM562C1 13802NE NR 1 ENGINE UNLOCKED A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23824BX 45946 693160 OKC - ON DEPARTURE, FLIGHT CREW NOTICED THE NR 1 ENGINE OIL QUANTITY WAS DECREASING. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO OKC FOR MAINTENANCE. SOME OIL QUANTITY WAS RETAINED, AND MINIMUM WINDMILLING OIL PRESSURE WAS MAINTAINED. ON THE GROUND IN OKC, DETERMINED THE NR 1 ENGINE OIL TANK CAP WAS NOT LOCKED ALLOWING LEAKAGE AROUND THE CAP. THE ENGINE WAS SERVICED, THE OIL CAP SECURED, AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F4 F 4A25 E2GL 19950421003341995042100334WP 1995 4 21 IXXA199543 119950404A3260 DOWNLOCK SWITCH DOUG DC8 DC871F 302199DWP NLG OUT OF ADJUST A IXXAO OTHER N FALSE WARNING APAPPROACH 1 GL23827BX 10228 45971 TOL - ON APPROACH, NO NOSE LANDING GEAR DOWN INDICATION WAS OBTAINED WHEN THE LANDING GEAR WAS EXTENDED, AND THE LANDING GEAR UNSAFE LIGHT WAS ILLUMINATED. THE LANDING GEAR WAS CYCLED FOUR TIMES, AND A SAFE INDICATION WAS OBTAINED AND VISUALLY VERIFIED. ON THE GROUND IN TOL, DETERMINED THAT NLG DOWNLOCK SWITCH REQUIRED ADJUSTMENT. THE SWITCH WAS ADJUSTED, THE NLG OPS CHECKED, AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F RT4A25 19950421003351995042100335 1995 4 21 IXXA199544 419950404A3421258733511 VERTICAL GYRO DOUG DC8 DC863F 302198FWP NR 2 FAILED A IXXAO OTHER O OTHER CLCLIMB 1 GL23784AL 46135 BQN - ON DEPARTURE, THE FIRST OFFICER'S ADI TUMBLED. THE AIRCRAFT RETURNED TO BQN FOR MAINTENANCE. MAINTENANCE REPLACED THE NR 2 VG, AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L74 4F 4A25 19950421003361995042100336WP 1995 4 21 IXXA9525 119950104A5313264661012000 LONGERON DOUG DC8 DC871F 302199DWP FS 980/1060 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK AND CORROSION PREVENTION AND CORROSION CONTROL INSPECTION, LEVEL 2 CORROSION WAS FOUND BETWEEN FS 980 AND FS 1060, LONGERON 31 LEFT. THE LONGERON WAS REMOVED AND REPLACED IAW AIRCRAFT SRM. CORROSION DAMAGE WAS CONFINED TO THE LONGERON. (X) 2L74 4F RT4A25 19950421003371995042100337WP 1995 4 21 IXXA9526 119950109A5312564400 BULKHEAD WEB DOUG DC8 DC871F 302199DWP BS 1766 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK, A 1 INCH CRACK WAS LOCATED IN THE AFT PRESSURE BULKHEAD, FS 1766, AT LONGERON 11 LEFT. REPAIR WAS ACCOMPLISHED IAW AIRCRAFT SRM AND SB 53-73. (X) 2L74 4F RT4A25 19950421003381995042100338WP 1995 4 21 IXXA9527 119950104A57305611310 SKIN DOUG DC8 DC871F 302199DWP WS 585 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT LEADING EDGE. THE CRACK MEASURED 6 INCHES AND WAS LOCATED AT XFS 585. THE REPAIR WAS ACCOMPLISHED IAW AIRCRAFT SRM. SRM REFERENCE 57-2-1. (X) 2L74 4F RT4A25 19950421003391995042100339WP 1995 4 21 IXXA9528 119950109A53305613861 SKIN DOUG DC8 DC871F 302199DWP NLG WW CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS LOCATED AT THE NOSE WHEELWELL DOOR CUT-OUT. THE EXTERNAL PLATING WAS CRACKED AT THE RIGHT AFT CORNER. REPAIR OF THE CRACK WAS ACCOMPLISHED IAW AIRCRAFT SRM 53-2-1 WHICH INSTALLED AN EXTERNAL REPAIR DOUBLER. (X) 2L74 4F RT4A25 19950421003401995042100340WP 1995 4 21 IXXA9529 119950109A53305751702 SKIN DOUG DC8 DC871F 302199DWP BS 280 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A 1 INCH CRACK WAS FOUND AT FS 280, AND LONGERON 36. REPAIR OF THE CRACK WAS ACCOMPLISHED IAW AIRCRAFT SRM. (X) 2L74 4F RT4A25 19950421003411995042100341WP 1995 4 21 IXXA9530 119950102A53203750277 FITTING DOUG DC8 DC871F 302199DWP FS 260 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION. LONGERON AND FITTINGS AT SEVERAL LOCATIONS WERE FOUND CRACKED. END FITTINGS AT FS 260, AND LONGERONS 34 AND 35 LEFT AS WELL AS LONGERON 36. ALL FITTINGS WERE REPLACED WITH NEW IAW AIRCRAFT SRM. (X) 2L74 4F RT4A25 19950421003421995042100342WP 1995 4 21 IXXA9531 119950103A52105615403219 SKIN DOUG DC8 DC871F 302199DWP PASSENGER DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE PLATING OF THE LT FORWARD ENTRY DOOR. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER. REPAIR TO THE EXTERNAL PLATING WAS ACCOMPLISHED IAW AIRCRAFT SRM. (X) 2L74 4F RT4A25 19950421003431995042100343WP 1995 4 21 IXXA9532 119950116A52407075T6 ANGLE DOUG DC8 DC871F 302199DWP SERVICE DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A CRACKED ANGLE ON THE RT AFT SERVICE DOOR WAS NOTED. THE ANGLE WAS REMOVED AND LOCALLY MANUFACTURED IAW DRAWING N821BX-04 WHICH WAS FAA DER APPROVED. THE NEW ANGLE WAS INSTALLED IAW AIRCRAFT SRM AND MM. (X) 2L74 4F RT4A25 19950421003441995042100344WP 1995 4 21 IXXA9533 119950103A53202646610 FITTING DOUG DC8 DC871F 302199DWP BS 857 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX 45811 DURING ROUTINE C-CHECK INSPECTION, A 1.25 INCH CRACK WAS FOUND ON THE STA 857 FITTING OF LONGERON 24. REPAIR ON THE LONGERON FITTING WAS ACCOMPLISHED IAW THE AIRCRAFT SRM. SRM REFERENCE 53-2-2. (X) 2L74 4F RT4A25 19950421003451995042100345WP 1995 4 21 IXXA9534 119950106A52402610010 FITTING DOUG DC8 DC871F 302199DWP SERVICE DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, A CRACKED FITTING ON THE LT AFT SERVICE DOOR WAS FOUND. THE FORWARD UPPER FITTING EXHIBITED A .250 INCH CRACK. THE FITTING WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM. (X) 2L74 4F RT4A25 19950421003461995042100346WP 1995 4 21 IXXA9535 119950118A57205615058501 FITTING DOUG DC8 DC871F 302199DWP LT WING SPAR CAPCRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING REPLACEMENT OF LT MLG TRUNNION FITTING, INSPECTION FOUND LT SPAR CAP FITTING CRACKED. THE SPAR CAP FITTING WAS REPLACED IAW DOUGLAS INSTALLATION GUIDE, THE AIRCRAFT SRM, AND MM. (X) 2L74 4F RT4A25 19950421003471995042100347WP 1995 4 21 IXXA9536 119950103A53135750198502 LONGERON DOUG DC8 DC871F 302199DWP RT FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION. LONGERON 24 WAS FOUND WITH 2 CRACKS. THE RT LONGERON 24 HAD BOTH A 7 INCH AND 1 INCH CRACK AT SEPARATE LOCATIONS. THE LONGERON WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM, DOUGLAS INSTALLATION GUIDE, AND THE MM. (X) 2L74 4F RT4A25 19950421003481995042100348WP 1995 4 21 IXXA9537 119950103A57435611425 TRUNNION DOUG DC8 DC871F 302199DWP LT MLG CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23821BX7241223811 45811 DURING ROUTINE C-CHECK INSPECTION, THE LT MLG TRUNNION FITTING WAS FOUND CRACKED. INSPECTION WAS ACCOMPLISHED IAW SB 57-94. THE CRACK WAS LOCATED, 8 INCHES, IN THE FORWARD LANDING GEAR ATTACH LUG. THE FITTING WAS REMOVED AND REPLACED IAW DOUGLAS INSTALLATION GUIDE, SRM, AND MM. THE BRAKE PLUMBING WAS CONFIRMED TO BE PROPERLY CONNECTED IAW DOUGLAS AOL 8-1091, JOB CARD 74201. (X) 2L74 4F RT4A25 19950421003491995042100349WP 1995 4 21 IXXA9538 119950212A54005803952509 DRAG ANGLE DOUG DC8 DC871 302199AWP NR 2 PYLON CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX2727514193 45946 DURING ROUTINE C-CHECK INSPECTION, A 2.200 INCH CRACK WAS FOUND IN THE NR 2 PYLON, INBOARD DRAG ANGLE. AFTER EVALUATION BY DOUGLAS AND FAA DER APPROVAL, THE AIRCRAFT WAS RETURNED TO SERVICE WITH FOLLOW-UP INSPECTIONS REQUIRED AT C-CHECK AND REPLACEMENT REQUIRED AT THE NEXT D-CHECK. (X) 2L74 4F 4A25 19950421003501995042100350WP 1995 4 21 IXXA9539 119950202A575357511841 HINGE FITTING DOUG DC8 DC871 302199AWP LT TE FLAP CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX6974114193 45946 DURING ROUTINE C-CHECK, THE LEFT OUTBOARD FLAP, INBOARD FLAP BASE HINGE FITTING WAS CRACKED IN HALF ON THE OUTBOARD HALF. THE FITTING WAS REPLACED IAW DOUGLAS SB 27-249 AND THE AIRCRAFT MM. (X) 2L74 4F 4A25 19950421003511995042100351WP 1995 4 21 IXXA9540 119950214A53115705291 BELT FRAME DOUG DC8 DC871 302199AWP FS 1020 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX6974114193 45946 DURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND AT STA 1020 BELT FRAME. TWO AREAS, ONE AT LONGERON 34.5 RT AND ONE AT 34.5 LT, WERE 1 INCH BY 1 INCH AREAS. CORROSION REMOVAL WENT BEYOND SRM LIMITS. REPAIR OF THE BELT FRAME IAW DRAWING HSE27-53-157, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-143. (X) 2L74 4F 4A25 19950421003521995042100352WP 1995 4 21 IXXA9541 119950214A53115705291 BELT FRAME DOUG DC8 DC871 302199AWP FS 1120 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX6974114193 45946 DURING ROUTINE C-CHECK INSPECTION, STA 1120 BELT FRAME WAS FOUND CORRODED. DAMAGE WAS LIMITED TO ONE AREA JUST INBOARD OF LONGERON 35 RT AND APPROXIMATELY 1 INCH IN DIAMETER. THE DAMAGE WAS REPAIRED BY CUT-OUT, INSTALLING A FILLER, AND INSTALLING AN EXTERNAL DOUBLER TO THE CAP. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-157, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-144. (X) 2L74 4F 4A25 19950421003531995042100353WP 1995 4 21 IXXA9542 119950217A5730561134018 SKIN DOUG DC8 DC871 302199AWP WS 74.8 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX 45946 DURING ROUTINE C-CHECK INSPECTION, EXTERNAL PLATING OF THE RIGHT WING EXHIBITED FOUR CRACKS. THE DAMAGE WAS AT WS XRS 74.8 BETWEEN STR 9 THROUGH STR 12. REPAIR OF THE AREA WAS ACCOMPLISHED BY CUTTING OUT THE CRACKS, INSTALLING FILLERS FOR THE REMOVED MATERIAL, AND INSTALLING AN EXTERNAL REPAIR DOUBLER. REPAIR WAS ACCOMPLISHED IAW DRAWING N824BX-02, WHICH IAW DOUGLAS ENGINEERING, AND FAA DER APPROVED, AND E.O. 57-DC8-145. (X) 2L74 4F 4A25 19950421003541995042100354NM 1995 4 21 MZZA9512 119950317A2751106081917 SWITCH 651781820 BOEING727 727212 138407GNM NR 3 LE FLAP FAILED A MZZAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 WP13309AS 21947 CJU - FLT 922 - AFTER TAKEOFF, L/E FLAP AMBER LIGHT REMAINED ON IN RETRACT POSITION. AIRCRAFT RETURNED TO CJU. MAINTENANCE FOUND NR 3 L/E FLAP SWITCH FAULTY IN 'UP' POSITION. REPLACED SWITCH AND SYSTEM GROUND OPERATION CHECKED GOOD. (X) 2L73 4F A3WE 19950421003551995042100355NM 1995 4 21 MZZA9513 119950318A3230106122615 SENSOR BOEING727 727227 1384078NM LT MLG FAILED A MZZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP1389427 3062 21365 GUM - FLT 990 - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO GUM. MAINTENANCE FOUND SENSOR M-682 GROUND SENSOR SHORTED. REPLACED SENSOR PER MM 32-09-221. SYSTEM CHECKED GOOD AND GEAR RETRACTION CHECKED NORMAL. (X) 2L73 4F A3WE 19950421003561995042100356NM 1995 4 21 MZZA9515 119950314A5730 SKIN BOEING727 727224 1384076NM CENTER WING CORRODED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1369741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION FOUND ON CENTER WING LOWER SKIN AT STIFFENER S-5, LBL 27. THE CORRODED SKIN WAS CLEANED UP AND REPAIRED PER EC/RA 5710-01663. HANGAR NON-ROUTINE REPAIR, ITEM CARD NR 0729690 (SEQ NR 01038). (X) 2L73 4F A3WE 19950421003571995042100357NM 1995 4 21 MZZA9516 119950314A3231 ROLLER BOEING727 727224 1384076NM RT MLG DOOR DAMAGED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1369741 22250 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FROZEN WATER FOUND ON RT MLG DOOR GROUND RELEASE CRANK ROLLER. THE DAMAGED ROLLER WAS REMOVED AND REPLACED PER B727 MM 32-34-21 AND OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON-ROUTINE REPAIR, ITEM CARD NR 0729691 (SEQ NR 01027). (X) 2L73 4F A3WE 19950421003581995042100358NM 1995 4 21 MZZA9517 119950331A3610 GASKET BOEING727 727224 1384076NM NR 1 ENGINE FAILED A MZZAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 WP1369741 22250 GUM - FLT 917 - APPROXIMATELY 25 MINUTES OUT OF SAIPAN, FLT 917, ACFT 741, CREW REPORTED STRUT OVERHEAT LIGHT CAME ON WHEN CLIMBING THROUGH APPROXIMATELY 10,000 FEET. THROTTLE WAS BROUGHT TO IDLE AND LIGHT WENT OUT. ABNORMAL CHECKLIST WAS RUN (ENGINE BLEEDS OFF AND POWER WAS RESTORED TO NR 1 ENGINE). ACFT WAS AIR DIVERTED TO GUAM. MAINTENANCE, IN TROUBLESHOOTING, FOUND HEAT EXCHANGE MANIFOLD WITH A BAD GASKET. INSTALLED NEW GASKETS, RAN ENGINE AT HIGH POWER, NO LEAKS FOUND. NR 1 STRUT OVERHEAT LIGHT DID NOT ILLUMINATE. ACFT CHECK FOR SERVICE. (X) 2L73 4F A3WE 19950421003591995042100359CE 1995 4 21 PLGA321951 119950308A2750 RETRACT MECH BEECH 1900 1900C 1154161CE TE FLAPS LACK OF LUBE A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05815BE UB54 THIS SDR (DATED 3-21-95) IS TO CLOSE OUT AN SDR DATED 3-8-95 WHERE THE FLAPS WERE MEL'D AFTER FAILING IN THE TAKEOFF POSITION. MAINTENANCE CLEANED AND LUBED THE FLAP ASYMMETRY SWITCHES AND PERFORMED SATISFACOTRY OPERATIONAL CHECK OF THE SYSTEM. (X) 2L72 4T RTA24CE 19950421003601995042100360GL 1995 4 21 PLGA322951 319950314A6114A3087 WASHER BEECH 1900 1900C 1154161CE HARTZLHCB4M HCB4M GL PROPELLER DOME FAILED A APLGAK NONE O OTHER ININSP/MAINT 1 NE05817BE4476 UB52 FW309 THIS SDR (DATED 3-22-95) IS TO SUPPLEMENT AN SDR DATED 3-14-95. PRELIMINARY FINDINGS FROM THE OVERHAUL FACILITY VERIFIED A FAILURE OF WASHER, PN A3087. THE OVERHAUL FACILITY CONTACTED THE MANUFACTURER WHO CONFIRMED A POTENTIAL PROBLEM DUE TO A 'SOFT' BATCH OF WASHERS. (X) 2L72 4T RTA24CE 6 CP56GL 19950421003611995042100361EU 1995 4 21 PLGA323952 119950323A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU AVIONICS RACK MALFUNCTIONED A PLGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NE05365BE A2912 340B299 BOS/IAD - EN ROUTE, AVIONICS SMOKE DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO AVP LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. ALL COMPONENTS IN THE AVIONICS RACK WERE INSPECTED WITH NO FAULTS OR EVIDENCE OF SMOKE FOUND. THE AIRCRAFT WAS THEN GROUND RUN AND ALL SYSTEMS WERE OPERATIONALLY CHECKED WITH NO FAULTS FOUND OR SMOKE DETECTED. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR AS A PRECAUTION AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T RTA52EU 19950421003621995042100362EU 1995 4 21 RAIA950343 119950328A2820HTE8815 CROSSFEED VALVE BAG JETSTMJETSTM3201 1500217EU FUEL SYSTEM MALFUNCTIONED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03432AM8791 883 STL - FLT 7406 - WITH FUEL CROSS-FEED VALVE IN THE OPEN POSITION AND LEFT BOOST PUMP ON, THERE IS A 150 POUND FUEL IMBALANCE. MAINTENANCE REPLACED FUEL CROSS-FEED VALVE ACTUATOR. SYSTEM TEST GOOD. (X) 2L72 4T RTA56EU 19950421003631995042100363EU 1995 4 21 RAIA950344 119950326A33508GS00545328 EEL BAG JETSTMJETSTM3201 1500217EU RT WING FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03433AM8520 885 STL - EMERGENCY LIGHT OVER RIGHT WING EXIT INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB. (X) 2L72 4T RTA56EU 19950421003641995042100364EU 1995 4 21 UF6A950307 119950328A6120S56000756 CONNECTOR BAG ATP ATP EU NR 2 ENGINE DIRTY A UF6AD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03858AW6267 2035 PIA - FLT 5090 - THE NR 2 ENGINE AUTOFEATHER UNIT WOULD NOT TEST. MAINTENANCE CLEANED CANNON PLUG 'A'. (X) 2L72 4T RTA27NM 19950421003651995042100365EU 1995 4 21 UF6A950308 119950329A3350362624 EEL STRIP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03852AW8521 2021 RON - SBN FIRST STRIP OF EMERGENCY FLOOR LIGHTING FAILED. MAINTENANCE REPLACED FAILED LIGHT STRIP. (X) 2L72 4T RTA27NM 19950421003661995042100366NE 1995 4 21 USAA950304 219950330A7314 FUEL PUMP DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE RIGHT FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA19979VJ 47372 PIT - FLT 0233 - LOW POWER ON THE RIGHT ENGINE ON CLIMB-OUT. FLIGHT RETURNED TO PIT. SINGLE ENGINE TIME WAS TWELVE MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL PUMP. THE RIGHT ENGINE FUEL CONTROL UNIT WAS ALSO REPLACED AS A PRECAUTION. OPERATIONS CHECKED GOOD. REFERENCE CONTROL 95ZZZX1856. (X) 2L72 4F4 F A6WE E2EA 19950421003671995042100367NM 1995 4 21 9505766305 119950414A5315 FLOORBEAM BOEING747 747451 1384940NM FS 980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM AT FS 980, RBL 33 TO 75. REMOVED CORROSION AND INSTALLED REPAIR STRAP. 2L74 4F RTA20WE 19950421003681995042100368NM 1995 4 21 9505776305 119950414A5347 SEAT TRACK BOEING747 747451 1384940NM FS 800-815 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 800 TO 815, LBL 98. REPLACED SEAT TRACK. 2L74 4F RTA20WE 19950421003691995042100369NM 1995 4 21 9505786305 119950414A5320 SUPPORT BOEING747 747451 1384940NM FS 2276 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 2276, LBL 20 TO 30. REPLACED FLOOR SUPPORT. 2L74 4F RTA20WE 19950421003701995042100370NM 1995 4 21 9505796305 119950415A5320 SUPPORT BOEING747 747451 1384940NM FS 820-920 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 820 TO 920, LBL 38. REMOVED CORROSION AND INSTALLED REPAIR PER EA 63-97882. 2L74 4F RTA20WE 19950421003711995042100371NM 1995 4 21 9505806305 119950414A5347 SEAT TRACK BOEING747 747451 1384940NM FS 1640-1670 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1640 TO 1670, LBL 75. REPLACED SEAT TRACK. 2L74 4F RTA20WE 19950421003721995042100372NM 1995 4 21 9505816305 119950414A5320 CHANNEL BOEING747 747451 1384940NM FS 995 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE HAT CHANNEL AT FS 995, LBL 15 IN THE UPPER DECK GALLEY AREA. REPLACED HAT CHANNEL. 2L74 4F RTA20WE 19950421003731995042100373NM 1995 4 21 9505826305 119950415A5347 SEAT TRACK BOEING747 747451 1384940NM FS 480-885 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 480 TO 885, RBL 75. REPLACED SEAT TRACK. 2L74 4F RTA20WE 19950421003741995042100374NM 1995 4 21 9505836305 119950416A5730 DOORS BOEING747 747451 1384940NM LT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEALING FLANGES OF THE LEFT LOWER WING FUEL ACCESS DOORS 545BB, 553JB, 553HB, 553DB, 553CB, AND 556DB. REPLACED ACCESS DOORS. 2L74 4F RTA20WE 19950421003751995042100375NM 1995 4 21 9505846305 119950415A5720 SUPPORT BOEING747 747451 1384940NM WS 547 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING INBOARD TRAILING EDGE LATERAL SUPPORT AT PANEL 572BB TO WS 547. STOP DRILLED AND INSTALLED DOUBLER. 2L74 4F RTA20WE 19950421003761995042100376NM 1995 4 21 9505852771 119950413A52206521082 FRAME BOEING727 7272M7 138407SNM EMERGENCY EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01742RW 21952 DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT AFT EMERGENCY EXIT OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEMENT PER MAINTENANCE MANUAL 52-21-00. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS. 2L73 4F A3WE 19950421003771995042100377NM 1995 4 21 9505862771 119950413A52206521082 FRAME BOEING727 7272M7 138407SNM EMERGENCY EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01742RW 21952 DURING PERIODIC CHECK, MAINTENANCE FOUND RIGHT FORWARD EMERGENCY EXIT OUTSIDE HANDLE OPENING FRAME CRACKED. DEFERRED CASTING REPLACEDMENT PER MAINTENANCE MANUAL 52-21-00. NWA IS REPLACING MAGNESIUM CASTINGS WITH AN ALUMINUM PART DUE TO MULTIPLE FINDINGS. 2L73 4F A3WE 19950421003781995042100378NE 1995 4 21 9505871153 219950416A7230 NR 3 BEARING DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 3 ENGINE FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01153US 46762 686171 DURING CLIMB AT ABOUT 7000 FEET, SMOKE AND FUMES APPEARED IN THE CABIN AND THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS MADE. NO FUEL WAS DUMPED. THE NR 3 ENGINE NR 3 BEARING COMPARTMENT SHOWED EVIDENCE OF DISTRESS AND BLACK OIL WAS FOUND. THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19950421003791995042100379WP 1995 4 21 9505889872 119950410A213094840213 PRESSURE AMP DOUG DC9 DC951 3022051WP E/E COMPARTMENT MALFUNCTIONED A NWAAB EMER. DESCENT O OTHER CRCRUISE 1 GL01781NC5247317946 48121 LOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET EN ROUTE MEM TO SAT. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FEET AND CABIN PRESSURE WAS REGAINED. FLIGHT CONTINUED AND LANDED SAFELY WITHOUT INCIDENT. REPLACED CABIN PRESSURE AMPLIFIER, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421003801995042100380 1995 4 21 DHL95741003 419950414A3421258733511 VERTICAL GYRO BOEING727 7272Q9 138448MNM NR 2 INOPERATIVE A TDHLAA UNSCHED LANDING IG FLT. ATTITUDE INST. MULTIPLE FAILURE TOTAKEOFF 1 SO01741DH 21931 ON TAKE OFF, F/O ADI FAILED INTERMITTANTLY AT BANK ANGLES GREATER THAN 4 DEGREES. DIVERTED TO CVG, LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 VERTICAL GYRO PER DHL 727 MM 34-22-21, ALL INICATIONS NORMAL. 2L73 4F RTA3WE 19950421003811995042100381WP 1995 4 21 DHL95805001 119950412A324426014111 TIRE DOUG DC8 DC873F 302199FWP MLG FAILED A TDHLAO OTHER O OTHER LDLANDING 1 SO01805DH 46125 ON LANDING TIRES 1 AND 2 BLEW-OUT DURING ROLLOUT. TIRES 5 AND 6 BADLY WORN, WHEEL ASSEMBLIES 1, 2, 5, AND 6 CHANGED PER DC-8 MM 32-40-1. REPLACED 1 AND 2 BRAKES PER MM 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO FURTHER DEFECTS NOTED. 2L74 4F RT4A25 19950421003821995042100382EU 1995 4 21 WWMA9500034 119950403A2150 OIL SYST BAG JETSTMJETSTM3201 1500217EU ACM OVERSERVICED I WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15958AE 958 FLT 3306 - SBP-LAX - PILOT REPORTED, THAT WHILE IN FLIGHT A BURNT OIL SMELL WAS DETECTED COMING FROM THE LEFT BLEED AIRFLOW. MAINTENANCE PERSONNEL INSPECTED THE SYSTEM AND DETERMINED THAT THE LEFT ACM HAD BEEN OVERSERVICED. THE UNIT WAS DESERVICED, OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA56EU 19950421003831995042100383EU 1995 4 21 WWMA9500035 119950408A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO COMPT MALFUNCTIONED I WWMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 WP15256AE 340B256 FLT 5033 - DFW-SPS - PILOT REPORTED, THAT THE CARGO SMOKE WARNING LIGHT CAME ON AND FIRED THE NR 1 CARGO EXTINGUISHER. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR FAULTY INDICATIONS. MAINTENANCE CLEANED THE SMOKE DETECTOR AND REMOVED AND REPLACED THE CARGO FIRE EXTINGUISHER NR 1 BOTTLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950421003841995042100384 1995 4 21 WWMA9500036 419950413A23206228587502 ACARS SCREEN SAAB SF340 340B 7860101EU CENTER PEDESTAL DEFECTIVE I WWMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP15306AE 340B306 FLT 3434 - PSP-LAX - PILOT REPORTED, THAT AFTER LANDING AT LAX AND WHILE DOING A POSTFLIGHT INSPECTION OF THE AIRCRAFT, HE OBSERVED SMOKE ACCOMPANIED BY A BURNT ELECTRICAL ODOR COMING FROM THE CENTER CONSOLE NEARS THE ACARS UNIT. MAINTENANCE PERSONNEL FOUND THAT THE ACARS SCREEN CANNON PLUG WAS 'LIVE' AND DETECTED A BURNT SMELL ASSOCIATED WITH THE ACARS UNIT. THE ACARS SCREEN WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA52EU 19950421003851995042100385EU 1995 4 21 WWMA9500037 119950416A243523079009 STARTER GEN BAG JETSTMJETSTM3201 1500217EU LT ENG DEFECTIVE I WWMAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 WP15959AE3986 959 FLT 3233 - LAX-SBP - PILOT REPORTED, THAT DURING FLIGHT A MODERATE VIBRATION WAS ENCOUNTERED IN THE LEFT ENGINE, THE GENERATOR THEN FAILED. THE LEFT ENGINE WAS SHUTDOWN AS A PRECAUTION. MAINTENANCE REPLACED THE LEFT HAND STARTER GENERATOR. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950421003861995042100386EU 1995 4 21 95ZZZW487 119950326A2910HTE9531101 VALVE ASSY BAG BAE146BAE146100A 1500260EU NR 3 ENG PUMP MALFUNCTION A A6WAK NONE O OTHER TXTAXI/GRND HDL 1 GL31463AP E1063 NR 3 ENGINE DRIVEN HYDRAULIC PUMP CAN NOT BE SHUTOFF. REPLACED THE NR 3 ENGINE DRIVE PUMP SHUTOFF VALVE. (W) 2H74 4F RTA49EU 19950421003871995042100387EU 1995 4 21 95ZZZW488 119950327A5320 FIREWALL BAG BAE146BAE146300A 1500267EU APU BAY CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31616AW E3145 CRACKING HAS BEEN NOTED AT THE FORWARD FACE OF THE APU BAY FORWARD FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W) 2H74 4F RTA49EU 19950421003881995042100388EU 1995 4 21 95ZZZW489 119950327A5320 FIREWALL BAG BAE146BAE146300A 1500267EU APU BAY CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 CRACKING HAS BEEN NOTED AT THE FORWARD FACE OF THE APU BAY FORWARD FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W) 2H74 4F RTA49EU 19950421003891995042100389EU 1995 4 21 95ZZZW490 119950327A5320 FIREWALL BAG BAE146BAE146300A 1500267EU APU BAY CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31614AW E3132 CRACKING HAS BEEN NOTED AT FWD FACE OF THE APU BAY FWD. FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W) 2H74 4F RTA49EU 19950421003901995042100390EU 1995 4 21 95ZZZW491 119950327A5320 FIREWALL BAG BAE146BAE146300A 1500267EU APU BAY CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 CRACKING HAS BEEN NOTED AT FORWARD FACE OF APU BAY FORWARD FIREWALL IN THE AREA OF THE EXHAUST PIPE. DEACTIVATED APU AND PLACED ON MEL. (W) 2H74 4F RTA49EU 19950421003911995042100391EU 1995 4 21 95ZZZW492 119950306A3230 MAIN GEAR BAG BAE146BAE146300A 1500267EU MLG ICED UP A A6WAO OTHER J WARNING INDICATION CLCLIMB 1 GL31611AW E3120 BOTH MAIN GEAR INDICATED INTRANSIT AFTER MAIN GEAR RETRACTION. SUBSEQUENT EXTENSION NORMAL. REMOVED ICE FROM LANDING GEAR AREA. SWUNG GEAR SEVERAL TIMES. OPS CHECKED OK. (W) 2H74 4F RTA49EU 19950421003921995042100392EU 1995 4 21 95ZZZW493 119950306A3230 MAIN GEAR BAG BAE146BAE146200A 1500266EU LT MLG ICED UP A A6WAO OTHER J WARNING INDICATION CLCLIMB 1 GL31607AW E2052 LEFT GEAR STAYED DOWN COULD FEEL THE YAW, SHOWED GEAR GEAR INTRANSIT. CLEANED ICE FROM GEAR, SWUNG GEAR SEVERAL TIMES. (W) 2H74 4F RTA49EU 19950421003931995042100393NE 1995 4 21 95ZZZW494 219950308A7200 ENG BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENG FAILED A A6WAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL31609AW E2070 AFTER TAKEOFF CLIMBING OUT OF ASE NR 1 ENGINE LOW OIL PRESS LT FLICKERED ON AND OFF COUPLE OF TIMES, CREW FOLLOWED ENG LOW OIL PRESS CHECKLIST, LATER THE LOW OIL PRESS LT CAME BACK ON, OIL QTY WAS BOUNCING OFF EMPTY, CREW SHUT ENGINE DOWN AND PROCEEDED TO DEN. (W) 2H74 4F4 FRTA49EU E6NE 19950421003941995042100394EU 1995 4 21 95ZZZW495 119950306A3520 PBE MASK BAG BAE146BAE146200A 1500266EU FWD CABIN MALFUNCTION A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW E2033 FORWARD CABIN PBE MASK RED IND SHOWING. REMOVED AND REPLACED PBE ASSY. (W) 2H74 4F RTA49EU 19950421003951995042100395NE 1995 4 21 95ZZZW496 219950312A7200 ENGINE BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NR 4 ENG FAILED A A6WAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 GL31616AW E3145 NR 4 ENGINE OIL QUANTITY AND PRESSURE WENT TO ZERO ON A 15 MILE FINAL INTO ORD. ENGINE SECURED. LOCKED DOWN ENGINE AND 3 ENG FERRIED TO ATW FOR ENG CHANGE. (W) 2H74 4F4 FRTA49EU E6NE 19950421003961995042100396EU 1995 4 21 95ZZZW497 119950109A5400 BOLT BAG BAE146BAE146200A 1500266EU NR 4 PYLON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 REMOVED NR 4 PYLON FORWARD YOKE TO ENGINE BOLTS FOR NDT (4 EACH) SSI 54-00-123 (1 EACH REJECTED DUE TO CORROSION). REINSTALLED 3 ORIGINAL BOLTS AFTER NDT AND 1 NEW BOLT AT RT LOWER POSITION, TORQUED AND SAFETIED. (W) 2H74 4F RTA49EU 19950421003981995042100398EU 1995 4 21 95ZZZW499 119950109A7120NAS631027 BOLT BAG BAE146BAE146200A 1500266EU ENG MOUNT SCORED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 ENGINE MOUNTS BOLTS (4 EACH) REQUIRE INSPECTION. PERFORMED VISUAL AND FLOURSCENT DYE PENETRANT INSPECTION ON 4 BOLTS. FOUND 1 WITH DEEP SCORE AND INDICATION AT HEAD TO SHANK RADIUS. SCRAPPED THAT BOLT. THREE BOLTS GOOD FOR RETURN TO SERVICE. ISSUED NEW BOLT FROM STOCK TO REPLACE THE ONE SCRAPPED. (W) 2H74 4F RTA49EU 19950421003991995042100399EU 1995 4 21 95ZZZW500 119950113A5520 BOLT BAG BAE146BAE146200A 1500266EU LT ELEV HINGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 LEFT HINGE BOLT NR 1 POSITION CORRODED. REMOVED AND REPLACED BOLT AS REQ'D IAW MM. (W) 2H74 4F RTA49EU 19950421004001995042100400EU 1995 4 21 95ZZZW501 119950113A5520 BOLT BAG BAE146BAE146200A 1500266EU RT ELEV HINGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 RT ELEVATOR HINGE BOLT NR 1 POSITION CORRODED. REMOVED AND REPLACED RT ELEVATOR HINGE BOLT AS REQ'D IAW MM. (W) 2H74 4F RTA49EU 19950421004011995042100401EU 1995 4 21 95ZZZW502 119950116A5753HC57960282000 STUB PIN BAG BAE146BAE146200A 1500266EU LT NR 2 FLAP CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 LEFT NR 2 FLAP TRACK STUB PIN INBOARD P/N HC57960282000 FAILED NDT CRACKED INDICATION SSI 57-55-125. REPLACED LEFT NR 2 FLAP TRACK INBOARD STUB PIN. (W) 2H74 4F RTA49EU 19950421004101995042100410EU 1995 4 21 95ZZZW511 119950103A3610 VALVE BAG BAE146BAE146300A 1500267EU NR 4 ENG AIR DEFECTIVE A A6WAK NONE O OTHER NRNOT REPORTED 1 GL31611AW E3120 NR 4 ENGINE AIR VALVE INDICATES OPEN WITH SWITCH SELECTED OFF. ORD MAINTENANCE CONFIRMED VALVE IN CLOSED POSITION. DEFERRED INDICATION PER MEL. DEFERRED AND PLACARDED, SE LG PG 21354/03. 2H74 4F RTA49EU 19950421004111995042100411EU 1995 4 21 95ZZZW512 119950118A3230 UPLOCK JACK BAG BAE146BAE146300A 1500267EU RT MLG REQ BLEED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31614AW E3132 AFTER TAKEOFF FROM ATW RT MAIN GEAR WOULD NOT COME UP. RECYCLE ONE TIME GEAR CAME UP. JACKED A/C AND BLEED RT UPLOCK JACK. OPS CK OK. GEAR SWING OK. 2H74 4F RTA49EU 19950421004121995042100412EU 1995 4 21 95ZZZW513 119950106A2140 BREAKER BAG BAE146BAE146300A 1500267EU Q-HEATER TRIPPED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31614AW E3132 AFTER TAKEOFF FROM ATW, Q-HEATER FAIL WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ATW. MAINTENANCE RESET HEATER ELEMENTS C/B, OPS TESTED OK SEVERAL TIMES. 2H74 4F RTA49EU 19950421004131995042100413NE 1995 4 21 95ZZZW514 219950105A7200 ENG BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NR 4 FAILED A A6WAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 GL31615AW E3141 ON CLIMB-OUT THROUGH 10,400 FEET THERE WAS A LOUD 'BANG' FOLLOWED BY ROLLBACK OF NR 4 ENG N1 AND N2. PRECAUTIONARY SHUTDOWN OF NR 4 ENGINE. REPLACED ENG NR 4 IAW 71-00-00 PG 401. 2H74 4F4 FRTA49EU E6NE 19950421004141995042100414EU 1995 4 21 95ZZZW515 119950304A5320 FRAME BAG BAE146BAE146100A 1500260EU AIRBRAKE AREA CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 CRACK IN LOWER RIGHT CORNER OF UPPER FRAME AIRBRAKE AREA. REPAIRED CRACK AS PER 146 SRM, 51-71-11 PAGE 4. 2H74 4F RTA49EU 19950421004151995042100415EU 1995 4 21 95ZZZW516 119950217A5510AC551B0086000 BOLT BAG BAE146BAE146100A 1500260EU RT STAB CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 NR 1 'A' FRAME UPPER BOLT RT STABILIZER SCRAPED DUE TO CORROSION AND RIDGE WEAR. REMOVED AND REPLACED BOLT AS REQUIRED IAW MM. 2H74 4F RTA49EU 19950421004161995042100416EU 1995 4 21 95ZZZW517 119950216A5510 BOLT BAG BAE146BAE146100A 1500260EU LT STAB CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 NR 2 'A' FRAME UPPER BOLT LEFT STABILIZER SCRAPED DUE TO CORROSION. REMOVED AND REPLACED BOLT AS REQ'D IAW MM. 2H74 4F RTA49EU 19950421004171995042100417EU 1995 4 21 95ZZZW518 119950216A5510 BOLT BAG BAE146BAE146100A 1500260EU LT STAB CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 NR 4 'A' FRAME BOLT UPPER, LEFT STABILIZER SCRAPPED DUE TO CORROSION. REMOVED AND REPLACED BOLT AS REQ'D IAW MM. 2H74 4F RTA49EU 19950421004181995042100418EU 1995 4 21 95ZZZW519 119950216A5330 SKIN BAG BAE146BAE146200A 1500266EU FRAME 10 DENTED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 REF LOG PAGE 21852/03, DENT ON LEFT SIDE OF FUSELAGE AT FRAME 10, ABOUT EVEN WITH CO-PILOT. FLOOR NEEDS PERMANENT REPAIR C/W BY 26997 TOTAL CYCLES. REF FAX AVRO NR DJR/RJ0221-95 AND DJR/RJ022295. COMPLIED WITH PERMANENT REPAIR IAW AVRO FAX REF NR DJR/RJ0224-95, SRM 53-10-12 FIG 202 AND 53-10-14 FIG 201. 2H74 4F RTA49EU 19950421004191995042100419EU 1995 4 21 95ZZZW520 119950215A5320 STIFFENER BAG BAE146BAE146100A 1500260EU FRAME 29 DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 COMPLIED WITH EO E95/005/653 ON FRAME 29 STIFFENERS AT STATION 25.94 LEFT AND RIGHT LOCATIONS. REPAIRED FRAME 29 LEFT AND RT STIFFENERS 25.94 IAW EO E95/005/653 ORIG ISSUE. 2H74 4F RTA49EU 19950421004201995042100420EU 1995 4 21 95ZZZW521 119950214A5751 BOLT BAG BAE146BAE146100A 1500260EU RT AIL HINGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 RIGHT AILERON INBOARD HINGE BOLT GIVES CRACK INDICATIONS VIA MAGNAFLUX UNDERHEAD RADIUS. INSTALLED A NEW BOLT IN THE RT AILERON INBOARD HINGE PER MM. 2H74 4F RTA49EU 19950421004211995042100421EU 1995 4 21 95ZZZW522 119950214A5751 BOLT BAG BAE146BAE146100A 1500260EU RT AIL CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 RT AILERON CENTER BOLT HAS CRACK INDICATIONS. REMOVED AND REPLACED RT AILERON CENTER HINGE BOLT PER MM. 2H74 4F RTA49EU 19950421004221995042100422EU 1995 4 21 95ZZZW523 119950311A5711 BOLT BAG BAE146BAE146300A 1500267EU RT WING AFT SPARBROKEN A A6WAK NONE K FLUID LOSS ININSP/MAINT 1 GL31616AW E3145 RIGHT WING REAR SPAR LEAKING FUEL, FOUND DURING ACCOMPLISHMENT OF EO E92/083/657. RT WING REAR SPAR ROOT JOING ATTACH FITTING AT RIB 2, BOLT 'C' BROKEN, AND BOLT 'A' FOUND LOOSE. REPLACED BOLTS IAW BAE REPAIR INSTRUCTIONS HC536H9043, AND RESEALED AND LEAK CHECKED. 2H74 4F RTA49EU 19950421004231995042100423CE 1995 4 21 95ZZZW524 119950117A3260 SWITCH BEECH 1900 1900C 1154161CE GEAR WELL DIRTY A MASAO OTHER N FALSE WARNING CLCLIMB 1 SW0191YV UC91 CREW SELECTED LANDING GEAR UP AND OBSERVED A GEAR HANDLE 'INTRANSIT LIGHT'. MAINTENANCE INSPECTED GEAR SWITCHES, CLEANED AND LUBED AS NEEDED, FUNCTION CHECKED GEAR. RETURNED TO SERVICE. 2L72 4T RTA24CE 19950421004241995042100424EU 1995 4 21 95ZZZW525 119950326A3350 EEL BATTERY PACK FOKKERF28 F28MK4000 4990810EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19486US 11237 CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK. OPERATIONS CHECKED GOOD. REFERENCE USAA950307. 2L72 4F RTA20EU 19950421004251995042100425EU 1995 4 21 USAA950256 119950224A5312 ANGLE FOKKERF28 F28MK4000 4990810EU FWD PRESS BLKHD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19479AU19953 11228 PIT - DURING SCHEDULED SIP INSPECTION, FOUND CRACK IN THE FORWARD PRESSURE BULKHEAD LOWER CONNECTION ANGLE AT FRAME 1550 BETWEEN STATION 72 AND 3. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 53-11-00. (W) 2L72 4F RTA20EU 19950421004261995042100426EU 1995 4 21 USAA950258 119950316A5230 HINGE FOKKERF28 F28MK4000 4990810EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19484US18772 11234 PIT - DURING SCHEDULED SIP INSPECTION, FOUND .1250 INCH CRACK IN MID CARGO DOOR HINGE FWD END. EDDY CURRENT INSPECTION REF SIP 52-30-09 PG 2. REMOVED AND REPLACED CARGO DOOR PER F28 MM 52-30-01. (W) 2L72 4F RTA20EU 19950421004271995042100427EU 1995 4 21 USAA950259 119950219A5230D28410401 HINGE FOKKERF28 F28MK4000 4990810EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU21538 11222 PIT - DURING SCHEDULED STRUCTURES VISIT (SIP) FOUND A .375 INCH CRACK IN AFT CARGO DOOR HINGE LUG (AFT END). REMOVED AND REPLACED HINGE LUGS WITH NEW MODIFIED HINGE P/N D28410-409 PER USAIR EO NR 5294X201. (W) 2L72 4F RTA20EU 19950421004281995042100428EU 1995 4 21 USAA950260 119950219A5230D28410401 HINGE FOKKERF28 F28MK4000 4990810EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU21538 11222 PIT - DURING SCHEDULED STRUCTURES VISIT (SIP) FOUND .1250 INCH CRACK IN MID CARGO DOOR HINGE LUG. EDDY CURRENT INSPECTION REF SIP 52-31-09. REMOVED AND REPLACED HINGE LUG WITH NEW MODIFIED HINGE P/N D28410-409 PER USAIR EA NR 5294X201. (W) 2L72 4F RTA20EU 19950421004291995042100429NM 1995 4 21 USAA950306 119950328A3350 EEL ASSY BOEING727 727247 138408FNM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19749US 21393 PIT - THE EMERGENCY LIGHTS AT ROW 15ABC WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD. (W) 2L73 4F A3WE 19950421004301995042100430EU 1995 4 21 USAA950307 119950326A3350 EEL ASSY FOKKERF28 F28MK4000 4990810EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19486US 11237 CLT - THE MID CABIN OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK. OPERATIONS CHECKED GOOD. REFERENCE 95ZZZW525. 2L72 4F RTA20EU 19950421004311995042100431NM 1995 4 21 USAA950308 119950227A5330 SKIN BOEING737 7373B7 1384580NM BS 860-887 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL EDDY CURRENT INSPECTION, FOUND 27 INCH CHAFED AREA BY .25 INCH WIDE BS 860 TO BS 887 S-2 LEFT TO S-2 RIGHT. REPAIRED PER SRM 53-00-01 AND TR 53-30-03. (W) 2L72 4F RTA16WE 19950421004321995042100432WP 1995 4 21 USAA950310 119950315A5330 SKIN DOUG DC9 DC931 3022065WP FWD BELLY CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION UNDER FWD BELLY AT MARKER BEACON ANTENNA. INSTALLED DOUBLER REPAIR PER USAIR EA 29959. (W) 2L72 4F A6WE 19950421004331995042100433WP 1995 4 21 USAA950312 119950306A5330 SKIN DOUG DC9 DC931 3022065WP BS 263/300 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION LONGERON NR 1 AND SKIN LAP JOINT STATION 263-275 NR ADF LOOP AND STATION 300-308 NR 2 ADF LOOP ANTENNA. CLEANED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29 AND USAIR EA 29614A. (W) 2L72 4F A6WE 19950421004341995042100434WP 1995 4 21 USAA950325 119950224A5311 FRAME DOUG DC9 DC981 3022081WP BS 1463 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND CRACK .75 INCH LONG AT STATION 1463 CANTED FRAME WEB. CUT OUT DAMAGED SECTION OF WEB AND MANUFACTURED NEW WEB PER USAIR EA 27544. (W) 2L72 4F A6WE 19950421004351995042100435WP 1995 4 21 USAA950326 119950224A5330 SKIN DOUG DC9 DC981 3022081WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK AT STATION 1437 LONGERON 3L IN SKIN. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PER SRM 53-04 FIG 38 FIG 38 VIEW L. (W) 2L72 4F A6WE 19950421004361995042100436WP 1995 4 21 USAA950335 119950315A5320 MEMBRANE DOUG DC9 DC981 3022081WP BS 1287/1309 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND A 1.75 INCH CRACK BETWEEN STATION 1287 AND STATION 1309 LEFT SIDE CUSP MEMBRANE. MANUFACTURED NEW SECTION OF CUSP MEMBRANE AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 97. (W) 2L72 4F A6WE 19950421004371995042100437WP 1995 4 21 USAA950336 119950316A532099100781 ANGLE DOUG DC9 DC981 3022081WP BS 180/203 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION BETWEEN STATION 180 AND 203 FORWARD GALLEY AREA AND SERVICE DOOR THRESHOLD JAMB PAN, CUSP ANGLE LOWER CORNER OF SERVICE DOOR OPENING. (W) 2L72 4F A6WE 19950421004381995042100438WP 1995 4 21 USAA950337 119950316A5320 DOOR JAMB DOUG DC9 DC981 3022081WP BS 370/427 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT FORWARD CARGO DOOR JAMB BETWEEN STATION 370 AND 427. REPLACED PAN AND SPLICED WITH REPAIR DOUBLERS PER SRM 53-05 FIG 44. (W) 2L72 4F A6WE 19950421004391995042100439NM 1995 4 21 USAA950354 119950404A3350 EEL BATTERY PACK BOEING727 727214 138407RNM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19754US 21958 BOS - THE EMERGENCY EXIT LIGHT ON THE LOWER RIGHT WING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EMERGENCY BATTERY PACK AND BATTERY. (W) 2L73 4F A3WE 19950421004401995042100440NM 1995 4 21 USAA950355 119950327A3350 EEL BATTERY PACK BOEING727 727214 138407RNM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19754US 21958 PIT - THE RIGHT EMERGENCY EXIT LIGHTS WERE INTERMITTENT. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED NORMAL. (W) 2L73 4F A3WE 19950421004411995042100441EU 1995 4 21 USAA950356 119950328A3350 EEL DIODE FOKKERF28 F28MK4000 4990810EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19488US 11240 CLT - THE EMERGENCY EVACUATION LIGHTS WILL NOT ILLUMINATE WHEN THE COCKPIT SWITCH IS USED. MAINTENANCE REPLACED THE DIODE (LV96) FOR THE EMERGENCY LIGHTS. OPERATIONS CHECKED NORMAL. (W) 2L72 4F RTA20EU 19950421004421995042100442WP 1995 4 21 AALA950038 119950110A7603580291751 CONTROL CABLE DOUG DC10 DC1010 3022110WP NR 2 ENGINE DEFECTIVE A AALAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 SW07126AA 46947 LAX-BOS - FLT 94 - DURING CRUISE, NR 2 ENGINE THROTTLE LEVER FROZE. ACFT PROCEEDED TO BOS. NR 2 ENGINE SHUTDOWN DURING APPROACH TO BOS AND ACFT LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE THROTTLE CABLE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A22WE 19950421004431995042100443EU 1995 4 21 AALA950315 119950216A5320 SHEAR TIE FOKKERF28 F28MK0100 4990807EU STR 34/42 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071459A 11479 SHEAR TIES CRACKED AT OBLIQUE FRAME NR 1 AT STR 34 AND 42. REMOVED OLD SHEAR TIES AND INSTALLED NEW PARTS PER SRM 53-00-02 REPAIR NR 2. (Z) 2L72 4F RT 19950421004441995042100444EU 1995 4 21 AALA950316 119950216A5330 SKIN FOKKERF28 F28MK0100 4990807EU FS 5805 DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW071459A 11479 DENT IN LT SIDE OF FUS STA 5305 SEC 58, 1 INCH BY .9375 INCH DEEP. INSTALLED TEMPORARY REPAIR PER SRM 53-00-02 AND REPAIR PER ESO 51000 DATED 2/13/95. (Z) 2L72 4F RT 19950421004451995042100445EU 1995 4 21 AALA950391 119950307A2910 O-RING FOKKERF28 F28MK0100 4990807EU NR 2 ENGINE DEFECTIVE A AALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW071455K 11467 DFW-BHM - FLT 1412 - EN ROUTE, HYDRAULIC SYSTEM 1 LOW QUANTITY ALERT CAME ON. ON APPROACH NR 1 HYDRAULIC SYSTEM FAILED, ACCOMPLISHED ALTERNATE GEAR EXTENSION. LANDED BHM WITHOUT INCIDENT. REPLACED O-RING ON NR 2 ENGINE PUMP. PRESSURE CHECKED SYSTEM, NO LEAKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RT 19950421004461995042100446NM 1995 4 21 AALA950413 119950308A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07320AA 22321 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BETWEEN R1 AND R3 DOORS INOPERATIVE. REPAIRED BROKEN WIRE IN FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004471995042100447NM 1995 4 21 AALA950430 119950312A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN NEEDED SECURED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT ROW 35B INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT ROW 35B. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004481995042100448NM 1995 4 21 AALA950432 119950310A3350 EEL ARROW BOEING767 767323 1385205NM RT OVERWING MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW07382AN 25451 MIA - DURING OVERNIGHT CHECK, RT AISLE EMERGENCY LIGHT RED ARROW MISSING AT OVERWING EXIT. REPLACED RED ARROW AT RT AISLE OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004491995042100449WP 1995 4 21 AALA950454 119950316A3350A3060719104 EEL STRIP DOUG DC9 DC982 3022082WP CABIN CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW077517A 49894 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS VERY DIM. FURTHER INVESTIGATION FOUND CORRODED STRIPS AT FWD GALLEY. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F A6WE 19950421004501995042100450NM 1995 4 21 AALA950458 119950313A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07323AA 22324 SFO - DURING OVERNIGHT CHECK, FLIGHT ATTENDANT SEAT CONTROL EMERGENCY LIGHT TRACK HAS BROKEN WIRE. REPAIRED BROKEN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004511995042100451WP 1995 4 21 AALA950459 119950313A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07133AA 47828 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT 34H INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A22WE 19950421004521995042100452NM 1995 4 21 AALA950460 119950320A33508100022601 EEL STRIP BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07361AA 24042 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING RIPPED FROM FLOOR AT SEAT 4H. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004531995042100453NM 1995 4 21 AALA950461 119950320A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07320AA 22321 SFO - DURNG OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 7G INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004541995042100454NM 1995 4 21 AALA950462 119950320A3350A3060722 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07882AA 21521 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 24 INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A3WE 19950421004551995042100455NM 1995 4 21 AALA950463 119950320A33501001141 LIGHT BOEING727 727223 1384074NM AFT AIRSTAIR EELDEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07715AA 22470 MIA - DURING OVERNIGHT CHECK, AFT AIRSTAIRS EMERGENCY OVERHEAD LIGHT INOPERATIVE. REPLACED AFT AIRSTAIRS EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A3WE 19950421004561995042100456NM 1995 4 21 AALA950498 119950322A33508100022002 EEL BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07378AN 25447 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR PROXIMITY AISLE LIGHTS AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR PROXIMITY AISLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004571995042100457NM 1995 4 21 AALA950500 119950325A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07870AA 21382 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING BY FWD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FWD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A3WE 19950421004581995042100458WP 1995 4 21 AALA950501 119950326A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1030 3023501WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07142AA 46714 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING AT BOTTOM OF FIRST CLASS CREDENZA INOPERATIVE. RESECURED EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT CREDENZA. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L73 4F A22WE 19950421004591995042100459WP 1995 4 21 AALA950502 119950326A3350A3060719104 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07482AA 49675 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING AT PAX SEAT ROW 21D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (Z) 2L72 4F A6WE 19950421004601995042100460EU 1995 4 21 AALA950503 119950324A3231 LOCK PIN FOKKERF28 F28MK0100 4990807EU LT MLG DOOR STOPNEEDED ADJUST A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071402K 11353 ORD-LIT - FLT 1061 - EN ROUTE, THE LT MLG MFDU WARNING INDICATION. CYCLED GEAR THREE TIMES DID NOT CLEAR MESSAGE. RETURNED ORD AND LANDED OVERWEIGHT WITHOUT INCIDENT. RIGGED LT MLG DOOR STOP LOCKING KEY AND INSTALLED NEW LOCKING CLIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DEFECTS FOUND. (Z) 2L72 4F RT 19950421004611995042100461NM 1995 4 21 AALA950513 419950323A256531073105 SLIDE BOEING727 727223 1384074NM PAX DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07702AA 22460 ORD - DURING SHOP TEST INFLATION, EMERGENCY EVACUATION SLIDE SEAM FAILED, SCRAPPED EMERGENCY EVACUATION SLIDE. (Z) 2L73 4F A3WE 19950421004621995042100462NM 1995 4 21 AALA950514 119950323A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07313AA 22316 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRES AT FWD FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 19950421004631995042100463NM 1995 4 21 AALA950526 119950328A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07380AN 25449 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 25JH THROUGH 35JH INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH CONNECTOR AT SEAT ROW 25JH. SYSTEM GROUND CHECKS NORMAL OPERATION. (Z) 2L72 4F RTA1NM 19950421004641995042100464NM 1995 4 21 AALA950527 119950328A3350AAP2661 EEL ASSEMBLY BOEING727 727223 1384074NM COCKPIT DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07701AA 22459 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN COCKPIT. SYSTEM GROUND CHECKS NORMAL OPERATION. (Z) 2L73 4F A3WE 19950421004651995042100465NM 1995 4 21 AWXA9500162 119950320A5347 SEAT TRACK BOEING737 737275 1384485NM FS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CORROSION ON GALLEY SUPPORT TRACK, STA 328 RBL 55, RBL 45 AND RBL 24. REMOVED AND REPLACED DAMAGED SECTION OF TRACK WITH NEW TRACK PER BOEING SRM 51-10-1 AND SRM 51-30-2. (Z) 2L72 4F A16WE 19950421004661995042100466NM 1995 4 21 AWXA9500163 119950320A5347 SEAT TRACK BOEING737 737275 1384485NM FS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 55720 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CORROSION BEYOND LIMITS ON SEAT TRACK AT STA 312, RBL 18 AND RBL 45. REMOVED, FABRICATED AND INSTALLED NEW SEAT TRACK PER BOEING SRM 51-10-1 AND SRM 51-30-2. (Z) 2L72 4F A16WE 19950421004671995042100467EU 1995 4 21 AWXA9500174 119950322A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EVERY OTHER EMERGENCY EXIT LIGHT INOPERATIVE WITH ACFT POWER OFF. REMOVED AND REPLACED BATTERY PACK 11WL, OPS CHECK GOOD. (Z) 2L72 4F RTA28NM 19950421004681995042100468NM 1995 4 21 AWXA9500187 119950328A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND NUMEROUS FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REATTACHED WIRING TO LIGHT MODULES AT SEVERAL LOCATIONS, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950421004691995042100469NM 1995 4 21 AWXA9500189 119950401A3350 EEL WIRING BOEING737 7373G7 1384595NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LAST TWO FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED WIRING, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950421004701995042100470NM 1995 4 21 AWXA9500190 119950331A2150L20TF4156NA CONNECTOR BOEING737 737277 1384570NM NR 2 PACK WORN A AWXAK NONE O OTHER TXTAXI/GRND HDL 1 WP28180AW 22647 PHX - DURING TAXI FROM GATE, CREW NOTED A STRONG BURNING RUBBER ODOR. ACFT RETURNED TO GATE AND MAINTENANCE COMPLIED WITH MEL PROCEDURES FOR 21 01 NR 2 PACK. MX ACTIONS LATER REPLACED THE COMPRESSOR DISCHARGE SENSOR CANNON PLUG. OPS CHECK OK. MEL REMOVED. (Z) 2L72 4F RTA16WE 19950421004711995042100471NM 1995 4 21 AWXA9500191 119950401A3233654491027 ACTUATOR BOEING737 7372A6 138448BNM RT MLG FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28145AW TSC1445 20194 ONT-LAS - DURING CLIMB, CREW RETRACTED GEAR AND RT MAIN GEAR DID NOT RETRACT. GEAR HANDLE PLACED TO OFF AND RT MAIN GEAR EXTENDED WITH GREEN LIGHT. CREW SELECTED GEAR DOWN, NOSE AN LT MAIN GEARS EXTENDED WITH GREEN LIGHTS. CREW RETURNED TO ONT AND LANDED WITHOUT FURTHER INCIDENT. RT MAIN GEAR INSPECTED AND FOUND SAFE FOR MX FERRY TO PHX. MX FOUND RT MAIN GEAR ACTUATOR AT FAULT, AND REMOVED AND REPLACED RT MAIN GEAR ACTUATOR. ACFT RELEASED FOR SERVICE. (Z) 2L72 4F A16WE 19950421004991995042100499EA 1995 4 21 95ZZZX1891 219950330A852075458 CRANKSHAFT PIPER PA31 PA31P 7103120SO LYC O541 TIGO541E1A 41539EA NR 4 CTWEIGHT FAILED A AEKIAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP0718MC 2200 952 31P7300143 RL37262 DURING CRUISE, LT ENGINE LOST POWER, OIL PRESSURE OKAY. ENGINE SHUT DOWN AND SAFE LANDING MADE. FOUND BOLTS BROKE ON NR 3 CYCLINDER CONNECTING ROD. ALSO, NR 4 COUNTERWEIGHT BROKE LOOSE FROM CRANKSHAFT DUE TO FAILURE OF ATTACH POINT ON CRANKSHAFT. NO PRIOR INDICATION OF FAILURE. SUSPECT COUNTERWEIGHT BROKE LOOSE CAUSING ROD TO FAIL. 1L72 3O3 O A8EA E19EA 19950421005041995042100504 1995 4 21 AALA950423 419950308A2565101655101 SLIDE BFGOODRICH BOEING767 767 1385102NM LT O/WING FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 3043 LAX - DURING SHOP VISIT DEPLOYMENT, EMERGENCY EVACUATION SLIDE HAD SEVERAL SEAMS LEAKING DUE TO MATERIAL DETERIORATION. SCRAPPED EMERGENCY EVACUATION SLIDE. (X) 2L72 4F EXPA2L72 19950421005051995042100505 1995 4 21 AALA950425 419950308A2565101623109 SLIDE BFGOODRICH BOEING767 767 1385102NM FWD ENTRY DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 3249 LAX - DURING SHOP VISIT DEPLOYMENT, EMERGENCY EVACUATION SLIDE HAD SEVERAL LARGE AREAS OF POROSITY LEAKS. SCRAPPED EMERGENCY EVACUATION SLIDE. (X) 2L72 4F EXPA2L72 19950421005061995042100506 1995 4 21 AALA950491 419950320A2565101623111 SLIDE BFGOODRICH BOEING767 767 1385102NM FWD ENTRY DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 B23354 LAX - DURING SHOP VISIT DEPLOYMENT, B767 EMERGENCY EVACUATION SLIDE HAD SLIDE SEAMS SEPARATING AND FLOOR LOOSE. SCRAPPED EMERGENCY EVACUATION SLIDE. (X) 2L72 4F EXPA2L72 19950421005231995042100523EU 1995 4 21 95ZZZW526 119950309A5320 SHEAR ANGLE BAG BAE146BAE146100A 1500260EU FR 25 STR 18 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 CRACKED SHEAR ANGLE AT FRAME 25 BETWEEN STRINGER 18 AND 19 LEFT, FORWARD SIDE OF FRAME. REPLACED SHEAR ANGLE. 2H74 4F RTA49EU 19950421005241995042100524EU 1995 4 21 95ZZZW527 119950309A5320 SHEAR ANGLE BAG BAE146BAE146100A 1500260EU FR 25 STR 19 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 CRACKED SHEAR ANGLE AT FWD SIDE OF FRAME 25 BETWEEN STRINGERS 19 AND 20 LEFT. REPLACED SHEAR ANGLE. (W) 2H74 4F RTA49EU 19950421005251995042100525EU 1995 4 21 95ZZZW528 119950310A5280 PLATE BAG BAE146BAE146100A 1500260EU LT MLG DR CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS E1003 LEFT MLG DOOR REAR HINGE BRACKET, FORWARD PLATE NEEDS TO BE REPLACED DUE TO CRACKS FOUND DURING THE COMPLIANCE OF EO E92/067/632RA. CRACKS WERE CONFIRMED WITH ET. AFTER BOTH FORWARD AND AFT PLATES WERE REMOVED FOUND DETECTION WAS EXFOLIATION. REPLACED LEFT MLG AFT DOOR BRACKET ASSY IAW 146 MM 32-10-21, PROFILE CHECK TO BE COMPLIED WITH, WORK CARD GENERATED FOR PROFILE CHECK. REF W/C 70. 2H74 4F RTA49EU 19950421005261995042100526 1995 4 21 95ZZZW529 319950330A61124E30171 DE-ICE BOOT BEECH 1900 1900D 1154162CE LT PROPELLER MISSING A AJJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01838CA394 UE34 LEFT PROP, ONE BLADE MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INVESTIGATION, ITS APPARENT THAT THE PROBLEM LIES WITH THE PAINT THAT IS APPLIED PRIOR TO BOOT INSTALLATION. (W) 2L72 4T RTA24CE 19950421005271995042100527WP 1995 4 21 95ZZZW530 119950303A5711 SPAR CAP DOUG DC8 DC862 3021970WP RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION RT WING LEADING EDGE UPPER AT FRONT SPAR CAP ATTACH FLANGE HAS CORROSION AROUND SCREW HEADS OUTBOARD OF NR 4 PYLON FROM APPROXIMATELY XFS 503 TO XFS 710. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950421005281995042100528WP 1995 4 21 95ZZZW531 119950303A5512 SKIN DOUG DC8 DC862 3021970WP HORIZ STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-1. (W) 2L74 4F 4A25 19950421005291995042100529WP 1995 4 21 95ZZZW532 119950303A5330 SKIN DOUG DC8 DC862 3021970WP FS 670-685 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN FRAMES 670 TO FS 685 HAS SKIN CRACK AND BULGING AROUND FASTENER HEADS LGRN 21R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH DWG RCH D85330-5018. (W) 2L74 4F 4A25 19950421005301995042100530WP 1995 4 21 95ZZZW533 119950303A5512 SKIN DOUG DC8 DC862 3021970WP HORIZ STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, RT HORIZONTAL STAB UPPER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 55-3-0. (W) 2L74 4F 4A25 19950421005311995042100531WP 1995 4 21 95ZZZW534 119950303A5320 WINDOW FRAME DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, WINDOW NR 23R HAS CORROSION INSIDE FRAME. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH EO 9402289. 2L74 4F 4A25 19950421005321995042100532WP 1995 4 21 95ZZZW535 119950303A5512 SKIN DOUG DC8 DC862 3021970WP HORIZ STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LOWER SURFACE SKI AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2. (W) 2L74 4F 4A25 19950421005331995042100533WP 1995 4 21 95ZZZW536 119950224A5330 SKIN DOUG DC8 DC862 3021970WP BS 1530/1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) 2L74 4F 4A25 19950421005341995042100534WP 1995 4 21 95ZZZW537 119950224A5320 FITTING DOUG DC8 DC862 3021970WP BS 1530 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT BATHTUB FITTING IS CORRODED AT BS 1530R, LONGERON 30R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950421005351995042100535WP 1995 4 21 95ZZZW538 119950224A5320 FITTING DOUG DC8 DC862 3021970WP BS 1606 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 32 RIGHT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19950421005361995042100536WP 1995 4 21 95ZZZW539 119950224A5315 FLOOR BEAM DOUG DC8 DC862 3021970WP BS 1586 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, ENTIRE FLOOR BEAM CAP AT BS 1586 IS CORRODED FROM LEFT TO RIGHT SIDE OF CABIN. CLEANED CORROSION, FABRICATED, AND INSTALLED NEW FLOOR BEAM PER SRM 53-1-0. 2L74 4F 4A25 19950421005381995042100538WP 1995 4 21 95ZZZW541 119950227A5330 SKIN LKHEED1011 10113851 5265010WP BS 700 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19303EA 193A1004 LEVEL 2 CORROSION, CORROSION AT STATION 700 BETWEEN STRINGER 33 AND 34 ON SKIN. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-12-00. 2L73 4F A23WE 19950421005391995042100539WP 1995 4 21 95ZZZW542 119950301A5315 FLOOR BEAM DOUG DC8 DC862 3021970WP BS 1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FLOOR BEAM CAP AT BS 1540 IS CORRODED FROM 45 INCHES LBL TO 45 INCHES. REMOVED AND REPLACED FLOOR BEAM CAP PER SRM 53-1-0. 2L74 4F 4A25 19950421005401995042100540WP 1995 4 21 95ZZZW543 119950301A5311 FRAME DOUG DC8 DC862 3021970WP BS 1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN CIRCUMFERENTIAL FRAME IS CORRODED AT BS 1574L FROM LONGERON 24 TO 26L. REMOVED CORROSION AND REPLACED FRAME SECTION PER SRM 53-1-0. 2L74 4F 4A25 19950421005411995042100541WP 1995 4 21 95ZZZW544 119950301A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN TRIANGLE FLOOR WEB SUPPORT IS CORRODED AT BS 1574 CENTER, CENTER LINE 12 INCHES LBL 12 INCHES RBL. REMOVED AND REPLACED TRIANGLE FLOOR WEB PER SRM 53-1-0. 2L74 4F 4A25 19950421005421995042100542WP 1995 4 21 95ZZZW545 119950301A5720 FLANGE DOUG DC8 DC862 3021970WP AUX TANK CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LEFT AUXILLARY TANK UPPER ATTACH FLANGE HAS INTERGRANULAR CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19950421005431995042100543WP 1995 4 21 95ZZZW546 119950301A5753 SLOT DOOR DOUG DC8 DC862 3021970WP LT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LEFT WING NR 1 SLOT DOOR HAS DOUBLER REPAIR THAT IS SURROUNDED BY CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER DOUGLAS FILE NR 258324. 2L74 4F 4A25 19950421005441995042100544WP 1995 4 21 95ZZZW547 119950301A5330 SKIN DOUG DC8 DC862 3021970WP BS 1530-1606 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT MAIN CABIN LOWER FUSELAGE SKIN IS CORRODED FROM BS 1530 TO BS 1606 LONGERON 35L TO 35R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. 2L74 4F 4A25 19950421005451995042100545WP 1995 4 21 95ZZZW548 119950302A5330 SKIN DOUG DC8 DC862 3021970WP BS 1586 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FUSELAGE SKIN IS CORRODED BETWEEN BS 1586L AND 1574, LONGERON 26L AND LONGERON 24L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. 2L74 4F 4A25 19950421005461995042100546NM 1995 4 21 AWXA9500214 119950412A5320 INTERCOSTAL BOEING737 7372Q8 138448KNM STA 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 DURING C12 INSPECTION, FOUND INTERCOSTAL STATION 294 TO 312 RBL 12 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-30-2 AND 53-10-2, FIGURE 7. 2L72 4F RTA16WE 19950421005471995042100547NE 1995 4 21 M3HA95005 219950327A7320 CONNECTOR AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE RT ENG LOOSE A M3HACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP13983MA 308 R121188 FLT NR 1530 - DURING TAKEOFF ROLL NR 2 TORQUE GAUGE INDICATED ZERO. PILOT ABORTED TAKEOFF. FOUND RIGHT TORQUE INDICATOR AND FUEL CLOG CAUTION CIRCUIT BREAKERS BOTH POPPED. PERFORMED A VISUAL CHECK INSIDE RIGHT ENGINE NACELLE AND FOUND THE TOP CANNON PLUG ON FUEL CONTROL ASSEMBLY BACKED OFF. CLEANED AND RESEATED CANNON PLUG. RESET BOTH POPPED CIRCUIT BREAKERS. AIRCRAFT OPERATIONALLY CHECKED GOOD DURING TWO FULL POWER TAXI-RUNS. AIRCRAFT RELEASED FOR SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950421005481995042100548NM 1995 4 21 USAA950194 119950227A79301163P181 SWITCH BOEING737 737201 1384454NM NR 2 ENG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19242US 22444 JAX - FLT 1606 - ON CLIMB NR 2 OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDED THROTTLE AND LIGHT WENT OUT. FLIGHT DIVERTED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. REPLACED RIGHT MAIN OIL FILTER BYPASS SWITCH AND RIGHT MAIN OIL SCREEN. (W) 2L72 4F A16WE 19950421005491995042100549WP 1995 4 21 USAA950287 119950217A5531 RIB DOUG DC9 DC931 3022065WP VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK IN VERTICAL STAB STATION ZFS 52.3 5TH RIB, CRACK AT SIDE END. INSTALLED DOUBLER REPAIR PER SRM 55-02 FIG 27. (W) 2L72 4F A6WE 19950421005501995042100550WP 1995 4 21 USAA950288 119950215A5320 MEMBRANE DOUG DC9 DC931 3022065WP BS 604/598 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH SKIN CRACK AT CUSP MEMBRANE AT STATION 604 LONGERON 18R STATION 598 18L. INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 96. (W) 2L72 4F A6WE 19950421005511995042100551WP 1995 4 21 USAA950289 119950209A5320 MEMBRANE DOUG DC9 DC931 3022065WP BS 945 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL I CORROSION AT CUSP MEMBRANE AT STATION 945 RT SIDE. REMOVED CORRODED SECTION OF MEMBRANE AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 96. (W) 2L72 4F A6WE 19950421005521995042100552WP 1995 4 21 USAA950290 119950213A5532 SKIN DOUG DC9 DC931 3022065WP VERT STAB GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .035 GAUGE 7 INCH LONG IN VERTICAL STAB AT STA ZV133 LT SIDE. INSTALLED DOUBLER REPAIR PER SRM 35-01 FIG 2. (W) 2L72 4F A6WE 19950421005531995042100553WP 1995 4 21 USAA950291 119950222A5720 FITTING DOUG DC9 DC931 3022065WP CTR TANK CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND .25 INCH CRACK IN KEEL FITTING BELOW CENTER TANK REAR SPAR FWD OF MLG DOOR. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (W) 2L72 4F A6WE 19950421005541995042100554WP 1995 4 21 USAA950292 119950210A5400 ANGLE DOUG DC9 DC931 3022065WP BS 1019 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK RIGHT UPPER PYLON ATTACH ANGLE STATION 1019. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W) 2L72 4F A6WE 19950421005561995042100556WP 1995 4 21 USAA950294 119950223A5330 SKIN DOUG DC9 DC931 3022065WP BS 503 DAMAGMED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND TEMPORARY CLASS II REPAIR INSTALLED AT STATION 503 LONGERON 25L AND 24L. REMOVED TEMPORARY REPAIR AND INSTALLED FLUSH REPAIR PER USAIR TYPICAL REPAIR 53-30-08. (W) 2L72 4F A6WE 19950421005571995042100557WP 1995 4 21 USAA950295 119950228A575399574503 SPAR CAP DOUG DC9 DC931 3022065WP LT TE FLAP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK LEFT FLAP UPPER STRINGER UPPER SPAR CAP AT XFIS-244. INSTALLED DOUBLER REPAIR PER DACO DWG 995750 AND USAIR EA 29548. (W) 2L72 4F A6WE 19950421005581995042100558WP 1995 4 21 USAA950296 119950224A5711 SPAR DOUG DC9 DC931 3022065WP LT WING CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND CORROSION LEFT WING AFT LOWER SPAR, LOWER FLANGE STATION XRS 546. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 57-09 FIG 11. (W) 2L72 4F A6WE 19950421005591995042100559WP 1995 4 21 USAA950297 119950223A5330 SKIN DOUG DC9 DC931 3022065WP BS 996 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND A .75 INCH CRACK ON EACH SIDE OF RIVET HEAD AT STATION 996 ABOVE RT PYLON LAWN ATTACH ANGLE, IN SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17A. (W) 2L72 4F A6WE 19950421005601995042100560WP 1995 4 21 USAA950298 119950301A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND CORROSION .033 DEEP AT NR 2 ADF LOOP ANTENNA IN SKIN. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 29. (W) 2L72 4F A6WE 19950421005611995042100561WP 1995 4 21 USAA950299 119950223A5330 SKIN DOUG DC9 DC931 3022065WP BS 945 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL I CORROSION REF C57-5330 FUSELAGE SKIN AFT SIDE OF FRAME STATION 945 BETWEEN LONGERON 28R AND 29R. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B. (W) 2L72 4F A6WE 19950421005621995042100562WP 1995 4 21 USAA950300 119950227A5320 WEB DOUG DC9 DC931 3022065WP BS 900 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19971VJ72252 47051 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND SMALL DENT AND CRACK .1250 INCH AT 5910158-35 WEB AT FUSELAGE STATION 900 LONGERON 25R SID PSE 53.09.035A. INSTALLED DOUBLER REPAIR PER DACO 5910158 AND USAIR EA NR 29704. (W) 2L72 4F A6WE 19950421005631995042100563NM 1995 4 21 USAA950309 119950330A5320 BEAM BOEING737 737201 1384454NM BS 227 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19252AU34119 22758 GSO - DURING UNSCHEDULED MAINTENANCE VISUAL INSPECTION, FOUND 1.5 INCH CRACK, FORWARD END OF WEB AT THE NLG ACTUATOR SUPPORT FITTING BEAM AT STATION 227. REPAIRED PER EA 30088, SRM 51-40-2 FIG 1. (W) 2L72 4F A16WE 19950421005641995042100564WP 1995 4 21 USAA950327 119950228A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND .1250 INCH CRACK STATION 160 LONGERON 4 LEFT. CUT OUT DAMAGED SECTION AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG 02. (W) 2L72 4F A6WE 19950421005651995042100565WP 1995 4 21 USAA950328 119950303A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK STATION 160 LONGERON 3 LEFT. CUT OUT DAMAGED SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950421005661995042100566WP 1995 4 21 USAA950329 119950303A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND .3125 INCH CRACK STATION 160 LONGERON 2 LEFT. CUT OUT DAMAGE SECTION OF LONGERON AND SPLICED IN NEW SECTION PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950421005671995042100567WP 1995 4 21 USAA950330 119950228A5320 MEMBRANE DOUG DC9 DC981 3022081WP BS 200 GOUGE A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND GOUGE JUST AFT OF SERVICE DOOR CUSP MEMBRANE STATION 200 LONG 18R. CUT OUT CUSP MEMBRANE SECTION AND INSTALLED REPAIR SECTION PER SRM 53-05 FIG 9. (W) 2L72 4F A6WE 19950421005681995042100568WP 1995 4 21 USAA950331 119950228A5330 SKIN DOUG DC9 DC981 3022081WP BS 408 DENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND A 1 INCH BY 100 INCH DEEP DENT AT STATION 408 LONGERON 17 LEFT. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW G. (W) 2L72 4F A6WE 19950421005691995042100569WP 1995 4 21 USAA950332 119950224A5330 SKIN DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q2 INSPECTION, FOUND CRACK .5 INCH LONG STATION 160 FORWARD AIR STAIR CUT OUT UPPER FWD CORNER SKIN. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A VIEW G. (W) 2L72 4F A6WE 19950421005701995042100570WP 1995 4 21 USAA950333 119950303A5532593614318 SKIN DOUG DC9 DC981 3022081WP RT VERT STAB GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND GOUGE RT VERTICAL STAB SKIN PANEL. BURNISHED GOUGES AREA AND INSTALLED INTERNAL DOUBLER PER USAIR EA 29729 AND SRM 55-01 FIG 2 SHEET 2. (W) 2L72 4F A6WE 19950421005711995042100571WP 1995 4 21 USAA950334 119950228A5313 LONGERON DOUG DC9 DC981 3022081WP BS 256 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 256 LONGERON 17 LEFT. CUT OUT DAMAGED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950421005721995042100572WP 1995 4 21 USAA950338 119950316A5320 WEB DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1338 AFT CARGO AREA BETWEEN LONGERONS 28L AND 28R. REMOVED CORROSION, CLEANED AND TREATED. INSTALLED REPAIR DOUBLERS PER SRM 53-03 FIG 3 PER USAIR TYPICAL REPAIR 53-30-10. (W) 2L72 4F A6WE 19950421005731995042100573WP 1995 4 21 USAA950339 119950316A532059364423 THRESHOLD DOUG DC9 DC981 3022081WP BS 1155-1220 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AFT CARGO DOOR THRESHOLD AT STATION 1155-1220 WEB AND STRAP. REMOVED AND REPLACED WEB AND STRAP PER DACO DWG NR 5936442. (W) 2L72 4F A6WE 19950421005741995042100574WP 1995 4 21 USAA950340 119950301A5330 SKIN DOUG DC9 DC981 3022081WP BS 1155-1174 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION ON FUSELAGE LOWER SKIN BETWEEN 1155 AND 1174. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR WITH EXTERNAL DOUBLER PER SRM 53-04 FIG 12B AND USAIR EA NR 29833. (W) 2L72 4F A6WE 19950421005751995042100575WP 1995 4 21 USAA950341 119950316A5311 BELT FRAME DOUG DC9 DC981 3022081WP STA 1309 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1309 BETWEEN LONGERON 28L AND 29R ON BELTFRAME 'J'. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-03 FIG 7. (W) 2L72 4F A6WE 19950421005761995042100576WP 1995 4 21 USAA950342 119950310A5320 BEAM DOUG DC9 DC981 3022081WP BS 1368 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL I CORROSION AT STATION 1322 BETWEEN AFT GALLEY AND AFT LAV CENTER AISLE. REMOVED CORRODED AREA AND INSTALLED FILLER AND REPAIR ANGLE PER USAIR TYPICAL REPAIR 53-10-19. (W) 2L72 4F A6WE 19950421005771995042100577WP 1995 4 21 USAA950343 119950312A5330 SKIN DOUG DC9 DC981 3022081WP BS 769 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION SKIN AT STATION 769 LONGERON 28 RT. CLEANED AND TREATED CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53. (W) 2L72 4F A6WE 19950421005781995042100578WP 1995 4 21 USAA950344 119950312A5330 SKIN DOUG DC9 DC981 3022081WP BS 807 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 807 LONGERON 29 LEFT SKIN. CLEANED AND TREATED CORRODED AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 53. (W) 2L72 4F A6WE 19950421005791995042100579WP 1995 4 21 USAA950345 119950303A532039146771N SPLICE DOUG DC9 DC981 3022081WP BS 1193-1212 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193-1212 LONGERON 28L. REMOVED REPLACED SPLICE PER SRM 53-02 FIG 16. (W) 2L72 4F A6WE 19950421005801995042100580WP 1995 4 21 USAA950346 119950316A532039146771N SPLICE DOUG DC9 DC981 3022081WP BS 1193-1212 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION BETWEEN STATION 1193 AND 1212 LONGERON 29 LEFT. REMOVED AND REPLACED CORRODED SPLICE PER SRM 53-00 FIG 16. (W) 2L72 4F A6WE 19950421005811995042100581WP 1995 4 21 USAA950347 119950316A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1322 FLOOR BEAM AFT RT LAV. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND REPAIR ANGLE DOUBLERS PER SRM 53-10-19. (W) 2L72 4F A6WE 19950421005821995042100582WP 1995 4 21 USAA950348 119950301A532059137002 FITTING DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION AT STATION 1338 RT SIDE UPPER TO LOWER FRAME ATTACH LONGERON 18R CUSP. REMOVED CORROSION, TREATED AND REPLACED FITTING PER DACO PRINT REF NR 5913700. (W) 2L72 4F A6WE 19950421005831995042100583WP 1995 4 21 USAA950349 119950309A5320 WEB DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION STATION 1338 RT SIDE UNDER LAV THRESHOLD FLOOR BEAM AREA. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72. (W) 2L72 4F A6WE 19950421005841995042100584WP 1995 4 21 USAA950350 119950228A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP BS 1344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND LEVEL II CORROSION REF C58-53301 AT STATION 1344 AFT LEFT GALLEY ATTACHMENT AT FLOOR BEAM 1338 TO AFT PRESSURE BULKHEAD AT FLOOR LEVEL. MANUFACTURED INTERCOSTAL AND REPLACED PER SRM 53-14. (W) 2L72 4F A6WE 19950421005851995042100585WP 1995 4 21 USAA950351 119950316A5330 SKIN DOUG DC9 DC981 3022081WP BS 275-294 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19811US37113 48043 PIT - DURING Q-2 INSPECTION, FOUND DENT 1 INCH BY 1.75 INCH BY .75 INCH DEEP BETWEEN STATION 275 AND 294 LONGERON 23L AND 27L IN SKIN AREA. INSTALLED DOUBLER REPAIR PER SRM 53-04 SH 17 FIG 38. (W) 2L72 4F A6WE 19950421005861995042100586NE 1995 4 21 USAA950352 219950331A7200 ENGINE BOEING737 7372B7 1384560NM PWA JT8 JT8D15A 52051NE RIGHT BIRDSTRIKE A USAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 EA19279AU 22891 ORF - FLT 2323 - ON TAKEOFF AT V2, CREW HEARD A LOUD BANG. FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT. BIRD STRIKE ON RT ENGINE. INSPECTED PER MM 5-51-201, PAGE 201. RAN ENGINE AND ALL PARAMETERS NORMAL. (W) 2L72 4F4 F A16WE E2EA 19950421005871995042100587NM 1995 4 21 USAA950358 119950404A3610 CLAMP BOEING737 737201 1384454NM 13TH STAGE DUCT LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19239US 22354 CLT - NR 2271 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 ENGINE INDICATED HIGH EGT AND FUEL FLOW. FLIGHT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE SECURED LOOSE CLAMP ON 13 STAGE DUCT. LEAK CHECK OK. RAN ENGINES, CHECKS NORMAL. NO SPLIT IN THROTTLES OR PARAMETERS. (W) 2L72 4F A16WE 19950421005881995042100588NM 1995 4 21 9505896615 119950403A5730 PANEL BOEING747 747251B 1384892NM WS 338 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01615US 20360 DURING PERIODIC CHECK, FOUND THE LEFT WING LEADING EDGE UPPER WING FIBERGLASS PANEL CORRODED AT APPROXIMATELY ILES 338 AND GOING OUTBOARD APPROXIMATELY 24 INCHES OR TWO RIBS. INSTALLED NEW CHORD FROM BAC 1506-2664 EXTRUSION AND INSTALLED REPAIR. 2L74 4F A20WE 19950421005891995042100589NM 1995 4 21 9505906615 119950324A5311 FRAME BOEING747 747251B 1384892NM FS 400 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01615US 20360 DURING PRIODIC CHECK, THE FRAME INNER CHORD WAS FOUND CORRODED ON THE FRAME AT FS 400, STR 26L. THE FRAME INNER CHORD P/N 65B07936-327 IS MADE FROM 7075 EXTRUSION PER BAC 1506-2031. MADE REPAIR PER EA 66-97919. 2L74 4F A20WE 19950421005901995042100590NM 1995 4 21 9505916631 119950403A5740 RIB BOEING747 747251B 1384892NM RT WING DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01631US 23111 DURING PERIODIC CHECK, THE RIGHT WING LEADING EDGE RIB WAS DAMAGED WHILE INSTALLING THE NR 3 ENGINE STRUT. THE LOWER 'TEE' CHORD WAS BENT. CHORD MATERIAL 1507075-T6 EXTRUSION PER BAC 1505-10042. MADE REPAIR PER EA 66-97904. 2L74 4F A20WE 19950421005911995042100591NM 1995 4 21 9505926305 119950418A5347 SEAT TRACK BOEING747 747451 1384940NM FS 2265-2270 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 2265 TO 2270, RBL 34. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 63-97884. 2L74 4F RTA20WE 19950421005921995042100592NM 1995 4 21 9505945526 119950413A5414 SKIN BOEING757 757251 1384970NM NR 1 NACELLE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01526US 25864 23620 DURING PERIODIC CHECK, THE NR 1 ENGINE NACELLE STRUT SKIN PANEL WAS FOUND WITH A CRACK COMING OUT OF THE 433AL ACCESS PANEL. CRACKS WERE APPROXIMATELY 0.75 INCH LONG IN THE SKIN, DOUBLER, AND TRIPLER. INSTALLED REPAIR PER NWA EA 55-98174. MFG PART NUMBER 311N3450-13, -15. 2L72 4F RTA2NM 19950421005931995042100593WP 1995 4 21 9505959755 119950405A57555910055515 PANEL DOUG DC9 DC941 302207NWP LT SPOILER DISBONDING A NWAAK NONE O OTHER ININSP/MAINT 1 GL01755NW 9830 47179 DURING FLIGHT DTW-ATL, FOUND THAT SHEET METAL WAS LOOSE AND FLAPPING UNDER THE LEFT INBOARD SPOILER PANEL. CONTINUED TO ATL WITHOUT FURTHER INCIDENT. FOUND PREVIOUS REPAIR DISBONDING. REPLACED SPOILER PER MM 27-60. 2L72 4F A6WE 19950421005941995042100594WP 1995 4 21 9505969958 119950407A5230 BRACKET DOUG DC9 DC931 3022065WP FWD CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01917RW 47145 DURING PERIODIC CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR JAMB 'U' CHANNELS AND CORRESPONDING ATTACH ANGLES BETWEEN DOOR HINGES. REPLACED PARTS PER EA 99-097461. 2L72 4F A6WE 19950421005951995042100595WP 1995 4 21 9505979995 119950407A5313 LONGERON DOUG DC9 DC931 3022065WP FS 210 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN LONGERON 15L TO FS 210 FRAME STRAP. REPAIRED PER EA 99-092452. 2L72 4F A6WE 19950421005961995042100596WP 1995 4 21 9505989963 119950407A5330 SKIN DOUG DC9 DC931 3022065WP FS 440 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01913RW 47171 DURING PERIODIC CHECK, FOUND CORROSION ON ANTENNA DOUBLER AND FUSELAGE SKIN FS 440 BETWEEN LONGERONS 29L TO 30. REPLACED DOUBLER PER SRM 51-30-2 AND REPAIRED SKIN PER EA 99-097430. 2L72 4F A6WE 19950421005971995042100597WP 1995 4 21 9505999162 119950407A5743 FITTING DOUG DC9 DC914 3022034WP LT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018907E 45748 DURING LINE CHECK, FOUND CORROSION AND PREVIOUS REWORK ON THE LEFT MAIN LANDING GEAR SIDE BRACE ATTACH LUG FACES. REWORKED PER EA 91-64916, SEC 1. 2L72 4F A6WE 19950421005981995042100598WP 1995 4 21 9506009948 119950408A5712 BULKHEAD DOUG DC9 DC931 3022065WP WS 42 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018929E 45866 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .375 INCH CRACK IN LEFT BULKHEAD 42 LOWER 'T' EXTRUSION AT AFT END. REPAIRED PER EA 99-092430. 2L72 4F A6WE 19950421005991995042100599WP 1995 4 21 9506019944 119950408A5720 DOUBLER DOUG DC9 DC931 3022065WP WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING LINE CHECK, FOUND CRACK AND CORROSION IN LEFT UPPER WING DIAMOND DOUBLER APPROXIMATELY 12 INCHES FROM FORWARD END. REPAIRED PER EA 99-097073, SEC 1. 2L72 4F A6WE 19950421006001995042100600WP 1995 4 21 9506029948 119950409A5753 SKIN DOUG DC9 DC931 3022065WP FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018929E 45866 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT FLAP INNER SURFACE OF LOWER SKIN XFLS 71 TO 112. REPAIRED PER EA 99-094116. 2L72 4F A6WE 19950421006011995042100601WP 1995 4 21 9506039995 119950409A5320 FITTING DOUG DC9 DC931 3022065WP FS 980 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION IN FLOOR SUPPORT FITTING FS 980 BETWEEN LONGERON 27R TO 28R. REPLACED FITTING. 2L72 4F A6WE 19950421006021995042100602WP 1995 4 21 9506049753 119950410A5320 SUPPORT DOUG DC9 DC941 302207NWP FS 408 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01753NW 47117 DURING PERIODIC CHECK, FOUND .5 INCH CRACK RADIATING FROM FS 408 VERTICAL FLOORBEAM SUPPORT ATTACH FASTENER, RIGHT OUTBOARD END OF BEAM. REPAIRED PER EA 97-097464. 2L72 4F A6WE 19950421006031995042100603WP 1995 4 21 9506059988 119950411A5312 FRAME DOUG DC9 DC931 3022065WP FS 69 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION ON THE FS 69 FRAME, LOWER END FLANGE. REPAIRED PER XEA X9-53-87. 2L72 4F A6WE 19950421006041995042100604WP 1995 4 21 9506069990 119950411A5744 HINGE DOUG DC9 DC931 3022065WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN FLAP HINGE FITTING BORES, RIGHT WING FORWARD HINGE NR 3 AND LEFT WING FORWARD HINGE NR 2. REPLACED RIGHT WING FITTING AND REPAIRED LEFT WING FITTING PER OHM 27-50-5. 2L72 4F A6WE 19950421006051995042100605WP 1995 4 21 9506079958 119950411A5230 FITTING DOUG DC9 DC931 3022065WP AFT CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01917RW 47145 DURING PERIODIC CHECK, FOUND CRACK IN AFT CARGO DOOR NR 1 BEAM END FITTING AT AFT SIDE OF INNER PAN. REPLACED FITTING. 2L72 4F A6WE 19950421006061995042100606WP 1995 4 21 9506089753 119950411A5313 LONGERON DOUG DC9 DC941 302207NWP FS 389 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01753NW 47117 DURING PERIODIC CHECK, FOUND (2) .5 INCH CRACKS RADIATING FROM LONGERON 17R TO FS 389 FRAME ATTACH FASTENERS. REPAIRED LONGERON PER SRM 53-02 FIG 4 AND EA 97-097460. 2L72 4F A6WE 19950421006071995042100607WP 1995 4 21 9506099163 119950411A5753 TE PANEL DOUG DC9 DC914 3022034WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING LINE CHECK, FOUND THAT THE RIGHT SIDE TRIPLE SLOTTED FLAP ARM BECAME DISCONNECTED RESULTING IN A 5 INCH CRACK IN THE TRAILING EDGE PANEL XEF 111.250, 2 FEET FORWARD OF THE TRAILING EDGE. ALSO, FOUND A CRACK IN THE -12R ANGLE. REPLACED PANEL AND REPAIRED ANGLE PER EA 91-097074. 2L72 4F A6WE 19950421006081995042100608WP 1995 4 21 9506109988 119950412A5713 LONGERON DOUG DC9 DC931 3022065WP LT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FORWARD SIDE OF THE LEFT WING STRINGER 17 AT THE ROOT. REPAIRED STRINGER PER XEA X9-57-14. 2L72 4F A6WE 19950421006091995042100609WP 1995 4 21 9506119958 119950412A5311 FITTING DOUG DC9 DC931 3022065WP FS 148 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01917RW 47145 DURING PERIODIC CHECK, FOUND CORROSION IN FS 148 FRAME FITTING AT RIGHT SIDE CUSP. REPLACED FITTING PER SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950421006101995042100610WP 1995 4 21 9506129604 119950412A5320 CASTING DOUG DC9 DC932 3022066WP FS 945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOOR STRAP ATTACH CASTING FS 945 AT LBL 20. REPLACED CASTING PER SRM 51-40. 2L72 4F A6WE 19950421006111995042100611WP 1995 4 21 9506139759 119950412A5320 FITTING DOUG DC9 DC941 302207NWP FS 642 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING PERIODIC CHECK, FOUND CRACK IN LEFT HALF OF LONGERON 30 END FITTING AT FS 642. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950421006121995042100612WP 1995 4 21 ABXA9500334 119950417A335041B004AD07G3 EEL BATTERY GRIMES 60031431 DOUG DC9 DC933F 302207AWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23930AX 8803 47363 EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERIES. OPS CHECKED NORMAL IAW DC-9 SUPP MM 33-53-00. 2L72 4F A6WE 19950421006131995042100613SO 1995 4 21 COM11864 119950417A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO011105G15952 120105 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2. P/N 120-17056-013, 2 EA, 120-17056-007, 2 EA, 120-17062-013, 1 EA, 120-17060-007, 1 EA, 120-17063-009, 2 EA. 2L72 4T RTA31SO 19950421006141995042100614EA 1995 4 21 COM60454 119950417A3231 LINKAGE CNDAIRCL600 CL6002B19 EA LT NLG DOOR OUT OF ADJUST A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01932CA2521 7038 THUMPING NOISE FROM NLG AREA AFTER LANDING GEAR SELECTED UP. RIGGED THE LT NLG DOOR TO MM SPECIFICATIONS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950421006151995042100615NM 1995 4 21 DL72S951490 119950412A5522657278411 SKIN BOEING727 727232 1384082NM LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 AT HMV, LEFT ELEVATOR WAS FOUND WITH CRACKED SKIN AT THE TRAILING EDGE. REPAIRED PER SRM 55-20-3. 2L73 4F A3WE 19950421006161995042100616NM 1995 4 21 DL72S951491 119950411A5754 SLAT BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11537DA 22073 49810 FOUND DURING A-2 LETTER CHECK, .5 INCH CRACK AT I/B STOP PAD NR 6 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950421006171995042100617NM 1995 4 21 DL72S951495 119950402A5313 STRINGER BOEING727 727232 1384082NM BS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 49810 FOUND ON CV2 CHECK, CORROSION AROUND RIVETS STRINGER 25L FROM 950A TO 950B. REPAIRED PER SRM 53-10-3 AND PER PS 900-5-1. 2L73 4F A3WE 19950421006181995042100618NM 1995 4 21 DL72S951496 119950412A57546516221100 RIB BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 49810 DURING SHOP, INSPECTION RT WING NR 5 L/E SLAT WAS FOUNED WITH RIB NR 12 CRACKED. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19950421006191995042100619NM 1995 4 21 DL72S951521 119950412A5313 STRINGER BOEING727 727232 1384082NM FS 950 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 49810 FOUND DURING CV-2 CHECK, CORROSION AROUND RIVETS IN STRINGER 25L BETWEEN STA 950D AND 950E. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950421006201995042100620NM 1995 4 21 DL72S951522 119950412A5320 CLIP BOEING727 727232 1384082NM FS 970 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 49810 FOUND DURING CV-2 CHECK, CORROSION WHERE FORMER 970 ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 PG 825. 2L73 4F A3WE 19950421006211995042100621NM 1995 4 21 DL72S951523 119950412A5320 CLIP BOEING727 727232 1384082NM FS 950 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 49810 FOUND DURING CV-2 CHECK, CORROSION FWD OF FORMER 950F WHERE IT ATTACHES TO SKIN BETWEEN STR 30 AND 28L. REPAIRED PER MM 53-11-0 FIG 825. 2L73 4F A3WE 19950421006221995042100622NM 1995 4 21 DL72S951540 119950413A5754 SKIN BOEING727 727232 1384082NM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11540DA 22386 49810 FOUND DURING A-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E SLAT AFT SKIN ATTACH ANGLE AT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19950421006231995042100623NM 1995 4 21 DL72S951548 119950414A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11522DA 21582 49810 UPON SHOP INSPECTION, 4TH RIB FROM INBOARD FOUND CRACKED, RT WING NR 6 L/E SLAT. REPAIRED PER SRM 57-54-00. 2L73 4F A3WE 19950421006241995042100624NM 1995 4 21 DL72S951553 119950414A5751 SKIN 652176634 BOEING727 727232 1384082NM RT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 170 21074 49810 AT HMV, FOUND RT WING O/B AILERON WITH LOOSE FASTENERS ON LOWER SKIN. REPAIRED PER SRM 57-51-00. 2L73 4F A3WE 19950421006251995042100625NM 1995 4 21 DL72S951560 119950409A5347 SEAT TRACK BOEING727 727232 1384082NM FS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND LT O/B SEAT TRACK CRACKED IN VERTICAL SUPPORT WEB CUTOUT 3 INCHES FWD OF STA 760 FLOORBEAM. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950421006261995042100626NM 1995 4 21 DL72S951561 119950411A5754 RIB BOEING727 727232 1384082NM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND NR 1 SLAT I/B END 2ND FRAME CRACKED. REPLACED RIB PER MM 57-54-00. 2L73 4F A3WE 19950421006271995042100627NM 1995 4 21 DL72S951562 119950407A5313 STRINGER BOEING727 727232 1384082NM FS 481 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND STR 26L CRACKED AT FASTERNER HOLE STA 481. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950421006281995042100628NM 1995 4 21 DL72S951563 119950409A5315 FLOORBEAM BOEING727 727232 1384082NM FS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND FLOORBEAM CAP CORRODED STA 400 FROM LBL 10 THROUGH RIGHT DOOR OPENING. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950421006291995042100629NM 1995 4 21 DL72S951564 119950411A5311 FRAME BOEING727 727232 1384082NM FS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND STA 380 FRAME AT R-1 DOOR CORRODED AT Z ANGLE JOINT. REPAIRED PER SRM 53-10-4 FIG 23. 2L73 4F A3WE 19950421006301995042100630NM 1995 4 21 DL72S951565 119950412A5320 CLIP BOEING727 727232 1384082NM FS 1070 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND SKIN ATTACH CLIP CRACKED AT STA 1070 STR 29R. REPAIRED PER MM 53-11-0 PG 825. 2L73 4F A3WE 19950421006311995042100631NM 1995 4 21 DL72W951481 119950405A5330 SKIN BOEING727 727247 138408FNM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND FUSELAGE SKIN WITH CORROSION DAMAGE AT FS 1050 AT STRINGER 28L. REPAIRED PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950421006321995042100632NM 1995 4 21 DL72W951483 119950401A5313 STRINGER BOEING727 727247 138408FNM FS 990 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND FUSELAGE FRAME AND STRINGER CORRODED AT FS 990 AT STRINGER 29L. REPAIRED FRAME PER MM 53-11-0 PG 825. 2L73 4F A3WE 19950421006331995042100633NM 1995 4 21 DL72W951484 119950405A5315 FLOORBEAM BOEING727 727247 138408FNM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 FLOORBEAM CORRODED STA 344 RBL 22 TO LBL 54 AT FASTENER HOLES. REPAIRED PER SRM 53-10-8 FIG 8. FOUND AT HMV. 2L73 4F A3WE 19950421006341995042100634NM 1995 4 21 DL72W951485 119950401A5311 FRAME BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 CORROSION ON BOTTOM LEG OF FORMER AT STA 1010 BETWEEN S30 AND S29R. REPAIRED PER SRM 53-10-4 FIG 4. FOUND AT HMV. 2L73 4F A3WE 19950421006351995042100635NM 1995 4 21 DL72W951497 119950405A5315 FLOORBEAM BOEING727 727247 138408FNM FS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 FLOORBEAM CORRODED STA 380 RBL 12 TO 44, FOUND AT HMV. REPAIRED PER SRM 53-10-8 FIG 1. 2L73 4F A3WE 19950421006361995042100636NM 1995 4 21 DL72W951499 119950303A57536521630188A SKIN BOEING727 727247 138408FNM NR 3 FORE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 49810 727 NR 3 FORE FLAP HAS L/E EDGE DAMAGE 16 AND 22 INCHES FROM I/B END. THIS DAMAGE WAS REPAIRED PER SRM 57-50-4 FIG 1. FOUND AT HMV SHOP INSPECTION. 2L73 4F A3WE 19950421006371995042100637NM 1995 4 21 DL72W951500 119950329A57536521634150K SKIN BOEING727 727247 138408FNM NR 3 AFT FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 LOWER L/E SKIN HAS CRACK APPROX 61 INCHES FROM I/B END. THIS WAS REPAIRED PER SRM 57-50-4 FIG 9, FOR NR 3 AFT FLAP AT HVM SHOP INSPECTION. 2L73 4F A3WE 19950421006381995042100638NM 1995 4 21 DL72W951511 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, STRINGER 15L WAS FOUND CRACKED AT ITS END AT FS 72OC LEFT WING ICE LIGHT HOUSING. REPAIRED PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19950421006391995042100639NM 1995 4 21 DL72W951512 119950412A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, STRINGER 15R FOUND CRACKED AT AFT SIDE OF RT WING LEADING EDGE ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950421006401995042100640NM 1995 4 21 DL72W951513 119950411A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, STRINGER 15R FOUND CRACKED AT FWD SIDE OF RT WING L/E ICE LIGHT HOUSING AT FS 720C. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950421006411995042100641NM 1995 4 21 DL72W951518 119950412A5311 FRAME BOEING727 727247 138408FNM FS 1030 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND FUSELAGE FRAME FS 1030 ABOVE STRINGER 25L CRACKED. CUT OUT DAMAGE SECTION AND REPAIRED PER DL ERA 301494-14. 2L73 4F A3WE 19950421006421995042100642NM 1995 4 21 DL72W951536 119950303A5753652163362 LE SKIN BOEING727 727247 138408FNM NR 4 MID FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 49810 NR 4 MID FLAP, L/E SKIN WORN AT I/B END OF FLAP. REPAIRED PER MM 575200, REMOVED WORN AREA INSTALLED INLAY AND DOUBLER. AT HMV, SHOP INSPECTION. 2L73 4F A3WE 19950421006431995042100643NM 1995 4 21 DL72W951541 119950330A7110 COWL FRAME BOEING727 727247 138408FNM NR 2 ENG WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FS 1353 FRAME AT RBL 11 WAS FOUND WORN BEYOND LIMITS FROM WEAR BY NR 2 ENGINE AFT COWL PANELS. REPAIRED PER MM 53-11-0 PG 801. 2L73 4F A3WE 19950421006441995042100644NM 1995 4 21 DL72W951554 119950408A5320 INTERCOSTAL BOEING727 727247 138408FNM FS 348-60 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 INTERCOSTAL AT STA 348 TO 360 STR 16L IS CRACKED. REPAIRED PER SRM 53-10-4 FIG 28. FOUND AT HMV. 2L73 4F A3WE 19950421006451995042100645NM 1995 4 21 DL72W951555 119950411A5754 SKIN BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 SKIN CRACKED, NR 4 SLAT HAS 6 CRACKS AT FENCE ATTACH POINTS. REPAIRED PER MM 57-54-0 PG 817. FOUND AT HMV. 2L73 4F A3WE 19950421006461995042100646NM 1995 4 21 DL72W951557 119950401A5313 STRINGER BOEING727 727247 138408FNM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 STA 1050 STR 28L HEAVY CORROSION BETWEEN SKIN AND STR BELOW FRAME AND INSIDE STRINGER. REPAIRED PER SRM 53-10-3 FIG 1. FOUND AT HMV. 2L73 4F A3WE 19950421006471995042100647NM 1995 4 21 DL73E951506 119950411A5280 DOOR BOEING737 737247 138448DNM LT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11243WA 23517 49810 FOUND DURING LETTER CHECK, MLG FLY DOOR O/B FWD EDGE REPAIR DAMAGED, LT WING SIDE. REPAIRED PER SRM 52-80-2 INSTALLED DOOR PER MM 51-40-15. 2L72 4F A16WE 19950421006481995042100648NM 1995 4 21 DL73E951532 119950412A5240 SKIN BOEING737 737247 138448DNM R 1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11375DL 23602 49810 FOUND DURING LETTER CHECK INSP, R-1 DOOR UPPER HINGE HAS CRACK FROM CUTOUT TO DRAIN HOLE. REPAIRED PER SRM 52-00-3. 2L72 4F A16WE 19950421006491995042100649NM 1995 4 21 DL757951487 119950404A5315 FLOORBEAM BOEING757 757232 1384965NM FS 720 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11628DL 22918 36176 DEFERRED NR CARD C/N 7648, DFW - 3-30-95 - J1 CHECK NR 164. CORROSION AROUND NUTPLATES ON FLOORBEAM STA 720 BETWEEN LBL 45.5 AND CENTERLINE. REPAIRED PER SRM 53-30-51. 2L72 4F RTA2NM 19950421006501995042100650NM 1995 4 21 DL757951498 119950411A5320 STRAP BOEING757 757232 1384965NM FS 380 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11684DA 27104 49810 FOUND DURING LETTER CHECK E/E COMPT STRAP CRACKED FWD OF STA 380 RT SIDE OF NOSE GEAR WELL. REPAIRED PER SRM 53-10-51. 2L72 4F RTA2NM 19950421006511995042100651NM 1995 4 21 DL757951534 119950412A5350 RADOME BOEING757 757232 1384965NM FWD FUSELAGE PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 23614 49810 FOUND DURING LETTER CHECK, RADOME HAS 2 PUNCTURES ON LT SIDE. REPAIRED PER SRM 53-10-72. 2L72 4F RTA2NM 19950421006521995042100652NM 1995 4 21 DL767951547 119950413A5753 FAIRING BOEING767 767232 1385132NM LT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11112DL 22224 49810 DURING LETTER CHECK, LEFT WING OUTBOARD T/E FLAP INBOARD CANOE FAIRING WAS FOUND DELAMINATED. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950421006531995042100653WP 1995 4 21 DLL10951558 119950414A2530LA16452 DRAIN LKHEED1011 10113851 5265010WP MID GALLEY PLUGGED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11721DA 193C1139 49810 DRAIN ON CAPTS SIDE IN MID GALLEY STOPPED UP AND WATER SEEPED INTO SERVICE OUTLET. OUTLET BEGAN TO SMOKE, SHUT OFF ALL GALLEY POWER AND PULLED C/B. CLEARED DRAIN LINE AND REPLACED OUTLET RECEPTACLE. 2L73 4F A23WE 19950421006541995042100654WP 1995 4 21 DLL17951501 119950408A3020 INLET RING LKHEED1011 10113853 5265020WP NR 2 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND RING CRACKED, INSIDE PANEL 311KC. FABRICATED REPAIR DOUBLER PER SRM 54-34-00 FIG 804, INSTALLED UPPER REPAIR, TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER ERA 270632-14. 2L73 4F A23WE 19950421006551995042100655WP 1995 4 21 DLL17951502 119950321A5330 DOUBLER LKHEED1011 10113853 5265020WP FS 943-983 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND INTERNAL DOUBLER CORRODED ON BOTH SIDES OF STR 33 FROM FS 943 TO 983, LOWER FUSELAGE SKIN. MADE NEW REPLACEMENT INTERNAL SPLICE STRAP AS PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006561995042100656WP 1995 4 21 DLL17951503 119950321A5330 SKIN LKHEED1011 10113853 5265020WP FS 967 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND SKIN CORRODED FS 967 BL 3L IN THE MESC. ROUTED OUT DAMAGE AND FABRICATED REPAIR DOUBLER PER SRM 53-31-00 FIG 836. 2L73 4F A23WE 19950421006571995042100657WP 1995 4 21 DLL17951504 119950321A5320 CENTER STRAP LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 901 TO 943. MADE NEW REPLACEMENT INTERNAL SPLICE STRAP AS PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006581995042100658WP 1995 4 21 DLL17951505 119950321A5330 CENTER STRAP LKHEED1011 10113853 5265020WP FS 886 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 886 TO 901. REPLACED INTERNAL STRAP AS PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006591995042100659WP 1995 4 21 DLL17951507 119950321A5320 CENTER STRAP LKHEED1011 10113853 5265020WP FS 679-709 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT STR 33, STA 679 TO 709. REPLACED INTERNAL SPLICE STRAP PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006601995042100660WP 1995 4 21 DLL17951508 119950321A5320 CENTER STRAP LKHEED1011 10113853 5265020WP FS 539 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT RT SIDE STR 33, STA 539 TO 549. REPLACED SECTION OF SPLICE STRAP PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006611995042100661WP 1995 4 21 DLL17951509 119950321A5320 CENTER STRAP LKHEED1011 10113853 5265020WP FS 499 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT LT AND RT SIDE OF STR 33, STA 499. REPLACED DAMAGED SECTION OF STRAP PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006621995042100662WP 1995 4 21 DLL17951510 119950321A5320 CENTER STRAP LKHEED1011 10113853 5265020WP FS 479 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND CENTER STRAP CORRODED IN C-1 B/B AT LT SIDE OF STR 33, STA 479. REPLACED DAMAGED SECTION OF STRAP PER SRM 53-31-00 FIG 822. 2L73 4F A23WE 19950421006631995042100663WP 1995 4 21 DLL17951514 119950322A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 281 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND HEAVY CORROSION ON FLOORBEAM AT FS 281 ON ALMOST THE ENTIRE UPPER CAP. REPAIRED BY REPLACING UPPER T-CAP PER SRM 53-21-00. 2L73 4F A23WE 19950421006641995042100664WP 1995 4 21 DLL17951515 119950322A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND FLOORBEAM CORRODED AT FS 1725, AREAS OF CORROSION FROM LBL 59 TO RBL 59. REPLACED SECTION OF T-ANGLE PER SRM 53-21-00. 2L73 4F A23WE 19950421006651995042100665WP 1995 4 21 DLL17951516 119950322A5320 DOUBLER LKHEED1011 10113853 5265020WP FS 1665-1685 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, INSPECTION FOUND THE INTERNAL SPLICE DOUBLER CORRODED AT STA 1665 TO 1685, LOWER CENTER FUSELAGE SKIN. REPAIRED PER SRM 53-31-00 FIG 825 SH 4. 2L73 4F A23WE 19950421006661995042100666WP 1995 4 21 DLL17951525 119950322A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 1665 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND FLOORBEAM CORRODED AT STA 1665 FROM DOOR SILL I/B 24 INCHES. REPLACED DAMAGED SECTION OF T-CAP PER SRM 53-23-00 PG 803. 2L73 4F A23WE 19950421006671995042100667WP 1995 4 21 DLL17951526 119950322A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 1685 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND FLOORBEAM UPPER CAP AT FS 1685 WITH CORROSION DAMAGE AT DOOR SILL TO LEFT SIDE SEAT TIE DOWN TRACK. TRIMMED OUT DAMAGED SECTION A RBL 3.5 PER SRM 53-23-00 FIG 802. FABRICATED NEW FLOOR CAP, INSTALLED REPAIR PER SRM 53-23-00. 2L73 4F A23WE 19950421006681995042100668WP 1995 4 21 DLL17951527 119950224A5330 CENTER STRAP LKHEED1011 10113853 5265020WP FS 609-649 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND CENTER STRAP CORRODED FROM FS 609 TO FS 649. MADE NEW STRAP PER AND INSTALLED PER SRM 53-31-00. 2L73 4F A23WE 19950421006691995042100669WP 1995 4 21 DLL17951528 119950328A5313 STRINGER LKHEED1011 10113853 5265020WP FS 923-983 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND STRINGER CORRODED STR 34 AT FS 923 TO 983. DRILLED NEW STRINGER AND SPLICE, INSTALLED PER SRM 53-13-00 FROM STA 913 TO 983. 2L73 4F A23WE 19950421006701995042100670WP 1995 4 21 DLL17951529 119950401A5320 DOUBLER LKHEED1011 10113853 5265020WP FS 629-669 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND EDGE DOUBLER CORRODED C1 B/B RT SIDE, FROM STA 629 TO 669. CUT OUT CORRODED SECTION OF DOUBLER AND REPLACED PER SRM 53-31-00 PG 863 FIG 825. 2L73 4F A23WE 19950421006711995042100671WP 1995 4 21 DLL17951530 119950402A5320 DOUBLER LKHEED1011 10113853 5265020WP FS 459 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND DOUBLER CORRODED AT STA 459 BL 0 FUSELAGE SKIN. REPLACED DAMAGED SECTION PER SRM 53-31-00. 2L73 4F A23WE 19950421006721995042100672WP 1995 4 21 DLL17951537 119950324A5400 ANGLE LKHEED1011 10113853 5265020WP NR 2 S DUCT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND NR 2 ENGINE INLET STRUCTURE CRACKED INSIDE PANEL 311UL AND 311UR AT FS 1705 JUST AFT OF NR 2 INLET L/E LIP. REPAIRED PER SRM 54-12-00 FIG 803. 2L73 4F A23WE 19950421006731995042100673WP 1995 4 21 DLL17951538 119950410A5313 STRINGER LKHEED1011 10113853 5265020WP FS 297 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND FUSELAGE STRINGER 37 WAS CRACKED IN LOWER RADIUS AT FS 297. REPAIRED PER SRM 53-13-00 PG 806 FIG 804. 2L73 4F A23WE 19950421006741995042100674WP 1995 4 21 DLL17951539 119950324A5415 BUSHING LKHEED1011 10113853 5265020WP NR 3 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, NR 3 PYLON O/B WING, PYLON MAIN ATTACH I/B BUSHING WAS WORN BEYOND LIMITS. REPAIRED PER SRM 54-11-00. ALSO, O/B WING, PYLON MAIN ATTACH CENTER BEARING IS GOUGED. REPAIRED PER SRM 54-11-00. 2L73 4F A23WE 19950421006751995042100675NM 1995 4 21 DLM88951488 119950408A5313 STRINGER DOUG MD88 MD88 3023688NM FS 1418 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 36176 AT HMV, STRINGER 2L IS CRACKED JUST AFT OF FS 1418. FABRICATED AND INSTALLED REPAIR PER SRM 53-02 FIG 5. 2L72 4F RTA6WE 19950421006761995042100676NM 1995 4 21 DLM88951489 119950411A5330 SKIN DOUG MD88 MD88 3023688NM FS 1338/1380 LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11965DL 49984 49810 FOUND DURING E-2 LETTER CHECK, TWO LIGHTNING STRIKES AT FS 1338 AND 1380 RT SIDE ABOVE NR 2 ENG PYLON. REPLACED DAMAGED FASTENERS PER SRM 53-04 FIG 38. 2L72 4F RTA6WE 19950421006771995042100677NM 1995 4 21 DLM88951493 119950411A5330 SKIN DOUG MD88 MD88 3023688NM FWD FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11965DL 49984 49810 FOUND DURING E-2 LETTER CHECK, .375 INCH CRACK IN FUSELAGE SKIN AT AFT HINGE CUTOUT FOR RNLG DOOR. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950421006791995042100679NM 1995 4 21 DLM88951519 119950412A3230 ANGLE DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11999DN 53371 49810 FOUND DURING C-2 LETTER CHECK, LT WHEEL WELL AFT STRIKER ANGLE CRACKED. REPAIRED PER SRM 53-05. 2L72 4F RTA6WE 19950421006801995042100680NM 1995 4 21 DLM88951520 119950412A3620 SENSE LINE DOUG MD88 MD88 3023688NM TAIL COMP LOOSE A DALAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11907DL 49538 49810 CLIMB-OUT OF ATL 18,000 FEET MASTER WARNING AND TAIL COMP HIGH LIGHT CAME ON. TURNED OFF PNEU HANDLES AND CLOSED HP BLEEDS, LIGHT WENT OUT AFTER 1 MIN. FOUND ON LEFT AUG VALVE LOW PRESS SENSE LINE LOOSE, TIGHTENED AND CKD OK PER PFHB. 2L72 4F RTA6WE 19950421006811995042100681NM 1995 4 21 DLM88951535 119950407A5320 ANGLE DOUG MD88 MD88 3023688NM LT MLG WW DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 49810 DURING HMV, FOUND TEMPORARY REPAIR AFT MLG WHEEL WELL DOOR CLOSEOUT ANGLE O/B SIDE. REPAIRED BY DYE CHECK AREA NOT CRACKED PAST STOP DRILL. FABRICATED REPAIR ANGLES AND INSTALLED PER SRM 53-05 FIG 81A. 2L72 4F RTA6WE 19950421006821995042100682NM 1995 4 21 DLM88951556 119950407A5754 SKIN DOUG MD88 MD88 3023688NM NR 2 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 49810 DURING HMV, FOUND 2 REPAIRS ON BOTTOM OF NR 2 SLAT INTERFERE WITH L/E OF WING. REPAIRED PER SRM 57-09 PG 35 REF. 2L72 4F RTA6WE 19950421006831995042100683NM 1995 4 21 DLM88951559 119950407A5311 FRAME DOUG MD88 MD88 3023688NM FS 389 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11939DL 49812 49810 DURING HMV, FOUND FRAME DENTED/CRACKED LT SIDEWALL AREA STA 389. REPAIRED BY REMOVING DAMAGED FRAME SECTION, BEGAN FABRICATION OF SPLICE DOUBLERS PER SRM 53-03. CUT AND DRILLED REPLACEMENT FRAME SECTION AND FINISHED DOUBLERS. TREAT AND PAINTED PER SRM 53-03, INSTALLED REPAIR PER SRM 53-03. 2L72 4F RTA6WE 19950421006841995042100684WP 1995 4 21 9505939868 119950407A5350 RELEASE MECH DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERNAL HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. REPLACED THE CLIPS AND RE-RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950421006851995042100685NM 1995 4 21 9506146601 119950327A5400 SPAR WEB BOEING747 747251B 1384892NM NR 3 STRUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01631US 23111 DURING PERIODIC CHECK, FOUND CRACK IN THE MID SPAR WEB OF THE NR 3 ENGINE STRUT STARTING AT A FASTENER NEXT TO THE INBOARD MID SPAR FITTING RUNNING FORWARD AND UNDER THE FITTING. MADE REPAIR PER EA 66-97901. 2L74 4F A20WE 19950421006861995042100686NE 1995 4 21 9506156625 219950418A7532 BLEED VALVE BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A NWAAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL01625US 21707 702173 DURING TAKEOFF, THE NR 4 ENGINE EXPERIENCED EGT RISE AND POWER WAS REDUCED TO KEEP WITHIN LIMITS. DURING CLIMB THE FAULT LIGHT CAME ON INDICATING IN THE 8 TO 10 RANGE. THE NACELLE DETECTOR WAS SWITCHED TO 'B' AND THE BELL AND LIGHT CAME ON. THE ENGINE WAS SHUTDOWN, THE FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT RETURNED TO MNL WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. THE CSD AND START VALVE WERE REPLACED DUE TO WIRING. THE FIRE BOTTLES, HIGH STAGE BLEED VALVE, CONTROLLER PRESSURE RELIEF VALVE, AND PRESSURE RELIEF PANEL WERE REPLACED. GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19950421006871995042100687NM 1995 4 21 9506162290 119950418A2820DWGAE7027072 HOSE BOEING727 727251 138408HNM NR 2 ENGINE LEAKING A NWAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL01290US 21378 DURING TAXI OUT, KEROSENE SMELL IN AFT CABIN. CAPTAIN REQUESTED CFR AND TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL FEED LINE LEAKING ABOVE APU EXHAUST SHROUD. REPLACED THE FUEL FEED HOSE. 2L73 4F A3WE 19950421006881995042100688WP 1995 4 21 9506179307 119950417A2720 PEDAL ADJUSTMENT DOUG DC9 DC982 3022082WP RUDDER LACK OF LUBE A NWAAC ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 GL01309RC 48088 FIRST OFFICER HAD NO RUDDER INPUT FOR STEERING ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. LUBED FIRST OFFICER'S RUDDER PEDAL ADJUSTMENT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421006891995042100689WP 1995 4 21 9506189860 119950418A2120 AIR DISTR DOUG DC9 DC951 3022051WP CABIN SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01769NC 47757 FLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN IMMEDIATELY AFTER TAKEOFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION. RAN BOTH ENGINES AT TAKEOFF AND CLIMB POWER SETTINGS FOR TWENTY MINUTES, NO PROBLEMS WERE FOUND. OPERATED BOTH AIR CONDITIONING PACKS WITH SAME RESULTS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421006901995042100690 1995 4 21 9506199937 419950418A344220671570153 RT UNIT DOUG DC9 DC931 3022065WP RADAR MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01908H 337794405 47517 RADAR FAILED TO PAINT, SWEEP, OR TEST EN ROUTE DTW-MSN. FLIGHT RETURNED TO DTW DUE TO THUNDERSTORMS AHEAD. REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421006911995042100691 1995 4 21 9506209959 419950418A3442 ANTENNA DOUG DC9 DC931 3022065WP RADAR FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01919RW 47162 RADAR WOULD NOT PAINT KNOWN WEATHER AFTER TAKEOFF (REGARDLESS IF STABILIZATION WAS ON OR OFF). FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RADAR ANTENNA, TRANSCEIVER, AND VERTICAL GYRO. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950421006921995042100692NM 1995 4 21 9506226613 119950413A5315 FLOORBEAM BOEING747 747251B 1384892NM FS 660 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, THE MAIN DECK FLOORBEAM WAS FOUND CORRODED ON THE UPPER SURFACE OF UPPER CHORD AT FS 660, LBL 56. MAXIMUM DEPTH OF CORROSION AFTER BLEND-OUT WAS BEYOND 50 PERCENT OF FLANGE THICKNESS AT SEVERAL AREAS. FLOORBEAM UPPER CHORD IS MADE OF .085 INCH 7075-T6511 EXTRUSION. MADE REPAIR PER EA 66-98000. 2L74 4F A20WE 19950421006931995042100693NM 1995 4 21 95UAL727032 119950404A2910106056326 HYD HOSE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 2 ENGINE RUPTURED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP297456U 21910 NR 1 AND 2 ENGINE 'A' SYS HYD LOW PRESS LIGHT ON INTERMITTENTLY. BOTH PUMPS WENT INOPERATIVE AND AIRCRAFT OPERATED FOR ONE HOUR WITHOUT FLUID FLOW. TURNED OFF BOTH PUMPS. REPLACED NR 2 ENGINE 'A' SYSTEM HYDRAULIC SUPPLY HOSE, NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS AND CASE DRAIN FILTERS. 2L73 4F4 F A3WE E2EA 19950421006941995042100694NM 1995 4 21 95UAL747022 119950418A2612 FIRE LOOP BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE OUT OF POSITION A UALAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP29153UA 20102 NR 4 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO FIRE WARNING INDICATION. DISCHARGED BOTH FIRE BOTTLES. UPPER FORWARD B-LOOP WIRE FOUND CHAFING AGAINST ENGINE CAUSING FALSE FIRE INDICATION. WIRE REPAIRED. 2L74 4F4 F A20WE E20EA 19950421006951995042100695NM 1995 4 21 95UAL747023 119950418A7120310U40317 AFT LOWER MOUNT BOEING747 747422 1384935NM PWA 4056 PW4056 NE ENGINE RUSTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29176UA220038842 24383 724366 DURING PERIODIC INSPECTION, THE AFT LOWER ENGINE MOUNT WAS FOUND COVERED WITH RUST. MOUNT REMOVED FROM ENGINE, REPLACED MOUNT. RUST WAS CAUSED BY THE LOSS OF THE PROTECTIVE COATING. MOUNT CLEANED WITH MILD STODDARD SOLVENT WHICH REMOVED MAJORITY OF THE SURFACE RUST. REMAINING RUST IS MAX OF 0.003 INCH DEEP AROUND BUSHING AREA AT BOTH ENDS. REMOVED REMAINING RUST WITH LOW PRESSURE GLASS BEAD BLAST AND REAPPLIED PROTECTIVE COATING. 2L74 4F4 FRTA20WE E24NE 19950421006961995042100696NM 1995 4 21 95UAL747024 119950418A2612 FIRE WARNING BOEING747 747422 1384935NM PWA 4056 PW4056 NE CARGO COMPT ACTIVATED A UALAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP29187UA 26876 CREW REPORTED, AFT CARGO FIRE WARNING INDICATION. FIRE BOTTLES DISCHARGED. FALSE ALARM ATTRIBUTED TO MOISTURE FROM HIGH MOISTURE CARGO BEING INGESTED INTO THE CARGO SMOKE DETECTION SYSTEM. 2L74 4F4 FRTA20WE E24NE 19950421006971995042100697SO 1995 4 21 COM11865 119950418A323112012347001 LATCH EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01256CA 120245 RT MLG INBD DOOR LATCH IS BROKEN. REPLACED LATCH ASSY. 2L72 4T RTA31SO 19950421006981995042100698SW 1995 4 21 COM20363 119950419A77102719158007 TQ INDICATOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01704CA129634022 AC704 RIGHT ENGINE TORQUE INDICATOR FAILED DURING TAKEOFF. REPLACED THE TORQUE INDICATOR. 1L72 4T A8SW 19950421006991995042100699EU 1995 4 21 COM31063 119950418A33506104781 EEL BATTERY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01158CA 340A158 EMERGENCY LIGHTS AT LT EMERG EXIT AND 5A, 7A ARE INOP. REPLACED BATTERY PACKS. 2L72 4T RTA52EU 19950421007001995042100700EA 1995 4 21 COM60455 119950418A32405010520 BRAKE ASSY CNDAIRCL600 CL6002B19 EA LT MLG LEAKING A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO01937CA1605 7044 LT MLG BRAKE ASSY LEAKING. REPLACED BRAKE ASSY. 2L72 4F RTA21EA 19950421007011995042100701NM 1995 4 21 DL72E951580 119950322A531365564412 STRINGER BOEING727 727247 138408FNM FS 950-1007 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 49810 DURING HMV, CORROSION WAS FOUND FROM STA 950F TO 1007, STR 29L AROUND FASTENER LOCATIONS ON THE UPPER SURFACE OF THE O/B SKIN ATTACH FLANGE. REPAIRED PER DL ERA 3012174-14. 2L73 4F A3WE 19950421007021995042100702NM 1995 4 21 DL72E951581 119950328A5320 TORQUE BOX BOEING727 727247 138408FNM FS 1273/1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11283WA 21485 49810 AT THE LETTER CHECK, THE RT TORQUE BOX UPPER TRANSVERSE BEAM AND SUPPORT ANGLE AT FS 1273 AND THE UPPER TRANSVERSE CHANNEL AT FS 1263 WERE FOUND CRACKED. REPAIRED PER DL ERA 301422-14. 2L73 4F A3WE 19950421007031995042100703NM 1995 4 21 DL72S951572 119950408A5313 STRINGER BOEING727 727232 1384082NM FLOODLIGHT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 AT HMV, FOUND STRINGER CRACKED AT FWD AND AFT SIDE OF L/E FLOODLIGHT HOUSING. DRILLED AND INSTALLED REPAIR PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19950421007041995042100704NM 1995 4 21 DL72S951573 119950408A5313 STRINGER BOEING727 727232 1384082NM RT FLOODLIGHT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 AT HMV, FOUND STRINGER CRACKED AT RT LE FLOODLIGHT HOUSING. FABRICATED AND DRILLED REPAIR PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950421007051995042100705NM 1995 4 21 DL72S951574 119950416A5412 FIREWALL BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 AT HMV, FOUND NR 2 FIREWALL UPPER LT SECTION CRACKED AT OVERLAP AT INLET DUCT. FABRICATED AND INSTALLED REPAIR PER SRM 54-10-3 PG 2. 2L73 4F A3WE 19950421007061995042100706NM 1995 4 21 DL72S951578 119950406A5320651841483 SIDEWALL BOEING727 727232 1384082NM FS 294.5-285.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11476DA 20753 49810 THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAS A 1 INCH CRACK BET STA 294.5 AND 285.5 APPROX AT WL 170. THE WEB AT THIS LOCATION IS 0.040 INCH THK 2024-T3 CLAD. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND STRAP WILL BE INSTALLED. REPAIRED PER DL ERA 301493-14AD. 2L73 4F A3WE 19950421007071995042100707NM 1995 4 21 DL72S951579 119950329A533065C139131 SKIN BOEING727 727232 1384082NM FS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 49810 CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT STA 950D PLUS 10 BETWEEN STR 28R AND 27R. A 1.625 INCH BY 3.125 INCH CUT OUT IN THE 0.150 INCH BONDED 2024-T3 CLAD SKIN WAS REQUIRED. AN EXTERNAL REPAIR DOUBLER AND TRIPLER WILL BE INSTALLED PER DL ERA 301441-14. 2L73 4F A3WE 19950421007081995042100708NM 1995 4 21 DL72S951582 119950328A53136554583164 STRINGER BOEING727 727232 1384082NM FS 1040-1052 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 49810 AT THE CV2 VISIT, THE SKIN ON THE LOWER O/B FUSELAGE STR 28R AT STA 1040 THROUGH STA 1052 WAS FOUND CORRODED. REPAIRED PER DL ERA 301444-14. 2L73 4F A3WE 19950421007091995042100709NM 1995 4 21 DL72S951583 119950328A533065545906 SKIN BOEING727 727232 1384082NM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 49810 AT CV2 VISIT, CORROSION WAS FOUND JUST AFT OF FS 700 BETWEEN S-28L AND S-28R. CORROSION REQUIRES A 12.5 INCH BY 3.25 INCH CUT OUT AT THIS AREA. REPAIRED SKIN PER DL ERA 301443-14AD. 2L73 4F A3WE 19950421007101995042100710NM 1995 4 21 DL72S951584 119950321A575465216024 ANTI-ICE DUCT BOEING727 727232 1384082NM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 49810 WHILE IN SHOP 380, THE NR 4 KRUEGER FLAP ANTI-ICE DUCT TORQUE TUBE WAS FOUND WITH TWO CRACKS EXTENDING FROM AN EXISTING CUT OUT LOCATED 22.5 INCH FROM THE I/B EDGE OF THE FLAP. REPAIRED PER DL ERA 270445-14. 2L73 4F A3WE 19950421007111995042100711NM 1995 4 21 DL72W951567 119950416A552265727842 SKIN BOEING727 727247 138408FNM RT ELEV DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 FOUND DURING SHOP INSP, RT ELEV UPPER I/B SURFACE DENTED. REPAIRED SKIN PER SRM 55-20-3. 2L73 4F A3WE 19950421007121995042100712NM 1995 4 21 DL72W951568 119950416A552265727842 SKIN BOEING727 727247 138408FNM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING SHOP INSP, AN ELONGATED HOLE WAS DISCOVERED IN THE 4TH ACCESS PANEL FROM O/B. REPAIRED PER SRM 55-10-3. DURING SHOP INSP, AN UNIDENTIFIED REPAIR WAS DISCOVERED ON THE LWR SKIN 12 INCHES FROM I/B END. REPAIRED PER SRM 55-20-3 FOR RIGHT ELEVATOR ASSEMBLY. 2L73 4F A3WE 19950421007131995042100713NM 1995 4 21 DL72W951586 119950417A5347 SEAT TRACK BOEING727 727247 138408FNM FS 1030-1136 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 AT HMV, RT INBD SEAT TRACK CORRODED STA 1030 TO 1136, RT OUTBD TRACK CORRODED AT FS 1090 TO 1136 AND RT GALLEY TRACK CORRODED FS 1070 TO 1136. REPLACED SECTIONS OF TRACK PER SRM 53-10-5. 2L73 4F A3WE 19950421007141995042100714NM 1995 4 21 DL757951599 119950417A5315 FLOORBEAM BOEING757 757232 1384965NM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 000008 AT HMV, THE CABIN FLOORBEAM UPPER CAP WAS FOUND TO BE CORRODED FROM LBL 10 TO 16. REPAIRED PER SRM 53-30-51 FIG 202. 2L72 4F RTA2NM 19950421007151995042100715NM 1995 4 21 DL757951600 119950417A5315 FLOORBEAM BOEING757 757232 1384965NM FS 760 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 000008 AT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 760 FROM LBL 15 TO RBL 15. THE CORROSION WAS REMOVED AT BL0 TO RBL 15 WITHIN LIMITS PER SRM 53-00-51 FIG 101. CORR REM AT LBL 5 TO BL 0 NOT IN EXCESS OF .040 DEPTH. REPAIR FABRICATED PER SRM 53-30-51 FIG 203. REPAIR INSTALLED PER ABOVE SRM. 2L72 4F RTA2NM 19950421007161995042100716NM 1995 4 21 DL76S951575 119950407A5754114T4111 TE WEDGE BOEING767 767332 1382001NM NR 1 LE SLAT DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11122DL 23436 49810 DURING LTR CHECK, THE NR 1 L/E SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROXIMATELY 5 INCHES IN DIAMETER AND IS LOCATED 75 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIRED PER DL ERA 270615-14AD. 2L72 4F RTA1NM 19950421007171995042100717WP 1995 4 21 DLL10951566 119950416A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 865 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 FOUND FLOORBEAM CORRODED AT FUS STN. 865 RBL 40, CORROSION FOUND AT INITIAL INSPECTION DURING HMV. MADE FLOORBEAM REPAIR PER SRM 53-21-00 FIG 823. 2L73 4F A23WE 19950421007181995042100718WP 1995 4 21 DLL10951587 119950417A53201513968102 THRESHOLD LKHEED1011 10113851 5265010WP R4 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 R4 DOOR LWR INNER THRESHOLD AFT CORNER FTG CORRODED. REPLACED CORNER FITTING PER SRM 51-10-05, SMALL PARTS REPLACEMENT. FOUND AT HMV. 2L73 4F A23WE 19950421007191995042100719WP 1995 4 21 DLL10951588 119950417A53201513965102 FITTING LKHEED1011 10113851 5265010WP R 4 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 R4 DOOR LWR INNER THRESHOLD FWD CORNER FTG CORRODED, FOUND DURING INITIAL INSPECTION AT HMV. REPLACED CORNER FITTING PER SRM 51-10-05. 2L73 4F A23WE 19950421007201995042100720WP 1995 4 21 DLL10951590 119950408A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 HEAVY CORROSION ON THE FS 901 FLOORBEAM IN FRONT OF THE CART STORAGE AREA AT THE NR 2 CROSS AISLE. TYPICAL PROBLEM AT OVERHAUL. REPAIRED PER SRM 53-21-00 FIG 823. 2L73 4F A23WE 19950421007211995042100721WP 1995 4 21 DLL10951593 119950413A5311 FRAME LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11715DA 193C1092 DURING SPECIAL INSPECTION, FUSELAGE MAIN FRAMES WERE FOUND CRACKED AT THE FOLLOWING LOCATIONS, RIGHT SIDE FS 589, 649, 669, 689, 1063, 1103, 1123, 1685, LEFT SIDE FS 509, 1003, 1103, 1183, 1303, 1323, 1343, 1383, 1605, 1645, 1665. ALL CRACKS WERE AT WL 280. THESE WERE FOUND AS A RESULT OF A SPECIAL INSPECTION SET UP FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER. THIS IS THE FIRST REPORTED CRACKING AT THESE LOCATIONS ON DALA AIRCRAFT. REPAIRS WERE PERFOMED PER DL ERA 270665. 2L73 4F A23WE 19950421007221995042100722WP 1995 4 21 DLL10951595 119950417A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11713DA 193C1089 000008 DURING SPECIAL INSPECTION, FOUND MAIN FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS, RIGHT SIDE FS 609, 649, 669, 689, 709, 749, 1625, 1685, 1705, LEFT SIDE FS 1605, 1645, 1685, 1705, 1745. ALL CRACKS WERE AT WL 280. THESE CRACKS WERE FOUND AS A RESULT OF SPECIAL INSPECTION OF DL AIRCRAFT WITH 22,000 CYCLES AND HIGHER. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT. REPAIRS WERE PERFORMED PER DL ERA 270686. 2L73 4F A23WE 19950421007231995042100723WP 1995 4 21 DLL10951596 119950413A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 AT HMV, FOUND MAIN FUSELAGE FRAMES CRACKED AT THE FOLLOWING LOCATIONS, RIGHT SIDE FS 649, 669, 680, 709, 729, 1685, 1705, THE LT SIDE, 1023, 1303, 1645, 1665, 1705. ALL CRACKS WERE AT WL 280. A SPECIAL INSPECITON FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER WAS SET UP. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT. 2L73 4F A23WE 19950421007241995042100724WP 1995 4 21 DLL10951597 119950418A5313LS11011 LONGERON LKHEED1011 10113851 5265010WP FS 1123-1143 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 DURING INITIAL INSPECTION FOR HMV, THE OUTBOARD FLOOR SUPPORT 'T' ANGLE WAS FOUND CRACKED AT FS 1123, 1143 RT. REPAIR PER SRM 53-21-00 FIG 825. 2L73 4F A23WE 19950421007251995042100725WP 1995 4 21 DLL13951594 119950414A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 DURING SPECIAL INSPECTION, CRACKS WERE FOUND IN MAIN FUSELAGE FRAMES AT RT SIDE FS 649, 669, AND 689. ALL CRACKS WERE AT WL 280. THESE CRACKS WERE FOUND AS A RESULT OF A SPECIAL INSPECTION FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT. REPAIRS WERE PERFORMED PER DL ERA 270665. 2L73 4F A23WE 19950421007261995042100726WP 1995 4 21 DLL13951606 119950417A382089481503 HOT WATER HEATER LKHEED1011 10113851 5265010WP AFT LAV MALFUNCTIONED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11783DL 193A1009 DURING CLIMB, FLIGHT ATTENDANT REPORTED SMOKE IN AFT LAVATORY. RETURNED TO DFW. FOUND LAV SINK OVERFLOWING WITH EXTREMELY HOT WATER DUE TO FAULTY WATER HEATER. REPLACED WATER HEATER OPERATION NORMAL. 2L73 4F A23WE 19950421007271995042100727WP 1995 4 21 DLL17951359 119950318A57551529102178 SKIN LKHEED1011 10113853 5265020WP NR 2 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND UNDERSIDE OF NR 2 SPOILER HAD GOUGES. REPAIRED PER SRM 57-52-00. ALSO, FOUND CORROSION AND CRACK ON LOWER SIDE JUST ABOVE SEAL. REPAIRED PER SRM 57-52-00. 2L73 4F A23WE 19950421007281995042100728WP 1995 4 21 DLL17951570 119950331A5311 FRAME LKHEED1011 10113853 5265020WP FS 923 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND FUSELAGE FRAME CORRODED, STA 923 BETWEEN STR 30 TO 31, AFT SIDE. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 53-12-00. 2L73 4F A23WE 19950421007291995042100729WP 1995 4 21 DLL17951571 119950325A5320 PANEL LKHEED1011 10113853 5265020WP FS 1542 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 AT HMV, FOUND PANEL CORRODED, C2 C/C 1542. DRILLED NEW PANEL, REPLACED PANEL PER SRM 53-24-00. 2L73 4F A23WE 19950421007301995042100730WP 1995 4 21 DLL17951577 119950323A53131554989 LONGERON LKHEED1011 10113853 5265020WP FS 1860 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 DURING HMV, THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT APPROX STA 1860 AND WL 328 WAS FOUND CRACKED IN THE RADIUS. THE CRACK EXTENDS FROM THE AFT END OF THE PART FWD APPROX 6 INCHES ALONG THE RADIUS. REPAIRED PER DL ERA 270462-14AD. 2L73 4F A23WE 19950421007311995042100731NM 1995 4 21 SCNA95058 119950417A2760BACC2A4B00283EG CONTROL CABLE BOEING727 727259 138408JNM RT SPOILER OUT OF LIMITS A SCNAK NONE J WARNING INDICATION ININSP/MAINT 1 GL15289SC 22475 SPOILERS 10 THROUGH 14 WOULD NOT COMPLETELY STOW. PERFORMED SPOILER PANEL DEFLECTION CHECK PER B727 MM PAGES 531-532-2917. FOUND CABLES OUT OF LIMITS. REMOVED AND REPLACED RIGHT HAND SPOILER CONTROL CABLES, IPC REFERENCE 27-10-0-2 FIGURE 2 PAGE 1 ITEMS 90 AND 130. ADJUSTED RIGHT WING SPOILER CONTROL SYSTEM WING CABLES AND ACTUATORS PER BMM CHAPTER 27-61-0 PAGE 513 A. OPS CHECK NORMAL. 2L73 4F A3WE 19950421007321995042100732CE 1995 4 21 95ZZZX1913 119950205A26122440915 FIRE LOOP BEECH 1900 1900D 1154162CE RT ENGINE BROKEN A MASAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SW0162ZV 3589 UE62 MTH - AIRCRAFT DEPARTED. ON CLIMB AT APPROXIMATELY 9,000 FEET, YELLOW LOOP ANN FLICKERED AND RED FIRE T-HANDLE ILLUMINATED. PILOT MADE PRECAUTIONARY RT ENGINE SHUT-DOWN AND RETURNED TO MTH. INSPECTION REVEALED RT ENG AFT FIRE LOOP BROKEN, VIBRATION CAUSED. 2L72 4T RTA24CE 19950421007361995042100736 1995 4 21 95ZZZX1917 319950311A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE LT/RT PROPELLERSSEPARATED A AMASAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SW01124YV534 UE124 TWO EACH PROP DE-ICE BOOTS ON RT PROP AND 1 EACH DE-ICE BOOT ON LEFT PROP. DE-ICE BOLTS SEPARATING FROM LEADING EDGE EROSION SHIELD DUE TO PAINT BENEATH SEPARATING FROM NICKEL TORSION SHIELD. SUGGEST IMPROVING INSTALLATION PROCEDURE FOR PAINT ON PROPS OR LEAVING PAINT OFF OF EROSION SHIELD. 2L72 4T RTA24CE 19950421007371995042100737EA 1995 4 21 95ZZZX1918 219950125A7230 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RIGHT FAILED A AMASAAE UNSCHED LANDING ENGINE SHUTDOWN AY FLAME/FIRE ENGINE STOPPAGE CRCRUISE 1 SW01158YV UC158 97316 DURING FLIGHT, CREW REPORTS A FLASH FROM RT ENGINE FOLLOWED BY FLAMES COMING OUT OF EXHAUST STACKS. RT ENGINE WAS THEN SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. AFTER FURTHER INVESTIGATION BY MAINTENANCE, RT ENGINE OIL FILTER WAS FOUND TO HAVE LARGE AMOUNTS OF METAL IN IT AND AXIAL COMPRESSOR WAS UNABLE TO TURN FREELY. 2L72 4T4 TRTA24CE E4EA 19950421007381995042100738SO 1995 4 21 95ZZZX1919 119950404A2434 BRUSH BENDIX 30E2041B GULSTMG1159 G1159 3953505SO DC GENERATOR WORN A AJJBAK NONE O OTHER ININSP/MAINT 1 EA01125WM 3 874 77 ONE DC GENERATOR FAILED IN-FLIGHT. MAINTENANCE PERSONNEL FOUND THE DC GENERATOR TO HAVE PREMATURE BUSH WEAR (75 PERCENT WORN). OVERHAULED BY A REPAIR STATION. CAUSE OF BRUSH WEAR NOT DETERMINED. BRUSH PART NUMBER NOT DETERMINED, SUSPECT DEFECTIVE BRUSHES OR IMPROPER INSTALLATION/OVERHAUL PROCEDURE. 2L72 4F RTA12EA 19950421007391995042100739SO 1995 4 21 95ZZZX1920 119950330A2434 BRUSH BENDIX 30E20111B GULSTMG1159 G1159 3953505SO DC GENERATOR WORN A ABQVAK NONE O OTHER ININSP/MAINT 1 EA01900DH 1511 111 BLACK STREAKS WERE NOTICED ON THE ENGINE COWLING BY MAINTENANCE PERSONNEL. FOUND THE DC GENERATOR TO HAVE PREMATURE BRUSH WEAR, WORN BEYOND LIMITS (NO WEAR MARK REMAINING - 100 PERCENT WORN). RECENT OVERHAUL BY REPAIR STATION, CAUSE OF WEAR NOT DETERMINED. BRUSH PART NUMBER NOT DETERMINED. SUSPECT DEFECTIVE BRUSH MATERIAL COMPOSITION OR IMPROPER INSTALLATION/MAINTENANCE OVERHAUL PROCEDURE. 2L72 4F RTA12EA 19950421007401995042100740SO 1995 4 21 95ZZZX1921 119950316A2434 BRUSH BENDIX 30E20111B GULSTMG1159 G1159 3953505SO DC GENERATOR WORN A ABQVAK NONE O OTHER ININSP/MAINT 1 EA01900DH R46E 111 BLACK STREAKS WERE NOTICED ON THE ENGINE COWLING BY MAINTENANCE PERSONNEL. FOUND THE D. C. GENERATOR TO HAVE PREMATURE BRUSH WEAR, WORN BEYOND LIMITS (NO WEAR MARK REMAINING - 100 PERCENT WORN). RECENT OVERHAUL BY REPAIR STATION. CAUSE OF BRUSH WEAR COULD NOT BE DETERMINED. BRUSH PART NUMBER NOT DETERMINED. SUSPECT DEFECTIVE BRUSH MATERIAL COMPOSITION OR IMPROPER INSTALLATION/MAINTENANCE OVERHAUL PROCEDURE. 2L72 4F RTA12EA 19950421007411995042100741WP 1995 4 21 95ZZZX1922 119950321A2612 CONNECTOR DOUG DC8 DC863F 302198FWP NR 2 ENGINE LOOSE A RRXAE ENGINE SHUTDOWN NL FALSE WARNING NO TEST DEDESCENT 1 WP15921R 46145 MOMENTARY FIRE WARNING ON NR 2 ENGINE. PULLED THROTTLE BACK. TESTED FIRE WARNING. NO TEST. SHUT NR 2 ENGINE DOWN. MAINTENANCE RE-SECURED NR 2 ENGINE FIRE WARNING LOOP CANNON PLUG. SYSTEM OPERATIONAL CHECKED GOOD. 2L74 4F 4A25 19950421007421995042100742WP 1995 4 21 95ZZZX1923 119950324A2612D5020 FIRE LOOP DOUG DC8 DC863F 302198FWP NR 2 ENGINE DEFECTIVE A RRXAE ENGINE SHUTDOWN NL FALSE WARNING NO TEST DEDESCENT 1 WP15921R 46145 KDAY/KDFW - FLT 022 - ON DESCENT INTO KDFW, GIT A FIRE WARNING ON NR 2 ENGINE. PULLED THROTTLE BACK TO FLIGHT IDLE, LIGHT WENT OUT, BUT BELL WOULD NOT TEST. SHUT ENGINE DOWN ON DESCENT. KDFW MAINTENANCE REPLACED NR 2 LOWER FIRE LOOP. LEAK CHECKED ALL PNEUMATIC DUCTS AND LINES FOR LEAKS. CHECKED ENGINE FOR CRACKS. FOUND LOWER LOOP DAMAGED BY ENGINE COWL-LOOP WOULD SHORT WHEN FLEXED. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950421007431995042100743WP 1995 4 21 95ZZZX1924 119950325A2612D502551114121 FIRE LOOPS DOUG DC8 DC863F 302198FWP NR 2 ENGINE DEFECTIVE A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15921R 46145 KDFW/KDAY - FLT 021 - HAD A FIRE WARNING ON NR 2 ENGINE AT TOP OF CLIMB WHEN REDUCING POWER TO CRUISE. WARNING WAS INTERMITTENT AND SHORT. KDAY MAINTEANNCE REPLACED UPPER FORWARD AND AFT FIRE LOOPS. REPAIRED TWO WIRES AND REPLACED CANNON PLUG ON AFT LOOP. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950421007441995042100744NM 1995 4 21 95ZZZX1925 119950405A282065B9301425 FUEL LINE BOEING747 747132 1384882NM NR 2 PYLON LEAKING A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23857FT 20246 JFK - DURING WALK-AROUND INSPECTION, FUEL WAS FOUND LEAKING FROM INBD SIDE OF NR 2 PYLON ABOVE ENGINE. REMOVED L/E GAP COVER PANEL. FOUND FUEL FEED TUBE LEAKING DUE TO A HOLE CHAFED IN TUBE BY THE PNEUMATIC DUCT CLAMP. REMOVED TUBE AND ACCOMPLISHED A TEMPORARY REPAIR IAW MM 20-11-05. LINE REINSTALLED AND PRESSURE CHECKED IAW 28-22-00. LINE WILL BE REPLACED WITHIN 250 HOURS PER MM. PNEUMATIC DUCT CLAMP HAD ROTATED AGAINST FUEL TUBE BECAUSE ANTI-ROTATION SPRINGS WERE MISSING FROM CLAMP. FCD ISSUED TO CHECK OTHER PYLONS FOR SIMILAR CONDITION. 2L74 4F A20WE 19950421007451995042100745SW 1995 4 21 95ZZZX1926 119950315A75006876294 LINE BELL 206 206B 1181511SW ENGINE BLEED CRACKED A ALGAO OTHER O OTHER CRCRUISE 1 SW032299U 3415 DURING NORMAL FLIGHT, NOTED THE TOT WAS HIGHER THAN NORMAL (45 DEGREES - 50 DEGREES). REPLACED CRACKED LINE FROM BLEED VALVE TO COMPRESSOR. 1G71 3U H2SW 19950421007471995042100747SO 1995 4 21 95ZZZX1928 219950401A8530538304 PUSHROD CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 1 POSITION BENT A FAHAA UNSCHED LANDING ERKVIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS CRCRUISE 1 SO1964PB 402CO528 242951R ON 4-1-95, A ZERO TIME OVERHAULED ENGINE WAS INSTALLED ON NR 1 POSITION. THE AIRCRAFT WAS TEST FLOWN FOR ENGINE INSTALLATION AND OPS CHECKED OKAY. THE AIRCRAFT WAS RELEASED FOR SERVICE. ON THE FIRST REVENUE FLIGHT TO TREASURE CAY, NR 1 ENGINE BEGAN RUNNING ROUGH AND LOSING OIL PRESSURE. THE AIRCRAFT DIVERTED TO FREEPORT AND LANDED. UPON INSPECTION OF THE ENGINE, NR 2 CYLINDER EXHAUST PUSHROD WAS FOUND BENT AND THE PUSHROD HOUSING WAS BROKEN CAUSING THE LOSS OF OIL. 1L72 3O3 O A7CE E8CE 19950421007481995042100748WP 1995 4 21 95ZZZX1929 119950409A32607000010101 SWITCH DOUG DC9 DC931 3022065WP RT MLG UPLOCK MALFUNCTIONED A VJ6AO OTHER J WARNING INDICATION CLCLIMB 1 SO11940VJ 47053 PBI/ATL - FLT 502 - RIGHT GEAR UNSAFE LIGHT ON AFTER GEAR RETRACTION, RIGHT GEAR FAILED UPLOCK CHECK; CYCLED GEAR, OPS CHECK OKAY, ALL GEAR INDICATION NORMAL. REMOVED AND REPLACED RIGHT MLG UPLOCK SWITCH PER MM 32-00. 2L72 4F A6WE 19950421007491995042100749WP 1995 4 21 95ZZZX1931 119950406A32601864 BULB DOUG DC9 DC932 3022066WP RT MLG FAILED A VJ6AO OTHER N FALSE WARNING CRCRUISE 1 SO11904VJ 47377 MSY/ATL - FLT 160 - RIGHT GEAR UNSAFE LIGHT ON WITH GEAR HANDLE UP. FOUND DEFECTIVE LAMP. RELAMPED, JACKED AND SWUNG GEAR. ALL OPERATIONS NORMAL PER MM 32-60. 2L72 4F A6WE 19950421007501995042100750WP 1995 4 21 95ZZZX1932 119950410A2130 CONTROL SYSTEM DOUG DC9 DC932 3022066WP CABIN PRESS MALFUNCTION A VJ6AAG UNSCHED LANDING O2 MASK DEPLOYED O OTHER CRCRUISE 1 SO11904VJ 47377 DFW/ATL - FLT 234 - HAD TO DIVERT TO MEM DUE TO CABIN DE-RESSURIZATION. AUTOPRESSURIZATION FAILED AND OXYGEN MASKS DEPLOYED, EXCEPT 4 AT ROWS 5C, D, AND E. REMOVED AND REPLACED OYGEN BOTTLE AND DROP-CHECKED OXYGEN MASKS. OPS CHECK OKAY, PLACED AUTOPRESS ON MEL. 2L72 4F A6WE 19950421007511995042100751WP 1995 4 21 95ZZZX1933 119950327A2133AYLG6475G ACTUATOR DOUG DC8 DC8F54 3021926WP OUTFLOW VALVE MOTOR INOP A FXLAAI UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CLCLIMB 1 SO19426FB6263220207 45667 MIA - AFTER TAKEOFF, COULD NOT PRESSURIZE AIRCRAFT. RETURNED TO MIAMI AND MADE LANDING WITHOUT INCIDENT. PERFORMED OVERWEIGHT INSPECTION. GROUND INSPECTION REVEALED DEFECTIVE OUTFLOW VALVE ACTUATOR. REPLACED ACTUATOR AND GROUND CHECKED OKAY. RETURNED AIRCRAFT TO SERVICE. 2L74 4F 4A25 19950421007521995042100752WP 1995 4 21 95ZZZX1934 119950405A7830 DOOR DOUG DC8 DC861 3021952WP LT ENG CASCADE OPEN A FXLAAJ UNSCHED LANDING DUMP FUEL F FLT CONT AFFECTED CLCLIMB 1 SO1929UA 41602 46159 WINDSOR LOCKS, CN - DURING CLIMB, HEARD BANG AND AIRCRAFT YAWED LEFT. DUMPED FUEL TO LANDING WEIGHT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. INSPECTION OF AIRCRAFT REVEALED NO DAMAGE. AFTER SHUT DOWN, NOTED LT CASCADE DOORS ON NR 1 ENGINE OPEN. RAN ENGINE AND OPS CHECKED OKAY. DEACTIVATED THRUST REVERSER AS PRECAUTION PER MEL 78-5. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES, 22,038. 2L74 4F 4A25 19950421007531995042100753NE 1995 4 21 95ZZZX1935 219950406A7200 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 FAILED A RIAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SO19319EA322961846 193A1040 10338 KCLE/KLAS - FLT 605 - DURING CLIMB, NR 3 ENGINE HAD LOSS OF OIL PRESSURE/OIL QUANTITY. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO KCLE. AIRCRAFT WAS FERRIED TO MIAMI ON TWO ENGINES FOR ENGINE CHANGE. ENGINE ON SN 10120 TSN-34056 CSN-16394. AIRCRAFT TAT-45426.32, TAC-21603. 2L73 4F4 F A23WE E12EU 19950421007541995042100754NM 1995 4 21 95ZZZX1936 119950404A3610 PNEUMATIC SYSTEM BOEING707 707321C 138367BNM ACFT BAY LEAK A MAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL09722GS 19373 KFLL/KFLL - FLT 0X0 931 - UNABLE TO PRESSURIZE AFTER TAKEOFF. RETURNED TO DEPARTURE POINT. FIXED PNEUMATIC LEAK IN AIRCRAFT BAY COMPARTMENT PERFORMED LEAK CHECK ON GROUND NORMAL IAW MM 21-0-0. 2L74 4F 4A26 19950421007551995042100755NM 1995 4 21 95ZZZX1937 119950407A29106517840409 LINE BOEING727 72722C 138400FNM NR 2 SPOILER HYDCRACKED A RYNAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 CE07429EX 19100 LOST A-SYSTEM HYDRAULICS IN-FLIGHT, ACCOMPLISHED MANUAL GEAR EXTENSION AND LANDED IN SAT WITHOUT FURTHER INCIDENT. FOUND NR 2 SPOILER RETURN LINE CRACKED. REPLACED LINE, A-SYSTEM FILTERS AND THE A-SYSTEM ENGINE PUMPS. 2L73 4F A3WE 19950421007561995042100756CE 1995 4 21 95ZZZX1938 119950301A575310116000144 FLAP BEECH 1900 1900C 1154161CE RT WING INBD CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV10814 UC137 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 2 INCH CRACK IN THE BOTTOM SKIN ALONG THE TRAILING EDGE BETWEEN THE THIRD AND FOURTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER. 2L72 4T RTA24CE 19950421007571995042100757CE 1995 4 21 95ZZZX1939 119950302A575310116000144 FLAP BEECH 1900 1900C 1154161CE RT WING INBD CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV10436 UC134 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 1 INCH CRACK IN THE UPPER SKIN DIRECTLY AFT OF THE AFT NACELLE FAIRING. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER. 2L72 4T RTA24CE 19950421007581995042100758CE 1995 4 21 95ZZZX1940 119950314A575310116000144 FLAP BEECH 1900 1900C 1154161CE RT WING INBD CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV11626 UC119 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A CRACK IN THE UPPER SKIN ALONG THE TRAILING EDGE APPROXIMATELY 26 INCHES OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER. 2L72 4T RTA24CE 19950421007591995042100759CE 1995 4 21 95ZZZX1941 119950318A575335165050259 FLAP BEECH 1900 1900C 1154161CE RT WING OUTBD CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0769ZR 11876 UC69 REPAIRED A 1 INCH CRACK IN LOWER SKIN ALONG TRAILING EDGE APPROXIMATELY 38 INCHES OUTBOARD FROM INBOARD END OF THE RIGHT OUTBOARD FLAP. REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER IAW TECH ORDER NR 1900-27-00-0001. 2L72 4T RTA24CE 19950421007601995042100760SW 1995 4 21 95ZZZX1942 119950327A324631418 WHEEL ASSY BFGOODRICH SWRNGNSA227 SA227AC 8780603SW NOSE GEAR OUT OF BALANCE A CHQAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA233115K AC586 PILOT RETURNED TO FIELD DUE TO VIBRATION AFTER GEAR RETRACTION. THE NOSE WHEEL ASSEMBLIES WERE REPLACED. A TEST FLIGHT WAS PERFORMED WITH ALL INDICATIONS NORMAL. 1L72 4T A8SW 19950421007611995042100761 1995 4 21 95ZZZX1943 419950405A25644600109 LIFE RAFT BOEING727 727231 1384079NM CABIN LOW PRESSURE A YAUAK NONE O OTHER ININSP/MAINT 1 SO03590CA I140 20098 DURING AN INSPECTION OF LIFE RAFT BOTTLE PRESSURES, THE RAFT LOCATED IN THE OVERHEAD AT RIGHT OVERWING EXIT WAS FOUND TO HAVE ONE BOTTLE WITH LOW PRESSURE. THE RAFT WAS REMOVED AND A SERVICEABLE RAFT WAS INSTALLED. 2L73 4F A3WE 19950421007621995042100762 1995 4 21 95ZZZX1944 419950307A22107003180901 COMPUTER BEECH 1900 1900C 1154161CE YAW DAMPER BURNED A AMASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW011568G UC58 AFTER TAKEOFF, CREW REPORTED SMOKE COMING INTO COCKPIT AND CIRCUIT BREAKER (YAW DAMPER SERVO) TRIPPED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED YAW DAMPER SYSTEM AND FOUND YAW DAMPER COMPUTER BURNED. SYSTEM WAS DISABLED AND DEFERRED. OPERATOR CONTROL NR SW01950572105855. 2L72 4T RTA24CE 19950421007631995042100763NE 1995 4 21 95ZZZX1945 219950409A7261 LINE DOUG DC8 DC8F54 3021926WP PWA JT3D JT3D3B 52039NE NR 3 ENGINE LOOSE A MAIAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL0943UA 45677 632952 MPTO/MPTO - FLT APW 615 - RETURNED TO PANAMA DUE TO LOSS OF OIL, NR 3 ENGINE. FOUND FEED OIL LINE LOOSE, TIGHTENED B-NUT -- OKAY. 2L74 4F4 F 4A25 1E8 19950421007641995042100764WP 1995 4 21 95ZZZX1946 119950410A3222 STRUT DOUG DC9 DC932 3022066WP NLG FLAT A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11909VJ 47322 RDU/ATL - FLT 299 - AIR RETURNED TO RDU DUE TO LANDING GEAR HANDLE WOULD NOT RETRACT, CABIN WOULD NOT PRESSURIZE AND NOSE WHEEL STEERING STILL WORKED. CYCLED GROUND CONTROL CIRCUIT BREAKERS, NO HELP. FOUND FLAT NOSE STRUT SERVICED PER MM 12. LANDING GEAR HANDLE OPS CHECK OKAY. 2L72 4F A6WE 19950421007651995042100765WP 1995 4 21 95ZZZX1947 119950331A32304647408 HOOK ASSY DOUG DC8 DC851 3021920WP LT MLG DRY LUBE A FXLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19507DC64764 45855 BOG - AFTER TAKEOFF, RECEIVED LEFT MLG UNSAFE LIGHT. RETURNED TO BOG. LANDED WITHOUT INCIDENT. INSPECTION REVEALED LT MLG UPLATCH STUCK IN UNLATCH POSITION. LUBRICATED UPLATCH, PERFORMED GEAR RETRACTION TEST AND FOUND OKAY. PERFORMED OVERWEIGHT LANDING INSPECTION. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES, 29,448. 2L74 4F 4A25 19950421007661995042100766WP 1995 4 21 95ZZZX1948 119950407A2910AN83310 ELBOW DOUG DC8 DC851 3021920WP NR 3 HYD PUMP CRACKED A FXLAO OTHER K FLUID LOSS DEDESCENT 1 SO19508DC60653 45935 MIAMI - ON DESCENT, EXPERIENCED LOSS OF HYDRAULIC FLUID AND PRESSURE, EXECUTED EMERGENCY CHECK LIST. LANDING MIA WITHOUT INCIDENT. INSPECTION FOUND ELBOW FITTING CRACKED AT NR 3 ENGINE DRIVEN PUMP. REPLACED FITTING, SERVICED SYSTEM, CHECKED OKAY ON RUN-UP. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES, 27,992. 2L74 4F 4A25 19950421007671995042100767WP 1995 4 21 95ZZZX1949 119950407A49303602310141 FUEL CONTROL DOUG DC9 DC932 3022066WP APU DEFECTIVE A VJ6AK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11918VV 47320 ATL/TPA - FLT 537 - FLIGHT CREW UPON STARTING APU, NOTICED A FUEL SMELL. PLACED APU ON MEL 49-1 SEQUENCY NR 1331 DUE TO INOPERATIVE FUEL CONTROL DIAPHRAGM. 2L72 4F A6WE 19950421007681995042100768SW 1995 4 21 95ZZZX1950 119950306A53112722093105 FRAME SWRNGNSA227 SA227AC 8780603SW FS 189.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728B MSP - DURING AN INSPECTION, MECHANICS REPAIRED A .500 INCH CRACK TO FUSELAGE FRAME AT FS 189.06 IAW FAC 53-9-20, REPAIR NR 20. 1L72 4T A8SW 19950421007691995042100769WP 1995 4 21 95ZZZX1951 119950404A2781H2021BN5N SWITCH DOUG DC9 DC932 3022066WP LT/RT SLAT MALFUNCTIONED A VJ6ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO11925VV 47397 ATL/SDF - FLT 350 - RETURNED TO THE GATE FOR A SLAT DISAGREEMENT LIGHT. REMOVED AND REPLACED LT AND RT SLAT DISAGREEMENT WITH, PN H20-21B-N5N. 2L72 4F A6WE 19950421007701995042100770CE 1995 4 21 95ZZZX1952 119950110A61201143890495 CONTROL CABLE BEECH 1900 1900D 1154162CE LT DROP CONTROL WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW0131YV UE31 WHILE PERFORMING DETAIL INSPECTION, LT PROP GOVERNOR CABLE WAS FOUND TO HAVE THE OUTER CABLE HOUSING WORN THROUGH EXPOSING THE INNER CABLE. CABLE WAS WORN THROUGH WHERE IT ATTACHES TO RETAINER CLIP PART NR RA1039C. CABLE WAS REMOVED AND REPLACED. 2L72 4T RTA24CE 19950421007711995042100771EU 1995 4 21 AALA950365 119950222A5320 SHEAR TIE FOKKERF28 F28MK0100 4990807EU STR 42 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071422J5684 11405 FORWARD CANTED (OBLIQUE) ANGLE SHEAR TIE CRACKED AT STR 42 AT FUSELAGE ATTACHMENT. CYCLES, 4734. (X) 2L72 4F RT 19950421007721995042100772NM 1995 4 21 AALA950493 119950321A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07383AN 26995 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 27 TO ROW 40 FOUND INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT 40 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950421007731995042100773WP 1995 4 21 AALA950535 119950327A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07594AA 53284 DFW - FLT 0594 - DURING DEPLANING, EMERGENCY EXIT FLOOR PATH LIGHTS ON RIGHT SIDE OF AIRCRAFT FOUND INOPERATIVE. REPAIRED WIRING IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP AFT SECTION. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F RTA6WE 19950421007741995042100774NM 1995 4 21 BJNA53001 119950308A3397 WIRE BOEING737 7372H4 138448CNM CABIN EEL BROKEN A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 EMERGENCY LIGHTING INOP, ROWS 1-6. REPAIRED BROKEN WIRE WITH BUTT SPLICE PER BSWP 20-30-22. SYSTEM OP CHECKED GOOD PER BMM 33-51-0. (X) 2L72 4F A16WE 19950421007751995042100775WP 1995 4 21 GRAA119531 119950314A2130 CONTROL SYSTEM DOUG DC9 DC915 3022036WP CABIN PRESS MALFUNCTION A GRAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 WP111064T 45778 CHEYENNE, WYOMING - ON CLIMB-OUT, AIRCRAFT HAD A CABIN PRESSURE LOSS. THE CABIN FAILED TO MAINTAIN PRESSURE AT 14,000 FEET. THE FLIGHT CREW LOCKED THE SYSTEM INTO MANUAL, THEN TRIED THE AUTOSYSTEM AGAIN ON DESCENT AND THE SYSTEM WORKED NORMALLY. THE AIRCRAFT RETURNED TO CHEYENNE, WITH NO FURTHER INCIDENTS. A CERTIFIED MECHANIC STORED ALL OF THE MASKS AND CHECKED THE DOORS WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. AT WENDOVER, MAINTENANCE OPERATED THE CABIN PRESSURE SYSTEM ON THE GROUND WITH NO DEFECTS NOTED. (X) 2L72 4F A6WE 19950421007761995042100776NM 1995 4 21 IXKA9500011 119950317A38301437051 MOTOR BOEING727 727225 1384077NM LEFT AFT LAV DEFECTIVE A IXKAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA25356PA PA079 20626 EWR - AFTER AN OVERNIGHT SERVICE, AIRCRAFT WAS TAXIING FROM HARD STAND TO GATE, SMOKE WAS COMING FROM LEFT AFT LAV. FOUND AFT LAV FLUSH MOTOR EMITTING SMOKE. REPLACED LAV FLUSH MOTOR, TIMER AND CIRCUIT BREAKER. TIMER, PN 2123M100, BREAKER, PN BACC18W5. (X) 2L73 4F A3WE 19950421007771995042100777NM 1995 4 21 IXKA9500012 119950323A3150655449923 AURAL WARN UNIT BOEING727 727225 1384077NM COCKPIT DEFECTIVE A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25352PA D01027 20616 PBI - FLT 54 - ON TAKEOFF, WHEELWELL LIGHT AND BELL CAME ON. RETURNED TO PBI. REMOVED AND REPLACED NOSE WHEELWELL FIRE LOOP AND AURAL WARNING CONTROL UNIT. FIRE WARNING TEST PERFORMED ON ALL ENGINES, WHEELWELL, FIRE WALL AND APU. ALL CHECKED GOOD. NLG WHEELWELL LOOP, PN 356802255. (X) 2L73 4F A3WE 19950421007781995042100778NM 1995 4 21 IXKA9500013 119950326A27821U109592 ACTUATOR BOEING727 727225 1384077NM NR 8 LE SLAT DEFECTIVE A IXKAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA258880Z 669BDFIN 21453 MCO - FLT 74 - AFTER TAKEOFF ON RETRACTION TO 2 DEGREES, NR 8 LEADING EDGE SLAT INDICATED IN-TRANSIT, THE FLAP POSITION INDICATOR WAS YELLOW. NR 8 LEADING EDGE DID NOT RETRACT. RETURNED TO MCO. REMOVED AND REPLACED NR 8 SLAT ACTUATOR PER MM 27-81-20. OPS CHECKED ACTUATOR PER MM 27-81-02. OPS CHECKED GOOD. LEAK CHECKED GOOD. (X) 2L73 4F A3WE 19950421007791995042100779NM 1995 4 21 IXKA9500014 119950324A323065571538 WALKING BEAM 651783012 BOEING727 727224 1384076NM MLG ASSY LT DEFECTIVE A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA2532719 199X 20388 FLT 9719 - AFTER TAKEOFF, LEFT GEAR AND DOOR LIGHT ON. RETURNED TO EWR. REMOVED AND REPLACED LEFT MLG WALKING BEAM ASSY IAW MM 32-32-2. PERFORMED MULTIPLE GEAR SWINGS IAW MM 32-10-0. ALL INDICATIONS SATISFACTORY. (X) 2L73 4F A3WE 19950421007801995042100780SW 1995 4 21 MALA954357 119950306A53112722093146 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728B MSP - DURING INSPECTION, MAINTENANCE REPAIRED A .500 INCH CRACK ON FUSELAGE FRAME, FS 174.24, IAW FAC SRM 53-90-20, REPAIR NR 20, AND SRM 51-00-00. (X) 1L72 4T A8SW 19950421007811995042100781NE 1995 4 21 MZZA9514 219950323A7200 ENGINE BOEING727 727224 1384076NM PWA JT8 JT8D15 52051NE NR 2 FAILED A MZZAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP1379743 22252 685535 GUM - FLT 976 - NR 2 ENGINE LOST OIL PRESSURE APPROXIMATELY 33 MINUTES OUT OF GUAM. ENGINE SHUT-DOWN PROCEDURE PERFORMED. ENGINE WINDMILL TIME 33 MINUTES, N1 18 PERCENT, N2 24 PERCENT, OIL PRESSURE 2 PSI, OIL PRESSURE AT TIME OF SHUT DOWN 5 PSI, OIL QUANTITY NORMAL. MAINTENANCE INSPECTED MAIN OIL FILTER ASSEMBLY AND FOUND METAL CHIP IN FILTER. REMOVED AND REPLACED ENGINE ASSEMBLY. (X) 2L73 4F4 F A3WE E2EA 19950421007821995042100782NE 1995 4 21 PLGA326951 219950326A7261J221P035 O-RING SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE LT ENGINE FAILED A PLGAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NE05747BA 340A148 DCA - ON CLIMB-OUT, LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. POWER REDUCED TO FLIGHT IDLE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT DIVERTED TO BWI LANDING WITHOUT INCIDENT WITH THE LT ENGINE AT FLIGHT IDLE. MAINTENANCE DISPATCHED TO THE AIRCRAFT AND FOUND AN O-RING IN THE AXIS O-RING IN THE AXIS BB SEAL HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE SEAL, PERFORMED THE REQUIRED GROUND RUNS AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T4 TRTA52EU E8NE 19950421007831995042100783NE 1995 4 21 USAA950357 219950403A75106553864800 DUCT BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE NR 1 ENG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19239US 22354 ORF - FLT 2271 - DURING CLIMB-OUT OF ORF, NR 1 ENGINE REVERSE LIGHT AND NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED DUCT ASSEMBLY AND REPAIRED WIRING IN WIRING BUNDLE 2198. ENGINE OPERATION AND LEAK CHECK SATISFACTORY. (W) 2L72 4F4 F A16WE E2EA 19950421007841995042100784NM 1995 4 21 WRLA95012 119950331A27104600030001 TENSION REG DOUG MD11 MD11F 3023600NM AILERON CONTROL DIRTY A WRLAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 EA27274WA 48633 ON TAXI OUT DURING FLIGHT CONTROL CHECK, CAPTAIN DID NOT GET PROPER INDICATION. FIRST OFFICER CONTROL WHEEL SEEMED TO DISENGAGE FROM FLIGHT CONTROLS. YOKES WOULD MOVE IN OPPOSITE DIRECTIONS WITH LITTLE RESISTANCE. AIRCRAFT RETURNED TO GATE. MAINTENANCE PERSONNEL CLEANED AILERON TENSION REGULATORS WITH DEGREASING AGENT IAW MM 27-11-01, AND PERFORMED FLIGHT CONTROL CHECK. YOKE MOVEMENT AND ALL AILERON INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950421007851995042100785NM 1995 4 21 WRLA95013 119950403A5270 DOOR WARNING DOUG MD11 MD11 3023602NM APU ILLUMINATED A WRLAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27275WA 48631 ON TAXI OUT, 'APU DOOR OPEN' LIGHT ILLUMINATED WHEN FLIGHT CREW ATTEMPTED APU SHUT DOWN. CAPTAIN ELECTED TO RETURN TO GATE. AFTER RETURN TO GATE AND SHUT DOWN OF NR 1 AND NR 3 ENGINE, APU DOOR CLOSED AND LIGHT EXTINGUISHED. MAINTENANCE PERSONNEL RECYCLED APU DOOR. OPS CHECK OKAY. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950421007861995042100786NM 1995 4 21 WRLA95014 119950404A2910DC6210CLK3SN CONNECTOR DOUG MD11 MD11 3023602NM NR 1 ENGINE LOOSE A WRLAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27271WA 48518 ON TAXI OUT, FLIGHT CREW NOTED HYDRAULIC SYSTEM TEST FAILED. MANUAL TEST PERFORMED BY FLIGHT CREW. NR 1 HYDRAULIC SYSTEM RIGHT PUMP WOULD NOT TURN OFF WHEN COMMANDED OFF. CAPTAIN ELECTED TO RETURN TO GATE. MAINTENANCE PERSONNEL INSPECTED AND FOUND NR 1 ENGINE LEFT HYDRAULIC PUMP PRESSURE TRANSMITTER CANNON PLUG LOOSE. PROPERLY TIGHTENED AND SECURED CANNON PLUG. GROUND RAN ENGINE HYDRAULIC SYSTEM. ALL CHECKS NORMAL. RTS TEST OF HYDRAULIC SYSTEM PASSED. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950421007871995042100787SO 1995 4 21 WTAA950124 119950319A5270MS250851 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A WTAAK NONE N FALSE WARNING CRCRUISE 1 WP17275UE 120058 FAT - CARGO DOOR WARNING LIGHT ILLUMINATED IN-FLIGHT. MAINTENANCE ADJUSTED CARGO DOOR MICROSWITCH AND PERFORMED OPERATIONAL CHECK OF SYSTEM. CARGO DOOR INDICATION SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950421007881995042100788NE 1995 4 21 AWXA9500153 219950405A7320 FUEL CONTROL BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE NR 1 ENGINE OUT OF ADJUST A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28307AW 24634 LAS-IND - FLT 280 - DURING CRUISE, THE NR 1 ENGINE THROTTLE HAD A THREE KNOB SPLIT. ACFT RETURNED TO LAS AND LANDED WITHOUT FURTHER PROBLEMS. MX PERFORMED OVERWEIGHT LANDING INSPECTION PER BMM 05 51 74 PG 201, NO FAULTS NOTED. MX TROUBLESHOOTING FOUND THE NR 1 ENGINE OUT OF TRIM. MX TRIMMED ENGINE PER BMM 71-00-01, OPS CHECK NORMAL. ACFT RETURNED TO SERVICE. (W) 2L72 4F4 FRTA16WE E2GL 19950421007891995042100789NM 1995 4 21 AWXA9500155 119950319A5320654587545 THRESHOLD BOEING737 73733A 1384673NM R1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW30225 23633 PHX - DURING C10 INSPECTION, FOUND R1 DOOR THRESHOLD CHORD CORRODED BEYOND CLEAN UP LIMITS. REMOVED AND REPLACED CHORD PER BOEING SRM 51-30-2. TOTAL CYCLES 18333. (W) 2L72 4F RTA16WE 19950421007901995042100790NM 1995 4 21 AWXA9500156 119950319A5245 DOOR BOEING737 73733A 1384673NM RT AC BAY DAMAGE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW30225 23633 PHX - DURING C10 INSPECTION, FOUND HOLE ON INNER SURFACE OF RT AC PACK DOOR. FOIL REPAIR INSTALLED PER ER 1 51 00 04. TOTAL CYCLES 18333. (W) 2L72 4F RTA16WE 19950421007911995042100791NM 1995 4 21 AWXA9500157 119950319A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28174AW30225 23633 PHX - DURING C10 INSPECTION, FOUND CORROSION AROUND FASTENER HOLES OF FLOORBEAM 328 LBL 48. INSTALLED REPAIR PER BOEING SRM 53-10-9 PG 29. TOTAL CYCLES 18333. (W) 2L72 4F RTA16WE 19950421007921995042100792NM 1995 4 21 AWXA9500159 119950320A53206939839 THRESHOLD BOEING737 737275 1384485NM R1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND R1 DOOR THRESHOLD CHORD CORRODED BEYOND LIMITS. FABRICATED NEW ANGLE PER BOEING DRAWING AND INSTALLED REPAIR PER BOEING SRM 51-30-2. (W) 2L72 4F A16WE 19950421007931995042100793NM 1995 4 21 AWXA9500160 119950320A5315 FLOORBEAM BOEING737 737275 1384485NM FS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CORROSION ON UPPER CAP OF FLOORBEAM, STA 328 RBL 12 TO R1 DOORWAY. INSTALLED NEW T-CAP PER BOEING STRUCTURAL REPAIR MANUAL 53-10-9 PG 29. (W) 2L72 4F A16WE 19950421007941995042100794NM 1995 4 21 AWXA9500161 119950320A5315 FLOORBEAM BOEING737 737275 1384485NM FS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20959 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CORROSION ON TOP CAP OF FLOORBEAM, STA 312 LBL 12 TO RBL 12. INSTALLED REPAIR PER BOEING STRUCTURAL REPAIR MANUAL 51 10 9. (W) 2L72 4F A16WE 19950421007951995042100795EU 1995 4 21 AWXA9500188 119950331A5270 DOOR WARNING AIRBUS320 A320231 3930325EU CARGO COMPT ACTIVATED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28636AW 098 FLT 845 - PHX-SEA - AIR TURNBACK DUE TO AFT CARGO DOOR OPEN INDICATION IN FLIGHT, PRESSURE OK. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. ECAM DOOR WARNING INDICATION WAS GREEN WHEN AIRCRAFT RETURNED TO GATE. AFT CARGO DOOR WAS CLOSED AND ALL LATCHES WERE IN GREEN. ECAM DOOR PAGE INDICATOR WAS PLACED ON MEL 52-70-01. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA28NM 19950421007961995042100796NM 1995 4 21 AWXA9500192 119950404A2932211C223209 PRESSURE SWITCH BOEING757 7572S7 1384962NM LT HYD MODULE FAILED A AWXAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP28901AW 23321 LAS-JFK - FLT 297 - AIR TURNBACK DUE TO LOSS OF LT HYDRAULIC SYSTEM FLUID, EICAS MESSAGE INDICATED FLUID LEVEL DROPPED TO .25. ACFT RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MX FOUND PRESSURE SWITCH ON LT HYDRAULIC MODULE IN LT PYLON DEFECTIVE. REMOVED AND REPLACED PRESSURE SWITCH. HYDRAULIC SYSTEM SERVICED, OPS AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. (W) 2L72 4F RTA2NM 19950421007971995042100797EU 1995 4 21 AWXA9500196 119950406A2410 IDG AIRBUS320 A320231 3930325EU NR 1 ENGINE REQ'D SERVICE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28632AW 81 CMH-DCA - FLT 266 - CREW RECEIVED MESSAGE FOR E1 IDG LOW OIL PRESSURE. CREW SHUT GEN OFF LINE AND RETURNED TO CMH WITHOUT FURTHER INCIDENT. MX FOUND IDG OIL LEVEL LOW AND RESERVICED TO PROPER LEVEL. NO EVIDENCE OF LEAK OR METAL. RAN ENGINE, FREQS, VOLTS AND TEMP, ALL IN GREEN BAND. ACFT RELEASED FOR SERVICE. (W) 2L72 4F RTA28NM 19950421007981995042100798NM 1995 4 21 AWXA9500197 119950405A52106517688 CHORD BOEING737 7372Q8 138448KNM BS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND L1 DOOR INNER CHORD CORRODED BEYOND CLEAN UP LIMITS AROUND SCREW HOLES, STATION 312 TO 340. REMOVED AND REPLACED CHORD PER SRM 51-10-1 AND 51-30-02. (W) 2L72 4F RTA16WE 19950421007991995042100799NM 1995 4 21 AWXA9500198 119950405A5210654587545 CHORD BOEING737 7372Q8 138448KNM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING SCHEDULED INSPECTION OF TASK C53-107-02, FOUND R1 DOOR INNER CHORD CORRODED BEYOND LIMITS, STATION 294 STR 17. REPLACED CHORD PER SRM 53-10-1 AND 51-30-2. (W) 2L72 4F RTA16WE 19950421008001995042100800NM 1995 4 21 AWXA9500199 119950405A5315 FLOOR BEAM BOEING737 7372Q8 138448KNM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND CORROSION BEYOND CLEAN UP LIMITS AROUND SCREW HOLES ON FLOOR BEAM, STATION 328 RBL 30 TO RBL 50. REPLACED DAMAGED TOP CAP SECTION OF FLOOR BEAM PER SRM 53-10-9, FIGURE 5. (W) 2L72 4F RTA16WE 19950421008011995042100801NM 1995 4 21 AWXA9500200 119950405A5315 FLOOR BEAM BOEING737 7372Q8 138448KNM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND CORROSION BEYOND CLEAN UP LIMITS AROUND SCREW HOLES ON FLOOR BEAM, STA 328 RBL 15 TO RBL 25. REPLACED TOP CAP AND SPLICE ANGLES PER SRM 53-10-9. (W) 2L72 4F RTA16WE 19950421008021995042100802NM 1995 4 21 AWXA9500201 119950405A5315 FLOOR BEAM BOEING737 7372Q8 138448KNM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING SCHEDULED INSPECTION OF TASK C53 107 02, FOUND TWO AREAS OF CORROSION THAT WERE BEYOND CLEAN UP LIMITS AROUND SCREW HOLES OF STATION 294 FLOOR BEAM, RBL 8 AND RBL 30. REMOVED DAMAGED AREAS OF FLOOR BEAM AND INSTALLED REPAIR TOP CAP AND ANGLES PER SRM 53-10-9. (W) 2L72 4F RTA16WE 19950421008031995042100803NM 1995 4 21 AWXA9500202 119950405A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 7 THROUGH 9. RECONNECTED WIRES AS REQUIRED, OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950421008041995042100804EU 1995 4 21 AWXA9500203 119950407A73311801802 FF TRANSMITTER AIRBUS320 A320231 3930325EU NR 2 ENGINE FAILED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28636AW 0154 098 FLT 651 - CMH-PHX - AIRCRAFT DIVERTED TO DEN DUE TO IN FLIGHT FUEL LEAK OF NR 2 ENGINE. FUEL FLOW ON NR 2 ENGINE WAS APPROXIMATELY 1000 PPH HIGHER THAN NR 1 ENGINE. VISUAL INSPECTION REVEALED A VAPOR TRAIL FROM NR 2 ENGINE. CONTRACT MX TROUBLESHOOTING FOUND BAD FUEL FLOW TRANSMITTER HELICOILS. REPLACED FUEL FLOW TRANSMITTER, OPEATIONAL AND LEAK CHECK NORMAL. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4F RTA28NM 19950421008051995042100805EU 1995 4 21 AWXA9500204 119950409A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW 082 PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT AFT BATTERY PACK FAILED EMERGENCY LIGHT TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950421008061995042100806NM 1995 4 21 AWXA9500205 119950410A215021L11 RETAINER BOEING737 737277 1384570NM A/C RELAY BROKEN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28180AW 22647 LAX-PHX - CREW UNABLE TO PRESSURIZE CABIN, AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. CONTRACT MX FOUND AIR CONDITIONING RELAY MODULE LOOSE DUE TO RETAINING FORK BROKEN OFF. MX RESEATED MODULE, INSTALLED NEW RETAINER AND OPERATIONALLY CHECKED SYSTEM. NO FAULTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4F RTA16WE 19950421008071995042100807NM 1995 4 21 AWXA9500206 119950412A5330 SKIN BOEING737 7372Q8 138448KNM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUT OUT. DAMAGE REPAIRED PER SRM 53-30-3, FIGURE 35. (W) 2L72 4F RTA16WE 19950421008081995042100808NM 1995 4 21 AWXA9500207 119950412A5330 SKIN BOEING737 7372Q8 138448KNM BS 370 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND SKIN CRACKED AT STATION 370 BL 0. DAMAGE REPAIRED PER EO 53-30-13. (W) 2L72 4F RTA16WE 19950421008091995042100809NM 1995 4 21 AWXA9500208 119950412A5330 SKIN BOEING737 7372Q8 138448KNM BS 344 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 DURING C12 INSPECTION, FOUND SKIN CRACKED AT R1 DOOR CUT OUT LOWR AFT CORNER. REPAIRED DAMAGE PER SRM 53-30-3, FIGURE 26. (W) 2L72 4F RTA16WE 19950421008101995042100810NM 1995 4 21 AWXA9500209 119950412A5320 INTERCOSTAL BOEING737 7372Q8 138448KNM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND INTERCOSTAL FORWARD OF STATION 294 LBL 12 CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 53-10-2 AND 51-30-2. (W) 2L72 4F RTA16WE 19950421008111995042100811NM 1995 4 21 AWXA9500210 119950412A5320 ANGLE BOEING737 7372Q8 138448KNM BS 300 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 DURING C12 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BEYOND CLEAN UP LIMITS. REMOVED, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2. (W) 2L72 4F RTA16WE 19950421008121995042100812NM 1995 4 21 AWXA9500211 119950412A532065528941 INTERCOSTAL BOEING737 7372Q8 138448KNM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND INTERCOSTAL BETWEEN STATION 540 BL0 TO LBL 24.75 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-2 AND 51-10-1. (W) 2L72 4F RTA16WE 19950421008131995042100813NM 1995 4 21 AWXA9500212 119950412A5320654580731 ANGLE BOEING737 7372Q8 138448KNM STATION 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND INTERCOSTAL ANGLE BETWEEN STATION 294.5 AND 303.9 CRACKED AT STRINGER 12R, 13R AND 14R. FABRICATED NEW ANGLES AND INSTALLED PER SRM 51-30-02. (W) 2L72 4F RTA16WE 19950421008141995042100814NM 1995 4 21 AWXA9500213 119950412A5320 PLATE BOEING737 7372Q8 138448KNM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28137AW 23148 PHX - DURING C12 INSPECTION, FOUND L1 DOOR FORWARD GIRT BAR ATTACH PLATE CORRODED. FABRICATED AND INSTALLED NEW PLATE PER SRM 51-10-1. (W) 2L72 4F RTA16WE 19950421008151995042100815EU 1995 4 21 RAIA950339 119950322A2121011260100 EXTRACT FAN AEROSPATR72 ATR72202 8680940EU FWD FUSE SHORTED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE 283 STL - ELECTRIC SMOKE INDICATION AND SMELL IN COCKPIT AND CABIN. MAINTENANCE REPLACED EXTRACT FAN. FURTHER INVESTIGATION REVEALED NO DEFECTS. (W) 2H72 4T RTA53EU 19950421008161995042100816EU 1995 4 21 RAIA950341 119950325A3350OL60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 199 STL - EMERGENCY LIGHT IN CABIN DOOR IS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (W) 2H72 4T RTA53EU 19950421008171995042100817EU 1995 4 21 RAIA950342 119950326A3350311701 EEL POWER SUPPLY BAG JETSTMJETSTM3201 1500217EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03433AM 885 STL - FLT 7087 - FWD TOP EMERGENCY LIGHT IS INOP. MAINTENANCE REPLACED FWD EMERGENCY LIGHT POWER SUPPLY. (W) 2L72 4T RTA56EU 19950428000011995042800001NM 1995 4 28 9506216613 119950418A5320 BRACKET BOEING747 747251B 1384892NM FS 1220 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, FOUND CRACKED SHEAR TIE BETWEEN STR 10R AND 11R, FS 1220. REMOVED CRACKED SHEAR TIE, FABRICATED REPAIR, AND INSTALLED. 2L74 4F A20WE 19950428000021995042800002WP 1995 4 28 9506231156 119950412A5330 SKIN DOUG DC10 DC1040 3023508WP DOOR 2L DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01156US 46765 DURING OVERNIGHT INSPECTION, FOUND FUSELAGE SKIN WAS TORN JUST FORWARD OF DOOR 2L. REMOVED DAMAGE AND REPAIRED PER EA 11-96714. 2L73 4F A22WE 19950428000031995042800003NM 1995 4 28 9506246305 119950420A5315 FLOOR BEAM BOEING747 747451 1384940NM FS 660 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE FLOOR BEAM SPLICE PLATE AT FS 660, LBL 5. REPLACED SPLICE PLATE. 2L74 4F RTA20WE 19950428000041995042800004NM 1995 4 28 9506255526 119950411A5315141N5113 FLOOR BEAM BOEING757 757251 1384970NM FS 377 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01526US 23620 23620 DURING PERIODIC CHECK, THE FS 377 FLOOR BEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-98175. 2L72 4F RTA2NM 19950428000051995042800005NM 1995 4 28 9506265526 119950411A5315141N5112 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01526US 25864 23620 DURING PERIODIC CHECK, THE FS 365 FLOOR BEAM UPPER CHORD WAS FOUND WITH TYPICAL CORROSION. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER NWA EA 55-98176. 2L72 4F RTA2NM 19950428000061995042800006NM 1995 4 28 9506276613 119950420A5753 CARRIAGE BOEING747 747251B 1384892NM TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, THE RIGHT INBOARD TRAILING EDGE FLAP NR 5 CARRIAGE THRUST BEARING BORE WAS FOUND CORRODED AND CRACKED. MACHINED CORROSION, COMPLETED HFEC, FLAP PEENED BORE, AND INSTALLED WET BUSHING, BORE TREATED AND PRIMED PER EA 66-97885. 2L74 4F A20WE 19950428000071995042800007NM 1995 4 28 9506286613 119950420A5315 FLOOR BEAM BOEING747 747251B 1384892NM FS 660 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, THE FLOOR BEAM AT FS 660, BL 0 WAS FOUND CORRODED. REPLACED FLOOR BEAM FROM RBL 56 TO LBL 47 AT FS 66 PER EA 66-98000. 2L74 4F A20WE 19950428000081995042800008WP 1995 4 28 9506291158 119950420A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1801 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FUSELAGE SKIN WAS FOUND DENTED AND GOUGED AT FS 1801, STR 2L TO 4L. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS. 2L73 4F A22WE 19950428000091995042800009NM 1995 4 28 9506306305 119950421A5315 FLOOR BEAM BOEING747 747451 1384940NM FS 720 DENTED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, FOUND THE FORWARD CARGO FLOOR BEAM DENTED AT FS 720, LBL 54. REPAIRED FLOOR BEAM PER DRAWING 6A-53-38129. 2L74 4F RTA20WE 19950428000101995042800010NM 1995 4 28 9506316305 119950421A5320 WEB BOEING747 747451 1384940NM FS 540 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, FOUND FORWARD CARGO COMPARTMENT WEB DAMAGED AT FS 540, RBL 50. REMOVED DAMAGE AND INSTALLED DOUBLER. 2L74 4F RTA20WE 19950428000111995042800011EU 1995 4 28 9506323219 119950420A291312652 PUMP AIRBUS320 A320211 3930320EU B HYD SYST MAKING METAL A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01319US1265212652 208 DURING CLIMBOUT FROM DTW, RECEIVED 'HYD B SYS LO PR' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND PRESSURE RETURNED TO 1750 PSI. DECISION WAS MADE TO RETURN TO DTW WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE BLUE HYDRAULIC SYSTEM CASE DRAIN FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950428000121995042800012SO 1995 4 28 BIER950010 119950421A7714640925 ADAPTER SHAFT PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360E 17025SO TACH DRIVE SHEARED A BIEAO OTHER O OTHER CRCRUISE 1 EA219211K 208 347670191 265924R TACH INDICATED 0 RPM BUT ENGINE RAN NORM. FOUND TACH DRIVE ADAPTER SHEARED AT ATTACH NUT. REMOVED AND REPL WITH NEW. 1L72 3O3 O A7SO E9CE 19950428000131995042800013NM 1995 4 28 DHL95724004 119950418A3260W16001270 WIRE BOEING727 727228 NM LT MLG DOOR BROKEN A TDHLAK NONE N FALSE WARNING LDLANDING 1 SO01724DH 19862 WHEN LANDING GEAR RETRACTED, LEFT HAND GEAR DOOR LIGHT DID NOT ILLUMINATE. AFTER RETRACTION, AMBER LIGHT CYCLED ON THEN OFF. WHEN LANDING GEAR EXTENDED, LEFT AMBER LIGHT DID NOT COME ON. AFTER EXTENSION WAS COMPLETE, LIGHT CYCLED ON THEN OFF. REPAIRED BROKEN WIRE AT SWITCH, IAW MM 20-10-00. 2L73 4F A3WE 19950428000141995042800014NM 1995 4 28 DL72K951635 119950419A3350900835A EEL BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11410DA 21222 ON PRE-FLIGHT CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19950428000151995042800015NM 1995 4 28 DL72S951618 119950414A5320 BEAM BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11540DA 22386 000008 THE RIGHT HAND TORQUE BOX FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED. THE ER/A WILL REPLACE THE DAMAGED PLACE IN ACCORDANCE WITH S/B 53-0129. 2L73 4F A3WE 19950428000161995042800016NM 1995 4 28 DL72S951619 119950413A532000678811 BEAM BOEING727 727232 1384082NM BS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 000008 THE BS 1273 FRAME BEAM AND I/B UPPER CHORD OF THE RT TORQUE BOX AT THE AIRSTAIR ACTUATOR FITTING WERE FOUND CRACKED. REPAIRED PER S/B 53-0129. DAMAGE FOUND AT LETTER CHECK. 2L73 4F A3WE 19950428000171995042800017NM 1995 4 28 DL72W951634 119950405A5315 FLOOR BEAM BOEING727 727247 138408FNM FS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 FLOOR BEAM CORRODED AT FS 400 FROM LBL 20 TO RBL 36. REPAIRED PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950428000181995042800018NM 1995 4 28 DL73S951641 119950419A2730654513210 COMPUTER BOEING737 737232 1384475NM E/E COMPT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11332DL 23104 ON CLIMBOUT HAD ELEV, FEEL DIFF. PRESSURE LITE ON. RETURNED DFW, REPLACED FEEL COMPUTER, FOR RETURN TO SERVICE. 2L72 4F RTA16WE 19950428000191995042800019NE 1995 4 28 DL76L951637 219950418A7200PW4060 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE DAMAGE A DALAO OTHER O OTHER ININSP/MAINT 1 SO11174DN19372 24802 724144 NR 2 ENGINE FAILED BORESCOPE INSPECTION, FOUND FIRST STAGE GUIDE VANE DAMAGE BEYOND LIMITS. REPLACED ENGINE FOR RETURN TO SERVICE. 2L72 4F4 FRTA1NM E24NE 19950428000201995042800020WP 1995 4 28 DLL10951609 119950419A5320 FITTING LKHEED1011 10113851 5265010WP FS 1043 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 HORIZONAL TRUSS MEMBER FS 1043 LT SIDE IS CRACKED IN TWO, FOUND DURING HMV INITIAL INSP. REPAIRED PER SRM 53-21-00, PG 861-863. 2L73 4F A23WE 19950428000211995042800021WP 1995 4 28 DLL10951610 119950419A5311 FORMER LKHEED1011 10113851 5265010WP FS 1383 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 FORMER CRACKED STA 1883 AT STRINGER 19, FOUND AT HMV. REPAIRED PER SRM 53-12-00 PG 823. 2L73 4F A23WE 19950428000221995042800022WP 1995 4 28 DLL10951638 119950418A77228DJ175LXKI TGT INDICATOR LKHEED1011 10113851 5265010WP NR 2 SMOKING A DALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11728DA 193C1173 DURING CRUISE, NR 2 TGT GAUGE BEGAN SMOKING IN FLIGHT. OFF FLAG APPEARED, PULLED CIRCUIT BREAKER, SMOKE STOPPED. LANDED IAD. REPLACED NR 2 TGT INDICATOR OPERATION NORMAL. 2L73 4F A23WE 19950428000231995042800023 1995 4 28 DLL10951639 419950418A2330RDAX5341M0D1 DECODER LKHEED1011 10113851 5265010WP MID GALLEY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11723DA 193C1150 ON TAXI IN AFTER LANDING, HAD HEAVY ELECTRICAL BURNING ODOR IN MID GALLEY AREA. FOUND FWD DECODER MID RT ROW ZONE C FAULTY. REPLACED DECODER OPERATION NORMAL. 2L73 4F A23WE 19950428000241995042800024WP 1995 4 28 DLL10951640 119950417A3610 DUCT LKHEED1011 10113851 5265010WP LOWER MID FUS BLOWN A DALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO11728DA 193C1173 ON TAKOFF ROLL HAD LOUD BANG MID CABIN AREA. RETURNED TO GATE, FOUND RUPTURED NR 3 ENGINE PNEUMATIC DUCT AT RT MID FUSELAGE AFT OF GALLEY SERVICE DOOR. REPLACED DUCT AND AS A PRECAUTION, REPLACED NR 3 OVERPRESSURE SHUTOFF VLV AND ENGINE ISOLATION VLV. OPERATION NORMAL. 2L73 4F A23WE 19950428000251995042800025NM 1995 4 28 DLM88951636 119950419A2910AS15408140327 HOSE DOUG MD88 MD88 3023688NM TAIL COMP FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11916DL 49591 DURING CRUISE, RT HYDRAULIC SYSTEM FAILED, PRESS WENT TO ZERO. FOUND RT EDP PRESSURE LINE RUPTURED. REPLACED LINE OPERATION NORMAL. 2L72 4F RTA6WE 19950428000261995042800026EU 1995 4 28 QXEA9500123 119950418A2560S9007 ASPIRATOR SWITLIK S130508 FOKKERF28 F28MK1000 4990808EU SLIDE FAILED A AQXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 1713 348 11107 PDX: ESCAPE SLIDE TO FULLY INFLATE DURING DEPLOYMENT TEST DURING ROUTINE SHOP VISIT. THE ASPIRATOR VALVE FAILED BECAUSE IT WAS COVERED WITH DUCT TAPE. WHEN THE TAPE WAS REMOVED THE VALVE WORKED NORMALLY. SLIDE SCHEDULED MAINTENANCE WAS PERFORMED AND TESTED AND THE SLIDE WAS REPACKED. THE AIR CARRIER THAT LAST REPACKED THE SLIDE WAS NOTIFIED OF THE DISCREPANCY. THE SLIDE WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19950428000271995042800027NM 1995 4 28 UPS202945 119950420A53102024T3 PRESS BOX BOEING727 727180C 138406GNM BS 740-758 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RT PRESSURE BOX AT BS 740-758. REPLACED PRESS BOX SKIN PER SRM 53-10-1, 51-20-1, 51-10-2. 2L73 4F A3WE 19950428000281995042800028NM 1995 4 28 UPS202946 119950420A5320653414422 EXPANSION LINK BOEING727 727180C 138406GNM BS 848-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 848-870 AND FITTING AT STA 870, WL 206. REPLACED LINK PER SRM 51-30-2. 2L73 4F A3WE 19950428000291995042800029NM 1995 4 28 UPS202947 119950420A5320654661110 SUPPORT BOEING727 727180C 138406GNM BS 848 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT STA 848, LBL 26. REPLACED SUPPORT PER SRM 51-10-6, 53-10-1, 51-30-2. 2L73 4F A3WE 19950428000301995042800030NM 1995 4 28 UPS202948 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 1 SPOILER PANEL DELAMINATED ON UPPER SURFACE AT I/B CORNER AND AT CENTER. REPAIRED SKIN WITH FIBERGLASS PER SRM 51-40-6. 2L73 4F A3WE 19950428000311995042800031NM 1995 4 28 UPS202949 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 7 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK MAINTENANCE FOUND NR 7 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD I/B UPPER EDGE. REPAIRED DAMAGE PER SRM 57-50-6. 2L73 4F A3WE 19950428000321995042800032NM 1995 4 28 UPS202950 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 6 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 6 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD I/B CORNER. REPAIRED DAMAGE PER SRM 57-50-6, 51-40-6. 2L73 4F A3WE 19950428000331995042800033NM 1995 4 28 UPS202951 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 5 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 5 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD O/B CORNER. REPAIRED DAMAGE PER SRM 57-50-6. 2L73 4F A3WE 19950428000341995042800034NM 1995 4 28 UPS202952 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 3 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 3 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD I/B CORNER. REPAIRED DAMAGE PER SRM 57-50-6. 2L73 4F A3WE 19950428000351995042800035NM 1995 4 28 UPS202953 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 13 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 13 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD I/B CORNER. REPAIRED DAMAGE PER SRM 57-50-6, 51-40-6. 2L73 4F A3WE 19950428000361995042800036NM 1995 4 28 UPS202954 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 10 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK,MAINTENANCE FOUND NR 10 SPOILER DELAMINATED ON UPPER SURFACE AT THE FORWARD O/B CORNER. REPAIRED DAMAGE PER SRM 57-50-6, 51-40-6. 2L73 4F A3WE 19950428000371995042800037NM 1995 4 28 UPS202955 119950420A5755 PANEL BOEING727 727180C 138406GNM NR 9 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 9 SPOILER DELAMINATED ON UPPER SURFACE AT THE I/B END. REPAIRED DAMAGE PER SRM 57-50-6, 51-40-6. 2L73 4F A3WE 19950428000381995042800038NM 1995 4 28 UPS202956 119950420A5753 SKIN BOEING727 727180C 138406GNM RT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND RIGHT WING I/B FORE FLAP HAS DELAMINATION AT THE I/B EDGE UPPER SURFACE. REPAIRED DAMAGE PER SRM 51-40-6. 2L73 4F A3WE 19950428000391995042800039NM 1995 4 28 UPS202957 119950420A5753 SKIN BOEING727 727180C 138406GNM RT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND RIGHT WING I/B FORE FLAP HAS DELAMINATION AT THE O/B EDGE UPPER SURFACE. REPAIRED DAMAGE PER SRM 51-40-6. 2L73 4F A3WE 19950428000401995042800040NM 1995 4 28 UPS202958 119950420A575465162261 FLANGE BOEING727 727180C 138406GNM NR 2 K FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP I/B LOWER BONDING JUMPER HAS CORROSION ON BULLNOSE FLANGE. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950428000411995042800041NM 1995 4 28 UPS202959 119950420A575465162261 RIB BOEING727 727180C 138406GNM NR 2 K FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP I/B LOWER BONDING JUMPER HAS CORROSION ON RIB. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950428000421995042800042NM 1995 4 28 UPS202960 119950420A575465162261 FLANGE BOEING727 727180C 138406GNM NR 2 K FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSION ON BULLNOSE FLANGE. REPLACED PER MM 27-81-01. 2L73 4F A3WE 19950428000431995042800043NM 1995 4 28 UPS202961 119950420A5315 FLOOR BEAM BOEING727 727180C 138406GNM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACKS ON BEAM AT BS 1183, LBL 8, WL 182. REPAIRED PER UPS EO B727-5311-0635. 2L73 4F A3WE 19950428000441995042800044NM 1995 4 28 UPS202962 119950420A5320 CREASE BEAM BOEING727 727180C 138406GNM BS 306-330 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF CREASE BEAM AT STA 306-330, RBL 55, WL 208. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. 2L73 4F A3WE 19950428000451995042800045NM 1995 4 28 UPS202963 119950420A5753 TE SKIN BOEING727 727180C 138406GNM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND RT WING I/B MID FLAP TRAILING EDGE WEDGE HAS DELAMINATION 62 INCHES FROM OUTBOARD END UPPER SURFACE. REPAIRED DAMAGE PER SRM 51-40-6. 2L73 4F A3WE 19950428000461995042800046NM 1995 4 28 UPS202967 119950418A551165956137 RIB BOEING727 72751C 1384015NM LT HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LT HORIZONTAL STAB, NR 4 T/E SUPPORT RIB ON LWR T/E BEAM AFT O/B ATTACH BOLT. REPLACED PER SRM 51-30-2, 51-10-2, MM 27-30-05. 2L73 4F A3WE 19950428000471995042800047NM 1995 4 28 UPS202968 119950418A5320661758866 CHORD BOEING727 72751C 1384015NM 25 G BEAM CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON 25 G-BEAM CHORD FILLER PLATE. REPLACED 25G BEAM PER SRM 53-10-8, 51-10-01, 51-10-02, 51-30-2, MM 51-20-121. 2L73 4F A3WE 19950428000481995042800048NM 1995 4 28 UPS202969 119950418A5751 SKIN BOEING727 72751C 1384015NM LT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON UPPER SKIN ON LT WING LWR O/B AILERON, O/B EDGE ON SKIN DOUBLER. REPAIRED PER SRM 57-50-05. 2L73 4F A3WE 19950428000491995042800049NM 1995 4 28 UPS202970 119950418A5751 SPAR BOEING727 72751C 1384015NM LT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON LT WING O/B AILERON, AFT SPAR. INSTALLED REPAIRED PER SRM 51-40-3, 57-50-2. 2L73 4F A3WE 19950428000501995042800050NM 1995 4 28 UPS202971 119950418A552265256391 SKIN BOEING727 72751C 1384015NM LT ELEVATOR OIL-CANNED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN 'C' CHECK, MAINTENANCE FOUND OIL-CANNED UPPER SKIN PANEL ON LT ELEVATOR, STA 173.2-209.96. REPLACED PER SRM 51-30-2, 51-80-7. 2L73 4F A3WE 19950428000511995042800051NM 1995 4 28 UPS202972 119950418A553069195321 CHORD BOEING727 727180C 138406GNM BS 1343 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD, LT SIDE, BS 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950428000521995042800052NM 1995 4 28 UPS202973 119950418A553069195322 CHORD BOEING727 727180C 138406GNM BS 1343 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD FTG, RT SIDE, BS 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950428000531995042800053NM 1995 4 28 UPS202974 119950418A5712 RIB BOEING727 727180C 138406GNM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT WING RIB UPPER CHORD AT LBL 70.5 TEE CLIP AND STRAP. INSTALLED REPAIR UPS EO B727-5710-1271. 2L73 4F A3WE 19950428000541995042800054NM 1995 4 28 UPS202975 119950418A5346652368723 RING CHORD BOEING727 727180C 138406GNM NR 2 ENGINE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RING CHORD ON NR 2 ENGINE AT BS 1352, AT EXISTING REPAIR. REPLACED PER UPS EO B727-7100-2729C. 2L73 4F A3WE 19950428000551995042800055NM 1995 4 28 UPS202976 119950418A5320 FITTING BOEING727 727180C 138406GNM BS 940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK ON FRAME FITTING AT THE FLOOR BEAM ATTACH FLANGE, BS 940, LT FWD SIDE. INSTALLED REPAIR PER UPS EO B727-5310-5596A. 2L73 4F A3WE 19950428000561995042800056NM 1995 4 28 UPS502977 119950419A5415311N52171 FUSE PIN BOEING757 75724APF 1384969NM NR 2 ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01409UP 23731 WHILE IN 'C' CHECK, MAINTENANCE PERFORMED INSPECTION OF FUSE PIN P/N 311N5217-1 PER SB 757-54A0019R5 ON P AND W AIRCRAFT. FOUND PIN TO BE CRACKED. REPLACED FUSE PIN PER UPS EO B757-5440-0431-H. 2L72 4F RTA2NM 19950428000571995042800057WP 1995 4 28 UPS802978 119950419A5312 J BEAM DOUG DC8 DC873F 302199FWP AFT PRESS BULK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01801UP 46101 WHILE IN 'B' CHECK, MAINTENANCE FOUND APPROX. 4 INCH CRACK ON NR 3 J-ANGLE, LWR RADIUS, AND APPROX. 4 INCH CRACK ON NR 4 J-ANGLE LWR RADIUS. ACCOMPLISHED UPS EO DC8-5310-6598B. 2L74 4F RT4A25 19950428000581995042800058CE 1995 4 28 95ZZZW549 119950323A6120 BETA SYSTEM BEECH 1900 1900C 1154161CE LT ENGINE OUT OF RIG A MASAA UNSCHED LANDING O OTHER CLCLIMB 1 SW01118YV UC118 AIRCRAFT LEFT PROP FEATHERED AT LIFT OFF AT DIA. RETURNED TO GATE WITHOUT INCIDENT FOUND BETA SYSTEM OUT TO RIG. FOUND BETA VALVE STICKING ALL THE WAY OUT. SUSPECT BETA CABLE WAS STRETCHED. RERIGGED BETA SYSTEM AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950428000591995042800059NM 1995 4 28 95ZZZW550 119950403A213032144464 HIGH STAGE VALVE BOEING737 7373Y0 1384671NM NR 1 ENG INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 1011 23747 FLT 66 - SNA-LAS - AIR TURNBACK, UNABLE TO PRESSURIZE A/C DURING TAKEOFF/CLIMB. A/C RETURNED TO SNA. A/C WAS MX FERRIED UNPRESSURIZED TO PHX. PHX MX RESEALED OUTFLOW VLV, REINSTALLED SEALED AROUND POTABLE WATER TANK DRAIN, AND RECONNECTED UPPER AND LOWER HALVES OF NOSE GEAR VIEWING PORT ASSY. MX ALSO REMOVED AND REPLACED FAN AIR VALVE TO BLEED REGULATOR LINE, NR 1 ENG BLEED AIR REG HIGH STAGE VLV, AND 490 DEGREE THERMOSTATIC SWITCH. COMPLIED WITH A/C BLEED DOWN TEST IAW MM 05-51-91, SYS TEST OK. PERFORMED OPS CK OF CABIN PRESS CONTROLLER PER MM 21-31-00, PAGE 201/205. OPS CHECK GOOD. POST INSTALLATION TEST ACCOMPLISHED PER MM 36-11-16, TEST OK. A/C RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950428000601995042800060NM 1995 4 28 95ZZZW551 119950403A21309750172006 THERMOSTATIC BOEING737 7373Y0 1384671NM NR 1 ENG INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 9437 23747 FLT 66 - SNA-LAS - AIR TURNBACK, UNABLE TO PRESSURIZE A/C DURING TAKEOFF/CLIMB. A/C RETURNED TO SNA. A/C WAS MX FERRIED UNPRESSURIZED TO PHX. PHX MX RESEALED OUTFLOW VLV, REINSTALLED SEALED AROUND POTABLE WATER TANK DRAIN, AND RECONNECTED UPPER AND LOWER HALVES OF NOSE GEAR VIEWING PORT ASSY. MX ALSO REMOVED AND REPLACED FAN AIR VALVE TO BLEED REGULATOR LINE, NR 1 ENG BLEED AIR REG HIGH STAGE VLV, AND 490 DEGREE THERMOSTATIC SWITCH. COMPLIED WITH A/C BLEED DOWN TEST IAW MM 05-51-91, SYS TEST OK. PERFORMED OPS CK OF CABIN PRESS CONTROLLER PER MM 21-31-00, PAGE 201/205. OPS CHECK GOOD. POST INSTALLATION TEST ACCOMPLISHED PER MM 36-11-16, TEST OK. A/C RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950428000611995042800061WP 1995 4 28 95ZZZW552 119950403A54005753054501 FOOT STOOL DOUG DC8 DC873F 302199FWP NR 2 PYLON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH 46123 DURING AD 93-21-08 PYLON FOOT STOOL FITTING INSPECTION, NR 2 POSITION WAS FOUND TO BE CRACKED APPROX .45 INCHES. STOP DRILLED PER DOUGLAS TELEX REINSPECTION WEEKLY PER SB 57-99. 2L74 4F RT4A25 19950428000621995042800062NM 1995 4 28 95ZZZW553 119950327A3350 EEL DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07924HA 105 FLT 3111 - LYH-DCA - DURING PREFLIGHT WALKAROUND, FOUND FIRST TWO EMERGENCY LIGHTS AT ROW 1 BURNED OUT. CLEANED CONNECTOR 3352-PS3, OPERATIONAL CHECK GOOD. (W) 2H72 4T RTA13NM 19950428000631995042800063NM 1995 4 28 95ZZZW554 119950330A3231 RETRACT MECH DHAV DHC8 DHC8102 2809003NM RT MLG MALFUNCTIONED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07920HA 084 FLT NR 3442 - TPA-JAX - AFTER TAKEOFF AND DURING GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR AMBER ADVISORY LIGHT ILLUMINATED. VISUAL INSPECTION CONFIRMED THE RIGHT MAIN GEAR FORWARD DOOR WAS OPEN. AIRCRAFT LANDED IN JAX WITHOUT INCIDENT. REGAPPED FORWARD DOOR ACTUATOR PROXIMITY SENSOR, CYCLED LANDING GEAR SEVERAL TIMES, OPERATIONAL CHECK GOOD. (W) 2H72 4T RTA13NM 19950428000641995042800064NM 1995 4 28 95ZZZW555 119950401A323282970018009 ACTUATOR DHAV DHC8 DHC8102 2809003NM RT MLG DOOR FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07920HA20924 205 084 FLT 3465 - MIA-MCO - AFTER TAKEOFF AND AFTER GEAR RETRACTION, THE RIGHT MAIN GEAR DOOR FAILED TO CLOSE. AIRCRAFT TURNED BACK AND LANDED IN MIA WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT FORWARD GEAR DOOR ACTUATOR. (W) 2H72 4T RTA13NM 19950428000651995042800065NM 1995 4 28 95ZZZW556 119950303A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM BAG COMPT FAILED A HNAAD RETURN TO BLOCK BJNSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 EA07980HA2659 0071W 376 FLT 3068 - CLT-LYH - ON TAXI OUT RECEIVED FALSE BAG BAY SMOKE WARNING, THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BAG BAY SMOKE DETECTORS. (W) 2H72 4T RTA13NM 19950428000661995042800066NM 1995 4 28 95ZZZW557 119950303A2611302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM BAG COMPT FAILED A HNAAD RETURN TO BLOCK BJNSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FALSE WARNING TXTAXI/GRND HDL 1 EA07980HA17117 31544 376 FLT 3068 - CLT-LYH - ON TAXI OUT RECEIVED FLASE BAG BAY SMOKE WARNING, THE CREW DECLARED AN EMERGENCY AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BAG BAY SMOKE DETECTORS. (W) 2H72 4T RTA13NM 19950428000671995042800067NM 1995 4 28 95ZZZW558 119950402A3240214665 BRAKE ASSY DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 EA07938HA9875 329 1159 152 FLT 3099 - MIA-JAX - LEFT BRAKE CHATTERS VIOLENTLY ON TAXI, RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. (W) 2H72 4T RTA13NM 19950428000681995042800068NM 1995 4 28 95ZZZW559 119950402A3240214665 BRAKE ASSY DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 EA07938HA10119636 0839 152 FLT 3099 - MIA-JAX - LEFT BRAKE CHATTERS VIOLENTLY ON TAXI, RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. (W) 2H72 4T RTA13NM 19950428000691995042800069NM 1995 4 28 95ZZZW560 119950323A33501317 BULB DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07934HA16863 139 FLT NR 3460 - MCO-MIA - DURING MORNING WALKAROUND, FOUND AFT CABIN CENTER AISLE OVERHEAD EMERGENCY WHITE DOWN LIGHT INOP. REMOVED AND REPLACED BULB. (W) 2H72 4T RTA13NM 19950428000701995042800070NM 1995 4 28 AWXA9500193 119950403A5230 SEAL BOEING737 7373Y0 1384671NM CARGO DOOR LOOSE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 23747 FLT 2806 - SNA-LAS - AIR TURNBACK, CREW UNABLE TO PRESSURIZE AIRCRAFT DURING TAKEOFF/CLIMB. AIRCRAFT RETURNED TO SNA AND LANDED WITHOUT FURTHER INCIDENT. CONTRACK MX FOUND A 24 INCH SEGMENT OF AFT CARGO DOOR SEAL PULLED LOOSE FROM ITS TRACK. REINSTALLED SEAL, PRESSURIZED AIRCRAFT USING THE APU AND/OR RT ENGINE BLEED, AND PERFORMED THE PRESSURIZATION CONTROL SYSTEM OPERATIONAL TEST. NO FURTHER FAULTS NOTED AT THIS TIME. SEAL TO BE INSPECTED AT LAS. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950428000711995042800071NM 1995 4 28 AWXA9500194 119950403A21301074922 BLEED AIR REG BOEING737 7373Y0 1384671NM NR 1 ENG INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 844 23747 FLT 66 - SNA-LAS - AIR TURNBACK, UNABLE TO PRESSURIZE A/C DURING TAKEOFF/CLIMB. A/C RETURNED TO SNA. A/C WAS MX FERRIED UNPRESSURIZED TO PHX. PHX MX RESEALED OUTFLOW VLV, REINSTALLED SEALED AROUND POTABLE WATER TANK DRAIN, AND RECONNECTED UPPER AND LOWER HALVES OF NOSE GEAR VIEWING PORT ASSY. MX ALSO REMOVED AND REPLACED FAN AIR VALVE TO BLEED REGULATOR LINE, NR 1 ENG BLEED AIR REG HIGH STAGE VLV, AND 490 DEGREE THERMOSTATIC SWITCH. COMPLIED WITH A/C BLEED DOWN TEST IAW MM 05-51-91, SYS TEST OK. PERFORMED OPS CK OF CABIN PRESS CONTROLLER PER MM 21-31-00, PAGE 201/205. OPS CHECK GOOD. POST INSTALLATION TEST ACCOMPLISHED PER MM 36-11-16, TEST OK. A/C RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950428000721995042800072SW 1995 4 28 BDHA9500006 119950316A2432IN4005 DIODE SWRNGNSA226 SA226TC 8780404SW LT BATTERY SHORTED A BDHAK NONE L NO TEST ININSP/MAINT 1 GL15327BA TC249 ON MAINTENANCE RUN, THE LEFT BATTERY DISCONNECT LIGHT WOULD STAY ILLUMINATED WHEN THE BATTERY SWITCH WAS TURNED ON. INSPECTION OF THE SYSTEM FOUND THE DIODE AT THE BATTERY RELAY SHORTED. THE SYSTEM WAS REPAIRED AND AIRCRAFT RELEASED. (W) 1L72 4T A8SW 19950428000731995042800073WP 1995 4 28 BDHA9500007 219950317A72108937421 CHIP DETECTOR SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE DIRTY A BDHAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 GL15328BA TC253 P54269 MSP - FLT 421 - LT ENGINE CHIP LIGHT ILLUMINATED WHILE TAXIING. AIRCRAFT RETURNED TO HANGER. THE CHIP DETECTOR WAS CLEANED AND PENALTY RUN PERFORMED. THE CHIP DETECTOR WAS REINSPECTED AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT WAS RELEASED. (W) 1L72 4T4 T A8SW E4WE 19950428000741995042800074SW 1995 4 28 BDHA950008 119950327A7714AG34 TACH GENERATOR SWRNGNSA226 SA226TC 8780404SW RT ENGINE MALFUNCTIONED A BDHAK NONE O OTHER ININSP/MAINT 1 GL15328BA 754 D33808 TC253 MSP - FLT 421 - WHILE PERFORMING ENGINE START THE IGNITION WAS INTERMITTENT FROM FOURTY TO FIFTY FIVE PERCENT. THE TACH GENERATOR SIGNAL WAS INTERRUPTING THE SPEED SWITCH POWER TO THE START CONTROL RELAYS. THE RPM INDICATION OPERATED NORMAL. THE TACH GENERATOR WAS REPLACED AND THE AIRCRAFT RELEASED. (W) 1L72 4T A8SW 19950428000751995042800075EU 1995 4 28 C2XA95CL053 119950330A5610NP1588011 WINDSHIELD AEROSPATR42 ATR42300 8680920EU LT COCKPIT BIRD STRIKE A C2XAK NONE C F.O.D. CRCRUISE 1 SW0916824 86H727210 166 FLT NR 3719 - PWM-EWR - CAPTIAN WINDSHIELD CRACKED BY BIRD STRIKE. EWR MAINTENANCE INSPECTED THE WINDSHIELD FOR THE PURPOSE OF A FERRY FLIGHT FROM EWR TO BTV FOR REPLACEMENT. BTV MAINTENANCE REMOVED AND REPLACED THE CAPTIANS WINDSHIELD IAW ATR-42 MAINTENANCE MANUAL JIC 56-11-00 RAI 10000-005. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950428000761995042800076 1995 4 28 C2XA95CL054 419950331A341845150560 ANGLE OF ATTACK AEROSPATR42 ATR42320 8680930EU RT FUSELAGE MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW094283612414 571 200 FLT NR 3724 - EWR- STICK PUSHER/SHAKER FAULT IN FLIGHT. AIR RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED RIGHT AOA PROBE. AIRCRAFT WENT ON A SATISFACTORY TEST FLIGHT AND RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950428000771995042800077NE 1995 4 28 C2XA95CL055 219950331A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT FAILED A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN JX WARNING INDICATION ENGINE FLAMEOUT CLCLIMB 1 SW0951726128687081 115188 120174 115188 FLT NR 3122 - LAN - LEFT ENGINE FAILED AT 6000 FEET ON CLIMB-OUT. DID NOT FEATHER WITH CONDITION LEVER, USED ELECTRIC FEATHER. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED IN LAN WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. AIRCRAFT RETURNED TO SERVICE ON 04/02/95. (W) 2L72 4T4 TRTA31SO E20NE 19950428000781995042800078SO 1995 4 28 C2XA95IA043 119950330A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950428000791995042800079SO 1995 4 28 C2XA95IA044 119950330A572012004350017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 3 AND NR 4 UPPER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950428000801995042800080SO 1995 4 28 C2XA95IA045 119950330A572012004350017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 2, NR 4 AND NR 5 UPPER AND LOWER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED REPLACED THE AFFECTED SUPPORTS. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950428000811995042800081SO 1995 4 28 C2XA95IA046 119950330A572012017057006 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0927707 120095 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950428000821995042800082SW 1995 4 28 MALA954358 119950306A53112722093106 FRAME SWRNGNSA227 SA227AC 8780603SW FS 144.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING AN INSPECTION IN MSP, MAINTENANCE REPAIRED A .250 INCH CRACK TO FUSELAGE FRAME P/N 27-22093-106, FS 144.24 IAW FAC ARP 53-20-9148, REV A AND LAR 95-MALA-072 AND SRM 51-00-00 STANDARD PRACTICES. (W) 1L72 4T A8SW 19950428000841995042800084NM 1995 4 28 MALA954361 119950305A33506104781 EEL BATT PACKS DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15827MA 331 FLT 3132 - DURING THE PREFLIGHT IN DTW, THE EMERGENCY LIGHTS WOULD ONLY ILLUMINATE INTERMITTENTLY. MAINTENANCE REPLACED THE BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428000851995042800085WP 1995 4 28 RAIA950338 219950324A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RIGHT SMOKING A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE03337TE7933 1833 929 66075 STL - FLT 7303 - AFTER LANDING NOTICED RIGHT ENGINE SMOKING VERY BAD AND OIL TEMPERATURE RAPIDLY CLIMBING. CREW SHUT DOWN ENGINE. MAINTENANCE REPLACED RT ENGINE. (W) 2L72 4T4 TRTA56EU E4WE 19950428000861995042800086SO 1995 4 28 RAIA950340 119950327A7920AE7079361 OIL LINE EMB 120 EMB120RT SO RT ENGINE CHAFED A RAIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03125AM12924 120017 BHM - FLT 7463 - RT ENGINE OIL PRESSURE DROPPED TO ZERO. CREW SHUT ENGINE DOWN PER EMERGENCY CHECKLIST AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT ENGINE OIL BYPASS LINE. GROUND RUNS REVEALED NO FURTHER LEAKS. ENGINE OIL WAS REPLENISHED. (W) 2L72 4T RTA31SO 19950428000871995042800087EU 1995 4 28 UF6A950306 119950325A2750M300D4A RELAY BAG ATP ATP EU TL FLAP FAILED A AUF6AD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CE03852AW8500 2021 FLT 5008 - AZO - FLAPS WOULD NOT MOVE FROM ZERO POSITION. MAINTENANCE REPLACED FLAP RELAY 'CG19'. (W) 2L72 4T RTA27NM 19950428000881995042800088WP 1995 4 28 USAA950311 119950307A5330 SKIN DOUG DC9 DC931 3022065WP BS 912-996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 912-996 SKIN PANEL 5919707 LONGERON 26R TO 26L SKIN PANEL 5911424 LONGERON 18R-26R. SPLICED IN 2 EACH SKIN PANELS PER USAIR EA 29955. (W) 2L72 4F A6WE 19950428000901995042800090WP 1995 4 28 USAA950314 119950228A5330 SKIN DOUG DC9 DC931 3022065WP BS 313-332 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR INSTALLED STATION 313-332 LONGERON 22-24 RIGHT. INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B. (W) 2L72 4F A6WE 19950428000911995042800091WP 1995 4 28 USAA950315 119950221A5347 TRACK DOUG DC9 DC931 3022065WP BS 897-965 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT INBOARD SEAT TRACK STATION 897 AND 965. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4E. (W) 2L72 4F A6WE 19950428000921995042800092WP 1995 4 28 USAA950316 119950208A5313 LONGERON DOUG DC9 DC931 3022065WP BS 465-484 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 30 AT SPLICE BETWEEN BELTFRAMES AT STATION 465 AND 484. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14. (W) 2L72 4F A6WE 19950428000931995042800093WP 1995 4 28 USAA950317 119950223A5313 LONGERON DOUG DC9 DC931 3022065WP BS 1038 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 14 LEFT STATION 1038. SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950428000941995042800094WP 1995 4 28 USAA950318 119950224A5400 ANGLE DOUG DC9 DC931 3022065WP BS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND ONE .5 INCH CRACK IN STATION 980 TOP PYLON TO FUSELAGE ATTACH ANGLE RT. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W) 2L72 4F A6WE 19950428000951995042800095WP 1995 4 28 USAA950319 119950223A5313 LONGERON DOUG DC9 DC931 3022065WP BS 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 200 LONGERON 3 LEFT. SPLICED IN SECTION OF LONGERON PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950428000961995042800096WP 1995 4 28 USAA950320 119950214A5347 SEAT TRACK DOUG DC9 DC931 3022065WP BS 896-965 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION STATION 896-965 LEFT OUTBOARD SEAT TRACK. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W) 2L72 4F A6WE 19950428000971995042800097WP 1995 4 28 USAA950321 119950215A5320 WEB DOUG DC9 DC931 3022065WP BS 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION RT LAV STATION 996 WEB. CLEANED CORROSION AND INSTALLED DOUBLER PER SRM 53-05 FIG 72. (W) 2L72 4F A6WE 19950428000981995042800098WP 1995 4 28 USAA950322 119950210A5347 SEAT TRACK DOUG DC9 DC931 3022065WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD END OF LEFT OUTBOARD SEAT TRACK STATION 200. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W) 2L72 4F A6WE 19950428000991995042800099WP 1995 4 28 USAA950323 119950216A5320 ANGLE DOUG DC9 DC931 3022065WP BS 1019 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND 2 INCH CRACK IN FUSELAGE EXT PYLON ATTACH ANGLE TOP RT PYLON STATION 1019. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W) 2L72 4F A6WE 19950428001001995042800100WP 1995 4 28 USAA950324 119950213A5220 CORNER STOP DOUG DC9 DC931 3022065WP LT EMER EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19946VJ70949 47026 PIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK LEFT FORWARD OVERWING EMERGENCY EXIT UPPER FORWARD CORNER DOOR STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (W) 2L72 4F A6WE 19950428001011995042800101CE 1995 4 28 95ZZZX1953 119950208A53111144200365 FRAME BEECH 1900 1900C 1154161CE AIR STAIR DOOR CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01130UE9482 UC130 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE FUSELAGE FRAME CRACKED AT THE POINT WHERE THE FIRST AIR DOOR SNUBBER BRACKET IS ATTACHED. REPAIRED FRAME IAW BEECH SRM 51-70-00, PAGE 52. 2L72 4T RTA24CE 19950428001021995042800102CE 1995 4 28 95ZZZX1954 119950210A7540131823E4M2480 EVA TUBING BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01123UE12592 UC123 SPW - AFTER TAKEOFF, CREW ELECTED AN AIR TURN-BACK WHEN THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPAIRED AND LEAK CHECKED THE EVA TUBING. 2L72 4T RTA24CE 19950428001031995042800103CE 1995 4 28 95ZZZX1955 119950218A3260 DOWNLOCK WIRE BEECH 1900 1900C 1154161CE RT MLG BROKEN A GLBAO OTHER J WARNING INDICATION APAPPROACH 1 CE0167UE UC67 MSP - CREW REPORTED THE RT MAIN GEAR UNSAFE INDICATION ILLUMINATED WHEN GEAR SELECTED DOWN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPAIRED A BROKEN WIRE AT THE DOWNLOCK SWITCH ON THE DRAG LEG. A GEAR SWING WAS SATISFACTORY. 2L72 4T RTA24CE 19950428001041995042800104EA 1995 4 28 95ZZZX1956 219950219A7532310687001 BLEED VALVE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE FAULTY A GLBAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 CE01130UE 1 3N328 UC130 PCE32372 MSP - ON APPROACH THE RT ENGINE STALLED, AFTER WHICH THE CREW SHUT DOWN AND SECURED THE ENGINE. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE COMPRESSOR BLEED VALVE. AFTER A SUCCESSFUL TEST FLIGHT, THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2L72 4T4 TRTA24CE E4EA 19950428001051995042800105CE 1995 4 28 95ZZZX1957 119950221A21301143641407 CIRCUIT BOARD BEECH 1900 1900D 1154162CE ENVIRON SYSTEM FAILED A GLBAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE0194UX 2345 860794 UE94 ISN - THE CREW ELECTED AN AIR TURN-BACK AFTER THE LEFT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE PC BOARD. RAN AIRCRAFT AND OPS CHECKED GOOD. 2L72 4T RTA24CE 19950428001061995042800106EA 1995 4 28 95ZZZX1958 219950223A73218061328 FUEL CONTROL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE OUT OF ADJUST A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01104GL 7966 1998693 UC104 SPI - CREW ELECTED AN AIR TURN-BACK AFTER TAKEOFF DUE TO LEFT ENGINE TORQUE SURGES OF PLUS OR MINUS 200 FEET/POUNDS. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE FUEL CONTROL UNIT. POWER RUNS WERE SATISFACTORY. 2L72 4T4 TRTA24CE E4EA 19950428001071995042800107CE 1995 4 28 95ZZZX1959 119950224A27501005240731 FLAP MOTOR BEECH 1900 1900C 1154161CE TE FLAP WORN A GLBAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE0155782 2580 5849 UC168 ESC - CREW REPORTED THE FLAP MOTOR RAN SLOW AND THEY SMELLED ELECTRICAL SMOKE IN THE COCKPIT. REPLACED FLAP MOTOR WHICH CHECKED GOOD. 2L72 4T RTA24CE 19950428001081995042800108CE 1995 4 28 95ZZZX1960 119950304A32341013841377 CONTROL HANDLE BEECH 1900 1900C 1154161CE LANDING GEAR SHORTED A GLBAO OTHER O OTHER APAPPROACH 1 CE01105GL 1614 047 UC105 MSP - CREW REPORTED THE LANDING GEAR WOULD BLOW THE CIRCUIT BREAKER WHEN SELECTED TO EXTEND. GEAR LOWERED MANUALLY AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED LANDING GEAR CONTROL HANDLE, THE CIRCUIT BREAKER, AND REPAIRED A BROKEN WIRE. 2L72 4T RTA24CE 19950428001091995042800109GL 1995 4 28 95ZZZX1961 319950305A6110 PROPELLER BEECH 1900 1900C 1154161CE HARTZLHCB4M HCB4M GL RT ENGINE DAMAGED A GLBAK NONE C F.O.D. TXTAXI/GRND HDL 1 CE01130UE 344 UC130 FW1179 MSP - DURING TAXI TO THE TERMINAL, THE RT PROPELLER CONTACTED A RAMP BAGGAGE CART. THE PROPELLER WAS CHANGED AND AS A PRECAUTION, ENGINE AND TRUSS WERE CHANGED. SMALL REPAIRS WERE ACCOMPLISHED TO THE FUSELAGE SKIN IAW THE BEECH SRM. 2L72 4T RTA24CE 6 CP56GL 19950428001101995042800110CE 1995 4 28 95ZZZX1962 119950316A754013182366M0260 EVA TUBING BEECH 1900 1900D 1154162CE LT BLEED SYSTEM SEPARATED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0194UX 2508 UE94 ISN - AFTER TAKEOFF, CREW ELECTED AN AIR TURN BACK WHEN THE LT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPAIRED THE SEPARATED EVA TUBING. FUNCTION CHECK OKAY. 2L72 4T RTA24CE 19950428001111995042800111CE 1995 4 28 95ZZZX1963 119950320A712011490363S TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01122GL3477 466 UC122 SPW - DURING SCHEDULED VISUAL INSPECTION REQUIRED BY AD 95-02-18 IAW BEECH SB 2255R6, AREA OF THE RT ENGINE TRUSS WAS FOUND CRACKED. REPLACED TRUSS WITH SERVICEABLE. 2L72 4T RTA24CE 19950428001121995042800112CE 1995 4 28 95ZZZX1964 119950321A553011440002437 SKIN BEECH 1900 1900C 1154161CE AFT FUSELAGE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01122GL12622 UC122 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND DORSAL FIN CRACKED ON LT SIDE AT REAR PRESSURE BULKHEAD ATTACH POINT. THE CRACK WAS BETWEEN TWO RIVET HOLES. INSTALLED REPAIR IAW BEECH 1900 SRM 51-70-00, PAGE 17. 2L72 4T RTA24CE 19950428001131995042800113CE 1995 4 28 95ZZZX1965 119950325A5542114630000147 TE SKIN BEECH 1900 1900C 1154161CE RUDDER CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0145GL 14759 UC45 SPW - DURING ROUTINE MAINTENANCE, RUDDER TRAILING EDGE FAIRING WAS FOUND CRACKED AND HAD SEVERAL WORKING RIVETS. THE CRACK WAS REPAIRED AND RIVETS WERE REPLACED IAW DER APPROVED FROM 8110-3. RUDDER BALANCE CHECKED AND RESINSTALLED. 2L72 4T RTA24CE 19950428001141995042800114 1995 4 28 95ZZZX1966 419950307A22107003180901 COMPUTER BEECH 1900 1900C 1154161CE YAW DAMPER BURNED A MASAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW011568G UC58 AFTER TAKEOFF, CREW REPORTED SMOKE COMING INTO COCKPIT AND CIRCUIT BREAKER (YAW DAMPER SERVO) TRIPPED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED YAW DAMPER SYSTEM AND FOUND YAW DAMPER COMPUTER BURNED. SYSTEM WAS DISABLED DEFERRED. 2L72 4T RTA24CE 19950428001151995042800115CE 1995 4 28 95ZZZX1967 119950328A7120 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143AM10499 UC143 RIGHT INBD FORWARD CRACK WAS FOUND DURING SCHEDULED MAINTENANCE AND REPAIRED BY WELDING PER TO 1900-71-20-0001, AND REPAIRED BY WELDING PER TO 1900-71-20-0001. 2L72 4T RTA24CE 19950428001161995042800116CE 1995 4 28 95ZZZX1968 119950301A575335165050259 END CAP BEECH 1900 1900C 1154161CE TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07160AM9610 556 UC160 ON SCHEDULED MAINTENANCE, A SMALL CRACK INBD END CAP, WAS FOUND 4 INCHES UP FROM T/E ON TOP OF FLAP. REPAIRED WITH PATCH. 2L72 4T RTA24CE 19950428001171995042800117CE 1995 4 28 95ZZZX1969 119950408A575310116000144 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143AM10590 723 UC143 ON SCHEDULED MAINTENANCE A 1.5 INCH CRACK LOCATED OUTBOARD OF FIFTH RIB ON BOTTOM OF FLAP, FORWARD OF SPAR. REPAIRED WITH A 3.5 INCH BY 2.0 INCH PATCH. 2L72 4T RTA24CE 19950428001181995042800118WP 1995 4 28 95ZZZX1970 119950403A275057511521 DRIVE LINK DOUG DC8 DC873F 302199FWP TE FLAPS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH 46123 DURING AD 88-10-07, FLAP DRIVE LINK INSPECTION FOUND RIGHT STA 97 LINK DRIVE CRACKED. 2L74 4F RT4A25 19950428001191995042800119WP 1995 4 28 BDHA9500005 219950308A7412103784003 IGNITION EXCITER SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE331* 01514WP RT ENGINE OPEN A BDHAK NONE O OTHER ININSP/MAINT 1 GL15328BA 447623 TC253 MSP - FLT 421 - RIGHT ENGINE WOULD NOT START WITH IGNITION LIGHT AND FUEL FLOW NORMAL. INSPECTION OF THE SYSTEM FOUND IGNITION EXCITER HAD FAILED. THE IGNITION EXCITER WAS REPLACED AND ENGINE START PERFORMED. THE AIRCRAFT WAS RELEASED. (X) 1L72 4T3 T A8SW E2WE 19950428001201995042800120 1995 4 28 C2XA95CL061 419950405A31606227711003 DISPLAY UNIT EMB 120 EMB120RT SO LT COCKPIT INTERMITTENT A C2XACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW09587331068710687 3589 120197 CLE/CLE - FLT 3136 - ABORTED TAKEOFF DUE TO THE CAPTAIN'S EADI AND EHSI INTERMITTENTLY FAILED ON TAKEOFF ROLL. CLE MAINTENANCE REMOVED AND REPLACED THE NR 1 DPU IAW EMB-120 MM 34-23-03. OPERATIONAL CHECKS WERE GOOD IAW EMB-120, MM 34-21-00. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428001211995042800121 1995 4 28 C2XA95CL063 419950408A34426227337001 RT UNIT EMB 120 EMB120RT SO AVIONICS BAY FAILED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW09127158503 580 120125 CLE/BUF - FLT 3202 - RADAR FAILED, GAVE FALSE RETURNS AND NO RETURNS WHEN IT SHOULD. MAINTENANCE REMOVED AND REPLACED RADAR RECEIVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428001221995042800122 1995 4 28 C2XA95CL064 419950408A34426227338002 RADAR CONTROL EMB 120 EMB120RT SO COCKPIT FAILED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW091271510736 1878 120125 CLE/BUF - FLT 3202 - RADAR FAILED, GAVE FALSE RETURNS AND NO RETURNS WHEN IT SHOULD. MAINTENANCE REMOVED AND REPLACED RADAR RECEIVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428001231995042800123SO 1995 4 28 C2XA95CL065 119950409A2622898052 FIRE EXTINGUISH EMB 120 EMB120RT SO COCKPIT CRACKED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW09167291195 V086251 120185 CLE/SYR - FLT 3180 - DURING FLIGHT, COCKPIT FIRE EXTINGUISHER DISCHARGED. AIRCRAFT DIVERTED TO ROC, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428001241995042800124SO 1995 4 28 C2XA95IA048 119950411A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915732 120195 IAH - DURING C-CHECK INSPECTION FOUND LEFT AFT SEAT TRACK CORRODED. MAINTENANCE INSPECTED TRACK AND FOUND IT OUT OF LIMITS, THE SEAT TRACK WAS REMOVED AND REPLACED IAW EMB 120 MM 53-01-05. TT - 8693.4. TC - 13,197. (X) 2L72 4T RTA31SO 19950428001251995042800125NM 1995 4 28 CAL950219 119950320A2997 WIRE BOEING737 7373T0 1384582NM HYD PUMP CHAFED A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0914307 23358 IAH - FLT 0501 - SYSTEM 'B' ELECTRIC PUMP LOW PRESSURE LIGHT ILLUMINATED AT CRUISE ALT ELEC PUMP FAILED AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ELECTRIC PUMP WIRE CHAFED. INSULATED WIRE AND REPOSITIONED, RESET PUMP OPS CKS GOOD. (X) 2L72 4F RTA16WE 19950428001261995042800126NM 1995 4 28 CAL950234 119950327A331065B475293 CAPACITOR BOEING747 747243B 1384830NM COCKPIT FAILED A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0933021 20520 NRT - FLT 0908 - SMOKE WAS OBSERVED IN THE COCKPIT SHORTLY AFTER TAKEOFF FROM NRT. THE AIRCRAFT WAS RETURNED TO NRT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BURNED OUT CAPACITOR ON THE A-6 CONTROL CARD IN THE MASTER DIM AND TEST MODULE. THE A-6 CONTROL CARD WAS REMOVED AND REPLACED. NO OTHER DEFECTS WERE FOUND. (X) 2L74 4F A20WE 19950428001271995042800127NM 1995 4 28 CAL950235 119950327A291065446913 HYD MODULE BOEING737 737217 1384464NM RT MLG INOPERATIVE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW091623215013 19886 MSY - FLT 1275 - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. THE GEAR WAS CYCLED AND RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED AGAIN WHEN THE GEAR HANDLE WAS PLACED IN THE OFF POSITION, BUT WENT OUT WHEN THE UP POSITION WAS SELECTED. MAINTENANCE REMOVED AND REPLACED THE RT MLG HYDRAULIC INSTALLATION MODULE. THE GEAR WAS CYCLED 15 TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. (X) 2L72 4F A16WE 19950428001281995042800128WP 1995 4 28 CAL950236 119950327A335041B004AD0763 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0983870 48056 ATL - FLT 1440 - TWO SECTIONS OF CABIN OVERHEAD EMERGENCY LIGHTING WOULD NOT ILLUMINATE IN THE TEST POSITION DURING A PRE-FLIGHT CHECK. THE NI-CAD BATTERIES AT ROWS 8 AND 22 WERE REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY LIGHTING WAS RESTORED. (X) 2L72 4F A6WE 19950428001291995042800129NM 1995 4 28 CAL950237 119950326A3260 RETRACT MECH BOEING737 7373T0 1384582NM LANDING GEAR LACK OF LUBE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0914325 23455 CLE - FLT 1483 - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF FROM CLE. THE GEAR WAS EXTENDED WITH ALL INDICATIONS NORMAL AND THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE INSPECTED THE NLG AND FOUND NO DEFECTS. ALL NLG FITTINGS WERE LUBRICATED AND SENSORS WERE CLEANED. THE NOSE GEAR WAS SWUNG THREE TIMES WITH OPERATION AND INDICATIONS CHECKING NORMAL. THE AIRCRAFT HAS COMPLETED OVER 15 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM. (X) 2L72 4F RTA16WE 19950428001311995042800131WP 1995 4 28 CAL950239 119950328A3260 TARGET DOUG DC9 DC982 3022082WP LT MLG OUT OF ADJUST A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW09809NY 49263 CLE - FLT 1473 - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. THE LIGHT EXTINGUISHED WHILE ON DESCENT. MAINTENANCE FOUND THE LT MLG UPLOCK SENSOR TARGET OUT OF ADJUSTMENT. THE TARGET/SENSOR WAS ADJUSTED PER MM 32-60-05 AND GEAR OPERATION AND INDICATIONS CHECK GOOD. (X) 2L72 4F A6WE 19950428001321995042800132NM 1995 4 28 CAL950252 119950404A3230656021132 ACCESSORY UNIT BOEING727 727232 1384082NM LANDING GEAR INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09277835555764828 20638 DEN - FLT 0759 - THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF FROM DEN. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE GEAR SEVERAL TIMES, BUT WERE UNABLE TO DUPLICATE THE FAILURE. THE LANDING GEAR ACCESSORY UNIT WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. (X) 2L73 4F A3WE 19950428001331995042800133NM 1995 4 28 CAL950253 119950404A4920360452426 COMBUSTOR UNIT BOEING737 737130 1384435NM APU INOPERATIVE A CALAK NONE JE WARNING INDICATION VIBRATION/BUFFET CRCRUISE 1 SW09142063022 723 19023 DTW - FLT 1851 - A RUMBLING NOISE FOLLOWED BY A SERIES OF BANGS WAS HEARD IN THE AFT SECTION OF AIRCRAFT WHILE IN FLIGHT. INSPECTION BY MAINTENANCE FOUND THAT THE NOISE WAS CAUSED BY SURGING OF THE APU. THE APU COMBUSTOR UNIT WAS FOUND AT FAULT. THE APU COMBUSTOR UNIT WAS REMOVED AND REPLACED. THE APU WAS RUN AND OPERATION WAS NORMAL WITH NO SURGING NOTED. (X) 2L72 4F A16WE 19950428001341995042800134NM 1995 4 28 CAL950254 119950401A5330 SKIN BOEING737 737130 1384435NM BS 188-253 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND CRACK INDICATIONS IN SKIN AT LEFT FS BS 188-253, WL 208.1 TO WL 234.35. THE CRACKS WERE APPROXIMATELY .50 INCH LONG. THE CRACKED AREAS OF SKIN WERE CUT OUT AND DOUBLERS AND FILLERS WERE INSTALLED IAW EA 5310-01188. (X) 2L72 4F A16WE 19950428001351995042800135NM 1995 4 28 CAL950255 119950401A5320 WEB BOEING737 737130 1384435NM NLG WW CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - THE NOSE WHEELWELL, RT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION INSIDE FASTENER HOLE. AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950428001361995042800136NM 1995 4 28 CAL950256 119950401A5320 WEB BOEING737 737130 1384435NM NLG WW CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - NOSE WHEELWELL, LEFT UPPER PANEL WEB, WAS FOUND BULGED AT FORWARD EDGE AND THERE WAS CORROSION ON UPPER SURFACE AND INSIDE FASTENER HOLES. AN INTECOSTAL WAS FABRICATED AND INSTALLED IAW SRM 54-10-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950428001371995042800137NM 1995 4 28 CAL950257 119950401A5320 ANGLE BOEING737 737130 1384435NM BS 440 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND CORROSION INSIDE WEB OF DOOR SILL ANGLE AND NUT PLATES AT STA 440, STR 25R. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND SRM 51-1-21A. (X) 2L72 4F A16WE 19950428001381995042800138NM 1995 4 28 CAL950258 119950401A5313 STRINGER BOEING737 737130 1384435NM BS 446 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND CORROSION ON STR 27R AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19950428001391995042800139NM 1995 4 28 CAL950259 119950401A5313 STRINGER BOEING737 737130 1384435NM FS 420-440 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND A 1 INCH CRACK IN STR 28R, LOCATED IN THE FORWARD PIT AT STA 420 - STA 440. THE DAMAGED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE INSTALLED IAW SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2. (X) 2L72 4F A16WE 19950428001401995042800140NM 1995 4 28 CAL950260 119950401A5320 ANGLE BOEING737 737130 1384435NM FS 333 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND A .50 INCH CRACK IN FRAME TO STRINGER ATTACH ANGLE AT STR 26R, STA 333. THE CRACKED ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND SRM 53-10-3. (X) 2L72 4F A16WE 19950428001411995042800141NM 1995 4 28 CAL950261 119950401A5320 INTERCOSTAL BOEING737 737130 1384435NM BS 984 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720465653 19021 GSO - INSPECTION FOUND A .50 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-0. (X) 2L72 4F A16WE 19950428001421995042800142WP 1995 4 28 CAL950262 119950406A3260 SENSOR DOUG DC9 DC982 3022082WP NLG OUT OF ADJUST A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0998876 49444 IAH - FLT 0458 - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. THE POSITION SENSOR ON THE NOSE GEAR DRAG BRACE WAS ADJUSTED PER MM 32-60-00, PAGE 218. THE AIRCRAFT HAS FLOWN OVER 15 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (X) 2L72 4F A6WE 19950428001431995042800143NE 1995 4 28 CAL950266 219950410A7250 T1 BLADE BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE NR 2 ENGINE FAILED A CALAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 SW0988770517661392 20839 674184 NAS - FLT 1901 - A LOUD BANG WAS HEARD AND THE NR 2 ENGINE EPR DROPPED TO ZERO WHILE CLIMBING THROUGH 1,100 FEET. FUEL WAS DUMPED AND ACFT RETURNED TO NAS WHERE IT LANDED WITHOUT INCIDENT. NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPLEMENT - INVESTIGATION REVEALED THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO LIBERATION OF A T1 BLADE. (X) 2L73 4F4 F A3WE E2EA 19950428001451995042800145CE 1995 4 28 SW019505853 119950317A3260 BRACKET BEECH 1900 1900C 1154161CE NLG BENT A MASAO OTHER N FALSE WARNING APAPPROACH 1 SW0177YV UC77 PIT - UPON FINAL, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWNLOCK INDICATION. MAINTENANCE REPAIRED DOWNLOCK ADJUSTMENT BRACKET AND RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19950428001461995042800146EA 1995 4 28 SW019505854 119950330A323010800311 UPLOCK HOOK DHAV DHC8 DHC8311 1386006EA LT MLG DIRTY A MASAO OTHER J WARNING INDICATION APAPPROACH 1 SW01432AW7765 286 DEN - ON APPROACH, LEFT MAIN GEAR DID NOT EXTEND WHEN SELECTED DOWN, CREW PUMPED GEAR DOWN AND LANDED WITHOUT INCIDENT. GEAR WAS THEN PINNED IN THE DOWN AND LOCKED POSITION AND GEAR PINS SECURED AND FERRIED DIRECT FROM DEN TO GJT FOR MAINTENANCE INSPECTION. MAINTENANCE PERFORMED INSPECTION OF LT MLG UPLOCK, CLEANED AND LUBRICATED, PERFORMED RETRACT AND EXTENSION OPERATIONAL CHECK IAW DHC-8-300 MM SYSTEM OPS CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19950428001471995042800147EU 1995 4 28 VTZA95123 119950409A2750TY175802A SELECT SWITCH JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27303UE 41015 ORF/IAD - FLT 6344 - DURING TAKEOFF AT 1520 HOURS ON 4-9-95. ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SOUNDING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. ALL ITEMS WERE CONFIRMED TO BE IN PROPER POSITION AND TAKEOFF WAS ATTEMPTED WITHOUT FURTHER INCIDENT. WHEN AIRCRAFT ARRIVED IN IAD, MAINTENANCE CLEANED THE FLAP SELECTOR SWITCH. OPS CHECKS GOOD. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428001481995042800148EU 1995 4 28 VTZA95124 219950425A73208974575 BYPASS VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG FUEL FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27470UE 814 IAD-HPN - FLT 6405 - ABORTED THE TAKEOFF, DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 021143 IAW MEL 76-2. MAINTENANCE LATER CLEARED DMI NR 02113 BY RUNNING ENGINE AND FOUND A FAULTY TTL BYPASS VALVE, AND REPLACED THE VALVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA56EU E4WE 19950428001491995042800149 1995 4 28 VTZA95125 419950408A3425703360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU NOSE ELEC BAY FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27310UE 41028 EWR/IAD - FLT 6422 - DURING TAKEOFF AT 930 HRS ON 4-8-95. ABORTED TAKEOFF DUE TO HEADING COMPARISON FLAG AND CAPTAINS' EADI LOST HEADING DISPLAY WITH HEADING FLAGS. MAINTENANCE REPLACED THE AHRS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428001501995042800150EU 1995 4 28 VTZA95126 119950403A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27310UE 41028 IAD/BWI - FLT 6181 - DURING TAKEOFF ROLL AT 0730 HRS ON 4-3-95, ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03335 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 03335 ON 4-8-95 BY REPLACING THE AFT BAGGAGE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428001511995042800151NM 1995 4 28 9506335533 119950422A4900GTCP331200ER APU BOEING757 757251 1384970NM AFT FUSELAGE FAILED A NWAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 GL01533US2565211018 24264 THE APU FAILED DURING CRUISE AND RESTART ATTEMPTS WERE UNSUCCESSFUL. THE RIGHT IDG WAS ON MEL, SO THE AIRCRAFT DIVERTED TO ATL. REPLACED THE RIGHT IDG, PERFORMED BITE ON APU, NO FAULTS WERE DETECTED. APU OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA2NM 19950428001521995042800152NM 1995 4 28 9506346729 119950419A323069B8035827 DNLOCK ACTUATOR BOEING747 747251F 1384898NM LT MLG LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01629US 22388 DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED, THE NR 4 HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. SECURED NR 4 HYDRAULIC SYSTEM AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING GEAR DOWNLOCK ACTUATOR. OPERATIONAL CHECK OK. 2L74 4F A20WE 19950428001531995042800153NM 1995 4 28 9506352282 119950418A315032EN144 SWTICH BOEING727 727251 138408HNM STABILIZER INOPERATIVE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01282US 21161 DURING APPLICATION OF TAKEOFF POWER, AURAL WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND UPPER STABILIZER SWITCH S532 DEFECTIVE. REPLACED SWITCH AND PERFORMED TAKEOFF WARNING TEST PROCEDURE, NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950428001541995042800154 1995 4 28 9506362711 419950419A3417HG480B13 ADC BOEING727 7272S7 138407ZNM EE COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED TOTAKEOFF 1 GL01715RC35303231 22019 DURING DEPARTURE CLIMB AT 1600 FEET, AUTO-PILOT SYSTEM DISCONNECTED WITH AIRCRAFT OUT OF TRIM AND UNCOMMANDED RUDDER INPUT. RETURNED TO MIA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 AIR DATA COMPUTER. OPERATIONAL CHECK NORMAL PER MM. 2L73 4F A3WE 19950428001551995042800155NM 1995 4 28 9506376718 119950422A29102680222M6 CONTROL MODULE BOEING747 747251F 1384898NM TE FLAPS LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01618US2804512124 21122 DURING APPROACH UPON FLAP EXTENSION, THE NR 1 HYDRAULIC QUANTITY DROPPED TO ZERO. SECURED NR 1 HYDRAULIC SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE TRAILING EDGE FLAP CONTROL MODULE. OPERATIONAL CHECK OK. 2L74 4F A20WE 19950428001561995042800156NM 1995 4 28 9506382291 119950420A213310328051 OUTFLOW VALVE BOEING727 727251 138408HNM AFT FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01291US4281055 21379 DURING CLIMB AT FL210, CABIN PRESSURIZATION STARTED A SLOW UNCONTROLLABLE ASCENT. UPON CABIN ALTITUDE REACHING 10,000 FEET, INITIATED AIRCRAFT DESCENT AND RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT OUTFLOW VALVE. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950428001571995042800157NM 1995 4 28 9506402284 119950420A21506075103 CONTROLLER BOEING727 727251 138408HNM E/E COMPARTMENT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01284US3304729108 21323 DURING APPLICATION OF POWER ON TAKEOFF ROLL, LOUD RUMBLE NOISE AND HIGH RATE OF CLIMB AND DESCENT ON PRESSURIZATION INDICATION. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE FOUND LEFT PACK 35 DEGREE VALVE INOPERATIVE CAUSING PACK TO ICE. REPLACED VALVE AND TEMPERATURE CONTROLLER. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950428001581995042800158WP 1995 4 28 ABXA9500368 119950421A3260313 BULB DOUG DC9 DC932 3022066WP LT MLG DEFECTIVE A ABXAO OTHER P NO WARNING INDICATION LDLANDING 1 GL23903AX 47427 LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE, RECYCLED GEAR AND FAILED AGAIN. WHILE TRYING TO GET BULBS OUT, ONE LIGHT ILLUMINATED. PUT GEAR DOWN, GOT NORMAL INDICATION BACKED UP WITH GROUND PROXIMITY SWITCH. FOUND BOTH LEFT MAIN LANDING GEAR SAFE BULBS HAD DEFECTIVE CONTACTS. RELAMPED, OPS CHECKED GOOD IAW GMM CHAPTER 6 SECTION 12-01 PAGE 37. 2L72 4F A6WE 19950428001591995042800159 1995 4 28 COM31064 419950420A3454MS33205 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU NR 1 NAV TRIPPED A COMAK NONE O OTHER UKUNKNOWN 1 SO01380CA 340A012 NR 1 NAV IS INOP. RESET TRIPPED BREAKER ON PILOTS C/B PANEL. 2L72 4T RTA52EU 19950428001601995042800160WP 1995 4 28 MWEA95174 119950418A3251 O-RING 39146255501 DOUG DC9 DC915 3022036WP NLG STEERING LEAKING A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL31500ME ASN048 45841 PILOT REPORTS DURING CLIMBOUT AT MKE, NOTICED RIGHT HYDRAULIC QUANTITY DECREASING AND RETURNED TO MKE. MAINTENANCE FOUND O-RING ON NOSE STEERING ACTUATOR LEAKING. REPLACED O-RING, CYCLED SEVERAL TIMES AND NO LEAKS NOTED. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950428001611995042800161WP 1995 4 28 MWEA95175 119950408A4910 APU GARRTT GTCP8598D DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31202ME P28137 47672 PILOT REPORTS, APU GIVES OFF LIGHT SMOKE INTO CABIN WITH AIR SUPPLY ON ONLY. SMOKE ALARMS ACTIVATED. MAINTENANCE DEFERRED APU UNTIL IT CAN BE REPLACED. RETURNED A/C TO SERVICE. NAPU REPLACED 4/20/95. 2L72 4F A6WE 19950428001621995042800162NM 1995 4 28 MWEA95176 119950420A25603952273501 GIRT BAR DOUG MD88 MD88 3023688NM GALLEY DOOR LACK OF LUBE A MWEAK NONE O OTHER UKUNKNOWN 1 GL31601ME 49762 AFT GALLEY SERVICE DOOR GIRT BAR DIFFICULT TO DISARM. LUBRICATED GIRT BAR RETAINER. A/C RETURNED TO SERVICE. 2L72 4F RTA6WE 19950428001631995042800163NM 1995 4 28 QXEA9500124 119950421A3231001A52800150001 DOOR LATCH DORNERDO32 DO328100 2996000NM NLG MALFUNCTIONED A QXEAK NONE O OTHER CLCLIMB 1 NM09339PH 3015 PDX - LOUD NOISE AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD. NOSE GEAR RIGHT FORWARD DOOR CAME UNLATCHED. LATCHED DOOR AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950428001641995042800164NM 1995 4 28 UPS203012 119950423A553065225512 CHANNEL BOEING727 727180C 138406GNM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL, BS 1342 RT. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950428001651995042800165NM 1995 4 28 UPS203013 119950423A5720 UPPER CHORD BOEING727 727180C 138406GNM BL 760.95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON UPPER CHORD, LT WING BL 760.95. INSTALLED REPAIR PER UPS EO B727-5710-1271E. 2L73 4F A3WE 19950428001661995042800166NM 1995 4 28 UPS203014 119950423A553065225511 CHANNEL BOEING727 727180C 138406GNM BS 1343 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL STA 1343 LT SIDE. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950428001671995042800167NM 1995 4 28 UPS203015 119950423A553065225514 CENTER CHANNEL BOEING727 727180C 138406GNM BS 1343 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01921UP 19874 WHILE IN NAPLES FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL STA 1343. REPLACED PER UPS EO B727-5530-4601. 2L73 4F A3WE 19950428001681995042800168NM 1995 4 28 UPS402979 119950423A5210 DOUBLER BOEING747 747123F NM PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK ON DOUBLER OF LWR HINGE ARM CUTOUT, ON MAIN RT MAIN ENTRY DOOR. INSTALLED REPAIR PER SB 747-52-2144. 2L74 4F A20WE 19950428001691995042800169NM 1995 4 28 UPS402980 119950423A5314 KEEL BEAM BOEING747 747123F NM BS 1241 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION RT WLG W/W BSTA 1241, CANTED PRESSURE DECK KEEL BEAM T-CHORD AT RBL 4, BETWEEN APU FUEL FEED CLOSE-OUT PANEL AND T-CHORD. INSTALLED REPAIR PER SRM 53-10-07. 2L74 4F A20WE 19950428001701995042800170NM 1995 4 28 UPS402981 119950423A5400 D-BEAM BOEING747 747123F NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN D-BEAM, FRONT SIDE, NR 3 PYLON. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-02. 2L74 4F A20WE 19950428001711995042800171NM 1995 4 28 UPS402982 119950423A5315 FLOORBEAM BOEING747 747123F NM BS 640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD, RBL 45, STA 760. INSTALLED REPAIR PER SRM 51-10-01, 53-10-07. 2L74 4F A20WE 19950428001721995042800172NM 1995 4 28 UPS402984 119950423A5314 KEEL BEAM BOEING747 747123F NM LT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION LT WLG, LWR SIDE OF CANTED PRESSURE DECK AND CORNER OF CENTER LINE KEEL BEAM WEB. INSTALLED REPAIR PER SRM 53-10-07. 2L74 4F A20WE 19950428001731995042800173NM 1995 4 28 UPS402985 119950423A5720 STIFFENER BOEING747 747123F NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION INSIDE RT WLG W/W STIFFENER RUNNING FROM STA 1241 TO 1255 ON CENTERLINE WEB. REPLACED PER SRM 51-30-02. 2L74 4F A20WE 19950428001741995042800174NM 1995 4 28 UPS402986 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK LBL 33, BS 880. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001751995042800175NM 1995 4 28 UPS402987 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 1496 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK HORIZONTAL FLANGE, RBL 75.92, BS 1496. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001761995042800176NM 1995 4 28 UPS402988 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 1440-1495 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK HORIZONTAL FLANGE, RBL 33.99, BS 1440 TO 1490 AND 1495. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001771995042800177NM 1995 4 28 UPS402989 119950423A5330 SKIN BOEING747 747123F NM BS 460 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK AT BS 460, RT BETWEEN STR 14E AND 16. INSTALLED REPAIR PER UPS EO B747-5330-0661C. 2L74 4F A20WE 19950428001781995042800178NM 1995 4 28 UPS402990 119950423A5315 FLOORBEAM BOEING747 747123F NM BS 520 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD, STA 520, LBL 11.33 TO LBL 55. REPLACED PER SRM 51-40-04. 2L74 4F A20WE 19950428001791995042800179NM 1995 4 28 UPS402991 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACKED FASTENR HOLE IN SEAT TRACK, STA 600, LBL 33.99. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001801995042800180NM 1995 4 28 UPS402992 119950423A5320 UPPER CHORD BOEING747 747123F NM BS 520 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD STA 520, LBL 33 TO 75. REPLACED PER SRM 51-30-02. 2L74 4F A20WE 19950428001811995042800181NM 1995 4 28 UPS402993 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK, STA 640, RBL 98. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001821995042800182NM 1995 4 28 UPS402994 119950423A5320 INTERCOSTAL BOEING747 747123F NM BS 1367 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL, BS 1367, LBL 11.33, AND LBL 33.99. REPLACED PER SRM 51-10-01. 2L74 4F A20WE 19950428001831995042800183NM 1995 4 28 UPS402995 119950423A5320 INTERCOSTAL BOEING747 747123F NM BS 1367 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL, BS 1367, LBL 11.33, AND RBL 11.33. REPLACED PER SRM 51-10-01. 2L74 4F A20WE 19950428001841995042800184NM 1995 4 28 UPS402996 119950423A5315 FLOORBEAM BOEING747 747123F NM BS 800 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 800, LBL 75 TO 80. INSTALLED REPAIR PER SRM 53-10-07. 2L74 4F A20WE 19950428001851995042800185NM 1995 4 28 UPS402997 119950423A5347 SEAT TRACK BOEING747 747123F NM BS 480-510 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 480 TO 510, LBL 98. REPLACED PER SRM 53-10-05. 2L74 4F A20WE 19950428001861995042800186NM 1995 4 28 UPS402998 119950423A5315 FLOORBEAM BOEING747 747123F NM BS 520 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND CRACK IN FLOORBEAM WEB BS 520, LBL 11 TO 33. INTSALLED REPAIR PER SRM 51-40-02. 2L74 4F A20WE 19950428001871995042800187NM 1995 4 28 UPS403017 119950422A3350 EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, THE TWO EMER LIGHTS ABOVE UPPER DECK CREW EMER DOOR EXIT INOP. REPLACED BATTERY PACK. 2L74 4F A20WE 19950428001881995042800188NM 1995 4 28 UPS403018 119950420A3350900814 EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, UPPER DECK CREW EMER EXIT DOOR SILL/SLIDE LIGHTS (2 EA) INOP. REPLACED BATTERY PACK, OPS CHECK OK. 2L74 4F A20WE 19950428001891995042800189NM 1995 4 28 UPS403019 119950422A3350S135610A EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, STAIRWELL EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK OK. 2L74 4F A20WE 19950428001901995042800190NM 1995 4 28 UPS403020 119950422A3350S1356B35 EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, LT UPPER DECK AISLE EMER LIGHT INOP. REPLACED EMER LIGHT ASSY, OPS CK OK. 2L74 4F A20WE 19950428001911995042800191NM 1995 4 28 UPS403021 119950422A3350 EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, EMER EXIT SIGN ABOVE CREW EMER DOOR EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CHECK OK. 2L74 4F A20WE 19950428001921995042800192NM 1995 4 28 UPS403022 119950422A3350S135610A EEL BATTERY PACK BOEING747 747SR46 NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01680UP 20923 MAINTENANCE REPORTED, EMER CEILING LIGHT, UPPER DECK MOST AFT INOP ON TEST. REPLACED BATTERY PACK, OPS CK OK. 2L74 4F A20WE 19950428001931995042800193WP 1995 4 28 UPS803016 119950421A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST CRCRUISE 1 SO01813UP 46059 PILOT REPORTED, EMERGENCY LIGHTS CAME ON IN FLIGHT, ALL ELECTRICAL SYS GOOD. COULD NOT TURN OFF LIGHTS WITH ARM /DISARM SWITCH. REPLACED EMERGENCY BATTERY PACK ASSY. 2L74 4F RT4A25 19950428002011995042800201NM 1995 4 28 95ZZZX1978 119950403A2436B003063 REGULATOR LAMAR PIPER PA60 PA60601P 7106012NM DC VOLTS FAILED A GXPAK NONE BM SMOKE/FUMES/ODORS/SPARKS OVER TEMP NRNOT REPORTED 1 GL23601GA 61P0282064 VOLTAGE REGULATOR FAILED CAUSING AN OVER-VOLT CONDITON WHICH RESULTED IN SEVERAL WIRES BEHIND THE INSTRUMENT PANEL OVERHEATING AND CREATING SMOKE IN THE COCKPIT. 1M72 3O RTA17WE 19950428002181995042800218NM 1995 4 28 95ZZZW561 119950311A552185520100102 RIB DHAV DHC8 DHC8102 2809003NM RT ELEV CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15866MA 366 DURING A SCHEDULED INSPECTION IN CKB, MAINTENANCE FOUND THE RIGHT ELEVATOR STATIC WICK FAIRING CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD SKIN PANEL, P/N 8550057-014 AND RIBS P/N'S 85520100-102 AND 855200028-102 IAW DEHAVILLAND SRM 51-40-00. (W) 2H72 4T RTA13NM 19950428002191995042800219NM 1995 4 28 95ZZZW562 119950311A5521855200028102 RIB DHAV DHC8 DHC8102 2809003NM RT ELEV CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15866MA 366 DURING A SCHEDULED INSPECTION IN CKB, MAINTENANCE FOUND THE RIGHT ELEVATOR STATIC WICK FAIRING CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD SKIN PANEL, P/N 8550057-014 AND RIBS P/N'S 85520100-102 AND 855200028-102 IAW DEHAVILLAND SRM 51-40-00. (W) 2H72 4T RTA13NM 19950428002201995042800220SW 1995 4 28 95ZZZW563 119950325A27302743042001 FITTING SWRNGNSA227 SA227AC 8780603SW RT ELEV WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B DURING A SCHEDULED INSPECTION IN MSP, MECHANICS FOUND THE ELEVATOR BELLCRANK ATTACH FITTING P/N 27-43042-001 SHOWING SIGNS OF WEAR AT RT ELEVATOR INNER BEARING ATTACH POINT. A REPAIR TO THE ELEVATOR AFT SPAR FITTING WAS COMPLETED BY REMOVING, DRILLING AND INSTALLING NEW FITTING IAW FAIRCHILD SRM 51-00-00 PAGE 4 FOR PART FOR PART REPLACEMENT, AND 51-40-05 FOR HI-LOCK INSTALLATION. 1L72 4T A8SW 19950428002211995042800221SW 1995 4 28 MALA954277 119950126A32503505051 SERVO VALVE SWRNGNSA227 SA227AC 8780603SW NLG STEERING FAILED A AMALAO OTHER O OTHER LDLANDING 1 GL15421MA AC634 FLT 3398 - DURING THE LANDING ROLL IN LEX, BELOW 90 KTS, THE AIRCRAFT VEERED TO THE RIGHT. MAINTENANCE REPLACED THE NOSE WHEEL STEERING SERVO. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002221995042800222SW 1995 4 28 MALA954356 119950301A53112720085 FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD FUSELAGE FRAME OF THE AFT CARGO DOOR (P/N 27-20085) AT FS 491 CRACKED AT THE GAS STRUT ATTACHMENT HOLE. COMPLETED REPAIR TO THE FRAME IAW FAIRCHILD ARP 53-20-9503 AND SRM. (W) 1L72 4T A8SW 19950428002231995042800223SW 1995 4 28 MALA954362 119950303A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG LACK OF LUBE A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15158MC AC762B FLT 3377 - ON APPROACH TO DTW, THE LEFT GEAR DOWN LIGHT DIDN'T ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR AND RECEIVED A NORMAL INDICATION. MAINTENANCE CLEANED AND LUBED THE GEAR DOWN SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002241995042800224NM 1995 4 28 MALA954363 119950303A552285520057103 SKIN DHAV DHC8 DHC8102 2809003NM LT ELEVATOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15802MA 245 DURING A SCHEDULED INSPECTION IN CKB, THE LEFT ELEVATOR INBOARD TRAILING EDGE SKIN CRACKED AND RIVETS PULLED THROUGH. ALSO, THE SPAR WS FOUND TO BE DAMAGED FROM LOOSE RIVETS. REPAIRS WERE COMPLETED BY REPLACING THE TRAILING EDGE SKIN, RIBS AND DOUBLERS, AND BY SPLICING THE SPAR IAW DEHAVILLAND RD8-55-232 DATED 28 FEB 95. (W) 2H72 4T RTA13NM 19950428002251995042800225SW 1995 4 28 MALA954364 119950308A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER O OTHER CLCLIMB 1 GL15439MA AC722 FLT 3298 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR BEGAN TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR THREE TIMES BEFORE THE GEAR REMAINED UP AND LOCKED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLIATE THE DISCREPANCY. MAINTENANCE ADJUSTED THE UPLIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950428002261995042800226SW 1995 4 28 MALA954365 119950303A53112720085 FRAME SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING ROUTINE MAINTENANCE IN MSP, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME CRACKED AT GAS STRUT MOUNT POST HOLE, FS 438. REPAIRS WERE COMPLETED PER FAC ARP 53-20-9503. (W) 1L72 4T A8SW 19950428002271995042800227SW 1995 4 28 MALA954367 119950309A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15428MA AC646 FLT 3355 - ON CLIMB-OUT FROM YXU, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO YXU. MAINTENANCE ADJUSTED THE NOSE GEAR UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002281995042800228NM 1995 4 28 MALA954368 119950309A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15831MA 339 FLT 3462 - ON APPROACH TO DTW, THE LEFT GEAR DID NOT SHOW DOWN AND LOCKED. THE CREW PERFORMED AN ALTERNATE GEAR EXTENSION AND LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428002291995042800229SW 1995 4 28 MALA954369 119950311A3260 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15422MA AC635 FLT 3235 - ON CLIMB-OUT FROM YQT, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW RECYCLED THE GEAR AND THE GEAR RETRACTED NORMALLY. MAINTENANCE ADJUSTED THE RIGGING OF THE NOSE LANDING GEAR UP LIMIT SWITCH AND RERIGGED THE NOSE LANDING GEAR DOORS AND THE RIGHT NOSE LANDING GEAR STRIKER ROD. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950428002301995042800230NM 1995 4 28 MALA954370 119950312A27207G773 PRESS SWITCH DHAV DHC8 DHC8102 2809003NM RUDDER FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15824MA 327 FLT 3130 - ON CLIMB-OUT FROM DTW, THE RUD FULL PRESS LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RUDDER FULL PRESSURE INDICATOR SWITCHES. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428002311995042800231EU 1995 4 28 MALA954371 119950313A33506008905 EEL BATTERY PACK FOKKERF27 F27MK200 4990620EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15278MA 10280 DURING ROUTINE MAINTENANCE IN CWA, MAINTENACNE FOUND THE RIGHT FORWARD EVACUATION LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T A817 19950428002321995042800232NM 1995 4 28 MALA954372 119950311A55228550057014 SKIN DHAV DHC8 DHC8102 2809003NM RT ELEV CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15866MA 366 DURING A SCHEDULED INSPECTION IN CKB, MAINTENANCE FOUND THE RIGHT ELEVATOR STATIC WICK FAIRING CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD SKIN PANEL, P/N 8550057-014 AND RIBS P/N'S 85520100-102 AND 855200028-102 IAW DEHAVILLAND SRM 51-40-00. (W) 2H72 4T RTA13NM 19950428002331995042800233SW 1995 4 28 MALA954373 119950311A52102790066111 DOOR CABLE SWRNGNSA227 SA227AC 8780603SW PAX DOOR FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15445MA AC687 FLT 3140 - ON CLIMB-OUT FROM DTW, THE AIRCRAFT WOULDN'T PRESSURIZE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND THE PASSENGER DOOR CABLE WEDGED BETWEEN THE DOOR AND THE FRAME. MAINTENANCE REPLACED THE FORWARD CABLE RETRACTOR ASSY. SYSTEMS OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002341995042800234SW 1995 4 28 MALA954374 119950313A32332752010003 ACTUATORS SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER O OTHER CRCRUISE 1 GL15422MA AC635 FLT 3306 - IN CRUISE FLIGHT TO MSP, THE NOSE GEAR BEGAN TO CYCLE IN THE WHEEL WELL. THE CREW LOWERED THE GEAR AND CONTINUED TO MSP. MAINTENANCE REPLACED THE LEFT AND RIGHT NOSE LANDING GEAR ACTUATORS. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950428002351995042800235SW 1995 4 28 MALA954375 119950311A5730 SKIN SWRNGNSA227 SA227AC 8780603SW WS 99.510 LE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING MAINTENANCE IN MSP, A .25 INCH CRACK WAS FOUND EXTENDING FROM A RIVET HOLE ON THE LEFT WING LOWER LEADING EDGE AT WS 99.510. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED AREA AND FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 57-90-20 PAGES 3-8. (W) 2L72 4T RTA8SW 19950428002361995042800236SW 1995 4 28 MALA954376 119950315A53202731110033 SUPPORT SWRNGNSA227 SA227AC 8780603SW LWR FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE FORWARD FUSELAGE BELLY SUPPORT CHANNEL (P/N 27-31110-033) AT BL 0.00 TO BE CRACKED. COMPLETED REPAIR TO THE SUPPORT CHANNEL IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002371995042800237SW 1995 4 28 MALA954377 119950315A53202722108035 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 287.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE RT LOWER INTERCOSTAL P/N 27-22108-035 TO BE CRACKED AT THE LOWER, CENTER AISLE SUPPORT FLANGE RELIEF RADIUS OF FS 287.27. COMPLETED REPAIR TO THE INTERCOSTAL FRAME IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002381995042800238SW 1995 4 28 MALA954378 119950315A53112720085 FRAME SWRNGNSA227 SA227AC 8780603SW AFT FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTNENANCE INSPECTION IN MSP, MECHANICS FOUND THE REAR FUSELAGE MOUNTED FRAME OF THE AFT CARGO DOOR (P/N 27-0085) TO BE CRACKED AT THE GAS STRUT ATTACHMENT HOLE. COMPLETED REPAIR TO THE FRAME IAW FAIRCHILD ARP 53-20-9503 AND THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002391995042800239SW 1995 4 28 MALA954379 119950315A53112722100036 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE LEFT LOWER BELT FRAME, P/N 27-22100-036, TO BE CRACKED AT THE UPPER, OUTBOARD FLANGE RELIEF RADIUS OF FS 242.27. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002401995042800240SW 1995 4 28 MALA954380 119950315A53112722104047 FRAME SWRNGNSA227 SA227AC 8780603SW FS 212.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE RT LOWER BELT FRAME P/N 27-22104-047 TO BE CRACKED AT THE UPPER, OUTBOARD RELIEF RADIUS OF FS 212.27. COMPLETED REPAIR TO THE LOWER BELT FRAME IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002411995042800241SW 1995 4 28 MALA954381 119950315A57302731361331 SKIN SWRNGNSA227 SA227AC 8780603SW WS 266 DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED INSPECTION IN MSP, MECHANICS FOUND THE UPPER ATTACHMENT SCREWS FOR LEFT WING EXTENSION SKIN PANEL (P/N 27-31361-331) TO BE PULLING THROUGH THE SKIN PANEL ALONG WSL 266.0. COMPLETED REPAIR TO THE LEFT UPPER WING SKIN IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002421995042800242SW 1995 4 28 MALA954382 119950315A57302731361332 SKIN SWRNGNSA227 SA227AC 8780603SW WS 266 DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728 DURING A SCHEDULED MAINTENANCE INSPECTION IN MSP, MECHANICS FOUND THE UPPER ATTACHMENT SCREWS FOR RT WING EXTENSION SKIN PANEL (P/N 27-31361-332) TO BE PULLING THROUGH THE SKIN PANEL, ALONG WS 266.0. COMPLETED REPAIR TO THE UPPER RT WING SKIN IAW THE FAIRCHILD SRM. (W) 1L72 4T A8SW 19950428002431995042800243SW 1995 4 28 MALA954383 119950321A32602782186057 POSITION IND SWRNGNSA227 SA227AC 8780603SW RT MLG INTERNAL FAULT A MALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL15422MA AC635 FLT 3213 - ON APPROACH TO BJI, THE CREW DID NOT RECEIVE A GREEN DOWN AND LOCKED INDICATION FROM THE RIGHT GEAR. THE CREW PUSHED ON THE INDICATOR HOUSING AND THE LIGHT ILLUMINATED. THE CREW PERFORMED A FLY BY AND THE GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT IN BJI. MAINTENANCE REPLACED THE LANDING GEAR POSITION INDICATOR. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 1L72 4T A8SW 19950428002441995042800244SW 1995 4 28 MALA954385 119950324A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL152692P AC658B FLT 3013 - ON CLIMB-OUT FROM AZO, THE NOSE GEAR CYCLED ONCE AFTER GEAR RETRACTION. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE ADJUSTED THE UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002451995042800245NM 1995 4 28 MALA954386 119950326A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15854MA 357 DURING THE PREFLIGHT IN DTW, ONE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LEFT FORWARD BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428002461995042800246 1995 4 28 MALA954387 419950325A34255222638007 HSI SWRNGNSA227 SA227AC 8780603SW LT COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15160MC AC733B FLT 3211 - ON CLIMB-OUT FROM MSP, THE CAPTAINS HSI FAILED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 1 HSI. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002471995042800247SW 1995 4 28 MALA954389 119950328A5270U31 SWITCH SWRNGNSA227 SA227AC 8780603SW CARGO DOOR OUT OF ADJUST A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15159MC AC728 FLT 3218 - IN CRUISE FLIGHT FROM MSP, THE PRIMARY AND SECONDARY CARGO DOOR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE CARGO DOOR HANDLE WARNING SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002481995042800248NM 1995 4 28 MALA954390 119950329A3350 EEL CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15865MA 364 FLT NR 3107 - DURING THE PREFLIGHT INSPECTION IN DTW, THE EMERGENCY LIGHT ABOVE THE MAIN PASSENGER DOOR WOULDN'T ILLUMINATE. MAINTENANCE RESECURED THE CANNON PLUG TO THE OVERHEAD EMERGENCY LIGHT ASSY. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428002491995042800249SW 1995 4 28 MALA954391 119950402A215020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW WING SEIZED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15426MA AC645 FLT NR 3316 - WHILE TAXIING THE AIRCRAFT INTO THE GATE IN CWA, SMOKE BECAME EVIDENT IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED THE COOLING TURBINE. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002501995042800250SW 1995 4 28 MALA954393 119950331A57532731441001 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING SCHEDULED MAINTENANCE IN MSP, THE LEFT FLAP ROLLER DOUBLER WAS FOUND TO BE WORN. REPAIRS WERE COMPLETED BY REPLACING THE LEFT FLAP ROLLER DOUBLER, P/N 27-31441-001, IAW FAIRCHILD SRM ARP 57-20-9207 AND ARP 57-20-9424. (W) 1L72 4T A8SW 19950428002511995042800251NM 1995 4 28 MALA954394 119950403A2761A44700009 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT SPOILER FAILED A MALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL15828MA 333 FLT 3118 - ON APPROACH TO MLI, THE LEFT INBOARD ROLL SPOILER STUCK UP. THE CREW HAD TO PUT ABOUT ONE-THIRD CONTROL INPUT TO THE RIGHT FOR LEVEL FLIGHT. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND LANDED IN MLI WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT INBOARD ROLL SPOILER ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950428002521995042800252SW 1995 4 28 MALA954395 119950404A32302719248003 DNLOCK SPRING SWRNGNSA227 SA227AC 8780603SW NLG BROKEN A MALAO OTHER O OTHER APAPPROACH 1 GL15160MC AC733B FLT NR 3074 - ON APPROACH TO MSP, THE NOSE GEAR REMAINED UP AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE NOSE GEAR EXTENDED NORMALLY. THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT DOWN LOCK SPRING MISSING. MAINTENANCE REPLACED THE SPRING ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002531995042800253SW 1995 4 28 MALA954396 119950405A53112722093105 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.247 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 DURING SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND FUSELAGE FRAME FS 159.247 P/N 27-22093-105 CRACKED AT THE INNER FLANGE OF CONSTANT SECTION .005 INCH LONG. REPAIRS WERE COMPLETED IAW FAC SRM 53-90-20 REPAIR NR 20. (W) 1L72 4T A8SW 19950428002541995042800254SW 1995 4 28 MALA954402 119950407A5720 ANGLE SWRNGNSA227 SA227AC 8780603SW RT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT WING TO NACELLE UPPER INBOARD ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR ANGLE AS PER ARP 54-20-9101 REVISION B. (W) 1L72 4T A8SW 19950428002551995042800255NM 1995 4 28 MALA954403 119950408A541485410025011 SKIN DHAV DHC8 DHC8102 2809003NM RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15819MA 251 DURING A C-CHECK INSPECTION IN CKB, THE RIGHT EXHAUST SHROUD WAS FOUND TO HAVE THE RIGHT BOTTOM ANGLE BY THE AFT HOLE CHAFED AND THE LEFT AFT SIDE SKIN CRACKED. REPAIRS WERE COMPLETED IAW WVAC EO-DHC8-93-7 REVISION A. (W) 2H72 4T RTA13NM 19950428002561995042800256NM 1995 4 28 MALA954404 119950408A541485410025009 SKIN DHAV DHC8 DHC8102 2809003NM LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15819MA 251 DURING A C-CHECK INSPECTION IN CKB, THE LEFT EXHAUST FINGERNAIL WAS FOUND TO HAVE THE DOVETAIL SUPPORT ANGLES AND THE LEFT AND RIGHT SIDE SKINS CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING THE TOP HALF RING IAW WVAC EO-DHC-8-93-07 REVISION A. (W) 2H72 4T RTA13NM 19950428002571995042800257NM 1995 4 28 MALA954405 119950408A5522 SKIN DHAV DHC8 DHC8102 2809003NM ELEVATOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15819MA 251 DURING SCHEDULED MAINTENANCE IN MSP, MAINTENANCE FOUND THE ELEVATOR SKIN TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE SECTIONS IAW RD 8-55-232 AND DASH 8 SRM CHAPTERS AS APPLICABLE. (W) 2H72 4T RTA13NM 19950428002581995042800258SW 1995 4 28 MALA954406 119950408A77222719149003 EGT INDICATOR SWRNGNSA227 SA227AC 8780603SW RT COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15425MA AC640 FLIGHT NR 3218 - IN CRUISE FLIGHT FROM MSP, THE RIGHT EGT READ 150 DEGREES LOWER THAN THE LEFT EGT. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT EGT INDICATOR. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950428002591995042800259SW 1995 4 28 MALA954407 119950410A5310 CONSTANT SECT SWRNGNSA227 SA227AC 8780603SW FS 144.22 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING SCHEDULED MAINTENANCE IN MSP, THE CONSTANT SECTION RELIEF RADIUS AT RIGHT FS 144.22 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20 PAGES 83-85. (W) 1L72 4T A8SW 19950428002601995042800260SW 1995 4 28 95ZZZX1995 119950405A5320272441500734 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING A SCHEDULED INSPECTION, REPAIRS WERE COMPLETED TO THE PASSENGER DOOR BY REPLACING THE FOLLOWING PARTS DUE TO CRACKING AT NUT PLATE AREA, LOWER FORWARD DOOR FRAME CORNER, PN 27-24044-010, AND LOWER FORWARD DOOR FRAME ASSEMBLY, PN 27-244150-0734, DOUBLER, PN 27K244151-025. REFERENCE CONTROL NR MALA954398. 1L72 4T A8SW 19950428002611995042800261SW 1995 4 28 95ZZZX1996 119950325A53202731110033 SUPPORT SWRNGNSA227 SA227AC 8780603SW LOWER FLANGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND THE FORWARD BELLY SUPPORT CHANNEL (PN 27-31110-033) AT BL 0.00 CRACKED AT THE LOWER CHANNEL FLANGE. COMPLETED REPAIRS BY THE PART-FOR-PART REPLACEMENT OF THE CHANNEL AND CHANNEL REINFORCEMENT IAW THE FAIRCHILD SRM. 1L72 4T A8SW 19950428002621995042800262SW 1995 4 28 95ZZZX1997 119950325A53202722100035 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 242 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE LOWER CENTER AISLE INTERCOSTAL CRACKED IN THE LOWER FLANGE BEND RELIEF RADIUS AT FS 242 OF BELT FRAME, PN 27-22100-035. COMPLETED REPAIR TO THE CENTER AISLE INTERCOSTAL IAW THE FAIRCHILD SRM. 1L72 4T A8SW 19950428002631995042800263SW 1995 4 28 95ZZZX1998 119950325A53102722125021 CONSTANT SECTION SWRNGNSA227 SA227AC 8780603SW FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND THE RT LOWER CONSTANT SECTION CRACKED AT RELIEF RADIUS. REPAIR WAS COMPLETED BY STOP DRILLING THE CRACK, FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950428002641995042800264SW 1995 4 28 95ZZZX1999 119950325A5320 INTERCOSTAL SWRNGNSA227 SA227AC 8780603SW FS 159 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND RT INTERCOSTAL FS 159 CRACKED. REPAIR COMPLETED TO RT LOWER BELT FRAME (PN 27-22093-145) BY STOP DRILLING THE CRACKS AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950428002651995042800265SW 1995 4 28 95ZZZX2000 119950325A5532 REBATE SWRNGNSA227 SA227AC 8780603SW VERTICAL STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANICS FOUND VERTICAL STABILIZER ACCESS PANEL REBATE CRACKED, FOR PANEL NR 803, FABRICATED A NEW REBATE USING SAME MATERIAL AS ORIGINAL AND INSTALLED IAW WITH SRM 55-30-00 AND SRM 51-30-00. 1L72 4T A8SW 19950428002661995042800266SW 1995 4 28 95ZZZX2001 119950325A5320 FLANGE SWRNGNSA227 SA227AC 8780603SW FS 212 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS FOUND FS 212 RT LOWER CONSTANT SECTION FLANGE CRACKED AND LT FS 212 LOWER CONSTANT SECTION CRACKED AT RELIEF RADIUS. REPAIRS COMPLETED AS FOLLOWS: RT FS 212 FLANGE WAS REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW 53-90-20 REPAIR NR 20, AND RELIEF RADIUS CRACK WAS REPAIRED BY INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20 REPAIR NR 19. 1L72 4T A8SW 19950428002671995042800267SW 1995 4 28 95ZZZX2002 119950325A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW RT MACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANCIS FOUND RT NACELLE UPPER INBOARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. REPAIR COMPLETED BY FABRICATING NEW ANGLE USING SAME MATERIAL AS ORIGINAL AND INSTALLING. 1L72 4T A8SW 19950428002681995042800268SW 1995 4 28 95ZZZX2003 119950325A53112721052035 FRAME SWRNGNSA227 SA227AC 8780603SW FS 107 DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING SCHEDULED MAINTENANCE INSPECTION, MECHANCIS FOUND REPAIR TO FUSELAGE FRAME, PN 27-21052-035, FS 107. INSTALLED REPAIR DOUBLER IAW FAC SRM 53-90-10, REPAIR NR 7 AND LAR 95-MALA-063. 1L72 4T A8SW 19950428002691995042800269SW 1995 4 28 95ZZZX2004 119950325A5320 FLANGE SWRNGNSA227 SA227AC 8780603SW FS 212 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED MAINTENANCE INSPECTION, MECHANICS COMPLETED REPAIRS TO FUSELAGE, PN 27-22104-047, AT FS 212 DUE TO A CRACK IN FLANGE, AND A CRACK IN RELIEF RADIUS. REPAIRED BY INSTALLING REPAIR DOUBLERS IAW FAC SRM 53-90-20, REPAIRS NR 19 AND NR 20. 1L72 4T A8SW 19950428002701995042800270SW 1995 4 28 95ZZZX2005 119950325A5311272212502 FRAME SWRNGNSA227 SA227AC 8780603SW FS 133 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANCIS COMPLETED A REPAIR TO FUSELAGE FRAME, PN 27-22125-02, FS 133, DUE TO A CRACK IN RADIUS RT SIDE. REPAIR DONE IAW FAC SRM 53-90-20, REPAIR NR 19. 1L72 4T A8SW 19950428002711995042800271SW 1995 4 28 95ZZZX2006 119950325A57122731240 RIB SWRNGNSA227 SA227AC 8780603SW WS 51 LT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANICS COMPLETED A REPAIR TO LT WING RIB, PN 27-31240, AT WS 51, DUE TO CRACK AT HYDRAULIC BULKHEAD FITTING. WORK DONE IAW FAC ARP 57-20-9313, REV. A. 1L72 4T A8SW 19950428002721995042800272SW 1995 4 28 95ZZZX2007 119950325A52102624037011 CHANNEL SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, MECHANICS COMPLETED REPAIR TO PASSENGER DOOR BY REPLACING CHANNEL, PN 26-24037-011, AND BRACKET, PN 27-24048-009, DUE TO CRACKS. REPAIRS WERE COMPLETED IAW FAC SRM 51-00-00, PAGE 4, AND THE SRM STANDARD PRACTICES. 1L72 4T A8SW 19950428002731995042800273NM 1995 4 28 CAL950240 119950328A21215007024620 FAN BOEING727 727227 1384078NM A/C BAY CONTAMINATED A CALAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09167612438010150 21119 OKC - FLT 0121 - SMOKE APPEARED IN THE CABIN WHILE EN ROUTE FROM IAH TO DEN. THE SMOKE CEASED AFTER THE AIR DISTRIBUTION FAN WAS TURNED OFF AND CIRCUIT BREAKERS WERE PULLED. THE SMOKE RE-APPEARED ABOUT 10 MINUTES LATER. THE SOURCE OF SMOKE COULD NOT BE ISOLATED. THE AIRCRAFT WAS DIVERTED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR DISTRIBUTION FAN INLET CONTAMINATED. THE CONTAMINANT WAS REMOVED FROM THE INLET. THE FAN WAS RUN FOR 45 MINUTES AND NO SMOKE WAS OBSERVED. (X) 2L73 4F A3WE 19950428002741995042800274EU 1995 4 28 CAL950265 119950409A76035802194 CONTROL CABLE AIRBUS300 A300B4203 3930306EU NR 2 ENGINE BINDING A ACALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW091596727584 121 CLE - FLT 0639 - NR 2 ENGINE THROTTLE JAMMED AFTER LEVEL OFF WHILE ACCELERATING TO CRUISE SPEED. THE PILOT BEGAN A DESCENT AND THE THROTTLE STARTED TO UNJAM. THE THROTTLE WAS COMPLETELY FREE AT 14,000 FEET. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE THROTTLE CONTROL CABLE BETWEEN THE MEC AND PRIMARY TRANSMISSION IAW MM 76-11-00. A POWER ASSURANCE RUN WAS PERFORMED ON THE NR 2 ENGINE AND ALL ENGINE PARAMETERS WERE WITHIN LIMITS AND THROTTLE OPERATION WAS NORMAL. THIS PART MAY HAVE FROZEN IN FLIGHT ACCORDING TO CAL MOC. (X) 2L72 4F RTA35EU 19950428002751995042800275EA 1995 4 28 LCFA950321 219950321A7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR 2 MALFUNCTIONED A LCFAO OTHER O OTHER NRNOT REPORTED 1 NM09276647766 136 30974 CPPS61557 BOTH ENGINES WERE AT FLIGHT IDLE. NR 2 ENGINE SUDDENLY ACCELERATED. NR 2 ENGINE WAS SHUT DOWN WITHIN 5 SECONDS. NR 2 ENGINE N2 RPM WAS NOTED TO BE 110 PERCENT. SUSPECT MANUAL/AUTOMATIC FUEL CONTROL MALFUNCTION. ENGINE REMOVED FOR OVERSPEED INSPECTION. (X) 1G71 4U4 U H4SW E22EA 19950428002761995042800276SW 1995 4 28 MALA954384 119950323A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B MSP - DURING ROUTINE MAINTENANCE, LEFT FUSELAGE CONSTANT SECTION LOWER BELT FRAME AT FS 174.06 WAS FOUND CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A DOUBLER IAW FAC ARP 53-20-9148. (X) 1L72 4T A8SW 19950428002771995042800277NM 1995 4 28 MALA954388 119950325A323185420014101 GEAR DOOR DHAV DHC8 DHC8102 2809003NM RT MLG CAME OPEN A MALAK NONE O OTHER CRCRUISE 1 GL15816MA 231 LSE - FLT 3216 - EN ROUTE, RIGHT FORWARD MLG DOOR CAME OPEN. THE AIRCRAFT CONTINUED TO LSE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AFT FORWARD GEAR DOOR ATTACH ARM/HINGE, PN 85420014-101. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950428002781995042800278SW 1995 4 28 MALA954397 119950405A531127222093104 FRAME SWRNGNSA227 SA227AC 8780603SW FS 332.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING SCHEDULED INSPECTION, FOUND FUSELAGE FRAME FS 332.27, PN 27-22093-104, HAD A .125 INCH CRACK AT RELIEF RADIUS IN LOWER BELT FRAME OF CONSTANT SECTION. REPAIRS WERE COMPLETED IAW SRM 53-90-20, REPAIR NR 19. (X) 1L72 4T A8SW 19950428002791995042800279SW 1995 4 28 MALA954398 119950405A53202724044010 CORNER SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING A SCHEDULED INSPECTION, REPAIRS WERE COMPLETED TO THE PASSENGER DOOR BY REPLACING THE FOLLOWING PARTS DUE TO CRACKING AT NUT PLATE AREA, LOWER FORWARD DOOR FRAME CORNER, PN 27-24044-010, AND LOWER FORWARD DOOR FRAME ASSEMBLY, PN 27-244150-0734, DOUBLER, PN 27K244151-025. REFERENCE OPER CONTROL NR 95ZZZX1995. (X) 1L72 4T A8SW 19950428002801995042800280SW 1995 4 28 MALA954399 119950405A53202731110032 STIFFENER SWRNGNSA227 SA227AC 8780603SW BELLY CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE REPAIRED THE BELLY FAIRING CENTER CHANNEL STIFFENER AT BL 0.00, PN 27-31110-032, DUE TO CRACKING. REPLACED ASSEMBLY, INSTALLED DOUBLER IAW FAC SRM 57-90-30 REPAIR NR 1 AND ADDED TEE ANGLES TO REDUCE POSSIBILITY OF CRACKING RECURRING IAW FAC SRM REPAIR NR 2. (X) 1L72 4T A8SW 19950428002811995042800281SW 1995 4 28 MALA954400 119950405A5753 TE SKIN SWRNGNSA227 SA227AC 8780603SW RT TE FOREFLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT INBOARD FOREFLAP TRAILING EDGE WORN. REPLACED THE RT INBOARD FOREFLAP, PN 27-36000-006. (X) 1L72 4T A8SW 19950428002821995042800282SW 1995 4 28 MALA954401 119950405A5320 DOOR SILL SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR OVERSIZED HOLE A MALAK NONE O OTHER ININSP/MAINT 1 GL15425MA AC640 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE COMPLETED A REPAIR TO THE FUSELAGE PASSENGER DOOR SILL DUE TO OVERSIZED RIVET HOLES AT HINGE ATTACHMENT. REMOVED AND RPELACED DOOR SILL IAW FAC LAR 95-MALA-105. ALSO, INSTALLED MOD KIT 27K24182 ON FUSELAGE AND STAINLESS STEEL HINGE, PN 27K24182-005. (X) 1L72 4T A8SW 19950428002831995042800283EU 1995 4 28 VTZA95128 119950410A56101379510C SEAL BAG JETSTMJETSTM3201 1500217EU RT DV WINDOW UNGLUED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27370MT 800 IAD/ROC - FLT 6326 - DURING CLIMBOUT AT 125 HRS ON 4-10-95, RETURNED TO IAD DUE TO THE FO'S DV WINDOW SEAL LEAKING. AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RE-GLUED THE DV WINDOW SEAL AND PRESSURIZED THE AIRCRAFT. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950428002841995042800284WP 1995 4 28 ABXA9500355 119950417A78305858782503 LINK 5910294507 DOUG DC9 DC9 3022002WP NR 2 TR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23 ABX1908 DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB 78-38, 78-66, 78-40, 78-36, FOUND THE NR 2 THRUST REVERSER LOWER RIGHT DRIVER LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 MM 78-32. LINK WAS SCRAPPED. 2L72 4F A6WE 19950428002851995042800285WP 1995 4 28 ABXA9500356 119950331A57534916865501 BASE DOUG 5910134521 DOUG DC9 DC941 302207NWP LT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 38 47493 DURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT FLAP BASE FOR SPRING. REPLACED WITH NEW BASE FOR SPRING IAW DC-9 OVERHAUL MANUAL 27-50-1. 2L72 4F A6WE 19950428002861995042800286WP 1995 4 28 ABXA9500357 119950411A32313923161503 LINK DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WHERE ROD ASSEMBLIES MEET HAD EXCESSIVE PLAY. REPLACED LINK ASSEMBLY AND ATTACHING HARDWARE IAW DC-9 OVERHAUL MANUAL. 2L72 4F A6WE 19950428002871995042800287WP 1995 4 28 ABXA9500358 119950407A5330592032379 SKIN DOUG DC9 DC941 302207NWP FS 389 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION, FOUND DENT AT FS 389R, LONGERON 18R AND 19R. REPAIRED DENT IAW ABX REA D953-11392-MR. 2L72 4F A6WE 19950428002881995042800288WP 1995 4 28 ABXA9500359 119950408A5713NAS1468 SRTINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER 11 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002891995042800289WP 1995 4 28 ABXA9500360 119950408A5713NAS1468 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 51017 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER 12 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002901995042800290WP 1995 4 28 ABXA9500361 119950408A5713NAS1468 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 13 AT XWC 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002911995042800291WP 1995 4 28 ABXA9500362 119950408A5713NAS1468 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON STRINGER NR 15 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002921995042800292WP 1995 4 28 ABXA9500363 119950408A5713NAS1468 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 17 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002931995042800293WP 1995 4 28 ABXA9500364 119950408A5713NAS1468 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION DURING COMPLIANCE OF AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 18 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002941995042800294WP 1995 4 28 ABXA9500365 119950408A5713HLT426 STRINGER DOUG DC9 DC941 302207NWP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING C-CHECK INSPECTION DURING COMPLIANCE OF AD 90-18-03, SB 57-98, FOUND CORRODED HILOCKS ON FORWARD SIDES OF LEFT WING STRINGER 18, 19, 21 AND 22 AT STA XCW 58. REPLACED HILOCKS IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950428002951995042800295WP 1995 4 28 ABXA9500366 119950422A52803923166501 FITTING DOUG DC9 DC933F 302207AWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR ARTICULATING DOOR LINK ARM TO HAVE EXCESSIVE PLAY. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950428002961995042800296WP 1995 4 28 ABXA9500367 119950422A528052210370P4109 BUSHING DOUG DC9 DC933F 302207AWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR DOUBLE TO SINGLE LINK TO HAVE EXCESSIVE PLAY. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950428002971995042800297WP 1995 4 28 ABXA9500369 119950422A32313923158501 LINK DOUG DC9 DC933F 302207AWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK BEARING TO HAVE EXCESSIVE PLAY. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-106. 2L72 4F A6WE 19950428002981995042800298SO 1995 4 28 BIER 950011 119950425A7120LW15952 BOLT PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE MOUNT MISINSTALLED A ABIEAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA2127508 800 317852031 RL281261A AT COMPLIANCE WITH LYC SI 1384, FOUND TOP BOLTS FOR MOUNT INSTALLED BACKWARDS AND TOP AND BOTTOM WASHERS INSTALLED ON WRONG SIDE OF BOLT ON LYCOMING OVERHAULED ENGINE. INSP TWO MATTITUCK ENGINES AND FOUND SIMILAR DISCREPENCIES. 1L72 3O3 O A20SO E14EA 19950428002991995042800299NM 1995 4 28 DL767951700 119950421A3230273T63008 LOCK ACTUATOR BOEING767 767232 1385132NM LT MLG BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11114DL 22226 ON CLIMBOUT, WHEN GEAR HANDLE WAS PLACED TO UP THE AMBER DOORS AND GEAR LIGHT STAYED ON. CYCLED GEAR, NO HELP AND RETURNED ATL. FOUND LT MLG, FORWARD JURY BRACE LOCK ACTUATOR PISTON BROKEN. REPLACED SAME OPERATION NORMAL. 2L72 4F RTA1NM 19950428003001995042800300NM 1995 4 28 DL76L951693 119950422A36107738555 VALVE BOEING767 767332 1382001NM LT PNEUMATIC SYSFAULTY A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11176DN 25061 ON CLIMBOUT, HAD LEFT BLEED OVERHEAT LIGHT WITH EICAS MSG, RETURNED ATL. AIR SUPPLY BITE FAULTS FAN, AIR VALVE AND FAN AIR TEMP SENSOR. REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR. AIR SUPPLY BITE CHECKS GOOD OPERATION NORMAL. 2L72 4F RTA1NM 19950428003011995042800301NM 1995 4 28 DL76S951720 119950421A3211161T111033 TRUNNION BOEING767 767332 1382001NM LT MLG FRACTURED A ADALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11119DL27117 23278 AFTER ARRIVAL AT GATE WHILE AIRCRAFT WAS MOTIONLESS, THE LEFT MAIN LANDING GEAR TRUNNION OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BORE. THE LOWER 180 OF THE AFT END SEPARATED REMOVING A 6 INCH LONG PIECE. INITIAL VISUAL EXAMINATION REVEALS SEVERE CORROSION PRESENT IN THE CHAMBER UNDER THE SEALED BUSHING FLANGE. THE LANDING GEAR TRUNNION WAS REPLACED. THIS IS THE FIRST OCCURANCE OF THIS TYPE OF FAILURE ON DALA 767 AIRCRAFT. 2L72 4F RTA1NM 19950428003021995042800302 1995 4 28 DLM88951698 419950423A22971C610R20RD WIRE DOUG MD88 MD88 3023688NM YAW DAMPER CHAFED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO11914DL 49545 AFTER T/O LOST DFGC CONTROL, DGF CIRCUIT BREAKER C-17 POPPED UNABLE TO RESET, LANDED CHA. FOUND WIRE 1C610R20RD CHAFING AND SHORTED AT APPROX 1 FOOT IN FRONT OF YAW DAMPENER ACTUATOR. REPAIRED WIRE OPERATION NORMAL. 2L72 4F RTA6WE 19950428003031995042800303 1995 4 28 DLM88951701 419950421A34204055900905M0DT SYB GENERATOR DOUG MD88 MD88 3023688NM LEFT FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11919DE 53422 DURING CRUISE, CAPTAINS PFD WENT BLANK, LANDED CVG. REPLACED SYB GENERATOR OPERATION NORMAL. 2L72 4F RTA6WE 19950428003041995042800304WP 1995 4 28 MWEA95177 119950421A495012955211 THERMOSTAT DOUG DC9 DC932 3022066WP APU FAILED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31202ME 47672 CREW REPORTS, ON GROUND WITH APU RUNNING AND RIGHT PACK ON, CABIN FILLED WITH SMOKE. MAINTENANCE REPLACED LOAD THERMOSTAT. ALSO, INSTALLED LOAD CONTROL VALVE. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950428003051995042800305WP 1995 4 28 MWEA95178 119950421A25605917689103 SLIDE COVER DOUG DC9 DC915 3022036WP PAX DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31900ME 45841 CREW REPORTS, EVACUATION SLIDE COVER FELL OFF OF MAIN ENTRANCE DOOR. MAINTENANCE RE-INSTALLED EVACUATION SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950428003061995042800306WP 1995 4 28 MWEA95179 119950423A3350100865 EEL POWER SUPPLY DOUG DC9 DC914 3022034WP AFT LAV DISCHARGED A MWEAK NONE L NO TEST CRCRUISE 1 GL31500ME 45711 CREW REPORTS, THAT EMERGENCY FLOOR TRACK LIGHTS CAME ON DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY FOR SECTION OF TRACK LIGHTING AFFECTED. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950428003071995042800307WP 1995 4 28 MWEA95180 119950423A33501001191 FLASHLIGHT DOUG DC9 DC932 3022066WP CABIN INOP A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31202ME 47672 CREW REPORTS, FWD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950428003081995042800308WP 1995 4 28 MWEA95181 119950424A253062000111 OVEN DOUG DC9 DC914 3022034WP GALLEY INOP A MWEAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL31600ME 45725 CREW REPORTS, 3 OVEN CIRCUIT BREAKER POPPED IN FLIGHT AND F/A SMELLED BURNING ODOR IN CABIN. MAINTENANCE REMOVED AND REPLACED OVEN. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950428003091995042800309EU 1995 4 28 QXEA9500125 119950424A3350MGG1280 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - EMERGENCY EXIT SIGN OVER COCKPIT DOOR ALL 28V LAMPS INOP. RELAMPED ALL 28 VOLT LAMPS ON EXIT SIGN. LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950428003101995042800310EU 1995 4 28 QXEA9500126 119950424A3350MGG1280 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - OVERHEAD EMERGENCY EXIT SIGN IN CABIN 28 VOLT LIGHTS INOP ON BOTH SIDES. RELAMPED ALL 28 VOLT LAMPS FORWARD AND AFT SIDES. LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950428003111995042800311EU 1995 4 28 95ZZZX2009 119950405A3220 NOSE GEAR SAAB SF340 340B 7860101EU NLG WELL MALFUNCTION A NVEAO OTHER J WARNING INDICATION LDLANDING 1 SO03323AE 340B323 ROC - FLT 4905 - NOSE GEAR WOULD NOT EXTEND DURING LANDING APPROACH. INVESTIGATION FOUND NOSE TIRES TURNED TO THE LEFT IN THE WHEELWELL. 2L72 4T RTA52EU 19950428003121995042800312WP 1995 4 28 95ZZZX2010 119950401A3230 FLIGHT LOCK DOUG DC8 DC871 302199AWP RT MLG STICKING A RRXAO OTHER J WARNING INDICATION CLCLIMB 1 WP158084U 45974 RIGHT MAIN GEAR DOOR LIGHT ON DURING UPLATCH CHECK. LIGHTS WENT OUT ON 3RD RECYCLE WITH FLAPS UP. MAINTENANCE PERFORMED ELECTRICAL AND MECHANICAL FUNCTIONAL TEST OF LT AND RT GEAR FLIGHT LOCKS. FOUND RT FLIGHT LOCK STICKING. CLEANED AND LUBED FLIGHT LOCKS. OPS CHECK GOOD THROUGH MANY CYCLES PER MM 32-6. 2L74 4F 4A25 19950428003131995042800313 1995 4 28 95ZZZX2011 419950404A3197 WIRE BOEING757 757225 1384959NM INSTRUMENT PANELDAMAGED A AWXAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP28915AW 22209 PHX/LAX - FLT 33 - AIR TURNBACK. DURING CLIMB, FIRST OFFICER'S INSTRUMENTS ON FORWARD PANEL WENT BLANK AND FLAGGED FOR APPROXIMATELY 10 SECONDS, THEN RETURNED TO NORMAL. BOTH CAPTAIN AND FIRST OFFICER NOTICED SMELL OF ELECTRICAL WIRES BURNING. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND WIRES CHAFED THROUGH A CLAMP AND STAND-OFF NEAR P37 PANEL. REPLACED DAMAGED WIRES TO P50 PANEL. PERFORMED OPS CHECK PER MM REFERENCES FOR P50 PANEL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA2NM 19950428003141995042800314EU 1995 4 28 95ZZZX2012 119950413A33507012210 LAMP AEROSPATR42 ATR42320 8680930EU PAX DOOR EEL OPEN A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13988MA619 380 HNL - FLT 704 - DURING PRE-FLIGHT, PILOT NOTED THE PASSENGER STAIR EMERGENCY FLOOD LIGHT WOULD NOT COME ON. REPLACED LAMP. 2H72 4T RTA53EU 19950428003151995042800315CE 1995 4 28 95ZZZX2013 119950308A32601143610441 DOWNLOCK SWITCH BEECH 1900 1900D 1154162CE GEAR WELL FROZEN A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE01101UX2020 UE101 ISN - AFTER TAKEOFF, CREW ELECTED AN AIR TURN BACK WHEN THE DOWNLOCK SWITCH WOULD NOT ACTIVATE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE THAWED OUT THE DOWNLOCK SWITCH AND ACCOMPLISHED A SATISFACTORY GEAR SWING. 2L72 4T RTA24CE 19950428003161995042800316NM 1995 4 28 95ZZZX2014 119950402A2781H1010261 SWITCH EATON H1010261 BOEING727 727259 138408JNM NR 1 LE FLAP FAILED A UHVAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO17203AV 0222 22474 LEFT WING NR 1 LEADING EDGE FLAP LIGHT CAME ON AT 13,000 FEET. REDUCED SPEED AND EXTENDED FLAPS TO 5 DEGREES WITH NORMAL INDICATIONS. RETRACTED FLAPS WITH NORMAL INDICATIONS. THEN 15 TO 20 SECONDS LATER, FLAP LIGHT CAME ON AGAIN. EXTENDED FLAPS AND RETURNED TO CUN. AIRCRAFT FERRY CUN-FLL FOR REPAIR AND HAS BEEN RETURNED TO SERVICE. 2L73 4F A3WE 19950428003171995042800317WP 1995 4 28 95ZZZX2015 119950405A274095906 TRIM MOTOR DOUG DC9 DC932 3022066WP PRIMARY TRIM FAILED A VJ6AO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO11923VV 47488 ATL/PBI - FLT 501 - STARTED DESCENT WHEN CREW NOTICED STABILIZER TRIM NOT FUNCTIONING. AIRCRAFT LANDED WITHOUT INCIDENT IN PBI. REPLACED PRIMARY TRIM MOTOR, PN 9590-6, SN ON 441, SN OFF 819. 2L72 4F A6WE 19950428003181995042800318NE 1995 4 28 95ZZZX2016 219950407A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A VJ6AO OTHER JE WARNING INDICATION VIBRATION/BUFFET APAPPROACH 1 SO11923VV333571064 47488 666987 FLL/ATL - FLT 128 - ON FINAL APPROACH, LEFT THRUST REVERSER UNLOCK LIGHT ILLUMINATED AND CREW FELT HEAVY VIBRATION FROM THE TAIL OF THE AIRCRAFT. REMOVED AND REPLACED NR 1 ENGINE. 2L72 4F4 F A6WE E2EA 19950428003191995042800319WP 1995 4 28 95ZZZX2017 119950407A324095607887 BRAKE ASSY DOUG DC9 DC932 3022066WP NR 1 LOCK UP A VJ6AO OTHER O OTHER TXTAXI/GRND HDL 1 SO11923VV 47488 FLL/ATL - FLT 128 - AFTER LANDING, AIRCRAFT TAXIED OFF OF ACTIVE RUNWAY WHERE THE NR 1 BRAKE LOCKED UP. REMOVED AND REPLACED THE NR 1 AND NR 2 BRAKE ASSEMBLIES. 2L72 4F A6WE 19950428003201995042800320EU 1995 4 28 95ZZZX2018 119950408A29109302631001 LINE SAAB SF340 340B 7860101EU PUMP OUTLET BURST A NVEAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO03177AE 340B177 DFW - FLT 4456 - HYDRAULIC LINE BURST AT HYDRAULIC PUMP CAUSING NWS TO FAIL. ACFT DEPARTED TAXI-WAY INTO THE GRASS. LEFT GEAR THEN HIT A SIGN. NO INJURIES. REPLACED HYDRAULIC LINE. 2L72 4T RTA52EU 19950428003211995042800321NE 1995 4 28 95ZZZX2019 219950408A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE STALLS A NVEAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO03222NE 340B222 785219 CLT - FLT 4632 - CREW REPORTS RT ENGINE COMP STALLS ALONG WITH TORQUE AND PROP RPM FLUX. RETURNED TO CLT SAFELY. PERFORMED COMPRESSOR WASH AND ACFT RETURNED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950428003221995042800322CE 1995 4 28 95ZZZX2020 119950328A5751118130000601 AILERON BEECH 1900 1900C 1154161CE LT WING DENTED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01167GL8190 UC109 UC167 ORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, A BAGGAGE TUG STRUCK THE LEFT AILERON. THE AILERON WAS REMOVED, THE SURROUNDING AREA INSPECTED, AND A SERVICEABLE AILERON INSTALLED. A TEST FLIGHT WAS SATISFACTORY. 2L72 4T RTA24CE 19950428003231995042800323CE 1995 4 28 95ZZZX2021 119950325A5730AN42647 RIVET BEECH 1900 1900C 1154161CE TOP SIDE WING LOOSE A GLBAK NONE K FLUID LOSS ININSP/MAINT 1 CE0145GL 14759 UC45 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 4 RIVETS IN RT FUEL TANK TOP SIDE BETWEEN THE NACELLE AND STALL FORCE LOOSE AND LEAKING FUEL. THE RIVETS WERE REPLACED, THE TANK SEALED, AND LEAK CHECK OKAY. 2L72 4T RTA24CE 19950428003241995042800324NM 1995 4 28 CAL950241 119950330A2910AE1008787H0334 HYDRAULIC LINE BOEING737 737130 1384435NM B-HYD SYS CHAFED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0977215 19032 EWR - FLT 1204 - THE B-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE TO EWR. THE A-SYSTEM QUANTITY GAUGE DECREASED TO ONE GALLON. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND A B-SYSTEM HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A16WE 19950428003251995042800325NM 1995 4 28 CAL950243 119950401A3610652673833 DUCT BOEING727 727232 1384082NM NR 1 ENGINE RUPTURED A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW09523PE 20646 EWR - FLT 0288 - THE NR 1 ENGINE FIRE LIGHT AND BELL ACTIVATED AT CLIMB POWER AND 6,000 FEET. THE NR 1 ENGINE THROTTLE WAS RETARDED AND THE WARNING CEASED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HIGH PRESSURE DUCT TO NOSE COWL ANTI-ICE VALVE RUPTURED. THE DUCT WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND NO LEAKS WERE NOTED. (X) 2L73 4F A3WE 19950428003261995042800326WP 1995 4 28 CAL950244 119950402A2910AE2460001H0292 HYDRAULIC LINE DOUG DC9 DC932 3022066WP NR 2 ENGINE RUPTURED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0910556 47423 IAH - FLT 1853 - THE RT HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP IN FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC SUPPLY LINE RUPTURED. THE SUPPLY LINE WAS REMOVED AND REPLACED. THE NR 2 ENGINE WAS RUN AFTER SERVICING THE RT HYDRAULIC SYSTEM AND NO LEAKS WERE NOTED. (X) 2L72 4F A6WE 19950428003271995042800327NM 1995 4 28 CAL950245 119950402A2910 HYD LINE BOEING727 727227 1384078NM B-HYD SYST CHAFED A CALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW0913759 21044 IAH - FLT 1498 - HYDRAULIC FLUID WAS LOST FROM THE B-SYSTEM WHILE IN-FLIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO B-SYSTEM HYDRAULIC LINES IN THE HYDRAULIC BAY CHAFED THROUGH. BOTH LINES WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950428003281995042800328NE 1995 4 28 CAL950246 219950331A7530 STATOR SUPPORT DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE BROKEN OUT A CALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW091481834112 49478 708412 IAD - FLT 0712 - PILOT REPORTED NR 1 ENGINE FAILURE WHILE EN ROUTE FROM IAD TO BOS. THE AIRCRAFT WAS DIVERTED TO IAD WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED AFTER BORESCOPE OF THE 6TH AND 7TH STAGE COMPRESSOR SECTION FOUND DAMAGE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO A BROKEN OUT EIGHTH STAGE STATOR SUPPORT. (X) 2L72 4F4 F A6WE E9NE 19950428003291995042800329WP 1995 4 28 CAL950250 119950328A52305910141405 DOOR PAN DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW098387339165 49121 HOU - INSPECTION FOUND A 1.5 INCH CRACK IN MAIN CARGO DOOR PAN AT AFT UPPER STOP PAN. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 652C0125. (X) 2L72 4F A6WE 19950428003301995042800330NM 1995 4 28 CAL950263 119950409A2750569670 HYD MOTOR BOEING727 727232 1384082NM LT TE FLAP CRACKED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW09523PE17271 20646 IAH - FLT 0777 - THE A-HYDRAULIC SYSTEM QUANTITY WAS LOST ON LANDING AT IAH. MAINTENANCE FOUND THE INBOARD FLAP DRIVE POWER UNIT HYDRAULIC FLAP MOTOR HOUSING CRACKED. THE HYDRAULIC MOTOR WAS REMOVED AND REPLACED. IN ADDITION, BOTH THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950428003311995042800331NM 1995 4 28 CAL950264 119950407A2750651920410 SPINDLE BOEING727 727227 1384078NM LT TE MID FLAP BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW0910756 21042 DEN - THE LT OUTBOARD MID-FLAP INBOARD CARRIAGE SPINDLE WAS FOUND BROKEN IN TWO DURING B-CHECK INSPECTION WITH RESULTANT DAMAGE TO THE FLAP. BOTH THE LT OUTBOARD MID AND AFT TRAILING EDGE FLAPS WERE REMOVED AND REPLACED. THE FLAPS WERE RIGGED IAW MM 27-51-13 AND OPERATION CHECKED GOOD. (X) 2L73 4F A3WE 19950428003321995042800332NM 1995 4 28 CALA950247 119950403A2910 O-RING BOEING727 727227 1384078NM SPOILER LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0970755 21366 EWR - FLT 0432 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO IN FLIGHT. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE GROUND SPOILER CONTROL VALVE IN THE LT WHEELWELL LEAKING AT FITTING. THE O-RING AND REDUCER WERE REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950428003331995042800333WP 1995 4 28 HAL95032 119950401A3350P4010049 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN EEL DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 4655 47662 HNL - ITEM FROM M-71 LOG PAGE NR 145453-1. AFT CABIN FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. THE OPERATIONAL CHECK WAS GOOD. (X) 2L72 4F A6WE 19950428003341995042800334WP 1995 4 28 IXXA9545 119950131A523037055816 FITTING DOUG DC8 DC871F 302199DWP LWR FUSELAGE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23825BX715362894 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS LOCATED AT THE FORWARD LOWER CARGO DOOR TRACK FITTING. THE FITTING WAS REMOVED AND MANUFACTURED IAW DRAWING HSE27-53-143 AND THE REMOVED FITTING. THIS DRAWING WAS FAA DER APPROVED. THE FITTING WAS INSTALLED IAW THE AIRCRAFT SRM AND MM. (X) 2L74 4F RT4A25 19950428003351995042800335WP 1995 4 28 IXXA9546 119950118A53305613861509 PLATING DOUG DC8 DC871F 302199DWP LWR FWD FUSELAGECRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23825BX715362894 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND AT THE AFT NOSE WHEELWELL DOOR CUT OUT IN EXTERNAL PLATING. REPAIR OF THE CRACK IN THE LEFT AFT CORNER WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, INSTALLING AN EXTERNAL REPAIR DOUBLER. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-139, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-140. (X) 2L74 4F RT4A25 19950428003361995042800336WP 1995 4 28 IXXA9547 119950124A523037050412 FITTING DOUG DC8 DC871F 302199DWP LWR FWD FUSELAGECRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23825BX715362894 45978 DURING ROUTINE C-CHECK INSPECTION, THE LOWER FORWARD CARGO DOOR, LOCK FITTING WAS FOUND CRACKED. THIS FITTING WAS LOCATED AT THE SECOND POSITION FORWARD. THE FITTING WAS REMOVED AND MANUFACTURED IAW DRAWING HSE27-52-142, WHICH WAS FAA DER APPROVED AND E.O. 52-DC8-136. REMOVAL AND REPLACEMENT OF THE FITTING WAS ACCOMPLISHED IAW AIR MM. (X) 2L74 4F RT4A25 19950428003371995042800337WP 1995 4 28 IXXA9548 119950124A53305779912501 PANEL DOUG DC8 DC871F 302199DWP FS 610 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23825BX715362894 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION REMOVAL FROM THE EXTERNAL PLATING AT FS 610 BETWEEN LONGERONS 29 AND 31 WENT BEYOND SRM LIMITS. THE DAMAGE WAS REPAIRED IAW DRAWING BSE27-53-140, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-137. (X) 2L74 4F RT4A25 19950428003381995042800338WP 1995 4 28 IXXA9549 119950125A53305779912501 PANEL DOUG DC8 DC871 302199AWP LWR CTR FS 610 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX715362894 45998 DURING ROUTINE C-CHECK, EXTERIOR CORROSION WAS NOTED AT FS 610, BETWEEN LONGERONS 34 LEFT AND RIGHT. THE CORROSION WAS REMOVED BY CUT OUT, ADDING A REPAIR FILLER, AND INSTALLING 2 EXTERNAL REPAIR DOUBLERS. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-141, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-139. (X) 2L74 4F 4A25 19950428003391995042800339CE 1995 4 28 SW019505848 119950329A3260 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG FAILED A MASAO OTHER N FALSE WARNING APAPPROACH 1 SW0190YV UC90 PIT - UPON APPROACH, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWNLOCK INDICATION. REMOVED AND REPLACED DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19950428003421995042800342EU 1995 4 28 VTZA95130 119950303A301029S7D525505 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT STABILIZER BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27471UE 821 RIGHT STABILIZER DEICER BOOT BLOWN. MAINTENANCE REMOVED AND REPLACED DEICER BOOT. (X) 2L72 4T RTA56EU 19950428003431995042800343EU 1995 4 28 VTZA95131 119950320A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27494UE 810 RIGHT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003441995042800344EU 1995 4 28 VTZA95133 119950330A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27496UE 900 RIGHT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003451995042800345EU 1995 4 28 VTZA95134 119950303A301029S7D525503 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU LT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27481UE 895 LEFT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003461995042800346EU 1995 4 28 VTZA95135 119950305A301029S7D525503 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU LT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27476UE 884 LEFT OUTBAORD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003471995042800347EU 1995 4 28 VTZA95136 119950316A301029S7D525510 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT INBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27494UE 810 RIGHT INBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003481995042800348EU 1995 4 28 VTZA95137 119950321A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27470UE 814 RIGHT OUTBOARD WING DEICER BOOT BLOWN. MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003491995042800349EU 1995 4 28 VTZA95138 119950321A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27491UE 911 RIGHT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003501995042800350EU 1995 4 28 VTZA95139 119950321A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27494UE 810 RIGHT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003511995042800351EU 1995 4 28 VTZA95140 119950331A301029S7D525503 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU LT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27492UE 790 LEFT OUTBOARD WING DEICER BOOT BLOWN. MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003521995042800352EU 1995 4 28 VTZAO5132 119950321A301029S7D525504 DEICER BOOT BFGOODRICH BAG JETSTMJETSTM3201 1500217EU RT OTBD WING BLOWN A VTZAK NONE O OTHER ININSP/MAINT 1 EA27480UE 894 RIGHT OUTBOARD WING DEICER BOOT BLOWN, MAINTENANCE REMOVED AND REPLACED BOOT. (X) 2L72 4T RTA56EU 19950428003531995042800353WP 1995 4 28 95ZZZW564 119950406A5330 SKIN LKHEED1011 10113851 5265010WP FS 1585-1605 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19764BE 193P1113 LEVEL 2 CORROSION, LEFT OF AFT FUSELAGE IS CRACKED BETWEEN FS 1585 AND FS 1605L, LONGERON 25L. CUTOUT DAMAGED AREA, TREATED AND PRIMED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00. (W) 2L73 4F A23WE 19950428003541995042800354WP 1995 4 28 95ZZZW565 119950301A5320 WINDOW FRAME DOUG DC8 DC862 3021970WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT FUSELAGE MAIN CABIN WINDOW FRAME FOR WINDOW 19R HAS CORROSION ON INSIDE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW RICH DRAWING 5164-6. (W) 2L74 4F 4A25 19950428003551995042800355WP 1995 4 28 95ZZZW566 119950301A5330 SKIN DOUG DC8 DC862 3021970WP BS 1606-1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) 2L74 4F 4A25 19950428003561995042800356WP 1995 4 28 95ZZZW567 119950301A5313 LONGERON DOUG DC8 DC862 3021970WP FS 1500-1480 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT FUSELAGE LONGERON 24R BETWEEN FS 1500 AND 1480 HAS SURFACE CORROSION AND BULGES. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) 2L74 4F 4A25 19950428003571995042800357WP 1995 4 28 95ZZZW568 119950303A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1574/1540 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 12 INCHES LBL. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W) 2L74 4F 4A25 19950428003581995042800358WP 1995 4 28 95ZZZW569 119950303A5330 SKIN DOUG DC8 DC862 3021970WP BS 1557 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, CORROSION BULGING OUT THROUGH FUSELAGE SKIN SURFACE AT AFT RIGHT SIDE OF FUSELAGE BS 1557R BETWEEN LONGERON 28R AND 26R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. (W) 2L74 4F 4A25 19950428003591995042800359WP 1995 4 28 95ZZZW570 119950303A5313 LONGERON DOUG DC8 DC862 3021970WP BS 1606/1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, LONGERON 30 LEFT IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W) 2L74 4F 4A25 19950428003601995042800360WP 1995 4 28 95ZZZW571 119950303A5320 SUPPORT DOUG DC8 DC862 3021970WP BS 1574 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19772CA 46131 LEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 7 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W) 2L74 4F 4A25 19950428003611995042800361WP 1995 4 28 95ZZZW572 119950406A3350RPS1B EEL POWER SUPPLY DOUG DC9 DC982 3022082WP AFT CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED WIRING TO LIGHT ASSY AND REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003621995042800362EA 1995 4 28 95ZZZW573 219950409A7230 COMPRESSOR DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA NR 2 ENG FAILED A HNAAE ENGINE SHUTDOWN M OVER TEMP CRCRUISE 1 EA07905HA5769 070 FLT 3021 - DCA-HPN - THE CREW SHUT THE NR 2 ENGINE DOWN IN FLIGHT DUE TO UNCONTROLLABLE HIGH T5. FOUND THE COMPRESSOR LOCKED UP, REMOVED AND REPLACED NR 2 ENGINE. (W) 2H74 4T4 T A20EA E4EA 19950428003631995042800363EA 1995 4 28 95ZZZW574 119950403A4900 APU DHAV DHC7 DHC7102 2802708EA COCKPIT SMOKING A HNAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07902HA 052 FLT 3132 - DCA-ORF - PRIOR TO TAKEOFF, SMOKE WAS PRESENT IN THE COCKPIT WITH THE AUXILLIARY POWER UNIT (APU) RUNNING. MEL APU BLEED 49-4. AT RON, CHECKED BOTH AIR CYCLE MACHINES OIL QUANTITY AND AIR CYCLE MACHINE OUTLET DUCTING FOR OIL, NONE FOUND. BOTH OIL QUANTITIES CHECK GOOD. ALSO, CHECKED APU BLEED AIR DUCT AND APU COMPARTMENT, NO DEFECTS NOTED. OPS CHECKED APU BLEED AND ALL ENGINE BLEED AIR SYSTEMS, NO SMELL OR SMOKE NOTED. (W) 2H74 4T A20EA 19950428003641995042800364NM 1995 4 28 95ZZZW575 119950403A3242214664 BRAKE ASSY DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 EA07934HA9829 1222 139 FLT 3074 - MCO-MIA - THE LEFT BRAKES WERE GRABBING EXCESSIVELY DURING TAXI OUT. RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. ALSO, REMOVED AND REPLACED ALL THREE HYDRAULIC FILTERS AS A PRECAUTION. (W) 2H72 4T RTA13NM 19950428003651995042800365NM 1995 4 28 95ZZZW576 119950403A324221565 BRAKE ASSY DHAV DHC8 DHC8102 2809003NM MLG FAILED A HNAAD RETURN TO BLOCK G MULTIPLE FAILURE TXTAXI/GRND HDL 1 EA07934HA6591 1321 139 FLT 3074 - MCO-MIA - THE LEFT BRAKES WERE GRABBING EXCESSIVELY DURING TAXI OUT. RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES. ALSO, REMOVED AND REPLACED ALL THREE HYDRAULIC FILTERS AS A PRECAUTION. (W) 2H72 4T RTA13NM 19950428003661995042800366NM 1995 4 28 95ZZZW577 119950412A326054C546349 SEQUENCE VLV DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07928HA1430423 0512 120 FLT 3214 - SBY TO BWI - AFTER TAKEOFF, UPON GEAR RETRACTION, THE NOSE GEAR DOOR AMBER LIGHT REMAINED ON. THE GEAR WAS CYCLED DOWN AND THE RED NOSE UNSAFE LIGHT REMAINED ON AFTER MAIN GEAR GREEN LIGHTS CAME ON. CYCLED GEAR AGAIN AND LIGHTS REMAINED ON. AIRCRAFT TURNED BACK TO SBY AND LANDED WITHOUT INCIDENT. INSPECTED NOSE GEAR COMPONENTS FOR CONDITION AND SECURITY. PERFORMED SEVERAL GEAR SWINGS AND REMOVED AND REPLACED THE SOLENOID SEQUENCE VALVE AS A PRECAUTION. (W) 2H72 4T RTA13NM 19950428003671995042800367NM 1995 4 28 ASAA9510018 119950326A3350883200312 EEL HOUSING RCVR BOEING737 737290C 138448VNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND INOPERATIVE. REPLACED FLOOR PROXIMITY LIGHT HOUSING RECEIVER ASSEMBLY AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950428003681995042800368NM 1995 4 28 ASAA9510019 119950327A33508731002142 EEL BOEING737 7372Q8C 138448SNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSY AND OPERATED NORMALLY. (W) 2L72 4F A16WE 19950428003691995042800369NM 1995 4 28 ASAA9510021 119950401A3350883200312 EEL RECEIVER BOEING737 7372X6C 1384552NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 7 WERE FOUND INOPERATIVE. REMOVED AND REPLACED RECEIVER AT ROW 7 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950428003701995042800370NM 1995 4 28 ASAA9510032 119950409A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 6 AND 7. REPLACED BATTERY BACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A16WE 19950428003711995042800371NM 1995 4 28 ASAA9540012 119950322A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR AND AFT FLOOR TRACK EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950428003721995042800372NM 1995 4 28 ASAA9540013 119950320A33503005939 EEL SOCKET BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01754AS 25095 SEA - LEFT TRAILING EDGE FLAP EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPAIRED LIGHT SOCKET. (W) 2L72 4F RTA16WE 19950428003731995042800373NM 1995 4 28 ASAA9540014 119950331A3350S417N5041 EEL SOCKET BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01772AS 25105 SEA - FORWARD EMERGENCY EXIT PEEPLES LIGHT INOP, ROW 1. MAINTENANCE REPLACED SOCKET. (W) 2L72 4F RTA16WE 19950428003741995042800374NM 1995 4 28 ASAA9540015 119950403A3320BV033000125 SOCKET BOEING737 7374Q8 NM AFT LAVATORY MELTED A AASAAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE ININSP/MAINT 1 NM01762AS 25099 PDX - DURING PRE-DEPARTURE ON THE GROUND AT PDX, ELECTRICAL SMELL NOTED IN AFT LEFT LAVATORY. MAINTENANCE REMOVED FLUORESCENT LIGHT COVER AND FOUND ARCING, FLAME AND SMOKE WITH LIGHT SOCKET MELTED. LAVATORY BLOCKED AND AIRCRAFT RELEASED PER MEL 25-10. MAINTENANCE SUBSEQUENTLY, REMOVED AND REPLACED SOCKET. (W) 2L72 4F RTA16WE 19950428003751995042800375WP 1995 4 28 ASAA9580055 119950322A335060030451 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01932AS 49233 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 14 THROUGH 18. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003761995042800376WP 1995 4 28 ASAA9580056 119950324A3350 EEL WIRING DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 SEA - EMERGENCY EVACUATION TRACK LIGHT INOP NEAR ROW 10. MAINTENANCE SECURED WIRES. (W) 2L72 4F RTA6WE 19950428003771995042800377WP 1995 4 28 ASAA9580058 119950325A335041B004AD07G3 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01956AS 48079 THREE CEILING EMERGENCY EXIT LIGHTS INOP AT ROWS 7-9. MAINTENANCE REMOVED AND REPLACED BATTERIES IN EMERGENCY LIGHT BATTERY PACK. (W) 2L72 4F A6WE 19950428003781995042800378WP 1995 4 28 ASAA9580059 119950330A3350303 EEL LAMP DOUG DC9 DC982 3022082WP CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01932AS 49233 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 24 WAS FOUND INOPERATIVE. RELAMPED AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003791995042800379WP 1995 4 28 ASAA9580064 119950331A3350L201913 EEL SOCKET DOUG DC9 DC982 3022082WP CABIN CORRODED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01932AS 49233 SEA - ONE CEILING EMERGENCY LIGHT INOP, ROW 24. MAINTENANCE CLEANED SOCKET. (W) 2L72 4F A6WE 19950428003801995042800380WP 1995 4 28 ASAA9580065 119950404A3350P4010014110 EEL BATTERY PACK DOUG DC9 DC982 3022082WP R1 DOOR DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01955AS 48080 SEA - DURING SHOP INSPECTION OF R1 DOOR EMERGENCY EVACUATION SLIDE (REMOVED DUE TO APPROACHING TIME LIMIT) THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE WHEN SLIDE WAS DEPLOYED. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003811995042800381WP 1995 4 28 ASAA9580067 119950405A335020131A EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS 53074 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 30 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950428003821995042800382WP 1995 4 28 ASAA9580068 119950406A335060030451 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950428003831995042800383WP 1995 4 28 ASAA9580069 119950406A3350 EEL WIRING DOUG DC9 DC982 3022082WP AFT CATWALK BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRED WIRING TO LIGHT ASSY AND REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003841995042800384WP 1995 4 28 ASAA9580071 119950407A335060030431 EEL BATT PACKS DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK THE OVERHEAD EMERGENCY LIGHTS FROM ROW 16 TO 30 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACKS AT ROWS 16, 20, 24 AND 28 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003851995042800385WP 1995 4 28 ASAA9580072 119950407A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, SEVERAL CATWALK AREA EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950428003861995042800386WP 1995 4 28 ASAA9580073 119950407A33501001191 EEL PORTABLE DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS11552 53449 OAK - DURING C-CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950428003871995042800387EU 1995 4 28 M3HA95006 119950407A3350SM150D19 EEL RELAY AEROSPATR42 ATR42320 8680930EU CABIN MALFUNCTIONED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13988MA 380 HNL - DURING PREFLIGHT PILOT NOTED THAT DC EMERGENCY DISCHARGE ARROW EEL WOULD NOT COME ON. INSPECTED RELAY 58PA CONTACTS. OPERATIONAL TEST IAW JIC 24-00-00-RAI-10020-001. NO DEFECTS NOTED AT THIS TIME. (W) 2H72 4T RTA53EU 19950428003881995042800388EU 1995 4 28 M3HA95007 119950407A3350SM150D19 EEL RELAY AEROSPATR42 ATR42320 8680930EU CABIN MALFUNCTIONED A M3HAK NONE L NO TEST TXTAXI/GRND HDL 1 WP13988MA 380 HNL - FLT 414 - UPON AIRCRAFT SHUTDOWN, PILOT NOTED THE DC EMERGENCY DISCHARGE ARROW EEL WOULD NOT COME ON. REPLACED RELAY 58PA. OPERATIONAL TEST GOOD. (W) 2H72 4T RTA53EU 19950428003891995042800389SW 1995 4 28 MALA954366 119950303A53112720085 FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING ROUTINE MAINTENANCE IN MSP, MAINTENANCE FOUND CARGO DOOR FUSELAGE FRAME CRACKED AT GAS STRUT MOUNT POST HOLE, FS 491. REPAIRED PER FAC ARP 53-20-9503. (W) 1L72 4T A8SW 19950428003901995042800390 1995 4 28 MALA954392 419950331A2360 STATIC WICK DHAV DHC8 DHC8102 2809003NM RT ELEV LOOSE A MALAK NONE O OTHER ININSP/MAINT 1 GL15802MA 245 DURING ROUTINE MAINTENANCE IN DTW, THE RIGHT ELEVATOR STATIC WICK WAS FOUND TO BE LOOSE. MAINTENANCE REPLACED THE TRAILING EDGE SKIN, STATIC WICK, AND BASE IAW SB 8-55-19. (W) 2H72 4T RTA13NM 19950428003911995042800391NM 1995 4 28 TAOA049501 119950401A3260H1010153 DN LOCK SWITCH BOEING727 727225 1384077NM NLG FAILED A TAOAO OTHER N FALSE WARNING APAPPROACH 1 EA15923TS 8107 20441 NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED DOWN. ALL GREEN WERE ILLUMINATED WHEN DOWN SELECTED. NOSE GEAR VISUALLY CONFIRMED DOWN. ABNORMAL PROCEDURES COMPLETED. REPLACED LOCK SWTICH PER MM 32-61-71. OPS CHECK OK. (W) 2L73 4F A3WE 19950428003921995042800392NM 1995 4 28 TWRA9528 119950402A2560803300 ASSIST BOTTLE BOEING747 747212B 1384886NM 4L MED DEPLETED A TWRAK NONE O OTHER ININSP/MAINT 1 EA156186 21439 DURING DAILY INSPECTION, IN JAKARTA, FOUND 4L MED ASSIST BOTTLE READING ZERO PSI. REMOVED AND REPLACED NR 4L ASSIST BOTTLE. (W) 2L74 4F A20WE 19950428003931995042800393WP 1995 4 28 95ZZZX2022 219950404A73201379287L405 HOSE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE DEFECTIVE A AVNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07853JS 730 PIT - FLT 4157 - DURING TAKEOFF ROLL AT APPROXIMATELY 90 KNOTS, CREW NOTICED LEFT ENGINE NOT MAKING ENOUGH TORQUE. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. PIT MAINTENANCE INSPECTED AIRCRAFT AND FOUND A BROKEN P3 AIR SUPPLY LINE, LEFT ENGINE. REPLACED LINE IAW MM 21-10-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19950428003941995042800394EU 1995 4 28 95ZZZX2023 119950406A7712 TQ SIG COND BAG JETSTMJETSTM3101 1500215EU LT ENGINE FAILED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07853JS 730 PIT - FLT 4092 - CREW ABORTED TAKEOFF, LT ENGINE NOT PRODUCING TARGET TORQUE. RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT MAINTENANCE ADJUSTED MAX FUEL FLOW, EGT COMP RESISTOR, AND TORQUE SIGNAL CONDITIONER ALL IAW GARRETT MM 72-00-00. ALSO, CONDUCTED ENGINE GROUND RUNS IAW GARRETT MM 72-00-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950428003951995042800395EU 1995 4 28 95ZZZX2024 119950412A3213B00A703065A GEAR LEG BAG JETSTMJETSTM3101 1500215EU LT MLG DAMAGED A VNAAA UNSCHED LANDING CKJF.O.D. FLUID LOSS WARNING INDICATION CLCLIMB 1 GL07834JS BADL235 726 IPT - FLT 4164 - AIRCRAFT SUFFERED DAMAGE TO LT MLG AS A RESULT OF IMPACTING A DEER ON TAKEOFF FROM IPT, AIRCRAFT DIVERTED TO MDT FOR EMERGENCY LANDING. LT MLG COLLAPSED ON LANDING CAUSING DAMAGE TO LT ENGINE, PROPELLER AND OUTBOARD WING TIP. LT MLG ENGINE AND PROPELLER REPLACED IAW BAE MM, ALL STRUCTURAL REPAIRS CONDUCTED IAW WITH BAE SRM. 2L72 4T RTA21EU 19950428003961995042800396EU 1995 4 28 95ZZZX2025 119950404A29101379305A77 LINE BAG JETSTMJETSTM3101 1500215EU RIGHT DEFECTIVE A VNAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL07833JS 725 FLT 4065 - DURING APPROACH AND PREPARATION FOR LAND ROA, CREW SELECTED GEAR 'DOWN', NO RESPONSE, EXTENDED GEAR AND FLAP WITH EMERGENCY SYSTEM. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED BROKEN HYDRAULIC PRESSURE LINE, RT ENGINE COMPARTMENT, REPLACED DEFECTIVE LINE IAW MM 29-10-15, ALSO, CONDUCTED LOST HYDRAULIC FLUID INSPECTION IAW MM 29-10-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950428003971995042800397SW 1995 4 28 95ZZZX2026 119950406A3110 ANN PANEL SWRNGNSA227 SA227AC 8780603SW COCKPIT LOOSE A CHQAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA233115K AC586 PILOT RETURNED TO FIELD DUE TO ANNUNCIATOR PANEL BEING UNSECURED IN INSTRUMENT PANEL. THE PANEL WAS SECURED AND CHECKED. ALL INDICATIONS WERE NORMAL. 1L72 4T A8SW 19950428003981995042800398WP 1995 4 28 CKSA95015 119950406A2910R124012 HYD LINE DOUG DC8 DC8F54 3021926WP LT WING LEAKING A CKSAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23803CK54514 45610 YIP/SFO - FLT 63060 - EN ROUTE AT 1315Z, LOST ALL MAIN SYSTEM HYDRAULIC PRESSURE, LOST QUANTITY, BUT STILL IN NORMAL RANGE. DECLARED EMERGENCY WITH ATC AND PROCEEDED TO DESTINATION. REPLACED LEAKING HYDRAULIC LINE, PN R124-01-2, AT LEFT AILERON POWER PACK SERVICED HYDRAULIC SYSTEM WITH 500 B-4 SKYDROL IAW DC-8 MM CHAPT. 12-30-1. NO LEAKS NOTED, CYCLED ALL SYSTEMS, HYDRAULIC RESERVOIR FULL. (X) 2L74 4F 4A25 19950428003991995042800399WP 1995 4 28 CKSA95016 119950411A361039216041 PRESS REGULATOR DOUG DC8 DC863F 302198FWP NR 1 ENGINE LEAKING A CKSAO OTHER J WARNING INDICATION CRCRUISE 1 GL23867BX74413 2998 46049 KLRD - FLT 63168 - NR 1 ENGINE FIRE WARNING CAME ON IN-FLIGHT MOMENTARILY, WARNING LIGHT EXTINGUISHED WHEN NR 1 POWER LEVER WAS PULLED BACK TO IDLE. FOUND PRESSURE REGULATOR VALVE LEAKING, REMOVED AND REPLACED PRESSURE REGULATOR VALVE IAW DMM 36-12-1. OPS CHECKED NORMAL IAW DMM 36-12-0. FIRE WARNING OPS CHECKED NORMAL IAW DMM 26-10-0. (X) 2L74 4F 4A25 19950428004001995042800400NM 1995 4 28 PCAA9500203 119950312A3260855401 UPLOCK SWITCH DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A PCAAO OTHER N FALSE WARNING CLCLIMB 1 EA13815EX 321 LEFT MAIN GEAR WILL NOT STAY UP AND LOCKED, GEAR REPEATEDLY UNLOCKS, THEN RETRACTS UP AND LOCKED. REPLACED LT UPLOCK ACTUATOR PROX SWITCH, OPS CHECK GOOD. ACFT RETURNED TO SERVICE. ACTC: 7994. (X) 2H72 4T RTA13NM 19950428004011995042800401NM 1995 4 28 PCAA9500204 119950308A3260841005 PROX CONT BOX DHAV DHC8 DHC8102 2809003NM NLG DOOR FAILED A PCAAO OTHER N FALSE WARNING CLCLIMB 1 EA13801MX205 000448 008 AFTER DEPARTURE AND SELECTING GEAR UP, NOSE GEAR DOOR AMBER LIGHT STAYED LIT, FOLLOWED CHECK LIST, RECYCLED GEAR, NOSE WHEEL DID NOT COME DOWN. PERFORMED ALT GEAR EXT CHECK LIST, THEN RECEIVED 3 GREEN. REMOVED AND REPLACED PSEU DUE TO VARIOUS FAULT INDICATIONS. JACKED NOSE GEAR AND MANUALLY SWUNG GEAR. ALL INDICATIONS NORMAL IN GEAR UP AND GEAR DOWN MODES. SATISFACTORY TEST FLIGHT PERFORMED. ACFT RETURNED TO SERVICE. ACTC: 18377. (X) 2H72 4T RTA13NM 19950428004021995042800402NM 1995 4 28 PCAA9500205 119950308A3231 CONTROL CABLE DHAV DHC8 DHC8102 2809003NM LT MLG DOOR STUCK A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13805AW11250 146 LEFT GEAR DOOR LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. FOUND ALT RELEASE CABLE FOR AFT DOORS HUNG UP ON FWD DOOR ACTUATOR. ROUTED CABLE CORRECTLY AND ADJUSTED FWD DOOR. PROX SWITCH RETRACTION CHECK GOOD. ACFT RETURNED TO SERVICE. ACTC: 12971. (X) 2H72 4T RTA13NM 19950428004031995042800403NM 1995 4 28 PCAA9500206 119950317A323054C546349 SEQ VALVE DHAV DHC8 DHC8102 2809003NM NLG FAILED A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13801MX3292 001039 008 WHEN LANDING GEAR WAS RETRACTED, NOSE GEAR ADVISORY LIGHT REMAINED ON. THE GEAR WAS SELECTED DOWN PER THE CHECK LIST; THE MAIN GEAR CAME DOWN AND LOCKED, THE NOSE GEAR INDICATED UNSAFE. THE CREW PERFORMED AN ALTERNATE EXTENSION. INSPECTED WIRING HARNESS FOR GEAR DOOR PROXIMITY SWITCH, FOUND TO BE OKAY. REMOVED AND REPLACED SEQUENCE SOLENOID VALVE, NOSE GEAR ACTUATOR, AND DRAG BRACE ACTUATOR. CYCLED GEAR SEVERAL TIMES IAW DASH 8 MM; OPERATIONAL CHECK IS GOOD. ACFT RETURNED TO SERVICE. ACTC: 18445. (X) 2H72 4T RTA13NM 19950428004041995042800404EU 1995 4 28 SIMA950921 119950402A532053171122200 WINDSHIELD FRAME AEROSPATR42 ATR42300 8680920EU LT COCKPIT CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21420MQ 012 SAT - MAINTENANCE COMPLYING WITH A BRIDGE INSPECTION FOUND A .25 INCH CRACK ON THE COCKPIT LEFT WINDSHIELD FRAME CORNER, LOWER NODE 5. MAINTENANCE BLENDED OUT THE CRACK AND SHOT PEENED IAW ATR FAX REF NR DS/ET 531.54/95. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950428004051995042800405EU 1995 4 28 SIMA950922 119950402A532053171122201 WINDSHIELD FRAME AEROSPATR42 ATR42300 8680920EU RT COCKPIT CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21420MQ 012 SAT - MAINTENANCE COMPLYING WITH A BRIDGE INSPECTION WHICH FOUND A .25 INCH CRACK ON THE COCKPIT RIGHT WINDSHIELD FRAME CORNER, LOWER NODE 5. MAINTENANCE BLENDED OUT THE CRACK AND SHOT PEENED IAW ATR FAX REF NR DS/ET 531.54/95. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950428004061995042800406EU 1995 4 28 SIMA950931 119950403A32465101469 WHEEL 5010488 SAAB SF340 340B 7860101EU MLG CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21329AE2860 JUL920671 340B329 LAW/SHOP - DURING TEAR DOWN AND INSPECTION OF WHEEL ASSEMBLY FOR TIRE REPLACEMENT IN THE SHOP, A .50 INCH CRACK WAS FOUND BY NDT. INSPECTION, TRAVELING ACROSS THE OUTER FLANGE RING IN THE AREA OF THE MFG. SN. THE FLANGE RING WAS REMOVED FROM SERVICE. PART TOTAL CYCLES 2970. PART TIME SINCE 137FH/193 CYC. (X) 2L72 4T RTA52EU 19950428004071995042800407EU 1995 4 28 SIMA950941 119950404A5320S53171101204 WINDOW FRAME AEROSPATR42 ATR42300 8680920EU COCKPIT CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 SAT - DURING A 24,000 CYCLE INSPECTION, EDDY CURRENT INSPECTION REVEALED A .25 INCH CRACK ON THE VERTICAL PLANE OF THE NODE 5 LEFT WINDOW FRAME. MAINTENANCE BLENDED THE CRACK IAW ATR DRAWING NR 11S53140122. THE AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950428004081995042800408EU 1995 4 28 SIMA950942 119950404A5320S53171101205 WINDOW FRAME AEROSPATR42 ATR42300 8680920EU COCKPIT CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 SAT - DURING A 24,000 CYCLE INSPECTION, EDDY CURRENT INSPECTION REVEALED A .25 INCH CRACK IN THE VERTICAL PLANE OF NODE 5 RIGHT WINDOW FRAME. MAINTENANCE BLENDED OUT THE CRACK IAW ATR DRAWING NR 11S53140122. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950428004091995042800409EU 1995 4 28 VTZA95141 119950413A3240190287 CONTROL CABLE JETAIRJETSTMJETSTM4101 1500501EU PARKING BRAKE LACK OF LUBE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27302UE 41013 IAD/BTV - FLT 6267 - DURING TAKEOFF AT 2210 HRS ON 4-13-95, ABORTED TAKEOFF DUE TO CONFIGURATION WARNING DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE LUBED THE PARKING BRAKE CABLE ASSEMBLY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428004101995042800410EU 1995 4 28 VTZA95142 119950414A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILURE A VTZAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27308UE 41023 DWN/IAD - FLT 6578 - DURING CRUISE AT 1815 HRS ON 4-14-95, RETURNED TO IAD DUE TO RT GENERATOR FAILING IN-FLIGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT START/GEN. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428004111995042800411EU 1995 4 28 VTZA95143 119950415A3260P302A701835 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR LOOSE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27301UE 41012 IAD/TYS - FLT 6160 - DURING CLIMBOUT AT 1250 HRS ON 4-15-95, THE INTRANSIT LIGHT ON THE GEAR HANDLE ILLUMINATED. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED ALL MICROSWITCHES AND CANNON PLUGS WITH NO DEFECTS NOTED. RESEATED CANNON PLUG ON THE GEAR HANDLE. PERFORMED 6 GEAR SWINGS, OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428004121995042800412 1995 4 28 VTZA95144 319950416A6140310389813 PRESS SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27308UE 41023 EWR/IAD - FLT 6472 - DURING TAKEOFF AT 1700 HRS ON 4-16-95, ABORTED TAKEOFF DUE TO RT RED BETA LIGHT ILLUMINATING ON TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. EWR CONTRACT MAINTENANCE REPLACED THE BETA PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950428004131995042800413SO 1995 4 28 WTAA950136 119950324A5350 RADOME EMB 120 EMB120RT SO FWD FUSELAGE LIGHTNING STRIKEA WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17455UE 120163 PDX - LIGHTNING STRIKE REPORTED ON RADOME. MAINTENANCE INSPECTED AIRCRAFT PER EMBRAER EMB-120RT MM 05-50-01. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004141995042800414SO 1995 4 28 WTAA950138 119950326A527012035399001 BRACKET EMB 120 EMB120RT SO CARGO DOOR CRACKED A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17275UE 120058 FAT - CARGO DOOR WARNING LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE DEFERRED DOOR WARNING SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED AFT CARGO DOOR MICROSWITCH BRACKETS. OPERATIONAL CHECK OF CARGO DOOR INDICATION SYSTEM NORMAL. (X) 2L72 4T RTA31SO 19950428004151995042800415SO 1995 4 28 WTAA950141 119950328A5330 SKIN EMB 120 EMB120RT SO FWD FUSELAGE BIRD STRIKE A WTAAK NONE C F.O.D. TOTAKEOFF 1 WP17288UE 120184 SFO - POSSIBLE BIRD STRIKE REPORTED ABOVE FIRST OFFICER'S WINDSCREEN DURING TAKEOFF AT FAT. MAINTENANCE INSPECTED AIRCRAFT. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004161995042800416SO 1995 4 28 WTAA950142 119950329A5400 NACELLE EMB 120 EMB120RT SO RT ENGINE BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17287UE 120183 SFO - BIRD STRIKE REPORTED AT RIGHT ENGINE NACELLE. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. FOUND SMALL DENT IN INBOARD RT ENGINE INLET COWL ACCESS PANEL. REMOVED DENT FROM PANEL. NO OTHER DAMAGE NOTED TO AIRCRAFT. RETURNED AIRCRAFT TO SERVICE. (X) 2L72 4T RTA31SO 19950428004171995042800417EU 1995 4 28 WTAA950146 119950330A32301862F RADIUS ROD BAG JETSTMJETSTM3101 1500215EU RT MLG WORN A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17424UE 796 LAX - RIGHT MLG 'GREEN' INDICATION REMAINS ILLUMINATED WITH GEAR RETRACTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RT MLG RADIUS ROD ASSEMBLY. LANDING GEAR POSITION INDICATIONS NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950428004181995042800418SO 1995 4 28 WTAA950147 119950331A275024A00534805 CONNECTOR EMB 120 EMB120RT SO RT TE FLAP CORRODED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17120AM 120012 LAX - OUTBOARD FLAP FAULT REPORTED DURING FLAP RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND CORROSION ON RIGHT OUTBOARD FLAP ACTUATOR CANNON PLUG. CLEANED CANNON PLUG PINS. FLAP SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004191995042800419SO 1995 4 28 WTAA950148 119950401A3260922AA2Y6A6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17269UE 120194 SFO - LEFT MLG 'A' AND 'B' SYSTEM INTRANSIT LIGHTS ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MLG 'A' AND 'B' SYSTEM DOWNLOCK PROXIMITY SENSORS. LANDING GEAR POSITION INDICATIONS NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004201995042800420SO 1995 4 28 WTAA950149 119950403A3220 LANDING GEAR EMB 120 EMB120RT SO NLG BIRD STRIKE A WTAAK NONE C F.O.D. LDLANDING 1 WP17276UE 120067 FAT - BIRD STRIKE REPORTED AT NLG DURING LANDING. MAINTENANCE INSPECTED AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004211995042800421NE 1995 4 28 WTAA950150 219950403A7250310900301 TURBINE BLADE 3035913E EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A WTAAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION TXTAXI/GRND HDL 1 WP17274UE12533 15A556 120054 115413 RNO - VIBRATION AND POWER LOSS REPORTED FROM LEFT ENGINE WHEN PROPELLER WAS BROUGHT OUT OF FEATHER AFTER LANDING. MAINTENANCE REMOVED AND REPLACED LT ENGINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENT INVESTIGATION REVEALED PT-1 DISK BLADE FAILURE TO BE CAUSE OF ENGINE VIBRATION AND LOSS OF POWER. (X) 2L72 4T4 TRTA31SO E20NE 19950428004221995042800422SO 1995 4 28 WTAA950151 119950405A323012038594001 CONTROL MODULE EMB 120 EMB120RT SO LANDING GEAR FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17269UE 120194 RDD - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR MAINTENANCE. REPLACED LANDING GEAR CONTROL MODULE. LANDING GEAR OPERATION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950428004231995042800423WP 1995 4 28 9506391158 119950421A5220 L3 DOOR DOUG DC10 DC1040 3023508WP FS 1305 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE DOOR 3L AFT LOWER LIGHTENING HOLE AT FS 1305. STOP DRILLED CRACK AND INSTALLED DOUBLER. 2L73 4F A22WE 19950428004241995042800424NM 1995 4 28 9506416613 119950424A5312 BLKHD WEB BOEING747 747251B 1384892NM FS 1480 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, THE LEFT BODY GEAR WHEEL WELL BULKHEAD WEB AT FS 1480 WAS FOUND CORRODED. REMOVED CORROSION, ROTO PEENED, TREATED, PRIMED, AND INSTALLED STRUCTURE PER EA 66-98011. 2L74 4F A20WE 19950428004251995042800425NM 1995 4 28 9506425517 119950406A5320 THRESHOLD BOEING757 757251 1384970NM FS 1380-1440 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01517US 28357 23205 DURING PERIODIC CHECK, THE AFT CARGO THRESHOLD BEAM CHORD WAS FOUND CORRODED AROUND NUTPLATE HOLES AT FS 1380 TO 1440, RBL 20. REMOVED CORROSION AND INSTALLED REPAIR PER NWA EA 55-98173. (MFG PART NO. 146N8522-51) 2L72 4F RTA2NM 19950428004261995042800426WP 1995 4 28 9506431158 119950424A5220 R3 DOOR DOUG DC10 DC1040 3023508WP FS 1260-1305 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, CRACKS WERE FOUND IN THE FORWARD AND AFT LOWER DOOR 3R STRUCTURE AT FS 1260 AND 1305. STOP DRILLED AND INSTALLED DOUBLER. 2L73 4F A22WE 19950428004271995042800427WP 1995 4 28 9506441158 119950424A5347 SEAT TRACK DOUG DC10 DC1040 3023508WP FS 440-485 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 440 - 485, RBL 9. REPLACED SEAT TRACK. 2L73 4F A22WE 19950428004281995042800428NE 1995 4 28 9506451156 219950424A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 3 ENGINE STALLED A NWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 GL01156US 46765 686148 DURING DESCENT WITH THE POWER LEVERS RETARDED, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH A RISE IN EGT FOLLOWED BY A FLAMEOUT. A RELIGHT WAS SUCCESSFUL AND ENGINE OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND FUEL PRESSURES WERE FOUND TO BE OK. A PRBC CHANGE, FLOW DIVIDER CHANGE, AND A BOROSCOPE ARE SCHEDULED. 2L73 4F4 F A22WE E20EA 19950428004291995042800429WP 1995 4 28 9506469103 119950421A2130 CONNECTOR DOUG DC9 DC915 3022036WP PRESS SYST BROKEN A NWAAB EMER. DESCENT O OTHER DEDESCENT 1 GL0193S 47078 LOSS OF CABIN PRESSURIZATION OCCURRED ON DESCENT INTO SYR. EMERGENCY DESCENT PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN CANNON PLUG TO AUGMENTATION VALVE SOLENOID 'A'. ALSO, REPLACED FLOW CONTROL VALVE AND PILOT PRESSURE REGULATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004301995042800430WP 1995 4 28 9506479152 119950422A3260 DOOR SWITCHES DOUG DC9 DC914 3022034WP MLG CONTAMINATED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL018911E 45825 DURING APPROACH INTO RIC, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND LIGHT STAYED ON. PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED MAIN GEAR DOOR SWITCHES. ALSO, CHECKED WIRING AND CANNON PLUGS. CYCLED DOORS SEVERAL TIMES AND ALL INDICATIONS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004311995042800431WP 1995 4 28 9506489152 119950423A3260 UPLOCK SWITCH DOUG DC9 DC914 3022034WP LT MLG MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL018911E 45825 DURING APPROACH INTO DTW, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED FOR LANDING. EXECUTED GO-AROUND PROCEDURES AND PERFORMED EMERGENCY EXTENSION PROCEDURES. REPLACED LEFT MAIN GEAR DOOR UPLOCK SWITCH. ALSO, REPLACED THE LEFT AND RIGHT GEAR DOOR SKIDS DUE TO DAMAGE ON LANDING. OPERATIONAL CHECK GOOD ON DOOR CYCLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004321995042800432NM 1995 4 28 9506492204 119950422A3260 INDICATION BOEING727 727251 138408HNM TAIL SKID MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 GL01204US 22544 DURING DEPARTURE CLIMB UPON PLACING GEAR HANDLE IN 'OFF' POSITION, TAIL SKID INDICATION REMAINED ILLUMINATED. JETTISONED 6000 LBS OF FUEL AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE VERIFIED INDICATION NOT DUE TO TAIL STRIKE. DEFERRED TAIL SKID INDICATION PER MEL 32-13. 2L73 4F A3WE 19950428004331995042800433NM 1995 4 28 9506502707 119950423A2530 OVEN BOEING727 727225 1384077NM CABIN DIRTY A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01816EA 22553 DURING CLIMB, FLIGHT ATTENDANT REPORTED SMOKE FROM FIRST CLASS OVEN 2-7B. PULLED CIRCUIT BREAKERS AND SMOKE DISSIPATED. NO FLAMES WERE NOTICED. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED DEBRIS AND GREASE FROM OVEN. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950428004341995042800434WP 1995 4 28 9506511155 119950424A3150 SWITCH DOUG DC10 DC1040 3023508WP SPEED BRAKE LACK OF LUBE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01155US 46764 DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. LUBED AND CYCLED SPEED BRAKE HANDLE SWITCH MECHANISM. 2L73 4F A22WE 19950428004351995042800435WP 1995 4 28 9506529907 119950420A3010 VALVE DOUG DC9 DC931 3022065WP AIRFOIL DE-ICE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL01957N 47253 AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WHEN ANTI-ICE WAS ACTIVATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE PRESSURE REGULATOR VALVE AND SHUTOFF VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004361995042800436WP 1995 4 28 9506539908 119950420A3231 CONTROL CABLE DOUG DC9 DC931 3022065WP NLG DOOR BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01958N 47254 A LOUD 'BANG' WAS HEARD WITH SUBESQUENT VIBRATION DURING GEAR RETRACTION AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CLE. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. FOUND LEFT NOSE GEAR DOOR STOP CABLE BROKEN. DEFERRED STOP CABLE PER MEL32-7. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004371995042800437WP 1995 4 28 9506549928 119950421A2780 T DUCTS DOUG DC9 DC931 3022065WP LE FLAPS LACK OF LUBE A NWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL018921E 45836 DURING APPROACH INTO DFW, SLAT EXTEND LIGHT DID NOT ILLUMINATE WHEN SLATS WERE SELECTED AND FLAPS AT 5 DEGREES. EXECUTED TO-AROUND AND RECYCLED FLAPS/SLATS. SLAT EXTEND LIGHT OPERATED NORMALLY. AIRCRAFT LANDED WITHOUT INCIDENT. LUBED SLAT 'T' DUCTS AND CYCLED FLAPS/SLATS SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004381995042800438NM 1995 4 28 9506556613 119950425A5330 SKIN BOEING747 747251B 1384892NM NLG WW CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, THE NOSE WHEEL WELL ACCESS RIGHT FORWARD HINGE FAIRING WAS FOUND CRACKED. REMOVED CRACK FROM OUTER SKIN, STOP DRILLED CRACK ON INNER SKIN. INSTALLED DOUBLER AND TRIPLER AND QUADRUPLER PER SA 5311-01064-6. 2L74 4F A20WE 19950428004391995042800439WP 1995 4 28 9506569951 119950421A2820 VENT VALVE DOUG DC9 DC932 3022066WP LT WING TANK MALFUNCTIONED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 GL019347 45827 FUEL BEGAN LEAKING FROM RIGHT WING TANK EN ROUTE PVD-DTW. LEAK WAS APPROXIMATELY 1600 LBS IN ONE HOUR. FLIGHT DIVERTED TO BUF AND LANDED WITHOUT INCIDENT. REPLACED CLIMB VENT VALVE IN LEFT MAIN FUEL TANK. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004401995042800440 1995 4 28 9506579966 419950421A3418 COMPUTER DOUG DC9 DC931 3022065WP NR 1 STALL WARN MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL019330 47138 STALL GLARESHIELD LIGHT AND STICK SHAKER ACTIVATED AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 STALL WARNING COMPUTER AND TRANSDUCER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004411995042800441WP 1995 4 28 9506589969 119950420A3260 DOOR LATCH DOUG DC9 DC931 3022065WP LANDING GEAR OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL019333 47246 DURING CLIMB-OUT FROM ROC, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FOUND RIGHT DOOR SWITCH SLIPPING OFF HEAD OF STRIKER BOLT (BAD ALIGNMENT). ADJUSTED DOOR LATCH/STRIKER MECHANISM. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004421995042800442WP 1995 4 28 9506599971 119950423A2780 T DUCTS DOUG DC9 DC931 3022065WP LE FLAPS LACK OF LUBE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL019335 47337 DURING APPROACH INTO PIT, SLAT DISAGREEMENT LIGHT ILLUMINATED UPON SELECTION OF SLATS AND FLAPS. CAPTAIN DECLARED AN EMERGENCY AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. LUBED SLAT 'T' DUCTS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004431995042800443WP 1995 4 28 9506609997 119950422A21505910244125 AIR COND DUCT DOUG DC9 DC931 3022065WP CABIN BLOWN A NWAAGB O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL018933E 47142 LOSS OF CABIN PRESSURIZATION OCCURRED AT 35,000 FEET EN ROUTE MEM-HOU. CABIN PRESSURE WARNING LIGHT ILLUMINATED AND EMERGENCY DESCENT WAS MADE TO 8,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN. PRESSURE WAS REGAINED AND FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. FOUND BLOWN AIR CONDITIONING DUCT. REPLACED THE CHECK VALVE AND DUCT ASSEMBLY. OPERATIONAL CHECK OK ON VESSEL LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. DATE 950423 CHANGED TO 950422. 2L72 4F A6WE 19950428004441995042800444WP 1995 4 28 9506619902 119950422A2130 CLAMP DOUG DC9 DC931 3022065WP WATER SEPARATOR LOOSE A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01952N 47073 LOSS OF CABIN PRESSURE OCCURRED AT 33,000 FEET EN ROUTE MSP-HOU. OXYGEN MASKS WERE DEPLOYED THROUGH CABIN. EMERGENCY DESCENT WAS ACCOMPLISHED AND CABIN PRESSURE WAS REGAINED. FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. FOUND CLAMP ON AFT SIDE OF WATER SEPARATOR LOOSE AND NOT POSITIONED PROPERLY. REPLACED CLAMP. ALSO, REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950428004451995042800445EU 1995 4 28 9506623201 119950423A3230 BOLT AIRBUS320 A320211 3930320EU NLG LOOSE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01301US 31 DURING CLIMB-OUT FROM MKE, THE NOSE LANDING GEAR WOULD NOT RETRACT. BOTH THE GREEN DOWN AND LOCKED AND RED IN TRANSIT INDICATION LIGHTS ILLUMINATED. THE MAIN LANDING GEAR RETRACTED AND THE NOSE LANDING GEAR DOORS INDICATED OPEN. THE LANDING GEAR WAS CYCLED AND ALL INDICATIONS REMAINED THE SAME. THE AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED A LOOSE BOLT SECURING THE NOSE LANDING GEAR PROXIMITY SENSOR ASSEMBLY. TIGHTENED BOLT. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950428004461995042800446 1995 4 28 9506631145 419950423A221137570818 ROLL COMPUTER DOUG DC10 DC1040 3023508WP AUTO PILOT MALFUNCTIONED A NWAAK NONE F FLT CONT AFFECTED DEDESCENT 1 GL01145US16714125 46754 DURING DESCENT WHEN DEPLOYING SPEEDBRAKES, AIRCRAFT ROLLED TO THE LEFT. VISUAL AND OPERATIONAL CHECK WAS NORMAL, NO FAULTS FOUND AND AUTO-PILOT BITE CHECK WAS NORMAL. RIGGED SPOILER CABLES AND REPLACED THE ROLL COMPUTER. 2L73 4F A22WE 19950428004471995042800447WP 1995 4 28 95UALD10037 119950424A3350MB10P1 EEL CONNECTOR DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN DIRTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP291853U 47812 EEL LIGHT AT DOOR 1 CROSS AISLE INOP. EEL CONNECTORS ON FLOOR SOAKED WITH WATER AND DIRTY. CLEANED AND DRIED CONNECTORS. 2L73 4F4 F A22WE E23EA 19950428004481995042800448WP 1995 4 28 95UALD10038 119950424A32465000414 WHEEL HALF DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL RT NLG FAILED A UALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP291814U 46613 RETURNED TO BLOCKS, RT NOSE TIRE WENT FLAT ON TAXI OUT (RT NOSE TIRE RIM FAILED). REPLACED BOTH NOSE WHEELS AND TIRES AND INSPECTED THE AREA FOR DAMAGE. 2L73 4F4 F A22WE E23EA 19950428004491995042800449WP 1995 4 28 95UALD10039 119950424A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291839U 46633 FOUND SECTION OF EEL LIGHTING INTERMITTENT BY DOOR 2R FIRST EEL SECTION GOING AFT. REPLACED FEEDER CABLE. 2L73 4F4 F A22WE E23EA 19950428004501995042800450WP 1995 4 28 ABXA9500335 119950221A571339112361 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 12 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950428004511995042800451WP 1995 4 28 ABXA9500336 119950421A57133911236501 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 15 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950428004521995042800452WP 1995 4 28 ABXA9500337 119950421A57133911238511 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORRROSION ON STRINGER NR 18 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950428004531995042800453WP 1995 4 28 ABXA9500338 119950421A57133911238503 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 22 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950428004541995042800454WP 1995 4 28 ABXA9500339 119950421A571399193691 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE IN STRINGER NR 22. REMOVED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950428004551995042800455WP 1995 4 28 ABXA9500340 119950421A571399193691 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE IN STRINGER NR 16. REMOVED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950428004561995042800456WP 1995 4 28 ABXA9500341 119950420A2420S4913802A5 CROSSFEED CABLE DOUG DC9 DC932 3022066WP FS 598 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND LEVEL I CORROSION ON BOTH CROSSFEED CABLES AT STA 598, JUST BELOW LONGERON 19R. CLEANED CABLES IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950428004571995042800457WP 1995 4 28 ABXA9500342 119950418A5320NAS1097 RIVET DOUG DC9 DC932 3022066WP FS 69 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND TWO EACH DEFECTIVE RIVET HEADS ON NOSE SECTION AT APPROXIMATELY STA 69, BETWEEN LEFT AND CENTER PITOT TUBES. REPLACED RIVETS IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004581995042800458WP 1995 4 28 ABXA9500343 119950421A5320NAS1473A3 NUT DOUG DC9 DC932 3022066WP FS 598 BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS JUST AFT OF STA 598, AT LONGERON 18L. REPLACED DOME NUTS IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004591995042800459WP 1995 4 28 ABXA9500344 119950421A5320NA1473A3 NUT DOUG DC9 DC932 3022066WP FS 658 PUNCTURED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND DOME NUTS JUST AFT OF STA 658, LONGERON 18L, PUNCTURED. REPLACED DOME NUTS IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004601995042800460WP 1995 4 28 ABXA9500345 119950421A5320NAS1473A3 NUT DOUG DC9 DC932 3022066WP FS 658 INCORRECT A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND INCORRECT FASTENER IN PLACE OF DOME NUT JUST AFT OF STA 658, LONGERON 18R. REPLACED FASTENER IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004611995042800461WP 1995 4 28 ABXA9500346 119950421A5320NA1473A3 NUT DOUG DC9 DC932 3022066WP FS 718-737 BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS AT STA 718 - 737, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004621995042800462WP 1995 4 28 ABXA9500347 119950421A5320NAS1473A3 NUT DOUG DC9 DC932 3022066WP FS 756 BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUT JUST AFT OF STA 756, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004631995042800463WP 1995 4 28 ABXA9500348 119950421A5320NAS1473A3 NUT DOUG DC9 DC932 3022066WP FS 680-699 BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND BROKEN DOME NUTS AT STA 680 - 699, LONGERON 18R. REPLACED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004641995042800464WP 1995 4 28 ABXA9500349 119950420A5320991050143 MEMBRANE DOUG DC9 DC932 3022066WP FS 598 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND CUSP MEMBRANE CRACKED JUST FORWARD OF STA 598L. REPAIRED CUSP MEMBRANE IAW DC-9 SRM 53-01, 51-30-2. 2L72 4F A6WE 19950428004651995042800465WP 1995 4 28 ABXA9500350 119950420A532099101515 MEMBRANE DOUG DC9 DC932 3022066WP FS 598 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND LEFT CUSP MEMBRANE CRACKED AT STA 598. REPLACED CUSP MEMBRANE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950428004661995042800466WP 1995 4 28 ABXA9500351 119950425A3241422551 CONTROL BOX DOUG DC9 DC941 302207NWP ANTI-SKID SYST DEFECTIVE A ABXAO OTHER J WARNING INDICATION LDLANDING 1 GL23954AX30967153 47612 ALL FOUR ANTI-SKID LIGHTS ILLUMINATED AFTER GEAR EXTENSION. RECYCLED SWITCH AND CHECKED CIRCUIT BREAKERS. NO EFFECT. LIGHTS WENT OUT ON THEIR OWN ABOUT TWO MINUTES LATER. ALSO RECYCLED GEAR. REPLACED ANTI-SKID CONTROL BOX IAW DC-9 MM 32-43-4. OPS CHECKED NORMAL. 2L72 4F A6WE 19950428004671995042800467WP 1995 4 28 ABXA9500352 119950426A532099579061 WEB DOUG DC9 DC932 3022066WP FS 427 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, FOUND HOLES DRILLED IN WEB AROUND LIGHTENING HOLE AT APPROXIMATELY STA 427, LONGERON 25R JUST ABOVE DOOR LOCKING CAM. REPAIRED IAW ABX REA D953-11484-MR. 2L72 4F A6WE 19950428004681995042800468WP 1995 4 28 ABXA9500353 119950423A531199196431 FRAME DOUG DC9 DC932 3022066WP FS 639 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 94-03-01, FOUND FRAME AT STA 639 CRACKED AT AFT OUTBOARD FLANGE BETWEEN LONGERONS 15L AND 16L. REPAIRED IAW ABX REA D953-11469-MR. 2L72 4F A6WE 19950428004691995042800469WP 1995 4 28 MWEA95186 119950424A71105910298501 INLET COWL DOUG DC9 DC914 3022034WP LT ENGINE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING ROUTINE INSPECTION A .5 INCH CRACK WAS FOUND ON LEFT ENGINE INLET LEADING EDGE SKIN. REPLACED LEFT ENGINE INLET. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950428004701995042800470EU 1995 4 28 QXEA9500127 119950425A33501820 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 GEG - RIGHT OVERWING EXIT 28V LIGHT INOP. RELACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950428004711995042800471NM 1995 4 28 QXEA9500128 119950425A3350MS1557081 EEL BULB DHAV DHAV DHC8 DHC8102 2809003NM UNDER WING FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09841PH 82 GEG - RIGHT AFT UNDER WING EGRESS LIGHT INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950428004721995042800472NM 1995 4 28 SCNA95059 119950415A5315 FLOOR BEAM BOEING727 727225 1384077NM BS 344 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15283SC 22559 DURING C-CHECK, THE FLOOR BEAM AND WEB LOCATED AT BS 344, LBL 5 TO RBL 5 WAS FOUND WITH CORROSION. REPAIR MEMBERS WERE FABRICATED AND INSTALLED IAW B727 SRM 53-10-8. 2L73 4F A3WE 19950428004731995042800473NM 1995 4 28 SCNA95060 119950419A3231661516623 CONTROL CABLE BOEING727 7272A1 138407FNM NLG DOOR OUT OF ADJ A SCNAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 GL15286SC 21601 NOSE GEAR DOOR LIGHT ON WITH GEAR DOOR CLOSED. FOUND FORWARD NOSE GEAR DOORS CABLE BELOW TENSION LIMITS. ADJUSTED GEAR DOORS CABLE PER 32-22-01, PAGE 501. OPS CHECK GOOD. 2L73 4F A3WE 19950428004741995042800474WP 1995 4 28 SCNA95061 119950421A5240M61006 CONNECTOR DOUG DC10 DC1010 3022110WP DOOR SWITCH DIRTY A SCNAK NONE P NO WARNING INDICATION UKUNKNOWN 1 GL15907WA 46946 UNABLE TO ARM R-3 AND R-4 DOORS. CYCLED R-3 DOOR, DOOR ARMED PROPERLY WITH R-3 DOOR LIGHT OFF. CLEANED R-4 DOOR SWITCH CANNON PLUG, R-4 DOOR OPERATIONAL CHECKED GOOD. 2L73 4F A22WE 19950428004751995042800475NM 1995 4 28 SCNA95062 119950423A323065727621 RETRACT MECH BOEING727 7272J4 1384006NM NLG MALFUNCTIONED A SCNAK NONE J WARNING INDICATION DEDESCENT 1 GL15288SC 20765 LANDING GEAR REQUIRED ONE RECYCLE TO GET NOSE GEAR TO COME DOWN. FIRST ATTEMPT MAIN LANDING GEAR INDICATED DOWN AND LOCKED, BUT NOSE DOORS AND GEAR REMAINED IN UP POSITION. PERFORMED NOSE GEAR SWING IAW 7-11-00, OPS CHECKED OK. 2L73 4F RTA3WE 19950428004761995042800476NM 1995 4 28 SWAA950296 119950415A5320 DOOR FRAME BOEING737 7375H4 138449DNM CARGO COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07502SW 24179 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CRACKED AT FWD LWR SIDE NEXT TO RELEASE UPLOCK HOOK. REPAIRED PER SWA ACO 3194-52. 2L72 4F RTA16WE 19950428004771995042800477NM 1995 4 28 SWAA950297 119950415A5330 SKIN BOEING737 7375H4 138449DNM RT FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07502SW 24179 DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT FUSELAGE SKIN CRACKED AT STRINGER S16R AT WING SCANNING LIGHT CUTOUT, AT AFT END OF FWD SECTION. REPAIRED PER SWA ACO 6405-53. 2L72 4F RTA16WE 19950428004781995042800478NM 1995 4 28 SWAA950298 119950415A5320 BELTFRAME BOEING737 7375H4 138449DNM BS 482 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07502SW 24179 DURING SCHEDULED 1/2 D CHECK, FOUND BELTFRAME CRACKED .125 INCHES AT RIVET HOLE, BS 482, RBL 1. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950428004791995042800479NM 1995 4 28 SWAA950299 119950415A5320 WEB BOEING737 7375H4 138449DNM BS 460 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07502SW 24179 DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO DOOR CUTOUT WEB CRACKED AT BS 460, LWR AFT CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950428004801995042800480NM 1995 4 28 SWAA950300 119950415A5315 FLOOR BEAM BOEING737 7375H4 138449DNM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07502SW 24179 DURING SCHEDULED 1/2 D CHECK, FOUND FWD CARGO FLOOR BEAM CRACKED AT BS 400, LBL 21.0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950428004811995042800481NM 1995 4 28 UPS202964 119950423A5753 TE WEDGE BOEING727 727180C 138406GNM LT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING INBOARD MID FLAP TRAILING EDGE WEDGE ON THE LOWER SURFACE 45 INCHES FROM THE OUTBOARD END, THE OTHER IS 85 INCHES FROM THE OUTBOARD END. MAINTENANCE REMOVED THE DELAMINATED SKIN, REPAIRED CORE AND REFINISHED PER SRM 51-40-6. 2L73 4F A3WE 19950428004821995042800482NM 1995 4 28 UPS202965 119950423A5753 SKIN BOEING727 727180C 138406GNM RT TEFORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION AT THE INBOARD AFT CORNER OF THE RIGHT WING INBOARD FORE FLAP. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED PER SRM 51-40-6. 2L73 4F A3WE 19950428004831995042800483NM 1995 4 28 UPS202966 119950423A5753 SKIN BOEING727 727180C 138406GNM LT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD FORE FLAP. MAINTENANCE REMOVED THE DAMAGED AREA AND REPAIRED PER SRM 51-40-6. 2L73 4F A3WE 19950428004841995042800484NM 1995 4 28 UPS203023 119950423A5320 ANGLE BOEING727 727180C 138406GNM FS 580 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE ANGLE ATTACHING THE OUTER SKIN TO FRAME ON TOP OF THE MAIN CARGO DOOR AT STATION 580. MAINTENANCE REMOVED THE CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED WET WITH SEALANT. INSTALLED ALL FASTENERS WET WITH SEALANT IAW SRM 51-30-2 AND 51-20-1. 2L73 4F A3WE 19950428004851995042800485NM 1995 4 28 UPS203024 119950423A5754 LUG BOEING727 727180C 138406GNM LT LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 1 K-FLAP INBOARD BULLNOSE LINKAGE ROD LUG. MAINTENANCE BLENDED THE CORROSION AND REPLACED THE NUMBER 1 K-FLAP IAW SRM 57-50-1 AND MM 27-81-01. 2L73 4F A3WE 19950428004861995042800486NM 1995 4 28 UPS203025 119950423A5753 TE SKIN BOEING727 727180C 138406GNM TE AFT FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION AT THE TRAILING EDGE OF THE RIGHT WING OUTBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED PORTION OF THE AFT FLAP AND INSTALLED REPAIR MATERIAL IAW SRM 51-40-6 AND MM 51-20-151. 2L73 4F A3WE 19950428004871995042800487NM 1995 4 28 UPS203026 119950423A5752 SKIN BOEING727 727180C 138406GNM RT AILERON TAB CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT WING OUTBOARD AILERON TAB ON THE INBOARD NOSE SKIN AND 4TH NOSE SKIN FROM THE INBOARD END. MAINTENANCE REMOVED THE DAMAGED SKIN, FABRICATED REPAIR PARTS, INSTALLED AND TREATED PER SRM 51-30-2 AND 51-20-1. 2L73 4F A3WE 19950428004881995042800488NM 1995 4 28 UPS203027 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUEL TANK AT STATION 850 TO 745, LBL 1 TO 24 AND WL 204 TO 190. MAINTENANCE REMOVED THE CORROSION AND REPAIRED IAW UPS EO 727-57-1347. 2L73 4F A3WE 19950428004891995042800489NM 1995 4 28 UPS203028 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 783 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUEL TANK AT STATION 783 TO 804, RBL 45 TO 62 AND WL 197. MAINTENANCE BLENDED THE CORROSION AND REPAIRED PER UPS EO 727-57-1347. 2L73 4F A3WE 19950428004901995042800490NM 1995 4 28 UPS203029 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 804 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF THE FUEL CENTER TANK AT STATION 804 TO 826, RBL 45 TO 62 AND WL 193. MAINTENANCE REMOVED THE CORROSION AND REPAIRED PER UPS EO 727-57-1347. 2L73 4F A3WE 19950428004911995042800491NM 1995 4 28 UPS203030 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 745 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUEL CELL AT STATION 745 TO 747, LBL 55 TO 56 AND WL 204. MAINTENANCE REMOVED THE CORROSION AND REPAIRED PER UPS EO 727-57-1347. 2L73 4F A3WE 19950428004921995042800492NM 1995 4 28 UPS203031 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 774 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUEL CELL AT STATION 774, LBL 53 AND WL 202. MAINTENANCE BLENDED CORRODED AREA AND REPAIRED PER UPS EO 727-57-1347. 2L73 4F A3WE 19950428004931995042800493NM 1995 4 28 UPS203032 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 804 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUEL TANK AT STATION 804 TO 826, LBL 45 TO 62 AND WL 196. MAINTENANCE BLENDED CORROSION AND REPAIRED PER UPS EO 727-57-1347. 2L73 4F A3WE 19950428004941995042800494NM 1995 4 28 UPS203033 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND EXPANSION LINK AT STATION 740 TO 760 AND LBL 62. MAINTENANCE REMOVED THE OLD LINK AND INSTALLED WITH NEW EXPANSION PER SRM 51-10-1, 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950428004951995042800495NM 1995 4 28 UPS203034 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS AND CORROSION THROUGHOUT THE LEFT PRESSURE BOX AT STATION 740 TO 758. MAINTENANCE FABRICATED THE SKIN IAW SRM 51-20-1 AND 53-10-2 AND INSTALLED SKIN PER 51-30-2. 2L73 4F A3WE 19950428004961995042800496NM 1995 4 28 UPS203035 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK FITTING AT STATION 740, BL 0 AND WL 206. MAINTENANCE REMOVED THE CORRODED FITTING AND INSTALLED WITH NEW FITTING IAW SRM 51-30-2 AND 51-10-1. 2L73 4F A3WE 19950428004971995042800497NM 1995 4 28 UPS203036 119950423A5753 CHORD BOEING727 727180C 138406GNM RT TE MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE LOWER AFT CHORD OF THE RIGHT WING INBOARD MID FLAP, OUTBOARD AFT FLAP ACTUATING ROD CUTOUT. MAINTENANCE REMOVED THE DAMAGED CHORD, FABRICATED A NEW CHORD AND REPAIR STRAP AND INSTALLED PER SRM 51-30-2 AND 51-40-4. 2L73 4F A3WE 19950428004981995042800498NM 1995 4 28 UPS203037 119950423A5754 K FLAP BOEING727 727180C 138406GNM LT LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 3 K-FLAP OUTBOARD LUG UPPER OUTBOARD BOLT HOLE. MAINTENANCE REMOVED THE OUTBOARD LUG UPPER INBOARD AND BOTH LOWER BOLT HOLES TO HAVE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED CORRODED K-FLAP AND INSTALLED WITH NEW IAW MM 27-81-01 AND SRM 51-30-2. 2L73 4F A3WE 19950428004991995042800499NM 1995 4 28 UPS203038 119950423A5315 FLOORBEAM BOEING727 727180C 138406GNM FS 880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C- CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER FLANGE OF THE FLOORBEAM AT STATION 880, RBL 45 TO 65 AND WL 200. MAINTENANCE REMOVED THE CORROSION, ALODINED, PRIMED PER UPS EO 2727-53-1578. 2L73 4F A3WE 19950428005001995042800500NM 1995 4 28 UPS203039 119950423A5320 NOSE CHORD BOEING727 727180C 138406GNM FS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER NOSE CHORD ON THE LEFT SIDE AT STATION 294.5, LBL 18 AND WL 148. MAINTENANCE REMOVED THE OLD NOSE CHORD, LEFT HAND SIDE AND INSTALLED WITH NEW LOWER NOSE CHORD PER SRM 51-10-1, 51-20-4 AND 51-30-2. 2L73 4F A3WE 19950428005011995042800501NM 1995 4 28 UPS203040 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AROUND BUSHING HOLES AT STATION 740 TO 760, BL 0 AND WL 206. MAINTENANCE REMOVED THE OLD LINK AND INSTALLED WITH NEW EXPANSION LINK AND BUSHING PER SRM 51-10-02, 51-30-5, OHM 20-50-03, 20-41-02 AND 20-50-02. 2L73 4F A3WE 19950428005021995042800502NM 1995 4 28 UPS203041 119950423A5320 FITTING BOEING727 727180C 138406GNM STA 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK FITTING AT STATION 740, LBL 25 AND WL 206. MAINTENANCE REPLACED THE EXPANSION LINK FITTING PER SRM 51-10-1, 51-30-5, OHM 20-50-03, SRM 51-10-6, 51-30-2 AND 53-10-1. 2L73 4F A3WE 19950428005031995042800503NM 1995 4 28 UPS203042 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK FITTING AT STATION 740, RBL 25 AND WL 206. MAINTENANCE REMOVED THE CORROSION AND REPLACED THE EXPANSION LINK IAW SRM 51-30-2 AND 51-10-1. 2L73 4F A3WE 19950428005041995042800504NM 1995 4 28 UPS203043 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK FITTING AT STATION 740, LBL 45 AND WL 206. MAINTENANCE REMOVED AND REPLACED THE EXPANSION LINK FITTING PER SRM 51-10-6, 51-30-2, 51-30-5, 53-10-1 AND OHM 20-50-3 AND 20-50-2. 2L73 4F A3WE 19950428005051995042800505NM 1995 4 28 UPS203044 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 848 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STATION 848 TO 870 AND LBL 62. MAINTENANCE REPLACED THE EXPANSION LINK PER SRM 51-10-1, 51-30-2 AND 51-30-5. 2L73 4F A3WE 19950428005061995042800506NM 1995 4 28 UPS203045 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AT STATION 740 TO 760, RBL 25 AND WBL 206. MAINTENANCE REMOVED AND REPLACED THE EXPANSION LINK IAW SRM 53-30-2, 51-10-1, 51-10-6 AND 51-30-5. 2L73 4F A3WE 19950428005071995042800507NM 1995 4 28 UPS203046 119950423A5754 K-FLAP BOEING727 727180C 138406GNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 6 K-FLAP ON ALL LUGS AT FASTENER HOLES. MAINTENANCE REPLACED THE K-FLAP PER MM 27-81-01 AND OHM 20-50-02. 2L73 4F A3WE 19950428005081995042800508NM 1995 4 28 UPS203047 119950423A5754 HINGE FITTING BOEING727 727180C 138406GNM NR 4 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 4 K-FLAP ON ALL LUGS. MAINTENANCE REMOVED AND REPLACED CENTER HINGE FITTING IAW SRM 51-30-2, 51-30-8, 51-10-1 AND MM 27-81-01. 2L73 4F A3WE 19950428005091995042800509NM 1995 4 28 UPS203048 119950423A5754 K-FLAP BOEING727 727180C 138406GNM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND PITTING CORROSION ON THE ATTACH POINTS OF THE NUMBER 5 K-FLAP BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE K-LFAP IAW OHM 20-50-03 AND MM 27-81-01. 2L73 4F A3WE 19950428005101995042800510NM 1995 4 28 UPS203049 119950423A5754 K-FLAP BOEING727 727180C 138406GNM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE OUTBOARD HINGE LOG OUTBOARD UPPER BOLT OF THE NUMBER 2 K-FLAP OUTBOARD BONDING JUMPER. MAINTENANCE REMOVED THE CORROSION THEN REPLACED THE K-FLAP IAW MM 27-81-01. 2L73 4F A3WE 19950428005111995042800511NM 1995 4 28 UPS203050 119950423A5320 FLOOR SUPPORT BOEING727 727180C 138406GNM FS 314 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM FLOOR SUPPORT AT STATION 314, RBL 15 TO 40 AND WL 208. MAINTENANCE REPLACED THE FLOOR SUPPORT PER SRM 53-10-1, 51-10-6, 51-30-8, 51-30-5 AND 51-10-2. 2L73 4F A3WE 19950428005121995042800512NM 1995 4 28 UPS203051 119950423A5320 HAT CHANNEL BOEING727 727180C 138406GNM FS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM HAT CHANNEL AT STATION 344, RBL 15 TO 40 AND WL 208. MAINTENANCE REPLACED THE HAT CHANNEL PER SRM 51-10-1, 51-30-2, 51-30-03 AND MM 51-20-151 AND 51-20-21. 2L73 4F A3WE 19950428005131995042800513NM 1995 4 28 UPS203052 119950423A5315 FLOOR BEAM BOEING727 727180C 138406GNM FS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE BOTTOM FLOOR BEAM AT STATION 312, LBL 3, 20, 45 AND WL 208. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR PARTS, TREATED AND INSTALLED PER SRM 51-10-6, 53-10-1 AND UPS EO 727-5310-6890A. 2L73 4F A3WE 19950428005141995042800514NM 1995 4 28 UPS203053 119950423A5320 HAT CHANNEL BOEING727 727180C 138406GNM FS 1138 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE HAT CHANNEL AT STATION 1138, RBL 25 TO 45 AND WL 208. MAINTENANCE REPLACED THE HAT CHANNEL PER SRM 51-10-1, 51-10-2, MM 51-20-151, SRM 51-30-2. 2L73 4F A3WE 19950428005151995042800515NM 1995 4 28 UPS203054 119950423A5320 FLOOR SUPPORT BOEING727 727180C 138406GNM FS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR SUPPORT AT STATION 312 - 238, LBL 35 AND WL 207. MAINTENANCE REPLACED THE FLOOR SUPPORT PER SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950428005161995042800516NM 1995 4 28 UPS203055 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 868 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER SKIN OF THE FUEL CELL AT STATION 868 - 870, LBL 67 - 65 AND WL 190. MAINTENANCE REMOVED THE CORROSION FROM THE CENTER TANK SKIN, BLENDED AREA, INSTALLED FILLER WASHERS IAW SRM 51-10-2, 51-20-151 AND UPS EO 727-57-1351. 2L73 4F A3WE 19950428005171995042800517NM 1995 4 28 UPS203056 119950423A5313 STRINGER BOEING727 727180C 138406GNM FS 757 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 17R AT STATION 757, RBL 70.5 AND WL 207. MAINTENANCE REMOVED THE CORROSION AND REPAIRED AREA PER UPS EO 727-53-1576. 2L73 4F A3WE 19950428005181995042800518NM 1995 4 28 UPS203057 119950423A5320 WEB BOEING727 727180C 138406GNM FS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL WEB OF THE NOSE LANDING GEAR DOG HOUSE AT STATION 294.5 - 330, RBL 25 AND WL 268 - 278. MAINTENANCE REMOVED THE CORROSION AND FABRICATED THE REPAIR DOUBLER PER UPS EO 727-5330-6923A. 2L73 4F A3WE 19950428005191995042800519NM 1995 4 28 UPS203058 119950423A5330 SKIN BOEING727 727180C 138406GNM FS 759 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF THE FUEL CELL AT STATION 759, RBL 65 AND WL 204. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2 AND 57-10-1. 2L73 4F A3WE 19950428005201995042800520NM 1995 4 28 UPS203059 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AT STATION 740 TO 760 AND RBL 45. MAINTENANCE REMOVED THE CORRODED EXPANSION LINK AND REPLACED IAW SRM 51-30-5, 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950428005211995042800521NM 1995 4 28 UPS203060 119950423A5347 SEAT TRACK BOEING727 727180C 138406GNM FS 780 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON OUTBOARD FLANGE OF SEAT TRACK AT STATION 780, RBL 63 AND WL 208. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 51-30-2 AND 51-10-2. 2L73 4F A3WE 19950428005221995042800522NM 1995 4 28 UPS203061 119950423A5320 FASTENER BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER ON LEFT HAND SIDE AT STATION 740, LBL 65 AND WL 207.5. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2 AND 51-40-2. 2L73 4F A3WE 19950428005231995042800523NM 1995 4 28 UPS203062 119950423A5320 PLUG CHORD BOEING727 727180C 138406GNM FS 865 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE PLUG CHORD AT STATION 865, LBL 69 AND WL 190. MAINTENANCE REMOVED CORROSION, TREATED AND INSTALLED ITEMS IAW UPS EO 727-53-1579. 2L73 4F A3WE 19950428005241995042800524NM 1995 4 28 UPS203063 119950423A5320 VERT BEAM BOEING727 727180C 138406GNM FS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL BEAM AT STATION 1183, RBL 8 AND LBL 8 AND WL 182. MAINTENANCE REPAIRED THE VERTICAL BEAMS IAW UPS EO 727-5311-0635. 2L73 4F A3WE 19950428005251995042800525NM 1995 4 28 UPS203064 119950423A5311 FRAME BOEING727 72751C 1384015NM FS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C- CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 760, LBL 60-66 AND WL 209-213. MAINTENANCE REMOVED AND REPAIRED THE AREA IAW UPS EO 727-53-1574. 2L73 4F A3WE 19950428005261995042800526NM 1995 4 28 UPS203065 119950423A5754 K FLAP BOEING727 72751C 1384015NM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 5 K-FLAP AND BULLNOSE. MAINTENANCE REMOVED AND REPLACE WITH A NEW K-FLAP AND BULLNOSE IAW OHM 20-50-01 AND MM 27-81-01. 2L73 4F A3WE 19950428005271995042800527NM 1995 4 28 UPS203066 119950423A5720 STIFFENER BOEING727 72751C 1384015NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK AND CORROSION ON THE STIFFENER ON THE WING CENTER SECTION REAR WEB AT STATION 870 AND LBL 33. MAINTENANCE REMOVED THE DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER PER SRM 51-30-2. 2L73 4F A3WE 19950428005281995042800528NM 1995 4 28 UPS203067 119950423A5320 BEAM BOEING727 72751C 1384015NM FS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE FASTENER ON THE NOSE LANDING GEAR DRAG BRACE SUPPORT BEAM AFT FLANGE AT THE RIGHT HAND OUTBOARD SIDE STATION 344 AND WL 198.5. MAINTENANCE REMOVED AND REPAIRED THE FORWARD DRAG BRACE SUPPORT BEAM IAW UPS EO 727-53-1573. 2L73 4F A3WE 19950428005291995042800529NM 1995 4 28 UPS203068 119950423A5320 STIFFENER BOEING727 72751C 1384015NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL STIFFENER AT STATION 870 AND LBL 44. MAINTENANCE REMOVED THE DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER PER SRM 51-30-2. 2L73 4F A3WE 19950428005301995042800530NM 1995 4 28 UPS203069 119950423A5320 CHORD BOEING727 72751C 1384015NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE CHORD AT STATION 740, WL 170 AND LBL 24 AND RBL 33. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-10-1, 51-10-2, 51-20-4 AND 51-30-2. 2L73 4F A3WE 19950428005311995042800531NM 1995 4 28 UPS203070 119950423A5313 STRINGER BOEING727 72751C 1384015NM FS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 18A ON THE RIGHT HAND LOWER VERTICAL FLANGE AT STATION 860 TO 865. MAINTENANCE REMOVED THE CORROSION AND REPAIRED IAW UPS EO 727-53-1575. 2L73 4F A3WE 19950428005321995042800532NM 1995 4 28 UPS203071 119950423A5320 CHORD BOEING727 72751C 1384015NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER 740 CHORD AT RBL 55, LBL 55 AND WL 165. MAINTENANCE REMOVED AND REPLACED THE LOWER CHORD IAW UPS EO 727-5710-6911A. 2L73 4F A3WE 19950428005331995042800533NM 1995 4 28 UPS203072 119950423A5730 SKIN BOEING727 72751C 1384015NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER FUEL CELL SKIN AT STATION 870 FROM LBL 65 TO RBL 65. MAINTENANCE REMOVED CORROSION, BLENDED AREAS, INSTALLED FILLER WASHERS, FLAP PEENED EFFECTED AREAS, ALODINED AND PRIMED AND RETURNED AIRCRAFT TO NORMAL PER SRM 51-10-2 AND MM 51-20-151. 2L73 4F A3WE 19950428005341995042800534NM 1995 4 28 UPS203073 119950423A5313 STRINGER BOEING727 72751C 1384015NM FS 742 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 17L AT STATION 742 AND WL 208. MAINTENANCE REMOVED THE CRACK AND REPAIRED THE STRINGER PER UPS 727-52-1580. 2L73 4F A3WE 19950428005351995042800535NM 1995 4 28 UPS203074 119950423A5320 EXPANSION LINK BOEING727 72751C 1384015NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AT STATION 740, WBL 168 AND RBL 13. MAINTENANCE REMOVED AND REPLACED THE EXPANSION LINK PER SRM 51-30-2 AND 51-10-1. 2L73 4F A3WE 19950428005361995042800536NM 1995 4 28 UPS203076 119950423A5730 SKIN BOEING727 72751C 1384015NM FS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE LOWER FUEL CELL SKIN AT STATION 740, LBL 18 TO LBL 24 AND WL 169. MAINTENANCE REPAIRED THE CRACK IAW UPS EO 727-5710-6914A. 2L73 4F A3WE 19950428005371995042800537NM 1995 4 28 UPS203077 119950423A5330 SKIN BOEING727 72751C 1384015NM FS 857 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF FUSELAGE FUEL CELL SKIN AT STATION 857 TO 870, RBL 60 TO 65 AND WL 190. MAINTENANCE BLENDED AREA PER UPS EO 727-57-1350. 2L73 4F A3WE 19950428005381995042800538NM 1995 4 28 UPS203078 119950423A5712 RIB CHORD BOEING727 72751C 1384015NM BL 70.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5. MAINTENANCE REPAIRED AND MODIFIED THE CHORD IAW UPS EO 727-5710-1271G. 2L73 4F A3WE 19950428005391995042800539NM 1995 4 28 UPS203079 119950423A5312 RIB CHORD BOEING727 72751C 1384015NM FS 759 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE RIB CHORD ON THE RIGHT HAND SIDE AT 12 AND 6 O'CLOCK POSITION AT STATION 759, BL 70.5. MAINTENANCE REPAIRED THE CRACKS IAW UPS EO 727-5710-1271G. 2L73 4F A3WE 19950428005401995042800540NM 1995 4 28 UPS203080 119950423A5711 SPAR CHORD BOEING727 72751C 1384015NM FS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE CENTER WING TANK UPPER SPAR CHORD AT STATION 870 AND LBL 37 TO 40. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-10-7, 51-30-2 AND 51-10-2. 2L73 4F A3WE 19950428005411995042800541NM 1995 4 28 UPS203081 119950423A5320 FITTING BOEING727 72751C 1384015NM FS 870 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS IN THE LEFT HAND TERMINAL FITTING AT STATION 870. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW UPS EO 727-5310-6913. 2L73 4F A3WE 19950428005421995042800542NM 1995 4 28 UPS203082 119950423A5320 CHORD BOEING727 72751C 1384015NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01904UP 18946 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE VERTICAL FLANGE OF THE LOWER CHORD AT STATION 870, WL 160, LBL 27 AND RBL 25. MAINTENANCE REMOVED THE CORRODED CHORD, FABRICATED NEW CHORD AND INSTALLED IAW UPS EO 727-5710-6912A. 2L73 4F A3WE 19950428005431995042800543NM 1995 4 28 UPS203083 119950423A5311 FRAME BOEING727 72731C 1384011NM FS 1342, LBL 20 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND FRAME CHORD AT STATION 1342 AND LBL 20. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2. 2L73 4F A3WE 19950428005441995042800544NM 1995 4 28 UPS203084 119950423A5311 FRAME BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND FRAME CHORD AT STATION 1342 AND RBL 20. MAINTENANCE REMOVED AND REPLACED THE CHORD. 2L73 4F A3WE 19950428005451995042800545NM 1995 4 28 UPS203085 119950423A5311 FRAME BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND LOWER FRAME CHORD AT STATION 1342 AND LBL 24. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-2. 2L73 4F A3WE 19950428005461995042800546NM 1995 4 28 UPS203086 119950423A5311 FRAME BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND LOWER FRAME CHORD AT STATION 1342 AND RBL 24. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950428005471995042800547NM 1995 4 28 UPS203087 119950423A5320 CHANNEL BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND CHANNEL AT STATION 1342, LBL 18 AND WL 247. MAINTENANCE REMOVED AND REPLACED THE CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950428005481995042800548NM 1995 4 28 UPS203088 119950423A5320 CHANNEL BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND CHANNEL AT STATION 1342, RBL 18 AND WL 247. MAINTENANCE REMOVED AND REPLACED THE CHANNEL PER SRM 51-30-2. 2L73 4F A3WE 19950428005491995042800549NM 1995 4 28 UPS203089 119950423A5320 CHORD BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HAND OUTBOARD CHORD AT STATION 1342, LBL 30 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-30-02. 2L73 4F A3WE 19950428005501995042800550NM 1995 4 28 UPS203090 119950423A5320 CHORD BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND OUTBOARD CHORD AT STATION 1342, RBL 30 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950428005511995042800551NM 1995 4 28 UPS203091 119950423A5320 CHORD BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CENTER CHORD AT STATION 1342 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHORD IAW SRM 51-10-1, 51-30-2 AND UPS EO 727-5530-4601B. 2L73 4F A3WE 19950428005521995042800552NM 1995 4 28 UPS203092 119950423A5320 CHANNEL BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT CENTER CHANNEL AT STATION 1342 AND WL 250. MAINTENANCE REMOVED AND REPLACED THE CHANNEL IAW SRM 51-10-1, 51-30-2 AND UPS EO 727-5530-4601B. 2L73 4F A3WE 19950428005531995042800553NM 1995 4 28 UPS203093 119950423A5320 WEB BOEING727 72731C 1384011NM FS 1223 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WEB AT THE INBOARD CHORD AT STATION 1223 AND WL 230. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-2. 2L73 4F A3WE 19950428005541995042800554NM 1995 4 28 UPS203094 119950423A5311 RIB BOEING727 72731C 1384011NM FS 1365 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND RIB FLANGE AT STATION 1365 AND WL 250. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PART PER SRM 57-40-3 AND 51-30-2. 2L73 4F A3WE 19950428005551995042800555NM 1995 4 28 UPS203095 119950423A5320 ANGLE BOEING727 72731C 1384011NM FS 1345 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND SKIN SUPPORT ANGLE AT FS 1345 AND FIN STATION 22.5. MAINTENANCE CUT OUT THE DAMAGED AREA AND INSTALLED FABRICATED SECTION AND SPLICE IAW SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19950428005561995042800556NM 1995 4 28 UPS203096 119950423A5531 SPAR BOEING727 72731C 1384011NM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER REAR SPAR LEFT HAND CHORD AT STATION 0 TO 12. MAINTENANCE STOP DRILLED AND INSTALLED THE REPAIR KIT. 2L73 4F A3WE 19950428005571995042800557NM 1995 4 28 UPS203097 119950423A5531 SPAR BOEING727 72731C 1384011NM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE VERTICAL STABILIZER RIGHT HAND REAR SPAR CHORD AT STATION 0 TO 12. MAINTENANCE REPAIRED THE ONE INCH CRACK STOP AT FASTENER HOLE. 2L73 4F A3WE 19950428005581995042800558NM 1995 4 28 UPS203098 119950423A5320 CHANNEL BOEING727 72731C 1384011NM FS 342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD SIDE AND BASE OF THE FLOOR SUPPORT IN THE LAV AREA AT STATION 342 FROM RBL 13 TO 20. MAINTENANCE FABRICATED AND REPLACED THE SUPPORT CHANNEL IAW SRM 51-30-2 AND 51-10-1. 2L73 4F A3WE 19950428005591995042800559NM 1995 4 28 UPS203099 119950423A5311 RIB BOEING727 72731C 1384011NM FS 760.95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01922UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5 AND STATION 760.95. MAINTENANCE CUT OUT DAMAGE AND REPAIRED IAW SRM 51-10-6 AND UPS EO 727-5710-1271F AND UPS EO 727-5710-6865A. 2L73 4F A3WE 19950428005601995042800560NM 1995 4 28 UPS203100 119950423A5320 CHORD BOEING727 727180C 138406GNM FS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 294.5 TO 360, RBL 25 AND WL 268. MAINTENANCE REMOVED THE CORROSION AND REPLACED WITH NEW PART IAW SRM 51-30-2. 2L73 4F A3WE 19950428005611995042800561NM 1995 4 28 UPS203101 119950423A5320 TEE CHORD BOEING727 727180C 138406GNM FS 758-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE TEE CHORD OF THE LONGITUDINAL BEAM AT STATION 758 TO 760, RBL 45 AND WL 203. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A NEW PART IAW SRM 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950428005621995042800562NM 1995 4 28 UPS203102 119950423A5320 FITTING BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK FITTING AT STATION 740, RBL 45 AND WL 206. MAINTENANCE REMOVED THE CORROSION AND REPLACED THE FITTING IAW SRM 51-30-2 AND 53-10-1. 2L73 4F A3WE 19950428005631995042800563NM 1995 4 28 UPS203103 119950423A5320 EXPANSION LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AT STATION 740 TO 760, LBL 25 AND WL 206. MAINTENANCE REPLACED THE EXPANSION LINK PER SRM 51-10-1, 51-30-2 AND 51-30-5. 2L73 4F A3WE 19950428005641995042800564NM 1995 4 28 UPS203104 119950423A5320 FORGING BOEING727 727180C 138406GNM FS 871 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION UNDER THE NUT COMMON WITH SEAT TRACK ON FORGING AT STATION 871, LBL 62 AND WL 207. MAINTENANCE REPAIRED IAW UPS EO 727-53-1585. 2L73 4F A3WE 19950428005651995042800565NM 1995 4 28 UPS203105 119950423A5320 LINK MOUNT BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK MOUNT AT STATION 740, LBL 16 AND WL 164. MAINTENANCE REMOVED AND REPLACED THE EXPANSION LINK AND LINK MOUNT IAW 727 SRM. 2L73 4F A3WE 19950428005661995042800566NM 1995 4 28 UPS203106 119950423A5315 FLOOR BEAM BOEING727 727180C 138406GNM FS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM FLOOR BEAM AT STATION 328, RBL 15 TO 50 AND WL 208. MAINTENANCE BLENDED THE CORROSION, FABRICATED NEW STRAPS FOR LOWER REPAIR, APPLIED ALODINE AND PRIMED TO FABRICATE PARTS AND INSTALLED PARTS WITH FASTENERS IAW SRM 53-10-1, 51-10-1 AND UPS EO 727-53-1584. 2L73 4F A3WE 19950428005671995042800567NM 1995 4 28 UPS203107 119950423A5320 STIFFENER BOEING727 727180C 138406GNM FS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER VERTICAL DOG HOUSE STIFFENER AT STATION 328, RBL 14 AND WL 175. MAINTENANCE REPLACED THE STIFFENER PER SRM 51-30-2, 51-10-1 AND 51-30-5. 2L73 4F A3WE 19950428005681995042800568NM 1995 4 28 UPS203108 119950423A5320 STIFFENER BOEING727 727180C 138406GNM FS 320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER VERTICAL STIFFENER AT STATION 320, RBL 14 AND WL 175. MAINTENANCE REPLACED THE STIFFENER PER SRM 51-30-2, 51-10-1 AND 51-30-5. 2L73 4F A3WE 19950428005691995042800569NM 1995 4 28 UPS203109 119950423A5315 FLOOR BEAM BOEING727 727180C 138406GNM FS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE BOTTOM FLOOR BEAM AT STATION 344, RBL 0 TO 45 AND WL 208. MAINTENANCE BLENDED OUT THE DAMAGE AND INSTALLED THE REPAIR STRAP IAW UPS EO 727-53-1588 AND SRM 53-10-1 AND 51-30-2. 2L73 4F A3WE 19950428005701995042800570NM 1995 4 28 UPS203110 119950423A5315 FLOOR BEAM BOEING727 727180C 138406GNM FS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM UPPER FLANGE AT STATION 344, RBL 13 AND WL 208. MAINTENANCE FABRICATED REPAIR PARTS FOR SPLICE AND TRIMMED NEW UPPER CHORD IAW SRM 53-10-1, 51-30-2, 51-10-6 AND UPS EO 727-5310-6889A. 2L73 4F A3WE 19950428005711995042800571NM 1995 4 28 UPS203111 119950423A5311 FRAME BOEING727 727180C 138406GNM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME FLANGE LEFT HAND SIDE WHERE THE SEAL RETAINER ATTACHES TO WL 190 AT STATION 870. MAINTENANCE REMOVED THE CORROSION IAW UPS EO 727-53-1583. 2L73 4F A3WE 19950428005721995042800572NM 1995 4 28 UPS203112 119950423A5320 STIFFENER BOEING727 727180C 138406GNM FS 335 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE OUTBOARD FLANGE OF THE UPPER VERTICAL STIFFENER AT STATION 335, RBL 15 AND WL 178. MAINTENANCE REPLACED THE STIFFENER PER SRM 51-30-2, 51-10-1 AND 51-30-5. 2L73 4F A3WE 19950428005731995042800573NM 1995 4 28 UPS203113 119950423A5320 HAT CHANNEL BOEING727 727180C 138406GNM FS 1138-1150 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL AT STA 1138-1150, LBL 25, WL208. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1, 51-30-8, 51-10-2, 51-30-2. 2L73 4F A3WE 19950428005741995042800574NM 1995 4 28 UPS203114 119950425A3350 EEL BATTERY PACK BOEING727 72727C 138400JNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01907UP 19118 MAINTENANCE REPORTED EMER EXIT LIGHT WOULD NOT ILLUMINATE AT CREW ENTRY DOOR WHEN TESTED DURING PREDEPARTURE CHECK. REPLACED BATTERY PACK. OPS CHECK GOOD. 2L73 4F A3WE 19950428005751995042800575NM 1995 4 28 UPS203115 119950423A5311 FRAME FORGING BOEING727 727180C 138406GNM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STA 870 FRAME FORGING AT RBL 70, WL 191. FABRICATED AND INSTALLED REPAIR PER UPS EO B727-5310-6930A. 2L73 4F A3WE 19950428005761995042800576NM 1995 4 28 UPS203116 119950423A5711 SPAR BOEING727 727180C 138406GNM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WING CENTER SECTION, UPPER SPAR CHORD, BS 870, BETWEEN LBL 40 AND RBL 25, WL 190. REPLACED PER UPS EO B727-5710-6939. 2L73 4F A3WE 19950428005771995042800577NM 1995 4 28 UPS203117 119950423A5320 MOUNT LINK BOEING727 727180C 138406GNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK MOUNT AT BS 740, RBL 16, WL164. REPLACED PER SRM 51-10-1. 2L73 4F A3WE 19950428005781995042800578NM 1995 4 28 UPS402999 119950423A5315 FLOORBEAM BOEING747 747123F NM FS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER CHORD OF THE FLOORBEAM AT STATION 860 AND LBL 75. MAINTENANCE REWORKED AND TREATED THE AREA ACCORDING TO SRM 51-10-01. 2L74 4F A20WE 19950428005791995042800579NM 1995 4 28 UPS403000 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND A CORROSION CRACK AT THE SEAT TRACK AT STATION 870 AND LBL 98. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005801995042800580NM 1995 4 28 UPS403001 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 860 AND RBL 98. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005811995042800581NM 1995 4 28 UPS403002 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 1300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK BETWEEN STATION 1300 AND 1420, RBL 11.33. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 51-30-02. 2L74 4F A20WE 19950428005821995042800582NM 1995 4 28 UPS403003 119950423A5320 INTERCOSTAL BOEING747 747123F NM FS 1327 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE INTERCOSTAL AT STATION 1327 BETWEEN LBL 11.33 AND RBL 11.33. MAINTENANCE REPLACED THE INTERCOSTAL IAW SRM 51-30-02. 2L74 4F A20WE 19950428005831995042800583NM 1995 4 28 UPS403004 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 800 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK AT STATION 800 TO 840 AND WBL 98.58. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005841995042800584NM 1995 4 28 UPS403005 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 780 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT THE LOWER SIDE OF STATION 780 TO 800 AND RBL 98. MAINTENANCE REPLACED THE SEAT TRACK AND INSTALLED NEW SPLICES IAW SRM 53-10-05. 2L74 4F A20WE 19950428005851995042800585NM 1995 4 28 UPS403006 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 520 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 520 AND LBL 75. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005861995042800586NM 1995 4 28 UPS403007 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR 'C' CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK AT STATION 860 AND RBL 33.99. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005871995042800587NM 1995 4 28 UPS403008 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 1300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON THE SEAT TRACK BETWEEN STATION 1300 AND 1420 AND LBL 11.33. MAINTENANCE REMOVED AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-30-02. 2L74 4F A20WE 19950428005881995042800588NM 1995 4 28 UPS403009 119950423A5320 WEB BOEING747 747123F NM FS 1245 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CENTERLINE WEB IN THE RIGHT HAND WLG WHEEL WELL AT STATION 1245. MAINTENANCE REMOVED CORROSION AND INSTALLED DOUBLER IAW EO 747-53-0711. 2L74 4F A20WE 19950428005891995042800589NM 1995 4 28 UPS403010 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 520 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 520 AND LBL 33.99. MAINTENANCE REPLACED THE SEAT TRACK IAW SRM 53-10-05. 2L74 4F A20WE 19950428005901995042800590NM 1995 4 28 UPS403011 119950423A5347 SEAT TRACK BOEING747 747123F NM FS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK AT STATION 680. MAINTENANCE REPLACED THE TRACK PER SRM 53-10-05. 2L74 4F A20WE 19950428005911995042800591NE 1995 4 28 95ZZZX2027 219950405A7261710170 RELIEF VALVE BOEING737 7372P6 NM PWA JT8 JT8D15 52051NE NR 1 ENGINE MISSING A AZZDAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO172FOR 21355 688646 DURING ROUTINE A-3 CHECK, NR 1 ENGINE MAIN OIL FILTER CHANGE, DISCOVERED OIL PRESSURE RELIEF VALVE ASSEMBLY WAS NOT INSTALLED. REPLACED PRESSURE RELIEF VALVE, PN 710170, RETAINING RING, PN 728373, KEY WASHER, PN 695395, AND GASKET, PN 6-961. 2L72 4F4 FRTA16WE E2EA 19950428005921995042800592CE 1995 4 28 95ZZZX2028 119950412A32139981002827 BRACE 101810000605BEECH 200 200BEECH 1152920CE LT MLG CRACKED ASAGONAK NONE O OTHER ININSP/MAINT 1 SW01130PA9109 1611 BB330 DURING 5-YEAR LANDING GEAR INSPECTION, CRACKS FOUND ON BOTH LEFT AND RIGHT MAIN BRACES USING FLUORESCENT PENETRANT INSPECTION. TWO CRACKS FOUND ON EACH BRACE. ONE CRACK ABOVE EACH TORQUE KNEE BOSS, ONE CRACK VISIBLE WITH NAKED EYE, THE OTHER 3 WERE ONLY VISIBLE WITH FLUORESCENT PENETRANT UNDER THE BLACK LIGHT. BOTH BRACES WERE REPLACED. CONTRIBUTING FACTORS TO THIS FAILURE COULD BE: 1. HIGH NUMBER OF LANDING CYCLES. 2. ROUGH FIELD USE. 3. INCIDENT WHERE AIRCRAFT WAS STUCK IN MUD. THE LARGEST CRACK WAS .25 INCH LONG; NO CRACK POSED DANGER OF IMMEDIATE FAILURE. TOTAL LANDING CYCLES: 10,918. CSO, 1,871. 1L72 4T A24CE 19950428005931995042800593CE 1995 4 28 95ZZZX2029 119950412A32139981002827 BRACE 101810000606BEECH 200 200BEECH 1152920CE RT MLG CRACKED A AGONAK NONE O OTHER ININSP/MAINT 1 SW01130PA9109 1611 BB330 DURING 5-YEAR LANDING GEAR INSPECTION, CRACKS FOUND ON BOTH LEFT AND RIGHT MAIN BRACES USING FLUORESCENT PENETRANT INSPECTION. TWO CRACKS FOUND ON EACH BRACE. ONE CRACK ABOVE EACH TORQUE KNEE BOSS, ONE CRACK VISIBLE WITH NAKED EYE, THE OTHER 3 WERE ONLY VISIBLE WITH FLUORESCENT PENETRANT UNDER THE BLACK LIGHT. BOTH BRACES WERE REPLACED. CONTRIBUTING FACTORS TO THIS FAILURE COULD BE: 1. HIGH NUMBER OF LANDING CYCLES. 2. ROUGH FIELD USE. 3. INCIDENT WHERE AIRCRAFT WAS STUCK IN MUD. THE LARGEST CRACK WAS .25 INCH LONG; NO CRACK POSED DANGER OF IMMEDIATE FAILURE. TOTAL LANDING CYCLES: 10,918. CSO, 1,871. 1L72 4T A24CE 19950428006711995042800671NM 1995 4 28 9506642276 119950419A5313 LONGERON BOEING727 727251 138408HNM FS 950-990 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01276US 21155 DURING PERIODIC CHECK, MAINTENANCE FOUND STR 29L, FS 950E TO 990 CORRODED. REPAIRED PER NWA EA 22-096715, MFG PART NUMBER 65-56441-3. 2L73 4F A3WE 19950428006721995042800672NM 1995 4 28 9506652703 119950419A5313 LONGERON BOEING727 727225 1384077NM FS 930 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018878Z 21451 DURING PERIODIC CHECK, MAINTENANCE FOUND FS 930 FRAME, STR 14R DAMAGED. REPAIRED PER NWA EA 27-096521, MFG PART NUMBER 65-16336-5. 2L73 4F A3WE 19950428006731995042800673NM 1995 4 28 9506662703 119950421A5330 SKIN BOEING727 727225 1384077NM FS 720 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018878Z 21451 DURING PERIODIC CHECK, MAINTENANCE FOUND FUSELAGE SKIN RAM AIR INLET LIP CORRODED AT FS 720B TO 720C, STR 28L TO 28R. REPAIRED PER NWA EA 27-096531, MFG PART NUMBER 65-54590-5. 2L73 4F A3WE 19950428006741995042800674NM 1995 4 28 95UAL767013 119950327A2420 IDG BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE RIGHT FAILED A UALAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 WP29611UA 21872 IN CRUISE, RIGHT GENERATOR DRIVE LIGHT FLASHING. GENERATOR DRIVE WOULD NOT DISCONNECT. RIGHT GENERATOR CONTROL SWITCH TURNED OFF, APU STARTED. REPLACED IDG, AND GCU. SYSTEM OP CHECKED OK. TESTED UNITS IN SHOP, COULD NOT FIND FAULT. OVERHAULED AS A PRECAUTION AND RETURNED TO STOCK. 2L72 4F4 FRTA1NM E3NE 19950428006751995042800675NE 1995 4 28 95UAL767016 219950426A7260506010 BEARING PWA BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 GEAR BOX FAILED A UALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP29652UA 24347 25390 724347 OIL FILTER BY-PASS LIGHT FOR THE NUMBER TWO ENGINE CAME ON, CREW BROUGHT BACK THROTTLE TO IDLE. SHORTLY, THEREAFTER THE NUMBER TWO ENGINE FLAMED-OUT. ANGLE GEARBOX BEARING FAILED. 2L72 4F4 FRTA1NM E24NE 19950428006761995042800676WP 1995 4 28 ABXA9500354 119950425A323129567311 ROD DOUG DC9 DC931 3022065WP RT MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION LDLANDING 1 GL23929AX 45874 DURING GEAR EXTENTION, GEAR DOOR OPEN LIGHT DID NOT EXTINGUISH. RECYCLED GEAR, GEAR DOOR OPEN LIGHT WENT OUT AFTER THIRTY SECONDS. ADJUSTED RIGHT MAIN LANDING GEAR DOOR PUSHROD IAW DC-9 MM 32-31-0. PERFORMED GEAR SWING CYCLE, OPS CHECKED GOOD. 2L72 4F A6WE 19950428006771995042800677WP 1995 4 28 ABXA9500370 119950425A2140 HEAT SYST DOUG DC8 DC863 302198AWP COCKPIT ODOR A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23823AX 46122 EN ROUTE TO EWR, WITH SUPPLEMENTAL HEAT ON, A BURNING ODOR WAS REPORTED IN THE COCKPIT. THE ODOR DISSIPATED WHEN THE HEAT WAS TURNED OFF. COULD NOT DUPLICATE. THE SUPPLEMENTAL HEAT WAS OPERATED FOR SEVERAL MINUTES ON THE GROUND AND NO ODOR WAS NOTED. HEATER OPS CHECKED GOOD. 2L74 4F 4A25 19950428006781995042800678WP 1995 4 28 ABXA9500371 119950426A2422F4510T INVERTER NIHON YS11 YS11A500 6310416WP NR 1 DEFECTIVE A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL23911AX5521 302 2051 SMOKE IN COCKPIT, EITHER NR 1 INVERTER OR AIR CONDITIONER. REPLACED NR 1 INVERTER IAW YS-11 MM CHAPTER 24. OPS CHECKED GOOD, NO SMOKE NOTED. 2L72 4T A1PC 19950428006791995042800679SO 1995 4 28 COM11869 119950424A27523082001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01156CA1223656 120156 FLAP CONTROL FAULT WARNING ACTIVATED. REPLACED LT NACELLE FLAP ACTUATOR. 2L72 4T RTA31SO 19950428006801995042800680SO 1995 4 28 COM11870 119950425A3150 TRIM WARNING EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01267CA 120259 AURAL TRIM WARNING DURING TAKEOFF. RESET CIRCUIT BREAKER, SYSTEM TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950428006811995042800681SO 1995 4 28 COM11871 119950424A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01156CA14147 120156 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED, DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT NR 1327-2. P/N 120-17056-007, 8 EA; 120-17056-009, 1 EA; 120-17056-019, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 3 EA; 120-17056-013, 2 EA; 120-17057-006, 1 EA; 120-17057-007, 1 EA; 120-17059-017, 1 EA; 120-17059-015, 1 EA. 2L72 4T RTA31SO 19950428006821995042800682EA 1995 4 28 COM60459 119950424A276054C54677E01 MANIFOLD CNDAIRCL600 CL6002B19 EA SPOILER FAILED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01938CA1498 7046 OUTBD GROUND SPOILER CAUTION MESSAGE ON EICAS. REPLACED THE SPOILER MANIFOLD ASSY. 2L72 4F RTA21EA 19950428006831995042800683EA 1995 4 28 COM60460 119950425A291673011 RESERVOIR CNDAIRCL600 CL6002B19 EA NR 1 HYD SYST FAILED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01912CA4940 7011 THE NR 1 HYDRAULIC SYSTEM FAILED. REPLACED THE NR 1 RESERVOIR ASSY. 2L72 4F RTA21EA 19950428006841995042800684EA 1995 4 28 COM60461 119950425A3231600861011001 RETRACT MECH CNDAIRCL600 CL6002B19 EA NLG DOOR DEFECTIVE A COMAO OTHER O OTHER UKUNKNOWN 1 SO01932CA2570 7038 CLICKING NOISE FROM NLG AREA AFTER GEAR RETRACTED. REPLACED THE NLG DOORS MECHANISM. 2L72 4F RTA21EA 19950428006851995042800685WP 1995 4 28 SCNA95063 119950424A29136506606 HYD PUMP DOUG DC10 DC1010 3022110WP NR 2 ENGINE LEAKING A SCNAK NONE KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 GL15572SC 46977 LOST ALL HYDRAULIC FLUID ON THE NUMBER TWO SYSTEM. FOUND RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP CASE LEAKING. REMOVED AND REPLACED PUMP IAW MM 29-11-01 SERVICED SYSTEM, OPS AND LEAK CHECKED GOOD. 2L73 4F A22WE 19950428006861995042800686NM 1995 4 28 UPS203119 119950425A5311 FRAME BOEING727 727180C 138406GNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01920UP 19873 WHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT BS 760, STR 17R RBL 70.5. INSTALLED REPAIR PER UPS EO FILE NR 727-53-1586. 2L73 4F A3WE 19950428006871995042800687NM 1995 4 28 UPS803120 119950425A2910 HYD LINE BOEING757 75724APF 1384969NM LT MLG RUPTURED A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01405UP 23727 PILOT REPORTED, DURING CLIMBOUT FROM SYR LEFT HYD SYSTEM QTY DECREASED TO NEAR ZERO AFTER GEAR AND FLAP RETRACTION. CONTINUED FLIGHT TO SDF. SDF RESCUE VEHICLES RESPONDED DUE TO THE DECLARED EMERGENCY. FLIGHT WAS UNEVENTFUL EXCEPT FOR LT HYD FAILURE. FOUND LT MLG DOWNLOCK ACTUATOR UP LINE RUPTURED. REPLACED HYD LINE ASSY, INSPECTED AND REPLACED CASE DRAIN FILTERS AND SERVICED LEFT HYD SYS. 2L72 4F RTA2NM 19950428006881995042800688WP 1995 4 28 UPS803121 119950427A3260 UPLATCH MECH DOUG DC8 DC871F 302199DWP MLG DOOR LACK OF LUBE A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01703UP 45939 PILOT REPORTED, AT 250 KNOTS ON CLIMBOUT, DOORS NOT LATCHED LIGHT ILLUMINATED. COMPLIED WITH AOM CHECKLIST. NO ALTERNATE DOOR WARNING ISOLATE LIGHTS WERE ILLUMINATED. AFTER RECYCLING GEAR, DOOR NOT LATCHED LIGHTS REMAINED ON. HOWEVER LIGHT EXTINGUISHED WHEN ANOTHER UPLATCH CHECK WAS PERFORMED. LIGHT REMAINED OUT UP TO EN ROUTE SPEEDS. CLEANED AND LUBRICATED MAIN GEAR UPLATCH MECHANISMS. OPS CK, SYSTEM PER 32-31-04. NO DEFECTS NOTED AT THIS TIME, OK FOR SERVICE. 2L74 4F RT4A25 19950428007091995042800709EU 1995 4 28 95ZZZX2077 119950217A6210365A11005008 BLADE AEROSPSA365 AS365N2 8680815EU M/R SEPARATION A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM19803 8036 6429 SEPARATION AT ROOT END OF BLADE. REMOVED AND REPLACED BLADE. 1G72 3U RTH10EU 19950428007101995042800710EU 1995 4 28 95ZZZX2078 119950109A7334642100021 TRANSMITTER AEROSPSA365 SA365N 8680669EU FUEL PRESS DEFECTIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365SJ 6018 NR 2 FUEL PRESS FLUCTUATES. REMOVED AND REPLACED TRANSMITTER. 1G72 3U H10EU 19950428007151995042800715NE 1995 4 28 95ZZZX2083 119950327A6320S1620641283 GEARBOX MOUNT SKRSKYS58T S58ET 8141803NE AIRFRAME MOUNT LUG MISSING A NYBAK NONE O OTHER ININSP/MAINT 1 EA1126567 581514 WHILE REPLACING THE INTERMEDIATE GEARBOX FOR A SCHEDULED OVERHAUL, NOTED GEARBOX AIRFRAME MOUNT MISSING A BOLT LUG EAR. NO APPARENT CAUSE CAN BE ATTRIBUTED TO THIS FAILURE. REPLACED GEARBOX AIRFRAME MOUNT PN S1620-64128-3 IAW S-58T MM. 2G72 4U 1H11 19950428007161995042800716SW 1995 4 28 95ZZZX2084 119950410A6410206010765001 BEARING 206016201127BELL 206 206B 1181511SW T/R BLADE CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11125NH CS6648 52099 MECHANIC NOTED A CRACKED FEATHERING BEARING ON TAIL ROTOR BLADE DURING POST-FLIGHT INSPECTION. REPLACED BEARING AND SLEEVE PN 206-010-765-001 AND PN 206-010-733-003 IAW BELL HELICOPTER TEXTRON 206L-4 CR & O MM ON T/R BLADE, SN CS-6648 INBOARD POSITION. 1G71 3U H2SW 19950428007171995042800717SW 1995 4 28 95ZZZX2085 119950403A6710206001053005 BEARING 206001552001BELL 206 206L4 1182110SW M/R BELLCRANK WORN A ANYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH PE119 52076 WHILE ACCOMPLISHING A 100-HOUR AIRFRAME INSPECTION, THE MECHANIC NOTED THE BEARINGS (PN 206-001-053-005) WERE FOUND OUT OF LIMITS IAW BELL 26L-4 MM. REPLACED BELLCRANK ASSY PN 206-001-552-001. 1G71 3U NCH2SW 19950428007181995042800718SW 1995 4 28 95ZZZX2086 119950409A6410206010765001 BEARING 206016201127BELL 206 206L4 1182110SW T/R BLADE CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH 52076 MECHANIC NOTED A CRACKED FEATHERING BEARING ON TAIL ROTOR BLADE DURING POST-FLIGHT INSPECTION. REPLACED BEARING AND SLEEVE PN 206-010-765-001 AND PN 206-010-733-003 IAW BELL HELICOPTER TEXTRON 206L-4 C R & O MM. 1G71 3U NCH2SW 19950428007191995042800719SW 1995 4 28 95ZZZX2087 119950408A3212206304001 FLOAT GUARD 206303300 BELL 206 206L4 1182110SW FLOATSTEP CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH 52076 DURING A DAILY INSPECTION, THE MECHANIC NOTED THAT BOTH FORWARD FLOAT GUARDS WERE FOUND CRACKED. THE CRACKS HAVE BEEN NOTED ONLY ON THE UPPER END OF THE GUARD WHERE THE GUARD ATTACHES TO THE FLIGHT STEP. NEW YORK HELICOPTER BELIEVES THE CRACKS NOTED IN THE FORWARD FLOAT GUARDS ARE ATTRIBUTED TO THE FLEXING OF THE FLIGHT STEP WHEN THE PILOT AND COPILOTS ENTER THE AIRCRAFT. REPLACED BOTH LT AND RT FLOAT GUARDS IAW AERONAUTICAL ACCESSORIES, INC., STC SH 132250. 1G71 3U NCH2SW 19950428007331995042800733NE 1995 4 28 MZZA95025 219950417A7261 OIL CAP BOEING727 727232 1384082NM PWA JT8 JT8D17 52049NE NR 2 ENGINE LOOSE A AMZZACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 WP1315781 20636 TNN - FLT 858 - DURING POST-MAINTENANCE CHECK FLIGHT ON AIRCRAFT AT AIR ASIA, OIL LOSS FOUND ON NR 2 ENGINE DUE TO OIL TANK FILLER CAP NOT PROPERLY SECURED. THE OIL WAS REFILLED AND OIL TANK FILLER CAP WAS PROPERLY SECURED PER B727 MM 70-11-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF: LINE NON-ROUTINE REPAIR ITEM CARD NR 7917132. (X) 2L73 4F4 F A3WE E2EA 19950428007341995042800734NM 1995 4 28 95ZZZW578 119950403A3350900835A EEL CHARGER BOEING727 727294 1384088NM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS T5582 22043 EMERGENCY EXIT SIGN AT ROW 3 INOPERABLE. REPLACED BATTERY PACK AND CHARGER. OPERATIONAL CHECK OK. REF TAOA049502. 0 4 A3WE 19950428007351995042800735NM 1995 4 28 95ZZZW579 119950406A71208DK1763001 ENGINE MOUNT DHAV DHC8 DHC8102 2809003NM NR 1 ENG CRACKED A AHNAAK NONE O OTHER ININSP/MAINT 1 EA07916HA5769 38814A 072 DURING 'A' CHECK, A CRACK WAS FOUND IN THE NR 1 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT. REMOVED AND REPLACED NR 1 ENGINE AFT OUTBOARD ENGINE MOUNT VERTICAL STRUT. 2H72 4T RTA13NM 19950428007361995042800736NM 1995 4 28 95ZZZW580 119950403A3244 TIRES BOEING747 747124 1384874NM NR 11/12 MLG DISINTEGRATED A P5CAO OTHER D INFLIGHT SEPARATION LDLANDING 1 WP23855FT 19733 ON LANDING AT ANC, NR 11 AND 12 MLG TIRES BLEW. KHV TOWER REPORTED THAT AIRCRAFT LEFT RUBBER ON RUNWAY ON TAKEOFF. POST FLIGHT INSPECTION REVEALED DAMAGE TO RT ADF PANEL AND RT. BODY LANDING GEAR STRUT DOOR ROD. MAINTENANCE REPLACED NR 11 AND 12 WHEEL ASSEMBLIES, REPLACED STRUT DOOR ROD AND PERFORMED SPECIAL INSPECTION PER MM 5-51-34. FUSELAGE FAIRING PANELS WERE REPAIRED PER SRM 51-40-03. ADF PANEL HAD INTERIM REPAIR PER SRM UNTIL REPLACEMENT OF RT ADF PANEL HAD INTERIM REPAIR PER SRM UNTIL REPLACEMENT OF RT ADF PANEL ON 4-11-95. AIRCRAFT RELEASED FOR SERVICE. 2L74 4F A20WE 19950428007371995042800737WP 1995 4 28 95ZZZW581 119950321A323149169131 TORQUE TUBE DOUG DC9 DC931 3022065WP RT MLG DOOR SHEARED RIVET A A4JAO OTHER J WARNING INDICATION LDLANDING 1 SO158931E 47140 FLT 9831 - ON APPROACH TO PIE, RIGHT MAIN GEAR DOOR WOULD NOT CLOSE ON GEAR EXTENSION. LANDED WITH GEAR DOOR OPEN. INSPECTION OF AREA NOTED DAMAGE TO RIGHT MLG DOOR. DAMAGE DID NOT PREVENT GEAR DOOR FROM LOCKING IN CLOSED POSITION. AIRCRAFT MADE GEAR DOWN MAINTENANCE FERRY FLIGHT TO MIA. FOUND SHEARED RIVET IN L/G SEQUENCE VALVE TORQUE TUBE. REPLACED RIVET, RT MLG DOOR AND HINGE ASSY. RETRACTION TEST NORMAL. 2L72 4F A6WE 19950428007381995042800738WP 1995 4 28 95ZZZW582 119950412A3244 TIRES DOUG DC8 DC873F 302199FWP MLG WORN A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH 46125 ON LANDING, TIRES NR 1 AND NR 2 BLEW-OUT DURING ROLLOUT. TIRES NR 5 AND NR 6 BADLY WORN. TIRES NR 1, NR 2, NR 5 AND NR 6 CHANGED PER DC-8 MM 32-40-1. REPLACED NR 1 AND NR 2 BRAKE PER 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO DEFECTS NOTED. REF 95ZZZW583. 2L74 4F RT4A25 19950428007391995042800739WP 1995 4 28 95ZZZW583 119950412A324226014111 BRAKES DOUG DC8 DC873F 302199FWP MLG WORN A DHLAO OTHER O OTHER LDLANDING 1 SO01805DH 46125 ON LANDING, TIRES NR 1 AND NR 2 BLEW-OUT DURING ROLLOUT. TIRES NR 5 AND NR 6 BADLY WORN. TIRES NR 1, NR 2, NR 5 AND NR 6 CHANGED PER DC-8 MM 32-40-1. REPLACED NR 1 AND NR 2 BRAKE PER 32-42-1. FUNCTIONAL CHECK COMPLIED WITH PER MM. NO DEFECTS NOTED. REF 95ZZZW582. 2L74 4F RT4A25 19950428007401995042800740NM 1995 4 28 95ZZZW584 119950414A278010617921 CONNECTOR BOEING727 7272Q9 138448MNM LE FLAPS DIRTY A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01741DH 21931 DURING CLIMB, LEADING EDGE DEVICES FAILED TO RETRACT ON SCHEDULE. PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. CLEANED CONNECTORS ON SLAT ACTUATORS AND LUBED SLAT TRACKS. GROUND CHECKS OK. 2L73 4F RTA3WE 19950428007411995042800741NM 1995 4 28 95ZZZW585 119950404A3230106122615 PROX SWITCH BOEING727 727228 NM LT MLG DIRTY A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01724DH 19862 ON CLIMBOUT, LANDING GEAR LEVER WOULD NOT GO PAST OFF MOVED LEVER TO UP USING OVER- RIDE SWITCH. LEVER LATCH AND LIGHTS CIRCUIT BREAKER POPPED P6-3. RESTORED ACFT TO FLIGHT MODE AS PER ALTERNATE PROCEDURE. CLEANED LT MAIN GEAR AIR/GROUND PROXIMITY SWITCHES. COULD NOT DUPLICATE ON GROUND. MM 32-30. 2L73 4F A3WE 19950428007421995042800742WP 1995 4 28 CAL950267 119950410A3350 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916883 48073 BOS - FLT 345 - INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS CABIN INOPERATIVE. THE OVERHEAD EMERGENCY LIGHT BATTERIES WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950428007431995042800743WP 1995 4 28 CAL950268 119950412A3350RPS1B EEL BATT CHARGER DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW09938MC 49525 IAH - INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING IN AFT SECTION OF CABIN INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. (W) 2L72 4F RTA6WE 19950428007441995042800744NM 1995 4 28 CAL950269 119950328A335020121 EEL BATT CHARGER BOEING737 7373T0 1384582NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0977303 23354 HOU - THE FWD ENTRY DOOR EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING A SCHEDULED MAINTENANCE TEST. THE BATTERY CHARGER AND BATTERY PACK WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (W) 2L72 4F RTA16WE 19950428007451995042800745NM 1995 4 28 CAL950270 119950413A3350 EEL WIRING BOEING737 7373T0 1384582NM CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917321 23372 EWR - FLT 135 - THE MID CABIN EMERGENCY AISLE LIGHTING WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND BROKEN WIRING, AND A BLOWN FUSE ON BATTERY CHARGER. THE BROKEN WIRES WERE SPLICED AND THE BATTERY CHARGER FUSE WAS REPLACED. OPERATION OF THE EMERGENCY AISLE LIGHTING WAS RESTORED. (W) 2L72 4F RTA16WE 19950428007461995042800746WP 1995 4 28 CAL950274 119950416A3350 EEL BATTERIES DOUG DC9 DC932 3022066WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0933506 47765 IAH - FLT 1853 - BOTH COCKPIT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950428007471995042800747WP 1995 4 28 CAL950287 119950417A3350 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916884 48074 EWR - FLT 301 - THE OVERHEAD EMERGENCY LIGHTS AT ROW 9 TO 14 WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERIES AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950428007481995042800748WP 1995 4 28 CAL950288 119950331A5311 FRAME DOUG DC10 DC1010 3022110WP BS 939/959 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096804474945 46903 KUL - THE FUSELAGE FRAME CAP AT STA 939 AND 959 IN THE FWD CARGO COMPARTMENT WERE FOUND CORRODED. REPAIRS WERE PERFORMED IAW ECRA 5310-03073. (W) 2L73 4F A22WE 19950428007491995042800749WP 1995 4 28 CAL950289 119950329A5320 DOUBLER DOUG DC10 DC1010 3022110WP BS 939-953 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096804474945 46903 KUL - INSPECTION FOUND CORROSION ON THE INNER DOUBLER OF THE FWD CARGO DOOR JAMB BETWEEN STA 939 TO 953 AT LONGERON 43R. REPAIR WAS PERFORMED IAW ECRA 5330-02255. (W) 2L73 4F A22WE 19950428007501995042800750WP 1995 4 28 CAL950290 119950402A5311 FRAME DOUG DC10 DC1010 3022110WP BS 1781 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096804474945 46903 KUL - THE FRAME CAP AT STA 1781 BETWEEN LONGERON 49R AND 49L WAS FOUND CORRODED. REPAIR WAS PERFORMED IAW ECRA 5310-03076. (W) 2L73 4F A22WE 19950428007511995042800751NM 1995 4 28 CAL950291 119950416A5330 SKIN BOEING737 737222 1384473NM BS 188-251 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223547721 19758 GSO - INSPECTION FOUND SEVERAL FASTENER HOLES CRACKED IN RT FUSELAGE SKIN AT BS 188 TO 251 BETWEEN WL 207 AND WL 234. THE CRACKS WERE ALL APPROXIMATELY .1 INCH LONG. THE CRACKED SKIN SECTIONS WERE CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW ECRA 5310-01188. (W) 2L72 4F A16WE 19950428007521995042800752NM 1995 4 28 CAL950292 119950418A5730 SKIN BOEING737 737222 1384473NM RT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09122354772147721 19758 GSO - INSPECTION FOUND A 1 INCH CRACK EXTENDING BEYOND STOP HOLE IN RT WING UPPER SURFACE FIXED LEADING EDGE. THE ADJACENT SKIN AT O/B TRACK FOR NR 5 SLAT WAS WARPED. THE DAMAGED AREA WAS ROUTED OUT IAW SRM 57-30-4. REPAIR DOUBLER AND FILTER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. (W) 2L72 4F A16WE 19950428007531995042800753NM 1995 4 28 CAL950296 119950322A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOORBEAM TOP CAP AT STA 328, LBL 20 TO RBL 40. THE FLOORBEAM CAP WAS REPLACED FROM LBL 65 TO RBL 65 IAW SRM 51-40-4. (W) 2L72 4F RTA16WE 19950428007541995042800754NM 1995 4 28 CAL950297 119950322A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOORBEAM TOP CAP AT FS 312, LBL 20 TO RBL 30. THE TOP CAP WAS REMOVED AND REPAIR ANGLES AND TOP CAP WERE INSTALLED IAW ECRA 5310-01102 AND SRM 51-40-4. (W) 2L72 4F RTA16WE 19950428007551995042800755NM 1995 4 28 CAL950298 119950322A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 294.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION AT CLIP NUTS FOR FLOORBEAM TOP CAP AT STA 294.5, LBL 40 TO RBL 40. REPAIR WAS PERFORMED IAW ECRA 5310-01102. (W) 2L72 4F RTA16WE 19950428007561995042800756NM 1995 4 28 CAL950299 119950322A5320 SUPPORT BOEING737 7373T0 1384582NM FS 294.5-312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN FS 294.5 AND FS 312, LBL 18. REPAIR WAS PERFORMED IAW ECRA 5320-01270. (W) 2L72 4F RTA16WE 19950428007571995042800757NM 1995 4 28 CAL950300 119950322A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON TOP CAP OF FLOORBEAM AT FS 1006, BL 0. THE CORRODED AREA WAS CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-01102. (W) 2L72 4F RTA16WE 19950428007581995042800758NM 1995 4 28 CAL950301 119950323A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM FS 986-1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON RT AFT LAV ANGLE FLOOR SUPPORT AT STA 986 TO 1016. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02 AND ECRA 5310-01102. (W) 2L72 4F RTA16WE 19950428007591995042800759NM 1995 4 28 CAL950302 119950322A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON AFT FLOORBEAM AT FS 986 RBL 15. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-01102. (W) 2L72 4F RTA16WE 19950428007601995042800760NM 1995 4 28 CAL950303 119950323A5315 FLOORBEAM BOEING737 7373T0 1384582NM FS 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091630131587 23352 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON RT AFT FLOORBEAM AT FS 967, RBL 41. THE CORRODED AREA WAS REMOVED AND REPAIRED IAW ECRA 5310-01102. (W) 2L72 4F RTA16WE 19950428007611995042800761WP 1995 4 28 HAL95035 119950413A33506011777 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13699HA 47763 HNL - THE LT OVERWING EXIT EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY BATTERY POWER PACK. THE OPERATIONAL CHECK WAS GOOD. (W) 2L72 4F A6WE 19950428007621995042800762WP 1995 4 28 HAL95036 119950416A33506011777 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13674MC 47735 AFT EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED BATTERY PACK. OPERATIONS CHECK OK. (W) 2L72 4F A6WE 19950428007631995042800763NM 1995 4 28 TAOA049502 119950403A3350900842 EEL BATT PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 9468 22043 EMERGENCY EXIT SIGN AT ROW 3 INOPERABLE. REPLACED BATTERY PACK AND CHARGER. OPERATIONAL CHECK OK. REF 95ZZZW578. 0 4 A3WE 19950428007641995042800764NM 1995 4 28 TAOA049503 119950408A335007912 EEL MODULE BRUCE BOEING727 727254 138408LNM CABIN MISSING A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15913TS 20250 'E' PATH LIGHTING CAPSULE AT ROW (6) MISSING. REPLACED CAPSULE AND LAMP. OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950428007651995042800765 1995 4 28 TWRA9525 419950401A2565D30440103 SLIDE BOEING747 747131 1384881NM 4R MED BROKEN A TWRAK NONE O OTHER ININSP/MAINT 1 EA15608FF 19672 DURING 'A-2' SERVICE, FOUND 4R MED SLIDE SPRING LATCH, LOCATED ADJACENT TO THE ARMING PULLEY, BROKEN. REMOVED AND REPLACED 4R MED SLIDE. OPS CHECK OK. (W) 2L74 4F A20WE 19950428007661995042800766NM 1995 4 28 TWRA9526 119950401A3350 EEL LAMP BOEING747 747131 1384881NM CABIN INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15608FF 19672 DURING 'A-2' SERVICE, FOUND EMERGENCY EXIT LIGHT ON 3L MED INOPERABLE, RELAMPED. OPS CHECK OK. (W) 2L74 4F A20WE 19950428007671995042800767NM 1995 4 28 TWRA9527 119950401A3350 EEL BOEING747 747131 1384881NM CABIN LOOSE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15608FF 19672 DURING 'A-2' SERVICE, FOUND 'E' ZONE E PATH LIGHTING INOPERABLE ON RIGHT SIDE. FOUND LOOSE CONNECTION AT SEAT 50, RECONNECTED. OPS CHECK OK. (W) 2L74 4F A20WE 19950428007681995042800768SO 1995 4 28 WTAA950121 119950311A323012043270001 RELAY CONTL BOX EMB 120 EMB120RT SO COCKPIT FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17280UE 120090 MRY - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT. MAINTENANCE REPLACED LANDING GEAR RELAY CONTROL BOX. ACCOMPLISHED LANDING GEAR RETRACTION CHECK ON GROUND. LANDING GEAR OPERATION AND POSITION INDICATIONS NORMAL. PERFORMED TEST FLIGHT AND FOUND SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505000011995050500001WP 1995 5 5 9506671158 119950426A5347 SEAT TRACK DOUG DC10 DC1040 3023508WP FS 1476-1510 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1476 - 1510, LBL 107. REMOVED CORROSION AND INSTALLED REPAIR. 2L73 4F A22WE 19950505000021995050500002NM 1995 5 5 9506686305 119950426A5320 SUPPORT BOEING747 747451 1384940NM FS 980-1000 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR BEAM AT FS 980 - 1000, RBL 20 - 30. REPLACED INTERCOSTAL AND REPAIRED PER EA 63-97992. 2L74 4F RTA20WE 19950505000031995050500003NM 1995 5 5 9506696305 119950419A5315 FLOOR BEAM BOEING747 747451 1384940NM FS 980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01665US 23820 DURING PERIODIC INSPECTION, FOUND CORROSION ON THE UPPER DECK FLOOR BEAM FAIL SAFE STRAP AT FS 980, RBL 16 - RBL 34. REMOVED DAMAGE AREA AND INSTALLED REPAIR DOUBLERS AND STRAP PER EA 63-97992. 2L74 4F RTA20WE 19950505000041995050500004NM 1995 5 5 9506706615 119950425A7711 EPR INDICATION BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 4 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01615US 20360 702451 DURING TAKEOFF ROLL BELOW 60 KTS (TPE), THE NR 4 ENGINE HAD SLOW EPR RISE AND THE TAKEOFF WAS ABORTED. AN EPR CHECK BY THE CREW ON THE TAXIWAY CHECKED OK AND A NORMAL TAKEOFF WAS THEN MADE. THE ENGINE WAS INSPECTED. ALL SENSE LINES AND ELECTRICAL CONNECTORS WERE CHECKED AND FOUND TO BE OK. 2L74 4F4 F A20WE E3NE 19950505000051995050500005WP 1995 5 5 9506711158 119950427A5320 SUPPORT DOUG DC10 DC1040 3023508WP FS 440 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 440, RBL 2 - 6. REPLACED THE FLOOR SUPPORT. 2L73 4F A22WE 19950505000061995050500006WP 1995 5 5 9506721158 119950427A5347 SEAT TRACK DOUG DC10 DC1040 3023508WP FS 1311-1399 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SEAT TRACK AT FS 1311 - 1399, LBL 107. REMOVED CORROSION AND REPAIRED SEAT TRACK. 2L73 4F A22WE 19950505000071995050500007WP 1995 5 5 9506731158 119950427A5320 SUPPORT DOUG DC10 DC1040 3023508WP FS 459 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT FS 459, LBL 6 TO RBL 56. REPLACED FLOOR SUPPORT. 2L73 4F A22WE 19950505000081995050500008NM 1995 5 5 DL72E951631 119950413A711065196854540 NOSE COWL BOEING727 727247 138408FNM NR 1 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 000008 DURING A ROUTINE SHOP INSPECTION THE OUTER SKIN OF A NOSE COWL WAS FOUND TO HAVE A CRACK BETWEEN 3 RIVET HOLES AT 3 O/C POSITION. INSTALLED FLUSH DOUBLER PER SRM 54-10-3 FIG 3A. 2L73 4F A3WE 19950505000091995050500009NM 1995 5 5 DL72E951632 119950413A711065196854540 NOSE COWL BOEING727 727247 138408FNM NR 1 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 000008 DURING SHOP INSP, NR 1 ENGINE NOSE COWL WAS FOUND WITH A CRACK IN AFT BULKHEAD INNER ANGLE. INSTALLED DOUBLER PER SRM 54-10-3 FIG 3. 2L73 4F A3WE 19950505000101995050500010NM 1995 5 5 DL72S951598 119950403A711065196854539 COWLING BOEING727 727232 1384082NM NR 1 ENG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 000008 NOSE COWL NR 1 ENG WAS FOUND WITH TIME LIMITED REPAIR AT 6 O'CLOCK POSITION. THE COWL WAS REPAIRED PER SRM 54-30-3. 2L73 4F A3WE 19950505000111995050500011NM 1995 5 5 DL72S951611 119950419A5320 WEB BOEING727 727232 1384082NM FS 1220 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 000008 CRACK, .25 INCH, IN WEB AT STA 1220 IN LT TORQUE BOX. TWO EA .25 INCH CRACKS IN RT TORQUE BOX WEB AT STA 1220, .1875 INCH CRACK AT LIGHTING HOLE AT STA 1220, RT TORQUE BOX. ALL CRACKS LOCATED IN 48 SECTION. FOUND AT E-2 LTR CHECK, REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950505000121995050500012NM 1995 5 5 DL72S951612 119950419A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 000008 NR 3 SLAT LWR CHORD ANGLE CRACKED .50 INCH BELOW TAI DUCT. FOUND DURING E-2 LTR CK TPA MM. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950505000131995050500013NM 1995 5 5 DL72S951613 119950419A5754 BRACKET BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 000008 NR 2 L/E FLAP I/B ACT ATTACH BRKT CRACKED UPPER AND LWR ENDS. FOUND DURING E-2 LTR CK. TPA MM. REPAIRED PER MM 57-20-21 PG 811. 2L73 4F A3WE 19950505000141995050500014NM 1995 5 5 DL72S951624 119950415A5311 FRAME BOEING727 727232 1384082NM FS 1090 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000008 DURING INSPECTIONS PER E.O. 4-52217-3AD, THE STA 1090 FRAME (0.080 INCH 7075-T6) WAS FOUND CRACKED ABOVE STR 27R. REPAIR/ MODIFICATION PER E.O. 4-52217-03AD WILL BE INCORPORATED. FOUND AND REPAIRED AT HMV. 2L73 4F A3WE 19950505000151995050500015NM 1995 5 5 DL72S951645 119950407A5720 BEAM BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000008 FOUND AT HMV. UPPER T/E SUPPORT BEAM CRACKED AT NR 8 SPOILER ACTUATOR CUTOUT. REPAIRED BEAM PER MM 57-20-22 FIG 809. 2L73 4F A3WE 19950505000161995050500016NM 1995 5 5 DL72S951646 119950401A5311 FRAME BOEING727 727232 1384082NM FS 910 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000008 AT HMV, COMPLIED WITH SCHEDULED PERMANENT REPAIR TO RT MLG UPLOCK ATTACH FRAME AT FS 910. INSTALLED REPAIRS PER MM 53-11-0 PG 814. 2L73 4F A3WE 19950505000171995050500017NM 1995 5 5 DL72S951647 119950401A5311 FRAME BOEING727 727232 1384082NM FS 913 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000008 AT HMV FROM SCHEDULED MTC SHEET. COMPLY WITH PERMANENT REPAIR PER 53-11-0 STA 913 AFT RT WHEEL WELL. REPAIRED PER MM 53-11-0 PG 814. 2L73 4F A3WE 19950505000181995050500018NM 1995 5 5 DL72S951648 119950409A5315 FLOOR BEAM BOEING727 727232 1384082NM FS 360 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000008 FOUND AT HMV. FLOOR BEAM CORRODED AT STA 360 BETWEEN RBL AND LBL 25 AT FLOOR MOUNT HOLES. REPAIRED PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950505000191995050500019NM 1995 5 5 DL72W951543 119950413A5347 SEAT TRACK BOEING727 727247 138408FNM FS 344-380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING HMV, FOUND RT INBD SEAT TRACK CORRODED STA 344-380. REPLACED PER SRM 53-10-5 FIG 8. 2L73 4F A3WE 19950505000201995050500020NM 1995 5 5 DL72W951544 119950413A5347 SEAT TRACK BOEING727 727247 138408FNM FS 350 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING HMV, FOUND LT INBD SEAT TRACK CORRODED STA 350. REPAIRED PER SRM 53-10-5. 2L73 4F A3WE 19950505000211995050500021NM 1995 5 5 DL72W951545 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING HMV, FOUND STRINGER 27R CORRODED AT END, FWD OF STA 740. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950505000221995050500022NM 1995 5 5 DL72W951546 119950401A5313 STRINGER BOEING727 727247 138408FNM FS 720 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING HMV, FOUND CORROSION IN S27R AT STA 720F. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950505000231995050500023NM 1995 5 5 DL72W951549 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 706 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND STRINGER 26R CORRODED AT STA 706. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950505000241995050500024NM 1995 5 5 DL72W951550 119950330A5350 BOW BOEING727 727247 138408FNM FAIRING NR 9705 FRETTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND BOW FRETTED ON BOTH SIDES AT FWD END OF FAIRING NR 9705. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950505000251995050500025NM 1995 5 5 DL72W951551 119950407A5743 ATTACH FITTING BOEING727 727247 138408FNM LT MLG ELONGATED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 DURING HMV, FOUND HOLES ELONGATED LMLG SUPPORT BEAM ATTACH FITTING. REPAIRED PER SRM 57-40 PG. 3. 2L73 4F A3WE 19950505000261995050500026NM 1995 5 5 DL72W951601 119950418A5755659892433 ANGLE BOEING727 727247 138408FNM NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112815W 20871 000008 NR 2 SPOILER I/B CASTING MOUNT LUG BROKEN. FOUND AT D-2 LETTER CHECK, REPLACED ATTACH ANGLE PER MM 57-42-0. 2L73 4F A3WE 19950505000271995050500027NM 1995 5 5 DL72W951602 119950418A5754 ANGLE BOEING727 727247 138408FNM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112815W 20871 000008 NR 2 SLAT, ANGLE CRACKED UNDER I/B STOP PAD. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 57-54-0 PG 12. 2L73 4F A3WE 19950505000281995050500028NM 1995 5 5 DL72W951603 119950418A5320 WEB BOEING727 727247 138408FNM FS 1213 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112815W 20871 000008 ONE-HALF INCH CRACK FOUND AT UPPER END OF VERT. WEB AT TORQUE BOX, RIGHT SIDE OF FS 1213. FOUND AT D-2 LETTER CHECK. REPAIRED PER MM 53-11-0 PG 832-833. 2L73 4F A3WE 19950505000291995050500029NM 1995 5 5 DL72W951614 119950405A5312 BLKHD SUPPORT BOEING727 727247 138408FNM FS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 DURING HMV, FOUND SUPPORT WORN LT BULKHEAD, FS 720D. REPAIRED PER SRM 53-10-9 FIG 8. 2L73 4F A3WE 19950505000301995050500030NM 1995 5 5 DL72W951615 119950405A5312 SUPPORT BOEING727 727247 138408FNM FS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 AT HMV, FOUND SUPPORT WORN RT BULKHEAD. FS 720D RBL 24. REPAIRED PER SRM 53-10-9 FIG 8. 2L73 4F A3WE 19950505000311995050500031NM 1995 5 5 DL72W951616 119950412A5755 PANEL BOEING727 727247 138408FNM NR 11 SPOILER DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 11 SPOILER PANEL REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950505000321995050500032NM 1995 5 5 DL72W951617 119950412A5755 PANEL BOEING727 727247 138408FNM NR 12 SPOILER DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 DURING HMV, FOUND SPOILER PANEL DISBONDING. NR 12 SPOILER PANEL REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950505000331995050500033NM 1995 5 5 DL72W951650 119950416A5240 FRAME BOEING727 727247 138408FNM L2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 THE L2 DOOR FRAME (ON DOOR) IS CRACKED AT UPPER HINGE, LWR O/B CORNER. REPAIRED PER SRM 52-40-2 PG13-15. 2L73 4F A3WE 19950505000341995050500034NM 1995 5 5 DL72W951651 119950331A5320 SUPPORT BEAM BOEING727 727247 138408FNM FS 848-870 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000008 BEAM CORRODED. STA 848-870 RBL-10 SUPPORT BEAM CORRODED AT PNL 3455R HINGE LOCATIONS, LOWER FUSELAGE ACCESS PANELS. FOUND AT HMV. 2L73 4F A3WE 19950505000351995050500035NM 1995 5 5 DL73S951629 119950317A71106585378396 NOSE COWL BOEING737 737232 1384475NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11314DA 23086 000008 DURING SHOP INSPECTION, A .5 INCH CRACK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. 2L72 4F RTA16WE 19950505000361995050500036NM 1995 5 5 DL73S951630 119950317A71106585378396 NOSE COWL BOEING737 737232 1384475NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11314DA 23086 000008 DURING SHOP INSPECTION, A DEEP NICK WAS FOUND IN THE LEADING EDGE LIP OF NR 2 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3 FIG. 4. 2L72 4F RTA16WE 19950505000371995050500037WP 1995 5 5 DLL10951620 119950420A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11712DA 193C1088 000008 DURING SPECIAL INSPECTION, CRACKS WERE FOUND IN MAIN FUSELAGE FRAMES AT RIGHT SIDE FS 569, 649, 669, 689, 769, 1625, 1685, 1705. LEFT SIDE AT FS 1023, 1063, 1343, 1665, 1705. ALL CRACKS WERE AT WL 280. THESE CRACKS WERE FOUND AS A RESULT OF A SPECIAL INSPECTION FOR AIRCRAFT WITH 22,000 CYCLES AND HIGHER. THIS IS THE FIRST TIME CRACKS WERE FOUND AT THESE LOCATIONS ON DL AIRCRAFT. 2L73 4F A23WE 19950505000381995050500038WP 1995 5 5 DLL10951649 119950404A55221524058112 SKIN LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000008 TEMPORARY REPAIR INSTALLED ON RT ELEVATOR LOWER OTBD END. REPLACED WITH PERMANENT REPAIR PER SRM 55-22-00 FIG 802 WHICH REQUIRES AN MRR. 2L73 4F A23WE 19950505000391995050500039NM 1995 5 5 DLM88951608 119950419A5311 FRAME DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11933DL 49720 000008 TWO INCH CRACK FOUND AT WHEELWELL FWD FRAME O/B END. FOUND AT A-1 LETTER CHECK. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950505000401995050500040NM 1995 5 5 DLM88951731 119950425A2910AS15408H0327 HYD HOSE DOUG MD88 MD88 3023688NM NR 2 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11927DA 49714 DURING CLIMBOUT, RIGHT HYDRAULIC SYSTEM FAILED ON GEAR RETRACTION. RETURNED ATL. FOUND HOSE FROM RIGHT ENGINE PUMP RUBBED THROUGH AT CLAMP. REPLACED HOSE AND CLAMP OPERATION NORMAL. 2L72 4F RTA6WE 19950505000411995050500041NM 1995 5 5 DLM88951732 119950425A2420947F9463 GEN CONTROL DOUG MD88 MD88 3023688NM EE COMPT FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11918DL 49583 ON CLIMBOUT, LOST RIGHT ENGINE GENERATOR. APU WAS DEFERRED, RETURNED JFK. REPLACED GENERATOR CONTROL UNIT OPERATION NORMAL. 2L72 4F RTA6WE 19950505000421995050500042NM 1995 5 5 QXEA9500129 119950429A2611376 LAMP KIDDE 302313 DHAV DHC8 DHC8102 2809003NM AFT CARGO COMPT FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09821PH 30250 104 MFR - DURING PREFLIGHT TEST, FOUND NR 1 SMOKE DETECTOR INOP. PLACED ON MEL AND CONTINUED TO PDX. AT PDX FOUND REFERENCE LAMP BURNED OUT, REPLACED BOTH LAMPS, TESTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950505000431995050500043WP 1995 5 5 SCNA95064 119950426A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 FORWARD CABIN LIGHT WILL NOT TEST. REMOVED AND REPLACED FORWARD CABIN EMERGENCY LIGHT POWER SUPPLY AND BATTERY. OPS CHECK GOOD. 2L73 4F A22WE 19950505000441995050500044WP 1995 5 5 SCNA95065 119950426A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 MID CABIN EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED MID CABIN EMERGENCY LIGHT POWER SUPPLY. FIXED SHORTED WIRE AT L2 DOOR EXIT LIGHT. LIGHTS OPS CHECKED GOOD. 2L73 4F A22WE 19950505000451995050500045NE 1995 5 5 SWAA950301 219950423A723065737691 COMPRESSOR BOEING737 7372H4 138448CNM GE CFM56 CFM563B1 13802NE NR 1 ENGINE STALLED A SWAAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SW07103SW 23109 667248 EN ROUTE PHX TO AUS, CREW EXPERIENCED NR 1 ENGINE COMPRESSOR STALL. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. BORESCOPED INSPECTED AND DETERMINED ENGINE CHANGE REQUIRED. REPLACED ENGINE ASSEMBLY AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F4 F A16WE E2GL 19950505000461995050500046NM 1995 5 5 SWAA950302 119950426A5330 SKIN BOEING737 7373Q8 1384670NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING LOCATIONS: BS 910, WL 185, ABOVE STRINGER 19R, AT BS 932, AT S24L, AND AT BS 324, BETWEEN S22 AND 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000471995050500047NM 1995 5 5 SWAA950303 119950426A5330 SKIN BOEING737 7373Q8 1384670NM BS 306 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED AT BS 306, WL 255, 3 INCHES BELOW FWD ENTRY DOOR AT HINGE UPPER HINGE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000481995050500048NM 1995 5 5 SWAA950304 119950426A5330 SKIN BOEING737 7373Q8 1384670NM FS 305/320 NICKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN NICKED AND SCRATCHED AT BS 305 AND 320, BETWEEN S3 AND 4L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000491995050500049NM 1995 5 5 SWAA950305 119950426A5210 SKIN BOEING737 7373Q8 1384670NM BS 990-1016 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOOR SKIN DENTED AT BS 990-1016, BETWEEN S8 AND 10L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000501995050500050NM 1995 5 5 SWAA950306 119950426A5315BAC1505100617 FLOORBEAM BOEING737 7373Q8 1384670NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 45, WL 208, AT BS 294.5, LBL 19, WL 208, AND AT BS 328, RBL 34 AND 48, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000511995050500051NM 1995 5 5 SWAA950307 119950426A53206937254114 CLIP BOEING737 7373Q8 1384670NM BS 570 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND LEFT AND RIGHT SKATE ANGLES CRACKED AT BS 570, WL 167.5, RBL 59. REPLACED PER BOEING M/M. 2L72 4F RTA16WE 19950505000521995050500052NM 1995 5 5 SWAA950308 119950426A5320 DOOR FRAME BOEING737 7373Q8 1384670NM BS 727B DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND AFT CARGO FRAME DENTED AT 727B, S24R, RBL 32. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000531995050500053NM 1995 5 5 SWAA950309 119950426A5311 FRAME BOEING737 7373Q8 1384670NM BS 1104 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND DEEP GOUGE AT FRAME AT BS 1104, AT S14R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000541995050500054NM 1995 5 5 SWAA950310 119950426A5311 FRAME BOEING737 7373Q8 1384670NM BS 439 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FWD CARGO DOOR FWD FRAME TO SIDEWALL SUPPORT DENTED AND GOUGED AT BS 439, WL 158, RBL 27. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000551995050500055NM 1995 5 5 SWAA950311 119950426A5312 BULKHEAD BOEING737 7373Q8 1384670NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 178, WL 195, ACCESS PLATE CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000561995050500056NM 1995 5 5 SWAA950312 119950426A5320 SHEAR TIE BOEING737 7373Q8 1384670NM BS 927 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND SHEAR TIE CORRODED AT BS 927, LBL 22, WL 164. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000571995050500057NM 1995 5 5 SWAA950313 119950426A5330 SKIN BOEING737 7373Q8 1384670NM FUSELAGE DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN FROM BS 520 TO 578, BETWEEN S1 AND 3R, AND AT BS 500D TO 520, BETWEEN S2 AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505000581995050500058WP 1995 5 5 UPS803122 119950421A3260 GEAR INDICATION DOUG DC8 DC873F 302199FWP NLG MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01819UP 46019 PILOT REPORTED THAT AFTER TAKE OFF GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND COMPLIED WITH CHECKLIST BUT LIGHT REMAINED ON. DURING CHECK, NOSE GEAR WAS UP. PERFORMED GEAR UP LIMIT SWITCH CHECK PER MM 32-60-00. NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF ALL THREE GEAR LATCHES. NO DEFECTS NOTED. 2L74 4F RT4A25 19950505000591995050500059CE 1995 5 5 95ZZZX2094 119950327A3297 WIRE 1013880083 BEECH 300 300BEECH 1152930CE LANDING GEAR SHORTED A RU3AO OTHER J WARNING INDICATION LDLANDING 1 SW2167 3432 3432 FF2 LANDING GEAR CIRCUIT BREAKER TRIPPED. WOULD NOT RESET, GEAR PUMPED DOWN, 3 GREEN INDICATED. PERFORMED INSPECTION OF ALL ACCESSIBLE LANDING GEAR COMPONENTS AND COMPLETED SYSTEMS OPERATIONAL CHECKS. NO DISCREPANCIES WERE FOUND DURING INSPECTION AND LANDING GEAR PERFORMS SATISFACTORILY IAW T14128.2. BEECHCRAFT TECHNICAL REPRESENTATIVE CONSULTED. INVESTIGATION OF THIS CONDITION CONTINUED AT THIS TIME. UPDATE: 3-29-95 - REPAIRED SHORTED WIRE ON MICROSWITCH FOR LANDING GEAR SERVICE VALVE. VERIFIED PROPER OPERATION OF LANDING GEAR. FINAL INSPECTION OF RII COMPLETED BY INSPECTOR. (X) 2L72 4T A24CE 19950505000601995050500060NM 1995 5 5 95ZZZX2095 119950415A3260 PROX SWITCH BOEING737 737297 1384480NM LT MLG MALFUNCTIONED A TSAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP13728AL 22629 HNL/ITO - FLT 42 - PILOT REPORT, LEFT MAIN GEAR UNSAFE LIGHT FLICKERS ON AND OFF WITH GEAR HANDLE IN UP AND OFF POSITION. UNABLE TO DUPLICATE ON GROUND. ADJUSTED LT MLG UPLOCK PROXIMITY SENSOR GAP PER MM 32-61-21 AND REPLACED LT MLG UPLOCK PROXIMITY SWITCH PC CARD A16, LANDING GEAR P/C CARD A-15 EXTENDED AND RETRACTED LT MLG SEVERAL TIMES. NO DISCREPANCIES NOTED. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. REFERENCE OPER CONTROL NR TSAA9532057. 2L72 4F A16WE 19950505000611995050500061NM 1995 5 5 CAL950233 119950326A2782651781822 ACTUATOR BOEING727 727227 1384078NM NR 3 SLAT CRACKED A CALAO OTHER JK WARNING INDICATION FLUID LOSS APAPPROACH 1 SW0916762 21245 FLL - FLT 0385 - THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO FLL. HYDAULIC LOSS CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 LEADING EDGE SLAT ACTUATOR CRACKED AND LEAKING. THE SLAT ACTUATOR WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950505000621995050500062NM 1995 5 5 CAL950271 119950414A323065404676 LOCK ACTUATOR BOEING727 727232 1384082NM NLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09523PE191255664 20646 IAH - FLT 9864 - THE AIRCRAFT HAD A BRIEF HISTORY OF SLOW NLG EXTENSION. WHEN MAINTENANCE SWUNG THE NOSE GEAR, NO DEFECTS WERE FOUND. THE NOSE GEAR LOCK ACTUATOR WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE NOSE GEAR WAS SWUNG AGAIN AND OPERATION CHECKED NORMAL. A NOSE GEAR EXTENSION AND RETRACTION TEST WAS PERFORMED IAW MM 32-33-0 AND THE GEAR OPERATED WITHIN SPECIFIED TIMES. IN ADDITION, NLG WAS LUBRICATED. (X) 2L73 4F A3WE 19950505000631995050500063NM 1995 5 5 CAL950273 119950415A2910 HYD MODULE BOEING737 737217 1384464NM A-HYD FAILED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914233 19887 GSO - FLT 1735 - THE A-HYDRAULIC SYSTEM PRESSURE DROPPED TO ZERO DURING CLIMB OUT OF GSO. CHECK LIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CHECK VALVE FAILURE OF THE A-HYDRAULIC SYSTEM MODULE. THE A-SYSTEM MODULE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE HYDRUALIC WAS SERVICED IAW MM 29-11-61. (X) 2L72 4F A16WE 19950505000641995050500064NM 1995 5 5 CAL950285 119950417A3260 CIRCUIT BREAKER BOEING737 7373T0 1384582NM NLG TRIPPED A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0970352 23590 EWR - FLT 1442 - ONLY THE RED NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER THE GEAR WAS SELECTED DOWN ON APPROACH TO EWR. IN AN ATTEMPT TO RECYCLE THE GEAR LOCK OVERRIDE HAD TO GET GEAR UP. THE GEAR WAS SELECTED DOWN AGAIN, BUT ONLY THE RED NOSE GEAR LIGHT ILLUMINATED. THE GEAR WAS CONFIRMED DOWN AND LOCKED THROUGH THE VIEW PORTS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR/GROUND LIGHTS CIRCUIT BREAKER TRIPPED. THE CIRCUIT BREAKER WAS RESET. MAINTENANCE WAS UNABLE TO DUPLICATE TRIPPING OF THE CIRCUIT BREAKER. (X) 2L72 4F RTA16WE 19950505000651995050500065NM 1995 5 5 CAL950294 119950418A291065445101472 HYD LINE BOEING737 737130 1384435NM A-HYD SYST LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW0933202 19019 EWR - FLT 1477 - THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON DESCENT INTO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE A-SYSTEM HYDRAULIC PRESSURE LINE IN LEFT WING ABOVE LEFT GEAR LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITH RIGID LINE WITHIN 500 FLIGHTS OR 1200 HOURS, WHICHEVER COMES FIRST. (X) 2L72 4F A16WE 19950505000661995050500066 1995 5 5 IXKA9500015 419950409A34565100283 OMEGA ANTENNA LITTON 5100283 BOEING727 727225 1384077NM HORIZ STAB MISSING A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 EWR - A/C INBOARD LOG ITEM OMEGA UNABLE TO RECEIVE ANY STATION. ON INSPECTION, FOUND OMEGA ANTENNA MISSING, MOUNTING RECEPTACLE AND CONNECTOR RIPPED OUT OF HORIZONTAL STABILIZER TAIL CONE. REPAIRED MOUNTING RECEPTACLES FOR OMEGA ANTENNA PER SRM 51-40-9 AND REPLACED CONNECTOR AND OMEGA ANTENNA PER MM 34-68-11, OPS CHECK OKAY. (X) 2L73 4F A3WE 19950505000671995050500067NM 1995 5 5 MZZA95018 119950409A3510 OXYGEN BOTTLE BOEING727 7272F9 138407DNM COCKPIT MALFUNCTIONED A MZZAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13298AS 21426 GUM - FLT 958 - CREW OXYGEN SYSTEM PRESSURE WENT TO ZERO DURING FLIGHT. PRE-FLIGHT PRESSURE WAS APPROX 1800 PSI, ALL REGULATORS CHECK OKAY, ALL SWITCHES CHECKED AT NORMAL, 100 PERCENT OXYGEN AND REGULATOR SUPPLY ON FOR 3 CREW MEMBERS, OFF FOR BOTH JUMP-SEAT REGULATORS. AIRCRAFT DIVERTED TO GUAM. MAINTENANCE REPLACED CREWS OXYGEN BOTTLE, LEAK CHECKED REGULATORS, HOSES, AND OXYGEN LINES AND FOUND NO LEAKS. OXYGEN PRESSURE CHECKED NORMAL AND INDICATE NO DECREASE IN SIX HOURS. (X) 2L73 4F RTA3WE 19950505000681995050500068NM 1995 5 5 MZZA95024 119950414A2611824PTY SMOKE DETECTOR BOEING727 727232 1384082NM LAVATORY INOPERATIVE A MZZAK NONE O OTHER ININSP/MAINT 1 WP1315781 20636 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FORWARD AND RT AFT LAVATORY SMOKE DETECTORS FOUND INOPERATIVE. THE DEFECTIVE SMOKE DETECTORS REMOVED AND REPLACED PER B727 MM 26-10-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0726932 AND NR 0726933 (SEQ. NR. 02142 AND NR 02143). (X) 2L73 4F A3WE 19950505000691995050500069NM 1995 5 5 MZZA9519 119950411A7931ST042 OIL PRESS TRANSM BOEING727 727224 1384076NM NR 1 ENGINE MALFUNCTIONED A MZZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP1379745 6969 22448 KHH - FLT 994 - L/P 7916155 - AFTER TAKEOFF, NR 1 ENGINE OIL PRESSURE WAS ABOVE RED LINE. WHEN THROTTLE RETARDED, OIL PRESSURE DECREASED. FLIGHT CREW REDUCED POWER AND AIR RETURNED TO KHH. MAINTENANCE REMOVED AND REPLACED THE OIL PRESSURE RELIEF VALVE AND OIL RPESSURE TRANSMITTER PER MM 79-32-1 AND ENGINE GROUND RUN, OPERATIONAL CHECK WAS NORMAL. (X) 2L73 4F A3WE 19950505000701995050500070NM 1995 5 5 MZZA9520 119950303A3350 EXIT SIGN BOEING727 727232 1384082NM AFT ENTRY DOOR CRACKED A MZZAK NONE O OTHER ININSP/MAINT 1 WP1315781 20636 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK FOUND ON PASSENGER CABIN AFT ENTRY DOOR EXIT SIGN COVER. THE DAMAGED EXIT SIGN ASSEMBLY REMOVED AND REPLACED WITH PN BR9279-105 ASSEMBLY PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF: HANGAR NON-ROUTINE REPAIR ITEM CARD NR 0729535 (SEQ NR 02045). (X) 2L73 4F A3WE 19950505000711995050500071NM 1995 5 5 MZZA9521 119950414A2820MA11A1062B VALVE 1715 BOEING727 727224 1384076NM FUEL MANIFOLD MALFUNCTIONED A MZZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP1379745 5931 22448 GUM - FLT 275 - L/P 7016123 - DUE TO NR 1 FUEL MANIFOLD VALVE PREVIOUSLY PLACARDED (MEL 28-07, L/P 791622) AND THE MANIFOLD VALVE SAFETIED IN THE OPEN POSITION, FLIGHT CREW REPORTED NR 1 TANK BURNED FUEL REGARDLESS IF THE BOOST PUMPS WERE TURNED OFF WHEN ATTEMPTING TO BURN FUEL FROM NR 2 TANK. CREW AIR RETURNED TO GUAM. MAINTENANCE REMOVED AND RPELACED NR 1 FUEL MANIFOLD VALVE PER MM 28-22-01 AND OPERATION CHECKED NORMAL. (X) 2L73 4F A3WE 19950505000721995050500072NM 1995 5 5 MZZA9522 119950417A73318TJ95GAB3 POWER SUPPLY GE BOEING727 727224 1384076NM FUEL FLOW SYS INOPERATIVE A MZZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP1379744 0171 22253 GUM - FLT 919 - L/P 7912625 - AFTER DEPARTURE, ALL FUEL FLOW INDICATORS WENT TO ZERO. AIRCRAFT RETURNED TO GUAM. AFTER TROUBLESHOOTING, THE AIRCRAFT FUEL FLOW POWER SUPPLY UNIT WAS FOUND AT FAULT. FUEL POWER SUPPLY UNIT WAS REMOVED AND REPLACED WITH SERVICEABLE UNIT. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. (X) 2L73 4F A3WE 19950505000731995050500073EU 1995 5 5 PAYA95A4015 119950329A5210 DOOR AEROSPATR42 ATR42300 8680920EU PASSENGER COMPT CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174201G17552 048 DURING C-CHECK, CORROSION FOUND AT SEVERAL POINTS ON PASSENGER DOOR. REPAIRED AFFECTED AREAS. (X) 2H72 4T RTA53EU 19950505000741995050500074EU 1995 5 5 PAYA95A4016 119950329A5210 DOUBLER AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174201G17552 048 DURING C-CHECK, FOUND PASSENGER DOOR STOP AFT UPPER DOUBLER CRACKED. REPAIRED DOUBLER. (X) 2H72 4T RTA53EU 19950505000751995050500075EU 1995 5 5 PAYA95A4017 119950329A5712 RIB AEROSPATR42 ATR42300 8680920EU LT WING CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174201G17552 048 DURING C-CHECK, FOUND LEFT WING TIP RIB (RIB NR 30,Z516) CRACKED. REPLACED RIB. (X) 2H72 4T RTA53EU 19950505000761995050500076CE 1995 5 5 RU3A95004 119950405A212115238203 BLOWER MOTOR MC0F647331 BEECH 300 300BEECH 1152930CE AIR CONDITIONINGFAILED A RU3AAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW2181 FF16 CREW NOTICED A BURNING SMELL FROM WITHIN THE AVIONICS COMPARTMENT INSIDE THE CABIN. SUSPECTING THE AUXILIARY AIR CONDITIONING AFT EVAPORATOR BLOWER MOTOR, DEACTIVATED THE MOTOR WITH THE SWITCH IN THE COCKPIT. MAINTENANCE FOUND MOTOR HAD OVERHEATED AND BRUSHES WERE WORN OUT. THE BLOWER MOTOR WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4T A24CE 19950505000771995050500077CE 1995 5 5 RU3A95005 119950328A3260327 BULB 308607084300BEECH 300 300BEECH 1152930CE RT MLG FAILED A RU3AA UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 SW2171 FF6 PRECAUTIONARY LANDING WAS MADE AFTER NOSE AND RT MLG LIGHTS FAILED TO LIGHT DURING MANUAL EXTENSION. LIGHT BULBS IN GEAR LIGHTS WERE FOUND BURNED OUT. LIGHT BULBS WERE REPLACED AND GEAR WAS OPERATIONALLY CHECKED THROUGH 6 CYCLES, CHECKED OKAY. COMPONENT PN 3086070843004. (X) 2L72 4T A24CE 19950505000781995050500078NM 1995 5 5 TSAA9532056 119950410A323165462059 LINK ASSY BOEING737 7372T4 1384492NM NLG DOOR BROKEN A TSAAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP13808AL 23445 KOA/HNL - FLT 207 - PILOT REPORT, NOISE AND VIBRATION ABOVE 230 KNOTS IN-FLIGHT FROM FORWARD NOSE WHEEL AREA. REPLACED NOSE GEAR DOOR RT UPPER LINK. NOSE GEAR RETRACTION COMPLETED. INSPECTED DOOR, OPS CHECKED OKAY. NO OTHER DAMAGE NOTED IN NOSE AREA. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19950505000791995050500079NM 1995 5 5 TSAA9532057 119950415A3260 PROX SENSOR BOEING737 737297 1384480NM LT MLG MALFUNCTIONED A TSAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP13728AL 22629 HNL/ITO - FLT 42 - PILOT REPORT, LEFT MAIN GEAR UNSAFE LIGHT FLICKERS ON AND OFF WITH GEAR HANDLE IN UP AND OFF POSITION. UNABLE TO DUPLICATE ON GROUND. ADJUSTED LT MLG UPLOCK PROXIMITY SENSOR GAP PER MM 32-61-21 AND REPLACED LT MLG UPLOCK PROXIMITY SWITCH PC CARD A16, LANDING GEAR P/C CARD A-15 EXTENDED AND RETRACTED LT MLG SEVERAL TIMES. NO DISCRPANCIES NOTED. OKAY FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. REFERENCE OPER CONTROL NR 95ZZZX2095. (X) 2L72 4F A16WE 19950505000801995050500080SO 1995 5 5 WTAA950152 119950402A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO OVERHEAD PANEL OPEN A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17451UE 120108 FAT - AURAL 'TRIM WARNING' ACTIVATED AT INITIATION OF TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. CREW DISCOVERED AURAL WARNING CIRCUIT BREAKER PULLED ON OVERHEAD PANEL. RESET CIRCUIT BREAKER. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL. (X) 2L72 4T RTA31SO 19950505000811995050500081 1995 5 5 WTAA950153 419950405A3418C771075 LIFT TRANSDUCER BAG JETSTMJETSTM3101 1500215EU RT WING FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17429UE 807 PSC - STALL WARNING SYSTEM ACTIVATED AT 70 KTS. DURING TAKEOFF ROLL, TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SEA FOR MAINTENANCE. FOUND WIRES TO RT WING LIFT TRANSDUCER SHORTING AT CONNECTION. REPOSITIONED WIRE HARNESS AND RESECURED. STALL WARNING SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950505000821995050500082EU 1995 5 5 WTAA950154 119950405A3260622800200 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17103XV 747 FAT - RT MLG RED INTRANSIT LIGHT REPORTED INTERMITTENT ILLUMINATION. MAINTENANCE FOUND RT MAIN GEAR RADIUS ROD MICROSWITCH WORN CAUSING FALSE GEAR POSITION INDICATION. REPLACED MICROSWITCH. GEAR POSITION INDICATIONS OPERATIONAL CHECK NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950505000831995050500083SO 1995 5 5 WTAA950157 119950406A33503071BPE EEL LAMP EMB 120 EMB120RT SO CABIN FAILED A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17455UE 120163 FAT - FORWARD CABIN EMERGENCY EXIT LIGHT REPORTED INOPERATIVE DURING PRE-FLIGHT CHECK. MAINTENANCE REPLACED LAMP. SYSTEM OPERATIONAL CHECK NORMAL. (X) 2L72 4T RTA31SO 19950505000841995050500084EU 1995 5 5 WTAA950161 119950415A7331 CONNECTOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE DIRTY A WTAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP17107XV 723 FAT - EN ROUTE SFO TO VIS WITH LEFT FUEL QUANTITY INDICATION PREVIOUSLY DEFERRED PER MEL 28-1, RT ENGINE FUEL FLOW INDICATION FAILED IN-FLIGHT. AIRCRAFT DIVERTED TO STATION DUE TO DISPATCH REQUEST. MAINTENANCE CLEARED LT FUEL QTY INDICATION DEFERRAL WITH REPLACEMENT OF LT FUEL QUANTITY BRIDGE AMPLIFIER AND DEFERRED RT ENG FUEL FLOW METER PER MEL 73-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE FUEL FLOW METER DEFERRAL BY CLEANING ELEC CONNECTION AT RT ENGINE FUEL FLOW TRANSMITTER (PN TNAS1024L1182). (X) 2L72 4T RTA21EU 19950505000851995050500085WP 1995 5 5 95ZZZW586 119950315A57111528363250 SPAR WEB LKHEED1011 10113851 5265010WP WS 325-346 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 DURING FUELING AIRCRAFT IN BQN, FUEL WAS NOTICED LEAKING FROM RT MLG TRUNNION AREA. INSPECT AREA AND FOUND APPROX 20 INCH CRACK FROM THE UPPER SPAR CAP AT APPROX WING STATION 325 TO THE MLG FORGING AT APPROX WING STATION 346 ON THE REAR SPAR WEB. AIRCRAFT DEFUELED AND FUEL CELL ENTRY MADE TO PERFORM NDT INSPECTIONS REQUIRED BY LOCKHEED. TEMPORARY REPAIR ENGINEERED BY LOCKHEED BEING INSTALLED FOR FERRY FLIGHT TO DELTA AIR LINES IN ALTANTA, GA. 2L73 4F A23WE 19950505000861995050500086NE 1995 5 5 95ZZZW587 219950410A7250311294301 LUGS BEECH 1900 1900D 1154162CE PWA PT6 PT6A67 52043NE ENGINE WORN A JJBAK NONE O OTHER TXTAXI/GRND HDL 1 EA01833CA4922 UE24 RIGHT ENGINE RUBBING NOISE COMING FROM POWER SECTION AFTER SHUTDOWN AND THEN DISAPPEARS UPON COMPLETE COOL DOWN OF ENGINE. INVESTIGATION REVEALED THAT ANTI-ROTATION LUGS WERE WORN APPROXIMATELY .060. UNIT WAS NOT MODIFIED BY S/B 14206. 2L72 4T4 TRTA24CE E26NE 19950505000871995050500087SO 1995 5 5 C2XA95CL067 119950414A7931APT79100080D PRESS SWITCH EMB 120 EMB120RT SO LT ENG MALFUNCTIONED A C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0934712 33649100 120111 FLT NR 3225 - CLE- WHILE EN ROUTE AT CRUISE, THE LEFT ENGINE OIL PRESSURE CLIMB WAS ABOVE REDLINE. PULLED POWER BACK TO 50 PERCENT AND THE OIL PRESSURE DROPPED BACK TO NORMAL. TRIED TO RESTORE CRUISE POWER BUT AT 70 PERCENT TORQUE THE OIL PRESSURE BEGAN RISING RAPIDLY. PULLED POWER BACK TO 50 PERCENT AND GOT NORMAL PRESSURE. CLE MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE SWITCH AND REMOVE ONE WASHER FROM THE REGULATOR VALVE IAW EMB-120 MM 79-21-00 AND 79-31-01. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505000881995050500088SO 1995 5 5 C2XA95CL068 119950414A7931310573501 PRESS VALVE EMB 120 EMB120RT SO LT ENGINE FAILED A C2XACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SW0934712 2540 120111 FLT NR 3292 - CLE - ON TAKEOFF ROLL LEFT ENGINE OIL PRESSURE EXCEEDED REDLINE. TAKEOFF WAS ABORTED. CLE MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE OIL PRESSURE REGULATOR VALVE IAW PW118 MM 72-01-50. ADJUSTED OIL PRESSURE IAW EMB-120 MM 79-21-00. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505000891995050500089NE 1995 5 5 C2XA95CL069 219950415A73103035681 FUEL FILTER AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 ENGINE DIRTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914821 160 120393 FLT NR 3763 - EWR - FUEL CLOG LIGHT (NR 1 ENGINE) CAME ON AFTER TAKEOFF. RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED NR 1 FUEL PUMP OUTLET FILTER. OPS CHECK GOOD. RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950505000901995050500090SO 1995 5 5 C2XA95CL070 119950416A7931SEDL0C4BC PRESSURE GAUGE EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A C2XACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SW0934712 0364 120111 FLT 3343 - CLE-CMH - ON TAKEOFF ROLL AT TAKEOFF POWER LEFT ENGINE OIL PRESSURE GAUGE PEGGED AT 80 PSI. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE GAUGE. OPS CHECKED GOOD RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505000911995050500091EU 1995 5 5 C2XA95CL071 119950416A2910S2918056213000 HYD LINE AEROSPATR42 ATR42320 8680930EU HYD BAY RUPTURE A C2XAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW0918814 103 FLT 3544 - EWR-PIT - LOST BRAKES WHILE TAXIING. MAINTENANCE REMOVED AND REPLACED LEFT (FORWARD) BRAKE METERING VALVE HYDRAULIC LINE. OPS AND LEAK CHECK GOOD. RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950505000921995050500092SO 1995 5 5 C2XA95IA049 119950413A572012017057005 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 34 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 34 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000931995050500093SO 1995 5 5 C2XA95IA050 119950413A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 22 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 22 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000941995050500094SO 1995 5 5 C2XA95IA051 119950413A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF RIVET, THE SKIN SUPPORT NR 25 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 25 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000951995050500095SO 1995 5 5 C2XA95IA052 119950413A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 35 ON RIB NR 16 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 35 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000961995050500096SO 1995 5 5 C2XA95IA053 119950413A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 24 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 24 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000971995050500097SO 1995 5 5 C2XA95IA054 119950413A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING A LINE CHECK INSPECTION A LOOSE RIVET WAS FOUND ON THE LEFT WING. UPON REPLACEMENT OF THE RIVET, THE SKIN SUPPORT NR 23 ON RIB NR 15 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT NR 23 IAW EMB 120 SRM 51-40-02. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4T RTA31SO 19950505000981995050500098SO 1995 5 5 C2XA95IA055 119950419A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED LEFT AFT SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505000991995050500099SO 1995 5 5 C2XA95IA056 119950419A572012017057007 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505001001995050500100SO 1995 5 5 C2XA95IA057 119950419A572012017056007 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505001011995050500101SO 1995 5 5 C2XA95IA058 119950419A572012017056015 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505001021995050500102SO 1995 5 5 C2XA95IA059 119950419A572012017056019 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505001031995050500103SO 1995 5 5 C2XA95IA060 119950419A572012017056017 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950505001041995050500104SO 1995 5 5 C2XA95IA061 119950419A572012017056007 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING C-CHECK INSPECTION, DISCOVERED CRACKED RIB TO WING SUPPORT BRACKET. MAINTENANCE REMOVED AND REPLACED BRACKET. RETURNED TO SERVICE. 2L72 4T RTA31SO 19950505001051995050500105EU 1995 5 5 C2XA95IA062 119950420A7120S5411020001000 MOUNT AEROSPATR42 ATR42320 8680930EU RT ENGINE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0934805 073 IAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE FORWARD MOUNT TUBE TO HAVE CHAFE DAMAGE, AND AN INCOMPLETE WELDED JOINT. MAINTENANCE REMOVED AND REPLACED THE MOUNT TUBE, AIRCRAFT APPROVED FOR RETURN TO SERVICE ATR 42 MM 54-11-61. (W) 2H72 4T RTA53EU 19950505001061995050500106EU 1995 5 5 C2XA95IA063 119950420A7120S5421020000400 MOUNT AEROSPATR42 ATR42320 8680930EU RT ENGINE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0934805 073 IAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE INBOARD AFT Z-MOUNT TUBE CHAFED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE INBOARD AFT Z-MOUNT. AIRCRAFT APPROVED FOR RETURN TO SERVICE ATR 42MM 54-21-61. (W) 2H72 4T RTA53EU 19950505001071995050500107EU 1995 5 5 C2XA95IA064 119950420A7120S54210200011000 MOUNT AEROSPATR42 ATR42320 8680930EU RT ENGINE CHAFED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0934805 073 IAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE OUTBOARD AFT Z-MOUNT TO HAVE CHAFE DAMAGE IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD Z-MOUNT. AIRCRAFT APPROVED FOR RETURN TO SERVICE ATR42 MM 54-21-61. (W) 2H72 4T RTA53EU 19950505001081995050500108EU 1995 5 5 SIMA950761 119950317A324650092361 WHEEL 5010488 SAAB SF340 SF340A 7850100EU NR 4 MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21346SB2875 88 AUG920551 340A118 ORD - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN ORD AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 10 INCHES OF FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950505001091995050500109EU 1995 5 5 SIMA950782 119950319A324650092361 WHEEL 5010488 SAAB SF340 SF340A 7850100EU NR 1 MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21107AE178 5 OCT941210 340A107 ORD - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN ORD AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 11 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950505001101995050500110EU 1995 5 5 SIMA950783 119950319A326050092361 WHEEL 5010488 SAAB SF340 340B 7860101EU NR 3 MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21588MA2236 11 MAY931236 340B169 TOL - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN TOL AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 18 INCHES OF INNER FLANGE BROKEN OF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950505001111995050500111NE 1995 5 5 SIMA950801 319950321A6114660714200 HUB SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE LT PROP CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21119AE5560 110979 340A119 DRG153788 LAW - DURING ROUTINE NDT INSPECTION OF PROPELLER HUB P/N 660714200, S/N 110979. A CRACK WAS FOUND RUNNING VERTICAL IN DOWEL PIN HOLE BETWEEN BOLT HOLES NR 5 AND NR 6. CRACK APPROXIMATELY .25 INCH LONG. HUB WAS REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 6 CP61GL 19950505001121995050500112NE 1995 5 5 SIMA950862 219950327A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RIGHT FAILED A ASIMAE ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 SW21589MA1060732766 340B172 GEE785130 ORD - FLT 4248 - ON TAKEOFF A LOUD POPPING OR BANGING WAS HEARD FOLLOWED BY A YAWING AND OVERTEMP LIGHT ON RIGHT ENGINE. ENGINE WAS SHUTDOWN. MAINTENANCE REMOVED AND REPLACED POWER PLANT. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T4 TRTA52EU E8NE 19950505001131995050500113EU 1995 5 5 SIMA950871 119950328A324650092361 WHEEL 5010488 SAAB SF340 340B 7860101EU NR 2 MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21329AE1964 233 AUG920810 340B329 MLJ - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN MLI AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 12 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950505001141995050500114EU 1995 5 5 SIMA951021 119950412A2710S2711009100100 BELL CRANK AEROSPATR42 ATR42300 8680920EU RT AILERON CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21262AT 0262 MQT - MAINTENANCE REPORTED THE RIGHT AILERON BELL CRANK JUST OUTBOARD OF FLAP, AFT BEARING CORRODED. THE BELL CRANK WAS REMOVED AND REPLACED AND OPS TEST GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950505001151995050500115EU 1995 5 5 SIMA951022 119950412A2721S2728192900200 CONTROL ROD AEROSPATR42 ATR42300 8680920EU RUDDER TAB CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21262AT 0262 MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE RUDDER TAB CONTROL ROD APPEARED TO BE CORRODED ON INTERNAL ROD. THE ROD WAS REMOVED AND CLEANED OF CORROSION IAW SRM SECTION 51. AFTER ROD INSTALLATION, OPERATIONAL CHECKS OF THE RUDDER TAB WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950505001161995050500116EU 1995 5 5 SIMA951051 119950415A33503011151 EEL BATTERY PACK 3011180 AEROSPATR42 ATR42300 8680920EU CABIN LOW CHARGE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21429MQ280 905 0135 ORD - FLT 4011 - DURING TURN AROUND MEL FOR FLOOR PROXIMITY, FLOOR LIGHT THIRD FROM FRONT INOP WAS WORKED. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK SYSTEM. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950505001171995050500117EU 1995 5 5 USAA950359 119950406A3231 CONTROL ROD FOKKERF28 F28MK0100 4990807EU RT MLG DOOR OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19859US 11293 MCO - FLT 1203 - FLIGHT RETURNED TO MCO DUE TO GEAR DOOR RETRACT PROBLEM. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE CONTROL ROD. OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950505001181995050500118WP 1995 5 5 USAA950361 119950408A3350 EEL DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19966VJ 47420 CLT - THE EMERGENCY LIGHT AT ROW 7 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY FLOOR TRACK LIGHT AT ROW 7. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950505001191995050500119NM 1995 5 5 USAA950363 119950407A2780114T01151 ROD ASSY BOEING767 7672B7 1385107NM LE SLAT FAILED A AUSAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA19655US 25257 CLT - FLT 1175 - FLIGHT DEVELOPED LEADING EDGE SLAT ASYMMETRY PROBELMS AFTER TAKEOFF AND RETURNED TO CLT. A SECOND ATTEMPT WAS MADE TO DEPART CLT AND THE FLIGHT AGAIN EXPERIENCED SLAT ASYMMETRY PROBLEMS. FLIGHT RETURNED TO CLT AGAIN. MAINTENANCE PERFORMED BITE TEST AND RESET THE PROXIMITY SENSOR AFTER THE FIRST RETURN TO FIELD. ALL BITES AND RESETS CHECKED GOOD. AFTER THE SECOND RETURN TO FIELD, MAINTENANCE FOUND THE OUTBOARD LEADING EDGE ACTIVATING ROD ON THE NR 7 SLAT FAILED. THE ROD WAS REPLACED. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED. (W) 2L72 4F RTA1NM 19950505001201995050500120WP 1995 5 5 USAA950365 119950408A3231 CONTROL CABLE DOUG DC9 DC931 3022065WP LT NLG DOOR FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19970VJ 47050 PIT - FLT NR 1206 - UPON GEAR RETRACTION, FLIGHT EXPERIENCED A LOUD NOISE AS THE NOSE GEAR WAS RETRACTED. CREW EXTENDED THE LANDING GEAR AND RETRACTED AGAIN AND RECEIVED AN UNSAFE NOSE GEAR LIGHT. FLIGHT RETURNED TO PIT. MAINTENANCE REPLACED THE LEFT NOSE GEAR DOOR RETRACT CABLE AND HINGE. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950505001221995050500122WP 1995 5 5 USAA950368 119950411A2781H2014B SWITCH DOUG DC9 DC931 3022065WP LT LE FLAPS STICKING A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19960VJ 47505 CLT - FLT 0346 - FLIGHT EXPERIENCED SLAT EXTENSION PROBLEMS. THE FLAPS/SLATS EXTEND LIGHT WOULD NOT STAY ON. FLIGHT RETURNED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT LEADING EDGE ADVISORY SWITCH STICKING. THE SWITCH WAS REPLACED AND THE FLAPS ALL CHECKED NORMAL. (W) 2L72 4F A6WE 19950505001231995050500123WP 1995 5 5 USAA950369 119950412A21335444722 ACTUATOR DOUG DC9 DC931 3022065WP CABIN PRESSURE INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19941VJ 47054 RIC - FLT 0739 - AT FL 350, THE CABIN PRESSURE RED LIGHT AND MASTER WARNING LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO TIC. MAINTENANCE INSTALLED THE OUTFLOW ACTUATOR AND PRESSURE AMPLIFIER. OPERATIONS CHECKED NORMAL. REF CONTROL NR. 95ZZZX2328. (X) 2L72 4F A6WE 19950505001321995050500132NE 1995 5 5 95ZZZX2104 219950412A7200 ENGINE LEAR 25 25D 5170514CE GE CJ610 CJ6106 30006NE LT ENGINE LOST POWER A KKFAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL23900WA8202 4396 25D248 211032 LEFT ENGINE RPM ROLLED BACK TO 40 PERCENT AFTER DEPARTURE. UNEVENTFUL LANDING ACCOMPLISHED. FOD DAMAGE NOTED. ENGINE REPLACED WITH SERVICEABLE UNIT. SUBMITTER RECOMMENDATION: AVOID FOD. SUSPECTED ICE INGESTION, NO FOREIGN MATERIAL WAS FOUND ON TEAR-DOWN. OPER CONTROL NR 4-12-95900WA. 2L72 4J4 J A10CE 1E16 19950505001471995050500147NM 1995 5 5 PCAA9500212 119950328A2422DH103024600CS2B INVERTER DHAV DHC8 DHC8102 2809003NM EE COMPT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA132FOR 6821 1572S8 258 PRIMARY INVERTER CAUTION LIGHT ILLUMINATED AND COCKPIT FILLED WITH SMOKE. REMOVED AND REPLACED PRIMARY INVERTER AND PARALLEL CONTROL BOX. PERFORMED FUNCTION TEST OF INVERTER SYSTEM IAW MM. OPS OKAY. ACFT RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19950505001481995050500148WP 1995 5 5 9506749958 119950418A5350 LOCK DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01917RW 47145 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE LOCK, CHECKED OK. 2L72 4F A6WE 19950505001491995050500149WP 1995 5 5 9506759301 119950418A5350 PIN DOUG DC9 DC982 3022082WP TAILCONE OUT OF POSITION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01301RC 48054 DURING PERIODIC CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP. A PIN HAD BACKED OUT OF THE SPRING CLIPS, ROTATED 90 DEGREES, AND WAS BINDING ON THE SUPPORT BRACKET. RESET PIN, CHECKED OK. 2L72 4F A6WE 19950505001501995050500150WP 1995 5 5 9506769993 119950414A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 965 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE FS 965 BULKHEAD RIGHT SIDE WEB (OUTBOARD LOWER CORNER) AND FITTING (INBOARD LOWER CORNER). REPLACED FITTING AND REPAIRED WEB PER EA 99-092469. 2L72 4F A6WE 19950505001511995050500151WP 1995 5 5 9506779993 119950415A5312 BLKHD ANGLE DOUG DC9 DC931 3022065WP NLG WW CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LOWER BULKHEAD ANGLE, NOSE LANDING GEAR WHEEL WELL LEFT TUNNEL. REPAIRED PER EA 99-094094. 2L72 4F A6WE 19950505001521995050500152WP 1995 5 5 9506789993 119950415A5312 BLKHD FITTING DOUG DC9 DC931 3022065WP FS 690 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON CANTED BULKHEAD 'T' FITTING FS 690, LBL 20. REPAIRED FITTING PER EA 99-094105. 2L72 4F A6WE 19950505001531995050500153WP 1995 5 5 9506799993 119950415A5315 FLOORBEAM DOUG DC9 DC931 3022065WP FS 965 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM FS 965. REPLACED FLOORBEAM PER EA 99-092469. 2L72 4F A6WE 19950505001541995050500154WP 1995 5 5 9506809993 119950415A5313 LONGERON DOUG DC9 DC931 3022065WP FS 347 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30 AT FS 347. REPAIRED PER EA 99-094092. 2L72 4F A6WE 19950505001551995050500155WP 1995 5 5 9506819993 119950416A5320 FITTING DOUG DC9 DC931 3022065WP FS 160 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 23L SPLICE FITTING AT FS 160. REPLACED FITTING PER SRM 53-02 FIG 2. 2L72 4F A6WE 19950505001561995050500156WP 1995 5 5 9506829993 119950416A5320 FITTING DOUG DC9 DC931 3022065WP FS 796-816 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE LONGERON 30 SPLICE FITTING AT FS 796 TO 816. REPLACED FITTING PER SRM 51-00. 2L72 4F A6WE 19950505001571995050500157WP 1995 5 5 9506839993 119950416A5320 FITTINGS DOUG DC9 DC931 3022065WP FS 776 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON BOTH LEFT AND RIGHT KEEL BEAM FITTINGS FS 776. REPLACED FITTINGS PER SRM 51-01. 2L72 4F A6WE 19950505001581995050500158WP 1995 5 5 9506849604 119950417A5230 FITTING DOUG DC9 DC932 3022066WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS AND CORROSION IN THE FORWARD CARGO DOOR FRAME LOWER ATTACH FITTING. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19950505001591995050500159WP 1995 5 5 9506859759 119950418A5230 FITTING DOUG DC9 DC941 302207NWP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING PERIODIC CHECK, FOUND CRACKS IN THE AFT CARGO DOOR BEAM END FITTINGS NR 3 AFT AND NR 4 FORWARD AND AFT. REPLACED FITTINGS PER SRM 51-30-2. 2L72 4F A6WE 19950505001601995050500160WP 1995 5 5 9506869990 119950419A5753 HINGE DOUG DC9 DC931 3022065WP NR 2 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN RIGHT WING FLAP NR 2 FORWARD HINGE FASTENER BORES. REPLACED HINGE PER X9-27-15 AND OHM 27-50-5. 2L72 4F A6WE 19950505001611995050500161WP 1995 5 5 9506879604 119950419A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN JACK PAD TO LONGERON 30 TIE FITTING FS 996. REPLACED TIE FITTING. 2L72 4F A6WE 19950505001621995050500162WP 1995 5 5 9506889886 119950419A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FS 1136 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01600TR 47783 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM FS 1136, LBL 24 LEFT LAV. REPAIRED PER EA 98-96705. 2L72 4F A6WE 19950505001631995050500163WP 1995 5 5 9506899988 119950422A5712 RIB DOUG DC9 DC931 3022065WP RT WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47167 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE RIGHT WING LEADING EDGE NOSE RIBS LOWER ENDS, 3RD, 4TH, AND 6TH RIBS OUTBOARD OF THE NR 10 SLAT TRACK. REPAIRED RIBS PER XEA X9-57-19. 2L72 4F A6WE 19950505001641995050500164WP 1995 5 5 9506909604 119950424A5320 FITTINGS DOUG DC9 DC932 3022066WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 26R, 27R, 28R, AND 29R END FITTINGS FS 604. REPLACED FITTINGS. 2L72 4F A6WE 19950505001651995050500165WP 1995 5 5 9506919762 119950424A5720 FITTING DOUG DC9 DC941 302207NWP TRAP PANEL CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NW 47395 DURING LINE CHECK, FOUND CRACK IN THE RIGHT TRAPEZOIDAL PANEL TO REAR SPAR ATTACH FITTING. REPLACED FITTING PER SRM 51-30-1. 2L72 4F A6WE 19950505001661995050500166WP 1995 5 5 9506929973 119950426A5320 FITTING DOUG DC9 DC931 3022065WP LONGERON 1L CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019337 47346 DURING PREFLIGHT CHECK, FOUND WATER DRIPPING FROM COMMUNICATIONS JACK BOX, FOUND SEALANT MISSING FROM UPPER LAP SEAM AND CORROSION AND CRACK IN LONGERON 1L FORWARD END SHOVEL FITTING. REPLACED SHOVEL FITTING PER SRM 51-30-2 AND RESEALED LAP SEAM. 2L72 4F A6WE 19950505001671995050500167WP 1995 5 5 9506939759 119950426A5343 FITTING DOUG DC9 DC941 302207NWP MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING PERIODIC CHECK, FOUND CORROSION ON FORWARD AND AFT SIDES OF THE MAIN LANDING GEAR FIXED SIDE BRACE ATTACH FITTING LUG. REWORKED LUG PER EA 97-097473. 2L72 4F A6WE 19950505001681995050500168WP 1995 5 5 9506949911 119950426A5320 DOOR FRAME DOUG DC9 DC931 3022065WP RIGHT MLG CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01961N 47405 DURING PERIODIC CHECK, FOUND CRACK IN THE RIGHT MAIN LANDING GEAR DOOR CUTOUT FRAME AT THE MICROSWITCH. REPAIRED FRAME PER EA 99-094843. 2L72 4F A6WE 19950505001691995050500169WP 1995 5 5 9506959977 119950426A5230 FITTING DOUG DC9 DC931 3022065WP FWD CARGO CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019341 47390 DURING PERIODIC CHECK, FOUND ONE INCH CRACK IN FORWARD CARGO DOOR UPPER AFT DOOR STOP SUPPORT FITTING. REPLACED FITTING AND INTERNAL STRAP PER SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950505001701995050500170EU 1995 5 5 9506963231 119950428A2700 COMPUTERS AIRBUS320 A320211 3930320EU FLIGHT CONTROL MALFUNCTIONED A ANWAAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 GL01331NW 318 AT 25,000 FEET DURING CLIMB, THE AIRCRAFT ROLLED RIGHT AND ELAC NR 1 FAULTED. RESET WAS OK, THREE MINUTES LATER THE AIRCRAFT ROLLED AGAIN WITH FAULT DISPLAY SYSTEM INDICATING ELAC NR 2 MALFUNCTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED BOTH SIDE STICK CONTROLLERS AND NR 1 AND NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTERS AND NR 1 AND NR 2 ELEVATOR AILERON COMPUTERS. DURING TEST FLIGHT, ALL SYSTEMS CHECKED NORMAL. 2L72 4F RTA28NM 19950505001711995050500171NM 1995 5 5 9506975530 119950428A2780 CIRCUIT BREAKER BOEING757 757251 1384970NM LE FLAPS TRIPPED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01530US 23845 ON TAKEOFF, THE LEADING EDGE SLAT DISAGREE MESSAGE AND LEADING EDGE LIGHTS ILLUMINATED. DURING FLAP RETRACTION, THE FLAP NEEDLES STOPPED AT FLAPS 1/2 POSITION AND DID NOT COME UP USING THE ALTERNATE PROCEDURES. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. RESET THE POWER CONTROL AND SENSOR CIRCUIT BREAKERS ON NR 1, NR 2, AND NR 3 FLAP/SLAT ELECTRONIC UNITS. NO FAULTS WERE INDICATED, SYSTEM CHECKED NORMAL. 2L72 4F RTA2NM 19950505001721995050500172NE 1995 5 5 9506989851 219950424A7314 FUEL PUMP DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01760NC 47708 696765 AS THROTTLES WERE ADVANCED FOR TAKEOFF, THE NR 2 ENGINE LOW FUEL PRESSURE WARNING STARTED TO FLICKER. THE CREW NOTED AN ENGINE VIBRATION, ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL PUMP ASSEMBLY AND PERFORMED AN ENGINE RUNUP. THE ENGINE CHECKED OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950505001731995050500173NM 1995 5 5 9506992202 119950429A3260 WARNING LIGHT BOEING727 727251 138408HNM LT MLG DOOR ILLUMINATED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01202US 22155 DURING CLIMB UPON LANDING GEAR RETRACITON, THE LEFT GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH PROPER INDICATIONS. MAINTENANCE DEFERRED LEFT GEAR DOOR WARNING INOPERATIVE PER MEL 32-1. 2L73 4F A3WE 19950505001741995050500174NM 1995 5 5 9507002768 119950429A315032EN144 SWITCH BOEING727 7272M7 138407SNM STAB TRIM OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01728RW 21741 DURING APPLICATION OF TAKEOFF THRUST WITH FLAPS 5 AND STABILIZER TRIM AT 2.7, AURAL WARNING HORN SOUNDED, ABORTED TAKEOFF. VERIFIED FLIGHT CONTROL CONFIGURATION, NO DISCREPANCIES NOTED. PERFORMED STATIC RUN AND AURAL WARNING SOUNDED AGAIN, RETURNED TO THE GATE. MAINTENANCE ADJUSTED UPPER STABILIZER TRIM WARNING SWITCH S532. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950505001751995050500175NM 1995 5 5 95UAL747025 119950426A3350 EEL GENERIC BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP294729U 19926 EMERGENCY OVERHEAD LIGHT IS INOPERATIVE AT DOOR 5 LEFT. REPLACED EMERGENCY LIGHT ASSEMBLY AND HARNESS. 2L74 4F4 F A20WE E20EA 19950505001761995050500176NM 1995 5 5 95UAL747026 119950426A5730 TE PANEL 65B116231 BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE LT WING DEPARTED ACFT A UALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 WP294719U 062 19880 CLIMBING THROUGH FLIGHT LEVEL 340, INDICATED AIR SPEED OF 315, FIXED TRAILING EDGE UPPER LEFT WING PANEL DEPARTED AIRCRAFT. REPLACED AND RE-RIGGED PANEL. 2L74 4F4 F A20WE E20EA 19950505001771995050500177NE 1995 5 5 95UAL757011 219950428A72001B362201 FUEL RETURN LINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENGINE CROSS THREADED A UALAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 WP29547UA 25368 726597 EXPERIENCED NR 2 ENGINE FIRE. SECURED ENGINE AND ACTIVATED FIRE EXTINGUISHERS. FOUND THE HPT CASE COOLING VALVE FUEL RETURN LINE CROSS THREADED AT THE 2.5 BLEED VALVE FUEL PRESSURE RETURN LINE. 2L72 4F4 FRTA2NM E17NE 19950505001781995050500178NE 1995 5 5 95UAL767012 219950327A726050R492 CHIP DETECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 ENGINE MISINSTALLED A UALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP29661UA 27158 717695 NR 2 ENGINE SHUTDOWN IN FLIGHT FOR LOW OIL PRESSURE (79-89PSI). ENGINE WINDMILLED APPROXIMATELY 20 TO 30 MINUTES WITH POSITIVE PRESSURE. THE NUMBER THREE CHIP DETECTOR WAS FOUND MISINSTALLED. RE-INSTALLED CHIP DETECTOR AND LEAK CHECKED SYSTEM. 2L72 4F4 FRTA1NM E24NE 19950505001791995050500179EU 1995 5 5 95UALA32002 119950110A3350 EEL AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29405UA 452 CABIN EMERGENCY LIGHT CHECK FAILED TEST. 2L72 4F RTA28NM E40NE 19950505001801995050500180EU 1995 5 5 95UALA32004 119950113A3350 EEL BATTERY GENERIC AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29412UA 465 LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY. 2L72 4F RTA28NM E40NE 19950505001811995050500181WP 1995 5 5 ABXA9500372 119950426A3231 RETRACT MECH DOUG DC8 DC863 302198AWP NLG DOOR MALFUNCTIONED A ABXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL23818AX 46075 AFTER TAKEOFF, A LOUD NOISE WAS HEARD IN THE NOSE AREA. CREW SUSPECTED THE NOSE LANDING GEAR DOOR BEING LEFT OPEN. CYCLED GEAR, NO HELP. A/C RETURNED TO BOS. VERIFIED, FOUND THE LEFT NOSE GEAR DOOR OPEN, RETURNED NOSE GEAR DOOR TO THE UP AND LATCHED POSITION. INSPECTED GEAR, DOOR AND WHEELWELL AREA FOR DAMAGE IAW DC-8 MM CHAPTER 32. SYSTEM OPS CHECKED GOOD ON SUBSEQUENT FLIGHT TO ILN. 2L74 4F 4A25 19950505001821995050500182SO 1995 5 5 COM11872 119950420A323112045381 HOSE ASSY EMB 120 EMB120RT SO LT MLG DOOR LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 SO011105G 120105 GREEN SYSTEM HYDRAULIC FLUID QUANTITY FELL TO ZERO DURING FLIGHT. REPLACED LEAKING DOOR ACTUATOR LINE ON LT MLG. 2L72 4T RTA31SO 19950505001831995050500183SO 1995 5 5 COM11873 119950424A273012031398001 TRIM WHEEL EMB 120 EMB120RT SO COCKPIT LOOSE A COMAK NONE O OTHER UKUNKNOWN 1 SO01257CA8937 120248 ELEVATOR NOSE DOWN TRIM KICKS BACK, NOSE UP TRIM IS OK. TIGHTENED LOOSE TRIM CONTROL WHEEL. 2L72 4T RTA31SO 19950505001841995050500184 1995 5 5 COM11874 419950427A34186225734002 SERVO EMB 120 EMB120RT SO STICK SHAKER DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01164D 13828 120164 AUTOPILOT SERVO APPEARS TO ENGAGE WITH AUTOPILOT OFF. REPLACED THE STICK PUSHER SERVO MOTOR. 2L72 4T RTA31SO 19950505001851995050500185 1995 5 5 COM11875 219950427A7310D10006 FITTING EMB 120 EMB120RT SO RT NACELLE LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01196CA 120196 FUEL LEAKING FROM RT MLG WHEELWELL AREA. REPAIRED PERMASWAGE FITTING ON MOTIVE FLOW LINE IN RT NACELLE. 2L72 4T RTA31SO 19950505001861995050500186SW 1995 5 5 COM20364 119950428A3230MS243314 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG DAMAGED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01704C AC704 LANDING GEAR DID NOT RETRACT. REPLACED DAMAGED LT MLG WEIGHT ON WHEELS SWITCH. 1L72 4T A8SW 19950505001871995050500187SW 1995 5 5 COM20365 119950427A291027810322642 HYD LINE SWRNGNSA227 SA227AC 8780603SW COCKPIT LEAKING A COMAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO01457AM AC694 WHEN LANDING GEAR EXTENDED, HYDRAULIC PRESSURE FELL TO ZERO. REPLACED LEAKING HYDRAULIC LINE UNDER COCKPIT FLOOR. 1L72 4T A8SW 19950505001881995050500188SW 1995 5 5 COM20366 119950414A26122789000183 FIRE CONTROL SWRNGNSA227 SA227AC 8780603SW INST PANEL LOOSE A COMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO01458AM AC699 LEFT ENGINE FIRE WARNING ACTIVATED, DURING TAXI AFTER LANDING. REPAIRED LOOSE FIRE CONTROL ASSY ON INSTRUMENT PANEL. 1L72 4T A8SW 19950505001891995050500189NE 1995 5 5 COM31066 219950429A72006053T88G01 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT FAILED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01356CA195064743 340A034 367222 RT ENGINE OIL BYPASS WARNING LIGHT AND CHIP DETECTOR WARNING INFLIGHT. REPLACED ENGINE. 2L72 4T4 TRTA52EU E8NE6 19950505001901995050500190 1995 5 5 DHL95726001 419950427A3442MI585161 RT UNIT BOEING727 727228 NM FWD FUS FAILED A TDHLAO OTHER O OTHER CRCRUISE 1 SO01726DH 20409 WEATHER RADAR FLASHED AND SCREEN WENT BLANK. RESET CIRCUIT BREAKERS, RADAR FLASHED AND WENT BLANK AGAIN. REMOVED AND REPLACED WEATHER RADAR. OPS CHECK GOOD, PER MM 34-40. 2L73 4F A3WE 19950505001911995050500191WP 1995 5 5 MWEA95187 119950428A5240 DOOR DOUG DC9 DC932 3022066WP E/E COMP NOT SECURED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31401ME 47133 PILOT REPORTS, AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO GATE. MAINTENANCE FOUND E AND E COMPARTMENT DOOR NOT PROPERLY SECURED. SECURED DOOR, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A6WE 19950505001921995050500192NM 1995 5 5 UPS203123 119950428A3230 RETRACT MECH BOEING727 72727C 138400JNM NLG LACK OF LUBE A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01914UP 19246 PILOT REPORTED, THAT ON INITIAL GEAR EXTENSION NOSE GEAR UNLOCKED, BUT DID NOT LOCK DOWN, HAD RED UNLOCK LIGHT AND NO GREEN LIGHT. CYCLED GEAR AND NOSE GEAR GREEN LIGHT ILLUMINATED. PERFORMED OPS CK OF GEAR INDICATION PER MM 32-61-01. CHECKED WIRING FOR NOSE GEAR PER WOM 32-64-01, 32-64-02. LUBED NOSE GEAR PER MM 12-21-11, ALSO PERFORMED MANUAL EXTENSION OF NOSE GEAR. ALL CK GOOD, NO DEFECTS, OK FOR SERVICE. 2L73 4F A3WE 19950505001931995050500193WP 1995 5 5 UPS803124 119950427A3260 SWITCH DOUG DC8 DC871F 302199DWP LT MLG DOOR INTERMITTENT A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01703UP 45939 PILOT REPORTED THAT AT 230 KNOTS ON CLIMBOUT, GOT A FLICKERING THEN STEADY DOOR NOT LATCHED LIGHT. COMPLIED WITH QRH CHECKLIST. LIGHT WENT OUT AFTER GEAR WAS CYCLED. FOUND LT UPLATCH SWITCH INTERMITTENT. REPLACED DOOR SWITCH PER MM 32-31-04. 2L74 4F RT4A25 19950505001941995050500194WP 1995 5 5 UPS803125 119950428A3230 UPLATCH MECH DOUG DC8 DC871F 302199DWP LT/RT MLG OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01703UP 45939 PILOT REPORTED THAT AFTER TAKE OFF GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR AND LIGHT EXTINGUISHED. ADJUSTED UPLATCH CLEARANCE PER MM 32-31-04, TEST GOOD. 2L74 4F RT4A25 19950505001951995050500195WP 1995 5 5 UPS803126 119950501A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE INNER DOUBLER AND SKIN AT FS 1350, LONGERONS 26 TO 27L. REPAIRED PER SRM 51-1-8, 53-2-1. 2L74 4F RT4A25 19950505001961995050500196WP 1995 5 5 UPS803127 119950501A53204646163501N FITTING DOUG DC8 DC871F 302199DWP FS 1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF LONGERON 25L SPLICE FITTING AT FS 1350. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950505001971995050500197WP 1995 5 5 UPS803128 119950501A53305615378509 SKIN DOUG DC8 DC871F 302199DWP FS 1148 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN AT FS 1148, LONGERON 33R AND FS 1280 TO 1300, LONGERONS 34 TO 35L. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-5330-2827D. 2L74 4F RT4A25 19950505001981995050500198WP 1995 5 5 UPS803129 119950501A53204646945N DOUBLER DOUG DC8 DC871F 302199DWP FS 70-80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON JACK PAD INNER DOUBLER AT FS 70 TO 80, LONGERON 34L TO 34R. REPLACED DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950505001991995050500199WP 1995 5 5 UPS803130 119950501A5532 SKIN DOUG DC8 DC871F 302199DWP VERTICAL STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON 4 MOUNTING HOLES OF VERTICAL STABILIZER ANTENNA ON STABILIZER SKIN. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950505002001995050500200WP 1995 5 5 UPS803131 119950501A5730 DOUBLER DOUG DC8 DC871F 302199DWP WS 373 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT STA XFS 373, RT WING LEADING EDGE LOWER SIDE. FABRICATED AND INSTALLED REPAIR PER UPS EO DC8-57-0546. 2L74 4F RT4A25 19950505002011995050500201WP 1995 5 5 UPS803132 119950501A5730 SKIN DOUG DC8 DC873F 302199FWP WS 307 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AT LOWER SURFACE SKIN OF RT WING STA XFS 307. REPAIRED SKIN PER SRM 57-2-1, 51-1-8, 57-2-0. 2L74 4F RT4A25 19950505003361995050500336 1995 5 5 95ZZZW588 319950410A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE RT PROPELLER MISSING A AJJBAO OTHER O OTHER TXTAXI/GRND HDL 1 EA01854CA361 UE60 DE-ICE BOOT UNBONDED FROM ONE BLADE ON RIGHT PROPELLER. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL 361 HOURS AGO AT WHICH TIME BOOT WAS INSTALLED. SUBMITTER STATES UPON INSPECTION OF BOOT AREA ITS APPARENT THAT THE PAINT APPLIED TO THE BLADE PRIOR TO BOOT APPLICATION UNBONDED WITH BOOT END COULD BE THE CAUSE. 2L72 4T RTA24CE 19950505003371995050500337CE 1995 5 5 95ZZZW589 119950331A7931AN8184D NUT AN9374 BEECH 99 C99 1154006CE LT ENGINE LOOSE A GPPAEA ENGINE SHUTDOWN UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 CE09113GP U211 FLT NR 2014 40 MILES OUTBOUND OF MCI, SHUTDOWN THE LEFT ENGINE WHEN THE FLIGHT CREW NOTICED A 40 PSI DROP IN OIL PRESSURE WITH AN ASSOCIATED WARNING ANNUNCIATOR ILLUMINATION. AIRCRAFT RETURNED SAFELY TO MCI. MCI MAINTENANCE FOUND THE 'B' NUT TO THE OIL PRESSURE SWITCH AND TRANSMITTER 'T' LOOSE. 'B' NUT WAS TIGHTENED AND A GROUND RUN WAS PERFORMED WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 3T A14CE 19950505003381995050500338WP 1995 5 5 95ZZZW590 119950413A3310BA1701 TRANSFORMER DOUG DC9 DC932 3022066WP COCKPIT FAILED A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11915VV 47443 FLT NR 523 - ATL-MCO - BURNED SMELL IN COCKPIT, SMELL DISSIPATED AND DID NOT RETURN. REPLACED BALLAST TRANSFORMER, P/N NR BA1701. 2L72 4F A6WE 19950505003391995050500339NM 1995 5 5 95ZZZW591 119950412A2130 PRESSURIZATION BOEING707 707330C 138367GNM CABIN MALFUNCTIONED A CLCAA UNSCHED LANDING O OTHER CLCLIMB 1 SO19707HE 20124 FLT 088 - IN FLIGHT PRESSURIZATION PROBLEM, RETURNED TO LIMA. REPOSITIONED LEFT A/C CABIN COND AIR VALVE AND FOLLOWED PRESSURIZATION PROCEDURES AND OPS CHECK GOOD, PER MM 21-58-01. 2L74 4F 4A26 19950505003401995050500340NM 1995 5 5 95ZZZW592 119950413A21331033741 VALVE BOEING707 707330C 138367GNM CABIN OUTFLOW FAILED A CLCAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19707HE 20124 FLT NR 049 - UNABLE TO CONTROL CABIN PRESSURIZATION. UNABLE TO CLOSE FORWARD OUTFLOW VALVE, RETURNED TO MIA. REMOVED, REPAIRED AND REINSTALLED FORWARD OUTFLOW VALVE PER MM 21-1-31. OPS CHECK NORMAL. 2L74 4F 4A26 19950505003411995050500341WP 1995 5 5 95ZZZW594 119950224A5320 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05985Z 47491 STL - DURING C-CHECK, FOUND CORROSION ON AFT CARGO BIN LOWER DOOR JAMB INNER PANEL, FROM FORWARD LOWER CORNER TO AFT SIDE. REPAIRED PER SRM 53-05, FIGURE 14. 2L72 4F A6WE 19950505003421995050500342WP 1995 5 5 95ZZZW595 119950223A5313 LONGERON DOUG DC9 DC931 3022065WP FS 446 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05990Z 47136 STL - DURING SPECIAL CHECK, FOUND CRACKS 1.75 INCHES LONG ON BOTH SIDES OF SPLICE, LONGERON 30, STATION 446. REPAIRED PER SRM 53-02, FIGURE 14, SHEETS 1 AND 2, AND STANDARD PRACTICES. 2L72 4F A6WE 19950505003431995050500343NM 1995 5 5 95ZZZW596 119950223A5313 STRINGER BOEING727 727231 1384079NM FS 990 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0584357 21989 MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990. REPAIRED PER ARA 9054. 2L73 4F A3WE 19950505003441995050500344NM 1995 5 5 95ZZZW597 119950306A5320 DECK BOEING727 727231 1384079NM FS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0552311 19830 MCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940. STOP DRILLED CRACK AND REPAIRED PER ARA 9117A. 2L73 4F A3WE 19950505003451995050500345NM 1995 5 5 95ZZZW598 119950410A2612895398 FIRE LOOP BOEING747 747131 1384881NM NR 1 ENGINE MALFUNCTIONED A TWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 CE0553116 20321 MADE UNSCHEDULED LANDING ACCOUNT NR 1 ENGINE 'A' FIREWARNING ILLUMINATED. SHUT DOWN ENGINE AND DISCHARGED EXTINGUISHER BOTTLES. 'B' LOOP PREVIOUSLY PLACARDED ON MEL. RESTORED 'B' LOOP BY REPLACEMENT OF LOWER AFT WARNING LOOP, MFG P/N 895398. REPLACED EXPENDED BOTTLES AND PLACARDED 'A' LOOP PER MEL. OPS CHECKS NORMAL. 2L74 4F A20WE 19950505003461995050500346NM 1995 5 5 95ZZZW599 119950223A5313 STRINGER BOEING727 727231 1384079NM FS 1000 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0584357 21989 MCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000. REPAIRED PER ARA 9054. 2L73 4F A3WE 19950505003471995050500347NM 1995 5 5 95ZZZW600 119950310A5313 STRINGER BOEING727 727231 1384079NM FS 656.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0552311 19830 MCI - DURING C-CHECK, FOUND A ONE INCH LONG CRACK IN STRINGER 16, STATION 656.5. REPAIRED PER SRM 57-20-201, FIGURE 207. 2L73 4F A3WE 19950505003481995050500348NM 1995 5 5 95ZZZW601 119950310A5311 FRAME BOEING727 727231 1384079NM FS 783.95 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0552311 19830 MCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN FUSELAGE FRAME, FS 783.95. REPAIRED PER SERVICE BULLETIN 727-53-0197, DRAWING NR 65C36280 AND EMLR 65639. 2L73 4F A3WE 19950505003491995050500349NM 1995 5 5 95ZZZW602 119950311A5711 SPAR BOEING747 747131 1384881NM WS 675.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0593107 19673 FCO - DURING PERIODIC SERVICE CHECK, FOUND A NINE INCH CRACK IN RIGHT WING FRONT WING FRONT SPAR AT FSSI 675.5. REPAIRED CRACK PER BOEING REPAIR DRAWING 691U0103 AND TWA ARA 9122. 2L74 4F A20WE 19950505003501995050500350WP 1995 5 5 95ZZZW603 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2. 2L72 4F A6WE 19950505003511995050500351WP 1995 5 5 95ZZZW604 119950411A5313 LONGERON DOUG DC9 DC951 3022051WP FS 832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 4L, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2. 2L72 4F A6WE 19950505003521995050500352WP 1995 5 5 95ZZZW605 119950412A5313 LONGERON DOUG DC9 DC931 3022065WP FS 1000 GOUGED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05980Z 47344 STL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STATION 1000. REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02. 2L72 4F A6WE 19950505003531995050500353WP 1995 5 5 95ZZZW606 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 734 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3R, STATION 734. REPAIRED PER SRM 53-02, FIGURE 2. 2L72 4F A6WE 19950505003541995050500354WP 1995 5 5 95ZZZW607 119950411A5313 LONGERON DOUG DC9 DC951 3022051WP FS 794/832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3L, STATION 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2. 2L72 4F A6WE 19950505003551995050500355NM 1995 5 5 95ZZZW608 119950419A323053173 PIN BOEING727 727231 1384079NM NLG MISSING A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0552312 19831 STL - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION. ACCOMPLISHED LANDING GEAR HANDLE LOCK CHECKLIST AND RETRACTED LANDING GEAR. FOUND NOSE LANDING GEAR TORQUE LINK PIN MISSING, MFG P/N 53173. INSTALLED NEW NOSE GEAR TORQUE LINK PIN. LANDING GEAR CHECKS NORMAL. 2L73 4F A3WE 19950505003561995050500356WP 1995 5 5 95ZZZW609 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 794 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2. 2L72 4F A6WE 19950505003571995050500357WP 1995 5 5 95ZZZW610 119950413A30402726129802 CONTROLLER LKHEED1011 1011385115 5265015WP R2 WINDHSHIELD FAILED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531031 193B1115 SJU - DURING CRUISE, WINDSHIELD HEAT WIRE HARNESS SHORTED AT R-2 WINDOW CAUSING ARCING AND SMOKE IN COCKPIT. TURNED OFF WINDSHIELD HEAT AND DISCHARGED HAND EXTINGUISHER. REPLACED WINDSHIELD WIRING HARNESS AND WINDSHIELD HEAT CONTROLLER, MFG P/N 27261298-02. WINDSHIELD HEAT OPERATION CHECKED NORMAL. 2L73 4F A23WE 19950505003581995050500358NM 1995 5 5 95ZZZW611 119950417A261260B00023163 DETECTOR BOEING747 747131 1384881NM NR 1 ENGINE FAILED A TWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE. THEN NR 1 ENGINE FIREWARNING SOUNDED. SHUTDOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES. FOUND BOTH DETECTORS SHORTED. REPLACED BOTH DETECTORS, MFG P/N 60B00023163 AND P/N 60B00023166. PERFORMED POWER RUNUP AND NACELLE DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL. 2L74 4F A20WE 19950505003591995050500359NM 1995 5 5 95ZZZW612 119950417A261260B00023166 DETECTOR BOEING747 747131 1384881NM NR 1 ENGINE FAILED A TWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE. THEN NR 1 ENGINE FIREWARNING SOUNDED. SHUTDOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES. FOUND BOTH DETECTORS SHORTED. REPLACED BOTH DETECTORS, MFG P/N 60B00023163 AND P/N 60B00023166. PERFORMED POWER RUNUP AND NACELLE DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL. 2L74 4F A20WE 19950505003601995050500360NM 1995 5 5 95ZZZW613 119950317A5311 FRAME BOEING727 727231 1384079NM FS 783.95 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554329 20307 MCI - DURING C-CHECK, FOUND TWO INCH CRACK IN INBOARD AFT SIDE OF FRAME, BELOW FLOOR LEVEL, FS 783.95. STOP DRILLED CRACK AND INSTALLED REPAIR PER EMLR 65661. 2L73 4F A3WE 19950505003611995050500361NM 1995 5 5 95ZZZW614 119950317A5320 DECK BOEING727 727231 1384079NM FS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554329 20307 MCI - DURING C-CHECK, FOUND .5 INCH CRACK IN PRESSURE DECK EIGHT INCHES INBOARD OF 940 CASTING. STOP DRILLED AND INSTALLED DOUBLER PER ARA 9130. 2L73 4F A3WE 19950505003621995050500362NM 1995 5 5 95ZZZW615 119950320A5330 SKIN BOEING727 727231 1384079NM FS 250 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554329 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 250, LOWER AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132. 2L73 4F A3WE 19950505003631995050500363NM 1995 5 5 95ZZZW616 119950320A5330 SKIN BOEING727 727231 1384079NM FS 252 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554329 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 252, AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132. 2L73 4F A3WE 19950505003641995050500364NM 1995 5 5 95ZZZW617 119950320A5330 SKIN BOEING727 727231 1384079NM FS 249 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554329 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STA 249, AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACKED AND INSTALLED DOUBLER PER ARA 9132. 2L73 4F A3WE 19950505003651995050500365WP 1995 5 5 IXXA199559 119950408A2410698870 CSD DOUG DC8 DC862 3021970WP NR 3 ENGINE FAILED A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23735PL 3818 46153 ON DEPARTURE OUT OF NZAA, THE NR 3 CSD OIL LIGHT ILLUMINATED ACCOMPANIED BY LOSS OF VOLTAGE AND FREQUENCY. THE AIRCRAFT RETURNED TO NZAA FOR MAINTENANCE. MAINTENANCE DEFERRED THE NR 3 CSD. THE AIRCRAFT RETURNED TO SERVICE, AND THE NR 3 CSD WAS SCHEDULED FOR REPLACEMENT. 2L74 4F 4A25 19950505003661995050500366WP 1995 5 5 IXXA9550 119950327A5712 RIB DOUG DC8 DC871 302199AWP RT WING CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND AT XRS-6 RIB. THE RIB WAS REPAIRED IAW DRAWING HSE27-57-169, WHICH WAS FAA DER APPROVED, AND EO 57-DC8-151. (W) 2L74 4F 4A25 19950505003671995050500367WP 1995 5 5 IXXA9551 119950324A57309803949502 PLATING DOUG DC8 DC871 302199AWP WS 453 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT WING LEADING EDGE, STUB WING, PLATING AT XRS 453. UPON DOUGLAS EVALUATION AND FAA DER APPROVAL THE CRACK WAS SUBJECTED TO ADDITONAL INSPECTION. INSPECTION RESULTS FOUND NO ADDITIONAL DAMAGE, AND THE AIRCRAFT WAS RETURNED TO SERVICE. PERMANENT REPAIR MUST BE AT THE NEXT C-CHECK. (W) 2L74 4F 4A25 19950505003681995050500368WP 1995 5 5 IXXA9552 119950315A5730561238519 PANEL DOUG DC8 DC871 302199AWP WS 441.5 CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE LEFT WING LOWER PLATING. THE CRACK MEASURED 1.75 INCHES AND WAS LOCATED AT XW 441.5, BETWEEN STRINGERS 63 AND 64. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE CRACK, ADDING A FILLER, AND INSTALLING BOTH A DOUBLER AND TRIPLER ON THE INTERNAL AND EXTERNAL SIDES OF THE PLATING. REPAIR ACCOMPLISHED IAW DOUG ROD SKETCH 94-07-11-009, WHICH IS FAA DER APPROVED AND EO 57-DC8-153. (W) 2L74 4F 4A25 19950505003691995050500369WP 1995 5 5 IXXA9553 119950315A53112641520 FRAME DOUG DC8 DC871 302199AWP BS 1397 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS NOTED AT THE BELTFRAME AT FUSELAGE STATION 1397, BETWEEN LONGERONS 34 LEFT AND RIGHT. THE LOCALIZED CORROSION WAS REMOVED BY CUT OUT, MANUFACTURE OF A NEW SECTION, ADDING A SPLICE CHANNEL, AND INSTALLING AN ORIGINAL SPLICE PLATE. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-171, WHICH IS FAA DER APPROVED AND EO 53-DC8-154. (W) 2L74 4F 4A25 19950505003701995050500370WP 1995 5 5 IXXA9554 119950315A533027796551 PANEL DOUG DC8 DC871 302199AWP FS 560-610 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, LEVEL 2 CORROSION WAS FOUND AT FUSELAGE STATION 560-610. THIS AREA HAD A PREVIOUS REPAIR AND THE CORROSION FOUND IS ATTRIBUTED TO NOT REMOVING ALL CORROSION AT THAT TIME. REPAIR OF THE AREA REQUIRED TWO CUTOUTS OF BOTH THE INTERNAL DOUBLER AND PLATING, ADDING FILLERS AND INSTALLING BOTH A REPAIR DOUBLER AND TRIPLER. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-167, WHICH IS FAA DER APPROVED AND EO 53-DC8-155. (W) 2L74 4F 4A25 19950505003711995050500371WP 1995 5 5 IXXA9555 119950315A53112750825 FRAME DOUG DC8 DC871 302199AWP BS 520 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND AT STATION 520, BETWEEN LONGERONS 33 AND 35 RIGHT. THE SECTION OF BELTFRAME WAS REMOVED MANUFACTURED AND REPLACED. REPAIR ACCOMPLISHED IAW DRAWING HSE27-53-163, WHICH IS FAA DER APPROVED AND EO 53-DC8-156. (W) 2L74 4F 4A25 19950505003721995050500372WP 1995 5 5 IXXA9556 119950316A5330 SKIN DOUG DC8 DC871 302199AWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS BLENDED BEYOND SRM LIMITS. THE EXTERIOR PLATING AT STATION 530-550 BETWEEN LONGERONS 33 RT AND 36. DAMAGE WAS REMOVED BY CUTOUT, ADDING A FILLER AND EXTERNAL DOUBLER. REPAIR ACCOMPLISHED IAW DRAWING HSE27-53-168, WHICH IS FAA DER APPROVED AND EO 53-DC8-157. (W) 2L74 4F 4A25 19950505003731995050500373WP 1995 5 5 IXXA9557 119950315A533027796551 PANEL DOUG DC8 DC871 302199AWP FUSELAGE CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING C-CHECK ROUTINE INSPECTION, FOUND LOADER DAMAGE AT THE FORWARD BASKET DOOR CUTOUT. THE FUSELAGE PLATING WAS ROUTED OUT AND AN EXTERNAL DOUBLER ADDED. REPAIR WAS ACCOMPLISHED IAW DRAWING HSE27-53-166, WHICH IS FAA DER APPROVED AND EO 53-DC8-158. (W) 2L74 4F 4A25 19950505003741995050500374WP 1995 5 5 IXXA9558 119950315A52307075T6 FITTING DOUG DC8 DC871 302199AWP CARGO DOOR CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23826BX7349514070 45998 DURING ROUTINE C-CHECK INSPECTION, AN AFT LOWER CARGO DOOR STOP FITTING WAS FOUND CRACKED. THE FITTING WAS MANUFACTURED IAW DRAWING HSE27-53-165, WHICH WAS FAA DER APPROVED AND EO 53-DC8-160. FITTING WAS INSTALLED IAW THE AIRCRAFT MM. (W) 2L74 4F 4A25 19950505004311995050500431NM 1995 5 5 9507012703 119950430A5241 FRAME BOEING727 727225 1384077NM AFT GALLEY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018878Z 21451 DURING PERIODIC CHECK AND SCHEDULED REMOVAL OF AFT LEFT GALLEY SERVICE DOOR, SHOP MAINTENANCE FOUND FORWARD FRAME CRACKED AT UPPER HINGE CUTOUT, LENGTH .5 INCH. REPAIRED PER NWA EA 27-096522 (MFG PART NUMBER 65-56992-3). 2L73 4F A3WE 19950505004321995050500432NM 1995 5 5 9507022703 119950430A5313 LONGERON BOEING727 727225 1384077NM FS 980-1015 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018878Z 21451 DURING PERIODIC CHECK, MAINTENANCE FOUND FUSELAGE BELLY SKIN AND SURROUNDING STRUCTURE STR 29R, FS 980 TO 1015 CORRODED AND CRACKED. REPAIRED PER NWA EA 27-096533 (MFG PART NUMBER 65C1391-1). 2L73 4F A3WE 19950505004331995050500433WP 1995 5 5 9507039878 119950420A26128920809040002 CONTROL UNIT DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01787NC 48149 688206 ON TAKEOFF ROLL, THE NR 2 ENGINE 'A' LOOP FIRE WARNING ILLUMINATED. THE TAKEOFF WAS ABORTED BELOW 30 KNOTS. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 FIRE DETECTION CONTROL UNIT. THE SYSTEM TESTED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950505004341995050500434WP 1995 5 5 ABXA9500373 119950429A3260 DOOR LIGHT DOUG DC9 DC931 3022065WP RT MLG DOOR ILLUMINATED A ABXAO OTHER J WARNING INDICATION LDLANDING 1 GL23942AX 47552 UPON GEAR RETRACTION, RED UNSAFE LIGHT FOR RIGHT MAIN ILLUMINATED. DURING UPLATCH CHECK, GEAR DOOR OPEN LIGHT CAME ON ALSO. AFTER PLACING GEAR HANDLE TO UP, RED UNSAFE LIGHT FOR RIGHT MAIN AND GEAR DOOR OPEN LIGHT EXTINGUISHED. CONTINUED FLIGHT WITH RIGHT HYDRAULIC PUMP ON HIGH. CYCLED GEAR AND DOORS IAW DC-9 MM CHAPTER 32-30-0, OPS CHECKED GOOD. 2L72 4F A6WE 19950505004351995050500435WP 1995 5 5 ABXA9500374 119950426A5312591013013 DOUBLER DOUG DC9 DC933F 302207AWP AFT PRESS BLKHD CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING COMPLIANCE OF AD 85-01-02, SB 53-137, FOUND LEFT UPPER CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR DOUBLER CRACKED IN RADIUS. REPAIRED IAW DC-9 SB 53-137, SERVICE REWORK DRAWING SR0J060088 AND ABX REA D953-11481-SB. 2L72 4F A6WE 19950505004361995050500436NE 1995 5 5 ABXA9500375 219950428A7200JT3D7 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 3 FAILED A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23811AX3385 46113 6697517 EN ROUTE TO FLL, CREW SHUTDOWN NR 1 ENGINE AS PRECAUTIONARY DUE TO LOW OIL PRESSURE INDICATION, LIGHT, AND HIGH OIL TEMPERATURE INDICATION. VERIFIED ENGINE FAILURE, LOSS OF OIL OUT TAIL PIPE AND METAL IN THE FILTER SCREEN. INSPECTED AND PREPARED AIRCRAFT FOR THREE ENGINE FERRY TO ILN. REPLACED THE NR 3 ENGINE, SYSTEMS OPS CHECKED GOOD IAW DC 8 MM. 2L74 4F4 F 4A25 1E8 19950505004371995050500437WP 1995 5 5 ABXA9500376 119950427A323177330 EYEBOLT DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD EYEBOLT HAD EXCESSIVE PLAY. REPLACED EYEBOLT, ADJUSTED AND FAIRED DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950505004381995050500438WP 1995 5 5 ABXA9500377 119950501A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 9100 47427 EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 MM CHAPTER 33, OPS CHECKED GOOD. 2L72 4F A6WE 19950505004391995050500439SO 1995 5 5 COM11876 119950429A3610744257C2 COUPLER EMB 120 EMB120RT SO RT ACM BROKEN A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01152CA 120152 RT DUCT LEAK WARNING DURING TAXI. REPLACED BROKEN CLAMP ON RT ACM. 2L72 4T RTA31SO 19950505004401995050500440SO 1995 5 5 COM11877 119950430A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01152CA14340 120152 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPORT 1327-2 P/N: 120-17056-019, 2 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 1 EA; 120-17057-006, 1 EA; 120-17057-007, 2 EA; 120-17056-007, 3 EA; 120-17057-005, 1 EA. 2L72 4T RTA31SO 19950505004411995050500441SO 1995 5 5 COM11878 119950424A760312029840002 POWER LEVER EMB 1200865500 EMB 120 EMB120RT SO FLIGHT COMPT WORN A COMAK NONE O OTHER ININSP/MAINT 1 SO01255CA9936 120238 CREW REPORTED, THAT POWER LEVERS WERE NOT EVEN AT FLIGHT IDLE STOP. THE RT POWER LEVER FLIGHT IDLE STOP PIN AND ROLLER WERE FOUND TO BE WORN OVER 50 PERCENT. THE RT POWER LEVER ASSY WAS REPLACED. 2L72 4T RTA31SO 19950505004421995050500442 1995 5 5 COM20367 419950430A34215040017921 ATTITUDE GYRO SWRNGNSA227 SA227AC 8780603SW INST PANEL DEFECTIVE A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01702M 12449978 AC702 COPILOTS ATTITUDE INDICATOR CIRCUIT BREAKER TRIPPED, WILL NOT RESET. REPLACED COPILOTS ATTITUDE INDICATOR. 1L72 4T A8SW 19950505004431995050500443EU 1995 5 5 COM31067 119950501A61201103P0620 PRESSURE SWITCH SAAB SF340 SF340A 7850100EU LT/RT NACELLE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01357CA3961 864 340A044 AUTO COARSEN FAIL WARNING DURING TAKEOFF. REPLACED THE P3 ARMING SWITCHES. 2L72 4T RTA52EU 19950505004441995050500444EA 1995 5 5 COM60462 119950501A276054C54677E01 CONTROL VALVE CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01936CA2059 7043 INBD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE GROUND SPOILERS CONTROL VALVE. 2L72 4F RTA21EA 19950505004451995050500445NM 1995 5 5 DHL95740001 119950429A292669171354 RESERVOIR BOEING727 7272Q9 138448MNM LEFT FAILED A TDHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01740DH 21930 ON CLIMB, LOST STANDBY HYDRAULIC QUANITY. ALL OTHER PRESSURES AND QUANITIES OK. REMOVED AND REPLACED STANDBY HYDRAULIC RESERVOIR AND LEFT WING TAI DUCT. 2L73 4F RTA3WE 19950505004461995050500446NM 1995 5 5 DL72E951714 119950421A321165192962 FWD TRUNNION BOEING727 727247 138408FNM RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 000043 RT/MLG FWD TRUNNION ATTACH FITTING HAS CORROSION IN UPPER AND LOWER BOLT HOLES. REPAIRED PER M/M 57-43-0 PAGE 803 FOUND ON CV-3 TRIPLE GEAR CHANGE. 2L73 4F A3WE 19950505004471995050500447NM 1995 5 5 DL72E951715 119950419A321165192962 TRUNNION FITTING BOEING727 727247 138408FNM RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 000043 R/MLG FWD TRUNNION ATTACH FITTING. CORROSION OTBD FITTING UPPER AND LWD BOLT HOLES. REPAIRED PER M/M 32-43-0. FOUND ON CV-3 TRIPLE GEAR CHANGE. 2L73 4F A3WE 19950505004481995050500448NM 1995 5 5 DL72E951716 119950419A321165192961 TRUNNION FITTING BOEING727 727247 138408FNM LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 000043 LT MLG FWD TRUNNION ATTACH FITTING. LT LOWER BUSHING HAS CORROSION. LOWER RT BUSHING HAS CORROSION. REPAIRED PER M/M 57-43-0 PG 804. 2L73 4F A3WE 19950505004491995050500449NM 1995 5 5 DL72E951717 119950419A321165192962 TRUNNION FITTING BOEING727 727247 138408FNM RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 000043 RT MLG FWD ATTACH FITTING LT/UPPER/LOWER BUSHINGS CORRODED. REPAIRED PER ERA 301600-14. FOUND ON CV-3, TRIPLE GEAR CHANGE. 2L73 4F A3WE 19950505004501995050500450NM 1995 5 5 DL72K951836 119950430A3340900835A EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11415DA 21257 DURING LAYOVER, R-2 DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19950505004511995050500451NM 1995 5 5 DL72L951660 119950418A5347 SEAT TRACK BOEING727 727232 1384082NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CORROSION ON L/T INBD SEAT TRACK JUST AFT OF STA 344. REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19950505004521995050500452NM 1995 5 5 DL72L951661 119950418A5347 SEAT TRACK BOEING727 727232 1384082NM FS 340 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CORROSION ON L/T OUTBD SEAT TRACK JUST AFT OF STA 344. REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19950505004531995050500453NM 1995 5 5 DL72L951662 119950418A5320 CLIP BOEING727 727232 1384082NM FS 1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CORROSION AT SKIN CLIP STA 1030 BETWEEN S29R AND 28R. REPAIRED PER M/M 53-11-0 AND IDENT PR 8.7 900-5-1 FIG 4. 2L73 4F A3WE 19950505004541995050500454NM 1995 5 5 DL72L951663 119950419A5320 CLIP BOEING727 727232 1384082NM FS 500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CORROSION ON AFT SIDE OF FORMER AT STATION 500, JUST INBD OF 27R. REPAIRED AS PER M/M 53-11-0 AND CHECKED LIMIT PER SRM 53-10-1. 2L73 4F A3WE 19950505004551995050500455NM 1995 5 5 DL72L951664 119950419A5320 CLIP BOEING727 727232 1384082NM FS 500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CORROSION ON SKIN CLIP AT STA 500 BETWEEN STR 28R AND 27R. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950505004561995050500456NM 1995 5 5 DL72L951665 119950419A5320 FORMER BOEING727 727232 1384082NM FS 480 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, 1 INCH CRACK ON STATION 480 FORMER ABOVE STRINGER 27L. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950505004571995050500457NM 1995 5 5 DL72L951702 119950417A5400 STIFFENER BOEING727 727232 1384082NM FS 1400 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 FOUND ON CV2 CHECK, CRACK IN STIFFENER STA 1400 OVERHEAD OF NR 2 ENGINE COMPARTMENT SECTION. REPAIRED PER SRM 54-10-3 AND IDENTIFIED PER PS 900-5-1 FIG 4. 2L73 4F A3WE 19950505004581995050500458NM 1995 5 5 DL72S951622 119950420A5753652163262 FITTING BOEING727 727232 1384082NM NR 2 TE FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 O/B CARRIAGE FITTING FOR ALL FOUR THRUST BEARING RETAINER BOLT HOLES HAVE CORROSION, NR 2 MID FLAP. FOUND AT SHOP INSPECTION, REAMED HOLES TO .312 TEATED AND INSTALLED BUSHING. 2L73 4F A3WE 19950505004591995050500459NM 1995 5 5 DL72S951623 119950420A5753 FITTING 652163262 BOEING727 727232 1384082NM NR 3 TE FLAP CORROISON A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA BN7 21061 NR 3 MID FLAP O/B CARRIAGE FITTING LOWER SURFACE HAS CORROSION IN ONE HOLE. FOUND AT SHOP INSPECTION, REAMED HOLE TO .312 TREATED AND INSTALLED BUSHING. 2L73 4F A3WE 19950505004601995050500460NM 1995 5 5 DL72S951625 119950420A5753 HOUSING 652163262 BOEING727 727232 1384082NM NR 3 TE FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA BN7 21061 NR 3 MID FLAP O/B CARRIAGE SUPPORT HOUSING LOWER SURFACE, TWO FASTENER HOLES CORRODED. REAMED HOLES TO .312 TREATED AND INSTALLED BUSHING. 2L73 4F A3WE 19950505004611995050500461NM 1995 5 5 DL72S951626 119950420A5753 ANGLE 652163262 BOEING727 727232 1384082NM NR 3 TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA BN7 21061 NR 3 MID FLAP AFT SPAR LOWER ANGLE DENTED APPROX 59 INCHES FROM I/B END. INSTALLED DOUBLER AND SPAR PER MM 57-52-0. 2L73 4F A3WE 19950505004621995050500462NM 1995 5 5 DL72S951679 119950322A711065196854540 NOSE COWL BOEING727 727232 1384082NM NR 3 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 0 OUTER FRAME AND BULKHEAD DAMAGED UNDER TEMP. REPAIR AT 3 O'CLOCK POSITION. DAMAGE WAS REPAIRED PER B-727 SRM 54-10-3 FIG 3 FOR NR 3 ENGINE NOSE COWL, DURING SHOP INSPECTION. 2L73 4F A3WE 19950505004631995050500463NM 1995 5 5 DL72S951690 119950412A5531 SPAR BOEING727 727232 1384082NM RT VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND VERTICAL STAB RT FRONT SPAR HAS CRACK STOP DRILLED. MANF, REPAIR DOUBLER, REMOVED DAMAGE, AND INSTALLED PER SRM 55-30-3. 2L73 4F A3WE 19950505004641995050500464NM 1995 5 5 DL72S951691 119950408A5522 SKIN BOEING727 727232 1384082NM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND UNIDENTIFIED REPAIR ON TOP SKIN OF RT ELEV BETWEEN NR 5 AND NR 6 HINGE. INSTALLED PERMANENT REPAIR PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950505004651995050500465NM 1995 5 5 DL72S951692 119950411A5754 FRAME BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND NR 3 L/E SLAT OB FRAME CRACKED. REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950505004661995050500466NM 1995 5 5 DL72S951694 119950411A5754 FRAME BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND NR 3 L/E SLAT NR 7 FRAME CRACKED INSIDE L/E. REPAIRED PER M/M 57-54-0 FIG 814. 2L73 4F A3WE 19950505004671995050500467NM 1995 5 5 DL72S951695 119950411A5754 FRAME BOEING727 727232 1384082NM NR 2 FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND NR 2 SLAT O/B END 2ND FRAME FROM END CRACKED. REPAIRED PER M/M 57-54-0 FIG 814. 2L73 4F A3WE 19950505004681995050500468NM 1995 5 5 DL72S951696 119950421A5320 CHANNEL BOEING727 727232 1384082NM ACCESS DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND J-CHANNEL CORRODED BEHIND T-CHORD AT HINGES FOR DOOR 3348. INSTALLED NEW DOUBLER AND NEW ANGLE PER SRM 51-40-3. 2L73 4F A3WE 19950505004691995050500469NM 1995 5 5 DL72S951697 119950409A5245 HINGES BOEING727 727232 1384082NM AC DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, FOUND HEAVY CORROSION BEHIND HINGES FOR ACCESS DOOR 3348L AC BAY. INSTALLED NEW REPAIR AND SPLICE PER M/M 53-30-1. 2L73 4F A3WE 19950505004701995050500470NM 1995 5 5 DL72W951666 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 AT HMV, STRINGER 27L WAS FOUND CORRODED JUST AFT OF FS 700. REMOVED CORROSION PER SRM 51-10-6. REMOVED SECTION OF STRINGER AND REPAIRED PER SRM 53-10-2. 2L73 4F A3WE 19950505004711995050500471NM 1995 5 5 DL72W951667 119950330A5313 STRINGER BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 AT HMV, FOUND STRINGER 28R WITH CORROSION DAMAGE AT FS 700. FABRICATED STRINGER SPLICE REPAIR PER SRM. INSTALLED REPAIR PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950505004721995050500472NM 1995 5 5 DL72W951668 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 AT HMV, FOUND STRINGER 28L WITH CORROSION DAMAGE AT FS 700. REMOVED SECTION OF STRINGER FROM STA 680 TO 720 AND INTERCOSTAL FROM 700 TO 720. FABRICATED REPAIR AS PER SRM 53-10-3. INSTALLED STRINGER, REPAIR, AND INTERCOSTAL. 2L73 4F A3WE 19950505004731995050500473NM 1995 5 5 DL72W951669 119950331A5313 STRINGER BOEING727 727247 138408FNM FS 640 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 AT HMV, FOUND STRINGER 26R CORRODED AFT OF FS 640. INSTALLED REPAIR AS PER ERA 301574-14. 2L73 4F A3WE 19950505004741995050500474NM 1995 5 5 DL72W951670 119950330A5315 FLOORBEAM BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 STA 700 FRAME CORRODED ON TOP IB OF RT FIXED FLOOR AND STA 700 FRAME CRACKED/BENT ON TOP IB OF LT FIXED FLOOR AT Z ANGLE ATTACH. REPAIRED PER SRM 53-10-1 PG 1. 2L73 4F A3WE 19950505004751995050500475NM 1995 5 5 DL72W951671 119950331A5312 BLKHD ANGLE BOEING727 727247 138408FNM FS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 STA 740 SKIN TO BULKHEAD CLOSEOUT ANGLE CORRODED BETWEEN STR 28R AND 27R. DAMAGE FOUND AND REPAIRED AT HMV. REPAIRED PER SRM 53-11-0 FIG 826, TREATED AND PAINTED. 2L73 4F A3WE 19950505004761995050500476NM 1995 5 5 DL733951675 119950424A7110314A101015 NOSE COWL BOEING737 737347 1384647NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO113301 23181 DURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL WAS FOUND WITH THE LEADING EDGE LIP DENTED AT THE 9 O'CLOCK POSITION. REPAIRED PER SRM 54-10-01. 2L72 4F RTA16WE 19950505004771995050500477NM 1995 5 5 DL733951709 119950424A5522 SKIN BOEING737 737347 1384647NM LT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313WA 23599 000043 FOUND DURING LETTER CHECK INSP, SMALL HOLE IN L/T ELEV, APPROX 24 INCHES FROM O/B END. REPAIRED PER SRM 51-70-05, WEIGHT ADDED IN REPAIR NEGLIGIBLE REBALANCE NOT REQUIRED PER SRM 51-60-04. 2L72 4F RTA16WE 19950505004781995050500478NM 1995 5 5 DL757951642 119950419A5330 SKIN BOEING757 757232 1384965NM FS 940-950 LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11629DL 22919 FOUND DURING LETTER CHECK, LIGHTNING STRIKE AT 12 O'CLOCK AT STA 940 TO 950 AND L2-L3 STRINGERS. INSTALLED BLIND FLUSH HEAD RIVET AT STATION 940, APPROX 14 INCHES LT SIDE OF CENTERLINE IAW SRM 53-00-01. EDDY CURRENT INSP, C/W FLUSH TEMP OVERSIZE FASTENER INSTALLED. RE-INSPECT AT 2,500 FLT CYCS 53-00-01D PG 221. 2L72 4F RTA2NM 19950505004791995050500479NM 1995 5 5 DL757951643 119950419A5330 SKIN BOEING757 757232 1384965NM FS 1040 LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11629DL 22919 FOUND DURING LETTER CHECK, LIGHTNING STRIKES AT TOP OF CROWN AT STA 1040. INSTALLED BLIND FLUSH HEAD RIVET AT STA 1020 AND STA 1060 APPROX 14 INCHES RT OF CENTERLINE PER SRM 53-00-01 PG 221. EDDY CURRENT INSP C/W TEMP AT 2,500 FLT CYCS 53-00-01. 2L72 4F RTA2NM 19950505004801995050500480NM 1995 5 5 DL757951680 119950417A5315 FLOORBEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 AT HMV, CORROSION WAS FOUND ON FLOORBEAM BL0 TO RT FUSELAGE SKIN STA 324. REMOVED CORR AND CK LIMITS PER SRM 53-10-8 FIG 101. DRILLED REPAIR SPLICE ANGLES PER SRM 53-10-8 AND INSTALLED PER SAME. 2L72 4F RTA2NM 19950505004811995050500481NM 1995 5 5 DL757951681 119950419A5751 WEIGHT BOEING757 757232 1384965NM RT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 AT HMV, THE LWR L/E AT THE O/B END OF THE I/B WEIGHT ON THE RT AILERON WAS FOUND CRACKED. THIS WAS REPAIRED PER SRM 57-60-01. 2L72 4F RTA2NM 19950505004821995050500482NM 1995 5 5 DL757951682 119950413A5414 SKIN BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 716311 AT HMV, PERM REPAIR OF NR 2 ENG NACELLE STRUT SKIN I/B WAS SCHEDULED. THE DAMAGE WAS ROUTED OUT, INSP FOR CRACKS (NONE DETECTED), AND DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED PER SRM 54-51-01. 2L72 4F4 FRTA2NM E17NE 19950505004831995050500483NM 1995 5 5 DL76L951703 119950215A7110314T401010A NOSE COWL BOEING767 767332 1382001NM NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11179DN 25144 225 DURING SHOP VISIT, A 2 INCH BY 6 INCH HOLE AT THE 6 O'CLOCK POSITION WAS REPAIRED PER SRM 54-13-01, FOR NR 1 ENGINE NOSE COWL. 2L72 4F RTA1NM 19950505004841995050500484NM 1995 5 5 DL76P951837 119950430A2530811150417 COFFEE MAKER BOEING767 767332 1382001NM FWD GALLEY FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11140LL 25988 DURING CRUISE, FORWARD GALLEY COFFEE MAKER STARTED TO POP AND EMIT SMOKE AND ELECTRICAL BURNING ODOR. SHUTOFF POWER, ODOR QUICKLY STOPPED. FOUND BURNED WIRES ON NR 2 COFFEE MAKER. REPLACED UNIT, OPERATION NORMAL. 2L72 4F RTA1NM 19950505004851995050500485WP 1995 5 5 DLL10951644 119950421A5330 SKIN LKHEED1011 10113851 5265010WP FS 769 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 AT LAYOVER, FUSELAGE SKIN AT FS 769, 2 INCHES LEFT OF CENTERLINE AT BOTTOM, WAS FOUND TO BE CRACKED. REPAIRED SKIN PER SRM 53-31-00 PG 824 FIG 813. 2L73 4F A23WE 19950505004861995050500486WP 1995 5 5 DLL10951672 119950412A5711 SPAR CAP LKHEED1011 10113851 5265010WP FS 1163 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 FS 1163 UPPER T-CAP IN DRY BAY IS CRACKED ON RT SIDE OF A/C ANGLE WAS REPAIRED BY THE SRM 57-11-00 FIGURE 809. FOUND AT HMV. 2L73 4F A23WE 19950505004871995050500487WP 1995 5 5 DLL10951674 119950424A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11714DA 193C1090 DURING SPECIAL INSPECTION, THE FOLLOWING MAIN FUSELAGE FRAMES WERE FOUND CRACKED, RT SIDE FS 509, 609, 669, 1023, 1043, 1063, 1103, 1163, 1685, 1705. LEFT SIDE FS 509, 1023, 1043, 1083, 1303, 1645, 1685, 1705, 1725. ALL CRACKS WERE AT WL 280. THESE CRACKS WERE FOUND AS A RESULT OF A SPECIAL INSPECTION FOR THIS AREA. ALL CRACKS WERE REPAIRED PER DL ERA 270741-14. 2L73 4F A23WE 19950505004881995050500488WP 1995 5 5 DLL10951686 119950425A5312 ANGLE LKHEED1011 10113851 5265010WP PRESS DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 AFT P-DOME CIRCUMFERENTIAL ATTACH ANGLE IS CORRODED AT STRINGER 27 AND 32. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 801 AND SRM 53-11-00 FIG 848. 2L73 4F A23WE 19950505004891995050500489WP 1995 5 5 DLL10951687 119950425A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 559 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 TEAR STRAP DISBONDED AT FS 559 STRINGER 25 TO 27, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 806-807. 2L73 4F A23WE 19950505004901995050500490WP 1995 5 5 DLL10951688 119950425A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 703 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 FAIL SAFE STRAP DISBONDED AFT OF FS 703, BETWEEN STRINGER 37 TO 38. FOUND DURING CORROSION INSP AT HMV. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950505004911995050500491WP 1995 5 5 DLL10951689 119950425A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 579 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 TEAR STRAP DISBONDED IN C1 FS 579 STRINGER 26, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950505004921995050500492WP 1995 5 5 DLL10951711 119950425A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP FS 846 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 FAILSAFE STRAP DISBONDED FS 846 BETWEEN STRINGER 31 TO 30. FOUND DURING CORROSION INSP AT HMV TASK NR C-53-130-05. CLEANED CORROSION PER SRM 53-31-00 FIG 801, INSTALLED REPAIR PER 53-31-00 FIG 804. 2L73 4F A23WE 19950505004931995050500493WP 1995 5 5 DLL13951652 119950422A7830RB21122B02 TR ANGLE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL52339 193A1121 010575 T/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802. UNDERLYING BULKHEAD REPAIR SPLICE ANGLE DAMAGE PER RB-211-22B ENGINE MANUAL 78-32-07 FIG 78-32-07-990-012. 2L73 4F4 F A23WE E12EU 19950505004941995050500494WP 1995 5 5 DLL13951653 119950422A5753 VANE LKHEED1011 10113851 5265010WP NR 2 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 NR 2 LT FLAP VANE, UPPER SKIN CRACKED. REPAIRED PER SRM 57-53-00 FIG 806, FOUND AT LETTER CHECK. 2L73 4F A23WE 19950505004951995050500495WP 1995 5 5 DLL13951673 119950419A5330 SKIN LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 SKIN CRACKED AT HINGE CUTOUT FWD OF ACS GROUND SERVICE DOOR. REPAIRED PER SRM 53-31-00 FIG 828. 2L73 4F A23WE 19950505004961995050500496WP 1995 5 5 DLL17951659 119950330A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 1792 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 AT HMV, FOUND FS 1792 CABIN FLOORBEAM CORRODED ATL LBL 55. REPAIRED PER SRM 53-21-00 PG 865-868. 2L73 4F A23WE 19950505004971995050500497NM 1995 5 5 DLM88951712 119950424A5330 SKIN DOUG MD88 MD88 3023688NM NLG DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11981DL 53268 000043 LT NOSE W/W DOOR AFT HINGE CUTOUT, .25 INCH CRACK IN FUSE SKIN. FOUND AT D-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950505004981995050500498NM 1995 5 5 DLM88951713 119950424A5330 SKIN DOUG MD88 MD88 3023688NM NLG W/W CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11981DL 53268 000043 R/T NOSE W/W DOOR HINGE AFT HINGE CUTOUT, .75 INCH CRACK FUSE SKIN. FOUND AT D-2 LTR CK. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950505004991995050500499NM 1995 5 5 DLM88951823 119950427A323139567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR WORN A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11938DL 49811 AFTER TAKOFF AND GEAR RETRACTION, HAD LOUD WIND NOISE FROM NOSE WHEELWELL AREA. NO OTHER ABNORMAL INDICATIONS WERE NOTED, RETURNED TO COS. FOUND LEFT NOSE GEAR DOOR OPEN, FOUND WORN DOOR LINK. REPLACED LINK, OPERATION NORMAL. 2L72 4F RTA6WE 19950505005001995050500500WP 1995 5 5 MWEA95188 119950502A3350 EEL BULB DOUG DC9 DC914 3022034WP CABIN FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31600ME 45725 DURING ROUTINE INSPECTION, THE FWD ENTRANCE EMERGENCY FLASHLIGHT WAS FOUND INOP. MAINTENANCE REPLACED LIGHT BULB OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950505005011995050500501NM 1995 5 5 QXEA950130 119950429A33506038441 EEL PWR SUPPLY DHAV DHAV DHC8 DHC8102 2809003NM CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09817PH 56 SEA - THE TWO FORWARD RED FLOOR PROXIMITY LIGHT ARE INO. REPLACED POWER SUPPLY AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950505005021995050500502WP 1995 5 5 SCNA95066 119950427A2611PU499R3 SMOKE DETECTOR DOUG DC10 DC1015 3022118WP NR 3 LAV FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15152SY 48289 NUMBER 3 LAVATORY SMOKE DETECTOR FOUND TO BE INOPERATIVE. REPAIRED BROKEN WIRE LEADING TO SMOKE DETECTOR, SYSTEM CHECKED GOOD. 2L73 4F A22WE 19950505005031995050500503WP 1995 5 5 SCNA95067 119950427A2560119821001 INDICATOR DOUG DC10 DC1015 3022118WP R4 DOOR SLIDE FAULTY A SCNAK NONE O OTHER ININSP/MAINT 1 GL15152SY 48289 THE R-4 DOOR SLIDE WOULD NOT TEST, FOUND BROKEN WIRE AT TEST LIGHT SOCKET. REPAIRED WIRE AND SLIDE TESTED GOOD. 2L73 4F A22WE 19950505005041995050500504NM 1995 5 5 SWAA950314 119950427A5330 SKIN BOEING737 7373Q8 1384670NM FS 380-440 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN FROM BS 380 TO 440, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505005051995050500505NM 1995 5 5 SWAA950315 119950427A5330 SKIN BOEING737 7373Q8 1384670NM BS 952 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 952, 6 INCHES BELOW S17L. REPAIRED PER TRAMCO EWO 95-0031. 2L72 4F RTA16WE 19950505005061995050500506NM 1995 5 5 SWAA950316 119950427A5242 SKIN BOEING737 7373Q8 1384670NM E/E DOOR DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND E AND E DOOR, LT FWD AND AFT O/B CORNERS DENTED AND GOUGED. INSTALLED NEW SKIN PER BOEING SRM. 2L72 4F RTA16WE 19950505005071995050500507NM 1995 5 5 SWAA950317 119950427A5320 SILL BOEING737 7373Q8 1384670NM FS 942-986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND AFT ENTRY DOORWAY LOWER MOP SILL CORRODED FROM BS 942 TO 986.5, WL 208, LBL 60. REPLACED PER BOEING SRM. 2L72 4F RTA16WE 19950505005081995050500508NM 1995 5 5 SWAA950318 119950427A5312 BLKHD WEB BOEING737 7373Q8 1384670NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED MAINT CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178, LBL 57 AND WL 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950505005091995050500509NM 1995 5 5 SWAA950319 119950501A335020131A EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07307SW 22947 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRYWAY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND HOUSING PER BOEING M/M. 2L72 4F RTA16WE 19950505005101995050500510NM 1995 5 5 SWAA950320 119950430A335062AT343 EEL SWITCH BOEING737 7373H4 1384600NM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07347SW 24374 DURING SCHEDULED SERVICE CHECK, FOUND AFT FLIGHT ATTENDANT PANEL EMERGENCY LIGHT SWITCH INOP. REPLACED SWITCH PER BOEING M/M. 2L72 4F RTA16WE 19950505005111995050500511NM 1995 5 5 SWAA950321 119950430A33506128251 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950505005121995050500512NM 1995 5 5 SWAA950322 119950430A33506042221 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07354SW 25219 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950505005131995050500513NM 1995 5 5 SWAA950323 119950430A33506104791 EEL BATTERY BOEING737 7372H4 138448CNM RT OVERWING DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0762SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK AND POWER SUPPLY PER BOEING M/M. 2L72 4F A16WE 19950505005141995050500514NM 1995 5 5 SWAA950324 119950430A3350 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07675AA 23253 AT GATE, FOUND AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950505005151995050500515NM 1995 5 5 SWAA950325 119950425A5711 SPAR WEB BOEING737 7372H4 138448CNM BS 616 PUNCTURED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0768SW 22357 DURING SCHEDULED C2 CHECK, FOUND SPAR WEB PUNCTURED AT BS 616, 4 INCHES FROM BOTTOM NEXT TO O/B SIDE OF O/B AUX TRACK OF NUMBER 1 SLAT. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19950505005161995050500516NM 1995 5 5 SWAA950326 119950425A5320 WEB BOEING737 7372T4 1384492NM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED C3 CHECK, FOUND WEB CRACKED AT FLOOR LEVEL FWD OF BELT FRAME AT BS 639. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19950505005171995050500517NM 1995 5 5 SWAA950327 119950426A5230 FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07357SW 26594 DURING SCHEDULED C4 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED ON INNER RADIUS OF FWD SIDE, JUST UNDER LOCK HOOK ASSY. REPAIRED PER SWA RA 1-A52-198. 2L72 4F RTA16WE 19950505005221995050500522CE 1995 5 5 95ZZZX2179 119950411A2140414183957 RESISTOR BEECH 18 E18S 1151006CE HEATER OPEN A VLLAK NONE O OTHER ININSP/MAINT 1 GL058627A BA283 THREE OHM, 10 WATT RESISTOR IN OVERHEAT CIRCUIT FOR HEATER WAS FOUND 'OPEN'. 1L72 3R A765 19950505005231995050500523CE 1995 5 5 95ZZZX2180 119950411A2140NAS44135 FUSE 414183957 BEECH 18 E18S 1151006CE HEATER WRONG PART A VLLAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL058711H BA87 INCORRECT FUSE WAS FOUND INSTALLED IN HEATER OVERHEAT CIRCUIT. 1L72 3R A765 19950505005371995050500537SO 1995 5 5 95ZZZX2194 219950401A8520SA646277LQ LIFTER CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 2 CYL EXH MISMFG APAFAHAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 SO1964PB 402C0528 242951R ZERO TIME ENGINE AFTER OVERHAUL WAS INSTALLED ON THIS AIRCRAFT AND ON FIRST REVENUE FLIGHT AFTER TEST FLIGHT, THE ENGINE BEGAN RUNNING ROUGH AND LOSING OIL PRESSURE. THE AIRCRAFT LANDED AND UPON INSPECTION OF ENGINE, THE NR 2 CYLINDER EXHAUST PUSH-ROD WAS FOUND BENT AND THE HOUSING TORN OPEN. UPON FURTHER INSPECTION, LIFTERS WERE REMOVED AND EXHAUST LIFTER WAS APPROXIMATELY .25 INCH SHORTER THAN MANUFACTURED SIZE. IT WAS DETERMINED THE LIFTER WAS MANUFACTURED IMPROPERLY AND THERE MAY BE MORE OUT IN THE INDUSTRY. 1L72 3O3 O A7CE E8CE 19950505005381995050500538WP 1995 5 5 95ZZZZ225 119950411A3230 RETRACT MECH DOUG DC8 DC873F 302199FWP LANDING GEAR MALFUNCTIONED A DHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01804DH 46124 ON APPROACH TO LANDING, GEAR DID NOT EXTEND WHEN GEAR LEVER PLACED IN DOWN POSITION, RECYCLED, WORKED NORMALLY. JACKED ACFT, PERFORMED 3 GEAR SWINGS, SEVERAL CYCLES. INSPECTED GEAR, NO DEFECTS NOTED. ALL GEAR SWINGS SUCCESSFUL. COULD NOT DUPLICATE. ALL WORK IAW 32-30. 2L74 4F RT4A25 19950505005391995050500539NM 1995 5 5 95ZZZZ226 119950411A27301864 BULB BOEING727 7272Q9 138448MNM ELEV FEEL SYST SHORTED A DHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01741DH 21931 DURING CRUISE, ELEVATOR DIFFERENTIAL PRESSURE LIGHT ON INERMITTENTLY FOR SEVERAL MINUTES. FOUND ELEVATOR FEEL LIGHT BULB SHORTING. NO OTHER DEFECTS NOTED. 2L73 4F RTA3WE 19950505005401995050500540 1995 5 5 95ZZZZ227 419950316A22107003180901 SERVO COMPUTER BEECH 1900 1900 1154160CE RUDDER CONTROL MALFUNCTIONED AL PLGAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NE05806BE UB41 BOS - AFTER T/O THE ACFT EXPERIENCED RUDDER CONTROL PROBLEMS. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, LANDING WITHOUT INCIDENT. MX INSPECTION WAS PERFORMED WITH NO DEFECTS NOTED. ALL FLIGHT CONTROLS WERE CHECKED, NO DEFECTS WERE FOUND. BOTH ENGINE TRUSSES INSPECTED AND BOTH TORQUE AND ITT SYSTEMS WERE CHECKED WITH NO FAULTS FOUND. RUNS PERFORMED ON ENGINES WITH NO DEFECTS, THE GYRO FOR THE YAW DAMP SYSTEM WAS REPLACED. THE TEST FLIGHT CREW REPORTED THAT THE ACFT STILL TENDED TO ROLL. THE YAW DAMP COMPUTER AND SERVO WERE REPLACED, NO DEFECTS NOTED. THE YAW DAMP COMPUTER AND SERVO WERE SENT FOR INVESTIGATION. REF PLGA316951. 2L72 4T RTA24CE 19950505005411995050500541NM 1995 5 5 AWXA9500215 119950412A2761S251N1116 ACTUATOR BOEING757 757225 1384959NM NR 8 SPOILER LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP28913AW 22207 EWR-PHX - FLT 68 - TWENTY MINUTES FROM PHX THE E1 HYD PUMP LOW PRESSURE LIGHT ILLUMINATED, AND DURING FINAL APPROACH THE HYD QUANTITY DECREASED TO BELOW MINIMUM. AFTER LANDING NOSE WHEEL STEERING WAS NOT AVAILABLE AND A/C WAS TOWED TO GATE. MAINTENANCE FOUND NR 8 SPOILER PCA LEAKING. REMOVED AND REPLACED SPOILER ACTUATOR PER BMM 27-61-02. OPS CHECK OK. ACFT RELEASED FOR SERVICE. (Z) 2L72 4F RTA2NM 19950505005421995050500542NM 1995 5 5 AWXA9500216 119950411A335020131A EEL BATT PACK BOEING737 7373S3 1384711NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHCEK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE ROWS 7 THROUGH 13. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950505005431995050500543NM 1995 5 5 AWXA9500217 119950411A3350 EEL ASSY BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND MID CABIN FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. RESECURED LIGHTS, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950505005441995050500544EU 1995 5 5 AWXA9500218 119950412A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU GALLEY DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN FWD GALLEY, OPS CHECK NORMAL. 2L72 4F RTA28NM 19950505005451995050500545NM 1995 5 5 AWXA9500219 119950413A33501614 EEL LAMP BOEING757 7572G7 1384963NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28908AW 24233 DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP, OPS CHECK GOOD. (Z) 2L72 4F RTA2NM 19950505005461995050500546NM 1995 5 5 AWXA9500220 119950416A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS IN AFT SECTION INOPERATIVE. REPAIRED WIRING, SYSTEM OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950505005471995050500547NM 1995 5 5 AWXA9500221 119950416A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 9 THROUGH 11 AND FIRST CLASS. REPAIRED LIGHTS AT ROWS 9 THROUGH 11, AND RECONNECTED WIRES IN FIRST CLASS SECTION. OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950505005481995050500548NM 1995 5 5 AWXA9500222 119950417A5511 RIB BOEING737 737275 1384485NM LT HORIZ STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND LT HORIZONTAL STABILIZER LE RIB 4TH AND 9TH FROM I/B END CRACKED. INSTALLED DOUBLER REPAIR PER SRM 51-40-3. (Z) 2L72 4F A16WE 19950505005491995050500549NM 1995 5 5 AWXA9500223 119950417A5320 ANGLE BOEING737 737275 1384485NM BS 294 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND FWD ENTRY DOOR INTERCOSTAL SUPPORT ANGLE BETWEEN STA 294 STR 10L AND 11L CRACKED. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-30-2. (Z) 2L72 4F A16WE 19950505005501995050500550NM 1995 5 5 AWXA9500224 119950417A5511 RIB BOEING737 737275 1384485NM RT HORIZ STAB CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND RT HORIZONTAL STABILIZER LE RIB 3RD, 4TH AND 9TH FROM I/B END CRACKED. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-3. (Z) 2L72 4F A16WE 19950505005511995050500551NM 1995 5 5 AWXA9500225 119950417A5320 SUPPORT BOEING737 737275 1384485NM BS 987 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND CORROSION BEYOND LIMITS ON LT LAV DOOR THRESHOLD SUPPORT, STA 987 TO 1006. FABRICATED NEW SUPPORT INTERCOSTAL PER SRM 51-10-1. (Z) 2L72 4F A16WE 19950505005521995050500552NM 1995 5 5 AWXA9500226 119950417A5320 ANGLE BOEING737 737275 1384485NM BS 987 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND LT LAV FWD WALL SUPPORT ANGLE CORRODED BEYOND CLEAN UP LIMITS. FABRICATED AND INSTALLED NEW SUPPORT ANGLE PER SRM 51-30-2. (Z) 2L72 4F A16WE 19950505005531995050500553NM 1995 5 5 AWXA9500227 119950417A5311 FRAME BOEING737 737275 1384485NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND STA 639 STR 17L FRAME WEB CRACKED. REPAIRED WITH DOUBLER REPAIR PER SRM 51 40 2 AND SRM 51 30 2. (Z) 2L72 4F A16WE 19950505005541995050500554NM 1995 5 5 AWXA9500228 119950417A5311 FRAME BOEING737 737275 1384485NM FS 597 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND STA 597 STR 17R FRAME CRACKED. INSTALLED REPAIR FILLER AND ANGLE PER ER 2 53 34 06. (Z) 2L72 4F A16WE 19950505005551995050500555NM 1995 5 5 AWXA9500229 119950417A5315 FLOORBEAM BOEING737 737275 1384485NM FS 597 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND FLOORBEAM CRACKED, STA 400 STR 27. SPLICED IN NEW REPAIR SECTION PER SRM 51-40-4. (Z) 2L72 4F A16WE 19950505005561995050500556NM 1995 5 5 AWXA9500230 119950417A5330 SKIN BOEING737 737275 1384485NM FS 747 DISBOND A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20922 PHX - DURING C6 INSPECTION, FOUND DELAMINATION IN WINDOW BELT AREA, STA 747 RT AND LT AND STA 847 RT. LOCATED AND REPAIRED PER EO 53-30-14. (Z) 2L72 4F A16WE 19950505005571995050500557EU 1995 5 5 AWXA9500231 119950416A3242ML215264 BRAKE ASSY AIRBUS320 A320231 3930325EU NR 3 BRAKE FAILED A AAWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP28621AW 053 STL - FLT 1406 - CREW REPORTED THAT TOWER NOTICED SPARKS FROM RT SIDE OF ACFT ON LANDING ROLL. ALL ENGINES, BRAKES AND LANDING NORMAL. ACFT TAXIED TO GATE WITHOUT FURTHER PROBLEMS. CONTRACT MAINTENANCE FOUND NR 3 BRAKE HAD COME A PART. REMOVED AND REPLACED NR 3 BRAKE ASSEMBLY. ACFT RETURNED TO SERVICE. (Z) 2L72 4F RTA28NM 19950505005581995050500558NM 1995 5 5 AWXA9500235 119950417A335011028337 EEL ASSY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28180AW 22647 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY, OPS CHECK NORMAL. (Z) 2L72 4F RTA16WE 19950505005591995050500559NM 1995 5 5 AWXA9500236 119950417A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LAST 7 ROWS OF FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE. SPLICED WIRES, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950505005601995050500560 1995 5 5 PLGA316951 419950502A22107002260903 SERVO BEECH 1900 1900 1154160CE YAW DAMPER MALFUNCTIONED A PLGAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NE05806BE 85040899 UB41 AIRCRAFT HAD RUDDER CONTROL PROBLEMS. THE YAW DAMP COMPUTER AND SERVO WERE BOTH SENT OUT FOR REPAIR AND TESTING. THE COMPUTER WAS RETURNED FROM REPAIR WITH NO FAULT FOUND. THE SERVO WAS RETURNED FROM REPAIR WITH BEARINGS AND DRIVE TRAIN CLEANED AND GREASED. (M) 2L72 4T RTA24CE 19950505005611995050500561EU 1995 5 5 PLGA46951 119950406A5347 SEAT TRACK SAAB SF340 340B 7860101EU FS 630.112 CORRODED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05354BE 340B246 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A PRE-EXTISTNG SEAT TRACK REPAIR AT FS 630.112. CORRODED REPAIR PATCH WAS REMOVED AND REPLACED WITH A NEW PATCH IAW SAAB SRM CHAPTER 53-70-60. (Z) 2L72 4T RTA52EU 19950505005621995050500562CE 1995 5 5 PLGA49951 119950409A53201144301167 INTERCOSTAL BEECH 1900 1900 1154160CE FS 498 CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05805BE UB38 DURING 21,000 HOUR STRUCTURAL INSPECTION, FOUND INTERCOSTAL AT FS 498, TO HAVE A .75 INCH CRACK EMANATING FROM OUTER FLANGE. REPLACED INTERCOSTAL WITH NEW PART IAW BEECHCRAFT STRUCTURAL REPAIR MANUAL. (W) 2L72 4T RTA24CE 19950505005631995050500563EU 1995 5 5 RAIA950407 119950406A7712 TQ TEMP LIMITER BAG JETSTMJETSTM3201 1500217EU RT ENGINE INOP A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03864AE 864 MRY - FLT 4716 - LOW POWER ON RIGHT ENGINE. MAINTENANCE DEFERRED RIGHT TORQUE TEMP LIMITER PER MEL 76-2, CATEGORY C. GROUND RUNS OK. (M) 2L72 4T RTA56EU 19950505005641995050500564SO 1995 5 5 RAIA950420 119950412A6120MS3456W10SL4S CONNECTOR EMB 120 EMB120RT SO RT ENG DIRTY A RAIAO OTHER O OTHER CLCLIMB 1 CE03125AM 120017 STL - FLT 7459 - NO CONTROL OVER RT RPM BETWEEN 83 PERCENT TO 90 PERCENT. MAINTENANCE CLEANED OIL RESIDUE FROM RT PROPELLER CONTROL UNIT CANNON PLUG. GROUND RUNS REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA31SO 19950505005651995050500565EU 1995 5 5 RAIA950422 119950416A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU LT ENG FAILED A RAIADO RETURN TO BLOCK OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 CE03431AM 881 STL - FLT 7442 - LEFT ENGINE VIBRATION. MAINTENANCE REPLACED LEFT ENGINE STARTER GENERATOR. GROUND RUNS REVEALED NORMAL OPERATION. NO FURTHER VIBRATION NOTED. (Z) 2L72 4T RTA56EU 19950505005661995050500566SO 1995 5 5 RAIA950423 119950416A5610NP1513112 WINDSHIELD EMB 120 EMB120RT SO RIGHT CRACKED A RAIAO OTHER C F.O.D. CLCLIMB 1 CE03125AM 120017 STL - FLT 7219 - LIGHTNING STRIKE TO THE FRONT OF WINDSHIELD, WINDSHIELD CRACKED. MAINTENANCE REPLACED RT FRONT WINDSHIELD. LIGHTNING INSPECTION REVEALED NO FURTHER DAMAGE. 2L72 4T RTA31SO 19950505005671995050500567 1995 5 5 RAIA950425 419950417A341606306206 ALTIMETER BAG JETSTMJETSTM3201 1500217EU LT COCKPIT FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03427AM 876 STL - FLT 7304 - CAPTAIN'S ALTIMETER FAILED AFTER TAKEOFF AND SO DID THE ENCODING ALTIMETER. MAINTENANCE REPLACED CAPTAIN'S ALTMETER. LEAK CHCK AND ENCODING CHECK GOOD. (Z) 2L72 4T RTA56EU 19950505005681995050500568EU 1995 5 5 UF6A950406 119950412A2430SX7EK6 CONTRACTOR BAG ATP ATP EU NR 1 FAILED A UF6AO OTHER O OTHER CRCRUISE 1 CE03860AW 2037 ORD - FLT 5092 - THE NR 1 TRANSFORMER RECTIFIER UNIT FELL OFF LINE. MAINTNANCE REPLACED THE NR 1 TRANSFORMER RECTIFIER UNIT REVERSE CURRENT CIRCUIT BREAKER CONTRACTOR. 2L72 4T RTA27NM 19950505005691995050500569EU 1995 5 5 UF6A950407 119950412A2433TR202B RECTIFIER BAG ATP ATP EU NR 2 FAILED A UF6AO OTHER O OTHER DEDESCENT 1 CE03854AW 2028 ORD FLT 5030 - THE NR 2 NON-ESSENTIAL BUSBAR FELL OFF LINE. MAINTENANCE REPLACED THE NR 2 TRANSFORMER RECTIFIER UNIT. (Z) 2L72 4T RTA27NM 19950505005701995050500570NM 1995 5 5 USAA950353 119950405A79201350M80G01 SCAVENGE TUBE BOEING767 767201 1385125NM RT ENGINE LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19648US 23900 LAS - FLT 90 - EN ROUTE LAX TO PHL, THE RIGHT ENGINE BEGAN TO STEADILY LOSE OIL. THE CREW DECIDED TO DIVERT TO LAS. FLIGHT LANDED WITHOUT INCIDENT. ENGINE WAS NOT SHUTDOWN. MAINTENANCE FOUND A PIN HOLE IN THE CHIP DETECTOR OIL SCAVENGE TUBE NEAR THE FUEL/OIL COOLER. THE TUBE WAS REPLACED. LEAK CHECKED GOOD. (Z) 2L72 4F RTA1NM 19950505005711995050500571WP 1995 5 5 USAA950370 119950412A3350 EEL BATT PACK DOUG DC9 DC981 3022081WP EXTERIOR DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19819US 48099 PHL - THE EXTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED NORMAL. (Z) 2L72 4F A6WE 19950505005721995050500572WP 1995 5 5 USAA950371 119950412A3350 EEL DOUG DC9 DC931 3022065WP CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19937VJ 48117 PIT - THE PORTABLE EMERGENCY LIGHT AT THE MAIN ENTRANCE DOOR WAS BROKEN. MAINTENANCE REPLACED THE PORTABLE EMERGENCY LIGHT FWD GALLEY. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950505005731995050500573WP 1995 5 5 USAA950372 119950413A3350 EEL BATTERIES DOUG DC9 DC981 3022081WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19819US 48099 CLT - THE COCKPIT EMERGENCY LIGHTS DO NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERIES ON THE COCKPIT EMERGENCY LIGHT POWER SUPPLY. OPERATIONS CHECKED GOOD. (Z) 2L72 4F A6WE 19950505005741995050500574WP 1995 5 5 USAA950373 119950414A5610 WINDSHIELD DOUG DC9 DC931 3022065WP COCKPIT LOST SEALANT A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19922VJ 48142 CLT - THE CAPTAINS WINDSHIELD LOST TAPING AND SEALER AT 12,000 FEET. THE SEALANT OBSTRUCTED THE VIEW OF THE WINDSHIELD. FLIGHT RETURNED TO CLT. MAINTENANCE RESEALED THE CAPTAINS WINDSHIELD. (M) 2L72 4F A6WE 19950505005751995050500575WP 1995 5 5 USAA950374 119950413A56105887275501 WINDOW DOUG DC9 DC931 3022065WP CENTER CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19986VJ 47209 PIT - THE CENTER WINDSHIELD CENTER PANE CRACKED EN ROUTE TO DTW. FLIGHT DIVERTED TO PIT. MAINTENANCE REPLACED THE CENTER WINDOW. (Z) 2L72 4F A6WE 19950505005761995050500576EU 1995 5 5 9507043208 119950421A5315D53070011 FLOORBEAM AIRBUS320 A320211 3930320EU FS 31577-32074 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BEAM AT Y EQUALS 1262. CORROSION WAS FOUND ON THE UPPER SURFACE OF THE UPPER FLANGE BETWEEN FRAMES 66 AND 67. CORROSION IS LOCALIZED AROUND FASTENER ATTACH HOLES FOR FLOOR BOARDS. REPAIRED PER NWA EA 32-97841. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005771995050500577EU 1995 5 5 9507053208 119950425A5313D5323105200 LONGERON AIRBUS320 A320211 3930320EU FS 13767-14300 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 32 AND 33. CORROSION IN LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97845. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005781995050500578EU 1995 5 5 9507063208 119950422A5320D53472172203 SUPPORT AIRBUS320 A320211 3930320EU FS 31577-32571 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -1292 BETWEEN FRAMES 66 AND 68. REPAIRED PER NWA EA 32-97981. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005791995050500579EU 1995 5 5 9507073208 119950426A5313D53231205200 LONGERON AIRBUS320 A320211 3930320EU FS 14300-14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 AND 34. CORROSION IS LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF THE CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97847. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005801995050500580EU 1995 5 5 9507083208 119950422A5320D53472089002 SUPPORT AIRBUS320 A320211 3930320EU FS 31577-33096 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACES OF THE FLOOR SUPPORTS AT Y EQUALS -1292 BETWEEN FRAMES 68 AND 69 AND AT Y EQUALS -464 BETWEEN FRAMES 66 AND 67. REPAIRED PER NWA EA 32-97984. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005811995050500581EU 1995 5 5 9507093208 119950429A5313 LONGERON AIRBUS320 A320211 3930320EU FS 10033-15367 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41L AND 43L. CORROSION IS LOCALIZED AROUND FASTENERS COMMON TO FUSELAGE SKIN. CORROSION ON STR 41L EXISTS BETWEEN FRAMES 25 AND 35. CORROSION ON STR 43L IS LOCATED BETWEEN FRAMES 29 AND 34. REPAIRED PER NWA EA 32-97848. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005821995050500582EU 1995 5 5 9507103208 119950428A5313D53231206200 LONGERON AIRBUS320 A320211 3930320EU FS 12167-12700 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON RIVETS COMMON TO STR 40L BETWEEN FRAMES 29 AND 30. AFTER REMOVAL OF THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EA 32-97855. SERIAL NR 32 CHANGED TO 107. 2L72 4F RTA28NM 19950505005831995050500583EU 1995 5 5 9507113208 119950421A5320D53112821200 FLOOR SUPPORT AIRBUS320 A320211 3930320EU FS 6053-9500 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 32 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -254 BETWEEN FRAMES 12 AND 24. REPAIRED PER NWA EA 32-97979. 2L72 4F RTA28NM 19950505005841995050500584EU 1995 5 5 9507123202 119950501A2150761A000004 ACTUATOR AIRBUS320 A320211 3930320EU LOWER FUSELAGE MALFUNCTIONED A NWAAAF UNSCHED LANDING ACTIVATE FIRE EXT. BJMSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OVER TEMP CRCRUISE 1 GL01302US114864073 32 DURING CRUISE WHILE AT FL 390, THE NR 2 PACK OVERHEATED TO 245 DEGREES CELSIUS, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. PACK OVERHEATED AGAIN TO 260 DEGREES CELSIUS, THE PACK WAS SHUTDOWN. LIGHT SMOKE WAS VISIBLE IN THE CABIN. RECEIVED 'SMOKE AFT CARGO SMOKE' MESSAGE. THE AFT CARGO FIRE BOTTLES WERE DISCHARGED. ACCOMPLISHED AN EMERGENCY DESCENT AND THE SMOKE CLEARED AFTER APPROXIMATELY 10 MINUTES. AIRCRAFT DIVERTED TO BIS WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED WITH EMERGENCY EQUIPMENT STANDING BY. MAINTENANCE REPLACED THE NR 2 PACK INLET AND OUTLET ACTUATORS. AFT CARGO COMPARTMENT FIRE BOTTLES WERE REPLACED. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950505005851995050500585WP 1995 5 5 9507139852 119950501A32302C6540 HYDRAULIC VALVE DOUG DC9 DC951 3022051WP NLG MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01761NC 47709 NOSE LANDING GEAR FAILED TO FULLY RETRACT AFTER TAKEOFF FROM TPA. RED UNSAFE LIGHT REMAINED ON AND NOISE LEVEL WAS CONSISTENT WITH GEAR BEING EXTENDED. NOSE GEAR RETRACTED NORMALLY WHEN HANDLE WAS MOVED TO 'UP' POSITION AFTER UPLATCH CHECK. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. REPLACED UPLOCK/DOWNLOCK HYDRAULIC CHECK VALVE DUE TO BYPASSING. CYCLED NOSE GEAR SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950505005861995050500586WP 1995 5 5 9507149855 119950425A215060529042 FAN DOUG DC9 DC951 3022051WP RIGHT PACK MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01764NC31200 47717 NUMEROUS CIRCUIT BREAKERS BEGAN POPPING DURING TAKEOFF ROLL AT 100 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED RIGHT PACK COOLING FAN DUE TO SUSPECTED PROBLEM WITH CAUSING BREAKERS TO POP. ALSO, REPLACED FORWARD CENTER BOOST PUMP DUE TO BOTH 'A' AND 'B' PHASE CIRCUIT BREAKERS POPPED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950505005871995050500587WP 1995 5 5 9507159907 119950424A2810 PUMP COVER DOUG DC9 DC931 3022065WP LT WING LOOSE A NWAAO OTHER K FLUID LOSS UKUNKNOWN 1 GL01957N 47253 EN ROUTE BWI-MSP, PASSENGER REPORTED FUEL LEAKING FROM FLAP AREA INBOARD OF LEFT WING. FIRST OFFICER'S VISUALLY CONFIRMED REPORT. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. FOUND FUEL LEAKING FROM LEFT WING TANK AFT BOOST PUMP COVER. TIGHTENED SEVERAL LOOSE SCREWS. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950505005881995050500588 1995 5 5 9507169969 419950502A341880098717 STALL TRANSDUCER DOUG DC9 DC931 3022065WP RT FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 GL019333 8922 989 47246 STALL WARNING SYSTEM ACTIVATED ON ROTATION. PULLED STALL WARNING COMPUTER CIRCUIT BREAKERS AND RETURNED TO DTW WITHOUT INCIDENT. FOUND NR 2 TRANSDUCER PIN POPPED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950505005891995050500589WP 1995 5 5 9507179984 119950429A2120 AIR DIST DOUG DC9 DC932 3022066WP CABIN SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01984US 47383 FLIGHT ATTENDANT REPORTED SMOKE IN FORWARD PORTION OF CABIN AFTER TAKEOFF. SHUT OFF GALLEY POWER, BUT SMOKE DID NOT DISSIPATE. FLIGHT RETURNED TO CID AND LANDED WITHOUT INCIDENT. CHECKED GALLEY WITH POWER ON AND CHECKED WIRING AND CANNON PLUGS TO OVENS. NO PROBLEMS WERE FOUND. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950505005901995050500590NM 1995 5 5 95UAL757012 119950502A2782 ACTUATOR SUNSTRAND 755299A BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 6 SLAT MALFUNCTIONED A UALAK NONE J WARNING INDICATION LDLANDING 1 WP29554UA A2466 26644 LANDED UNDER AMBER ALERT DUE TO SLAT ASYMMETRY INDICATION. SLAT CORRECTED FROM FLAP ORIGINALLY REPORTED. REPLACED NR 6 SLAT ROTARY ACTUATOR. 2L72 4F4 FRTA2NM E17NE 19950505005911995050500591GL 1995 5 5 95UALD10041 219950502A7200 ENGINE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 FAILED A UALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. TY ENGINE CASE PENETRATION ENGINE STOPPAGE TOTAKEOFF 1 WP291811U 46610 451592 NR TWO ENGINE FAILED UPON APPLICATION OF TAKEOFF POWER. LIBERATED ENGINE PARTS PENETRATED ENGINE CASE AND COWLING. THE BOLTS AT THE FIRST LPT DISK TO SECOND DISK ATTACH FLANGE WERE FOUND FAILED ALLOWING THE FIRST DISK TO RUB THROUGH THE LPT STATOR CASE. UAL REVISING PROCEDURES TO USE ONLY NEW BOLTS AND NUTS AT THE FLANGE JOINT AS A PRECAUTION. 2L73 4F4 F A22WE E23EA 19950505005921995050500592WP 1995 5 5 ABXA9500378 119950428A251059253791 SEAT DOUG DC9 DC931 3022065WP COCKPIT MALFUNCTIONED A ABXAK NONE O OTHER TOTAKEOFF 1 GL23929AX 45874 CAPTAIN'S SEAT SLIDES BACK ON TAKEOFF AND CLIMBOUT. DIFFICULT TO LOCK IN PLACE. REPLACED CAPTAIN'S SEAT IAW DC-9 MM 25-10-0. OPS CHECKED GOOD. SEAT WAS ROUTED TO SHOP WHERE FUNCTIONALLY CHECKED GOOD. SUBSEQUENT FLIGHTS HAVE HAD NO DISCREPANCIES. 2L72 4F A6WE 19950505005931995050500593NM 1995 5 5 QXEA9500131 119950501A3350P2070001201S EEL DORNERDO32 DO328100 2996000NM CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09339PH 3015 PDX - FLIGHT ATTENDANT FORWARD EMERGENCY FLASH LIGHT INOP. RELACED FLASHLIGHT AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950505005941995050500594NM 1995 5 5 QXEA9500132 119950501A33506104781 EEL BATTERY PACKDHAV DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09827PH 275 PDX - RIGHT HAND FORWARD FUSELAGE EMERGENCY LIGHT INOP. EMERGENCY LIGHT ON CABIN OVERHEAD AT ROW 1 INOP. REPLACED BATTERY PACK AT PS2 POSITION. LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950505005951995050500595NE 1995 5 5 95ZZZX2195 119950227A29137665009808101 PUMP ABEX SKRSKYS76 S76 8143010NE HYD SYS FAILED A HEEAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW03911MJ 198773 760231 ON TAKOFF, THE NR 2 SERVO LIGHT ILLUMINATED WITH DROP IN HYDRAULIC PRESSURE. REPLACED PUMP. CHAPTER 29-20-01, FIGURE 1, PAGE 0, ITEM 11. 1G72 3U H1NE 19950505006001995050500600GL 1995 5 5 95ZZZX2200 219950402A7321252464428 FUEL CONTROL BENDIX BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20 03013GL NR 2 ENG MALFUNCTION A HEEAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW035418A7234 2252 33099 S800 CAE836259 PILOT REPORTED TORQUE SPLITS AFTER TAKEOFF. UNABLE TO MATCH TORQUES. NR 2 ENGINE SURGING. REPLACED FUEL CONTROL. 1G72 3U3 UNCH3EU E4CE 19950505006011995050500601SW 1995 5 5 95ZZZX2201 119950406A6730212076004005 SERVO BELL 412 412 1182202SW T/R DEFECTIVE A HEEAK NONE O OTHER NRNOT REPORTED 1 SW032298Z 2605 33077 RIGHT TAIL ROTOR PEDAL MOTORED INTERMITTENTLY. INSPECTED SYSTEM, CHECKED RIG. REPLACED SERVO. IPC 67-19-22. 1G72 4U H4SW 19950505006021995050500602GL 1995 5 5 95ZZZX2202 219950404A7321252464428 FUEL CONTROL BENDIX BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20 03013GL NR 2 ENGINE FAILED A HEEAO OTHER O OTHER APAPPROACH 1 SW035418A 969 331438 S800 CAE836259 ON FINAL APPROACH WHEN POWER WAS APPLIED, NR 2 ENGINE TORQUE STOPPED AT 55. REPLACED FUEL CONTROL. 250C20 IPC FIGURE 9, ITEM 91. 1G72 3U3 UNCH3EU E4CE 19950505006031995050500603NE 1995 5 5 95ZZZX2203 219950406A753025490201 FLOW MODULATOR BOLKMS117 BK117B2 5626013EU LYC LTS101LTS101750B1 41560NE NR 2 ENGINE MALFUNCTION A HEEAO OTHER R PARTIAL RPM/PWR LOSS HOHOVERING 1 SW03136AE 513 1574 7234 LE456098 NR 2 ENGINE TORQUE SPLIT LOW WHEN THE AIRYCRAFT WAS PICKED UP TO A HOVER. CYCLED FLOW FENCE WITH SHOP AIR, LUBED ACTUATOR, CHECKED OPERATING RANGE. RETURNED TO SERVICE. 1G72 3U3 UNCH13EU E5NE10 19950505006041995050500604GL 1995 5 5 95ZZZX2204 219950401A7530C1052050000113 TUBE ASSY BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20 03013GL ENGINE BLEED LOOSE A HEEAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW035418A S800 CAE836259 IN FLIGHT, AIRCRAFT WAS UNABLE TO MAINTAIN N2 RPM. RETURNED TO BASE. FOUND CUSTOMER BLEED AIR LINE LOOSE AT FIREWALL FITTING. 1G72 3U3 UNCH3EU E4CE 19950505006051995050500605SW 1995 5 5 95ZZZX2205 119950330A6720412074101101 TRANSDUCER BELL 412 412 1182202SW YAW CHANNEL DEFECTIVE A HEEAK NONE O OTHER NRNOT REPORTED 1 SW0322608 33075 PEDALS WOULD NOT RESPOND TO NORMAL INPUT. FOUND YAW CHANNEL CONTROL MOTION TRANSDUCER STICKING. CLEANED AND LUBED. FIGURE 67-15, ITEM 45. 1G72 4U H4SW 19950505006061995050500606NE 1995 5 5 95ZZZX2207 119950330A62107615009043050 TIP CAP SKRSKYS76 S76A 8143006NE M/R MISSING A HEEAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SW035444X C76OTI1 760174 CREW FELT A SUDDEN VIBRATION FROM THE MAIN ROTOR SYSTEM. MADE A PRECAUTIONARY LANDING. FOUND ONE-THIRD OF THE TRAILING EDGE OF THE TIP CAP MISSING. S-76 IPC CHAPTER 65, SECTION 11, UNIT 00, FIGURE 1, ITEM 3.` 1G72 3U H1NE 19950505006071995050500607NE 1995 5 5 95ZZZX2208 119950127A2913APIVIII PUMP APEX SKRSKYS76 S76A 8143006NE NR 1 HYD SYS DEFECTIVE A HEEAK NONE O OTHER NRNOT REPORTED 1 SW03154601554 195812 760223 PILOT REPORTED 400-500 PSI FLUCTUATION IN NR 1 HYDRAULIC SYSTEM PRESSURE. REPLACED PUMP. IPC 29-10-01, FIGURE 1 ITEM 12. 1G72 3U H1NE 19950505006081995050500608GL 1995 5 5 95ZZZX2209 219950328A7200 ENGINE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 1 MAKING METAL A HEEAO OTHER J WARNING INDICATION CRCRUISE 1 SW0381982191511331 S818 CAE836263 NR 1 ENGINE CHIP LIGHT IN-FLIGHT. REDUCED POWER TO NR 1. LANDED WITH BOTH ENGINES ON LINE. FOUND SMALL FLAKES RINGING BOTH PLUGS AND IN FILTERS. ENGINE HAS HISTORY OF LIGHTS. REPLACED ENGINE. 1G72 3U3 U H3EU E4CE 19950505006091995050500609SW 1995 5 5 95ZZZX2210 119950127A6730MS21902W4 UNION BELL 230 230 1182149SW SERVO PORT CRACKED A HEEAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SW03236X 23015 LOST HYDRAULIC PRESSURE ON NR 1 SYSTEM ON LANDING. FOUND THE PRESSURE LINE UNION CRACKED ON THE CENTER SERVO. FIGURE 29-1001, ITEM 11. 1G72 3U NCH9SW 19950505006101995050500610EU 1995 5 5 95ZZZX2211 119950303A3310117920303 CONTROL UNIT BOLKMS117 BK117A4 5626017EU COPILOT DIMMER FAILED A HEEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03911NC 7026 PILOT REPORTED SMELLING SMOKE IN COCKPIT. RETURNED TO BASE. MECHANIC INSPECTED AND FOUND COPILOT INSTRUMENT LIGHT DIMMER CONTROL CAUSE OF SMOKE. FOUND WATER ON TOP OF UNIT. IPC FIGURE 923-50. 1G72 3U H13EU 19950505006111995050500611EA 1995 5 5 95ZZZX2212 219950227A7321025277300 FUEL PUMP SUNDSTRANDEM BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR 1 ENGINE FAILED A HEEAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SW031079U102783057 PE6155T 31122 PCE82959 NR 1 ENGINE FLAMED OUT IN-FLIGHT. FOUND FUEL PUMP DRIVE COUPLING FAILURE. MALE SPLINES ON DRIVE GEAR INSIDE PUMP WERE ROUNDED OFF. 1G71 4U4 U H4SW E22EA 19950505006121995050500612SW 1995 5 5 95ZZZX2213 119950127A7931206075677103 INDICATOR BELL 206 206L1 1182107SW ENGINE OIL DEFECTIVE A HEEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW033178K 45765 ENGINE INDICATED OIL PRESSURE DROPPED TO 50 PSI. LANDED. CONFIRMED OIL PRESSURE, REPLACED THE OIL PRESSURE INDICATOR. IPB 95-99-00, PAGE 12, FIG 95-4, ITEM 52. 1G71 3U H2SW 19950505006131995050500613EU 1995 5 5 95ZZZX2214 119950227A6310330A54020628 DISK COUPLING 355A35203400AEROSPAS355 AS355F1 8680810EU NR 2 ENGINE FAILED A HEEAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 SW035796T1610 PMA92 5166 PILOT DETECTED A HUM AND VIBRATION FOR APPROXIMATELY ONE MINUTE, FOLLOWED BY A BANG AND LOSS OF POWER ON NR 2 ENGINE. FOUND THE NR 2 FLEX COUPLING AT THE TRANSMISSION DESTROYED. CHAPTER 63-20-40, PAGE 6, FIGURE 3, ITEM 345. 1G72 3U H11EU 19950505006391995050500639NM 1995 5 5 95ZZZW618 119950329A5313 STRINGER BOEING727 727231 1384079NM FS 950-960 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055435237447 21984 MCI - DURING OP-17, FOUND CORROSION AND 20 INCH CRACK IN STRINGER 29R, STATION 950 TO 960F. REPAIRED PER ARA 9145. TOTAL CYCLES 24,387. 2L73 4F A3WE 19950505006401995050500640NM 1995 5 5 95ZZZW619 119950404A5330 SKIN BOEING727 727231 1384079NM FS 720-724 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055435237447 21984 MCI - DURING OP-17, FOUND CORROSION ON FUSELAGE SKIN, STATION 720 TO STATION 724, FROM FOUR INCHES LBL TO FOUR INCHES RBL. INSTALLED SKIN DOUBLER PER SRM 53-30-3, FIGURE 1. TOTAL CYCLES 24,387. 2L73 4F A3WE 19950505006411995050500641NM 1995 5 5 95ZZZW620 119950327A332061482 BALLAST BOEING737 737247 138448DNM FWD LAV SHORTED A A6XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO134515W 19612 CREW NOTICED A BAD SMOKEY SMELL IN FLIGHT COMPARTMENT AND DECLARED EMERGENCY LANDING. FORWARD LAVATORY MIRROR LIGHT BALLAST SHORTED OUT AND POPPED CIRCUIT BREAKER. REMOVED AND REPLACED BALLAST AND LIGHT ASSY. OPS CK OK. (W) 2L72 4F A16WE 19950505006421995050500642WP 1995 5 5 95ZZZW621 119950418A57111642862101 SPAR WEB LKHEED1011 10113851 5265010WP WS 228-423 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA38155 193A1012 WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W) 2L73 4F A23WE 19950505006431995050500643WP 1995 5 5 95ZZZW622 119950418A57111642862103 SPAR WEB LKHEED1011 10113851 5265010WP WS 228-423 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA38155 193A1012 WING REAR SPAR AND WEB UPPER CAP REPLACEMENT IWS 228-423. REPAIR CARRIED OUT BY DELTA AIRLINES IAW ERA 280196-14AD REV B DATED 3-29-94. REFERENCED BY FAA FORM 8110-3 DATED 3-31-95. (W) 2L73 4F A23WE 19950505006441995050500644NM 1995 5 5 95ZZZW623 119950302A2750 POWER DRIVE BOEING727 7272B7 138407LNM TE FLAPS LEAKING A AMTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL11762AT 22162 LAS - FLT 80 - 'A' SYSTEM FLUID LOSS IN FLIGHT. REMOVED AND REPLACED FLAP POWER DRIVE UNIT AS PER MM CHAPTER 27-51-62. LEAK OPS CHECK NORMAL. 2L73 4F A3WE 19950505006451995050500645NM 1995 5 5 95ZZZW624 119950314A3510 OXYGEN REG BOEING727 727227 1384078NM COCKPIT LOOSE A AMTAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL11769AT 21998 MKE - FLT 517 - DURING TAXI OUT CREW OXYGEN PRESSURE DROPPED FROM 1500 TO 1000 PSI. RESERVICED 0XYGEN, TIGHTENED FITTING ON OXYGEN REG/FE'S. 2L73 4F A3WE 19950505006461995050500646 1995 5 5 95ZZZW625 419950414A3421258733511 VERTICAL GYRO BOEING727 7272Q9 138448MNM NR 2 INOP A DHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01741DH 80112475 21931 ON TAKEOFF, FLIGHT OFFICER ADI FAILED INTERMITTENTLY AT BANK GREATER THAN 4 DEGREE. DIVERTED TO CVG. LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 VERTICAL GYRO, PER DHL 727 MM 34-22-21. ALL INDICATIONS NORMAL. 2L73 4F RTA3WE 19950505006471995050500647NM 1995 5 5 95ZZZW626 119950304A3510 OXYGEN MASK BOEING727 7272B7 138407LNM CABIN FAILED A AMTAO OTHER O OTHER TXTAXI/GRND HDL 1 GL11770AT 21953 DTW - FLT 228 - ROW 30 DEF OXYGEN MASK FELL FROM PSU. REPACKED OXYGEN MASK, OK FOR SERVICE. 2L73 4F A3WE 19950505006481995050500648WP 1995 5 5 95ZZZW627 119950414A5311 FRAME DOUG DC9 DC931 3022065WP FS 445 CORROSION B EF2RK NONE O OTHER ININSP/MAINT 1 SW07650UG 47418 MODERATE CORROSION DAMAGE ON BELTFRAME AFT SIDE FLANGE, FS 445, LONGERON 29L. REPAIRED FRAME PER SRM 53-03, FIGURE 32. (W) 2L72 4F A6WE 19950505006491995050500649WP 1995 5 5 95ZZZW628 119950414A5320 FITTING DOUG DC9 DC931 3022065WP FS 917 CORROSION B EF2RK NONE O OTHER ININSP/MAINT 1 SW07650UG 47418 MODERATE CORROSION DAMAGE ON 'T' FITTING LONGERON 19R, FS 917 (INSIDE TORQUE BOX LIGHTENING HOLE). REPLACED FITTING PER SRM 51-30-1. 2L72 4F A6WE 19950505006501995050500650WP 1995 5 5 95ZZZW629 119950414A5330 SKIN DOUG DC9 DC931 3022065WP FS 1044 CRACKED B EF2RK NONE O OTHER ININSP/MAINT 1 SW07650UG 47418 EDDY CURRENT INSPECTION INDICATES 2 CRACKS IN EXTERNAL SKIN AT FASTENER HOLES, FS 1044, BETWEEN LONGERONS 12-13 LEFT AND 12-13 RT. REPAIRED SKIN PER SRM 53-01, FIGURE 2, SHEET 3. 2L72 4F A6WE 19950505006511995050500651CE 1995 5 5 95ZZZW630 119950310A323099102251RX CONTROL VALVE CESSNA402 402C 207590RCE LANDING GEAR FAILED A GUUAO OTHER J WARNING INDICATION APAPPROACH 1 SO1962PB 679 402C0310 FLT 102 - GEAR WILL NOT EXTEND HYDRAULICALLY, USED EMERGENCY BOTTLE, WORKS OK. REMOVED AND REPLACED SELECTOR VALVE, BLED SYSTEM, LEAK CHECK OPS CHECKS GOOD. BLOW DOWN SYSTEM RESERVICED. AIRCRAFT TEST FLOWN SATISFACTORY AND RELEASED TO REVENUE SERVICE. 1L72 3O A7CE 19950505006521995050500652WP 1995 5 5 95ZZZW631 119950413A30402726129802 CONTROLLER LKHEED1011 1011385115 5265015WP WINDSHIELD HEAT FAILED A TWAAHF DEACTIVATE SYST/CIRCUITSACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531031 193B1115 SJU - DURING CRUISE, WINDSHIELD HEAT WIRE HARNESS SHORTED AT R-2 WINDOW CAUSING ARCING AND SMOKE IN COCKPIT. TURNED OFF WINDSHIELD HEAT AND DISCHARGED HAND EXTINGUISHER. REPLACED WINDSHIELD WIRING HARNESS AND WINDSHIELD HEAT CONTROLLER MFG, P/N 27261298-02. WINDSHIELD HEAT OPERATION CHECKED NORMAL. 2L73 4F A23WE 19950505006531995050500653NM 1995 5 5 95ZZZW632 119950417A261260B00023163 FIRE DETECTOR BOEING747 747131 1384881NM NR 1 ENGINE FAILED A TWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE. THE NR 1 ENGINE FIREWARNING SOUNDED. SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES. FOUND BOTH DETECTORS SHORTED. REPLACED BOTH DETECTORS, MFG P/N 60B00023-163 AND P/N 60B00023-166. PERFORMED POWER RUNUP AND NACELLED DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL. 2L74 4F A20WE 19950505006541995050500654NM 1995 5 5 95ZZZW633 119950417A261260B00023166 FIRE DETECTOR BOEING747 747131 1384881NM NR 1 ENGINE FAILED A TWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE, NR 1 NACELLE FIRE DETECTOR FAULT LIGHT ILLUMINATED WITH TEMPERATURES IN THE FAULT RANGE. THE NR 1 ENGINE FIREWARNING SOUNDED. SHUT DOWN NR 1 ENGINE AND DISCHARGED BOTH EXTINGUISHER BOTTLES. FOUND BOTH DETECTORS SHORTED. REPLACED BOTH DETECTORS, MFG P/N 60B00023-163 AND P/N 60B00023-166. PERFORMED POWER RUNUP AND NACELLED DETECTOR FAULT AND FIREWARNING SYSTEMS CHECKED NORMAL. 2L74 4F A20WE 19950505006551995050500655NM 1995 5 5 95ZZZW634 119950317A5311 FRAME BOEING727 727231 1384079NM FS 783.95 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432962027 20307 MCI - DURING C-CHECK, FOUND TWO INCH CRACK IN INBOARD AFT SIDE OF FRAME, BELOW FLOOR LEVEL, FS 783.95. STOP DRILLED CRACK AND INSTALLED REPAIR PER EMLR 65661. TOTAL CYCLES 42,060. 2L73 4F A3WE 19950505006561995050500656NM 1995 5 5 95ZZZW635 119950317A5320 PRESSURE DECK BOEING727 727231 1384079NM FS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432962027 20307 MCI - DURING C-CHECK, FOUND .5 INCH CRACK IN PRESSURE DECK EIGHT INCHES INBOARD OF 940 CASTING. STOP DRILLED AND INSTALLED DOUBLER PER ARA 9130. TOTAL CYCLES 42,060. 2L73 4F A3WE 19950505006571995050500657NM 1995 5 5 95ZZZW636 119950320A5330 SKIN BOEING727 727231 1384079NM FS 250 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432962027 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 250, LOWER AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132. TOTAL CYCLES 42,060. 2L73 4F A3WE 19950505006581995050500658NM 1995 5 5 95ZZZW637 119950320A5330 SKIN BOEING727 727231 1384079NM FS 252 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432962027 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 252, AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ARA 9132. TOTAL CYCLES 42,060. 2L73 4F A3WE 19950505006591995050500659WP 1995 5 5 95ZZZW638 119950223A5313 LONGERON DOUG DC9 DC931 3022065WP FS 446 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05990Z 47136 STL - DURING SPECIAL CHECK, FOUND CRACKS 1.75 INCHES LONG ON BOTH SIDES OF SPLICE, LONGERON 30, STATION 446. REPAIRED PER SRM 53-02, FIGURE 14, SHEETS 1 AND 2, AND STANDARD PRACTICES. 2L72 4F A6WE 19950505006601995050500660NM 1995 5 5 95ZZZW639 119950410A2612895398 FIRE LOOP BOEING747 747131 1384881NM NR 1 ENGINE MALFUNCTIONED A TWAAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 CE0553116 20321 SNN - MADE UNSCHEDULED LANDING ACCOUNT NR 1 ENGINE 'A' FIREWARNING ILLUMINATED. SHUT DOWN ENGINE AND DISCHARGED EXTINGUISHER BOTTLERS. 'B' LOOP PREVIOUSLY PLACARDED ON MEL. RESTORED 'B' LOOP BY REPLACEMENT OF LOWER AFT WARNING LOOP, MFG P/N 895398. REPLACED EXPENDED BOTTLES AND PLACARDED 'A' LOOP PER MEL. OPS CHECKS NORMAL. 2L74 4F A20WE 19950505006611995050500661NM 1995 5 5 95ZZZW640 119950223A5313 STRINGER BOEING727 727231 1384079NM FS 1000 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736843 21989 MCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000. REPAIRED PER ARA 9054. TOTAL CYCLES 22,210. 2L73 4F A3WE 19950505006621995050500662NM 1995 5 5 95ZZZW641 119950223A5313 STRINGER BOEING727 727231 1384079NM FS 990 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE058435736843 21989 MCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990. REPAIRED PER ARA 9054. TOTAL CYCLES 22,210. 2L73 4F A3WE 19950505006631995050500663WP 1995 5 5 BUFA9511 119950417A7931 OIL PRESS LIGHT DOUG DC8 DC861 3021952WP NR 2 ENGINE ILLUMINATED A BUFAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 CE05161DB 45980 FLT LIC035 - SVMI-KMIA - NR 2 ENGINE OIL PRESS LIGHT CAME ON AT 310 VERIFIED BY OIL PRESS INDICATOR AND OIL QUANTITY. SHUT NR 2 ENGINE DOWN, COMPLETED PROPER CHECK LIST AND PROCEDURE. (W) 2L74 4F 4A25 19950505006641995050500664WP 1995 5 5 CKSA95017 119950413A78105757S09501 EXHAUST DUCT DOUG DC8 DC863F 302198FWP NR 2 ENGINE DAMAGED A ACKSAF ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 GL23815CK32529 46151 KMIA - AFTER ROTATION AND PRIOR TO REACHING 2000 FEET, RECEIVED FIRE INDICATION ON NR 2 ENGINE. FIRE INDICATION DID NOT GO OUT AFTER SHUTTING DOWN ENGINE. FIRED ONE EXTINGUISHER BOTTLE, FIRE INDICATIONS WENT OUT. FOUND OUTBOARD SIDE EXHAUST NOZZLE LEAKING, HOT EXHAUST GAS CAUSING FIRE WARNING, REPLACED ALL BOLTS AND NUTS ON NOZZLE CASE, ALSO REPLACED DAMAGED TRANSITION DUCT AND FIRE BOTTLE. PERFORMED ENGINE RUN UP, CHECKED NORMAL IAW 26-20-0 AND 72-00-00. 2L74 4F 4A25 19950505006651995050500665NM 1995 5 5 CKSA95019 119950407A2612 CONNECTORS BOEING747 747146 NM NR 1 ENGINE DIRTY A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23703CK60196 19727 KHI-JED - EN ROUTE NR 1 ENGINE FIRE LOOP 'A' READ 9.5, AN ASSOCIATED FIRE DETECTION LIGHT ILLUMINATED ON THE PILOTS PANEL. OPERATED NORMALLY PER MEL 26-1-1 'B' LOOP FAILED 1 HR FROM JED. CLEANED CONTAMINATION OF CONNECTORS ON LOOP 'A' AND 'B' IAW BMM 26-11-00. OPS CHECKS NORMAL ON GROUND RUN. (W) 2L74 4F A20WE 19950505006661995050500666NM 1995 5 5 IXKA9500016 119950413A3244 TIRES BOEING727 727251 138408HNM MLG FAILED A IXKAK NONE O OTHER LDLANDING 1 EA25258US 19977 ACY - UPON LANDING, 3 EACH MAIN WHEEL ASSEMBLY TIRES BURST. REMOVED AND REPLACED NR 1, NR 2, NR 3, AND NR 4 MAIN WHEEL ASSEMBLIES PER MM 32-45-01. (X) 2L73 4F A3WE 19950505006671995050500667EU 1995 5 5 PAYA95A4018 119950417A3260 CONNECTOR AEROSPATR42 ATR42300 8680920EU RT MLG LOOSE A PAYAO OTHER N FALSE WARNING APAPPROACH 1 EA174206G 081 FLT 7760 - PHL-JFK - RIGHT MAIN LANDING GEAR POSITION INDICATION INTERMITTENT AT OVERHEAD INDICATOR POSITION (COCKPIT). FOUND LOOSE CONNECTOR AT RT MLG PROX SWITCH, RESECURED. (W) 2H72 4T RTA53EU 19950505006681995050500668EU 1995 5 5 PAYA95A4019 119950419A3610 SEAL AEROSPATR42 ATR42300 8680920EU AIR DUCT BLEED WORN A PAYAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA174207G 083 FLT 7736 - DCA - JFK - NR 1 BLEED LEAK LIGHT ILLUMINATED, WITH A BURNING SMELL NOTED BY THE CREW. REPLACED BLEED AIR SEAL IN NR 1 BLEED SUPPLY DUCTING. (W) 2H72 4T RTA53EU 19950505006691995050500669NM 1995 5 5 TAOA049504 119950418A33501000677 EEL ASSEMBLY GRIMES BOEING727 727254 138408LNM CABIN INOPERATIVE A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15914TS 25424 20251 EMERGENCY EXIT LIGHT AT DOOR L-2 INOPERATABLE. REPLACED LIGHT ASSY, OPERATIONAL CHECK OK. (W) 2L73 4F A3WE 19950505006701995050500670NM 1995 5 5 TAOA049506 119950420A335007312 EEL MODULE BOEING727 727254 138408LNM CABIN BROKEN A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15913TS 20250 ONE 'E' PATH LIGHT MODULE BROKEN AT ROW 29. REPLACED LIGHT MODULE ASSY OPERATIONAL CHECK, OK. (W) 2L73 4F A3WE 19950505006711995050500671EU 1995 5 5 VTZA95145 119950417A61208210263 PROP GOVERNOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27490UE 909 FLT NR 6383 - CMH-IAD - DURING TAKEOFF ABORTED THE TAKEOFF DUE TO THE RIGHT ENGINE ONLY MAKING 40 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. CONTRACT MAINTENANCE ADJUSTED THE PROP GOVERNOR LOW RESET. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950505006721995050500672EU 1995 5 5 VTZA95146 119950421A27007003897903 COMPUTER JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILURE A VTZAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 EA27318UE 41041 FLT NR 6523 - IAD-PWM - DURING CRUISE RETURNED TO IAD DUE TO THE AUTOPILOT FAILING AND MODE C INOP. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE SELECTED ATC WINDOW TO READ ATC ALTITUDE. PERFORMED TRANSPONDER CHECKS, OPS CHECKS GOOD. OPENED DMI NR 20959 IAW MEL 22-1 ON 4-21-95. MAINTENANCE LATER CLEARED DMI NR 20959 ON 2-24-95 BY REPLACING THE FLIGHT CONTROL COMPUTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950505006731995050500673EU 1995 5 5 VTZA95147 119950422A7603T412AL3001C FLT IDLE BAULK JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 FLT NR 8014 - IAD-MGW - DURING CLIMB-OUT THE GEAR WOULD NOT RETRACT WHEN HANDLE SELECTED UP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FLIGHT IDLE BAULK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950505006741995050500674EU 1995 5 5 VTZA95148 119950421A2750TY176004A POSITION TRANS JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS FAILURE A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27315UE 41033 FLT NR 6270 - IAD-EWR - DURING APPROACH THE FLAP ASYMMETRY LIGHT ILLUMINATED. AIRCRAFT LANDED AT EWR WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED BOTH FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950505006751995050500675EU 1995 5 5 VTZA95149 119950420A32307177011 CONTROL UNIT JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 FLT 6418 - IAD-BOS - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP AFTER TAKEOFF. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LANDING GEAR CONTROL UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950505006761995050500676WP 1995 5 5 9507189924 119950409A5320 DOOR FRAME DOUG DC9 DC932 3022066WP FS 817 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926RC 47473 DURING LINE CHECK, FOUND 2 CRACKS, 2.25 INCHES AND 3.50 INCHES LONG IN THE AFT CABIN DOOR FRAME UPPER RIGHT SIDE FS 817. REPAIRED PER EA 99-091494. 2L72 4F A6WE 19950505006771995050500677WP 1995 5 5 9507199977 119950424A5754 FITTING DOUG DC9 DC931 3022065WP NR 5 TE SLAT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019341 47390 DURING PERIODIC CHECK, FOUND CRACK IN THE NR 5 SLAT TO TRACK OUTBOARD ATTACH FITTING. REPLACED SLAT PER CITEXT 09-2782-1-9802. 2L72 4F A6WE 19950505006781995050500678WP 1995 5 5 9507209604 119950429A5210 FITTING DOUG DC9 DC932 3022066WP MAIN CABIN DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE MAIN CABIN DOOR HINGE SUPPORT FITTING. REPLACED FITTING PER SRM 52-11-0 AND MM 20-50-01. 2L72 4F A6WE 19950505006791995050500679NM 1995 5 5 9507216613 119950429A5312 BULKHEAD BOEING747 747251B 1384892NM FS 1241 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613US 20358 DURING PERIODIC CHECK, FOUND A CRACK AND CORROSION IN THE SLANTED PRESSURE PANEL LOWER EDGE FS 1241, RBL 76. REPAIRED PER EA 66-97906. 2L74 4F A20WE 19950505006801995050500680WP 1995 5 5 9507229875 119950430A7120 BOLT DOUG DC9 DC951 3022051WP RT ENG MOUNT SHEARED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01784NC 48109 DURING LINE CHECK, FOUND RIGHT ENGINE FORWARD MOUNT AFT SIDE UPPER AND LOWER STRUTS LOOSE. FURTHER INVESTIGATION REVEALED A SHEARED UPPER BOLT. REPLACED BOLT PER MM 71-20-03. 2L72 4F A6WE 19950505006811995050500681WP 1995 5 5 9507239604 119950430A5320 FITTING DOUG DC9 DC932 3022066WP FS 975 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FRAME "T" FITTING FS 975, LONGERON 18R. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950505006821995050500682WP 1995 5 5 9507249604 119950430A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP FS 579 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN INTERCOSTAL FITTING FS 579 BETWEEN LONGERONS 27L - 28L. REPLACED FITTING PER SRM 51-00. 2L72 4F A6WE 19950505006831995050500683WP 1995 5 5 9507259604 119950430A5320 FITTING DOUG DC9 DC932 3022066WP FS 935 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FRAME "T" FITTING FS 935 AT FLOOR LEVEL, LEFT SIDE. REPLACED FITTING PER SRM 51-42. 2L72 4F A6WE 19950505006841995050500684WP 1995 5 5 9507269163 119950428A5350 HANDLE DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ALSO, FOUND THAT THE TAILCONE DID NOT DROP USING THE INTERIOR HANDLE. ADJUSTED BOTH THE CLIPS AND THE LATCHES. CHECKED OK. 2L72 4F A6WE 19950505006851995050500685WP 1995 5 5 9507279759 119950428A5350 HANDLE DOUG DC9 DC941 302207NWP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01759NW 47287 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ALSO, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE CLIPS AND LATCHES. CHECKED OK. 2L72 4F A6WE 19950505006861995050500686SO 1995 5 5 COM11879 119950503A533012019230001 SKIN EMB 120 EMB120RT SO FUSELAGE CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01130G 15278 120130 INSPECTION REVEALED SEVERE CORROSION TO THE LOWER FUSELAGE SKIN AT FRAME 21, BETWEEN STRINGERS 21L AND 21R. THE DAMAGED AREA WAS REMOVED AND AN EXTERNAL DOUBLER AND FILLER REPAIR WAS INSTALLED PER AERODESIGN REPORT NR 1437-2. 2L72 4T RTA31SO 19950505006871995050500687EU 1995 5 5 COM31068 119950501A3260A259 LAMP SAAB SF340 SF340A 7850100EU INST PANEL FAILED A COMAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO01341CA 340A021 RT MLG DID NOT INDICATE DOWN AND LOCKED. CYCLED LANDING GEAR AND ALL INDICATIONS NORMAL. FOUND INDICATOR LAMPS IN CONTROL HANDLE TO BE AT FAULT. REPLACED LAMPS. 2L72 4T RTA52EU 19950505006881995050500688EU 1995 5 5 COM31069 119950503A32465009237 BEARING RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01342CA9268 910001 340A023 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950505006891995050500689EU 1995 5 5 COM31070 119950501A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01344CA3038 371 AUG930540 340A025 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR BUSHING REPAIR. 2L72 4T RTA52EU 19950505006901995050500690EU 1995 5 5 COM31071 119950501A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01358CA8642 502 AUG910014 340A047 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. WHEEL SUBASSY HAS BEEN REMOVED AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950505006911995050500691WP 1995 5 5 MWEA95189 119950426A5330 SKIN DOUG DC9 DC932 3022066WP FS 160 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, A TEMPORARY REPAIR AT LONGERON 22L STA 160 WAS REPLACED WITH PERMANENT REPAIR IAW SRO9530219. TEMP REPAIR WAS ORIGINALLY INSTALLED DUE TO SKIN CRACK AT DESCRIBED LOCATION. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950505006921995050500692WP 1995 5 5 MWEA95190 119950429A5712991932215 RIB DOUG DC9 DC932 3022066WP WS 134.921 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA.XIS 134.921 WAS FOUND CRACKED AT LOWER AFT END 1.3750 INCHES IN LENGTH. 2L72 4F A6WE 19950505006931995050500693WP 1995 5 5 MWEA95191 119950429A571299374639 RIB DOUG DC9 DC932 3022066WP WS 129.710 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA XIS 129.710 WAS FOUND CRACKED AT LOWER LEG 2.75 INCHES IN LENGTH. 2L72 4F A6WE 19950505006941995050500694WP 1995 5 5 MWEA95192 119950429A5711 SPAR DOUG DC9 DC932 3022066WP LT WING LE CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, THE LEFT WING FWD UPPER SPAR CAP INBD OF SLAT DRIVE MECHANISM AT STA XIS 136.42 WAS FOUND TO BE CORRODED. 2L72 4F A6WE 19950505006951995050500695WP 1995 5 5 MWEA95193 119950429A5712SS095700035 RIB DOUG DC9 DC932 3022066WP WS 137 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, 2 CRACKS WERE FOUND ON LT WING LEADING EDGE RIB STA.XIS 137.0. ONE CRACK AT AFT UPPER END 3 FEET IN LENGTH, THE OTHER CRACK AT FWD UPPER END 1.50 INCHES IN LENGTH. BOTH CRACKS TEMPORARILY REPAIRED PER DOUGLAS TELEX 5-57-20-6 AND WILL BE INSPECTED EVERY 30 DAYS UNTIL REPLACED WITH NEW RIB. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950505006961995050500696NM 1995 5 5 MWEA95194 119950503A3350P4010021 EEL BATTERY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31601ME 49762 CREW REPORTS FWD FLIGHT ATTENDANT LOWER EMERGENCY FLASHLIGHT IS INOP. MAINTENANCE REPLACED BATTERY. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950505006971995050500697EU 1995 5 5 QXEA9500133 119950503A33501315 EEL BULBS FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 GEG - SEVERAL OVERHEAD EMERGENCY EXITS LIGHTS INOP. REPLACED BULBS AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950505006981995050500698NM 1995 5 5 SCNA95068 119950501A3350MS1557081 EEL BULB BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 L2 DOOR EMERGENCY EXIT LIGHT HAD TWO BULBS INOPERATIVE. RELAMPED L2 EMERGENCY EXIT LIGHT AND OPS CHECKED GOOD IAW 33-50-00. 2L73 4F RTA3WE 19950505006991995050500699NE 1995 5 5 SWAA950328 219950501A732127436025 FUEL CONTROL BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 2 ENGINE MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0793SW 201635373 22965 AFTER TAKEOFF, EXPERIENCED NR 2 ENGINE POWER FLUCTUATION AT ALL SETTINGS. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED NR 2 ENGINE FUEL CONTROL UNIT PER BOEING M/M. 2L72 4F4 F A16WE E2EA 19950505007001995050500700NM 1995 5 5 SWAA950329 119950501A33506104781 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0773SW 22673 AT GATE, FOUND EMERGENCY LIGHT STRIP LOOSE AT ROW 8 AND LIGHTS DIM DURING TESTING. REPLACED BATTERY PACK AT FWD CABIN AREA PER BOEING M/M. 2L72 4F A16WE 19950505007171995050500717SW 1995 5 5 95ZZZX2256 119950415A5310 FUSELAGE SWRNGNSA226 SA226TC 8780404SW NOSE BAG DR BIRD STRIKE A BDHAO OTHER C F.O.D. APAPPROACH 1 GL15327BA TC249 BIRD STRIKE ON APPROACH AT 4000 AGL. BIRD STRUCK FUSELAGE LEFT SIDE, FORWARD OF LEFT NOSE BAGGAGE DOOR. NOSE BAGGAGE DOOR BENT OPEN AND BIRD ENTERED BAGGAGE AREA. AIRCRAFT INSPECTED AND NOSE DOOR SECURED FOR FERRY FLIGHT TO MSP. TTAF 20485.8. TTAC 21451. 1L72 4T A8SW 19950512000071995051200007CE 1995 5 12 95ZZZX2276 119950420A5210504300431291 INTERCOSTAL BEECH 90 F90 1152909CE CABIN DOOR CRACKED A KI1AK NONE O OTHER ININSP/MAINT 1 NE03771JB3212 LA03 CABIN DOOR INTERCOSTAL FOUND CRACKED. THIS PART SUPPORTS CABIN DOOR HANDRAIL ASSY TO DOOR. SUGGEST HEAVIER GAUGE METAL IN MANUFACTURING OR ADDITIONAL STIFFNESS NEEDED. IN SINGLE SUPPORT CABLE APPLICATION, INSPECTION SHOULD BE AT EVERY 150-HOUR INSPECTION AND PLACARD CABIN DOOR FOR 'ONE PERSON AT A TIME' ON DOOR. 1L72 4T A31CE 19950512000141995051200014WP 1995 5 12 95ZZZX2283 119950224A243693902171 REGULATOR DOUG DC9 DC932 3022066WP RT GENERATOR FAILED A VJ6ACD ABORTED TAKEOFF RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 SO11523MD 47320 FLL/ATL - FLT 128 - EXPERIENCED AN ELECTRICAL MALFUNCTION WHEN THE RIGHT GENERATOR DROPPED OFF-LINE AFTER THE AIRCRAFT STARTED ITS ROLL FOR TAKEOFF. PILOT POWERED BACK AND PROCEEDED BACK TO THE GATE. CREW RESET CIRCUIT BREAKERS AND GENERATOR RESET TO NORMAL OPERATING LEVELS. 2L72 4F A6WE 19950512000151995051200015NM 1995 5 12 95ZZZX2284 119950301A6120MS3474L2255S CONNECTOR DHAV DHC8 DHC8102 2809003NM NR 2 PROPELLER DIRTY A PCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13826EX 389 ALB - NR 2 PROPELLER EXPERIENCED AN UNSCHEDULED FEATHER ON CLIMB-OUT FROM ALB. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO FIELD. REPLACED RT WING ROOT C/P 9811-J14. RESEALED PLUG AFTER INSTALLATION. GROUND RUN-UP CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ACTT, 862.36. ACTC, 961. 2H72 4T RTA13NM 19950512000211995051200021SW 1995 5 12 LOVA950120 119950120A6420222012738001 RING BELL 230 230 1182149SW T/R HUB NUT LOOSE A LOVAK NONE O OTHER ININSP/MAINT 1 NM09230LF 23017 T/R HUB NUT LOOSE. (X) 1G72 3U NCH9SW 19950512000221995051200022SW 1995 5 12 LOVA950204 119950207A672022200117109 TUBE ASSY BELL 230 230 1182149SW T/R DAMAGED A LOVAK NONE O OTHER ININSP/MAINT 1 NM09230LF578 23017 TUBE ASSY ROD END - CLEVIS END THREADS WERE DAMAGED. (X) 1G72 3U NCH9SW 19950512000231995051200023 1995 5 12 LOVA950224 419950224A3421060000130001 GYRO BELL 230 230 1182149SW COCKPIT DG MALFUNCTION A LOVAK NONE O OTHER ININSP/MAINT 1 NM09230LF613 7157 23017 HEADING FLAG FAILS TO CANCEL ON EADI DISPLAY. REPLACED DIRECTIONAL GYRO WITH SERVICEABLE UNIT. OPS CHECKS OKAY. (X) 1G72 3U NCH9SW 19950512000241995051200024EU 1995 5 12 SIMA950752 119950316A324650092361 WHEEL 5010488 SAAB SF340 SF340A 7850100EU MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW2195MQ 581 14 DEC930939 340A095 ORD - LAW SHOP WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN ORD AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS 10.5 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. PART TOTAL CYCLES 690. (X) 2L72 4T RTA52EU 19950512000251995051200025EU 1995 5 12 SIMA950841 119950325A2710S271109100000 BELLCRANK AEROSPATR42 ATR42300 8680920EU LT AILERON CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 MQT - DURING A BRIDGE INSPECTION, MAINTENANCE FOUND LEFT AILERON INBOARD BELLCRANK TO HAVE A CORRODED BEARING. BELLCRANK WAS REMOVED AND REPLACED AND FUNCTIONAL TEST OF AILERON CONTROL SYSTEM WAS SATISFACTORY IAW ATR 42 J/C 27-10-00, FUT 10005-008. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950512000261995051200026NE 1995 5 12 SIMA950991 219950409A73206066176P16 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 ENGINE MALFUNCTIONED A ASIMAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW21301AE7097 340B301 GEE785328 ORD - FLT 4351 - DURING CRUISE FLIGHT, PILOT UNABLE TO CONTROL ENGINE NR 2 TORQUE WITH POWER LEVER, TORQUE WAS FIXED AT 8046. TORQUE MOTOR LOCK-OUT NO EFFECT. FLIGHT TURNED BACK TO ORD. NR 2 ENGINE SHUT DOWN IN FLIGHT. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. RAI NR 2 HMU - IAW SAAB MM 73-00-00 AND GE CT7. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES 6797. (X) 2L72 4T4 TRTA52EU E8NE 19950512000271995051200027NE 1995 5 12 SIMA951061 219950416A7321816001002 EEC AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENGINE FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21438AT124 438 127132 SGF/DFW - FLT 3948 - ON CLIMB-OUT, RT ENGINE TORQUE BEGAN FLUCTUATING. CREW ELECTED TO RETURN TO SGF AND REQUESTED PRIORITY HANDLING FROM ATC. LANDING WAS MADE WITHOUT INCIDENT. PART TOTAL CYCLES 112. (X) 2H72 4T4 TRTA53EU E20NE 19950512000281995051200028WP 1995 5 12 95ZZZW642 119950224A5320 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05985Z 47491 STL - DURING C-CHECK, CORROSION ON AFT CARGO BIN LOWER DOOR JAMB INNER PANEL, FROM FORWARD LOWER CORNER TO AFT SIDE. REPAIRED PER SRM 53-05, FIGURE 14. 2L72 4F A6WE 19950512000291995051200029NM 1995 5 12 95ZZZW643 119950306A5320 DECK BOEING727 727231 1384079NM FS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055231166475 19830 MCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940. STOP DRILLED CRACK AND REPAIRED PER ARA 9117A. TOTAL CYCLES 45,150. 2L73 4F A3WE 19950512000301995051200030NM 1995 5 12 95ZZZW644 119950404A5330 SKIN BOEING727 727231 1384079NM FS 720-724 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055435237447 21984 MCI - DURING OP-17, FOUND CORROSION ON FUSELAGE SKIN, STATION 720 TO STATION 724, FROM FOUR INCHES LBL TO FOUR INCHES RBL. INSTALLED SKIN DOUBLER PER SRM 53-30-3, FIGURE 1. TOTAL CYCLES 24,387. 2L73 4F A3WE 19950512000311995051200031NM 1995 5 12 95ZZZW645 119950320A5330 SKIN BOEING727 727231 1384079NM FS 249 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055432962027 20307 MCI - DURING C-CHECK, FOUND .25 INCH CRACK IN SKIN FROM UNDER RIVET, STATION 249, AFT RADIUS OF R3 COCKPIT WINDOW. STOP DRILLED CRACKED AND INSTALLED DOUBLER PER ARA 9132. TOTAL CYCLES 42,060. 2L73 4F A3WE 19950512000321995051200032NM 1995 5 12 95ZZZW646 119950329A5313 STRINGER BOEING727 727231 1384079NM FS 950-960 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055435237447 21984 MCI - DURING OP-17, FOUND CORROSION AND 20 INCH CRACK IN STRINGER 29R, STATION 950 TO 960F. REPAIRED PER ARA 9145. TOTAL CYCLES 24,387. 2L73 4F A3WE 19950512000331995051200033NM 1995 5 12 95ZZZW647 119950412A27521U1110 ACTUATOR BOEING727 72722C 138400FNM NR 2 TE FLAP FAILED A ARYNAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE07427EX 19090 LOST 'A' SYSTEM HYDRAULICS INFLIGHT, LANDED IN MCI WITHOUT FURTHER INCIDENT. FOUND THE NR 2 FLAP ACTUATOR SEAL RUPTURED. REPLACED THE NR 2 FLAP ACTUATOR. 2L73 4F A3WE 19950512000341995051200034CE 1995 5 12 95ZZZW648 119950411A5753 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV2172 853 UC134 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP P/N 10116000144, REVEALED A .75 INCH CRACK IN THE LOWER SKIN ALONG THE FIFTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER APPROX 1.1 INCHES BY 4.5 INCHES. 2L72 4T RTA24CE 19950512000351995051200035CE 1995 5 12 95ZZZW649 119950425A5753 SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0797YV 11651 500 UC97 DURING SCHEDULED MAINTENANCE, A .5 INCH CRACK AT 2ND RIB FROM INBOARD END TOP OF FLAP P/N 10116000143, NEAR LEADING EDGE WAS FOUND. STOP DRILLED CRACKS AND INSTALLED DOUBLER. 2L72 4T RTA24CE 19950512000361995051200036CE 1995 5 12 95ZZZW650 119950425A575335165050259 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143AM1515 332 UC143 DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD FLAP, P/N 35165050259, HAS A 1 INCH CRACK 9.75 INCH FROM INBOARD EDGE ON TRAILING EDGE OF UPPER SKIN. STOP DRILLED AND INSTALLED DOUBLER. 2L72 4T RTA24CE 19950512000371995051200037CE 1995 5 12 95ZZZW651 119950422A5753 LE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0797YV 1414 728 UC97 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RT OUTBOARD FLAP, P/N 35165050259, REVEALED A .375 INCH CRACK NEAR LEADING EDGE AT 2ND RIB INBOARD AND A CRACK, 2 INCH ON BOTTOM BETWEEN 1ST AND 2ND RIB FROM INBOARD END AT TRAILING EDGE. CRACKS WERE STOPPED DRILLED AND DOUBLER INSTALLED. 2L72 4T RTA24CE 19950512000381995051200038CE 1995 5 12 95ZZZW652 119950416A5753 TE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07143AM5402 723 UC143 DURING SCHEDULED MAINTENANCE, A CRACK .125 INCH WAS FOUND ON RIGHT FLAP, INBOARD TRAILING EDGE, NINTH RIB INBOARD AND WAS REPAIRED WITH A 2 INCH BY 2.5 INCH DOUBLER. 2L72 4T RTA24CE 19950512000391995051200039CE 1995 5 12 95ZZZW653 119950411A575310116000143 LE SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CHAFED HOLE A AMWAK NONE O OTHER ININSP/MAINT 1 CE0797YV 11603 UC97 DURING SCHEDULED MAINTENANCE, A CHAFED HOLE APPROXIMATELY .25 INCH WAS FOUND ON THE LEADING EDGE OF LEFT INBOARD FLAP, P/N 1011600143, LOCATED 3RD RIB INBOARD FROM OUTBOARD END. REPAIRED WITH DOUBLER 2 INCHES BY 2.5 INCHES. 2L72 4T RTA24CE 19950512000401995051200040NE 1995 5 12 95ZZZW654 219950411A7200 ENGINE DOUG DC8 DC8F54 3021926WP PWA JT3D JT3D3B 52039NE NR 4 ENGINE FAILED A RRXAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP15992CF 45884 645187 FLT 114 - KDAY-KBWI - DURING CRUISE NR 4 ENGINE FAILED. N-1 DROPPED OFF THEN N-2 FROZE. LOUD BANG FROM ENGINE WHEN FAILED. RETURNED TO KDAY. MAINTENANCE INSPECTED NR 4 ENGINE AND FOUND METAL IN TAIL PIPE. AIRCRAFT BEING SET UP TO FERRY FOR ENGINE CHANGE. 2L74 4F4 F 4A25 1E8 19950512000411995051200041WP 1995 5 12 95ZZZW655 119950415A2910 HYDRAULIC LINE DOUG DC8 DC863 302198AWP MLG DAMAGED A RRXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP15797AL 46163 FLT 009 - KSJC-DAY - DURING CRUISE AT FL 330 HYDRAULIC PRESSURE FLUCTUATED ERRATICALLY FOLLOWED BY FLIGHT CONTROLS TO MANUAL REVERSION. ACCOMPLISHED HYD EMERGENCY CHECK LIST. DURING DESCENT PASSING THROUGH FL 150 PRESSURE DROPPED TO '0' AFTER 5 MINUTES. COMPLETED CHECKLIST AND MADE NORMAL LANDING. MAINTENANCE FOUND DAMAGED LINE TO BOGIE TRIM CYLINDER. REPLACED LINE. LEAK AND OPS CHECK GOOD. (W) 2L74 4F 4A25 19950512000421995051200042WP 1995 5 12 95ZZZW657 119950425A575457695832 SLOT DOOR DOUG DC8 DC862 3021970WP RT LE FLAP CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 ON 'A' CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL II CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. (W) 2L74 4F 4A25 19950512000431995051200043WP 1995 5 12 95ZZZW658 119950425A575457695831 SLOT DOOR DOUG DC8 DC862 3021970WP LT LE FLAP CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 ON 'A' CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL II CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE. 2L74 4F 4A25 19950512000441995051200044SO 1995 5 12 95ZZZW659 119950418A6120582855 VALVE HOUSING LKHEED382 382B 5264104SO NR 1 ENGINE LOOSE A SRAAK NONE P NO WARNING INDICATION DEDESCENT 1 SO19916SJ 4134 DURING DESCENT INTO RMS ON FLT ADT3, NR 1 ENGINE WOULD NOT COME UP ABOVE 97 PERCENT. FOUND HOUSING GOVERNOR ASSEMBLY LOOSE. REPLACED VALVE HOUSING, PERFORMED ENGINE RUN, OPS CHECKED GOOD. 2H74 4T A1SO 19950512000451995051200045NM 1995 5 12 MZZA95026 119950419A33501000671 EEL BOEING727 727224 1384076NM CABIN INOPERATIVE A MZZAK NONE L NO TEST ININSP/MAINT 1 WP1369742 22251 GUM - ON B-CHECK, MAINTENANCE FOUND R-1 SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (W) 2L73 4F A3WE 19950512000461995051200046NM 1995 5 12 MZZA95027 119950423A323065404676 LOCK ACTUATOR BOEING727 727224 1384076NM NOSE GEAR DIRTY A MZZAK NONE O OTHER APAPPROACH 1 WP1369741 0597 22250 FLT NR 932 - GUM - ON FINAL, GEAR HANDLE DOWN, NOSE GEAR DID NOT EXTEND. NOSE GEAR DOORS DID NOT OPEN. UNSAFE GEAR LIGHT NOSE, DID NOT HAVE ANNUNCIATOR NOSE GEAR LIGHT. RECYCLE GEAR, OPERATED NORMALLY. MAINTENANCE FOUND LEFT AND RT NOSE GEAR DOOR FORWARD FAIRING DOOR SEALS COATED WITH TAR, WHICH CAUSING DOOR TO STICK. ALSO, FOUND SEVERAL GREASE FITTINGS DRY. CLEANED DOOR AREA AND LUBED NOSE LANDING GEAR AND DOOR PER MM 12-21. PRECAUTION REPLACED NOSE GEAR LOCK ACTUATOR. 2L73 4F A3WE 19950512000471995051200047WP 1995 5 12 ORJA9526 119950414A3350 EEL DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11750RA 49777 ONE RED FLOOR TRACK LIGHT INOP IN FORWARD AND AFT CABIN, TWO WHITE LIGHTS INOP IN FIRST CLASS CABIN. REPLACED BULB AT FORWARD RED LENS, SOLDERED BROKEN WHITE LENS SOCKET WIRES, REPLACED BULB AT AFT RED LENS. (W) 2L72 4F RTA6WE 19950512000481995051200048NM 1995 5 12 USAA950377 119950411A335008163000607 EEL TRACK BOEING737 7372B7 1384560NM CABIN CRACKED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19281AU 23114 CLT - FIRST CLASS LOW LEVEL LIGHTING STRIP CRACKED. MAINTENANCE REPLACED LIGHTING TRACK. (W) 2L72 4F A16WE 19950512000491995051200049NM 1995 5 12 USAA950379 119950413A29136507506 PUMP BOEING737 737201 1384454NM 'A' HYD SYS FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19244US 22752 CLT - FLT 2126 - FLIGHT EN ROUTE BWI TO ATL WHEN 'A' SYSTEM HYDRAULICS FAILED. CREW DIVERTED FLIGHT TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGNE HYDRAULIC PUMP. REPLACED 'A' SYSTEM RETURN AND BOTH CASE DRAIN FILTERS. NO LEAKS NOTED. (W) 2L72 4F A16WE 19950512000501995051200050NM 1995 5 12 USAA950380 119950414A3020 DUCT BOEING737 737201 1384454NM RT ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19255AU 22797 BOS - FLT 2176 - NR 2 ENGINE OVERHEAT CAME ON DURING CLIMB-OUT. RETARDED THROTTLE, LIGHT WENT OUT. FLIGHT RETURNED TO BOS WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT ENGINE COWL ANTI-ICE SUPPLY DUCT BLOWN BETWEEN CROSS OVER DUCT AND COWL ANTI-ICE VALVE. REPLACED ANTI-ICE DUCT. RUN UP AND LEAK CHECK OK. (W) 2L72 4F A16WE 19950512000511995051200051NM 1995 5 12 USAA950382 119950418A2410735511A CSD BOEING737 737301 1384611NM NR 1 ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19592US 23937 PIT - FLT 1669 - AFTER TAKEOFF FROM PHL EN ROUTE TO LAS, NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY NR 1 ENGINE GENERATOR DROPPING OFF LINE. CREW DISCONNECTED NR 1 CSD AND DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT ENGINE CSD. GROUND OPS CHECKS NORMAL. 2L72 4F RTA16WE 19950512000521995051200052NM 1995 5 12 USAA950383 119950419A335020131A EEL BATTERY PACK BOEING737 737401 1384701NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19423US 23990 CLT - COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RELEASED ON MEL 33-15A. REPLACED BATTERY PACK AND REMOVED MEL. OPS CHECKED OK. (W) 2L72 4F RTA16WE 19950512000531995051200053NM 1995 5 12 USAA950384 119950419A335010126213 EEL ASSY BOEING737 737301 1384611NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19339US 23236 PIT - EMERGENCY EXIT LIGHT AT EXIT ROW INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT AT EXIT ROW. OPS CHECKS NORMAL. (W) 2L72 4F RTA16WE 19950512000541995051200054NM 1995 5 12 USAA950388 119950227A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 34 INCHES CORROSION AREA AT NUT PLATE HOLES ON BS 328 FLOOR BEAM CAP, BS 328 RBL 2 TO RBL 36. REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512000551995051200055NM 1995 5 12 WRLA95025 119950501A26122215561507 FIRE LOOP DOUG MD11 MD11 3023602NM NR 1 ENGINE LOOSE A WRLAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CRCRUISE 1 EA27280WA 48458 DURING INITIAL CRUISE, APPROXIMATELY 1.5 HOURS AFTER TAKEOFF, NR 1 ENGINE 'FIRE DETECTION' FAIL ANNUNCIATED. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. ABNORMAL PROCEDURES WERE FOLLOWED IN DUMPING FUEL TO BRING AIRCRAFT TO BELOW MLW. AIRCRAFT LANDED AT RODN WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND SEVERAL BROKEN/LOOSE CLAMPS ON BOTH 1A AND 1B PYLON FIRE LOOPS. REPOSITIONED AND RE-CLAMPED BOTH LOOPS. PERFORMED RTS TEST OF BOTH SYSTEM WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950512000561995051200056WP 1995 5 12 9507289990 119950501A5753 HINGE DOUG DC9 DC931 3022065WP NR 3 TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT WING FLAP, FORWARD HINGE NR 3 FASTENER BORES. REPAIRED PER OHM 27-50-5 AND EA X9-27-16. 2L72 4F A6WE 19950512000571995051200057WP 1995 5 12 9507299989 119950502A5720 TRAPEZOID DOUG DC9 DC931 3022065WP LEFT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LEFT TRAPEZOIDAL PANEL AT THE FIXED STRUT ATTACH POINT. REPLACED PANEL. 2L72 4F A6WE 19950512000581995051200058WP 1995 5 12 9507309886 119950502A5313 LONGERON DOUG DC9 DC951 3022051WP FS 1258-1292 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01600TR 47783 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 25R FROM FS 1258 TO 1292 AND ON ATTACH FITTING. REPLACED LONGERON AND FITTING PER SRM 51-00. 2L72 4F A6WE 19950512000591995051200059EU 1995 5 12 9507313208 119950428A5313D53231204200 LONGERON AIRBUS320 A320211 3930320EU FS 14300-14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE RIVETS COMMON TO STR 44 BETWEEN FRAMES 33 AND 34. AFTER REMOVING THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE OF THE STRINGER FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EA 32-97859. 2L72 4F RTA28NM 19950512000601995051200060WP 1995 5 12 9507329160 119950503A2163 TEMP SENSOR DOUG DC9 DC914 3022034WP RT AIR CONDITIONMALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018903E 45744 RIGHT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMBOUT AT 14,000 FEET. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HIGH TEMPERATURE SENSOR AND THERMAL CONTROL BOX. ALSO, TIGHTENED LINE AT RIGHT AUGMENTATION VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512000611995051200061WP 1995 5 12 9507339301 119950503A2150 ACM DOUG DC9 DC982 3022082WP LT/RT FAILED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01301RC 48054 SMOKE FROM AIR CONDITIONING SYSTEM ACCUMULATED IN CABIN AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT AIR CYCLE MACHINES, LEFT AND RIGHT PILOT PRESSURE REGULATORS, AND LEFT AIR CONDITIONING PRESSURE REGULATOR VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512000621995051200062WP 1995 5 12 9507349161 119950504A3260 DNLOCK SWITCH DOUG DC9 DC914 3022034WP RT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL018905E 45746 DURING CLIMBOUT FROM DTW, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED AFTER APPROXIMATELY ONE MINUTE. FLIGHT CONTINUED TO DESTINATION (IAD) AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK. 2L72 4F A6WE 19950512000631995051200063WP 1995 5 12 9507359754 119950501A2420976J2544 GEN CONTL PANEL 4071 DOUG DC9 DC941 302207NWP LEFT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01754NW39774 47178 LEFT AC GENERATOR DROPPED OFF LINE WITH ASSOCIATED CROSSTIE LOCKOUT DURING TAKEOFF ROLL AT 50 KNOTS. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED THE LEFT GENERATOR CONTROL PANEL. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512000641995051200064WP 1995 5 12 9507369751 119950501A3260 INDICATION DOUG DC9 DC941 302207NWP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01751NW 47115 DURING CLIMBOUT FROM DTW, ALL THREE LANDING GEAR RED UNSAFE LIGHTS AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO DESTINATION (CMH) AND LANDED WITHOUT INCIDENT. INSPECTED GEAR AND DOOR SWITCHES AND CONNECTORS. ALL CHECKED OK. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512000651995051200065WP 1995 5 12 ABXA9500379 119950503A32600080004003 CONNECTOR DOUG DC9 DC931 3022065WP RT MLG DIRTY A ABXAO OTHER N FALSE WARNING LDLANDING 1 GL23942AX 47552 AFTER TAKEOFF AT LBB, RIGHT RED GEAR UNSAFE LIGHT ILLUMINATED WHEN GEAR WAS RETRACTED. RECYCLED GEAR, NO HELP. FOLLOWED ABNORMAL CHECKLIST WITH GEAR HANDLE UP AND RIGHT HYDRAULIC PUMP ON HIGH, AFTER FIFTEEN MINUTES OF FLIGHT GEAR DOOR OPEN LIGHT CAME ON. AFTER ONE HOUR, GEAR DOOR OPEN LIGHT WENT OUT. RED RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RIGHT MAIN LANDING GEAR DOWNLOCK PROXIMITY SWITCH CANNON PLUG NOT FULLY SEATED AND DIRTY. RIGHT MAIN GEAR DOOR CANNON PLUG DIRTY. CLEANED CANNON PLUGS AND RETIGHTENED. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW DC-9 SUPP MM 32-60-0. REPLACED PROXIMITY CONTROL BOX. PERFORMED GEAR SWING IAW DC-9 SUPP MM 32-60-0. 2L72 4F A6WE 19950512000661995051200066WP 1995 5 12 ABXA9500380 119950503A323004415221 UP LOCK ASSY NIHON YS11 YS11A500 6310416WP LT MLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23913AX 2053 PILOT REPORTED, LEFT GEAR FAILED UP LATCH CHECK. CLEANED AND LUBED LEFT GEAR UP LATCH. GEAR RETRACTION OPS TEST CHECKED GOOD IAW YS-11 MM, CHAPTER 32-30-0. 2L72 4T A1PC 19950512000671995051200067WP 1995 5 12 ABXA9500381 119950504A5610NAS679A4 CLEARVIEW WINDOW DOUG DC9 DC933F 302207AWP RT COCKPIT LOOSE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 RIGHT CLEARVIEW WINDOW HARD TO OPEN. NUT LOOSE ON UPPER FORWARD GUIDE BLOCK. TIGHTENED NUT AS REQUIRED, CYCLED WINDOW THIRTY TIMES WITH NO BINDING NOTED AT THIS TIME IAW DC-9 MM, CHAPTER 56-10-3. 2L72 4F A6WE 19950512000681995051200068NM 1995 5 12 DHL95727001 119950504A3233651786213 ACTUATOR BOEING727 727228 NM NOSE GEAR MALFUNCTIONED A TDHLAK NONE J WARNING INDICATION APAPPROACH 1 SO01727DH 20204 ON APPROACH, AFTER MAIN GEAR LOCKS DOWN (GREEN LIGHT), NOSE GEAR IS SLOW TO LOCKDOWN. NOSE GEAR TAKES AN ADDITIONAL 9 SECONDS TO LOCK DOWN. NOSE GEAR AND DOOR LIGHTS WERE BOTH SLOW TO EXTINGUISH. REMOVED AND REPLACED NOSE GEAR ACTUATOR. NOSE GEAR EXTENDS AND RETRACTS PER MM 32-20. 2L73 4F A3WE 19950512000691995051200069NM 1995 5 12 SWAA950330 119950501A53302024T3 SKIN BOEING737 7372H4 138448CNM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 524, BETWEEN S15 AND 16L, AT BS 360 TO 420, BETWEEN S21 AND 22R, AT BS 998, BETWEEN S22 AND 23L, AT BS 931, BELOW S21R, AT BS 346, S24R, AT BS 345-360, BETWEEN S21 AND 22R, AT BS 877, S26R, AT BS 260 TO 280, BETWEEN S23 AND 24R, AT BS 967, AT S20L, AND AT BS 184, AT WL 182, RBL 22. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000701995051200070NM 1995 5 12 SWAA950331 119950501A53207075T6 CLIPS BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 380, S22L AND 21L, AT BS 787, S24R, AT BS 616, S5R AND L, AT BS 360, AT S4 AND 5L, AT BS 807, S15L, AT BS 787, S15L, AT BS 887, S15L, AT BS 520, S19L, AT BS 706, S11R, AT BS 500B, S19L, AND AT BS 807, S16L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000711995051200071NM 1995 5 12 SWAA950332 119950501A5320 SHEAR TIE BOEING737 7372H4 138448CNM BS 400 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND OUTBOARD FLANGE OF SHEAR TIE ABOVE S16R CRACKED AT LOWER FASTENER AND IN RADIUS. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000721995051200072NM 1995 5 12 SWAA950333 119950501A5210 DOUBLER BOEING737 7372H4 138448CNM FWD ENTRY DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR REPAIR DOUBLER NEEDING REWORK. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000731995051200073NM 1995 5 12 SWAA950334 119950501A5712 RIB BOEING737 7372H4 138448CNM WS 453 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND RIB UPPER FLANGE CRACKED AT LEFT WING STA 453 AT FWD STRINGER ATTACH. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000741995051200074NM 1995 5 12 SWAA950335 119950501A5313 STRINGER BOEING737 7372H4 138448CNM BS 727 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND TOOLING MARKS ON STRINGER AND SKIN DOUBLER AT BS 727B AND S7R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000751995051200075NM 1995 5 12 SWAA950336 119950501A5311 FRAME BOEING737 7372H4 138448CNM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, S16L AND FRAME SHEAR TIE CRACKED AT BS 460, RBL 6. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000761995051200076NM 1995 5 12 SWAA950337 119950501A5320 INTERCOSTAL BOEING737 7372H4 138448CNM BS 295-311 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 295-311, S4L, AND AT BS 178 TO 188, LBL 26, WL 195. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000771995051200077NM 1995 5 12 SWAA950338 119950501A531365457931 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND STRINGER GOUGED AT BS 864, S15L, AND AT BS 928 TO 935, S14R, STRINGER CRACKED AT BS 1140, 12L, AT BS 787, S10R, AT BS 1016, S7L, AT BS 907, AT S4R AND L, AT BS 467, AT S22L, STRINGER CORRODED AT BS 1138, S13L, AND AT BS 520 TO 528, WL 216, LBL 65, AT BS 897-907, S20R, AND STRINGER CHANNEL CRACKED AT BS 360, S11L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000781995051200078NM 1995 5 12 SWAA950339 119950501A532065457931 ANGLE BOEING737 7372H4 138448CNM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND Z-ANGLE CORRODED AT BS 270, WL 208, LBL 10 RBL 10. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000791995051200079NM 1995 5 12 SWAA950340 119950501A5320 SUPPORT BOEING737 7372H4 138448CNM BS 312-344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 312 TO 344, LBL 60, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000801995051200080NM 1995 5 12 SWAA950341 119950501A5320 CHORD BOEING737 7372H4 138448CNM BS 947 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FAILSAFE CHORD CRACKED AT BS 947, WL 175, LBL 4.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000811995051200081NM 1995 5 12 SWAA950342 119950501A5320651768890 MOPSILL BOEING737 7372H4 138448CNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY MOPSILL CORRODED AT BS 312 TO 344, LBL 61, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000821995051200082NM 1995 5 12 SWAA950343 119950501A5320651768890 MOPSILL BOEING737 7372H4 138448CNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FORWARD ENTRY VERTICAL FLANGE ON MOPSILL CORRODED AT BS 312, LBL 61, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000831995051200083NM 1995 5 12 SWAA950344 119950501A5311651630364 FRAME BOEING737 7372H4 138448CNM BS 202 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FRAME LOWER CHORD CRACKED AT BS 202, RBL 2 TO 6, WL 165. ALS, FRAME CRACKED AT BS 1104, 1 INCH ABOVE S5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000841995051200084NM 1995 5 12 SWAA950345 119950501A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 5, RBL 14.5, RBL 20.5, RBL 26, RBL 31, WL 207 AND 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000851995051200085NM 1995 5 12 SWAA950346 119950501A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 45 TO 63, WL 208. REPAIRED PER TRAMCO EWO 95-0258. 2L72 4F A16WE 19950512000861995051200086NM 1995 5 12 SWAA950347 119950501A5315BAC1505100617 FLOORBEAM BOEING737 7372H4 138448CNM BS 987.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 987.5, WL 208 AND WL 207, RBL 44.5 AND LBL 43.5. REPAIRED PER SWA RA 1-253-465. 2L72 4F A16WE 19950512000871995051200087NM 1995 5 12 SWAA950348 119950501A5315BAC15015531 FLOORBEAM BOEING737 7372H4 138448CNM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 616, LBL 65, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000881995051200088NM 1995 5 12 SWAA950349 119950501A5320 DOUBLER BOEING737 7372H4 138448CNM BS 1155 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME DOUBLER STRAP CRACKED AT BS 1155, WL 303, RBL 24. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000891995051200089NM 1995 5 12 SWAA950350 119950501A5311 FRAME BOEING737 7372H4 138448CNM BS 663.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT FASTENER HOLES AT S3L, 2L, 1L, 2R AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000901995051200090NM 1995 5 12 SWAA950351 119950501A5311654657563 FRAME BOEING737 7372H4 138448CNM BS 1138 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 1138, S13L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000911995051200091NM 1995 5 12 SWAA950352 119950501A5311 FRAME BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED BETWEEN S13 AND 14L, BS 727. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000921995051200092NM 1995 5 12 SWAA950353 119950501A53136561777505 STRINGER BOEING737 7372H4 138448CNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000931995051200093NM 1995 5 12 SWAA950354 119950501A5511 SPAR WEB BOEING737 7372H4 138448CNM RT HORZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR WEB CRACKED AT L/E STA 128. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000941995051200094NM 1995 5 12 SWAA950355 119950501A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CRACKS AND HOLES AT BS 727 PLUS 18, LBL 6.5 AND 7.7, WL 149, I/B AND O/B FLANGES. REPAIRED PER TRAMCO EWO 95-0274 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000951995051200095NM 1995 5 12 SWAA950356 119950501A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 727 PLUS 7 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CORRODED UNDER SKIN AT BS 727 PLUS 7, WL 149, RBL 7. REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000961995051200096NM 1995 5 12 SWAA950357 119950501A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED D-CHECK, FOUND RIGHT KEEL BEAM INBOARD FLANGE CORRODED AT BS 727 PLUS 13.3, AND OUTBOARD FLANGE AT BS 727 PLUS 17.2, RBL 7.5. REPAIRED PER TRAMCO EWO 95-0260 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950512000971995051200097NM 1995 5 12 SWAA950358 119950505A5330 SKIN BOEING737 7373Q8 1384670NM BS 747-847 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND 14 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN FROM BS 747 TO 827, BETWEEN S2 AND 3R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512000981995051200098NM 1995 5 12 SWAA950359 119950505A53206546561509 DOOR FRAME BOEING737 7373Q8 1384670NM BS 957 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND AFT GALLEY DOORWAY UPPER FORWARD FRAME SECTION CRACKED AT BS957, WL 260, RBL 60. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512000991995051200099NM 1995 5 12 SWAA950360 119950505A5320 SUPPORT BOEING737 7373Q8 1384670NM BS 947-967 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND LONGITUDINAL FLOOR SUPPORT CORRODED FROM BS 947 TO 967, LBL 41, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001001995051200100NM 1995 5 12 SWAA950361 119950505A5320654795711 STRAP BOEING737 7373Q8 1384670NM BS 787-847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND THRESHOLD TIE STRAP CORRODED FROM BS 787 TO 847, RBL 21, WL 154. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001011995051200101NM 1995 5 12 SWAA950362 119950505A5320 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 328-344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND INTERCOSTAL WEB CORROSION FROM BS 328 TO 344, RBL 27, WL 208.1. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001021995051200102NM 1995 5 12 SWAA950363 119950505A53302024T3063 SKIN BOEING737 7373Q8 1384670NM BS 500 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND 11 LIGHTNING STRIKE DAMAGE AREAS TO FUSELAGE SKIN AT BS 500 TO 500D, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001031995051200103NM 1995 5 12 SWAA950364 119950501A5320 SUPPORTS BOEING737 7373Q8 1384670NM BS 992.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 992.5, LBL 15, 20, 27, AND 43, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001041995051200104NM 1995 5 12 SWAA950365 119950501A5330 SKIN BOEING737 7373Q8 1384670NM BS 440-500 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN LIGHTNING STRIKE DAMAGE FROM BS 440 TO 500, BETWEEN S2 AND 4R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001051995051200105NM 1995 5 12 SWAA950366 119950501A5320BAC150643707516 SUPPORTS BOEING737 7373Q8 1384670NM BS 956 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND LAVATORY WALL SUPPORTS CORRODED AT BS 956, LBL 27 AND 38, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001061995051200106NM 1995 5 12 SWAA950367 119950501A53306545776 SKIN BOEING737 7373Q8 1384670NM BS 806 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 806, BETWEEN S25 AND 26R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001071995051200107NM 1995 5 12 SWAA950368 119950501A532069414372 CLIP BOEING737 7373Q8 1384670NM BS 663.7 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663.7, S10L AND R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001081995051200108NM 1995 5 12 SWAA950369 119950501A53156546812187 FLOORBEAM BOEING737 7373Q8 1384670NM BS 1007-1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FLOOR SUPPORT CORRODED FROM BS 1007 TO 1016, LBL 0, WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001091995051200109NM 1995 5 12 SWAA950370 119950501A5315 FLOORBEAM BOEING737 7373Q8 1384670NM BS 1006 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CHORD CORROSION AT BS 1006, LBL 12, WL 208. REPAIRED PER TRAMCO EWO 95-0327. 2L72 4F RTA16WE 19950512001101995051200110NM 1995 5 12 SWAA950371 119950501A5315 FLOORBEAM BOEING737 7373Q8 1384670NM BS 807 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM HAS A HOLE IN RADIUS AFT SIDE, BS 807, LBL 47.5, WL 208. REPAIRED PER TRAMCO EWO 95-0318. 2L72 4F RTA16WE 19950512001111995051200111NM 1995 5 12 SWAA950372 119950501A5320 DOOR SILL BOEING737 7373Q8 1384670NM BS 440-490 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FWD CARGO DOOR SILL WEB CORRODED AT NUTPLATE HOLES AT BS 440 TO 490, WL 156, RBL 29. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001121995051200112NM 1995 5 12 SWAA950373 119950501A5315BAC14902734 FLOORBEAM BOEING737 7373Q8 1384670NM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM NUTPLATE HOLES CORRODED AT BS 344, BL 0, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001131995051200113NM 1995 5 12 SWAA950374 119950501A5320 ANGLE BOEING737 7373Q8 1384670NM BS 536 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND UPPER DRAG ANGLE CRACKED AT BS 536, WL 172, BETWEEN S21 AND 22R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950512001141995051200114WP 1995 5 12 9507371146 119950504A7711 EPR INDICATION DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01146US 46755 686110 DURING TAKEOFF ROLL, THE NR 1 ENGINE EPR INDICATION FAILED AND THE TAKEOFF WAS ABORTED. THE EPR INDICATOR WAS REPLACED AND A GROUND RUNUP CONFIRMED PROPER SYSTEM OPERATION. 2L73 4F4 F A22WE E20EA 19950512001151995051200115NE 1995 5 12 9507389968 219950504A7532 PRBC VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE MALFUNCTIONED A NWAAED ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL019332 47264 657754 ON SINGLE ENGINE TAXI, THE NR 2 ENGINE COMPRESSOR STALLED WHEN POWER WAS INCREASED. THE ENGINE WAS SHUTDOWN, STARTED THE NR 1 ENGINE AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC VALVE. THE ENGINE WAS RUNUP AND TESTED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950512001161995051200116NM 1995 5 12 9507396603 119950508A2612 FIRE WARNING BOEING747 747151 1384891NM APU ACTIVATED A NWAAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL01603US 19780 DURING OUTBOUND TAXI, THE APU FIRE WARNING LIGHT ILLUMINATED. THE FIRE BOTTLE WAS DISCHARGED, TWO MINUTES LATER DURING RETURN TO GATE, THE FIRE WARNING LIGHT ILLUMINATED AGAIN. APU WAS INSPECTED WITH NO EVIDENCE OF FIRE FOUND AND APU WAS PLACED ON MEL. 2L74 4F A20WE 19950512001171995051200117NE 1995 5 12 9507406614 219950506A7260AS3209 PACKING BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 2 GEARBOX CUT A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01614US 20359 689565 DURING CRUISE, THE NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN, 90,000 LBS OF FUEL WAS DUMPED, AND THE AIRCRAFT DIVERTED TO ANC WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. A DAMAGED PACKING WAS REPLACED ON THE ANGLE GEARBOX TOWER SHAFT COVER. THE ENGINE AND OIL FILTER WERE INSPECTED AND A GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E20EA 19950512001181995051200118NE 1995 5 12 95UALD10042 219950505A72616451136 OIL PUMP DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP291854U 47813 517575 RETURNED TO FIELD AFTER SHUTDOWN OF NR THREE ENGINE DUE TO ZERO OIL PRESSURE. A SPLINED COUPLING BETWEEN THE TWO SCAVENGE ELEMENTS ON THE PRESSURE SIDE OF THE OIL PUMP FAILED CAUSING LOSS OF OIL PRESSURE. 2L73 4F4 F A22WE E23EA 19950512001191995051200119WP 1995 5 12 95UALD10043 119950505A2410 CSD 70730E DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 ENGINE FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP291843U 46636 RETURNED TO FIELD UNDER AMBER ALERT, DUE TO ELECTRICAL BUS AND GENERATOR PROBLEMS. REPLACED NR 2 AND 3 GENERATORS, CSD'S, GCU'S, AND BCU'S. ROOT CAUSE OF INCIDENT UNDER INVESTIGATION. NR 3 ENG CSD EXPERIENCED INTERNAL FAILURE CAUSING ITS GEN TO GO INTO INCREASING SPEED CONDITION, ENDING IN FAILURE OF CHANNELS 2 AND 3. UA RECOMMENDS UPGRADE OF GCU TO -17, TO ADD OVER FREQUENCY PROTECTION. 2L73 4F4 F A22WE E23EA 19950512001201995051200120SO 1995 5 12 COM11880 119950505A315080055711 AUDIO WARNING EMB 120 EMB120RT SO E/E BAY DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01267CA104282680 120259 AURAL TRIM WARNING DURING TAKEOFF. ELEVATOR TRIM WAS CONFIRMED TO BE IN THE TAKEOFF RANGE. REPLACED THE AURAL WARNING UNIT. 2L72 4T RTA31SO 19950512001211995051200121EU 1995 5 12 COM31072 119950504A2820AV16B2117B1 SHUTOFF VALVE SAAB SF340 SF340A 7850100EU LT WING DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01347CA22946 340A028 LEFT FUEL VALVE 'CLOSED' INDICATOR ILLUMINATED INTERMITTENTLY. REPLACED THE L/T FUEL SHUTOFF VALVE. 2L72 4T RTA52EU 19950512001221995051200122 1995 5 12 COM31073 419950505A61228210163C GOVERNOR SAAB SF340 SF340A 7850100EU LT PROP DEFECTIVE A COMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01361CA263 45 340A056 L/T PROPELLER OVERSPEED TEST FAILED TO FUNCTION. REPLACED THE OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950512001231995051200123EU 1995 5 12 COM31074 119950506A2730NAS1580C3T29D BOLT SAAB SF340 SF340A 7850100EU LT ELEVATOR BROKEN A ACOMAK NONE O OTHER ININSP/MAINT 1 SO01341CA 340A021 DURING C-CHECK INSPECTION, FOUND LEFT ELEVATOR MOST INBD COUNTER WEIGHT BOLT BROKEN. REPLACED BROKEN COUNTER WEIGHT BOLT. 2L72 4T RTA52EU 19950512001241995051200124EU 1995 5 12 COM31075 119950506A2730NAS1580C3T29D BOLT SAAB SF340 SF340A 7850100EU LT ELEVATOR BROKEN A ACOMAK NONE O OTHER ININSP/MAINT 1 SO01342CA 340A023 DURING A 24 MONTH INSPECTION, FOUND LEFT ELEVATOR MOST INBD COUNTER WEIGHT 2ND BOLT BROKEN. REPLACED BROKEN BOLT. 2L72 4T RTA52EU 19950512001251995051200125EA 1995 5 12 COM60463 119950504A325016480101 MODULE CNDAIRCL600 CL6002B19 EA NLG STEERING LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01936CA2074 7043 HYDRAULIC FLUID LEAKING FROM NLG AREA. REPLACED THE NWS SERVO. 2L72 4F RTA21EA 19950512001261995051200126EA 1995 5 12 COM60464 119950504A27604916403 SECU CNDAIRCL600 CL6002B19 EA SPOILER SYST DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01943CA243 7062 OUTBD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE NR 1 SECU. 2L72 4F RTA21EA 19950512001271995051200127NE 1995 5 12 COM60465 219950503A73146078T39P01 FUEL PUMP CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT ENGINE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01917CA4883 7017 807042 FUEL LEAKING FROM R/T ENGINE. REPLACED THE ENGINE DRIVEN FUEL PUMP. 2L72 4F4 FRTA21EA E15NE 19950512001281995051200128 1995 5 12 MWEA95195 419950505A34445224255001 ANTENNA DOUG DC9 DC914 3022034WP LOWER FUSELAGE INOP A MWEACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL31203ME 45795 ON TAKEOFF ROLL, GPWS 'PULL UP' SQUAWKED SEVERAL TIMES, CAPT REPORTED SPEED UNDER 60 KNOTS. PULLED OFF TO DEFER (34-29A) AND SILENCE GPWS COMPUTER. MAINTENANCE VERIFIED BAD RADIO ALTIMETER ANTENNA. REPLACED ANTENNA, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950512001291995051200129WP 1995 5 12 MWEA95196 119950506A2560 LANYARD DOUG DC9 DC932 3022066WP GALLEY DOOR BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 47673 DURING ROUTINE INSPECTION, THE GALLEY SERVICE DOOR SLIDE COVER LANYARD WAS FOUND BROKEN. REPLACED GALLEY SLIDE COVER LANYARD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950512001301995051200130EU 1995 5 12 QXEA9500134 119950504A3350 EEL WIRE FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09803PH 11031 GEG - CENTER SECTION FLOOR PROXIMITY LIGHTING INOP. REPAIRED BORKEN WIRE AT ROW 8 AND OPS CHECKED GOOD. 2L72 4F RTA20EU 19950512001311995051200131NM 1995 5 12 UPS203168 119950505A532069204086 INTERCOSTAL BOEING727 72725C 138400HNM BS 259-276 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND FILLER PLATE CORRODED ON 25 G-BEAM BS 259 TO 276. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-30-2, 51-10-2. 2L73 4F A3WE 19950512001321995051200132NM 1995 5 12 UPS203169 119950505A5315BAC150539042 FLOORBEAM BOEING727 72725C 138400HNM BS 277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT STA 277, WL 208, LBL 7 TO 12, RBL 4 TO 16. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-4, 51-30-2. 2L73 4F A3WE 19950512001331995051200133NM 1995 5 12 UPS203170 119950505A5320651759318 INTERCOSTAL BOEING727 72725C 138400HNM BS 259-277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 259 TO 277, WL 208, LBL 15. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-20-1, 51-10-2. 2L73 4F A3WE 19950512001341995051200134NM 1995 5 12 UPS203171 119950505A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 277 TO 294, WL 208, LBL 14. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, 51-20-1. 2L73 4F A3WE 19950512001351995051200135NM 1995 5 12 UPS203172 119950505A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 277 TO 294, WL 208, RBL 15. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, 51-20-1. 2L73 4F A3WE 19950512001361995051200136NM 1995 5 12 UPS203173 119950505A5753 TE WEDGE BOEING727 72725C 138400HNM TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 DURING 'C' CHECK, MAINTENANCE FOUND L/W O/B MID FLAP T/E WEDGE DELAMINATED AT O/B. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950512001371995051200137WP 1995 5 12 UPS803158 119950505A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 70-90 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON FINGER DOUBLER AT FS 70 TO 90, LONGERON 21R. REPLACED DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19950512001381995051200138WP 1995 5 12 UPS803159 119950505A524047761241 FITTING DOUG DC8 DC871F 302199DWP AFT SERVICE DOORCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND AFT SERVICE DOOR CORRODED FITTING AT TOP FWD HINGE. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950512001391995051200139WP 1995 5 12 UPS803160 119950505A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 12-8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND FLIGHT DECK FASTENERS SHEARED DUE TO CORROSION ON DOUBLER AT FS 12 TO 8, L/T O/B SIDE. REPLACED DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950512001401995051200140WP 1995 5 12 UPS803161 119950505A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 1720-1760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON SKIN DOUBLER AT FS 1720 TO 1760, LONGERON 28L. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1, 51-1-21. 2L74 4F RT4A25 19950512001411995051200141WP 1995 5 12 UPS803162 119950505A5313602493 LONGERON DOUG DC8 DC871F 302199DWP FS 1746 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32L AT FS 1746. REPLACED LONGERON PER SRM 51-1-20D. 2L74 4F RT4A25 19950512001421995051200142WP 1995 5 12 UPS803164 119950505A532047723981 FITTING DOUG DC8 DC871F 302199DWP FS 1760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND LONGERON END FITTING 32R CORRODED AT FS 1760. REPLACED FITTING PER SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 19950512001431995051200143WP 1995 5 12 UPS803165 119950505A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 1360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 DURING 'S2' CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT FS 1360, LONGERON 25L TO 26L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-1. 2L74 4F RT4A25 19950512001441995051200144WP 1995 5 12 UPS803166 119950505A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS 220-400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 DURING 'C' CHECK, MAINTENANCE FOUND INNER DOUBLER CORRODED AT FS 220 TO 400, LONGERONS 35L TO 31R. REPLACED DOUBLERS PER DOUGLAS DRAWING NR 5755271, 9755878. 2L74 4F RT4A25 19950512001451995051200145WP 1995 5 12 UPS803167 119950505A53205755271 DOUBLER DOUG DC8 DC873F 302199FWP FS 190-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 DURING 'C' CHECK, MAINTENANCE FOUND SKIN CORRODED AT FS 190 TO 450. REPLACED SKIN PANEL PER DOUGLAS DRAWING NR 5755271. 2L74 4F RT4A25 19950512001461995051200146WP 1995 5 12 UPS803174 119950506A33505708458503 EEL DOUG DC8 DC873F 302199FWP FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01803UP 46073 ON PREFLIGHT CHECK, FLIGHT CREW FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK OK. 2L74 4F RT4A25 19950512001471995051200147WP 1995 5 12 UPS803175 119950505A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 81 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 (SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND TWO CRACKS APPROX 1.5 INCHES LONG EACH AT STA 81, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACKS, INSTALLED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950512001481995051200148WP 1995 5 12 UPS803176 119950505A5330 SKIN DOUG DC8 DC873F 302199FWP BS 182 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 (SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND ONE CRACK APPROX 2 INCHES LONG AT STA 182, LONGERON 33. NOTE: CORROSION PRESENT. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950512001491995051200149WP 1995 5 12 UPS803177 119950505A5330 SKIN DOUG DC8 DC873F 302199FWP FWD OF LT MLG DRCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 (SUPPLEMENTAL MRR) DURING DAILY CHECK, MAINTENANCE FOUND CRACK JUST FWD OF LT MLG DOOR. REMOVED FASTENERS, STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 51-1-20. 2L74 4F RT4A25 19950512001951995051200195NM 1995 5 12 95ZZZW660 119950325A2752 ACTUATOR BOEING727 7272Q8 138407WNM NR 2 SLAT FAILED A AMTAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL11776AT 21608 IND - FLT 209 - NR 2 SLAT WOULD NOT RETRACT. REPLACED NR 2 FAILED SLAT ACTUATOR, AS IN MM 27-81-32. OPS CHECKS GOOD. LEAK CHECK OK. 2L73 4F A3WE 19950512001961995051200196WP 1995 5 12 95ZZZW661 119950322A57545719014 SLOT DOOR DOUG DC8 DC873 302199CWP LT TE FLAP PUNCTURED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURING C-CHECK, FOUND LEFT INBOARD SLOT DOOR UPON SURFACE PUNCUTURED. REPAIRED PER DSRM 57-02-01 FIG 2A. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512001971995051200197WP 1995 5 12 95ZZZW662 119950322A532037558471 CORNER FITTING DOUG DC8 DC873 302199CWP NR 3 LOWER DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURING C-CHECK, NR 3 LOWER CARGO DOOR LOWER CORNER FITTINGS FOUND CRACKED. REPLACED FITTINGS. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512001981995051200198WP 1995 5 12 95ZZZW663 119950322A5330 SKIN DOUG DC8 DC873 302199CWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURING C-CHECK, FOUND NR 3 LOWER CARGO DOOR CUTOUT SKIN CRACKED FORWARD EDGE. REPAIRED PER DER DWG NR 239755124 DATED 3/14. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512001991995051200199WP 1995 5 12 95ZZZW664 119950322A57425753054502 PYLON FITTING DOUG DC8 DC873 302199CWP NR 3 ENGINE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURING C-CHECK, NR 3 ENGINE PYLON SUPPORT FITTING FOUND CRACKED AT LOWER INBOARD RADIUS. REPLACED FITTING. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512002001995051200200WP 1995 5 12 95ZZZW665 119950322A57445751102392N SUPPORT FITTING DOUG DC8 DC873 302199CWP RT INBD FLAP CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURINK C-CHECK, RT INBOARD FLAP INBOARD SUPPORT FITTING FOUND CRACKED. REPLACED FITTING. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512002011995051200201WP 1995 5 12 95ZZZW666 119950322A574357500922 SUPPORT MLG DOUG DC8 DC873 302199CWP RT MLG CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01802DH64780 46076 DURING C-CHECK, FOUND RT MLG SUPPORT FITTING CRACKED. REPAIRED FITTING PER DOUGLAS S/B 53-61. TOTAL CYCLES 25,289. 2L74 4F RT4A25 19950512002021995051200202EU 1995 5 12 95ZZZW667 119950413A2611FR3222 SMOKE DETECTOR AEROSPATR42 ATR42300 8680920EU BAGGAGE COMPT FAILED A NVEAO OTHER N FALSE WARNING CRCRUISE 1 SO03310DK 310 FLT 5770 - MIA - CREW REPORTS AFT BAGGAGE SMOKE DETECTOR WARNING ILLUMINATED IN FLIGHT. NO SMOKE OF FIRE FOUND. FALSE WARNING, REPLACED DETECTOR. 2H72 4T RTA53EU 19950512002031995051200203NE 1995 5 12 95ZZZW668 219950412A7200 ENGINE BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101650B1 41560NE NR 2 MALFUNCTIONED A NVEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO03214AE 7206 FLT NR 4917 - LGA - NR 2 TAIL PIPE HOT LIGHT CAME ON AT ABOUT 200 AGL THE CREW FOLLOWED QRH AND SHUT AFFECTED ENGINE DOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED FOR DAMAGE AND NONE WAS NOTED. THE AIRCRAFT WAS GROUND RAN AND PROBLEM COULD NOT BE DUPLICATED AND THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 1G72 3U3 U H13EU E5NE 19950512002041995051200204NM 1995 5 12 AWXA9500240 119950422A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, SEVERAL AREAS OF EMERGENCY EXIT LIGHTS FAILED TEST. FLOOR MOUNTED LIGHTS BETWEEN ROWS 18 AND 24, AND BOTH FLOOR AND OVERHEAD LIGHTS BETWEEN ROWS 27 AND 32. REPAIRED WIRES, OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950512002051995051200205WP 1995 5 12 CKSA95018 119950411A2612W89G18 WIRE DOUG DC8 DC863F 302198FWP NR 1 ENGINE BARE A CKSAO OTHER N FALSE WARNING APAPPROACH 1 GL23867BX 46049 KTOL - ON SHORT FINAL NR 1 ENGINE FIRE WARNING CAME ON MOMENTARILY. REPAIRED BARE WIRE NEAR FIRE LOOP PLUG, CHECKS OK IAW MM CHAPTER 26. (W) 2L74 4F 4A25 19950512002061995051200206NM 1995 5 12 USAA950389 119950307A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 727-740 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION ON FLOOR BEAM AT SCREW HOLES 30 PERCENT LOSS, BS 727 TO BS 740 RBL 13. REPAIRED PER SRM 53-00-53 FIG 202. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002071995051200207NM 1995 5 12 USAA950390 119950308A5320 ANGLE BOEING737 7373B7 1384580NM BS 986.5-1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH CORROSION 30 PERCENT LOSS, BS 986.5 TO BS 1006, ANGLE AT LEFT AFT BLUE ROOM DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002081995051200208NM 1995 5 12 USAA950391 119950308A532069761482 FLOOR WEB BOEING737 7373B7 1384580NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH SPOT, 3 INCH BY 6 INCH SPOT, 10 INCHES BY 12 INCHES SPOTS OF CORROSION TASK NR C53-107-02, CORRSOSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002091995051200209NM 1995 5 12 USAA950392 119950309A5320 T-CAP BOEING737 7373B7 1384580NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON T-CAP AT BS 986.5. REPAIRED PER TR 53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002101995051200210NM 1995 5 12 USAA950393 119950308A5320 HAT CHANNEL BOEING737 7373B7 1384580NM BS 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON HAT CHANNEL BS 996 RBL 18 INCHES TO DOOR FRAME. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-0, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002111995051200211NM 1995 5 12 USAA950394 119950323A532065C105925 INTERCOSTAL BOEING737 7373B7 1384580NM BS 957 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK, VISUAL INSPECTION, FOUND 2 INCH BY 12 INCH CORRODED AREA ON INTERCOSTAL AT BS 957 RBL 18 INCHES TO RBL 45 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002121995051200212NM 1995 5 12 USAA950395 119950323A5240 ANGLE BOEING737 7373B7 1384580NM SERVICE DOOR CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK, VISUAL INSPECTION FOUND 2 INCHES BY 40 INCHES CORRODED AREA, AFT SERVICE DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002131995051200213NM 1995 5 12 USAA950396 119950323A532065C10592906 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT BS 947 TO BS 967 RBL 45 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002141995051200214NM 1995 5 12 USAA950397 119950302A5320 'T' CAP BOEING737 7373B7 1384580NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH NUTPLATE HOLES CORRODED, BS 967 RBL 0 TO RBL 50 INCHES. REPAIRED PER SRM 53-00-51, FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002151995051200215NM 1995 5 12 USAA950398 119950323A53301128323 SKIN BOEING737 7373B7 1384580NM BS 804 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURNG Q-4 CHECK VISUAL INSPECTION, FOUND 16 INCH BY 8 INCH AREA OF SPOTS CORROSION ON DOOR SILL WEB SKIN, BS 804 AT AFT CARGO DOOR SILL AREA. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002161995051200216NM 1995 5 12 USAA950399 119950308A5320 'T' CAP BOEING737 7373B7 1384580NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION THE ENTIRE LENGTH OF BEAM 25 PERCENT TO 40 PERCENT LOSS, BS 1016 LEFT END TO RIGHT END. REPAIRED PER SRM 53-00-51 FIG 202. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002171995051200217NM 1995 5 12 USAA950400 119950308A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 967-987 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION INTERCOSTAL, BS 967 - BS 987 RBL 22 INCH. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-0. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002181995051200218NM 1995 5 12 USAA950401 119950302A53206546812170 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19395US27150 23317 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH BY 30 PERCENT LOSS OF METAL, BS 947 TO 967 RBL 24. REPAIRED PER SRM 51-10-2. CORRSOSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950512002191995051200219NM 1995 5 12 DL72L951728 119950419A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, FLOORBEAM STA 1166 LBL 47 WITH CORROSION DAMAGE. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950512002201995051200220NM 1995 5 12 DL72L951729 119950419A5320 INTERCOASTAL BOEING727 727232 1384082NM BS 680 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, CORROSION ON LWR LEG OF INTERCOSTAL AFT OF STA 680 I/B OF STR 26R. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950512002211995051200221NM 1995 5 12 DL72L951730 119950417A5754 RIB BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, (1) .25 INCH VISIBLE CRACK ON NR 5 SLAT L/E RIB O/B OF ACTUATOR ROD. (2) 2.0625 INCH CRACKS ON NR 5 SLAT L/E RIB I/B OF ACTUATOR ROD. REPAIRED PER M/M 57-54-0 PAR 3. 2L73 4F A3WE 19950512002221995051200222NM 1995 5 12 DL72L951734 119950417A5753 FOREFLAP BOEING727 727232 1384082NM NR 4 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, 1 INCH CRACK ON NR 4 FOREFLAP ABOVE NR 7 FLAPTRACK. REPAIRED AS PER SRM 57-50-4. 2L73 4F A3WE 19950512002231995051200223NM 1995 5 12 DL72L951735 119950417A5753 FOREFLAP BOEING727 727232 1384082NM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, 1 INCH CRACK ON NR 3 FOREFLAP ABOVE NR 6 FLAPTRACK CARRIAGE. REPAIRED AS PER SRM 57-50-4. 2L73 4F A3WE 19950512002241995051200224NM 1995 5 12 DL72L951736 119950417A5320 FLANGE BOEING727 727232 1384082NM BS 1342.4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 000043 FOUND ON CV2 CHECK, CRACKED FLANGE STA 1342.4 WHERE LOWER EDGE OF FWD COWLS MATES WITH FUSELAGE AT PREVIOUS REPAIR (6 O'CLOCK POSITION). REPAIRED PER M/M 53-11-0 PG 801 IDENTIFY REPAIR AS PERMANENT REPAIR PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950512002251995051200225NM 1995 5 12 DL72L951767 119950419A5313 STRINGER BOEING727 727232 1384082NM BS 1148/1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 019565 FOUND ON CV2 CHECK, CORROSION ON TOP OF STR 30 BETWEEN STA 1148 AND 1166 BL 0. REPAIRED AS PER SRM 53-10-3 AND ID PER PS 900-5-1 FIG 4. 2L73 4F A3WE 19950512002261995051200226NM 1995 5 12 DL72L951768 119950426A5330 SKIN BOEING727 727232 1384082NM BS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 019565 FOUND ON CV2 CHECK, CORROSION ON SKIN FOUND UPON REMOVAL OF STR SPLICE ON STA 1010 REF N/R 127. REPAIRED SKIN PER SRM 53-30-3 FIG 3A AND ID PER PS 900-5-1 FIG 4. 2L73 4F A3WE 19950512002271995051200227NM 1995 5 12 DL72L951774 119950417A5754 BRACKET BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 019565 FOUND ON CV2 CK, .5 INCH VISIBLE CRACK ON NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET IN LOWER RADIUS. REPAIRED PER M/M 57-20-21 PAR 12. 2L73 4F A3WE 19950512002281995051200228NM 1995 5 12 DL72S951542 119950410A57536521631274A SKIN BOEING727 727232 1384082NM NR 4 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11527DA 21587 49810 DURING SHOP INSPECTION, RT WING NR 4 FOREFLAP WAS FOUND WITH CRACKED SKIN AT BOTH TRACK CUTOUT PANS ON L/E. REPAIRED PER MM 57-50-4. 2L73 4F A3WE 19950512002291995051200229NM 1995 5 12 DL72S951569 119950416A5230 SKIN BOEING727 727232 1384082NM FWD BAGG DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 49810 DURING INSPECTION, THE FWD CARGO DOOR WAS FOUND WITH A .5 INCH CRACK IN THE OUTER SKIN. REPAIRED PER SRM 52-00-3. 2L73 4F A3WE 19950512002301995051200230NM 1995 5 12 DL72S951621 119950420A5753652163262 FITTING BOEING727 727232 1384082NM NR 3 MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 000008 NR 3 MID FLAP I/B CARRIAGE FITTING UPPER THRUST BEARING RETAINER BOLT AND HOLES HAVE CORROSION. FOUND AT SHOP INSPECTION. REAM HOLES TO .312 AND INSTALLED BUSHING. 2L73 4F A3WE 19950512002311995051200231NM 1995 5 12 DL72S951658 119950423A5330 SKIN BOEING727 727232 1384082NM BS 305 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11522DA 21582 000008 DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CRACKED AT RIVET ON FIGHT SIDE OF AIRCRAFT AT FS 305 WL 208. CRACK WAS .25 INCH LONG ON BOTH SIDES OF RIVET. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950512002321995051200232NM 1995 5 12 DL72S951684 119950425A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 000008 DURING SHOP INSPECTION, LEFT WING AILERON WAS FOUND WITH DAMAGE TO UPPER SKIN. SPLICED IN NEW SECTION OF SKIN PER SRM 57-50-1. 2L73 4F A3WE 19950512002331995051200233NM 1995 5 12 DL72S951685 119950425A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 000008 DURING INSPECTION, LEFT WING AILERON WAS FOUND WITH WEAR DAMAGE TO THE LOWER SKIN. REPAIRED PER SRM 57-51-0. 2L73 4F A3WE 19950512002341995051200234NM 1995 5 12 DL72S951718 119950425A7110 SKIN BOEING727 727232 1384082NM NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 000043 NR 2 ENG INLET HOUSING OUTER SKIN CRACKED .375 INCH AT ROUND ACCESS PANEL JUST ABOVE VERT STAB FWD SPAR. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 54-30-0 PG 803. 2L73 4F A3WE 19950512002351995051200235NM 1995 5 12 DL72S951719 119950425A5522 SKIN BOEING727 727232 1384082NM LT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 000043 L/T ELEV UPPER SKIN HAS 1 IN BY .5 INCH HOLE I/B END, 1 FT FWD OF TRAILING EDGE. FOUND AT F-1 LETTER CHECK. REPAIRED PER SRM 55-22-3 FIG 5. 2L73 4F A3WE 19950512002361995051200236NM 1995 5 12 DL72S951756 119950418A5311651633925 FRAME BOEING727 727232 1384082NM BS 970 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 THE BS 970 FRAME IS CRACKED JUST O/B OF STR 27L. THE CRACK RUNS FROM THE AFT FREE FLANGE, ACROSS THE UPPER FLANGE AND DOWN TO A FASTENER HOLE COMMON TO THE FAILSAFE CHORD. DAMAGE FOUND AT HMV, AND REPAIRED PER DL ERA 301580-14AD. 2L73 4F A3WE 19950512002371995051200237NM 1995 5 12 DL72S951758 119950409A5320 SUPPORT BOEING727 727232 1384082NM BS 700-720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND CENTER FLOOR SUPPORT CORRODED BETWEEN STA 700 TO 720 IN FWD B/B. REMOVED DAMAGE, REPAIRED PER SRM 53-10-5. 2L73 4F A3WE 19950512002381995051200238NM 1995 5 12 DL72S951759 119950410A5330 SKIN BOEING727 727232 1384082NM BS 1343 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND EXTERIOR SKIN GOUGED AT STR 20R, STA 1343. REMOVED DAMAGE, REPAIRED PER SRM 54-30-3 FIG 7. 2L73 4F A3WE 19950512002391995051200239NM 1995 5 12 DL72S951760 119950410A5320 FORMER BOEING727 727232 1384082NM FS 560 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND FS 560 FORMER UPPER RAIL BENT/DAMAGED ABOVE STR 25L TO STR 24L. REMOVED DAMAGE, REPAIRED PER SRM 53-10-4 PG 107. 2L73 4F A3WE 19950512002401995051200240NM 1995 5 12 DL72S951762 119950422A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND STRINGER CRACKED AT STR 3 LEFT RIB NR 4 INSIDE VERTICAL STAB. REPAIRED PER M/M 55-30-0 PG 803. 2L73 4F A3WE 19950512002411995051200241NM 1995 5 12 DL72S951764 119950410A5530 WEB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND STA 1303 WEB CRACKED IN LOWER LT CORNER, INSIDE VERT STAB. REPAIRED PER M/M 53-11-0 PG 856. 2L73 4F A3WE 19950512002421995051200242NM 1995 5 12 DL72S951765 119950410A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 000043 DURING HMV, FOUND STRINGER CRACKED AT VERT STAB INTERIOR STR 7L, CRACKED LOC 3RD BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-0 PG 803. 2L73 4F A3WE 19950512002431995051200243NM 1995 5 12 DL72S951785 119950323A57536521634149K SKIN BOEING727 727232 1384082NM NR 2 TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11404DA 21148 019565 NR 2 AFT FLAP, UPPER L/E SKIN WORN AT I/B END. REPAIRED PER SRM 575004, MFG'D AND INSTALLED FILLER AND DOUBLER. 2L73 4F A3WE 19950512002441995051200244NM 1995 5 12 DL72W951476 119950331A5522 ELEVATOR BOEING727 727247 138408FNM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND RT ELEVATOR LOWER SKIN WITH DAMAGED SKIN AT FASTENER HOLE AT FOURTH ACCESS PANEL FROM O/B END. ELEVATOR WAS SENT TO SHOP FOR REPAIRS. 2L73 4F A3WE 19950512002451995051200245NM 1995 5 12 DL72W951531 119950411A5754 SKIN BOEING727 727247 138408FNM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 AT HMV, FOUND RT WING NR 5 L/E SLAT WITH CRACKS IN THE SKIN AT WING FENCE ATTACH HOLE. REPAIRED PER MM 57-54-0 PG 817. 2L73 4F A3WE 19950512002461995051200246NM 1995 5 12 DL72W951592 119950418A52606519809242 STAIR BOEING727 727247 138408FNM AFT AIR STAIR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 000008 DURING SHOP INSP, A HOLE IN STR (CTR CHANNEL) 1.5 INCHES FROM THE AFT END WAS FOUND IN AFT AIRSTAIR ASSEMBLY. REPAIRED PER SRM 53-10-8 FIG 1. 2L73 4F A3WE 19950512002471995051200247NM 1995 5 12 DL72W951721 119950328A57536521631273 SKIN BOEING727 727247 138408FNM NR 2 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000043 ON INITIAL SHOP INSPECTION, MAINTENANCE FOUND A CRACK ON LEADING EDGE SKIN AT CLEARENCE CUTOUT APPROX 47 INCHES FROM OUTBOARD END. REPAIRED DAMAGED AREA PER SRM 57-50-4 FOR L/WING NR 2 FOREFLAP. 2L73 4F A3WE 19950512002481995051200248NM 1995 5 12 DL72W951742 119950420A5754651622296 ANGLE BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 RIB NR 7 CRACKED AT LWR ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT DURING SHOP INSPECTION. 2L73 4F A3WE 19950512002491995051200249NM 1995 5 12 DL72W951743 119950420A5754651622296 ANGLE BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 LOWER ANGLE CRACKED AT RIB NR 7 LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 805A, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950512002501995051200250NM 1995 5 12 DL72W951744 119950420A5754651622296 ANGLE BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 RIB NR 11 CRACKED AT LOWER ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950512002511995051200251NM 1995 5 12 DL72W951745 119950420A5754651622296 RIB BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 DOUBLER FOR I/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950512002521995051200252NM 1995 5 12 DL72W951746 119950420A5754651622296 RIB BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 DOUBLER FOR O/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950512002531995051200253NM 1995 5 12 DL72W951750 119950420A5754651622296 RIB BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 000043 NR 13 RIB CRACKED AT LOWER ANGLE LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND AT SHOP INSPECTION. 2L73 4F A3WE 19950512002541995051200254NM 1995 5 12 DL72W951753 119950329A5753652163396 FITTING BOEING727 727247 138408FNM NR 4 TE FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000043 NR 4 MID FLAP, O/B CARRIAGE SUPPORT FITTING UPPER I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. ALSO, I/B SUPPORT FITTING HAS LOWER I/B THRUST BEARING BOLT HOLE CORRODED. REPAIRED PER SRM 57-50-04 PG33. REAMED OVERSIZE AND INSTALLED BUSHINGS. FOUND AND REPAIRED DURING HMV SHOP INSPECTION. 2L73 4F A3WE 19950512002551995051200255NM 1995 5 12 DL72W951754 119950329A5753652163396 FITTING BOEING727 727247 138408FNM RT TE FLAP PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 000043 NR 4 MID FLAP, O/B THRUST BEARING BORE PITTED. REPAIRED PER SRM 57-50-04 PG 37. OVERSIZED BORE AND INSTALLED BUSHING. FOUND AND REPAIRED AT HMV, SHOP INSPECTION. 2L73 4F A3WE 19950512002561995051200256NM 1995 5 12 DL757951533 119950412A5330 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11633DL 23614 49810 FOUND DURING LETTER CHECK, 2 LIGHTNING STRIKES 1 PREVIOUSLY PAINTED OVER UPPER FUS CROWN AREA 6 FEET FWD VERT STAB. REPAIRED PER SRM 53-00-01. TIME LIMITED REP MUST BE REINSPECTED PRIOR TO 2,500 CYCLES AND REPLACED PRIOR TO 12,OOO CYCLES, E/C INSPD OK AT THIS TIME. 2L72 4F RTA2NM 19950512002571995051200257NM 1995 5 12 DL757951576 119950327A5754 SKIN 114N4005177ABOEING757 757232 1384965NM LT LE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11602DL 000008 22809 49810 DURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH SKIN DELAMINATED AT THE INBOARD EDGE UNDER DOUBLER. REPAIRED PER SRM 51-70-10. 2L72 4F RTA2NM 19950512002581995051200258NM 1995 5 12 DL757951607 119950418A5320 CHANNEL BOEING757 757232 1384965NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11608DA 22815 000008 FOUND DURING LETTER CHECK, DOOR CHANNEL HAS HOLE 12 INCHES AFT OF AFT DOOR CORNER, AFT B/B. REMOVED DAMAGE AND MFG DOUBLER PER SRM 51-70-11, INSTALLED DOUBLER PER SRM 51-70-11. 2L72 4F RTA2NM 19950512002591995051200259NM 1995 5 12 DL757951683 119950421A5330 SKIN BOEING757 757232 1384965NM BS 1330 HOLE A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 000008 AT HMV, BELLY SKIN AT FS 1330 HAS PUNCTURE DAMAGE AT FUSELAGE STATION 1330 ABOVE STRINGER 25L. REPAIRED PER SRM 53-00-01 FIG 208. 2L72 4F RTA2NM 19950512002601995051200260NM 1995 5 12 DL757951726 119950417A5754114N4005177A WEDGE BOEING757 757232 1384965NM NR 4 LE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 000043 LOWER AFT EDGE IS WORN ON NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 REF AD 90-23-06. FOUND AND REPAIRED DURING HMV. 2L72 4F RTA2NM 19950512002611995051200261NM 1995 5 12 DL757951727 119950421A5330 SKIN BOEING757 757232 1384965NM FS 1595 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 000043 AT HMV, FOUND LOWER FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 1595 BETWEEN STRINGERS 24L AND 23L. REPAIRED PER SRM 53-00-01 PG 212-214. 2L72 4F RTA2NM 19950512002621995051200262NM 1995 5 12 DL757951739 119950421A5247148N666016 DOOR BOEING757 757232 1384965NM APU ACCESS DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 000043 DURING HMV VISIT IN ATLANTA, HANGAR INSPECTION FOUND THAT THE APU ACCESS DOOR HAD A DENT IN THE OUTER SKIN. THE SKIN WAS REPAIRED PER SRM 52-40-01. 2L72 4F RTA2NM 19950512002631995051200263NM 1995 5 12 DL757951740 119950421A5247148N666016 DOOR BOEING757 757232 1384965NM APU ACCESS DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 000043 DURING HMV VISIT, HANGAR INSPECTION FOUND THAT THE OUTER SKIN WAS DENTED JUST FORWARD OF CENTER LATCH. THE DENT WAS REPAIRED PER SRM 52-40-01. 2L72 4F RTA2NM 19950512002641995051200264NM 1995 5 12 DL757951757 119950420A5754114N300219 TE WEDGE BOEING757 757232 1384965NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11604DL 22811 000043 THE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 5 L/E SLAT IS DELAMINATED AT ISS 109.00. THE DELAMINATION MEASURES 1 INCH ALONG THE EDGE OF THE PANEL AND PROGRESSES 0.25 INCH FORWARD FROM THE EDGE OF THE PANEL. DAMAGE FOUND AT LETTER CHECK, REPAIRS WERE ACCOMPLISHED PER DL ERA 301604-14AD. 2L72 4F RTA2NM 19950512002651995051200265NM 1995 5 12 DL757951773 119950423A5315 FLOORBEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 019565 AT HMV FOUND FLOORBEAM CORRODED, FS 324 BETWEEN RBL 16 AND RBL 64. REMOVED DAMAGED SECTION OF CHORD, FABRICATED REPAIR PARTS PER SRM 53-10-08 FIG 201. INSTALLED T-CAP SECTION PER SRM 53-10-08 FIG 201. 2L72 4F RTA2NM 19950512002661995051200266NM 1995 5 12 DL767951722 119950425A5753 LE SKIN BOEING767 767232 1385132NM NR 1 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11109DL 22221 000043 FOUND DURING LETTER CHECK NR 1 FLAP DAMAGE AT L/E JUST AFT OF NR 1 FLAP FAIRING. REPAIRED PER SRM 57-53-01 PAINTED AREA LT WING. 2L72 4F RTA1NM 19950512002671995051200267NM 1995 5 12 DL767951724 119950425A5753 TE WEDGE BOEING767 767232 1385132NM NR 1 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11109DL 22221 000043 FOUND DURING LETTER CHECK NR 1 FLAP DAMAGED 2 PLACES AT T/E EDGE LOWER SURFACE I/B OF NR 1 FLAP FAIRING. REPAIRED PER SRM 57-53-01, PAINTED AREA LT WING. 2L72 4F RTA1NM 19950512002681995051200268NM 1995 5 12 DL767951725 119950425A5753 CORNER BOEING767 767232 1385132NM NR 1 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11109DL 22221 000043 FOUND DURING LETTER CHECK, NR 1 FLAP UPPER INBD CORNER DAMAGED. REPAIRED PER SRM 57-53-01 PAINTED AREA LT WING. 2L72 4F RTA1NM 19950512002691995051200269WP 1995 5 12 DLL10951723 119950409A53201514674105 SUPPORT LKHEED1011 10113851 5265010WP FS 253 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 DURING OVERHAUL INITIAL INSPECTION, THE FWD LT LAV DOORWAY THRESHOLD HAT CHANNEL WAS FOUND CORRODED. REPLACED HAT CHANNEL WITH STAINLESS STEEL HAT PER SRM 53-21-00 FIG 826. 2L73 4F A23WE 19950512002701995051200270WP 1995 5 12 DLL10951747 119950419A5743 FITTING LKHEED1011 10113851 5265010WP MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 MLG FITTING, CORROSION HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. REAMED HOLES 17 THROUGH 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVED PER SRM 51-14-00 HFEC. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED FITTING. 2L73 4F A23WE 19950512002711995051200271WP 1995 5 12 DLL10951751 119950419A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 LT MLG FITTING HOLES 1 THROUGH 6 COMMON TO WING AT RETRACT FITTING ATTACH AREA ARE CORRODED. REMOVED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. CORROSION REMOVED PER 54-14-00 HFEC PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED. 2L73 4F A23WE 19950512002721995051200272WP 1995 5 12 DLL10951752 119950419A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 LT MLG FITTING CORRODED ON UPPER SURFACE OF LWR RETRACT ACT ATTACHMENT. REMOVED CORROSION BY LOCAL BLEND, .020 DEEP. REMOVED CORROSION PER SRM 57-14-00, HFEC PER SRM 54-14-00 PG 809. ROTO PEENED PER SRM 57-14-00 PG 809. CAD PLATE PER PS 900-3-9, PRIMED AND PAINTED. 2L73 4F A23WE 19950512002731995051200273WP 1995 5 12 DLL10951769 119950406A5330 TEAR STRAP LKHEED1011 10113851 5265010WP BS 1575 BULGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 TEAR STRAP BULGED STA 1575 BETWEEN STR 39 TO 40. REMOVED CORROSION UNDER TEAR STRAP. CHECKED LIMITS PER SRM 53-31-00 FIG 801, LIMITS CHECKED OK. TREATED AND PAINTED PER PS 900-3-6 AND FABRICATED SPLICE DOUBLER PER SRM 53-31-00. 2L73 4F A23WE 19950512002741995051200274WP 1995 5 12 DLL10951770 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUSELAGE FAIL-SAFE IS DISBONDED FS 901 IN BETWEEN STR 29 TO 28. REMOVED GLUE AND LIGHT SURFACE CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED AND PAINTED PER PS 900-3-6. INSTALLED REPAIR PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950512002751995051200275WP 1995 5 12 DLL10951771 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 923 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF 923 IN BETWEEN STR 39 TO 40. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER 900-3-6. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950512002761995051200276WP 1995 5 12 DLL10951772 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 923 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 40 TO 41. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER PS 900-3-6, REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950512002771995051200277WP 1995 5 12 DLL10951775 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FR 923 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 41 TO 42. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 AND PAINTED PS 900-3-6. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950512002781995051200278WP 1995 5 12 DLL10951776 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 923 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 42 TO 43. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950512002791995051200279WP 1995 5 12 DLL10951777 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 923 CORROSION A DALAK NONE K FLUID LOSS ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 923 IN BETWEEN STR 43 TO 44. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1 PAINTED PER PS 900-3-6, REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950512002801995051200280WP 1995 5 12 DLL10951778 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 901 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 BETWEEN STR 40 TO 41. REMOVED GLUE AND LIGHT CORROSION UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER 900-3-6, REINSTALLED STRAP PER SRM 53-31-00. 2L73 4F A23WE 19950512002811995051200281WP 1995 5 12 DLL10951779 119950409A5320 THRESHOLD LKHEED1011 10113851 5265010WP L 1 DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L-1 DOOR INNER LWR THRESHOLD PLATE HAS CORROSION IN SEVERAL PLACES. REMOVED CORROSION, WITHIN LIMITS PER SRM 53-15-00, LIMITS CK OK. TREATED AND PAINTED, REINSTALLED FASTENERS. 2L73 4F A23WE 19950512002821995051200282WP 1995 5 12 DLL10951780 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 901 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 41 TO 42. REMOVED GLUE AND LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6, REINSTALLED STRAP PER SRM 53-31-00. 2L73 4F A23WE 19950512002831995051200283WP 1995 5 12 DLL10951781 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 901 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 42 TO 43. REMOVED GLUE/LIGHT CORROSION FROM UNDER FAIL-SAFE STRAP. TREATED PER PS 900-2-4-1, PAINTED PER PS 900-3-6. REINSTALLED STRAP PER SRM 53-31-00. 2L73 4F A23WE 19950512002841995051200284WP 1995 5 12 DLL10951786 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 943 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 42 TO 43. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002851995051200285WP 1995 5 12 DLL10951787 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 943 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 44 TO 45. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002861995051200286WP 1995 5 12 DLL10951788 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 943 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 43 TO 44. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002871995051200287WP 1995 5 12 DLL10951789 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 943 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 943 IN BETWEEN STR 40 TO 41. NO CORROSION FOUND, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002881995051200288WP 1995 5 12 DLL10951790 119950425A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 LT GEAR FITTING FWD TRUNNION FWD BORE HAS CORROSION ON FWD/AFT SIDES AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.218 0 TO REMOVE CORROSION. BURNISHED FACES TO REMOVE PITS PER SRM 57-14-00. 2L73 4F A23WE 19950512002891995051200289WP 1995 5 12 DLL10951791 119950425A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 LT GEAR FITTING AFT TRUNNION FWD BORE PITTED IN BORE. BORED LUG TO 4.7095 INCHES TO REMOVE CORROSION. 2L73 4F A23WE 19950512002901995051200290WP 1995 5 12 DLL10951792 119950409A5320 THRESHOLD LKHEED1011 10113851 5265010WP L 3 DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L-3 DOOR LWR INNER THRESHOLD PLATE IS CORRODED IN SEVERAL PLACES. CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-15-00 FIG 808. REMANUFACTURED THRESHOLD PLATE. 2L73 4F A23WE 19950512002911995051200291WP 1995 5 12 DLL10951793 119950409A5320 FITTING LKHEED1011 10113851 5265010WP L3 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L3 DOOR LWR INNER THRESHOLD FWD CORNER FITTING IS CORRODED. CLEANED CORROSION PER SRM 53-15-00 FIG 809, TREATED AND PAINTED. 2L73 4F A23WE 19950512002921995051200292WP 1995 5 12 DLL10951794 119950409A5320 FITTING LKHEED1011 10113851 5265010WP L-3 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L3 DOOR LWR INNER THRESHOLD AFT CORNER FITTING IS CORRODED. CORRODED BEYOND LIMIT, REMOVED FITTING AND REMOVED AFT GIRT BAR LATCH FOR ACCESS. 2L73 4F A23WE 19950512002931995051200293WP 1995 5 12 DLL10951795 119950426A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 LT MLG AFT TRUNNION FITTING A HAS CORROSION ON AFT FACE OF FWD LUG. BURNISHED FACE TO REMOVE LIGHT CORROSION. 2L73 4F A23WE 19950512002941995051200294WP 1995 5 12 DLL10951796 119950426A5743 TRUNNION LKHEED1011 10113851 5265010WP RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 RT LOCAL BLEND 010 TO REMOVE CORROSION. REWORKED SRM LIMITS 57-14-00, C/W ON RC 1488 TO 1489. 2L73 4F A23WE 19950512002951995051200295WP 1995 5 12 DLL10951797 119950426A5743 TRUNNION LKHEED1011 10113851 5265010WP RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 RT MLG TRUNNION FWD/AFT LUG FACE HAS LIGHT CORROSION. SPOT FACED 019 DEEP ON FWD FACE AFT LUG OF FWD. TRUNNION TO REMOVE CORROSION. REWORK C/W ON R/C 1488 TO 1489, WITHIN LIMITS 57-14-00. 2L73 4F A23WE 19950512002961995051200296WP 1995 5 12 DLL10951798 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 809 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED AFT OF FS 809 IN BETWEEN STR 30 TO 29. CORROSION REMOVED WITHIN LIMITS PER SRM 53-31-00 PG 801 FIG 801. TREATED/PAINTED PER PS 900-3-6, INSTALL PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002971995051200297WP 1995 5 12 DLL10951799 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 729 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED AFT OF FS 729 IN BETWEEN STR 29 TO 28. VERIFIED NO CORROSION EXISTS. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950512002981995051200298WP 1995 5 12 DLL10951800 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 749 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 749 IN BETWEEN STR 24 TO 23. REMOVED CORROSION, CKD LIMITS PER SRM 53-31-00 FIG 801 PG 801, FOUND SKIN WITHIN LIMITS. FABRICATED AND DRILLED UP REPAIR DOUBLER PER SRM 53-31-00 FIG 804, INSTALL PER SRM 53-31-00 FIG 804, TREATED AND PAINTED. 2L73 4F A23WE 19950512002991995051200299WP 1995 5 12 DLL10951801 119950412A5330 SKIN LKHEED1011 10113851 5265010WP FS 1765-1785 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS SKIN IS CORRODED IN C-3 B/B BETWEEN FS 1765 TO 1785 AND STR 37 TO 38. CLEANED CORROSION OUT OF LIMITS PER 53-31-00 FIG 801. CUT OUT SKIN PER SRM 53-31-00 FIG 803. DRILLED REPAIR PARTS PER SRM 53-31-00 FIG 803. TREATED/PAINTED, PARTS INSTALLED PER SRM 53-31-00 FIG 803, CMOR, EDGE SEALED REPAIR. 2L73 4F A23WE 19950512003001995051200300WP 1995 5 12 DLL10951802 119950409A5320 DOOR FRAME LKHEED1011 10113851 5265010WP L 4 DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L-4 DOOR FRAME LWR AFT CORNER IS CORRODED. CORROSION OUT OF LIMITS. REMOVED LWR FITTING, DRILLED UP FITTING AND INSTALLED AS PER SRM 53-15-00 FIG 809. 2L73 4F A23WE 19950512003011995051200301WP 1995 5 12 DLL10951803 119950409A5320 THRESHOLD LKHEED1011 10113851 5265010WP L 4 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 L-4 DOOR EDGE LWR INNER THRESHOLD PLATE IS CORRODED IN SEVERAL PLACES. CORROSION OUT OF LIMITS. REMOVED LWR INNER THRESHOLD PLATE, DRILLED UP NEW THRESHOLD PLATE, TREATED, PAINTED PER SRM 53-150-00. 2L73 4F A23WE 19950512003021995051200302WP 1995 5 12 DLL10951804 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 883 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 883 IN BETWEEN STR 44 TO 45. REMOVED GLUE AND LIGHT SURFACE CORROSION FROM DISBONDED AREA, TREATED, PAINTED AS PER PS 900-3-6. INSTALLED REPAIR PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950512003031995051200303WP 1995 5 12 DLL10951805 119950406A5330 SKIN LKHEED1011 10113851 5265010WP BS 1433 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 019565 SKIN CORRODED AT STA 1433 BETWEEN STR 32 TO 33 AT TEAR STRAP. C-2 B/B DOUBLE SKIN REPLACEMENT ACCOMPLISHED ON N/R 1978 AND ERA 270691-14. 2L73 4F A23WE 19950512003041995051200304WP 1995 5 12 DLL13951733 119950419A5522 PANEL LKHEED1011 10113851 5265010WP LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 000043 DURING INSPECTION, FOUND LEFT ELEVATOR LOWER SURFACE WITH NUMEROUS RIVETS LOOSE AT T/E PANEL O/B END. ALSO, AFT O/B CORNER OF SAME PANEL IS CRACKED. REPAIRED PER SRM 55-22-00. 2L73 4F A23WE 19950512003051995051200305WP 1995 5 12 DLL13951766 119950419A7830 SLEEVE LKHEED1011 10113851 5265010WP NR 2 ENGINE DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 019565 T/R REPAIR NR 2 ENG TRANSLATING SLEEVE REPAIRED PER SRM 54-37-00 FIG 802 PG 803 AND UNDER LYING BULKHEAD. REPAIRED SPLICE ANGLE DAMAGE PER 222B ENG MANUAL 78-32-07 FIG 990-012. 2L73 4F A23WE 19950512003061995051200306NM 1995 5 12 DLM88951699 119950424A5280 FRAME DOUG MD88 MD88 3023688NM RT MLG DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11981DL 53268 000008 FOUND DURING D-2 LETTER CHECK, .25 INCH CRACK AT O/B CORNER OF MLG DOOR FRAME ON EXISTING DOUBLER. REPAIRED PER SRM 53-05 NR 81A. 2L72 4F RTA6WE 19950512003071995051200307NM 1995 5 12 DLM88951741 119950223A5523 TE SKIN DOUG MD88 MD88 3023688NM ELEVATOR TAB DELAMINATED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11938DL 49811 000043 AT HMV, ELEVATOR TAB WAS FOUND WITH DAMAGE ON TRAILING EDGE AT 8 INCHES FROM O/B END. REPAIRED PER SRM 55-04. 2L72 4F RTA6WE 19950512003081995051200308NM 1995 5 12 9507412290 119950506A27821U10955 ACTUATOR BOEING727 727251 138408HNM NR 8 LE FLAP FAILED A ANWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL01290US237523050 21378 DURING CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE SLAT REMAINED EXTENDED. UNABLE TO RETRACT SLAT. RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 8 LEADING EDGE SLAT ACTUATOR. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950512003091995051200309NM 1995 5 12 9507422716 119950505A2760 RETRACT MECH BOEING727 7272S7 138407ZNM NR 5 SPOILER OUT OF ADJUST A NWAAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 GL01720RC 22491 DURING DEPARTURE CLIMB UPON ACCELERATING TO 300 KTS, NOTED AIRFRAME VIBRATION. VISUALLY OBSERVED NR 5 SPOILER FLOATING. FLIGHT RETURNED TO DEN WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NR 5 SPOILER TO FLAP CLEARANCE. 2L73 4F A3WE 19950512003101995051200310EU 1995 5 12 9507433204 119950505A2150VFT300A1AMDTA VENT VALVE AIRBUS320 A320211 3930320EU FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01328NW146601310 298 DURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED UNEVENTFULLY IN AN OVERWEIGHT CONDITION. MAINTENANCE DEACTIVATED THE AVIONICS VENTILATION EXTRACT VALVE AND PLACARDED PER MEL 21-26-03. THE SKIN AIR OUTLET VALVE (22 HQ) WAS LATER REPLACED. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950512003111995051200311NE 1995 5 12 9507449871 219950505A7200 ENGINE DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 MALFUNCTIONED A NWAAA UNSCHED LANDING MR OVER TEMP PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01780NC 48102 696664 AFTER DEPARTURE TPA, THE NR 1 ENGINE PERFORMANCE BEGAN TO DETERIORATE. THE AIRCRAFT RETURNED TO TPA LANDING WITHOUT INCIDENT. A LEAK WAS FOUND AT THE 13TH STAGE BLEED DUCT ATTACH FLANGE. MAINTENANCE REPLACED THE ENGINE. THE ENGINE CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950512003121995051200312WP 1995 5 12 9507459873 119950505A3231 BUNGEE DOUG DC9 DC951 3022051WP LT NLG DOOR OUT OF ADJUST A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01782NC 48107 NOSE LANDING GEAR DOOR DID NOT CLOSE ON GEAR RETRACTION AFTER DEPARTURE. FLIGHT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT NOSE GEAR DOOR BUNGEE BY LENGTHENING 1/2 TURN. OPERATIONAL CHECK OK ON DOOR CYCLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512003131995051200313WP 1995 5 12 9507469976 119950507A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL019340 47389 LOSS OF CABIN PRESSURIZATION OCCURRED AT 29,000 FEET ENROUTE DFW-MSP. CABIN ALTITUDE EXCEEDED 10,000 FEET AND OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. EMERGENCY DESCENT WAS MADE TO 10,000 FEET AND CABIN PRESSURE WAS REGAINED USING MANUAL OPERATION. FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512003141995051200314WP 1995 5 12 9507479957 119950505A2150 AIR COND DUCT DOUG DC9 DC931 3022065WP LEFT WATER SEP LOOSE A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01915RW 47139 EN ROUTE MSP-AUS, CABIN PRESSURE BEGAN CLIMBING AT A RATE OF 400 FPM AND BECAME UNABLE TO CONTROL. CABIN ALTITUDE CLIMBED ABOVE 12,000 FEET AND OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. EMERGENCY DESCENT WAS MADE TO 10,000 FEET. CABIN PRESSURE WAS REGAINED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. FOUND AIR CONDITIONING DUCT LOOSE AT AFT END OF LEFT WATER SEPARATOR. SECURED DUCT. PRESSURIZED AIRCRAFT TO 5.0 CABIN DIFFERENTIAL. ALL CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950512003151995051200315EU 1995 5 12 9507483248 119950505A3350321454 EEL POWER SUPPLY AIRBUS320 A320211 3930320EU CABIN INOPERATIVE A NWAAK NONE L NO TEST APAPPROACH 1 GL01348NW163513632 410 DURING APPROACH INTO MSP, THE EMERGENCY EXIT SIGNS ABOVE THE AFT GALLEY DOORS DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950512003161995051200316EU 1995 5 12 9507493204 119950507A7603321400M01 THROTTLE CONTL AIRBUS320 A320211 3930320EU NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01304US 40 DURING CLIMBOUT FROM MSP, RECEIVED ENG 2 THR LEVER FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 2 ENGINE THROTTLE CONTROL UNIT. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950512003171995051200317NM 1995 5 12 9507502703 119950503A27821U109592 ACTUATOR BOEING727 727225 1384077NM NR 8 LE SLAT FAILED A ANWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018878Z4983 17 21451 DURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE SLAT REMAINED EXTENDED. FOLLOWED ASYMMETRICAL LEADING EDGE DEVICE PROCEDURE TO NO AVAIL. FLIGHT RETURNED TO BNA WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 8 SLAT ACTUATOR. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950512003181995051200318NM 1995 5 12 9507512290 119950507A5243 ACCESS DOOR BOEING727 727251 138408HNM HYD COMPT DAMAGED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01290US 21378 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, TAIL SKID INDICATION REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH PROPER INDICATIONS. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC PUMP ACCESS DOOR OPEN AND INTERFERING WITH TAIL SKID OPERATION. STRAIGHTENED AND CLOSED ACCESS DOOR. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950512003191995051200319NE 1995 5 12 ABXA9500382 219950508A7320PS4 PS 4 LINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 2 FUEL CONTL LOOSE A ABXAO OTHER JX WARNING INDICATION ENGINE FLAMEOUT DEDESCENT 1 GL23817AX 45928 67403 DURING DESCENT, THE NR TWO ENGINE FLAMED OUT WHEN THE ENGINE ANTI-ICE WAS TURNED OFF. THE FLAME OUT CHECK LIST WAS ACCOMPLISHED AND THE ENGINE WAS RESTARTED. ALL ENGINE INDICATIONS WERE NORMAL FOR THE REMAINDER OF THE FLIGHT. LOOSE PS-4 LINE WAS FOUND AT THE NR TWO FUEL CONTROL UNIT; TIGHTENED LINE. ANTI-ICE OPERATED NORMALLY AS WELL AS ALL OTHER ENGINE FUNCTIONS DURING ENGINE RUN. ENGINE OPERATIONALLY CHECKED GOOD IAW DC-8 MM. 2L74 4F4 F 4A25 1E8 19950512003201995051200320SO 1995 5 12 COM11881 119950507A323020885 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01463CA7034 120267 HYDRAULIC FLUID LEAK FROM LT MLG AREA. REPLACED UPLOCK ACTUATOR. 2L72 4T RTA31SO 19950512003211995051200321 1995 5 12 COM11882 419950508A34256225812004 FDU 70 EMB 120 EMB120RT SO NR 2 DEFECTIVE A ACOMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01161CA12808 120143 YELLOW HEADING FLAP ON COPILOT'S EHSI, RED OFF FLAG ON PILOT'S RMI. REPLACED THE NR 2 FDU-70. 2L72 4T RTA31SO 19950512003221995051200322EA 1995 5 12 COM60466 119950507A52106003131511 LINKAGE CNDAIRCL600 CL6002B19 EA CABIN DOOR OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01920CA4209 7022 PASSENGER DOOR WARNING ON EICAS, FLIGHT ATTENDANT HEARD CLUNKING NOISE FROM DOOR AND OBSERVED RED UNSAFE INDICATION ON DOOR LATCH. FOUND DOOR OUTER HANDLE NOT COMPLETELY STOWED. ADJUSTED DOOR LINKAGE FOR PROPER ALIGNMENT OF DOOR VISUAL INDICATORS. 2L72 4F RTA21EA 19950512003231995051200323EA 1995 5 12 COM60467 119950508A2150601R950671 DUCT CNDAIRCL600 CL6002B19 EA LT ACM DEFECTIVE A COMAB EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO01932CA 7038 LEFT BLEED AIR VALVE CLOSED DURING LEVEL OFF. AIRCRAFT DEPRESSURIZED BECAUSE RT ACM PACK WAS PREVIOUSLY DEFERRED. THE LT ACM WATER SEPARATOR DUCT WAS FOUND DETACHED. INSTALLED NEW WATER SEPARATOR DUCT. 2L72 4F RTA21EA 19950512003241995051200324EA 1995 5 12 COM60468 119950507A2760270003 PCU CNDAIRCL600 CL6002B19 EA LT SPOILER DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01933CA2540 7040 INBD GROUND LIFT DUMPERS WILL NOT DEPLOY. REPLACED LT INBD FLIGHT SPOILER PCU. 2L72 4F RTA21EA 19950512003251995051200325WP 1995 5 12 MWEA95198 119950506A5330 SKIN DOUG DC9 DC914 3022034WP FS 786 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING ROUTINE INSPECTION THE SKIN WAS FOUND CRACKED 1.50 INCHES IN LENGTH AT FASTENER HOLE STA 786 LONGERON 14L. MAINTENANCE REPAIRED SKIN BY CUTTING OUT CRACKED SKIN, INSTALLING FINGER DOUBLER AND SKIN FILLER TO REMAIN FLUSH IAW DOUGLAS TELEX SYS-ENG-DAC-028/GPG AND SRM 53-04, FIG. 38, VIEW H. 2L72 4F A6WE 19950512003261995051200326EU 1995 5 12 QXEA9500135 119950507A3310561408BVL2 LIGHT BALLAST FOKKER FOKKERF28 F28MK1000 4990808EU COCKPIT FAILED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09801PH 11097 BOI - STRONG ELECTRICAL BURNING SMELL IN COCKPIT AFTER REACHING GATE. REPLACED BALLAST TRANSFORMER AT POSITION LG 18. LIGHT OPS CHECKED GOOD. AIRCRFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950512003271995051200327EU 1995 5 12 QXEA9500136 119950508A3350 EEL WIRE FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 BOI - ROW 10 EMERGENCY LIGHT INOP. REPAIRED WIRING HARNESS ON SEAT 10 A/B. LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950512003281995051200328SO 1995 5 12 SWIA95548 119950402A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE FLAP CONTROL DIRTY A SWIAO OTHER J WARNING INDICATION CRCRUISE 1 NM07223SW 120291 NUMEROUS FLAP CONTROL FAULTS ENROUTE. CONTROL FAULTS RESET EACH TIME. CLEANED FLAP ACTUATOR CANNON PLUGS. RERACKED FLAP CONTROL BOX. ALL CHECKS GOOD AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 19950512003291995051200329SW 1995 5 12 SWIA95549 119950403A2750 CONTROL VALVE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP FLAP SYST MALFUNCTIONED A ASWIAK NONE J WARNING INDICATION CRCRUISE 1 NM072699Y AC666 DURING GROUND CHECKS, FLAPS GIVE FULL TRAVEL. IN-FLIGHT, FLAPS WILL NOT OPERATE ABOVE AIRSPEEDS OF 147 KNOTS WITH GEAR UP. DURING LANDING IN PHX, FLAPS WORKED WITH GEAR DOWN AT 160 KTS. TROUBLESHOT SYSTEM. TESTED LEFT FLAP LOCK OUT VALUE. TESTED GOOD. REMOVED AND REPLACED FLAP CONTROL VALVE. RAN FLAPS AND GEAR SEVERAL TIMES UP AND DOWN. OPS CKS GOOD ON GROUND. NO LEAKS NOTED AT FLAP CONTROL VALVE OR FLAP LOCKOUT VALUE. 1L72 4T4 T A8SW E4WE 19950512003301995051200330NE 1995 5 12 SWIA95550 219950405A7310 FUEL LINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE FAILED A SWIACED ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK X ENGINE FLAMEOUT TOTAKEOFF 1 NM07197SW 120186 ON TAKEOFF ROLL AT APPROX 60 KNOTS, THE RIGHT ENGINE FAILED. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND OIL AND FUEL LEAKING FROM THE RIGHT ENGINE NACELLE. REMOVED AND REPLACED HMU FUEL LINE. GROUND RAN THE NR TWO ENGINE AT FULL POWER. LEAK AND OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003311995051200331SO 1995 5 12 SWIA95551 119950405A27503069001005 ANNUNCIATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS FAILED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07193SW 120088 CONTROL FAULT ON OUTBD FLAP. CONTROL FAULT WILL NOT RESET. CHECKED CONNECTOR AT OUTBOARD ACTUATORS. FOUND GOOD. CYCLED FLAPS AND RECEIVED A CONTROL FAULT (INTERMITTENTLY) WITH OUTBOARD SEGMENTS FLASHING. RESET USING OVERRIDE SWITCH. SUSPECT BAD ANNUNICATOR PANEL. REPLACED FLAP ANNUNCIATOR PANEL ASSEMBLY. OPERATED FLAPS TEN TIMES. OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003321995051200332SO 1995 5 12 SWIA95552 119950404A27503472001001 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07223SW 120291 FLAP CONTROL FAULT. FAULT WILL NOT RESET. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003331995051200333 1995 5 12 SWIA95553 419950404A2220 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ELEV TRIM FAILED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07216SW 120285 ON TAKEOFF ROLL, AS POWER WAS APPLIED, RECIEVED AURAL WARNING FOR TAKEOFF TRIM. TAKEOFF WAS ABORTED. RETURNED TO GATE AND NOTICED AURAL WARNING CIRCUIT BREAKER OPEN. CIRCUIT BREAKER WOULD NOT RESET. REPLACED THE LEFT ELEVATOR TRIM PROXIMITY SENSOR WITH A NEW UNIT IN ACCORDANCE WITH MM 22-32-05. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003341995051200334SO 1995 5 12 SWIA95554 119950407A243523080013 STARTER GEN EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LEFT FAILED A SWIAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC DEDESCENT 1 NM07212SW4387 408 120276 LOST THE LEFT GENERATOR ON DESCENT. GENERATOR WILL NOT RESET. REPLACED THE LEFT STARTER/GENERATOR. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003351995051200335EA 1995 5 12 SWIA95555 119950409A5753 SKIN CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT TE FLAP DENTED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 NM07405SW 7029 ABORTED TAKEOFF IN FSD. AIRCRAFT RETURNED TO GATE. INSPECTED AIRCRAFT AND FOUND DENT IN LEFT INBOARD FLAP ACTUATOR PYLON. INSPECTED LEFT INBOARD FLAP ACTUATOR PYLON. POPPED OUT DENT. DETERMINED AIRCRAFT TO BE AIRWORTHY AND OK FOR RETURN TO SERVICE. REINSPECTED BY SKYWEST MAINTENANCE IN SLC. 2L72 4F4 FRTA21EA E15NE 19950512003361995051200336SW 1995 5 12 SWIA95556 119950412A6120 O-RING SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT PROP DAMAGED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07174SW AC620 DURING TAKEOFF, THE LEFT PROP WAS FLUCTUATING. REMOVED SPINNER, BETA CAP, AND TUBE. FOUND FLAT SPOT ON INNER O-RING. REPLACED BOTH O-RINGS. SET BLADE ANGLE AND REINSTALLED PROP CAP AND SPINNER. GROUND RAN THE NR ONE AND NR TWO ENGINES. CHECKED BLADE ANGLE AND FLIGHT IDLE FUEL FLOWS. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA8SW E4WE 19950512003371995051200337SW 1995 5 12 SWIA95557 119950412A3231 ACTUATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT MLG DOOR FAILED A SWIAO OTHER N FALSE WARNING LDLANDING 1 NM07686AV AC686 LEFT MAIN LANDING GEAR WOULD NOT GIVE GREEN DOWN AND LOCKED LIGHT UNTIL MANUALLY EXTENDED WITH EMERGENCY EXTENSION PROCEDURES. FOUND INBOARD GEAR DOOR BUCKLED DUE TO DOOR GOING TO FAR UP IN WELL. THIS CAUSED GEAR TO HANG UP. REPLACED LEFT INBOARD GEAR DOOR LANDING GEAR EXTENSION ACTUATOR. OPERATIONALLY CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950512003381995051200338NE 1995 5 12 SWIA95558 219950413A7320 EEC CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE DIRTY A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07187SW 120037 RIGHT ENGINE EEC (ELECTRONIC ENGINE CONTROL) FAILED AND WOULD NOT RESET. DEFERRED PER MEL 73-21-1. ABORTED TAKEOFF. INSPECTED WIRING. CLEANED CANNON PLUG AND RAN AIRCRAFT. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003391995051200339SO 1995 5 12 SWIA95559 119950415A3231 LOCKPIN EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT MLG DOOR BENT A SWIAK NONE O OTHER CRCRUISE 1 NM07214SW 120280 LEFT MAIN GEAR OUTBD GEAR DOOR WILL NOT REMAIN LATCHED WHILE IN FLIGHT. FOUND GEAR DOOR LATCH LOCK PIN BENT. REPAIRED LOCK RETAINER PIN. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003401995051200340SO 1995 5 12 SWIA95560 119950417A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAK NONE J WARNING INDICATION LDLANDING 1 NM07189SW 120048 INBOARD FLAPS WILL NOT GO DOWN. CLEANED HEAVY MOISTURE OUT OF ACTUATOR CANNON PLUG ON RIGHT OUTBOARD SIDE INBOARD AND OUTBOARD ACTUATORS. RAN FLAPS UP AND DOWN A FEW TIMES. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003411995051200341SO 1995 5 12 SWIA95561 119950414A5712 RIB EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07186SW 120034 LEFT WING (UPPER) IN FIRST CELL OUTBOARD OF NACELLE, FOUR EACH RIB ATTACH FLANGE RIVETED TO UPPER SKIN CRACKED. FABRICATED AND REPLACED FOUR EACH RIB ATTACH FLANGES AT UPPER SKIN FIRST CELL OUTBOARD OF LEFT NACELLE. 2L72 4T4 TRTA31SO E20NE 19950512003421995051200342SO 1995 5 12 SWIA95562 119950414A5712 RIB EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07186SW 120034 LEFT WING (UPPER) IN THIRD CELL OUTBOARD OF NACELLE, ONE EACH RIB ATTACH FLANGE SECOND AFT CRACKED. FABRICATED AND REPLACED ONE EACH RIB ATTACH FLANGE AT UPPER SKIN SECOND AFT IN THIRD CELL OUTBOARD OF LEFT NACELLE. 2L72 4T4 TRTA31SO E20NE 19950512003431995051200343SO 1995 5 12 SWIA95563 119950414A323012025262501 RELAY BOX EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIAK NONE J WARNING INDICATION LDLANDING 1 NM07186SW 120034 LANDING GEAR WOULD NOT EXTEND NORMALLY. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX. GEAR SWUNG MANY TIMES. OVERRIDE FEATURE AND POSITION INDICATOR SYSTEMS OPERATIONALLY CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003441995051200344SO 1995 5 12 SWIA95564 119950427A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAK NONE F FLT CONT AFFECTED LDLANDING 1 NM07195SW 120127 UPON SELECTING FLAPS TO 25 DEGREES, A CONTROL FAULT WAS EXPERIENCED. RESET FLAPS. TRIED NEW CONTROL BOX. STILL FAULTING. FOUND MOISTURE IN LEFT INBOARD FLAP CANNON PLUG. CLEANED BOTH LEFT AND RIGHT INBOARD FLAP ACTUATOR CANNON PLUGS. CYCLED FLAPS NUMEROUS TIMES. OPERATIONALLY CHECKS GOOD ON THE GROUND AT THIS TIME. 2L72 4T4 TRTA31SO E20NE 19950512003451995051200345SO 1995 5 12 SWIA95565 119950429A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAP ACTUATORMISWIRED A SWIAO OTHER JW WARNING INDICATION INADEQUATE Q C LDLANDING 1 NM07195SW 120127 FLAP CONTROL FAULT. INBOARD FLAPS STAY AT 15 DEGREES. TROUBLESHOT SYSTEM. FOUND INBOARD FLAP ACTUATOR CONNECTOR MISWIRED. REPLACED CANNON CONNECTOR AND WIRED CORRECTLY. OPERATIONALLY CHECKS NORMAL ON GROUND. 2L72 4T4 TRTA31SO E20NE 19950512003461995051200346EA 1995 5 12 SWIA95566 119950427A2750855D1003 BPSU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT TE FLAPS FAILED A SWIAO OTHER J WARNING INDICATION LDLANDING 1 NM07408SW714 7055 FLAP FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING. FLAPS WERE AT 45 DEGREES. REMOVED AND REPLACED RIGHT FLAP BPSU (BRAKE POSITION SENSING UNIT) IN ACCORDAMCE WITH MM 22-51-00. OPERATIONALLY CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 19950512003471995051200347SW 1995 5 12 SWIA95567 119950428A7720 TEMP CONTROL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT/RT ENGINE OUT OF ADJUST A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM072725D AC723 NEITHER ENGINE WOULD MAKE TARGET TORQUE. ABORTED TAKEOFF. ADJUSTED TEMPERATURE CONTROLLER PERMANENT CONTROL. IN SAN: REINSPECTED LEFT AND RIGHT EGT SYSTEM. FOUND TO BE WITHIN LIMITS SET BY DSC SHEETS. 1L72 4T4 T A8SW E4WE 19950512003481995051200348SW 1995 5 12 SWIA95568 119950429A3260 UPLOCK ROLLER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT MLG MISSING A SWIAO OTHER JD WARNING INDICATION INFLIGHT SEPARATION CLCLIMB 1 NM072726N AC727 AFTER DEPARTURE, THE RED GEAR LIGHT ON RIGHT MAIN GEAR REMAINED ILLUMINATED AND COULD NOT BE EXTINGUISHED EVEN AFTER REPEATED GEAR CYCLING. FOUND RIGHT MAIN UPLOCK ROLLER AND STRIKER ASSY MISSING. REPLACED ROLLER AND STRIKER ASSY. ALSO, FOUND UP POSITION SWITCH BENT. REMOVED UP POSITION SWITCH ON RIGHT MAIN LANDING GEAR. INSTALLED RIGHT MAIN LANDING GEAR UP POSITION SWITCH AND SAFETIED JAM NUTS. 1L72 4T4 T A8SW E4WE 19950512003491995051200349SO 1995 5 12 SWIA95569 119950430A27503203001007 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS FAILED A SWIAK NONE J WARNING INDICATION LDLANDING 1 NM07193SW 120088 FLAPS WILL NOT SET AT 15 DEGREES FOR TAKEOFF. SHOWS SWS FAILURE. WILL NOT RESET. REPLACED RIGHT OUTBOARD FLAP ACTUATOR AND CANNON PLUG. OPERATED FLAPS APPROXIMATELY SIX TIMES AT EACH INTERIM. FLAPS OPERATIONALLY CHECKS GOOD. LEAK CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950512003501995051200350SO 1995 5 12 SWIA95570 119950424A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 LEFT WING OUTBOARD OF NACELLE HAS FIVE CRACKED CLIPS. FOUR AT POSITION YA-4533.5, AND ONE AT YA-6750. FABRICATED SAME AS ORIGINAL AND INSTALLED CLIPS AT YA-4533.5 (FOUR EACH) AND YA-6750 (ONE EACH). 2L72 4T4 TRTA31SO E20NE 19950512003541995051200354CE 1995 5 12 95ZZZX2304 119950411A5220 WINDOW MTSBSIMU2 MU2B36 5780412CE CREW EMERG CRACKED ALACMWAK NONE O OTHER ININSP/MAINT 1 NM09500PJ 668 DURING A POST-INSPECTION WALK-AROUND, A CRACK WAS NOTED EXTENDING APPROXIMATELY 1 INCH INTO THE VISIBLE AREA OF THE OUTER WINDOW IN THE CREW EMERGENCY ESCAPE DOOR. WHEN WINDOW RETAINERS WERE REMOVED, A CRACK 16 INCHES LONG CONNECTING 11 BOLT HOLES ACROSS THE TOP EDGE OF THE WINDOW WAS FOUND. THE CREW ESCAPE DOOR IS AN AFTER-MARKET INSTALLATION INSTALLED PER STC SA 252350 BY PRECISION AIR, INC., FAA REPAIR STATION NR 709-18 ON 3-2-89. THIS IS THE SECOND OCCURRENCE OF CRACKING ON THIS AIRCRAFT. 1H72 3T RTA10SW 19950512003561995051200356EA 1995 5 12 95ZZZX2306 119950502A28102770086103 DE FUEL VALVE CNDAIRCL600 CL6002B16 1900305EA LT WING MISMANUFACTURED A AIMKAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA251868M 1395 5012 DURING AN INSPECTION, DISCOVERED LT WING DE-FUEL VALVE HAD DAMAGED THREADS, AND NEEDED TO BE REPLACED. REMOVED VALVE FROM AIRCRAFT AND ORDERED A REPLACEMENT VALVE, PN 2770086-103. RECEIVED A NEW VALVE, INSPECTED IT, AND FOUND IT OKAY TO INSTALL. AT INSTALLATION, FOUND THE HOLES SLIGHTLY MISALIGNED. VALVE DID FIT, HOWEVER, LEAK CHECKS FAILED. VALVE WAS REMOVED AND A REPLACEMENT VALVE ORDERED AND INSTALLED WITHOUT ANY MATING OR MISALIGNMENT PROBLEMS. THIS VALVE WAS A NEW VALVE, SN 1395, RECEIVED FROM CANADAIR AS THEY RECEIVED IT FROM PARKER. FINAL INSPECTION AT BOTH FACILITIES DID NOT REVEAL DEFECT. RECOMMEND A CHECK OF OTHER UNITS IN STOCK AND AT THE MFG TO PREVENT THESE OCCURRENCES FROM RECURRING. 2L72 4F RTA21EA 19950512003571995051200357EA 1995 5 12 95ZZZX2307 119950502A28102770086102 DE FUEL VALVE PARKER CNDAIRCL600 CL6002B16 1900305EA LT WING DAMAGED A AIMKAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA251868M 1395 5012 DURING AN INSPECTION, DISCOVERED LT WING DE-FUEL VALVE HAD DAMAGED THREADS, AND NEEDED TO BE REPLACED. REMOVED VALVE FROM AIRCRAFT AND ORDERED A REPLACEMENT VALVE, PN 2770086-103. RECEIVED A NEW VALVE, INSPECTED IT, AND FOUND IT OKAY TO INSTALL. AT INSTALLATION, FOUND THE HOLES SLIGHTLY MISALIGNED. VALVE DID FIT, HOWEVER, LEAK CHECKS FAILED. VALVE WAS REMOVED AND A REPLACEMENT VALVE ORDERED AND INSTALLED WITHOUT ANY MATING OR MISALIGNMENT PROBLEMS. THIS VALVE WAS A NEW VALVE, SN 1395, RECEIVED FROM CANADAIR AS THEY RECEIVED IT FROM PARKER. FINAL INSPECTION AT BOTH FACILITIES DID NOT REVEAL DEFECT. RECOMMEND A CHECK OF OTHER UNITS IN STOCK AND AT THE MFG TO PREVENT THESE OCCURRENCES FROM RECURRING. 2L72 4F RTA21EA 19950512003591995051200359NM 1995 5 12 AALA950566 119950403A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07618AA 24526 MIA - FLT NR 1723 - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM 5 IN FIRST CLASS TO ROW 15 IN COACH INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH CONNECTOR BETWEEN ROW 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA2NM 19950512003601995051200360NM 1995 5 12 AALA950567 119950402A3350S417N50914 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS ON LEFT SIDE BETWEEN FIRST AND BUSINESS CLASS INOPERATIVE. REPLACED EMERGENCY EXIT PATH MARKING LIGHT ASSEMBLY AT 9AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003611995051200361NM 1995 5 12 AALA950568 119950402A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY CROSSOVER LIGHTS FORWARD OF AFT GALLEY INOPERATIVE. RECONNECTED EMERGENCY EXIT PATH MARKING CROSSOVER LIGHTS CONNECTOR AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003621995051200362NM 1995 5 12 AALA950569 119950402A3350A3060719103 EEL STRIP BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 36 INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHTS AT 36HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003631995051200363NM 1995 5 12 AALA950570 119950401A33508100022002 EEL STRIP BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT RIGHT SIDE MID GALLEY INOPERATIVE. REPLACED MID GALLEY RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003641995051200364WP 1995 5 12 AALA950572 119950331A215017946081 SEPARATOR DOUG DC9 DC982 3022082WP ACM BAY OVERSERVICED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07467AA 49597 DFW - FLT 0311 - DURING CRUISE EN ROUTE DFW-PDX SMOKE IN CABIN, AIR INTERRUPTED BACK TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. NR 2 AIR CYCLE MACHINE OVERSERVICED. SERVICED TO PROPER LEVEL, PRECAUTIONARY REPLACED BOTH WATER SEPARATOR PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FCF, NO SMOKE NOTED AND SYSTEM CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950512003651995051200365NM 1995 5 12 AALA950573 119950401A2612310114 ENG FIRE LOOP BOEING727 727223 1384074NM NR 2 ENG DEFECTIVE A AALAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CRCRUISE 1 SW07896AA 22012 MIA - FLT 945 - DURING CRUISE, EN ROUTE MIA-PHL FIRE BELL SOUNDED WITH NO LIGHTS. ACCOMPLISHED ABNORMAL PROCEDURES, NO FIRE INDICATION. AFTER BELL SOUNDED AGAIN, ISOLATED PROBLEM TO NR TWO ENGINE. AIR INTERRUPTED BACK TO MIA AND DUMPED FUEL. FIRE BOTTLES WERE NOT BLOWN AND ENGINE WAS NOT SHUT DOWN. LANDED WITHOUT INCIDENT. REPLACED NR TWO ENGINE FIRE LOOP AND CONTROLLER. OPERATED NR 2 ENGINE AT HIGH POWER, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950512003661995051200366NM 1995 5 12 AALA950582 119950404A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07319AA 22320 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT 8B INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003671995051200367NM 1995 5 12 AALA950598 119950409A25308609010000 OVEN BOEING767 767323 1385205NM GALLEY DIRTY A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07357AA 24038 LHR - FLT 108 - EN ROUTE BOS-LHR - DURING CRUISE, FIRST CLASS GALLEY OVEN EMITTED SMOKE FROM INSIDE OVEN COMPARTMENT DURING USE. NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED LHR AND LANDED WITHOUT INCIDENT. CLEANED INTERIOR OF FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512003681995051200368WP 1995 5 12 AALA950648 119950411A5350 LATCH DOUG DC9 DC982 3022082WP AFT FUSELAGE OUT OF ADJUST A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0714551 53033 TUL - FLT 746 - AFTER TAKEOFF TUL DURING CLIMB-OUT, TAILCONE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO TUL AND LANDED WITHOUT INCIDENT. ADJUSTED TAILCONE LATCH. PRECAUTIONARY CHECKED TAILCONE RIGGING WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950512003691995051200369NM 1995 5 12 ASAA9540019 119950424A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 SEA - LAST FOUR EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. OPS CHECKED NORMAL. (W) 2L72 4F RTA16WE 19950512003701995051200370WP 1995 5 12 ASAA9580054 119950321A21216054577 FAN DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ASAAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM01962AS8968 53076 LAX - DURING CRUISE OF FLT 572 AT FL 330, FLIGHT ATTENDANTS REPORTED STRONG BURNING ODOR IN CABIN. CAPTAIN DESCENDED AIRCRAFT TO FL 250, COMPLETED CHECK LIST AND PULLED RECIRCULATING FAN CIRCUIT BREAKER, ODOR DISSIPATED. FOUND RECIRCULATION FAN INOPERATIVE. RELEASED AIRCRAFT PER MEL 21-43. SUBSEQUENTLY REPLACED FAN IN SEAT ON 3/22/95. SYSTEM OPERATED NORMALLY WITH NO ODORS NOTED. (W) 2L72 4F RTA6WE 19950512003711995051200371WP 1995 5 12 ASAA9580060 119950328A5311 FRAME DOUG DC9 DC982 3022082WP FS 1322 CORROSION A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28898 49231 PAE - DURING 30K CHECK, CORROSION WAS FOUND FOUND ON THE FRAME AT Y1322, Z15, PER SRM 51-30-5. (W) 2L72 4F A6WE 19950512003721995051200372WP 1995 5 12 ASAA9580061 119950328A5320575468828 DOUBLER DOUG DC9 DC982 3022082WP SLIDING WINDOW CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS 49231 PAE - DURING 30K CHECK, DOUBLER WAS FOUND CRACKED AT THE LOWER FORWARD FASTENER HOLE AT THE UPPER AFT RADIUS OF THE CO-PILOTS SLIDING WINDOW CUTOUT. REPLACED DOUBLER PER SRM 51-30-2. (W) 2L72 4F A6WE 19950512003731995051200373WP 1995 5 12 ASAA9580062 119950328A5240 CUSP WEB DOUG DC9 DC982 3022082WP AFT SVC DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28898 49231 PAE - DURING 30K CHECK, CUSP WEB AT AFT SERVICE DOOR WAS FOUND CORRODED AND WORN. REPLACED CUSP MEMBRANE PER EA 5320-01203. (W) 2L72 4F A6WE 19950512003741995051200374WP 1995 5 12 ASAA9580063 119950329A53200637075T6 WEB DOUG DC9 DC982 3022082WP FS 1145-1167 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28898 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON L-2 WEB, STATION 1145 TO 1167. REMOVED CORROSION PER SRM AND EA 5320-01203. (W) 2L72 4F A6WE 19950512003751995051200375WP 1995 5 12 ASAA9580066 119950404A32225910448541 STRUT DOUG DC9 DC982 3022082WP NLG LOW SERVICE A ASAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01937AS281186652 49364 OAK - AIR TURN BACK OF FLIGHT 443, CREW REPORTED THE NOSE LANDING GEAR INTRANSIT LIGHT ON. CYCLED GEAR TO DOWN AND GOT ALL DOWN AND LOCKED INDICATION. LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT LOW. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950512003761995051200376 1995 5 12 ASAA9580070 419950406A2565D29982107 SLIDE DOUG DC9 DC983 3022083WP L1 DOOR FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01942AS124101172 53052 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE PRESSURE WAS FOUND LOW. REPLACED THE EVACUATION SLIDE WITH A SERVICEABLE UNIT. (W) 2L72 4F RTA6WE 19950512003771995051200377WP 1995 5 12 ASAA9580075 119950413A5320 SPLICE DOUG DC9 DC982 3022082WP FS 588 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28900 49231 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON MANUFACTURE SPLICE CHANNEL AT Y588, LONGERON 28L. REMOVED AND REPLACED MANUFACTURE SPLICE CHANNEL IAW DC-9 SRM 51-10-03, PG 15, 53-01, PG 5, 51-10-04, PG 4A, 51-30-05, PG 1. (W) 2L72 4F A6WE 19950512003781995051200378WP 1995 5 12 ASAA9580076 119950413A5311 FRAME DOUG DC9 DC982 3022082WP FS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28900 49231 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME Y1250 BETWEEN LONGERON 28R AND 26L. REPLACED FRAME IAW DC-9 SRM 51-10-03. (W) 2L72 4F A6WE 19950512003791995051200379WP 1995 5 12 ASAA9580077 119950413A5347TMS6013506 CARGO TRACK DOUG DC9 DC982 3022082WP FS 1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28900 49231 PAE -DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1212, LONGERON 28R. REPLACED CARGO TRACK IAW DC-9 SRM 51-10-03. (W) 2L72 4F A6WE 19950512003801995051200380WP 1995 5 12 ASAA9580078 119950413A5347TMS6013506 CARGO TRACK DOUG DC9 DC982 3022082WP FS 1007-1320 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28900 49231 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1007-Y1320, LONGERON 28L. REPLACED CARGO TRACK IAW DC-9 SRM 51-10-03. (W) 2L72 4F A6WE 19950512003811995051200381WP 1995 5 12 ASAA9580079 119950413A53205936628181 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 786 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y786, X-15 TO X PLUS 15, Z-45. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-10-04. (W) 2L72 4F A6WE 19950512003821995051200382WP 1995 5 12 ASAA9580080 119950413A53205956034552 FLOOR SUPPORT DOUG DC9 DC982 3022082WP FS 788 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y788, X-5 TO X PLUS 4, Z-47 TO Z-50. REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-10-03, 51-30-05, 51-30-02, 51-20-00. (W) 2L72 4F A6WE 19950512003831995051200383WP 1995 5 12 ASAA9580081 119950413A532059512723 SUPPORT DOUG DC9 DC982 3022082WP FS 1030-1060 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FAIRING SUPPORT AT Y1030 TO Y1060, X-0 TO Z-50. REPLACED FAIRING SUPPORT IAW DC-9 ARM 51-10-03, 51-10-01, 51-30-05. (W) 2L72 4F A6WE 19950512003841995051200384WP 1995 5 12 ASAA9580082 119950413A53132777922325000 LONGERON DOUG DC9 DC982 3022082WP FS 219-220 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y219 TO Y220. REPLACED LONGERON IAW DC-9 SRM 51-01, 51-10-01, 51-10-03. (W) 2L72 4F A6WE 19950512003851995051200385WP 1995 5 12 ASAA9580083 119950413A533059360331 SKIN DOUG DC9 DC982 3022082WP FS 1100-1170 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON INTERNAL SKIN AT Y1100 TO Y1170, X-5 TO Z-53. BLENDED AND TREATED AREA AND INSTALLED EXTERNAL DOUBLER IAW DC-9 SRM 53-04. (W) 2L72 4F A6WE 19950512003861995051200386WP 1995 5 12 ASAA9580084 119950413A533099100785 SKIN DOUG DC9 DC982 3022082WP FS 216-221 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, DENTS WERE FOUND ON OUTER SKIN AT Y216 TO Y221, X PLUS 63 TO Z PLUS 4. REPAIRED SKIN IAW DC-9 SRM 53-04. (W) 2L72 4F A6WE 19950512003871995051200387WP 1995 5 12 ASAA9580085 119950413A5311 FRAME DOUG DC9 DC982 3022082WP FS 1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AND SHEAR TIE AT Y1231, X PLUS 15 TO X-15, Z-45 AND Y1231, X PLUS 0 TO X PLUS 12, Z-49. REMOVED CORRODED AREA OF FRAME. INSTALLED NEW FRAME, REPAIR ANGLES AND SPLICE PLATES IAW DC-9 SRM 53-03, 53-04, 53-10-03, 51-30-02. (W) 2L72 4F A6WE 19950512003881995051200388WP 1995 5 12 ASAA9580086 119950413A5311 FRAME DOUG DC9 DC982 3022082WP FS 1320 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1320, X PLUS 20 TO X-10, Z-45. REMOVED CORRODED AREA OF FRAME. INSTALLED NEW FRAME AND REPAIR ANGLES IAW DC-9 SRM 53-03 AND 53-10-03. (W) 2L72 4F A6WE 19950512003891995051200389WP 1995 5 12 ASAA9580087 119950413A53205644324 RETAINER DOUG DC9 DC982 3022082WP LT COCKPIT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, A CRACK WAS FOUND IN FASTENER HOLE OF WINDOW RETAINER BETWEEN LEFT CLEARVIEW WINDOW AND AFT COCKPIT WINDOW. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW DC-9 SRM 56-01 AND 51-60-00. (W) 2L72 4F A6WE 19950512003901995051200390WP 1995 5 12 ASAA9580088 119950414A33501001191 EEL PORTABLE DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01964AS2286815582 53078 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950512003911995051200391WP 1995 5 12 ASAA9580089 119950417A5311 FRAME DOUG DC9 DC982 3022082WP FS 1212 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, DAMAGE WAS FOUND ON FRAME AT Y1212, LONGERON 3L. REMOVED AND REPALCED DAMAGED FRAME IAW DC-9 SRM 53-03 AND 51-10-03. (W) 2L72 4F A6WE 19950512003921995051200392WP 1995 5 12 ASAA9580090 119950417A5330 SKIN DOUG DC9 DC982 3022082WP FS 560-592 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SKIN AT Y560 TO Y592, X PLUS 10 TO X-4, Z-50. REMOVED CORROSION AND INSTALLED INTERNAL DOUBLER IAW ASA EA 5330-01193. (W) 2L72 4F A6WE 19950512003931995051200393WP 1995 5 12 ASAA9580091 119950417A5313 LONGERON DOUG DC9 DC982 3022082WP FS 1128-1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R AT Y1128 TO Y1155. REMOVED CORROSION AND INSTALLED REPAIR IAW ASA EA 5310-01360. (W) 2L72 4F A6WE 19950512003941995051200394WP 1995 5 12 ASAA9580092 119950417A5311 FRAME DOUG DC9 DC982 3022082WP FS 503 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y503, Z PLUS 54, LONGERON 28L TO 28R. REPLACED FRAME IAW DC-9 SRM 53-03. (W) 2L72 4F A6WE 19950512003951995051200395WP 1995 5 12 ASAA9580093 119950417A53135932731501 LONGERON DOUG DC9 DC982 3022082WP FS 579 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01933AS28339 49234 PAE - DURING 30K CHECK, CORROISON WAS FOUND ON LONGERON 29L AT Y579. REPLACED LONGERON IAW DC-9 SRM 53-01 AND 53-02. (W) 2L72 4F A6WE 19950512003961995051200396WP 1995 5 12 ASAA9580094 119950417A53137075T6 LONGERON DOUG DC9 DC982 3022082WP FS 598 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01930AS28900 49231 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 28L AND Y598. REPLACED LONGERON IAW DC-9 SRM 53-02, 51-10-04, 51-10-03, 51-20-00, 51-30-05. (W) 2L72 4F A6WE 19950512003971995051200397WP 1995 5 12 ASAA9580095 119950418A3350 EEL DOUG DC9 DC983 3022083WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD NR 5200 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950512003981995051200398WP 1995 5 12 ASAA9580096 119950419A33501001191 EEL PORTABLE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01933AS148749293 49234 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSY AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950512003991995051200399 1995 5 12 ASAA9580097 419950420A2564 TETHER DOUG DC9 DC983 3022083WP LIFE RAFT DETACHED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01945AS 49643 SEA - DURING LIFE RAFT DEMONSTRATION INFLATION, THE SURVIVAL EQUIPMENT PACKAGE BECAME DETACHED FROM THE RAFT WHEN THE TETHER SECURING THE EQUIPMENT PACKAGE TO THE RAFT STITCHING FAILED AT THE ATTACHMENT TO THE EQUIPMENT PACKAGE. THE RAFT WAS RETURNED TO THE MANUFACTURER. (W) 2L72 4F RTA6WE 19950512004001995051200400WP 1995 5 12 ASAA9580098 119950421A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 29 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950512004011995051200401WP 1995 5 12 ASAA9580099 119950422A3350 EEL GROUND DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01932AS 49233 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 16 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD B5-102 AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950512004021995051200402WP 1995 5 12 ASAA9580100 119950422A335060030351 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01950AS 53023 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND SIGN OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950512004031995051200403EU 1995 5 12 95ZZZX2310 119950308A261121562B SMOKE DETECTOR AUTRONICS STBROSSD3 SD330 8100602EU NOSE BAGG COMPT MALFUNCTIONED A S2YAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL13335MV SH3017 DFW/TUL - EN ROUTE, NOSE BAGGAGE COMPARTMENT SMOKE WARNING SYSTEM ACTIVATED. PILOT DISCHARGED FIRE BOTTLE INTO NOSE COMPARTMENT, WARNING LIGHT EXTINGUISHED. UPON LANDING, NOSE BAGGAGE COMPARTMENT SMOKE WARNING LIGHT AND DOOR LIGHT CAME ON, THEN ON ROLL-OUT, THEY BOTH EXTINGUISHED. NOSE COMPARTMENT AND CARGO WAS CHECKED FOR SIGNS OF SMOKE OR FIRE, NONE WAS NOTED. SMOKE DETECTION SYSTEM WAS TESTED AND APPEARED TO BE NORMAL. BOTH NOSE COMPARTMENT SMOKE DETECTORS WERE CHANGED FOR PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2H72 4T A41EU 19950512004041995051200404WP 1995 5 12 95ZZZX2311 119950429A2810383104 CAP ASSY DOUG DC8 DC8F54 3021926WP NR 1 ALT TANK LEAKING A FXLAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO19426FB62764 45667 MIAMI - AFTER TAKEOFF, NOTED FUEL LOSS FROM NR 1 ALT FUEL TANK. RETURNED TO MIAMI. LANDED WITHOUT INCIDENT. INSPECTION REVEALED LEAKING FUEL TANK CAP AT NR 1 ALT TANK. REPLACED FUEL TANK CAP. AIRCRAFT RETURNED TO SERVICE. TOTAL CYCLES 20,256. 2L74 4F 4A25 19950512004051995051200405WP 1995 5 12 95ZZZX2312 119950421A52805616307213 DOOR DOUG DC8 DC851 3021920WP LT MAIN GEAR DAMAGED A FXLAA UNSCHED LANDING JC WARNING INDICATION F.O.D. CLCLIMB 1 SO19508DC60665 45935 PTY - AFTER TAKEOFF, RECEIVED LEFT MLG UNSAFE LIGHT. RETURNED TO PTY. INITIAL INSPECTION REVEALED LEFT MLG DOOR DAMAGE. REMOVED LEFT MLG DOOR AND FERRIED AIRCRAFT TO MIA. INVESTIGATION REVEALED IMPACT DAMAGE TO DOOR. REPLACED DOOR. PERFORMED SEVERAL RETRACTION TESTS AND SYSTEM WORKED NORMALLY. RETURNED AIRCRAFT TO SERVICE. TOTAL CYCLES, 27,998. 2L74 4F 4A25 19950512004061995051200406EU 1995 5 12 AWXA9500242 119950425A2121VD390002 FAN AIRBUS320 A320231 3930325EU RT RECIRC INOPERATIVE A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28632AW 81 LAS/SEA - FLT 26 - SUPPLEMENTAL CLOSED SDR; ORIGINAL DATED 95-04-25. EN ROUTE, CREW REPORTED A SMOKE ODOR IN CABIN, BUT NO VISIBLE SMOKE. RT CABIN FAN FAILED AND CIRCUIT BREAKER TRIPPED. UMSR 21 21 01 WAS ISSUED. A/C CONTINUED TO SEA WITHOUT FURTHER PROBLEMS. MX REPLACED FAN, OPS CHECK OKAY. MEL REMOVED. (X) 2L72 4F RTA28NM 19950512004071995051200407NM 1995 5 12 AWXA9500243 119950501A276165445617 ACTUATOR BOEING737 737277 1384570NM NR 6 FLT SPOILERFAILED A AAWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28186AW 2181 22653 LAS/PHX - FLT 897 - EN ROUTE, LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER PROBLEMS. A/C WAS TOWED TO GATE. MX FOUND BAD NR 6 SPOILER ACTUATOR. REMOVED AND REPLACED ACTUATOR. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (X) 2L72 4F RTA16WE 19950512004081995051200408EU 1995 5 12 AWXA9500245 119950425A3350321452 BATTERY PACK AIRBUS320 A320231 3930325EU CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW 091 PHX - DURING ROUTINE MAINTENANCE CHECK, LT FORWARD BATTERY PACK SHOWED EXTERNAL LOAD. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F RTA28NM 19950512004091995051200409NM 1995 5 12 AWXA9500246 119950426A335020131A BATTERY ASSEMBLY BOEING757 7572G7 1384963NM CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 20 THROUGH 25 AND FROM THE L3 DOOR THROUGH ROW 32. REMOVED AND REPLACED BATTERY ASSEMBLY AT M734, OPS CHECK GOOD. (X) 2L72 4F RTA2NM 19950512004101995051200410EU 1995 5 12 AWXA9500247 119950427A3350321452 BATTERY PACK AIRBUS320 A320231 3930325EU CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 PHX - DURING ROUTINE MAINTENANCE CHECK, LT MID-CABIN EPSU FAILED BITE TEST. REMOVED AND REPLACED EPSU BATTERY, OPS CHECK GOOD. (X) 2L72 4F RTA28NM 19950512004111995051200411NM 1995 5 12 AWXA9500249 119950428A3350 CONNECTOR BOEING757 7572G7 1384963NM CABIN EEL LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT AISLE OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT R2 AND R3 DOORS. RESEATED CONNECTORS AT M732, M734, AND M735. OPS CHECK GOOD. (X) 2L72 4F RTA2NM 19950512004121995051200412EU 1995 5 12 AWXA9500250 119950428A3350321452 BATTERY PACK AIRBUS320 A320231 3930325EU CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND A SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F RTA28NM 19950512004131995051200413NM 1995 5 12 AWXA9500251 119950428A3350 LIGHT ASSEMBLIES BOEING737 7373S3 1384711NM CABIN EEL LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 TO AFT OF AIRCRAFT. RECONNECTED SEVERAL LIGHT ASSEMBLIES, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950512004141995051200414NM 1995 5 12 AWXA9500252 119950429A335020131A BATTERY PACK BOEING737 7373G7 1384595NM CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28160AW 23782 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT OVERWING POSITION, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950512004151995051200415NM 1995 5 12 AWXA9500253 119950430A3350 LIGHT ASSY BOEING737 7373S3 1384711NM CABIN EEL DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 AFT. RECONNECTED AND INSTALLED LIGHTS, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950512004161995051200416NE 1995 5 12 C2XA95CL075 219950427A7261311225101 CARBON SEAL EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT ENGINE LEAKING A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW0947722 120166 115208 CLE/CLE - FLT 3265 - RIGHT ENGINE OIL PRESSURE WENT TO LESS THAN 40 P.S.I., ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. CLE MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE CASE VENT TUBE CARBON SEAL IAW PRATT AND WHITNEY MM 72-20-00. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950512004171995051200417SO 1995 5 12 C2XA95CL076 119950427A7722311270401 T6 PROBE EMB 120 EMB120RT SO RIGHT ENGINE DAMAGED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0947722 120166 CLE/CLE - FLT 3267 - RIGHT ENGINE T6 FLUCTUATES CONTINUOUSLY FROM 542 TO 648 DEGREES CELSIUS IN CRUISE. AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. CLE MAINTENANCE REMOVED AND REPLACED THE 4 AND 5 O'CLOCK POSITION T6 PROBES IAW PRATT & WHITNEY MM 72-01-60. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950512004181995051200418NE 1995 5 12 C2XA95CL077 219950429A731030357817 FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT ENGINE DIRTY A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0926714 120118 115267 CLE/ROC - FLT 3115 - AFTER TAKEOFF, FUEL FILTER LIGHT (NR 1 ENGINE) ILLUMINATED. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED FUEL FILTERS AND CLEANED CANNON PLUGS. OPS CHECKED GOOD. RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950512004191995051200419EU 1995 5 12 C2XA95CL078 119950429A273083001 ACTUATOR AEROSPATR42 ATR42320 8680930EU TAIL JAMMED A C2XAK NONE O OTHER ININSP/MAINT 1 SW09198129758 235 99 MHT/EWR - FLT 3557 - DURING PRE-FLIGHT CHECK, FOUND ELEVATOR CONTROL JAMMED AND THE STICK PUSHER CIRCUIT BREAKER TRIPPED. MAINTENANCE INSPECTED AND REMOVED STICKER PUSHER ACTUATOR FOR A FERRY FLIGHT TO EWR. UPON ARRIVAL IN EWR, MAINTENANCE INSTALLED NEW STICK PUSHER ACTUATOR IAW ATR42 JIC 27-36-31. OPS CHECKED GOOD IAW 27-36-00. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950512004201995051200420EU 1995 5 12 C2XA95CL080 119950502A3260D228830001 PROXIMITY SENSOR AEROSPATR42 ATR42320 8680930EU LEFT GEAR WOW SHORTED A C2XAD RETURN TO BLOCK JO WARNING INDICATION OTHER TXTAXI/GRND HDL 1 SW0914829 181 BWI/EWR - FLT 3772 - STICK PUSHER/SHAKER FAULTED ON GROUND. FERRIED AIRCRAFT TO EWR FOR REPAIR. MAINTENANCE REMOVED AND REPLACED LEFT WEIGHT ON WHEELS PROXIMITY SENSOR. OPS CHECKED GOOD. RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950512004211995051200421SO 1995 5 12 C2XA95IA065 119950427A534712026864007 SEAT TRACK EMB 120 EMB120RT SO LT AFT CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, FOUND LT AFT SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. AC TT, 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004221995051200422SO 1995 5 12 C2XA95IA066 119950504A523012020235001 BRACKET EMB 120 EMB120RT SO TORSION BAR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, CARGO DOOR TORSION BAR FORWARD MOUNTING BRACKET WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT, 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004231995051200423SO 1995 5 12 C2XA95IA067 119950504A534712026864007 SEAT TRACK EMB 120 EMB120RT SO LT FR 32-39 CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK FROM FRAMES 32-39 WERE FOUND TO HAVE VARYING DEGREES OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT, TT 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004241995051200424SO 1995 5 12 C2XA95IA068 119950504A540012004499033 RIB EMB 120 EMB120RT SO LEFT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, FOUND RIBS AT LEFT MLG OUTBOARD AFT GEAR DOOR ATTACH POINTS CRACKED. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED DOUBLERS ON AFFECTED RIBS, AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (EMB-120 SRM 54-20-04). AIRCRAFT TT, 11575.6. CYC - 16,520. (X) 2L72 4T RTA31SO 19950512004251995051200425SO 1995 5 12 C2XA95IA069 119950504A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING R15 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED ADN REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT TT, 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004261995051200426SO 1995 5 12 C2XA95IA070 119950504A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING R16 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 3 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT, TT, 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004271995051200427SO 1995 5 12 C2XA95IA071 119950504A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING R16 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0940717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 4 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. AIRCRAFT, TT, 11,575.6, CYC, 16,520. (X) 2L72 4T RTA31SO 19950512004281995051200428WP 1995 5 12 HAL94039 119950125A5730 TE PANEL DOUG DC9 DC951 3022051WP LEFT WING CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13673MC 47726 SBA - ITEM FROM C-CHECK TASK CARD NR 10-5730104Y. SURFACE CORROSION UNDER LEFT FLAP TRAILING EDGE PANEL LOWER SURFACE BOLT HOLES INBOARD OF MID-FLAP HINGE. CORROSION LEVEL 2. REPAIRED PER HAL M-105 FILE NR 64027. PAINTED PER SRM 51-10-3. INSTALLED PANEL. (X) 2L72 4F A6WE 19950512004291995051200429EU 1995 5 12 M3HA95009 119950419A3350167006 EEL LAMP AEROSPATR42 ATR42320 8680930EU CABIN FAILED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13986MH 360 HNL - FLT 204 - DURING POST-FLIGHT, PILOT NOTED ONE LAMP IN THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS INOP. REPLACED LAMP. (X) 2H72 4T RTA53EU 19950512004301995051200430EU 1995 5 12 PAYA95A4020 119950427A5210 STEP FRAME AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174202G 050 PASSENGER DOOR STEP FRAME CRACKED, THREE PLACES. REPAIR IAW SRM. REPAIRS ACCOMPLISHED BY TRANS WORLD EXPRESS DURING C-CHECK. (X) 2H72 4T RTA53EU 19950512004311995051200431EU 1995 5 12 PAYA95A4021 119950427A5210 SKIN AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174202G 050 PASSENGER DOOR LOWER INNER SKIN CORRODED. REPAIRED SKIN. REPAIRS ACCOMPLISHED BY TRANS WORLD EXPRESS DURING C-CHECK. (X) 2H72 4T RTA53EU 19950512004321995051200432 1995 5 12 SWHA95004 419950413A6122 PROP GOV WOODWARD 8210263 SWRNGNSA227 SA227AC 8780603SW LT ENGINE CRACKED A SWHAE ENGINE SHUTDOWN RO PARTIAL RPM/PWR LOSS OTHER CRCRUISE 1 SW17789C 4394 180671G AC540 AUS/TYR - FLT 558 - PILOT REPORTED ON SCHEDULED FLIGHT, 10 TO 15 MINUTES PRIOR TO LANDING, THE LEFT ENGINE LOST RPM CONTROL WITH THE SPEED LEVER. THE ENGINE WAS SHUT DOWN, AND THE AIRCRAFT LANDED IN TYR WITHOUT INCIDENT. INVESTIGATION REVEALED THE SPEED SETTING LEVER PN 3655024 OF THE PROP GOVERNOR FAILED CAUSING ENGINE TO FALL TO PROP GOV LOW RPM. THE PROP GOVERNOR WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19950512004331995051200433NM 1995 5 12 TAOA059502 119950501A21503216741 PACK VALVE GARRTT BOEING727 727254 138408LNM RT PACK MALFUNCTION A TAOAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15914TS 995992 20251 WITH BOTH PACKS OFF, THE RIGHT PACK TEMP INCREASED CAUSING A PACK TRIP OFF. TURNED RIGHT PACK ON AND SELECTED WARMER TEMPERATURE-PACK TEMP COOLED DOWN. SMOKE IN CABIN AT THE TIME OF PACK TRIP. RAN BOTH PACKS, ALL OPERATED NORMALLY. RESEATED AND CLEANED C/P ON BOTH PACK VALVES. ALL APPEARS NORMAL PER MM 21-51-61. (X) 2L73 4F A3WE 19950512004341995051200434NM 1995 5 12 TWRA9529 119950501A3350 LIGHT STRIP BOEING747 747282B 1384860NM MAIN CABIN EEL INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15611FF 20502 DURING AN A-SERVICE AT GAMCO, FOUND EMERGENCY LIGHT STRIPS AT SEATS 26 ABC TO 32 ABC, 57 ABC TO 65 ABC AND 25 KJ TO 20 KJ, NOT COMING ON. REPAIRED LIGHT STRIPS, OPERATIONAL CHECK OKAY. (X) 2L74 4F A20WE 19950512004351995051200435EU 1995 5 12 9507433228 119950505A2150VFT300A1AMDTA VALVE AIRBUS320 A320211 3930320EU FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01328NW146601310 298 DURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED UNEVENTFULLY IN AN OVERWEIGHT CONDITION. MAINTENANCE DEACTIVATED THE AVIONICS VENTILATION EXTRACT VALVE AND PLACARDED PER MEL 21-26-03. THE SKIN AIR OUTLET VALVE (22HQ) WAS LATER REPLACED. OPERATIONAL CHECK OK. OPERATOR CONTROL NUMBER 9507433204 CHANGED TO 9507043228. 2L72 4F RTA28NM 19950512004361995051200436WP 1995 5 12 9507529995 119950504A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE LEFT KEEL FITTING FS 604 AT LONGERON 30. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950512004371995051200437WP 1995 5 12 9507539990 119950504A5311 FRAME DOUG DC9 DC931 3022065WP FS 1143 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE FS 1143 CANTED FRAME FORWARD OF THE INTERIOR TAILCONE RELEASE HANDLE. REPAIRED PER XEA X9-53-88. 2L72 4F A6WE 19950512004381995051200438WP 1995 5 12 9507549990 119950505A5342 ANGLE DOUG DC9 DC931 3022065WP VERT STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 3 CRACKS IN THE RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT THE AFT END. REPAIRED PER XEA X9-53-83. 2L72 4F A6WE 19950512004391995051200439WP 1995 5 12 9507559993 119950507A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN BOTH THE LEFT AND RIGHT KEEL FITTINGS FS 604. REPLACED FITTINGS PER SRM 51-01 AND DWG 5911418. 2L72 4F A6WE 19950512004401995051200440WP 1995 5 12 9507569977 119950503A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019341 47390 DURING PERIODIC CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO RELEASE THE TAILCONE AND THAT THE INTERIOR HANDLE RETAINING CLIP WAS BROKEN. ALSO, FOUND CORROSION ON THE UPPER RIGHT RELEASE CABLE END. REPLACED THE CLIP AND CABLE AND RE-RIGGED THE TAILCONE. CHECKED OK. 2L72 4F A6WE 19950512004411995051200441WP 1995 5 12 9507579160 119950506A5350 RELEASE MECH DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ADJUSTED THE CLIPS AND RE-RIGGED THE LATCHES. CHECKED OK. 2L72 4F A6WE 19950512004421995051200442NM 1995 5 12 9507582705 119950503A7930 BYPASS SWITCHES BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 2 ENGINE MALFUNCTIONED A NWAAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL01802EA 22433 695204 EN ROUTE TO MEM, THE NR 2 ENGINE OIL FILTER BYPASS WARNING ILLUMINATED. THRUST WAS REDUCED TO IDLE. THE FLIGHT CONCLUDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL FILTER BYPASS AND LOW OIL PRESSURE SWITCHES. AN INSPECTION OF THE OIL FILTER REVEALED NO METAL CONTAMINATION. THE ENGINE WAS RUNUP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950512004431995051200443NM 1995 5 12 95UAL727036 119950508A33505623543 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AFT CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297273U 21420 BOTH AFT CABIN DOORS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950512004441995051200444NM 1995 5 12 95UAL757013 119950508A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 DOOR INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29567UA 26673 DOOR NR 2 EXTERIOR EEL LIGHT INOP. RELAMPED OPS CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950512004451995051200445NE 1995 5 12 95UAL757014 219950509A7314 FUEL PUMP SUNSTRAND 7315096 BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ENGINE OIL LEAK A UALAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29547UA 0673 25368 726562 DIVERTED TO DEN UNDER AMBER ALERT WITH NR 2 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS. OIL LEAK CAUSED BY FAULTY FUEL PUMP ALLOWING OIL TO LEAK THROUGH THE WET SPLINE AREA. 2L72 4F4 FRTA2NM E17NE 19950512004461995051200446NE 1995 5 12 95UAL767017 219950509A7532 BLEED VALVE HAM/STAN MR36153 BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 ENGINE MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29646UA 25283 724376 ABORTED TAKEOFF DUE TO NR 2 ENGINE BLEED VALVE PROBLEM. REPLACED HI-STAGE VALVE. 2L72 4F4 FRTA1NM E24NE 19950512004471995051200447WP 1995 5 12 ABXA9500383 119950509A335014597101 EEL BATTERY GRIMES 60030431 DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23975AX 8688 47512 EMERGENCY LIGHTS VERY DIM. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM CHAPTER 33. OPS CHECKED GOOD. 2L72 4F A6WE 19950512004481995051200448WP 1995 5 12 ABXA9500384 119950509A335060030431 EEL POWER SUPPLY DOUG DC9 DC931 3022065WP CABIN DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23946AX 3407 47003 EMERGENCY EXIT LIGHTS COME ON WHEN AIRCRAFT POWER IS SHUT OFF, EVEN WHEN LIGHT SWITCH IS OFF. REPLACED EMERGENCY POWER SUPPLY. 2L72 4F A6WE 19950512004491995051200449SO 1995 5 12 BIER950012 219950510A73205038901223 MIXTURE CABLE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO RT ENGINE FAILED A BSYAK NONE O OTHER UKUNKNOWN 1 EA214098S TH600 FOUND MIXTURE CABLE BROKEN AT MIXTURE END ROD END ATTACH. REMOVED AND REPLACED CABLE. SUBMITTER STATES PROBLEM SEEMS TO BE FROM INSUFFICIENT LUBRICATION OF CABLE, CABLE MOVEMENT WAS EXTREMELY STIFF WHEN REMOVED. 1L72 3O3 O 3A16 E5CE 19950512004501995051200450NM 1995 5 12 DHL95708001 119950506A324526045611 TIRE BOEING727 72725 1384006NM NR 3 MLG BLOWN A DHLAO OTHER O OTHER LDLANDING 1 SO01708DH 18275 ON LANDING NR 3 TIRE BLEW ON TOUCHDOWN. REMOVED AND REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES PER MM 32-45-01. RIGHT MAIN GEAR FLYING DOOR DAMAGED. AIRCRAFT FERRIED GEAR DOWN TO CVG. 2L73 4F A3WE 19950512004511995051200451NM 1995 5 12 SCNA95093 119950505A3350900835A EEL BATTERY BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 22438 AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED GOOD. 2L73 4F RTA3WE 19950512004521995051200452NM 1995 5 12 SCNA95094 119950505A33501000677 EEL BATTERY BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 22438 L-1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPS CHECKED OK. 2L73 4F RTA3WE 19950512004531995051200453NM 1995 5 12 SCNA95095 119950501A3350S106 EEL BATTERY BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 22559 FORWARD CEILING MOUNTED AREA EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SELF-CONTAINED BATTERY. OPS CHECK GOOD IAW MM 33-50-81. 2L73 4F A3WE 19950512004541995051200454NM 1995 5 12 UPS203178 119950508A5320 CHORD BOEING727 72725C 138400HNM BS 743 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM CHORD ON UPPER SIDE AT STA 743 LBL 13 WL 154. INSTALLED REPAIR PER SRM 53-10-1, 51-40-4. 2L73 4F A3WE 19950512004551995051200455NM 1995 5 12 UPS203179 119950508A5320 BEAM BOEING727 72725C 138400HNM BS 830 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STUB BEAM AT STA 830 RBL 55 TO 65. REPLACED PER SRM 51-10-1, 51-10-2, 51-20-31. 2L73 4F A3WE 19950512004561995051200456NM 1995 5 12 UPS203180 119950508A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 845 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON SEAT TRACK O/B FLANGE AT BS 845, LBL45, WL 208. INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950512004571995051200457NM 1995 5 12 UPS203181 119950508A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 800 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL FLOORBEAM AT STA 800, LBL 45, WL 208. FLAP PEENED PER UPS EO FILE 727-57-1365. 2L73 4F A3WE 19950512004581995051200458NM 1995 5 12 UPS203182 119950508A5520 BALANCE PANEL BOEING727 72725C 138400HNM ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ELEVATOR NR 5 BALANCE PANEL WHERE WEIGHT AND HINGE CONTACT PANEL. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-1, NMM 51-20-21, 51-20-31. 2L73 4F A3WE 19950512004591995051200459NM 1995 5 12 UPS203183 119950508A5754 FLAP BOEING727 72725C 138400HNM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01. 2L73 4F A3WE 19950512004601995051200460NM 1995 5 12 UPS203184 119950508A5754 FLAP BOEING727 72725C 138400HNM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION NR 1 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01. 2L73 4F A3WE 19950512004611995051200461NM 1995 5 12 UPS203185 119950508A5754 FLAP BOEING727 72725C 138400HNM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01. 2L73 4F A3WE 19950512004621995051200462NM 1995 5 12 UPS203186 119950508A5512 PANEL BOEING727 72725C 138400HNM HORIZ STAB CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN HORIZONTAL STAB. L/E PANEL 9203, AT 4TH RIB FROM I/B EDGE. INSTALLED REPAIR PER SRM 55-10-3. 2L73 4F A3WE 19950512004631995051200463NM 1995 5 12 UPS203187 119950508A5754 FLAP BOEING727 72725C 138400HNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP ASSY. REPLACED K-FLAP ASSY PER MM 27-81-01. 2L73 4F A3WE 19950512004641995051200464NM 1995 5 12 UPS203188 119950508A5754 SLAT BOEING727 72725C 138400HNM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 SLAT. REPLACED NR 1 SLAT PER MM 27-81-32. 2L73 4F A3WE 19950512004651995051200465NM 1995 5 12 UPS203189 119950508A5320 LAP FILLER BOEING727 72725C 138400HNM BS 948 DISBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE IN C-CHECK, MAINTENANCE FOUND LAP FILLER TO BE DISBONDED AT BS 948 LBL 27 WL 142. FABRICATED AND INSTALLED NEW FILLER PER SRM 51-30-2. 2L73 4F A3WE 19950512004661995051200466 1995 5 12 UPS403190 219950508A7530 CLAMP BOEING747 747123F NM NR 2 ENGINE FAILED A IPXAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SO01671UP 20327 FLIGHT CREW REPORTED, FIRE INDICATION ON NR 2 ENGINE. SHUTDOWN ENGINE VIA CHECKLIST. ALL INDICATIONS OF FIRE OUT, FL 330, TIME 0355Z. AFTER ENGINE WAS SECURED, OIL PRESSURE MAINTAINED 18-20 PSI, DISCHARGED FIRE BOTTLE. REMOVED AND REPLACED FIRE BOTTLE PER MM 26-21-03. INSPECTED ENGINE, FOUND BLEED AIR LEAK AT PRESSURE RELIEF VALVE. REPLACED CLAMP AND LEAK CHECKED GOOD. ACCOMPLISHED INSPECTION PER MM 72-00+00 698-17, NO DEFFECTS. 2L74 4F A20WE 19950512004671995051200467NM 1995 5 12 UPS403191 119950510A3350 EEL BOEING747 747121 1384871NM FLIGHT DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01681UP 19661 MAINTENANCE REPORTED, UPPER DECK EMERGENCY LIGHTS INOP. ALL UPPER DECK EMERGENCY LIGHTS TEST GOOD, NO FAULTS NOTED. 2L74 4F A20WE 19950512004681995051200468NM 1995 5 12 UPS403193 119950508A2612 FIRE LOOPS BOEING747 747123F NM NR 2 ENGINE MALFUNCTIONED A IPXAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 SO01671UP 20327 WHILE EN ROUTE TO SNN, FLIGHT CREW REPORTED AT ALTITUDE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. INDICATIONS WERE B-LOOP SHOWING 8.7 ON THE COMPARTMENT INDICATOR. ACCOMLISHED ENGINE FIRE BOLD FACE AND CHECKLIST ITEMS IN ACCORDANCE WITH SECTION II OF THE AOM. CHANGED FOUR DUAL FIRE DETECTOR WIRES P/N 895396, 89439, 895397, 895899. CHANGED BOTH FIRE BOTTLES S/N M2200 AND M1162, FIRE TEST OK ON LOOPS A AND B. 2L74 4F A20WE 19950512004821995051200482 1995 5 12 AALA950564 419950223A2565101655304 SLIDE BFGOODRICH BOEING767 767 1385102NM PASSENGER DOOR LEAKS A AAALAK NONE O OTHER ININSP/MAINT 1 SW07 3283 LAX - DURING SHOP VISIT DEPLOYMENT, B767 EMERGENCY EVACUATION SLIDE HAD SEVERAL LARGE AREAS WITH POROSITY LEAKS. SCRAPPED EMERGENCY EVACUATION SLIDE. (X) 2L72 4F EXPA2L72 19950512004831995051200483NM 1995 5 12 95ZZZW669 119950426A21201828202 HEAT EXCHANGER BOEING737 7373Y0 1384671NM NR 1 LT PRIMARY FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP282FOR 756874 23747 PHX-ABQ - FLT NR 200 - NR 1 PACK TRIP RESET TWICE. AIRCRAFT RETURNED TO PHX WITH ALL TEMPS AND PRESSURE NORMAL, LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 PRIMARY HEAT EXCHANGER AND NR 1 PACK FLOW CONTROL VALVE DUE TO LOW FLOW. LT PACK SYSTEM OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500244. 2L72 4F RTA16WE 19950512004841995051200484NM 1995 5 12 AALA950538 119950330A3350 EEL WIRE BOEING767 767323 1385205NM CABIN LOOSE GROUND A AALAK NONE L NO TEST ININSP/MAINT 1 SW07385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 32-41 INOPERATIVE. TIGHTENED LOOSE GROUND AT M734 BATTERY PACK. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512004851995051200485NM 1995 5 12 AALA950539 119950330A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 4H INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT 4H. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512004861995051200486NM 1995 5 12 AALA950571 119950401A2810 SCREW BOEING727 727223 1384074NM NR 3 FUEL TANK LOOSE A AALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW07868AA 21373 IAD - FLT 1161 - DURING CLIMB-OUT, EN ROUTE DCA-RDU, FUEL LEAKING FROM RIGHT WING POURING OVER OUTBOARD FLAPS. AIR INTERRUPTED AND LANDED IAD WITHOUT INCIDENT. TIGHTENED NR 15 AND 16 FUEL ACCESS PANEL SCREWS ON NR 3 TANK. INSTALLED TWO MISSING SCREWS ONE ON EACH PANEL. ACCOMPLISHED FCF, SYSTEM CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950512004871995051200487WP 1995 5 12 AALA950574 119950401A3350A3060720102 LIGHT STRIP DOUG DC10 DC1010 3022110WP CABIN INOPERATIVE A AALAK NONE L NO TEST TXTAXI/GRND HDL 1 SW07162AA 46943 HNL - PRIOR TO DEPARTURE EMERGENCY EXIT FLOOR PATH LGHTS AT ZONES A AND B ON RIGHT SIDE ILLUMINATED INTERMITTENTLY. DRIED MOISTURE AROUND MID GALLEY AT RIGHT SIDE. CLEANED AREA AROUND EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950512004881995051200488WP 1995 5 12 AALA950600 119950409A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07471AA 49601 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 12 AND 16 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950512004891995051200489NM 1995 5 12 AALA950602 119950407A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROW 7AB TO 12AB INOPERATIVE. RESEATED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 7AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA1NM 19950512004901995051200490NM 1995 5 12 AALA950604 119950407A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07630AA 24588 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATAIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA2NM 19950512004911995051200491NM 1995 5 12 AALA950606 119950407A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077375A 25202 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7H AND 21H INTERMITTENT. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT ROW 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950512004921995051200492WP 1995 5 12 AALA950626 119950409A326092278982 GEAR SWITCH DOUG DC9 DC982 3022082WP INSTR PANEL DEFECTIVE A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW0733502 49739 MIA - FLT NR 041 - DURING APPROACH TO MIA WHEN LANDING GEAR HANDLE LOWERED, ALL LANDING GEAR LIGHTS ILLUMINATED AND REMAINTED RED. RECYCLED LANDING GEAR AND LANDING GEAR EXTENDED WITH NO ABNORMAL INDICATIONS. AIRCRAFT LANDED MIA WITHOUT INCIDENT. REPLACED LANDING GEAR HANDLE SWITCH AND LUBRICATED ALL LANDING GEARS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950512004931995051200493NM 1995 5 12 AALA950628 119950409A532065561502 DOOR FRAME BOEING727 727223 1384074NM FORWARD GALLEY CRACKED A AALAK NONE O OTHER CRCRUISE 1 SW07871AA 21383 TUL - FLT 1393 - EN ROUTE DFW/TUL DURING CRUISE, AIR LEAK NOTED AT FORWARD GALLEY DOOR. AIRCRAFT LANDED TUL WITHOUT INCIDENT. CHECKED FORWARD GALLEY DOOR AREA AND FOUND UPPER AFT CORNER AREA OF DOOR SKIN BULGING OUT AND DOOR FRAME CRACKED FROM GATE HINGE DOWN APPROXIMATELY 6 INCHES. REPLACED FORWARD GALLEY DOOR. ACCOMPLISHED PRESSURIZATION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950512004941995051200494NM 1995 5 12 AALA950646 119950412A3350R70 EEL RELAY BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07880AA 21519 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ILLUMINATED WHEN SYSTEM ARMED. REPLACED EMERGENCY EXIT LIGHT RELAY R70. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950512004951995051200495NM 1995 5 12 AWXA9500244 119950426A21203964421 VALVE BOEING737 7374Y0 1384705NM PACK FLOW MALFUNCTION A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP282FOR 741 23747 PHX-ABQ - FLT NR 200 - NR 1 PACK TRIP RESET TWICE. AIRCRAFT RETURNED TO PHX WITH ALL TEMPS AND PRESSURE NORMAL, LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 PRIMARY HEAT EXCHANGER AND NR 1 PACK FLOW CONTROL VALVE DUE TO LOW FLOW. LT PACK SYSTEM OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE 95ZZZW669. 2L72 4F RTA16WE 19950512004961995051200496NM 1995 5 12 AWXA9500248 119950427A3350900835A BATTERY PACK BOEING737 737275 1384485NM CABIN EEL INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS IN FORWARD SECTION INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F A16WE 19950512004971995051200497NM 1995 5 12 CAL950275 119950411A5320 INTERCOSTAL BOEING727 727224 1384076NM BS 984 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL UPPER FLANGE AT BS 984, LBL 37. THE INTERCOSTAL WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-3-0. (W) 2L73 4F A3WE 19950512004981995051200498NM 1995 5 12 CAL950276 119950411A5313 STRINGER BOEING727 727224 1384076NM STA 420-440 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT STRINGER 28R BETWEEN STATION 420 AND 440. THE CRACKED AREA WAS CUT OUT AND CHANNEL FILLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (W) 2L73 4F A3WE 19950512004991995051200499NM 1995 5 12 CAL950277 119950411A5320 ANGLE BOEING727 727224 1384076NM STA 440 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND DOOR SILL ANGLE AND NUT PLATES CORRODED INSIDE WEB AT STATION 440, STRINGER 25R. THE CORROSION AND ANGLE WERE REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-1-21A. (W) 2L73 4F A3WE 19950512005001995051200500NM 1995 5 12 CAL950278 119950411A5320 SUPPORT BOEING727 727224 1384076NM L-2 DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (W) 2L73 4F A3WE 19950512005011995051200501NM 1995 5 12 CAL950279 119950411A5313 STRINGER BOEING727 727224 1384076NM STA 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND STRINGER 23R IN AFT PIT AT STA 1130 CORRODED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 53-10-3, AND 51-30-2. (W) 2L73 4F A3WE 19950512005021995051200502NM 1995 5 12 CAL950280 119950411A5320 FLOOR SUPPORT BOEING727 727224 1384076NM STA 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND CORROSION UNDER FLOOR SUPPORT AT STA 312. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-4. A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4. (W) 2L73 4F A3WE 19950512005031995051200503NM 1995 5 12 CAL950281 119950411A5313 STRINGER BOEING727 727224 1384076NM STA 446 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND STRINGER 27R CORRODED AT STA 446. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W) 2L73 4F A3WE 19950512005041995051200504NM 1995 5 12 CAL950282 119950411A5320 DOOR SILL BOEING727 727224 1384076NM AFT AIRSTAIR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND THE AFT AIRSTAIR DOOR SILL CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (W) 2L73 4F A3WE 19950512005051995051200505NM 1995 5 12 CAL950283 119950411A5730 SKIN BOEING727 727224 1384076NM NR 4 SLAT ACT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974941155 22451 GSO - INSPECTION FOUND A .375 INCH CRACK AND A DENT IN THE LEFT WING NR 4 SLAT ACTUATOR CUT OUT. A REPAIR DOUBLER WAS FORMED AND INSTALLED IAW EC5762-01020 AND SRM 51-30-2. (W) 2L73 4F A3WE 19950512005061995051200506WP 1995 5 12 CAL950293 119950418A335020131A BATTERY PACK DOUG DC9 DC982 3022082WP EEL LT ROW 26 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW09478AC 48063 FLT 182 - IAH - INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS AFT OF ROW 26 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. (W) 2L72 4F A6WE 19950512005071995051200507EU 1995 5 12 CAL950308 119950420A2910A5705441 LINE AIRBUS300 A300B4203 3930306EU RT MLG LEAKING A CALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW0914966 117 FLT 0474 - GSO - THE GREEN SYSTEM HYDRAULIC QUANTITY DECREASED SLOWLY INTO THE RED BAND WHILE IN FLIGHT. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE ON THE RT MLG LEAKING. THE HYDRAULIC LINE WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (W) 2L72 4F A35EU 19950512005081995051200508WP 1995 5 12 CAL950323 119950406A5313 LONGERON DOUG DC10 DC1010 3022110WP FS 1964 47L CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0968047 47801 KUL - C-CHECK INSPECTION, FOUND CORROSION AT LONGERON 47L AT STATION 1964 (AFT CARGO COMPT). CORROSION REMOVED AND REPAIRED PER ECRA5310-03089. (W) 2L73 4F A22WE 19950512005091995051200509WP 1995 5 12 CAL950324 119950418A3250 STEERING DOUG DC9 DC981 3022081WP NLG UNSECURED A CALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0914880 48044 KUL - DURING TAXI OUT STEERING HAD TO MUCH PLAY. REPLACED NLG TIRES AND SECURED STEERING PER MM 32-21-04. NO FURTHER INCIDENT. (W) 2L72 4F A6WE 19950512005101995051200510NM 1995 5 12 CAL950325 119950420A5347 SUPPORT ANGLE BOEING737 7373T0 1384582NM SEAT TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHN - SEAT TRACK ANGLE SUPPORT CRACKED AT OUTBOARD END SIDE OF WEB FS 519 LBL 24.75 .5 INCH IN LENGTH. INSTALLED ANGLE REPAIR PER IAW ECRA 5320-01239. (W) 2L72 4F RTA16WE 19950512005111995051200511NM 1995 5 12 CAL950326 119950420A5320 SUPPORT CHANNEL BOEING737 7373T0 1384582NM FS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - SUPPORT CHANNEL CRACKED AFT SIDE OF FLOOR BEAM AT FS 520 LBL 24.75 LENGTH OF CRACK .74 INCH. REPAIRED PER IAW ECRA 5320-01239. (W) 2L72 4F RTA16WE 19950512005121995051200512NM 1995 5 12 CAL950327 119950420A5315 FLOOR BEAM BOEING737 7373T0 1384582NM FS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - FLOOR BEAM CRACKED NEAR TOP OF WEB FS 520 LBL 24.75 APPROXIMATE LENGTH IS .75 INCH. INSTALLED REPAIR ANGLE PER IAW ECRA 5320-01234. (W) 2L72 4F RTA16WE 19950512005131995051200513NM 1995 5 12 CAL950328 119950420A5320 SUPPORT CHANNEL BOEING737 7373T0 1384582NM FS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - SUPPORT CHANNEL CRACKED AFT OF FLOOR BEAM FS 520 LBL 45.5 APPROXIMATE LENGTH 1 INCH. REPAIRED PER IAW ECRA 5320-01239 REPLACED. (W) 2L72 4F RTA16WE 19950512005141995051200514NM 1995 5 12 CAL950329 119950420A5315 BEAM BOEING737 7373T0 1384582NM FS 520 WEB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - FLOOR BEAM TOP OF WEB CRACKED FS 520 LBL 45.5. INSTALLED REPAIR ANGLE PER IAW ECRA 5320-01239. (W) 2L72 4F RTA16WE 19950512005151995051200515NM 1995 5 12 CAL950330 119950420A5320 SUPPORT CHANNEL BOEING737 7373T0 1384582NM FS 520-RBL 45 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - SUPPORT CHANNEL CRACKED AFT OF FLOOR BEAM FS 520 RBL 45.5 LENGTH APPROXIMATELY 1 INCH. REPAIRED PER IAW ECRA 5320-01239 REPLACED. (W) 2L72 4F RTA16WE 19950512005161995051200516NM 1995 5 12 CAL950331 119950424A5315 BEAM BOEING737 7373T0 1384582NM FS 520 RBL 45 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - FLOOR BEAM CRACKED NEAR TOP OF WEB FS 520 RBL 45.5 LENGTH OF CRACK APPROXIMATELY .75 INCH. INSTALLED REPAIR ANGLE PER IAW ECRA 5320-01239. (W) 2L72 4F RTA16WE 19950512005171995051200517NM 1995 5 12 CAL950332 119950420A5320 SUPPORT ANGLE BOEING737 7373T0 1384582NM FS 519 RBL 24 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - TRACK SUPPORT ANGLE CRACKED AT END ON INBOARD SIDE OF WEB FS 519 RBL 24.75 CRACK APPROXIMATELY .375 INCH. REPAIRED BY INSTALLED REPAIR ANGLE PER SRM 53-30-51. (W) 2L72 4F RTA16WE 19950512005181995051200518NM 1995 5 12 CAL950333 119950420A5320 SUPPORT ANGLE BOEING737 7373T0 1384582NM FS 519 RBL 45 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - TRACK SUPPORT ANGLE CRACKED END INBOARD SIDE FS 519 RBL 45.5 CRACKED APPROXIMATE .375 INCH MANUFACTURE AND INSTALLED ANGLE REPAIR PER SRM 51-70-11. (W) 2L72 4F RTA16WE 19950512005191995051200519NM 1995 5 12 CAL950334 119950420A5510 FITTING BOEING737 7373T0 1384582NM H STAB STA 1121 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 DHM - FITTING CRACKED ON HORIZONTAL STABILIZER CENTER SECTION, STATION 1121 BL 12R AFT END OF FITTING CRACKED .25 INCH. REMANUFACTURE NEW FITTING PER SRM 55-10-3. (W) 2L72 4F RTA16WE 19950512005201995051200520NM 1995 5 12 CAL950335 119950420A5311 FRAME BOEING737 7373T0 1384582NM FS 460 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0916301 23352 FORWARD BAGGAGE FRAME CRACKED AT STRINGER LEVEL, STRINGER 27R TO STRINGER 28R, STATION 460 CRACK LENGTH .75 INCH. REPAIR IAW 53-00-07 FIG 204 MANUFACTURE FRAME, CLIP HEAT TREATED, DRILLING, DEBURR, ALODINE, PRIME AND INSTALLED. (W) 2L72 4F RTA16WE 19950512005211995051200521WP 1995 5 12 CAL950338 119950427A27203772374 S/O VALVE DOUG DC9 DC932 3022066WP RUDDER LEAK A CALAO OTHER K FLUID LOSS LDLANDING 1 SW0914524300151469 47539 FLT NR 1581 - IAH - UPON LANDING FOUND HYDRAULIC FLUID LEAKING AT RUDDER. FOUND RUDDER POWER SHUTOFF VALVE LEAKING. REPLACED SHUTOFF VALVE NO FURTHER ACTION. (W) 2L72 4F A6WE 19950512005221995051200522NM 1995 5 12 95ZZZZ228 119950311A5711 SPAR BOEING747 747131 1384881NM WS 675.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059310795376 19673 FCO - DURING PERIODIC CHECK, FOUND A NINE INCH CRACK IN RT WING FRONT SPAR AT FSSI 675.5. REPAIRED CRACK PER BOEING REPAIR DRAWING 691U0103 AND TWA ARA 9122. TOTAL CYCLES 17,425. (Z) 2L74 4F A20WE 19950512005231995051200523NM 1995 5 12 95ZZZZ229 119950310A5313 STRINGER BOEING727 727231 1384079NM FS 656.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05523116647566475 19830 MCI - DURING CHECK-C, FOUND A ONE-INCH LONG CRACK IN STRINGER 16, STA 656.5. REPAIRED PER SRM 57-20-201 FIG 207. TOTAL CYCLES 45,150. (Z) 2L73 4F A3WE 19950512005241995051200524NM 1995 5 12 95ZZZZ230 119950310A5311 FRAME BOEING727 727231 1384079NM FS 783.95 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055231166475 19830 MCI - DURING CHECK-C, FOUND A ONE INCH CRACK IN FUSELAGE FRAME, FS 783.95. REPAIRED PER SERVICE BULLETIN 727-53-0197, DRAWING NR 65C36280 AND EMLR 65639. TOTAL CYCLES 45,150. (Z) 2L73 4F A3WE 19950512005251995051200525NM 1995 5 12 ASAA9510023 119950404A5315 FLOORBEAM BOEING737 737290C 138448VNM BS 807 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND IN THE FASTENER HOLES OF THE UPPER FWD AND AFT FLANGE OF THE FLOORBEAM AT BS 807, LBL 22 AND 27. REMOVED CORROSION PER EA 5310-01343 AND BOEING TELEX ASA-SEA-95-0199RR. (Z) 2L72 4F A16WE 19950512005261995051200526NM 1995 5 12 ASAA9510024 119950404A5315 FLOORBEAM BOEING737 737290C 138448VNM BS 420 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND AT A FASTENER HOLE ON THE UPPER CHORD FWD FLANGE OF THE FLOORBEAM AT BS 420 LBL 50. REMOVED CORROSION PER EA 5310-01341 AND BOEING TELEX ASA-SEA-95-0204RR. (Z) 2L72 4F A16WE 19950512005271995051200527NM 1995 5 12 ASAA9510025 119950404A5314 KEEL BEAM BOEING737 737290C 138448VNM BS 661-726 DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, FASTENERS WERE FOUND TO BE PULLING THROUGH A REPAIR STRAP ON THE LOWER SKIN OF THE KEEL BEAM BETWEEN BS 661 AND 726. REPAIRED PER EA 5330-01187 AND BOEING TELEX ASA-SEA-94--0146RR. (Z) 2L72 4F A16WE 19950512005281995051200528NM 1995 5 12 ASAA9510027 119950406A5315 FLOORBEAM BOEING737 737290C 138448VNM BS 847 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE BOTTOM SURFACE OF THE LOWER FWD FLANGE OF THE FLOORBEAM AT BS 847, RBL 26 TO RBL 61. REPAIRED PER EA 5310-01337 AND BOEING TELEX ASA-SEA-95-019RR. (Z) 2L72 4F A16WE 19950512005291995051200529NM 1995 5 12 ASAA9510031 119950407A531565549073 FLOORBEAM BOEING737 737290C 138448VNM BS 767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE BOTTOM SURFACE OF THE LOWER FWD FLANGE OF THE FLOORBEAM AT BS 767 BETWEEN RBL 26 AND RBL 44. REPAIRED PER EA 5310-01336 AND BOEING TELEX ASA-SEA-95-018RR. (Z) 2L72 4F A16WE 19950512005301995051200530EU 1995 5 12 RAIA950424 119950414A3350OL60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03425TE 125 STL - LOWER EMERGENCY LIGHT BY SERVICE DOOR HAS BULBS THAT ARE OUT. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (Z) 2H72 4T RTA53EU 19950512005311995051200531EU 1995 5 12 RAIA950427 119950418A7722CA3108R12S3SF80 CONNECTOR BAG JETSTMJETSTM3201 1500217EU NR 2 NAC FAILED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03436AM 891 STL - FLT 7086 - THE NR 2 ENGINE EGT FLUCTUATION. REPLACED T2 SENSOR CANNON PLUG. (Z) 2L72 4T RTA56EU 19950512005321995051200532EU 1995 5 12 RAIA950429 119950420A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU NR 2 ENG INOP A RAIAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 CE03343TE 955 SBN - FLT 7491 - THE NR 2 GENERATOR WENT OFF LINE. REPLACED STARTER GENERATOR. (Z) 2L72 4T RTA56EU 19950512005331995051200533EU 1995 5 12 RAIA950430 119950423A30402315M131 WIPER BAG JETSTMJETSTM3201 1500217EU RT BROKEN A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03430AM 880 STL - FLT 7029 - RIGHT WINDSCREEN WIPER BROKEN. REPLACED WIPER. (Z) 2L72 4T RTA56EU 19950512005341995051200534SO 1995 5 12 RAIA950432 119950421A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A ARAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03131AM 120158 TYS - FLT 7483 - FLAP DISSAGREEMENT DURING CLIMB. REPLACED RIGHT O/B FLAP ACTUATOR. (Z) 2L72 4T RTA31SO 19950512005351995051200535EU 1995 5 12 UF6A950408 119950416A2750ZS0030501 SWITCH BAG ATP ATP EU TE FLAPS DIRTY A UF6AO OTHER J WARNING INDICATION CRCRUISE 1 CE03854AW 2028 ORD - FLT 5030 - FLAP CENTRAL WARNING PANEL ILLUMINATED IN FLIGHT. MAINTENANCE CLEANED FLAP PROXIMITY CG24, CG25, CG34, CG35. (Z) 2L72 4T RTA27NM 19950512005361995051200536EU 1995 5 12 UF6A950409 119950419A2750D9311 CONTACTOR BAG ATP ATP EU TE FLAPS FAILED A AUF6AO OTHER J WARNING INDICATION LDLANDING 1 CE03852AW 2021 CWA - FLT 5033 - FLAPS WILL NOT EXTEND. MAINTENANCE REPLACED FLAP REVERSING CONTACTOR CG-9. (Z) 2L72 4T RTA27NM 19950512005371995051200537EU 1995 5 12 UF6A950410 119950419A2430SX7EK6 CONTACTOR BAG ATP ATP EU E/E COMPT FAILED A UF6AO OTHER O OTHER TXTAXI/GRND HDL 1 CE03859AW 2036 SBN - FLT 777 - THE NR ONE NON-ESSENTIAL BUSBAR TRIPPED OFF LINE. MAINTENANCE REPLACED THE NR 1 NON-ESSENTIAL CONTACTOR (PH-6). (Z) 2L72 4T RTA27NM 19950512005381995051200538 1995 5 12 UF6A950411 419950420A23102TC431250767 CIRCUIT BREAKER BAG ATP ATP EU CB PANEL POPPED A UF6AO OTHER O OTHER CRCRUISE 1 CE03851AW 2020 ORD - FLT 5018 - COMMUNICATIONS FAILED IN NORMAL MODE. MAINTENANCE RESET CIRCUIT BRAKER E25. (Z) 2L72 4T RTA27NM 19950512005391995051200539EU 1995 5 12 UF6A950412 119950420A33506013211 EEL POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03860AW 2037 ORD - THE EMERGENCY LIGHTS ARE INOP AT THE CENTER OF THE FUSELAGE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. (Z) 2L72 4T RTA27NM 19950512005401995051200540WP 1995 5 12 WRLA95016 119950419A2910P11593 CONNECTOR DOUG DC10 DC1030F 3023504WP NR 3 HYD SYS FAILED A WRLAD RETURN TO BLOCK FJ FLT CONT AFFECTED WARNING INDICATION TXTAXI/GRND HDL 1 EA27107WA 46836 DURING TAXI, FLIGHT CREW PERFORMED FLIGHT CONTROL DEFLECTION CHECK, DID NOT GET FULL DEFLECTION OF SPOILERS. CREW ELECTED TO RETURN TO GATE FOR TROUBLESHOOTING/CORRECTION. ACFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND CONNECTOR PIN PUSHED BACK IN CANNON PLUG TO NR 3 HYDRAULIC SYSTEM FLIGHT CONTROL BYPASS VALVE. PIN/WIRE WAS REPAIRED. OPS CHECK PERFORMED WITH NO MALFUNCTION NOTED. ACFT RETURNED TO SERVICE. (Z) 2L73 4F RTA22WE 19950512005411995051200541NM 1995 5 12 9507595516 119950428A5347 SUPPORT BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01516US 23204 DURING PERIODIC CHECK, FOUND CORROSION IN SEAT TRACK SUPPORT FS 365, RBL 45.5. REPAIRED PER EA 55-98202. MFG PART NUMBER 141N5131-4. 2L72 4F RTA2NM 19950512005421995051200542EU 1995 5 12 9507603208 119950428A5313D53231204200 LONGERON AIRBUS320 A320211 3930320EU FS 14300/14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01308US 107 DURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON LONGERON 44 OUTER FLANGE BETWEEN FR 33 TO 34. REPLACED LONGERON 44 PER EA 32-97859. 2L72 4F RTA28NM 19950512005431995051200543WP 1995 5 12 9507611158 119950428A5347 SEAT TRACK DOUG DC10 DC1040 3023508WP FS 1521 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CORROSION ON SEAT TRACK LBL 107, FS 1521. REPAIRED PER EA 11-98049. 2L73 4F A22WE 19950512005441995051200544WP 1995 5 12 9507621158 119950501A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD CARGO FLOOR FRAME FLANGE FS 879, LBL 38. REPAIRED PER EA 11-98027. MFG PART NUMBER ADA7034-3. 2L73 4F A22WE 19950512005451995051200545WP 1995 5 12 9507639989 119950502A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE APB T-FITTING AND BULKHEAD SKIN FS 996, LBL 38 TO BL 0 AND RBL 18. REPAIRED PER EA 99-094812. MFG PART NUMBER 5910130-65. 2L72 4F A6WE 19950512005461995051200546WP 1995 5 12 9507641158 119950502A5320 WEB DOUG DC10 DC1040 3023508WP FS 1900/1928 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CORROSION ON FLOOR WEB AND DOUBLER FS 1900 TO 1928, LBL 107. REPAIRED PER EA 11-98053. MFG PART NUMBER AGA3807-5. 2L73 4F A22WE 19950512005471995051200547NM 1995 5 12 9507655518 119950507A5315141N5111 FLOORBEAM BOEING757 757251 1384970NM FS 345 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01518US 23206 DURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD FS 345 FROM LBL 10 TO LBL 24. REPAIRED PER EA 55-98208. 2L72 4F RTA2NM 19950512005481995051200548WP 1995 5 12 9507661158 119950507A5320 PAN DOUG DC10 DC1040 3023508WP FS 1980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN INNER SURFACE FS 1980. REPAIRED PAN PER EA 11-98056. MFG PART NUMBER AGA3098-501. 2L73 4F A22WE 19950512005491995051200549WP 1995 5 12 9507679916 119950508A5313 LONGERON DOUG DC9 DC932 3022066WP FS 980/996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 23R END FITTING FS 980 TO 996. REPLACED FITTING AND REPAIRED LONGERON PER SRM 53-02 PG 3. 2L72 4F A6WE 19950512005501995051200550WP 1995 5 12 9507689604 119950508A5530 FITTING DOUG DC9 DC932 3022066WP VERT STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 3 INCH CRACK IN THE VERTICAL STABILIZER LOWER FORWARD RIGHT SPAR FITTING. REPLACED FITTING PER SRM 51-30-00. MFG PART NUMBER 5920103-2. 2L72 4F A6WE 19950512005511995051200551WP 1995 5 12 9507699604 119950508A5320 FITTINGS DOUG DC9 DC932 3022066WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 26L, 27L, 28L, 29L, AND 30 END FITTINGS FS 604. REPLACED FITTINGS PER SRM 51-00-00. 2L72 4F A6WE 19950512005521995051200552WP 1995 5 12 9507709995 119950508A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 23L END FITTING AT FS 996. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950512005531995051200553NM 1995 5 12 9507715518 119950508A5414 SKIN BOEING757 757251 1384970NM PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01518US 23206 DURING PERIODIC CHECK, FOUND CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN AT THE CUTOUT FOR ACCESS PANEL 433AL. REPAIRED PER EA 55-98206. MFG PART NUMBER 311N3450-15. 2L72 4F RTA2NM 19950512005541995051200554WP 1995 5 12 9507729105 119950505A5755 RIB DOUG DC9 DC915 3022036WP SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0195S 47205 DURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD SPOILER FITTING (RIB CAP). REPLACED RIB CAP. 2L72 4F A6WE 19950512005551995051200555WP 1995 5 12 9507739993 119950509A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 29R END FITTING AT FS 604. REPLACED FITTING PER SRM 51-01 AND DWG 5911418. 2L72 4F A6WE 19950512005561995051200556SO 1995 5 12 COM11883 119950507A3246MS2125005016 BOLTS BFGOODRICH 314461 EMB 120 EMB120RT SO LT MLG WHEEL BROKEN A ACOMAK NONE O OTHER UKUNKNOWN 1 SO01156CA339 339 2280 120156 LEFT MAIN INBOARD WHEEL S/N 2280 HAD 6 WHEEL HALVE BOLTS SHEARED AND TIRE IS FLAT. DISASSEMBLED WHEEL ASSY, CLEANED AND INSPECTED WHEEL HALVES VISUALLY, NO DEFECTES NOTED. EDDY CURRENT WHEEL ASSY AND BOLT HOLES, NO DEFECTS NOTED. 2L72 4T RTA31SO 19950512005571995051200557SO 1995 5 12 COM11884 119950511A61207757151 BALLSCREW SERVO HAMSTD 78249012 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE RED GEARBOX DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01168CA 900755 120168 115566 910344 WHILE PERFORMING HAMILTON STANDARDS S/B 14RF-9-61-A53 REV S, FOUND THE SPLINES OF THE BALLSCREW SERVO WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. THE PCU WAS SENT TO HAMILTON STANDARD FOR FURTHER EVALUATION. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 19950512005581995051200558SO 1995 5 12 COM11885 119950509A32463006041 WHEEL BFGOODRICH 314461 EMB 120 EMB120RT SO MLG WORN A COMAK NONE O OTHER ININSP/MAINT 1 SO01268CA4057 430 2740 120262 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INSERT LOOSE ON KEY BOSS. INBOARD SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO BFG FOR REPAIR OR WARRANTY. 2L72 4T RTA31SO 19950512005591995051200559SO 1995 5 12 COM11886 119950509A29163D237225 RESERVOIR EMB 120 EMB120RT SO LT/RT HYD SYST DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01463CA7200 6318 120267 LEFT AND RIGHT HYDRAULIC RESERVOIR LOW PRESSURE WARNINGS ILLUMINATED. REPLACED THE RESERVOIRS AIR PRESSURE REGULATOR. 2L72 4T RTA31SO 19950512005601995051200560SO 1995 5 12 COM11887 119950509A3241N610628023 RELAY EMB 120 EMB120RT SO ANTI-SKID SYST DEFECTIVE A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01266CA 120258 ANTI-SKID INOP LIGHTS ILLUMINATED DURING LANDING GEAR RETRACTION. REPLACED RELAY KO255. 2L72 4T RTA31SO 19950512005611995051200561EU 1995 5 12 COM31076 119950510A3250 STEERING SAAB SF340 SF340A 7850100EU NLG OUT OF ADJUST A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01340SF 340A014 NOSE WHEELS TURNED 180 DEGREES TO THE LEFT. REPOSITIONED NOSE WHEELS, INSPECTED SYSTEM AND FOUND TO BE SERVICEABLE. AIRCRAFT CONTINUED SERVICE. 2L72 4T RTA52EU 19950512005621995051200562EU 1995 5 12 COM31077 119950508A32465009237 WHEEL 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN RACE A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 8879 309 DEC910118 340A140 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN AND FOUND REPAIR BUSHING ALREADY HAD BEEN INSTALLED ONCE. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS. 2L72 4T RTA52EU 19950512005631995051200563EU 1995 5 12 COM31078 119950510A32465009237 WHEEL 5010488 SAAB SF340 SF340A 7850100EU LT MLG DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01357CA AUG930544 340A044 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950512005641995051200564EA 1995 5 12 COM60469 119950509A5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA RIGHT SHATTERED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01937CA1760 7044 RT WINDSHIELD SHATTERED AT 39,000 FEET. REPLACED WINDSHIELD. 2L72 4F RTA21EA 19950512005651995051200565NE 1995 5 12 DL757952017 219950507A732178360014068 EEC BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A DALAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SO11625DL 22915 716536 ON DESCENT INTO MSP, NR 2 ENGINE FLAMED-OUT, HAD SUCCESSFULL RESTART, LANDED MSP. PER FIM REPLACED EEC, ALT AND RT PDIU PER M/M. RUN UP OK PER M/M. 2L72 4F4 FRTA2NM E17NE 19950512005661995051200566WP 1995 5 12 DLL13952029 119950509A2100 SEPARATOR BAG LKHEED1011 10113851 5265010WP NR 2 PACK DIRTY A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11787DL 193A1126 ON CLIMBOUT, HAD HEAVY FUMES IN REAR HALF OF AICRAFT, HAD WING AND ENGINE ANTI-ICE ON. INSPECTED APU/ENG INLETS AND ACMS FOR OIL LEAKS, PERFORMED WING AND NOSE COWL ANTI-ICE TEST, COULD NOT DUPLICATE. SUBSEQUENT FLIGHT HAD ODOR AGAIN, DETERMINED IT WAS FROM NR 2 PACK. REPLACED DIRTY WATER SEPARATOR BAG FOR NR 2 PACK, NO ODOR NOTED RETURNED TO SERVICE. 2L73 4F A23WE 19950512005671995051200567NM 1995 5 12 DLM88952012 119950508A2913290051502 HYD PUMP DOUG MD88 MD88 3023688NM NR 1/2 ENGINE FAILED A DALAO OTHER JK WARNING INDICATION FLUID LOSS DEDESCENT 1 SO11977DL 53258 AT TOP OF DESCENT, WITH POWER BACK LT HYD PRESS LOW MSG ILL. LT HYD PRESS READ 0, LT HDY QTY WENT FROM 5 TO 17-C/W HYD PRESS LOW ABNORMAL. AS SOON AS AUX/TRANSFER PUMPS WERE TURNED ON. RT HYD PRESS WENT TO 0, RT HYD QTY READ 14, TURNED OFF AUX/TRANSFER PUMPS. CA-FOUND LEFT REVERSER LINE LEAKING. REPLACED SAME AND REPLACED NR 1 AND NR 2 ENG DRIVEN HYD PUMPS AND REPLACED ASSOCIATED FILTERS. 2L72 4F RTA6WE 19950512005681995051200568 1995 5 12 DLM88952028 419950508A344220412170416 RADAR DOUG MD88 MD88 3023688NM EE COMPT FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11949DL 49880 DURING CLIMBOUT, HAD TWO AIR TURNBACKS DUE TO FAILURE OF WEATHER RADAR. REPLACED AHARS, TRSCVR AND ANTENNA. OPERATION NORMAL. 2L72 4F RTA6WE 19950512005691995051200569 1995 5 12 QXEA9500137 319950508A6110D51143 TRANSFER TUBE DORNERDO32 DO328100 2996000NM PROP BROKEN A QXEAK NONE O OTHER ININSP/MAINT 1 NM09336PH 3014 PDX - PROPELLER TRANSFER TUBE FOUND BROKEN DURING REMOVAL. THE TUBE WAS BROKEN AT THE PROP END THROUGH THE LOCKING BOLT SLOT. NO ABNORMAL PROPELLER OPERATION WAS NOTED BY FLIGHT CREW. PROPELLER AND PCU WERE INSPECTED AND NO DEFECTS WERE NOTED. TRANSFER TUBE REPLACED AND PROP OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT AND PROPELLER MANUFACTURER NOTIFIED OF THE PROBLEM. 2H72 4T RTA45NM 19950512005701995051200570EU 1995 5 12 QXEA9500141 119950509A3310 LIGHTS FOKKERF28 F28MK1000 4990808EU COCKPIT MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09466US 11075 SEA - SMOKE SMELL IN COCKPIT, MAIN INSTRUMENT PANEL CIRCUIT BREAKER POPPED. LIGHTS PLACED ON MEL 33-01. 2L72 4F RTA20EU 19950512005711995051200571EU 1995 5 12 QXEA9500142 119950510A33500L301BPE EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 GEG - EMERGENCY LIGHT OUT AT SEAT 8A. REPLACED BULBS AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE, 2L72 4F RTA20EU 19950512005721995051200572EU 1995 5 12 QXEA9500143 119950510A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - TWO OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BULBS AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950512005731995051200573EU 1995 5 12 QXEA9500144 119950510A3350 EEL WIRE FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 GEG - EMERGENCY EXIT LIGHT ON SEAT 8B INOP. REPAIRED BROKEN WIRE UNDER SEAT 8B. LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950512005741995051200574NM 1995 5 12 UPS203194 119950509A5753 FLAP BOEING727 72762C 138402CNM RT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01913UP 19245 MAINTENANCE REPORTED, RT I/B FLAP T/E DELAMINATED. ACCOMPLISHED REPAIR PER UPS EO B727-5750-3081B. 2L73 4F A3WE 19950512005751995051200575NM 1995 5 12 UPS203195 119950509A5755 SPOILER BOEING727 72727C 138400JNM NR 3 DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 MAINTENANCE REPORTED, NR 3 FLIGHT SPOILER DELAMINATED AT FWD CORNERS. REPLACED NR 3 SPOILER PER SRM 27-61-01. 2L73 4F A3WE 19950512005761995051200576WP 1995 5 12 UPS803196 119950510A5311 FRAME DOUG DC8 DC873F 302199FWP FS 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME FS 1000, BETWEEN LONGERONS 35L TO 35R. INSTALLED REPAIR PER UPS EO DC8-5310-6966A. 2L74 4F RT4A25 19950512005771995051200577WP 1995 5 12 UPS803197 119950510A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING L/E, UPPER SURFACE, APPROX 12 FROM I/B SLOT, 28 FWD OF FRONT SPAR. INSTALLED REPAIR PER SRM 57-20-0. 2L74 4F RT4A25 19950512005781995051200578WP 1995 5 12 UPS803198 119950510A5400 FITTING DOUG DC8 DC873F 302199FWP NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 2 PYLON FOOT STOOL FITTING AT LWR I/B CORNER. REPLACED FITTING PER UPS EO FILE NR DC8-57-0551. 2L74 4F RT4A25 19950512005791995051200579WP 1995 5 12 UPS803199 119950510A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK (2EA) ON RT WING L/E LWR SURFACE AT XFS 591 AND 240. REPLACED SKIN PER SRM 57-2-0. 2L74 4F RT4A25 19950512005801995051200580WP 1995 5 12 UPS803200 119950510A5712 LE RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON 3 RIBS ON LT WING L/E AT XFS 291, 354, AND 201. REPAIRED RIBS PER SRM 57-2-0. 2L74 4F RT4A25 19950512005811995051200581WP 1995 5 12 UPS803201 119950510A5730 SKIN DOUG DC8 DC873F 302199FWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING L/E UPPER SKIN, STA XFS 285. REPAIR SKIN PER SRM 57-20-0. 2L74 4F RT4A25 19950512005821995051200582WP 1995 5 12 UPS803202 119950510A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E LWR SURFACE XFS 320. REPAIRED SKIN PER SRM 57-2-1. 2L74 4F RT4A25 19950512005831995051200583WP 1995 5 12 UPS803203 119950510A5320 FITTING DOUG DC8 DC873F 302199FWP FS 160 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON END FITTING AT LONGERON 21R, FS 160. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950512005841995051200584WP 1995 5 12 UPS803204 119950510A5320 FITTING DOUG DC8 DC873F 302199FWP FS 702 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT BELT FRAME END FITTING FS 702 LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950512005851995051200585WP 1995 5 12 UPS803205 119950510A5311 FRAME DOUG DC8 DC873F 302199FWP FS 720 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON BELT FRAME AT STA 720, LONGERON 34L. INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950512005861995051200586WP 1995 5 12 UPS803206 119950510A5320 FITTING DOUG DC8 DC873F 302199FWP FS 902/870 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON VERTICAL LEG OF TRAP FITTING AT STA 902 AFT SIDE, AND AT FWD LEG FS 870. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950512005871995051200587WP 1995 5 12 UPS803207 119950510A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 386-390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 35L AT FS 386 TO 390. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950512005881995051200588WP 1995 5 12 UPS803208 119950510A5730 SKIN DOUG DC8 DC873F 302199FWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E UPPER SKIN AT XFS 220. INSTALLED REPAIR PER UPS EO DC8-57-0557. 2L74 4F RT4A25 19950512005891995051200589WP 1995 5 12 UPS803209 119950510A5711 SPAR DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING REAR SPAR T-ANGLE AT XSF 64. INSTALLED REPAIR PER UPS EO FILE NR DC8-57-0558. 2L74 4F RT4A25 19950512005901995051200590WP 1995 5 12 UPS803210 119950510A5320 ANGLE DOUG DC8 DC873F 302199FWP FS 640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK AND CORROSION IN B-BAY BIN, AFT BULKHEAD, FS 640, LBL 24, LT TUNNEL VERTICAL ANGLE NEXT TO MAIN CARGO FLOOR. INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950519000011995051900001WP 1995 5 19 9507741158 119950504A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1980-1986 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT LAV SERVICE PAN AND SKIN DOUBLER AT FS 1980 - 1986, L50L TO L50R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-98047 AND 11-98056. MFG PART NUMBER: AGA3098-501. 2L73 4F A22WE 19950519000021995051900002WP 1995 5 19 9507751158 119950404A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 38. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER EA 11-98027. MFG PART NUMBER: ADA7034-3. 2L73 4F A22WE 19950519000031995051900003WP 1995 5 19 9507761158 119950426A5400 FASTENERS DOUG DC10 DC1040 3023508WP PYLON BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND BROKEN FASTENERS COMMON TO THE NR 4 BANJO FITTING AFT FLANGE AND THE PYLON CARRY THROUGH CAP. INSTALLED BUSHINGS AND REPAIRED CHANNELS PER EA 11-098170. MFG PART NUMBER AJC7054-1. 2L73 4F A22WE 19950519000041995051900004WP 1995 5 19 9507779908 119950510A3231NW29568461 CONTROL CABLE DOUG DC9 DC931 3022065WP RT NLG DOOR BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01958N 47254 VIBRATION FROM NOSE GEAR AREA OCCURRED DURING GEAR RETRACTION AFTER TAKEOFF. LOWERED GEAR AND VIBRATION CONTINUED. EXECUTED A GO-AROUND AND TOWER REPORTED THAT GEAR APPEARED TO BE NORMAL. FLIGHT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR STOP CABLE BROKEN. DEFERRED DOOR STOP CABLE PER MEL 32-7. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519000051995051900005 1995 5 19 9507789936 419950510A344220709620101 RADAR INDICATOR DOUG DC9 DC931 3022065WP COCKPIT MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER UKUNKNOWN 1 GL011799U2389630 47370 EN ROUTE MSP-IAD, RADAR BEGAN SPOKING IN LEFT 60 DEGREE QUADRANT AND WOULD NOT PAINT IN THIS AREA. FLIGHT DIVERTED TO CLE DUE TO THUNDERSTORMS AHEAD. REPLACED RADAR INDICATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519000061995051900006 1995 5 19 9507799986 419950510A2211 COMPUTER DOUG DC9 DC932 3022066WP AUTO PILOT MALFUNCTIONED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01986US 47480 AIRCRAFT EXPERIENCED ELEVATOR FLUTTER AND VIBRATION AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED AUTO-PILOT PITCH COMPUTER AND ELEVATOR SERVO DRIVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519000071995051900007WP 1995 5 19 9507809924 119950501A5330 SKIN DOUG DC9 DC932 3022066WP FS 160-200 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926RC 47473 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 160 - 200, LONGERON 22L. REPAIRED PER EA 99-097481. MFG PART NUMBER: 5911401-3. 2L72 4F A6WE 19950519000081995051900008WP 1995 5 19 9507819924 119950428A5330 SKIN DOUG DC9 DC932 3022066WP FS 160 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926RC 47473 DURING PERIODIC CHECK, FOUND CORROSION ON FUSEALGE SKIN FS 160, LONGERON 30. REPAIRED PER EA 99-097479. MFG PART NUMBER: 5911401-5. 2L72 4F A6WE 19950519000091995051900009WP 1995 5 19 9507829924 119950429A5342 ANGLE DOUG DC9 DC932 3022066WP FS 1095 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926RC 47473 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1095. REPAIRED PER EA 99-097075. MFG PART NUMBER: 5912141-59. 2L72 4F A6WE 19950519000101995051900010WP 1995 5 19 9507839977 119950429A5730 SKIN DOUG DC9 DC931 3022065WP RT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019341 47390 DURING PERIODIC CHECK, FOUND CORROSION ON THE RIGHT WING SKIN, LOWER FORWARD PANEL BETWEEN STR 17R AND 21R. REPAIRED PER EA 99-097072. MFG PART NUMBER: 5910465-4. 2L72 4F A6WE 19950519000111995051900011WP 1995 5 19 9507849924 119950420A5311 FRAME DOUG DC9 DC932 3022066WP FS 389 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926RC 47473 DURING PERIODIC CHECK, FOUND CRACK IN THE FS 389 FRAME FLANGE AT THE LONGERON 29R END FITTING. REPAIRED PER EA 99-097483. MFG PART NUMBER: 3912347-503. 2L72 4F A6WE 19950519000121995051900012NE 1995 5 19 9507859905 219950510A7200 TAILPIPE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE NR 2 ENGINE FIRE A NWAAE ENGINE SHUTDOWN A FLAME/FIRE ININSP/MAINT 1 GL01955N 47160 655286 A TAILPIPE FIRE OCCURRED DURING NR 2 ENGINE START SEQUENCE. THE ENGINE WAS SHUT DOWN. THE FIRE WAS EXTINGUISHED BY GROUND PERSONNEL. MAINTENANCE INSPECTED THE ENGINE, NO DISCREPANCIES NOTED. THE ENGINE WAS RUN-UP. SYSTEMS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950519000131995051900013WP 1995 5 19 9507869993 119950511A5230 FITTING DOUG DC9 DC931 3022065WP FWD CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE FORWARD CARGO DOOR UPPER SIDE PAN FITTING 6 INCHES FORWARD OF THE AFT HINGE. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950519000141995051900014WP 1995 5 19 9507879993 119950511A5230 FITTING DOUG DC9 DC931 3022065WP FWD CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE FORWARD CARGO DOOR INTERCOSTAL FITTINGS, UPPER AND LOWER. REPLACED FITTINGS PER SRM 51-30-2. P/N 3926046-501N, DASH 503. 2L72 4F A6WE 19950519000151995051900015WP 1995 5 19 9507889959 119950511A5744 HINGE DOUG DC9 DC931 3022065WP NR 3 LE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING PERIODIC CHECK, FOUND CORROSION IN LEFT FORWARD NR 3 FLAP HINGE FASTENER BORES. REPLACED HINGE PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950519000161995051900016NE 1995 5 19 95UAL727034 219950425A7320500707001 PS4 LINE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 ENGINE LOOSE A UALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP297297U 115 21892 700137 FLIGHT RETURNED TO MCO, NR 1 ENGINE SHUTDOWN DUE TO LOSS OF THRUST. FOUND EXTERNAL PS4 LINE BETWEEN THE FCU AND C/C/O FAN DUCT DISCONNECTED AT THE PS4 PROBE. THERE WAS NO EVIDENCE OF SAFETY WIRE IN THE PROBE TO B-NUT CONNECTION. RECONNECTED PS4 LINE TO PROBE AND SAFETIED. 2L73 4F4 F A3WE E2EA 19950519000171995051900017NM 1995 5 19 95UAL757015 119950511A3350 EEL LEAD BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29532UA 25072 EEL STRIP INOP SEAT 9C TO 16C. REPLACED EEL LEAD. 2L72 4F4 FRTA2NM E17NE 19950519000181995051900018NM 1995 5 19 95UAL767018 119950512A3350 EEL PLUG BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29609UA 21870 EEL LIGHTS FROM DOOR 1 TO MID GALLEY ON LEFT SIDE INOP. REPLACED DAMAGED PLUG AT LEFT MID GALLEY FORWARD OF STORAGE CONTAINER. 2L72 4F4 FRTA1NM E3NE 19950519000191995051900019WP 1995 5 19 95UALD10040 119950426A3246MS2125008042 TIE BOLT DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL RT NLG WHEEL BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP291814U 46613 RT NOSE TIRE HAS ONE BROKEN TIE BOLT. REPLACED NOSE GEAR WHEEL AND TIRE ASSEMBLIES. 2L73 4F4 F A22WE E23EA 19950519000201995051900020WP 1995 5 19 MWEA95199 119950511A3297 WIRE DOUG DC9 DC914 3022034WP RT WING BROKEN A MWEAO OTHER N FALSE WARNING DEDESCENT 1 GL31700ME 45696 WHEN GEAR LOWERED RIGHT MLG UNSAFE LIGHT DID NOT LIGHT DURING TRANSIT UNLESS THROTTLES RETARDED. FERRIED A/C TO MKE. FOUND WIRE 2G204E24 OPEN BETWEEN RT UPLOCK CONNECTOR AND TERMINAL STRIP S3-66. REPLACED WIRE. PERFORMED GEAR SWING. SYSTEM PERFORMS O.K. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519000211995051900021NM 1995 5 19 SCNA95096 119950509A33501000677 EEL ASSY BOEING727 727225 1384077NM COCKPIT FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 COCKPIT EMERGENCY EXIT SIGN INOPERATIVE WITH EMERGENCY LIGHT SWITCH ON. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED GOOD. 2L73 4F A3WE 19950519000221995051900022SW 1995 5 19 SWIA95571 119950502A2913PV304426 HYD PUMP SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NR 1 FAILED A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07176SW AC591 AIRCRAFT LOST ALL HYDRAULIC PRESSURE. BOTH LIGHTS ILLUMINATED AND GAUGE AT ZERO. EXTENDED GEAR PER EMERGENCY CHECK LIST. REPLACED THE NR ONE HYDRAULIC PUMP. PURGED AND SERVICED HYDRAULIC SYSTEMS. RAN THE LEFT AND RIGHT ENGINES. CYCLED FLAPS AND RESERVICED. LEAK CHECKED NR ONE HYDRAULIC PUMP. HYDRAULIC SYSTEM OPERATIONALLY CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950519000231995051900023SO 1995 5 19 SWIA95572 119950504A7712 TORQUE SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 NM07194SW 120120 RIGHT ENGINE TORQUE GAUGE INOPERATIVE. FLUCTUATES. REPLACED THE RIGHT TORQUE SIGNAL CONDITIONER. CLEANED AND SECURED CONNECTORS. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950519000241995051900024EA 1995 5 19 SWIA95573 119950501A301014463101 ANTI-ICE DUCT CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT WING SPLIT A SWIAK NONE JM WARNING INDICATION OVER TEMP CRCRUISE 1 NM07406SW 7030 ANTI-ICE DUCT RED EICAS MESSAGE WITH WING ANTI-ICE SELECTED ON. FOUND LEFT WING OUTBOARD DUCT SPLIT AT OUTBOARD END. LEADING EDGE AND DUCT REMOVED. INSTALLED SERVICEABLE ANTI-ICE DUCT IN LEFT OUTBOARD LEADING EDGE. INSTALLED LEADING EDGE IAW MM 51-41-01. OPS CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 19950519000251995051900025EA 1995 5 19 SWIA95574 119950502A3010144463101 TUBE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT WING CRACKED A SWIAK NONE JM WARNING INDICATION OVER TEMP CRCRUISE 1 NM07407SW 7034 ANTI-ICE DUCT MESSAGE ON EICAS WITH WING ANTI-ICE SWITCH IN NORMAL AND STANDBY POSITION. COULD NOT CLOSE THE RIGHT FOURTEENTH STAGE VALVE. SWITCH IN CLOSED POSITION DID NOT GIVE CLOSED LIGHT. NO INDICATION ON ANTI-ICE PAGE. REMOVED LEFT LEADING EDGE AND FOUND LEFT PICOLO TUBE CRACKED. REPLACED TUBE AND GROUND RAN THE NR ONE AND NR TWO ENGINES. ALL ANTI-ICE SYSTEMS CHECKED NORMAL. 2L72 4F4 FRTA21EA E15NE 19950519000261995051900026WP 1995 5 19 SWIA95575 219950504A7310 FUEL LINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE CRACKED A SWIAA UNSCHED LANDING KR FLUID LOSS PARTIAL RPM/PWR LOSS CRCRUISE 1 NM0727297 AC735 AT 14,000 FEET, THE RIGHT ENGINE LOST POWER. EGT DROPPED, TORQUE DROPPED, AND FUEL FLOW DROPPED. RPM STAYED AT 100 PERCENT. OIL PRESSURE AND TEMPERATURE REMAINED NORMAL. COULD ONLY GET 20 PERCENT TORQUE WITH POWER LEVER ALL THE WAY FORWARD. DIVERTED TO ONT. FOUND FUEL LINE CRACKED BETWEEN FUEL CONTROL UNIT AND FUEL FLOW TRANSMITTER. REMOVED AND REPLACED FUEL LINE. RAN THE RIGHT ENG TO TAKE OFF POWER. ALL PARAMETERS NORMAL. NO LEAKS FOUND. 1L72 4T4 T A8SW E4WE 19950519000271995051900027NE 1995 5 19 SWIA95576 219950507A7321 EEC EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM07189SW 120048 LT EEC FAILED ONCE ON TAKEOFF. ABORTED TAKE OFF. DEFERRED PER MEL 73-11-1. CHECKED CANNON PLUG AT LEFT ENGINE EEC. CHECKS OK. CLEAN OUT WIRING. CHECKS GOOD. RAN ENGINE. OPS CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950519000281995051900028SO 1995 5 19 SWIA95577 119950510A3150 AURAL WARNING EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE COCKPIT ACTIVATED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 NM07217SW 120286 UPON STARTING TAKEOFF ROLL, TRIM AURAL WARNING WENT OFF. RETURNED TO GATE AFTER ABORTING TAKE OFF. COULD NOT DUPLICATE PROBLEM. CYCLED TRIM AND POWER LEVER SWITCHES. OPS CKS GOOD. POWERED AIRCRAFT DOWN AND UP. 2L72 4T4 TRTA31SO E20NE 19950519000291995051900029WP 1995 5 19 SWIA95578 219950510A7320 P3 LINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP FUEL CONTROL LOOSE A SWIAK NONE R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM072725D AC723 AT 2,000 FEET, THE LEFT ENGINE TORQUE DROPPED TO 35 PERCENT. TEMPERATURE DROPPED TO 530 DEGREES. RESECURED B-NUT AT P3 AIR LINES AT FUEL CONTROL. GROUND RUN AND OPS CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950519000301995051900030NE 1995 5 19 95ZZZX2326 319950421A61124E30171 DEICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RIGHT PROPELLER MISSING A AJJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01844CA766 UE45 HJ246A RIGHT PROP, BLADE SN 398MA, HALF OF DEICE BOOT MISSING. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT'S APPARENT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. 2L72 4T RTA24CE 5 CP10NE 19950519000311995051900031NE 1995 5 19 95ZZZX2327 319950421A61124E30171 DEICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE LEFT PROPELLER MISSING A AJJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01833CA715 UE24 HJ114A LEFT PROP, BLADE SN 521MA MISSING DEICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT'S APPARENT THAT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO BLADES PRIOR TO BOOT INSTALLATION. 2L72 4T RTA24CE 5 CP10NE 19950519000321995051900032WP 1995 5 19 95ZZZX2328 119950412A213094840213 AMPLIFIER DOUG DC9 DC931 3022065WP CABIN PRESSURE INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19941VJ 47054 RIC - FLT 0739 - AT FL 350, THE CABIN PRESSURE RED LIGHT AND MASTER WARNING LIGHT ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO TIC. MAINTENANCE INSTALLED THE OUTFLOW ACTUATOR AND PRESSURE AMPLIFIER. OPERATIONS CHECKED NORMAL. REF CONTROL NR. USAA950369. 2L72 4F A6WE 19950519000331995051900033NM 1995 5 19 ASAA9510046 119950426A323069546154 GUIDE BRACKET BOEING737 737290C 138448VNM NLG LOCK ACT MISALIGNED A ASAAO OTHER O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK TEST HOP, CREW REPORTED THE NOSE LANDING GEAR FELL TO THE DOWN POSITION WHEN GEAR HANDLE WAS PLACED TO THE 'OFF' POSITION. RECYCLED GEAR SEVERAL TIMES AND OPERATED NORMALLY. REPOSITIONED NOSE LANDING GEAR LOCK ACTUATOR HYDRAULIC LINE GUIDE BRACKET, PERFORMED NOSE LANDING GEAR EXTENSION/RETRACTION TEST AND OPERATED NORMALLY. (X) 2L72 4F A16WE 19950519000341995051900034WP 1995 5 19 BUFA9512 119950329A5230AE2930100 TORQUE TUBE DOUG DC8 DC861 3021952WP CARGO DOOR BENT A BUFAK NONE O OTHER ININSP/MAINT 1 CE05915BV 45981 MGG/MIA - FLT CWC 148 - MAIN CARGO DOOR ALTERNATE LOCKING PINS VERY HARD TO REMOVE. INSPECTED, FOUND TORQUE TUBE BENT. REPLACED TORQUE TUBE AND RE-RIGGED CARGO DOOR LATCHES, PERFORMED OPS CHECK PER CARGO DOOR MM, OPS CHECK OKAY. DOOR WAS INSPECTED PER RII REQ. (X) 2L74 4F 4A25 19950519000351995051900035EU 1995 5 19 USAA950360 119950411A3230200498005 DNLOCK ACT FOKKERF28 F28MK4000 4990810EU RT MLG INOPERATIVE A USAAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA19494US 11167 YOW - FLT 0810 - CREW COULD NOT GET THE GREEN LIGHTS FOR THE RIGHT MAIN GEAR. THE CREW HAD TO RECYCLE THE GEAR SEVERAL TIMES TO GET THE GREEN LIGHTS. FLIGHT MADE A NORMAL LANDING. MAINTENANCE REPLACED THE RIGHT DOWNLOCK ACTUATOR. LANDING CHECKS NORMAL. (M) 2L72 4F RTA20EU 19950519000361995051900036EU 1995 5 19 USAA950362 119950409A33506008905 EEL POWER SUPPLY FOKKERF28 F28MK4000 4990810EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19478US 11227 CLT - THE EMERGENCY EXIT LIGHTS REMAIN ON WITH ALL POWER REMOVED FROM THE AIRCRAFT AND THE EMERGENCY EXIT LIGHT SWITCH 'OFF'. MAINTENANCE RPELACED BATTERY POWER SUPPLY. OPERATIONS CHECK GOOD. (X) 2L72 4F RTA20EU 19950519000371995051900037EU 1995 5 19 USAA950366 119950408A2820 CONNECTOR FOKKERF28 F28MK4000 4990810EU WHEELWELL FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19481US 11230 CLT - FLT 0052 - FLIGHT RETURNED TO CLT DUE TO A FUEL IMBALANCE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED A CONNECTOR IN THE WHEELWELL AND SEVERAL FLAG TERMINALS ON THE PROBES. (X) 2L72 4F RTA20EU 19950519000381995051900038EU 1995 5 19 USAA950385 119950415A335014597101 EEL BATTERY PACK FOKKERF28 F28MK4000 4990810EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19481US 11230 CLE - MAIN ENTRANCE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPS CHECKS GOOD. (X) 2L72 4F RTA20EU 19950519000391995051900039EU 1995 5 19 USAA950386 119950420A3350 LENS FOKKERF28 F28MK0100 4990807EU CABIN MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19890US 11365 PIT - RIGHT OVERWING EMERGENCY LIGHT LENS MISSING AND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LENS ON RIGHT SIDE AND REPLAMPED LEFT SIDE. BOTH OPS CHECK OKAY. (X) 2L72 4F RT 19950519000401995051900040EU 1995 5 19 USAA950387 119950419A3230 HARNESS FOKKERF28 F28MK4000 4990810EU RT MLG LOOSE A USAAO OTHER J WARNING INDICATION CLCLIMB 1 EA19479AU 11228 CLT - FLT 993 - AFTER TAKEOFF FROM TYS, RIGHT MLG RED LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND LIGHT WENT OUT. FLIGHT CONTINUED WITHOUT INCIDENT TO CLT. MAINTENANCE FOUND RIGHT MAIN GEAR HARNESS CONTACTING AFT DOOR HOOK BEFORE DOOR COULD LOCK. RESECURED LOWER HARNESS TO STRUT. (X) 2L72 4F RTA20EU 19950519000411995051900041EU 1995 5 19 VTZA95150 119950428A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILURE A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CRCRUISE 1 EA27476UE 884 SYR/IAD - FLT 6362 - DURING CRUISE AT 0735 HRS ON 4-28-95, DIVERTED TO BGM DUE TO THE LT ENGINE EGT AND TORQUE FLUCTUATION. AN EMERGENCY WAS DECLARED AND THE CREW SHUT THE ENGINE DOWN IN-FLIGHT. AIRCRAFT LANDED AT BGM WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950519000421995051900042EU 1995 5 19 WTAA950156 119950406A3260 INDICATOR BULB BAG JETSTMJETSTM3101 1500215EU LT MLG LOOSE A WTAAK NONE N FALSE WARNING CLCLIMB 1 WP17420UE 788 SFO - INTERMITTENT LEFT MLG INTRANSIT LIGHT ILLUMINATION REPORTED DURING GEAR RETRACTION. MAINTENANCE INSPECTED LANDING GEAR POSITION INDICATION SYSTEM. FOUND LEFT MAIN GEAR INTRANSIT LAMP LOOSE IN INDICATOR, PN DN1050ZMK2. RESECURED LAMP IN SOCKET. SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950519000431995051900043WP 1995 5 19 WTAA950159 219950413A73218974005 FUEL CONTL UNIT BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RT ENGINE FAILED A AWTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17421UE 2826 804 ACV - RIGHT ENGINE FLUCTUATING TORQUE AND EGT INDICATIONS REPORTED DURING CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL UNIT. ENGINE OPERATION NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19950519000441995051900044SO 1995 5 19 WTAA950160 119950414A27315299 TRIM ACTUATORS EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A WTAAK NONE F FLT CONT AFFECTED CRCRUISE 1 WP17282UE 120124 SFO - ELEVATOR TRIM STUCK AT 2 UNITS FORWARD OF GREEN DURING CRUISE FLIGHT. TRIM BEGAN TO FUNCTION ON DESCENT. AIRCRAFT LANDED IN SFO WITHOUT INCIDENT. MAINTENANCE INSPECTED AND LUBED BOTH ELEVATOR TRIM ACTUATORS. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950519000451995051900045NE 1995 5 19 WTAA950162 219950416A73207863904 HMU SHAFT EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LOOSE A WTAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 WP17280UE4461 120090 SFO - DURING CLIMB-OUT THROUGH 10,000 FEET, POWER LEVER SPLIT REPORTED. AT 14,00 FEET, LEFT POWER LEVER FAILED TO CONTROL ENGINE POWER. CREW SECURED LEFT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LEFT ENGINE HMU INPUT SHAFT NUT LOOSE. RIGGED INPUT SHAFT, TIGHTENED AND SECURED INPUT SHAFT NUT. POWER LEVER CONTROL NORMAL ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950519000461995051900046EU 1995 5 19 WTAA950163 119950417A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3101 1500215EU LT ENGINE FAILED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17428UE 806 LAX - LEFT ENGINE TORQUE INDICATION FLUCTUATION REPORTED IN-FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED AND ADJUSTED LEFT ENGINE TORQUE SIGNAL CONDITION UNIT. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950519000471995051900047SO 1995 5 19 WTAA950164 119950412A524212040389001 DOOR EMB 120 EMB120RT SO AVIONICS BAY UNLATCHED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17454UE 120155 FAT - SERVICE DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND AVIONICS BAY DOOR UNLATCHED. INSPECTED AND RESECURED AVIONICS BAY DOOR. WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950519000481995051900048WP 1995 5 19 WTAA950165 219950417A73218070297 FCU BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A AWTAAO OTHER O OTHER CRCRUISE 1 WP17331CA 793 SMF - LEFT ENGINE UNCOMMANDED INCREASE IN TORQUE FROM 40 PERCENT TO 100 PERCENT IN-FLIGHT. TORQUE REDUCED TO 30 PERCENT WITH PROPELLER BROUGHT TO FLIGHT IDLE POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FUEL CONTROL UNIT. LEFT ENGINE OPERATIONAL CHECK NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19950519000491995051900049EU 1995 5 19 WTAA950166 119950418A3260 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU LT MLG BROKEN A WTAAK NONE N FALSE WARNING NRNOT REPORTED 1 WP17428UE 806 LAX - LEFT MLG INTRANSIT LIGHT REPORTED INOPERATIVE. MAINTENANCE REPAIRED DAMAGED WIRE AT LEFT MLG UPLOCK SWITCH, PN 622800200. LANDING GEAR POSITION INDICATIONS OPERATIONAL CHECK NORMAL ON GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950519000501995051900050NE 1995 5 19 WTAA950167 219950411A7250310900301 PT DISK 3038613 EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FAILED A WTAAK NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 WP17280UE 19A964 120090 115435 SFO - NOISE AND VIBRATION REPORTED FROM RT ENGINE WITH POWER LEVER IN GROUND IDLE. MAINTENANCE REMOVED AND REPLACED RT ENGINE ASSY. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENT INVESTIGATION REVEALED PT-1 DISK BLADE FAILURE TO BE CAUSE OF ENGINE NOISE AND VIBRATION. (X) 2L72 4T4 TRTA31SO E20NE 19950519000511995051900051EU 1995 5 19 WTAA950168 119950421A2612021839 LAMP HOLDER BAG JETSTMJETSTM3101 1500215EU RT ENGINE CORRODED A WTAAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 WP17424UE 796 LAX - RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATED AFTER ENGINE START. MAINTENANCE INSPECTED ENGINE. DETERMINED FIRE INDICATION TO BE FALSE INDICATION. CLEANED CORROSION FROM LAMP HOLDER. ENGINE FIRE DETECTION SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950519000521995051900052SO 1995 5 19 WTAA950169 119950422A27315299 TRIM ACTUATORS EMB 120 EMB120RT SO HORIZ STAB LACK OF LUBE A WTAAK NONE O OTHER NRNOT REPORTED 1 WP17282UE 120124 SFO - ELEVATOR TRIM WHEEL REPORTED DIFFICULT TO MOVE MANUALLY. ELECTRIC TRIM FUNCTIONS NORMALLY. MAINTENANCE INSPECTED AND LUBED BOTH ELEVATOR TRIM ACTUATORS. OPERATIONAL CHECK OF ELEVATOR TRIM SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950519000531995051900053SO 1995 5 19 WTAA950170 119950516A281012016056001 FUEL PANEL EMB 120 EMB120RT SO LT WING LOOSE SCREWS A WTAAO OTHER K FLUID LOSS CRCRUISE 1 WP17275UE 120058 SBA - EN ROUTE LAX-SBA - FUEL LEAK REPORTED FROM LEFT WING. CREW DECLARED AN EMERGENCY AND LANDED AT STATION WITHOUT INCIDENT. MAINTENANCE FOUND FUEL DRIPPING FROM FIRST FUEL ACCESS PANEL OUTBOARD OF LEFT WING ENGINE NACELLE. TIGHTENED LOOSE SCREWS ON FUEL PANEL. NO FUEL LEAK NOTED DURING SUBSEQUENT LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950519000541995051900054NM 1995 5 19 9507892286 119950511A3260656021132 ACCESSORY UNIT BOEING727 727251 138408HNM E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01286US3535712547 21325 DURING DEPARTURE CLIMB UPON GEAR RETRACTION, LANDING GEAR HANDLE COULD NOT BE RAISED BEYOND OFF POSITION. NO LEFT MAIN GEAR DOOR INDICATION ON SECOND OFFICER'S ANNUNCIATION PANEL. AURAL WARNING HORN WAS SOUNDING UPON FLAP RETRACITON WITH GEAR DOWN. FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED A SERVICEABLE LANDING GEAR ACCESSORY UNIT. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950519000551995051900055NM 1995 5 19 9507906611 119950512A323069B803587 DNLOCK ACTUATOR BOEING747 747251B 1384892NM LT MLG MALFUNCTIONED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01611US5452454487 20356 DURING APPROACH FOR LANDING AND AFTER LOWERING THE LANDING GEAR, EXPERIENCED RAPID LOSS OF HYDRAULIC FLUID ON NO.1 SYSTEM. HYDRAULIC PRESSURE DECREASED TO ZERO AND BOTH LOW PRESSURE AND QUANTITY LIGHTS ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENT. REPLACED THE LEFT BODY GEAR DOWNLOCK ACTUATOR AND PERFORMED CHECK. UNIT CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19950519000561995051900056WP 1995 5 19 ABXA9500385 119950511A32303914464503 LINKAGE DOUG DC9 DC932 3022066WP NLG LACK OF LUBE A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23903AX312304463 47427 NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE ON FIRST EXTENSION ATTEMPT, BUT WORKED NORMALLY ON SECOND ATTEMPT. CLEANED AND LUBED OVERCENTER LINKAGE. PERFORMED OPS CHECK OF NOSE LANDING GEAR SYSTEM WHILE AIRCRAFT WAS JACKED. CYCLED GEAR THROUGH NUMEROUS TIMES. NO DEFECTS NOTED. OPS CHECKED GOOD IAW DC-9 MM 32-20-0. 2L72 4F A6WE 19950519000571995051900057SO 1995 5 19 COM11888 119950512A323018190003 SOLENOID VALVE EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01463CA7048 120267 WHEN LANDING GEAR RETRACTED, THE L/T MLG INTRANSIT INDICATORS REMAIN ON. REPLACED THE LANDING GEAR SOLENOID VALVE. 2L72 4T RTA31SO 19950519000581995051900058SO 1995 5 19 COM11889 119950511A77143033515 SENSOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01168CA116801736 120168 115249 R/T ENGINE WILL NOT START, NO NH INDICATION. REPLACED THE NH SENSOR. 2L72 4T4 TRTA31SO E20NE 19950519000591995051900059EU 1995 5 19 COM31079 119950511A335046683 EEL SWITCH SAAB SF340 SF340A 7850100EU CABIN BURNT A COMAK NONE L NO TEST UKUNKNOWN 1 SO01380CA 340A012 ROW 6 EMERGENCY EXIT SIGNS FLASH ON AND OFF DURING FLIGHT. REPLACED BURNT EMERGENCY LIGHTING ARM SWITCH ON FLIGHT ATTENDANT LIGHT PANEL. 2L72 4T RTA52EU 19950519000601995051900060EA 1995 5 19 COM60470 119950511A3241428853 CONTROL UNIT CNDAIRCL600 CL6002B19 EA ANTI-SKID SYST DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01927CA4725 658 7031 ANTI-SKID CAUTION MESSAGE ON EICAS. REPLACED THE ANTI-SKID CONTROL UNIT. 2L72 4F RTA21EA 19950519000611995051900061EA 1995 5 19 COM60471 119950511A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 2 SPOILER DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01918CA3466 1957 7018 GROUND SPOILERS AND SPOILERONS FAULT MESSAGE ON EICAS. REPLACED THE NR 2 SPOILER ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950519000621995051900062 1995 5 19 COM60472 419950512A34183995100106 STALL UNIT CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAK NONE J WARNING INDICATION DEDESCENT 1 SO01933CA2575 7040 STALL FAIL MESSAGE ON EICAS. REPLACED THE STALL PROTECTION UNIT. 2L72 4F RTA21EA 19950519000631995051900063EA 1995 5 19 COM60473 119950515A28427680941 FUEL PROBE CNDAIRCL600 CL6002B19 EA RT WING DEFECTIVE A COMAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO01918CA 7018 FUEL SPILL OUT OF RT WING VENT, APPROXIMATELY 25 GALLONS. REPLACED THE RT WING FUEL COMPENSATOR. 2L72 4F RTA21EA 19950519000641995051900064WP 1995 5 19 DHL95803002 119950511A21708323719 COALESCER BAG DOUG DC8 DC873 302199CWP LT/RT SERVICEABLE A TDHLAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01803DH 46123 CREW REPORTED STRONG ODOR OF CHLORINE IN CABIN. INSPECTED AIRCRAFT AND CARGO. REMOVED AND REPLACED COALESCER BAGS. PERFORMED ENGINE RUN, OPERATED HYDRAULIC, PNEUMATIC AND ELECTICAL SYSTEMS. COULD NOT DUPLICATE ODOR. 2L74 4F RT4A25 19950519000651995051900065EA 1995 5 19 ERA00005 119950513A6120CE10593 BETA SWITCH DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043EA RT ENGINE OUT OF ADJUST A ERAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 AL03885EA 454 RT PROPELLER FEATHERED (UNSCHEDULED) AND RT BETA LIGHT CAMEON. RETURNED TO SCC WITHOUT INCIDENT. ADJUSTED BETA SWITCHIAW DHC TAB 610/1, CONFIRMED NO OVER TORQUE. 1H72 3T4 T A9EA E4EA 19950519000661995051900066WP 1995 5 19 MWEA95200 119950511A2560113313 EVAC SLIDE DOUG DC9 DC932 3022066WP PAX DOOR LOOSE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31502ME 48132 CREW REPORTS FWD ENTRANCE DOOR EVACUATION SLIDE NEEDS TO BE RESECURED. MAINTENANCE RESECURED FWD ENTRANCE EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950519000671995051900067WP 1995 5 19 MWEA95201 119950513A5230 SKIN DOUG DC9 DC915 3022036WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING ROUTINE INSPECTION, THE FWD CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER FWD CORNER. MAINTENANCE INSTALLED REPAIR DOUBLER IAW 52-05 FIG 4. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950519000681995051900068WP 1995 5 19 MWEA95202 119950513A5230 SKIN DOUG DC9 DC915 3022036WP CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING ROUTINE INSPECTION, THE AFT CARGO DOOR SKIN WAS FOUND CRACKED ON LOWER EDGE. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 52-05 FIG 4. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950519000691995051900069WP 1995 5 19 MWEA95203 119950513A2560113313 EVAC SLIDE DOUG DC9 DC915 3022036WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31300ME 45718 CREW REPORTS, GALLEY DOOR EMERGENCY EXIT SLIDE CAME OFF DOOR. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950519000701995051900070NM 1995 5 19 UPS203212 119950510A3350 EEL BATTERY PACK BOEING727 72762C 138402CNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01913UP 19245 MAINTENANCE REPORTED ENTRY DOOR EMER EXIT LIGHTS INOP. REPLACED BATTERIES, OPS CHECK NORMAL. 2L73 4F A3WE 19950519000711995051900071NM 1995 5 19 UPS203213 119950510A3350 EEL ASSY BOEING727 72722C 138400FNM FLIGHT DECK MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01929UP 19092 MAINTENANCE REPORTED EMER EXIT LIGHT OVER FWD ENTRY DOOR, WHEN TURNED ON COMES ON BRIGHT FOR APPROX 45 SECONDS THEN GOES DIM. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECK NORMAL. 2L73 4F A3WE 19950519000721995051900072NM 1995 5 19 UPS403214 119950511A5220 LATCH ASSY BOEING747 747121 1384871NM FLIGHT DECK LOOSE A IPXAK NONE O OTHER CRCRUISE 1 SO01683UP 20353 PILOT REPORTED OVERHEAD HATCH HANDLE POPS OUT IN FLIGHT. TIGHTENED LATCH ASSY, PRESSURIZED A/C AND FOUND NO DEFFECTS AT THIS TIME. OK FOR SERVICE. 2L74 4F A20WE 19950519000731995051900073NM 1995 5 19 UPS403215 119950511A5512 PANEL BOEING747 747123F NM RT HORIZ STAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01674UP 20100 MAINTENANCE REPORTED PANEL DELAMINATED ON RT HORIZONTAL STAB, LWR SURFACE, 2ND PANEL FROM OUTBOARD. INSTALLED REPAIR PER UPS EO B747-5510-6994A. 2L74 4F A20WE 19950519000741995051900074WP 1995 5 19 UPS803163 119950512A5532564932975 SKIN DOUG DC8 DC871F 302199DWP FS 80-100 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON INNER SKIN BETWEEN LONGERONS 30L AND 32L, AT FS 1746. REPLACED SKIN PER DOUGLAS DRAWING NR 5649329. 2L74 4F RT4A25 19950519000751995051900075WP 1995 5 19 UPS803211 119950512A53202699432 FITTING DOUG DC8 DC873F 302199FWP FS 160 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON END FITTING, LONGERON 21R, FS 160. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519000761995051900076WP 1995 5 19 UPS803216 119950512A5530 DOUBLER DOUG DC8 DC873F 302199FWP FS 80-100 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01874UP 46074 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON FINGER DOUBLER AT FS 80 TO 100, LONGERON 28R. REPLACED DOUBLER PER SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 19950519000771995051900077WP 1995 5 19 UPS803229 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1870 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 36R END FITTING, FS 1870. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950519000781995051900078WP 1995 5 19 UPS803230 119950515A5313526571612000 LONGERON DOUG DC8 DC871F 302199DWP FS 1742 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 16L AT FS 1742. INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F RT4A25 19950519000791995051900079WP 1995 5 19 UPS803231 119950515A53203779659501 FITTING DOUG DC8 DC871F 302199DWP FS 850-857 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 4R END FITTING AT FS 850 TO 857. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950519000801995051900080WP 1995 5 19 UPS803232 119950515A57125770123 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E UPPER RIBS, 5 EA AT STATIONS XFS 884, 778, 766, 754, 748. INSTALLED REPAIR PER SRM 57-2-2. 2L74 4F RT4A25 19950519000811995051900081WP 1995 5 19 UPS803233 119950515A57535701110 VANE ASSY DOUG DC8 DC871F 302199DWP NR 6 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING NR 6 FLAP VANE ON AFT TRAILING EDGE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950519000821995051900082WP 1995 5 19 UPS803234 119950515A532057501891 SPLICE FITTING DOUG DC8 DC871F 302199DWP FS 920 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 24L SPLICE FITTING AT FS 920. INSTALLED REPAIR PER UPS EO DC8-5310-6968A. 2L74 4F RT4A25 19950519000831995051900083WP 1995 5 19 UPS803235 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 305 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON STA 305 FITTING, BETWEEN LONG 33A AND 33B RT. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950519000841995051900084WP 1995 5 19 UPS803236 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 322 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON STA 322 FITTING, BETWEEN LONG 33A AND 33B RT. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950519000851995051900085WP 1995 5 19 UPS803237 119950515A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 445-455 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2-CHECK, MAINTENANCE FOUND CORROSION ON SPLICE AND FINGER DOUBLERS AT FS 445 TO 455, LONGERON 34L TO 35R. REPLACED DOUBLERS PER DOUGLAS DRAWING 5755271-7. 2L74 4F RT4A25 19950519001531995051900153SW 1995 5 19 95ZZZX2329 119950404A5320206033110239 STIFFENER 206033110217BELL 206 206L4 1182110SW CENTER POST CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH2106 52076 WHILE PERFORMING AN INSPECTION OF CENTER POST AREA, MECHANIC NOTED A CRACK IN THE RT VERTICAL STIFFENER. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG STARTING AT RIVET AND EXTENDING OUT IN THE BEND. REPLACED RT VERTICAL STIFFENER IAW WITH AC 43.13-A, CHAPTER 2, SECTION 3. REPAIRED CRACKED RT WEB, PN 206-033-110-149, IAW WITH BELL 206 SRM-1, REPAIR 5-5-1. 1G71 3U NCH2SW 19950519001541995051900154NE 1995 5 19 95ZZZX2330 119950407A6310S163561202002 COUPLING SKRSKYS58T S58ET 8141803NE DRIVE SEPARATION A NYBAK NONE O OTHER ININSP/MAINT 1 EA11265671735 CHP026 581514 DURING 1750-HOUR INSPECTION, MECHANIC NOTED NUMEROUS RUBBER SEGMENTS WERE FOUND SEPARATED BEYOND LIMITS IAW S-58T MM. REPLACED FLEX COUPLING IAW WITH S-58T MM. 2G72 4U 1H11 19950519001551995051900155NE 1995 5 19 95ZZZX2331 119950407A6310S163561202002 COUPLING SKRSKYS58T S58ET 8141803NE DRIVE SEPARATION A NYBAK NONE O OTHER ININSP/MAINT 1 EA11265671728 CHP025 581514 DURING 1750-HOUR INSPECTION, MECHANIC NOTED NUMEROUS RUBBER SEGMENTS FOUND SEPARATED BEYOND LIMITS IAW WITH S-58T MM. REPLACED FLEX COUPLING IAW S-58T MM. 2G72 4U 1H11 19950519001561995051900156NM 1995 5 19 95ZZZX2332 119950321A3350 EEL CHARGER BOEING727 7272B7 138407LNM CABIN FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11760US 21954 IND - FLT 7339 - EGRESS FLOOR TRACK LIGHTS FROM ROW 17 FORWARD ARE VERY DIM. REPLACED BATTERY CHARGER. OPS CHECKS NORMAL. 2L73 4F A3WE 19950519001571995051900157NM 1995 5 19 95ZZZX2333 119950404A5311 FRAME BOEING727 727231 1384079NM FS 783 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554325 20232 MCI - DURING C-CHECK, FOUND FORMER FRAME CRACKED 2 INCHES AROUND RADIUS, 3 INCHES ABOVE FLOOR BEAM CAP, STA 783. STOP DRILLED CRACK PER SRM 51-10-4, PAGE 6A, AND INSTALLED DOUBLER REPAIR PER ARA 65686 AND DWG. NR 65C36280. AIRCRAFT TT: 61,023 HOURS; 41,008 CYCLES. 2L73 4F A3WE 19950519001581995051900158WP 1995 5 19 95ZZZX2335 119950408A5280 DOOR SEAL DOUG DC8 DC871 302199AWP LT NLG DOOR LOOSE A RRXAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP158177U 45983 KSAN/KONT - FLT 0033 - DURING CLIMB-OUT AFTER GEAR RETRACTION, LOUD VIBRATION IN NOSE AREA. RECYCLED GEAR AND GOT UNSAFE LIGHT. EXTENDED GEAR AND LIGHTS WERE NORMAL. RETURNED TO KSAN. MAINTENANCE INSPECTED NOSE LANDING GEAR DOWNLOCK AND UPLOCK MECHANISMS AND SWITCHES. FOUND LT FIXED DOOR SEAL CAME LOOSE CAUSING GEAR DOOR TO NOT CLOSE FULLY. TRIMMED AND RESEATED DOOR SEAL. 2L74 4F 4A25 19950519001591995051900159EU 1995 5 19 95ZZZX2336 119950424A3260 SWITCH AEROSPATR42 ATR42300 8680920EU LT MLG OUT OF ADJUST A NVEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO03144DD 74 MIA - FLT 5769 - CREW REPORTS: IDLE GATE FAILURE, NOSE GEAR RETRACTED, MAIN GEARS DID NOT RETRACT. RESET CIRCUIT BREAKER. STILL INOP. FOLLOWED QRH HANDBOOK, EXTENDED GEAR AND RETURNED TO MIA. READJUSTED THE PROXIMITY SWITCHES AND OPS CHECK GOOD. 2H72 4T RTA53EU 19950519001611995051900161 1995 5 19 95ZZZX2338 419950329A34256229682002 DISPLAY UNIT BEECH 1900 1900D 1154162CE LEFT HAND INOP A S2YAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL1381SK 1382 UE81 THE FLIGHT CREW RETURNED TO THE POINT OF DEPARTURE DUE TO RT EFIS INTERMITTENLTY GOES ON AND OFF, LT EHSI WENT BLANK. MAINTENANCE REMOVED AND REPLACED COLLINS NR 1 DISPLAY PROCESSOR UNIT AND BOTH SYSTEMS CHECK GOOD. 2L72 4T RTA24CE 19950519001621995051900162CE 1995 5 19 95ZZZX2339 119950420A27301016100195 TORQUE TUBE BEECH 1900 1900D 1154162CE LT ELEVATOR LOOSE RIVETS A S2YAK NONE O OTHER ININSP/MAINT 1 GL1381SK 2843 UE81 DURING A SCHEDULED INSPECTION, LT ELEVATOR TORQUE TUBE ASSEMBLY FOUND TO HAVE LOOSE RIVETS. THE PART WAS REPLACED. 2L72 4T RTA24CE 19950519001641995051900164CE 1995 5 19 95ZZZX2341 119950216A282011892000029 TRANSFER TUBE BEECH 1900 1900D 1154162CE LT MLG WW CHAFED A S2YAK NONE K FLUID LOSS ININSP/MAINT 1 GL1385SK 2416 UE85 FOUND FUEL LEAKING FROM LT WHEELWELL, MAINTENANCE OPENED UP THE INNER FENDER ASSEMBLY AND FOUND MAIN GEAR UPLOCK SWITCH, WIRE BUNDLE HAD CHAFED THROUGH THE FUEL TRANSFER TUBE ASSEMBLY JUST INBOARD OF THE FUEL CROSS-TRANSFER VALVE. THE LINE WAS REMOVED ADN REPLACED AND WIRE BUNDLE WAS REROUTED. 2L72 4T RTA24CE 19950519001651995051900165CE 1995 5 19 95ZZZX2342 119950323A2450J692007J690003 WIRE BEECH 1900 1900D 1154162CE AVIONICS BAY CHAFED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13118SK1349 UE108 EFIS AUXILIARY POWER ANNUNCIATOR FLICKERED, WENT OUT, AND THEN WOULD NOT TEST. MAINTENANCE FOUND RELAY MODULES K103, K104, AND 5-AMP FUSE F033 INOP AND REPLACED THEM. LATER, DURING TROUBLESHOOTING FOR ANOTHER ELECTRICAL PROBLEM, FOUND A CHAFED WIRE J692007-J690003 IN THE AVIONICS BAY, MIDDLE SHELF BETWEEN THE VERTICAL GYROS. REPAIRED THE CHAFED WIRE, AND OPS CHECK GOOD. 2L72 4T RTA24CE 19950519001661995051900166NM 1995 5 19 95ZZZX2343 119950423A3260 SWITCH WIRE BOEING727 727231 1384079NM NLG BROKEN A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE0594314 20047 STL - FLT 572 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR SHOWED AN UNSAFE INDICATION. VISUALLY CHECKED NLG FOR BEING DOWN AND LOCKED. FOUND BROKEN WIRE AT NLG DOWLOCK SWITCH CONNECTOR, D298. REPLACED D298 DOWNLOCK SWITCH CONNECTOR. NLG OPERATION AND INDICATION CHECKED NORMAL. CHECK C-2 - 9-7-94 - MCI. 2L73 4F A3WE 19950519001671995051900167WP 1995 5 19 95ZZZX2344 119950411A5313 LONGERON DOUG DC9 DC951 3022051WP FS 794/832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A .50 INCH CRACK IN LONGERON 3L, STA 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. 2L72 4F A6WE 19950519001681995051900168WP 1995 5 19 95ZZZX2345 119950412A5313 LONGERON DOUG DC9 DC931 3022065WP FS 1000 GOUGED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05980Z 47344 STL - DURING OP-15, FOUND A GOUGE IN LONGERON 6R, STA 1000. REPAIRED BY INSTALLING LONGERON SPLICE PER SRM 53-02. AIRCRAFT TOTAL TIME: 62,133 HOURS; 75,010 CYCLES. 2L72 4F A6WE 19950519001691995051900169WP 1995 5 19 95ZZZX2346 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 734 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND .50 INCH CRACK IN LONGERON 3R, STA 734. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. 2L72 4F A6WE 19950519001701995051900170WP 1995 5 19 95ZZZX2347 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. 2L72 4F A6WE 19950519001711995051900171WP 1995 5 19 95ZZZX2348 119950411A5313 LONGERON DOUG DC9 DC951 3022051WP FS 832 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND CRACK IN LONGERON 4L, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. 2L72 4F A6WE 19950519001721995051900172NM 1995 5 19 95ZZZX2349 119950419A323053173 LINK PIN BOEING727 727231 1384079NM NOSE GEAR MISSING A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0552312 19831 STL - FLT 10 - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE ABOVE OFF POSITION. ACCOMPLISHED LANDING GEAR HANDLE LOCK CHECKLIST AND RETRACTED LANDING GEAR. FOUND NLG TORQUE LINK PIN MISSING, MFG. PN 53173. INSTALLED NEW NOSE GEAR TORQUE LINK PIN. LANDING GEAR CHECKS NORMAL. CHECK C-3 - 3-24-95 - MCI. 2L73 4F A3WE 19950519001731995051900173WP 1995 5 19 95ZZZX2350 119950410A5313 LONGERON DOUG DC9 DC951 3022051WP FS 794 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES. 2L72 4F A6WE 19950519001741995051900174NE 1995 5 19 95ZZZX2351 219950427A731437340126 FUEL PUMP BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 1 ENGINE FAILED A TWAAO OTHER Y ENGINE STOPPAGE APAPPROACH 1 CE0593108 19674 LAX - FLT 841 - ON APPROACH, NR 1 ENGINE SHUT DOWN ON OWN ACCORD. REPLACED FUEL PUMP, MFG PN 373401-26 AND JFC, MFG PN 747999-5. OP CHECKS NORMAL. CHECK C-2 - 1-29-95 - MCI. 2L74 4F4 F A20WE E20EA 19950519001751995051900175WP 1995 5 19 95ZZZX2352 119950427A323149567371 LATCH BRACKET DOUG DC9 DC931 3022065WP RT MLG DOOR FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05976Z 47248 STL - FLT 147 - AFTER LANDING GEAR RETRACTION, RIGHT DOOR AND GEAR UNSAFE LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED GEAR WITH SAME RESULTS. REPLACED DOOR LATCH BRACKET, MFG PN 4956737-1, AND SPRINGS, MFG PN 2923594-1. OP CHECKS NORMAL. CHECK C - 5-2-94 - STL. 2L72 4F A6WE 19950519001761995051900176WP 1995 5 19 95ZZZX2353 119950427A323129235941 SPRINGS DOUG DC9 DC931 3022065WP RT MLG DOOR FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05976Z 47248 STL - FLT 147 - AFTER LANDING GEAR RETRACTION, RIGHT DOOR AND GEAR UNSAFE LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED GEAR WITH SAME RESULTS. REPLACED DOOR LATCH BRACKET, MFG PN 4956737-1, AND SPRINGS, MFG PN 2923594-1. OP CHECKS NORMAL. CHECK C - 5-2-94 - STL. 2L72 4F A6WE 19950519001771995051900177NM 1995 5 19 AWXA9500239 119950421A5414114N18099 PANEL BOEING757 75723A 1384967NM NR 1 PYLON DAMAGED A AAWXAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 WP28916AW 24291 PHX/JFK - FLT 290 - AIR TURNBACK, PANEL 911KT LOCATED ON TOP OF LT WING NR 1 ENGINE PYLON DEPARTED AIRCRAFT DURING TAKEOFF. PANEL WAS IMPROPERLY SECURED. AIRCRAFT RETURNED TO PHX LANDING UNEVENTFULLY. OVER WEIGHT LANDING INSPECTION C/W. PANEL REPLACED AND AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA2NM 19950519001781995051900178WP 1995 5 19 CAL950295 119950418A3350 POWER SUPPLY DOUG DC9 DC982 3022082WP OVERWING EEL INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0957837 49582 DCA - FLT 0799 - INSPECTION FOUND BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK AND OPERATION OF THE OVERWING EMERGENCY LIGHTS WAS RESTORED. (X) 2L72 4F A6WE 19950519001791995051900179EU 1995 5 19 RAIA950419 119950413A32307445B BYPASS VALVE JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR POPPED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03551HK571 41040 STL - FLT 7061 - LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. MAINTENANCE DISCOVERED LANDING GEAR BYPASS PIN POPPED. MAINTENANCE RESET BYPASS VALVE PIN, PERFORMED GROUND RUNS, SYSTEM CHECK GOOD. (X) 2L72 4T RTA41NM 19950519001801995051900180EU 1995 5 19 RAIA950428 119950418A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU NR 2 ENGINE FAILED A RAIAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 CE03871JX2200 727 871 SFO - FLT 4758 - NR 2 GENERATOR DROPPED OFF LINE. REPLACED NR 2 STARTER/GENERATOR. (X) 2L72 4T RTA56EU 19950519001811995051900181EU 1995 5 19 SIMA951091 119950419A33503012000 POWER SUPPLY AEROSPATR72 ATR72212 EU 61WL EEL DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21431AT2180 480 431 RFD - DURING LINE CHECK, MAINTENANCE FOUND THE RT FORWARD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. EMERGENCY LIGHT SYSTEM OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 2623.0. (X) 2H72 4T RTA53EU 19950519001821995051900182NM 1995 5 19 95ZZZW670 119950212A5315 BEAM BOEING737 7372T4 1384492NM FS 986-1006 CORRODED A SPAAK NONE O OTHER ININSP/MAINT 1 WP07703S 22529 DURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-107-01, FLOOR BEAM SECTION RUNNING VERTICALLY FROM BS 986 TO 1006 WAS FOUND CORRODED BEYOND LIMITS. THE DAMAGED AREA WAS REPAIRED PER B-737 SRM 51-20-1 AND 51-30-2. (W) 2L72 4F A16WE 19950519001831995051900183NM 1995 5 19 95ZZZW671 119950212A5315 BEAM BOEING737 7372T4 1384492NM FS 986 CORRODED A SPAAK NONE O OTHER ININSP/MAINT 1 WP07703S 22529 DURING COMPLIANCE WITH AD 90-25-01 CPCP TAKS C53-107-01, FLOOR BEAM RUNNING HORIZONTALLY AT BS 986 WAS FOUND CORRODED BEYOND LIMITS. THE DAMAGED FLOOR BEAM SECTION WAS REPAIRED PER B-737 SRM 53-10-9. (W) 2L72 4F A16WE 19950519001841995051900184GL 1995 5 19 95ZZZW672 219950330A72106898246 GARLOCK SEAL 6874193 CVAC 440 440 2422902WP ALLSN 501D 501D13 03004GL LT GEAR BOX DETERIORATED A SPAAEA ENGINE SHUTDOWN UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP0773157 600981 312 ON A REPOSITIONING FLIGHT FROM MCI TO AVW, THE LEFT ENGINE REDUCTION GEAR BOX OIL PRESSURE BEGAN TO FLUCTUATE FOLLOWED BY A LOW OIL PRESSURE WARNING LIGHT. THE LEFT OIL QUANTITY INDICATION DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED TO DDC. RUN UP CHECK REVEALED OIL LEAKING FROM THE LEFT ENGINE STARTER CASE DRAIN. THE REDUCTION GEARBOX STARTER DRIVE GARLOCK SEAL WAS REPLACED. SUBSEQUENT LEAK CHECK WS SATISFACTORY. (W) 2L72 4R4 T 6A6 E282 19950519001861995051900186NE 1995 5 19 95ZZZW674 219950420A73105905588 SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE FUEL PRESS FAILED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07920HA21084 084 FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 HIGT PRESSURE FUEL FILTER BYPASS PRESSURE SWITCH AND HIGH AND LOW PRESSURE FUEL FILTERS. (W) 2H72 4T4 TRTA13NM E20NE 19950519001871995051900187NE 1995 5 19 95ZZZW675 219950420A73105905587 FUEL FILTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE ENG NR 1 FAILED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07920HA21084 084 FLT 3289 - TPA - MIA - DURING TAKEOFF, THE NR 1 FUEL FILTER BYPASS CAUTION LIGHT CAME ON. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 HIGT PRESSURE FUEL FILTER BYPASS PRESSURE SWITCH AND HIGHT AND LOW PRESSURE FUEL FILTERS. (W) 2H72 4T4 TRTA13NM E20NE 19950519001881995051900188NM 1995 5 19 95ZZZW676 119950418A33506013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003NM CABIN EEL FAILED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07926HA12345 SBY45 114 FLT 3322 - RIC-DCA - DURING PREFLIGHT WALKAROUND, FOUND FORWARD RED EMERGENCY LIGHTS AT 33520-PS3 AND PS4 INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND BASE. (W) 2H72 4T RTA13NM 19950519001891995051900189NM 1995 5 19 95ZZZW677 119950418A33506104791X BASE GRIMES DHAV DHC8 DHC8102 2809003NM CABIN EEL FAILED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07926HA18174 18174 114 FLT 3322 - RIC-DCA - DURING PREFLIGHT WALKAROUND, FOUND FORWARD RED EMERGENCY LIGHTS AT 33520-PS3 AND PS4 INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND BASE. (W) 2H72 4T RTA13NM 19950519001901995051900190NE 1995 5 19 95ZZZW678 219950404A73105905588 BYPASS SWITCH LUCAS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 2 FUEL PUMP FAILED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07942HA15800 163 FLT 3398 - BWI-YYZ - NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED ON TAKEOFF. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 FUEL FILTER BYPASS SWITCH. (W) 2H72 4T4 TRTA13NM E20NE 19950519001911995051900191NM 1995 5 19 95ZZZW679 119950418A3260841004 PSEU DHAV DHC8 DHC8102 2809003NM CABIN CLOSET FAILED A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07928HA16579 120 FLT 3343 - RIC-DCA - AFTER GO AROUND TO DCA, THE GEAR WAS SELECTED UP AND THE RIGHT MAIN DOOR LIGHT REMAINED ON. AFTER SELECTING GEAR DOWN, RIGHT MAIN GEAR UNSAFE LIGHT CAME ON. SELECTED GEAR UP AND LL LIGHTS WENT OUT. UPON SELECTING GEAR DOWN AGAIN, LEFT AND RIGHT MAIN GEAR GREEN LIGHT CAME ON. THE NOSE GEAR UNSAFE LIGHT STAYED ON FOR APPROXIMATELY 5 SECONDS, THE WENT GREEN. INSPECTED THE RIGHT FORWARD DOOR, AFT DOOR AND SENSORS FOR OPERATION AND SECURITY. ADJUSTED THE RIGHT FORWARD DOOR ACTUATOR ROD END AND SENSOR TARGET. REMOVED AND REPALCED PROXIMITY SWITCH ELECTRONIC UNIT. (W) 2H72 4T RTA13NM 19950519001921995051900192WP 1995 5 19 95ZZZW680 119950328A5210 TRIPLER LKHEED1011 10113851 5265010WP L1 DOOR CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11188AT 193C1078 IND - DURING A 'C4' CHECK, THE L1 DOOR WAS FOUND WITH A CRACK AT THE LOWER AFT CORNER, APPROX 1.5 INCHES LONG. A VISUAL INSPECTION DETECTED THIS CRACK TO A TRIPLER CUTOUT. STACKED DOUBLER ARRANGEMENT INSTALLED IAW SRM 53-31-00, FIG 836. 2L73 4F A23WE 19950519001931995051900193NM 1995 5 19 95ZZZW681 119950308A2435 GENERATOR BOEING727 7272B7 138407LNM NR 3 ENG FAULTY A AMTAA UNSCHED LANDING HO ELECT. POWER LOSS-50 PC OTHER CLCLIMB 1 GL11770AT 21953 FLT 299 - ORD DURING CLIMB THE NR 3 ENGINE GENERATOR FAILED (NR 1 GENERATOR WAS ON DEFERRAL AT TIME OF DEPARTURE). THE AIRCRAFT WAS DIVERTED TO IND. THE NR 3 ENGINE GENERATOR WAS REPLACED IAW MM 24-10-11 AND A RUN TEST CONFIRMED PROPER OPERATION OF GENERATOR. 2L73 4F A3WE 19950519001941995051900194NM 1995 5 19 95ZZZW682 119950227A2781 SWITCH BOEING727 7272Q8 138407WNM LE FLAPS CONTAMINATED A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11776AT 21608 FLT 255 - ORD - DURING TAKEOFF THE LEADING EDGE FLAPS NR 1/2 DID NOT INDICATE CORRECT POSITION FOR FLAP SETTING. AIRCRAFT WAS DIVERTED TO IND. MAINTENANCE PERSONNEL CLEANED DE-ICING FLUID RESIDUE FROM NR 1/5 LE FLAP CANNON PLUGS AND SWITCH ASSY. TESTED SWITCHES FOR CONTINUITY AND CHECKED OK. OPS CHECKED LE FLAPS GOOD. RETURN TO SERVICE. 2L73 4F A3WE 19950519001951995051900195EU 1995 5 19 95ZZZW683 119950423A29163800069101 RESERVOIR SAAB SF340 SF340A 7850100EU LT NLG WELL FAILURE A CHQAK NONE O OTHER ININSP/MAINT 1 EA23360CA 0043 340A006 THE HYDRAULIC QUANTITY INDICATING SYSTEM (MECHANICAL AND ELECTRIAL) WAS FOUND TO BE INOPERATIVE. THE SYSTEM WAS TROUBLESHOT AND THE HYDRAULIC RESERVOIR WAS FOUND TO BE THE PROBLEM. THE RESERVOIR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. 2L72 4T RTA52EU 19950519001961995051900196EU 1995 5 19 95ZZZW684 119950418A3260IR130907 SWITCH HONEYWELL SAAB SF340 SF340A 7850100EU LT MLG WOW OUT OF ADJUST A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA23360CA 340A006 PILOT RETURNED TO FIELD DUE TO CONFIG WARNING ILLUMINATION. THROUGH TROUBLESHOOTING, THE LEFT WEIGHT ON WHEEL SWITCH WS FOUND TO BE OUT OF ADJUSTMENT. THE SWITCH WAS ADJUSTED AND TEST FLIGHT PERFORMED WITH ALL INDICATIONS NORMAL. 2L72 4T RTA52EU 19950519001971995051900197EU 1995 5 19 95ZZZW685 119950416A77127239060502 CTOT PANEL SAAB SF340 SF340A 7850100EU COCKPIT PEDESTALFAILURE A CHQACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA23125CH 0130 340A125 PILOT ABORTED TAKEOFF DUE TO CTOT SET FOR 108 PERCENT, WHEN CTOT ENGAGED THE LEFT ENGINE WENT TO 1O8 PERCENT AND THE RT ENGINE LAGGED MOMENTARILY AND THEN SHOT TO 120 PERCENT. MAINTENANCE REPLACED THE CTOT PANEL AND PERFORMED A FUNCTIONAL CHECK OF THE SYSTEM, WITH ALL INDICATIONS NORMAL. (W) 2L72 4T RTA52EU 19950519001981995051900198WP 1995 5 19 95ZZZW686 219950420A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENG MALFUNCTION A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07856JS 744 FLT 4021 - DURING TAKEOFF AT APPROXIMATELY 80 KNOTS CAPTAIN NOTICED ERRATIC TORQUE INDICATION, LEFT ENGINE. TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT MAINTENANCE CONDUCTED ENGINE GROUND IAW GARRETT MM 72-00-00. UNABLE TO DUPLICATE PROBLEM, AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T4 TRTA21EU E4WE 19950519001991995051900199EU 1995 5 19 95ZZZW687 119950421A7712 CONNECTOR BAG JETSTMJETSTM3101 1500215EU LT ENG TQ CONTAMINATED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07856JS 744 FLT 4145 - ON TAKEOFF ROLL LEFT ENIGNE TORQUE INDICATION FLUCTUATED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. PIT MAINTENANCE PERSONNNEL INSPECTED AIRCRAFT AND DISCOVERED A CONTAMINATED CANNON PLUG, LEFT ENGINE TORQUE SIGNAL CONDITIONAL. CLEANED CANNON PLUG AND GROUND RAN ENGINE IAW GARRETT MM 72-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950519002001995051900200SO 1995 5 19 95ZZZW688 119950421A323012043270501 RELAY BOX EMB 120 EMB120RT SO COCKPIT FLOOR DEFECTIVE A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07331JS 12008JR 120035 FLT NR 4162 - CREW UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED TO CAK WHERE MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR RELAY BOX IAW EMB MM 32-31-02. OPS CHECKED LANDING GEAR IAW EMB MM 32-32-00, CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950519002011995051900201NE 1995 5 19 95ZZZW689 219950421A73205007070001 PS4 LINE BOEING727 727233 138408ANM PWA JT8 JT8D15A 52051NE NR 2 ENGINE BROKEN A PCSAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SO17395AJ 21100 687598 AFTER TAKEOFF DURING CLIMB NR 2 ENGINE FLAMED OUT, ENGINE RESTARTED BUT WOULD NOT ACCELERATE FROM IDLE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. AFTER TROUBLESHOOTING, FOUND PS4 LINE ON TOP OF ENGINE BROKEN. REPLACED LINE, OPS CHECK OK. 2L73 4F4 FRTA3WE E2EA 19950519002021995051900202NE 1995 5 19 95ZZZW690 219950422A7314243600 FUEL PUMP BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A PCSAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 SO17794AJ 21243 666350 DURING CRUISE NR 1 ENGINE FLAMED OUT AND WOULD NOT RESTART. AIRCRAFT LANDED AT DESTINATION AIRPORT. AFTER TROUBLESHOOTING FOUND ENGINE DRIVED FUEL PUMP DEFECTIVE. REPLACED PUMP, OPS CHECK OK. 2L73 4F4 F A3WE E2EA 19950519002031995051900203 1995 5 19 C2XA95CL081 419950502A3452066011430301 TRANSPONDER EMB 120 EMB120RT SO AVIONICS BAY INOP A C2XAK NONE O OTHER ININSP/MAINT 1 SW09167291119 1826 120185 FLT NR 3183 - CLE-SYR - MODE C- INOP BOTH NR 1 AND NR 2 TRANSPONDERS. MAINTENANCE REMOVED AND REPLACED NR 1 TRANSPONDER RECEIVER/TRANSMITTER. OPS CHECKED NR 1 AND NR 2 GOOD. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950519002041995051900204WP 1995 5 19 CAL950319 119950424A2612 LOOP DOUG DC10 DC1030 3023501WP FWD HALF DAMAGED A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0912061 47851 FLT NR 56 - EWR - ON TAKEOFF WARNING BELL CAME ON AIRCRAFT RETURNED TO EWR 'NO EMERGENCY DECLARED'. MAINTENANCE FOUND DAMAGE TO FIRE LOOP FWD HALF. REPAIRED AND REPLACED DAMAGED AREA AND PARTS. OPS CHECKED, SYSTEMS ALL NORMAL. AIRCRAFT DEPARTED NO FURTHER OCCURANCE. (W) 2L73 4F A22WE 19950519002051995051900205NM 1995 5 19 CAL950320 119950425A5610995611990012 WINDSHIELD BOEING727 727227 1384078NM F/O WINDSHIELD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09107564415 21042 FLT NR 693 - EWR - FOUND FLIGHT OFFICER WINDSHIELD OUTER PANE CRACKED. REMOVED AND REPLACED NR 1 WINDOW IAW MM 56-11-11 PAGE 401-412. (W) 2L73 4F A3WE 19950519002061995051900206WP 1995 5 19 DALR950001 119950403A5743 FITTING LKHEED1011 10113851 5265010WP LT AND RT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10 DURING THE REPLACEMENT OF THE INBOARD LEFT AND RIGHT REAR SPAR WEB AND REWORK OF THE UPPER 1.1250 INCH (2 TOTAL) AND INBOARD .6250 INCH (4 TOTAL) HOLES AT THE MLG BACKUP FITTING IWS 346, CORROSION WAS FOUND ON THE BORES OF THE 4 LOWER 1.1250 INCH HOLES AND THE INBOARD .75 INCH HOLE ON BOTH THE LEFT ADN RIGHT SIDE. HOLES WERE REWORKED PER DL ERA 270574-14AD. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519002071995051900207WP 1995 5 19 DALR950010 119950330A53201512315101 DOUBLER LKHEED1011 10113851 5265010WP FS 328 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 FUSELAGE NLG WHEELWELL MOD. FS 328 PER DL EO.7-53207-3AD. AN ADDITIONAL CRACK WAS FOUND THAT WAS BEYOND THE SCOPE OF THE E.O. THE CRACK LIES IN THE SKIN DOUBLER AT THE FORWARD LEFT CORNER OF THE NLG CUT-OUT, LBL 22 AT FS 328. THE CRACK EXTENDS FROM THE EDGE OF THE DOUBLER FORWARD 3 INCHES. THERE WAS ALSO CORROSION FOUND ON THE DOUBLER AT THIS LOCATION. REPAIRS ACCOMPLISHED PER DL ERA 270555-14AD. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519002081995051900208WP 1995 5 19 DALR950011 119950322A53201624729102 ANGLE LKHEED1011 10113851 5265010WP FS 1163-1203 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. COMPLY WITH AD 94-05-01, FOUND FUSELAGE MAIN FRAME FAIL-SAFE ANGLES AT FS 1203 LEFT AND RIGHT SIDE AND FS 1163 LEFT SIDE WERE FOUND CRACKED THROUGH THE VERTICAL LEG AT THE FRAME-TO-WING ROOT JOINT REINFORCEMENT. REPAIRS WERE ACCOMPLISHED PER DL ERA 270455-14AD. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519002091995051900209WP 1995 5 19 DALR950012 119950321A5711 SPAR LKHEED1011 10113851 5265010WP WING REAR CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. COMPLYING WITH AD 94-05-01 AND AD 93-17-10. WING REAR SPAR WEB AND UPPER CAP WERE REPLACED PER LAC SB 093057-196, R6 AND SB 0930570212,R0. AIRFRAME TT 38,155 HRS. CYCLES 18905. (X) 2L73 4F A23WE 19950519002101995051900210WP 1995 5 19 DALR950013 119950405A5730 WING SKIN LKHEED1011 10113851 5265010WP WS 332 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK, COMPLYING WITH AD 94-05-01 AND AD 93-17-01. AT THE REPLACEMENT OF THE LEFT WING INBOARD REAR SPAR SECTION, A CRACK WAS FOUND IN THE UPPER WING SKIN AT APPROXIMATELY IWS 332 AT A FASTENER HOLE. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK PER DL ERA 270601-14AD. AIRFRAME 38,155 HRS. CYCLES 18905. (X) 2L73 4F A23WE 19950519002111995051900211WP 1995 5 19 DALR950014 119950323A5743 FITTING LKHEED1011 10113851 5265010WP RT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. THE LEFT MLG FORWARD AND AFT TRUNNION ATTACH LUGS, BOTH THE FORWARD AND AFT LUGS WERE FOUND WORN AND WITH SURFACE CORROSION ON THE FACE AND INSIDE THE BORE. REPAIRED PER SRM 57-1400, PAGES 802-803. AIRFRAME TT 38,155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519002121995051900212WP 1995 5 19 DALR950015 119950323A5743 FITTINGS LKHEED1011 10113851 5265010WP LEFT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR, LEFT MLG TRUNNION ATTACH FITTINGS (FWD AND AFT) WERE FOUND WITH WEAR DAMAGE AND CORROSION ON THE FACE AND IN THE BORE OF THE FWD AND AFT LUGS. REPAIRED PER SRM 57-14-00, PAGE 803. AIRFRAME TT 38,155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519002131995051900213SW 1995 5 19 MALA954418 119950418A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 438.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 DURING BLOCK INSPECTION IN MSP, MAINTENANCE FOUND AT CARGO DOOR FRAME, FORWARD GAS STRUT MOUNT HOLE CRACKED OUT, FS 438.060. REPAIRED IAW FAIRCHILD ARP 53-20-9503 DATED MARCH 1, 1995. 1L72 4T A8SW 19950519002141995051900214SW 1995 5 19 MALA954419 119950418A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 DURING BLOCK INSPECTION IN MSP, FOUND LOWER LEFT BELT FRAME CRACKED AT RELIEF RADIUS, LOCATION FS 242.27 AND WL 81.07, RIGHT BELOW STRINGER NR 11. REPAIRED IAW FAC SRM 53-90-20 NR 19. (W) 1L72 4T A8SW 19950519002151995051900215SW 1995 5 19 MALA954420 119950418A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 332.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 DURING BLOCK INSPECTION IN MSP, FOUND LOWER LEFT BELT FRAME CRACKED AT RELIEF RADIUS, FS 332.27 AND WL 81.07, RIGHT BELOW STRINGER NR 11. REPAIRED IAW FAC SRM 53-90-20 NR 19. (W) 1L72 4T A8SW 19950519002161995051900216SW 1995 5 19 MALA954427 119950418A2931SS10127 PRESSURE SWITCH SWRNGNSA227 SA227AC 8780603SW RT HYD SYSTEM FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15442MA AC725 FLT 3016 - ON CLIMB-OUT FROM DTW, THE RIGHT HYDRAULIC CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT HYDRAULIC PRESSURE SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950519002171995051900217NM 1995 5 19 MALA954428 119950421A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT INOP A MALAK NONE L NO TEST ININSP/MAINT 1 GL15854MA 357 FLT 3205 - DURING THE PREFLIGHT IN MSP, THE COCKPIT HAND HELD EMERGENCY LIGHT WAS INOP. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950519002181995051900218NM 1995 5 19 MALA954430 119950421A7933 CONNECTOR DHAV DHC8 DHC8102 2809003NM RT ENGINE LOOSE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15819MA 251 FLT 3382 - ON CLIMB-OUT FROM DTW, THE RIGHT ENGINE OIL TEMP WAS HIGH. ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT RETURNED DTW. MAINTENANCE RESECURED A LOOSE CANNON PLUG. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950519002191995051900219SW 1995 5 19 MALA954431 119950419A32502782529041 POTENTIOMETER SWRNGNSA227 SA227AC 8780603SW NLG OUT OF NULL A MALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL15158MC AC762B FLT 3409 - DURING THE TAKEOFF ROLL IN CVG, THE NOSE STEERING FAIL LIGHT ILLUMINATED AND THE AIRCRAFT VEERED SLIGHTLY TO THE LEFT. THE AIRCRAFT RETURNED TO THE GATE. NWS DEFERRED IN CVG. MAINTENANCE NOTED NWS POTENTIOMETER OUT OF NULL. MAINTENANCE NULLED THE POTENTIOMETER. OPS CHECKED GOOD IAW FAC MM. (W) 1L72 4T A8SW 19950519002201995051900220EU 1995 5 19 SIMA950553 119950224A324050092361 WHEEL 5010488 SAAB SF340 SF340A 7850100EU NR 1 BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21112AE 340A112 ORD - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN ORD AND SENT OT WHEEL SHOP. THE WHEEL ASSY HAS 13 INCHES OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950519002211995051900221EU 1995 5 19 SIMA950721 119950313A324050092361 WHEEL SAAB SF340 340B 7860101EU NR 3 BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21594MA 340B212 WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN DFW AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS A 15 INCH OF INNER FLAGNE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. (W) 2L72 4T RTA52EU 19950519002221995051900222NE 1995 5 19 SIMA951131 219950423A72603022375 GARLOCK SEAL AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RT ENG LEAKAGE A SIMAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW21216AT 216 JAX - FLT 3528 - RT ENGINE OIL PRESSURE STEADILY DECREASED AFTER TAKEOFF BUT DID NOT DROP BELOW 42 PSI. AIRCRAFT RETURNED TO JAX. SENT MIA MTX TO JAX, INSPECTION ENGINE AND FOUND THE DC GENERATOR GEARLOCK SEAL LEAKING. REMOVED AND INSPECTED GARLOCK SEAL. NO LEAKS DETECTED. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950519002231995051900223EU 1995 5 19 SIMA951141 119950426A33503011210 LIGHT ASSY AEROSPATR42 ATR42300 8680920EU PAX/CREW DOOR DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21433MQ 603 151 RFD - DURING PS-2 CHECK, MAINTENANCE FOUND THE PAX DOOR EMERGENCY PROX LIGHT INOP. MAINTENANCE REPLACED PAX DOOR EMERGENCY LIGHT ASSY. EMERGENCY LIGHT SYSTEM OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950519002241995051900224NM 1995 5 19 TSAA9524075 119950425A242094103391 TRANSFORMER BOEING737 737297 1384480NM NR 1 ENG CURRENTINOP A TSAACD ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 WP13726AL 22426 PILOT REPORTED FLIGHT 88 - HNL-KOA - NR 1 GEN TRIPPED OFF BUS ON TAKEOFF, UNABLE TO RECONNECT. ABORTED TAKEOFF. DEFERRED PER MEL 24-1. TRANSCRIBED TOM-54 NR 03356, PLACARD INSTALLED. REPLACED NR 1 ENGINE CURRENT TRANSFORMER. OPS CHECK OK. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950519002251995051900225EU 1995 5 19 VTZA95151 119950429A3250AIR86002 SELECTOR BAG JETSTMJETSTM3201 1500217EU COCKPIT STEERINGFAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27497UE 904 FLT NR 6300 - IAD-ISP - DURING THE TAKEOFF ROLL, ABORTED THE TAKEOFF DUE TO THE STEERING UNCONTROLLABLE THEN PULLED HARD LEFT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NOSEWHEEL STEERING SELECTOR AND BOTH NLG TIRES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950519002261995051900226EU 1995 5 19 VTZA95152 119950501A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU RT ENGINE FIRE A AVTZAED ENGINE SHUTDOWN RETURN TO BLOCK A FLAME/FIRE TXTAXI/GRND HDL 1 EA27485UE 10 6122 901 FLIGHT NR 6242 - PHF-IAD - DURING ENGINE START UP EXPERIENCED AN ENGINE FIRE IN THE RT ENGINE. THE FLIGHT CREW SHUT THE ENGINE DOWN AND RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. AIRCRAFT REMAINS IN PHF AWAITING FURTHER INSPECTION. UPON FURTHER INSPECTION MAINTENANCE DISCOVERED THAT THE RT GENERATOR HAD CAUGHT FIRE. MAINTENANCE REPLACED THE STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950519002271995051900227NE 1995 5 19 VTZA95153 219950501A732031055016 TT2 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27311UE 41029 PT5037 FLT 6208 - BWI-IAD - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE IEC FAILURE ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTNENANCE REPLACED THE LEFT ENGINE TT2 SENSOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA41NM E18NE 19950519002281995051900228EU 1995 5 19 VTZA95154 119950502A3230S2700003 AOG SLAVE RELAY JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 FLT 64898 - IAD-ORF - DURING TAKEOFF, RETURNED TO IAD WITH NO FURTHER INCIDENTS DUE TO THE GEAR NOT RETRACTING WHEN SELECTED UP. MAINTENANCE REPLACED THE NR 1 AND NR 2 AOG SLAVE RELAYS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950519002291995051900229NE 1995 5 19 95ZZZX2354 219950427A731437340126 FUEL PUMP BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 1 ENGINE FAILED A TWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 CE0593108 19674 LAX - FLT 841 - DURING APPROACH, NR 1 ENGINE, SN 4162, SPUN DOWN. SHUT DOWN ENGINE. REPLACED NR 1 ENGINE FUEL PUMP, MFG PN 373401-26, AND FUEL CONTROL, MFG PN 747999-5. ENGINE GROUND RUN UP OPERATION CHECKED NORMAL. CHECK C-2 - 1-29-95 - MCI. 2L74 4F4 F A20WE E20EA 19950519002301995051900230NE 1995 5 19 95ZZZX2355 219950427A73217379995 FUEL CONTROL BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 1 ENGINE FAILED A TWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 CE0593108 19674 LAX - FLT 841 - DURING APPROACH, NR 1 ENGINE, SN 4162, SPUN DOWN. SHUT DOWN ENGINE. REPLACED NR 1 ENGINE FUEL PUMP, MFG PN 373401-26, AND FUEL CONTROL, MFG PN 747999-5. ENGINE GROUND RUN UP OPERATION CHECKED NORMAL. CHECK C-2 - 1-29-95 - MCI. 2L74 4F4 F A20WE E20EA 19950519002311995051900231WP 1995 5 19 95ZZZX2356 119950424A3245 TIRE DOUG DC9 DC983 3022083WP NLG FAILED A TWAAO OTHER O OTHER TOTAKEOFF 1 CE059302B 49528 PHX - FLT 730 - ON TAKEOFF FOLLOWING A SHARP IMPACT ON FUSELAGE FROM RIGHT NOSE TIRE TREAD FAILURE, BOTH COMPASSES, FLIGHT DIRECTORS, AND ATTITUDE DIRECTOR INDICATORS FAILED. AFTER LANDING, REMOVED AND RE-ESTABLISHED POWER TO ATTITUDE AND HEADING REFERENCE SYSTEMS. ALIGNMENT OF BOTH SYSTEMS WAS NORMAL AND SYSTEMS OPERATIONAL CHECK WAS NORMAL. CHECK C-1D - 4-6-95 - MCI. 2L72 4F RTA6WE 19950519002321995051900232SW 1995 5 19 95ZZZX2357 119950421A32302751008041 BELLCRANK SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15422MA AC635 MSP - FLT 3494 - ON APPROACH, RIGHT MAIN GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE RIGHT INBOARD GEAR ACTUATOR, PN 27-51016-003, AND BELLCRANK ASSEMBLY, PN 27-51008-041. SYSTEM OPERATED SATISFACTORILY. REF OPERATOR CONTROL NR MALA954429. 1L72 4T A8SW 19950519002331995051900233SW 1995 5 19 MALA954408 119950327A32301EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL1560NE AC760B CMS - FLT 3129 - ON CLIMBOUT, NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW PULLED, THEN AFTER 5 MINUTES, RESET THE LANDING GEAR CONTROL CIRCUIT BREAKER. ONCE THE BREAKER WAS RESET, THE GEAR UPLOCKED NORMALLY. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE ADJUSTED THE RIGGING OF THE UPLIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950519002341995051900234NM 1995 5 19 MALA954409 119950411A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15831MA 339 MSP - FLT 3426 - DURING POST-FLIGHT, SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE COAT CLOSET UPPER EMERGENCY BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950519002351995051900235SW 1995 5 19 MALA954410 119950411A32302752000077 UPLOCK ROLLER SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15428MA AC646 DTW - FLT 3014 - AFTER TAKEOFF, NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NOSE GEAR DOOR UPLOCK ROLLER. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950519002361995051900236NM 1995 5 19 MALA954411 119950412A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15833MA 343 DTW - FLT 3422, DURING THE PRE-FLIGHT FOR THE FIRST FLIGHT OF THE DAY, ALL OF THE CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED ALL OF THE EMERGENCY LIGHT BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950519002371995051900237NM 1995 5 19 MALA954412 119950416A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15828MA 333 DTW - DURING SCHEDULED MAINTENANCE, THE COCKPIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMRGENCY EXIT LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950519002381995051900238SW 1995 5 19 MALA954413 119950416A215020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW RT WING SEIZED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15446MA AC693 TVF - FLT 3446 - IN CRUISE FLIGHT, CREW NOTED THE RIGHT BLEED WAS PRODUCING SMOKE IN THE CABIN AND COCKPIT. THE CREW PERFORMED QUICK REFERENCE HANDBOOK PROCEDURES AND DIVERTED TO MJI. MAINTENANCE REPLACED THE RIGHT COOLING TURBINE. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950519002391995051900239WP 1995 5 19 MALA954414 219950416A7530 BLEED AIR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RIGHT ODOR A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15160MC AC733B MSP - FLT 3235 - EN ROUTE, CREW NOTED A HOT SMELL FROM THE RIGHT BLEED SYSTEM. THE CREW SHUT OFF THE RIGHT BLEED SYSTEM AND THE SMELL DISSIPATED. THE AIRCRAFT CONTINUED TO MSP. THE SYSTEM IS CURRENTLY DEFERRED UNDER MEL 21-9C. (X) 1L72 4T4 T A8SW E4WE 19950519002401995051900240SW 1995 5 19 MALA954415 119950417A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL1526863 AC650B MSP - FLT 3229 - ON APPROACH, RIGHT LANDING GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. ALL OTHER GEAR INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE RIGHT UP POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950519002411995051900241NM 1995 5 19 MALA954416 119950417A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15817MA 249 DTW - FLT 3064 - DURING PRE-FLIGHT, THE EXIT SIGN OVER THE MAIN ENTRANCE DOOR WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE TOP WARDROBE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950519002421995051900242SW 1995 5 19 MALA954417 119950418A3260 DOOR LIGHT SWRNGNSA227 SA227AC 8780603SW LANDING GEAR ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15425MA AC640 DTW - FLT 3452 - ON CLIMBOUT, GEAR DOOR POSITION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950519002431995051900243SW 1995 5 19 MALA954421 119950418A5320 DOOR SILL SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 MSP - DURING BLOCK CHECK, FOUND SMALL CRACK APROXIMATELY .250-.300 INCH AT RADIUS OF CUT-OUT FOR FUSELAGE FRAME AT FS 438.0 IN CARGO DOOR SILL. REPAIRED BY STOP DRILLING CRACK, FABRICATING AND INSTALLING DOUBLERS IAW FAIRCHILD LAR-95-MALA-114 DATED APRIL 10, 1995. (X) 1L72 4T A8SW 19950519002441995051900244SW 1995 5 19 MALA954422 119950418A5753 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 MSP - DURING BLOCK INSPECTION, FOUND LT FLAP WALKING BEAM ROLLER DOUBLER WORN. REPAIRED WORN DOUBLER WITH NEW. PN 27-31141-001, IAW FAC SRM 57-90-10, NR 11 AND FAC ARP 57-20-9424. (X) 1L72 4T A8SW 19950519002451995051900245SW 1995 5 19 MALA954423 119950418A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 317.21 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 MSP - DURING BLOCK INSPECTION, FOUND LOWER LT BELT FRAME CRACKED AT RELIEF RADIUS. LOCATION: FS 317.21 AND WL 81.07, RIGHT BELOW STR 11. REPAIRED IAW FAC SRM 53-90-20, NR 19. (X) 1L72 4T A8SW 19950519002461995051900246SW 1995 5 19 MALA954424 119950418A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 MSP - DURING BLOCK INSPECTION FOUND RT LOWER BELT FRAME CRACKED AT RELIEF RADIUS. LOCATION FS 159.24 AND WL 81.00, RIGHT BELOW STR 11A. REPAIRED IAW FAC SRM 53-90-29, NR 19. (X) 1L72 4T A8SW 19950519002471995051900247SW 1995 5 19 MALA954425 119950418A27202742051037 TQ TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER TWISTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 MSP - DURING BLOCK CHECK, FOUND RUDDER TORQUE TUBE, PN 27-42051-037, TWISTED. REPLACED WITH SERVICEABLE PN 27-42051-0837 IAW FAIRCHILD MM 27-20-20, PAGES 201-202, AND FAC SRM 51-00, PAGE 4. (X) 1L72 4T A8SW 19950519002481995051900248SW 1995 5 19 MALA954426 119950420A3240 BRAKES SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15158MC AC762B FLT 3378 - WHILE TAXIING AIRCRAFT, CREW REPORTED THE RIGHT BRAKE WAS WEAK. MAINTENANCE BLED THE RIGHT BRAKES. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950519002491995051900249SW 1995 5 19 MALA954429 119950421A32332751016003 ACTUATOR SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15422MA AC635 MSP - FLT 3494 - ON APPROACH, RIGHT MAIN GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE RIGHT INBOARD GEAR ACTUATOR, PN 27-51016-003, AND BELLCRANK ASSEMBLY, PN 27-51008-041. SYSTEM OPERATED SATISFACTORILY. REF OPERATOR CONTROL NR 95ZZZX2357. (X) 1L72 4T A8SW 19950519002501995051900250NE 1995 5 19 9507915519 219950514A7200 ENGINE BOEING757 757251 1384970NM PWA 2037 PW2037 NE RIGHT FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01519US 23207 716347 ON TAKEOFF, THE RIGHT ENGINE SPOOLED UP SLOWER THAN THE LEFT ENGINE. A POP WAS HEARD AND THE TAKEOFF WAS ABORTED. EGT STAYED AT APPROXIMATELY 535, OTHER PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO THE GATE. ENGINE CHANGE IS IN PROGRESS. 2L72 4F4 FRTA2NM E17NE 19950519002511995051900251NE 1995 5 19 9507929301 219950513A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL01301RC 48054 708440 IN CRUISE AT FL310, THE NR 1 ENGINE OIL QUANTITY STARTED DECREASING RAPIDLY. THE FLIGHT DIVERTED TO MKE. APPROXIMATELY 10 MINUTES PRIOR TO LANDING, THE OIL QUANTITY INDICATED 2 QUARTS AND OIL PRESSURE BEGAN TO DETERIORATE. A PRECAUTIONARY SHUTDOWN WAS PERFORMED, THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE. ENGINE SYSTEMS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E9NE 19950519002521995051900252WP 1995 5 19 9507939864 119950511A3610 ACM DUCT DOUG DC9 DC951 3022051WP LEFT SIDE BLOWN A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01773NC 47775 TAIL COMPARTMENT TEMPERATURE HIGH AND MASTER WARNING LIGHTS ILLUMINATED DURING CLIMBOUT FROM RDU. LIGHTS STAYED ON FOR APPROXIMATELY THREE SECONDS THEN EXTINGUISHED. AFTER A FEW MINUTES, AGENT 2 LOW LIGHT ILLUMINATED AND REMAINED ON. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. FOUND LEFT ACM DUCT BLOWN AND NR 2 FIRE AGENT BOTTLE HAD DISCHARGED. REPLACED DUCT AND NR 2 FIRE AGENT BOTTLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519002531995051900253WP 1995 5 19 9507949905 119950511A2780 RETRACT MECH DOUG DC9 DC931 3022065WP LE FLAPS LACK OF LUBE A NWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL01955N 47160 ON APPROACH INTO GRR DURING SLAT EXTENSION, SLAT DISAGREEMENT LIGHT ILLUMINATED AND AIRCRAFT ROLLED TO THE RIGHT. CYCLED SLATS SEVERAL TIMES WITH NO HELP. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT RETURNED TO DTW. AN UNEVENTFUL LANDING WAS MADE WITHOUT SLATS EXTENDED. CLEANED FLAP HYDRAULIC LINE RESTRICTORS AND SLAT RESTRICTOR VALVES, LUBRICATED SLAT CARRIAGE ROLLERS AND FLAP TRACK ROLLERS. ALSO, CHECKED T-DUCTS FOR BINDING, CYCLED SLATS NUMEROUS TIMES. ALL CHECKED OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519002541995051900254WP 1995 5 19 9507959905 119950512A2780 T-DUCTS DOUG DC9 DC931 3022065WP LE FLAPS LACK OF LUBE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01955N 47160 DURING APPROACH INTO MBS, SLAT DISAGREEMENT LIGHT ILLUMINATED AND AIRCRAFT ROLLED TO THE RIGHT. CYCLED SLATS WITH NO HELP. FIRST OFFICER VISUALLY CONFIRMED RIGHT SLAT TO BE APPROXIMATELY 3 INCHES SHORT OF FULL EXTENSION. SLATS EVENTUALLY ACHIEVED NORMAL CONFIGURATION. AIRCRAFT LANDED WITHOUT INCIDENT. LUBRICATED SLAT T-DUCTS. CYCLED SLAT SEVERAL TIMES WITH NO PROBLEMS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519002551995051900255WP 1995 5 19 9507969947 119950514A2130 CONNECTOR DOUG DC9 DC931 3022065WP PRESS SYST CONTAMINATED A NWAAO OTHER J WARNING INDICATION UKUNKNOWN 1 GL018938E 47161 LOSS OF CABIN PRESSURIZATION OCCURRED AT 33,000 FEET. CABIN ALTITUDE CLIMBED TO 11,000 FEET. OXYGEN MASKS DID NOT DEPLOY. CABIN PRESSURE WAS REGAINED AT 23,000 FEET AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. CLEANED CANNON PLUG ON PRESSURE AMPLIFIER. ALSO, CHECKED ALL LINES AND HOSES IN AFT TAIL SECTION AND ACCESS PANEL TO OUTFLOW VALVE IN AFT CARGO. ALL CHECKED OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519002561995051900256WP 1995 5 19 9507979976 119950514A3610 DUCTS DOUG DC9 DC931 3022065WP RT PACK LEAKING A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019340 47389 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. LIGHT EXTINGUISHED WHEN POWER WAS PULLED BACK, BUT CAME ON AGAIN ONCE POWER WAS ADDED. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT RETURNED TO MEM, LANDING WAS UNEVENTFUL. FOUND TWO DUCT LEAKS AT RIGHT PACK AND TEMPERATURE SENSOR PLUGGED. REPAIRED LEAKS AND REPLACED SENSOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519002571995051900257NM 1995 5 19 9507982282 119950512A3230 RETRACT MECH BOEING727 727251 138408HNM NLG LACK OF LUBE A NWAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL01282US 21161 DURING APPROACH UPON GEAR EXTENSION, NOSE LANDING GEAR UNSAFE INDICATION REMAINED ILLUMINATED. PERFORMED GO-AROUND AND RETRACTED GEAR. SECOND EXTENSION WAS NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBED AND SERVICED NOSE LANDING GEAR ASSEMBLY. OPERATIONAL GEAR SWING WAS NORMAL. 2L73 4F A3WE 19950519002581995051900258NE 1995 5 19 9507999909 219950513A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7 52053NE NR 2 FAILED A NWAAO OTHER JX WARNING INDICATION ENGINE FLAMEOUT APAPPROACH 1 GL01959N 47255 657274 ON APPROACH TO MSP, THE NR 2 ENGINE FLAMED-OUT. RELIGHT ATTEMPTS WERE UNSUCCESSFUL. THE FLIGHT WAS CONCLUDED WITHOUT INCIDENT. GROUND START ATTEMPTS PRODUCED NO N2 ROTATION ON STARTER ENGAGEMENT. METAL CONTAMINATION WAS FOUND IN THE GEARBOX. MAINTENANCE REPLACED THE ENGINE. ENGINE SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. N1 ROTATION CHANGED TO N2 ROTATION. 2L72 4F4 F A6WE E2EA 19950519002591995051900259NM 1995 5 19 9508002708 119950515A27821U109592 ACTUATOR BOEING727 727225 1384077NM NR 8 LE FLAP FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01817EA468063699 22554 DURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE UNSAFE INDICATION REMAINED ILLUMINATED. CAPTAIN REQUESTED CFR TO STANDBY AND RETURNED TO MKE WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED JUMPER ON NR 8 LEADING EDGE SLAT AND DEFERRED ACTUATOR FOR REPLACEMENT. 2L73 4F A3WE 19950519002601995051900260SO 1995 5 19 COM11890 119950515A27503472001001 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01246CA6976 892 120223 FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 15 DEGREES. REPLACED THE FLAP CONTROL UNIT. 2L72 4T RTA31SO 19950519002611995051900261 1995 5 19 COM20368 419950515A34182782181041 SAS CONTROL SWRNGNSA227 SA227AC 8780603SW AVIONICS DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01702M 15072 AC702 SAS ARM INDICATOR REMAINED ON ABOVE 145 KNOTS. REPLACED THE SAS CONTROL BOX. 1L72 4T A8SW 19950519002621995051900262SW 1995 5 19 COM20369 119950515A324631418 WHEEL SWRNGNSA227 SA227AC 8780603SW NLG DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01704C 1075594 AC704 LT NOSE WHEEL IS SLINGING GREASE. REPLACED WHEEL ASSY. 1L72 4T A8SW 19950519002631995051900263EA 1995 5 19 COM60474 119950515A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 2 DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01918CA89 29 7018 FLIGHT SPOILER STATUS MESSAGE ON EICAS. REPLACED THE NR 2 SECU. 2L72 4F RTA21EA 19950519002641995051900264NM 1995 5 19 DHL95741004 119950512A2497 WIRE BOEING727 7272Q9 138448MNM P6 PANEL FAILED A ADHLACD ABORTED TAKEOFF RETURN TO BLOCK BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TOTAKEOFF 1 SO01741DH 21931 APPROACHING V1, EXPERIENCED PARTIAL LOSS OF ELECTRICAL POWER WITH ARCHING AND SMOKE FROM LOWER P6 PANEL. ABORTED TAKEOFF AND RETURNED TO BLOCKS. NR 1 GEN BKR AND FIELD RELAY TRIPPED AND NR 1 DIFFERENTIAL FAULT ILLUMINATED. ARCHING AND SMOKE CONTINUED UNTIL NR 1 ENGINE SHUTDOWN. FOUND SEVERAL WIRES SEVERED BY HEAT. REPLACED WIRES, OPS CHECKED GOOD IAW M/M 24-54-0. 2L73 4F RTA3WE 19950519002651995051900265EU 1995 5 19 DL31L951876 119950503A5330A53611171200 SKIN AIRBUS310 A310324 3930206EU FUS BELLY LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11840AB 682 49810 APPARENT LIGHTNING STRIKE AT LWR CENTER LINE OF ACFT BELLY FRAME 4 REQUIRES SRM REPAIR 53-11-12 PG 207 TO 210. 2L72 4F RTA35EU 19950519002661995051900266EU 1995 5 19 DL31L952121 119950511A3260DSB112 SENSOR AIRBUS310 A310324 3930206EU NLG FAILED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11843AB 689 AT FL 350 PITCH TRIM 2 ATS DROPPED OFF, STBY PITOT ALSO OFF AND FD NR 2 OFF. ALL WOULD RESET, BUT FAULT AGAIN. DIVERTED TO JFK. REPLACED NOSE GEAR PROX SENSOR 82GB. RETURNED TO SERVICE. 2L72 4F RTA35EU 19950519002671995051900267NM 1995 5 19 DL72E951890 119950502A5320 LIGHTNING HOLE BOEING727 727247 138408FNM FS 1236 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, .25 INCH CRACK IN LIGHTNING HOLE, RBL 20, FS 1236, LOWER HOLE. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950519002681995051900268NM 1995 5 19 DL72E951891 119950502A5320 LIGHTNING HOLE BOEING727 727247 138408FNM FS 1239 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, .25 INCH CRACK IN LIGHTNING HOLE, LBL 20, STA 1239, LOWER HOLE. REPAIRED AS PER M/M 53-11-0. 2L73 4F A3WE 19950519002691995051900269NM 1995 5 19 DL72E951892 119950502A5754 SLAT BOEING727 727247 138408FNM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, NR 7 L/E SLAT CRACKED BELOW TAI DUCT SLAT S/N 1172. REPAIRED PER M/M 57-54-0 PAR 5A P807A. 2L73 4F A3WE 19950519002701995051900270NM 1995 5 19 DL72K952125 119950511A3350900542 EEL RACK BOEING727 727232 1384082NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11472DA 20749 ON LAYOVER, FOUND RT OVERWING EMERGENCY EXIT SIGN INOP DURING TEST. REPLACED RACK ASSEMBLY OPERATION NORMAL. 2L73 4F A3WE 19950519002711995051900271NM 1995 5 19 DL72S951806 119950130A5753 TE FLAP 652163262 BOEING727 727232 1384082NM LEFT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA BN7 21061 49810 AFT I/B CONTROL ROD CUTOUT HAS CRACKED O/B CORNER (MARKED). MANUFACTURED AND INSTALLED DOUBLER PER MM 57-52-0 PAGE 819 FOR NR 3 MID FLAP AT HMV, SHOP INSPECTION. 2L73 4F A3WE 19950519002721995051900272NM 1995 5 19 DL72S951809 119950430A5751 SKIN 65217659 BOEING727 727232 1384082NM LT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 196 21150 49810 727 I/B AILERON, LOWER I/B EDGE SKIN CRACKED, FOUND AT LTR CHECK. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950519002731995051900273NM 1995 5 19 DL72S951825 119950410A5530 WEB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND WEB CRACKED STA 1303 LWR RT CORNER INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 16. 2L73 4F A3WE 19950519002741995051900274NM 1995 5 19 DL72S951826 119950410A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND STR 8L CRACKED 3RD BAY UP FROM ACCESS HOLE INSIDE VERT STAB. REPAIRED PER M/M 55-30-00 PG 803. 2L73 4F A3WE 19950519002751995051900275NM 1995 5 19 DL72S951838 119950501A5754 WEB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 49810 FOUND ON F1 LTR CK, NR 6 SLAT OTBD ACT ROD END WEB CRACKED AFT SIDE. REPAIRED PER M/M 57-54-0 PAR 3. 2L73 4F A3WE 19950519002761995051900276NM 1995 5 19 DL72S951857 119950202A5753652163261X SKIN BOEING727 727232 1384082NM NR 2 MID FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 49810 NR 2 MID FLAP DURING HMV SHOP INSP, WAS FOUND TO BE DELAMINATED FROM 0 TO 3 FROM O/B END AND POTTING COMPOUND DETERIOIATED. REPAIRD PER SRM 57-50-4 . 2L73 4F A3WE 19950519002771995051900277NM 1995 5 19 DL72S951870 119950416A5313 STRINGER BOEING727 727232 1384082NM FS 1148 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, STR 25L CORRODED STA 1148. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950519002781995051900278NM 1995 5 19 DL72S951871 119950501A5312 WEB BOEING727 727232 1384082NM FS 870 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND STA 870 WEB CRACKED AT APU BLEED VALVE CUTOUT. REPAIRED PER SRM 53-10-9. 2L73 4F A3WE 19950519002791995051900279NM 1995 5 19 DL72S951873 119950422A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 49810 DURING HMV, FOUND STRINGER 1 LEFT CRACKED AT RIB 3A INSIDE VERT STAB. REPAIRED PER M/M 53-30-0 PG 803. 2L73 4F A3WE 19950519002801995051900280NM 1995 5 19 DL72S951883 119950427A5753652163362 FITTING BOEING727 727232 1384082NM RT TE MID FLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 4 MID FLAP, I/B CARRIAGE SUPPORT FITTING, BOTTOM I/B THRUST BEARING RETAINER BOLT HOLE CORRODED. ALSO, O/B CARRIAGE SUPPORT FITTING, BOTH BOTTOM THRUST BEARING RETAINER BOLT HOLES CORRODED. REPAIRED PER SRM 57-50-04 PG 34. REAMED OVERSIZE AND INSTALLED BUSHINGS. 2L73 4F A3WE 19950519002811995051900281NM 1995 5 19 DL72S951887 119950429A5230 SKIN BOEING727 727232 1384082NM C3 DOOR HOLE A DALAI CABIN DEPRESSURIZATION O OTHER ININSP/MAINT 1 SO11545DA 22494 HOLE IN INNER SKIN, C3 DOOR ABOUT 6 FWD OF FWD LOWER DOOR STOP FITTING. REPAIRED PER MM 52-30-2 FIG 3. 2L73 4F A3WE 19950519002821995051900282NE 1995 5 19 DL72S952055 219950510A731437820113 FUEL PUMP BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE SHEARED SHAFT A DALAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SO11411DA 21223 687377 AFTER TAKEOFF, AT 500 FEET NR 1 ENGINE FLAMED-OUT. RETURNED BDL. TROUBLESHOOTING FOUND NO FUEL FLOW TO ENGINE. REPLACED ENGINE DRIVEN PUMP AND FUEL CONTROL, OPERATION NORMAL. 2L73 4F4 F A3WE E2EA 19950519002831995051900283NM 1995 5 19 DL72W951748 119950420A5754651622296 SPAR BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 49810 DURING SHOP INSPECTION, RT WING NR 6 L/E SLAT WAS FOUND WITH THE SPAR CRACKED AT THE CUTOUT FOR THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0 FIG 810. 2L73 4F A3WE 19950519002841995051900284NM 1995 5 19 DL72W951827 119950123A5753 FLAP 65162255A BOEING727 727247 138408FNM NR 3 FORE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112825W 21330 49810 UPON SHOP INSPECTION, A CRACK WAS FOUND AT CUTOUT FOR THE AFT FLAP LINKAGE. NR 3 FOREFLAP. REPAIRED PER DL ERA 270769-14. 2L73 4F A3WE 19950519002851995051900285NM 1995 5 19 DL72W951846 119950329A5753652163396 RIB BOEING727 727247 138408FNM NR 4 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 NR 4 MID FLAP, I/B AFT CLOSE-OUT RIB CRACKED. REPAIRED PER M/M 57520 FIG 808, MFG'D AND INSTALLED DOUBLER. FOUND AND REPAIRED DURING SHOP INSPECTION. 2L73 4F A3WE 19950519002861995051900286NM 1995 5 19 DL72W951856 119950502A5330 SKIN BOEING727 727247 138408FNM FS 530 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 49810 FOUND DURING LETTER CHECK, FUSELAGE SKIN BULGED AND SKIN CRACKED EXTENDING FROM RIVET HOLES .0625 INCH 2 EA AT STA 530 AT FUSELAGE LAP JOINT STRINGER 26R. REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950519002871995051900287NM 1995 5 19 DL72W951860 119950502A5210 WEB BOEING727 727247 138408FNM L1 ENTRY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 49810 FOUND DURING F-1 LETTER CHECK, 1.5 INCH CRACK AT MAIN ENTRY DOOR UPPER AFT CLOSE-OUT WEB. SPLICED IN NEW SECTION OF DOOR FRAME PER MM 52-11-1. 2L73 4F A3WE 19950519002881995051900288NM 1995 5 19 DL72W952126 119950429A2530 OVEN BOEING727 727247 138408FNM FWD GALLEY SMOKING A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO112813W 20869 DURING CRUISE, FLT ATTENDANT REPORTED FWD GALLEY OVEN EMITTED SMOKE AS SOON AS IT WAS TURNED ON. OVEN WAS INSPECTED, PROBLEM COULD NOT BE DUPLICATED, RETURNED TO SERVICE. 2L73 4F A3WE 19950519002891995051900289NM 1995 5 19 DL73S951842 119950424A575365464350276A FLAP SKIN BOEING737 737232 1384475NM NR 4 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11332DL 23104 49810 DURING SHOP INSP, RT WING NR 4 AFT FLAP WAS FOUND WITH A TIME LIMITED REPAIR 10 INCHES FROM THE IN/B END ON THE L/E OF FLAP. INSTALLED PERMANENT REPAIR PER SRM 57-50-4 FIG 5. 2L72 4F RTA16WE 19950519002901995051900290NM 1995 5 19 DL73S952122 119950513A3320 CONTROL PANEL BOEING737 737232 1384475NM FWD CABIN SHORTED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11327DL 23099 ON TAXI OUT, HAD SMOKE AND SPARKS COMING FROM CABIN LIGHT CONTROL PANEL AT FWD ENTRY DOOR. REPAIRED SHORTED WIRES, RETURNED TO SERVICE. 2L72 4F RTA16WE 19950519002911995051900291NM 1995 5 19 DL757951708 119950227A5743114N3002119A SKIN BOEING757 757232 1384965NM LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11611DL 22818 49810 AT SHOP INSPECTION, L/E SLAT PANEL WAS FOUND WITH THE TRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519002921995051900292NM 1995 5 19 DL757951810 119950425A5400 LIGHTNING HOLE BOEING757 757232 1384965NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 49810 NR 1 PYLON OUTBD LIGHTNING HOLE SHOWS CRACK INDICATION BY E/C ON UPPER AFT CORNER. FOUND AT HMV, REPAIRS ACCOMPLISHED PER DL ERA 270637-14. 2L72 4F RTA2NM 19950519002931995051900293NM 1995 5 19 DL757951813 119950421A5320 FORMER BOEING757 757232 1384965NM FS 1540 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 49810 AT HMV, FOUND RT FORMER DENTED AT STA 1540 ABOVE FIXED FLOOR PANEL. CUT OUT DAMAGED AREA AND INST REPAIR DOUBLER PER SRM 51-70-11 PAGE 1 TO 5. 2L72 4F RTA2NM 19950519002941995051900294NM 1995 5 19 DL757951814 119950421A5414 SKIN BOEING757 757232 1384965NM RT ENG STRUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 49810 AT HMV, FOUND NR 2 ENG STRUT CRACKED AT OVAL ACCESS HOLE AT FWD END OF STRUT RT SIDE ABOVE FWD ENG MOUNT. REPAIRED PER SRM 54-51-01 FIG 203. 2L72 4F RTA2NM 19950519002951995051900295NM 1995 5 19 DL757951820 119950320A5350 RADOME 141N782013 BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11666DN DL76 25034 49810 RECEIVED RADOME IN SHOP FOR DELAMINATION. INSPECTED RADOME AND FOUND EXCESSIVE MOISTURE. REMOVED INSIDE SKIN TO DRY MOISTURE. REPLACED DAMAGE CORE, REPLACED INSIDE SKIN AS PER SRM 53-10-72 ERROSION PROTECTION AND PAINT APPLIED AS PER PS 900-9-1-11, NR 05. TRANSMISSIVITY TESTED AND PASSED TEST. RADOME SENT TO STOCK. 2L72 4F RTA2NM 19950519002961995051900296NM 1995 5 19 DL757951839 119950407A5350 RADOME 141N782013 BOEING757 757232 1384965NM NOSE DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11616DL DL16 22823 49810 RADOME HAD A BIRD STRIKE ON CENTER OF NOSE. AFTER INSPECTION RADOME DELAMINATION AND MOISTURE ABOVE LIMITS. REBUILD RADOME COMPLETE PER SRM 53-10-72. CUT RADOME OFF ABOVE BASE RING AND REBUILD IN 757 MOLD SYSTEM. PAINT PER SP 900-9-1-11, NR 05, TRANSMISSIVITY TESTED. RETURN TO STOCK SERVICABLE. 2L72 4F RTA2NM 19950519002971995051900297NM 1995 5 19 DL757951840 119950502A5754114N4004171A TE WEDGE BOEING757 757232 1384965NM NR 3 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 DURING INSPECTION LEFT WING NR 3 L/E SLAT WAS FOUND WITH NUMEROUS DENTS ON UPPER SURFACE OF WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519002981995051900298NM 1995 5 19 DL757951841 119950502A5754114N4003183A SKIN BOEING757 757232 1384965NM NR 2 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 DURING INSPECTION, LEFT WING NR 2 L/E SLAT T/E WEDGE UPPER SKIN WAS FOUND WITH NUMEROUS DENTS. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519002991995051900299NM 1995 5 19 DL757951844 119950418A5754114N4002148A TE WEDGE BOEING757 757232 1384965NM NR 10 TE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11638DL 23761 49810 DURING SHOP INSPECTION, RT WING NR 10 L/E SLAT WAS FOUND WITH DELAMINATION TO THE T/E WEDGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519003001995051900300NM 1995 5 19 DL757951845 119950502A5754114N4003184A SKIN BOEING757 757232 1384965NM NR 9 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 DURING INSPECTION, FOUND RT WING NR 9 L/E SLAT WEDGE UPPER SKIN DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519003011995051900301NM 1995 5 19 DL757951849 119950502A5754114N4005157 SKIN BOEING757 757232 1384965NM NR 4 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11653DL 24393 49810 UPPER OUTBOARD SECTION OF TRAILING EDGE WEDGE DELAMINATED. LOWER SKIN OF TRAILING EDGE WEDGE PUNCTURED. REPLACED TRAILING EDGE WEDGE AS PER SRM 57-43-02. FOUND AND REPAIRED DURING SHOP INSPECTION. 2L72 4F RTA2NM 19950519003021995051900302NM 1995 5 19 DL757951855 119950501A5754114N4004172A SKIN BOEING757 757232 1384965NM NR 8 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 DURING INSPECITON, RT WING NR 8 SLAT WAS FOUND WITH WEDGE UPPER SKIN DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519003031995051900303NM 1995 5 19 DL757951858 119950503A5754114N3002120A WEDGE BOEING757 757232 1384965NM NR 6 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 DURING INSPECTION, RT WING NR 6 L/E SLAT WEDGE WAS FOUND DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519003041995051900304NM 1995 5 19 DL757951859 119950430A5754 WEDGE 114N3002119ABOEING757 757232 1384965NM NR 5 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL A10538 25981 49810 DURING INSPECITON, LEFT WING NR 5 L/E SLAT WEDGE WAS FOUND DENTED BEYOND LIMITS. REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950519003051995051900305NM 1995 5 19 DL757951864 119950430A5751 SKIN 113N710057H BOEING757 757232 1384965NM AILERON DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11676DL 372441H 25981 49810 UPON GROUND INSPECTION DFW AFTER HAIL STORM, FOUND HOLES ON UPPER SURFACE OF AILERON. REPAIRED PER SRM 57-60-01. 2L72 4F RTA2NM 19950519003061995051900306NM 1995 5 19 DL757951874 119950430A5754114N4002147A WEDGE BOEING757 757232 1384965NM NR 1 TE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 NUMBER 1 SLAT T/E WEDGE HAS MANY DENTS. REPAIRED PER SRM 57-43-02 FIGURE 202. 2L72 4F RTA2NM 19950519003071995051900307NM 1995 5 19 DL757951877 119950430A5754114N4005178A SKIN BOEING757 757232 1384965NM NR 7 TE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 49810 NR 7 SLAT T/E HAS MANY DENTS. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202. 2L72 4F RTA2NM 19950519003081995051900308NM 1995 5 19 DL757951881 119950503A7110 COWL BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11626DL 22916 726698 FOUND DURING LETTER CHECK INSP, INBD SIDE OF INLET COWL HAS SMALL HOLE. REPAIRED INLET COWL PER SRM 54-11-01. 2L72 4F4 FRTA2NM E17NE 19950519003091995051900309NM 1995 5 19 DL757951893 119950502A5754114N4003153 TE WEDGE BOEING757 757232 1384965NM NR 2 LE SLAT HAIL DAMAGE A DALAK NONE C F.O.D. TXTAXI/GRND HDL 1 SO11620DL 22910 THE BOEING 757 NR 2 LEADING EDGE SLAT RECEIVED CONSIDERABLE HAIL DAMAGE TO THE TRAILING EDGE WEDGE. THE SLAT WAS RECEIVED INTO THE SHOP AND THE WEDGE WAS REPLACED PER SRM 57-43-02 FIG 202. 2L72 4F RTA2NM 19950519003101995051900310NM 1995 5 19 DL757952123 119950511A3230273N20873 VALVE BOEING757 757232 1384965NM LT MLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO11645DL 24216 ON TAKEOFF, EICAS PROBE HEAT ADVISORY DISPLAYED. EICAS STATUS NOSE A/G DISAGREE. UNABLE TO RAISE GEAR. RETURNED DFW. FOUND LEFT TRUCK SHUTTLE VALVE FAULTY. REPLACED VALVE, SWUNG GEAR RETURNED TO SERVICE. 2L72 4F RTA2NM 19950519003111995051900311NM 1995 5 19 DL767951878 119950502A7110314T10101E COWL BOEING767 767232 1385132NM NR 2 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11109DL 22221 49810 DENT IN NOSE LIP SKIN AT 7 O/C POSITION. REPAIRED PER SRM 54-11-01 FOR NR 2 ENGINE INTAKE COWL. 2L72 4F RTA1NM 19950519003121995051900312NM 1995 5 19 DL76L952051 119950510A3310233N322188 CONTROL PANEL BOEING767 767332 1382001NM INSTR PNL LIGHTSFAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11181DN 25986 ON DESCENT HAD A STRONG SMOKE ODOR IN FWD CABIN AND FLT DECK. UTILITY BUSES OFF. SMOKE ODOR DIMINISHED QUICKLY. FOUND SMOKE ODOR COMING FROM FLIGHT DECK INSTRUMENT LIGHT CONTROL PANEL. REPLACED PANEL OPERATION NORMAL. 2L72 4F RTA1NM 19950519003131995051900313 1995 5 19 DL76L952068 419950510A2397 WIRE BOEING767 767332 1382001NM FWD CABIN BURNED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11175DN 24803 DURING L/O CHECK, SMOKE WAS SEEN COMING FROM FORWARD CABIN AREA, GROUND POWER WAS IMMEDIATELY DISCONNCTED, FOUND THREE SHORTED WIRES INSIDE LEFT SEAT ATTACH TRACK AT SEAT LOCATIONS 1C AND 2C. SHORT CAUSED MINOR BURN DAMAGE TO AREA. REPAIRED SHORTED WIRING FOR SEAT FOOT REST MOTOR AND REPLACED ADJACENT DAMAGED CABLE ASSEMBLY. 2L72 4F RTA1NM 19950519003141995051900314NM 1995 5 19 DL76S951782 119950427A5330 SKIN BOEING767 767332 1382001NM FWD FUS LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11130DL 24080 49810 FOUND DURING LETTER CHECK. SEVERAL LIGHTNING STRIKES ABOVE COCKPIT AREA. REPAIRED PER SRM 53-00-01. 2L72 4F RTA1NM 19950519003151995051900315NM 1995 5 19 DL76S951783 119950427A5330 SKIN BOEING767 767332 1382001NM FUSELAGE LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11130DL 24080 49810 FOUND DURING LETTER CHECK, LIGHTNING STRIKE ABOVE L/E OF LEFT WING. REPAIRED PER SRM 53-00-01, DYE CHECKED OK AND PAINTED. 2L72 4F RTA1NM 19950519003161995051900316NM 1995 5 19 DL76S951829 119950430A5755 SKIN 113T5201101 BOEING767 767332 1382001NM NR 2 SPOILER DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 002893 25145 49810 DURING SHOP INSPECTION, NR 2 SPOILER HAD A DENT FROM HAIL DAMAGE AND WAS REPAIRED PER 57-70-01. 2L72 4F RTA1NM 19950519003171995051900317NM 1995 5 19 DL76S951852 119950430A5751 SKIN 113T61008A BOEING767 767332 1382001NM RT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 000362 25145 49810 DURING GROUND INSPECTION DAMAGE FOUND ON UPPER SURFACE OF RT I/B AILERON. REPAIRED PER SRM 57-60-01 REF 51-70-17. 2L72 4F RTA1NM 19950519003181995051900318NM 1995 5 19 DL76S951853 119950430A5751 SKIN 113T710062 BOEING767 767332 1382001NM RT AILERON DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 0737 25145 49810 DAMAGE FOUND DURING GROUND INSPECTION AFTER HAIL STORM IN DFW. DAMAGE WAS FOUND ON UPPER SURFACE O/B RT AILIRON IN VARIOUS AREAS. REPAIR WAS PERFORMED BY SRM 51-70-03 REF SRM 57-60-02. 2L72 4F RTA1NM 19950519003191995051900319NM 1995 5 19 DL76S951854 119950430A5522 SKIN 183T200129 BOEING767 767332 1382001NM LT ELEV DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 000370 25145 49810 DURING GROUND INSPECTION, DAMAGE FOUND TO UPPER SURFACE OF LT I/B ELEVATOR. REPAIRD PER SRM 55-20-01 REF 51-70-17. 2L72 4F RTA1NM 19950519003201995051900320NM 1995 5 19 DL76S951863 119950430A5755 SKIN 015T068346 BOEING767 767332 1382001NM NR 7 SPOILER DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL DL1 25145 49810 UPON GROUND INSP, IN DFW AFTER HAIL STORM UPPER SURFACE WAS FOUND TO BE DENTED ON THE NR 7 SPOILER. REPAIRED PER SRM 51-70-17. 2L72 4F RTA1NM 19950519003211995051900321NM 1995 5 19 DL76S951865 119950430A5755 SKIN 113T510218 BOEING767 767332 1382001NM WING DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 002883 25145 49810 UPON GROUND INSPECTION DFW AFTER HAIL STORM, FOUND HOLES ON UPPER SURFACE OF NR 9 SPOILER. REPAIRED PER SRM 57-70-01 REF 51-17-17. 2L72 4F RTA1NM 19950519003221995051900322NM 1995 5 19 DL76S951866 119950430A5755 SKIN 113T510210SPBOEING767 767332 1382001NM NR 10 SPOILER DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL DL1 25145 49810 UPON GROUND INSPECTION AT DFW AFTER HAIL STORM FOUND A DENT IN NUMBER 10 SPOILER ON THE UPPER SURFACE. REPAIRED PER SRM 57-70-01 REFERENCE TO SRM 51-70-17. 2L72 4F RTA1NM 19950519003231995051900323NM 1995 5 19 DL76S951867 119950501A5754114T410226A SKIN BOEING767 767332 1382001NM NR 11 TE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 25145 49810 NR 11 SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950519003241995051900324NM 1995 5 19 DL76S951872 119950430A5754114T410530A TE WEDGE BOEING767 767332 1382001NM NR 8 LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 49810 RT WING NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED TRAILING EDGE WEDGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950519003251995051900325NM 1995 5 19 DL76S951879 119950430A5754 TE WEDGE 114T410225A BOEING767 767332 1382001NM NR 2 LE FLAP DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 000388 25145 49810 NR 2 L/E SLAT FOUND TO HAVE DENTS APPARENTLY CAUSED BY HAIL. REPLACED TRAILING EDGE WEDGE AS PER CMM 57-43-61. 2L72 4F RTA1NM 19950519003261995051900326NM 1995 5 19 DL76S951882 119950430A5754 TE WEDGE BOEING767 767332 1382001NM NR 5 LE SLAT DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 25145 NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED T/E WEDGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950519003271995051900327NM 1995 5 19 DL76S951884 119950430A5754114T310022A TE WEDGE BOEING767 767332 1382001NM NR 7 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 RT WING NR 7 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950519003281995051900328NM 1995 5 19 DL76S951885 119950430A5754114T410131A WEDGE BOEING767 767332 1382001NM NR 1 SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 25145 DURING INSPECITON NR 1 SLAT WEDGE WAS FOUND DENTED FROM HAIL. REPLACED WEDGE PER SRM 57-43-61. 2L72 4F RTA1NM 19950519003291995051900329NM 1995 5 19 DL76S952117 119950512A21216066223 FAN BOEING767 767332 1382001NM AC DIST FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11129DL 24079 ON DESCENT, FTL DECK AND CABIN CREW REPORTED SMOKE ODOR. THEN LEFT RECIC FAN ADVISORY MESSAGE ILLUMINATED, DEACTIVATED FAN. FAN WAS REPLACED OPERATION NORMAL. 2L72 4F RTA1NM 19950519003301995051900330WP 1995 5 19 DLL10951654 119950407A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 599 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 C-1 BB TEAR STRAP AT FS 599 BETWEEN STGRS 38 AND 39 IS DISBONDED, UNDER AIR DUCT. REPAIRED PER SRM 53-30-00. 2L73 4F A23WE 19950519003311995051900331WP 1995 5 19 DLL10951656 119950407A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 599 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 C-1 BB TEAR STRAP AT FS 599 AND STGRS 27 AND 28 IS DISBONDED UNDER DUCT. REPAIRED PER SRM 53-30-00. 2L73 4F A23WE 19950519003321995051900332WP 1995 5 19 DLL10951657 119950421A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 599 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TEAR STRAP IS DISBONDED ABOVE STR 25 TO 24 AT FS 599. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003331995051900333WP 1995 5 19 DLL10951676 119950407A5330 STRAP LKHEED1011 10113851 5265010WP FS 829 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 FUSELAGE FAIL-SAFE STRAP IS DISBONDED AFT OF FS 829 IN BETWEEN STR 28 TO 27. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003341995051900334WP 1995 5 19 DLL10951677 119950407A5330 STRAP LKHEED1011 10113851 5265010WP FS 829 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 FUSELAGE FAIL-SAFE STRAP IS DISBONDED AFT OF FS 829 IN BETWEEN STR 29 TO 28. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003351995051900335WP 1995 5 19 DLL10951704 119950425A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 519 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 C1 B/B TEAR STRAP DISBONDED AT FS 519 BETWEEN STGRS 26 AND 27. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003361995051900336WP 1995 5 19 DLL10951705 119950407A5330 TEAR STRAP LKHEED1011 10113851 5265010WP STA 519 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TEAR STRAP AT STA 519 AND STGRS 25 AND 26 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003371995051900337WP 1995 5 19 DLL10951706 119950407A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 579 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 C-1 BB TEAR STRAP AT FS 579 BETWEEN STGRS 37 AND 38 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003381995051900338WP 1995 5 19 DLL10951707 119950407A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 699 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 C-1 BB TEAR STRAP AT FS 699 AND STGR 36 IS DISBONDED. REPAIRED PER SRM 53-30-00. FOUND AT HMV. 2L73 4F A23WE 19950519003391995051900339WP 1995 5 19 DLL10951749 119950415A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 000043 LT MLG FITTING TRUNION FITTING HAS CORROSION ON FACE AT FWD ATTACH POINTS. REMOVED CORROSION PER SRM 51-21-02 MAX MATERIAL REMOVED .005 ROTO PEENED PER 51-21-00 CAD PLATE PER PS 900-3-9 PRIMED AND PAINTED. 2L73 4F A23WE 19950519003401995051900340WP 1995 5 19 DLL10951807 119950407A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 901 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 AT HMV, FUS FAIL-SAFE STRAP IS DISBONDED FWD OF FS 901 IN BETWEEN STR 43 TO 44. REPAIRED PER SRM 53-31-00 PG 809. 2L73 4F A23WE 19950519003411995051900341WP 1995 5 19 DLL10951808 119950425A5743 TRUNNION FITTING LKHEED1011 10113851 5265010WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 LEFT GEAR FITTING AFT TRUNNION AFT BORE HAS CORROSION FWD FACE. CORR SPOT FACED .004 DEEP AND LOCALLY BLENDED AREA, REMOVED CORROSION PER SRM 57-14-00. ALL REMAINING REWORK COMPLIED WITH ON RC'S 1453/1454. 2L73 4F A23WE 19950519003421995051900342WP 1995 5 19 DLL10951815 119950430A3211 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 RT MLG FITTING IS CORRODED ON VERTICAL WALL AREA EXPOSED BY REMOVAL OF ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00. 2L73 4F A23WE 19950519003431995051900343WP 1995 5 19 DLL10951816 119950430A3211 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 RT MLG FTG CORRODED UPPER SURFACE OF LWR ATTACHMENT FOR ACTUATOR FTG. FOUND AT HMV, REPAIRED PER SRM 57-14-00. 2L73 4F A23WE 19950519003441995051900344WP 1995 5 19 DLL10951817 119950430A5714 WEB LKHEED1011 10113851 5265010WP FS 1103 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 WEB CORRODED AND PITTED INTERIOR OF CTR WING AT FS 1103, BETWEEN RBL 22 AND RBL 42 WITHIN 4 INCHES OF CTR BOX UPPER SKIN FWD SIDE 4 AREAS OF CORROSION AT FASTENERS. FOUND DURING HMV/CORROSION VISIT. REPAIRED PER SRM 57-11-00 FIG 811. 2L73 4F A23WE 19950519003451995051900345WP 1995 5 19 DLL10951818 119950430A3211 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 LT MLG RETRACT FTG CORRODED ON FACES OF FTG COMMON TO HOLES 17 THROUGH 20 AND HOLES HAVE CORROSION IN THEM. FOUND DURING HMV. REPAIRED PER SRM 57-14-00. 2L73 4F A23WE 19950519003461995051900346WP 1995 5 19 DLL10951819 119950430A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1792 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TEAR STRAP LIFTING AFT WASTE COMPARTMENT FS 1792 AND 1809 FROM STRGR 30 TO 31, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 807. 2L73 4F A23WE 19950519003471995051900347WP 1995 5 19 DLL10951821 119950430A5510 STIFFENER LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341A. FOUND DURING HMV INITIAL. REAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519003481995051900348WP 1995 5 19 DLL10951822 119950409A53201549499103 FITTING LKHEED1011 10113851 5265010WP R 3 DOOR SILL CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 DURING INITIAL INSPECTION FOR OVERHAUL, THE AFT LOWER CORNER FITTING WAS FOUND TO BE CORRODED IN THE R-3 DOORWAY. THE PART WAS REPLACED BY A DELTA MANUFACTURED FITTING NR 1549499-103. 2L73 4F A23WE 19950519003491995051900349WP 1995 5 19 DLL10951828 119950501A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1505 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 STA 1505 FLOORBEAM CORRODED LBL 4 ON T-CAP. FOUND AT HMV. REPAIRED PER SRM 53-23-00 FIG 801. 2L73 4F A23WE 19950519003501995051900350WP 1995 5 19 DLL10951830 119950501A3211 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 RT MLG FITTING CORRODED AT RETRACT ACTUATOR ATTACHMENT HOLES 1 TO 6. FOUND AT HVM, REPAIRED PER SRM 57-14-00. 2L73 4F A23WE 19950519003511995051900351WP 1995 5 19 DLL10951831 119950501A3211 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 RT MLG FITTING CORRODED AT RETRACT ACTUATOR FTG HOLE 17. FOUND DURING HMV/CORROSION CK. REPAIRED PER SRM 57-14-00. 2L73 4F A23WE 19950519003521995051900352WP 1995 5 19 DLL10951833 119950501A5311 FRAMES LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 49810 THE FOLLOWING FRAMES WERE FOUND CRACKED AT WL 280.6 ON THE RT SIDE, 649, 669, 1043, 1103, 1123, 1665, 1685, 1705. THE LT SIDE, 509, 529, 1023, 1043, 1123, 1303, 1323, 1343, 1403, 1605, 1665. CRACKS WERE FOUND DURING SPECIAL INSPECTION, AND REPAIRED PER DL ERA 270790-14. 2L73 4F A23WE 19950519003531995051900353WP 1995 5 19 DLL10951834 119950421A5312 BULKHEAD LKHEED1011 10113851 5265010WP LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 LT MLG WHEEL WELL AFT BULKHEAD HAS 5 CRACK BETWEEN STIFFENERS (LWR MID AREA). 2L73 4F A23WE 19950519003541995051900354WP 1995 5 19 DLL10951835 119950425A5400 SPLICE LKHEED1011 10113851 5265010WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 BLKD SPLICE TEE CRACKED LT FS 1705 WL 405 VIEWED THROUGH PANEL 313A-1 AND 311UL. 2L73 4F A23WE 19950519003551995051900355WP 1995 5 19 DLL10951862 119950406A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1423-1443 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TEAR STRAP BETWEEN STA 1423 AND 1443 AT STR NR 27 IS DISBONDED AT BOTH SIDES OF STRINGER C-2 B/B. REMOVED CORROSION, WITHIN LIMITS PER SRM 53-31-00-801, TREATED/PAINTED. REPAIRED TEAR STRAP PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950519003561995051900356WP 1995 5 19 DLL10951897 119950406A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1373 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 TEAR STRAP DISBONDED STA 1373 ABOVE AND BELOW STR 40. REMOVED FASTENERS, CUT TEAR STRAP AND CLEANED CORROSION PER SRM 51-21-01, WITHIN LIMITS PER SRM 53-31-00. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950519003571995051900357WP 1995 5 19 DLL10951898 119950416A5510 STIFFENER LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 INTERNAL STIFFENERS, CRACKED LT HORIZ L/E PNL 331B. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519003581995051900358WP 1995 5 19 DLL10951899 119950416A5510 STIFFENER LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 INTERNAL STIFFENERS, CRACKED RT HORIZ L/E PNL 341B. REPAIRED STIFFENERS PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519003591995051900359WP 1995 5 19 DLL10951900 119950408A5330 SKIN LKHEED1011 10113851 5265010WP FS 479 BULGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 EXTERIOR SKIN, BULGED AND A RIVET IS SHEARED AT STA 479 BETWEEN STR 39 TO 40, JUST BELOW PURGE LINES. REMOVED FIX FLR PURGE LINES AND LWR ANGLE. OPENED/REMOVED CORROSION ON INNER SKIN PER SRM 900-2-4-1. CUT OUT GOUGE AND DYE CKD AREA FOR EXTERNAL REPAIR, NO CRACKS FOUND PER ERA 270810-14, TREAT/PAINTED AREA. 2L73 4F A23WE 19950519003601995051900360WP 1995 5 19 DLL10952114 119950513A2782720002C ACTUATOR LKHEED1011 10113851 5265010WP NR 4 SLAT FAILED A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO11722DA 193C1147 ON APPROACH, LEFT 3 OUTBOARD L/E SLATS WERE STUCK IN THE UP POSITION WHEN FLAPS WERE SELECTED TO 4 DEGREES. REPLACED NR 4 SLAT ACTUATOR, OPERATION NORMAL. 2L73 4F A23WE 19950519003611995051900361WP 1995 5 19 DLL10952124 119950513A33505165741 EEL PWR SUPPLY LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST APAPPROACH 1 SO11712DA 193C1088 ON FINAL APPROACH, EMERGENCY LIGHTS CAME ON, WILL NOT RESET. FOUND FLIGHT COMPARTMENT EMERGENCY LIGHT POWER PACK (L1) STUCK IN ON POSITION. REPLACED PACK OPERATION NORMAL. 2L73 4F A23WE 19950519003621995051900362WP 1995 5 19 DLL13952067 119950506A2121165001 FAN LKHEED1011 10113851 5265010WP GALLEY FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11785DL 193A1121 DURING DESCENT, HAD STRONG ELECTRICAL BURNING ODOR MID CABIN AND LOWER GALLEY AREA. FOUND GALLEY EXHAUST FAN C/B C-11 TRIPPED WILL NOT RESET. REPLACED GALLEY EXHAUST FAN, OPERATION NORMAL. 2L73 4F A23WE 19950519003631995051900363WP 1995 5 19 DLL17951737 119950410A57111605415 REAR SPAR LKHEED1011 10113853 5265020WP RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 49810 DURING ACCOMPLISHMENT OF EO 7-59089-3, CRACKS WERE FOUND EMANATING FROM FOUR EXISTING FASTENER HOLES IN THE UPPER CAP, THE SPAR WEB, AND THE RIGHT WING UPPER SKIN. REPAIRS WERE ACCOMPLISHED PER DL ERA 270612-14AD. 2L73 4F A23WE 19950519003641995051900364NM 1995 5 19 DLM88951761 119950427A5320 DOOR FRAME DOUG MD88 MD88 3023688NM LT MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11934DL 49721 49810 MLG FWD DOOR FRAME CRACKED 3.5 INCHES AT O/B RADIUS. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950519003651995051900365NM 1995 5 19 DLM88951763 119950427A5230 DOOR FRAME DOUG MD88 MD88 3023688NM CARGO DOOR WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11934DL 49721 49810 C-1 DOOR PAN AND UNDERLYING INTERCOSTAL WORN FWD SIDE. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 52-05 FIG 27. 2L72 4F RTA6WE 19950519003661995051900366NM 1995 5 19 DLM88951784 119950428A5230 DOOR FRAME DOUG MD88 MD88 3023688NM NR 1 CARGO DOOR GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11913DE 49956 49810 C-1 CARGO DOOR AFT PAN GOUGED AND WORN THROUGH FIRST LAYER OF PAN. FOUND AT B-2 LTR CK. REPAIRED PER SRM 52-05 FIG 27. 2L72 4F RTA6WE 19950519003671995051900367NM 1995 5 19 DLM88951832 119950501A5320 CROSS OVER RIB DOUG MD88 MD88 3023688NM LWR FUS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11902DE 53379 49810 FOUND DURING C-2 LETTER CHECK, CROSS OVER RIB BETWEEN MLG WHEEL WELL DOORS AFT SIDE CRACKED ON LT SIDE OF RIB AND RT SIDE 1 INCH EACH. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950519003681995051900368NM 1995 5 19 DLM88951847 119950429A5523 SKIN DOUG MD88 MD88 3023688NM LT ELEV TAB DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11918DE 49959 49810 FOUND AFTER HAIL STORM, LT ELEV MIDDLE TRIM TAB HAS HAIL DAMAGE S/N 891LRH MADE BONDED REPAIR PER MD 88 SRM 55-04, BAL WEIGHT 5.38 LBS 5-1-95. 2L72 4F RTA6WE 19950519003691995051900369NM 1995 5 19 DLM88951848 119950429A5523 SKIN DOUG MD88 MD88 3023688NM RT ELEV TAB DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11918DE 49959 49810 FOUND HAIL DAMAGE, RT ELEV MIDDLE TAB HAS HAIL DAMAGE. MADE BONDED REPAIRS PER MD 88 SRM 55-04 WEIGHT 5.48 LBS 5-1-95. 2L72 4F RTA6WE 19950519003701995051900370NM 1995 5 19 DLM88951850 119950502A5320 DOOR FRAME DOUG MD88 MD88 3023688NM C-1 CARGO COMP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11980DL 53267 49810 FOUND DURING D-2 LETTER CHEC, CORROSION AT C-1 DOOR FRAME LOWER RADIUS. REPAIRED PER SRM 53-05 FIG 63. 2L72 4F RTA6WE 19950519003711995051900371NM 1995 5 19 DLM88951851 119950502A5330 SKIN DOUG MD88 MD88 3023688NM FWD FUS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11980DL 53267 49810 FOUND DURING D-2 LETTER CHECK, .125 INCH CRACK AT LT NLG DOOR HING CUTOUT IN FUSELAGE SKIN. REPAIRED PER SRM 53-05 FIG 2A. 2L72 4F RTA6WE 19950519003721995051900372NM 1995 5 19 DLM88951868 119950503A5230 PAN DOUG MD88 MD88 3023688NM C 1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11905DL 49536 49810 C-1 DOOR AFT PAN CRACKED 1 INCH, FOUND AT C-2 LTR CK. REPAIRED PER SRM 52-05 FIG 26A. 2L72 4F RTA6WE 19950519003731995051900373NM 1995 5 19 DLM88951869 119950503A5330 SKIN DOUG MD88 MD88 3023688NM LT NLG DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11905DL 49536 49810 FUSELAGE SKIN CRACKED LT NLG DOOR AFT HINGE CUTOUT. FOUND DURING C-2 LTR CK TPAMM. REPAIRED PER SRM 53-05 FIG 62. 2L72 4F RTA6WE 19950519003741995051900374NM 1995 5 19 DLM88951875 119950503A5320 ANGLE DOUG MD88 MD88 3023688NM RT WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11905DL 49536 49810 MLG W/W AFT O/B STRIKER ANGLE CRACKED. FOUND AT C-2 LTR CK. REPAIRED PER SRM 53-05 FIG 81A.5. 2L72 4F RTA6WE 19950519003751995051900375NM 1995 5 19 DLM88951886 119950504A5330 SKIN DOUG MD88 MD88 3023688NM NLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11964DL 49983 FOUND DURING E-2 LETTER CHECK, SKIN CRACKED AT NLG DOOR FWD HINGE CUTOUT RT SIDE. REPAIRED PER SRM 53-05 FIG 62. 2L72 4F RTA6WE 19950519003761995051900376NM 1995 5 19 DLM88952065 119950510A323139567851 LINK DOUG MD88 MD88 3023688NM RT NLG DOOR BROKEN A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11983DL 53247 ON CLIMBOUT, HAD LOUD NOISE AND VIBRATION FROM NOSE GEAR AREA. RETURNED TO DFW. FOUND RT NOSE GEAR DOOR OPEN. REPLACED THE RT NOSE GEAR DOOR FORWARD LINK, OPERATION NORMAL. 2L72 4F RTA6WE 19950519003771995051900377WP 1995 5 19 MWEA95204 119950515A335060030431 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN FAILED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31302ME 47102 CREW REPORTS, TWO PANEL LIGHTS IN COCKPIT AND GALLEY EMERGENCY LIGHTS COME ON, THEN DIM QUICKLY. MAINTENANCE REMOVED AND REPLACED NR 1 OVERHEAD BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950519003781995051900378WP 1995 5 19 UPS 803238 119950515A532046401621 FITTING DOUG DC8 DC871F 302199DWP FS 1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON UPPER CUSP FITTING, LONGERON 21L, FS 1560. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003791995051900379WP 1995 5 19 UPS 803239 119950515A532051415997 SPLICE DOUG DC8 DC871F 302199DWP FS 420-440 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK AND CORROSION ON LONGERON 36 SPLICE FITTING, FS 420 TO 440. REPLACED FITTNG PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003801995051900380WP 1995 5 19 UPS 803240 119950515A53204647657 FITTING DOUG DC8 DC871F 302199DWP FS 100 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON END FITTING, LONGERON 36, FS 100. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003811995051900381WP 1995 5 19 UPS 803241 119950515A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 70-100 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R, FS 70 TO 100. INSTALLED REPAIRED PER UPS EO DC8-5310-6898A. 2L74 4F RT4A25 19950519003821995051900382WP 1995 5 19 UPS 803242 119950515A5730 SKIN DOUG DC8 DC871F 302199DWP WS 426.76 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E LWR SKIN AND DOUBLER, XFS 426.76. INSTALLED REPAIR PER UPS EO FILE NR DC8-57-0547. 2L74 4F RT4A25 19950519003831995051900383WP 1995 5 19 UPS 803243 119950515A5311561237618 FRAME DOUG DC8 DC871F 302199DWP FS 52 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON FUSE FRAME AT FS 52 RT SIDE, 6 INCHES ABOVE FLIGHT DECK SUB FLOOR, APPROX 1 INCH LONG. INSTALLED REPAIR PER UPS EO FILE DC8-5310-6967A. 2L74 4F RT4A25 19950519003841995051900384WP 1995 5 19 UPS 803244 119950515A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 53-32 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FLIGHT DECK PRESSURE DOUBLER, LT SIDE, JOINING WITH FUSELAGE, FS -53 TO FS -32. REPLACED DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19950519003851995051900385WP 1995 5 19 UPS 803245 119950515A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1740-1766 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN, FS 1766, LONGERON 34L AND FS 1740 TO 1766, LONGERON 28L TO 30L. REPLACED BELLY SKIN PER DOUGLAS DRAWING 5649329. 2L74 4F RT4A25 19950519003861995051900386WP 1995 5 19 UPS 803246 119950515A532047585721 FITTING DOUG DC8 DC871F 302199DWP FS 1535-1542 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON FITTING LONGERON 33, AT FS 1535 TO 1542. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003871995051900387WP 1995 5 19 UPS 803247 119950515A5313259396N LONGERON DOUG DC8 DC871F 302199DWP FS 1650 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R, FS 1650. INSTALLED REPAIR PER UPS EO DC8-5310-6977A. 2L74 4F RT4A25 19950519003881995051900388WP 1995 5 19 UPS 803248 119950515A53305615374187 SKIN DOUG DC8 DC871F 302199DWP FS 1490-1690 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BELLY SKIN FS 1490 TO 1690, LONGERON 31L TO 31R. REPLACED BELLY SKIN PER DOUGLAS DRAWING 5615374. 2L74 4F RT4A25 19950519003891995051900389WP 1995 5 19 UPS 803249 119950515A53139754007 LONGERON DOUG DC8 DC871F 302199DWP FS 280-360 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L-A, FS 280 TO 360, AND END FITTING, FS 360. 2L74 4F RT4A25 19950519003901995051900390WP 1995 5 19 UPS 803250 119950515A532037552171 SPLICE DOUG DC8 DC871F 302199DWP FS 1350 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE, FS 1350, LONGERON 31L. REPLACED SPLICE PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003911995051900391WP 1995 5 19 UPS 803251 119950515A532052615551 SHEAR TIE DOUG DC8 DC871F 302199DWP FS 1060 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE FWD AND AFT SIDES, LONGERONS 36 TO 35L, FS 1060. INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F RT4A25 19950519003921995051900392WP 1995 5 19 UPS 803252 119950515A5347 CARGO TRACK DOUG DC8 DC871F 302199DWP FS 980-1070 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON CARGO TRACK AROUND FASTENER HOLES, FS 980 TO 1070, LT. INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950519003931995051900393WP 1995 5 19 UPS 803253 119950515A5347 CARGO TRACK DOUG DC8 DC871F 302199DWP FS 1310-1410 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON CARGO TRACK AROUND FASTENER HOLES, FS 1310 TO 1410, LT. INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F RT4A25 19950519003941995051900394WP 1995 5 19 UPS 803254 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1179 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON AT FITTING, FS 1179, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0. 2L74 4F RT4A25 19950519003951995051900395WP 1995 5 19 UPS 803255 119950515A5320 CASTING DOUG DC8 DC871F 302199DWP FS 290 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON T-HOOK CASTING FS 290, LONGERON 33A. INSTALLED REPAIR PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003961995051900396WP 1995 5 19 UPS 803256 119950515A5320 CASTING DOUG DC8 DC871F 302199DWP FS 320 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON T-HOOK CASTING FS 320, LONGERON 33A. INSTALLED REPAIR PER SRM 51-1-20D. 2L74 4F RT4A25 19950519003971995051900397WP 1995 5 19 UPS 803257 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 290 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING, FS 290, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 19950519003981995051900398WP 1995 5 19 UPS 803258 119950515A5320 FITTING DOUG DC8 DC871F 302199DWP FS 299 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING, FS 299, LONGERON 33R. REPLACED FITTING PER SRM 53-2-0, 51-1-20D. 2L74 4F RT4A25 19950519003991995051900399WP 1995 5 19 UPS 803259 119950515A5311 FRAME DOUG DC8 DC871F 302199DWP FS 100 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME, FS 100, BETWEEN LONGERONS 36R AND 34R. INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F RT4A25 19950519004001995051900400WP 1995 5 19 UPS 803260 119950515A5320 ANGLE DOUG DC8 DC871F 302199DWP FS 1540 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CRACK ON ATTACH ANGLE FS 1540, LONGERON 33R. REPLACED ANGLE PER SRM 51-1-21D. 2L74 4F RT4A25 19950519004011995051900401WP 1995 5 19 UPS 803261 119950515A53203755217 SPLICE DOUG DC8 DC871F 302199DWP FS 1270 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE IN S2 CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE, FS 1270, LONG 34L, ON BOTTOM SIDE. REPLACED SPLICE PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004021995051900402WP 1995 5 19 UPS803217 119950516A532036169472 FITTING DOUG DC8 DC873F 302199FWP FS 717 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME FITTING, LONGERON 21L, FS 717. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004031995051900403WP 1995 5 19 UPS803218 119950516A5320461397 FITTING DOUG DC8 DC873F 302199FWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R END FITTING, FS 70. REPLACED FITTING PER SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 19950519004041995051900404WP 1995 5 19 UPS803219 119950516A53204613972 FITTING DOUG DC8 DC873F 302199FWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 31R, FS 70. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004051995051900405WP 1995 5 19 UPS803220 119950516A53203649551 FITTING DOUG DC8 DC873F 302199FWP FS 70-80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 36, FS 70 TO 80. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004061995051900406WP 1995 5 19 UPS803221 119950516A53204611067N FITTING DOUG DC8 DC873F 302199FWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING, LONGERON 24R, FS 70. REPLACED FITTING PER SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 19950519004071995051900407WP 1995 5 19 UPS803222 119950516A5313261034020000 LONGERON DOUG DC8 DC873F 302199FWP FS 1085 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 28L, FS 1085. INSTALLED REPAIR PER SRM 53-2-2. 2L74 4F RT4A25 19950519004081995051900408WP 1995 5 19 UPS803223 119950516A532037584952 FITTING DOUG DC8 DC873F 302199FWP FS 1270-1280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FRAME FITTING, FS 1270 TO 1280, LONGERON 33R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004091995051900409WP 1995 5 19 UPS803224 119950516A532046110671 FITTING DOUG DC8 DC873F 302199FWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34R END FITTING, FS 70. REPLACED FITTNG PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004101995051900410WP 1995 5 19 UPS803225 119950516A53205759540 SPLICE DOUG DC8 DC873F 302199FWP FS 1080 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AFT BB LT TUNNEL ON BELT FRAME SPLICE, BS 1080 LONGERON 24L. REPLACED SPLICE PER SRM 51-1-20D. 2L74 4F RT4A25 19950519004111995051900411WP 1995 5 19 UPS803226 119950516A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS 80-70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON DOUBLER JOINING FLOOR TO FUSELAGE, FS -80 TO -70 LT. REPLACED DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19950519004121995051900412WP 1995 5 19 UPS803227 119950516A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS -86 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM SIDE OF DOUBLER, AT RT SIDE OF FLIGHT DECK SUB FLOOR, FS -86. REPLACED DOUBLER PER SRM 53-01-0, 51-1-20D. 2L74 4F RT4A25 19950519004131995051900413WP 1995 5 19 UPS803228 119950516A5530 SPLICE DOUG DC8 DC873F 302199FWP VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND DELAMINATION ON LWR VERTICAL STAB L/E BOTTOM SPLICES. REPLACED SPLICE STRAPS (2EA) PER SRM 51-1-9. 2L74 4F RT4A25 19950519004141995051900414WP 1995 5 19 UPS803263 119950513A3260 BULB DOUG DC8 DC871F 302199DWP GEAR INDICATION FAILED A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01709UP 45914 PILOT REPORTED, GEAR DOWN LT LANDING GEAR LIGHT NOT ILLUMINATED. CHANGED BULBS AND RECYCLED GEAR. COMMENT NOTED BY MAINTENANCE INPECTED AND CHECKED SWITCH, PLUG, AND SOCKET, OK. NO OTHER DEFECTS NOTED AT THIS TIME. 2L74 4F RT4A25 19950519004151995051900415WP 1995 5 19 UPS803264 119950513A3210 LANDING GEAR DOUG DC8 DC871F 302199DWP RT MLG FAILED A IPXAO OTHER O OTHER LDLANDING 1 SO01707UP 45907 (SUPPLEMENTAL MRR) PILOT REPORTED RT MAIN LANDING GEAR COLLAPSED ON LANDING ROLL AT SDF. REPLACED RT MAIN GEAR. OPS CK GOOD PER T/C 2535. 2L74 4F RT4A25 19950519004161995051900416NM 1995 5 19 95ZZZW691 119950212A5510 BOLT BOEING737 7372T4 1384492NM LT HORIZ STAB GALLED A SPAAK NONE O OTHER ININSP/MAINT 1 WP07703S 22529 DURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, THE LEFT HORIZONTAL STABILIZER AFT, LOWER BOLT WAS EXTREMELY DIFFICULT TO LOOSEN/REMOVE. ONCE REMOVED, THE BOLT AND BUSHINGS WERE FOUND GALLED. EVIDENCE OF CORROSION AROUND BUSHING TO FITTING LUG MATING SURFACES. THE BUSHINGS WERE REPLACED PER BOEING SB 737-55-1033 AND 737-55-1055. THE BOLT WAS REPLACED WITH A NEW UNIT. (W) 2L72 4F A16WE 19950519004171995051900417NM 1995 5 19 95ZZZW692 119950212A5510 BOLT BOEING737 7372T4 1384492NM RT HORIZ STAB GALLED A SPAAK NONE O OTHER ININSP/MAINT 1 WP07703S 22529 DURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, THE RT HORIZONTAL STABILIZER AFT, LOWER BOLT WAS EXTREMELY DIFFICULT TO LOOSEN/REMOVE. ONCE REMOVED, THE BOLT AND BUSHINGS WERE FOUND GALLED. EVIDENCE OF CORROSION AROUND BUSHING TO FITTING LUG MATING SURFACES. THE BUSHINGS WERE REPLACED PER BOEING SB 737-55-1033 AND 737-55-1055. THE BOLT WAS REPLACED WITH A NEW UNIT. (W) 2L72 4F A16WE 19950519004181995051900418NM 1995 5 19 95ZZZW693 119950214A5510 LUGS BOEING737 7372T4 1384492NM LT HORIZ STAB CORRODED A SPAAK NONE O OTHER ININSP/MAINT 1 WP07703S 22529 DURING COMPLIANCE WITH AD 90-25-01, CPCP TASK C53-701-02, CORROSION FOUND AT THE LEFT HORIZONTAL STABILIZER AFT, UPPER CENTER SECTION LUG AROUND THE BUSHINGS. THE BUSHINGS WERE REPLACED PER BOEING SB 737-55-1033 AND 737-55-1055. 2L72 4F A16WE 19950519004191995051900419NM 1995 5 19 AWXA9500261 119950504A3350 EEL BOEING737 7373S3 1384711NM CABIN DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS DAMAGED AND INTERMITTENT. REPAIRED WIRING, AND REMOVED AND REPLACED LIGHT TRACK AND ASSY, OPS CHECK GOOD. 2L72 4F RTA16WE 19950519004201995051900420NM 1995 5 19 AWXA9500276 119950509A5315 FLOOR BEAM BOEING737 7373G7 1384595NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX- DURING C11 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED, BS 986.5 RBL 40. REPAIRED WITH ANGLE REPAIR PER SRM 53-00-51. (W) 2L72 4F RTA16WE 19950519004211995051900421WP 1995 5 19 DALR950002 119950417A53431506932101 FITTING LKHEED1011 10113851 5265010WP FS 449L CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR, THE NLG SHOCK STRUT SUPPORT FITTING ON THE RBL 22 BULKHEAD WAS FOUND CRACKED NEAR FS 449. CRACKS WERE REPAIRED PER DER APPROVED DATA, EL ERA 270628-14. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004221995051900422WP 1995 5 19 DALR950003 119950403A57111503230101 SPAR CAP LKHEED1011 10113851 5265010WP FS 1103 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETER CHECK AT DALR. THE WING CENTER SECTION INTERMEDIATE SPAR UPPER CAP AT FS 1103 WAS FOUND CRACKED AT THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLISHED PER DL ERA 270579-14. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004231995051900423WP 1995 5 19 DALR950004 119950403A57111503229101 SPAR CAP LKHEED1011 10113851 5265010WP FS 1043 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR, WING CENTER SECTION FS 1043 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE LEFT SIDE OUTBOARD END. THE CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPLIHSED PER DL ERA 270578-14. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004241995051900424WP 1995 5 19 DALR950005 119950403A57111503231101 SPAR CAP LKHEED1011 10113851 5265010WP FS 1163 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP WAS FOUND WITH A CRACK IN ITS LEFT SIDE OUTBOARD END. THIS CRACK IS TYPICAL AS DESCRIBED PER LAC SB 093-57-087. REPAIRS WERE ACCOMPISHED PER DL ERA 270580-14. TT, 38155 HRS. CYLES, 18905. (X) 2L73 4F A23WE 19950519004251995051900425WP 1995 5 19 DALR950006 119950406A5720 FITTING LKHEED1011 10113851 5265010WP RIGHT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVESIZED TO CLEAN UP CORROSION PER DL ERA 270605-14. TT 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004261995051900426WP 1995 5 19 DALR950007 119950327A5743 FITTING LKHEED1011 10113851 5265010WP LT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA38155 193A1012 ATL - DURING LETTER CHECK AT DALR, THE LEFT HAND MAIN LANDING GEAR UPPER ACTUATOR ATTACH FITTING LUGS WERE FOUND CORRODED ON THE INSIDE DIAMETER. THE LUG HOLES WERE BORED OUT TO CLEAN UP CORROSION PER DL ERA 270493-14. (W) 2L73 4F A23WE 19950519004271995051900427WP 1995 5 19 DALR950008 119950331A5330 SKIN LKHEED1011 10113851 5265010WP FS 983 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK A DALR. THE FUSELAGE SKIN WAS FOUND CRACKED AT THE LOWER RIGHT SIDE OF THE FS 983 PRESSURE BULKHEAD UNDER THE FUSELAGE-TO-WING BOX LONGERON. THE SKIN WAS FOUND WITH A 1.5 INCH LONG CRACK IN THE SECOND FASTENER ROW FORWARD OF THE BULKHEAD. THE ATTACHED FUSELAGE-TO-WING BOX LONGERON WAS ALSO FOUND CRACKED. REPAIRS WERE ACCOMPLISHED PER DL ERA 270485-14 FOR THE LONGERON AND DL ERA 270563-14 FOR THE FUSELAGE SKIN. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004281995051900428WP 1995 5 19 DALR950009 119950330A53131503579103 LONGERON LKHEED1011 10113851 5265010WP FS 339 CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR. CONSIDERABLE CORROSION WAS FOUND AT FS 328 ON THE VERTICAL FLANGE OF THE LBL 22 NLG WHEELWELL SIDEWALL LOWER LONGERON. A NEW SECTION OF LONGERON WAS SPLICED IN PER DL ERA 270527-14. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950519004291995051900429NM 1995 5 19 IXKA9500017 119950428A2420 WIRE BOEING727 727251 138408HNM NR 1 GENERATOR BROKEN A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25264US 19983 MCO - FLT NR 74, AFTER TAKEOFF, NR 1 GEN UNDEREXCITED, ISOLATED GEN LEFT FWD BOOST PUMP CIRCUIT BREAKER POP IN NR 2 TANK, RESET, FORWARD RT BOOST PUMP CIRCUIT BREAKER POPPED, LEFT NR 2 CIRCUIT BREAKER POPPED AGAIN, NR 1 CIRCUIT BREAKER LEFT TANK BOOST PUMP POPPED. AIRCRAFT RETURNED TO MCO. FOUND T1 WIRE BROKEN AT NR 1 GEN, REPAIRED T1 WIRE PER 24-50, OPS CHECK OK. (W) 2L73 4F A3WE 19950519004301995051900430NM 1995 5 19 MZZA95031 119950422A521065C1990119 LATCH CABLE BOEING727 727227 1384078NM R2 ENTRY DOOR BROKEN A MZZAK NONE O OTHER ININSP/MAINT 1 WP1389427 21365 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON R2 ENTRY DOOR ESCAPE SLIDE LATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727-MM 25-60-15. HANGAR NON ROUTINE REPAIR ITEM CARD NR 0757626. (W) 2L73 4F A3WE 19950519004311995051900431NM 1995 5 19 MZZA9528 119950427A4900380678111 APU BOEING727 727224 1384076NM CABIN FAILED A MZZAB EMER. DESCENT O OTHER ININSP/MAINT 1 WP1369741 22250 FLT NR 93827 - CTS - DURING BOARDING, MAIN CABIN FILLED WITH SMOKE, OFF LOADED PASSENGERS. TRACED SMOKE TO FAILED APU. PLACARDED APU INOPERATIVE PER MEL 49-01. RAN ENGINES AND CLEARED CABIN AND PACKS OF RESIDUE. (W) 2L73 4F A3WE 19950519004321995051900432EU 1995 5 19 RAIA950433 119950421A33500L60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST TXTAXI/GRND HDL 1 CE032FOR 11653 176 TWO EMERGENCY LIGHTS INOP. REPLACED BULBS. (W) 2H72 4T RTA53EU 19950519004331995051900433EU 1995 5 19 RAIA950434 119950424A7722CA3108R12S3SF80 CONNECTOR BAG JETSTMJETSTM3201 1500217EU NR 2 ENG FAILED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03431AM8964 881 STL - 7332 - RIGHT SRL WOULD NOT COME ON LINE. REPLACED T2 SENSOR CANNON PLUG. (W) 2L72 4T RTA56EU 19950519004341995051900434 1995 5 19 RAIA950435 319950423A6112 BLADE DE-ICE AEROSPATR42 ATR42300 8680920EU NR 1 PROP INOP A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03423TE13181 5231 119 STL - FLT 7110 - LEFT PROP DE-ICE HEAT INOP. REPLACED PROP BLADE. (W) 2H72 4T RTA53EU 19950519004351995051900435 1995 5 19 RAIA950436 319950424A6112660716235 PROP DE-ICE BAG JETSTMJETSTM3201 1500217EU NR 2 INOP A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03433AM6055 79 885 STL - 7454 - NR 2 PROP DE-ICE INOP. REPLACED PROP ASSY. (W) 2L72 4T RTA56EU 19950519004361995051900436EU 1995 5 19 RAIA950437 119950424A32307445B RELEASE VALVE BAG JETSTMJETSTM3201 1500217EU CENTER SECT MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03343TE5677 955 STL - FLT NR 7316 - WHEN GEAR SELECTED UP, INTRANSIT LIGHT WOULD NOT EXTINGUISH. RESET HYDRAULIC BYPASS VALVE. (W) 2L72 4T RTA56EU 19950519004371995051900437WP 1995 5 19 RAIA950438 219950425A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 1 MALFUNCTIONED A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03866AE7705 1716 866 66076 PSP - FLT 4773 - NR 1 ENGINE WOULD ONLY PRODUCE 93 PERCENT TORQUE. REPLACED NR 1 ENGINE. (W) 2L72 4T4 TRTA56EU E4WE 19950519004381995051900438EU 1995 5 19 RAIA950439 119950427A521091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03342TE5980 954 DEC - FLT NR 7301 - PASSENGER DOOR WARNING LIGHT ILLUMINATED. ADJUSTED HANDLE MICROSWITCH. (W) 2L72 4T RTA56EU 19950519004391995051900439EU 1995 5 19 RAIA950440 119950426A3150350A23008314 CCAS COMPUTER AEROSPATR42 ATR42300 8680920EU AVIONICS RACK NORMAL A RAIAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03426TE106837046 228 STL - FLT 7174 - IN FLIGHT PROP BRAKE AND CABIN ALTITUDE CCAS WARNING OCCURRED. RERACKED CCAS COMPUTER AND PERFORMED GROUND RUNS SYSTEM NORMAL. (W) 2H72 4T RTA53EU 19950519004401995051900440 1995 5 19 RAIA950441 319950429A6112SFM13M10A BLADE AEROSPATR42 ATR42300 8680920EU RT PROP BOOT LOOSE A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03426TE138817337 228 STL - FLT 7176 - AFTER TAKEOFF HAD VIBRATION ON AIRCRAFT. RT PROPELLER BLADE DE-ICE BOOT CAME LOOSE. MAINTENANCE REPLACED RT PROPELLER BLADE. GROUND CHECK REVEALED NO VIBRATION. (W) 2H72 4T RTA53EU 19950519004411995051900441EU 1995 5 19 RAIA950442 119950428A77228974696 CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENG MOISTURE A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03431AM8985 881 STL - FLT 7316 - LEFT EGT FLUX WITH SRL ON OR OFF. MAINTENANCE CLEANED LEFT EGT HARNESS CANNON PLUG. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950519004421995051900442EU 1995 5 19 RAIA950443 119950429A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03971JX3916 971 FAT - EMERGENCY LIGHT IS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY. (W) 2L72 4T RTA56EU 19950519004431995051900443SO 1995 5 19 RAIA950444 119950429A3260922FS2A6N2735 WOW SWITCH EMB 120 EMB120RT SO LT MLG FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03124AM17564 120016 STL - RT PACK FILLED SMOKE IN CABIN. MAINTENANCE REPLACED LEFT WEIGHT ON WHEEL SWITCH. RT PACK OPERATIONAL CHECK GOOD NO SMOKE NOTED. (W) 2L72 4T RTA31SO 19950519004441995051900444EU 1995 5 19 RAIA950445 119950429A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03341TE6113 950 STL - TWO EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (W) 2L72 4T RTA56EU 19950519004451995051900445SO 1995 5 19 RAIA950446 119950429A2121EVAC2322C2 FAN EMB 120 EMB120RT SO RT PACK FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03125AM4716 120017 STL - RT PACK SMELLS LIKE IT IS GETTING HOT ON GROUND. MAINTENANCE REPLACED RT GROUND COOLING FAN. GROUND TEST CHECK NORMAL. NO SMELL NOTED. (W) 2L72 4T RTA31SO 19950519004461995051900446SO 1995 5 19 RAIA950501 119950502A27503075001007 CONTROL UNIT EMB 120 EMB120RT SO TE FLAP SYS FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03130AM14637 120134 STL - FLT 7213 - NACELLE FLAP FAULT IN FLIGHT. MAINTENANCE REPLACED FLAP CONTROL UNIT. SYSTEM CHECK GOOD. (W) 2L72 4T RTA31SO 19950519004471995051900447EU 1995 5 19 UF6A950413 119950421A27313094318B SWITCH BAG ATP ATP EU ELEV TRIM FAILED A UF6AK NONE O OTHER CRCRUISE 1 CE03852AW8624 2021 FLT 5970 - SBN - THE ELECTRIC ELEVATOR TRIM SWITCH STUCK IN FLIGHT. MAINTENANCE REPLACED THE ELECTRIC TRIM SWTICH ON THE NR TWO SIDE. (W) 2L72 4T RTA27NM 19950519004481995051900448 1995 5 19 UF6A950414 419950430A34254608001210 AHRU BAG ATP ATP EU NR 1 FAILED A UF6AO OTHER J WARNING INDICATION CRCRUISE 1 CE03851AW7366 0915 2020 AZO - FLT 5003 - THE NR ONE PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY FAILED. MAINTENANCE REPLACED THE NR ONE ATTITUDE HEADING REFERENCE UNIT. (W) 2L72 4T RTA27NM 19950519004491995051900449NE 1995 5 19 WRLA95018 219950424A73209053M30G02 SENSE LINE DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 1 ENGINE BLOCKED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27107WA 46836 DURING TAXI OUT, FLIGHT CREW NOTICED NR 1 N1 AT 16 PERCENT, NR 1 EGT AT 480 DEGREES, NR 1 N2 AT 48 PERCENT, AND FUEL FLOW WAS AT 1,000 LBS. THROTTLE MOVEMENT HAD NO EFFECT. CAPTAIN ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BLOCKAGE IN CIT SENSE LINE. REMOVED AND CLEARED CIT SENSE LINE, AND RE-CONNECTED. AS A PRECAUTION, CDP SENSE LINE WAS ALSO REMOVED, CLEANED AND RE-INSTALLED. OPS CHECK PERFORMED ON NR 1 ENGINE WITH NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F4 FRTA22WE E23EA 19950519004501995051900450WP 1995 5 19 WRLA95019 119950424A7714P18077 CONNECTOR DOUG DC10 DC1030F 3023504WP NR 2 ENGINE N1 DIRTY A WRLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27107WA 46836 DURING TAKEOFF, AT 140KTS, CAPTAIN NOTED 'ENGINE FAILED' LIGHT ON. CAPTAIN ABORTED TAKEOFF, STOPPING AIRCRAFT NORMALLY WITH THRUST REVERSE AND BRAKING. AIRCRAFT TAXIED BACK TO GATE WITHOUT FURTHER INCIDENT. CREW DEBRIEFED WITH MAINTENANCE AND STATED THAT THERE WAS NO INDICATION IN COCKPIT (DURING DECELERATION) AS TO WHICH ENGINE WAS MALFUNCTIONING, HOWEVER CREW FELT THAT THE NR 2 ENGINE WAS AT FAULT. MAINTENANCE FOUND CANNON PLUG AT N1 SPEED SENSOR OF NR 2 ENGINE TO BE DIRTY. CLEANED CANNON PLUG AND RECONNECTED. RAN NR 2 ENGINE, NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950519004511995051900451NE 1995 5 19 WRLA95020 219950426A73208010002 FUEL METER UNIT DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 3 ENG FAILED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27274WA 48633 DUE TO A LACK OF FACILITIES FOR 'HIGH-POWER' RUN UP, MX PERSONNEL HAD REQUESTED THAT FLT CREW CONDUCT PWR ASSURANCE RUN (UP TO 1.3 EPR) AT END TO TAXIWAY, PRIOR TO DEPARTURE. REQUEST WAS A FOLLOW UP TO PREVIOUS REPORT OF ENG VIBRATION (MX HAD ALREADY CONDUCTED IDLE PWR RUNS WITH NO FAULT FOUND). DURING PWR ASSURANCE RUN, FLT CREW NOTED 'RUMBLE/SURGE' IN NR 3 ENG. FLT CREW ELECTED TO RETURN TO GATE FOR MX ACTION. A/C RETURNED TO GATE W/O FURTHER INCIDENT. MX INSPECTED ENG FOR COMPRESSOR STALL AND PERFORMED BORESCOPE, NO MALFUNCTION/DAMAGE NOTED. CFDS INDICATED FAULT IN FMU. FMU REPLACED. ADDITIONAL PRECAUTION, NR 3 EEC REPLACED. ENG GROUND RUN WITH NO FAULT FOUND. A/C RETURNED TO SERVICE. 2L73 4F4 FRTA22WE E24NE 19950519004521995051900452NM 1995 5 19 WRLA95022 119950429A2420316BL WIRE DOUG MD11 MD11 3023602NM NR 1 AC BUS SHORTED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27271WA 48518 DURING TAXI, CREW NOTED NR 1 AC BUS TIE LOCKED OUT. CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE TROUBLESHOOTING. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING DETERMINED THAT WIRE NR 3-16BL WAS SHORTED TO GROUND, BETWEEN GCU CONNECTOR (FRM13A) AND NR 8 PIN OF IDG CANNON PLUG. REPLACED SHORTED WIRE. OPS CHECKS PERFORMED WITH NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950519004531995051900453NM 1995 5 19 WRLA95023 119950429A5247R1071M2 CABLE DOUG MD11 MD11 3023602NM APU DOOR LACK OF LUBE A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27275WA 48631 DURING TAXI, CREW NOTED APU DOOR OPEN LIGHT ON. CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE TROUBLESHOOTING. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOT DETERMINED THAT APU DOOR CABLE WAS BINDING. CABLE WAS CLEANED AND RELUBRICATED. OPS CHECK PERFORMED WITH NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950519004541995051900454WP 1995 5 19 95ZZZX2358 119950420A55413913411 RIB DOUG DC9 DC951 3022051WP RUDDER CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA N/R NR 1144. DURING C-CHECK, FOUND CORROSION ON CASTING AND ANGLE INTERNAL RIB OF RUDDER AT STA ZR-30 AND STA ZR-40. REMOVED AND REPLACED THE CASTING PER SRM 51-10-04. REF CONTROL NR HAL95043. 2L72 4F A6WE 19950519004551995051900455NM 1995 5 19 95ZZZX2359 119950417A5315 FLOOR BEAM BOEING727 727251 138408HNM FS 1070 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25258US 19977 DURING C-CHECK AND C.P.C.P. INPSECTION, FOUND FLOOR BEAM AT BS 1070 BESIDE R2 DOOR CORRODED. REMOVED CORRODED SECTION OF UPPER CHORD. FABRIATED REPAIR SECTIONS IAW SRM 53-10-8 USING PN BAC 1490-2785, BAC 1490-2831, AND BAC 1505-100617 MATERIAL. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR SECTION IAW SRM 53-10-8 AND SRM 51-30-2. 2L73 4F A3WE 19950519004561995051900456NM 1995 5 19 95ZZZX2360 119950417A5330 SKIN BOEING727 727251 138408HNM FS 1323 CRACKED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25258US 19977 DURING C-CHECK AN C.P.C.P. INSPECTION, FOUND BS 1323 SKIN CRACKED AT LOWER FORWARD CORNER OF CUT-OUT FOR THE LT NEG. RELIEF DOOR. (1.33 INCH IN LENGTH.) STOP DRILLED IAW SRM 51-10-1, PAGE 65, PARAGRAPH C. FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIGURE 1, SHEET NR 4, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2, FIGURE NR 1. SEALED PER SRM 51-20-4, (DOUBLER MATERIAL, 7075-T6, .063 INCH, LOT NR 393421). 2L73 4F A3WE 19950519004571995051900457NM 1995 5 19 95ZZZX2361 119950417A5320 STIFFENER BOEING727 727251 138408HNM FS 1183 RBL 24 CRACKED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25258US 19977 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND VERTICAL STIFFENER ON FORWARD SIDE OF BS 1183 BULKHEAD AT RBL 24 HAS CRACKED WEBBING APPROXIMATELY 5 FEET ABOVE FLOOR LEVEL. FABRICATED REPAIR SECTIONS IAW SB 727-53-0182. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR CHANNEL PN 65-33556-48 IAW DWG 69-33556 (BOEING) AND SB 727-53-0182, TUP II. 2L73 4F A3WE 19950519004581995051900458NM 1995 5 19 95ZZZX2362 119950417A5347 SEAT TRACK BOEING727 727251 138408HNM FS 1010 RBL 42 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25258US 19977 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK CORRODED AT RBL 42 FROM FS 1010 TO BS 1030. REMOVED CORRODED SECTION. ALSO, NR 4 SEAT TRACK AT BS 480 CORRODED. CUT OUT DAMAGED SECTION. FABRICATED REPLACEMENT TRACK SECTIONS OUT OF BAC 1520-1430 7178-76511 EXTRUSTION IAW SRM 51-30-2. 2L73 4F A3WE 19950519004601995051900460EA 1995 5 19 95ZZZX2364 119950502A28102770086102 DE-FUEL VALVE CNDAIRCL600 CL6002B16 1900305EA LT WING PANEL LEAKS A AIMKAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA251868M 5012 DURING INSTALLATION OF EITHER PART NUMBER VALVE LEAK CHECKS OF THESE UNITS KEPT FAILING. THE INSTRUCTIONS FOR TORQUING THE ATTACHING HARDWARE ARE FOUND ON THE VALVE AND RATED AT 24-27 INCH/POUNDS. CANADAIR DOES NOT HAVE ANY PROCEDURES TO ACCOMPLISH A CHANGE OF THESE UNITS. AFTER CONTACTING CANADAIR FIELD SERVICE, DETERMINED THE TORQUE UNITS ARE TOO HIGH AND CRUSHED THE GASKET RESULTING IN LEAKS. THE RECOMMENDED TORQUE ON THE HARDWARE SHOULD BE BETWEEN 8-10 INCH/POUNDS. CANADAIR WORKING ON REVISING THESE PROCEDURES. FIELD SERVICE HAS PREVIOUS DATA ON SIMILAR SITUATIONS. SUBMITTER RECOMMENDS CANADAIR ISSUE AN INFORMATION LETTER INFORMING OPERATORS OF THIS SITUATION FOLLOWED BY A MM REV. REVISION. 2L72 4F RTA21EA 19950519004661995051900466 1995 5 19 95ZZZX2370 419950427A235095251 SWITCH ROBSINR22 R22 7640102WP MIC SWITCH STUCK A LXPFK NONE O OTHER ININSP/MAINT 1 NM01505PR324 1380 SWITCH IS STUCK IN 'ON' POSITION RESULTING IN CONSTANT INTERCOM 'HOT MIC' OPERATION. REMOVED AND REPLACED SWITCH WITH THE SAME PART NUMBERED COMPONENT. 1G71 3O H10WE 19950519004781995051900478SO 1995 5 19 95ZZZX2382 219950413A8550 GEAR CESSNA401 401 207590CCE CONT O520 TSIO520E 17040SO OIL PUMP FAILED A OAWAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO058438F 4010286 18219171ER PILOT REPORTED OIL STREAMING FROM LEFT ENGINE NACELLE WITH LOSS OF OIL PRESSURE AT CRUISE. HE SECURED THE LEFT ENGINE AND NOTIFIED ATC OF THE SITUATION. ATC CLEARED THE AIRCRAFT FOR STRAIGHT-IN APPROACH AT RDU. LANDING MADE WITHOUT FURTHER INCIDENT. INVESTIGATION REVEALED THE OIL PUMP HOUSING HAD CRACKED DUE TO BREAKAGE OF THE PUMP GEARS. TCM SB M90-6 ADDRESSES REPLACEMENT OF 635334 AND 639388 SCAVENGE PUMP GEARS. INVESTIGATION IS IN PROGRESS TO SEE IF THESE GEARS WERE INSTALLED IN THIS ENGINE. 1L72 3O3 O A7CE E8CE 19950519004801995051900480CE 1995 5 19 95ZZZX2385 119950403A56105070170 WINDSHIELD CESSNA501 501 2076603CE COCKPIT LT MISMANUFACTURED A AISYAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL2568EA 7028 5010068 DURING PRE-PURCHASE INSPECTION, WINDSHIELDS MEASURED UNDER MINIMUM THICKNESS SPECIFICED BY CESSNA AIRCRAFT. THESE ARE ORIGINAL EQUIPMENT AND MAINTENANCE RECORDS REFLECT NO REPAIRS. ITS IS SUSPECTED UNDER SPEC UNITS WERE INSTALLED NEW AT FACTORY. THIS AIRCRAFT WAS PURCHASED USED FROM CESSNA IN 1989 AND NO REPAIRS WERE ACCOMPLISHED TO UNITS SINCE. RECOMMEND AD NOTE BE ISSUED REQUIRING ONE TIME INSPECTION OF WINDSHIELDS FOR MINIMUM THICKNESS ON ALL 500 SERIES CESSNAS. 1L72 4F A27CE 19950519004811995051900481CE 1995 5 19 95ZZZX2386 119950403A56105070180 WINDHSIELD CESSNA501 501 2076603CE COCKPIT RT MISMANUFACTURED A AISYAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL2568EA 7028 H11128 5010068 DURING PRE-PURCHASE INSPECTION, BOTH WINDSHIELDS WERE MEASURED UNDER MINIMUM THICKNESS SPECIFIED BY CESSNA AIRCRAFT. THESE ARE ORIGINAL UNITS AND MAINTENANCE RECORDS REFLECT NO REPAIRS SINCE NEW. IT IS SUSPECTED UNDER SPEC UNITS WERE INSTALLED NEW AT FACTORY. THIS AIRCRAFT WAS PURCHASED USED FROM CESSNA AND NO REPAIRS WERE ACCOMPLISHED. SUBMITTER RECOMMENDS AN AD NOTE BE ISSUED REQUIRING ONE TIME INSPECTION OF ALL WINDSHIELDS FOR THICKNESS IN ALL 500 SERIES CESSNAS. 1L72 4F A27CE 19950519004891995051900489EA 1995 5 19 95ZZZX2394 219950428A853069444R ROCKER ARM PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA INT-EXH VALVES MISINSTALLED ALAHYIAK NONE W INADEQUATE Q C ININSP/MAINT 1 NE016514A 650 277854130 L1268748A PERFORMED 400-HOUR VALVE INSPECTION, AND FOUND ALL ROCKER ARMS REVERSED ON ALL 6 CYLINDERS. EXHAUST ROCKER ARM OIL PORT SHOULD SPRAY OIL TOWARDS VALVE AND INTAKE ROCKER ARM OIL PORT SHOULD SPRAY OIL TOWARDS PUSH ROD ON THIS ENGINE. 1L72 3O3 O 1A10 1E4 19950519004911995051900491CE 1995 5 19 95ZZZX2396 119950510A2823 SELECTOR CESSNA175 175 2072502CE SELECTOR SHAFT MISMANUFACTURED ASASK6AK NONE O OTHER ININSP/MAINT 1 NE05 AFTER RE-WORK, ACFT RETURNED TO SERVICE. NUMEROUS HRS SPENT TRYING TO START REPAIRED ENGINE. IT WOULD START & RUN AT PARTIAL POWER, BUT DIE. PROBLEM TRACED TO NEWLY INSTALLED FUEL SELECTOR SHAFT THAT WAS 90 DEGREES IN ERROR. ERROR DISCOVERED WHILE DISCUSSING FLAWED PART WITH CESSNA PARTS REPS WHO WERE COMPARING OUR PART, THEIR INVENTORY PART, & BLUEPRINT. ALL SEEMED TO MATCH UNTIL ROLL PIN REMOVED THAT HOLDS INDICATOR HANDLE TO TOP. DISCOVERED 2 SETS OF HOLES, 90 DEGREES APART, ASKED CESSNA TO DISASSEMBLE THEIRS (REQUIRED TO INSTALL PART). SHAFT THEY HAD, HAD 2 SETS OF HOLES, & COULD BE ASSEMBLED 2 WAYS, 1 WOULD INDICATE LT TANK, BUT WOULD BE OFF. SELECTING BOTH, ONLY LT TANK WOULD SUPPLY FUEL. 1H71 3O NT3A17 19950519004921995051900492WP 1995 5 19 HAL95040 119950420A5330 SKIN DOUG DC9 DC951 3022051WP FS 1258 CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA N/R NR 827. DURING C-CHECK FOUND LEVEL 2 CORROSION ON FUSELAGE SKIN AT BUTT JOINT, FS 1258, STR 24R-24L. REMOVED AND REPLACED THE SKIN PER SRM 51-10-0. (X) 2L72 4F A6WE 19950519004931995051900493WP 1995 5 19 HAL95041 119950420A5320 THRESHOLD DOUG DC9 DC951 3022051WP FS 370-427 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA N/R NR 18N01242. DURING C-CHECK, FOUND LEVEL 2 CORROSION AT FORWARD CARGO PIT, THRESHOLD AREA AT DOOR CUT-OUT, THRESHOLD CHANNEL FROM STA 370 TO STA 427. ALSO, FOUND CRACK AT NT-PLATE TABS. FABRICATED AND INSTALLED NEW CHANNEL PER SRM 51-30-02 AND SRM 51-10-02. (X) 2L72 4F A6WE 19950519004941995051900494WP 1995 5 19 HAL95042 119950420A575339176602 FITTING DOUG DC9 DC951 3022051WP RT TE FLAP BROKEN A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA N/R NR 18N01049. DURING C-CHECK, FOUND BROKEN CASTING INSIDE RT TRAILING EDGE FLAP AT THE INBOARD CORNER. REMOVED AND REPLACED THE FITTING PER SRM 51-30-92. (X) 2L72 4F A6WE 19950519004951995051900495WP 1995 5 19 HAL95043 119950420A55403913410 ANGLE DOUG DC9 DC951 3022051WP RUDDER CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA N/R NR 1144. DURING C-CHECK, FOUND CORROSION ON CASTING AND ANGLE INTERNAL RIB OF RUDDER AT STA ZR-30 AND STA ZR-40. REMOVED AND REPLACED THE CASTING PER SRM 51-10-04. REF CONTROL NR 95ZZZX2358. (X) 2L72 4F A6WE 19950519004961995051900496NM 1995 5 19 9508016306 119950510A5315 BEAM BOEING747 747451 1384940NM FS 1630-1670 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01666US 23821 DURING PERIODIC CHECK, FOUND CORROSION ON FLOOR SUPPORT BEAM FS 1630 TO 1670 AT LBL 42. REPAIRED PER EA 63-98066. 2L74 4F RTA20WE 19950519004971995051900497WP 1995 5 19 9508029604 119950513A5320 FITTING DOUG DC9 DC932 3022066WP FWD CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE FORWARD CARGO DOOR UPPER FORWARD STOP FITTING. REPLACED FITTING PER SRM 51-30-00. 2L72 4F A6WE 19950519004981995051900498WP 1995 5 19 9508039993 119950514A5320 FITTING DOUG DC9 DC931 3022065WP FS 598 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE LONGERON 28L END FITTING AT FS 598. REPLACED END FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950519004991995051900499WP 1995 5 19 9508049989 119950515A5230 FITTING DOUG DC9 DC931 3022065WP AFT CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT CARGO DOOR LOWER HORIZONTAL BEAM FORWARD END FITTING. REPLACED FITTING PER SRM 51-01, 51-10-1, AND 51-30-1. MFG PART NUMBER 3914025-2B. 2L72 4F A6WE 19950519005001995051900500 1995 5 19 9508052717 419950516A344220704100112 RADAR TR UNIT BOEING727 7272S7 138407ZNM E/E COMPARTMENT FAILED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01721RC23352981 22492 EN ROUTE TO MSP, WEATHER RADAR STABILIZATION FAILED. DIVERTED TO DTW DUE TO THUNDERSTORMS. MAINTENANCE REPLACED RADAR CONTROL PANEL AND TRANSCEIVER. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950519005011995051900501NM 1995 5 19 95UAL747030 119950515A2612MS250893G FIRE TEST SWITCH BOEING747 747222B 1384904NM PWA JT9 JT9D7R4G2 52054NE WHEEL WELL FAILED A UALAK NONE N FALSE WARNING ININSP/MAINT 1 WP29152UA 23737 WHEEL WELL FIRE LIGHT IS ILLUMINATED AFTER TEST. REPLACED WHEEL WELL FIRE TEST SWITCH. 2L74 4F4 FRTA20WE E3NE 19950519005021995051900502NM 1995 5 19 95UAL747031 119950515A3350 EEL PWR LINE BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29159UA 21140 EEL INOP AT RIGHT HAND ROW 44 THROUGH ROW 50. REPLACED POWER LINE. 2L74 4F4 F A20WE E20EA 19950519005031995051900503NM 1995 5 19 95UAL747032 119950515A3350 EEL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CABIN MALFUNCTIONED A UALAK NONE N FALSE WARNING ININSP/MAINT 1 WP29155UA 20104 EEL IN ZONE E ILLUMINATED AT ALL TIMES. RESET CIRCUIT BREAKER ON P12. OPS CHECKS NORMAL. 2L74 4F4 F A20WE E20EA 19950519005041995051900504 1995 5 19 95UAL747033 419950516A2565 SLIDE BF GOODRICH 7A14311 BOEING747 747422 1384935NM NR 3 MED FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29 G013 SPARE MED NR 3 SLIDE/RAMP INTERNAL BULKHEAD SEPARATED DURING INFLATION USING SHOP AIR. REPLACED UNIT. 2L74 4F RTA20WE 19950519005051995051900505 1995 5 19 95UAL747034 419950516A25653A24024 ASPIRATORS BF GOODRICH 7A1323107 BOEING747 747422 1384935NM PWA 4056 PW4056 NE SLIDE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29186UA G683 26875 AT DISASSEMBLY FOUND SUD SLIDE TURBO-FAN ASPIRATORS WITH BLADE DAMAGE. ADDITIONALLY, THE FLAPPER VALVE ROD FELL OUT. REPLACED 2 EACH TURBO FANS ASPIRATORS AND FLAPPER VALVE ROD. 2L74 4F4 FRTA20WE E24NE 19950519005061995051900506NM 1995 5 19 95UAL757016 119950515A3350 EEL CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DIRTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29544UA 25322 EEL INOPERATIVE ON ROWS 24ABC TO 32ABC. CLEANED AND DRIED MOISTURE FROM LAMP CONNECTION AT ROW 24. CHECKS OKAY. 2L72 4F4 FRTA2NM E17NE 19950519005071995051900507NM 1995 5 19 95UAL767019 119950517A2420 IDG FEEDER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE RT GENERATOR DAMAGED A UALAK NONE L NO TEST CRCRUISE 1 WP29620UA 21880 DURING CRUISE RIGHT GENERATOR TRIPPED OFF, UNABLE TO START APU. UNSCHEDULED LANDING WAS MADE AT ORD. PROBLEM CAUSED BY SHORTING OF IDG FEEDER TO THE LEFT CORE COWL. REPLACED FEEDER AND PROPERLY ROUTED. 2L72 4F4 FRTA1NM E3NE 19950519005081995051900508WP 1995 5 19 ABXA9500386 119950510A53207075T6 DOOR JAMB DOUG DC8 DC861 3021952WP FS 1080-1120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND FORWARD AND AFT DOOR JAMB ON THE CENTER SERVICE DOOR STA 1080 TO 1120 CORRODED. REPAIRED IAW ABX REA D853-11006. 2L74 4F 4A25 19950519005091995051900509WP 1995 5 19 ABXA9500387 119950510A57302024T3511 PANEL DOUG DC8 DC861 3021952WP LT WING LE CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND LEFT WING LEADING EDGE OUTBOARD CLOSING PANEL CORRODED. REPAIRED PANEL IAW ABX REA D857-11142. 2L74 4F 4A25 19950519005101995051900510WP 1995 5 19 ABXA9500388 119950505A5230 DOOR JAMB DOUG DC8 DC861 3021952WP C2 DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE FORWARD CARGO PIT'S AFT DOOR JAMB CRACKED AND DENTED WITH NUMEROUS AREAS OF CORROSION. REPAIRED DOOR JAMB IAW ABX REA D583-10998MR. 2L74 4F 4A25 19950519005111995051900511WP 1995 5 19 ABXA9500389 119950505A54002014T6 SPAR CAP DOUG DC8 DC861 3021952WP NR 4 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE NR 4 PYLON INBOARD SPAR CAP CRACKED IN TWO PLACES. REPAIRED CRACKED SPAR CAP IAW REA D854-11009MR. 2L74 4F 4A25 19950519005121995051900512WP 1995 5 19 ABXA9500390 119950505A53302024T3 SKIN DOUG DC8 DC861 3021952WP FS 320-340 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE DOOR CUTOUT AT STATION 320 TO 340 AFT BOTTOM CORNER CRACKED. REPAIRED CRACKED FUSELAGE SKIN AT C1 LOWER DOOR SILL IAW ABX REA D853-11002. 2L74 4F 4A25 19950519005131995051900513WP 1995 5 19 ABXA9500391 119950505A5753 HINGE FITTING DOUG DC8 DC861 3021952WP RT TE FLAP CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE INBOARD HALF OF THE RIGHT INBOARD FLAP HINGE WORN AND CHAFED. REPAIRED HINGE FITTING IAW REA D857-11001MR. 2L74 4F 4A25 19950519005141995051900514WP 1995 5 19 ABXA9500392 119950510A53117075T6 FRAME DOUG DC8 DC861 3021952WP FS1400 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE FRAME AT STATION 1400, LONGERON 36R AND 34R, CORRODED AND CRACKED IN TWO PLACES. REPAIRED FRAME IAW ABX REA D853-11164. 2L74 4F 4A25 19950519005151995051900515WP 1995 5 19 ABXA9500393 119950510A5210 CORNER DOUG DC8 DC861 3021952WP PAX DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE LEFT AFT ENTRY DOOR UPPER CORNER OF CUT OUT TO HAVE A REPAIR THAT DOES NOT HAVE AN SRO DRAWING. REPAIRED IAW REA D853-11171. 2L74 4F 4A25 19950519005161995051900516WP 1995 5 19 ABXA9500394 119950510A53205613861301 DOUBLER DOUG DC8 DC861 3021952WP FS 8-25 MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND REPAIR AT STATION 8 TO 25, LONGERON 24L TO 25L MISSING FINGER DOUBLERS. REPAIRED LONGERON IAW ABX REA D853-11013. 2L74 4F 4A25 19950519005171995051900517WP 1995 5 19 ABXA9500395 119950510A53307075T5 SKIN DOUG DC8 DC861 3021952WP FS 1055-1350 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND BELLY SKIN AT STATION 1050 TO 1350, LONGERON 34L TO 35L CORRODED. REPAIRED BELLY SKIN IAW ABX REA D853-11143. 2L74 4F 4A25 19950519005181995051900518WP 1995 5 19 ABXA9500396 119950510A53137075T6511 LONGERON DOUG DC8 DC861 3021952WP FS 1410 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND LONGERON SPLICE AT STATION 1410 WITH CRACK UNDER FRAME. REPAIRED LONGERON IAW ABX REA D853-11139. 2L74 4F 4A25 19950519005191995051900519WP 1995 5 19 ABXA9500397 119950510A54147075T6 SKIN DOUG DC8 DC861 3021952WP NR 2 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND NR 2 PYLON OUTBOARD LOWER SURFACE AND INNER SKIN CRACKED. REPAIRED IAW ABX REA D857-11163. 2L74 4F 4A25 19950519005201995051900520WP 1995 5 19 ABXA9500398 119950510A54007075T6 SPAR DOUG DC8 DC861 3021952WP NR 2/3 PYLONS CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND NR 2 AND NR 3 PYLONS WITH CRACKS ON THE UPPER SPAR CAP. REPAIRED IAW ABX REA D854-11147. 2L74 4F 4A25 19950519005211995051900521WP 1995 5 19 ABXA9500399 119950510A53117075T6 FRAME DOUG DC8 DC861 3021952WP FS 1100 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE AFT PIT FRAME AT STATION 1100 CRACKED AT LONGERON 36. REPAIRED IAW REA D853-11165. 2L74 4F 4A25 19950519005221995051900522WP 1995 5 19 ABXA9500400 119950510A52402024 FRAME DOUG DC8 DC861 3021952WP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND FRAME AND WEB AT RIGHT FORWARD SERVICE DOOR DENTED AND CRACKED. REPAIRED FRAME AND WEB IAW ABX REA D853-11169. 2L74 4F 4A25 19950519005231995051900523WP 1995 5 19 ABXA9500401 119950510A5320 JAMB DOUG DC8 DC861 3021952WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE FORWARD PIT AFT DOOR LOWER JAMB CRACKED AND DENTED WITH NUMEROUS AREAS OF CORROSION. REPAIRED IAW ABX REA D853-10998MR. 2L74 4F 4A25 19950519005241995051900524WP 1995 5 19 ABXA9500402 119950510A5753 HINGE FITTING DOUG DC8 DC861 3021952WP TE FLAP CHAFFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE RIGHT INBOARD HINGE INBOARD HALF WORN. REPAIRED CHAFED AND WORN HINGE FITTINGS IAW ABX REA D857-11001MR. 2L74 4F 4A25 19950519005251995051900525WP 1995 5 19 ABXA9500403 119950510A53302024T3 SKIN DOUG DC8 DC861 3021952WP FS 320-340 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE DOOR CUTOUT AT STATION 320 TO 340 BOTTOM CORNER CRACKED. REPAIRED CRACKED FUSEAGE SKIN AT C1 DOOR IAW ABX REA D853-11002. 2L74 4F 4A25 19950519005261995051900526WP 1995 5 19 ABXA9500404 119950510A55417075T6 SPAR DOUG DC8 DC861 3021952WP RUDDER CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND RIGHT FORWARD RUDDER SPAR CORRODED AT STATION ZR 284 AND ZR 330 TO 338. REPAIRED IAW ABX REA D855-11005. 2L74 4F 4A25 19950519005271995051900527WP 1995 5 19 ABXA9500405 119950510A540057692526 ANGLE DOUG DC8 DC861 3021952WP NR 1 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK, FOUND THE NR 1 PYLON LEADING EDGE INTERIOR CRACKED AT STA 237. REPAIRED IAW ABX REA D854-11007. 2L74 4F 4A25 19950519005281995051900528WP 1995 5 19 ABXA9500444 119950516A52303485173 SEAL DOUG DC8 DC861 3021952WP CARGO DOOR DEFECTIVE A ABXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL23849AX 45891 AT APPROXIMATELY 26,000 FT, 7 PSID, AND 4,500 FT CABIN, THE CABIN RATE OF CLIMB INDICATOR WENT FROM 500 TO 2500 FPM ASCENT. REGAINED CONTROL OF CABIN AT APPROXIMATELY 18,000 FT AND 3 PSID. AIRCRAFT CONTINUED TO ATL. RE-INSTALLED SEAL IN RETAINER ON MAIN CARGO DOOR IAW DC 8 MM. ALSO, MADE SMALL REPAIR IN TORN SEAL IAW DC 8 TEMP REV SRM CHAPTER 52-2-1. 2L74 4F 4A25 19950519005291995051900529NM 1995 5 19 DL72E951982 119950509A5510 BALANCE BOARD BOEING727 727247 138408FNM HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV-2 CHECK, .8125 CRACK AT LT INBD BALANCE BOARD ACCESS PANEL 9114. REPAIRED AS PER 55-10-3 FIG 3. 2L73 4F A3WE 19950519005301995051900530NM 1995 5 19 DL72E951984 119950503A5347 SEAT TRACK BOEING727 727247 138408FNM FS 400-420 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION ON I/B SEAT TRACK RBL 24 BETWEEN STA 400 AND ST 420. REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950519005311995051900531NM 1995 5 19 DL72E951985 119950502A5347 SEAT TRACK BOEING727 727247 138408FNM FS 420 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION STA 420, 43 RBL I/B SIDE MIDDLE RT SEAT TRACK. REPAIRED PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950519005321995051900532NM 1995 5 19 DL72E951987 119950502A5347 SEAT TRACK BOEING727 727247 138408FNM FS 420-440 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK RBL 24 RT I/B SEAT TRACK BETWEEN STA 420 AND STA 440. REPAIRED PER SRM FIG 7. 2L73 4F A3WE 19950519005331995051900533NM 1995 5 19 DL72E952006 119950503A5311 FORMER BOEING727 727247 138408FNM FS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION ON FORMER FWD SIDE STA 740 BETWEEN STR 28R TO 27R. REPAIRED FORMER PER M/M 53-11-0 FIG 826. 2L73 4F A3WE 19950519005341995051900534NM 1995 5 19 DL72E952007 119950503A5320 CLIP BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD OF STA 700 INBD OF STR 28L. REPAIRED PER M/M 53-10-0 PG 825. 2L73 4F A3WE 19950519005351995051900535NM 1995 5 19 DL72E952008 119950503A5320 CLIP BOEING727 727247 138408FNM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 49810 FOUND ON CV2 CHECK, CORROSION ON SKIN CLIP FWD STA 700 INBD OF STR 28R W/W 257. REPAIRED PER M/M 53-11-0 PG 825. 2L73 4F A3WE 19950519005361995051900536NM 1995 5 19 DL72L951955 119950422A532069678811 GUSSET BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 49810 THE RT TORQUE BOX HORIZONTAL BEAM GUSSET AT FS 1273 WAS FOUND CRACKED. REPAIRS WERE ACCOMPLISHED PER S/B 53-0129. 2L73 4F A3WE 19950519005371995051900537NM 1995 5 19 DL72S951902 119950505A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE FLAP CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11522DA 21582 49810 UPON INSPECTION, FOUND CRACK IN RIB OF NR 6 L/E SLAT. REPAIRED ITEM PER MM 57-54-0 FIG 814. FOUND DURING SHOP VISIT. 2L73 4F A3WE 19950519005381995051900538NM 1995 5 19 DL72S951921 119950430A5311 FRAME BOEING727 727232 1384082NM FS 804 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 FRAME CRACKED, FS 804 FUSELAGE FRAME IS CRACKED AT STR 14R. REPAIRED AS PER SRM 53-10-4 FIG 22. FOUND AT HMV. 2L73 4F A3WE 19950519005391995051900539NM 1995 5 19 DL72S951923 119950428A5755 ANGLE BOEING727 727232 1384082NM NR 7 SPOILER BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 ANGLE IS BROKEN AT LOWER MOUNT OF NR 7 SPOILER FITTING. REMOVED REPAIR ANGLE AND MANUFACTURED NEW AS PER MM 57-20-22. FOUND AT HMV. 2L73 4F A3WE 19950519005401995051900540NM 1995 5 19 DL72S951926 119950428A5311 FRAME BOEING727 727232 1384082NM FS 930 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 AT HMV, FUSELAGE FRAME CRACKED STA 930 RIGHT SIDE STR 14. REPAIRED FRAME PER SRM 53-10-4. 2L73 4F A3WE 19950519005411995051900541NM 1995 5 19 DL72S951927 119950428A5330 SKIN BOEING727 727232 1384082NM FS 1243 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 SMALL DENT 1 BY 1 BY .09375 AFT LT FUSELAGE 3 FEET SWD OF AFT LAV SVC PANEL STA 1243 ST 20L. REPAIRED SKIN PER SRM 53-30-3 PG 74. 2L73 4F A3WE 19950519005421995051900542NM 1995 5 19 DL72S951952 119950430A5311 FRAME BOEING727 727232 1384082NM FS 277 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 AT HMV, FRAME CRACKED .5 CRACK IN FRAME STA 277 STGR 16L. ROUTED OUT DAMAGE IN FRAME STGR 16L STA 277. FABRICATED REPAIR PER SRM 51-40-2 FIG 1, INSTALLED REPAIR PER SRM 51-40-2 FIG 1. 2L73 4F A3WE 19950519005431995051900543NM 1995 5 19 DL72S951973 119950429A5313 STRINGER BOEING727 727232 1384082NM FS 34 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 49810 A HMV, STRINGER CRACKED, .25 INCH CRACK IN STGR 20R JUST FWD OF STA 344. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED REPAIRS PER SRM 53-10-3. 2L73 4F A3WE 19950519005441995051900544NM 1995 5 19 DL72S952000 119950425A5754651622374 SLAT BOEING727 727225 1384077NM NR 7 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 49810 THE TOP I/B CORNER OF THE ANTI-ICE DUCT CUTOUT IS CRACKED. REPAIRED PER M/M 57-54-0 FIG 801 FOR NR 7 L/E SLAT. 2L73 4F A3WE 19950519005451995051900545NM 1995 5 19 DL72S952001 119950425A5754651622374 RIB BOEING727 727225 1384077NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 49810 RIB NR 19 CRACKED AND WAS REPAIRED PER M/M 57-54-0 FIG 814, FORNR #7 L/E SLAT, DURING SHOP INSPECTION. 2L73 4F A3WE 19950519005461995051900546NM 1995 5 19 DL72W951953 119950424A53306554590 SKIN BOEING727 727247 138408FNM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 49810 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT ALONG THE AFT EDGE. REPAIRS WERE ACCOMPLISHED PER ERA 301584-14. 2L73 4F A3WE 19950519005471995051900547NM 1995 5 19 DL72W951954 119950424A532065175186 BEAM BOEING727 727247 138408FNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 49810 THE RT TORQUE BOX UPPER TRANSVERSE BEAM AT FS 1273 WAS FOUND CRACKED. REPAIRS WERE ACCOMPLISHED PER S/B 53-0129. 2L73 4F A3WE 19950519005481995051900548NM 1995 5 19 DL72W951993 119950502A5754 ANGLE BOEING727 727247 138408FNM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 49810 FOUND ON LTR CK, NR 8 SLAT ANGLE CRACKED JUST I/B OF I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12. 2L73 4F A3WE 19950519005491995051900549NM 1995 5 19 DL73E951920 119950505A5230 SKIN BOEING737 7372T4 1384492NM CARGO DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO112FOR 22369 49810 C-1 B/B DOOR DENTED AND OIL CANNING. REPAIR REF ERA 301714-14. 2L72 4F A16WE 19950519005501995051900550NM 1995 5 19 DL73E951956 119950504A5330 SKIN BOEING737 7372T4 1384492NM FS 764 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112FOR 22369 49810 THE FUSELAGE SKIN AT STA 764 HAS A 4 CRACK JUST BELOW STR 17L. EXTERNAL REPAIR DOUBLER WILL BE INSTALLED PER THE SRM. 2L72 4F A16WE 19950519005511995051900551NM 1995 5 19 DL73S951941 119950430A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND ON INSP DFW, LT ELEVATOR DAMAGE JUST OUTBOARD OF STA 3902, 4 INCHES FROM TRAILING EDGE 1 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301771-14. 2L72 4F RTA16WE 19950519005521995051900552NM 1995 5 19 DL73S951942 119950430A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, LT ELEVATOR DAMAGED BETWEEN STA 94.27 AND 66.54, 15 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE STARTED REPAIR PER SRM 55-20-3. REPAIRED ELEV PER SRM 55-20-3. INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005531995051900553NM 1995 5 19 DL73S951943 119950430A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 149.12 AND 121.59, 12 INCHES FROM TRAILING EDGE 2.5 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005541995051900554NM 1995 5 19 DL73S951944 119950430A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, LT ELEVATOR DAMAGE BETWEEN STA 176.64 AND 149.12, 13 INCHES FROM TRAILING EDGE 2 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005551995051900555NM 1995 5 19 DL73S951945 119950430A5522 SKIN BOEING737 737232 1384475NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, LT ELEVATOR DAMAGE OUTBOARD OF STA 176.64, 6 INCHES FROM TRAILING EDGE 1.25 INCH DAMAGE. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 91.08 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005561995051900556NM 1995 5 19 DL73S951946 119950430A5522 SKIN BOEING737 737232 1384475NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, RT ELEVATOR DAMAGED INDB OF STA 66.54 APPROX 10.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005571995051900557NM 1995 5 19 DL73S951947 119950430A5522 SKIN BOEING737 737232 1384475NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 66.54 APPROX 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005581995051900558NM 1995 5 19 DL73S951948 119950430A5522 ELEVATOR BOEING737 737232 1384475NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, RT ELEVATOR DAMAGED OUTBD OF STA 39.02 APPROXIMATELY 20.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3 INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005591995051900559NM 1995 5 19 DL73S951949 119950430A5522 SKIN BOEING737 737232 1384475NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, RT ELEVATOR DAMAGED INBD OF STA 149.12, 15.0 INCHES FROM TRAILING EDGE 3.0 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005601995051900560NM 1995 5 19 DL73S951950 119950430A5522 SKIN BOEING737 737232 1384475NM RT ELEVATOR DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 49810 FOUND DURING INSP DFW, RT ELEVATOR DAMAGED JUST OUTBD OF TRIM TAB APPROXIMATE STATION 121.59, APPROX 3.0 INCHES FROM TRAILING EDGE 1.5 INCHES IN DIAMETER. REPAIRED ELEV PER SRM 55-20-3, INSTALLED NEW BALANCE WEIGHT 89.20 PLACARD PER ERA 301711-14. 2L72 4F RTA16WE 19950519005611995051900561NM 1995 5 19 DL757951903 119950505A5754114N4002132 TE WEDGE BOEING757 757232 1384965NM NR 10 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 49810 HAIL DAMAGE ON NR 10 SLAT. REPLACED T/E WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519005621995051900562NM 1995 5 19 DL757951904 119950504A5350 RADOME BOEING757 757232 1384965NM FWD FUSELAGE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11653DL 24393 49810 DURING LETTER CHECK, FOUND RADOME WITH DAMAGED AREA AT RBL 34.5, WL 190, A 1 BY 7 DENT ON RT SIDE. REPAIRED DAMAGED AREA OF RADOME AS PER SRM 53-10-72 AND PAINTED. 2L72 4F RTA2NM 19950519005631995051900563NM 1995 5 19 DL757951905 119950504A5753 TE SKIN BOEING757 757232 1384965NM LT TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11653DL 24393 49810 FOUND DURING LETTER CHECK, I/B FLAP BOTTOM T/E CRACKED O/B OF AFT TRUNNION FAIRING, LT WING. REPAIRED PER SRM 51-70-07 AND PAINTED. 2L72 4F RTA2NM 19950519005641995051900564NM 1995 5 19 DL757951906 119950502A5754114N4003172 TE WEDGE BOEING757 757232 1384965NM NR 9 LE SLAT DENTED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 REPLACED TRAILING EDGE WEDGE ON NUMBER 9 LEADING EDGE SLAT AS PER SRM REF 57-43-02, DURING SHOP VISIT FOR HAIL DAMAGE. 2L72 4F RTA2NM 19950519005651995051900565NM 1995 5 19 DL757951908 119950506A5754114N300264 SKIN BOEING757 757232 1384965NM NR 6 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 49810 DURING SHOP VISIT, NR 6 L/E SLAT WAS REPAIRED FOR HAIL DAMAGE, PER SRM 57-43-02. 2L72 4F RTA2NM 19950519005661995051900566NM 1995 5 19 DL757951917 119950506A5754114N4002137 SKIN BOEING757 757232 1384965NM NR 1 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 DURING SHOP INSPECITON, NR 1 L/E SLAT, T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519005671995051900567NM 1995 5 19 DL757951918 119950506A5754114N4004146 TE WEDGE BOEING757 757232 1384965NM NR 8 LE SLAT DENTS A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 HAIL DAMAGE ON NR 8 SLAT T/E WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519005681995051900568NM 1995 5 19 DL757951919 119950501A5754114N4005178A SLAT BOEING757 757232 1384965NM NR 7 SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 NR 7 SLAT HAIL DAMAGE. REPLACED T/E WEDGE PER SRM 57-43-02, DURING SHOP VISIT. 2L72 4F RTA2NM 19950519005691995051900569NM 1995 5 19 DL757951924 119950507A5754114N300263 SKIN BOEING757 757232 1384965NM NR 5 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 HAIL DAMAGE TO NUMBER 5 SLAT. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950519005701995051900570NM 1995 5 19 DL757951925 119950507A5754114N4005163 SKIN BOEING757 757232 1384965NM NR 4 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11620DL 22910 49810 HAIL DAMAGE OCCURED, T/E WEDGE HAS MANY DENTS. REPLACED T/E WEDGE PER SRM 57-43-02, FOR NR 4 L/E SLAT. 2L72 4F RTA2NM 19950519005711995051900571NM 1995 5 19 DL757951939 119950423A5315 FLOORBEAM BOEING757 757232 1384965NM FS 345 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 49810 AT HMV, FLOORBEAM AT FS 345 IS CORRODED FROM LBL 5 TO LBL 19. REPAIRED PER SRM 53-30-51 PG 212. 2L72 4F RTA2NM 19950519005721995051900572NM 1995 5 19 DL757951940 119950423A5315 FLOORBEAM BOEING757 757232 1384965NM FS 365 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 49810 AT HMV, FLOORBEAM AT FS 365 IS CORRODED IN SEVERAL AREAS FROM OBL TO RBL 64. REPAIRED PER SRM 53-00-51 PG 212. 2L72 4F RTA2NM 19950519005731995051900573NM 1995 5 19 DL757951977 119950424A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11631DL 23612 49810 RECEIVED RADOME INTO SHOP. UPON INSPECTION FOUND CHIPPED PAINT, EXCESSIVE MOISTURE AND AREA OF DELAMINATION AT 12 O'CLOCK JUST AFT OF THE ERROSION BOOT. REBUILT BOTH SKINS OF RADOME USING ORIGINAL BASE OF RADOME AS PER SRM 53-10-72. APPLIED ERROSION BOOT AND PAINT AS PER PS 900-9-1-11 NR 05. RADOME SENT TO TRANSMISSIVITY TESTING AND PASSED TEST. RADOME PASSED FINAL INSPECTION AND ROUTED TO STOCK. 2L72 4F RTA2NM 19950519005741995051900574NM 1995 5 19 DL757951983 119950314A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11659DL 24421 49810 RECEIVED RADOME INTO SHOP AND UPON INSPECTION, FOUND EXCESSIVE MOISTURE IN CORE OF RADOME. REMOVED INSIDE SKIN TO DRY OUT CORE OF RADOME AS PER SRM 53-10-72. REPLACED INSIDE SKIN PER SRM 53-10-72. APPLIED EROSSION BOOT AND PAINT AS PER PS 900-9-1-11 NR 05. RADOME PASSED TRANSMISSIVITY TEST. RADOME PASSED FINAL INSPECTION AND SENT TO STOCK. 2L72 4F RTA2NM 19950519005751995051900575NM 1995 5 19 DL767951989 119950430A5512 WEDGE BOEING767 767232 1385132NM LT HORIZ STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 49810 FOUND DURING INSPECTION DFW, HOLE IN T/E WEDGE LEFT HORIZ STAB 3 INCHES FWD OF T/E 30 INCH INBD OF TIP. REPAIRED PER SRM 55-10-01. 2L72 4F RTA1NM 19950519005761995051900576NM 1995 5 19 DL767951990 119950430A5751 SKIN BOEING767 767232 1385132NM RT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 49810 FOUND DURING INSPECTION DFW, 2 EA CRACKS IN O/B END OF O/B AILERON UPPER SURFACE. REPAIRED PER SRM 57-60-02. 2L72 4F RTA1NM 19950519005771995051900577NM 1995 5 19 DL767951991 119950430A5751 SKIN BOEING767 767232 1385132NM LT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 49810 FOUND DURING INSPECTION DFW, 1 CRACK IN UPPER SURFACE OF I/B AILERON. REPAIRED I/B AILERON AS PER SRM 57-60-01 SANDED AND REPAINTED AREA. 2L72 4F RTA1NM 19950519005781995051900578NM 1995 5 19 DL767951998 119950505A5522 SKIN 183T20011 BOEING767 767232 1385132NM LT ELEVATOR PUNCTURED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11114DL 000080 22226 49810 LT ELEVATOR HAS 7 PUNCTURES ON UPPER SURFACE FROM THE HAIL STORM AT DFW. PUNCTURES WERE REPAIRED PER SRM 55-20-01. 2L72 4F RTA1NM 19950519005791995051900579NM 1995 5 19 DL76S951907 119950430A5754114T410337A SKIN BOEING767 767332 1382001NM NR 3 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 25145 49810 SLAT T/E WEDGE HAIL DAMAGED. REPAIRED PER CMM 57-43-61, FOR NR 3 L/E SLAT DURING SHOP VISIT. 2L72 4F RTA1NM 19950519005801995051900580NM 1995 5 19 DL76S951930 119950508A5754114T310021A SKIN BOEING767 767332 1382001NM NR 6 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 49810 DURING SHOP VISIT, NR 6 L/E SLAT WEDGE WAS REPLACED DUE TO HAIL DAMAGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950519005811995051900581WP 1995 5 19 DLL10951909 119950407A5330 SKIN DOUBLER LKHEED1011 10113851 5265010WP NR 3 EXCHANGER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 AT HMV, PNL DOUBLER CRACKED UPPER FWD CORNER FOR NR 3 HEAT EXCHANGER. REPAIRED PER SRM 53-31-00 FIG 834. 2L73 4F A23WE 19950519005821995051900582WP 1995 5 19 DLL10951910 119950419A5743 FITTING LKHEED1011 10113851 5265010WP MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 AT HMV, MLG FITTING, CORRODED HOLES 17 THROUGH 20 COMMON TO WING AT THE RETRACT FITTING ATTACH AREA ARE CORRODED. CONTINUED ON N/R 2125. REAMED HOLES 17 TO 20 TO .625 TO REMOVE CORROSION. CORROSION REMOVAL OK PER SRM 57-14-00, HFEC PER SRM 57-14-00 CK OK. ROTO PEENED PER SRM 57-14-00 PG 809, CAD PLATED PER PS 900-3-9. 2L73 4F A23WE 19950519005831995051900583WP 1995 5 19 DLL10951911 119950419A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 LT MLG RETRACT FITTING, CORRODED HOLES 1 THROUGH 6 TO .750 TO REMOVE CORROSION. SPOT FACED NR 2 HOLE TO .060 DEEP. HOLE ID'S ARE WITHIN LIMITS PER SRM 57-14-00. CORROSION REMOVAL IN HOLES IS OK. FUTHER REPAIR COMPLETED ON JPC 032169 TRK NR MRL465. COMPLETED WITH ERA 270721-14. 2L73 4F A23WE 19950519005841995051900584WP 1995 5 19 DLL10951912 119950425A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 935 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 AT HMV, LWR GALLEY TEAR STRAP DISBONDED FS 935 BETWEEN STR 40 TO 45, ON FUSELAGE SKIN. REPAIRED PER SRM 53-31-00 FIG 805. 2L73 4F A23WE 19950519005851995051900585WP 1995 5 19 DLL10951914 119950425A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 LT GEAR FITTING FWD TRUNNION AFT BORE HAS CORROSION ON FWD FACE AND CORROSION AND PITTING IN BORE. BORED LUG TO 4.229 TO REMOVE CORROSION. BLENDED AREAS TO REMOVE MINOR CORROSION. TREATED/PAINTED PER SRM 57-14-00. 2L73 4F A23WE 19950519005861995051900586WP 1995 5 19 DLL10951916 119950406A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1605 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TOP OF FLOORBEAM CORRODED STA 1605 LBL 3 TO 9. REMOVED DAMAGED AREA AND FABRICATED NEW CAP PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950519005871995051900587WP 1995 5 19 DLL10951972 119950509A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 476 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 SKIN BULGED/RIVETS SHEARED FS 476 STRGR 27 TO 26. FOUND DURING INITAIL INSP AT HMV. CLEANED CORROSION PER 53-31-00 FIG 801 REPAIRED TEAR STRAP PER 53-31-00 FIG 804/836. 2L73 4F A23WE 19950519005881995051900588WP 1995 5 19 DLL10951974 119950509A5510 STIFFENER LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005891995051900589WP 1995 5 19 DLL10951975 119950509A5510 STIFFENER LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENER CRACKED LT HORIZ LE PANEL 331E, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005901995051900590WP 1995 5 19 DLL10951976 119950509A5510 STIFFENER LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENER CRACKED RT HORIZ LE PANEL 341D, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005911995051900591WP 1995 5 19 DLL10951999 119950509A5510 STIFFENER LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331F, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005921995051900592WP 1995 5 19 DLL10952002 119950509A5510 STIFFENER LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341C, FOUND DURING HMV. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005931995051900593WP 1995 5 19 DLL10952003 119950406A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1615 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 TEAR STRAP DISBONDED AT FS 1615 BETWEEN STRINGER 39 AND 40. REPAIRED PER SRM 53-31-00 PG 30, FOUND AT HMV. 2L73 4F A23WE 19950519005941995051900594WP 1995 5 19 DLL10952004 119950406A5320 PRESSURE DECK LKHEED1011 10113851 5265010WP FS 1243 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 PRESSURE DECK CRACKED RIGHT WHEEL WELL FS 1243 RBL 115 AT EXPANSION JOINT. REPAIRED PER SRM 53-11-00 FIG 844. 2L73 4F A23WE 19950519005951995051900595WP 1995 5 19 DLL10952005 119950416A5510 STIFFENER LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 49810 INTERNAL STIFFENER CRACKED IN LEFT HAND HORIZONTAL STABILIZER LEADING EDGE PANEL 331C. FOUND AT HMV, REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950519005971995051900597WP 1995 5 19 MWEA95205 119950516A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A MWEAO OTHER J WARNING INDICATION CRCRUISE 1 GL31501ME 47132 WHILE AT CRUISE 330 CABIN PRESSURE WAS SLOWLY LOST AND MASKS DROPPED. REGAINED CABIN PRESSURE CONTROL AT 250. A/C FERRY TO MKE. REPACKED ALL O2 MASKS, GROUND PRESSURIZED A/C. COULD NOT DUPLICATE PROBLEM. PERFORMED EVALUATION FLIGHT. NO AUTO PRESSURIZATION PROBLEMS REPORTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950519005981995051900598SO 1995 5 19 SWIA95579 119950513A275012039902002 FITTING EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT TE FLAP BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RIGHT OUTBOARD NACELLE FLAP BELL CRANK BROKEN AT HARD MOUNT. REPLACED RT NACELLE FLAP IAW MM 27-50-02 AND PER RII CARD NUMBER 18. OPERATIONALLY CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950519005991995051900599SO 1995 5 19 SWIA95580 119950513A2913PV302229 HYD PUMP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE FAILED A SWIAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07207SW 120266 LOST ALL HYDRAULIC PRESSURE IN FLIGHT, LOW PRESSURE ELECTRICAL STANDBY FAILED TO OPERATE. REPLACED A BROKEN RETURN LINE AT ENGINE PUMP IN THE LEFT HYDRAULICS BAY. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP. OPERATIONALLY AND LEAK CHECKS GOOD. DECONTAMINATION COMPLIED WITH IN ACCORDANCE WITH EMB 120 MM 20-00-02. ALL SYSTEMS OPERATIONALLY CHECK GOOD ON BLUE HYDRAULIC SYSTEM. 2L72 4T4 TRTA31SO E20NE 19950519006001995051900600 1995 5 19 95ZZZW694 319950423A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE RT PROPELLER MISSING A AJJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01836CA321 UE32 RIGHT PROPELLER, ONE DE-ICE BOOT MISSING. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL ON 1/18/95, AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, ITS APPARENT THAT THE PROBELM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. 2L72 4T RTA24CE 19950519006011995051900601CE 1995 5 19 95ZZZW695 119950424A712011491002537 ENGINE TRUSS BEECH 1900 1900C 1154161CE LT WING CRACKED A AXZWAK NONE O OTHER ININSP/MAINT 1 WP0711ZR 18873 UB11 DURING A SCHEDULED INSPECTION, THE ENG TRUSS INSPECTION WAS COMPLIED WITH AS REQUIRED BY AD 95-0218, AND BEECH SB 2255, REV VI. THE TRUSS WAS FOUND BROKEN IN AREA A, ONE OF THE INSPECTION POINTS REQUIRED BY THE AD. THE ENGINE TRUSS WAS LAST INSPECTED ON 4/11/95, 86 HOURS PREVIOUS TO THIS INSPECTION. ENGINE TRUSS MOUNT REMOVED FROM TEH AIRCRAFT AND REPLACED WITH NEW TRUSS. (W) 2L72 4T RTA24CE 19950519006021995051900602CE 1995 5 19 95ZZZW696 119950418A6120310047303 WIRE ROPE BEECH 1900 1900 1154160CE NR 1 ENG OUT OF RIG A AXZWAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP07719GL17586 UB19 ON TAKEOFF, JUST AFTER ROTATION, NR 1 ENGINE LOST POWER. RPM DROPPED, TORQUE WENT TO 4500 LBS PROP WOULD NOT FEATHER WITH PROP LEVER. PROP WAS FEATHERED BY SHUTTING DOWN ENGINE. MAINTENANCE INSPECTED ALL CONTROLS AND LINKAGE. FOUND BETA CABLE STOP BALL UNSEATED AT FORWARD END. RIGGED THROTTLE CABLE TO BETA VALVE. PERFORMED GROUND RUNS AND MAINTENANCE IAW PWA MM 76-16-01. FLEET CAMPAIGN CONDUCTED. NO OTHER PROBLEMS FOUND. (W) 2L72 4T RTA24CE 19950519006031995051900603CE 1995 5 19 95ZZZW697 119950418A6120319257 BALL END BEECH 1900 1900 1154160CE NR 1 ENGINE NOT SEATED A AXZWAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP07719GL17586 UB19 ON TAKEOFF, JUST AFTER ROTATION, NR 1 ENGINE LOST POWER. RPM DROPPED, TORQUE WENT TO 4500 LBS PROP WOULD NOT FEATHER WITH PROP LEVER. PROP WAS FEATHERED BY SHUTTING DOWN ENGINE. MAINTENANCE INSPECTED ALL CONTROLS AND LINKAGE. FOUND BETA CABLE STOP BALL UNSEATED AT FORWARD END. RIGGED THROTTLE CABLE TO BETA VALVE. PERFORMED GROUND RUNS AND MAINTENANCE IAW PWA MM 76-16-01. FLEET CAMPAIGN CONDUCTED. NO OTHER PROBLEMS FOUND. (W) 2L72 4T RTA24CE 19950519006041995051900604CE 1995 5 19 95ZZZW698 119950426A24301143810231 DC POWER PANEL BEECH 1900 1900C 1154161CE LT NACELLE OPEN RELAY A PLGAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 NE0531240 0206 UC28 BOS - FLT NR 4736 - AFTER TAKEOFF THE RIGHT DC GENERATOR DROPPED OFF LINE AND WOULD NOT RESET. THE AIRCRAFT RETURNED TO BOS, LANDING UNEVENTFULLY. MX WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE LEFT DC POWER PANEL IAW THE BEECH MM AND RETURNED THE AIRCRAFT TO SERVICE. (W) 2L72 4T RTA24CE 19950519006051995051900605EU 1995 5 19 95ZZZW699 119950419A2420MS1051425 CIRCUIT BREAKER SAAB SF340 SF340A 7850100EU AC GEN SYSTEM FAILED A PLGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE05748BA 340A149 LEFT AC GEN HAD AN INDICATION FAILURE IN FLIGHT BOS TO BDL, FLIGHT 4864 AND RETURNED TO BOS DUE TO BAD WEATHER IN BDL. FOUND CIRCUIT BREAKER 25HE INLEFT WHEEL WELL BAD. REPLACED BREAKER AMP NO DEFECTS FOUND ON TEST FLIGHT. (W) 2L72 4T RTA52EU 19950519006061995051900606WP 1995 5 19 95ZZZW700 119950430A5730 SKIN DOUG DC8 DC862 3021970WP WS 281.5/329 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROISION AT RIGHT LEADING EDGE AT XFS 291.500 TO 329.00. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER USING CLAS 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DONE PER EO ARW 950037-75/76. CORROSION FOUND LEVEL II. (W) 2L74 4F 4A25 19950519006071995051900607WP 1995 5 19 95ZZZW701 119950403A5730 SKIN DOUG DC8 DC862 3021970WP WS 310.25 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE XFS 182.500. CORROSION FOUND IS BEYOND LIMIT. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER USING CLAD 7075-T6.071. PICKED UP EXISTING ATTACHMENT WHERE POSSIBLE. ALL WORK DONE PER EO NR ARW 650037-75/76. CORROSION FOUND WAS LEVEL II. 2L74 4F 4A25 19950519006081995051900608WP 1995 5 19 95ZZZW702 119950405A5730 SKIN DOUG DC8 DC862 3021970WP WS 207.159 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSION. 2L74 4F 4A25 19950519006091995051900609WP 1995 5 19 95ZZZW703 119950405A5730 SKIN DOUG DC8 DC862 3021970WP WS 207.159 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSION. (W) 2L74 4F 4A25 19950519006101995051900610EU 1995 5 19 95ZZZW704 119950421A331013730389K9 PANEL BAG JETSTMJETSTM3101 1500215EU LWR INST PANEL WATER CONTAM A VNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07853JS 730 FLT 4129 - DURING CLIMB-OUT CAPTAIN NOTICED SMOKE COMING FROM THE LOWER INTSTRUMENT PANEL. CREW ELECTED TO RETURN TO THE FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. SUBSEQUENT INVESTIGATION BY MAINTENANCE PERSONNEL REVEALED WATER UNDER LIGHT PANEL CAUSING SHORT CIRCUIT. FURTHER INVESTIGATION FAILED TO REVEAL SOURCE OF WATER. WATER WAS CLEANED FROM LIGHT PANEL AND AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950519006111995051900611WP 1995 5 19 95ZZZW705 119950403A5730 SKIN DOUG DC8 DC862 3021970WP WS 310.25 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE XFS 182.500. CORROSION FOUND IS BEYOND LIMIT. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER USING CLAD 7075-T6.071. PICKED UP EXISTING ATTACHMENT WHERE POSSIBLE. ALL WORK DONE PER EO NR ARW 950037-75/76. CORROSION FOUND WAS LEVEL II. (W) 2L74 4F 4A25 19950519006121995051900612WP 1995 5 19 95ZZZW706 119950403A5730 SKIN DOUG DC8 DC862 3021970WP WS 281.5-329 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE AT XFS 291.500 TO 329.00. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER USING CLAD 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DONE PER EO ARW 950037-75/76. CORROSION FOUND WAS LEVEL II. 2L74 4F 4A25 19950519006131995051900613WP 1995 5 19 95ZZZW707 119950403A5730 SKIN DOUG DC8 DC862 3021970WP WS 281.5-329 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RT LEADING EDGE AT XFS 291.500 TO 329. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER DOUBLER USING CLAD 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DONE PER EO ARW 950037-75/76. CORROSION FOUND WAS LEVEL II. (W) 2L74 4F 4A25 19950519006141995051900614WP 1995 5 19 95ZZZW708 119950405A5730 SKIN DOUG DC8 DC862 3021970WP WS 207.159 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSION. 2L74 4F 4A25 19950519006151995051900615WP 1995 5 19 95ZZZW709 119950405A5730 SKIN DOUG DC8 DC862 3021970WP WS 207.159 CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO1942086 46132 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSION. 2L74 4F 4A25 19950519006161995051900616EU 1995 5 19 95ZZZW710 119950417A3260848401 PROX SENSOR AIRBUS320 A320231 3930325EU LT MG DOOR MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28626AW 3246 65 DCA-CMH - AIR TURN BACK, DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT AFTER THREE ATTEMPTS. NO FAULTS OR MESSAGES APPEARED EXCEPT 'GEAR NOT UP'. AIRCRAFT RETURNED TO DCA AND LANDED WITHOUT FURTHER INCIDENT. LANDING WEIGHT GOOD. MX REMOVED AND REPLACED THE NR 1 LGCIU. GEAR SWING ACCOMPLISHED, NO FAULTS NOTED. MX ALSO REPLACED PROXIMTIY SENSOR 33GA AS A PRECAUTIONARY. AIRCRAFT RELEASED FOR SERVICE. REFERENCE AWXA9500232 . 2L72 4F RTA28NM 19950519006171995051900617EU 1995 5 19 AWXA9500232 119950417A3230664700500A4B LGCIU AIRBUS320 A320231 3930325EU LANDING GEAR FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28626AW 587M88M 65 DCA-CMH - AIR TURN BACK, DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT AFTER THREE ATTEMPTS. NO FAULTS OR MESSAGES APPEARED EXCEPT 'GEAR NOT UP'. AIRCRAFT RETURNED TO DCA AND LANDED WITHOUT FURTHER INCIDENT. LANDING WEIGHT GOOD. MX REMOVED AND REPLACED THE NR 1 LGCIU. GEAR SWING ACCOMPLISHED, NO FAULTS NOTED. MX ALSO REPLACED PROXIMTIY SENSOR 33GA AS A PRECAUTIONARY. AIRCRAFT RELEASED FOR SERVICE. REFERENCED 95ZZZW710. 2L72 4F RTA28NM 19950519006181995051900618NM 1995 5 19 AWXA9500254 119950518A2612106109639 FIRE LOOP BOEING737 737275 1384485NM APU MALFUNCTIONED A AWXAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING APAPPROACH 1 WP282FOR 20959 PHX-OMA - ON FINAL APPROACH CREW ATTEMPTED APU START AND APU FIRE WARNING ILLUMINATED. FIRE HANDLE PULLED AND WARNING SILENCED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER PROBLEMS. CONTRACT MAINTENANCE REMOVED APU SHROUD AND CONFIRMED NO EVIDENCE OF FIRE. UNMANNED STATION RELEASE WAS ISSUED AND AIRCRAFT CONTINUED IN SERVICE TO LAS. LAS MAINTENANCE PLACARDED APU INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LOWER FIRE LOOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950519006191995051900619 1995 5 19 AWXA9500255 419950502A3442M15851641 ANTENNA BOEING737 7372U9 1384498NM RADAR SYSTEM FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28149AW 1857 22575 FLT 1938 - CMH-LGA - AIR TURNBACK DUE TO COMPLETE RADAR FAILURE. ANTENNA LIGHT FLASHING, WORKS FOR 15 SECONDS THEN OFF FOR 2 TO 4 MINUTES. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. CMH MX REMOVED AND REPLACED RADAR ANTENNA, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950519006201995051900620EU 1995 5 19 AWXA9500256 119950501A3350321452 EEL PWR SUPPLY AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW 053 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT AT POSITION 4000VB. OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950519006211995051900621NE 1995 5 19 AWXA9500273 219950518A7200 ENGINE BOEING737 737275 1384485NM PWA JT8 JT8D9A 52048NE NR 1 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP282FOR 20922 P674296B PHX-IAH - AT ROTATION, THE WIND SHEAR ALERT CAME ON. PILOT ADVANCED THROTTLES. NR 1 ENG EGT WENT TO 640 DEGREES FOR APPROXIMATELY 5 SECONDS AND NR 2 ENG EGT WENT TO 620 DEGREES FOR APPROXIMATELY 5 SECONDS. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH OVER TEMP INSPECTION AND BORESCOPE OF NR 2 ENG AND FOUND NO EVIDENCE OF DISTRESS, ENG TO CONTINUE IN SERVICE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4F4 F A16WE E2EA 19950519006221995051900622NM 1995 5 19 AWXA9500274 119950509A5315 FLOOR BEAM BOEING737 7373G7 1384595NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND CORROSION ON FLOOR BEAM TOP CAP, BS 986.5 LBL 38. INSTALLED ANGLE REPAIR PER ER 3-53-16-25. (W) 2L72 4F RTA16WE 19950519006231995051900623NM 1995 5 19 AWXA9500275 119950509A5315 FLOOR BEAM BOEING737 7373G7 1384595NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED, BS 986.5 BL 0 TO RBL 16. REPAIRED WITH ANGLE REPAIR PER SRM 53-00-51. (W) 2L72 4F RTA16WE 19950519006241995051900624NM 1995 5 19 AWXA9500277 119950509A532065C807351 THRESHOLD BOEING737 7373G7 1384595NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND R2 DOOR THRESHOLD CHORD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CHORD PER SRM 51-10-02 AND SRM 51-40-02. (W) 2L72 4F RTA16WE 19950519006251995051900625NM 1995 5 19 AWXA9500278 119950509A5347 TRACK BOEING737 7373G7 1384595NM FS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 DURING C11 INSPECTION, FOUND SEAT TRACK CORRODED BEYOND LIMITS AT STATION 1016 RBL 45.5. FABRICATED NEW SECTION OF SEAT TRACK PER SRM 51-40-02. (W) 2L72 4F RTA16WE 19950519006261995051900626NM 1995 5 19 AWXA9500279 119950509A5320 WEB BOEING737 7373G7 1384595NM FS 847 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND WEB ON FRAME STATION 847 STRINGER 847 STR 25R DAMAGED. FABRICATED AND INSTALLED NEW WEB PER SRM 51-70-13. (W) 2L72 4F RTA16WE 19950519006271995051900627NM 1995 5 19 AWXA9500281 119950509A5330 SKIN BOEING737 7373G7 1384595NM AFT DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND A .5 INCH CRACK IN SKIN AT AFT GALLEY DOOR HINGE CUT OUT. REPAIRED PER ER 3-53-35-01. (W) 2L72 4F RTA16WE 19950519006281995051900628NM 1995 5 19 AWXA9500282 119950509A5320 WEB BOEING737 7373G7 1384595NM FS 947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND INNER WEB CRACKED AT STA 947 STRINGER 10R. FABRICATED NEW WEB AND INSTALLED PER SRM 51-40-02. (W) 2L72 4F RTA16WE 19950519006291995051900629EU 1995 5 19 GAIA955A 219950304A7260 ACCESS GEAR BOX CVAC 340 34031 2422704WP RROYCEDART DART5424 54522EU NR 1 ENGINE LEAKING A AGAIAAE UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SW07866TA194903421 283 FLT 123 - PILOT NOTED NR 1 ENGINE OIL PRESSURE DROPPING TWO PSI EVERY TEN MINUTES UNTIL OIL PRESSURE WARNING LIGHT ILLUMINATED AT 9 PSI, AT THIS TIME THE FLIGHT CREW SHUT DOWN NR 1 ENGINE AND FEATHERED AND PROPELLER USING EMERGENCY PROCEDURES, AND EMERGENCY WAS DECLARED WHICH DIVERTED THE AIRCRAFT TO (SDF) LOUISVILLE, KENTUCKY WHERE AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED TWO LOOSE NUTS ON ACCESSORY GEAR DRIVE. THE TWO NR 10 NUTS WERE TIGHTENED ENGINE RAN, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4R4 T 6A6 E5EU 19950519006311995051900631SW 1995 5 19 MALA954433 119950426A3260 SQUAT SW SWRNGNSA227 SA227AC 8780603SW LANDING GEAR MALFUNCTIONED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15425MA AC640 FLT 3017 - ON CLIMB-OUT FROM MKG, THE GEAR DOOR POSITION ANNUNCIATOR LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT RE-ILLUMINATED. THE LIGHT EXTINGUISHED WITH THE GEAR FULLY RETRACTED OR EXTENDED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY IN AIR AND GROUND MODES. AS A PRECAUTION, THE K-34 RELAY AND SQUAT SWITCH WERE REPLACED. THE SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950519006321995051900632NM 1995 5 19 MALA954440 119950503A27207G772 SWITCH DHAV DHC8 DHC8102 2809003NM RUDDER FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15829MA 335 FLT 3422 - ON CLIMB-OUT FROM LAF, THE NR 2 RUN HYD LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO LAF. MAINTENANCE REPLACED THE NR 2 RUDDER PRESSURE SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950519006331995051900633NM 1995 5 19 MALA954441 119950418A731210839 FUEL HEATER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT NACELLE FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15829MA 335 FLT 3339 - IN CRUISE FLIGHT TO ESC, THE FUEL TEMP INDICATION CLIMBED TO THE RED LINE. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REPLACED THE FUEL HEATER. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T4 TRTA13NM E20NE 19950519006341995051900634NM 1995 5 19 MALA954442 119950418A3040 WIPER BLADE DHAV DHC8 DHC8102 2809003NM RT WINDSHIELD DETACHED A MALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 GL15833MA 343 FLT 3177 - ON CLIMB-OUT FROM DTW, THE FIRST OFFICERS WIPER BLADE DETACHED FROM THE WINDSCREEN. THE AIRCRFT RETURNED TO DTW. MAINTENANCE RESECURED THE FIRST OFFICERS WIPER BLADE. SECURITY CHECK WAS SATISFACTORY. (W) 2H72 4T RTA13NM 19950519006351995051900635SW 1995 5 19 MALA954443 119950502A5210 SEAL SWRNGNSA227 SA227AC 8780603SW PAX DOOR FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL152692P AC658B FLT 3467 - ON CLIMB-OUT FROM DTW, THE AIRCRAFT WAS SLOW TO PRESSURIZE AND A SQUEALING NOISE WAS NOTED FROM THE PASSENGER DOOR SEAL. THE AIRCRAFT RETURNED TO DTW. THE SYSTEM IS CURRENTLY DEFERRED PER MEL 52-76. (W) 1L72 4T A8SW 19950519006361995051900636NM 1995 5 19 MALA954444 119950501A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15824MA 327 FLT NR 3320 - DURING THE PREFLIGHT INSPECTION IN DTW, THE CREW REPORTED THAT THE COCKPIT HAND HELD EMERGENCY LAMP ASSEMBLY HAD A LOW CHARGE. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LAMP ASSEMBLY. SYSTEM OPERERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950519006371995051900637CE 1995 5 19 PLGA418951 119950115A2750 RETRACT MECH BEECH 1900 1900C 1154161CE TE FLAPS MALFUNCTIONED A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05809BE UB40 BOS - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO LAND WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. FLAPS WERE SECURED IN THE 'FULL-UP' POSITION AND DEFERRED IAW WITH THE MEL. ACFT WAS RELEASED TO SERVICE.MAINTENANCE REPLACED THE BUSHINGS IN THE RIGHT HAND FLAP SPLIT LINKAGE IAW THE BEECHCRAFT MM AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTA24CE 19950519006381995051900638NE 1995 5 19 PLGA58951 319950508A6114660714200 HUB ASSY SAAB SF340 340B 7860101EU ROTOL R375 R3754123F21 NE LT ENGINE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05363BE 340B293 DRG126191 PROPELLER ASSY WAS REMOVED FROM THE AIRCRAFT LEFT SIDE FOR COMPLIANCE WITH AD 93-19-01. DURING THE DYE PENETRANT A CRACK WAS FOUND IN THE DOWEL HOLE BETWEEN NR 3 AND NR 4 BLADES. THE HUB WAS THEN REJECTED PER AD REQUIREMENTS AND ASSEMBLY WAS DISASSEMBLED FOR SHIPMENT. DURING DISASSEMBLY, A LARGE QUANTITY OF OIL WAS NOTED IN THE HUB AREA AND THE BUSHING FOR THE CROSSHEAD ON THE FORWARD HUB HALF WAS DISLODGED WHICH RESULETED IN EXCESSIVE MOVEMENT IN THE CROSSHEAD. HUB AND CROSSHEAD ASSEMBLIES WERE SHIPPED TO DOWTY AEROSPACE FOR REPAIR. THIS REPORT REMAINS OPEN PENDING TEARDOWN REPORT. 2L72 4T RTA52EU 6 CP17NE 19950519006391995051900639NM 1995 5 19 9508066611 119950516A275065B8112718 TRANSMISSION BOEING747 747251B 1384892NM TE FLAPS FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01611US4822229994 20356 DURING CLIMBOUT, THE OUTBOARD TRAILING EDGE FLAPS WOULD NOT RETRACT PAST 10 DEGREES IN NORMAL OR ALTERNATE POSITION. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 58,000 LBS OF FUEL, AND MADE AN UNEVENTFUL LANDING IN NRT. MAINTENANCE REPLACED SCREW ASSEMBLY AND NR 2 AND NR 7 TRANSMISSIONS. PERFORMED SYSTEM OPERATION AND CHECK WAS NORMAL. 2L74 4F A20WE 19950519006401995051900640WP 1995 5 19 9508079162 119950514A5350 GUIDE TUBE DOUG DC9 DC914 3022034WP TAILCONE OUT OF POSITION A NWAAK NONE O OTHER ININSP/MAINT 1 GL018907E 45748 DURING LINE CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP. FURTHER INVESTIGATION REVEALED THAT THE TURNBUCKLE WAS STICKING IN THE CABLE GUIDE TUBE (BETWEEN THE INNER AND OUTER HANDLE) PREVENTING THE UPPER LATCHES FROM COMPLETELY RELEASING. ALSO, FOUND 3 WORN GUIDE PINS AND A WORN UPPER LEFT LEVER ARM. REPOSITIONED THE GUIDE TUBE AND REPLACED THE PINS AND LEVER, CHECKED OK. 2L72 4F A6WE 19950519006411995051900641WP 1995 5 19 9508089880 119950515A5270 CONNECTOR DOUG DC9 DC951 3022051WP ACCESSORY DOOR CONTAMINATED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01675MC 47651 AFTER TAKEOFF ORD-DTW, THE FORWARD ACCESSORY COMPARTMENT DOOR WARNING LIGHT ILLUMINATED. RETURNED TO ORD WITHOUT FURTHER INCIDENT. THE WARNING LIGHT EXTINGUISHED ON LANDING AND REMAINED OUT DURING TAXI. CLEANED DOOR SWITCH CONNECTION AND RELAMPED ANNUNCIATOR AS PRECAUTIONARY. INDICATION AND DOOR LATCHING MECHANISM CHECKED OK. 2L72 4F A6WE 19950519006421995051900642NM 1995 5 19 95UAL747035 119950518A3350 EEL STRIP BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 EEL STRIP AT LAV 101 AND AT ROW 5 AND 6, ON THE RIGHT AISLE INOP. REPLACED JUMPER STRIP AT ROW 5. 2L74 4F4 FRTA20WE E24NE 19950519006431995051900643SO 1995 5 19 COM11891 119950515A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01162CA14579 120150 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED, DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT 1327-2 P/N 120-17059-015, 1 EA; 120-17056-007, 5 EA; 120-17056-015, 4 EA; 120-17056-017, 2 EA; 120-17056-019, 2 EA; 120-17057-007, 2 EA; 120-17057-006, 1 EA; 120-17056-013, 1 EA; 120-17057-015, 1 EA; 120-17057-005, 1 EA. 2L72 4T RTA31SO 19950519006441995051900644SO 1995 5 19 COM11892 119950516A5270 WARNING LIGHT EMB 120 EMB120RT SO CARGO DOOR ILLUMINATED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01269CA 120263 CARGO DOOR WARNING ILLUMINATED DURING TAKEOFF. DOOR WARNING SYSTEM DETERMINED TO BE AT FAULT. DEFERRED WARNING SYSTEM AND AIRCRAFT CONTINUED SERVICE. 2L72 4T RTA31SO 19950519006451995051900645 1995 5 19 COM11893 419950517A34256226190204 AHARS COMPUTER EMB 120 EMB120RT SO AVIONICS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01189CA3273 1598 120189 PILOTS AND COPILOTS YELLOW HEADING FLAGS. REPLACED THE NR 2 AHRS COMPUTER. 2L72 4T RTA31SO 19950519006461995051900646SO 1995 5 19 COM11894 119950517A275012042642001 SWITCH EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01266CA8278 120258 FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR CONTROL. 2L72 4T RTA31SO 19950519006471995051900647SO 1995 5 19 COM11895 119950517A7931310573501 REGULATOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01200CD 120200 115513 LEFT ENGINE SECURED DURING FLIGHT DUE TO LOW OIL PRESSURE. REPLACED THE OIL PRESSURE REGULATOR FITTING P/N 3112525-01, PULLED OUT OF REGULATOR HOUSING. PWC SB 21186 REPLACES THIS WITH IMPROVED P/N 3117892-01 FITTING. 2L72 4T4 TRTA31SO E20NE 19950519006481995051900648EU 1995 5 19 COM31080 119950516A3020NH2466881 INLET SAAB SF340 SF340A 7850100EU LT ENGINE CHIPPED A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA156313579 340A064 LEFT ENGINE INTAKE, ANTI-ICE COATING IS DAMAGED. REPLACED INLET. 2L72 4T RTA52EU 19950519006491995051900649EU 1995 5 19 COM31081 119950517A2731DL3827M137 ACTUATOR SAAB SF340 SF340A 7850100EU ELEVATOR TRIM DEFECTIVE A COMAK NONE F FLT CONT AFFECTED TOTAKEOFF 1 SO01370CA118227228 340A010 WITH TRIMS SET FOR TAKEOFF, THE AIRCRAFT REQUIRES EXCESSIVE BACK PRESSURE TO ROTATE. REPLACED THE ELEVATOR TRIM ACTUATOR. 2L72 4T RTA52EU 19950519006501995051900650EU 1995 5 19 COM31082 119950517A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01358CA10145413 FEB920250 340A047 MECHANIC REMOVED WHEEL FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950519006511995051900651EA 1995 5 19 COM60475 119950516A27604916403 SECU CNDAIRCL600 CL6002B19 EA NR 1/2 DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01917CA1791 17 7017 FLIGHT SPOILERS FAULT MESSAGE ON EICAS. REPLACED THE NR 1 AND 2 SECU. 2L72 4F RTA21EA 19950519006521995051900652NM 1995 5 19 DHL95720002 119950514A3010BACC10DU350AB CLAMP BOEING727 727228 NM NR 1 ENGINE LOOSE A TDHLAAJ UNSCHED LANDING DUMP FUEL JM WARNING INDICATION OVER TEMP CLCLIMB 1 SO01720DH 19544 ON CLIMBOUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED. ACCOMPLISHED ENGINE STRUT OVERHEAT AND FUEL DUMP CHECKLIST. AIR TURNBACK, LANDED WITHOUT INCIDENT. OPENED STRUT, FOUND WING ANTI-ICE VALVE UPPER FLANGE LOOSE, TIGHTENED SAME. RAN ENGINE AT TAKEOFF POWER, COULD NOT DUPLICATE. REINSTALLED ACCESS PANELS AND TOOK UP TO TAKEOFF POWER AGAIN, STILL COULD NOT DUPLICATE. WORK PER M/M 30-13-00. 2L73 4F A3WE 19950519006531995051900653WP 1995 5 19 SCNA95097 119950512A3350141111001 EEL BATTERIES DOUG DC10 DC1010 3022110WP L1 DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 L1 DOOR, PRESS TO TEST SLIDE SWITCH INOPERATIVE. FOUND C-CELL BATTERIES INOPERATIVE, REMOVED AND REPLACED BATTERIES AND OPS CHECKED GOOD. 2L73 4F A22WE 19950519006541995051900654NM 1995 5 19 SWAA950381 119950516A532035479576 WEB BOEING737 7373Q8 1384670NM BS 822/860 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND UPPER FLANGE OF VERTICAL SUPPORT WEB CORRODED AT BS 822 AND AT 860, RBL22, WL 154. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950519006551995051900655NM 1995 5 19 SWAA950382 119950516A5320BAC14902807 CHORD BOEING737 7373Q8 1384670NM BS 847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FAILSAFE CHORD CORRODED AT BS 847, BL 0, WL 148. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950519006561995051900656NM 1995 5 19 SWAA950383 119950516A53302024T3 SKIN BOEING737 7373Q8 1384670NM BS 300-312 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND 12 FUSELAGE SKIN DENT AT BS 300 TO 312, S20R. INSTALLED REPAIR PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950519006571995051900657NM 1995 5 19 SWAA950384 119950516A5320 SHEAR TIE BOEING737 7373Q8 1384670NM BS 727D GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE GOUGED AT BS 727D, BETWEEN S19 TO 20R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950519006581995051900658NM 1995 5 19 SWAA950385 119950512A2750 CONNECTOR BOEING737 7373H4 1384600NM RRT TE FLAP CORRODED A SWAAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 SW07351SW 24572 DURING CLIMBOUT, FLAPS REMAINED AT FIVE DEGREES. AIRCRAFT RETURNED TO SLC AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND RIGHT FLAP POSITION TRANSMITTER CANNON PLUG CORRODED. CLEANED PLUG AND OPERATED FLAPS THROUGH ALL SETTINGS, OK PER BOEING MAINTENANCE MANUAL. 2L72 4F RTA16WE 19950519006591995051900659NM 1995 5 19 SWAA950386 119950514A27512061141 INDICATOR BOEING737 7373H4 1384600NM TE FLAPS INOP A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07351SW 24572 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT PAST 5 DEGREES, EXTENDED FLAPS NORMALLY. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED FLAP POSITION INDICATOR PER BOEING MAINTENANCE MANUAL. 2L72 4F RTA16WE 19950519006601995051900660NM 1995 5 19 SWAA950387 119950513A5320 DOOR FRAME BOEING737 7372T4 1384492NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER END AT BS 294.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950519006611995051900661NM 1995 5 19 SWAA950388 119950516A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED IN FWD FLANGE RADIUS, BS 520, LBL 45.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950519006621995051900662NM 1995 5 19 SWAA950389 119950516A5320 DOORWAY BOEING737 7372T4 1384492NM AFT GALLEY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB CRACKED BELOW DOOR ASSIST HANDLE. REPAIRED PER SWA ACO 471-53. 2L72 4F A16WE 19950519006631995051900663NM 1995 5 19 SWAA950390 119950516A5330 SKIN BOEING737 7372T4 1384492NM BS 500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT SCANNING LIGHT CUTOUT, BS 500B AT S16L AND AT BS 500B PLUS 13.5. REPAIRED PER SWA ACO 6405-53. 2L72 4F A16WE 19950519006641995051900664NM 1995 5 19 SWAA950391 119950516A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0724SW 20925 FOUND PRESSURE BULKHEAD CRACKED AT BS 727, AFT WALL OF WHEEL WELL. REPAIRED PER SWA RA 253-1194. 2L72 4F A16WE 19950519006651995051900665NM 1995 5 19 SWAA950392 119950516A5311 FRAME BOEING737 7373Q8 1384670NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07663SW 23256 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, WL 160, RBL 24. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950519006661995051900666NM 1995 5 19 UPS203265 119950517A5754 SKIN BOEING727 727247 138408FNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01212UP 21392 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP, JUST ABOVE THE DATA PLATE. INSTALLED REPAIR PER UPS EO FILE NR B727-57-1361. 2L73 4F A3WE 19950519006671995051900667NM 1995 5 19 UPS203266 119950517A5754 ATTACH RIB BOEING727 727247 138408FNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01212UP 21392 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 6 SLAT ACTUATOR ATTACH RIB, O/B SIDE. REPLACED RIB PER SRM 51-30-2, MM 27-81-32. 2L73 4F A3WE 19950519006681995051900668NM 1995 5 19 UPS203267 119950517A5753 TE WEDGE BOEING727 727247 138408FNM LT TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01212UP 21392 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON T/E WEDGE, LT WING I/B IN FLAP. INSTALLED REPAIR PER SRM 51-30-2. 2L73 4F A3WE 19950519006691995051900669NM 1995 5 19 UPS403268 119950517A5320 DOUBLER BOEING747 747121 1384871NM FS 1180-1200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WINDOW DOUBLER, STA 1180 TO 1200, STRINGER 14R. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0715. 2L74 4F A20WE 19950519006701995051900670NM 1995 5 19 UPS403269 119950517A5320 DOUBLER BOEING747 747121 1384871NM RT MLG WW CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT BS 1241, CANTED PRESSURE DECK WEB AND DOUBLER, RT WHEEL WELL, RBL 20, BEHIND SPOILER MIXER. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0713. 2L74 4F A20WE 19950519006711995051900671NM 1995 5 19 UPS403270 119950517A5320 WEB BOEING747 747121 1384871NM BS 1240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON WEB AT BS 1240, LBL 105. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-02. 2L74 4F A20WE 19950519006721995051900672NM 1995 5 19 UPS403271 119950517A5347 SEAT TRACK BOEING747 747121 1384871NM BS 810 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK, BS 810, LBL 76. REPLACED SEAT TRACK PER SRM 53-10-05. 2L74 4F A20WE 19950519006731995051900673NM 1995 5 19 UPS403272 119950517A5315 FLOORBEAM BOEING747 747121 1384871NM BS 76-90 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION FLOORBEAM, STA 866, BETWEEN LBL 76 TO 90, UNDER SIDE OF UPPER CHORD. INSTALLED REPAIR PER UPS EO 51-40-04. 2L74 4F A20WE 19950519006741995051900674WP 1995 5 19 UPS803277 119950513A2910 HYD LINE DOUG DC8 DC871F 302199DWP RUDDER CHAFED A IPXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01729UP 46029 (SUPPLEMENTAL MRR) PILOT REPORTED DURING CLIMBOUT, EXPERIENCED LOSS OF HYD FLUID. FLUID QTY DOWN TO APPROX 6 GALLONS WHEN QRH PROCEDURE COMPLETED. FLUID LEVEL ROSE TO APPROX 7 GALLONS. EMERGENCY PROCEDURES ACCOMPLISHED. ITEM DEFERRED WITH TEMP FLEX HOSE INSTALLED. TEMP FLEX HOSE REPLACED. LK CK OK. 2L74 4F RT4A25 19950519006881995051900688CE 1995 5 19 95ZZZX2410 119950411A2140 HEATER JANITROL G93A22 BEECH 18 E18S9700 1151008CE FUSE CIRCUIT MISINSTALLED A ALEAAK NONE M OVER TEMP ININSP/MAINT 1 GL179669N 118861 BA382 ACFT HEATER INOP. INSP OF HEATER, LOCATED IN RT WING, REVEALED IT HAD OVERHEATED. HEATER HOT ENOUGH TO CAUSE DISTORTION OF WING RIB ADJ TO HEATER & WRINKLE WING SKIN ABOVE HEATER. HEATER REMOVED & SENT TO OVERHAUL SHOP WHERE NO DEFECTS FND. SUSPECTED CAUSE OF HEATER OVERHEAT WAS OPERATION OF HEATER WITH A FOAM 'BIRD BUNG' INSTALLED IN AIR INTAKE. THIS WOULD NOT ALLOW AIR PASSAGE OVER HEATER CAUSING IT TO OVERHEAT. ACFT HEATER SYSTEM DOES HAVE OVERHEAT FUSE LOCATED FWD FUSE BELOW COCKPIT FLOOR THAT WILL SHUT DOWN HEATER TO PREVENT DAMAGE. INSP OF ACFT OVERHEAT SYS REVEALED HEATER OVERHEAT FUSE BLK INCORRECTLY INSTALLED. FUSE HOLDER NOT ORIGINAL EQUIP & WIRE H9-18 (FIG 7-27-3 OF MM). NOT CONNECTED. 1L72 3R A765 19950519006891995051900689CE 1995 5 19 95ZZZX2411 119950411A2140 HEATER JANITROL G93A22 BEECH 18 E18S9700 1151008CE OVERHEAT PROBE WRONG FUSE A ALEAAK NONE O OTHER ININSP/MAINT 1 GL178711H BA87 HEATER INSPECTION REVEALED OVERHEAT FUSE WAS OF THE CORRECT AMPERAGE, BUT WAS OF THE TIME DELAY (SLOW BLOW) TYPE FUSE. HEAT WAS APPLIED TO THE OVERHEAT PROBE AND 45 SECONDS AFTER ACTUATION OF THE PROBE, THE FUSE HAD NOT BLOWN. THE FUSE WAS REPLACED WITH THE CORRECT QUICK ACTING TYPE AND IT BLEW AFTER APPROXIMATELY 10 SECONDS OF PROBE ACTUATION. 1L72 3R A765 19950519006901995051900690CE 1995 5 19 95ZZZX2412 119950411A2140 RESISTOR JANITROL G93A22 BEECH 18 E18S9700 1151008CE OVERHEAT PROBE OPEN A ALEAAK NONE O OTHER ININSP/MAINT 1 GL178627A BA283 HEATER INSPECTION REVEALED THE CORRECT TYPE OF FUSE WAS INSTALLED. ACTUATION OF THE OVERHEAT PROBE FAILED TO BLOW THE FUSE. FURTHER INSPECTION REVEALED THAT THE 3 OHM 10 WATT RESISTOR, LOCATED IN THE WIRING BETWEEN THE OVERHEAT PROBE AND THE FUSE, WAS 'OPEN'. THE RESISTOR WAS REPLACED AND THE SYSTEM FUNCTION TESTED SATISFACTORY. 1L72 3R A765 19950519007051995051900705NM 1995 5 19 ASAA9510020 119950328A5210507945155 HANDLE BOEING737 737210C 1384459NM L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01744AS 21822 ANC - FLT 50 - DIFFICULT TO GET L1 DOOR HANDLE ALL THE WAY CLOSED. LUBED HANDLE ASSEMBLY AND OVER MECHANISM, DOOR OPERATED NORMALLY. (Z) 2L72 4F A16WE 19950519007061995051900706NM 1995 5 19 ASAA9510022 119950403A521065867841 ARM BOEING737 737210C 1384459NM L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01744AS 21822 ANC - FLT 112 - DIFFICULT TO GET L-1 DOOR HANDLE ALL THE WAY CLOSED. ADJUSTED UPPER LOCKING ARM AND DOOR OPERATED NORMALLY. (Z) 2L72 4F A16WE 19950519007071995051900707NM 1995 5 19 ASAA9510026 119950404A5315 FLOORBEAM BOEING737 737290C 138448VNM BS259 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE HORIZONTAL FLANGE AT LBL 6.2 AND RBL 6.2 OF THE UPPER ANGLE CHORD OF THE FLOORBEAM AT BS 259 BETWEEN RBL 10 AND LBL 10. REMOVED CORROSION PER EA 5310-01348 AND BOEING TELEX ASA-SEA-95-0224RR. (Z) 2L72 4F A16WE 19950519007081995051900708NM 1995 5 19 ASAA9510028 119950407A531565549062 FLOORBEAM BOEING737 737290C 138448VNM BS 500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE UPPER FWD AND AFT FLANGE OF FLOORBEAM BS 500A, RBL 9 TO RBL 42. REPAIRED PER EA 5310-01352 AND BOEING TELEX ASA-SEA-95-0196RR. (Z) 2L72 4F A16WE 19950519007091995051900709NM 1995 5 19 ASAA9510029 119950407A531565549072 FLOORBEAM BOEING737 737290C 138448VNM BS 747 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LOWER FWD FLANGE BETWEEN RBL 24.5 AND RBL 44.5 OF FLOORBEAM BS 747. REPAIRED PER EA 5310-01339 AND BOEING TELEX ASA-SEA-95-0186RR. (Z) 2L72 4F A16WE 19950519007101995051900710NM 1995 5 19 ASAA9510030 119950407A531565549073 FLOORBEAM BOEING737 737290C 138448VNM BS 767 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE UPPER FWD AND AFT FLANGE OF FLOORBEAM 767, RBL 24 TO RBL 45. REPAIRED PER EA 5310-01349 AND BOEING TELEX ASA-SEA-95-0197RR. (Z) 2L72 4F A16WE 19950519007111995051900711NM 1995 5 19 ASAA9510033 119950412A531565549054 FLOORBEAM BOEING737 737290C 138448VNM BS 460 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LOWER CHORD FWD FLANGE OF THE FLOORBEAM AT BS 460 BETWEEN LBL 10 AND LBL 31. REPAIRED PER EA 5310-01344 AND BOEING TELEX ASA-SEA-95-0179RR. (Z) 2L72 4F A16WE 19950519007121995051900712NM 1995 5 19 ASAA9510034 119950412A53206562107505 SILL WEB BOEING737 737290C 138448VNM FS 364 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, THE LOWER SILL WEB WAS REMOVED AND FOUR RIVETS COMMON TO THE FITTING AND WEB COULD NOT BE RE-INSTALLED WITHOUT TAKING THE LATCH SUPPORT FITTING OUT. REPAIRED AND REPLACED MAIN CARGO DOOR SILL WEB PER EA 5310-01350 AND BOEING TELEX ASA-SEA-95-0217RR. (Z) 2L72 4F A16WE 19950519007131995051900713NM 1995 5 19 ASAA9510035 119950414A531565549072 FLOORBEAM BOEING737 737290C 138448VNM FS 747 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD FWD FLANGE AT RBL 31.75 ON THE FLOORBEAM AT BS 747. REPAIRED PER EA 5310-01356 AND BOEING TELEX ASA-SEA-95-0249RR. (Z) 2L72 4F A16WE 19950519007141995051900714NM 1995 5 19 ASAA9510036 119950414A335086210144 EEL BATT PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' EMERGENCY LIGHTS WERE FOUND TO BE DIM. REPLACED BATTERY PACK ON SMOKE BARRIER AND LIGHTS OPERATED NORMALLY. (Z) 2L72 4F A16WE 19950519007151995051900715NM 1995 5 19 ASAA9510037 119950414A33508821004 EEL BATT PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 7 TO 10 WOULD NOT EXTINGUISH. REPLACED BATTERY PACK TO RECEIVER AND LIGHTS OPERATED NORMALLY. (Z) 2L72 4F A16WE 19950519007161995051900716NM 1995 5 19 ASAA9510038 119950415A21215007024620 GASPER FAN BOEING737 737210C 1384459NM COCKPIT OVERHEATED A ASAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 NM01743AS 21821 ANC - FLT 893 - CREW REPORTED AN ACRID ODOR ASSOCIATED WITH BURNING ELECTRICAL WIRING APPEARED IN THE COCKPIT DURING DESCENT AND A SMALL AMOUNT OF SMOKE FOLLOWED. GASPER FAN CIRCUIT BREAKER TRIPPED AND THE SMOKE AND ODOR LESSENED. LANDED WITHOUT INCIDENT. REPLACED INOPERATIVE GASPER FAN AND OPERATED NORMALLY WITH NO EVIDENCE OF SMOKE OR ODOR. (Z) 2L72 4F A16WE 19950519007171995051900717NM 1995 5 19 ASAA9510039 119950416A5510 ATTACH LUGS BOEING737 737290C 138448VNM HORIZ STAB CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FACES AND IN THE INTERNAL DIAMETER OF THE HORIZONTAL STABILIZER ATTACHMENT LUGS. REPAIRED PER EA 5510-01029 AND BOEING SB 737-55-1055. (Z) 2L72 4F A16WE 19950519007181995051900718NM 1995 5 19 ASAA9510040 119950415A531565549073 FLOORBEAM BOEING737 737290C 138448VNM FS 787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LOWER FWD FLANGE AT BS 787, LBL 3 TO LBL 50. REPAIRED PER EA 5310-01351 AND BOEING TELEX ASA-SEA-95-0210RR. (Z) 2L72 4F A16WE 19950519007191995051900719NM 1995 5 19 ASAA9510041 119950415A531565549055 FLOORBEAM BOEING737 737290C 138448VNM FS 500 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LOWER FWD AND AFT FLANGE, CONCENTRATED IN THE FASTENER HOLES AT BS 500, BL 0.0 TO LBL 50. REPAIRED PER EA 5310-01342 AND BOEING TELEX ASA-SEA-95-0223RR. (Z) 2L72 4F A16WE 19950519007201995051900720NM 1995 5 19 ASAA9510042 119950417A531565549081 FLOORBEAM BOEING737 737290C 138448VNM BS 787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE LOWER FWD FLANGE AT BS 787, RBL 3 TO RBL 58.5. REPAIRED PER EA 5310-01335 AND BOEING TELEX ASA-SEA-95-0187RR. (Z) 2L72 4F A16WE 19950519007211995051900721NM 1995 5 19 ASAA9510043 119950417A3350900835A EEL BATT PACK BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 15 WERE FOUND INOPERATIVE. RELAMPED ONE LIGHT AND RELEASED THE REMAINING LIGHT PER MEL 33-19. SUBSEQUENTLY RELAMPED BATTERY PACK AT ROW 15 AND LIGHTS OPERATED NORMALLY. REMOVED PLACARD. (Z) 2L72 4F A16WE 19950519007221995051900722NM 1995 5 19 ASAA9510044 119950418A531565549011 FLOORBEAM BOEING737 737290C 138448VNM BS 947 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FLOORBEAM TOP FLANGE AT BS 947, LBL 24 TO LBL 56. REPAIRED PER EA 5310-0146 AND BOEING TELEX ASA-SEA-95-0230RR. (Z) 2L72 4F A16WE 19950519007231995051900723NM 1995 5 19 ASAA9510045 119950421A531565549052 FLOORBEAM BOEING737 737290C 138448VNM BS 420 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, CORROSION WAS FOUND ON THE FWD LOWER FLANGE OF THE FLOORBEAM AT BS 420 LBL 6 TO LBL 39. REPAIRED PER EA 5310-01338 AND BOEING TELEX ASA-SEA-95-0274RR. (Z) 2L72 4F A16WE 19950519007241995051900724NM 1995 5 19 ASAA9540016 119950415A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - PILOT REPORTED, AFT TWO EMERGENCY TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. (Z) 2L72 4F RTA16WE 19950519007251995051900725NM 1995 5 19 ASAA9540017 119950415A33501619 EEL LAMP BOEING737 7374Q8 NM CABIN INOP A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - CHECK, ROW 25ABC OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. (Z) 2L72 4F RTA16WE 19950519007261995051900726NM 1995 5 19 ASAA9540018 119950416A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 ANC - CHECK, 4 AFT TRACK LIGHTS INOP. MAINTENANCE SECURED WIRING AND OPS CHECKED OK. (Z) 2L72 4F RTA16WE 19950519007271995051900727WP 1995 5 19 ASAA9580074 119950413A3350D29984103 EEL DOUG DC9 DC983 3022083WP TAILCONE FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS 53449 OAK - DURING C-CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST, CURRENT LOW. REPLACED THE EVACUATION SLIDE WITH A SERVICEABLE UNIT. (Z) 2L72 4F RTA6WE 19950519007281995051900728SO 1995 5 19 C2XA95IA073 119950511A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING O/B CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 16 NR 2 UPPER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, ACFT APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950519007291995051900729SO 1995 5 19 C2XA95IA074 119950511A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 15 AFT LOWER SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, ACFT APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950526000011995052600001WP 1995 5 26 ABXA9500422 119950501A5330591140659 SKIN DOUG DC9 DC933F 302207AWP FWD FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, A PREVIOUSLY INSTALLED DOUBLE STACK REPAIR WAS REMOVED FROM THE LOWER AFT CORNER OF THE FORWARD ENTRY DOOR CUTOUT ON THE FUSELAGE SKIN. THE REPAIR HAD BEEN CLASSIFIED AS TEMPORARY. REPAIRED SKIN IAW ABX REA D953-11400-MR. 2L72 4F A6WE 19950526000021995052600002WP 1995 5 26 ABXA9500423 119950426A5330592032339 SKIN DOUG DC9 DC933F 302207AWP FS 367-341 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, A CREASE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE FORWARD LOWER CARGO DOOR, BETWEEN LONGERONS 26R AND 25R. THE CREASE SPANNED FROM STATIONS 367 TO 341. REPAIRED THE SKIN IAW ABX REA D953-11408-MR. 2L72 4F A6WE 19950526000031995052600003WP 1995 5 26 ABXA9500424 119950427A57305910466 SKIN DOUG DC9 DC933F 302207AWP WS 20 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING UPPER SKIN AT XCW 20. REPAIRED IAW ABX REA D957-11411-MR. 2L72 4F A6WE 19950526000041995052600004WP 1995 5 26 ABXA9500425 119950428A533059248034 SKIN DOUG DC9 DC933F 302207AWP FS 718 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO HAVE A DOUBLE DRILLED HOLE JUST FORWARD OF STA 718R AT CUSP. REPAIRED SKIN IAW ABX REA D953-11414-MR. 2L72 4F A6WE 19950526000051995052600005WP 1995 5 26 ABXA9500426 119950414A53159958190501 BEAM DOUG DC9 DC933F 302207AWP FS 737 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON A FLOORBEAM AT STA 737R RBL 44. REPAIRED BEAM IAW ABX REA D953-11422-MR. 2L72 4F A6WE 19950526000061995052600006WP 1995 5 26 ABXA9500427 119950421A5315995821225 FLOORBEAM DOUG DC9 DC933F 302207AWP FS 756-737 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH TEE AT STA 756, FROM APPROXIMATELY X EQUALS -18 TO OUTBOARD END. REPAIRED IAW ABX REA D953-11425-MR. 2L72 4F A6WE 19950526000071995052600007WP 1995 5 26 ABXA9500428 119950417A53309910155105 PANEL DOUG DC9 DC933F 302207AWP FS 751 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE UPPER SIDE OF THE PRESSURE PANEL AT X EQUALS A D953-11427-MR. 2L72 4F A6WE 19950526000081995052600008WP 1995 5 26 ABXA9500429 119950501A531199115126 FRAME DOUG DC9 DC933F 302207AWP FS 134 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FUSELAGE FRAME AT STATION 134 BETWEEN LONGERONS 24R AND 25R. REPAIRED FRAME IAW ABX REA D953-11505-MR. 2L72 4F A6WE 19950526000091995052600009WP 1995 5 26 ABXA9500430 119950506A53115911448521 FRAME DOUG DC9 DC933F 302207AWP FS 503 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE ROLLED ZEE FRAME AT STA 530 ON THE UPPER FLANGE AT LONGERON 30. REPAIRED FRAME IAW ABX REA D953-11525-MR. 2L72 4F A6WE 19950526000101995052600010WP 1995 5 26 ABXA9500431 119950425A532199578273 FLOOR PANEL DOUG DC9 DC933F 302207AWP COCKPIT CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE COCKPIT CENTER FLOOR PANEL. REPLACED THE PANEL IAW DC-9 SRM 51-30-2, 51-30-1. 2L72 4F A6WE 19950526000111995052600011WP 1995 5 26 ABXA9500432 119950427A532059197416 INTERCOSTAL DOUG DC9 DC933F 302207AWP FS 503-522 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 503 LONGERON 19R. REPLACED IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526000121995052600012WP 1995 5 26 ABXA9500433 119950424A532039258141 SUPPORT DOUG DC9 DC933F 302207AWP FS 598 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, A MAIN FLOOR SUPPORT WAS FOUND CRACKED AT STA 598 LBL 36. REPLACED IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526000131995052600013WP 1995 5 26 ABXA9500434 119950427A532049128172 FITTING DOUG DC9 DC933F 302207AWP FS 370 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, A BATHTUB FITTING WAS FOUND CRACKED AT STA 370 LONGERON 22R. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526000141995052600014WP 1995 5 26 ABXA9500435 119950422A53135920319508 LONGERON DOUG DC9 DC933F 302207AWP FS 375-579 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 415. REPLACED LONGERON IAW DC-9 SRM 51-30-5, 51-30-7 AND 51-30-1. 2L72 4F A6WE 19950526000151995052600015WP 1995 5 26 ABXA9500436 119950424A53203920595501 FITTING DOUG DC9 DC933F 302207AWP FS 566 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND LONGERON 28R END FITTING CRACKED AT STA 566. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950526000161995052600016WP 1995 5 26 ABXA9500437 119950420A53135920319508 LONGERON DOUG DC9 DC933F 302207AWP FS 475-579 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 579. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526000171995052600017WP 1995 5 26 ABXA9500438 119950422A532039132091 FITTING DOUG DC9 DC933F 302207AWP FS 583 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, FOUND LONGERON 29L END FITTING CRACKED AT STA 583. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 19950526000181995052600018WP 1995 5 26 ABXA9500439 119950411A276039545571 LINK DOUG DC9 DC933F 302207AWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED IAW DC-9 SUPP MM 27-61-1. 2L72 4F A6WE 19950526000191995052600019WP 1995 5 26 ABXA9500440 119950413A27603954557 LINK DOUG DC9 DC933F 302207AWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE LEFT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 27-61-1. 2L72 4F A6WE 19950526000201995052600020WP 1995 5 26 ABXA9500441 119950413A27603954558501 FITTING DOUG DC9 DC933F 302207AWP RT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER AFT ATTACH FITTING CRACKED. REPLACED THE FITTING IAW DC-9 MM 27-61-1. 2L72 4F A6WE 19950526000211995052600021WP 1995 5 26 ABXA9500442 119950415A276039545571 LINK DOUG DC9 DC933F 302207AWP RT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING INBOARD SPOILER DRIVE LINK CRACKED. REPLACED LINK IAW DC-9 MM 27-61-1. 2L72 4F A6WE 19950526000221995052600022WP 1995 5 26 ABXA9500443 119950413A27603923251501 LINK DOUG DC9 DC933F 302207AWP RT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23933AX 47291 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 85-01-03, FOUND THE RIGHT WING OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED THE LINK IAW DC-9 MM 27-61-1. 2L72 4F A6WE 19950526000231995052600023WP 1995 5 26 ABXA9500445 119950503A53305911408125 SKIN DOUG DC9 DC932 3022066WP FS 256 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 94-03-01, FOUND LEVEL I CORROSION ON FUSELAGE SKIN AT FORWARD ADF ANTENNA. REPAIRED IAW DC-9 SRM 53-04. 2L72 4F A6WE 19950526000241995052600024WP 1995 5 26 ABXA9500446 119950426A57133911240504 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING STRINGER NR 17 AT XCW 58. REPAIRED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950526000251995052600025WP 1995 5 26 ABXA9500447 119950422A571339112362 STRINGER DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING STRINGER NR 12 AT XCW 58. REPAIRED IAW DC-9 SB 57-98. 2L72 4F A6WE 19950526000261995052600026WP 1995 5 26 ABXA9500448 119950426A572099193692 T CAP DOUG DC9 DC932 3022066WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT LOWER T-CAP BETWEEN STRINGERS 11 TO 12, 12 TO 13, 13 TO 14 AND 14 TO 15. REPAIRED IAW DC-9 SRM 51-22-1 AND DC-9 SB 57-98. 2L72 4F A6WE 19950526000271995052600027WP 1995 5 26 ABXA9500449 119950429A531159135955 FRAME DOUG DC9 DC932 3022066WP FS 1079 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, FOUND FRAME 1079 CRACKED AT LONGERON 19L. REPAIRED IAW ABX REA D953-11507-MR.` 2L72 4F A6WE 19950526000281995052600028WP 1995 5 26 ABXA9500450 119950430A533059114065 SKIN DOUG DC9 DC932 3022066WP FS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, FOUND SCREWS IN BARREL NUTS NOT SEATED PROPERLY AROUND REPAIR AT FORWARD UPPER CORNER OF ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-11476-MR. 2L72 4F A6WE 19950526000291995052600029WP 1995 5 26 ABXA9500451 119950423A531199196431 FRAME DOUG DC9 DC932 3022066WP FS 639 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION, FOUND FRAME STA 639, CRACKED AT AFT OUTBOARD FLANGE BETWEEN LONGERON 15L AND 16L. REPAIRED IAW ABX REA D953-11469-MR. 2L72 4F A6WE 19950526000301995052600030WP 1995 5 26 ABXA9500452 119950517A56105714863505 TRACK DOUG DC9 DC931 3022065WP CAPT WINDOW LACK OF LUBE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 CAPTAIN'S CLEARVIEW WINDOW HARD TO SLIDE. LUBED WINDOW TRACK. OPS CHECKED GOOD IAW DC-9 M.M. 2L72 4F A6WE 19950526000311995052600031WP 1995 5 26 ABXA9500453 119950518A561036412431 LOCK DOUG DC9 DC931 3022065WP CAPT WINDOW OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47072 DURING POST FLIGHT INSPECTION FOUND CAPTAIN'S SLIDING WINDOW HARD TO OPEN. ADJUSTED UPPER LOCK. OPS CHECKED SEVERAL TIMES. OPS CHECKED GOOD IAW DC-9 M.M. 2L72 4F A6WE 19950526000321995052600032WP 1995 5 26 ABXA9500454 119950517A78307614033769 LINE DOUG DC8 DC863 302198AWP LT TR UNIT RUPTURED A ABXAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 GL23815AX 46097 DURING ROLLOUT, THE THRUST REVERSER SYSTEM HYDRAULIC RETURN LINE RUPTURED. DEFERRED AND DEACTIVATED THE T/R SYSTEM. INSPECTED AND PREPARED AIRCRAFT FOR FERRY FLIGHT TO ILN, AT ILN, THE HYDRAULIC LINE WAS REPLACED. SYSTEM OPERATIONALLY AND LEAKED CHECKED GOOD IAW DC-8 MM CHAPTER 78 AND 29. 2L74 4F 4A25 19950526000331995052600033 1995 5 26 DHL95720003 419950516A22102588880901 COUPLER BOEING727 727228 NM YAW DAMPER FAILED A TDHLAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01720DH 19544 ON CLIMBOUT, HAD UNCOMMANDED RUDDER INPUTS. PERFORMED AIR TURN BACK, LANDED WITHOUT INCIDENT. FOUND UPPER RUDDER PULSATING IN BOTH DIRECTIONS FROM NEUTRAL. TURNED OFF UPPER YAW DAMPER, PULSATING STOPPED. DEFERRED SYSTEM PER MEL 22-6. UPON LANDING AT CVG, REPLACED YAW DAMPER COUPLER PER BOEING M/M 22-10-0. 2L73 4F A3WE 19950526000341995052600034NM 1995 5 26 DL72E952164 119950517A2612894120 FIRE LOOP BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE SHORTED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11830WA 21482 700445 AFTER TAKOFF, NR 3 ENGINE B FAULT DETECTOR LIGHT CAME ON. COMPLIED WITH POM, APPROXIMATELY 15 MINUTES LATER B-LOOP ILLUMINATED, SHUTDOWN ENGINE AND DISCHARGED BOTH BOTTLES. INDICATION REMAINED UNTIL SHUTDOWN AT GATE. FOUND LOWER FIRE DETECTOR LOOP SHORTED. REPLACED LOOP ASSEMBLY AND BOTTLES. 2L73 4F4 F A3WE E2EA 19950526000351995052600035NM 1995 5 26 DL72S951929 119950508A5311 FRAME BOEING727 727232 1384082NM BS 804 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FRAME TO STRINGER ATTACH ANGLE FOUND CRACKED AT FS BS 804 STR 14L. REPAIRED PER SRM 53-10-4 PG 87 TO 89. 2L73 4F A3WE 19950526000361995052600036NM 1995 5 26 DL72S952149 119950515A5330 SKIN BOEING727 727232 1384082NM FWD BAG BIN DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 WIND BLEW BAG CART INTO A/C FWD OF LT WING. REMOVED FWD BAG BIN SIDEWALL PANELS AT STA 720A, FABRICATED AND PAINTED REPAIR DOUBLER AND STRINGER SPLICE INSTALLED. COMPLETED REPAIR PER SRM 53-30-3 AND 53-10-3. 2L73 4F A3WE 19950526000371995052600037NM 1995 5 26 DL72S952162 119950515A56105717623134 WINDOW 91213H5464 BOEING727 727232 1384082NM FLIGHT DECK SMOKING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11401DA 6110 21145 CLIMBING THROUGH FL 320, HAD VISIBLE SMOKE AND FUMES COMING FROM CONDUIT BETWEEN R-2 AND R-3 COCKPIT WINDOWS ON F/O SIDE. SMOKE CLEARED WHEN WINDOW HEAT TURNED OFF. REPLACED R-2 WINDOW AND CONTROLLER. 2L73 4F A3WE 19950526000381995052600038NM 1995 5 26 DL72S952165 119950510A711065196854540 NOSE COWL BOEING727 727232 1384082NM NR 3 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 000 UPON MAINT INSPECTION, A CRACK WAS FOUND IN OUTER SKIN OF NR 3 ENGINE NOSE COWL. REPAIRED PER SRM 54-30-3. 2L73 4F A3WE 19950526000391995052600039NM 1995 5 26 DL72S952169 119950516A5753 LE SKIN BOEING727 727232 1384082NM NR 4 FORE FLAP DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 RT WING NR 4 FORE FLAP FLAP L/E DAMAGE DUE TO HITTING T/E BRACKETS IN UP POSITION. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950526000401995052600040NM 1995 5 26 DL72W951928 119950507A5330 SKIN BOEING727 727247 138408FNM FS 684 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112821W 21059 FUSELAGE SKIN CRACKED 1 INCH LONG STA 684 ONE INCH ABOVE STR 18R. CUT OUT SKIN DAMAGE 2.5 LONG BY 1.0625 WIDE, .5 INCH RAD TYP, USING THE SRM 53-30-3 PAGES 6 AND 7. 2L73 4F A3WE 19950526000411995052600041NM 1995 5 26 DL72W951979 119950508A5532 SKIN BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112810W 20648 FOUND ON B-2 LETTER CHECK, .375 CRACK AT VERTICAL STABILIZER EXTERIOR SKIN RT SIDE STR 910 AT BASE OF VERTICAL. REPAIRED AS PER M/M 55-30-0 PG 801. 2L73 4F A3WE 19950526000421995052600042NM 1995 5 26 DL72W951980 119950508A5320 WEB BOEING727 727247 138408FNM FS 1213 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112810W 20648 FOUND ON B-2 LETTER CHECK, .5 INCH CRACK TORQUE BOX VERTICAL WEB STA 1213 LT ABOVE AFT STAIRS STEPS CLOSE-OUT PANEL. REPAIRED PER M/M 53-11-0 PG 832. 2L73 4F A3WE 19950526000431995052600043NM 1995 5 26 DL72W951981 119950508A5414 SKIN BOEING727 727247 138408FNM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112810W 20648 FOUND ON B-2 LETTER CHECK, .25 INCH CRACK VERTICAL STABILIZER EXTERIOR SKIN AT RT SIDE FWD OF ACCESS PANEL 9524 NR 2 ENGINE INTAKE COWL. REPAIRED PER SRM 54-30-01. 2L73 4F A3WE 19950526000441995052600044NM 1995 5 26 DL73E952167 119950517A5755 SPOILER BOEING737 737247 138448DNM RT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11242WA 23516 FOUND DURING LETTER CHECK, INBD LOWER SIDE OF GROUND SPOILER DAMAGED. REPAIRED PER SRM 57-50-5 PAINTED AREA. 2L72 4F A16WE 19950526000451995052600045NM 1995 5 26 DL757951627 119950301A5350141N7820 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11610DL 22817 RADOME WAS ROUTED TO SHOP FOR REWORK, DUE TO DAMAGE FROM DELAMINATION AND MOISTURE ENTRAPMENT. REWORKED RADOME PER SRM 53-10-72. 2L72 4F RTA2NM 19950526000461995052600046NM 1995 5 26 DL757951628 119950307A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11667DN 25035 RADOME WAS ROUTED TO SHOP FOR REPAIRS DUE TO DELAMINATION AND MOISTURE ENTRAPMENT. REWORKED RADOME PER SRM 53-10-72. 2L72 4F RTA2NM 19950526000471995052600047NM 1995 5 26 DL757951938 119950508A5754114N4003177A SKIN BOEING757 757232 1384965NM NR 2 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11653DL 24393 DURING SHOP INSP, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202. 2L72 4F RTA2NM 19950526000481995052600048NM 1995 5 26 DL757951960 119950430A5755 SKIN BOEING757 757232 1384965NM NR 12 SPOILER DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11676DL 25981 NR 12 SPOILER HAS 2 HOLES IN UPPER SURFACE, DUE TO HAIL DAMAGE. REPAIRED PER SRM 51-70-17, 05/04/95. 2L72 4F RTA2NM 19950526000491995052600049NM 1995 5 26 DL757951961 119950430A5755 SKIN BOEING757 757232 1384965NM RT SPOILER DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11676DL 25981 NR 11 SPOILER HAS 3 HOLES IN UPPER SURFACE FROM HAIL DAMAGE. REPAIRED PER SRM 57-70-01. 2L72 4F RTA2NM 19950526000501995052600050NM 1995 5 26 DL757951962 119950430A5755 SKIN BOEING757 757232 1384965NM NR 9 SPOILER DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11676DL 25981 NR 9 SPOILER HAS 2 HOLES IN UPPER SURFACE, FROM HAIL DAMAGE. REPAIRED PER SRM 57-70-03, AND SRM 57-70-01. 2L72 4F RTA2NM 19950526000511995052600051NM 1995 5 26 DL757951963 119950430A5755 SKIN BOEING757 757232 1384965NM RT SPOILER DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11676DL 25981 NR 7 SPOILER HAS 5 HOLES IN UPPER SURFACE FROM HAIL DAMAGE. REPAIRED PER DL ERA 207835-14 WITH REF TO SRM 57-70-01. 2L72 4F RTA2NM 19950526000521995052600052NM 1995 5 26 DL757952153 119950510A5753 SKIN BOEING757 757232 1384965NM RT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 AT HMV, SET UP TO COMPLY WITH ERA 236853-14A CODE 6-57-53 PERM REPAIR WING RT FLAP AFT I/B LOWER SKIN PERMANENT REPAIR. REPAIR WAS ACCOMPLISHED PER ERA 236853-14 PERM REPAIR. 2L72 4F RTA2NM 19950526000531995052600053NM 1995 5 26 DL757952154 119950515A5755 SKIN BOEING757 757232 1384965NM NR 8 SPOILER PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 AT HMV, A .25 INCH HOLE WAS LOCATED 4.75 INCHES FROM AFT EDGE AND 16.5 INCHES FROM I/B EDGE OF NR 8 SPOILER. THIS WAS REPAIRED PER SRM 51-70-17 AS REFERRED FROM SRM 51-70-14. 2L72 4F RTA2NM 19950526000541995052600054NM 1995 5 26 DL757952155 119950509A5315 FLOORBEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 AT HMV, THE FLOORBEAM WAS FOUND TO BE CORRODED AT STA 324 BL0 TO RT HAND O/B END AROUND FASTENER HOLES. THE CORROSION WAS REMOVED PER SRM 51-10-00 AND WAS FOUND OUT OF LIMITS. REPAIR ITEMS WERE FABRICATED PER SRM 51-10-08 FIG 201 AND INSTALLED PER SAME. 2L72 4F RTA2NM 19950526000551995052600055NM 1995 5 26 DL757952156 119950516A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1640 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING HMV, FOUND FS 1640 FLOORBEAM CORRODED AT APPROX RBL 39. REPAIRED BY REMOVING CORROSION AND REPAIRED PER SRM 53-30-51 PG 208. 2L72 4F RTA2NM 19950526000561995052600056NM 1995 5 26 DL757952157 119950515A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1640 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING HMV, FOUND FS 1640 FLOORBEAM IS CORRODED ACROSS ENTIRE BEAM. REPAIRED BY CLEANING CORROSION, CHECKED DEPTH PER SRM 53-00-51, TREATED AND PAINTED AREA FROM RBL 5 TO O/B END, EXCEPT RBL 39 PER PS 900-2-4-1 NR 2 AND PS 900-3-6-03. FABRICATED T-CAP AND DOUBLERS PER SRM 530-30-51 PG 212, TREATED AND PAINTED T-CAP AND DOUBLERS PER PS 900-2-4-1 NR 2 AND PS 900-3-6-03. INSTALLED REPAIR T-CAP SPLICED AT LBL 51 TO RBL 5 PER SRM 53-50-51 PG 212. 2L72 4F RTA2NM 19950526000571995052600057NM 1995 5 26 DL757952160 119950419A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 RECEIVED RADOME INTO SHOP WITH TWO INCH GOUGE AT 4 O'CLOCK, TWENTY FOUR INCHES FROM AFT EDGE. REMOVED DAMAGED SKIN AND CORE. REPLACED SKIN AND CORE AS PER SRM 53-10-72. APPLIED ERROSION BOOT AND PAINT AS PER PS 900-9-1-11, NR 05. FINAL INSPECTED AND SENT TO STOCK. 2L72 4F RTA2NM 19950526000581995052600058NM 1995 5 26 DL757952168 119950514A5532 LE SKIN BOEING757 757232 1384965NM VERT STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING HMV, FOUND A TEMPORARY REPAIR INSTALLED ON THE LEADING EDGE OF THE VERTICAL STAB. THE REPAIR IS LOCATED MID SPAN. THE SHOP INSTALLED A PERMANENT REPAIR PER THE SRM 55-30-01. 2L72 4F RTA2NM 19950526000591995052600059NM 1995 5 26 DL767952014 119950505A5522183T20011 SKIN BOEING767 767232 1385132NM LT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 HAIL DAMAGE IN DFW; DURING SHOP INSP MAINT, FOUND 7 ONE INCH DIAMETER HOLES IN UPPER SKIN. ALL HOLES WERE REPAIRED PER SRM 55-20-01 AND ERA 270858-14. 2L72 4F RTA1NM 19950526000601995052600060NE 1995 5 26 DL76L952163 219950514A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11174DN14969 24802 724166 AFTER REVIEW OF ENGINE HISTORY, NR 1 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS, DUE TO HIGH EGT AT ISA RESTRICTION. 2L72 4F4 FRTA1NM E24NE 19950526000611995052600061WP 1995 5 26 DLL13952166 119950509A5330 SKIN LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND THE FUSELAGE SKIN CRACKED 2 INCHES LONG AT THE AFT GROUND CONDITIONED AIR CUTOUT AT THE HINGE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 828. 2L73 4F A23WE 19950526000621995052600062NM 1995 5 26 DLM88951951 119950508A5320 ANGLE DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11903DE 53380 FOUND DURING C-2 LETTER CHECK, RT AFT MLG FRAME SUPPORT ANGLE CRACKED .5 INCH AT KEEL BEAM. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950526001571995052600157NM 1995 5 26 95ZZZW711 119950501A3350 EEL BATT BOEING737 737219 1384469NM RT EXTERIOR DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910248 20344 GSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE CAL950354 . 2L72 4F A16WE 19950526001581995052600158NM 1995 5 26 95ZZZW712 119950504A30406552803 HEAT CONTROLLER BOEING737 737277 1384570NM CAPT NR 1 MALFUNCTIONED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28178AW 2000118 22645 MCO-CMH - FLT 245 - CREW REPORTED ELECTRICAL ARCING IN TOP LEFT OF CAPTAINS NR 1 WINDOW ACCOMPANIED BY LOUD BANG AND WINDOW HEAT BECOMING INOPERATIVE. NO APPARENT CRACKS OR DELAMINATION WERE NOTED. AIRCRAFT LANDED IN CMH WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED CAPTAINS NR 1 WINDOW PER AWA TASK CARD R1B56001. MAINTENANCE ALSO REPLACED WINDSHIELD HEAT CONTROLLER AS PRECAUTIONARY. GROUND OPS CHECK OK. SEALANT COVERED WITH MYLAR TAPE AND PLACED ON DMI 53454. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500263. 2L72 4F RTA16WE 19950526001591995052600159NM 1995 5 26 95ZZZW713 119950430A2913 PUMP BOEING727 727232 1384082NM 'A' HYD SYSTEM FAILED A CALAAB UNSCHED LANDING EMER. DESCENT KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0933785153708139 20640 FLT NR 0134 - EWR - AIRCRAFT DECLARED EMERGENCY LANDING DUE TO 'A' SYSTEM LOST HYD PRESSURE AND FLUID. DURING INSPECTION FOUND 'A' SYSTEM PRESSURE LINE CRACK, CHANGE LINE AND PUMP. LEAK CHECKED SYSTEM ALL OK. REFERENCE CAL950340. 2L73 4F A3WE 19950526001601995052600160NM 1995 5 26 AALA950772 119950429A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07357AA 24038 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS UNDER AFT FLIGHT ATTTENDANT SEATS INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR UNDER AFT FLIGHT ATTENDANT SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526001611995052600161NM 1995 5 26 AALA950773 119950428A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RT AISLE OF BUSINESS CLASS INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT AFT AREA OF RT AISLE BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526001621995052600162NM 1995 5 26 AALA950788 119950501A3350 EEL WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07351AA 24032 MIA - DURING OVERNIGHT CHECK, EMERGNECY EXIT LIGHTS BY MID-GALLEY INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGT WIRE AT LEFT SIDE OF MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526001631995052600163NM 1995 5 26 AWXA9500257 119950501A3350 EEL ASSEMBLIES BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED LIGHTS AND WIRING IN SEVERAL AREAS, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950526001641995052600164NM 1995 5 26 AWXA9500258 119950502A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 12 TO 15. REPAIRED BROKEN WIRE AT ROWS 12 TO 15. REPAIRED BROKEN WIRE AT ROW 12, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950526001651995052600165NM 1995 5 26 AWXA9500259 119950503A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY LIGHTS INOPERATIVE AT ROWS 18 THROUGH 20. CRIMPED NEW CONNECTOR ON BROKEN WIRE, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950526001661995052600166NM 1995 5 26 AWXA9500260 119950503A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 13 THROUGH 22. RECONNECTED WIRE AT ROW 13, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950526001671995052600167EU 1995 5 26 AWXA9500262 119950504A3350321451 EEL PWR SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304RX 304 PHX - DURING ROUTINE MAINTENANCE CHECK, AFT LT EMERGENCY LIGHT POWER SUPPLY FAULTED DURING TEST. REPLACED POWER SUPPLY UNIT, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950526001681995052600168NM 1995 5 26 AWXA9500263 119950504A5610893543109 LT WINDOW BOEING737 737277 1384570NM CAPT NR 1 FAILED A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28178AW 03311399 22645 MCO-CMH - FLT 245 - CREW REPORTED ELECTRICAL ARCING IN TOP LEFT OF CAPTAINS NR 1 WINDOW ACCOMPANIED BY LOUD BANG AND WINDOW HEAT BECOMING INOPERATIVE. NO APPARENT CRACKS OR DELAMINATION WERE NOTED. AIRCRAFT LANDED IN CMH WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED CAPTAINS NR 1 WINDOW PER AWA TASK CARD R1B56001. MAINTENANCE ALSO REPLACED WINDSHIELD HEAT CONTROLLER AS PRECAUTIONARY. GROUND OPS CHECK OK. SEALANT COVERED WITH MYLAR TAPE AND PLACED ON DMI 53454. AIRCRAFT RETURNED TO SERVICE. REFERENCE 95ZZZW712. 2L72 4F RTA16WE 19950526001691995052600169NM 1995 5 26 AWXA9500264 119950515A7830657360634 ACCESSORY UNIT BOEING737 737275 1384485NM E/E COMPT MALFUNCTION A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR M00296 20922 PHX-SFO - FLT 605 - AFTER TAKEOFF, THE TAKEOFF WARNING HORN WOULD NOT SHUT OFF. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED TAKEOFF WARNING TEST PER AWA TASK CARD A1B31007, NO DEFECTS WERE NOTED. MAINTENANCE ALSO REPLACED ENGINE ACCESSORY UNIT AS A PRECAUTION. OPERATIONALLY TESTED ACCESSORY UNIT PER BMM 78-34-91, NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4F A16WE 19950526001701995052600170NM 1995 5 26 AWXA9500265 119950507A3350 EEL WIRE BOEING737 737277 1384570NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28179AW 22646 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND CABIN EMERGNCY EXIT LIGHTS ILLUMINATED WHEN SWITCH WAS IN OFF, ARMED OR ON POSITION. REPAIRED BROKEN WIRE AT ROW 14, OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950526001711995052600171EU 1995 5 26 AWXA9500266 119950508A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, LT COMMON EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950526001721995052600172NM 1995 5 26 AWXA9500272 119950508A2750 SEQ ROD BOEING737 73733A 1384673NM RT TE FLAPS LOOSE A AAWXAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 WP28168AW 23629 FLT 700 - LAS-PHX - ON TAKEOFF, AIRCRAFT ENCOUNTERED WAKE TURBULENCE AND DEVELOPED VERY STRONG VIBRATIONS WITH FLAPS EXTENDED. AIRCRAFT RETURNED TO LAS WITHOUT FURTHER INCIDENT. MX INSPECTED FLIGHT CONTROLS AND FOUND THE RT OUTBOARD AFT FLAP SEQUENCING ROD JAM NUT LOOSE. MX TIGHTENED AND SAFETIED NUT. AIRCRAFT RELEASED FOR FURTHER SERVICE. (W) 2L72 4F RTA16WE 19950526001731995052600173NM 1995 5 26 AWXA9500280 119950509A5400 ANGLE BOEING737 7373G7 1384595NM NR 1 PYLON CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28150AW 23218 PHX - DURING C11 INSPECTION, FOUND NR 1 ENGINE PYLON TRAILING EDGE SUPPORT ANGLE CRACKED IN UPPER INBOARD CORNER. REPAIRED PER SRM 51-40-02 AND SRM 51-10-02. NEW ANGLE FABRICATED AND INSTALLED. (W) 2L72 4F RTA16WE 19950526001741995052600174NM 1995 5 26 CAL950305 119950420A3350 EEL BATTERY PACK BOEING727 727224 1384076NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0979746 22449 FLT NR 0279 - EWR - A FORWARD SECTION OF EMERGENCY TRACK LIGHTING ILLUMINATED WHEN TESTED, BUT WENT DIM SHORTLY AFTER. THE FORWARD BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY TRACK LIGHTING WAS RESTORED. (W) 2L73 4F A3WE 19950526001751995052600175NM 1995 5 26 CAL950307 119950418A33501000677 EEL BOEING727 727224 1384076NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW096974210424 22251 GUM - THE R-1 SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING B-CHECK. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REPLACED. (W) 2L73 4F A3WE 19950526001761995052600176NM 1995 5 26 CAL950312 119950422A5512 SKIN BOEING737 7373T0 1384582NM LT HORIZ STAB GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0970330 23460 FLT NR 0225 - FLL - ON OVERNIGHT INSPECTION, FOUND 5 INCH .125 INCH DEEP GOUGE WITH SMALL HOLE ON THE MOST INBOARD LEFT HORIZ STABILIZER, REQUIRED PER ECRA 55-10-01299 AND SETUP REPETIVE INSPECTION. (W) 2L72 4F RTA16WE 19950526001771995052600177NM 1995 5 26 CAL950313 119950422A5330 SKIN BOEING737 7373T0 1384582NM FUSELAGE DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914308 23359 FLT NR 1698 - IAH - HOLE IN FORWARD SIDE OF AIRCRAFT FWD OF L-1 DOOR REPAIRED PER SRM 53-00-01 BLIND RIVIT REPAIR. INSPECTION EVERY 2500 FLT HOURS. REPLACE PRIOR TO 20,000 FLT HOURS. INITIATED DIP NR 24087. (W) 2L72 4F RTA16WE 19950526001781995052600178NM 1995 5 26 CAL950317 119950423A256003256090001 SLIDE BOEING737 7373T0 1384582NM L-1 DOOR FELL OFF A CALAK NONE O OTHER ININSP/MAINT 1 SW0914320 23371 IAH - FLT 0717 - L1 DOOR SLIDE FELL OFF DOOR AT PUSH BACK REINSTALLED SLIDE ASSY. (W) 2L72 4F RTA16WE 19950526001791995052600179NM 1995 5 26 CAL950337 119950427A5230 CORNER BOEING727 727227 1384078NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0910756 21042 FLT NR 0610 - EWR - FOUND CRACK IN UPPER FORWARD CARGO DOOR CORNER. REPAIRED PER ECRA 5230-01008. NO FURTHER INCIDENT AIRCRAFT DEPARTED. (W) 2L73 4F A3WE 19950526001801995052600180NE 1995 5 26 CAL950339 219950428A7230817401 FAN BLADE BOEING737 737217 1384464NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE BENT A CALAK NONE O OTHER ININSP/MAINT 1 SW0914233113666453 19887 FLT NR 1464 - IAH - ON MAINTENANCE WALKAROUND, FOUND NR 2 ENGINE FAN BLADE BENT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE ENGINE C1 DISK FAN ASSY. CHANGE COMPLETED, OPS CHECK GOOD. (W) 2L72 4F4 F A16WE E2EA 19950526001811995052600181NM 1995 5 26 CAL950340 119950430A2910651785064 HYD LINE BOEING727 727232 1384082NM 'A' HYD SYSTEM CRACK A CALAAB UNSCHED LANDING EMER. DESCENT KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0933785153708139 20640 FLT NR 0134 - EWR - AIRCRAFT DECLARED EMERGENCY LANDING DUE TO 'A' SYSTEM LOST HYD PRESSURE AND FLUID. DURING INSPECTION FOUND 'A' SYSTEM PRESSURE LINE CRACK, CHANGE LINE AND PUMP. LEAK CHECKED SYSTEM ALL OK. 95ZZZW713. 2L73 4F A3WE 19950526001821995052600182NM 1995 5 26 CAL950341 119950430A3350 EEL WIRING BOEING737 737219 1384469NM CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910248 20344 FLT NR 1275 - GSO - AIRCRAFT ARRIVED WITH EMERGENCY PATH LIGHTS ON, LIGHTS WOULD NOT GO OUT REPLACED BATTERY PACK OPS CHECK GOOD. THE BATTERY PACK WAS NOT AT FAULT. MAINTENANCE FOUND WIRING BROKEN AT BOTH THE AFT BULLNOSE LIGHT ASSEMBLY AND AT THE EMERGENCY EXIT SWITCH. THE BROKEN WIRES WERE REPAIRED. THE WIRING WAS CONFIRMED PER B737-200 WD33-51-01, PG 921 AND HOOK-UP CHART 91-21-51. (W) 2L72 4F A16WE 19950526001841995052600184NE 1995 5 26 CAL950353 219950507A7250 RETAINING BOLT BOEING747 747243B 1384830NM PWA JT9 JT9D7A 52054NE TURBINE VANE FRACTURED A ACALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW09330216019059265 20520 662746 FLT NR 9860 - HNL - THE NR 1 ENGINE GAVE OFF A LOUD BOOM AND THE EGT ROSE TO 963 DEGREES, SHORTLY AFTER TAKEOFF FROM HNL. THE NR 1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION CONCLUDED THAT THIS FAILURE WAS DUE TO THE PRIMARY FAILURE OF A STAGE 2 TURBINE VANE OUTER RETAINING BOLT WHICH WAS THE RESULT OF A MANUFACTURING DEFECT. (M) 2L74 4F4 F A20WE E20EA 19950526001851995052600185NM 1995 5 26 CAL950354 119950501A3350 EEL POWER SUPPLY BOEING737 737219 1384469NM RT EXTERIOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910248 20344 GSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE 95ZZZW711. 2L72 4F A16WE 19950526001861995052600186NM 1995 5 26 CAL950355 119950502A5330 SKIN BOEING727 727224 1384076NM BS 513 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .125 INCH CRACK IN SKIN AT LAP SPLICE 26L, BS 513. THE CRACKED AREA WAS CUT OUT. REPAIRED DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-30-3. (W) 2L73 4F A3WE 19950526001871995052600187NM 1995 5 26 CAL950356 119950502A5320 SUPPORT BOEING727 727224 1384076NM FS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND FLOOR SUPPORT CORRODED ON BOTTOM SIDE AT FORWARD PIT STATION 720. THE CORROSION WAS REMOVED AND A REPAIR WEB WAS INSTALLED IAW SRM 51-30-2. (W) 2L73 4F A3WE 19950526001881995052600188NM 1995 5 26 CAL950357 119950502A5320 CHORD BOEING727 727224 1384076NM FS 1183 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND REINFORCEMENT CHORD AT STATION 1183 CORRODED. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2. (W) 2L73 4F A3WE 19950526001891995052600189NM 1995 5 26 CAL950358 119950502A5712 RIB BOEING727 727224 1384076NM WS 738.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK ON LOWER SIDE OF LEFT WING INTERNAL RIB AT WS 738.5, ABOVE S-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W) 2L73 4F A3WE 19950526001901995052600190NM 1995 5 26 CAL950359 119950502A5320 SUPPORT BOEING727 727224 1384076NM FS 720 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND FLOOR SUPPORT IN FORWARD PIT AT STATION 720 ABOVE STRINGER 26L CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 53-10-5. (W) 2L73 4F A3WE 19950526001911995052600191NM 1995 5 26 CAL950360 119950502A5320 SUPPORT BOEING727 727224 1384076NM FS 990 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT FLANGE AT BS 990. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 53-10-2. (W) 2L73 4F A3WE 19950526001921995052600192NM 1995 5 26 CAL950361 119950502A5320 WEB BOEING727 727224 1384076NM FS 308.9 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .25 INCH CRACK IN WEB AT STRINGER 16L, STATION 308.9 INSIDE CONTROL CABIN AT MAIN ENTRY DOOR FRAME. THE CRACKED WEB WAS REPLACED IAW SRM 51-30-2 AND 51-10-1. (W) 2L73 4F A3WE 19950526001931995052600193NM 1995 5 26 CAL950362 119950502A5320 PRESSURE WEB BOEING727 727224 1384076NM RT LAVATORY CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND CORROSION ON PRESSURE WEB IN RT LAVATORY. THE CORROSION WAS REMOVED. DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-2. (W) 2L73 4F A3WE 19950526001941995052600194NM 1995 5 26 CAL9503624 119950502A5320 ANGLE BOEING727 727224 1384076NM BS 760 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT ANGLE AT BS 760, BL 0 - BL 24L. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-40-4, AND 51-30-2. (W) 2L73 4F A3WE 19950526001951995052600195NM 1995 5 26 CAL950363 119950502A5320 ANGLE BOEING727 727224 1384076NM FS 760 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN FLOOR PANEL SUPPORT ANGLE AT BS 760, BL 0 - BL 24R. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-40-3, AND 51-30-2. (W) 2L73 4F A3WE 19950526001961995052600196NM 1995 5 26 9508092704 119950518A32402114730PT3 BRAKE BOEING727 727225 1384077NM MLG DAMAGED A NWAAK NONE O OTHER TOTAKEOFF 1 GL01801EA32282539 22432 AFTER DEPARTURE, TOWER NOTED TIRE CARCASS ON RUNWAY. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 4 MAIN LANDING GEAR TIRE AND BRAKE DAMAGED. IN ADDITION, DAMAGE WAS SUSTAINED TO FORE, MID, AND AFT TRAILING EDGE FLAP. DENTS WERE ALSO FOUND ON NR 1 ENGINE COWL. REPLACED NR 4 MAIN LANDING GEAR TIRE AND BRAKE ASSEMBLY. OPERATIONAL CHECK OK. 2L73 4F A3WE 19950526001971995052600197WP 1995 5 26 9508109863 119950520A7711 EPR INDICATION DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01772NC 47773 696729 ON TAKEOFF, THE NR 2 ENGINE EPR INDICATION HUNG AT 1.7. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR. DURING RUNUP THE SYSTEM CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950526001981995052600198NM 1995 5 26 9508112295 119950519A3150 WARNING SWITCH BOEING727 727251 138408HNM COCKPIT SOUNDED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01295US 21506 WHEN TAKEOFF POWER WAS APPLIED, THE TAKEOFF WARNING HORN SOUNDED. FLAPS AND LEADING EDGE DEVICES INDICATED NORMAL. AIRCRAFT RETURNED TO THE GATE. REPLACED THE UPPER TRIM WARNING SWITCH. OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950526001991995052600199NE 1995 5 26 COM1083 319950519A6111 PROP BLADE SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE RT ENGINE DAMAGED A COMAK NONE O OTHER ININSP/MAINT 1 SO01341CA 1386 340A021 277084 RT PROPELLER, BLADE LEADING EDGE ERROSION GUARD IS LOOSE. REPLACED PROPELLER ASSY. 2L72 4T RTA52EU 6 CP61GL 19950526002001995052600200SW 1995 5 26 COM20370 119950518A5230 LATCH MECH SWRNGNSA227 SA227AC 8780603SW CARGO DOOR LACK OF LUBE A COMAK NONE O OTHER CLCLIMB 1 SO012711914746 AC701 CARGO DOOR WARNING DURING TAKE OFF. LUBRICATED CARGO DOOR LATCHING MECHANISM AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950526002011995052600201EU 1995 5 26 COM31084 119950519A2720MS289126C BEARINGS SAAB SF340 SF340A 7850100EU RUDDER FROZEN A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01140N 340A140 RUDDER TRIM INDICATED FULL LEFT IN FLIGHT, AUTO TRIM LIGHT ILLUMINATED. REPLACED FROZEN RUDDER TRIM TAB BEARINGS. 2L72 4T RTA52EU 19950526002021995052600202EA 1995 5 26 COM60476 119950518A2751855D1004 BPSU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01915CA4231 3731 7013 FLAPS FAIL MESSAGE ON EICAS. FLAPS STUCK AT 30 DEGREES. REPLACED THE LT AND RT FLAP BRAKE AND POSITION SENSOR UNITS. 2L72 4F RTA21EA 19950526002031995052600203NM 1995 5 26 SWAA950393 119950517A5330 SKIN BOEING737 7372T4 1384492NM AFT GALLEY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN AT AFT GALLEY DOOR HINGE CUTOUT, CRACKED .375 AT TOP CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002041995052600204NM 1995 5 26 SWAA950394 119950517A5320 WEB BOEING737 7372T4 1384492NM AFT GALLEY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB FWD OF DOOR CRACKED BELOW DOOR ASSIST HANDLE. REPAIRED PER SWA ACO 471-53. 2L72 4F A16WE 19950526002051995052600205NM 1995 5 26 SWAA950395 119950517A80122730426 START VALVE BOEING737 7372H4 138448CNM NBR 1 FAILED A SWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW0723SW 21338 AT 17,000, NUMBER 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW PERFORMED NUMBER 1 ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT IND WITHOUT INCIDENT. REPLACED ENGINE STARTER, START VALVE, STARTER CUTOUT PRESSURE SWITCH AND COCKPIT START SWITCH PER BOEING M/M. 2L72 4F A16WE 19950526002061995052600206NM 1995 5 26 SWAA950396 119950517A5330 SKIN BOEING737 7372T4 1384492NM LT FUS CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND LEFT FWD FUSELAGE SKIN CRACKED AT AIRSTAIR DOOR HANDLE CUTOUT, AFT END. REPAIRED PER SWA ACO 485-53. 2L72 4F A16WE 19950526002071995052600207NM 1995 5 26 SWAA950397 119950517A5320 WEB BOEING737 7372T4 1384492NM LT FUS CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY WEB CORRODED BETWEEN BS 986 AND 1006, RBL 46, LOWER SURFACE. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002081995052600208NM 1995 5 26 SWAA950398 119950517A5320 WEB BOEING737 7372T4 1384492NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY WEB CRACKED AT LOWER AFT END. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002091995052600209NM 1995 5 26 SWAA950399 119950517A5320 SHEAR TIE BOEING737 7372T4 1384492NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20L, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD. REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025. 2L72 4F A16WE 19950526002101995052600210NM 1995 5 26 SWAA950400 119950517A5320 SHEAR TIE BOEING737 7372T4 1384492NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20R, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD. REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025. 2L72 4F A16WE 19950526002111995052600211NM 1995 5 26 SWAA950401 119950517A5320 SUPPORT BOEING737 7372T4 1384492NM BS 540 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR SUPPORT HAT SECTION CRACKED AT BS 540, LBL 46. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002121995052600212NM 1995 5 26 SWAA950402 119950517A5313 STRINGER BOEING737 7372T4 1384492NM BS 947.5-970 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND S27L CORRODED FROM BS 947.5 TO 970. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002131995052600213NM 1995 5 26 SWAA950403 119950517A5320 SHEAR TIE BOEING737 7372T4 1384492NM BS 1006 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT LOWER LOBE AT BS 1006 BELTFRAME SHEAR TIE AFT LEG CORRODED FROM BL 0 TO LBL 3. REPLACED SHEAR TIE PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002141995052600214NM 1995 5 26 SWAA950404 119950517A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT UPPER CHORD FWD FLANGE RADIUS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950526002151995052600215NM 1995 5 26 SWAA950405 119950517A5313 STRINGER BOEING737 7372T4 1384492NM BS 500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT CENTER CABIN STRINGER S16R END FWD OF SCANNING LIGHT CUTOUT CRACKED AT BS 500B PLUS 2.5 AND AT 13.5. REPAIRED PER SWA ACO 6405-53. 2L72 4F A16WE 19950526002161995052600216NM 1995 5 26 UPS403273 119950517A5315 FLOOR BEAM BOEING747 747121 1384871NM FS 980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 980, LBL80 AND 90. INSTALLED REPAIR PER SRM 51-40-04. 2L74 4F A20WE 19950526002171995052600217NM 1995 5 26 UPS403274 119950517A5315 FLOOR BEAM BOEING747 747121 1384871NM FS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM STA 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712. 2L74 4F A20WE 19950526002181995052600218NM 1995 5 26 UPS403275 119950517A3800 WATER FILL PANEL BOEING747 747121 1384871NM FS 980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION AT THE WATER FILL PANEL, STA 980, RT LOWER SIDE, FUSELAGE. INSTALLED REPAIR PER SRM 51-20-01, 53-10-01, 51-10-01. 2L74 4F A20WE 19950526002191995052600219NM 1995 5 26 UPS403276 119950517A5315 FLOOR BEAM BOEING747 747121 1384871NM FS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE IN AMSTERDAM FOR C CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, BS 640, RBL 99. INSTALLED REPAIR PER UPS EO FILE NR B747-53-0712. 2L74 4F A20WE 19950526002201995052600220SW 1995 5 26 95ZZZX2468 119950501A215020475546 TURBINE SWRNGNSA226 SA226TC 8780404SW LT COOLING BEARING FAILED A BDHAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL15328BA TC253 SMOKE IN COCKPIT DUE TO LEFT COOLING TURBINE FAILURE. 1L72 4T A8SW 19950526002211995052600221SW 1995 5 26 95ZZZX2469 119950411A6320124112230 SWITCH BELL 206 206L1 1182107SW XMSN THERMO FAILED A HEEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW03513EH 45421 IN-FLIGHT, TRANSMISSION OIL TEMP LIGHT ILLUMINATED SEVERAL TIMES. TEMP INDICATOR READING NORMAL. AIRCRAFT DIVERTED TO FOURCHON. 206L-1 IPC, CHAPER 63-99-00, PAGE 8, FIGURE 63-2, ITEM 23. 1G71 3U H2SW 19950526002251995052600225EU 1995 5 26 95ZZZX2473 119950215A6410355A12004008 BLADE SNIAS 350 AS350B2 8680813EU T/R NR 2 TE TAB CRACKED A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH542 542 5835 2804 CRACKS AT BLADE NR 2 T.E. TAB, INBOARD AREA. CRACK BEYOND LIMITS. 1G71 3U H9EU 19950526002271995052600227NE 1995 5 26 95ZZZX2475 219950501A7250RRN125 RETAIN RING BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE NR 8 BEARING MAKING METAL A RMXAK NONE O OTHER ININSP/MAINT 1 SW05117VU1973 7211 45627 NOTED NUMEROUS CHIPS LARGER THAN .025 INCH. CHIP ALSO ON NG PICK-UP. REMOVED AND REPLACED ENGINE. 1G72 3U3 U H13EU E5NE10 19950526002281995052600228EU 1995 5 26 95ZZZX2476 119950421A7712G555674 TRANSMITTER BOLKMS117 BK117B1 5626012EU NR 2 ENGINE TQ FAILED A RMXAK NONE O OTHER ININSP/MAINT 1 SW05460H 7142 NR 2 ENGINE TORQUE TRANSMITTER FAILED. 1G72 3U H13EU 19950526002291995052600229NE 1995 5 26 95ZZZX2477 219950501A7412 EXCITER BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101750B1 41560NE ENGINE IGNITION DEFECTIVE A RMXAK NONE O OTHER ININSP/MAINT 1 SW05313LF 7138 LE45253 ENGINE IGNITION EXCITER DEFECTIVE. 1G72 3U3 U H13EU E5NE10 19950526002301995052600230CE 1995 5 26 95ZZZX2478 119950328A27501005240731 FLAP MOTOR BEECH 1900 1900D 1154162CE ZONE 163 INOP A S2YAO OTHER BF SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED DEDESCENT 1 GL13801SK1140 UE80 PILOT REPORTED FLAPS COULD NOT BE SELECTED DOWN AND DURING DESCENT THEY HAD SMELL OF BURNING CARDBOARD OR SIMILAR MATERIAL. MAINTENANCE FOUND THE FLAP RELAY HOT DURING TROUBLESHOOTING. MAINTENANCE PULLED AND TY-WRAPPED BOTH FLAP MOTOR CIRCUIT BREAKERS AND MEL'D THE FLAPS. NO EVIDENCE OF SMOKE OR FUMES FOUND IN CABIN DURING INSPECTION. 2L72 4T RTA24CE 19950526002311995052600231CE 1995 5 26 95ZZZX2479 119950417A571211412003327 RIB BEECH 1900 1900D 1154162CE WS 83.00 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13831SK2783 UE83 DURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER SECTION MID-RIB AT WS 83.00 TO HAVE A CRACK 1.1250 INCH LONG. THE CRACK WAS ALONG THE TOP BEND RADIUS AT THE RIB CENTER STIFFENER ATTACH POINT. THE FORWARD REINFORCEMENT PN 114-120033-15 WAS ALSO CRACKED AT EACH END. MAINTENANCE PERFORMED A MAJOR REPAIR BY STOP-DRILLING THE CRACKS, ADDING A DOUBLER, AND REPLACING THE FORWARD REINFORCEMENT. 2L72 4T RTA24CE 19950526002321995052600232CE 1995 5 26 95ZZZX2480 119950418A571211412003327 RIB BEECH 1900 1900D 1154162CE WS 83.00 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13841SK2812 UE84 DURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER MID-RIB AT WS 83.00 TO HAVE A CRACK 5 INCHES LONG. THE CRACK WAS LOCATED IN THE TOP BEND RADIUS, EXTENDING DOWN AT AN ANGLE FROM THE FORWARD REINFORCEMENT ATTACH POINT. THE FORWARD REINFORCEMENT, PN 114-120033-15, WAS ALSO CRACKED ON TOP. MAINTENANCE PERFORMED A MAJOR REPAIR BY STOP-DRILLING THE CRACK, ADDING TWO DOUBLERS, AND REPLACING FORWARD REINFORCEMENT. 2L72 4T RTA24CE 19950526002331995052600233CE 1995 5 26 95ZZZX2481 119950407A27301016100195L TORQUE TUBE BEECH 1900 1900D 1154162CE LT ELEVATOR LOOSE RIVETS A S2YAK NONE O OTHER ININSP/MAINT 1 GL13891SK2460 UE89 DISCOVERED LOOSE RIVETS ON LEFT ELEVATOR TORQUE TUBE DURING UNSCHEDULED MAINTENANCE ON TAIL. MAINTENANCE REMOVED AND REPLACED THE TORQUE TUBE ASSEMBLY. 2L72 4T RTA24CE 19950526002341995052600234CE 1995 5 26 95ZZZX2482 119950206A27301016100195 TORQUE TUBE BEECH 1900 1900D 1154162CE RT ELEVATOR LOOSE RIVETS A S2YAK NONE O OTHER ININSP/MAINT 1 GL13891SK2064 UE89 RIGHT ELEVATOR TORQUE TUBE ASSEMBLY FOUND TO HAVE LOOSE RIVETS AT THE ELEVATOR ATTACH BRACKET. THE PROBLEM WAS FOUND AT A DETAIL NR 6 AND THE RIVETS WERE REMOVED AND REPLACED. 2L72 4T RTA24CE 19950526002351995052600235CE 1995 5 26 95ZZZX2483 119950301A27301016100196 TORQUE TUBE BEECH 1900 1900D 1154162CE RT ELEVATOR LOOSE RIVETS A S2YAK NONE O OTHER ININSP/MAINT 1 GL13901SK2128 UE90 DURING SCHEDULED INSPECTION, MAINTENANCE DISCOVERED THE RIGHT ELEVATOR TORQUE TUBE RIVETS LOOSE AND FRETTING. REPLACED THE TORQUE TUBE ASSEMBLY. 2L72 4T RTA24CE 19950526002401995052600240NM 1995 5 26 95ZZZX2488 119950502A792228E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM NR 2 NACELLE FAILED A HNAAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA07910HA5769 337 37920028 022 YYZ/BWI - FLT 3393 - THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY LOSS OF OIL PRESSURE ON THE NR 2 ENGINE OIL PRESSURE GAUGE. POWER WAS REDUCED IMMEDIATELY AND THE ENGINE WAS SHUT DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO SCE AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL COOLER, OIL COOLER VALVE, AND THE VALVE ACTUATOR. 2H72 4T RTA13NM 19950526002411995052600241NM 1995 5 26 95ZZZX2489 119950502A792245E041 VALVE DHAV DHC8 DHC8102 2809003NM NR 2 OIL TEMP FAILED A HNAAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA07910HA5779 346 45E041 022 YYZ/BWI - FLT 3393 - THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY LOSS OF OIL PRESSURE ON THE NR 2 ENGINE OIL PRESSURE GAUGE. POWER WAS REDUCED IMMEDIATELY AND THE ENGINE WAS SHUT DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO SCE AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL COOLER, OIL COOLER VALVE, AND THE VALVE ACTUATOR. 2H72 4T RTA13NM 19950526002421995052600242NM 1995 5 26 95ZZZX2490 119950502A792037051 VALVE ACTUATOR DHAV DHC8 DHC8102 2809003NM NR 2 NACELLE FAILED A HNAAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA07910HA25007 0014 022 YYZ/BWI - FLT 3393 - THE NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY LOSS OF OIL PRESSURE ON THE NR 2 ENGINE OIL PRESSURE GAUGE. POWER WAS REDUCED IMMEDIATELY AND THE ENGINE WAS SHUT DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO SCE AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OIL COOLER, OIL COOLER VALVE, AND THE VALVE ACTUATOR. 2H72 4T RTA13NM 19950526002431995052600243WP 1995 5 26 95ZZZX2491 119950320A5330 SKIN DOUG DC8 DC863F 302198FWP FS 500 L30R CORRODED AS ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 FS 500.0, L30R, CORROSION ON SKIN. REPAIRED PER DER ARW 950037-0008 ON FILE. 2L74 4F 4A25 19950526002441995052600244WP 1995 5 26 95ZZZX2492 119950220A5730 SKIN DOUG DC8 DC862F 3021972WP WS 69.5 LE CORROSION A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 LEFT WING LEADING EDGE WS 69.500 AT FRONT SPAR, SMALL AREA AROUND SCREW, HAS CORROSION LEVEL II UPPER SURFACE. REMOVED CORROSION, FOUND AREA BEYOND LIMITS, FABRICATED DOUBLER AND FILLED REWORKED AREA IAW SRM 57-24. COMPLETED THICKNESS CHECK, TREATED, PRIMED, AND INSTALLED IAW SRM 57-2-1, F837. 2L74 4F 4A25 19950526002451995052600245WP 1995 5 26 95ZZZX2493 119950316A5320 FLOOR SUPPORT DOUG DC8 DC862F 3021972WP AFT LWR CARGO CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 AFT LOWER CARGO COMPARTMENT, FS 1100 AND STR 32L AND STR 35L. FRAME ATTACH FLOOR SUPPORT IS CRACKED AT 2 PLACES. W.O. 95007, CTL NR 5161, NR 0412. REMOVED FLOOR SUPPORT, WELDED CRACKS PER D.P.S. 10225 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND SRM 51-1-21. 2L74 4F 4A25 19950526002461995052600246WP 1995 5 26 95ZZZX2494 119950217A532057738443 INTERCOSTAL DOUG DC8 DC862F 3021972WP FS 1600.0 CRACK A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 FS 1600, STR 28L, INTERCOSTAL IS CRACKED. REMOVED DAMAGED INTERCOSTAL, FABRICATED NEW INTERCOSTAL PER ORIGINAL HEAT TREATED TO 7075-T6 AND INSTALLED PER SRM 53-1-0. DOCUMENTED UNDER W/O 950007, ITEM 5110. 2L74 4F 4A25 19950526002471995052600247WP 1995 5 26 95ZZZX2495 119950313A53471240000 CARGO TRACK DOUG DC8 DC862F 3021972WP AFT LWR CARGO CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 AFT LOWER CARGO COMPARTMENT, LT TRACK, HAS LEVEL II CORROSION AT FS 1080 - FS 1120, W.O. NR 950007, C/N 5163. REMOVED DAMAGED AREAS, TREATED, PRIMED AND INSTALLED NEW SECTION OF TRACKS PER SRM 53-2-3, AND SRM 51-1-21D. 2L74 4F 4A25 19950526002481995052600248WP 1995 5 26 95ZZZX2496 119950217A5730 SKIN DOUG DC8 DC862F 3021972WP WS STA XFS 885 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 EXFOLIATING CORROSION AROUND PREVIOUS REPAIRS ON LEFT WING LEADING EDGE UPPER SURFACE, WS XFS 885, WS XFS 890, XFS 908, AND XFS 920. REMOVED SECTION OF THE LEADING EDGE, REMOVED CORROSION, FOUND BEYOND LIMITS. ACCOMPLISHED REPAIR PER SRM 57-2-1, SRM 51-1-6, AND SRM 51-1-8. 2L74 4F 4A25 19950526002491995052600249WP 1995 5 26 95ZZZX2497 119950217A5330 SKIN DOUG DC8 DC862F 3021972WP FS 857 CORROSION A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 CORROSION AT FS 857.0, LEFT, IN THE WING BOX AREA. PERFORMED REPAIRS PER E.O. 9502201, W/O 950040, ITEM 9026. 2L74 4F 4A25 19950526002501995052600250WP 1995 5 26 95ZZZX2498 119950306A5312 BULKHEAD DOUG DC8 DC863F 302198FWP NOSE WHEELWELL CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 ACCOMPLISHED REPAIR TO FORWARD PRESS BULKHEAD IN NOSE WHEELWELL. CUT OUT DAMAGED AREA, FABRICATED ALL PARTS PER ARW D85330-3075. INSTALL PARTS IAW ARW D95330-3075. 2L74 4F 4A25 19950526002511995052600251NM 1995 5 26 TSAA9531076 119950205A3150 SWITCH BOEING737 737497 1384946NM SPEED BRAKE MALFUNCTIONED A TSAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP13401AL 25663 FLT 232 - ABORT TAKEOFF: WARNING HORN SOUNDED WHEN POWER PUSHED UP. GOT OFF RUNWAY AND CHECKED CONFIGURATION. EVERYTHING IN CORRECT POSITION. SECOND TAKEOFF OKAY. AS A PRECAUTIONARY, CLEANED AND ADJUSTED SPEED BRAKE HANDLE SWITCH. OPS CHECK PER MM 31-36-00. TAKEOFF WARNING SYSTEM TEST OKAY. TAT: 5371:03. TAC: 12660. (X) 2L72 4F RTA16WE 19950526002521995052600252NM 1995 5 26 TSAA9553077 119950503A5330 SKIN BOEING737 737297 1384480NM FS 794 S26R CORROSION A TSAAK NONE O OTHER ININSP/MAINT 1 WP13728AL 22629 DURING AN OVERNIGHT INSPECTION, DISCOVERED A FUSELAGE SKIN BULGE DUE TO CORROSION AT BS 794.30 AT S26R. REPAIRED PER ECO 2585. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TIME: 27614:55. CYCLE: 67081. (X) 2L72 4F A16WE 19950526002531995052600253NE 1995 5 26 VTZA95156 219950504A732031055015 SENSOR JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE TT2 FAILED A VTZAO OTHER J WARNING INDICATION DEDESCENT 1 EA27309UE 41022 P76014 IAD/JFK - FLT 6305 - DURING DESCENT AT 1330 HRS ON 5-4-95, FLIGHT EXPERIENCED A RIGHT IEC FAILURE WITH A LARGE TORQUE, RPM AND FUEL FLOW DIFFERENCE BETWEEN BOTH ENGINES. AIRCRAFT LANDED WTIH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE TT2 SENSOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950526002541995052600254EU 1995 5 26 VTZA95157 119950505A3230AIR864960 RETRACTION JACK JETAIRJETSTMJETSTM4101 1500501EU RT MAIN GEAR FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27315UE 41033 IAD/TYS - FLIGHT 6353 - DURING CLIMBOUT AT 0730 ON 5 MAY 95, RETURNED TO IAD DUE TO RT MAIN GEAR INTRANSIT LIGHT REMAINING ILLUMINATED AFTER GEAR SELECTED UP AND LOCKED. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT MAIN GEAR RETRACTION JACK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950526002551995052600255NE 1995 5 26 VTZA95158 219950505A732031058691 DELTA P/P BOX JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27311UE 41029 P75037 BDL/IAD - FLT 6541 - DURING TAKEOFF AT 0725 ON 5 MAY 95, ABORTED THE TAKEOFF DUE TO THE LT IEC FAILING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. AIRCRAFT WAS THEN FERRIED TO IAD. AIRCRAFT ARRIVED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DELTA P OVER P BOX. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950526002561995052600256NM 1995 5 26 WRLA95026 119950501A2610710129 DETECTOR DOUG MD11 MD11 3023602NM NR 1 'A' LOOP BROKEN A WRLAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CRCRUISE 1 EA27280WA 48458 DURING INITIAL CRUISE, APPROXIMATELY 2 HOURS AFTER TAKEOFF, NR 1 ENGINE 'FIRE DETECTION' FAIL ANNUNCIATED. FLIGHT CREW ELECTED TO DIVERT TO ALTERNATE AIRPORT. ABNORMAL PROCEDURES WERE FOLLOWED IN DUMPING FUEL TO BRING AIRCRAFT TO BELOW MLW. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND PYLON DETECTOR LOOP 'A' BROKEN (GAS-FILLED TUBE). REPLACED DETECTOR. ADDITIONALLY, FOUND WIRE BROKEN AT TERMINAL 'B' LOOP DETECTOR. REPAIRED WIRE AT 'B' LOOP DETECTOR. PERFORMED RTS TEST OF BOTH SYSTEMS WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950526002571995052600257NM 1995 5 26 95ZZZW714 119950330A573011173013 SKIN BOEING767 767223 1385123NM FS 956 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07324AA 22325 AFW - HEAVY CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN. FABRICATE A REPAIR STRAP FROM .100 THICK 7075-T6 ALUMINUM AND INSTALL WET WITH BMS 5-25. SEALANT FLAPPER PEEN, ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB B767-858. 2L72 4F RTA1NM 19950526002581995052600258NM 1995 5 26 95ZZZW715 119950408A5315141T511 FLOOR BEAM BOEING767 767223 1385123NM FS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07324AA 22325 AFW - FLOOR BEAM HAS CORROSION ON UPPER CHORD. FABRICATE A REPAIR STRAP FROM .050 INCH 301 1/2 HARD STAINLESS STEEL AND INSTALL WET WITH BMS 5-25 SEALANT. ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB 767. 2L72 4F RTA1NM 19950526002591995052600259NM 1995 5 26 95ZZZW716 119950505A27801U109592 ACTUATOR SWITCH RONSON BOEING727 727225 1384077NM NR 1 LE SLAT DEFECTIVE A AMYWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19803MA 1766 4417 22434 LEADING EDGE SLAT 'AMBER' LIGHT ON FORWARD INSTRUMENT PANEL 'ON' WITH FLAPS RETRACTED. INDICATION WAS CONFIRMED ON FLIGHT ENGINEER'S PANEL. NR 1 LE SLAT SHOWED INTRANSIT. RECYCLED FLAPS, NO HELP. AOM PROCEDURES FOLLOWED. ADVISED ATL ATC AND RETURNED TO CHS. NO PRIORITY HANDLING REQUESTED. AIRCRAFT WAS FERRIED TO MIA AND TROUBLESHOT TO A DEFECTIVE LIMIT SWITCH IN THE NR 1 SLAT ACTUATOR. THE SLAT ACTUATOR WAS REPLACED IAW MM 27-80-00. OPERATIONAL CHECK AND LEAK CHECK WAS OK. (W) 2L73 4F A3WE 19950526002601995052600260GL 1995 5 26 AALA950210 219950206A74219331M72P22 NOZZLE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C GL NR 10 POSN BROKEN A AAALAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 SW0733069 512 695280 PAP - FLT 1292 - AFTER TAKEOFF PAP, DURING CLIMB-OUT AT 19,000 FEET A LOAD BANG WAS HEARD AND HAD A INDICATION OF FIRE ON THE NR 2 ENGINE. DISCHARGED NR 1 AND NR 2 FIRE BOTTLES, FIRE INDICATION EXTINGUISHED. RETURNED AND LANDED PAP WITHOUT INCIDENT. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKS NORMAL OPERATION. NR 10 FUEL NOZZLE (P/N 9331M72P22, S/N PHG24A85) TIP FAILED IN HEAT AFFECTED ZONE OF MANUFACTURERS ASSY WELD. PART DELIVERED TO GENERAL ELECTRIC FOR FURTHER EVALUATION. ENGINE PROCESSED THROUGH SHOP FOR RETURN TO SERVICE. (W) 2L72 4F4 FRTA35EU E23EA 19950526002611995052600261EU 1995 5 26 AALA950303 119950221A3260141FL01D3 SWITCH AIRBUS300 A300B4605R 3930308EU RT MLG DEFECTIVE A AALAK NONE O OTHER CLCLIMB 1 SW0770054 461 BOS - FLT NR 1218 - AFTER TAKEOFF SJU WHEN LANDING GEAR RETRACTED AND AGAIN DURING APPROACH BOS WHEN LANDING GEAR EXTENDED, RT MAIN LANDING GEAR DOOR AMBER LIGHT DID NOT ILLUMINATE WHEN GEAR INTRANSIT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED BOS WITHOUT INCIDENT. REPLACED RT MAIN LANDING GEAR DOOR SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002621995052600262EU 1995 5 26 AALA950354 119950227A3230D226550002 DAMPER AIRBUS300 A300B4605R 3930308EU LT MLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0770079 B246 619 SDQ - FLT NR 1454 - AFTER TAKEOFF SDQ WHEN LANDING GEAR HANDLE RAISED, ECAM DISPLAYED MESSAGE INDICATING LANDING GEAR RETRACTION FAULT. PLACED LANDING GEAR HANDLE DOWN AND AIRCRAFT RETURNED TO SDQ, LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR PITCH TRIM DAMPER. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002631995052600263EU 1995 5 26 AALA950536 119950324A3230DSB1102 SENSOR AIRBUS300 A300B4605R 3930308EU NLG DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0791050 423 SJU - FLT 0105 - AFTER TAKEOFF FROM BOS LANDING GEAR WOULD NOT RETRACT WHILE IN HYDRAULIC SYSTEM 2. SWITCHED TO HYDRAULIC SYSTEM 1 AND GEAR RETRACTED SUCCESSFULLY. LANDING SJU WITHOUT INCIDENT. REPLACED PROXIMITY UNIT AND CLEANED PROXIMITY TARGETS. SYSTEM GROUND CHECKS NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002641995052600264EU 1995 5 26 AALA950624 119950408A3230D226550002 DAMPER AIRBUS300 A300B4605R 3930308EU LT MLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0734078 615 JFK - FLT 1473 - AFTER TAKEOFF JFK, UNABLE TO RETRACT LANDING GEAR WITH EITHER SYSTEM 1 OR 2. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002651995052600265NM 1995 5 26 AALA950679 119950413A33507024092007 EEL ASSY BOEING767 767323 1385205NM R1 DOOR BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07360AA 24041 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT LOWER EXIT SIGN AT R1 DOOR BROKEN. REPLACED EMERGENCY FLOOR LIGHT LOWER EXIT SIGN AT R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002661995052600266NM 1995 5 26 AALA950683 119950416A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07339AA 22336 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT 20 AB INOPERATIVE. RESERCURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 20 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002671995052600267NM 1995 5 26 AALA950685 119950417A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739356 24037 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT 30AB INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 30 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002681995052600268NM 1995 5 26 AALA950687 119950413A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT LEFT AISLE BETWEEN PAX SEAT ROWS 8 AND 12 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT LEFT AISLE BY PAX SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002691995052600269NM 1995 5 26 AALA950689 119950413A33508100022601 EEL BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BETWEEN PAX SEAT ROWS 7 AND 12 INOPERTIVE. REPLACED EMERGENCY FLOOR LIGHTS ASSEMBLIES AT RT AISLE BETWEEN PAX SEAT ROWS 7 AND 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002701995052600270NM 1995 5 26 AALA950694 119950417A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07850AA 20991 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT PAX SEAT ROW 17 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE AT PAX SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002711995052600271NM 1995 5 26 AALA950699 119950419A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07366AA 25193 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS INOPERATIVE FROM PAX SEAT ROWS 8AB TO 23AB. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 23AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002721995052600272EU 1995 5 26 AALA950711 119950421A3350 EEL PIN AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0714061 471 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS ILLUMINATED WITH SWITCH IN DISARM POSITION AND NO POWER ON THE AIRCRAFT. RESECURED PIN '0' ON BURNDY BLOCK 5702VT BLOCK 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002731995052600273NM 1995 5 26 AALA950713 119950422A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07382AN 25451 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN PAX SEAT ROWS 7HJ TO 21HJ. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002741995052600274EU 1995 5 26 AALA950715 119950424A3350A3030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0790070 513 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BY PAX SEAT ROW 15 INOPERATIVE. REPLACED EMEGENCY FLOOR LIGHT CONNECTOR AT RT AISLE BY PAX SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002751995052600275WP 1995 5 26 AALA950717 119950424A3350A3060723 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077544A 53026 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT CABIN BY EMERGENCY EXIT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN BY EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950526002761995052600276NM 1995 5 26 AALA950719 119950421A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07330AA 22330 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT ROW 7G INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT ROW 7G. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (W) 2L72 4F RTA1NM 19950526002771995052600277NM 1995 5 26 AALA950721 119950422A33500201922001 EEL WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07366AA 25193 MIA - DURING OVERNIGHT CHECK, SEAT MOUNTED EMERGENCY EXIT LIGHT WIRING HARNESS BROKEN AT PAX SEAT 12J. REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 12J. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002781995052600278NM 1995 5 26 AALA950723 119950423A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002791995052600279NM 1995 5 26 AALA950724 119950421A3230AAP2448A ACCESSORY UNIT BOEING727 727223 1384074NM E/E COMPT DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW07703AA 22461 DFW - FLT 0636 - AFTER TAKEOFF HOU, UNABLE TO RAISE LANDING GEAR HANDLE. DEPRESSED LANDING GEAR OVERRIDE TRIGGER AND LANDING GEAR HANDLE MOVED TO UP POSITION AND LANDING GEAR RETRACTED. AIRCRAFT PROCEEDED TO DFW, LANDING WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002801995052600280NM 1995 5 26 AALA950729 119950425A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7H AND 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002811995052600281NM 1995 5 26 AALA950731 119950426A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07361AA 24042 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LEFT AISLE BETWEEN PAX SEAT ROWS 8 TO 11 INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT LEFT AISLE PAX SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002821995052600282NM 1995 5 26 AALA950735 119950425A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07330AA 22330 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT RT AISLE BY PAX SEAT ROW 10H INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT RT AISLE BY PAX SEAT ROW 10H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002831995052600283NM 1995 5 26 AALA950737 119950426A33508100022602 EEL BOEING767 767323 1385205NM GALLEY DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07379AA 25448 SFO - EMERGENCY EXIT LIGHT BY FIRST CLASS GALLEY UNDER CENTER FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BY FIRST CLASS GALLEY UNDER CENTER FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002841995052600284NM 1995 5 26 AALA950739 119950426A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07323AA 22324 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT AFT CABIN CROSS-AISLE INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT AFT CABIN CROSS-AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002851995052600285NM 1995 5 26 AALA950751 119950427A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07368AA 25195 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT ROWS 22HJ THROUGH 24HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950526002861995052600286NM 1995 5 26 AALA950774 119950428A3350A3060719102 EEL BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07897AA 22013 MIA - DURING OVERNIGHT CHECK, 10 FOOT SECTION OF EMERGENCY FLOOR LIGHTS AT FRONT OF MAIN CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT TRACK AND LIGHTS AT FRONT OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002871995052600287NM 1995 5 26 AALA950777 119950430A3350A3060719104 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07712AA 22468 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 27 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002881995052600288NM 1995 5 26 AALA950778 119950430A3350A3060712101 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07712AA 22468 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 6 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002891995052600289NM 1995 5 26 AALA950779 119950430A3350P2010031302 EEL BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07712AA 22468 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BY RT OVERWING EXIT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT BY RT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002901995052600290NM 1995 5 26 AALA950780 119950427A33408710K15 LIGHT SWITCH BOEING727 727223 1384074NM COCKPIT DEFECTIVE A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW076822 19700 DFW - FLT NR 1902 - DURING DESCENT INTO DFW, ELECTRICAL BURNING SMELL NOTED IN COCKPIT. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. CHECK OF COCKPIT WIRING DETERMINED LEFT RUNWAY TURNOFF LIGHT SWITCH FAILED. PULLED AND COLLARED ASSOCIATED CIRCUIT BREAKER AND DEFERRED LEFT RUNWAY TURNOFF LIGHT. SUBSEQUENTLY REPLACED LEFT RUNWAY TURNOFF LIGHT SWITCH AT DTW/28. REACTIVATED SYSTEM AND SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950526002911995052600291EU 1995 5 26 AALA950791 119950430A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0711060 470 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT 4L/4R CROSS AISLE INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED EMERGENCY FLOOR LIGHTS AT 4L/4R CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA35EU 19950526002921995052600292WP 1995 5 26 AALA950819 119950504A3350A3060719104 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07278AA 49294 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BY FORWARD GALLEY HAD ONE BULB INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950526002931995052600293NM 1995 5 26 CKSA95020 119950421A261260B0002383 FIRE LOOP BOEING747 747146 NM NR 1 ENGINE INTERMITTENT A CKSAO OTHER N FALSE WARNING ININSP/MAINT 1 GL23703CK60351 19727 JED - NR 1 ENGINE FIRE WARNING CAME ON MOMENTARILY, TEST OK. REMOVED AND REPLACED 'A' LOOP FIRE DETECTOR FWD LOWER LOOP. OPS CHECKED GOOD IAW MM CHAPT 26. (W) 2L74 4F A20WE 19950526002941995052600294NM 1995 5 26 EIAA9515 119950422A335020131A EEL BATTERY PACK BOEING747 747212B 1384886NM CABIN DISCHARGED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09482EV 20713 JED - LOG PAGE E 0844 - ZONE 'D' EMERGENCY PATH LIGHT FAILS TO ILLUMINATE ON TEST. REPLACED ZONE 'D' EPLS BATTERY PAC IAW MM 33-51-50, TESTED OK. (X) 2L74 4F A20WE 19950526002951995052600295NE 1995 5 26 EIAA9516 219950429A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 1 FLAMED OUT A EIAAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 NM09485EV 20712 662254 JFK - LOG PAGE A7122 - AT FLIGHT LEVEL 340, NR 1 ENGINE FLAMED OUT. WHEN THROTTLE WAS RETARDED TO IDLE, BOOST PUMPS WERE ON AND NR 2 IGNITION SYSTEM WAS IN 'FLT START' POSITION. EGT MOMENTARILY WENT TO 830 DEGREES CELCIUS. ANTI-ICING USED PREVIOUSLY, BUT NOT ON AT THIS TIME. DURING RE-LIGHT, EGT WENT TO APPROX 610 DEGREES CELCIUS. ACCOMPLISHED INSPECTION PROCEDURE PER FIM 71-01-00, FAULT CODE DA-DD AND ENGINE PROCEDURE CHK NR 2, PAGE 203. NO WATER CONTAMINATION FOUND, REPLACED NR 1 ENG MAIN FUEL FILTER PER MM 73-11-02, LEAK CHECK OKAY ON RUN-UP. INSP CHK CARRIED OUT PER MM 73-00-42 & MM 71-00-46, PROCEDURES 5 & 1. NIL DEFECTS FOUND. NR 1 MAIN TANK SUMPED-NO WATER IN SUMP. ACFT RETURNED TO SERVICE. (X)2L74 4F4 F A20WE E20EA 19950526002961995052600296EU 1995 5 26 WTAA950176 119950426A7933MS280343 OIL TEMP BULB BAG JETSTMJETSTM3101 1500215EU RT ENGINE CONTAMINATED A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17424UE 796 CIC - RIGHT ENGINE OIL TEMPERATURE REPORTED HIGH AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED OIL TEMPERATURE BULB CANNON PLUG. RIGHT ENGINE OIL TEMPERATURE INDICATIONS NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950526002971995052600297NM 1995 5 26 95UAL757017 119950519A3350 EEL STRIP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29555UA 26647 AFT LT LAVATORY EEL STRIP INOPERATIVE. REPLACED EEL STRIP ASSEMBLY. 2L72 4F4 FRTA2NM E17NE 19950526002981995052600298NE 1995 5 26 95UAL757018 219950519A7200 ENGINE BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A UALAA UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 WP29519UA 24872 726574 RETURN TO IAH DUE TO LOSS OF POWER ON NR 1 ENGINE. HOT GAS IMPINGING ON THE TRANSITION DUCT MOUNT BOLTS CAUSED THEM TO FAIL. THE TRANSITION DUCT BLOCKED THE GAS PATH AND CAUSED THE ENGINE TO STALL. 2L72 4F4 FRTA2NM E17NE 19950526002991995052600299WP 1995 5 26 95UALD10044 119950519A3350 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291847U 48263 OVERHEAD EMERGENCY EXIT LIGHT BY DOOR 4L INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A22WE E23EA 19950526003001995052600300NM 1995 5 26 DHL95740002 119950518A2913371380 HYD PUMP BOEING727 7272Q9 138448MNM NR 1 FAILED A TDHLAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO01740DH 21930 A SYSTEM LOSS SHUT DOWN NR 1 A PUMP OFF AND FLUID LOSS SLOWED CONSIDERABLY. REMOVED AND REPLACED NR 1 A SYSTEM PUMP AND DRAIN FILTER PER M/M 29-11-41 AND 29-11-33, BLED SYSTEM. A SYSTEM OPS AND LEAK CHECK GOOD . 2L73 4F RTA3WE 19950526003011995052600301NM 1995 5 26 UPS203279 119950519A5754 RIB BOEING727 727247 138408FNM NR 4 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01212UP 21392 WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON NR 4 SLAT ACTUATOR ROD END SUPPORT RIBS, I/B AND O/B SIDES IN SLAT COVES. INSTALLED REPAIR PER SRM 51-30-2, MM27-80-00, OHM 20-50-01. 2L73 4F A3WE 19950526003021995052600302NM 1995 5 26 UPS203280 119950519A3260 SWITCH BOEING727 727247 138408FNM NLG INOP A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01212UP 21392 WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON LT WING, I/B MID FLAP, LWR T/E CHORD AT THE I/B AFT FLAP, I/B TRACK CUTOUT, I/B AFT FLAP ACTUATING MECHANISM CUTOUT AND THE AFT FLAP I/B CENTER TRACK CUTOUT. REPLACED CHORD PER SRM 51-30-2, 51-40-4, OHM20-50-01. 2L73 4F A3WE 19950526003031995052600303NM 1995 5 26 UPS203281 119950520A3350 EEL BATTERY BOEING727 72722C 138400FNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01928UP 19091 MAINTENANCE REPORTED EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN SWITCHED TO ON. REPLACED EMERGENCY EXIT LIGHT BATTERY, OPS CK NORMAL. 2L73 4F A3WE 19950526003041995052600304NM 1995 5 26 9508126306 119950516A5315 FLOORBEAM BOEING747 747451 1384940NM FS 1720 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01666US 23821 DURING PERIODIC CHECK, FOUND CORROSION ON THE UPPER FLOORBEAM CHORD FS 1720, LBL 76 TO 99. REPAIRED PER EA 63-98269. 2L74 4F RTA20WE 19950526003051995052600305NM 1995 5 26 9508135527 119950516A5315141N5112 FLOORBEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01527US 23842 DURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD FS 365. REPAIRED PER EA 55-98478. 2L72 4F RTA2NM 19950526003061995052600306WP 1995 5 26 9508149959 119950517A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING PERIODIC CHECK, FOUND CRACK IN THE INTERCOSTAL SUPPORT FITTING BETWEEN LONGERONS 27R TO 28R, FS 996. REPLACED THE FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950526003071995052600307WP 1995 5 26 9508151155 119950517A5730 SKIN DOUG DC10 DC1040 3023508WP LT WING TORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING LINE CHECK, FOUND A 21 BY 8 SECTION OF TRAILING EDGE SKIN TORN FROM THE LEFT WING OUTBOARD OF THE OUTBOARD AILERON. REPAIRED PER EA 11-98538, MFG PART NUMBER ARC0550-1. 2L73 4F A22WE 19950526003081995052600308WP 1995 5 26 9508169140 119950517A5230 FITTING DOUG DC9 DC914 3022034WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND A .25 CRACK IN THE AFT CARGO DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING. 2L72 4F A6WE 19950526003091995052600309WP 1995 5 26 9508179140 119950517A5320 FITTING DOUG DC9 DC914 3022034WP FS 629 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WHEEL WELL LONGERON 30 END FITTING AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5. 2L72 4F A6WE 19950526003101995052600310WP 1995 5 26 9508189140 119950517A5320 FITTING DOUG DC9 DC914 3022034WP FS 629 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL KEEL FITTING LONGERON 29L AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5. 2L72 4F A6WE 19950526003111995052600311NE 1995 5 26 9508195503 219950521A7321 FUEL CONTROL BOEING757 757251 1384970NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A ANWAAD RETURN TO BLOCK AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 GL01503US 23192 716373 DURING TAXI AND AFTER BOTH ENGINES STABILIZED, THE LEFT ENGINE SHUTDOWN BY ITSELF. RECEIVED LOW OIL PRESSURE WARNING AND LEFT ENGINE PIRMARY CONT MESSAGE. THE FUEL CONTROL WAS THEN SHUTOFF AND THERE WAS A TAILPIPE FIRE. AIRCRAFT WAS RETURNED TO GATE WHERE THE ENGINE FUEL CONTROL AND EEC WERE REPLACED. 2L72 4F4 FRTA2NM E17NE 19950526003121995052600312EU 1995 5 26 9508203214 119950522A7932 CONNECTOR AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 OIL QTY INDLOOSE A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL01314US 160 73140 DURING CRUISE, THE NR 1 OIL QUANTITY INDICATION DROPPED TO 1.5. THE CIRCUIT BREAKER WAS RESET, BUT INDICATION STAYED THE SAME. THE PRESSURE PROCEEDED TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO ORD WHERE AN UNEVENTFUL LANDING WAS MADE. THE OIL QUANTITY CANNON CONNECTOR PLUG WAS CLEANED AND SECURED AND NO ADDITIONAL PRESSURE FLUCTUATION WAS NOTED. 2L72 4F4 FRTA28NM 19950526003131995052600313WP 1995 5 26 ABXA9500456 119950308A32315221037014101 BUSHINGS DOUG DC9 DC941 302207NWP FS 775 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD BUSHINGS WORN. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL. 2L72 4F A6WE 19950526003141995052600314WP 1995 5 26 ABXA9500457 119950317A323139231597 RETRACT MECH DOUG DC9 DC941 302207NWP FS 775 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR DOOR BUSHINGS WORN IN ACTUATING ARM. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950526003151995052600315WP 1995 5 26 ABXA9500458 119950308A5532591216610AX SKIN DOUG DC9 DC941 302207NWP FS 1367 CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT VERTICAL SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. REPLACED SKIN IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19950526003161995052600316WP 1995 5 26 ABXA9500459 119950404A57555910055514 SKIN DOUG DC9 DC941 302207NWP RT SPOILER DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING INBOARD SPOILER TRAILING EDGE DELAMINATED. REPLACED RIGHT INBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1. 2L72 4F A6WE 19950526003171995052600317WP 1995 5 26 ABXA9500460 119950404A57555910055513 SKIN DOUG DC9 DC941 302207NWP LT SPOILER DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED LEFT OUTBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1. 2L72 4F A6WE 19950526003181995052600318WP 1995 5 26 ABXA9500461 119950331A572059124382 DOUBLER DOUG DC9 DC941 302207NWP WS 111.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING UPPER MAIN LANDING GEAR DOUBLER CORRODED IN PREVIOUS BLENDOUTS. REPLACED RIGHT WING UPPER MAIN LANDING GEAR DOUBLER IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950526003191995052600319WP 1995 5 26 ABXA9500462 119950330A53125910130387N BLKDH DOUG DC9 DC941 302207NWP FS 1072 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP AT FS 1072 CORRODED AT LONGERON 30. REPLACED AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526003201995052600320WP 1995 5 26 ABXA9500463 119950324A532099115433 SUPPORT DOUG DC9 DC941 302207NWP FS 908 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT VERTICAL FRAME SUPPORT CRACKED AT FS 908 IN AFT BAG BIN. REPLACED FRAME SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526003211995052600321WP 1995 5 26 ABXA9500464 119950324A5312991555861 BLKHD FORMER DOUG DC9 DC941 302207NWP FS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A RADIAL STIFFENER CRACKED ON FORWARD FACE OF AFT PRESSURE BULKHEAD FS 1072 AND LONGERON 14L. REPLACED STIFFENER IAW DC-9 SB 53-166 AND SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526003221995052600322WP 1995 5 26 ABXA9500465 119950323A5312595604043 BLKHD SUPPORT DOUG DC9 DC941 302207NWP FS 794 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT 22R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950526003231995052600323WP 1995 5 26 ABXA9500466 119950323A5312595604013 BLKHD SUPPORT DOUG DC9 DC941 302207NWP FS 794 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT LONGERON 22 R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950526003241995052600324WP 1995 5 26 ABXA9500467 119950320A53305910228183 SKIN DOUG DC9 DC941 302207NWP FS 1197-1208 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT FUSELAGE SKIN CORRODED ALONG LONGERON 20L BETWEEN FS 1197 AND FS 1208. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950526003251995052600325WP 1995 5 26 ABXA9500468 119950316A531159135877 FRAME DOUG DC9 DC941 302207NWP FS 1152 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND FUSELAGE FRAME AT FS 1152 CRACKED AT LONGERON 14R. REPLACED FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526003261995052600326WP 1995 5 26 ABXA9500469 119950315A531359197079 LONGERON DOUG DC9 DC941 302207NWP FS 879-1031 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 30 CORRODED FROM FS 908 TO FS 946 IN AFT BAG BIN. REPLACED LONGERON SECTION IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526003271995052600327WP 1995 5 26 ABXA9500470 119950322A53209955840506 PANEL DOUG DC9 DC941 302207NWP FS 756 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER PAD. REPLACED RIGHT TRAPEZOIDAL PANEL IAW DC-9 SB 53-182. 2L72 4F A6WE 19950526003281995052600328WP 1995 5 26 ABXA9500507 119950522A32300142101321 RETRACT MECH NIHON YS11 YS11A500 6310416WP NLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23914AX 10810 2056 NOSE GEAR FAILED TO EXTEND ON INITIAL TRY. RECYCLED GEAR AND IT CAME DOWN ON SECOND ATTEMPT. LUBED NOSE LANDING GEAR ASSEMBLY. OPS CHECKED GOOD IAW YS-11 MM CHAPTER 32. 2L72 4T A1PC 19950526003291995052600329SO 1995 5 26 COM11896 119950522A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01161CA14928 120143 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-552/652-01I AND 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO DESIGN REPORT NR 1327.2. P/N 120-17056-007, 4 EA; 120-17056-011, 1 EA; 120-17056-013, 1 EA; 120-17056-015, 2 EA; 120-17056-017, 1 EA; 120-17056-019, 1 EA; 120-17062-013, 1 EA; 120-17063-009, 3 EA; 120-17062-005, 1 EA; 120-17060-007, EA. 2L72 4T RTA31SO 19950526003301995052600330SO 1995 5 26 COM11897 119950521A612078249012 PCU EMB 120 EMB120RT SO LT PROP OUT OF ADJUST A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01241CA113151254 120211 DURING TAKEOFF LT NP INDICATED 99.3 PERCENT. ADJUSTED PCU FOR 100 PERCENT PROPELLER RPM. 2L72 4T RTA31SO 19950526003311995052600331SO 1995 5 26 COM11898 119950522A2731922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01200CD 120200 TAKEOFF TRIM WARNING SOUNDED DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. 2L72 4T RTA31SO 19950526003321995052600332 1995 5 26 COM20371 419950521A34183219023001 SAS SERVO SWRNGNSA227 SA227AC 8780603SW AVIONICS DEFECTIVE A COMAK NONE O OTHER DEDESCENT 1 SO01459AM12006 AC700 THERE IS BINDING IN THE CONTROLS WHEN PULLING AFT ON THE CONTROL YOKE. REPLACED THE SAS SERVO AND CAPSTAN. 1L72 4T A8SW 19950526003331995052600333SW 1995 5 26 COM20372 119950521A3234 SELECTOR SWRNGNSA227 SA227AC 8780603SW LANDING GEAR NOT STOWED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01703CA AC703 LANDING GEAR DID NOT RETRACT, INTRANSIT INDICATORS ILLUMINATED. FOUND LANDING GEAR EMERGENCY SELECTOR NOT PROPERLY STOWED. SECURED SELECTOR AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950526003341995052600334EU 1995 5 26 COM31085 119950522A27107227150781 LEVER SAAB 7227150148 SAAB SF340 SF340A 7850100EU LT/RT AILERONS BINDING A COMAK NONE O OTHER CRCRUISE 1 SO01359CA 340A053 AILERON CONTROL IS SLOPPY WITH FLAPS EXTENDED. REPLACED THE LT AND RT AILERON CENTERING CAMS AND ROLLERS. 2L72 4T RTA52EU 19950526003351995052600335EA 1995 5 26 COM60477 119950522A2750855D1004 BPSU CNDAIRCL600 CL6002B19 EA RT TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01926CA4383 3453 7027 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE RT BPSU. 2L72 4F RTA21EA 19950526003361995052600336 1995 5 26 COM60478 419950522A3400 CIRCUIT BREAKER CNDAIRCL600 CL6002B19 EA COCKPIT TRIPPED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01912CA 7011 IAPS DEGRADED STATUS MESSAGE ON EICAS. RESET CIRCUIT BREAKER AND SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950526003371995052600337EU 1995 5 26 DL31L952127 119950515A7110 COWL AIRBUS310 A310324 3930206EU NR 1 ENG DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11838AB 676 NR 1 ENG INLET COWL OUTER BARREL COMPOSITE SKIN DELAMINATED BEHIND LIP ASSY. ALSO, CRACKED AT THE 3 O'CLOCK POS SANDED AREA AROUND DAMAGE AND APPLIED EA 9390 AT 1230. REPAIRED SKIN PER SRM 54-10-00 PG 201. 2L72 4F RTA35EU 19950526003381995052600338NM 1995 5 26 DL72E952142 119950516A5320 CLIP BOEING727 727247 138408FNM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND DURING C-2 LETTER CHECK, SKIN CLIP CRACKED AT STA 1263 LT SIDE. REPAIRED PER MM 54-11-0 PG 825. 2L73 4F A3WE 19950526003391995052600339NM 1995 5 26 DL72E952143 119950516A5754 ANGLE BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND DURING C-2 LETTER CHECK, LWR COVE PANEL ATTACH ANGLE CRACKED NR 3 L/E SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950526003401995052600340NM 1995 5 26 DL72E952144 119950516A5754 LE RIB BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON C2 LTR CK, .5 INCH CRACK AT LEADING EDGE NOSE RIB ON 6 SLAT INBOARD OF ACTUATOR. REPAIR PER M/M 57-54-0. 2L73 4F A3WE 19950526003411995052600341NM 1995 5 26 DL72E952146 119950516A5754 ANGLE BOEING727 727247 138408FNM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON C2 LTR CK, NR 1 SLAT O/B STOP CASTING LOWER CHORD ANGLE CRACKED .25 INCH VISIBLE. REPAIRED LWR CHORD ANGLE PER M/M 57-54-0. 2L73 4F A3WE 19950526003421995052600342NM 1995 5 26 DL72K952200 119950519A7110 SKIN BOEING727 727232 1384082NM NR 2 INTAKE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11415DA 21257 A 6 INCH BY .25 INCH CRACKS FROM RIVETS ON LT VERT SPAR SKIN, JUST FWD AND BELOW BOTTOM CORNER OF SADDLE PANEL 9501. ALSO, 2 INCH BY .25 INCH CRACKS ON RT SIDE SAME LOCATION AS ITEM 1 ABOVE, AT NR 2 INTAKE STRUCTURE. REPAIRED PER MM 54-30-0. 2L73 4F A3WE 19950526003431995052600343NM 1995 5 26 DL72L952219 119950515A5313 STRINGER BOEING727 727232 1384082NM FS 580-600 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11501DA 21303 FOUND ON CV2 CHECK, CORROSION ON STR 27L BETWEEN STA 580 AND 600. REPAIRED PER SRM 53-10-3 FIG 1, IDENTIFIED AS PERMANENT REPAIR PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950526003441995052600344NM 1995 5 26 DL72S951492 119950412A5522657278411 TE SKIN BOEING727 727232 1384082NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 DURING SHOP INSPECTION, THE LEFT ELEVATOR WAS FOUND WITH CRACKS IN THE TRAILING EDGE. REPAIRS ACCOMPLISHED PER SRM 55-20-3. 2L73 4F A3WE 19950526003451995052600345NM 1995 5 26 DL72S952170 119950518A5754 ANGLE BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11519DA 21470 COVE SKIN ATTACH ANGLE CRACKED NR 4 SLAT OUTBRD TRACK .25 INCH, FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950526003461995052600346NM 1995 5 26 DL72S952171 119950518A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11519DA 21470 DOUBLER CRACKED COVE SKIN ATTACH ANGLE NR 2 SLAT INBD STOP PAD, FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950526003471995052600347NM 1995 5 26 DL72S952172 119950518A5755 ANGLE BOEING727 727232 1384082NM NR 3 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11519DA 21470 OUTBD ATTACH CASTING CRACKED 1.75 INCH NR 3 SPOILER AT ACTUATOR. CRACK REPAIR TO BE ACCOMPLISHED WITHIN 30 DAYS PER SRM 57-50-6. 2L73 4F A3WE 19950526003481995052600348NM 1995 5 26 DL72S952187 119950514A5315 FLOORBEAM BOEING727 727232 1384082NM FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 FOUND AT HMV, MOUNT HOLES CORRODED FLOOR SUPPORT ANGLE AT L-1 DOORWAY, STA 312 THROUGH 360. HOLE CORRODED FLOORBEAM STA 328, LBL 45. REPAIRED PER MM 53-20-11 FIG 804A. 2L73 4F A3WE 19950526003491995052600349NM 1995 5 26 DL72S952188 119950514A5311 FRAME BOEING727 727232 1384082NM FS 950 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 FOUND AT HMV, FRAME 950C CORROSION LWR SIDE BETWEEN STR 30 AND 29R. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER MM 53-11-0 PG 825. 2L73 4F A3WE 19950526003501995052600350NM 1995 5 26 DL72S952190 119950513A5313 STRINGER BOEING727 727232 1384082NM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND STR 15L CRACKED AT STA 720B. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950526003511995052600351NM 1995 5 26 DL72S952191 119950513A5313 STRINGER BOEING727 727232 1384082NM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND STR 15L CRACKED AT STA 720C. REPAIRED PER SRM 53-10-3 DETAIL 2 FIG 2. 2L73 4F A3WE 19950526003521995052600352NM 1995 5 26 DL72S952192 119950513A5311 FRAME BOEING727 727232 1384082NM FS 312 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND FRAME AT STA 312 CRACKED AT STR 13R. REPAIRED PER SRM 53-10-4 FIG 1 DETAIL 3. 2L73 4F A3WE 19950526003531995052600353NM 1995 5 26 DL72S952193 119950510A5520 RIVET BOEING727 727232 1384082NM RT ELEVATOR MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND RIVET MISSING ON LOWER SURFACE OF RT ELEVATOR INBD TRAILING EDGE CORNER. REPAIRED PER SRM 55-20-3 FIG 2. 2L73 4F A3WE 19950526003541995052600354NM 1995 5 26 DL72S952194 119950512A2780 ACT BRACKET BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND NR 5 L/E FLAP O/B ACTUATOR SUPPORT BRACKET CRACKED. REPAIRED PER M/M 57-20-21 PG 811. 2L73 4F A3WE 19950526003551995052600355NM 1995 5 26 DL72S952195 119950517A5713 STRINGER BOEING727 727232 1384082NM WS 546 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, FOUND LT WING STRINGER 8 AT STA 546.5 CRACKED. REPAIRED PER M/M 57-13-0 PG 801. 2L73 4F A3WE 19950526003561995052600356NM 1995 5 26 DL72S952198 119950508A5320 SUPPORT BEAM BOEING727 727232 1384082NM FS 830-850 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 RT FAIRING SUPPORT BEAM HAS AREAS OF HEAVY CORROSION FROM STA 830 TO STA 850, FOUND AT HMV. 2L73 4F A3WE 19950526003571995052600357NM 1995 5 26 DL72S952207 119950428A5313 STRINGER BOEING727 727232 1384082NM FS 560 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 STRINGER 27L BETWEEN STA 560 AND STA 580 FWD CARGO CORRODED. REMOVED DAMAGED SECTION OF STRINGER, SPLICED PER SRM 53-10-3 PG 3, FOUND AT HMV. 2L73 4F A3WE 19950526003581995052600358NM 1995 5 26 DL72S952215 119950521A3350S106 EEL BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST CRCRUISE 1 SO11528DA 21702 L-2 OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19950526003591995052600359NM 1995 5 26 DL72S952216 119950521A3350900835A EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11528DA 21702 R-2 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19950526003601995052600360NM 1995 5 26 DL72S952227 119950514A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND 2ND FROM IB RIB CRACKED IN THE NR 2 SLAT LE. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950526003611995052600361NM 1995 5 26 DL72S952228 119950514A5754 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NR 2 LE SLAT 3RD RIB FROM IB END IS CRACKED. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950526003621995052600362NM 1995 5 26 DL72S952229 119950514A5754 RIB BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NR 5 LE SLAT 10TH RIB FROM IB END CRACKED. REPAIRED PER MM 52-54-0 PG 819. 2L73 4F A3WE 19950526003631995052600363NM 1995 5 26 DL72S952230 119950513A5320 FRAME BOEING727 727232 1384082NM R1 DOORWAY CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND R1 DOORWAY FWD FRAME CRACKED AT BOTTOM CORNER. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-4 PG 23. 2L73 4F A3WE 19950526003641995052600364NM 1995 5 26 DL72S952231 119950514A5754 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NR 4 LE SLAT 11TH RIB FROM OB END CRACKED. INSTALLED NEW DOUBLER PER MM 57-54-00 PG 812. 2L73 4F A3WE 19950526003651995052600365NM 1995 5 26 DL72S952232 119950514A5754 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NR 4 LE SLAT 4TH LE RIB FROM OB END IS CRACKED. DRILLED UP AND INSTALLED NEW DOUBLER PER MM 57-54-0 PG 806. 2L73 4F A3WE 19950526003661995052600366NM 1995 5 26 DL72S952237 119950519A215010614267 EXCHANGER BOEING727 727232 1384082NM RT PACK FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11520DA 21471 ON CLIMBOUT FL 2,900 CABIN WARNING HORN CAME ON, CABIN ALT ROSE 12,000 TO 13,000 FT. MADE EMEMERGENCY DESCENT, RETURNED TO ATL. FOUND RIGHT PACK HEAT EXCHANGER BURST AND LEAKING. REPLACED HEAT EXCHANGER OPERATION NORMAL. 2L73 4F A3WE 19950526003671995052600367NM 1995 5 26 DL72W951988 119950508A5522 SKIN BOEING727 727247 138408FNM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112810W 20648 FOUND ON B2 LTR CK, .75 BY .625 HOLE LOWER SKIN RT ELEVATOR AFT NR 4 BALANCE BOARD. REPAIRED PER SRM 55-20-3. 2L73 4F A3WE 19950526003681995052600368NM 1995 5 26 DL72W952141 119950510A57536521630188 SKIN BOEING727 727247 138408FNM NR 3 TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 21327 LE SKIN WAS FOUND WORN APPOX 16 INCHES FROM IB END. DAMAGE WAS REPAIRED PER SRM 57574, BY INSTALLING A REPAIR DOUBLER. ALL THE ABOVE ACTION WAS DURING A SHOP VISIT, FOR NR 3 FORE FLAP. 2L73 4F A3WE 19950526003691995052600369NM 1995 5 26 DL733952183 119950518A5753 SKIN BOEING737 737347 1384647NM LT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11305WA 23346 FOUND DURING LETTER CHECK, NR 1 FORE FLAP UPPER SIDE MIDWAYS HAS GROVES CUT INTO THE SKIN. STARTED REPAIR PER SRM 57-53-02, REPAIR COMPLETED TESTS GOOD PAINTED TO MATCH. FOUND LOOSE FASTENER ON SPOILER SEAL CONTACTING FLAP TIGHTENED SAME NEEDS, FLAPS CYCLED TO CHK CLEARANCE. CLEARANCE CHECK GOOD. 2L72 4F RTA16WE 19950526003701995052600370NM 1995 5 26 DL73S951971 119950501A55326573783519 LE SKIN BOEING737 737232 1384475NM VERT STAB DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11316DL 23088 DURING SHOP INSPECTION, VERTICAL STABILIZER LEADING EDGE PANEL WAS REPAIRED FOR A DENT AT 51 INCHES FROM THE LOWER END OF PANEL. DAMAGE WAS REPAIRED PER SRM 55-30-6. 2L72 4F RTA16WE 19950526003711995052600371NM 1995 5 26 DL757951964 119950509A5754114N4004165A SKIN BOEING757 757232 1384965NM LT LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11659DL 24421 DURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH DELAMINATION OF THE T/E WEDGE AT THE SLAT SPAR. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950526003721995052600372NM 1995 5 26 DL757951965 119950430A5755 SKIN BOEING757 757232 1384965NM LT SPOILER DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11676DL 25981 DURING INSPECITON, LEFT WING SPOILER PANEL WAS FOUND WITH 6 PUNCTURE HOLES DUE TO HAIL DAMAGE. REPAIRED PER SRM 57-70-1. 2L72 4F RTA2NM 19950526003731995052600373NM 1995 5 26 DL757951966 119950430A5755 SKIN BOEING757 757232 1384965NM NR 4 SPOILER DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11676DL 25981 DURING INSPECTION, NR 4 SPOILER PANEL WAS FOUND WITH 2 PUNCTURES ON THE UPPER SKIN DUE TO HAIL DAMAGE. REPAIRED PER SRM 51-70-17. 2L72 4F RTA2NM 19950526003741995052600374NM 1995 5 26 DL757951967 119950430A5754 SKIN BOEING757 757232 1384965NM NR 2 LE SLAT DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11676DL 25981 DURING INSPECTION, NR 2 SLAT PANEL WAS FOUND WITH NUMEROUS DENTS IN T/E WEDGE DUE TO HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-002. 2L72 4F RTA2NM 19950526003751995052600375NM 1995 5 26 DL757951969 119950430A5751 SKIN BOEING757 757232 1384965NM LT AILERON DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11676DL 25981 LT WING AILERON HAS 10 HOLES ON UPPER SURFACE OF T/E WEDGE DUE TO HAIL DAMAGE. REPAIRED PER SRM 57-60-02 PG 202 TABLE 1. 2L72 4F RTA2NM 19950526003761995052600376NM 1995 5 26 DL757951970 119950430A5751 SKIN BOEING757 757232 1384965NM RT AILERON DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11676DL 25981 RT WING AILERON HAS 5 HOLES ON UPPER SURFACE DUE TO HAIL DAMAGE. REPAIRED DAMGE PER SRM 57-60-01 WITH REF TO SRM 51-70-4 AND SRM 51-70-05. 2L72 4F RTA2NM 19950526003771995052600377NM 1995 5 26 DL757951997 119950507A5754114N4003177A SKIN BOEING757 757232 1384965NM NR 2 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11659DL 24421 DURING SHOP INSPECTION, NR 2 SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-03. 2L72 4F RTA2NM 19950526003781995052600378NM 1995 5 26 DL757952118 119950504A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1640 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 FLOORBEAM CORRODED STA 1640 UPPER FLANGE. REMOVED CORR FROM UPPER FLANGE FWD FLANGE, WITHIN LIMITS PER SRM 53-00-51 FIG 101. DRILLED UP REPAIR, APPLIED ALODINE AND EPOCART 15-11 TO DAMAGED AREA PAINTED AND INSTALLED REPAIR. 2L72 4F RTA2NM 19950526003791995052600379NM 1995 5 26 DL757952119 119950504A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1661 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 FLOORBEAM CORRODED AT AFT GALLEY STA 1661 LBL 48 AND LBL 54C. REMOVED CORROSION FROM BEAM UPPER FLANGE .030 AT LBL 48 AND LBL 54. MANUF PARTS PER SRM, INSTALLED DOUBLERS. 2L72 4F RTA2NM 19950526003801995052600380NM 1995 5 26 DL757952147 119950515A5315 FLOORBEAM BOEING757 757232 1384965NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING HMV, FOUND FLOORBEAM CORRODED AT FS 720 BETWEEN LBL 14 AND BL 36. REPAIRED BY REMOVING CORROSION TREATED AND PAINTED LBL 14 AND RBL 36. INSTALLED REPAIR ANGLE AT RBL 3 AND 8. TREATED AND PAINTED PER PS 900-2-4-4 NR 02 AND PS 900-3-6 NR 03. INSTALLED REPAIR ANGLE AS PER SRM 53-30-51. 2L72 4F RTA2NM 19950526003811995052600381NM 1995 5 26 DL757952150 119950516A7110 SKIN BOEING757 757232 1384965NM NR 1 ENG COWL DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11637DL 23760 FOUND DURING LETTER CHECK, NOSE COWL L/E DAMAGED AT 5 O'CLOCK POS. ALSO, SMALL HOLES IN NOSE COWL 3 O'CLOCK POS. REPAIRED PER SRM 54-11-01. 2L72 4F RTA2NM 19950526003821995052600382NM 1995 5 26 DL757952201 119950514A5400 DOUBLER BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 NR 2 ENG PYLON CRACKED IN LWR AFT RADIUS OF FWD LIGHTNING HOLE INBD SIDE OF PYLON. REPAIRED PER SRM 54-51-01 PG 206 TO 211. 2L72 4F RTA2NM 19950526003831995052600383NM 1995 5 26 DL757952214 119950516A5315 FLOORBEAM BOEING757 757232 1384965NM FS 345 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 AT HMV, FLOORBEAM CORRODED AT FS 345 FROM 0BL TO LBL 18. CLEANED CORROSION, FOUND OUT OF LIMITS PER SRM 53-00-51 PG 103. MADE BEAM REPAIR PER SRM 53-30-51 PG 208. 2L72 4F RTA2NM 19950526003841995052600384NM 1995 5 26 DL757952217 119950515A5315 FLOORBEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 AT HMV, FS 324 FLOORBEAM IS CORRODED AT BL 0. REPAIRED PER SRM 53-00-51 AND SRM 53-10-08. 2L72 4F RTA2NM 19950526003851995052600385NM 1995 5 26 DL767951994 119950509A5754114T410222A SKIN BOEING767 767232 1385132NM NR 11 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 DURING INSPECTION, NR 11 L/E SLAT PANEL UPPER T/E WEDGE WAS FOUND DENTED. REPAIRED PER SRM 57-43-61. 2L72 4F RTA1NM 19950526003861995052600386NM 1995 5 26 DL767952128 119950430A5522 SKIN BOEING767 767232 1385132NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 AFTER HAIL STORM ELEVATOR WAS FOUND DAMAGED. REPAIRED AS PER SRM 55-20-01 REF ERA 270854-14. 2L72 4F RTA1NM 19950526003871995052600387NM 1995 5 26 DL76S952151 119950516A5330 SKIN BOEING767 767332 1382001NM FS 355 LIGHTNING STRIKEA DALAK NONE C F.O.D. ININSP/MAINT 1 SO11123DN 23437 FOUND DURING LETTER CHECK, LIGHTNING STRIKES ABOVE COCKPIT SECTION OF FUSELAGE. BURNISHED OUT DAMAGES, FOUND ONE LIGHTING STRIKE OUT OF LIMITS. REPLACED RIVETS STA 355 BETWEEN STR 3 AND 4R STA 400 STR 4R, STA 484 STR 3R. DYE CHECKED AREAS, TREATED AND PAINTED. OUT LIMIT REPAIR STA 460 STR 3 AND 4R REPAIRED PER SRM 53-00-01. 2L72 4F RTA1NM 19950526003881995052600388NM 1995 5 26 DL76S952238 119950519A323017014110CR0720S HOSE BOEING767 767332 1382001NM RT MLG LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11120DL 23279 AFTER TAKEOFF, RT MAIN LANDING GEAR WOULD NOT RETRACT, RETURNED MCO. FOUND RT MLG TRUCK TILT PRESSURE LINE BROKEN. REPLACED LINE OPERATION NORMAL. 2L72 4F RTA1NM 19950526003891995052600389WP 1995 5 26 DLL10952152 119950517A5743 ATTACH FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11722DA 193C1147 LMLG FWD ATTACH FITTING CORRODED FWD AND AFT LUG. BORED FWD LUG TO 2.726 AND AFT LUG TO 2.727 TO REMOVE CORROSION, SIZES WITHIN LIMITS PER SRM 57-14-00. 2L73 4F A23WE 19950526003901995052600390WP 1995 5 26 DLL10952206 119950411A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 AT HMV, RT CUSP ANGLE AT FLOOR LINE CRACKED, AT ATTACH FASTENERS TO FLOORBEAMS, FS 1103, 1123, 1143. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950526003911995052600391WP 1995 5 26 DLL13952173 119950510A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT 8.328, LBL 30. REMOVED BEAM FROM LBL 48 TO I/B END, FABRICATED DRILLED UP AND INSTALLED NEW BEAM, PER SRM 53-21-00 PG 823. 2L73 4F A23WE 19950526003921995052600392WP 1995 5 26 DLL13952174 119950510A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT FS 328 RBL 24 AT TIE DOWN. REMOVED BEAM FROM RBL 10 TO RBL 69. DRILLED UP NEW BEAM AND SPLICE ANGLES, INSTALLED NEW BEAM PER SRM 53-21-00 FIG 815. 2L73 4F A23WE 19950526003931995052600393WP 1995 5 26 DLL13952175 119950511A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1763 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT FS 1763 RBL 52. REMOVED BEAM, FABRICATED, DRILLED UP AND INSTALLED REPAIR PER SRM 53-21-00 PG 823. 2L73 4F A23WE 19950526003941995052600394WP 1995 5 26 DLL13952197 119950510A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1685 LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 DURING HMV, INSPECTION FOUND A TEAR STRAP LOOSE BETWEEN STA 1685 AND 1705 BETWEEN STR 39 AND 40. AREA CLEANED, SEALED AND RIVETED DOWN PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950526003951995052600395WP 1995 5 26 DLL13952208 119950510A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 297 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT FS 297 RBL 30 TO 36 FWD GALLEY. CLEANED CORROSION, DAMAGE OUT OF LIMITS, CUT AND DRILLED NEW CAP. FABRICATED PARTS PAINTED AND INSTALLED PER SRM 53-21-00. 2L73 4F A23WE 19950526003961995052600396WP 1995 5 26 DLL13952210 119950511A5320 INTERCOSTAL LKHEED1011 10113851 5265010WP FS 282-298 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND INTERCOASTAL CORRODED BETWEEN FS 282 TO 298. FABRICATED NEW INTERCOASTAL AND INSTALLED PER SRM 51-10-05. 2L73 4F A23WE 19950526003971995052600397WP 1995 5 26 DLL13952211 119950511A5313 STRINGER LKHEED1011 10113851 5265010WP FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND STRINGER 33 CORRODED AT FS 328. REMOVED STRINGER FROM S278 TO 328, FABRICATED NEW STRINGER AND SECTION INSTALLED PER SRM 53-13-00. 2L73 4F A23WE 19950526003981995052600398WP 1995 5 26 DLL13952212 119950511A5330 SPLICE STRAP LKHEED1011 10113851 5265010WP FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SPLICE STRAP CORRODED AT FS 328. REMOVED STRAP AT FS 300 TO 328. FABRICATED NEW STRAP, INSTALLED PER SRM 53-31-00. 2L73 4F A23WE 19950526003991995052600399WP 1995 5 26 DLL13952213 119950511A5330 STRAP LKHEED1011 10113851 5265010WP FS 1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FAILSAFE STRAP CORRODED IN C3 B/B, FS 1725 BETWEEN STR 33 AND 34. REMOVED STRAP FS 1725 FROM STR 33 TO 29. REMOVED DAMAGED, TREATED AND PAINTED PER PS 900-2 NR 5, INSTALLED PER SRM 53-31-00. 2L73 4F A23WE 19950526004001995052600400WP 1995 5 26 DLL13952220 119950511A5330 STRAP LKHEED1011 10113851 5265010WP FS 789 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FAILSAFE STRAP DISBONDED FWD SIDE FORMER FS STA 789 BETWEEN STR 28 AND 29. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950526004011995052600401WP 1995 5 26 DLL13952221 119950511A5320 DRAIN PAN LKHEED1011 10113851 5265010WP GALLEY DOOR AREACRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND MESG DRAIN PAN CRACKED AND BROKEN ABOVE DOOR TO LOWER GALLEY. PERFORMED REPAIR PER SRM 51-50-05 PG 16 TO 18. 2L73 4F A23WE 19950526004021995052600402WP 1995 5 26 DLL13952222 119950510A5320 PRESSURE DECK LKHEED1011 10113851 5265010WP NLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND 2 INCH CRACK IN NLG WHEEL WELL PRESSURE DECK AT CEILING TO SIDEWALL, WEB LT FS 409. DYE PENETRANT, INSP SHOWS VISIBLE CRACK. STOP DRILLED BOTH ENDS, FABRICATED NEW DOUBLER, INSTALLED DOUBLER PER SRM 53-11-00. 2L73 4F A23WE 19950526004031995052600403WP 1995 5 26 DLL13952223 119950511A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1665-1685 LIFTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FAILSAFE STRAP LIFTED FROM SKIN C-1 B/B BETWEEN FS 1665 TO 1685, STR 43 AND 44. REPAIRED PER SRM 51-31-00. 2L73 4F A23WE 19950526004041995052600404WP 1995 5 26 DLL13952224 119950503A5755 SPAR CAP LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 NR 2 SPOILER SUPPORT STRUCTURE, UPPER SPAR CAP CRACKED ABOVE INBD AND OTBD HINGE FITTINGS. REPAIRED SPAR CAP PER SRM 57-22-00 FIG 806. 2L73 4F A23WE 19950526004051995052600405WP 1995 5 26 DLL13952225 119950505A5755 ANGLE LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 DURING LETTER CHECK, FOUND ANGLE CRACKED, UPPER T/E CLOSE OUT PANEL ATTACH RIB Z ANGLE. A .5 INCH CRACK INTO SCREW HOLE JUST INBOARD OF NR 2 SPOILER ACTUATOR. REPAIRED PER SRM 57-22-00 PG 807, 808. 2L73 4F A23WE 19950526004061995052600406NM 1995 5 26 DLM88951978 119950508A5210 SKIN DOUG MD88 MD88 3023688NM C 1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11903DE 53380 FOUND ON C2 LETTER CHECK, C-1 DOOR EXTERIOR HANDLE CUTOUT. REPAIRED PER SRM 52-05 FIG 30. 2L72 4F RTA6WE 19950526004071995052600407NM 1995 5 26 DLM88952199 119950519A5400 ANGLE DOUG MD88 MD88 3023688NM NR 2 ENG PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11986DL 53313 NR 2 ENG PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED 1 INCH. FOUND DURING D-1 LTR CK TPAMM. REPAIRED PER SRM 54-04A FIG 4. 2L72 4F RTA6WE 19950526004081995052600408EU 1995 5 26 QXEA9500160 119950522A33501820 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 GEG - LAV EMERGENCY LIGHT INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950526004091995052600409WP 1995 5 26 SCNA95098 119950515A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP L 2 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 MID CABIN OVERHEAD EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED WALL MOUNTED EXIT LIGHT POWER SUPPLY AT L-2 DOOR AND PERFORMED SYSTEM CHECK PER 33-50-00. 2L73 4F A22WE 19950526004101995052600410WP 1995 5 26 SCNA95099 119950516A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP AFT EMER EXIT FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15571SC 46645 AFT EMERGENCY LIGHT POWER SUPPLY FAILS COCKPIT SELF-TEST. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPPLY (OVERHEAD) PER MM 33-51-01. OPS CHECKED GOOD. 2L73 4F A22WE 19950526004111995052600411WP 1995 5 26 SCNA95100 119950518A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15571SC 46645 AFT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK FOR AFT EMERGENCY LIGHTS. ALL LIGHTS TEST GOOD. 2L73 4F A22WE 19950526004121995052600412SW 1995 5 26 SWIA95581 119950519A2910 HYDRAULIC LINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT MLG WW FAILED A SWIAK NONE KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 NM072685L AC648 BOTH RED HYD LIGHTS ILLUMINATED AND HYDRAULIC PRESSURE DROPPED TO 400 PSI ON 10 MILE FINAL TO PHX. LIGHTS CAME ON BEFORE WE EXTENDED EITHER FLAP OR GEAR. FOUND BAD FLAIR ON .25 INCH LINE IN LEFT WHEEL WELL CAUSING LEAK. CUT OFF FLAIR AND REPLACED LINE. OPS AND LEAK CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950526004131995052600413NM 1995 5 26 95ZZZM1 119950419A57546546421214 SKIN BOEING737 737297 1384480NM NR 6 LE SLAT DELAMINATED A ZZDAK NONE O OTHER TXTAXI/GRND HDL 1 SO17462AT 22631 ON 4-18-95, THE PILOT IN COMMAND OF A/C FOUND NR 6 LE SLAT DELAMINATED DURING PREFLIGHT AT CVG. MAINTENANCE CONTROL CONTACTED AN EMERGENCY MAINTENANCE CREW TO EVALUATE THE DAMAGE. PER BOEING SPECS, THE AIRCRAFT WAS FERRIED TO MCO FOR MAINTENANCE. THE NR 6 LE SLAT WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 19950526004141995052600414NM 1995 5 26 95ZZZM2 119950505A2820 FUEL SHUTOFF VLV BOEING747 747122 1384872NM NR 3 ENGINE FAILED A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23853FT 19753 FLT 81 - HNL - ON CLIMB-OUT NR 3 ENGINE FUEL SHUTOFF VALVE INTRANSIT LIGHT ILLUMINATED BRIGHT, ENGINE SHUT DOWN. REWIRED VALVE CIRCUIT WIRING FROM WING ROOT TO VALVE. REPLACED FUEL SHUTOFF VALVE ACTUATOR MOTOR. SYSTEM CHECKED NORMAL. (M) 2L74 4F A20WE 19950526004151995052600415NM 1995 5 26 95ZZZM3 119950407A5330 SKIN BOEING747 747121 1384871NM BS 1740-1960 MISDRILLED A P5CAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP23830FT 19642 DURING STRUCTURAL INSPECTION REQUIRED BY AD 95-01-04, MISDRILLED AND PLUGGED FUSELAGE SKIN WAS FOUND BETWEEN BS 1740 AND 1960 AT STRINGER 4. REPAIR ACCOMPLISHED PER FAA APPROVED DRAWING POLAR 747 53-830-1. AIRCRAFT RELEASE FOR SERVICE. 2L74 4F A20WE 19950526004161995052600416NM 1995 5 26 95ZZZM4 119950506A242536R17D TEMP BULB SUNDSTRANDEM705117G BOEING747 747122 1384872NM NR 1 CSD FAILED A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23854FT 19754 FLT 281 - JFK - AIR TURN BACK, AFTER TAKEOFF NR 1 CSD TEMPERATURE HIGH RISE OUT ALSO HIGH. NR 4 CSD ALREADY PLACARDED. REPLACED NR 1 CSD OUT TEMPERATURE BULB OPERATIONAL CHECK OK. RECONNECTED NR 4 CSD, CLEANED AND SECURED MAIN DISCONNECT CANNON PLUG. OPERATIONAL CHECK OK. (M) 2L74 4F A20WE 19950526004171995052600417NM 1995 5 26 95ZZZM5 119950425A5754 SKIN BOEING747 747121 1384871NM NR 4 LE FLAP CREASED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 DURING ROUTINE MAINTENANCE CHECK, GROUND DAMAGE OCCURRED TO THE FOLDING NOSE SKIN OF THE NR 4 LEADING EDGE VARIABLE CAMBER FLAP. FLAP REPAIRED PER 747 SRM 57-50-03. REPAIR DEVIATED FROM SRM. DER APPROVED REPAIR FOR 50 HOUR LIMIT. FOLDING NOSE ASSY REPLACED IN JFK ON 4-27-95. AIRCRAFT RELEASED FOR SERVICE. 2L74 4F A20WE 19950526004181995052600418NM 1995 5 26 95ZZZM6 119950424A5512 SKIN BOEING747 747121 1384871NM LT ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 DURING SERVICE CHECK, FOUND OUTBOARD ELEVATOR UPPER SKIN DELAMINATED. REPAIRED PER SRM 51-40-09 FIG B-200 DEGREES WET LAYUP. REPAIR IS CLASSIFIED AS TIME LIMITED. PERMANENT REPAIR MUST BE ACCOMPLISHED PER SRM 51-40-12 AT NEXT C-CHECK NOT TO EXCEED 18 MONTHS. (M) 2L74 4F A20WE 19950526004191995052600419NM 1995 5 26 95ZZZM7 119950427A5230A523H03171 LOCK ARM BOEING747 747121 1384871NM CARGO DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 AT JFK, WHILE OPENING MAIN DECK CARGO DOOR, FOUND NR 11 AND NR 12 DOOR LATCH LOCK ARMS CRACKED. REPLACED LOCK ARMS PER GATX MM 52-32-00. AIRCRAFT RELEASED FOR SERVICE. 2L74 4F A20WE 19950526004201995052600420NE 1995 5 26 95ZZZM8 219950509A7250 TURBINE SLEEVE BOEING747 747122 1384872NM PWA JT9 JT9D7 52054NE NR 3 ENGINE BUCKLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662315 NR 3 ENGINE TURBINE SLEEVE BUCKELED ALONG LEADING EDGE 6 AND 9 O'CLOCK POSITION. REPAIRED IAW SRM 51-40-2 AND 51-10-01. (M) 2L74 4F4 F A20WE E20EA 19950526004211995052600421NM 1995 5 26 95ZZZM9 119950508A2897 WIRE BOEING747 747122 1384872NM FUEL SHUTOFF FAILED A P5CAO OTHER J WARNING INDICATION CRCRUISE 1 WP23853FT 19753 NR 3 ENGINE FUEL SHUTOFF VALVE INTRANSIT LIGHT ON BRIGHT, ENGINE CONTINUED TO RUN. REPLACED ALL FUSELAGE FUEL SHUTOFF VALVE WIRING (PREVIOUSLY REPLACED ALL WING SHUTOFF VALVE WIRING). REPLACED FUEL SHUTOFF VALVE ACTUATOR AND INDICTION RELAY PRECAUTIONARY. 2L74 4F A20WE 19950526004221995052600422EU 1995 5 26 C2XA95IA072 119950505A5320S53575102206 DOUBLER AEROSPATR42 ATR42320 8680930EU LT MLG WW CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0925811 094 DURING A SCHEDULED INSPECTION, THE DOUBLER OVER THE LEFT MAIN WHEEL WELL STRAP WAS FOUND TO BE CRACKED, REF NDT MANUAL 53-51-26. MAINTENANCE REMOVED CRACKED PORTION OF DOUBLER AND A FILLER WAS INSTALLED. A REPAIR DOUBLER WAS INSTALLED PER ATR REPAIR DWG NR 15S53R0045 AND COEX EC 5340-01023. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950526004231995052600423SO 1995 5 26 C2XA95IA077 119950511A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 4TH LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950526004241995052600424SO 1995 5 26 C2XA95IA078 119950511A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 15 3RD LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950526004251995052600425SO 1995 5 26 C2XA95IA079 119950511A532012005735001 ANGLE EMB 120 EMB120RT SO CARGO UPPER CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN TO FRAME ATTACH ANGLE CRACKED AT BOTH ENDS, FRAME 44 BETWEEN STRINGERS NR 1 LEFT AND NR 1 RIGHT. MAINTENACNE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950526004261995052600426WP 1995 5 26 HAL95051 119950503A5320NCA624627 SUPPORT BEAM DOUG DC10 DC1010 3022110WP FS 578 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13146AA 46701 LAX - ITEM WAS DISCOVERED DURING GENERAL (WALKAROUND) IN LAX. CHECK B-17, CARD 0096, VISUAL WAS CONFIRMED WITH DYE PENETRANT. SIX CRACKS .5 TO 1 INCH LONG OUT OF RIVET HOLES AND SLIGHT WEB WAVINESS ACROSS AREA AT ABOUT 35 DEGREES ANGLE FROM HORIZONTAL FORWARD AND DOWN IN NOSE WHEEL WELL LEFT SIDE APPROX Y578. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-30-00 FIG 6. (M) 2L73 4F A22WE 19950526004271995052600427WP 1995 5 26 HAL95052 119950503A5320NCA624628 SUPPORT BEAM DOUG DC10 DC1010 3022110WP FS 578 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13146AA 46701 LAX - ITEM WAS DISCOVERED DURING GENERAL CHECK (WALKAROUND) IN LAX. CHECK B-17, CARD 0096. VISUAL WAS CONFIRMED WITH DYE PENETRANT. THREE CRACKS .375 TO .75 INCH LONG OUT OF RIVET HOLES AND SLIGHT WEB WAVINESS ACROSS AREA AT ABOUT 35 DEGREE ANGLE FROM HORIZONTAL FORWARD AND DOWN IN NOSE WHEEL WELL RT SIDE APPROX Y578. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-30-00 FIG 6. (M) 2L73 4F A22WE 19950526004281995052600428WP 1995 5 26 HAL95053 119950426A5320NCA624628 SUPPORT BEAM DOUG DC10 DC1010 3022110WP FS 578 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13153AA 46708 ITEM WAS DISCOVERED DURING GENERAL CHECK (WALKAROUND) IN LAX. CHECK B-4, VISUAL WAS CONFIRMED WITH DYE PENETRANT. 2 CRACKS .125 - .25 INCH LONG OUT OF RIVET HOLES AND SLIGHT WEB WAVINESS ACROSS AREA AT ABOUT 35 DEGREE ANGLE FROM HORIZONTAL FORWARD AND DOWN IN NOSE WHEEL WELL RT SIDE APPROX Y578. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-30-00 FIG 6. (M) 2L73 4F A22WE 19950526004291995052600429NM 1995 5 26 MGMA950177 119950413A3260 SWITCH BOEING727 727191 1384063NM LT MLG DEFECTIVE A MGMAK NONE O OTHER ININSP/MAINT 1 WP23503MG 19392 AFTER LANDING, TAKEOFF WARNING HORN SOUNDED WITH SPEED BRAKE HANDLE FULLY UP AND FLAPS 25 DEGREES. REMOVED AND REPLACED LEFT GEAR SAFETY SWITCH. OPS CHECK PER MM 32-07-211 OK. (M) 2L73 4F A3WE 19950526004301995052600430NM 1995 5 26 MGMA950187 119950504A3350900835A EEL BATT PACK BOEING727 727191 1384063NM LT OVERWING DISCHARGED A MGMAK NONE L NO TEST ININSP/MAINT 1 WP23504MG 9097 19395 LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND OPS RESTORED TO NORMAL. 2L73 4F A3WE 19950526004311995052600431WP 1995 5 26 USAA950430 119950319A532059101423 DOOR PAN DOUG DC9 DC981 3022081WP CARGO COMPT CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19802US37968 48036 IND - DURING CD-2 INSPECTION, FOUND CORROSION ON AFT SIDE OF FORWARD DOOR STOP FITTING IN LOWER SILL PAN. CUT OUT CORRODED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 44 AND USAIR EA 29986. (M) 2L72 4F A6WE 19950526004321995052600432EU 1995 5 26 USAA950431 119950330A5312 BEAM FOKKERF28 F28MK4000 4990810EU FS 17065 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING SCHEDULED SIP VISIT, FOUND 1.5 INCH CRACK IN REAR PRESSURE BULKHEAD STATION 17065 HORIZONTAL BEAM NR 3 AT BL 425 RT HIGH FREQUENCY EDDY CURRENT INSPECTION SIP REF 53-10-03. STOP DRILLED CRACK AND INSTALLED ANGLE AND DOUBLER REPAIR PER USAIR EA 30104. 2L72 4F RTA20EU 19950526004331995052600433EU 1995 5 26 USAA950432 119950329A5330 SKIN FOKKERF28 F28MK4000 4990810EU DOOR OPENING CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING SCHEDULED SIP VISIT, FOUND .5 INCH CRACK SERVICE EMERGENCY DOOR APERTURE AFT LOWER CORNER EDDY CURRENT INSPECTION REF SIP 53-10-20. ACCOMPLISHED SHEET METAL REPAIR PER SRM 53-02-16 PG 7, 8 AND 11. (M) 2L72 4F RTA20EU 19950526004341995052600434EU 1995 5 26 USAA950433 119950321A5330 SKIN FOKKERF28 F28MK4000 4990810EU NLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING SCHEDULED SIP VISIT, FOUND .25 INCH CRACK 2 EACH FUSELAGE SKIN JUST FORWARD OF RT CORNER NOSE WHEEL WELL CUTOUT, EDDY CURRENT INSPECTION SIP REF 53-10-24. INSTALLED REPAIR PER SRM 53-02-18 FIG 10. (M) 2L72 4F RTA20EU 19950526004351995052600435EU 1995 5 26 USAA950434 119950324A5347 TRACK FOKKERF28 F28MK4000 4990810EU FS 197-237 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED LEFT INBOARD SEAT TRACK STATION 197-237. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2L72 4F RTA20EU 19950526004361995052600436EU 1995 5 26 USAA950435 119950324A5330 SKIN FOKKERF28 F28MK4000 4990810EU FS 347 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH SKIN CRACK AT RIVET HEAD STATION 347 BETWEEN LONGERON 23L AND 24L. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 38. (M) 2L72 4F RTA20EU 19950526004371995052600437EU 1995 5 26 USAA950436 119950322A5330 SKIN FOKKERF28 F28MK4000 4990810EU FS 219 DENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 CHECK INSPECTION, FOUND DENT OUT OF LIMITS JUST AFT OF NOSE JACK PAD STATION 218 LONGERON 30. INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 EFG. (M) 2L72 4F RTA20EU 19950526004381995052600438EU 1995 5 26 USAA950437 119950322A5330 SKIN FOKKERF28 F28MK4000 4990810EU AFT OF NLG DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 INSPECTION, FOUND TEMPORARY REPAIR INSTALLED RT AFT NOSE GEAR DOOR HINGE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-09. (M) 2L72 4F RTA20EU 19950526004391995052600439EU 1995 5 26 USAA950438 119950324A5320 FITTING FOKKERF28 F28MK4000 4990810EU FS 691 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT BOLT HOLE AT REAR SPAR KEEP FITTING STATION 691 LEFT WHEEL WELL. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (M) 2L72 4F RTA20EU 19950526004401995052600440EU 1995 5 26 USAA950439 119950322A5330 SKIN FOKKERF28 F28MK4000 4990810EU BS 229 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU19670 11229 PIT - DURING Q-3 CHECK INSPECTION, FOUND TEMPORARY REPAIR INSTALLED STATION 229 LONGERON 17L TO LONGERON 18L. INSTALLED FLUSH REPAIR PER SRM 53-04 FIG 47. (M) 2L72 4F RTA20EU 19950526004411995052600441EU 1995 5 26 USAA950442 119950428A3231 RETRACT MECH FOKKERF28 F28MK4000 4990810EU LT/RT MLG DOOR LACK OF LUBE A USAAJ DUMP FUEL O OTHER CLCLIMB 1 EA19476US 11224 MIA - FLT 1798 - AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR RED LIGHT ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. MAINTENANCE LUBRICATED THE LINKAGES AT THE LEFT DOOR LOCK MECHANISM AND ADJUSTED THE RIGHT GEAR DOOR LOCK MECHANISM AND SWITCHES. GEAR INDICATION SYSTEM CHECKS NORMAL. (M) 2L72 4F RTA20EU 19950526004421995052600442WP 1995 5 26 USAA950443 119950428A3350 EEL ASSY DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19916VJ 47023 CLT - FLT 1727 - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY LIGHT ASSEMBLY. (M) 2L72 4F A6WE 19950526004431995052600443WP 1995 5 26 USAA950444 119950428A3350 EEL BATT PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19967VJ 47375 BOS - FLT 2493 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950526004441995052600444EU 1995 5 26 USAA950445 119950504A5610 WINDSHIELD FOKKERF28 F28MK0100 4990807EU LEFT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19869US 11314 PIT - FLIGHT NR 0403 - ON CLIMB-OUT, A CRACK DEVELOPED IN THE CAPTAINS WINDSHIELD. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. (M) 2L72 4F RT 19950526004451995052600445NM 1995 5 26 USAA950449 119950429A3230 PIN BOEING737 7372B7 1384560NM NLG NOT REMOVED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19270AU 22882 BDL - FLT 2074 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. CREW RECYCLED GEAR AND NOSE GEAR STILL WOULD NOT RETRACT. FLIGHT RETURNED TO BDL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NOSE GEAR RETRACT PIN INSTALLED. REMOVED AND INSTALLED IN FLIGHT DECK. OK FOR SERVICE. (M) 2L72 4F A16WE 19950526004461995052600446EU 1995 5 26 USAA950450 119950507A27803G4203A SENSOR FOKKERF28 F28MK0100 4990807EU LE FLAPS FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19859US 11293 MCO - FLT 0244 - AFTER TAKEOFF, THE CAPTAIN RECEIVED A FLAP DISAGREEMENT LIGHT. THE FLAPS WERE RECYCLED BUT THE INDICATAION STILL REMAINED. MAINTENANCE REPLACED THE FLAP LEVER RVDT. ALL TEST CHECKED GOOD. (M) 2L72 4F RT 19950526004471995052600447EU 1995 5 26 VTZA95161 119950508A21701375527 WATER SEPARATOR BAG JETSTMJETSTM3201 1500217EU CABIN DIRTY A VTZAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27496UE 900 HPN/IAD - FLT 6388 - DURING CRUISE AT 1739 ON 5-8-95, A STRONG OIL SMELL WAS COMING FROM BOTH FLOWS. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED WATER SEPARATOR SOCKS. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950526004481995052600448EU 1995 5 26 VTZA95162 119950509A523091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU POD DOOR OUT OF ADJUST A VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27310UE 41028 FLT NR 6444 - IAD-RIC - ABORTED THE TAKEOFF DUE TO THE POD DOOR LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03339 IAW MEL 52-3 ON THE DOOR WARING SYSTEM. MAINTENACNE LATER CLEARED DMI NR 03339 ON 5-9-95 BY ADJUSTING THE MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950526004491995052600449EU 1995 5 26 VTZA95163 119950509A3233AIR864960 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27313UE 41026 FLT 6181 - IAD-BWI - DURING CLIMB-OUT, RETURNED TO IAD DUE TO RIGHT MAIN GEAR NOT RETRACTING WHEN THE GEAR SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE BLED THE RT MAIN GEAR RETRACTION ACTUATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950526004501995052600450EU 1995 5 26 VTZA95165 119950509A2810457101512 FUEL CAP BAG JETSTMJETSTM3201 1500217EU RT WING LOOSE A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27470UE 814 FLT 6909 - LYH-IAD - DURING CLIMB-OUT, RETURNED TO LYH DUE TO THE RT FUEL CAP COMING UNSECURED IN FLIGHT. AIRCRAFT RETURNED TO LYH WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AREA AND RESECURED CAP. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950526004511995052600451WP 1995 5 26 VTZA95166 219950510A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LEFT MALFUNCTIONED A VTZAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA27476UE 884 P66048 FLT 6598 - IAD-RDU - DURING CRUISE DECLARED AN EMERGENCY AND DIVERTED TO LYH DUE TO THE LEFT ENGINE SURGING WITH AN INDICATED TORQUE OF 120 PERCENT AND ASSOCIATED YAW. CREW SHUT DOWN ENGINE. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. LYH IN CURRENTLY CHANGING ENGINE. (M) 2L72 4T4 TRTA56EU E4WE 19950526004521995052600452WP 1995 5 26 VTZA95167 219950510A732189778025 FUEL CONTL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27475UE 850 P66078 FLT 6362 - SYR-IAD - TAKEOFF ABORTED DUE TO THE LEFT ENGINE MAKING ONLY 65 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED AND REPLACED THE FUEL CONTROL UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950526004531995052600453EU 1995 5 26 VTZA95168 119950509A2611 SMOKE DET BAG JETSTMJETSTM3201 1500217EU BAGG COMPT DIRTY A VTZAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA27474UE 849 FLT 6583 - SWF-BOS - DURING TAXI FOR TAKEOFF RETURNED TO GATE DUE TO THE MAIN BAGGAGE SMOKE LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE SMOKE DETECTOR CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950526004541995052600454SO 1995 5 26 WTAA950173 119950425A21332093K010800 VALVE OUTFLOW EMB 120 EMB120RT SO FS 16128 FAILED A WTAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 WP17281UE 120092 SFO - EN ROUTE RDM TO SFO, FAILURE OF PRESSURIZATION SYSTEM 'AUTO' MODE REPORTED. CREW REPORTED LIMITED PRESSURIZATION CONTROL AVAILABLE IN 'MANUAL' MODE. AIRCRAFT DESCENDED TO LOWER ALTITUDE. DURING DESCENT, CABIN OXYGEN MASKS DEPLOYED (14,000 FT SWITCH). MASKS WERE NOT UTILIZED AS AIRCRAFT CONTINUED FLIGHT IN UNPRESSURIZED CONFIGURATION. MAINTENANCE REPLACED PNEUMATIC OUTFLOW VALVE AND RESTOWED OXYGEN MASKS. PRESSURIZATION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950526004551995052600455SO 1995 5 26 WTAA950174 119950427A323012038594001 CONTROL MODULE EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAAO OTHER J WARNING INDICATION CLCLIMB 1 WP17276UE 120067 FAT - LANDING GEAR SELECTION HANDLE WOULD NOT MOVE TO THE 'GEAR UP' POSITION ON LANDING GEAR RETRACTION AFTER TAKEOFF. CREW USED GEAR OVERRIDE TO SELECT GEAR UP. MAINTENANCE REPLACED LANDING GEAR CONTROL MODULE. LANDING GEAR EXTENSION/RETRACTION OPERATION CHECKS NORMAL ON GROUND AND SUBSEQUENT TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950526004561995052600456EU 1995 5 26 WTAA950175 119950426A261251653151 FIRE DETECTOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE FAILED A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17424UE 796 ACV - RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED ENGINE. DETERMINED FIRE INDICATION TO BE FALSE INDICATION. REPLACED FIRE DETECTOR CONTROL UNIT. ENGINE FIRE DETECTION SYSTEM OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950526004571995052600457SO 1995 5 26 WTAA950178 119950429A3150922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO ELEVATOR LOOSE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17120AM 120012 MRY - TAKEOFF TRIM AURAL WARNING OBTAIN DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENACNE COULD NOT DUPLICATE DISCREPANCY. INSPECTED SYSTEM FOUND ELECTRICAL CONNECTOR AT TRIM PROXIMITY SENSOR LOOSE. TIGHTENED CONNECTION. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950526004581995052600458EU 1995 5 26 WTAA950179 119950430A261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU BAGGAGE COMPT MALFUNCTIONED A WTAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP17107XV 723 SFO - 'SMOKE' CAPTION ILLUMINATED DURING AIRCRAFT TAXI OUT FOR TAKEOFF. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED BAGGAGE COMPARTMENT SMOKE DETECTOR. SMOKE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950526004591995052600459SO 1995 5 26 WTAA950180 119950430A3620 LEAK LIGHT EMB 120 EMB120RT SO BLEED AIR ILLUMINATED A WTAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP17250YV 120250 PSP - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. CREW SHUTOFF RIGHT ENGINE BLEED AIR VALVE. LIGHT REMAINED ON. CREW SECURED RIGHT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLEED AIR SYSTEM, WITH NO EVIDENCE OF AIR LEAK NOTED. DEFERRED RIGHT ENGINE BLEED 'DUCT LEAK' LIGHT PER MEL 36-21-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950526004601995052600460SO 1995 5 26 WTAA950181 119950502A3350MS277892K EEL SWITCH WIRE EMB 120 EMB120RT SO CABIN CHAFED A WTAAK NONE L NO TEST CRCRUISE 1 WP17216YV 120216 SFO - EMERGENCY LIGHTING CAME ON DURING FLIGHT. EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED AFTER LIGHT ACTIVATION. UNABLE TO RESET CIRCUIT BREAKER. MAINTENANCE DEFERRED EMERGENCY LIGHTING SYSTEM PER ;MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY REPAIRED CHAFED WIRE AT FLIGHT ATTENDANTS EMERGENCY LIGHT CONTROL SWITCH. CABIN EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA31SO 19950526004611995052600461NM 1995 5 26 9508216625 119950520A3230 LINE BOEING747 747251B 1384892NM RT MLG CHAFED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01625US 21707 DURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND BOTH PRIMARY AND ALTERNATE GEAR WOULD NOT RETRACT. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND MADE AN UNEVENTFUL LANDING IN MNL. MAINTENANCE FOUND RIGHT TILT ACTUATOR HYDRAULIC LINE CHAFED. REPLACED LINE AND PERFORMED LEAK CHECK. UNIT CHECKED NORMAL. 2L74 4F A20WE 19950526004621995052600462NM 1995 5 26 9508226625 119950520A3230 RETRACT MECH BOEING747 747251B 1384892NM RT MLG REQD SERVICE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01625US 21707 DURING CLIMB, THE RIGHT BODY GEAR TILT LIGHT ILLUMINATED AND GEAR WOULD NOT RETRACT IN BOTH PRIMARY AND ALTERNATE. CREW FOLLOWED COCKPIT OPERATING MANUAL AND PROCEEDED FOR LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE BLED THE SYSTEM AND RECYCLED CIRCUIT BREAKER. AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19950526004631995052600463WP 1995 5 26 9508231227 119950523A2780 WARNING HORN DOUG DC10 DC1030 3023501WP FLAP/SLAT SYST SOUNDED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01227NW 46969 DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED WITH AN AMBER SLAT DISAGREEMENT LIGHT ILLUMINATED, ABORTED TAKEOFF. RECYCLED FLAP/SLAT AND TAKEOFF WARNING SYSTEM OPERATIONALLY CHECKED OK. 2L73 4F A22WE 19950526004641995052600464WP 1995 5 26 9508241158 119950504A5312 BULKHEAD DOUG DC10 DC1040 3023508WP FS 1156 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01158US 46767 DURING PERIODIC CHECK, FOUND CORROSION ON THE CENTER ACCESS PRESSURE BULKHEAD FS 1156 AT LONGERON 43R. REPAIRED PER EA 11-98042. 2L73 4F A22WE 19950526004651995052600465WP 1995 5 26 9508259916 119950509A5320 BEAM DOUG DC9 DC932 3022066WP FS 1039-1059 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING PERIODIC CHECK, FOUND CRACK IN THE TAIL SKID BEAM FORWARD RIGHT END FS 1039 TO 1059. REPAIRED PER EA 99-088139, MFG PART NUMBER 9919660-4. 2L72 4F A6WE 19950526004661995052600466NM 1995 5 26 9508262707 119950511A5313 LONGERON BOEING727 727225 1384077NM FS 970-1010 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01816EA 22553 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 29L BETWEEN FS 970 TO 1010. REPAIRED LONGERON P/N 65-56441-3, PER EA 27-98377. 2L73 4F A3WE 19950526004671995052600467WP 1995 5 26 9508279989 119950512A5320 FRAME DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE AFT CARGO DOOR JAMB INTERNAL DOUBLER. REPAIRED PER EA 99-094819, MFG PART NUMBER 5910158-25. 2L72 4F A6WE 19950526004681995052600468NM 1995 5 26 9508282707 119950512A5753 CHORD BOEING727 727225 1384077NM LT TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01816EA 22553 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT INBOARD MID FLAP UPPER MID SPAR T-CHORD WBL 70.6. REPAIRED PER EA 27-098378. 2L73 4F A3WE 19950526004691995052600469WP 1995 5 26 9508299874 119950515A5320 SUPPORT DOUG DC9 DC951 3022051WP FS 237-299 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01783NC 48108 DURING PERIODIC CHECK, FOUND CORROSION ON FLOOR SUPPORT CAP FS 237 TO 299, BL 0. REPAIRED CAP P/N 5910760-23 PER EA 98-097524. 2L72 4F A6WE 19950526004701995052600470WP 1995 5 26 9508309916 119950516A5330 SKIN DOUG DC9 DC932 3022066WP FS 568 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING PERIODIC CHECK, FOUND CORROSION IN EXTERNAL FUSELAGE SKIN FS 568, LONGERON 29L TO 29R. REPAIRED PER EA 99-097539, MFG PART NUMBER 5911412-113. 2L72 4F A6WE 19950526004711995052600471WP 1995 5 26 9508319304 119950516A5320 DOOR JAMB DOUG DC9 DC982 3022082WP CARGO COMPT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01931MC 48057 DURING PERIODIC CHECK, FOUND CORROSION ON THE MID CARGO LOWER DOOR JAMB BEAM. REPAIRED BEAM P/N 5936038-1 PER EA 93-98421. 2L72 4F A6WE 19950526004721995052600472NM 1995 5 26 9508325527 119950517A5414 SKIN BOEING757 757251 1384970NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01527US 23842 DURING PERIODIC CHECK, FOUND A ONE INCH CRACK IN THE NR 1 ENGINE NACELLE STRUT SKIN PANEL, NACELLE STA 115. REPAIRED PANEL P/N 311N3450-11, -13, -15 PER EA 55-98479. 2L72 4F RTA2NM 19950526004731995052600473WP 1995 5 26 9508339959 119950518A5320 FITTING DOUG DC9 DC931 3022065WP FS 598 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING PERIODIC CHECK, FOUND CRACK IN LONGERON 30 END FITTING AT FS 598. REPLACED FITTING PER SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526004741995052600474WP 1995 5 26 9508349959 119950518A5320 FITTING DOUG DC9 DC931 3022065WP FS 620 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING PERIODIC CHECK, FOUND CRACK IN THE FORWARD KEEL FITTING ON LONGERON 30, FS 620. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950526004751995052600475WP 1995 5 26 9508359604 119950518A5320 FITTING DOUG DC9 DC932 3022066WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN SUPPORT FITTINGS FS 604 AT LONGERONS 23L AND 23R. REPLACED FITTINGS P/N 591297-213, 5912797-1 AND REPAIRED PER EA 5344-4A0008. 2L72 4F A6WE 19950526004761995052600476WP 1995 5 26 9508369886 119950518A5312 FITTING DOUG DC9 DC951 3022051WP FS 1292 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01600TR 47783 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN THE CANTED BULKHEAD TO VENTRAL STAIR OPENING ATTACH FITTING FS 1292, LEFT SIDE WEB. REPLACED FITTING P/N 3957175-501 PER SRM 51-30-5. 2L72 4F A6WE 19950526004771995052600477WP 1995 5 26 9508379965 119950518A5755 SUPPORT DOUG DC9 DC931 3022065WP SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01911RW 47149 DURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD SPOILER INBOARD TORSION BAR SUPPORT. REPLACED SUPPORT AND FOUND A CRACK IN THE RIGHT SPOILER SPLICE BAR. REPLACED SPLICE BAR. 2L72 4F A6WE 19950526004781995052600478WP 1995 5 26 9508389942 119950518A5313 LONGERON DOUG DC9 DC932 3022066WP FS 160 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING PERIODIC CHECK, FOUND A CRACK COMPLETELY THROUGH LONGERON 25L AT FS 160. REPAIRED LONGERON PER SRM 53-02, FIG 2. 2L72 4F A6WE 19950526004791995052600479WP 1995 5 26 9508399140 119950519A5320 FITTING DOUG DC9 DC914 3022034WP FS 525 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL FITTING FS 525. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950526004801995052600480NM 1995 5 26 9508406622 119950519A5711 CHORD BOEING747 747251B 1384892NM WS 1019-1027 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01622US 21704 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING FRONT SPAR WEB FSSI 1023 AND ON THE LOWER T-CHORD AT FSSI 1019 AND 1027. REPAIRED PER EA 66-98527. 2L74 4F A20WE 19950526004811995052600481WP 1995 5 26 9508419886 119950520A5320 FITTING DOUG DC9 DC951 3022051WP FS 1292 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01600TR 47783 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 17R END FITTING AT FS 1292. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950526004821995052600482WP 1995 5 26 9508429140 119950520A5343 FITTING DOUG DC9 DC914 3022034WP FS 585 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL TO MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING FS 585. REPLACED FITTING P/N 9915511-5 PER DWG 9910164. 2L72 4F A6WE 19950526004831995052600483WP 1995 5 26 9508439916 119950521A5320 ANGLE DOUG DC9 DC932 3022066WP LAVATORY CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING PERIODIC CHECK, FOUND CORROSION IN FUSELAGE CUSP ANGLE LEFT LAV, LOWER AFT END. REPAIRED PER EA 99-099776. 2L72 4F A6WE 19950526004841995052600484NM 1995 5 26 95UAL747036 119950523A2910 HYD LINE BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE NR 1 HYD SYST DAMAGED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 WP29164UA 21657 CREW REPORTS LOSS OF NR 1 HYDRAULIC SYSTEM. TIRE TREAD THROWN FROM WHEEL 4F ON TAKEOFF. RESULTANT DAMAGE TO LEFT BODY GEAR AND SPOILER HYDRAULIC LINE. REPLACED HYDRAULIC LINE. 2L74 4F4 F A20WE E20EA 19950526004851995052600485WP 1995 5 26 ABXA9500471 119950412A53209955840505 TRAP PANEL DOUG DC9 DC941 302207NWP FS 756 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER. REPLACED LEFT TAPEZOIDAL PANEL IAW DC-9 SB 53-182. 2L72 4F A6WE 19950526004861995052600486WP 1995 5 26 ABXA9500472 119950308A323129242891 BUSHING DOUG DC9 DC941 302207NWP FS 756 MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT MAIN LANDING GEAR FLYING DOOR HAD ONE MISSING BUSHNG IN THE HINGE LOBE. INSTALLED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950526004871995052600487WP 1995 5 26 ABXA9500473 119950315A53305911412221 SKIN DOUG DC9 DC941 302207NWP FS 617 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FUSELAGE SKIN REPAIR AT FS 617 BETWEEN LONGERONS 28R AND 28L NOT IAW DC-9 SRM. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11104-MR. 2L72 4F A6WE 19950526004881995052600488WP 1995 5 26 ABXA9500474 119950328A5330591140659 SKIN DOUG DC9 DC941 302207NWP FS 198 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK INDICATION COMING OUT OF AFT LOWER PRESSURE STOP HOLE ON THE FORWARD ENTRY DOOR JAMB. REPAIRED SKIN AT FORWARD ENTRY DOOR IAW ABX REA D953-11122-MR. 2L72 4F A6WE 19950526004891995052600489WP 1995 5 26 ABXA9500475 119950325A532099578383 INTERCOSTAL DOUG DC9 DC941 302207NWP FS 184 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN ANGLE GOUGED AT FS 184 AND LBL 56, ABOVE THE AIR STAIR DOOR SWITCH. REPAIRED INTERCOSTAL IAW ABX REA D953-11252-MR. 2L72 4F A6WE 19950526004901995052600490WP 1995 5 26 ABXA9500476 119950331A5730591046522 SKIN DOUG DC9 DC941 302207NWP WS 64 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING LOWER SKIN GOUGED AND CHAFED AT TRAILING EDGE, OUTBOARD OF THE MAIN LANDING GEAR DOOR JAMB. REPAIRED RIGHT WING LOWER SKIN IAW ABX REA D957-11255-MR. 2L72 4F A6WE 19950526004911995052600491WP 1995 5 26 ABXA9500477 119950327A5330592032379 SKIN DOUG DC9 DC941 302207NWP FS 440-462 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR BETWEEN FS 440 AND 462, FROM LONGERON 24L AND 25L WAS GOUGED AND DOUBLE DRILLED. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11258-MR. 2L72 4F A6WE 19950526004921995052600492WP 1995 5 26 ABXA9500478 119950328A5312591013013 BULKHEAD DOUG DC9 DC941 302207NWP FS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK IN THE UPPER LEFT HORIZONTAL EDGE OF THE AFT VENTRAL STAIR DOOR. REPAIRED IAW ABX REA D953-11275-SB REV A. 2L72 4F A6WE 19950526004931995052600493WP 1995 5 26 ABXA9500479 119950330A5330592032379 SKIN DOUG DC9 DC941 302207NWP FS 332 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 WHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A GOUGE AFT OF A PREVIOUS REPAIR AT FS 332 AND LONGERON 25R. REPAIRED SKIN IAW ABX REA D953-11278-MR. 2L72 4F A6WE 19950526004941995052600494WP 1995 5 26 ABXA9500480 119950329A5320591015837 DOOR JAMB DOUG DC9 DC941 302207NWP FS 993 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE WEB AROUND THE AFT BAG BIN DOOR JAMB CORRODED. REPAIRED WEB IN JAMB AREA IAW ABX REA D953-11279-MR. 2L72 4F A6WE 19950526004951995052600495WP 1995 5 26 ABXA9500481 119950331A57309919375 SKIN DOUG DC9 DC941 302207NWP LT WING LE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING LEADING EDGE CRACKED JUST INBOARD OF THE NR 5 SLAT OUTBOARD TRACK. REPAIRED CRACK IAW ABX REA D957-11284. 2L72 4F A6WE 19950526004961995052600496WP 1995 5 26 ABXA9500482 119950331A53205910244151 CHANNEL DOUG DC9 DC941 302207NWP FS 1152 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A MOUNT CHANNEL CRACKED AT FS 1152 AND LONGERON 14R. REPAIRED CHANNEL IAW ABX REA D925-11297 AND RE-INSTALLED CHANNEL IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950526004971995052600497WP 1995 5 26 ABXA9500483 119950418A5330591140659 SKIN DOUG DC9 DC941 302207NWP FS 198 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A REPAIR AT THE AFT LOWER CORNER OF THE LEFT FORWARD ENTRY DOOR NOT IAW DC-9 SRM. REPAIRED DOOR JAMB SKIN IAW ABX REA D953-11405-MR. 2L72 4F A6WE 19950526004981995052600498WP 1995 5 26 ABXA9500484 119950224A531327779223 LONGERON DOUG DC9 DC941 302207NWP FS 408 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE COMPLYING WITH AD 94-03-01, FOUND LONGERON 17R CRACKED AT FS 408. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526004991995052600499WP 1995 5 26 ABXA9500485 119950306A532029129015 ANGLE DOUG DC9 DC941 302207NWP FS 655 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT HAND FLOOR BEAM ATTACH ANGLE CRACKED AT FS 655. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526005001995052600500WP 1995 5 26 ABXA9500486 119950307A5320991050313 WEB DOUG DC9 DC941 302207NWP FS 984 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB FROM FS 973 TO 1041 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526005011995052600501WP 1995 5 26 ABXA9500487 119950307A53204911388501 FITTING DOUG DC9 DC941 302207NWP FS 984 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME FITTING AT FS 984 HAD LEVEL II CORROSION. REPLACED RIGHT TEE FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526005021995052600502WP 1995 5 26 ABXA9500488 119950307A532049113832 FITTING DOUG DC9 DC941 302207NWP FS 1005 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING HAD LEVEL II CORROSION AT FS 1005. REPLACED RIGHT FUSELAGE FRAME FITTING AT FS 1005 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526005031995052600503WP 1995 5 26 ABXA9500489 119950307A5320391295502 FITTING DOUG DC9 DC941 302207NWP FS 1013 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT FUSELAGE FRAME TEE FITTING AT FS 1013 HAD LEVEL II CORROSION. REPLACED FUSELAGE FRAME TEE FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19950526005041995052600504WP 1995 5 26 ABXA9500490 119950307A5320991050315 WEB DOUG DC9 DC941 302207NWP FS 946 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 94-03-01, FOUND THE RIGHT CUSP WEB AT FS 946 HAD LEVEL II CORROSION. REPLACED RIGHT CUSP WEB IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526005051995052600505WP 1995 5 26 ABXA9500491 119950228A531327779221 LONGERON DOUG DC9 DC941 302207NWP FS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 2R CRACKED AT FS 718. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005061995052600506WP 1995 5 26 ABXA9500492 119950227A531327779223 LONGERON DOUG DC9 DC941 302207NWP FS 775 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 4R CRACKED AT FS 775. REPLACED LONGERON SECTON IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005071995052600507WP 1995 5 26 ABXA9500493 119950227A531327779221 LONGERON DOUG DC9 DC941 302207NWP FS 794 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND LONGERON 3R CRACKED AT FS 794. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005081995052600508WP 1995 5 26 ABXA9500494 119950223A53207075T6 DOOR JAMB DOUG DC9 DC941 302207NWP FS 207 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT MAIN ENTRY DOOR JAMB WEB CRACKED AT FS 207 AND LONGERON 11L AND 15L. REPAIRED IAW DC-9 SRM SUPPLEMENTAL DRAWING K05012. 2L72 4F A6WE 19950526005091995052600509WP 1995 5 26 ABXA9500495 119950314A532059124921 DOOR JAMB DOUG DC9 DC941 302207NWP FS 200 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE SERVICE DOOR JAMB AFT STRUCTURE DENTED IN THE BAYONET AREA. REPAIRED RIGHT HAND SERVICE DOOR JAMB IAW DC-9 SRM 53-05 FIGURE 42. 2L72 4F A6WE 19950526005101995052600510WP 1995 5 26 ABXA9500496 119950404A531199234092 FRAME DOUG DC9 DC941 302207NWP FS 737 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND RIGHT MAIN FUSELAGE FRAME AT FS 737 CRACKED. REPAIRED RIGHT MAIN FRAME AT FS 737 IAW DC-9 SB 53-131. 2L72 4F A6WE 19950526005111995052600511WP 1995 5 26 ABXA9500497 119950331A531199234362 FRAME DOUG DC9 DC941 302207NWP FS 756 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE RIGHT FUSELAGE MAIN FRAME CRACKED AT FS 756. REPLACED RIGHT MAIN FRAME IAW DC-9 SRM 51-30-1, 51-30-2 AND SB 53-131. 2L72 4F A6WE 19950526005121995052600512WP 1995 5 26 ABXA9500498 119950327A531199234361 FRAME DOUG DC9 DC941 302207NWP FS 756 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE LEFT FUSELAGE MAIN FRAME AT FS 756 CRACKED. REPLACED MAIN FRAME AT FS 756 IAW DC-9 SB 53-131. 2L72 4F A6WE 19950526005131995052600513WP 1995 5 26 ABXA9500499 119950228A531327779221 LONGERON DOUG DC9 DC941 302207NWP FS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 2R CRACKED AT FS 718. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005141995052600514WP 1995 5 26 ABXA9500500 119950227A531327779223 LONGERON DOUG DC9 DC941 302207NWP FS 775 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 4R CRACKED AT FS 775. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005151995052600515WP 1995 5 26 ABXA9500501 119950227A531327779223 LONGERON DOUG DC9 DC941 302207NWP FS 794 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 88-24-08 REV 2; SB A53-230 REV 3, FOUND LONGERON 3R CRACKED AT FS 794. REPAIRED LONGERON IAW DC-9 SRM 53-02 FIGURE 2. 2L72 4F A6WE 19950526005161995052600516WP 1995 5 26 ABXA9500502 119950307A53207075T6 INTERCOSTAL DOUG DC9 DC941 302207NWP FS 180 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN INTERCOSTAL CRACKED AT FS 180, LBL 42. REPAIRED INTERCOSTAL IAW DC-9 SRM SUPPLEMENTAL DRAWING NR K05195. 2L72 4F A6WE 19950526005171995052600517WP 1995 5 26 ABXA9500503 119950307A532099101409 WEB DOUG DC9 DC941 302207NWP FS 218 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE CUSP WEB CRACKED AT FS 218, LBL 55. REPLACED CUSP WEB FROM FS 218 TO FS 237 IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19950526005181995052600518WP 1995 5 26 ABXA9500504 119950302A5754SS095700036 RIB DOUG DC9 DC941 302207NWP WS 128 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING NR 2 INBOARD SLAT TRACK FITTING CRACKED AT LOWER ATTACHMENT. REPLACED FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950526005191995052600519WP 1995 5 26 ABXA9500505 119950404A57555910055513 SPOILER PANEL DOUG DC9 DC941 302207NWP XRS 324 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED PANEL IAW DC-9 MM 27-61-1. 2L72 4F A6WE 19950526005201995052600520WP 1995 5 26 ABXA9500506 119950315A5315991556141 FLOORBEAM DOUG DC9 DC941 302207NWP FS 1072 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D953-11128MR. 2L72 4F A6WE 19950526005211995052600521WP 1995 5 26 ABXA9500516 119950315A5315991556169 FLOORBEAM DOUG DC9 DC941 302207NWP FS 1072 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23990AX 47493 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND REPAIRS ON FLOORBEAM AT FS 1072, LBL 46 AND 48 NOT IAW THE SRM. REPAIRED FLOORBEAM IAW ABX REA D 953-11128-MR. 2L72 4F A6WE 19950526005221995052600522WP 1995 5 26 MWEA95206 119950522A213071145730016 DUCT DOUG DC9 DC914 3022034WP CABIN RUPTURED A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31500ME 45711 EN ROUTE TO DCA FROM OMA AT 33,000 FT, NOTICED CABIN ALT INCREASE 100 FPM PLUS DIFFERENTIAL DECREASE. UNABLE TO CONTROL IN AUTO AND MANUAL, DIVERTED TO MKE. REPLACED RUPTURED DUCT DOWNSTREAM OF TEMP CONTROL VALVE. CONTINUED FLIGHT TO DCA. 2L72 4F A6WE 19950526005231995052600523NM 1995 5 26 SCNA95101 119950519A3350900835A EEL BATTERY BOEING727 727282 2F0R NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 EMERGENCY EXIT SIGN ABOVE R-2 DOOR FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPS CHECKED GOOD. 2L73 4F RTA3WE 19950526005241995052600524NM 1995 5 26 SCNA95102 119950520A33501000677 EEL POWER SUPPLY BOEING727 727225 1384077NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 AFT ENTRY EMERGENCY LIGHT DID NOT TEST. REMOVED AND REPLACED AFT ENTRY OVERHEAD POWER SUPPLY IN OVERHEAD LIGHT IAW MM 33-50-101. 2L73 4F A3WE 19950526005251995052600525NM 1995 5 26 SCNA95103 119950520A33501001143 EEL POWER SUPPLY BOEING727 727225 1384077NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 AFT AIRSTAIR OVERHEAD LIGHTS DID NOT TEST. REMOVED AND REPLACED POWER SUPPLY FOR AFT AIRSTAIR EMERGENCY LIGHTS IAW 33-50-61. LIGHTS CHECKED GOOD. 2L73 4F A3WE 19950526005261995052600526NM 1995 5 26 SCNA95104 119950520A33501102832 EEL ASSY BOEING727 727227 1384078NM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT FOUND TO BE INOPERATIVE. REPLACED BATTERIES IN LIGHT ASSEMBLY OPS CHECK GOOD. 2L73 4F A3WE 19950526005271995052600527WP 1995 5 26 95ZZZM10 119950507A3241922444733643 RELAYS DOUG DC8 DC871 302199AWP ANTI-SKID SYST FAILED A RRXAO OTHER J WARNING INDICATION LDLANDING 1 WP158087U 45977 FLT 2702 - MGGT-KJFK - ANTI-SKID FAILED ON LANDING AT KJFK. USED EMERGENCY BRAKE TO STOP AIRCRAFT. AFTER COMING TO COMPLETE STOP, TURNED OFF ANTI-SKID. BRAKES OPERATED NORMALLY. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL RELAY AND LANDING GEAR INTERLOCK RELAY. SPUN TRANSDUCERS, ANTI-SKID SYSTEM CHECKED NORMALLY. (M) 2L74 4F 4A25 19950526005281995052600528WP 1995 5 26 95ZZZM11 119950505A3260 CONNECTOR DOUG DC8 DC863F 302198FWP LT MLG UPLATCH MALFUNCTIONED A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15952R 46061 FLT 101 - KPDX-KDAY - DURING GEAR UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. CYCLED GEAR TWO TIMES FOR SUCCESSFUL CHECK. KDAY MAINTENANCE FOUND WIRE PIN ON LEFT GEAR UPLATCH STRIKER RECESSED. RESET PIN IN PLUG. UPLATCH TEST CHECKS GOOD IAW MM 32-30-0. (M) 2L74 4F 4A25 19950526005291995052600529NE 1995 5 26 95ZZZM12 219950504A7200 ENGINE DOUG DC8 DC871 302199AWP GE CFM56 CFM562C1 13802NE NR 1 FAILED A RRXAO OTHER JY WARNING INDICATION ENGINE STOPPAGE CLCLIMB 1 WP158079U 45947 693285 NR 1 ENGINE FLAMED OUT WHILE CLIMBING THROUGH FL 370. RELIGHTED ENGINE AT APPROXIMATELY FL 280 DESCENDING FROM FL 310. CONTINUED TO SVMI WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL. PERFORMED NR 1 ENGINE INSPECTION IAW CFM MM CHAPTER 71-00-0. NO DEFECTS NOTED ON GROUND RUN. NR 1 ENGINE CHECK NORMAL. (M) 2L74 4F4 F 4A25 E2GL 19950526005301995052600530CE 1995 5 26 95ZZZM13 119950506A5753 TE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV 1518 712 UC134 DURING SCHEDULED MAINTENANCE AND INSPECTION OF RIGHT OUTBOARD TE FLAP (P/N 35165050259) REVEALED A 1.5 INCH CRACK, LOCATED AT TRAILING EDGE APPROXIMATELY 10 INCHES INBOARD OF END CAP. STOP DRILLED CRACK AND INSTALLED DOUBLER. 2L72 4T RTA24CE 19950526005311995052600531CE 1995 5 26 95ZZZM14 119950428A573010116000144 LE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0769ZR 12057 343 UC69 AN .625 INCH CRACK LOCATED AT THIRD RIB FROM INBOARD END ON BOTTOM OF FLAP NEAR LEADING EDGE OF TE FLAP (P/N 10116000144). STOP DRILLED AND INSTALLED DOUBLER CRACK WAS FOUND DURING SCHEDULED MAINTENACNE. 2L72 4T RTA24CE 19950526005321995052600532CE 1995 5 26 95ZZZM15 119950502A57301181100478 LE SKIN BEECH 1900 1900C 1154161CE RT WING DENTED A AMWAK NONE C F.O.D. APAPPROACH 1 CE0769ZR 8224 UC69 INBOUND TO MCI A BIRD STRUCK THE RIGHT WING DENTING RIGHT WINGS LEADING EDGE. REPAIRED WITH FLUSH PATCH APPROXIMATLELY, 12 INCHES BY 10 INCHES ON LEADING EDGE. (M) 2L72 4T RTA24CE 19950526005331995052600533CE 1995 5 26 95ZZZM16 119950413A6120 BETA CABLE BEECH 1900 1900C 1154161CE LT ENGINE LOOSE A AMWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07160AM UC160 FLT 5630 - AFTER TAKEOFF LEFT TORQUE AND PROP RPM INDICATION FLUCTUATED. FOUND BETA CABLE LOOSE, TIGHTENED CABLE, RERIGGED LEFT ENGINE. OPS CHECK NORMAL. (M) 2L72 4T RTA24CE 19950526005341995052600534CE 1995 5 26 95ZZZM17 119950427A5753 LE SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV 1490 121 UC137 FLAP CRACKED .75 INCH ON BOTTOM LEADING EDGE, 4TH RIB INBOARD. STOP DRILLED AND INSTALLED DOUBLER, ON LT TE FLAP (P/N 35165050258). CRACK WAS FOUND DURING SCHEDULED MAINTENANCE. (M) 2L72 4T RTA24CE 19950526005351995052600535CE 1995 5 26 95ZZZM18 119950427A575335165050258 SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV 1490 121 UC137 FLAP IS CRACKED .5 INCH BETWEEN THIRD AND SECOND RIB FROM INBOARD END ON BOTTOM OF FLAP ON SPAR LINE AND A .75 INCH CRACK ON BOTTOM LEADING EDGE THIRD RIB FROM OUTBOARD END OF TE FLAP (P/N 35165050258). STOP DRILLED CRACKS AND INSTALLED DOUBLER CRACKS WERE FOUND DURING SCHEDULED MAINTENANCE. 2L72 4T RTA24CE 19950526005361995052600536CE 1995 5 26 95ZZZM19 119950505A7120118910025121 ENG MOUNT BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0780ZR 11676 UC80 DURING SCHEDULED MAINTENANCE, AN INSPECTION OF LEFT TRUSS REVEALED A .375 INCH CRACK AT OUTBOARD UPPER MOUNT BOLT. CRACK AT LOWER OUTBOARD GUSSETT .5 INCH CRACK AT TOP INBOARD GUSSETT .5 INCH. CRACK AT TOP AFT, GUSSETT .375 INCH. REPAIRED BY WELDING ALL CRACKS. 2L72 4T RTA24CE 19950526005371995052600537CE 1995 5 26 95ZZZM20 119950503A5753 TE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07160AM 1570 556 UC160 DURING ROUTINE MAINTENANCE A CRACK 1 INCH WAS FOUND ON TRAILING EDGE SKIN APPROXIMATELY 1 FOOT INBOARD OF END CAP. ON TE FLAP (P/N 3516505259). STOP DRILLED AND INSTALLED DOUBLER. (M) 2L72 4T RTA24CE 19950526005381995052600538EA 1995 5 26 95ZZZM21 219950429A7240 HOT SECTION BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE FAILED A AMWAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE07134YV132435743 UC134 32359 FLT 5657 - ON INBOUND FLIGHT TO ICT CREW REPORTED SMOKE IN BLEED AIR SYSTEM. REMOVED POWER SECTION AND FOUND OIL IN GAS GENERATOR, HOT SECTION. REPLACED GAS GENERATOR SECTION. (M) 2L72 4T4 TRTA24CE E4EA 19950526005391995052600539CE 1995 5 26 95ZZZM22 119950426A7933MS280343 OIL TEMP SENSOR BEECH 1900 1900C 1154161CE LT ENGINE FLUCTUATES A AMWAK NONE N FALSE WARNING CRCRUISE 1 CE0785YV UC85 FLT 5659 - EN ROUTE LEFT ENGINE OIL TEMP. FLUCTUATED FROM 60 TO 140 CELSIUS. CLEANED AND RESEATED CANNON PLUG, OPS CHECKED NORMAL. (M) 2L72 4T RTA24CE 19950526005401995052600540NE 1995 5 26 95ZZZM23 219950505A732069B475853 F/E MODULE CARD BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE DEFECTIVE A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23853FT 19753 EN ROUTE FROM LAX FL 33, NR 3 ENGINE VALVE LIGHT INDICATED BRIGHT, ENGINE FAILED. AFTER FAILURE EXCESSIVE VIBRATION OCCURRED. AIRCRAFT TURNED BACK TO LAX. F/E FUEL CONTROL MODULE DEFECTIVE, REPLACED MODULE, REPLACED FUEL SHUTOFF VALVE ACTUATOR. OPERATIONAL CHECK OK. RETURNED TO SERVICE. (M) 2L74 4F4 F A20WE E20EA 19950526005411995052600541NM 1995 5 26 95ZZZM24 119950516A5753 SKIN BOEING747 747124 1384874NM RT TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 AREA 5 INCHES BY 3 INCHES DELAMINATED, TOPSIDE RIGHT WING INBOARD MID FLAP (P/N 65B0262528) 8 INCHES FROM INBOARD EDGE AND 26 INCHES FROM AFT EDGE. REPAIRED IAW BOEING SRM 51-40-9. 2L74 4F A20WE 19950526005421995052600542NM 1995 5 26 95ZZZM25 119950516A575565B0225043 SKIN BOEING747 747124 1384874NM NR 3 SPOILER DELAMINATION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION NR 3 FLIGHT SPOILER P/N 65B0225043 UPPER AND LOWER SURFACES. TWO LARGE AREAS INBOARD EDGE. THE COMPLETE LENGTH ON OUTBOARD TRAILING EDGE APPROXIMATELY 15 SQUARE INCHES. REPLACED SPOILER ASSEMBLY IAW BOEING MM 27-61-02. 2L74 4F A20WE 19950526005431995052600543NM 1995 5 26 95ZZZM26 119950516A573065B067319 PANEL BOEING747 747124 1384874NM WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATIONPANEL 193C AFT OF LEFT BODY GEAR. REPAIRED EPR BOEING SRM 51-40-9. 2L74 4F A20WE 19950526005441995052600544NM 1995 5 26 95ZZZM27 119950516A575365B020707 SKIN BOEING747 747124 1384874NM TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION (3 INCHES BY 5 INCHES) BOTTOM SIDE AIRCRAFT LEFT INBOARD TRAILING EDGE FLAP P/N 65B020707 APPROXIMATELY 4 INCHES FROM INBOARD END. REPAIRED IAW BOEING SRM 51-40-06. 2L74 4F A20WE 19950526005451995052600545NM 1995 5 26 95ZZZM28 119950516A5753 SKIN BOEING747 747124 1384874NM TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 SKIN DELAMINATION RIGHT WING INBOARD MID FLAP P/N 65B0202527 TRAILING EDGE AT NR 2 ACTUATION ARM. REPAIRED IAW BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005461995052600546NM 1995 5 26 95ZZZM29 119950516A575365B0192538 SKIN BOEING747 747124 1384874NM TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATED SKIN BOTTOM SIDE RIGHT OUTBOARD MID FLAP P/N 65B0192538, 50 INCHES OUTBOARD OF THE INBOARD JACK SCREW. REPAIRED AREA IAW BOEING SRM 51-40-09. 2L74 4F A20WE 19950526005471995052600547NM 1995 5 26 95ZZZM30 119950516A5753 SKIN BOEING747 747124 1384874NM TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION LEFT INBOARD FLAP P/N 65B620701 LOWER SURFACE DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED PER BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005481995052600548NM 1995 5 26 95ZZZM31 119950516A5751 SKIN BOEING747 747124 1384874NM LT AILERON DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 LEFT OUTBOARD AILERON P/N 65B001171 UPPER SURFACE SMALL AREA AT DELAMINATION AREA 1.5 INCH BY 1.5 INCH. REPAIRED IAW BOEING SRM 51-40-06. 2L74 4F A20WE 19950526005491995052600549NM 1995 5 26 95ZZZM32 119950516A5753 SKIN BOEING747 747124 1384874NM TE FLAP WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 WEAR DAMAGE AT OUTBOARD LEFT TRAILING EDGE FLAP P/N 65B019001. REPAIRED IAW BOEING SRM 51-40-15 TO 51-40-09 TABLE 1. 2L74 4F A20WE 19950526005501995052600550NM 1995 5 26 95ZZZM33 119950516A575365B020707 SKIN BOEING747 747124 1384874NM LT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION AT LEFT INBOARD TRAILING EDGE FLAP P/N 65B020707 INBOARD SECTION CENTER PANEL LOWER SURFACE. REPAIRED DELAMINATION IAW BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005511995052600551NM 1995 5 26 95ZZZM34 119950516A575365B39011601 SKIN BOEING747 747124 1384874NM TE FORE FLAP CHAFED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DEEP CHAFED AREA LEFT INBOARD FORE FLAP P/N 65B39011601 LOWER INBOARD SURFACE 4 INCHES BY 1 INCH. REPAIRED IAW WITH BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005521995052600552NM 1995 5 26 95ZZZM35 119950516A5753 SKIN BOEING747 747124 1384874NM LT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 LEFT INBOARD MID FLAP P/N 65B0202527 INBOARD LOWER SURFACE NEAR END DELAMINATED. REPAIRED PER BOEING SRM 51-40-09 TABLE 1 AND 51-40-15. 2L74 4F A20WE 19950526005531995052600553NM 1995 5 26 95ZZZM36 119950516A5753 SKIN BOEING747 747124 1384874NM TE MID FLAP CRACKED A P5CAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 WP23855FT 19733 LEFT INBOARD MID FLAP P/N 65B0202527 LOWER SURFACE BETWEEN INBOARD AND OUTBOARD CARRIAGE FORWARD SECTION HAS 3 INCH BY 3 INCH CRACKED AND DELAMINATED AREA. REPAIRED IAW BOEING SRM 51-40-15 TO 51-40-9 TABLE 1. 2L74 4F A20WE 19950526005541995052600554NM 1995 5 26 95ZZZM37 119950516A5753 SKIN BOEING747 747124 1384874NM TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION ON LOWER SURFACE AT THE LEFT INBOARD FLAP FORE FLAP P/N 65B39011601, OUTBOARD AT THE OUTBOARD CARRIAGE. REPAIRED IAW BOEING SRM 51-40-1 TO 51-40-09 TABLE 1. 2L74 4F A20WE 19950526005551995052600555NM 1995 5 26 95ZZZM38 119950516A575365B019001 SKIN BOEING747 747124 1384874NM LT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATED FIBERGLASS STRIP LOWER SURFACE AT LEFT OUTBOARD TRAILING EDGE FLAP P/N 65B019001. REPAIRED FLAP IAW BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005561995052600556NM 1995 5 26 95ZZZM39 119950516A5753 SKIN BOEING747 747124 1384874NM RT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 GOUGE IN TOP SIDE OF THE RIGHT OUTBOARD AFT FLAP P/N 65B019002 15 INCHES FROM OUTBOARD END. REPLACED BOLT CAUSING DAMAGE. REPAIRED GOUGE IAW BOEING SRM 51-40-6. 2L74 4F A20WE 19950526005571995052600557NM 1995 5 26 95ZZZM40 119950516A5753 SKIN BOEING747 747124 1384874NM LT TE FLAPS WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 THREE DEEP CHAFED AND WORN AREAS UPPER LEADING EDGE SURFACE LEFT OUTBOARD FORE FLAP P/N 65B019013. REPAIRED IAW BOEING SRM 51-40-09 AND 51-40-15. 2L74 4F A20WE 19950526005581995052600558NM 1995 5 26 95ZZZM41 119950516A5753 SKIN BOEING747 747124 1384874NM LT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 CRACKED AND DELAMINATED AREA LEFT OUTBOARD MID FLAP P/N 65B0192537 LOWER SURFACE AT THE THIRD TRAILING EDGE FLAP ATTACHMENT. REPAIRED IAW BOEING SRM 51-40-14. 2L74 4F A20WE 19950526005591995052600559NM 1995 5 26 95ZZZM42 119950516A5753 SKIN BOEING747 747124 1384874NM RT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DELAMINATION TOPSIDE RIGHT OUTBOARD MID FLAP TRAILING EDGE P/N 65B0192538, 72 INCHES FROM OUTBOARD END (1 INCH BY 5 INCHES). REPAIRED IAW BOEING SRM 51-40-15. 2L74 4F A20WE 19950526005601995052600560NM 1995 5 26 95ZZZM43 119950516A5753 O/B MIDFLAP SKIN BOEING747 747124 1384874NM LT TE FLAP WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 HONEYCOMB SHOWING (LIGHT SHOWS THROUGH) LEFT OUTBOARD MID FLAP P/N 65B0192537, UPPER AND LOWER SURFACE APPROXIMATELY 1 INCH BY 1 INCH AREA. REPAIRED IAW SRM 51-40-06. 2L74 4F A20WE 19950526005611995052600561NM 1995 5 26 CAL950367 119950502A5320 SUPPORT BOEING727 727224 1384076NM BS 620 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND CORROSION ON LOWER SIDE OF FLOOR SUPPORT IN FORWARD PIT AT STATION 620. THE CORRODED AREA WS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. (M) 2L73 4F A3WE 19950526005621995052600562NM 1995 5 26 CAL950368 119950502A5730 TE PANEL BOEING727 727224 1384076NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND THE LEFT WING UPPER SURFACE TRAILING EDGE PANEL AT OUTBOARD END OF OUTBOARD FLAP WITH A 1 INCH CRACK IN DOUBLER ATTACHED TO INBOARD SIDE. THE CRACKED DOUBLER WAS REMOVED. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-1 AND 51-30-2. (M) 2L73 4F A3WE 19950526005631995052600563NM 1995 5 26 CAL950369 119950502A5754 SKIN BOEING727 727224 1384076NM NR 2 LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .125 INCH CRACK IN THE NR 2 LEADING EDGE FLAP INNER SKIN UNDER ACTUATOR. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5720-01064 AND SRM 51-30-2. (M) 2L73 4F A3WE 19950526005641995052600564NM 1995 5 26 CAL950370 119950502A5712 RIB BOEING727 727224 1384076NM NR 4 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN NR 4 SLAT OUTBOARD SECOND RIB. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (M) 2L73 4F A3WE 19950526005651995052600565NM 1995 5 26 CAL950371 119950502A5754 RIB BOEING727 727224 1384076NM NR 7 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN NR 7 SLAT RIB AT OUTBOARD SIDE ON OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-3 AND 57-50-3. (M) 2L73 4F A3WE 19950526005661995052600566NM 1995 5 26 CAL950372 119950502A5754 RIB BOEING727 727224 1384076NM NR 3 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND A .5 INCH CRACK IN NR 3 SLAT RIB INBOARD OF TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 57-50-3. (M) 2L73 4F A3WE 19950526005671995052600567EA 1995 5 26 95ZZZX2499 219950411A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RIGHT FAILED A GLBAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0184GL 9983 UC84 PCE97024 BIS - OUTBOUND FROM BIS, THE CREW EXECUTED AN AIR TURN-BACK AFTER THE RT ENGINE LOST OIL PRESSURE AND WAS SECURED. THE SINGLE ENGINE FLIGHT AND LANDING WERE UNEVENTFUL. MAINTENANCE REPLACED THE ENGINE AND THE TEST FLIGHT WAS SATISFACTORY. FAILURE IS ASSUMED TO BE A NR 4 BEARING FAILURE. A TEAR-DOWN AT PRATT AND WHITNEY IS PENDING. 2L72 4T4 TRTA24CE E4EA 19950526005681995052600568CE 1995 5 26 95ZZZX2500 119950414A53201144200365 FRAME BEECH 1900 1900C 1154161CE DOORWAY CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0187GL 14488 UC87 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND CABIN DOOR FRAME CRACKED AT THE SNUBBER ATTACH BRACKET. THE FRAME WAS INSPECTED AND REPAIRED BY INSTALLING A 2024T3 .063 INCH DOUBLER IAW SRM 51-70-00, PAGES 52-53. 2L72 4T RTA24CE 19950526005691995052600569 1995 5 26 95ZZZX2501 419950414A3416066306200 ALTIMETER BEECH 1900 1900C 1154161CE NR 1 INOP A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01125GL 3771 UC125 GRI - AFTER TAKEOFF, CREW ELECTED AN AIR TURN-BACK WHEN THE NR 1 ALTIMETER FLAGGED AND THE ALTITUDE ALERT WENT BLANK. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED ALTIMETER WHICH TESTED SATISFACTORILY. 2L72 4T RTA24CE 19950526005701995052600570EA 1995 5 26 95ZZZX2502 219950413A73103037677 FUEL LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A65B 52043EA LT NACELLE LEAKING A GLBAK NONE BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS LDLANDING 1 CE01118UX1117 UE118 DEN - UPON LANDING, CREW REPORTED A NOXIOUS ODOR IN THE COCKPIT WHEN THE LEFT BLEED VALVE WAS ON. MAINTENANCE FOUND FUMES CREATED BY A SMALL LEAK IN A FUEL LINE. THE LINE WAS REPLACED. 2L72 4T4 TRTA24CE E4EA 19950526005711995052600571WP 1995 5 26 95ZZZX2503 119950228A261224490222 CONNECTOR DOUG DC8 DC862 3021970WP NR 2 ENGINE DIRTY A ARWAK NONE L NO TEST ININSP/MAINT 1 SO1966656 45953 DURING POST-FLIGHT, NR 2 ENGINE FIRE WARNING WOULD NOT TEST. FOUND NR 2 LOWER LOOP CONNECTOR OIL SOAKED, REMOVED AND CLEANED CONNECTOR, REINSTALLED, OPS CHECK GOOD IAW MM 26-10. 2L74 4F 4A25 19950526005721995052600572NM 1995 5 26 95ZZZX2504 119950314A26121061096125 FIRE LOOP BOEING727 727225 1384077NM NR 2 ENGINE OUT OF POSITION A ARWAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19807EA 22438 DURING FLIGHT, NR 2 ENGINE FIRE DETECTOR GROUND CIRCUIT LIGHT ON P6-3 CAME ON INTERMITTENTLY. REPOSITIONED FIRE LOOP CLAMP INSULATORS AS NECESSARY. GROUND FIRE TEST, OPS CHECKED GOOD IAW MM 26-10. 2L73 4F A3WE 19950526005731995052600573NM 1995 5 26 95ZZZX2505 119950316A261265249203 FIRE CONTROL BOX 6F249203 BOEING727 727225 1384077NM AFT BODY FAILED A AWRAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 WP25808EA R00660 22439 FINAL REPORT. LOWER AFT BODY OVER-HEAT LIGHT ON, WOULD NOT GO OUT. AIRCRAFT RETURNED TO TOL. PRELIMINARY REPORT ON 3-10-95, INDICATED TROUBLESHOOTING WAS IN PROGRESS. MAINTENANCE REPLACED A FAULTY FIRE DETECTION CONTROL BOX. 2L73 4F A3WE 19950526005741995052600574CE 1995 5 26 95ZZZX2506 119950404A2750BZ7RW82255518T SWITCH BEECH 1900 1900C 1154161CE RT TE FLAPS FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01123UE UC123 HON - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURN-BACK DUE TO THE FLAPS BEING STUCK IN THE TAKEOFF POSITION. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED RT FLAP MICROSWITCH. THE FLAPS CYCLED SUCCESSFULLY. 2L72 4T RTA24CE 19950526005751995052600575CE 1995 5 26 95ZZZX2507 119950404A53501014100959 RADOME BEECH 1900 1900C 1154161CE NOSE CRACKED A GLBAK NONE C F.O.D. TXTAXI/GRND HDL 1 CE01105GL13886 UC105 ORD - WHILE AIRCRAFT WAS PARKED, A BAG CART IMPACTED THE RADOME. THE RADOME WAS REMOVED, THE MOUNTING STRUCTURE INSPECTED, AND REPLACED THE RADOME WITH SERVICEABLE. 2L72 4T RTA24CE 19950526005761995052600576CE 1995 5 26 95ZZZX2508 119950402A57511181300001 AILERON BEECH 1900 1900C 1154161CE LT WING DENTED A GLBAK NONE C F.O.D. TXTAXI/GRND HDL 1 CE0145GL 14835 UC146 UC45 ORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, THE LEFT WING TIP AND OUTBOARD TRAILING EDGE WERE DENTED BY A BAG CART TOW TRACTOR. MAINTENANCE REMOVED THE AILERON AND WING TIP AND INSPECTED THOSE AREAS FOR FURTHER DAMAGE. A SERVICEABLE AILERON AND WING TIP ASSEMBLY WERE INSTALLED. A TEST FLIGHT WAS SUCCESSFUL. 2L72 4T RTA24CE 19950526005771995052600577EA 1995 5 26 95ZZZX2509 219950401A72612380 ENGINE OIL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE LOW A GLBAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 CE0145GL UC45 DLH - INBOUND TO DLH, CREW EXPERIENCED THE RT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 40-100 PSI ACCOMPANIED BY THE ILLUMINATION OF THE RT OIL PRESSURE ANNUNCIATOR. THE RT ENGINE WAS SECURED AFTER WHICH AN UNEVENTFUL LANDING WAS COMPLETED. MAINTENANCE INSPECTED FOR OIL LEAKS, SERVICED OIL LEVEL, AND MADE SEVERAL ENGINE RUNS, BUT COULD NOT DUPLICATE THE FLUCTUATION. 2L72 4T4 TRTA24CE E4EA 19950526005781995052600578CE 1995 5 26 95ZZZX2510 119950422A2720MS29561012 O-RING BEECH 1900 1900D 1154162CE LT ENGINE LEAKING A GLBAD RETURN TO BLOCK BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TXTAXI/GRND HDL 1 CE01100UX2447 UE100 ISN - CREW REPORTED FUMES IN THE COCKPIT. MAINTENANCE FOUND AN O-RING UNDER THE RUDDER BOOST TRANSMITTER LEAKING OIL. THE O-RING WAS REPLACED AND LEAK CHECKED GOOD. 2L72 4T RTA24CE 19950526005791995052600579CE 1995 5 26 95ZZZX2511 119950430A712012991003279 ENGINE TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01159GL9157 UC159 SPW - DURING ROUTINE MAINTENANCE, THE RT ENGINE TRUSS WAS FOUND CHAFED IN AREA 'C' AS DESCRIBED IN AD 95-02-18 AND BEECH SB 2255, REV 6. REPLACED TRUSS AND OPS CHECKED. 2L72 4T RTA24CE 19950526005801995052600580NE 1995 5 26 95ZZZX2512 219950420A7321CPW3040760 FUEL CONTROL BEECH 1900 1900D 1154162CE PWA PT6 PT6A67 52043NE LT ENGINE LEAKS A UUAAO OTHER K FLUID LOSS LDLANDING 1 SO1745AR 1483 UE12 AFTER LANDING, PILOTS NOTED FUEL LEAK FROM ENGINE DRAIN. LEAK ISOLATED TO FCU/FUEL PUMP DRAIN. REMOVED AND REPLACED FCU/FUEL PUMP. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA24CE E26NE 19950526005811995052600581 1995 5 26 95ZZZX2513 419950420A34181675 LIFT DETECTOR C6W1001 DHAV DHC6 DHC6300 EA OUTBOARD SHORTED A ASWAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 WP07297SA 361 250077 297 FLIGHT CREW REPORTED STALL WARNING CAME ON DURING CRUISE FLIGHT. PULLED CIRCUIT BREAKER. MIANTENANCE REPLACED OUTBOARD STALL WARING VANE/SWITCH. DEFECTIVE SWITCH WAS REPAIRED BY THE MANUFACTURER PREVIOUSLY. AIRCRAFT WAS FLOWN THROUGH MOISTURE ON THIS DATE. 1H72 3T A9EA 19950526005821995052600582 1995 5 26 95ZZZX2514 419950419A34181675 LIFT DETECTOR C6W1001 DHAV DHC6 DHC6300 EA INBOARD SHORTED A ASWAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 WP07148SA 82 409 STALL WARNING OCCURRED AFER TAKEOFF FROM GEN AIRPORT. CREW PULLED APPLICABLE CIRCUIT BREAKER AND REMAINDER OF FLIGHT FLOWN FLAPS UP. MAINTENANCE REPLACED FAILED INBOARD STALL WARNING SWITCH. THIS AIRCRAFT WAS FLOWN THROUGH MOIST WEATHER ON THIS DATE. THIS SWITCH WAS REPAIRED BY THE MANUFACTURER 82.1 FLIGHT HRS TO THIS FAILURE. 1H72 3T A9EA 19950526005831995052600583 1995 5 26 95ZZZX2515 419950419A34181675 LIFT DETECTOR C6W1001 DHAV DHC6 DHC6300 EA INBOARD SHORTED A ASWAO OTHER N FALSE WARNING APAPPROACH 1 WP07245SA 1420 388 CREW REPORTED STALL WARNING OCCURRED WHEN SELECTING FLAPS FROM 10 DEGREES TO 20 DEGREES. MAINTENANCE REPLACED OUTBOARD STALL WARNING SWITCH. NOTE: THIS AIRCRAFT WAS FLOWN THROUGH MOIST WEATHER ON THIS DATE. 1H72 3T A9EA 19950526005841995052600584 1995 5 26 95ZZZX2516 419950419A34181675 LIFT DETECTOR C6W1001 DHAV DHC6 DHC6300 EA INBOARD FAILED A ASWAO OTHER N FALSE WARNING ININSP/MAINT 1 WP07241SA 556 STALL WARNING SOUNDED WHEN FLAPS SELECTED TO 10 DEGREES ON GROUND. MAINTENANCE REPLACED INBOARD STALL WARNING SWITCH. NOTE: AIRCRAFT WAS OPERATED IN MOIST WEATHER ON THIS DATE. 1H72 3T A9EA 19950526005851995052600585 1995 5 26 95ZZZX2517 419950419A34181675 LIFT DETECTOR C6W1001 DHAV DHC6 DHC6300 EA OUTBOARD FAILED A ASWAO OTHER N FALSE WARNING APAPPROACH 1 WP0772GC 265 264 AT 100 KNOTS, AIRSPEED STALL WARNING CAME ON WHEN FLAPS WERE EXTENDED. MAINTENANCE REPLACED OUTBOARD STALL WARING SWITCH. NOTE: AIRCRAFT WAS FLOWN IN MOIST WEATHER ON THIS DATE. 1H72 3T A9EA 19950526005861995052600586NE 1995 5 26 AWXA9500271 219950508A7510 ANTI-ICE VALVE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A AAWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28181AW 22648 OMA/LAS - FLT 780 - AIRCRAFT DIVERTED TO ICT. DURING PREVIOUS FLIGHT TO OMA, NR 2 ENGINE RT ANTI-ICE VALVE BECAME INOPERATIVE. CONTRACT MX WAS INSTRUCTED TO LOCK THE VALVE IN THE OPEN POSITION AND MX CONTROL ISSUED AN UNMANNED STATION RELEASE. SHORTLY AFTER TAKEOFF FROM OMA, NR 2 ENGINE FUEL HEAT VALVE WOULD NOT CLOSE AND OIL TEMPERATURE ROSE TO 140 DEGREES. CREW SHUT NR 2 ENGINE DOWN AND DIVERTED AIRCRAFT TO ICT. CONTRACT MX FOUND FUEL HEAT VALVE LOCKED IN OPEN POSITION. MAINTENANCE UNLOCKED FUEL HEAT AND LOCKED RT ANTI-ICE VALVE OPEN. ALSO, PERFORMED WINDMILL INSPECTION PROCEDURE WITH NO DEFECTS NOTED. ACFT RELEASED FOR FURTHER SERVICE. (X) 2L72 4F4 FRTA16WE E2EA 19950526005871995052600587SO 1995 5 26 C2XA95IA075 119950511A572012017057006 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LT RIB 16 LOWER AFT SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 11,865.9. CYCLES - 16,738. (X) 2L72 4T RTA31SO 19950526005881995052600588SO 1995 5 26 C2XA95IA076 119950511A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH- DURING C-CHECK INSPECTION, FOUND LT WING RIB NR 16, 4TH LOWER SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 11,865.9. CYCLES - 16,738. (X) 2L72 4T RTA31SO 19950526005891995052600589WP 1995 5 26 DLAR950007 119950327A5743 FITTING LKHEED1011 10113851 5265010WP LEFT WING CORRODED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA 193A1012 ATL - DURING LETTER CHECK AT DALR, THE LEFT MLG UPPER ACTUATOR ATTACH FITTING LUGS WERE FOUND CORRODED ON THE INSIDE DIAMETER. THE LUG HOLES WERE BORED OUT TO CLEAN UP CORROSION PER DL ERA 270493-14. TT, 38155 HRS. CYCLES, 18905. (X) 2L73 4F A23WE 19950526005901995052600590NM 1995 5 26 MALA954434 119950425A2120 AIR DIST DHAV DHC8 DHC8102 2809003NM CABIN FUMES A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15859MA 361 FLT 3442 - WHILE TAXIING IN FNT, WITH THE BLEED AIR SELECTED ON, THE CABIN AND FLIGHT COMPARTMENT FILLED WITH FUMES. THE CREW SELECTED THE BLEED AIR OFF AND SMOKE WAS NOTED IN THE FLIGHT COMPARTMENT. INVESTIGATION IS CONTINUING. (W) 2H72 4T RTA13NM 19950526005911995052600591NM 1995 5 26 MALA954435 119950429A5414 SKIN DHAV DHC8 DHC8102 2809003NM RT NACELLE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15802MA 245 FLT NR 3203 - DURING THE POST FLIGHT INSPECTION IN MSP, THE CREW FOUND THE RIGHT INBOARD NACELLE SKIN DAMAGED AT THE MAIN LANDING GEAR DOOR EDGE. REPAIRS WERE COMPLETED BY REMOVING THE DAMAGED SECTION AND INSTALLING A DOUBLER IAW RD 8-54-377. (W) 2H72 4T RTA13NM 19950526005921995052600592SW 1995 5 26 MALA954436 119950430A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP DOUBLER WORN. REPAIRS WERE COMPLETED BY REPLACING THE ROLLER DOUBLER, P/N 27-31141-001, IAW FAC SRM 51-00-00 PAGE 4. (W) 1L72 4T A8SW 19950526005931995052600593SW 1995 5 26 MALA954437 119950502A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 144.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING BLOCK CHECK INSPECTION MSP, MAINTENANCE FOUND A CRACK IN LOWER RT BELT FRAME RELIEF RADIUS AT FS 144.24 AND WL 80.39 RIGHT BELOW STRINGER NR 11A. REPAIRS WERE COMPLETED BY STOP DRILLING AND FABRICATING REPAIR DOUBLER IAW FAIRCHILD SRM NR 19 53-90-20, PAGES 83-95 REV JAN 18/93. (W) 1L72 4T A8SW 19950526005941995052600594SW 1995 5 26 MALA954438 119950502A53202731110 STIFFENER SWRNGNSA227 SA227AC 8780603SW FS 254.52 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING BLOCK CHECK IN MSP, MAINTENANCE FOUND CENTER STIFFENER ASSY P/N 27-31110 AT BL 0.00 AND FS 254.52 CRACKED. REPAIRED BY REPLACING CENTER STIFFENER ASSY WITH NEW P/N STIFFENERS 27-31110-031, 032 AND CLIP P/N 27-31110-017, 027. ALSO, INSTALLED STIFFENER DOUBLER PATTERNED AFTER FAIRCHILD SRM 57-90-30 REPAIR NR 1 REV NOV/94 AND ADDITION OF TEE ANGLES PER SRM 57-90-30 REPAIR NR 2 REV NOV/94. (W) 1L72 4T A8SW 19950526005951995052600595SW 1995 5 26 MALA954439 119950502A5753 LE SKIN SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CHAFED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND THE RT FLAP CHAFED AT LEADING EDGE SKIN OUTBOARD END. REPAIRED CHAF DAMAGED ITEMS (2) TO LEADING EDGE FORWARD OF FRONT SPAR AT WS 160.00. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIRS IAW FAIRCHILD SRM 57-90-60, REV NOV 1/94 PGS 11-14. (W) 1L72 4T A8SW 19950526005961995052600596NE 1995 5 26 PCAA9500213 219950402A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LEFT FAILED A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA13805EX7783 228 121102 SMOKE IN CABIN ON SHORT FINAL. TROUBLESHOT AND FOUND ENGINE OIL COMING FROM LEFT ENGINE BLEEDS. REMOVED AND REPLACED LEFT ENGINE. ACFT RETURNED TO SERVICE. ACTT: 10956:12. ACTC: 12829. (X) 2H72 4T4 TRTA13NM E20NE 19950526005971995052600597NM 1995 5 26 PCAA9500214 119950405A3350 EEL WIRING DHAV DHC8 DHC8102 2809003NM CABIN FAILED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13800MX 007 AFT EMERGENCY LIGHT STRIP FOUND INOPERATIVE. REPAIRED EMERGENCY LIGHT WIRING AND REPLACED BAD LIGHTING TUBES, TESTED OKAY. AIRCRAFT RETURNED TO SERVICE. ACTT: 17604:12. ACTC: 18749. (X) 2H72 4T RTA13NM 19950526005981995052600598NM 1995 5 26 PCAA9500215 119950523A273182760160 ACTUATOR DHAV DHC8 DHC8102 2809003NM ELEVATOR TRIM FROZEN A PCAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED NRNOT REPORTED 1 EA13820EX 019 AT HIGHER ALTITUDES, THE MISS TRIM NOSE DOWN LIGHT ILLUMINATED ON THE ADVISORY DISPLAY PANEL. COULD NOT MANUALLY MOVE THE ELEVATOR TRIM AND STANDBY ELEVATOR TRIM WAS INEFFECTIVE. DESCENDED TO TEMPS BELOW FREEZING AND TRIM OPERATED NORMALLY. INSPECTED ELEVATOR TRIM CIRCUIT PULLEYS AND CABLES. CHECKED OPERATION OF ELEVATOR SERVO. REMOVED AND REPLACED LT AND RT ELEVATOR TRIM ACTUATORS AND TENSION CABLES IAW WITH DHC-8 MM. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ACTC: 16,483. (X) 2H72 4T RTA13NM 19950526005991995052600599NM 1995 5 26 PCAA9500217 119950426A3260864202 PROX SWITCH DHAV DHC8 DHC8102 2809003NM RT MLG OUT OF ADJUST A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13820EX 019 RT MAIN GEAR RED INDICATOR LIGHT AND GEAR HANDLE INDICATOR LIGHT FLASHED OFF AND ON INTERMITTENTLY. INSPECTED MLG SYSTEM AND PERFORMED PSEU TEST. NO FAULTS FOUND. FOUND RT MLG PROX SWITCH AT HIGH END OF ADJUSTMENT. ADJUSTED AS REQUIRED. ACFT RETURNED TO SERVICE. ACTT: 15693:48. ACTC: 16591. (X) 2H72 4T RTA13NM 19950526006001995052600600EU 1995 5 26 VTZA95159 119950508A3230ATG135020 WOW SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 IAD/LGA - FLT 6595 - DURING CLIMB-OUT AT 1205 ON 5-8-95, RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT WOW SWITCH. AIRCRAFT WAS THEN RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950526006011995052600601NE 1995 5 26 WRLA95027 219950504A7200 ENGINE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 1 FAILED A WRLAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 EA27274WA 48633 LAX - DURING APPROACH, FLIGHT CREW NOTICED DROP IN ENGINE NR 1 RPM'S AND ALSO HEARD LOUD NOISE FROM ENGINE. AT THE SAME TIME, AIRCRAFT LURCHED FORWARD. UTILIZNG ABNORMAL PROCEDURES. FLIGHT CREW PERFORMED AN IN-FLIGHT ENGINE SHUT DOWN OF THE NR 1 ENGINE AND LANDED WITHOUT INCIDENT AT LAX. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE PER WOA MD-11 MM-71-00-01. PERFORMED INSPECTION OF REMOVED ENGINE AND OBSERVED ENGINE WAS SEIZED AND METAL FRAGMENTS FOUND. ACCOMPLISHED AD 95-04-15, WING PYLON UPPER SPAR INSPECTION AND NO DAMAGE NOTED. GROUND TESTED NR 1 ENGINE. OPS OKAY. AIRCRAFT RETURNED TO SERVICE. WILL SUPPLY FURTHER INFO ON CAUSE OF ENGINE PROBLEM UPON RECEIPT OF ENGINE TEAR-DOWN INFO. (X) 2L73 4F4 FRTA22WE E24NE 19950526006021995052600602NM 1995 5 26 DL72E952030 119950502A5320 CLIP BOEING727 727247 138408FNM FS 950 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK CORROSION ON AND UNDER SKIN CLIP FWD SIDE STA 950F BETWEEN STR 30L AND 29L. REPAIRED PER M/M 53-11-0 PG 825. 2L73 4F A3WE 19950526006031995052600603NM 1995 5 26 DL72E952031 119950502A5320 CLIP BOEING727 727247 138408FNM FS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, CORROSION FWD SIDE OF SKIN CLIP STA 1070 BETWEEN STR 29L AND 28L. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19950526006041995052600604NM 1995 5 26 DL72E952032 119950503A5320 SPLICE BOEING727 727247 138408FNM FS 480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, CORROSION ON STRINGER SPLICE STR 26L AFT OF STA 480 FORMER. REPAIRED PER SRM 53-10-3 FIG. 1. 2L73 4F A3WE 19950526006051995052600605NM 1995 5 26 DL72E952033 119950502A5320 WEB BOEING727 727247 138408FNM FS 1236 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, TWO .25 INCH CRACKS AT LIGHTENING HOLE, RBL 20, FS 1236, AT PREVIOUS REPAIRS. REPAIRED PER M/M 53-11-0 PG 828. 2L73 4F A3WE 19950526006061995052600606NM 1995 5 26 DL72E952034 119950509A5311 FRAME BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK, FRAME CRACKED STA 720 5 INCHES ABOVE STRINGER 28L. REPAIRED PER SRM 53-10-4 FIG 26. 2L73 4F A3WE 19950526006071995052600607NM 1995 5 26 DL72E952050 119950502A5330 SKIN BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV2 CHECK CORROSION ON SKIN OUTBD OF STR 28L, 2 AFT OF STA 1010. REPAIRED PER SRM 53-30-3 FIG. 3A, 2L73 4F A3WE 19950526006081995052600608NM 1995 5 26 DL72E952082 119950512A5754 FLANGE BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112826W 21331 0 FOUND ON A1 LTR CK, NR 7 SLAT CRACKED FLANGE TWO PLACES UNDER ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0 P 802. 2L73 4F A3WE 19950526006091995052600609NM 1995 5 26 DL72L952074 119950512A5754651622374 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKS A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 0 FOUND CRACKS ON RIBS NR 13 AND NR 14 DURING SHOP INSPECTION OF NR 7 L/E SLAT. REPAIRED PER SRM 57-54-00. 2L73 4F A3WE 19950526006101995052600610NM 1995 5 26 DL72S952025 119950429A5542 SKIN BOEING727 727232 1384082NM RUDDER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 RUDDER SKIN CRACKED. ONE .125 CRACK, ONE .25 CRACK AND 3 SHEARED RIVETS ON LEFT SIDE OF LWR RUDDER, 6 BELOW A. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV. 2L73 4F A3WE 19950526006111995052600611NM 1995 5 26 DL72S952040 119950427A57536521631324 LE SKIN BOEING727 727232 1384082NM RT TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 4 FORE FLAP, L/E WORN 86 FROM I/B END OF FLAP. REPAIRED PER SRM 575004 FIG 1, FOUND AT HMV, SHOP VISIT. 2L73 4F A3WE 19950526006121995052600612NM 1995 5 26 DL72S952042 119950511A5320 WEB BOEING727 727232 1384082NM FS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11404DA 21148 FOUND DURING E-1 LETTER CHECK, .375 INCH CRK 48 SEC TORQUE BOX WEB STA 1303 RT AT LIGHTENING HOLE. REPAIRED PER SRM 53-11-0. 2L73 4F A3WE 19950526006131995052600613NM 1995 5 26 DL72S952043 119950511A5754 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11404DA 21148 FOUND DURING E-1 LETTER CHECK, NBR 7 L/E SLAT NOSE RIB HAS .25 INCH CRK AT FWD SIDE RT SIDE OF ACTUATOR ATTACH POINT. REPAIRED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950526006141995052600614NM 1995 5 26 DL72S952044 119950511A5320 WEB BOEING727 727232 1384082NM FS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11404DA 21148 FOUND DURING E-1 LETTER CHECK, 1 INCH CRACK AT STA 1223 ABOVE LIGHTENING HOLE IN TORQUE BOX WEB LT. REPAIRED PER SRM 53-11-0. 2L73 4F A3WE 19950526006151995052600615NM 1995 5 26 DL72S952046 119950429A5754 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 RIB CRACKED, NR 6 SLAT-RIB MARKED NR 7 O/B OF TAI DUCT. REPAIR IS CRACKED AFT LOWER CORNER OF RIB. REPLACED REPAIR AS PER MM57-54-0 FIG 805. FOUND AT HMV. 2L73 4F A3WE 19950526006161995052600616NM 1995 5 26 DL72S952047 119950429A5754 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 RIB CRACKED, NR 6 SLAT RIB MARKED NR 11 CRACKED LOWER AFT CORNER BY N/P (1 RIB OUTBOARD OF ACTUATOR). REPAIR PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950526006171995052600617NM 1995 5 26 DL72S952048 119950429A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 ANGLE CRACKED, ANGLE BELOW TAI DUCT CRACKED AT BOTTOM OF CUTOUT FOR TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A, FOR NR 7 L/E SLAT AT HMV. 2L73 4F A3WE 19950526006181995052600618NM 1995 5 26 DL72S952049 119950429A5754 SPAR BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 SPAR CRACKED, TOP I/B CORNER OF CUTOUT FOR TAI DUCT. NR 7 SLAT. REPAIRED PER MM 57-54-0 FIG 810. FOUND AT HMV. 2L73 4F A3WE 19950526006191995052600619NM 1995 5 26 DL72S952076 119950429A5754 SPAR BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 0 SPAR CRACKED, NR 8 SLAT-TOP I/B CORNER OF CUTOUT FOR TAI DUCT INSIDE OF SLAT, BN525. REPAIRED PER MM 57-54-0 FIG 802A. 2L73 4F A3WE 19950526006201995052600620NM 1995 5 26 DL72S952077 119950429A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 0 RIB CRACKED, NR 2 SLAT, RIB MARKED NR 19 CRACKED AT LOWER AFT END BY CUT OUT. REPAIRED PER MM 57-54-0 FIG 805. 2L73 4F A3WE 19950526006211995052600621NM 1995 5 26 DL72S952078 119950429A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 0 RIB CRACKED, NR 2 SLAT, RIB MARKED NR 8 CRACKED LOWER AFT CORNER BY N/P. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950526006221995052600622NM 1995 5 26 DL72S952080 119950429A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 0 RIB CRACKED, NR 2 SLAT, RIB MARKED NR 10 CRACKED LOWER AFT CORNERBY N/P. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950526006231995052600623NM 1995 5 26 DL72S952081 119950511A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 0 TOOLMARKS ON INNER CLOSE OUT SKIN ATTACH ANGLE INSIDE AT 8TH RIB IN FROM OUTBD END OF NR 2 SLAT. REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950526006241995052600624NM 1995 5 26 DL72S952243 119950513A5320 FLANGE BOEING727 727232 1384082NM FS 950 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV TRANS FROM SCH MTC SHEET, PERM REPAIR SKIN FLANGE NEAR FS 950 STR 18A LT REM TEMP REPAIR INSTALLED NEW REPAIR PER M/M 53-12-0. 2L73 4F A3WE 19950526006251995052600625NM 1995 5 26 DL72S952244 119950514A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NR 3 L/E SLAT 19TH RIB FROM IB END SLAT CRACKED. REPAIRED RIB PER M/M 57-40-0 PG 819. 2L73 4F A3WE 19950526006261995052600626NM 1995 5 26 DL72S952245 119950513A5713 STRINGER BOEING727 727232 1384082NM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND RT WING UPPER STR TO RIB CRACKED AT WS 629.00 2ND STR AFT OF VENT BOX. INSTALLED REPAIR DOUBLER PER M/M 57-13-0 PG 801. 2L73 4F A3WE 19950526006271995052600627NM 1995 5 26 DL72W952241 119950412A800069496141 START SWITCH 97907841 BOEING727 727247 138408FNM FLT DECK WORN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11291WA P4280 22109 ON CLIMB-OUT FROM LIT NR 1 START VALVE LIGHT ILLUMINATED. SHUTDOWN NR 1 RETURNED LIT. INSPECTED STARTER, CLEANED CANNON PLUG COULD NOT DUPLICATE PROBLEM. AS A PRECAUTION REPLACED START VALVE. ON A SUBSEQUENT FLIGHT START VALVE LIGHT ILLUMINATED MOMENTARILY AFTER TURNING ANTI-ICE AND IGNITION SWITCH TO OFF. NO FURTHER PROBLEMS NOTED. FOUND NR 1 ENGINE START/IGNITION SWITCH SPONGY, WOULD NOT LOCK IN OFF POSITION. REPLACED START PANEL, OPERATION NORMAL. 2L73 4F A3WE 19950526006281995052600628NM 1995 5 26 DL73S952021 119950510A552265C25746919A SKIN BOEING737 737232 1384475NM LT ELEV GOUGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 FOUND SMALL .25 INCH BY .125 INCH GOUGE IN LOWER SKIN OF LEFT ELEV APPROX 6 INCHS FWD OF TAB. INSTALLED REPAIR PER SRM 55-20-03 FIG 01. 2L72 4F RTA16WE 19950526006291995052600629NM 1995 5 26 DL757952019 119950510A5315BAC1518338 FLOOR BEAM BOEING757 757232 1384965NM FS 345 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 FWD GALLEY FLOOR BEAM CORRODED STA 345 RBL 36 UPPER FLANGE AREA APPROX 1 INCH BY .75 INCH. REPAIRED PER SRM 53-30-51. 2L72 4F RTA2NM 19950526006301995052600630NM 1995 5 26 DL757952020 119950510A5315AND101362409 FLOOR BEAM BOEING757 757232 1384965NM FS 324 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 FWD GALLEY FLOOR BEAM BS 324 UPPER CHORD CORRODED NUMEROUS AREAS ON A 4 FOOT SECTION. SPLICED IN NEW SECTION FLOOR BEAM. 2L72 4F RTA2NM 19950526006311995052600631NM 1995 5 26 DL757952039 119950502A5754114N4005177A TE WEDGE BOEING757 757232 1384965NM NR 4 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 T/E WEDGE DELAMINATED NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 FIGURE 202. REPAIRED DURING SHOP INSPECTION. 2L72 4F RTA2NM 19950526006321995052600632NM 1995 5 26 DL757952069 119950511A7110 COWL BOEING757 757232 1384965NM NR 1 ENGINE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 FOUND IN LETTER CHECK, OUTBOARD LWR SIDE OF ENG INLET DELAMINATED IN 2 AREAS. REPAIRED COWL PANEL PER DL ERA 301749-14 AND SRM 54-11-01 FIG 201. 2L72 4F RTA2NM 19950526006331995052600633NM 1995 5 26 DL757952079 119950509A5315 FLOOR BEAM BOEING757 757232 1384965NM FS 365 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 0 AT HMV, THE FLOOR BEAM AT STA 365 WAS FOUND CORRODED AT RBL 3. THE CORROSION WAS REMOVED NOT WITHIN LIMITS PER SRM 53-00-51. REMOVED UPPER CAP LBL 12 IN TO RT O/B END. DRILLED AND INSTALLED REPLACEMENT SECTION OF FLOOR BEAM PER SRM 53-30-57 FIG 204. 2L72 4F RTA2NM 19950526006341995052600634NM 1995 5 26 DL757952233 119950512A7110314N301025A COWL BOEING757 757232 1384965NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 AT HMV, NR 1 ENGINE NOSE COWL WAS FOUND WITH DENT IN L/E LIP ON LOWER EDGE. REPAIRED PER SRM 54-11-01. 2L72 4F RTA2NM 19950526006351995052600635NM 1995 5 26 DL757952249 119950512A7110314N301016B COWL BOEING757 757232 1384965NM NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 AT HMV, FOUND NR 1 ENGINE NOSE COWL WITH HOLE IN COMPOSITE PANEL AT 1 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01. 2L72 4F RTA2NM 19950526006361995052600636NM 1995 5 26 DL757952254 119950514A4900 FIREWALL BOEING757 757232 1384965NM APU DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING HMV, FOUND LOWER VERTICAL FIREWALL HAS DEEP CHAFING MARKS FROM RIDING ON DOOR SAFETY LATCH ON RIGHT DOOR APU COMPARTMENT. REPAIRED PER SRM 53-80-08 FIG 202. 2L72 4F RTA2NM 19950526006371995052600637NM 1995 5 26 DL757952260 119950522A21326259782 SENSOR 6259782 BOEING757 757232 1384965NM LT PACK FAILED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11649DL 108C997 24389 AT FL 330 CABIN ALTITUDE WARNING SOUNDED, INITIATED EMERGENCY DESCENT. CABIN WAS AT 10,000 AND CLIMBING. DURING DESCENT HAD LEFT AIRCONDITIONING INOP LIGHT. UNABLE TO MAINTAIN CABIN PRESSURE BECAUSE RT PACK WAS MEL DEFFERRED. LANDED SLC. REPLACED LEFT PACK CONTROLLER AND COMPRESSOR DISCHARGE SENSOR. RETURNED TO SERVICE. 2L72 4F RTA2NM 19950526006381995052600638NM 1995 5 26 DL767952026 119950509A5754144T310022SP TE WEDGE BOEING767 767232 1385132NM NR 7 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 T/E WEDGE OF NR 7 SLAT HAS DENTED BY HAIL STORM CHANGED T/E WEDGE PER CMM 57-43-37. 2L72 4F RTA1NM 19950526006391995052600639NM 1995 5 26 DL767952226 119950522A5754271003896 TE WEDGE BOEING767 767232 1385132NM NR 4 SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH TRAILING EDGE WEDGE DELAMINATED AND DENTED FROM HAIL. REPLACED WEDGE PER CMM 57-43-55. 2L72 4F RTA1NM 19950526006401995052600640NM 1995 5 26 DL76S952035 119950127A5754114T410229 TE WEDGE BOEING767 767332 1382001NM NR 2 SLAT DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11117DL 23276 FOUND T/E DAMAGE DURING INSPECTION, REPLACE T/E WEDGE PER CMM 57-43-45, FOR NR 2 L/E SLAT PANEL. 2L72 4F RTA1NM 19950526006411995052600641NM 1995 5 26 DL76S952066 119950511A5753 SKIN BOEING767 767332 1382001NM NR 1 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11117DL 23276 0 FOUND ON J2 LETTER CHECK, HOLE IN NBR 1 FLAP I/B T/E LOWER SURFACE MARKED. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950526006431995052600643NM 1995 5 26 DL76S952088 119950430A5522 SKIN BOEING767 767332 1382001NM RT ELEV DAMAGED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11135DL 25145 X RT ELEVATOR UPPER SURFACE DAMAGED, OUTBOARD ELEVATOR. SEALED AND POTTED AREAS OF DAMAGE AS PER SRM 59-70-00. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006441995052600644NM 1995 5 26 DL76S952089 119950430A5755 SKIN BOEING767 767332 1382001NM NR 6 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING UPPER SURFACE NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL. REMOVED DAMAGE AND FABRICATED REPLACEMENT CORE AS PER SRM 51-70-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006451995052600645NM 1995 5 26 DL76S952090 119950430A5522 SKIN BOEING767 767332 1382001NM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER ERA 270814-14 AND SRM 55-70-01. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006461995052600646NM 1995 5 26 DL76S952091 119950430A5522 SKIN BOEING767 767332 1382001NM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT ELEVATOR UPPER SURFACE DAMAGED. OUTBOARD ELEVATOR. SANDED AND POTTED AREAS OF DAMAGE AS PER SRM 55-70-01. REPAIRED PER SRM 55-70-01. REPAIRED PER ERA 270814-14. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006471995052600647NM 1995 5 26 DL76S952092 119950430A5755 SKIN BOEING767 767332 1382001NM NR 5 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING UPPER SURFACE NR 5 SPOILER DENTED. REMOVED AND REPAIRED PER SRM 51-70-17 REF FROM 57-70-01. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006481995052600648NM 1995 5 26 DL76S952093 119950430A5755 SKIN BOEING767 767332 1382001NM NR 2 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING UPPER SURFACE OF NR 2 SPOILER DENTED. REPAIRED PER SRM 57-70-01. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006491995052600649NM 1995 5 26 DL76S952094 119950430A5755 SKIN BOEING767 767332 1382001NM NR 6 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING UPPER SURFACE OF NR 6 SPOILER DENTED. REMOVED AND INSTALLED ON RC7. REMOVED PANEL, REMOVED DAMAGE AND FABRICATED REPLACEMENT AS PER SRM 51070-17. REPAIRED PER 51-70-17. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006501995052600650NM 1995 5 26 DL76S952095 119950430A5751 SKIN BOEING767 767332 1382001NM LT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING UPPER SURFACE OF I/B AILERON DENTED. REPAIRED AS PER SRM 57-60-01 REF 51-70-17. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006511995052600651NM 1995 5 26 DL76S952096 119950430A5753 SKIN BOEING767 767332 1382001NM RT TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT WING I/B AFT FLAP UPPER SURFACE DENTED. REPAIRED TWO BONDED AREAS PER SRM 57-53-01 REF 51-70-10. FILLED AND SANDED ALL OTHER DENTS AND ALODINED PER 51-70-01. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006521995052600652NM 1995 5 26 DL76S952097 119950430A5753 SKIN BOEING767 767332 1382001NM RT TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT WING O/B AFT FLAP UPPER SURFACE DENTED. REPAIRED AS PER SRM 51-70-06. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006531995052600653NM 1995 5 26 DL76S952098 119950430A5755 SKIN BOEING767 767332 1382001NM NR 8 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT WING UPPER SURFACE NR 8 SPOILER DENTED, REMOVED. REPAIRED PER B767 SRM 57-70-01 REF 51-70-17. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006541995052600654NM 1995 5 26 DL76S952099 119950501A5522 SKIN BOEING767 767332 1382001NM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X RT INBOARD ELEVATOR UPPER SURFACE DAMAGED BY HAIL. MADE BONDING REPAIRS. REPAIRED PER ERA 270806-14. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006551995052600655NM 1995 5 26 DL76S952100 119950502A5753 SKIN BOEING767 767332 1382001NM LT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 X LT WING O/B AFT FLAP T/E WEDGE HAS SEVERAL DELAMINATED AREAS UPPER SURFACE. MADE REPAIRS PER SRM 51-70-17 REF 57-53-01 AND COMPLY WITH ERA 270849-14. DAMAGE FROM HAIL. 2L72 4F RTA1NM 19950526006561995052600656WP 1995 5 26 DLL10952259 119950523A2150 AIR COND LKHEED1011 10113851 5265010WP CABIN SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO111732D 193C1213 AFTER TAKEOFF SMOKE OCCURED IN CABIN, MOSTLY IN MID TO AFT AREA. RETURNED TO LAX ODOR CLEARED ON LANDING. RAN ALL 3 PACKS INDIVIDUALLY AND WITH AIR FROM ENGINES AND APU, COULD NOT DUPLICATE PROBLEM, RETURNED TO SERVICE. 2L73 4F A23WE 19950526006571995052600657WP 1995 5 26 DLL13952070 119950509A5330 SKIN LKHEED1011 10113851 5265010WP FS 775 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 0 TA HMV FOUND FUSELAGE SKIN CRACKED AND DENTED, AT FS 775 APPROX BETWEEN STRINGERS 20-21. CUTOUT AND DYE CHECKED AREA, ALL DAMAGE REMOVED. FABRICATED DAMPER AND INSTALLED PER SRM 53-31-00 FIG 811. 2L73 4F A23WE 19950526006581995052600658WP 1995 5 26 DLL13952071 119950510A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 579 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 0 AT HMV, FOUND C1 B/B TEAR STRAP DISBONDED, FS 579 BETWEEN STRINGERS 38-39. SAME COND FS 659 BETWEEN STRINGERS 42 AND 44. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950526006591995052600659WP 1995 5 26 DLL13952255 119950511A5330 FAIL/SAFE STRAP LKHEED1011 10113851 5265010WP FS 749-769 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 DISBONDED FAIL/SAFE STRAP BETWEEN STR 37 AND 38 AND FORMER 749 AND 769. FOUND AT HMV, REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950526006601995052600660NM 1995 5 26 DLM88952022 119950510A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11956DL 49887 FOUND DURING F-1 LETTER CHECK, .25 INCH CRACK AT AFT HINGE CUTOUT OF LEFT AFT NOSE GEAR DOOR IN FUSELAGE SKIN. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950526006611995052600661NM 1995 5 26 DLM88952023 119950510A5230 DOOR SKIN DOUG MD88 MD88 3023688NM CARGO COMP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11956DL 49887 FOUND DURING F-1 LETTER CHECK, C-3 DOOR HANDLE CUTOUT SKIN CRACKED .75 INCH FWD SIDE. REPAIRED PER SRM 52-05 FIG 30. 2L72 4F RTA6WE 19950526006621995052600662NM 1995 5 26 DLM88952024 119950510A5400 ANGLE DOUG MD88 MD88 3023688NM LT PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11956DL 49887 FOUND DURING F-1 LETTER CHECK, NBR 1 ENG UPPER PYLON ATTACH ANGLE CRACKED 1.5 INCHES APPROX 10 INCHES FROM AFT END REPAIRED PER SRM 54-04A FIG 4. 2L72 4F RTA6WE 19950526006631995052600663NM 1995 5 26 DLM88952027 119950510A5320 RIB DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11956DL 49887 FOUND ON F1 LTR CK, AFT CROSS OVER RIB AT KEEL BEAM CRACKED. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950526006641995052600664NM 1995 5 26 DLM88952045 119950511A5320 ANGLE DOUG MD88 MD88 3023688NM MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11906DL 49537 FOUND DURING C-1 LETTER CHECK, MLG WHEEL WELL AFT JAMB AFT ANGLE CRACKED .75 INCH. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950526006651995052600665NM 1995 5 26 DLM88952234 119950522A5753 DEFECTOR DOUG MD88 MD88 3023688NM LT TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11926DL 49713 DEBRIS DEFLECTOR SHIELD CRACKED 1.25 INCH ON LEFT WING FLAP. FOUND DURING A-1 LTR CK. REPAIRED PER SRM 57-09 FIG 42. 2L72 4F RTA6WE 19950526006661995052600666NM 1995 5 26 DLM88952235 119950522A5330 SKIN DOUG MD88 MD88 3023688NM NLG DR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11926DL 49713 LEFT NLG DOOR HINGE CUTOUT CRACKED ( AFT HINGE ). FOUND AT A-1 LTR CK. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950526006671995052600667NM 1995 5 26 DLM88952248 119950306A55235910414503 ELEV TAB DOUG MD88 MD88 3023688NM LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11908DL 49539 THREE INCH CRACK FOUND IN TRAILING EDGE SIX INCHES IBD FROM OUTBOARD, TRAILING EDGE AND LARGE AREA OF DELAMINATION, ON LEFT ELEVATOR GEAR TAB. REPAIRED PER SRM-55-04. 2L72 4F RTA6WE 19950526006701995052600670NM 1995 5 26 UPS203284 119950521A5311 FRAME BOEING727 72725C 138400HNM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION IN E/E COMPARTMENT, BS 360, FRAME AT APPROX LBL 35, STRINGER 24-25L. INSTALLED REPAIR PER SRM 53-10-1, 51-40-3. 2L73 4F A3WE 19950526006711995052600671NM 1995 5 26 UPS203285 119950521A5330 SKIN BOEING727 72725C 138400HNM BS 1080 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON SKIN APPROX 1 INCH ABOVE STRINGER 10R, BS 1080, AFT CIRCUMFERENTIAL JOINT. INSTALLED REPAIR PER UPS EO B727-5330-1177K. 2L73 4F A3WE 19950526006721995052600672NM 1995 5 26 UPS203286 119950521A5320 DOOR SILL BOEING727 72725C 138400HNM BS 520-550 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL (SHEAR WEB), LBL 47, STA 520-550 WL 208. INSTALLED REPAIR PER SRM 51-40-2. 2L73 4F A3WE 19950526006731995052600673NM 1995 5 26 UPS203287 119950521A5320 DOOR SILL BOEING727 72725C 138400HNM BS 630 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR SILL (SHEAR WEB), LBL 49, STA 630, WL 208. INSTALLED REPAIR PER SRM 51-40-2. 2L73 4F A3WE 19950526006741995052600674NM 1995 5 26 UPS203288 119950521A5510 BALANCE PANEL BOEING727 72725C 138400HNM LT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON LEFT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 55-10-1, 51-30-2, MM 51-20-21, 51-20-00, 27-30-21. 2L73 4F A3WE 19950526006751995052600675NM 1995 5 26 UPS203289 119950521A5510 BALANCE PANEL BOEING727 72725C 138400HNM RT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB, NR 5 BALANCE PANEL DOUBLER. INSTALLED REPAIR PER SRM 51-30-2, 51-20-1, 55-20-2, 51-10-2, MM 27-30-21. 2L73 4F A3WE 19950526006761995052600676NM 1995 5 26 UPS203290 119950521A5320 MOP SILL BOEING727 72725C 138400HNM GALLEY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON MID GALLY DOOR MOP SILL STA 640-680, RBL 56, WL 208. REPLACED SILL PER SRM 53-10-1, 51-20-1, 51-10-2, 51-30-2, 51-20-4, MM 51-20-151. 2L73 4F A3WE 19950526006771995052600677NM 1995 5 26 UPS203291 119950521A5523 SKIN BOEING727 72725C 138400HNM RT ELEV TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND DELAMINATION ON RT ELEVATOR TAB, UPPER SURFACE. REPLACED TAB PER MM 27-30-00. 2L73 4F A3WE 19950526006781995052600678NM 1995 5 26 UPS203292 119950521A5754 BULLNOSE BOEING727 72725C 138400HNM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION ON NR 2 K FLAP BULLNOSE. REPLACED BULLNOSE PER SOHM 57-51-11 AND MM27-81-11. 2L73 4F A3WE 19950526006791995052600679NM 1995 5 26 UPS203294 119950521A5312 BLKHD FLANGE BOEING727 72725C 138400HNM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSION AROUND NUT PLATE HOLES ON BOTTOM OF FWD FLANGE OF BEAM AT STA 870, LBL6-15, WL 207. REPAIRED FWD FLANGE OF 870 BULKHEAD UPPER CHORD PER UPS EO B727-5310-7012A. 2L73 4F A3WE 19950526006801995052600680NM 1995 5 26 UPS203295 119950521A5313 STRINGER BOEING727 72725C 138400HNM BS 560-590 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CORROSSION ON STR 2R, STA 560-590. INSTALLED REPAIR PER SRM 51-20-4, 53-10-4, 53-10-3, MM 51-20-151. 2L73 4F A3WE 19950526006811995052600681NM 1995 5 26 UPS203296 119950521A5754 COVE PANEL BOEING727 72725C 138400HNM NR 4 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CRACK IN CUTOUT, NR 4 SLAT COVE PANEL, JUST O/B OF ACTUATOR ROD END. INSTALLED REPAIR PER SRM 51-30-2, 51-40-2. 2L73 4F A3WE 19950526006821995052600682NM 1995 5 26 UPS203297 119950521A5751 RIB BOEING727 72725C 138400HNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01946UP 19721 WHILE IN C CHECK, MAINTENANCE FOUND CRACK ON RT ELEVATOR NOSE RIB AT ELEVATOR STA 191.58. REPLACED RIB PER SRM 51-30-2. 2L73 4F A3WE 19950526006831995052600683NM 1995 5 26 UPS403282 119950520A3350 EEL BULBS BOEING747 747121 1384871NM FLIGHT DECK FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20349 MAINTENANCE REPORTED, CREW SVC DOOR SILL EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK. 2L74 4F A20WE 19950526006841995052600684NM 1995 5 26 UPS403283 119950521A3350 EEL BULBS BOEING747 747121 1384871NM FLIGHT DECK FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20349 MAINTENANCE REPORTED, CREW SVC DOORWAY EMERGENCY EXIT LIGHTS OUT. REPLACED LIGHT BULBS. OPS CHECKED OK. 2L74 4F A20WE 19950526006851995052600685WP 1995 5 26 UPS803299 119950524A532036917681 CASTING DOUG DC8 DC873F 302199FWP FS 200 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND CASTING HAS .5 INCH LONG CRACK AT FS 200, LONGERON 26R. REPLACED CASTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950526006861995052600686WP 1995 5 26 UPS803300 119950524A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS 178 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND FINGER DOUBLER CRACKED AT FS 178, LONGERON 31L. REPLACED FINGER DOUBLER SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950526006871995052600687WP 1995 5 26 UPS803301 119950524A54005802736 ANGLE DOUG DC8 DC873F 302199FWP NR 1 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND CRACK AT THE NR 1 PYLON FORWARD HOLE OF THE INBD. SKATE ANGLE LOWER FRONT SPAR. 2L74 4F RT4A25 19950526006881995052600688WP 1995 5 26 UPS803302 119950524A53204251625 FITTING DOUG DC8 DC873F 302199FWP FS 680 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND LONGERON FITTING CRACKED AT FS 680, LONGERON 11R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950526006891995052600689WP 1995 5 26 UPS803303 119950524A53204250521 FITTING DOUG DC8 DC873F 302199FWP FS 857 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND LONGERON 1R END FITTING CRACKED AT FS 857. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950526006901995052600690WP 1995 5 26 UPS803304 119950524A57205616874503 FITTING DOUG DC8 DC873F 302199FWP WS 463 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND LEFT WING STRINGER END FITTING CRACKED AT STA XW 463 AFT OF CENTER SPAR UPPER. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950526006911995052600691WP 1995 5 26 UPS803305 119950524A55317075T6 RIBS DOUG DC8 DC873F 302199FWP VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND VERTICAL STAB LEADING EDGE, 4 RIBS CRACKED AT STA ZFS 217, ZFS 36, ZFS 104, AND ZFS 123. REPAIRED RIBS PER SRM 55-2-0. 2L74 4F RT4A25 19950526006921995052600692WP 1995 5 26 UPS803306 119950524A53139755803 LONGERON DOUG DC8 DC873F 302199FWP FS 1572/1592 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND WEBBING CRACKED AT LONG 21R, FS 1572 AND FS 1592. REPAIRED LONGERON WEB PER SRM 53-2-0. 2L74 4F RT4A25 19950526006931995052600693WP 1995 5 26 UPS803307 119950524A53202024T3 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C-CHECK, MAINTENANCE FOUND LEFT AND RIGHT PRIMARY HEAT EXCHANGER EXHAUST ON LOWER FUSE SKIN DOUBLER CUTOUTS CRACKED AT AFT LOWER CORNERS. REPAIRED PER UPS DC8-5330-4732-0. 2L74 4F RT4A25 19950526006941995052600694WP 1995 5 26 UPS803308 119950524A57535701446 VANES DOUG DC8 DC873F 302199FWP LT/RT TE FLAPS DELAMINATATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND NR 3 LEFT AND RIGHT FLAP VANES DELAMINATED. REPLACED VANE ASSYS PER MM 27-51-14. 2L74 4F RT4A25 19950526006951995052600695WP 1995 5 26 UPS803309 119950524A57535701473 VANES DOUG DC8 DC873F 302199FWP NR 5 TE FLAP DELAMINATATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01802UP 46100 WHILE IN C CHECK, MAINTENANCE FOUND NR 5 FLAP VANES DELAMINATED ON LEFT AND RIGHT WINGS. REPLACED VANE ASSYS PER MM 27-51-14. 2L74 4F RT4A25 19950602000011995060200001NM 1995 6 2 95ZZZM44 119950516A5753 SKIN BOEING747 747124 1384874NM RT TE FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 FOUR AREAS OF DAMAGE RIGHT WING INBOARD AFT FLAP P/N 65B0207020, TWO DEEP GOUGES, ONE IS AFT OF THE NR 3 EXTEND/RETRACT ARM AND THE OTHER ONE IS 34 INCHES FROM THE NR 2 EXTENSION/RETRACTION ARM. TWO AREAS OF DELAMINATION, ONE 6 INCHES FROM TRAILING EDGE OUTBOARD AT THE NR 2 EXTEND/RETRACT ARM. THE OTHER 14 INCHES FROM THE TRAILING EDGE OUTBOARD AT THE NR 2 EXTEND/RETRACT ARM. REPLACED AFT FLAP ASSEMBLY IAW BOEING MM 27-51-03. TOTAL CYCLES 18248. 2L74 4F A20WE 19950602000021995060200002NM 1995 6 2 95ZZZM45 119950517A5753 LE SKIN FLAP BOEING747 747124 1384874NM RT TE FLAP GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 GOUGED LEADING EDGE RIGHT WING OUTBOARD FORE FLAP P/N 65B019014, 28.5 INCHES FROM OUTBOARD EDGE. REPAIRED IAW SRM 51-40-09 TABLE 1. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000031995060200003NM 1995 6 2 95ZZZM46 119950517A5755 SKIN BOEING747 747124 1384874NM LT T/E PANEL DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 LEFT WING TRAILING EDGE PANEL OUTBOARD OF FLIGHT SPOILER P/N 65B0817173, DELAMINATED (FORWARD EDGE AND OUTBOARD REAR). REPAIRED IAW BOEING SRM 51-40-14. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000041995060200004NM 1995 6 2 95ZZZM47 119950516A5730 SKIN BOEING747 747124 1384874NM NR 1 SPOILER DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 LEFT WING TRAILING EDGE PANEL OUTBOARD OF NR 1 SPOILER, P/N 65B0817173, LOWER CORNER DELAMINATED AND WORN TO HONEYCOMB (2 INCH BY 3 INCH AREA). REPAIRED IAW WITH BOEING SRM 51-40-06. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000051995060200005NM 1995 6 2 95ZZZM48 119950517A572065B116152 SKIN BOEING747 747124 1384874NM RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 DELAMINATION (4 INCHES BY 6 INCHES) RIGHT WING PANEL JUST BELOW R3 DOOR. REPAIRED IAW BOEING SRM 51-40-09. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000061995060200006NM 1995 6 2 95ZZZM49 119950517A5751 SKIN BOEING747 747124 1384874NM LT INBD AILERON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 LOWER SURFACE LEFT INBOARD AILERON, P/N 65B001173, 5 INCH AREA CRACKED TO HONEYCOMB. REPAIRED IAW BOEING SRM 51-40-09 TABLE 1. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000071995060200007NM 1995 6 2 95ZZZM50 119950517A5753 SKIN BOEING747 747124 1384874NM LT TE FLAP DEBONDED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 INBOARD LEFT MID FLAP, P/N 65B0202527, OVER 2ND ATTACH ARM OF THE AFT TRAILING EDGE FLAP HAS 2 INCH DEBONDED AREA. REPAIRED IAW BOEING SRM 51-40-15. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000081995060200008NM 1995 6 2 95ZZZM51 119950517A5753 SKIN BOEING747 747124 1384874NM LT TE FLAP DEBONDED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 LEFT INBOARD MID FLAP, P/N 65B0202527, LOWER SURFACE, INBOARD SURFACE NEAR INBOARD TRACK, LEADING EDGE PANEL HAS DEBONDED INBOARD EDGE. REPAIRED IAW BOEING SRM 51-40-15. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000091995060200009NM 1995 6 2 95ZZZM52 119950517A5753 SKIN BOEING747 747124 1384874NM LT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 LEFT INBOARD FORE FLAP, P/N 65B89011601, LOWER SURFACE AFT OF CARRIAGE ATTACH BRACKET HAS 25 INCH AREA OF DELAMINATION. REPAIRED IAW BOEING SRM 51-40-06. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000101995060200010NM 1995 6 2 95ZZZM53 119950517A5751 SKIN BOEING747 747124 1384874NM LT AILERON DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT51131 19733 DELAMINATION LEFT INBOARD AILERON, P/N 65B001173, INBOARD CORNER UPPER AND LOWER SURFACE HAS 12 INCH AREA OF DELAMINATION. REPAIRED AILERON IAW SRM 51-40-15 TABLE 1. TOTAL CYCLES 18,248. 2L74 4F A20WE 19950602000111995060200011NM 1995 6 2 95ZZZM54 119950506A2410731753 CSD BOEING737 737201 1384454NM RIGHT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19252AU2666312122 22758 CLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED. APU WAS ON MEL. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD. OPS CHECK NORMAL. REFERENCE USAA950457. 2L72 4F A16WE 19950602000121995060200012EU 1995 6 2 USAA950206 119950305A3350 EEL WIRING FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19880US 11331 PIT - THE FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. FIXED WIRING PROBLEM AT PREVIOUS REPAIR, ROW 12. (M) 2L72 4F RT 19950602000131995060200013WP 1995 6 2 USAA950412 119950427A5620 WINDOW DOUG DC9 DC931 3022065WP EMERG DOOR EXIT NOISY A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19995VJ 47334 EVV - FLT 1547 - RIGHT FRONT EMERGENCY DOOR EXIT WINDOW NOISY ON CLIMBOUT. FLIGHT RETURNED TO EVV WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE RESEALED THE WINDOW. (Z) 2L72 4F A6WE 19950602000141995060200014WP 1995 6 2 USAA950413 119950416A5320 BEAM DOUG DC9 DC931 3022065WP FS 965-996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 2 CORROSION STATION 965-996 ON RT LAV THRESHOLD BEAM REF C58-53300. MFG THRESHOLD SKIN AND INSTALLED PER DAC DRAWING 9915532-235. (M) 2L72 4F A6WE 19950602000151995060200015WP 1995 6 2 USAA950414 119950324A5330 SKIN DOUG DC9 DC931 3022065WP BS 110 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 110 JUST ABOVE AFT RT MLG DOOR. INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19950602000161995060200016WP 1995 6 2 USAA950415 119950328A5220 PAN DOUG DC9 DC931 3022065WP LT EMER EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .125 INCH CRACK FWD STOP AND .25 INCH CRACK AFT STOP LEFT AFT EMERGENCY EXIT WINDOW. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-20-03. (M) 2L72 4F A6WE 19950602000171995060200017WP 1995 6 2 USAA950416 119950330A5311 BELTFRAME DOUG DC9 DC931 3022065WP FS 1096 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND GOUGE IN STATION 1076 BELTFRAME LONGERON 20R. SPLICED IN SECTION OF BELTFRAME PER SRM 53-03 FIG 32. (M) 2L72 4F A6WE 19950602000181995060200018WP 1995 6 2 USAA950417 119950331A5330 SKIN DOUG DC9 DC931 3022065WP BS 1096 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND TEMP REPAIR STATION 1096 LONGERON 42. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-01 FIG 2. (M) 2L72 4F A6WE 19950602000191995060200019WP 1995 6 2 USAA950418 119950331A5313 LONGERON DOUG DC9 DC931 3022065WP FS 965 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 16R AT STATION 965 RT LAV. ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 4. (M) 2L72 4F A6WE 19950602000201995060200020WP 1995 6 2 USAA950419 119950404A5330 SKIN DOUG DC9 DC931 3022065WP FS 983 DENT A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .075 INCH DEEP .75 INCH LONG AT STATION 983 LONGERON 25L AND 24L. INSTALLED FLUSH DOUBLER REPAIR PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19950602000211995060200021WP 1995 6 2 USAA950420 119950404A5330 FINGER DOUBLER DOUG DC9 DC931 3022065WP FS 965-996 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED FINGER DOUBLER FROM STATION 965 TO 996 LONG 26R. REMOVED AND REPLACED FINGER DOUBLER PER DACO DWG. (M) 2L72 4F A6WE 19950602000221995060200022WP 1995 6 2 USAA950421 119950416A5315991556171 FLOORBEAM DOUG DC9 DC931 3022065WP FS 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL II CORROSION STATION 996 RT LAV FLOORBEAM TOP SIDE, REF C58-53300. MFG FLOORBEAM AND CAP ANGLE 7075-TL AND INSTALLED PER SRM 53-05 FIG 72. 2L72 4F A6WE 19950602000231995060200023WP 1995 6 2 USAA950422 119950416A5315 FLOORBEAM DOUG DC9 DC931 3022065WP FS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL II CORROSION AT STATION 980 LEFT LAV FLOORBEAM, REF C58-53300. REMOVED CORROSION AND INSTALLED FILLER TYPE REPAIR PER USAIR TYPICAL REPAIR 53-10-19 AND SRM 53-05 FIG 20. (M) 2L72 4F A6WE 19950602000241995060200024WP 1995 6 2 USAA950423 119950413A5330 SKIN DOUG DC9 DC931 3022065WP FS 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH SKIN CRACK LOWER AFT CORNER FORWARD AIRSTAIR DOOR AREA STATION 200. INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 57A. (M) 2L72 4F A6WE 19950602000251995060200025WP 1995 6 2 USAA950424 119950411A5311 BELTFRAME DOUG DC9 DC931 3022065WP FS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT STATION 980 BELTFRAME LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER USAIR TYPICAL REPAIR 53-10-13. (M) 2L72 4F A6WE 19950602000261995060200026WP 1995 6 2 USAA950425 119950421A5347 SEAT TRACK DOUG DC9 DC931 3022065WP FS 200-236 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL I CORROSION PREVIOUSLY REWORKED, REF C46-53302 AT RT OUTBOARD SEAT TRACK STATION 200 TO 236. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2L72 4F A6WE 19950602000271995060200027WP 1995 6 2 USAA950426 119950421A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 996 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .25 INCH CRACK AT REAR PRESSURE BULKHEAD STATION 996 TOP RIGHT DOOR FRAME AREA. INSTALLED DOUBLER REPAIR DACO DWG J060088-507. (M) 2L72 4F A6WE 19950602000281995060200028WP 1995 6 2 USAA950427 119950420A5320 FITTING DOUG DC9 DC931 3022065WP OUTBD KEEL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND 1 INCH CRACK AT SUPPORT FITTING AFT SPAR 7 INCHES OUTBOARD OF KEEL BEAM LEFT WHEEL WELL. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (M) 2L72 4F A6WE 19950602000291995060200029WP 1995 6 2 USAA950428 119950418A5311 BELTFRAME DOUG DC9 DC931 3022065WP FS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN STATION 980 BELTFRAME AT HI-LOCK FASTENER LONGERON 16L LEFT LAV AREA. SPLICED IN NEW SECTION OF BELTFRAME PER SRM 53-03 FIG 32 SHT 2. (M) 2L72 4F A6WE 19950602000301995060200030WP 1995 6 2 USAA950429 119950407A5540 ANGLE DOUG DC9 DC931 3022065WP VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING Q-1 CHECK INSPECTION, FOUND A 2 INCH CRACK AT VERTICAL STAB ATTACH ANGLE RT SIDE AFT END OF DRAG ANGLE. INSTALLED EXTERNAL DOUBLER PER SRM 53-05 FIG 23 AND 23A. (M) 2L72 4F A6WE 19950602000311995060200031WP 1995 6 2 USAA950440 119950520A532099577397 CLIP DOUG DC9 DC931 3022065WP FS 995 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19956VJ54443 47588 PIT - SCHEDULED PRODUCTION CONTROL ITEM. FOUND .75 INCH CRACK STATION 995 BETWEEN LONGERSON 15 AND 16 RIGHT SKIN CLIP. SPLICED NEW SECTION OF SKIN CLIP PER SRM 53-03 FIG 6. (M) 2L72 4F A6WE 19950602000321995060200032EU 1995 6 2 USAA950446 119950504A2910 HYD SYSTEM FOKKERF28 F28MK0100 4990807EU NR 1 SYSTEM MALFUNCTIONED A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19898US 11398 MCI - FLT NR 1481 - EN ROUTE TO MCI, CAPTAIN RECEIVED A NR 1 SYSTEM LOW PRESSURE WARNING LIGHT. THE CAPTAIN CONTINUED TO MCI BUT DECLARED AN EMERGENCY. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. (M) 2L72 4F RT 19950602000331995060200033EU 1995 6 2 USAA950451 119950506A3411 LINES FOKKERF28 F28MK0100 4990807EU INSTRUMENTS UNINSTALLED A AUSAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19897US 11392 PIT - FLT 8554 - DURING TAKEOFF AT ROTATION, THE AC LOST ALL INSTRUMENTATION. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO PIT. MAINTENANCE REINSTALLED THE PITOT AND STATIC LINES. OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950602000341995060200034WP 1995 6 2 USAA950452 119950506A3222 STRUT DOUG DC9 DC931 3022065WP NLG REQ'D SERVICE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19969VJ 47421 CLT - FLT NR 2461 - DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT RETURNED TO CLT. MAINTENANCE SERVICED THE STRUT, CLEANED THE TARGET AND TIGHTENED THE CANNON PLUG. THE NOSE GEAR WAS THEN CYCLED. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950602000351995060200035EU 1995 6 2 USAA950453 119950508A213021183865 CONTROL PANEL FOKKERF28 F28MK0100 4990807EU COCKPIT INOP A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19862US9005 11300 BTR - FLT NR 0431 - AT FL 310, CREW RECEIVED RED LIGHTS IN THE COCKPIT. THE CABIN PRESSURE BEGAN CLIMBING RAPIDLY. AIRCRAFT MADE AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO BTR. REPLACED OVERHEAD SELECTOR PANEL DUE TO CONTROLLER INOP. (W) 2L72 4F RT 19950602000361995060200036EU 1995 6 2 USAA950454 119950509A262133100007 FIRE BOTTLE FOKKERF28 F28MK0100 4990807EU APU FIRED A USAAO OTHER NF FALSE WARNING FLT CONT AFFECTED APAPPROACH 1 EA19896US 11391 PHL - FLT NR 0298 - ON APPROACH, CREW RECEIVED AND APU FIRE INDICATION. THE APU AUTOMATICALLY SHUTDOWN AND THE BOTTLE FIRED, P/N 33100007. THERE WERE NO OTHER INDICATIONS OF A FIRE. MAINTENANCE INSPECTED THE APU FIRE EXIT SYSTEM. THE FIRE EXTINGUISHER BOTTLE WAS REPLACED. OPERATIONS CHECKED GOOD. (M) 2L72 4F RT 19950602000381995060200038EU 1995 6 2 USAA950456 119950511A2410 IDG FOKKERF28 F28MK0100 4990807EU RIGHT REQ'D SERVICE A USAAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 EA19865US 11308 PIT - FLT 0214 - EN ROUTE FROM CLT TO MKE, AIRCRAFT LOST APU AND ITS GENERATOR. AIRCRAFT DIVERTED TO PIT. MAINTENANCE SERVICED THE RIGHT IDG WITH OIL. OPERATIONS CHECKED GOOD. (M) 2L72 4F RT 19950602000391995060200039NM 1995 6 2 USAA950457 119950506A2421976J4981 GENERATOR BOEING737 737201 1384454NM RIGHT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19252AU117548013 22758 CLT - FLT 1810 - ON CLIMB-OUT, NR 2 GENERATOR TRIPPED. APU WAS ON MEL. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE GENERATOR AND NR 2 ENGINE CSD. OPS CHECK NORMAL. REFERENCE 95ZZZM54. 2L72 4F A16WE 19950602000401995060200040WP 1995 6 2 9508449302 119950515A3260 UNSAFE LIGHT DOUG DC9 DC982 3022082WP NLG ILLUMINATED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01302RC 48055 DURING CLIMBOUT FROM MSP, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AT SPEED ABOVE 238 KNOTS. RECYCLED GEAR AND LIGHT OPERATED NORMALLY. FLIGHT CONTINUED TO DESTINATION (ONT) AND LANDED WITHOUT INCIDENT. PERFORMED BITE CHECK OF PROXIMITY CONTROL UNIT AND CHECKED WIRING TO NOSE GEAR INDICATION SENSORS. ALL CHECKED OK. ALSO, JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000411995060200041WP 1995 6 2 9508459866 119950515A3150 SWITCH DOUG DC9 DC951 3022051WP PARKING BRAKE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01775NC 47785 TAKEOFF WARNING HORN SOUNDED AS THROTTLES WERE PUSHED FORWARD FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. FOUND PARKING BRAKE SWITCH HAD FAILED, FERRIED AIRCRAFT TO MSP. REPLACED PARKING BRAKE SWITCH. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000421995060200042WP 1995 6 2 9508469910 119950520A2450914F5654 CONTROL PANEL DOUG DC9 DC931 3022065WP AC BUS MALFUNCTIONED A ANWAAO OTHER BE SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET UKUNKNOWN 1 GL01960N 224663464 47256 DURING FLIGHT AND ON APPROACH, AN UNUSUAL VIBRATION WAS ENCOUNTERED WHICH SEEMED TO BE COMING FROM BELOW OR FORWARD OF COCKPIT. AFTER LANDING AND PASSENGER DEPLANEMENT, BLACK SMOKE FILLED THE COCKPIT. EXTINGUISHED ALL POWER TO AIRCRAFT AND PULLED ALL CIRCUIT BREAKERS OVERHEAD. SMOKE CEASED, FOUND AC BUS CONTROL PANEL HAD FAILED. REPLACED PANEL, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000431995060200043NM 1995 6 2 9508472296 119950523A3213659864221 STRUT BOEING727 727251 138408HNM LT MLG FAILED A ANWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01296US237921735 21788 UPON TAKING THE ACTIVE RUNWAY AND CLEARED FOR TAKEOFF, THE AIRCRAFT TAXIED OVER A BUMP. A LARGE NOISE WAS HEARD AND AN UNSAFE INDICATION OF THE LEFT GEAR OCCURRED. THE AIRCRAFT LISTED TWO DEGREES TO THE LEFT, TAKEOFF WAS ABORTED. THE GEAR WAS PINNED AND THE AIRCRAFT TAXIED BACK TO THE GATE. FOUND THE LEFT GEAR OUTER CYLINDER FRACTURED AT THE AFT TRUNNION BEARING JOURNAL. INCIDENT IS UNDER INVESTIGATION. 2L73 4F A3WE 19950602000441995060200044WP 1995 6 2 9508489940 119950516A3010460450 SEALS DOUG DC9 DC932 3022066WP ANTI-ICE DUCT FAILED A NWAAO OTHER O OTHER APAPPROACH 1 GL013322L 47031 ON APPROACH INTO MEM, PASSENGER AT ROW 16 REPORTED EXCESSIVE HEAT COMING FROM FLOOR AREA. BOTH FLOOR AND SIDEWALL WERE HOT TO TOUCH. ENGINE AND WING ANTI-ICE WERE ACTIVATED. CAPTAIN DECLARED AN EMERGENCY AND EQUIPMENT WAS CALLED AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BLOWN SEALS AT ANTI-ICE DUCT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000451995060200045WP 1995 6 2 9508499964 119950514A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAABG UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01912RW 47150 DURING CRUISE AT 33,000 FEET, CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED. CABIN ALTITUDE ROSE ABOVE 10,000 FEET AND OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN. EMERGENCY DESCENT WAS INITIATED AND FLIGHT DIVERTED TO GSP. REPLACED THE CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000461995060200046 1995 6 2 9508509971 419950518A344220852680104 RADAR INDICATOR DOUG DC9 DC931 3022065WP FWD PEDESTAL MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL019335 47337 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. GROUND RETURN WAS PAINTED ON BOTTOM HALF OF SCREEN. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE RADAR INDICATOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000471995060200047WP 1995 6 2 9508519976 119950520A213354447222 OUTFLOW ACTUATOR DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019340 3114523005 47389 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED OUTFLOW VALVE ACTUATOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000481995060200048 1995 6 2 9508529981 419950518A344220671570153 RADAR TR UNIT DOUG DC9 DC931 3022065WP FWD FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01994Z 1108142 47097 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FALSE RETURNS WERE BEING PAINTED AND SPOKING WAS ALSO APPARENT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000491995060200049WP 1995 6 2 9508539857 119950517A3230 DOOR CABLE DOUG DC9 DC951 3022051WP LT MLG FAILED A NWAAO OTHER J WARNING INDICATION UKUNKNOWN 1 GL01766NC 47739 EN ROUTE BIS-MSP, MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT CONTINUED TO DESTINATION AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR SEQUENCING PUSH/PULL CABLE. ALSO, REPLACED TORQUE TUBE LOWER BEARINGS, DOOR SKIDS, AND INSTALLED DOUBLERS ON BOTH DOORS. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000501995060200050WP 1995 6 2 9508549993 119950522A2781 CONNECTOR DOUG DC9 DC931 3022065WP RT LE SLAT LOOSE A NWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL018986E 47402 DURING APPROACH INTO BWI, SLAT BLUE EXTEND LIGHT DID NOT ILLUMINATE AFTER SLAT EXTENSION. PERFORMED GO-AROUND PROCEDURES AND RECYCLED SLATS, STILL NO BLUE LIGHT. FIRST OFFICER VISUALLY CONFIRMED SLATS TO BE EXTENDED. SUCCESSFUL LANDING WAS ACCOMPLISHED USING NO SLATS PROCEDURES. RESEATED CANNON PLUG ON RIGHT SLAT EXTEND SWITCH. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602000511995060200051WP 1995 6 2 9508559959 119950522A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01919RW 47162 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE FROM THE CLIPS USING BOTH THE INTERIOR AND EXTERIOR HANDLES. ADJUSTED BOTH SETS OF CLIPS, CHECKED OK. 2L72 4F A6WE 19950602000521995060200052NM 1995 6 2 9508566622 119950517A5414 SKIN BOEING747 747251B 1384892NM NR 2 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01622US 21704 DURING PERIODIC CHECK, FOUND A CRACK IN THE NR 2 PYLON INBOARD SKIN, NACELLE STA 174, NACELLE WL 151. REPAIRED PER EA 66-098523. 2L74 4F A20WE 19950602000531995060200053WP 1995 6 2 9508579912 119950522A5610 WINDOW SEAL DOUG DC9 DC931 3022065WP RT COCKPIT DETERIORATED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01962N 47406 DURING FLIGHT DFW-DTW, THE FIRST OFFICER'S SLIDING WINDOW DEVELOPED AN EXTREMELY LOUD AIR LEAK THAT INTERFERED WITH FLIGHT COMMUNICATIONS. DIVERTED TO MEM AND LANDED WITHOUT FURTHER INCIDENT. RESEALED WINDOW, CHECKED OK. 2L72 4F A6WE 19950602000541995060200054NE 1995 6 2 95UAL727037 219950515A7314 O-RING BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 FUEL PUMP MISINSTALLED A UALAO OTHER JW WARNING INDICATION INADEQUATE Q C NRNOT REPORTED 1 WP297295U 21573 NR 3 OIL QUANTITY ZERO, POWER REDUCED TO IDLE. OIL PRESSURE 45 AND LIGHT OUT. FOUND THE WRONG O-RING INSTALLED ON THE FUEL PUMP DRIVE SHAFT, REPLACED O-RING. 2L73 4F4 F A3WE E2EA 19950602000551995060200055NM 1995 6 2 95UAL727038 119950525A3232 ACTUATOR WESTERN HYDR731414 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT MLG DOOR MALFUNCTIONED A UALAK NONE L NO TEST TOTAKEOFF 1 WP297251U 21398 RT MLG DOOR LIGHT ON WITH HANDLE IN OFF POS, USED OVERRIDE TO GET HANDLE TO UP POS, LIGHT WENT OUT. ON SECOND TRY GEAR HANDLE HARD TO MOVE UP, NEEDED TRIGGER. REPLACED RIGHT GEAR DOOR ACTUATOR. ALSO, REPLACED LANDING GEAR ACCESSORY MODULE PROX CARDS A11, AND A12. 2L73 4F4 F A3WE E2EA 19950602000561995060200056NE 1995 6 2 95UAL737043 219950403A75307064003 DRIVE MOTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENG BLEED MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29325UA 2086 23957 723220 NUMBER ONE ENGINE EXHAUST GAS TEMPERATURE WENT TO 947 DEGREES FOR LESS THAN TEN SECONDS ON TAKEOFF ROLL. ABORTED TAKEOFF AT 110 KNOTS, SHUTDOWN ENGINE. FOUND BLEED VALVE DRIVE MOTOR INTERMITTENTLY STICKING OPEN. REPLACED BLEED VALVE DRIVE MOTOR. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000571995060200057NM 1995 6 2 95UAL737052 119950413A32466546116 WHEEL BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE MAIN GEAR FAILED A AUALAA UNSCHED LANDING D INFLIGHT SEPARATION TOTAKEOFF 1 WP299040U 19078 ON DEPARTURE, MAIN GEAR WHEEL AND TIRE ASSEMBLY SEPARATED FROM THE AIRCRAFT, RETURNED TO ORD. REPLACED MAIN GEAR INNER CYLINDER DUE TO POSSIBLE HEAT DAMAGE. REPLACED NUMBER ONE ANTI-SKID TRANSDUCER, NUMBER ONE AND TWO TIRE AND BRAKE ASSEMBLY. GEAR SWING CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000581995060200058NM 1995 6 2 95UAL737053 119950418A2910BACH8A08NN04045 HOSE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE WHEEL WELL FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP299061U 19942 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT CAME ON AND HYDRAULIC QUANTITY READS ZERO. REPLACED FAILED 'A' SYSTEM HYDRAULIC HOSE. SERVICED RESERVOIR AND LEAKS CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000591995060200059NM 1995 6 2 95UAL737057 119950426A261217051 FIRE LOOP BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE SHORTED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP299015U 19053 AT 17,000 FEET IN CLIMB, NUMBER 2 FIRE HANDLE FLICKERED INTERMITTENTLY AND EMITTED AN ARCING SOUND. SEEMED TO FLICKER MORE WITH THROTTLE MOVEMENT. FOUND M337 FIRE LOOP DETECTOR SHORTED INTERNALLY. REPLACED DETECTOR AND CORRODED CONNECTOR. CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000601995060200060NM 1995 6 2 95UAL737058 119950503A3350 EEL CHARGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29366UA 24535 FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTING INOP IN FIRST CLASS CABIN. REPLACED M1132 CHARGER AND BATTERY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000611995060200061NM 1995 6 2 95UAL737059 119950508A3230 RETRACT MECH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NLG PINNED A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29907UA 25007 NOSE GEAR DID NOT RETRACT AFTER TAKE OFF. FOUND TOOL INSTALLED IN GEAR PIN DOWN LOCK HOLE. REMOVED TOOL AND INSPECTED, FOUND NO DAMAGE. 2L72 4F4 FRTA16WE E2GL 19950602000621995060200062NM 1995 6 2 95UAL737060 119950508A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29371UA 24540 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 THROUGH ROW 17. REPLACED BATTERY PACK. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000631995060200063NM 1995 6 2 95UAL737061 119950508A3350 EEL BATTERY BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29905UA 25005 EMERGENCY ESCAPE PATH LIGHTING INOP IN FIRST CLASS. REPLACED BATTERY PACK. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000641995060200064NM 1995 6 2 95UAL737062 119950508A3350 EEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN SHORTED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29905UA 25005 EMERGENCY ESCAPE PATH LIGHT STRIP INOP IN FIRST CLASS. FOUND FORWARD LIGHT STRIP SHORTED. REPLACED FORWARD LIGHT STRIP. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000651995060200065NM 1995 6 2 95UAL737063 119950508A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29304UA 23665 RIGHT OVER WING EMERGENCY EXIT LIGHT INOP. SWAPPED BATTERY PACKS. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000661995060200066NM 1995 6 2 95UAL737064 119950510A7930FZH6DE145 CONNECTOR BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE UNMODIFIED A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP299018U 19056 NUMBER ONE ENGINE SLOW TO SPOOL UP, ABORTED TAKEOFF. THE BACKSCHELL OF THE FILTER BYPASS SWITCH CONNECTOR WAS INTERFERING WITH THE THROTTLE LEVER ARM. MODIFIED FILTER BYPASS SWITCH CONNECTOR PER COA 9-9198. CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000671995060200067NM 1995 6 2 95UAL737065 119950515A3350 EEL BATTERY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29311UA 23672 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 3 THROUGH ROW 9. REPLACED BATTERY PACK. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000681995060200068NM 1995 6 2 95UAL737066 119950515A335060243 EEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29905UA 25005 EMERGENCY ESCAPE PATH LIGHTING INOP IN FIRST CLASS. REPLACED LIGHT ASSEMBLY. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000691995060200069NM 1995 6 2 95UAL737067 119950515A3350 EEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29940UA 26675 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000701995060200070NM 1995 6 2 95UAL737068 119950517A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29327UA 24147 EMERGENCY ESCAPE PATH LIGHT STRIPS INOP IN AFT CABIN AND CARPET IS WET. REPLACE EMERGENCY ESCAPE PATH LIGHT AND DRIED CABLE. CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950602000711995060200071NM 1995 6 2 95UAL737069 119950518A3350 EEL BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29989UA 21751 EMERGENCY ESCAPE PATH LIGHTING INOP AT FORWARD ENTRY DOOR. REPLACED LIGHT, CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000721995060200072NM 1995 6 2 95UAL737070 119950522A2150 BOOT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT PACK LOOSE A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29301UA 23642 AUDIBLE SHUDDER OCCURRED AFTER LIFT OFF, ACCOMPANIED BY AIRFRAME SHUDDER. OCCURRED AT FIRST POWER REDUCTION. VIBRATION CONTINUED UNTIL AIRCRAFT RETURNED TO ORD. SECURED RIGHT PACK PRESSURIZATION BOOT AT FORWARD END OF PACK BAY. 2L72 4F4 FRTA16WE E2GL 19950602000731995060200073NM 1995 6 2 95UAL737071 119950522A3260189915 UPLOCK SWITCH BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE RT MLG MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP299075U 19956 ON GEAR RETRACTION THE RIGHT GEAR RED LIGHT ILLUMINATED WITH GEAR HANDLE UP OR OFF. CYCLED GEAR DOWN AND GOT THREE GREEN LIGHTS. RETRACTED GEAR AGAIN AND GOT RED LIGHT CONDITION, RETURNED TO ORD. REPLACED RIGHT MLG UPLOCK SENSORS. ALSO, REPLACED THE A8 RIGHT MLG UPLOCK PROXIMITY CARD. SYSTEM OP CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000741995060200074 1995 6 2 95UAL737072 419950522A3418MR41229 AOA SENSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LEFT MISSING A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29366UA 24535 IMMEDIATELY AFTER TAKEOFF FLAP RETRACTION, STICK SHAKER CAME ON CONTINUOUSLY. STICK SHAKER SOUNDED ALL THE WAY TO THE GATE. LEFT AOA SENSOR WAS FOUND MISSING. 2L72 4F4 FRTA16WE E2GL 19950602000751995060200075NE 1995 6 2 95UAL737073 219950522A7230756506C C-6 BLADE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP299069U 19950 656021 IN CRUISE, FLIGHT LEVEL 290, NUMBER TWO ENGINE EXHAUST GAS TEMPERATURE PEAKED AND EXPERIENCED SEVERE VIBRATION. PULLED THROTTLE BACK TO IDLE AND DIVERTED TO CLE. FAILED C-6 BLADE DAMAGED HIGH AND LOW COMPRESSORS. BLADE FAILED DUE TO TRAILING EDGE IMPACT DAMAGE AND HIGH CYCLE FATIGUE CRACK. 2L72 4F4 F A16WE E2EA 19950602000761995060200076NM 1995 6 2 95UAL737074 119950524A3350 EEL BATTERY BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29988UA 21750 LEFT EMERGENCY EXIT OVERWING ILLUMINATION LIGHT INOP. REPLACED BATTERY PACK. CHECKS OK. 2L72 4F4 F A16WE E2EA 19950602000771995060200077NE 1995 6 2 95UAL737075 219950524A7230 COMPRESSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29342UA 24246 721719 CREW REPORTS, HEARD LOUD BANG AND NUMBER ONE ENGINE N2 STARTED TO DECREASE, CREW SHUTDOWN ENGINE. ENGINE FAILED AT 31,000 FEET, SAW EXHAUST GAS TEMPERATURE SPIKED FOR A SHORT TIME. REPLACED ENGINE, SHOP FINDINGS SHOWED THIRD STAGE COMPRESSOR FAILURE CAUSED BY A THIRD STAGE VARIABLE STATOR VANE. 2L72 4F4 FRTA16WE E2GL 19950602000781995060200078NM 1995 6 2 95UAL747037 119950524A2750 RETRACT MECH BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE TE FLAPS MALFUNCTIONED A UALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP29157UA 20106 EXPERIENCED LOW NOISE AND SLIGHT PITCH AT FL 350. DURING APPROACH WHEN FLAPS GOING FROM 5 TO 10 AND 10 TO 20 DEGREES, EXPERIENCED CONSIDERABLE VIBRATION. 2L74 4F4 F A20WE E20EA 19950602000791995060200079NM 1995 6 2 95UAL767020 119950522A2741 SAM MODULE BOEING 285T0015116 BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE STAB INDICATION MALFUNCTIONED A UALAK NONE N FALSE WARNING TOTAKEOFF 1 WP29605UA 000136 21866 UNWANTED STABILIZER TRIM INDICATION AT 30-40 KNOTS ON TAKEOFF ROLL. WENT OUT WITHIN 2-3 SECONDS, THEN CAME ON AGAIN AT ABOUT 60 KNOTS. AGAIN WENT OUT WITHIN 2-3 SECONDS. ABORTED TAKEOFF. REPLACED THE RIGHT SAM MODULE. OP CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19950602000801995060200080WP 1995 6 2 95UALD10045 119950525A5730 PANEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL LT WING CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP291847U 48263 UNDERWING PANEL JUST OUTBOARD OF NR 3 ENG PYLON HAS A LARGE CIRCULAR, CRACK APPROX 10 INCHES LONG. DAMAGE OCCURRED ON GROUND WHEN CATERING TRUCK STRUCK A/C. REPLACED PANEL. 2L73 4F4 F A22WE E23EA 19950602000811995060200081SO 1995 6 2 COM11899 119950523A30102957D513526 DE-ICER BOOT EMB 120 EMB120RT SO RT LOOSE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01164D 120164 A 4 INCH AREA OF THE RT INBD DE-ICE BOOT HAS COME LOOSE. REPLACED DE-ICE BOOT. 2L72 4T RTA31SO 19950602000821995060200082SO 1995 6 2 COM11900 119950524A2731ATG120TR SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01266CA 120258 TAKEOFF TRIM AURAL WARNING REMAINS ON. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSOR. 2L72 4T RTA31SO 19950602000831995060200083SO 1995 6 2 COM11901 119950524A32311201234700 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01130G 120130 LT MLG INBD GEAR DOOR DOES NOT CLOSE. REPAIRED BROKEN LATCH ASSY ON LANDING GEAR DOOR. 2L72 4T RTA31SO 19950602000841995060200084SO 1995 6 2 COM11902 119950524A326012043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMAK NONE N FALSE WARNING CLCLIMB 1 SO01267CA128171087 120259 LT MLG INTRANSIT LIGHTS REMAIN ON AFTER GEAR RETRACTION. REPLACED THE LANDING GEAR RELAY BOX. 2L72 4T RTA31SO 19950602000851995060200085SO 1995 6 2 COM11903 119950519A2731ATG120TR SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01266CA 120258 TAKEOFF TRIM AURAL WARNING DURING TAKEOFF. REPLACED DEFECTIVE ELEVATOR TRIM TAB PROXIMITY SENSOR. 2L72 4T RTA31SO 19950602000861995060200086SO 1995 6 2 COM11904 119950519A215032144143 SHUTOFF VALVE EMB 120 EMB120RT SO LT PACK INOP A COMAK NONE O OTHER UKUNKNOWN 1 SO01196CA12754158 120196 LT COOLING PACK PRESSURE REDUCING SHUTOFF VALVE FAILED TO CLOSE WHEN PACK FAILED. REPLACED THE LT PRESSURE REDUCING SHUTOFF VALVE. 2L72 4T RTA31SO 19950602000871995060200087SW 1995 6 2 COM20373 119950523A5270 DOOR WARNING SWRNGNSA227 SA227AC 8780603SW CARGO COMPT MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01703CA AC703 CARGO DOOR WARNING ACTIVATED AFTER TAKEOFF. INSPECTED CARGO DOOR AND LATCHING SYSTEM, NO DEFECTS NOTED. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950602000881995060200088SW 1995 6 2 COM20374 119950523A3297 TERMINAL SWRNGNSA227 SA227AC 8780603SW NLG LOOSE A COMAO OTHER N FALSE WARNING CLCLIMB 1 SO01457AM AC694 NLG INTRANSIT INDICATOR DOES NOT WORK. REPAIRED WIRE TERMINAL AT TERMINAL STRIP 114. 2L72 4T RTA8SW 19950602000891995060200089EA 1995 6 2 COM60479 119950524A32465010598 WHEEL 5010598 CNDAIRCL600 CL6002B19 EA NLG VIBRATION A COMAK NONE E VIBRATION/BUFFET CLCLIMB 1 SO01932CA3311 101 AUG910026 7038 VERY HEAVY VIBRATION AND LOUD THUMP FROM NLG AREA AFTER GEAR RETRACTION. REPLACED THE NLG WHEEL ASSY. 2L72 4F RTA21EA 19950602000901995060200090EA 1995 6 2 COM60480 119950523A2760601R751523 SWITCH CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01917CA4787 7017 FLIGHT SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE HYDRAULIC PRESSURE SWITCH 2A. 2L72 4F RTA21EA 19950602000911995060200091WP 1995 6 2 DHL95801003 119950518A323045973405505 RETRACT MECH DOUG DC8 DC873F 302199FWP RT MLG MALFUNCTIONED A TDHLAO OTHER J WARNING INDICATION CLCLIMB 1 SO01801DH 46033 DURING UPLATCH CHECK, GEAR NOT LATCHED LIGHT CAME ON WITH RIGHT GEAR UNSAFE LIGHT ON S/O PANEL. COMPLETED ABNORMAL PROCEDURE. UPLATCH CHECK NORMAL DURING A SECOND TRY. INSPECTED GEAR, UPLATCH AND LINKAGE, PERFORMED SYSTEM TEST PER MM 32-32-5. NO DEFECTS NOTED. 2L74 4F RT4A25 19950602000921995060200092WP 1995 6 2 DHL95804002 119950523A3411B2895003023 PITOT TUBE DOUG DC8 DC873F 302199FWP FIRST OFFICERS PLUGGED A TDHLACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01804DH 46124 ON TAKEOFF FROM BRU, THERE WAS NO AIRSPEED INDICATION ON FIRST OFFICERS SIDE. FOUND FIRST OFFICERS PITOT TUBE BLOCKED BY INSECT. REMOVED AND REPLACED PITOT TUBE IAW M/M 34-12-1. 2L74 4F RT4A25 19950602000931995060200093EU 1995 6 2 QXEA9500162 119950524A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09802PH 11017 GEG - OVERHEAD EMERGENCY LIGHT, SECOND ONE FORWARD OF THE AFT CABIN WALL IS INOP. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURND TO SERVICE. 2L72 4F RTA20EU 19950602000941995060200094NE 1995 6 2 95ZZZX2518 219950404A7310 COUPLING DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 3 FUEL TANK SEPARATED A SRAAK NONE X ENGINE FLAMEOUT LDLANDING 1 SO19875SJ 46063 FLT 3571 - UPON LANDING AT DABAI, NR 3 ENGINE FLAMED OUT. FOUND GAMMA COUPLING ON NR 3 FUEL TANK PRESSURE MANIFOLD SEPARATED, REPLACED SEAL AND ENGINE DRIVEN BOOST PUMP, RE-CONNECTED COUPLING, OPS CHECKED GOOD PER MM. 2L74 4F4 FRT4A25 E2GL 19950602000961995060200096WP 1995 6 2 95ZZZX2520 119950428A3222 STRUT DOUG DC9 DC982 3022082WP NOSE GEAR REQ'D SERVICE A TWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE05907TW 49165 PHL - FLT 139 - RETURNED FROM FLIGHT ACCOUNT WHEN LANDING GEAR WAS RAISED, NOSE GEAR DOOR DID NOT CLOSE. FOUND NOSE GEAR STRUT LOW ON NITROGEN CHARGE. SERVICE TO NORMAL CHARGE. CHECK C-2D - 3-9-95 - MCI. 2L72 4F A6WE 19950602000971995060200097EU 1995 6 2 95ZZZX2521 119950410A5330 SKIN BRAERODH125 HS125700A 4230170EU FUSELAGE CRACKED A KKYAK NONE O OTHER ININSP/MAINT 1 NE03270KA6733 NA0307 A TWO INCH CRACK WAS DETECTED ON THE TOP OF THE FUSELAGE 2 INCHES FORWARD OF FRAME 9, BETWEEN 2 RIVETS THAT ATTACH AN ANTENNA DOUBLER. THERE WAS ALSO MODERATE SURFACE CORROSION. THE CORROSION WAS THE RESULT OF WATER INTRUSION UNDER THE ANTENNA. PART CYCLES, 5281. 2L72 4F A3EU 19950602001011995060200101GL 1995 6 2 95ZZZX2526 219950401A73201564T1005 ACTUATOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 ENG FUEL FAILED A DYRAK NONE O OTHER ININSP/MAINT 1 NM07722MB 146 1287 S754 NR 2 ACTUATOR FAILED. THIS ACTUATOR HAS 1454.9 HOURS SINCE OVERHAUL AND INSTALLATION. THIRD KNOWN PROBLEM WITH OVERHAULED ACTUATOR 'ALSO SPARE ACTUATOR FAILED'. OVERHAUL FACILITY NEEDS MORE THOROUGH BENCH TEST OR SEEK OTHER VENDOR. 1G72 3U3 U H3EU E4CE 19950602001021995060200102GL 1995 6 2 95ZZZX2527 219950401A73201564T1005 ACTUATOR BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL NR 2 ENG FUEL DEFECTIVE A DYRAO OTHER J WARNING INDICATION CRCRUISE 1 NM07722MB S754 IN-FLIGHT FAILURE OF N2 BEEP OF NR 2 ENGINE. INSTALLED OVERHAULED ACTUATOR. CIRCUIT BREAKER TRIPPED, ACTUATOR WAS CAUSE. REPLACED DIODE AND INSTALLED SECOND ACTUATOR FUNCTION CHECK GOOD. 11-23-94 ACTT 3938.0. 1G72 3U3 U H3EU E4CE 19950602001031995060200103NM 1995 6 2 AALA950618 119950407A3350 EEL WIRE BOEING727 727227 1384078NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07728AA 20735 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 24 FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BETWEEN FLOOR LIGHTS AND BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950602001041995060200104NM 1995 6 2 AALA950620 119950407A3350 EEL WIRE BOEING727 727227 1384078NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07728AA 20735 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO BATTERY PACK IN CABIN OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950602001051995060200105NM 1995 6 2 AALA950681 119950415A33500201922001 EEL ASSY BOEING767 767323 1385205NM CABIN INTERMITTENT A AALAK NONE L NO TEST ININSP/MAINT 1 SW07388AA 27448 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT AT PASSENGER SEAT ROW 40B INTERMITTENT. REPLACED EMERGENCY FLOOR LIGHT AT PASSENGER SEAT ROW 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950602001061995060200106NM 1995 6 2 AALA950744 119950427A3297 WIRE BOEING727 727227 1384078NM RT MLG BROKEN A AALAO OTHER N FALSE WARNING DEDESCENT 1 SW07728AA 20735 DFW - FLT 0371 - DURING DESCENT INTO DFW, RT MLG RED AND GREEN LIGHTS ILLUMINATED WITH NO HORN OR DOOR WARNING AND THEN EXTINGUISHED AFTER APPROXIMATELY 1 MINUTE. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPAIRED BROKEN/SHORTED WIRING AT RT MLG LOCK SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950602001071995060200107WP 1995 6 2 AALA950746 119950426A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07219AA 49171 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRED EMERGENCY FLOOR LIGHT WIRING IN FIRST CLASS CABIN FOUND CORRODED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19950602001081995060200108NM 1995 6 2 AALA950775 119950430A33500L3071BPEGL EEL ASSY BOEING757 757223 1384957NM 1R DOOR BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07619AA 24577 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT FORWARD EDGE OF 1R DOOR FOUND BROKEN. REPLACED EMERGENCY EXIT LIGHT AT FORWARD EDGE OF 1R DOOR. SYSTEM GOUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950602001091995060200109NM 1995 6 2 AALA950792 119950502A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07642AA 24600 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950602001111995060200111EU 1995 6 2 SIMA951151 119950425A2710S271100880002 BELLCRANK ASSY AEROSPATR42 ATR42300 8680920EU LT AILERON WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21429MQ 0135 MQT - DURING MBV INSPECTION, MAINTENANCE FOUND LT WING NR 7 BELLCRANK BEARING LOOSE. REPLACED NR 7 BELLCRANK ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001121995060200112EU 1995 6 2 SIMA951152 119950425A2710S2711009100500 BELLCRANK ASSY AEROSPATR42 ATR42300 8680920EU RT AILERON RUSTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21429MQ 0135 MQT - DURING MBV INSPECTION, MAINTENANCE FOUND RT WING OUTBOARD BELLCRANK BEARING RUSTED AND DRY. REPLACED RT WING OUTBOARD BELLCRANK ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001131995060200113NE 1995 6 2 SIMA951212 219950501A73218108001002 EEC AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE RT ENGINE INOP A SIMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW21438AT202 931090127 438 127132 DFW - FLT 3851 - DURING TAKEOFF, RIGHT ENGINE TORQUE 15 PERCENT LOW. CREW ABORTED AND RETURNED TO THE GATE. REMOVED AND REPLACED RIGHT EEC. PERFORMED GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 179. (X) 2H72 4T4 TRTA53EU E20NE 19950602001141995060200114EU 1995 6 2 SIMA951222 119950502A2121011260100 EXTRACT FAN AEROSPATR72 ATR72202 8680940EU COCKPIT FAILED A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21274AT A01353 274 DFW - FLT 3863 - DURING TAXI OUT 'SMELLED SOMETHING BURNING IN COCKPIT, NO VISUAL OF SMOKE'. RETURNED TO GATE. MTX REPLACED EXTRACTION FAN. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001151995060200115EU 1995 6 2 SIMA951231 119950425A2710S2718141700206 LEVER ASSY AEROSPATR42 ATR42300 8680920EU CENTER WING RUSTED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21429MQ 0135 MQT - RT WING AILERON INBOARD BELLCRANK FORWARD BEARING RUSTED. FOUND DURING MBV INSPECTION. REPLACED LEVER ASSY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001161995060200116EU 1995 6 2 SIMA951232 119950503A3350 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A SIMAK NONE C F.O.D. ININSP/MAINT 1 SW21223AT 223 ORD - FORWARD EMERGENCY EXIT AND FLOOR LIGHTS INOP. FOUND WIRE NOT CONNECTED TO POWER SUPPLY. RECONNECTED WIRES - OCK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001171995060200117NE 1995 6 2 SIMA951281 219950508A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LT/RT MALFUNCTIONED A SIMAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SW21266AT 266 121068 GRR - FLT 4288 - DURING TAKEOFF FROM GRR, EXPERIENCED BRIEF LOSS OF POWER REQUIRING FLIGHT CONTROL CORRECTION. POWER LOSS WAS NOTICEABLE, BUT HAPPENED TOO BRIEFLY TO BE NOTICED ON ENGINE INDICATION. MAINTENANCE GROUND RAN AIRCRAFT AND RE-TRIMMED BOTH ENGINES. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T4 TRTA53EU E20NE 19950602001181995060200118EU 1995 6 2 SIMA951291 119950509A33503012001 EEL BATTERY PACK AEROSPATR72 ATR72212 EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21399AT 630 399 DFW - DURING LINE CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE FORWARD PART OF THE CABIN FLASHING. BATTERY PACK FOR POWER SUPPLY 43WL WAS REMOVED AND REPLACED. OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950602001191995060200119EU 1995 6 2 VTZA95155 119950504A3260AIR135022 SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT MAIN GEAR OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27315UE 41033 IAD/PWM - FLT 6578 - DURING TAKEOFF AT 1755 HRS ON 5-4-95, RETURNED TO IAD DUE TO RT MAIN GEAR UNSAFE LIGHT NOT EXTINGUISHING WITH GEAR UP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND ADJUSTED UPLOCK MICROSWITCH. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950602001201995060200120 1995 6 2 WRLA95021 419950428A221119905488 PITCH COMPUTER DOUG DC10 DC1030F 3023504WP NR 1 AUTOPILOT FAILED A WRLAAJ UNSCHED LANDING DUMP FUEL FE FLT CONT AFFECTED VIBRATION/BUFFET CLCLIMB 1 EA27116WA 47906 DURING INITIAL CLIMB, CREW NOTED NR 1 AUTOPILOT UNUSABLE (PITCHING VIOLENTLY). AS NR 2 AUTOPILOT WAS ALREADY ON DEFERRAL, CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. CREW UTILIZED ABNORMAL PROCEDURES INCLUDING DUMPING OF FUEL TO BRING ACFT TO BELOW MAXIMUM LANDING WEIGHT (DUMPED APPROXIMATELY 50,000 POUNDS), AND MADE NORMAL LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING DETERMINED THAT PITCH COMPUTER WAS FAULTING. PITCH COMPUTER REPLACED AND ALL GROUND CHECKS PERFORMED WITH NO FAULT FOUND. ACFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950602001211995060200121 1995 6 2 WRLA95024 419950429A221119905487 PITCH COMPUTER DOUG DC10 DC1030F 3023504WP NR 1 AUTOPILOT FAILED A WRLAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CRCRUISE 1 EA27116WA 47906 UPON COMPLETION OF INITIAL CLIMB, NR 1 AUTOPILOT WOULD NOT CAPTURE DESIGNATED ALTITUDE. AUTOPILOT WOULD NOT HOLD SELECTED ALTITUDE OR SPEED. NR 2 AUTOPILOT ON DEFERRAL. CREW DIVERTED ACFT FOR T/S. FLT CREW USED ABNORMAL PROCEDURES & DUMPED 50,000 POUNDS OF FUEL TO REDUCE ACFT BELOW MLW. ACFT LANDED WITHOUT INCIDENT. MX CONFIRMED NR 1 AUTOPILOT PITCH COMPUTER MALFUNCTIONING. REPLACED NR 1 AUTOPILOT PITCH COMPUTER. NR 2 AUTOPILOT SYS T/S, FAULT DETERMINED TO BE SHORT IN PINS 38-39 OF J3A CANNON PLUG ON LT, OTBD ELEV ACT. SHORT CORRECTED. BITE & STATUS TESTS REMAIN AT CAT I UNTIL SUCCESSFUL FLT TESTS. MX HAD CONTACT WITH FLT CREWS DURING 3 SUCCEEDING FLTS. FLT CREWS REPORT NO MALFUNCTIONS. (X) 2L73 4F RTA22WE 19950602001221995060200122 1995 6 2 95ZZZW717 319950505A61401680640 MONO-POLE BAG JETSTMJETSTM3101 1500215EU LT PROP GOV DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07833JS 725 FLT 4116 - AIRCRAFT RETURNED TO GATE AFTER CREW NOTICED LEFT SRL COMPUTER MALFUNCTION, AND ABORTED TAKEOFF. MAINTENANCE REPLACED SRL COMPUTER MONO-POLE PICK IAW MM 72-10-00. GROUND RAN ENGINE IAW MM 72-00-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602001231995060200123EU 1995 6 2 95ZZZW718 119950505A5270 HARNESS BAG JETSTMJETSTM3101 1500215EU BAG POD DOOR DAMAGED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07837JS 736 FLT 4054 - DOOR 'CAP' LIGHT ILLUMINATED ON TAKEOFF ROLL, CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED DAMAGED WIRE HARNESS TO BAGGAGE POD DOOR MICROSWITCH. DAMAGED WIRE REPLACED IAW MM 20-00-00 STANDARD PRACTICES. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602001241995060200124EU 1995 6 2 95ZZZW719 119950506A3297 WIRE BAG JETSTMJETSTM3101 1500215EU LT MLG UPLOCK CHAFED A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07849JS 812 FLT 4055 - AFTER TAKEOFF GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS RETRACTED, CREW ELECTED TO RETURN TO FIELD. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED CHAFED WIRE LEFT MLG UPLOCK SWITCH HARNESS. REPAIRED CHAFED WIRE IAW MM CHAPTER 20-00-00 STANDARD PRACTICES. FUNCTIONAL CHECK FLIGHT (FCF) CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602001251995060200125NE 1995 6 2 95ZZZW720 219950513A72006058T83G01 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT SIDE FLAME OUT A NVEACD ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TOTAKEOFF 1 SO03273AE 340B273 6058T83G01 FLT NR 4483 - BNA - LEFT ENGINE FLAME OUT ON TAKEOFF. REPLACED LEFT ENGINE. 2L72 4T4 TRTA52EU E8NE 19950602001261995060200126NM 1995 6 2 95ZZZW721 119950511A324060B0015026 BRAKE ASSY BOEING747 747122 1384872NM NR 2 POSITION FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 ON WALKAROUND FOUND NR 2 BRAKE COMING APART. REPLACED BRAKE AND WHEEL ASSEMBLY. PERFORMED INSPECTION PER BOEING MM 5-51-09, NO DAMAGE TO AXLE NOTED. (W) 2L74 4F A20WE 19950602001271995060200127NM 1995 6 2 95ZZZW722 119950505A2910BACU24K6 UNION BOEING747 747124 1384874NM NR 1 PYLON LOOSE NUT A P5CAO OTHER K FLUID LOSS CRCRUISE 1 WP23855FT 19733 AIRCRAFT LEFT ORD WITH 10.5 GALLONS HYDRAULIC FLUID, UPON ARRIVAL AT JFK HYDRAULIC QUANTITY FOR SYSTEM 1 6.5 GALLONS. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W) 2L74 4F A20WE 19950602001281995060200128SO 1995 6 2 C2XA95CL082 119950514A33503071BPE LAMP EMB 120 EMB120RT SO RT FWD EEL BURNED OUT A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0958733 120197 DURNG SCHEDULED MAINTENANCE CHECK, FOUND INTERNAL EMERGENCY LIGHT INOP AT SEAT 6C. MAINTENANCE REMOVED AND REPLACED LAMP IAW 33-51-01. OPERATIONAL CHECK GOOD IAW 33-50-00. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602001291995060200129EU 1995 6 2 C2XA95IA080 119950517A33503011210 LIGHT AEROSPATR42 ATR42320 8680930EU PAX/CREW DOOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0915818 0720 153 IAH - DURING 3A CHECK INSPECTION, FOUND PASSENGER/CREW ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2H72 4T RTA53EU 19950602001301995060200130SO 1995 6 2 C2XA95IA081 119950518A534712026824007 SEAT TRACK EMB 120 EMB120RT SO LT AFT CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950602001311995060200131NE 1995 6 2 C2XA95IA082 219950518A7210RG118 RED GEARBOX EMB 120 EMB120RT SO PWA 118 PW118 NE NR 1 ENGINE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916719111944632 115289 120138 IAH - DURING C-CHECK INSPECTION, FOUND NR 1 ENGINE PROPELLER SHAFT FACE PITTED AND HEAVY RUST ON INSIDE OF PROPELLER SHAFT. MAINTENANCE REMOVED AND REPLACED THE REDUCTION GEARBOX, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA31SO E20NE 19950602001321995060200132EU 1995 6 2 RAIA950502 119950505A3240ACM26810 MASTER CYLINDER BAG JETSTMJETSTM3201 1500217EU COCKPIT REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03427AM9186 876 STL - LEFT FLIGHT OFFICERS BRAKE PEDAL MUSHY, GAUGE SHOWS PRESSURE BUT FEEL MUSHY. MAINTENANCE SERVICED LEFT BRAKE PEDAL FLIGHT OFFICERS SIDE MASTER CYLINDER. TAXI CHECK REVEALED NORMAL, NO LEAKS NOTED. (W) 2L72 4T RTA56EU 19950602001331995060200133EU 1995 6 2 RAIA950503 119950507A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU STA 130 OUT OF CAL A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03431AM9014 9014 881 STL - FLT 7400 - LEFT ENGINE NOT MAKING TORQUE. MAINTENANCE ADJUSTED RT TAKEOFF RPM AND RECALIBRATED LEFT TORQUE SIGNAL CONDITIONER. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950602001341995060200134EU 1995 6 2 RAIA950504 119950506A3350311701 BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN EEL LOW VOLTS A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03433AM8728 1634 885 STL - EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (W) 2L72 4T RTA56EU 19950602001351995060200135WP 1995 6 2 RAIA950505 219950510A7320A218C14 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENG OUT OF ADJ A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03429AM7649 1549 879 66157 STL - FLT NR 7418 - RT ENGINE RPM ACCELERATED TO 104 PERCENT RPM AND STAYED THERE FOR ABOUT 5 SECONDS THEN CAME DOWN TO 103 PERCENT. MAINTENANCE ADJUSTED RT ENGINE ADJUSTMENT SCREWS X AND V AND FLIGHT IDLE FUEL FLOW. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T4 TRTA56EU E4WE 19950602001361995060200136EU 1995 6 2 RAIA950506 119950511A2910B79305A153 LINE BAG JETSTMJETSTM3201 1500217EU RT WHEEL WELL CHAFED A RAIAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 CE03432AM12631 883 STL - FLT 7051 - LOST HYDRAULIC PRESSURE DURING FLIGHT. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC FLEX LINE IN RT GEAR WELL. GEAR SWINGS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (W) 2L72 4T RTA56EU 19950602001371995060200137EU 1995 6 2 RAIA950507 119950511A7712KPT06F84S CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENG MOISTURE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03428AM9124 877 STL - FLT 7341 - LEFT ENGINE LOST POWER, TORQUE DROPPED TO 50 PERCENT. MAINTENANCE CLEANED AND RESEATED LEFT FUEL BY-PASS VALVE CONNECTOR. PERFORMED GROUND RUNS ON SRL AND TTL SYSTEM ON LEFT SIDE ALL ENGINE PARAMETERS NORMAL. (M) 2L72 4T RTA56EU 19950602001391995060200139EU 1995 6 2 RAIA950509 119950513A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF CAL A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03436AM3412 3412 891 STL - FLT 7094 - LEFT TORQUE DROPPED FROM 75 PERCENT TO ZERO, ALL OTHER ENGINE PARAMETERS NORMAL. MAINTENANCE SWAPPED BRIDGES ON LEFT TORQUE SIGNAL CONDITIONER, AND CALIBRATED. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950602001401995060200140EU 1995 6 2 RAIA950510 119950513A61303038240 PROP BRAKE AEROSPATR72 ATR72202 8680940EU RT ENGINE SEIZED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03722TE6153 220 PIA - FLT 7123 - ON TAXI OUT MFC FAULTED, PROPELLER TRIED TO ENGAGE CAUSING IT TO EMIT SMOKE. MAINTENANCE INSPECTED RT ENGINE AND DISCOVERED PROP BRAKE TO BE DAMAGED. REPLACED PROP BRAKE. NO FURTHER DAMAGE NOTED. 2H72 4T RTA53EU 19950602001411995060200141EU 1995 6 2 RAIA950511 119950515A32609EN1C11HB2BB2 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR OUT OF ADJ A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03338TE9953 932 ALO - FLT 7471 - NOSE GEAR INTRANSIT LIGHT WILL NOT EXTINGUISH. MAINTENANCE RESECURED AND ADJUSTED UPLOCK SWITCH ON NOSE GEAR. GEAR SWINGS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950602001421995060200142SO 1995 6 2 RAIA950512 119950517A3610MI160140242 SENSOR EMB 120 EMB120RT SO ZONE 100 MOISTURE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03130AM14139 120134 STL - FLT 7215 - DUCT LEAK LIGHT ILLUMINATED ON 'MAP' PANEL. MAINTENANCE INSPECTED AND CLEANED WATER/MOISTURE FROM DUCT LEAK SENSORS. PERFORMED GROUND RUNS WITH BLEED AIR ON, NO LEAK LIGHT ILLUMINATED. SYSTEM CHECK NORMAL. 2L72 4T RTA31SO 19950602001431995060200143EU 1995 6 2 RAIA950513 119950516A273082363 ACTUATOR AEROSPATR42 ATR42300 8680920EU TAIL FAULTY A RAIAB EMER. DESCENT F FLT CONT AFFECTED DEDESCENT 1 CE032FOR 11830 176 MDW - FLT 7017 - PITCH TRIM ASYMMETRY FAILED INFLIGHT. MAINTENANCE REPLACED PITCH TRIM ACTUATOR. OPERATIONAL TEST OF SYSTEM CHECK GOOD. (W) 2H72 4T RTA53EU 19950602001441995060200144NE 1995 6 2 UF6A950501 219950505A73103035681 FUEL FILTER BAG ATP ATP EU PWA PW120 PW126A NE ZONE 460 CLOGGED A UF6AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03852AW1461 2021 124230 FLT 5102 - SBN - THE NR 2 IMPENDING BYPASS FUEL FILTER CENTRAL WARNING PANEL LIGHT ILLUMINATED. MAINTENANCE REPLACED THE HIGH PRESSURE FUEL FILTER. (W) 2L72 4T4 TRTA27NM E2ONE 19950602001451995060200145EU 1995 6 2 UF6A950502 119950509A335058791 LEAD ASSEMBLY BAG ATP ATP EU 243AS EEL FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03852AW8698 2021 SBN - THE AFT EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED THE AFT LEAD ASSEMBLY. (W) 2L72 4T RTA27NM 19950602001461995060200146EU 1995 6 2 UF6A950503 119950514A33506013211 POWER SUPPLY BAG ATP ATP EU CABIN EEL FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03856AW2381 608 16832 2032 SBN - EMERGENCY LIGHTS INOP, ROW 8 C/D. MAINTENANCE REPLACED THE POWER SUPPLY POSITION 3. (W) 2L72 4T RTA27NM 19950602001471995060200147EU 1995 6 2 VTZA95164 119950512A2751TY176004A TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU RT WING FLAP FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27303UE 41015 FLT 6226 - MHT-IAD - ABORTED TAKEOFF DUE TO THE TAKEOFF WARNING COMING ON DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACE THE RT FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950602001481995060200148WP 1995 6 2 VTZA95169 219950512A732189737527 FCU BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK OR OTHER PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27494UE 810 FLT 6284 - HPN-IAD - ABORTED THE TAKEOFF DUE TO THE RIGHT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT FCU. AIRCRAFT WAS THEN RELEASED FOR A FERRY FLIGHT TO IAD DUE TO THE RIGHT ENGINE VERY SLOW TO MAKE TAKEOFF TORQUE. AIRCRAFT LANDED IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED SCREW 'X'. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T4 TRTA56EU E4WE 19950602001491995060200149EU 1995 6 2 VTZA95170 119950513A56201379595C3 WINDOW BAG JETSTMJETSTM3201 1500217EU FUSELAGE CRACKED A VTZAK NONE O OTHER CLCLIMB 1 EA27487UE 906 FLT NR 6338 - IAD-SYR - DURING CLIMB-OUT, THE WINDOW AT SEAT 3C CRACKED. AIRCRAFT LANDED AT SYR WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THE FERRIED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE WINDOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950602001501995060200150EU 1995 6 2 VTZA95171 119950512A79311241012 TRANSDUCER BAG JETSTMJETSTM3201 1500217EU LT ENG FUEL FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27484UE 899 FLT NR 6906 - LYH-CHO - ABORTED THE TAKEOFF, DUE TO THE LEFT FUEL CAP ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL PRESSURE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950602001521995060200152EU 1995 6 2 VTZA95173 119950513A3233AIR864960 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU RT MAIN GEAR FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27313UE 41026 FLT 6214 - IAD-ORF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE RT MAIN GEAR INTRANSIT LIGHT AND HANDLE LIGHT REMAINING ILLUMINATED AFTER GEAR SELECTED UP. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RETRACTION ACTUATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950602001531995060200153EU 1995 6 2 VTZA95177 119950517A771231033826 SIGNAL COND BAG JETSTMJETSTM3201 1500217EU COCKPIT TORQUE OUT OF LIMITS A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27488UE 907 FLT 6258 - IAD-ALB - ABORTED THE TAKEOFF DUE TO THE RT ENGINE HAVING LOW TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE SWAPPED TO BRIDGE NR 2 AND RECALIBRATED PER CURRENT DSC SHEET. PERFORMED ENGINE RUNS AND ALL PARAMETERS WITHIN LIMITS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA56EU 19950602001541995060200154EU 1995 6 2 VTZA95180 119950517A2761TY176301B ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU RT WING SPOILER FAILURE A VTZAO OTHER J WARNING INDICATION CRCRUISE 1 EA27317UE 41031 FLT 6216 - PVD-IAD - DURING CRUISE, THE RIGHT SPOILER CAPTION LIGHT ILLUMINATED. AIRCRAFT CONTINUED TO IAD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT SPOILER ACTUATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950602001551995060200155 1995 6 2 WTAA950183 419950504A31606227236012 MFD UNIT EMB 120 EMB120RT SO COCKPIT INOPERATIVE A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP17284UE 120145 FAT - AVIONICS MULTIFUNCTION DISPLAY (MFD) CIRCUIT BREAKER TRIPPED ACCOMPANIED BY ELECTRICAL SMOKE ODOR IN COCKPIT REPORTED. MAINTENANCE REMOVED AND REPLACED MFD 85A UNIT. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602001561995060200156NE 1995 6 2 WTAA950184 219950509A73203038025 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17274UE 120054 115413 SFO - LEFT ELECTRONIC ENGINE CONTROL (EEC) TRIPPED OFF LINE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE RESET LEFT EEC. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T4 TRTA31SO E20NE 19950602001581995060200158EU 1995 6 2 WTAA950186 119950418A3260622800200 SWITCH BAG JETSTMJETSTM3101 1500215EU LT MLG UPLOCK BROKEN WIRE A WTAAK NONE N FALSE WARNING APAPPROACH 1 WP17428UE 806 LAX - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REPORTED INOPERATIVE. MAINTENANCE FOUND BROKEN WIRE TERMINAL AT LEFT MAIN LANDING GEAR UPLOCK MICROSWITCH. REPLACED WIRE TERMINAL. LANDING GEAR POSITION INDICATIONS OPERATIONAL CHECK NORMAL ON GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602001591995060200159SO 1995 6 2 WTAA950187 119950506A4920 APU EMB 120 EMB120RT SO COCKPIT FUMES A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP17251YV 120251 SFO - OIL FUMES REPORTED IN COCKPIT WITH APU IN OPERATION. FUMES DIMINISHED AFTER SHUTDOWN OF APU. MAINTENANCE DEFERRED APU PER MEL 49-00-01. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602001601995060200160SO 1995 6 2 WTAA950188 119950508A2121 AIR DIST EMB 120 EMB120RT SO COCKPIT ODOR A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 WP17201YW 120201 RDM - ELECTRICAL BURNING ODOR REPORTED IN COCKPIT AND CABIN DURING FLIGHT. MAINTENANCE INSPECTED AIRCRAFT AND ACCOMPLISHED AIRCRAFT GROUND RUN. NO DEFECTS NOTED. UNABLE TO DUPLICATE REPORTED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602001611995060200161SO 1995 6 2 WTAA950189 119950511A27503075001007 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17280UE 120090 SMF - FLAP CONTROL FAULT REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP CONTROL UNIT AND FLAP ANNUNCIATOR. FLAP SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SRVICE. TEARDOWN REPORT CONFIRMED FLAP CONTROL UNIT TO HAVE CAUSED INTERMITTENT FAULT. (M) 2L72 4T RTA31SO 19950602001621995060200162EU 1995 6 2 95ZZZX2528 119950418A6420 TRUNNION AGUSTAA109 A109K2 0260502EU T/R HUB SLEEVE LOOSE AS DYRAK NONE O OTHER ININSP/MAINT 1 NM07123RX397 10018 UPON 100-HOUR INSPECTION OF AIRCRAFT, TAIL ROTOR HUB ASSY WAS DISASSEMBLED FOR INSPECTION. UPON REMOVAL OF TRUNNION, THE PRESSED-ON SLEEVE HAD MOVED .1250 INCH TO .25 INCH OUTBOARD. TRUNNION AND BUSHINGS WERE REPLACED. AIRCRAFT TT, 396.5. 1G72 3U RTH7EU 19950602001631995060200163EU 1995 6 2 95ZZZX2529 119950424A3340000030279 LENS AGUSTAA109 A109K2 0260502EU LOGO LIGHT FAILED A DYRAK NONE O OTHER ININSP/MAINT 1 NM07123RX450 10018 UPON POST-FLIGHT INSPECTION, ALL 4 'LOGO LIGHTS' HAD BROKEN LENS, APPROXIMATELY ONE-HALF OF THE LENS DEPARTED THE AIRCRAFT IN-FLIGHT. REPLACED LENS AND INSPECTED MAIN AND TAIL ROTOR BLADES. NO DAMAGE FOUND. LENS RETURNED TO DEVORE AVIATION FOR INSPECTION. 1G72 3U RTH7EU 19950602001641995060200164EU 1995 6 2 95ZZZX2530 119950424A33400000302717 LENS AGUSTAA109 A109K2 0260502EU LOGO LIGHT FAILED A DYRAK NONE O OTHER ININSP/MAINT 1 NM07123RX450 10018 UPON POST-FLIGHT INSPECTION, ALL 4 'LOGO LIGHTS' HAD BROKEN LENS, APPROXIMATELY ONE-HALF OF THE LENS DEPARTED THE AIRCRAFT IN-FLIGHT. REPLACED LENS AND INSPECTED MAIN AND TAIL ROTOR BLADES. NO DAMAGE FOUND. LENS RETURNED TO DEVORE AVIATION FOR INSPECTION. 1G72 3U RTH7EU 19950602001651995060200165EU 1995 6 2 95ZZZX2531 119950424A63201090729243 TRANSDUCER AGUSTAA109 A109K2 0260502EU TRANSMISSION OILDEFECTIVE A DYRAK NONE O OTHER ININSP/MAINT 1 NM07123RX57 014 10018 UPON LANDING, PILOT REPORTS TRANSMISSION OIL PRESSURE WAS PEGGED TO THE HIGH SIDE ON APPROACH TO HOSPITAL HELIPAD. REPLACED TRANSDUCER, OPS CHECKED OKAY. 1G72 3U RTH7EU 19950602001781995060200178CE 1995 6 2 95ZZZX2544 119950427A2910AE1003957G0310 LINE CESSNA402 402C 207590RCE RT ENG HYD FAILED A SQFAAO UNSCHED LANDING OTHER JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SO175736C 402C0031 PILOT REPORTED BOTH FLOW LIGHTS CAME ON AND STAYED ON AFTER TAKEOFF. IMMEDIATELY, GEAR WAS LOWERED, MAINS LOCKED AND NOSE GEAR UNSAFE. BLEW GEAR BOTTLE, NOSE GEAR LOCKED DOWN. FOUND RT LINE FROM PUMP TO FIREWALL BLOWN, PN AE1003957G0310. REPLACED LINE WITH NEW LINE. OPERATED GEAR MORE THAN TEN TIMES FOR BLEEDING, ALL NORMAL. 1L72 3O A7CE 19950602001871995060200187EU 1995 6 2 95ZZZX2553 119950410A6700 BELLOWS BOLKMS117 BK117B2 5626013EU FLIGHT CONTROL TORN A RMXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW05 BELLOWS PULLED FROM STOCK, PART WAS RIPPED/TORN WHEN REMOVED FROM PACKAGE (2 EACH). 1G72 3U NCH13EU 19950602001881995060200188WP 1995 6 2 HAL95047 119950417A57535913560156 NOSE CAP DOUG DC9 DC951 3022051WP RT WING T/E FLAPCORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA NR 310, C-CHECK, LEVEL 2 WIDESPREAD CORROSION AND DISBONDING OF BONDED DOUBLER ON INTERIOR AND EXTERIOR SURFACES OF RT WING TRAILING EDGE FLAP, TRAILING EDGE PANEL. REMOVED AND REPLACED LEADING EDGE CAP ON WORK ORDER B00380900018. (X) 2L72 4F A6WE 19950602001891995060200189WP 1995 6 2 HAL95048 119950420A5313 STRINGER DOUG DC9 DC951 3022051WP FS 699 RBL 13 CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA NR 18N00907 C-CHECK, LEVEL 2 CORROSION ON STRINGER AND AROUND FASTENERS STA 699 - STA 770, RBL 13 (KEEL BEAM AREA). REMOVED CORROSION, CLEANED AND TREATED PER SRM 51-10-3. INSTALLED REPAIRED SPLICE PER SRM 53-02. (X) 2L72 4F A6WE 19950602001901995060200190WP 1995 6 2 HAL95049 119950417A5330 SKIN DOUG DC9 DC951 3022051WP FS 674 STR 29L CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA NR 18N00094 C-CHECK, D.P.M. P061002, SEVERE CORROSION, FUSELAGE SKIN STA 674 BETWEEN LONGERON 30 AND LONGERON 29 LEFT. REMOVED TEMPORARY REPAIR, REMOVED CORROSION AND TREATED. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-10-1 AND SRM 53-04, FIGURE 43, PAGE 251. (X) 2L72 4F A6WE 19950602001911995060200191WP 1995 6 2 HAL95050 119950420A5320 STIFFENER DOUG DC9 DC951 3022051WP FS 868 STR 21R CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - ITEM FROM SBA NR 18N00882 C-CHECK, LEVEL 2 CORROSION EXTERNAL SKIN STIFFENER STA 868, AT STR 21R. REMOVED DAMAGED STIFFENER AND REINSTALLED NEW STIFFENER PER SRM 51-30-2 AND SRM 51-10-03. (X) 2L72 4F A6WE 19950602001921995060200192 1995 6 2 COM11905 419950526A3418C818061 COMPUTER EMB 120 EMB120RT SO E/E COMPT DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01255CA10150 120238 DURING TAKEOFF ROLL, THE STALL WARNING CAME ON. REPLACED STALL WARNING COMPUTER. 2L72 4T RTA31SO 19950602001931995060200193SW 1995 6 2 COM20375 119950525A29102781032315 HYD LINE SWRNGNSA227 SA227AC 8780603SW LT WING LEAKING A COMAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01459AM AC700 HYDRAULIC FLUID LEAKING FROM LT WING. REPLACED LANDING GEAR EXTENSION, HYDRAULIC TUBING IN LT WING CENTER SECTION. 1L72 4T A8SW 19950602001941995060200194EU 1995 6 2 COM31086 119950525A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01342CA5989 DEC910155 340A023 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950602001951995060200195EU 1995 6 2 COM31087 119950523A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA9870 355 JAN920203 340A064 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950602001961995060200196EU 1995 6 2 COM31088 119950525A2613 HOT WARNING SAAB SF340 SF340A 7850100EU RT TAIL PIPE ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01341CA 340A021 RT TAIL PIPE HOT WARNING LIGHT CAME ON AFTER TAKEOFF. COULD NOT DUPLICATE PROBLEM. INSPECTED SYSTEM AND FOUND NO DEFECTS. 2L72 4T RTA52EU 19950602001971995060200197EU 1995 6 2 COM31089 119950528A6120 GEAR BOX SAAB SF340 SF340A 7850100EU RT PROP LOW OIL A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01356CA 340A034 RT PROPELLER WILL NOT COME OUT OF FEATHER. SERVICED RT PROPELLER GEAR BOX TO PROPER OIL LEVEL. 2L72 4T RTA52EU 19950602001981995060200198EU 1995 6 2 COM31090 119950529A7603C822246 CABLE ASSY SAAB SF340 SF340A 7850100EU LT ENGINE BROKEN A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01380CA 340A012 LEFT ENGINE CONDITION CONTROL IS INOP. REPLACED BROKEN CONDITION CONTROL CABLE. 2L72 4T RTA52EU 19950602001991995060200199EU 1995 6 2 COM31091 119950525A7712 CTOT SYST SAAB SF340 SF340A 7850100EU RT ENGINE MALFUNCTIONED A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01340SF 340A014 WITH CTOT ENGAGED, THE RT ENGINE TORQUE ADVANCED TO 120 PERCENT. PLACED CTOT SYSTEM ON DEFERRED MAINTENANCE LIST AND AIRCRAFT CONTINUED SERVICE. 2L72 4T RTA52EU 19950602002001995060200200EA 1995 6 2 COM60481 119950525A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT TE FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION LDLANDING 1 SO01937CA2681 230 7044 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE LT FLAP BRAKE AND POSITION SENSING UNIT. 2L72 4F RTA21EA 19950602002011995060200201 1995 6 2 COM60482 419950524A3170MS27473T14B19 CONNECTOR CNDAIRCL600 CL6002B19 EA CABIN DOOR DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01934CA2261 7042 OVERBOARD COOL MESSAGE ON EICAS. CLEANED PASSENGER DOOR WIRING CONNECTORS CLEARED FAULT CODES FROM PSEU. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950602002021995060200202EA 1995 6 2 COM60483 119950525A3230 RETRACT MECH CNDAIRCL600 CL6002B19 EA NLG LACK OF LUBE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01914CA 7012 NLG DISAGREE MESSAGE DURING GEAR EXTENSION. COULD NOT DUPLICATE PROBLEM, LUBRICATED NLG AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950602002031995060200203EA 1995 6 2 COM60484 119950529A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 EA LT COCKPIT CRACKED A COMAK NONE O OTHER APAPPROACH 1 SO01914CA2330 7012 PILOTS WINDSHIELD INNER PANE CRACKED. REPLACED WINDSHIELD. 2L72 4F RTA21EA 19950602002041995060200204EA 1995 6 2 COM60485 119950529A275026WC98SN BPSU WIRE CNDAIRCL600 CL6002B19 EA RT TE FLAP BROKEN A COMAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SO01933CA2710 7040 FLAPS FAIL MESSAGE ON EICAS. REPAIRED BROKEN WIRE AT CONNECTOR 2P2CE AT RT BPSU. 2L72 4F RTA21EA 19950602002051995060200205NM 1995 6 2 DL72W952278 119950524A3350900835A EEL BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112820W 21058 DURING PREFLIGHT CHECK, CABIN OVERHEAD EMERGENCY LIGHT AT FS 480 WERE FOUND INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950602002061995060200206NM 1995 6 2 DL73S952279 119950524A2761654496112 ACTUATOR BOEING737 737232 1384475NM LT WING SPOILER CRACKED A DALAO OTHER K FLUID LOSS APAPPROACH 1 SO11318DL 23090 ON APPROACH DURING FLAP EXTENSION, LOST A SYSTEM HYDRAULICS. PRESSURE AND QTY WENT TO ZERO, LANDED CVG. FOUND LEFT OUTBOARD SPOILER ACTUATOR WITH A CRACKED HOUSING. REPLACED ACTUATOR, OPERATION NORMAL. 2L72 4F RTA16WE 19950602002071995060200207NM 1995 6 2 DL757952280 119950524A5754114N3002119A TE PANEL BOEING757 757232 1384965NM NR 5 LE SLAT SEPARATED A ADALAA UNSCHED LANDING ED VIBRATION/BUFFET INFLIGHT SEPARATION CLCLIMB 1 SO11646DL 24217 ON CLIMBOUT FROM CVG HAD AIRFRAME VIBRATION, RETURNED CVG. FOUND A 4 FOOT SECTION OF LEFT WING NR 5 L/E SLAT TRAILING EDGE WEDGE HAD SEPARATED FROM THE SLAT PANEL. THE SLAT WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS, NEW SLAT PANEL WAS INSTALLED FOR RETURN TO SERVICE. 2L72 4F RTA2NM 19950602002081995060200208WP 1995 6 2 DLL13952270 119950501A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 DURING INSPECTION, FS 1363 LOWER CAP ANGLE WAS FOUND CRACKED BETWEEN STRINGERS 27 AND 28. REPAIRED ANGLE PER DL ERA 270932-14 AND SRM 53-11-00. 2L73 4F A23WE 19950602002091995060200209WP 1995 6 2 DLL13952271 119950502A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 DURING INSPECTION, FOUND FS 1363 LOWER CAP ANGLE CRACKED BETWEEN STRINGERS 37 AND 38. REPAIRED PER DL ERA 270932-14 AND SRM 53-11-00. 2L73 4F A23WE 19950602002101995060200210WP 1995 6 2 DLL13952272 119950503A5330 SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 DURING X-RAY INSPECTION OF PREVIOUS REPAIR AT FS 1363 BETWEEN STRINGERS 23 AND 24, CRACK WAS FOUND EXTENDING PAST PREVIOUS STOP DRILL. NEW REPAIRS WERE ACCOMPLISHED PER SRM 53-11-00 PG 853. 2L73 4F A23WE 19950602002111995060200211WP 1995 6 2 DLL13952273 119950504A5330 SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKS A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 X-RAY INSPECTION SHOWS 2EA CRACKS IN FUS SKIN AT FS 1363 BETWEEN STR 43 AND 44, WITH NO STOP DRILL SHOWN AT PREVIOUS REPAIR. REMOVED INTERNAL DOUBLERS, FOUND STOP DRILL HOLE .3750 IN E/C INSP NO CRACK INDICATIONS PAST HOLE. REPAIRED PER SRM 53-11-00 PG 826. 2L73 4F A23WE 19950602002121995060200212NM 1995 6 2 DLM88952281 119950524A2150 PACK DOUG MD88 MD88 3023688NM CABIN ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11959DL 49978 AFTER TAKEOFF HAD STRONG BURNING ODOR IN MID CABIN AREA, RETURNED ATL. TROUBLESHOOTING DETERMINED CAUSE OF ODOR FROM OIL CONTAMINATION IN PACK. REPLACED WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT. RETURNED TO SERVICE. 2L72 4F RTA6WE 19950602002141995060200214NM 1995 6 2 MWEA95207 119950526A2560 GIRT BAR DOUG MD88 MD88 3023688NM AFT GALLEY DOOR JAMMED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 CREW REPORTS AFT GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR DIFFICULT TO DISARM. MAINTENANCE COULD NOT DUPLICATE PROBLEM. HOWEVER, THEY SUSPECT GIRT BAR FABRIC GETTING JAMMED IN LATCHES WHILE ARMING. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950602002151995060200215WP 1995 6 2 MWEA95208 119950527A3260H164 SWITCH DOUG DC9 DC915 3022036WP RT MLG MALFUNCTIONED A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31400ME 45727 CREW REPORTED, AFTER GEAR RETRACTION, AND DURING CLIMB CHECK LIST, RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MKE. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED RIGHT MAIN GEAR UPLATCH SWITCH AS A PRECAUTIONARY. PERFORMED GEAR SWING IAW DOUGLAS MM. ALL FUNCTIONS NORMAL. 2L72 4F A6WE 19950602002161995060200216NM 1995 6 2 MWEA95209 119950528A5754 SKIN DOUG MD88 MD88 3023688NM RT NR 2 LE SLAT CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31701ME 49760 DURING ROUTINE INSPECTION, 2 - 3 INCH CRACKS WERE FOUND ON THE RT NR 2 SLAT APPROX 8 INCHES APART, UNDERSIDE OF SLAT. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER IAW SRM 57-10-1 AND 51-10-3. RETURNED AC TO SERVICE. 2L72 4F RTA6WE 19950602002171995060200217WP 1995 6 2 MWEA95210 119950528A5312 DOOR FRAME DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 47673 DURING ROUTINE INSPECTION, A 3 INCH CRACK WAS FOUND IN RADIUS OF DOOR FRAME STRUCTURE IN AFT PRESSURE BULKHEAD RT SIDE. MAINTENANCE INSTALLED SPLICE REPAIR IAW DOUGLAS TELEX NR SVC-ORD-0062/DMF. REF REWORK DWG J060110 2N 56 THROUGH 60. PERFORMED PRESSURIZED LEAK CHECK. RETURNED AC TO SERVICE. 2L72 4F A6WE 19950602002181995060200218NM 1995 6 2 SCNA95117 119950524A3350900835A EEL BATTERY PACK BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 FORWARD LEFT AND AFT OVERWING EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1090 PER MM 33-50-22 PAGE 22. LIGHTS OPS CHECKED GOOD. 2L73 4F RTA3WE 19950602002191995060200219NM 1995 6 2 UPS203310 119950526A531270705T6 ANGLE BOEING727 72730C 1384009NM FS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 31 TO 39, WL 160. INSTALLED NEW SUPPORT ANGLE IAW SRM 51-30-2, 51-30-8, 51-20-4 AND 53-10-1. 2L73 4F A3WE 19950602002201995060200220NM 1995 6 2 UPS203311 119950526A53117075T6 FRAME BOEING727 72730C 1384009NM FS 235.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON AFT SIDE OF WEB BS 235.8, LBL 44 TO 48, WL 226 TO 234. REMOVED AND SPLICED NEW WEB SECTION PER SRM 51-40-2. 2L73 4F A3WE 19950602002211995060200221NM 1995 6 2 UPS203313 119950526A532066147361 EXPANSION LINK BOEING727 72730C 1384009NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK (PN 66-14736-1, 69-20112-2), ATTACH FITTING AT STA 740, RBL 13, WL 165. REMOVED AND INSTALLED NEW EXPANSION LINK IAW SRM 51-10-1. 2L73 4F A3WE 19950602002221995060200222NM 1995 6 2 UPS203314 119950526A53307075T6 DOUBLER BOEING727 72730C 1384009NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON ACCESS PANEL DOUBLER STA 870, LBL 58, WL 181. REMOVED AND INSTALLED NEW DOUBLER IAW SRM 51-20-1, 51-30-5, 51-30-8, 51-10-2, 51-30-2, 51-10-4, AND M/M 51-20-151. 2L73 4F A3WE 19950602002231995060200223NM 1995 6 2 UPS203315 119950526A53207075T6 DOUBLER BOEING727 72730C 1384009NM FS 312-315 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON WEB DOUBLER AT BS 312 TO 315, LBL 12, WL 181. REPLACED DOUBLER PER SRM 53-10-2, 51-20-1, 53-10-1, 51-10-6, 51-10-2. 2L73 4F A3WE 19950602002241995060200224NM 1995 6 2 UPS203316 119950526A5320654414173 BRACKET BOEING727 72730C 1384009NM FS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FRAME BRACKET MOUNT BS 480, RBL 28 TO 48. INSTALLED NEW BRACKET PER SRM 51-10-2, 51-30-2, 53-10-1 AND M/M 51-20-151. 2L73 4F A3WE 19950602002251995060200225NM 1995 6 2 UPS203317 119950526A53202024T3 WEB BOEING727 72730C 1384009NM FS 840 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON WEB AT STA 840 TO 848, RBL 65, WL 208. INSTALLED NEW WEB IAW SRM 51-10-1, 51-30-2, 51-10-2, 53-10-1 AND M/M 51-20-151. 2L73 4F A3WE 19950602002261995060200226NM 1995 6 2 UPS203318 119950526A5754 RIB BOEING727 72730C 1384009NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 6 SLAT RIB CRACKED. INSTALLED NEW DOUBLER IAW 727 SRM 57-50-3. 2L73 4F A3WE 19950602002271995060200227NM 1995 6 2 UPS203319 119950526A5754 RIB BOEING727 72730C 1384009NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 6 SECOND RIB O/B OF ACTUATOR ROD END CRACKED. REPAIRED IAW SRM 57-50-3. 2L73 4F A3WE 19950602002281995060200228NM 1995 6 2 UPS203320 119950526A574169139017 BOTTLE PIN BOEING727 72730C 1384009NM RIGHT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTLE PIN FOR RIGHT WING, ZONE 6 AREA 75. REMOVED AND REPLACED BOTTLE PIN IAW SRM 57-41-01, 57-10-7, 57-41-11. 2L73 4F A3WE 19950602002291995060200229NM 1995 6 2 UPS203321 119950526A53207075T6 ANGLE BOEING727 72730C 1384009NM FS 259.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON L-ANGLE, AFT SIDE OF WEB FRAME, BS 259.5, WL 218, LBL 45 TO 51. REMOVED AND INSTALLED NEW L-ANGLE IAW SRM 51-10-2, 51-30-2. 2L73 4F A3WE 19950602002301995060200230NM 1995 6 2 UPS203322 119950526A53202024T3 SHEAR WEB BOEING727 72730C 1384009NM FS 1151/1165 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON LT AFT SHEAR WEB AT STA 1151, LBL 49, STA 1165, LBL 37, WL 208. REMOVED AND INSTALLED NEW SHEAR WEB IAW 51-30-2, 51-40-2, 51-10-2, 51-10-6. 2L73 4F A3WE 19950602002311995060200231NM 1995 6 2 UPS203323 119950526A53207075T6 WEB BOEING727 72730C 1384009NM FS 259.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON AFT SIDE OF STA 259.5, RBL 51, WL 212 TO 214. REMOVED AND FABRICATED REPAIR PARTS IAW 51-40-2, 53-10-2, 51-40-2. 2L73 4F A3WE 19950602002321995060200232NM 1995 6 2 UPS203324 119950526A52306518620114 FRAME BOEING727 72730C 1384009NM CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FORWARD CARGO DOOR, LOWER AFT FRAME. INSTALLED NEW AFT LOWER FRAME IAW SRM 51-30-2. 2L73 4F A3WE 19950602002331995060200233NM 1995 6 2 UPS203325 119950526A5241651672060 BEAM BOEING727 72730C 1384009NM GALLEY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON MID GALLEY DOOR ON TRANSVERSE BEAM, THIRD FROM TOP 7 INCHES AND 19 INCHES FROM AFT EDGE OF DOOR. REMOVED AND REPLACED TRANSVERSE BEAM IAW SRM 53-10-1, 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950602002341995060200234NM 1995 6 2 UPS203326 119950526A5313 STRINGER BOEING727 72730C 1384009NM FS 388 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 18L BS 388. SPLICED NEW STRINGER SECTION IAW SRM 53-10-3. 2L73 4F A3WE 19950602002351995060200235NM 1995 6 2 UPS203327 119950526A5313 STRINGER BOEING727 72730C 1384009NM FS 370-375 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 24 RT, BS 370 TO 375. FABRICATED STRINGER REPAIR PARTS AND INSTALLED IAW SRM 53-10-3, 51-20-151, 51-10-2. 2L73 4F A3WE 19950602002361995060200236NM 1995 6 2 UPS203328 119950526A53117075T6 FRAME BOEING727 72730C 1384009NM FS 900 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKED STUB FRAME STA 900, STR 15R, RBL 70.5. INSTALLED FABRICATED REPAIR DOUBLER IAW SRM 51-30-2 AND M/M 51-20-151. 2L73 4F A3WE 19950602002371995060200237NM 1995 6 2 UPS203329 119950526A53152024T3 FLOORBEAM BOEING727 72730C 1384009NM FS 825 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AT STA 825, RBL 62, WL 208. INSTALLED FABRICATED SUPPORT ANGLE IAW SRM 53-10-1, 53-10-2, 51-30-2, 51-20-4 AND M/M 51-20-151. 2L73 4F A3WE 19950602002381995060200238NM 1995 6 2 UPS203330 119950526A5320652617313 INTERCOSTAL BOEING727 72730C 1384009NM FS 312-320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL STATION 312 TO 320, LBL 31, WL 208. REMOVED AND REPLACED INTERCOSTAL IAW SRM 53-10-1, 51-10-6. 2L73 4F A3WE 19950602002391995060200239NM 1995 6 2 UPS203331 119950526A53477075T6 SEAT TRACK BOEING727 72730C 1384009NM FS 660-720 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK STA 660 TO 720, RBL 55, WL 208. INSTALLED FABRICATED SEAT TRACK IAW SRM 51-30-5, 51-30-2. 2L73 4F A3WE 19950602002401995060200240NM 1995 6 2 UPS203332 119950526A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 480-490 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AT BS 480 TO 490, RBL 45, WL 208. SPLICED IN NEW SECTION IAW SRM 53-10-5. 2L73 4F A3WE 19950602002411995060200241NM 1995 6 2 UPS203333 119950526A5543 SKIN BOEING727 72730C 1384009NM RUDDER TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND DELAMINATION ON LOWER RUDDER TAB. REPAIRED IAW M/M 51-20-151. 2L73 4F A3WE 19950602002421995060200242NM 1995 6 2 UPS203334 119950526A5543 SKIN BOEING727 72730C 1384009NM RUDDER TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB. REPAIRED IAW M/M 51-20-151 AND SRM 51-40-6. 2L73 4F A3WE 19950602002431995060200243NM 1995 6 2 UPS203335 119950526A540065174853 WEB BOEING727 72730C 1384009NM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND LT PYLON WEB CRACKED ON UPPER VERTICAL STAB. REMOVED AND REPLACED WEB IAW SRM 51-30-2. 2L73 4F A3WE 19950602002441995060200244NM 1995 6 2 UPS203336 119950526A5511 RIB BOEING727 72730C 1384009NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB UPPER RIB CHORD AT STAB STA 32.08, ABOVE ACCESS PANELS 9205 AND 9212. 2L73 4F A3WE 19950602002451995060200245NM 1995 6 2 UPS203337 119950526A57207075T6 SUPPORT BOEING727 72730C 1384009NM WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 1 K-FLAP ACTUATOR I/B SUPPORT CHANNEL CRACKED. INSTALLED FABRICATED I/B SUPPORT IAW SRM 57-20-2, 51-30-2, M/M 27-81-22. 2L73 4F A3WE 19950602002461995060200246NM 1995 6 2 UPS203338 119950526A575465162275 K-FLAP BOEING727 72730C 1384009NM NR 1 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 1 K-FLAP HAS PITTING CORROSION. INSTALLED NEW K-FLAP IAW M/M 27-81-01. 2L73 4F A3WE 19950602002471995060200247NM 1995 6 2 UPS203339 119950526A5755659892420 ANGLE BOEING727 72730C 1384009NM NR 12 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 12 SPOILER SUPPORT O/B SPAR ATTACH ANGLE CRACKED. REMOVED AND REPLACED SPOILER SUPPORT ANGLE IAW SRM 51-30-2. 2L73 4F A3WE 19950602002481995060200248NM 1995 6 2 UPS203340 119950526A57547075T6 RIB BOEING727 72730C 1384009NM NR 7 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 7 SLAT SECOND RIB FROM I/B END CRACKED. INSTALLED FABRICATED FILLER AND DOUBLER IAW SRM 57-50-3. 2L73 4F A3WE 19950602002491995060200249NM 1995 6 2 UPS203341 119950526A53207075T6 WEB BOEING727 72730C 1384009NM FS 251.6-259 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION BELOW NR 2 WINDOW WEB BETWEEN STA 259 TO 251.6, LBL 42 TO 46, WL 227. REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 19950602002501995060200250NM 1995 6 2 UPS203343 119950526A53207075T6 ANGLE BOEING727 72730C 1384009NM FS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKED ANGLE AT STA 294 STR 14L. INSTALLED FABRICATED ANGLE IAW SRM 53-30-2. 2L73 4F A3WE 19950602002511995060200251NM 1995 6 2 UPS203344 119950526A5755651734742 SUPPORT BOEING727 72730C 1384009NM NR 4 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND HINGE BEARINGS, ACTUATOR SUPPORTS AND HINGE MOUNTS CORRODED, NR 4 SPOILER DAMAGED. INSTALLED NEW SPOILER IAW M/M 27-61-10. 2L73 4F A3WE 19950602002521995060200252NM 1995 6 2 UPS203345 119950526A5754 RIB BOEING727 72730C 1384009NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 5 SLAT RIB CRACKED LOCATED ON 1ST RIB OF I/B ACTUATOR ROD END. REPAIRED IAW SRM 57-50-3. 2L73 4F A3WE 19950602002531995060200253NM 1995 6 2 UPS203346 119950526A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 1141-1149 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM SEAT TRACK FLANGE AT STA 1149 TO 1141, BL 0, WL 208. REMOVED AND REPLACED IAW SRM 53-10-1. 2L73 4F A3WE 19950602002541995060200254NM 1995 6 2 UPS203347 119950526A5320 DOUBLER BOEING727 72730C 1384009NM FS 620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FRAME DOUBLER BS 620, RBL 52, WL 169. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-3. 2L73 4F A3WE 19950602002551995060200255NM 1995 6 2 UPS203348 119950526A5320 WEB BOEING727 72730C 1384009NM FS 243.7 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON AFT SIDE OF STA 243.7 WEB RBL 47, WL 212. REMOVE AND REPAIR IAW SRM 51-40-2. 2L73 4F A3WE 19950602002561995060200256NM 1995 6 2 UPS203349 119950526A5311 FRAME BOEING727 72730C 1384009NM FS 251.6 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF STA 251.6, RBL 47 TO 51, WL 219 AND WL 222. INTSTALLED FABRICATED PARTS IAW SRM 51-40-2. 2L73 4F A3WE 19950602002571995060200257NM 1995 6 2 UPS203350 119950526A5311 FRAME BOEING727 72730C 1384009NM FS 251.6 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON AFT SIDE OF STA 251.6, RBL 48 PLUS 50, WL 217 PLUS WL 225. INSTALLED FABRICATED PARTS IAW 51-40-2, 53-10-1, 51-10-6, 53-10-2. 2L73 4F A3WE 19950602002581995060200258NM 1995 6 2 UPS203351 119950526A5320 WEB BOEING727 72730C 1384009NM FS 1286 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON LT LOWER TORQUE BOX AT LIGHTNING HOLE EDGE, STA 1286, LBL 21, WL 179. INSTALLED FABRICATED PARTS IAW SRM 51-30-2, 51-10-2, 51-40-2. 2L73 4F A3WE 19950602002591995060200259NM 1995 6 2 UPS203352 119950526A5320 WEB BOEING727 72730C 1384009NM FS 1240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON LT LOWER TORQUE BOX AT LIGHTNING HOLE EDGE, STA 1240, LBL 21, WL 172. INSTALL FABRICATED PARTS IAW SRM 51-30-2, 51-10-2, 51-40-2. 2L73 4F A3WE 19950602002601995060200260NM 1995 6 2 UPS203353 119950526A53206012015 ANGLE BOEING727 72730C 1384009NM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON DELTA BEAM ATTACH ANGLE STA 740, LBL 8 TO RBL 8, WL 158. REMOVED AND REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 19950602002611995060200261NM 1995 6 2 UPS203354 119950526A53206012015 CHORD BOEING727 72730C 1384009NM FS 746 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON CHORD OF BEAM LBL 13, STA 746, WL 154. REPAIRED CHORD IAW SRM 53-10-1. 2L73 4F A3WE 19950602002621995060200262NM 1995 6 2 UPS203355 119950526A5313 STRINGER BOEING727 72730C 1384009NM FS 475-478 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STR 24R BS 475 TO 478. REMOVED CORROSION AND REPAIRED IAW SRM 53-10-2. 2L73 4F A3WE 19950602002631995060200263NM 1995 6 2 UPS203356 119950526A5311 CLIP BOEING727 72730C 1384009NM FS 970 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACK IN THE TOP HOLE IN THE STRINGER TIE CLIP, AFT SIDE OF FRAME AT BS 970, STR 28R. INSTALLED FABRICATED BRACKET IAW SRM 51-20-21, 51-30-2, 51-20-1. 2L73 4F A3WE 19950602002641995060200264NM 1995 6 2 UPS203357 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 304-344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM AT FASTENER HOLES, BS 304 TO 344, RBL 58, WL 208 UPPER AND LOWER. INSTALLED FABRICATED PARTS IAW SRM 51-40-3. 2L73 4F A3WE 19950602002651995060200265NM 1995 6 2 UPS203358 119950526A5320 WEB BOEING727 72730C 1384009NM FS 948 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKED HORIZONTAL WEB LBL 64, STA 948 WL 208. INSTALLED FABRICATED WEB IAW SRM 51-20-1, 51-30-2. 2L73 4F A3WE 19950602002661995060200266NM 1995 6 2 UPS203359 119950526A5330 SKIN BOEING727 72730C 1384009NM FS 262/268 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKS EMINATING FROM FASTENER HOLES ADJACENT TO CENTER LINE OF RT UPPER SILL ON BOTTOM ROW BS 262.5, 265, 266.5 AND 268 BETWEEN STR'S 8R AND 10R. REMOVED DAMAGE AND INSTALLED FABRICATED PARTS IAW SRM 53-30-3. 2L73 4F A3WE 19950602002671995060200267NM 1995 6 2 UPS203360 119950526A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 640-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK AROUND NUTPLATE HOLES BS 640 TO 680, RBL 25, WL 208. REPAIR IAW SRM 51-10-2, M/M 51-20-151. 2L73 4F A3WE 19950602002681995060200268NM 1995 6 2 UPS203361 119950526A5310 FRAME BOEING727 72730C 1384009NM FS 1166 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACK IN FRAME ABOVE SHEAR TIE BS 1166 BETWEEN STRINGER 29 RT AND 30 RT. REMOVED AND INSTALLED NEW FRAME IAW SRM 51-10-1, 51-20-1, 53-10-1. 2L73 4F A3WE 19950602002691995060200269NM 1995 6 2 UPS203362 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT BS 560, RBL 6, WL 199. REMOVED AND INSTALLED REPAIR SECTION IAW UPS EO NR B727-5310-7026A. 2L73 4F A3WE 19950602002701995060200270NM 1995 6 2 UPS203363 119950526A5330 SKIN BOEING727 72730C 1384009NM FS 1370.4 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION UNDER SKIN AT BS 1370.4, RBL 20, WL 255. INSTALLED FABRICATED REPAIR PARTS IAW UPS EO 95-2581, SRM 51-30-8, 51-30-2, 51-20-4, 51-10-2, M/M 51-20-02. 2L73 4F A3WE 19950602002711995060200271NM 1995 6 2 UPS203364 119950526A5720 CHORD BOEING727 72730C 1384009NM FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FLANGE OF 870, LOWER CHORD BLO TO RBL 45, WL 175. REPAIRED PER EO 727-87-1369, SRM 51-50-1, 51-10-1, 51-10-6. 2L73 4F A3WE 19950602002721995060200272NM 1995 6 2 UPS203365 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FASTENERS OF FLOORBEAM BS 312, RBL 50, WL 208. INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-10-2, M/M 51-20-151, 51-40-3, EWO 95-2552. 2L73 4F A3WE 19950602002731995060200273NM 1995 6 2 UPS203366 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 1090 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM FLOORBEAM AT STA 1090, LBL 48 TO 57, WL 208. SPLICED IN REPAIR SECTION IAW SRM 51-30-2, 51-10-2, 51-10-6, 53-10-8, M/M 51-20-151. 2L73 4F A3WE 19950602002741995060200274NM 1995 6 2 UPS203367 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT STA 640 LBL 45 TO 59. REPAIRED IAW UPS EO NR B727-5310-7014A. 2L73 4F A3WE 19950602002751995060200275NM 1995 6 2 UPS203368 119950526A53131498140132 STRINGER BOEING727 72730C 1384009NM FS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 18 LT BS 360. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 53-10-3, 51-30-2. 2L73 4F A3WE 19950602002761995060200276NM 1995 6 2 UPS203369 119950526A5313 STRINGER BOEING727 72730C 1384009NM FS 440-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 25 RT BS 440 TO 450. REMOVED DAMAGE AND INSTALL FABRICATED REPAIR PARTS IAW SRM 53-10-3. 2L73 4F A3WE 19950602002771995060200277NM 1995 6 2 UPS203370 119950526A534715201430 SEAT TRACK BOEING727 72730C 1384009NM FS 820 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BS 820 WL 208, RBL 65. REMOVED, FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-10-2, 51-30-2, 51-20-1, M/M 51-20-15. 2L73 4F A3WE 19950602002781995060200278NM 1995 6 2 UPS203371 119950526A5311 FRAME BOEING727 72730C 1384009NM FS 804 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKED FRAME O/B CHORD STA 804, WL 229, LBL 70.5 AT STRINGER 14L. INSTALLED REPAIR DOUBLER IAW SRM 51-40-3. 2L73 4F A3WE 19950602002791995060200279NM 1995 6 2 UPS203372 119950526A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF FLANGE BL0, LBL 30, WL 208 OF FLOORBEAM BS 560. INSTALLED FABRICATED PARTS IAW 51-10-1, 51-10-2, 51-30-2, 53-10-8. 2L73 4F A3WE 19950602002801995060200280NM 1995 6 2 UPS203373 119950526A534715201430 SEAT TRACK BOEING727 72730C 1384009NM FS 480-610 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP SEAT TRACK FLANGE STA 480 TO 610, LBL 45, WL 208. REPLACED IAW SRM 53-10-5, 51-10-2, 51-10-1, 51-30-2. 2L73 4F A3WE 19950602002811995060200281NM 1995 6 2 UPS203374 119950526A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 620-640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK FLANGE AROUND NUTPLATE HOLES AT STA 620 TO 640, 680 TO 710, BL 0, WL 208. INSTALLED FABRICATED PARTS IAW SRM 53-10-5, 51-10-2. 2L73 4F A3WE 19950602002821995060200282NM 1995 6 2 UPS203375 119950526A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 580-640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION AND MECHANICAL DAMAGE ON SEAT TRACK STA 580 TO 640, RBL 55, WL 208. REMOVED AND REPLACED IAW SRM 53-10-1. 2L73 4F A3WE 19950602002831995060200283NM 1995 6 2 UPS203376 119950526A551065206644 CHORD BOEING727 72730C 1384009NM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CRACKED T-CHORD ON RT HORIZ STAB. UPPER SURFACE SKIN SUPPORT CRACKED AT ATTACH POINT OF NR 1 ELEV HINGE SUPPORT RIB (ACCESS THROUGH PANEL 9213). REMOVED AND REPLACED T-CHORD IAW SRM 51-30-2, 51-30-2, 51-30-5. 2L73 4F A3WE 19950602002841995060200284NM 1995 6 2 UPS203377 119950526A575465162276 K-FLAP BOEING727 72730C 1384009NM NR 6 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION NR 6 K-FLAP ATTACH POINT. REMOVED AND REPLACED NEW K-FLAP IAW M/M 27-81-0. 2L73 4F A3WE 19950602002851995060200285NM 1995 6 2 UPS203378 119950526A5754 FLAP TRACK BOEING727 72730C 1384009NM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION EMITTING FROM THE NR 6 FLAP TRACK AFT ATTACH BOLTS. INSTALLED NEW FABRICATED PARTS, REPLACED FLAP TRACK IAW OHM 57-40-01, 20-50-1, SRM 51-10-2, M/M 27-51-31, 27-52-2. 2L73 4F A3WE 19950602002861995060200286NM 1995 6 2 UPS203379 119950526A5751652177614 FITTING BOEING727 72730C 1384009NM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON RIGHT WING O/B AILERON LOCKOUT FITTING. INSTALLED NEW FITTING IAW SRM 51-30-2, M/M 27-10-131. 2L73 4F A3WE 19950602002871995060200287NM 1995 6 2 UPS203380 119950526A575365216329 SUPPORT BOEING727 72730C 1384009NM TE MID FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND LEFT WING I/B MID FLAP CARRIAGE THRUST BEARING SUPPORT PITTED. MID FLAP REPLACED IAW EO B727-5750-5879-A. 2L73 4F A3WE 19950602002881995060200288NM 1995 6 2 UPS203381 119950526A5753652163210 FITTING BOEING727 72730C 1384009NM RT TE MID FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND RT I/B MID FLAP O/B THRUST BEARING FITTING IS CORRODED. MID FLAP ASSY OVERHAULED IAW OHM 57-52-01, UPS EO B727-5750-5879-A. 2L73 4F A3WE 19950602002891995060200289NM 1995 6 2 UPS203382 119950526A575565173448 PANEL BOEING727 72730C 1384009NM NR 14 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 14 SPOILER PANEL DELAMINATED AT MIDDLE OF L/E. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950602002901995060200290NM 1995 6 2 UPS203383 119950526A57546529618 FITTING BOEING727 72730C 1384009NM NR 8 TE SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION IN BORE OF TRACK ATTCH RIB FITTINGS O/B AND I/B OF NR 8 SLAT. INSTALLED NEW FITTINGS IAW SRM 51-30-02. 2L73 4F A3WE 19950602002911995060200291NM 1995 6 2 UPS203384 119950526A575465296167 FITTINGS BOEING727 72730C 1384009NM NR 3 LE SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION IN BORE OF TRACK ATTCH RIB FITTINGS O/B AND I/B OF NR 3 SLAT. INSTALLED NEW FITTINGS IAW SRM 51-30-02. 2L73 4F A3WE 19950602002921995060200292NM 1995 6 2 UPS203385 119950526A534765246216 SEAT TRACK BOEING727 72730C 1384009NM FS 848-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP OF SEAT TRACK FLANGE STA 848 TO 870, LBL 45, WL 208. INSTALLED NEW TRACK IAW SRM 51-10-1. 2L73 4F A3WE 19950602002931995060200293NM 1995 6 2 UPS203386 119950526A534715201432 SEAT TRACK BOEING727 72730C 1384009NM FS 1030 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK FLANGE AROUND NUTPLATE HOLES. STA 1030, LBL 25, WL 208. INSTALLED NEW TRACK IAW SRM 51-30-2, 53-10-5. 2L73 4F A3WE 19950602002941995060200294NM 1995 6 2 UPS203390 119950526A5755651734748 PANEL BOEING727 72730C 1384009NM NR 12 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 12 O/B SPOILER PANEL IS DELAMINATING. REMOVED AND REPLACED SPOILER IAW M/M 27-61-01. 2L73 4F A3WE 19950602002951995060200295NM 1995 6 2 UPS203391 119950526A5754 BULL NOSE BOEING727 72730C 1384009NM NR 4 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919 19012 WHILE IN SI CHECK, MAINTENANCE FOUND ATTACH POINTS BONDING JUMPERS ON NR 4 K-FLAP AND BULL NOSE OUTER LOWER SIDE HAS CORROSION. REPAIRED K-FLAP IAW 727-57-1370. 2L73 4F A3WE 19950602002961995060200296CE 1995 6 2 95ZZZW723 119950508A5210002430000205 STOP BEECH 36 A36 1151604CE CABIN DOOR WORN ON END A ECBAK NONE O OTHER ININSP/MAINT 1 GL094182S E668 PILOT REPORTED THAT THE CABIN ENTRANCE DOOR STOP WAS MISSING OR BROKEN. INVESTIGATION REVEALED THAT THE STOP HAD BECOME DISENGAGED FROM THE DOOR FRAME. THE AIRCRAFT HAS A HIGH NUMBER OF FLIGHT HOURS, AND THE STOP AND CHANNEL HAD BECOME WORN TO THE POINT THAT THEY SEPARATED. REPLACED STOP, AND REWORKED THE DOOR FRAME AREA TO ALLOW FOR PROPER ENGAGEMENT. SUGGEST PERIODIC REPLACEMENT OF THE DOOR STOP TO PRECLUDE SEPARATION DUE TO WEAR. 1L71 3O 3A15 19950602002971995060200297WP 1995 6 2 95ZZZW724 219950504A726131021231 TUBE ASSY SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENG OIL CRACKED A CHQAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 EA2327330 AC756 P44510 PILOT SHUT DOWN RIGHT ENGINE DUE TO LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE GAUGE INDICATED 50 PSI. UPON TROUBLE SHOOTING THE PROBLEM, THE OIL SCAVENGE TUBE ASSY WAS FOUND CRACKED. THE TUBE ASSY WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL AND NO LEAKS NOTED. (W) 1L72 4T4 T A8SW E4WE 19950602002981995060200298NM 1995 6 2 95ZZZW725 119950504A27521176T1001 MOTOR BOEING747 747124 1384874NM INBOARD T/E FLAPFAILED A P5CAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23855FT 19733 EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYDRAULIC RETURN LINE UNION IN WIG TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W) 2L74 4F A20WE 19950602002991995060200299NM 1995 6 2 95ZZZW726 119950504A2910 B-NUT BOEING747 747124 1384874NM NR 1 HYD LOOSE A P5CAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23855FT 19733 EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYD RETURN LINE UNION IN WING TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON REF IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W) 2L74 4F A20WE 19950602003001995060200300NM 1995 6 2 95ZZZW727 119950504A32971176T1001 WIRE BOEING747 747124 1384874NM GEAR EXT FAULTY A P5CAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 WP23855FT 19733 EN ROUTE TO ORD, AIRCRAFT EXPERIENCED LOSS OF NR 1 SYSTEM HYDRAULIC QUANTITY. ON APPROACH TRIED TO LOWER FLAPS AND GEAR USING ALTERNATE SYSTEM. RT BODY GEARS WOULD NOT LOWER AND INBOARD FLAPS WOULD NOT EXTEND. REVERTED TO HYDRAULIC MODE. OPERATION OF GEAR AND FLAPS WAS NORMAL. ON POST FLIGHT INSPECTION, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 PYLON. OPERATION CHECK OF ALTERNATE FLAP FOUND ELECTRIC DRIVE MOTOR FAILED. CHECK OF ALTERNATE GEAR EXTENSION SYSTEM INDICATES WIRING PROBLEM. SECURED B-NUT ON HYD RETURN LINE UNION IN WING TO UPPER PYLON DISC BOX. TIGHTENED B-NUT AT CHECK VALVE IN PYLON RED IPC 29-11-03-01 FIG 335. LEAK CHECK OK. (W) 2L74 4F A20WE 19950602003011995060200301NE 1995 6 2 95ZZZW728 219950428A7250 BLADES BOEING747 747124 1384874NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE FAILURE A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING EXJVIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 WP23855FT 19733 663048 EN ROUTE SYD TO HKG, WHILE RETARDING ENGINES IN CRUISE, NR 4 ENGINE FLAMED OUT, COULD NOT RESTART UNTIL DESCENT TO FL 210. IN KHG, INSPECTED ENGINE PER MM 71-00-00, NO DAMAGE FOUND, AIRCRAFT DISPATCHED. ON CLIMB-OUT FROM HKG, AT FL 164, NR 4 ENGINE STALLED, EGT WENT TO 960 DEGREES WITH VIBRATION. ENGINE SHUT DOWN USING ALTERNATE PROCEDURES. AIRCRAFT RETURNED TO HKG. POST FLIGHT INSPECTION REVEALED METAL IN TAIL PIPE. ENGINE CHANGE CALLED. ADDITIONAL INFORMATION WILL BE SENT WHEN AVAILABLE. AFTER ENGINE CHANGE, AIRCRAFT RELEASED FOR SERVICE. 2L74 4F4 F A20WE E20EA 19950602003021995060200302NM 1995 6 2 95ZZZW729 119950501A5753 FOREFLAP BOEING747 747124 1384874NM LT INBD FOREFLAPDELAMINATION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 LEFT INBOARD FOREFLAP, LEADING EDGE OF OUTBOARD SECTION HAS OVERLAY MISSING FROM PREVIOUS REPAIR AND HAS APPROXIMATELY 4 DELAMINATION. REMOVED FOREFLAP LEADING EDGE. REPAIRS ACCOMPLISHED PER SRM 51-40-09. REINSTALLED LEADING EDGE OF FOREFLAP. AIRCRAFT RELEASED FOR SERVICE. (W) 2L74 4F A20WE 19950602003031995060200303NM 1995 6 2 95ZZZW730 119950501A5730 PANEL BOEING747 747124 1384874NM LT WING L/E FLAPDELAMINATION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 TOP LEFT WING, PREVIOUS REPAIR OF HONEYCOMB UPPER SKIN ABOVE NR 6 LEADING EDGE FLAP COMING APART, MARKED. REMOVED OLD REPAIR, POTTED CORE AND OVERLAYED AREA. REPAIR ACCOMPLISHED PER SRM 51-40-09. AIRCRAFT RELEASED FOR SERVICE. (W) 2L74 4F A20WE 19950602003041995060200304NM 1995 6 2 95ZZZW731 119950501A5730 PANEL BOEING747 747124 1384874NM LT WING SPOILER CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 TOP LEFT WING, FIBERGLASS PANEL FWD OF NR 6 SPOILER LEADING EDGE IS CRACKED MARKED. SANDED AREA, CLEANED AND REPAIRED PE SRM 51-40-09. AIRCRAFT RELEASED FOR SERVICE. (W) 2L74 4F A20WE 19950602003051995060200305CE 1995 6 2 95ZZZW732 119950508A3230 BREAKER BEECH 1900 1900C 1154161CE MLG TRIPPED A GUUAO OTHER O OTHER CLCLIMB 1 SO19198GA UB5 FLT 487A - MCO-MIA - LANDING GEAR CIRCUIT BREAKER POPPED ON RETRACT OUT OF MCO. TROUBLE SHOT SYSTEM WIRING. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD, COULD NOT DUPLICATE. 2L72 4T RTA24CE 19950602003061995060200306CE 1995 6 2 95ZZZW733 119950505A3230993641571 RELAY BEECH 99 C99 1154006CE TIME DELAY MALFUNCTION A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19232BH U232 FLT 416A - MIA-DAB - GEAR UNSAFE LIGHT REMAINS ON. REMOVED AND REPLACED TIME DELAY RELAY ASSEMBLY SWING GEAR ON JACKS. OPS CHECK GOOD. RELEASED TO SERVICE. 1L72 3T A14CE 19950602003071995060200307NM 1995 6 2 95ZZZW734 119950511A2820 CROSSFEED VALVE BOEING747 747131 1384881NM NR 2 MALFUNCTIONED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0593108 19674 CDG - DURING SECOND SEGMENT CLIMB, WHEN CROSSFEED FROM NR 2 AND NR 3 MAIN FUEL TANKS WAS INITIATED, NR 1 ENGINE SPUN DOWN. TURN ON ALL BOOST PUMPS. ENGINE RESTART WAS NORMAL. NR 2 CROSSFEED VALVE HAD BEEN PREVIOUSLY PLACARDED PER MEDP. USED ALTERNATE CROSSFEED PROCEDURES. OPERATION WAS NORMAL. 2L74 4F A20WE 19950602003081995060200308WP 1995 6 2 95ZZZW735 119950511A79328DJ130KWA1 CONNECTOR DOUG DC9 DC982 3022082WP CTR INSTR PANEL SHORTED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE05906TW 49160 STL - DURING LANDING, SMOKE AND ELECTRICAL ODOR EMITTED FROM CENTER INSTRUMENT PANEL. FOUND LEFT ENGINE OIL QUANTITY INDICATOR CONNECTOR SHORTED, MFG P/N 8DJ130KWA1. REPLACED OIL QUANTITY INDICATOR AND OPERATION CHECKED NORMAL. 2L72 4F A6WE 19950602003091995060200309 1995 6 2 95ZZZW736 419950508A25657A127512 VALVE DOUG DC9 DC982 3022082WP SLIDE FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05918TW 49367 MCI - DURING SHOP TEST, FOUND EVACUATION SLIDE, MFG P/N 7A127512, WOULD NOT MAINTAIN AIR PRESSURE. FOUND ASPIRATOR VALVE NOT PROPERLY CLOSING. REPAIRED ASPIRATOR VALVE. RETEST OF EVACUATION SLIDE OPERATION CHECKED NORMAL. (W) 2L72 4F A6WE 19950602003101995060200310WP 1995 6 2 95ZZZW737 119950420A5400 ANGLE DOUG DC9 DC932 3022066WP FS 978 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05923L 47109 STL - DURING C-CHECK, FOUND .375 INCH CRACK AT TOP PYLON ATTACH ANGLE, STATION 978, LEFT PYLON. REPAIRED PER SRM 54-04, FIGURE 10, SHEET 2. 2L72 4F A6WE 19950602003111995060200311WP 1995 6 2 95ZZZW738 119950424A5320 DOUBLER DOUG DC9 DC951 3022051WP FS 1167 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05409EA 47728 STL - DURING SPECIAL CHECK, FOUND ONE .1875 INCH CRACK IN -85 LOWER LEFT CORNER, STATION 1167. STOP DRILLED CRACK AND REPAIRED PER SERVICE BULLETIN 137 AND EMLR 65694. (W) 2L72 4F A6WE 19950602003121995060200312WP 1995 6 2 95ZZZW739 119950417A5313 LONGERON DOUG DC9 DC915 3022036WP FS 218 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05969Z 47001 DURING SPECIAL CHECK, FOUND A TWO INCH CRACK IN LONGERON 19L, STATION 218. REPAIRED PER SRM 53-02. 2L72 4F A6WE 19950602003131995060200313WP 1995 6 2 95ZZZW740 119950502A5320 FITTING DOUG DC9 DC931 3022065WP LEFT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05980Z 47344 STL - DURING OP-15, FOUND 12 INCH CRACK IN LEFT PORK CHOP FITTING HORIZONTAL LEG. REPLACED LEFT PORK CHOP FITTING PER DOUGLAS MM 20-10, 20-14, 20-16 AND PER TWA STANDARD PRACTICES. (W) 2L72 4F A6WE 19950602003141995060200314WP 1995 6 2 95ZZZW741 119950504A5330 SKIN DOUG DC9 DC931 3022065WP FS 985 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05987Z 47137 STL - DURING C-CHECK, FOUND FUSELAGE SKIN BULGE AT STATION 985, LONGERON 24R. REMOVED LONGERON, CLEANED AREA, REPLACED LONGERON SERCTION AND END CAP PER SRM 53-02, FIGURE 4. (W) 2L72 4F A6WE 19950602003151995060200315NM 1995 6 2 AWXA9500267 119950508A5320 ANGLE BOEING757 7572G7 1384963NM BS 660 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - DURING C6 INSPECTION, FOUND FLOOR BEAM TO INTERCOSTAL VERTICAL ANGLE CRACKED, BS 660. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-10-00 AND SRM 51-40-02. (W) 2L72 4F RTA2NM 19950602003161995060200316NM 1995 6 2 AWXA9500268 119950508A5315 FLOORBEAM BOEING757 7572G7 1384963NM BS 364 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - DURING C6 INSPECTION, FOUND UPPER CAP OF FLOORBEAM AT STATION 364 RBL 23 AND RBL 60 CORRODED BEYOND CLEAN UPLIMITS. REPAIRED PER ER 5-53-12-03. (W) 2L72 4F RTA2NM 19950602003171995060200317NM 1995 6 2 AWXA9500270 119950508A5320 THRESHOLD BOEING757 7572G7 1384963NM L4 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - DURING C6 INSPECTION, FOUND L4 DOOR FORWARD THRESHOLD PLATE CRACKED. REMOVED WELD REPAIR AND INSTALLED PER ER 5-53-30-02B. (W) 2L72 4F RTA2NM 19950602003181995060200318NM 1995 6 2 AWXA9500289 119950512A555265C2577318 HINGE BRACKET BOEING737 73733A 1384673NM LT ELEV TRIM WORN A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28166AW 23627 IND-CMH - FLT 280 - CREW REPORTED AIRFRAME VIBRATION AT HIGH SPEED. AIRCRAFT LANDED IN CMH WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND LEFT ELEVATOR TRIM TAB ATTACH BEARINGS WORN. REMOVED AND REPLACED LT TAB NR 1 HINGE BRACKET AND HARDWARE, AND REINSTALLED PER BMM 27-31-31. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950602003191995060200319WP 1995 6 2 GRAA9532 119950403A3350110049 EEL PWR SUPPLY DOUG DC9 DC987 3022087WP CABIN FAILED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111075T 49724 DURING C-CHECK, MAINTNENANCE FOUND THE AFT FLOOR TRACK LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY POWER SUPPLY, OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4F RTA6WE 19950602003201995060200320WP 1995 6 2 HAL94045 119950420A5320352518121 FITTING DOUG DC9 DC951 3022051WP FS 775 LBL 45 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 27420 47796 DURING C-CHECK, FOUND FLOOR SUPPORT CRACKED AT UPPER SURFACE OF THE CENTER WING SECTION STAION 775 LBL 45 OUTBOARD SIDE. INSTALLED A NEW FITTING PER SRM 51-30-2. (W) 2L72 4F A6WE 19950602003211995060200321NM 1995 6 2 MZZA95029 119950502A2410 CSD BOEING727 727227 1384078NM NR 2 GEN MALFUNCTION A MZZAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 WP1386426 21364 FLT NR 954 - ROR - WITH NR 1 ENGINE GENERATOR ALREADY ON MEL DEFERAL, AFTER AIRCRAFT DEPARTURE OUT OF ROR, NR 2 GENERATOR TRIPPED AND UNABLE TO RESET, PERFORMED APPROPRIATE ABNORMAL CHECKLIST. AIRCRAFT DIVERTED BACK TO ROR. MAINTENANCE TROUBLESHOT AND FOUND NR 2 GENERATOR CONTROL PANEL WAS AT FAULT. DUE TO PARTS NOT AVAILABLE, SWAPPED NR 1 GCU WITH NR 2 GCU MFG P/N 902F242-5 S/N ON NR 1 5742, ON NR 2 2966. ALL SYSTEMS CHECKS GOOD AND AIRCRAFT RETURN BACK IN SERVICE. AFTER ARRIVAL GUAM, MAINTENANCE REPLACED NR 1 GENERATOR CSD ASSY MFG P/N 700842A S/N OFF 0880 ON 9236. PRECAUTIONARY REPLACED NR 2 GENERATOR ASSY, MFG P/N 976J498-1 S/N OFF 7566 ON 6168. ALL SYSTEM CHECKS GOOD. (W) 2L73 4F A3WE 19950602003221995060200322NE 1995 6 2 PLGA414951 219950414A7250 BLADES SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE TURBINE SECTION FAILED A PLGACD ABORTED TAKEOFF RETURN TO BLOCK YJ ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 NE05744BA 340A105 367268 FLT 4864 - BOS-BDL - EXPERIENCED AN ENGINE FAILURE DURING TAKEOFF ROLL. AS POWER APPROACHED 80 PERCENT TORQUE, ITT ROSE TO 920 DEGREES CELSIUS AND 4TH STAGE TURBINE BLADES SEPARATED FROM THE TURBINE WHEEL. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE ENGINE IAW THE SAAB MM. ALL GROUND RUNS CHECKED GOOD AND THE AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T4 TRTA52EU E8NE6 19950602003231995060200323EU 1995 6 2 SIMA950951 119950405A532053171122200 FRAME AEROSPATR42 ATR42300 8680920EU CABIN WINDOW CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21423MQ 030 SAT - DURING A 24,000 CYCLE INSPECTION, DISCOVERED BY EDDY CURRENT INSPECTION A .19 INCH CRACK ON THE NODE 5 LEFT SIDE OF WINDOW FRAME VERTICAL FLANGE. BLENDING WAS ACCOMPLISHED IAW ATR DRAWINGS 11S531RO125, ATTACHED. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602003241995060200324EU 1995 6 2 SIMA950952 119950405A532053171122201 FRAME AEROSPATR42 ATR42300 8680920EU CABIN WINDOW CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21423MQ 030 SAT - DURING A 24,000 CYCLE INSPECTION, DISCOVERED BY EDDY CURRENT INSPECTION A .29 INCH CRACK ON THE NOSE 5 WINDOW FRAME RIGHT SIDE OF VERTICAL FLANGE. BLENDING WAS ACCOMPLISHED IAW ATR DRAWINGS 11S531RO125, ATTACHED. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602003251995060200325EU 1995 6 2 SIMA951331 119950513A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU CABIN DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21223AT2628 547 223 RFD - DURING PS-2 CHECK, MAINTENANCE FOUND THE PASSENGER/CREW AIRSTAIRS EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. EMERGENCY LIGHT SYSTEM OPERATIONALLY CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602003261995060200326EU 1995 6 2 SIMA951332 119950513A3230E0217XUU001A RELAY AEROSPATR42 ATR42300 8680920EU LANDING GEAR FAILED A SIMAO OTHER J WARNING INDICATION LDLANDING 1 SW21223AT 223 MLI - FLT 4185 - DURING DESCENT MLG WOULD NOT EXTEND BY NORMAL MEANS. CREW USED EMERGENCY EXTENSION AND LANDED WITHOUT INCIDENT. THE LANDING GEAR WAS DEFERRED PER MEL 32-03 AND FLOWN TO ORD. INSPECTION REVEALED THE DOWN RELAY 14GA BAD. THE RELAY WAS REPLACED AND OPERATIONAL CHECK REVEALED NO FAULTS. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602003271995060200327EU 1995 6 2 SIMA951341 119950514A33503012000 EEL BALLAST AEROSPATR72 ATR72212 EU CABIN FAILED A SIMAK NONE L NO TEST CRCRUISE 1 SW21349AT 4976 408 349 FLT 4207 - IN CRUISE THE BACK HALF OF THE EMERGENCY FLOOR LIGHTING SYSTEM ILLUMINATED. AIRCRAFT CONTINUED TO DESTINATION WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A BALLAST CONVERTER. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602003281995060200328NE 1995 6 2 SIMA951352 219950515A73218108001002 EEC AEROSPATR72 ATR72202 8680940EU PWA PW120 PW127 NE NR 2 ENGINE MALFUNCTIONED A SIMAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW21244AT3346 92100424 244 127003 GRB - FLT 4026 - NR 2 ENGINE TQ SURGES 30 PERCENT ON TAKEOFF. REMOVED AND INSPECTED NR 2 EEC, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950602003301995060200330NM 1995 6 2 95ZZZZ231 119950421A21317638102 CONTROLLER BOEING737 7372B7 1384560NM PRESS SYS FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19272AU 22884 PIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB. AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE. UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. REF USAA950402. 2L72 4F A16WE 19950602003311995060200331NM 1995 6 2 95ZZZZ232 119950421A2130 CONTROL PANEL BOEING737 7372B7 1384560NM PRESS SYS FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19272AU 22884 PIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B. REPLACED OVERHEAD CONTROL PANEL. ALL CHECKS NORMAL. REF USAA950403. 2L72 4F A16WE 19950602003321995060200332NM 1995 6 2 95ZZZZ233 119950423A2150 VALVE BOEING737 7374B7 1384702NM LT PACK INOP A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19447US 24874 PBI - FLT 188 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO PBI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DUCT CLAMP AND SEAL LOOSE ON AFT SIDE OF AFT PRESSURE BULKHEAD. REINSTALLED CLAMP AND SEAL. FOUND PACK VALVE ON LEFT PACK NOT OPENING. REPLACED LEFT PACK VALVE. REF USAA950404. 2L72 4F RTA16WE 19950602003331995060200333WP 1995 6 2 95ZZZZ234 119950504A3231510361 ROD ASSY DOUG DC8 DC8F54 3021926WP NLG DOOR UNLOCKED A FXLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19426FB 45667 AFTER TAKEOFF MIAMI FELT SEVERE VIBRATION. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RT NOSE LANDING GEAR DOOR OPEN. CLEANED, LUBED AND RESET RT FWD DOOR ROD AND OPS CHECKED OK. PERFORMED OVERWEIGHT LANDING INSPECTION. RETURNED ACFT TO SERVICE. 2L74 4F 4A25 19950602003341995060200334WP 1995 6 2 95ZZZZ235 119950505A2612244F70G36 SENSOR DOUG DC8 DC851 3021920WP NR 2 ENG DENTED A FXLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19507DC 45855 AFTER TAKEOFF FROM MIAMI, RECEIVED FIRE WARNING ON NR 2 ENGINE. RETURNED TO MIAMI AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A DENTED SENSOR ON RT AFT COWL. REPLACED SENSOR, SYSTEM OPS CHECKED OK. RETURNED ACFT TO SERVICE. 2L74 4F 4A25 19950602003351995060200335WP 1995 6 2 95ZZZZ236 119950504A2612 WIRE DOUG DC8 DC851 3021920WP N 2 ENG LOOSE A FXLAO OTHER N FALSE WARNING APAPPROACH 1 SO19507DC 45855 ON DESCENT TO MIAMI, RECEIVED FIRE WARNING ON NR 2 ENGINE, REDUCED POWER AND FIRE WARNING CEASED. LANDED MIAMI WITHOUT INCIDENT. REPAIRED BROKEN WIRE ON RT FWD DOOR CANNON PLUG. SYSTEM CHECKED OK, RETURNED ACFT TO SERVICE. 2L74 4F 4A25 19950602003361995060200336SW 1995 6 2 BDHA9500010 119950408A24001401AA22S WIRE SWRNGNSA226 SA226TC 8780404SW LT FUEL PRESS CHAFED A BDHAO OTHER J WARNING INDICATION APAPPROACH 1 GL15229AM TC305 RAP - FLT 475 - LEFT ENGINE FUEL PRESSURE CIRCUIT BREAKER POPPED IN FLIGHT. REMOVED AND REPLACED 1 AMP CIRCUIT BREAKER AND INSPECTED WIRING. REPAIRED WIRE NR 1401AA-22S FOR CHAFING AT GENERATOR RELAY AREA. GROUND RUN FOR CHECK OF SYSTEM CHECKED OKAY. ACFT RELEASED FOR FLIGHT. (Z) 2L72 4T RTA8SW 19950602003371995060200337SW 1995 6 2 BDHA9500011 119950414A29102781006309 TUBE ASSY SWRNGNSA226 SA226TC 8780404SW RT NACELLE CHAFED A BDHAK NONE K FLUID LOSS ININSP/MAINT 1 GL15328BA TC253 MOT - FLT 421 - UPON PREFLIGHT, THE CREW DISCOVERED THE RT NACELLE WAS LEAKING HYDRAULIC FLUID. INSPECTION REVEALED A CHAFED HYDRAULIC RETURN LINE IN THE RT NACELLE WALL. HYDRAULIC LINE WAS REPLACED AND LEAK CHECK PERFORMED. ACFT RELEASED FOR SERVICE. (Z) 1L72 4T A8SW 19950602003381995060200338WP 1995 6 2 CAL950343 119950424A2612AUL71221 FIRE LOOP DOUG DC10 DC1030 3023501WP FWD PYLON DAMAGED A CALAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 SW0912061 47851 EWR - FLT 56 - AFTER TAKEOFF. NR 3 ENGINE 'A' FIRE LIGHT AND BELL CAME ON. DUMPED FUEL AND RETURNED TO EWR. FOUND FWD PYLON DETECTION ASSY DAMAGED. REF MM 26-15-01 ITEM 117, REPLACED PART AUL7122-1 OPS. CHECK SYSTEM, ALL NORMAL. (Z) 2L73 4F A22WE 19950602003391995060200339NM 1995 6 2 CAL950352 119950405A5311658005120 FRAME BOEING737 7373T0 1384582NM NLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091232214185 23373 EWR - FLT 1827 - MAINTENANCE FOUND NLG TRUNNION LOOSE, FURTHER INSPECTION FOUND NLG 'A' FRAME CRACKED. REMOVED AND REPLACED UPPER NLG DRAG BRACE PN NR 65-80051-20. (Z) 2L72 4F RTA16WE 19950602003401995060200340NM 1995 6 2 CAL950365 119950502A5313 STRINGER BOEING727 727224 1384076NM FS 500-520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND, CRACKS AND CORROSION IN STRINGER 20R AT STA 500 TO 520. THE CRACKS WERE .125 INCH TO .25 INCH IN LENGTH. THE DAMAGED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (Z) 2L73 4F A3WE 19950602003411995060200341NM 1995 6 2 CAL950366 119950502A5320 INTERCOSTAL BOEING727 727224 1384076NM BS 890 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096673460271 20663 GSO - INSPECTION FOUND THE LT MAIN LANDING GEAR BAY INTERCOSTAL AT BS 890 CRACKED AND CORRODED. THE CRACK WAS .75 INCH LONG. THE DAMAGED AREA OF INTERCOSTAL WAS CUT OUT. REPAIR FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-3. (Z) 2L73 4F A3WE 19950602003421995060200342EA 1995 6 2 PLGA413951 219950413A7250310076701 SUNGEAR BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE SHEARED A APLGAECD ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NE05810BE UB48 PCE32063 PVD - ON TAKEOFF ROLL, THE LT ENGINE EXPERIENCED A LOSS OF POWER AND OIL PRESSURE. THE TAKEOFF WAS ABORTED, ENGINE WAS SHUTDOWN AND ACFT RETURNED TO GATE. INITIAL ON SITE INVESTIGATION REVEALED LOSS OF POWER TURBINE BLADES, PUNCTURED EXHAUST DUCTS AND DEBRIS IN EXHAUST AREA. INSPECTION OF MAIN ENGINE OIL FILTER REVEALED HEAVY METAL PARTICLE CONTAMINATION. COMPLETE ENGINE CHANGE OUT WAS ACCOMPLISHED ON SITE, WITH FAILED ENGINE AND PROPELLER RETURNED TO PSM. ENGINE TO BE DIRECTED TO O/H FACILITY FOR FURTHER INVESTIGATION. S/D - THE POWERPLANT REFERENCE ABOVE EXPERIENCED A POWER SECTION FAILURE OF THE SUNGEAR. (Z) 2L72 4T4 TRTA24CE E4EA 19950602003431995060200343NM 1995 6 2 USAA950402 119950421A21337110033 OUTFLOW VALVE BOEING737 7372B7 1384560NM PRESS SYS FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19272AU 22884 PIT - FLT 19 - AFTER TAKEOFF, AC CABIN PRESSURIZATION BEGAN TO CLIMB. AUTO CABIN PRESSURE SYSTEM WAS ON MEL, ACFT WAS IN STANDBY MODE. UNABLE TO CONTROL PRESSURIZATION IN STANDBY AC AND DC MODE. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER. REF 95ZZZZ231. 2L72 4F A16WE 19950602003441995060200344NM 1995 6 2 USAA950403 119950421A2130 CIRCUIT BREAKER BOEING737 7372B7 1384560NM PRESS SYS TRIPPED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19272AU 22884 PIT - FLT 19 - UNABLE TO CONTROL PRESSURIZATION AFTER TAKEOFF. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MANUAL DC CIRCUIT BREAKER POPPED, RESET C/B. REPLACED OVERHEAD CONTROL PANEL. ALL CHECKS NORMAL. REF 95ZZZZ232. 2L72 4F A16WE 19950602003451995060200345NM 1995 6 2 USAA950404 119950423A21203964981 CLAMP BOEING737 7374B7 1384702NM BULKHEAD LOOSE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19447US 24874 PBI - FLT 188 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO PBI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DUCT CLAMP AND SEAL LOOSE ON AFT SIDE OF AFT PRESSURE BULKHEAD. REINSTALLED CLAMP AND SEAL. FOUND PACK VALVE ON LEFT PACK NOT OPENING. REPLACED LEFT PACK VALVE. REF 95ZZZZ233. 2L72 4F RTA16WE 19950602003461995060200346NM 1995 6 2 USAA950405 119950423A3350 EEL SIGN BOEING737 737301 1384611NM CABIN MISSING A USAAK NONE L NO TEST ININSP/MAINT 1 EA19354US 23557 CLT - LOW LEVEL EMERGENCY EXIT SIGN MISSING, ROW 10AC. MAINTENANCE REPLACED EXIT SIGN. (Z) 2L72 4F RTA16WE 19950602003471995060200347 1995 6 2 USAA950406 419950423A3417693732551 ADC BOEING737 7373B7 1384580NM E/E BAY FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19534AU 24516 CLT - FLT 1157 - CAPTAIN'S FLIGHT INSTRUMENTS, AIRSPEED, ALTIMETER FAILED AND GPWS WARNING CAME ON. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ADC. OPS CHECK OK. PERFORMED OVERWEIGHT LANDING INSPECTION, CHECKS OK. (Z) 2L72 4F RTA16WE 19950602003481995060200348WP 1995 6 2 USAA950407 119950423A3350 EEL DIODES DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19937VJ 48117 PIT - FORWARD SECTION OF FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPLACED BOTH DIODES IN EMERGENCY CABIN FLOOR LIGHTING SYSTEM. (Z) 2L72 4F A6WE 19950602003491995060200349EU 1995 6 2 USAA950408 119950423A3233125757 ACTUATORS FOKKERF28 F28MK0100 4990807EU RT MLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19859US 11293 SRQ-TPA - FLT 2030 - ON TAKEOFF CREW RECEIVED RIGHT LANDING ALERT AFTER GEAR UP SELECTION, GEAR INDICATIONS NORMAL. RECYCLED GEAR SEVERAL TIMES AND DIVERTED FLIGHT TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH MAIN LANDING GEAR DOOR UPLOCK ACTUATORS ON THE RIGHT HAND MAIN LANDING GEAR. OPS CHECK OK. (Z) 2L72 4F RT 19950602003501995060200350EU 1995 6 2 USAA950409 119950425A28209507445 FUEL VENT VALVE FOKKERF28 F28MK0100 4990807EU LT WING FAILED A USAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 EA19856US 11286 DCA - FLT 200 - ON TAKEOFF, TOWER ADVISED FLIGHT THAT FUEL WAS BEING SIPHONED OUT OF WING. FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED LT O/B FUEL VENT VALVE. NO LEAKS NOTED. (Z) 2L72 4F RT 19950602003511995060200351NM 1995 6 2 USAA950410 119950426A801297907821 START VALVE BOEING737 737201 1384454NM NR 1 ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19254AU 22796 GSO - FLT 2243 - FLIGHT EN ROUTE TPA TO BWI WHEN NR 1 START VALVE OPEN LIGHT CAME ON. CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TO GSO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED START VALVE ASSEMBLY AND START VALVE SWITCH. RAN NR 1 ENGINE, LEAK AND OPS CHECK NORMAL. (Z) 2L72 4F A16WE 19950602003521995060200352EU 1995 6 2 USAA950411 119950426A3350FCA410319 EEL RELAY FOKKERF28 F28MK0100 4990807EU CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19864US 11306 PIT - FOUR OVERWING EXIT LIGHTS AND OVERHEAD EXIT LIGHTS DO NOT ILLUMINATE WITH GEAR DOWN. MAINTENANCE REPLACED RELAY K2618-A, CHECK NORMAL. (Z) 2L72 4F RT 19950602003531995060200353 1995 6 2 9508636637 419950527A34417883450041 INS BOEING747 747251B 1384892NM E/E COMPARTMENT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01637US22107 23548 DURING CRUISE, THE NR 1 AND NR 2 INS RED WARNING LIGHT ILLUMINATED CONSECUTIVELY. CREW FOLLOWED COCKPIT OPERATING MANUAL AND DIVERTED FLIGHT TO ANC. MAINTENANCE REPLACED THE NR 1 INS AND PERFORMED CHECK, CHECK WAS NORMAL. THE NR 1 INS RED WARNING LIGHT ILLUMINATED. THE NR 2 INS DID NOT HAVE A PROBLEM. THE FLIGHT DIVERTED TO ANC, BECAUSE THE FLIGHT COULD NOT USE RUSSIAN AIRSPACE. 2L74 4F A20WE 19950602003541995060200354EU 1995 6 2 9508643218 119950525A2710 COMPUTERS AIRBUS320 A320211 3930320EU AILERON FAILED A NWAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL01318US 206 DURING CLIMBOUT FROM ORD, AIRCRAFT EXPERIENCED APPROXIMATELY 45 SECONDS OF APPROXIMATELY 10 VERY SMALL QUICK AILERON MOVEMENTS ACCOMPANIED BY ELEC 1 FAULT. DURING APPROACH INTO MEM AIRCRAFT EXPERIENCED ONE AILERON JERK. AIRCRAFT LANDED WITHOUT INCIDENT IN MEM WHERE MAINTENANCE REPLACED THE NR 1 AND NR 2 ELEVATOR AILERON COMPUTERS AND THE PILOT AND COPILOT SIDE STICK CONTROLLERS. THE DIGITAL FLIGHT DATA RECORDER WAS REMOVED FOR ANALYSIS. ALL OPERATIONAL CHECKS OK. A/C TT 13454 CHANGED TO 13464. 2L72 4F RTA28NM 19950602003551995060200355NE 1995 6 2 9508659950 219950529A7230 COMPRESSOR DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE NR 1 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL019346 47376 COMPRESSOR STALLS OCCURRED ON POWER APPLICATION FOR TAKEOFF (ENGINE POSITION UNDETERMINED). TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. BOTH ENGINES WERE INSPECTED AND RUN-UP. STALLS COULD NOT BE DUPLICATED. THE SYSTEMS CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. CORRECTION: NR 1 ENGINE CSEHM 373 CHANGED TO CSEHM 3731. NR 1 ENGINE: 09-7110-9-0020, JT8D-9, SN 655056, TT 47631, TC 42725, TSREP 5054. CSREP 3731, TSEHM 5054, CSEHM 3731. INSTALLED 20 SEP 94. NR 2 ENGINE: 09-7110-9-0020, JT8D-9, SN 657594, TT 54656, TC 63164, TSREP 5199. CSREP 4052, TSEHM 5199, CSEHM 4052. INSTALLED 12 NOV 94. 2L72 4F4 F A6WE E2EA 19950602003561995060200356NE 1995 6 2 9508666719 219950526A7230LWAJT9D7F COMPRESSOR BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 4 ENGINE STALLED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JR WARNING INDICATION PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01619US498874740 21321 689481 DURING CLIMB 200 FEET GSL, THE NR 4 ENGINE N1 WENT TO MAX SPEED FOLLOWED BY A LOUD BANG AND COMPRESSOR STALL. THE ENGINE WAS SHUT DOWN, 129,000 POUNDS OF FUEL WAS DUMPED, AND THE AIRCRAFT RETURNED TO ANC WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. THE NR 4 ENGINE WAS REPLACED. CORRECTION: A/C TT 49888 CHANGED TO 49887, S/N 602954 CHANGED TO S/N 689481, PART TOTAL TIME 71028 CHANGED TO 49887, PART TOTAL CYCLES 17360 CHANGED TO 12345, PART TIME SINCE 4740, AND PART DEFECT LOC. NR 3 POSITION CHANGED TO NR 4 POSITION. 2L74 4F4 F A20WE E20EA 19950602003571995060200357NM 1995 6 2 9508676608 119950525A3244 TIRE BOEING747 747151 1384891NM RT MLG FAILED A ANWAAO OTHER J WARNING INDICATION LDLANDING 1 GL01608US 19785 DURING LANDING, CREW EXPERIENCED UNUSUAL DECELERATION AND PULLING TO THE RIGHT WITHOUT BRAKE APPLICATION. ANTI-SKID HYDRAULIC AND GEAR NOT CENTERED LIGHTS ILLUMINATED. INSPECTION FOUND EIGHT TIRES BLOWN. MAINTENANCE REPLACED DAMAGED BRAKES, WHEEL ASSEMBLIES, AND TIRES AS NEEDED. PERFORMED CHECK AND CHECK WAS NORMAL. 2L74 4F A20WE 19950602003581995060200358NM 1995 6 2 9508686622 119950527A8012 START VALVE 7265746 BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE FAILED A NWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL01622US 31911 21704 702240 DURING DESCENT AT FL240, THE NR 3 ENGINE START VALVE LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT CONTINUED TO MSP WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. THE START VALVE AND PRESSURE SWITCH WERE REPLACED AND THE SYSTEM OPERATIONALLY CHECKED OK. 2L74 4F4 F A20WE E3NE 19950602003591995060200359NE 1995 6 2 DHL95706001 219950526A7200JT8D7B ENGINE BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE NR 1 FAILED A TDHLAAJ UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CLCLIMB 1 SO01706DH 19192 65736 DURING DEPARTURE, EXPERIENCED MODERATE AIRFRAME VIBRATION. RETARDED NR 1 THUST LEVER BELOW 75 PERCENT N1, VIBRATION STOPPED. DURING CRUISE, VIBRATION APPEARED AT 90 PERCENT N1. JETTISONED FUEL, PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE, PER BOEING M/M. 2L73 4F4 F A3WE E2EA 19950602003601995060200360 1995 6 2 DHL95805003 419950525A34212587633511 VERTICAL GYRO DOUG DC8 DC873F 302199FWP NR 2 MALFUNCTIONED A DHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01805DH 46125 RADAR STABILIZATION FAILED ON TAKEOFF. REMOVED AND REPLACED NR 2 VERTICAL GYRO. OPS CHECK OK. 2L74 4F RT4A25 19950602003611995060200361NM 1995 6 2 SCNA95105 119950425A5320 DOOR CUTOUT BOEING727 727225 1384077NM FWD ENTRY DOOR CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15284SC 21438 DURING C-CHECK, FOUND A CRACK AT THE FORWARD ENTRY DOOR UPPER RIGHT HINGE. BLENDED OUT DAMAGED AREA IAW SRM 51-10-06, ALODINED AND PRIMED DAMAGED AREA, FABRICATED DOUBLERS AND INSTALLED IAW SRM 52-00-03. 2L73 4F A3WE 19950602003621995060200362NM 1995 6 2 SCNA95106 119950426A27612145014 ACTUATOR BOEING727 727225 1384077NM 1-2/12 SPOILERS FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15284SC 21438 DURING C-CHECK, THE NUMBER 1, 2, AND 12 SPOILERS FAILED THE HOLD DOWN TEST PER SUN COUNTRY WORK CARD 3295, STEP 6 - F. REMOVED AND REPLACED NUMBER 1, 2, AND 12 SPOILER ACTUATORS IAW MM 27-61-00. 2L73 4F A3WE 19950602003631995060200363NM 1995 6 2 SCNA95107 119950426A5315 FLOORBEAM BOEING727 727225 1384077NM BS 340-344 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15284SC 21438 DURING C-CHECK, FOUND THE MAIN FLOOR CABIN BEAM AT BS 340 TO 344 CORRODED. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS IAW SRM 53-10-08 FIGURE 3. ALODINED AND PRIMED PARTS IAW SRM 51-10-02 AND INSTALLED IAW SRM 53-10-08. 2L73 4F A3WE 19950602003641995060200364NM 1995 6 2 SCNA95108 119950510A5330 SKIN BOEING727 7272J4 1384006NM BS 340 DAMAGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15285SC 21676 DURING C-CHECK, FOUND A HOLE IN THE FUSELAGE, 2 INCHES BELOW STRINGER 19 RIGHT AT BODY STATION 340. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM 53-30-3. 2L73 4F RTA3WE 19950602003651995060200365NM 1995 6 2 SCNA95109 119950510A5315 FLOORBEAM BOEING727 7272J4 1384006NM BS 34O CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15285SC 21676 DURING C-CHECK, TWO BULGES WHERE FOUND IN THE FLOOR BOARDS AT BODY STATION 340. UPON REMOVAL, THE FLOOR BOARD CORROSION WAS FOUND ON THE UNDERLYING FLOORBEAM. CUT OUT DAMAGED SECTION FOR FLOORBEAM, FABRICATED AND INSTALLED REPAIR MEMBERS PER AERO CORP ENGINEERING ORDER 95-154. 2L73 4F RTA3WE 19950602003661995060200366NM 1995 6 2 SCNA95110 119950505A5330 SKIN BOEING727 7272J4 1384006NM BS 680 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15288SC 20765 DURING C-CHECK, FOUND 3 DISHED RIVETS AND SKIN BULGES IN THE FUSELAGE BELLY SKIN, AT BODY STATION 680 BUTT SEAM BL3R. FABRICATED DOUBLERS AND FILLERS, INSTALLED IAW SRM 53-30-03 AND 51-30-02. 2L73 4F RTA3WE 19950602003671995060200367NM 1995 6 2 SCNA95111 119950426A5512 SKIN BOEING727 727227 1384078NM RT HORIZ STAB DISBONDING A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, FOUND DISBONDING OF PREVIOUS REPAIR ON RIGHT HAND SIDE OF HORIZONTAL STABILIZER. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 55-10-03 FIGURE 2. 2L73 4F A3WE 19950602003681995060200368NM 1995 6 2 SCNA95112 119950426A5315 FLOORBEAM BOEING727 727227 1384078NM AFT CARGO CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, FOUND AFT CARGO CEILING STRUCTURE TO HAVE CORROSION AT STATION 1130, RBL 45. CUT OUT CORRODED SECTION AND REPAIRED PER SRM 51-40-03. 2L73 4F A3WE 19950602003691995060200369NM 1995 6 2 SCNA95113 119950426A5330 SKIN BOEING727 727227 1384078NM FS 1338 DENTED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, FOUND A DENT IN FUSELAGE SKIN AT STATION 1338, FOUR INCHES FROM VENTRAL STAIR CUTOUT ON RIGHT SIDE. DENT MEASURES 2.5 BY .75 BY .065. CUT OUT DAMAGED SKIN, REPAIRED WITH FILLER AND DOUBLER PER SRM 53-30-03 FIGURE 1. 2L73 4F A3WE 19950602003701995060200370NM 1995 6 2 SCNA95114 119950422A534365C8067862 FITTING BOEING727 727227 1384078NM NLG CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, FOUND PITTING CORROSION AROUND FASTENERS OF GEAR DOOR UPPER RADIUS ROD ATTACH CASTING. REMOVED AND REPLACED FITTING PER SRM 53-30-03. 2L73 4F A3WE 19950602003711995060200371NM 1995 6 2 SCNA95115 119950421A5330 SKIN BOEING727 727227 1384078NM FS 344 DENTED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, REPAIRED FUSELAGE DENT AT STATION 344 STRINGER 23 R, 2.5 BY 1.5 BY .076. REPAIRED DAMAGED AREA BY INSTALLING FILLER AND DOUBLER REPAIR PER SRM 53-30-03 FIGURE 3. 2L73 4F A3WE 19950602003721995060200372NM 1995 6 2 SCNA95116 119950422A5730 SKIN BOEING727 727227 1384078NM WS 436.5 LE CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING C-CHECK, FOUND RIGHT WING, FIXED LEADING EDGE UPPER SURFACE AFT OF NUMBER 5 SLAT, WING STATION 436.5 IS CRACKED IN 4 PLACES ALONG RIVET ROW. CRACKS BLEND TOGETHER MEASURING A TOTAL OF 8.25 INCHES LONG, AND 6 RIVET HEADS ARE SHEARED. HIGH FREQUENCY EDDY CURRENT SHOWED NO CRACKS, FABRICATED AND INSTALLED DOUBLER, ANGLE DOUBLER, AND FILLER PER 57-30-04. 2L73 4F A3WE 19950602003731995060200373NM 1995 6 2 SWAA950406 119950522A5230 ANGLE BOEING737 7372H4 138448CNM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0794SW 23053 DURING SCHEDULED B2 CHECK, FOUND AFT CARGO DOOR WEB ANGLE CRACKED AT 4TH RIVET AT LOWER FWD STOP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950602003741995060200374NM 1995 6 2 SWAA950407 119950522A5320 SHEAR TIE BOEING737 7372T4 1384492NM BS 967 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND BELTFRAME AT BS 967 CORRODED AT SHEAR TIE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950602003751995060200375NM 1995 6 2 SWAA950408 119950522A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 520 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS UNDER SEAT TRACK, BS 520 RBL 25. REPAIRED PER SWA ACO 583-53 R1. 2L72 4F A16WE 19950602003761995060200376NM 1995 6 2 SWAA950409 119950522A5730 SKIN BOEING737 7372T4 1384492NM RT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT WING NUMBER 4 SLAT O/B AUX TRACK CUTOUT CRACKED. REPAIRED PER SWA RA 1-257-0277. 2L72 4F A16WE 19950602003771995060200377NM 1995 6 2 SWAA950410 119950522A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 294.5 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB GROOVED AT BS 294.5 RBL 15. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950602003781995060200378NM 1995 6 2 SWAA950411 119950522A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB CORROSION AT BS 1016 AT FWD FLANGE LBL 10. REPAIRED PER SWA RA 1-253-1298. 2L72 4F A16WE 19950602003791995060200379NE 1995 6 2 SWIA95582 219950523A7261 SCAVENGE LINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT ENGINE LOOSE A SWIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM07403SW 7028 RIGHT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT, 16000 FT. PRESSURE FLUCTUATION BETWEEN 27 TO 22 PSI. ALL OTHER INDICATIONS WERE NORMAL. ANTI-ICE WAS SELECTED ON PRIOR TO LOW OIL PRESSURE READ OUT. WHEN PRESSURE WAS STEADY AT 22 PSI, ENGINE WAS SHUTDOWN. ENGINE OIL TEMPERATURE STAYED NORMAL. TIGHTENED LOOSE SCAVENGE LINE AT TAIL PIPE AREA, SERVICED ENGINE WITH OIL AND RAN ENGINE. OPS CHECKS AND LEAK CHECKS GOOD. 2L72 4F4 FRTA21EA E15NE 19950602003801995060200380SO 1995 6 2 SWIA95583 119950523A2730 SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ELEV TRIM MALFUNCTIONED A SWIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM07205SW 120260 ABORTED TAKEOFF DUE TO TAKEOFF TRIM AURAL WARNING. TRIM WAS SET AT ABOUT 34 PERCENT. REMOVED AND REPLACED THE RIGHT ELEVATOR TRIM SENSOR. OPS CHECKS GOOD IAW MM 27-70-20. 2L72 4T4 TRTA31SO E20NE 19950602003811995060200381SW 1995 6 2 SWIA95584 119950523A7722 EGT COMPENSATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE OUT OF ADJUST A SWIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 NM07174SW AC620 ON TAKEOFF ROLL THE LEFT ENGINE FAILED TO MAKE FULL POWER AT REDUCED TAKEOFF TORQUE. ADJUSTED THE LEFT ENGINE EGT COMPENSATOR. RUN CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950602003821995060200382SW 1995 6 2 SWIA95585 119950527A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LANDING GEAR LACK OF LUBE A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM072720B AC715 GEAR WOULD NOT RETRACT AFTER TAKEOFF. CHECKED SERVICING OF STRUTS, CHECKS GOOD. LUBED GEAR, ALL CHECKS GOOD ON GEAR SWING. 1L72 4T4 T A8SW E4WE 19950602003831995060200383NE 1995 6 2 SWIA95586 219950528A753038E966A VALVE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MIS INSTALLED A SWIAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 NM07217SW 120286 AFTER TAKEOFF, THE RIGHT RED DUCT LIGHT ILLUMINATED. COMPLETED CHECK LISTS AND SHUTDOWN THE RIGHT ENGINE, AIRCRAFT RETURNED TO AIRPORT. FOUND THE RIGHT DE-ICE PRESSURE REGULATING VALVE INSTALLED BACKWARDS, CAUSING BLEED AIR TO VENT INFO FWD WING BOOT FAIRING AREA. REMOVED AND REPLACED VALVE WITH SERVICEABLE UNIT IAW MM 30-10-06. OPERATED DE-ICING SYSTEM, OPS CHECKS GOOD. DUCT LEAK LIGHT DID NOT ILLUMINATE DURING GROUND RUNS. 2L72 4T4 TRTA31SO E20NE 19950602003841995060200384WP 1995 6 2 SWIA95587 219950519A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LEFT FLAMED-OUT A SWIAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 NM07179SW AC643 NR 1 ENGINE FLAMED-OUT ON DESCENT WITH POWER LEVERS PULLED TOWARDS FLIGHT IDLE FOLLOWED BY AUTO RELIGHT ENGINE. ENGINE RETURNED TO NORMAL OPERATION. INSPECTED LEFT ENGINE, ALL CHECKS NORMAL. PERFORMED RUN SHEET ST109. FOUND FUEL FLOW FLIGHT IDLE LOW, ADJUSTED FIFF. RAN ENGINE, CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19950602003851995060200385NM 1995 6 2 UPS203387 119950531A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 948-952 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN C-CHECK, MAINTENANCE FOUND SEAT TRACK CRACKED STA 948 TO 952, RBL 61, WL 207. INSTALLED FABRICATED PARTS IAW SRM 53-10-5, 51-30-2. 2L73 4F A3WE 19950602003861995060200386NM 1995 6 2 UPS203388 119950531A5320653414423 EXPANSON LINK BOEING727 72730C 1384009NM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN C-CHECK, MAINTENANCE FOUND EXPANSION LINK STA 740 TO 760, BL 0, WL 208 CORRODED. REMOVED AND REPLACED EXPANSION LINK IAW SRM 51-10-1. 2L73 4F A3WE 19950602003871995060200387NM 1995 6 2 UPS203389 119950531A532065255918 FITTINGS BOEING727 72730C 1384009NM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN C-CHECK, MAINTENANCE FOUND STRINGER 3A RT AT STA 1183 I/B AND O/B FITTINGS, (PN 65-22547-5, 65-25591-8), CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950602003881995060200388NM 1995 6 2 UPS203392 119950531A5320 SKIN BOEING727 72731C 1384011NM BS 1243-1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED AND CORRODED BS 1243 TO 1342 BETWEEN STRINGERS 10R AND 14R. INSTALLED FABRICATED PARTS IAW SRM 63-30-2, 51-30-2. 2L73 4F A3WE 19950602003891995060200389NM 1995 6 2 UPS203393 119950531A553069154053 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD AT BS 1342, LBL 20 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003901995060200390NM 1995 6 2 UPS203394 119950531A553069154054 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND RT FRAME CHORD AT BS 1342, RBL 20 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003911995060200391NM 1995 6 2 UPS203395 119950531A5530651750855 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD AT BS 1342, LBL 24 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003921995060200392NM 1995 6 2 UPS203396 119950531A553065175086 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND RT FRAME CHORD AT BS 1342, RBL 24 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003931995060200393NM 1995 6 2 UPS203397 119950531A553065225511 CHANNEL BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND LT CHANNEL AT BS 1342, LBL 18, WL 247 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003941995060200394NM 1995 6 2 UPS203398 119950531A553065225512 CHANNEL BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND RT CHANNEL AT BS 1342, RBL 18, WL 247 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003951995060200395NM 1995 6 2 UPS203399 119950531A553065195321 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND LT O/B CHORD AT BS 1342, LBL 30, WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003961995060200396NM 1995 6 2 UPS203400 119950531A553065145322 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND RT O/B CHORD AT BS 1342, RBL 30, WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003971995060200397NM 1995 6 2 UPS203401 119950531A553065209811 CHORD BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND FORWARD CENTER CHORD AT BS 1342 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003981995060200398NM 1995 6 2 UPS203402 119950531A553065225517 CHANNEL BOEING727 72731C 1384011NM WL 250 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND AFT CENTER CHANNEL AT WL 250 CORRODED. REMOVED AND REPLACED CHORD IAW EO B727-5530-4601. 2L73 4F A3WE 19950602003991995060200399NM 1995 6 2 UPS203403 119950531A5320 BRACKET BOEING727 72731C 1384011NM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01924UP 19231 WHILE IN C-CHECK, MAINTENANCE FOUND MAIN CARGO DOOR AFT LATCH ACTUATOR, FWD MOUNT BRACKET AND ATTACH ANGLE CRACKED. INSTALLED FABRICATED PARTS IAW SRM 51-30-1, 51-30-2. 2L73 4F A3WE 19950602004001995060200400NM 1995 6 2 UPS203405 119950531A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER SURFACE OF TOP CHORD STA 344, BL 0, RBL 45. INSTALLED FABRICATED PARTS IAW SRM 51-30-2, 51-20-151, 51-10-2. 2L73 4F A3WE 19950602004011995060200401NM 1995 6 2 UPS203406 119950531A534769246213 SEAT TRACK BOEING727 72730C 1384009NM BS 760-780 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AT STA 760 TO 780, BL 0, WL 208. INSTALLED NEW TRACK IAW SRM 53-10-1. 2L73 4F A3WE 19950602004021995060200402NM 1995 6 2 UPS203407 119950531A5511 SPAR BOEING727 72730C 1384009NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON LT HORIZ STAB UPPER FWD SPAR CHORD, VERT FLANGE AFT SIDE AT SPAR STA 16.08. REPAIRED IAW SRM 55-10-5, 55-10-4. 2L73 4F A3WE 19950602004031995060200403NM 1995 6 2 UPS203408 119950531A5511 SPAR BOEING727 72730C 1384009NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON RT HORIZ STAB FRONT SPAR UPPER CHORD, STAB STA 114, AROUND FASTENER HOLE AFT HORIZ FLANGE. REPAIRED IAW SRM 51-30-2, 55-10-1, 51-10-6, OHM 20-10-3. 2L73 4F A3WE 19950602004041995060200404NM 1995 6 2 UPS203409 119950531A5754651622359 SKIN BOEING727 72730C 1384009NM NR 2 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND NR 2 SLAT HAS 2 GOUGES ON T/E ABOVE THE I/B GUIDE HOOK. REPLACED SLAT IAW B727-5750-1235. 2L73 4F A3WE 19950602004051995060200405NM 1995 6 2 UPS203410 119950531A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 1100-1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK UNDERSIDE BS 1100 TO 1110, LBL 55, WL 204. INSTALLED FABRICATED PARTS IAW SRM 53-10-5. 2L73 4F A3WE 19950602004061995060200406NM 1995 6 2 UPS203411 119950531A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM OF AFT UPPER FLANGE OF FLOORBEAM STA 480, LBL 60. INSTALLED REPAIR ANGLE IAW B727-5310-7006A. 2L73 4F A3WE 19950602004071995060200407NM 1995 6 2 UPS203412 119950531A5320 TIES BOEING727 72730C 1384009NM BS 1183 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TIES STR 20L, BS 1183, WL 185. INSTALLED FABRICATED TIES IAW SRM 51-30-2, 51-20-1. 2L73 4F A3WE 19950602004081995060200408NM 1995 6 2 UPS203413 119950531A5320 WEB BOEING727 72730C 1384009NM FUSELAGE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND WALKWAY PANEL, UPPER TORQUE BOX WEB, LEFT SIDE DELAMINATING. INSTALLED FABRICATED PARTS IAW 53-10-2, 51-10-2. 2L73 4F A3WE 19950602004091995060200409NM 1995 6 2 UPS203414 119950531A53306517555112 SKIN BOEING727 72730C 1384009NM BS 1386 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN PANEL AT BS 1386, RBL 20, WL 255. REMOVED CORROSION AND INSTALLED NEW CHORD IAW SRM 51-30-2, 51-10-1, 53-10-1. 2L73 4F A3WE 19950602004101995060200410NM 1995 6 2 UPS203415 119950531A5320651621928 FITTING BOEING727 72730C 1384009NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B FLANGE RT AFT BOTTLE PIN FITTING STA 870, RBL 60 TO 70.5, WL 192 TO 178. REPLACED FITTING IAW 727-57-1372. 2L73 4F A3WE 19950602004111995060200411NM 1995 6 2 UPS203416 119950531A5320651621928 FITTING BOEING727 72730C 1384009NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B FLANGE LT AFT BOTTLE PIN FITTING STA 870, RBL 60 TO 70.5, WL 194 TO 184. REPLACED FITTING IAW 727-57-1372. 2L73 4F A3WE 19950602004121995060200412NM 1995 6 2 UPS203417 119950531A571165162338 SPAR BOEING727 72730C 1384009NM X 70.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON I/B SIDE RT UPPER SPAR CHORD BETWEEN WEB AND SPAR CHORD 70.5, BS 870. REPLACED CHORD IAW B727-5710-7020A. 2L73 4F A3WE 19950602004131995060200413NM 1995 6 2 UPS203418 119950531A532065255916 FITTING BOEING727 72730C 1384009NM FS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND STRINGER 3A LT AT STA 1183 I/B FWD FITTING HAS CRACK INDICATION. REMOVED FITTING AND REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 19950602004141995060200414NM 1995 6 2 UPS203419 119950531A5313BAC1498138 STRINGER BOEING727 72730C 1384009NM BS 390-400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 25 LT BS 390 TO 400. REPAIRED STRINGER IAW SRM 53-10-1, 53-10-3, 53-10-2. 2L73 4F A3WE 19950602004151995060200415NM 1995 6 2 UPS203420 119950531A5712 RIB BOEING727 72730C 1384009NM X 70.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK, MAINTENANCE FOUND LEFT AND RIGHT 70.5 RIB CHORDS CRACKED. REPAIRED IAW B727-5710-7024A, B727-5710-7023A. 2L73 4F A3WE 19950602004161995060200416NM 1995 6 2 UPS203421 119950531A5753 SKIN BOEING727 72727C 138400JNM TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01910UP 19117 MAINTENANCE REPORTED CRACK AND DELAMINATION OF T/E MID SPAN OF O/B FLAP. REPAIRED FLAP IAW SRM 53-10-00. 2L73 4F A3WE 19950602004171995060200417WP 1995 6 2 WWMA9500038 219950414A723031070512 COMPRESSOR SEAL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENGINE DEFECTIVE I WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15968AE 968 FLIGHT 3280 - BFL/LAX - PILOT REPORTED THAT THE LEFT ENGINE FLOW SMELLS OF OIL. MAINTENANCE REMOVED THE COMPRESSOR SEAL AND ROTOR AND REPLACED WITH NEW SERVICABLE UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T4 TRTA56EU E4WE 19950602004181995060200418EU 1995 6 2 WWMA9500039 119950515A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG DEFECTIVE I WWMAO OTHER N FALSE WARNING CRCRUISE 1 WP15963AE 963 FLIGHT 3367 - IYK/LAX - PILOT REPORTED THAT THE NOSE GEAR LOCKED DOWN LIGHT REMAINED ON AFTER RAISING THE GEAR ON TAKEOFF. THE LIGHT WENT OUT AFTER CYCLING THE GEAR IN FLIGHT, INDICATIONS WERE OKAY ON LANDING AT LAX. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA56EU 19950602004191995060200419EU 1995 6 2 WWMA9500040 119950524A3520K386371 O2 MASKS BAG JETSTMJETSTM3201 1500217EU CABIN DEPLOYED I WWMAG O2 MASK DEPLOYED O OTHER TXTAXI/GRND HDL 1 WP15946AE 946 FLIGHT 3240 - LAX/PSP - PILOT REPORTED THAT UPON LANDING IN PSP AND WHILE TAXIING THE O2 MASKS AT SEATS 2B/C DEPLOYED BY THEMSELVES. THE O2 SYSTEM WAS DEFERRED PER MEL AUTHORITY 35-01 AND THE AIRCRAFT RETURNED TO LAX AT WHICH TIME MAINTENANCE PERSONNEL RESTOWED THE MASKS. MEL WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950602004201995060200420EU 1995 6 2 WWMA9500041 119950528A3222185550185551 RINGS BAG JETSTMJETSTM3201 1500217EU NLG STRUT BROKEN I WWMAK NONE J WARNING INDICATION TOTAKEOFF 1 WP15962AE 962 FLIGHT 3260 - SBP/LAX - PILOT REPORTED AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE LANDING GEAR RETRACTED WHEN THE PILOT SELECTED OVERIDE. MAINTENANCE FOUND THE UPPER PISTON RINGS BROKEN CAUSING BINDING. MAINTENANCE REPLACED PISTON RINGS AND OUTER GLAND SEAL. A GEAR SWING WAS PERFORMED AND THE LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950602004211995060200421EU 1995 6 2 95ZZZX2554 119950312A64201053170023 BEARING BOLKMS117 BK117B1 5626012EU T/R WORN A RMXAK NONE O OTHER ININSP/MAINT 1 SW05117LU208 7144 WORN BEARING (2 EACH) IN TAIL ROTOR. REMOVED AND REPLACED. 1G72 3U H13EU 19950602004221995060200422EU 1995 6 2 95ZZZX2555 119950404A77141179405303 INDICATOR BOLKMS117 BK117B1 5626012EU NR 2 ENG TACH INOPERATIVE A RMXAK NONE O OTHER ININSP/MAINT 1 SW05460H 53 460 7142 NR 2 ENGINE INDICATOR INOPERATIVE. 1G72 3U H13EU 19950602004231995060200423SW 1995 6 2 95ZZZX2556 119950203A6710206010421101 BUSHING BELL 206 206L3 1182108SW COLLECTIVE DEFECTIVE A RMXAK NONE O OTHER ININSP/MAINT 1 SW05725RE 51007 TEFLON COATING ON INSIDE DIAMETER OF BUSHING APPLIED INCORRECTLY, CANNOT INSTALL COLLECTIVE LEVER PINS, DIMENSION TOO SMALL. REPLACED 2 EACH. 1G71 3U H2SW 19950602004241995060200424SW 1995 6 2 95ZZZX2557 119950425A3340A469B FLASH TUBE BELL 206 206L1 1182107SW STROBE FAILED A RMXAK NONE O OTHER ININSP/MAINT 1 SW052070Z9 45730 FLASH TUBE BURNED OUT. SAME PROBLEMS AS ALL THE OTHERS. REMOVED AND REPLACED. 1G71 3U H2SW 19950602004251995060200425EU 1995 6 2 95ZZZX2558 119950321A672011788659 BELLCRANK BOLKMS117 BK117A3 5626015EU T/R WORN BEARING A RMXAK NONE O OTHER ININSP/MAINT 1 SW05117M 243 233 S7023 BEARING WORN, SMALL HOLE. REMOVED AND REPLACED. 1G72 3U H13EU 19950602004261995060200426EU 1995 6 2 95ZZZX2559 119950406A6220ELT302301 FREQ ADAPTER AEROSPSA365 AS365N2 8680815EU M/R CASE SPLIT A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM315 7906 6429 INSPECTION FOUND FREQUENCY ADAPTER CASING SPLIT. REMOVED AND REPLACED FREQUENCY ADAPTER (2 EACH). 1G72 3U RTH10EU 19950602004271995060200427EU 1995 6 2 95ZZZX2560 119950406A6220ELT302301 FREQ ADAPTER AEROSPSA365 AS365N2 8680815EU M/R CASE SPLIT A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM315 7905 6429 INSPECTION FOUND FREQUENCY ADAPTER CASING SPLIT. REMOVED AND REPLACED FREQUENCY ADAPTER (2 EACH). 1G72 3U RTH10EU 19950602004281995060200428EU 1995 6 2 95ZZZX2561 119950405A2913704A44310025 PUMP AEROSPSA365 AS365N2 8680815EU HYD INOPERATIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM659 00332919 6429 HYDRAULIC PUMP INOPERATIVE. 1G72 3U RTH10EU 19950602004291995060200429EU 1995 6 2 95ZZZX2562 119950405A2436D26 REGULATOR AEROSPSA365 AS365N2 8680815EU DC SYSTEM INOPERATIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM659 8025220 6429 VOLTAGE REGULATOR INOPERATIVE. REMOVED AND REPLACED VOLTAGE REGULATOR. 1G72 3U RTH10EU 19950602004301995060200430EU 1995 6 2 95ZZZX2563 119950418A2436D26 REGULATOR AEROSPSA365 AS365N2 8680815EU DC SYSTEM INOPERATIVE A ZYWAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL09365WM 4889050 6429 VOLT REGULATOR INSTALLED, INOPERATIVE. REMOVED AND REPLACED VOLTAGE REGULATOR. 1G72 3U RTH10EU 19950602004311995060200431EU 1995 6 2 95ZZZX2564 119950418A2436D26 GENERATOR AEROSPSA365 AS365N2 8680815EU DC SYSTEM SHORTED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM11 4496196 6429 VOLTAGE REGULATOR SHORTED BY ELECTRICAL PROBLEM IN GENERATOR CIRCUIT. TRACED TO EMERGENCY GENERATOR RESET BUTTON. REMOVED AND REPLACED VOLTAGE REGULATOR. 1G72 3U RTH10EU 19950602004321995060200432EU 1995 6 2 95ZZZX2565 119950414A2436D26 REGULATOR AEROSPSA365 AS365N2 8680815EU DC SYSTEM SHORTED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 8044610 6429 VOLTAGE REGULATOR SHORTS BY ELECTRICAL PROBLEM IN GENERATOR CIRCUIT. TRACED TO EMERGENCY GENERATOR RESET BUTTON. REMOVED AND RESET VOLTAGE REGULATOR. 1G72 3U RTH10EU 19950602004331995060200433EU 1995 6 2 95ZZZX2566 119950417A2430220010 RELAY AEROSPSA365 AS365N2 8680815EU REV CURRENT SHORTED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM 11516 6429 REVERSE CURRENT RELAYS SHORTED BY ELECTRICAL PROBLEM IN GENERATOR CIRCUIT TRACED TO EMERGENCY GENERATOR RESET BUTTON. REMOVED AND REPLACED REVERSE CURRENT RELAYS. REPLACED 2 EACH. 1G72 3U RTH10EU 19950602004341995060200434EU 1995 6 2 95ZZZX2567 119950417A2430220010 RELAY AEROSPSA365 AS365N2 8680815EU REV CURRENT SHORTED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 11509 6429 REVERSE CURRENT RELAYS SHORTED BY ELECTRICAL PROBLEM IN GENERATOR CIRCUIT TRACED TO EMERGENCY GENERATOR RESET BUTTON. REMOVED AND REPLACED REVERSE CURRENT RELAYS. REPLACED 2 EACH. 1G72 3U RTH10EU 19950602004351995060200435EU 1995 6 2 95ZZZX2568 119950416A7110365A24101518 HINGE AEROSPSA365 AS365N2 8680815EU COWL BROKEN A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 6429 HINGE BROKEN. REMOVED AND REPLACED HINGE. 1G72 3U RTH10EU 19950602004361995060200436EU 1995 6 2 95ZZZX2569 119950417A2430580GC01402 CIRCUIT CARD AEROSPSA365 AS365N2 8680815EU DC SYSTEM DEFECTIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 1188 6429 SUSPECTED CONTRIBUTING CAUSE TO ELECTRICAL GENERATING SYSTEM. CHANGED PER PRODUCT SUPPORT. REMOVED AND REPLACED CARDS, 2 EACH. 1G72 3U RTH10EU 19950602004371995060200437EU 1995 6 2 95ZZZX2570 119950417A2430580GC01402 CIRCUIT CARD AEROSPSA365 AS365N2 8680815EU DC SYSTEM DEFECTIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 1175 6429 SUSPECTED CONTRIBUTING CAUSE TO ELECTRICAL GENERATING SYSTEM. CHANGED PER PRODUCT SUPPORT. REMOVED AND REPLACED CARDS, 2 EACH. 1G72 3U RTH10EU 19950602004381995060200438EU 1995 6 2 95ZZZX2571 119950417A2430365A62151900 DIODE PLATE AEROSPSA365 AS365N2 8680815EU DC SYSTEM INOPERATIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM670 6429 D-5 DIODES INOPERATIVE. REMOVED AND REPLACED DIODE PLATE. 1G72 3U RTH10EU 19950602004391995060200439EU 1995 6 2 95ZZZX2572 119950407A7332642100021 TRANSDUCER AEROSPSA365 SA365N 8680669EU NR 2 FUEL PRESS DEFECTIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365SJ103 103 982 6018 NR 2 FUEL PRESSURE FLUCTUATES. REMOVED AND REPLACED FUEL PRESSURE TRANSDUCER. 1G72 3U H10EU 19950602004411995060200441NE 1995 6 2 95ZZZX2574 219950202A7210430125302 BEARING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE RED GEARBOX WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07127HH559 7060 LE45244E EXCESSIVE WEAR TO BALL BEARINGS. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19950602004421995060200442NE 1995 6 2 95ZZZX2575 219950202A7230430124202 BEARING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 1 PITTED A RXMAK NONE O OTHER ININSP/MAINT 1 NM07127HH559 3548 7060 LE45244E BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19950602004431995060200443NE 1995 6 2 95ZZZX2576 219950202A7250410106701 SEAL RING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE 1ST TURBINE WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07127HH127 7060 LE45244E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19950602004441995060200444NE 1995 6 2 95ZZZX2577 219950202A7210230001302 BEARING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE RED GEARBOX WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07127HH559 7060 LE45244E EXCESSIVE WEAR TO BALL BEARINGS. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19950602004471995060200447NE 1995 6 2 95ZZZX2581 219950317A7250414129001 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM077060G882 SC17191 7173 LE45988 ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 1 -0.022 INCH. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. PART TOTAL CYCLES, 2377.4 1G72 3U3 U H13EU E5NE10 19950602004491995060200449 1995 6 2 95ZZZX2583 419950328A221111788292 COMPUTER BOLKMS117 BK117A3 5626015EU SPAS INOPERATIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM07528SF138 0592259 7104 SPAS COMPUTER UNIT INOPERATIVE. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U H13EU 19950602004501995060200450EU 1995 6 2 95ZZZX2584 119950328A28411179405403 INDICATOR BOLKMS117 BK117B1 5626012EU FUEL QTY READS HIGH A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911VU61 1105 7141 FUEL QUANTITY GAUGE READS HIGH. COULD NOT CALIBRATE DOWN. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U H13EU 19950602004511995060200451NE 1995 6 2 95ZZZX2585 219950405A7250414129001 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 929 168 SC20433 7231 LE45806 ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. NR 12 -0.009 INCH, NR 17 -0.014 INCH. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. PART TOTAL CYCLES 3109.6. 1G72 3U3 U H13EU E5NE10 19950602004521995060200452NE 1995 6 2 95ZZZX2586 219950405A7250414129001 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 1098 696 SC17254 7231 LE45807 ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. NR 10 PLUS 0.011 INCH. REPLACED. PART TOTAL CYCLES 1098.1. 1G72 3U3 U H13EU E5NE10 19950602004531995060200453EU 1995 6 2 95ZZZX2587 119950417A28411179405403 INDICATOR BOLKMS117 BK117B1 5626012EU NR 1 FUEL QTY FLUCTUATES A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911VU62 1158 7141 NR 1 SUPPLY TANK NEEDLE FLUCTUATES ERRATICALLY. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U H13EU 19950602004551995060200455 1995 6 2 95ZZZX2589 419950208A3425071105200 TRANSMITTER BENDIX KMT112 SNIAS 350 AS350B2 8680813EU MAG AZIMUTH DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM0794LG 2728 HSI WILL NOT LOCK ON MAGNETIC HEADING UPON INITIAL POWER UP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19950602004681995060200468NE 1995 6 2 95ZZZX2602 219950119A7230430135703 SEAL BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM075188B196 787 7163 LE45518E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT. CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19950602004721995060200472WP 1995 6 2 95ZZZW742 119950507A2822 PUMP DOUG DC9 DC932 3022066WP LT FUEL TANK MALFUNCTIONED A AVJ6AK NONE JK WARNING INDICATION FLUID LOSS DEDESCENT 1 SO11908VJ 47321 FLT NR 542 - PBI - ATL, INBOUND TO ATL PILOT REPORTED TO DISPATCH THAT LEFT MAIN FUEL TANK INDICATOR READS 3800 LBS LESS THAN RIGHT MAIN TANK AND DECLARED EMERGENCY WITH LEFT TANK DEPLETED. FOUND LT TANK EMPTY AND FOUND CENTER TANK WITH 5400 LBS OF FUEL. TRANSFERRED FUEL FROM CENTER TANK TO LT TANK. RAN PUMPS IN LT TANK FOR TWO HOURS, NO TRANSFER OBSERVED, NO EXT LEAKS ON AIRFRAME OR ENGINE NOTED. FUELED LT AND RT MAIN TANKS TO FULL, CENTER TANK EMPTY PER STICKS AND DISPATCHED ON LOCAL ACCEPTANCE FLIGHT FOR FURTHER EVALUATION. ACCEPTANCE FLT AND OPS CHECK GOOD. 2L72 4F A6WE 19950602004731995060200473NM 1995 6 2 95ZZZW743 119950501A2612 LOOP CONNECTOR BOEING747 747131 1384881NM NR 4 ENGINE DIRTY A TWAAO OTHER N FALSE WARNING CRCRUISE 1 CE0553116 20321 CDG - DURING CRUISE NR 4 ENGINE NACELLE TEMPERATURE INDICATOR SHOWED BOTH FIRE DETECTION LOOPS IN THE OVERHEAT RANGE. REDUCTION OF ENGINE THRUST AND SUBSEQUENT SHUTDOWN REVEALED TEMPERATURE INDICATOR IN ERROR. CLEANED LOOP CONNECTORS AND CONNECTORS OF LOWER AFT LOOP. OP CHECKS NORMAL. 2L74 4F A20WE 19950602004741995060200474WP 1995 6 2 95ZZZW744 119950508A3240NAS6405U70D BOLT LKHEED1011 10113851 5265010WP NR 1 BRAKE MISSING A TWAAK NONE O OTHER ININSP/MAINT 1 CE0581027 193B1107 STL - DURING POST FLIGHT, FOUND NR 1 FRONT BRAKE TORQUE ARM DISCONNECTED FROM BRAKE. BOLT, MFG P/N NAS6405U70D, AND PIN, MFG P/N 1523067-101, WERE MISSING. REPLACED NR 1 BRAKE, BRAKE TORQUE ARM, PIN, BOLT AND LANDING GEAR STRUT DOOR. LANDING GEAR OPERATION AND BRAKE SYSTEMS CHECKED NORMAL. REF 95ZZZW744. 2L73 4F A23WE 19950602004751995060200475WP 1995 6 2 95ZZZW745 119950508A32401523067101 PIN LKHEED1011 10113851 5265010WP NR 1 BRAKE MISSING A TWAAK NONE O OTHER ININSP/MAINT 1 CE0581027 193B1107 STL - DURING POST FLIGHT, FOUND NR 1 FRONT BRAKE TORQUE ARM DISCONNECTED FROM BRAKE. BOLT, MFG P/N NAS6405U70D, AND PIN, MFG P/N 1523067-101, WERE MISSING. REPLACED NR 1 BRAKE, BRAKE TORQUE ARM, PIN, BOLT AND LANDING GEAR STRUT DOOR. LANDING GEAR OPERATION AND BRAKE SYSTEMS CHECKED NORMAL. REF 95ZZZW744. 2L73 4F A23WE 19950602004761995060200476WP 1995 6 2 95ZZZW746 119950509A2497B036682 WIRE LKHEED1011 10113851 5265010WP SERVING CART FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531013 193B1035 STL - DURING CRUISE SINGLE SERVING CART ELECTRICAL CABLE SHORTED CAUSING SMOKE IN CABIN. DISCONNECTED ELECTRICAL CABLE. REPLACED ELECTRICAL CABLE, MFG P/N B03668-2. SINGLE SERVING CART OPERATION CHECKED NORMAL. 2L73 4F A23WE 19950602004771995060200477WP 1995 6 2 95ZZZW747 119950514A3350 EEL WIRE DOUG DC9 DC982 3022082WP FS 1060 OUT OF POSITION A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05953U 49267 MCI - DURING INVESTIGATION OF EMERGENCY LIGHT PROBLEMS, FOUND RUDDER CABLE B-1 BURNT. FOUND EMERGENCY LIGHT BATTERY PACK WIRE RUBBING ON RUDDER CABLE AT STA 1060. REPLACED RUDDER CABLE AND REPAIRED BATTERY PACK WIRE, CLAMPED WIRE TO CLEAR CABLE. RUDDER OPERATION AND EMERGENCY LIGHT OPERATION CHECKED NORMAL. 2L72 4F A6WE 19950602004781995060200478NE 1995 6 2 95ZZZW748 219950513A7230UL26735 COMP BLADES LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 ENG FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0531008 193B1028 4405 STL - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO HIGH AVM AND N2 OVERSPEED. REPLACED NR 2 ENGINE. GROUND RUNUP AND OPERATIONS CHECKED NORMAL. S/D INVESTIGATION INTO THE SHUTDOWN OF ENGINE, S/N 4405, DUE TO HIGH AVM AND N2 OVERSPEED, REVEALED HIGH PRESSURE COMPRESSOR 5TH SHROUD RING, MFG P/N UL26735, HAD ANTI-FRET PADS LIBERATE FROM VANE SLOTS IMPACTING BLADES, CAUSING BLADE FRACTURES. ENGINE WAS REPAIRED AND RETURNED TO SERVICE. (M) 2L73 4F4 F A23WE A12EU 19950602004791995060200479WP 1995 6 2 95ZZZW749 119950516A4990 APU DOUG DC9 DC983 3022083WP AFT FUS OIL LEAK A TWAAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE059307R 49663 LGA - DURING CRUISE AT FL 370 A BLUE HAZE APPEARED IN CABIN. DESCENDED TO FL 330 AND TURNED OFF HIGH PRESSURE BLEEDS AND BLUE HAZE DISSIPATED. FOUND APU LEAKING OIL. PLACARDED APU INOPERATIVE PER MEL. REPLACED BOTH WATER SEPARATOR COALESCER BAGS. PRESSURIZATION AND AIR CONDITIONING SYSTEMS CHECKED NORMAL. 2L72 4F RTA6WE 19950602004801995060200480WP 1995 6 2 95ZZZW750 119950520A323159151695506 DOOR LATCH DOUG DC9 DC931 3022065WP RT MLG OUT OF ADJUST A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05980Z 47344 STL - AFTER TAKEOFF RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION, AND LANDING GEAR DOOR OPENED DURING UPLATCH CHECK. FOUND DOOR LATCH MECHANISM, MFG P/N 5915169-5506, WOULD NOT ALWAYS ENGAGE DOOR ROLLERS. RIGGED DOOR LATCH MECHANISM. LANDING GEAR DOOR AND LIGHT INDICATION CHECKED NORMAL. 2L72 4F A6WE 19950602004811995060200481WP 1995 6 2 95ZZZW751 119950519A253050381 OVEN DOUG DC9 DC982 3022082WP GALLEY FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05950U 49230 STL - DURING CRUISE E GALLEY OVEN, MFG P/N 50381, BEGAN SMOKING WHEN TURNED ON. TURNED OFF OVEN. REPLACED OVEN AND OPERATION CHECKED NORMAL. 2L72 4F A6WE 19950602004831995060200483NM 1995 6 2 95ZZZW753 119950515A521065299932 PLATE BOEING727 727254 138408LNM PAX DOOR WORN A TAOAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15913TS 20250 ON TAKOFF, LOUD AIR LEAK FROM FORWARD ENTRY DOOR. DOOR LIGHT WAS OUT. FLIGHT ATTENDANT COULD SEE LIGHT THROUGH UPPER LEFT CORNER OF DOOR. AIRCRAFT RETURNED TO LGA. REPLACED 2 GUIDE PLATES AT THE DOOR UPPER HINGE AND RIGGED DOOR PER MM 52-11-01. REFERENCE TAOA059509. 2L73 4F A3WE 19950602004841995060200484SW 1995 6 2 95ZZZW755 119950510A7712 TQ SIG COND SWRNGNSA227 SA227AC 8780603SW RT ENGINE OUT OF ADJUST A CHQAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA233117V AC604 PILOT RETURNED TO FIELD FOR RIGHT ENGINE APPEARING SHY OF TORQUE. THE ENGINE WAS INSPECTED. THE SIGNAL CONDITIONER CALIBRATION CHECKED. ENGINE GROUND RUN WITH ALL INDICATIONS NORMAL. (W) 1L72 4T A8SW 19950602004851995060200485SW 1995 6 2 95ZZZW756 119950505A2435230790001 STARTER/GEN SWRNGNSA227 SA227AC 8780603SW RT ENG FAILED A CHQAO OTHER O OTHER ININSP/MAINT 1 EA2327330 31 4822 AC756 PILOT REPORTED THE RIGHT ENGINE WOULD NOT START. UPON TROUBLE SHOOTING BY MAINTENANCE THE STARTER/GENERATOR WAS FOUND TO BE THE PROBLEM. THE STARTER/GENERATOR WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. 1L72 4T A8SW 19950602004861995060200486NM 1995 6 2 95ZZZW757 119950508A5320141N516078 INTERCOSTAL BOEING757 7572G7 1384963NM BS 364 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - DURING C6 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT AND INTERCOSTAL CORRODED BEYOND LIMITS AT STATION 344. REPLACED DAMAGED PARTS PER SRM 51-10-00. REFERENCE AWXA9500269. 2L72 4F RTA2NM 19950602004871995060200487NM 1995 6 2 95ZZZW758 119950509A5743BACB30856K32 BOLT BOEING737 73733A 1384673NM LT MLG SHEARED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28168AW 23629 LAS-ABQ - FLT NR 212 - CREW REPORTED FLIGHT CONTROL FLUTTER ON TAKEOFF. WHEN FLAPS WERE RETRACTED THE FLUTTER WAS NOT NOTICED. AIRCRAFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LT MLG BEAM SUPPORT TO REAR SPAR ATTACH BRACKET BOLT, THE NR 2 CANOE ARM ASSEMBLY, THE NR 7 JACK SCREW BOLTS AND BEARING, AND TOGGLE AND BOLTS. ADJUSTED TURN BUCKLE TO ALIGN PANEL. AIRCRAFT RETURNED TO SERVICE FOR TEST FLIGHT. TEST FLIGHT COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. REF AWXA9500283 AND 95ZZZW759. 2L72 4F RTA16WE 19950602004881995060200488NM 1995 6 2 95ZZZW759 119950509A2750656826919 ARM ASSY BOEING737 73733A 1384673NM NR 2 CANOE LOOSE A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28168AW 23629 LAS-ABQ - FLT NR 212 - CREW REPORTED FLIGHT CONTROL FLUTTER ON TAKEOFF. WHEN FLAPS WERE RETRACTED THE FLUTTER WAS NOT NOTICED. AIRCRAFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LT MLG BEAM SUPPORT TO REAR SPAR ATTACH BRACKET BOLT, THE NR 2 CANOE ARM ASSEMBLY, THE NR 7 JACK SCREW BOLTS AND BEARING, AND TOGGLE AND BOLTS. ADJUSTED TURN BUCKLE TO ALIGN PANEL. AIRCRAFT RETURNED TO SERVICE FOR TEST FLIGHT. TEST FLIGHT COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. REF AWXA9500283 AND 95ZZZW758. 2L72 4F RTA16WE 19950602004891995060200489NM 1995 6 2 AWXA9500269 119950508A5320141NT16079 SUPPORT BOEING757 7572G7 1384963NM BS 364 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28909AW 24522 PHX - DURING C6 INSPECTION, FOUND R1 DOOR THRESHOLD SUPPORT AND INTERCOSTAL CORRODED BEYOND LIMITS AT STATION 344. REPLACED DAMAGED PARTS PER SRM 51-10-00. REF 95ZZZW757. 2L72 4F RTA2NM 19950602004901995060200490NM 1995 6 2 AWXA9500283 119950509A275065C343141 TOGGLE ASSY BOEING737 73733A 1384673NM NR 7 JACK SCREW LOOSE A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28168AW 23629 LAS-ABQ - FLT NR 212 - CREW REPORTED FLIGHT CONTROL FLUTTER ON TAKEOFF. WHEN FLAPS WERE RETRACTED THE FLUTTER WAS NOT NOTICED. AIRCRAFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE LT MLG BEAM SUPPORT TO REAR SPAR ATTACH BRACKET BOLT, THE NR 2 CANOE ARM ASSEMBLY, THE NR 7 JACK SCREW BOLTS AND BEARING, AND TOGGLE AND BOLTS. ADJUSTED TURN BUCKLE TO ALIGN PANEL. AIRCRAFT RETURNED TO SERVICE FOR TEST FLIGHT. TEST FLIGHT COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. REF 95ZZZW758 AND 95ZZZW759. 2L72 4F RTA16WE 19950602004911995060200491 1995 6 2 BUFA9513 419950514A3418C267072 LIFT TRANSDUCER DOUG DC8 DC861 3021952WP STALL WARNING DEFECTIVE A BUFAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE05161DB 45980 FLT 792 - STALL WARNING CAME ON RIGHT AFTER ROTATION, STALL WARNING STILL ON AT 220 KTS IN LEVEL FLIGHT, ALL OTHER INDICATIONS NORMAL. RETURNED TO MMMX. REMOVED AND REPLACED STALL WARNING LIFT TRANSDUCER, SYSTEM OP CHECK NORMAL PER MM 34-16. (W) 2L74 4F 4A25 19950602004921995060200492NE 1995 6 2 P2EA95004 219950501A72602196882 GARLOC SEAL BOEING737 737281 138448PNM PWA JT8 JT8* 52044NE NR 1 ENGINE FAILED A P2EAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE05219US 20414 FLT NR 114A - MCI - NR 2 ENGINE LOST OIL QUANTITY THEN OIL PRESSURE. ENGINE WAS SHUT DOWN INFLIGHT. MAINTENANCE REMOVED AND REPLACED GEARBOX GARLOC SEAL. (W) 2L72 4F4 F A16WE E2EA 19950602004931995060200493EU 1995 6 2 SIMA951271 119950517A2720S2728178120000 TUBE LEVER AEROSPATR42 ATR42300 8680920EU RUDDER WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21424MQ 045 SAT - DURING 8 YEAR INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE TO LEVER ATTACHMENT POINT LOOSE AND HOLES ELONGATED. REMOVED AND REPLACED TUBE LEVER ATTACHMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602004941995060200494EU 1995 6 2 SIMA951351 119950515A33503011180 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN INOP A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21235RM 235 MQT - DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602004951995060200495EU 1995 6 2 SIMA951353 119950515A77143039242 PROBE PICKUP AEROSPATR72 ATR72212 EU NR 1 ENGINE MALFUNCTIONED A SIMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW21410AT 410 NR 1 ENGINE TQ SURGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 1 NH SENSOR, IAW PW MM (PROBE PULSE PICKUP). COMPLETED SUCCESSFUL TEST FLIGHT AND RETURNED AIRCRAFT TO SERVICE. (W) 2H72 4T RTA53EU 19950602004961995060200496EU 1995 6 2 SIMA951391 119950519A2710S2711009100300 BELLCRANK AEROSPATR42 ATR42300 8680920EU RT AILERON CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21427MQ 091 MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND THE RIGHT AILERON BELLCRANK (INBOARD) AFT BEARING RUSTED AND BINDING. MAINTENANCE REMOVED AND INSPECTED BELLCRANK ASSEMBLY AND COMPLIED WITH FUNCTIONAL CHECK OF AILERON SYSTEM IAW ATR 42 J/C 27-10-00 FUT 10005. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602004971995060200497EU 1995 6 2 SIMA951392 119950519A2710S2718141600000 BELLCRANK AEROSPATR42 ATR42300 8680920EU RT AILERON BINDING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21427MQ 091 MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND CENTER WING BOX RIGHT AILERON BELLCRANK FORWARD BEARING BINDING. MAINTENANCE REMOVED AND INSPECTED BELLCRANK ASSEMBLY AND COMPLIED WITH FUNCTIONAL CHECK OF AILERON SYSTEM IAW ATR 42 J/C 27-10-00 FUT 10005. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602004981995060200498EU 1995 6 2 SIMA951393 119950519A2710S5761003900020 SHACKLE ASSY AEROSPATR42 ATR42300 8680920EU RT AILERON WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21427MQ 091 MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE RIGHT AILERON OUTBOARD HINGE TO HAVE EXCESSIVE PLAY. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SHACKLE ASSY ON THE RIGHT AILERON. A FUNCTIONAL CHECK OF THE AILERONS WAS COMPLIED WITH IAW ATR 42 J/C 27-10-00. AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602004991995060200499EU 1995 6 2 SIMA951394 119950519A2710S5761003900020 SHACKLE ASSY AEROSPATR42 ATR42300 8680920EU LT AILERON WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21427MQ 091 MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE LEFT AILERON OUTBOARD HINGE TO HAVE EXCESSIVE PLAY. MAINTENANCE REMOVED AND REPLACED THE OUTBOARD SHACKLE ASSY ON THE LEFT AILERON. A FUNCTIONAL CHECK OF THE AILERONS WAS COMPLIED WITH IAW ATR 42 J/C 27-10-00. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602005001995060200500EU 1995 6 2 SIMA951395 119950519A2710S5761004600004 CRANK ASSY AEROSPATR42 ATR42300 8680920EU LT AILERON WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21427MQ 091 MQT - DURING BRIDGE INSPECTION, MAINTENANCE FOUND THE LEFT AILERON HINGE POINT TO HAVE A BAD BEARING. MAINTENANCE REMOVED AND REPLACED THE LEFT AILERON MIDDLE HINGE ASSY. A FUNCTIONAL CHECK OF THE AILERONS WAS COMPLIED WITH IAW ATR 42 J/C 27-10-00. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602005011995060200501EU 1995 6 2 SIMA951396 119950519A5330S53172101202 SKIN AEROSPATR42 ATR42300 8680920EU FWD FUSELAGE DAMAGED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21426MQ 037 ORD - MAINTENANCE REPORTED THE RIGHT FORWARD NOSE AREA HAD EXTENSIVE DAMAGE FROM CONTACT WITH GROUND POWER UNIT. MAINTENANCE PERFORMED A TEMPORARY REPAIR AND AIRCRAFT WAS FERRIED TO MQT. TEMPORARY REPAIR WAS REMOVED AND AREA WAS REPAIRED WITH A DOUBLER PATCH, IAW EO E1-5300-125. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950602005021995060200502NM 1995 6 2 TAOA059509 119950515A521065594491 PLATE BOEING727 727254 138408LNM PAX DOOR WORN A TAOAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15913TS 20250 ON TAKEOFF, LOUD AIR LEAK FROM FORWARD ENTRY DOOR. DOOR LIGHT WAS OUT. FLIGHT ATTENDANT COULD SEE LIGHT THROUGH UPPER LEFT CORNER OF DOOR. AIRCRAFT RETURNED TO LGA. REPLACED 2 GUIDE PLATES AT THE DOOR UPPER HINGE AND RIGGED DOOR PER MM 52-11-01. REF 95ZZZW753. 2L73 4F A3WE 19950602005031995060200503EU 1995 6 2 VTZA95175 119950504A524014153133207 SERVICE DOOR JETAIRJETSTMJETSTM4101 1500501EU LAVATORY MISSING A VTZAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA27315UE 41033 IAD-PVD - FLT 6215 - DURING PREFLIGHT WALK AROUND IT WAS DISCOVERED THAT THE LAVATORY SERVICE DOOR WAS MISSING. MAINTENANCE OPENED DMI NR 17224 IAW CDL 52-40. MAINTENANCE LATER CLEARED DMI NR 17244 BY REPLACING THE LAVATORY SERVICE DOOR. (W) 2L72 4T RTA41NM 19950602005041995060200504EU 1995 6 2 VTZA95176 119950516A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27314UE 41027 FLT 6204 - MHT-IAD - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR LIGHT ILLUMINATING ON THE TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENACNE OPENED DMI NR 40042 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 40042 BY ADJUSTING BOTH DOOR MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950602005051995060200505SO 1995 6 2 WTAA950190 119950512A4950 APU EMB 120 EMB120RT SO CABIN SMOKING A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP17122AM 120013 RNO - SMOKE ODOR REPORTED IN CABIN FROM LEFT PACK WITH AIRCRAFT ON GROUND. SMOKE ODOR NOT NOTED DURING FLIGHT OPERATION. MAINTENANCE DEFERRED APU BLEED AIR SYSTEM PER MEL 49-52-1. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602005061995060200506EU 1995 6 2 WTAA950191 119950511A3250 CONNECTOR BAG JETSTMJETSTM3101 1500215EU NLG STEERING LOOSE A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17430UE 784 SEA - LANDING GEAR FAILED TO MOVE TO UP POSITION DURING ATTEMPTED GEAR RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED ELECTRICAL CONNECTION AT NOSEWHEEL STEERING ISOLATION VALVE P/N A1424D. PERFORMED LANDING GEAR RETRACTION CHECK. ALL OPERATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602005071995060200507EU 1995 6 2 WTAA950192 119950511A32305EN16 SQUAT SWITCH BAG JETSTMJETSTM3101 1500215EU NLG FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17430UE 784 EUG - LANDING GEAR FAILED TO MOVE TO UP POSITION DURING ATTEMPTED GEAR RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR SQUAT SWITCH. PERFORMED LANDING GEAR RETRACTION CHECK. ALL OPERATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA21EU 19950602005081995060200508SO 1995 6 2 WTAA950193 119950517A2730922AA2YA6PZ722 PROX SENSORS EMB 120 EMB120RT SO LT/RT ELEVATOR OUT OF ADJUST A WTAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP17285UE 120153 FAT - AURAL 'TAKEOFF TRIM' WARNING SOUNDED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED ELEVATOR TRIM SYSTEM. DISCOVERED ELEVATOR TRIM TAB PROXIMITY SENSORS OUT OF ADJUSTMENT. ADJUSTED SENSORS PER EMB-120RT MM 27-32-00, PG 501. ELEVATOR TRIM SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950602005091995060200509WP 1995 6 2 WTAA950194 219950518A73208974575 BYPASS VALVE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE331* 01514WP LT ENG FUEL FAILED A WTAAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION LDLANDING 1 WP17420UE 788 CIC - LEFT ENGINE FLAMEOUT REPORTED DURING ROLLOUT FROM LANDING. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE FUEL BYPASS VALVE. ENGINE LEAK CHECK AND OPERATIONAL CHECK NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4T3 TRTA21EU E2WE 19950602005311995060200531NE 1995 6 2 95ZZZX2628 219950508A7230 BLADE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE 1ST STAGE COMP BENT A AWHAK NONE O OTHER NRNOT REPORTED 1 WP17790FE 208B0288 19165 PILOT REPORTED HIGH PITCHED NOISE FROM ENGINE AT POWER. FOUND ONE BLADE ON 1ST STAGE COMPRESSOR BENT. BLADE WAS BENT AT THE LEADING EDGE AT THE END OF THE BLADE. SUSPECT CAUSE WAS ICE FOD. NO OTHER DAMAGE WAS NOTED TO 1ST, 2ND OR 3RD STAGE COMPRESSORS. 1H71 3T3 T A37CE E4EA 19950602005331995060200533WP 1995 6 2 95ZZZX2630 219950515A7261 SEAL SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110U 01514WP OIL PUMP LEAK A BDHAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL15328BA 253 RIGHT ENGINE LOST OIL PRESSURE IN-FLIGHT AND WAS SHUT DOWN. SEAL FAILURE WAS DUE TO WORN OIL PUMP SHAFT. 1L72 4T4 T A8SW E4WE 19950602005361995060200536NE 1995 6 2 95ZZZX2633 219950508A7230 BLADE CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE 1ST STAGE COMP BENT A AWHAK NONE E VIBRATION/BUFFET NRNOT REPORTED 1 WP17781FE1527 208B0278 19154 PILOT REPORTED VIBRATION AT LOW RPM. FOUND ONE BLADE ON 1ST STAGE COMPRESSOR BENT AND CRACKED AT LEADING EDGE AT END OF BLADE. NO OTHER DAMAGE NOTED TO 1ST, 2ND, OR 3RD STAGE COMPRESSORS. SUSPECT CAUSE, ICE INGESTION. 1H71 3T3 T A37CE E4EA 19950602005381995060200538NM 1995 6 2 PCAA9500216 119950421A323010800109 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA132FOR 3482 L28387 215 RT MAIN GEAR UNSAFE INDICATION WHEN GEAR WAS EXTENDED. REMOVED AND REPLACED RT UPLOCK ACTUATOR, OPS CHECK OKAY. LUBED UPLOCK ROLLER IAW MM. AIRCRAFT RETURNED TO SERVICE. ACTC: 14298.(X) 2H72 4T RTA13NM 19950602005391995060200539NE 1995 6 2 9508691144 219950528A7200 ENGINE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 1 FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01144JC 46753 686164 DURING CRUISE, THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE FOLLOWED BY DECREASE IN OIL PRESSURE. THE ENGINE WAS SHUT DOWN. APPROXIMATELY 85,000 POUNDS OF FUEL WAS DUMPED AND THE AIRCRAFT DIVERTED TO YUL WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. THE AIRCRAFT WAS FERRIED TO MSP WHERE THE NR 1 ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19950602005401995060200540 1995 6 2 9508709153 419950527A3455 NAV/COMM PANEL DOUG DC9 DC914 3022034WP CONTROL PEDEST. NOT SEATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018912E 45829 LOSS OF NR 1 NAV RECEIVER OCCURRED AFTER TAKEOFF. VOR/LOC FLAG WAS IN VIEW AND NO BEARING WAS AVAILABLE. PULLED AND RESET NAV CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NR 1 NAV/COMM CONTROL PANEL NOT SEATED PROPERLY. REPOSITIONED PANEL. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602005411995060200541WP 1995 6 2 9508719881 119950530A324495502673 TIRES DOUG DC9 DC951 3022051WP RT NLG OUT OF ROUND A NWAACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL01676MC3403 185 47652 ABORTED TAKEOFF AT 60 KNOTS DUE TO EXCESSIVE VIBRATION FROM NOSE GEAR AREA. FOUND BOTH NOSE TIRES WITH OUT OF ROUND CONDITION. REPLACED BOTH TIRES. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602005421995060200542WP 1995 6 2 9508729924 119950529A2420 CONTROL PANEL DOUG DC9 DC932 3022066WP LEFT MALFUNCTIONED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01926RC 47473 LEFT AC GENERATOR TRIPPED OFF LINE DURING TAKEOFF ROLL AT APPROXIMATELY 80 KNOTS. AFTER CLEARING RUNWAY, GENERATOR WAS RESET AND REMAINED ON LINE. REPLACED THE LEFT GENERATOR CONTROL PANEL AND VOLTAGE REGULATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950602005431995060200543WP 1995 6 2 9508739882 119950527A3231 CONTROL CABLE DOUG DC9 DC951 3022051WP RT NLG DOOR BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01670MC 47659 A LOUD POP ACCOMPANIED BY EXCESSIVE NOSE WHEEL VIBRATION OCCURRED DURING GEAR RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND THE RIGHT NOSE GEAR DOOR IN DOWN POSITION AND DOOR STOP CABLE BROKEN. REPLACED THE RIGHT NOSE STRUT AND DOOR STOP CABLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 19950602005441995060200544NM 1995 6 2 9508742280 119950531A5270 WARNING LIGHT BOEING727 727251 138408HNM CARGO DOOR ILLUMINATED A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01280US 21159 DURING TAKEOFF ROLL, AFT CARGO DOOR WARNING INDICATION ILLUMINATED. ABORTED TAKEOFF AT 65 KNOTS. MAINTENANCE DEFERRED AFT CARGO DOOR WARNING INDICATION SYSTEM INOPERATIVE PER MEL 52-4. 2L73 4F A3WE 19950602005451995060200545NE 1995 6 2 9508755522 219950528A75323830041103 BLEED VALVE BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A NWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01522US 23616 16495 DURING CLIMB, THE NR 2 COMPRESSOR STALLED TWICE. TWO LOUD BANGS AND A BRIGHT FLASH WERE OBSERVED. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. AIRCRAFT WAS RETURNED TO MEM WHERE TROUBLESHOOTING FOUND THE 2.5 BLEED VALVE SEIZED. THE ENGINE WAS REPLACED. 2L72 4F4 FRTA2NM E17NE 19950602005461995060200546WP 1995 6 2 ABXA9500517 119950516A55127075T6 SKIN DOUG DC8 DC861 3021952WP RT HORIZ STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 DURING D-CHECK AND COMPLIANCE OF ASB A55-16, FOUND THE RIGHT HORIZONTAL STABILIZER OUTBOARD UPPER CENTER SKIN PLANK CRACKED AT BOLT HOLES 10 AND 11. REMOVED AND REPLACED THE RIGHT HORIZONTAL STABILIZER IAW DC-8 MM CHAPTER 55. 2L74 4F 4A25 19950602005471995060200547WP 1995 6 2 ABXA9500518 119950524A275057511521 FLAP DRIVE LINK DOUG DC8 DC862 3021970WP STATION 98 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23803AX 45917 DURING C-CHECK, COMPLIANCE OF A.D. 88-10-07 AND USING ULTRASONIC INSPECTION, FOUND THE FLAP DRIVE LINK AT STATION 98, POINT J TO BE CRACKED. REPAIRED LEFT FLAP DRIVE LINK IAW DC-8 MM CHAPTER 27. 2L74 4F 4A25 19950602005481995060200548WP 1995 6 2 ABXA9500519 119950525A56105912880505 WINDOW SEAL DOUG DC8 DC862 3021970WP LT COCKPIT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23805AX 45906 DURING MAINTENANCE INSPECTION, DISCOVERED THAT THE CAPTAIN'S CLEAR VIEW WINDOW WOULD NOT OPEN. REMOVED EXCESS FILLER FROM THE SEAL SURFACE OF WINDOW FRAME. RESURFACED SEAL AND ADJUSTED THE UPPER LATCH IAW DC-8 MM CHAPTER 56. 2L74 4F 4A25 19950602005491995060200549SO 1995 6 2 COM11906 119950530A27503471001001 ANNUNCIATOR EMB 120 EMB120RT SO INST PANEL DEFECTIVE A COMAK NONE N FALSE WARNING DEDESCENT 1 SO01246CA9762 95 120223 FLAP CONTROL FAULT WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE FLAP ANNUNCIATOR UNIT. 2L72 4T RTA31SO 19950602005501995060200550SO 1995 6 2 COM11907 119950530A7600 RIGGING EMB 120 EMB120RT SO RT PROP OUT OF ADJUST A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01267CA 1 120259 RIGHT PROPELLER WILL NOT FEATHER BY USING THE CONDITION LEVER. ADJUSTED ENGINE RIGGING. 2L72 4T RTA31SO 19950602005511995060200551SO 1995 6 2 COM11908 119950530A2150215483432 THERMOSTAT EMB 120 EMB120RT SO LEFT DEFECTIVE A COMAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01137H 120137 LEFT DUCT OVERHEAT WARNING ON. REPLACED THE LEFT DUCT THERMOSTAT. 2L72 4T RTA31SO 19950602005521995060200552EU 1995 6 2 COM31092 119950530A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01361CA10833 JAN920195 340A056 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950602005531995060200553EA 1995 6 2 COM60486 119950530A2750860D10014 FECU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01915CA3465 1007 7013 FLAPS FAILED AT 20 DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950602005541995060200554EA 1995 6 2 COM60487 119950530A28202421143 SHUTOFF VALVE CNDAIRCL600 CL6002B19 EA RIGHT FAILED A COMAK NONE J WARNING INDICATION CRCRUISE 1 SO01943CA422 7062 RIGHT TRANSFER SHUT-OFF VALVE FAILED. REPLACED THE SHUT-OFF VALVE. 2L72 4F RTA21EA 19950602005551995060200555EA 1995 6 2 COM60488 119950526A2750857SD10013 FLEX DRIVE CNDAIRCL600 CL6002B19 EA RT TE FLAP DAMAGED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01938CA 7046 FLAPS FAIL AT 20 DEGREES DURING APPROACH. REPLACED DEFECTIVE RIGHT INBD FLAP FLEX DRIVE CABLE. 2L72 4F RTA21EA 19950602005561995060200556NM 1995 6 2 DL72E952112 119950513A5320 CLIP BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 UNK FOUND ON CV2 CK - CORROSION ON FUSELAGE FRAME TO SKIN ATTACH CLIP FWD SIDE STA 1010 BETWEEN STR 30/29R - REPAIR - REPLACED SKIN CLIP PER M/M 53-11-0. 2L73 4F A3WE 19950602005571995060200557NM 1995 6 2 DL72E952113 119950513A5313 STRINGER BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 UNK FOUND ON CV2 CK - CORROSION INSIDE STR 30 AFT OF SIDE STA 1010 JUST AFT OF FACTORY SPLICE - REPAIR - REPAIRED PER ERA 301748-14. 2L73 4F A3WE 19950602005581995060200558NM 1995 6 2 DL72E952329 119950520A335090052 EEL BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11282WA 21484 DURING LAYOVER, FOUND FORWARD CABIN EMERGENCY EXIT LIGHT INOP. REPLACE RACK AND BATTERY. OPERATION NORMAL. 2L73 4F A3WE 19950602005591995060200559NM 1995 6 2 DL72L952262 119950525A5754651622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 UPON INSPECTION BY MAINT. RIB NR 11 IN NR 7 L/E SLAT WAS FOUND CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950602005601995060200560NM 1995 6 2 DL72S952018 119950510A57536521630188 SKIN BOEING727 727232 1384082NM RT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 TOP SKIN DENTED 19 INCHES FROM I/B, BOTTOM SKIN DENTED AND TORN AWAY FROM SPAR 19 INCHES FROM I/B, BOTTOM SKIN DENTED 30 INCHES FROM I/B. THESE WERE ALL REPAIRED PER SRM 51-40-6. DEEP GOUGE IN L/E FWD OF I/B ARM, CHAFING MARKS AT 62 INCHES FROM I/B, CHAFING MARKS AT 68 AND 72 INCHES ON L/E. THESE WERE ALL REPAIRED PER SRM 57-50-4 FOR RIGHT WING FLAP PANEL, DURING SHOP INSPECTION. 2L73 4F A3WE 19950602005611995060200561NM 1995 6 2 DL72S952101 119950414A5753652163261 THRUST BEARING BOEING727 727232 1384082NM NR 2 MID FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 X NR 2 MID-FLAP DURING HMV SHOP INSP WAS FOUND TO HAVE CORROSION IN THE I/B THRUST BEARING TOP I/B AND O/B RETAINER BOLT HOLES. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950602005621995060200562NM 1995 6 2 DL72S952102 119950414A5753652163261 FITTING BOEING727 727232 1384082NM NR 2 MID FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 X NR 2 MID-FLAP DURING HMV SHOP INSPECTION WAS FOUND TO HAVE CORROSION IN THE O/B CARRIAGE SUPPORT FITTING, IN THE TOP I/B AND O/B THRUST RETAINER BOLT HOLES. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950602005631995060200563NM 1995 6 2 DL72S952103 119950414A5753652163261 SPAR BOEING727 727232 1384082NM NR 2 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 X NR 2 MID-FLAP DURING HMV SHOP WAS FOUND TO HAVE CRACK IN THE AFT SPAR RAIL AT THREE SPOTS, AT 19, 33, AND 50 FROM I/B END. REPAIRED PER SRM 57-52-0. 2L73 4F A3WE 19950602005641995060200564NM 1995 6 2 DL72S952105 119950411A5753652163234 SKIN BOEING727 727232 1384082NM NR 3 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AT HMV, SHOP INSPECTION, NR 3 MID-FLAP WAS FOUND WITH LOWER AFT SKIN PANEL (COVE SKIN) CRACKED AT CUT-OUT 32 INCHES FROM THE IB END. REPAIR DOUBLER WAS INSTALLED AND REPAIR WAS ACCOMPLISHED PER MM 57520, PAGE 819. 2L73 4F A3WE 19950602005651995060200565NM 1995 6 2 DL72S952106 119950417A5753652163234 DOUBLERS BOEING727 727232 1384082NM NR 3 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 AFT LOWER CHORD HAS TWO CRACKED DOUBLERS 23 AND 32 FROM IB END OF NR 3 MID-FLAP PANEL. SPLICED IN NEW SECTION OF AFT CHORD PER MM 57-52-0. FOUND AT HMV, SHOP VISIT. 2L73 4F A3WE 19950602005661995060200566NM 1995 6 2 DL72S952107 119950411A5753652163234 CHORD BOEING727 727232 1384082NM NR 3 MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 LOWER AFT CHORD IS CRACKED 55 INCHES FROM IB END OF NR 3 MID-FLAP. CHORD WAS REPAIRED PER MM 57-52-0. DAMAGE FOUND AND REPAIRED AT HMV SHOP VISIT. 2L73 4F A3WE 19950602005671995060200567NM 1995 6 2 DL72S952108 119950430A5311 FRAME BOEING727 727232 1384082NM FS 720 DOUBLE DRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND FS 720B FUSELAGE FRAME WITH DOUBLE DRILLED HOLE JUST INBOARD OF STRINGER 4R. REMOVED DAMAGED SECTION OF FRAME AND SPLICED IN REPAIR PER SRM 53-10-4 FIG 26. 2L73 4F A3WE 19950602005681995060200568NM 1995 6 2 DL72S952111 119950429A5754 RIBS BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 UNK RIB CRACKED NR 2 SLAT O/B ACTUATOR MARKED NR 11 LOWER AFT CORNER. RIB CRACKED NR 2 SLAT I/B ACTUATOR MARKED NR 12 LOWER AFT CORNER. REMOVED DOUBLER AND INSTALLED NEW DOUBLER PER MM 57-54-0 FIG 805. REMOVED DOUBLER FABRICATED NEW DOUBLER PER MM 57-54-0 PAGE 804. DAMAGE FOUND AND REPAIRED DURING HMV. 2L73 4F A3WE 19950602005691995060200569NM 1995 6 2 DL72S952131 119950506A532065175172 ANGLE BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11541DA 22387 THE RT TORQUE BOX FORWARD TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE AFT TRANSVERSE BEAM WAS ALSO FOUND CRACKED. THIS DAMAGED AREA OF THE TORQUE BOX IS THE SUBJECT OF S/B 53-0129. REPAIRS WILL REPLACE THE DAMAGED GUSSET ANGLE AND THE UPPER TRANSVERSE BEAM IN ACCORDANCE WITH THE S/B. 2L73 4F A3WE 19950602005701995060200570NM 1995 6 2 DL72S952132 119950515A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11536DA 22049 ONE-HALF INCH CRACK NR 2 SLAT NOSE RIB ANGLE O/B OF ACTUATOR ATTACH. REPAIRED PER MM 57-54-0. FOUND AT A-2 LETTER CHECK. 2L73 4F A3WE 19950602005711995060200571NM 1995 6 2 DL72S952133 119950515A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11536DA 22049 DOUBLER CRACKED FOR FLANGE UNDER ANTI ICE DUCT FOR NR 2 SLAT. FOUND DURING A-2 LTR CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950602005721995060200572NM 1995 6 2 DL72S952134 119950516A5713 STRINGER BOEING727 727232 1384082NM WS 656.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, RT WING STA 656.5, FOUND STR 9 CRACKED JUST OUTBOARD OF BOLT HOLE. REPAIRED PER MM 57-13-0 FIG 802. 2L73 4F A3WE 19950602005731995060200573NM 1995 6 2 DL72S952250 119950524A5521657278420 SPAR BOEING727 727232 1384082NM RT ELEV OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 OVERSIZED HOLES WERE FOUND IN THE REAR SPAR AND SKIN. THE SPAR WAS REPAIRED PER SRM 55-20-1 AND THE SKIN WAS REPAIRED PER SRM 55-20-3, FOR THE RIGHT ELEVATOR AT HMV. 2L73 4F A3WE 19950602005741995060200574NM 1995 6 2 DL72S952265 119950525A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11475DA 20752 FOUND DURING D-2 LETTER CHECK - 1 INCH CRACK AT SKIN WHERE NR 4 JACKSCREW FAIRING BUTTS. REPAIRED PER SRM 53-50-3 FIG 2. 2L73 4F A3WE 19950602005751995060200575NM 1995 6 2 DL72S952266 119950525A5753 LE SKIN BOEING727 727232 1384082NM NR 3 FOREFLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11475DA 20752 FOUND DURING D-2 LETTER CHECK - NR 3 T/E FOREFLAP LEADING EDGE SKIN DAMAGED. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950602005761995060200576NM 1995 6 2 DL72S952313 119950514A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV FOUND NR 7 LE SLAT RIB CRACKED 2ND FROM OUTBOARD END. INSTALLED DOUBLER AND STOPPED DRILL CRACK PER M/M 57-40-0 PG 819. 2L73 4F A3WE 19950602005771995060200577NM 1995 6 2 DL72S952314 119950514A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV FOUND NR 7 L/E SLAT RIB IB OF TAI DUCT CRACKED. INSTALLED DOUBLERS PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950602005781995060200578NM 1995 6 2 DL72W952130 119950509A533065545771 SKIN BOEING727 727247 138408FNM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112810W 20648 DURING LETTER CHECK, FOUND LOWER FUSELAGE SKIN AT FS 720 BETWEEN STR 28L AND 28R WITH CORROSION DAMAGE THAT REQUIRED AN 8.5 INCH X 3 INCH SKIN CUT-OUT. AN EXTERNAL DOUBLER WAS INSTALLED PER DL ERA 301729-14 AD. 2L73 4F A3WE 19950602005791995060200579NM 1995 6 2 DL73E952264 119950523A55126573783519 SKIN BOEING737 737247 138448DNM LT HORIZ STAB LECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11244WA 23518 DURING SHOP INSPECTION, THE LEFT HORIZONTAL STABILIZER LEADING EDGE PANEL WAS FOUND CRACKED. REPAIRED PER SRM 55-10-3. 2L72 4F A16WE 19950602005801995060200580NM 1995 6 2 DL757951880 119950504A5754114N4005177A TE WEDGE BOEING757 757232 1384965NM LT LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 LEFT WING SLAT PANEL TRAILING EDGE WEDGE WAS FOUND WITH HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950602005811995060200581NM 1995 6 2 DL757951894 119950503A5754114N4004151 TE WEDGE BOEING757 757232 1384965NM NR 3 SLAT DAMAGED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11620DL 22910 LEFT WING NR 5 SLAT PANEL TRAILING EDGE WEDGE WAS FOUND WITH DENTS FROM HAIL. REPLACED T/E WEDGE PER SRM 57-54-02. 2L72 4F RTA2NM 19950602005821995060200582NM 1995 6 2 DL757951968 119950502A5754114N4005158 TE WEDGE BOEING757 757232 1384965NM LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11651DL 24391 DURING SHOP INSPECTION, 757 SLAT PANEL WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950602005831995060200583NM 1995 6 2 DL757952060 119950503A5755 SKIN BOEING757 757232 1384965NM NR 8 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 NR 8 SPOILER PANEL WAS FOUND WITH DAMAGE TO UPPER SURFACE FROM HAIL. REPAIRED SPOILER PER SRM 51-70-17. 2L72 4F RTA2NM 19950602005841995060200584NM 1995 6 2 DL757952061 119950503A5751 SKIN BOEING757 757232 1384965NM RT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 RIGHT WING AILERON UPPER SURFACE WAS FOUND WITH HAIL DAMAGE. REPAIRS WERE ACCOMPLISHED PER SRM 57-60-01. 2L72 4F RTA2NM 19950602005851995060200585NM 1995 6 2 DL757952062 119950503A5522 SKIN BOEING757 757232 1384965NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 RIGHT ELEVATOR SUSTAINED HAIL DAMAGE TO UPPER SURFACE. REPAIRS WERE ACCOMPLISHED PER SRM 55-20-01 PG 202 TABLE 1. 2L72 4F RTA2NM 19950602005861995060200586NM 1995 6 2 DL757952063 119950503A5753 SKIN BOEING757 757232 1384965NM LT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 LEFT WING AFT FLAP PANEL SUSTAINED HAIL DAMAGE TO UPPER SURFACE. REPAIRS WERE ACCOMPLISHED PER SRM 57-53-01 WITH REF TO SRM 51-70-05. 2L72 4F RTA2NM 19950602005871995060200587NM 1995 6 2 DL757952064 119950507A5315 FLOOR BEAM BOEING757 757232 1384965NM FS 345 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 DURING INSPECTION, FOUND FS 345 CABIN FLOOR BEAM WITH CORROSION ON THE UPPER CAP. REPAIRS WERE ACCOMPLISHED PER SRM 53-30-51 PG 217-219. 2L72 4F RTA2NM 19950602005881995060200588NM 1995 6 2 DL757952110 119950515A5754114N4002148A SKIN BOEING757 757232 1384965NM NR 10 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 UNK RIGHT WING NR 10 L/E SLAT SUSTAINED HAIL DAMAGE TO UPPER SURFACE OF T/E WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202. 2L72 4F RTA2NM 19950602005891995060200589NM 1995 6 2 DL757952129 119950516A5754114N4005157 SKIN BOEING757 757232 1384965NM NR 4 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 UNK DURING SHOP INSPECTION, RT WING NR 4 SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950602005901995060200590NM 1995 6 2 DL757952261 119950502A5350655446565 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11612DL 22819 RECEIVED RADOME INTO SHOP AND UPON INITIAL INSPECTION FOUND DELAMINATION AT 12, 9, AND 6 O'CLOCK POSITIONS AROUND STATIC STRIP INSERT HOLES. ALSO FOUND MOISTURE IN CORE OF RADOME. REMOVED INSIDE SKIN TO DRY CORE AND REPLACED DAMAGED CORE AT INSERT HOLES, THEN REPLACED INSIDE SKIN PER SRM 53-10-72. APPLIED EROSION BOOT AND PAINT AS PER PS 900-9-1-11, NR 05. RADOME PASSED TRANSMISSIVITY TEST WITH 90.6 PERCENT. RADOME PASSED FINAL INSPECTION AND SENT TO STOCK. 2L72 4F RTA2NM 19950602005911995060200591NM 1995 6 2 DL757952312 119950518A5754114N4003178A TE WEDGE BOEING757 757232 1384965NM NR 9 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 23614 DURING SHOP INSPECTION, DELAMINATION WAS FOUND ON THE T/E WEDGE OF A NR 9 SLAT. THE WEDGE WAS REPLACED PER SRM 54-43-02. 2L72 4F RTA2NM 19950602005921995060200592NM 1995 6 2 DL757952322 119950528A5754114N4003171 TE WEDGE BOEING757 757232 1384965NM NR 2 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11641DL 23995 T/E WEDGE DELAMINATED. COMPLIED WITH AD 90-23-06 PER SRM 57-54-02 FIG 202, FOR NR 2 L/E SLAT AT SHOP INSPECTION. 2L72 4F RTA2NM 19950602005931995060200593NM 1995 6 2 DL757952324 119950525A5754 SKIN 114N4004145 BOEING757 757232 1384965NM NR 3 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11641DL A10177 23995 TRAILING EDGE WEDGE DELAMINATED. REPLACED TRAILING EDGE WEDGE PER SRM 57-43-02 FIG. 202, DURING SHOP INSPECTION OF NR 3 L/E SLAT. 2L72 4F RTA2NM 19950602005951995060200595NM 1995 6 2 DL76E952109 119950515A7110015T043751 COWL BOEING767 767232 1385132NM NR 1 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11111DN 22223 UNK FOUND LWR CHANNEL, AFT END OF CORE COWL TO BE CRACKED. REPAIRED PER SRM 54-41-02 PG 217. FOUND AND REPAIRED AT SHOP INSPECTION. 2L72 4F RTA1NM 19950602005961995060200596NM 1995 6 2 DL76L952330 119950525A2121732591D FAN BOEING767 767332 1382001NM FWD EQUIP FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11177DN 25122 DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN FLIGHT DECK, THEN HAD STATUS MESSAGE FWD EQ. EXH. FAN. AND ASSOCIATED CB. 11P22 TRIPPED. ODOR QUICKLY DISSIPATED. FAN WAS REPLACED. 2L72 4F RTA1NM 19950602005971995060200597WP 1995 6 2 DLL10952104 119950506A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1023 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 X DURING SERVICE CHECK FOUND TOOLING DAMAGE ON STR 14 RT AT STA 1023. REPAIRED PER SRM 53-13-00 PG. 806. 2L73 4F A23WE 19950602005981995060200598WP 1995 6 2 DLL13952258 119950525A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 649-749 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT OVERHAUL THE SEAT TRACK AT STA 649-749, 1ST TRACK TO LEFT OF CENTER, WAS FOUND CORRODED. REPLACED SEAT TRACK PER SRM 5321-00 PG 836. 2L73 4F A23WE 19950602005991995060200599WP 1995 6 2 DLL13952301 119950510A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 1545-1665 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND SEAT TRACKS CORRODED AT STA 1545-1665 LBL 75. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950602006001995060200600WP 1995 6 2 DLL13952303 119950511A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 1763 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND CABIN FLOOR BEAM CORROSION AT F.S. 1763 AT RBL 52. REPAIRED BY REPLACING SECTION OF T CAP PER SRM 53-21-00 PG 823. 2L73 4F A23WE 19950602006011995060200601WP 1995 6 2 DLL13952304 119950511A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 298 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND CORROSION ON FLOOR BEAM AT FS 298 LBL 28. RII. CORRECTION: INSTALLED NEW T CAP ON NR 811. 2L73 4F A23WE 19950602006021995060200602WP 1995 6 2 DLL13952309 119950515A5330 SKIN DOUBLER LKHEED1011 10113851 5265010WP FS 328 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND .020 EDGE DOUBLER AT SKIN SPLICE BOTTOM LEFT OF STR 33 AT STA 328 CORRODED. FABRICATED NEW EDGE DOUBLER SEGMENT IAW SRM 53-31-00 PG 863 AND INSTALLED. 2L73 4F A23WE 19950602006031995060200603WP 1995 6 2 DLL13952310 119950515A5320 DOUBLER LKHEED1011 10113851 5265010WP FS 325 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND .020 BONDED DOUBLER CORRODED AT STA 325 RIGHT OF CENTERLINE. REMOVED DAMAGE SECTION OF EDGE DOUBLER AND INSTALLED REPAIR PER SRM 53-31-00 PG 863. 2L73 4F A23WE 19950602006041995060200604WP 1995 6 2 DLL13952323 119950512A5320 STRAP LKHEED1011 10113851 5265010WP FS 901-923 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FUSELAGE SKIN FAILSAFE STRAP WAS FOUND LIFTED AND CORRODED IN LOWER GALLEY FS 901 TO 923 STR 40 TO 45. REPAIRED STRAP AND CLEANED CORROSION PER SRM 53-31-00 FIG 804 AND 816. 2L73 4F A23WE 19950602006051995060200605WP 1995 6 2 DLL15952327 119950527A2450 WIRE LKHEED1011 10113853 5265020WP FWD CARGO SHORTED A ADALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11754DL 193Y1181 DURING LAYOVER, WHILE WORKING DEFERRED ITEM FOR TRIPPED GALLEY POWER BREAKERS, FOUND FWD GALLEY FEEDER WIRES BURNED BELOW FWD CARGO COMPARTMENT FLOOR. WIRES WERE DAMAGED BY RUBBING ON EDGES OF LIGHTNING HOLE BETWEEN PANEL 132CR AND THE CARGO FLOOR. THE CLAMP HOLDING THE WIRES WAS FOUND BROKEN. ALL THREE CABLES WERE FOUND COMPLETELY BURNED THROUGH. WIRE NR 567A8A, 568A8B, 569A8C. DAMAGED SECTIONS OF WIRE WERE REPLACED AND SECURED. 2L73 4F A23WE 19950602006061995060200606NM 1995 6 2 DLM88952256 119950524A5320 ANGLE DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11916DL 49591 OUTBD AFT MLG DOOR FRAME STRIKER CRACKED 1.50 INCH. FOUND DURING B-1 LTR CK. REPAIRED PER SRM 53-05 FIG 81A. 2L72 4F RTA6WE 19950602006071995060200607NM 1995 6 2 DLM88952325 119950528A3610 PNEUMATIC SYSTEM DOUG MD88 MD88 3023688NM CABIN ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11911DL 49542 DURING CRUISE, HAD SMOKE AND ODOR IN CABIN AFTER ANTI ICE WAS TURNED ON. DIVERTED TO TYS SMOKE DISSIPATED WHEN ANTI ICE WAS TURNED OFF. CHECKED APU AND ENGINE OIL QTY. FOUND NORMAL. PERFORMED DUCT BURN-OUT PROCEDURES, RETURNED TO SERVICE. 2L72 4F RTA6WE 19950602006081995060200608NM 1995 6 2 DLM88952326 119950528A56105887275501 WINDSHIELD 6172 DOUG MD88 MD88 3023688NM FLT DECK CRACKED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11927DA 49714 DURING CRUISE, CENTER WINDSHIELD DEVELOPED TWO CRACKS AND STARTED TO DELAMINATE. LANDED ATL. REPLACED WINDOW AND CONTROLLER, RETURNED TO SERVICE. 2L72 4F RTA6WE 19950602006091995060200609NM 1995 6 2 DLM88952328 119950526A494020008662 STARTER DOUG MD88 MD88 3023688NM APU OIL LEAK A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11976DL 53257 ON CLIMBOUT F/A REPORTED SMOKE ODOR IN CABIN, TURNED RT PACK OFF, SMOKE SEEMED TO DISSIPATE, RETURNED FLT TO PHL. FOUND OIL LEAK ON APU STARTER. ITEM WAS DEFFERRED PER MEL, ROR RETURN TO SERVICE, LATER STARTER WAS REPLACED, OPERATION NORMAL. 2L72 4F RTA6WE 19950602006101995060200610NM 1995 6 2 DLM88952331 119950525A29107936913842 HYD LINE DOUG MD88 MD88 3023688NM TAIL COMP FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11985DL 53312 DURING CRUISE, LOST RIGHT SYSTEM HYD QTY AND PRESS. LANDED MSY. FOUND HYDRAULIC LINE CHAFED THROUGH IN TAIL COMP. INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE. SUBSEQUENTLY, A PERMANENT LINE WAS INSTALLED. 2L72 4F RTA6WE 19950602006111995060200611NM 1995 6 2 DLM88952334 119950525A2910290051500 TUBE DOUG MD88 MD88 3023688NM RT HYD SYST LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11904DL 49535 DURING CRUISE, HAD LOSS OF RT SYSTEM HYDRAULIC QUANTITY. TURNED SYSTEM OFF, RETURNED ATL. RE-POWERED SYSTEM FOR LANDING, LOST ALL FLUID AND PRESSURE ON BRAKE APPLICATION, AND ROLL-OUT. FOUND RT HYD PRESSURE LINE LEAKING, INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE. PERMANENT LINE REPLACEMENT WAS SCHEDULED. 2L72 4F RTA6WE 19950602006121995060200612NM 1995 6 2 QXEA9500164 119950526A3234574205 SELECTOR VALVE DHAV DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09822PH1826218262 106 SEA - GEAR SELECTED DOWN, DOORS DIDN'T OPEN AND GEAR DIDN'T EXTEND. PERFORMED ALTERNATE GEAR EXTENSION AND GEAR EXTENDED. LANDED WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. REPLACED GEAR SELECTOR VALVE AND GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950602006131995060200613NM 1995 6 2 SCNA95121 119950529A3350S106 EEL BATTERIES BOEING727 7272J4 1384006NM COCKPIT DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 21438 OVERHEAD EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED BATTERIES IN COCKPIT EMERGENCY LIGHT AND UNIT TESTED GOOD PER MM 33-50-01. 2L73 4F RTA3WE 19950602006141995060200614NM 1995 6 2 SCNA95122 119950527A335090052 EEL POWER SUPPLY BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 LEFT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, EMERGENCY LIGHTS TEST GOOD. 2L73 4F RTA3WE 19950602006151995060200615NM 1995 6 2 SCNA95123 119950529A361065244419 DUCT BOEING727 727259 138408JNM NR 1 ENGINE CRACKED A SCNAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 GL15289SC 22475 NR 1 ENGINE FIRE WARNING INDICATOR ILLUMINATED DURING FLIGHT. ENGINE WAS SHUTDOWN, ONE FIRE BOTTLE WAS DISCHARGED AND FIRE WARNING CEASED. TEN MINUTES LATER FIRE WARNING RE-ILLUMINATED AND SECOND BOTTLE WAS DISCHARGED, FIRE WARNING LIGHT CEASED. FIRE WARNING LIGHT ILLUMINATED AND BELL CAME ON ABOUT SIX MORE TIMES BEFORE LANDING IN ICT. A CRACK WAS FOUND IN THE 8TH STAGE DUCT WITHIN THE FIXED COWL AREA. DUCT WAS REPLACED AND LEAK CHECKED AT TAKE-OFF POWER, NO LEAKS NOTED. 2L73 4F A3WE 19950602006161995060200616NM 1995 6 2 UPS203422 119950601A3350 EEL BOEING727 7271A7C 13840X2NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01935UP 20143 MAINTENANCE FOUND EMERGENCY LIGHTS FAILED TO TEST ON PRE-FLIGHT. REPLACED EMER. LIGHTS. 2L73 4F A3WE 19950602006171995060200617NM 1995 6 2 UPS203423 119950601A5730 SKIN BOEING727 72730C 1384009NM WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK MAINTENANCE FOUND CORROSION INSIDE BREATHER WEB ON SKIN SURFACE OF LOWER CENTER FUEL CELL. REPAIRED IAW E.O. B727-5710-7042A AND SRM 57-30-3. 2L73 4F A3WE 19950602006181995060200618NM 1995 6 2 UPS203424 119950601A5754651622611 FLAP BOEING727 72730C 1384009NM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP HAS CORROSION. REMOVED AND REPLACED NR 2 K-FLAP IAW M/M 27-81-01. 2L73 4F A3WE 19950602006191995060200619NM 1995 6 2 UPS203425 119950601A5754 CHANNEL BOEING727 72730C 1384009NM NR 2 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP O/B ACTUATOR SUPPORT CHANNEL CRACKED. INSTALLED FABRICATED PARTS IAW SRM 57-20-2, 51-20-1, 51-30-2, M/M 20-50-21. 2L73 4F A3WE 19950602006201995060200620NM 1995 6 2 UPS203426 119950601A575565C8067822 FITTING BOEING727 72730C 1384009NM NR 9 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01919UP 19012 WHILE IN SI CHECK MAINTENANCE FOUND NR 9 SPOILER SUPPORT FITTING CORRODED. REPLACED FITTING IAW SRM 51-30-2. 2L73 4F A3WE 19950602006211995060200621NM 1995 6 2 UPS203427 119950601A5330 SKIN BOEING727 72727C 138400JNM FS 1213 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01914UP 19246 WHILE IN PHL, MAINTENANCE FOUND AFT BODY SKIN CRACKED APPROX. STA 1213, LWR RIGHT SIDE JUST O/B OF GROUND PNEUMATIC CONN. DOOR. REPAIRED IAW SRM 53-30-3. 2L73 4F A3WE 19950609000011995060900001NM 1995 6 9 95ZZZM55 119950512A5311146T12804 FRAME BOEING767 767223 1385123NM CARGO DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - FRAME LOCATED AT THE FORWARD SIDE OF BULK CARGO DOOR CUTOUT WAS CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. FABRICATED AND INSTALLED DOUBLER USING .071 INCH 7075-T6. A PERMANENT REPAIR MUST BE ACCOMPLISHED WITHIN 18 MONTHS FROM MAY 12, 1995 OR WITH 3000 CYCLES FROM 7395 CYCLES, WHICHEVER COMES FIRST. APPROVED BY ENGINEERING PER MRB 767-920. 2L72 4F RTA1NM 19950609000021995060900002NM 1995 6 9 95ZZZM56 119950512A5320146T1204 T-CAP BOEING767 767223 1385123NM FS 1153 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - AFT CARGO T-CAP CHORD WAS CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED, PRIMED AND PAINTED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRG 767-925. 2L72 4F RTA1NM 19950609000031995060900003NM 1995 6 9 95ZZZM57 119950512A5315 FLOORBEAM BOEING767 767223 1385123NM FS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - FOUND FLOORBEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINE BLENDED AREA. FILLED BLEND OUTS WITH BMS5-92. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 .5 HARD STAINLESS STEEL. PRIMED AND PAINTED APPROVED BY ENGINEERING PER MRB 767-918. 2L72 4F RTA1NM 19950609000041995060900004NM 1995 6 9 95ZZZM58 119950512A5315141TS111 FLOORBEAM BOEING767 767223 1385123NM FS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - FOUND FLOORBEAM CORRODED. AFTER REMOVAL OF CORROSION FOUND DAMAGE BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREAS WITH BMS5-92. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 .5 HARD STAINLESS STEEL. PRIMED AND PAINTED, APPROVED BY ENGINEERING PER MRB767-917. 2L72 4F RTA1NM 19950609000051995060900005NM 1995 6 9 95ZZZM59 119950512A5320146T1205 T-CAP BOEING767 767223 1385123NM FS 1175 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - FOUND AFT CARGO FLOOR T-CAP CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED, PRIMED AND PAINTED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MBB 767-924. 2L72 4F RTA1NM 19950609000061995060900006WP 1995 6 9 95ZZZM60 119950501A32225910448531 STRUT DOUG DC9 DC982 3022082WP NLG LOW PRESS A ASAAO OTHER J WARNING INDICATION CLCLIMB 1 NM01936AS 49363 SEA - ON ARRIVAL OF FLT 443, CREW REPORTED THE LANDING GEAR HANDLE WOULD NOT GO TO RETRACT POSITION. HAD TO PUSH INTERLOCK BUTTON TO RAISE HANDLE. FOUND NOSE LANDING GEAR STRUT PRESSURE LOW AND TORQUE LINK APEX BOLT OVER TORQUED. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION AND RETORQUED APEX BOLT. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE ASAA9580108. 2L72 4F A6WE 19950609000071995060900007NM 1995 6 9 AALA950014H 119950511A5347143T521142 SEAT TRACK BOEING767 767323 1385205NM FS 772 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07381AN 25450 FOUND CORROSION ON INBOARD FLANGE OF SEAT TRACK LBL 1106 STATION 772. REPAIRED PER MRB 767-908 DATED 4/23/95. (M) 2L72 4F RTA1NM 19950609000081995060900008NM 1995 6 9 AALA950029H 119950517A5315111T50485 FLOORBEAM BOEING767 767323 1385205NM FS 902 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07382AN 25451 FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM. BLEND FLAP PEEN AND REFINISHED, APPROVED FOR SERVICE PER MRB 767-916, DATED 5/5/95. (M) 2L72 4F RTA1NM 19950609000091995060900009NM 1995 6 9 AALA950030H 119950517A5315141T511 FLOORBEAM BOEING767 767223 1385123NM FS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 FOUND CORROSION ON TOP FLANGE OF FLOORBEAM. BLENDED TREATED AND FILLED AREA. INSTALLED REPAIR STRAP. APPROVED PER MRB 767-917. (M) 2L72 4F RTA1NM 19950609000101995060900010NM 1995 6 9 AALA950031H 119950517A5311146T1204 FRAME BOEING767 767223 1385123NM FS 1153 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - FOUND CORROSION ON INNER CHORD OF FRAME AT STATION 1153. UPPER CHORD AT RBL 7 AND LOWER CHORD AT LBL 7. BLENDOUTS EXCEED SRM LIMITS. BLENDED AND REFINISHED AREAS. APPROVED FOR SERVICE PER MRB 767-925. (M) 2L72 4F RTA1NM 19950609000111995060900011NM 1995 6 9 AALA950748 119950426A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW076835 20188 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRING AT FORWARD AREA OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950609000121995060900012NM 1995 6 9 AALA950784 119950502A326063200036 SWITCH BOEING727 727223 1384074NM RT MLG DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07701AA 22459 MIA - FLT 0480 - AFTER TAKEOFF, WHEN LANDING GEAR RETRACTED, RT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME RESULTS. AIRCRAFT RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED RT MAIN LANDING GEAR DOOR LIGHT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950609000131995060900013NM 1995 6 9 AALA950807 119950502A3350GMA15 EEL FUSE BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07385AM 27059 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 20H AND 21H INOPERATIVE. REPLACED FUSE AT EMERGENCY EXIT LIGHT POWER PACK FOR PASSENGERS SEATS 20H AND 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000141995060900014NM 1995 6 9 AALA950835 119950505A3350233T321033 EEL CONTROL PNL BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07372AA D00857 25199 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS COME ON WITH SWITCH IN DISARM POSITION. REPLACED CONTROL PANEL. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000151995060900015EU 1995 6 9 AALA950836 119950506A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW077062A 474 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FRONT OF R1 DOOR INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950609000161995060900016NM 1995 6 9 AALA950838 119950506A3350A3060719101 EEL STRIP BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07689AA 25731 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHTS ON AFT RIGHT DOOR INOPERATIVE. REPLACED LOWER AFT FORWARD EMERGENCY FLOOR PATH LIGHT STRIP MODULE. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950609000171995060900017NM 1995 6 9 AALA950844 119950508A3230AAP2448A ACCESSORY UNIT BOEING727 727223 1384074NM LT MLG DEFECTIVE A AALAK NONE J WARNING INDICATION TOTAKEOFF 1 SW07896AA 22012 SJU - FLT 2009 - AFTER TAKEOFF LEFT MAIN LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. LANDED SJU WITHOUT INCIDENT. REPLACED LANDING GEAR ACCESSORY UNIT. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2L73 4F A3WE 19950609000181995060900018NM 1995 6 9 AALA950845 119950508A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE ON RIGHT SIDE OF BUSINESS CLASS. RESECURED LOOSE EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 12HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000191995060900019WP 1995 6 9 AALA950846 119950508A3350 EEL WIRE DOUG DC9 DC982 3022082WP TAILCONE BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW077509 49803 DFW - DURING OVERNIGHT CHECK, FORWARD CEILING EMERGENCY EXIT LIGHT IN TAILCONE INOPERATIVE. REPAIRED WIRING TO FORWARD CEILING EMERGENCY EXIT LIGHT IN TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950609000201995060900020NM 1995 6 9 AALA950847 119950508A33501722331 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07377AN 25446 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT SEAT 34H. RESECUERD LOOSE EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT LEG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000211995060900021NM 1995 6 9 AALA950848 119950508A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW076835 20188 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950609000221995060900022EU 1995 6 9 AALA950864 119950510A3350A3060719102 EEL STRIP FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071411G 11369 BNA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 12 AND 16 INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 12 AND 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950609000231995060900023NM 1995 6 9 AALA950904 119950513A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 7H THROUGH 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY PASSENGER SEAT ROW 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000241995060900024NM 1995 6 9 AALA950907 119950512A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07353AA 24034 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RIGHT AISLE IN BUSINESS CLASS AND MAIN CABINS INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR IN BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950609000251995060900025NM 1995 6 9 AALA950924 119950517A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07645AA 24603 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 1 THROUGH 6 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 1. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950609000261995060900026NM 1995 6 9 ASAA9510047 119950427A33506013211 EEL BATTERY PACK BOEING737 737290C 138448VNM AFT EVAC SLIDE DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING D-CHECK, THE AFT EMERGENCY EXIT EVACUATION SLIDE LIGHTS WERE FOUND INOPERATIVE. REPAIRED CHAFED WIRING AND REPLACED BATTERY PACK, SLIDE LIGHTS ILLUMINATED NORMALLY. (M) 2L72 4F A16WE 19950609000271995060900027NM 1995 6 9 ASAA9510048 119950427A3350873203041 EEL TRANSMITTER BOEING737 737290C 138448VNM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS CYCLED ON AND OFF. REPLACED FORWARD EMERGENCY EXIT FLOOR TRACK LIGHT TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950609000281995060900028NM 1995 6 9 ASAA9510049 119950430A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 ANC - DURING MAINTENANCE CHECK, THE SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950609000291995060900029NM 1995 6 9 ASAA9510050 119950502A335020131A EEL BATTERY BOEING737 737298C 1384490NM MAIN CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - FLT 42 - ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTING ILLUMINATED AND COULD NOT BE TURNED OFF. REPLACED BATTERY IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950609000301995060900030NM 1995 6 9 ASAA9510052 119950509A3350303 EEL LAMP BOEING737 737210C 1384459NM CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - FLOOR TRACK EMERGENCY LIGHT 18D INOP AND COVER MISSING. MAINTENANCE RELAMPED AND REPLACED COVER. (M) 2L72 4F A16WE 19950609000311995060900031NM 1995 6 9 ASAA9520051 119950509A5753657194038 REAR SPAR BOEING737 737210C 1384459NM RT TE MID FLAP CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01743AS431713016 21821 SEA - DURING C-CHECK, A GOUGE AND CRACK WAS IDENTIFIED IN THE AFT FLANGE OF THE REAR SPAR UPPER CHORD, LOCATED APPROXIMATELY 30 INCHES OUTBOARD FROM THE INBOARD END OF THE TRAILING EDGE MID FLAP (P/N 657194038). REPAIRED BY INSTALLATION OF AN ANGLE DOUBLER PER EA 5750-01159 AS APPROVED BY BOEING TELEX ASA-SEA-95-0325RR, DATED MAY 3, 1995. (M) 2L72 4F A16WE 19950609000321995060900032NM 1995 6 9 ASAA9540020 119950429A3350BPS73 EEL BATT CHARGER BOEING737 7374Q8 NM CABIN MALFUNCTIONED A ASAAK NONE L NO TEST UKUNKNOWN 1 NM01779AS 25111 SEA - SEVERAL EMERGENCY LIGHTS IN AFT CABIN CAME ON FOR A FEW SECONDS, THEN WENT OFF FOR A FEW SECONDS. THIS HAPPENED THREE TIMES. MAINTENANCE REPLACED BOTH AFT CABIN BATTERY PACKS. (M) 2L72 4F RTA16WE 19950609000331995060900033WP 1995 6 9 ASAA9580101 119950426A33506011779 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK,THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950609000341995060900034WP 1995 6 9 ASAA9580102 119950428A335060030451 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000351995060900035WP 1995 6 9 ASAA9580103 119950428A335060030451 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 20 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000361995060900036WP 1995 6 9 ASAA9580104 119950428A335060030451 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN AFT GALLEY WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000371995060900037WP 1995 6 9 ASAA9580105 119950428A335060030451 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000381995060900038WP 1995 6 9 ASAA9580106 119950429A335060030451 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950609000391995060900039WP 1995 6 9 ASAA9580107 119950501A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01936AS 49363 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000401995060900040WP 1995 6 9 ASAA9580108 119950501A323039632951N TORQUE LINK BOLT DOUG DC9 DC982 3022082WP NLG OVER TORQUED A ASAAO OTHER J WARNING INDICATION CLCLIMB 1 NM01936AS2804813699 49363 SEA - ON ARRIVAL OF FLT 443, CREW REPORTED THE LANDING GEAR HANDLE WOULD NOT GO TO RETRACT POSITION. HAD TO PUSH INTERLOCK BUTTON TO RAISE HANDLE. FOUND NOSE LANDING GEAR STRUT PRESSURE LOW AND TORQUE LINK APEX BOLT OVER TORQUED. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION AND RETORQUED APEX BOLT. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE 95ZZZM60. 2L72 4F A6WE 19950609000411995060900041 1995 6 9 ASAA9580109 419950503A2565D29985107 EVAC SLIDE DOUG DC9 DC982 3022082WP L2 DOOR FAILED A AASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS195808289 49235 SEA - DURING TRAINING DEMONSTRATION, THE L2 DOOR EMERGENCY EVACUATION SLIDE WAS DEPLOYED. AS THE SLIDE BEGAN TO DEPLOY, A RUPTURE OCCURRED AT THE UPPER END OF THE SLIDE. THE SLIDE CONTINUED TO DEPLOY BUT HAD A COMPLETE AIR LOSS. REPLACED THE L2 DOOR EMERGENCY EVACUATION. (M) 2L72 4F A6WE 19950609000421995060900042WP 1995 6 9 ASAA9580110 119950504A33506011779 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS 49364 SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609000431995060900043WP 1995 6 9 ASAA9580113 119950516A335014597101 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950609000441995060900044NM 1995 6 9 AWXA9500284 119950510A335020131A EEL BATT CHARGER BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28160AW 23782 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 5 THROUGH 11. REMOVED AND REPLACED OVERHEAD BATTERY CHARGER AT ROW 13, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000451995060900045EU 1995 6 9 AWXA9500285 119950511A3350 EEL WIRE AIRBUS320 A320231 3930325EU CABIN SHORTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28621AW 053 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED SHORTED WIRES AT ROW 17, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950609000461995060900046NM 1995 6 9 AWXA9500287 119950512A3350900835A EEL BATT CHARGER BOEING737 737222 1384473NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28144AW 19074 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950609000471995060900047NM 1995 6 9 AWXA9500288 119950514A3350 EEL ASSY BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL EMERGENCY TRACK LIGHTS BROKEN. REPAIRED BROKEN FLOOR LIGHTING, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950609000481995060900048NM 1995 6 9 AWXA9500297 119950515A335058783 EEL WIRE STRIP BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 13 THROUGH 15 FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED SECTIONAL WIRE STRIP FROM CABIN SIDE WALL TO FLOOR TRACK, OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950609000491995060900049NM 1995 6 9 AWXA9500298 119950516A3350 EEL CONNECTOR BOEING737 7372Q8 138448KNM CABIN DIRTY A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28137AW 23148 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS IN AFT SECTION OF AIRCRAFT INOPERATIVE. REMOVED AND CLEANED BATTERY PACK CONNECTOR AT ROW 18. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000501995060900050NM 1995 6 9 AWXA9500299 119950518A3350 EEL HARNESS BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 BACK. RECONNECTED HARNESS PINS TO LIGHT AT ROW 14, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000511995060900051NM 1995 6 9 AWXA9500302 119950520A3350S106 EEL BATT PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28183AW 22650 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000521995060900052NM 1995 6 9 AWXA9500303 119950520A3350900835A EEL BATTERY BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28185AW 22652 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT OVERWING, L2 DOOR AND R2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000531995060900053NM 1995 6 9 AWXA9500305 119950521A3350900835A EEL BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 13 THROUGH 17 RIGHT SIDE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950609000541995060900054NM 1995 6 9 AWXA9500306 119950521A3350900835A EEL BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD CEILING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950609000551995060900055NM 1995 6 9 AWXA9500307 119950521A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28315AW 23734 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROWS 3 THROUGH 11 EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 3. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000561995060900056NM 1995 6 9 AWXA9500309 119950522A335020121 EEL BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950609000571995060900057WP 1995 6 9 CKSA95021 119950509A3260 SWITCHES DOUG DC8 DC851 3021920WP LANDING GEAR DIRTY A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23804CK52448 45689 YIP-PHL - UPON INITIAL GEAR RETRACTION GEAR AND DOOR INDICATOR LIGHTS REMAINED ILLUMINATED. AFTER SECOND GEAR RETRACTION LIGHTS EXTINGUISHED. OPERATIONS NORMAL, UPLATCH CHECK GOOD. INSPECTED LANDING GEAR, FOUND NO DEFECTS. LUBED ALL LANDING GEARS, CLEANED SWITCHES AND CANNON PLUGS. INSTALLED GEAR PIN, CYCLED GEAR HANDLE SEVERAL TIMES. GROUND OPS NORMAL PER MM 32-60. (M) 2L74 4F 4A25 19950609000581995060900058WP 1995 6 9 CKSA95022 119950510A3260H2024B SWITCH DOUG DC8 DC851 3021920WP MLG DOOR MALFUNCTIONED A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23804CK52450 45689 YIP-PHL - ON GEAR RETRACTION GEAR UNSAFE AND MAIN GEAR DOOR LIGHTS REMAINED ILLUMINATED. RECYCLED THE GEAR. REMOVED AND REPLACED MAIN LANDING GEAR DOOR SWITCH, OPS CHECK GOOD IAW MM 32-60-0. (M) 2L74 4F 4A25 19950609000591995060900059WP 1995 6 9 9508769140 119950526A5350 RELEASE MECH DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01930RC 45729 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950609000601995060900060WP 1995 6 9 9508779916 119950526A5350 RELEASE MECH DOUG DC9 DC932 3022066WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01949N 47566 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS AND THAT THE UPPER LEFT AND RIGHT LATCHES WOULD NOT RELEASE THE TAILCONE. ALSO, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE CLIPS AND RE-RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950609000611995060900061WP 1995 6 9 9508789880 119950530A5350 LATCHES DOUG DC9 DC951 3022051WP TAILCONE OUT OF RIG A NWAAK NONE O OTHER ININSP/MAINT 1 GL01675MC 47651 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. RERIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950609000621995060900062WP 1995 6 9 9508799915 119950526A5230 FITTING DOUG DC9 DC931 3022065WP AFT CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING PERIODIC CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 3 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950609000631995060900063WP 1995 6 9 9508809989 119950529A5313 LONGERON DOUG DC9 DC931 3022065WP FS 937-945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30, FS 937 TO 945. REPAIRED LONGERON PER EA 99-094824. 2L72 4F A6WE 19950609000641995060900064WP 1995 6 9 9508819915 119950530A5320 FITTING DOUG DC9 DC931 3022065WP KEEL BEAM CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING PERIODIC CHECK, FOUND A CRACK IN THE LONGERON 30 END FITTING IN THE KEEL AREA. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950609000651995060900065WP 1995 6 9 9508829995 119950530A5751 STUDS DOUG DC9 DC931 3022065WP LT AILERON CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE,FOUND CORROSION ON THE LEFT WING AILERON A BRACKET ATTACH STUDS FOR HINGES NR 1 TO NR 4. REPLACED STUDS PER MM 20-16-0. 2L72 4F A6WE 19950609000671995060900067WP 1995 6 9 SCNA95124 119950530A2560541589001 TEST LAMP DOUG DC10 DC1010 3022110WP R 2 DOOR SLIDE FAULTY A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 FOUND R-2 SLIDE BOTTLE INTEGRITY TEST INOPERATIVE. RELAMPED R-2 DOOR TEST MODULE AND SLIDE TESTED GOOD. 2L73 4F A22WE 19950609000681995060900068NM 1995 6 9 SCNA95125 119950601A261265602097 FIRE DET BOX BOEING727 727259 138408JNM NR 1 ENGINE FAULTY A SCNAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 GL15289SC 22475 DURING LANDING ROLL WHILE APPLYING REVERSE THRUST HAD NUMBER 1 ENGINE FIRE WARNING INDICATION. BLEW ONE FIRE BOTTLE AND SHUTDOWN ENGINE, FIRE WARNING INDICATION EXTINGUISHED. POST FLIGHT INSPECTION SHOWED NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE DETECTION WARNING BOX, SYSTEM OPS CHECKED GOOD. 2L73 4F A3WE 19950609000701995060900070NE 1995 6 9 95ZZZX2636 219950427A73142PR400BR05 PUMP PESCO DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN1 52008NE ENGINE FUEL DEFECTIVE A ELRAK NONE O OTHER ININSP/MAINT 1 AL0362469 697 PE110 1237 4217671 PILOT REPORTED EXCESSIVE FUEL CONSUMPTION. DETERMINED FUEL PUMP (ENGINE DRIVEN) TO BE DEFECTIVE. REPLACED FUEL PUMP WITH ZERO TSO UNIT. OPS CHECK SATISFACTORY. 1H71 3R3 R A806 5E1 19950609001861995060900186NM 1995 6 9 95ZZZW760 119950518A335030043213 EEL BOEING737 737317 138447PNM CABIN BROKEN B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 28219 23173 EMERGENCY EXIT LIGHTS ABOVE AFT ENTRY AND SERVICE DOORS HAVE BROKEN LENSES. REPLACED BOTH LIGHT ASSEMBLIES PER SRM 51-40-0. (W) 2L72 4F RTA16WE 19950609001871995060900187NM 1995 6 9 95ZZZW761 119950518A53306545775 SKIN BOEING737 737317 138447PNM FS 727 CRACKED B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 28219 23173 TWO CRACKS IN FUSELAGE SKIN BETWEEN FS 727B-727D, LONGERON 23R. REPAIRED SKIN PER DALFORT AVIATION XEA NR X2-53-114, REVISION 1. (W) 2L72 4F RTA16WE 19950609001881995060900188NM 1995 6 9 95ZZZW762 119950519A5320BAC1498156 SPLICE BOEING737 737317 138447PNM FS 907 CORROSION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 28219 23173 FS 907, STRINGER 23L SPLICE HEAVY CORROSION. REPLACED STRINGER SPLICE PER SRM 51-30-2. (W) 2L72 4F RTA16WE 19950609001891995060900189NM 1995 6 9 95ZZZW763 119950519A5315BAC1498100246 FLOORBEAM BOEING737 737317 138447PNM FS 344 CORROSION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 28219 23173 HEAVY CORROSION AT MAIN CABIN FLOORBEAM FS 344, BETWEEN LBL 65 TO RBL 10. REPAIRED FLOORBEAM PER SRM 51-70-12, PAGES 2-6. (W) 2L72 4F RTA16WE 19950609001901995060900190NM 1995 6 9 95ZZZW764 119950519A57526546455 SKIN BOEING737 737317 138447PNM LT AILERON TAB DELAMINATION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 LEFT AILERON TAB DELAMINATED ON UPPER AND LOWER SURFACES. REPAIRED TAB PER SRM 57-61-01. (W) 2L72 4F RTA16WE 19950609001911995060900191WP 1995 6 9 95ZZZW765 119950513A324441X15018 TIRE 95608591 DOUG DC9 DC951 3022051WP NR 2 WHEEL SEPARATED A A4JAK NONE O OTHER TOTAKEOFF 1 SO15919PJ 47663 FLT 220 - NR 2 MAIN TIRE BLEW ON TAKEOFF. REPLACED NR 1 AND NR 2 MAIN WHEEL ASSY. INSPECTED BRAKES AND FOUND TO BE OK. REPAIRED SMALL AREA OF LEFT FLAP IAW SRM. REPLACED LEFT MLG DOWNLOCK SWITCH. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A6WE 19950609001921995060900192WP 1995 6 9 95ZZZW766 119950511A3244H445X16520 TIRE 50043204 DOUG DC9 DC981 3022081WP RT MLG SEPARATED A A4JAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO15818SJ 48058 FLT 807 - NR 3 TIRE RECAP SEPARATED FROM TIRE CARCASS ON TAKEOFF. FOUND RIGHT FLAP DAMAGE AND ENGINE C-1 BLADE DAMAGE. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSY. REPLACED NR 3 AND NR 4 MAIN WHEEL BRAKES. REPAIRED RIGHT FLAP PANEL IAW SRM. REPLACED 14 ENGINE C-1 BLADES. REPLACED FRONT AND REAR ACCOUSTICAL FAN CASES. REPLACED RT GEAR DOWNLOCK SWITCH. ENGINE BORESCOPE REVEALED NO OTHER DEFECTS. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A6WE 19950609001931995060900193NE 1995 6 9 95ZZZW767 219950518A7230 NR 3 BEARING BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE CRACKED A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23853FT31626 19753 695755 ON ARRIVAL IN LAX, POST FLIGHT INSPECTION REVEALED OIL IN TAILPIPE ON NR 3 ENGINE. AFTER TROUBLESHOOTING, FOUND OIL LEAKING NR 3 BEARING HOUSING. AIRCRAFT THREE ENGINE FERRY TO SAT FOR ENGINE CHANGE. (W) 2L74 4F4 F A20WE E20EA 19950609001941995060900194NM 1995 6 9 95ZZZW768 119950519A528065B11668X DOOR BOEING747 747121 1384871NM RT MLG DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT84252 20347 RIGHT WING LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW BOEING SRM 51-40-02. TOTAL CYCLES 18,464. 2L74 4F A20WE 19950609001951995060900195NM 1995 6 9 95ZZZW769 119950519A528065B116681 DOOR BOEING747 747121 1384871NM LT MLG DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 LEFT WING LANDING GEAR LOWER OUTBOARD STRUT DOOR DELAMINATED. REPAIRED IAW WITH BOEING SRM 51-40-09. TOTAL CYCLES 18,464. 2L74 4F A20WE 19950609001961995060900196NM 1995 6 9 95ZZZW770 119950525A2910BACU24L16 HYD UNION BOEING747 747124 1384874NM NR 1 PYLON CRACKED A P5CAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23855FT 19733 FLT 9601 - MIA-ASU - AIRCRAFT EXPERIENCED RAPID LOSS OF FLUID FROM HYDRAULIC SYSTEM 1. DEPRESSURIZED ENGINE DRIVEN PUMP. DIVERTED TO CCS. GEAR EXTENSION AND LANDING NORMAL. FOUND UNION FITTING CRACKED INTERIOR OF THE PYLON AT BULKHEAD MID PYLON. REPLACED FITTING, LEAK CHECK OK. (W) 2L74 4F A20WE 19950609001971995060900197NM 1995 6 9 95ZZZW771 119950526A5400 DOUBLER BOEING747 747122 1384872NM NAC STA 180 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT69304 19753 ON B-CHECK INSPECTION, FOUND CRACK IN DOUBLER PLATE NACELLE STATION 180, ON 4 PYLON INBOARD. INSTALLED REPAIR DOUBLER IAW SERVICE BULLETIN 54-2034 REV 4. TOTAL CYCLES 18,040. 2L74 4F A20WE 19950609001981995060900198NM 1995 6 9 95ZZZW772 119950526A575565B116281 PANEL BOEING747 747122 1384872NM NR 5 SPOILER DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 B-CHECK INSPECTION, LEFT WING TOP SIDE PANEL FORWARD AT NR 5 SPOILER DELAMINATED. REPAIRED IAW BOEING SRM 51-40-06. TOTAL CYCLES 18,040. 2L74 4F A20WE 19950609001991995060900199NM 1995 6 9 95ZZZW773 119950526A575565B0225041 TE PANEL BOEING747 747122 1384872NM NR 9 SPOILER TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 B-CHECK INSPECTION, RIGHT WING NR 9 SPOILER HAS A 6 INCH BY 5 INCH TEAR IN TRAILING EDGE 20 INCHES FROM INBOARD EDGE. REPAIRED IAW BOEING SRM 51-10-06 AND 57-50-05. TOTAL CYCLES 18,040. 2L74 4F A20WE 19950609002001995060900200EU 1995 6 9 C2XA95IA083 119950518A33507012210 EEL BULB AEROSPATR42 ATR42320 8680930EU CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0997841 280 IAH - DURING 2A CHECK INSPECTION, FOUND EMERGENCY LIGHT AT AFT RT FUSELAGE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2H72 4T RTA53EU 19950609002011995060900201WP 1995 6 9 CAL950306 119950420A5330 SKIN DOUG DC9 DC932 3022066WP BS 965 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753567383 47111 IAH - A .875 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 965R, THREE INCHES ABOVE L15. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 12B. (W) 2L72 4F A6WE 19950609002021995060900202WP 1995 6 9 CAL950309 119950419A215020495054 ACM DOUG DC9 DC982 3022082WP RIGHT OIL LEAK A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0972822191216569 49482 FLT NR 1529 - IAH - THE AIRCRAFT WAS RETURNED TO IAH FOR SMOKE IN CABIN AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT AIR CYCLE MACHINE LEAKING OIL. THE RIGHT AIR CYCLE MACHINE WAS REMOVED AND REPLACED. AN OPERATIONAL CHECK OF THE RT AIR CYCLE MACHINE WAS NORMAL WITH NO LEAKS NOTED. (W) 2L72 4F A6WE 19950609002031995060900203WP 1995 6 9 CAL950311 119950422A256008256190001 SLIDE DOUG DC9 DC982 3022082WP L-1 DOOR FELL OFF A CALAK NONE O OTHER ININSP/MAINT 1 SW09578373139 49582 FLT NR 0274 - IAH - L-1 DOOR SLIDE FELL OFF. MAINTENANCE REINSTALLED PRIOR TO DISPATCH. NO FURTHER DISCREPANCIES. OK FOR DEPARTURE. (W) 2L72 4F A6WE 19950609002041995060900204WP 1995 6 9 CAL950318 119950424A3350 EEL BATTERY PACK DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0937882 48027 FLT NR 0301 - EWR - ROW 15 AND 32 HAD OVERHEAD EMERGENCY LIGHT INOP. RELAMPED OVERHEAD LIGHTS, OPS CHECK GOOD. FLIGHT DEPARTED WITH NO FURTHER OCCURRANCE. (W) 2L72 4F A6WE 19950609002051995060900205WP 1995 6 9 CAL950342 119950425A33107071 BALLAST DOUG DC10 DC1010 3022110WP COCKPIT FAILED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0968044 46903 FLT NR 6325 - NRT - DURING FLIGHT, SMOKE WAS OBSERVED IN THE COCKPIT. COCKPIT DOME LIGHT CIRCUIT BREAKER POPPED OUT AND THE SMOKE QUICKLY DISSIPATED. THE DOME LIGHTS WERE DEACTIVATED AND PROBLEM TRACED TO BALLAST. REMOVED AND REPLACED BALLAST ALL LIGHTS CHECK GOOD. (W) 2L73 4F A22WE 19950609002061995060900206WP 1995 6 9 CAL950345 119950205A2120 BRACKET DOUG DC9 DC932 3022066WP LT AIR COND BAY BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914534 47110 FLT NR 1859 - IAH - AFTER TAKEOFF TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON, RETURNED TO IAH. 'NO' EMERGENCY WAS DECLARED. FOUND DUCT LEFT SIDE OF AIRCRAFT A-C BAY ATTACHMENT BROKEN. REPAIRED BRACKET PER DC-9 OVERHAUL MANUAL 20-10-9. OPS CHECK GOOD. (W) 2L72 4F A6WE 19950609002071995060900207WP 1995 6 9 CAL950350 119950405A2820770400 VENT VALVE DOUG DC9 DC932 3022066WP LT WING FUEL MALFUNCTIONED A CALAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 SW0912532 45791 FLT NR 1454 - IAH - ON CLIMB-OUT FUEL VENTING OVERBOARD OUT LEFT WING. AIRCRAFT RETURNED TO IAH. FOUND THAT CLIMB VENT VALVE NEEDED TO BE REPLACED. REMOVED AND REPLACED VENT VALVE P/N 770400. FILLED RT WING TO 9300 LBS AND OPS CHECK GOOD. (W) 2L72 4F A6WE 19950609002081995060900208WP 1995 6 9 CAL950374 119950509A3350008400013012 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916883 48073 FLT NR 0344 - EWR - INSPECTION FOUND THE OVERHEAD EMERGENCY CEILING LIGHTS INOPERATIVE IN FIRST CLASS SECTION. THE BATTERIES FOR THE OVERHEAD LIGHTS IN FIRST CLASS WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950609002091995060900209WP 1995 6 9 CAL950375 119950509A3350 EEL BATT DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916883 48073 FLT NR 0344 - EWR - INSPECTION FOUND THE OVERHEAD EMERGENCY CEILING LIGHTS IN AFT CABIN INOPERATIVE. THE BATTERIES AND POWER SUPPLY CHARGER FOR THE OVERHEAD LIGHTS IN AFT CABIN WERE REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950609002101995060900210NM 1995 6 9 CAL950377 119950510A5320 SHEAR TIE BOEING727 727227 1384078NM FS 400 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A 1 INCH CRACK IN SHEAR TIE AT STATION 400 BETWEEN STRINGERS 27-28L. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (W) 2L73 4F A3WE 19950609002111995060900211NM 1995 6 9 CAL950378 119950510A5320 ANGLE BOEING727 727227 1384078NM FS 1183 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A .5 INCH CRACK IN AFT ENTRY DOOR SILL ANGLE AT STATION 1183 (BELOW FLOOR) ON BOTH SIDES, RBL 15 AND LBL 15. THE DOOR SILL ANGLE WAS REMOVED, A NEW DOOR SILL ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (W) 2L73 4F A3WE 19950609002121995060900212NM 1995 6 9 CAL950379 119950510A5720 WEB BOEING727 727227 1384078NM WS 139 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND RIGHT WING CENTER INBOARD OF STATION 139 WITH CRACKS IN WEBBING AROUND FASTENER HOLES. THE CRACKS WERE .8 INCH IN LENGTH. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-6. (W) 2L73 4F A3WE 19950609002131995060900213NM 1995 6 9 CAL950380 119950510A5712 RIB BOEING727 727227 1384078NM WS 738 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF RT RIB LOWER FORWARD ATTACH HOLE AT WS 738. THE CRACK WAS STOP DRILLED. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W) 2L73 4F A3WE 19950609002141995060900214NM 1995 6 9 CAL950381 119950510A5754 INTERCOSTAL BOEING727 727227 1384078NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND THE NR 6 SLAT INTERIOR WITH A CRACK IN EACH OF TWO INTERCOSTALS AT INBOARD SLAT TRACK ATTACH FITTING. THE CRACKS WERE 1.2 INCHES LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (W) 2L73 4F A3WE 19950609002151995060900215NM 1995 6 9 CAL950382 119950510A5730 SKIN BOEING727 727227 1384078NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A .9 INCH CRACK IN LEFT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUTOUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (W) 2L73 4F A3WE 19950609002161995060900216NM 1995 6 9 CAL950383 119950510A5754 INTERCOSTAL BOEING727 727227 1384078NM NR 2 SLAT TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT SLAT TRACK ATTACH FITTING AREA OF NR 2 SLAT INBOARD SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-02. (W) 2L73 4F A3WE 19950609002171995060900217NM 1995 6 9 CAL950384 119950510A5321 FLOORBOARD BOEING727 727227 1384078NM FS 940 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND A 1.5 INCH CRACK AT MLG PRESSURE FLOOR, STATION 940R. THE CRACK WAS APPROXIMATELY 12 INCHES INBOARD OF OUTSIDE EDGE OF THE FLOOR. THE CRACKED FLOORBOARDS WERE REMOVED AND REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (W) 2L73 4F A3WE 19950609002181995060900218NM 1995 6 9 CAL950385 119950510A5754 RIB BOEING727 727227 1384078NM NR 3 LE SLAT CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777353625 21045 GSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-2. (W) 2L73 4F A3WE 19950609002191995060900219WP 1995 6 9 CAL950386 119950512A2420947F9452 PANEL DOUG DC9 DC982 3022082WP GEN CONTROL INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW091080118631 49127 FLT NR 0679 - EWR - WHILE OPERATING THE APU, WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE. THE APU GENERATOR FEEDER FAULT LIGHT ILLUMINATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU GENERATOR CONTROL UNIT AT FAULT. THE APU GENERATOR CONTROL UNIT WAS REMOVED AND REPLACED. (W) 2L72 4F A6WE 19950609002201995060900220WP 1995 6 9 CAL950390 119950516A335041B004AD073 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916884 48074 FLT NR 0344 - EWR - INSPECTION FOUND THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN AT ROWS 9-14 AND 23-27 INOPERATIVE. THE BATTERIES FOR THREE BATTERY PACKS WERE REPLACED AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (W) 2L72 4F A6WE 19950609002211995060900221WP 1995 6 9 CAL950391 119950516A3350 EEL WIRE DOUG DC9 DC981 3022081WP CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916884 48074 FLT NR 0344 - EWR - INSPECTION FOUND THE EMERGENCY EXIT LIGHT ON THE OUTSIDE WALL OF AFT LEFT LAV INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT THE EXIT LIGHT. THE WIRE WAS REMOVED AND REPLACED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (W) 2L72 4F A6WE 19950609002221995060900222NM 1995 6 9 CKSA95023 119950505A31507400111 AURAL WARN BOEING747 747146 NM LT COCKPT MALFUNCTIONED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23701CK78491 19725 PHNL - PILOTS GREEN GEAR DOWN LIGHT STAYS ILLUMINATED WITH GEAR RETRACTED. LANDING GEAR EXTENSION AND RETRACTION ARE NORMAL VIA F/E LANDING GEAR ANNUNCIATOR PANEL. REMOVED AND REPLACED AURAL WARNING MODULE M470 PER BMM 31-26-02. REPAIRED THE AURAL WARNING HORN ALSO REPAIRED THE PILOTS GEAR LIGHT. OPS CHECK GOOD. (W) 2L74 4F A20WE 19950609002231995060900223NE 1995 6 9 TAOA059507 219950512A7250 TURBINE BOEING727 727254 138408LNM PWA JT8 JT8D7B 52053NE NR 1 ENGINE FAILED A TAOAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 EA15916TS521296554 20437 657192 NR 1 ENGINE FAILED ON TAKEOFF FROM DCA AT 1500 FT. EGT INCREASED, ENGINE SHUTDOWN. RETURNED DCA. FOUND TURBINE SECTION FAILED, REPLACED ENGINE. TRIMMED ENGINE AND CHECKED OPERATION PER MM 71-00. (W) 2L73 4F4 F A3WE E2EA 19950609002241995060900224 1995 6 9 WRLA95028 419950515A34174059060901 ADC DOUG MD11 MD11 3023602NM NR 2 POSITION INOPERATIVE A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27275WA 48631 ON CLIMB-OUT OF LSZH, FLIGHT CREW EXPERIENCED AN AIRSPEED MISMATCH BETWEEN FLIGHT OFFICERS AND CAPTAINS AIRSPEED INDICATORS. CAPTAINS AIRSPEED WAS IN AGREEMENT WITH THE STANDBY AIRSPEED INDICATOR. CAPTAIN ELECTED TO RETURN TO LSZH. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REPLACED NR 2 CADC AND BLEW OUT LINE FROM PITOT TUBE. PERFORMED TEST WITH P/S TEST SET. AIRSPEED CONSTANT THROUGHOUT. NO LEAK DETECTED. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950609002251995060900225WP 1995 6 9 WRLA95029 119950516A276005011681 TENS REGULATORS DOUG DC10 DC1030F 3023504WP NR 5 SPOILER LACK OF LUBE A WRLAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 EA27107WA 46836 WHILE TAXIING OUT FROM GATE, CAPTAIN PERFORMED FLIGHT CONTROL CHECK. NR 5 SPOILER SEGMENT RIGHT WING WOULD NOT FULLY DEPLOY. CAPTAIN ELECTED TO RETURN TO GATE FOR MAINTENANCE. MAINTENANCE CLEANED AND LUBED TENSION REGULATORS AND CABLE RUNS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L73 4F RTA22WE 19950609002261995060900226NE 1995 6 9 PLGA412951 319950412A6111 BLADE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R354 R3544123F13 NE NR 3 LOOSE A APLGAK NONE O OTHER ININSP/MAINT 1 NE05366BE 340B303 785429 DRG189889 DURING A ROUTINE INSPEC, THE NR 3 BLADE HAD EXCESSIVE MOVEMENT O/B OF THE OUTER SLEEVE. ONE OF THE SLIDER BLOCKS HAD DETACHED FROM THE CROSSHEAD AND WAS MOVING AROUND THE HUB ASSY. ALSO, SEVEN SMALL PINS WERE FOUND INSIDE THE HUB ASSY. ALL PINS WERE MISSING ON THE NR 3 BLADE, ON NR 1 BLADE 2 WERE MISSING AND ON NR 4 BLADE ONE WAS MISSING. OIL WAS FOUND INSIDE THE HUB. THE PROP ASSY WAS SHIPPED TO DOWTY AEROSPACE PROP, LTD FOR REPAIR. S/D THIS SDR CLOSES THE SDR OPENED 6/2/94. INSPECTION REVEALED THE DOWEL PINS MIGRATED OUT OF POSITION DUE TO A FAILURE OF THE WEDGE AND OUTER SLEEVE, WHICH RESULTED IN EXCESSIVE TIP MOVEMENT, AND CRACKING OF THE OUTER SLEEVE. (Z) 2L72 4T4 TRTA52EU E8NE 6 CP61GL 19950609002271995060900227NE 1995 6 9 PLGA417951 219950417A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE MALFUNCTIONED A PLGAA UNSCHED LANDING M OVER TEMP CRCRUISE 1 NE05350BE 340B197 785387 FLT 4418 - AT FL 17.0 IN CRUISE CONFIGURATION, PILOT REPORTED HEARING A LOUD BANG FROM THE RT ENGINE FOLLOWED BY TEMPERATURE RISE TO APPROX 1036 DEGREES CELSIUS. PILOT REDUCED POWER LEVER AND TEMPERATURE FOLLOWED. POWER LEVER WAS SET AT FLIGHT IDLE AND LANDING WAS MADE AT ACY. AC WAS EN ROUTE FROM IAD TO BOS. FDR AND ENGINE REMOVED FOR FURTHER INVESTIGATION. S/D - THIS SDR CLOSES OUT THE SDR INITIATED ON 19 DEC 94 REPORTING AN IN FLIGHT ENGINE SURGE EVENT. THE POWERPLANT WAS DETERMINED TO BE REMOVED DUE TO HEAVY OIL IN THE COMPRESSOR AIR FLOW PATH. (Z) 2L72 4T4 TRTA52EU E8NE 19950609002281995060900228NE 1995 6 9 PLGA51952 319950501A6114 REAR SEAL SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROP HUB WORN A PLGAEA ENGINE SHUTDOWN UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 NE05340BE 340A062 DRG743586 JFK - 4308 - THE AC STARTED VIBRATING, THE CREW ISOLATED THE VIBRATION TO THE RT SIDE OF THE AC. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RT ENG PROP GEARBOX OIL PRESS DROPPED TO 0 PSI. UPON REACHING 0 PSI THE RT PROP RPM DROPPED FROM 1220 TO 1040 RPM THEN RETURNED TO 1220 RPM. AS THE PROP RPM STARTED TO DROP AGAIN THE CREW SHUTDOWN THE RT ENG. THE AC DIVERTED TO BDL. MX DETERMINED THE REAR HUB CROSS SHAFT O-RING HAD FAILED ALLOWING PGB OIL TO FLOOD THE PROP HUB. THE PROP WAS REMOVED AND REPLACED AND THE AC WAS RETURNED TO SERV. S/D - DISASSEMBLY INSPECTION CONFIRMED THE VIBRATION TO BE THE RESULT OF OIL MIGRATION PAST THE REAR SEAL GROOVE O-RING INTO THE HUB CAUSING THE OUT OF BALANCE CONDITION. (Z)2L72 4T RTA52EU 6 CP61GL 19950609002291995060900229NM 1995 6 9 9508835529 119950603A5210 SEAL BOEING757 757251 1384970NM DOOR 4R LOOSE A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01529US 23844 A BUMPING NOISE WAS REPORTED NEAR DOOR 4R AFTER TAKEOFF, AIRCRAFT RETURNED TO SFO. FOUND THE INNER (NOISE) DOOR SEAL OUT OF THE SEAL RETAINER AND PROTRUDING OUTSIDE OF DOOR 4R. REINSTALLED SEAL, NO DAMAGE FOUND. 2L72 4F RTA2NM 19950609002301995060900230 1995 6 9 95UAL737078 419950602A2210 YAW DAMPER BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE E/E COMPT MALFUNCTIONED A UALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 WP299017U 19055 AUTOPILOT ENGAGED WITH ALTITUDE HOLD, HEADING HOLD AND YAW DAMPER ON. RECEIVED ONE JOLT IN RUDDER PEDALS FOR LEFT RUDDER INPUT. DISENGAGED YAW DAMPER AND AUTOPILOT. 2L72 4F4 F A16WE E2EA 19950609002311995060900231NM 1995 6 9 95UAL737079 119950602A3350 EEL BATTERY PACK BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299071U 19952 FOUND LEFT OVER WING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. 2L72 4F4 F A16WE E2EA 19950609002321995060900232NE 1995 6 9 95UAL737080 219950605A7200 ENGINE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 1 VIBRATION A UALAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 WP29382UA 24657 NR 1 ENG VIBRATION. UNABLE TO DUPLICATE VIBRATION IN TEST CELL. NO CORRECTIVE ACTION REQUIRED. 2L72 4F4 FRTA16WE E2GL 19950609002331995060900233NM 1995 6 9 95UAL737081 119950605A2820 CHECK VALVE 2172005 BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE NR 2 FUEL TANK MIS INSTALLED A UALAK NONE W INADEQUATE Q C CRCRUISE 1 WP29974UA 21597 CREW REPORTS FUEL IS USED FROM NR 2 FUEL TANK INSTEAD OF CENTER TANK WITH ALL PUMPS ON. FOUND CENTER TANK CHECK VALVE INSTALLED IN THE NR 2 MAIN TANK CHECK VALVE POSITION. 2L72 4F4 F A16WE E2EA 19950609002341995060900234NM 1995 6 9 95UAL747038 119950605A3350 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29183UA 25379 2 AFT RT OVERWING EMERGENCY LIGHTS INOP ON TEST. REPLACED POWER SUPPLY, OPS CHECKED SATISFACTORY. 2L74 4F4 FRTA20WE E24NE 19950609002351995060900235WP 1995 6 9 95UALD10046 119950605A2130MS211512 CHECK VALVE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 PACK FAILED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP291855U 47837 NO CONTROL OF PRESSURIZATION. OUTFLOW VALVE FULL CLOSED, NO DOOR OPEN LIGHTS ON, NO CONTROL IN AUTO, SEMI-AUTO, OR STANDBY. PNEUMATICS IN AUTO, PACKS IN AUTO-HI. THE NUMBER THREE OUTLET COUPLING HAD FAILED PREVIOUSLY AND WAS DEFERRED INOP. ON CLIMBOUT, THE NUMBER THREE AIR CONDITION CHECK VALVE DID NOT SEAT, RESULTING IN LIMITED PRESSURIZATION. CHECK VALVE WAS FOUND TO HAVE A FAILED BEARING. 2L73 4F4 F A22WE E23EA 19950609002361995060900236WP 1995 6 9 95UALD10047 119950605A2120 AIR DISTR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN ODOR A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 WP291844U 48260 PUNGENT ODOR, SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. 2L73 4F4 F A22WE E23EA 19950609002371995060900237SO 1995 6 9 COM11909 119950523A575312037340004 END RIB EMB 1204032700 EMB 120 EMB120RT SO RT TE FLAP CHAFED A COMAK NONE O OTHER ININSP/MAINT 1 SO011105G 120212 120105 ROUTINE INSPECTION, FOUND A SMALL HOLE CHAFED THROUGH THE INBOARD END CLOSING RIB OF THE RIGHT NACELLE FLAP. A SHEET METAL DOUBLER REPAIR WAS FABRICATED AND INSTALLED PER AERODESIGN REPORT NR 1538-1, REV IR, DATED 5-23-95. 2L72 4T RTA31SO 19950609002381995060900238SW 1995 6 9 COM20376 119950601A3297 WIRE SWRNGNSA227 SA227AC 8780603SW NLG BROKEN A COMAO OTHER N FALSE WARNING APAPPROACH 1 SO01457AM AC694 NLG INTRANSIT LIGHT IS INOP. REPAIRED TERMINAL ENDS ON WIRING AT TERMINAL STRIP NR TS114. 2L72 4T RTA8SW 19950609002391995060900239EU 1995 6 9 COM31093 119950602A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01356CA3475 304 MAY930526 340A034 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950609002401995060900240EU 1995 6 9 COM31094 119950601A3240HP14081004 BRAKE VALVE SAAB SF340 SF340A 7850100EU NLG DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01344CA11401928 340A025 BOTH PILOTS AND COPILOTS BRAKES WILL NOT STOP THE AIRCRAFT. REPLACED THE BRAKE CONTROL VALVE. 2L72 4T RTA52EU 19950609002411995060900241EU 1995 6 9 COM31095 119950601A2612 FIRE WIRE SAAB SF340 SF340A 7850100EU RT ENGINE DIRTY A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01344CA 340A025 RT FIRE DETECTOR FAIL WARNING CAME ON AFTER FLIGHT THROUGH HEAVY RAIN. NO DEFECTS FOUND. CLEANED FIRE DETECTION WIRING CONNECTIONS. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950609002421995060900242EA 1995 6 9 COM60489 119950530A3411 PITOT CNDAIRCL600 CL6002B19 EA FWD FUS MOISTURE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01915CA4836 7013 MACH TRIM CAUTION MESSAGE ON EICAS. REMOVED WATER FROM NR1 AND NR 2 PITOT/STATIC SYSTEM. 2L72 4F RTA21EA 19950609002431995060900243EA 1995 6 9 COM60490 119950601A3250601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 EA NLG STEERIUG DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01929CA3387 7035 NLG STEERING IS INOP. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 19950609002441995060900244EA 1995 6 9 COM60491 119950602A275126WC98SN CONNECTOR CNDAIRCL600 CL6002B19 EA RT TE FLAPS DEFECTIVE A COMAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01933CA2844 7040 FLAPS FAIL MESSAGE ON EICAS. FLAPS FAILED AT ZERO DEGREES. RESEATED PIN IN WIRING CONNECTOR AT THE RT BPSU. 2L72 4F RTA21EA 19950609002451995060900245EA 1995 6 9 COM60492 119950601A3230601R751461 VALVE CNDAIRCL600 CL6002B19 EA NLG DEFECTIVE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01929CA3387 7035 GEAR DISAGREE MESSAGE ON EICAS, NLG DID NOT DOWN LOCK. EMERGENCY PROCEDURE USED TO EXTEND LANDING GEAR. REPLACED NLG SELECTOR VALVE. 2L72 4F RTA21EA 19950609002461995060900246WP 1995 6 9 MWEA95213 119950603A5350 LATCH DOUG DC9 DC932 3022066WP TAILCONE FAILED TEST A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31202ME 47672 DURING ROUTINE INSPECTION, THE TAILCONE LEFT HAND LATCHES DID NOT RELEASE DURING FUNCTIONAL TEST. MAINTENANCE RIGGED TAILCONE RELEASE SYSTEM IAW DOUGLAS MM 53-50-3. OPS CHECKED GOOD, RETURN A/C TO SERVICE. 2L72 4F A6WE 19950609002511995060900251CE 1995 6 9 95ZZZX2679 119950516A3230727725 BREAKER CESSNA402 402C 207590RCE MLG FAILED A OEZAO OTHER O OTHER CLCLIMB 1 WP19760EA 402C0056 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED SWITCH AND CHECKED CIRCUIT BREAKERS. RECYCLED HYDRAULIC CIRCUIT BREAKER AGAIN AND GEAR WENT UP WITH NO FURTHER PROBLEMS. MAINTENANCE WAS ABLE TO DUPLICATE THE PROBLEM AND CHANGED CIRCUIT BREAKER. NO FURTHER PROBLEMS NOTED. SUBMITTER RECOMMENDS CHANGING CIRCUIT BREAKERS WHENEVER THEY TRIP AND SHOULD CHANGE THEM WHEN THEY ARE IN SERVICE FOR AN EXTENDED LENGTH OF TIME. 1L72 3O A7CE 19950609002961995060900296NM 1995 6 9 95ZZZZ237 119950519A57536573732 SKIN BOEING737 737317 138447PNM LT TE FOREFLAP DELAMINATION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 LT WING OUTBOARD FOREFLAP DELAMINATED ON UPPER OUTBOARD EDGE. REPAIRED FLAP PER SRM 51-70-10. 2L72 4F RTA16WE 19950609002971995060900297NM 1995 6 9 95ZZZZ238 119950518A53156546817 FLOORBEAMS BOEING737 737317 138447PNM FS 294\312\328 CORROSION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 HEAVY CORROSION AT FLOORBEAMS FS 294, 312, AND 328, JUST BELOW FWD LAVATORY AND GALLEY. REPAIRED BEAMS PER SRM 51-70-12. 2L72 4F RTA16WE 19950609002981995060900298NM 1995 6 9 95ZZZZ239 119950518A7110 DUCT BOEING737 737317 138447PNM LT ENGINE DELAMINATION B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 THE NR 1 ENGINE FAN COWL INNER DUCT SKIN DELAMINATED AT 3 O'CLOCK POSITION. REPAIRED PER DALFORT AVIATION XEA NR X2-78-6. 2L72 4F RTA16WE 19950609002991995060900299NM 1995 6 9 95ZZZZ240 119950518A5400 ANGLE BOEING737 737317 138447PNM LT PYLON CRACKED B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 LT PYLON ANGLE HAS 1 INCH LONG CRACK ON LOWER SIDE, 6 INCHES OF AFT CONE BOLT. REPLACED ANGLE PER SRM 51-40-12. 2L72 4F RTA16WE 19950609003001995060900300NM 1995 6 9 95ZZZZ241 119950518A5320 DOOR FRAME BOEING737 737317 138447PNM CARGO COMPT CRACKED B EF2RK NONE O OTHER ININSP/MAINT 1 SW072FOR 23173 FORWARD CARGO DOOR OUTER FRAME HAS A .375 INCH LONG CRACK AT LOWER FORWARD CORNER. REPAIRED FRAME PER SRM 51-70-11. 2L72 4F RTA16WE 19950609003011995060900301WP 1995 6 9 95ZZZZ242 119950516A2612 FIRE LOOP DOUG DC8 DC851 3021920WP NR 1 ENGINE DIRTY A TC8AE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23805CK 45649 ENGINE NR 1 IN FLIGHT FIRE WARNING. COMPLIED WITH ALL CHECK LISTS, ENGINE SHUTDOWN AT 1650Z. FOUND B-NUT UNSCREWED ON I/B CASCADE, RESECURED. LOWER FIRE LOOP CONNECTOR FULL OF ENGINE OIL, CLEANED CONNECTOR AND REINSTALLED IAW MM. GROUND RAN ENGINE FOR SEVERAL MINUTES IAW MM, GROUND OPS CHECKS GOOD. 2L74 4F 4A25 19950609003031995060900303EU 1995 6 9 95ZZZZ244 119950516A2410342A010100 IDG THERMOSTAT AIRBUS320 A320231 3930325EU NR 1 ENGINE FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28627AW 66 LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ245, AWXA9500291. 2L72 4F RTA28NM 19950609003041995060900304EU 1995 6 9 95ZZZZ245 119950516A2421740119F GENERATOR AIRBUS320 A320231 3930325EU NR 2 ENGINE FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28627AW 66 LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ244, AWXA9500291. 2L72 4F RTA28NM 19950609003051995060900305CE 1995 6 9 95ZZZZ246 119950503A3260 SWITCH BEECH 99 C99 1154006CE RT MLG UPLOCK REQ ADJ A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO19216EE U206 FPO-MIA - FLT 426 - RED GEAR LIGHT ILLUMINATED AND GEAR HORN SOUNDS INTERMIITTENTLY WITH GEAR UP IN CRUISE AND WITH GEAR DOWN AND LOCKED. MAINTENANCE ADJUSTED RT UPLOCK SWITCH, SWING GEAR ON JACKS, OPS CHECK GOOD. RELEASED FOR TEST FLIGHT, TEST FLIGHT SATISFACTORY RETURNED TO SERVICE. 1L72 3T A14CE 19950609003061995060900306CE 1995 6 9 95ZZZZ247 119950508A3260503800481 RELAY BEECH 99 C99 1154006CE GEAR WARN MALFUNCTIONED A GUUAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO19216EE U206 MHH-MIA - FLT 439 - AFTER LANDING, GEAR WARNING HORN COMES ON AND GEAR HANDLE ILLUMINATED CONTINUOUSLY. MAINTENANCE REMOVED AND REPLACED GEAR WARNING RELAY NR K161, SWING GEAR OPS CHECK GOOD. RELEASED FOR TEST FLIGHT, TEST FLIGHT SATISFACTORY. RETURNED TO SERVICE. 1L72 3T A14CE 19950609003071995060900307CE 1995 6 9 95ZZZZ248 119950503A32601003810061 SWITCH BEECH 99 C99 1154006CE RT MLG UPLOCK INTERMITTENT A GUUAO OTHER N FALSE WARNING TOTAKEOFF 1 SO19216EE U206 FLL-MIA - FLT 458 - GEAR HORN SOUNDS INTERMITTENTLY ON TAKEOFF AND ROTATION. MAINTENANCE REMOVED AND REPLACED RT UPLOCK SWITCH, SWING GEAR, OPS CHECKS GOOD. 1L72 3T A14CE 19950609003081995060900308CE 1995 6 9 95ZZZZ249 119950502A3260 SWITCH BEECH 99 C99 1154006CE RT MLG UPLOCK REQ ADJ A GUUAO OTHER N FALSE WARNING CRCRUISE 1 SO19216EE U206 FLL-MIA FLT 472 - LANDING GEAR WARNING HORN SOUNDS IN FLIGHT WITH GEAR UP. MAINTENANCE ADJUSTED RT UPLOCK SWITCH, SWING GEAR ON JACKS, OPS CHECK GOOD. 1L72 3T A14CE 19950609003091995060900309EU 1995 6 9 AWXA9500291 119950516A24105844000 IDG COOLER AIRBUS320 A320231 3930325EU NR 2 ENGINE CONTAMINATED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28627AW 66 LAS-MKE - ON CLIMBOUT, LOST NR 2 ENG IDG. ACFT RETURNED TO LAS WITHOUT FURTHER PROBLEMS, NO OVERWEIGHT LANDING. MX REMOVED AND REPLACED THE NR 2 ENG IDG PER AWA TASK CARD R3M24301. REMOVED AND REPLACED NR 1 ENG TEMP CONTROL THERMOSTAT PER AMM. REMOVED AND REPLACED THE NR 2 ENG IDG OIL COOLER PER AMM, LEAK CHECK GOOD. NR 2 ENG IDG LEAK CHECK GOOD AND PARAMETERS WITHIN LIMITS OF AWA TASK CARD R3M24301. NR 1 ENG TCT OPS CHECK NORMAL. BLEED PRESSURE AND TEMP NORMAL. ACFT RETURNED TO SERVICE. REF 95ZZZZ244, 95ZZZZ245. 2L72 4F RTA28NM 19950609003101995060900310NM 1995 6 9 CAL950373 119950509A3350RPF1B EEL CHARGER BOEING727 727243 138408DNM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917410 21663 TPA - FLT 618 - THE EMERGENCY EXIT STRIP LIGHTS ON THE SEATS IN FIRST CLASS SECTION WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERY PACK CHARGER WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT STRIP LIGHTS WAS RESTORED. 2L73 4F RTA3WE 19950609003111995060900311WP 1995 6 9 HAL95054 119950420A5330 SKIN DOUG DC9 DC951 3022051WP FS 927 CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND LEVEL 2 CORROSION ON LT FUSELAGE SKIN AT STATION 927 TO 851 STR 18 TO 22 AROUND FAIRING ATTACH POINTS. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-09 FIG 53. (Z) 2L72 4F A6WE 19950609003121995060900312WP 1995 6 9 HAL95056 119950421A5400 FAIRING DOUG DC9 DC951 3022051WP NR 2 PYLON CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND RT PYLON AFT FAIRING HAS LEVEL 2 CORROSION AT FUSELAGE ATTACH HOLES AND IN BETWEEN SKIN LAYERS. CUT OUT CORRODED AREA AND INSTALLED DOUBLER REPAIR PER SRM 54-01 FIG 4. (Z) 2L72 4F A6WE 19950609003131995060900313WP 1995 6 9 HAL95057 119950419A5330 SKIN DOUG DC9 DC951 3022051WP FS 851-860 CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND WIDE SPREAD LEVEL 2 CORROSION ON FUSELAGE SKIN INCLUDING BRACKET AT STATION 851 TO 860 STR 30. INSTALLED STRAP AND DOUBLER REPAIR PER ENGINEERING DRAWING NR SKB003818N00253. (Z) 2L72 4F A6WE 19950609003141995060900314WP 1995 6 9 HAL95058 119950418A5311 FRAME DOUG DC9 DC951 3022051WP FS 1320 CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND AFT TAIL COMPARTMENT INTERNAL STRUCTURE HAS LEVEL 2 CORROSION ON FRAME WEB JUST BELOW AIRSTAIR ACTUATOR CONTROL VALVE STA 1320 STR 26L. FABRICATED WEB AND CLIP PER SRM 53-01 FIG 4 AND INSTALLED PER SRM 51-30-2 AND 51-30-5. (Z) 2L72 4F A6WE 19950609003151995060900315WP 1995 6 9 HAL95059 119950420A5320 STIFFENER DOUG DC9 DC951 3022051WP FS 1292 CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND AFT TAIL COMPARTMENT INTERNAL STRUCTURE HAS LEVEL 2 CORROSION ON FRAME STIFFENER AT STA 1292 STR 13L. FABRICATED AND INSTALLED STIFFENER PER SRM 51-01 AND 51-30-2. (Z) 2L72 4F A6WE 19950609003161995060900316WP 1995 6 9 HAL95060 119950427A5330 SKIN DOUG DC9 DC951 3022051WP FS 1314-1339 CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND LEVEL 2 CORROSION AROUND FASTENERS ON EXTERIOR FUSELAGE STA 1314 TO 1339 STR 20L TO 25L. REMOVED CORROSION AND INSTALLED REPAIR PER 51-10-3, 53-01 AND 52-01 FIG 3 SHEET 3. (Z) 2L72 4F A6WE 19950609003171995060900317WP 1995 6 9 HAL95061 119950516A33502078C EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 47726 HNL - FLOOR EMERGENCY EVACUATION LIGHTS ARE VERY DIM. REPLACED AFT BATTERY PACKS AND OPERATIONAL CHECK WAS GOOD. (Z) 2L72 4F A6WE 19950609003181995060900318WP 1995 6 9 HALA95055 119950420A5753B0038N005311 SPAR DOUG DC9 DC951 3022051WP NR 2 TE FLAP CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47796 SBA - DURING D-CHECK, FOUND LEVEL 2 CORROSION UNDER NUT CHANNELS AND 4 BROKEN SCREWS ON LT FLAP AFT SPAR NR 2 TRAILING EDGE. REMOVED CORROSION AND INSTALLED STRAP PER ENGINEERING DRAWING NR SKB0038N00531 AND SRM 51-10-3 AND 51-01. (Z) 2L72 4F A6WE 19950609003191995060900319EU 1995 6 9 SIMA951221 119950502A33503011210 EEL ASSEMBLY AEROSPATR42 ATR42300 8680920EU CABIN INOP A SIMAK NONE O OTHER ININSP/MAINT 1 SW21429MQ 135 MQT - DURING MAINTENANCE INSPECTION EMERGENCY LIGHT IN PAX DOOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. ACFT WAS RETURNED TO SERVICE. (Z) 2H72 4T RTA53EU 19950609003201995060900320NM 1995 6 9 95ZZZW774 119950508A2910 HYD LINES DUNLOP AHA1648 BOEING757 75723APF 1384966NM LT MLG BROKEN A ACLCAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO19572CA MG169 24868 FLT NR 92 - AFTER TAKEOFF FROM BOGOTA, LOST HYDRAULIC SYSTEM QUANTITY AND PRESSURE. ABNORMAL CHECK LIST COMPLIED WITH. AIRCRAFT DIVERTED TO CALI. FOUND THREE BROKEN LINES AT LEFT LANDING GEAR SEQUENCE VALVE, CAUSED BY NR SIX MAIN TIRE SEPARATED RECAP. REPLACED BROKEN LINES. LEAK CHECKED OK PER MM 29-11-00. REPLACED NR SIX WHEEL/TIRE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA2NM 19950609003211995060900321NM 1995 6 9 95ZZZW775 119950516A2611302842 SMOKE DETECTOR BOEING727 72721 1384003NM CARGO COMPT MALFUNCTION A RYNAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE07329QS 19038 SMOKE DETECTOR CAME ON WHILE IN CRUISE FLIGHT, MADE UNSCHEDULED LANDING INTO SWF, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OPENED THE MAIN CARGO DOOR AND THE SMOKE DETECTOR LIGHT WENT OUT. UNLOADED CARGO AND INSPECTED. NOTED STRANGE ODOR FROM THE AFT LOWER CARGO PIT. UNLOADED CARGO AND HAD CARGO INSPECTED, FOUND NO EVIDENCE OF SMOKE OF FIRE. SMOKE DETECTOR SYSTEM TESTED NORMAL. (W) 2L73 4F A3WE 19950609003221995060900322WP 1995 6 9 95ZZZW776 119950504A3230 RETRACT PIN DOUG DC8 DC871F 302199DWP RT MLG STRUT SHEARED A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP158076U 45941 KDAY-KRDU - ON TAKEOFF ROLL AT KDAY AIRCRAFT YAWED TO LEFT. ON GEAR RETRACTION DOOR LIGHT AND LANDING GEAR UNSAFE LIGHT STAYED ON ALONG WITH RT ALT GEAR DOOR LIGHT. GEAR PLACED DOWN AND ALL INDICATIONS WERE NORMAL. RETURNED TO KDAY. MAINTENANCE FOUND RT MAIN GEAR RETRACT PIN SHEARED OFF STRUT. PREPARED AIRCRAFT TO FERRY FOR REPAIRS. 2L74 4F RT4A25 19950609003231995060900323NE 1995 6 9 95ZZZW777 219950422A7230 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE STALLED A TWAAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE05901TW 49166 1422 LAX - AFTER TAKEOFF NR 2 ENGINE, S/N 1422, HAD COMPRESSOR STALLS. REDUCED POWER ON NR 2 ENGINE. FOUND METAL PARTICLES IN TAIL PIPE. REPLACED ENGINE S/N 1422. ENGINE OPERATION CHECKS NORMAL. ENGINE TOTAL TIME 6,334, TOTAL CYCLES 7,267. 2L72 4F4 F A6WE E9NE 19950609003241995060900324NM 1995 6 9 95ZZZW778 119950505A243168001008010 TEMP MONITOR DHAV DHC8 DHC8102 2809003NM INST PANEL SHORTED A SABAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO05881CC 294 FLT NR 5040 - AVL-CLT - EXPERIENCED SMOKE IN THE COCKPIT WHILE STILL ON THE GROUND. THE AIRCRAFT WAS INSPECTED FOR DAMAGE AND FERRIED TO CLT. MAINTENANCE PERSONNEL TROUBLESHOT THE DISCREPANCY AND FOUND THAT THE BATTERY TEMPERATURE MONITOR HAD SHORTED OUT. MAINTENANCE THEN REMOVED AND REPLACED THE BATTERY TEMPERATURE MONITOR AND BOTH MAIN AND AUXILLARY BATTERIES. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 2H72 4T RTA13NM 19950609003251995060900325WP 1995 6 9 95ZZZW779 119950510A3310TA4715 RECEPTACLE DOUG DC9 DC932 3022066WP RT CABIN FS 909 BURNED A VJ6AK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11933VV 47489 FLT NR 515 - ATL-FLL - ON THE GATE IN ATL SMOKE WAS REPORTED IN AFT CABIN ROW 25 CDE. FOUND RT CABIN UTITLITY RECEPTACLE (R5-213) AT STATION 909-R BURNED. INSPECTED SURROUNDING AREA FOR DAMAGE. NO DEFECTS NOTED. DAMAGE LIMITED TO RECEPTACLE. REPLACED RECEPTACLE. OPS CHECK NORMAL PER MM 33-20. (W) 2L72 4F A6WE 19950609003261995060900326NM 1995 6 9 95ZZZW780 119950512A3245551650 TUBE 551766 PIPER PA60 PA60600 7106001NM NOSEGEAR DEFECTIVE A ECBAK NONE O OTHER ININSP/MAINT 1 GL099823Q 600466154 PILOT NOTICED THAT THE NOSEGEAR TIRE WAS FLAT DURING PREFLIGHT INSPECTION. FURTHER INVESTIGATION REVEALED THAT THE INNER TUBE, P/N 551-650, HAD FAILED AT THE BASE OF THE VALVE STEM. TUBE WAS REPLACED, WHEEL AND TIRE INSPECTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. SUGGEST CAREFUL INSPECTION OF INNER TUBES AT TIRE CHANGE, AND ESTABLISHING LIFE LIMITS FOR TUBES THAT ARE REUSED. (W) 1M72 3O RTA17WE 19950609003271995060900327 1995 6 9 95ZZZW781 419950508A34417510100921 INT NAV UNIT JETAIRJETSTMJETSTM4101 1500501EU E/E COMP FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27321UE 41045 FLT 6266 - IAD-BTV - DURING CLIMB-OUT RETURNED TO IAD DUE TO A COMPASS SPLIT AND THE MODE C INOP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED THE INU AND REINITIALIZED THE AHRS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE VTZA95160. 2L72 4T RTA41NM 19950609003281995060900328NE 1995 6 9 CAL950272 219950414A7260 SEAL DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE NR 2 ENGINE WORN A CALAJK DUMP FUEL NONE E VIBRATION/BUFFET APAPPROACH 1 SW0912539 45792 666851 THE NR 2 ENGINE OIL QUANTITY DECREASED TO EIGHT QUARTS DURING CRUISE, BUT THE QUANTITY STABILIZED. THE QUANTITY DECREASED TO FOUR QUARTS DURING APPROACH, BUT STABILIZED AGAIN. THE QUANTITY HAD DROPPED TO ZERO BY LANDING. THE NR 2 ENGINE WAS SHUTDOWN ON LANDING ROLL. THE NR 2 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. *S/D* SHOP FINDINGS REPORTED A WORN 4.5 CARBON SEAL AND SPACER. 2L72 4F4 F A6WE E2EA 19950609003291995060900329WP 1995 6 9 CAL950284 119950416A3260 SENSOR DOUG DC9 DC982 3022082WP NLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0972824 49824 FLT NR 0459 - IAH - THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THIS WAS THE SECOND AIR RETURN FOR THE SAME INDICATION PROBLEM. MAINTENANCE FOUND THE NOSE GEAR OVERCENTER SENSOR AT FAULT. THE SENSOR WAS REMOVED AND REPLACED. NOSE GEAR OPERATION AND INDICATION CHECKED NORMAL. (W) 2L72 4F A6WE 19950609003301995060900330WP 1995 6 9 CAL950286 119950417A3260 SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR OUT OF ADJUST A CALAO OTHER N FALSE WARNING TOTAKEOFF 1 SW0914534 47110 FLT NR 0743 - IAH - THE LEFT MLG DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. THE GEAR DOOR LIGHT DID NOT EXTINGUISH WHEN THE GEAR WAS EXTENDED FOR LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MLG DOOR LIGHT SWITCH. THE GEAR DOOR LIGHT OPERATED NORMALLY. (M) 2L72 4F A6WE 19950609003321995060900332NM 1995 6 9 CAL950392 119950516A323065C1623753 CARDFILE BOEING737 7373T0 1384582NM LG LOGIC UNIT INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0969311131658274 23362 FLT NR 0578 - IAH - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE OVERRIDE TRIGGER WAS USED AND THE GEAR RETRACTED, BUT THE WARNING HORN SOUNDED INTERMITTENTLY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LANDING GEAR LOGIC UNIT CARDFILE AT FAULT. THE CARDFILE WAS REMOVED AND REPLACED. A TAKEOFF WARNING CHECK AND SIMULATED GEAR RETRACTION WAS PERFORMED AND ALL SYSTEMS CHECKED GOOD. (W) 2L72 4F RTA16WE 19950609003331995060900333CE 1995 6 9 PLGA419951 119950419A3310 LIGHT SYSTEM BEECH 1900 1900 1154160CE INSTR PANEL WET A PLGAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NE057210R UB30 BOS - FLT 4361 - DURING TAXI THE CREW HEARD AN ARCING SOUND FOLLOWED BY AN ELECTRICAL BURNING SMELL. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND WATER ON THE TRANSISTORS FOR THE LIGHT DIMMING SYSTEM BEHIND THE FUEL QUANTITY INDICATORS. MAINTENANCE DRIED THE AREA, RESEALED THE PANEL AND RETURNED THE AIRCRAFT TO SERVICE. (W) 2L72 4T RTA24CE 19950609003341995060900334NE 1995 6 9 SIMA951211 219950501A732132448713 MFCU AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENG FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21309AM2236 309 127077 ORD - FLT 4298 - AFTER CRUISE POWER WAS SELECTED. THE RIGHT ENGINE TORQUE SURGED 70 PERCENT. AIRCRAFT RETURNED TO ORD. NO EMERGENCY DECLARED. REPLACED RT ENGINE MFCU AND FUEL PUMP, GROUND AND FLIGHT TEST SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950609003351995060900335NM 1995 6 9 TAOA059508 119950513A499038067811 APU BOEING727 727225 1384077NM WHEEL WELL LEAKING OIL A TAOAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 EA15922TS P35420 20415 PRIOR TO BOARDING, APU FILLED CABIN WITH SMOKE. FOUND OIL ON GROUND AROUND APU AND APU COVERED WITH OIL. M841141 ASSIGNED PER MEL SEQ 49-1. MAINTENANCE LATER REPLACED APU ASSEMBLY. (W) 2L73 4F A3WE 19950609003361995060900336 1995 6 9 VTZA95160 419950508A34257003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU E/E COMP FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27321UE 41045 FLT 6266 - IAD-BTV - DURING CLIMB-OUT RETURNED TO IAD DUE TO A COMPASS SPLIT AND THE MODE C INOP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED THE INU AND REINITIALIZED THE AHRS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA41NM 19950609003371995060900337WP 1995 6 9 9508849604 119950601A5320 FITTING DOUG DC9 DC932 3022066WP FS 408 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FS 408 FRAME FITTING AT LONGERON 18R. REPLACED FITTING PER SRM 51-30-02. 2L72 4F A6WE 19950609003381995060900338NE 1995 6 9 9508851152 219950603A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 3 ENGINE STALLED A NWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL01152US 46761 686117 DURING CRUISE WHILE TAKING WHITE LINE READINGS, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL AND WAS SHUTDOWN. THE AIRCRAFT CONTINUED TO MSP WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE, NO FUEL WAS DUMPED. THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19950609003391995060900339EU 1995 6 9 9508863226 119950602A2910 HYD FLUID AIRBUS320 A320211 3930320EU B-HYD SYST LOW LEVEL A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01326US 282 AFTER APPLYING T/O THRUST FOR TAKEOFF ROLL, RECEIVED HYD B RSVR LO LVL MESSAGE. THE TAKEOFF WAS ABORTED AT 60 KNOTS. MAINTENANCE SERVICED THE BLUE HYDRAULIC SYSTEM. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950609003401995060900340EU 1995 6 9 9508873205 119950605A2910 O-RING AIRBUS320 A320211 3930320EU YELLOW HYD SYST LEAKING A NWAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01305US 41 DURING CLIMBOUT AT FL280, RECEIVED HYD Y RSVR LO LVL MESSAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCO AND LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STANDING BY. MAINTENANCE REPLACED AN 'O' RING ON THE HYDRAULIC POWER TRANSFER UNIT HYDRAULIC FITTING, SERVICED YELLOW HYDRAULIC SYSTEM RESERVOIR. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950609003411995060900341WP 1995 6 9 ABXA9500521 119950421A571339112361 STRINGER DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 12 NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950609003421995060900342WP 1995 6 9 ABXA9500522 119950421A57133911236501 STRINGER DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 15 NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950609003431995060900343WP 1995 6 9 ABXA9500523 119950421A572099193691 CAP DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 16. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950609003441995060900344WP 1995 6 9 ABXA9500524 119950421A57133911238513 STRINGER DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 18, NEAR T-CAP. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950609003451995060900345WP 1995 6 9 ABXA9500525 119950421A57133911238503 STRINGER DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON STRINGER NR 22 NEAR T-CAP. REMOVED CORROSION ON AFT SIDE STRINGER 22, ALODINED AND PRIMED AREA IAW DC-9 SRM 57-03. 2L72 4F A6WE 19950609003461995060900346WP 1995 6 9 ABXA9500526 119950421A572099193691 CAP DOUG DC9 DC932 3022066WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23983AX 47257 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND CORROSION ON HORIZONTAL FLANGE OF T-CAP, INSIDE BARREL NUT HOLE, STRINGER NR 22. REMOVED CORROSION FROM BOTTOM OF BARREL NUT HOLE AND PRIMED IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950609003471995060900347SO 1995 6 9 COM11910 119950605A612078249012 PCU EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01247CA8726 170 120225 LEFT PROPELLER IS SLOW TO UNFEATHER. REPLACED THE PROP PITCH CONTROL UNIT. 2L72 4T RTA31SO 19950609003481995060900348SO 1995 6 9 COM11911 119950602A771230005000053 TQ COND UNIT EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 SO01248CA6220 1065 120228 LT PROPELLER AUTO FEATHER WILL NOT TEST. REPLACED THE TORQUE SIGNAL CONDITIONER. 2L72 4T RTA31SO 19950609003491995060900349SO 1995 6 9 COM11912 119950602A612078249024 PCU EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254CA7686 836 120233 RT ENGINE NP DROPPED TO 50 PERCENT; TORQUE CLIMBED TO 125 PERCENT. REPLACED THE PITCH CONTROL UNIT. 2L72 4T RTA31SO 19950609003501995060900350EA 1995 6 9 COM60493 119950603A3297GB5D22 WIRE CNDAIRCL600 CL6002B19 1900309EA ANTI-SKID SYST CHAFED A COMAO OTHER O OTHER LDLANDING 1 SO01912CA5234 7011 ANTI-SKID CIRCUIT BREAKER TRIPPED AND WILL NOT RESET. REPAIRED DEFECTIVE WIRING AT LANDING GEAR CONTROL PANEL. 2L72 4F RTA21EA 19950609003511995060900351NM 1995 6 9 DL72L952275 119950515A5313 STRINGER BOEING727 727232 1384082NM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11501DA 21303 FOUND ON CV2 CHECK, CORROSION INSIDE OF STR 28L AND OUTBD SIDE AFT OF STA 1010. REPAIRED PER ERA 301845-14. 2L73 4F A3WE 19950609003521995060900352NM 1995 6 9 DL72L952291 119950517A7110 LIP BOEING727 727232 1384082NM NR 2 ENG CUTOUT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11501DA 21303 FORWARD COWLING LIP DAMAGED AT 6 O'CLOCK POSITION NR 2 ENG CUTOUT. FOUND DURING CV-2 CHECK. REPAIRED PER M/M 53-11-0 PG 801. 2L73 4F A3WE 19950609003531995060900353NM 1995 6 9 DL72L952292 119950527A5754651622374 HEAT SHIELD BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 UPON INSPECTION, A CRACK WAS FOUND IN HEAT SHIELD BETWEEN RIBS 11 AND 12, AND BETWEEN RIBS 12 AND 13. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT. 2L73 4F A3WE 19950609003541995060900354NM 1995 6 9 DL72L952293 119950527A5754650622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 UPON INSPECTION, A CRACK WAS FOUND IN THE LOWER FWD CORNER OF NR 10 RIB. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT. 2L73 4F A3WE 19950609003551995060900355NM 1995 6 9 DL72L952294 119950527A5754651622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 UPON INSPECTION, RIB NR 11 FOUND CRACKED IN LWR FWD CORNER. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT. 2L73 4F A3WE 19950609003561995060900356NM 1995 6 9 DL72S951933 119950430A5230 SKIN BOEING727 727232 1384082NM C-3 CARGO DOOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND DENT IN C-3 DOOR OUTER SKIN 1.25 BY 1.5 BY .1562 INCH DEEP. INSTALLED REPAIR PER SRM 52-20-2 PG 1. 2L73 4F A3WE 19950609003571995060900357NM 1995 6 9 DL72S951934 119950428A5313 STRINGER BOEING727 727232 1384082NM FS 1144 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND FUSELAGE STRINGER 26R WITH CORROSION DAMAGE AT FS 1144. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950609003581995060900358NM 1995 6 9 DL72S951935 119950501A5315 FLOORBEAM BOEING727 727232 1384082NM FS 400 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND CABIN FLOOR SUPPORT BEAM AT FS 400 WITH CORROSION DAMAGE TO UPPER CAP AT RBL 12 TO LBL 24. REPAIRED PER SRM 53-10-8 FIG 3. 2L73 4F A3WE 19950609003591995060900359NM 1995 6 9 DL72S951936 119950428A5313 STRINGER BOEING727 727232 1384082NM FS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND CORROSION DAMAGE TO STRINGER 27R AT FS 740. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950609003601995060900360NM 1995 6 9 DL72S952015 119950430A5313 STRINGER BOEING727 727232 1384082NM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND STRINGER 15R CRACKED AT ITS END JUST FWD OF WING ICE LIGHT HOUSING AT FS 720B. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950609003611995060900361NM 1995 6 9 DL72S952084 119950429A5754 RIB BOEING727 727232 1384082NM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND NR 1 SLAT PANEL WITH CRACKED RIB JUST O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0 FIG 804. 2L73 4F A3WE 19950609003621995060900362NM 1995 6 9 DL72S952086 119950429A5754 RIB BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND NR 8 SLAT WITH CRACKED RIBS INBD OF TAI DUCT AND IB RIG AT W/P. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950609003631995060900363NM 1995 6 9 DL72S952295 119950514A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 RIB CRACKED, NR 7 L/E SLAT, 2ND RIB FROM I/B END. REPAIRED PER MM 57-54-0 PG 819, FOUND AT HMV. 2L73 4F A3WE 19950609003641995060900364NM 1995 6 9 DL72S952296 119950514A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 RIB CRACKED NR 3 L/E SLAT. THE 7TH RIB I/E END SLAT IS CRACKD AT NUT LOCATION. INSTALLED REPAIR PER MM 57-54-0 PG 807, FOUND AT HMV. 2L73 4F A3WE 19950609003651995060900365NM 1995 6 9 DL72S952297 119950528A5754651622718A SKIN BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 6 L/E FLAP HAD A CRACK AT I/B HINGE FITTING AFT END. REPAIRED PER SRM 57-50-03 PG 32. 2L73 4F A3WE 19950609003661995060900366NM 1995 6 9 DL72S952298 119950528A5754651622718A SKIN BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 6 L/E FLAP HAD A PREVIOUS REPAIRED CRACK WHICH CRACKED FURTHER. REPAIRED PER SRM 57-50-3, FOUND AT HMV. 2L73 4F A3WE 19950609003671995060900367NM 1995 6 9 DL72S952333 119950511A5754 BRACKET BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND UPPER/LOWER CORNERS CRACKED FOR NR 2 LE FLAP ACT MOUNT BRACKET. INSTALLED DOUBLER PER M/M 57-20-21 PG 811. 2L73 4F A3WE 19950609003681995060900368NM 1995 6 9 DL72S952344 119950531A2730 BEARING BOEING727 727232 1384082NM NR 1 ELEV FROZEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND ELEV TO STAB BEARING FROZEN, NR 1 ELEV TO STAB MOUNT WORN. REPAIRED PER MM 55-50-0. 2L73 4F A3WE 19950609003691995060900369NE 1995 6 9 DL72S952462 219950602A73217436025 FUEL CONTROL BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 3 ENGINE MALFUNCTIONED A DALAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO11482DA 20862 700578 DURING CRUISE, NR 3 ENGINE HAD FLUCTUATING FUEL FLOW AND N1, AND EPR. RETARDED THROTTLE, THEN ENGINE FLAMED-OUT. LANDED PHL WITHOUT INCIDENT. ENGINE WAS CHECKED PER MM, ALL PARAMETERS NORMAL. AS A PRECAUTION, THE FUEL CONTROL AND FUEL PUMP WERE REPLACED. 2L73 4F4 F A3WE E2EA 19950609003701995060900370NM 1995 6 9 DL72S952464 119950602A2121215201 FAN BOEING727 727232 1384082NM AC COMP SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11496DA 21076 DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN AND FLIGHT DECK. ODOR STOPPED AFTER SECURING GASPER FAN. GASPER FAN WAS FOUND SHORTED. REPLACED FAN, OPERATION NORMAL. 2L73 4F A3WE 19950609003711995060900371NM 1995 6 9 DL72S952484 119950429A5754 RIBS BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND NR 5 L/E SLAT WITH 2 CRACKED RIBS INBD AND OTBD OF SLAT ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950609003721995060900372NM 1995 6 9 DL72W952139 119950125A575465162267A SKIN BOEING727 727247 138408FNM LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112825W 21330 DURING INSP, A CRACK WAS FOUND IN THE SKIN AT THE INBD SIDE. THIS WAS REPAIRED PER SRM 57-50-3, FOR L/E KRUGER FLAP PANEL. 2L73 4F A3WE 19950609003731995060900373NM 1995 6 9 DL72W952140 119950125A575465162267A LUG BOEING727 727247 138408FNM LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112825W 21330 DURING INSP, A CRACK WAS FOUND IN THE NOSE FLAP AT THE INBD LUG. THIS WAS REPAIRED PER SRM 57-50-3 PG 20. 2L73 4F A3WE 19950609003741995060900374NM 1995 6 9 DL72W952319 119950507A5753 SKIN 652163087A BOEING727 727247 138408FNM NR 2 TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 575 21327 THE LEADING EDGE HAD A WORN AREA APPROX 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE AREA WAS REPAIRED PER SRM 57-50-4 FIG 1, FOR NR 2 FLAP PANEL DURING SHOP INSPECTION. 2L73 4F A3WE 19950609003751995060900375NM 1995 6 9 DL72W952320 119950505A5753 SKIN 6521630187 BOEING727 727247 138408FNM LT TE FLAP WORN A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112822W 575 21327 TRANSFER FROM N/R CARD NR 6348, THE L/E WAS WORN 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE WRONG TYPE OF RIVETS WERE INSTALLED ON THE ORIGINAL DOUBLER. CARD 6477 WAS ISSUED TO CORRECT THIS ACTION. THE REPAIR WAS PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950609003761995060900376NM 1995 6 9 DL73S952115 119950508A5523 SKIN BOEING737 737232 1384475NM LT ELEV TAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 LT ELEV TAB CRACKED AT BOTH ENDS. BAL AFTER REPAIR. REPAIRED TAB PER ARM 55-20-01. 2L72 4F RTA16WE 19950609003771995060900377NM 1995 6 9 DL73S952116 119950509A5523 SKIN BOEING737 737232 1384475NM LT ELEV TAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 LT ELEV TAB O/B HINGE UPPER AND LOWER SKIN CRACKED, COMPLIED WITH SRM 55-20-3. 2L72 4F RTA16WE 19950609003781995060900378NM 1995 6 9 DL757951958 119950430A5522 SKIN BOEING757 757232 1384965NM ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 TOP SURFACE OF LEFT ELEVATOR, WAS FOUND WITH 13 HOLES FROM HAIL DAMAGE. ACCOMPLISHED REPAIRS PER SRM 55-20-01 AND DL ERA 301679-14. 2L72 4F RTA2NM 19950609003791995060900379NM 1995 6 9 DL757951959 119950430A5522 SKIN BOEING757 757232 1384965NM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11676DL 25981 TOP SURFACE OF RT ELEVATOR HAS 9 HOLES FROM HAIL DAMAGE. REPAIRS WERE ACCOMPLISHED PER SRM 55-20-01 AND DL ERA 301670-14. 2L72 4F RTA2NM 19950609003801995060900380NM 1995 6 9 DL757952052 119950503A5754 TE WEDGE BOEING757 757232 1384965NM NR 1 LE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 LEFT WING NR 1 L/E SLAT TRAILING EDGE WEDGE, WAS FOUND DAMAGED FROM HAIL. WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950609003811995060900381NM 1995 6 9 DL757952053 119950503A5754 TE WEDGE BOEING757 757232 1384965NM NR 3 LE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 LEFT WING NR 3 L/E SLAT TRAILING EDGE WEDGE, WAS DAMAGED BY HAIL. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950609003821995060900382NM 1995 6 9 DL757952054 119950503A5754 TE WEDGE BOEING757 757232 1384965NM NR 9 LE SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 RT WING NR 9 L/E SLAT TRAILING EDGE WEDGE, WAS FOUND WITH HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950609003831995060900383NM 1995 6 9 DL757952056 119950503A5755 SKIN BOEING757 757232 1384965NM LT SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 NR 1 SPOILER PANEL, WAS FOUND WITH HAIL DAMAGE TO UPPER SKIN. REPAIRED AREA PER SRM 51-70-17. 2L72 4F RTA2NM 19950609003841995060900384NM 1995 6 9 DL757952057 119950503A5755 SKIN BOEING757 757232 1384965NM LT SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 NR 4 SPOILER PANEL, WAS FOUND WITH HAIL DAMAGE TO UPPER SKIN. REPAIRED PER SRM 51-70-17 AND ERA 270835-14. 2L72 4F RTA2NM 19950609003851995060900385NM 1995 6 9 DL757952058 119950503A5755 SKIN BOEING757 757232 1384965NM LT SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 NR 5 SPOILER PANEL WAS FOUND WITH HAIL DAMAGE TO UPPER SKIN. REPAIRED PER SRM 51-70-17, 57-70-01 AND ERA 270835-14. 2L72 4F RTA2NM 19950609003861995060900386NM 1995 6 9 DL757952059 119950503A5755 SKIN BOEING757 757232 1384965NM NR 6 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 NR 6 SPOILER PANEL, WAS FOUND WITH HAIL DAMAGE TO UPPER SKIN. REPAIRED PER SRM 57-70-01. 2L72 4F RTA2NM 19950609003871995060900387NM 1995 6 9 DL757952268 119950509A5414 PLATE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 716504 AT HMV, THE NR 2 PYLON WAS FOUND TO BE CRACKED AT THE UPPER FWD CORNER OF THE O/B PLATE OPENING. THE CRACK WAS ROUTED OUT PER SRM 54-51-01. HFEC FOUND NO DEFECTS. REPAIR DOUBLER DRILLED UP AND INSTALLED PER SRM 54-51-01. 2L72 4F4 FRTA2NM E17NE 19950609003881995060900388NM 1995 6 9 DL757952269 119950509A5414 PLATE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 716504 AT HMV, THE NR 2 PYLON WAS FOUND TO HAVE TWO CRACKS ON THE UPPER FWD CORNER OF THE I/B PLATE OPENING. THE DAMAGE WAS REMOVED AND HFEC OF AREA CHECKED OK. REPAIR DOUBLERS WERE DRILLED UP AND INSTALLED PER SRM 54-51-01. 2L72 4F4 FRTA2NM E17NE 19950609003891995060900389NE 1995 6 9 DL76P952466 219950602A7230 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO11140LL5798 25988 724688 ON CLIMBOUT AT 500, NR 2 ENGINE HAD COMPRESSOR STALL, AND EGT OVERTEMP TO 735 DEGREES. REDUCED ENGINE POWER AND RETURNED TO JFK. ENGINE WAS REPLACED AND ROUTED TO SHOP. ETOPS UNSCHEDULED ENGINE REMOVAL. 2L72 4F4 FRTA1NM E24NE 19950609003901995060900390NM 1995 6 9 DL76S952463 119950603A3610 PNEUMATIC SYS BOEING767 767332 1382001NM NR 2 ENGINE CONTAMINATED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11120DL 23279 ON TAKEOFF AND CLIMB, HAD SMOKE ODOR AND FUMES IN MID GALLEY LAV AREA, RETURNED FLT TO ATL. FOUND COMPRESSOR WASH FLUID CONTAMINATION IN NR 2 ENGINE INLET. RAN ENGINE UNTIL ODOR WAS GONE, RETURNED TO SERVICE. 2L72 4F RTA1NM 19950609003911995060900391WP 1995 6 9 DLL10952276 119950526A3246 WHEEL BEARING 48385 LKHEED1011 10113851 5265010WP LT MLG FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11735D 193C1226 ON ROLL INTO LETTER CHECK INSPECTION, FOUND METAL BETWEEN NR 2F WHEEL AND BRAKE ASSY. UPON FURTHER INVESTIGATION FOUND INNER AND OUTER WHEEL BEARING DISINTEGRATED AND INNER BEARING RACE SEIZED ON AXLE. AXLE WAS FOUND DAMAGED AND WAS REPLACED PER MM. 2L73 4F A23WE 19950609003921995060900392WP 1995 6 9 DLL13952282 119950510A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 297-313 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND CORROSION ON FLANGES OF SEAT TRACK BETWEEN FS 297 TO 313 RBL 30, FWD GALLEY. REPLACED SEAT TRACK PER SRM 53-21-00 PG 836-840. 2L73 4F A23WE 19950609003931995060900393WP 1995 6 9 DLL13952283 119950511A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 729-709 DISBODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND THE FAIL STRAP BETWEEN FORMER FS 729 TO 709 AT STR 29 DISBONDED. REMOVED CORROSION PER SRM 51-21-01, WITHIN NEGLIGIBLE LIMITS PER SRM 53-31-00 FIG 801. TREATED AND PAINTED PER SRM 51-21-02, REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950609003941995060900394WP 1995 6 9 DLL13952284 119950511A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 865 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND FAILSAFE STRAP DISBONDED BETWEEN STR 28 AND 29 AFT SIDE OF FORMER FS 865. CUT TEARSTRAP, REMOVED ADHESIVE, NO CORROSION FOUND. CHECKED NEGLIGIBLE DAMAGE LIMITS PER SRM AND FOUND TO BE WITHIN LIMITS REF SRM 53-31-00. INSTALLED REPAIR PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950609003951995060900395WP 1995 6 9 DLL13952285 119950511A5400 ANGLE LKHEED1011 10113851 5265010WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FT AFT OF THE NR 2 INLET FS 1705, 3 0'CLOCK POSITION, INSIDE OVAL ACCESS OPENING. REMOVED CRACKED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00 PG 805. 2L73 4F A23WE 19950609003961995060900396WP 1995 6 9 DLL13952286 119950511A5400 ANGLE LKHEED1011 10113851 5265010WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND AN ANGLE CRACKED 6 FEET AFT OF NR 2 INLET, LT SIDE, 9 O'CLOCK POSITION, ON FWD SIDE OF BULKHEAD RING. REMOVED ANGLE, FABRICATED T-ANGLE AND FILLER PER SRM 54-12-00. 2L73 4F A23WE 19950609003971995060900397WP 1995 6 9 DLL13952308 119950511A5313 STRINGER LKHEED1011 10113851 5265010WP FS 328 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INSPECTION FOUND STRINGER 33 CORRODED AT FS 328. REMOVED STR FROM STA 278 TO 328, FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-13-00 PG 806 FIG 804. 2L73 4F A23WE 19950609003981995060900398WP 1995 6 9 DLL16952460 119950530A2410729640 IDG LKHEED1011 10113853 5265020WP NR 1 ENGINE FAILED A DALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11763DL 193Y1197 ON CLIMBOUT, NR 1 GEN BREAKER OPEN LIGHT CAME ON, GENERATOR WOULD NOT PARALLEL, LANDED LGW. REPLACED NR 1 IDG, OPERATION NORMAL. 2L73 4F A23WE 19950609003991995060900399NM 1995 6 9 DLM88952288 119950526A5320 RIB DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11971DL 53214 FOUND DURING E-1 LETTER CHECK, CRACK AT KEEL BEAM CROSSOVER RIB. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950609004001995060900400NM 1995 6 9 DLM88952289 119950526A5320 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11971DL 53214 FOUND DURING E-1 LETTER CHECK, CRACK AT WHEEL WELL FWD FRAME O/B, LT WHEEL WELL. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950609004011995060900401NM 1995 6 9 DLM88952461 119950601A323159359731 ARM DOUG MD88 MD88 3023688NM LT MLG DOOR FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11961DL 49980 ON CLIMBOUT FROM IAH, MAIN GEAR DOOR OPEN MESSAGE WOULD NOT GO OUT, DIVERTED DFW. FOUND LEFT INBOARD FLAP INBOARD HINGE WITH BROKEN ARM. THE ARM WAS LODGED IN GEAR DOOR PREVENTING IT TO CLOSE FULLY. REPLACED ARM, OPERATION NORMAL. 2L72 4F RTA6WE 19950609004021995060900402WP 1995 6 9 QXEA9500165 219950526A721031011607 SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP GEARBOX DETERIORATED A QXEAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09380PH 595 P44319 SEA - CABIN FILLS WITH SMOKE WHEN NR 2 BLEED IS SELECTED ON. REPLACED NR 2 ENGINE GEARBOX CARBON SEAL IAW MAINT MANUAL. NR 2 BLEED AIR OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA8SW E4WE 19950609004031995060900403NM 1995 6 9 UPS203428 119950601A5753 SKIN BOEING727 72727C 138400JNM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01910UP 19117 MAINTENANCE REPORTED, RT I/B FLAP HAS EDGE DELAMINATION AT 19, 26, 39, 43, 51. INSTALLED REPAIR PER E/O B727-5750-3081C. 2L73 4F A3WE 19950609004041995060900404NM 1995 6 9 UPS203429 119950602A3230 LOCK ASSY BOEING727 727108C 1384039NM NLG LACK OF LUBE A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01936UP 19503 PILOT REPORTED, NOSE GEAR FAILED TO EXTEND ON FINAL, CYCLED GEAR PER AOM AND GEAR OPERATED NORMAL. CLEANEDAND INSPECTED UPLOCK ASSY, LUBRICATED PER MM 12-21-11. 2L73 4F A3WE 19950609004051995060900405NM 1995 6 9 UPS203431 119950606A5753 FIBERGLASS BOEING727 72725C 138400HNM LT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 MAINTENANCE FOUND LEFT WING I/B FLAP FIBERGLASS DELAMINATED FROM T/E OF MID FLAP. REPAIRED IAW B727-5750-6197B. 2L73 4F A3WE 19950609004061995060900406NM 1995 6 9 UPS403430 119950530A3350900835A EEL BATT PACK BOEING747 747123F NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 (SUPPLEMENTAL MRR) MAINTENANCE REPORTED THAT ON PRE-FLIGHT, THE EMERGENCY EXIT SIGN ABOVE THE CREW SERVICE DOOR WOULD NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. WORKS OK. 2L74 4F A20WE 19950609004621995060900462NM 1995 6 9 AWXA9500322 119950522A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 13 AFT. REPAIRED BROKEN WIRE AT ROW 13, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950609004631995060900463NM 1995 6 9 AWXA9500329 119950526A5320654587545 ANGLE BOEING737 7372E3 NM R1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28138AW 22792 PHX - DURING SCHEDULED C14 INSPECTION, FOUND 'L' ANGLE CORRODED AT R1 ENTRY THRESHOLD. REMOVED AND REPLACED THRESHOLD CHORD IAW SRM 51-30-2. (W) 2L72 4F RTA16WE 19950609004641995060900464NM 1995 6 9 AWXA9500330 119950526A53206517688125 ANGLE BOEING737 7372E3 NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28138AW 22792 PHX - DURING SCHEDULED C14 INSPECTION, FOUND 'L' ANGLE CORRODED AT L1 ENTRY. REMOVED AND REPLACED L1 DOOR CHORD IAW SRM 51-30-2. (W) 2L72 4F RTA16WE 19950609004651995060900465NM 1995 6 9 AWXA9500331 119950526A53151505101168 FLOORBEAM BOEING737 7372E3 NM FS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28138AW 22792 PHX - DURING SCHEDULED C14 INSPECTION, FOUND TOP OF FLOORBEAM CORRODED AT STATION 312, APPROXIMATELY 12 INCHES LEFT OF BL 0. REPAIRED FLOORBEAM IAW SRM 53-10-9, FIGURE 5. (W) 2L72 4F RTA16WE 19950609004661995060900466EU 1995 6 9 SIMA951451 119950525A2710S2711009100000 BELLCRANK AEROSPATR42 ATR42300 8680920EU LT AILERON LACK OF LUBE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21430MQ 0136 MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND THE INBOARD BELLCRANK ON THE LEFT AILERON TO HAVE A DRY BEARING. THE BELLCRANK WAS REMOVED AND INSPECTED AND A FUNCTIONAL CHECK OF THE AILERON SYSTEM WAS COMPLIED WITH IAW EO E9-2700-001. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609004671995060900467EU 1995 6 9 SIMA951452 119950525A2710S2711001400100 IDLER LEVER AEROSPATR42 ATR42300 8680920EU RT AILERON LOOSE BEARING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21430MQ 0136 MQT - DURING BRIDGE INSPECTION AND COMPLIANCE OF EO E9-2700-001, MAINTENANCE FOUND THE FIFTH FROM INBOARD IDLER LEVER ON THE RIGHT WING TO HAVE EXCESSIVE PLAY IN THE BEARING. THE IDLER LEVER WAS REMOVED AND INSPECTED AND A FUNCTIONAL CHECK OF THE AILERON SYSTEM WAS COMPLIED WITH IAW EO E9-2700-001. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609004681995060900468EU 1995 6 9 SIMA951453 119950525A532057112241000260 FITTING AEROSPATR42 ATR42300 8680920EU WING/FUS CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21424MQ 045 SAT - DURING A 24K CYCLE INSPECTION, MECHANICS DISCOVERED A .375 INCH LONG CRACK ON THE FRAME 27L WING TO FUSELAGE SUPPORT FITTING. THE FITTING WAS RE-WORKED BY INSTALLING A BUSHING AS PER ATR DRAWING 15S535RO137. INTEGRITY OF REPAIR WAS VERIFIED BY EDDY CURRENT INSPECTION. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609004691995060900469EU 1995 6 9 SIMA951454 119950525A532053171122201 FRAME AEROSPATR42 ATR42300 8680920EU RT WINDSHIELD CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21424MQ 045 SAT - DURING A 24K CYCLE INSPECTION, MECHANICS FOUND A .25 INCH LONG CRACK IN THE RT WINDSHIELD LOWER CORNER NODE 5. THE CRACK WAS REWORKED BY REPEATING BLENDING IAW ATR DRAWING 11S531RO128. SURFACE WAS SHOT PEENED AND RE-COATED. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609004701995060900470EU 1995 6 9 SIMA951461 119950526A6120 CONNECTOR SAAB SF340 SF340A 7850100EU AUTO COARSEN LOOSE A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2191MQ 340A091 DFW - FLT 3871 - AUTO COARSENING FAILED AFTER TAKEOFF. FOUND LOOSE CANNON PLUG ON CTOT PANEL. TIGHTENED PLUG SYSTEM. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (W) 2L72 4T RTA52EU 19950609004711995060900471NE 1995 6 9 SIMA951481 219950528A73203033515 NH SENSOR BOEING737 7373G7 1384595NM PWA PW120 PW127 NE NR 2 ENGINE MALFUNCTIONED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21309AW 24711 127077 FWA - FLT 4393 - NR 2 ENGINE TORQUE SURGE DURING CLIMB. REMOVED AND INSPECTED NR 2 ENGINE NH SENSOR, IAW MM 72-00-00. PERFORMED GROUND PERFORMANCE RUNS. AIRCRAFT RELEASED FOR SERVICE. (W) 2L72 4F4 TRTA16WE E20NE 19950609004721995060900472NE 1995 6 9 SIMA951501 219950530A7320311479301A HARNESS AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 1 ECU CHAFED A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21427MQ 84432 091 121114 ORD - FLT 4047 - NR 1 ECU FAULTED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE HARNESS. OPS CHECK ON GROUND GOOD, IAW JIC 73-23-61 RUNUP PROCEDURES. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T4 TRTA53EU E20NE 19950609004731995060900473EU 1995 6 9 SIMA951502 119950530A3030E0308028C0 RELAY AEROSPATR72 ATR72212 EU PITOT HEAT FAILED A SIMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW21447AM 447 DFW - FLT 3831 - DURING TAXI-OUT F/O'S PITOT HEAT FAULT LIGHT CAME ON. AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED CURRENT SENSING RELAY 33DA. AIRCRAFT RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609004741995060900474NM 1995 6 9 USAA950441 119950501A5610 WINDSHIELD BOEING757 757225 1384959NM RIGHT DEFECTIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19606AU 22202 STL - FLT 1143 - THE FIRST OFFICERS OUTER WINDOW SHATTERED WHILE IN FLIGHT. THE FLIGHT DIVERTED TO STL. MAINTENANCE REPLACED THE FIRST OFFICERS WINDSHIELD AND REPLACED THE RIGHT WINDSHIELD HEAT CONTROLLER, P/N 6240665. 2L72 4F RTA2NM 19950609004751995060900475NM 1995 6 9 USAA950447 119950427A521065907373382 SEAL BOEING737 7373B7 1384580NM L2 DOOR LEAKING A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19395US 23317 LAX - FLT 2139 - AIR LEAK FROM MAIN ENTRANCE DOOR AFTER TAKEOFF. FLIGHT RETURNED TO LAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FORWARD ENTRY DOOR SEAL. OPS AND LEAK CHECK OK. (W) 2L72 4F RTA16WE 19950609004761995060900476NM 1995 6 9 USAA950448 119950429A7930 CIRCUIT BREAKER BOEING737 737301 1384611NM LT ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA19592US 23937 PHL - FLT 941 - FLIGHT EN ROUTE BOS TO DCA, WHEN NR 1 ENGINE OIL TEMPERATURE AND PRESSURE INDICATORS DROPPED TO ZERO. CREW SHUT DOWN NR 1 ENGINE AND DIVERTED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE RESET D8 CIRCUIT BREAKER. ALL ENGINE INDICATIONS NORMAL. (W) 2L72 4F RTA16WE 19950609004771995060900477NM 1995 6 9 USAA950458 119950507A335020131A EEL BATTERY PACK BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19426US 24548 CLT - EXTERIOR EXIT LIGHTS BY AFT OVERWING EXITS ON BOTH SIDES OF AIRCRAFT ARE INOPERATIVE. MAINTENANCE RELEASED ON MEL 33-14. REPLACED BATTERY PACKS ON EMERGENCY LIGHTS. SYSTEM OPS CHECK GOOD. REMOVED MEL. (W) 2L72 4F RTA16WE 19950609004791995060900479NM 1995 6 9 USAA950461 119950508A3350 EEL FUSE BOEING737 737401 1384701NM CABIN INOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19408US 23878 PVD - ROWS 10, 11, 12L AISLE MARKER EMERGENCY LIGHTS INOPERATIVE AND EMERGENCY LIGHT FOR LEFT ESCAPE WINDOW INOPERATIVE. MAINTENANCE REPLACED FUSE IN BATTERY PACK M1479 AT STATION 598. (W) 2L72 4F RTA16WE 19950609004801995060900480WP 1995 6 9 USAA950464 119950417A5320991556171 ANGLE DOUG DC9 DC981 3022081WP BS 1338 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROSION REF CPCP TASK NR C58-53300 FLOORBEAM TOP ANGLE STATION 1338 RIGHT LAV. ACCOMPLISHED SPLICE REPAIR FLOORBEAM AND REPLACED ANGLE PER USAIR TYPICAL REPAIR 53-10-14. (W) 2L72 4F A6WE 19950609004811995060900481WP 1995 6 9 USAA950465 119950417A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1416 CRACKED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND .75 INCH CRACK RT AND 1 INCH CRACK LT STATION 1416 LONGERON 4 AND 5 RIGHT AND 4 AND 5 LEFT. INSTALLED TEMPORARY REPAIR PER USAIR EA 30225 AND SRM 53-03 FIG 30. (W) 2L72 4F A6WE 19950609004821995060900482WP 1995 6 9 USAA950466 119950417A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1401-1418 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND CHAFED AREA STATION 1401-1418 LONGERON 8 LEFT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950609004831995060900483WP 1995 6 9 USAA950467 119950417A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19825US37344 49237 PIT - DURING Q-6 CHECK INSPECTION, FOUND CRACK 1.25 INCHES LEFT UPPER FORWARD CORNER OF MAIN ENTRANCE DOOR FUSELAGE SKIN (X-RAY INSPECTION). CUT OUT DAMAGED AREA AND INSTALLED FILLER EXTERNAL DOUBLERS PER SRM 53-05 FIG 26. (W) 2L72 4F A6WE 19950609004841995060900484WP 1995 6 9 USAA950468 119950417A5347 TRACK DOUG DC9 DC981 3022081WP LT COCKPIT ELONGATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED CAPTAINS AFT OUTBOARD SEAT TRACK. INSTALLED SET TRACK REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A. (W) 2L72 4F A6WE 19950609004851995060900485WP 1995 6 9 USAA950469 119950417A5347 TRACK DOUG DC9 DC981 3022081WP RT COCKPIT ELONGATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND HOLES ELONGATED FLIGHT OFFICER AFT OUTBOARD SEAT TRACK. INSTALLED REPAIR KIT PER USAIR TYPICAL REPAIR 53-20-06 REV A. (W) 2L72 4F A6WE 19950609004861995060900486WP 1995 6 9 USAA950470 119950417A5330 SKIN DOUG DC9 DC981 3022081WP BS 296 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND DENT 2.375 INCH BY 1.75 INCH BY .080 INCH DEEP STATION 296 BETWEEN LONGERON 24L AND 23L. CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38. (W) 2L72 4F A6WE 19950609004871995060900487WP 1995 6 9 USAA950471 119950417A5330 SKIN DOUG DC9 DC981 3022081WP BS 484 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH BY 2 INCH BY .030 INCH DEEP DENT STATION 484 BETWEEN LONGERON 21L AND 22L. CUT OUT DAMAGED AREA AND INSTALLED INTERNAL FINGER DOUBLER REPAIR PER SRM 53-04 FIG 38 VIEW L. (W) 2L72 4F A6WE 19950609004881995060900488WP 1995 6 9 USAA950472 119950417A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT -DURING Q-6 CHECK INSPECTION, FOUND .75 INCH CRACK STATION 160 LONGERON 4 LEFT. SPLICED NEW SECITON OF LONGERON IN PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950609004891995060900489EU 1995 6 9 USAA950480 119950427A5312 ANGLE FOKKERF28 F28MK4000 4990810EU FWD PRES BLKD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19493US29263 11161 PIT - DURING FC- CHECK INSPECTION, FOUND 4 INCH CRACK BETWEEN STRINGER 72 AND 74 AFT SIDE OF FORWARD PRESSURE BULKHEAD CONNECTION ANGLE. SIP INSPECTION REF 53-10-06. STOP DRILLED CRACK FABRICATED AND INSTALLED NEW CONNECTION ANGLE DOUBLER PER SRM 53-11-08 PG 2. (W) 2L72 4F RTA20EU 19950609004901995060900490EU 1995 6 9 USAA950481 119950427A5530 ANGLE FOKKERF28 F28MK4000 4990810EU VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19493US29263 11161 PIT - DURING FC-2 CHECK INSPECTION, FOUND 5 .125 INCH LONG CRACKS, 3 IN VERTICAL STAB CONNECTION ANGLE INTERMEDIATE SPAR II AND 2 IN INTERMEDIATE SPAR I CONNECTION ANGLE RT. CONFIRMED VISUAL BY EDDY CURRENT. REMOVED DAMAGED AREA, INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-31-00 PG 2. (W) 2L72 4F RTA20EU 19950609004911995060900491WP 1995 6 9 USAA950482 119950503A53205912528501 PAN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19952VJ57006 47574 IND - DURING CX-2 INSPECTION, FOUND A .25 INCH CRACK AND CORROSION THE AFT CARGO DOOR LOWER SILL DOOR JAM PAN STATION 732 TO 749 AT LONGERON 28R. REMOVED CORROSION AND CRACKED AREA AND ACCOMPLISHED PAN SPLICE REPAIR PER SRM 53-05 FIG 44. (W) 2L72 4F A6WE 19950609004921995060900492WP 1995 6 9 USAA950483 119950506A5313 LONGERON DOUG DC9 DC931 3022065WP FS 68 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19962VJ63809 47507 PIT - WHILE ACCOMPLISHING PRODUCTION CONTROL ITEM 949, FOUND A .5 INCH CRACK RADIALLY IN LONGERON 2R STATION 680 VISUAL INSPECTION. ACCOMPLISHED SPLICE REPAIR PER SRM53-02 FIG 2 AND USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950609004931995060900493WP 1995 6 9 USAA950486 119950419A5313 LONGERON DOUG DC9 DC931 3022065WP BS 408 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19916VJ67447 47023 IND - DURING CX-2 INSPECTION ACCOMPLISHED SID INSPECTION PSE REF 53.09.001, FOUND .5 INCH CRACK ACROSS LONGERON AT STATION 408 LONGERON 17 RIGHT. ACCOMPLISHED LONGERON SPLICE REPAIR PER SRM 53-02 PG 2A AND USAIR EA 30247. (W) 2L72 4F A6WE 19950609004941995060900494WP 1995 6 9 USAA950487 119950419A5330 SKIN DOUG DC9 DC931 3022065WP BS 775 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19916VJ67447 47023 IND - DURING SCHEDULED PRODUCTION CONTROL ITEM NR 949, FOUND .125 INCH CRACK IN SKIN OF RIVET STATION 775 LONGERON 1 RT. EDDY CURRENT INSPECTION. ACCOMPLISHED REPAIR IAW SRM 53-04. (W) 2L72 4F A6WE 19950609004951995060900495NM 1995 6 9 USAA950514 119950426A5311 FRAME BOEING737 7372B7 1384560NM BS 500 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19267AU34647 22879 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA .5 INCH BY .5 INCH STATION 500 RT. REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950609004961995060900496NM 1995 6 9 USAA950516 119950426A5311 FRAME BOEING737 7372B7 1384560NM BS 500 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19267AU34647 22879 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 2 INCH BY 2 ICH F/S 500 A RT S-26 R. REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950609004971995060900497NM 1995 6 9 USAA950517 119950417A5320654587545 ANGLE BOEING737 7372B7 1384560NM BS 302-322 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19267AU34647 22879 INT - DURING 'Q-1' CHECK VISUAL INSPECTION, FOUND 20 INCH BY 1 INCH AREA OF CORROSION FORWARD SERVICE DOOR 'Z' ANGLE STATION 302 TO 322, WL 208. REPAIRED PER BOEING DRAWING NR 65-45875 SRM 51-10-1 PG 5. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950609004981995060900498EU 1995 6 9 USAA950521 119950517A2421CAN4214 GEN SHAFT FOKKERF28 F28MK4000 4990810EU NR 1 ENGINE LEAKING A USAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 EA19486US 11237 EVV - FLT 0689 - ON DESCENT TO EVV, CREW RECEIVED FLUCTUATING OIL PRESSURE ON THE NR 1 ENGINE THEN RECEIVED A CAWS WARNING. AN EMERGENCY WAS DECLARED. THE CREW SHUTDOWN THE NR 1 ENGINE. SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE REMOVED THE OIL FILTER AND SCREWS TO CHECK FOR MATERIAL. ALL CHECKED GOOD. THEY FOUND THE OIL LEAK TO BE COMING FROM THE GENERATOR. THE SHAFT AND SEAL ASSEMBLY WAS REPLACED. OPERATIONAL CHECKED NORMAL. (W) 2L72 4F RTA20EU 19950609004991995060900499WP 1995 6 9 USAA950525 119950512A335060030451LB EEL POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19820US 49119 CAE - THE EMERGENCY LIGHTS WOULD NOT SHUT OFF. MAINTENANCE REPLACED THE POWER SUPPLY. (W) 2L72 4F A6WE 19950609005001995060900500NE 1995 6 9 9508886304 219950605A7200 ENGINE BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 4 FAILED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL K FLUID LOSS CRCRUISE 1 GL01664US 23819 717579 DURING CRUISE, THE NR 4 ENGINE BEGAN LOSING OIL QUANTITY AND WHEN PRESSURE BEGAN TO DROP THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO NRT WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE AND 165,000 LBS OF FUEL WAS DUMPED. METAL WAS FOUND ON THE MAG PLUGS AND THE ENGINE WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 19950609005011995060900501WP 1995 6 9 9508899988 119950601A5270 SWITCH DOUG DC9 DC931 3022065WP STAIRWAY DOOR OUT OF ADJUST A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018944E 47167 AFTER TAKEOFF MSP-DFW AT APPROXIMATELY 6000 FEET MSL, THE FORWARD STAIRWAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. ADJUSTED THE SWITCH PER MM 52-62-0 PG 501, OPERATIONAL CHECK OK. 2L72 4F A6WE 19950609005021995060900502WP 1995 6 9 9508909311 119950530A2910 HYD LINE DOUG DC9 DC982 3022082WP RT HYD SYST BROKEN A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01314RC 49110 RIGHT HYDRAULIC SYSTEM QUANTITY WENT TO ZERO ON APPROACH, LANDED WITH MAIN GEAR DOORS OPEN. FOUND AUXILIARY PUMP PRESSURE LINE LEAKING INTERNALLY. REPLACED LINE AND SERVICED TO PROPER LEVEL. ALSO, REPLACED MAIN GEAR DOORS DUE TO DAMAGE INCURRED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005031995060900503WP 1995 6 9 9508919871 119950605A2150 PACK DOUG DC9 DC951 3022051WP LEFT FAILED A NWAAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 GL01780NC 48102 AFTER TAKEOFF AT 11,000 FEET, LEFT AIR CONDITIONING PACK OVERHEATED AND SHUT ITSELF DOWN. CABIN FILLED WITH A LIGHT FOG SMOKE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THERMOSTAT, ANTICIPATOR, TEMPERATURE CONTROLLER, TEMPERATURE SENSOR, AND COCKPIT SENSOR. ALL WERE UNSUCCESSFUL IN CORRECTING THE PROBLEM. DEFERRED PER MEL 21-30A, LEFT PACK INOP IN AUTO. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005041995060900504WP 1995 6 9 9508929916 119950604A3260 SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01949N 47566 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOOR SWITCH. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005051995060900505WP 1995 6 9 9508939916 119950603A3260 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG DOOR LOOSE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01949N 47566 DURING CLIMBOUT FROM MSP, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND AIRCRAFT LANDED WITHOUT INCIDENT. RESEATED LEFT MAIN GEAR DOOR SWITCH CANNON PLUG. OPERATIONAL CHECK OK ON GEAR DOOR CYCLE. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005061995060900506WP 1995 6 9 9508949916 119950604A3260 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG DOOR LOOSE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01949N 47566 DURING CLIMBOUT FROM BWI, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND LEFT MAIN GEAR DOOR SWITCH CANNON PLUG NOT SEATED PROPERLY. RESEATED CANNON PLUG. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005071995060900507WP 1995 6 9 9508959964 119950602A2130 HEAT EXCHANGER DOUG DC9 DC931 3022065WP AFT ACCESS COMP INOPERATIVE A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01912RW 47150 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN ALTITUDE WAS CLIMBING AT AN EXCESSIVE RATE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED HEAT EXCHANGER. LEAK AND OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005081995060900508WP 1995 6 9 9508969990 119950604A3260 GEAR LIGHT DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL018950E 47186 NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO MSP. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. FLIGHT LANDED WITHOUT INCIDENT. LUBED NOSE LANDING GEAR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950609005091995060900509NM 1995 6 9 DHL95702002 119950601A2120652536411 DUCT BOEING727 72730C 1384009NM APU FAILED A TDHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01702DH 19793 RIGHT PACK WILL NOT MAINTAIN A 10,000 FOOT CABIN IN AUTO OR MANUAL MODE WITH CARGO HEAT OUTFLOW VALVE CLOSED AND MIX VALVE AT HALF POSITION. CABIN CLIMBED AT 1200 FPM. ACCOMPLISHED ALTERNATE PROCEDURE PER AOM 5.02. REPLACED APU AIR DUCT. OPS CHECK GOOD PER M/M 21-20. 2L73 4F A3WE 19950609005101995060900510NM 1995 6 9 DL72E952416 119950602A5754 SKIN BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 FOUND DURING F-1 LETTER CHECK, .375 INCH CRACK ON COVE SKIN SUPPORT ANGLE, NR 7 SLAT AT THERMAL ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950609005111995060900511NM 1995 6 9 DL72E952417 119950602A5754 SLAT BOEING727 727247 138408FNM NR 7 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 FOUND DURING F-1 LETTER CHECK, .75 INCH CRACK AT NR 7 SLAT UNDER I/B STOP FITTING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950609005121995060900512NM 1995 6 9 DL72E952456 119950531A5347 SEAT TRACK BOEING727 727247 138408FNM FS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK LBL 24 AT STA 380. REPAIRED BY REPLACING SEAT TRACK FROM STA 380 TO 400 PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950609005131995060900513NM 1995 6 9 DL72E952457 119950531A5347 SEAT TRACK BOEING727 727247 138408FNM FS 344-380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK RBL 56 FROM STA 344 TO 380. REPAIRED PER SRM 53-10-5 FIG 9. 2L73 4F A3WE 19950609005141995060900514NM 1995 6 9 DL72E952458 119950531A5347 SEAT TRACK BOEING727 727247 138408FNM FS 1070-1090 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK, CORROSION ON SEAT TRACK AT RBL 45 BETWEEN STA 1070 AND 1090. REPAIRED SEAT TRACK AS PER SRM 53-10-5 FIG 7. 2L73 4F A3WE 19950609005151995060900515NM 1995 6 9 DL72E952459 119950601A5347 SEAT TRACK BOEING727 727247 138408FNM FS 344-380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK, REF NR 42 CORROSION ON SEAT TRACK RBL 56 FROM FS 344 TO 380. REPAIRED PER SRM 53-10-5. 2L73 4F A3WE 19950609005161995060900516NM 1995 6 9 DL72L952469 119950605A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11512DA 21314 NR 7 SLAT COVE SKIN ATTACH ANGLE UNDER TAI DUCT CRACKED 1 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950609005171995060900517NM 1995 6 9 DL72L952470 119950605A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11512DA 21314 A .5 INCH CRACK NR 3 SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950609005181995060900518NM 1995 6 9 DL72L952471 119950605A5754 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11512DA 21314 THE NR 7 SLAT ACTUATOR ATTACH NOSE RIB LWR SIDE AFT CRACKED .5 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PAR 3B. 2L73 4F A3WE 19950609005191995060900519NM 1995 6 9 DL72L952481 119950605A5330 SKIN BOEING727 727232 1384082NM PAX DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11512DA 21314 FOUND ON A1 LTR CK, 1.125 INCH CRACK AT MAIN ENT DOOR UPPER HINGE CUTOUT. REPAIR PER M/M 53-30-0 AND ERA 301886-14. 2L73 4F A3WE 19950609005201995060900520NM 1995 6 9 DL72S952412 119950514A5320 ANGLE BOEING727 727232 1384082NM NR 2 COWL WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, THE NR 2 ENGINE FWD COWLING CLOSEOUT RIM AT STA 1352 IS DAMAGED AND WORN FROM 5 TO 7 O'CLOCK POSITION. REPAIRED PER MM 53-11-0 PAGE 801. 2L73 4F A3WE 19950609005211995060900521NM 1995 6 9 DL72S952413 119950529A5330 SKIN BOEING727 727232 1384082NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 CORROSION ON SKIN AFT OF STA 720 BETWEEN STR 28L AND 28R. REPAIRED PER SRM 53-30-3 FIG 1, FOUND AT HMV. 2L73 4F A3WE 19950609005221995060900522NM 1995 6 9 DL72S952427 119950529A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 THE LEFT AND RIGHT NLG TRUNNION BEARING FITTINGS HAD CORROSION ON THE FACES AND THE BORES. CORROSION REMOVAL RESULTED IN THE LT BORE ID 2.608, RT BORE ID 2.5885, UPPER FITTING SPOT FACED THICKNESS IS 1.506, CAP SPOT FACED THICKNESS IS 1.460. ALL CORROSION REMOVAL WITHIN TOLERANCE PER M/M 53-40-00. ALL REWORKED AREAS DYE CHECKED AND ROTO PEENED PER P/S 900-4 NR 5. BUSHING MFG AND INSTALLED PER M/M 53-40-0. 2L73 4F A3WE 19950609005231995060900523NM 1995 6 9 DL72S952434 119950513A5320 CLIP BOEING727 727232 1384082NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 SKIN CLIP CORRODED FS 720 FRAME FWD SIDE BETWEEN STR28L AND R. REPAIRED PER MM 53-11-0 FIG 815, FOUND AND REPAIRED AT HMV. 2L73 4F A3WE 19950609005241995060900524NM 1995 6 9 DL72S952465 119950513A5311 FRAME BOEING727 727232 1384082NM FS 560 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND TOP OF FRAME CRACKED AT STA 560, 6 INCHES RBL ABOVE INTERCOSTAL. FABRICATED AND INSTALLED REPAIR PER ERA 301859-14. 2L73 4F A3WE 19950609005251995060900525NM 1995 6 9 DL72S952479 119950502A5753 THRUST BEARING 652163362 BOEING727 727232 1384082NM NR 4 TE MIDFLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA BN334 22494 DURING HMV FOUND CORROSION, I/B THRUST BEARING BORE NR 4 MIDFLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950609005261995060900526NM 1995 6 9 DL72S952480 119950504A5753 RIB 652163362 BOEING727 727232 1384082NM NR 4 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA BN334 22494 DURING SHOP INSPECTION, THE I/B AFT RIB WAS FOUND CRACKED AT BOTTOM AFT CORNER. REPAIRED PER MM 57-52-0, RT WING NR 4 MIDFLAP. 2L73 4F A3WE 19950609005271995060900527NM 1995 6 9 DL72S952482 119950515A5330 SKIN BOEING727 727232 1384082NM FS 480-680 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV, FOUND NUMEROUS TEMP REPAIRS ON FWD B/B LWR SKIN STA 480 TO 680. INSTALLED AND FABRICATED NEW SKIN PANELS PER SRM 53-30-3. 2L73 4F A3WE 19950609005281995060900528NM 1995 6 9 DL73S952455 119950502A552365C2638425SP SKIN BOEING737 737232 1384475NM LT ELEVATOR TAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11328DL 23100 DURING INITIAL SHOP INSPECTION, MAINTENANCE FOUND A ONE INCH HOLE IN UPPER IB SKIN, 10 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIR WAS ACCOMPLISHED PER ERA 270848-14. ALSO, A 4 INCH DELAMINATED AREA WAS FOUND 14 INCHES FROM INBOARD END. THIS WAS REPAIRED IN ACCORDANCE WITH SRM 51-40-15, FOR LEFT ELEVATOR TAB. 2L72 4F RTA16WE 19950609005291995060900529NM 1995 6 9 DL76S952404 119950601A5753 TE WEDGE BOEING767 767332 1382001NM TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11125DL 24075 FOUND ON I-2 LETTER CHECK, 2 HOLES BOTTOM OF T/E WEDGE FLAP. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950609005301995060900530NM 1995 6 9 DL76S952405 119950601A5753 SKIN BOEING767 767332 1382001NM RT TE FLAP DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11125DL 24075 FOUND ON I-2 LTR CK, DELAMINATION ON RT O/B FLAP LOWER SURFACE. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950609005311995060900531WP 1995 6 9 DLL10952407 119950527A5400 INTERCOSTAL LKHEED1011 10113851 5265010WP NR 2 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, WEB CRACKED 2 INCHES LONG JUST AFT OF NR 2 ENG INLET RING INTERCOSTAL PNL 311AR, 11 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609005321995060900532WP 1995 6 9 DLL10952408 119950527A5400 INTERCOSTAL LKHEED1011 10113851 5265010WP NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, WEB CRACKED 2 INCHES LONG JUST AFT NR 2 ENG INLET RING INTERCOSTAL PNL 311DR, 4 O'CLOCK. REPAIARED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609005331995060900533WP 1995 6 9 DLL10952409 119950527A5400 WEB LKHEED1011 10113851 5265010WP NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, WEB CRACKED 3 EACH THE RIVET BUCKTAIL, EACH APPROX 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311DR, 3 O'CLOCK. REPAIRED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609005341995060900534WP 1995 6 9 DLL10952410 119950527A5400 WEB LKHEED1011 10113851 5265010WP NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, WEB CRACKED 1.5 INCH LONG JUST AFT OF NR 2 ENG INLET RING INTERIOR TO PNL 311NL. REPAIRED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609005351995060900535WP 1995 6 9 DLL10952414 119950602A52421552745165 SKIN LKHEED1011 10113851 5265010WP E/E DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 E AND E DOOR, CORROSION FOUND ON FORWARD SKIN EDGE. REPAIRED PER SRM 52-11-00 FIG 802, FOUND AT HMV. 2L73 4F A23WE 19950609005361995060900536WP 1995 6 9 DLL10952415 119950602A52421552745165 HINGE ARMS LKHEED1011 10113851 5265010WP E/E DOOR WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, E/E DOOR LEFT AND RIGHT AFT HINGE ARMS WORN ON TOP EDGE NEAR CENTER OF ARM. REPAIRED PER SRM 52-11-00 FIG 801. 2L73 4F A23WE 19950609005371995060900537WP 1995 6 9 DLL10952421 119950528A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 519 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FWD B/B 39 AND 40 STA 519. REPAIRED TEAR STRAP AT FS 519 BETWEEN STR 39 AND 40 PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950609005381995060900538WP 1995 6 9 DLL10952422 119950601A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1370 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED ABOVE STR 40 AT FS 1370. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AS PER SRM 53-31-00 FIG 801. REPAIRED PER SRM 53-31-00 FIG 804, TREATED/PAINTED PER MM 51-09-00. 2L73 4F A23WE 19950609005391995060900539WP 1995 6 9 DLL10952423 119950601A5330 SKIN LKHEED1011 10113851 5265010WP FS 1490 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, BONDED SKIN AT FS 1490, OUTBOARD OF STR 39 IS CORRODED. CUT OUT DAMAGE AND REPAIRED PER SRM 53-31-00 FIG 836 PG 965. 2L73 4F A23WE 19950609005401995060900540WP 1995 6 9 DLL10952424 119950531A5330 SKIN LKHEED1011 10113851 5265010WP FS 1473 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, SKIN CORRODED AND TEAR STRAP DISBONDED AT STA 1473, BETWEEN STR 26 TO 27. REPAIRED AREA PER SRM 53-31-00 FIG 836. 2L73 4F A23WE 19950609005411995060900541WP 1995 6 9 DLL10952425 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 759 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED BETWEEN STR 28 AND 29 STA 759. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS AS PER SRM 53-31-00 PG 801. DRILLED UP TEAR STRAP SPLICE REPAIR AS PER SRM 53-31-00 FIG 816. INSTALLED TEAR STRAP SPLICE, TREATED/PAINTED REPAIR AREA. 2L73 4F A23WE 19950609005421995060900542WP 1995 6 9 DLL10952426 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 779 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED AT STA 779 BETWEEN STR 31 TO 32. DRILLED TEAR STRAP AS PER SRM 53-31-00 FIG 816. REPAIRED AREA AS PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950609005431995060900543WP 1995 6 9 DLL10952428 119950520A5311 FORMER LKHEED1011 10113851 5265010WP FS 963 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11722DA 193C1147 TOOLING DAMAGE ON 963 FORMER FLANGE BETWEEN STRINGERS 19 AND 20, ABOVE ELECT LOAD CENTER DOOR. ROUTED OUT DAMAGE AND INSTALLED REPAIRS PER SRM 53-12-00 FIG 815. 2L73 4F A23WE 19950609005441995060900544WP 1995 6 9 DLL10952429 119950526A5320 SUPPORT LKHEED1011 10113851 5265010WP CABIN FLOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11722DA 193C1147 C-2 BB FLOOR SUPPORT CHANNEL CRACKED AT LBL 8.5 AND RBL 8.5. REPAIRED CHANNEL PER SRM 53-24-00. 2L73 4F A23WE 19950609005451995060900545WP 1995 6 9 DLL10952432 119950526A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 349 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FLOOR FRAME CRACKED AT FS 349 LBL 105 BELOW CABIN FLOOR AT WL 180. REPAIRED PER SRM 53-21-00 FIG 817. 2L73 4F A23WE 19950609005461995060900546WP 1995 6 9 DLL10952433 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 599 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED IN C-1 B/B AT FS 599 BETWEEN STR 35 AND 36. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950609005471995060900547WP 1995 6 9 DLL10952435 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1635 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 1635 BETWEEN STR 39 AND 40. REMOVED CORROSION AND FOUND WITHIN LIMITS PER SRM 53-31-00 FIG 801, TREATED AND PAINTED. INSTALLED TEAR STRAP REPAIR PER SRM 53-31-00 FIG 830. 2L73 4F A23WE 19950609005481995060900548WP 1995 6 9 DLL10952436 119950526A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1565 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FUSELAGE FAIL-SAFE STRAP DISBONDED AT STR 40 FS 1565. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950609005491995060900549WP 1995 6 9 DLL10952437 119950527A5400 WEB LKHEED1011 10113851 5265010WP NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, WEB CRACKED 1 INCH LONG JUST AFT NR 2 ENG INLET RING INTERIOR TO PNL 311RL. REPAIRED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609005501995060900550WP 1995 6 9 DLL10952438 119950526A5311 FORMER LKHEED1011 10113851 5265010WP FS 1063 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FORMER CRACKED LOCATED FS 1063, 1 INCH ABOVE FLOOR LBL. REPAIRED PER SRM 53-12-00 FIG 816. 2L73 4F A23WE 19950609005511995060900551WP 1995 6 9 DLL10952439 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1480-1501 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED AT FS 1480 TO 1501 BETWEEN STR 38 AND 39. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950609005521995060900552WP 1995 6 9 DLL10952440 119950603A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1625-1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, STR 35 CORRODED BETWEEN FS 1625 TO 1645. REPAIRED BY REPLACING SECTION OF STRINGER PER SRM 53-13-00 FIG 806. 2L73 4F A23WE 19950609005531995060900553WP 1995 6 9 DLL10952441 119950531A5320 CLIPS LKHEED1011 10113851 5265010WP FS 1605 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, SKIN CLIP CORRODED FS 1605 FROM STR 29 TO 34. FABRICATED SKIN CLIPS PER SRM 53-12-00 FIG 817, TREATED AND PAINTED. INSTALLED REPAIR PER SRM. 2L73 4F A23WE 19950609005541995060900554WP 1995 6 9 DLL10952446 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1605-1625 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STR 34 CORRODED FS 1605 TO 1625. FOUND AT HMV, REPAIRED PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950609005551995060900555WP 1995 6 9 DLL10952447 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1585-1625 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STR 33 CORRODED FROM FS 1585 TO 1625. FOUND AT HMV, REPAIRED BY REPLACING STRINGER PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950609005561995060900556WP 1995 6 9 DLL10952448 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1625 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 32 CORRODED FS 1625. FOUND AT HMV, REPAIRED PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950609005571995060900557WP 1995 6 9 DLL10952449 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1565-1585 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 34 CORRODED FS 1565 TO 1585. FOUND AT HMV, REPLACED STRINGER PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950609005581995060900558WP 1995 6 9 DLL10952450 119950605A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 759 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP DISBONDED FS 759 STRINGER 26 TO 27. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950609005591995060900559WP 1995 6 9 DLL10952451 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1530-1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 27 CORRODED FS 1530, 1545 TO 1585, 1523 TO 1545, 1585 TO 1605 AND 1625 TO 1645. FOUND AT HMV, REPLACED STRINGER PER SRM 53-13-00 FIG 804. 2L73 4F A23WE 19950609005601995060900560WP 1995 6 9 DLL10952452 119950605A5320 CLIP LKHEED1011 10113851 5265010WP FS 1625-1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 CLIP AND DOUBLERS CORRODED BETWEEN STRINGER 33 AND 34 UNDER FWD FRAME AND ALONG STRINGER 33. FOUND AT HMV, REPAIRED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950609005611995060900561WP 1995 6 9 DLL10952453 119950605A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 943 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FLOORBEAM CORRODED FS 943 LBL 50 TOP OF BEAM, FOUND AT HMV. REPAIRED PER SRM 53-21-00 FIG 823. 2L73 4F A23WE 19950609005621995060900562WP 1995 6 9 DLL10952454 119950605A5320 FITTING LKHEED1011 10113851 5265010WP L1 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 L1 DOOR FRAME STOP FITTING CORRODED FWD SIDE 2ND AND 3RD FROM BOTTOM. FOUND AT HMV, REPLACED FITTINGS PER SRM 53-15-00 FIG 805. 2L73 4F A23WE 19950609005631995060900563WP 1995 6 9 DLL10952468 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 599 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED, C-1 B/B RT SIDE, STA 599 BETWEEN STR 20 AND STR 24. REPAIRED PER SRM 53-10-00. 2L73 4F A23WE 19950609005641995060900564WP 1995 6 9 DLL10952473 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 559-599 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 32 CORRODED FROM FS 559 TO FS 599, FOUND AT HMV. REPAIRED PER SRM 53-13-00. 2L73 4F A23WE 19950609005651995060900565WP 1995 6 9 DLL10952474 119950605A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1695 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP DISBONDED FS 1695 BETWEEN STRINGER 29 AND 30, FOUND AT HMV. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950609005661995060900566WP 1995 6 9 DLL10952475 119950605A5330 DOUBLER LKHEED1011 10113851 5265010WP FS 1363 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 INTERNAL DOUBLER HAS 2 INCH CUT BETWEEN STRINGER 41 AND 42 FS 1363, FOUND DURING HMV. REPAIRED PER SRM 53-31-00 FIG 836. 2L73 4F A23WE 19950609005671995060900567WP 1995 6 9 DLL13952430 119950511A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 953 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV FOUND TEAR STRAP DISBONDED, AT FS 953 BETWEEN STR 37 AND 38. CLEANED AREA AND REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950609005681995060900568WP 1995 6 9 DLL13952477 119950512A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1765-1785 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FAIL-SAFE STRAP CORRODED IN C3 B/B AT FS 1765 TO 1785 BETWEEN STR 42 TO 34. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950609005691995060900569WP 1995 6 9 DLL13952478 119950512A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1763-1778 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FAIL-SAFE STRAP CORRODED C3 B/B FS 1763 TO 1778 BETWEEN STR 43 TO 45. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950609005701995060900570NM 1995 6 9 DLM11952467 119950605A5720 WINGLET DOUG MD11 MD11 3023602NM RT WING LIGHTNING STRIKEA DALAO OTHER C F.O.D. CRCRUISE 1 SO11810DE 48565 LIGHTNING STRIKE, RIGHT WING LWR WINGLET T/E BURNED NEAR WING TIP. REPAIRED PER SRM 57-90-00. 2L73 4F RTA22WE 19950609005711995060900571NM 1995 6 9 DLM88952472 119950605A5311 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11901DL 49532 LT MLG DOOR JAMB FWD FRAME CRACKED 1 INCH IN RADIUS OF UPPER FLANGE, FOUND AT C-2 LTR CK. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950609005721995060900572NM 1995 6 9 DLM88952476 119950605A5320 DOOR JAMB DOUG MD88 MD88 3023688NM LT MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11901DL 49532 FOUND ON C2 LTR CK, LT MLG DOOR JAMB FWD FRAME IS CRACKED 1 INCH IN RADIUS OF UPPER FLANGE. REPAIRED PER SRM FIG 78A. 2L72 4F RTA6WE 19950609005731995060900573NM 1995 6 9 SWAA950419 119950529A33506042221 EEL BATTERY BOEING737 7373H4 1384600NM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07322SW 23343 DURING SCHEDULED MAINT CHECK, FOUND AFT SECTION OF CABIN EMERGENCY EXIT LIGHTING INOP. REPLACED BATTERY PACK PER BOEING MM. 2L72 4F RTA16WE 19950609005741995060900574NM 1995 6 9 SWAA950420 119950528A3350 EEL WIRES BOEING737 7373H4 1384600NM CABIN DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07368SW 26579 DURING SCHEDULED C1 CHECK, FOUND 2 FLOOR TRACK LIGHTS INOP AT AFT SECTION OF CABIN. REPAIRED AND RECONNECTED TWO WIRES PER BOEING MM. 2L72 4F RTA16WE 19950609005751995060900575NM 1995 6 9 SWAA950421 119950527A3350 EEL WIRES BOEING737 7373H4 1384600NM CABIN DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07602SW 27953 DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTING FROM ROWS 19 THROUGH 21 INOP. RECONNECTED WIRE TERMINALS TO LIGHT ASSEMBLY PER BOEING MM. 2L72 4F RTA16WE 19950609005761995060900576NM 1995 6 9 SWAA950422 119950528A3397 WIRE BOEING737 7373H4 1384600NM CABIN DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07673SW 23251 PASSENGER KICKED RED EMERGENCY EXIT LIGHTS APART. REPAIRED AND SECURED WIRES PER BOEING M/M. 2L72 4F RTA16WE 19950609005771995060900577NM 1995 6 9 SWAA950423 119950529A335020131A EEL BATTERY BOEING737 7375H4 138449DNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07521SW 25320 DURING SCHEDULED A2 CHECK, FOUND NUMEROUS EMERGENCY LIGHTS IN AFT CABIN AREA NOT TESTING. REPLACED LIGHT BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950609005781995060900578NM 1995 6 9 SWAA950424 119950529A5313 STRINGER BOEING737 7373H4 1384600NM BS 334 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER DAMAGED AT BS 334, S10R, AND STRINGER CRACKED AT BS 294, AT S4R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005791995060900579NM 1995 6 9 SWAA950425 119950529A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN DENTED AT BS 265, BETWEEN S17R AND S18L, BS 282, S15L, BS 827, BETWEEN S9 AND 10R, BS 920, WL 204, S17-18L, BS 342 AND 350, BETWEEN S20 AND 21R, BS 355, BETWEEN S18R AND 19R, AT BS 338, S18R, BS 1064, AT S22R, BS 378, BETWEEN S19 AND 20R, AND BS 920, BETWEEN S17 AND 18L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005801995060900580NM 1995 6 9 SWAA950426 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 767-820/460 CREASE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN CREASED AT BS 767 TO 820, AT S24 TO 26L, AND BS 460, FROM S28L TO S28R, AT SHEAR TIE LOCATION. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005811995060900581NM 1995 6 9 SWAA950427 119950529A5320 SHEAR TIE BOEING737 7373H4 1384600NM BS 887 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED AT BS 887, BETWEEN S27 R AND L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005821995060900582NM 1995 6 9 SWAA950428 119950529A5241 DOOR FRAME BOEING737 7373H4 1384600NM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED FROM LOWER EDGE TO FASTENER HOLE, BS 294, WL 208, RBL 55. REPLACED FRAME PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005831995060900583NM 1995 6 9 SWAA950429 119950529A5320 ANGLE BOEING737 7373H4 1384600NM BS 270 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND TOP CHORD Z-ANGLE CORRODED AT BS 270, RBL 2 LBL 10, WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005841995060900584NM 1995 6 9 SWAA950430 119950529A5754 SKIN BOEING737 7373H4 1384600NM NR 5 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND NR 5 SLAT SKIN LOWER T/E SKIN CRACKED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING BAC 65C30133. 2L72 4F RTA16WE 19950609005851995060900585NM 1995 6 9 SWAA950431 119950529A5320 CLIP BOEING737 7373H4 1384600NM BS 616/663.75 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND STRINGER CLIPS CRACKED AT BS 616, S8L, AND AT BS 663.75 AT S10L AND R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005861995060900586NM 1995 6 9 SWAA950432 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 300-400 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND FUSELAGE SKIN GOUGED FROM BS 390 TO 400, BETWEEN S19 AND 20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005871995060900587NM 1995 6 9 SWAA950433 119950529A5315 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND FLOORBEAM CORRODED AT BS 328 LBL 49 WL 208, BS 294 LBL 10 TO RBL 10 WL 208, BS 986.5 WL 208 RBL 57 TO LBL 57, BS 312 LBL 10 RBL 10 WL 208, AND AT BS 344 RBL 10 TO LBL 40 WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609005881995060900588NM 1995 6 9 SWAA950434 119950529A5312 BLKHD WEB BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07662SW 23255 DURING SCHEDULED TRANSITION CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT BS 178 RBL 5.5 WL 198. REPAIRED PER TRAMCO EWO 95-0337. 2L72 4F RTA16WE 19950609005891995060900589NM 1995 6 9 SWAA950435 119950529A5312 BULKHEAD BOEING737 7372T4 1384492NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED AT REINFORCING STRAP, LBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950609005901995060900590NM 1995 6 9 SWAA950436 119950529A5320 WEB BOEING737 7375H4 138449DNM BS 726 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN WEB AT BS 726, STRINGER 18A RIGHT SIDE. REPAIRED PER SWA RA 1-553-1286. 2L72 4F RTA16WE 19950609005911995060900591NM 1995 6 9 SWAA950437 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 4 TO RBL 2. REPAIRED PER SWA RA 1-553-1277. 2L72 4F RTA16WE 19950609005921995060900592NM 1995 6 9 SWAA950438 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 5.0. REPAIRED PER SWA RA 1-553-1282. 2L72 4F RTA16WE 19950609005931995060900593NM 1995 6 9 SWAA950439 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 5.0. REPAIRED PER SWA RA 1-553-1279. 2L72 4F RTA16WE 19950609005941995060900594NM 1995 6 9 SWAA950440 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, LBL 21.0. REPAIRED PER SWA RA 1-553-1278. 2L72 4F RTA16WE 19950609005951995060900595NM 1995 6 9 SWAA950441 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 48 TO RBL 53. REPAIRED PER SWA RA 1-553-1283. 2L72 4F RTA16WE 19950609005961995060900596NM 1995 6 9 SWAA950442 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947, RBL 15. REPAIRED PER SWA RA 1-553-1280. 2L72 4F RTA16WE 19950609005971995060900597NM 1995 6 9 SWAA950443 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25.75 TO 43. REPAIRED PER SWA RA 1-553-1284. 2L72 4F RTA16WE 19950609005981995060900598NM 1995 6 9 SWAA950444 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8 TO LBL 10. REPAIRED PER SWA RA 1-553-1275. 2L72 4F RTA16WE 19950609005991995060900599NM 1995 6 9 SWAA950445 119950529A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07507SW 24184 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 8. REPAIRED PER SWA RA 1-553-1274. 2L72 4F RTA16WE 19950609006001995060900600NM 1995 6 9 SWAA950446 119950529A5320 CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 639 S1 S2L AND S2R, BS 616 S6L, BS 480 S8R, BS 727A S26L AND S25R, BS 500D S19R, BS 616 S2L, BS 616 S1 AND S5R, BS 887 S25R, BS 277 S15R, BS 663 S10L AND R, AND AT BS 520 S16L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006011995060900601NM 1995 6 9 SWAA950447 119950529A5320 ANGLE BOEING737 7373H4 1384600NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE CRACKED AT BS 328 WL 174, BETWEEN S20 AMD 21L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006021995060900602NM 1995 6 9 SWAA950448 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 969 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 969, 2 INCHES ABOVE S19L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006031995060900603NM 1995 6 9 SWAA950449 119950529A5311 FRAME BOEING737 7373H4 1384600NM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277 S16L WL 217. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006041995060900604NM 1995 6 9 SWAA950450 119950529A5313 STRINGER BOEING737 7373H4 1384600NM BS 727 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED AT BS 727 PLUS 11, S7R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006051995060900605NM 1995 6 9 SWAA950451 119950529A5320 DOOR SILL BOEING737 7373H4 1384600NM BS 277-360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR MOPSILL CORRODED FROM BS 277 TO 360 WL 208. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006061995060900606NM 1995 6 9 SWAA950452 119950529A5311 FRAME BOEING737 7373H4 1384600NM BS 500 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FWD CARGO COMPT FRAME DENTED AT BS 500 RBL 46 WL 169, BETWEEN S22 AND 23R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006071995060900607NM 1995 6 9 SWAA950453 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 344 RBL 65 WL 211. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 65C27287-11. 2L72 4F RTA16WE 19950609006081995060900608NM 1995 6 9 SWAA950454 119950529A5320 WEB BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL WEB TIES CRACKED AT BS 360 LBL 61 WL 274 AND AT WL 253.5. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006091995060900609NM 1995 6 9 SWAA950455 119950529A5320 SPLICE BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908 S4R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006101995060900610NM 1995 6 9 SWAA950456 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 360-368 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND NUMEROUS SKIN GOUGES AT BS 360 TO 368, S4L TO 5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006111995060900611NM 1995 6 9 SWAA950457 119950529A5320 DOORWAY FRAME BOEING737 7373H4 1384600NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOORWAY LOWER FWD FRAME SECTION CRACKED AT LOWER I/B CORNER, BS 294.5 WL 208 RBL 55. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006121995060900612NM 1995 6 9 SWAA950458 119950529A5241 SKIN BOEING737 7373H4 1384600NM GALLEY DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR OUTER SKIN CRACKED ABOVE LOWER HINGE CUTOUT FWD CORNER, BS 300 WL 228 RBL 65. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006131995060900613NM 1995 6 9 SWAA950459 119950529A5330 SKIN BOEING737 7373H4 1384600NM BS 998-1003 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07314SW 23336 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED FROM BS 998 TO 1003, BETWEEN S13 AND 14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950609006521995060900652NE 1995 6 9 95ZZZX2817 119950502A2910SS48CT3A1320000 HOSE SKRSKYS76 S76A 8143006NE NLG WELL LEAKING A ALGAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW03712AL1158950 760280 DURING CRUISE FLIGHT, NR 2 HYDRAULIC SYSTEM STARTED A SLIGHT DROP BELOW RED LINE (3000 PSI) TO 2350-2500 PSI. LANDING GEAR ACTUATED TO DOWN POSITION. LANDING GEAR INDICATED SAFE. UPON INSPECTION, NOSE LANDING GEAR UP HYD FLEX HOSE WAS FOUND LEAKING. FLEX HOSE HAS NO APPARENT EXTERNAL DEFECTS. NOTE: HOSE WAS MANUFACTURED 8-83. 1G72 3U H1NE 19950609006561995060900656NM 1995 6 9 95ZZZW782 119950414A21317638102 PRESS CONTROLLER BOEING737 7372B7 1384560NM AIR COND SYS FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19272AU5632 22884 CLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. REFERENCE USAA950381. 2L72 4F A16WE 19950609006571995060900657CE 1995 6 9 95ZZZW783 119950217A5210 SEAL 1144002339 BEECH 1900 1900C 1154161CE CABIN DOOR FAILED A AGPPAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 CE09120GP UC59 PBI-TPA - FLT NR 2283 WAS LEVEL AT 16,000 FEET AND READY TO BEGIN DESCENT TO 10,000 FEET WHEN A LOUD EXPLOSION FOLLOWED BY CABIN PRESSURIZATION WAS EXPERIENCED. AIRCRAFT WAS LANDED SAFELY IN TPA WHERE GP EXPRESS MAINTENANCE FOUND THE CABIN DOOR SEAL BLWON OUT. UPPER AND LOWER DOOR SEAL TRACKS (P/N 1144002317, P/N 1144002321) WERE REPLACED AND A NEW SEAL WAS INSTALLED. (W) 2L72 4T RTA24CE 19950609006581995060900658SO 1995 6 9 C2XA95CL085 119950518A27513069001017 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A C2XAD RETURN TO BLOCK P NO WARNING INDICATION TXTAXI/GRND HDL 1 SW091970411579 0255 120086 FLT 3335 - PIT-CLE - ON TAXI OUT, RECEIVED FLAP ASYMMETRY. BROUGHT FLAP LEVER UP AND ALL FLAPS CAME UP, HOWEVER, NO FLAP INDICATION ON OVERHEAD PANEL. FERRIED AIRCRAFT TO CLE. MAINTENANCE REMOVED AND REPLACED THE FLAP ANNUNCIATOR. OPS CHECKED GOOD. RETURNED TO SERVICE. (W) 2L72 4T RTA31SO 19950609006591995060900659EU 1995 6 9 C2XA95CL086 119950517A2613S2611006500060 DETECTOR AEROSPATR42 ATR42320 8680930EU NR 2 ENGINE SHORTED A C2XACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SW0999838 131 259 FLT NR 3637 - SYR-SYR - NACELLE OVERHEAT ILLUMINATED ON TAKEOFF. RETURNED TO GATE. AIRCRAFT RELEASED IAW MEL 26-12-3. BDL MAINTENANCE CLEARED MEL BY REMOVING AND REPLACING THE NR 2 OVERHEAT DETECTOR. OPS CHECKED GOOD. (W) 2H72 4T RTA53EU 19950609006601995060900660EU 1995 6 9 C2XA95IA084 119950518A33506VEAF EEL BATTERY AEROSPATR42 ATR42320 8680930EU CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0914834 193 IAH - DURING AN A-CHECK INSPECTION, SEVERAL AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS. THE EMERGENCY LIGHTS OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (W) 2H72 4T RTA53EU 19950609006611995060900661SO 1995 6 9 C2XA95IA085 119950522A3350GE1317 EEL BULB EMB 120 EMB120RT SO EXTERNAL FUS INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0957734 120199 IAH - DURING PREFLIGHT CHECK, FOUND AFT EXTERNAL EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED THE BULBS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2L72 4T RTA31SO 19950609006621995060900662SO 1995 6 9 C2XA95IA086 119950524A571312004367001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW091671012706 120106 IAH - DURING A CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 10 CRACKED BETWEEN RIBS NR 8 AND NR 9. MAINTENANCE CUT, REMOVED CRACKED SECTION, AND INSTALLED STRINGER SPLICE USING DER APPROVED EMBRAER FAX NR EST-235/95. (W) 2L72 4T RTA31SO 19950609006631995060900663EU 1995 6 9 C2XA95IA087 119950524A33503011210 EEL WIRE AEROSPATR42 ATR42320 8680930EU CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0914804 069 IAH - DURING 4A CHECK INSPECTION, FOUND PASSENGER CREW ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRING AT LIGHT ASSEMBLY, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (W) 2H72 4T RTA53EU 19950609006641995060900664WP 1995 6 9 CAL950394 119950511A5311 FRAME DOUG DC10 DC1030 3023501WP FS 1701/1721 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097607367130 46940 KUL - INSPECTION FOUND CORROSION ON FRAME CAPS AT STATION 1701 AND 1721 BETWEEN LONGERONS 50L AND 50R. THE FRAME CAPS WERE REPAIRED IAW ECRA 5310-03101. (W) 2L73 4F A22WE 19950609006651995060900665WP 1995 6 9 CAL950395 119950430A5320 CORNER DOUG DC10 DC1030 3023501WP CARGO DR CUTOUT CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097607367130 46940 KUL - INSPECTION FOUND CORROSION ON THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER. THE FORWARD CARGO DOOR CUTOUT FORWARD LOWER CORNER WAS REPAIRED IAW ECRA 5330-02272. (W) 2L73 4F A22WE 19950609006661995060900666WP 1995 6 9 CAL950396 119950419A3233716581660 ACTUATOR BOLT DOUG DC10 DC1030 3023501WP RT MLG SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW097607367130 46940 KUL - THE RT MLG RETRACT ACTUATOR ATTACH FITTING UPPER FORWARD BOLT WAS FOUND SHEARED. THE BOLT WAS REPLACED PER STANDARD PRACTICE CHAPTER 20 OF THE MAINTENANCE MANUAL AND SERVICE BULLETIN 57-67. (W) 2L73 4F A22WE 19950609006671995060900667NM 1995 6 9 CAL950409 119950520A291065445101385 HYD LINE BOEING737 7372C0 1384488NM NR 2 ENGINE CHAFED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0910242 20071 FLT NR 1758 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC FLUID WHILE AT CRUISE. THE 'ABNORMAL' CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HYDRAULIC PRESSURE LINE CHAFED THROUGH. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. THE ENGINES WERE RUN, AND LEAK CHECKS WERE GOOD. (W) 2L72 4F A16WE 19950609006681995060900668GL 1995 6 9 CAL950413 219950521A7230 COMPRESSOR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 ENGINE STALLED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW0968046518231913 47800 451387 SYD - FLT 0909 - NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS AT 37,000 FEET AFTER DEPARTING SYD. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO SYD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE READIED THE AIRCRAFT FOR FERRY FLIGHT TO GUM WHERE THE NR 1 ENGINE WILL BE REMOVED AND REPLACED. SUPPLEMENT - THE STALLS WERE CAUSED BY HIGH PRESSURE BLEED AIR REVERSE FLOW INTO THE 8TH STAGE BLEED AIR DUCT. THE ENGINE WAS NOT DAMAGED, IT WAS REMOVED AS A PRECAUTION FOR POST-STALL BORESCOPE. IT IS BELIEVED THAT FAILURE OF 1 OR ALL 3 OF THE FOLLOWING COMPONENTS COULD HAVE RESULTED IN THE REVERSE FLOW CONDITION: LOWER PRESS CHECK VALVE, PRESS REGULATOR VALVE, AND FAN REVERSER OVERPRESS VALVE. (W) 2L73 4F4 F A22WE E23EA 19950609006691995060900669NE 1995 6 9 USAA950375 219950406A7532658385 PRBC BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE LT ENGINE FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19239US35272 22354 GSO - FLT 8002 - FLIGHT EN ROUTE MLB TO BWI WHEN THROTTLES SPLIT. AIRCRAFT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT ENGINE PRBC. RAN ENGINE, OPS CHECK GOOD. (W) 2L72 4F4 F A16WE E2EA 19950609006701995060900670NM 1995 6 9 USAA950378 119950412A3260 UPLOCK SENSOR BOEING737 7372B7 1384560NM LT MLG OUT OF ADJUST A USAAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 EA19277AU 22889 CLT - FLT 1263 - AFTER TAKEOFF GSP, LEFT LANDING GEAR RED LIGHT REMAINED ON. CREW RECYCLED NO HELP. LIGHT FLICKERED OFF AND ON THROUGHOUT FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED LEFT GEAR UPLOCK SENSOR. SENSOR TEST PER MM 32-61-0 CHECKS OK. (W) 2L72 4F A16WE 19950609006711995060900671NM 1995 6 9 USAA950381 119950414A21337110033 OUTFLOW BOEING737 7372B7 1384560NM AIR COND SYS FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19272AU16394 22884 CLT 2234 - UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. FLIGHT RETURNED TO CLT WHERE AN OVERWEIGHT LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED INSULATION FROM OUTFLOW VALVE AND REPLACED OUTFLOW VALVE AND PRESSURE CONTROLLER. REFERENCE 95ZZZW782. 2L72 4F A16WE 19950609006721995060900672WP 1995 6 9 USAA950463 119950417A531599581883 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1322 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND LEVEL II CORROISON REF CPCP TASK NR C58-5330 STATION 1322 RIGHT LAV FLOORBEAM. REMOVED CORROSION TRIMMED OUT DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLES AND STRAP PER USAIR TYPICAL REPAIR 53-10-19. (W) 2L72 4F A6WE 19950609006731995060900673WP 1995 6 9 USAA950473 119950417A5311 FRAME DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN FRAME STATION 160 AT CENTER OF AIRCRAFT IN E/E COMPARTMENT. STOP DRILLED CRACK AND INSTALLED SPLICE REPAIR AND DOUBLER PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950609006741995060900674WP 1995 6 9 USAA950474 119950417A5320 BEAM DOUG DC9 DC981 3022081WP STA 1174-1193 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND A GOUGE BEYOND LIMITS AT STATION 1174 AND 1193 LOWER FLANGE OF BEAM, AFT CARGO CEILING STRUCTURE. ROUTED OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR ANGLES PER SRM 53-05 FIG 86. (W) 2L72 4F A6WE 19950609006751995060900675WP 1995 6 9 USAA950475 119950417A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1322 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.375 INCH CRACK AT STATION 1322 LONGERON 17 LEFT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-03 FIG 32. (W) 2L72 4F A6WE 19950609006761995060900676WP 1995 6 9 USAA950476 119950417A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1290-1300 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND 2 INCH CRACK AT STATION 1290-1300 CUSP MEMBRANE LEFT SIDE LONGERON 18L. SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97. (W) 2L72 4F A6WE 19950609006771995060900677WP 1995 6 9 USAA950477 119950417A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 1305 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STATION 1305 RT SIDE CUSP MEMBRANE. SPLICED IN NEW SECTION OF CUSP MEMBRANE PER SRM 53-05 FIG 97. (W) 2L72 4F A6WE 19950609006781995060900678WP 1995 6 9 USAA950478 119950417A5330 SKIN DOUG DC9 DC981 3022081WP BS 807 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19826US37344 48026 PIT - DURING Q-6 CHECK INSPECTION, FOUND CORROSION AT STATION 807 LONGERON 28-30 RIGHT IN SKIN. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 53. (W) 2L72 4F A6WE 19950609006791995060900679EU 1995 6 9 USAA950484 119950327A5312 BEAM FOKKERF28 F28MK4000 4990810EU FWD PRESS BLKHD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19483US18918 11233 PIT - DURING SCHEDULED SIP INSPECTION REF 53-10-05, FOUND .5 INCH CRACK CENTER LINE BEAM VI FORWARD PRESSURE BULKHEAD. STOP DRILLED CRACK ENDS AND INSTALLED TWO ANGLE DOUBLERS PER USAIR EA 30058. (W) 2L72 4F RTA20EU 19950609006801995060900680EU 1995 6 9 USAA950485 119950328A5330 SKIN FOKKERF28 F28MK4000 4990810EU DOOR CUTOUT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19483US18918 11233 PIT - DURING SCHEDULED SIP VISIT REF 53-10-20, FOUND .5 INCH CRACK UPPER FORWARD CORNER OF THE SERVICE EMERGENCY DOOR APERTURE CUTOUT. EDDY CURRENT INSPECTION. REMOVED DAMAGED AREA AND INSTALLED FILLER PLUG AND DOUBLERS PER SRM 53-0216. (W) 2L72 4F RTA20EU 19950609006811995060900681WP 1995 6 9 USAA950488 119950323A5330 SKIN DOUG DC9 DC931 3022065WP FS 370 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19950VJ57252 47564 PIT - DURING ACCOMPLISHMENT OF SCHEDULED PRODUCTION CONTROL ITEM NR 105, FOUND 13/16 INCH CRACK AT TOP FORWARD CORNER OF FWD CARGO DOOR FRAME AT STA 370 BELOW LONGERON 19. VISUAL INSPECTION AND HFEC. INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-05 FIG 68. (W) 2L72 4F A6WE 19950609006821995060900682NM 1995 6 9 USAA950515 119950411A532065C10592906 INTERCOSTAL BOEING737 7372B7 1384560NM FS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19267AU34647 22879 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 15 INCH AREA OF SURFACE CORROSION, STATION 947 TO 967 AT RBL 46. REPAIRED PER SRM 51-10-9. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950609006831995060900683NM 1995 6 9 USAA950518 119950410A5315 FLOORBEAM BOEING737 7372B7 1384560NM FS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19267AU34647 22879 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .017 DEEP CORROSION, STATION 312 RIGHT SIDE NEXT TO DOOR SILL. REPAIRED PER TR BG 53-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950609006841995060900684WP 1995 6 9 9508979982 119950503A5312 BULKHEAD DOUG DC9 DC932 3022066WP FS 718 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01982US 45790 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT MAIN LANDING GEAR WELL PRESSURE PANEL FS 718, RBL 50-58. REPAIRED PER EA 99-094841. 2L72 4F A6WE 19950609006851995060900685WP 1995 6 9 9508981141 119950520A5311 FRAME DOUG DC10 DC1040 3023508WP FS 939 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON THE FORWARD CARGO FLOOR FRAME FS 939, LBL 38. REPAIRED PER EA 11-98542. 2L73 4F A22WE 19950609006861995060900686NM 1995 6 9 9508996718 119950522A5312 BULKHEAD BOEING747 747251F 1384898NM FS 1394 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01618US 21122 DURING PERIODIC CHECK (LON), FOUND CORROSION ON THE RIGHT BODY MAIN LANDING GEAR WELL PRESSURE DECK WEB FS 1394, RBL 91 - 97. REPAIRED PER EA 67-98212. 2L74 4F A20WE 19950609006871995060900687NM 1995 6 9 9509006622 119950523A5711 SPAR WEB BOEING747 747251B 1384892NM WS 556-562 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01622US 21704 DURING PERIODIC CHECK, FOUND CORROSION ON THE RIGHT WING FRONT SPAR WEB FSSI 556 - 562. REPAIRED PER EA 66-98544. 2L74 4F A20WE 19950609006881995060900688WP 1995 6 9 9509011141 119950523A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON THE FS 879 FORWARD CARGO FLOOR FRAME AT LBL 38. REPAIRED PER EA 11-98535. 2L73 4F A22WE 19950609006891995060900689WP 1995 6 9 9509021141 119950523A5710 LE SKIN DOUG DC10 DC1040 3023508WP WS 610.8 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CRACKS IN THE RIGHT WING FIXED LEADING EDGE SKIN, XOS 610.8; ARB 1137-4 WEB AND ARB 1137-9 TEE. REPAIRED ALL PER EA 11-98524. 2L73 4F A22WE 19950609006901995060900690NM 1995 6 9 9509035528 119950524A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 1640 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01528US 23843 DURING PERIODIC CHECK, FOUND CORROSION ON THE FS 1640 FLOOR BEAM UPPER CHORD RBL 12 - 59. REPAIRED BEAM PER EA 55-98486. 2L72 4F RTA2NM 19950609006911995060900691NM 1995 6 9 9509045528 119950524A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01528US 23843 DURING PERIODIC CHECK, FOUND CORROSION ON THE FS 365 FLOOR BEAM UPPER CHORD FASTENER HOLES RBL 8 AND RBL 16. REPAIRED PER EA 55-98483. 2L72 4F RTA2NM 19950609006921995060900692WP 1995 6 9 9509051141 119950524A5311 FRAME DOUG DC10 DC1040 3023508WP FS 979 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON THE FORWARD CARGO FLOOR FRAME FS 979 AT LBL 29. REPAIRED PER EA 11-98545. 2L73 4F A22WE 19950609006931995060900693WP 1995 6 9 9509061141 119950524A5311 FRAME DOUG DC10 DC1040 3023508WP FS 939 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON THE FS 939 FORWARD CARGO FRAME AT LONGERON 51R. REPAIRED PER EA 11-98552. 2L73 4F A22WE 19950609006941995060900694NM 1995 6 9 9509075528 119950525A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 377 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01528US 23843 DURING PERIODIC CHECK, FOUND CORROSION ON THE FS 377 FLOOR BEAM UPPER CHORD FASTENER HOLES LBL 6 - 23. REPAIRED BEAM PER EA 55-98485. 2L72 4F RTA2NM 19950609006951995060900695WP 1995 6 9 9509081141 119950526A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 1710-1781 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON STR 52 FROM FS 1710 - 1781. REPAIRED PER EA 11-97970. 2L73 4F A22WE 19950609006961995060900696WP 1995 6 9 9509091141 119950526A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 850 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01141US 46750 DURING 'T' CHECK, FOUND CORROSION ON LONGERON 37R AT FS 850. REPAIRED PER EA 11-98559. 2L73 4F A22WE 19950609006971995060900697NM 1995 6 9 9509105528 119950527A5315141N5112 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01528US 23843 DURING PERIODIC CHECK, FOUND CORROSION ON THE FS 365 FLOOR BEAM UPPER CHORD FASTENER HOLES RBL 0 - 19. REPAIRED BEAM PER EA 55-98483. 2L72 4F RTA2NM 19950609006981995060900698NM 1995 6 9 9509115528 119950528A5400 BRACKET BOEING757 757251 1384970NM NAC STA 105 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01528US 23843 DURING PERIODIC CHECK, FOUND A 3.75 INCH CRACK IN THE NR 1 ENGINE FAN COWL SUPPORT BEAM ANGLE STA 105. REPAIRED ANGLE PER EA 55-98490. 2L72 4F RTA2NM 19950609006991995060900699NM 1995 6 9 9509122709 119950602A7120 MOUNT BOEING727 727225 1384077NM NR 2 ENGINE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING 'H' CHECK, FOUND CORROSION IN THE NR 2 ENGINE AFT MOUNT FITTING, AFT FLANGE. REPLACED FITTING PER SRM 54-40-1, PG.1-2. 2L73 4F A3WE 19950609007001995060900700WP 1995 6 9 9509139976 119950602A5320 FITTING DOUG DC9 DC931 3022065WP FS 590 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND A CRACK IN THE LONGERON 27L END FITTING AT FS 590. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950609007011995060900701WP 1995 6 9 9509149976 119950602A5210 FITTING DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND A CRACK IN THE AFT CABIN DOOR UPPER HINGE FITTING. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19950609007021995060900702WP 1995 6 9 9509151143 119950603A5320 FITTING DOUG DC10 DC1040 3023508WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01133JC 46752 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR ACTUATOR SUPPORT FITTING. REPLACED FITTING. 2L73 4F A22WE 19950609007031995060900703WP 1995 6 9 9509169976 119950603A5241 FITTING DOUG DC9 DC931 3022065WP GALLEY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND A CRACK IN THE GALLEY SERVICE DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-10. 2L72 4F A6WE 19950609007041995060900704WP 1995 6 9 9509179976 119950604A5320 FITTING DOUG DC9 DC931 3022065WP FS 598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND CORROSION IN THE FS 598 INTERCOSTAL FITTING BETWEEN LONGERONS 27L - 28L. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950609007051995060900705NM 1995 6 9 95UAL727039 119950607A2130 PRESSURE VALVE HAMILTON STA724827 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP297262U 108416 21409 RETURNED TO FIELD UNDER AMBER ALERT, DUE TO INABILITY TO MAINTAIN CABIN PRESSURE. REPLACED RIGHT SAFETY RELIEF VALVE AND NR 3 ENGINE HIGH PRESSURE VALVE. 2L73 4F4 F A3WE E2EA 19950609007071995060900707NM 1995 6 9 95UAL747039 119950607A2612 FIRE LIGHT BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE ILLUMINATED A UALAFC ACTIVATE FIRE EXT. ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP29153UA 20102 662783 THE NR THREE ENGINE FIRE LIGHT CAME ON DURING TAKEOFF. 2L74 4F4 F A20WE E20EA 19950609007081995060900708 1995 6 9 ABXA9500527 419950605A344220852680106 INDICATOR NIHON YS11 YS11A500 6310416WP RADAR DEFECTIVE A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23920AX 629 2114 WEATHER RADAR SHOWED UNUSUAL DISPLAY AND THEN STARTED SMOKING. PULLED RADAR CIRCUIT BREAKER. REPLACED RADAR INDICATOR. SYSTEM CHECKED GOOD ON THE GROUND IAW YS-11 M.M. 2L72 4T A1PC 19950609007091995060900709WP 1995 6 9 ABXA9500528 119950605A3260313 BULB DOUG DC8 DC861 3021952WP RT MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23848AX 46032 WHEN GEAR WAS LOWERED, NO DOWN AND LOCKED INDICATION ON RIGHT MAIN GEAR. PUT GEAR UP AND RELAMPED RIGHT MAIN GEAR INDICATION. LOWERED GEAR AND RIGHT MAIN SHOWED DOWN AND LOCKED. VERIFIED BOTH RIGHT MAIN GEAR DOWN AND LOCK INDICATION BULBS BURNED OUT. RELAMPED, PERFORMED OPS CHECK ON RIGHT GEAR IAW DC-8 M.M. SYSTEM OPS CHECKED GOOD. INSPECTED RIGHT GEAR DOWNLOCK SWITCH AND WIRING ON RIGHT GEAR. ALL WIRING AND SWITCH CHECKED GOOD IAW DC-8 M.M. 2L74 4F 4A25 19950609007101995060900710 1995 6 9 COM31096 319950607A6140522792 RPM INDICATOR SAAB SF340 SF340A 7850100EU RT PROP DEFECTIVE A COMAK NONE O OTHER DEDESCENT 1 SO01342CA16663888 340A023 RT PROPELLER RPM INDICATION IS NOT INDICATING PROPERLY. REPLACED THE RT RPM INDICATOR. 2L72 4T RTA52EU 19950609007111995060900711EA 1995 6 9 COM60494 119950606A7830 TR UNIT CNDAIRCL600 CL6002B19 EA LT ENGINE MALFUNCTIONED A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01941CA 7050 LEFT ENGINE AMBER REVERSE MESSAGE AND LEFT REVERSE UNLOCKED MESSAGE ON EICAS. MANUALLY DEPLOYED AND STOWED THRUST REVERSER. GROUND RUNS AND SYSTEM OEPRATED NORMALLY. 2L72 4F RTA21EA 19950609007121995060900712EA 1995 6 9 COM60495 119950606A3241864806 PSEU CNDAIRCL600 CL6002B19 EA ANTI SKID DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01937CA2295 950 7044 ANTI-SKID CAUTION MESSAGE IS ON WHEN PARKING BRAKE IS RELEASED. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19950609007131995060900713NM 1995 6 9 DL72E952420 119950602A5753 FOREFLAP BOEING727 727247 138408FNM NR 4 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 FOUND DURING F-1 LETTER CHECK - ONE CRACK AT NR 4 FOREFLAP ABOVE NR 8 FLAP TRACK AT CUTOUT AREA. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950609007141995060900714NM 1995 6 9 DL72E952501 119950531A5754 ATTACH BRACKET BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED. REPAIR: REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950609007151995060900715NM 1995 6 9 DL72E952503 119950530A5753 LE SKIN BOEING727 727247 138408FNM NR 3 TE FOREFLAPDAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON CV2 CHECK DAMAGE TO L/E SKIN OF NR 3 FOREFLAP O/B OF NR 5 FLAPTRACK. REPAIR: REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950609007161995060900716NM 1995 6 9 DL72L952364 119950531A3350900835A EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11503DA 21305 RIGHT OVERWING EMERGENCY EXIT SIGN LIGHTS INOP. REPLACED BATTERY, CHECKS GOOD. 2L73 4F A3WE 19950609007171995060900717NM 1995 6 9 DL72S952343 119950531A5400 S DUCT BOEING727 727232 1384082NM NR 2 ENGINE BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV FOUND S-DUCT LE RIM BENT AND WORN. REPAIRED PER SRM 54-10-3 FIG 13. 2L73 4F A3WE 19950609007181995060900718NM 1995 6 9 DL72S952382 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE LWR HOLE ON THE I/B SURFACE OF THE O/B LUG. REPAIRED PER MM 57-43-00 PG 803. 2L73 4F A3WE 19950609007191995060900719NM 1995 6 9 DL72S952383 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND UPPER HOLE ON THE I/B AND O/B SURFACE OF THE I/B LUG. REPAIRED PER MM 57-43-00 PG 803. 2L73 4F A3WE 19950609007201995060900720NM 1995 6 9 DL72S952483 119950606A575465162268A FLAP BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 PREVIOUS REPAIR CRACKED AT CENTER ATTACH POINT FOR BULLNOSE, 36 INCHES FROM INBD END, OF NR 5 L/E KRUGER FLAP. REPAIRED PER SRM 57-50-3, FIG. 11 REFERENCE ERA NR 270969-14. 2L73 4F A3WE 19950609007211995060900721NM 1995 6 9 DL72S952489 119950606A5754 RIB BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 1) NR 7 SLAT ACT ROD END WEB CRACKED I/B AFT SIDE. 2) NR 7 SLAT ACT ROD END WEB CRACKED O/B AFT SIDE. FOUND DURING C-1 LTR CK. REPAIRED BOTH ITEMS PER MM 57-54-0 PAR 3B. 2L73 4F A3WE 19950609007221995060900722NM 1995 6 9 DL72S952490 119950606A5754 FAIRING BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 NR 5 SLAT I/B TRACK FAIRING CRACKED. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 820. 2L73 4F A3WE 19950609007231995060900723NM 1995 6 9 DL72S952491 119950606A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 ANGLE CRACKED .50 INCH BELOW TAI DUCT ON NR 3 SLAT. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 807. 2L73 4F A3WE 19950609007241995060900724NM 1995 6 9 DL72S952493 119950606A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 1.25 INCH CRACK IN NR 7 SLAT ACT I/B ATTACH FITTING, AFT OF UPPER MOUNT BOLT ON WING FRONT SPAR. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-42-0. 2L73 4F A3WE 19950609007251995060900725NM 1995 6 9 DL72S952499 119950512A5754 RIB BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 RIBS CRACKED, NR 3 L/E SLAT. NINTH RIB FROM I/B END OF SLAT IS CRACKED IN RADIUS, TENTH RIB SAME CONDITION. REPAIRED PER MM 57-54-0 PG 817. 2L73 4F A3WE 19950609007261995060900726NM 1995 6 9 DL72W952361 119950531A5754 SLAT BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112817W 20873 FOUND DURING E-1 LETTER CHECK - .50 INCH CRACK AT I/B STOP PAD ON NR 2 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950609007271995060900727NM 1995 6 9 DL72W952362 119950531A5754 RIB BOEING727 727247 138408FNM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112817W 20873 FOUND DURING E-1 LETTER CHECK - .1875 INCH CRACK BOTTOM OF NOSE RIB JUST LEFT OF SLAT ACTUATOR ROD END ON NR 4 SLAT. ONE INCH CRACK ON NR 4 SLAT I/B TRACK LOWER FAIRING RADIUS. BOTH REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950609007281995060900728NM 1995 6 9 DL72W952363 119950531A5754 SLAT BOEING727 727247 138408FNM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112817W 20873 FOUND DURING E-1 LETTER CHECK - .25 INCH CRACK AT NR 7 SLAT O/B STOP PAD BELOW COVE PNL. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950609007291995060900729NM 1995 6 9 DL73S952370 119950531A5330 SKIN BOEING737 737232 1384475NM FS 847 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11302DL 23047 FOUND ON LAY OVER-DENT AFT OF AFT B/B DOOR APPROX. .25 INCH IN DIAMETER. REPAIRED PER SRM 53-30-3 FIG. 23. 2L72 4F RTA16WE 19950609007301995060900730NM 1995 6 9 DL757952371 119950601A5754114NN3002119A TE WEDGE BOEING757 757232 1384965NM NR 5 TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11646DL 24217 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02. 2L72 4F RTA2NM 19950609007311995060900731WP 1995 6 9 DLL10952356 119950531A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1675 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP DISBONDED FS 1675 BETWEEN STRS 36 AND 37. FOUND AT HMV, REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950609007321995060900732WP 1995 6 9 DLL10952357 119950531A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1695 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP DISBONDED FS 1695 BETWEEN STRS 35 AND 36. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 801. 2L73 4F A23WE 19950609007331995060900733WP 1995 6 9 DLL10952372 119950531A5320 CLIP LKHEED1011 10113851 5265010WP FS 1645 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FS 1645 SKIN CLIP CORRODED BETWEEN STR 33 TO STR 35. CORR: REMOVED CLIP DETWEEN STR 33, 35. CUT NEW PIECE AND DRILLED UP. INSTALLED REPAIR PARTS PER SRM 53-12-00 PG 817. 2L73 4F A23WE 19950609007341995060900734WP 1995 6 9 DLL10952373 119950531A5313 STRINGER LKHEED1011 10113851 5265010WP FS 975 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, MESC STRINGER CRACKED AT ATR 33, FS 975. CORR: DRILLED UP NEW STRINGER AND SPLICE PER SRM 53-13-00. INSTALLED NEW STRINGER/SPLICE PER SRM 53-13-00 FIG 804. 2L73 4F A23WE 19950609007351995060900735WP 1995 6 9 DLL10952375 119950526A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 861 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TOP OF FLOOR BEAM IS CORRODED AT FS 861 LBL 50. CORR: TRIMMED CORRODED FLANGE AS PER SRM 53-21-00 FIG 823. INSTALLED REPAIR ANGLES PER SRM 53-21-00 FIG 823. 2L73 4F A23WE 19950609007361995060900736WP 1995 6 9 DLL10952390 119950525A5320 ATTACH FITTING LKHEED1011 10113851 5265010WP FS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11735D 193C1226 CABIN FLOOR FRAME 1103 IS CRACKED AT VERTICAL LEG OF ATTACH FITTING RT SIDE ABOVE FAIL SAFE ANGLE. REPAIRED PER SRM 53-12-00 PG 813-815. 2L73 4F A23WE 19950609007371995060900737WP 1995 6 9 DLL10952400 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 739 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED AT STA 739 BETWEEN STR 38-39. CORR: REMOVED TEAR STRAP AND REMOVED CORROSION. TREATED/PAINTED. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950609007381995060900738NE 1995 6 9 DLL10952494 219950606A7260 GEARBOX M06157 LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 ENGINE FAILED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO11718DA AM670 193C1097 010672 AT FLT LEVEL 330, NR 3 OIL PRESSURE WENT TO ZERO FOLLOWED BY LOSS OF THRUST. NR 3 ENG SHUT DOWN, OIL QTY AND TEMP NORMAL. FOUND NR 3 GEARBOX FAILED. REPLACED GEARBOX, RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 19950609007391995060900739WP 1995 6 9 DLL13952365 119950510A3020 ANTI-ICE DUCT LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 NR 2 ENG INLET AT 5:30 O'CLOCK POSITION; ANTI-ICE DUCT SKIN CRACKED AROUND RIVET. ACCESS THRU PANEL 311GR-MARKED. REMOVED DAMAGED AREA. FABRICATED NEW REPAIR DOUBLERS PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609007401995060900740WP 1995 6 9 DLL13952366 119950530A3020 ANTI-ICE DUCT LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 NR 2 ENG INLET AT 5:30 O'CLOCK POS. ANTI-ICE DUCT SKIN CRACKED AROUND RIVET. ACCESS THRU PANEL 311 GR-MARKED, REF NR 712. REMOVED DAMAGED AREA. FABRICATED DOUBLER SPACERS AND SHIMS PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609007411995060900741WP 1995 6 9 DLL13952367 119950511A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP FS 933 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FAILSAFE STRAP DISBONDED BETWEEN STR 37-38 AT F.S. 933. FOUND AT HMV, REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950609007421995060900742WP 1995 6 9 DLL13952368 119950511A3020 ANTI-ICE BAFFLE LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 NR 2 ENG INLET ANTI-ICE BAFFLE IS CRACKED AT 7:00 O'CLOCK POS. REPAIRED PER SRM 54-34-00 FIG 804. FOUND AT HMV. 2L73 4F A23WE 19950609007431995060900743WP 1995 6 9 DLL13952369 119950517A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 313 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FLOOR BEAM F.S. 313 CORRODED ON UPPER CAP FROM APPROX. RBL 16-LBL 16. REF TASK NR C-53-100-02. REPAIRED PER SRM 51-21-01, 53-21-00 PG 823-824. 2L73 4F A23WE 19950609007441995060900744WP 1995 6 9 DLL13952374 119950509A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 1103-1203 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 ON HMV, FOUND SEAT TRACK CORRODED STA 1103 - 203 RT OUTBOARD TRACK CORRODED AT SEVERAL LOCATIONS FULL LENGTH OF TRACK. INSTALLED NEW TRACK PER SRM 53-21-00. 2L73 4F A23WE 19950609007451995060900745WP 1995 6 9 DLL13952380 119950510A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 297 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 ON HMV, FLOOR BEAM CORRODED F/S 279 AT RBL 30-36. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950609007461995060900746WP 1995 6 9 DLL13952381 119950512A5320 PRESSURE DECK LKHEED1011 10113851 5265010WP FS 1243 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 ON HMV, FOUND RT PRESSURE DECK CRACKED STA 1243 6 INCHES INBD OF FRAME. REPAIRED PER SRM 53-11-00 FIG 844. 2L73 4F A23WE 19950609007471995060900747WP 1995 6 9 DLL13952495 119950510A7110 INLET LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SKIN CRACKED, AT NR 2 ENG INLET, ANTI-ICE DUCT. TRIMMED OUT DAMAGE, FABRACATED AND DRILLED FILLERS, AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950609007481995060900748NM 1995 6 9 DLM11952505 119950602A2910 SWIVEL DOUG MD11 MD11 3023602NM CENTER GEAR LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11811DE 48566 DURING CRUISE, HAD HYDRAULILC 3 ELEVATOR OFF ALERT ILLUMINATED WITH 4.4 GAL. HYD FLUID. AFTER GEAR LOWERED, HYD QTY DROPPED TO 3.1 AND FALLING. DIVERTED NRT. FOUND GLAND HYDRAULIC SWIVEL LEAKING ON CENTER GEAR. REPLACED GLAND, LEAK CHECK OK. 2L73 4F RTA22WE 19950609007491995060900749NM 1995 6 9 DLM88952360 119950531A5400 ANGLE DOUG MD88 MD88 3023688NM RT ENG PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11992DL 53344 FOUND DURING D-1 LETTER CHECK - .25 INCH CRACK IN RT UPPER ENG PYLON TO FUSELAGE ANGLE 12 INCHES FROM AFTM EDGE. REPAIRED PER SRM 54-04A PG17 FIG 4. 2L72 4F RTA6WE 19950609007501995060900750NM 1995 6 9 DLM88952488 119950606A5400 ANGLE DOUG MD88 MD88 3023688NM NR 1 ENG PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11970DL 43173 .50 INCH CRACK IN UPPER PYLON ATTACH ANGLE 18 INCHES FROM AFT WEDGE. FOUND DURING E-1 LTR CK. REPAIRED PER SRM 54-04A PG 17-18. 2L72 4F RTA6WE 19950609007511995060900751NM 1995 6 9 UPS203432 119950607A5320 ANGLE BOEING727 72725C 138400HNM BS 280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ANGLE AT B.S. 280, WL 177 NOSE WHEELWELL. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 51-20-1, 53-30-2. 2L73 4F A3WE 19950609007521995060900752NM 1995 6 9 UPS203433 119950607A5347 SEAT TRACK BOEING727 72725C 138400HNM FS 595-600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON SEAT TRACK TABS I/B AND O/B B.S. 595 TO 600, LBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 53-10-1, 53-10-5. 2L73 4F A3WE 19950609007531995060900753NM 1995 6 9 UPS203434 119950607A5320 HAT CHANNEL BOEING727 72725C 138400HNM FS 1145-1148 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON HAT CHANNEL STA 1145-1148, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-10-2, 51-20-4, 51-30-6, 51-10-1. 2L73 4F A3WE 19950609007541995060900754NM 1995 6 9 UPS203435 119950607A5320 WEB BOEING727 72725C 138400HNM FS 1170 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR WEB STA 1170, RBL 25, WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-40-2, 51-30-8, 51-10-2, 51-30-2, M/M 51-20-151. 2L73 4F A3WE 19950609007551995060900755NM 1995 6 9 UPS203436 119950607A5320651841713 STIFFENER BOEING727 72725C 138400HNM BS 301 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 301, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1, 51-30-2. 2L73 4F A3WE 19950609007561995060900756NM 1995 6 9 UPS203437 119950607A5320651841713 STIFFENER BOEING727 72725C 138400HNM BS 308 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER B.S. 308, LBL 12 TO RBL 12 WL 180. REPLACED STIFFENER IAW SRM 53-10-1, 51-10-1. 2L73 4F A3WE 19950609007571995060900757NM 1995 6 9 UPS203438 119950607A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 697-703 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL B.S. 697-703, LBL 65, WL 208. INSTALLED NEW TRACK STA. 620-740 IAW SRM 53-10-1, 51-30-2. 2L73 4F A3WE 19950609007581995060900758NM 1995 6 9 UPS203439 119950607A5347 SEAT TRACK BOEING727 72725C 138400HNM BS 580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SEAT TRACK B.S. 580, RBL 65, WL 208. REPLACED TRACK IAW SRM 51-30-2. 2L73 4F A3WE 19950609007591995060900759NM 1995 6 9 UPS203440 119950607A5347654198243 SEAT TRACK BOEING727 72725C 138400HNM BS 1130-1135 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK WELL AND TABS B.S. 1130-1135, RBL 45, WL 208. REPLACED TRACK IAW SRM 53-10-5, 53-10-2, 51-30-2, M/M 51-20-151. 2L73 4F A3WE 19950609007601995060900760NM 1995 6 9 UPS203441 119950607A5753 TE WEDGE BOEING727 72725C 138400HNM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE 36 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007611995060900761NM 1995 6 9 UPS203442 119950607A5753 TE WEDGE BOEING727 72725C 138400HNM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 27 INCHES FROM I/B END. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007621995060900762NM 1995 6 9 UPS203443 119950607A5753 TE WEDGE BOEING727 72725C 138400HNM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B MID FLAP T/E WEDGE ON O/B CORNER. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007631995060900763NM 1995 6 9 UPS203444 119950607A5753 TE WEDGE BOEING727 72725C 138400HNM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B MID FLAP T/E WEDGE 7 INCHES FROM O/B END ON LOWER SURFACE. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007641995060900764NM 1995 6 9 UPS203445 119950607A552165174382 RIB BOEING727 72725C 138400HNM RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND RT ELEVATOR SUPPORT RIB AT STA 99.79 IS CRACKED. REPLACED RIB IAW SRM 51-30-2. 2L73 4F A3WE 19950609007651995060900765NM 1995 6 9 UPS203446 119950607A5320 WEB BOEING727 72725C 138400HNM FS 259.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AROUND LOCKBOLT STA 259.5, LBL 21, WL 192.5. REPAIRED IAW SRM 51-40-2, 51-10-2, 51-30-2, 53-10-2. 2L73 4F A3WE 19950609007661995060900766NM 1995 6 9 UPS203447 119950607A53206519862 CHORD BOEING727 72725C 138400HNM FS 294-350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD B.S. 294-350, LBL 15, WL 169. REPLACED IAW SRM 51-30-5, 51-30-2. 2L73 4F A3WE 19950609007671995060900767NM 1995 6 9 UPS203448 119950607A5320 WEB BOEING727 72725C 138400HNM BS 294-350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT B.S. 294-350, LBL 14, WL 180-160. INSTALLED FABRICATED PARTS IAW E.O 727-53-1612. 2L73 4F A3WE 19950609007681995060900768NM 1995 6 9 UPS203449 119950607A575465162275 K-FLAP BOEING727 72725C 138400HNM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED IAW M/M 27-81-1. 2L73 4F A3WE 19950609007691995060900769NM 1995 6 9 UPS203450 119950607A575465162261 K-FLAP BOEING727 72725C 138400HNM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED IAW M/M 27-81-1. 2L73 4F A3WE 19950609007701995060900770NM 1995 6 9 UPS203451 119950607A5752 TAB BOEING727 72725C 138400HNM RT AILERON DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B AILERON TAB. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007711995060900771NM 1995 6 9 UPS203452 119950607A5752 TAB BOEING727 72725C 138400HNM RT AILERON DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING I/B AILERON TAB. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950609007721995060900772NM 1995 6 9 UPS203453 119950607A5730 SKIN BOEING727 72725C 138400HNM FS 259.5-272 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS AROUND FASTENERS (HIGH FREQUENCY EDDY CURRENT INSPECTION) AT B.S. 259.5 TO 272, STR 9R, WINDSHIELD UPPER SILL. REPAIRED IAW SRM 51-30-2, 53-30-3. 2L73 4F A3WE 19950609007731995060900773NM 1995 6 9 UPS203454 119950607A5711 SPAR CHORD BOEING727 72725C 138400HNM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SPAR CHORD B.S. 870, RBL 35, WL 188. REPAIRED IAW E.O. B727-5710-7063A. 2L73 4F A3WE 19950609007741995060900774NM 1995 6 9 UPS203455 119950607A532066147361 EXPANSION LINK BOEING727 72725C 138400HNM BS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSEAGE TO WING CENTER SECTION EXPANSION LINKS (LT AND RT) AT B.S. 740, RBL 13, LBL 13, WL 150. 2L73 4F A3WE 19950609007751995060900775NM 1995 6 9 UPS203456 119950607A5730 SKIN BOEING727 72725C 138400HNM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL SKIN AT B.S. 870, RBL 32-39, WL 188. REPAIRED IAW E.O. 727-57-1386. 2L73 4F A3WE 19950609007761995060900776NM 1995 6 9 UPS203457 119950607A575465162251 K-FLAP BOEING727 72725C 138400HNM NR 3 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED IAW M/M 27-81-1. 2L73 4F A3WE 19950609007771995060900777NM 1995 6 9 UPS203460 119950607A5330 SKIN BOEING727 72725C 138400HNM BS 850-870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FUEL CELL SKIN B.S. 850-870, RBL 45-65. REPAIRED IAW E.O. 727-57-1385. 2L73 4F A3WE 19950609007781995060900778NM 1995 6 9 UPS203461 119950607A5730 SKIN BOEING727 72725C 138400HNM BS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FUEL CELL SKIN STA. 740, LBL 39 AND 45. REPAIRED IAW E.O. 727-5710-7079A. 2L73 4F A3WE 19950609007791995060900779NM 1995 6 9 UPS203475 119950607A5320 CHANNEL BOEING727 72731C 1384011NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHANNEL AT STA. 1342 LT SIDE. REPLACED IAW SRM 51-30-2, E.O. B727-5330-4501B. 2L73 4F A3WE 19950609007801995060900780NM 1995 6 9 UPS203476 119950607A533065195321 CHORD BOEING727 72731C 1384011NM FUSELAGE CORRODED A IPXAO OTHER O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD FITTING AT STA 1362 LT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2. 2L73 4F A3WE 19950609007811995060900781NM 1995 6 9 UPS203477 119950607A532065225514 FITTING BOEING727 72731C 1384011NM BS 1362 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHORD FITTING AT STA 1362. REPLACED IAW B727-5330-4601B AND SRM 51-30-2. 2L73 4F A3WE 19950609007821995060900782NM 1995 6 9 UPS203478 119950607A532065225514 FITTING BOEING727 72731C 1384011NM FS 1362 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD FITTING AT STA 1362 RT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2. 2L73 4F A3WE 19950609007831995060900783NM 1995 6 9 UPS203479 119950607A5330 FITTING BOEING727 72731C 1384011NM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD FITTING AT STA 1342 RT SIDE. REPLACED IAW B727-5330-4601B AND SRM 51-30-2. 2L73 4F A3WE 19950609007841995060900784NM 1995 6 9 UPS203486 119950608A5754 SKIN BOEING727 72725C 138400HNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING NR 6 K-FLAP BULLNOSE O/B HINGE UPPER SURFACE OF UPPER ATTACH POINTS HAVE CORROSION. INSTALLED FABRICATED PARTS IAW SRM 57-50-1, 51-10-6, 51-10-1, 51-20-04. 2L73 4F A3WE 19950609007851995060900785NM 1995 6 9 UPS203487 119950608A57116595600763 SPAR CHORD BOEING727 72725C 138400HNM FS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER FRONT SPAR CHORD AT STA. 740, WL 166.5, BL 0. REPLACED CHORD IAW E.O. B727-5710-7078A. 2L73 4F A3WE 19950609007861995060900786NM 1995 6 9 UPS203488 119950608A5730 SKIN BOEING727 72725C 138400HNM FS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01948UP 19357 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON LOWER FUEL CELL SKIN AT STA 740, RBL 1-15. REPAIRED IAW E.O. B727-5710-7079A. 2L73 4F A3WE 19950609007871995060900787NM 1995 6 9 UPS203489 119950609A5330 SKIN BOEING727 7272A1 138407FNM BS 1097 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN GOUGED 1.5 WIDE AND .065 DEEP AT BS 1097, RBL 70, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 53-30-3, M/M 51-20-151. 2L73 4F A3WE 19950609007881995060900788NM 1995 6 9 UPS203490 119950608A5730 SKIN BOEING727 7272A1 138407FNM RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED SKIN ON RT L/E PANEL NR 9203 AT SECOND TO LAST RIB UPPER SIDE. INSTALLED FABRICATED PARTS IAW SRM 55-10-03. 2L73 4F A3WE 19950609007891995060900789NM 1995 6 9 UPS403458 119950607A3350 EEL SWITCH BOEING747 747123F NM FLIGHT DECK DIRTY A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01676UP 20101 MAINTENANCE FOUND EMERGENCY LIGHT SWITCH ON PILOTS OVERHEAD PANEL GOES TO ON VIA ARM WITH SWITCH CLOSED. CLEANED CONTACTS. 2L74 4F A20WE 19950609007901995060900790NM 1995 6 9 UPS403480 119950608A5320 TENSION TIE BOEING747 747123F NM FS 900 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK AT THE TENSION TIE RT SIDE STA 900. REPAIRED IAW SRM 51-10-01, 51-40-03. 2L74 4F A20WE 19950609007911995060900791NM 1995 6 9 UPS403481 119950608A5312 BULKHEAD BOEING747 747123F NM FS 140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK AT BULKHEAD SKIN AT STA. 140 RT WL 215. REPAIRED IAW SRM 51-10-01, E.O. B747-5310-3279 REV. C FIG 3. 2L74 4F A20WE 19950609007921995060900792NM 1995 6 9 UPS403482 119950608A5320 SPLICE BOEING747 747123F NM FS 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SPLICE OF LOWER CHORD OF FORWARD LOWER CARGO COMPARTMENT AT STA. 1000 BETWEEN STR. 40 AND 41 LT. 2L74 4F A20WE 19950609007931995060900793NM 1995 6 9 UPS403483 119950608A5311 FRAME BOEING747 747123F NM FS 880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME OF FORWARD LOWER CARGO COMPARTMENT AT STA 880, NEAR STR 39 RT. REPAIRED IAW SRM 53-10-04. 2L74 4F A20WE 19950609007941995060900794NM 1995 6 9 UPS403484 119950608A5320 CHORD BOEING747 747123F NM FS 1000 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN LOWER CHORD OF FORWARD CARGO COMPARTMENT AT STA 1000, BETWEEN STRINGER 46 AND 47 LT 46 AND 47 RT. REPAIRED IAW SRM. 2L74 4F A20WE 19950609007951995060900795NM 1995 6 9 UPS403485 119950608A5311 FRAME BOEING747 747123F NM FS 840 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME 8 INCHES LONG IN FORWARD LOWER CARGO COMPARTMENT AT STA 840, NEAR STRINGER 38 RT. REPAIRED IAW SRM 53-10-04. 2L74 4F A20WE 19950609007961995060900796NM 1995 6 9 UPS503459 119950607A3350 EEL BATTERY PACK BOEING757 75724APF 1384969NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01426UP 25457 MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMER. BATTERY PACK. 2L72 4F RTA2NM 19950609007971995060900797WP 1995 6 9 UPS803462 119950607A5311 FRAME DOUG DC8 DC873F 302199FWP FS 1260 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME LOWER FLANGE, F.S. 1260, LONGS 33R-36. REPAIRED IAW SRM 53-2-0, FIG 2. 2L74 4F RT4A25 19950609007981995060900798WP 1995 6 9 UPS803463 119950607A532046401621 FITTING DOUG DC8 DC873F 302199FWP FS 1460 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME END FITTING AT F.S. 1460 ABOVE LONGERON 21R. REPLACE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950609007991995060900799WP 1995 6 9 UPS803464 119950607A5320 FITTING DOUG DC8 DC873F 302199FWP FS 1200 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF B/T FITTING F.S. 1200, LONGERONS 33L-34L. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950609008001995060900800WP 1995 6 9 UPS803465 119950607A531352597424 LONGERON DOUG DC8 DC873F 302199FWP FS 458 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION AT LONGERON 34R, F.S. 458. REPAIRED LONGERON. IAW SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 19950609008011995060900801WP 1995 6 9 UPS803466 119950607A53309754011505 SKIN DOUBLER DOUG DC8 DC873F 302199FWP FS 260-280 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON INNER SKIN DOUBLER, F.S. 260 - 280, LONGERONS 33R TO 34L. REPAIRED IAW DC8-53-1375. 2L74 4F RT4A25 19950609008021995060900802WP 1995 6 9 UPS803467 119950607A53155613301504 FLOOR BEAM DOUG DC8 DC873F 302199FWP FS 940 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, LOWER ATTACH ANGLE, F.S. 940, LBL 50. REPAIRED IAW DC8-5310-6988A. 2L74 4F RT4A25 19950609008031995060900803WP 1995 6 9 UPS803468 119950607A5320561229817 CEILING PANEL DOUG DC8 DC873F 302199FWP NLG WW CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NOSE WHEELWELL CEILING PRESSURE PANEL. REPAIRED IAW DC8-5330-7094-A. 2L74 4F RT4A25 19950609008041995060900804WP 1995 6 9 UPS803469 119950607A57125770123 LE RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS ON LT WING O/B LEADING EDGE RIBS. UPPER RIBS NR 5, 10, 12, 13, 14, 15, 19, 22. REPAIRED IAW SRM 57-00-00. 2L74 4F RT4A25 19950609008051995060900805WP 1995 6 9 UPS803470 119950607A53129751649 BULKHEAD DOUG DC8 DC873F 302199FWP FS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKS ON LT AND RT SIDE OF BULKHEAD, F.S. 683, LONGERONS 31L AND 31R. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950609008061995060900806WP 1995 6 9 UPS803471 119950607A575556551672 SKIN DOUG DC8 DC873F 302199FWP NR 3 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING NR 3 SPOILER ON LOWER O/B END. REPLACED SPOILER IAW M/M 27-01-01. 2L74 4F RT4A25 19950609008071995060900807WP 1995 6 9 UPS803472 119950607A54005253054508 FITTING DOUG DC8 DC873F 302199FWP NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 3 PYLON SUPPORT FITTING. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950609008081995060900808WP 1995 6 9 UPS803473 119950607A57305769600 SKIN DOUG DC8 DC873F 302199FWP WS 647.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT WING O/B LEADING EDGE UPPER SURFACE AROUND FASTENERS, STA XFS 647.500. REPAIRED IAW DC8-5720-7067-A. 2L74 4F RT4A25 19950609008091995060900809WP 1995 6 9 UPS803474 119950607A5313577992523 LONGERON DOUG DC8 DC873F 302199FWP FS 130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 36, F.S. 130. REPAIRED IAW DC8-5310-7068-A. 2L74 4F RT4A25 19950609008101995060900810WP 1995 6 9 UPS803491 119950608A2150 PACK DOUG DC8 DC873F 302199FWP LT PACK MALFUNCTIONED A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01813UP 46059 SUPPLEMENTAL MRR - UPON PUSH BACK AT SAN JUAN, LEFT PACK OVERHEATED 200 DEGREES, SMOKE IN COCKPIT, BLOCK TURNBACK. DEFERRED AS PER MEL 21-38-1 AND MMOC. MAINTENANCE PROCEDURES PERFORMED. OPS CHECK LT PACK, NO OVERTEMP, NO PACK TRIP, NO SMOKE IN COCKPIT. OAT 95F PACK TEMP 130F THROUGH FULL RANGE. OK FOR SERVICE. 2L74 4F RT4A25 19950609008151995060900815CE 1995 6 9 95ZZZX2825 119950512A3233 ACTUATOR LEAR 24 24 5170302CE LT MLG O-RING FAILED A KKFAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL2363CK 24119 HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. UNEVENTFUL LANDING ACCOMPLISHED. O-RING LT MAIN GEAR ACTUATOR LEAKING. INSTALLED NEW O-RING, LANDING GEAR HYDRAULIC RESERVOIR SERVICED AND GEAR FUNCTIONALLY CHECKED PER LEAR MM. O-RING PN MS287786. OPER CONTROL NR 5/15/9563CK. 2L72 4J A10CE 19950609008211995060900821EU 1995 6 9 95ZZZX2831 119950517A29127581452 FILTER ASSY ISRAEL1124 1124A 4500103EU GARRTTTFE731TFE7313 01518WP RT HYD O-RING CRIMPED A AJCAO OTHER J WARNING INDICATION CRCRUISE 1 EA2576ER 6 322 369 P77486 ABOUT 30 MINUTES BEFORE LANDING IN GRI, RT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BRAKES, BOTH HYDRAULIC ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE WAS LOST. A CRIMPED TEFLON O-RING BACKING ON THE RIGHT FILTER ASSEMBLY WAS FOUND. ADVISE USE OF EXTREME CARE WHEN INSTALLING FILTER. 2M72 4F4 F A2SW E6WE 19950609008251995060900825CE 1995 6 9 95ZZZX2835 119950321A27202300003179 CONTROL CABLE LEAR 25 25D 5170514CE RUDDER MISROUTED A AVNRAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW05347AC2270 347 UPON FINISHING AN AILERON CABLE TENSION CHECK, CENTER SECTION PANELS WERE OPENED TO CHECK CABLES AT AILERON CENTER SECTOR PULLEY. FOUND RIGHT RUDDER AND RIGHT ELEVATOR CABLES ROUTED OVER FUSELAGE TANK CROSSOVER HOSE PN E-161-16-35. THIS HOSE WAS REPLACED AT 12-YEAR INSPECTION. AIRCRAFT TT AT REPLACEMENT WAS 4255.5 HOURS. PART IN SERVICE TIME WAS 415.3 HRS. THE FLIGHT CONTROL CABLES AND HOSE WERE CHANGED. IT IS SUGGESTED THAT A THOROUGH INSPECTION BE DONE AFTER ANY MAINTENANCE REQUIRING CABLE LOOSENING/REPLACEMENT BE ACCOMPLISHED. 2L72 4J A10CE 19950609008261995060900826CE 1995 6 9 95ZZZX2836 119950321A27302300003172 CONTROL CABLE LEAR 25 25D 5170514CE ELEVATOR MISROUTED A AVNRAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW05347AC2270 347 UPON FINISHING AN AILERON CABLE TENSION CHECK, CENTER SECTION PANELS WERE OPENED TO CHECK CABLES AT AILERON CENTER SECTOR PULLEY. FOUND RIGHT RUDDER AND RIGHT ELEVATOR CABLES ROUTED OVER FUSELAGE TANK CROSSOVER HOSE PN E-161-16-35. THIS HOSE WAS REPLACED AT 12-YEAR INSPECTION. AIRCRAFT TT AT REPLACEMENT WAS 4255.5 HOURS. PART IN SERVICE TIME WAS 415.3 HRS. THE FLIGHT CONTROL CABLES AND HOSE WERE CHANGED. IT IS SUGGESTED THAT A THOROUGH INSPECTION BE DONE AFTER ANY MAINTENANCE REQUIRING CABLE LOOSENING/REPLACEMENT BE ACCOMPLISHED. 2L72 4J A10CE 19950616000011995061600001NM 1995 6 16 9509182291 119950607A3260656021132 ACCY UNIT BOEING727 727251 138408HNM LANDING GEAR MALFUNCTIONED A ANWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01291US275839956 21379 DURING APPROACH UPON LANDING GEAR EXTENSION, THREE GREEN AND THREE RED GEAR LIGHTS ILLUMINATED. RECYCLED GEAR WITH PROPER INDICATION, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ACCESSORY UNIT, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950616000021995061600002NE 1995 6 16 95UAL727040 219950609A7321 FUEL CONTROL HAMILTON STA7438023 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP297266U 46321 21413 700105 ABORTED TAKEOFF DUE TO NR 2 ENGINE UNABLE TO MAKE TAKEOFF POWER. REPLACED FAILED FUEL CONTROL UNIT. FUNCTIONALLY CHECKED ENGINE PER JET RUNUP HANDBOOK, CHECKS OK. 2L73 4F4 F A3WE E2EA 19950616000031995061600003NE 1995 6 16 95UAL747040 219950609A7230 COMPRESSOR BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 1 ENGINE STALLED A UALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29180UA 25224 717551 AT 800 FEET ON CLIMB-OUT NR 1 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE AND FIRED BOTTLES. 2L74 4F4 FRTA20WE E24NE 19950616000041995061600004NM 1995 6 16 95UAL757019 119950609A3230 LOCK PIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE NLG INSTALLED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29558UA 26654 UNABLE TO RAISE NOSE GEAR WHEN GEAR RETRACTED. REMOVED DOWNLOCK PIN FROM NOSE LANDING GEAR. 2L72 4F4 FRTA2NM E17NE 19950616000051995061600005WP 1995 6 16 ABXA9500529 119950606A3260313 BULB DOUG DC9 DC932 3022066WP NLG INDICATOR DEFECTIVE A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23903AX 47427 WHEN LOWERING LANDING GEAR GOT UNSAFE LIGHT. CYCLED NOSE GEAR, LIGHT DID NOT COME ON, CYCLED GEAR HANDLE, LIGHT CAME ON AND STAYED ON THROUGH OUT LANDING. TAPPED LIGHT WHEN IN BLOCKS, LIGHT WENT OUT. VERIFIED BOTH BULBS BURNT OUT ON NOSE GEAR DOWN INDICATION. REPLACED BOTH BULBS. GROUND OPS CHECKED GOOD IAW DC-9 SUPP MM 32-60-00. 2L72 4F A6WE 19950616000061995061600006WP 1995 6 16 ABXA9500530 119950608A335060030431 EEL DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23906AX 47072 EMERGENCY LIGHTS INOP. OPERATED EMERGENCY EXIT LIGHTS PER DC-9 MM. OPS CHECKED GOOD, NO DEFECTS NOTED. 2L72 4F A6WE 19950616000071995061600007NM 1995 6 16 DL72E952526 119950607A56105893543110RPR WINDSHIELD BOEING727 727247 138408FNM RT FLT DECK SHORTED/ARCING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO112824W 21329 DURING CRUISE, COPILOTS WINDSHIELD SHORTED WITH SPARKS BEING EMITTED. SHUT-OFF WINDOW HEAT, NO FURTHER ARCING. REPLACED WINDSHIELD AND CONTROLLER. 2L73 4F A3WE 19950616000081995061600008NM 1995 6 16 DL72L952500 119950607A5210 SKIN BOEING727 727232 1384082NM MAIN ENTRY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11504DA 21306 MAIN ENTRY DOOR OUTER SKIN IS CRACKED .125 AT RIVET, AFT UPPER CORNER. FOUND AT E-1 LTR CK. REPAIRED PER MM 52-11-01 PG 806. 2L73 4F A3WE 19950616000091995061600009NE 1995 6 16 DL72L952504 219950604A7250 TURB SHEAR PIN 38322211 BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A ADALAF ACTIVATE FIRE EXT. J WARNING INDICATION ININSP/MAINT 1 SO11503DA 11040 21305 700395 THIS ENGINE WAS EXHIBITING HIGH EGT INDICATIONS AND SENT TO ATL FOR ENGINE TEST RUN ON WING. A NORMAL START WAS PERFORMED WITH START VALVE LIGHT EXTINGUISHING. THEN, 15 MINUTES AFTER START AND IDLE THE ENGINE FIRE WARNING LIGHT ILLUMINATED, JUST PRIOR TO REACHING TAKEOFF POWER. LIGHT EXTINGUISHED AS ENGINE WAS SHUTDOWN. THE STARTER WAS FOUND TO HAVE HAD A TURBINE BEARING FAILURE FOLLOWED BY THE SHEARING OF THE EXDUCER ROLL PIN WHICH ALLOWED THE EXDUCER TO EXIT THE REAR OF THE CONTAINMENT BASKET. THE REMAINDER OF THE TURBINE WHEEL WAS CONTAINED IN THE STARTER SCROLL EXHAUST DUCT. 2L73 4F4 F A3WE E2EA 19950616000101995061600010NM 1995 6 16 DL72S952502 119950526A5753652163262 DOUBLER BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DOUBLER CRACKED AT AFT CHORD ANGLE 19 INCHES FROM I/B END. REMOVED AND REPLACED DOUBLER PER MM 57-52-0, NR 3 MIDFLAP AT HMV, SHOP VISIT. 2L73 4F A3WE 19950616000111995061600011NM 1995 6 16 DL72S952507 119950523A5313 STRINGER BOEING727 727232 1384082NM FS 540 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 FWD B/B STR 28R CORRODED ON UPPER FLANGE, JUST FWD OF STA 540. REPAIRED PER SRM 53-10-3 PG 4C, FOUND AT HMV. 2L73 4F A3WE 19950616000121995061600012NM 1995 6 16 DL72S952524 119950607A2120 AIR DISTR BOEING727 727232 1384082NM CABIN ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11527DA 21587 ON APPROACH, SEVEN MINUTES PRIOR TO LANDING HAD SULFUR TYPE ODOR IN CABIN. SHUTDOWN GALLEY POWER AND GASPER, FAN ODOR QUICKLY DISSIPATED. LANDED TUL, INSPECTED CABIN LIGHTS GALLEYS, RAN AND INSPECTED PACKS, COULD NOT DUPLICATE. REPLACED WATER SEPARATOR BAGS, RETURNED TO SERVICE. 2L73 4F A3WE 19950616000131995061600013NM 1995 6 16 DL757952510 119950607A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1660 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE CABIN FLOORBEAM AT STA 1660 WAS FOUND TO HAVE SEVERAL FASTENER HOLES CORRODED THE ENTIRE LENGTH OF THE BEAM. CORROSION WAS CLEANED PER SRM 51-10-00 AND FOUND WITHIN LIMITS, EXCEPT HOLE AT RBL 4. REPAIR WAS FABRICATED FOR RBL 4 PER SRM 53-10-51 AND INSTALLED PER SAME, AREA WAS TREATED AND PAINTED. 2L72 4F RTA2NM 19950616000141995061600014NM 1995 6 16 DL757952525 119950607A3350BPS73 EEL BATTERY BOEING757 757232 1384965NM CABIN DEPLETED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11631DL 23612 DURING LAY OVER, FWD CABIN FLOOR TRACK EMERGENCY LIGHTS WERE INOP. REPLACED BATTERY OPERATION NORMAL. 2L72 4F RTA2NM 19950616000151995061600015WP 1995 6 16 DLL10952508 119950523A57551529101151 PANEL LKHEED1011 10113851 5265010WP SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THE SPOILER PANEL HAD 2 AREAS OF DELAMINATION. THE DELAMINATED AREAS WERE REPAIRED PER SRM 57-52-00, FOUND AT HMV. 2L73 4F A23WE 19950616000161995061600016WP 1995 6 16 DLL10952509 119950526A5320 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1575 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRAP DISBONDED, FUSELAGE FAIL-SAFE STRAP DISBONDED ABOVE STR 40 FS 1575. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950616000171995061600017WP 1995 6 16 DLL10952514 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 923/903 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAPS DISBONDED AT STR 29 AND 27 BETWEEN STA 923 AND 903. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950616000181995061600018WP 1995 6 16 DLL13952520 119950509A5743 ANGLE LKHEED1011 10113851 5265010WP RT MLG TRUNNION WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND VERTICAL ANGLE WORN DOWN, AFT OF RM6 TRUNNION OUT BD EDGE OF TRIANGULAR PANEL. CUT OUT, DRILLED UP AND PAINTED NEW ANGLE, INSTALLED PER SRM 57-22-00. 2L73 4F A23WE 19950616000191995061600019WP 1995 6 16 DLL13952521 119950513A5311 FRAME LKHEED1011 10113851 5265010WP FS 267 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FRAME CRACKED STA 267 RT SIDE OF E AND E ABOVE STR 9. REPAIRED PER SRM 53-12-00 FIG 805 AND DL ERA 271044-14. 2L73 4F A23WE 19950616000201995061600020WP 1995 6 16 DLL13952522 119950513A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1783 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND TEAR STRAP DISBONDED AT FS 1783 BETWEEN STR 23 THROUGH 24. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950616000211995061600021NE 1995 6 16 95ZZZW784 219950422A7230771706 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 2 ENGINE FAILED A TWAAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE05901TW 49166 FLT 280 - LAX - AFTER TAKEOFF NR 2 ENGINE STALLS. REDUCED POWR NR 2 ENGINE. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE S/N 1422. ENGINE OPERATION CHECKS NORMAL. S/D - INVESTIGATION INTO ENGINE S/N 1422 COMPRESSOR STALLS, REVEALED A 6TH STAGE COMPRESSOR BLADE, MFG P/N 771706, FRACTURED DUE TO IMPACT CAUSING THREE OTHER 6TH STAGE BLADES TO FRACTURE RESULTING IN HEAVY DOWN STREAM DAMAGE TO LOW PRESSURE AND HIGH PRESSURE COMPRESSORS. ENGINE REPAIRED AND RETURNED TO SERVICE. (W) 2L72 4F4 F A6WE E9NE 19950616000221995061600022WP 1995 6 16 CAL950344 119950501A335000060932658 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09938MC 49525 FLT NR 0477 - EWR - EMERGENCY LIGHTING IN OVERHEAD AND PATH INOP. REMOVED AND REPLACED BATTERY PACK AND RELAMPED SEVERAL LIGHT BULBS. (W) 2L72 4F RTA6WE 19950616000231995061600023NM 1995 6 16 CAL950376 119950510A32301U1085 SEQ VALVE BOEING727 727243 138408DNM RT MLG CRACKED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW091740716901 21270 FLT NR 0362 - EWR - THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY WAS LOST IMMEDIATELY AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MAIN GEAR LOCK OPERATED SEQUENCE VALVE CRACKED. THE SEQUENCE VALVE WAS REMOVED AND REPLACED AND THE 'S' HYDRAULIC SYSTEM WAS SERVICE TO FULL. A GEAR SWING WAS PERFORMED WITH NO LEAKS OR DEFECTS NOTED. (W) 2L73 4F RTA3WE 19950616000241995061600024WP 1995 6 16 CAL950387 119950514A3246 BEARING 5920604501 DOUG DC9 DC982 3022082WP NLG AXLE WORN A CALAK NONE O OTHER TXTAXI/GRND HDL 1 SW0916815 CPI352 49113 FLT NR 0692 - EWR - THE NOSE GEAR MADE A GRINDING NOISE WHILE TAXIING. MAINTENANCE FOUND THE NOSE GEAR WHEEL BEARING WORN CAUSING THE WHEEL TO GAUGE AXLE. THE NLG AXLE WAS REMOVED AND REPLACED. THE NOSE GEAR SHOCK STRUCT WAS REPACKED PER MM 32-21-02, PAGE 801. IN ADDITION, BOTH NOSE TIRES WRE REPLACED AS A PRECAUTIONARY MEASURE. (W) 2L72 4F A6WE 19950616000251995061600025NM 1995 6 16 CAL950397 119950518A29136507506 HYD PUMP BOEING727 727227 1384078NM NR 1 ENGINE LEAKING A CALAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW09177736437 57 21045 FLT NR 0693 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 HYDRAULIC PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (W) 2L73 4F A3WE 19950616000261995061600026NM 1995 6 16 CAL950398 119950510A5311 FRAME BOEING737 737130 1384435NM FS 460 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S22L AND S23L AT STATION 460. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME AND DOUBLERS WERE INSTALLED IAW BOEING PRINT NR 65C25113. (W) 2L72 4F A16WE 19950616000271995061600027NM 1995 6 16 CAL950399 119950510A5311 FRAME BOEING737 737130 1384435NM FS 480 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 480. THE CRACKED SECTION OF FRAME WAS CUOTUT. A NEW SECTION OF FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W) 2L72 4F A16WE 19950616000281995061600028NM 1995 6 16 CAL950400 119950510A5311 FRAME BOEING737 737130 1384435NM FS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 500. THE CRACKED SECTION OF FRAME WAS CUTOUT. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW BOEING BLUE PRINT NR 65C25113 AND EA 5310-01211. (W) 2L72 4F A16WE 19950616000291995061600029NM 1995 6 16 CAL950401 119950510A5311 FRAME BOEING737 737130 1384435NM FS 440 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME BETWEEN S20L AND S21L AT STATION 440. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING NR 65C25113 AND EA 5310-01211. (W) 2L72 4F A16WE 19950616000301995061600030NM 1995 6 16 CAL950402 119950510A5311 FRAME BOEING737 737130 1384435NM FS 529 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND CORROSION ON FRAME ABOVE STRINGER 26R AT STATION 529. A NEW FRAME AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2. (W) 2L72 4F A16WE 19950616000311995061600031NM 1995 6 16 CAL950403 119950510A5330 SKIN BOEING737 737130 1384435NM FS 908 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND A .5 INCH CRACK IN EXTERNAL SKIN AT STRINGER 4L, STATION 908. THE CRACKED AREA WAS CUTOUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (W) 2L72 4F A16WE 19950616000321995061600032NM 1995 6 16 CAL950404 119950510A5330 SKIN BOEING737 737130 1384435NM BS 188-251.6 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL LOCATIONS BETWEEN BS 188-251.6 RIGHT SIDE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED SECTION OF SKIN WAS REMOVED. REPAIR DOUBLER S AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188 AND SRM 51-30-2. (W) 2L72 4F A16WE 19950616000331995061600033NM 1995 6 16 CAL950405 119950510A5330 SKIN BOEING737 737130 1384435NM WL 207.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420862609 19025 GSO - INSPECTION FOUND FUSELAGE SKIN FASTENER HOLES CRACKED IN SEVERAL PLACES BETWEEN WL 207.5 AND 234.35, SECTION 41. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE CRACKED AREA WAS REMOVED. DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188 AND SRM 51-30-2. (W) 2L72 4F A16WE 19950616000341995061600034NM 1995 6 16 CAL950407 119950519A2910 HYD LINE BOEING737 7373T0 1384582NM LT MLG LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0917309 23360 FLT NR 0419 - CLE - THE 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE IN FLIGHT. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT. THE AIRCRAFT LANED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG ACTUATOR DOWN FLEX LINE LEAKING. THE FLEX LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. IN ADDITION, THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. (W) 2L72 4F RTA16WE 19950616000351995061600035NM 1995 6 16 CAL950408 119950519A3610652673831 DUCT BOEING727 727227 1384078NM NR 2 ENGINE RUPTURED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0915774 21242 FLT NR 0238 - SFO - THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF FROM SFO. WHEN THE THROTTLE WAS REDUCED THE WARNING CEASED, BUT UPON INCREASING POWER THE WARNING WOULD ACTIVATE AGAIN. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE HIGH PRESSURE SUPPLY DUCT RUPTURED. THE DUCT WAS REMOVED AND REPLACED. THE NR 2 ENGINE WAS RUN AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (W) 2L73 4F A3WE 19950616000361995061600036NM 1995 6 16 CAL950412 119950522A2782269002911 ACTUATOR BOEING727 727232 1384082NM NR 3 LE SLAT LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW091777917169 20634 FLT NR 0209 - IAH - THE 'A' HYDRAULIC SYSTEM QUANTITY BEGAN TO DROP WHILE EN ROUTE TO IAH. THE FLUID LOSS WAS STABILIZED BY THE CREW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 LEADING EDGE SLAT ACTUATOR LEAKING. THE SLAT ACTUATOR WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (W) 2L73 4F A3WE 19950616000371995061600037NM 1995 6 16 CAL950415 119950523A3230 SELECT VALVE BOEING737 7373T0 1384582NM LT MLG WW INOPERATIVE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0976354 23592 FLT NR 0356 - BOS - THE LANDING GEAR INADVERTENTLY REMOVED WHILE CLIMBING THROUGH 17,000 FEET WITH THE GEAR HANDLE IN THE OFF POSITION. THE GEAR HANDLE WAS MOVED TO THE UP POSITION AND THE LANDING GEAR RETRACTED. WHEN THE GEAR WAS EXTENDED FOR LANDING, EXTENSION WAS NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENACNE FOUND THE L/G CONTROL SELECTOR VALVE AT FAULT. THE VALVE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. A LANDING GEAR TEST WAS PERFORMED PER MM 32-31-51 AND A LANDING GEAR CONTROL ADJUSTMENT AND TEST WAS PERFORMED PER MM 32-31-00. IN ADDITION, A LANDING GEAR DOWN OVERSPEED CONDITION CHECK WAS PERFORMED PER MM 05-51-47. NO DEFECTS WERE NOTED. (W) 2L72 4F RTA16WE 19950616000381995061600038NM 1995 6 16 CAL950418 119950524A29136507506 HYD PUMP BOEING727 727232 1384082NM 'A' HYD SYSTEM INOPERATIVE A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0910791 20645 FLT NR 0774 - IAH - THE 'A' SYSTEM HYDRAULIC QUANTITY WENT TO ZERO AND WAS ACCOMPANIED BY LOSS OF 'A' SYSTEM PRESSURE WHLE IN FLIGHT. THE LANDING GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH THE NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS. THE ENGINES WERE RUN AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (W) 2L73 4F A3WE 19950616000391995061600039NM 1995 6 16 USAA950459 119950508A2550 CARGO NET BOEING737 737301 1384611NM CARGO DOOR OUT OF POSITION A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19559AU 23513 ABQ - FLT 1473 - FLIGHT EN ROUTE PHX TO CLT WHEN CABIN PRESSURIZATION WARNING SOUNDED. FLIGHT DIVERTED TO ABQ WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CARGO NET LODGED IN FORWARD CARGO DOOR. REMOVED NET AND CLOSED DOOR. OPS CHECK OK. (W) 2L72 4F RTA16WE 19950616000401995061600040NM 1995 6 16 USAA950489 119950420A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 747-767 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 747 TO BSL 767 LBL 24 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000411995061600041NM 1995 6 16 USAA950490 119950328A532065C333701 INTERCOSTAL BOEING737 737401 1384701NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 967 LBL 24. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000421995061600042NM 1995 6 16 USAA950491 119950331A53206546812169 INTERCOSTAL BOEING737 737401 1384701NM BS 975 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER CORROSION AT SCREW HOLE, BS 975 RBL 18. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000431995061600043NM 1995 6 16 USAA950492 119950323A5320 ANGLE BOEING737 737401 1384701NM BS 727-827 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 180 INCHES OF CORROSION BS 727C TO BS 827 S-25L. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000441995061600044NM 1995 6 16 USAA950493 119950330A5315 FLOORBEAM BOEING737 737401 1384701NM BS 987 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 2 INCH CORRODED AREA BS 987 LBL 50. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000451995061600045NM 1995 6 16 USAA950494 119950404A5315 FLOORBEAM BOEING737 737401 1384701NM BS 987 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 4 SQUARE INCH BS 987 LBL 50 TO RBL 50. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-10-01A, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000461995061600046NM 1995 6 16 USAA950495 119950404A5315 FLOORBEAM BOEING737 737401 1384701NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.75 INCH DIAMETER CORROSION BS 947 LBL 4. REPAIRED PER EA 39037. REPAIRED PER EA 39037. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000471995061600047NM 1995 6 16 USAA950496 119950404A5320 ANGLE BOEING737 737401 1384701NM BS 927-1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 927 TO BS 1006 AT AFT ENTRY DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000481995061600048NM 1995 6 16 USAA950497 119950404A5320 ANGLE BOEING737 737401 1384701NM BS 967-986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORRODED AREA (SIZE UNKNOWN) BS 967-986.5 AT AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000491995061600049NM 1995 6 16 USAA950498 119950329A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES BS 967 RBL 18 INCHES. REPAIRED PER SRM 53-60-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000501995061600050NM 1995 6 16 USAA950499 119950329A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH BS 947 TO 967 LBL 18 INCHES. REPAIRED PER SRM 53-60-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000511995061600051NM 1995 6 16 USAA950500 119950327A532065C333671 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 3 INCH BY 3 INCH CORROSION TOP FLANGE AREA BS 947 TO BS 967 LBL 60 INCHES. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000521995061600052NM 1995 6 16 USAA950501 119950303A532069434772 ANGLE BOEING737 737401 1384701NM BS 787-767 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROISON AT SCREW HOLES, BS 787-767 S-25R. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000531995061600053NM 1995 6 16 USAA950502 119950323A53206545895527 ANGLE BOEING737 737401 1384701NM BS 294-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19407US19492 23877 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 36 INCH BY 3 INCH CORRODED AREA BETWEEN BS 294 AND 344 RBL 55. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000541995061600054NM 1995 6 16 USAA950509 119950405A53201126536 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA BS 947-967 48 INCHES LBL AT AFT ENTRY DOOR. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000551995061600055NM 1995 6 16 USAA950510 119950330A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 INCH LONG BY 2 INCH WIDE CORROSION TOP OF INTERCOSTAL BS 312 TO BS 328 RBL 12 INCHES. REPAIRED PER SRM 53-10-01. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000561995061600056NM 1995 6 16 USAA950511 119950410A5320654795711 STRAP BOEING737 7373B7 1384580NM BS 787-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 40 INCH CORRODED AREA AFT CARGO STRAP BS 787-847. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950616000571995061600057CE 1995 6 16 95ZZZX2845 119950501A361099120256 COUPLING CESSNA500 S550 2076607CE RT ENG BLEED DETACHED ALADXTAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL07126QS S5500126 CREW REPORTED HIGH OIL TEMP, LOW OIL PRESS, AND HIGH ITT. A RAPID SHIFT IN GAUGES WAS NOTED ALONG WITH AN INTERMITTENT FIRE LIGHT. UPON LANDING, RT ENGINE COWLING WAS OPENED AND THE INBOARD BLEED AIR COUPLING AND PERISEALS WERE FOUND IN THE LOWER COWL. THE HOUSING CLAMPS WERE STILL ATTACHED TO THE BLEED AIR PIPES. 1L72 4F RTA22CE 19950616000651995061600065NM 1995 6 16 95ZZZX2853 119950505A5320 INTERCOSTAL BOEING727 727225 1384077NM FS 1050 BL 12L CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK INSPECTION, FOUND INTERCOSTAL Z-CHANNEL CORRODED OUT OF LIMITS FORWARD AND AFT OF FLOOR BEAM AT BS 1050, BL 12L. 2L73 4F A3WE 19950616000661995061600066NM 1995 6 16 95ZZZX2854 119950505A5330 SKIN BOEING727 727225 1384077NM FS 930-940 CRACKED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND 5 INCH CRACK ON SKIN KEEL BEAM AREA BETWEEN STA 930 AND STA 940 RIGHT. 2L73 4F A3WE 19950616000671995061600067NM 1995 6 16 95ZZZX2855 119950505A5320 INTERCOSTAL BOEING727 727225 1384077NM FS 950A-950B ANGLE CRACKED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK INSPECTION, FOUND INTERCOSTAL UPPER ATTACH ANGEL CRACKED FIVE PLACES BETWEEN FLOOR BEAM 950A AND 950B, B.L.O. 2L73 4F A3WE 19950616000681995061600068NM 1995 6 16 95ZZZX2856 119950505A5315 FLOORBEAM BOEING727 727225 1384077NM BS 1090 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM AT BS 1090, B.L.O., CORRODED OUT OF LIMITS (4 INCH AREA). 2L73 4F A3WE 19950616000691995061600069NM 1995 6 16 95ZZZX2857 119950505A5330 SKIN BOEING727 727225 1384077NM FS 500 STR 27L CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK INSPECTION AND C.P.C.P. INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CORRODED AT BS 500, STR 27L (APPROXIMATELY 3 INCH AREA). CORROSION OUT OF LIMITS. 2L73 4F A3WE 19950616000701995061600070NM 1995 6 16 95ZZZX2858 119950505A2782 MOUNT BOEING727 727225 1384077NM NR 2 SLAT ACT LUG CRACKED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258883Z 21580 DURING C-CHECK INSPECTION, FOUND NR 2 SLAT ACTUATOR INBOARD TRUNNION MOUNT LUG CRACKED. 2L73 4F A3WE 19950616000721995061600072NM 1995 6 16 95ZZZX2860 119950316A5320 INTERCOSTAL BOEING727 727225 1384077NM FS 344-360 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM INTERCOSTAL FROM BS 344 - BS 360 AT BL 10R CORRODED. FABRICATED REPLACEMENT INTERCOSTAL OF 7075-T6, DASH 090 T-ANGLE PER SRM 51-40-3. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2. 2L73 4F A3WE 19950616000731995061600073NM 1995 6 16 95ZZZX2861 119950316A5330 SKIN BOEING727 727225 1384077NM FS 1070 STR 28R CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SKIN BULGED AT STA 1070, STR 28R. FOUND STRINGER SECTION (10 INCH) CORRODED. REMOVED DAMAGED SECTION, FABRICATED REPAIR SECTION PER SRM 53-10-3. TREATED AND PRIMED AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-3. 2L73 4F A3WE 19950616000741995061600074NM 1995 6 16 95ZZZX2862 119950316A5320 INTERCOSTAL BOEING727 727225 1384077NM FS 1070 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND INTERCOSTAL CORRODED AT BS 1070, JUST INSIDE L2 DOOR, CORRODED BEYOND LIMITS. FABRICATED REPLACEMENT INTERCOSTAL USING 7075-T6, .040 INCH PER SRM 51-10-1. TREATED. PRIMED, INSTALLED PER SRM 51-10-2, SRM 51-30-2, AND SOP 20-50-1. 2L73 4F A3WE 19950616000751995061600075NM 1995 6 16 95ZZZX2863 119950316A5347 SEAT TRACK BOEING727 727225 1384077NM FS 344-380 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK BENEATH NR 1 GALLEY FROM BS 344 - BS 380 AT BL 22R AND BL 52R. REMOVED DAMAGED SECTIONS. FABRICATED REPLACEMENT SEAT TRACK SECTIONS. TREATED AND RPIMED PER SRM 51-10-1, SRM 51-10-2. INSTALLED PER SRM 51-30-2. 2L73 4F A3WE 19950616000761995061600076NM 1995 6 16 95ZZZX2864 119950316A5347 SEAT TRACK BOEING727 727225 1384077NM FS 420-450 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK AT BS 420 - BS 450, BL 52R, CORRODED. REMOVED SEAT TRACKS, FABRICATED REPLACEMENT TRACKS IAW SRM 51-10-1. TREATED, PRIMED, AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-5. 2L73 4F A3WE 19950616000771995061600077NM 1995 6 16 95ZZZX2865 119950316A5347 SEAT TRACK BOEING727 727225 1384077NM FS 380-400 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND SEAT TRACK AT BS 380 - BS 400, BL 24R, CORRODED. REMOVED SEAT TRACKS, FABRICATED REPLACEMENT TRACKS IAW SRM 51-10-1. TREATED, PRIMED, AND INSTALLED PER SRM 51-10-2 AND SRM 53-10-5. 2L73 4F A3WE 19950616000781995061600078NM 1995 6 16 95ZZZX2866 119950316A5315 FLOOR BEAM BOEING727 727225 1384077NM FS 344 BL 10R CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM AT BS 344 FROM BL 10R TO BL 45R CORRODED. FABRICATED REPLACEMENT UPPER CHORD FROM BAC1505-100617, 7075-T3 EXTRUSION PER SRM 51-30-5. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED PER SRM 53-10-8. 2L73 4F A3WE 19950616000791995061600079NM 1995 6 16 95ZZZX2867 119950316A5315 FLOOR BEAM BOEING727 727225 1384077NM FS 328 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM CORRODED AT STA 328 - BL0 18L. REMOVED DAMAGED SECTION. FABRICATED REPAIRS PER BOEING REPAIR PLAN M-7272-95-0282. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED PER M-7272-95-0282 AND SRM 51-30-2. 2L73 4F A3WE 19950616000801995061600080NM 1995 6 16 95ZZZX2868 119950316A5315 FLOOR BEAM BOEING727 727225 1384077NM FS 380 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA258880Z 21453 DURING C-CHECK AND C.P.C.P. INSPECTION, FOUND FLOOR BEAM CORRODED AT BS 380, BL 0-10L, AND BL 10-40R. REMOVED DAMAGED SECTION OF FLOOR BEAM UPPER CHORD. FABRICATED REPAIRS WITH 7075-T6; .050 INCH, AND 7075-T6; .080 INCH, MATERIAL PER SRM 53-10-8 AND BOEING REPAIR FAX M-7272-95-0287. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2 AND SRM 53-10-8, FIGURE 3. 2L73 4F A3WE 19950616000811995061600081NM 1995 6 16 95ZZZX2870 119950217A5313 STRINGER BOEING727 727251 138408HNM FS 675 STR 19L CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25259US 19978 DURING INSPECTION OF AD 91-06-06, FOUND STR 19L AT BS 675 EXFOLIATED ON INBOARD LOWER FLANGE. REMOVED DAMAGED AREA OF STRINGER. FABRICATED STRINGER SPLICE FROM BAC 1498-125, 7075-T6 STRINGER MATERIAL AND NEW STRINGER TIE FROM .040 INCH, 7075-T6. TREATED MATERIALS, PRIMED, AND INSTALLED IAW SRM 51-20-1, SRM 53-10-3, SRM 51-10-2, AND SRM 51-30-2. 2L73 4F A3WE 19950616000821995061600082NM 1995 6 16 95ZZZX2871 119950217A5313 STRINGER BOEING727 727251 138408HNM FS 359 STR 26 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25259US 19978 DURING BOEING C.P.C.P. INSPECTION, FOUND SKIN BULGE AT STR 26R, STA 359. CUT OUT DAMAGED STRINGER SECTION. SKIN NOT DAMAGED. FABRICATED REPAIR FILLER AND DOUBLER FROM 7075-T6. TREATED PARTS AND PRIMED, AND INSTALLED IAW SRM 51-40-4, SRM 51-20-2, SRM 51-20-4, AND SRM 51-30-2. 2L73 4F A3WE 19950616000831995061600083NM 1995 6 16 95ZZZX2872 119950127A5315 FLOOR BEAM BOEING727 727251 138408HNM FS 400 BL10 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25264US 19983 DURING C-CHECK INSPECTION, FOUND CORROSION DAMAGE ON UPPER CHORD OF THE BS 400, FLOOR BEAM FROM RBL 9.1 TO RBL 11.6. CUT OUT DAMAGED AREA, FABRICATED SHIMS, AND REPAIR ANGLES. TREATED AND INSTALLED PER BOEING REPAIR FAX M-7272-95, AND SRM 53-10-8, DATED JANUARY 16, 1995. 2L73 4F A3WE 19950616000841995061600084NM 1995 6 16 95ZZZX2873 119950127A5320 INTERCOSTAL BOEING727 727251 138408HNM FS 1090-1100 CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25264US 19983 DURING C-CHECK INSPECTION, FOUND INTERCOSTAL BETWEEN STA 1090 - STA 1100, STR 6L, GOUGED ON INBOARD FLANGE. BLENDED DAMAGE OUT OF LIMITS PER SRM 53-10-1, FIGURE 1. FABRICATED REPAIR DOUBLER, FROM 7075-T6, .071 INCH, TREATED, PRIMED, AND INSTALLED PER SRM 51-40-3, FIGURE 1, SRM 51-10-2, S.O.H.M. 20-41-02. 2L73 4F A3WE 19950616000851995061600085NM 1995 6 16 95ZZZX2874 119950127A5330 SKIN BOEING727 727251 138408HNM FS 490 STR 19R CORRODED A IXKAK NONE O OTHER ININSP/MAINT 1 EA25264US 19983 DURING C-CHECK INSPECTION OF AD 91-06-06 PER KIWI INTERNATIONAL AIRLINES EA 2753S001 PTS II AND III, FOUND SKIN CORRODED AT LAP STR 19R, STA 490. CUT OUT DAMAGED AREA (3 INCHES), FABRICATED REPAIR DOUBLERS, TREATED, PRIMED, INSTALLED, AND SEALED PER SRM 53-30-3, FIGURE 5, SRM 53-30-03, FIGURE 3, SRM 51-20-4, SRM 51-30-5, AND SRM 20-49-03. 2L73 4F A3WE 19950616000881995061600088NM 1995 6 16 9509192255 119950610A2424902F2425 GEN CONTL PNL BOEING727 727251 138408HNM NR 3 ENGINE FAILED A NWAACDH ABORTED TAKEOFF RETURN TO BLOCK DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TOTAKEOFF 1 GL01255US444502441 19974 DURING TAKEOFF, THE NR 3 GENERATOR BREAKER TRIPPED AND WOULD NOT RESET. ABORTED DEPARTURE AT 10 KNOTS. MAINTENANCE DEFERRED NR 3 GENERATOR PER MEL 24-1B. DTW MAINTENANCE REPLACED THE NR 3 ENGINE GENERATOR CONTROL PANEL. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950616000891995061600089SO 1995 6 16 COM11913 119950611A5610BP1513111 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT CRACKED A COMAO OTHER O OTHER CRCRUISE 1 SO01463CA106 106 120267 LT WINDSHIELD CRACKED DURING FLIGHT. REPLACED WINDSHIELD. 2L72 4T RTA31SO 19950616000901995061600090NE 1995 6 16 COM11914 219950611A731110718D FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMAO OTHER K FLUID LOSS UKUNKNOWN 1 SO01137H 9349 194 120137 RT ENGINE IS LEAKING FUEL. REPLACED THE ENGINE FUEL HEATER. 2L72 4T4 TRTA31SO E20NE 19950616000911995061600091SO 1995 6 16 COM11915 119950605A5720 SUPPORT EMB 120 EMB120RT SO LT/RT WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01130G 15510 120130 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERODESIGN REPAIR 1327-2. P/N: 120-17062-005, 1 EA; 120-17056-017, 2 EA; 120-17056-015, 4 EA; 120-17056-013, 2 EA; 120-17057-005, 1 EA; 120-17057-007, 2 EA; 120-17056-011, 1 EA; 120-17056-019, 1 EA; 120-17057-006, 1 EA; 120-17059-017, 1 EA. 2L72 4T RTA31SO 19950616000921995061600092EU 1995 6 16 COM31097 119950609A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01359CA11429468 OCT910026 340A053 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERIVCE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950616000931995061600093EU 1995 6 16 COM31098 119950609A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU RT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01380CA10147337 FEB920232 340A012 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950616000941995061600094EU 1995 6 16 COM31099 119950608A56108103731 WINDSHIELD SAAB SF340 SF340A 7850100EU LT COCKPIT LEAKING A COMAK NONE O OTHER CRCRUISE 1 SO01343CA4114 1852 340A024 PILOTS WINDSHIELD SQUEALS LOUDLY DUE TO DEFECTIVE SEAL. REPLACED PILOTS WINDSHIELD ASSY. 2L72 4T RTA52EU 19950616000951995061600095EU 1995 6 16 COM31100 119950607A33506013211 EEL POWER SUPPLY SAAB SF340 SF340A 7850100EU CABIN FAILED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01146CA 340A146 THREE EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY POWER SUPPLY CASE. 2L72 4T RTA52EU 19950616000961995061600096EU 1995 6 16 COM31101 119950609A3150004WS00 WEU SAAB SF340 SF340A 7850100EU AVIONICS DEFECTIVE A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01344CA16177129 340A025 RT FIRE DETECTION FAIL WARNING ILLUMINATED. REPLACED THE WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19950616000971995061600097EU 1995 6 16 COM31102 119950608A8097 WIRE SAAB SF340 SF340A 7850100EU LT BATT BAY BROKEN A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01358CA22198 340A047 LEFT ENGINE WILL NOT START, NO ROTATION. REPAIRED BROKEN WIRE AT RELAY 83PC AND ENGINE STARTS NORMAL. 2L72 4T RTA52EU 19950616000981995061600098EA 1995 6 16 COM60496 119950611A3260 INDICATION CNDAIRCL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01914CA 7012 LANDING GEAR DISAGREE MESSAGE, WHEN GEAR SELECTED DOWN. CYCLED GEAR AND INDICATIONS NORMAL. COULD NOT DUPLICATE DISCREPANCY, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950616000991995061600099NM 1995 6 16 DL72K952550 119950609A3350900835A EEL BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11410DA 21222 DURING LAY OVER, R2 OVERWING EMERGENCY EXIT LIGHT FAILED TO TEST. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19950616001001995061600100 1995 6 16 DL76L952551 419950609A221015405005 ACTUATOR BOEING767 767332 1382001NM YAW DAMPER LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11183DN 27110 DURING CRUISE, HAD LEFT HYDRAULIC QUANTITY EICAS MSSG WITH ASSOCIATED LEFT HYD RSVR LIGHT. RETURNED JFK, FOUND LEFT YAW DAMPENER ACTUATOR LEAKING. REPLACED ACTUATOR, OPERATION NORMAL. 2L72 4F RTA1NM 19950616001011995061600101NM 1995 6 16 DLM88952548 119950608A3020777790 PNEUMATIC TUBE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO11916DL 49591 725436 ON CLIMBOUT HAD NR 2 ENGINE FIRE WARNING. REDUCED POWER AND FIRE WARNING STOPPED. RETURNED TO ATL, FOUND ENGINE INLET ANTI-ICE PNEUMATIC TUBE BURST AT MID SPAN. REPLACED TUBE, OPERATION NORMAL. 2L72 4F4 FRTA6WE E9NE 19950616001021995061600102NM 1995 6 16 DLM88952549 119950610A2150 PACK DOUG MD88 MD88 3023688NM CABIN ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11977DL 53258 ON CLIMBOUT, FLT ATTENDANT REPORTED BURNING ODOR COMING FROM AIR CONDITIONING SYSTEM, NO SMOKE WAS VISIBLE. RT PACK WAS SHUTDOWN, ODOR DISSIPATED. INSPECTED PACK, ALL NORMAL. PERFORMED DUCT BURNOUT, RETURNED TO SERVICE. 2L72 4F RTA6WE 19950616001031995061600103NM 1995 6 16 QXEA9500177 119950609A33501013075 EEL BULB DHAV DHAV DHC8 DHC8102 2809003NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09822PH 106 SEA - ONE BULB INOP IN FORWARD RED FLOOR PROXIMITY LIGHT. REPLACED BULB AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950616001041995061600104NM 1995 6 16 UPS203493 119950609A5521659561310 RIB BOEING727 7272A1 138407FNM RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND RT NR 4 BALANCE BAY I/B RIB CRACKED. REPLACED RIB IAW SRM 51-30-2, 51-30-5. 2L73 4F A3WE 19950616001051995061600105NM 1995 6 16 UPS203494 119950609A575465217515A BULLNOSE BOEING727 7272A1 138407FNM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND NR 3 K-FLAP BULLNOSE I/B LOWER ADJUSTMENT ROD ATTACH POIINT CORRODED. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11. 2L73 4F A3WE 19950616001061995061600106NM 1995 6 16 UPS203495 119950609A575465217505A BULLNOSE BOEING727 7272A1 138407FNM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP BULLNOSE AROUND LOWER ATTACH POINT HAS CORROSION. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11, 20-20-00, M/M 27-81-00. 2L73 4F A3WE 19950616001071995061600107NM 1995 6 16 UPS203496 119950609A5320 SHEAR TIE BOEING727 7272A1 138407FNM FS 1268 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01214UP 21342 WHILE IN C-CHECK, MAINTENANCE FOUND TWO CRACKS IN SHEAR TIE AT BS 1268, BETWEEN STR 11 AND 12, 13 AND 14. INSTALLED FABRICATED PARTS IAW SRM 53-10-04. 2L73 4F A3WE 19950616001081995061600108NM 1995 6 16 UPS203497 119950609A5320 WEB BOEING727 72725C 138400HNM FS 1110-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT STA 1110 THROUGH 1130, RBL 25, WL 200. INSTALLED FABRICATED PARTS IAW SRM 53-10-2, 51-20-1, 51-30-2, 51-10-2, M/M 51-20-151. 2L73 4F A3WE 19950616001091995061600109NM 1995 6 16 UPS203498 119950609A5753651927015 FLAP TRACK BOEING727 72725C 138400HNM NR 5 TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 5 FLAP TRACK. INSTALLED NEW TRACK IAW M/M 27-51-31. 2L73 4F A3WE 19950616001101995061600110NM 1995 6 16 UPS203499 119950609A5320 WEB BOEING727 72725C 138400HNM FS 1110-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON WEB AT STA 1110 THROUGH 1130, RBL 45, WL 200. INSTALLED FABRICATED PARTS IAW SRM 51-20-1, 51-20-4, 51-30-2. 2L73 4F A3WE 19950616001111995061600111NM 1995 6 16 UPS203500 119950609A5753 SKIN BOEING727 72725C 138400HNM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON RT WING O/B FLAP AT I/B END UPPER SURFACE. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950616001121995061600112NM 1995 6 16 UPS203501 119950609A5315 FLOORBEAM BOEING727 72725C 138400HNM FS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER AND LOWER FLOORBEAM AT STA 1130, RBL 25, WL 200 TO 208. REPAIRED IAW EO 727-53-1614, SRM 51-10-1. 2L73 4F A3WE 19950616001131995061600113NM 1995 6 16 UPS203502 119950609A5320651986219 CHORD BOEING727 72725C 138400HNM FS 318 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT UPPER NOSE CHORD AT STA 318, LBL 13, WL 170. REPLACED CHORD IAW SRM 51-30-2. 2L73 4F A3WE 19950616001141995061600114NM 1995 6 16 UPS203510 119950612A5320 CHORD BOEING727 72725C 138400HNM FS 329 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT UPPER NOSE CHORD STA 329, RBL 13, WL 170. REPAIRED IAW EO 727-53-1617. 2L73 4F A3WE 19950616001151995061600115NM 1995 6 16 UPS203511 119950612A5754 GUIDE HOOKS BOEING727 72725C 138400HNM NR 5 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND WORN AND CRACKED NR 5 SLAT GUIDE HOOKS. INSTALLED FABRICATED PARTS IAW SRM 57-30-3, M/M 27-81-11. 2L73 4F A3WE 19950616001161995061600116NM 1995 6 16 UPS203512 119950612A5754 GUIDE HOOKS BOEING727 72725C 138400HNM NR 1 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01951UP 19850 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED AND WORN NR 1 SLAT I/B GUIDE HOOK. INSTALLED FABRICATED PARTS IAW SRM 57-50-3, 51-30-2, M/M 27-81-0. 2L73 4F A3WE 19950616001171995061600117NM 1995 6 16 UPS23508 119950607A2910 HYD FLUID BOEING727 72721C 138400MNM B HYD SYST LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01934UP 19135 BEGINNING OF DESCENT INTO SDF, AS THRUST LEVERS WERE BROUGHT TO IDLE THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYSTEM 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO 0. LOSS OF SYSTEM 'B' CHECKLIST WAS ACCOMP AND EMERGENCY DECLARED, UNEVENTFUL LANDING. STILL OPEN. 2L73 4F A3WE 19950616001181995061600118WP 1995 6 16 UPS803503 119950609A532037734792 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM END FITTING AT FS 120. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616001191995061600119WP 1995 6 16 UPS803504 119950609A53203755842502 FITTING DOUG DC8 DC873F 302199FWP FS 1230 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED BANANA FITTING ON AFT SIDE OF FS 1230, BETWEEN LONGS 33R AND 30R. REPLACED IAW SRM 51-4-20D. 2L74 4F RT4A25 19950616001201995061600120WP 1995 6 16 UPS803505 119950609A53203755222 FITTING DOUG DC8 DC873F 302199FWP FS 800 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM SPLICE FITTING AT FS 700, FS 720 AND FS 800, RBL 20. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616001211995061600121WP 1995 6 16 UPS803506 119950609A53203755222 FITTING DOUG DC8 DC873F 302199FWP FS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FLOORBEAM SPLICE FITTING AT FS 760, RBL 20. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616001221995061600122WP 1995 6 16 UPS803507 119950609A53209754003505 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FUSELAGE INNER DOUBLER AT RIVET HOLE. REPAIRED IAW DC8-53-1376. 2L74 4F RT4A25 19950616001231995061600123WP 1995 6 16 UPS803509 119950610A3350 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01797UP 45897 WHILE ON GROUND IN SDF, MAINTENANCE FOUND EMERGENCY BATTERY PACK LOW. REPLACED PACK, OPS CHECK GOOD ON GROUND. 2L74 4F RT4A25 19950616001321995061600132SO 1995 6 16 95ZZZX2885 119950518A2434902241 FAN PRESTOLITE ALU8421LS PIPER PA31 PA31350 7103110SO ALTERNATOR CRACKED A RMMAK NONE O OTHER ININSP/MAINT 1 CE01331MB833 317405455 ALTERNATOR FAN WAS SUSPECTED TO BE CRACKED DUE TO FACE PLATE RUBBING THE DRIVE BELT. ALTERNATOR WAS REMOVED AND FAN DISASSEMBLED. THERE WAS A CRACK FROM OUT OF THE DRIVE KEY HOLE, SPIRALING APPROXIMATELY ONE-HALF WAY AROUND THE FAN THEN GOING STRAIGHT TO A BLADE CUT OUT. A SECOND CRACK HAD STARTED TO FORM A 'Y'. THIS WAS ALSO GOING TOWARD A BLADE CUT OUT. HAD IT PROGRESSED, APPROXIMATELY ONE-THIRD OF THE FAN WOULD HAVE DEPARTED THE ASSEMBLY. 1L72 3O A20SO 19950616001541995061600154WP 1995 6 16 95ZZZZ250 119950523A216160714622 AMPLIFIER DOUG DC9 DC951 3022051WP RT PACK MALFUNCTIONED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05410EA 47731 STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE. REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR COALESCER, (P/N 179460-8-1). AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-12 - 1-11-95 - STL. REF 95ZZZZ251. 2L72 4F A6WE 19950616001551995061600155WP 1995 6 16 95ZZZZ251 119950523A217017946081 COALESCER DOUG DC9 DC951 3022051WP RT PACK DIRTY A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE05410EA 47731 STL - FLT 518 - DURING CLIMB A SMOKE ODOR APPEARED IN CABIN. TURNED RIGHT AIR CONDITIONING PACK TO FULL COLD, ODOR AND HAZE DISSIPATED, RETURNED TEMPERATURE CONTROL TO NORMAL RANGE. REPLACED TEMPERATURE CONTROL AMPLIFIER, (P/N 607146-2-2) AND WATER SEPARATOR COALESCER, (P/N 179460-8-1). AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-12 - 1-11-95 - STL. REF 95ZZZZ250. 2L72 4F A6WE 19950616001561995061600156NE 1995 6 16 AWXA9500241 219950427A7261 OIL TUBE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENGINE OUT OF POSITION A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28185AW 22652 708914 PHX-IAH - AIR TURNBACK DUE TO NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATING. AC RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MX FOUND MAIN OIL FILTER CONTAMINATED WITH MAGNETIC SHAVINGS AND CHIPS. REMOVED AND REPLACED NR 2 ENGINE. AC RETURNED TO SERVICE. FURTHER INFORMATION UPON ENGINE/GEARBOX TEARDOWN REPORT. TEARDOWN REVEALED OIL TUBE MISALIGNED CAUSING OIL PUMP FAILURE. (Z) 2L72 4F4 FRTA16WE E2EA 19950616001571995061600157EU 1995 6 16 AWXA9500286 119950512A2910 B-NUT AIRBUS320 A320231 3930325EU YELLOW HYD SYST LOOSE A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28627AW 66 CMH-LAS - FLT 255 - IN CRUISE, LOST YELLOW HYDRAULIC QUANTITY. AC RETURNED TO CMH WITHOUT FURTHER PROBLEMS. MX TIGHTENED B-NUT AT YELLOW SYSTEM VALVES, HYDRAULIC PRESS MANIFOLD. SYSTEM SERVICED AND LEAK CHECKS OK. AC RETURNED TO SERVICE. (Z) 2L72 4F RTA28NM 19950616001581995061600158NM 1995 6 16 AWXA9500292 119950512A5320 ANGLE BOEING757 7572G7 1384963NM FS 780 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DURING C-6 INSPECTION, FOUND MID CABIN FLOOR STABILIZER BEAM ANGLE FITTING CRACKED BETWEEN STA 780 AND 800. REMOVED, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-02. (Z) 2L72 4F RTA2NM 19950616001591995061600159NM 1995 6 16 AWXA9500293 119950512A5320 INTERCOSTAL BOEING757 7572G7 1384963NM BS 310 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DURING C-6 INSPECTION, FOUND INTERCOSTAL AT FWD LAV THRESHOLD CORRODED, BS 310 TO 325. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02. (Z) 2L72 4F RTA2NM 19950616001601995061600160NM 1995 6 16 AWXA9500294 119950512A5320 CHANNEL BOEING757 7572G7 1384963NM BS 400 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DURING C-6 INSPECTION, FOUND FLOOR HAT CHANNEL CORRODED, STA 400 RBL 24 TO TO RBL 45. REMOVED, FABRICATED AND INSTALLED NEW HAT CHANNEL PER SRM 51-40-02. (Z) 2L72 4F RTA2NM 19950616001611995061600161NM 1995 6 16 AWXA9500295 119950512A5320 SUPPORT BOEING757 7572G7 1384963NM FS 398 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DURING C-6 INSPECTION, FOUND SEAT TRACK SUPPORT ASSEMBLY UPPER CHORD CORRODED BEYOND LIMITS AT STA 398 RBL 24. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SUPPORT PER SRM 51-40-02. (Z) 2L72 4F RTA2NM 19950616001621995061600162NM 1995 6 16 AWXA9500296 119950512A5315 FLOORBEAM BOEING757 7572G7 1384963NM BS 377.7 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28910AW 24523 PHX - DURING C-6 INSPECTION, FOUND CORROSION OUT OF LIMITS ON FLOORBEAM AT BS 377.7 LBL 1, 2, 6, 10, 47 AND 51. REPAIRED PER ER 5 53 12 04 AND SRM 53 10 51. (Z) 2L72 4F RTA2NM 19950616001631995061600163NM 1995 6 16 AWXA9500301 119950520A2120S210N701S SENSOR BOEING737 73733A 1384673NM CABIN FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28173AW 23632 PHX-AUS - FLT 223 - DURING CRUISE FLIGHT, CREW REPORTED BOTH ELECTRONIC EQUIPMENT COOLING EXHAUST FANS FAILED, NORMAL AND ALTERNATE. AC RETURNED TO PHX WITHOUT INCIDENT. MX REPLACED EQUIPMENT COOLING EXHAUST LOW FLOW SENSOR. OPERATIONAL CHECK NORMAL. AC RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950616001641995061600164EU 1995 6 16 AWXA9500304 119950520A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28624AW 55 PHX - DURING ROUTINE MAINTENANCE CHECK, LT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAULTED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F RTA28NM 19950616001651995061600165EU 1995 6 16 AWXA9500308 119950522A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, LT AFT EMERGENCY BATTERY PACK FAILED TEST ON WEEKLY CHECK. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F RTA28NM 19950616001661995061600166NE 1995 6 16 AWXA9500310 219950522A75302760000101 SHUTOFF VALVE BOEING737 737275 1384485NM PWA JT8 JT8D9A 52048NE NR 2 ENGINE SHORTED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP282FOR 20958 PHX-DFW - FLT 544 - DURING CRUISE, THE NR 2 BLEED VALVE CIRCUIT BREAKERS POPPED AND WOULD NOT RESET. PILOT ELECTED TO RETURN TO PHX DUE TO KNOWN ICING CONDITIONS. AC LANDED WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED NR 2 ENGINE BLEED AIR SHUTOFF VALVE PER MM 36 11 11 PG 401. OPS CHECK GOOD, AC RETURNED TO SERVICE. (Z) 2L72 4F4 F A16WE E2EA 19950616001671995061600167NM 1995 6 16 AWXA9500311 119950522A5270 DOOR WARNING BOEING737 7373G7 1384595NM CARGO DOOR ACTIVATED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28150AW 23218 IND-PHX - FLT 656 - DURING CLIMB AT 4,000 FEET, THE AFT CARGO DOOR OPEN LIGHT ILLUMINATED. AC EXPERIENCED NO PRESSURIZATION PROBLEMS AND RETURNED TO IND, LANDING WITHOUT INCIDENT. NO OVERWEIGHT LANDING REQUIRED. CONTRACT MX UNABLE TO DUPLICATE PROBLEM, INSPECTION REVEALED NO DEFECTS. MX CONTROL ISSUED UNMANNED STATION RELEASE. PHX MX FOUND NOTHING WRONG WITH DOOR OR POSITION SENSING. DOOR OPERATED MANY TIMES ON INSIDE AND OUT WITHOUT PROBLEMS. BAG FOUND IN WAY WHEN DOOR WAS FIRST OPENED. CLEARED MEL 52-03 CONTROL NR 18637. AC RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950616001681995061600168NM 1995 6 16 AWXA9500312 119950522A3244 TIRE TREAD BOEING737 7372A6 138448BNM RT NLG SEPARATED A AAWXAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP28145AW 20194 PHX-ABQ - ON TAKEOFF, THE NR 2 NOSE TIRE CAP SEPARATED FROM THE CARCASS. PARTS OF TIRE CAP WERE INGESTED BY NR 2 ENGINE. CREW SHUTDOWN NR 2 ENGINE AND RETURNED TO ABQ WITHOUT FURTHER PROBLEMS. NO OVERWEIGHT LANDING REQUIRED. MX FOUND DAMAGE TO C1 AND C2 COMPRESSOR BLADES, AND FIRST STAGE STATORS. MX REMOVED AND REPLACED NR 2 NOSE TIRE PER AWM363 AND THE NR 2 ENGINE PER AWA TASK CARD R5M71003. STATIC RIG PERFORMED PER CARD F5M76001. TAIL PIPE TRANSFERRED PER CARD R5M78002. ENGINE TRIMMED PER CARD F5M71002. AC RETURNED TO SERVICE. (Z) 2L72 4F A16WE 19950616001691995061600169NM 1995 6 16 AWXA9500320 119950520A53206546921168 DOOR FRAME BOEING737 73733A 1384673NM CARGO COMPT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - DURING SCHEDULED C-12 INSPECTION, FOUND CRACK IN FWD CARGO DOOR FRAME, FWD LOWER CORNER. REMOVED AND REPLACED CORNER FRAME IAW SRM 51-40-02. (Z) 2L72 4F RTA16WE 19950616001701995061600170NM 1995 6 16 AWXA9500321 119950520A53156035017075T6 FLOORBEAM BOEING737 73733A 1384673NM FS 294.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28173AW 23632 PHX - DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION AT 2 FASTENER HOLES ON BOTTOM SIDE OF TOP CAP, STA 294.5. REMOVED AND REPLACED TOP CAP PER SRM 51-40-02. (Z) 2L72 4F RTA16WE 19950616001711995061600171WP 1995 6 16 ORJA9538 119950524A335041B004AD073 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11823RA 49889 EMERGENCY LIGHTS, CEILING FROM ROWS 6 TO 9 INOP. REPLACED EMERGENCY BATTERY PACK OPS CHECK GOOD. (Z) 2L72 4F A6WE 19950616001721995061600172WP 1995 6 16 ORJA9539 119950524A335041B004AD073 EEL BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11823RA 49889 EMERGENCY LIGHTS CEILING, INOP FROM ROWS 18 TO 21. REPLACED EMERGENCY BATTERY PACK OPS CHECK GOOD. (Z) 2L72 4F A6WE 19950616001731995061600173EU 1995 6 16 RAIA950515 119950519A77148DJ8WDJ4 RPM GAUGE BAG JETSTMJETSTM3201 1500217EU LT COCKPIT FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03973JX 973 FAT - FLT 4750 - THE LT ENGINE RPM INDICATION FELL FROM 100 PERCENT TO 98 PERCENT, WOULD NOT RESET OVER 98.5 PERCENT RPM. MAINTENANCE REPLACED LT RPM GAUGE GROUND RUNS REVEALED NORMAL OPERATION. ALL ENGINE PARAMETERS NORMAL. (Z) 2L72 4T RTA56EU 19950616001741995061600174EU 1995 6 16 RAIA950516 119950520A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT/RT ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03342TE 954 STL - FLT 7050 - LT AND RT ENGINES DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED LT AND RT ENGINE TORQUE SIGNAL CONDITIONERS PER DSC SETTING. GROUND RUNS REVEALED NORMAL OPERATION AND ALL ENGINE PARAMETERS NORMAL. (Z) 2L72 4T RTA56EU 19950616001751995061600175EU 1995 6 16 RAIA950517 119950523A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03430AM 880 STL - FLT 7420 - THE LT COULD NOT MAKE TARGET TORQUE. MAINTENANCE CALIBRATED LT TORQUE SIGNAL CONDITIONER AND ADJUSTED LT EGT TO GARRETT DSC SETTINGS. GROUND RUNS REVEALED NORMAL OPERATION. (Z) 2L72 4T RTA56EU 19950616001761995061600176EU 1995 6 16 RAIA950518 119950523A3610 BLEED AIR SYST AEROSPATR42 ATR42300 8680920EU CABIN MALFUNCTIONED A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03424TE 124 STL - FLT 7176 - AIRFRAME/AIRBLEED FAULTED WOULD NOT RESET. MAINTENANCE INSPECTED SYSTEM AND PERFORMED GROUND RUNS. NO FAULTS WERE NOTED. COULD NOT DUPLICATE PROBLEM. SYSTEM CHECK NORMAL. (Z) 2H72 4T RTA53EU 19950616001771995061600177EU 1995 6 16 RAIA950519 119950522A3350OL60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN MISSING A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03424TE 124 STL - FLOOR EMERGENCY LIGHT MISSING AT SEAT 11B. MAINTENANCE INSTALLED EMERGENCY LIGHT BULB AT SEAT 11B. (Z) 2H72 4T RTA53EU 19950616001781995061600178EU 1995 6 16 RAIA950520 119950522A3350OL60424P EEL BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE 283 STL - EMERGENCY EXIT LIGHT INOP ON FLOOR. MAINTENANCE REPLACED LIGHT BULB. (Z) 2H72 4T RTA53EU 19950616001791995061600179WP 1995 6 16 RAIA950521 219950526A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LEFT FAILED A RAIAE ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 CE03871AE 871 66069 FAT - FLT 4732 - THE LT ENGINE LOW PRESSURE, HIGH OIL TEMP, CEW SHUTDOWN ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE. ALL ENGINE RUNS REVEALED NORMAL OPERATION. (Z) 2L72 4T4 TRTA56EU E4WE 19950616001801995061600180EU 1995 6 16 RAIA950522 119950527A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03424TE 124 STL - EMERGENCY LIGHTS ARE NOT ILLUMINATING. MAINTENANCE REPLACED FWD AND AFT EMERGENCY LIGHTING BATTERIES. (Z) 2H72 4T RTA53EU 19950616001811995061600181SO 1995 6 16 RAIA950524 119950529A3350D36604001 EEL BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A RAIAOK OTHER NONE OL OTHER NO TEST ININSP/MAINT 1 CE03126AM 120102 STL - AFT EMERGENCY FLOOR LIGHTING IS INOPERATIVE. MAINTENANCE REPLACED AFT EMERGENCY LIGHTING BATTERY. (Z) 2L72 4T RTA31SO 19950616001821995061600182EU 1995 6 16 RAIA950525 119950529A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 199 STL - BOTH FWD EMERGENCY EXIT SIGNS ARE INOP. MAINTENANCE REPLACED FWD LOWER EMERGENCY LIGHTING BATTERY. (Z) 2H72 4T RTA53EU 19950616001831995061600183EU 1995 6 16 RAIA950526 119950529A5311S53672406200 FRAME AEROSPATR42 ATR42300 8680920EU FS 17734 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE032FOR 199 STL - MAINTENANCE DISCOVERED CORROSION ON RT FRAME 36 BTW STRINGER 14 AND 16. MAINTENANCE REPAIRED FRAME 36 CORRODED AREA AS PER TRANS STATES AIRLINES DER APPROVAL 8110-3 AND ATR DWG 16S536R0052. (Z) 2H72 4T RTA53EU 19950616001841995061600184EU 1995 6 16 RAIA950527 119950529A5311S53672406200 FRAME AEROSPATR42 ATR42300 8680920EU FS 17734 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE032FOR 199 STL - MAINTENANCE DISCOVERED CORROSION ON RT FRAME 37 BTW STRINGER 14 AND 16. MAINTENANCE REPAIRED FRAME 37 CORRODED AREA AS PER TRANS STATES AIRLINES DER APPROVAL 8110-3 AND ATR DWG 16S536R0052. (Z) 2H72 4T RTA53EU 19950616001851995061600185NE 1995 6 16 SLIA951 219950425A8510222490 PINION GEAR CVAC 440 440 2422902WP PWA R2800 CB16 52026NE NR 2 ENGINE FAILED A SLIAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NM01356SA 432 P33557 BMEP DROPPED TO ZERO, OIL QUANTITY DECLINING. ENGINE SHUTDOWN/FEATHERED. INVESTIGATION REVEALED AND INTERNAL FAILURE OF THE ENGINE NOSE CASE, (REDUCTION GEARING) WHICH RESULTED IN FAILURE OF SCAVENGE PUMP, AND BMEP PUMP. (M) 2L72 4R4 R 6A6 E264 19950616001861995061600186EU 1995 6 16 UF6A950504 119950519A61207863364 PCU BAG ATP ATP EU LT ENGINE FAILED A UF6AK NONE O OTHER ININSP/MAINT 1 CE03857AW 2034 ORD - FLT 5030 - THE LT PROPELLER DID NOT FULLY FEATHER ON SHUTDOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK, OPS CHECK GOOD. (Z) 2L72 4T RTA27NM 19950616001871995061600187EU 1995 6 16 UF6A950505 119950521A2932APTE3610004000S6PRESS TRANS BAG ATP ATP EU NR 2 HYD SYST FAILED A UF6AD RETURN TO BLOCK JK WARNING INDICATION FLUID LOSS CLCLIMB 1 CE03852AW 2021 GRB - FLT 5062 - THE NR TWO HYDRAULIC PUMP PRESSURE DROPPED TO 0 PSI. MAINTENANCE REPLACED THE NR TWO PRESSURE TRANSMITTER. (Z) 2L72 4T RTA27NM 19950616001881995061600188EU 1995 6 16 UF6A950506 119950522A33506013211 EEL PWR SUPPLY BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03859AW 2036 ORD - DAILY INSPECTION, THE NR 3 EMERGENCY LIGHT POWER SUPPLY INOP. MAINTENANCE REPLACED THE NR 3 POWER SUPPLY. (Z) 2L72 4T RTA27NM 19950616001891995061600189EU 1995 6 16 UF6A950507 119950523A33506013211 EEL PWR SUPPLY BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 CE03851AW 2020 CWA - FLT 5026 - EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED THE NR 7 POWER SUPPLY. (Z) 2L72 4T RTA27NM 19950616001901995061600190EU 1995 6 16 UF6A950508 119950530A61207863361 PCU BAG ATP ATP EU LT ENGINE FAILED A UF6AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CE03853AW 2022 ORD - FLT 5089 - THE LT ENGINE WOULD NOT AUTOFEATHER TEST. MAINTENANCE REPLACED THE LT PROPELLER CONTROL UNIT. (Z) 2L72 4T RTA27NM 19950616001911995061600191NM 1995 6 16 95ZZZW785 119950515A57546546422268 SKIN BOEING737 7372P6 NM NR 3 SLAT CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO152FOR BN186 21355 DURING WALKAROUND INSPECTION A CRACK WAS NOTED ON THE RIGHT WING NR 3 SLAT. THE CRACK WAS LOCATED ON THE UPPER SURFACE OUTBOARD TRAILING EDGE CORNER. THE CRACK WAS 6 INCHES IN LENGTH IN ADDITION, THE SLAT UPPER SKIN WAS DELAMINATED APPROXIMATELY 10 PERCENT. REPLACED DAMAGED SLAT WITH SERVICEABLE UNIT. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F RTA16WE 19950616001921995061600192WP 1995 6 16 95ZZZW786 119950501A32607000010101 LIMIT SWITCH DOUG DC9 DC932 3022066WP LT MLG FAILED A VJ6AA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11919VV 47260 FLT 558 - ATL-BNA - RETURNED TO ATL DUE TO A LEFT MAIN GEAR GREEN LIGHT ON. DURING APPROACH TO ATL NO NOSE DOWN LOCK INDICATION. REMOVED AND REPLACED LEFT GEAR DOWN LIMIT SWITCH AND LIGHT BULBS FOR NOSE GEAR DOWN LOCK LIGHT. (W) 2L72 4F A6WE 19950616001931995061600193SW 1995 6 16 95ZZZW787 119950509A32302752000192 UPLOCK BUSHINGS SWRNGNSA227 SA227AC 8780603SW NLG CORRODED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1526906 AC654B FLT 3254 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE AIRCRAFT CONTINUED TO BRD. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK BUSHINGS. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950616001941995061600194SW 1995 6 16 95ZZZW788 119950517A54142735001180 SKIN SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING PHASE INSPECTION IN MSP, FOUND SMALL CRACK IN RT INBOARD NACELLE FORMER P/N 27-35025-968. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER, P/N 27-35025-968 AND SKIN PANEL, P/N 27-35001-180, IAW FAC SRM 51-00-00 PAGE 4, 51-40-00, 51-30-00 AND 54-90-10. (W) 1L72 4T A8SW 19950616001951995061600195SW 1995 6 16 MALA954445 119950504A3250 STEERING SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A MALAD RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL15158MC AC762B FLT 3018 - DURING THE TAKEOFF ROLL IN DTW, THE NOSE STEER FAIL LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. THE SYSTEM WAS DEFERRED PER MEL 32-1-C. (W) 1L72 4T A8SW 19950616001961995061600196SW 1995 6 16 MALA954446 119950504A5320 DOOR SILL SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAO OTHER O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, THE CARGO DOOR SILL AT FS 438 WAS FOUND CRACKED AT RADIUS OF THE CUT OUT FOR THE FUSELAGE FRAME. REPAIRS WERE COMPLETED BY REPLACING THE CARGO DOOR SILL CUT OUT, P/N 27-22081, IAW FAC ARP 53-30-5507. (W) 1L72 4T A8SW 19950616001971995061600197SW 1995 6 16 MALA954447 119950508A2431 WIRES SWRNGNSA227 SA227AC 8780603SW BATTERY LIGHT BROKEN A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL1526906 AC654B FLT 3496 - ON APPROACH TO STC, THE LEFT BATTERY AMBER CAUTION LIGHT ILLUMINATED. THE CREW DISCONNECTED THE LEFT BATTERY AND THE BATTERY TEMPERATURE ROSE. THE RED HOT LIGHT ILLUMINATED MOMENTARILY AND THEN THE TEMPERATURE DECREASED UNTIL ALL CAUTION LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN STC WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED WIRES AT THE LEFT TEMP PROBE CANNON PLUG. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950616001981995061600198 1995 6 16 MALA954448 419950509A3442071131900 TRANSCEIVER DHAV DHC8 DHC8102 2809003NM RADAR FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15832MA 341 FLT 3319 - IN CRUISE FLIGHT TO CMI, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616001991995061600199SW 1995 6 16 MALA954449 119950509A7931APTE10002006 TRANSDUCER SWRNGNSA227 SA227AC 8780603SW LT ENG OIL PRESSFAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1527465 AC755B FLT 3218 - ON CLIMB-OUT FROM MSP, THE LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT OIL PRESSURE TRANSDUCER. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950616002001995061600200SW 1995 6 16 MALA954450 119950509A32302752000191 UPLOCK BUSHINGS SWRNGNSA227 SA227AC 8780603SW NLG CORRODED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL1526906 AC654B FLT 3254 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR WOULD NOT REMAIN UP AND LOCKED AFTER GEAR RETRACTION. THE AIRCRAFT CONTINUED TO BRD. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK BUSHINGS. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950616002011995061600201NE 1995 6 16 MALA954451 219950509A73207863916L27 HMU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15833MA 343 FLT 3165 - DURING TAKEOFF FROM DTW, THE NR 2 ENGINE TORQUE SURGED FROM 89 PERCENT TO 105 PERCENT. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 2 HMU. THE SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (W) 2H72 4T4 TRTA13NM E20NE 19950616002021995061600202NM 1995 6 16 MALA954452 119950512A521085210003001 SKIN DHAV DHC8 DHC8102 2809003NM PAX DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15817MA 249 DURING THE C-CHECK INSPECTION IN CKB, THE PASSENGER DOOR EXTERIOR SKIN WAS DENTED. REPAIRS WERE COMPLETED BY REPLACING THE EXTERIOR SKIN PANEL. (W) 2H72 4T RTA13NM 19950616002031995061600203SW 1995 6 16 MALA954453 119950514A57202731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW WS 27 WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15421MA AC634 DURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT FLAP WALKING BEAM ROLLER DOUBLER, LOCATED AT WS 27.0 WAS FOUND TO BE WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER, P/N 27-31141, IAW FAC SRM 57-90-10 PAGES 45 AND 46, AND FAC ARP 57-20-9424. (W) 1L72 4T A8SW 19950616002041995061600204NM 1995 6 16 MALA954454 119950513A3260 INDICATOR BULB DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15865MA 364 FLT NR 3370 - ON APPROACH TO DTW, THE RIGHT MAIN GEAR DID NOT SHOW A GREEN DOWN AND LOCKED INDICATION AFTER GEAR EXTENSION. THE LIGHT WOULD ALSO NOT TEST. THE CREW PERFORMED APPROPRIATE PROCEDURES AND LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE LANDING GEAR POSITION INDICATING BULB. ALL SYSTEMS OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616002051995061600205SW 1995 6 16 MALA954455 119950515A32302752004045 HOOK ASSY SWRNGNSA227 SA227AC 8780603SW NLG STICKING A MALAK NONE O OTHER CLCLIMB 1 GL15428MA AC646 FLT 3298 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR CONTINUED TO CYCLE IN THE GEARWELL AFTER IT WAS RETRACTED. THE CREW RECYCLED THE GEAR UNTIL THE GEAR REMAINED UP AND LOCKED. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED THE UPLOCK HOOK ASSY, P/N 27-52004-045, ACTUATOR ARMS, P/N 27-52000-191, AND BUSHINGS, P/N 6JB373110B. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950616002061995061600206NM 1995 6 16 MALA954456 119950515A5280 SEAL DHAV DHC8 DHC8102 2809003NM RT MLG DOOR OUT OF POSITION A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15824MA 327 DURING A PREFLIGHT WALKAROUND, THE CREW NOTED THAT THE RIGHT GEAR DOORS, CENTER AND AFT, RELEASE INTERMITTENTLY. MAINTENANCE REPOSITIONED THE AFT DOOR SEAL AND RETAINER. ALL CHECKS SATISFACTORY. (W) 2H72 4T RTA13NM 19950616002071995061600207NM 1995 6 16 MALA954457 119950515A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15848MA 346 DURING SCHEDULED MAINTENANCE IN DTW, TWO FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED AN EMERGENCY LIGHT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616002081995061600208SW 1995 6 16 MALA954462 119950517A54002735025968 FORMER SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING PHASE INSPECTION IN MSP, FOUND SMALL CRACK IN RT INBOARD NACELLE FORMER P/N 27-35025-968. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER, P/N 27-35025-968 AND SKIN PANEL, P/N 27-35001-180, IAW FAC SRM 51-00-00 PAGE 4, 51-40-00, 51-30-00 AND 54-90-10. (W) 1L72 4T A8SW 19950616002091995061600209SW 1995 6 16 MALA954463 119950517A5400 FORMER SWRNGNSA227 SA227AC 8780603SW NAC STA 120 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING A PHASE INSPECTION IN MSP, FOUND A CRACK IN LEFT INBOARD NACELLE FORMER AT NS 120.00. THE REPAIRS WERE COMPLETED BY REPLACING THE FORMER P/N 27-35025-967 AND A SKIN PANEL, P/N 27-35001-178. ALL WORK WAS PERFORMED IAW FAC SRM 51-00-00 PAGE 4, 51-30-00, 51-40-00, AND FAC LAR 95-MALA-144. (W) 1L72 4T A8SW 19950616002101995061600210SW 1995 6 16 MALA954464 119950517A53112722104048 FRAME SWRNGNSA227 SA227AC 8780603SW FS 212.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING BLOCK INSPECTION AT MSP, FOUND CRACK IN BELT FRAME RELIEF RADIUS AT FS 212.27 DUE TO A CRACK. REPAIRS WERE COMPLETED USING A DOUBLER AND STIFFENER IAW FAC SRM 53-90-20 REPAIR NR 20. (W) 1L72 4T A8SW 19950616002111995061600211SW 1995 6 16 MALA954468 119950518A215020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW LT FAILED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15438MA AC721B FLT 3222 - DURING TAXI AT LNK, THE AIRCRAFT FILLED WITH SMOKE EMANATING FROM THE LEFT BLEED SOURCE. THE LEFT AIR CONDITIONING SYSTEM WAS DEFERRED AND THE AIRCRAFT PROCEEDED TO MSP. MAINTENANCE REPLACED THE LEFT COOLING TURBINE AND MASTER VALVE. THE SYSTEM PERFORMED SATISFACTORILY. (W) 1L72 4T A8SW 19950616002121995061600212WP 1995 6 16 95ZZZX2908 119950512A28423912791501 FLOAT VALVES DOUG DC9 DC932 3022066WP LT WING TANK DEFECTIVE A VJ6ACD ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TOTAKEOFF 1 SO11919VV 47260 ATL/BDL - FLT 450 - AIRCRAFT RETURNED TO GATE DUE TO THE LOSS OF FUEL OUT OF THE RIGHT WING TIP VENT. REPLACED BOTH FLOAT VALVES IN LEFT WING AND REPLACED FORWARD AND AFT FUEL PUMP VOLUTES. 2L72 4F A6WE 19950616002131995061600213WP 1995 6 16 95ZZZX2909 119950512A28226550942 PUMP VOLUTE DOUG DC9 DC932 3022066WP LT WING TANK DEFECTIVE A VJ6ACD ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TOTAKEOFF 1 SO11919VV 47260 ATL/BDL - FLT 450 - AIRCRAFT RETURNED TO GATE DUE TO THE LOSS OF FUEL OUT OF THE RIGHT WING TIP VENT. REPLACED BOTH FLOAT VALVES IN LEFT WING AND REPLACED FORWARD AND AFT FUEL PUMP VOLUTES. 2L72 4F A6WE 19950616002141995061600214WP 1995 6 16 95ZZZX2910 119950508A2820 CROSSFEED DOUG DC9 DC932 3022066WP FUEL SYSTEM MALFUNCTION A VJ6AO OTHER K FLUID LOSS CLCLIMB 1 SO11919VV 47260 PBI\IAD - FLT 466 - CREW EXPERIENCED AN 800 POUND FUEL IMBALANCE FROM RIGHT WING TO LEFT. AIRCRAFT LANDED IN IAD WITHOUT INCIDENT. IAD MAINTENANCE FILLED AIRCRAFT FULL OF FUEL AND RAN ALL PUMPS. NEXT, TAXIED AIRCRAFT USING BRAKES AND THROTTLE ABRUPTLY, NO LOSS OF FUEL. COULD NOT DUPLICATE. 2L72 4F A6WE 19950616002151995061600215WP 1995 6 16 95ZZZX2911 119950511A3260 SWITCH WIRE DOUG DC8 DC873F 302199FWP LT MLG DOOR BROKEN A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15792FT 46046 KDAY/KATL - FLT 038 - DURING UPLATCH CHECK, FORWARD MLG DOOR WARNING CAME ON. RECYCLED GEAR AND FORWARD LIGHT REMAINED ON. THE AFT DOOR WARNING WAS EXTINGUISHED. MAINTENANCE REPAIRED WIRING TO THE LT MLG DOOR PROXIMITY SWITCH. OPERATIONAL CHECK OF THE MLG RETRACTION AND WARNING SYSTEMS WAS GOOD. (X) 2L74 4F RT4A25 19950616002161995061600216NE 1995 6 16 95ZZZX2912 219950506A7230 COMPRESSOR BOEING707 707369C 1383661NM PWA JT3D JT3D3B 52039NE NR 2 ENGINE STALLED A MIRACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 SO19851JB 20084 667946 OXO - FLT 405 - KMIA/KMIA - REJECTED TAKEOFF NR 2 ENGINE STALLED ONCE. INSPECTED ENGINE NR 2, BLEED VALVE FOR OPERATION, LUBRICATED, FOUND GOOD, REMOVED OIL FILTER (MAIN) FOUND CLEAN, NO METAL CHIPS, NOT DIRTY. DRAINED FUEL TRAP OF FUEL CONTROL UNIT. REINSTALLED OIL FILTER, REFILLED OIL (5 QUARTS), CHECKED ENGINE RUN-UP, PARAMETERS NORMAL. AROUND ENGINE, NO OIL LEAKS. NO OTHER DISCREPANCY OBSERVED. REFERENCE MM CHAPTER 71-5-0. (X) 2L74 4F4 F 4A26 1E8 19950616002171995061600217NE 1995 6 16 95ZZZX2913 219950511A7532563881 BLEED VALVE BOEING707 707369C 1383661NM PWA JT3D JT3D3B 52039NE NR 2 ENGINE MALFUNCTIONED A AMIRACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 SO19851JB 20084 667946 OXO - FLT 505 - KMIA/KMIA - ABORTED TAKEOFF DUE TO COMPRESSOR STALL ON ENGINE NR 2. CHECKED FOR CONDITION, NO DAMAGE FOUND, SURGE BLEED VALVE LUBRICATED. PERFORMED HIGH POWER RUN-UP ENGINES. ALL PARAMETER OKAY PER BMM 71-5-0. REMOVED AND REPLACED SURGE BLEED VALVE. OPERATIONS CHECKED AND RUN-UP ENGINE OKAY. ALL PARAMETERS OKAY PER BMM 71-5-0. (X) 2L74 4F4 F 4A26 1E8 19950616002381995061600238NM 1995 6 16 AALA950020H 119950511A5347143T5211 SEAT TRACK BOEING767 767323 1385205NM FS 772 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07377AN11647 25446 AFW - FOUND AND BLENDED OUT CORROSION ON UPPER SURFACE OF SEAT TRACK AT RBL 11.0, STA 772. BLEND BEYOND SRM LIMITS. REPAIRED PER MRB 767-909 DATED 4-23-95. CYCLES, 1808. (X) 2L72 4F RTA1NM 19950616002391995061600239WP 1995 6 16 AALA950840 119950507A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN MISINSTALLED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07298AA 49310 DFW - DURING OVERNIGHT CHECK, FOUND LEFT AFT ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REVERSED WIRES BY SEAT 24. SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F A6WE 19950616002401995061600240EU 1995 6 16 SIMA951455 119950525A2150776910 ACM SAAB SF340 340B 7860101EU LEFT FAILED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21314AE9203 340B314 DFW - FLT 3944 - AFTER TAKEOFF, CREW REPORTED THEY COULD NOT CONTROL COCKPIT AIR TEMP WHICH WAS BLOWING FULL HOT. REMOVED AND REPLACED LEFT ACM. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19950616002411995061600241WP 1995 6 16 WRLA95030 119950521A492036005792 COMPRESSOR SEAL DOUG DC10 DC1030 3023501WP APU RUPTURED A WRLAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA273024W 48318 JED - DURING TAXI, FLIGHT CREW SMELLED A BAD ODOR AND SAW SMOKE FILLING THE AIRCRAFT. CAPTAIN ELECTED TO RETURN TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL OPENED AIR CONDITIONING PACKS AND OBSERVED TURBINE OIL ON COALESCER BAGS. SUSPECT SEAL RUPTURE IN APU. APU INOP'D AND ENTERED ON DMI LOG. ENGINES RUN TO VENT OIL SMELL/SMOKE FROM AIRCRAFT AND AIR QUALITY DETERMINED NORMAL. AIRCRAFT RETURNED TO SERVICE. QUALITY CONTROL WILL SUPPLY FURTHER INFORMATION UPON RECEIPT OF TEAR-DOWN INFORMATION. (X) 2L73 4F A22WE 19950616002421995061600242WP 1995 6 16 9509209915 119950528A5744 FITTING DOUG DC9 DC931 3022065WP NR 2 FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING NR 2 FLAP FORWARD HINGE BEARING BORE. REPLACED FITTING PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950616002431995061600243WP 1995 6 16 9509219919 119950530A5230 BEAM DOUG DC9 DC932 3022066WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01941N 47450 DURING PERIODIC CHECK, FOUND A .375 INCH CRACK IN THE FORWARD CARGO DOOR LOWER BEAM FORWARD END. REPAIRED BEAM (P/N 5910141-63) PER EA 99-98388. 2L72 4F A6WE 19950616002441995061600244WP 1995 6 16 9509229996 119950601A5330 SKIN DOUG DC9 DC931 3022065WP FS 332 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018932E 47141 DURING LINE CHECK, FOUND CORROSION AND SHEARED FASTENERS IN THE FUSELAGE SKIN FS 332 AT LONGERON 29L TO 30. REPAIRED PER EA 99-98462. 2L72 4F A6WE 19950616002451995061600245EU 1995 6 16 9509233240 119950603A5347 SEAT TRACK AIRBUS320 A320211 3930320EU FS 8077-9500 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01340NW 372 DURING C-CHECK, FOUND CORROSION IN THE SEAT TRACKS FR 20 TO 24 AT Y=-765 AND -1292. REPAIRED TRACK PER EA 32-098322. 2L72 4F RTA28NM 19950616002461995061600246WP 1995 6 16 9509249976 119950605A5320 FITTING DOUG DC9 DC931 3022065WP CARGO DR CUTOUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR JAMB INTERCOSTAL END FITTINGS AFT OF THE FORWARD DOOR HINGE AND FORWARD OF THE AFT DOOR HINGE. REPLACED FITTINGS PER SRM 51-30. 2L72 4F A6WE 19950616002471995061600247NM 1995 6 16 9509256729 119950606A5344 DOOR HINGE BOEING747 747251F 1384898NM AFT CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01629US 22388 DURING PERIODIC CHECK, FOUND CORROSION IN THE AFT 3 SEGMENTS OF THE AFT CARGO DOOR HINGE. REPLACED AFT 3 SEGMENTS PER OHM 52-34-11 FIG 601 SEC B. 2L74 4F A20WE 19950616002481995061600248WP 1995 6 16 9509269915 119950607A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01965N 47417 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19950616002491995061600249NE 1995 6 16 9509272285 219950609A7310 MOISTURE TRAP BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE CONTAMINATED A NWAAAJ UNSCHED LANDING DUMP FUEL R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01285US 21324 696473 ON CLIMBOUT FROM PHX, THE NR 2 ENGINE WOULD NOT RESPOND PROPERLY TO CHANGES IN THRUST LEVER SETTING. THE CREW JETTISONED 24,000 LBS OF FUEL AND RETURNED TO PHX LANDING WITHOUT INCIDENT. MAINTENANCE FOUND AND REMOVED CONTAMINANTS IN THE FCU MOISTURE TRAP. ENGINE PERFORMANCE RETURNED TO NORMAL ON RUNUP, AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950616002501995061600250NM 1995 6 16 9509282709 119950608A5313 LONGERON BOEING727 727225 1384077NM FS 950-985 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING H-CHECK, FOUND CORROSION AND CRACKS ON STR 29R FROM BS 950E TO 985. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98461. 2L73 4F A3WE 19950616002511995061600251NM 1995 6 16 9509292709 119950608A5313 LONGERON BOEING727 727225 1384077NM FS 950-1000 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING H-CHECK, FOUND CORROSION ON STR 29L FROM FS 950B TO 1000. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98455. 2L73 4F A3WE 19950616002521995061600252NM 1995 6 16 9509302709 119950608A5320 CHORD BOEING727 727225 1384077NM FS 336 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WELL LEFT SIDE PANEL CHORD FS 336. REPAIRED CHORD (P/N 65-19861-7) PER EA 27-98463. 2L73 4F A3WE 19950616002531995061600253NM 1995 6 16 9509316631 119950609A3244 TIRE BOEING747 747251B 1384892NM NR 8 MLG FLAT A NWAAA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL01631US 23111 AFTER FLIGHT 17 TAKEOFF AT JFK, OPERATIONS AT JFK ADVISED DISPATCH THAT TIRE PIECES WERE FOUND ON THE RUNWAY. FLIGHT DIVERTED TO ANC. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE NR 8 TIRE RECAP MISSING AND FLAT. REPLACED THE NR 7 AND NR 8 MAIN TIRE AND WHEEL ASSEMBLIES. PERFORMED CHECK AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19950616002541995061600254WP 1995 6 16 9509329976 119950609A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED BOTH SETS OF CLIPS AND RERIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950616002551995061600255WP 1995 6 16 ABX9500531 119950609A561046536092 SPRING DOUG DC8 DC862 3021970WP RT CV WINDOW DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23801AX 46077 DURING MAINTENANCE INSPECTION, FOUND THAT FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT UNLOCK. ADJUSTED FORWARD UPPER STOP TO CENTER WINDOW WHICH CORRECTED UPPER LATCH ENGAGEMENT IAW DC-8 MM CHAPTER 56-10-3, AT ILN AS PRECAUTIONARY. MAINTENANCE INSTALLED NEW SPRING IN FIRST OFFICER'S CLEARVIEW WINDOW HOLD OPEN LATCH MECHANISM. 2L74 4F 4A25 19950616002561995061600256WP 1995 6 16 ABXA9500532 119950612A3231510361C LINK DOUG 56496991 DOUG DC8 DC863 302198AWP NLG DOOR DEFECTIVE A ABXAO OTHER E VIBRATION/BUFFET TOTAKEOFF 1 GL23818AX 46075 AFTER TAKEOFF FROM SMF, GEAR UPLATCH CHECK OK. AIRCRAFT HAD A VIBRATION WHICH SEEMED TO COME FROM THE NOSE. THE VIBRATION PROGRESSIVELY GOT WORSE, CYCLED GEAR SEVERAL TIMES AND LOUD POP WAS HEARD. VIBRATION AND NOISE WENT AWAY, DID FLY BY AT SMF AND GROUND REPORTED ALL GEAR DOORS IN PLACE. REPLACED LEFT FORWARD NOSE LANDING GEAR DOOR LINK. RIGGED AND OPS CHECKED GOOD IAW DC-8 MM 32-22-1. 2L74 4F 4A25 19950616002571995061600257WP 1995 6 16 ABXA9500533 119950612A32313700614 STOP DOUG 56496991 DOUG DC8 DC863 302198AWP NLG DOOR DEFECTIVE A ABXAO OTHER E VIBRATION/BUFFET TOTAKEOFF 1 GL23818AX 56075 AFTER TAKEOFF FROM SMF, GEAR UPLATCH CHECK OK. AIRCRAFT HAD A VIBRATION WHICH SEEMED TO COME FROM THE NOSE. THE VIBRATION PROGRESSIVELY GOT WORSE, CYCLED GEAR SEVERAL TIMES AND LOUD POP WAS HEARD. VIBRATION AND NOISE WENT AWAY. DID FLY BY AT SMF AND GROUND REPORTED ALL GEAR DOORS IN PLACE. REPLACED LEFT AFT STOP LINK. RIGGED AND OPS CHECKED GOOD IAW DC-8 MM 32-22-1. 2L74 4F 4A25 19950616002581995061600258SO 1995 6 16 COM11916 119950606A7931APT79100080D TRANSDUCER EMB 120 EMB120RT SO RT ENGINE DEFECTIVE A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01263CA 120255 RT ENGINE OIL PRESSURE INDICATES TOO HIGH. REPLACED OIL PRESSURE TRANSDUCER. 2L72 4T RTA31SO 19950616002591995061600259NE 1995 6 16 COM11917 219950612A73207863904 HMU EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE LEAKING A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO01259CA1172519 120252 RT ENGINE IS LEAKING FUEL. REPLACED THE ENGINE HMU. 2L72 4T4 TRTA31SO E20NE 19950616002601995061600260EU 1995 6 16 COM31103 119950612A2730DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100EU ELEVATOR DEFECTIVE A COMAK NONE F FLT CONT AFFECTED LDLANDING 1 SO01361CA17416818 340A056 STANDBY PITCH TRIM IS INOP. REPLACED THE PITCH TRIM ACTUATOR. 2L72 4T RTA52EU 19950616002611995061600261EU 1995 6 16 COM31104 119950612A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01347CA5828 AUG910006 340A028 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950616002621995061600262EU 1995 6 16 COM31105 119950612A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 7180 JAN920181 340A140 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND, INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950616002631995061600263EA 1995 6 16 COM60497 119950611A361020035008067 CONTROL UNIT CNDAIRCL600 CL6002B19 EA RT BLEED AIR DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01943CA504 7062 RT DUCT MESSAGE CAME ON 3 TIMES. REPLACED THE BLEED AIR LEAK CONTROL UNIT. 2L72 4F RTA21EA 19950616002641995061600264 1995 6 16 DHL95802001 419950613A342025883021 DIR GYRO DOUG DC8 DC873F 302199FWP E/E COMPT MALFUNCTIONED A TDHLAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01802DH 46076 AFTER DEPARTURE FROM STANSTEAD ENGLAND, CAPT COMPASS PRECESSED 80 DEGREES IN TWO HOURS IN MAGNETIC MODE. PERFORMED AIR TURNBACK AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED CAPTAINS DIRECTIONAL GYRO PER M/M 34-21-1. 2L74 4F RT4A25 19950616002671995061600267 1995 6 16 MWEA95214 419950611A34212588369901 ADI DOUG DC9 DC932 3022066WP LT COCKPIT FLAGGED A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31501ME 47132 PILOT REPORTS ON CLIMBOUT OF MKE THE ATTITUDE FLAG ON CAPTAINS ADI APPEARED. CYCLED CIRCUIT BREAKERS, FLAG STILL IN VIEW, RETURNED TO MKE. MAINTENANCE REPLACED CAPTAIN'S ADI. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950616002681995061600268SW 1995 6 16 95ZZZW789 119950517A52102724043035 FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING BLOCK INSPECTION AT MSP, FOUND PASSENGER DOOR FRAME TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING FRAME SECTIONS P/N 27-24043-033 AND 27-24043-035. REPAIRS WERE PERFORMED IAW FAC SRM 51-00-00 PARAGRAPH 5, 51-30-04, AND 51-40-01. (W) 1L72 4T A8SW 19950616002691995061600269WP 1995 6 16 95ZZZW790 119950524A5242 DOOR DOUG DC9 DC932 3022066WP E/E COMPT NOT LATCHED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11902VJ 47177 FLT 290-1 - RDU-IAD - RETURNED TO RDU WITH THE E/E DOOR OPEN LGHT ON. CLOSED E/E DOOR, LIGHT WENT OUT. (W) 2L72 4F A6WE 19950616002701995061600270EU 1995 6 16 95ZZZW791 119950511A2910MS287831 O-RING 7581452 ISRAEL1124 1124A 4500103EU HYD SYSTEM CRIMPED A AJCAK NONE JK WARNING INDICATION FLUID LOSS DEDESCENT 1 EA2576ER 6 322 369 ABOUT 30 MINUTES BEFORE LANDING IN GRI THE RIGHT HYDRAULIC ANNUNCIATOR STARTED FLICKERING, ALL OTHER INDICATIONS NORMAL. AFTER PARKING AND WHEN SETTING THE PARKING BRAKES BOTH HYDRAULIC ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE WAS LOST. A CRIMPED TEFLON O-RING BACKING ON THE RIGHT FILTER ASSEMBLY WAS FOUND. ADVISE USE OF EXTREME CARE WHEN INSTALLING FILTER. (W) 2M72 4F A2SW 19950616002711995061600271NM 1995 6 16 MALA954458 119950517A335082410162007 EEL CONTROL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15819MA 251 FLIGHT 3204 - DURING THE POST FLIGHT INSPECTION IN MSP, THE CREW SELECTED THE COCKPIT EMERGENCY EVACUATION LIGHT OFF, BUT THE LIGHT REMAINED ILLUMINATED. MAINTENANCE REPLACED THE EVACUATION LIGHT CONTROL BOX. THE SYSTEM PERFORMED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616002721995061600272NM 1995 6 16 MALA954459 119950517A3350 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15848MA 346 FLT 3203 - AFTER SHUTDOWN IN MSP, COCKPIT EMERGENCY LIGHT REMAINED ILLUMINATED AFTER POWER WAS TURNED OFF. MAINTENANCE CYCLED POWER TO SWITCH AND THE LIGHT EXTINGUISHED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616002731995061600273NM 1995 6 16 MALA954460 119950518A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE K FLUID LOSS ININSP/MAINT 1 GL15848MA 346 FLT 3244 - DURING PREFLIGHT IN MSP, THE CREW FOUND THE EMERGENCY EXIT LIGHT IN THE FRONT RT SIDE OF THE CABIN TO BE INOPERATIVE. MAINTENANCE REPLACED THE WARDROBE LOWER BATTERY PACK. THE SYSTEM PERFORMED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950616002741995061600274SW 1995 6 16 MALA954461 119950517A33102719115075 LIGHTING PANEL SWRNGNSA227 SA227AC 8780603SW RT COCKPIT OVERHEATED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL1526863 AC650B FLT 3068 - DURING CRUISE BETWEEN DAY AND DTW, CREW NOTED SMOKE COMING FROM THE RT ESSENTIAL BUS CIRCUIT BREAKER PANEL. THE CREW SHUT OFF THE RT ESSENTIAL BUS AND THE AIRCRAFT RETURNED TO DAY. MAINTENANCE REPLACED THE RT ESSENTIAL BUS CIRCUIT BREAKER LIGHTING PANEL. THE SYSTEM PERFORMED SATISFACTORILY. (W) 1L72 4T A8SW 19950616002751995061600275SW 1995 6 16 MALA954465 119950517A52102724043033 FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING BLOCK INSPECTION AT MSP, FOUND PASSENGER DOOR FRAME TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING FRAME SECTIONS P/N 27-24043-033 AND 27-24043-035. REPAIRS WERE PERFORMED IAW FAC SRM 51-00-00 PARAGRAPH 5, 51-30-04, AND 51-40-01. (W) 1L72 4T A8SW 19950616002761995061600276SW 1995 6 16 MALA954466 119950517A57532736004010 RIB SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING BLOCK INSPECTION IN MSP, FOUND RT FLAP TO BE CRACKED AND CHAFED. REPAIRS WERE COMPLETED BY REPLACING THE INBOARD END NOSE RIB P/N 27-36004-010 DUE TO CRACKS AND THE INBOARD END AFT RIB P/N 27-36003-002 DUE TO A CHAFED AREA. ALL REPAIRS WERE COMPLETED IAW FAC SRM 57-90-60 REPAIR NR 10, 51-00-00 PAGE 4, 51-30-01, 51-40-02, AND 51-30-02. (W) 1L72 4T A8SW 19950616002771995061600277SW 1995 6 16 MALA954467 119950517A52102724150253 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING BLOCK INSPECTION IN MSP, FOUND PASSENGER DOOR FRAME TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER AN STRAP TO THE DOOR FRAME IAW FAC LAR 95-MALA-141 DATED 11 MAY 95. (W) 1L72 4T A8SW 19950616002781995061600278SW 1995 6 16 MALA954469 119950519A5730 SKIN SWRNGNSA227 SA227AC 8780603SW WS 131.899 LE BIRDSTRIKE A MALAK NONE C F.O.D. ININSP/MAINT 1 GL15434MA AC717 DURING POSTFLIGHT INSPECTION IN FFM, THE CREW FOUND A DENT IN THE LEFT LEADING EDGE DUE TO A BIRDSTRIKE JUST INBOARD OF WS 131.899. THE AIRCRAFT WAS FERRIED TO MSP FOR REPAIR. MAINTENANCE REPAIRED THE LEADING EDGE BY INSTALLING A FILLER AND REPAIR DOUBLER IAW FAC SRM 57-90-20 PAGES 3-8, DATED 1 NOV 94. (W) 2L72 4T RTA8SW 19950616002791995061600279SW 1995 6 16 MALA954470 119950520A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159.247 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721B DURING PHASE INSPECTION IN MSP, FOUND CRACK .375 INCH LONG IN LOWER RT BELT FRAME RELIEF RADIUS AT FS 159.247 AND WL 75.13. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW FAIRCHILD SRM 53-90-20 REV 1/83 PAGE 87-90. (W) 1L72 4T A8SW 19950616002801995061600280SW 1995 6 16 MALA954471 119950520A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 145.95 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15438MA AC721B DURING PHASE INSPECTION IN MSP, FOUND .5 INCH CRACK IN LOWER RT BELT FRAME RELIEF RADIUS AT FS 145.95 AND WL 75.13. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD SRM 53-90-20 REPAIR NR 20, DATED 6/83. (W) 1L72 4T A8SW 19950616002811995061600281NM 1995 6 16 MZZA95033 119950514A2913371380 HYD PUMP BOEING727 727232 1384082NM NR 1 ENG FAILED A MZZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP1315781 20636 GUM - FLT 965 - AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM OSAKA, JAPAN TO SAIPAN, CNMI. FLIGHT WAS DIVERTED TO GUAM. MAINTENANCE FOUND NR 1 ENGINE DRIVEN HYDRAULIC PUMP FAILED. MECHANIC REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PER MM 29-11-31. SYSTEM OPERATIONAL AND LEAKAGE CHECK GOOD. (W) 2L73 4F A3WE 19950616002821995061600282NM 1995 6 16 MZZA95034 119950519A291355097 HYD PUMP BOEING727 7272F9 138407DNM NR 2 ENGINE FAILED A MZZAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP13298AS 157181K 21426 FLT 938 - GUM - ON DESCENT INTO GUAM, CREW DECLARED AN EMEGENCY DUE TO 'A' SYSTEM HYDRAULIC QUANTITY LOST. AFTER LANDING, MAINTENACNE CHECKED 'A' SYSTEM QUANTITY WITH 3.5 GALLONS REMAINED. MECHANIC PERFORMED AND EXTERIOR CHECK FOR EVIDENCE OF HYDRAULIC LEAKS AND NONE FOUND. DURING ENGINE RUN UP, MECHANIC COULD NOT PRESSURIZE NR 2 HYDRAULIC SYSTEM. FURTHER TROUBLESHOOT, CONFIRMED NR 2 ENGINE DRIVEN HYDRAULIC PUMP INTERNAL FAILURE. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE DRIVED HYDRAULIC PUMP ASSY, FLUSHED LINES, REPLACED PRESSURE AND CASE DRAIN FILTERS. AIRCRAFT RETURN BACK TO SERVICE. (W) 2L73 4F RTA3WE 19950616002831995061600283WP 1995 6 16 ORJA9525 119950406A33501001191 EEL DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11834RA 53124 FOUND FORWARD EMERGENCY LIGHT ASSY INOP. REPLACED LIGHT ASSY. OPS NORMAL. (W) 2L72 4F RTA6WE 19950616002841995061600284WP 1995 6 16 ORJA9527 119950417A3350 EEL DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11878RA 53184 SEVEN EMERGENCY FLOOR LAMPS INOP. RELAMPED, OPS CHECK NORMAL. (W) 2L72 4F RTA6WE 19950616002851995061600285WP 1995 6 16 ORJA9528 119950416A3350 EEL WIRE DOUG DC9 DC987 3022087WP CABIN LOOSE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11750RA 49777 FLOOR AISLE LIGHTS INOP FROM EMERGENCY EXIT TO REAR. REPAIRED LOOSE WIRE. OPS CHECK NORMAL. (W) 2L72 4F RTA6WE 19950616002861995061600286WP 1995 6 16 ORJA9529 119950425A335041B004AD073 EEL BATTERY EA1D113D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11875RA 53182 OVERHEAD EMERGENCY LAMPS AT ROWS 18-21 INOP. REPLACED BATTERY PACK AND OPS CHECKED GOOD. (W) 2L72 4F RTA6WE 19950616002871995061600287WP 1995 6 16 ORJA9530 119950504A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11832RA 53044 AFT ACCESSORY EMPENNAGE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK/CHARGER AND RELAMPED BULBS. OPS CHECK GOOD. (W) 2L72 4F RTA6WE 19950616002881995061600288WP 1995 6 16 95ZZZZ252 119950517A5320 THRESHOLD LKHEED1011 10113851 5265010WP AFT CARGO CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, AFT CARGO DOOR CUTOUT THRESHOLD IS CORRODED FROM FS 1545 TO 1625. REMOVED CORROSION, TREATED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-50-04. 2L73 4F A23WE 19950616002891995061600289WP 1995 6 16 95ZZZZ253 119950510A5320 SUPPORT LKHEED1011 10113851 5265010WP CABIN CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, CABIN FLOOR AREA OF 3L DOOR FRAME FWD OF I/B SEAT TRACK, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, TREATED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950616002901995061600290WP 1995 6 16 95ZZZZ254 119950515A5320 DOOR FRAME LKHEED1011 10113851 5265010WP L3 DOOR AREA CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, L3 DOOR FRAME LOWER SILL PLATE HAS CORROSION. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950616002911995061600291WP 1995 6 16 95ZZZZ255 119950516A5320 SILL PLATE LKHEED1011 10113851 5265010WP L3 DOOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, L3 DOOR AREA, PLATE I/B OF LOWER SILL PANEL HAS CORROSION. REMOVED DAMAGED AREA, TREATED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-12-00. 2L73 4F A23WE 19950616002921995061600292WP 1995 6 16 95ZZZZ256 119950504A5313 LONGERON LKHEED1011 10113851 5265010WP FS 315 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19313EA 193A1020 LEVEL 2 CORROSION, INSIDE OF NR 1 HEAT EXCHANGER COMPT FWD BULKHEAD AT FS 315 LOWER I/B CORNER NEAR GEAR DOOR HINGE HOUSING, LONGERON 36. REMOVED DAMAGED AREA, TREATED AND PRIMED, FABRICATED AND INSTALLED REPAIR PER SRM 53-11-00. 2L73 4F A23WE 19950616002931995061600293WP 1995 6 16 95ZZZZ257 119950427A5313 LONGERON LKHEED1011 10113851 5265010WP FS 449 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19313EA 193A1020 LEVEL 2 CORROSION, C1 CARGO LONGERON, DOUBLER AFT OF FS 449 BULKHEAD BELOW CARGO FLOOR BBL-0 HAS CORROSION. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00. 2L73 4F A23WE 19950616002941995061600294WP 1995 6 16 95ZZZZ258 119950427A5320 SUPPORT LKHEED1011 10113851 5265010WP CABIN CORRODED A RIAAK NONE L NO TEST ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, CABIN L4 DOOR FRAME, FLOOR AREA AFT OF I/B SEAT TRACK FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGE AREA TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950616002951995061600295WP 1995 6 16 95ZZZZ259 119950519A5320 JAMB LKHEED1011 10113851 5265010WP CARGO DOOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19304EA 193A1005 LEVEL 2 CORROSION, C3 FWD DOOR JAMB IS CORRODED AT BOTTOM DOOR STOP FITTING. REMOVED DAMAGE, TREATED AREA, FABRICATED AND INSTALLED REPAIR PER DRAWING RCHL 105310-5430. 2L73 4F A23WE 19950616002961995061600296WP 1995 6 16 95ZZZZ260 119950519A5313 STRINGER LKHEED1011 10113851 5265010WP FS 953-965 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19313EA 193A1020 LEVEL 2 CORROSION, MID ELECTRICAL SERVICE CENTER RT SIDE BELOW FLOOR STRINGER 31 STA 953 TO 965 HAS CORROSION. REMOVED DAMAGE, TREATED, FABRICATED AND INSTALLED REPAIR PER DRAWING NR RCHL15330-5503. 2L73 4F A23WE 19950616002971995061600297SO 1995 6 16 C2XA95IA090 119950528A572012017056010 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 DURING C-CHECK INSPECTION, THE RT WING DEFUEL VALVE DISCHARGE BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950616002981995061600298SO 1995 6 16 C2XA95IA091 119950528A572012004357018 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 3 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950616002991995061600299SO 1995 6 16 C2XA95IA097 119950528A572012004357012 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 16 AFT LOWER SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950616003001995061600300CE 1995 6 16 HERA9510 119950404A79311013890233 TRANSMITTER BEECH 1900 1900C 1154161CE NR 2 ENGINE DEFECTIVE A HERAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AL031553C UC24 ANC - FLT 3423 - AIR TURN DUE TO THE NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING BETWEEN 20 AND 120 PSI. THE ACFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 OIL PRESSURE TRANSMITTER AND RETURNED THE ACFT TO SERVICE. (Z) 2L72 4T RTA24CE 19950616003011995061600301EA 1995 6 16 HERA9511 119950414A3310 RHEOSTAT DHAV DHC6 DHC6300 EA RT COCKPIT DEFECTIVE A HERAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL03724CA 793 ANC - FLT 1133 - AIR RETURN DUE TO SMOKE IN COCKPIT. ACFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE FOUND THE COPILOTS COCKPIT LIGHTS DIMMING RHEOSTAT DEFECTIVE. THE RHEOSTAT WAS REMOVED AND REPLACED AND THE ACFT WAS RETURNED TO SERVICE. (Z) 1H72 3T A9EA 19950616003021995061600302 1995 6 16 HERA9512 419950420A61228210004 GOVERNOR DHAV DHC6 DHC6300 EA NR 2 PROP MALFUNCTIONED A HERACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 AL03724CA 793 ANC - FLT 1121 - ABORTED TAKEOFF DUE TO ACFT YAWED TO THE RT BEFORE REACHING V1 SPEED. THE ACFT STOPPED ON THE RUNWAY WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 PROPELLER GOVERNOR AND RETURNED THE ACFT TO SERVICE. (Z) 1H72 3T A9EA 19950616003031995061600303NM 1995 6 16 MRKA9543 119950406A2120 AIR DISTR BOEING737 7372X6C 1384552NM FLIGHT DECK ODOR A MRKAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 AL03673MA 23124 HOT ODOR NOTICED IN FLIGHT DECK ON TAKEOFF, AFTER LANDING GEAR RETRACTED DISAPPEARED RAPIDLY. UNABLE TO NOTICE ANY ODOR WHILE OPERATING ENGINES, APU, ELECTRICAL SYSTEMS, AND AIR CONDITIONING SYSTEM ON GROUND. ACFT RETURNED TO SERVICE. (Z) 2L72 4F RTA16WE 19950616003041995061600304NM 1995 6 16 MRKA9544 119950410A35304566M7B042N PBE BOEING737 7372T4C 1384501NM COCKPIT SEAL BROKEN A MRKAK NONE O OTHER ININSP/MAINT 1 AL03676MA 23066 CONTROL CABIN PBE VACUUM SEAL BROKEN. REMOVED AND REPLACED PBE. (Z) 2L72 4F RTA16WE 19950616003051995061600305WP 1995 6 16 ORJA9535 119950521A3350 EEL WIRES DOUG DC9 DC983 3022083WP CABIN LOOSE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 EMERGENCY FLOOR EXIT LIGHTS BETWEEN FIRST AND Y CLASS PARTITION INOP. RESECURED HOT WIRE EMERGENCY FLOOR LIGHTS BETWEEN FIRST AND Y CLASS. OPS GOOD. (Z) 2L72 4F RTA6WE 19950616003061995061600306WP 1995 6 16 ORJA9536 119950521A335041B004AD073 EEL BATTERY DOUG DC9 DC983 3022083WP AFT DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 EMERGENCY EXIT LIGHTS ON AFT SECTION FLOOR LIGHTS INOP. REPLACED BATTERY PACK ON EMERGENCY FLOOR LIGHTS AFT. OPS GOOD. (Z) 2L72 4F RTA6WE 19950616003071995061600307WP 1995 6 16 ORJA9537 119950522A3350 EEL CONNECTOR DOUG DC9 DC983 3022083WP CABIN LOOSE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 EMERGENCY FLOOR LIGHTS SEAT INOP. RECONNECTED ELECTRICAL PLUG, CHECKS OK. (Z) 2L72 4F RTA6WE 19950616003081995061600308NM 1995 6 16 9509336729 119950609A5313 LONGERON BOEING747 747251F 1384898NM FS 1950 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01629US 22388 DURING PERIODIC CHECK, FOUND CORROSION ON STR 51L AT FS 1950. REPAIRED STRINGER (P/N 65B04483-6) PER EA 67-96734. 2L74 4F A20WE 19950616003091995061600309NM 1995 6 16 9509345509 119950609A5315 FLOORBEAM BOEING757 757251 1384970NM FS 345 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01509US 23198 DURING PERIODIC CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 345 AT LBL 22 TO RBL 25. REPAIRED BEAM (P/N 141N5111) PER EA 55-98496. 2L72 4F RTA2NM 19950616003101995061600310EU 1995 6 16 9509353250 119950609A3250C24736001 SERVO UNIT AIRBUS320 A320211 3930320EU NLG STEERING MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL01350NA8686 89 418 EN ROUTE LGA TO MSP, NOSE WHEEL STEERING FAULT APPEARED, RESETS WERE UNSATISFACTORY. A NORMAL LANDING WAS MADE AND THE AIRCRAFT TAXIED CLEAR OF THE RUNWAY. AIRCRAFT WAS TOWED TO THE GATE. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL. OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA28NM 19950616003111995061600311WP 1995 6 16 9509369302 119950606A3260D06A10SL3S CONNECTOR DOUG DC9 DC982 3022082WP NLG BROKEN A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01302RC 48055 LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED DOWNLOCK SENSOR DISCONNECT P1-1157 AND D1-32 INSIDE CONDUIT. OPERATIONAL CHECK OK ON NUMEROUS GEAR CYCLES. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003121995061600312WP 1995 6 16 9509379752 119950611A2420 WIRE DOUG DC9 DC941 302207NWP LT AC GENERATOR BROKEN A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01752NW 47116 SHORTLY AFTER TAKEOFF, LEFT GENERATOR OFF, DC BUS OFF, LEFT AC BUS OFF, AND AC CROSSTIE LOCKOUT LIGHTS ILLUMINATED. INITIATED COCKPIT OPERATING MANUAL PROCEDURES AND TRIED RESTORING GENERATOR BACK ON LINE WITH NO SUCCESS. FLIGHT RETURNED TO YEG AND LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE TO FIELD CONNECTOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003131995061600313 1995 6 16 9509389882 419950606A344220412170413 RADAR TRANS DOUG DC9 DC951 3022051WP FWD ACCESS COM MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL01670MC258852598 47659 WEATHER RADAR SYSTEM FAILED EN ROUTE DTW TO GRB. FLIGHT RETURNED TO DTW DUE TO THUNDERSTORMS AHEAD. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003141995061600314WP 1995 6 16 9509399908 119950609A3231 RETRACT MECH DOUG DC9 DC931 3022065WP NLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01958N 47254 EXCESSIVE VIBRATION FROM NOSE WHEEL AREA ON GEAR RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR OPEN, SECURED DOOR. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003151995061600315WP 1995 6 16 9509409997 119950607A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING P NO WARNING INDICATION UKUNKNOWN 1 GL018933E 47142 LOSS OF CABIN PRESSURE OCCURRED EN ROUTE MSP TO DFW. INITIATED EMERGENCY DESCENT AND FLIGHT DIVERTED TO MCI, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. CABIN PRESSURE WARNING LIGHT DID ILLUMINATE. HOWEVER, CABIN ALTITUDE WAS NOT HIGH ENOUGH TO ACTIVATE OXYGEN MASK DEPLOYMENT. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. ALSO, MADE INTERIM REPAIR TO AFT VENTRAL PLUG DOOR SEAL. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003161995061600316WP 1995 6 16 9509419945 119950609A56105912290505 WINDSHIELD DOUG DC9 DC931 3022065WP LEFT COCKPIT DELAMINATED A NWAAA UNSCHED LANDING O OTHER UKUNKNOWN 1 GL018925E654 654 45840 LEFT COCKPIT WINDSHIELD CRACKED EN ROUTE DFW TO MSP. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO STL, AN UNEVENTFUL LANDING WAS ACCOMPLISHED. FOUND CAPTAIN'S WINDSHIELD DELAMINATED ON ALL SIDES. REPLACED WINDSHIELD AND TEMPERATURE CONTROLLER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003171995061600317WP 1995 6 16 ABXA9500534 119950609A32305916405509 CONTROL VALVE DOUG DC9 DC931 3022065WP LANDING GEAR DEFECTIVE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23942AX 47552 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED ENTIRE TRIP. DURING UPLATCH CHECK GEAR DOOR OPEN LIGHT ILLUMINATED, GEAR WAS RECYCLED. REPLACED LANDING GEAR CONTROL VALVE IAW DC-9 MM 32-32-1 PAGES 201 TO 205. SYSTEM OPS CHECKED GOOD IAW DC-9 MM 32-32-0 PAGES 201 TO 203. 2L72 4F A6WE 19950616003181995061600318CE 1995 6 16 BIER950013 119950614A2720031019613 SPRING CESSNA150 152 2071835CE RT RUDDER PEDAL BROKEN B BIEAK NONE O OTHER TXTAXI/GRND HDL 1 EA21757ZR 15280138 FOUND BROKEN RUDDER PEDAL RETURN SPRING (P/N 0310196-13), ON RT PEDAL, WHICH CAUSED PEDAL TO FALL TO FLOOR. SUBMITTER STATES BOTH SPRINGS SHOULD BE INSPECTED CLOSELY, ANNUALLY AND REPLACED AT 5 YEAR INTERVALS. 1H71 3O NT3A19 19950616003191995061600319WP 1995 6 16 ERA00006 119950524A32601HE1912 SWITCH BRACKET CVAC 340 34031 2422704WP ALLSN 501D 501D13H 03004GL LT MLG LOOSE A ERAALA ABORTED APPROACH UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 AL03569JA 69 LEFT GEAR DOWN LIGHT WOULD NOT ILLUMINATE. RETURNED TO ANC AND MADE UNEVENTFUL LANDING. TIGHTENED AND RERIGGED LOOSE LT MLG DOWNLOCK SWITCH BRACKET IAW CV580 M/M 32-61-31 PG 501 AND 502. RETRACT TEST SUCCESSFUL. 2L72 4R4 T 6A6 E282 19950616003201995061600320NM 1995 6 16 SCNA95127 119950605A274165276781 SWITCH BOEING727 727227 1384078NM HORIZ STAB FAILED A SCNAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL15275AF 22092 TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES ADVANCED. AIRCRAFT RETURNED TO GATE, FOUND UPPER STABILIZER TAKEOFF WARNING SWITCH S532 BAD. REMOVED AND REPLACED SWITCH PER MM 31-26-24 PAGE 401. SYSTEM OPS CHECKED GOOD. 2L73 4F A3WE 19950616003211995061600321NM 1995 6 16 SCNA95128 119950607A26126120272 FIRE WIRE BOEING727 7272J4 1384006NM APU FAULTY A SCNAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL15288SC 20765 WHILE STARTING THE APU IN DFW THE FIRE WARNING LIGHT ILLUMINATED, BUT DID NOT RECEIVE THE WARNING BELL. THE FIRE HANDLE WAS PULLED AND ONE FIRE BOTTLE WAS DISCHARGED AND THE FIRE WARNING LIGHT EXTINGUISHED. THE APU WAS INSPECTED AND NO SIGNS OF FIRE WERE NOTED. FOUND FAULT IN FIRE DETECTION SYSTEM ATTRIBUTED TO SHORTED WIRES IN PLUG D4858, PINS 4 AND 9, REPAIRED WIRES. REMOVED AND REPLACED APU FIRE LOOP PER MM 26-15-02 PAGE 401. REPLACED BLOWN FIRE BOTTLE PER MM 26-23-01. 2L73 4F RTA3WE 19950616003271995061600327NE 1995 6 16 95ZZZX2939 219950419A7240 COMB CHAMBER DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE ENG HOLE BURNED A AENAK NONE O OTHER ININSP/MAINT 1 WP191271L49767 47319 674577 DURING AN 'N' CHECK INSPECTION, A SMALL .3750 INCH HOLE WAS FOUND IN THE COMBUSTION CHAMBER CASE AT APPROXIMATELY THE 10 O'CLOCK POSITION. (THE OUTER FAN DUCT ALSO BURNED THROUGH). REFERENCE: OPER CONTROL NR AENA131C. 2L72 4F4 F A6WE E2EA 19950616003351995061600335CE 1995 6 16 95ZZZX2947 119950524A7120075100113 MOUNT CESSNA180 180J 2072622CE ENG CRACKED A ASQPAK NONE O OTHER ININSP/MAINT 1 NM07520954700 18052496 DURING INSPECTION OF ENGINE MOUNT AFTER ENGINE REMOVAL FOR OVERHAUL, CRACKS WERE FOUND AT BOTH FORWARD ENGINE MOUNTING BRACKET LOCATIONS. SUSPECT THAT CRACKS ARE DUE TO FATIGUE. CRACKS ARE DIFFICULT TO SEE WITH THE ENGINE INSTALLED DUE TO THE CLOSE PROXIMITY OF THE RUBBER MOUNTING PADS. RECOMMEND CLOSE INSPECTION OF THIS AREA AT ANNUAL INSPECTIONS. 1H71 3O 5A6 19950616003401995061600340SO 1995 6 16 95ZZZX2952 119950426A81204066109020 TURBOCHARGER PIPER PA31 PA31325 7103105SO LYC O540 TIO540F2BD 41532EA RT ENGINE LEAKING A AVRAA UNSCHED LANDING KR FLUID LOSS PARTIAL RPM/PWR LOSS CLCLIMB 1 GL21325YH 1587 TCR0167 317812007 SHORTLY AFTER TAKEOFF, RT ENGINE LOST POWER. MAP DROP TO 15 INCHES. AIRCRAFT RETURNED TO FARGO. INSPECTION REVEALED OIL LEAKING FROM INTAKE DRAIN. FOUND OIL SEAL RUPTURE IN TURBOCHARGER AND FLOODED OUT INTAKE SYSTEM. EST 1 QUART OF OIL IN INTAKE SYSTEM, ALL PLUGS WERE OIL SOAKED. 1L72 3O3 O A20SO E14EA 19950616003641995061600364WP 1995 6 16 95ZZZW792 119950530A2410 CSD DOUG DC9 DC932 3022066WP NR 2 MALFUNCTIONED A VJ6AH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO11933VV 47489 FLT 518 - EN ROUTE FROM ATL-PHL, EXPERIENCED ERRATIC VOLTS AND FREQUENCIES ON NR 2 GENERATOR. CREW DISCONNECTED CSD. PLACED ON MEL 24-1-1, MEL LOG PAGE NR 3037. (W) 2L72 4F A6WE 19950616003651995061600365WP 1995 6 16 95ZZZW793 119950530A2420976J2544 GEN CONTL PNL DOUG DC9 DC932 3022066WP COCKPIT FAILED A VJ6AH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO11933VV 47489 FLIGHT NR 392 - EN ROUTE FROM FLL-ATL - HAD TO DISCONNECT NR 2 CSD DUE TO ERRACTIC VOLTS AND FREQUENCIES. REMOVED AND REPLACED GENERATOR CONTROL PANEL. (W) 2L72 4F A6WE 19950616003661995061600366WP 1995 6 16 95ZZZW794 119950527A3350 EEL WIRE DOUG DC9 DC932 3022066WP CABIN BROKEN A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11905VJ 47378 EMERGENCY ESCAPE PATH LIGHTING AT ROWS 14 THROUGH 21 INOP. FOUND BROKEN SPLICE IN OVERHEAD AT AFT BATTERY PACK/CHARGER. REPLACED SPLICE, OPS CHECKED OK. (W) 2L72 4F A6WE 19950616003671995061600367WP 1995 6 16 ASAA9580115 119950518A33501001191 EEL PORTABLE DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS7320 697 53449 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950616003681995061600368WP 1995 6 16 ASAA9580117 119950523A33501001191 EEL PORTABLE DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS6848 49236 PAE - DURING 30K CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950616003691995061600369 1995 6 16 F3LA95009 419950328A22104050735903 PITCH CONTROL BOEING737 737201 1384454NM AUTO PILOT MALFUNCTIONED A F3LAO OTHER O OTHER DEDESCENT 1 NM03207AU619461465 19423 DEN - UPON DESCENT INTO DEN, FLIGHT CREW REPORTED THEY WERE UNABLE TO MOVE THE ELEVATOR WITH THE CONTROL WHEEL WHILE THE AUTO PILOT WAS ENGAGED. THE AUTO PILOT WAS DISENGAGED, NORMAL CONTROL WAS RESUMED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PITCH CONTROL CHANNEL AND CHECKED OK. (W) 2L72 4F A16WE 19950616003701995061600370WP 1995 6 16 HAL95064 119950521A53205939711501 ANGLE DOUG DC9 DC951 3022051WP FS 1230 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA 47689 THE LEFT DORSAL FIN ATTACH ANGLE HAS A CONDITION 2 CRACK IN THE VERTICAL LEG REF EO 53-92-32-91 FIG 1. REMOVED THE LEADING EDGE PANEL, REMOVED AND REPLACED THE DORSAL FIN ATTACH ANGLE WITH A NEW ATTACH ANGLE. REINSTALLED THE LEADING EDGE PANEL PER SRM 51-30-AND SRM 51-30-1. (W) 2L72 4F A6WE 19950616003711995061600371WP 1995 6 16 HAL95065 119950521A53203912073501N1 FITTING DOUG DC9 DC951 3022051WP FS 794 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA 47689 LEFT REAR SPAR TO TRAPEZOIDAL PANEL ATTACH FITTING CRACKED AT THE LOWER INBOARD BOLT HOLE. THE CRACK WAS DETECTED DURING AN ULTRA-SONIC INSPECTION. REMOVED AND REPLACED THE REAR SPAR TRAPEZOIDAL FITTING AT LEFT FUSELAGE STATION 794, PER SRM 51-30-02. (W) 2L72 4F A6WE 19950616003721995061600372WP 1995 6 16 HAL95066 119950523A57535913560173 LE CAP DOUG DC9 DC951 3022051WP LT TE FORE FLAP CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA 47689 SBA - THE LEFT WING OUTBOARD LEADING EDGE CAP IS EXFOLIATED ON FLAP AT THE BASE OF FOREFLAP MOUNTS IN 3 LOCATIONS. REMOVED THE DAMAGED CAP AND SENT OUT FOR OVERHAUL. INSTALLED THE OVERHAULED CAP PER SRM 51-30-01. (W) 2L72 4F A6WE 19950616003731995061600373WP 1995 6 16 HAL95067 119950523A5531 FITTING DOUG DC9 DC951 3022051WP VERT STAB CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13420EA 47689 SBA - THE UPPER LEFT RUDDER HINGE AT THE REAR SPAR OF THE VERTICAL STABILIZER HAS SURFACE CORROSION AND FITTING IS CRACKED AT THE OUTBOARD SIDE OF THE FASTENER HOLE. REPLACED RUDDER HINGE 'A' ARM IAW MM 27-20-1. (W) 2L72 4F A6WE 19950616003741995061600374EU 1995 6 16 PAYA95A4022 119950509A3260 GEAR LIGHTS AEROSPATR42 ATR42300 8680920EU LANDING GEAR MALFUNCTIONED A PAYAO OTHER N FALSE WARNING CLCLIMB 1 EA174205G 77 FLT NR 7664 - PNE-JFK - AFTER LANDING GEAR WAS SELECTED UP, THE GEAR RETRACTED BUT ALL SIX TRANSIT LIGHTS REMAINED ON. RESET EMERGENCY EXTENSION HANDLE. (W) 2H72 4T RTA53EU 19950616003751995061600375EU 1995 6 16 PAYA95A4023 119950510A3260 PROX SW AEROSPATR42 ATR42300 8680920EU NLG DIRTY A PAYAO OTHER N FALSE WARNING APAPPROACH 1 EA174205G 77 FLT NR 7740 - DCA-JFK - SECONDARY NOSE LANDING GEAR TRANSIT LIGHT ON WITH LANDING GEAR SELECTED UP. REMOVED EXCESSIVE DIRT AND GREASE FROM NOSE GEAR SECONDARY PROX SWITCH TARGET AND PERFORMED RETRACTION CHECKS. (W) 2H72 4T RTA53EU 19950616003761995061600376EU 1995 6 16 PAYA95A4024 119950520A3234F96GA0102 SELECTOR AEROSPATR42 ATR42300 8680920EU LANDING GEAR MALFUNCTIONED A PAYAO OTHER J WARNING INDICATION CLCLIMB 1 EA174203G14380 052 DCA - JFK - FLT NR 7742 - LANDING GEAR SELECT HANDLE HARD TO MOVE TO THE GEAR UP POSITION. REPLACED LANDING GEAR SELECTOR AND COMPLIED WITH RETRACTION CHECK. (W) 2H72 4T RTA53EU 19950616003771995061600377EU 1995 6 16 PAYA95A4025 119950522A5210 FRAME AEROSPATR42 ATR42300 8680920EU PAX DOOR STEP CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174203G16961 052 PASSENGER DOOR STEP FRAME CRACKED. REPAIRED IAW SRM. (W) 2H72 4T RTA53EU 19950616003781995061600378EU 1995 6 16 PAYA95A4026 119950528A3240S2918056210800 HYD LINE AEROSPATR42 ATR42300 8680920EU MLG BRAKE CRACKED A PAYAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 EA174209G 129 FLT NR 7732 - BWI-JFK - CREW REPORTED LANDING GEAR SLOW TO RETRACT. UPON EXTENSION AN UNUSUAL SOUND WAS NOTED COMING FROM THE AREA OF THE NOSE GEAR AND THE GEAR WAS SLOW TO EXTEND. JFK MAINTENANCE FOUND HYDRAULIC QUANTITY LOW AS A RESULT OF A CRACKED BRAKE LINE AT THE METERING VALVE. THE LINE WAS REPLACED AND HYDRAULICS SERVICED AT JFK. THE AIRCRAFT WAS THEN FERRIED TO PNE WHERE AFTER INSPECTION AND OPS CHECKS THE REPORTED LANDING GEAR PROBLEM COULD NOT BE DUPLICATED. (W) 2H72 4T RTA53EU 19950616003791995061600379NM 1995 6 16 TSAA9553078 119950508A5320 INTERCOSTAL BOEING737 737297 1384480NM FUSELAGE CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13728AL 22629 DURING SCHEDULED INSPECTION OF FUSELAGE, FORWARD SERVICE DOORWAY AFT FRAME (AD88-03-03 AMDT 39-5832). FOUND STRINGER S-8A INTERCOSTAL WITH 2.75 INCH CRACK. REPAIRED PER DRAWING 65C33288. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950616003801995061600380NM 1995 6 16 TSAA9553079 119950518A5330 SKIN BOEING737 737297 1384480NM BS 7272 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP1370723 21739 DURING OVERNIGHT SCHEDULED INSPECTIONS, DISCOVERED FUSELAGE SKIN CRACKS AT BS 727A, S-18L (TWO .375 INCH), AND AT BS 727A, S-17A (4 INCH). REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950616003811995061600381NM 1995 6 16 TSAA9575083 119950523A3610655812310 DUCT ASSY BOEING737 7372Q9 138448MNM NR 2 ENGINE CRACKED A TSAAO OTHER J WARNING INDICATION CRCRUISE 1 WP13809AL 21720 PILOT REPORT FLIGHT NR 30 - LIH-OGG - NR 2 ENGINE START VALVE OPEN LIGHT CAME ON AND STAYED ON INFLIGHT. SHUT DOWN ENGINE AND DIVERTED TO HNL. FOUND 13TH STAGE BLEED AIR DUCT BLOWN OUT OVER STARTER VALVE PRESSURE SWITCH. REPLACED DUCT, NO LEAKS NOTED. OPS CHECK START VALVE, CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950616003821995061600382NE 1995 6 16 TSAA9577081 219950521A7200 ENGINE BOEING737 737297 1384480NM PWA JT8 JT8D9A 52048NE NR 1 FOD A TSAACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 WP1370723 21739 FLT NR 71 - HNL-LIH - TWO ABORTED TAKEOFFS. ON FIRST TAKEOFF ROLL NR 2 ENGINE EPR VERY HIGH, OTHER INDICATIONS NORMAL. REMOVED FOD FROM NR 2 ENGINE INLET OVER PT2. GROUND RUN CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ON SECOND TAKEOFF, MAX EPR NR 1 ENGINE 1.73 ON TAKEOFF ROLL. THROTTLE MOVEMENT ABNORMAL. ABORTED TAKEOFF. FIELD TRIM NR 1 ENGINE. OPS CHECK OK. THROTTLE MOVEMENT NORMAL. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F4 F A16WE E2EA 19950616003831995061600383NM 1995 6 16 TSAA9580082 119950522A800035C552651 START VALVE BOEING737 7372Q9 138448MNM NR 2 ENGINE MALFUNCTIONED A TSAAO OTHER J WARNING INDICATION CRCRUISE 1 WP13809AL 1110H 21720 PILOT REPORT FLIGHT 480 - HNL-KOA - NR 2 START VALVE OPEN LIGHT FLICKERED ON MOMENTARILY IN FLIGHT THEN EXTINGUISHED. DECLARED IN FLIGHT EMERGENCY. LANDED WITH NO INCIDENT IN KOA. CHECKED STARTER AND START VALVE AND CLEANED CANNON PLUG ON START VALVE. FUNCTIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950616003841995061600384NM 1995 6 16 9509425530 119950613A2780 RETRACT MECH BOEING757 757251 1384970NM LE FLAPS MALFUNCTIONED A NWAAL ABORTED APPROACH JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 GL01530US 23845 LEADING EDGE SLAT DISAGREE LIGHT CAME ON DURING APPROACH. AIRCRAFT MADE A GO-AROUND AND EMERGENCY EQUIPMENT WAS REQUESTED BY THE CREW. USED ALTERNATE FLAP PROCEDURE AND LANDED WITHOUT INCIDENT. MAINTENANCE IS IN PROGRESS. 2L72 4F RTA2NM 19950616003851995061600385WP 1995 6 16 9509439908 119950614A3231 DOOR LINK DOUG DC9 DC931 3022065WP NLG BINDING A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01958N 47254 VIBRATION FROM NOSE LANDING GEAR AREA WAS EXPERIENCED AFTER TAKEOFF. FLIGHT RETURNED TO DTW. INSPECTED AND FOUND RIGHT FORWARD GEAR DOOR HANGING DOWN AND DOOR LINK LOCKING UP INTERMITTENTLY. REPLACED THE RIGHT NOSE GEAR DOOR LINK. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003861995061600386WP 1995 6 16 9509449953 119950613A2130 PRESSURIZATION DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01918RW 47158 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. PERFORMED CHECK OF AUTO AND MANUAL PRESSURIZATION SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003871995061600387WP 1995 6 16 9509459992 119950614A213354447211 OUTFLOW ACT DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAG O2 MASK DEPLOYED J WARNING INDICATION DEDESCENT 1 GL018960E632 632 45869 LOSS OF PRESSURIZATION OCCURRED ON DESCENT INTO BDL. NORMAL PRESSURE WAS REGAINED USING MANUAL OPERATION, HOWEVER, OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. REPLACED OUTFLOW VALVE ACTUATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950616003881995061600388WP 1995 6 16 ABXA9500535 119950612A335060030431 EEL POWER SUPPLY DOUG DC9 DC941 302207NWP CABIN DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23969AX 2141 47464 EMERGENCY LIGHTS COME ON WHEN POWER IS TURNED OFF. REPLACED EMERGENCY LIGHTS POWER PACK. OPS CHECKED GOOD IAW DC-9 M.M., CHAPTER 33. 2L72 4F A6WE 19950616003891995061600389SO 1995 6 16 COM11918 119950613A323012043270501 RELAY BOX EMB 120 EMB120RT SO NLG DEFECTIVE A COMAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO01243CA6029 1000 120212 STRONG VIBRATION FROM NLG AREA AFTER TAKEOFF. FOUND LANDING GEAR DOORS REMAINED OPEN AFTER GEAR RETRACTION. REPLACED LANDING GEAR RELAY BOX. 2L72 4T RTA31SO 19950616003901995061600390SW 1995 6 16 COM20377 119950609A8010H2211 START SWITCH SWRNGNSA227 SA227AC 8780603SW RT ENGINE DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01458AM AC699 START TEST SWITCH WILL CAUSE RT ENGINE TO START. (FUEL FLOW AND IGNITION). REPLACED THE START SWITCH. 1L72 4T A8SW 19950616003911995061600391SW 1995 6 16 COM20378 119950609A32972782640011 HARNESS SWRNGNSA227 SA227AC 8780603SW NLG DEFECTIVE A COMAO OTHER P NO WARNING INDICATION CRCRUISE 1 SO01457AM AC694 NLG INTRANSIT INDICATION IS INOP. REPLACED THE NLG UP POSITION AND LIMIT SWITCH HARNESS ASSY. 2L72 4T RTA8SW 19950616003921995061600392EU 1995 6 16 COM31106 119950613A33506104781 EEL BATTERY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01158CA 340A158 EMERGENCY EXIT SIGN AT MAIN CABIN DOOR WILL NOT ILLUMINATE. REPLACED EMERGENCY BATTERY. 2L72 4T RTA52EU 19950616003931995061600393EU 1995 6 16 COM31107 119950612A2450A2042C PDU SAAB SF340 SF340A 7850100EU LEFT DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01140N 11630597 340A140 LEFT MAIN ELECTRIC BUS FAILED IN FLIGHT AND DID NOT AUTO TRANSFER. REPLACED THE LT POWER DISTRIBUTION UNIT. 2L72 4T RTA52EU 19950616003941995061600394 1995 6 16 DHL95720004 419950616A3414B024781101 AIRSPEED IND BOEING727 727228 NM LT COCKPIT MALFUNCTIONED A TDHLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01720DH 19544 DURING CLIMB, CAPTAIN'S AIRSPEED INDICATOR ERRATIC AND UNRELIABLE, PLUS OR MINUS 300 KNOTS. CAPT IVSI ERRATIC PLUS OR MINUS 400 AND STICKING. STANDBY ALTIMETER UNRELIABLE UP TO 10,000 FEET AT 310 KNOTS. DIVERTED TO CVG, LANDED WITHOUT INCIDENT. CONFIRMED CAPTAIN'S AIRSPEED INDICATOR HAS SEVERE CASE LEAK. REPLACED INICATOR. CHECKS GOOD PER DHL MTM 34-22-01. REPAIRED A STATIC LEAK. IVSI AND STANDBY ALTIMETER CHECKS GOOD PER DHL MTM 34-22-01. 2L73 4F A3WE 19950616003951995061600395CE 1995 6 16 JGVR061501 119950615A5210 SKIN CESSNA500 S550 2076607CE CABIN DOOR BENT B JGVRK NONE O OTHER ININSP/MAINT 1 CE097007Q 0030 UPPER CABIN DOOR LINTEL CHAFED AT FWD CORNER, APPROX. .010 INCH DEEP. CHAFING CAUSED BY DOOR SKIN WHICH WAS BENT SLIGHTLY INWARD AND OUT OF ADJUSTMENT DOOR. 1L72 4F RTA22CE 19950616003961995061600396WP 1995 6 16 MWEA95215 119950613A7603188001 CONTROL CABLE DOUG DC9 DC915 3022036WP LT ENGINE SEPARATED A MWEAO OTHER O OTHER LDLANDING 1 GL31300ME 45718 PILOT REPORTS ON LANDING IN OMA THE LEFT THRUST REVERSER WOULD NOT DEPLOY. THE UNLOCK LIGHT CAME ON BUT COULD NOT FEEL INTERLOCK STOP IN THROTTLE. MAINTENANCE FOUND LEFT THROTTLE CABLE SEPARATED AT SWIVEL JOINT NEAR ENGINE. REMOVED AND REPLACED CABLE. PERFORMED ENGINE RUN. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950616003971995061600397 1995 6 16 MWEA95216 419950614A3454001124101 SWITCHING UNIT DOUG DC9 DC932 3022066WP E/E COMPT FAILED A MWEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31401ME 47133 PILOT REPORTS NR 1 AND NR 2 NAVS FAILED ENROUTE TO BOS. A/C RETURNED TO MKE. MAINTENANCE FOUND NAV SWITCHING UNIT FAILED. REMOVED AND REPLACED SWITCHING UNIT. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950616003981995061600398SW 1995 6 16 QXEA9500169 119950530A215020475546 COOLING TURBINE GARRTT SWRNGNSA227 SA227AC 8780603SW NR 2 OVER SERVICED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09380PH AC582 PDX - NR 2 BLEED AIR EMITS SMOKE. DRAINED ANY EXCESS OIL FROM COOLING TURBINE. WATER SEPERATOR SOCK CLEANED. NR 2 BLEED OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950616003991995061600399NM 1995 6 16 UPS203513 119950613A5530 CHORD BOEING727 72731C 1384011NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B. 2L73 4F A3WE 19950616004001995061600400NM 1995 6 16 UPS203514 119950613A5530 CHORD BOEING727 72731C 1384011NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD RT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B. 2L73 4F A3WE 19950616004011995061600401NM 1995 6 16 UPS203515 119950613A5530 CHORD BOEING727 72731C 1384011NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B. 2L73 4F A3WE 19950616004021995061600402NM 1995 6 16 UPS203516 119950613A5530 CHORD BOEING727 72731C 1384011NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER UPPER CHORD LT SIDE AT B.S. 1342. REPLACED IAW SRM 51-30-2, E.O. B727-5530-4601B. 2L73 4F A3WE 19950616004031995061600403NM 1995 6 16 UPS203517 119950613A5320 ANGLE BOEING727 72731C 1384011NM FS 1370 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CRACKED ANGLE AT B.S. 1370, LT SIDE WL 254.5. INSTALLED FABRICATED PARTS IAW SRM 54-10-2, 51-10-2. 2L73 4F A3WE 19950616004041995061600404NM 1995 6 16 UPS203518 119950613A5320 ANGLE BOEING727 72731C 1384011NM FS 1370 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-CHECK, MAINTENANCE FOUND CRACKED ANGLE AT B.S. 1370, RT SIDE WL 259.5 INSTALLED FABRICATED PARTS IAW SRM 54-10-2, 51-10-2. 2L73 4F A3WE 19950616004051995061600405NM 1995 6 16 UPS203519 119950613A5531 SPAR CHORD BOEING727 72722C 138400FNM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND LT VERTICAL FIN REAR SPAR CHORD CRACKED STA 22.5, F.S. 1342. REPAIRED IAW SRM 51-10-3. 2L73 4F A3WE 19950616004061995061600406NM 1995 6 16 UPS203520 119950613A5531 SPAR CHORD BOEING727 72722C 138400FNM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND RT VERTICAL FIN REAR SPAR CHORD CRACKED AT STA 22.5, F.S. 1342. REPAIRED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004071995061600407NM 1995 6 16 UPS203521 119950613A5530 FRAME BOEING727 72722C 138400FNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT FRAME CHORD B.S. 1342, RBL 20, WL 238. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004081995061600408NM 1995 6 16 UPS203522 119950613A5311 FRAME BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON RT LOWER FRAME CHORD B.S. 1342, RBL 24, WL 220. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004091995061600409NM 1995 6 16 UPS203523 119950613A5311 FRAME BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT LOWER FRAME CHORD B.S. 1342, LBL 24, WL 220. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004101995061600410NM 1995 6 16 UPS203524 119950613A5320 CHANNEL BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL B.S. 1342. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004111995061600411NM 1995 6 16 UPS203525 119950613A5320 CHANNEL BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CENTER CHANNEL B.S. 1342, RBL 18, WL 247. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004121995061600412NM 1995 6 16 UPS203527 119950613A5530 CHORD BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON CHORD B.S. 1342, RBL 30, WL 250. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004131995061600413NM 1995 6 16 UPS203528 119950613A5530 CHORD BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON O/B CHORD B.S. 1342, LBL 30, WL 250. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004141995061600414NM 1995 6 16 UPS203529 119950613A5530 CHORD BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CENTER FWD CHORD CORRODED B.S. 1342. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004151995061600415NM 1995 6 16 UPS203530 119950613A5311 FRAME BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND LT FRAME CHORD CORRODED B.S. 1342, LBL 20, WL 238. REPLACED IAW E.O. B727-5530-4601. 2L73 4F A3WE 19950616004161995061600416NM 1995 6 16 UPS203531 119950613A5320 WEB BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON RT SIDE OF AFT AIRSTAIRS, TOP ROW OF LIGHTENING HOLES, 2ND FROM FRONT. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950616004171995061600417NM 1995 6 16 UPS203532 119950613A5320 WEB BOEING727 72722C 138400FNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON LT SIDE OF AFT AIRSTAIRS, TOP ROW OF LIGHTENING HOLES, 4TH FROM FRONT. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950616004181995061600418NM 1995 6 16 UPS203533 119950613A5320 WEB BOEING727 72722C 138400FNM FS 1283 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND .50 INCH CRACK ON UPPER TORQUE BOX WEB, STA 1283, RBL 27.8, WL 201.3. REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 19950616004191995061600419NM 1995 6 16 UPS203534 119950613A5330 SKIN BOEING727 72722C 138400FNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN INNER SURFACE AT THE AFT LOWER CORNER OF THE RT AFT EMERGENCY EXIT. REPAIRED IAW SRM 53-30-3. 2L73 4F A3WE 19950616004201995061600420NM 1995 6 16 UPS203535 119950613A5751 SKIN BOEING727 72722C 138400FNM RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED SKIN ON THE LOWER I/B SIDE OF RT AILERON. REPAIRED IAW SRM 57-50-5. 2L73 4F A3WE 19950616004211995061600421NM 1995 6 16 UPS203536 119950613A7110652368723 ENGINE RING BOEING727 72722C 138400FNM FS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND ENGINE RING CORRODED AT STA 1342. REPLACED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950616004221995061600422NM 1995 6 16 UPS203537 119950613A5347 SEAT TRACK BOEING727 72722C 138400FNM FS 598-603 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND MAIN CABIN SEAT TRACK CRACKED, STA 598-603, LBL 48. INSTALLED FABRICATED PARTS IAW SRM 51-30-2, 53-10-5. 2L73 4F A3WE 19950616004231995061600423NM 1995 6 16 UPS203538 119950613A5320 ANGLE BOEING727 72722C 138400FNM FS 1342 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN C-CHECK, MAINTENANCE FOUND LT SKIN SUPPORT ANGLE CRACKED AT F.S. 1345. INSTALLED FABRICATED PARTS IAW SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950616004241995061600424NM 1995 6 16 UPS403560 119950614A7331 FUEL FLOW MODULE BOEING747 747121 1384871NM NR 2 MALFUNCTIONED A IPXAO OTHER O OTHER CRCRUISE 1 SO01682UP 20349 WHILE EN ROUTE TO EWR FROM CGN AT FL 350 .84M APPROXIMATELY 5 HOURS INTO FLIGHT, THE NR 2 FUEL FLOW CIRCUIT BREAKER POPPED ACCOMPANIED BY AN ACRID BURNING SMELL FROM THE P6 PANEL. CREW ELECTED NOT TO RESET. FUEL FLOW MODULE REMOVED AND REPLACED IAW M/M 73-31-02. 2L74 4F A20WE 19950616004251995061600425WP 1995 6 16 UPS803539 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 677 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER L/E RIB CRACKED AT STA XFS 677.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004261995061600426WP 1995 6 16 UPS803540 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 607 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 607.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004271995061600427WP 1995 6 16 UPS803541 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 593 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 593.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004281995061600428WP 1995 6 16 UPS803542 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 770 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 770.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004291995061600429WP 1995 6 16 UPS803543 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 770 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 777.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004301995061600430WP 1995 6 16 UPS803544 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 720 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 720.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004311995061600431WP 1995 6 16 UPS803545 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 727 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 727.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004321995061600432WP 1995 6 16 UPS803546 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 734 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 734.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004331995061600433WP 1995 6 16 UPS803547 119950613A5712 RIB DOUG DC8 DC871F 302199DWP WS 748 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING UPPER L/E RIB CRACKED AT STA XFS 748.0. REPAIRED IAW M/M 57-00-00. 2L74 4F RT4A25 19950616004341995061600434WP 1995 6 16 UPS803548 119950613A5720576985938G INTERCOSTAL DOUG DC8 DC871F 302199DWP WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT L/E O/B OF AUX TANK, UPPER INTERCOSTAL ANGLE CRACKED. INSTALLED FABRICATED PARTS IAW SRM 51-1-21, 51-1-30. 2L74 4F RT4A25 19950616004351995061600435WP 1995 6 16 UPS803549 119950613A5751 SKIN DOUG DC8 DC871F 302199DWP LT AILERON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT I/B AILERON, O/B END TOP SKIN DAMAGED. REPAIRED IAW SRM 51-1-21, 51-1-8. 2L74 4F RT4A25 19950616004361995061600436WP 1995 6 16 UPS803550 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 784 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER RIB AT STA. XFS 784.00 CRACKED. REPAIRED IAW SRM 57-00-00, 51-01-8. 2L74 4F RT4A25 19950616004371995061600437WP 1995 6 16 UPS803551 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 747.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 747.50 CRACKED. REPAIRED IAW SRM 57-00-00, 51-1-21. 2L74 4F RT4A25 19950616004381995061600438WP 1995 6 16 UPS803552 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 795.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT WING L/E UPPER RIB AT STA. XFS 795.5 CRACKED. REPAIRED IAW SRM 51-1-20, 51-1-21. 2L74 4F RT4A25 19950616004391995061600439WP 1995 6 16 UPS803553 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 803.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 803.75 CRACKED. REPAIRED IAW SRM 57-00-00, 51-1-21. 2L74 4F RT4A25 19950616004401995061600440WP 1995 6 16 UPS803554 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 847.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 847.50 CRACKED. REPAIRED IAW SRM 51-01-8, 51-1-21. 2L74 4F RT4A25 19950616004411995061600441WP 1995 6 16 UPS803555 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 778.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 778.25 CRACKED. REPAIRED IAW SRM 51-1-21. 2L74 4F RT4A25 19950616004421995061600442WP 1995 6 16 UPS803556 119950613A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 316.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT WING L/E UPPER RIB AT STA. XFS 316.5 CRACKED. REPAIRED IAW SRM 57-00-00. 2L74 4F RT4A25 19950616004431995061600443WP 1995 6 16 UPS803557 119950613A5751 TE SKIN DOUG DC8 DC871F 302199DWP RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND LT O/B AILERON T/E HAS SMALL CRACK EXTENDING TO FASTENER HOLE. REPAIRED IAW SRM 57-8-1, 51-1-21. 2L74 4F RT4A25 19950616004441995061600444WP 1995 6 16 UPS803558 119950613A5751 TE SKIN DOUG DC8 DC871F 302199DWP RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND RT O/B AILERON T/E HAS CRACK. REPAIRED IAW SRM 57-8-1, 51-1-21. 2L74 4F RT4A25 19950616004451995061600445WP 1995 6 16 UPS803559 119950613A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP FS 88 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON VERTICAL INTERCOSTAL AT BOTTOM END OF COCKPIT SUB FLOOR AT STA. 80, RBL 56. REPAIRED IAW SRM 51-1-20, 51-3-1. 2L74 4F RT4A25 19950616004461995061600446WP 1995 6 16 UPS803561 119950613A3260 DOOR LIGHT DOUG DC8 DC871F 302199DWP LANDING GEAR ILLUMINATED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01703UP 45939 DURING CLIMB OUT TO BOS FROM SDF, DOORS NOT LATCHED LIGHT CAME ON DURING GEAR RETRACTION. CREW RAN APPROPRIATE CHECKLIST, CYCLED GEAR TWICE, LIGHT WENT OUT. MAINTENANCE NOTED COMMENT. 2L74 4F RT4A25 19950616004471995061600447WP 1995 6 16 UPS803562 119950615A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP FS 340-380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND NR 1 SEAT TRACK CORRODED F.S. 340-380. REPLACED IAW SRM 53-2-3. 2L74 4F RT4A25 19950616004481995061600448WP 1995 6 16 UPS803563 119950615A531155603501 FRAME DOUG DC8 DC873F 302199FWP FS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME F.S. 1240, LONGERON 36. REPAIRED IAW SRM 53-2-0,51-1-20D. 2L74 4F RT4A25 19950616004491995061600449WP 1995 6 16 UPS803564 119950615A531397585041 LONGERON DOUG DC8 DC873F 302199FWP FS 1220 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L F.S. 1220. REPAIRED IAW SRM DC8-5310-7070A. 2L74 4F RT4A25 19950616004501995061600450WP 1995 6 16 UPS803565 119950615A5320 FITTING DOUG DC8 DC873F 302199FWP FS 1175 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING BETWEEN LONGERONS 33A-33B RT, F.S. 1175. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004511995061600451WP 1995 6 16 UPS803566 119950615A532037558411 FITTING DOUG DC8 DC873F 302199FWP FS 1220 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING AT F.S. 1220, LONGERONS 34R-33R. REPLACED IAW SRM 53-2-0. 2L74 4F RT4A25 19950616004521995061600452WP 1995 6 16 UPS803567 119950615A53204640162 FITTING DOUG DC8 DC873F 302199FWP FS 1400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING F.S. 1400, LONGERON 21R. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004531995061600453WP 1995 6 16 UPS803568 119950615A5347S2772660 SEAT TRACK DOUG DC8 DC873F 302199FWP FS 70-120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BOTTOM OF SEAT TRACK NR 9 F.S. 70-120, RT SIDE. REPLACED IAW SRM 53-02-03. 2L74 4F RT4A25 19950616004541995061600454WP 1995 6 16 UPS803569 119950615A53203754047506 FITTING DOUG DC8 DC873F 302199FWP FS 1346 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CUSP FITTING F.S. 1346, LONGERON 21L. REPLACED IAW SRM 51-3-0. 2L74 4F RT4A25 19950616004551995061600455WP 1995 6 16 UPS803570 119950615A53203754047506 CHANNEL DOUG DC8 DC873F 302199FWP FS 1395 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF CHANNEL, F.S. 1395, LONGERON 35R. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950616004561995061600456WP 1995 6 16 UPS803571 119950615A53205754739 ANGLE DOUG DC8 DC873F 302199FWP FS 330 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ATTACH ANGLE, LONGERON 21R, F.S. 330. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004571995061600457WP 1995 6 16 UPS803572 119950615A532037558432N FITTING DOUG DC8 DC873F 302199FWP FS 1160 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BATH TUB FITTING BETWEEN LONGERONS 35R-36, F.S. 1160. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004581995061600458WP 1995 6 16 UPS803573 119950615A53204758514509 FITTING DOUG DC8 DC873F 302199FWP FS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING I/B SIDE OF LONGERON 33A, RT F.S. 1240. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004591995061600459WP 1995 6 16 UPS803574 119950615A53139754913 LONGERON DOUG DC8 DC873F 302199FWP FS 280-300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R F.S. 280-300. REPAIRED IAW SRM 53-2-2, 51-1-20D. 2L74 4F RT4A25 19950616004601995061600460WP 1995 6 16 UPS803575 119950615A53115722958 FRAME DOUG DC8 DC873F 302199FWP FS 1060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON AFT BAG BIN ON TOP OF BELT FRAME B.S. 1060, LONGERONS 35L AND 35R. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950616004611995061600461WP 1995 6 16 UPS803576 119950615A53132597742 LONGERON DOUG DC8 DC873F 302199FWP FS 80-145 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32R, F.S. 80-145. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004621995061600462WP 1995 6 16 UPS803577 119950615A53209754011 DOUBLER DOUG DC8 DC873F 302199FWP FS 220-260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER F.S. 220-260, LONGERONS 32R-35L. REPLACED IAW SRM 51-1-20D, SRM 51-1-21. 2L74 4F RT4A25 19950616004631995061600463WP 1995 6 16 UPS803578 119950615A53203754930 FITTING DOUG DC8 DC873F 302199FWP FS 1180/1190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FITTING F.S. 1180 AND F.S. 1190 BETWEEN LONGERONS 33A-33B, RT SIDE. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004641995061600464WP 1995 6 16 UPS803579 119950615A53203759258 FITTING DOUG DC8 DC873F 302199FWP FS 1270 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON SPLICE FITTINGS AT F.S. 1270, LONGERONS 35L AND 35R. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004651995061600465WP 1995 6 16 UPS803580 119950615A53203755172 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON 3RD AND 4TH T-LOCK FITTINGS END OF C X-SLIDE DOOR. REPLACED FITTINGS IAW SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 19950616004661995061600466WP 1995 6 16 UPS803581 119950615A533057503223 SKIN DOUG DC8 DC873F 302199FWP FS 1050-1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN F.S. 1050-1350. REPLACED SKIN IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004671995061600467WP 1995 6 16 UPS803582 119950615A53205643483501 FITTING DOUG DC8 DC873F 302199FWP FS 878 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME ATTACH FITTING LT STA. 878. REPAIRED IAW E.O. DC8-5310-7069-A. 2L74 4F RT4A25 19950616004681995061600468WP 1995 6 16 UPS803583 119950615A533057799253 SKIN DOUG DC8 DC873F 302199FWP FS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN STA 70-190. REPLACED SKIN IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004691995061600469WP 1995 6 16 UPS803584 119950615A533057552713 SKIN DOUG DC8 DC873F 302199FWP FS 240-260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION BULGE AT F.S. 240-260, LONGERON 35L. REPAIRED IAW DC8-5330-7046-A. 2L74 4F RT4A25 19950616004701995061600470WP 1995 6 16 UPS803585 119950615A53204641324N FITTING DOUG DC8 DC873F 302199FWP FS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING F.S. 1690, LONGERON 36 AFT SIDE. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950616004711995061600471WP 1995 6 16 UPS803586 119950615A5330561537285 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01812UP 46112 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN UNDER D BAGG IN SCUFF PLATE. REPAIRED IAW DC8-5330-7108-A. 2L74 4F RT4A25 19950616004851995061600485EA 1995 6 16 95ZZZX3009 219950601A855061174 SHAFT CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA OIL PUMP DEFECTIVE A AGNMAK NONE O OTHER ININSP/MAINT 1 SW015209R2500 17263426 L3807827A REMOVED ACCESSORY CASE TO CHECK COMPLIANCE WITH AD 81-18-04 OIL PUMP GEARS. LOG BOOKS NON-SPECIFIC. FOUND OIL PUMP DRIVING GEAR AND SHAFT WITH SHEARED WOODRUFF KEY. OIL PUMP ASSEMBLY ON VERGE OF COMPLETE FAILURE. PUMP HOUSING BADLY DAMAGED. ENGINE MANUFACTURER RECOMMENDS REPLACING OIL PUMP GEARS AT ENGINE OVERHAUL, 2,000 HRS, AND MAKING DETAILED, SPECIFIC LOG BOOK ENTRY. 1H71 3O3 ONT3A12 E274 19950616004861995061600486EA 1995 6 16 95ZZZX3010 219950601A855060746 GEAR CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA OIL PUMP DEFECTIVE A GNMAK NONE O OTHER ININSP/MAINT 1 SW015209R2500 17263426 L3807827A REMOVED ACCESSORY CASE TO CHECK COMPLIANCE WITH AD 81-18-04 OIL PUMP GEARS. LOG BOOKS NON-SPECIFIC. FOUND OIL PUMP DRIVING GEAR AND SHAFT WITH SHEARED WOODRUFF KEY. OIL PUMP ASSEMBLY ON VERGE OF COMPLETE FAILURE. PUMP HOUSING BADLY DAMAGED. ENGINE MANUFACTURER RECOMMENDS REPLACING OIL PUMP GEARS AT ENGINE OVERHAUL, 2,000 HRS, AND MAKING DETAILED, SPECIFIC LOG BOOK ENTRY. 1H71 3O3 ONT3A12 E274 19950616004871995061600487CE 1995 6 16 95ZZZX3011 119950106A2810M913 CELL CESSNA182 182B 2072706CE SUPPLY NIPPLE LEAKING A GNFAK NONE K FLUID LOSS ININSP/MAINT 1 SW012496G 51796 SECOND REPORT - FOLLOW-UP TO 21 MAY REPORT. RT FUEL CELL FOUND TO HAVE A SMALL LEAK IN AND AROUND MAIN FUEL SUPPLY NIPPLE. FUEL CELL REPLACED AND CORE SENT IN FOR INSPECTION. LEAK COMING FROM NIPPLE BONDING PATCH SEALING COMPOUND. 1H71 3O NT3A13 19950616004881995061600488CE 1995 6 16 95ZZZX3012 119950509A5312054112111 BULKHEAD CESSNA182 182B 2072706CE LT MLG ATTACH CRACKED A GNFAK NONE O OTHER ININSP/MAINT 1 SW012496G2941 51796 FORWARD OF BULKHEAD CRACK FOUND - UNKNOWN ORIGIN. CRACK FOUND DURING ANNUAL INSPECTION OF LT MLG OUTB THROUGH-BOLT. 1H71 3O NT3A13 19950623000011995062300001NM 1995 6 23 9509465533 119950615A26112156204A SMOKE DETECTOR BOEING757 757251 1384970NM E/E BAY FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01533US1872818728 24264 DURING CLIMB, THE SMOKE LIGHT CAME ON FOLLOWED BY EQUIPMENT OVERHEAT FIVE MINUTES LATER. DECISION WAS MADE TO RETURN WHEN THE FLIGHT INSTRUMENTS WENT DIM. EQUIPMENT OVERHEAT LIGHT WENT OUT WHEN ALTERNATE SYSTEM WAS USED. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 AND NR 2 FORWARD EQUIPMENT SMOKE DETECTORS. ALL SYSTEMS CHECKED NORMAL. 2L72 4F RTA2NM 19950623000021995062300002NM 1995 6 23 9509476635 119950604A5210 FRAME BOEING747 747227B 1384888NM DOOR 4R CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL016635U 15402 21682 DURING FLIGHT NRT-BKK, THE PILOT REPORTED A LOUD HISSING SOUND AT DOOR 4R DURING CRUISE. CONTINUED TO BKK WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AND REPAIRED A 14 INCH CRACK IN THE DOOR FRAME (P/N 65B04311-16), LOWER FORWARD CORNER PER SRM 52-10-02. 2L74 4F A20WE 19950623000031995062300003NM 1995 6 23 9509482288 119950612A5330 SKIN BOEING727 727251 138408HNM FS 320 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US 21376 DURING LINE CHECK, FOUND A 6 INCH CRACK IN THE FUSELAGE SKIN AT APPROXIMATELY FS 320, RIGHT SIDE AFT OF FORWARD LAV SERVICE PANEL. REPAIRED PER SRM 53-30-3 FIG 3A. 2L73 4F A3WE 19950623000041995062300004WP 1995 6 23 9509499995 119950612A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE AFT CARGO DOOR FORWARD AND AFT NR 1 BEAM END FITTINGS. REPLACED THE FITTINGS (P/N 3914025-501 AND -502) PER SRM 57-30-5. 2L72 4F A6WE 19950623000051995062300005NM 1995 6 23 95UAL900000 119950616A7931 OIL PRESS SW CUSTOM COMPO42D107A1 BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP299011U 19049 649085 A/C RETURNED TO ICT, WITH NR 2 OIL BYPASS LIGHT ON AND ENGINE POWER REDUCED TO IDLE. REPLACED OIL PRESSURE DIFFERENTIAL SWITCH. 2L72 4F4 F A16WE E2EA 19950623000061995062300006NM 1995 6 23 95UAL900001 119950616A5230 DOOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO COMPT NOT SECURE A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29309UA 23670 RETURNED TO FIELD WITH CARGO DOOR WARNING LIGHT. FOUND FORWARD CARGO DOOR NOT FULLY SECURED. 2L72 4F4 FRTA16WE E2GL 19950623000071995062300007NM 1995 6 23 95UAL900002 119950616A3233 ACTUATOR 654482517 BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE RT MLG FAILED A UALAO OTHER J WARNING INDICATION APAPPROACH 1 WP29987UA 21749 RIGHT MAIN GEAR WOULD NOT EXTEND, CREW HAD TO USE MANUAL EXTENSION. REPLACED RT MLG ACTUATOR. FOUND ACTUATOR ROD END BROKEN. 2L72 4F4 F A16WE E2EA 19950623000081995062300008NE 1995 6 23 95UAL900003 219950616A726050R492 CHIP DETECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE NR 2 ENGINE FELL OUT A UALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP29649UA 25286 727402 RETURNED TO FIELD WITH NR 2 ENGINE SHUTDOWN, DUE TO LOW OIL QUANTITY. FOUND CHIP DETECTOR LYING IN COWL. CHANGED PROCEDURES TO REQUIRE LOCKWIRE OF THESE CHIP DETECTORS. 2L72 4F4 FRTA1NM E24NE 19950623000091995062300009NM 1995 6 23 DL72S952619 119950610A5754 SKIN BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 ON WALK-AROUND FOUND CRACKS IN NR 5 KRUGER FLAP. CRACKS WERE REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19950623000101995062300010WP 1995 6 23 DLL10952620 119950609A57551529102178 SPAR LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A ADALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO11723DA 193C1150 ON DESCENT WITH FLAPS UP AND SPEED BRAKE LEVER PULLED FULL AFT, THE 2R SPOILER ONLY COMES UP TO TOP OF DLC RANGE. AIRPLANE TRIES TO ROLL LEFT, NEEDED ABOUT 30 DEGREES RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FOUND 2R SPOILER WITH ACTUATOR ATTACH FITTING CRACKED AT UPPER END OF FITTING. THE SPOILER MAIN FWD SPAR WAS FOUND CRACKED IN THE UPPER RADIUS AT THE ACTUATOR AND RUNNING DIAGONALLY DOWN TO THE LOWER RADIUS OF THE SPAR AND EXTENDING 18 ON BOTH SIDES OF THE ACTUATOR FITTING. THE SPOILER WAS REPLACED AND ROUTED TO SHOP FOR REPAIRS. 2L73 4F A23WE 19950623000111995062300011NM 1995 6 23 SCNA95129 119950609A33501000677 EEL BOEING727 727259 138408JNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 FOUND AFT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-101 PAGE 201. OPS CHECKED GOOD. 2L73 4F A3WE 19950623000121995062300012NM 1995 6 23 SCNA95130 119950613A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 222559 FOUND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, LIGHT OPS CHECKED NORMAL. 2L73 4F A3WE 19950623000131995062300013NM 1995 6 23 SCNA95131 119950613A335020131 EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 222559 FOUND THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND TRACK LIGHTING TESTED GOOD. 2L73 4F A3WE 19950623000141995062300014NM 1995 6 23 SCNA95132 119950612A25308001070000 OVEN BOEING727 727259 138408JNM AFT GALLEY SMOKING A SCNAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL15289SC 22475 DURING CLIMB FROM LAS, AFT OVEN STARTED SMOKING. FLIGHT ATTENDANT TURNED OFF OVEN AND SMOKE STOPPED. DURING INSPECTION OF OVEN, FOUND NO EVIDENCE OF FIRE. FOUND CLEANING SOLVENT ON OUTBOARD OVEN HEATING COILS. CLEANED COILS AND TESTED OVENS PER MM 25-20-00, OVENS TESTED GOOD. 2L73 4F A3WE 19950623000151995062300015WP 1995 6 23 SCNA95133 119950612A2560119821001 LIGHT MODULE DOUG DC10 DC1010 3022110WP R4 DOOR SLIDE FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15907WA 46946 FOUND THE R4 DOOR SLIDE INTEGRITY TEST INOPERATIVE. REMOVED AND REPLACED LIGHT MODULE AND BATTERY HOLDER, SLIDE TESTED GOOD. 2L73 4F A22WE 19950623000161995062300016WP 1995 6 23 SCNA95134 119950613A2560119821001 INDICATOR DOUG DC10 DC1010 3022110WP R2 DOOR SLIDE FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46645 FOUND THE R2 DOOR SLIDE INTEGRITY TEST INOPERATIVE. REMOVED AND REPLACED THE R2 DOOR SLIDE LIGHT INDICATOR, LIGHT TESTED GOOD. 2L73 4F A22WE 19950623000181995062300018SW 1995 6 23 95ZZZX3017 119950504A7800209062534003 VENT FITTING BELL 412 412 1182202SW NR 2 ENG EXH DEPARTED ASAHEEAA UNSCHED LANDING ED VIBRATION/BUFFET INFLIGHT SEPARATION CRCRUISE 1 SW033893N 33010 AIRCRAFT WAS EN ROUTE TO AN OFFSHORE PLATFORM WHEN THE PILOT IN COMMAND HEARD A MUFFLED POP FOLLOWED BY A VIBRATION TO THE AIRCRAFT AND ITS CONTROLS. THE PILOT THEN RETURNED TO BASE. INSPECTION OF THE AIRCRAFT BY MAINTENANCE PERSONNEL AFTER THE FLIGHT REVEALED THAT STAINLESS STEEL VENT FITTING ON NR 2 ENGINE EXHAUST EJECTOR BELL PN 209-062-534-003, FIGURE 71-3, INDEX 37, CAME LOOSE DURING FLIGHT CAUSING DAMAGE TO TWO OF THE FOUR MAIN ROTOR BLADES AND THE TAIL ROTOR BLADES. 1G72 4U H4SW 19950623000351995062300035NM 1995 6 23 ASAA9540021 119950506A5210507945178 L1 DOOR BOEING737 7374Q8 NM FWD CABIN LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01779AS3568 25111 ANC - PILOT REPORT - FORWARD ENTRY DOOR DIFFICULT TO CLOSE AND MAKES CREAKING NOISE DURING LAST FEW INCHES UNTIL CLOSED. MAINTENANCE GREASED, VISUALLY INSPECTED AND OPS CHECKED OKAY. (X) 2L72 4F RTA16WE 19950623000561995062300056NE 1995 6 23 PLGA51951 319950122A6111 PROP BLADES SAAB SF340 SF340A 7850100EU ROTOL R389 R3894123F25 NE NR 1 BLADE LOOSE A APLGAO OTHER O OTHER NRNOT REPORTED 1 NE05342BE12631 340A096 DR6942886 ON JANUARY 22, 1995, PROPELLER ASSY WAS REMOVED FOR PROP DE-ICE FAILURE ON THE NR 1 BLADE. AFTER REMOVAL OF THE BAD DE-ICE BOOT, MOVEMENT WAS NOTED BETWEEN THE OUTER SLEEVE AND THE COMPOSITE MATERIAL. ALL BLADES WERE THEN INSPECTED AND 2 MORE BLADES WERE FOUND TO HAVE MOVEMENT. NO MOVEMENT IS ALLOWED IN THE AREA PER DOWTY CMM 61-10-36. THE PROPELLER WAS TAKEN OUT OF SERVICE AND SENT TO DOWTY AEROSPACE FOR INSPECTION. THE SUBSEQUENT DISASSEMBLY INSPECTION VERIFIED THE REMOVAL REASON. 2L72 4T RTA52EU 6 CP30NE 19950623000571995062300057NM 1995 6 23 95ZZZX3054 119950604A324626019011 WHEEL BOEING747 747121 1384871NM NR 6 TIRE FAILED A P5CAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 WP23832FT 382 20347 GRU - DURING TAKEOFF AT V1, MASTER FIRE WARNING LIGHTS AND WW FIRE WARNING ILLUMINATED. CONTINUED TAKEOFF. UNABLE TO RETRACT BODY GEAR AND WW DOOR WARNING LIGHT REMAINED ILLUMINATED, THEN THE NR 1 HYDRAULIC SYSTEM QUANTITY WARNING LIGHT CAME ON. AFTER FUEL JETTISON, RETURNED TO GRU. INITIAL GROUND INSPECTION REVEALED DAMAGE TO NR 1 HYDRAULIC SYSTEM PLUMBING, APU PNEUMATIC DUCT, LT BODY GEAR WW DOOR AND NR 6 ML6 TIRE BLOWN. REPLACED WHEEL AND TIRE ASSEMBLIES NR 6 AND NR 7, DAMAGED HYDRAULIC LINES, APU PNEUMATIC DUCT, WHEELWELL FIRE LOOP, BROKEN ROD AND REPAIRED DOOR. INSPECTED WHEELWELL PRESSURE WEB, NO DISCREPANCIES. 2L74 4F A20WE 19950623000581995062300058NM 1995 6 23 95ZZZX3055 119950530A5414 SKIN BOEING747 747122 1384872NM NR 3 PYLON LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS PER BOEING SRM 51-30-02. AIRCRAFT TOTAL TIME: 69560. AIRCRAFT TOTAL CYCLES: 17553. 2L74 4F A20WE 19950623000591995062300059NE 1995 6 23 95ZZZX3056 219950511A8530327627 PISTON DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 ENG NR 18 RING FAILURE A NACAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03313RS 1106 44663 35358 FLT 40 - SHUT DOWN NR 3 ENGINE DUE TO BACKFIRING AND RUNNING ROUGH AT 2145Z. MAINTENANCE REPLACED NR 18 CYLINDER DUE PISTON RING LAND FAILURE. 2L74 4R4 R 6A3 E264 19950623000601995062300060NE 1995 6 23 95ZZZX3057 219950505A8530327627 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 4 ENG NR 2 CRACKED A NACAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AL032907F 392 44636 31966 FLT 20 - SHUT DOWN NR 4 ENGINE DUE TO LOSS OF BMEP AT 1752Z ON CLIMB-OUT AND ROUGH RUNNING ENGINE. MAINTENANCE REPLACED NR 2 CYLINDER DUE TO CRACKED HEAD. 2L74 4R4 R 6A3 E264 19950623000611995062300061NE 1995 6 23 95ZZZX3059 219950420A8530327627 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 ENG NR 8 CRACKED A NACAA UNSCHED LANDING O OTHER CRCRUISE 1 AL032907F 1133 44636 510318 ANC - FLT 80 - RETURNED TO ANC DUE TO NR 3 ENGINE BACKFIRED IN CRUISE. REPLACED NR 8 CYLINDER DUE TO CRACKED HEAD. 2L74 4R4 R 6A3 E264 19950623000621995062300062NE 1995 6 23 95ZZZX3060 219950502A8530327628 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 1 ENG NR 7 CRACKED A CALAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 SW092907F 1018 44636 36323 FLT 80 - SHUT DOWN NR 1 ENGINE AT 2207Z DUE TO RUNNING ROUGH. REPLACED NR 4 CYLINDER DUE TO CRACKED HEAD. 2L74 4R4 R 6A3 E264 19950623000631995062300063NE 1995 6 23 95ZZZX3061 219950405A8530327628 CYLINDER DOUG DC6 DC6B 3021712WP PWA R2800 CB3 52026NE NR 4 ENG NR 3 CRACKED A NACAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AL03434TA 663 44434 31026 FLT 690 - SHUT DOWN NR 4 ENGINE DUE TO BACKFIRING. REPLACED NR 3 CYLINDER. 2L74 4R4 R 6A4 E264 19950623000641995062300064NE 1995 6 23 95ZZZX3062 219950523A8530223113 ROCKER ASSY DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 1 ENGNR 10CYLBROKEN A NACAER ENGINE SHUTDOWN AUTOROTATION E VIBRATION/BUFFET CRCRUISE 1 AL032907F 1987 44636 30608 FLT 80 - SHUT DOWN NR 1 ENGINE DUE TO CONTINUOUS BACKFIRING IN AUTO RICH AT 1827Z. MAINTENANCE REPLACED BROKEN EXHAUST VALVE ROCKER ASSY AND PUSHROD ON NR 10 CYLINDER. 2L74 4R4 R 6A3 E264 19950623000651995062300065NE 1995 6 23 95ZZZX3063 219950523A8530327627 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 14 CYL NR 3 RING FAILURE A NACACD ABORTED TAKEOFF RETURN TO BLOCK ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL034213X 1348 44605 28818 OTZ - FLT 43 - ABORTED TAKEOFF FROM OTZ DUE TO NR 3 ENGINE BACKFIRING. MAINTENANCE REPLACED NR 14 CYLINDER DUE TO RING LAND FAILURE. 2L74 4R4 R 6A3 E264 19950623000661995062300066EU 1995 6 23 95ZZZX3064 119950602A3234D49412001 SELECTOR SAAB SF340 SF340A 7850100EU MLG FAILURE A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23125CH 3070590 340A125 AIRCRAFT RETURNED TO FIELD DUE TO GEAR WOULD NOT RETRACT WITHOUT THE USE OF OVERRIDE. THE SYSTEM WAS TROUBLESHOT AND THE LANDING GEAR SELECTOR WAS FOUND TO BE THE PROBLEM. THE UNIT WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. 2L72 4T RTA52EU 19950623000671995062300067NE 1995 6 23 95ZZZX3065 219950530A75325056T88P01 VALVE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT NACELLE INTERMITTENT A CHQAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 EA23360CA AEX10386 340A006 AIRCRAFT RETURNED TO FIELD DUE TO RIGHT BLEED CLOSE LIGHT DID NOT ILLUMINATE WHEN SELECTED CLOSED. THE SYSTEM WAS TROUBLESHOT AND THE RIGHT BLEED SHUT-OFF VALVE WAS DETERMINED TO BE THE PROBLEM. THE VALVE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. 2L72 4T4 TRTA52EU E8NE6 19950623000681995062300068NM 1995 6 23 95ZZZX3066 119950517A33502410070 EEL CHARGER BOEING727 727264 138408MNM CABIN FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11763AT 023960 22983 IND - RIGHT OVERWING EXIT LIGHTS INOPERATIVE (EMERGENCY). REPLACED BATTERY CHARGER - OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950623000691995062300069NM 1995 6 23 95ZZZX3067 119950428A5314 BEAM BOEING727 727227 1384078NM FUSELAGE CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11768AT 21996 BFM - RT AND LT KEEL BEAMS, STA 950 - STA 1010, HAS CORROSION AROUND FASTENERS HOLES, ENTIRE LENGTH (AFT CARGO BAY). REMOVED AND REPLACED LT/RT KEEL BEAM CHORDS PER SB 727-53-0179. 2L73 4F A3WE 19950623000701995062300070NE 1995 6 23 95ZZZX3068 219950426A72007121000 ENGINE BOEING757 757212 NM PWA 2037 PW2037 NE NR 2 OVERTEMP A AMTAK NONE M OVER TEMP TOTAKEOFF 1 GL11757AT202555446 23127 716315 SNN- NR 2 ENGINE EXCEEDED EGT LIMIT 652 DEGREES CELSIUS FOR 20 SECONDS. AREA 'A' ON OVERHEAT CHART. DID NOT OCCUR DURING SURGE. REMOVED AND REPLACED NR 2 ENGINE IAW M57-71-01. 2L72 4F4 FRTA2NM E17NE 19950623000711995062300071NE 1995 6 23 95ZZZX3069 219950418A73217791005 FUEL CONTROL BOEING757 757212 NM RROYCERB211 RB211535E43754555NE LT ENGINE FAILED A AMTAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 GL11751AT 6086 0A4124 23125 LAX - IN-FLIGHT ENGINE FAILURE (LT ENGINE). REMOVED AND REPLACED LT ENGINE FUEL CONTROL UNIT. ENGINE RUN-UP CHECK OKAY. 2L72 4F4 FRTA2NM E12EU 19950623000721995062300072 1995 6 23 95ZZZX3070 419950502A34603420038 FM COMPUTER BOEING757 757212 NM RT SYSTEM FAILED A AMTAK NONE J WARNING INDICATION DEDESCENT 1 GL11757AT 080255 23127 EICAS MSG - RIGHT FMC FAIL DISPLAYED. DEFERRED PER MEL 34-61-1. S/D REMOVED AND REPLACED RT FMC. OPS CHECK NORMAL. 2L72 4F RTA2NM 19950623000731995062300073NM 1995 6 23 95ZZZX3071 119950522A3350 EEL POWER SUPPLY BOEING757 7572Q8 1384972NM AFT CABIN FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11755AT 24965 MDW - ON DAILY SERVICE CHECK, FOUND AFT AISLE LIGHTS (EMERGENCY) WOULD NOT ILLUMINATE. REMOVED AND REPLACED AFT POWER SUPPLY PER 33 IN MM. OPS CHECK GOOD. 2L72 4F RTA2NM 19950623000741995062300074NE 1995 6 23 95ZZZX3072 219950520A73147320092 FUEL PUMP BOEING757 757212 NM RROYCERB211 RB211535E43754555NE ENGINE NR 1 LEAKING A AMTAK NONE K FLUID LOSS ININSP/MAINT 1 GL11751AT 000267 23125 DTW - ON A CHECK, FOUND FUEL LEAK FROM NR 1 ENGINE FUEL PUMP PAD SEAL DRAIN. REMOVED AND REPLACED NR 1 FUEL PUMP IAW MM73-11-01. OPS CHECK GOOD. NO LEAKS NOTED. 2L72 4F4 FRTA2NM E12EU 19950623000751995062300075WP 1995 6 23 95ZZZX3073 119950521A3340 FLASHER UNIT LKHEED1011 10113851 5265010WP GALLEY AREA DEFECTIVE A AMTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11189AT 193C1081 SFO - APPROXIMATELY 30 MINUTES PRIOR TO DESCENT, A STRONG SMELL RESEMBLING BURNING INSULATION APPEARED IN THE LOWER GALLEY. AFTER ALL GALLEY POWER REMOVED ODOR DISAPPEARED. FOUND STROBE LIGHT FLASHER UNIT PRODUCING SMELL. PLACED GALLEY POWER ON BUSES 1, 2, 3, NO ODOR NOTED. NO PARTS REPLACED. 2L73 4F A23WE 19950623000761995062300076WP 1995 6 23 CAL950416 119950524A217017946081 SEPARATOR DOUG DC9 DC982 3022082WP L&R AIR COND SYSFROZEN SHUT A ACALAGO O2 MASK DEPLOYED OTHER O OTHER CRCRUISE 1 SW091488920022 49118 IAH - FLT 0108 - THE AIRCRAFT STARTED LOSING PRESSURE AT 37,000 FEET WITH DE-ICING ON, AND OXYGEN MASKS WERE DROPPED MANUALLY. CREW ATTEMPTED SECONDARY WHICH INDICATED FAILURE, SO SWITCHED BACK TO PRIMARY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE OBSERVED SEVERAL OXYGEN MASKS HAD NOT DEPLOYED. BOTH LEFT AND RIGHT WATER SEPARATOR PRESSURE RELIEF PLUNGERS WERE FOUND FROZEN SHUT UPON INSPECTION OF AIR CONDITIONING SYSTEM. BOTH WATER SEPARATOR ASSEMBLIES REMOVED AND REPLACED. MASK RELEASE SOLENOID AT AFT GALLEY ATTENDANT SEAT FOUND SHORTED. SOLENOID REPLACED. THE USED OXYGEN GENERATORS ALSO REPLACED. ACFT PRESSURIZATION CHKS AND FUNCTIONAL TEST OF OXYGEN SYSTEM WERE GOOD. (X) 2L72 4F A6WE 19950623000771995062300077WP 1995 6 23 CAL950419 119950525A7920 LINE DOUG DC9 DC982 3022082WP OIL PRESS SWITCHCRACKED A CALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW09819NY 49479 LAS - FLT 0724 - THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED, ACCOMPANIED BY A LOSS OF OIL WHILE IN-FLIGHT. THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LINE TO LOW OIL PRESSURE SWITCH CRACKED. THE LINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A6WE 19950623000781995062300078NM 1995 6 23 CAL950422 119950525A5753651859923 CARRIAGE BOEING727 727224 1384076NM MIDFLAP, I/B BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW099373812624 20666 EWR - MAINTENANCE FOUND LT MID-FLAP INBOARD CARRIAGE BROKEN. THE LT MID-FLAP INBOARD CARRIAGE WAS REMOVED AND REPLACED IAW MM 27-51-3 AND OPERATION CHECKED GOOD. (X) 2L73 4F A3WE 19950623000791995062300079NM 1995 6 23 CAL950425 119950526A2910 LINE BOEING727 727225 1384077NM HYD BAY B-SYS WORN THROUGH A CALAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW098885Z 21854 EWR - FLT 0376 - THE CREW REPORTED B-SYSTEM HYDRAULIC QUANTITY LOSS IN-FLIGHT. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF B-PUMP LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE TO B-SYSTEM MODULE IN THE HYDRAULIC BAY WORN THROUGH. THE RIGID LINE WAS REPLACED USING TWO FLEX LINES AND A DIP WAS ISSUED TO REPLACE THE FLEX LINES WITHIN 1200 HOURS OR 500 FLIGHTS. IN ADDITION, BOTH B-SYSTEM ELECTRIC HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950623000801995062300080EU 1995 6 23 CAL950426 219950529A75301555M23G01 DUCT ASSY AIRBUS300 A300B4103 3930104EU NR 1 ENG,14 STG RUPTURED A ACALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0913983341893839 92 EWR - FLT 0487 - THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE 14TH STAGE DUCT RUPTURED WITH RESULTANT DAMAGE TO ENGINE COWLING AND THRUST REVERSER. THE SDR WILL REMAIN OPEN FOR CORRECTIVE ACTION AND RESULTS OF INVESTIGATION. (X) 2L72 4F A35EU 19950623000811995062300081WP 1995 6 23 CAL950427 119950529A79207938314501 LINE DOUG DC9 DC982 3022082WP PRESS SWITCH CRACKED A CALAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW09819NY 49479 MCO - FLT 0678 - THE LEFT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED IN-FLIGHT. THE ENGINE WAS REDUCED TO FLIGHT IDLE AND THE LIGHT EXTINGUISHED, BUT CAME ON AGAIN WITH POWER. THE AIRCRAFT WAS RETURNED TO MCO WITH ENGINE AT FLIGHT IDLE AND WITH THE OIL CLOG LIGHT EXTINGUISHED. MAINTENANCE FOUND THE LEFT ENGINE OIL LINE TO THE DIFFERENTIAL PRESSURE SWITCH CRACKED. THE OIL LINE WAS REPLACED. THE LEFT ENGINE WAS RUN AND LEAK CHECK WAS GOOD AND THE OIL CLOG LIGHT REMAINED OUT. (X) 2L72 4F A6WE 19950623000821995062300082NM 1995 6 23 CAL950429 119950530A3350 EEL FUSE BOEING737 737217 1384464NM FWD BAT CHARGER BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912230 19884 SDF - FLT 1679 - INSPECTION FOUND A FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. TROUBLESHOOTING FOUND BAD FUSE ON FORWARD BATTERY CHARGER. THE FUSE WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (X) 2L72 4F A16WE 19950623000831995062300083NM 1995 6 23 CAL950431 119950531A2910 LINE BOEING737 737217 1384464NM LT REAR SPAR RUPTURED A CALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW0913234 19888 MCO - FLT 1594 - THE A-SYSTEM HYDRAULIC FLUID QUANTITY WAS LOST IN-FLIGHT. THE LANDING GEAR AND FLAPS WERE EXTENDED MANUALLY AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A RUPTURED HYDRAULIC LINE AT THE LT REAR SPAR. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE A-HYDRAULIC SYSTEM WAS PRESSURIZED AFTER SERVICING AND NO LEAKS WERE NOTED. (X) 2L72 4F A16WE 19950623000841995062300084EU 1995 6 23 CAL950436 119950603A2910A3233161502000 LINE AIRBUS300 A300B4203 3930306EU RT MLG DR ACT LEAKING A CALAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW0913971 262 MCO - FLT 0487 - THE GREEN HYDRAULIC SYSTEM QUANTITY INDICATED IN THE YELLOW BAND WHILE AT CRUISE. THE QUANTITY WAS AT THE 11 O'CLOCK POSITION AFTER ARRIVAL AT MCO. MAINTENANCE FOUND THE RT MLG DOOR ACTUATOR HYDRAULIC PRESSURE LINE LEAKING. THE LINE WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECK WAS GOOD. (X) 2L72 4F A35EU 19950623000851995062300085NM 1995 6 23 CAL950437 119950509A5320 FITTING BOEING737 737130 1384435NM BS 695 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094421463384 19031 31J - INSPECTION FOUND A .3750 INCH CRACK IN THE RT BS 695 FRAME AFT LOWER FITTING AT THE OUTBOARD FASTENERS IN THE AFT HORIZONTAL FLANGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SB 737-53-1080, REV. 2 AND BOEING DRAWING 65C34490. (X) 2L72 4F A16WE 19950623000861995062300086NM 1995 6 23 CAL950438 119950508A5210 FRAME BOEING737 737130 1384435NM L2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094421463384 19031 31J - A 1 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF THE L-2 DOOR FRAME. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5210-01224. (X) 2L72 4F A16WE 19950623000871995062300087NM 1995 6 23 CAL950439 119950508A5320 SHEAR BEAM BOEING737 737130 1384435NM BS 664 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094421463384 19031 3LJ - A .3750 INCH CRACK WAS FOUND IN THE RADIUS OF THE INBOARD FLANGE AT THE FORWARD END OF THE LT S18A SHEAR BEAM, AFT SIDE OF BS 664 BULKHEAD. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-40-3, SRM 51-10-2, SRM 51-30-0, AND MM 51-00. (X) 2L72 4F A16WE 19950623000881995062300088NM 1995 6 23 CAL950440 119950511A5320 LAP SEAM BOEING737 737130 1384435NM BS 420 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW094421463384 19031 31J - INSPECTION FOUND CORROSION IN THE LAP SEAM AT BS 420, STR 27R. THE CORRODED AREA WAS REMOVED. A DOUBLER AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-03. (X) 2L72 4F A16WE 19950623000891995062300089WP 1995 6 23 HAL95068 119950605A335041B004A007G3 EEL BATTERY DOUG DC9 DC951 3022051WP ROWS 18-21 DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13420EA 47689 HNL - EMERGENCY CEILING LIGHTS ROWS 18-21 ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950623000901995062300090NM 1995 6 23 9509506615 119950615A5245 DOOR BOEING747 747251B 1384892NM AIR COND COMPT MISSING A NWAAK NONE D INFLIGHT SEPARATION DEDESCENT 1 GL01615US 20360 DURING DESCENT INTO NRT AT 15,000 FT, A LARGE BANG SOUND AND VIBRATION WAS EXPERIENCED. AFTER LANDING, FOUND THE NR 2 AIR CONDITION PACK ACCESS DOOR PANEL MISSING. ALSO, FOUND DAMAGE TO NR 3 AND NR 4 CANOE AND FUSELAGE PANEL 191KL. REPLACED THE NR 2 PACK DOOR AND NR 3 CANOE FORWARD FAIRING. REPAIRS MADE AS NECESSARY PER 51-40-09. AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19950623000911995062300091NM 1995 6 23 9509516302 119950617A524565B4001019 DOOR BOEING747 747451 1384940NM AIR COND COMPT MISSING A NWAAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 GL01662US 23720 UPON ARRIVAL INTO NRT, THE NR 3 AIR CONDITIONING PACK INLET DOOR WAS DISCOVERED MISSING, ACCOMPANIED WITH ADJACENT PANEL DAMAGE. REPLACED DOOR ASSSEMBLY, AIRCRAFT APPROVED FOR SERVICE. 2L74 4F RTA20WE 19950623000921995062300092NE 1995 6 23 9509526626 219950616A7200 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 3 FAILED A ANWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01626US 21708 702165 DURING CLIMB, THE NR 3 ENGINE DEVELOPED LOW EPR, N1 AND FUEL FLOW WITH HIGH EGT. THE ENGINE HAD NO RESPONSE TO POWER LEVER MOVEMENT. THE AIRCRAFT BEGAN A RETURN TO NRT, DUMPING 170,000 LBS OF FUEL. DURING DESCENT, THE ENGINE EXPERIENCED A COMPRESSOR STALL AND THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED AT NRT. THE ENGINE WAS REPLACED AND A RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19950623000931995062300093WP 1995 6 23 ABXA9500536 119950521A532059114065 JAMB DOUG DC9 DC931 3022065WP FS 160 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION, FOUND ENTRY DOOR CUTOUT SKIN AND REPAIR SEPARATED AT UPPER FORWARD CORNER. REPAIRED IAW DC-9 SRM 53-05 FIGURE 25A AND ABX REA D953-11613-MR. 2L72 4F A6WE 19950623000941995062300094WP 1995 6 23 ABXA9500537 119950525A5320591014211 JAMB DOUG DC9 DC931 3022065WP FS 383 PUNCTURED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION, FOUND FLC DOOR JAMB WEB PUNCTURED AT STA 383 AND LONGERON 29R. REPAIRED IAW ABX REA D953-11695-MR. 2L72 4F A6WE 19950623000951995062300095WP 1995 6 23 ABXA9500538 119950525A53305911412 SKIN DOUG DC9 DC931 3022065WP FS 425 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED AT STA 425 LONGERON 30. REPAIRED IAW ABX REA D953-11709-MR. 2L72 4F A6WE 19950623000961995062300096WP 1995 6 23 ABXA9500539 119950530A53305911408125 SKIN DOUG DC9 DC931 3022065WP FS 268 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION AROUND THE NR 1 AND NR 2 ADF LOOP ANTENNAS ON THE UPPER FUSELAGE SKIN. REPAIRED IAW ABX REA D953-11673-MR. 2L72 4F A6WE 19950623000971995062300097WP 1995 6 23 ABXA9500540 119950602A5530591143267 SKIN DOUG DC9 DC931 3022065WP FS 1087 HOLES ELONGATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION, FOUND LOOSE SCREWS ON THE VERTICAL STABILIZER, LEFT SIDE FORWARD BOTTOM ATTACH ANGLE. REPAIRED IAW ABX REA D953-11728-MR. 2L72 4F A6WE 19950623000981995062300098WP 1995 6 23 ABXA9500541 119950522A57202645830 BRACKET DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION AND CRACKED BRACKET BETWEEN STRINGERS 15 AND 16 AT STA XCW 58 ON THE RIGHT WING. REPLACED BRACKET IAW DC-9 SRM 51-30-5. CLEANED CORROSION BELOW BRACKET IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950623000991995062300099WP 1995 6 23 ABXA9500542 119950522A571399193692 STRINGER DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL 1 CORROSION INSIDE BARREL NUT HOLE IN STRINGER 16, RIGHT WING. REMOVED CORROSION IAW DC-9 SB 57-98, DC-9 SRM 51-10-3. 2L72 4F A6WE 19950623001001995062300100WP 1995 6 23 ABXA9500543 119950522A572099193692 T-CAP DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 17 TO 18, 18 TO 19 AND 19 TO 20 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950623001011995062300101WP 1995 6 23 ABXA9500544 119950521A572099193691 T-CAP DOUG DC9 DC931 3022065WP WS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL 1 CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 11 TO 12 AND 16 TO 17 AT STA XCW 58. REMOVED CORROSION IAW DC-9 SRM 51-10-3. 2L72 4F A6WE 19950623001021995062300102WP 1995 6 23 ABXA9500545 119950518A52805910557159 DOOR DOUG DC9 DC931 3022065WP WS 111.5 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEVEL 1 CORROSION, SHEARED FASTENERS AND CHAFING ON LEFT FLYING DOOR. ALSO, FOUND SKIN BENT AT AFT END OF HINGE. REPLACED FLYING DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19950623001031995062300103WP 1995 6 23 ABXA9500546 119950519A52805910557135 DOOR DOUG DC9 DC931 3022065WP WS 111.5 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR HAD DENT ON INBOARD END. REPLACED DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950623001041995062300104WP 1995 6 23 ABXA9500547 119950519A52803923166501 FITTING DOUG DC9 DC931 3022065WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR ARTICULATING DOOR FORWARD DRIVE LINK HAD SIDE PLAY. REPLACED DRIVE LINK ATTACH FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950623001051995062300105WP 1995 6 23 ABXA9500548 119950519A3231S24312155A017 BUSHING DOUG DC9 DC931 3022065WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT FLYING DOOR DRIVE ROD OUTBOARD END HAD SIDE PLAY. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950623001061995062300106WP 1995 6 23 ABXA9500549 119950520A32313923159503 ARM DOUG DC9 DC931 3022065WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR ARTICULATING DOOR DRIVE ROD END HAD SIDE PLAY. REPLACED ARM IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950623001071995062300107WP 1995 6 23 ABXA9500550 119950522A3231S24312155A017 BUSHING DOUG DC9 DC931 3022065WP WS 111.5 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT FLYING DOOR DRIVE ROD OUTBOARD END HAD SIDE PLAY. REPLACED BUSHINGS IAW DC-9 MM 32-10-6. 2L72 4F A6WE 19950623001081995062300108WP 1995 6 23 ABXA9500551 119950601A5320575468828 DOUBLER DOUG DC9 DC931 3022065WP FS 125 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 56-11, REV 3, FOUND CRACKED DOUBLER AROUND RIGHT CLEARVIEW WINDOW FRAME UPPER AFT CORNER. REPAIRED BY REPLACING DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19950623001091995062300109WP 1995 6 23 ABXA9500552 119950523A3231NAS110417 BOLT DOUG DC9 DC932 3022066WP RT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23987AX 47364 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE HAD EXCESSIVE PLAY. REPLACED WORN BOLT AT DOOR HINGE BRACKET IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19950623001101995062300110WP 1995 6 23 ABXA9500553 119950509A78305958782503 DRIVE LINK PWA 4310003 DOUG DC9 DC941 302207NWP TR UNIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX RC1090 47498 DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03, SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND OUTBOARD LOWER THRUST REVERSER DRIVE LINK HAD A CRACK INDICATION. REPLACED OUTBOARD LOWER THRUST REVERSER DRIVE LINK IAW DC-9 MM 78-32, LINK WAS SCRAPPED. 2L72 4F A6WE 19950623001111995062300111WP 1995 6 23 ABXA9500554 119950511A5311591016373 FRAME DOUG DC9 DC941 302207NWP FS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 DURING C-CHECK INSPECTION, FOUND FRAME 1072 CRACKED AT LONGERON 7R. REPAIRED FRAME IAW ABX REA D953-11564-MR. 2L72 4F A6WE 19950623001121995062300112WP 1995 6 23 ABXA9500555 119950511A5330591142487 SKIN DOUG DC9 DC941 302207NWP FS 945 WRINKLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23969AX 47464 DURING C-CHECK INSPECTION, FOUND EXTERIOR SKIN WRINKLED AT STA 945 TO 965, LONGERON 25R. REPAIRED ABX REA D953-11561-MR. 2L72 4F A6WE 19950623001131995062300113WP 1995 6 23 ABXA9500556 119950615A793142D491C PRESS SWITCH DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 1 DEFECTIVE A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23817AX 3906 45928 671404 EN ROUTE FROM FLL NR 1 ENGINE SECURED DUE TO ILLUMINATION OF THE NR 1 ENGINE OIL PRESSURE LIGHT DURING CLIMBOUT. OIL QUANTITY, OIL PRESSURE AND OIL TEMPERATURE WERE NORMAL. THRUST WAS REDUCED, BUT LIGHT REMAINED ON. ENGINE SECURED AT 0222 Z. FOUND DIFFERENTIAL PRESSURE SWITCH CRACKED AND LEAKING. CHANGED SWITCH AND FILTER, PERFORMED ENGINE INSPECTION IAW PRATT AND WHITNEY 72-0-15. GROUND RAN ENGINE, OPS CHECKED GOOD. 2L74 4F4 F 4A25 1E8 19950623001141995062300114WP 1995 6 23 ABXA9500557 119950616A29107761892796 LINE DOUG DC8 DC863F 302198FWP LEFT DEFECTIVE A ABXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23811AX 46113 AFTER LIFT OFF, LOST ALL HYDRAULIC PRESSURE, RESERVOIR LOW PRESSURE AND AILERON MANUAL CONTROL LIGHTS ILLUMINATED. HYDRAULIC QUANTITY INDICATED FULL, WAS NOT ABLE TO RECOVER PRESSURE WITH AUX PUMP. REPAIRED .5 INCH STEEL HYDRAULIC LINE BEHIND ACCESS PANELS 525 AND 562 IN LEFT FLAP WELL, OUTBOARD NR 5 MAIN WHEEL IAW GMM, CHAPTER 3, 29-01-01. SYSTEM LEAK CHECKED GOOD. SERVICED HYDRAULIC RESERVOIR IAW DC-8 MM 12-08. 2L74 4F 4A25 19950623001151995062300115NM 1995 6 23 DL72E952593 119950509A5330 SKIN 65545771 BOEING727 727247 138408FNM FS 700-720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 65727433 21482 DURING CORROSION VISIT INSPECTION, THE LOWER FUSELAGE SKIN BETWEEN STA 700 TO 720 AND S-28L AND S-28R WAS FOUND TO HAVE CORROSION THAT REQUIRED A 33.0 BY 17.5 SKIN CUTOUT. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH AD 91-09-09, AND THE ASSOCIATED BAC S/B 727-53-0203 REV 2. 2L73 4F A3WE 19950623001161995062300116NM 1995 6 23 DL72E952594 119950512A5330 SKIN BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 DURING CORROSION VISIT INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 1010, BETWEEN STRINGER 29L AND STRINGER 30. A 2.5 BY 2.5 CUTOUT IN THE SKIN WAS REQUIRED, STRINGER 30 WAS CUT AFT OF THE FACTORY SPLICE. BOTH DAMAGE LOCATIONS WILL BE REPAIRED IN ACCORDANCE WITH B727 SRM 53-10-3 FIG 1 FOR THE STR AND B727 SRM 53-30-3 FIG 3A, FOR THE SKIN. 2L73 4F A3WE 19950623001171995062300117NM 1995 6 23 DL72E952595 119950513A5320 ANGLE 65147186 BOEING727 727247 138408FNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112826W 65174172 21331 DURING LETTER CHECK INSPECTION, THE RH TORQUE BOX FORWARD TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. ALSO, THE FWD TRANSVERSE BEAM WAS FOUND CRACKED. IN ACCORDANCE WITH B727 S/B 53-0129 REV 4, BOTH THE BEAM AND THE ANGLE WERE REPLACED. 2L73 4F A3WE 19950623001181995062300118NM 1995 6 23 DL72E952634 119950518A57546516221100 RIB BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INITIAL INSPECTION, CRACK FOUND ON THE O/B RIB OF THE O/B SLAT TRACK RIB. A REPAIR WAS INSTALLED PER THE M/M CHAPTER 57-54-00 FIG 814, FOR NR 5 SLAT. 2L73 4F A3WE 19950623001191995062300119NM 1995 6 23 DL72E952670 119950613A5315 FLOORBEAM BOEING727 727247 138408FNM FS 360 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM AROUND NUTPLATE HOLES FROM LBL 10 RBL 12 STA 360. REPAIRED AS PER M/M 53-20-11 PG 802 ITEM 6C. 2L73 4F A3WE 19950623001201995062300120NM 1995 6 23 DL72E952671 119950613A5347 SEAT TRACK BOEING727 727247 138408FNM FS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, O/B RT SEAT TRACK CRACKED AT FWD END HOLE AT STA 760. REPAIRED PER SRM 53-10-8 FIG 11. 2L73 4F A3WE 19950623001211995062300121NM 1995 6 23 DL72E952673 119950613A5347 SEAT TRACK BOEING727 727247 138408FNM FS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, I/B RT SEAT TRACK CRACKED AT FWD END HOLE AT STA 760. REPAIRED PER SRM 53-10-8 FIG 11. 2L73 4F A3WE 19950623001221995062300122NM 1995 6 23 DL72E952675 119950613A5347 SEAT TRACK BOEING727 727247 138408FNM FS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, O/B LT SEAT TRACK CRACKED AT FWD END HOLE AT STA 760. REPAIRED AS PER SRM 53-10-8 FIG 11. 2L73 4F A3WE 19950623001231995062300123NM 1995 6 23 DL72E952676 119950613A5311 FORMER BOEING727 727247 138408FNM FS 500 BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, FORMER BENT STA 500 O/B STR 25R. REPAIRED PER SRM 53-10-4 FIG 26. 2L73 4F A3WE 19950623001241995062300124NM 1995 6 23 DL72K952650 119950616A5320 WEB BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11472DA 20749 FOUND DURING A-2 LETTER CHECK, 2 CRACKS TORQUE BOX WEB UPPER ROW OF RIVETS FWD SIDE RT. REPAIRED PER MM 53-11-0 PAR 19. 2L73 4F A3WE 19950623001251995062300125NM 1995 6 23 DL72K952651 119950616A5754 SKIN BOEING727 727232 1384082NM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11472DA 20749 FOUND DURING A-2 LETTER CHECK, NR 1 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 12. 2L73 4F A3WE 19950623001261995062300126NM 1995 6 23 DL72K952652 119950616A5754 SKIN BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11472DA 20749 FOUND DURING A-2 LETTER CHECK, NR 2 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19950623001271995062300127NM 1995 6 23 DL72K952653 119950616A5754 ANGLE BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11472DA 20749 FOUND DURING A-2 LETTER CHECK, NR 4 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19950623001281995062300128NM 1995 6 23 DL72K952654 119950616A5320 ANGLE BOEING727 727232 1384082NM FS 910 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11472DA 20749 FOUND DURING A-2 LETTER CHECK, ANGLE AT STA 910 CRACKED. REPAIRED PER M/M 53-11-0 PAR 20. 2L73 4F A3WE 19950623001291995062300129NM 1995 6 23 DL72S952591 119950531A5330 DOUBLER BOEING727 727232 1384082NM R1 DOOR AREA CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING HMV, A CRACK WAS FOUND IN THE DOORWAY SURROUND DOUBLER AT THE UPPER FORWARD CORNER OF THE UPPER HINGE CUTOUT AT THE R1 DOOR. IN ACCORDANCE WITH BAC TWX DAL-ATL-95-0573RR DATED 30 MAY 1995, THE CRACK WAS STOP DRILLED AND A EXTENRNAL DOUBLER WILL BE USED AS PER BAC S/B 727-53-0136. 2L73 4F A3WE 19950623001301995062300130NM 1995 6 23 DL72S952592 119950515A5330 SKIN BOEING727 727232 1384082NM FS 570-590 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 DURING HMV INSPECTION, CORROSION WAS FOUND ON THE SKIN BETWEEN STA 570 AND STA 590 UNDER STRINGER 27L REQUIRING A 5 BY 9 CUTOUT. THE CUTOUT WAS REPAIRED IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950623001311995062300131NM 1995 6 23 DL72S952596 119950518A5320 CHANNEL 651751724 BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11525DA 65175172 21585 DURING LETTER CHECK INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM CHANNEL AT FS 1263 WAS FOUND CRACKED. IN ACCORDANCE WITH BAC S/B 727-53-0129 REV 4, THE CHANNEL WAS REPLACED. 2L73 4F A3WE 19950623001321995062300132NM 1995 6 23 DL72S952604 119950613A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11483DA 20863 FOUND DURING A-2 LETTER CHECK, 7.25 INCH CRACK LT ELEVATOR UPPER SKIN ELEVATOR STA 120.00. REPAIRED PER SRM 55-20-3 AND ID PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950623001331995062300133NM 1995 6 23 DL72S952605 119950613A7110 NOSE COWL BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 3 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11483DA 20863 700256 FOUND DURING A-2 LETTER CHECK, NOSE COWL AFT WEB CRACKED 6 INCHES AT 5 O'CLOCK POS/AFT WEB DOUBLER CRACKED 2 INCHES 5:30 POS. REPAIRED PER SRM 54-10-3 FIG 3. 2L73 4F4 F A3WE E2EA 19950623001341995062300134NM 1995 6 23 DL72S952645 119950615A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11408DA 21152 FOUND DURING E-1 LETTER CHECK, COVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT AT NR 3 SLAT. REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950623001351995062300135NM 1995 6 23 DL72S952646 119950615A5754 SKIN BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11408DA 21152 COVE SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT NR 2 SLAT, FOUND DURING E-1 LETTER CHECK. REPAIRED PER M/M 57-54-0 PG 80. 2L73 4F A3WE 19950623001361995062300136NM 1995 6 23 DL72S952648 119950609A5330 BEAR STRAP 65545932 BOEING727 727232 1384082NM FS 1137 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 6572746 21077 DURING OVERHAUL, THE C-3 DOOR INTERNAL BEAR STRAP (.125 THICK 2024-T42 BARE) WAS FOUND CORRODED AT STA 1137 AND STA 1094, STR 27R. IN ACCORDANCE WITH FAA/DER FORM 8110, DATED 09 JUNE 1995, AN INTERNAL TITANIUM REPAIR DOUBLER WAS INSTALLED AT EACH LOCATION. 2L73 4F A3WE 19950623001371995062300137NM 1995 6 23 DL72W952631 119950614A5754 FAIRING BOEING727 727247 138408FNM NR 8 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11297WA 22534 FOUND DURING E-2 LETTER CHECK, SEVERAL CRACKS AT NR 8 SLAT I/B TRACK FAIRING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950623001381995062300138NM 1995 6 23 DL72W952632 119950614A5320 ANGLE BOEING727 727247 138408FNM FS 910 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11297WA 22534 FOUND DURING E-2 LETTER CHECK, ANGLE AT STATION LEFT FS 910 MLG UPLOCK ATTACH FRAME WAS FOUND CRACKED. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950623001391995062300139NM 1995 6 23 DL72W952635 119950614A5320 WEB BOEING727 727247 138408FNM FS 1223 MIS MFG A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11297WA 22534 FOUND DURING E-2 LETTER CHECK, LIGHTNING HOLE TRIMMED OUT PAST STIFFENER LIP LT LWR TORQUE BOX, JUST AFT OF STA 1223. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950623001401995062300140NM 1995 6 23 DL73E952649 119950607A5330 SKIN 654580023 BOEING737 7372S3 NM FS 303.9 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11367DL 6545800219 21774 DURING INSPECTION, THE FUSELAGE SKIN AT STA 303.9 BETWEEN STR 10 AND STR 14 WAS CRACKED AT THE LOWER FORWARD CORNER OF THE FORWARD ENTRY DOORWAY (L-1) LOWER HINGE CUTOUT. THE CRACK MEASURED APPROX 1.8 LONG. FAA FORM 8110-3 DATED 6/7/95, THE DAMAGE WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. 2L72 4F RTA16WE 19950623001411995062300141NM 1995 6 23 DL757952603 119950605A5754114N4005127 TE WEDGE BOEING757 757232 1384965NM NR 4 LE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11608DA 22815 T/E WEDGE WORN BOTTOM SIDE 36 INCHES FROM I/B END OF NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02, DURING SHOP VISIT. 2L72 4F RTA2NM 19950623001421995062300142NM 1995 6 23 DL757952621 119950614A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11620DL 22910 HAIL DAMAGE TO TOP HALF OF RADOME. REPAIRED DAMAGE AT SHOP INSPECTION PER SRM 53-10-72. 2L72 4F RTA2NM 19950623001431995062300143NM 1995 6 23 DL757952622 119950614A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11653DL 24393 RADOME WAS ROUTED TO SHOP FOR DELAMINATION, DUE TO LIGHTNING STRIKE. REPAIRED PER SRM 53-10-72. 2L72 4F RTA2NM 19950623001441995062300144NM 1995 6 23 DL757952655 119950606A5751 AILERON BOEING757 757232 1384965NM RT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE LWR O/B L/E OF THE RT AILERON WAS FOUND TO BE WORN. THE AILERON WAS REPAIRED PER SRM 51-70-03 REF FROM 57-60-01. 2L72 4F RTA2NM 19950623001451995062300145NM 1995 6 23 DL757952656 119950606A5751 LE SKIN BOEING757 757232 1384965NM RT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE UPPER I/B L/E SURFACE OF THE RT AILERON WAS FOUND TO BE WORN. THIS WAS REPAIRED PER SRM 51-70-03 REF FROM 57-60-01. 2L72 4F RTA2NM 19950623001461995062300146NM 1995 6 23 DL757952657 119950608A5753 TE WEDGE BOEING757 757232 1384965NM TE 3 TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE T/E WEDGE FOR NR 3 FLAP WAS FOUND TO BE DELAMINATED APPROX TWO FEET OF I/B END. THIS DAMAGED AREA WAS REPAIRED PER SRM 51-70-07. 2L72 4F RTA2NM 19950623001471995062300147NM 1995 6 23 DL767952589 119950505A5522 LE SKIN 183T30012 BOEING767 767232 1385132NM RT ELEVATOR CHIPPED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, LEADING EDGE WAS FOUND TO BE CHIPPED AT UPPER SURFACE 75.5 INCHES FROM O/B END. REPAIRED AS PER SRM 51-70-03, FOR RIGHT ELEVATOR. 2L72 4F RTA1NM 19950623001481995062300148NM 1995 6 23 DL767952590 119950505A5522 SKIN 183T30012 BOEING767 767232 1385132NM RT ELEVATOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, NUMEROUS SKIN PUNCTURES WERE LOCATED ON UPPER SURFACE. REPAIRED AS PER SRM 51-70-17, FOR RIGHT ELEVATOR. 2L72 4F RTA1NM 19950623001491995062300149NM 1995 6 23 DL767952597 119950505A5522 SKIN 183T20012 BOEING767 767232 1385132NM RT ELEVATOR DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, DELAMINATION WAS FOUND AT HINGE CUTOUTS. REPAIRED AS PER SRM 55-20-2 PG 102, FOR RT ELEVATOR. 2L72 4F RTA1NM 19950623001501995062300150NM 1995 6 23 DL767952598 119950505A5521 RIB 183T20012 BOEING767 767232 1385132NM RT ELEVATOR DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, NR 1 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, NR 2 RIB FROM I/B EDGE FOUND TO BE CRACKED AT FWD EDGE, AND NR 8 RIB FROM I/B EDGE WAS DELAMINATED AT FWD EDGE. REPAIRED RIBS AS PER SRM 55-20-02, FOR RT ELEVATOR. 2L72 4F RTA1NM 19950623001511995062300151NM 1995 6 23 DL767952599 119950505A5522 LE SKIN 183T20012 BOEING767 767232 1385132NM RT ELEVATOR DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, LOWER SURFACE OF RT ELEVATOR L/E WAS FOUND DELAMINATED AND CRACKED. ALSO, UPPER SURFACE O/B L/E HAD SOME DELAMINATION. REPAIRED AS PER SRM 55-20-02. 2L72 4F RTA1NM 19950623001521995062300152NM 1995 6 23 DL767952600 119950505A5520 ELEVATOR 183T20012 BOEING767 767232 1385132NM RIGHT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION FOUND HOLE 1.5 DIA 31 FROM T/E AND 12 FROM I/B EDGE, 1 HOLE FOUND 1 DIA, 37 FROM T/E AND 12 FROM I/B EDGE, 1 HOLE FOUND 1.5 DIA, 11 AFT OF SPAR AND 13 FROM I/B EDGE, AND 1 HOLE FOUND 1.5 DIA, 6 AFT OF SPAR AND 26 FROM I/B EDGE. REPAIRED AS PER SRM 55-20-01, FOR RT ELEVATOR. 2L72 4F RTA1NM 19950623001531995062300153NM 1995 6 23 DL767952601 119950505A5520 ELEVATOR 183T20012 BOEING767 767232 1385132NM RIGHT HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 000080 22226 DURING SHOP INSPECTION, SEVERAL HOLES FOUND. ONE HOLE FOUND 1 DIA, 14 AFT OF SPAR AND 29 FROM O/B EDGE, 1 HOLE FOUND 1 DIA, 27 FROM T/E AND 37 FROM O/B EDGE, 1 HOLE FOUND 1.5 DIA, 14 FROM T/E AND 32 FROM O/B EDGE, AND 1 HOLE FOUND 1 DIA, 21 FROM O/B EDGE AND 25 FROM T/E. REPAIRED AS PER SRM 55-20-01, FOR RT ELEVATOR. 2L72 4F RTA1NM 19950623001541995062300154WP 1995 6 23 DLL10952602 119950613A5755LS118151 TE SKIN LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 ANGLE CRACKED, UPPER TRAILING EDGE BAT STRUCTURE IS CRACKED FROM UPPER FWD LEG TO FASTENER HOLE OUTBOARD OF INBOARD NR 2 SPOILER HINGE AND INBOARD OF INBOARD HINGE. REPAIRED PER SRM 57-20-00. 2L73 4F A23WE 19950623001551995062300155WP 1995 6 23 DLL10952613 119950526A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TOP OF FLOORBEAM IS CORRODED IN SEVERAL PLACES, FS 901 FROM LBL 60 TO RBL 60. REMOVED OLD FLOORBEAM, CUT NEW BEAM, DRILLED HOLES, TREATED AND PAINTED PER SRM 53-21-00 PG 849. 2L73 4F A23WE 19950623001561995062300156WP 1995 6 23 DLL10952624 119950608A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 897 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FUSELAGE SKIN TEAR STRAP WITH CORROSION AND DISBONDED AT FS 897 BETWEEN STRINGES 40, 41 AND 42. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950623001571995062300157WP 1995 6 23 DLL10952625 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 897 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 897 STR 43 TO 42, STRAP HAS CORROSION UNDERNEATH. REPAIRED PER SRM 53-31-00 PG 807 FIG 804. 2L73 4F A23WE 19950623001581995062300158WP 1995 6 23 DLL10952626 119950520A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 897 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 897 STR 43 TO 44, STRAP HAS CORROSION UNDERNEATH. REMOVED CORROSION, FOUND WITHIN LIMITS PER SRM 53-31-00 PG 801, REPAIRED PER SRM 53-31-00 PG 830 FIG 816. 2L73 4F A23WE 19950623001591995062300159WP 1995 6 23 DLL10952627 119950531A5311 FRAME LKHEED1011 10113851 5265010WP FS 235 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FUSELAGE FRAME AT FS 235, WAS FOUND CORRODED 14 LEFT AND RIGHT AT FESC ACCESS OPENING. CLEANED CORROSION, OUT OF LIMITS PER SRM 53-12-00. INSTALLED REPAIR PER SRM 53-12-00. 2L73 4F A23WE 19950623001601995062300160WP 1995 6 23 DLL10952628 119950529A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 HOLE BORE CORRODED LT MLG FITTING HOLE NR 11 FOR RETRACT ACTUATOR FITTING (FWD/LWR HOLE LOOKING OUTBD) HAS CORROSION IN BORE. DAMAGE WAS FOUND AT HMV. OPENED HOLE NR 11 TO .562 TO REMOVE CORROSION. REMOVAL OK, HEFC OK. OXIDE BLASTED AREA, ROTO-PEENED AREA, CAD PLATED AREA PER PS 900-3-9 NR 4 PRIMED AND PAINTED, SRM REF 57-14-00. 2L73 4F A23WE 19950623001611995062300161WP 1995 6 23 DLL10952629 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FASTENER HOLES IN LT WING FOR RETRACT ACTUATOR ATTACH HOLES NR 1, 2, 3, 4, 5, AND 6 ARE CORRODED, FOUND AT HMV. REAMED HOLES TO .718 TO REMOVE CORROSION PER SRM 57-14-00. REMOVAL OK, HEFC OK. OXIDE BLASTED AREA, ROTO-PEENED AREA, CAD PLATED AREA PER PS 900-3-9 NR 4 PRIMED AND PAINTED. 2L73 4F A23WE 19950623001621995062300162WP 1995 6 23 DLL10952636 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1770 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP DISBONDED FS 170 BETWEEN STR 38 AND 39. REMOVED STRAP, DRILLED STRAP AND SPLICE PER SRM 53-31-00 PG 830. INSTALLED STRAP PER SRM 53-31-00 PG 830, FOUND AT HMV. 2L73 4F A23WE 19950623001631995062300163WP 1995 6 23 DLL10952637 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1677 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 1677 BETWEEN STR 29 TO 31 UNDER FRAME. REPLACED STRAP PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950623001641995062300164WP 1995 6 23 DLL10952638 119950526A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP FS 1755 UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FAILSAFE STRAP UNBONDED C3 B/B STA 1755 BETWEEN STR 35 AND 36 AND 38 TO 40, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950623001651995062300165WP 1995 6 23 DLL10952639 119950526A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP FS 1784 UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FAILSAFE STRAP UNBONDED C3 B/B STA 1784 BETWEEN STR 35 TO 40, FOUND AT HMV. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950623001661995062300166WP 1995 6 23 DLL10952640 119950613A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1750 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 1750 BETWEEN STR 35 TO 36. PEELED BACK TEAR STRAP AND FOUND NO CORROSION. REPAIRED PER SRM 53-31-00 FIG 816 NOTE 6. 2L73 4F A23WE 19950623001671995062300167WP 1995 6 23 DLL10952641 119950613A5313 STRINGER LKHEED1011 10113851 5265010WP FS 690 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, STRINGER FOUND MISSDRILLED, STR 40 FS 690. ROUTED OUT DAMAGE, WITHIN LIMITS PER SRM 53-13-00 PG 801, TREATED AND PAINTED. 2L73 4F A23WE 19950623001681995062300168WP 1995 6 23 DLL10952642 119950603A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 739 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 LOWER GALLEY TEAR STRAPS DISBONDED AT FS 739 FROM STR 23 TO 24 AND 25 TO 27, FOUND AT HMV. CUT STRAP AND CLEANED CORROSION, AREA FOUND TO BE WITHIN LIMITS PER SRM 53-31-00 PG 801. DRILLED NEW SPLICE PER SRM, TREATED AND PAINTED, INSTALLED NEW SPLICE REPAIR PER SRM 53-31-00 PG 804. 2L73 4F A23WE 19950623001691995062300169WP 1995 6 23 DLL10952667 119950613A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1750 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, STR 39 FS 1750 CRACKED. REPAIRED PER SRM 53-13-00 FIG 804. 2L73 4F A23WE 19950623001701995062300170WP 1995 6 23 DLL13952606 119950609A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 769-789 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND TEAR STRAP DISBONDED, AFT CORNER LOWER GALLEY AREA BETWEEN FS 769 TO 789 STA 38. CORROSION REMOVED, PER SRM 51-21-01, FOUND TO BE WITHIN LIMITS PER SRM 53-31-00 FIG 801. MFG AND INSTALLED DOUBLER PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950623001711995062300171WP 1995 6 23 DLL13952607 119950613A5330 DOUBLER LKHEED1011 10113851 5265010WP FS 1490 TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND INTERNAL DOUBLER FOR FUS TORN AT STA 1490 BETWEEN STR 27 TO 28, C2 B/B. REMOVED DAMAGE INSTALLED DOUBLER PER SRM 53-31-00. 2L73 4F A23WE 19950623001721995062300172WP 1995 6 23 DLL13952647 119950510A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FITTING CORRODED, RT MLG CORRODED AT UPPER SIDE OF LOWER SUPPORT FOR RETRACT ACTUATOR, FOUND AT HMV. MACHINED .030 FROM FACE TO REMOVE CORROSION, WITHIN LIMITS OF SRM 57-14-00. HFEC OF SUPPORT FITTING FOUND NO CRACKS. ROTO-PEENED PER PS 900-4-5, CAD PLATED PER 900-3-9 NR 4, OXIDE BLASTED, PRIMED AND PAINTED. 2L73 4F A23WE 19950623001731995062300173WP 1995 6 23 DLL13952658 119950615A55221524058108 SKIN LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 THE O/B L/E UPPER SIDE PANEL WAS FOUND TO BE CRACKED. REPAIRED PER SRM 55-22-00, AT HMV FOR RIGHT ELEVATOR. 2L73 4F A23WE 19950623001741995062300174WP 1995 6 23 DLL13952659 119950608A55221524058108 SKIN LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 THE T/E TIP SKIN WAS FOUND TO BE CRACKED ON THE LOWER SIDE. THIS WAS REPAIRED PER SRM 55-22-00 FIG 802, AT HMV FOR RT ELEVATOR. 2L73 4F A23WE 19950623001751995062300175WP 1995 6 23 DLL13952661 119950522A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1560 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 AT HMV, FOUND STRINGER DAMAGED, STRINGER 34 AT STA 1560. REMOVED DAMAGED AREA, DRILLED NEW STRINGER SPLICES, INSTALLED NEW STRINGER SPLICE DOUBLER AND STRINGER SECTIONS PER SRM 53-13-00 PG 806 FIG 804. 2L73 4F A23WE 19950623001761995062300176WP 1995 6 23 DLL13952662 119950613A5320 SUPPORT LKHEED1011 10113851 5265010WP LBL 8.5-RBL 8.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SUPPORT CRACKED C2 B/B LBL 8.5 AND RBL 8.5. DYE PENETRANT, INSPECTED CRACKS AND STOP DRILLED BOTH CRACKS. FABRICATED NEW ANGLES, DRILLED NEW ANGLES, TREAT AND PAINTED, AND INSTALLED NEW ANGLES PER SRM 53-24-00 PG 807 FIG 805. 2L73 4F A23WE 19950623001771995062300177WP 1995 6 23 DLL13952664 119950509A5330 SKIN LKHEED1011 10113851 5265010WP FS 1645-1665 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SKIN CORRODED, STA 1645 TO 1665. REPAIRED PER SRM 53-31-00 FIG 804. 2L73 4F A23WE 19950623001781995062300178WP 1995 6 23 DLL13952665 119950612A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 649 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOOR SUPPORT CORRODED FS 649 O/B. REMOVED FLOOR SUPPORT, DRILLED NEW FLOOR SUPPORT AND SPLICE ANGLE, INSTALLED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950623001791995062300179WP 1995 6 23 DLL13952666 119950612A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 689 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOOR SUPPORT CORRODED, C1 B/B AT FS 69. REMOVED SUPPORT, DRILLED TREAT AND PAINTED, INSTALLED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950623001801995062300180NM 1995 6 23 DLM88952633 119950614A5320 ANGLE DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11989DL 53341 FOUND DURING D-1 LETTER CHECK, KEEL BEAM AFT ANGLE CRACKED BOTH ENDS. INSTALLED DOUBLER PER MM 53-05 FIG 101. 2L72 4F RTA6WE 19950623001811995062300181NM 1995 6 23 DLM88952644 119950615A5230 PAN DOUG MD88 MD88 3023688NM C-3 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11990DL 53342 FOUND DURING D-1 LETTER CHECK, C3 DOOR FWD PAN CRACKED AT HOLD OPEN FITTING. REPAIRED PER SRM 52-05 FIG 26A. 2L72 4F RTA6WE 19950623001821995062300182WP 1995 6 23 MWEA95217 119950617A3350DCELLS EEL BATTERY DOUG DC9 DC932 3022066WP FWD CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31401ME 47133 DURING ROUTINE INSPECTION, THE OVERHEAD EMERGENCY LIGHTS NEAR ROWS 2, 3 AND 5 WERE VERY DIM DURING TEST. MAINTENANCE REMOVED AND REPLACED BATTERIES IN POWER SUPPLY. 2L72 4F A6WE 19950623001831995062300183NM 1995 6 23 P5CA9500005 119950530A5314 KEEL BEAM BOEING747 747122 1384872NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 ADF ANTENNA MOUNT STRUCTURE IS CORRODED LEVEL 1, LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01 PAGES 13, 14, 15, 16 PAR 6 AND 7. 2L74 4F A20WE 19950623001841995062300184NM 1995 6 23 P5CA9500006 119950530A5312 BLKHD LINER BOEING747 747122 1384872NM FS 2160 HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD NEAR CENTER. REPAIRED AS PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950623001851995062300185NM 1995 6 23 P5CA9500007 119950530A5330 SKIN BOEING747 747122 1384872NM BS 2040 BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FUSELAGE SKIN AT AFT BULK CARGO DOOR OPENING STATION 2040 IS BENT OUTWARD. REPAIRED AS PER BOEING SRM 51-40-01, PRIMED AND PAINTED. 2L74 4F A20WE 19950623001861995062300186NM 1995 6 23 P5CA9500008 119950530A255065B60291 PALLET GUIDE BOEING747 747122 1384872NM BS 663L PEELED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FORWARD CARGO COMPARTMENT STATION 663 LEFT SIDE PALLET GUIDE SUPPORT METAL PEELED BACK. REMOVED AND REPLACED PALLET GUIDE AS PER SRM 51-10-01. 2L74 4F A20WE 19950623001871995062300187NM 1995 6 23 P5CA9500009 119950530A5312 BLKHD LINER BOEING747 747122 1384872NM BS 2160 HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LT SIDE. REPAIRED AS PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950623001881995062300188NM 1995 6 23 P5CA9500010 119950530A7830 SKIN BOEING BOEING747 747122 1384872NM NR 1 TR UNIT WORKING RIVETS A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 SMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623001891995062300189NM 1995 6 23 P5CA9500011 119950530A711069B906788 SIDE COWL BOEING747 747122 1384872NM NR 1 ENGINE WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 TOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN WITH FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07. 2L74 4F A20WE 19950623001901995062300190NM 1995 6 23 P5CA9500012 119950530A5414 SKIN BOEING747 747122 1384872NM NR 3 PYLON LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVITS. INSTALLED ALL MISSING AND LOOSE AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623001911995062300191NM 1995 6 23 P5CA9500013 119950530A5412 FIRE WALL BOEING BOEING747 747122 1384872NM NR 3 PYLON WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 NR 3 PYLON IN 3RD AND 4TH INSPECTION PANEL TOP HOLE HYDRAULIC PRESSURE LINE FIREWALL FITTING JAM NUT NOT INSTALLED HOLE IS WORN ELOGATED. DRESSED AND CLEANED BULKHEAD FITTING HOLE AS PER SRM 51-10-02, INSTALLED AND SECURED SHOULDER BUSHING, AND BULKHEAD FITTING. 2L74 4F A20WE 19950623001921995062300192NM 1995 6 23 P5CA9500014 119950530A7830 TR SLEEVE BOEING747 747122 1384872NM NR 4 ENG SCRATCHED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 SCRATCHES RIGHT SIDE NR 4 ENGINE THRUST REVERSER SLEEVE FROM 3:30 TO 4:00 POSITION. REMOVED SCRATCHES AS PER BOEING SRM 51-10-01 PAGE 11 TREATED AND PAINTED AREA. 2L74 4F A20WE 19950623001931995062300193NM 1995 6 23 P5CA9500015 119950530A5414 SKIN BOEING747 747122 1384872NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 RIVET HEAD CRACKED ON NR 4 PYLON AFT OF SLOT SEAT LEFT SIDE LOWER SECTION. REMOVED AND REPLACED DAMAGED RIVET PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623001941995062300194NM 1995 6 23 P5CA9500016 119950530A5730 NUTPLATE BOEING747 747122 1384872NM ABOVE NR 2 ENG LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 ONE NUTPLATE LOOSE AND ONE NUTPLATE MISSING ON TOP LEADING EDGE ACCESS PANEL ABOVE NR 2 ENGINE. REMOVED AND REPLACED NUTPLATES PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623001951995062300195NM 1995 6 23 P5CA9500017 119950530A575165B02200X SKIN BOEING747 747122 1384872NM LT AILERON PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 SMALL PUNCTURE 1.5 BY .5 LEFT WING INBOARD AILERON LOWER SKIN ALONG OUTER EDGE. SANDED AREA APPLIED FILLER PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623001961995062300196NM 1995 6 23 P5CA9500018 119950530A5320 RIVET BOEING747 747122 1384872NM BS 2040 SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 RIVET HEAD SHEARED ON LAP SEAM NR 34R STA 2040 JUST AFT OF BULK CARGO DOOR. REMOVED RIVET, NO CORROSION FOUND CLEANED AND SEALED AREA AND REPLACED RIVET AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623001971995062300197NM 1995 6 23 P5CA9500019 119950530A7830 TR SLEEVE BOEING747 747122 1384872NM NR 1 ENGINE GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 FORWARD EDGE OF FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH. 2L74 4F A20WE 19950623001981995062300198NM 1995 6 23 P5CA9500020 119950603A3240 TIRE CAP BOEING747 747121 1384871NM NR 6 WHEEL DEPARTED A P5CAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 WP23832FT 20347 ON TAKEOFF, NR 6 TIRE CAP CAME OFF DAMAGING THE LEFT BODY GEAR DOOR FIXED ROD THE ROD DAMAGED NR 1 HYDRAULIC SYSTEM LINES (7 EACH), WHEEL WELL FIRE WARNING LOOP, AND APU PNEUMATIC DUCTING CAUSING LOSS OF NR 1 HYDRAULIC SYSTEM AND APU PNEUMATIC AIR. REPLACED DAMAGED LINES, WHEEL WELL FIRE LOOP, APU DUCT, DOOR ROD, AND WHEEL ASSEMBLY IN ACCORDANCE WITH BOEING MAINTENANCE MANUALS. 2L74 4F A20WE 19950623001991995062300199NM 1995 6 23 P5CA9500021 119950602A5730 TE PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL LOCATED FWD OF PANEL 571 CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09 FIG 10. 2L74 4F A20WE 19950623002001995062300200NM 1995 6 23 P5CA9500022 119950602A5730 TE PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A .5 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FWD OF NR 6 SPOILER. REPAIRED PANEL PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623002011995062300201NM 1995 6 23 P5CA9500023 119950602A5730 TE PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A 32 INCH CRACK IN LEFT WING TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER INBOARD END. REPAIRED IN ACCORDANCE WITH BOEING SRM 51-40-09. 2L74 4F A20WE 19950623002021995062300202NM 1995 6 23 P5CA9500024 119950602A5730 TE PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A 17 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER CENTER HINGE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623002031995062300203NM 1995 6 23 P5CA9500025 119950602A5720 RIVET BOEING747 747122 1384872NM WING POPPED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 RIVET HEAD POPPED ON FORWARD SPAR CAP AFT OF NR 9 SLAT, INBD END. REPLACED RIVET PER BOEING SRM 51-30-03. 2L74 4F A20WE 19950623002041995062300204NM 1995 6 23 P5CA9500026 119950602A575365B0853351 SKIN BOEING747 747122 1384872NM LT TE MID FLAP WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 LEFT WING OUTBOARD MIDFLAP OUTBOARD ENG WORN DOWN TO HONEYCOMB TOP SIDE. REPAIRED PER BOEING SRM 51-40-06 AND 51-70-09. 2L74 4F A20WE 19950623002051995062300205NM 1995 6 23 P5CA9500027 119950602A5720096520357 ROD BOEING747 747122 1384872NM LT WING LE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 LEFT WING LEADING EDGE SUPPORT ROD CRACKED AREA OF NR 2 LEFT LEADING EDGE PDU. REMOVED AND REPLACED SUPPORT ROD AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623002061995062300206NM 1995 6 23 P5CA9500028 119950602A5414 PLATE BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 NR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950623002071995062300207NM 1995 6 23 P5CA9500029 119950602A5512 PANEL BOEING747 747122 1384872NM RT HORIZ STAB DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 HOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950623002081995062300208NM 1995 6 23 P5CA9500030 119950602A2730 ROD END BOEING747 747122 1384872NM ELEVATOR RUSTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 RIGHT ELEVATOR HINGE NUT RUSTED AND ACTUATOR ROD END RUSTED. CLEANED AND TERATED AREA PER 747 SRM 51-12-01, LEVEL 1. 2L74 4F A20WE 19950623002091995062300209NM 1995 6 23 P5CA9500031 119950602A5321 FLOOR PLATE BOEING747 747122 1384872NM FS 603 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 PLATE TORN FLOOR AT STA 603 FWD OF BALL MAT AREA CENTER OF FLOOR. REPLACED PLATE AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623002101995062300210NM 1995 6 23 P5CA9500032 119950602A5330 SKIN BOEING747 747122 1384872NM FWD FUSELAGE GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 COPILOTS WINDSHIELD WIPER ARM HAS GOUGED FUSELAGE SKIN IN PARKED POSITION. SMOOTH BLENDED MILD GOUGE OUT PER BOEING SRM 51-10-01, RERIGGED WIPER. 2L74 4F A20WE 19950623002111995062300211NM 1995 6 23 P5CA9500033 119950602A5730 PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A 6 INCH CRACK IN FIBERGLASS PANEL FORWARD OF NR 8 SPOILER AT OUTBOARD END. REPAIRED CRACKED PANEL PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623002121995062300212NM 1995 6 23 P5CA9500034 119950602A5730 PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 1100 19756 A .25 INCH CRACK IN FIBERGLASS PANEL, FWD OF NR 9 SPOILER. REPAIRED PER SRM 51-40-09. 2L74 4F A20WE 19950623002131995062300213NM 1995 6 23 P5CA9500045 119950611A2910148065 SHUT OFF VALVE BOEING747 747132 1384882NM NR 2 HYD SYSTEM FAILED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23857FT 20246 NR 2 STABILIZER TRIM HYDRAULIC CONTROL CIRCUIT BREAKER POPPED. REMOVED AND REPLACED SYSTEM NR 2 HYDRAULIC SHUTOFF VALVE ACTUATOR ON STABILIZER TRIM HYDRAULIC MODULE. 2L74 4F A20WE 19950623002141995062300214NM 1995 6 23 P5CA9500046 119950611A324426019011 TIRE BOEING747 747124 1384874NM RT BODY GEAR BLOWN A P5CAK NONE O OTHER TOTAKEOFF 1 WP23855FT 19733 DURING TAKEOFF, SLIGHT SHUDDER FELT SUSPECTED TIRE DAMAGE, CONTINUED TAKEOFF. ON LANDING IN NAN FOUND NR 9 AND NR 10 TIRES BLOWN ALONG WITH MINOR DAMAGE TO RT INBOARD BODY GEAR SHOCK STRUT DOOR. ALSO, FOUND NR 12 WHEEL DAMAGED. REMOVED AND REPLACED NR 9, 10 AND 12 WHEEL AND TIRE ASSEMBLIES. PERFORMED INTERIM REPAIR ON GEAR DOOR. 2L74 4F A20WE 19950623002151995062300215NM 1995 6 23 P5CA9500047 119950419A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT84048 20347 DURING INSPECTION AND REPAIR PER AD 94-01-04, FOUND SEVERAL AREAS OF CORROSION IN THE UPPER AND LOWER LAP JOINTS AT STRINGER 4L. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, LEVEL 1. 2L74 4F A20WE 19950623002161995062300216NM 1995 6 23 P5CA9500048 119950419A5313 STRINGER BOEING747 747121 1384871NM BS 1595 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT84048 20347 DURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION STRINGER 4L AT BS 1595, LEVEL 2. REPLACED STRINGER SECTION PER BOEING SRM 53-10-3 FIGURE 5. 2L74 4F A20WE 19950623002171995062300217NM 1995 6 23 P5CA9500049 119950419A5313 STRINGER BOEING747 747121 1384871NM BS 1539 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT84048 20347 DURING INSPECTION/REPAIR PER AD 95-01-04, FOUND CORROSION BETWEEN FASTENER HOLES STRINGER 4L AT BS 1539. CLEANED CORROSION AND FOUND WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, ALODINED AND PRIMED. 2L74 4F A20WE 19950623002181995062300218NM 1995 6 23 P5CA9500050 119950612A3250 COVER BOEING747 747122 1384872NM NLG STEERING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 1100 19755 SMALL CRACK IN COVER AT LEFT INSPECTION HOLE ON NOSE GEAR STEERING CABLE COVER. BLENDED SMALL CRACK PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623002191995062300219NM 1995 6 23 P5CA9500051 119950612A5280 DOOR BOEING747 747122 1384872NM NLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 1100 19755 CRACK ON AFT INBOARD CORNER OF AFT LEFT NOSE GEAR DOOR. INSTALLED REPAIR PER BOEING SRM 51-40-03 PAGE 9-12. 2L74 4F A20WE 19950623002201995062300220NM 1995 6 23 P5CA9500052 119950612A5280 SKIN BOEING747 747122 1384872NM NLG DOOR WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 1100 19755 NOTCH WORN INTO OUTER SKIN AT RIGHT AFT NOSE GEAR DOOR, AFT HINGE CUTOUT. REPAIRED PER BOEING SRM 51-10-01 PAGE 20. 2L74 4F A20WE 19950623002211995062300221NM 1995 6 23 P5CA9500053 119950612A5280 DOOR BOEING747 747122 1384872NM NLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 1100 19755 CRACK IN AFT INBOARD CORNER OF AFT RIGHT NOSE GEAR DOOR. INSTALLED REPAIR AS PER BOEING SRM 51-40-03 PAGE 9-12. 2L74 4F A20WE 19950623002221995062300222NM 1995 6 23 P5CA9500054 119950612A5280 RIVET BOEING747 747122 1384872NM NLG DOOR SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 1100 19755 RIVET HEAD SHEARED ON AFT STRIKER PLATE FOR AFT LEFT NOSE GEAR DOOR, INBD CORNER. REPLACED RIVET AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623002231995062300223NM 1995 6 23 P5CA9500055 119950613A3244262603561X TIRE BOEING747 747124 1384874NM RT BODY GEAR BLOWN A P5CAK NONE O OTHER TOTAKEOFF 1 WP23855FT 21 19733 AFTER TAKEOFF OUT OF KHV, TOWER REPORTED RUBBER ON RUNWAY. ON LANDING IN ANC FOUND NR 9 AND NR 10 TIRES BLOWN. DAMAGE TO BODY GEAR DOOR LINKAGE, GEAR DOOR HANDLE, SEVERAL CONDUITS, HYDRAULIC LINES, PRESSURE WEB STIFFENERS. INVESTIGATING CAUSE OF FAILURES WILL UPDATE. 2L74 4F A20WE 19950623002241995062300224NM 1995 6 23 P5CA9500056 119950614A2741S334 SWITCH BOEING747 747122 1384872NM STABILIZER FAILED A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23851FT 19756 DURING TAXI FOR TAKEOFF, CONSTANT TAKEOFF WARNING. RECYCLED ALL FLIGHT CONTROLS, NO HELP. RETURNED TO BLOCKS, OPERATIONAL CHECK OK PER BOEING MAINTENANCE MANUAL 31-26-00. 2L74 4F A20WE 19950623002251995062300225NM 1995 6 23 P5CA9500057 119950614A5753 TE SKIN BOEING747 747122 1384872NM RT TE MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23854FT 600 19754 DURING POST FLIGHT INSPECTION, FOUND RIGHT OUTBOARD TRAILING EDGE MIDFLAP DAMAGED AND DELAMINATED. REPAIRED IN ACCORDANCE WITH BOEING SRM. 2L74 4F A20WE 19950623002261995062300226NM 1995 6 23 P5CA9500058 119950616A323065B21500523524 RETRACT MECH BOEING747 747122 1384872NM LANDING GEAR LACK OF LUBE A P5CAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 WP23850FT 2798 19755 AFTER TAKEOFF LEFT AND RIGHT WING LANDING GEAR WOULD NOT RETRACT. DUMPED FUEL, RETURNED TO MIA. LUBRICATED LANDING GEAR, CHECKED ALL RIGGING. FUNCTIONAL CHECKED GOOD, RETURNED TO SERVICE. 2L74 4F A20WE 19950623002271995062300227NM 1995 6 23 UPS203587 119950616A5712 RIB BOEING727 72731C 1384011NM BS 760.95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-MAINTENANCE, FOUND CRACKS ON WING RIB UPPER CHORD AT BS 760.95. REPAIRED IAW EO B727-5710-1271. 2L73 4F A3WE 19950623002281995062300228NM 1995 6 23 UPS203588 119950616A5712 RIB BOEING727 72731C 1384011NM BS 758.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-MAINTENANCE, FOUND CRACK ON VERTICAL FLANGE OF RIB CHORD AT BS 758.5, RT SIDE. REPAIRED IAW B727-55710-1271. 2L73 4F A3WE 19950623002291995062300229NM 1995 6 23 UPS203589 119950616A5712 RIB BOEING727 72731C 1384011NM BS 760.95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01925UP 19230 WHILE IN NAPLES FOR C-MAINTENANCE, FOUND ON WING RIB UPPER CHORD AT BS 760.95. REPAIRED IAW EO B727-5710-1271. 2L73 4F A3WE 19950623002301995062300230NM 1995 6 23 UPS203590 119950616A5312 BULKHEAD BOEING727 72725C 138400HNM BS 178 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON BULKHEAD BS 178, RBL 1 WL 197. REAPIRED IAW SRM 53-10-9, 53-10-2. 2L73 4F A3WE 19950623002311995062300231NM 1995 6 23 UPS203591 119950616A5330 SKIN BOEING727 72725C 138400HNM BS 1228 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACK ON EXTERNAL SKIN AT BS 1228, RBL 9 WL 148. REPAIRED IAW SRM 53-30-3. 2L73 4F A3WE 19950623002321995062300232NM 1995 6 23 UPS203592 119950616A5330 SKIN BOEING727 72725C 138400HNM BS 400 LIGHTNING STRIKEA IPXAK NONE C F.O.D. ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND DAMAGE TO SKIN DUE TO LIGHTNING AT STA 400, STR 4 LT. REPAIRED IAW SRM 53-30-3, 51-10-2, 51-30-2, 51-20-4. 2L73 4F A3WE 19950623002331995062300233NM 1995 6 23 UPS203593 119950616A5753 SKIN BOEING727 72725C 138400HNM RT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON R/W O/B AFT FLAP ON UPPER SKIN 14 INCHES FROM I/B SIDE. REPAIRED IAW SRM 51-40-06. 2L73 4F A3WE 19950623002341995062300234NM 1995 6 23 UPS203594 119950616A551165956138 RIB BOEING727 72725C 138400HNM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CRACKED SUPPORT RIB ON RT HORIZ STAB T/E AT STA 99.79. REPLACED RIB IAW SRM 51-20-4, 51-20-5, 57-30-2, M/M 27-30-5. 2L73 4F A3WE 19950623002351995062300235NM 1995 6 23 UPS203595 119950616A5320 SHEAR WEB BOEING727 72725C 138400HNM BS 1173 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON SHEAR WEB AND HAT CHANNEL AT BS 1173, LBL 23 TO 28 WL 208. REPLACED HAT CHANNEL AND WEB IAW SRM 57-10-2, 51-30-2, 51-30-8, 51-40-2, 53-10-1. 2L73 4F A3WE 19950623002361995062300236NM 1995 6 23 UPS203596 119950616A5711 SPAR BOEING727 72725C 138400HNM WS 198 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER CHORD OF LEFT WING REAR SPAR AT WS 198.0. REPAIRED IAW SRM 57-10-6, 51-30-2, M/M 28-11-0. 2L73 4F A3WE 19950623002371995062300237NM 1995 6 23 UPS203597 119950616A5230 DOOR BOEING727 72725C 138400HNM AFT CARGO CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON MAIN CARGO DOOR AFT LIFT ACTUATOR LOWER CUTOUT. REPAIRED IAW EO B727-52-0153. 2L73 4F A3WE 19950623002381995062300238NM 1995 6 23 UPS203598 119950616A5753 SKIN BOEING727 72725C 138400HNM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN FOR C-CHECK MAINTENANCE, FOUND DELAMINATION ON L/W I/B FLAP. REPAIRED IAW SRM 51-40-6, M/M 51-20-0. 2L73 4F A3WE 19950623002391995062300239NM 1995 6 23 UPS203614 119950616A575265849505 TAB BOEING727 72725C 138400HNM AILERON CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01950UP 19718 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON L/W O/B AILERON TAB, I/B TAB CORRODED. INSTALLED TAB IAW SRM 51-10-1, M/M 27-10-4. 2L73 4F A3WE 19950623002401995062300240NM 1995 6 23 UPS403615 119950619A5311 FRAME BOEING747 747123 1384873NM FS 360 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CRACK IN FRAME AT STA 360 LT BETWEEN STR 25 AND 26. REPAIRED IAW 747-53-0066. 2L74 4F A20WE 19950623002411995062300241NM 1995 6 23 UPS403616 119950619A5313 STRINGER BOEING747 747123 1384873NM FS 2160 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CORROSION ON STRING 45 AT STA 2160, 30 RBL. REPAIRED IAW SRM 51-10-07, 53-10-07, 53-10-03. 2L74 4F A20WE 19950623002421995062300242NM 1995 6 23 UPS403617 119950619A5720 CHORD BOEING747 747123 1384873NM WS 440 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND RT WING UPPER T-CHORD CRACKED ON FWD SIDE WS 440. REPAIRED IAW EO 747-57-0257. 2L74 4F A20WE 19950623002431995062300243NM 1995 6 23 UPS403628 119950619A5347 SEAT TRACK BOEING747 747123 1384873NM FS 510 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE IN AMSTERDAM FOR C-CHECK MAINTENANCE, FOUND CORROSION ON SEAT TRACK STA 510, RBL 58. REPLACED TRACK IAW SRM 53-10-5. 2L74 4F A20WE 19950623002441995062300244NM 1995 6 23 UPS403630 119950618A3350 EEL BOEING747 747123 1384873NM UPPER DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 WHILE ON GROUND IN SDF, MAINTENANCE FOUND UPPER ESCAPE SLIDE DOOR AFT EMER LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW M/M 33-51-04. OPS CHECK GOOD. 2L74 4F A20WE 19950623002451995062300245NM 1995 6 23 UPS503629 119950617A3350 EEL BATTERY PACK BOEING757 75724APF 1384969NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01446UP 27735 WHILE ON GROUND IN SDF, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. 2L72 4F RTA2NM 19950623002461995062300246WP 1995 6 23 UPS803599 119950616A53139753768 LONGERON DOUG DC8 DC871F 302199DWP FS 1020 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER LONGERON 21R, FS 1020. REPAIRED IAW SRM 53-2-5. 2L74 4F RT4A25 19950623002471995062300247WP 1995 6 23 UPS803600 119950616A5320 SUPPORT DOUG DC8 DC871F 302199DWP FS 70 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON UPPER RT HORIZ SUPPORT FS 70, BULKHEAD RBL 65. REPLACED SUPPORT IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002481995062300248WP 1995 6 23 UPS803601 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 7075 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON END FITTING 30R AT FS 7075. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002491995062300249WP 1995 6 23 UPS803602 119950616A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 200-220 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON ANTENNA DOUBLER FS 200 TO 220, AND FS 360 TO 380, LONGS 35L TO 35R. REPLACED DOUBLER IAW SRM 51-3-2. 2L74 4F RT4A25 19950623002501995062300250WP 1995 6 23 UPS803603 119950616A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 400-450 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON FINGER DOUBLER AT FS 400 TO 450, LONG 31R. REPLACED DOUBLER IAW SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 19950623002511995062300251WP 1995 6 23 UPS803604 119950616A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 460 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BELT FRAME REINFORCEMENT DOUBLER AT FS 460, LONG 27R TO 29R. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950623002521995062300252WP 1995 6 23 UPS803605 119950616A5311 FRAME DOUG DC8 DC871F 302199DWP FS 460 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BELT FRAME FWD SIDE, FS 460 BETWEEN LONGS 29R TO 31R. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950623002531995062300253WP 1995 6 23 UPS803606 119950616A5313975491332N LONGERON DOUG DC8 DC871F 302199DWP FS 240-387 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 35L, FS 240 TO 387. REPLACED LONGERON IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002541995062300254WP 1995 6 23 UPS803607 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 190-205 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 36 END FITTING, FS 190 TO 205. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002551995062300255WP 1995 6 23 UPS803608 119950616A5313475491335 LONGERON DOUG DC8 DC871F 302199DWP FS 230-235 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON LONGERON 35R, FS 285, I/B SIDE AND O/B SIDE AT FS 230 TO 235. REPLACED LONGERON SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002561995062300256WP 1995 6 23 UPS803609 119950616A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 450-610 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON FINGER DOUBLER, FS 450 TO 610, LONG 31L AND FS 456, LONGS 32L TO 31R. REPLACED DOUBLER IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002571995062300257WP 1995 6 23 UPS803610 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1160 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 1160, FS 1200 BETWEEN LONGS 34R TO 35R. REPLACED FITTINGS IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002581995062300258WP 1995 6 23 UPS803611 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 320 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 320, BETWEEN LONGS 34L TO 35L AND LONGS 34L AND 33L. REPLACED FITTINGS IAW SRM 51-1-20D, 53-2-0. 2L74 4F RT4A25 19950623002591995062300259WP 1995 6 23 UPS803612 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 280 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 280, BETWEEN LONGS 34L TO 35L AND LONGS 34R AND 35R. REPLACED FITTINGS IAW SRM 51-1-20D, 53-2-0. 2L74 4F RT4A25 19950623002601995062300260WP 1995 6 23 UPS803613 119950616A5320 FITTING DOUG DC8 DC871F 302199DWP FS 270/300 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BATHTUB FITTING AT FS 270 AND FS 300, BETWEEN LONGS 34R TO 35. REPLACED FITTINGS IAW SRM 53-2-0. 2L74 4F RT4A25 19950623002611995062300261WP 1995 6 23 UPS803618 119950619A532052651332 CHANNEL DOUG DC8 DC871F 302199DWP FS 857-880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON CHANNEL BETWEEN FS 880 TO 857, LBL 15 TO 30. REPLACED CHANNEL IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002621995062300262WP 1995 6 23 UPS803619 119950619A5532 SKIN DOUG DC8 DC871F 302199DWP VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION AND CRACKS AROUND FASTENERS AT VERTICAL STAB LEADING EDGE ON UPPER EDGE LT SIDE. REPAIRED IAW SRM 55-2-0. 2L74 4F RT4A25 19950623002631995062300263WP 1995 6 23 UPS803620 119950619A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 220-420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON INNER DOUBLER FS 220 TO 420, LONG 31R. REPLACED DOUBLER IAW SRM 51-1-20D. 2L74 4F RT4A25 19950623002641995062300264WP 1995 6 23 UPS803621 119950619A5330 SKIN DOUG DC8 DC871F 302199DWP FS 190-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION BULGES AT FUSELAGE BELLY SKIN STA 190 TO 450. REPLACED SKIN. 2L74 4F RT4A25 19950623002651995062300265WP 1995 6 23 UPS803622 119950619A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND 1 CRACK FWD UPPER SKIN AROUND FUEL SERVICE DOOR. REPAIRED IAW SRM DC8-5310-7089-A. 2L74 4F RT4A25 19950623002661995062300266WP 1995 6 23 UPS803623 119950619A531297537513 BULKHEAD DOME DOUG DC8 DC871F 302199DWP FS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED AFT PRESSURE BULKHEAD DOME FS 683, LONG 31L TO 30L. REPAIRED IAW EO DC8-5310-7080-A. 2L74 4F RT4A25 19950623002671995062300267WP 1995 6 23 UPS803624 119950619A53135750198 LONGERON DOUG DC8 DC871F 302199DWP FS 857 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED LONGERON 24R ABOVE BOTTLE BOLT, FS 857. REPAIRED LONGERON IAW SRM 53-2-2, 51-1-20D. 2L74 4F RT4A25 19950623002681995062300268WP 1995 6 23 UPS803625 119950619A53135750196 LONGERON DOUG DC8 DC871F 302199DWP FS 980 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CRACKED LONGERON 24L FS 980. REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19950623002691995062300269 1995 6 23 UPS803626 419950619A25655779894 ESCAPE SLIDE DOUG DC8 DC871F 302199DWP DOOR SEPARATING A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND ESCAPE SLIDE CASE SEPARATING AT THE TOP. REPAIRED IAW SRM 51-1-2. 2L74 4F RT4A25 19950623002701995062300270WP 1995 6 23 UPS803627 119950619A52304754597 FRAME DOUG DC8 DC871F 302199DWP CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN C-CHECK MAINTENANCE, FOUND CORROSION ON BOTTOM FWD FRAME ON A CROSS SLIDE DOOR AND 2 INCH LONG CRACK. REPLACED FRAME SECTION IAW SRM 51-1-20A, 51-1-21. 2L74 4F RT4A25 19950623002711995062300271WP 1995 6 23 9509539986 119950615A5350 LATCH PIN DOUG DC9 DC932 3022066WP TAILCONE MALFUNCTIONED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01986US 47480 DURING PERIODIC CHECK, FOUND THAT THE TAILCONE DID NOT DROP DUE TO THE LOWER LEFT LATCH. REPLACED THE LATCH PIN AND RERIGGED THE TAILCONE. 2L72 4F A6WE 19950623002721995062300272NM 1995 6 23 9509542709 119950607A5341 RIB BOEING727 727225 1384077NM FS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING H-CHECK, FOUND CRACKS IN THE RIGHT WING-TO-BODY UPPER RIB CHORD BS 760 AT RBL 70.5. REPAIRED CHORD (P/N 65-18522-14) PER EA 27-98434. 2L73 4F A3WE 19950623002731995062300273NM 1995 6 23 9509552709 119950609A5311 FRAME BOEING727 727225 1384077NM FS 1303 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING H-CHECK, FOUND TWO, 2 INCH CRACKS IN THE BS 1303 FRAME BETWEEN THE LEFT AND RIGHT TORQUE BOXES AT THE LOWER LEFT AND RIGHT CORNERS. REPAIRED THE FRAME (P/N 65-17506) PER EA 27-98457. 2L73 4F A3WE 19950623002741995062300274NM 1995 6 23 9509566729 119950610A5347 SEAT TRACK BOEING747 747251F 1384898NM FS 1960-1982 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01629US 22388 DURING PERIODIC CHECK, FOUND CORROSION IN THE RBL 11 SEAT TRACK CROWN FROM BS 1960 TO 1982. REPLACED SEAT TRACK (P/N 65B38274-2) PER EA 67-98620. 2L74 4F A20WE 19950623002751995062300275WP 1995 6 23 9509579976 119950610A5320 DOOR JAMB DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019340 47389 DURING PERIODIC CHECK, FOUND CRACKS IN THE FORWARD PASSENGER DOOR JAMB, AFT SIDE EXTERNAL SKIN AT THE 1ST AND 4TH DOOR STOP HOLES. REPAIRED PER EA 99-97086. 2L72 4F A6WE 19950623002761995062300276WP 1995 6 23 9509589178 119950614A5210 FLANGE DOUG DC9 DC914 3022034WP AFT CABIN DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013310L 45705 DURING LINE CHECK, FOUND A 4 INCH CRACK IN THE AFT CABIN DOOR LOWER LEFT FLANGE. REPLACED DOOR PER MM. 2L72 4F A6WE 19950623002771995062300277WP 1995 6 23 9509599612 119950614A5320 FITTING DOUG DC9 DC932 3022066WP FS 994 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 23L END FITTING AT FS 994. REPLACED THE END FITTING PER SRM 53-01. 2L72 4F A6WE 19950623002781995062300278WP 1995 6 23 9509609612 119950614A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE TAIL JACK ADAPTER FITTING AT FS 996, ABOVE THE AFT FUSELAGE BELLY SKIN. REPLACED FITTING PER SRM 53-01. 2L72 4F A6WE 19950623002791995062300279WP 1995 6 23 9509619986 119950614A5330 SKIN DOUG DC9 DC932 3022066WP FS 579 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01986US 47480 DURING PERIODIC CHECK, FOUND CORROSION IN THE SKIN AT FS 579 BETWEEN LONGERONS 28R TO 29R. REPLACED SKIN (P/N 5911412-157) PER EA 99-99789. 2L72 4F A6WE 19950623002801995062300280WP 1995 6 23 9509629944 119950615A5320 FITTING DOUG DC9 DC931 3022065WP FS 718 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 15L END FITTING AT FS 718. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19950623002811995062300281WP 1995 6 23 9509639971 119950615A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND A .25 INCH CRACK IN THE AFT CARGO DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING. 2L72 4F A6WE 19950623002821995062300282WP 1995 6 23 9509649986 119950615A5313 LONGERON DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01986US 47480 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT CUSP LONGERON 18R AT FS 996. REPAIRED CUSP (P/N 9910503-4) PER EA 99-99793. 2L72 4F A6WE 19950623002831995062300283EU 1995 6 23 9509653216 119950619A2150 BUSHING AIRBUS320 A320211 3930320EU RAM AIR DOOR WORN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01316US 192 DURING CLIMBOUT AT 22,000 FEET AND 315 KNOTS, AIRCRAFT BEGAN VIBRATING. VIBRATION WAS FELT THROUGHOUT THE CABIN. ENGINE VIBRATION MONITORS WERE NORMAL. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT FORWARD END RAM AIR INLET DOOR ACTUATOR BUSHING. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950623002841995062300284NM 1995 6 23 9509662717 119950612A7711 EPR TRANSMITTER BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 3 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01721RC 22492 707904 ON TAKEOFF, THE NR 3 ENGINE EPR INDICATION WAS UNSTABLE AND EXCEEDED THE TARGET VALUE OF THE DAY. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE. THE NR 3 EPR SYSTEM WAS PLACED ON MEL AND THE AIRCRAFT CONTINUED IN SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED THE EPR TRANSMITTER. THE ENGINE WAS RUNUP AND CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950623002851995062300285NM 1995 6 23 95UAL737082 119950607A528063023 SENSOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CARGO DOOR OUT OF ADJUST A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29309UA 23670 RETURNED TO FIELD WITH CARGO DOOR WARNING LIGHT. ADJUSTED PROX PLATE FOR DOOR WARNING SENSOR. OPS CHECKS OK. DOOR WAS FOUND CLOSED AND SECURED UPON ARRIVAL AT SFO. 2L72 4F4 FRTA16WE E2GL 19950623002861995062300286NM 1995 6 23 95UAL900004 119950619A2910 HYD HOSE AE2464163E01BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE RIGHT FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP299053U 19934 RETURNED TO FIELD UNDER AN AMBER ALERT DUE TO LOSS OF HYDRAULIC PRESSURE. RIGHT UPLOCK ACTUATOR HOSE FAILED AT THE B-NUT. REPLACED HOSE SYSTEM OP CHECKS OK. 2L72 4F4 F A16WE E2EA 19950623002871995062300287NM 1995 6 23 95UAL900005 119950619A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29581UA 26701 EMERGENCY LIGHT AT ROW 33 BULLNOSE INOP. RELAMPED, OPS CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950623002881995062300288NM 1995 6 23 95UAL900006 119950619A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29565UA 26669 RIGHT FORWARD EMERGENCY OVERWING LIGHT INOP. RELAMPED, OPS CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950623002891995062300289NM 1995 6 23 95UAL900007 119950619A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29572UA 26682 LEFT FORWARD EMERGENCY OVERWING LIGHT INOP. RELAMPED, OPS CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950623002901995062300290NM 1995 6 23 95UAL900008 119950619A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE DOOR 1 L/R INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297263U 21410 DOOR 1 LT AND RT EMERGENCY SLIDE LIGHT IS ON WITH EMERGENCY EXIT LIGHT SWITCH IN THE OFF POSITION. REPLACED EMERGENCY SLIDE LIGHT BATTERY AND POWER SUPPLY. 2L73 4F4 F A3WE E2EA 19950623002911995062300291NM 1995 6 23 95UAL900009 119950619A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297299U 21894 LEFT EMERGENCY GROUND ILLUMINATION LIGHT INOP. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950623002921995062300292NM 1995 6 23 95UAL900011 119950620A3350 EEL BATTERY PACK BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29992UA 22089 EEL LIGHTING EXIT MARKER AT AFT ENTRY DOOR INOP. REPLACED BATTERY. 2L72 4F4 F A16WE E2EA 19950623002931995062300293NM 1995 6 23 95UAL900012 119950620A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297262U 21409 LEFT OVERWING EEL LIGHT INOP. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950623002941995062300294WP 1995 6 23 ABXA9500559 119950619A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23956AX 3197 47620 DURING PREDEPARTURE CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 SUPP MM 33-50-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950623002951995062300295NE 1995 6 23 ABXA9500560 219950615A7200JT8D9A ENGINE DOUG DC9 DC933F 302207AWP PWA JT8 JT8D9A 52048NE LEFT FAILED A ABXACED ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL23934AX35218218 47462 667084 ON TAKEOFF ROLL, HEARD A LOUD EXPLOSION, FOLLOWED BY A VIBRATION AND A LOSS OF POWER ON THE LEFT ENGINE. EGT REACHED 680 DEGREES. REPLACED THE NR 1 ENGINE IAW ABX JOB CARD J7001. OPS CHECKED GOOD, NO LEAKS NOTED AT THIS TIME. 2L72 4F4 F A6WE E2EA 19950623002961995062300296SO 1995 6 23 2XA95IA094 119950528A572012017063011 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING RIB NR 15, NR 1 FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623002971995062300297WP 1995 6 23 95ZZZZ264 119950512A323057146745503 CONTROL VLV DOUG DC8 DC863F 302198FWP MLG DEFECTIVE A RRXAO OTHER J WARNING INDICATION CLCLIMB 1 WP15952R 46061 KDAL-KORD - FLT 35 - DOOR WARNING AND UPLATCH WARNING LIGHTS ON AFTER GEAR RETRACTION. RECYCLED GEAR AND WARNING LIGHTS EXTINGUISHED. MAINTENANCE REMOVED AND REPLACED THE MLG CONTROL VALVE. OPERATIONAL CHECK OF THE MLG RETRACTION AND WARNING SYSTEM WAS GOOD. 2L74 4F 4A25 19950623002981995062300298SO 1995 6 23 95ZZZZ265 119950515A3246GYS187C35 BOLT GULSTMG1159 G1159 3953505SO NR 2 WHEEL BROKEN A KKYAK NONE O OTHER ININSP/MAINT 1 NE03220FL 50 DURING A POST FLT INSPECTION, MAINTENANCE FOUND A BROKEN BOLT ON THE NR 2 MLG WHEEL. FLT CREW INDICATED THAT ALL OPS WERE NORMAL. WHEEL WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA12EA 19950623002991995062300299NE 1995 6 23 95ZZZZ266 219950523A7200 ENGINE DOUG DC8 DC8F54 3021926WP PWA JT3D JT3D* 52039NE NR 2 FAILED A FXLAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19427FB 45684 MIA - IN CLIMB, THE NR 1 ENGINE EGT INCREASED AND EXPERIENCED ENGINE VIBRATION. SHUTDOWN NR 1 ENGINE AND RETURNED AND LANDED AT MIA WITHOUT INCIDENT. INSPECTION REVEALED METAL IN THE TAIL PIPE. REPLACED NR 1 ENGINE. 2L74 4F4 F 4A25 1E8 19950623003001995062300300SO 1995 6 23 C2XA95IA092 119950528A572012017063004 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 15, NR 4 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003011995062300301SO 1995 6 23 C2XA95IA093 119950528A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING 15, NR 3 FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003021995062300302SO 1995 6 23 C2XA95IA095 119950528A572012004357009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 2 LOWER FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003031995062300303SO 1995 6 23 C2XA95IA096 119950528A572012004356009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING, RIB 15, NR 2 FROM FWD SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003041995062300304SO 1995 6 23 C2XA95IA098 119950528A572012017056014 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916731 120190 IAH - DURING C-CHECK INSPECTION, THE RT WING RIB 16, NR 2 UPPER FROM AFT SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003051995062300305WP 1995 6 23 ORJA9531 119950505A335041B004AD073 EEL BATTERY DOUG DC9 DC987 3022087WP OVERWING DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11750RA 49777 EMERGENCY OVERWING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY OVERWING LIGHTING POWER SUPPLY. OPS CHECK GOOD. (Z) 2L72 4F RTA6WE 19950623003061995062300306WP 1995 6 23 ORJA9532 119950505A335041B004AD073 EEL BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11871RA 49788 CEILING EMERGENCY LIGHTS INOP IN FWD PART OF COACH CABIN. REMOVED AND REPLACED BATTERY, OP CHECK NORMAL. (Z) 2L72 4F RTA6WE 19950623003071995062300307WP 1995 6 23 ORJA9533 119950510A335041B004AD073 EEL BATTERY DOUG DC9 DC983 3022083WP EMPENNAGE OVHD DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11878RA 53184 EMPENNAGE OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS NORMAL. (Z) 2L72 4F RTA6WE 19950623003091995062300309EU 1995 6 23 VTZA95184 119950521A73321103P171 LOW PRESS SW BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27484UE 899 IAD-ORF - FLT 6531 - DURING THE TAKEOFF ROLL, ABORTED THE TAKEOFF DUE TO THE LT ENGINE FUEL LOW PRESSURE WARNING LIGHT ILLUMINATED. ACFT RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT ENGINE FUEL LOW PRESSURE SWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950623003101995062300310EU 1995 6 23 VTZA95187 119950526A73321103P0645 FUEL PRESS SW BAG JETSTMJETSTM3201 1500217EU LT NACELLE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27484UE 899 LYH-IAD - FLT 6186 - DURING THE TAKEOFF ROLL, ABORTED THE TAKEOFF DUE TO THE LT FUEL PRESSURE CAP LIGHT ILLUMINATING. ACFT RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03627 IAW MEL 73-2. MAINTENANCE LATER CLEARED DMI NR 03627 ON 5-29-95 BY REPLACING THE FUEL PRESSURE SWITCH. ACFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (Z) 2L72 4T RTA56EU 19950623003111995062300311WP 1995 6 23 WTAA950196 219950522A732189737526 FCU BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A WTAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP17430UE 784 PSC-SEA - EN ROUTE, THE LT ENGINE TORQUE FLUCTUATION REPORTED. ACFT DIVERTED TO YKM. CREW REPORTED LT ENGINE TORQUE REMAINED AT 40 PERCENT WITH ENGINE AT FLIGHT IDLE. CREW ACCOMPLISHED INFLIGHT SHUTDOWN OF LT ENGINE. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT ENGINE FUEL CONTROL UNIT. ENGINE OPERATIONAL AND LEAK CHECK NORMAL DURING ENGINE GROUND RUN. ACFT RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA21EU E4WE 19950623003121995062300312WP 1995 6 23 WTAA950197 219950528A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17428UE 806 THE LT ENGINE FAILED TO OBTAIN REQUIRED TAKEOFF TORQUE. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUN. ALL ENGINE PARAMETERS NORMAL. UNABLE TO DUPLICATE DISCREPANCY. ACFT RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA21EU E4WE 19950623003131995062300313SO 1995 6 23 WTAA950198 119950529A7720ST3152 TRIM RESISTOR EMB 120 EMB120RT SO LT ENGINE FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17451UE 120108 FAT - THE LT ENGINE T6 LIMITED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE TRIM RESISTOR, PERFORMED ENGINE GROUND RUN. ALL ENGINE PARAMETERS WITHIN LIMITS. ACFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003141995062300314SO 1995 6 23 WTAA950199 119950529A215012011639001 CHECK VALVE EMB 120 EMB120RT SO FS 10587,0 FAILED A WTAAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP17122AM 120013 SMF - OIL ODOR REPORTED IN CABIN FROM LT AIR CONDITIONING PACK ON GROUND. PACK FAILS TO COOL CABIN. MAINTENANCE DEFERRED LT PACK PER MEL 21-50-2. MAINTENANCE SUBSEQUENTLY CLEARED THE PREVIOUS DEFERRAL WITH THE REPLACEMENT OF THE LT RAM AIR CHECK VALVE. LT PACK OPERATIONAL CHECK NORMAL. ACFT RETURNED TO SERVICE. (Z) 2L72 4T RTA31SO 19950623003151995062300315WP 1995 6 23 WTAA950200 219950530A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LEFT MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17401UE 729 SFO - THE LT ENGINE FAILED TO OBTAIN REQUIRED TAKEOFF POWER DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED ENGINE GROUND RUN. UNABLE TO DUPLICATE REPORTED DISCREPANCY. ALL ENGINE PARAMETERS NORMAL DURING GROUND RUN. ACFT RETURNED TO SERVICE. (Z) 2L72 4T4 TRTA21EU E4WE 19950623003171995062300317CE 1995 6 23 95ZZZX3075 119950605A812047090813 VALVE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO WASTEGATE DETERIORATED A HYIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NE0168391 1773 402C0483 PILOT ABORTED TAKEOFF DUE TO ENGINE OVERBOOST. FOUND TOP SECTION OF BUTTERFLY VALVE WARPED DUE TO HEAT. FOUND THAT ON WASTEGATES OVERHAULED USING CONTINUED TIME VALVES, THIS OFTEN HAPPENS ALONG WITH VARING MANIFOLD PRESSURE. ON COMPONENTS WITH NEW VALVES INSTALLED AT OVERHAUL, NO PROBLEMS ARE NOTED THROUGH THE LIFE OF THE COMPONENT - 2100 HRS. 1L72 3O3 O A7CE E8CE 19950623003261995062300326EA 1995 6 23 95ZZZX3084 219950426A8530LW12966 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HEAD NR 1 CYL HOLE E F2PAE ENGINE SHUTDOWN EK VIBRATION/BUFFET FLUID LOSS APAPPROACH 1 SO19684JJ 317952194 L486361A DURING AN APPROACH TO LANDING, PILOT REPORTED A VIBRATION IN THE LEFT ENGINE AND OIL LEAKING FROM THE COWLING. HE PERFORMED A PRECAUTIONARY SHUT DOWN AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A HOLE IN NR 1 CYLINDER UNDER THE INTAKE PUSHROD HOUSING. THE HOLE ALLOWED EXHAUST GASSES TO BURN A HOLE IN THE HOUSING ALLOWING OIL LEAKAGE. SUSPECT PROBLEM MAY HAVE BEEN CAUSED BY A POOR WELD. 1L72 3O3 O A20SO E14EA 19950623003301995062300330CE 1995 6 23 95ZZZX3088 119950609A36105555043148 COUPLING CESSNA500 S550 2076607CE RT ENG INBD DEFECTIVE A DXTAK NONE O OTHER ININSP/MAINT 1 GL07274QS3115 S5500074 THE INBOARD PERI-SEAL COUPLING WAS FOUND WITH THE FORWARD END PULLED OUT OF THE RETAINER. REPLACED THE FORWARD DUCT ASSY, THE RETAINER AND BOTH PERI-SEALS ON INBOARD SIDE OF THE RT ENGINE. THIS WAS DISCOVERED DURING INSPECTION AND, IF LEFT, IT MAY HAVE COME APART. 1L72 4F RTA22CE 19950623003421995062300342 1995 6 23 95ZZZM61 419950518A25624530150 ELT ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE BROKEN A JJBAK NONE O OTHER UKUNKNOWN 1 EA01848CA2358 UE53 DURING DETAILED INSPECTION, ELT MOUNTING TRAY (PLASTIC) P/N 452-3050 WAS DISCOVERED BROKEN IN NUMEROUS PIECES RENDERING ELT INOPERATIVE. MOUNTING TRAY WAS REPLACED WITH NEW UNIT. (M) 2L72 4T RTA24CE 19950623003431995062300343 1995 6 23 95ZZZM62 419950424A25624530150 ELT ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER UKUNKNOWN 1 EA01833CA1404 52426 UE24 ELT TRANSMITS CONTINOUSLY. COMPLETE UNIT CONTAMINATED WITH MOISTURE. REMOVED AND REPLACED ELT ASSEMBLY. 2L72 4T RTA24CE 19950623003441995062300344 1995 6 23 95ZZZM63 419950429A25624530150 ELT ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE BROKEN A JJBAK NONE O OTHER UKUNKNOWN 1 EA01831CA UE20 ELT TRANSMITTING (45 MINUTES). FOUND UNIT WET AND MOUNTING TRAY CRACKED. REMOVED AND REPLACED MOUNTING TRAY, P/N 452-3050. 2L72 4T RTA24CE 19950623003451995062300345NE 1995 6 23 95ZZZM64 219950523A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE NR 2 FAILED A VJ6AA UNSCHED LANDING E VIBRATION/BUFFET DEDESCENT 1 SO11907VJ 47444 655214 FLT 248 - EN ROUTE FROM ATL TO MDW DIVERTED TO IND, CREW FELT VIBRATIONS FROM THE NR 2 ENGINE AND HAD 2 COMPRESSOR STALLS AS WELL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE (RT SIDE). 2L72 4F4 F A6WE E2EA 19950623003461995062300346NM 1995 6 23 95ZZZM65 119950527A32311U1085 SEQUENCE VALVE BOEING727 72744C 1384100NM MLG DOOR WORN A RYNAO OTHER J WARNING INDICATION APAPPROACH 1 CE072688Z 20476 ON APPROACH INTO SAIPAN, THE LEFT MAIN LANDING GEAR DOOR RED WARNING LIGHT STAYED ON WHEN GEAR WAS SELECTED TO DOWN, PERFORMED MANUAL GEAR EXTENSION AND LIGHT EXTINGHISHED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE MAIN LANDING GEAR DOOR SEQUENCE VALVE, OPS CHECKED GOOD. 2L73 4F A3WE 19950623003471995062300347WP 1995 6 23 95ZZZM66 119950522A5313 LONGERON DOUG DC8 DC863F 302198FWP FS 1070-1090 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 LEVEL II CORROSION FOUND ON OUTBOARD FLANGE OF LONGERON 31R BETWEEN FS 1070 AND FS 1090. 2L74 4F 4A25 19950623003481995062300348WP 1995 6 23 95ZZZM67 119950518A5320 STIFFENER DOUG DC8 DC863F 302198FWP FS 980 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 LEVEL II CORROSION FOUND AFT SIDE FS 980.00 BULKHEAD AT LONGERON 30L ATTACHMENT. 2L74 4F 4A25 19950623003491995062300349NM 1995 6 23 95ZZZM68 119950526A5320 SILL BOEING747 747122 1384872NM CARGO COMPT CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT69304 19753 B-CHECK INSPECTION, FOUND CORROSION ON FORWARD CARGO COMPARTMENT LOWER SILL (LEVEL 1). REMOVED CORROSION AND TREATED IAW WITH BOEING SRM 51-10-01. AIRCRAFT TOTAL CYCLES 18,040. (M) 2L74 4F A20WE 19950623003501995062300350NM 1995 6 23 ASAA9510053 119950521A335086210144 EEL BATTERY PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST TXTAXI/GRND HDL 1 NM01741AS 21959 SEA - FLT 7958 - SMOKE BARRIER EMERGENCY EXIT LIGHT ILLUMINATED ON THE GROUND. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950623003511995062300351NM 1995 6 23 ASAA9510054 119950530A335086210144 EEL BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 ANC - DURING MAINTENANCE CHECK, THE FORWARD SMOKE BARRIER EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950623003521995062300352NM 1995 6 23 ASAA9510055 119950601A33506012541 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950623003531995062300353NM 1995 6 23 ASAA9540023 119950523A3350S417N5048 EEL ASSY BOEING737 7374Q8 NM CABIN DAMAGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 EMERGENCY FLOOR TRACK LIGHTS INOP AFT OF ROW 27. MAINTENANCE REPLACED ROW 27 LIGHT ASSY. (M) 2L72 4F RTA16WE 19950623003541995062300354NM 1995 6 23 ASAA9540024 119950531A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 JNU - DURING CHECK, EMERGENCY TRACK LIGHTING WAS OUT AT ROW 11-14. MAINTENANCE RECONNECTED WIRE AT ROW 11. (M) 2L72 4F RTA16WE 19950623003551995062300355SO 1995 6 23 ASOA95013 119950501A2460 CIRCUIT BREAKER EMB 120 EMB120RT SO LT COCKPIT TRIPPED A ASOAO OTHER H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SO11274AS 120229 DURING FLT FROM ATL-DHN, EMERGENCY DC BUS ONE FAILED, CAUSING THE LOSS OF CAPTAINS ALTIMETER, COMM 1, NDB, LEFT T6, LEFT TORQUE, CAPTAINS FLIGHT DIRECTOR, N/W/S (TILLER AND PEDALS), ONE CHANNEL OF MAP, AND LANDING GEAR 'B' LIGHTS. FLIGHT DIVERTED TO MCN WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. RESET EMERGENCY DC BUS ONE CIRCUIT BREAKER IN CAPTAINS LEFT FORWARD CONSOLE. OPERATIONAL CHECKS WERE GOOD AND THE FLIGHT TO DHN WAS RESUMED. THE EMERGENCY DC BUS ONE CIRCUIT BREAKER ON THIS AIRCRAFT WILL BE REPLACED AS A PRECAUTION. (M) 2L72 4T RTA31SO 19950623003561995062300356NM 1995 6 23 AWXA9500324 119950522A335020121 EEL POWER SUPPLY BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950623003571995062300357NM 1995 6 23 AWXA9500326 119950526A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRE AT MID CABIN, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950623003581995062300358NM 1995 6 23 AWXA9500327 119950526A335058783 EEL HARNESS BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE, ROWS 1 THROUGH 5. REMOVED AND REPLACED FEEDER HARNESS FROM SIDEWALL TO FLOOR TRACK, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950623003591995062300359EA 1995 6 23 BUFA9515 119950521A32302875006 SELECTOR VALVE CNDAIRCL44 CL44D4 1900102EA MLG INOP A BUFAO OTHER J WARNING INDICATION APAPPROACH 1 CE052FOR 16 FLT BVA777 - MQY-IAB - NOSE GEAR EXTENDS NORMALLY, BUT BOTH MAIN GEARS WOULD NOT EXTEND. EMERGENCY GEAR EXTENSION USED. NO EMERGENCY DECLARED. REMOVED AND REPLACED MLG SELECTOR VALVE IAW MM 4-21-127. NO JACKS AVAILABLE IAB FOR GEAR SWING. FERRY FLIGHT TO MQY FOR GEAR SWING. AIRCRAFT JACKED AND GEAR SWING ACCOMPLISHED IAW MM 7-00 AND 32-00. ALL OPERATIONS CHECKED NORMAL. (M) 2L74 4T 1A20 19950623003601995062300360WP 1995 6 23 CKSA95024 119950516A5313 STRINGER DOUG DC8 DC863F 302198FWP FS 70 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - EVIDENCE OF CORROSION AT STATION 70 AND STRINGER 31R. REPAIRED AREA AT STATION 70 AND STRINGER 31R IAW EA 95-135 AND DAC FAX FILE NR 268167. (M) 2L74 4F 4A25 19950623003611995062300361WP 1995 6 23 CKSA95025 119950516A5313 STRINGER DOUG DC8 DC863F 302198FWP FS 70 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - EVIDENCE OF CORROSION AT STATION 70 AND STRINGER 30R. REPAIRED AREA AT STATION 70 AND STRINGER 30R IAW EA 95-135 AND DAC FAX FILE NR 268167. (M) 2L74 4F 4A25 19950623003621995062300362WP 1995 6 23 CKSA95027 119950516A5730 PANEL DOUG DC8 DC863F 302198FWP RT WING CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - INBOARD WING SLOT CRACKED, CENTER AREA. REMOVED AND REPLACED RIGHT INBOARD UPPER SLOT PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1. (M) 2L74 4F 4A25 19950623003631995062300363WP 1995 6 23 CKSA95028 119950516A5313 STRINGER DOUG DC8 DC863F 302198FWP FS 70 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - EVIDENCE OF CORROSION STATION 70 STRINGER 27R TO 34L. REPAIRED CORRODED AREA AT STATION 70 BETWEEN STRINGER 27R AND 34L IAW EA 95-135 AN DAC FAX FILE NR 268167. (M) 2L74 4F 4A25 19950623003641995062300364WP 1995 6 23 CKSA95029 119950516A53204640436 FITTING DOUG DC8 DC863F 302198FWP CARGO DOOR FRAMECORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - CORROSION 'D' PIT DOOR FRAME AFT SIDE. REMOVED, CLEANED AND TREATED IAW SRM 51-1-0. REMOVED AND REPLACED 1 BATH TUB FITTING AND GILL LINER ANGLE IAW SRM 53-2-0. (M) 2L74 4F 4A25 19950623003651995062300365WP 1995 6 23 CKSA95030 119950516A5315 FLOORBEAM DOUG DC8 DC863F 302198FWP FS 1660-1670 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - AFT ACCESSORY COMPARTMENT STATION 1660-1670 AT RIGHT OUTBOARD SEAT TRACK FLOORBEAM AND FLOOR HAVE CORROSION. REPAIRED FLOORBEAM AT STATION 1660 RIGHT SIDE IAW EA 95-135.B AND DWG NR SKA95093-1. CLEANED AND TREATED FLOOR IAW SRM 51-1-8. (M) 2L74 4F 4A25 19950623003661995062300366WP 1995 6 23 CKSA95031 119950516A5320 ANGLE DOUG DC8 DC863F 302198FWP FS 1723 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - AFT ACCESSORY COMPARTMENT STATION 1725 AT 28L LONG LOWER LEG HAS EVIDENCE OF CORROSION. REPAIRED LOWER LEG OF LONG 28L AT STATION 1723 IAW DC-8 SRM 53-2-2 FIG 11. (M) 2L74 4F 4A25 19950623003671995062300367WP 1995 6 23 CKSA95032 119950516A53472615891 SEAT TRACK DOUG DC8 DC863F 302198FWP FS 850-990 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - CABIN NR 2 AND NR 3 SEAT TRACKS (DUAL TRACK) APPROXIMATELY 850-990 CORRODED. REPLACED DOUBLE WIDE SEAT TRACK TO TWO SINGLE TRACKS LEFT SIDE FROM STATION 850-990 IAW EA 95-066.J R1 AND SKETCH NR AIA/E/2012. (M) 2L74 4F 4A25 19950623003681995062300368WP 1995 6 23 CKSA95034 119950516A5330 SKIN DOUG DC8 DC863F 302198FWP FS 25 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - EVIDENCE OF CORROSION UNDER SKIN BETWEEN FS 25 AND 35 AT L30R. REMOVED CORROSION AND REPAIRED IAW DC-8 SRM CHAPTER 53-2-0, FIG 18 SHEET 3. TREATED AND PRIMED IAW 51-1-8. (M) 2L74 4F 4A25 19950623003691995062300369NE 1995 6 23 IXKA9500018 219950528A7310320115 VALVE WHITTAKER BOEING727 727224 1384076NM PWA JT8 JT8D17 52049NE NR 1 ENG POS FAILED A IXKAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 EA2532719 A5307 20388 ON APPROACH EWR, FLT NR 10, NR 1 ENG SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMPERATURE PER A 6-7. FOUND FUEL HEAT VALVE FAILED OPEN. REMOVED AND REPLACED VALVE PER 73-14-11. PERFORMED INSPECTION AND GROUND RUN OPS CHECK OK AS PER PW MM 72-00, PG 518D. (M) 2L73 4F4 F A3WE E2EA 19950623003701995062300370NE 1995 6 23 M3HA95011 219950530A7321 ECU AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 2 ENGINE FAILED A M3HAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP13987MH 368 PCE121279 HNL - FLT 800 - DURING FLIGHT, NR 2 ENGINE ECU FAULT LIGHT ILLUMINATED. CREW WAS UNABLE RESET IN FLIGHT. CAPTAIN DISCONTINUED FLIGHT AND RETURNED TO HNL. NR 2 ENGINE ECU RESET ON GROUND BY MAINTENANCE. COULD NOT DUPLICATE. (M) 2H72 4T4 TRTA53EU E20NE 19950623003711995062300371EU 1995 6 23 M3HA95012 119950621A3234F96GA0102022 BLACK HANDLE AEROSPATR42 ATR42320 8680930EU COCKPIT BROKE A M3HAA UNSCHED LANDING O OTHER CRCRUISE 1 WP13985MA 358 HNL - FLT NR 2 - LANDING GEAR HANDLE BROKE IN FLIGHT. REPLACED HANDLE WITH SERVICEABLE UNIT. (M) 2H72 4T RTA53EU 19950623003721995062300372NE 1995 6 23 M3LA95010 219950524A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 FAILED A AM3HAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13988MA 380 PCE121304 HNL - FLT 420 - AT AN ALTITUDE OF 9,000 FEET, JUST AFTER LEVELING OFF, THE CAPTIN NOTED THE NR 1 ENGINE OIL PRESSURE DROPPING, MASTER WARNING FLASHED AND AURAL WARNING SOUND FOLLOWED BY A NR 1 ENGINE FLUCTUATING TORQUE INDICATION. SHUTDOWN PROCEDURES WERE INITIATED AND THE AIRCRAFT RETURNED SAFELY TO HONOLULU INTERNATIONAL. POST-FLIGHT INSPECTION OF THE NR 1 ENGINE REVEALED A FULL SUPPLY OF ENGINE OIL AND NO EXTERNAL INDICATIONS OF A MALFUNCTION. A MAINTENANCE TURN OF THE ENGINE WAS ATTEMPTED RESULTING IN A UNSUCCESSFUL START. FURTHER EVIDENCE SUGGESTED AN INTERNAL ENGINE SEIZE. THE NR 1 ENGINE WAS SUBSEQUENTLY REMOVED AND REPLACED WITH A SERVICEABLE ENGINE. (M) 2H72 4T4 TRTA53EU E20NE 19950623003731995062300373NM 1995 6 23 USAA950503 119950403A5330 CHANNEL BOEING737 7373B7 1384580NM BS 305 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF CORROSION BS 305 AT LBL 36. REPAIRED PER 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003741995062300374NM 1995 6 23 USAA950504 119950403A5320 ANGLE BOEING737 7373B7 1384580NM BS 294.5 -312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA CORROSION FLOORBOARD SUPPORT ANGLE 294.5 TO 312 LBL 12. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003751995062300375NM 1995 6 23 USAA950505 119950410A5320 ANGLE BOEING737 7373B7 1384580NM BS 727D-945 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 137 INCH CORRODED AREA BS 727 D TO BS 945 AT RBL 14 INCHES. REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003761995062300376NM 1995 6 23 USAA950506 119950403A53201716748 HAT CHANNEL BOEING737 7373B7 1384580NM AFT CABIN CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORRODED AREA INBOARD END RT LAVATORY FORWARD WALL HAT CHANNEL AFT CABIN. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003771995062300377NM 1995 6 23 USAA950507 119950403A5320 SUPPORT ANGLE BOEING737 7373B7 1384580NM BS 957 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 7 INCH AREA CORRODED BS 957 RBL 25 TO RBL 50. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003781995062300378NM 1995 6 23 USAA950508 119950404A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 967 LBL 40. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950623003791995062300379NM 1995 6 23 USAA950512 119950510A3350 EEL BOEING737 737301 1384611NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19587US 23932 LGA - FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY IN FORWARD ENTRY AREA. OPS CHECK OK. (M) 2L72 4F RTA16WE 19950623003801995062300380EU 1995 6 23 USAA950520 219950518A7220 SPINNER FOKKERF28 F28MK0100 4990807EU RROYCETAY TAYMK65015 EU NR 2 ENGINE MOISTURE A USAAO OTHER O OTHER CRCRUISE 1 EA19857US 11289 MEM - FLT 0358 - THE CREW RECEIVED AN ENGINE VIBRATION READING FROM THE NR 2 ENGINE. THE CAPTAIN CUT THE ENGINE BACK TO IDLE AND DECLARED AND EMERGENCY. FLIGHT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REMOVED THE SPINNER DUE TO THE PRESENCE OF MOISTURE AND REINSTALLED. (M) 2L72 4F4 FRT 19950623003811995062300381WP 1995 6 23 95ZZZM69 119950516A524047731461 FITTING DOUG DC8 DC863F 302198FWP SERVICE DOOR CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - RIGHT AFT SERVICE DOOR LOWER AFT CORNER 2 EACH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAQ DC-8 SRM 53-2-0. (M) 2L74 4F 4A25 19950623003821995062300382EU 1995 6 23 AWXA9500234 119950418A3230D5288011800100 HINGE ASSY AIRBUS320 A320231 3930325EU RT MLG WORN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28626AW 65 CMH-PHX - FLT 860 - AIR TURNBACK, DURING CLIMB THE LANDING GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE INSPECTED AIRCRAFT AND FOUND AIRWORTHY FOR FERRY FLIGHT TO PHX. PHX MAINTENANCE CHECKED ADJUSTMENT OF RIGHT MLG DOOR OPEN PROXIMITY SENSORS PER AMM 32-31-73, PAGE 601. REPLACED BOTH SENSOR TARGETS. RIGHT MLG DOOR FORWARD HINGE FITTING BOLT HOLES OVERSIZED PER ER 32-52-82-08. PERFORMED GEAR SWING WITH NO FAULTS NOTED. TEST FLIGHT PERFORMED WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19950623003831995062300383NM 1995 6 23 AWXA9500237 119950418A3350417N521038 EEL ASSY BOEING757 757225 1384959NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28913AW 22207 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT 35C. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950623003841995062300384NM 1995 6 23 AWXA9500238 119950418A335020131A EEL BATTERY PACK BOEING757 7572S7 1384962NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN FORWARD CABIN. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950623003851995062300385NM 1995 6 23 AWXA9500313 119950525A5311 FRAME BOEING757 7572S7 1384962NM FS 820 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 820. REPAIRED IAW SRM 53-00-07. (M) 2L72 4F RTA2NM 19950623003861995062300386NM 1995 6 23 AWXA9500314 119950525A5311 FRAME BOEING757 7572S7 1384962NM FS 800 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 800. FABRICATED DOUBLER AND SUPPORT, INSTALLED REPAIR AND SUPPORTS IAW WITH SRM 53-00-07, FIGURE 301. (M) 2L72 4F RTA2NM 19950623003871995062300387NM 1995 6 23 AWXA9500315 119950525A5311 FRAME BOEING757 7572S7 1384962NM FS 780 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 780. FABRICATED REPAIR PARTS, AND INSTALLED PARTS PER SRM 53-00-07, FIG 201. (M) 2L72 4F RTA2NM 19950623003881995062300388NM 1995 6 23 AWXA9500316 119950525A5311 FRAME BOEING757 7572S7 1384962NM FS 760 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND DEEP GOUGE IN MAIN FRAME AT CENTER LINE, STATION 760. FABRICATED DOUBLER AND SUPPORTS, AND INSTALLED PARTS PER SRM 53-00-07, FIG 201. (M) 2L72 4F RTA2NM 19950623003891995062300389NM 1995 6 23 AWXA9500317 119950525A5230 CORNER BOEING757 7572S7 1384962NM AFT CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND AFT CARGO DOOR LOWER FORWARD CORNER CRACKED. REMOVED AND REPLACED CORNER PER SRM 51-40-02 AND SRM 51-10-00. (M) 2L72 4F RTA2NM 19950623003901995062300390NM 1995 6 23 AWXA9500318 119950525A5315 FLOORBEAM BOEING757 7572S7 1384962NM FS 345 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND FWD GALLEY AREA 'I' BEAM CORRODED BEYOND LIMITS AT STATION 345 LBL 10. FABRICATED REPAIR PART AND INSTALLED PER SRM 51-70-12, FIG 2. (M) 2L72 4F RTA2NM 19950623003911995062300391NM 1995 6 23 AWXA9500319 119950525A5315 FLOORBEAM BOEING757 7572S7 1384962NM FS 377 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28905AW 23567 PHX - DURING SCHEDULED C3 INSPECTION, FOUND 'I' BEAM IN FORWARD GALLEY AREA CORRODED BEYOND LIMITS AT STATION 377 LBL 0 TO LBL 10. FABRICATED REPAIR PART AND INSTALLED PER SRM 51-70-12. (M) 2L72 4F RTA2NM 19950623003921995062300392EU 1995 6 23 AWXA9500328 119950529A5270 DOOR WARNING AIRBUS320 A320231 3930325EU CARGO COMPT ACTIVATED A AWXAO OTHER N FALSE WARNING DEDESCENT 1 WP28621AW 053 PHX-YVR - FLT 819 - ON DESCENT FROM FLT LEVEL 260/250 THE AFT CARGO DOR INDICATION 'OPEN' APPEARED ON ECAM. NO PRESSURIZATION PROBLEMS WERE NOTED. AIRCRAFT CONTINUED TO GATE WITHOUT FURTHER PROBLEMS. CONTACT MAINTENANCE INSPECTED DOOR, OPENING AND CLOSING IT SEVERAL TIMES. NO DEFECTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RTA28NM 19950623003931995062300393NM 1995 6 23 AWXA9500332 119950531A5742311N52171 FUSE PIN BOEING757 7572S7 1384962NM NR 1 STRUT CRACKED A AWXAO OTHER Z SIGNIFICANT FAILURE REPORT ININSP/MAINT 1 WP28903AW 23323 PHX - FLT 1272 - DURING SCHEDULED MAINTENANCE INSPECTION, FOUND NR 1 ENGINE OUTBOARD STRUT TO WING FUSE PIN CRACKED. CRACK VERIFIED WITH EDDY CURRENT NDT TEST. MAINTENANCE REPLACED FUSE PIN PER EO 54-51-03. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RTA2NM 19950623003941995062300394EU 1995 6 23 AWXA9500333 119950531A3350 EEL WIRE AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28626AW 65 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE AT 26L. REPAIRED BROKEN WIRE AT WALL CONNECTOR AT 26L, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950623003951995062300395NM 1995 6 23 AWXA9500335 119950601A3350276005 EEL FUSES BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENACNE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 16 THROUGH ROW 20. STRAIGHTENED BENT PINS ON CONNECTOR D3688 AND REPLACED THREE FUSES IN EMERGENCY CHARGERS M1197 AND M1137. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950623003961995062300396NM 1995 6 23 AWXA9500336 119950601A33509005242 EEL PWR SUPPLY BOEING737 7372M8 1384483NM AFT BAG PIT INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY IN AFT BAG PIT, OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950623003971995062300397NM 1995 6 23 AWXA9500337 119950601A3350900835A EEL BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28184AW 22651 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 5 AND 6. REMOVED AND REPLACED BATTERY PACK AT ROW 4, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950623003981995062300398NM 1995 6 23 AWXA9500341 119950605A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CORROSION ON TOP CHORD OF FLOORBEAM, STATION 986.5 RBL 22 TO LBL 22. REMOVED AND REPLACED DAMAGED AREA PER MM 51-21-99 AND SRM 53-00-51. (M) 2L72 4F RTA16WE 19950623003991995062300399NM 1995 6 23 AWXA9500342 119950605A5320 THRESHOLD BOEING737 73733A 1384673NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CORROSION ON UNDER SIDE OF R2 DOOR THRESHOLD CHORD, STATION 986.5 TO STATION 967. REMOVED AND REPLACED DAMAGED AREA PER SRM 53-60-15 AND SRM 51-10-02. (M) 2L72 4F RTA16WE 19950623004001995062300400NM 1995 6 23 AWXA9500343 119950605A5320 INTERCOSTAL BOEING737 73733A 1384673NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND SURFACE CORROSION ON TOP SIDE OF INTERCOSTAL, STATION 967 TO STATION 947 RBL 45. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. (M) 2L72 4F RTA16WE 19950623004011995062300401NM 1995 6 23 AWXA9500344 119950605A5320 INTERCOSTAL BOEING737 73733A 1384673NM FS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CORROSION ON INTERCOSTAL BETWEEN STATION 967 AND STATION 986.5 LBL 20. REMOVED AND REPLACED INTERCOSTAL PER ER 1-53-10-01B. (M) 2L72 4F RTA16WE 19950623004021995062300402NM 1995 6 23 AWXA9500345 119950605A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CORROSION ON LEFT AFT LAVATORY THRESHOLD 'I' BEAM BETWEEN STATION 986.5 AND STATION 1006. REMOVED AND REPLACED FILLER IAW SRM 51-40-21 AND SRM 51-10-02, PARAGRAPH 8 AND 9. (M) 2L72 4F RTA16WE 19950623004031995062300403NM 1995 6 23 AWXA9500346 119950605A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND STATION 1016 'I' BEAM CORRODED UNDER LAVATORY. REMOVED AND REPLACED DAMAGED AREA PER SRM 51-70-12. (M) 2L72 4F RTA16WE 19950623004041995062300404NM 1995 6 23 AWXA9500347 119950605A5315 FLOORBEAM BOEING737 73733A 1384673NM FS 1006/1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CORROSION ON LEFT AFT LAVATORY THRESHOLD SUPPORT 'I' BEAM AT STATION 1006 AND STATION 1016. REMOVED AND REPLACED DAMAGED AREA PER SRM 51-40-02. (M) 2L72 4F RTA16WE 19950623004051995062300405NM 1995 6 23 AWXA9500348 119950605A5720 ANGLE BOEING737 73733A 1384673NM NR 3 FLAP TRACK CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND BOOMERANG FRAME CRACKED AT AFT END OF NR 3 FLAP TRACK FAIRING. REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2L72 4F RTA16WE 19950623004061995062300406NM 1995 6 23 AWXA9500349 119950605A5210 SKIN BOEING737 73733A 1384673NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND CRACK IN L2 DOOR SKIN AT UPPER HINGE CUTOUT LOWER AFT CORNER. REMOVED DAMAGE IAW SRM 52-10-01, FIGURE 101. (M) 2L72 4F RTA16WE 19950623004071995062300407NM 1995 6 23 AWXA9500350 119950605A323065461067 UNIVERSAL LINK BOEING737 73733A 1384673NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 1927 23631 PHX - DURING C4 INSPECTION, FOUND UNIVERSAL LINK ASSEMBLY CORRODED ON INBOARD FACE OF INBOARD LUG OF SIDE BRACE ATTACH LUGS. REMOVED AND REPLACED UNIVERSAL LINK ASSY PER MM 32-11-41, PAGE 405. (M) 2L72 4F RTA16WE 19950623004081995062300408NM 1995 6 23 AWXA9500351 119950605A3230656337811 LINK BOEING737 73733A 1384673NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW KR3151 23631 PHX - DURING C4 INSPECTION, FOUND FORWARD TRUNNION LINK CORRODED AT BUSHING ATTACH POINTS. INSTALLED NEW TRUNNION LINK PER AWA TASK CARD R4M32018, STEP 2H. (M) 2L72 4F RTA16WE 19950623004091995062300409NM 1995 6 23 AWXA9500352 119950605A3210655223520 BEAM BOEING737 73733A 1384673NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28172AW 23631 PHX - DURING C4 INSPECTION, FOUND RT MLG STABILIZER BEAM AFT LUGS CORRODED. INSTALLED NEW SERVICEABLE STABILIZER BEAM PER AWA TASK CARD R4M32018. (M) 2L72 4F RTA16WE 19950623004101995062300410NM 1995 6 23 AWXA9500354 119950605A27512061141 POSITION BOEING737 7373S3 1384711NM TE FLAPS MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28313AW 1769 23712 LAS-PHX - FLT 1229 - ON CLIMB-OUT, UNABLE TO RAISE FLAPS PAST FLAPS 1. AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND FLAP POSITION INDICATOR BAD. REMOVED AND REPLACED FLAP POSITION INDICATOR. FLAPS WERE CYCLED NUMEROUS TIMES AND NO MALFUNCTIONS NOTED, PER MM 27-51-00. SYSTEM OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950623004111995062300411WP 1995 6 23 CKSA95026 119950516A5730 PANEL DOUG DC8 DC863F 302198FWP LT WING CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - INBOARD WING SLOT CRACKED, CENTER AREA. REMOVED PANEL, STOP DRILLED CRACK IN INBOARD LEFT UPPER SLOT PANEL IAW EA95-135.1. REINSTALLED PANEL IAW DC-8 SRM 51-3-0 AND DC-8 MM 27-80-1. (M) 2L74 4F 4A25 19950623004121995062300412WP 1995 6 23 CKSA95033 119950516A524026499432 FITTING DOUG DC8 DC863F 302198FWP SERVICE DOOR CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23815CK32661 46151 OSC - RIGHT AFT SERVICE DOOR LOWER AFT CORNER 2 EACH FITTINGS CORRODED. REMOVED AND REPLACED FITTINGS IAQ DC-8 SRM 53-2-0. (M) 2L74 4F 4A25 19950623004131995062300413EU 1995 6 23 VTZA95179 119950518A73321103P0645 PRESS SWITCH BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27861AE 861 IAD-ALB - FLT NR 6155 - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE FUEL PRESSURE CAP LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17810 IAW MEL 73-2. MAINTENACNE LATER CLEARED DMI NR 17810 ON 5-24-95 BY REPLACING THE LEFT FUEL LOW PRESSURE WARNING SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950623004141995062300414NE 1995 6 23 VTZA95181 219950526A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33114 01514NE LEFT BIRD STRIKE A VTZAC ABORTED TAKEOFF C F.O.D. TOTAKEOFF 1 EA27471UE6767 614 821 P66210 CHO-IAD - FLT NR 6166 - ABORTED TAKEOFF DUE TO A BIRD INGESTION INTO THE NR 1 ENGINE. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. LYH MAINTENANCE SENT A MECHANIC CREW TO CHO TO INSPECT FOR DAMAGE. LYH MAINTENANCE CHANGED ENGINE IN CHO AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE ON 5-27-95. (M) 2L72 4T4 TRTA56EU E18NE 19950623004151995062300415WP 1995 6 23 VTZA95182 219950522A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LEFT FAILURE A VTZAF ACTIVATE FIRE EXT. Y ENGINE STOPPAGE APAPPROACH 1 EA27478UE107075046 892 P66098 IAD-PHL - FLT NR 6229 - DURING SHORT FINAL AND EMERGENCY WAS DECLARED DUE TO THE LEFT ENGINE FAILING. AIRCRAFT LANDED AT PHL WITH NO FURTHER INCIDENTS. MAINTENANCE IN THE PROCESS OF CHANGING THE ENGINE. MAINTENANCE COMPLETED CHANGING THE ENGINE ON 5-23-95. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950623004161995062300416 1995 6 23 VTZA95183 419950525A34214020531574 ADI BAG JETSTMJETSTM3201 1500217EU COCKPIT FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27472UE 823 IAD-SYR - FLT NR 6387 - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE RADAR ONLY PAINTS GROUND ON RIGHT SIDE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE CAPTAINS ADI. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950623004171995062300417EU 1995 6 23 VTZA95188 119950604A261172111211000 SMOKE DETECTOR JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE COMPT FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27307UE 41021 FLT NR 6320 - IAD-RDU - DURING CLIMB-OUT DECLARED AN EMERGENCY AND RETURNED TO IAD DUE TO THE BAGGAGE BAY SMOKE DETECTION LIGHT ILLUMINATING. FLIGHT CREW EVACUATED PASSENGERS ON THE RUNWAY. AIRCRAFT THEN TAXIED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950623004181995062300418EU 1995 6 23 VTZA95189 119950607A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE COMPT STUCK A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27303UE 41015 FLT NR 6217 - IAD-PVD - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE POD DOOR LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND POD DOOR MICROSWITCH STUCK AND RELEASED THE SWITCH. RESECURED POD DOOR AND OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950623004191995062300419EU 1995 6 23 VTZA95190 119950607A21501379211L403 ACU JETAIRJETSTMJETSTM4101 1500501EU LT STUB WING FROZEN A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27307UE 41021 FLT 6578 - IAD-PWM - DURING CRUISE RETURNED TO IAD DUE TO THE LEFT DUCT FAIL LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE LEFT ACM FROZEN. MAINTENANCE UNFROZE THE ACM AND PERFORMED OPS CHECK, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950623004201995062300420WP 1995 6 23 95ZZZX3100 119950519A52803924290502 DOOR HINGE DOUG DC9 DC932 3022066WP RT MLG DOOR FAILED A VJ6AO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO11934VV 47488 PHL/ATL - FLT 547 - THE RIGHT FLYING DOOR SEPARATED FROM THE AIRCRAFT, FLYING DOOR HINGE BROKEN. REPLACED FLYING DOOR HINGE ASSY. 2L72 4F A6WE 19950623004311995062300431SW 1995 6 23 LCFR950515 119950515A6720212010783101 ROD END 212011710001BELL 212 212 1181420SW TAIL ROTOR SHEARED BARREL A ALCFAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 NM091082G 31109 TAIL ROTOR PITCH LINK ASSEMBLY SEPARATED IN-FLIGHT. AIRCRAFT LANDED SAFELY. ROD END BARREL SHEARED. NO SIGNS OF CORROSION NOTED. SUSPECT EXCESSIVE ROD END BEARING WEAR PREVENTED BEARING ROTATION. (X) 1G71 4U H4SW 19950623004321995062300432NE 1995 6 23 9509672706 219950614A7200 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 1 MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 GL01815EA 22552 700622 NR 1 ENGINE DID NOT REACH TARGET EPR ON TAKEOFF. THE CREW ELECTED TO COMPLETE THE TAKEOFF, JETTISON 5,000 LBS OF FUEL WHILE IN FLIGHT AND RETURNED TO MSP. SUBSEQUENT LANDING OCCURRED WITHOUT INCIDENT. MAINTENANCE TRIMMED AND TESTED THE ENGINE, PERFORMANCE WAS SATISFACTORY. THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950623004331995062300433NM 1995 6 23 9509682294 119950619A21311310461 MANUAL CONTROL BOEING727 727251 138408HNM FLIGHT DECK MALFUNCTIONED A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01294US4527518567 21505 DURING CRUISE AT FL345, CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE CLIMBING AT 500 RPM AND COULD NOT CONTROL MANUALLY. DECLARED AN EMERGENCY AND INITIATED DESCENT TO FL100. PASSENGER OXYGEN MASKS DEPLOYED. MAXIMUM CABIN ALTITUDE WAS 15,000 FT. FLIGHT LANDED AS SCHEDULED WITHOUT FURTHER INCIDENT. DTW MAINTENANCE REPLACED THE AUTO AND MANUAL CONTROLLERS, COALESCER BAG, AND 35 DEGREE TEMPERATURE SENSOR. OPERATIONAL CHECK NORMAL. STATION BUF CHANGED TO LGA. 2L73 4F A3WE 19950623004341995062300434SO 1995 6 23 COM11919 119950617A5720 SKIN SUPPORT EMB 120 EMB120RT SO WINGS CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01241CA11989 120211 THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK NR 5720-551/651-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO-DESIGN REPORT NR 1327-2. P/N; 120-17056-005, 1 EA; 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-017, 1 EA; 120-17056-015, 2 EA; 120-17060-013, 1 EA; 120-17056-013, 1 EA; 120-17056-011, 1 EA; 120-17057-007, 1 EA; 120-17057-006, 1 EA; 120-17059-015, 1 EA; 120-17059-017, 1 EA. 2L72 4T RTA31SO 19950623004351995062300435SO 1995 6 23 COM11920 119950620A61207757151 BALLSCREW SERVO HAMSTD 78249024 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE REDUCTION GRBOX DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01258CA 891112 120247 115553 900102 WHILE PERFORMING HAMILTON STANDARDS S/B 14RF-9-61-A53 REV 5, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. THE PCU WAS SENT TO HAMILTON STANDARD FOR FURTHER EVALUATION. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 19950623004361995062300436EU 1995 6 23 COM31108 119950616A2730DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100EU LT ELEV DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01343CA14852306 340A024 CONFIG WARNING DURING TAKEOFF ROLL. REPLACED THE LT PITCH TRIM ACTUATOR. 2L72 4T RTA52EU 19950623004371995062300437EU 1995 6 23 COM31109 119950616A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01158CA5180 NOV920498 340A158 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950623004381995062300438EA 1995 6 23 COM60498 119950618A276054C54677E01 CONTROL ASSY CNDAIRCL600 CL6002B19 EA SPOILER DEFECTIVE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01920CA2399 797 7022 INBD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE SPOILER MANIFOLD CONTROL ASSY. 2L72 4F RTA21EA 19950623004391995062300439EA 1995 6 23 COM60499 119950617A2750860D10016 FECU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01918CA459 7018 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950623004401995062300440EA 1995 6 23 COM60500 119950616A274070623 CONTROL UNIT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01920CA3078 992 7022 STABILIZER TRIM CHANNEL 2 IS INOP. REPLACED THE STABILIZER MOTOR CONTROL UNIT. 2L72 4F RTA21EA 19950623004411995062300441NE 1995 6 23 DL31L952674 219950618A73208010003 FMU AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11843AB 689 724926 DURING CRUISE HAD FLUCTUATING NR 1 ENGINE EPR INDICATIONS, RETURNED JFK. REPLACED NR 1 FMU, PERFORMED RUNUP, OPERATION NORMAL. 2L72 4F RTA35EU E24NE 19950623004421995062300442NM 1995 6 23 DL72E952690 119950613A5315 FLOORBEAM BOEING727 727247 138408FNM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 000156 FOUND ON CV2 CHECK, CORROSION TOP AND BOTTOM OF FLOORBEAM STA 1050 BETWEEN RBL 25 AND RBL 45. REPAIRED PER ERA NR 301959-14 CODE 4-53-21-02. 2L73 4F A3WE 19950623004431995062300443NM 1995 6 23 DL72E952691 119950613A5522 TE SKIN BOEING727 727247 138408FNM RT ELEVATOR DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, RIGHT ELEVATOR DELAMINATED JUST OUTBD OF TRIM TAB ON TE. REPAIRED PER M/M 55-20-0 PG 801 ITEM 2. 2L73 4F A3WE 19950623004441995062300444NM 1995 6 23 DL72E952704 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 1120 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, CORROSION AT STRINGER 27R AT STA 1120. REPAIRED PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950623004451995062300445NM 1995 6 23 DL72S952572 119950611A5313 STRINGER BOEING727 727232 1384082NM FS 1010-1017 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 CORROSION ON OB SIDE OF STGR 29L STA 1010 TO 1017, OB SIDE OF STGR 29L IS CRACKED AT STA 1012. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950623004461995062300446NM 1995 6 23 DL72S952612 119950613A5532 SKIN BOEING727 727232 1384082NM STA 110.4 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11483DA 20863 FOUND ON A2 LTR CK, 1.125 INCH CRACK VERTICAL STABILIZER SKIN LT SIDE STA 110.400 S-9. REPAIR INSTALLED DOUBLER PER SRM 55-30-3. 2L73 4F A3WE 19950623004471995062300447NM 1995 6 23 DL72W952571 119950612A5754 ANGLE BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11290WA 22108 FOUND DURING A-1 LETTER CHECK, 1.75 INCH CRACK IN ANGLE ON THE LOWER AFT SIDE I/B CORNER OF NR 6 SLAT. REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950623004481995062300448NM 1995 6 23 DL72W952574 119950605A5312 BULKHEAD BOEING727 727247 138408FNM FS 178 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 PERFORM BODY STA 178 BULKHEAD ACCESS HOLE INSTALLATION PER SRM 53-10-9 PG 8 TO FOM. INSTALLED REPAIR PER SRM 53-10-9 PG 8 AND 9. 2L73 4F A3WE 19950623004491995062300449NM 1995 6 23 DL72W952686 119950619A5311 FRAME BOEING727 727247 138408FNM BS 913 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 21327 FOUND DURING E-2 LETTER CHECK, BS 913 FRAME CRACKED LT MLG WHEEL WELL. REPAIRED PER MM 53-11-0 PAR 20. 2L73 4F A3WE 19950623004501995062300450NM 1995 6 23 DL72W952687 119950619A5754 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 21327 FOUND DURING E-2 LETTER CHECK, NR 4 L/E SLAT L/E RIB CRACKED I/B OF ACTUATOR ROD END AND RIB CRACKED O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0 PAR 3. 2L73 4F A3WE 19950623004511995062300451NM 1995 6 23 DL733952672 119950618A2782 ACTUATOR BOEING737 737347 1384647NM NR 3 SLAT LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11303WA 23183 DURING CRUISE LOST B-SYS HYDRAULICS, COULD NOT LOWER T/E FLAPS. FOUND NR 3 SLAT ACTUATOR LEAKING, HOUSING WAS CRACKED AT PARTING SURFACE. REPLACED ACTUATOR, OPERATION NORMAL. 2L72 4F RTA16WE 19950623004521995062300452NM 1995 6 23 DL73S952588 119950601A5315 FLOORBEAM 6545410223 BOEING737 737232 1384475NM FS 661 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11326DL 6545410515 23098 DURING LAY OVER, INSPECTION FOUND THE FLOORBEAM AT BL 0.07 OF THE WING CENTER SECTION CRACKED AT STA 661. IN ACCORDANCE WITH BAC S/B 737-57-1210, THE CRACKS ARE TYPICAL AND WILL BE REPAIRED BY THE S/B 737-57-1210. 2L72 4F RTA16WE 19950623004531995062300453 1995 6 23 DL73S952692 419950619A345091252ZC7C4001 RELAY BOEING737 737232 1384475NM LT FLT DECK FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11319DL 23091 ON CLIMBOUT, LOST ALL FLT INSTRUMENTS ON LEFT SIDE, RETURNED TO CVG. FOUND NORMAL TRANSFER C/B TRIPPED. REPLACED R3 TRANSFER RELAY, OPERATION NORMAL. 2L72 4F RTA16WE 19950623004541995062300454NM 1995 6 23 DL757952556 119950608A5753 SKIN BOEING757 757232 1384965NM RT TE FLAP PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, A SMALL HOLE WAS FOUND IN THE LWR SKIN APPROX 35 INCHES FROM THE I/B END AND 8 INCHES FROM THE T/E OF THE RT O/B AFT FLAP. THIS WAS REPAIRED AS PER SRM 57-53-01. 2L72 4F RTA2NM 19950623004551995062300455NM 1995 6 23 DL757952557 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON THE FUEL ACCESS OPENING 542 CB. THIS WAS CLEANED PER SRM 57-20-01 TREATED AND PAINTED PER SAME AND ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004561995062300456NM 1995 6 23 DL757952558 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 531 CB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004571995062300457NM 1995 6 23 DL757952559 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 531 BB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004581995062300458NM 1995 6 23 DL757952560 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON ACCESS PANEL 531 AB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01 AND ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004591995062300459NM 1995 6 23 DL757952561 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENING 542 BB. THIS WAS CLEANED, TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004601995062300460NM 1995 6 23 DL757952562 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 MB 541 LB AND 541 KB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004611995062300461NM 1995 6 23 DL757952563 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 JB 541 HB AND 541 EB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004621995062300462NM 1995 6 23 DL757952564 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 FB AND 541 EB. THIS WAS CLEANED TREATED AND PAINTED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004631995062300463NM 1995 6 23 DL757952565 119950607A5730 SKIN BOEING757 757232 1384965NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING CORROSION WAS FOUND ON FUEL ACCESS OPENINGS 541 CB 541 BB AND 541 AB. THIS WAS CLEANED AND TREATED PER SRM 57-20-01. ALSO, ROTOPEENED PER PS 900-4 NR 5. 2L72 4F RTA2NM 19950623004641995062300464NM 1995 6 23 DL757952566 119950606A7110 COWL BOEING757 757232 1384965NM NR 1 ENG ERODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE NR 1 ENG NOSE COWL WAS FOUND ERODED ON THE COMPOSITE L/E. THIS WAS REPAIRED PER SRM 54-11-01 REF 51-70-03. 2L72 4F RTA2NM 19950623004651995062300465NM 1995 6 23 DL757952567 119950607A5730 SKIN BOEING757 757232 1384965NM RT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 641 BB AND 641 CB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01. 2L72 4F RTA2NM 19950623004661995062300466NM 1995 6 23 DL757952568 119950607A5730 SKIN BOEING757 757232 1384965NM RT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 631 CB AND 641 AB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01. 2L72 4F RTA2NM 19950623004671995062300467NM 1995 6 23 DL757952569 119950607A5730 SKIN BOEING757 757232 1384965NM RT WING WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, FRETTING WEAR WAS FOUND AROUND OPENINGS FOR TANK PLATES 631 AB AND 631 BB. THIS WAS REMOVED PER SRM 57-20-01, ROTOPEENED PER PS 900-4 NR 5, TREATED AND PAINTED PER SRM 57-20-01. 2L72 4F RTA2NM 19950623004681995062300468NM 1995 6 23 DL757952680 119950618A7110314N301016R NOSE COWL 314N301016R BOEING757 757232 1384965NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 000156 23614 GROUND DAMAGE TO NOSE COWL AT 10 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01. 2L72 4F RTA2NM 19950623004691995062300469WP 1995 6 23 DLL10952577 119950602A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 569-589 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP BETWEEN FS 569 TO 589 BETWEEN STRINGERS 24 AND 25 DISBONDED. REPAIRED PER SRM 53-31-00 FIG 816, FOUND AT HMV. 2L73 4F A23WE 19950623004701995062300470WP 1995 6 23 DLL10952578 119950525A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG MIGRATED BUSHINGA DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 BUSHING MIGRATED ON THE RT MLG ACTUATOR FITTING, FWD LUG FWD SIDE, FOUND AT HMV. REWORKED ER SRM 57-14-00 . 2L73 4F A23WE 19950623004711995062300471WP 1995 6 23 DLL10952579 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FASTENER HOLES NR 17, 18, 19, 20 ARE CORRODED AND HOLES NR 19, 20 HAVE DAMAGED BUSHINGS. REPAIRED PER SRM 57-14-00 FIG 808. FOUND DURING HMV, FOR LEFT MLG ATTACH FITTING. 2L73 4F A23WE 19950623004721995062300472WP 1995 6 23 DLL10952580 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND FOLLOWING HOLES ON LT MLG RETRACT ACTUATOR FITTING. BUSHINGS ARE NOT SEATED AND HOLES CORRODED 1, 2, 3, 4, 5, 6. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17. 2L73 4F A23WE 19950623004731995062300473WP 1995 6 23 DLL10952581 119950526A5743 LUGS LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 BOTH LUGS ON LT MLG RETRACT ACTUATOR FITTING ARE CORRODED, FOUND AT HMV. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17. 2L73 4F A23WE 19950623004741995062300474WP 1995 6 23 DLL10952582 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, LT MLG RETRACT SUPPORT FITTING IS CORRODED MANY AREAS, ALL SURFACES. REPAIRED PER SRM 57-14-00 FIG 808 JPC 17. 2L73 4F A23WE 19950623004751995062300475WP 1995 6 23 DLL10952583 119950525A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORROSION ON LOWER SURFACE AND 45 DEGREE SURFACE JUST ABOVE ON MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18. 2L73 4F A23WE 19950623004761995062300476WP 1995 6 23 DLL10952584 119950525A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORROSION INSIDE SEVERAL ATTACH HOLES ON MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18. 2L73 4F A23WE 19950623004771995062300477WP 1995 6 23 DLL10952585 119950525A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORROSION ON OUTBD SURFACE OF MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18. 2L73 4F A23WE 19950623004781995062300478WP 1995 6 23 DLL10952586 119950525A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORROSION ON TOP SURFACE OF MLG RETRACT ACTUATOR FITTING. REWORKED PER SRM 57-14-00 JPC 18. 2L73 4F A23WE 19950623004791995062300479WP 1995 6 23 DLL10952668 119950618A53121553612101 BLKHD CLIP LKHEED1011 10113851 5265010WP FS 1223 CRACKED A DALAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SO11723DA 193C1150 DURING INSPECTION, FOUND FS 1223 CANTED BULKHEAD CLIP CRACKED. REPAIRED PER SRM 53-11-00 PG 859. 2L73 4F A23WE 19950623004801995062300480WP 1995 6 23 DLL10952682 119950525A5330 TEAR STRAPS LKHEED1011 10113851 5265010WP FS 659/679 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 000156 AT HMV, TEAR STRAPS DISBONDED BETWEEN STR 39 AND 40 STA 659 AND 679. REPAIRED PER SRM 53-31-00 PAGE 830. 2L73 4F A23WE 19950623004811995062300481WP 1995 6 23 DLL10952683 119950525A5330 TEAR STRAPS LKHEED1011 10113851 5265010WP FS 599/589-569 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 000156 TEAR STRAPS DISBONDED BETWEEN STR 37 AND 38 STA 599. TEAR STRAPS DISBONDED BETWEEN STA 589 TO 569 BETWEEN STR 40 AND 41, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PAGES 801 AND 807. 2L73 4F A23WE 19950623004821995062300482WP 1995 6 23 DLL10952684 119950619A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1770 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 39 CRACKED AND CORRODED AT FS 1770, FOUND AT HMV. SPLICED IN SECTION OF NEW STRINGER PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950623004831995062300483WP 1995 6 23 DLL10952695 119950526A5312 BULKHEAD LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 REF EO 07-69959-12 OPN 0205 HFEC INSP LT FS 1363 BULKHEAD. CRACK INDICATION BETWEEN NR 4 AND 5 BULKHEAD WEB STIFFENERS INBD IND, FOUND AT HMV. REPLACED BULKHEAD PER ERA 271056-14 REV B. 2L73 4F A23WE 19950623004841995062300484WP 1995 6 23 DLL13952677 119950510A5320 RIB LKHEED1011 10113851 5265010WP FS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND RIB CRACKED STA 1705 ABOVE STR 39. FABRICATED NEW DOUBLER, DRILLED UP REPAIR, AND INSTALLED REPAIR PER SRM 53-12-00 FIG 608. 2L73 4F A23WE 19950623004851995062300485WP 1995 6 23 DLL13952678 119950510A5320 RIB LKHEED1011 10113851 5265010WP FS 1685 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND RIB CRACKED STA 1865 ABOVE STR 39. FABRICATED DOUBLER, DRILLED REPAIR, AND INSTALLED PER SRM 53-12-00 PG 806. 2L73 4F A23WE 19950623004861995062300486WP 1995 6 23 DLL13952679 119950531A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 1443-1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SEAT TRACK CORRODED STA 1443 TO 1545. REMOVED SEAT TRACK AND INSTALLED NEW TRACK PER SRM 53-21-00 PG 836. 2L73 4F A23WE 19950623004871995062300487WP 1995 6 23 DLL13952688 119950616A53301503541217 SKIN LKHEED1011 10113851 5265010WP FS 1453-1815 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 000156 THE AFT BELLY SKIN WAS FOUND CORRODED AND HAD SEVERAL PREVIOUS REPAIRS REQUIRING REPLACEMENT OF THE BELLY SKIN AT FS 1453 TO 1815, DAMAGE FOUND AT HMV. REPAIRS ACCOMPLISHED PER DL ERA 270891AD. 2L73 4F A23WE 19950623004881995062300488WP 1995 6 23 DLL13952689 119950616A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 000156 THE LT WING WAS FOUND WITH 4 CRACKS ON CASTELLATION OF THE IWS 555 UPPER RIB CAP, FOUND AT HMV. REPAIRS ACCOMPLISHED PER DL ERA 270733. 2L73 4F A23WE 19950623004891995062300489WP 1995 6 23 DLL13952696 119950512A5312 P-DOME LKHEED1011 10113851 5265010WP FS 1809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND P-DOME CORRODED, LOWER WEB AFT OF FS 1809 STRINGER 1809. REMOVED CORROSION, FABRICATED NEW SECTION, AND INSTALLED PER SRM 53-11-00 FIG 848. 2L73 4F A23WE 19950623004901995062300490WP 1995 6 23 DLL14952573 119950320A57551529102177 SKIN LKHEED1011 1011385115 5265015WP NR 2 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO111739D 193C1237 DURING SHOP INSPECTION, MAINTENANCE FOUND 2 DELAMINATED AREAS APPROX 45 AND 75 INCHES FROM I/B END LOCATED UNDER ANTI-FLUTTER SEAL. BOTH AREAS ARE LIMITED TO APPROX SIX INCHES OF DELAMINATION. REPAIRED PER SRM 57-52-00, FOR NR 2 LT SPOILER PANEL. 2L73 4F A23WE 19950623004911995062300491WP 1995 6 23 DLL14952694 119950611A2820394491 SENSOR 394473149 LKHEED1011 1011385115 5265015WP NR 1 TANK MALFUNCTIONED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11737D 2083 193C1228 ON CLIMBOUT AND CRUISE WITH FULL FUEL LOADS, AIRCRAFT EXPERIECNED SEVERAL INSTANCES OF EXCESSIVE FUEL VENTING OVERBOARD, RESULTING IN AIR TURNBACK. EXTENSIVE TROUBLESHOOTING DETERMINED PROBLEM WAS WITH FUEL TRANSFER SYSTEM. A FAULTY THERMISTOR AND SIGNAL CONDITIONER RESULTED IN SIGNALS THAT TRANSFERRED FUEL TO A FULL TANK, THUS CAUSING IT TO VENT THE FUEL OVERBOARD. REPLACED WAS THE HIGH LEVEL FLOAT SWITCH (PN 739400107), FOUND CONTAMINATED, THERMISTOR(FOUND INTERMITTENT)AND SIGNAL CONDITIONER, FOUND TRANSFER CIRCUIT FAULTY. 2L73 4F A23WE 19950623004921995062300492NM 1995 6 23 DLM88952570 119950612A5320 ANGLE DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11906DE 53415 FOUND DURING C-1 LETTER CHECK, LT WHEEL WELL AFT JAMB CRACKED 1 INCH LT O/B SIDE. INSTALLED DOUBLER PER MM 53-05 FIG 101. 2L72 4F RTA6WE 19950623004931995062300493NM 1995 6 23 DLM88952685 119950619A5320 RIB DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11957DL 49976 FOUND DURING F-1 LETTER CHECK, KEEL BEAM CROSS OVER RIB CRACKED AFT OF LT GEAR DOOR. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950623004941995062300494NM 1995 6 23 SWAA950460 119950605A215039267831 SENSOR BOEING737 7373H4 1384600NM RT PACK INOP A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07663SW 23256 AFTER TAKEOFF, UNABLE TO CONTROL CABIN PRESSURIZATION USING AUTO, STANDBY OR MANUAL. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED BITE TEST, ALL SYSTEMS NORMAL PER BOEING M/M. RIGHT PACK THEN TRIPPED ON GROUND AND WOULDN'T RESET. REPLACED TURBINE INLET SENSOR PER BOEING M/M. 2L72 4F RTA16WE 19950623005091995062300509NM 1995 6 23 95ZZZZ267 119950606A27502061141 FLAP POS IND BOEING737 73733A 1384673NM TE FLAPS NOISY A AWXAO OTHER O OTHER APAPPROACH 1 WP28174AW 582 23633 MCI-PHX - FLT 830 - ON APPROACH, THE FLAPS DID NOT EXTEND BEYOND 1 UNIT. USING ALT FLAPS, THE T/E FLAPS WOULD NOT GO BEYOND 10 UNIT. NO ASYMMETRICAL INDICATIONS NOTED IN L/E OR T/E FLAPS. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED ALTERNATE FLAP MOTOR PER BMM 27 51 55, PG 401/403. REMOVED AND REPLACED INDICATOR PER MM 27 58 41, PG 401/404. OPS CK OK. REMOVED AND REPLACED FLAP CONTROL CABLE TENSION SWITCH PER MM 27 51 97. DRAINED AND SERVICED ALL 8 FLAP TRANSMISSIONS AND PER MM 27 51 00, ADJUSTED FLAP TRANSMISSIONS TO 180 DEGREES OFF UP STOPS. OPS CK OK, ACFT RETURNED TO SERVICE. REF 95ZZZZ268, AWXA9500355. 2L72 4F RTA16WE 19950623005101995062300510NM 1995 6 23 95ZZZZ268 119950606A2750793T1007 FLAP DRIVE ASSY BOEING737 73733A 1384673NM TE FLAPS BAD A AWXAO OTHER O OTHER APAPPROACH 1 WP28174AW 7488 23633 MCI-PHX - FLT 830 - ON APPROACH, THE FLAPS DID NOT EXTEND BEYOND 1 UNIT. USING ALT FLAPS, THE T/E FLAPS WOULD NOT GO BEYOND 10 UNIT. NO ASYMMETRICAL INDICATIONS NOTED IN L/E OR T/E FLAPS. ACFT LANDED WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED ALTERNATE FLAP MOTOR PER BMM 27 51 55, PG 401/403. REMOVED AND REPLACED INDICATOR PER MM 27 58 41, PG 401/404. OPS CK OK. REMOVED AND REPLACED FLAP CONTROL CABLE TENSION SWITCH PER MM 27 51 97. DRAINED AND SERVICED ALL 8 FLAP TRANSMISSIONS AND PER MM 27 51 00, ADJUSTED FLAP TRANSMISSIONS TO 180 DEGREES OFF UP STOPS. OPS CK OK, ACFT RETURNED TO SERVICE. REF 95ZZZZ267, AWXA9500355. 2L72 4F RTA16WE 19950623005111995062300511EU 1995 6 23 95ZZZZ269 119950610A33501013081 LIGHT ASSEMBLY AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN SEVERAL AREAS, AND THE LT MID CABIN OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED MID CABIN POWER SUPPLY AND EMERGENCY EXIT SIGN ASSEMBLY. ALL OPS CHECK GOOD. REF AWXA9500362. 2L72 4F RTA28NM 19950623005121995062300512NM 1995 6 23 AWXA9500338 119950602A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28174AW 23633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 9ABC. REPAIRED BROKEN WIRE, OPS CHECK GOOD. 2L72 4F RTA16WE 19950623005131995062300513NM 1995 6 23 AWXA9500339 119950604A3350 EEL WIRING BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 THROUGH ROW 29. RESECURED AND REPAIRED WIRING AT ROWS 18, 24 AND 25, OPS CHECK GOOD. (Z) 2L72 4F RTA2NM 19950623005141995062300514NM 1995 6 23 AWXA9500340 119950604A3350900835A EEL BATT PACK BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28181AW 22648 DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950623005151995062300515NM 1995 6 23 AWXA9500355 119950606A2750F75935 CONTROL SWITCH BOEING737 73733A 1384673NM TE FLAPS INOP A AWXAO OTHER O OTHER APAPPROACH 1 WP28174AW WN0003 23633 MCI-PHX - FLT 830 - ON APPROACH, THE FLAPS DID NOT EXTEND BEYOND 1 UNIT. USING ALT FLAPS, THE T/E FLAPS WOULD NOT GO BEYOND 10 UNIT. NO ASYMMETRICAL INDICATIONS NOTED IN L/E OR T/E FLAPS. AC LANDED WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED ALTERNATE FLAP MOTOR PER BMM 27 51 55, PG 401/403. REMOVED AND REPLACED INDICATOR PER MM 27 58 41, PG 401/404. OPS CK OK. REMOVED AND REPLACED FLAP CONTROL CABLE TENSION SWITCH PER MM 27 51 97. DRAINED AND SERVICED ALL 8 FLAP TRANSMISSIONS AND PER MM 27 51 00, ADJUSTED FLAP TRANSMISSIONS TO 180 DEGREES OFF UP STOPS. OPS CK OK, AC RETURNED TO SERVICE. REF 95ZZZZ267, 95ZZZZ268. 2L72 4F RTA16WE 19950623005161995062300516NM 1995 6 23 AWXA9500357 119950605A335020121 EEL BATT CHG BOEING757 757225 1384959NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28907AW 22691 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECK NORMAL. (Z) 2L72 4F RTA2NM 19950623005171995062300517NM 1995 6 23 AWXA9500358 119950608A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE IN AREA OF L2 DOOR. RECONNECTED WIRES, OPS CHECK GOOD. (Z) 2L72 4F RTA2NM 19950623005181995062300518NM 1995 6 23 AWXA9500361 119950610A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGECNY EXIT LIGHTS INOPERATIVE FROM AFT LAVS TO AFT GALLEY, APPROXIMITELY 20 ROWS. REPAIRED SEVERAL BROKEN WIRES, OPS CHECK GOOD. (Z) 2L72 4F RTA2NM 19950623005191995062300519EU 1995 6 23 AWXA9500362 119950610A3350321452 POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN SEVERAL AREAS, AND THE LT MID CABIN OVERWING EXIT SIGN INOPERATIVE. REMOVED AND REPLACED MID CABIN POWER SUPPLY AND EMERGENCY EXIT SIGN ASSEMBLY. ALL OPS CHECK GOOD. REF 95ZZZZ269. 2L72 4F RTA28NM 19950623005201995062300520EU 1995 6 23 AWXA9500363 119950610A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 PHX - DURING A ROUTINE MAINTENANCE CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAULTED DURING TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (Z) 2L72 4F RTA28NM 19950623005211995062300521NM 1995 6 23 AWXA9500367 119950610A5347BAC1520792 SEAT TRACK BOEING737 737277 1384570NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND RT O/B SEAT TRACK BETWEEN BS 328R AND BS 344R RBL 45 CORRODED. REMOVED AND REPLACED CORRODED SECTION PER SRM 53 10 5 FIG 2. (Z) 2L72 4F RTA16WE 19950623005221995062300522NM 1995 6 23 AWXA9500368 119950610A5330 SKIN BOEING737 737277 1384570NM R1 DOOR AREA CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND A 1 INCH CRACK IN R1 DOOR CUTOUT AFT LOWER CORNER. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 53-30-3 FIG 26. (Z) 2L72 4F RTA16WE 19950623005231995062300523NM 1995 6 23 AWXA9500376 119950610A5754 SKIN BOEING737 737277 1384570NM NR 1 SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND NR 1 SLAT LOWER L/E CRACKED AT RIVETS. FABRICATED AND INSTALLED REPAIRS IAW ER 2 57 55 33. TOTAL CYCLES 34804. (W) 2L72 4F RTA16WE 19950623005241995062300524WP 1995 6 23 95ZZZM70 119950529A32607000010101 SWITCH DOUG DC9 DC931 3022065WP NOSE GEAR INOPERATIVE A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19972VJ 47052 CLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND THE WIRING CONDUIT. THE GEAR WAS CYCLED SEVERAL TIMES. OPERATIONS CHECKED GOOD. 2L72 4F A6WE 19950623005251995062300525EU 1995 6 23 95ZZZM71 119950519A49307511151 FUEL FILTER FOKKERF28 F28MK4000 4990810EU APU INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19480AU 11229 BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED. THE CAPTAIN COULD NOT RESTART. THE DECISION WAS MADE TO DIVERT TO BWI. MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER. OPERATIONS CHECKED GOOD. 2L72 4F RTA20EU 19950623005261995062300526NM 1995 6 23 95ZZZM72 119950519A3350500000043 CHARGER BOEING737 7372B7 1384560NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19277AU 22889 CLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER. 2L72 4F A16WE 19950623005271995062300527WP 1995 6 23 95ZZZM73 119950606A3260 GEAR SWITCH DOUG DC9 DC932 3022066WP RT MLG FAILED A VJ6AL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO11908VJ 47321 FLT NR 7001 - ATL-ATL - PILOT TRAINER, ON APPROACH TO ATL HAD A RT GEAR UNSAFE IND, VISUALLY CHECKED GEAR BY TOWER AND PERISCOPE, LANDED. ATL MAINTENANCE INSTALLED GEAR PINS ON TAXIWAY. TAXI TO RAMP. FOUND PUSHED PIN ON RT GEAR DOWN SWITCH, REPAIRED PIN, GEAR CHECKS OK PER MM 32-00. (M) 2L72 4F A6WE 19950623005281995062300528WP 1995 6 23 95ZZZM74 119950512A5320 BRACKETS DOUG DC8 DC873F 302199FWP CARGO DECK CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND CARGO DECK INTERCOSTAL BRACKETS CRACKED 5 A 22 INCHES PLUS X, 2 INCHES Z AT Y 781.500, Y789, Y822.5, Y742.250 AND Y759.000. REPAIRED IAW DWG HSE 27-53-176 DATED 4-20-95 DOC ON FAA 8110-3 DATED 4-26-95, DWG HSE 27-53-177 DATED 4-20-95 DOC ON FAA 8110-3 DATED 4-26-95 BY FAA DER. 2L74 4F RT4A25 19950623005291995062300529WP 1995 6 23 95ZZZM75 119950512A5330 SKIN DOUG DC8 DC873F 302199FWP FS 67-80 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND CREW CABIN FUSELAGE STATION 80.000 TO 67.000 NLG WHEEL WELL UPPER SKIN WITH CORROSION. REPAIRED BY REPLACING FRAME SECTION IAW SRM 51-1-21. 2L74 4F RT4A25 19950623005301995062300530WP 1995 6 23 95ZZZM76 119950512A5320 SPLICE DOUG DC8 DC873F 302199FWP FS 1480 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, AT AFT C/C Y1480 BETWEEN LONGERON 25R AND 27R FRAME SPLICE HAS CORROSION. REPAIR SPLICE IAW SRM 53-1-0 AND 51-1-20. 2L74 4F RT4A25 19950623005311995062300531WP 1995 6 23 95ZZZM77 119950512A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1520-1540 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND AT AFT C/C FROM Y1520 TO Y1540 LONGERON 31L WITH CORROSION. REPAIRED IAW SRM 51-1-20 AD FAB ANGLE DWG NR HSE 27-53-187 DATED 4-25-95 DOC ON FAA 8110-3 DATED 4-30-95. 2L74 4F RT4A25 19950623005321995062300532WP 1995 6 23 95ZZZM78 119950512A5311 FRAME DOUG DC8 DC873F 302199FWP FS 140 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND L/COMP Y140 BETWEEN LONGERON 34L PLUS 35R FRAME LOWER FLANGE WITH CORROSION PLUS CRACK AT 35 RT. REPAIR FRAME SECTION AT Y140 BETWEEN 34L PLUS 35R IAW SRM 53-2-0 FIG 2 CLASS A. 2L74 4F RT4A25 19950623005331995062300533WP 1995 6 23 95ZZZM79 119950512A5230 BRACKET DOUG DC8 DC873F 302199FWP BAGGAGE DOOR CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, DOOR SUPPORT BRACKET AT PIT C DOOR CRACK. REPAIR IAW SRM 53-1-0, 51-1-8, 51-1-20 AND DWG NR HSE 27-53-179 AND EO NR C 0027-53-20-95 DATED 4-24-95 DOC FAA 8110-3 DATED 4-26-95. 2L74 4F RT4A25 19950623005341995062300534WP 1995 6 23 95ZZZM80 119950512A5320 T-FITTING DOUG DC8 DC873F 302199FWP FS 440-480 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND LOWER FUSELAGE FORWARD CARGO COMPARTMENT FROM Y 480.000 TO Y 440.000 LONGERON 21R TEE FITTING WITH CORROSION. REPAIRED IN CUSP EXTRUSION IAW ROO SKETCH 95-04-18-002 FROM DOUGLAS A/C COMPANY, DOC ON FORM 8110-3 DATED 4-20-95. 2L74 4F RT4A25 19950623005351995062300535WP 1995 6 23 95ZZZM81 119950512A5311 FRAME DOUG DC8 DC873F 302199FWP FS 1140 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND LOWER FUSELAGE AFT CARGO COMPARTMENT Y1140 BETWEEN LONGERON 25L AND 26L FRAME CORRODED. REPAIRED IAW EO NR C 00-27-57-012-95 PLUS DWG NR HSE-27-53-175 DATED 4/20/95 DOC ON FAA 8110-3 DATED 4-26-95. 2L74 4F RT4A25 19950623005361995062300536WP 1995 6 23 95ZZZM82 119950512A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19873SJ 46091 DURING C-CHECK, FOUND 2 CRACKS ON EXT SKIN BY PIT 'A' DOOR. REPAIRED SKIN IAW SRM 52-20-0 FIG 4. 2L74 4F RT4A25 19950623005371995062300537NM 1995 6 23 95ZZZM83 119950525A5210507945114 DOOR BOEING727 727225 1384077NM CABIN NOT SEALED A UHVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17355PA56567 20625 RETURN FROM FLIGHT, A HISSING SOUND WAS HEARD JUST AFTER VR COMING FROM THE L-1 CABIN DOOR AREA. THE AIRCRAFT FAILED TO PRESSURIZE, CAPTAIN DECIDED TO RETURN TO MYR. AFTER LANDING MAINTENANCE INSPECTED THE DOOR AND FOUND EVERYTHING TO BE NORMAL, NO DISCREPANCIES FOUND. 2L73 4F A3WE 19950623005381995062300538WP 1995 6 23 95ZZZM84 119950522A5313 LONGERON DOUG DC8 DC863F 302198FWP FS 1070/1090 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 LEVEL 2 CORROSION FOUND ON OUTBOARD FLANGE OF LONGERON 31R BETWEEN FS 1070 AND FS 1090. MECHANICALLY REMOVED CORROSION FROM LONGERON 31R, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER IAW DER DRAWING ARW 30218-10. 2L74 4F 4A25 19950623005391995062300539WP 1995 6 23 95ZZZM85 119950518A5312 BLKHD STIFFENER DOUG DC8 DC863F 302198FWP FS 980 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 LEVEL 2 CORROSION FOUND AFT SIDE FS 980.00 BULKHEAD AT LONGERON 30L ATTACHMENT. MECHANICALLY REMOVED CORROSION, TREATED, PRIMED AREA, AND INSTALLED REPAIR DOUBLER IAW DER DRAWING ARW 5598-3. 2L74 4F 4A25 19950623005401995062300540WP 1995 6 23 95ZZZM86 119950525A53204779940 FITTING DOUG DC8 DC863F 302198FWP FS 1050 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 SPLICE FITTING AT FS 1050 ON TOP SIDE OF L-31R HAS LEVEL 2 CORROSION. REMOVED SPLICE FITTING. REMOVED LIGHT CORROSION FROM AREA. DRILLED NEW FITTING. TREATED, PRIMED, AND INSTALLED FITTING IAW SRM 51-1-8 AND 51-1-20A. AREA UNDER FITTING WITHIN LIMITS IAW 53-2-0. 2L74 4F 4A25 19950623005411995062300541WP 1995 6 23 95ZZZM87 119950531A5330 SKIN DOUG DC8 DC863F 302198FWP NLG DOOR CUTOUT CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 PREVIOUS FUSELAGE PLATING REPAIR AFT OF NLG RT SIDE IS LOOSE AND RIVET HEAD SHEARED (NLG DOOR CUTOUT). REMOVED DOUBLER. FOUND PROPAGATION OF PREVIOUS STOP DRILLED CRACK. CUT TO DAMAGED AREA APPROXIMATELY 6 INCHES BY 8 INCHES FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-21A. 2L74 4F 4A25 19950623005421995062300542WP 1995 6 23 95ZZZM88 119950525A53203759545502 FITTING DOUG DC8 DC863F 302198FWP FS 1050 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 LONGERON SPLICE FITTING AT FS 1050 ON LONGERON 35R IS CRACKED. REMOVED LONGERON SPLICE FITTING, LOCATED FITTING. DRILLED UP NEW FITTING. TREATED AND PRIMED AREA. INSTALLED, TREATED, AND PRIMED NEW FITTING IAW SRM 51-1-8 AND 51-1-20. 2L74 4F 4A25 19950623005431995062300543WP 1995 6 23 95ZZZM89 119950531A532097549441 DOOR JAMB DOUG DC8 DC863F 302198FWP BAGG COMPT CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING AN 'A' CHECK INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON NR 3 BAG BIN DOOR JAMB AT APPROXIMATELY MIDWAY HIGH. MECHANICALLY REMOVED CORROSION PER DC8 SRM 51-1-8. TREATED AND PRIMED ARE IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER DWG ARW 29976-38. 2L74 4F 4A25 19950623005441995062300544WP 1995 6 23 95ZZZM90 119950531A53112537716 FRAME DOUG DC8 DC863F 302198FWP FS 1040 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING 'A' CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION ON CIRCUMFERENTIAL FRAME AT FS 1040, LONGERON 30L. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DER DWG ARW 12564-74. 2L74 4F 4A25 19950623005451995062300545SO 1995 6 23 C2XA95CL090 119950602A26126468 MODULE CONTROL EMB 120 EMB120RT SO RT ENGINE FAILED A C2XAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 SW094772210813 1079 120166 FLT NR 3211 - BUF-CLE - RIGHT ENGINE FIRE WARNING LIGHT CAME ON DURING TAXI IN TO GATE IN CLEVELAND. RIGHT ENGINE WAS SHUTDOWN ON TAXI WAY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FIRE DAMAGE. MAINTENANCE REMOVED AND REPLACED RIGHT FORWARD DETECTION CONTROL MODULE IAW 26-11-02. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT WAS TEST FLOWN, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950623005461995062300546SO 1995 6 23 C2XA95CL091 119950602A26126468 MODULE CONTROL EMB 120 EMB120RT SO RT ENG FAILED A C2XAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 SW094772210813 1075 120166 FLT NR 3211 - BUF-CLE - RIGHT ENGINE FIRE WARNING LIGHT CAME ON DURING TAXI IN TO GATE IN CLEVELAND. RIGHT ENGINE WAS SHUTDOWN ON TAXI WAY. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO FIRE DAMAGE. MAINTENANCE REMOVED AND REPLACED RIGHT AFT DETECTION CONTROL MODULE IAW 26-11-02. OPS CHECKED GOOD AT THIS TIME. AIRCRAFT WAS TEST FLOWN, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950623005471995062300547 1995 6 23 USAA950513 419950514A344220671570153 TRANSCEIVER BOEING737 737201 1384454NM RADAR FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19229US 21818 CLT - FLT 1257 - FLIGHT EN ROUTE FLL TO DCA WHEN WEATHER RADAR FAILED. AIRCRAFT DIVERTED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WEATHER RADAR TRANSCEIVER. (M) 2L72 4F A16WE 19950623005481995062300548WP 1995 6 23 USAA950519 119950416A5315991556171 FLOORBEAM DOUG DC9 DC931 3022065WP FS 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19938VJ37875 48119 PIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL 2 CORROSION. REF, TASK NR C58-5330 STATION 996 LEFT FLOORBEAM. MANUAL FLOORBEAM CAP ANGLE FROM 7075-T6 EXTENSION AND INSTALLED REPAIR ANGLE PER SRM 53-05 FIG 72. (M) 2L72 4F A6WE 19950623005491995062300549WP 1995 6 23 USAA950522 119950518A3350 EEL BATTERIES DOUG DC9 DC931 3022065WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19929VJ 48118 BOS - FLT 0051 - THE COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2L72 4F A6WE 19950623005501995062300550EU 1995 6 23 USAA950523 119950519A49306925451 FUEL VALVE FOKKERF28 F28MK4000 4990810EU APU INOPERATIVE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19480AU 11229 BWI - FLT NR 0451 - EN ROUTE TO CLT, THE APU FAILED. THE CAPTAIN COULD NOT RESTART. THE DECISION WAS MADE TO DIVERT TO BWI. MAINTENANCE REPLACED THE APU FUEL SOLENOID VALVE AS A PRECAUTION AND THE FUEL FILTER. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA20EU 19950623005511995062300551WP 1995 6 23 USAA950524 119950520A3350 EEL BATTERIES DOUG DC9 DC931 3022065WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19973VJ 47099 PIT - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE LIGHTS AND REPLACED THE BATTERIES IN THE BATTERY PACK NR 1. OPERATIONS CHECKED NORMAL. (M) 2L72 4F A6WE 19950623005521995062300552WP 1995 6 23 USAA950526 119950523A2550 CARGO NET DOUG DC9 DC982 3022082WP CARGO COMPT OUT OF POSITION A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19829US 49429 BOS - FLIGHT 0120 - WHILE ON ROTATION, THE CREW FELT A BUMP THEN NOTICED THE FORWARD CARGO DOOR LIGHT ILLUMINATED. THE CAPTAIN DECIDED TO RETURN TO BOS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PRESSURIZED THE AIRCRAFT AND CHECKED FOR LEAKS. NONE WERE FOUND. REMOVED CARGO NETTING OBSTRUCTING THE TARGET SWITCH. OPERATION OF THE CARGO DOOR AND SEALS CHECKED GOOD. (M) 2L72 4F A6WE 19950623005531995062300553NM 1995 6 23 USAA950527 119950517A7830 FITTING BOEING737 737201 1384454NM RT TR UNIT CRACKED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19232US12437 22018 JFK - FLT 968 - ON INITIAL CLIMB-OUT OF LGA, 'A' SYSTEM HYDRAULICS FAILED. FLIGHT DIVERTED INTO JFK WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED TEE FITTING AT RIGHT THRUST REVERSER PRESSURE SWITCH, 'A' SYSTEM HYDRAULICS RETURN, PRESSURE AND CASE DRAIN FILTERS, AND NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS. (M) 2L72 4F A16WE 19950623005541995062300554NM 1995 6 23 USAA950528 119950519A3350900835A BATTERY PACK BOEING737 7372B7 1384560NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19277AU 22889 CLT - EXTERIOR AFT EMERGENCY LIGHTS AT BOTH AFT DOORS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND CHARGER. (M) 2L72 4F A16WE 19950623005551995062300555NM 1995 6 23 USAA950529 119950520A2810 FUEL TANK BOEING737 7374B7 1384702NM LEFT WING LEAK A USAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 EA19433US 24555 CLT - FLT NR 2195 - ON TAKEOFF FROM DCA EN ROUTE MSY, FUEL LEAK NOTICED ON LEFT WING AT ENGINE COWLING. FLIGHT DIVERETED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. SECURED SCREW IN PANEL AT LEFT ENGINE TOP COWL AND RESEALED TANK, CHECKS OK. (M) 2L72 4F RTA16WE 19950623005561995062300556NM 1995 6 23 USAA950532 119950522A3010 ANTI-ICE DUCT BOEING737 737201 1384454NM NR 1 ENG CRACKED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19260AU 22866 TPA - FLT 1569 - ON CLIMB-OUT OF TPA, NR 1 ENGINE OVERHEAT LIGHT CAME ON. FLIGHT RETURNED TO TPA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE COWL ANTI-ICE DUCT. (M) 2L72 4F A16WE 19950623005571995062300557WP 1995 6 23 USAA950533 119950529A32601D32241051 CONDUIT DOUG DC9 DC931 3022065WP NOSE GEAR INOPERATIVE A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19972VJ 47052 CLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY. MAINTENANCE REPLACED THE NOSE GEAR DOWNLOCK SWITCH AND THE WIRING CONDUIT. THE GEAR WAS CYCLED SEVERAL TIMES. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950623005581995062300558NE 1995 6 23 USAA950534 219950528A7261 FILTER DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE LEAKING A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19965VJ 47374 CVG - FLIGHT 0404 - CREW RECEIVED AN ERRATIC 'RIGHT OIL STRAINER CLOGGING' ANNUNCIATOR LIGHT BUT DID NOT EXTINGUISH WITH THE THROTTLE TO IDLE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. THE FLIGHT DIVERTED TO CVG. SINGLE ENGINE TIME WAS APPROXIMATELY 15 MINUTES. MAINTENANCE DRAINED THE OIL TANK AND INSTALLED A NEW RIGHT MAIN OIL FILTER. THE ENGINE OIL WAS SERVICED. NO LEAKS WERE FOUND. (M) 2L72 4F4 F A6WE E2EA 19950623005591995062300559NE 1995 6 23 USAA950535 219950529A7314378200 FUEL PUMP DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE LT ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19951VJ32447 47576 ROC - FLT NR 0581 - THE LEFT ENGINE FAILED AS THE GEAR WAS RETRACTED. THE CREW RETURNED TO ROC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED FUEL PUMP. (M) 2L72 4F4 F A6WE E2EA 19950623005601995062300560NM 1995 6 23 USAA950537 119950501A335086210066 EEL BATTERY PACK BOEING757 7572B7 1384964NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19624AU 27245 PHL - THE EMERGENCY FLOOR LIGHTING BATTERY PACKS WERE FOUND TO BE INOPERATIVE AT ROWS 1, 4, 6, 9, 13, 19, 25, 26, AND 29. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTING BATTERY PACKS. (M) 2L72 4F RTA2NM 19950623005611995062300561EU 1995 6 23 USAA950541 119950415A335014597101 EEL BATTERY PACK FOKKERF28 F28MK4000 4990810EU MAIN DOOR DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19481US 11230 CLE - THE MAIN ENTRANCE DOOR OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA20EU 19950623005621995062300562NM 1995 6 23 USAA950543 119950527A2740 BEARINGS BOEING737 7373B7 1384580NM STAB TRIM COLUMNDETERIORATED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19398US 23507 GSO - FLT NR 2622 - AFTER TAKEOFF FROM CLT EN ROUTE ALB, STAB TRIM WHEEL MADE A LOUD GRINDING NOISE. AUTOPILOT TRIM WAS THE SAME. FLIGHT DIVERTED TO GSO WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BEARINGS FOR STAB TRIM MAINSHAFT IN PEDESTAL. STAB TRIM OPERATES NORMAL IN BOTH MANUAL AND ELECTRIC MODE. (M) 2L72 4F RTA16WE 19950623005631995062300563NM 1995 6 23 USAA950544 119950529A32414271902 CONTROL UNIT BOEING737 737301 1384611NM ANTI-SKID SYSTEMFAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19592US 23937 BWI - FLT 126 - FLIGHT EN ROUTE MCO TO DCA WHEN ANTI-SKID INOP LIGHT ILLUMINATED. FLIGHT DIVERTED TO BWI DUE TO RUNWAY LENGTH. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT. (M) 2L72 4F RTA16WE 19950623005641995062300564WP 1995 6 23 95ZZZM100 119950603A2750 RETRACT MECH DOUG DC8 DC863 302198AWP TE FLAPS MALFUNCTIONED A RRXAO OTHER O OTHER DEDESCENT 1 WP15964R 46000 FLT NR 102 - KDAY-KPDX - DURING DESCENT INTO KPDX FLAPS AT 12 DEGREES OK. GREATER THAN 12 DEGREES CAUSES EXCESSIVE RIGHT ROLL. AT 35 DEGREES INDICATION IS 28 DEGREES. UNDER INVESTIGATION. 2L74 4F 4A25 19950623005651995062300565WP 1995 6 23 95ZZZM101 119950602A5414 PLANK DOUG DC8 DC862F 3021972WP NR 1 PYLON CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15997CF 46154 FLT 040 - KDAY-KMEM - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STATION YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS. 2L74 4F 4A25 19950623005661995062300566CE 1995 6 23 95ZZZM102 119950522A3260H111541 UPLOCK SWITCH BEECH 1900 1900C 1154161CE RT MLG SHORTED A GPPAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 CE09317BH UB32 AFTER DEPARTURE FROM GJT, FLIGHT NR 2259 RETURNED TO GJT WHEN THE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. GP EXPRESS MAINTENANCE FOUND A DEFECTIVE RT MLG UPLOCK SWITCH. SWITCH WAS REPLACED WITH A NEW UNIT AND GEAR WAS CYCLED SEVERAL TIMES WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19950623005671995062300567EA 1995 6 23 95ZZZM103 219950509A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LEFT FAILED A GPPAE ENGINE SHUTDOWN JY WARNING INDICATION ENGINE STOPPAGE APAPPROACH 1 CE09318BH15630 UB33 32173 FLT NR 2094 - ON APPROACH TO BFF EXPERIENCED A SLIGHT VIBRATION FOLLOWED BY LEFT ENGINE SHUTDOWN, SHORTLY AFTER REDUCING POWER FOR APPROACH. AIRCRAFT LANDED SAFELY IN BFF WHERE GP EXPRESS MAINTENANCE FOUND THE ENGINE COMPLETELY SEIZED. ENGINE WAS REPLACED WITH A SERVICEABLE UNIT AND AIRCRAFT WAS RETURNED TO SERVICE. ENGINE WAS SHIPPED TO OVERHAUL FACILITY FOR TEARDOWN. 2L72 4T4 TRTA24CE E4EA 19950623005681995062300568CE 1995 6 23 95ZZZM104 119950522A712011491003279 TRUSS ASSY BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GPPAK NONE O OTHER ININSP/MAINT 1 CE09319BH UB36 WHILE COMPLYING WITH AD 95-02-18, AREA A, GP EXPRESS MAINTENANCE FOUND THE RT ENGINE TRUSS CRACKED IN THE FORWARD UPPER OUTBOARD POSITION. TRUSS WAS REPLACED WITH NEW P/N 114-910032-79 TRUSS ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19950623005691995062300569CE 1995 6 23 95ZZZM105 119950522A32601003810061 UPLOCK SWITCH BEECH 99 C99 1154006CE NLG MALFUNCTIONED A GPPAO OTHER N FALSE WARNING CRCRUISE 1 CE09112GP U214 FLT NR 2090 - DEN - UPON LANDING REPORTED THAT THE GEAR INTRANSIT LIGHT HAD ILLUMINATED DURING FLIGHT. AIRCRAFT WAS FERRIED TO GRI WHERE GP EXPRESS MAINTENANCE FOUND A DEFECTIVE NOSE GEAR UPLOCK SWITCH. SWITCH WAS REPLACED WITH A NEW UNIT AND GEAR WAS RETRACTED SEVERAL TIMES WITH NO DISCREPANCIES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 3T A14CE 19950623005701995062300570CE 1995 6 23 95ZZZM106 119950513A54001149800211 KEEL BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05812BE UB50 DURING LEFT ENGINE AND TRUSS REPLACEMENT THE LEFT NACELLE INBOARD AND OUTBOARD UPPER KEEL WEBS WERE FOUND TO BE CRACKED. TWO CRACKS WERE FOUND ON THE OUTBOARD KEEL, P/N 114-98002201. ONE CRACK, APPROXIMATELY 1.25 INCH LONG, WAS LOCATED BETWEEN THE UPPER 2 RIVETS ON THE FORWARD SIDE OF THE KEEL WEB JUST BELOW THE UPPER OUTBOARD TRUSS ATTACH FITTING. A SECOND CRACK, APPROX 3 INCHES LONG, ON THE LOWER SIDE OF THE SAME FLANGE THROUGH THE ATTACHING HI-LOK FASTENERS WAS ALSO FOUND. ONE CRACK APPROX 1.25 INCH LONG, WAS FOUND ON THE INBOARD KEEL P/N 114-980021-1 RUNNING VERTICALLY THROUGH THE TOP TWO RIVETS ON THE FWD SIDE OF THE KEEL WEB JUST BEING DEVELOPED AT THE TIME OF THIS WRITING. 2L72 4T RTA24CE 19950623005711995062300571CE 1995 6 23 95ZZZM107 119950513A54001149800221 KEEL BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05812BE UB50 DURING LT ENG & TRUSS REPLACEMENT, LT NACELLE INBD & OTBD UPPER KEEL WEBS FND CRACKED. TWO CRACKS FND ON OTBD KEEL, P/N 114-98002201. ONE CRACK, APPROX 1.25 INCH LONG, LOCATED BETWEEN UPPER 2 RIVETS ON FWD SIDE OF KEEL WEB JUST BELOW UPPER OTBD TRUSS ATTACH FITTING. A SECOND CRACK, APPROX 3 INCHES LONG, ON LOWER SIDE OF SAME FLANGE THRU THE ATTACHING HI-LOK FASTENERS WAS ALSO FOUND. ONE CRACK APPROX 1.25 INCH LONG FND ON INBD KEEL, P/N 114-9800211, RUNNING VERTICALLY THRU TOP 2 RIVETS ON FWD SIDE OF KEEL WEB JUST BEING DEVELOPED. SDR IS TO CLOSE SDR OF 5-13-95 WHERE LT NACELLE INBD & OTBD UPPER KEEL WEBS WERE FND CRACKED. ACFT REPAIRED IAW APROVED DATA & RETND TO SERVICE. REF OPR CNTRL NR PLGA11195G1.(X)2L72 4T RTA24CE 19950623005721995062300572NE 1995 6 23 95ZZZM108 319950620A61116607132886 SLEEVE SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE PROP BLADE WORN A PLGAO OTHER E VIBRATION/BUFFET ININSP/MAINT 1 NE05366BE 340B303 DRG189789 PROP ASSEMBLY REMOVED FOR A REPORTED VIBRATION. FURTHER INSPECTION REVEALED MOVEMENT WAS NOTED OUTBOARD OF THE COUNTER WEIGHT ASSEMBLY ON ALL FOUR BLADES. THIS MOVEMENT WAS DEEMED UNSERVICEABLE PER DOWTY CM 61-10-36 CHECK SECTION PG 501-506. ASSEMBLY WAS DISASSEMBLED FOR SHIPMENT TO DOWTY AEROSPACE AVIATION SERVICES FOR FURTHER INSPECTION AND OVERHAUL. AFTER DISASSEMBLY OIL WAS FOUND IN THE HUB AREA. S/D - THE REPORTED DISCREPANCY WAS VERIFIED BY THE SERVICE SHOP AND DETERMINDED TO BE THE RESULT OF A WORN SEAL GROOVE IN THE HUB AND WEAR BEYOND MANUAL LIMITS IN THE BLADE INNER SLEEVES. (M) 2L72 4T RTA52EU 6 CP61GL 19950623005731995062300573NM 1995 6 23 95ZZZM91 119950522A3350080202120 EEL FLOOR TRACK BOEING737 737242 1384477NM CABIN SHORTED A A6XAK NONE L NO TEST ININSP/MAINT 1 SO13159PL 21186 FIRST SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOP. WATER FROM ICE COOLER ENTERING AREA BETWEEN BASE TRACK AND LIGHT COVER CAUSING FIRST SECTION SHORT AND CORRODING CONNECTIONS. REPLACED LEAD FROM WALL TO TRACK, CLEANED AND DRIED TRACK AND CONNECTIONS. APPLIED SEALANT TO TRACK AND COVER IN AREA AFFECTED. (M) 2L72 4F A16WE 19950623005741995062300574WP 1995 6 23 95ZZZM92 119950526A291355096 HYDRAULIC PUMP DOUG DC8 DC851 3021920WP NR 2 ENGINE FAILED A FXLAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO19508DC 45935 ON APPROACH MIAMI EXPERIENCED LOSS OF HYDRAULIC FLUID. SHUTDOWN HYDRAULIC SYSTEM. NOTIFIED MIAMI TOWER AND LANDED MIAMI WITHOUT INCIDENT. INSPECTION REVEALED FLUID LEAK AT NR 2 ENGINE HYD PUMP SHAFT. REPLACED HYDRAULIC PUMP. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19950623005751995062300575WP 1995 6 23 95ZZZM93 119950606A3411 STATIC LINE DOUG DC8 DC851 3021920WP LT COCKPIT LOOSE A FXLAA UNSCHED LANDING O OTHER CLCLIMB 1 SO19508DC 45935 ON DEPARTURE MIAMI, CAPTAIN'S AIRSPEED AND ALT INOP. RETURNED AND LANDED MIAMI WITHOUT INCIDENT. INSPECTION FOUND LOOSE STATIC LINE AT CAPTAIN ALTIMETER TIGHTENED STATIC CONNECTIONS, PERFORMED STATIC SYSTEM CHECK AND FOUND TO BE NORMAL. PERFORMED OVERWEIGHT INSPECTION. RETURNED AIRCRAFT TO SERVICE. (M) 2L74 4F 4A25 19950623005761995062300576WP 1995 6 23 95ZZZM94 119950606A2612244F70G80 SENSOR DOUG DC8 DC8F54 3021926WP NR 2 ENGINE DETACHED A FXLAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO1957FB 45669 ON DEPARTURE MIAMI EXPERIENCED FIRE WARNING ON NR 2 ENGINE. SHUTDOWN ENGINE AND RETURNED AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED DETACHED FIRE WARNING SENSOR ON AFT COWL. PERFORMED OVERWEIGHT LANDING INSPECTION AND REPLACED FIRE WARNING SENSOR. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19950623005771995062300577WP 1995 6 23 95ZZZM95 119950601A2120 AIR DISTR DOUG DC9 DC932 3022066WP CABIN ODOR A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11918VV 47320 FLT 522 - SMOKE SMELL AFT OF EMERGENCY OVERWING EXITS. INSPECTION OF LIGHTS, SPEAKERS, CALL BUTTONS AND WIRING IN OVERWING EXIT AREAS AND BEHIND PANELS. NO DEFECTS NOTED MM 25-00. (M) 2L72 4F A6WE 19950623005781995062300578WP 1995 6 23 95ZZZM96 119950601A35304566M37B042NN PBE DOUG DC9 DC932 3022066WP CABIN FAILED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11933VV 47489 FLIGHT 528 - AFT PBE WAS FOUND TO BE FAULTY AND DETERIORATED. MAINTENANCE REPLACED PBE IN AFT OVERHEAD BIN RIGHT SIDE, THE LAST BIN, P/N 4566M37-B-042NN S/N OFF E9446743 S/N ON E9547745. 2L72 4F A6WE 19950623005791995062300579EU 1995 6 23 95ZZZM97 119950519A2430M833830111 RCCB CUTLERHAM SAAB SF340 SF340A 7850100EU E/E BAY LOOSE A CHQAK NONE O OTHER NRNOT REPORTED 1 EA23360CA 05759 340A006 WHEN ACTIVATING LEFT RECIRCULATION FAN SWITCH TO ON, CIRCUIT BREAKER WOULD POP. INSPECTED AND FOUND ON RCCB LOOSE AND ELECTRICAL CONNECTOR HAD SLIGHT HEAT DISTRESS. RCCB AND CONNECTOR WAS REMOVED AND REPLACED, SYSTEM OPERATES NORMALLY. (M) 2L72 4T RTA52EU 19950623005801995062300580NM 1995 6 23 95ZZZM98 119950530A5312 BLKHD LINER BOEING747 747122 1384872NM BS 2160 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02. (M) 2L74 4F A20WE 19950623005811995062300581NM 1995 6 23 95ZZZM99 119950530A5314 KEEL BEAM BOEING747 747122 1384872NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 ADF ANTENNA MOUNT STRUCTURE IS CORRODED (LEVEL 1) LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING SRM 51-10-01, PAGES 13, 14, 15, 16 PAR 6 AND 7. (M) 2L74 4F A20WE 19950623005821995062300582NM 1995 6 23 AALA950033H 119950518A5315 FLOORBEAM BOEING767 767223 1385123NM FS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 FLOORBEAM AT STATION 347 CORRODED FROM RBL 61 TO RBL 71.5 BEYOND SRM LIMITS. BLENDED AND TREATED AREA. INSTALLED REPAIR STRAP PER MRB 767-918. (M) 2L72 4F RTA1NM 19950623005831995062300583NM 1995 6 23 AALA950035H 119950518A5311146T1280 FRAME BOEING767 767223 1385123NM FS 1417 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - CORROSION ON WEB BLENDED BEYOND SRM LIMITS. INSTALLED REPAIR DOUBLER. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 18 MONTHS OR 3000 CYCLES REF RES 169518. ACCOMPLISHED PER MRB 767-920. (M) 2L72 4F RTA1NM 19950623005841995062300584NM 1995 6 23 AALA950038H 119950525A5311146T1205 FRAME BOEING767 767223 1385123NM FS 1175 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07319AA 22320 AFW - BLENDED CORROSION ON INNER CHORD FRAME, LOCATED ON LOWER SURFACE OF UPPER CHORD AT RBL 21 STATION 1175, EXCEEDS SRM LIMITS. BLENDED AND TREATED AREA. APPROVED FOR SERVICE PER MRB 767-924 DATED 5/12/95. (M) 2L72 4F RTA1NM 19950623005851995062300585EU 1995 6 23 AALA950839 119950507A3260 UPLOCK TARGET FOKKERF28 F28MK0100 4990807EU RT MLG OUT OF ADJUST A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW071461C 11481 ORD - FLT 1959 - AFTER DEPARTURE RIGHT LANDING GEAR DOOR LOCK MESSAGE ON MULTI FUNCTION DISPLAY UNIT CAME ON INTERMITTENTLY THEN EXTINGUISHED. LANDED ORD WITHOUT INCIDENT. ADJUSTED AFT UPLOCK TARGET. SYSTEM GROUND CHECKS NORMAL OPERATION. (M) 2L72 4F RT 19950623005861995062300586WP 1995 6 23 AALA950900 119950510A3350 EEL TERMINAL DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07479AA 49654 ORD - FLT 224 - DURING PREFLIGHT CHECK, EMERGENCY FLOOR LIGHT TERMINAL FOUND BROKEN AFFECTING LIGHT STRIP FROM PASSENGER SEAT ROW 7 AND AFT. REPLACED EMERGENCY FLOOR LIGHT FEMALE TERMINAL END BY PASSENGER SEAT ROW 7. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950623005871995062300587EU 1995 6 23 AALA950905 119950513A323171539 VALVE FOKKERF28 F28MK0100 4990807EU NLG DOOR DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW071448A 11457 DFW - FLT 1438 - AFTER TAKEOFF HRL WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEAR AND NOSE LANDING GEAR RETRACTED SLOWLY. AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950623005881995062300588EU 1995 6 23 AALA950908 119950515A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770054 461 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY R1 DOOR INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY R1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950623005891995062300589WP 1995 6 23 AALA950925 119950517A3350P2010031303 EEL DOUG DC9 DC982 3022082WP FWD GALLEY DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077533A 49987 RDU - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT FORWARD CORNER OF FORWARD GALLEY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AT FORWARD CORNER OF FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950623005901995062300590NM 1995 6 23 AALA950947 119950519A3350A3060698101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071768D 48436 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 7D AND 15C INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTORS AT PAX SEAT ROWS 7D AND 15C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19950623005911995062300591NM 1995 6 23 AALA950948 119950519A3350A3060698101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071768D 48436 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 21G THROUGH 38G INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19950623005921995062300592EU 1995 6 23 AALA950953 119950522A323171539 VALVE FOKKERF28 F28MK0100 4990807EU NLG DOOR DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071447L 11456 DFW - FLT 1618 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, UNABLE TO RETRACT NOSE LANDING GEAR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE AND VALVE RESTRICTOR. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950623005931995062300593WP 1995 6 23 AALA950954 119950519A3320MS3124E1415S CONNECTOR DOUG DC9 DC982 3022082WP CABIN OVERHEAD SHORTED A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW07486AA 49679 ORD - FLT NR 0205 - UPON ARRIVAL AT THE GATE, OVERHEAD FLUORESCENT LIGHT NEAR PASSENGER SEAT ROW 6 ARCED CAUSING SMOKE IN THE CABIN. PASSENGER DEPLANED NORMALLY. REPLACED OVERHEAD FLUORESCENT LIGHT CONNECTOR PI2101 AND RECEPTACLE R52105 IN CABIN OVERHEAD BY PASSENGER SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950623005941995062300594WP 1995 6 23 AALA950967 119950527A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07127AA 46948 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT AT 2L ILLUMINATED WITH SWITCH IN ARMED POSITION. RESET PIN IN CONNECTOR AM1-9 AND REPLACED BATTERY PACK AND CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950623005951995062300595NM 1995 6 23 AALA950968 119950527A3350A3060712101 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07847AA 20988 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS DIM AFT OF ROW 7. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT CLASS DIVIDER, REPLACED CENTER CAB CONTROL MODULE, AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950623005961995062300596EU 1995 6 23 AALA950977 119950529A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770073 516 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 14 TO 25 INOPERATIVE. REPAIRED WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950623005971995062300597EU 1995 6 23 AALA951005 119950530A3350A3060819104 EEL STRIP AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0718066 509 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FRONT OF THE L3 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FROM SIDE WALL TO LIGHT TRACK BY L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950623005981995062300598NM 1995 6 23 AALA951007 119950601A25302274501 CART BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07336AA 22334 BHX - FLT NR 0024 - BUSINESS CLASS GALLEY WARMING CARTS OVERHEATS SEVERELY WITH ELECTRICAL SMELL. REPLACED BUSINESS CLASS GALLEY WARMING CART. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950623005991995062300599WP 1995 6 23 AALA951010 119950601A3350 EEL WIRE DOUG DC10 DC1010 3022110WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07162AA 46943 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS ON LEFT SIDE OF FIRST CLASS AND LEFT FORWARD COACH INOPERATIVE. REPAIRED WIRE AT GALLEY CERACE SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950623006001995062300600EU 1995 6 23 AALA951025 119950602A3350A3060819104 EEL STRIP AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077082A 643 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING BY LAVATORY M INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP BY LAVATORY M. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950623006011995062300601WP 1995 6 23 AALA951055 119950605A3350P4010051127 EEL MODULE DOUG DC10 DC1010 3022110WP CABIN DEFECTIVE A AALAK NONE L NO TEST CRCRUISE 1 SW07162AA 46943 SFO - FLT 0028 - EN ROUTE HNL-SFO, DURING CRUISE, EMERGENCY FLOOR LIGHTS AT RT AISLE IN FIRST CLASS CABIN ILLUMINATED. AIRCRAFT PROCEEDED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED EMERGENCY FLOOR LIGHT CONTROL MODULE AT RT AFT AREA OF FIRST CLASS CABIN. ALSO, REPLACED ASSOCIATED EMERGENCY FLOOR LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950623006021995062300602SO 1995 6 23 C2XA95CL087 119950524A3350W220105324 EEL WIRE EMB 120 EMB120RT SO CABIN BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0951726 120174 DURING 1-A INSPECTION, FOUND EMERGENCY LIGHT ON OVERHEAD BIN 8 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE IAW 20-50-00. OPS CHECKED GOOD. (M) 2L72 4T RTA31SO 19950623006031995062300603CE 1995 6 23 PLGA523951 119950523A54001149800221 KEEL BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05817BE UB52 DURING NR 1 DETAIL (WING) INSPECTION, THE LEFT NACELLE UPPER FORWARD KEEL (OUTBOARD) WAS FOUND TO HAVE 4 CRACKS ON FORWARD EDGE FLANGE. THESE CRACKS WERE FROM .375 INCH TO 1 INCH IN LENGTH BETWEEN RIVETS ON FORWARD EDGE FLANGE. AN APPROVED REPAIR IS BEING DEVELOPED AT THE TIME OF THIS WRITING. THIS SDR IS TO CLOSE OUT AN SDR DATED 5-23-95 WHERE THE LEFT NACELLE UPPER FORWARD KEEL (OUTBOARD) WAS FOUND CRACKED. THE AIRCRAFT WAS REPAIRED IAW APPROVED DATA AND RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19950623006801995062300680WP 1995 6 23 ABXA9500561 119950621A323056487405502 UPLATCH DOUG DC8 DC863F 302198FWP RT MLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23819AX 45927 RIGHT MAIN LANDING GEAR DOOR FAILED UPLATCH CHECK. RECYCLED GEAR. LIGHT EXTINGUISHED. CLEANED, INSPECTED AND LUBED THE RIGHT MAIN GEAR DOOR UPLATCH. PERFORMED ADJUSTMENT TEST IAW MAB 32-6. OPS CHECKED GOOD. 2L74 4F 4A25 19950623006811995062300681WP 1995 6 23 ABXA9500562 119950620A56102654622 ROLLER 5613217508 DOUG DC9 DC941 302207NWP LT CV WINDOW OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING PREFLIGHT INSPECTION, FOUND CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. FOUND LOWER ROLLER OUT OF TRACK. REALIGNED ROLLER. CAPTAIN'S WINDOW OPS CHECKED GOOD IAW DC-9 M.M. 2L72 4F A6WE 19950623006821995062300682SO 1995 6 23 COM11921 119950615A275012042642507 FLAP HANDLE EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMAK NONE J WARNING INDICATION DEDESCENT 1 SO01246CA3342 120223 FLAP WARNING SYSTEM INDICATED CONTROL FAULT MALFUNCTION THREE TIMES DURING DESCENT. REMOVED AND REPLACED FLAP CONTROL HANDLE WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4T RTA31SO 19950623006831995062300683 1995 6 23 COM20379 419950620A341651928702502 ALTIMETER SWRNGNSA227 SA227AC 8780603SW LEFT DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO0127119161052168 AC701 PILOTS ALTIMETER RED FLAG. REPLACED ALTIMETER. 1L72 4T A8SW 19950623006841995062300684EU 1995 6 23 COM31110 119950621A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01146CA3212 302 AUG930548 340A146 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950623006851995062300685EA 1995 6 23 COM60501 119950615A2722AL00102 ACTUATOR CNDAIRCL600 CL6002B19 EA RUDDER INOP A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01936CA2377 7043 RUDDER CONFIG MESSAGE ALTHOUGH SYSTEM IS DEFERRED. WITH RUDDER TRIM INDICATING ZERO DEGREES. REMOVED AND REPLACED RUDDER TRIM ACTUATOR WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD. 2L72 4F RTA21EA 19950623006861995062300686 1995 6 23 COM60502 419950615A34256229336400 AHRS COMPUTER CNDAIRCL600 CL6002B19 EA E/E COMPT FAILED A COMAK NONE J WARNING INDICATION CRCRUISE 1 SO01926CA3451 7027 YAW DAMPENER FAILED IN FLIGHT WOULD NOT RESET. REMOVED AND REPLACED AHRS COMPUTER. OPS CHECK GOOD. 2L72 4F RTA21EA 19950623006871995062300687 1995 6 23 COM60503 419950620A34446222855011 RADIO ALTIMETER CNDAIRCL600 CL6002B19 EA NR 1 DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01933CA2889 7040 GROUND LIFT DUMP IS SLOW TO DEPLOY. REPLACED THE NR 1 RADIO ALTIMETER. 2L72 4F RTA21EA 19950623006881995062300688NM 1995 6 23 DL72E952707 119950613A5330 SKIN BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, CORROSION AT SKIN AFT OF STA 1010 O/B OF STR. 29L. REPAIR: REPAIRED PER ERA N0. 301979-14. 2L73 4F A3WE 19950623006891995062300689NM 1995 6 23 DL72E952708 119950613A5330 SKIN BOEING727 727247 138408FNM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, CORROSION AT SKIN O/B STR. 27R AFT OF STA 1010. REPAIR: REPAIRED PER ERA NO. 301979-14. 2L73 4F A3WE 19950623006901995062300690NM 1995 6 23 DL72E952709 119950613A5330 SKIN BOEING727 727247 138408FNM FS 1120 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK SKIN BULGE (VIEWED FROM OUTSIDE) AT STA. 1120 AND STR. 27R. REPAIR: REPAIRED PER SRM 53-30-3 FIG. 3. 2L73 4F A3WE 19950623006911995062300691NM 1995 6 23 DL72E952710 119950613A5320 FORMER BOEING727 727247 138408FNM FS 720 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK .50 INCH X .3750 INCH HOLE ON THE TOP OF FORMER 720C O/B STR 26R. REPAIR: REPAIRED PER SRM 53-10-4 FIG. 26. 2L73 4F A3WE 19950623006921995062300692NM 1995 6 23 DL72K952531 119950609A5754 SKIN BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11412DA 21232 FOUND DURING A-2 LETTER CHECK - .25 INCH CRACK COVESKIN ATTACH ANGLE NR 6 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0, PG 807. 2L73 4F A3WE 19950623006931995062300693NM 1995 6 23 DL72K952532 119950609A5754 SKIN BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11412DA 21232 FOUND DURING A-2 LETTER CHECK - .50 INCH CRACK COVESKIN ATTACH ANGLE UNDER I/B STOP PAD NR 7 SLAT. REPAIRED PER MM 57-54-0 OG 807.ER M/M 57-54-0 P807. 2L73 4F A3WE 19950623006941995062300694NM 1995 6 23 DL72K952533 119950609A5754 SKIN BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11412DA 21232 FOUND DURING A-2 LETTER CHECK- .50 INCH CRACK COVESKIN ATTACH ANGLE BELOW I/B STOP PAD NR 8 SLAT, 1 INCH CRACK COVESKIN ATTACH ANGLE BELOW O/B STOP PAD NR 8 SLAT. REPAIRED BOTH CRACKS PER MM 57-54-0, PG 807. 2L73 4F A3WE 19950623006951995062300695NM 1995 6 23 DL72K952534 119950609A5754 SKIN BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11412DA 21232 FOUND DURING A-2 LETTER CHECK - NR 2 L/E SLAT LOWER FORWARD SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0, PG 807A. 2L73 4F A3WE 19950623006961995062300696NM 1995 6 23 DL72K952535 119950609A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11412DA 21232 FOUND DURING A-2 LETTER CHECK - 3 EACH, .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 LT SIDE, 3 EA .25 INCH CRACKS JUST FORWARD OF LOWER CORNER OF PNL 9501 RT SIDE. BOTH ITEMS REPAIRED PER MM 54-30-0, PG 801. 2L73 4F A3WE 19950623006971995062300697NM 1995 6 23 DL72S952384 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE LWR HOLE ON THE I/B AND O/B SURFACE ON THE I/B LUG. REF MM REPAIR 57-43-00, PG 803. 2L73 4F A3WE 19950623006981995062300698NM 1995 6 23 DL72S952385 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION FITTING ALL FOUR ATTACH BORES CORRODED. REF REPAIR 57-43-00, PG 803. 2L73 4F A3WE 19950623006991995062300699NM 1995 6 23 DL72S952386 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION BEARING FITTING HAS CORROSION ON THE O/B SURFACE OF THE I/B LUG. REF MM57-43-00, PG 803. 2L73 4F A3WE 19950623007001995062300700NM 1995 6 23 DL72S952387 119950601A5743 TRUNNION BOEING727 727232 1384082NM LT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT MLG FWD TRUNNION BEARING FITTING IS PITTED AROUND THE UPPER HOLE ON THE I/B AND O/B SURFACE OF THE O/B LUG. REF MM 57-43-00, PG 803. 2L73 4F A3WE 19950623007011995062300701NM 1995 6 23 DL72S952389 119950601A5743 FITTING BOEING727 727232 1384082NM RT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 RIGHT MLG SIDE BRACE AFT BEARING FITTING IS PITTED. REF MM REPAIR 57-43-00, PG 803. 2L73 4F A3WE 19950623007021995062300702NM 1995 6 23 DL72S952391 119950601A5743 TRUNNION BOEING727 727232 1384082NM RT MLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 RIGHT MLG FWD TRUNNION ATTACH FITTING BUSHING IS PITTED. REPAIRED PER M/M 57-43-0. 2L73 4F A3WE 19950623007031995062300703NM 1995 6 23 DL72S952392 119950530A5743 TRUNNION BOEING727 727232 1384082NM RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 RIGHT GEAR - FWD TRUNNION ATTACH FITTING IS CORRODED ON BOTH LEGS. REMOVED SEALANT, NO CORROSION FOUND. INSTALL SHIMS PER M/M 57-43-0. 2L73 4F A3WE 19950623007041995062300704NM 1995 6 23 DL72S952393 119950530A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 NOSE L/G UPPER TRUNNION FITTING LOWER SURFACE IS CORRODED (CAP MATING SURFACE). REPAIR PER M/M 53-40-0. 2L73 4F A3WE 19950623007051995062300705NM 1995 6 23 DL72S952394 119950530A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 NLG RT UPPER TRUNNION BEARING FITTING IS PITTED ON THE I/D OF FITTING, FWD HOLE IN UPPER FITTING IS PITTED. REPAIR PER E.O. 4-57751-3. 2L73 4F A3WE 19950623007061995062300706NM 1995 6 23 DL72S952395 119950531A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 NOSE LG TRUNNION LT FWD AND AFT BOLT HOLES CORRODED. REPAIR PER M/M 53-40-0. 2L73 4F A3WE 19950623007071995062300707NM 1995 6 23 DL72S952396 119950530A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 NLG RT UPPER TRUNNION BEARING FITTING CORRODED IN LINE UP PINHOLE. REPAIR PER ERA 301860-14. 2L73 4F A3WE 19950623007081995062300708NM 1995 6 23 DL72S952397 119950531A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 LEFT NLG UPPER TRUNNION FITTING LOWER SURFACE IS CORRODED (CAP MATING SURFACE). REPAIR PER M/M 53-40-0. 2L73 4F A3WE 19950623007091995062300709NM 1995 6 23 DL72S952398 119950530A5343 TRUNNION BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 NLG LT/RT TRUNNION BEARING FITTINGS CORRODED IN THE BORES AND ON THE FACES. REPAIR PER M/M 53-40-0. 2L73 4F A3WE 19950623007101995062300710NM 1995 6 23 DL72S952506 119950515A7110 INLET BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 2 ENGINE INLET AFT LWR EDGE, BENT AND CRACKING IN SEVERAL PLACES. REPAIRED PER SRM 54-10-3. 2L73 4F A3WE 19950623007111995062300711NM 1995 6 23 DL72S952542 119950514A5311 FRAME BOEING727 727232 1384082NM FS1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AT HMV FOUND FORWARD LOWER FLANGE OF FRAME 1070 CORRODED LOC BETWEEN STR 30 AND 29R. INSTALLED NEW CLIP PER MM 53-11-0. 2L73 4F A3WE 19950623007121995062300712NM 1995 6 23 DL72S952660 119950602A5753 SKIN 6521634149K BOEING727 727232 1384082NM NR 2 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA BN574 22046 NR 2 AFT FLAP REPLACED TEMP. REPAIR 50 FROM INBD END LOWER SKIN PER SRM 57-50-4, FIG. 10 AND ERA 27109-14. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19950623007131995062300713NM 1995 6 23 DL72S952713 119950617A5343 FITTING BOEING727 727232 1384082NM NLG PITTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING SCHEDULED TRIPLE LANDING GEAR CHANGE FOUND LT AND RT NOSE GEAR TRUNNION CAPS AND BEARINGS WORN AND PITTED. REPAIRED PER M/M 53-40-0. 2L73 4F A3WE 19950623007141995062300714NM 1995 6 23 DL72S952718 119950619A2150 PACK BOEING727 727232 1384082NM LEFT OVERHEAT A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO11516DA 21432 ON SHORT FINAL AND LANDING, HAD LEFT PACK OVERHEAT WITH SOME BURNING ODOR IN CABIN. FOUND COOLING FAN C/B TRIPPED. RESET C/B OPERATION TEST, NO TROUBLE FOUND, RETURNED TO SERVICE. 2L73 4F A3WE 19950623007151995062300715NM 1995 6 23 DL72W952321 119950507A5753 SKIN 6521630187A BOEING727 727247 138408FNM LT TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 575 21327 THE LE WAS WORN 51 INCHES FROM THE I/B END. AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 57-50-4 FIG 1 DURING SHOP INSPECTION OF NR 2 FORE FLAP. 2L73 4F A3WE 19950623007161995062300716NM 1995 6 23 DL72W952511 119950608A5754 ANGLE BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112811W 20649 NR 2 SLAT I/B STOP PAD LWR ATTACH ANGLE IS CRACKED. FOUND AT B-2 LTR CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950623007171995062300717NM 1995 6 23 DL72W952512 119950608A5754 WEB BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112811W 20649 NR 6 SLAT O/B ACT ROD END WEB CRACKED AFT SIDE. FOUND AT B-2 LTR CK. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950623007181995062300718NM 1995 6 23 DL72W952513 119950608A5753 SKIN BOEING727 727247 138408FNM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112811W 20649 .3750 INCH CRACK, NR 3 AFT FLAP UPPER SURFACE AFT OF 2ND FROM O/B LOWER ROLLER TRACK CUTOUT. FOUND AT B-2 LTR CK. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950623007191995062300719NM 1995 6 23 DL757952527 119950607A5753 SKIN BOEING757 757232 1384965NM RT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11617DL 22907 FOUND DURING LETTER CHECK, HOLE IN LOWER SURFACE OF RIGHT I/B AFT FLAP. REPAIRED PER SRM 57-53-01. 2L72 4F RTA2NM 19950623007201995062300720NM 1995 6 23 DL757952528 119950607A5753 SKIN BOEING757 757232 1384965NM RT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11617DL 22907 FOUND DURING LETTER CHECK, TWO HOLES IN THE UPPER SURFACE OF THE RT I/B AFT FLAP AT O/B END. REPAIRED PER SRM 57-53-01. 2L72 4F RTA2NM 19950623007211995062300721NM 1995 6 23 DL757952530 119950605A5414 SKIN BOEING757 757232 1384965NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE NR 1 PYLON O/B SKIN WAS FOUND TO BE CRACKED ON TOP AFT CORNER OF CUTOUT FOR PANEL 433 AT INSIDE OF STRUT BOX. THE DAMAGE WAS CUT OUT, HFEC OF CUTOUT WAS OK. DOUBLER WAS DRILLED AND REAMED TO FINAL SIZE AND INSTALLED PER SRM 54-51-01. 2L72 4F RTA2NM 19950623007221995062300722NM 1995 6 23 DL757952547 119950609A5753 SKIN BOEING757 757232 1384965NM LT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11673DL 25978 FOUND DURING LETTER CHECK, HOLE IN UNDERSIDE OF NR 2 FOREFLAP T/E REPAIRED PER SRM 57-53-01. 2L72 4F RTA2NM 19950623007231995062300723NM 1995 6 23 DL757952726 119950618A7111 COWL BOEING757 757232 1384965NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11633DL 23614 000156 GROUND DAMAGE TO NOSE LIP AT THE 11 O'CLOCK POSITION. REPAIRED PER SRM 54-11-01, FOR NR 2 INTAKE COWL AT SHOP INSPECTION. 2L72 4F RTA2NM 19950623007241995062300724NM 1995 6 23 DL757952727 119950619A5753 SKIN BOEING757 757232 1384965NM LT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, 3 EACH PUNCTURES IN O/B AFT FLAP UPPER SURFACE. REPAIRED PUNCTURE PER SRM 57-53-01, PAINTED REPAIR. 2L72 4F RTA2NM 19950623007251995062300725NM 1995 6 23 DL757952728 119950619A5755 SKIN BOEING757 757232 1384965NM LT WING PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, PUNCTURE IN NR 2 SPOILER I/B AFT UPPER SURFACE. REPAIRED PER SRM 57-70-01, PAINTED REPAIR. 2L72 4F RTA2NM 19950623007261995062300726NM 1995 6 23 DL757952730 119950619A5755 SKIN BOEING757 757232 1384965NM LT WING PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, PUNCTURE IN NR 4 SPOILER O/B UPPER MID AREA REPAIRED. PER SRM 57-70-01. REPAINTED REPAIR. 2L72 4F RTA2NM 19950623007271995062300727NM 1995 6 23 DL757952731 119950619A5522 SKIN BOEING757 757232 1384965NM ELEVATOR PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, LEFT ELEVATOR HAS A PUNCTURE ON THE TOPSIDE. REPAIRED DAMAGED AREA PER SRM 55-20-01. OK TO PAINT PAINTED AREA. 2L72 4F RTA2NM 19950623007281995062300728NM 1995 6 23 DL757952732 119950619A5753 SKIN BOEING757 757232 1384965NM LT TE FLAP PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, PUNCTURE IN I/B AFT FLAP UPPER SURFACE. REPAIRED PER SRM 57-53-01 PAINTED REPAIR. 2L72 4F RTA2NM 19950623007291995062300729NM 1995 6 23 DL757952733 119950619A5755 SKIN BOEING757 757232 1384965NM NR 8 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, NR 8 SPOILER HAS SEVERAL DELAMINATED AREAS. INSTALLED PERMANENT REPAIR AS PER SRM 57-70-01. OK TO PAINT PAINTED REPAIRS. 2L72 4F RTA2NM 19950623007301995062300730NM 1995 6 23 DL757952734 119950619A5755 SKIN BOEING757 757232 1384965NM NR 9 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHK, NR 9 SPOILER HAS DELAMINATED AREA. BEGAN PERMANENT REPAIR AS PER SRM 57-70-01. COMPLETED REPAIR AND PAINTED. 2L72 4F RTA2NM 19950623007311995062300731NM 1995 6 23 DL757952735 119950619A7111 COWL BOEING757 757232 1384965NM NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 000156 FOUND DURING LETTER CHECK, 2 HOLES IN NOSE COWL AT 1 AND 2 O'CLOCK POSITION. REPAIRED PER SRM 51-70-17. REPAINTED AREA. 2L72 4F RTA2NM 19950623007321995062300732NM 1995 6 23 DL767952519 119950608A5754114T31001B TE WEDGE BOEING767 767232 1385132NM NR 6 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 TRAILING EDGE WEDGE HAD HAIL DAMAGE. REPLACED WEDGE PER CMM 57-43-37. REPAIRS ACCOMPLISHED DURING SHOP VISIT FOR NR 6 L/E SLAT PANEL. 2L72 4F RTA1NM 19950623007331995062300733NM 1995 6 23 DL76L952721 119950604A5313 STRINGER BOEING767 767332 1382001NM FS 1461 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11174DN 24802 AT L/O STRINGER 39R DAMAGED AT STA 1461. REMOVED AND REPLACED DAMAGED SECTION OF STRINGER AND SPLICE IN NEW SECTION AT STA 1450 TO STA 1562. DAMAGE WAS FROM TAIL STRIKE ON LANDING. 2L72 4F RTA1NM 19950623007341995062300734NM 1995 6 23 DL76L952722 119950604A5313 STRINGER BOEING767 767332 1382001NM FS 1500 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11174DN 24802 L/O CHK STRINGER 38R DAMAGED AT STA 1500. REPLACED DAMAGED STRINGER AND SPLICED AT STA 1472 AND STA 1547. 2L72 4F RTA1NM 19950623007351995062300735NM 1995 6 23 DL76L952723 119950619A5313 STRINGER BOEING767 767332 1382001NM FS 1540 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11174DN 24802 L/O CHK STRINGER 39L HAS .75 INCH CRACK AT STA 1540, FABRICATED REPAIR PARTS PER 53-00-03. OK TO INSTALL, INSTALLED SPLICE PER SRM. DAMAGE WAS FROM TAIL STRIKE ON LANDING. 2L72 4F RTA1NM 19950623007361995062300736NM 1995 6 23 DL76L952725 119950604A5313 STRINGER BOEING767 767332 1382001NM FS 1461 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11174DN 24802 STRINGER 39L DAMAGED AT STA 1461. REMOVED DAMAGED STRINGER 39L. SPLICED STRINGER STA 1470, 1509, AND 1530 PER SRM 53-00-03. INSTALLED SPLICED STRINGER AT STA 1450 TO STA 1562 PER SRM 53-00-03. DAMAGE WAS FROM TAIL STRIKE ON LANDING. 2L72 4F RTA1NM 19950623007371995062300737WP 1995 6 23 DLL10952299 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FASTENER HOLES CORRODED IN LT MLG RETRACT ACTUATOR FITTING. HOLES NR 7, 8, 9, 11, 12, 13, 16, FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 808. 2L73 4F A23WE 19950623007381995062300738WP 1995 6 23 DLL10952300 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 HOLES CORRODED IN LT MLG FITTING FOR RETRACT ACTUATOR. HOLES NR 9, 14, 15, 16, FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 804. 2L73 4F A23WE 19950623007391995062300739WP 1995 6 23 DLL10952311 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 579 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 TEAR STRAP - DISBONDED IN C-1 BB AT FS 579 FROM STA 34 TO STA 37, FOUND AT HMV. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007401995062300740WP 1995 6 23 DLL10952335 119950527A5320 THRESHOLD LKHEED1011 10113851 5265010WP R 4 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THRESHOLD CORRODED - R-1 DOOR UPPER SURFACE, FWD END, FOUND DURING HMV. REPAIRED PER SRM 53-15-00 PG 816-820. 2L73 4F A23WE 19950623007411995062300741WP 1995 6 23 DLL10952336 119950531A5320 SKIN CLIPS LKHEED1011 10113851 5265010WP FS 1463 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FS 1463 SKIN CLIPS BETWEEN STR 33 AND 36 ARE CORRODED. REPAIRED PER SRM 53-12-00, FIG. 817. 2L73 4F A23WE 19950623007421995062300742WP 1995 6 23 DLL10952337 119950526A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, ANGLE CORRODED IN BETWEEN STR 28-29, FS 1565 C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 804. 2L73 4F A23WE 19950623007431995062300743WP 1995 6 23 DLL10952338 119950525A5330 TEAR STRAPS LKHEED1011 10113851 5265010WP FS 559 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - TEAR STRAPS DISBONDED FROM STR 34 TO STR 37. CORR: REPAIRED PER SRM 53-31-00, PG. 830. 2L73 4F A23WE 19950623007441995062300744WP 1995 6 23 DLL10952339 119950525A5330 TEAR STRAPS LKHEED1011 10113851 5265010WP FS 559 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - TEAR STRAPS DISBONDED BETWEEN STR 40 AND 41, STA 559, ALSO BETWEEN STR 38-39 AND STR 39-40. REPAIRED PER SRM 53-31-00, PG 830. 2L73 4F A23WE 19950623007451995062300745WP 1995 6 23 DLL10952340 119950526A5320 SKIN CLIP LKHEED1011 10113851 5265010WP FS 1523 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - SKIN CLIP CORRODED FS 1523 AFT SIDE IN BETWEEN STR 28-27 C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 804. 2L73 4F A23WE 19950623007461995062300746WP 1995 6 23 DLL10952341 119950526A5320 SKIN CLIP LKHEED1011 10113851 5265010WP FS 1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - SKIN CLIP CORRODED IN BETWEEN STR 33-34 FS 1565 AFT C-2 B/B. REPAIRED PER SRM 53-12-00, FIG 817. 2L73 4F A23WE 19950623007471995062300747WP 1995 6 23 DLL10952342 119950526A5320 SKIN CLIP LKHEED1011 10113851 5265010WP FS 1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - SKIN CLIP CORRODED IN BETWEEN STR 33-32 FS 1565 AFT SIDE C-2. REPAIRED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950623007481995062300748WP 1995 6 23 DLL10952406 119950601A5330 SKIN STRAPS LKHEED1011 10113851 5265010WP CARGO COMPT UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, C-3 CARGO FUSELAGE SKIN, FAILSAFE STRAPS UNBONDED STA 1770 BETWEEN STR 30 AND 31 AND 37 AND 38. REPAIRED PER SRM 53-31-00, PG 830. 2L73 4F A23WE 19950623007491995062300749WP 1995 6 23 DLL10952442 119950528A5330 SKIN LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FUSELAGE SKIN HAS .3750 INCH CRACK AT RT AFT PNEUMATIC GROUND CONNECTOR FLANGE CRACK LOC. AT FWD HINGE CORNER CUT-OUT. FOUND AT HMV, REPAIRED PER SRM 53-31-00, PG 923-922. 2L73 4F A23WE 19950623007501995062300750WP 1995 6 23 DLL10952443 119950528A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 DEEP CORROSION ON AREA EXPOSED BY RT MLG FITTING. FOUND IN HMV. REPAIRED PER SRM 57-14-00, PG 811. 2L73 4F A23WE 19950623007511995062300751WP 1995 6 23 DLL10952444 119950525A5743 FITTING BUSHING LKHEED1011 10113851 5265010WP RT MLG MIGRATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 BUSHING MIGRATED IN RT MLG FITTING FWD TRUNNION, AFT LUG BUSHING. FOUND IN HMV. REPAIRED PER SRM 57-14-00, FIG 802, PG 803. 2L73 4F A23WE 19950623007521995062300752WP 1995 6 23 DLL10952485 119950602A5311 FRAME LKHEED1011 10113851 5265010WP FS 1763 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STA 1763 FRAME CAP IN C-3 CUT AT APPROX LBL 9 1/2 AND RBL 16 FOR MTC. FOUND IN HMV. REPAIRED PER SRM 53-12-00, FIG 817. 2L73 4F A23WE 19950623007531995062300753WP 1995 6 23 DLL10952486 119950604A5320 STRINGER SPLICE LKHEED1011 10113851 5265010WP FS 826-869 IMPROPER A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11721DA 193C1139 STR 33 HAS IMPROPER SPLICES AT STA 826 TO 869. FOUND IN HMV. REPLACED SPLICES PER SRM 53-13-00, FIG 804. 2L73 4F A23WE 19950623007541995062300754WP 1995 6 23 DLL10952487 119950605A5313 STRINGER LKHEED1011 10113851 5265010WP FS 789 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 34 HAS CRACK JUST BELOW FORMER STA. 789. FOUND HMV. REPAIRED PER SRM 53-13-00. SPLICED IN NEW STRINGER SECTION. 2L73 4F A23WE 19950623007551995062300755WP 1995 6 23 DLL10952497 119950527A5320 THRESHOLD LKHEED1011 10113851 5265010WP L2 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THRESHOLD CORRODED L-2 DOOR, TOP SURFACE AT AFT END. FOUND IN HMV. REPAIRED PER SRM 51-1-05 AND LAC DRAWING 1506385 AND DRAWING 1506415. 2L73 4F A23WE 19950623007561995062300756WP 1995 6 23 DLL10952498 119950526A5320 FORMER LKHEED1011 10113851 5265010WP FS 769 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FORMER CRACKED AT STA 769 STRINGER 40. FOUND IN HMV. REPAIRED PER SRM 53-12-00, PG 823-824. 2L73 4F A23WE 19950623007571995062300757WP 1995 6 23 DLL10952515 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 933 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND FUSELAGE SKIN FAIL SAFE STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 40 AND 41. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007581995062300758WP 1995 6 23 DLL10952516 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 933 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 40-41. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007591995062300759WP 1995 6 23 DLL10952517 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 933 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND FUSELAGE SKIN FAILSAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 43-44. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007601995062300760WP 1995 6 23 DLL10952518 119950530A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 933 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND FUSELAGE SKIN FAIL SAFE TEAR STRAP DISBONDED AT FS 933 BETWEEN STRINGERS 44-45. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007611995062300761WP 1995 6 23 DLL10952543 119950526A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1695 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - TEAR STRAP DISBONDED FS 1695 BETWEEN STR 29 AND 3. CORR: REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950623007621995062300762WP 1995 6 23 DLL10952544 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV - LT MLG FITTING FLANGE FOR RETRACT ACTUATOR LOWER SURFACE IS CORRODED. REPAIRED PER SRM 57-14-00, FIG 804. 2L73 4F A23WE 19950623007631995062300763WP 1995 6 23 DLL10952545 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 LEFT MLG FITTING I/B SURFACE CORRODED. FOUND AT HMV, REPAIRED PER SRM 57-14-00, FIG 804. 2L73 4F A23WE 19950623007641995062300764WP 1995 6 23 DLL10952546 119950526A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, LT MLG FITTING CORRODED ON UPPER WING LOWER SURFACE. CORR: REPAIRED PER SRM 57-14-00, FIG 804. 2L73 4F A23WE 19950623007651995062300765WP 1995 6 23 DLL10952552 119950530A5330 TEARSTRAP LKHEED1011 10113851 5265010WP FS 779 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, TEAR STRAP DISBONDED FS 779 STR 40-41. STRAP HAS CORROSION UNDERNEATH. REPAIRED PER SRM 53-31-00, FIG 804. 2L73 4F A23WE 19950623007661995062300766WP 1995 6 23 DLL10952554 119950602A5720 WEB LKHEED1011 10113851 5265010WP NR 5 TORQUE BOX GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 NR 5 TORQUE BOX, FWD EDGE OF WEB PANEL GOUGED INSIDE AFT END BELOW AND AFT OF LINKAGE. FOUND DURING HMV. REPAIRED PER SRM 51-50-04, FIG 2 SHT 2. INSTALLED DOUBLER. REF NR 539. 2L73 4F A23WE 19950623007671995062300767WP 1995 6 23 DLL10952719 119950526A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FLOOR SUPPORT LOWER SECTION CORRODED ABOVE STR 33 FS 1545 C-2 B/B AT HMV. REPAIRED PER SRM 53-23-00, FIG 802. 2L73 4F A23WE 19950623007681995062300768WP 1995 6 23 DLL10952720 119950610A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORRODED FLOOR BEAM UNDER T-CAP 2 LT OF B/L 0.0 C-2 B/B STA 1545. REPAIRED PER SRM 53-23-00, FIG 802. 2L73 4F A23WE 19950623007691995062300769WP 1995 6 23 DLL13952537 119950510A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FITTING CORRODED, AT I/B SIDE RMLG HOLE 17-20. REAMED HOLES TO .625 INCH, CORROSION REMOVED WITHIN LIMITS. HFEC OF FACE AND HOLES, REOPENED PER PS 900-4-5, CAD PLATED PER PS 900-3-9 NR 4. TURNED BUSHING TO SIZE AND TREATED, INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED. PRIMED AND PAINTED. PER SRM 57-14-00. 2L73 4F A23WE 19950623007701995062300770WP 1995 6 23 DLL13952538 119950510A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FITTING CORRODED, I/B RMLG ACT FITTING FLANGE. MACHINED TO .030 INCH FROM VERTICAL FACE IM\N LOWER AREA. LOCAL BLENDED SMALL AREA. PER SRM 57-14-00 PG 811. CORROSION REMOVED, HFEC OF FITTING, ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-3-9 NR 4. OXIDE BLASTED, PRIMED, AND PAINTED. MFG AND TREATED SHIM. INSTALLED SHIM PER SRM 57-14-00. 2L73 4F A23WE 19950623007711995062300771WP 1995 6 23 DLL13952539 119950510A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND HOLE CORRODED. NR 4 HOLE RMLG UPPER FLANGE FOR ACT ATTACHED FITTING. REAMED HOLE TO .718 INCH, CORROSION REMOVED. SPOT FACED .750 INCH DIA AND .025 INCH. CORROSION REMOVED. HFEC FOUND OK. ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER 900-3-9 NR 4, WITHIN SRM 57-14-00 LIMITS. TURNED BUSHINGS TO SIZE TREATED. INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED, PRIME, AND PAINTED. MFG AND TREATED WASHER, INSTALLED WASHER. 2L73 4F A23WE 19950623007721995062300772WP 1995 6 23 DLL13952540 119950511A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV FOUND HOLE CORRODED, 1, 2, 3, 5, 6, RMLG ACT FITTING. REAMED TO .688 INCH, CORROSION REMOVED. SPOT FACED NR 3 HOLE 1.750 INCH DIA AND .010 INCH DEEP CORROSION REMOVED. HFIC HOLES AND FACE. ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-3-9 NR 5. HOLES AND SPOT FACE WITHIN SRM 57-14-00 LIMITS. TURNED BUSHING TO SIZE AND TREATED INSTALLED BUSHING AND REAMED TO SIZE OXIDE BLASTED, PRIMED, AND PAINTED. MFG, TREATED, INSTALLED WASHER. 2L73 4F A23WE 19950623007731995062300773WP 1995 6 23 DLL13952541 119950511A5743 HOLES LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND HOLES CORRODED, RMLG 11-16 ACT ATTACH FITTING. REAMED HOLES TO .562 INCH, CORROSION REMOVED WITHIN LIMITS PER SRM 57-14-00. HFEC HOLED AND FACE, ROTO PEENED PER PS 900-4 NR 5. CAD PLATED PER PS 900-9 NR 4. TURNED BUSHINGS TO SIZE AND TREATED. INSTALLED BUSHING AND REAMED TO SIZE. OXIDE BLASTED, PRIMED, AND PAINTED. 2L73 4F A23WE 19950623007741995062300774WP 1995 6 23 DLL13952714 119950510A5330 TEAR STRAP LKHEED1011 10113851 5265010WP FS 1433 UNBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND TEAR STRAP DISBONDED, C2 B/B FS 1413 BETWEEN STRINGER 30-31. REPAIRED PER SRM 53-31-00 PG 801. 2L73 4F A23WE 19950623007751995062300775WP 1995 6 23 DLL13952715 119950510A5320 T-CAP LKHEED1011 10113851 5265010WP FS 1525 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND CAP CORRODED, C2 FLOOR T-CAP STR 1525 RBL 10 LBL 25. DRILLED AND INSTALLLED NEW T-CAP PER SRM 53-20-00. 2L73 4F A23WE 19950623007761995062300776WP 1995 6 23 DLL13952717 119950509A5330 SKIN LKHEED1011 10113851 5265010WP FS 1645-1665 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND SKIN CORROSION, STA 1645-1665, AND AROUND TEAR STRAPS. ACCOMPLISHED REPAIRS PER DL ERA 270891-14. 2L73 4F A23WE 19950623007771995062300777WP 1995 6 23 DLL14952555 119950323A5755 SKIN 1529102177 LKHEED1011 1011385115 5265015WP LT WING SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO111739D HO268 193C1237 DURING SHOP INSPECTION SPOILER WAS FOUND TO BE DELAMINATED. REPAIRED AS PER SRM 57-52-00. 2L73 4F A23WE 19950623007781995062300778NM 1995 6 23 DLM88952399 119950601A5320 RIB DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11904DE 53409 FOUND ON C2 LTR CK - CRACK LOCATED ON KEEL BEAM RIB AFT END REPAIR - REPAIRED PER SRM 53-05, FIG 101. 2L72 4F RTA6WE 19950623007791995062300779NM 1995 6 23 DLM88952536 119950609A5314 CLIP DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11982DL 53273 FOUND DURING D-2 LETTER CHECK - KEEL BEAM AFT CROSSOVER RIB ATTACH CLIP CRACKED. REPAIRED PER SRM 53-05, FIG 101. 2L72 4F RTA6WE 19950623007801995062300780NM 1995 6 23 DLM88952705 119950620A5311 FRAME DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11931DL 49718 FOUND DURING A-1 LETTER CHECK - RT FWD WHEELWELL FRAME CRACKED O/B SIDE. REPAIRED PER SRM 53-05, FIG 78A. 2L72 4F RTA6WE 19950623007811995062300781NM 1995 6 23 DLM88952724 119950619A2150 AIR COND DOUG MD88 MD88 3023688NM FLIGHT DECK ODOR A DALAK NONE BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION APAPPROACH 1 SO11906DL 49537 ON FINAL APPROACH TO ATL, HAD AFT LAV SMOKE DETECTORS ACTIVATE. NOTICED SOME SMOKE ODOR IN FLT DECK. MTC CHECKED PACK OPERATION AND APU INTAKE FOR CONTAMINATION, COULD NOT DUPLICATE, RETURNED TO SERVICE. 2L72 4F RTA6WE 19950623007821995062300782WP 1995 6 23 MWEA95218 119950621A25603952273501 GIRT BAR LATCH DOUG DC9 DC914 3022034WP GALLEY DOOR LACK OF LUBE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31600ME 45725 CREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LATCH IS VERY HARD TO LATCH. MAINTENANCE CLEANED AND LUBRICATED GIRT BAR LATCHES. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950623007831995062300783NM 1995 6 23 P5CA9500062 119950620A495069B400331 DUCT BOEING747 747121 1384871NM APU BLOWN A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23832FT 20347 PRIOR TO TAKEOFF, APPLIED POWER AND WHEELWELL FIRE WARNING LIGHT CAME ON. LIGHT WENT OUT WHEN RETURNED TO IDLE, RETURNED TO BLOCKS. ON LEAK CHECK BY MAINTENANCE, APU SUPPLY DUCT BURST. INSTALLED BLOCKING PLATE AND PLACARDED APU INOPERATIVE. 2L74 4F A20WE 19950623007841995062300784NM 1995 6 23 P5CA9500063 119950424A321165B21500524 TRUNNION BOEING747 747121 1384871NM RT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 11014 19648 DURING INSPECTION PER AD 90-06-18 R1, FOUND CRACK INDICATION ON RIGHT WING LANDING GEAR TRUNNION JOURNAL OUTBOARD BOLT HOLE. REPAIRED BY REAMING HOLE PER BOEING M/M 32-11-47 AND INSTALLING BUSHING PER BOEING MM 32-11-49. 2L74 4F A20WE 19950623007851995062300785NM 1995 6 23 P5CA9500064 119950517A5313 STRINGER BOEING747 747121 1384871NM BS 1740-1750 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DURING BASE LINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STRINGER 41 BS 1740 TO 1750. 2L74 4F A20WE 19950623007861995062300786NM 1995 6 23 P5CA9500065 119950517A5753 TE SKIN BOEING747 747121 1384871NM AFT TE FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND LEFT OUTBOARD TRAILING EDGE AFT FLAP OUTBOARD TRAILING EDGE DAMAGED. REPAIRED ACCORDING TO BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007871995062300787NM 1995 6 23 P5CA9500066 119950521A5754 SKIN REPAIR BOEING747 747121 1384871NM LT TE MID FLAP PEELING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING INBOARD MID FLAP LOWER SKIN HAS FIBERGLASS REPAIR PEELING OFF. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007881995062300788NM 1995 6 23 P5CA9500067 119950521A5744 AFT FLAP BOEING747 747121 1384871NM LT TE FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR REQUIRING UPGRADE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007891995062300789NM 1995 6 23 P5CA9500068 119950528A5200 DOOR PANEL BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOWER) HAS DELAMINATION. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007901995062300790NM 1995 6 23 P5CA9500069 119950527A5744 MID FLAP BOEING747 747121 1384871NM LT TE MID FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT INBOARD TRAILING EDGE MID FLAP HAS 2 AREAS DAMAGED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007911995062300791NM 1995 6 23 P5CA9500070 119950527A5200 DOOR PANEL BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMAINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007921995062300792NM 1995 6 23 P5CA9500071 119950527A5200 DOOR PANEL BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 3 HEAT EXCHANGER EXIT DOOR PANEL (AFT OF LOUVERS) DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007931995062300793NM 1995 6 23 P5CA9500072 119950527A5320 TENSION TIES BOEING747 747121 1384871NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 UPPER DECK TENSION TIE AT STA. 780, 800, 820, 860, 880, 900, 920, 940 LH AND RH, FOUND CRACKS. REPAIRED PER BOEING SERVICE BULLETIN 53-2371. 2L74 4F A20WE 19950623007941995062300794NM 1995 6 23 P5CA9500073 119950527A5320 TENSION TIE BOEING747 747121 1384871NM FS 760 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 UPPER DECK TENSION TIE AT STA. 760 LEFT AND RIGHT, FOUND CRACKED. MODIFIED PER BOEING SERVICE BULLETIN 53-2088. 2L74 4F A20WE 19950623007951995062300795NM 1995 6 23 P5CA9500074 119950621A2612 FIRE WARN BOEING747 747121 1384871NM WHEEL WELL MALFUNCTIONED A P5CAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP23832FT 20347 ON CLIMB OUT, WHEELWELL FIRE LIGHT CAME ON, RETURNED TO SYD. TROUBLESHOT THE FIRE WARNING SYSTEM, UNABLE TO LOCATE POSITIVE CAUSE. NO AIR LEAKS PLACARDED, FIRE WARNING SYSTEM PER MEL 26-06. 2L74 4F A20WE 19950623007961995062300796NM 1995 6 23 P5CA9500075 119950521A5753 SKIN BOEING747 747121 1384871NM LT ET FLAP DELAMINATING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING OUTBOARD FLAP AFT FLAP HAS LARGE REPAIR DELAMINATING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623007971995062300797NM 1995 6 23 P5CA9500076 119950527A5730 SKIN BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 CORROSION ON 3 POINTS ON LEFT WING UPPER SKIN BETWEEN MID AND AFT SPARS BETWEEN WBL. 586 AND 617 (LEVEL 1). CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01. 2L74 4F A20WE 19950623007981995062300798NM 1995 6 23 P5CA9500077 119950527A5730 SKIN BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 CORROSION ON LEFT WING UPPER SKIN BETWEEN MID AND REAR SPAR AT WBL 724. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA IS WITHIN LIMITS PER BOEING SRM 57-20-01. 2L74 4F A20WE 19950623007991995062300799NM 1995 6 23 P5CA9500078 119950521A5720 FASTENERS BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AROUND FASTENERS AT WBL 862 AND 1056 AT THE MID SPAR. CLEANED CORROSION AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623008001995062300800NM 1995 6 23 P5CA9500079 119950527A5730 SKIN BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 CORROSION 3 POINTS ON LEFT WING UPPER SKIN BETWEEN WBL 832 AND 907 AT THE MID SPAR. CLEANED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 57-20-01. 2L74 4F A20WE 19950623008011995062300801NM 1995 6 23 P5CA9500080 119950527A5414 PANEL BOEING747 747121 1384871NM NR 2 PYLON DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 DAMAGE (DENT) AND RIVET IS PENETRATING SKIN ON RIGHT FAIRING PYLON TO WING. DENT HAS BEEN REMOVED AND RIVET REPLACED AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623008021995062300802NM 1995 6 23 P5CA9500081 119950527A5414 SKIN BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON NR 2 PYLON EXTERNAL SKIN ON RIGHT FORWARD LOWER SPAR EDGE. NEW STRAP FABRICATED PER BOEING SRM 54-10-02, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623008031995062300803NM 1995 6 23 P5CA9500082 119950527A5730 SKIN BOEING747 747121 1384871NM WS 586 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN MID AND REAR SPAR AT THE WS. 586 AREA. REMOVED CORROSION PER BOEING SRM 51-10-01, AREA WITHIN LIMITS PER BOEING SRM 57-20-01. 2L74 4F A20WE 19950623008041995062300804NM 1995 6 23 P5CA9500083 119950527A5730 SKIN BOEING747 747121 1384871NM WS 528-724 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 528 AND 724 AT THE REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950623008051995062300805NM 1995 6 23 P5CA9500084 119950527A5730 SKIN BOEING747 747121 1384871NM WS 782-1084 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 FOUND CORROSION ON RIGHT WING SKIN AND AROUND FASTENERS BETWEEN WS. 782 TO 1084 AT REAR SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950623008061995062300806NM 1995 6 23 P5CA9500085 119950527A5730 SKIN BOEING747 747121 1384871NM WS 323/586 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 RIGHT WING UPPER SKIN CORROSION ON SKIN AND AROUND FASTENERS BETWEEN WS 323 AND WS 586 AT THE MID SPAR. REMOVED CORROSION PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950623008071995062300807NM 1995 6 23 P5CA9500086 119950527A5730 SKIN BOEING747 747121 1384871NM WS 724-972 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WS 724 AND WS 972 AT THE MID SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND FOUND WITHIN LIMITS PER SRM 53-10-01. 2L74 4F A20WE 19950623008081995062300808NM 1995 6 23 P5CA9500087 119950521A5730 SKIN BOEING747 747121 1384871NM WS 724-972 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 FOUND CORROSION ON RIGHT WING UPPER SKIN AND AROUND FASTENERS BETWEEN WBS 724 AND WS 972 AT THE FRONT SPAR AREA. CORROSION REMOVED PER BOEING SRM 51-10-01 AND FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950623008091995062300809NM 1995 6 23 P5CA9500088 119950521A3230 ARM BOEING747 747121 1384871NM NLG CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NOSE LANDING GEAR ARM CONNECTED TO LANDING GEAR ACTUATOR IS CORRODED ON FORWARD SIDE. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623008101995062300810NM 1995 6 23 P5CA9500089 119950527A5320 ANGLE BOEING747 747121 1384871NM FS 400 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NOSE LANDING GEAR WHEELWELL BS 400 LEFT SIDE ANGLE BRACKET IS BROKEN. MANUFACTURED NEW ANGLE BRACKET FROM 7075-T6 0.50 INCH MATERIAL PER BOEING SRM 53-10-20 AND INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950623008111995062300811NM 1995 6 23 P5CA9500090 119950521A4980 EXHAUST BOEING747 747121 1384871NM APU CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 APU EXHAUST AFT END AT 12 O'CLOCK IS CRACKED. TRIMMED AND SMOOTHED THE CRACK PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623008121995062300812NM 1995 6 23 P5CA9500091 119950527A5400 STRAP BOEING747 747121 1384871NM NR 2 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 PYLON RIGHT SIDE FORWARD LOWER STRAP IS DAMAGED AT NS. 128. NEW STRAP FABRICATED AS PER SRM 54-10-02 AND INSTALLED AS PER SRM 51-30-02. 2L74 4F A20WE 19950623008131995062300813NM 1995 6 23 P5CA9500092 119950527A5400 STRAP BOEING747 747121 1384871NM NR 2 PYLON BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 PYLON STRAP VENT ON LOWER SPAR AT NS. 180. NEW STRAP FABRICATED PER SRM 54-30-03, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950623008141995062300814NM 1995 6 23 P5CA9500093 119950527A5414 PANEL BOEING747 747121 1384871NM NR 2 PYLON CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON SCREW HEADS AND RIVETS NR 2 PYLON FAIRING TO WING LEFT SIDE, ALSO LOOSE RIVETS. REPLACED LOOSE RIVETS PER BOEING SRM 51-30-02 AND CLEANED SURFACE CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950623008151995062300815NM 1995 6 23 P5CA9500094 119950521A5347 SEAT TRACK BOEING747 747121 1384871NM FS 530-540 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 UPPER DECK SEAT TRACK LBL 6O BETWEEN STA. 530 TO 540 CORRODED. REMOVED CORROSION PER SRM 51-10-01 WITHIN LIMITS. 2L74 4F A20WE 19950623008161995062300816NM 1995 6 23 P5CA9500095 119950527A5400 FAIRING BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 PYLON HAS CRACK WITH STOP HOLE ON LOWER SAIL BOAT AT NS. 286. DAMAGED SECTION REMOVED FROM SAIL BOAT, FOUND WITHIN LIMITS PER SRM 54-10-01. 2L74 4F A20WE 19950623008171995062300817NM 1995 6 23 P5CA9500096 119950527A5400 BLOW OUT PANEL BOEING747 747121 1384871NM NR 2 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 PYLON DAMAGE ON CUT-OUT ON BLOW OUT PANEL AT NS. 180. INSTALLED DOUBLER PER BOEING SRM 54-10-02 AND 51-30-02. 2L74 4F A20WE 19950623008181995062300818NM 1995 6 23 P5CA9500097 119950527A5400 SPAR BOEING747 747121 1384871NM NS 180-236 CHAFING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CHAFING ON BOTH SIDES LOWER SPAR FROM INSIDE NS. 180 TO NS. 236. FABRICATED NE STRAPS AS PER BOEING SRM 54-10-02, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950623008191995062300819NM 1995 6 23 P5CA9500098 119950527A5712 RIB BOEING747 747121 1384871NM WS 790 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE FLAP NR 18 CAVITY WS 790 FORGED RIB LEFT UPPER STIFFENER AND CHORD ARE CRACKED. REPAIRED PER BOEING SERVICE BULLETIN 57-2116 AND BOEING SRM 51-30-02. 2L74 4F A20WE 19950623008201995062300820NM 1995 6 23 P5CA9500099 119950521A5720 COVER BOEING747 747121 1384871NM WS 1120 DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE WS. 1120 FIBER COVER ABOVE PYLON NR 4 COMING OFF. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950623008211995062300821NM 1995 6 23 P5CA9500100 119950528A5712 RIB BOEING747 747121 1384871NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE CAVITY F.S.S. 1200 ON FORGED RIB AFT END OF UPPER CHORD CRACKED. REPAIRED AS PER BOEING SERVICE BULLETIN 57-2116. 2L74 4F A20WE 19950623008221995062300822NM 1995 6 23 SWAA950461 119950619A291065C268101022 HYD LINE BOEING737 7373T5 NM RT MLG RUPTURED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07692SW 23062 DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO ONT AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND HYDRAULIC LINE TO RIGHT MAIN GEAR UPLOCK ACTUATOR RUPTURED. REPLACED LINE AND SERVICED SYSTEM PER BOEING M/M. 2L72 4F RTA16WE 19950623008231995062300823NM 1995 6 23 SWAA950462 119950619A2913887477 PUMP BOEING737 7373H4 1384600NM HYD SYST INOP A SWAAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07313SW 23335 DURING CLIMBOUT, EXPERIENCED SYSTEM A HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO ELP AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND A SYSTEM HYDRAULIC PUMP INOP. REPLACED AND SERVICED SYSTEM PER BOEING M/M. 2L72 4F RTA16WE 19950623008241995062300824NM 1995 6 23 SWAA950463 119950619A5311 FRAME BOEING737 7372T4 1384492NM BS 520 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME AT BS 520, FAILSAFE ATTACH ANGLE HAS TOOLING MARK DAMAGE AT S16R AFT OF RT WING SCANNING LIGHT HOUSING. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008251995062300825NM 1995 6 23 SWAA950464 119950619A5320 CHORD BOEING737 7372T4 1384492NM BS 1156 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND CRACK EXTENDING FROM BENEATH RT UPPER TORQUE TUBE SUPPORT FITTING IN O/B CHORD, BS 1156 BULKHEAD. REPAIRED PER SWA ACO 473-53. 2L72 4F A16WE 19950623008261995062300826NM 1995 6 23 SWAA950465 119950619A5315 FLOOR BEAM BOEING737 7372T4 1384492NM RBL 45.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS AT RBL 45.5. REPAIRED PER SWA ACO 583-53-R3. 2L72 4F A16WE 19950623008271995062300827NM 1995 6 23 SWAA950466 119950619A5320 WEB BOEING737 7372T4 1384492NM APU COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT LIGHTENING HOLE ON TOP SIDE OF APU CAVITY. INSTALLED WEB REPAIR PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008281995062300828NM 1995 6 23 SWAA950467 119950619A5320 WEB BOEING737 7372T4 1384492NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE AT BS 344 AT BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008291995062300829NM 1995 6 23 SWAA950468 119950619A5320 SHEAR TIE BOEING737 7372T4 1384492NM BS 598 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE CRACKED AT BS 598, FWD SIDE S17L, BELOW CREASE BEAM. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008301995062300830NM 1995 6 23 SWAA950469 119950619A5312 BLKHD CHORD BOEING737 7372T4 1384492NM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 663, AT INBOARD EDGE OF VERTICAL SUPPPORT ANGLE, RBL 24.75. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 691A0032. 2L72 4F A16WE 19950623008311995062300831NM 1995 6 23 SWAA950470 119950619A5320 WEB BOEING737 7372T4 1384492NM BS 599 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT BS 599, AT FLOOR LEVEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008321995062300832NM 1995 6 23 SWAA950471 119950619A5311 FRAME BOEING737 7372T4 1384492NM BS 540 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME CRACKED BELOW WING ROOT, BS 540. REPAIRED PER SWA ACO 518-53. 2L72 4F A16WE 19950623008331995062300833NM 1995 6 23 SWAA950472 119950619A5315 FLOOR BEAM BOEING737 7372T4 1384492NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950623008341995062300834NM 1995 6 23 SWAA950473 119950619A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0. REPAIRED PER BOEING STR. 2L72 4F A16WE 19950623008351995062300835 1995 6 23 SWIA95588 419950531A3418 STALL WARN PNL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE E/E COMPT MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 NM07209SW 120269 ON TAKEOFF ROLL, THE STALL SYSTEM ACTIVATED. ABORTED TAKEOFF. RT SYSTEM FAILS TO TEST PROPERLY. DEFERRED PER MEL 27-36-2. REMOVED STALL WARNING PANEL AND REPLACED IT WITH A SERVICEABLE ONE, IAW MM 27-34-08, OPS CKS GOOD, SEE F/L 75803. 2L72 4T4 TRTA31SO E20NE 19950623008361995062300836SO 1995 6 23 SWIA95589 119950530A2750 CONTROL BOX EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAK NONE J WARNING INDICATION CLCLIMB 1 NM07186SW 120034 ON TAKEOFF WHEN FLAPS WERE RAISED, DISAGREEMENT WARNING OCCURRED. RERACKED FLAP CONTROL UNIT CYCLES FLAPS, OPS CKS GOOD, SEE F/L 74638. 2L72 4T4 TRTA31SO E20NE 19950623008371995062300837SW 1995 6 23 SWIA95590 119950603A3260 LAMP SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NLG INDICATING FAILED A SWIAO OTHER P NO WARNING INDICATION LDLANDING 1 NM07176SW AC591 NOSE GEAR LANDING POSITION LIGHT (GREEN) DID NOT ILLUMINATE UPON GEAR DOWN. REPLACED LAMPS IN INDICATOR. AIRCRAFT WAS FERRIED TO PSP WHERE THE GEAR WAS SWUNG. OPS CHECKS GOOD AT THIS TIME. 1L72 4T4 T A8SW E4WE 19950623008381995062300838SO 1995 6 23 SWIA95591 119950615A2750 ROLLER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT TE FLAP FAILED A SWIAK NONE J WARNING INDICATION CLCLIMB 1 NM07190SW 120050 ON DEPARTURE, THE OUTBOARD FLAPS WOULD NOT RETRACT PAST 6 DEGREES. REPLACED THE ROLLER (INBOARD ROLLER) ON THE LEFT OUTBOARD MOVEABLE FLAP. OPS CHECKS OK. 2L72 4T4 TRTA31SO E20NE 19950623008391995062300839SO 1995 6 23 SWIA95592 119950612A27503075001007 CONTROL UNIT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07194SW 120120 FLAP DISAGREEMENT ON RETRACTION AFTER TAKEOFF. REPLACED FLAP CONTROL BOX, CYCLED FLAP 10 TIMES, OPS CKS GOOD IN ALL MODES OF OPERATION, SEE F/L 75838. 2L72 4T4 TRTA31SO E20NE 19950623008401995062300840EA 1995 6 23 SWIA95593 119950618A301014463101 DE-ICE TUBE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT WING FAILED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 LT ANTI-ICE DUCT WARNING WING ANTI-ICE SWITCH NORMAL OR STANDBY POSITION. REMOVED LT OUTBD WING LEADING EDGE, REMOVED PICCALO TUBE, INSTALLED LEADING EDGE, IAW MM 57-41-01, GROUND RAN A/C OPS CKS GOOD, SEE F/L 2536. 2L72 4F4 FRTA21EA E15NE 19950623008411995062300841SO 1995 6 23 SWIA95594 119950616A6120 PCU EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 NM07216SW 120285 RT SIDE PROP OVERSPEED ON TAKEOFF. ABORTED TAKEOFF. PROPELLER NP STABILIZED AT 102.5 TO 102.6 PERCENT AFTER 103.1 MAX. INSPECTED THE PCU (PROPELLER CONTROL UNIT) RIGGING AND INSPECTED BETA TUBE SEALS. REINSTALLED BETA TUBE IAW 61-10-02. FOUND TO BE WITHIN LIMITS PER 61-00-00. 2L72 4T4 TRTA31SO E20NE 19950623008421995062300842NM 1995 6 23 UPS203632 119950621A5320 WEB BOEING727 72751C 1384015NM FS 351 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON B.S. 351 WEB AT RBL 217, WL 172. REPAIRED IAW SRM 51-40-2. 2L73 4F A3WE 19950623008431995062300843NM 1995 6 23 UPS203633 119950621A5330 SKIN BOEING727 72751C 1384015NM FS 1330 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN SKIN AT BLOWOUT DOOR CUTOUT, B.S. 1333, LBL 48, WL 217. REPAIRED IAW SRM 51-10-2, 53-30-3, 51-30-2, 51-20-4, 51-10-1, 51-10-2, M/M 51-20-151. 2L73 4F A3WE 19950623008441995062300844NM 1995 6 23 UPS203634 119950621A5350 BOX FAIRING BOEING727 72751C 1384015NM FS 277 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK MAINTENANCE FOUND CRACK EXTRUDING PAST STOP DRILL IN NOSE WHEELWELL SIDE BOX FAIRING. B.S. 277, RBL 23.5, WL 168. REPAIRED IAW SRM 51-10-2, 51-30-2, 51-21-1. 2L73 4F A3WE 19950623008451995062300845NM 1995 6 23 UPS203635 119950621A5320 WINDSHIELD SILL BOEING727 72751C 1384015NM FS 267 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL LT SIDE AT B.S. 267. REPAIRED IAW SRM 727-53-1620. 2L73 4F A3WE 19950623008461995062300846NM 1995 6 23 UPS203636 119950621A5320 WINDSHIELD SILL BOEING727 72751C 1384015NM FS 269 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON WINDSHIELD UPPER SILL RT SIDE AT B.S. 269. REPAIRED IAW SRM 53-30-3, 51-30-2. 2L73 4F A3WE 19950623008471995062300847NM 1995 6 23 UPS203637 119950621A5320 STRAP BOEING727 72751C 1384015NM FS 351 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRAP B.S. 351, RBL 30, WL 172. REPAIRED IAW SRM 51-40-4. 2L73 4F A3WE 19950623008481995062300848NM 1995 6 23 UPS203638 119950621A5315BAC1505100746 FLOOR BEAM BOEING727 72751C 1384015NM FS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION UNDER UPPER FLOOR BEAM FLANGE, FORWARD SIDE STA 344, RBL 2, WL 208. REPAIRED IAW SRM 51-20-1, 51-10-1, 53-10-8, 51-30-2. 2L73 4F A3WE 19950623008491995062300849NM 1995 6 23 UPS203639 119950621A5542 SKIN BOEING727 72751C 1384015NM RUDDER TAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER RUDDER TAB ON LOWER RT SIDE. REPAIRED IAW SRM 51-40-9. 2L73 4F A3WE 19950623008501995062300850NM 1995 6 23 UPS203640 119950621A5753 WEDGE BOEING727 72751C 1384015NM RT TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND DISBONDED R/W I/B MID FLAP T/E WEDGE UPPER SURFACE AND WATER IN HONEY COMB. REPAIRED IAW SRM 51-40-6. 2L73 4F A3WE 19950623008511995062300851NM 1995 6 23 UPS203641 119950621A57546516200104 STIFFENER BOEING727 72751C 1384015NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER R/W L/E NR 6 SLAT I/B TRACK I/B SIDE LOWER END SLAT STA 135.5. REPAIRED IAW SRM 51-30-2, 51-10-2, M/M 28-11-21, 36-00-01, OHM 20-50-01. 2L73 4F A3WE 19950623008521995062300852NM 1995 6 23 UPS203642 119950621A5720651621648 ANGLE BOEING727 72751C 1384015NM WS 120 BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK MAINTENANCE, FOUND BROKEN ANGLE SUPPORT BRACKET AT WING BASE LINE STA 120, BEHIND THE NR 8 SPOILER ACTUATOR FITTING. REPAIRED IAW SRM 51-20-1, 51-30-2. 2L73 4F A3WE 19950623008531995062300853NM 1995 6 23 UPS203643 119950621A5320BAC1505100257 ANGLE BOEING727 72751C 1384015NM FS 920 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT B.S. 920, LBL 65, WL 189 AROUND LOWER FASTENERS. REPAIRED IAW SRM 51-10-2, 51-30-5, 51-30-2, 51-20-1, M/M 51-20-31. 2L73 4F A3WE 19950623008541995062300854NM 1995 6 23 UPS203644 119950621A5311 FRAME BOEING727 72751C 1384015NM FS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN C-CHECK, MAINTENANCE FOUND CRACKED FRAME ON STA 760, LBL 72, WL 205. REPAIRED IAW B727-5310-7117-A. 2L73 4F A3WE 19950623008551995062300855NM 1995 6 23 UPS203645 119950621A5753 WEDGE BOEING727 72751C 1384015NM RT TE MID FLAP DISBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W O/B MID FLAP T/E WEDGE UPPER SURFACE DISBONDED. REPAIRED IAW SRM 57-40-6, 51-40-6. 2L73 4F A3WE 19950623008561995062300856NM 1995 6 23 UPS203655 119950621A3230 CONTROL VALVE BOEING727 727180C 138406GNM LANDING GEAR MALFUNCTIONED A IPXAO OTHER O OTHER CLCLIMB 1 SO01940UP 19826 FELT RESTRICTION OF GEAR HANDLE DURING RETRACTION. CYCLED GEAR, SAME RESPONSE. REPLACED GEAR CONTROL VALVE. 2L73 4F A3WE 19950623008571995062300857NM 1995 6 23 UPS203656 119950622A3350 EEL BOEING727 72727C 138400JNM CABIN LOOSE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01910UP 19117 WHILE ON GROUND MAINTENANCE FOUND EMERGENCY LIGHT FIXTURE OVER ENTRY DOOR WILL NOT STAY UP. RETORQUED MOUNT SCREW. 2L73 4F A3WE 19950623008581995062300858NM 1995 6 23 UPS203657 119950620A3260 GEAR LIGHT BOEING727 7272A1 138407FNM RT MLG ILLUMINATED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01213U 21341 RED GEAR LIGHT FOR RIGHT MAIN REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED GEAR AND STILL REMAINED ILLUMINATED. GEAR DOOR LIGHTS ON S/O PANEL WORKED PROPERLY. (CREW REPORTED THAT LIGHT WENT OUT AFTER TEN MINUTES). MAINTENANCE COULD NOT DUPLICATE PROBLEM ON OPERATIONAL TEST IAW M/M 32-09-121. 2L73 4F A3WE 19950623008591995062300859NM 1995 6 23 UPS203660 119950621A571265C215248 RIB BOEING727 72751C 1384015NM WS 70.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142. 2L73 4F A3WE 19950623008601995062300860NM 1995 6 23 UPS203661 119950622A5522 SKIN BOEING727 72722C 138400FNM LT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT ELEVATOR UPPER SKIN BEADED DOUBLER AT STA 40 HAS A 1 INCH CRACK FROM DRAIN HOLE. REPAIRED IAW SRM 55-20-3. 2L73 4F A3WE 19950623008611995062300861NM 1995 6 23 UPS203662 119950622A5320 RIB BOEING727 72722C 138400FNM FS 1367 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN FOR C-CHECK, MAINTENANCE FOUND F.S. 1367 RT RIB CRACKED. REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950623008621995062300862NM 1995 6 23 UPS203663 119950622A5712 LE RIB BOEING727 72722C 138400FNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT THE O/B END OF THE NR 6 SLAT UPPER FLANGE CRACKED IN 3 PLACES. REPAIRED IAW SRM 51-40-3. 2L73 4F A3WE 19950623008631995062300863NM 1995 6 23 UPS403631 119950620A5320 CHORD BOEING747 747123 1384873NM FS 720 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FORWARD LOWER CARGO COMPARTMENT CRACK IN UPPER CHORD STA 720 RBL 1. REPAIRED IAW E.O. 747-53-0717. 2L74 4F A20WE 19950623008641995062300864NM 1995 6 23 UPS503658 119950620A5610 WINDSHIELD BOEING757 75724APF 1384969NM LT FLIGHT DECK SHATTERED A IPXAK NONE O OTHER CRCRUISE 1 SO01440UP 25471 CAPTAIN'S WINDSHIELD SHATTERED IN FLIGHT AT FL 350. FIELD OF VIEW OBSCURED. REPLACED WINDOW IAW M/M 56-11-01. 2L72 4F RTA2NM 19950623008651995062300865WP 1995 6 23 UPS803646 119950621A53205643483501 FITTING DOUG DC8 DC871F 302199DWP FS 880 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME LOWER FITTING AT BOLT HOLES AT F.S. 880, LT AT FLOOR BEAM. 2L74 4F RT4A25 19950623008661995062300866WP 1995 6 23 UPS803647 119950621A53205646955503 FITTING DOUG DC8 DC871F 302199DWP FS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME END FITTING, F.S. 960, LONGERON 22L. REPAIRED IAW DC8-5310-7126-A. 2L74 4F RT4A25 19950623008671995062300867WP 1995 6 23 UPS803648 119950621A53159887426 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 1660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM UPPER FLANGE LOWER SURFACE FORWARD SIDE AT F.S. 1660 UNDER NR 3 SEAT TRACK. 2L74 4F RT4A25 19950623008681995062300868WP 1995 6 23 UPS803649 119950621A531157556003 FRAME DOUG DC8 DC871F 302199DWP FS 1140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME AFT ANGLE CRACKED AT F.S. 1140, LONGERON 35L. REPAIRED IAW DC8-5310-7129-A. 2L74 4F RT4A25 19950623008691995062300869WP 1995 6 23 UPS803650 119950621A53159887426 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 1680 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER FLANGE LOWER SURFACE OF FLOOR BEAM F.S. 1680, UNDER NR 3 SEAT TRACK. REPAIRED IAW DC8-5310-7125-A. 2L74 4F RT4A25 19950623008701995062300870WP 1995 6 23 UPS803651 119950621A5311975508712 FRAME DOUG DC8 DC871F 302199DWP FS 1345 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON BELT FRAME 1.5, LONGERON AT F.S. 1345, LONGERON 21R. REPAIRED IAW DC8-5310-7120-A. 2L74 4F RT4A25 19950623008711995062300871WP 1995 6 23 UPS803652 119950621A53205612298 PANEL DOUG DC8 DC871F 302199DWP FS 12 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE UNDER REPAIR AT NOSE WHEELWELL CEILING ABOVE LIGHT F.S. 12. REPAIRED IAW DC8-5310-7121-A. 2L74 4F RT4A25 19950623008721995062300872WP 1995 6 23 UPS803653 119950621A53305615372 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 INCH CRACK IN SKIN AT LOWER FORWARD CORNER AFT CARGO BIN DOOR CUT OUT. REPAIRED IAW DC8-5330-7124-A. 2L74 4F RT4A25 19950623008731995062300873WP 1995 6 23 UPS803654 119950621A53159753797501 FLOOR BEAM DOUG DC8 DC871F 302199DWP FS 1580 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM, F.S. 1580, LONGERON 22R. REPAIRED IAW DC8-5310-7128-A. 2L74 4F RT4A25 19950630000021995063000002CE 1995 6 30 95ZZZX3127 119950411A3230 DRAG LINK BEECH 58 58 1152740CE NLG BROKEN A BVYAK NONE O OTHER ININSP/MAINT 1 CE076493S5200 TH710 POST-FLIGHT INSPECTION DETECTED BROKEN NOSE DRAG LINK. OLD STYLE DRAG LINK IS MADE FROM WELDED TUBE STEEL. IT APPEARS PART CORRODED FROM INSIDE. INSTALLED SERVICE KIT 35-4012-1S. NEW DRAG LINK IS A CAST PART NOW. 1L72 3O 3A16 19950630000431995063000043SW 1995 6 30 95ZZZX3168 119950413A324613600L BEARING BFGOODRICH 313571 SWRNGNSA227 SA227AC 8780603SW RT INBD WHEEL FAILED A VPOAO OTHER O OTHER TOTAKEOFF 1 WP173109B 3806 AC522 DURING TAKEOFF, THE OUTBOARD BEARING ON THE RT INBOARD TIRE FAILED. AFTER THE BEARING BROKE DOWN, IT LET THE WHEEL ASSEMBLY LEAVE THE AXLE WITH THE NUT AND COTTER PINS STILL INSTALLED. NO DAMAGE TO THE AXLE OR BRAKE ASSY. CAUSE OF FAILURE IS UNKNOWN. BEARINGS HAD GREASE. 1L72 4T A8SW 19950630000441995063000044SW 1995 6 30 95ZZZX3169 119950605A80103003724 DIODE BELL 222 222B 1182124SW START CKT FAILED A MXIAK NONE O OTHER ININSP/MAINT 1 EA21492CK 47145 ACTT 1990.5. PILOT ATTEMPTED TO START NR 1 ENGINE AT 12 PERCENT NG. STARTER DROPPED OFF-LINE. ON SUBSEQUENT ATTEMPT, ONLY ENGINE IGNITER OPERATED. DURING TROUBLESHOOTING, FOUND BOTH GROUND CIRCUIT DIODES HAD FAILED. REPLACED BOTH DIODES, OPS CHECK OF START SYSTEM CHECKED GOOD. REF: OPER CONTROL NR MXIA627G. 1G72 3U H9SW 19950630000471995063000047WP 1995 6 30 9509699758 119950617A7711LG80A2 EPR TRANSMITTER DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01758NW8162 8162 47286 666694 NR 2 ENGINE EPR INDICATION BEGAN DECREASING SHORTLY AFTER DEPARTURE. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE EPR TRANSMITTER. THE AIRCRAFT WAS RUNUP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950630000481995063000048NM 1995 6 30 9509702282 119950621A2780 ACTUATOR DOOR BOEING727 727251 138408HNM NR 8 LE FLAP MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01282US 21161 DURING CLIMB UPON FLAP RETRACTION, THE NR 8 LEADING EDGE SLAT REMAINED EXTENDED. JETTISONED 12,000 LBS OF FUEL AND RETURNED TO DTW. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED NR 8 SLAT ACTUATOR DOOR TO BE CAUSE, ITEM DEFERRED. 2L73 4F A3WE 19950630000491995063000049NM 1995 6 30 9509712298 119950621A315032EN144 SWITCH BOEING727 727251 138408HNM STABILIZER DEFECTIVE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01298US 22152 DURING APPLICATION OF TAKEOFF POWER, AURAL WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND LOWER STABILIZER TRIM WARNING SWITCH S533 DEFECTIVE. REPLACED SWITCH AND PERFORMED OPERATIONAL CHECK. NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950630000501995063000050EU 1995 6 30 9509723237 119950621A36106740B050000 VALVE AIRBUS320 A320211 3930320EU NR 1 ENGINE MALFUNCTIONED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01337NW 358 DURING TAKEOFF ROLL, RECEIVED AIR ENG 2 BLEED FAULT. TAKEOFF WAS ABORTED AT LESS THAN 80 KNOTS. ALSO, RECEIVED AIR LT WING LEAK AND RIGHT PACK OVERHEAT MESSAGES. MAINTENANCE REPLACED THE NR 1 ENGINE OVER PRESSURE VALVE. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950630000511995063000051NM 1995 6 30 DL72E952758 119950621A5313 STRINGER BOEING727 727247 138408FNM FS 510 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CHECK, CORROSION IN STRINGER 26R AT STATION 510. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950630000521995063000052NM 1995 6 30 DL72S952072 119950512A57536521631365K LE SKIN 6521631365K BOEING727 727232 1384082NM NR 1 FOREFLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 DURING SHOP INSPECTION, NR 1 FOREFLAP WAS FOUND WITH DAMAGE TO L/E SKIN AT 52 TO 55 FROM THE O/B END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950630000531995063000053NM 1995 6 30 DL72S952073 119950512A57536521631325K LE SKIN 6521631325K BOEING727 727232 1384082NM NR 1 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 DURING SHOP INSPECTION, NR 1 FOREFLAP L/E SKIN WAS FOUND DAMAGED AT 7 TO 11 FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950630000541995063000054NM 1995 6 30 DL72S952148 119950517A57536521631324 LE SKIN 6521631324 BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA BN26 22494 DURING SHOP INSPECTION, NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO L/E AT 86 FROM THE I/B END. REPAIRED PER SRM 57-50-4 FIG 1. 2L73 4F A3WE 19950630000551995063000055NM 1995 6 30 DL72S952159 119950429A5330 SKIN BOEING727 727232 1384082NM AFT OF E/E COMP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 AT HMV, FOUND LOWER FUSELAGE SKIN WITH CORROSION DAMAGE JUST AFT OF E/E COMPARTMENT OPENING. REPAIRED DAMAGE PER SRM 53-30-3 FIG 2. 2L73 4F A3WE 19950630000561995063000056NM 1995 6 30 DL72S952317 119950511A5753 SKIN 6521631247A BOEING727 727232 1384082NM NR 4 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA BN224 21077 DURING SHOP INSPECTION, NR 4 FOREFLAP WAS FOUND WITH WEAR DAMAGE TO THE L/E SKIN AT 12 FROM THE 0/B END. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950630000571995063000057NM 1995 6 30 DL72S952738 119950621A5720 STIFFENER BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11405DA 21149 FOUND DURING E-1 LETTER CHECK, WING SPAR STIFFENER AT NR 6 LE SLAT I/B TRACK O/B SIDE HAS 1 INCH CRACK FROM BOTTOM. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950630000581995063000058NM 1995 6 30 DL73S952135 119950422A57536546435236 LE SKIN 6546435236 BOEING737 737232 1384475NM NR 4 AFT FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11332DL 23104 DURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH TIME LIMITED REPAIR ON L/E AT 16 FROM THE I/B END OF FLAP. REPAIRED PER SRM 57-50-4 FIG 5. 2L72 4F RTA16WE 19950630000591995063000059NM 1995 6 30 DL73S952136 119950422A57536546435236 TE WEDGE 6546435236 BOEING737 737232 1384475NM NR 4 AFT FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11332DL 23104 DURING SHOP INSPECTION, NR 4 AFT FLAP WAS FOUND WITH T/E WEDGE WITH DAMAGE TO O/B AFT CORNER. REPAIRED PER SRM 57-53-01. 2L72 4F RTA16WE 19950630000601995063000060NM 1995 6 30 DL73S952137 119950422A57536546435236 TE WEDGE 6546435236 BOEING737 737232 1384475NM NR 4 AFT FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11332DL 23104 DURING SHOP INSPECTION, NR 4 AFT FLAP T/E WEDGE WAS FOUND DELAMINATED 10 FROM THE INBD END OF FLAP. REPAIRED PER SRM 51-70-10. 2L72 4F RTA16WE 19950630000611995063000061NM 1995 6 30 DL757952138 119950516A5754114N400512 SKIN 114N400512 BOEING757 757232 1384965NM NR 4 LE SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING SHOP INSPECTION, FOUND NR 4 SLAT WITH HOLE IN LOWER SURFACE OF T/E WEDGE. REPAIRED PER SRM 57-43-02 REF 51-70-10 PG 21 FIG 8. 2L72 4F RTA2NM 19950630000621995063000062NM 1995 6 30 DL757952739 119950621A5753 SKIN BOEING757 757232 1384965NM NR 1 AFT FLAP DAMAGED A DALAK NONE O OTHER CRCRUISE 1 SO11657DL 24419 DURING LETTER CHECK, COMPLETED SCHEDULED PERMANENT REPAIR FOR CRACKS IN NR 1 AFT FLAP. REPAIRED PER SRM 57-53-01 AND SRM 51-70-17. 2L72 4F RTA2NM 19950630000631995063000063NM 1995 6 30 DL757952740 119950621A5754 SKIN BOEING757 757232 1384965NM NR 9 LE SLAT DENTED A DALAK NONE O OTHER CRCRUISE 1 SO11657DL 24419 DURING LETTER CHECK FROM SCHEDULED MTC, INSTALLED PERMANENT REPAIR FOR DENT ON NR 9 L/E SLAT, PER SRM 57-43-02. 2L72 4F RTA2NM 19950630000641995063000064NM 1995 6 30 DL757952752 119950618A7110314N301016B COWL BOEING757 757232 1384965NM NR 1 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 23614 GROUND DAMAGE TO NOSE COWL PANEL WAS FOUND AT 10 O'CLOCK POSITION, DURING HMV. DAMAGE WAS REPAIRED PER SRM 54-11-01 REF 51-70-17. 2L72 4F RTA2NM 19950630000651995063000065NM 1995 6 30 DL757952754 119950619A5754114N4005158 TE WEDGE BOEING757 757232 1384965NM NR 7 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11627DL 22917 DURING HMV NR 7 SLAT T/E WEDGE WAS FOUND TO HAVE DELAMINATION ON THE T/E WEDGE 33 FROM THE I/B END. 2L72 4F RTA2NM 19950630000661995063000066NM 1995 6 30 DL767952712 119950613A5522 LE SKIN 183T30012 BOEING767 767232 1385132NM RT ELEV GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11109DL 000098 22221 DURING LETTER CHECK, FOUND RT O/B ELEVATOR WITH GOUGE IN L/E SKIN. REPAIRED PER SRM 55-20-02. 2L72 4F RTA1NM 19950630000671995063000067WP 1995 6 30 DLL10952736 119950621A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1523 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FLOORBEAM AT STA 1523 CORRODED 0 BL TO 30 LBL. FOUND DURING HMV CORROSION INSP. REPAIRED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950630000681995063000068WP 1995 6 30 DLL10952741 119950617A57531529113112 SKIN LKHEED1011 10113851 5265010WP NR 2 TE VANE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING LETTER CHECK, FOUND LEFT WING NR 2 FLAP VANE WITH DENT IN SKIN. REPAIRED PER SRM 57-53-00. 2L73 4F A23WE 19950630000691995063000069WP 1995 6 30 DLL10952742 119950617A5312 BLKHD ANGLE LKHEED1011 10113851 5265010WP FS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 RT SIDE FS 1223 CANTED BULKHEAD ANGLE IS CRACKED. REMOVED DAMAGED ANGLE AND INSTALLED NEW ANGLE PER SRM 53-11-00 PG 859, FOUND AT LETTER CHECK. 2L73 4F A23WE 19950630000701995063000070WP 1995 6 30 DLL13952209 119950511A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 297 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT STA 298 LBL 28. INSTALLED NEW CAP PER SRM 53-21-00. 2L73 4F A23WE 19950630000711995063000071WP 1995 6 30 DLL13952745 119950512A5330 STRAP LKHEED1011 10113851 5265010WP FS 1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1725 BETWEEN STR 33 AND 34, FOUND DURING HMV. REPAIRED PER SRM 53-31-00. FIG 801. 2L73 4F A23WE 19950630000721995063000072WP 1995 6 30 DLL13952746 119950512A5330 STRAP LKHEED1011 10113851 5265010WP FS 1665-1685 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, FAILSAFE STRAP LIFTED FROM SKIN C-3 B/B BETWEEN FS 1665 TO 1685 STR 43 AND 44. REPAIRED PER SRM 53-31-00 PG 807. 2L73 4F A23WE 19950630000731995063000073WP 1995 6 30 DLL13952747 119950514A5330 STRAP LKHEED1011 10113851 5265010WP BS 1745 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1745 BETWEEN STR 44 AND 45. REPAIRED PER SRM 53-31-00 FIG 801. 2L73 4F A23WE 19950630000741995063000074WP 1995 6 30 DLL13952748 119950512A5330 STRAP LKHEED1011 10113851 5265010WP BS 1763 1778 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED C-3 B/B FS 1763 TO 1778 BETWEEN STR 43 TO 45. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950630000751995063000075WP 1995 6 30 DLL13952749 119950512A5330 STRAP LKHEED1011 10113851 5265010WP BS 1685-1705 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, FAILSAFE STRAP LIFTED/CORRODED FROM FUSELAGE SKIN, FS 1685 TO 1705 BETWEEN STR 39 AND 40. REPAIRED PER SRM 53-31-00 FIG 801. 2L73 4F A23WE 19950630000761995063000076WP 1995 6 30 DLL13952750 119950512A5313 STRINGER LKHEED1011 10113851 5265010WP BS 1645-1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, C-3 B/B STRINGER CORRODED FS 1645 TO 1725 STR 39. REPLACED DAMAGED STRINGER FROM FS 1675 TO 1695 PER SRM 53-13-00 PG 806. 2L73 4F A23WE 19950630000771995063000077WP 1995 6 30 DLL13952751 119950509A5210 SKIN LKHEED1011 10113851 5265010WP C-2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FOUND DURING HMV, BOTTOM LIP OF C-2 DOOR CRACKED IN CENTER. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER REF 52-11-00 FIG 804. INSTALLED REPAIR PER SRM 52-11-00 PG 804 FIG 804. 2L73 4F A23WE 19950630000781995063000078WP 1995 6 30 DLL13952755 119950512A5311 FRAME LKHEED1011 10113851 5265010WP BS 281 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FUSELAGE FRAME IN FESC LT SIDEWALL IS CRACKED AT FRAME SPLICE AT STA 281 BETWEEN STR 47 AND 48. REPAIRED PER SRM 53-12-00 FIG 814. 2L73 4F A23WE 19950630000791995063000079WP 1995 6 30 DLL13952756 119950512A5315 FLOORBEAM LKHEED1011 10113851 5265010WP BS 1505 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FLOORBEAM CORRODED AFT OF FS 1505 BELOW LEFT FIXED FLOOR PANEL ABOVE STRINGER 40. REPAIRED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950630000801995063000080WP 1995 6 30 DLL13952757 119950510A5315 FLOORBEAM LKHEED1011 10113851 5265010WP BS 1521 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FLOORBEAM CORRODED AT FS 1521 ABOVE STRINGER 33. REPAIRED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950630000811995063000081WP 1995 6 30 DLL13952759 119950510A5315537201318 FLOORBEAM LKHEED1011 10113851 5265010WP BS 1605 MISDRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FLOORBEAM T-CAP WAS FOUND MISSDRILLED AND 2 HOLES PLUGGED IN SPLICE AT FS 1605 AT RBL 5. REMOVED DAMAGED CAP AND INSTALLED REPAIR PER SRM 53-23-00 PG 803. 2L73 4F A23WE 19950630000821995063000082WP 1995 6 30 DLL13952760 119950511A5743 ACT FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, RT MLG ACTUATOR ATTACH FITTING UPPER FLANGE HOLES 1, 2, 3, 5, 6 ARE CORRODED. REAMED HOLES TO REMOVE CORROSION, SPOTFACED, ROTOPEEND AND INSTALLED BUSHINGS PER SRM 57-14-00. 2L73 4F A23WE 19950630000831995063000083WP 1995 6 30 DLL13952761 119950512A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP BS 1403-1423 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 FAILSAFE STRAP LIFTED/CORRODED C2 BB AT FS 1403 TO 1423 STR 35 AND 36, FOUND AT HMV. REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950630000841995063000084NM 1995 6 30 P5CA9500101 119950623A326060B4001826 SENSOR BOEING747 747121 1384871NM LT MLG SHORTED A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23832FT 20347 ON TAXI OUT, CREW FOUND AUTOSPOILER LIGHT ILLUMINATED AND FOUND THE LANDING GEAR ALTERNATE CONTROL CIRCUIT BREAKER OPEN. RESET CIRCUIT BREAKER, 20 TO 30 SECONDS BREAKER OPENED. FOUND LEFT WING GEAR ALTERNATE DOWN AND LOCK SENSOR TO BE AT FAULT. DEACTIVATED PER MEL AND DISPATCHED AIRCRAFT. 2L74 4F A20WE 19950630000851995063000085NM 1995 6 30 P5CA9500102 119950527A5730 SKIN BOEING747 747121 1384871NM WS 1100-1250 PEELING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING UPPER SURFACE WS 1100 TO 1250 FIBER PEELING OFF. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630000861995063000086NM 1995 6 30 P5CA9500103 119950521A5754 TE FIBER BOEING747 747121 1384871NM NR 21 LE FLAP DETERIORATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE FLAP NR 21 VARIABLE CAMBER TRAINING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630000871995063000087NM 1995 6 30 P5CA9500104 119950527A5712 RIB BOEING747 747121 1384871NM WS 1322 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE CAVITY FS 1322 FORGED RIB AFT UPPER CHORD END IS CRACKED. REPAIRED PER BOEING SB 57-2116 FIGURE 6. 2L74 4F A20WE 19950630000881995063000088NM 1995 6 30 P5CA9500105 119950621A5754 TE FIBER BOEING747 747121 1384871NM NR 25 LE FLAP DETERIORATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING NR 25 LEADING EDGE FLAP VARIABLE CAMBER TRAILING EDGE FIBER IS DETERIORATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630000891995063000089NM 1995 6 30 P5CA9500106 119950528A572069B120591 FITTING BOEING747 747121 1384871NM WS 956 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON SUPPORT ROD BASE, ON LOWER FIXED PANEL ON RIGHT WING LEADING EDGE CAVITY WS 956, UNDER NR 8 PDU. INSTALLED NEW FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630000901995063000090NM 1995 6 30 P5CA9500107 119950521A5350 FAIRING BOEING747 747121 1384871NM BS 1620 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON AFT FAIRING AT STA 1620 STRINGER 47 AREA. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630000911995063000091NM 1995 6 30 P5CA9500108 119950521A5330 SKIN BOEING747 747121 1384871NM BS 1480-1680 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FUSELAGE SKIN AT THE CENTER LINE BETWEEN S50L AND S50R BETWEEN STA 1480 AND 1680. CORROSION REMOVED AS PER BOEING SRM 51-10-10. 2L74 4F A20WE 19950630000921995063000092NM 1995 6 30 P5CA9500109 119950521A5330 SKIN BOEING747 747121 1384871NM BS 1660 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FITTING SUPPORT FAIRING AT STA 1660 STR 49 AREA. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950630000931995063000093NM 1995 6 30 P5CA9500110 119950528A5320 RIVETS BOEING747 747121 1384871NM BS 1480 LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LOOSE RIVETS AT STA 1480 LBL 75. RIVETS CHANGED PER BOEING SRM 51-30-02, 52-10-02. 2L74 4F A20WE 19950630000941995063000094NM 1995 6 30 P5CA9500111 119950528A5320 SUPPORT BOEING747 747121 1384871NM BS 1620-1660 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON OMEGA SUPPORT BETWEEN STA 1620 AND 1660. CORROSION REMOVED AS PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950630000951995063000095NM 1995 6 30 P5CA9500112 119950521A5320 SUPPORT BOEING747 747121 1384871NM BS 1620-1660 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT ON OMEGA SUPPORT BETWEEN STA 1620 TO 1660 STR 40 AREA. REPAIRED AS PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950630000961995063000096NM 1995 6 30 P5CA9500113 119950521A5320 SUPPORT BOEING747 747121 1384871NM BS 1480-1620 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT FAIRING AT THE CENTER LINE BETWEEN STATION 1480 TO 1620. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630000971995063000097NM 1995 6 30 P5CA9500114 119950521A5330 SKIN BOEING747 747121 1384871NM BS 1480-1680 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SKIN BETWEEN STR 40 TO 50 AND BETWEEN STA 1480 TO 1680 LT AND RT. REMOVED AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630000981995063000098NM 1995 6 30 P5CA9500115 119950521A5320 SUPPORT BOEING747 747121 1384871NM BS 1540 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT FAIRING STA 1540 BETWEEN STR 25 TO 50. CORROSION REMOVED AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630000991995063000099NM 1995 6 30 P5CA9500116 119950521A5320 SUPPORT BOEING747 747121 1384871NM BS 1580 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT FAIRING STA 1580 BETWEEN STR 28 TO 50 RT AND LT. CORROSION REMOVED PER SRM 51-10-01. 2L74 4F A20WE 19950630001001995063000100NM 1995 6 30 P5CA9500117 119950521A5320 SUPPORT BOEING747 747121 1384871NM BS 1660 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT FAIRING STA 1660 BETWEEN STR 33 TO 46 LT AND RT. REPAIRED AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630001011995063000101NM 1995 6 30 P5CA9500118 119950521A5320 ANGLE BOEING747 747121 1384871NM BS 580 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 UPPER DECK FLOORBEAM CHORD AT STA 580 RBL 45, FOUND CRACKED ANGLE. INSTALLED NEW ANGLE PER BOEING SRM 51-10-00. 2L74 4F A20WE 19950630001021995063000102NM 1995 6 30 P5CA9500119 119950521A5347 SEAT TRACK BOEING747 747121 1384871NM BS 620-640 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 UPPER DECK SEAT TRACK CORRODED AT LBL 22 BETWEEN STA 620 TO 640. REMOVED CORROSION AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630001031995063000103NM 1995 6 30 P5CA9500120 119950521A5350 FAIRING BOEING747 747121 1384871NM NR 5 DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 5 FAIRING PANEL DELAMINATED ON OUTER SIDE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001041995063000104NM 1995 6 30 P5CA9500121 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 4 LT DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 4 LEFT FAIRING PANEL DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001051995063000105NM 1995 6 30 P5CA9500122 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 3 RT DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 3 RIGHT FAIRING PANEL HAS HOLES AND DELAMINATIONS. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001061995063000106NM 1995 6 30 P5CA9500123 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 3 LT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 3 LEFT FAIRING PANEL DELAMINATIONS AND DENTS. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001071995063000107NM 1995 6 30 P5CA9500124 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 2 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 RIGHT FAIRING PANEL DELAMINATIONS AND DENTS. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001081995063000108NM 1995 6 30 P5CA9500125 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 2 LT DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 LEFT FAIRING PANEL HAS DELAMINATION AND HOLES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001091995063000109NM 1995 6 30 P5CA9500126 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 1 LT DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 LEFT LOWER FAIRING PANEL DENTS AND DAMAGED. REPAIRED PER SRM 51-40-09. 2L74 4F A20WE 19950630001101995063000110NM 1995 6 30 P5CA9500127 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 1 RT DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 RIGHT LOWER FAIRING PANEL HOLES ON INNER AND OUTER SIDES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001111995063000111NM 1995 6 30 P5CA9500128 119950527A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LOOSE RIVETS ON RIGHT EXTERIOR SURFACE SKIN ON NR 3 PYLON. REPLACED RIVETS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630001121995063000112NM 1995 6 30 P5CA9500129 119950527A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK WITH STOP DRILLED ENDS ON NR 3 PYLON LEFT SURFACE SKIN AT LOWER SPAR APPROXIMATELY NS 255. REPLACED SKIN PANEL. 2L74 4F A20WE 19950630001131995063000113NM 1995 6 30 P5CA9500130 119950527A5400 SPAR BOEING747 747121 1384871NM NR 3 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON LOWER SPAR STRAP NS 222 FIREWALL NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03 FIG 35. 2L74 4F A20WE 19950630001141995063000114NM 1995 6 30 P5CA9500131 119950527A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LOOSE RIVETS ON NR 3 PYLON LEFT SURFACE SKIN. REPLACED RIVETS PER SRM 51-30-02. 2L74 4F A20WE 19950630001151995063000115NM 1995 6 30 P5CA9500132 119950527A5414 SKIN BOEING747 747121 1384871NM NR 3 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON LOWER SPAR LEFT SURFACE SKIN APPROXIMATELY NS 230 NR 3 PYLON. REPAIRED PER BOEING SRM 54-30-03. 2L74 4F A20WE 19950630001161995063000116NM 1995 6 30 P5CA9500133 119950527A5400 SAIL BOAT BOEING747 747121 1384871NM NR 3 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON LOWER SAIL BOAT NS 301 NR 3 PYLON. REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630001171995063000117NM 1995 6 30 P5CA9500134 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 1 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 RIGHT FAIRING PANEL HAS DENTS AND HOLES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001181995063000118NM 1995 6 30 P5CA9500135 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 2 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 RIGHT FORWARD FAIRING PANEL DENTED. REPAIRED PER SRM 51-40-09. 2L74 4F A20WE 19950630001191995063000119NM 1995 6 30 P5CA9500136 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 1 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 RIGHT LOWER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001201995063000120NM 1995 6 30 P5CA9500137 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 10 DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 10 FAIRING PANEL DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001211995063000121NM 1995 6 30 P5CA9500138 119950528A5330 PANEL BOEING747 747121 1384871NM NR 192B DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 PANEL NR 192B DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001221995063000122NM 1995 6 30 P5CA9500139 119950528A5330 PANEL BOEING747 747121 1384871NM NR 192 DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 PANEL NR 192 DENTED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001231995063000123NM 1995 6 30 P5CA9500140 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 6 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 6 RIGHT LOWER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001241995063000124NM 1995 6 30 P5CA9500141 119950528A5330 PANEL BOEING747 747121 1384871NM NR 192A DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 PANEL NR 192A DELAMINATED. REPAIRED PER BOEING 51-40-09. 2L74 4F A20WE 19950630001251995063000125NM 1995 6 30 P5CA9500142 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 6 RT DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 6 RIGHT UPPER FAIRING PANEL DELAMINATED AND DENTED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001261995063000126NM 1995 6 30 P5CA9500143 119950528A5350 FAIRING BOEING747 747121 1384871NM NR 192C DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 192C FAIRING PANEL DENTED ON INNER AND OUTER PANELS. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001271995063000127NM 1995 6 30 P5CA9500144 119950528A5730 PANEL BOEING747 747121 1384871NM RT WING LE PEELED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING INTERIOR OF LEADING EDGE CAVITY LOWER SURFACE PANEL 611DB INBOARD SIDE PART OF HONEYCOMB COVER IS MISSING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001281995063000128NM 1995 6 30 P5CA9500145 119950528A575360B001801 TRACK FITTING BOEING747 747121 1384871NM NR 1 TE FLAP MIGRATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 MIGRATION ON NR 1 TRAILING EDGE FLAP TRACK UNDER WING FITTING. REPAIRED ACCORDING TO BOEING SB 57-2262. 2L74 4F A20WE 19950630001291995063000129NM 1995 6 30 P5CA9500146 119950528A575360B001803 TRACK FITTING BOEING747 747121 1384871NM NR 3 TE FLAP MIGRATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT86895 19648 MIGRATION ON NR 3 FLAP TRACK UNDER WING FITTING. REPAIRED PER BOEING SERVICE BULLETIN 57-2262. 2L74 4F A20WE 19950630001301995063000130NM 1995 6 30 P5CA9500147 119950528A5246 FUEL DOOR BOEING747 747121 1384871NM LT WING DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 PART OF FIBER ON INBOARD SURFACE OF INBOARD FUELING BAY DOOR IS PEELING OFF ON LEFT WING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001311995063000131NM 1995 6 30 P5CA9500148 119950527A5730 SKIN BOEING747 747121 1384871NM LT WING WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 EXPOSED FIBER ON LEFT WING LEADING EDGE LOWER EXTERNAL SKIN, UNDER LANDING LIGHT. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001321995063000132NM 1995 6 30 P5CA9500149 119950527A5754 SKIN BOEING747 747121 1384871NM LT LE FLAPS DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TOP EDGES OF EACH LEFT WING LEADING EDGE FLAP NR 1 TO NR 10 ARE DAMAGED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001331995063000133NM 1995 6 30 P5CA9500150 119950527A5730 PANEL BOEING747 747121 1384871NM LT WING PEELING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 THE MICARTA STRIP ON LEFT WING TRAILING EDGE LOWER SURFACE OF TOP FIXED PANEL, NEST TO NR 1 SPOILER IS PEELING OFF. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630001341995063000134EU 1995 6 30 QXEA9500190 119950621A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 GEG - THREE OVERHEAD EMERGENCY LIGHTS INOP. BULBS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950630001351995063000135NM 1995 6 30 SCNA95135 119950620A3350900835A EEL BATTERY PACK BOEING727 727259 138408JNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 FOUND THE R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, SIGN TESTED GOOD PER MM 33-50-71. 2L73 4F A3WE 19950630001471995063000147WP 1995 6 30 9509739944 119950616A5320 PRESS PANEL DOUG DC9 DC931 3022065WP FS 83 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WELL PRESSURE PANEL, FS 83 AT THE RIGHT OUTBOARD SIDE FITTING. REPAIRED PER EO 5310-01134. 2L72 4F A6WE 19950630001481995063000148WP 1995 6 30 9509749944 119950618A5210 FITTING DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A 2 INCH CRACK IN THE AFT ENTRY DOOR NR 3 BEAM END FITTING, LEFT SIDE. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950630001491995063000149WP 1995 6 30 9509759944 119950620A5312 BULKHEAD DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A CRACK IN THE DOOR JAMB TO AFT PRESSURE BULKHEAD ATTACH FITTING, LEFT SIDE JUST ABOVE THE THIRD HORIZONTAL BEAM. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950630001501995063000150WP 1995 6 30 9509769609 119950621A5320 FITTING DOUG DC9 DC932 3022066WP FS 699 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 3 INCH CRACK IN THE FS 699 FRAME FITTING JUST BELOW THE FLOOR LEVEL, LEFT SIDE. REPLACED FITTING PER SRM 51-30-02. 2L72 4F A6WE 19950630001511995063000151WP 1995 6 30 9509779971 119950620A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19950630001521995063000152WP 1995 6 30 9509789966 119950620A5350 PINS DOUG DC9 DC931 3022065WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL019330 47138 DURING LINE CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP. REPLACED 5 WORN PINS AND CLEANED THE SEAL, CHECKED OK. 2L72 4F A6WE 19950630001531995063000153NM 1995 6 30 9509792280 119950616A5270 SWITCH BOEING727 727251 138408HNM AFT CARGO DOOR LOOSE A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01280US 21159 DURING TAKEOFF ROLL DTW-BOS FLT 382, AFT CARGO DOOR LIGHT ILLUMINATED, ABORTED TAKEOFF WITHOUT INCIDENT. FOUND JAMB NUT LOOSE ON THE SWITCH. ADJUSTED SWITCH, CHECKED OK. 2L73 4F A3WE 19950630001541995063000154EU 1995 6 30 9509803238 219950624A7200 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 MALFUNCTIONED A ANWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01338NW 03238 31709 DURING ROTATION, AIRCRAFT YAWED TO THE LEFT ACCOMPANIED BY A LOUD AIR NOISE AND VIBRATION FELT IN THE COCKPIT. NO MESSAGES WERE INDICATED ON ECAM OR STATUS PAGE. OPERATING PROCEDURE WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SEA WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE NR 1 ENGINE WAS REPLACED. 2L72 4F4 FRTA28NM 19950630001551995063000155NM 1995 6 30 9509812255 119950624A2934EA1093A2408 QUANTITY TRANS BOEING727 727251 138408HNM A HYD SYST FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01255US 19974 EN ROUTE TO YUL, A-SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.0 GALLON DURING GEAR/FLAP RETRACTION. AFTER RETRACTION WAS COMPLETED, QUANTITY INDICATED 1.5 GALLONS. FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A-SYSTEM QUANTITY TRANSMITTER AND SERVICED TO 4.2 GALLONS. LEAK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950630001561995063000156 1995 6 30 9509822287 419950623A344220709430201 RADAR INDICATOR BOEING727 727251 138408HNM FLIGHT DECK FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 GL01287US 21375 EN ROUTE TO MCO, WEATHER RADAR INDICATOR CIRCUIT BREAKER POPPED. ATTEMPTED ONE RESET TO NO AVAIL. FLIGHT JETTISONED 16,600 LBS OF FUEL AND RETURNED TO DTW. MAINTENANCE REPLACED INDICATOR, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950630001571995063000157EA 1995 6 30 COM60504 119950623A274283963 TRIM ACT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SO01940CA1828 7048 STABILIZER TRIM CHANNEL 1 INOP MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2L72 4F RTA21EA 19950630001581995063000158EA 1995 6 30 COM60505 119950622A322016410101 DRAG BRACE CNDAIRCL600 CL6002B19 EA NLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01926CA4139 7027 HYDRAULIC LEAK NOSE LANDING GEAR. REPLACED THE NLG DRAG BRACE. 2L72 4F RTA21EA 19950630001591995063000159EA 1995 6 30 COM60506 119950622A3240 BRAKE CNDAIRCL600 CL6002B19 EA RT MLG SMOKING A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01940CA 7048 RT MLG INBD BRAKE SMOKING. CLEANED AND INSPECTED BRAKE ASSEMBLY, NO DEFECTS FOUND. AIRCRFT CONTINUED SERVICE. 2L72 4F RTA21EA 19950630001601995063000160EA 1995 6 30 COM60507 119950622A3820 WATER HEATER CNDAIRCL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMAK NONE M OVER TEMP TXTAXI/GRND HDL 1 SO01934CA 7042 CARGO COMPARTMENT BULKHEAD VERY HOT TO TOUCH. FOUND LAVATORY WATER HEATER OVERHEATING. DISABLED WATER HEATER AND PLACED ON DEFERRED MAINTENANCE LIST. 2L72 4F RTA21EA 19950630001611995063000161 1995 6 30 MWEA95222 419950622A2565 CABLE DOUG DC9 DC932 3022066WP ESCAPE SLIDE DETACHED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31203ME 47673 CREW REPORTS, GALLEY SERVICE DOOR GIRT BAR ATTACH CABLE CAME UNATTACHED. MAINTENANCE REATTACHED GIRT BAR CABLE, REINSTALLED SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950630001621995063000162WP 1995 6 30 MWEA95223 119950625A3350100865 EEL BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 CREW REPORTS, THE AFT HALF OF EMERGENCY FLOOR TRACK LIGHTS CAME ON AT GATE WITH SWITCH IN ARM POSITION. MAINTENANCE REMOVED AND REPLACED AFT BATTERY PACK. OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950630001631995063000163EU 1995 6 30 QXEA9500186 119950619A495038075412 APU FOKKERF28 F28MK1000 4990808EU AFT FUSELAGE SMOKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09450US2368430 11101 PDX - APU CAUSING SMOKE IN CABIN AND COCKPIT. APU REPLACED IAW MAINT MANUAL. APU OPS CHECKED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950630001641995063000164NM 1995 6 30 SWAA950474 119950620A5330 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07341SW 24091 DURING SCHEDULED TERM CHECK, FOUND A 1.7 FUSELAGE SKIN CRACK AT S23R, BS 727D AND AT S23R, MEASURING 1.6 LONG. REPAIRED BOTH PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950630001651995063000165NM 1995 6 30 SWAA950475 119950620A5330 SKIN BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED A CHECK, FOUND A 1.8 CRACK AT NOSE WHEEL WELL VERTICAL WEB RIGHT SIDE BELOW FWD ACCESS PANEL CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001661995063000166NM 1995 6 30 SWAA950476 119950620A5320 WEB BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED A-CHECK, FOUND NOSE GEAR RETACT ACTUATOR SUPPORT VERT WEB CRACKED AT RADIUS. REPLACED WEB PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001671995063000167NM 1995 6 30 SWAA950477 119950620A5330 SKIN BOEING737 7372H4 138448CNM BS 320 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW0760SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGE AT BS 320 AND S20R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001681995063000168NM 1995 6 30 SWAA950478 119950620A5320 WEB BOEING737 7372H4 138448CNM BS 344 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW0760SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND WEB AND FAILSAFE CHORD DAMAGE AT BS 344 AND S21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001691995063000169NM 1995 6 30 SWAA950479 119950620A5311 BELTFRAME BOEING737 7372H4 138448CNM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0760SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND BELTFRAME CRACKED 17 BELOW FLOORBEAM AT BS 328, RIGHT SIDE BETWEEN S20 AND 21R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001701995063000170NM 1995 6 30 SWAA950480 119950620A5313 STRINGER BOEING737 7372T4 1384492NM BS 907 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 27R CORRODED AT FWD END AT BS 907. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001711995063000171NM 1995 6 30 SWAA950481 119950620A5320 WEB BOEING737 7372T4 1384492NM BS 492 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY AFT CORNER WEB DAMGED AT L/E LOWER CORNER BS 492. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001721995063000172NM 1995 6 30 SWAA950482 119950620A5320 WEB BOEING737 7372T4 1384492NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOORBEAM ATTACH POINT AT BS 360 AND BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001731995063000173NM 1995 6 30 SWAA950483 119950620A5320 WEB BOEING737 7372T4 1384492NM BS 599 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT SIDE WEB CRACKED .5 AT FLANGE TO FUSELAGE SKIN, FLOOR LEVEL, BS 599. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630001741995063000174NM 1995 6 30 UPS203664 119950622A531565C1191217 FLOORBEAM BOEING727 72751C 1384015NM BS 940 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON FLOORBEAM ATTACH FLANGE NEAR BS 940. REPAIRED IAW B727-5310-5596. 2L73 4F A3WE 19950630001751995063000175NM 1995 6 30 UPS203682 119950623A5753 SKIN BOEING727 72725C 138400HNM TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 19717 WHILE ON GROUND, MAINTENANCE FOUND FLAP DELAMINATED AT RT, O/B TRAILING EDGE. REPAIRED IAW B727-5750-3081C. 2L73 4F A3WE 19950630001761995063000176WP 1995 6 30 UPS803665 119950623A5711 SPAR DOUG DC8 DC871F 302199DWP LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT WING LOWER AFT SPAR CAP. REPAIRED IAW SRM 57-10-0, 51-1-20D. 2L74 4F RT4A25 19950630001771995063000177WP 1995 6 30 UPS803666 119950623A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP BS 80 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON BOTTOM END OF COCKPIT SUB FLOOR AT STA 80 LBL 56, VERTICAL INTERCOSTAL. REPAIRED IAW SRM 53-3-1, 51-1-20D. 2L74 4F RT4A25 19950630001781995063000178WP 1995 6 30 UPS803667 119950623A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1406-1324 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND INNER DOUBLER FROM PREVIOUS REPAIR AT STA 1306 TO 1324 BETWEEN LONGS 24L TO 25L DAMAGED. REPAIRED IAW SRM 51-1-8. 2L74 4F RT4A25 19950630001791995063000179WP 1995 6 30 UPS803668 119950623A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1399 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON AFT LOWER CARGO SKIN UNDER FINGER DOUBLER AT STA 1399 BETWEEN LONGS 30L TO 31L. REPAIRED IAW SRM 53-3-1, 51-1-8, 51-1-20, 51-1-11. 2L74 4F RT4A25 19950630001801995063000180WP 1995 6 30 UPS803669 119950623A5712 RIB DOUG DC8 DC871F 302199DWP WS 416.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING RIB CHAFED AT STA SFX 416.5. REPAIRED IAW SRM 51-2-0, 57-2-0. 2L74 4F RT4A25 19950630001811995063000181WP 1995 6 30 UPS803670 119950623A532047533602 FITTING DOUG DC8 DC871F 302199DWP BS 822 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON TIE FITTING HAS LARGE CRACK AT STA 822, LONG 21R. REPAIRED IAW SRM 51-1-20. 2L74 4F RT4A25 19950630001821995063000182WP 1995 6 30 UPS803671 119950623A5320 ANGLE DOUG DC8 DC871F 302199DWP LT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK AROUND RADIUS OF ANGLE LT W/W O/B AFT FORWARD OF FLAP. REPAIRED IAW SRM 53-2-0, 51-1-21, 51-1-20D. 2L74 4F RT4A25 19950630001831995063000183WP 1995 6 30 UPS803672 119950623A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 26L AT FS 1350. REPAIRED IAW SRM 51-1-20D, 53-4-1, 53-1-0. 2L74 4F RT4A25 19950630001841995063000184WP 1995 6 30 UPS803673 119950623A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1010 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CARGO COMPARTMENT NR 3 PIT, RT STA 1010 SUP EXTRUSION LONGERON 21. REPAIRED IAW SRM 55-2-5, 51-1-20D, 53-2-0. 2L74 4F RT4A25 19950630001851995063000185WP 1995 6 30 UPS803674 119950623A5330 SKIN DOUG DC8 DC871F 302199DWP BS 400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SKIN IN FWD LOWER CARGO STA 400 BETWEEN LONGS 36 AND 35L. REPAIRED IAW SRM 53-2-1. 2L74 4F RT4A25 19950630001861995063000186WP 1995 6 30 UPS803675 119950623A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1879-1890 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKS ON FRAMES INSIDE ACCESS DOOR NR 62 STA 1870 TO 1890. REPAIRED IAW SRM 53-2-0, 53-2-5. 2L74 4F RT4A25 19950630001871995063000187WP 1995 6 30 UPS803676 119950623A5320 FLANGE DOUG DC8 DC871F 302199DWP BS 258 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO HORIZ FLANGE CRACKED AT STA 258, LONG 35L. REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19950630001881995063000188WP 1995 6 30 UPS803677 119950623A5330 SKIN DOUG DC8 DC871F 302199DWP BS 218-222 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO INNER SKIN/DOUBLER CORRODED STA 218 TO 222, LONGS 36 AND 35L. REPAIRED IAW SRM 51-2-2, 53-2-0. 2L74 4F RT4A25 19950630001891995063000189WP 1995 6 30 UPS803678 119950623A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 193 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD LWR CARGO LT LOWER FLANGE OF LONGERON 35R AT STA 193. REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19950630001901995063000190WP 1995 6 30 UPS803679 119950623A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP BS 1000-1020 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND INTERCOSTAL BELOW WINDOW PLUG LT SIDE STA 1000 TO 1020 CORRODED. REPAIRED IAW SRM 53-4-1, 51-1-21. 2L74 4F RT4A25 19950630001911995063000191WP 1995 6 30 UPS803680 119950623A5320 SPLICE FITTING DOUG DC8 DC871F 302199DWP BS 1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 25L SPLICE FITTING AT STA 1350 CORRODED. REPAIRED IAW SRM 53-4-1, 51-1-20D. 2L74 4F RT4A25 19950630001921995063000192WP 1995 6 30 UPS803681 119950623A5542 SKIN DOUG DC8 DC871F 302199DWP RUDDER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RUDDER SKIN RT SIDE STA 2283 DAMAGED. REPAIRED IAW SRM 55-2-0, 51-1-21A. 2L74 4F RT4A25 19950630001931995063000193WP 1995 6 30 UPS803683 119950626A5313 LONGERON DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE ON GROUND, MAINTENANCE FOUND CRACK ON LONGERON 24. REPAIRED IAW DC8-5310-6259. 2L74 4F RT4A25 19950630001941995063000194WP 1995 6 30 95ZZZX3172 119950609A5414 PLANK DOUG DC8 DC862F 3021972WP NR 1 PYLON CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15997CF 46154 KDAY/KMEM - FLT 040 - DURING SERVICE CHECK, MAINTENANCE FOUND THE NR 1 PYLON INTERMEDIATE SIDE PLANK CRACKED AT STA YN 226. THE AIRCRAFT WAS FERRIED TO KMCN TO FACILITATE PERMANENT REPAIRS. SD - ZANTOP MAINTENANCE REMOVED SIDE PLANK TO FACILITATE REPAIR. REPAIRED AND INSTALLED INTERMEDIATE SIDE PLANK IAW SRM 54-2-1 AND SRM 51-3-0. (X) 2L74 4F 4A25 19950630001951995063000195WP 1995 6 30 95ZZZX3173 119950521A3231 UPLATCH DOUG DC8 DC871 302199AWP MLG DOOR LACK OF LUBE A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP158084U 45974 KPHX/KDFW - FLT 298 - THE MLG DOOR NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION. THE FLIGHT CREW RECYCLED THE LANDING GEAR AND THE LIGHT DID NOT EXTINGUISH. MAINTENANCE CLEANED AND LUBED THE RT UPLATCH MECHANISM. AN OPERATIONAL CHECK OF THE LANDING GEAR WARNING SYSTEM WAS GOOD. 2L74 4F 4A25 19950630001961995063000196WP 1995 6 30 95ZZZX3174 119950523A3231 UPLATCH DOUG DC8 DC863 302198AWP MLG DOOR LACK OF LUBE A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15797AL 46163 KLRD/KDAY - FLT 529 - THE MLG DOOR NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE LIGHT EXTINGUISHED NORMALLY. MAINTENANCE CLEANED AND LUBED THE UPLATCH OVER-CENTER MECHANISM. AN OPERATIONAL CHECK OF THE LANDING GEAR WARNING SYSTEM WAS GOOD. 2L74 4F 4A25 19950630001971995063000197WP 1995 6 30 95ZZZX3175 119950528A2612 CONNECTOR DOUG DC8 DC873F 302199FWP NR 3 ENGINE SHORTED A RRXAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP15792FT 46046 PHNL/NZAA - FLT 6981 - DURING CRUISE, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND WARNING BELL SOUNDED, ACCOMPLISHED ENGINE FIRE OR DAMAGE CHECK LIST. BOTH FIRE BOTTLES FIRED. NR 3 ENGINE FIRE WARNING ILLUMINATED INTERMITTENTLY THROUGH THE REMAINDER OF THE FLIGHT. MAINTENANCE FOUND A FIRE LOOP CONNECTOR SHORTED TO GROUND. MAINTENANCE REPAIRED SHORTED CONNECTOR AND AN OPERATIONAL TEST OF THE NR 3 ENGINE FIRE WARNING SYSTEM WAS GOOD. (X) 2L74 4F RT4A25 19950630001981995063000198NE 1995 6 30 95ZZZX3176 219950602A7200 ENGINE BOEING747 747130 1384880NM PWA JT9 JT9D7A 52054NE NR 1 DAMAGED A TWRAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 EA15603FF 19746 DURING CLIMB, NR 1 ENGINE SHUT DOWN DUE TO HEAVY STALL EGT RISE TO 920 DEGREES. THREE ENGINE FERRY TO JFK, REMOVED AND REPLACED NR 1 ENGINE. 2L74 4F4 F A20WE E20EA 19950630001991995063000199NM 1995 6 30 95ZZZX3177 119950604A521080330033 ASSIST BOTTLE BOEING747 747136 1384883NM CABIN DOOR DEPLETED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15605FF 20271 DURING MAINTENANCE SERVICE FOUND R1 MAIN ENTRY DOOR ASSIST BOTTLE DEPLETED. REPLACED R1 MAIN ENTRY DOOR BOTTLE. 2L74 4F A20WE 19950630002001995063000200WP 1995 6 30 95ZZZX3178 119950605A5730 PLATING DOUG DC8 DC863F 302198FWP WS 257 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 ON A ROUTINE 'A' CHECK, MAINTENANCE FOUND LEVEL 3 CORROSION AT APPROXIMATELY L/E STA XFS 257 TOP SIDE, LEFT WING. 2L74 4F 4A25 19950630002011995063000201WP 1995 6 30 95ZZZX3179 119950529A33505708458503600 EEL BATTERY PACK DOUG DC8 DC863F 302198FWP CABIN DISCHARGED A AWRAK NONE L NO TEST ININSP/MAINT 1 WP25441J 45988 EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. SYSTEM OPS CHECK NORMAL IAW DC-8 MM 33-50-00. 2L74 4F 4A25 19950630002021995063000202WP 1995 6 30 95ZZZX3180 119950611A326092743643 RELAY DOUG DC9 DC931 3022065WP LANDING GEAR MALFUNCTIONED A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE05985Z 47491 MCI - FLT 117 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND GREEN LIGHT CAME ON. REPLACED LANDING GEAR LEVER RELAY R2-28, MFG PN 9274-3643. NLG OPERATION AND INDICATION CHECKED NORMAL. CHECK C - 3-1-95 - STL. 2L72 4F A6WE 19950630002031995063000203WP 1995 6 30 95ZZZX3181 119950610A3260H146 DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP NLG FAILED A TWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 CE05985Z 47491 STL - FLT 631 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG GREEN LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND SWAPPED LIGHT BULBS. ON SECOND APPROACH, GREEN LIGHT CAME ON. REPLACED NLG DOWNLOCK SWITCH, MFG H14-6. NLG INDICATION AND OPERATION CHECKED NORMAL. CHECK C - 3-1-95 - STL. 2L72 4F A6WE 19950630002041995063000204NE 1995 6 30 95ZZZX3182 219950609A7200 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 FAILED A TWAAE ENGINE SHUTDOWN JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 CE0511003 193B1015 STL - FLT 324 - AFTER TAKEOFF, SHUT DOWN NR 2 ENGINE, SN 4468, DUE TO HIGH AVM ON BOTH A AND B VIBRATION CHANNELS. CHECKED OIL SYSTEM CHIP DETECTORS, LUBRICATED FAN BLADES; PERFORMED FAN TRIM BALANCE. ENIGNE OPERATION CHECKED NORMAL. CHECK C-9B - 2-1-95 - JFK. 2L73 4F4 F A23WE A12EU 19950630002051995063000205NE 1995 6 30 95ZZZX3183 219950613A7230804509 NR 3 BEARING BOEING727 727231 1384079NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE FAILED A TWAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE0554332 20310 ONT - FLT 54 - RETURNED FROM FLIGHT ACCOUNT NR 3 ENGINE OIL BYPASS LIGHT CAME ON AND OIL TEMPERATURE ROSE. FOUND METAL IN MAIN OIL SCREEN. REPLACED ENGINE SN 1543. ENGINE TOTAL TIME: 34,195 HOURS; 22,195 CYCLES. CHECK C-2 - 1-4-95 - MCI. INVESTIGATION INTO NR 3 ENGINE, SN 1543, OIL BYPASS LIGHT ILLUMINATING AND OIL TEMPERATURE RISE, REVEALED NR 3 BEARING, MFG P/N 804509, FAILED. REPLACED NR 3 BEARING AND REPAIRED RELATED COMPONENTS. ENGINE S/N 1543 REPAIRED AND RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950630002061995063000206WP 1995 6 30 95ZZZX3184 119950614A3297G216B24 WIRE DOUG DC9 DC931 3022065WP NLG INDICATION FAILED A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE05985Z 47491 ORF - FLT 694 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR GREEN, DOWN, AND LOCKED LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR. FOUND WIRE, C216B24, WITH HIGH RESISTANCE AND INTERMITTENTLY OPEN. REPLACED WIRE, G216B24, BETWEEN CONNECTOR P1-133 PIN 6 AND S3-49 TERMINAL STRIP. NOSE LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL. CHECK C - 3-1-95 - STL. 2L72 4F A6WE 19950630002071995063000207WP 1995 6 30 95ZZZX3185 119950605A5730 L/E SKIN DOUG DC8 DC863F 302198FWP WS 207 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 ON A ROUTINE A-CHECK, MAINTENANCE FOUND .6250 INCH CRACK AT APPROXIMATELY L/E STATION XFS 207 TOP SIDE, LEFT WING. 2L74 4F 4A25 19950630002081995063000208WP 1995 6 30 95ZZZX3186 119950609A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION/FLOOR BEAM AT FS 901 RBL 13 HAS SURFACE CORROSION. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950630002091995063000209WP 1995 6 30 95ZZZX3187 119950609A5315 FLOOR BEAM LKHEED1011 10113851 5265010WP FS 901 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION/FLOOR BEAM AT FS 901 RBL 7 HAS CORROSION. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED REPAIR PER SRM 53-21-00. 2L73 4F A23WE 19950630002101995063000210WP 1995 6 30 95ZZZX3188 119950601A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1625 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION/C-2 COMPARTMENT AFT BULKHEAD COMPARTMENT FS 1625 FLOOR ANGLE SUPPORT IS CORRODED FROM END TO END. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-50-02. 2L73 4F A23WE 19950630002111995063000211WP 1995 6 30 95ZZZX3189 119950605A5320 ANGLE LKHEED1011 10113851 5265010WP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION/BOTTOM OF FUSELAGE FILLET PANEL 194A HAS CORROSION AT ATTACH ANGLE. REMOVED DAMAGE, TREATED AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 51-50-04. 2L73 4F A23WE 19950630002121995063000212NE 1995 6 30 95ZZZX3190 219950606A73207436025 FCU DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE CONTAMINATED A Y2PACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL23197US 391 47154 P654600 DTW - ABORTED TAKEOFF. NR 1 ENGINE WOULD NOT REACH TAKEOFF E.P.R. DRAINED F.C.U. MOISTURE TRAP, CLEANED VENT HOLE. ENGINE IS A LOANER, SCHEDULED FOR REMOVAL 6-7-95. ENGINE OWNER NOTIFIED OF CONDITION. REF: OPERATOR CONTROL NR Y2PA95006. 2L72 4F4 F A6WE E2EA 19950630002131995063000213WP 1995 6 30 CKSA95035 119950601A3260BAN35A BOLT DOUG DC8 DC861 3021952WP NOSE GEAR LOOSE A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL2324UA 42169 45963 RDU - NOSE GEAR DOWN WARNING LIGHT INTERMITTENT, CYCLED GEAR, WARNING LIGHT REMAINS INTERMITTENT. TIGHTENED LOOSE ATTACHING HARDWARE. OPS CHECK GOOD ON GROUND. INSPECTED AND FOUND NO DEFECTS PER DC-8, MM 32-60-0. (X) 2L74 4F 4A25 19950630002141995063000214NM 1995 6 30 IXKA9500019 119950612A2197 WIRE BOEING727 727251 138408HNM CONTROL VALVE BROKEN A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25264US 19983 EWR/TPA - FLT 39, AFTER TAKEOFF, UNABLE TO PRESSURIZE AIRCRAFT. AIRCRAFT RETURNED TO EWR. FOUND LT FLOW CONTROL VALVE FAILED IN CLOSED POSITION DUE TO 3 BROKEN WIRES. REPAIRED WIRES AND C/P REPINNED. PRESSURE CHECKED PER MM 21-00-01 AND MM 21-31-00. OPS CHECK NORMAL. (X) 2L73 4F A3WE 19950630002151995063000215NM 1995 6 30 MALA954472 119950523A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15853MA 353 MSP - FLT 3263 - DURING POST-FLIGHT IN MSP, THE CREW REPORTED THE OVERHEAD EMERGENCY LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002161995063000216SW 1995 6 30 MALA954473 119950525A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LEFT INBOARD LOWER WING TO NACELLE ANGLE PN 27-35112 FORWARD END, AT APPROXIMATE STA 115.00 CRACKED APPROXIMATELY 1 INCH IN RADIUS AND HAS AN ELONGATED RIVET HOLE. FABRICATED AND INSTALLED NEW ANGLE PN 27-35112. ALSO, INCORPORATED FAIRCHILD ARP 54-20-9101 REPAIR ANGLE, DATED JAN 15/91. ALL WORK PERFORMED IAW FAIRCHILD SRM 51-00-00, PAGE 4, 51-30-00, AND 51-40-00. (X) 1L72 4T A8SW 19950630002171995063000217SW 1995 6 30 MALA954474 119950525A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING PHASE INSPECTION IN MSP, MAINTENANCE FOUND LT INBOARD UPPER WING TO NACELLE ANGLE PN 27-335112 FORWARD END AT STA 115.00 CRACKED APPROXIMATELY 1 INCH IN RADIUS. FABRICATED AND INSTALLED NEW ANGLE IAW FAIRCHILD SRM 51-00-00, PAGE 4, 51-30-00, AND 51-40-00. (X) 1L72 4T A8SW 19950630002181995063000218SW 1995 6 30 MALA954475 119950527A52102724089005 SEAL SWRNGNSA227 SA227AC 8780603SW CABIN DOOR LEAKING A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL1526906 AC654B MSP - FLT 3222 - IN CRUISE FLIGHT FROM MSP, A SQUEALING NOISE WAS NOTED COMING FROM THE CABIN DOOR. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE DOOR SEAL. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002191995063000219NM 1995 6 30 MALA954476 119950528A3040 WIPER BLADE DHAV DHC8 DHC8102 2809003NM WINDSHIELD LOOSE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15849MA 347 DTW - FLT 3092 - ON CLIMB-OUT FROM DTW, THE CAPTAIN'S WINDSHIELD WIPER PULLED AWAY FROM THE WINDSHIELD. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE RESECURED THE WIPER ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002201995063000220 1995 6 30 MALA954477 419950528A3418 COMPUTER SWRNGNSA227 SA227AC 8780603SW STALL WARNING FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15423MA AC636 MSP - FLT 3352 - ON CLIMB-OUT FROM MSP, THE GEAR WARNING HORN BEGAN TO SOUND. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, MAINTENANCE REPLACED THE SAS COMPUTER. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950630002211995063000221SW 1995 6 30 MALA954478 119950529A3260V31 SWITCH SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15423MA AC636 MSP - FLT 3218 - ON CLIMB-OUT FROM MSP, THE GEAR WARNING HORN SOUNDED. THE WARNING HORN CONTINUED TO SOUND UNTIL THE GEAR WAS SELECTED DOWN. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED A MICROSWITCH AT THE RIGHT POWER LEVER. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002221995063000222SW 1995 6 30 MALA954479 119950531A6120 LINKAGE SWRNGNSA227 SA227AC 8780603SW PROP GOVERNOR DIRTY A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15426MA AC645 MSP - FLT 3327- IN CRUISE FLIGHT, THE ENGINE RPM DID NOT RESPOND TO POWER LEVER MOVEMENT. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE PROP GOVERNOR LINKAGE. THE PROBLEM COULD NOT BE DUPLICATED DURING GROUND RUNS. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (X) 1L72 4T A8SW 19950630002231995063000223 1995 6 30 MALA954480 419950601A341628702502 ALTIMETER SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15424MA AC639 DTW - FLT 3092 - ON CLIMB-OUT OF DTW, CAPTAIN'S ALTIMETER FLAGGED INTERMITTENTLY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 ALTIMETER. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002241995063000224SW 1995 6 30 MALA954481 119950601A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER O OTHER APAPPROACH 1 GL15424MA AC639 DTW - FLT 3092 - ON APPROACH TO DTW, THE RIGHT RED GEAR INTRANSIT LIGHT WAS DIM DURING THE GEAR EXTENSION. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED THE RIGHT GEAR POSITION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002251995063000225 1995 6 30 MALA954482 419950602A3442071131900 RT UNIT DHAV DHC8 DHC8102 2809003NM RADAR INTERNAL FAULT A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15802MA 245 DTW - FLT 3319 - ON CLIMB-OUT FROM DTW, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RADAR R/T. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002261995063000226NM 1995 6 30 MALA954483 119950602A33506101781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15822MA 326 DTW - FLT 3066 - DURING PRE-FLIGHT IN DTW, CREW FOUND AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED EVACUATION LIGHT BATTERY PACK AT THE AFT RIGHT CABIN CEILING POSITION. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002271995063000227NM 1995 6 30 MALA954484 119950602A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15848MA 346 DTW - DURING A MAINTENANCE WALKAROUND, THE EMERGENCY EXIT LIGHT OVER THE PASSENGER DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EVACUATION LIGHT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002281995063000228SW 1995 6 30 MALA954485 119950604A57122731240 RIB SWRNGNSA227 SA227AC 8780603SW WS 51 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 MSP - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT WING RIB CRACKED AT THE HYDRAULIC LINE FITTING AT WS 51. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC SRM 57-90-10. (X) 1L72 4T A8SW 19950630002291995063000229SW 1995 6 30 MALA954486 119950604A57532736004 RIB SWRNGNSA227 SA227AC 8780603SW TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 MSP - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP OUTBOARD NOSE END RIB CRACKED AT WS 171.00. REPAIRS WERE COMPLETED BY REPLACING THE OUTBOARD NOSE END RIB, PN 27-36004, IAW FAC SRM 57-90-60. (X) 1L72 4T A8SW 19950630002301995063000230SW 1995 6 30 MALA954487 119950603A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG INTERNAL FAULT A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL1526906 AC654B MSP - FLT 3201 - ON APPROACH TO MSP, THE NOSE GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING THE GEAR EXTENSION. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE NOSE GEAR UP POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002311995063000231SW 1995 6 30 MALA954488 119950605A242051509002B GCU SWRNGNSA227 SA227AC 8780603SW LT ENGINE FAILED A MALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 GL1527465 AC755B MSP/YQT - FLT 3084 - IN CRUISE FLIGHT TO YQT, THE LEFT GENERATOR FAIL LIGHT ILLUMINATED. THE CREW WAS UNABLE TO RESET THE GENERATOR. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT GENERATOR CONTROL UNIT. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002321995063000232SW 1995 6 30 MALA954489 119950607A5330 SKIN SWRNGNSA227 SA227AC 8780603SW FS 422.27 DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND A SMALL DENT IN THE LEFT SIDE OF THE FUSELAGE FORWARD OF THE REAR CARGO DOOR AT FS 422.27 AND STR 11. REPAIRS COMPLETED BY INSTALLING A REPAIR DOUBLER AND FILLER PIECE IAW FAC SRM 51-90-04, REPAIR NR 2. (X) 1L72 4T A8SW 19950630002331995063000233SW 1995 6 30 MALA954491 119950607A53112722093105 FRAME SWRNGNSA227 SA227AC 8780603SW FS 189.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 MSP - DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .125 INCH CRACK AT RELIEF RADIUS IN LOWER BELT FRAME OF CONSTANT SECTION AT FS 189.06, LT SIDE, PN 27-22093-105. REPAIRED BY INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20, REPAIR NR 19. (X) 1L72 4T A8SW 19950630002341995063000234NM 1995 6 30 MALA954495 119950607A291082970010141 HYD LINE DHAV DHC8 DHC8102 2809003NM LT NACELLE CRACKED A MALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15865MA 364 DFW/MQT - FLT 3187 - IN CRUISE FLIGHT TO MQT, THE CREW NOTED A SLOW LEAK DOWN OF THE NR 1 HYDRAULIC SYSTEM. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED A CRACKED FLARE ON THE HYDRAULIC LINE FROM THE LEFT MANIFOLD TO THE ANTI-SKID CONTROL VALVE. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950630002351995063000235SW 1995 6 30 MALA954497 119950606A32502782529041 FEED BACK POT SWRNGNSA227 SA227AC 8780603SW NLG STEERING FAILED A MALAO OTHER O OTHER LDLANDING 1 GL15430MA AC710 DTW - FLT 3186 - DURING LANDING AT DTW, AIRCRAFT PROCEEDED LEFT UNCOMMANDED WHEN NOSE WHEEL STEERING WAS ENGAGED. MAINTENANCE REPLACED THE NOSE WHEEL STEERING FEEDBACK POT MOUNT ASSEMBLY. THE SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002361995063000236SW 1995 6 30 MALA954499 119950608A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL15424MA AC639 CVG/DTW - FLT 3409 - DURING DEPARTURE FROM CVG, RT MLG INTRANSIT LIGHT DID NOT ILLUMINATE WHEN LANDING GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED THE LANDING GEAR INTRANSIT MICROSWITCH. THE SYSTEM FUNCTIONED SATISFACTORILY. (X) 1L72 4T A8SW 19950630002371995063000237SW 1995 6 30 MALA954500 119950608A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW RT WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE RT LOWER WING TO NACELLE TRANSIT ANGLE WAS CRACKED AT THE LEADING EDGE. MAINTENANCE REPLACED THE FORWARD 8 INCH SEGMENT AND APPLIED A DOUBLER IAW FAIRCHILD ARP 54-20-9101. (X) 1L72 4T A8SW 19950630002381995063000238EU 1995 6 30 VTZA95191 119950611A3246AHA1837 WHEEL ASSY JETAIRJETSTMJETSTM4101 1500501EU NR 4 MLG CRACKED A VTZAK NONE O OTHER LDLANDING 1 EA27313UE 41026 RIC/IAD - FLT 6225 - DURING LANDING EXPERIENCED A FLAT ON THE NR 4 MAIN TIRE. AIRCRAFT TAXIED TO GATE WITH NO FURTHER INCIDENTS. UPON FURTHER INSPECTION, MAINTENANCE FOUND 4 THROUGH-BOLTS ON THE NR 4 MAIN WHEEL ASSY CRACKED AND CAUSED TIRE TO LOSE PRESSURE. MAINTENANCE REPLACED THE MAIN WHEEL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950630002391995063000239NE 1995 6 30 Y2PA95006 219950606A7261MOBILE254 OIL DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE CONTAMINATED A Y2PACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL23197US 47154 P654600 DTW - ABORTED TAKEOFF. NR 1 ENGINE OIL CLOGGED LIGHT ILLUMINATED. REMOVED OIL FILTER, FOUND CARBON IN FILTER, DRAINED AND RESERVICED OIL TANK. REPLACED FILTER. REF: OPERATOR CONTROL NR 95ZZZX3190. (X) 2L72 4F4 F A6WE E2EA 19950630002401995063000240WP 1995 6 30 9409949982 119950507A5330 SKIN DOUG DC9 DC932 3022066WP FS 750 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01982US 45790 DURING PERIODIC CHECK, FOUND CORROSION AND PUNCTURE IN THE FUSELAGE SKIN FS 750 BETWEEN LONGERON 29L AND 30. REPAIRED PER EA 99-94860. 2L72 4F A6WE 19950630002411995063000241WP 1995 6 30 9509839993 119950503A5330 SKIN DOUG DC9 DC931 3022065WP EXT PWR PANEL CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO CRACKS IN THE EXTERNAL POWER PANEL NEAR THE UPPER GROUND STUD HOLE. REPAIRED PANEL PER EA 99-93520. 2L72 4F A6WE 19950630002421995063000242WP 1995 6 30 9509849993 119950504A5320 JAMB DOUG DC9 DC931 3022065WP CABIN DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO CRACKS IN THE MAIN CABIN DOOR JAMB UPPER FORWARD CORNER AND IN THE TITANIUM SKIN DOUBLER. REPAIRED BOTH PER EA 99-93545. 2L72 4F A6WE 19950630002431995063000243WP 1995 6 30 9509859993 119950505A5311 FORMER DOUG DC9 DC931 3022065WP FS 1019 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 1019 FORMER BETWEEN LONGERONS 15L AND 16L. REPAIRED PER EA 99-92194. 2L72 4F A6WE 19950630002441995063000244WP 1995 6 30 9509869993 119950512A5330 SKIN DOUG DC9 DC931 3022065WP DOOR CUTOUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018986E 47402 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE SERVICE DOOR CUTOUT SKIN UPPER FORWARD CORNER. REPAIRED PER EA 99-93535. 2L72 4F A6WE 19950630002451995063000245NM 1995 6 30 9509872717 119950607A5712 RIB BOEING727 7272S7 138407ZNM FS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RC 22492 DURING PERIODIC CHECK, FOUND CRACKS IN THE WING TO BODY UPPER RIB CHORD, BS 760, UPPER FORWARD FASTENER BORE AT LBL 70.5 AND THE LOWER FORWARD FASTENER BORE AT RBL 70.5. REPAIRED CHORD (P/N 65-18522-14) PER EA 27-98429 AND EA 27-98432, RESPECTIVELY. 2L73 4F A3WE 19950630002461995063000246WP 1995 6 30 9509889942 119950607A5311 FRAME DOUG DC9 DC932 3022066WP FS 598 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING PERIODIC CHECK, FOUND A CRACK IN FS 598 FRAME AT LONGERON 24L. REPAIRED FRAME (P/N 99-19621-1) PER EA 99-100379. 2L72 4F A6WE 19950630002471995063000247WP 1995 6 30 9509891156 119950619A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1975-1986 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01156US 46765 DURING PERIODIC CHECK, FOUND CORROSION IN THE FUSELAGE SKIN DOUBLER FS 1975 TO 1986, LONGERON 50L AND 50R. REPAIRED DOUBLER (AGA 7053-1) PER EA 11-98627. 2L73 4F A22WE 19950630002481995063000248EU 1995 6 30 9509903222 119950624A2750 FLAP INDICATION AIRBUS320 A320211 3930320EU TE FLAPS MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01322US 263 DURING APPROACH INTO LAS, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT, WHEN SELECTING FLAPS 2 POSITION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. AIRCRAFT OK FOR SERVICE. 2L72 4F RTA28NM 19950630002491995063000249NE 1995 6 30 9509912255 219950623A7320 FUEL CONTROL BOEING727 727251 138408HNM PWA JT8 JT8D7 52053NE NR 3 ENGINE OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01255US 19974 657626 NR 3 ENGINE DID NOT DEVELOP TARGET TAKEOFF THRUST. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TRIMMED AND INSPECTED THE ENGINE. SUBSEQUENT PERFORMANCE CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950630002501995063000250NE 1995 6 30 9509922288 219950620A7200 ENGINE BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 3 MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01288US 21376 696475 NR 3 ENGINE SLOW TO ACCELERATE AS POWER WAS APPLIED FOR TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED AN ACCELERATION CHECK. NO DISCREPANCIES WERE NOTED AND THE ENGINE ACCELERATION WAS WITHIN P AND W LIMITS. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950630002511995063000251NM 1995 6 30 9509932712 119950617A5210 DOOR BOEING727 7272S7 138407ZNM CABIN NOT LATCHED A NWAAAJ UNSCHED LANDING DUMP FUEL P NO WARNING INDICATION CLCLIMB 1 GL01712RC 22020 DURING TAKEOFF TPA-MSP, NOTICED MAIN CABIN DOOR AIR LEAK WITH NO CORRESPONDING DOOR WARNING INDICATION. DUMPED 25,000 LBS OF FUEL AND RETURNED TO TPA WITHOUT FURTHER INCIDENT. INSPECTED DOOR AND FRAME ASSEMBLY. NO TROUBLE FOUND, OPERATIONAL CHECK OK. 2L73 4F A3WE 19950630002521995063000252 1995 6 30 9509951144 419950626A34417883450041 INS COMPUTER DOUG DC10 DC1040 3023508WP NR 2 UNRELIABLE A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01144JC2218073 46753 DURING CRUISE, THE NR 2 INS BECAME UNRELIABLE. THE NR 3 INS WAS ALREADY ON MEL. FLIGHT DIVERTED TO BOS. REPLACED THE NR 2 INS COMPUTER. 2L73 4F A22WE 19950630002531995063000253WP 1995 6 30 9509969139 119950619A3150 CONNECTOR DOUG DC9 DC914 3022034WP TAKEOFF WARNING DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01948L 47049 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. ABORTED AT 20 KNOTS AND RETURNED TO GATE. CLEANED CONNECTOR P10-1009. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630002541995063000254WP 1995 6 30 9509979301 119950616A3230 RETRACT MECH DOUG DC9 DC982 3022082WP LT MLG MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01301RC 48054 DURING CLIMBOUT FROM PHX, THE LEFT MAIN GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHTS STAYED ON INITIALLY, BUT EXTINGUISHED A FEW MOMENTS LATER. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. PERFORMED GEAR SWING AND CHECKED PROXIMITY SWITCH CLEARANCE, NO PROBLEMS WERE FOUND. LUBED THE LEFT MAIN GEAR AND DOOR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630002551995063000255WP 1995 6 30 9509989752 119950615A2420 WIRE DOUG DC9 DC941 302207NWP LT GEN TRANS BROKEN A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01752NW 47116 LOSS OF LEFT GENERATOR WITH CROSSTIE LOCKOUT OCCURRED DURING TAKEOFF ROLL. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO GATE. FOUND BROKEN WIRE AT TERMINAL ON LEFT GENERATOR CURRENT TRANSFORMER. INSTALLED NEW TERMINAL. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630002571995063000257NM 1995 6 30 95UAL900015 119950626A2611 SMOKE DETECTOR 2156204A BOEING757 757222 1384956NM PWA 2037 PW2037 NE CARGO DOOR MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29524UA 7899A 24977 ABORTED TAKEOFF AT 70 KNOTS DUE TO CARGO PIT FIRE INDICATION. NO EVIDENCE OF FIRE FOUND. REPLACED CARGO SMOKE DETECTOR, SYSTEM OP CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950630002581995063000258NM 1995 6 30 95UAL900016 119950626A2810 FUEL SYS BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE LT WING VENTING A UALAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 WP297258U 21405 ABORTED TAKEOFF AT 80 KNOTS, WHEN FUEL STARTED VENTING FROM THE LEFT WING. 2L73 4F4 F A3WE E2EA 19950630002591995063000259NM 1995 6 30 95UAL900018 119950626A2760 MECHANISM 254N10535 BOEING757 757222 1384956NM PWA 2037 PW2037 NE SPEED BRAKES FAILED A UALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 WP29506UA 24627 SPEED BRAKES AUTOMATICALLY DEPLOYED IN FLIGHT. A/C LOST 1500 FEET WHILE CAPTAIN STOWED SPEED BRAKES. BOTH PILOTS WERE REQUIRED TO PULL A/C FROM NOSE DOWN ATTITUDE. FOUND SPEED BRAKE LEVER RESISTANCE INCONSISTENT. THE SPEED BRAKE MECHANISM WAS FOUND TO BE BAD. 2L72 4F4 FRTA2NM E17NE 19950630002601995063000260NM 1995 6 30 95UAL900019 119950626A3300 EEL BATTERY PACK BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29154UA 20103 EMERGENCY EXIT LIGHT SIGNS INOP AT DOOR 1L. REPLACED BATTERY PACK. 2L74 4F4 F A20WE E20EA 19950630002611995063000261NM 1995 6 30 95UAL900020 119950626A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297454U 21908 EMERGENCY EXIT SIGN ON AFT DROP CEILING INOP. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950630002621995063000262WP 1995 6 30 95UAL900021 119950627A3350 EEL BATTERY PACK DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291854U 47813 EEL LIGHTS FAIL BATTERY TEST. REPLACED MID AND OW BATTERIES. 2L73 4F4 F A22WE E23EA 19950630002631995063000263NM 1995 6 30 95UAL900022 119950627A3350 EEL BATTERY PACK BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299052U 19933 RIGHT OW EMERGENCY LIGHTS STAYED ON. REPLACED OW BATTERIES. 2L72 4F4 F A16WE E2EA 19950630002641995063000264NM 1995 6 30 95UAL900023 119950627A3350 EEL BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29376UA 24641 LEFT OW EEL LIGHTS INOP. REPLACED BATTERY PACK. 2L72 4F4 FRTA16WE E2GL 19950630002651995063000265EU 1995 6 30 95UAL900024 119950627A3350 EEL BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29402UA 439 EEL LIGHTS INOP AT DOOR 1L. REPLACED BATTERY PACK. 2L72 4F RTA28NM E40NE 19950630002661995063000266NM 1995 6 30 95UAL900025 119950627A5312BACN10HR5 NUT BOEING BACB30MT BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE AFT PRESS BLKHD CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29607UA 21868 DURING OVERHAUL, A DETAILED INSPECTION OF THE .3125 INCH PLUS DIAMETER FASTENERS COMMON TO THE AFT PRESSURE BULKHEAD ATTACH RING, LOCATED BETWEEN STRINGER END FITTINGS, WAS ACCOMPLISHED. THIS INSPECTION REVEALED AT LEAST 70 CRACKED NUTS. FURTHER INSPECTION FOUND AT LEAST 65 PERCENT OF THE STRINGER END FITTINGS HAD VARIOUS LEVELS OF CORROSION ON THE TENSION BOLTS. ALL OF THE .3125 INCH SHEAR BOLTS WERE REPLACED AS WELL AS ANY CORRODED .3125 INCH SHEAR BOLTS. ALL STRINGER END FITTING BOLTS AND ATTACH HARDWARE WERE REPLACED EXCEPT BETWEEN STR 4L AND STR 4R. 2L72 4F4 FRTA1NM E3NE 19950630002671995063000267WP 1995 6 30 ABXA9500563 119950622A32607000010101 DNLOCK SWITCH DOUG DC9 DC932 3022066WP NLG DEFECTIVE A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23902AX 47426 ON APPROACH, THE NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE. VISUALLY CHECKED GEAR FOR DOWN AND LOCKED, CONTINUED WITH NORMAL OPERATION IAW DC9 ABNORMAL CHECKLIST. REMOVED AND REPLACED THE NOSE DOWN LOCK SWITCH IAW DC 9 MM. SYSTEM OPS CHECKED GOOD. 2L72 4F A6WE 19950630002681995063000268WP 1995 6 30 ABXA9500564 119950622A32601819 BULB DOUG DC9 DC932 3022066WP MLG DOOR DEFECTIVE A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23981AX 47273 ON APPROACH, THE GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE. REPLACED BULB, RECYCLED GEAR, SYSTEM OPS CHECKED GOOD. CHECKED LAMP FOR CORRECT LAMP P/N, CYCLED MAIN GEAR DOOR SEVERAL TIMES, SYSTEM OPS CHECKED GOOD IAW DC 9 MM. 2L72 4F A6WE 19950630002691995063000269SO 1995 6 30 COM11922 119950623A275012042642507 SELECT LEVER EMB 120 EMB120RT SO FLAP CONTROL DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01246CA6715 62 120223 FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR LEVER ASSY. 2L72 4T RTA31SO 19950630002701995063000270NM 1995 6 30 DHL95701001 119950621A3230631352 BUSHING BOEING727 72730C 1384009NM NOSE GEAR MISSING A TDHLAO OTHER J WARNING INDICATION LDLANDING 1 SO01701DH 19011 PRIOR TO LANDING, NOSE GEAR VERY SLOW TO EXTEND AND INDICATE DOWN AND LOCKED. DURING LANDING ROLLOUT, NOSE GEAR GREEN LIGHT EXTINGUISHED AND LANDING WARNING HORN SOUNDED FOR APPROXIMATELY 5 SECONDS. JACKED AIRCRAFT, SWUNG NOSE GEAR, AND REPLACED MISSING BUSHING. OPS CHECK GOOD PER MM 32-33-0. 2L73 4F A3WE 19950630002711995063000271NM 1995 6 30 DL72E952769 119950623A5311 FORMER BOEING727 727247 138408FNM BS 640 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CK, CORROSION ON FORMER BEHIND T-ANGLE STA 640 O/B STR 27R. INSTALLED DOUBLER PER SRM 53-10-4 FIG 13. 2L73 4F A3WE 19950630002721995063000272NM 1995 6 30 DL72E952770 119950623A5311 FORMER BOEING727 727247 138408FNM BS 560 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 FOUND ON CV2 CK, .75 INCH CRACK IN FORMER STA 560 STR 25L. INSTALLED DOUBLER PER SRM 53-10-4 FIG 26. 2L73 4F A3WE 19950630002731995063000273NM 1995 6 30 DL72S952792 119950429A5753652163261 ANGLE BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 2 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE AFT CHORD ATTACH ANGLE CRACKED. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950630002741995063000274NM 1995 6 30 DL72S952793 119950513A5753652163261 CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 2 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO AFT LOWER CHORD CRACKED AT THREE PLACES I/B AT I/B MOST AFT FLAP TRACK AND AFT FLAP I/B DRIVE. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950630002751995063000275NM 1995 6 30 DL72S952801 119950429A5753652163395 FITTING BOEING727 727232 1384082NM NR 1 TE MIDFLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 THE NR 1 MIDFLAP I/B CARRIAGE SUPPORT FITTING THRUST BEARING RETAINER BOLT HOLES, 3 EACH WERE FOUND CORRODED. THE HOLES WERE REPAIRED PER SRM 57504 FIG 14, BY REAMING HOLES TO REMOVE DAMAGE AND A BUSHING WAS INSTALLED. FOUND AT HMV SHOP VISIT. 2L73 4F A3WE 19950630002761995063000276NM 1995 6 30 DL72S952802 119950429A5753652163395 FITTING BOEING727 727232 1384082NM NR 1 TE MIDFLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 THE NR 1 MIDFLAP O/B CARRIAGE SUPPORT FITTING HAD 4 EACH, THRUST BEARING RETAINER BOLT HOLES CORRODED FOUND DURING SHOP INSP. THE HOLES WERE REPAIRED PER SRM 57504 FIG 14, BY REAMING HOLES TO REMOVE THE CORROSION AND INSTALLING A BUSHING. FOUND AT HMV SHOP VISIT. 2L73 4F A3WE 19950630002771995063000277NM 1995 6 30 DL72S952803 119950429A5753652163395 FITTING BOEING727 727232 1384082NM NR 1 TE MIDFLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 THE NR 1 MIDFLAP I/B CARRIAGE SUPPORT FITTING THRUST BEARING BORE WAS FOUND CORRODED. FOUND AT HMV SHOP VISIT. THE BORE WAS REPAIRED BY MACHINING BORE TO REMOVE CORROSION AND INSTALLING A BUSHING PER SRM 57504 FIG 15. 2L73 4F A3WE 19950630002781995063000278NM 1995 6 30 DL72S952805 119950507A5753652163395A BOLT BOEING727 727232 1384082NM NR 1 TE MIDFLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 1 MIDFLAP, DURING HMV SHOP INSP FOUND THE FOURTH HOLE FOR THE THRUST BEARING RETAINER BOLTS IS DAMAGED. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950630002791995063000279NM 1995 6 30 DL72W952753 119950622A5754 L/E RIB BOEING727 7272Q8 138407WNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831L 21826 A .5 INCH CRACK ON NR 4 SLAT L/E RIBS AT I/B AND O/B SIDES OF TRACK. FOUND DURING A-2 LETTER CHECK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950630002801995063000280NM 1995 6 30 DL72W952781 119950331A5753652163253 FITTING BOEING727 727247 138408FNM NR 3 TE MIDFLAP HOLE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 I/B CARRIAGE SUPPORT FITTING WAS FOUND TO HAVE LOWER O/B RETAINER BOLT HOLE CORRODED, IN NR 3 MIDFLAP. FOUND AT SHOP INSP, THE HOLE WAS REAMED AND BUSHED PER SRM 57504. 2L73 4F A3WE 19950630002811995063000281NM 1995 6 30 DL72W952782 119950622A5754651622295 RIB BOEING727 727247 138408FNM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112809W 20581 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 9 CRACKED. REPAIRED PER SRM 57-54-0 FIG 805. 2L73 4F A3WE 19950630002821995063000282NM 1995 6 30 DL72W952786 119950621A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, STRINGER CRACKED INSIDE VERTICAL STAB STR 7L CRACKED AT RIB ATTACH HOLE, THIRD BAY DOWN FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19950630002831995063000283NM 1995 6 30 DL72W952788 119950622A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, STRINGER CRACKED INSIDE VERTICAL STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC SECOND BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19950630002841995063000284NM 1995 6 30 DL72W952790 119950624A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, STRINGER CRACKED INSIDE VERT STAB STR 9R CRACKED AT RIB ATTACH HOLE LOC IN FIFTH BAY UP FROM ACCESS HOLE. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19950630002851995063000285NM 1995 6 30 DL72W952791 119950620A5713 STRINGER BOEING727 727247 138408FNM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, LT UPPER WING STR 10 CRACKED AT WING RIB CAP WS 686.5. REPAIRED PER MM 57-13-0 PG 801-805. 2L73 4F A3WE 19950630002861995063000286NM 1995 6 30 DL72W952806 119950623A5313570359500 STRINGER 570359500 BOEING727 727247 138408FNM FS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 PER M/M COMPLIED WITH PREVENTIVE MODIFICATION OF UPPER STR 9 AT STA 686.5, DUE TO CRACKED STR 10 AT STA 686.5. REPAIRED PER M/M 57-13-0 FIG 807, FOUND AT HMV. 2L73 4F A3WE 19950630002871995063000287NM 1995 6 30 DL72W952807 119950619A5311 FORMER BOEING727 727247 138408FNM BS 1050 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 FORMER CRACKED AT STA 1050 BELOW STR 25R. CUT OUT DAMAGE, INSTALLED REPAIR PER SRM 53-10-4 FIG 26, FOUND AT HMV. 2L73 4F A3WE 19950630002881995063000288NM 1995 6 30 DL72W952808 119950619A5755 SKIN BOEING727 727247 138408FNM LT SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 1937 22110 THE NR 1 SPOILER PANEL T/E HAS DELAMINATED, FOUND AT HMV. REMOVED DAMAGED AREA, COMPLETED REPAIR PER SRM 57-50-6 REF 51-40-6. 2L73 4F A3WE 19950630002891995063000289NM 1995 6 30 DL757952766 119950511A7110314N301016B NOSE COWL BOEING757 757232 1384965NM ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING AN UNSCHEDULED SHOP O/H DUE TO GROUND DAMAGE, THE LEADING EDGE LIP WAS REPAIRED PER SRM 54-11-01 FIG 203 AT THE 12 O/C POS. 2L72 4F RTA2NM 19950630002901995063000290NM 1995 6 30 DL757952774 119950624A5754114N4004165A T/E WEDGE BOEING757 757232 1384965NM NR 3 L/E SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH DELAMINATION DAMAGE TO T/E WEDGE. REPLACED WEDGE PER SRM 57-43-02 FIG 202. 2L72 4F RTA2NM 19950630002911995063000291NM 1995 6 30 DL757952795 119950624A2197W26322008B20 WIRE BOEING757 757232 1384965NM OUT FLOW VALVE SHORTED A DALAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO11623DL 22913 ON TAKOFF HAD STATUS MSG CABIN AUTO INOP, RETURNED BOS. FOUND OUTFLOW VALVE AC MOTOR WIRE NR W2632-2008B-20, SHORTED TO GROUND AT STANCHION IN AFT COMPARTMENT. REPAIRED WIRE, OPERATION NORMAL. 2L72 4F RTA2NM 19950630002921995063000292NM 1995 6 30 DL757952797 119950605A5414 SKIN BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 716442 AT HMV, THE NR 2 PYLON O/B SKIN WAS FOUND CRACKED AT TOP FWD CORNER OF CUTOUT FOR PANEL 443 AR. THE CRACK WAS ROUTED OUT PER SRM 54-51-01 DYE PEN. INSP PER PS 900-6-3, NO CRACK FOUND. DOUBLER PER SRM 54-57-01 WAS FABRICATED AND INSTALLED. 2L72 4F RTA2NM 19950630002931995063000293NM 1995 6 30 DL757952798 119950605A5414 SKIN BOEING757 757232 1384965NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 716442 AT HMV, THE NR 1 PYLON I/B SKIN WAS FOUND CRACKED PAST STOP DRILL ON TOP FWD CORNER OF CUTOUT FOR PANEL 433 AR. THE DAMAGE WAS REMOVED AND AREA DYE PENETRANT INSP PER PS 900-6-3 NR 01, NO CRACK FOUND. HFEC INSP, NO CRACK FOUND. DRILLED AND INSTALLED DOUBLERS PER SRM 54-51-01. 2L72 4F RTA2NM 19950630002941995063000294NM 1995 6 30 DL757952800 119950606A5753 T/E WEDGE BOEING757 757232 1384965NM LT T/E AFT FLAP CHIPPED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 AT HMV, THE LT I/B AFT FLAP WAS FOUND TO BE CHIPPED ON THE TRAILING EDGE. THIS WAS REPAIRED PER SRM 57-53-01 REF 51-70-17. 2L72 4F RTA2NM 19950630002951995063000295WP 1995 6 30 DLL10952764 119950622A5743 TRUNNION FITTING LKHEED1011 10113851 5265010WP LANDING GEAR RUSTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 LANDING GEAR FWD TRUNNION FITTING HAS RUST BACK OF GLAND NUT. REMOVED RUST PER SRM 51-21-01. 2L73 4F A23WE 19950630002961995063000296WP 1995 6 30 DLL10952765 119950623A57531529517114 SKIN LKHEED1011 10113851 5265010WP NR 3 T/E VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 NR 3 RT FLAP VANE HAD A CRACK 3 INCHES LONG, TOP SIDE SKIN 60 INCHES FROM I/B END. REPAIRED CRACK AS PER SRM FLUSH REPAIR 5753-00. 2L73 4F A23WE 19950630002971995063000297WP 1995 6 30 DLL10952768 119950530A5330 SKIN LKHEED1011 10113851 5265010WP FS 869-983 OUT OF LIMITS A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FOUND LOWER FUSELAGE SKIN PANEL AT FS 869 TO FS 983 BETWEEN STR 32 TO 35 OUT OF LIMITS DUE TO CORROSION. REPLACED SKIN PANEL PER SRM 53-31-00 FIG 826, AND DL ERA 271106-14. 2L73 4F A23WE 19950630002981995063000298WP 1995 6 30 DLL10952771 119950526A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1501 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FLOORBEAM CORRODED FS 1501 ABOVE STR 39 BELOW CARGO TIE DOWN SUPPORT. REPAIRED PER SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950630002991995063000299WP 1995 6 30 DLL10952772 119950528A5711 SPAR CAP LKHEED1011 10113851 5265010WP FS 1163 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THE T-CAP FS 1163, CTR TANK INTERMEDIATE SPAR UPPER CAP IS CRACKED IN RADIOUS AT RT OUTBD END. ACCOMPLISHED REPAIRS PER DL ERA 271114-14. 2L73 4F A23WE 19950630003001995063000300WP 1995 6 30 DLL10952773 119950621A5753 SKIN LKHEED1011 10113851 5265010WP NR 2 T/E VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING LETTER CHECK, FOUND LEFT WING NR 2 FLAP VANE WITH A 2 INCH CRACK IN UPPER SKIN AT 60 INCHES FROM I/B END OF FLAP. REPAIRED PER SRM 57-53-0. 2L73 4F A23WE 19950630003011995063000301WP 1995 6 30 DLL10952775 119950614A55221524058110 L/E SKIN LKHEED1011 10113851 5265010WP RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 DURING SHOP INSPECTION, A GOUGE AND CRACK WAS FOUND IN A LEADING EDGE PANEL OF THE RT ELEVATOR. REPAIRED PER SRM 55-22-00 FIG 802. 2L73 4F A23WE 19950630003021995063000302WP 1995 6 30 DLL10952776 119950529A5330 SKIN LKHEED1011 10113851 5265010WP FS 509-529 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, CORROSION ON C-1 B/B FUSELAGE SKIN AND SPLICE BETWEEN STR 32 AND 33 FS 509 AND 529. REMOVED CORROSION AND DRILLED UP NEW EDGE DOUBLER PER SRM 53-31-00 FIG 801. TREATED AND PAINTED PER PS 400-2-4-1 NR 2. INSTALLED FASTENERS PER SRM 53-31-00. 2L73 4F A23WE 19950630003031995063000303WP 1995 6 30 DLL10952777 119950526A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FLOOR SUPPORT CORRODED 4 RBL FS 1565. REMOVED CORROSION, OUT OF LIMITS PER SRM 53-23-00 FIG 802. DRILLED UP AND INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00. 2L73 4F A23WE 19950630003041995063000304WP 1995 6 30 DLL10952778 119950526A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1463 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FLOORBEAM CORRODED FS 1463 RT SIDE BELOW CARGO TIE DOWN ABOVE STR 27. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-23-00 FIG 801. REMOVED CORRODED BEAM AND INSTALLED REPLACEMENT BEAM PER LAC DWG NR 1505121. 2L73 4F A23WE 19950630003051995063000305WP 1995 6 30 DLL13952763 119950512A5330 FAILSAFE STRAP LKHEED1011 10113851 5265010WP FS 1525-1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FUSELAGE SKIN FAILSAFE TEAR STRAP WAS FOUND LIFTED AND CORRODED AT FS 1525 TO FS 1545 STRINGER 35. ACCOMPLISHED REPAIRS PER ERA 270891-14 REV C. 2L73 4F A23WE 19950630003061995063000306WP 1995 6 30 DLL13952779 119950622A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1523 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND FLOORBEAM CORRODED AT FS 1525, RIGHT SIDE. REMOVED SECTION OF FLOORBEAM AT STA 1523 RT SIDE. FAB REPAIR PARTS REF SRM 53-23-00 FIG 802. 2L73 4F A23WE 19950630003071995063000307WP 1995 6 30 DLL13952780 119950622A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, C-2 CARGO COMPT FLOORBEAM FS 1480 LBL 60 CORRODED. REMOVE CAP SECTION, FAB NEW CAP PER SRM 53-23-00 FIG 802 PG 803/804. 2L73 4F A23WE 19950630003081995063000308WP 1995 6 30 DLL13952784 119950622A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1525 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, C-2 CARGO COMPT FLOORBEAM FS 1525 FOUND CORRODED AT LBL 3. REPAIRED PER SRM 53-23-00 PG 803. 2L73 4F A23WE 19950630003091995063000309WP 1995 6 30 DLL17952796 119950624A32311512449107 ROD LKHEED1011 10113853 5265020WP NLG DOOR BROKEN A DALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO11766DA 193H1207 AFTER TAKOFF WHEN GEAR RETRACTED, HAD VIBRATION AND NOISE FROM NOSE GEAR AREA, RETURNED ATL. REPLACED BROKEN LEFT ROD ASSEMBLY FOR FWD DOOR. RIGGED DOORS, OPERATION NORMAL. 2L73 4F A23WE 19950630003101995063000310NM 1995 6 30 DLM88952737 119950622A5311 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11902DL 49533 FOUND DURING C-2 LETTER CHECK, 2 INCH CRACK AT MAIN WHEEL WELL FWD FRAME O/B END. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950630003111995063000311NM 1995 6 30 DLM88952813 119950623A2150 AIR COND SYS DOUG MD88 MD88 3023688NM CABIN SMOKE ODOR A DALAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11921DL 49645 DURING CLIMB, HAD SMOKE ODOR IN CABIN WHEN ENGINE ANTI-ICE WAS TURNED ON. LAV SMOKE DETECTORS TURNED ON. SUSPECT AIR SYSTEM CONTAMINATED FROM HYDRAULIC LEAK IN LEFT WHEEL WELL. REPAIRED LEAK, RAN ENGINES AND PACKS NO SMOKE ODOR NOTED. 2L72 4F RTA6WE 19950630003121995063000312NM 1995 6 30 DLM88952814 119950625A2120U3452900S DUCT COUPLING DOUG MD88 MD88 3023688NM TAIL COMP BLOWN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11925DL 49712 MIA - ON CLIMBOUT, AT FL110 AMBER FLOW LIGHT ON PRESSURIZATION CONTROLLER ILLLUMINATED. UNABLE TO PRESSURIZE, DIVERTED MCO. FOUND BLOWN DUCT AT LEFT WATER SEPARATOR. REPLACED SAME, OPERATION NORMAL. 2L72 4F RTA6WE 19950630003131995063000313WP 1995 6 30 MWEA95224 119950624A5230 PAN DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 DURING ROUTINE INSPECTION, THE AFT CARGO DOOR OUTER PAN FWD EDGE WAS FOUND CRACKED APPROX .24 INCH LENGTH. MAINTENANCE REPAIRED DOOR PAN IAW SRM 52-03 FIG 8 SHEET 1. REINSTALLED DOOR, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950630003141995063000314 1995 6 30 MWEA95225 419950626A34252587335 VERT GYRO DOUG DC9 DC932 3022066WP LEFT INOPERATIVE A MWEAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31502ME 48132 PILOT REPORTS, ON CLIMBOUT OF MKE THE CAPTAINS ADI SHOWS 25 TO 30 DEGREES PITCH UP, F/O'S ADI SHOWS 15 TO 20 DEGREES PITCH UP. APPEARS CAPTAINS ADI IS IN ERROR, RETURNED TO MKE. MAINTENANCE REMOVED AND REPLACED NR 1 VERTICAL GYRO. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950630003151995063000315WP 1995 6 30 MWEA95226 119950626A2560 LANYARD DOUG DC9 DC932 3022066WP GALLEY DOOR BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE MAINTENANCE, THE GALLEY SERVICE DOOR EVACUATION SLIDE LANYARD WAS FOUND TO BE BROKEN. MAINTENANCE REPLACED EVAC SLIDE LANYARD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950630003241995063000324CE 1995 6 30 95ZZZX3200 119950515A361015600110D184 HOSE ASSY BEECH 90 B90 1152912CE LT ENG PNEU DETERIORATED A SFOAK NONE O OTHER ININSP/MAINT 1 EA23320E LJ378 PILOT REPORTED PNEUMATIC PRESSURE AND VACUUM LOW AND DROPPING. FOUND PNEUMATIC REGULATOR CONTAMINATED WITH BLACK 'DUST' AND LARGER PIECES OF DEBRIS IN INLET LINE. TRACED PROBLEM TO PNEUMATIC SUPPLY HOSE AT LT ENGINE. APPROX ONE-THIRD OF INTERNAL PORTION OF HOSE WAS GONE AND REMAINDER OF INTERIOR 'DRY ROTTED' AND WOULD CRUMBLE WHEN HOSE BENT. PNEUMATIC SYS PURGED TO REMOVE DEBRIS AND HOSES ON BOTH ENGINES REPLACED. PNEUMATIC REGULATOR WAS CLEANED AND RE-INSTALLED. PNEU AND VACUUM SYSTEMS ADJUSTED PER MM. BELIEVE HOSE ON LT ENG INCORRECT P/N AND SUBSEQUENTLY INCORRECT MATERIAL TO WITHSTAND HIGH TEMPS COMING FROM ENGINE. RT HOSE APPEARED CORRECT P/N. BOTH HOSES HAD SAME MFG DATE. 1L72 3T 3A20 19950630003621995063000362WP 1995 6 30 9509999948 119950624A535059102331 TAILCONE DOUG DC9 DC931 3022065WP AFT FUS DEPARTED ACFT A NWAAK NONE JW WARNING INDICATION INADEQUATE Q C LDLANDING 1 GL018929E204 204 45866 DURING LANDING ROLLOUT RDU AT APPROXIMATELY 60 KNOTS, THE TAILCONE SEPARATED FROM THE AIRCRAFT WITH AN ACCOMPANYING WARNING INDICATION. THE SLIDE DID NOT DEPLOY, TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. FOUND THAT THE EXTERIOR HANDLE WAS NOT STOWED IN THE CLIPS AND THAT THE SLIDE LANYARD WAS IMPROPERLY RIGGED. REPLACED AND RIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950630003631995063000363WP 1995 6 30 9510009755 119950621A3222 STRUT DOUG DC9 DC941 302207NWP NOSE GEAR DEFLATED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01755NW 47179 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TUS. FLIGHT CONTINUED TO PHX AND LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. FOUND NOSE STRUT UNDERSERVICED, SERVICED STRUT TO PROPER LEVELS. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630003641995063000364WP 1995 6 30 9510019951 119950621A362012911021 THERMOSTAT DOUG DC9 DC932 3022066WP CROSSFEED DUCT LEAKING A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL019347 45827 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO GATE. FOUND SMALL AIR LEAK AT THERMOSTAT, TIGHTENED THERMOSTAT. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630003651995063000365WP 1995 6 30 9510029150 119950624A5320 FITTING DOUG DC9 DC914 3022034WP FS 786 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND CORROSION ON RIGHT CUSP FITTING AT FS 786. REPLACED FITTING (P/N9912243-68) PER SRM 51-30-1. 2L72 4F A6WE 19950630003661995063000366WP 1995 6 30 9510039971 119950625A5320 FITTING DOUG DC9 DC931 3022065WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 END FITTING AT FS 756 BULKHEAD. REPLACED FITTING PER SRM 53-02 FIG 12. 2L72 4F A6WE 19950630003671995063000367WP 1995 6 30 9510049911 119950617A3231 CABLES DOUG DC9 DC931 3022065WP NLG DOORS BINDING A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01961N 47405 STRONG VIBRATION AND A LOUD NOISE FROM THE NOSE GEAR AREA, AFTER TAKEOFF. FLIGHT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. FOUND BOTH NOSE GEAR DOOR CABLES AND BINDING AT PIVOT POINTS, CAUSING CABLE TO CATCH ON DOOR LINK AND BINDING DOORS. ADJUSTED LEFT CABLE PIVOT POINT ON DOOR AND RELACED RIGHT NOSE GEAR DOOR DUE TO DAMAGE INCURRED. OPERATIONAL CHECK OK ON GEAR RETRACTION TEST. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630003681995063000368WP 1995 6 30 9510059953 119950615A2781 INDICATION DOUG DC9 DC931 3022065WP LE SLAT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TOTAKEOFF 1 GL01918RW 47158 SLAT EXTEND, BLUE LIGHT DID NOT ILLUMINATE WITH FLAPS EXTENDED TO 15 DEGREES FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. PULLED AND RESET SLAT EXTEND SWITCH CIRCUIT BREAKERS, CYCLED SLATS SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950630003691995063000369WP 1995 6 30 9510069881 119950624A5350 CLIPS DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01676MC 47652 DURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE TAILCONE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS. 2L72 4F A6WE 19950630003701995063000370WP 1995 6 30 ABXA9500565 119950626A335060030431 EEL BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23924AX 901 47403 DURING MAINTENANCE INSPECTION, FOUND COCKPIT EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK IAW DC9 MM ABX SUPPLEMENT 33-53-0. SYSTEM OPS CHECKS GOOD. 2L72 4F A6WE 19950630003711995063000371WP 1995 6 30 ABXA9500566 119950625A335060030431 EEL BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23906AX 52713 47072 DURING PREFLIGHT INSPECTION, FOUND EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC9 MM. OPS CHECK GOOD. 2L72 4F A6WE 19950630003721995063000372WP 1995 6 30 ABXA9500567 119950626A335041B004AD07G3 EEL BATTERY PACKGRIMES 60030431 DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23980AX 2448 47176 DURING MONDAY MORNING CHECK, FOUND EMERGENCY LIGHTS DIM. REPLACED BATTERIES IN BATTERY PACK. OPS CHECK BATTERY PACK IAW DC-9 SUPP MM 33-53-0. 2L72 4F A6WE 19950630003731995063000373WP 1995 6 30 ABXA9500568 119950627A335014597010 EEL BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23939AX 47201 DURING PREFLIGHT INSPECTION, FOUND EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY BATTERIES IAW DC9 MM. 2L72 4F A6WE 19950630003741995063000374WP 1995 6 30 ABXA9500569 119950625A56105613217508 CV WINDOW DOUG DC9 DC932 3022066WP RT COCKPIT MALFUNCTIONED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 DURING PREFLIGHT INSPECTION, FOUND FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT CLOSE. OPENED, INSPECTED, CLOSED FIRST OFFICER'S WINDOW. OPS CHECKED GOOD IAW DC9 MM. 2L72 4F A6WE 19950630003751995063000375WP 1995 6 30 ABXA9500570 119950628A32300142101321 RETRACT MECH NIHON YS11 YS11A500 6310416WP NLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23914AX 10873 2056 NOSE LANDING GEAR DID NOT LOCK DOWN ON FIRST EXTENSION, SLOW TO LOCK DOWN ON SECOND. CLEANED AND LUBED NOSE LANDING GEAR, EXTENDED AND RETRACTED GEAR IAW YS11 MM 32-30-0. OPS CHECKED GOOD. 2L72 4T A1PC 19950630004001995063000400EA 1995 6 30 95ZZZX3262 219950606A7414 BUSHING BNORM BN2 BN2A26 1520226EU LYC O540 O540E4C5 41532EA IMPULSE COUPLINGLOOSE A DCRAK NONE O OTHER ININSP/MAINT 1 WP1336MR 1122 900 L2231340A DURING COMPLIANCE OF AD78-09-07R3, MAGNETO IMPULSE COUPLING INSPECTION, DISCOVERED THAT PREVIOUS COMPLIANCE WITH LYCOMING SI NR 114D, THE MAGNETO DRIVE BUSHING HAD WORKED LOOSE. FABRICATED AND RE-INSTALLED NEW BUSHING IAW LYCOMING SI NR 1140. 1H72 3O3 O A17EU E295 19950630004071995063000407EU 1995 6 30 95ZZZM109 119950612A2910HTE400004 NON RETURN VLV BAG JETSTMJETSTM3201 1500217EU RT LOSS OF FLUID A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27476UE 884 FLT 6384 - ROC-IAD - DURING TAXI HAD TO GET TOWED OFF OF THE RUNWAY DUE TO A TOTAL LOSS OF HYDRAULIC PRESSURE. AIRCRAFT WAS TOWED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED A CRACKED HYDRAULIC LINE, THE RIGHT NON RETURN VALVE AND THE BOTH HYDRAULIC PUMP DUE TO CAVITATION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950630004081995063000408EU 1995 6 30 95ZZZM110 119950612A291013711D1455 HYDRAULIC LINE BAG JETSTMJETSTM3201 1500217EU FUSELAGE CRACKED A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27476UE 884 FLT 6384 - ROC-IAD - DURING TAXI HAD TO GET TOWED OFF OF THE RUNWAY DUE TO A TOTAL LOSS OF HYDRAULIC PRESSURE. AIRCRAFT WAS TOWED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED A CRACKED HYDRAULIC LINE, THE RIGHT NON RETURN VALVE AND THE BOTH HYDRAULIC PUMP DUE TO CAVITATION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950630004091995063000409WP 1995 6 30 95ZZZM111 119950420A5330 SKIN DOUG DC8 DC863F 302198FWP FS 1030-1080 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 FUSELAGE SKIN BULGED AROUND FASTENERS IN THREE AREAS BETWEEN FS 1030 AND FS 1080 BETWEEN LONGERONS 19L AND 21L. OPENED GILL LINER TO GAIN ACCESS, FOUND LEVEL 3 CORROSION. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLERS AND FILLERS IAW DER DRAWING ARW .29925-12. 2L74 4F 4A25 19950630004101995063000410WP 1995 6 30 95ZZZM112 119950511A5330 SKIN DOUG DC8 DC863F 302198FWP FS 1060-1080 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 LEVEL 3 CORROSION FOUND ON BELLY SKIN UNDER LONGERONS 35L AND 35R BETWEEN FS 1060 AND FS 1080 CIRCUMFERENTIALS. (M) 2L74 4F 4A25 19950630004111995063000411WP 1995 6 30 95ZZZM113 119950508A2810 FUEL DOUG DC9 DC932 3022066WP LT/RT WINGS IMBALANCE A VJ6AJ DUMP FUEL K FLUID LOSS CLCLIMB 1 SO11919VV 47260 FLT NR 466 - PBI-IAD - CREW EXPERIENCED AN 400 LB FUEL IMBALANCE FROM RIGHT WING TO LEFT. AIRCRAFT LANDED IN IAD WITHOUT INCIDENT. IAD MAINTENANCE FILLED AIRCRAFT FULL OF FUEL AND RAN ALL PUMPS. NEXT, TAXIED AIRCRAFT USING BRAKES AND THROTTLE ABRUPTLY, NO LOSS OF FUEL. COULD NOT DUPLICATE. 2L72 4F A6WE 19950630004121995063000412WP 1995 6 30 95ZZZM114 119950428A2820 FUEL DOUG DC9 DC932 3022066WP RT WING SIPHONING A VJ6AA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 SO11919VV 47260 FLT NR 513 - ATL-MCO - AFTER AIRCRAFT WAS ON CLIMB-OUT FROM ATL, ANOTHER AIR CARRIER REPORTED FUEL COMING FROM THE RIGHT WING TIP. AIRCRAFT IMMEDIATELY RETURNED FOR LANDING. TRANSFERRED FUEL FROM LEFT TANK TO RIGHT TANK WHICH STOPPED SIPHONING OF FUEL. TRIED TO DUPLICATE CONDITIONS UNSUCCESSFULLY. PERFORMED TEST FLIGHT, SYSTEM CHECKS OK. (M) 2L72 4F A6WE 19950630004131995063000413NE 1995 6 30 95ZZZM115 219950504A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE NR 2 MALFUNCTIONED A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO11903VJ 47261 654641 FLT 154 - AFTER AIRCRAFT STARTED IT CLIMB-OUT FROM MSY, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO MSY WITHOUT INCIDENT. REMOVED ADN REPLACED THE NR 2 ENGINE. 2L72 4F4 F A6WE E2EA 19950630004141995063000414WP 1995 6 30 95ZZZM116 119950517A2611 SMOKE DETECTOR DOUG DC9 DC932 3022066WP AFT LAV MALFUNCTIONED A VJ6AO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SO11930VV 47723 FLT NR 179 - AFTER LANDING IN ATL, CREW SHUTDOWN NR 2 ENGINE FOR SINGLE ENGINE TAXI. BOTH AFT LAV SMOKE DETECTORS STARTED SOUNDING. FLIGHT ATTENDANT REPORTED TO THE PILOTS AND CAPTAIN SHUTDOWN THE RIGHT PACK OFF. ONE SMOKE DETECTOR SHUT OFF. NO SMOKE OR FLAMES WERE REPORTED BY THE CREW. RAN BOTH ENGINE AND PACKS, CHECKED AIRCRAFT CABIN AND TAIL COMPARTMENT, CHECKED AFT CABIN BALLAST AND NOTED NO OVERHEAT CONDITION OR INOP ITEMS. 2L72 4F A6WE 19950630004151995063000415NM 1995 6 30 95ZZZM117 119950602A5754 RIVET BOEING747 747122 1384872NM NR 9 SLAT POPPED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIVET HEAD POPPED ON FORWARD SPAR CAP AFT OF NR 9 SLAT (INBOARD END). REPLACED RIVET PER BOEING SRM 51-30-03. (M) 2L74 4F A20WE 19950630004161995063000416NM 1995 6 30 95ZZZM118 119950602A5730 PANEL BOEING747 747122 1384872NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND 17 INCH CRACK IN TRAILING EDGE LEFT WING FIBERGLASS PANEL FORWARD OF NR 6 SPOILER CENTER HINGE. REPAIRED PER BOEING SRM 51-40-09. (M) 2L74 4F A20WE 19950630004171995063000417WP 1995 6 30 AALA950650 119950410A2150 ACM DOUG DC9 DC982 3022082WP CABIN MALFUNCTIONED A AALABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW07227AA 49177 DFW-FLT 2016-DURING CRUISE AT FL 370 AND JUST PRIOR TO BEGINNING DESCENT, RT AIR CYCLE MACHINE FAILED. CABIN ALT BEGAN UNCONTROLLED CLIMB AS A/C INITIATED EMERG DESCENT. PAX OXYGEN MASKS WERE MANUALLY DEPLOYED AND ALL MASKS DROPPED. CABIN ALTITUDE REACHED MAX FL 150 BEFORE DESCENDING WITH A/C TO FL 100. A/C CONTINUED TO DFW AND LANDED W/O INCIDENT. ACCOMP GROUND ENG RUN AND PERFORMED CHECK OF LT AND RT AIR CYCLE MACHINES WITH NO DEFECTS FOUND. PRESSURIZATION CONTROLLERS WITH NO DEFECTS FOUND. UNABLE TO DUP PROBLEM. REPLACED OXYGEN CANNISTERS AND RESTOWED ALL OXYGEN MASKS. RE-SAFETIED MANUAL DROP SWITCH. ACCOMPLISHED FUNCTIONAL CHECK FLT WITH NO DEFECTS FOUND. SYSTEM OPS CHECK OK. 2L72 4F A6WE 19950630004181995063000418WP 1995 6 30 AALA950911 119950514A2130 PRESSURIZATION DOUG DC9 DC982 3022082WP CABIN MALFUNCTIONED A AALAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW0733414 49325 BNA - FLT NR 0807 - EN ROUTE LGA/DFW, DURING CRUISE AT FL 370, CABIN ALTITUDE ALARM SOUNDED WITH FLOW LIGHT ILLUMINATED. SELECTED MANUAL CABIN ALTITUDE CONTROL AND WITH OUTFLOW VALVES CLOSED, CABIN CONTINUED TO CLIMB. AS CABIN ALTITUDE APPROACHED FL 110, INITIATED EMERGENCY DESCENT AND ALL PAX OXYGEN MASKS DEPLOYED. A/C DIVERETED TO BNA AND LANDED W/O INCIDENT. ACCOMPLISHED BITE CHECK OF BOTH PRESS CONTROLLERS WITH NO DEFECTS FOUND. OUTFLOW VALVE CHECKED NORMAL OPERATION. ACCOMP GROUND ENG RUN AND PRESSURIZED A/C IN AUTO AND MANUAL MODES WITH NO DEFECTS FOUND. ACCOMP PRESS LEAK CHECKS WITH NO DEFECTS FOUND. RESTOWED ALL PAX OXYGEN MASKS. UNABLE TO DUP PROBLEM. A/C RETURNED TO SERVICE. (M) 2L72 4F A6WE 19950630004191995063000419WP 1995 6 30 AALA950912 119950513A2130 PRESSURIZATION DOUG DC9 DC982 3022082WP CABIN MALFUNCTIONED A AALAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW07426AA 49338 DCA - FLT 1416 - EN ROUTE DFW-BDL, DURING CRUISE AT FL 370, CABIN BEGAN A 100 FPM CLIMB AND FLOW LIGHT ILLUMINATED FOLLOWED BY AN INCREASE IN CABIN CLIMB RATE. INITIATED EMERGENCY DESCENT. ALL PAX OXYGEN MASKS DEPLOYED SUCCESSFULLY. AIRCRAFT DIVERTED TO DCA AND LANDED WITHOUT INCIDENT. CHECKED AIR CYCLE MACHINE DUCTING FOR LEAKS WITH NO DEFECTS FOUND. ACCOMPLISHED GROUND ENGINE RUN AND PRESSURIZATION SYSTEM CHECKED NORMAL IN AUTO AND MANUAL MODES. RESTOWED ALL PASSENGER OXYGEN MASKS. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. UNABLE TO DUPLICATE PROBLEM AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19950630004201995063000420NM 1995 6 30 AALA950958 119950519A3350A3060698101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07688AA 25730 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 5E AND 17D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PASSENGER SEAT ROW 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950630004211995063000421NM 1995 6 30 AALA950960 119950521A33505013CW EEL BOEING727 727223 1384074NM AFT GALLEY DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07863AA 21090 DFW - DURING OVERNIGHT CHECK, LEFT AFT GALLEY DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT AFT GALLEY DOOR OVERHEAD EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950630004221995063000422NM 1995 6 30 AALA950961 119950521A3350 EEL WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739356 24037 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RT AISLE IN FIRST CLASS INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT FORWARD AREA OF RIGHT AISLE IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004231995063000423NM 1995 6 30 AALA950962 119950520A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07371AA 25198 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ON PASSENGER SEAT 20HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CABIN SIDEWALL CONNECTOR BY PASSENGER SEAT 20HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004241995063000424NM 1995 6 30 AALA950963 119950520A33508100022002 EEL ASSY BOEING767 767323 1385205NM MID-GALLEY DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07357AA 24038 SFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY LIGHT LEFT SIDE OF LAMP INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT MID-GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004251995063000425NM 1995 6 30 AALA950964 119950522A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN NEEDED RESECURE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07351AA 24032 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LEFT AISLE BETWWEN PASSENGER SEAT ROWS 3 THROUGH 8 INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 8B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004261995063000426NM 1995 6 30 AALA950965 119950525A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07328AA 22328 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT 26HJ INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004271995063000427NM 1995 6 30 AALA950966 119950525A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07363AA 24044 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT FORWARD GALLEY INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950630004281995063000428NM 1995 6 30 AALA951006 119950531A3350 EEL WIRE BOEING757 757223 1384957NM CABIN EXPOSED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07688AA 25730 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT WIRING EXPOSED. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950630004291995063000429EU 1995 6 30 RAIA950528 119950530A21502205120 COOLING TURBINE AEROSPATR72 ATR72202 8680940EU LT PACK FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE6667 1887 283 STL - FLT 7167 - WITH LEFT PACK ON, SMELLED SMOKE, TURNED OFF PACK. MAINTENANCE DEFERRED LEFT PACK AS PER MEL 21-50-1 CAT C. (M) 2H72 4T RTA53EU 19950630004301995063000430 1995 6 30 RAIA950601 419950602A3442MI5853505 UNIT AEROSPATR42 ATR42300 8680920EU FWD FUSELAGE FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03425TE8518 3551 125 STL - FLT 7002 - RADAR WILL NOT PAINT. MAINTENANCE REPLACED RADAR R/T. (M) 2H72 4T RTA53EU 19950630004311995063000431EU 1995 6 30 RAIA950602 119950604A32609EN1C11HB2BB2 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG LACK OF LUBE A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03422AM13533 856 STL - FLT 7330 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. MAINTENANCE CLEANED AND LUBED NOSE GEAR UPLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19950630004321995063000432WP 1995 6 30 RAIA950603 219950602A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE LEAKING A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03337TE7754 929 66161 STL - FLT 7364 - LT ENGINE TORQUE BYPASSED AT 86 PERCENT. MAINTENANCE REPLACED LEFT BLEED AIR GASKETS AND ADJUSTED LEFT EGT COMPENSATOR PER GARRETT DSC SHEET SETTINGS. GROUND RUNS REVEALED NORMAL OPERATIONS. (M) 2L72 4T4 TRTA56EU E4WE 19950630004331995063000433EU 1995 6 30 RAIA950604 119950605A2910137311D1447 LINE BAG JETSTMJETSTM3201 1500217EU HYD BAY CHAFED A RAIAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03436AM8938 891 STL - FLT 7328 - HYDRAULIC PRESSURE WENT TO ZERO, CREW PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE AT HYDRAULIC PRESSURE FILTER. LEAK CHECK GOOD ON GROUND TEST OF SYSTEM. (M) 2L72 4T RTA56EU 19950630004341995063000434 1995 6 30 RAIA950605 419950605A3418C771065 SUMMING UNIT BAG JETSTMJETSTM3201 1500217EU RT STALL WARN FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03429AM9104 879 STL - FLT 7393 - RT STALL LIGHT ILLUMINATED, HORN SOUNDED. MAINTENANCE REPLACED RT STALL WARNING SUMMING UNIT. SYSTEM TEST REVEALED NORMAL OPERATIONAL. (M) 2L72 4T RTA56EU 19950630004351995063000435 1995 6 30 RAIA950606 319950605A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU LT ENG FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03425AM5392 870 STL - FLT 7082 - LEFT BETA LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED LEFT BETA LIGHT SWITCH. GROUND RUNS AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950630004361995063000436EU 1995 6 30 RAIA950607 119950605A33500L60424P EEL BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE6689 283 STL - FLT 7110 - EMERGENCY ESCAPE PATH LIGHT IN ROW 5 IS OUT. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH LIGHT BULB. (M) 2H72 4T RTA53EU 19950630004371995063000437 1995 6 30 RAIA950608 419950608A235012147AGKX759 SWITCH AEROSPATR42 ATR42300 8680920EU RT YOKE STICKING A RAIAO OTHER O OTHER CRCRUISE 1 CE032FOR 11985 176 STL - FLT 7478 - FLIGHT OFFICERS PUSH TO TALK SWITCH IS STICKING. MAINTENACNE REPLACED FLIGHT OFFICERS PUSH TO TALK SWITCH. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19950630004381995063000438WP 1995 6 30 RAIA950609 219950608A732189778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE FAILED A RAIAK NONE O OTHER CLCLIMB 1 CE03431AM4034 881 66178 POWER LEVER SPLIT WITH TORQUES MATCHED. ALSO, RT ENGINE POWER 22 PERCENT AT FLIGHT IDLE. MAINTENANCE REPLACED RIGHT FUEL CONTROL UNIT GROUND RUNS AND LEAK CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19950630004391995063000439EU 1995 6 30 RAIA950610 119950606A3350311701 EEL PWR SUPPLY BAG JETSTMJETSTM3201 1500217EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03343TE5982 857 955 STL - RIGHT EXIT LIGHT AND CENTER OVERHEAD LIGHT WILL NOT ILLUMINATE WITH EMERGENCY LIGHTING ON. MAINTENANCE REPLACED EMERGENCY LIGHTING POWER SUPPLY. (M) 2L72 4T RTA56EU 19950630004401995063000440EU 1995 6 30 RAIA950612 119950607A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU FWD CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03424TE5234 1634 124 STL - FWD EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED FWD EMERGENCY LIGHTING BATTERY. (M) 2H72 4T RTA53EU 19950630004411995063000441EU 1995 6 30 UF6A950601 119950601A2750D9311 CONTACTOR BAG ATP ATP EU TE FLAPS FAILED A UF6AO OTHER J WARNING INDICATION APAPPROACH 1 CE03852AW3261 P5282 2021 FLT 5106 - ORD - FLAPS FAILED TO EXTEND. MAINTENANCE REPLACED THE FLAP REVERSING CONTACTOR. (M) 2L72 4T RTA27NM 19950630004421995063000442EU 1995 6 30 UF6A950602 119950602A2611CG7PT2 SMOKE DETECTOR BAG ATP ATP EU LAVATORY FAILED A UF6AO OTHER J WARNING INDICATION CLCLIMB 1 CE03851AW764 1527 2020 FLT 5042 - ORD - ON CLIMB, THE SMOKE CENTRAL WARNING ILLUMINATED. MAINTENANCE REPLACED THE LAVATORY SMOKE DETECTOR. (M) 2L72 4T RTA27NM 19950630004431995063000443EU 1995 6 30 UF6A950604 119950606A2731JM5 SWITCH BAG ATP ATP EU COCKPIT FAILED A UF6ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03859AW6937 2036 FLT 5020 - CWA - TAKEOFF CONFIGURATION WARNING SOUNDED. MAINTENANCE REPLACED THE ELEVATOR TRIM WHEEL MICROSWITCH. (M) 2L72 4T RTA27NM 19950630004441995063000444WP 1995 6 30 VTZA95192 219950607A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LEFT FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27493UE117675729 805 P66088 FLT NR 6423 - IAD-ROC - DURING TAKEOFF, ABORTED TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 88 PERCENT TORQUE. MAINTENANCE IS IN THE PROCESS OF CHANGING THE ENGINE. MAINTENANCE COMPLETED CHANGING ENGINE ON 6-10-95. ENGINE RUNS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950630004451995063000445EU 1995 6 30 VTZA95193 119950606A21301419100165 FLEX HOSE JETAIRJETSTMJETSTM4101 1500501EU PRESS SYST KINKED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27312UE 41025 FLT NR 6418 - IAD-BOS - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE PRESSURIZATION BEING INOP IN BOTH AUTO AND MANUAL. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 03558 IAW MEL 21-7-3. MAINTENANCE LATER CLEARED DMI NR 03558, BY REPLACING THE NEGATIVE PRESSURE AND REFERENCE PRESSURE FLEX HOSES TO PRESSURE CONTROLLER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950630004461995063000446EU 1995 6 30 VTZA95194 119950612A29131379125H HYDRAULIC PUMP BAG JETSTMJETSTM3201 1500217EU LT/RT CAVITATED A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 EA27476UE 884 FLT 6384 - ROC-IAD - DURING TAXI HAD TO GET TOWED OFF OF THE RUNWAY DUE TO A TOTAL LOSS OF HYDRAULIC PRESSURE. AIRCRAFT WAS TOWED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED A CRACKED HYDRAULIC LINE, THE RIGHT NON RETURN VALVE AND THE BOTH HYDRAULIC PUMP DUE TO CAVITATION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950630004471995063000447NM 1995 6 30 95ZZZM119 119950602A5730 PANEL BOEING747 747122 1384872NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND 32 INCH CRACK IN LEFT WING TRAILING EDGE FIBERGLASS PANEL FORWARD OF NR 6 SPOILER INBOARD END. REPAIRED IAW BOEING SRM 51-40-09. 2L74 4F A20WE 19950630004481995063000448NM 1995 6 30 95ZZZM120 119950602A5730 PANEL BOEING747 747122 1384872NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND .5 INCH CRACK IN TRAILING EDGE LEFT WING FIBERGLASS PANEL FORWARD OF NR 6 SPOILER. REPAIRED PANEL PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630004491995063000449NM 1995 6 30 95ZZZM121 119950602A5730 PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF PANEL 571CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09, FIGURE 10. 2L74 4F A20WE 19950630004501995063000450NM 1995 6 30 95ZZZM122 119950605A33506104791X EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST TXTAXI/GRND HDL 1 EA07911HA24618 PS111 034 FLT 3158 - HPN-PHL - DURING PREFLIGHT WALKAROUND, FOUND THE CENTER OVERHEAD EMERGENCY DOWN LIGHTS AND EGRESS LIGHTS INOP. REMOVED AND REPLACED PS4 POWER SUPPLY AND BATTERY. 2H72 4T RTA13NM 19950630004511995063000451NM 1995 6 30 95ZZZM123 119950605A33506013211X EEL BATTERY GRIMES DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A HNAAK NONE L NO TEST TXTAXI/GRND HDL 1 EA07911HA12662 ORF167 034 FLT 3158 - HPN-PHL - DURING PREFLIGHT WALKAROUND, FOUND THE CENTER OVERHEAD EMERGENCY DOWN LIGHTS AND EGRESS LIGHTS INOP. REMOVED AND REPLACED PS4 POWER SUPPLY AND BATTERY. 2H72 4T RTA13NM 19950630004521995063000452NM 1995 6 30 95ZZZM124 119950524A3350 EEL CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07912HA 40 FLT NR 3427 - HPN-PHL - DURING PREFLIGHT WALKAROUND, TWO RED EMERGENCY FLOOR LIGHTS WERE FOUND INOP AT ROW 1. SECURED THE CONNECTOR UNDER THE FLOOR AT ROW 1. 2H72 4T RTA13NM 19950630004531995063000453EA 1995 6 30 95ZZZM125 119950523A5730 SKIN DHAV DHC7 DHC7102 2802708EA WS 237.5 CRACKED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07901HA 042 AT RON, FOUND THE UPPER RIGHT WING SKIN CRACKED AT STATION YW237.5. REPAIRED IAW E07-57-95-011. 2H74 4T A20EA 19950630004541995063000454NM 1995 6 30 95ZZZM126 119950525A612082455011S011 ENGINE HARNESS DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A HNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA07922HA19853 094 FLT NR 3068 - PHL-LYH - ON TAKEOFF, THE RIGHT PROP DECREASED FROM 1200 RPM TO 600 RPM. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED THE ENGINE HARNESS BETWEEN P3 AND P42 AND REMOVED AND REPLACED THE REVERSION RELAY 7611-K2. 2H72 4T RTA13NM 19950630004551995063000455NM 1995 6 30 95ZZZM127 119950525A6120M390166105L REVERSION RELAY DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A HNAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA07922HA19853 094 FLT NR 3068 - PHL-LYH - ON TAKEOFF, THE RIGHT PROP DECREASED FROM 1200 RPM TO 600 RPM. THE CREW ABORTED THE TAKEOFF WITHOUT INCIDENT. REMOVED AND REPLACED THE ENGINE HARNESS BETWEEN P3 AND P42 AND REMOVED AND REPLACED THE REVERSION RELAY 7611-K2. 2H72 4T RTA13NM 19950630004561995063000456NM 1995 6 30 95ZZZM128 119950525A61207898426009 ECU HAMSTD DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A HNAAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 EA07922HA19853 89115652 094 FLT 3217 - LYH-PHL - AFTER LANDING, THE NR 2 PROP STABILIZED AT 650 RPM. THE CREW CYCLED THE CONDITION LEVER TO START FEATHER, THEN BACK TO MINIMUM AND THE PROP WOULD NOT COME OUT OF FEATHER. REMOVED AND REPLACED THE NR 2 ELECTRONIC CONTROL UNIT. 2H72 4T RTA13NM 19950630004571995063000457EA 1995 6 30 95ZZZM129 119950504A79311G3572 OIL PRESSURE SW DHAV DHC7 DHC7102 2802708EA NR 1 ENG FAILED A HNAAC ABORTED TAKEOFF JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 EA07905HA2601 1273 070 FLT NR 3060 - PHL-DCA - ON TAKEOFF ROLL, THE ENGINE FAILURE WARNING LIGHT ILLUMINATED ON BOTH SIDES OF THE COCKPIT. THE TAKEOFF WAS ABORTED AND THE CREW DETERMINDED THERE HAD BEEN A FAILURE OF THE AUTO FEATHER ENGINE FAILURE WARNING SYSTEM. AFTER RECEIVING AN MEL ASSIGNMENT. THE AIRCRAFT PROCEEDED WITH A NORMAL TAKEOFF. AT RON, THE READ OUT WIRING TO ALL ENGINE PRESSURE SWITCHES WAS GOOD. OPS CHECKED NR 1, 2, 3, AND 4 SWITCHES. FOUND NR 1 BAD. REMOVED AND REPLACED NR 1 OIL PRESSURE SWITCH. 2H74 4T A20EA 19950630004581995063000458 1995 6 30 95ZZZM130 319950512A6140 AUTO FEATHER LTS DHAV DHC8 DHC8102 2809003NM COCKPITS MALFUNCTIONED A HNAAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 EA07927HA 117 FLT 3068 - PHL-LYH - AIRCRAFT RETURNED TO THE GATE WHEN THE AUTO FEATHER LIGHTS WOULD NOT ILLUMINATE DURING STATIC TEST WHILE ENGINES WERE RUNNING, BUT THE PROPELLERS WERE FEATHERING. REMOVED AND REPLACED THE DC REMOTE CONTROL CIRCUIT BREAKER, NO FIX. PULLED CIRCUIT BREAKER FOR AUTO FEATHER PUMP INDICATION AND RESET. 2H72 4T RTA13NM 19950630004591995063000459EA 1995 6 30 95ZZZM131 119950517A32317323015105 SPIGOT DHAV DHC7 DHC7102 2802708EA RT MLG DOORS WORN A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07902HA35309 052 FLT 3003 - ORF-DCA - RIGHT MAIN GEAR DOORS WILL NOT CLOSE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TORQUE TUBE, SPIGOT, SCREWS, AND NUT PLATES. 2H74 4T A20EA 19950630004601995063000460EA 1995 6 30 95ZZZM132 119950517A32317323011055 TQ TUBE DHAV DHC7 DHC7102 2802708EA RT MLG DOORS WORN A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07902HA35309 052 FLT 3003 - ORF-DCA - RIGHT MAIN GEAR DOORS WILL NOT CLOSE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TORQUE TUBE, SPIGOT, SCREWS, AND NUT PLATES. 2H74 4T A20EA 19950630004611995063000461NM 1995 6 30 95ZZZM133 119950514A26118006221 CONTROL BOX GRIMES DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A HNAAO OTHER N FALSE WARNING LDLANDING 1 EA07923HA14642 0050 099 FLT 3246 - PHF-CLT - AFTER LANDING, THE BAG BAY SMOKE WARNING LIGHT ILLUMINATED. RESET, AND LIGHT CAME ON AGAIN. SMOKE WARNING BUTTON WOULD NOT RESET IN A THIRD TIME. CAPTAIN CALLED THE FIRE DEPARTMENT BUT PROCEEDED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE WARNING CONTROL BOX AND WARNING ANNUNCIATOR PANEL. 2H72 4T RTA13NM 19950630004621995063000462NM 1995 6 30 95ZZZM134 119950514A26117504341 ANNUNCIATOR PNL GRIMES DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A HNAAO OTHER N FALSE WARNING LDLANDING 1 EA07923HA8748 0082 099 FLT 3246 - PHF-CLT - AFTER LANDING, THE BAG BAY SMOKE WARNING LIGHT ILLUMINATED. RESET, AND LIGHT CAME ON AGAIN. SMOKE WARNING BUTTON WOULD NOT RESET IN A THIRD TIME. CAPTAIN CALLED THE FIRE DEPARTMENT BUT PROCEEDED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE WARNING CONTROL BOX AND WARNING ANNUNCIATOR PANEL. 2H72 4T RTA13NM 19950630004631995063000463WP 1995 6 30 95ZZZM135 119950526A5311 FRAME DOUG DC8 DC861 3021952WP FS 1400 CORRODED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION WAS FOUND ON THE FUSELAGE FRAME AT FS 1400 BETWEEN L34R AND L35L. REMOVED AND REPLACED FUSELAGE FRAME AT FS 1400, INSTALLED STRAP DOUBLER AND ACCOMPLISHED REPAIR SPLICE ON FUSELAGE FRAME IAW EO 9505071. 2L74 4F 4A25 19950630004641995063000464WP 1995 6 30 95ZZZM136 119950526A5320 ANGLE DOUG DC8 DC861 3021952WP FS 1680 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION DAMAGE FOUND ON THE FUSELAGE RING ANGLE AT FS 1680 BETWEEN L28R TO L33L. REMOVED AND REPLACED RING ANGLE AND INSTALLED TWO SPLICES IAW EO 9505073. 2L74 4F 4A25 19950630004651995063000465WP 1995 6 30 95ZZZM137 119950526A5330 SKIN DOUG DC8 DC861 3021952WP FS 1680 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK ON FUSELAGE RING ANGLE, CORROSION REPAIR ON FS 1680 IAW EO 9505073 WAS NECESSARY TO ACCOMPLISH A FUSELAGE SKIN CUTOUT AT FS 1680, BETWEEN L26L TO L26R TO ACCOMPLISH RING ANGLE REPAIR. AFTER COMPLETION OF RING ANGLE REPAIR, INSTALLED A .071 7075-T6 SKIN TO FILL CUTOUT, WITH AN .080 7075-T6 SPLICE STRAP INSTALLED. ALSO, AN .080 7075-T6 EXTERNAL DOUBLER INSTALLED AT FS 1680 BETWEEN L28L TO L30L. ALL REPAIRS ACCOMPLISHED IAW EO 9505221. 2L74 4F 4A25 19950630004661995063000466WP 1995 6 30 95ZZZM138 119950526A5330 SKIN DOUG DC8 DC861 3021952WP FS 1680 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK CORROSION WAS FOUND ON RIGHT SIDE OF THE AIRCRAFT IN THE FUSELAGE SKIN FS 1680. TRIMMED OUT DAMAGED SKIN. INSTALLED A .071 7075-T-6 FILLER AND INSTALLED A .080 7075-T6 EXTERNAL DOUBLER IAW EO 9505251. 2L74 4F 4A25 19950630004671995063000467NM 1995 6 30 95ZZZM139 119950530A5412 FIRE WALL BOEING747 747122 1384872NM NR 3 PYLON WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 NR 3 PYLON IN 3RD AND 4TH INSPECTION PANEL TOP HOLE HYDRAULIC PRESSURE LINE FIREWALL FITTING JAM NUT NOT INSTALLED HOLE IS WORN ELONGATED. DRESSED AND CLEANED BULKHEAD FITTING HOLE AS PER SRM 51-10-02, INSTALLED AND SECURED SHOULDER BUSHING, AND BULKHEAD FITTING. 2L74 4F A20WE 19950630004681995063000468CE 1995 6 30 95ZZZM140 119950518A21301143641407 CONTROL MODULE BEECH 1900 1900D 1154162CE LEFT FAILED A GLBAK NONE JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0196UX 2983 873E94 UE96 MDT - PILOT REPORTED, THE LEFT ENVIRONMENTAL FAIL LIGHT ILLUMINATED AND THAT THERE WAS A HINT OF SMOKE IN THE COCKPIT. MAINTENANCE REPLACED FAULTY CONTROL MODULE PCB. OPS CHECKED GOOD. 2L72 4T RTA24CE 19950630004691995063000469CE 1995 6 30 95ZZZM141 119950512A3230571302 PWR PACK MOTOR BEECH 1900 1900C 1154161CE LANDING GEAR INOP A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0179GL 16046 1047A UC79 ESC - THE CREW ELECTED AN AIR TURN BACK WHEN THEY WERE UNABLE TO RETRACT THE LANDING GEAR. AFTER AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR POWER PACK MOTOR. BOTH THE GEAR SWING AND THE TEST FLIGHT WERE SATISFACTORY. 2L72 4T RTA24CE 19950630004701995063000470CE 1995 6 30 95ZZZM142 119950511A7170131823E6M0260 EVA TUBE BEECH 1900 1900D 1154162CE LT WING LE LEAKING A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01100UX2504 UE100 ISN - AFTER NOTING THAT THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED, THE CREW ELECTED AN AIR TURN BACK AND ACCOMPLISHED AND UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED EVA TUBING IN LEFT LEADING EDGE. LEAK CHECKED OK. 2L72 4T RTA24CE 19950630004711995063000471EA 1995 6 30 95ZZZM143 219950503A7532310687001 BLEED VALVE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE MALFUNCTIONED A GLBAK NONE O OTHER APAPPROACH 1 CE01123UE 3N374 UC123 MHE - DURING APPROACH THE CREW REPORTED THAT THE LEFT ENGINE WAS COMPRESSOR STALLING. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE LEFT BLEED VALVE AND SEAT. A TEST FLIGHT WAS SUCCESSFUL. 2L72 4T4 TRTA24CE E4EA 19950630004721995063000472EU 1995 6 30 95ZZZM144 119950518A612078249020 PCU SAAB SF340 340B 7860101EU LT ENGINE MALFUNCTIONED A ANVEAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 SO03284AE7308 340B284 FLT 4519 - CLE - LEFT PROP RPM FLUCUATION ON APPROACH, THE THE RPM DROPPED TO 1000. THE PILOT SHUT DOWN THE ENGINE AND LANDED WITHOUT INCIDENT. REPLACED LEFT PROP CONTROL UNIT. 2L72 4T RTA52EU 19950630004731995063000473EU 1995 6 30 95ZZZM145 119950520A3234F96GA0102 GEAR HANDLE AEROSPATR42 ATR42300 8680920EU FLT DECK SHORTED A NVEAO OTHER J WARNING INDICATION APAPPROACH 1 SO03314AM 314 FLT 4519 - CLE - CREW REPORT LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. CREW USED EMERGENCY EXTENSION SYSTEM. REPLACED LANDING GEAR SELECTOR HANDLE. 2H72 4T RTA53EU 19950630004741995063000474NE 1995 6 30 95ZZZM146 219950502A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE STALLED A NVEAA UNSCHED LANDING X ENGINE FLAMEOUT TOTAKEOFF 1 SO03323AE5628 340B323 FLT 5798 - EYW - CREW REPORTS, ON TAKEOFF LEFT ENGINE HAD COMPRESSOR STALLS. THEN FAILED DIVERTED INTO NQX. LANDED WITHOUT INCIDENT. BORESCOPED LEFT ENGINE AND FOUND INTERNAL DAMAGE. ENGINE IS CURRENTLY BEING REPLACED. 2L72 4T4 TRTA52EU E8NE 19950630004751995063000475CE 1995 6 30 95ZZZM147 119950502A32301143880009 HYD PWR PACK BEECH 1900 1900C 1154161CE LANDING GEAR INOP A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0187GL 14615 UC87 LAN - AFTER LIFTOFF, THE CREW ELECTED AN AIR TURN BACK WHEN THE GEAR WOULD NOT RETRACT. THEY REPORTED THAT THE MOTOR RUNS AND POPS CIRCUIT BREAKER. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE HYDRAULIC POWER PACK AND MOTOR P/N 571302. ALL TESTS WERE SATISFACTORY. 2L72 4T RTA24CE 19950630004761995063000476SO 1995 6 30 95ZZZM148 219950525A8500 ENGINE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO LEFT FAILED A AFAHAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO1963PB 402C0335 290163R DURING CRUISE FLIGHT, THE LEFT ENGINE MADE A LOUD BANG. THE RPM AND POWER DECREASED, SO THE PILOT SHUT IT DOWN. THE AIRCRAFT LANDED IN LEE STOCKING ISLAND 25 MILES SHORT OF GEORGETOWN. THE CAUSE OF ENGINE FAILURE HAS NOT BEEN DETERMINED, UNTIL A MECHANIC CAN GO AND INSPECT THE ENGINE. 1L72 3O3 O A7CE E8CE 19950630004771995063000477NM 1995 6 30 95ZZZM149 119950530A5314 KEEL BEAM BOEING747 747122 1384872NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 ADF ANTENNA MOUNT STRUCTURE IS CORRODED (LEVEL 1) LOCATED ON KEEL BEAM BETWEEN NR 1 AND NR 3 ACM'S. REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING SRM 51-10-01, PAGES 13, 14, 15, 16 PAR 6 AND 7. 2L74 4F A20WE 19950630004781995063000478NM 1995 6 30 95ZZZM150 119950530A5312 BLKHD LINER BOEING747 747122 1384872NM FS 2160 HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD NEAR CENTER. REPAIRED AS PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950630004791995063000479NM 1995 6 30 95ZZZM151 119950530A5330 SKIN BOEING747 747122 1384872NM BS 2040 BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FUSELAGE SKIN AT AFT BULK CARGO DOOR OPENING STATION 2040 IS BENT OUTWARD. REPAIRED AS PER BOEING SRM 51-40-01, PRIMED AND PAINTED. 2L74 4F A20WE 19950630004801995063000480SO 1995 6 30 C2XA95IA100 119950614A572012017056021 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916718 120136 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB 16 CENTER LOWER SKIN SUPPORT BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950630004811995063000481NM 1995 6 30 F3LA95010 119950425A3260MS253831 SWITCH BOEING737 737201 1384454NM GEAR HANDLE MALFUNCTION A F3LAO OTHER N FALSE WARNING APAPPROACH 1 NM03205AU661641918 19421 DEN - UPON ARRIVAL, FLIGHT CREW REPORTED LANDING GEAR UNSAFE (INTRANSIT) LIGHTS ILLUMINATED WITH GEAR HANDLE UP. MAINTENANCE REPLACED THE LANDING GEAR HANDLE MICROSWITCH AND CHECKED OK. (M) 2L72 4F A16WE 19950630004821995063000482EU 1995 6 30 PAYA95A4027 119950604A2121EVTA1926DB EXHAUST FAN AEROSPATR42 ATR42300 8680920EU CARGO COMPT FAILED A PAYAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 EA174211G12319 178 FLT NR 7763 - JFK-PHL - CREW REPORTED THAT THE EXHAUST MODE AND AIR CAUTION LIGHTS ILLUMINATED FOLLOWED BY SMOKE IN THE COCKPIT AND CABIN. REPLACED EXHAUST FAN. (M) 2H72 4T RTA53EU 19950630004831995063000483NM 1995 6 30 PCAA9500218 119950502A4920 APU DHAV DHC8 DHC8102 2809003NM CABIN SMOKING A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA13816EX7403 329 AFTER TAKEOFF AIRCRAFT FILLED WITH FUMES AFTER BLEEDS WERE SELECTED ON. FOUND APU USING OIL, PUTTING OIL INTO BLEED SYSTEM, RAN AIRCRAFT WITH ENGINE BLEEDS ONLY. SYSTEM OPS CHECK NORMAL, OK FOR SERVICE. APU INOP PER MEL 49-1. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950630004841995063000484NM 1995 6 30 PCAA9500219 119950503A5610 WINDSHIELD DHAV DHC8 DHC8102 2809003NM LT COCKPIT DAMAGED A PCAAO OTHER C F.O.D. NRNOT REPORTED 1 EA13822EX10546 187 BIRD STRIKE LEFT WINDSHIELD. REPAIRED DAMAGED AREA IAW DHC REPAIR DRAWING 8-53-1493. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950630004851995063000485NM 1995 6 30 PCAA9500225 119950510A2120 AIR DISTR DHAV DHC8 DHC8102 2809003NM CABIN ODOR A PCAAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA13417AW8149 285 AIRCRAFT FILLED WITH STRONG FUEL ODOR AND BELIEVED TO BE COMING FROM APU BAY AREA. RAN APU BLEED NOTED NO FUEL SMELL OR ABNORMAL ODOR, SUSPECT APU BLEED OPERATION WITH RIGHT ENGINE RUNNING IN FEATHER. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950630004861995063000486NM 1995 6 30 95ZZZM152 119950530A255065B60291 PALLET GUIDE BOEING747 747122 1384872NM BS 6631 PEELED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FORWARD CARGO COMPARTMENT STATION 663 LEFT SIDE PALLET GUIDE SUPPORT METAL PEELED BACK. REMOVED AND REPLACED PALLET GUIDE AS PER SRM 51-10-01. 2L74 4F A20WE 19950630004871995063000487NM 1995 6 30 95ZZZM153 119950530A5312 BLKHD LINER BOEING747 747122 1384872NM BS 2160 HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 BULK CARGO STATION 2160 SMALL HOLE IN BULKHEAD LEFT SIDE. REPAIRED AS PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950630004881995063000488NM 1995 6 30 95ZZZM154 119950530A7830 TR SLEEVE BOEING747 747122 1384872NM NR 1 ENGINE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 SMALL AREA OF NR 1 ENGINE THRUST REVERSER SLEEVE SKIN AFT EDGE DELAMINATED. REMOVED AND REPLACED WORKING RIVETS IN DAMAGED AREA AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630004891995063000489NM 1995 6 30 95ZZZM155 119950530A5414 SKIN BOEING747 747122 1384872NM NR 3 PYLON LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 NR 3 PYLON LOWER AFT ABOVE EXHAUST LOOSE AND MISSING RIVETS. INSTALLED ALL MISSING AND LOOSE RIVETS AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630004901995063000490NM 1995 6 30 95ZZZM156 119950530A711069B906788 COWL BOEING747 747122 1384872NM NR 1 ENGINE WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 TOP AFT EDGE OF RIGHT SIDE COWL IS WORN AWAY AND BENT DOWN ONE FOOT FORWARD OF AFT END. REPAIRED AS PER SRM 54-14-07. 2L74 4F A20WE 19950630004911995063000491NM 1995 6 30 95ZZZM157 119950530A7830 TR SLEEVE BOEING747 747122 1384872NM NR 1 ENGINE GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FORWARD EDGE OF NR 1 ENGINE FAN THRUST REVERSER SLEEVE WORN TO KNIFE EDGE 4 O'CLOCK POSITION. SMOOTH BLENDED GOUGE AS PER BOEING SRM 54-36-01 AND RESTORED TO NORMAL FINISH. 2L74 4F A20WE 19950630004921995063000492NM 1995 6 30 95ZZZM158 119950530A5330 PANEL BOEING747 747122 1384872NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 AREA OF CORROSION ON FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 ACM ACCESS DOORS (LEVEL 1). REMOVED CORROSION, ALODINED AND PAINTED AS PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15, PARAGRAPH 6 AND 7. 2L74 4F A20WE 19950630004931995063000493NM 1995 6 30 95ZZZM159 119950530A533060B0671413 PANEL BOEING747 747122 1384872NM FUSELAGE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FIBERGLASS PANEL NR 191X IS DAMAGED AT RADIO ALTIMETER INSTALLATION HOLE BOTTOM FUSELAGE 2ND PANEL AFT. REPAIRED PER BOEING 747 SRM 51-50-09, PAINTED. 2L74 4F A20WE 19950630004941995063000494NM 1995 6 30 95ZZZM160 119950524A5320 SILL BOEING747 747122 1384872NM FWD CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FORWARD CARGO DOOR LOWER SILL UPPER LIP JUST AFT OF NR 3 ROLLER HAS AREA OF CORROSION (LEVEL 1). REPAIRED IAW BOEING SRM 51-10-01. 2L74 4F A20WE 19950630004951995063000495NM 1995 6 30 95ZZZM161 119950530A5330 PANEL BOEING747 747122 1384872NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND SMALL AREA OF CORROSION FORWARD AND AFT END OF PANEL BOTTOM OF FUSELAGE BETWEEN NR 1 AND NR 3 AIR CYCLE MACHINE ACCESS DOORS (LEVEL 1). REMOVED CORROSION ALODINED AND PAINTED PER BOEING 747 SRM 51-10-01, PAGES 13, 14, 15 AND 16, PARAGRAPH 6, 7. 2L74 4F A20WE 19950630004961995063000496NM 1995 6 30 95ZZZM162 119950530A5330 SKIN BOEING747 747122 1384872NM LT NLG CUTOUT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 LEFT NOSE GEAR TRUNNION CUTOUT HAS CRACK IN FORWARD UPPER CORNER IN W/W SKIN, CRACK IN CORNER RADIUS GOING UP UNDER DOUBLER. ITEM REVIEWED BY BOEING, DETAILED VISUAL INSPECTION TO BE PERFORMED EVER 250 CYCLES. REFERENCE BOEING LETTER PAOE 950531. 2L74 4F A20WE 19950630004971995063000497NM 1995 6 30 95ZZZM163 119950530A5330 SKIN BOEING747 747122 1384872NM RT NLG CUTOUT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIGHT NOSE GEAR TRUNNION CUTOUT HAS CRACK IN FORWARD UPPER CORNER IN WHEEL WELL SKIN, CRACK IN CORNER RADIUS GOING UP UNDER DOUBLER. ITEM REVIEWED BY BOEING, DETAILED VISUAL INSPECTION TO BE PERFORMED EVERY 250 CYCLES. REFERENCED BOEING LETTER PAOE 950531. 2L74 4F A20WE 19950630004981995063000498NM 1995 6 30 95ZZZM164 119950530A5210 SKIN BOEING747 747122 1384872NM NR 3 DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACKS COMING OUT OF 4 RIVETS HOLES IN VERTICAL LINE OF RIVETS APPROXIMATELY 18 INCHES BELOW FORWARD EDGE OF WINDOW IN NR 3 REAR DOOR SKIN. CUT OUT DAMAGE PER BOEING SRM 52-10-00, FIG 9. INSTALLED REPAIR DOUBLER PER SRM 50-10-00 FIG 9. 2L74 4F A20WE 19950630004991995063000499NM 1995 6 30 95ZZZM165 119950530A5210 SKIN BOEING747 747122 1384872NM NR 3 DOOR CRACKS A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACKS COMING OUT OF 4 RIVET HOLES IN VERTICAL ROW APPROXIMATELY 18 INCHES BELOW WINDOW IN NR 3 REAR DOOR SKIN, MARKED. CUT OUT DAMAGE PER BOEING SRM 52-10-00, FIG 9. INSTALLED REPAIR DOUBLER PER SRM 50-10-00, FIG 9. 2L74 4F A20WE 19950630005001995063000500NM 1995 6 30 95ZZZM166 119950602A528065B1166838 GEAR DOOR BOEING747 747122 1384872NM RT MLG LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 REPAIR COMING LOOSE AT OUTBOARD WING GEAR DOOR AT BOTTOM FORWARD END. REPAIRED PER BOEING 747 SRM 51-40-09. 2L74 4F A20WE 19950630005011995063000501NM 1995 6 30 95ZZZM167 119950602A5730 PANEL BOEING747 747122 1384872NM RT WING LE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND DAMAGED PANEL BOTTOM OF RIGHT WING LEADING EDGE AFT OF NR 23 LEADING EDGE SLAT AT JACK POINT. REPAIRED PER BOEING 747 SRM 51-40-09. 2L74 4F A20WE 19950630005021995063000502NM 1995 6 30 95ZZZM168 119950602A5730 PANEL BOEING747 747122 1384872NM WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND 6 INCH CRACK IN FIBERGLASS PANEL FORWARD OF NR 8 SPOILER AT OUTBOARD END. REPAIRED CRACKED PANEL PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630005031995063000503NM 1995 6 30 95ZZZM169 119950602A5330 SKIN BOEING747 747122 1384872NM FWD FUSELAGE GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CO-PILOTS WINDSHIELD WIPER ARM HAS GOUGED FUSELAGE SKIN IN PARKED POSITION. SMOOTH BLENDED MILD GOUGE OUT PER BOEING SRM 51-10-01, RERIGGED WIPER. 2L74 4F A20WE 19950630005041995063000504NM 1995 6 30 95ZZZM170 119950602A5321 PLATE BOEING747 747122 1384872NM FS 603 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FLOOR PLATE TORN AT FS 603 FORWARD OF BALL MAT AREA CENTER OF FLOOR. REPLACED PLATE AS BOEING SRM 51-10-01. 2L74 4F A20WE 19950630005051995063000505NM 1995 6 30 95ZZZM171 119950602A2730 NUT BOEING747 747122 1384872NM RT ELEVATOR RUSTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIGHT ELEVATOR HINGE NUT RUSTED AND ACTUATOR ROD END RUSTED. CLEANED AND TREATED AREA PER 747 SRM 51-12-01 (LEVEL 1). 2L74 4F A20WE 19950630005061995063000506NM 1995 6 30 95ZZZM172 119950602A5512 PANEL BOEING747 747122 1384872NM RT HORIZ STAB HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND HOLE IN PANEL 334GRB LOWER STABILIZER. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950630005071995063000507NM 1995 6 30 95ZZZM173 119950602A5414 PLATE BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND NR 3 PYLON LOWER RIGHT AFT PLATE CRACKED 2 INCHES LONG AND .75 INCH PAST STOP DRILL. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950630005081995063000508NM 1995 6 30 95ZZZM174 119950602A5720096520357 ROD BOEING747 747122 1384872NM LT WING LE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND LEFT WING LEADING EDGE SUPPORT ROD CRACKED AREA OF NR 2 LEFT LEADING EDGE PDU. REMOVED AND REPLACED SUPPORT ROD AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950630005091995063000509NM 1995 6 30 95ZZZM175 119950602A575365B0853351 MID FLAP BOEING747 747122 1384872NM LT WING WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND LEFT WING OUTBOARD MID FLAP OUTBOARD END WORN DOWN TO HONEYCOMB TOP SIDE. REPAIRED PER BOEING SRM 51-40-06 AND 51-70-09. 2L74 4F A20WE 19950630005101995063000510NM 1995 6 30 95ZZZM176 119950602A5730 PANEL BOEING747 747122 1384872NM RT WING DELAMINATING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND RIGHT WING BOTTOM LEADING EDGE PANEL REPAIR IS DELAMINATING AT THREE CORNERS AFT OF NR 16 LEADING EDGE JACK SCREW. REPAIRED AS PER BOEING 747 SRM 51-40-06. 2L74 4F A20WE 19950630005111995063000511NM 1995 6 30 95ZZZM177 119950530A5320 RIVET BOEING747 747122 1384872NM BS 2040 SHEAR A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIVET HEAD SHEARED ON LAP SEAM NR 34R STATION 2040 JUST AFT OF BULK CARGO DOOR. REMOVED RIVET, NO CORROSION FOUND, CLEANED AND SEALED AREA AND REPLACED RIVET AS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950630005121995063000512NM 1995 6 30 95ZZZM178 119950530A575165B02200X SKIN BOEING747 747122 1384872NM LT AILERON PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND SMALL PUNCTURE (1.5 INCH BY .5 INCH) LEFT WING INBOARD AILERON LOWER SKIN ALONG OUTER EDGE. SANDED AREA AND APPLIED FILLER PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950630005131995063000513SO 1995 6 30 95ZZZM179 219950531A85306461401 STUD CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO NR 2 CYL RT ENG BROKEN A FAHAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO1926371 579 402C0327 266829H DEPARTED FROM INAGUA, BAHAMAS, AFTER ABOUT 20 MINUTES RT ENGINE OIL PRESSURE DROPPED TO RED LINE AND ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO INAGUA. AFTER INSPECTION THE RT ENG, FOUND 4 STUDS ON NR 2 CYLINDER BROKEN. REMOVED THE CYLINDER AND REPLACED THE BROKEN STUDS, RAN THE ENGINE AND IT CHECKED OK. AIRCRAFT WAS BROUGHT BACK TO MIAMI AND AIRMARK ENGINES SENT A MECHANIC TO OUR FACILITY TO OBSERVE THIS FAILURE. AIRMARK ENGINES RECOMMENDED TO REPLACE THE NR 2 CYLINDER AND ALL THE HOLD DOWN STUDS. 1L72 3O3 O A7CE E8CE 19950630005141995063000514CE 1995 6 30 95ZZZM180 119950609A5210 DOOR SEAL BEECH 1900 1900C 1154161CE AIRSTAIR DOOR DISLODGED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW0190YV UC90 EN ROUTE TO UTICA, NY, AIRCRAFT WAS 17,000 FT WHEN DOOR SEAL STARTED LEAKING (APPROX 2000 TO 3000 FEET CABIN ASCENT). AIRCRAFT DESCENDED TO 10,000 FEET AND WAS ABLE TO MAINTAIN 3000 FEET CABIN ALTITUDE. AFTER LANDING INSPECTION SHOWED DOOR SEAL WAS DISLODGED AT UPPER RT CORNER. DOOR SEAL WAS RESECURED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA24CE 19950630005151995063000515WP 1995 6 30 95ZZZM181 219950526A72613103314 OIL PUMP BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RT ENGINE FAILED A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL07850JS 826 P63148 FLT NR 4114 - DURING APPROACH TO DAY, RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO. CREW SHUTDOWN AND SECURED RT ENGINE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ENGINE AND DISCOVERED AFT OIL SCAVENAGE PUMP FAILED. REPLACED RT ENGINE IAW MM 71-00-00, GROUND RAN IAW MM 71-00-00. OPS CHECK, AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19950630005161995063000516EU 1995 6 30 95ZZZM182 119950514A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3101 1500215EU LT ENGINE OUT OF ADJUST A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07851JS 834 FLT 4062 - CREW ELECTED TO ABORT TAKEOFF WHEN LEFT ENGINE FAILED TO ACHEIVE TARGET TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL ADJUSTED LEFT ENGINE TORQUE SIGNAL CONDITIONER IAW MM 72-00-00, CONDUCTED ENGINE GROUND RUNS IAW MM 72-00-00. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950630005171995063000517NM 1995 6 30 95ZZZM183 119950608A5270622EN71 SWITCH BOEING747 747121 1384871NM CARGO DOOR OUT OF ADJUST A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23832FT 20347 MAINTENANCE FERRY FLIGHT NR 832 OUT OF JFK (UNPRESSURIZED) LOWER AFT CARGO DOOR LIGHT CAME ON DURING CLIMB-OUT. RETURNED TO JFK. ADJUSTED VENT DOOR SWITCH. 2L74 4F A20WE 19950630005181995063000518NE 1995 6 30 95ZZZM184 219950609A7230 COMP BLADES BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE ENG FAILED A P5CAE ENGINE SHUTDOWN EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 WP23854FT673865985 19754 662590 THREE HOURS INTO FLIGHT CLIMBING FROM FL 330 TO FL 370, EXPERIENCED SHUDDER, MUFFLED BOOM, EGT RISE TO 920 DEGREES, EGT WARNING LIGHT, ERP AND N1 LOSS FOLLOWED BY EGT DROP AND ENGINE FAILURE. SHUT DOWN ENGINE, VISUAL INSPECTION NO APPARENT PHYSICAL DAMAGE. FLIGHT CONDITIONS, SMOOTH, VMC. PERFORMED INSPECTION OF ENGINE PER MM 71-00-2 AND 71-00-46. WHICH REVEALED DAMAGE TO 8TH STAGE. ENGINE TO BE REPLACED. 2L74 4F4 F A20WE E20EA 19950630005191995063000519SO 1995 6 30 95ZZZM185 119950602A3260922AA2YA6PZ722 PROXIMITY SENSOR EMB 120 EMB120RT SO NLG OUT OF ADJUST A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17251YV 120251 SFO - NOSE GEAR RED 'B' LIGHT REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE DEFERRED LANDING GEAR 'B' POSITION INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL WITH THE ADJUSTMENT OF THE NOSE GEAR 'B' SYSTEM UPLOCK PROXIMITY SENSOR. (M) 2L72 4T RTA31SO 19950630005201995063000520SO 1995 6 30 C2XA95CL092 119950612A3260922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0912715 120125 FLT NR 3276 - RIC-CLE - AFTER TAKEOFF, TWO RED LEFT MAIN 'A' AND 'B' RED LIGHTS ILLUMINATED AND A VIBRATION WAS FELT. RECYCLED GEAR WITH SAME RESULT. RETURNED TO RIC. MAINTENANCE INSPECTED AND RELEASED FOR FERRY FLIGHT TO CLE. IN CLE MAINTENANCE ADJUSTED LEFT GEAR UPLOCK PROXIMITY SENSOR IAW EMB 120 MM 32-61-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950630005211995063000521SO 1995 6 30 C2XA95CL093 119950613A32302112600000 ROD END EMB 120 EMB120RT SO LT MLG WORN OUT A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0912715 120125 FLT NR 3150 - DTW-CLE - AFTER TAKEOFF LANDING GEAR SELECTED UP, LEFT MAIN GEAR REMAINED DOWN, LANDING GEAR RED 'A' AND 'B' LIGHTS ILLUMINATED. RETURNED TO DTW. MAINTENANCE INSPECTED AND RELEASED FOR FERRY FLIGHT TO CLE. IN CLE MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR ROD END. ADJUSTED IAW EMB 120 MM 32-32-10. OPS CHECKED GOOD IAW 32-32-00 AND 32-30-00. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950630005221995063000522EU 1995 6 30 C2XA95IA099 119950601A33503011180 EEL POWER SUPPLY AEROSPATR42 ATR42320 8680930EU CABIN MALFUNCTIONING A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0993840 271 IAH - DURING A LINE CHECK INSPECTION, THE FIRST THREE AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. UPON TROUBLESHOOTING, THE NR 2 POWER SUPPLY/BATTERY WAS FOUND MALFUNCTIONING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY, THE LIGHTS OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19950630005231995063000523SO 1995 6 30 C2XA95IA101 119950615A571312016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916718 120136 IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND TO BE CRACKED, BETWEEN RIBS 8 AND 9. MAINTENANCE PERFORMED A REPAIR TO THE AFFECTED STRINGER BY REMOVING THE CRACKED SECTION OF THE STRINGER AND INSERTING A STRINGER SPLICE. ALL WORK WAS ACCOMPLISHED IN ACCORDANCE WITH EMBRAER DER FAX EST 269/95, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950630005241995063000524SO 1995 6 30 WTAA950203 119950531A3260 WARNING LIGHT EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17280UE 120090 SFO - CREW FAILED TO RECEIVE NOSE GEAR 'GREEN' DOWN AND LOCKED INDICATIONS ON EITHER 'A' OR 'B' SYSTEM DURING INITIAL GEAR EXTENSION. GEAR POSITION INDICATION NORMAL AFTER CREW CYCLED LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING POSITION INDICATION SYSTEM. NO DEFECTS NOTED. PERFORMED GEAR SWING. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950630005251995063000525EU 1995 6 30 WTAA950205 119950605A771231024575 TORQUE RING BAG JETSTMJETSTM3101 1500215EU LT ENGINE SHORTED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17402UE 734 SFO - LEFT ENGINE TORQUE GAUGE INDICATION FLUCTUATED PLUS AND MINUS 10 PERCENT DURING CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE SWAPPED TO 'BRIDGE 1' ON ENGINE TORQUE RING. TORQUE INDICATIONS NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950630005261995063000526NM 1995 6 30 95ZZZM186 119950524A3350RPS1B CHARGER BOEING737 7374B7 1384702NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19449US 24893 CLT - EXTERIOR EXIT LIGHTS AT THE AFT ENTRY DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSY. REFERENCE USAA950531. 2L72 4F RTA16WE 19950630005271995063000527NM 1995 6 30 95ZZZM187 119950606A3260696R10SL3S135 CONNECTOR BOEING727 72751C 1384015NM NLG CORRODED A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE07435EX 19288 THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NOSE GEAR POSITION SWITCH CONNECTOR, OPS CHECKED GOOD. (M) 2L73 4F A3WE 19950630005281995063000528SO 1995 6 30 C2XA95CL088 119950602A27503075001017 FLAP CONTL UNIT EMB 120 EMB120RT SO AVIONICS BAY FAILED A C2XAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SW09127156490 0196 120125 FLT 3136 - CLE-ROC - AFTER LANDING WITH FLAPS AT 45 DEGREES, INBOARD PAIR OF FLAPS STAYED AT 45 UPON FLAP RETRACTION. FLAP CONTROL PANEL READ INBOARDS AT 45, ANALOG GAUGE READS FLAPS AT 25 DEGREES. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-06. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950630005291995063000529SO 1995 6 30 C2XA95CL095 119950531A524312007993612 ACCESS DOOR EMB 120 EMB120RT SO RT HYDRAULIC BAYDEPARTED ACFT A C2XAK NONE D INFLIGHT SEPARATION CRCRUISE 1 SW0927716 120128 FLT NR 3308 - TOL-CLE - RIGHT HYDRAULIC BAY ACCESS DOOR SEPARATED FROM AIRCRAFT IN CRUISE FLIGHT, ALSO DAMAGED SKIN AFT OF EMERGENCY EXIT. MAINTENANCE INSTALLED NEW HYDRAULIC BAY ACCESS DOOR IAW EMB SRM 51-30-01 AND 51-40-00. REPAIRED SMALL HOLE IN FUSELAGE IAW EMB SRM 53-00-01. ALSO, DENT IN FUSELAGE PLACED ON DMI NR 515747 IAW EMB SRM 53-00-01. (M) 2L72 4T RTA31SO 19950630005301995063000530EU 1995 6 30 SIMA951522 119950601A33503011210 EEL ASSY AEROSPATR72 ATR72212 EU GALLEY INOP A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21270AT6413 8604 174 270 DFW - FLT 3812 - EMERGENCY EXIT LIGHT OUT ON AIRSTAIR DOOR. MAINTENANCE REMOVED AND REPLACED LIGHT ASSY. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950630005311995063000531EU 1995 6 30 SIMA951541 119950603A3610600250 SEAL AEROSPATR72 ATR72212 EU CROSS FEED VALVELEAKING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21408AT 408 DFW - FLT 3863 - NR 2 ENGINE BLEED LEAK WHEN CROSS FEED ON. REPLACED SEALS AT CROSS FEED VALVE UNDER FLOOR. PERFOREMD LEAK CHECKS. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950630005321995063000532EU 1995 6 30 SIMA951591 119950608A61208210153 PCU SAAB SF340 SF340A 7850100EU RT ENG MALFUNCTIONED A ASIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW2189MQ 8210153 340A089 DFW - FLT NR 3877 - DURING TAKEOFF RIGHT ENGINE PROPELLER RPM FLUCTUATED APPROXIMATELY 200 RPM. TAKEOFF ABORTED AND AIRCRAFT RETURNED TO GATE. REMOVED AND INSPECTED PROP CONTROL UNIT. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950630005331995063000533EU 1995 6 30 SIMA951592 119950608A77143039242 NH SENSOR AEROSPATR72 ATR72212 EU LT ENG MALFUNCTIONED A SIMAK NONE N FALSE WARNING CLCLIMB 1 SW21369AT3106 CH10259 369 GRR - FLT 4194 - NR 1 ENGINE TQ SURGED 30 TO 35 PERCENT AFTER TAKEOFF. AIRCRAFT CONTINUED TO DESTINATION WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND INSPECTED SENSOR, SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950630005341995063000534EU 1995 6 30 SIMA951641 119950613A32301005383340 SELECTOR VALVE AEROSPATR72 ATR72212 EU LT MLG WW FAILED A SIMAO OTHER J WARNING INDICATION DEDESCENT 1 SW21270AT 88 270 DFW - FLT 3810 - LANDING GEAR FAILED TO EXTEND WHEN SELECTED. EMERGENCY EXTENSION WAS SELECTED AND THE GEAR EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND INSPECTED GEAR SELECTOR VALVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950630005351995063000535EU 1995 6 30 SIMA951642 119950613A7712311649902 TQ SENSOR AEROSPATR72 ATR72212 EU NR 2 ENGINE MALFUNCTIONED A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21429AT CH491 429 DFW - FLT 3805 - AIR TURN BACK, NR 2 ENGINE TORQUE SURGED WHILE LEVEL AT 4000 FEET ON DEPARTURE. REMOVED AND INSPECTED NR 2 ENGINE TORQUE SENSOR AND INTERTURBINE BLEED VALVE. COMPLIED WITH OVER TORQUE INSPECTION. GROUND OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950630005361995063000536NM 1995 6 30 USAA950530 119950523A3350 EEL WIRE BOEING737 7374B7 1384702NM CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19449US 24893 MIA - SEAT MOUNTED EMERGENCY EXIT LIGHTS AT ROWS 24 AND 25 DO NOT ILLUMINATE. MAINTENANCE REPAIRED A BROKEN WIRE AT ROW 24. RELEASED EXIT LIGHT ON ROW 25 ON MEL 33-19A. REPLACED CHARGER (P/N RPSIB) AND BATTERY PACK. (M) 2L72 4F RTA16WE 19950630005371995063000537NM 1995 6 30 USAA950531 119950524A335020131A EEL BATTERY PACK BOEING737 7374B7 1384702NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19449US 24893 CLT - EXTERIOR EXIT LIGHTS AT THE AFT ENTRY DOORS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND CHARGER ASSY. (M) 2L72 4F RTA16WE 19950630005381995063000538NE 1995 6 30 USAA950548 219950531A73208063207 MEC BOEING737 7374B7 1384702NM GE CFM56 CFM563B1 13802NE NR 1 ENGINE FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19782AU 25021 CLT - FLT 44 - FLIGHT EN ROUTE FLL TO LGA WHEN NR 1 ENGINE PARAMETERS BEGAN FLUCTUATING. CREW DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE MEC. PERFORMED TRIM RUN AND LEAK CHECK, OPS CHECKS OK. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F4 FRTA16WE E2GL 19950630005391995063000539NM 1995 6 30 USAA950551 119950522A5320 SILL BOEING737 7373B7 1384580NM BS 794-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND DOOR SILL SKIN CORRODED BS 794-847 IN AFT CARGO DOOR CUTOUT. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005401995063000540NM 1995 6 30 USAA950552 119950501A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 2 INCH CORRODED AREA, BS 328 FLOORBEAM, RBL 14 AND RBL 21. REPAIRED PER TR 53-10-03 AND SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005411995063000541NM 1995 6 30 USAA950553 119950501A532069407654 ANGLE BOEING737 7373B7 1384580NM BS 312-372 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 60 INCH CORRODED AREA S-17L, BS 312-372 (FORWARD ENTRY DOOR SILL ANGLE). REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005421995063000542NM 1995 6 30 USAA950554 119950505A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 294-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TOTAL AREA OF CORROSION .25 INCH BY 10 INCH, 6 INTERCOSTALS CORRODED AND NUTPLATE HOLES BS 294-344, 3 AT LBL 11 BS 294-344, 3 AT RBL 11 BS 294-344. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005431995063000543NM 1995 6 30 USAA950555 119950503A53201128907 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION OUT OF LIMITS .25 INCH BY 10 INCHES ON INTERCOSTAL AT BS 947 THROUGH 967 RBL 10 INCHES. REPAIRED PER SRM 51-10-0. CORROSION TASK NR C53-108-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005441995063000544NM 1995 6 30 USAA950556 119950504A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 907-947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19396US27247 23318 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA ON INTERCOSTAL AT CABIN BS 907 THROUGH 947 RBL 10 INCHES. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005451995063000545NM 1995 6 30 USAA950557 119950424A5315 FLOORBEAM BOEING737 737401 1384701NM FS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION (FULL WIDTH OF T-CAP) STATION 986.5 FLOORBEAM FROM 44 LBL TO 44 RBL. REPAIRED PER SRM 51-70-13 EA 39205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005461995063000546NM 1995 6 30 USAA950558 119950428A5315 FLOORBEAM BOEING737 737401 1384701NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROX 1 INCH BY 5 INCH CORROSION ON FLOORBEAM AT STATION 947, RBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005471995063000547NM 1995 6 30 USAA950559 119950428A5315 FLOORBEAM BOEING737 737401 1384701NM FS 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH AREA ON FLOORBEAM, CORRODED AT STATION 947, LBL 12. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005481995063000548NM 1995 6 30 USAA950560 119950502A5320 SUPPORT BOEING737 737401 1384701NM FS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 20 INCH AREA CORRODED ON FLOOR SUPPORT AT STATION 947 TO STATION 967, LBL 50. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005491995063000549NM 1995 6 30 USAA950561 119950425A532065C340593 INTERCOSTAL BOEING737 737401 1384701NM BS 967-947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 6 INCH BY 1 INCH TOTAL CORROSION ON INTERCOSTAL, BETWEEN BS 967 AND BS 947 LBL 16 INCHES. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-10-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005501995063000550NM 1995 6 30 USAA950562 119950426A532065C333701 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 7 INCH BY 1 INCH CORROSION ON INTERCOSTAL BETWEEN BS 947 AND BS 967 RBL 25 INCHES. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005511995063000551NM 1995 6 30 USAA950563 119950503A53206546812169 INTERCOSTAL BOEING737 737401 1384701NM STA 967-986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 12 INCHES CORRODED AREA ON INTERCOSTAL AT STATION 967 TO 986.5, LBL 17. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005521995063000552NM 1995 6 30 USAA950564 119950509A5315 FLOORBEAM BOEING737 737401 1384701NM STA 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 10 INCHES CORRODED AREA ON FLOORBEAM AT STATION 967 RBL 9 TO RBL 36. REPAIRED PER EA 39247. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005531995063000553NM 1995 6 30 USAA950565 119950502A5320 ANGLE BOEING737 737401 1384701NM DOOR THRESHOLD CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 36 INCHES OF CORROSION, AFT ENTRY THRESHOLD. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005541995063000554NM 1995 6 30 USAA950566 119950424A5320 ANGLE BOEING737 737401 1384701NM DOOR THRESHOLD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 2 INCHES BY 30 INCHES 'Z' ANGLE IN THRESHOLD OF AFT SERVICE DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-2, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005551995063000555NM 1995 6 30 USAA950567 119950427A5320 DOOR SILL BOEING737 737401 1384701NM BS 807-845 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19415US19714 23883 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH DIAMETER AND 3 INCH DIAMETER SPOTS OF CORROSION 40 TO 50 PERCENT LOSS TO .375 INCH DIAMETER 100 PERCENT LOSS 3 INCH BY 4 INCH CORROSION BS 807 TO BS 845 ON DOOR SILL BELOW AFT CARGO DOOR. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005561995063000556NM 1995 6 30 USAA950568 119950427A5320 HAT CHANNEL BOEING737 7373B7 1384580NM BS 308 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19506AU27233 23381 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 5 INCH CORRODED AREA ON FLOOR HAT CHANNEL, BS 308 (AFT BULKHEAD FOR FORWARD LAVATORY). REPAIRED PER SRM 51-10-1 FIG 1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005571995063000557NM 1995 6 30 USAA950569 119950516A53206545834257 INTERCOSTAL BOEING737 737301 1384611NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27236 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH AREA OF CORROSION ON INTERCOSTALS BS 328 THROUGH BS 344 RBL 12 AND LBL 12. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005581995063000558NM 1995 6 30 USAA950570 119950505A5314 KEEL BEAM BOEING737 737301 1384611NM BS 540 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27235 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK, 5.25 INCH BY 2 INCH CORRODED AREA BS 540, RBL 6.5 (LOWER FLANGE OF KEEL BEAM). REPAIRED PER EA 5369-20 EA 39273 EA 39272. CORROSION TASK NR C53-212-01. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005591995063000559NM 1995 6 30 USAA950571 119950530A5315 FLOORBEAM BOEING737 737301 1384611NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27236 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH TOTAL CORROSION, CORROSION AT SCREW HOLES ON FLOORBEAM AT BS 312 LBL 12 INCHES THROUGH RBL 24 INCHES. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005601995063000560NM 1995 6 30 USAA950572 119950515A5315 FLOORBEAM BOEING737 737301 1384611NM FS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27236 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AT STATION 328 RBL 48. REPAIRIED PER 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005611995063000561NM 1995 6 30 USAA950573 119950512A5315 FLOORBEAM BOEING737 737301 1384611NM FS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27236 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 SQUARE INCHES OF CORROSION OF FLOORBEAM AT STATION 344 BL 0 TO LBL 12. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005621995063000562NM 1995 6 30 USAA950574 119950530A53206545834260 INTERCOSTAL BOEING737 737301 1384611NM BS 312-328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19336US27236 23233 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 15 INCH CORRODED AREA ON INTERCOSTAL AT BS 312 THROUGH BS 328. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950630005631995063000563EU 1995 6 30 USAA950577 119950516A5320 WINDOW POST FOKKERF28 F28MK4000 4990810EU RT NR 2 WINDOW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19482US20272 11231 PIT - DURING AN FC-6 CHECK INSPECTION, FOUND .75 INCH CRACK IN RIGHT NR 2 WINDOW POST (TYPE 3) REF SIP 53-10-08. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-10-01 REV A. (M) 2L72 4F RTA20EU 19950630005641995063000564EU 1995 6 30 USAA950578 119950516A5320 DOOR FRAME FOKKERF28 F28MK4000 4990810EU CARGO COMPT DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19482US20272 11231 PIT - DURING AN FC-6 CHECK INSPECTION, FOUND 2 DENTS IN THE FORWARD SIDE OF THE AFT CARGO COMPARTMENT DOOR FRAME IN AREA OF HOLD OPEN ROD SUPPORT. INSTALLED DOUBLER REPAIR PER SRM 53-02-16 PG 4. (M) 2L72 4F RTA20EU 19950630005651995063000565EU 1995 6 30 USAA950582 119950526A5330 SKIN FOKKERF28 F28MK4000 4990810EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19498US29573 11181 PIT - DURING SCHEDULED SIP VISIT INSPECTION, FOUND .375 INCH CRACK IN THE SED APERATURE AT THE FORWARD UPPER CORNER REF SIP 53-10-20 OUTSIDE LAYER OF SKIN (EDDY CURRENT INSPECTION). CUT OUT CRACKED AREA AND INSTALLED FILLER AND DOUBLER REPAIRS (2 EACH) PER SRM 53-02-16 PG 7, 8 AND 9. (M) 2L72 4F RTA20EU 19950630005661995063000566NM 1995 6 30 95ZZZZ270 119950510A5313 STRINGER BOEING727 7272J7 138400ENM FS 950 CRACKED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07128NA 20879 IN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER. 2L73 4F A3WE 19950630005671995063000567NM 1995 6 30 95ZZZZ271 119950321A5313 STRINGER BOEING727 7272J7 138400ENM FS 950 CRACKED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07128NA 20879 IN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, CHORD STRINGER (P/N 65-56441-7) WAS FOUND TO BE CRACKED AT FWD BOLT HOLES. THE ED IN THAT AREA SEEMS TO BE MARGINAL. 2L73 4F A3WE 19950630005681995063000568NM 1995 6 30 95ZZZZ273 119950510A5313 STRINGER BOEING727 7272J7 138400ENM STA 950 CRACKED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07128NA 20879 IN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT STRINGER (P/N 65-56441 WAS FOUND TO BE CRACKED AT BOLT HOLES FWD END OF STRINGER. 2L73 4F A3WE 19950630005691995063000569NM 1995 6 30 95ZZZZ274 119950512A5313 STRINGER BOEING727 7272J7 138400ENM BS 950 CORRODED B KT3RK NONE O OTHER ININSP/MAINT 1 WP07128NA 20879 IN THE PROCESS OF COMPLYING WITH S/B 53-159 BELLY SKIN REPLACEMENT, STRINGER (P/N 65-56441-8) WAS FOUND CORRODED ALONG TOPSIDE. STRINGER WAS REPLACED. 2L73 4F A3WE 19950630005701995063000570NM 1995 6 30 AWXA9500356 119950605A3350 EEL CONNECTORS BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 11 AND ROW 19. RESEATED CONNECTIONS, OPS CHECK GOOD. (Z) 2L72 4F RTA16WE 19950630005711995063000571NM 1995 6 30 AWXA9500369 119950610A5330 SKIN BOEING737 737277 1384570NM R2 DOOR AREA CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND R2 DOOR FUSELAGE TORQUE TUBE CUTOUT UPPER FORWARD CORNER CRACKED. FABRICATED DOUBLER REPAIR PER SRM 53 30 3 FIG 21A AND INSTALLED REPAIR PER SRM 53 30 03 FIG 21A. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005721995063000572NM 1995 6 30 AWXA9500370 119950610A5330 SKIN BOEING737 737277 1384570NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND L1 DOOR UPPER HINGE CUTOUT CRACKED. ROUTED OUT SKIN, BONDED AND INSTALLED REPAIR PER SRM 53 30 3 FIG 21 AND ER 2 53 32 15. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005731995063000573NM 1995 6 30 AWXA9500371 119950610A5330 SKIN BOEING737 737277 1384570NM FS 727 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND SEVERAL FASTENERS CORRODED ON KEEL BEAM IN AREA OF STA 727. REMOVED CORROSION PER SRM 53 10 01 FIG 7 AND INSTALLED DOUBLER PER SRM 53 30 03 FIG 28. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005741995063000574NM 1995 6 30 AWXA9500372 119950610A523065C8073535 WEB BOEING737 737277 1384570NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FORWARD BAG PIT DOOR AFT LOWER CORNER WEB CRACKED. REPLACED WEB PER SRM 51 30 2. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005751995063000575NM 1995 6 30 AWXA9500373 119950610A52306548921509 ANGLE BOEING737 737277 1384570NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FORWARD BAG PIT DOOR AFT LOWER CORNER 'T' ANGLE CRACKED. REPLACED 'T' ANGLE PER SRM 51 30 2. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005761995063000576NM 1995 6 30 AWXA9500374 119950610A52306846921169 ANGLE BOEING737 737277 1384570NM CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FORWARD BAG PIT AFT LOWER CORNER CRACKED. REMOVED AND REPLACED AFT LOWER DOOR FRAME PER SRM 51 40 3. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005771995063000577NM 1995 6 30 AWXA9500375 119950610A5320 DOOR FRAME BOEING737 737277 1384570NM FWD BAG PIT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CRACK IN FORWARD BAG PIT DOOR CUTOUT AFT FRAME AT STOP NR 5. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE IAW SRM 51 40 3. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005781995063000578NM 1995 6 30 AWXA9500377 119950610A5210 WEB BOEING737 737277 1384570NM R2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28178AW41581 22645 PHX - DURING SCHEDULED C8 INSPECTION, FOUND R2 DOOR INNER TORQUE BOX WEB CRACKED. REMOVED CRACKED WEB AND INSTALLED TYPICAL WEB REPAIR PER SRM 51 30 02 AND SRM 51 40 02. TOTAL CYCLES 34804. (Z) 2L72 4F RTA16WE 19950630005791995063000579NM 1995 6 30 CAL950442 119950517A5330 SKIN BOEING737 737247 138448DNM BS 449-469 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424666439 20129 SVC - FLT 31J - INSPECTION FOUND A 10 INCH CRACK IN FUSELAGE SKIN AT BS 449 TO 469 STR 16R. THE CRACKED SECTION WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-03. (Z) 2L72 4F A16WE 19950630005801995063000580NM 1995 6 30 CAL950443 119950517A5320 LAP SEAM BOEING737 737247 138448DNM BS 420-440 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424666439 20129 SVC - FLT 31J - INSPECTION FOUND THE LAP SEAM AT STRINGER 429 CORRODED. THE SEAM WAS OPENED FROM BS 420 TO 440 AND THE CORROSION WAS REMOVED. A REPAIR WAS PERFORMED IAW SRM 51-10-2, 51-10-6, 51-30-2 AND SERVICE BULLETIN 737-53-1087. (Z) 2L72 4F A16WE 19950630005811995063000581WP 1995 6 30 ORJA9540 119950511A5330 SKIN DOUG DC9 DC987 3022087WP FS 420-455 DENTED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 EXTERIOR SKIN, RT STA 420-455, B/T LONGS 19 AND 20, 3 AREAS OF DAMAGE. FABRICATED DOUBLER AND FINGER DOUBLER INSTALLED FAB PARTS PER SM 53-04 FIG 38. (Z) 2L72 4F RTA6WE 19950630005821995063000582WP 1995 6 30 ORJA9541 119950516A5320 STRAKE DOUG DC9 DC987 3022087WP FS 168-180 DENTED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 RT STRAKE, AFT BETWEEN STA 168 AND 180 AND S21 AND 22 DENTED IN TWO PLACES. FABRICATED AND INSTALLED FLUSH SKIN REPAIR PER SRM 53-04 FIG 38. (Z) 2L72 4F RTA6WE 19950630005831995063000583WP 1995 6 30 ORJA9542 119950518A5330 SKIN DOUG DC9 DC987 3022087WP FS 209 DENTED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 STA 209 STR 17 FUSELAGE HAS A DENT JUST AFT OF RT GALLEY DOOR MEASURING 3 INCHES LONG BY 2.5 WIDE BY .103 DEEP, DENT IS OUT OF LIMITS PER SRM 53-04 FIG 38. CUT 2.5 DIA HOLE TO REMOVE DAMAGE. FAB DOUBLER AND FILLER, INSTALLED PER SRM 53-04 FIG 38. (Z) 2L72 4F RTA6WE 19950630005841995063000584WP 1995 6 30 ORJA9543 119950526A5320 FLOOR SUPPORT DOUG DC9 DC987 3022087WP FS 200 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 LEVEL 2 CORROSION ON FLOOR SUPPORT LBL 13 RBL 40 STA 200. RMOVED AND REPLACED 3 EACH, FLOORBOARD SUPPORTS PER SRM 51-10-2. (Z) 2L72 4F RTA6WE 19950630005851995063000585WP 1995 6 30 ORJA9544 119950526A5347 SEAT TRACK DOUG DC9 DC987 3022087WP FS 150-200 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 LEVEL 2 CORROSION, ON SEAT TRACK LBL 7 STA 150-200. FABRICATED AND INSTALLED STRAP DOUBLERS PER DWG SKB009418N00132. (Z) 2L72 4F RTA6WE 19950630005861995063000586WP 1995 6 30 ORJA9545 119950526A5320 SUPPORT DOUG DC9 DC987 3022087WP FS 160 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 LEVEL 2 CORROSION, ON SUPPORT STA 160 LBL 14-44 WL 200. REMOVED CORROSION AND TREATED PER SRM 51-10-3. CUT AREA FABRICATED DOUBLER AND FILLER PER SRM 51-01 AND INSTALLED PER SRM 51-10-4. (Z) 2L72 4F RTA6WE 19950630005871995063000587EU 1995 6 30 QXEA9500200 119950628A3234A76209405 GEAR HANDLE FOKKER FOKKERF28 F28MK1000 4990808EU COCKPIT LACK OF LUBE A QXEAK NONE O OTHER CLCLIMB 1 NM09469US 11096 PDX - LANDING GEAR HANDLE STICKS IN THE DOWN POSITION. HANDLE CAN BE MOVED UP WITH SLIGHT FORCE. GEAR HANDLE, TELEFLEX CABLE AND COAX CABLE WERE LUBED AND HANDLE OPS CHECKED GOOD. ANTI-RETRACTION SOLENOID VERIFIED AS WORKING CORRECTLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950630005881995063000588NE 1995 6 30 SWAA950484 219950625A7210641000 GEARBOX BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A SWAADE RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW0796SW 23055 DURING CLIMBOUT FROM LIT, CREW EXPERIENCED NR 1 ENGINE LOW OIL PRESSURE INDICATION WITH ASSOCIATED WARNING LIGHT. CREW PERFORMED NR 1 ENGINE SHUTDOWN CHECKLIST. AIRCRAFT RETURNED TO LIT AND MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE. REPLACED NR 1 ENGINE OIL PUMP, ENGINE GEARBOX ASSEMBLY, AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. OIL PUMP P/N: 734340. S/N OFF: AV2800. S/N ON: AV3829. 2L72 4F4 F A16WE E2EA 19950630005891995063000589NM 1995 6 30 SWAA950485 119950624A2782654465116 ACTUATOR BOEING737 7372H4 138448CNM NR 4 LE SLAT FAILED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0774SW 22674 DURING CLIMBOUT FROM ELP, NR 4 L/E SLAT WOULD NOT FULLY RETRACT. INDICATED IN TRANSIT. CYCLED SYSTEM TWICE, NO HELP. AIRCRAFT RETURNED TO ELP AND MADE AN UNEVENTFUL LANDING. REPLACED NR 4 L/E SLAT ACTUATOR PER BOEING M/M. 2L72 4F A16WE 19950630005901995063000590NM 1995 6 30 SWAA950486 119950624A5330 SKIN BOEING737 7372H4 138448CNM BS 227.8 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0726SW 21117 DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L. REPAIRED PER DALFORT XEA X2-53-154. 2L72 4F A16WE 19950630005911995063000591NM 1995 6 30 SWAA950487 119950624A5330 SKIN BOEING737 7372H4 138448CNM BS 227.8 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0726SW 21117 DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT THREE PLACES AT BS 227.8, BETWEEN S13 AND 16L. REPAIRED PER DALFORT XEA X2-53-154. 2L72 4F A16WE 19950630005921995063000592NM 1995 6 30 SWAA950488 119950624A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0726SW 21117 DURING SCHEDULED MAINT VISIT, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FORWARD AIRSTAIRS DOORWAY CUTOUT AT DOUBLER. REPAIRED PER DALFORT XEA X2-53-153. 2L72 4F A16WE 19950630005931995063000593NM 1995 6 30 SWAA950489 119950624A5313 STRINGER BOEING737 7372T4 1384492NM BS 1088 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 19L CRACKED AT END OF STUB, BS 1088. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630005941995063000594NM 1995 6 30 SWAA950490 119950624A5313 STRINGER BOEING737 7372T4 1384492NM BS 1047 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07722WN 22698 DURING SCHEDULED 1/2 D CHECK, FOUND A HOLE IN STRINGER 27L ON INNER J FLANGE, BS 1047. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950630006041995063000604EA 1995 6 30 95ZZZX3278 219950612A741467542 BEARING BNORM BN2 BN2A26 1520226EU LYC O540 O540E4C5 41532EA LT MAG DRIVE FAILED A ADCRAK NONE O OTHER ININSP/MAINT 1 WP1332MR 1770 891 L1351340A DURING COMPLIANCE OF AD78-09-07R3 MAGNETO IMPULSE COUPLING, DISCOVERED BEARING ASSY LOST ITS BALL BEARING CAGE ASSY. ONE-HALF OF CAGE ASSY WAS FOUND IN THE OIL SUMP. THIS COULD LEAD TO COMPLETE FAILURE OF ENGINE IF UNDETECTED. SUBMITTER STATED THIS IS FOURTH KNOWN DISCOVERY IN THE FLEET. 1H72 3O3 O A17EU E295 19950707000061995070700006NM 1995 7 7 95ZZZX3299 119950525A331061213 LIGHT BALLAST BOEING727 72725 1384006NM FLIGHT DECK BURNED A PCSAGA O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO178104N 18255 SLC/OMA - DURING CRUISE, CREW EXPERIENCED SMOKE IN THE COCKPIT. THE CREW DONNED OXYGEN MASKS AND LANDED UNEVENTFULLY AT DSM. MAINTENANCE FOUND ONE BALLAST FOR THE GLARESHIELD LIGHTS BURNED. 2L73 4F A3WE 19950707000071995070700007WP 1995 7 7 95ZZZX3300 119950609A575357511852 SUPPORT FITTINGS DOUG DC8 DC863 302198AWP RT TE FLAP BROKEN A ARRXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 WP15964R 46000 KDAY/KPDX - FLT 102 - DURING DESCENT INTO KPDX, FLAPS AT 12 DEGREES OK. GREATER THAN 12 DEGREES CAUSES EXCESSIVE RIGHT ROLL. AT 35 DEGREES INDICATION IS 28 DEGREES. SD - AFTER LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND BOTH T/E FLAP SUPPORT FITTINGS BROKEN AT STA 219.498 AND THE OTBD FITTING AT STA 339.723 CRACKED. THE DAMAGED SUPPORT FITTINGS WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 19950707000081995070700008WP 1995 7 7 95ZZZX3301 119950609A575357511842 SUPPORT FITTINGS DOUG DC8 DC863 302198AWP RT TE FLAP BROKEN A ARRXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 WP15964R 46000 KDAY/KPDX - FLT 102 - DURING DESCENT INTO KPDX, FLAPS AT 12 DEGREES OK. GREATER THAN 12 DEGREES CAUSES EXCESSIVE RIGHT ROLL. AT 35 DEGREES INDICATION IS 28 DEGREES. SD - AFTER LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND BOTH T/E FLAP SUPPORT FITTINGS BROKEN AT STA 219.498 AND THE OTBD FITTING AT STA 339.723 CRACKED. THE DAMAGED SUPPORT FITTINGS WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 19950707000091995070700009WP 1995 7 7 95ZZZX3302 119950609A575357511862 SUPPORT FITTINGS DOUG DC8 DC863 302198AWP RT TE FLAP CRACKED A ARRXAO OTHER F FLT CONT AFFECTED DEDESCENT 1 WP15964R 46000 KDAY/KPDX - FLT 102 - DURING DESCENT INTO KPDX, FLAPS AT 12 DEGREES OK. GREATER THAN 12 DEGREES CAUSES EXCESSIVE RIGHT ROLL. AT 35 DEGREES INDICATION IS 28 DEGREES. SD - AFTER LANDING, MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND BOTH T/E FLAP SUPPORT FITTINGS BROKEN AT STA 219.498 AND THE OTBD FITTING AT STA 339.723 CRACKED. THE DAMAGED SUPPORT FITTINGS WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. 2L74 4F 4A25 19950707000101995070700010EU 1995 7 7 AALA950747 119950425A5330 SKIN FOKKERF28 F28MK0100 4990807EU FS 6805-7305 DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW071462C 11482 TULE - FUSELAGE SKIN DENTED AND SCRATCHED, FORWARD AND ABOVE LT FORWARD FUSELAGE BETWEEN STA 6805 TO STA 7305, BELOW STR 14. CUT OUT DAMAGE SECTION OF FUSELAGE SKIN. INSTALLED FILLER AND REPAIR DOUBLERS PER F-100 SRM 53-00-02, NR 2, SRM 51-70-06 NR 5, AND AARD 53-00-02 NR 3. (PERMANENT REPAIR.) TST 2821. CYCLES 2111. (X) 2L72 4F RT 19950707000111995070700011EU 1995 7 7 AALA950906 119950514A3231A633592 VALVE HYDROAIRE FOKKERF28 F28MK0100 4990807EU NLG DOOR BYPASSING A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071452B 11464 DFW - FLT 2012 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, NLG DID NOT RETRACT. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RT 19950707000121995070700012WP 1995 7 7 AALA950910 119950513A2150WWD398 CLAMP DOUG DC9 DC982 3022082WP LT ACM BROKEN A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07553AA 53083 DFW - FLT 789 - AFTER TAKEOFF DFW DURING CLIMB-OUT, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND AIRCRAFT RETURNED DFW, LANDING WITHOUT INCIDENT. REPLACED LT AIR CYCLE MACHINE SUPPLY DUCT CLAMP. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F A6WE 19950707000131995070700013NM 1995 7 7 AALA950972 119950528A3350A3060698101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071763 48553 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FOUND INOPERATIVE ON RIGHT SIDE OF FIRST CLASS SECTION. REPLACED CONNECTOR AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F RTA22WE 19950707000141995070700014NE 1995 7 7 C2XA95CL089 219950531A7250 TURBINE BLADE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE RT ENGINE MISSING A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW091880910455 090 120884 EWR/EWR - FLT 3848 - ABNORMAL VIBRATION AND NOISE COMING FROM RIGHT ENGINE DURING FEATHER AND UNFEATHER. NO NOISE WITH PROP BRAKE ON. BORESCOPE INSPECTION FOUND 1ST STAGE POWER TURBINE MISSING A BLADE. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. OPS CHECKED GOOD. RETURNED TO SERVICE 6-2-95. (X) 2H72 4T4 TRTA53EU E20NE 19950707000151995070700015WP 1995 7 7 ORJA9546 119950527A5320 SUBFLOOR DOUG DC9 DC987 3022087WP FS 200 CORROSION A ORJAK NONE O OTHER ININSP/MAINT 1 WP11752RA 49780 FUSELAGE STA 200, LBL 10-20 SUB-FLOOR STRUCTURE, HAS LEVEL 2 CORROSION AS SEEN FROM E AND E BAY. REMOVED CORRODED AREA, FAB, AND INSTALLED DOUBLER PER SRM 53-01, FIGURE 4. 2L72 4F RTA6WE 19950707000261995070700026WP 1995 7 7 9510079301 119950626A3260 PROX SWITCH DOUG DC9 DC982 3022082WP LT MLG OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01301RC 48054 DURING CLIMBOUT FROM PHX, THE LEFT MAIN GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT FURTHER INCIDENT. FOUND LEFT MAIN GEAR DOOR OPEN AND GEAR UPLOCK PROXIMITY SWITCHES OUT OF ADJUSTMENT. SECURED DOOR AND ADJUSTED SWITCHES PER MM 32-60-05. CYCLED GEAR SEVERAL TIMES, ALL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000271995070700027WP 1995 7 7 9510089301 119950504A3250 CONTROL VALVE DOUG DC9 DC982 3022082WP NLG STEERING MALFUNCTIONED A NWAAO OTHER O OTHER CLCLIMB 1 GL01301RC 48054 NOSE LANDING GEAR WOULD NOT RETRACT DURING TEST FLIGHT. REPLACED NOSE GEAR BUNGEE CYLINDER AND RESTRICTOR VALVES, WAS NO HELP. REPLACED STEERING CONTROL VALVE. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000281995070700028WP 1995 7 7 9510099908 119950624A213045016 PNEU SWITCHES DOUG DC9 DC931 3022065WP AFT ACCESS COMP MALFUNCTIONED A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION DEDESCENT 1 GL01958N 47254 LOSS OF CABIN PRESSURIZATION OCCURRED ON INITIAL DESCENT INTO MIA. CABIN ALTITUDE BEGAN CLIMBING AT A RATE OF 1000 FPM EVENTUALLY REACHING 12,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN. EMERGENCY DESCENT WAS MADE TO 25,000 FEET. CABIN PRESSURE WAS REGAINED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. REPLACED LEFT AND RIGHT SECOND SEGMENT CLIMB SWITCHES. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000291995070700029WP 1995 7 7 9510109930 119950626A2440HDX9A0113 RELAY DOUG DC9 DC931 3022065WP EXTERNAL POWER MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0189S 47042 GROUND SERVICE BUS FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED R2-48 EXTERNAL POWER GROUND SERVICE RELAY. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000301995070700030WP 1995 7 7 9510119942 119950624A3260 UPLOCK SWITCH DOUG DC9 DC932 3022066WP LT MLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL013991C 47175 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000311995070700031WP 1995 7 7 9510129942 119950625A3260 UPLATCH ASSY DOUG DC9 DC932 3022066WP LT MLG LACK OF LUBE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL013991C 47175 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ADJUSTED TENSION ON LEFT MAIN GEAR UPLATCH ASSEMBLY AND LUBRICATED, CYCLED GEAR SEVERAL TIMES. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000321995070700032WP 1995 7 7 9510131156 119950619A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1509-1515 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01156US 46765 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN, FS 1509 TO 1515, LONGERON 50L AND 50R. REPAIRED SKIN (P/N AYB 7065-1,-2) PER EA 11-98643. 2L73 4F A22WE 19950707000331995070700033WP 1995 7 7 9510149997 119950626A5313 LONGERON DOUG DC9 DC931 3022065WP FS 588 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 29R END FITTING AT FS 588. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950707000341995070700034WP 1995 7 7 9510159997 119950626A5313 LONGERON DOUG DC9 DC931 3022065WP FS 584 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND CORROSION IN LONGERON 30 END FITTING AT FS 584. REPLACED END FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950707000351995070700035WP 1995 7 7 9510169971 119950626A5313 LONGERON DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 28R END FITTING AT FS 604. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950707000361995070700036WP 1995 7 7 9510179971 119950626A5311 FRAME DOUG DC9 DC931 3022065WP FS 637 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND A CRACK IN THE FS 637 SADDLE FITTING AS IT CROSSES THE KEEL LONGERON 29.5R. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950707000371995070700037WP 1995 7 7 9510189971 119950626A5320 FITTING DOUG DC9 DC931 3022065WP FS 760 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND CORROSION ON THE RIGHT MLG WELL KEEL FITTING AT THE AFT BULKHEAD. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950707000381995070700038WP 1995 7 7 9510199944 119950628A5320 FITTING DOUG DC9 DC931 3022065WP FS 680 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A 2 INCH CRACK IN THE LEFT OUTBOARD SEAT TRACK VERTICAL SUPPORT FITTING, FS 680. 2L72 4F A6WE 19950707000391995070700039WP 1995 7 7 9510209947 119950628A3260 SWITCH WIRE DOUG DC9 DC931 3022065WP NLG BROKEN A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL018938E 47161 DURING APPROACH INTO BWI, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. ALSO, RED UNSAFE LIGHT WAS INOPERATIVE. PERFORMED GO-AROUND AND TOWER VISUALLY CONFIRMED THAT GEAR WAS EXTENDED. REQUESTED EMERGENCY EQUIPMENT ON STANDBY. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED WIRE FROM S1-90 PIN 5 TO GROUND STUD 385 ROUTED OUTSIDE OF CONDUIT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000401995070700040WP 1995 7 7 9510219993 119950627A3260 GREEN LIGHT DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL018986E 47402 DURING APPROACH INTO ATL, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. CYCLED GEAR SEVERAL TIMES, DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707000411995070700041NE 1995 7 7 9510226729 219950702A7230 COMPRESSOR BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE STALLED A ANWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LDLANDING 1 GL01629U 22388 89563 DURING LANDING, THE NR 1 ENGINE COMPRESSOR STALLED DURING REVERSE. THE EGT SPIKED TO 850 DEGREES CELSIUS AND THE ENGINE WAS SHUTDOWN. THE ENGINE AND REVERSER WERE RUN AT GATE AND BOTH CHECKED OK. 2L74 4F4 F A20WE E20EA 19950707000421995070700042WP 1995 7 7 9510231224 119950701A3610 CONNECTOR DOUG DC10 DC1030 3023501WP PNEUMATIC SYST CROSSED A NWAAAJ UNSCHED LANDING DUMP FUEL JW WARNING INDICATION INADEQUATE Q C CRCRUISE 1 GL01224NW 46581 DURING CRUISE, THE NR 1 PNEUMATIC SUPPLY VALVE STUCK OPEN. DUMPED 6000 LBS OF FUEL AND RETURNED TO SEA. AIRCRAFT WAS INSPECTED AND SYSTEM WAS MEL'ED. CANNON PLUGS R5-8012 AND R5-8026 WERE REPOSITIONED. OPERATIONAL CHECK OK. 2L73 4F A22WE 19950707000431995070700043NM 1995 7 7 9510246626 119950630A2420 NR 1 AC/DC BUS BOEING747 747251B 1384892NM FLIGHT DECK ELECT SMOKE A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01626US 21708 DURING CRUISE, A BURNING ELECTRICAL SMOKE WAS DETECTED IN THE COCKPIT. THE CREW FOLLOWED PROCEDURES AND ISOLATED THE NR 1 GENERATOR, DUE TO HIGH LOAD AND ISOLATED THE NR 1 AC AND DC BUS, THE SMOKE DISSIPATED. AIRCRAFT CONTINUED WITHOUT FURTHER INCIDENT. PERFORMED FULL INSPECTION OF AIR CONDITIONING SYSTEM, RESET THE NR 1 KVAR INDICATOR CONNECTOR, AND REPLACED COALESCER BAGS. AIRCRAFT APPROVED FOR SERVICE. 2L74 4F A20WE 19950707000441995070700044NM 1995 7 7 9510256622 119950701A3230 SEQUENCE VALVE BOEING747 747251B 1384892NM RT MLG LEAKING A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01622US 21704 DURING CLIMB AND GEAR RETRACTION, THE RED GEAR LIGHT REMAINED ILLUMINATED. AIRCRAFT DUMPED APPROXIMATELY 140,000 LBS OF FUEL AND RETURNED TO KIX. UPON INSPECTION, FOUND THE RIGHT WING GEAR SEQUENCE VALVE LEAKING. ALSO, FOUND 6 BROKEN CLAMPS. TIGHTENED LOOSE NUT AND REPLACED CLAMPS. LEAK AND OPERATIONAL CHECK NORMAL. 2L74 4F A20WE 19950707000451995070700045NM 1995 7 7 95UAL737077 119950526A2600 FIRE CONTL UNIT 1061096101 BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP299008U 19046 LANDED UNDER AMBER ALERT, DUE TO A FIRE WARNING INDICATION ON THE NUMBER 1 ENGINE. REPLACED ENGINE FIRE CONTROL UNIT. 2L72 4F4 F A16WE E2EA 19950707000461995070700046NM 1995 7 7 95UAL900027 119950630A21307110024 PRESSURIZATION HS711Q BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN MALFUNCTIONED A UALAB EMER. DESCENT J WARNING INDICATION ININSP/MAINT 1 WP29987UA 21749 A/C EXPERIENCED COMPLETE LOSS OF PRESSURE AT FL 280 MADE RAPID DESCENT TO 16,000 FEET MSL. REPLACED OUTFLOW VALVE, CONTROL PANEL AND CONTROLLER. SYSTEM OP CHECKS OK. 2L72 4F4 F A16WE E2EA 19950707000471995070700047GL 1995 7 7 95UAL900028 219950630A7321 MEC DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 3 ENGINE FAILED A UALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP291833U 47965 451351 RETURNED TO FIELD UNDER AMBER ALERT WITH NR 3 ENGINE SHUTDOWN. REPLACED MEC. SHOP INSPECTION OF MEC SHOWS EXCESSIVE LEAKAGE WITHIN THE CDP SENSOR, WHICH CAUSES A FUEL SCHEDULE SHIFT. 2L73 4F4 F A22WE E23EA 19950707000481995070700048WP 1995 7 7 ABXA9500571 119950628A3260MS250081 SWITCH DOUG DC8 DC863F 302198FWP THROTTLE ASSY FAULTY A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23819AX 45927 LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK OK, WARNING HORN AUDIBLE WITH FLAPS OUT OF ZERO POSITION. RECYCLED GEAR, NO CHANGE NOTED. FOUND THROTTLE SWITCH AT FAULT. CORRECTED PROBLEM, GEAR INDICATION OPS CHECKED GOOD IAW DC-8 SUPPLEMENTAL MM 32-60-00. 2L74 4F 4A25 19950707000491995070700049WP 1995 7 7 ABXA9500572 119950629A561029190701 SPRING DOUG DC8 DC861F 3021953WP RT CV WINDOW WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23849AX 45891 FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND SPRING ON LOWER AFT LOCKING HOOK STRETCHED AND INOPERATIVE. REPLACED LOWER LOCK HOOK SPRING IAW DC-8 MM 56-10-3, WINDOW OPS CHECKED GOOD. 2L74 4F 4A25 19950707000501995070700050SO 1995 7 7 COM11923 119950629A3260922AA2YA6PZ7 WOW SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01156CA 120156 LANDING GEAR SELECTOR HANDLE COULD NOT BE SELECTED TO RAISE THE LANDING GEAR. REPLACED THE LT MLG WEIGHT ON WHEELS PROXIMITY SENSOR. 2L72 4T RTA31SO 19950707000511995070700051SW 1995 7 7 COM20380 119950627A29102781032135 TUBE ASSY SWRNGNSA227 SA227AC 8780603SW TE FLAPS BROKEN A COMAK NONE KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01702M AC702 HYDRAULIC LEAK LT MLG AREA. REPLACED BROKEN FLAP HYDRAULIC LINE ASSY. 1L72 4T A8SW 19950707000521995070700052EA 1995 7 7 COM60508 119950628A2611473052 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA CARGO COMPT DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01917CA5040 7017 INTERMITTENT CARGO SMOKE WARNING MESSAGE ON EICAS. REPLACED THE NR 2 CARGO SMOKE DETECTOR. 2L72 4F RTA21EA 19950707000531995070700053EA 1995 7 7 COM60509 119950628A2910139719452 SHUTOFF VALVE CNDAIRCL600 CL6002B19 EA LEFT DEFECTIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01936CA2439 7043 NR 1 HYDRAULIC SHUTOFF VALVE WILL NOT OPEN. REPLACED THE LT HYDRAULIC SHUTOFF VALVE. 2L72 4F RTA21EA 19950707000541995070700054EA 1995 7 7 COM60510 119950628A276054C54677E01 MANIFOLD CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SO01941CA1868 40 7050 OUTBD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE SPOILER MANIFOLD ASSY. 2L72 4F RTA21EA 19950707000551995070700055EA 1995 7 7 COM60511 119950701A325016650101 TILLER CNDAIRCL600 CL6002B19 EA NLG STEERING DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01912CA5435 7011 NOSE WHEEL STEERING IS INOP. REPLACED THE STEERING TILLER MODULE. 2L72 4F RTA21EA 19950707000561995070700056NM 1995 7 7 DHL95702003 119950629A36106522422 DUCT BOEING727 72730C 1384009NM NR 1 ENGINE LEAKING A TDHLAAJF UNSCHED LANDING DUMP FUEL ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 SO01702DH 19793 AT 1,000 FEET AGL, FIRE INDICATION NR 1 ENGINE. WHILE REDUCING THRUST, FIRE INDICATION EXTINGUISHED. COMPLETED ALL REQUIRED CHECKS AND LANDED NORMALLY. CHECKED NR 1 FIRE WARNING SYSTEM, FOUND LOWER 13TH STAGE DUCT LEAKING. REMOVED AND REPLACED DUCT PER M/M 36-10-0. RAN ENGINE TO TAKEOFF POWER, NO LEAKS NOTED. REMOVED AND REPLACED NR 1 FIRE BOTTLE AND DISCHARGE DISK PER M/M 26-21 NAD 26-25. 2L73 4F A3WE 19950707000571995070700057NM 1995 7 7 DHL95702004 119950704A315021EN1076 SWITCH BOEING727 72730C 1384009NM T/O WARNING SERVICABLE A TDHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01701DH 19011 TAKEOFF WARNING SOUNDED IN FLAPS 25 DEGREE POSITION. CHECKS OK IN FLAP 5 DEGREE POSITION. ADJUSTED TAKEOFF WARNING SWITCH PER MM 31-26-0, CHECKS NORMAL. 2L73 4F A3WE 19950707000581995070700058NM 1995 7 7 DL72L952839 119950628A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11508DA 21310 NR 2 SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED, FOUND AT B2 LTR CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950707000591995070700059NM 1995 7 7 DL72L952840 119950628A5330 SKIN BOEING727 727232 1384082NM FS 1075 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11508DA 21310 CORROSION/RIVET SHEARED STA 1075 STRINGER 27L, FOUND DURING B-2 LTR CK TPAMM. INSTALLED TIME LIMITED REPAIR PER SRM 53-30-3. 2L73 4F A3WE 19950707000601995070700060NM 1995 7 7 DL72S952818 119950626A5320 WEB BOEING727 727232 1384082NM FS 1226 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 FOUND DURING A-1 LETTER CHECK, 1 INCH CRACK IN RT WEB OF 48 SEC LOCATED AT STA 1226 LWR LIGHTNING HOLE. A .25 INCH CRACK IN RT WEB OF 48 SEC LOCATED AT STA 1233. REPAIRED PER M/M 53-11-0 PAR 16. 2L73 4F A3WE 19950707000611995070700061NM 1995 7 7 DL72S952819 119950626A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 FOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12. 2L73 4F A3WE 19950707000621995070700062NM 1995 7 7 DL72S952820 119950626A5754 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 FOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT L/E RIB CRACKED, .5 INCH I/B OF ACTUATOR MOUNT. REPAIRED PER MM 57-54-0 PAR 3. 2L73 4F A3WE 19950707000631995070700063NM 1995 7 7 DL72S952821 119950626A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 FOUND DURING A-1 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19950707000641995070700064NM 1995 7 7 DL72S952828 119950502A5753652163262 DOUBLER BOEING727 727232 1384082NM NR 3 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A REPAIR DOUBLER CRACKED TWO PLACES AFT OF I/B BELL CRANK ON AFT ATTACH ANGLE. REPAIRED BY SPLICING IN NEW ANGLE WITH ATTACH DOUBLER PER SRM 57-52-0. 2L73 4F A3WE 19950707000651995070700065NM 1995 7 7 DL72S952829 119950502A5753652163262 DOUBLER BOEING727 727232 1384082NM NR 3 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A REPAIR DOUBLER CRACKED TWO PLACES AT I/B AFT FLAP TRACK. REPAIRED PER SRM 57-52-0. 2L73 4F A3WE 19950707000661995070700066NM 1995 7 7 DL72S952831 119950502A5753652163262 SKIN BOEING727 727232 1384082NM NR 3 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11545DA 22494 NR 3 MIDFLAP, DURING HMV SHOP INSP WAS FOUND TO HAVE A CORNER CRACKED ON CUTOUT COVER SKIN 32 FROM I/B END. INSTALLED DOUBLER PER M/M 57-52-0. 2L73 4F A3WE 19950707000671995070700067NM 1995 7 7 DL72S952844 119950627A801297907841 VALVE BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO11490DA 21020 665503 ON CLIMBOUT, HAD NR 2 ENGINE START VALVE LIGHT ILLUMINATE. PER CHECKLIST, ENGINE WAS SHUTDOWN. FOUND NR 2 ENGINE START VALVE WITH SOLENOID SEPARATED FROM HOUSING. REPLACED VALVE, OPERATION NORMAL. 2L73 4F4 F A3WE E2EA 19950707000681995070700068NM 1995 7 7 DL72S952845 119950612A271065178234 CONTROL MODULAR BOEING727 727232 1384082NM AILERON CRACKED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11526DA 21586 ON TAXIOUT, HAD SMOKE IN CABIN. AIRCRAFT WAS EVACUATED. FOUND AILERON CONTROL MODULE WITH BLOWN SEAL AND CRACKED HOUSING, CAUSING HYDRAULIC LEAK AND CONTAMINATING APU INLET, WHICH CAUSED SMOKE IN CABIN. REPLACED MODULE, OPERATION NORMAL. 2L73 4F A3WE 19950707000691995070700069NM 1995 7 7 DL72S952846 119950627A3350 EEL WIRE BOEING727 727232 1384082NM CABIN SHORTED A DALAK NONE L NO TEST CRCRUISE 1 SO11525DA 21585 DURING CRUISE, HAD EMERGENCY LIGHTS COME ON WHEN SWITCH IN ARMED POSITION. THE EMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER TRIP. FOUND WIRES 9004-20 AND 9010-20 SHORTED. REPAIRED WIRES AND REPLACED LITGHT SWITCH AND BATTERY IN 9027. OPERATION NORMAL. 2L73 4F A3WE 19950707000701995070700070NM 1995 7 7 DL72S952852 119950619A5751 SKIN 657273411W BOEING727 727232 1384082NM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 7 20745 DURING A SHOP INSPECTION, THE LOWER OUTBOARD SKIN WAS FOUND TO HAVE SEVERAL FASTENERS PULLING THROUGH THE SKIN. A REPAIR WAS INSTALLED PER THE M/M 57-51-0, FOR LEFT OUTBOARD AILERON. 2L73 4F A3WE 19950707000711995070700071NM 1995 7 7 DL72S952859 119950627A5315 FLOORBEAM BOEING727 727232 1384082NM FS 344 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, FLOORBEAM CRACKED AT FLOOR PANEL SCREW HOLE STA 344 8 INCHES OUT LBL 25. REPAIRED PER SRM 53-10-8 FIG 8. 2L73 4F A3WE 19950707000721995070700072NM 1995 7 7 DL72S952860 119950627A5315 FLOORBEAM BOEING727 727232 1384082NM BS 312 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION AT FLOORBEAM STA 312 LBL 25. REPAIRED AS PER ERA 302020-14. 2L73 4F A3WE 19950707000731995070700073NM 1995 7 7 DL72W952716 119950621A5751652176658 SKIN BOEING727 727247 138408FNM AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND DENT IN UPPER SKIN OF OUTBOARD AILERON. REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950707000741995070700074NM 1995 7 7 DL72W952794 119950617A5755651734781A SKIN 651734781A BOEING727 727247 138408FNM SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 1937 22110 DURING SHOP INSPECTION, SPOILER PANEL WAS FOUND WITH DELAMINATION. REPAIRED PER SRM 57-50. 2L73 4F A3WE 19950707000751995070700075NM 1995 7 7 DL72W952824 119950619A5753106189911 BUSHINGS BOEING727 727247 138408FNM NR 4 FLAP TRACK LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, BUSHINGS LOOSE IN MLG WING DOOR LUG ON FWD END OF NR 4 FLAP TRACK. REPAIRED PER MM 57-43-0. 2L73 4F A3WE 19950707000761995070700076NM 1995 7 7 DL72W952825 119950625A5753 BUSHING BOEING727 727247 138408FNM NR 5 FLAP TRACK WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, BUSHINGS WORN IN MLG DOOR LUG ON FWD END OF NR 5 FLAP TRACK. REPAIRED PER MM 57-43-0. 2L73 4F A3WE 19950707000771995070700077NM 1995 7 7 DL72W952850 119950626A5330 SKIN BOEING727 727247 138408FNM NOSE GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112809W 20581 DURING INSPECTION, FOUND TOOLING DAMAGE TO RT FUSELAGE NOSE AT FS 243.7, APPROXIMATELY HALFWAY UP THE SKIN PANEL. REPAIRED PER SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950707000781995070700078NM 1995 7 7 DL72W952851 119950622A5312 BULKHEAD BOEING727 727247 138408FNM FS 178 MISMFG A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112809W 20581 DURING INSPECTION, FS 178 RT BULKHEAD HAD AN ACCESS HOLE. INSTALLED PER SRM 53-10-0 FIG 3. 2L73 4F A3WE 19950707000791995070700079NM 1995 7 7 DL72W952853 119950622A5312 BULKHEAD BOEING727 727247 138408FNM NOSE MISMFG A DALAK NONE O OTHER ININSP/MAINT 1 SO112809W 20581 DURING INSPECTION, LT FS 178 BULKHEAD HAD ACCESS HOLE. INSTALLED PER SRM 53-10-9 FIG 3. 2L73 4F A3WE 19950707000801995070700080NM 1995 7 7 DL72W952855 119950620A5754 ANGLE BOEING727 727247 138408FNM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 1 L/E SLAT CRACKED, .25 INCH CRACK IN ANGLE ON LOWER T/E 7 INCHES FROM I/B END. REPAIRED PER MM 57-54-0, FOUND AT HMV. 2L73 4F A3WE 19950707000811995070700081NM 1995 7 7 DL72W952861 119950622A5754651622295 RIB BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112809W 20581 DURING SHOP INSPECTION, NR 3 SLAT PANEL WAS FOUND WITH L/E RIB NR 17 CRACKED. REPAIRED PER MM 57-54-00 FIG 809. 2L73 4F A3WE 19950707000821995070700082NM 1995 7 7 DL73S952830 119950509A5752654645527SP SKIN BOEING737 737232 1384475NM AILERON TAB DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11303DL 23075 ON INITIAL SHOP INSPECTION, 2 AREAS OF DELAMINATION WERE FOUND. THE FIRST AREA OF DAMAGE IS ON BOTTOM SKIN, APPROX 12 INCHES FROM I/B END. THE DAMAGED AREA IS DELAMINATED APPROX 8 INCH BY 2 INCH. THIS DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 57-50-6 WITH REF TO SRM 51-40-12. THE SECOND DELAMINATED AREA IS DAMAGED 22 INCHES FROM I/B ON TOP SKIN. THIS DAMAGE WAS REPAIRED IN ACCORDANCE WITH SRM 57-50-6 WITH REF TO SRM 51-40-12, FOR AILERON TAB PANEL. 2L72 4F RTA16WE 19950707000831995070700083NM 1995 7 7 DL73S952862 119950628A2450948F4581 GCU BOEING737 737232 1384475NM E/E COMP FAILED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO11319DL 23091 DURING CRUISE, LOST NR 1 GENERATOR, GCU BREAKER TRIPPED. STARTED APU, UNABLE TO TRANSFER POWER, DIVERTED BOS. REPLACED NR 1 GCU AND NR 1 GEN BREAKER. OP CHECK NORMAL. 2L72 4F RTA16WE 19950707000841995070700084NM 1995 7 7 DL757952811 119950620A5755113N550139A SKIN BOEING757 757232 1384965NM SPOILER PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11657DL 24419 PUNCTURE IN THE UPPER SKIN OF SPOILER, APPROX 25.5 FROM O/B EDGE, 4 INCHES FROM TRAILING EDGE. REPAIR CONSISTED OF BONDING 3 REPAIR PLIES USING GRAPHITE CLOTH REPAIR MATERIAL AND 9390 ADHESIVE RESKIN SYSTEM, CURED AT 200 DEGREES FOR A TOTAL OF FOUR HOURS AS CALLED OUT IN THE 57-70-01 REF 51-70-17. 2L72 4F RTA2NM 19950707000851995070700085NM 1995 7 7 DL757952827 119950628A5755113N450120 SKIN BOEING757 757232 1384965NM NR 8 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11657DL 24419 EXTERIOR SKIN HAD TWO SMALL HOLES CAUSED BY HAIL IN DFW. BOTH HOLES WHERE LESS THAN 2 INCHES IN DIAMETER. DAMAGE WAS REPAIRED IN ACCORDANCED WITH SRM 57-70-01 WITH REF TO 51-70-17. FOUND DURING SHOP VISIT FOR NR 8 SPOILER PANEL. 2L72 4F RTA2NM 19950707000861995070700086NM 1995 7 7 DL757952833 119950620A5753113N280061 SKIN BOEING757 757232 1384965NM LT TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11657DL 24419 LT I/B AFT FLAP SUFFERED HAIL DAMAGE ON UPPER SURFACE. FLAP WAS REPAIRED PER SRM 57-53-01. 2L72 4F RTA2NM 19950707000871995070700087NM 1995 7 7 DL757952834 119950628A5754114N4003178A SKIN BOEING757 757232 1384965NM NR 9 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING SHOP INSPECTION, NR 9 SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. REPAIRED PER SRM 57-42-03. 2L72 4F RTA2NM 19950707000881995070700088NM 1995 7 7 DL757952841 119950627A5754114N4004165A TE WEDGE BOEING757 757232 1384965NM NR 3 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11664DN 25012 DURING INSP, THE T/E WEDGE ON NR 3 SLAT WAS FOUND TO BE DELAMINATED. THE WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950707000891995070700089NM 1995 7 7 DL757952842 119950531A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 RADOME TEST FOUND DELAMINATION AND MOISTURE ABOVE LIMITS. ALSO, FOUND OLD WET LAY-UPS. RADOME WAS REBUILT, COMPLETE FROM BASE RING UP PER SRM 53-10-72. 2L72 4F RTA2NM 19950707000901995070700090NM 1995 7 7 DL757952848 119950601A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11654DL 24394 RADOME HAD THREE SMALL HOLES AT 4 O'CLOCK. AFTER INITIAL INSPECTION, FOUND OLD WET LAY-UP AND MOISTURE ABOVE LIMITS. REBUILT RADOME COMPLETE FROM BASE RING UP PER SRM 53-10-72. REPAIRS ACCOMPLISHED AT SHOP VISIT. 2L72 4F RTA2NM 19950707000911995070700091NM 1995 7 7 DL757952849 119950515A7110314N301016B NOSE COWL BOEING757 757232 1384965NM ENGINE ERROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 DURING INSPECTION, ENGINE NOSE COWL WAS FOUND WITH EROSION DAMAGE ON T/E COMPOSITE SKIN AT 6 O'CLOCK POSITION, APPROX 5 INCHES LONG. REPAIRED PER SRM 54-11-01 AND 51-70-03. 2L72 4F RTA2NM 19950707000921995070700092NM 1995 7 7 DL757952854 119950628A5315 FLOORBEAM BOEING757 757232 1384965NM FS 680 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 DURING HMV IN ATL, INSPECTION FOUND THE UPPER CAP OF FS 680 FLOORBEAM CORRODED BC 0 TO RBL 60, CUSP LINE. ACCOMPLISHED REPAIRS PER SRM 53-00-51 AND 53-30-51 FIG 205. 2L72 4F RTA2NM 19950707000931995070700093NM 1995 7 7 DL76L952817 119950626A5753 FLAP BOEING767 767332 1382001NM NR 4 AFT FLAP SOFT SPOT A DALAK NONE O OTHER ININSP/MAINT 1 SO11177DN 25122 FOUND DURING LETTER CHECK, SOFT SPOT ON NR 4 AFT FLAP LOWER O/B END. REPAIRED PER SRM 57-53-01. 2L72 4F RTA1NM 19950707000941995070700094NM 1995 7 7 DL76S952822 119950628A5754114T310037 TE WEDGE BOEING767 767332 1382001NM LT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11117DL 23276 DURING SHOP INSPECTION, SLAT PANEL WAS FOUND WITH T/E WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-37. 2L72 4F RTA1NM 19950707000951995070700095WP 1995 7 7 DLL10952783 119950625A5313 STRINGER LKHEED1011 10113851 5265010WP FS 1475-1605 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 STRINGER 29 CORRODED FS 1475, FS 1523 TO 1545, FS 1585, FS 1565 TO 1585, FS 1585 TO 1605. FOUND AT HMV, CORROSION SAMPLE INSP. REPLACED STRINGER PER SRM 53-13-00 PG 804. 2L73 4F A23WE 19950707000961995070700096WP 1995 7 7 DLL10952835 119950627A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1163 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 FLOOR PANEL SUPPORT RAIL CRACKED IN RADIUS AT STA 1163 FORMER, LBL 104. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950707000971995070700097WP 1995 7 7 DLL10952838 119950614A55201524058110 DOUBLER 1524058110 LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA DL20 193C1139 DURING SHOP INSPECTION, A DOUBLER WAS FOUND TO BE CRACKED AT THE AFT EDGE OF THE ELEVATOR TIP. A REPAIR WAS INSTALLED PER SRM 55-22-00 FIG 802. 2L73 4F A23WE 19950707000981995070700098WP 1995 7 7 DLL13952858 119950628A5414 SKIN LKHEED1011 10113851 5265010WP NR 3 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, INTERFACE BOX CRACKED, NR 3 PYLON FWD END. REPAIRED PER SRM 54-11-00 PG 812. 2L73 4F A23WE 19950707000991995070700099WP 1995 7 7 DLL14952812 119950625A5755 TE CORNER 1529102178 LKHEED1011 1011385115 5265015WP RT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11736DY HO221 193C1227 DURING INSPECTION, RT WING SPOILER PANEL WAS FOUND WITH TRAILING EDGE CORNER DAMAGE APPROXIMATELY 6 INCH BY 6 INCH AREA TO TOP AND BOTTOM SKIN. ACCOMPLISHED BONDED REPAIRS PER SRM 57-52-00. 2L73 4F A23WE 19950707001001995070700100NM 1995 7 7 DLM88952804 119950626A5320 ANGLE DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11958DL 49977 KEEL BEAM AFT ANGLE CROSSOVER RIB CRACKED LT AND RT SIDES, FOUND DURING F-1 LTR CK. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950707001011995070700101NM 1995 7 7 DLM88952816 119950612A32301951635501 SPRING DOUG MD88 MD88 3023688NM NLG BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11932DL 49719 AFTER TAKEOFF, HAD NOSE GEAR UNSAFE LIGHT WITH GEAR HANDLE UP. NOSE GEAR FAILED TO RETRACT INITIALLY, AFTER ABOUT 10 MIN NOSE GEAR DID FINALLY RETRACT WITH A LOUD BANG. FOUND THE RIGHT RETRACT SPRING ASSEMBLY BROKEN. REPLACED SPRING, OPERATION NORMAL. 2L72 4F RTA6WE 19950707001021995070700102 1995 7 7 DLM88952843 419950627A34254608000307 RDMI UNIT DOUG MD88 MD88 3023688NM FLIGHT DECK MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11953DL 49884 ON CLIMBOUT, HAD ATTITUDE FAIL ON COPILOTS, PRIMARY FLIGHT DISPLAY AND CAPTAINS RDMI. REPLACE TE NR 2 ATTITUDE HEADING REFERENCE SYSTEM. OPERATION NORMAL. 2L72 4F RTA6WE 19950707001031995070700103WP 1995 7 7 MWEA95229 119950628A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP FWD PAX DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31204ME 47680 CREW REPORTS, FWD ENTRANCE DOOR EVAC SLIDE COVER FELL OFF. MAINTENANCE RESECURED SLIDE COVER, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950707001041995070700104NE 1995 7 7 P5CA9500151 219950629A7261 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7F 52054NE NR 3 FAILED A AP5CAAE UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CLCLIMB 1 WP23850FT50530133 19755 685956 DURING CLIMBOUT FROM SEA, PASSING 10,000 FEET ALTITUDE, NR 3 ENGINE OIL PRESSURE WENT O, NR 3 ENGINE OIL PRESSURE LIGHT AND NR 3 ENGINE FILTER BYPASS LIGHT ILLUMINATED. SHUTDOWN ENGINE IAW IN FLIGHT ENGINE CHECK LIST. ON GROUND RUN, OIL RUNNING FROM ENGINE NR 3 BEARING VENT TUBE AND METAL IN ENGINE OIL FILTER. ENGINE TO BE REPLACED. 2L74 4F4 F A20WE E20EA 19950707001051995070700105NM 1995 7 7 P5CA9500152 119950528A5330 PANEL BOEING747 747121 1384871NM LEFT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS AND HOLES ON INBOARD SURFACE OF HINGE PANEL NR 591CB. LEFT WING LEADING EDGE CAVITY. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001061995070700106NM 1995 7 7 P5CA9500153 119950528A5730 DOOR BOEING747 747121 1384871NM LEFT WING BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LONG HINGE DOOR UNDER LEFT INBOARD AILERON WALKING BEAM AND MAIN ACTUATOR IS BROKEN. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001071995070700107NM 1995 7 7 P5CA9500154 119950528A5730 PANEL BOEING747 747121 1384871NM LT WING DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FIBERGLASS DAMAGED AROUND THE EDGES OF DOOR HINGE PANEL 573CB. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001081995070700108NM 1995 7 7 P5CA9500155 119950528A5730 PANEL BOEING747 747121 1384871NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SMALL SURFACE CRACKS AND HOLES OVER INBD SURFACE OF LEFT WING TRAILING EDGE FIXED LOWER PANEL, UNDER NR 4 GROUND SPOILER. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001091995070700109NM 1995 7 7 P5CA9500157 119950528A5751 LE SKIN BOEING747 747121 1384871NM LT AILERON TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON LEADING EDGE SKIN LOWER SURFACE ON LEFT INBOARD AILERON IS TORN. REPLACED SKIN PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707001101995070700110NM 1995 7 7 P5CA9500158 119950528A5720 BRACKET BOEING747 747121 1384871NM HINGE DOOR WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BRACKET UNDER HINGE DOOR NR 573CB IS WORN OUT. MANUFACTURED NEW PART PER BOEING SRM 57-10-02 AND INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707001111995070700111NM 1995 7 7 P5CA9500159 119950528A5320 BRACKET BOEING747 747121 1384871NM FUSELAGE CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON OMEGA BRACKET, LEVEL 1. REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001121995070700112NM 1995 7 7 P5CA9500160 119950528A5320 SUPPORT BOEING747 747121 1384871NM FS 800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON OMEGA SUPPORT AT STA 800 BETWEEN S38 AND S39, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001131995070700113NM 1995 7 7 P5CA9500161 119950528A5320 ANGLE BOEING747 747121 1384871NM FS 800-880 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON ANGLE ABOVE AIR CONDITIONING CHANNEL BETWEEN STA 800 AND 880 RIGHT. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001141995070700114NM 1995 7 7 P5CA9500162 119950528A5320 FAIRING SUPPORT BOEING747 747121 1384871NM FS 800-920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT FROM SIDE STA 800 TO 920 RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER SRM 51-10-01. 2L74 4F A20WE 19950707001151995070700115NM 1995 7 7 P5CA9500163 119950704A5720 BRACKET BOEING747 747123 1384873NM LEFT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23859FT 20326 FOUND NR 4 LEADING EDGE DRIVE FWD SUPPORT BRACKET HAS TWO CRACKS IN RADIUS NEAR INBOARD ATTACH BRACKET, STA 1400 LEFT WING. REPAIRED AS PER SRM 51-40-03. 2L74 4F A20WE 19950707001161995070700116NM 1995 7 7 P5CA9500164 119950528A5320 SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON RIGHT FAIRING SUPPORT FROM STA 800 TO 840 AND 880 TO 920, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001171995070700117NM 1995 7 7 P5CA9500165 119950528A5320 SUPPORT BOEING747 747121 1384871NM FUSELAGE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FWD FAIRING OMEGA SUPPORT AND ANGLE BETWEEN STA 840 TO 880 AND 920 TO 960, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001181995070700118NM 1995 7 7 P5CA9500166 119950528A5330 SKIN BOEING747 747121 1384871NM FS 820-860 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FUSELAGE SKIN BETWEEN BS 820 TO 860 BETWEEN S45L AND S45R, LEVEL 1. CORROSION REMOVED AS PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001191995070700119NM 1995 7 7 P5CA9500167 119950528A5320 SUPPORT BOEING747 747121 1384871NM FS 820-860 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT BETWEEN S43R AND S47R STA 820 AND 860, LEVEL 1. REMOVED CORROSION PER SRM 51-10-01. 2L74 4F A20WE 19950707001201995070700120NM 1995 7 7 P5CA9500168 119950528A5320 ANGLE BOEING747 747121 1384871NM FS 860-920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON Z-ANGLE, BETWEEN BS 860 AND 920 S47L AND S47R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001211995070700121NM 1995 7 7 P5CA9500169 119950528A5320 SUPPORTS BOEING747 747121 1384871NM FS 920-960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORTS BS 920 TO 960 AND 100 S40R TO S47R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001221995070700122NM 1995 7 7 P5CA9500170 119950528A5320 SUPPORT BOEING747 747121 1384871NM FS 920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT BS 920 BETWEEN S40R AND S47R, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001231995070700123NM 1995 7 7 P5CA9500171 119950528A5330 PANEL BOEING747 747121 1384871NM BS 980-1000 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT ON THE CORNER PANEL BETWEEN BS 980 AND 1000 RIGHT SIDE NEAR THE CENTER LINE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001241995070700124NM 1995 7 7 P5CA9500172 119950528A5320 SUPPORT BOEING747 747121 1384871NM FS 980 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT BS 980 BETWEEN S40L AND S47L, LEVEL 1. REMOVED CORROSION AS PER SRM 51-10-01. 2L74 4F A20WE 19950707001251995070700125NM 1995 7 7 P5CA9500173 119950528A5330 SKIN BOEING747 747121 1384871NM BS 1000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK FUSELAGE SKIN BS 1000 S43L. REPAIRED AS PER BOEING SRM 53-30-03 FIG 11. 2L74 4F A20WE 19950707001261995070700126NM 1995 7 7 P5CA9500174 119950528A5753 BUSHING BOEING747 747121 1384871NM NR 4/6 TE FLAPS MIGRATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CLEVIS BUSHINGS MIGRATED ON NR 4 AND NR 6 TRAILING EDGE FOREFLAP SEQUENCE CARRIAGES. PERFORMED SERVICE BULLETIN 747-57-2166 FIG 1 ITEMS 2 THROUGH 4. 2L74 4F A20WE 19950707001271995070700127NM 1995 7 7 P5CA9500175 119950528A5280 DOOR BOEING747 747121 1384871NM LT MLG BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT BODY GEAR UPPER DOOR HAS BENT EDGE. DAMAGE TRIMMED AND REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707001281995070700128NM 1995 7 7 P5CA9500176 119950528A561065B0761612 CHORD BOEING747 747121 1384871NM NR 2 RT WINDOW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CREW WINDOW NR 2 RIGHT, FOUND CRACK IN UPPER CHORD INBOARD SIDE AT BS 320. REMOVED AND REPLACED CHORD PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707001291995070700129NM 1995 7 7 P5CA9500177 119950528A575360B001801 BEARING BOEING747 747121 1384871NM NR 8 FLAP TRACK MIGRATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING FLAP TRACK NR 8 FORWARD MOUNT LUG BEARING HAS MIGRATED. REPAIRED PER BOEING SB 747-57-2262, FITTING INSTALLED PER BOEING SB 747-57-2238. 2L74 4F A20WE 19950707001301995070700130NM 1995 7 7 P5CA9500178 119950528A5730 PANEL BOEING747 747121 1384871NM RT WING SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING TRAILING EDGE UPPER SURFACE NEAR OUTBOARD AILERON INBOARD SIDE HAS FIBERGLASS SEPARATION. REPAIRED ACCORDING TO BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001311995070700131NM 1995 7 7 P5CA9500179 119950528A5720 FAIRING BOEING747 747121 1384871NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK RIGHT REAR SPAR LOWER TRAILING EDGE FAIRING AT WS 740. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001321995070700132NM 1995 7 7 P5CA9500180 119950528A5753 FAIRINGS BOEING747 747121 1384871NM TE FLAPS DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATIONS AND DENTS ON FLAP FIXED FAIRINGS AT TRACKS NR 2, 3, 7, 8. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001331995070700133NM 1995 7 7 P5CA9500181 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HOLES IN INNER SIDE OF FAIRING PANEL NR 191C. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001341995070700134NM 1995 7 7 P5CA9500182 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SMALL HOLES DENTS AND DELAMINATION ON NR 2 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001351995070700135NM 1995 7 7 P5CA9500183 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS AND CRACKS ON FAIRING PANEL 191P. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001361995070700136NM 1995 7 7 P5CA9500184 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS NR 5 RIGHT AFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001371995070700137NM 1995 7 7 P5CA9500185 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATIONS ON NR 9 LEFT FAIRING PANEL. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707001381995070700138NM 1995 7 7 P5CA9500186 119950528A5400 SPAR BOEING747 747121 1384871NM NR 3 PYLON CHAFED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CHAFING ON INSIDE OF LOWER SPAR FROM NS 180 TO NS 236, NR 3 PYLON. REPLACED WEAR STRAPS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707001391995070700139NM 1995 7 7 P5CA9500187 119950528A5400 RIB BOEING747 747121 1384871NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK WITH STOP HOLE ON INNER RIB SIDE AT NS 222 NR 3 PYLON. REPAIRED PER BOEING SRM 54-10-03. 2L74 4F A20WE 19950707001401995070700140NM 1995 7 7 P5CA9500188 119950528A5400 ANGLE BOEING747 747121 1384871NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND DAMAGE ON ANGLE THAT ATTACHES FAIRING TO WING RIGHT ADJACENT TO UPPER LINK FITTING NS 222 NR 3 PYLON. REPLACED ANGLE PER BOEING SRM 54-10-02. 2L74 4F A20WE 19950707001411995070700141NM 1995 7 7 P5CA9500189 119950528A5400 ANGLE BOEING747 747121 1384871NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON ANGLE ON NR 3 PYLON CLOSURE SPAR RIGHT INSIDE, APPROXIMATELY NS 215 TO 290. FABRICATED NEW ANGLE AS PER SRM 54-10-02, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950707001421995070700142NM 1995 7 7 P5CA9500190 119950528A5400 BRACKET BOEING747 747121 1384871NM NR 3 PYLON BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN BRACKET THAT ATTACHES FUEL FEED LINE ON NR 3 PYLON CLOSURE SPAR APPROXIMATELY NS 236. FABRICATED NEW BRACKET PER SRM 54-30-02. 2L74 4F A20WE 19950707001431995070700143NM 1995 7 7 P5CA9500191 119950528A5210 FRAME BOEING747 747121 1384871NM NR 5L DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 5 LEFT DOOR FORWARD FRAME DAMAGED INBOARD OF BOTH LOWER STOP FITTINGS. REWORKED DAMAGED AREA PER BOEING SRM 51-10-02. 2L74 4F A20WE 19950707001441995070700144NM 1995 7 7 P5CA9500192 119950528A5320 ANGLES BOEING747 747121 1384871NM BS 260 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED ANGLES ON NOSE WHEEL WELL CEILING STA 260 WL 180 RBL 10 AND LBL 10. NEW ANGLES MANUFACTURED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707001451995070700145NM 1995 7 7 P5CA9500193 119950528A5347 SEAT TRACK BOEING747 747121 1384871NM BS 260 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SEAT TRACK IS BROKEN AT STA 260 LBL 60. INSTALLED NEW SEAT TRACK PER BOEING SRM 53-10-05. 2L74 4F A20WE 19950707001461995070700146NM 1995 7 7 P5CA9500194 119950528A5751 HINGE BOEING747 747121 1384871NM RT INBD AILERON GROOVED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 GROOVE AT RIGHT WING INBOARD AILERON LOWER OUTBOARD HINGE LEADING EDGE. DAMAGE CLEANED UP WITHIN LIMITS PER BOEING SRM 57-20-01, TREATED PER SRM 51-10-01. 2L74 4F A20WE 19950707001471995070700147NM 1995 7 7 P5CA9500195 119950528A5230 ANGLE BOEING747 747121 1384871NM FWD CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN ANGLE BRACKET AT CUTOUT FOR THE FORWARD CARGO DOOR. REPAIRED ANGLE BRACKET PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707001481995070700148NM 1995 7 7 P5CA9500196 119950528A5330 SKIN BOEING747 747121 1384871NM FS 1265-1280 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1265 AND 1280 UNDER DOOR NR 3L S26L, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001491995070700149NM 1995 7 7 P5CA9500197 119950528A5330 SKIN BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE FUSELAGE SKIN AT BS 2360, LEFT SIDE BETWEEN S4L AND S9L, LEVEL 1. CORROSION REMOVED AND TREATED PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707001501995070700150NM 1995 7 7 P5CA9500198 119950528A5330 SKIN BOEING747 747121 1384871NM BS 2200 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DEEP HIT IN THE FUSELAGE SKIN RIGHT SIDE AT BS 2200 S3R. BLENDED OUT DAMAGE IN THE SKIN PER BOEING SRM 51-10-01, DENT IS WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707001511995070700151NM 1995 7 7 P5CA9500199 119950528A5320 RAIN CHANNEL BOEING747 747121 1384871NM BS 1265 SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SHEARED RIVET AND 1 BLIND FASTENER IN RAIN CHANNEL BS 1265 AT S15R. INSTALLED NEW RIVETS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707001521995070700152NM 1995 7 7 P5CA9500200 119950528A5330 SKIN BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FUSELAGE SKIN AT STA 2360 BETWEEN S4R AND S7R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707001531995070700153NM 1995 7 7 P5CA9500201 119950701A7920635496CL2 GASKET BOEING747 747132 1384882NM PWA JT9 JT9D7 52054NE NR 4 ENGINE WORN A AP5CAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP23857FT 20246 663028 PRECAUTIONARY SHUTDOWN DUE TO DECREASING OIL PRESSURE, DROPPED BELOW 30 PSI WITH INCREASED BREATHER TEMPERATURE, ENGINE OIL PRESSURE LOW LIGHT ON WINDMILL TIME 1 PLUS 20 OIL PRESSURE ALWAYS 10 TO 15 PSI. FOUND OIL LEAK AT NR 1 AND NR 2 OIL BREATHER LINE. REPLACED GASKET, LEAK CHECK OK. 2L74 4F4 F A20WE E20EA 19950707001541995070700154EU 1995 7 7 QXEA9500201 119950629A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 EMERGENCY LIGHTS FORWARD HALF OF CABIN INOP. BULBS WERE REPLACED AND LIGHTS OPS GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950707001551995070700155NM 1995 7 7 SCNA95136 119950622A3350900542 EEL POWER SUPPLY BOEING727 727259 138408JNM R-2 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 FOUND THE EMERGENCY EXIT SIGN AT THE R2 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT SIGN POWER SUPPLY AND BATTERY PACK. SIGN OPS CHECKED NORMAL. 2L73 4F A3WE 19950707001561995070700156NM 1995 7 7 SCNA95137 119950627A3350S106 EEL BATTERY BOEING727 7272J4 1384006NM COCKPIT CORRODED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15284SC 21438 FOUND THE COCKPIT PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. BATTERIES IN THE BATTERY PACK WERE FOUND TO BE CORRODED. REMOVED AND REPLACED BATTERIES AND LIGHT OPS CHECKED GOOD IAW MM 33-50-101. 2L73 4F RTA3WE 19950707001571995070700157NM 1995 7 7 UPS203728 119950703A5330651986219 CHORD BOEING727 72725C 138400HNM BS 340-348 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT UPPER NOSE CHORD BS 340 TO 348, LBL 15, WL 170. REPAIRED IAW SRM 53-10-1, 51-10-1, 51-30-5, 51-20-4, 51-30-2. 2L73 4F A3WE 19950707001581995070700158NM 1995 7 7 UPS203729 119950703A5320 SUPPORT BOEING727 72725C 138400HNM FS 302-312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT STA 302 TO 312. REPAIRED IAW SRM 51-10-6, 51-30-6, 51-20-1, 51-30-5, 51-30-02. 2L73 4F A3WE 19950707001591995070700159NM 1995 7 7 UPS203730 119950703A5320653414423 EXPANSION LINK BOEING727 72725C 138400HNM FS 740-780 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT STA 740 TO 760 AT RBL 25, WL 208. REPAIRED IAW SRM 53-10-1, 51-30-8, OHM 20-50-03, 20-50-02, 20-50-1. 2L73 4F A3WE 19950707001601995070700160NM 1995 7 7 UPS203731 119950703A5753 FLAP BOEING727 72725C 138400HNM RT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATION OF I/B RT AFT FLAP ON THE O/B CORNER. REPAIRED IAW SRM 51-40-6, M/M 51-20-151. 2L73 4F A3WE 19950707001611995070700161NM 1995 7 7 UPS203732 119950703A534765234104 SEAT TRACK BOEING727 72725C 138400HNM FS 580-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LWR CARGO RT SEAT TRACK AT FS 580 TO 680. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950707001621995070700162NM 1995 7 7 UPS203733 119950703A5320651631291 SHEAR TIE BOEING727 72725C 138400HNM FS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294 BETWEEN STRINGER 10L AND 11L. REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950707001631995070700163NM 1995 7 7 UPS203734 119950703A5320 INTERCOSTAL BOEING727 72725C 138400HNM FS 303 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STA 303, STR 16L. REPAIRED IAW SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950707001641995070700164NM 1995 7 7 UPS203735 119950703A5320 SHEAR TIE BOEING727 72725C 138400HNM FS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SHEAR TIE AT FS 294, STA 8 TO 9L. REPAIRED IAW SRM 51-40-3, 51-30-2, B727-5310-1259. 2L73 4F A3WE 19950707001651995070700165NM 1995 7 7 UPS203736 119950703A5320 WEB BOEING727 72725C 138400HNM FS 227 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 277 AT STR 14L AND 16L. REPAIRED IAW SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950707001661995070700166NM 1995 7 7 UPS203737 119950703A5320 SHEAR TIE BOEING727 72725C 138400HNM FS 294 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BROKEN SHEAR TIE FS 294, STR 9 TO 10L. REPAIRED IAW SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950707001671995070700167NM 1995 7 7 UPS203738 119950703A5320 INTERCOSTAL BOEING727 72725C 138400HNM FS 303 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT STR 15L, FS 303. REPAIRED IAW SRM 51-40-3, 51-30-2. 2L73 4F A3WE 19950707001681995070700168NM 1995 7 7 UPS203739 119950703A5320 WEB BOEING727 72725C 138400HNM FS 1175 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR WEB AT STA 1175, AT RBL 40. REPAIRED IAW SRM 51-40-2, 51-30-2. 2L73 4F A3WE 19950707001691995070700169NM 1995 7 7 UPS203740 119950703A5320 TEE BOEING727 72725C 138400HNM FS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, LBL 70.5, WL 200. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950707001701995070700170NM 1995 7 7 UPS203741 119950703A5320 TEE BOEING727 72725C 138400HNM FS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TEE AT FS 760, RBL 70.5, WL 200 ON THE I/B FLANGE. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950707001711995070700171NM 1995 7 7 UPS203742 119950703A5320 WEB BOEING727 72725C 138400HNM FS 294-312 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED WEB AT STA 294 TO 312, RBL 40, WL 207. REPAIRED IAW SRM 51-30-2, 51-20-1, M/M 51-20-151. 2L73 4F A3WE 19950707001721995070700172NM 1995 7 7 UPS203743 119950703A5755 SKIN BOEING727 72725C 138400HNM NR 9 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER, 4 INCH BY 4.5 INCH ON THE NR 9. REPAIRED IAW SRM 51-40-06. 2L73 4F A3WE 19950707001731995070700173NM 1995 7 7 UPS203744 119950703A5755 SKIN BOEING727 72725C 138400HNM NR 5 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED SPOILER AT UPPER I/B CORNER 4 INCH BY 4.5 INCH ON THE NR 5. REPAIRED IAW SRM 51-40-06. 2L73 4F A3WE 19950707001741995070700174EU 1995 7 7 WWMA00045 119950614A3230 CIRCUIT BREAKER SAAB SF340 340B 7860101EU LANDING GEAR TRIPPED A WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15339SB 340B339 FLIGHT 5204 AMA/DFW, PILOT REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT, AN ATTEMPT TO OVERRIDE AND RETRACT THE GEAR WAS NOT SUCCESSFUL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO AT AMA WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THE PROBLEM TO BE A POPPED CIRCUIT BREAKER FOR THE LANDING GEAR CONTROL. THE CB WAS RESET, OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE. 2L72 4T RTA52EU 19950707001751995070700175NE 1995 7 7 WWMA9500042 219950609A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE STALLED A AWWMAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 WP15332AE 340B332 FLIGHT 3420 - LAS/LAX - PILOT REPORTED THAT DURING TAKEOFF, AT APPROXIMATELY 400 FEET A LOUD BANG WAS HEARD COMING FROM THE LT ENGINE, AT WHICH TIME THE ENGINE STARTED TO SHUTDOWN CONSISTENT WITH A COMPRESSOR STALL. INFLIGHT SHUTDOWN PROCEDURES WERE EFFECTED ON THE LT ENGINE AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED AN INLET COMPRESSOR INSPECTION AS WELL AS A BORESCOPE ON THE COMPRESSOR AND HOT SECTION, WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT WHICH IT SUBSEQUENTLY FAILED FOR THE IDENTICAL PROBLEM. 2L72 4T4 TRTA52EU E8NE 19950707001761995070700176NE 1995 7 7 WWMA9500043 219950609A73206068T72P09 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE DEFECTIVE A AWWMAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 WP15332AE 340B332 FUNCTIONAL CHECK, FLIGHT 7794 LAS/LAX - PILOT REPORTED THAT DURING TAKEOFF AT 400 FEET HE ENCOUNTERED A COMPRESSOR STALL ON THE LT ENGINE. INFLIGHT SHUTDOWN PROCEDURES WERE EFFECTED ON LT ENGINE AND AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED LEFT ENGINE HMU AND LT ENGINE ANTI-ICE BLEED VALVE. PERFORMED SATISFACTORY GROUND RUNS AND THE AIRCRAFT WAS RELEASED FOR FCF. THE FUNCTIONAL CHECK FLIGHT WAS CONDUCTED WITHOUT ANY PROBLEMS AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19950707001771995070700177EU 1995 7 7 WWMA9500044 119950612A3520K386371 O2 MASK BAG JETSTMJETSTM3201 1500217EU CABIN SEAT 7A DEPLOYED A WWMAK NONE O OTHER CRCRUISE 1 WP15969AE 969 FLIGHT 3243 - BFL/LAX - PILOT REPORTED THAT THE O2 MASK AT SEAT 7A DEPLOYED FOR NO APPARENT REASON. MAINTENANCE PERSONNEL RESTOWED THE MASK AND THE AIRCRAFT WAS RELEASED BACK TO SERVICE. 2L72 4T RTA56EU 19950707001781995070700178EU 1995 7 7 WWMA9500045 119950615A2120 AIR DISTR SAAB SF340 340B 7860101EU CABIN ODOR A WWMAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP15313AE 340B313 FLIGHT 3432 - LAS/LAX - PILOT REPORTED DURING CLIMB AND DESCENT A VERY STRONG ODOR WAS EMITTED FROM THE GASPERS AND A/C VENTS. MAINTENANCE INSPECTED THE RECIRCULATION FAN FILTERS AND INSPECTED THE RIGHT AND LEFT ACM OIL LEVELS. GROUND RUNS PERFORMED ON BOTH ACM PACKS AND ALL CHECKS WERE GOOD. NO ABNORMAL ODOR EMITTED DURING THE GROUND RUN CYCLE. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA52EU 19950707001791995070700179EU 1995 7 7 WWMA9500046 119950622A32309902A SHUTTLE VALVE BAG JETSTMJETSTM3201 1500217EU LT MLG DEFECTIVE A WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15952AE 952 FLIGHT 3269 - LAX/IYK - PILOT REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THE LT SIDE SHUTTLE VALVE HAD FAILED AND REPLACED THE VALVE. GEAR SWINGS AND OPERATIONAL CHECKS WERE PERFORMED WITH SATISFACTORY RESULTS. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19950707001801995070700180WP 1995 7 7 9510269944 119950626A5720 DOUBLER DOUG DC9 DC931 3022065WP LT MLG CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A CRACK IN THE LEFT UPPER MLG SUPPORT DIAMOND DOUBLER. REPAIRED DOUBLER PER EA 99-100790 (P/N 5912438-1). 2L72 4F A6WE 19950707001811995070700181WP 1995 7 7 9510279944 119950628A5311 FRAME DOUG DC9 DC931 3022065WP FS 598 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND A CRACK IN THE FS 598 FRAME AT LONGERON 11R. REPAIRED FRAME (P/N 9919621-2) PER EA 99-99924. 2L72 4F A6WE 19950707001821995070700182WP 1995 7 7 9510289150 119950629A5241 SUPPORT DOUG DC9 DC914 3022034WP GALLEY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND A 1 INCH CRACK IN THE FORWARD GALLEY DOOR STOP FITTING SUPPORT AT THE NR 3 BEAM AFT END. REPLACED THE SUPPORT PER SRM 51-30-1. 2L72 4F A6WE 19950707001831995070700183WP 1995 7 7 9510299944 119950629A5412 BLKHD WEB DOUG DC9 DC931 3022065WP FS 965 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011309T 47316 DURING H-CHECK, FOUND OIL CANNING IN THE LEFT AND RIGHT PYLON BULKHEAD WEBS, FS 965. REPAIRED WEB PER EA 99-99925 (P/N 9912243-81). 2L72 4F A6WE 19950707001841995070700184WP 1995 7 7 9510309997 119950629A5312 BLKHD ANGLE DOUG DC9 DC931 3022065WP FS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND CORROSION ON THE FS 110 BULKHEAD 'T' ANGLE FROM LONGERONS 27R TO 28R. REPAIRED ANGLE (P/N 9911509-85) PER EA 99-99926. 2L72 4F A6WE 19950707001851995070700185WP 1995 7 7 9510319997 119950629A5320 SUPPORT DOUG DC9 DC931 3022065WP FS 579 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A CRACK AND CORROSION IN THE FLOORBOARD SUPPORT CAP, FS 579 BL 0. REPAIRED CAP (P/N 5910148-13) PER EA 99-99930. 2L72 4F A6WE 19950707001861995070700186NM 1995 7 7 9510322708 119950629A5313 LONGERON BOEING727 727225 1384077NM FS 950-990 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01817EA 22554 DURING PERIODIC CHECK, FOUND CORROSION ON THE KEEL BEAM CHORD, STRINGER 29L AT BS 950D AND BS 970 TO 990. REPAIRED CHORD (P/N 65-56441-4) PER EA 27-99048. 2L73 4F A3WE 19950707001871995070700187WP 1995 7 7 9510339947 119950627A3260 BULBS DOUG DC9 DC931 3022065WP GEAR INDICATION FAILED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL018938E 47161 DURING APPROACH INTO MSP, NEITHER GEAR UNSAFE LIGHTS OR DOWN AND LOCK GREEN LIGHTS ILLUMINATED ON GEAR EXTENSION. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. RELAMPED ALL GEAR POSITION ANNUNCIATORS. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707001881995070700188NM 1995 7 7 9510346614 119950630A3241392331A ANTI-SKID MODULE BOEING747 747251B 1384892NM LT BODY GEAR LEAKING A NWAAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01614US7152271522 20359 DURING CLIMB AND GEAR RETRACTION, THE NR 4 HYDRAULIC SYSTEM QUANTITY DECREASED TO 1 GALLON. THE CREW DUMPED APPROXIMATELY 100,000 LBS OF FUEL, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT BODY GEAR ANTI-SKID CONTROL MODULE, LEAK AND OPERATIONAL CHECK OK. 2L74 4F A20WE 19950707001891995070700189NM 1995 7 7 9510352709 119950701A5210507945177 DOOR BOEING727 727225 1384077NM MAIN CABIN OUT OF RIG A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01818EA16793131 22555 DURING CLIMB MSP-GEG, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE. FURTHER INVESTIGATION REVEALED AN AIR LEAK AT THE MAIN CABIN DOOR. DOOR WARNING INDICATED THAT THE DOOR WAS CLOSED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THAT THE DOOR WAS OUT OF RIG. ADJUSTED GUIDE ARM. PRESSURE CHECKED OK. CORRECTED COPY: MCD WAS CHANGED TO MAIN CABIN DOOR. 2L73 4F A3WE 19950707001901995070700190NM 1995 7 7 DL72W952743 119950620A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND STR 15L CRACKED AT AFT END ON AFT SIDE OF WING ICE LIGHT HOUSING AT FS 720B PLUS 15. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950707001911995070700191NM 1995 7 7 DL72W952762 119950622A5730 DOOR 570206002 BOEING727 727247 138408FNM LT WING TIP MISSING A DALAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 SO11293WA 0000 22111 ON ARRIVAL LGA, NAV LIGHTS ACCESS DOOR ON LT WING TIP WAS FOUND MISSING. INSTALLED NEW DOOR. 2L73 4F A3WE 19950707001921995070700192NM 1995 7 7 DL72W952832 119950617A5755 TE SKIN 651734781A BOEING727 727247 138408FNM NR 13 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 1969 22110 AT HMV, FOUND SPOILER 13 HAS T/E SEPARATION. REMOVED DAMAGED AREA AND COOKED IN NEW CORE. COMPLETED REPAIR PER SRM 57-50-6. 2L73 4F A3WE 19950707001931995070700193NM 1995 7 7 DL72W952847 119950620A5754 PANEL BOEING727 727247 138408FNM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND .5 INCH CRACK IN I/B UPPER CORNER OF WEB CUTOUT FOR FWD END OF ANTI-ICE DUCT OF NR 1 SLAT PANEL. STOP DRILLED CRACK, FABRICATED DOUBLER PER M/M 57-54-0. 2L73 4F A3WE 19950707001941995070700194NM 1995 7 7 DL72W952928 119950629A3350 EEL BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112814W 20870 DURING INSPECTION, LEFT OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK M654, OPERATION NORMAL. 2L73 4F A3WE 19950707001951995070700195NM 1995 7 7 DL72W952930 119950701A2130 SEAL BOEING727 727247 138408FNM FWD CARGO FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO112820W 21058 ON CLIMBOUT, HAD RT PACK FAILURE LEFT PACK UNABLE TO MAINTAIN PRESSURE. EMERGENCY DESCENT WAS MADE, LANDED ATL. FOUND HULL SEAL CENTER TANK AND FWD CARGO JUNCTION DISPLACED AND TORN. REPAIRED SEAL AND REPLACED RT PACK CONTROL VALVE, OPERATION NORMAL. 2L73 4F A3WE 19950707001961995070700196NM 1995 7 7 DL757952681 119950619A5754114N4005178A PANEL BOEING757 757232 1384965NM LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11640DL 23994 DURING SHOP INSPECTION, SLAT PANEL WAS FOUND WITH T/E WEDGE DELAMINATED. WEDGE WAS REPLACED PER SRM 57-43-02. 2L72 4F RTA2NM 19950707001971995070700197NM 1995 7 7 DL757952926 119950630A2410 IDG BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11656DL 24396 716361 ON CLIMBOUT AT FL 180, HAD LEFT GEN DRIVE EICAS MSG, FOLLOWED BY LEFT ENGINE FIRE WARNING. ENGINE WAS SHUTDOWN, FIRE BOTTLES DISCHARGED, FIRE WARNING WENT OUT. RETURNED TO DFW. FOUND NR 1 ENGINE IDG WITH UNCONTAINED FAILURE. ENGINE WAS REPLACED AND ROUTED TO SHOP. 2L72 4F4 FRTA2NM E17NE 19950707001981995070700198NM 1995 7 7 DL76L952924 119950703A2597 WIRE BOEING767 767332 1382001NM FWD CABIN 1C SHORTED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11184DN 27111 DURING CRUISE, HAD SMOKE AND SPARKS FROM UNDER F/C SEAT 1C. FOUND WIRE FOR SEAT ADJUSTMENT MOTOR CHAFED AND SHORTED. REPAIRED WIRE, OPERATION NORMAL. 2L72 4F RTA1NM 19950707001991995070700199 1995 7 7 DL76L952927 419950702A34604058650931 CDU BOEING767 767332 1382001NM RT FLT DECK FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11182DN 25987 DURING CRUISE, RIGHT FMC CDU WENT BLANK. DIVERTED TO JFK. REPLACED RT CDU, OPERATION NORMAL. 2L72 4F RTA1NM 19950707002001995070700200WP 1995 7 7 DLL13952379 119950509A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 649-749 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 ON HMV, SEAT TRACK CORRODED STA 649 TO 749, 2ND FROM LT SIDE. REPLACED SEAT TRACK PER SRM 53-23-00. 2L73 4F A23WE 19950707002011995070700201WP 1995 7 7 DLL13952744 119950531A5347 TRACK LKHEED1011 10113851 5265010WP FS 1445-1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 AT HMV, FOUND CABIN SEAT TRACKS WITH CORROSION DAMAGE AT FS 1445 TO 1545. REPLACED TRACK PER SRM 53-23-00. 2L73 4F A23WE 19950707002021995070700202NM 1995 7 7 DLM88952925 119950702A4990 APU DOUG MD88 MD88 3023688NM TAIL OIL LEAK A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO11951DL 49882 ON CLIMBOUT, HAD ALL 3 LAV SMOKE DETECTORS ACTIVATE, RETURNED TO BDL. FOUND APU LEAKING OIL AT STARTER CLUTCH ASSEMBLY AND CONTAMINATING APU AIR INTAKE. PERFORMED DUCT BURNOUT AND PLACED APU ON MCO FOR RETURN TO SERVICE. 2L72 4F RTA6WE 19950707002031995070700203WP 1995 7 7 OXEA9500206 219950703A7200 ENGINE GARRTT 31025401 SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NR 1 FAILED A QXEAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 NM09384PH P44326 AC592 P44326 NR 1 ENG FAILED ON APPROACH INTO SEA. AN ATTEMPTED AIR START, NO SUCCESS APPEARS, NO FUEL FLOW. REMOVED AND REPLACED NR 1 ENGINE AND COMPLIED WITH GROUND RUNS. AIRCRAFT WAS TEST FLOWN AND RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19950707002041995070700204NE 1995 7 7 P5CA9500202 219950704A7200JT9D7F ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 4 FAILED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 WP23857FT 20246 663028 ON CLIMBOUT FROM HKG PASSING THROUGH FL 230, NR 4 ENGINE SURGED WITH EGT GOING TO 940 C, ALL PARAMATERS INDICATED FAILED ENGINE. SECURED ENGINE AS PER EMERGENCY CHECK LIST. ON GROUND INSPECTION FOUND METAL IN TAIL PIPE. ENGINE REPLACED. 2L74 4F4 F A20WE E20EA 19950707002051995070700205NM 1995 7 7 P5CA9500203 119950528A5330 SKIN BOEING747 747121 1384871NM FS 1600-1620 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FUSELAGE SKIN, RIGHT SIDE BETWEEN BS 1600 AND 1620 S12R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002061995070700206NM 1995 7 7 P5CA9500204 119950528A5330 SKIN BOEING747 747121 1384871NM FS 2280-2360 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT AND CHAFING IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 2280 AND 2360 BETWEEN S21L AND S23L. DENT STRAIGHTENED AND SMOOTHED PER BOEING SRM 51-40-01 AND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002071995070700207NM 1995 7 7 P5CA9500205 119950528A5330 SKIN BOEING747 747121 1384871NM FS 1720-1740 BULGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BULGE IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1720 AND 1740 AT S32L. REMOVED THE RIVET AND CLEANED PER BOEING SRM 51-10-01. INSTALLED NEW RIVET PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707002081995070700208NM 1995 7 7 P5CA9500206 119950528A5330 SKIN BOEING747 747121 1384871NM FS 1580-1740 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1580 AND 1740 AT S12L, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002091995070700209NM 1995 7 7 P5CA9500207 119950528A5230 HINGE BOEING747 747121 1384871NM CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FWD AND AFT CARGO DOOR HINGES, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01 AND TREATED PER 51-10-02. 2L74 4F A20WE 19950707002101995070700210NM 1995 7 7 P5CA9500208 119950528A5330 SKIN BOEING747 747121 1384871NM FS 2240 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT AND SCRATCHES IN FUSELAGE SKIN RIGHT SIDE AT BS 2240 UNDER NR 5R DOOR. BLENDED OUT SCRATCHES PER BOEING SRM 51-10-01, DENT WITHIN LIMITS PER BOEING SRM 53-10-1. 2L74 4F A20WE 19950707002111995070700211NM 1995 7 7 P5CA9500209 119950528A5330 SKIN BOEING747 747121 1384871NM FS 1800-1820 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN THE FUSELAGE SKIN BETWEEN BS 1800 TO BS 1820 AND BETWEEN S46R AND S46R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002121995070700212NM 1995 7 7 P5CA9500210 119950528A5330 SKIN BOEING747 747121 1384871NM FS 2360 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN FUSELAGE SKIN RIGHT SIDE BS 2360 BETWEEN S22R AND S25R, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002131995070700213NM 1995 7 7 P5CA9500211 119950528A5330 SKIN BOEING747 747121 1384871NM FS 720-740 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 720 AND 740, BETWEEN S27L AND S28L. SMOOTHED DENT PER BOEING SRM 51-40-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950707002141995070700214NM 1995 7 7 P5CA9500212 119950528A5320 RAIN CHANNEL BOEING747 747121 1384871NM BS 860 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT IN RAIN CHANNEL AT FUSELAGE LEFT SIDE ABOVE L2 DOOR AT BS 860. BLENDED OUT DENT PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707002151995070700215NM 1995 7 7 P5CA9500213 119950528A5330 SKIN BOEING747 747121 1384871NM BS 1700-1720 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT WITH SCRATCH IN FUSELAGE SKIN LEFT SIDE BETWEEN BS 1700 AND 1720, BETWEEN S37L AND S38L. STRAIGHTENED DENT AND BLENDED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002161995070700216NM 1995 7 7 P5CA9500214 119950528A5414 SKIN BOEING747 747121 1384871NM NR 1 PYLON CHAFED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CHAFED SKIN AT NR 1 NACELLE STRUT TOP SKIN AT NS 222. SMOOTHED OUT SKIN, WITHIN LIMITS PER BOEING SRM 54-10-01. 2L74 4F A20WE 19950707002171995070700217NM 1995 7 7 P5CA9500215 119950528A5753 BEARING BOEING747 747121 1384871NM NR 7 FLAP TRACK MIRGATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BEARING HAS ROTATION AND MIGRATED RIGHT WING, NR 7 FLAP TRACK UNDER WING FORWARD LUG MOUNT. REPAIRED ACCORDING TO BOEING SERVICE BULLETIN 747-57-2262. 2L74 4F A20WE 19950707002181995070700218NM 1995 7 7 P5CA9500216 119950528A5751 RIB BOEING747 747121 1384871NM RT INBD AILERON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR IN LIGHTENING HOLE RIGHT INBOARD AILERON NEAR INBOARD HINGE. REPAIRED PER BOEING SRM 57-20-01. 2L74 4F A20WE 19950707002191995070700219NM 1995 7 7 P5CA9500217 119950528A5720 ANGLE BOEING747 747121 1384871NM WS 600 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO ANGLE BRACKETS ARE CRACKED RIGHT WING TRAILING EDGE WS 600, UNDER NR 7 SPOILER PCU. MANUFACTURED NEW ANGLES PER BOEING SRM 57-20-02, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707002201995070700220NM 1995 7 7 P5CA9500218 119950528A5730 SKIN BOEING747 747121 1384871NM WS 630 LE LOOSE RIVETS A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LOOSE RIVETS AND 1 MISSING RIVET ON WING LEADING EDGE SKIN WS 630 ABOVE NACELLE NR 3. REPLACED RIVETS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707002211995070700221NM 1995 7 7 P5CA9500219 119950528A5720 FAIRING BOEING747 747121 1384871NM RT WING DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE FAIRING WS 630 EDGE IS DAMAGED AND FIBERGLASS AROUND FASTENER HEADS ARE PEELING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707002221995070700222NM 1995 7 7 P5CA9500220 119950528A5320 SUPPORT BOEING747 747121 1384871NM FS 1000-1240 CORRODED A AP5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT AND AROUND ACCESS FOR AIR CONDITIONING BETWEEN BS 1000 AND 1240, BETWEEN LBL 16 AND LBL 90, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002231995070700223NM 1995 7 7 P5CA9500221 119950528A5320 SPLICE STRAP BOEING747 747121 1384871NM BS 1241 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS IN AFT HOLES OF THE BS 1241 SPLICE STRAP LEFT AND RIGHT SIDE. REPLACED STRAPS PER BOEING SERVICE BULLETIN 747-53-2283. 2L74 4F A20WE 19950707002241995070700224NM 1995 7 7 P5CA9500222 119950528A5320 SUPPORT BOEING747 747121 1384871NM BS 1030 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FAIRING SUPPORT AT BS 1030 RBL 120. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707002251995070700225NM 1995 7 7 P5CA9500223 119950528A5320 WALL BOEING747 747121 1384871NM BS 1100 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR IN WALL AT BS 1100 RBL 98. REPAIRED PER BOEING SRM 53-40-02. 2L74 4F A20WE 19950707002261995070700226NM 1995 7 7 P5CA9500224 119950528A5200 DOOR BOEING747 747121 1384871NM BS 1050 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON DOOR AT BS 1050 NEAR HINGE RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002271995070700227NM 1995 7 7 P5CA9500225 119950528A5312 BLKHD ANGLE BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION Z-ANGLE, ON THE BULKHEAD BS 1240 RIGHT SIDE, LEVEL 1. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. 2L74 4F A20WE 19950707002281995070700228NM 1995 7 7 P5CA9500226 119950528A5320 SUPPORT BOEING747 747121 1384871NM BS 1050 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT BRACKET BS 1050 RIGHT SIDE, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950707002291995070700229NM 1995 7 7 P5CA9500227 119950528A5320 SUPPORT BOEING747 747121 1384871NM BS 1240 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FAIRING SUPPORT BS 1240 LBL 125. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707002301995070700230NM 1995 7 7 P5CA9500228 119950528A5320 SUPPORT BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FAIRING SUPPORT AT BS 1240 LEFT SIDE. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002311995070700231NM 1995 7 7 P5CA9500229 119950528A5414 SKIN BOEING747 747121 1384871NM NR 1 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 A .25 INCH CRACK AT NS 222 AND .5 INCH CRACK AT NS 236. DISCOVERED AFTER REMOVAL OF DOUBLER NR 1 PYLON. REPAIRED PER BOEING SRM 54-30-03 PAGE 113. 2L74 4F A20WE 19950707002321995070700232NM 1995 7 7 P5CA9500230 119950528A5330 SKIN BOEING747 747121 1384871NM BS 1470 TEAR A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON SHEET METAL AT BS 1470 LBL 15. REPAIRED PER BOEING SRM 52-10-02. 2L74 4F A20WE 19950707002331995070700233NM 1995 7 7 P5CA9500231 119950528A5350 FAIRINGS BOEING747 747121 1384871NM LOWER FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FAIRING PANELS NR 1 RT AND 292C DENTED. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707002341995070700234NM 1995 7 7 P5CA9500232 119950528A5350 FAIRING BOEING747 747121 1384871NM LOWER FUSELAGE DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION AND DENTS, FAIRING PANELS NR 191H, 191E, AND 191F. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707002351995070700235NM 1995 7 7 P5CA9500233 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION ON FAIRING PANEL NR 192E. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707002361995070700236NM 1995 7 7 P5CA9500234 119950528A5350 FAIRING BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS AND DELAMINATION ON FAIRING PANELS NR 292C, 294A, 291D, 5L AND 6L. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950707002371995070700237NM 1995 7 7 P5CA9500235 119950528A5343 FITTING BOEING747 747121 1384871NM BS 1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION BS 1350 RT UPPER CORNER FITTING RIGHT BODY GEAR WHEEL WELL. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002381995070700238NM 1995 7 7 P5CA9500236 119950528A5320 ANGLE BOEING747 747121 1384871NM BS 1287 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN ANGLE SUPPORT FOR HYD TUBE AT STA 1287 IN THE RIGHT WING GEAR WHEEL WELL. MANUFACTURED NEW ANGLE PER BOEING SRM 57-10-02. 2L74 4F A20WE 19950707002391995070700239NM 1995 7 7 P5CA9500237 119950629A5314 KEEL BEAM BOEING747 747121 1384871NM RIGHT CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON UPPER SIDE OF KEEL BEAM BOX, RIGHT BODY GEAR WHEEL WELL, LEVEL 1. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950707002401995070700240NM 1995 7 7 P5CA9500238 119950629A5412 BULKHEAD BOEING747 747121 1384871NM NR 1 PYLON BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 PYLON BULKHEAD LOWER SIDE BADLY BENT NS 180. REPAIRED PER BOEING SRM 51-10-02 AND 51-30-02. 2L74 4F A20WE 19950707002411995070700241NM 1995 7 7 P5CA9500239 119950629A5400 DOUBLER BOEING747 747121 1384871NM NR 1 PYLON GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DEEP SKIN GOUGE LEFT SIDE NS 240 NR 1 PYLON. REPLACED DOUBLER PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707002421995070700242NM 1995 7 7 P5CA9500240 119950629A5400 FAIRING BOEING747 747121 1384871NM NR 1 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HOLE ON UNDER WING AT TRAILING EDGE FAIRING RIGHT SIDE NR 1 PYLON. REPAIRED PER 51-40-02. 2L74 4F A20WE 19950707002431995070700243NM 1995 7 7 SWAA950491 119950627A5240 SKIN BOEING737 7373H4 1384600NM FWD SERVICE DOORGOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT AT LOWER OUTER SKIN. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002441995070700244NM 1995 7 7 SWAA950492 119950627A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 709 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM WEB CRACKED AT BS 709, BL 0 WL 204. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002451995070700245NM 1995 7 7 SWAA950493 119950627A5240 SKIN BOEING737 7373H4 1384600NM FWD SERV DOOR GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT LOWER EDGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002461995070700246NM 1995 7 7 SWAA950494 119950627A5240 SKIN BOEING737 7373H4 1384600NM FWD SERV DOOR GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN GOUGED AT LOWER HINGE CUTOUT LOWER EDGE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002471995070700247NM 1995 7 7 SWAA950495 119950627A5240 SKIN BOEING737 7373H4 1384600NM FWD SERV DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOOR OUTER SKIN DAMAGED 6 INCHES ABOVE LOWER HINGE CUTOUT OUTER EDGE AND CRACKED AT RIVET HEAD 1 INCH ABOVE LOWER CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002481995070700248NM 1995 7 7 SWAA950496 119950627A5311 FRAME BOEING737 7373H4 1384600NM BS 807-887 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 807 AND BS 887, AT S9L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002491995070700249NM 1995 7 7 SWAA950497 119950627A5311 FRAME BOEING737 7373H4 1384600NM BS 344 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 344, S8R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002501995070700250NM 1995 7 7 SWAA950498 119950627A5311 FRAME BOEING737 7373H4 1384600NM BS 867/907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT LOWER HAT SECTION SUPPORT AT BS 867, S9L AND AT BS 907, S9L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002511995070700251NM 1995 7 7 SWAA950499 119950627A532069414376 CLIPS BOEING737 7373H4 1384600NM BS 663/1138 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, S10L AND S10R, AND AT BS 1138, S13L. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002521995070700252NM 1995 7 7 SWAA950500 119950627A5754 TE SKIN BOEING737 7373H4 1384600NM NR 3/4 LE SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND NR 3 SLAT CRACKED AT T/E SKIN O/B OF ACTUATOR AND NR 4 SLAT CRACKED AT LOWER T/E SKIN, I/B OF ACTUATOR. REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002531995070700253NM 1995 7 7 SWAA950501 119950627A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 727E PLUS 13 BETWEEN S2 AND 3L, AT BS 796, S3L, AT BS 278, BETWEEN S2 AND 3L, AT BS 488, S3L, AT BS 847 AND 858, S3L, AND AT BS 727D PLUS 3.75, ABOVE S3L. REPAIRED ALL PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002541995070700254NM 1995 7 7 SWAA950502 119950627A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR UPPER HINGE CUTOUT AT LOWER I/B CORNER. REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002551995070700255NM 1995 7 7 SWAA950503 119950627A5312 BLKHD WEB BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND BS 178 PRESSURE WEB CRACKED AT WL 219, LBL 11.4 AND AT WL 212, LBL 4.7. REPAIRED PER BOEING BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002561995070700256NM 1995 7 7 SWAA950504 119950627A5320 SPLICE BOEING737 7373H4 1384600NM BS 908 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, S4L. REPLACED PER BOEING BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002571995070700257NM 1995 7 7 SWAA950505 119950627A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FLOOR BEAM CORROSION AT BS 986.5, RBL 27 AND 31.5. REPLACED PER SWA RA 1-353-542. 2L72 4F RTA16WE 19950707002581995070700258NM 1995 7 7 SWAA950506 119950627A5330 SKIN BOEING737 7373H4 1384600NM BS 860-887 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DAMAGE FROM BS 860 TO BS 887, BETWEEN S2L AND S2R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002591995070700259NM 1995 7 7 SWAA950507 119950627A531365617777 STRINGER BOEING737 7373H4 1384600NM BS 360 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND STRINGER 15L CHANNEL CRACKED AT BS 360. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002601995070700260NM 1995 7 7 SWAA950508 119950627A5330 SKIN BOEING737 7373H4 1384600NM BS 1054 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07311SW 23333 DURING SCHEDULED D-CHECK, FOUND FUSLAGE SKIN DENTED AT BS 1054, S17-18R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950707002611995070700261NM 1995 7 7 SWAA950509 119950703A5320 WEB BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED CHECK, FOUND NOSE GEAR WHEELWELL LEFT VERTICAL WEB CRACKED JUST BELOW LEFT FWD ACCESS PANEL CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950707002621995070700262NM 1995 7 7 SWAA950510 119950703A5320 WEB BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED CHECK, FOUND NOSE GEAR RETRACT ACTUATOR SUPPORT VERTICAL WEB CRACKED JUST BELOW LEFT FWD ACCESS PANEL CUTOUT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950707002631995070700263NM 1995 7 7 SWAA950511 119950630A5270 DOOR WARNING BOEING737 7373H4 1384600NM FWD ENTRY MALFUNCTIONED A SWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW07673AA 23251 ABORTED TAKEOFF DUE TO MASTER CAUTION INDICATING FWD ENTRY DOOR OPEN. RETURNED TO GATE. INSPECTED AND FOUND DOOR SECURED AND LOCKED. PLACED DOOR WARNING ON MEL 52-2. INSPECTED TIRES/BRAKES AND CONTINUED PER BOEING M/M. 2L72 4F RTA16WE 19950707002641995070700264NM 1995 7 7 SWAA950512 119950630A2910 HYD LINE BOEING737 7372T4 1384492NM AILERON PCU RUPTURED A SWAAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW07702ML 22054 ON APPROACH, CREW EXPERIENCED A-SYSTEM PRESSURE LOSS. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AND FOUND AN AILERON PCU LINE RUPTURED. REPLACED LINE, FLUSHED SYSTEM, AND INSPECTED FILTERS PER BOEING M/M. 2L72 4F A16WE 19950707002651995070700265NM 1995 7 7 SWAA950513 119950701A7930 FILTER LIGHT BOEING737 7372T4 1384492NM NR 2 ENGINE ILLUMINATED A SWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SW07129SW 22340 NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE POWER WAS REDUCED TO IDLE, NO HELP. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT ABQ WITHOUT INCIDENT. INSPECTED ENGINE FILTER, NO DEFECTS NOTED. CLEANED FILTER, PLACED INDICATOR ON MEL 79-2, AND CONTINUED PER BOEING M/M. 2L72 4F A16WE 19950707002661995070700266NM 1995 7 7 UPS403745 119950701A5522 TE SKIN BOEING747 747123 1384873NM RT ELEVATOR DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND IN ONT, MAINTENANCE FOUND RT I/B ELEVATOR T/E DELAMINATED. REPAIRED IAW SRM 51-40-15. 2L74 4F A20WE 19950707002671995070700267EU 1995 7 7 WWMA00047 119950614A3230 CIRCUIT BREAKER SAAB SF340 340B 7860101EU LANDING GEAR TRIPPED A WWMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15339SB 340B339 FLIGHT 5204 - AMA/DFW - PILOT REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. AN ATTEMPT TO OVERRIDE AND RETRACT THE GEAR WAS NOT SUCCESSFUL. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED AND LANDED AT AMA WITHOUT INCIDENT. MAINTENANCE PERSONNEL DETERMINED THE PROBLEM TO BE A POPPED CIRCUIT BREAKER FOR THE LANDING GEAR CONTROL. THE CB WAS RESET, OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED BACK TO SERVICE. 2L72 4T RTA52EU 19950707004221995070700422NM 1995 7 7 95ZZZM188 119950606A323065178105 DNLOCK ACTUATOR BOEING727 72721 1384003NM NLG FAILED A RYNAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE07359QS 19007 ON APPROACH INTO DAYTON, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATED ON GEAR EXTENSION. PERFORMED MANUAL GEAR EXTENSION AND ALL GEARS INDICATED DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NOSE GEAR DOWNLOCK ACTUATOR, OPS CHECKED GOOD. 2L73 4F A3WE 19950707004231995070700423WP 1995 7 7 95ZZZM189 119950511A5330 SKIN DOUG DC8 DC863F 302198FWP FS 1060-1080 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 LEVEL 3 CORROSION FOUND ON BELLY SKIN UNDER LONGERONS 35L, 35R BETWEEN FS 1060 AND FS 1080 CIRCUMFERENTIALS. CUTOUT DAMAGED SKIN AT LONGERONS 35L AND 35R BETWEEN FS 1060 AND FS 1080. ALSO, CUTOUT DAMAGE SKIN AT FS 1100 LONGERONS 35L. INSTALLED REPAIR FILLERS AND DOUBLERS IAW DER DWG ARW 26467-53. 2L74 4F 4A25 19950707004241995070700424WP 1995 7 7 95ZZZM190 119950531A53111616373 FRAME CAP DOUG DC8 DC863F 302198FWP FS 1120 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 CIRCUMFERENTIAL FRAME CAP AT FS 1120 BETWEEN LONGERONS 33L AND 34L HAS LEVEL 3 CORROSION. REMOVED CORROSION FROM CAP. FABRICATED AND INSTALLED DOUBLER IAW DER DWG ARW 26494-64. 2L74 4F 4A25 19950707004251995070700425WP 1995 7 7 95ZZZM191 119950526A5330 SKIN DOUG DC8 DC861 3021952WP FS 1350-1450 CORRODED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION WAS FOUND AFT LOWER SKIN FROM FS STATION 1350 TO FS 1450 BETWEEN LONGERONS 31L TO 31R. REMOVED AND REPLACED AFT LOWER SKIN FROM FS 1350 TO FS 1450 BETWEEN 31L TO LONGERON 31R IAW SRM 51-1-21. 2L74 4F 4A25 19950707004261995070700426WP 1995 7 7 95ZZZM192 119950526A5330 SKIN DOUG DC8 DC861 3021952WP FS 1680 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION WAS FOUND LEFT SIDE OF THE AIRCRAFT IN THE FUSELAGE SKIN FS 1680 BETWEEN L-22L TO L-24L. TRIMMED OUT DAMAGED SKIN, INSTALLED A .071 7075-T6 FILLER AND INSTALLED A .080 7075-T6 EXTERNAL DOUBLER IAW EO 9505251. AN 8110-3 ISSUED BY DER SW-713. 2L74 4F 4A25 19950707004271995070700427WP 1995 7 7 95ZZZM193 119950526A5320 JAMB DOUG DC8 DC861 3021952WP CARGO DOOR CRACKED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, MAINTENANCE FOUND A CRACK ON THE FORWARD CARGO COMPARTMENT FORWARD DOOR FORWARD LOWER JAMB CORNER. CUTOUT CRACKED SKIN, INSTALLED FILLER AND INSTALLED EXTERNAL DOUBLERS IAW DOUGLAS SRO DRAWING SR08530019 AND DOUGLAS LETTER NR MISC 2400/RKK. 2L74 4F 4A25 19950707004281995070700428WP 1995 7 7 95ZZZM194 119950526A5320 JAMB DOUG DC8 DC861 3021952WP CARGO DOOR CRACKED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, MAINTENANCE FOUND A CRACK ON FORWARD CARGO COMPARTMENT FORWARD DOOR UPPER AFT JAMB CORNER. CUTOUT CRACKED SKIN, INSTALLED FILLER AND INSTALLED EXTERNAL DOUBLERS IAW DOUGLAS SRO DRAWING 8530019. 2L74 4F 4A25 19950707004291995070700429WP 1995 7 7 95ZZZM195 119950526A5751 SKIN DOUG DC8 DC861 3021952WP RT AILERON CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION AND DISBONDING WAS FOUND ON THE RIGHT OUTBOARD AILERON LOWER SKIN PANEL. REMOVED LOWER SKIN AND REPLACED WITH AN 040 2024-T3 SKIN PANEL IAW EO 9505072. AN 8110-3 ISSUED BY DER SW-713. 2L74 4F 4A25 19950707004301995070700430WP 1995 7 7 95ZZZM196 119950526A5320 DOUBLER DOUG DC8 DC861 3021952WP FS 1160 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AROUND THE OPENING OF THE C-3 DOOR FS 1160. TRIMMED OFF CORROSION DAMAGE, INSTALLED .125 7075-T6 FILLER WITH .125 7075-T6 EXTERNAL DOUBLER IAW EO 9505061. AN 8110-3 ISSUED BY DER SW-713. 2L74 4F 4A25 19950707004311995070700431WP 1995 7 7 95ZZZM197 119950526A5311 FRAME DOUG DC8 DC861 3021952WP FS 1700 CORRODED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1927UA 43107 45942 DURING C-CHECK, CORROSION DAMAGE WAS FOUND ON THE FUSELAGE FRAME AT FS 1700 BETWEEN L34R AND L35L. REMOVED AND REPLACED FUSELAGE FRAME AT FS 1700. INSTALLED STRAP DOUBLER AND ACCOMPLISHED REPAIR SPLICE ON FUSELAGE FRAME IAW EO 9505191. AN 8110-3 ISSUED BY DER SW-713. 2L74 4F 4A25 19950707004321995070700432CE 1995 7 7 95ZZZM198 119950609A575335165050258 TE SKIN BEECH 1900 1900C 1154161CE LT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE0785YV 1837 874 UC85 DURING SCHEDULED MAINTENANCE, A 1 INCH CRACK 3 INCHES FROM INBOARD EDGE AND .625 INCH FROM TRAILING EDGE. STOPPED DRILLED AND INSTALLED PATCH. 2L72 4T RTA24CE 19950707004331995070700433CE 1995 7 7 95ZZZM199 119950510A575335165050259 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV1628 745 UC137 DURING SCHEDULED MAINTENANCE, A 1.5 INCH CRACK WAS FOUND ON RIGHT OUTBOARD FLAP, 16 INCHES INBOARD OF END CAP AND 5 INCHES AFT OF LEADING EDGE. REPAIRED BY STOP DRILLED CRACK AND INSTALLED DOUBLER. (M) 2L72 4T RTA24CE 19950707004341995070700434CE 1995 7 7 95ZZZM200 119950514A57301181100477 LE SKIN BEECH 1900 1900C 1154161CE LT WING DENTED A AMWAK NONE O OTHER APAPPROACH 1 CE0797YV 11841 UC97 INBOUND TO DSM THE LEFT WING TOOK A BIRD STRIKE 3 FEET INBOARD OF WING TIP. REPAIRED WITH 14 INCH FILLER PATCH. 2L72 4T RTA24CE 19950707004351995070700435CE 1995 7 7 95ZZZM201 119950524A575310116000144 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07160AM 5283 635 UC160 DURING SCHEDULED MAINTENANCE, A .875 INCH CRACK WAS FOUND 15 INCHES FROM OUTBOARD EDGE AND 6 INCHES FROM TRAILING EDGE OF RIGHT INBOARD FLAP. STOPPED DRILLED AND INSTALLED DOUBLER. 2L72 4T RTA24CE 19950707004361995070700436CE 1995 7 7 95ZZZM202 119950531A7120 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV11110 UC134 DURING AD 95-02-18 AREA 'A' INSPECTION A .5 INCH CRACK WAS FOUND JUST AFT OF INBOARD UPPER BOSS ON RIGHT TRUSS. WELDED TRUSS AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950707004371995070700437EU 1995 7 7 95ZZZM203 119950531A772221180422 SRL COMP GARRTT BAG JETSTMJETSTM3101 1500215EU RT ENGINE DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07843JS 16580 757 FLT 4105 - DURING TAKEOFF ROLL RT ENGINE SRL CAP LIGHT ILLUMINATED. CREW ELECTED TO ABORT TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REMOVED AND REPLACED SRL COMPUTER IAW MM 72-00-00. OPS GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950707004381995070700438NE 1995 7 7 95ZZZM204 319950609A6110HCE4A3A PROPELLER BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RT ENGINE LEAKING A AMASAK NONE K FLUID LOSS ININSP/MAINT 1 SW012YV 3129 3129 UE2 HJ192A DURING PREFLIGHT INSPECTION, CAPTAIN NOTICED EXCESSIVE AMOUNT OF OIL ON RIGHT ENGINE COWL. MAINTENANCE CONTROL NOTIFIED AND MAINTENANCE DISPATCHED TO AIRCRAFT TO INVESTIGATE. UPON INVESTIGATION DETERMINED OIL COMING FROM PROP BLADE AREA FORWARD OF SPINNER BULKHEAD. AIRCRAFT FERRIED TO BULLHEAD CITY MAINTENANCE FACILITY. PROP WAS REMOVED AND REPAIRED BY CHANGING PITCH CHANGE ROD. PROP WAS RE-INSTALLED AND AIRCRAFT RETURNED TO SERVICE. REFERENCE HARTZELL SB 214. 2L72 4T RTA24CE 5 CP10NE 19950707004391995070700439 1995 7 7 95ZZZM205 319950619A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE RT PROP MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01852CA4056 1079 UE55 ON RIGHT PROP, THREE INCHES MISSING FROM DE-ICE BOOT ON ONE BLADE. A SECTION OF LEADING EDGE METAL ABRASION STRIP WAS ALSO FOUND DETACHED FROM THE COMPOSITE BLADE. PROP WAS REMOVED AND REPLACED WITH AN AIRWORTHY UNIT. APPARENT CAUSE IMPROPER BONDING. (M) 2L72 4T RTA24CE 19950707004401995070700440WP 1995 7 7 EIAA95001 119950501A3230 RETRACT MECH DOUG DC9 DC932F 3022067WP NOSE GEAR LACK OF LUBE A EIAAO OTHER J WARNING INDICATION CLCLIMB 1 NM09932F 47355 SEA - UNSATISFACTORY GEAR UPLATCH CHECK AFTER TAKEOFF, RED NOSE GEAR UNSAFE LIGHT ON. NOSE GEAR EXTENDED DURING UPLATCH CHECK. RECYCLED GEAR, SAME SITUATION. CONTINUED TO SEA WITH RIGHT HYDRAULIC SYSTEM ON HIGH. NOTED SLIGHT NOISE AND VIBRATION FROM NOSE IN CRUISE. PERFORMED OPERATIONAL CHECK OF NOSE GEAR IAW MM 32-20-00. NO DEFECTS FOUND. ALL OPERATIONS WERE NORMAL. UPLATCH CHECK WAS NORMAL WITH AND WITHOUT LOAD. FREE FALL CHECKS OPERATION WAS NORMAL. AFT NOSE GEAR DOOR PRE-LOAD IS GOOD. LUBED NOSE AND MAIN GEAR ASSEMBLIES. NOSE STRUT SERVICED IAW MM 32-21-2. (M) 2L72 4F A6WE 19950707004411995070700441WP 1995 7 7 EIAA9503 119950114A57115911300502 SPAR CAP DOUG DC9 DC933F 302207AWP WS 133-137 CORRODED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09933F 48543 47191 DURING C-CHECK INSPECTION, FOUND CORROSION ON RIGHT UPPER REAR SPAR CAP AFT FLANGE XRS -133 TO -137. CORROSION BLENDOUT EXCEEDED DC9 SRM LIMITS. THE BLENDED AREA WAS TEMPORARILY REPAIRED USING 7075-T6 DOUBLERS, ANGLES AND FILLERS INSTALLED WET WITH SEALANT. REPETITIVE INSPECTION IS REQUIRED ON REPAIR AREA AT 120 FLIGHT HOUR INTERVALS. REPLACEMENT OF SPAR CAP TERMINATES REPAIR AT 2000 FLIGHT HOURS OF 2 YEARS AFTER COMPLETION OF REPAIR. ACCOMPLISHED IAW EVERGREEN INTERNATIONAL AIRLINES, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR 933-57-028-2. (M) 2L72 4F A6WE 19950707004421995070700442WP 1995 7 7 EIAA9505 119950203A3231 RETRACT MECH DOUG DC9 DC932F 3022067WP NLG DOOR MALFUNCTIONED A EIAAO OTHER J WARNING INDICATION CLCLIMB 1 NM09932F 47355 SEA - NOSE GEAR UNSAFE LIGHT CAME ON, UPON DEPARTURE FROM PAJN. RECYCLED GEAR TWICE, NO CHANGE. VISUAL INSPECTION THROUGH PEEP HOLE REVEALED LIGHT IN THE NOSE WHEEL AREA. INSPECTED NOSE GEARS AND DOORS PER MM 32-20-0, PG 201. ALL CHECKS GOOD. GEAR SWING CHECKS GOOD. (M) 2L72 4F A6WE 19950707004431995070700443WP 1995 7 7 EIAA9506 119950207A3260 HANDLE DOUG DC9 DC933F 302207AWP LANDING GEAR LACK OF LUBE A EIAAO OTHER P NO WARNING INDICATION APAPPROACH 1 NM09933F 47191 LEFT MAIN GEAR DOWN, GREEN LIGHT INOPERABLE. DID NOT WORK ON GEAR EXTENSION. WILL NOT TEST ON GROUND. COULD NOT PULL EMERGENCY GEAR EXTENSION LEVER TO FULL TRAVEL UPWARD. BEGAN TO BIND WHEN PULLED UP ON HALF OF FULL TRAVEL. RETURNED TO SECURED POSITION BECAUSE OF GRINDING NOISE DURING MOVEMENT OF HANDLE UP OR DOWN. FOUND PUSHED PIN IN CANNON PLUG AT MAIN GEAR DOWNLOCK SWITCH. RESEATED PIN, LIGHT OPS CHECKS GOOD. CLEANED DIRT AND DUST FROM EXTENSION HANDLE PIVOT POINT. HANDLE OPERATES SMOOTHLY, LUBED HANDLE PIVOT POINT. HANDLE OPERATES SMOOTHLY, LUBED HANDLE PIVOT, TESTED WITH FISH SCALE, 60 LBS OF PRESSURE TO LOCK DETENT, WITHIN LIMITS PER MM 32-31-02, PG 204. (M) 2L72 4F A6WE 19950707004441995070700444NM 1995 7 7 IXKA9500020 119950614A2782651781821 ACTUATOR BOEING727 727225 1384077NM NR 8 LE SLAT MALFUNCTIONED A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA258881Z 770 21578 ATL-MDW - FLT 79 - ON CLIMB-OUT, NR 8 LEADING EDGE SLAT SHOWS INTRANSIT WHEN FLAP ARE RAISED. AIRCRAFT RETURNED TO ATL. REMOVED AND REPLACED NR 8 LEADING EDGE SLAT ACTUATOR AS PER MM 27-31-32. OPS CHECK OK. (M) 2L73 4F A3WE 19950707004451995070700445WP 1995 7 7 IXXA199562 119950612A3231 UPLOCK ASSY DOUG DC8 DC862 3021970WP MLG DOORS LACK OF LUBE A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2361CX 46142 ON DEPARTURE OUT OF RJTY, THE UPLATCH CHECK WAS ACCOMPLISHED AND BOTH THE GEAR DOOR AND GEAR WARNING LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO RJTY FOR MAINTENANCE. MAINTENANCE JACKED THE AIRCRAFT, CLEANED AND LUBRICATED BOTH THE LANDING GEAR AND THE GEAR DOOR UPLATCHES. THE GEAR DOOR LATCHES WERE ADJUSTED PER THE DC-8 MM. THE LANDING GEAR WAS OPERATIONALLY CHECKED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19950707004461995070700446NE 1995 7 7 PAYA95A4028 219950620A73145006488B FUEL PUMP AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 2 ENGINE FAILED A PAYAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 EA174205G7987 77 120481 FLT NR 7754 - ORF-JFK - ON APPROACH NR 2 ENGINE FLAMED OUT. REMOVED AND REPLACED FUEL PUMP. (M) 2H72 4T4 TRTA53EU E20NE 19950707004471995070700447NE 1995 7 7 PLGA522951J 219950704A7250 RIVETS 6053T90G01 SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE STAGE 4 DISK BROKEN A PLGAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 NE05344BE16175826 067185 340A104 367355 A SEIZED POWER TURBINE MODULE DURING START WAS REPORTED. THE UNIT WAS REMOVED AND DIRECTED TO AN OVERHAUL FACILITY WHERE, UPON DISASSEMBLY THE DISCREPANCY WAS CONFIRMED AS CAUSED BY TWO BROKEN RIVET HEADS. ON WAS JAMMED BETWEEN THE NOZZLE AND STAGE 4 DISK. (M) 2L72 4T4 TRTA52EU E8NE 19950707004481995070700448NE 1995 7 7 PLGA613951J 219950613A72406064T10P01 COOLING PLATE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE HOT SECTION CRACKED A APLGAK NONE O OTHER ININSP/MAINT 1 NE05364BE7446 340B294 785426 THE ABOVE REFERENCED ENGINE WAS REMOVED FOR HOT SECTION DISTRESS. IN AN EFFORT TO LOCALLY REPAIR, THE HOT SECTION MODULE WAS REMOVED AND DURING DISASSEMBLY THE STG 2 FORWARD COOLING PLATE WAS FOUND WITH A CRACK RADIALLY THROUGH ID OUT TO THE OD. ADDITIONALLY, A CRACK WAS MIGRATING CIRCUMFERENTIALLY ON THE INNER DIAMETER AFT OF THE FORWARD LABRYNTH SEAL. (M) 2L72 4T4 TRTA52EU E8NE 19950707004491995070700449NE 1995 7 7 PLGA6159516 219950615A7260 CHIP LIGHT SAAB SF340 SF340A 7850100EU GE CT7TP CT75A 30030NE LT ENGINE ILLUMINATED A PLGAO OTHER N FALSE WARNING CRCRUISE 1 NE05742BA 340A092 FLT NR 4416 - BOS-BGR - WHILE EN ROUTE THE LEFT ENGINE CHIP LIGHT ILLUMINATED. THE CREW PERFORMED ABNORMAL CHECKLIST PROCEDURES AND CONTINUED TO BGR LANDING WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE TROUBLESHOOTING PER TROUBLE NR 16 OF THE GE MAINTENANCE MANUAL. CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 19950707004501995070700450NE 1995 7 7 PLGA61953 319950601A6114660714200 PROP HUB SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE PROP ASSY CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05359BE105594470 340B285 DRG189689 PROPELLER ASSEMBLY WAS REMOVED FROM THE AIRCRAFT TO COMPLY WITH AD93-19-01. DURING EDDY CURRENT INSPECTION A CRACK WAS FOUND IN THE DOWEL HOLE BETWEEN THE NR 1 AND NR 2 BLADE STATIONS. THE PROPELLER ASSEMBLY WAS DISASSEMBLED AND HUB ASSEMBLY P/N 660714200, WAS SHIPPED TO DOWTY AEROSPACE STERLING FOR FURTHER INVESTIGATION. (M) 2L72 4T RTA52EU 6 CP61GL 19950707004511995070700451NE 1995 7 7 PLGA66951 219950606A72506044T92P03 COOLING PLATE GE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ENGINE FRACTURED A APLGAE ENGINE SHUTDOWN M OVER TEMP CLCLIMB 1 NE05366BE6397 340B303 785453 DURING DEPARTURE CLIMB-OUT OF FLT NR 4380, PIT-JFK, PILOT WAS PERFORMING A CTOT DIAL DOWN AND ENGINE FAILED, ITT CLIMBED TO 1000 DEGREES PRIOR TO INFLIGHT SHUTDOWN. SUBSEQUENT BORESCOPE INSPECTION OF THE REMOVED ENGINE REVEALED A FAILED STG 1 TURBINE COOLING PLATE. SUBMITTER STATES THIS IS THE 4TH COOLING PLATE FAILURE EXPERIENCED BY THIS OPERATOR IN THE PAST 12 MONTHS. (M) 2L72 4T4 TRTA52EU E8NE 19950707004521995070700452EU 1995 7 7 RAIA950613 119950611A33500L60424P EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 12015 176 STL - AFT CABIN EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT SEAT IS INOP. MAINTENANCE REPLACED AFT CABIN EMERGENCY EXIT SIGN LIGHT BULB. (M) 2H72 4T RTA53EU 19950707004531995070700453WP 1995 7 7 RAIA950614 219950613A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE LEAKING A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03864AE6773 864 66126 FAT - FLT NR 4752 - RT ENGINE COULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED RT ENGINE BLEED AIR GASKETS. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T4 TRTA56EU E4WE 19950707004541995070700454EU 1995 7 7 RAIA950615 119950614A771294959411 TTL BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03864AE9063 864 SAN - FLT 4747 - RT ENGINE COULD NOT MAKE TARGET TORQUE. MAINTENANCE DEFERRED RT TORQUE TEMP LIMITER AS PER MEL. (M) 2L72 4T RTA56EU 19950707004551995070700455SO 1995 7 7 RAIA950616 119950613A540012026820001 LATCH EMB 120 EMB120RT SO LT ENGINE UNLATCHED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03124AM19069 120016 STL - FLT 7460 - LEFT ENGINE INBOARD FORWARD COWL LATCH NOT SECURED. CREW LANDED IN PAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE COWL NO DEFECTS WERE NOTED. MAINTENANCE SECURED LATCH. LATCH REINSPECTED NEXT STATION FOR SECURITY, CHECK OK. (M) 2L72 4T RTA31SO 19950707004561995070700456NE 1995 7 7 SIMA951581 219950607A75321004821 BLEED VALVE 311671503 AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENG FAILED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21438AT2462 176 438 127135 MAF - FLT 3838 - AIRCRAFT ABORTED TAKEOFF FOR NR 1 ENGINE EXCEEDING ITT LIMITS AT TAKEOFF TORQUE. AIRCRAFT WAS INSPECTED FOR MTX FERRY TO DFW. THE INTERCOMPRESSOR BLEED VALVE WAS REPLACED WITH A SATISFACTORY GROUND RUN. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19950707004571995070700457EU 1995 7 7 SIMA951582 119950607A324650092361 WHEEL ASSY 5010488 SAAB SF340 340B 7860101EU NR 2 MLG BROKEN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21329AE2709 JUL920711 340B329 DFW - WHEEL ASSEMBLY P/N 5010488, S/N JUL920711, WAS REMOVED FROM AIRCRAFT IN DFW AND SENT TO WHEEL SHOP. THE WHEEL ASSEMBLY HAS A 10 INCH SECTION OF INNER FLANGE BROKEN OFF OF WHEEL INNER ASSY. THE INNER WHEEL ASSEMBLY HAS BEEN REMOVED FROM SERVICE. 2L72 4T RTA52EU 19950707004581995070700458EU 1995 7 7 SIMA951631 119950612A77127239060502 CTOT PANEL SAAB SF340 SF340A 7850100EU NR 1 ENGINE MALFUNCTIONED A SIMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW21112AE 0091 340A112 LAW - FLT 3804 - ON TAKEOFF, POWER WAS MANUALLY SET AT APPROXIMATELY 85 PERCENT WHEN CTOT WAS ENGAGED FOR A MAX POWER TAKEOFF LEFT TQ 120 PLUS DEGREES, ABORTED TAKEOFF, RETURNED TO GATE. TORQUE NOT EXCEEDED 12 SEC TRANS IAW GE MM 72-00-00. REMOVED AND INSPECTED CTOT PANEL IAW 76-10-30. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950707004591995070700459EU 1995 7 7 UF6A950605 119950613A612330048000014 CONTROL UNIT BAG ATP ATP EU NR 2 ENG FAILED A UF6AD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 CE03855AW6989 2029 FLT NR 5108 - SBN - AUTO FEATHER SYSTEM WILL NOT TEST. MAINTENANCE REPLACED NR 2 ENGINE AUTO FEATHER CONTROL UNIT. (M) 2L72 4T RTA27NM 19950707004601995070700460SO 1995 7 7 WTAA950201 119950528A3260922AA2YA6PZ722 PROXIMITY SENSOR EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17286UE 120175 FAT - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LEFT GEAR 'A' SYSTEM UP PROXIMITY SENSOR INTERMITTENT. SWAPPED 'A' AND 'B' SYSTEM PROXIMTIY SENSOR CANNON PLUGS (LEFT GEAR UP SENSORS) PER SNL 120-032-0015. PERFORMED GEAR RETRACTION CHECK. SYSTEM OPERATIONAL CHECK NORMAL. DEFERRED 'B' GEAR POSITION INDICATION SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENACNE SUBSEQUENTLY CLEARED DMI WITH THE REPLACEMENT OF THE LEFT GEAR 'B' SYSTEM UP PROXIMTIY SENSOR. (M) 2L72 4T RTA31SO 19950707004611995070700461SO 1995 7 7 WTAA950202 119950530A32502050000002 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING FAILED A AWTAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP17276UE 120067 SFO - TILLER STEERING MADE UNCOMMANDED RIGHT TURN DURING TAXI. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REPLACED STEERING FEEDBACK POTENTIOMETER. TILLER STEERING OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004621995070700462NE 1995 7 7 95ZZZM206 219950519A73217436025 FUEL CONTROL BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 2 ENG MALFUNCTIONED A AIXKAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA258880Z 61665 21453 MCO-ATL - FLT NR 22 - DURING CLIMB-OUT, NR 2 ENGINE N1 ACCELERATED TOWARD RED LINE, THROTTLE RETARDED AND N1 STABILIZED AT 80 PERCENT. NO RESPONSE TO THROTTLE MOVEMENT. ENGINE SHUTDOWN NORMAL AFTER AIR RETURN TO MCO. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL FOR NR 2 ENGINE PER MM 73-21-2 AND MM 73-11-1, OPS CHECK OK. 2L73 4F4 F A3WE E2EA 19950707004631995070700463NE 1995 7 7 95ZZZM207 219950608A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 2 FAILED A AVJ6ACEF ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. AT FLAME/FIRE ENGINE CASE PENETRATION TOTAKEOFF 1 SO11908VJ 47321 666966 NR 2 ENGINE FAILED CREATING A FIRE THAT DESTROYED AIRCRAFT. MOVED AIRCRAFT FROM RUNWAY TO EAL HANGAR AREA FOR FURTHER INVESTIGATION INTO THE CAUSE OF ENGINE FAILURE. 7TH STAGE DISK DISINTEGRATED. 2L72 4F4 F A6WE E2EA 19950707004641995070700464NM 1995 7 7 95ZZZM208 119950620A2611302842 SMOKE DETECTOR BOEING727 727222 1384073NM CABIN MALFUNCTIONED A RYNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE077635U 19908 CABIN SMOKE DETECTOR WARNING LIGHT ILLUMINATED INFLIGHT. MADE ATB BACK INTO BRADLEY, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OFF LOADED AIRCRAFT, INSPECTED ALL CONTAINERS AND CARGO PITS FOR SMOKE. FOUND NO EVIDENCE OF SMOKE OR FIRE. TESTED ALL CABIN SMOKE DETECTORS. OPS CHECKED NORMAL. 2L73 4F A3WE 19950707004651995070700465CE 1995 7 7 95ZZZM209 119950609A5210 SEAL BEECH 1900 1900C 1154161CE AIRSTAIR DOOR OUT OF POSITION A MASAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW0190YV UC90 EN ROUTE TO UTICA, NY, AIRCRAFT WAS 17,000 FEET WHEN DOOR SEAL STARTED LEAKING (APPROX 2000 TO 3000 FEET CABIN ASCENT). AIRCRAFT DESENDED TO 10,000 FEET AND WAS ABLE TO MAINTAIN A 3000 FT CABIN ALTITUDE. AFTER LANDING, INSPECTION SHOWED DOOR SEAL WAS DISLODGED AT UPPER RT CORNER. DOOR SEAL WAS RESECURED AND AIRCRAFT WAS RETURNED TO SERVICE. DID NOT REQUIRE EMERGENCY ACTION. 2L72 4T RTA24CE 19950707004661995070700466CE 1995 7 7 95ZZZM210 119950609A32601003810061 DNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG FAILED A MASAK NONE P NO WARNING INDICATION APAPPROACH 1 SW01158YV UC158 DURING APPROACH INTO CLARKSBURG, WV, PILOT SELECTED LANDING GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE DOWNLOCK SWITCH AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950707004671995070700467WP 1995 7 7 95ZZZM211 119950606A5244 DOOR DOUG DC9 DC932 3022066WP ACCESSORY COMPT NOT CLOSED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11915VV 47443 FLT NR 537 - EN ROUTE TO TPA - AFTER TAKEOFF THE FORWARD ACCESSORY COMPARTMENT DOOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ATL. RESET FORWARD ACCESSORY COMPARTMENT DOOR. 2L72 4F A6WE 19950707004681995070700468SO 1995 7 7 C2XA95CL094 119950613A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091271529081 252 120125 FLT NR 3216 - CLE-CLE - AFTER TAKEOFF LEFT MAIN GEAR REMAINED DOWN AFTER GEAR WAS SELECTED UP. RED 'A' AND'B' LIGHTS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR IAW EMB MM 32-32-10. OPS CHECK GOOD IAW 32-30-00. AIRCRAFT WAS SENT ON TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004691995070700469SO 1995 7 7 C2XA95CL096 119950617A27513069001005 ANNUNCIATOR PNL EMB 120 EMB120RT SO COCKPIT FAILED A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW09167295420 120185 FLT NR 3263 - CLE-CVG - AFTER TAKEOFF FLAPS SELECTOR TO OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED ANNUNCIATOR UNIT IAW EMB MM 27-50-05. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950707004701995070700470SO 1995 7 7 C2XA95CL097 119950617A275012042642504 SELECTOR HANDLE EMB 120 EMB120RT SO TE FLAPS FAILED A AC2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916729 120185 FLT NR 3263 - CLE-CVG - AFTER TAKEOFF, FLAPS SELECTOR TO 0. OUTBOARD FLAPS STAYED AT 15. DISAGREEMENT LIGHT CAME ON. RETURNED TO CLE. MAINTENACNE REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW EMB 120 MM 27-50-01. AIRCRAFT WAS TEST FLOWN. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004711995070700471SO 1995 7 7 C2XA95CL098 119950618A3260922AA2YA6P2722 PROX SENSOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A C2XAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW0915721 120160 FLT NR 3253 - GSO-CLE - RIGHT LANDING GEAR RED 'A' LIGHT ON, GREEN 'A' LIGHT OFF. MAINTENANCE INSPECTED AND ADJUSTED RIGHT LANDING GEAR DOWNLOCK PROXIMITY SENSOR IAW EMB MM 32-61-1. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004721995070700472NE 1995 7 7 C2XA95CL099 219950619A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE RT FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW092581113280 094 120560 FLT NR 3456 - EWR-EWR - ON CLIMB-OUT HAD TO ADJUST RIGHT POWER LEVER TO KEEP FROM EXCEEDING 816C ITT. FERRIED AIRCRAFT TO BTV. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW TASK CARD 72-00-00. ALL OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19950707004731995070700473NM 1995 7 7 EIAA9504 119950501A3231 RETRACT MECH BOEING747 747132 1384882NM RT MLG DOOR MALFUNCTIONED A EIAAO OTHER J WARNING INDICATION CLCLIMB 1 NM09479EV 19898 SEA - AFTER GEAR RETRACTION AND GEAR HANDLE PLACED TO 'OFF' POSITION, RT BODY GEAR DOOR WOULD NOT STAY IN 'UP' POSITION CONFIRMED BODY IN PRIMARY AND ALTERNATE OF F/E'S ANNUNCIATOR PANEL. WITH HANDLE IN 'UP' POSITION DOOR OPERATES NORMAL. RESET MANUAL GEAR DOOR HANDLE. TEST SYSTEM PER MM 32-33-08, PROCEDURE NR 7. FOUND SYSTEM TO CHECK GOOD. (M) 2L74 4F A20WE 19950707004741995070700474WP 1995 7 7 EIAA9507 119950208A3260 CONNECTOR DOUG DC9 DC933F 302207AWP LT MLG LOOSE A EIAAO OTHER P NO WARNING INDICATION APAPPROACH 1 NM09933F 47191 DEN - ON LANDING GEAR EXTENSION LEFT MAIN LANDING RED LIGHT AND GEAR DOWN GREEN LIGHT WOULD NOT ILLUMINATE. AFTER NORMAL LANDING, THE RED LIGHT AND GEAR DOWN GREEN LIGHT STILL WOULD NOT ILLUMINATE. REPLACED PIN'S AT CONNECTOR P1-132 AT LEFT MAIN DOWNLOCK SWITCH. OPS CHECK GOOD. (M) 2L72 4F A6WE 19950707004751995070700475NE 1995 7 7 EIAA9509 219950403A7230 COMPRESSOR BOEING747 747131 1384881NM PWA JT9 JT9D7F 52054NE NR 1 ENG STALLED A AEIAAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 NM09472EV 20320 662389 NR 1 ENG COMPRESSOR STALLS DURING INITIAL DESCENT, DOES NOT RESPOND TO THROTTLE MOVEMENT. ENG SHUTDOWN. EGT AROUND 810 DEGREES WITH THROTTLE AT IDLE. ATTEMPTED ENG START ABOVE FL 200 STALL DID NOT CLEAR. BELOW FL 200 ENG STARTED. ALL PARAMETERS WERE NORM. INSPECTED INLET, EXHAUST AND 3.5 BLEEDS FOR METAL PARTICLES NOTHING ABNORM NOTED. PERFORMED PWR RUN PER MM 71-00-00, CHECKING HI-STAGE, TANDEM BLEED AND AIR GROUND LOGIC BLEED OPERATION. ALL NORM. PERFORMED EVC TRACK CHKS AND PT2 LEAK CHK AND FOUND OK. CHK'D EVC UNISON RING, PT3 AND PS3 SENSE LINE FOR SECURITY AND FOUND OK. REPLACED EVC PH FILTER AND PRBC VALVE AS PRECAUTIONARY. PERFORMED PWR RUN PER 71-00-00, ENG T/S, ENG OPERATION WAS NORM. (M) 2L74 4F4 F A20WE E20EA 19950707004761995070700476NE 1995 7 7 EIAA9510 219950311A7200 ENGINE BOEING747 747131 1384881NM PWA JT9 JT9D7F 52054NE WING MALFUNCTIONED A AEIAAO OTHER J WARNING INDICATION DEDESCENT 1 NM09472EV 20320 662389 DURING DESCENT ENG 'ROLLED BACK' AND STAGNATED. FUEL FLOW WAS NORM, HIGH EGT, LOW N1 AND N2 WITH NO RESPONSE WITH THROTTLE. INFLIGHT SHUTDOWN CHECKLIST AND INFLIGHT START CHECKLIST WITH ENG OPERATING NORM. (EGT 805 DEGREES, EPR .80, N1 24 PERCENT, N2 48 PERCENT) EGT WITHIN OPERATING LIMITS. CARRIED OUT WINDMILL INSPECT PER MM 72-00-00, PG 682R. ALL CHKS FOUND SATISFACTORY. ACCOMPLISHED IDLE RUN. ALL PARAMETERS NORM. EPR 1.015, N1 25 PERCENT, EGT 419, FF 1.5, N2 62 PERCENT CARRIED OUT BLEED SHIFT CHK. FOUND SATISFACTORY, TANDEM BLEED CLOSED AT 1.22 EPR, THRUSTS LEVER RESPONSE NORM. ALL BLEED SHIFTS NORM. VISUALLY INSP ALL BLEED PORTS, INLET AND EXHAUST. FOUND SATISFACTORY. ENG OPERATED NORM. (M) 2L74 4F4 F A20WE E20EA 19950707004771995070700477NE 1995 7 7 EIAA9511 219950403A7230 COMPRESSOR BOEING747 747131 1384881NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE STALLED A AEIAAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 NM09472EV 20320 662389 NR 1 ENG COMPRESSOR STALLS DURING INITIAL DESCENT, DOES NOT RESPOND TO THROTTLE MOVEMENT. ENG SHUTDOWN, EGT AROUND 810 DEGREES WITH THROTTLE AT IDLE. ATTEMPTED ENG START ABOVE FL 200 STALL DID NOT CLEAR. BELOW FL 200 ENG STARTED. ALL PARAMETERS WERE NORM. INSPECT INLET, EXHAUST AND 3.5 BLEEDS FOR METAL PARTICLES NOTHING ABNORM NOTED. PERFORMED PWR RUN PER MM 71-00-00, CHECKING HI-STAGE, TANDEM BLEED AND AIR GROUND LOGIC BLEED OPERATION, ALL NORMAL. PERFORMED EVC TRACK CHECKS AND PT2 LK CHK AND FOUND OK. CHECKED EVC UNISON RING, PT3 AND PS3 SENSE LINE FOR SECURITY AND FOUND OK. REPLACED EVC PH FILTER AND PRBC VALVE AS PRECAUTIONARY. PERFORMED PWR RUN PER 71-00-00, ENG T/S. ENG OPERATION NORMAL. M 2L74 4F4 F A20WE E20EA 19950707004781995070700478NE 1995 7 7 EIAA9512 219950404A7230 COMPRESSOR BOEING747 747131 1384881NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE STALLED A AEIAAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 NM09472EV 20320 662389 JFK - ON DESCENT NR 1 ENGINE COMPRESSOR STALLED, FLT LEVEL 390 STALL OCCURRED IN CONJUNCTION WITH HIGH STAGE VALVE OPENING. MAXIMUM TEMPERATURE 500 DEGREES. ENGINE SHUTDOWN AND RESTARTED. 2L74 4F4 F A20WE E20EA 19950707004791995070700479WP 1995 7 7 EIAA9513 119950406A5730 SKIN DOUG DC9 DC933F 302207AWP WS 250 BIRDSTRIKE A EIAAO OTHER C F.O.D. APAPPROACH 1 NM09944F 47194 ON APPROACH TO DEN, BIRD STRIKE OCCURRED ON LEFT WING. THE BIRD IMPACTED THE NR 2 SLAT AND THE FIXED LEADING EDGE AT WING STATION XFS EQUALS 250. SLAT WAS DAMAGED AND THE WING LEADING EDGE WAS DENTED JUST FORWARD OF THE ROUND ACCESS PANEL. (M) 2L72 4F A6WE 19950707004801995070700480NE 1995 7 7 IXKA9500021 219950519A7314378200 FUEL PUMP BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 2 ENG MALFUNCTIONED A IXKAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA258880Z 767M 21453 MCO-ATL - FLT NR 22 - DURING CLIMB-OUT, NR 2 ENGINE N1 ACCELERATED TOWARD RED LINE, THROTTLE RETARDED AND N1 STABILIZED AT 80 PERCENT. NO RESPONSE TO THROTTLE MOVEMENT. ENGINE SHUTDOWN NORMAL AFTER AIR RETURN TO MCO. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL FOR NR 2 ENGINE PER MM 73-21-2 AND MM 73-11-1, OPS CHECK OK. 2L73 4F4 F A3WE E2EA 19950707004811995070700481CE 1995 7 7 PLGA63951 119950603A7722 ITT INDICATOR BEECH 1900 1900C 1154161CE RIGHT MALFUNCTIONED A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE0515553 UC128 AFTER TAKEOFF OF FLIGHT NR 4354, THE CREW NOTICED THE RIGHT HAND ITT INDICATOR WAS READING VERY HIGH. AIRCRAFT RETURNED TO ALB MAINTENANCE WHICH FOUND THE ITT INDICATOR OUT OF CAL. MAINTENANCE RECALIBRATED INDICATOR. OPERATIONS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19950707004821995070700482CE 1995 7 7 PLGA64951 119950604A54001149800221 KEEL WEB BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05807BE UB44 DURING PERFORMANCE OF A NR 1 DETAIL WING INSPECTION THE LEFT NACELLE OUTBOARD KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE A CRACK APPROXIMATELY 3 INCHES IN LENGTH. THE CRACK WAS ON THE FORWARD FLANGE THAT RIVETS TO THE ENGINE BAY AFT FIREWALL, ON THE LOWER SIDE OF THE KEEL FLANGE, ADJACENT TO THE THREE ATTACHING HI-LOCK FASTENERS. THE KEEL WAS TEMPORARILY REPAIRED USING APPROVED DATA AND WILL BE REPLACED WHEN PARTS BECOME AVAILABLE. (M) 2L72 4T RTA24CE 19950707004831995070700483EU 1995 7 7 SIMA951651 119950614A33503011210 EEL ASSY AEROSPATR72 ATR72212 EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT3287 263 RFD - FLT NR 4254 - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE PASSENGER ENTRANCE STAIRS EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY, AND PERFORMED OPERATIONAL CHECK, IAW JIC 335000. SYSTEM CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004841995070700484EU 1995 7 7 SIMA951652 119950614A3240215492 BRAKE AEROSPATR42 ATR42300 8680920EU LT MLG FAILED A SIMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW21243AT1619 0127 0243 ORD - FLT 4076 - CAPTAIN NOTICED LEFT MAIN FELT SPONGY AND STOPPED AIRCRAFT. MAINTENANCE INSPECTED LEFT MAIN AND DECIDED TO TAXI AIRCRAFT BACK TO GATE. SPARKS STARTED COMING FROM NR 1 BRAKE, AIRCRAFT WAS PARKED OUT AT PENALTY BOX. CHANGED NR 1 BRAKE. NO FURTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004851995070700485EU 1995 7 7 SIMA951671 119950616A33503011206 EEL ASSY AEROSPATR72 ATR72212 EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT6751 494 263 ORD - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSY IAW JIC 335120. PERFORMED OPERATIONAL CHECK IAW JIC 335000. SYSTEM CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004861995070700486EU 1995 7 7 SIMA951672 119950616A2150 LT PACK AEROSPATR72 ATR72212 EU CABIN ODOR A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21355AT 355 DFW - FLT 3829 - AIRCRAFT RETURNED TO GATE WITH LOUD SQUEAL AND ELECTRICAL SMELL FROM LEFT PACK. INSPECTION REVEALED NO EVIDENCE OF SMOKE. MAINTENANCE TIGHTENED THE CLAMPS ON THE PACK VALVE. GROUND RUN REVEALED NO FAULTS. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004871995070700487NE 1995 7 7 SIMA951673 219950616A73218108001002 EEL AEROSPATR72 ATR72212 EU PWA 120 PW120 NE NR 1 ENGINE MALFUNCTIONED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21369AT 124 C94030023 369 127053 DFW - FLT 3831 - NR 1 ENGINE LOST TORQUE ON TAKEOFF ROLL DOWN TO 50 PERCENT. REMOVED AND REPLACED NR 1 EEC, PERFORMED GROUND RUNS. AIRCRAFT RELEASED FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19950707004881995070700488EU 1995 7 7 SIMA951691 119950618A36105595C970 DUCT AEROSPATR72 ATR72212 EU RT ACM LOOSE A SIMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SW21417AT 417 ORD - FLT NR 4152 - DURING TAXI NR 2 BLEED LEAK WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RECONNECTED BLOWN DUCTING AT AIR CYCLE MACHINE INLET. (M) 2H72 4T RTA53EU 19950707004891995070700489EU 1995 7 7 SIMA951692 119950618A6120311809101 PROP CONTL UNIT AEROSPATR72 ATR72212 EU NR 2 ENGINE MALFUNCTIONED A SIMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SW21369AT MM1169 369 DFW - FLT 3835 - NR 2 ENGINE ONLY ACHIEVED 70 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. CHANGED FEATHERING CONTROL UNIT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004901995070700490EU 1995 7 7 SIMA951701 119950619A2910NTA152506 PACKING AEROSPATR42 ATR42300 8680920EU DUAL BRAKE VALVEFAILED A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW21235RM 235 EVV - FLT 4106 - GREEN HYDRAULIC SYSTEM LOW LEVEL ILLUMINATED IN BOUND TO EVV. CREW COMPLETED CHECK LIST IN QRH AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FAILED O-RING ON PRESS LINE TO DUAL POWER BRAKE VALVE. REMOVED AND INSPECTED O-RING AND FITTING. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004911995070700491 1995 7 7 SIMA951702 319950619A61403039242 NP SENSOR AEROSPATR42 ATR42300 8680920EU NR 2 ENGINE FAILED A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21243AT CH10177 0243 NR 2 ENGINE NP 100 PERCENT TO 60 PERCENT DURING TAKEOFF. AIRCRAFT RETURNED TO ORD. MAINTENANCE REPLACED THE NP SENSOR. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950707004921995070700492 1995 7 7 WTAA950207 419950611A61221680640 MONOPOLE BAG JETSTMJETSTM3101 1500215EU RT ENGINE FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17403UE 743 CIC - RIGHT ENGINE POWER SURGE WITH TORQUE AND EGT FLUCTUATION REPORTED DURING CLIMB WITH SRL ON. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. ACCOMPLISHED ENGINE GROUND RUN. CONFIRMED RT SRL SYSTEM FAILURE. DEFERRED RIGHT SRL PER MEL 76-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CORRECTED THE SRL SYSTEM DEFERRAL WITH THE REPLACEMENT OF THE RIGHT ENGINE PROPELLER GOVERNOR MONOPOLE. (M) 2L72 4T RTA21EU 19950707004931995070700493EU 1995 7 7 WTAA950209 119950610A771231024575 TORQUE RING BAG JETSTMJETSTM3101 1500215EU LT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17428UE 806 FAT - LEFT ENGINE TORQUE FLUCTUATION REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. ENGINE GROUND RUN-UP ACCOMPLISHED AFTER ABORTED TAKEOFF. UNABLE TO DUPLICATE DISCREPANCY. SUBSEQUENT TAKEOFF ATTEMPT ABORTED WITHOUT INCIDENT DUE TO SAME DISCREPANCY. MAINTENANCE SWAPPED LEFT TORQUE INDICATION FROM BRIDGE '1' TO BRIDGE '2'. PERFORMED ENGINE GROUND RUN. LEFT ENGINE TORQUE INDICATION NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950707004941995070700494EU 1995 7 7 WTAA950211 119950613A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NOSE GEAR FAILED A WTAAO OTHER N FALSE WARNING DEDESCENT 1 WP17431UE 813 FAT - NOSE GEAR 'GREEN' GEAR DOWN POSITION INDICATOR ILLUMINATED WITH GEAR IN THE RETRACTED POSITION ON DESCENT. BOTH NOSE GEAR 'RED' INTRANSIT LIGHT AND 'GREEN' GEAR DOWN LIGHT REMAINED ILLUMINATED FOLLOWING GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR DOWNLOCK MICROSWITCH. GEAR POSITION INDICATIONS NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950707004951995070700495 1995 7 7 WTAA950212 219950617A732189737519 FUEL CONTL UNIT BAG JETSTMJETSTM3101 1500215EU RT ENG FAILED A AWTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17431UE 813 LAX - RIGHT ENGINE LOSS OF POWER REPORTED AFTER DEPARTURE. RIGHT ENGINE TORQUE INDICATION DROPPED TO 60 PERCENT AND FLUCTUATED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950707004961995070700496SO 1995 7 7 WTAA950213 119950531A3250MS250851 SWITCH EMB 120 EMB120RT SO NLG STEERING CORRODED A WTAAO OTHER O OTHER TXTAXI/GRND HDL 1 WP17455UE 120163 SFO - NOSEWHEEL TILLER STEERING UNRESPONSIVE TO INPUT. PEDAL STEERING OPERATION NORMAL. MAINTENANCE CLEANED CORROSION FROM TILLER STEERING ENABLE MICROSWITCH. TILLER STEERING OPERATIONAL CHECK NORMAL DURING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004971995070700497SO 1995 7 7 WTAA950214 119950531A3250MS3476L106S CONNECTOR EMB 120 EMB120RT SO NLG STEERING CORRODED A WTAAO OTHER O OTHER TXTAXI/GRND HDL 1 WP17455UE 120163 SFO - NOSEWHEEL TILLER STEERING FAILED DURING PARKING. MAINTENANCE REMOVED CORROSION FROM NOSEWHEEL STEERING FEEDBACK POTENTIOMETER ELECTRICAL CONNECTOR. TILLER STEERING OPERATIONAL CHECK NORMAL DURING TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950707004981995070700498EU 1995 7 7 WTAA950216 119950704A5330 SKIN BAG JETSTMJETSTM3101 1500215EU FUSELAGE BIRD STRIKE A WTAAK NONE C F.O.D. APAPPROACH 1 WP17417UE 794 BFL - BIRD STRIKE REPORTED AT LOWER LEFT SIDE OF FUSELAGE DURING APPROACH TO LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950707004991995070700499 1995 7 7 95ZZZM212 419950501A61225U1881 GOVERNOR DOUG DC6 DC6 3021702WP NR 1 ENG PROP NOT CONTROLLABLEA NACAA UNSCHED LANDING O OTHER CLCLIMB 1 AL0343872 329 533294 FLT NR 32 RETURNED TO BET DUE TO NR 1 ENGINE RPM 2900 ON TAKEOFF AND THE PROPELLER NOT CONTROLLABLE WITH TOGGLE SWITCH OR MASTER LEVER. REPLACED PROP GOVERNOR. 2L74 4R A781 19950707005001995070700500EU 1995 7 7 AWXA9500300 119950519A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28626AW 65 PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT AND RIGHT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED BITE TEST. REMOVED AND REPLACED BATTERY PACKS, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950707005011995070700501EU 1995 7 7 AWXA9500323 119950522A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT AFT EMERGENCY BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950707005021995070700502EU 1995 7 7 AWXA9500325 119950523A3350321452 EEL PWR SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW 091 PHX - DURING ROUTINE MAINTENANCE CHECK, EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED LEFT OVERWING POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950707005031995070700503EU 1995 7 7 AWXA9500334 119950601A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28627AW 66 PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT AFT EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950707005041995070700504NM 1995 7 7 AWXA9500353 119950605A275010613556 FLAP SWITCH BOEING737 73733A 1384673NM AFT BAG PIT FAILED A AAWXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP28174AW 23633 MSP-PHX - FLT NR 883 - ON APPROACH INTO PHX THE FLAPS WOULD NOT EXTEND TO FLAPS 1, ALT FLAPS EXTENDED FLAPS TO 15. AIRCRAFT DID A GO AROUND AND CALLED FOR EMERGENCY EQUIPMENT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED FLAP LOAD CONTROL SWITCH ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950707005051995070700505NM 1995 7 7 AWXA9500364 119950610A3350 EEL WIRE BOEING737 737277 1384570NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28181AW 22648 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 16 AND 17. RESECURED WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950707005061995070700506NM 1995 7 7 AWXA9500365 119950611A3350900835A EEL BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 16 AND ROW 21. REPLACED BATTERY PACK AT ROW 18, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950707005071995070700507NM 1995 7 7 AWXA9500366 119950612A3350900835A EEL BATTERY PACK BOEING737 7372M8 1384483NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950707005081995070700508NM 1995 7 7 CAL950446 119950524A5330 SKIN BOEING727 727227 1384078NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND ACTUATOR ACCESS PANEL AND LOWER FUSELAGE BL 0, BS 720 SKIN CORRODED AT RT RAM AIR SCOOP. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. THE ACCESS PANEL WAS REPLACED WITH A NEW PANEL IAW SRM 51-10-1. (M) 2L73 4F A3WE 19950707005091995070700509NM 1995 7 7 CAL950449 119950524A5730 SKIN BOEING727 727227 1384078NM WS 90 LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09707554570845708 21366 GSO - INSPECTION FOUND RT WING LEADING EDGE CAVITY INTERIOR OF LEADING EDGE SKIN CRACKED AT RIVET HOLES AT STATION 90. THE CRACK WAS .25 INCH LONG. THE CRACK WAS STOP DRILLED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED PER ECRA 5720-01064. (M) 2L73 4F A3WE 19950707005101995070700510NM 1995 7 7 CAL950450 119950524A5321 FLOOR BOEING727 727227 1384078NM BS 1130-1140 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - THE FLOORBOARD SUPPORTS, FLOORBEAM, AND ATTACHING WEB IN AFT GALLEY AREA AT STATION 1130-1140 WERE FOUND CORRODED. THE CORRODED SECTIONS WERE REMOVED IAW ECRA 5310-01508. REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-01508 AND SRM 51-30-2. (M) 2L73 4F A3WE 19950707005111995070700511NM 1995 7 7 CAL950451 119950524A5315 FLOORBEAM BOEING727 727227 1384078NM FS 1110 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND THE FLOORBEAM CORRODED AT FS 1110, RBL 20-RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS CUTOUT IAW ECRA 5310-01102. A SPLICE T-CHORD, FOUR ANGLE SPLICES, AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5310-01102 AND SRM 51-30-2. (M) 2L73 4F A3WE 19950707005121995070700512NM 1995 7 7 CAL950452 119950524A5320 ANGLE BOEING727 727227 1384078NM BS 720 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - A .80 INCH CRACK WAS FOUND IN THE LOWER FUSELAGE INTERCOSTAL SUPPORT ANGLE AT BS 720. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-20-4. (M) 2L73 4F A3WE 19950707005131995070700513NM 1995 7 7 CAL950453 119950524A5313 STRINGER BOEING727 727227 1384078NM BS 570 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND STRINGER 28L CORRODED UNDER FLOOR SUPPORT IN FORWARD PIT AT STATION 570. THE CORRODED AREA OF STRINGER WAS CUT OUT IAW SRM 53-10-3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (M) 2L73 4F A3WE 19950707005141995070700514NM 1995 7 7 CAL950454 119950524A5311 FRAME BOEING727 727227 1384078NM BS 990 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND A 1 INCH CRACK IN FRAME AT UPPER LIP IN AFT CARGO HOLD STATION 990, BETWEEN S27L AND S28L. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-3. (M) 2L73 4F A3WE 19950707005151995070700515NM 1995 7 7 CAL950458 119950524A5730 SKIN BOEING727 727227 1384078NM RT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09707554570845708 21366 GSO - INSPECTION FOUND A .75 INCH CRACK IN RT WING FIXED LEADING EDGE ABOVE CUTOUT FOR NR 6 SLAT OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (M) 2L73 4F A3WE 19950707005161995070700516NM 1995 7 7 CAL950459 119950524A5720 ANGLE BOEING727 727227 1384078NM WS 118 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - A .25 INCH CRACK WAS FOUND IN THE RT WING LEADING EDGE CAVITY AT STATION 118 WEB LOWER ATTACH ANGLE. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (M) 2L73 4F A3WE 19950707005171995070700517NM 1995 7 7 CAL950460 119950524A5710 LE STRUCTURE BOEING727 727227 1384078NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND THE LEFT WING LEADING EDGE CAVITY NR 1 SLAT ACTUATOR INBOARD ATTACH AREA CRACKED AT MOUNT BOLT. THE CRACK WAS .5 INCH LONG. A SUPPORT RIB REPAIR WAS INSTALLED IAW ECRA 557C187. (M) 2L73 4F A3WE 19950707005181995070700518NM 1995 7 7 CAL950461 119950524A5315 FLOORBEAM BRACE BOEING727 727227 1384078NM FORWARD LAV CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND A 1.3 INCH CRACK IN FORWARD LAVATORY FLOORBEAM BRACE. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-21 AND 51-30-2. (M) 2L73 4F A3WE 19950707005191995070700519NM 1995 7 7 CAL950467 119950608A291310605565 HYD PUMP BOEING727 727232 1384082NM NR1/NR2 ENGINES LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0916784 20639 FLT NR 525 - IAH - THE 'B' SYSTEM HYDRAULIC QUANTITY GAUGE INDICATED ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 'B' SYSTEM PUMP LIGHT WHILE IN FLIGHT. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 'B' SYSTEM PUMPS DUE TO LEAKAGE. THE SYSTEM WAS PRESSURIZED AND NO LEAKS WERE FOUND. (M) 2L73 4F A3WE 19950707005201995070700520NE 1995 7 7 PLGA55951 319950704A6110600713285 DE-ICE BOOT SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE BLADE WORN A PLGAK NONE O OTHER ININSP/MAINT 1 NE05364BE 340B294 DRG639187 THE PROP ASSY WAS REMOVED FROM SERVICE DUE TO ALL FOUR BLADE DE-ICE BOOTS DEBONDING. THE CAUSE WAS DETERMINDED TO BE OIL AND GREASE MIGRATING BETWEEN THE INNER AND OUTER SLEEVE AND EXITING UNDER THE BLADE CUFF. AFTER DISASSEMBLY FOR SHIPMENT OIL WAS OBSERVED IN THE HUB AREA. COMPLETE ASSY WAS THEN SHIPPED TO DOWTY AEROSPACE STIERLING FOR REPAIR. THE PROP WAS REPAIRED AND RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 6 CP61GL 19950707005211995070700521 1995 7 7 PLGA68951 419950608A341651928702051 ALTIMETER BEECH 1900 1900C 1154161CE LT COCKPIT FAILED A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE05820BE UB64 BOS - FLT NR 4864 - AFTER TAKEOFF THE CAPTAIN'S ALTIMETER FAILED, THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ALTIMETER AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19950707005221995070700522NE 1995 7 7 PLGA69951 219950609A7200 ENGINE GE SAAB SF340 340B 7860101EU GE CT7TP CT75A 30030NE LEFT FOD A PLGAK NONE C F.O.D. CRCRUISE 1 NE05360BE 785205 340B287 FLT NR 4410 - BOS-BGR - EXPERIENCED FAILURE OF THE LEFT ENGINE. THE AIRCRAFT DIVERTED TO PSM, LANDING WITHOUT INCIDENT. PSM MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. PRELIMINARY INSPECTION APPEARS TO FOD. 2L72 4T4 TRTA52EU E8NE 19950707005231995070700523EU 1995 7 7 PLGA69952 119950609A3040XW21160G1 MOTOR SAAB SF340 SF340A 7850100EU WINDSHIELD WIPERFAILED A PLGAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NE05751BA 340A157 BOS - DURING APPROACH THE CREW NOTED A SMELL OF SMOKE IN THE COCKPIT WHILE OPERATING THE FIRST OFFICERS WINDSHIELD WIPER. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS THEN DISPATCHED TO THE AIRCRAFT. BOS MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD WIPER MOTOR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA52EU 19950707005241995070700524NM 1995 7 7 TAOA069504 119950617A3230TA12C59WH16EP CLAMP BOEING727 727294 1384088NM NLG HARNESS BROKEN A TAOAO OTHER J WARNING INDICATION CLCLIMB 1 EA15921TS 22043 RED GEAR DOORS LIGHT REMAINED ON BY GEAR HANDLE AND NOSE GEAR DOOR LIGHT ON SECOND OFFICERS PANEL STAYED ON AFTER GEAR RETRACTION. FLEW TO BOS AT 230 KTS, LANDED WITH ALL NORMAL INDICATIONS WITH NORMAL GEAR EXTENSION. NOSE WHEEL STEERING NORMAL ON WITH TAXI IN. FOUND NOSE GEAR CONDUIT CLAMP BROKEN LETTING CONDUIT HANG BETWEEN DOORS. REPLACED CLAMP AND RETRACTED GEAR SEVERAL TIMES, CHECKED OK PER MM 32-33-0. (M) 0 4 A3WE 19950707005251995070700525NM 1995 7 7 TWRA9534 119950614A575365B134301 FITTING BOEING747 747212B 1384886NM TE FLAPS SHEARED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15616FF 21939 DURING A SCHEDULED B-2 SERVICE, FOUND A SHEARED CROSSTIE FITTING ON NR 3 FLAP TRACK CARRIAGE. REMOVED AND REPLACED CROSSTIE FITTING, OPS CHECK OK. (M) 2L74 4F A20WE 19950707005261995070700526EU 1995 7 7 VTZA95195 119950618A21302758A000 SWITCH BAG JETSTMJETSTM3201 1500217EU LT ACM FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27470UE 814 FLT NR 6343 - IAD-SYR - DURING CRUISE, RETURNED TO IAD DUE TO THE LEFT AIR OFF LIGHT ILLUMINATING. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT AIR OFF SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950707005271995070700527WP 1995 7 7 VTZA95196 219950616A732189737527 FUEL CONTL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILURE A AVTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27478UE 892 P66059 FLT NR 6543 - IAD-ROA - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 60 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950707005281995070700528 1995 7 7 VTZA95197 419950615A3418C7771076 LIFT TRANSDUCER BAG JETSTMJETSTM3201 1500217EU LT/RT WINGS FAILURE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27488UE 907 FLT NR 6435 - IAD-EWR - RETURNED TO IAD DUE TO THE STICK SHAKER COMING ON AFTER ROTATION. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED THE LEFT WING TRANSDUCER AND REPLACED AND RECALIBRATED THE RIGHT WING TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950707005291995070700529EU 1995 7 7 VTZA95198 119950616A793141SG107150G14 TRANSDUCER BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27497UE 904 FLT NR 6198 - IAD-PIT - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE OIL PRESSURE DROPPING TO ZERO FOR 15 SECONDS DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE OIL PRESSURE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950707005301995070700530EU 1995 7 7 VTZA95199 119950616A3230ATG135020 SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27302UE 41013 FLT NR 6261 - IAD-EWR - DURING CLIMB-OUT RETURNED TO IAD DUE TO GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT MAIN GEAR WEIGHT ON WHEELS MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950707005311995070700531EU 1995 7 7 VTZA95200 119950617A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGG COMPT DOOR OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27315UE 41033 FLT NR 6595 - RDU-IAD - DURING CLIMB-OUT RETURNED TO RDU DUE TO THE MAIN BAGGAGE DOOR LIGHT ILLUMINATING ON CLIMB-OUT. AIRCRAFT RETURNED TO RDU WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17230 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 17230 ON, BY ADJUSTING THE FORWARD MICROSWITCH ON THE BAGGAGE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950707005321995070700532EU 1995 7 7 VTZA95202 119950610A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE BAY OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27313UE 41026 FLT NR 6450 - CLE-IAD - ABORTED TAKEOFF DUE TO THE MAIN BAGGAGE DOOR WARNING ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 40118 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 40118, BY ADJUSTING THE BAGGAGE DOOR MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950707005331995070700533EU 1995 7 7 VTZA95203 119950614A2750P232A801210 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU TE FLAP DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27318UE 41041 FLT NR 6551 - IAD-CLE - ABORTED TAKEOFF DUE TO CONFIGURATION WARNING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED CONNECTOR ON THE FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950707005341995070700534EU 1995 7 7 VTZA95205 119950619A29131379125H HYD PUMP BAG JETSTMJETSTM3201 1500217EU LT/RT FAILED A VTZAO OTHER K FLUID LOSS APAPPROACH 1 EA27492UE 790 FLT NR 6348 - IAD-GSO - DURING APPROACH TO LANDING DECLARED AN EMERGENCY DUE TO BOTH HYDRAULIC PUMPS FAILING ON THE APPROACH, AND CREW HAD TO PUMP THE LANDING GEAR DOWN. AIRCRAFT LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RT ENGINE HYDRAULIC LINE AND BOTH PUMPS DUE TO CAVITATION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950707005351995070700535EU 1995 7 7 VTZA95206 119950620A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT/RT ENGINES OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27485UE 901 FLT NR 6377 - IAD-CRW - ABORTED TAKEOFF, DUE TO A TORQUE SIGNAL SPLIT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CALIBRATED BOTH TORQUE SIGNAL CONDITIONERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950707005361995070700536EU 1995 7 7 9510363224 119950626A2910201042091 HOSE AIRBUS320 A320211 3930320EU RT MLG WW BROKEN A NWAAO OTHER JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01324US 273 DURING CLIMBOUT FROM SAN, THE GREEN HYDRAULIC SYSTEM INDICATED ZERO AFTER GEAR RETRACTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN LAX WHERE MAINTENANCE FOUND THE RIGHT MLG LOCK STAY ACTUATOR OUTBOARD HOSE, LOWER COLLAR, BROKEN. REPLACED HOSE. OPS AND LEAK CHECKS OK. 2L72 4F RTA28NM 19950707005371995070700537EU 1995 7 7 9510373224 119950626A2910 HYD SYST AIRBUS320 A320211 3930320EU GREEN HYD SYST REQD SERVICE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01324US 273 DURING APPROACH INTO SAN, THE GREEN HYDRAULIC SYSTEM PRESSURE AND QUANTITY DECREASED TO ZERO. ACCOMPLISHED MANUAL EXTENSION OF THE LANDING GEAR. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO LEAKS. SERVICED GREEN HYDRAULIC RESERVOIR AND EXERCISED FLIGHT CONTROLS AND RESERVICED RESERVOIR. OPS AND LEAK CHECKED OK. 2L72 4F RTA28NM 19950707005381995070700538WP 1995 7 7 9510389853 119950630A3610 DUCT DOUG DC9 DC951 3022051WP RT ACM LOOSE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01762NC 47710 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING INITIAL CLIMBOUT. FLIGHT RETURNED TO TPA AND LANDED WITHOUT INCIDENT. REINSTALLED FLEX DUCT AT RIGHT ACM OUTLET. ALSO, TIGHTENED CLAMPS AT LEFT AUGMENTATION VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707005391995070700539WP 1995 7 7 9510399930 119950626A3150DT2RA7 POSITION SWITCH DOUG DC9 DC931 3022065WP STABILIZER BINDING A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL0189S 47042 TAKE-OFF WARNING HORN SOUNDED WITH ALL CONDITIONS MET FOR TAKE-OFF. ABORTED TAKE-OFF AND RETURNED TO GATE. FOUND STABILIZER TAKE-OFF POSITION SWITCH (S1-141) STICKING. CLEANED AND LUBED SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707005401995070700540WP 1995 7 7 9510409978 119950628A30105919526504 ANTI ICE DUCT DOUG DC9 DC931 3022065WP RT WING BINDING A NWAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL019342 47391 ON INITIAL SLAT EXTENSION AT 240 KNOTS, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH BLUE SLAT EXTEND LIGHT OFF. AIRCRAFT ROLLED TO THE LEFT. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING ANTI-ICE 'T' DUCT BINDING. REPLACED 'T' DUCT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950707005411995070700541NM 1995 7 7 9510412712 119950704A5343659864326 TRUNNION BOEING727 7272S7 138407ZNM RT MLG CRACKED A NWAAO OTHER O OTHER LDLANDING 1 GL01712RC455995850 22020 ON LANDING ROLL OUT, AIRCRAFT EXPERIENCED A RIGHT MAIN LANDING GEAR AFT TRUNNION FAILURE. DEPLANED PASSENGERS UTILIZING PORTABLE STAIRS AND TOWED AIRCRAFT OFF RUNWAY. MAINTENANCE FOUND AFT TRUNNION JOURNAL CRACKED AT THE MAIN LANDING GEAR BEAM. ITEM UNDER REPAIR. 2L73 4F A3WE 19950707005421995070700542NM 1995 7 7 95UAL900031 119950705A3350 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29549UA 25397 DOOR 2 RIGHT EMERGENCY EXIT LIGHT INOP. RELAMPED. OP CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950707005431995070700543NM 1995 7 7 95UAL900032 119950705A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29310UA 23671 EEL LIGHTING INOP FROM ROW 17 TO AFT CABIN. REPLACED EEL STRIP. OP CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950707005441995070700544NM 1995 7 7 95UAL900033 119950705A3350 EEL BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29385UA 24660 EEL LIGHTING INOP IN FIRST CLASS. REPLACED BATTERY PACK. OP CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950707005451995070700545NE 1995 7 7 95UAL900034 219950705A7230 COMPRESSOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE ENGINE STALLED A UALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29654UA21856 25392 724626 ABORTED TAKEOFF AT 121 KNOTS DUE TO COMPRESSOR STALL. FOUND EXCESSIVE BLADE TIP CLEARANCE IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. OVERHAULED COMPRESSOR TO THE NEW PRATT BUILD STANDARD. 2L72 4F4 FRTA1NM E24NE 19950707005461995070700546NM 1995 7 7 95UAL900035 119950705A2611 SMOKE DET BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CARGO COMPT MALFUNCTIONED A UALAO OTHER N FALSE WARNING CRCRUISE 1 WP294729U 19926 FORWARD LOWER CARGO FIRE WARNING LIGHT CAME ON DURING FLIGHT. NO EVIDENCE OF FIRE. REPLACED SMOKE DETECTOR. FOUND GROUND WIRE BROKEN AT PC BOARD GOING TO CONNECTOR PIN 5. 2L74 4F4 F A20WE E20EA 19950707005471995070700547 1995 7 7 COM11924 419950628A34256226190204 AHRS EMB 120 EMB120RT SO NR 1 DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01205CA1347286 120205 PILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS. 2L72 4T RTA31SO 19950707005481995070700548SO 1995 7 7 COM11925 119950624A2751 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01152CA 120152 FLAP CONTROL FAULT WARNING. RE-RACKED FLAP CONTROL UNIT. COULD NOT DUPLICATE PROBLEM. 2L72 4T RTA31SO 19950707005491995070700549EU 1995 7 7 COM31111 119950629A32465009237 RACE 5010488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 2967 AUG930541 340A140 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION, FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950707005501995070700550EU 1995 7 7 COM31112 119950703A5520DAS623A41 BEARING SAAB SF340 SF340A 7850100EU RT ELEVATOR WORN A COMAK NONE E VIBRATION/BUFFET CRCRUISE 1 SO01146CA 340A146 VIBRATION FROM AIRCRAFT FUSELAGE AREA. PASSENGERS COMPLAINED OF LOUD NOISE AND VIBRATION IN AIRCRAFT CABIN. REPLACED THE RIGHT ELEVATOR HINGE BEARINGS. 2L72 4T RTA52EU 19950707005511995070700551EU 1995 7 7 COM31113 119950705A36107221100643 DUCT ASSY SAAB SF340 SF340A 7850100EU LEFT CRACKED A COMAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TXTAXI/GRND HDL 1 SO01358CA 340A047 LEFT BLEED LEAK WARNING ACTIVATED. REPLACED CRACKED BLEED AIR DUCT AT LEFT WING ROOT. 2L72 4T RTA52EU 19950707005521995070700552EU 1995 7 7 COM31114 119950703A2730DL3827M157 ACTUATOR SAAB SF340 SF340A 7850100EU LT PITCH TRIM DEFECTIVE A COMAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 SO01343CA4215 53 340A024 BOTH PILOT'S AND COPILOT'S PITCH TRIM CAN BE ACTIVATED WITH ONLY HALF OF THE TRIM SWITCH DEPRESSED. REPLACED THE LT PITCH TRIM ACTUATOR. 2L72 4T RTA52EU 19950707005531995070700553NM 1995 7 7 DL72K952948 119950613A5312 BLKHD WEB BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 SEVERAL CRACKS WERE FOUND IN FS 1183 BULKHEAD WEB AND STIFFENERS AFTER AIRCRAFT FAILED TO PRESSURIZE IN BOS. A 4 INCH LONG L-SHAPED CRACK WAS FOUND IN FS 1183 BLKHD WEB AT LBL 46.9 AND WL 213.67. THE LBL 46.93 VERTICAL STIFFENER HAD MULTIPLE CRACKS WITH MAXIMUM LENGTH OF 8 INCHES BETWEEN WL 205 AND WL 215. THE WL 209 HORIZONTAL STIFFENER WAS FOUND CRACKED AT LBL 46 AND LBL 27, MAXIMUM CRACK LENGTH WAS 3.5 INCHES. THE BLKHD WEB AT LBL 27 AND WL 209 WAS ALSO FOUND WITH A 6 INCH CRACK. REPAIRS WERE ACCOMPLISHED PER DER APPROVED DATA, DL ERA 301908-14. 2L73 4F A3WE 19950707005541995070700554NM 1995 7 7 DL72L952919 119950701A53206517517 ANGLE BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11510DA 21312 DURING LETTER CHECK, A 1 INCH CRACK WAS FOUND IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. REPLACED DAMAGED PART IN ACCORDANCE WITH S/B 727-53-0129, REV. 4. 2L73 4F A3WE 19950707005551995070700555NM 1995 7 7 DL72S952921 119950630A53306572743 SKIN BOEING727 727232 1384082NM FS 600-660 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV, CORROSION DAMAGE TO THE SKIN AND STR 27L WAS FOUND IN SEVERAL LOCATIONS BETWEEN STATIONS 600 AND 660. THE SKIN WAS CRACKED AND CORRODED AT APPROX FS 627 AND STR 27L. THERE WAS AN EXISTING EXTERNAL REPAIR AT APPROX FS 620 AND STR 27L. REPAIRED PER B727 SRM 53-30-3, FIG. 3 (SKIN) AND B727 SRM 53-10-3, FIG. 1 (STRINGER). 2L73 4F A3WE 19950707005561995070700556NE 1995 7 7 DL76L952950 219950701A7250PW4060 HPT BLADE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11173DN13325 24800 724415 DURING BORESCOPE INSPECTION, FOUND AN HPT BLADE MISSING. ENGINE WAS REMOVED AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19950707005571995070700557WP 1995 7 7 DLL10952922 119950629A53301641603 SKIN LKHEED1011 10113851 5265010WP FS 1363 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11725DA 193C1162 DURING LAYOVER, WHILE ACCOMPLISHING REPAIR OF FS 1363 BULKHEAD PER S.I. 7-69959-12, 18 FASTENER HOLES IN RIGHT SIDE AND 30 FASTENER HOLES IN LEFT SIDE OF FUSELAGE SKIN AND E.O. 7-47702-3 MOD DOUBLERS WERE TOOL DAMAGED. THE SUBJECT HOLES WERE OVERSIZED TO ELIMINATE THE DAMAGE. THE UNDERLYING BULKHEAD CAP WAS REPLACED. FAA APPROVAL PER FAA FORM 8110-3 06-29-95. 2L73 4F A23WE 19950707005581995070700558 1995 7 7 MWEA95230 419950705A2565113313DG EVAC SLIDE DOUG DC9 DC932 3022066WP CABIN DOOR LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31501ME 47132 FOUND THE MAIN CABIN EMERGENCY EVAC DOOR SLIDE PRESSURE GAUGE JUST BELOW PRESSURE (IN THE RED). REPLACED THE FWD CABIN DOOR EVACUATION SLIDE. 2L72 4F A6WE 19950707005591995070700559NM 1995 7 7 P5CA9500241 119950629A5320 ANGLES BOEING747 747121 1384871NM BS 1300-1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON LOWER SKIN ANGLES ON INTERCOSTAL BETWEEN BS 1300 AND BS 1350 BETWEEN LBL 16 AND RBL 16 (LEVEL 2). MANUAFACTURED AND INSTALLED REINFORCEMENT ANGLES PER BOEING SRM 53-10-22. 2L74 4F A20WE 19950707005601995070700560NM 1995 7 7 P5CA9500242 119950629A5210 ANGLES BOEING747 747121 1384871NM NR 3L DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED AND BROKEN STRAP ANGLES THAT ATTACH TRIM PANELS NR 3 LEFT ENTRY DOOR. REPLACED ANGLES PER BOEING SRM 52-10-02. 2L74 4F A20WE 19950707005611995070700561NM 1995 7 7 P5CA9500243 119950629A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 1430-1480 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SKIN FITTINGS AND INTERCOSTAL BETWEEN BS 1430 AND BS 1480 BETWEEN LBL 16 AND RBL 16. MANUFACTURED AND INSTALLED REINFORCING BRACKET PER BOEING SRM 53-10-22. 2L74 4F A20WE 19950707005621995070700562NM 1995 7 7 P5CA9500244 119950630A5280 BUSHING BOEING747 747132 1384882NM LT MLG DOOR WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 LEFT MAIN WING LANDING GEAR LOWER DOOR FORWARD HINGE BADLY WORN. REMOVED AND REPLACED BUSHINGS PER BOEING MAINTENANCE MANUAL 32-12-00. 2L74 4F A20WE 19950707005631995070700563NM 1995 7 7 P5CA9500245 119950630A5280MS1410316 BUSHINGS BOEING747 747132 1384882NM RT MLG DOOR WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 RIGHT BODY GEAR OUTBOARD DOOR ACTUATOR UPPER ATTACH BUSHING BADLY WORN. REPLACED BUSHINGS PER OVERHAUL MANUAL 20-50-03. INSTALLED ACTUATOR PER MAINTENACE MANUAL 32-33-27. 2L74 4F A20WE 19950707005641995070700564NM 1995 7 7 P5CA9500246 119950630A7800 RIVETS BOEING747 747132 1384882NM NR 1 ENG EXHAUSTLOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE EXHAUST SLEEVE HAS PULLED THROUGH, LOOSE AND MISSING FASTENERS ON THE TRAILING EDGE FROM 10 O'CLOCK TO 2 O'CLOCK POSTION. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707005651995070700565NM 1995 7 7 P5CA9500247 119950630A5280 RIVETS BOEING747 747132 1384882NM RT MLG DOOR LOOSE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 RIGHT BODY GEAR INBOARD DOOR INNER SKIN LOOSE AT 2 ROWS OF FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707005661995070700566NM 1995 7 7 P5CA9500248 119950630A5230 SEAL LAND BOEING747 747132 1384882NM FWD CARGO DOOR BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 FORWARD CARGO BAY DOOR FORWARD SEAL LAND 10 INCHES AND 30 INCHES UP FROM INBOARD BOTTOM CORNER IS BENT. STRAIGHTENED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950707005671995070700567NM 1995 7 7 P5CA9500249 119950630A5315 FLOOR BEAM BOEING747 747132 1384882NM BS 1780 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 BS 1780 LOWER AFT CARGO FLOOR BEAM CAP IS DAMAGED (TORN) AT LBL 30. REPLACED SECTION OF CAP ANGLE PER BOEING SRM 51-10-01, 51-12-00, AND 51-30-02. 2L74 4F A20WE 19950707005681995070700568NM 1995 7 7 P5CA9500250 119950630A5315 FLOOR BEAM BOEING747 747132 1384882NM BS 1780 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 BS 1780 LBL 30 FLOOR SUPORT WEB IS TORN ABOUT 6 INCHES BELOW FLOOR BEAM AFT CARGO COMPARTMENT. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950707005691995070700569NM 1995 7 7 P5CA9500251 119950630A5315 FLOOR BEAM BOEING747 747132 1384882NM BS 1800 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 BS 1800, RBL 50, FLOOR BEAM CAP ANGLE IS CRACKED ON FORWARD SIDE OUTBOARD END AFT LOWER CARGO. REPLACED SECTION OF FLOOR BEAM CAP PER BOEING SRM 51-10-01, P 18, 51-12-00, AND 5130-02. 2L74 4F A20WE 19950707005701995070700570NM 1995 7 7 P5CA9500252 119950630A5321 FLOOR BOEING747 747132 1384882NM BS 1820 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 ONE INCH HOLE IN AFT CARGO COMPARTMENT AT BS 1820 TO BS 1780, LBL 30. REPAIRED PER BOEING SRM 51-40-02 AND SRM 51-30-02. 2L74 4F A20WE 19950707005711995070700571NM 1995 7 7 P5CA9500253 119950630A5320 SUPPORT BOEING747 747132 1384882NM BS 1800 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 FLOOR SUPPORT CHANNEL BROKEN AT AFT LOWER CARGO COMPARTMENT BS 1800, LBL 30. REMOVED, FABRICATED, AND INSTALLED SUPPORT CHANNEL PER BOEING SRM 51-10-01, 51-12-00, 51-30-02. 2L74 4F A20WE 19950707005721995070700572NM 1995 7 7 P5CA9500254 119950630A5320 ANGLE BOEING747 747132 1384882NM BS 1820 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 1100 20246 CORROSION AT AFT LOWER CARGO FLOOR SUPPORT ANGLE UNDER NUT PLATE BS 1820, RBL 30. REMOVED AND REPLACED FLOOR SUPPORT ANGLE PER BOEING SRM 51-10-01, 51-12-00, 51-30-02. 2L74 4F A20WE 19950707005731995070700573NM 1995 7 7 P5CA9500255 119950630A5320 SUPPORT BOEING747 747132 1384882NM BS 1800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 CORROSION UNDER NUTPLATE AFT LOWER CARGO STA 1800 TO STA 1810, FLOOR SUPPORT CHANNEL AT RBL 30. REMOVED, FABRICATED, AND INSTALLED FLOOR SUPPORT CHANNEL PER BOEING SRM 51-10-01, 51-12-00, AND 51-30-02. 2L74 4F A20WE 19950707005741995070700574NM 1995 7 7 P5CA9500256 119950630A2510 LADDER BOEING747 747132 1384882NM CREW ENTRY CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 CREW ENTRY LADDER, TOP RUNG CRACKED LEFT AND RIGHT SIDES. WELD REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950707005751995070700575NM 1995 7 7 P5CA9500257 119950629A5210 STRUCTURE BOEING747 747121 1384871NM DOOR CUT OUT DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON CUT-OUT INTERNAL STRUCTURE ABOVE NR 3L ENTRY DOOR. DAMAGE SMOOTHED AND TREATED ACCORDING TO BOEING SRM 51-10-01. 2L74 4F A20WE 19950707005761995070700576NM 1995 7 7 P5CA9500258 119950629A5210 STRAP BOEING747 747132 1384882NM NR 3L DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 CRACK WITH STOP DRILL HOLE ON STRAP ON INTERNAL STRUCTURE REAR FRAME AT NR 3 LEFT ENTRY DOOR. REPAIRED PER BOEING SRM 51-40-03 AND 51-30-02. 2L74 4F A20WE 19950707005771995070700577NM 1995 7 7 P5CA9500259 119950629A5320 BRACKET BOEING747 747121 1384871NM BS 1242 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON BRACKET AT BS 1242, LBL 50. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950707005781995070700578NM 1995 7 7 P5CA9500260 119950629A5320 ANGLE BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON ANGLE AT THE BULKHEAD BS 1240, LBL 50. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01 (LEVEL 1). 2L74 4F A20WE 19950707005791995070700579SW 1995 7 7 QXEA9500207 119950705A32602782186017 INDICATOR-LDG SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A QXEAK NONE P NO WARNING INDICATION APAPPROACH 1 NM09385PH24181 AC595 PDX: DURING APPROACH TO PDX, GEAR CAME DOWN AND LOCKED. ON TOUCHDOWN, THE LEFT MAIN GREEN INDICATOR LIGHT EXTINGUISHED THEN CAME BACK ON AGAIN. THE LIGHT EXTINGUISHED AGAIN DURING BRAKING AND REVERSE AND REMAINED OUT. INDICATOR WAS REPLACED AND GROUND OPERATIONAL TEST PERFORMED WITH NO FURTHER DISCREPANCIES. AIRCRAFT RELEASED FOR SERVICE. 1L72 4T A8SW 19950707005801995070700580NM 1995 7 7 UPS203746 119950705A531165224972 FRAME BOEING727 72725C 138400HNM BS 930 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01947UP 19722 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS ON FRAME AT B.S. 930, RBL 64 AND 67, WL 199 RT WHEELWELL. REPAIRED IAW E.O. B727-5310-7167-A. 2L73 4F A3WE 19950707005811995070700581NM 1995 7 7 UPS203747 119950703A57556517348107A SKIN BOEING727 727247 138408FNM NR 10 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01209UP 21698 WHILE ON GROUND IN ST. PETERSBURG, FL, MAINTENANCE FOUND NR 10 SPOILER HAS 12 INCH CRACK IN TOP PANEL. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950707005821995070700582WP 1995 7 7 UPS803748 119950706A5330 SKIN DOUG DC8 DC871F 302199DWP BS 1350-1490 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE ON FUSELAGE BELLY SKIN, F.S. 1350-1490. REPLACED IAW SRM 51-1-20D, 51-1-21. 2L74 4F RT4A25 19950707005831995070700583WP 1995 7 7 UPS803749 119950706A532036169481 FITTING DOUG DC8 DC871F 302199DWP BS 702 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED FRAME END FITTING BELOW LONGERON 21L, F.S. 702. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005841995070700584WP 1995 7 7 UPS803750 119950706A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 0.75 INCH CRACK AT SKIN LOWER FWD CORNER OF LT GROUND AIR CONNECT CUT OUT. REPAIRED IAW E.O. DC8-5330-0793. 2L74 4F RT4A25 19950707005851995070700585WP 1995 7 7 UPS803751 119950706A53135757779 LONGERON DOUG DC8 DC871F 302199DWP FS 1650 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 29R CRACKED AT F.S. 1650. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005861995070700586WP 1995 7 7 UPS803752 119950706A53135757779 LONGERON DOUG DC8 DC871F 302199DWP FS 1650 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 32R CRACKED AT F.S. 1650. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005871995070700587WP 1995 7 7 UPS803753 119950706A53204647557 FITTING DOUG DC8 DC871F 302199DWP FS 1650 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON END FITTINGS AT F.S. 1650 ON LONGERONS 32R AND 34R. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005881995070700588WP 1995 7 7 UPS803754 119950706A532036431121 ANGLE DOUG DC8 DC871F 302199DWP FS 798 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 4.0 INCH CRACK ON FLOOR BEAM TO CENTER WING BOX ATTACH ANGLES, F.S. 798, LBL 50, 6.0 INCH CRACK ON SAME, F.S. 798, RBL 50. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005891995070700589WP 1995 7 7 UPS803755 119950706A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1740-1746 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKS ON OUTER FUSELAGE SKIN F.S. 1740 BETWEEN LONGERONS 17R TO 18R, AND F.S. 1746, LONGERON 14L. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950707005901995070700590WP 1995 7 7 UPS803756 119950706A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 550 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT END OF DOUBLER F.S. 550, B-BAG BIN DOOR LOWER JAMB. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950707005911995070700591WP 1995 7 7 UPS803757 119950706A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1650 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 34R AT F.S. 1650. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005921995070700592 1995 7 7 UPS803758 419950706A256551561004 SLIDE DOUG DC8 DC871F 302199DWP ENTRY DOOR FRAYED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ENTRY DOOR SLIDE GIRT FRAYED AND EXP DATE HAS THREE MONTHS LEFT. REPLACED ASSY IAW M/M 25-60-01. 2L74 4F RT4A25 19950707005931995070700593WP 1995 7 7 UPS803759 119950706A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1663-1680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE BELLY SKIN F.S. 1680-1663, LONGERON 32R. REPLACED IAW SRM 51-1-21, 51-1-20D. 2L74 4F RT4A25 19950707005941995070700594WP 1995 7 7 UPS803760 119950706A53132597242 LONGERONS DOUG DC8 DC871F 302199DWP FS 1490-1620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERONS 36 AND 35R, F.S. 1490-1620. REPLACED SECTIONS IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005951995070700595WP 1995 7 7 UPS803761 119950706A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 1620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INNER DOUBLER AT F.S. 1620, LONGERONS 32L-33L. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005961995070700596WP 1995 7 7 UPS803762 119950706A5330 SKIN DOUBLER DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT AND RT INNER SKIN DOUBLERS, F.S. 1610-1660, LONGERON 31R AND F.S. 1613-1650 LONGERON 31L. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707005971995070700597WP 1995 7 7 UPS803763 119950706A5330 FINGER DOUBLER DOUG DC8 DC871F 302199DWP FS 1510 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FINGER DOUBLER, F.S. 1510, LONGERON 30 RT. REPLACED IAW SRM 51-1-21. 2L74 4F RT4A25 19950707005981995070700598WP 1995 7 7 UPS803764 119950706A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP FS 140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME SHEAR TIE, F.S. 140, BETWEEN LONGERONS 36-35R. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950707005991995070700599WP 1995 7 7 UPS803765 119950706A534037558272N BATHTUB FITTING DOUG DC8 DC871F 302199DWP FS 280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BATHTUB FITTING F.S. 280, LONGERON 33A RT. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950707006001995070700600WP 1995 7 7 UPS803766 119950706A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1620-1640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN, F.S. 1620-1640, BETWEEN 29R-30R. REPAIRED IAW E.O. DC8-53-1407. 2L74 4F RT4A25 19950707006011995070700601WP 1995 7 7 UPS803767 119950706A5313575778 LONGERONS DOUG DC8 DC871F 302199DWP FS 1650 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01772UP 46072 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERONS 29L, 29R, AND 33L AT F.S. 1650, P\N 575778 AND P/N 575779. REPAIRED IAW E.O. DC8-5310-7156. 2L74 4F RT4A25 19950707006021995070700602WP 1995 7 7 UPS803768 119950703A3244 TIRE DOUG DC8 DC873F 302199FWP NR 3 MLG FAILED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01808UP 46008 WHILE IN CLIMBOUT FROM SEOUL TO ANCHORAGE, DOOR AND GEAR NOT LATCHED ILLUMINATED PASSING 15,000 FEET. AFTER SUCCESSFUL UPLATCH CHECK, EXECUTED PROCEDURES IAW QUICK REFERENCE HANDBOOK. LIGHTS REMAINED ILLUMINATED. GEAR AND DOOR CHECK PERFORMED REVEALED NR 3 MAIN TIRE TORN AND FLAT, TOUCHES INSIDE WELL. REPAIRED AND CHECKED IAW M/M 32-31-03. 2L74 4F RT4A25 19950707006161995070700616CE 1995 7 7 95ZZZX3326 119950521A2810 CELL CESSNA182 182B 2072706CE RT WING LEAKING A GNFAA UNSCHED LANDING BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CRCRUISE 1 SW012496G 51796 AT LEVEL OFF AS POWER WAS REDUCED, CABIN FILLED WITH FUEL VAPORS. FLIGHT ABORTED. AFTER LANDING, FUEL WAS FOUND DRIPPING FROM RIGHT WING. CAUSE AND SPECIFIC INFORMATION PENDING INVESTIGATION BY MECHANIC. 1H71 3O NT3A13 19950714000011995071400001SW 1995 7 14 MEJA9504002 119950422A26136801DD22 OVERTEMP WIRE FENWAL 1734361350 SWRNGNSA227 SA227AT 8780610SW LT WING DEFECTIVE A AMEJAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SW17566UP AT566 DURING TAXI WHEN THE SPEED LEVER WAS ADVANCED TO HIGH, THE LEFT WING OVERTEMP LIGHT FLICKERED. AIRCRAFT WAS FERRIED TO SAT. REPAIRED WIRE FROM FUSELAGE CONNECTOR TO BLEED AIR FAIL SENSOR IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED WIRING MANUAL 26-10-02. FUNCTIONAL CHECKED AND FLIGHT CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950714000021995071400002SW 1995 7 14 MEJA9504003 119950425A29102781006105 TUBE ASSY SWRNGNSA226 SA226TC 8780404SW RT MLG WW CRACKED A AMEJAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW17162MA TC234E ON FLIGHT 9935, BIS TO FSD, THE HYDRAULIC PRESSURE WENT TO ZERO AND BOTH THE LT AND RT ANNUNCIATOR LIGHTS CAME ON. EXTENDED GEAR WITH THE FREE-FALL HANDLE AND LANDED AT FSD WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CRACKED HYDRAULIC TUBE IN RT WHEELWELL. REMOVED AND REPLACED TUBE ASSY IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT MAINTENANCE MANUAL. PRESSURE CHECK AND FUNCTIONAL CHECK WERE PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950714000031995071400003SW 1995 7 14 MEJA9505001 119950503A3242212033 BRAKE ASSY SWRNGNSA227 SA227AT 8780610SW LT MLG DRAGGING A AMEJAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW17566UP AT566 DURING TAXI OUT FOR FLIGHT 1971, MAF TO DFW, THE LEFT BRAKE WAS DRAGGING AND BECAME MORE NOTICABLE THE FURTHER THE AIRCRAFT TAXIED. THE FLIGHT CREW RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT THE BRAKES AND FOUND THE LEFT BRAKES NOT RELEASING. REMOVED AND REPLACED THE LEFT INBOARD AND OUTBOARD BRAKE ASSEMBLIES IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950714000041995071400004SW 1995 7 14 MEJA9505002 119950510A324250116401 BRAKE ASSY SWRNGNSA227 SA227AT 8780610SW LT MLG LOCKED A AMEJAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SW17807M AT454B AFTER LANDING AT TOCUMEN (MPTO) AND DURING TAXI TO THE RAMP, THE AIRCRAFT STARTED TO VIBRATE AND BOUNCE WHEN EXITING FROM TAXIWAY TO THE RAMP. STOPPED AND SHUT DOWN ENGINES. FLIGHT CREW EXITED THE AIRCRAFT AND OBSERVED SMOKE AND FLAMES COMING FROM THE LEFT BRAKE. THE CREW PUT THE FIRE OUT AND WAITED FOR HELP. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD BRAKE ASSEMBLY WAS LOCKED. REMOVED AND REPLACED THE BRAKE ASSEMBLY IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL. FUNCTIONAL CHECK WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950714000051995071400005WP 1995 7 14 MEJA9505003 219950523A732031021781 P3 LINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE LOOSE A AMEJAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SW173108X AC517 P44056 WHILE ON DESCENT IN LIGHT TURBULANCE FROM 8000 TO 6000 FEET, THE RIGHT ENGINE FLAMED OUT. SECURED ENGINE AND LANDED AT DAL WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND P3 LINE TO FUEL CONTROL LOOSE AT ENGINE. TORQUED B-NUT AND PERFORMED FUNCTIONAL CHECK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19950714000061995071400006SW 1995 7 14 MEJA9506001 119950613A29102781006015 TUBE ASSY SWRNGNSA226 SA226TC 8780404SW FUSELAGE CRACKED A AMEJAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW17162MA TC234E ON BASE TO FINAL AT ABR, BOTH HYDRAULIC PRESSURE LIGHTS ILLUMINATED AND PRESSURE GAUGE WENT TO ZERO. LANDED AT ABR WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND TUBE ASSEMBLY CRACKED IN LOWER FUSELAGE NEAR WING ROOT EXIT. REMOVED AND REPLACED TUBE ASSEMBLY IN ACCORDANCE WITH FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL. FUNCTIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950714000071995071400007WP 1995 7 14 MWEA95231 119950707A5241 BEAM DOUG DC9 DC932 3022066WP GALLEY DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING 'A' CHECK INSP, A CRACK IN THE GALLEY SERVICE DOOR NR 3 BEAM WAS FOUND IN THE FORWARD END. INSTALLED REPAIR FITTING OVER THE CRACK PER SRM 52-05, FIG. 25. 2L72 4F A6WE 19950714000081995071400008WP 1995 7 14 MWEA95232 119950707A5241 DOOR PAN DOUG DC9 DC932 3022066WP GALLEY DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING 'C' CHECK, A CRACK WAS FOUND IN THE GALLEY SERVICE DOOR PAN SKIN .75 INCH LONG. THE CRACK RUNS FROM THE FWD PAN SKIN (IN THE NR 1 PAN AREA) AND TERMINATES IN THE BOTTOM FWD DOOR STOP HOLE. INSTALLED DOUBLER ON DOOR PAN PER SRM 52-03, FIG. 3. 2L72 4F A6WE 19950714000091995071400009WP 1995 7 14 MWEA95233 119950707A5241 BEAM DOUG DC9 DC932 3022066WP GALLEY DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING 'A' CHECK INSP, A CRACK WAS FOUND IN THE NR 1 BEAM FORWARD LOWER DOOR HINGE SUPPORT FITTING AREA, 2.50 INCHES IN LENGTH. INSTALLED REPAIR FITTING AND ATTACH ANGLE PER SRM 52-05, FIG. 25. 2L72 4F A6WE 19950714000101995071400010NM 1995 7 14 P5CA9500261 119950705A3244260356112 TIRE BOEING747 747124 1384874NM NR 9 BLOWN A P5CAO OTHER O OTHER TOTAKEOFF 1 WP23855FT 834 19733 NR 9 TIRE CAME APART OUT OF SEL. REPLACED NR 9 AND NR 10 TIRES, REPLACED BROKEN BODY GEAR CONNECTING ROD, TESTED ANTI-SKID SYSTEM, AND PERFORMED BLOWN TIRE INSPECTION. 2L74 4F A20WE 19950714000111995071400011NM 1995 7 14 P5CA9500262 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 1350/1480 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON PANEL SUPPORT BETWEEN BS 1350 AND BS 1480 BETWEEN LBL 16.5 AND RBL 16.5. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950714000121995071400012NM 1995 7 14 P5CA9500263 119950630A5712 RIB BOEING747 747121 1384871NM WS 1042 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK RIGHT WING LEADING EDGE CAVITY WS 1042, FORGED RIB UPPER CHORD FOUND WITH HFEC. REPAIRED PER BOEING SB 747-57-2116, FIG 6. 2L74 4F A20WE 19950714000131995071400013NM 1995 7 14 P5CA9500264 119950630A5320 SILL BOEING747 747121 1384871NM CARGO DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGED DOOR SILL ON BULK CARGO FORWARD SIDE. REPAIR PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000141995071400014NM 1995 7 14 P5CA9500265 119950630A5320 OMEGA BOEING747 747121 1384871NM BS 2000 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BULK CARGO NR 2 OMEGA FOR RIGHT BS 2000 IS BROKEN. PERFORMED REPAIR PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000151995071400015NM 1995 7 14 P5CA9500266 119950630A532165B604001 FLOOR PANEL BOEING747 747121 1384871NM AFT CARGO DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 AFT CARGO LEFT FORWARD FLOOR PANEL IS DAMAGED IN SEVERAL PLACES. REPAIRED PER BOEING SRM 51-40-02, FIG. 1. 2L74 4F A20WE 19950714000161995071400016NM 1995 7 14 P5CA9500267 119950630A2550 ROLLER TRAYS BOEING747 747121 1384871NM AFT CARGO BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 AFT CARGO 2 ROLLER TRAYS FROM RIGHT SIDE ARE BROKEN ON AFT POINT. REPAIR PERFORMED PER BOEING SRM 53-10-06, FIG 1. 2L74 4F A20WE 19950714000171995071400017NM 1995 7 14 P5CA9500268 119950630A7110 STIFFENER BOEING747 747121 1384871NM NR 3 NOSE COWL BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 ENGINE NR 3 FAN NOSE COWL AFT BULKHEAD AT 3 O'CLOCK, FOUND BROKEN PIECE IN STIFFNER. TRIMMED AND TREATED PER SRM 51-10-01. MATERIAL IS WITHIN LIMITS PER BOEING SRM 54-12-01. 2L74 4F A20WE 19950714000181995071400018NM 1995 7 14 P5CA9500269 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 960-980 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN INTERCOSTAL BETWEEN BS 960-980 (FLOOR BEAM) AT BRL 73. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950714000191995071400019NM 1995 7 14 P5CA9500270 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 620 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SEAT TRACK LBL 11.33 AT BS 620. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000201995071400020NM 1995 7 14 P5CA9500271 119950630A5321 FLOOR PANEL BOEING747 747121 1384871NM BS 700 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN FLOOR PANEL BS 700 FORWARD CARGO RIGHT SIDE. MANUFACTURED NEW PART PER BOEING SRM 53-10-21. INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000211995071400021NM 1995 7 14 P5CA9500272 119950630A2550 ROLLER TRAY BOEING747 747121 1384871NM BS 660 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 ROLLER TRAY BROKEN SECOND FROM RIGHT SIDE BS 660 FORWARD CARGO PIT. REPAIRED PER BOEING SRM 53-10-06, FIG. 1. 2L74 4F A20WE 19950714000221995071400022NM 1995 7 14 P5CA9500273 119950630A5321 FLOOR PANEL BOEING747 747121 1384871NM BS 720-760 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGED FLOOR PANELS FORWARD CARGO LEFT SIDE AT BS 720-760. MANUFACTURED NEW PART PER BOEING SRM 53-10-02. 2L74 4F A20WE 19950714000231995071400023NM 1995 7 14 P5CA9500274 119950630A5320 ATTACH ANGLE BOEING747 747121 1384871NM BS 820-840 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE IN MAIN DECK FLOOR ATTACH ANGLE BETWEEN BS 820-840 AT LBL 105. CLEANED AND SMOOTHED DAMAGE PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000241995071400024NM 1995 7 14 P5CA9500275 119950630A5320 SPLICE BOEING747 747121 1384871NM BS 1480 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SPLICE FITTING BS 1480 S41L. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02. 2L74 4F A20WE 19950714000251995071400025NM 1995 7 14 P5CA9500276 119950630A532065B0437029 FITTING BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION MAIN DECK AT BS 2360 S18L. FOUND CORROSION IN FITTING ATTACH FASTENERS TO THE WEB. REPLACED FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000261995071400026NM 1995 7 14 P5CA9500277 119950630A5320 CLIP BOEING747 747121 1384871NM BS 1740 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 MAIN DECK BS 1740 S16R HAS A CLIP WITH CRACK. FABRICATED NEW CLIP PER BOEING SRM 53-10-02 AND INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950714000271995071400027NM 1995 7 14 P5CA9500278 119950630A5320 CLIP BOEING747 747121 1384871NM BS 1780 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED CLIP MAIN RIGHT SIDE BS 1780 S16R. FABRICATED NEW CLIP PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000281995071400028NM 1995 7 14 P5CA9500279 119950630A5320BAC6604 FASTENERS BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 MAIN DECK BS 2360 IN S14R, S14L, S15L, S15R, S18R, S19R, S20R, S21R HAS CORRODED FASTENERS, REPLACED FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000291995071400029NM 1995 7 14 P5CA9500280 119950630A5320 FASTENERS BOEING747 747121 1384871NM BS 2300 MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 MAIN DECK BETWEEN S17L AND S18L HAS 5 MISSING FASTENERS ON BS 2300. INSTALLED MISSING FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000301995071400030NM 1995 7 14 P5CA9500281 119950630A5320 DOOR SILL BOEING747 747121 1384871NM BS 2235 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND MISSING 2 RIVETS AT BS 2235 S22L ON SILL OF DOOR 5L. CORROSION CLEANED AND TREATED PER BOEING SRM 51-10-01. FOUND WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950714000311995071400031NM 1995 7 14 P5CA9500282 119950630A5320 STRAP BOEING747 747121 1384871NM BS 680 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON STRAP AT BOTTOM OF MAIN DECK FLOOR BEAM BS 680 BETWEEN RBL 57 AND RBL 98. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000321995071400032NM 1995 7 14 P5CA9500283 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 600-640 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS AND CRACK ON CEILING SUPPORT BETWEEN BS 600 AND BS 640, RBL 98. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000331995071400033NM 1995 7 14 P5CA9500284 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 970 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON CEILING SUPPORT BS 970. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-21. INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000341995071400034NM 1995 7 14 P5CA9500285 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 580 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON CEILING SUPPORT AT BS 580 RBL 75. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000351995071400035NM 1995 7 14 P5CA9500286 119950630A5311 FRAME BOEING747 747121 1384871NM BS 600 TEAR A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR AROUND NUTPLATE HOLE BS 600 RBL 98. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000361995071400036NM 1995 7 14 P5CA9500287 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 560 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND CORROSION ON CEILING SUPPORT BS 560 RBL 75-98. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-21. INSTALLED PER 51-30-02. 2L74 4F A20WE 19950714000371995071400037NM 1995 7 14 P5CA9500288 119950630A5320 SUPPORT BOEING747 747121 1384871NM BS 660-680 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON CEILING SUPPORT AT BS 660-680 AND RBL 57-75. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000381995071400038NM 1995 7 14 P5CA9500289 119950630A5753 RIBS BOEING747 747121 1384871NM NR 1 FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT OUTBOARD MID-FLAP 2 RIBS NEXT TO INBOARD FORE FLAP TRACK CRACKED. MANUFACTURED 2 RIBS PER BOEING SRM 57-10-02. INSTALLED PER 51-30-02. 2L74 4F A20WE 19950714000391995071400039NM 1995 7 14 P5CA9500290 119950630A5753 SKIN BOEING747 747121 1384871NM NR 1 FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SKIN DAMAGE LEFT OUTBOARD MID-FLAP LEADING EDGE UPPER SURFACE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714000401995071400040NM 1995 7 14 P5CA9500291 119950630A5753 TE STRIP BOEING747 747121 1384871NM NR 1 FLAP GAPPED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT OUTBOARD MID-FLAP TRAILING EDGE STRIP IS GAPPED ALONG THE FLAP. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714000411995071400041NM 1995 7 14 P5CA9500292 119950630A5210 SKIN BOEING747 747121 1384871NM NR 2L DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2L ENTRY DOOR HAS 2 CRACKS, ONE IN INNER SKIN AND ONE IN OUTER SKIN. CRACKS WERE TRIMMED PER BOEING 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000421995071400042NM 1995 7 14 P5CA9500293 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1940-2040 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN FLOOR SUPPORT ANGLE RBL 37.5 BS 1940-2040. REPAIRED AS PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000431995071400043NM 1995 7 14 P5CA9500294 119950630A5340 ANGLE BOEING747 747121 1384871NM BS 2040 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND CRACK IN SUPPORT ANGLE FLOOR PANEL BS 2040 RBL 20 TO RBL 40. REPAIRED PER BOEING SRM 51-40-03, FIG 2. 2L74 4F A20WE 19950714000441995071400044NM 1995 7 14 P5CA9500295 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2060 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FLOOR PANEL RBL 22 AT BS 2060. REPAIRED PER BOEING SRM 51-40-03, FIG 2. 2L74 4F A20WE 19950714000451995071400045NM 1995 7 14 P5CA9500296 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2080-2100 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FLOOR PANEL RBL 30 BETWEEN BS 2080-2100. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000461995071400046NM 1995 7 14 P5CA9500297 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 1940 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FLOOR PANEL LBL 7.5 BETWEEN BS 1940-2060. REPAIRED PER BOEING SRM 51-30-02, SRM 53-10-23. 2L74 4F A20WE 19950714000471995071400047NM 1995 7 14 P5CA9500298 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2160 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT ANGLE FLOOR PANEL BS 2160 BETWEEN RBL 40 AND LBL 53. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN THE LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000481995071400048NM 1995 7 14 P5CA9500299 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2100 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE CARGO FLOOR PANEL BS 2100 RBL 75. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000491995071400049NM 1995 7 14 P5CA9500300 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 2140-2160 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT IN INTERCOSTAL AT S31R BETWEEN BS 2140-2160. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950714000501995071400050NM 1995 7 14 P5CA9500301 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2280-2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FLOOR OMEGAS AND ANGLE BRACKET BETWEEN BS 2280-2360 LBL 0 TO RBL 70. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000511995071400051NM 1995 7 14 P5CA9500302 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2280-2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN CONNECTION FLOOR ANGLE BETWEEN BS 2280-2360 AT S26L. REMOVED THE CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000521995071400052NM 1995 7 14 P5CA9500303 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 2000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN BS 2000 AT S33L. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000531995071400053NM 1995 7 14 P5CA9500304 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 2240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S42L BETWEEN BS 2240-2260. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000541995071400054NM 1995 7 14 P5CA9500305 119950630A5315 FLOOR BEAM BOEING747 747121 1384871NM BS 2280 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE WEB AT BS 2280 UNDER UPPER CHORD FLOOR BEAM AT WL 188 RBL 33 TO LBL 33. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000551995071400055NM 1995 7 14 P5CA9500306 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 2300 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S49L NEAR BS 2300. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000561995071400056NM 1995 7 14 P5CA9500307 119950630A5320 WEB BOEING747 747121 1384871NM BS 2300 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN WEB AT BS 2300 ABOVE S45L TO S46L. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000571995071400057NM 1995 7 14 P5CA9500308 119950630A5320 ANGLES BOEING747 747121 1384871NM BS 2320/2340 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN ANGLES AT WEB BS 2320 AND BS 2340 ABOVE S45L AND S46L. INSTALLED NEW ANGLES PER BOEING SRM 53-10-23. 2L74 4F A20WE 19950714000581995071400058NM 1995 7 14 P5CA9500309 119950630A5312 BULKHEAD BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN BS 2360 BETWEEN S50R TO S50L. CORROSION REMOVED PER BOEING SRM 51-50-01. 2L74 4F A20WE 19950714000591995071400059NM 1995 7 14 P5CA9500310 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 2280/2300 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN INTERCOSTAL NEAR S33L BETWEEN BS 2280 AND BS 2300. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000601995071400060NM 1995 7 14 P5CA9500311 119950630A5312 BLKHD SKIN BOEING747 747121 1384871NM BS 2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN AT PRESSURE BULKHEAD BS 2360 S46L - S48L. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000611995071400061NM 1995 7 14 P5CA9500312 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2340 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN ANGLE AT LOWER SIDE AREA AT WEB BS 2340 NEAR S48R. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000621995071400062NM 1995 7 14 P5CA9500313 119950630A5320 FLANGE BOEING747 747121 1384871NM BS 2240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN LOWER FLANGE AT BS 2240 AT CONNECTION TO SKIN BETWEEN S44L - W46L (LEVEL 2). REPAIRED PER SRM 53-10-23. 2L74 4F A20WE 19950714000631995071400063NM 1995 7 14 P5CA9500314 119950630A5320 FLANGE BOEING747 747121 1384871NM BS 2260 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON LOWER FLANGE BS 2260 AT CONNECTION TO SKIN BETWEEN S50L AND S51L. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000641995071400064NM 1995 7 14 P5CA9500315 119950630A5320 FLANGE BOEING747 747121 1384871NM BS 2180 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON LOWER FLANGE OF BS 2180 ON UPPER SURFACE BETWEEN S44L AND S48L. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000651995071400065NM 1995 7 14 P5CA9500316 119950630A5320 FLANGE BOEING747 747121 1384871NM BS 2200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN LOWER FLANGE AT BS 2200 AT CONNECTION SKIN AT S44L TO S48L. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714000661995071400066NM 1995 7 14 P5CA9500317 119950630A5753 LE SKIN BOEING747 747121 1384871NM NR 2 FORE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING INBOARD FORE FLAP LEADING EDGE HAS DELAMINATION AT LEADING EDGE CENTER AREA. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950714000671995071400067NM 1995 7 14 P5CA9500318 119950630A5753 TE SKIN BOEING747 747121 1384871NM NR 2 FORE FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING INBOARD FORE FLAP AT UPPER SURFACE OF TRAILING EDGE PATCHES REQUIRE UPGRADE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714000681995071400068NM 1995 7 14 P5CA9500319 119950630A5753 LE SKIN BOEING747 747121 1384871NM NR 1 FORE FLAP DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT OUTBOARD FORE FLAP DAMAGE TO LEADING EDGE SKIN NEXT TO INBOARD FITTING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714000691995071400069NM 1995 7 14 P5CA9500320 119950630A5511 PANEL BOEING747 747121 1384871NM HORIZ STAB DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT STABILIZER UPPER SURFACE HAS DELAMINATION ON PANEL JUST AHEAD OF OUTBOARD ELEVATOR. PANEL REPLACED. 2L74 4F A20WE 19950714000701995071400070NM 1995 7 14 P5CA9500321 119950630A5720 ROD BOEING747 747121 1384871NM FSS 1100 DISCONNECTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING FSS 1100 LEADING EDGE CAVITY SUPPORTING ROD FROM RIB TO LOWER SURFACE FAIRING IS DISCONNECTED FROM BRACKET. REPAIRED PER BOEING SRM 57-10-02 AND SRM 51-30-02. 2L74 4F A20WE 19950714000711995071400071NM 1995 7 14 P5CA9500322 119950630A571265B106312 RIB BOEING747 747121 1384871NM FSS 1385 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE CAVITY FSS 1385 FORGED RIB RIGHT AND LEFT SIDES OF UPPER CHORD CRACKED. REPLACED RIB INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000721995071400072NM 1995 7 14 P5CA9500323 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1000-1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SHEET METAL PANELS UNDER HINGE DOORS LEFT AND RIGHT SIDES BETWEEN BS 1000 AND BS 1240. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000731995071400073NM 1995 7 14 P5CA9500324 119950630A532065B105461011 RETAINERS BOEING747 747121 1384871NM BS 1090 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON ANGLE ON DOOR BS 1090 LEFT SIDE. REPLACED SEAL RETAINER FASTENERS. INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714000741995071400074NM 1995 7 14 P5CA9500325 119950630A5730 SKIN BOEING747 747121 1384871NM WING CENTER SEC CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE UPPER SKIN (CEILING) AND STRINGERS AND ANGLE BETWEEN FRONT SPAR TO STR 28C IN DRY BAY (INTERNAL) CENTER-SECTION. REMOVED CORROSION FROM UPPER SKIN PER BOEING SRM 51-10-01 WITHIN LIMITS PER SRM 53-10-01. TREATED PER 51-10-02. 2L74 4F A20WE 19950714000751995071400075NM 1995 7 14 P5CA9500326 119950630A5730 SKIN BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE WALL AT BS 1000 AT RBL 9, RBL 10 AREA IN DRY-BAY (INTERNAL) CENTER SECTION RIGHT. REMOVED CORROSION PER BOEING SRM 51-10-01. TREATED AND PAINTED PER 51-10-02 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000761995071400076NM 1995 7 14 P5CA9500327 119950630A5711 SPAR BOEING747 747121 1384871NM BS 1000 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE UPPER SPAR AT BS 1000 BETWEEN LBL 30 TO RBL 120 IN DRY-BAY (INTERNAL) CENTER SECTION RIGHT. REMOVED CORROSION PER BOEING SRM 51-10-01. TREATED PER 51-10-02 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000771995071400077NM 1995 7 14 P5CA9500328 119950630A5280 DOOR BOEING747 747121 1384871NM RT MLG DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LANDING GEAR WHEELWELL INBOARD DOOR FORWARD LOWER CORNER IS DAMAGED. REPAIRED PER SRM 51-40-03, FIG. 1. 2L74 4F A20WE 19950714000781995071400078NM 1995 7 14 P5CA9500329 119950630A5311 FRAME BOEING747 747121 1384871NM BS 640 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN STA 640 LEFT SIDE BETWEEN S17L AND S18L. REPAIRED PER IAI MF-MAN-B47-53-83987. 2L74 4F A20WE 19950714000791995071400079NM 1995 7 14 P5CA9500330 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN STRINGER S45L AT BS 1960. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000801995071400080NM 1995 7 14 P5CA9500331 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1940 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 1940 LBL 45. REPAIRED PER SRM 51-40-03 AND SRM 53-10-23. 2L74 4F A20WE 19950714000811995071400081NM 1995 7 14 P5CA9500332 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 2000 LBL 22. REPAIRED PER BOEING SRM 53-10-03 AND SRM 5130-02. 2L74 4F A20WE 19950714000821995071400082NM 1995 7 14 P5CA9500333 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2040/2080 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FLOOR PANEL BETWEEN BS 2040 AND BS 2080 LBL 50. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000831995071400083NM 1995 7 14 P5CA9500334 119950630A5320 ANGLE BOEING747 747121 1384871NM AFT CARGO CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 2080 LBL 37. REPAIRED PER SRM 51-40-03. 2L74 4F A20WE 19950714000841995071400084NM 1995 7 14 P5CA9500335 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1920/2120 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS AND CRACKS IN SUPPORT ANGLE FOR PANEL BETWEEN BS 2120 AND BS 1920 LBL 30. MANUFACTURED AND REPLACED PER BOEING SRM 51-30-02 AND SRM 53-10-23. 2L74 4F A20WE 19950714000851995071400085NM 1995 7 14 P5CA9500336 119950630A5320 SPLICE BOEING747 747121 1384871NM BS 1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S47R SPLICE AT BS 1960. REPLACED SPLICE FITTING PER BOEING SRM 53-10-03. 2L74 4F A20WE 19950714000861995071400086NM 1995 7 14 P5CA9500337 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S44R BS 1960. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000871995071400087NM 1995 7 14 P5CA9500338 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1920-1940 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND DENT IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 1940 BL 0. CORROSION REMOVED AND DENT SMOOTHED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000881995071400088NM 1995 7 14 P5CA9500339 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1320 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT ON SUPPORT ANGLE FOR FLOOR PANEL BS 1320 RBL 5. STRAIGHTENED AND SMOOTHED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000891995071400089NM 1995 7 14 P5CA9500340 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1340 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT ANGLE FOR FLOOR PANEL BS 1340 RBL 22. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000901995071400090NM 1995 7 14 P5CA9500341 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL AT BS 1960 RBL 15. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000911995071400091NM 1995 7 14 P5CA9500342 119950630A5340 ANGLE BOEING747 747121 1384871NM BS 2020 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN EXISTING REPAIR ON SUPPORT ANGLE FOR FLOOR PANEL BS 2020 RBL 10 TO RBL 7.5. MANUFACTURED NEW SUPPORT PER BOEING SRM 53-10-23 AND SRM 53-10-01. 2L74 4F A20WE 19950714000921995071400092NM 1995 7 14 P5CA9500343 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1970 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN EXISTING REPAIR SUPPORT ANGLE FOR FLOOR PANEL BS 1970 RBL 22. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000931995071400093NM 1995 7 14 P5CA9500344 119950630A5340 ANGLE BOEING747 747121 1384871NM BS 2000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 15. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000941995071400094NM 1995 7 14 P5CA9500345 119950630A5320 BEAM BOEING747 747121 1384871NM BS 2040 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN UPPER CHORD BEAM BS 2040 BETWEEN RBL 7 AND RBL 15. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000951995071400095NM 1995 7 14 P5CA9500346 119950630A5320 BEAM BOEING747 747121 1384871NM BS 2020 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN UPPER CHORD BEAM BS 2020 RBL 15. CORROSION REMOVED PER SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714000961995071400096NM 1995 7 14 P5CA9500347 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2040 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN SUPPORT ANGLE FOR FLOOR PANEL BS 2040 RBL 25. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950714000971995071400097NM 1995 7 14 P5CA9500348 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 15 AND RBL 75. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000981995071400098NM 1995 7 14 P5CA9500349 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2000-2020 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 2000 AND BS 2020 RBL 5 AND RBL 53. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714000991995071400099NM 1995 7 14 P5CA9500350 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2000 RBL 45. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714001001995071400100NM 1995 7 14 P5CA9500351 119950630A5340 ANGLE BOEING747 747121 1384871NM BS 2040 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL BS 2040 BL 0. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714001011995071400101NM 1995 7 14 P5CA9500352 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2000-2020 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SUPPORT ANGLE FOR FLOOR PANEL RBL 25 BETWEEN BS 2000 AND BS 2020. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714001021995071400102NM 1995 7 14 P5CA9500353 119950630A5753 WEAR STRIP BOEING747 747121 1384871NM NR 2 FORE FLAP BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING INBOARD FORE FLAP INBOARD FIBERGLASS STRIP BROKEN. MANUFACTURED NEW STRIP PER BOEING SRM 57-10-02 AND SRM 51-30-02. 2L74 4F A20WE 19950714001031995071400103NM 1995 7 14 P5CA9500354 119950630A5753 WEAR STRIP BOEING747 747121 1384871NM NR 2 FORE FLAP MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING INBOARD FORE FLAP INBOARD SIDE MOVABLE SURFACE WEAR STRIP MISSING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714001041995071400104NM 1995 7 14 P5CA9500355 119950630A5753 SKIN BOEING747 747121 1384871NM NR 2 AFT FLAP HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HOLE IN LEFT AFT INBOARD FLAP AT LEADING EDGE NEXT TO OUTBOARD LINK. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714001051995071400105NM 1995 7 14 P5CA9500356 119950630A5753 SKIN BOEING747 747121 1384871NM NR 2 MID FLAP DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 THREE LARGE DENTS LEFT INBOARD MID-FLAP INBOARD OF INBOARD CARRIAGE LOWER SURFACE. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950714001061995071400106NM 1995 7 14 P5CA9500357 119950630A5753 SKIN BOEING747 747121 1384871NM NR 2 MID FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATIONS ON LEFT INBOARD MID-FLAP UPPER SKIN SECOND ROW MOST OUTBOARD PANEL. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950714001071995071400107NM 1995 7 14 P5CA9500358 119950630A5753 PROFILE FIBER BOEING747 747121 1384871NM NR 3 TE FLAP MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING INBOARD FLAP INBOARD PROFILE FIBER IS MISSING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950714001081995071400108NM 1995 7 14 P5CA9500359 119950630A5310 STRUCTURE BOEING747 747121 1384871NM BS 1760-1780 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND BEND IN FLOOR RIB, GOUGE, AND HIT IN FLOOR COVER SHEET METAL BETWEEN BS 1760 AND BS 1780, RBL 25 AND RBL 45. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950714001091995071400109NM 1995 7 14 P5CA9500360 119950630A5315 FLOOR BEAM BOEING747 747121 1384871NM BS 1760 BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BEND IN UPPER CHORD AT FLOOR BEAM AT BS 1760 AT LBL 30. REPAIRED PER BOEING SRM 51-40-01 AND SRM 51-10-01. 2L74 4F A20WE 19950714001101995071400110NM 1995 7 14 P5CA9500361 119950630A5310 STRUCTURE BOEING747 747121 1384871NM BS 1780-1800 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND DENTS IN THE FLOOR COVER SHEET METAL BETWEEN BS 1780 AND BS 1800, LBL 45 AND LBL 35. REPAIRED PER BOEING SRM 53-10-23. 2L74 4F A20WE 19950714001111995071400111NM 1995 7 14 P5CA9500362 119950630A5315 FLOOR BEAM BOEING747 747121 1384871NM BS 1820 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN UPPER CHORD AT FLOOR BEAM BS 1820 AT RBL 15. REPAIRED PER BOEING SRM 51-40-04, FIG 1. 2L74 4F A20WE 19950714001121995071400112NM 1995 7 14 P5CA9500363 119950630A2550 ROLLER TRAY BOEING747 747121 1384871NM BS 1780-1820 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN ROLLER TRAY LBL 35 BETWEEN BS 1780 AND BS 1820. REPAIRED PER BOEING SRM 53-10-06. 2L74 4F A20WE 19950714001131995071400113NM 1995 7 14 P5CA9500364 119950630A5320 CHORD BOEING747 747121 1384871NM BS 1820 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 EXISTING REPAIR UNACCEPTABLE, UPPER CHORD BS 1820 ABOVE S42L. REPLACED REPAIR WITH REPAIR PER BOEING SRM 53-40-03, FIG. 3. 2L74 4F A20WE 19950714001141995071400114NM 1995 7 14 P5CA9500365 119950630A532065B063254 FITTING BOEING747 747121 1384871NM BS 1840-1860 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND CORROSION IN FLOOR FITTING AT FLOOR COVER BETWEEN BS 1840 AND BS 1860. REPLACED FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714001151995071400115NM 1995 7 14 P5CA9500366 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1900-1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 1900 AND BS 1920 NEAR S45R. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714001161995071400116NM 1995 7 14 P5CA9500367 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1860-1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN CENTER COVER SHEET METAL BETWEEN BS 1860 TO BS 1920. REPLACED COVER PER BOEING SRM 51-10-23 AND SRM 51-30-02. 2L74 4F A20WE 19950714001171995071400117NM 1995 7 14 P5CA9500368 119950630A5720 FLANGE BOEING747 747121 1384871NM BS 1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION FOUND IN THE UPPER FLANGE AT BS 1920 ABOVE S42L. REPAIRED PER BOEING SRM 53-10-28 AND SRM 51-30-02. 2L74 4F A20WE 19950714001181995071400118NM 1995 7 14 P5CA9500369 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1900 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S46L NEAR BS 1900. REPAIRED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950714001191995071400119NM 1995 7 14 P5CA9500370 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 1780-1900 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN TRACK RBL 45 TO RBL 25 AND LBL 25 BETWEEN BS 1900 AND BS 1780. REPAIRED PER BOEING SRM 53-10-05. 2L74 4F A20WE 19950714001201995071400120NM 1995 7 14 P5CA9500371 119950630A5512 STRIP BOEING747 747121 1384871NM HORIZ STAB TE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT STABILIZER TRAILING EDGE STRIP CRACKED BETWEEN NAV LIGHT AND ELEVATOR. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950714001211995071400121NM 1995 7 14 P5CA9500372 119950630A5280 SKIN BOEING747 747121 1384871NM LT MLG DOOR CUT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING LANDING GEAR INBOARD DOOR HAS A CUT ON INNER SKIN SURFACE. REPAIRED PER BOEING SRM 52-80-02-1. 2L74 4F A20WE 19950714001221995071400122NM 1995 7 14 P5CA9500373 119950630A5320 WEB BOEING747 747121 1384871NM BS 1960-1980 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN WEB BETWEEN BS 1960 AND BS 1980 UNDER SUPPORT ANGLE FOR FLOOR PANEL RBL 45. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02. 2L74 4F A20WE 19950714001231995071400123NM 1995 7 14 P5CA9500374 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1920-1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SUPPORT ANGLE FOR FLOOR PANEL BETWEEN BS 1920 AND BS 1960, RBL 7.5 AND RBL 15. REPAIRED PER BOEING SRM 53-10-23 AND SRM 51-30-02. 2L74 4F A20WE 19950714001241995071400124NM 1995 7 14 P5CA9500376 119950630A5320 TENSION TIE BOEING747 747121 1384871NM BS 780 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN TENSION TIE AT BS 780 LBL 85. CRACK AROUND 1 HOLE ONLY. REPAIRED PER BOEING SRM 51-40-03 AND SRM 51-30-02. 2L74 4F A20WE 19950714001251995071400125NM 1995 7 14 P5CA9500377 119950630A5320 BRACKET BOEING747 747121 1384871NM FWD CARGO BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 WATER TANK AIR FILTER MOUNTING BRACKET BROKEN. MANUFACTURED NEW BRACKET PER BOEING SRM 51-20-02 AND SRM 51-30-02. 2L74 4F A20WE 19950714001261995071400126NM 1995 7 14 P5CA9500378 119950630A5400 FAIRING DOOR BOEING747 747121 1384871NM NR 4 PYLON CHAFED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 4 STRUT LEFT FAIRING DOOR INTERNAL LOWER CHORD SKIN IS GOUGED AND CHAFED BADLY. REPAIRED PER BOEING SRM 51-10-01, 53-50-00, AND 51-10-02. 2L74 4F A20WE 19950714001271995071400127NM 1995 7 14 P5CA9500379 119950630A5400 FAIRING DOOR BOEING747 747121 1384871NM NR 2 PYLON CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND SMALL CRACK ON LOWER EDGE NR 2 PYLON FAIRING EXTERIOR SURFACE SKIN. REMOVED CORROSION AND CRACK PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950714001281995071400128NM 1995 7 14 P5CA9500380 119950630A5400MS2000162800 HINGE BOEING747 747121 1384871NM NR 3 PYLON BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN HINGE AND LOOSE RIVETS ON BLOW OUT PANEL AT NR 3 RIGHT PYLON FAIRING DOOR. REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950714001581995071400158NE 1995 7 14 95ZZZX3361 119950605A2612 FIRE WARNING SKRSKYS76 S76 8143010NE NR 1 ENGINE MALFUNCTION A ALGAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SW035446E 760175 IN LEVEL FLIGHT, NR 1 FIRE LIGHT ILLUMINATED AND AUDIO SOUNDED. WAS UNABLE TO EXTINGUISH LIGHT OR TURN HORN OFF. SECURED NR 1 ENGINE. APPROXIMATELY 3 MINUTES LATER, LIGHT WENT OUT AND HORN WENT OFF. UPON FINAL APPROACH, RESTARTED NR 1 ENGINE, FIRE LIGHT DID NOT ILLUMINATE. THE A/C WAS INSPECTED AND FOUND IN THE ELECTRICAL COMPARTMENT THERE WERE NUMEROUS WIRES THAT HAD CHAFED. THE WIRES WERE REPAIRED AND THE A/C WAS OPS CHECKED WITH NO FURTHER DEFECTS NOTED. 1G72 3U H1NE 19950714001711995071400171NE 1995 7 14 95ZZZX3374 119950622A29107665103004068 LINE SKRSKYS76 S76 8143010NE XMSN AREA LEAKING A ALGAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW03702AL 760243 IN CRUISE FLIGHT APPROXIMATELY 25 MINUTES AFTER TAKEOFF, NR 1 SERVO SYSTEM CAUTION LIGHT ILLUMINATED. RESET SERVO JAM CIRCUIT BREAKER AND LIGHT EXTINGUISHED. TWO MINUTES LATER, NR 1 SERVO SYSTEM LIGHT ILLUMINATED AGAIN. RESET SERVO JAM CIRCUIT BREAKER AND LIGHT EXTINGUISHED. AIRCRAFT TURNED BACK TO BASE. ONE MINUTE LATER, NR 1 HYDRAULIC SERVO SYSTEM LIGHT ILLUMINATED AGAIN. RESET CIRCUIT BREAKER, BUT LIGHT REMAINED ILLUMINATED. AIRCRAFT LANDED FIRST AVAILABLE PLACE. NR 1 HYDRAULIC SYSTEM WAS FOUND TO REQUIRE SERVICING. SERVICED SYSTEM AND GROUND RAN ACFT. TAIL ROTOR RETURN LINE FOUND LEAKING AT B-NUT. ACFT WAS SHUT DOWN. B-NUT FOUND BACKED OFF. B-NUT TIGHTENED, ACFT GROUND RAN AND LEAK CHECKED OK. 1G72 3U H1NE 19950714001721995071400172NM 1995 7 14 BJNA95502 119950524A3350SPLICE EEL BOEING737 7372H4 138448CNM CABIN BROKEN A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 ROW 7 EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE ON ROW 7 EMERGENCY EXIT LIGHT. SYSTEM OPS CHECKED GOOD PER BMM 33-51-11. 2L72 4F A16WE 19950714001731995071400173WP 1995 7 14 HAL95069 119950614A3350P4010049 EEL BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13603DC 6988 47784 HNL - STA 504 - EMERGENCY FLOOR LIGHTS WILL NOT TEST PROPERLY. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. ACFT TT 31,850. TOTAL CYCLES 43,602. (X) 2L72 4F A6WE 19950714001741995071400174WP 1995 7 14 HAL95070 119950617A33502078 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13673MC 1229 47726 HNL - EMERGENCY FLOOR LIGHTS WILL NOT GO ON. REPLACED EMERGENCY LIGHT POWER SUPPLY. OPERATION CHECK GOOD. (X) 2L72 4F A6WE 19950714001751995071400175NM 1995 7 14 TSAA8553125 119950620A5330 SKIN BOEING737 7372Q9 138448MNM BS 727 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13804AL 21719 DURING OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK 1.6250 INCHES LONG AT BS 727B PLUS 16.5, 1 INCH ABOVE S17L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. TAT - 36,534.34. TAC - 60,358. (X) 2L72 4F A16WE 19950714001761995071400176NM 1995 7 14 WRLA95031 119950614A3230AYG741550012B INTERLOCK CYL DOUG MD11 MD11 3023602NM RT WW FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27280WA 48458 AFTER TAKEOFF, CAPTAIN OBSERVED LANDING GEAR WOULD NOT RETRACT. CAPTAIN ELECTED TO RETURN TO AIRPORT OF DEPARTURE. AIRCRAFT RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND TRIM INTERLOCK CYLINDER WOULD NOT EXTEND AND ALLOW GEAR HANDLE TO BE RAISED. REMOVED AND REPLACED CYLINDER. INSTALLED ALL FOUR GEAR DOWNLOCK PINS, PRESSURIZED HYDRAULIC SYSTEM NR 3, AND RAISED AND LOWERED GEAR HANDLE. ALL OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950714001771995071400177WP 1995 7 14 9510429162 119950627A213110256861 PRESS CONTROLLER DOUG DC9 DC914 3022034WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018907E640313192 45748 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE CONTROLLER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950714001781995071400178WP 1995 7 14 9510439993 119950705A3231 RETRACT MECH DOUG DC9 DC931 3022065WP LANDING GEAR DR MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL018986E 47402 DURING APPROACH INTO GRR, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. LANDING GEAR DOORS AND SKIDS SCRAPED ON LANDING. CHECKED SWITCH AND ROLLERS ON MAIN GEAR DOORS. REPLACED SKIDS AND REPAIRED DAMAGE TO BOTH DOORS. ALL CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950714001791995071400179NE 1995 7 14 9510442714 219950630A7310 FUEL FILTER BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 GL01718RC 22344 88827 AT FL 370, THE NR 2 ENGINE FLAMED OUT. NO ASSOCIATED VIBRATION. RESTARTED AT FL 200 WITHOUT INCIDENT. MAINTENANCE REPLACED FUEL PUMP FILTER. NO OTHER ANOMALIES NOTED. 2L73 4F4 F A3WE E2EA 19950714001801995071400180NM 1995 7 14 9510452705 119950630A3244657276187 TIRE BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE LEFT MLG FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01802EA 163 22433 700219A DURING TAKEOFF, THE LEFT MAIN GEAR OUTBOARD TIRE RECAP SEPARATED AND INGESTED IN NR 1 ENGINE. THE NR 1 ENGINE COMPRESSOR STALLED. REDUCED THE NR 1 THRUST TO IDLE, JETTISONED 11,000 POUNDS OF FUEL, AND RETURNED TO DEN WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AND NR 2 MAIN TIRES AND NR 1 ENGINE. 2L73 4F4 F A3WE E2EA 19950714001811995071400181NM 1995 7 14 9510465522 119950708A213320224807 OUTFLOW ACT BOEING757 757251 1384970NM CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01522US2591218371 23616 DURING CLIMB, BOTH AUTO PRESSURE CONTROLLERS WERE INOPERATIVE WITH CABIN AUTO INOPERATIVE STATUS MESSAGE. AIRCRAFT RETURNED TO MSP. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM CHECK WAS NORMAL. 2L72 4F RTA2NM 19950714001821995071400182NM 1995 7 14 9510472294 119950708A3150 TO WARNING BOEING727 727251 138408HNM FLIGHT DECK SOUNDED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01294US 21505 TAKEOFF WARNING HORN SOUNDED UPON APPLICATION OF DEPARTURE THRUST. TAKEOFF WAS ABORTED. NOTE: FLAP SETTING WAS 25 DEGREES. AIRCRAFT GROSS WEIGHT REDUCED FOR A 15 DEGREE FLAP DEPARTURE. MSP MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. CORRECTION: DATE 950709 CHANGED TO 950708. 2L73 4F A3WE 19950714001831995071400183NM 1995 7 14 9510482203 119950709A3150 TO WARNING BOEING727 727251 138408HNM FLIGHT DECK SOUNDED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01203US 22543 UPON APPLICATION OF TAKEOFF THRUST, AURAL WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. NOTE: FLAP SETTING WAS 5 DEGREES. RECYCLED FLAPS AND SPEED BRAKES, SUBSEQUENT DEPARTURE WAS NORMAL. MAINTENANCE CONTROL WAS ADVISED. 2L73 4F A3WE 19950714001841995071400184NE 1995 7 14 9510491144 219950708A7311808899 FUEL/OIL COOLER DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 2 ENGINE LEAKING A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01144JC 144JC DURING CRUISE, STRONG SMELL AND SOME SMOKE AND FUMES WERE PRESENT IN THE CABIN. RETURNED TO MSP. REPLACED THE NR 2 ENGINE FUEL/OIL COOLER AND AIR CONDITIONING SOCKS. 2L73 4F4 F A22WE E20EA 19950714001851995071400185NM 1995 7 14 DL72S952941 119950705A5330 SKIN BOEING727 727232 1384082NM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 FOUND DURING F-1 LETTER CHECK - LWR LT TORQUE BOX SKIN CRACKED .1250 INCH AT LWR FWD LIGHTNING HOLE STA 1223, LWR RT TORQUE BOX SKIN CRACKED .3750 INCH AT LWR FWD LIGHTNING HOLE STA 1223. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950714001861995071400186NM 1995 7 14 DL72S952942 119950705A5754 SLAT BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 FOUND DURING F-1 LETTER CHECK - .75 INCH CRACK BELOW NB 8 SLAT O/B STOP PAD. REPAIRED PER MM 75-54-0. 2L73 4F A3WE 19950714001871995071400187NM 1995 7 14 DL72S952943 119950705A5720 STIFFENER BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 FOUND DURING F-1 LETTER CHECK - I/B L/E SPAR STIFFENER CRACKED AT NR 5 SLAT TRACK. REPLACED WING SPAR STIFFENER PER M/M 57-20-21, PG 813. 2L73 4F A3WE 19950714001881995071400188NM 1995 7 14 DL72S952944 119950705A5720 STIFFENER BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 FOUND DURING F-1 LETTER CHECK - L/E WING SPAR STIFFENER CRACKED AT NR 3 SLAT O/B TRACK O/B LEG. REPLACED WING SPAR STIFFENER PER M/M 57-20-21. 2L73 4F A3WE 19950714001891995071400189NM 1995 7 14 DL72S952954 119950628A5210 SKIN BOEING727 727232 1384082NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FRAME CRACKED. THE LOWER FWD CORNER OF THE L1 MAIN ENTRANCE DOOR HAS A 2 INCH CRACK (VIEWED FROM LWR FWD LIGHTING HOLE). REPAIRED PER MM 52011091, PAGE 805. 2L73 4F A3WE 19950714001901995071400190NM 1995 7 14 DL72S952955 119950705A5720 FITTING BOEING727 727232 1384082NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 LEFT WING - REF OPN 5522. HFEC INSP ON BORE OF AFT TERMINAL FITTING SHOWS CRACK INDICATION AT 6 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7, FIG 1. 2L73 4F A3WE 19950714001911995071400191NM 1995 7 14 DL72S952957 119950628A5210 SKIN BOEING727 727232 1384082NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 SKIN CRACKED, L1 DOOR. THE L1 MAIN ENTRY DOOR HAS EXT SKIN CRACK AT THE LWR FWD CORNER. REPAIRED PER SRM5 2-11-01, FIG 804. FOUND AT HMV. 2L73 4F A3WE 19950714001921995071400192NM 1995 7 14 DL72S952961 119950626A5532 SKIN BOEING727 727232 1384082NM RT VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 SKIN CRACKED, .50 INCH CRACK IN VERT STAB SKIN RT SIDE AT FRONT SPAR AREA BELOW PANEL 9501. REPAIRED PER SRM 55-30-3 FIG 2, AT HMV. 2L73 4F A3WE 19950714001931995071400193NM 1995 7 14 DL72S952969 119950628A5240 SKIN BOEING727 727232 1384082NM LT AFT SVC DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, LEFT AFT SERVICE DOOR S/N 506 HAS .75 INCH CRACK AT UPPER HINGE CUTOUT. REPAIR: REPAIRED PER SRM 52-40-2, FIG 4. 2L73 4F A3WE 19950714001941995071400194NM 1995 7 14 DL72S952970 119950626A5753 FOREFLAP BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CRACK RIGHT WING OB FOREFLAP AT FLAP TRACK. REPAIR: REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950714001951995071400195NM 1995 7 14 DL72S952979 119950628A5754 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 AT HMV, NR 4 SLAT, NR 18 RIB WAS FOUND CRACKED, REPAIRED PER MM 57-54-0, PG 807. 2L73 4F A3WE 19950714001961995071400196NM 1995 7 14 DL72S952980 119950629A5312 BLKHD SKIN BOEING727 727232 1384082NM BS 1183 MISDRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 MISDRILLED HOLE AFT SIDE STA 1183 BULKHEAD, RBL 36.83 APPROX 38 INCHES ABOVE FLOOR LINE. HOLE IS DRILLED THROUGH THE SKIN BUT NOT THROUGH THE FRAME. HOLE IS DRILLED NEXT TO AN EXISTING FASTENER AND WAS DRILLED WHILE ACCOMPLISHING EO 4-59821-3. REPAIRED PER SRM 53-10-9, FIG 4. DAMAGE AT HMV. 2L73 4F A3WE 19950714001971995071400197NM 1995 7 14 DL72S952981 119950707A301065162255A ANTI ICE DUCT BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 ANTI-ICE DUCT CRACKED 22 INCHES FROM OUTBOARD END. REPAIRED PER SRM 57-50-03, FIG 12, AT HMV SHOP VISIT FOR WING L/E KRUGER FLAP. 2L73 4F A3WE 19950714001981995071400198NM 1995 7 14 DL72S952982 119950707A5414 SKIN BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 CRACKS COMING OUT OF FASTENERS, FASTENER HOLES ON LEFT AND RIGHT SIDE OF SADDLE FAIRING NR 2 INTAKE VERTICAL STAB PANEL. FOUND DURING B-2 LTR CK. REPAIRED PER SRM 54-30-0. 2L73 4F A3WE 19950714001991995071400199NM 1995 7 14 DL72W952936 119950625A5313 STRINGER BOEING727 727247 138408FNM BS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, STR 27L CORRODED AT STA 720F PLUS 10. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950714002001995071400200NM 1995 7 14 DL72W952937 119950702A5347 SEAT TRACK BOEING727 727247 138408FNM BS 1070-1110 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, SEAT TRACK CORRODED, FROM FS 1070-1110 RT IB TRACK RBL 24.5. REMOVED CORROSION PER SRM 51-10-06. REPLACED TRACK FROM FS 1070 TO 1110 PER MM 53-20-11, PG 806. 2L73 4F A3WE 19950714002011995071400201NM 1995 7 14 DL72W952938 119950622A5347 SEAT TRACK BOEING727 727247 138408FNM BS 980-1036 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, SEAT TRACK CORRODED, RBL 45 FROM FS 980 TO FS 1036 AND RBL 55 FROM FS 1030 TO FS 1100. REPLACED SECTIONS OF TRACK PER MM 53-20-11, PG 804. 2L73 4F A3WE 19950714002021995071400202NM 1995 7 14 DL72W952946 119950619A7110 COWL BOEING727 727247 138408FNM BS 1352 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 2 PYLON BS 1352 MATING SURFACE BETWEEN ENG COWLS AND AFT FUSELAGE ARE WORN AT LOWER AREAS. DRILLED, HEAT TREATED, AND INSTALLED REPAIR PER MM 53-11-0. 2L73 4F A3WE 19950714002031995071400203NM 1995 7 14 DL72W952949 119950620A5320 WEB BOEING727 727247 138408FNM BS 1263/1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 WEB CRACKED-48 SECTION INTERIOR. CLOSE OUT WEB CRACKED AT LIGHTING HOLE. LT SIDE BETWEEN STA 1263 AND STA 1273. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0, PG 802. FOUND AT HMV. 2L73 4F A3WE 19950714002041995071400204NM 1995 7 14 DL72W952960 119950622A5347 SEAT TRACK BOEING727 727247 138408FNM BS 1110-1140 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV: SEAT TRACK CORRODED STA 1110 TO STA 1140 LB 25 JUST FWD OF AFT LT LAV. SEAT TRACK CORRODED STA 1110 TO STA 1140 RBL 25 JUST FWD OF AFT RT LAV. REPLACED SECTIONS OF SEAT TRACK PER MM 53-20-11, FIG 2. TRACK PER M/M 53-20-11. 2. 2L73 4F A3WE 19950714002051995071400205NM 1995 7 14 DL72W952965 119950706A5754 SKIN BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 6 SLAT SKIN CRACKED AT TAB FOR INBD TRACK FAIRING ATTACH. INSTALLED REPAIR PER MM 57-54-0, PG 820/821. FOUND AT HMV. 2L73 4F A3WE 19950714002061995071400206NM 1995 7 14 DL72W952976 119950620A5754 RIB BOEING727 727247 138408FNM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 5 SLAT CRACKED AT LOWER END OF AFT FLANGE ON RIB 19. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER PER MM 57-54-0, PG 818 AND PG 819. FOUND AT HMV. 2L73 4F A3WE 19950714002071995071400207NM 1995 7 14 DL72W952977 119950621A5754 RIB BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 7 SLAT CRACK IN LOWER END OF AFT FLANGE ON SLAT RIB 6 FROM INBD END. INSTALLED REPAIR DOUBLERS PER MM 57-54-0. FOUND AT HMV. 2L73 4F A3WE 19950714002081995071400208NM 1995 7 14 DL72W952983 119950619A5330 SKIN BOEING727 727247 138408FNM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, SKIN CORRODED BELOW LEVELING COMPOUND OB OF STR 28R FWD OF STA 1050. REPAIRED PER SRM 53-10-3, FIG 3. 2L73 4F A3WE 19950714002091995071400209NM 1995 7 14 DL72W952998 119950620A5754 ANGLE BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND NR 7 SLAT ANGLE CRACKED ON LWR TE IB OF TRACK. FABRICATED AND INSTALLED NEW ANGLE PER MM 57-54-0, PG 812. 2L73 4F A3WE 19950714002101995071400210NM 1995 7 14 DL72W952999 119950620A5754 RIBS BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND NR 6 SLAT RIBS 8, 9, 11, 14, 15, 18, 19 CRACKED. INSTALLED REPAIRS ON ALL RIBS PER MM 57-54-0, FIG 814. 2L73 4F A3WE 19950714002111995071400211NM 1995 7 14 DL72W953000 119950707A5754 ANGLE BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND NR 4 SLAT ATTACH ANGLE ABOVE NR 13 RIB CRACKED. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, PG 807. 2L73 4F A3WE 19950714002121995071400212NM 1995 7 14 DL72W953001 119950707A5754 SKIN BOEING727 727247 138408FNM NR 4 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND NR 4 SLAT INNER ANTI-ICE SKIN BETWEEN NR 12, NR 13 RIBS HAS HOLE. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, FIG 803A. 2L73 4F A3WE 19950714002131995071400213NM 1995 7 14 DL72W953006 119950708A5754 RIB BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 ITEM: NR 6 SLAT RIB CRACKED AT RIVET FWD FLANGE OF RIB NR 7. CORRECTION: REPAIRED PER S.R.M. 57-50-03, FIG 09. DAMAGE FOUND AT HMV. 2L73 4F A3WE 19950714002141995071400214NM 1995 7 14 DL72W953009 119950702A2910000AE954D0157 HYD HOSE BOEING727 727247 138408FNM LT ELEVATOR LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11297WA 22534 ON GEAR RETRACTION, HAD LOSS OF A-SYSTEM HYD QTY AND PRESS. RETURNED SLC. FOUND LINE TO LEFT ELEVATOR ACTUATOR CRACKED. REPLACED LINE, OPERATION NORMAL. 2L73 4F A3WE 19950714002151995071400215NM 1995 7 14 DL73S952987 119950707A5320 ANGLE BOEING737 737232 1384475NM FWD LAV CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11323DL 23095 FWD LAV SERVICE PANEL, CORROSION AROUND THE DUMP CHUTE DUCT CONNECTION. FABRICATED PARTS PER SRM 51-00, PG 1. FOUND AT LETTER CHECK. 2L72 4F RTA16WE 19950714002161995071400216NM 1995 7 14 DL757952951 119950507A7110314N301016B NOSE COWL BOEING757 757232 1384965NM RT WING PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11613DL 22820 COWL WAS DAMAGED IN STORES, .50 INCH PUNCTURE IN OUTER SKIN AT CENTER OF PANEL AND IN THE 9 O'CLOCK POSITION. THE COWL WAS REPAIRED USING 9390 RESIN. SYSTEM APPROX SIZE OF REPAIR IS 4 INCHES, USING 2 REPAIR PLIES FOR EVERY DAMAGED PLY PER SRM 51-70-17. 2L72 4F RTA2NM 19950714002171995071400217NM 1995 7 14 DL757952952 119950625A5414 SKIN BOEING757 757232 1384965NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 AT HMV, NR 1 ENGINE PYLON NACELLE/STRUT SKIN O/B SKIN NAC. STA. 107 HAD TIME LIMITED REPAIR FOR CRACK IN LIGHTENING HOLE. ACCOMPLISHED PERMANENT REPAIRS PER DL ERA 259151-14. 2L72 4F RTA2NM 19950714002181995071400218NM 1995 7 14 DL757952958 119950628A5730 FUEL TANK PLATES BOEING757 757232 1384965NM LEFT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 AT HMV IN ATL, INSPECTION FOUND THE FOLLOWING FUEL TANK PLATES TO HAVE CORROSION ON THE MATING SURFACE: 541KB, 541MB, 542BB, AND 542CB. REMOVED CORROSION PER SRM 57-20-01, REPAIRED PER SRM 57-20-01, FIG 205. 2L72 4F RTA2NM 19950714002191995071400219NM 1995 7 14 DL757952959 119950628A5730 FUEL TANK PLATES BOEING757 757232 1384965NM RT WING CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 DURING HMV IN ATL, INSPECTION FOUND THE FOLLOWING FUEL TANK PLATES TO HAVE LIGHT CORROSION ON THE MATING SURFACE: 641CB, 641JB, 642CB, 643CB. REMOVED CORROSION AND ROTOPEENED PER PS 900-4 NR 5, AND SRM 57-2-01, FIG 205. 2L72 4F RTA2NM 19950714002201995071400220NM 1995 7 14 DL757952964 119950622A5755113N420032 SKIN BOEING757 757232 1384965NM SPOILERS HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11657DL 24419 AT LETTER CHECK, FOUND SPOILER PANEL WITH PUNCTURE AT 53 INCHES FROM LEFT EDGE AND 13 INCHES FROM AFT EDGE OF PANEL AND TWO CRACKS IN LOWER SURFACE SKIN AT 14 INCHES FROM IB END. REPAIRED ALL DAMAGE PER SRM 57-70-01 WITH REF TO SRM 51-70-17. 2L72 4F RTA2NM 19950714002211995071400221NM 1995 7 14 DL757952978 119950707A575411404005158 SKIN BOEING757 757232 1384965NM NR 7 LE SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 AT HMV, NR 7 L/E SLAT WAS FOUND WITH HAIL DAMAGE TO UPPER SKIN. REPAIRED PER SRM 57-43-02. 2L72 4F RTA2NM 19950714002221995071400222NM 1995 7 14 DL757952985 119950708A5754114N4004146 SKIN BOEING757 757232 1384965NM NR 8 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 AT HMV, FOUND NR 8 L/E SLAT WITH TIME LIMITED REPAIRS DUE TO HAIL DAMAGE. COMPLETED PERMANENT REPAIRS PER SRM 57-43-02. 2L72 4F RTA2NM 19950714002231995071400223NM 1995 7 14 DL757952988 119950706A2131 PRESS CONTROLLER 21173885 BOEING757 757232 1384965NM CABIN MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11632DL 33445 23613 LOG ITEM-CABIN PRESS EICAS MSG RED AND CABIN WARN SOUNDED AT FL 330. EMERG DESCENT ACCOMPLISHED. MANUAL CONT WORKS OK. STATUS MSG CABIN ALT AUTO 1 AND CABIN ALT AUTO 2 CAME ON IN FLT. CORRECTIVE ACTION-NR 1 CONTROLLER FAULTS CONTROLLER AND LOW INFLOW. NR 2 CONTROLLER FAULTS LOW INFLOW. REPLACED NR 1 AND NR 2 CABIN PRESS CONTROLLERS. RPL COCKPIT PRESS AND IND WARN MODULE. PRESSURIZED A/C TO 6 PSI, A/C HELD PRESS. PERFORMED BITE TEST OF PRESS CONTROLLERS AND OPN CHECKED NORMAL PER M/M CONTROLLER REPLACEMENT. 2L72 4F RTA2NM 19950714002241995071400224NM 1995 7 14 DL767952940 119950705A2121 FAN 6066223 BOEING767 767232 1385132NM AC COMP FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11109DL 55670 22221 ON APPROACH, THE LT RECIRC FAN EICAS MSG CAME ON WITH SOME SMOKE IN THE CABIN. AFTER TURNING THE FAN OFF, THE SMOKE DISSIPATED. FWD TO MCO AND PLAC PER MEL 21-25-01A. FAN WAS REPLACED, OPERATION NORMAL. 2L72 4F RTA1NM 19950714002251995071400225WP 1995 7 14 DLL10953002 119950629A5312 BLKHD FRAME LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 AT B-LETTER CHECK, FOUND BULKHEAD FRAME CRACKED, AT FS 1363 HORZ LEG LT SIDE WL160. REPAIRED PER SRM 53-11-00, PG 932-933 2L73 4F A23WE 19950714002261995071400226WP 1995 7 14 DLL10953008 119950705A32301642699101 PIN LKHEED1011 10113851 5265010WP LT MLG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11735D 193C1226 DURING PRE-FLIGHT INSPECTION, FOUND LEFT MLG ACTUATOR LOWER LINK ATTACH FITTING PIN ASSEMBLY CRACKED. REPLACED SAME OPERATION NORMAL. 2L73 4F A23WE 19950714002271995071400227WP 1995 7 14 DLL13952966 119950703A5347 SEAT TRACK LKHEED1011 10113851 5265010WP BS 349 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SEAT TRACK CORRODED, STA 349. CLEANED CORROSION FOUND OUT OF LIMITS, INSTALLED NEW TRACK PER SRM 53-21-00, PG 836. 2L73 4F A23WE 19950714002281995071400228WP 1995 7 14 DLL13953003 119950609A5711 SPAR CAP LKHEED1011 10113851 5265010WP WS 580.6 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 CAP CRACKED IWS 580.6 FRT SPAR LWR CAP, AT RADIUS INSIDE TANK 4 OB RIB. ACCOMPLISHED REPAIRS PER SRM 57-11-00, FIG 807. 2L73 4F A23WE 19950714002291995071400229WP 1995 7 14 DLL13953007 119950703A5320 CLIP LKHEED1011 10113851 5265010WP BS 589 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FS 589 FRAME TO SKIN ATTACH CLIP CORRODED BETWEEN STRINGERS 34-36. REPAIRED PER SRM 53-12-00, FIG 817. 2L73 4F A23WE 19950714002301995071400230NM 1995 7 14 DLM88952945 119950705A5753 SKIN DOUG MD88 MD88 3023688NM RT TE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11947DL 49878 FOUND DURING F-2 LETTER CHECK - DENT FOUND ON UNDERSIDE OF I/B FLAP MEASURING APPROX .50 INCH DIA. REPAIRED PER SRM 57-03, FIG 7. 2L72 4F RTA6WE 19950714002311995071400231NM 1995 7 14 DLM88952962 119950706A5330 SKIN DOUG MD88 MD88 3023688NM AFT OF ENTRY DR SCRATCHED A DALAK NONE O OTHER ININSP/MAINT 1 SO11993DL 53345 FOUND DURING D-1 LETTER CHECK - MINOR SCRATCHES BELOW AND AFT OF ENTRY DOOR. DYE CHECKED AREA - BURNISHED - TREATED - AND TOUCHED UP PER SRM 53-04, FIG 38, I.D. AREA PER PS 900-5-1, NR 4 NO MRR. GT 595 07/10/95. 2L72 4F RTA6WE 19950714002321995071400232NM 1995 7 14 DLM88952963 119950707A52405914984 SKIN DOUG MD88 MD88 3023688NM RT SERVICE DOOR PUNCTURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11997DL 53364 SHOP INSPECTION FOUND INNER SKIN PUNCTURE ON FWD SERVICE DOOR. REPAIRED PER SRM 52-05, FIG 7. 2L72 4F RTA6WE 19950714002331995071400233NM 1995 7 14 DLM88952984 119950707A5320 ANGLE DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11918DE 49959 FOUND DURING B-1 LETTER CHECK - RT WHEELWELL AFT O/B STRIKER ANGLE CRACKED - REPAIRED PER SRM 53-05, FIG 81A. 2L72 4F RTA6WE 19950714002341995071400234NM 1995 7 14 UPS203776 119950707A5320 INTERCOSTAL BOEING727 72730C 1384009NM FS 240-250 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT B.S. 240-250, RT WL 185, RBL 42. REPAIRED IAW SRM 51-20-01, 20-43-03, 20-44-04, 51-30-2. 2L73 4F A3WE 19950714002351995071400235NM 1995 7 14 UPS203777 119950707A5311 FRAME BOEING727 72730C 1384009NM FS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FRAME AT STA 1130, STR 8-10, RT SIDE. REPAIRED IAW SRM 51-40-3, 53-10-1, 51-10-2, M/M 51-20-151. 2L73 4F A3WE 19950714002361995071400236NM 1995 7 14 UPS203778 119950707A5311 FRAME BOEING727 72730C 1384009NM FS 340 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK ON FLANGE OF FRAME AT BS 340, BETWEEN STR 11 AND STR 12R BEHIND SIDE WALL SUPPORT. REPAIRED IAW SRM 51-40-3, 51-10-2, 51-30-2. 2L73 4F A3WE 19950714002371995071400237 1995 7 14 UPS203779 419950707A2360 STATIC WICK BOEING727 72730C 1384009NM ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON ELEVATOR O/B STATIC WICK BASE. REPAIRED IAW SRM 55-20-3, M/M 51-20-21, 51-20-31, 51-20-13, 23-61-00. 2L73 4F A3WE 19950714002381995071400238NM 1995 7 14 UPS203780 119950707A57531510407 RETAINER BOEING727 72730C 1384009NM TE FLAPS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED L/W O/B MID-FLAP AFT LOWER CHORD AND ATTACHED BULB SEAL RETAINER 21 INCHES FROM O/B END. REPAIRED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950714002391995071400239NM 1995 7 14 UPS203781 119950707A5320651862526 ANGLE BOEING727 72730C 1384009NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AND SUPPORT ANGLE BETWEEN END FRAME AND NR 1 TRANSVERSE BEAM 15 INCHES FWD OF AFT EDGE. REPAIRED IAW SRM 53-10-1, 51-30-2, 51-10-6. 2L73 4F A3WE 19950714002401995071400240NM 1995 7 14 UPS203782 119950707A53131493521 STRINGER BOEING727 72730C 1384009NM BS 488 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON TOP STRINGER FLANGE AT BS 488, STR 24 LT WL 165. REPAIRED IAW SRM 53-10-3, 51-30-2, M/M 51-20-151. 2L73 4F A3WE 19950714002411995071400241NM 1995 7 14 UPS203783 119950707A532065184175 STIFFENER BOEING727 72730C 1384009NM BS 302 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER AT BS 302, WL 180, ON TOP OF PANEL OF NOSE GEAR WELL RBL 3. REPLACED IAW SRM 51-30-2, 51-30-5. 2L73 4F A3WE 19950714002421995071400242NM 1995 7 14 UPS203784 119950707A5330 WEB BOEING727 72730C 1384009NM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON TOP EDGE OF STA 870 WHEELWELL WEB RBL 0-65 WL 178. REPAIRED IAW SRM 53-10-9, 51-30-2. 2L73 4F A3WE 19950714002431995071400243NM 1995 7 14 UPS203785 119950707A5320651841566 STIFFENER BOEING727 72730C 1384009NM BS 320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STIFFENER ON SIDE PANEL OF NOSE GEAR WHEELWELL (INSIDE DOG HOUSE) BS 320, RBL 14, WL 182. REPLACED IAW SRM 51-10-1, 51-30-2, 51-20-4. 2L73 4F A3WE 19950714002441995071400244NM 1995 7 14 UPS203786 119950707A5315 FLOOR BEAM BOEING727 72730C 1384009NM BS 306-312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM BS 306-312 RBL 56, WL 208 AT FLOORBOARD FASTENER HOLES. REPAIRED IAW SRM 51-40-3. 2L73 4F A3WE 19950714002451995071400245NM 1995 7 14 UPS203787 119950707A5320651768527 WEB BOEING727 72730C 1384009NM BS 348-360 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK ON HORIZ. WEB BETWEEN FRAME AT 348 TO 360, LT WL 216. REPAIRED IAW SRM 51-10-07, M/M 51-20-151, SRM 51-40-2. 2L73 4F A3WE 19950714002461995071400246NM 1995 7 14 UPS203788 119950707A532065261731314 INTERCOSTAL BOEING727 72730C 1384009NM BS 304-344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON INTERCOSTAL STA 304-344, LBL 30, WL 208. REPAIRED IAW SRM 51-30-2, 53-10-1, 51-10-2, M/M 51-20-15. 2L73 4F A3WE 19950714002471995071400247NM 1995 7 14 UPS203789 119950707A5315 FLOOR BEAM BOEING727 72730C 1384009NM BS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON TOP FLANGE OF FLOOR BEAM STA 344, RBL 52 - LBL 46, WL 208. REPAIRED IAW SRM 51-30-2, 53-10-8, 51-10-6. 2L73 4F A3WE 19950714002481995071400248NM 1995 7 14 UPS203790 119950707A5330BAC1518338 SKIN BOEING727 72730C 1384009NM BS 420 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES STA 420, LBL 45 TO 62.5, WL 208. REPAIRED IAW SRM 53-10-8. 2L73 4F A3WE 19950714002491995071400249NM 1995 7 14 UPS203791 119950707A5543 TAB BOEING727 72730C 1384009NM RUDDER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION OF UPPER RUDDER TAB (SEVEN AREAS), CORE CONTAMINATED WITH WATER. REPAIRED IAW SRM 51-40-6, M/M 51-20-151. 2L73 4F A3WE 19950714002501995071400250NM 1995 7 14 UPS203792 119950707A5753 FOREFLAP BOEING727 72730C 1384009NM LT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION OF LT I/B FOREFLAP UNDER RUB STRIP ON I/B END. REPAIRED IAW M/M 51-51-11. 2L73 4F A3WE 19950714002511995071400251NM 1995 7 14 UPS203793 119950707A5520 STIFFENER BOEING727 72730C 1384009NM RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED LOWER SKIN STIFFENER ON RT ELEVATOR AT ELEV STA 17.2 INSIDE ACCESS PANEL 9406 APPROX 5.25 INCHES AFT OF FRONT SPAR CHORD. REPAIRED IAW SRM 51-20-2, 51-30-2, 51-20-1, 55-20-2. 2L73 4F A3WE 19950714002521995071400252NM 1995 7 14 UPS203794 119950707A5320654353132 CLIP BOEING727 72730C 1384009NM FS 1010 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED STRINGER CLIPS STA 1010 STR 6, 8 RT. REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 19950714002531995071400253NM 1995 7 14 UPS203795 119950707A532065453132 CLIP BOEING727 72730C 1384009NM BS 1070 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED STRINGER CLIPS STA 1070 STR 5, 8 RT. REPLACED IAW SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950714002541995071400254NM 1995 7 14 UPS203796 119950707A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 472-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORRODED SEAT TRACK STRAPS STA 472-480, LBL 45, WL 208. REPLACED IAW SRM 51-30-2, M/M 51-20-151. 2L73 4F A3WE 19950714002551995071400255NM 1995 7 14 UPS203797 119950707A5320 STUB BEAM BOEING727 72730C 1384009NM BS 762 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES ON STUB BEAM AT BS 762, LBL 55 UNDERSIDE WL 207. REPAIRED IAW SRM 51-40-4. 2L73 4F A3WE 19950714002561995071400256NM 1995 7 14 UPS203798 119950707A5320 BEAM BOEING727 72730C 1384009NM BS 760-850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, LBL 45, WL 208. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-10-2, M/M 51-20-00. 2L73 4F A3WE 19950714002571995071400257NM 1995 7 14 UPS203799 119950707A5320 BEAM BOEING727 72730C 1384009NM BS 760-850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, LBL 25, WL 208. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-10-2, M/M 51-20-00. 2L73 4F A3WE 19950714002581995071400258NM 1995 7 14 UPS203800 119950707A5320 BEAM BOEING727 72730C 1384009NM BS 760-850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND SEVERAL NUTPLATE HOLES ON UNDERSIDE LONGITUDINAL BEAM AT BS 760-850, RBL 45, WL 208. REPAIRED IAW SRM 51-10-1, 53-10-1, 53-10-2. 2L73 4F A3WE 19950714002591995071400259NM 1995 7 14 UPS203801 119950707A5315 FLOOR BEAM BOEING727 72730C 1384009NM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION FLOOR BEAM STA 680, RBL 37-60, WL 208 UPPER AND LOWER SIDE OF UPPER CHORD. 2L73 4F A3WE 19950714002601995071400260NM 1995 7 14 UPS203804 119950705A2910 HYD FLUID BOEING727 72722C 138400FNM A HYD SYST LOSS A IPXAO OTHER K FLUID LOSS CLCLIMB 1 SO01930UP 19096 AFTER TAKEOFF FROM VIE TO NUE DURING GEAR RETRACTION, THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO 1.8 GALLONS. A-SYSTEM LOSS CHECKLIST ACCOMPLISHED AND AFTER MANUAL GEAR EXTENSION, THE A-SYSTEM QUAN. RETURNED TO 3.4 GALS. UNEVENTFUL EMERGENCY LANDING PERFORMED IN NUE. SERVICED HYD SYSTEM BY 1.5 GALLONS, PRESSURIZED ALL HYD SYSTEMS AND ENGINES, RAN ALL HYD SYSTEMS, NOTHING FOUND ABNORMAL. 2L73 4F A3WE 19950714002611995071400261NM 1995 7 14 UPS403802 119950709A33501356B37 EEL BOEING747 747121 1384871NM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01682UP 20349 WHILE ON GROUND IN ONTARIO, MAINTENANCE FOUND L-1 ENTRY DOOR FWD EMERGENCY LIGHT INOP. REPLACED A ZONE EMERGENCY LIGHT ASSY, OPS CHECK GOOD. 2L74 4F A20WE 19950714002621995071400262WP 1995 7 14 UPS803769 119950707A53135750198 LONGERON DOUG DC8 DC871F 302199DWP BS 902 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 24L AT FS 902 FWD OF TRAPEZOID FITTING. REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19950714002631995071400263WP 1995 7 14 UPS803770 119950707A5320561214815 ANGLE DOUG DC8 DC871F 302199DWP BS 1810 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED CENTER SPAR/AFT SPAR ANGLE ON SLANTED BELT FRAME BETWEEN HORIZONTAL STAB AT F.S. 1810, BETWEEN LONGERONS 2L-2R. REPLACED IAW SRM 51-1-21. 2L74 4F RT4A25 19950714002641995071400264WP 1995 7 14 UPS803771 119950707A5312 BULKHEAD DOUG DC8 DC871F 302199DWP BS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED PRESSURE BULKHEAD ON LT SIDE TOP AT F.S. 683. REPAIRED IAW SRM 53-2-5. 2L74 4F RT4A25 19950714002651995071400265WP 1995 7 14 UPS803772 119950707A5522 SKIN DOUG DC8 DC871F 302199DWP RT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED RT ELEVATOR LOWER SURFACE AT AFT I/B TRAILING EDGE. REPLACED IAW M/M 27-30-00. 2L74 4F RT4A25 19950714002661995071400266WP 1995 7 14 UPS803773 119950707A532037577811 FITTING DOUG DC8 DC871F 302199DWP BS 1640-1660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 32R END FITTING AT F.S. 1640-1660. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950714002671995071400267WP 1995 7 14 UPS803774 119950707A532037577811 FITTING DOUG DC8 DC871F 302199DWP BS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED LONGERON 32R END FITTING AT F.S. 1690. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950714002681995071400268WP 1995 7 14 UPS803775 119950707A575556551681 SKIN DOUG DC8 DC871F 302199DWP NR 4 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DELAMINATED LT AND RT NR 4 SPOILER PANEL. REPLACED IAW M/M 27-01-01. 2L74 4F RT4A25 19950714002691995071400269WP 1995 7 14 UPS803803 119950709A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP FUSELAGE DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01804UP 46004 WHILE ON GROUND IN ONTARIO, MAINTENANCE FOUND BATTERY WOULD LIGHT EMERGENCY LIGHT FOR A FEW SECONDS THEN LIGHTS WOULD GO DEAD. REPLACED BATTERY PACK. 2L74 4F RT4A25 19950714002701995071400270WP 1995 7 14 UPS803805 119950706A57425753054502 FITTING DOUG DC8 DC873F 302199FWP NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 WHILE ON GROUND IN SDF, MAINTENANCE FOUND NR 3 PYLON FRONT SPAR SUPPORT FITTING CRACKED. MAINTENANCE REMOVED FOOTSTOOL FITTING AND INSTALLED NEW FOOTSTOOL IAW EO DC8-5710-4080D. 2L74 4F RT4A25 19950714002711995071400271WP 1995 7 14 95ZZZX3375 119950624A3241 CONNECTOR DOUG DC8 DC873F 302199FWP ANTI-SKID SYSTEMLOOSE A RRXAO OTHER O OTHER LDLANDING 1 WP15870TV 46086 KDAY/KFLL - FLT 032 - NO BRAKING ACTION ON LANDING WITH ANTI-SKID ON. MAINTENANCE RESECURED RECEPTACLE ON THE ANTI-SKID CONTROL BOX. BLED BRAKES, AND PERFORMED A REAR WHEEL SPIN-UP TEST IAW MM, CHAPTER 32-00. OPERATIONAL CHECKS OF THE ANTI-SKID AND MLG BRAKING SYSTEM WERE GOOD. (X) 2L74 4F RT4A25 19950714002721995071400272WP 1995 7 14 95ZZZX3376 119950610A783014650515 TR VALVE DOUG DC8 DC873F 302199FWP LT ENGINE WW LEAKING A RRXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP152674U 46062 MROC/KATL - FLT EB814 - DURING CLIMB, LOST HYDRAULIC FLUID AFTER UPLATCH CHECK DEPARTING MROC. ACCOMPLISHED EMERGENCY CHECK LIST AND PROCEDED TO KATL. EMERGENCY DECLARED AT KATL AND LANDED SUCCESSFULLY. MAINTENANCE ISOLATED FLUID LOSS TO THRUST REVERSER SOLENOID VALVE. REMOVED AND REPLACED SOLENOID VALVE. LEAK AND OPS CHECK GOOD. 2L74 4F RT4A25 19950714002731995071400273WP 1995 7 14 95ZZZX3377 119950613A323048023301 RETRACT PIN DOUG DC8 DC871F 302199DWP RT MLG SHEARED A ARRXACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP158076U 45941 KDAY/KRDU - FLT 028 - ON TAKEOFF ROLL AT KDAY, AIRCRAFT YAWED TO LEFT. ON GEAR RETRACTION, DOOR LIGHT AND LANDING GEAR UNSAFE LIGHT STAYED ON ALONG WITH RT ALT GEAR DOOR LIGHT. GEAR PLACED DOWN AND ALL INDICATIONS WERE NORMAL. RETURNED TO KDAY. MAINTENANCE FOUND RT MAIN GEAR RETRACT PIN SHEARED OFF STRUT. PREPARED ACFT TO FERRY FOR REPAIRS. SD 05-05-95 - ZANTOP MAINTENANCE REMOVED AND REPLACED RT RETRACT PIN AND REMOVED MINOR CORROSION FROM PIN BOSS IAW MM 32-30-0 AND EWA MAINTENANCE AUTHORIZATION (M.A.) A-3210-01:02. OPS CHECK GOOD. 2L74 4F RT4A25 19950714002741995071400274WP 1995 7 14 95ZZZX3378 119950614A275257726925011 ACTUATOR DOUG DC8 DC863 302198AWP RT TE MID-FLAP CORRODED A ARRXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP15797AL 46163 KSJC/KDAY - FLT 009 - DURING TAXI FOR DEPARTURE FROM KSJC, HAD FLAP ASSEMETRY INDICATION. CONFIRMED BY GROUND CREW OBSERVATION AT DEPARTURE END OF RUNWAY. RETURNED TO RAMP. MAINTENANCE FOUND EYEBOLT PULLED OUT FROM MID-FLAP ACTUATOR PISTON. REMOVED AND REPLACED ACTUATOR PER MM 27-51-0. GROUND CHECKS NORMAL. 2L74 4F 4A25 19950714002751995071400275NE 1995 7 14 95ZZZX3379 219950614A7200 ENGINE DOUG DC8 DC8F54 3021926WP PWA JT3D JT3D3B 52039NE NR 1 FIRE A ARRXAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 WP15992CF 45884 644597 KDAY/KBWI - FLT 114 - DURING DESCENT INTO KBWI, SHUT DOWN NR 1 ENGINE FOR FIRE WARNING. MAINTENANCE INSPECTED NR 1 ENGINE AND FOUND VARIOUS DAMAGE FROM POSSIBLE FIRE. THE AIRCRAFT WAS FERRIED TO GTC FOR REPAIRS AND ENGINE CHANGE. CURRENTLY UNDER INVESTIGATION. SUPPLEMENTAL REPORT WILL BE FILED UPON RECEIPT OF ADDITIONAL INFORMATION. 2L74 4F4 F 4A25 1E8 19950714002761995071400276WP 1995 7 14 95ZZZX3380 119950614A3260 INDICATOR LIGHT DOUG DC8 DC863 302198AWP GEAR DOORS MALFUNCTIONED A RRXAO OTHER N FALSE WARNING CLCLIMB 1 WP15797AL 46163 KDAY/KSJC - FLT 110 - RED DOOR NOT LATCHED LIGHT STAYED ON AFTER LANDING GEAR WAS RETRACTED. CYCLED THE GEAR AND LIGHT EXTINGUISHED. KSJC MAINTENANCE CHECKED DOOR LATCHES AND STRIKERS. CYCLED DOORS AND LATCHES INDICATION LIGHTS OPS CHECK NORMAL. 2L74 4F 4A25 19950714002771995071400277WP 1995 7 14 95ZZZX3381 119950612A282211230311 BOOST PUMP DOUG DC8 DC873F 302199FWP NR 4 ENGINE FAILED A SRAAO OTHER J WARNING INDICATION CRCRUISE 1 SO19873SJ 46091 FRANKFURT/BRUSSELS - FLT 193 - DURING FLIGHT, NR 4 ALTERNATE FUEL TANK WAS SELECTED APPROXIMATELY 2 MINUTES LATER. NR 4 ENGINE FLAMED OUT, RETURNED TO MAIN TANK AND ENGINE RE-LIGHTED. FOUND NR 3 ALTERNATE TANK FUEL BOOST PUMP FAILED. REPLACED PUMP, OPS CHECKED AND LEAK CHECKED GOOD. 2L74 4F RT4A25 19950714002781995071400278CE 1995 7 14 95ZZZX3382 119950613A575310116000144 END CAP BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07106YV 2553 547 UC106 DURING SCHEDULED MAINTENANCE, A CRACK OF .5 INCH WAS FOUND 30 INCHES INBOARD OF END CAP ON BOTTOM SIDE .5 INCHES FROM TRAILING EDGE AND A .375 INCH CRACK ON BOTTOM SIDE 46 INCHES FROM INBOARD END .5 INCH AFT OF LEADING EDGE. STOPPED DRILLED AND INSTALLED PATCH. 2L72 4T RTA24CE 19950714002791995071400279CE 1995 7 14 95ZZZX3383 119950613A575310116000144 END CAP BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV 1277 378 UC119 DURING SCHEDULED MAINTENANCE, A CRACK OF 1.5 INCHES WAS FOUND 4 INCHES INBOARD OF OUTBOARD END CAP 3 INCHES FROM TRAILING EDGE. STOPPED DRILLED AND INSTALLED DOUBLER. 2L72 4T RTA24CE 19950714002801995071400280NE 1995 7 14 95ZZZX3384 219950622A73217436025 FUEL CONTROL BOEING727 72751C 1384015NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE FAILED A RYNAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 CE07417EX 19290 LAX - NR 3 ENGINE WOULD NOT RESPOND TO THROTTLE ON APPROACH INTO LAX. MINIMUM FUEL FLOW 2500 POUNDS/HOUR WAS ALL IT WOULD PRODUCE, AT IDLE IT SPOOLED DOWN. IN-FLIGHT, ENGINE SHUT-DOWN PERFORMED; RYAN CHECKLIST AND PROCEDURES COMPLIED WITH. REMOVED AND REPLACED NR 3 ENGINE FUEL CONTROL UNIT AND FUEL PUMP. LEAK CHECKED GOOD. PERFORMED ENGINE RUN; ENGINE MEETS ALL PARAMETERS. 2L73 4F4 F A3WE E2EA 19950714002811995071400281WP 1995 7 14 95ZZZX3385 119950613A261130303A4 SMOKE DETECTOR DOUG DC8 DC863F 302198FWP CABIN INOP A ARWAO OTHER N FALSE WARNING CRCRUISE 1 SO19661AV 45969 LOG BOOK ITEM NR 6, LOG PAGE 63734. SMOKE DETECTOR LIGHT ON IN-FLIGHT AT 39,000, CABIN CLEAR. REMOVED AND REPLACED SMOKE DETECTOR CONTROLLER IAW MM 26-10-0. OPS NORMAL. 2L74 4F 4A25 19950714002821995071400282WP 1995 7 14 95ZZZX3386 219950620A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LEFT DEFECTIVE A AVNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07842JS 753 FLT 4141 - SHORTLY AFTER TAKEOFF, LT ENGINE LOST POWER, NO TORQUE OR OIL PRESSURE. CREW DECLARED AN EMERGENCY, RETURNED TO FIELD, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. INSPECTION OF LT ENGINE REVEALED A PROBLEM WITH ENGINE FUEL PUMP DRIVE. MAINTENANCE REMOVED AND REPLACED LT ENGINE IAW MM 72-00-00. CONDUCTED ENGINE GROUND RUNS IAW 72-00-00. OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19950714002831995071400283EU 1995 7 14 95ZZZX3387 119950615A3260622800200 UPLOCK SWITCH BAG JETSTMJETSTM3101 1500215EU NLG DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07854JS 735 FLT 4014 - AIRCRAFT RETURNED TO FIELD, NLG INTRANSIT LIGHT WOULD NOT EXTINGUISH. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT/MX REMOVED AND REPLACED NLG UPLOCK MICROSWITCH IAW MM 32-60-05. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950714002841995071400284SO 1995 7 14 C2XA95IA104 119950628A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING INSPECTION CHECK 6C, FOUND RT WING RIB NR 15 LOWER SURFACE SKIN SUPPORT CRACKED. CRACKED BRACKET IS NR 4 FROM FRONT OF RIB. REPLACED SKIN SUPPORT. WORK ACCOMPLISHED IAW AIRCRAFT MANUFACTURER SRM. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X) 2L72 4T RTA31SO 19950714002851995071400285SO 1995 7 14 C2XA95IA105 119950629A2730MS276434 BEARING EMB 120 EMB120RT SO RT ELEVATOR RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT ELEVATOR INBOARD PIVOT POINT BEARING RUSTED. MAINTENANCE REMOVED AND REPLACED THE BEARING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X) 2L72 4T RTA31SO 19950714002861995071400286SO 1995 7 14 C2XA95IA106 119950629A572012017056005 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 16 LOWER, NR 4 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X) 2L72 4T RTA31SO 19950714002871995071400287SO 1995 7 14 C2XA95IA107 119950629A572012017056021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 16 LOWER, NR 3 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT, 9,056.6. ACFT TOTAL CYCLES - 13,433. (X) 2L72 4T RTA31SO 19950714002881995071400288SO 1995 7 14 C2XA95IA108 119950629A572012017056009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB, NR 15 LOWER, NR 4 SKIN SUPPORT, CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9,056.6. ACFT TOTAL CYCLES - 13,433. (X) 2L72 4T RTA31SO 19950714002891995071400289EU 1995 7 14 RAIA950617 119950617A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03424TE14184 124 STL - PASSENGER DOOR EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED PASSENGER DOOR LIGHT ASSY. (X) 2H72 4T RTA53EU 19950714002901995071400290 1995 7 14 RAIA950618 419950619A34257003360944 AHRS AEROSPATR42 ATR42300 8680920EU AVIONICS FAULTY A RAIAD RETURN TO BLOCK O OTHER CRCRUISE 1 CE03424TE7396 6321 124 STL - FLT 7417 - CAPTAIN'S AHRS DATA INVALID. MAINTENANCE REPLACED CAPTAIN'S AHRS. (X) 2H72 4T RTA53EU 19950714002911995071400291EU 1995 7 14 RAIA950619 119950619A5270915E13 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENER DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE03338TE6951 932 STL - FLT 7417 - PASSENGER DOOR LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ADJUSTED PASSENGER DOOR MICROSWITCH. SYSTEM CHECK NORMAL. (X) 2L72 4T RTA56EU 19950714002921995071400292EU 1995 7 14 RAIA950620 119950616A3020991938943822 LINE BAG JETSTMJETSTM3201 1500217EU LT ENGINE CRACKED A RAIAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CE03342TE8295 954 STL - FLT 7506 - LEFT ENGINE FAILED TO MAKE TARGET TORQUE. MAINTENANCE REPLACED LT ENGINE INLET DE-ICE VALVE BLEED SUPPLY LINE. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714002931995071400293EU 1995 7 14 RAIA950621 119950616A32609EN1C11HB2BB2 SWITCH BAG JETSTMJETSTM3201 1500217EU LT MLG DIRTY A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03862AE8286 862 LAX - FLT 4774 - LEFT GEAR INTRANSIT LIGHT STAYED ILLUMINATED AFTER GEAR UP IN THE WELL. MAINTENANCE CLEANED GRIME FROM LEFT MAIN GEAR UPLOCK SWITCH. LUBED SWITCH, GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714002941995071400294GL 1995 7 14 RAIA950622 319950620A6111 PROPELLER BAG JETSTMJETSTM3201 1500217EU ROTOL R333 R333482F12 GL RT ENGINE OUT OF ADJUST A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03343TE8507 2673 955 DRG7859 STL - FLT 7071 - RT ENGINE DID NOT MAKE TORQUE. MAINTENANCE ADJUSTED RT PROPELLER BLADE ANGLE. GROUND RUNS GOOD. (X) 2L72 4T RTA56EU 6 CP61GL 19950714002951995071400295EU 1995 7 14 RAIA950623 119950620A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU ENGINES OUT OF ADJUST A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03343TE6052 955 STL- FLT 7513 - BOTH ENGINES FAILED TO ACHIEVE TARGET TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONERS. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714002961995071400296EU 1995 7 14 RAIA950624 119950620A5270915E13 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE03338TE6960 932 STL -FLT 7034 - PASSENEGR DOOR LIGHT ILLUMINATED IN-FLIGHT. MAINTENANCE ADJUSTED MICROSWITCH IN DOOR HANDLE PER J32 MM 527000. SYSTEM CHECK GOOD. (X) 2L72 4T RTA56EU 19950714002971995071400297EU 1995 7 14 RAIA950625 119950620A52101371027C5 ROD END BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03338TE6960 932 STL - FLT 7071 - PASSENGER DOOR LIGHT CAME ON IN-FLIGHT. MAINTENANCE ADJUSTED LOWER ROD END TO LIMITS. REPOSITIONED LOWER STRIKER MICROSWITCH. GROUND TEST OF SYSTEM REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714002981995071400298EU 1995 7 14 RAIA950626 119950620A32609EN1C11HB2BB2 UPLOCK SW BAG JETSTMJETSTM3201 1500217EU NLG DIRTY A RAIAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE03422AM9622 856 STL - FLT 7034 - NOSE GEAR RED LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE CLEANED NOSE GEAR UPLOCK SWITCH FROM GRIME. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714002991995071400299EU 1995 7 14 RAIA950627 119950618A3350 EEL BULBS BAG JETSTMJETSTM3201 1500217EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03433AM8939 885 STL - FRONT EMERGENCY LIGHT AND RT WINDOW EMERGENCY LIGHT INOP. MAINTENANCE RE-BULBED EMERGENCY LIGHTS. (X) 2L72 4T RTA56EU 19950714003001995071400300EU 1995 7 14 RAIA950628 119950618A33503011206 EEL SOCKET AEROSPATR72 ATR72202 8680940EU EXTERIOR OUT OF ADJUST A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE6780 283 STL - OUTSIDE EMERGENCY LIGHT BY THE SERVICE DOOR IS INOP. MAINTENANCE ADJUSTED EMERGENCY LIGHT SOCKET. (X) 2H72 4T RTA53EU 19950714003011995071400301NE 1995 7 14 SIMA951713 219950620A73217086M60G11 ECU 6053T88G01 SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE MALFUNCTIONED A ASIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21112AE3115 138 CADE5115 340A112 GEE367370 MQB - FLT 3944 - AIR TURN BACK - AFTER SETTING CTOT, THE LEFT ENGINE CONTINUED TO CLIMB TO 120 PERCENT PLUS TORQUE. CREW DEPARTED AND RETURNED TO MQB. AN OVERTORQUE INSPECTION WAS PERFORMED ALONG WITH A GROUND RUN IN WHICH THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS FERRIED TO LAW FOR AN OVERWEIGHT LANDING INSPECTION. THE ECU AND TORQUE/HP SENSOR, SN SIM2A385, WERE REPLACED AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA52EU E8NE6 19950714003021995071400302 1995 7 14 SIMA951722 419950621A3417102EU2EF ADC AEROSPATR72 ATR72212 EU NR 1 ENG FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW21369AT3198 19833E 369 DFW - FLT 3807 - AFTER TAKEOFF, LT ENGINE TORQUE SURGED 15 PERCENT. PILOTS RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RAI LT DAT SENSOR AND NR 1 ADC. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 3,520. (X) 2H72 4T RTA53EU 19950714003031995071400303EU 1995 7 14 SIMA951731 119950622A3230DHE1148 PROX SWITCH AEROSPATR72 ATR72212 EU NLG FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21349AT 2599 349 SHV - FLT 3800 - AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACTED POSITION. THE AIRCRAFT RETURNED TO SHV AND LANDED WITHOUT INCIDENT. THE LANDING GEAR EXTENSION/RETRACTION SYSTEM WAS DEFERRED PER THE MEL AND AIRCRAFT FLOWN TO DFW FOR REPAIR. DFW MTX RAI PROXIMITY SWITCH AND PERFORMED GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950714003041995071400304EU 1995 7 14 SIMA951761 119950625A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21423MQ 030 FRD - WHILE MAINTENANCE WAS PERFORMING A PS2 CHECK, FOUND PASSENGER/CREW DOOR EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW JIC 335124. OPS CHECK GOOD IAW JIC 335000. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950714003051995071400305 1995 7 14 SIMA951762 319950625A6140522792 INDICATOR SAAB SF340 SF340A 7850100EU RT ENGINE FAILED A SIMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW21107AE 128 340A107 DFW - FLT 3539 - DURING TAKEOFF, THE RIGHT ENGINE PROPELLER RPM INDICATOR DROPPED TO ZERO. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. THE INDICATOR WAS REPLACED WITH A SATISFACTORY GROUND RUN PERFORMED. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19950714003061995071400306EU 1995 7 14 VTZA95178 119950605A524014153133207 LAV SERVICE DOOR JETAIRJETSTMJETSTM4101 1500501EU FUSELAGE MISSING A VTZAO OTHER O OTHER ININSP/MAINT 1 EA27308UE 41023 LGA/IAD - FLT 6431 - DURING POST-FLIGHT WALK AROUND AT 1447 HRS ON 6-5-95, FLIGHT CREW DISCOVERED THE LAVATORY SERVICE DOOR WAS MISSING. MAINTENANCE OPENED DMI NR 02538 IAW CDL 52-40. MAINTENANCE LATER CLEARED DMI NR 02538 ON 6-8-95 BY REPLACING LAV SERVICE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950714003071995071400307EU 1995 7 14 VTZA95208 119950623A2751TY176004A POTENTIOMETER JETAIRJETSTMJETSTM4101 1500501EU RT TE FLAP FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27303UE 41015 JFK/IAD - FLT 6486 - DURING TAKEOFF AT 1600 HRS, ON 6-23-95, ABORTED TAKEOFF DUE TO THE FLAP POSITION INDICATOR SHOWS A RETRACTION OF SEVERAL DEGREES DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 06308 IAW MEL 27-7. MAINTENANCE LATER CLEARED DMI NR 06308 ON 6-26-95, BY REPLACING THE RT FLAP POSITION POTENTIOMETER. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950714003081995071400308EU 1995 7 14 VTZA95209 119950627A77228974763 EGT COMPENSATOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27487UE 906 IAD/BWI - FLT 6181 - DURING TAKEOFF AT 0650 HRS ON 6-27-95, ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT ENGINE EGT COMPENSATOR AND RECALIBRATED. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950714003091995071400309WP 1995 7 14 Y2PA95007 119950616A323039147385001 BUNGEE CYL DOUG DC9 DC915F 3022037WP NLG FAILED A Y2PAO OTHER J WARNING INDICATION APAPPROACH 1 GL23196US 47155 DTW/CLE - FLT AVR6023 - NOSE GEAR FAILED TO EXTEND ON APPROACH TO 'CLE'. RECYCLED THE GEAR AND RECEIVED A DOWN AND LOCKED INDICATION. LANDED WITHOUT FURTHER INCIDENT. FERRIED AIRCRAFT TO DTW FOR REPAIR (REF: USA JET FERRY FLIGHT AUTHORIZATION NR 95-002). PERFORMED RETRACTION TEST OF NOSE GEAR RETRACTION/EXTENSION SYSTEM, COULD NOT DUPLICATE MALFUNCTION. REPLACED NOSE GEAR UPLOCK RELEASE BUNGEE AS A PRECAUTION, SYSTEM OPERATIONALLY CHECKED GOOD. (X) 2L72 4F A6WE 19950714003101995071400310WP 1995 7 14 Y2PA95008 119950623A323059151695505 UPLATCH ASSY DOUG DC9 DC915F 3022037WP LT MLG BINDING A Y2PAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23197US 47154 YIP - FLT AVR6244 - LEFT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO YIP. DISASSEMBLED, CLEANED, AND LUBED LEFT MLG UPLATCH ASSY. OPERATIONALLY CHECKED GOOD. (X) 2L72 4F A6WE 19950714003111995071400311WP 1995 7 14 9510509942 119950528A5340 SKIN DOUG DC9 DC932 3022066WP SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING PERIODIC CHECK, FOUND A .1250 INCH CRACK IN THE UPPER AFT FUSELAGE SKIN AT THE SERVICE DOOR CUTOUT. REPAIRED PER EA 99-097386. 2L72 4F A6WE 19950714003121995071400312 1995 7 14 9510511156 419950614A3444 MOUNTING RINGS DOUG DC10 DC1040 3023508WP RADIO ALT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01156US 46765 DURING PERIODIC CHECK, FOUND CORROSION ON THE NR 1 AND NR 2 RADIO ALTIMETER ANTENNA MOUNTING RINGS. REPAIRED PER EA 11-98574. 2L73 4F A22WE 19950714003131995071400313WP 1995 7 14 9510529942 119950619A5713 LONGERON DOUG DC9 DC932 3022066WP WS 111/164 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING PERIODIC CHECK, FOUND CORROSION ON THE RIGHT WING STR 13-15 AND STR 18-22, XRS 58-69, AND ON THE RIB ATTACH FOOT FITTINGS BETWEEN STR 12-14, XRS 164, AND BETWEEN STR 18-20, XRS 111. REPAIRED ALL PER EA 99-97379. 2L72 4F A6WE 19950714003141995071400314WP 1995 7 14 9510539971 119950623A5220 DOOR PAN DOUG DC9 DC931 3022065WP EMERG EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND .50 INCH CRACK IN THE LEFT AFT OVERWING EMERGENCY EXIT DOOR PAN (P/N 5913195-1) AT THE UPPER FORWARD EDGE. REPAIRED PER EA 99-97092. 2L72 4F A6WE 19950714003151995071400315WP 1995 7 14 9510549942 119950623A5730 SKIN DOUG DC9 DC932 3022066WP WS 58/200 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING PERIODIC CHECK, FOUND CORROSION ON THE LEFT WING LOWER SKIN INTERIOR SURFACE XRS 58-XRS 200, STR 13-23. REPAIRED PER EA 99-100385. 2L72 4F A6WE 19950714003161995071400316WP 1995 7 14 9510559971 119950627A5412 BLKHD WEB DOUG DC9 DC931 3022065WP PYLON OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019335 47337 DURING H-CHECK, FOUND OIL CANNING IN BOTH THE LEFT AND RIGHT PYLON BULKHEAD WEB. REPAIRED WEB (P/N 9912243-81) PER EA 99-97094. 2L72 4F A6WE 19950714003171995071400317NM 1995 7 14 9510562286 119950627A5330 SKIN BOEING727 727251 138408HNM FS 450 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01286US 21325 DURING PERIODIC CHECK, FOUND CORROSION ON THE SKIN DOUBLER NEAR THE E/E COMPARTMENT ACCESS CUTOUT FS 450 BETWEEN STR 28L-28R. REPAIRED SKIN DOUBLER (P/N 65-18220-96) PER EA 22-98876. 2L73 4F A3WE 19950714003181995071400318WP 1995 7 14 9510579609 119950630A5320 FITTING DOUG DC9 DC932 3022066WP FS 937 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 26L ATTACH FITTING AT FS 937. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950714003191995071400319WP 1995 7 14 9510581224 119950630A5730 SKIN DOUG DC10 DC1030 3023501WP WS 948 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01224NW 46581 DURING L-CHECK, FOUND A CRACK, CORROSION, AND RIVETS PULLING THROUGH THE RIGHT WING OUTBOARD ISLAND PANEL (LOWER TRAILING EDGE) STA XC 948. REPAIRED SKIN DOUBLER AND T-ANGLE PER EA 12-98578. 2L73 4F A22WE 19950714003201995071400320NM 1995 7 14 9510592286 119950630A5313 LONGERON BOEING727 727251 138408HNM FS 950 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01286US 21325 DURING PERIODIC CHECK, FOUND CORROSION ON THE LOWER OUTBOARD FLANGE OF STR 29L AT BS 950E. REPAIRED STRINGER (P/N 65-56441-3) PER EA 22-98884. 2L73 4F A3WE 19950714003211995071400321NM 1995 7 14 9510602708 119950630A5311 FRAME BOEING727 727225 1384077NM FS 1303 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01817EA 22554 DURING PERIODIC CHECK, FOUND CRACKS IN THE BS 1303 FRAME WEB BETWEEN STR 8L-9L AND BETWEEN STR 8R-9R. REPAIRED FRAME (P/N 65-17506) PER EA 27-99049. 2L73 4F A3WE 19950714003221995071400322WP 1995 7 14 9510619997 119950701A5320 FITTING DOUG DC9 DC931 3022065WP FS 218 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A CRACK IN THE FS 218 INTERCOSTAL END FITTING BETWEEN LONGERONS 27R-28R. REPLACED END FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950714003231995071400323WP 1995 7 14 9510629997 119950703A5320 FITTING DOUG DC9 DC931 3022065WP FS 737-756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL BEAM (LONGERON 30) END FITTING AT FS 737-756. REPLACED FITTING PER SRM 51-30-1. 2L72 4F A6WE 19950714003241995071400324NM 1995 7 14 9510632708 119950703A5330 SKIN BOEING727 727225 1384077NM FS 683 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01817EA 22554 DURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE SKIN BS 683, STR 26L-STR 28L. REPAIRED SKIN (P/N 65-54590-6) PER EA 27-98880. 2L73 4F A3WE 19950714003251995071400325NM 1995 7 14 9510642286 119950705A5314 KEEL BEAM BOEING727 727251 138408HNM FS 950 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01286US 21325 DURING PERIODIC CHECK, FOUND A 1.50 INCH CRACK AND CORROSION ON THE KEEL BEAM CHORD STR 29R AT BS 950. REPAIRED CHORD (P/N 65-56441-4) PER EA 22-98879. 2L73 4F A3WE 19950714003261995071400326NM 1995 7 14 9510652286 119950706A5315 FLOOR BEAM BOEING727 727251 138408HNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01286US 21325 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM LOWER CHORD FROM LBL 35-RBL 35, FORWARD FLANGE. REPAIRED CHORD (P/N 65-20838-17) PER EA 22-98891. 2L73 4F A3WE 19950714003271995071400327NE 1995 7 14 9510669947 219950703A7321 FUEL CONTROL DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018938E 47161 657741 DURING CLIMBOUT, NR 1 ENGINE EPR AND FUEL FLOW INDICATORS WERE FLUCTUATING. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE, DRAINED THE F.C.U. MOISTURE TRAP, AND RAN THE ENGINE. NO ANOMALIES WERE NOTED. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENT SIMILAR PIREP RESULTED IN THE REPLACEMENT OF THE F.C.U. 2L72 4F4 F A6WE E2EA 19950714003281995071400328NE 1995 7 14 9510679951 219950704A7321 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D9 52048NE NR 1 ENGINE REQD SERVICE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL019347 45827 654648 NR 1 ENGINE EPR FLUCTUATED WHILE ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT 70 KTS, FLIGHT RETURNED TO THE GATE. MAINTENANCE DRAINED THE F.C.U. MOISTURE TRAP AND RAN THE ENGINE. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950714003291995071400329NM 1995 7 14 9510682289 119950705A7711LG80A6 EPR TRANSMITTER BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01289US5186 734 21377 695258 NR 2 EPR INDICATION DETERIORATED ON TAKEOFF. TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND PLACED THE NR 2 EPR SYSTEM ON M.E.L. AIRCRAFT CONTINUED IN SERVICE. THE EPR TRANSMITTER WAS SUBSEQUENTLY REPLACED. THE SYSTEM OPERATION RETURNED TO NORMAL. 2L73 4F4 F A3WE E2EA 19950714003301995071400330NM 1995 7 14 95UAL900036 119950710A3300 EEL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29653UA 25391 EEL LIGHT IN RIGHT AISLE OF FORWARD GALLEY INOP. REPLACED POWER STRIP CONNECTOR. 2L72 4F4 FRTA1NM E24NE 19950714003311995071400331SO 1995 7 14 COM11926 119950707A32463006031 WHEEL HALF BFGOODRICH 314461 EMB 120 EMB120RT SO LT OTBD MAIN CRACKED A COMAK NONE O OTHER UKUNKNOWN 1 SO01137H 11706339 1566 120137 WHEEL S/N 1566 WAS REMOVED FROM AIRCRAFT 1137 LEFT OUTBOARD GEAR, DUE TO THE TIRE BEING WORN TO LIMITS. WHEEL ASSY CAME THROUGH MCO TIRE SHOP. WHEEL WAS DUE EDDY CURRENT, UPON EDDY CURRENT ON WHEEL, FOUND A 2 INCH CRACK ON BEAD SEAT ON INNER WHEEL HALF. SENT WHEEL ASSY TO CVG TIRE SHOP FOR FURTHER INSPECTION. 2L72 4T RTA31SO 19950714003321995071400332SO 1995 7 14 COM11927 119950709A323112012347001 LATCH EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01269CA 120263 LEFT OUTBD MAIN LANDING GEAR DOOR OPENED IN FLIGHT. REPLACED DOOR LATCH ASSY. 2L72 4T RTA31SO 19950714003331995071400333SW 1995 7 14 COM20381 119950629A32469550624 WHEEL HALF LORAL 50073971B SWRNGNSA227 SA227AC 8780603SW RT OTBD MAIN CRACKED A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01702M 109761899 FEB88192 AC702 RAMP AGENT NOTICED A PART 0F THE OTBD WHEEL HALF CAME APART, WHILE THE AIRCRFT WAS TAXIING INTO GATE AREA. REMOVED WHEEL S/N FEB88-192 AND TOOK IT OUT OF SERVICE. SENT TO CVG WHEEL SHOP. 1L72 4T A8SW 19950714003341995071400334SW 1995 7 14 COM20382 119950710A53112623001025 FRAME SWRNGNSA227 SA227AC 8780603SW FS 512.81 BENT A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01703C 15253 AC703 THE FUSELAGE AFT FRAME AT FS 512.81 WAS DAMAGED BY GROUND EQUIPMENT BETWEEN STRINGERS 39 AND 40. A REPAIR DOUBLER WAS INSTALLED PER FAA APPROVED AERODESIGN REPORT NR 1574-1, DATED 7-8-95. 1L72 4T A8SW 19950714003351995071400335SW 1995 7 14 COM20383 119950710A53302723000013 SKIN SWRNGNSA227 SA227AC 8780603SW BS 473-512 DENTED A COMAK NONE O OTHER UKUNKNOWN 1 SO01703C 15253 AC703 THE FUSELAGE AFT LOWER SKIN WAS DENTED BY GROUND EQUIPMENT. THE DENT IS APPROXIMATELY ONE INCH WIDE AND RUNS FROM FS 473 TO FS 512 BETWEEN STRINGERS 39 AND 40. A REPAIR DOUBLER WAS INSTALLED PER FAA APPROVED AERODESIGN REPORT NR 1574-1, DATED 7-8-95. 1L72 4T A8SW 19950714003361995071400336EU 1995 7 14 COM31115 119950710A32465009237 RACE LORAL 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01370C 10161 DEC910119 340A010 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION, FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO A.B.S. FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950714003371995071400337EA 1995 7 14 COM60512 119950707A2932P9630111 TRANDUCER CNDAIRCL600 CL6002B19 EA NR 1 SYSTEM DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01916CA5456 7014 HYDRAULIC SYSTEM NR 1 INDICATES ZERO PSI. REPLACED THE PRESSURE TRANSDUCER. 2L72 4F RTA21EA 19950714003381995071400338EA 1995 7 14 COM60513 119950710A3230 RETRACT MECH CNDAIRCL600 CL6002B19 EA NLG LACK OF LUBE A COMAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01914CA 7012 NLG DID NOT DOWNLOCK ON FIRST ATTEMPT. CYCLED LANDING GEAR AND EXTENSION CYCLE WAS NORMAL. COULD NOT DUPLICATE. CLEANED AND LUBED NLG, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950714003391995071400339EA 1995 7 14 COM60514 119950709A2913601R751131 HYD PUMP CNDAIRCL600 CL6002B19 EA NR 1 SYST FAILED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01926CA3312 1307 7027 NR 1 HYDRAULIC SYSTEM HAS ZERO PRESSURE. REPLACED THE NR 1 HYDRAULIC PUMP. 2L72 4F RTA21EA 19950714003401995071400340EA 1995 7 14 COM60515 119950708A32465010571 WHEEL ASSY MICHEL 0334380 CNDAIRCL600 CL6002B19 EA LT MLG MISSING A ACOMAK NONE D INFLIGHT SEPARATION TOTAKEOFF 1 SO01915CA2347 117 7013 DURING POST-FLIGHT INSPECTION, FOUND LT INBD TIRE TO BE MISSING. TIRE AND DEMOUNTABLE FLANGE WERE FOUND IN OKC, WHERE IT EVIDENTLY DEPARTED AIRCRAFT DURING TAKE OFF. FAILURE LIKELY OCCURED BECAUSE TIRE WAS FLAT. 2L72 4F RTA21EA 19950714003411995071400341NE 1995 7 14 DHL95727002 219950711A7261334820 OIL CAP BOEING727 727228 NM PWA JT8 JT8D7 52053NE NR 2 ENGINE MISSING A TDHLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01727DH 20204 DURING CLIMB, NR 2 ENGINE OIL QTY DROPPED FROM 4 GALLONS TO 1.5 GALLONS WITH OIL TEMPERATURE CLIMBING. PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. INSTALLED CAP AND SERVICED OIL. 2L73 4F4 F A3WE E2EA 19950714003421995071400342NM 1995 7 14 SCNA95138 119950628A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM RT OVERWING DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 FOUND THE RIGHT WING EMERGENCY EXIT LIGHTS INOPERATIVE IN CABIN. REPLACED BATTERY PACK FOR RIGHT WING EMERGENCY EXIT LIGHTS. LIGHTS OPS CHECKED GOOD. 2L73 4F A3WE 19950714003431995071400343NM 1995 7 14 SCNA95139 119950701A25301439 OVEN BOEING727 727282 2F0R NM AFT GALLEY FAULTY A SCNAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15281SC 21949 AFT OVEN SWITCHED OFF WHILE COOKING MEALS, AFTER REMOVING MEALS, OVEN BEGAN TO SMOKE AND SMELL BURNED. REMOVED AND REPLACED OVEN AND UNIT CHECKED GOOD. 2L73 4F RTA3WE 19950714003441995071400344NM 1995 7 14 SCNA95140 119950702A4900GTCP8598CK APU BOEING727 7272A1 138407FNM AFT FUS FAILED A SCNAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15286SC 21601 WHILE AIRCRAFT WAS TAXIING, THE CABIN FILLED WITH SMOKE. MAINTENANCE FOUND THE APU INTERNALLY FAILED CAUSING SMOKE, IT WAS THEN INTRODUCED INTO THE CABIN THOUGH THE AIRCRAFT PACKS. THE APU WAS REMOVED AND REPLACED AND OPERATIONS CHECKED NORMAL. 2L73 4F A3WE 19950714003451995071400345WP 1995 7 14 SCNA95141 119950701A261172130000010 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP FWD GALLEY FAILED A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15573SC 46905 SMOKE DETECTOR ON FORWARD GALLEY BEEPS ONCE EVERY 10 MINUTES. TIGHTENED CANNON PLUG ON SMOKE DETECTOR AND DETECTOR CHECKED GOOD. 2L73 4F A22WE 19950714003461995071400346WP 1995 7 14 SCNA95142 119950702A261172130000010 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 4 LAV MALFUNCTIONED A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15573SC 46905 SMOKE DETECTOR IN THE NR FOUR LAVATORY WENT OFF FOR NO APPARENT REASON DURING FLIGHT. BLEW DUST OUT OF SMOKE DETECTOR AND UNIT TESTED GOOD. 2L73 4F A22WE 19950714003471995071400347NM 1995 7 14 SCNA95143 119950704A3350 EEL WIRE BOEING727 727259 138408JNM CABIN DAMAGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 FOUND THE AFT FLOOR TRACK LIGHTS INOPERATIVE. WIRES WERE FOUND DAMAGED; REPAIRED WIRES AND FLOOR TRACK LIGHTING SYSTEM TESTED GOOD. 2L73 4F A3WE 19950714003481995071400348NM 1995 7 14 SCNA95144 119950704A33501000677 EEL BOEING727 727259 138408JNM L1 DOOR INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 FOUND THE L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY SIGN OVER L1 DOOR, OPS TESTED GOOD PER B727 MM 33-50-101. 2L73 4F A3WE 19950714003491995071400349EU 1995 7 14 95ZZZX3388 119950623A242123079009 GENERATOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 CE03971JX8746 467 971 STL - FLT 4752 - RT GENERATOR FELL OFF LINE. MAINTENANCE REPLACED RT STARTER/GENERATOR. (X) 2L72 4T RTA56EU 19950714003501995071400350WP 1995 7 14 95ZZZX3389 119950620A3350 EEL WIRE DOUG DC9 DC932 3022066WP COCKPIT BROKEN A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11933VV 47489 EMERGENCY PATH LIGHTING WOULD NOT COME ON WITH COCKPIT SWITCH FOUND ON MAINTENANCE CHECK RON ATL. REPAIRED BROKEN WIRE FROM S1-177 TO S1-387. 2L72 4F A6WE 19950714003511995071400351NE 1995 7 14 95ZZZX3390 219950618A7200 ENGINE DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 1 FAILED A AAWRAE ENGINE SHUTDOWN M OVER TEMP CLCLIMB 1 WP25441J 45988 AFTER 27 MINUTES IN FLIGHT FROM SAN JUAN, PR, WITH DESTINATION MIAMI, FL, THE CREW DESCRIBED THE PROBLEM AS: IN CLIMB-OUT OF 10,000 FEET, GOT LOUD BANG AND ACFT YAW. NR 1 EPR DOWN AND EGT APPROACHING 600 CELSIUS. SHUT ENGINE DOWN AT 17037 AND RETURNED TO SJU. ACFT THREE ENGINE FERRIED TO MIAMI. NR 1 ENGINE REMOVED AND REPLACED. 2L74 4F4 F 4A25 1E8 19950714003521995071400352CE 1995 7 14 95ZZZX3391 119950626A2140320570 BUTT-SPLICE LEAR 35 35A 5170602CE CABIN HEAT SYS BURNED ASAROSAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW01135DE 667 LEAR JET WIRING MANUAL 21-42-00, PAGE 7, AUXILIARY CABIN HEAT SYSTEM. WIRE NR HC47A10T, A 10-GAUGE WIRE, IS BUTT-SPLICED TO A 16-GAUGE WIRE AT THE AUXILIARY HEAT RELAY PANEL. THE BUTT-SPLICE AND THE 16-GAUGE WIRE OVERHEATED CAUSING THE PLASTIC TO MELT ON THE SPLICE AND MAKES THE 16-GAUGE WIRE BROWN. THIS IS THE SECOND OCCURRENCE OF OVERHEATING AT THIS SPLICE. 2L72 4F A10CE 19950714003531995071400353 1995 7 14 95ZZZX3392 419950601A34256226342022 EFIS TUBE COLLINS SAAB SF340 340B 7860101EU COCKPIT SHORTED A NVEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO03198AE 340B198 ALB - FLT 4850 - SMOKE IN THE COCKPIT FROM EFIS TUBE. REPLACED THE RT PDU AND EFIS TUBE. 2L72 4T RTA52EU 19950714003541995071400354EU 1995 7 14 95ZZZX3393 119950620A3240AIR124470 SWIVEL 5012589 SAAB SF340 340B 7860101EU BRAKE HOUSING BROKEN A NVEAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO03204NE APR931065 340B204 MIA - FLT 5700 - WHILE TAXIING TO THE GATE, THE HYDRAULIC PRESSURE FELL TO ZERO AND HYDRAULIC FLUID WAS LOST. STOPPED THE ACFT AND CALLED FOR MAINTENANCE. MAINTENANCE TOWED ACFT INTO GATE AREA AND REPLACED THE BRAKE ASSEMBLY, WHEEL ASSEMBLY, BRAKE LINE, SWIVEL AND TIRE. 2L72 4T RTA52EU 19950714003551995071400355NE 1995 7 14 95ZZZX3394 219950617A72105074T51G10 GEARBOX SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE FAILED A NVEAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 SO03218AE 340B218 785304 LIT - FLT 7895 - RIGHT ENGINE PROPELLER RPM FLUCTUATED, THEN OIL PRESSURE ROSE TO 200 PSI. CREW SHUT DOWN RIGHT ENGINE. SAFELY DIVERTED TO LITTLE ROCK. DETERMINED RT GEARBOX HAD FAILED. COMPLIED WITH RIGHT ENGINE CHANGE. 2L72 4T4 TRTA52EU E8NE 19950714003561995071400356WP 1995 7 14 95ZZZX3395 119950605A5730 PLATING DOUG DC8 DC863F 302198FWP WS 257 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 ON A ROUTINE A-CHECK, MAINTENANCE FOUND LEVEL 3 CORROSION AT APPROXIMATELY L/E STA XFS 257 TOP SIDE, LEFT WING. REMOVED FASTENERS, CUT OUT AREAS OF CORROSION, FABRICATED AND INSTALLED DOUBLER FROM 7075-T6.090 AND 2 EACH FILLERS FROM 7075-T6. REPAIRED AND AREA TREATED, PRIMED, AND INSTALLED IAW DER DWG ARW 3216-16. 2L74 4F 4A25 19950714003571995071400357WP 1995 7 14 95ZZZX3396 119950605A5730 PLATING DOUG DC8 DC863F 302198FWP WS 207 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 ON A ROUTINE A-CHECK, MAINTENANCE FOUND .6250 INCH CRACK AT APPROXIMATELY L/E STATION XFS 207 TOP SIDE, LEFT WING. REMOVED FASTENERS, CUT OUT CRACKED AREA. FABRICATED AND INSTALLED DOUBLER FROM 7075-T6.071 AND FILLER FROM 7075T-6.063. INSTALLED, TREATED, PRIMED IAW SRM 51-1-8, 57-2-0. (X) 2L74 4F 4A25 19950714003581995071400358NM 1995 7 14 BJNA95501 119950517A3350 EEL BOEING737 737214 138446RNM RT EXTERIOR INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11457TM 20156 RIGHT AFT EXTERIOR EXIT LIGHT INOP. REPLACED LIGHT IAW 33-51-21. OPS CHECKED OK AT THIS TIME. (X) 2L72 4F A16WE 19950714003591995071400359WP 1995 7 14 CKSA95037 119950614A3231 RETRACT MECH DOUG DC8 DC861 3021952WP NLG DOORS MALFUNCTIONED A CKSAA UNSCHED LANDING O OTHER CLCLIMB 1 GL23816CK 45892 KBUF - FLT 64648 - AFTER TAKEOFF, LOUD NOISE WAS HEARD FROM NOSE GEAR. RECYCLED GEAR, NO CHANGE. RETURNED TO BUF. MAINTENANCE INSPECTED NOSE GEAR WHEELWELL DOORS. NO DEFECTS NOTED. RESET NOSE GEAR DOORS IAW MM CHAPTER 52. (X) 2L74 4F 4A25 19950714003601995071400360WP 1995 7 14 CKSA95038 119950620A2612 FIRE LOOP DOUG DC8 DC851 3021920WP NR 4 ENGINE LOOSE A CKSAO OTHER N FALSE WARNING ININSP/MAINT 1 GL23804CK52564 45689 KHUF - FIRE WARNING BELL AND LIGHT ON STARTING NR 4 ENGINE. SHUT DOWN AND DISCHARGED FIRE AGENT AS. SECURED LOOSE SECTION OF AFT FIRE LOOP, RAN ENGINE FOR SEVERAL MINUTES FOUND NO DEFECTS. NR 4 FIRE WARNING OPS CHECKS GOOD IAW DC-8 MM 26-2-0. REMOVED AND REPLACED NR 4 FIRE BOTTLE IAW DC-8 MM 26-4-1. (X) 2L74 4F 4A25 19950714003611995071400361EU 1995 7 14 RAIA950629 119950621A5280137414B418 DOOR BAG JETSTMJETSTM3201 1500217EU RT MLG CRACKED A RAIAO OTHER E VIBRATION/BUFFET CRCRUISE 1 CE03338TE6969 932 STL - FLT 7471 - VIBRATION IN-FLIGHT EVIDENCED BY CONTROL YOKE VIBRATING BADLY. MAINTENANCE DISCOVERED RT MAIN GEAR DOOR CRACKED. REPLACED RT GEAR DOOR. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714003621995071400362EU 1995 7 14 RAIA950630 119950622A3230DHE1148 SWITCH AEROSPATR72 ATR72202 8680940EU NLG FAULTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03721TE9229 217 STL - FLT 7130 - LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. MAINTENANCE REPLACED NOSE GEAR WEIGHT ON WHEEL PROXIMITY SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2H72 4T RTA53EU 19950714003631995071400363WP 1995 7 14 RAIA950632 219950623A75308961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03866AE7725 625 866 66119 SMF - FLT 4720 - RT ENGINE TARGET TORQUE SHY BY 70 PERCENT. MAINTENANCE REPLACED RT ENGINE P3 BLEED AIR GASKETS. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T4 TRTA56EU E4WE 19950714003641995071400364WP 1995 7 14 RAIA950635 219950625A732089778025 FUEL CONTROL 10922 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03338TE109224213 932 66083 STL - FLT 7039 - RT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED RIGGING ON RT FUEL CONTROL UNIT AND ADJUSTED RT EGT COMPENSATOR. (X) 2L72 4T4 TRTA56EU E4WE 19950714003651995071400365EU 1995 7 14 RAIA950639 119950626A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03342TE8844 4735 954 STL - FLT 7061 - RT ENGINE TORQUE LOW. ADJUSTED RT ENGINE, SIGNAL CONDITIONER SETTING PER GARRETT DSC. POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714003661995071400366NE 1995 7 14 UF6A950606 219950622A72613034778 OIL TUBE BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAILED A UF6AE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03851AW5429 2020 124459 SBN - FLT 5115 - RIGHT ENGINE LOW OIL PRESSURE LIGHT ON THE CWP ILLUMINATED IN-FLIGHT. FLIGHT CREW SHUT DOWN RIGHT ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL SCAVENGE LINE FRACTURED. MAINTENANCE REPLACED THE OIL SCAVENGE LINE. (X) 2L72 4T4 TRTA27NM E2ONE 19950714003671995071400367NE 1995 7 14 UF6A950607 219950624A7313310146901 O-RING BAG ATP ATP EU PWA PW120 PW126A NE RT ENGINE FAILED A AUF6AO OTHER X ENGINE FLAMEOUT APAPPROACH 1 CE03860AW391 2037 124400 ORD - FLT 5061 - NR 2 ENGINE TORQUE WOULD NOT MAKE POWER. ON APPROACH, ENGINE FLAMED OUT. MAINTENANCE REPLACED FUEL NOZZLE O-RING. OPS CHECK GOOD. (X) 2L72 4T4 TRTA27NM E2ONE 19950714003681995071400368NE 1995 7 14 UF6A950608 219950624A73213244841 MJC BAG ATP ATP EU PWA PW120 PW126A NE RT ENGINE FAULTY A UF6ACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03854AW3493 824 2028 124451 ORD - FLT 5108 - NR 2 ENGINE TORQUE DID NOT MAKE SETTING ON TAKEOFF. MAINTENANCE REPLACED THE FUEL CONTROL UNIT. (X) 2L72 4T4 TRTA27NM E2ONE 19950714003691995071400369EU 1995 7 14 UF6A950609 119950624A7931ATP7610001000W PRESS TRANSDUCER BAG ATP ATP EU RT ENGINE FAULTY A UF6AA UNSCHED LANDING O OTHER CLCLIMB 1 CE03851AW3532 2020 ORD - FLT 5009 - NR 2 ENGINE OIL PRESSURE FLUCTUATED ON CLIMB. MAINTENANCE REPLACED OIL PRESSURE TRANSDUCER. (X) 2L72 4T RTA27NM 19950714003701995071400370EU 1995 7 14 UF6A950610 119950625A61207863364 PCU BAG ATP ATP EU LT ENGINE FAULTY A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 CE03857AW6049 2034 ORD - FLT 5115 - LEFT PROPELLER WOULD NOT FEATHER ON ENGINE SHUT DOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK. OPS CHECK GOOD. (X) 2L72 4T RTA27NM 19950714003711995071400371 1995 7 14 UF6A950611 419950626A34254608001210 AHRS COMPUTER BAG ATP ATP EU AVIONICS COMPT FAILED A UF6AA UNSCHED LANDING O OTHER CRCRUISE 1 CE03853AW8596 0986 2022 ORD - FLT 5047 - WEATHER RADAR WENT INOPERABLE IN-FLIGHT. MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER. (X) 2L72 4T RTA27NM 19950714003721995071400372EU 1995 7 14 VTZA95207 119950623A243523095002 STARTER/GEN JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILURE A VTZAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 EA27311UE 41029 IAD/RDU - FLT 6573 - DURING CRUISE AT 1050 HRS ON 6-23-95, RETURNED TO IAD DUE TO LT ENGINE VIBRATION IN-FLIGHT WITH TORQUE. SETTING ABOVE 64 PERCENT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950714003731995071400373SO 1995 7 14 WTAA950222 119950627A361038E966A REGULATOR VALVE EMB 120 EMB120RT SO NR 2 DEICE SYS LEAKING GASKET A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17250YV 120250 FAT - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF AT APPROXIMATELY 4,000 FEET. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLEED AIR SYSTEM WITH NO EVIDENCE OF AIR LEAK NOTED. DEFERRED RIGHT ENGINE BLEED 'DUCT LEAK' LIGHT PER MEL 36-21-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE PREVIOUSLY DEFERRED ITEM WITH THE REPLACEMENT OF THE NR 2 DEICE SYSTEM PRESSURE REGULATOR VALVE. (X) 2L72 4T RTA31SO 19950714003741995071400374WP 1995 7 14 9505209909 119950707A2410696233B CSD DOUG DC9 DC931 3022065WP RT ENGINE UNDERSERVICED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01959N 47255 RIGHT CSD OIL PRESSURE LOW LIGHT ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 70 KNOTS AND RETURNED TO THE GATE. SERVICED THE RIGHT CSD TO PROPER LEVELS. OPERATIONAL CHECK OK ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950714003751995071400375WP 1995 7 14 9510699918 119950710A324695502673 WHEEL ASSEMBLY DOUG DC9 DC932 3022066WP LT MLG VIBRATING A NWAACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL01940N 20824170 47572 EXCESSIVE NOSE WHEEL VIBRATION ON TAKEOFF ROLL AT APPROXIMATELY 35 TO 40 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950714003761995071400376WP 1995 7 14 9510709150 119950707A5320 FITTING DOUG DC9 DC914 3022034WP FS 472 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND A 1 INCH CRACK IN THE LONGERON 27R END FITTING AT FS 472. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950714003771995071400377WP 1995 7 14 ABXA9500573 119950707A793141800044 TRANSMITTER DOUG DC8 DC861 3021952WP PWA JT3D JT3D7 52039NE NR 1 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23842AX 1602 46015 643160 ENROUTE TO ILN, NR 1 ENGINE OIL PRESSURE PEGGED TO THE HIGH SIDE. CREW SHUT DOWN ENGINE AS PRECAUTIONARY PROCEDURE. OIL PRESSURE STILL READ PEGGED HIGH. WITH ENGINE SHUT DOWN, OIL PRESSURE READ 100 PSI; SHUT DOWN FOR APPROXIMATELY 20 MINUTES. ALL OTHER INDICATIONS WERE NORMAL. REMOVED AND REPLACED THE NR 1 ENGINE OIL PRESSURE TRANSMITTER AND THE MAIN OIL SYSTEM FILTER. SYSTEM OPS CHECKED GOOD IAW DC 8 MM. 2L74 4F4 F 4A25 1E8 19950714003781995071400378WP 1995 7 14 ABXA9500574 119950710A278037155495501 PACKING DOUG DC8 DC861 3021952WP SLOT CONTL VLV LEAKING A ABXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23850AX 45894 ON CLIMB-OUT OF ONT, HYDRAULIC QUANTITY LOSS AND PRESSURE OF ZERO WAS INDICATED. RESERVOIR LOW PRESSURE LIGHT ILLUMINATED AT 6 GALLONS HYDRAULIC QUANTITY. REPACKED SLOT CONTROL VALVE. ALSO, REMOVED AND REPLACED NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS IAW DC 8 MM. 2L74 4F 4A25 19950714003791995071400379WP 1995 7 14 ABXA9500575 119950710A7931318100D1 OIL PRESS TRANS DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 3 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 GL23824AX3975 3975 46141 671308 ENROUTE TO DAL, NR 3 ENGINE OIL PRESSURE INCREASED 100 PSI DURING CRUISE. OIL QUANTITY AND TEMPERATURE REMAINED NORMAL. CREW SHUT DOWN ENGINE FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER. GROUND OPERATION AND LEAK CHECKED GOOD IAW DC 8 MM. 2L74 4F4 F 4A25 1E8 19950714003801995071400380WP 1995 7 14 ABXA9500576 119950706A53207921002 JAMB NIHON YS11 YS11A500 6310416WP CARGO DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23915AX39476 2062 DURING B-CHECK WHILE ACCOMPLISHING WORK CARD 14002, TWO CRACKS WERE FOUND IN THE RADIUS OF THE UPPER JAMB OF THE MAIN CARGO DOOR. REPAIRED I/A/W R.E.A. 1153-12032-MR. 2L72 4T A1PC 19950714003811995071400381NM 1995 7 14 DHL95741006 119950705A2150 PACK BOEING727 7272Q9 138448MNM RIGHT MALFUNCTIONED A TDHLAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO01741DH 21931 AT FL 240, LOWER AFT BODY OVERHEAT LIGHT CAME ON. REDUCED NR 2 THRUST TO IDLE. TEN MINUTES LATER WHEN RT PACK WAS TURNED OFF WITH NR 2 THRUST AT IDLE, LIGHT WENT OFF. OVERHEAT SMELL EVIDENT THROUGHOUT COCKPIT. RAN BOTH ENGINGES, CHECKED FOR LEAKS AT AFT STAIRWELL AND AFT BAGGAGE AREA. NO LEAKS FOUND. UNABLE TO DUPLICATE ON GROUND. RUN AT HIGH POWER. ALSO, CHECKED KEEL BEAM AREA. SUSPECT RT PACK CAUSING PROBLEM. DEF RT PACK PER MEL 21-1-5. 2L73 4F RTA3WE 19950714003821995071400382SW 1995 7 14 95ZZZM213 119950707A57402731B32004 ATTACH FITTINGS SWRNGNSA227 SA227AC 8780603SW LT WING WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT WING EXTENSION BOLT HOLES WORN. REPAIRS WERE COMPLETED BY REPLACING THE WING EXTENSION ATTACH FITTINGS AND HARDWARE IAW THE SRM 51-90-40. REFERENCE MALA954501. 1L72 4T A8SW 19950714003831995071400383SW 1995 7 14 95ZZZM214 119950607A52102724044010 FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THAT THE PASSENGER DOOR FRAME HAD CRACKS IN THE NUTPLATE AREA FOR THE DOOR HANDRAIL MOUNTS. COMPLETED REPAIR TO PASSENGER DOOR FRAME BY REPLACEMENT OF FOUR AFT LOWER CORNERS P/N 27-24044-009 AND 27-24044-010 IAW FAC SRM 51-00-00 PG 4 AND 51-40-01, 51-40-02 AND 51-30-04. REFERENCE NR MALA954492. 1L72 4T A8SW 19950714003841995071400384WP 1995 7 14 95ZZZM215 119950425A3350330015 CHARGER ASSY LKHEED1011 10113851 5265010WP CABIN EEL NOT CHARGING A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11181AT 193L1125 IND - EGRESS LIGHTS 1-10 BOTH SIDES, GO OUT AFTER ONE MINUTE. REPLACED FORWARD EGRESS CHARGER, OPS CHECK GOOD. 2L73 4F A23WE 19950714003851995071400385WP 1995 7 14 95ZZZM216 119950510A33503351100 BATTERY PACK LKHEED1011 10113851 5265010WP NR 1 DOOR EEL WEAK A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11197AT 006484 193P1082 BOS - LEFT NR 1 DOOR EGRESS 'EXIT' LIGHT WILL NOT TEST. REMOVED AND REPLACED LEFT NR 1 BATTERY PACK, OPS CHECK GOOD IAW MM CHAP 33. (M) 2L73 4F A23WE 19950714003871995071400387NM 1995 7 14 95ZZZM218 119950515A3340 SWITCH BOEING727 727227 1384078NM COCKPIT FAILED A AMTAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 GL11766AT 21999 MDW - SMOKE AND ELECTRICAL SMELL IN THE COCKPIT BELOW 10,000 FEET INTO MDW, COMING FROM OVERHEAD PANEL. FOUND RT RUNWAY TURNOFF SWITCH BAD SECURED WIRES. COLLAR CIRCUIT BREAKER SWITCH WAS REPLACED 5-10-95 SYSTEM OPS CEHCK GOOD. (M) 2L73 4F A3WE 19950714003881995071400388WP 1995 7 14 95ZZZM219 119950531A3231 RETRACT MECH DOUG DC8 DC871 302199AWP NLG DOOR MALFUNCTIONED A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP158087U 45977 FLT NR 127 - KIAH-KBRO - AFTER GEAR RETRACTION A STRONG VIBRATION WAS FELT IN THE NOSE GEAR AREA. RETURNED KIAH. MAINTENANCE FOUND THE RT NOSE GEAR DOOR OPEN. MAINTENANCE INSPECTED THE NOSE GEAR AND FOUND NO DEFECTS. THE NLG RETRACT SYSTEM OPERATED NORMALLY DURING OPERATIONAL CHECK. (M) 2L74 4F 4A25 19950714003891995071400389WP 1995 7 14 CAL950410 119950521A3397 WIRE DOUG DC9 DC932 3022066WP EEL CHARGING LOOSE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917557 47424 FLT NR 1781 - GSO - THE EMERGENCY CHARGING LIGHT AT FORWARD ENTRANCE WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND WIRE AT PIN 'B' OF EMERGENCY LIGHT PACK LOOSE. THE WIRE WAS REPAIRED IAW MM 33-52-0 AND OPERATION CHECKED GOOD. (M) 2L72 4F A6WE 19950714003901995071400390WP 1995 7 14 CAL950417 119950524A79317938314506 LINE DOUG DC9 DC982 3022082WP OIL PRESS CRACKED A CALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW0914839 49635 FLT NR 0478 - GSO - THE NR 1 ENGINE BEGAN TO LOSE OIL WHILE EN ROUTE FROM TPA TO CLE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OIL LINE FROM THE OIL PRESSURE TRANSMITTER CRACKED. THE OIL LINE TO THE TRANSMITTER WAS REMOVED AND REPLACED. LEAKS CHECKS WERE GOOD. (M) 2L72 4F A6WE 19950714003911995071400391NM 1995 7 14 CAL950423 119950521A575365799496 CARRIAGE SPINDLE BOEING737 737130 1384435NM RT O/B FLAP SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914209 19026 IAH - INSPECTION FOUND THE RIGHT OUTBOARD FLAP OUTBOARD CARRIAGE SPINDLE SHEARED AT FORWARD RETAINING NUT. THE CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2L72 4F A16WE 19950714003921995071400392WP 1995 7 14 CAL950430 119950530A3350 EEL BATT CHARGER DOUG DC9 DC982 3022082WP AFT CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914889 49118 FLT NR 1421 - EWR - WHEN EXTERNAL POWER WAS DISCONNECTED AT THE GATE, NONE OF THE OVERHEAD EMERGENCY LIGHTS BEHIND ROW 28 CAME ON. SOME BURNT OUT BULBS HAD TO BE REPLACED AND THE AFT BATTERY CHARGER WAS REMOVED AND REPLACED. OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19950714003931995071400393 1995 7 14 CAL950432 419950601A2210 AUTOPILOT BOEING757 757224 1384958NM RT SYSTEM MALFUNCTION A ACALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW0917104 27294 FLT NR 0124 - LAX - WHEN THE RIGHT AUTOPILOT WAS ENGAGED AT 1000 FEET ON DEPARTURE FROM SNA, THE NOSE PITCHED UP AND AIRCRAFT APPROACHED STALL. THE RIGHT AUTOPILOT WAS DISCONNECTED. THE FLAPS WOULD NOT MOVE FROM 20 DEGREE SETTING. THE AIRCRAFT WAS DIVERTED TO LAX WHERE IT LANDED WITHOUT INCIDENT. THE FLAPS AND SLATS WERE INSPECTED AND NO DEFECTS WERE FOUND. A BITE TEST WAS CONDUCTED WITH NO FAULTS FOUND. THE FLAPS WERE CYCLED AND OPERATION CHECKED NORMAL. MAINTENANCE WAS UNABLE TO FIND ANY DISCREPANCIES. THE FLIGHT DATA RECORDER WAS REMOVED FOR READOUT. (M) 2L72 4F RTA2NM 19950714003941995071400394WP 1995 7 14 CAL950433 119950602A79317938314501 OIL LINE DOUG DC9 DC982 3022082WP NR 1 ENGINE CRACKED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09819NY 49479 FLT NR 0133 - CLE - THE LEFT OIL STRAINER CLOG LIGHT CAME ON WHILE EN ROUTE FROM LGA TO IAH. THE FLIGHT WAS DIVERTED TO CLE. THE LIGHT WENT OUT DURING DESCENT AT LOW POWER, BUT CAME BACK ON DURING FINAL APPROACH. THE LEFT ENGINE OIL QUANTITY WAS SLOWLY DECREASING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE OIL PRESSURE SWITCH LINE CRACKED. THE OIL LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. (M) 2L72 4F A6WE 19950714003951995071400395WP 1995 7 14 CAL950434 119950602A4920 ENGINE GARRTT 3812761 DOUG DC9 DC981 3022081WP APU FLAMED OUT A CALAO OTHER O OTHER CRCRUISE 1 SW0916883 P172 48073 FLT NR 0692 - EWR - THE APU FLAMED OUT AT FL 290, OPERATION OF THE APU CHECKED GOOD AT ALL ALTITUDES BELOW FL 290. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE APU ON THE GROUND AND NO DEFECTS WERE NOTED. (M) 2L72 4F A6WE 19950714003961995071400396NM 1995 7 14 CAL950444 119950518A5315 FLOORBEAM BOEING737 737247 138448DNM BS 700-720 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424666439 20129 INSPECTION FOUND FLOORBEAM CRACKED IN THE WEB AT LOWER FASTENERS FROM BS 700-720. THE CRACK RAN THROUGH SEVERAL FASTENER HOLES FOR A TOTAL LENGTH OF NINE INCHES. A WEB AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW CONTINENTAL AIRLINES SA013-5710-01322 ILLUSTRATION (REF 5710-01322). (M) 2L72 4F A16WE 19950714003971995071400397WP 1995 7 14 CAL950445` 119950428A5320 ANGLE DOUG DC9 DC982 3022082WP FS 1474 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09478AC38725 48063 INSPECTION FOUND A 1.5 INCH CRACK IN THE RADIUS OF THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE AT FS 1474. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05. (M) 2L72 4F A6WE 19950714003981995071400398NM 1995 7 14 CAL950447 119950524A5312 CHORD BOEING727 727227 1384078NM BS 1176.9 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - THE MAIN CABIN BS 1183 BULKHEAD REINFORCEMENT CHORD AT BS 1176.9 AT RT CUSP TO AFT ENTRY DOOR CUTOUT HAD CORROSION AND BLUE WATER STAINS. THE REINFORCEMENT CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-1. (M) 2L73 4F A3WE 19950714003991995071400399NM 1995 7 14 CAL950448 119950524A5713 STRINGER BOEING727 727227 1384078NM WS 656.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GOS - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING UPPER STRINGER S10 AT WS 656.50. THE STRINGER WAS REPAIRED IAW EA 5762-01050. (M) 2L73 4F A3WE 19950714004001995071400400NM 1995 7 14 CAL950455 119950524A5720 ANGLE BOEING727 727227 1384078NM WS 119 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND A .5 INCH CRACK IN WEB LOWER ATTACH ANGLE OF RT WING LEADING EDGE CAVITY AT STATION 119. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. (M) 2L73 4F A3WE 19950714004011995071400401NM 1995 7 14 CAL950456 119950524A5753 WEB BOEING727 727227 1384078NM RT TE MID FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097075545708 21366 GSO - INSPECTION FOUND THE RT OUTBOARD MID-FLAP INBOARD END WEB CRACKED AT TWO PLACES. BOTH CRACKS WERE .5 INCH LONG. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M) 2L73 4F A3WE 19950714004021995071400402WP 1995 7 14 CAL950457 119950603A7931 OIL LINE DOUG DC9 DC982 3022082WP NR 1 ENGINE CRACKED A ACALAAEL UNSCHED LANDING ENGINE SHUTDOWN ABORTED APPROACH KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09819NY 49479 FLT NR 0424 - JFK - THE NR 1 ENGINE OIL QUANTITY BEGAN TO DROP IN FLIGHT WITH AN ASSOCIATED DROP IN PRESSURE. THE NR 1 ENGINE WAS SHUT DOWN. WHILE ON APPROACH TO EWR WINDSHEAR WAS ENCOUNTERED, APPROACH WAS ABORTED AND AIRCRAFT WAS DIVERTED TO JFK WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE OIL LINE TO DIFFERENTIAL PRESSURE SWITCH CRACKED. THE LINE WAS CAPPED OFF. A DECISION WAS MADE TO REPLACED THE NR 1 ENGINE AS A PRECAUTIONARY MEASURE DUE TO HISTORY OF OIL LOSS ON THIS ENGINE. (M) 2L72 4F A6WE 19950714004031995071400403WP 1995 7 14 CAL950462 119950606A2560 MEGAPHONE DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW09541NY 45793 FLT NR 1805 - CLE - THE FORWARD CABIN MEGAPHONE WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE FORWARD CABIN MEGAPHONE WAS REPLACED. (M) 2L72 4F A6WE 19950714004041995071400404NM 1995 7 14 CAL950463 119950607A3260 UPLOCK SENSOR BOEING737 737130 1384435NM RT MLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0914208 19025 FLT NR 9860 - CLE - THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE RT MLG UPLOCK SENSOR WAS REMOVED AND REPLACED. THE GEAR WAS SWUNG AND OPERATION AND INDICATIONS CHECKED GOOD. (M) 2L72 4F A16WE 19950714004051995071400405WP 1995 7 14 CAL950464 119950607A33506011779 EEL PWR SUPPLY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0972821 49481 FLT NR 0305 - EWR - BOTH OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE POWER SUPPLY WAS REPLACED AND OPERATION OF THE OVERWING EMERGENCY EXIT LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19950714004061995071400406NM 1995 7 14 CAL950465 119950607A3230106122629 SWITCH BOEING737 7373T0 1384582NM RT WHEEL WELL INOPERATIVE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0969333 23571 FLT NR 0608 - BOS - THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF AND WAS ACCOMPANIED BY AN INTERMITTENT WARNING HORN. OVERRIDE WAS EMPLOYED AND THE GEAR RETRACTED. THE AIRCRAFT RETURNED TO BASE THE DAY BEFORE FOR THE LANDING GEAR NOT RETRACTING, BUT TROUBLESHOOTING FOUND NO DEFECTS. MAINTENANCE FOUND THE S106 AIR SAFETY SWITCH AT FAULT. THE SWITCH WAS REPLACED. A LANDING GEAR HANDLE SOLENOID TEST WAS PERFORMED PER MM 32-31-31 AND OPERATION CHECKED GOOD. (M) 2L72 4F RTA16WE 19950714004071995071400407NM 1995 7 14 CAL950466 119950607A7722WL202EED4 EGT INDICATOR BOEING737 737524 1384721NM NR 1 ENGINE INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW09586063735 27319 FLT NR 1646 - DFW - THE NR 1 ENGINE OVERHEATED ACCOMPANIED BY ILLUMINATION OF RED LIGHT WHILE AT CRUISE. THE THROTTLE WAS REDUCED TO IDLE AND THE ENGINE SHUTDOWN MOMENTS LATER. THE AIRCRAFT WAS RETURNED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE BOROSCOPED THE NR 1 ENGINE AND INSPECTED THE EGT HARNESS WITH NO EVIDENCE OF HEAT OR OTHER DEFECTS FOUND. THE FUEL FILTER AND CHIP DETECTORS WERE FOUND CLEAN. THE NR 1 ENGINE EGT INDICATOR WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. BOTH ENGINES WERE RUN AT IDLE, PART, AND TAKEOFF POWER WITH EGT'S INDICATING WITHIN 15 DEGREES OF EACH OTHER. (M) 2L72 4F RTA16WE 19950714004081995071400408NM 1995 7 14 CAL950471 119950610A3260656021132 ACCESSORY UNIT BOEING727 727232 1384082NM RT MLG INOPERATIVE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW091678416088 20639 FLT NR 0551 - IAH - THE RT MLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED ON FINAL APPROACH TO IAH. CYCLING THE GEAR DID NOT HELP. THE GEAR WAS CYCLED AGAIN DURING A 'GO AROUND' AND THE RED LIGHT EXTINGUISHED. IN ADDITION, A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE LANDING GEAR ACCESSORY UNIT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2L73 4F A3WE 19950714004091995071400409WP 1995 7 14 CAL950472 119950609A2150 SEAL DOUG DC9 DC932 3022066WP HEAT EXCHANGER FAILED A CALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0914524 47539 FLT NR 1781 - GSO - THE CABIN BEGAN TO FILL WITH SMOKE DURING TAXI OUT FOR DEPARTURE. THE AIRCRAFT BEGAN A RETURN TO THE GATE AND WAS ACCOMPANIED BY EMERGENCY VEHICLES AS A PRECAUTIONARY MEASURE. NO EVIDENCE OF FIRE WAS OBSERVED. THE PASSENGERS WERE DEPLANED AT THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND OIL IN THE RIGHT WATER SEPARATOR BAG AND THE REAR SEAL ON SECONDARY HEAT EXCHANGER PROTRUDING. THE HEAT EXCHANGER SEAL WAS REINSTALLED AND BOTH THE LEFT AND RIGHT WATER SEPARATOR BAGS WERE REMOVED AND REPLACED. (M) 2L72 4F A6WE 19950714004101995071400410WP 1995 7 14 CAL950473 119950611A2910 O-RING DOUG DC9 DC982 3022082WP RT MLG WW LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914816 49370 FLT NR 0208 - MCO - THE RIGHT HYDRAULIC SYSTEM SHOWED A DECREASE IN QUANTITY FROM 17 QUARTS TO 3 QUARTS WHILE EN ROUTE FROM IAH TO MCO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE O-RING AT FITTING ON BRAKE CONTROL VALVE IN RT WHEEL WELL LEAKING. THE O-RING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD. (M) 2L72 4F A6WE 19950714004111995071400411WP 1995 7 14 CAL950475 119950611A24336RW176YN3 TRANSFORMER RECT DOUG DC9 DC931 3022065WP E/E COMPT INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914564 47490 FLT NR 1279 - IAH - THE NR 2 TRANSFORMER RECTIFIER FAILED ON ROTATION LEAVING IAH (NR 1 RIGHT TRANSFORMER RECTIFIER WAS ON PLACARD). THE DC BUS OFF LIGHT ILLUMINATED AND THE GROUND SERVICE BUS CONTROL BREAKER POPPED. DC BUS TIE WAS CLOSED AND DC BUS WAS RECOVERED. THE AIRCRAFT WAS RETURNED TO IAH. THE NR 1 RT TRANSFORMER RECTIFIER WAS REMOVED AND REPLACED. SYSTEM OPERATION CHECKED NORMAL ON ALL TRANSFORMER RECTIFIERS. MAINTENANCE COULD NOT DUPLICATE ORIGINAL PROBLEM WITH NR 2 RT TRANSFORMER. ALL SYSTEM OPERATION CHECKED NORMAL ON RT NR 2 TRANSFORMER RECTIFIER. 2L72 4F A6WE 19950714004121995071400412WP 1995 7 14 CAL950476 119950612A2910 O-RING DOUG DC9 DC982 3022082WP RT HYD SYST LEAKING A ACALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09478AC 48063 FLT NR 0436 - IAH - THE RT THRUST REVERSER ACCUMULATOR LIGHT ILLUMINATED WHILE AT CRUISE EN ROUTE FROM LAX TO SAT. THE LIGHT EXTINGUISHED AFTER PULLING CIRCUIT BREAKER AND TURNING OFF RIGHT SYSTEM, BUT REAPPEARED ABOUT TWO MINUTES LATER. SEVERAL MINUTES LATER THE RT HYDRAULIC SYSTEM QUANTITY WAS OBSERVED TO BE DROPPING. THE RT HYDRAULIC SYSTEM WAS TURNED OFF AND CREW ELECTED TO OVERFLY SAT FOR A LANDING AT IAH. THE AIRCRAFT LANDED SAFELY AT IAH. MAINTENANCE FOUND THE RT 'ACCUM LOW' PRESSURE SWITCH UNION O-RING LEAKING. THE O-RING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE NORMAL. (M) 2L72 4F A6WE 19950714004131995071400413SW 1995 7 14 MALA954490 119950607A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 332.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MECHANICS FOUND A .125 INCH CRACK AT RELIEF RADIUS IN LOWER BELT FRAME OF CONSTANT SECTION AT FS 332.27 RIGHT SIDE, P/N 27-22093-103. REPAIRED BY INSTALLING REPAIR DOUBLER IAW FAC SRM 53-90-20 REPAIR 319. (M) 1L72 4T A8SW 19950714004141995071400414SW 1995 7 14 MALA954492 119950607A5210272404402 FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THAT THE PASSENGER DOOR FRAME HAD CRACKS IN THE NUTPLATE AREA FOR THE DOOR HANDRAIL MOUNTS. COMPLETED REPAIR TO PASSENGER DOOR FRAME BY REPLACEMENT OF FOUR AFT LOWER CORNERS P/N 27-24044-009 AND 27-24044-010 IAW FAC SRM 51-00-00 PG 4 AND 51-40-01, 51-40-02 AND 51-30-04. 95ZZZM214. 1L72 4T A8SW 19950714004151995071400415SW 1995 7 14 MALA954494 119950607A5712 RIB SWRNGNSA227 SA227AC 8780603SW WS 99.51 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CRACK ON RT WING RIB, OUTBOARD OF FLAP CENTER HINGE, WS 99.510. COMPLETED REPAIR TO WING TRAILING EDGE RIB STATION 98.38 BY BLENDING OUT DAMAGE. INSTALLED REPAIR DOUBLER P/N 27-31086-022. ALSO, INSTALLED DOUBLER ONTO RIB P/N 27-31085-024, IAW 57-90-10 FAC SRM AND FAC DRAWING 27C36075. (M) 1L72 4T A8SW 19950714004161995071400416SW 1995 7 14 MALA954501 119950707A57402731B32003 ATTACH FITTINGS SWRNGNSA227 SA227AC 8780603SW LT WING WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT WING EXTENSION BOLT HOLES WORN. REPAIRS WERE COMPLETED BY REPLACING THE WING EXTENSION ATTACH FITTINGS AND HARDWARE IAW THE SRM 51-90-40. REFERENCE 95ZZZM213. 1L72 4T A8SW 19950714004171995071400417NM 1995 7 14 TWRA9532 119950607A21507192233 TURBINE BYPASS BOEING747 747212B 1384886NM NR 2 PACK FAILED A TWRAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA156186 21439 DURING CRUISE, CABIN FILLED WITH SMOKE ON FLIGHT FROM HLP TO JED, SHUT DOWN NR 2 PACK. REPLACED NR 2 TURBINE BYPASS UNIT, OPS CHECK OK. (M) 2L74 4F A20WE 19950714004181995071400418SW 1995 7 14 TWRA954493 119950607A5400 STRUCTURE SWRNGNSA227 SA227AC 8780603SW RT NACELLE DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15446MA AC693 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND RT NACELLE INBOARD LOWER FORMER, NS 99.79, CRACKED AT LOWER KEELSON ATTACH FLANGE. COMPLETED REPAIRS TO RT NACELLE. REPLACED SKIN P/N 27-35112-2-03, ANGLE 27-31128-016, FORMER 27-35025-968. REPAIRED FORMER P/N 27-35043-010 AT NS 109.89, AND FORMER P/N 27-35023-025 AT NS 99.79 DUE TO CRACKS AT FLANGES. WORK DONE IAW FAC SRM 51-00-00 PG 4, 51-40-01, 51-30-04, 51-30-03, 51-90-02, FIG 2 PG 5, AND ARP 51-70-9132. REPLACED LOOSE FASTENERS IAW FAC 95-MALA-155 IN AREA OF DRAG BRACE BRACKET. (M) 1L72 4T A8SW 19950714004191995071400419EU 1995 7 14 VTZA95185 119950522A52701XE201 DOOR SWITCH JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY EXITS OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27312UE 41025 FLTN 6529 - IAD-JFK - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE EMERGENCY EXIT DOOR WARNING ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED ALL THREE OF THE EMERGENCY DOOR EXIT MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950714004201995071400420EU 1995 7 14 VTZA95186 119950521A2751TY176004A TRANSDUCERS JETAIRJETSTMJETSTM4101 1500501EU LT/RT FLAPS OUT OF ADJUST A VTZAD RETURN TO BLOCK N FALSE WARNING CRCRUISE 1 EA27319UE 41042 FLT NR 6345 - IAD-LGA - DURING THE CRUISE, RETURNED TO IAD DUE TO THE FLAP ASYMMETRY WARNING ILLUMINATING IN FLIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE LEFT AND RT FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950714004211995071400421NE 1995 7 14 95ZZZM220 219950607A73143017790010 FUEL PUMP BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE NR 1 ENG MALFUNCTIONED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28166AW 11090 23627 SNA-PHX - FLT 207 - AIRCRAFT VIBRATES EXCESSIVELY IN ALL FLIGHT REGIMENS EXCEPT WITH POWER BACK, DURING DESCENT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE MEC POWER AWA TASK CARD R8M73001. RIGGED PER AWA TASK CARD F8M75001 AND TESTED PER AWA TASK CARD F5M71001. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER AWA TASK CARD R8M73001 AND TESTED PER TASK CARD F5M71001. AIRCRAFT RELEASED FOR SERVICE. REFERENCE AWXA9500359. 2L72 4F4 FRTA16WE E2GL 19950714004221995071400422 1995 7 14 95ZZZM221 419950518A25624530150 ELT ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER UKUNKNOWN 1 EA01857CA UE71 ELT TRANSMITS CONTINUOUSLY. INVESTIGATION REVEALED THAT REMOTE SW WAS SHORTED DUE TO BEING WET. REMOVED AND REPLACED REMOTE SW P/N 118-34002-1 AND ELT BATTERY PACK P/N 452-0130. (M) 2L72 4T RTA24CE 19950714004231995071400423NE 1995 7 14 95ZZZM222 219950301A72403033351 VANE RING BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE LT ENGINE FAILED A ASVBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL2732SV BB865 PCE93644 ON CLIMB-OUT AT 16,000 FEET, A LOUD BANG WAS HEARD. AFTER THE LOUD BANG, THE LEFT ENGINE TEMPERATURE STARTED TO RISE AND THE ENGINE STARTED LOOSING POWER. THE ENGINE WAS THEN SHUTDOWN AND THE AIRCRAFT RETURNED FOR AN EMERGENCY LANDING WITHOUT FURTHER INCIDENT. ENGINE REMOVED AND SENT FOR OVERHAUL. UNITED TECH PRATT AND WHITNEY CANADA REPORTED CT VANE RING BURNED THROUGH POSSSIBLY DUE TO AN UNSATISFACTORY FUEL NOZZLE SPRAY PATTERN. 1L72 4T4 T A24CE E4EA 19950714004241995071400424SW 1995 7 14 95ZZZM223 119950610A32342719093005 SELECT LEVER SWRNGNSA227 SA227AC 8780603SW COCKPIT OUT OF POSITION A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA23361AE AC676 LANDING GEAR WOULD NOT RETRACT FULLY WHEN FLIGHT CREW SELECTED UP. GEAR WAS CYCLED DOWN AND AIRCRAFT RETURNED TO THE FIELD. INSPECTION FOUND THE EMERGENCY GEAR SELECT LEVER TO BE OUT OF THE NORMAL AND LOCKED POSITION. LEVER WAS RE-POSITIONED, GEAR SWING PERFORMED WITH ALL INDICATIONS NORMAL. (M) 1L72 4T A8SW 19950714004251995071400425SW 1995 7 14 95ZZZM224 119950610A2431P60014B TEMP SENSOR SWRNGNSA227 SA227AC 8780603SW BATTERY FAILED A CHQAO OTHER N FALSE WARNING ININSP/MAINT 1 EA2327330 AC756 AFTER ACCOMPLISHING A BATTERY START, THE RIGHT BATTERY HOT LIGHT ILLUMINATED. INSPECTION FOUND IT WAS AN INDICATION PROBLEM AND BATTERY WAS PLACED ON THE MEL. THE BATTERY WAS REMOVED AND REPLACED AND MEL CLEARED. INSPECTION FOUND THE BATTERY TEMP SENSOR FAULTY. SENSOR WAS REPLACED AND BATTERY WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19950714004261995071400426SW 1995 7 14 95ZZZM225 119950610A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A CHQAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA233115M AC588 RIGHT MAIN LANDING GEAR DOWN AND LOCKED, GEAR LIGHT WOULD NOT ILLUMINATE. FLIGHT CREW PERFORMED AN EMERGENCY EXTENSION, AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION FOUND INBOARD DOWN AND LOCK SWITCH INOPERATIVE. SWITCH WAS REPLACED, GEAR SWING PERFORMED WITH ALL INDICATIONS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19950714004271995071400427NE 1995 7 14 AWXA9500359 219950607A73218063208 MEC BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE NR 1 ENG MALFUNCTIONED A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28166AW WYG43871 23627 SNA-PHX - FLT 207 - AIRCRAFT VIBRATES EXCESSIVELY IN ALL FLIGHT REGIMENS EXCEPT WITH POWER BACK, DURING DESCENT. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE MEC POWER AWA TASK CARD R8M73001. RIGGED PER AWA TASK CARD F8M75001 AND TESTED PER AWA TASK CARD F5M71001. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER AWA TASK CARD R8M73001 AND TESTED PER TASK CARD F5M71001. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F4 FRTA16WE E2GL 19950714004281995071400428NM 1995 7 14 AWXA9500360 119950610A335058783 EEL CABLE ASSY BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 19 THROUGH ROW 22. REMOVED AND REPLACED CABLE ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950714004291995071400429NM 1995 7 14 AWXA9500378 119950614A3350 EEL ASSY BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMEREGNCY EXIT LIGHTS INOPERATIVE ROW 16 THROUGH ROW 21. RECONNECTED LIGHT ASSEMBLY AT ROW 21, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950714004301995071400430NM 1995 7 14 AWXA9500379 119950614A3350 EEL WIRING BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28164AW 23625 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 7 THROUGH 9 AND FROM ROW 17 BACK. RECONNECTED LOOSE WIRES, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950714004311995071400431 1995 7 14 AWXA9500381 419950616A3418861CA53 AOA SENSOR BOEING737 73733A 1384673NM LT COCKPIT BROKEN A AWXAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 WP28168AW 00636 23629 FLT 515 - PHX-OMA - ON CLIMB-OUT, THE STICK SHAKER ACTIVATED. PULLED AC STALL WARNING AND DC BREAKER TO SILENCE STICK SHAKER. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAINS SIDE AOA VANE PER MM 27-32-11, PG 401/405. SYSTEM OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950714004321995071400432NM 1995 7 14 AWXA9500382 119950616A5315 FLOORBEAM BOEING737 7373G7 1384595NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FLOORBEAM AT STATION 1016 LBL 20 CORRODED ON TOP FLANGE. REPAIRED BEAM IAW SRM 53-00-51, PAGE 202. (M) 2L72 4F RTA16WE 19950714004331995071400433NM 1995 7 14 AWXA9500383 119950616A532065C807351 THRESHOLD BOEING737 7373G7 1384595NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - DURING SCHEDULED C11 INSPECTION, FOUND R2 DOOR CHORD UPPER AND LOWER FLANGES CORRODED. REPLACED THRESHOLD CHORD IAW SRM 51-40-02 AND SRM 53-60-15. (M) 2L72 4F RTA16WE 19950714004341995071400434NM 1995 7 14 AWXA9500384 119950616A534765538446 FLOOR TRACK BOEING737 7373G7 1384595NM FS 787-802 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - DURING SCHEDULED C11 INSPECTION, FOUND AFT CARGO COMPARTMENT FLOOR TRACK CORRODED AT STATION 787 THROUGH STATION 802 S 26R. REPAIRED PER SRM 51-10-02, PAGE 16 AND SRM 53-00-53, PAGE 205. (M) 2L72 4F RTA16WE 19950714004351995071400435NM 1995 7 14 AWXA9500385 119950616A52306591700865 CORNER BOEING737 7373G7 1384595NM FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28151AW 23219 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FORWARD CARGO DOOR INSIDE CORNER OF AFT LOWER DOOR STOP CRACKED. REPLACED WITH NEW CORNER PER SRM 51-40-02. (M) 2L72 4F RTA16WE 19950714004361995071400436NM 1995 7 14 AWXA9500386 119950619A2120 CONNECTOR BOEING737 7373S3 1384711NM COOLING FAN DIRTY A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28313AW 23712 ABQ-PHX - FLT 475 - CREW REPORTED THE EQUIPMENT COOLING WAS INOPERATIVE AND ELECTED TO RETURN TO ABQ. CONTRACT MAINTENANCE FOUND EQUIPMENT COOLING NORMAL, THE SUPPLY FAN FAILED. AN UNMANNED STATION RELEASE WAS GIVEN AND THE AIRCRAFT RETURNED TO PHX. UPON ARRIVAL IN PHX, MAINTENANCE CLEANED THE CONNECTOR FOR EQUIPMENT COOLING NORMAL FAN. NO FURTHER DISCREPANCY NOTED. UNMANNED STATION RELEASE REMOVED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950714004371995071400437EU 1995 7 14 AWXA9500387 119950711A492038423201 BEARING GARRTT 38002783 AIRBUS320 A320231 3930325EU APU TURBINE FRACTURED A AWXAO OTHER AB FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP28620AW 93 R247C 052 LAS - FLT NR 100 - PHX-LAS - AT GATE AREA, RAMP PERSONNEL REPORTED SMOKE AND FLAMES FROM THE APU TAIL PIPE. APU WAS SHUT DOWN WITH REMOTE SWITCH. FIRE BOTTLES WERE NOT DISCHARGED. FIRE TRUCKS RESPONDED, BUT TOOK NO ACTION. SMOKE WAS REPORTED IN CABIN. NO FURTHER PROBLEMS NOTED. MAINTENANCE FOUND NO OIL SHOWING IN APU. APU WAS PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. APU REPLACED WITH SERVICEABLE UNIT. TEARDOWN REPORT OF APU REVEALED A TURBINE BEARING SEPARATOR FRACTURED. SUBMITTER STATES, THE SUSPECTED CAUSE OF BEARING FAILURE IS CONTAMINATION FROM THE BEARING CARRIER, P/N 38466121. (M) 2L72 4F RTA28NM 19950714004381995071400438EU 1995 7 14 SIMA951751 119950624A3233S5357840000151 ACT BRACKET AEROSPATR42 ATR42300 8680920EU RT MLG WW BROKEN A ASIMAO OTHER O OTHER APAPPROACH 1 SW21209AT 0209 MQT - AFTER LANDING AT ORD, THE PILOT REPORTED THE GEAR MADE A LOUD BANG NOISE WHEN IT WAS LOWERED. MAINTENANCE INSPECTED THE GEAR AND FOUND THE RIGHT GEAR ACTUATOR BRACKET LOWER BOLTS HAD SHEARED AND THE BRACKET WAS PULLED FROM THE FUSELAGE. THE GEAR WAS PINNED AND FERRIED TO MQT. MQT MAINTENANCE INSTALLED A NEW BRACKET AFTER SPOT FACING IAW SB ATR42-5300-0045. THE GEAR RETRACTION CHECK WAS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950714004391995071400439NM 1995 7 14 TSAA9553120 119950530A5330 SKIN BOEING737 737297 1384480NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION AROUND STATIC PORT AT AFT BELLY. REPAIRED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004401995071400440NM 1995 7 14 TSAA9553121 119950530A5330 SKIN BOEING737 737297 1384480NM FUSELAGE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND SKIN BULGING AT FORWARD BOTTOM CORNER AT OUTFLOW VALVE. REPAIRED PER ECO 2596. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004411995071400441NM 1995 7 14 TSAA9555122 119950530A5511 SPAR BOEING737 737297 1384480NM HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, DISCOVERED CORROSION ON LEFT HORIZONTAL STABILIZER, TOP FORWARD INBOARD SPAR. REPAIRED PER ECO 1889R2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004421995071400442NE 1995 7 14 USAA950536 219950529A7320 PT2 LINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D209 52053NE NR 2 ENGINE CRACKED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19809US 48041 MIA - FLT NR 1166 - THE EPR GAUGE FOR THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE FLIGHT DIVERTED TO MIA. REPLACED PT2 LINE AND TIGHTENED PT7 LINE. (M) 2L72 4F4 F A6WE E9NE 19950714004431995071400443WP 1995 7 14 USAA950539 119950530A2711 MIXER ASSY DOUG DC9 DC931 3022065WP FLT CONTROLS LACK OF LUBE A USAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 EA19996VJ 47335 PIT - FLIGHT 0856 - AIRCRAFT RETURNED TO PIT DUE TO THE LEFT AILERON BINDING. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE LUBED THE LATCHED CONTROL MIXER ASSEMBLY AND RECHECKED THE AILERON TAB DEFLECTION FORCE LEFT AND RIGHT WING. (M) 2L72 4F A6WE 19950714004441995071400444WP 1995 7 14 USAA950540 119950530A7910 OIL TANK ASSY DOUG DC9 DC931 3022065WP NR 2 ENGINE LEAKING A USAAO OTHER J WARNING INDICATION CRCRUISE 1 EA19933VJ 47216 DAY - FLT NR 0152 - FLIGHT DIVERTED TO DAY DUE TO THE NR 2 ENGINE OIL PRESSURE DECREASING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TANK DUE TO LEAKAGE. LEAK CHECKED GOOD. (M) 2L72 4F A6WE 19950714004451995071400445WP 1995 7 14 USAA950542 119950531A5210 TRIM DOUG DC9 DC931 3022065WP ENTRY DOOR LOOSE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19977VJ 48155 PIT - FLT 0728 - AFTER TAKEOFF, THE TOWER NOTICED A PIECE OF THE MED TRIM FLAPPING. FLIGHT RETURNED TO PIT. MAINTENANCE CUT THE LOOSE INTERIOR TRIM THAT WAS HANGING OUTSIDE OF THE DOOR. OPERATIONAL GOOD. (M) 2L72 4F A6WE 19950714004461995071400446WP 1995 7 14 USAA950545 119950529A3350 EEL WIRE DOUG DC9 DC931 3022065WP CABIN DAMAGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19978VJ 47371 CLT - FLT NR 1287 - THE EMERGENCY FLOOR PATH LIGHTING BETWEEN ROWS 6 AND 11 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A DAMAGED WIRE ON THE FLOOR TRACK LIGHT. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950714004471995071400447WP 1995 7 14 USAA950546 119950601A215020495052 TURBINE DOUG DC9 DC982 3022082WP LT PACK INOPERATIVE A USAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 EA19816US 48096 BWI - FLT 2101 - AT FL 370 - THE AIRCRAFT LOST THE RIGHT PACK. CREW DESCENDED TO FL 250. THE AIRCRAFT COULD NOT MAINTAIN CABIN ALTITUDE AND THE PRESSURIZATION WAS LOST. CREW MADE AN EMERGENCY DESCENT TO 10,000 FEET. THE CABIN ALTITUDE THEN ROSE TO 15,000 FEET AND THE PASSENGER OXYGEN MASKS DEPLOYED. THE AIRCRAFT LANDED IN BWI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT COOLING TURBINE. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950714004481995071400448WP 1995 7 14 USAA950547 119950601A3350 EEL DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19984VJ 47207 PHL - FLT 0059 - THE EMERGENCY LOW LEVEL LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHECKED THE OPERATION OF THE EMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT AND COCKPIT POSITIONS. OPERATIONS CHECKED NORMAL. (M) 2L72 4F A6WE 19950714004491995071400449WP 1995 7 14 USAA950549 119950607A5210 RAIN SEAL DOUG DC9 DC981 3022081WP MAIN DOOR UNSECURE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19805US 48053 PHL - FLT 1150 - CREW RETURNED TO PHL DUE TO A LOUD FLAPPING NOISE. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FUOND PART OF THE RAIN SEAL NOT SECURED. THEY REMOVED THE RAIN SEAL. AIRCRAFT CHECKED GOOD. (M) 2L72 4F A6WE 19950714004501995071400450WP 1995 7 14 USAA950550 119950607A323359370365501 CYLINDER DOUG DC9 DC982 3022082WP RT MLG LEAKING A USAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA19823US1706315044 00SP32 49142 PHL - FLT NR 1468 - PRIOR TO FLAP EXTENSION, THE RIGHT HYDRAULIC QUANTITY DROPPED TO TWO QUARTS. EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR LEAKING AT THE CYLINDER AND REPLACED THE CYLINDER. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950714004511995071400451EU 1995 7 14 USAA950575 119950608A4900740514C GCU FOKKERF28 F28MK0100 4990807EU APU FAILED A USAAA UNSCHED LANDING JN WARNING INDICATION FALSE WARNING CLCLIMB 1 EA19865US6730 673 11308 CLT - FLT 1170 - CAPTAIN ADVISED THAT THE APU GENERATOR WAS LOST AT APPROXIMATELY 40 MILES OUT OF CLT. FLIGHT RETURNED TO CLT. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. REPLACED GCU. (M) 2L72 4F RT 19950714004521995071400452EU 1995 7 14 USAA950579 119950505A5313 STRINGER FOKKERF28 F28MK0100 4990807EU BS 3870 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19897US5637 11392 PIT - DURING SCHEDULED INSPECTION USAIR PCI 289 CD 53F00762, FOUND A .5 INCH CRACK IN STRINGER 68 RT SIDE AFT OF FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 PER SRM 51-70-06. (M) 2L72 4F RT 19950714004531995071400453EU 1995 7 14 USAA950580 119950505A5313 STRINGER FOKKERF28 F28MK0100 4990807EU BS 3870 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19897US5637 11392 PIT - DURING SCHEDULED INSPECTION OF USAIR CD 53F00762 HFEC INSPECTION OF STRINGERS NR 6, 7, 68 AFT OF FRAME STATION 3870, FOUND .5 INCH CRACK (RADICAL) AT STRINGER NR 68 RT SIDE FRAME 3870. INSTALLED SPLICE REPAIR TO STRINGER 68 RT SIDE AFT OF FRAME STATION 3870 PER SRM 51-70-06. (M) 2L72 4F RT 19950714004541995071400454WP 1995 7 14 USAA950581 119950607A53135911415407 LONGERON DOUG DC9 DC931 3022065WP BS 756 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ65509 47188 IND - DURING BX CHECK VISIT AND SCHEDULED PRODUCTION CONTROL ITEM USAIR EO NR 5388D292F EDDY CURRENT INSPECTION OF EXTERNAL FUSELAGE SKIN FOUND A CRACK IN LONGERON NR 3R STATION 756. REMOVED CRACKED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER SRM 53-02 FIG NR 2. (M) 2L72 4F A6WE 19950714004551995071400455NM 1995 7 14 USAA950599 119950607A2130 CONNECTOR BOEING737 7374B7 1384702NM OUTFLOW VALVE LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19780AU 24997 CLT - FLT 263 - UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CANNON PLUG LOOSE ON THE OUTFLOW VALVE. CLEANED AND SECURED CANNON PLUG. (M) 2L72 4F RTA16WE 19950714004561995071400456EU 1995 7 14 USAA950600 119950611A3260 SENSOR FOKKERF28 F28MK0100 4990807EU LANDING GEAR INOPERATIVE A USAAO OTHER N FALSE WARNING APAPPROACH 1 EA19866US 11310 CAK - FLT 0237 - ON APPROACH, THE COMPUTER REPORTED ERRONEOUS GEAR NOT DOWN MESSAGES. A FLYBY WAS PERFORMED. THE CAPTAIN DECLARED AND EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE SENSOR. OPERATIONS CHECKED GOOD. (M) 2L72 4F RT 19950714004571995071400457EU 1995 7 14 USAA950601 119950711A5330 SKIN FOKKERF28 F28MK4000 4990810EU BS 3820 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19487US20640 11238 YYC - DURING FC-06 CHECK, FOUND 2MM TYPE 1 CRACK AT STATION 3820 STRINGER 2 SKIN. REMOVED FINGER STRIP PER REPAIR DOCUMENT SRM 53-02-18. (M) 2L72 4F RTA20EU 19950714004581995071400458NM 1995 7 14 TSAA5353106 119950601A5320 CHORD BOEING737 737297 1384480NM BS 178 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND RT SIDE OUTER CHORD CRACKED AT BS 178, FORWARD NOSE COMPARTMENT. REPAIRED PER SRM 53-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004591995071400459NM 1995 7 14 TSAA953099 119950601A5313 STRINGER BOEING737 737297 1384480NM BS 420 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FORWARD CARGO COMPARTMENT BS 420 AT STRINGER 27R CORROSION NOTED. REPAIRED PER SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004601995071400460NM 1995 7 14 TSAA9552092 119950601A5240 SKIN BOEING737 737297 1384480NM SERVICE DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND FORWARD SERVICE DOOR, BOTH UPPER AND LOWER DOOR HINGE CUT OUTS CRACKED. REPAIRED PER ECO 1904 PART II. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004611995071400461NM 1995 7 14 TSAA9553088 119950602A5313 STRINGER BOEING737 737297 1384480NM BS 970 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, CUT STRINGER 22R UPPER FLANGE INBOARD SIDE AT BS 970, FOR ACCESS TO CORROSION. REPAIRED PER ECO2596. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004621995071400462NM 1995 7 14 TSAA9553089 119950603A5313 STRINGER BOEING737 737297 1384480NM BS 970 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, NOTED EXFOLIATION ON STRINGER 25R AT BS 970. REPAIRED PER SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004631995071400463NM 1995 7 14 TSAA9553090 119950605A5312 BLKHD CHORD BOEING737 737297 1384480NM BS 178 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND BS 171 BULKHEAD RT CENTER CHORD CRACKED. REPAIRED PER ECO2518. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004641995071400464NM 1995 7 14 TSAA9553093 119950601A5330 SKIN BOEING737 737297 1384480NM BS 947 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FUSELAGE SKIN CRACK NOTED AT BS 947, STRINGER 23L. REPAIRED PER ECO2598. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004651995071400465NM 1995 7 14 TSAA9553097 119950601A5313 STRINGER BOEING737 737297 1384480NM BS 907 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, EXFOLIATION CORROSION AT BS 907, STRINGER 27R. REPAIRED EPR ECO2599. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004661995071400466NM 1995 7 14 TSAA9553098 119950601A5314 KEEL BEAM BOEING737 737297 1384480NM BS 520 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, EXFOLIATION CORROSION NOTED AT 520 LEFT KEEL BEAM. REPAIRED PER ECO2588. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004671995071400467NM 1995 7 14 TSAA9553101 119950601A5320 SUPPORT BEAM BOEING737 737297 1384480NM BS 685 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND SEAT TRACK SUPPORT BEAM CRACKED AT BS 685-7.0, BBL 0 PLUS 15.0L. REPAIRED PER ECO2299R2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004681995071400468NM 1995 7 14 TSAA9553103 119950601A5330 SKIN BOEING737 737297 1384480NM BS 1070 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FUSELAGE SKIN CRACK NOTED AT BS 1070 APPROXIMATELY 3.25 INCHES, FORWARD OF THE LEFT HORIZ STABILIZER. REPAIRED PER ECO2011. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004691995071400469NM 1995 7 14 TSAA9553104 119950601A5330 SKIN BOEING737 737297 1384480NM BS 907 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING MAINTENANCE VISIT, FILIFORM CORROSION NOTED ON THE CIRCUMFERENTIAL SKIN LAP JOINT AT BS 907, STRINGER 20L THROUGH STRINGER 20R. REPAIRED PER SRM 53-30-3 FIG 28. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004701995071400470NM 1995 7 14 TSAA9553105 119950601A5312 BULKHEAD BOEING737 737297 1384480NM BS 178 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND BS 178 BULKHEAD LEFT CENTER CHORD CRACKED. REPAIRED PER ECO2518. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004711995071400471NM 1995 7 14 TSAA9553107 119950601A5311 FRAME BOEING737 737297 1384480NM BS 500 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURNG HEAVY MAINTENANCE VISIT, FOUND 2 CRACKS ON FRAME AT BS 500 BETWEEN STRINGER 22L AND STRINGER 23L, FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 51-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004721995071400472NM 1995 7 14 TSAA9553108 119950601A5311 FRAME BOEING737 737297 1384480NM BS 440-460 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKS ON FRAME BETWEEN BS 440 AND BS 460 UNDER PLATE AT S-26R, FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 51-40-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004731995071400473NM 1995 7 14 TSAA9553109 119950601A5311 FRAME BOEING737 737297 1384480NM BS 480 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND 4 CRACKS ON FRAME AT BS 480 BETWEEN S-22L AND S-26L. REPAIRED PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004741995071400474NM 1995 7 14 TSAA9553110 119950601A5311 FRAME BOEING737 737297 1384480NM BS 460 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENACNE VISIT, FOUND CRACKED FRAME AT BS 460 STRINGER 23L, FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004751995071400475NM 1995 7 14 TSAA9553111 119950601A5311 FRAME BOEING737 737297 1384480NM BS 440 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKED FRAME AT 440, STRINGER 22L FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004761995071400476NM 1995 7 14 TSAA9553112 119950601A5311 FRAME BOEING737 737297 1384480NM BS 420 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKED FRAME AT BS 420 STRINGER 23L, FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004771995071400477NM 1995 7 14 TSAA9553113 119950601A5311 FRAME BOEING737 737297 1384480NM BS 400 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKED FRAME AT BS 400 STRINGER 22L, FORWARD CARGO COMPARTMENT. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004781995071400478NM 1995 7 14 TSAA9555116 119950601A5511 SPAR BOEING737 737297 1384480NM HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, NOTED CORROSION IN SEVERAL PLACES RT HORIZONTAL STABILIZER TOP SIDE AFT SPAR INBOARD END. REPAIRED PER ECO1889R1. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 19950714004791995071400479NM 1995 7 14 TSAA9555117 119950601A5511 SPAR BOEING737 737297 1384480NM HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, NOTED CORROSION BULGE TOP OF RT HORIZONTAL STABILIZER AFT SPAR OUTBOARD END. INTERIM REPAIRED PER ECO2591. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004801995071400480NM 1995 7 14 TSAA9555118 119950530A5511 SPAR BOEING737 737297 1384480NM HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, CORROSION NOTED AT TOP OF LEFT HORIZONTAL STABILIZER INBOARD END, REAR SPAR. REPAIRED EPR ECO 1889R1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004811995071400481NM 1995 7 14 TSAA9557091 119950601A5711 SPAR WEB BOEING737 737297 1384480NM WS 541 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING FRONT SPAR WEB EXFOLIATED AT CHORD VERTICAL LEG AT WS 541. REPAIRED PER ECO2587. AIRCRAFT RETURNED TO SERVICE. (M). 2L72 4F A16WE 19950714004821995071400482NM 1995 7 14 TSAA9557094 119950601A5711 SPAR BOEING737 737297 1384480NM WS 542-554 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING EXFOLIATION CORROSION NOTED ON LOWER INTERSPAR SKIN TRAILING EDGE FROM WS 542 TO WS 554. REPAIRED PER ECO1684R6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004831995071400483NM 1995 7 14 TSAA9557095 119950601A5711 SPAR BOEING737 737297 1384480NM WS 536 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING EXFOLIATION CORROSION NOTED ON LOWER INTERSPAR SKIN TRAILING EDGE AT WS 536. REPAIRED PER ECO1684RT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004841995071400484NM 1995 7 14 TSAA9557096 119950601A5711 SPAR BOEING737 737297 1384480NM WS 464 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING EXFOLIATION CORROSION NOTED ON LOWER INTERSPAR SKIN TRAILING EDGE AT WS 464. REPAIRED PER ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004851995071400485NM 1995 7 14 TSAA9557100 119950601A5711 SPAR BOEING737 737297 1384480NM FSS 552 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING EXFOLIATION CORROSION NOTED AT FRONT SPAR WEB FSS 552 AT NR 1 SLAT ACTUATOR. REPAIRED PER ECO2587. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004861995071400486NM 1995 7 14 TSAA9557102 119950601A5720 CHORD BOEING737 737297 1384480NM WS 453 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, LEFT WING STATION 453 EXFOLIATION CORROSION NOTED ON THE LOWER HORIZONTAL CHORD, OUTBOARD OF NR 2 SLAT ACTUATOR. REPAIRED PER ECO2135R1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004871995071400487NM 1995 7 14 TSAA9557114 119950601A5711 SPAR BOEING737 737297 1384480NM WS 462.47 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, EXFOLIATION CORROSION NOTED ON RT WING LOWER INNER SPAR SKIN AT WS 462.47. REPAIRED PER ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004881995071400488NM 1995 7 14 TSAA9557115 119950601A5730 SKIN BOEING737 737297 1384480NM LT WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENACNE VISIT, NOTED CORROSION TOP OF LEFT WING FORWARD OF OUTBOARD VORTEX GEN. REPAIRED PER ECO1722R5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004891995071400489NM 1995 7 14 TSAA9557119 119950530A5711 SPAR BOEING737 737297 1384480NM WS 487.3 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURIGN HEAVY MAINTENANCE VISIT, LEFT WING STATION 487.3 EXFOLIATION CORROSION FOUND ON THE LOWER HORIZONTAL CHORD OF FRONT SPAR. REPAIRED PER ECO2135R1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950714004901995071400490WP 1995 7 14 USAA950587 119950420A5400 ANGLE DOUG DC9 DC931 3022065WP BS 1019 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK TOP PYLON TO FUSELAGE ATTACH ANGLE STATION 1019 LEFT PYLON. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 10. (M) 2L72 4F A6WE 19950714004911995071400491WP 1995 7 14 USAA950588 119950418A5330 SKIN DOUG DC9 DC931 3022065WP BS 294-313 CLASS II REPAIR A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR RT SIDE FUSELAGE AT STATION 294-313 LONGERON 18R AND 21R. INSTALLED CLASS I REPAIR PER SRM 53-04 FIG 12B. (M) 2L72 4F A6WE 19950714004921995071400492WP 1995 7 14 USAA950589 119950418A5330 SKIN DOUG DC9 DC931 3022065WP BS 965 CLASS II REPAIR A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR RT FUSELAGE SKIN AT STATION 965 LONGERON 14R. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 32. (M) 2L72 4F A6WE 19950714004931995071400493WP 1995 7 14 USAA950590 119950412A5320 BRACKET DOUG DC9 DC931 3022065WP BS 692 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK BRACKET STATION 692 JUST OUTBOARD OF KEEL BEAM FORWARD OF MAIN GEAR DOOR ACTUATOR UPPER ATTACH POINT. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 11. (M) 2L72 4F A6WE 19950714004941995071400494WP 1995 7 14 USAA950591 119950413A5220 DOOR PAN DOUG DC9 DC931 3022065WP EMERG EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .5 INCH CRACK RT FORWARD EMERGENCY EXIT WINDOW TOP AFT STOP. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (M) 2L72 4F A6WE 19950714004951995071400495WP 1995 7 14 USAA950592 119950417A5313 LONGERON DOUG DC9 DC931 3022065WP FS 965 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 965 LONGERON 13L AT TOP HI-LOCK. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19950714004961995071400496WP 1995 7 14 USAA950593 119950413A5330 SKIN DOUG DC9 DC931 3022065WP BS 37 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR. INSTALLED FUSELAGE NOSE SKIN RADOME HINGE AREA STATION 37. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 77. (M) 2L72 4F A6WE 19950714004971995071400497WP 1995 7 14 USAA950594 119950504A5315991556169 FLOORBEAM DOUG DC9 DC931 3022065WP BS 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION OUTBOARD WEB OF FLOORBEAM WHERE IT ATTACHED TO BELTFRAME STATION 996. CORROSION TASK NR C58-53300. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 72 AND USAIR EA NR 30252. (M) 2L72 4F A6WE 19950714004981995071400498WP 1995 7 14 95ZZZM226 119950605A3260SS092200017017 THROTTLE SWITCH DOUG DC9 DC983 3022083WP FWD PEDESTAL DEFECTIVE A ASAAO OTHER N FALSE WARNING APAPPROACH 1 NM01960AS8567 53074 SEA - ON ARRIVAL OF FLT 451 CREW REPORTED, DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED, THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON. CYCLED LANDING GEAR, APPROXIMATELY 15 SECONDS AFTER GEAR EXTENDED THE SECOND TIME, THE WARNING HORN SILENCED AND ALL GEAR POSITION LIGHTS INDICATED DOWN AND LOCKED. REPLACED THE LANDING GEAR HANDLE SWITCH AND THE LEFT THROTTLE SWITCH ASSEMBLY. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE ASAA9580136. 2L72 4F RTA6WE 19950714004991995071400499NM 1995 7 14 ASAA9510059 119950611A335086210151 EEL BATT PACK BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - FORWARD EMERGENCY FLOOR LIGHT TRANSMITTER INOP. MAINTENANCE REPLACED BATTERY PACK. (M) 2L72 4F A16WE 19950714005001995071400500NM 1995 7 14 ASAA9540027 119950615A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - AFT THREE PEEPLS LIGHTS INOP. MAINTENANCE RECONNECTED WIRING. (M) 2L72 4F RTA16WE 19950714005011995071400501WP 1995 7 14 ASAA9580111 119950513A5210 HANDLE MECH DOUG DC9 DC982 3022082WP FWD ENTRY DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01933AS 49234 SEA - ON ARRIVAL OF FLIGHT 367 - CREW REPORTED, THE FORWARD ENTRY DOOR HANDLE DIFFICULT TO UNLATCH. LUBED DOOR HANDLE MECHANISM AND DOOR OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005021995071400502 1995 7 14 ASAA9580112 419950514A2565D37013109 SLIDE BOTTLE DOUG DC9 DC983 3022083WP FWD ENTRY DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE. (M) 2L72 4F RTA6WE 19950714005031995071400503WP 1995 7 14 ASAA9580116 119950519A5210 BAYONETS DOUG DC9 DC983 3022083WP L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01945AS 49643 ANC - PRIOR TO DEPARTURE OF FLIGHT 196, CREW REPORTED L1 DOOR JAMMED IN PARTLY OPEN POSITION WHILE ATTEMPTING TO CLOSE DOOR FOR DEPARTURE. OPENED AND INSPECTED L1 DOOR, RELEASED STUCK BAYONETS AND DOOR OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950714005041995071400504 1995 7 14 ASAA9580118 419950523A2565D37013115 SLIDE BOTTLE DOUG DC9 DC982 3022082WP R1 DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS 49111 SFO - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2L72 4F A6WE 19950714005051995071400505WP 1995 7 14 ASAA9580119 119950522A53137075T7351 LONGERON DOUG DC9 DC982 3022082WP BS 692-694 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS27146 49236 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y692 TO Y694, X PLUS 7, Z MINUS 49. REMOVED CORROSION AND INSTALLED REPAIR IAW DC-9 SRM 53-01, 51-10-03, 51-10-01, 53-14-02, 53-02. (M) 2L72 4F A6WE 19950714005061995071400506WP 1995 7 14 ASAA9580120 119950522A53203957317504 FITTING DOUG DC9 DC982 3022082WP BS 1214-1216 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS27146 49236 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON MOUNT BRACKET AT Y1214 TO Y1216, X-4. REPLACED BRACKET IAW DC-9 SRM 51-10-01 AND 51-30-01. (M) 2L72 4F A6WE 19950714005071995071400507WP 1995 7 14 ASAA9580121 119950522A5347TMS6019609 CARGO TRACK DOUG DC9 DC982 3022082WP BS 1007-1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS27146 49236 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1007 TO Y1155, X-15, Z-45. REPLACED CARGO TRACK IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-01. (M) 2L72 4F A6WE 19950714005081995071400508WP 1995 7 14 ASAA9580126 119950522A5347TMS6019609 CARGO TRACK DOUG DC9 DC982 3022082WP BS 218-370 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS27146 49236 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y218 TO Y370, X-14, Z-44. REPLACED CARGO TRACK IAW DC-9 SRM 53-05. (M) 2L72 4F A6WE 19950714005091995071400509WP 1995 7 14 ASAA9580127 119950522A5311 FRAME DOUG DC9 DC982 3022082WP BS 1250 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01935AS27146 49236 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1250, X-7 TO X PLUS 16, Z-45. REPLACED FRAME IAW DC-9 SRM 51-10-03 AND 53-03. (M) 2L72 4F A6WE 19950714005101995071400510WP 1995 7 14 ASAA9580130 119950528A3350 EEL TERMINAL DOUG DC9 DC982 3022082WP TAILCONE LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, THE TAILCONE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INTERMITTENT. SECURED LOOSE TERMINAL TO SOCKET ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005111995071400511WP 1995 7 14 ASAA9580131 119950530A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01956AS 48079 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 25 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005121995071400512WP 1995 7 14 ASAA9580132 119950530A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY AND FORWARD GALLEY AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005131995071400513WP 1995 7 14 ASAA9580133 119950602A335060030451 EEL BATT PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005141995071400514WP 1995 7 14 ASAA9580134 119950603A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT SIGN AT ROW 22 WAS FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005151995071400515WP 1995 7 14 ASAA9580135 119950603A33501001191 PORTABLE EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01974AS19480 53450 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950714005161995071400516WP 1995 7 14 ASAA9580136 119950605A3260DT2RA7 GEAR SWITCH DOUG DC9 DC983 3022083WP CTR INST PANEL DEFECTIVE A ASAAO OTHER N FALSE WARNING APAPPROACH 1 NM01960AS 53074 SEA - ON ARRIVAL OF FLT 451 CREW REPORTED, DURING APPROACH WHEN THE LANDING GEAR WAS EXTENDED THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON. CYCLED LANDING GEAR, APPROXIMATELY 15 SECONDS AFTER GEAR EXTENDED THE SECOND TIME, THE WARNING HORN SILENCED AND ALL GEAR POSITION LIGHTS INDICATED DOWN AND LOCKED. REPLACED THE LANDING GEAR HANDLE SWITCH AND THE LEFT THROTTLE SWITCH ASSEMBLY. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. REFERENCE 95ZZZM226. 2L72 4F RTA6WE 19950714005171995071400517WP 1995 7 14 ASAA9580137 119950605A3260833702 UPLOCK SENSOR DOUG DC9 DC982 3022082WP NLG DEFECTIVE A ASAAO OTHER N FALSE WARNING CLCLIMB 1 NM01967AS 49103 PDX - ON ARRIVAL OF FLT 453 - CREW REPORTED UPON DEPARTURE FROM SJC WHEN THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. ACCOMPLISHED CHECKLIST WITH SAME RESULT. LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UPLOCK SENSOR. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005181995071400518WP 1995 7 14 ASAA9580138 119950608A335020131A EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND DIM. REPLACED THE FORWARD AND AFT BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005191995071400519WP 1995 7 14 ASAA9580139 119950612A3350 EEL TERMINAL DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01930AS 49231 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. SECURED LOOSE GROUND TERMINAL FOR LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005201995071400520WP 1995 7 14 ASAA9580140 119950615A33501001191 PORTABLE EEL DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01933AS16358 49234 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT CHARGE INDICATOR LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005211995071400521WP 1995 7 14 ASAA9580141 119950615A33501001191 PORTABLE DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01932AS4644 49233 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005221995071400522WP 1995 7 14 ASAA9580142 119950616A33501001191 PORTABLE EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS13907 53018 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950714005231995071400523WP 1995 7 14 ASAA9580143 119950616A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950714005241995071400524WP 1995 7 14 ASAA9580144 119950618A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN WAS FOUND DIM. REPLACED THE BATTERIES AND SIGN OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005251995071400525WP 1995 7 14 ASAA9580145 119950618A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN COCKPIT, FORWARD GALLEY AND FORWARD ENTRY WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950714005261995071400526EU 1995 7 14 USAA950576 219950608A7230 COMPRESSOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515P 54521EU ENGINE STALLED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19481US24820 11230 CLT - FLT 0456 - WHILE CLIMBING OUT OF CLT, FLIGHT ENCOUNTERED A COMPERSSOR STALL. THE CAPTAIN POWERED BACK TO IDLE THEN UP AGAIN AND GOT ANOTHER COMPRESSOR STALL. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. REPLACED ENGINE ASSEMBLY. (M) 2L72 4F4 FRTA20EU E2EU 19950714005271995071400527WP 1995 7 14 USAA950585 119950424A5312 BULKHEAD DOUG DC9 DC931 3022065WP BS 965 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND DENT IN BOTTOM OF BULKHEAD STATION 965 RT. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 19. (M) 2L72 4F A6WE 19950714005281995071400528WP 1995 7 14 USAA950586 119950424A5330 SKIN DOUG DC9 DC931 3022065WP BS 965 CLASS II REPAIR A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND CLASS II REPAIR LEFT FUSELAGE SKIN STATION 965 BETWEEN LONGERON 13L AND 14L. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 32. (M) 2L72 4F A6WE 19950714005291995071400529 1995 7 14 USAA950596 419950604A344220671570153 R/T UNIT BOEING737 737201 1384454NM WEATHER RADAR FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19228US63288 21817 CLT - FLT 97 - FLIGHT EN ROUTE PIT TO MIA WHEN RADAR QUIT WORKING. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENACNE REPLACED R/T UNIT. RADAR WORKED NORMAL. (M) 2L72 4F A16WE 19950714005301995071400530 1995 7 14 USAA950597 419950605A34426225132108 RT UNIT BOEING737 7372B7 1384560NM WEATHER RADAR FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19271AU12703 22883 PIT - FLT 1069 - AFTER DEPARTURE FROM PIT, CREW WAS UNABLE TO TURN RADAR ON. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED R/T UNIT. RADAR WORKED NORMAL. (M) 2L72 4F A16WE 19950714005311995071400531NM 1995 7 14 USAA950598 119950606A261365528087A OVERHEAT UNIT BOEING737 7372B7 1384560NM LT WING FAILED A USAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA19266AU23779 22878 CLT - FLT 955 - FLIGHT EN ROUTE BWI TO BHM WHEN LEFT WING BODY OVERHEAT LIGHT CAME ON. FLIGHT DIVERTED TO CLT WHERE LANDING WAS MADE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OVERHEAT ACCESSORY UNIT. OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950714005321995071400532NE 1995 7 14 USAA950612 219950617A73147436024 FUEL PUMP BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19227AU 21816 PHL - FLT NR 63 - CREW NOTICED FLUCTUATION IN NR 1 ENGINE DURING CLIMB-OUT OF PHL. FUEL FLOW/EPR AND N1 FLUCTUATIONS WERE NOTED ALONG WITH A SLIGHT OIL PRESSURE FLUCTUATION. CREW RETURNED TO PHL WITH NR 1 ENGINE AT IDLE. MAINTENANCE REPLACED FUEL PUMP AND FUEL CONTROL UNIT PER M/M 73-21-2. RAN ENGINE AND LEAK CHECKS GOOD. (M) 2L72 4F4 F A16WE E2EA 19950714005331995071400533NM 1995 7 14 USAA950613 119950618A3230 FLEX HOSE BOEING737 737201 1384454NM NOSE GEAR FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19249US 22756 JAX - FLT 104 - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. FLIGHT RETURNED TO JAX WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR DOWNLOCK ACTUATOR HYDRAULIC FLEX LINE. (M) 2L72 4F A16WE 19950714005341995071400534NM 1995 7 14 USAA950614 119950619A5241 STRAP BOEING737 737201 1384454NM 1R DOR LOOSE A AUSAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19228US 21817 EWR - FLT 371 - LOUD BANGING NOISE ON CLIMB-OUT. WARNING STRAP CAUGHT IN FORWARD GALLEY SERVICE DOOR. FLIGHT RETURNED TO EWR WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED STRAP FROM FORWARD GALLEY SERVICE DOOR. INSPECTED DOOR AND FUSELAGE, NO DAMAGE FOUND. (M) 2L72 4F A16WE 19950714005351995071400535NM 1995 7 14 USAA950615 119950619A79301163P181 SWITCH BOEING737 737201 1384454NM NR 2 ENGINE FAILED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19241US 22443 BWI - FLT 2190 - FLIGHT EN RUOTE ORD TO PHL, WHEN NR 2 ENGINE FILTER BYPASS LIGHT CAME ON AND NR 2 ENGINE SHUTDOWN. FLIGHT DIVERTED TO BWI WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL FILTER BYPASS SWITCH AND ENGINE OIL FILTER. (M) 2L72 4F A16WE 19950714005361995071400536WP 1995 7 14 USAA950618 119950618A36105910244655 DUCT DOUG DC9 DC981 3022081WP RT BLOCKED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19804US 48052 BOS-BWI - FLT 1187 - AFTER TAKEOFF, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT DUCT ASSEMBLY BETWEEN THE FLOW CONTROL VALVE AND HEAT EXCHANGER, LEAK AND OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950714005371995071400537NM 1995 7 14 USAA950623 119950313A5313 STRINGER BOEING737 7373B7 1384580NM BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19534AU19250 24516 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 16L BS 500 C PLUS 4 INCHES. REPAIRED PER EO 5393X228. (M) 2L72 4F RTA16WE 19950714005381995071400538NM 1995 7 14 95ZZZX3397 119950509A3246NAS67043 BOLT BFGOODRICH 313061 BOEING727 727225 1384077NM NR 3 WHEEL ASSY SHEARED A AMYWAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SO19887MA 45377253 21857 ON POST FLT INSPECTION, FOUND NR 3 TIRE/WHEEL ASSEMBLY MISSING FROM AIRCRAFT. REPLACED NR 3 AXLE SLEEVE AFTER AXLE INSPECTION. REPLACED NR 3 AND NR 4 BRAKES. REPLACED THE NR 3 AND NR 4 TIRE/WHEEL ASSEMBLIES. ACCOMPLISHED TIRE BURST INSPECTION IAW MM 32-40-0 AND CHAPTER 5. REPLACED NR 3 AXLE NUT, SPACER AND NUT LOCKING BOLTS. INSPECTED AIRCRAFT, NO DAMAGE NOTED. ON TOUCHDOWN, ANOTHER AIRCRAFT REPORTED TIRE/WHEEL ASSEMBLY DEPARTING THE AIRCRAFT. INVESTIGATION REVEALS WHEEL NUT LOCKING BOLT, PN NAS 6704-3, SHEARED RESULTING IN THE WHEEL NUT LOSING ITS TORQUE RESULTING IN THE TIRE/WHEEL ASSEMBLY DEPARTING THE AIRCRAFT. 2L73 4F A3WE 19950714005391995071400539SW 1995 7 14 95ZZZX3400 119950622A7712TVS06RF1135S CONNECTOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE CONTAMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA23359AE AC674 AIRCRAFT RETURNED TO FIELD DUE TO RIGHT ENGINE TORQUE FLUCTUATION. THE SYSTEM WAS TROUBLESHOT AND THE TORQUE STRAIN GAUGE CANNON PLUG WAS FOUND CONTAMINATED. THE CANNON PLUG WAS CLEANED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. 1L72 4T A8SW 19950714005401995071400540SO 1995 7 14 C2XA95CL100 119950625A3231MS203922C59 PIN EMB 120 EMB120RT SO LT MLG DOOR WORN A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0915725 120173 CLE/BUF - FLT 3180 - GEAR DOOR ON THE LEFT LANDING GEAR REMAINED OPEN AFTER GEAR WAS RETRACTED. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED LEFT OUTBOARD MLG DOOR HANDLE HOLD-UP PIN IAW 52-81-00. OPS CHECKED DOORS IAW 52-00-00. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950714005411995071400541SO 1995 7 14 C2XA95IA109 119950629A572012017056021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB NR 15 LOWER NR 3 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT - 9056.6. CYCLES - 13433. (X) 2L72 4T RTA31SO 19950714005421995071400542SO 1995 7 14 C2XA95IA110 119950629A572012017056013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND RT WING RIB NR 15 LOWER NR 2 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950714005431995071400543SO 1995 7 14 C2XA95IA111 119950629A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0958733 120197 IAH - DURING C-CHECK INSPECTION, FOUND LT WING LOWER SKIN SUPPORT NR 4 AFT, CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. ACFT TT 9056.6. CYCLES - 13433. (X) 2L72 4T RTA31SO 19950714005441995071400544WP 1995 7 14 CAL950428 119950530A2530 OVENS DOUG DC9 DC982 3022082WP GALLEY FAILED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09809NY 49263 SFO - FLT 0151 - THE GALLEY POWER NR 2 PHASE 'A' 50 AMP CIRCUIT BREAKER ON AFT COCKPIT BULKHEAD TRIPPED DURING FLIGHT AND WAS ACCOMPANIED BY THE COPILOT'S INSTRUMENTS SHOWING FLAGS MOMENTARILY. THE FLIGHT ATTENDANT ALSO REPORTED SPARKS COMING FROM BEHIND OVENS LOCATED IN FIRST CLASS. THE SPARKS CEASED AFTER PULLING CIRCUIT BREAKERS. THE CAMLOCK RETAINER WAS REMOVED. THE OVENS LOCATED IN FIRST CLASS WERE PLACARDED INOPERATIVE AND THE CIRCUIT BREAKERS WERE PULLED AND COLLARED. 2L72 4F A6WE 19950714005451995071400545NM 1995 7 14 CAL950483 119950614A3260 SENSOR TARGET BOEING737 737524 1384721NM NLG OUT OF ADJUST A CALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW0958606 27319 EWR - FLT 1535 - THE NLG RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANIDNG AT IAH. THE GEAR WAS CYCLED WITH NO CHANGE. EMERGENCY PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY CONFIRMED THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR SENSOR TARGET IAW MM 32-33-00. THE NOSE GEAR WAS SWUNG WITH ALL OPERATION AND INDICATIONS CHECKING GOOD. (X) 2L72 4F RTA16WE 19950714005461995071400546NM 1995 7 14 CAL950484 119950613A52306546921528 CARGO DOOR BOEING737 737217 1384464NM CARGO COMPT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423372784 19887 CLE - FLT 1639 - MAINTENANCE FOUND TWO CRACKS IN THE FORWARD CARGO DOOR AT THE SEAL RETAINER WHILE UNDERGOING A DECAY CHECK FOR PRESSURIZATION PROBLEMS. THE CRACKS WERE 8 INCHES AND 4.5 INCHES LONG. THE FORWARD CARGO DOOR WAS REMOVED AND REPLACED IAW MM 52-31-0. A SUBSEQUENT DECAY CHECK WAS GOOD. (X) 2L72 4F A16WE 19950714005471995071400547NE 1995 7 14 CAL950491 219950615A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 3 FAILED A CALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW0915069404487550 46584 517714 IAH - FLT 0010 - THE NR 3 ENGINE N2 EXCEEDED LIMITS AND BOTH THE NR 1 AND NR 2 ENGINE EGT'S ROSE TO 980 DEGREES ON ROTATION LEAVING IAH. ALL ENGINE THROTTLES WERE RETARDED WITH THE NR 1 AND NR 2 EGT'S DROPPING BELOW RED LINE AND THE NR 3 ENGINE N2 RETURNING TO WITHIN LIMITS. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 3 ENGINE WAS REMOVED AND REPLACED. BOTH THE NR 1 AND NR 2 ENGINES UNDERWENT A BORESCOPE, A VSV/VBV RIG CHECK, AND POWER ASSURANCE RUN WITH NO FAULTS FOUND. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION INTO NR 3 ENGINE FAILURE. SUPPLEMENT - INVESTIGATION DID NOT REVEAL ANY CAUSE FOR THE NR 3 ENGINE N2 OVERSPEED. (X) 2L73 4F4 F A22WE E23EA 19950714005481995071400548NM 1995 7 14 CAL950493 119950616A3260 SENSOR WIRE BOEING727 727232 1384082NM LT MLG BROKEN A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0917779 20634 IAH - FLT 0775 - OVERRIDE WAS REQUIRED TO RETRACT THE LANDING GEAR AFTER TAKEOFF FROM SJO. REPLACING THE LANDING GEAR LEVER LOCK SOLENOID DID NOT HELP. MAINTENANCE FOUND A BROKEN WIRE TO THE LEFT GEAR SAFETY SENSOR. THE WIRE WAS REPAIRED. AN OPERATIONAL CHECK OF THE LEVER LATCH SYSTEM WAS CONDUCTED AND OPERATION CHECKED GOOD. (X) 2L73 4F A3WE 19950714005491995071400549NE 1995 7 14 CAL950498 219950618A7230 COMPRESSOR AIRBUS300 A300B4103 3930104EU GE CF6 CF650C2 30018NE NR 2 ENGINE DAMAGED A CALAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 SW091398337663 92 455845 LAX - FLT 0290 - TAKEOFF WAS REJECTED AT APPROXIMATELY 100 KNOTS AFTER A LOUD BANG WAS HEARD WITH THE NR 2 ENGINE EGT POINTER AT MAX. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. A POWER ASSURANCE RUN WAS PERFORMED AND ALL ENGINE PARAMETERS WERE WITHIN LIMITS. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION CONFIRMED IMPACT DAMAGE TO COMPRESSOR ROTOR SECTION DUE TO FOD, WHICH RESULTED IN BLADE LIBERATION. (X) 2L72 4F4 F A35EU E23EA 19950714005501995071400550WP 1995 7 14 CAL950500 119950618A2910 HYD LINE DOUG DC10 DC1030 3023501WP NR 1 HYD SYS LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0912061 47851 EWR - FLT 0010 - THE NR 1 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ENROUTE FROM IAH TO ORY. THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE FROM THE LEFT ENGINE DRIVEN PUMP TO THE PRESSURE MODULE LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMOVED AND REPLACED. IN ADDITION, BOTH THE LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM WAS SERVICED. THE ENGINES WERE RUN AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A22WE 19950714005511995071400551EU 1995 7 14 CALA950495 119950617A29136506606 HYD PUMP AIRBUS300 A300B4103 3930104EU NR 2 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0911985 119 LAX - FLT 0187- THE YELLOW HYDRAULIC SYSTEM FLUID DROPPED TO THE ORANGE DOT DURING CRUISE. THE HYDRAULIC PUMP WAS DUMPED AND THE FLUID LEVEL REMAINED AT THE ORANGE DOT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE YELLOW SYSTEM NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. (X) 2L72 4F A35EU 19950714005521995071400552WP 1995 7 14 GRAA9533 119950519A3350110049 EEL POWER SUPPLY DOUG DC9 DC987 3022087WP CABIN FAILED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111074T 49727 DURING ROUTINE MAINTENANCE, FOUND FORWARD FLOOR TRACK LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY POWER SUPPLY. OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA6WE 19950714005531995071400553WP 1995 7 14 GRAA9534 119950610A55433913180 SKIN DOUG DC9 DC915 3022036WP RUDDER TAB SERVICEABLE A GRAAK NONE O OTHER ININSP/MAINT 1 WP111070T 45784 DURING C-CHECK, RUDDER TRAILING EDGE, RT SIDE, HAD 3 SURFACE CRACKS. ONE CRACK IS 3 INCHES LONG. ONE CRACK IS 1.50 INCHES LONG. ONE CRACK IS 5.25 INCHES LONG. RUDDER WAS REPAIRED PER FLIGHT VEHICALS IAW ER NR DC-9-55-001. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950714005541995071400554WP 1995 7 14 GRAA9535 119950612A533059114103 SKIN DOUG DC9 DC915 3022036WP FS 313 CORRODED A GRAAK NONE O OTHER ININSP/MAINT 1 WP111070T 45784 DURING C-CHECK, MAINTENANCE FOUND CORROSION IN THE FORWARD BAGGAGE BIN, FS 313, LONGERON 26 LEFT. REPAIRED PER FLIGHT VEHICALS, IAW ER NR DC-9-53-001. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950714005551995071400555WP 1995 7 14 GRAA9536 119950618A3350DSIZE EEL BATTERIES DOUG DC9 DC915 3022036WP CABIN DISCHARGED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111068T 45782 DURING LINE MAINTENANCE, MECHANICS DISCOVERED THE CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERIES. THE EMERGENCY LIGHT SYSTEM WAS OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19950714005561995071400556WP 1995 7 14 HAL95079 119950626A3350 EEL BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13674MC 47735 HNL - INFORMATION FROM M-71 LOG PAGE 148439-2. EMERGENCY FLOOR LIGHTS ARE VERY DIM. REPLACED EMERGENCY FLOOR LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950714005571995071400557WP 1995 7 14 HAL95080 119950626A335026CN3363 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13674MC 10360 47735 INFORMATION FROM M-71 LOG PAGE 148442. FORWARD AND MID-CEILING LIGHTS DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY SUPPLY PACK. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950714005581995071400558WP 1995 7 14 HAL95081 119950626A3350 EEL BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13672MC 47661 INFORMATION FROM M-71 LOG PAGE 142700-2. AFT EMERGENCY FLOOR LIGHTS INOPERABLE. REPLACED AFT EMERGENCY FLOOR LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950714005591995071400559EU 1995 7 14 RAIA950636 119950624A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE151001683 106 STL - EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE. MAINTENANCE REPLACED CABIN EMERGENCY LIGHTING BATTERY PACK. (X) 2H72 4T RTA53EU 19950714005601995071400560EU 1995 7 14 RAIA950637 119950624A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03339TE2927 876 935 STL MX - FORWARD EMERGENCY LIGHTS WILL NOT STAY ON. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (X) 2L72 4T RTA56EU 19950714005611995071400561EU 1995 7 14 RAIA950638 119950624A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03339TE5073 307 935 STL - MX- AFT EMERGENCY LIGHTS WILL NOT STAY ON. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (X) 2L72 4T RTA56EU 19950714005621995071400562 1995 7 14 RAIA950640 419950627A34427006921302 CONTROL PANEL AEROSPATR72 ATR72202 8680940EU COCKPIT FAILED A RAIAO OTHER O OTHER CRCRUISE 1 CE03722TE5846 220 STL - FLT 7110 - WX RADAR INOPERATIVE. MAINTENANCE REPLACED RADAR CONTROL PANEL. (X) 2H72 4T RTA53EU 19950714005631995071400563EU 1995 7 14 RAIA950641 119950627A75001379287L405 LINE BAG JETSTMJETSTM3201 1500217EU LEFT ENGINE CRACKED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03341TE5782 950 FWA - FLT 7533 - LEFT ENGINE NOT MAKING TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE BLEED AIR LINE. GROUND RUNS REVEALED ALL ENGINE PARAMETERS TO BE NORMAL. (X) 2L72 4T RTA56EU 19950714005641995071400564EU 1995 7 14 RAIA950642 119950628A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03434AM8456 4874 887 STL- FLT 7446 - LEFT ENGINE LOW TORQUE, WITH TTL ON AT 80 PERCENT. MAITNENANCE ADJUSTED LEFT ENGINE TORQUE SIGNAL CONDITIONER. GROUND POWER RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950714005651995071400565EU 1995 7 14 RAIA950643 119950627A33501LF15 EEL WIRE JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03551HK1124 41040 STL - FLT 7528 - LAST 5 FEET OF FLOOR EMERGENCY LIGHTS ARE OUT. MAINTENANCE RECONNECTED JUMPER WIRE BETWEEN LAST 2 SECTIONS OF EMERGENCY LIGHTS. (X) 2L72 4T RTA41NM 19950714005661995071400566EU 1995 7 14 RAIA950645 119950630A771294959411 TTL BAG JETSTMJETSTM3201 1500217EU STA 130 FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03864AE5764 864 RIGHT ENGINE BYPASS AT 80 PERCENT TORQUE. AFTER CREW PERFORMED STATIC GROUND RUNS, DETERMINED RIGHT TTL CAUSING ENGINE BYPASS. DEFERRED RT TTL PER MEL76-2, CAT. C. (X) 2L72 4T RTA56EU 19950714005671995071400567WP 1995 7 14 95ZZZX3401 119950614A3260 IND WIRE DOUG DC9 DC931 3022065WP NLG OPEN A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE05985Z 47491 ORF - FLT 694 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR GREEN, DOWN, AND LOCKED LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR. FOUND WIRE, G216B24, WITH HIGH RESISTANCE AND INTERMITTENTLY OPEN. REPLACED WIRE, G216B24, BETWEEN CONNECTOR P1-133 PIN 6 AND SE-49 TERMINAL STRIP. NOSE LANDING GEAR OPERATION AND INDICATION SYSTEM CHECKED NORMAL. CHECK C - 3-1-95 - STL. 2L72 4F A6WE 19950714005681995071400568NE 1995 7 14 95ZZZX3402 219950620A7261 TUBE BOEING747 747156 1384884NM PWA JT9 JT9D7AH 52054NE NR 3 BEARING LEAKING A TWAAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE05134TW 19958 LGW - FLT 721 - DURING CLIMB, SHUT DOWN NR 4 ENGINE, SN 4103, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATING. FOUND OIL AND OIL FILTER HIGHLY CARBONATED. REPLACED ENGINE, SN 4103. ENGINE OPERATION CHECKED NORMAL. CHECK C-1 - 11-14-94 - JFK. SUPPLEMENTAL DATA - INVESTIGATION OF NR 4 ENGINE, SN 4103, OIL FILTER BYPASS LIGHT ILLUMINATION REVEALED NR 3 BEARING TUBE ASSY LEAKING AT THE JOINT ALLOWING CARBON THAT HAD BUILT UP IN THE NR 3 BEARING COMPARTMENT TO MIGRATE TO THE FILTER CAUSING THE BYPASS INDICATION. ENGINE, SN 4103, REPAIRED AND RETURNED TO SERVICE. 2L74 4F4 F A20WE E20EA 19950714005691995071400569NM 1995 7 14 95ZZZX3403 119950602A5330 SKIN BOEING727 727231 1384079NM BS 680-686 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554353 21985 MCI - DURING OP-17, FOUND CORROSION IN FORWARD CARGO BELLY SKIN, STA 680 TO STA 686, BETWEEN STR 28R AND STR 27L. REPAIRED PER SRM 53-30-3, FIGURE 3A, SHEETS 1-3. AIRCRAFT TOTAL TIME: 37,842 HOURS; 23,911 CYCLES. 2L73 4F A3WE 19950714005701995071400570WP 1995 7 14 95ZZZX3404 119950604A5320 JAMB DOUG DC9 DC941 302207NWP VENTRAL DOOR CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05935L 47603 DURING CHECK C, FOUND A 1.25 INCH RADIAL CRACK AT TOP LEFT SIDE OF AFT VENTRAL DOOR JAMB, RUNNING CIRCUMFERENTIALLY IN RADIUS OF DASH 13 ANGLE. STOP DRILLED PER EMLR NR 65704 AND REPLACED FASTENERS PER SRM CHAPTER 51 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 43,613 HOURS; 43,279 CYCLES. 2L72 4F A6WE 19950714005711995071400571NM 1995 7 14 95ZZZX3405 119950614A5320 SERVICE PANEL BOEING727 727231 1384079NM BS 1183 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554345 21632 MCI - DURING CHECK C, FOUND CORROSION AT AFT EDGE OF AFT SERVICE PANEL, STA 1183. REPAIRED PER ARA NR 9346. AIRCRAFT TOTAL TIME: 40,176 HOURS; 26,185 CYCLES. 2L73 4F A3WE 19950714005721995071400572NM 1995 7 14 95ZZZX3406 119950614A5712 RIB BOEING727 727231 1384079NM WS 686 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554349 21968 MCI - DURING OP-17, FOUND RIGHT WING RIB CRACKED AT STR 9, STA 686. REPAIRED PER SB 57-A159 AND SSRM 57-20-201. AIRCRAFT TOTAL TIME: 38,173 HOURS; 24,723 CYCLES. 2L73 4F A3WE 19950714005731995071400573WP 1995 7 14 95ZZZX3407 119950617A5313 LONGERON DOUG DC9 DC931 3022065WP BS 484-503 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05976Z 47248 STL - DURING OP-15, FOUND CORROSION ON LONGERON 30, AT 6 FASTENERS BETWEEN STA 484 AND STA 503. REPAIRED PER SRM 53-02, FIGURE 14, AIRCRAFT TOTAL TIME: 66,307 HOURS; 81,289 CYCLES. 2L72 4F A6WE 19950714005741995071400574WP 1995 7 14 95ZZZX3408 119950615A5313 LONGERON DOUG DC9 DC931 3022065WP BS 160-200 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05984Z 47412 STL - DURING CHECK C, FOUND .0312 INCH CRACKS COMING OUT OF 4 RIVET HOLES, STA 160 TO STA 200, LONGERON 22L. REPAIRED PER ARA 65706. AIRCRAFT TOTAL TIME: 61,210 HOURS; 72,666 CYCLES. 2L72 4F A6WE 19950714005751995071400575NM 1995 7 14 95ZZZX3409 119950622A33201695 LAMP BASE BOEING747 747131 1384881NM CABIN BROKEN A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0593119 20083 LGW - FLT 720 - DURING CRUISE, SMOKE AND ELECTRICAL ODOR EMITTED FROM OVERHEAD LIGHT NEAR FIRST CLASS GALLEY. FOUND BROKEN LAMP BASE, MFG PN 1695, IN SOCKET. REMOVED LAMP BASE AND INSTALLED NEW LAMP. LIGHT OPERATION CHECKED NORMAL. CHECK C-2 - 10-19-94 - MCI. 2L74 4F A20WE 19950714005761995071400576WP 1995 7 14 95ZZZX3410 119950614A5320 TRAP PANEL DOUG DC9 DC931 3022065WP RIGHT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05976Z 47248 STL - DURING OP-15, FOUND .75 INCH CRACK BETWEEN 5 AND 6 HOLE FORWARD END OF RIGHT TRAPEZOIDAL PANEL. INSTALLED NEW PANEL PER SRM 57-09. AIRCRAFT TOTAL TIME: 66,307 HOURS; 31,289 CYCLES. 2L72 4F A6WE 19950714005771995071400577NE 1995 7 14 95ZZZX3411 219950622A7230809407 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE COMPRESSOR FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 CE05914TW 49185 DEN - FLT 427 - DURING DESCENT, SHUT DOWN LEFT ENGINE DUE TO SPOOLED DOWN WITH INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. CHANGED ENGINE, S/N 1205. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 21,594 HOURS; 10,979 CYCLES. OP-15 - 12-3-94 - MCI. INVESTIGATION INTO ENGINE S/N 1205 SPOOL DOWN REVEALED SEVENTH STAGE COMPRESSOR BLADE, MFG P/N 809407, FRACTURED DUE TO IMPACT CAUSING DOWNSTREAM COMPRESSOR DAMAGE. ENGINE WAS REPAIRED AND RETURNED TO SERVICE. 2L72 4F4 F A6WE E9NE 19950714005781995071400578NM 1995 7 14 95ZZZX3412 119950619A5320 STRUCTURE BOEING727 727231 1384079NM BS 948 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564319 20052 MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A .75 INCH CRACK AND A 1 INCH CRACK AT LBL 60, STA 948. REPAIRED BY INSTALLING DOUBLER PER ARA 9335. AIRCRAFT TOTAL TIME: 64,349 HOURS; 43,814 CYCLES. 2L73 4F A3WE 19950714005791995071400579NM 1995 7 14 95ZZZX3413 119950619A5320 STRUCTURE BOEING727 727231 1384079NM BS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564319 20052 MCI - DURING AIRCRAFT SERVICE NR 4, FOUND A 1 INCH CRACK AT LBL 57, STA 940. REPAIRED BY INSTALLING DOUBLER PER ARA 9335. AIRCRAFT TOTAL TIME: 64,349 HOURS; 43,814 CYCLES. 2L73 4F A3WE 19950714005801995071400580NM 1995 7 14 AWXA9500398 119950623A33501614 EEL LAMP BOEING737 737277 1384570NM R1 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED R1 DOOR, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005811995071400581NM 1995 7 14 AWXA9500399 119950624A3350 EEL BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28167AW 23628 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE ROW 14 THROUGH ROW 18. RECONNECTED LIGHT AT ROW 14, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005821995071400582NM 1995 7 14 AWXA9500402 119950626A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE ROW 18 THROUGH ROW 23. REPAIRED WIRING, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005831995071400583NM 1995 7 14 AWXA9500403 119950628A335020121 EEL BATTERY PACK BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28183AW 22650 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND THE OVERWING EMERGENCY EXIT LIGHT STAYS ON IN FLIGHT AND IS INOPERATIVE ON GROUND. REMOVED AND REPLACED POWER SUPPLY AND BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005841995071400584NM 1995 7 14 AWXA9500405 119950629A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH ROW 21. REPAIRED BROKEN WIRE AT ROW 20, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005851995071400585NM 1995 7 14 AWXA9500406 119950630A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PATH EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 7 THROUGH ROW 13. REPAIRED WIRE AT ROW 7, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950714005861995071400586NM 1995 7 14 AWXA9500412 119950626A53471A0870130 SEAT TRACK BOEING737 7373G7 1384595NM LT COCKPIT WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING SCHEDULED C6 INSPECTION, FOUND CAPTAIN'S ADJUSTABLE SEAT STOP TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED TRACK ASSEMBLY PER SRM 53 00 52. (X) 2L72 4F RTA16WE 19950714005871995071400587EU 1995 7 14 RAIA950644 119950629A73321103P0645 PRESS SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENG TRUSS FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03426AM6776 874 STL - FLT 7418 - SUPPLEMENT - FUEL LIGHT ON CAPTAIN'S PANEL ILLUMINATED. MAINTENANCE REPLACED LEFT FUEL PRESSURE SWITCH. (X) 2L72 4T RTA56EU 19950721000021995072100002 1995 7 21 95UAL900037 419950712A2564 TUBE BF GOODRICH 7A14371 BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE SLIDE RAFT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP294735U G1061 19928 SLIDE RAFT WAS FOUND TO HAVE POROSITY ON BOTH THE RT AND LT UPPER TOP TUBES AND IN BOTH ASPIRATOR TUBE AREAS. SCRAPPED SLIDE. 2L74 4F4 F A20WE E20EA 19950721000031995072100003 1995 7 21 95UAL900038 419950712A2564 TUBE BF GOODRICH 7A14381 BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE SLIDE RAFT FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29154UA G1080 20103 SLIDE RAFT WAS FOUND TO HAVE POROSITY ON THE LT BOTTOM TUBE, CROSS OVER TUBE, AND ON THE CENTER TUBE. IN ADDITION, SLIDE/RAFT HAS SEAM LEAKS ON THE RT AND LT SIDE TUBES. SCRAPPED SLIDE. 2L74 4F4 F A20WE E20EA 19950721000041995072100004EU 1995 7 21 95UAL900039 119950712A5520D5528000100160 ELEVATORS AIRBUS, LUCAD55280001000AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE LT/RT OUT OF TOL A AUALAK NONE E VIBRATION/BUFFET CLCLIMB 1 WP29403UA 442 CREW REPORTS HIGH SPEED BUFFET, WHEN SPEED IS BETWEEN 305 AND 320 KNOTS AT FLIGHT LEVEL 28.0, APPEARS TO GO AWAY WHEN SPEED DROPS BELOW 300 KNOTS. REPLACED BOTH ELEVATORS AND THS ACTUATOR. 2L72 4F RTA28NM E40NE 19950721000051995072100005 1995 7 21 95UAL900040 419950713A2565 TUBE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE SLIDE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP294718U 19879 SLIDE HAS POROSITY ON BOTH LT AND RT UPPER TOP TUBES, ASPIRATOR TUBE AREAS, AND ON THE ASPIRATOR TUBE SLEEVE. SCRAPPED SLIDE. 2L74 4F4 F A20WE E20EA 19950721000061995072100006NM 1995 7 21 95UAL900041 119950713A3350 EEL BATTERY PACK BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE EXTERIOR DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299006U 19044 EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS. 2L72 4F4 F A16WE E2EA 19950721000071995072100007WP 1995 7 21 ABXA9500577 119950711A3260801801 SENSOR DOUG DC9 DC941 302207NWP NLG DEFECTIVE A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23953AX 47608 ON FINAL, AFTER NORMAL GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT CAME ON. GREEN NOSE GEAR LIGHT WENT OUT AND GEAR WARNING HORN SOUNDED. RECYCLED GEAR AND GOT NORMAL INDICATIONS. VERIFIED BROKEN WIRE ON NOSE GEAR DOWN LOCK PROXIMITY SENSOR. REPLACED SENSOR IAW DC-9 MM 32-60-1. OPS CHECKED GOOD. 2L72 4F A6WE 19950721000081995072100008WP 1995 7 21 ABXA9500578 119950711A2910AE2460001J0630 FLEX LINE DOUG DC8 DC861 3021952WP NR 3 ENG LEAKING A ABXAO OTHER K FLUID LOSS CRCRUISE 1 GL23842AX 46015 HYD SYS PRESS GAUGE READ ZERO WITH BOTH AILERON AND RUDDER REVERSION LIGHTS ON. HYD QTY READ FULL WITH LOW RESERVOIR, LOW PRESS, AND TEMP LIGHTS OUT. REPOWERED AILERONS WITH AUX PUMP; PRESS AND QTY CHECKED OK. AILERON LIGHT EXTINGUISHED, COULD NOT RESTORE NORMAL ENG DRIVEN PUMP PRESS. TESTED HYD SELECTOR LEVER AND COULD READ A 'BUMP' IN PRESS; WHEN CYCLED IT WORKED OK. REPLACED BOTH ENG DRIVEN HYD PUMPS. REPLACED ALL 3 LINES AT LT HYD PUMP. FOUND NR 3 ENG PRESSURE FLEX LINE FROM HYD PUMP TO PYLON CONNECTION TO HAVE A HOLE IN IT; REPLACED LINE. WORK, SYSTEM AND LEAK CHECK DONE IAW DC 8 MM. 2L74 4F 4A25 19950721000091995072100009 1995 7 21 COM11928 419950712A341825C1175A AOA SENSOR EMB 120 EMB120RT SO LT ELEC RACK DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01268CA 120262 LEFT AND RIGHT AOA SENSOR AND SLIP ANTI-ICE INOP. REPLACED THE AOA CURRENT SENSOR. 2L72 4T RTA31SO 19950721000101995072100010EU 1995 7 21 COM31116 119950712A2910MS24142D1 RELAY SAAB SF340 SF340A 7850100EU AVIONICS FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01358CA 340A047 HYDRAULIC PUMP FAILED. REPLACED RELAY 7LM. 2L72 4T RTA52EU 19950721000111995072100011EA 1995 7 21 COM605116 119950711A2760270003 PCU CNDAIRCL600 CL6002B19 EA LT SPOILER DEFECTIVE A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01937CA2223 7044 FLIGHT SPOILER FAULT MESSAGE ON EICAS. REPLACED THE LT FLIGHT SPOILER PCU. 2L72 4F RTA21EA 19950721000121995072100012EA 1995 7 21 COM60517 119950710A3150864806 PSEU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01912CA3222 2492 7011 WOW INPUT, WOW OUTPUT, NOSE WHEEL STEERING CAUTION MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19950721000131995072100013NM 1995 7 21 DL72E953067 119950710A3244324002809 TIRE 324002809 BOEING727 727247 138408FNM RT MLG FAILED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 SO11830WA 524AB 21482 DURING CRUISE, A LOUD NOISE WAS HEARD IN CABIN. RETURNED TO ATL. THE RIGHT GEAR NR 3 TIRE HAD THE RETREAD BLOW OFF. DAMAGE OCCURED TO APU EXHAUST DUCT, GEAR DOOR RELEASE BRACKETS, L/E OF NR 3 PYLON AND RIGHT INBD AFT FLAP. WHEN WHEEL ASSEMBLY WAS CHANGED IT WAS NOTICED THAT ONLY THE RETREAD HAD SEPARATED AND THE TIRE STILL MAINTAINED PRESSURE. FOR RETURN TO SERVICE REPLACED NR 3 AND 4 WHEEL ASSEMBLIES, APU EXHAUST DUCT, L/G DOOR BRACKERS, PYLON L/E AND AFT FLAP. 2L73 4F A3WE 19950721000141995072100014NM 1995 7 21 DL72K953019 119950710A5754 SKIN BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 A CRACK IN NR 3 L/E FLAP I/B EDGE, 1 INCH FROM LIP. FOUND DURING A-2 LTR CK TPAMM. REPAIRED PER MM 57-53-0 PG 804. 2L73 4F A3WE 19950721000151995072100015NM 1995 7 21 DL72K953058 119950710A2910651784967DM TUBE BOEING727 727232 1384082NM B-HYD SYSTEM CRACKED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11412DA 21232 DURING CRUISE, HAD LOSS OF B-SYSTEM HYDRAULIC FLUID AND PRESSURE. FLIGHT DIVERTED TO JFK. FOUND CRACKED LINE FROM PUMP TO FILTER HOUSING. REPLACED LINE, PUMPS AND FILTERS, RETURNED TO SERVICE. 2L73 4F A3WE 19950721000161995072100016NM 1995 7 21 DL72S953017 119950710A5754 SKIN BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 FOUND DURING A-2 LETTER CHECK, CRACK IN LWR COVE SKIN SUPPORT ANGLE, BELOW TAI DUCT ON NR 3 SLAT. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950721000171995072100017NM 1995 7 21 DL72S953018 119950710A5754 SKIN BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 FOUND DURING A-2 LETTER CHECK, NR 6 SLAT COVE SKIN ANGLE, UNDER TAI DUCT CRACKED. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950721000181995072100018NM 1995 7 21 DL72S953034 119950711A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 NR 7 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721000191995072100019NM 1995 7 21 DL72S953035 119950711A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11496DA 21076 NR 7 SLAT COVE SKIN ANGLE DOUBLER CRACKED AT I/B STOP PAD. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721000201995072100020NM 1995 7 21 DL72W952986 119950708A2150 CONTROLLER 6075103 BOEING727 727247 138408FNM LT PACK FAULTY A DALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SO112812W 87C343 20868 DURING CRUISE, AT FL 250 WITH SINGLE PACK OPERATION HAD CABIN ALTITUDE HORN. INITIATED EMERGENCY DESCENT, LANDED BOS. REPLACED LEFT PACK 35 DEG CONTROLLER, PACK OPERATION NORMAL. 2L73 4F A3WE 19950721000211995072100021NM 1995 7 21 DL72W953005 119950709A2613 OVERHEAT LOOP 356802255 BOEING727 727247 138408FNM LWR AFT BODY CUT A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO112821W 21059 AT FL 270, 25 MIN INTO FL, LOWER AFT BODY O/H LIGHT ILLUM INTERMITTENTLY FOR APPROX 1 MIN, THEN STEADY. C/W POM PROC AND LIGHT REMAINED ILLUM FOR 15 TO 20 MIN WITH NR 2 THROTTLE AT IDLE. AFTER 20 MIN WITH NR 2 THROTTLE AT IDLE LIGHT EXT WITH A COUPLE OF FLICKERS, THEN OUT. FLIGHT DIVERTED TO ATL. FOUND CUT IN DETECTOR LOOP. REPLACED LOOP, OPERATION NORMAL. 2L73 4F A3WE 19950721000221995072100022NM 1995 7 21 DL72W953011 119950619A5320 ANGLE BOEING727 727247 138408FNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 ANGLE CORRODED UNDER HINGES FOR PANEL 3355L. REMOVED ANGLE FABRICATED NEW, INSTALLED PER MM 53-30-1 PG 808. FOUND AT HMV. 2L73 4F A3WE 19950721000231995072100023NM 1995 7 21 DL72W953012 119950619A5320 ANGLE BOEING727 727247 138408FNM BS 846 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 ANGLE CORRODED FWD SIDE STA 846 RBL 10 AND LBL 10, BELOW DELTA BEAM. REMOVED ANGLE, MANUFACTURED NEW ANGLE PER M/M 53-30-1 PG 808. FOUND AT HMV. 2L73 4F A3WE 19950721000241995072100024NM 1995 7 21 DL72W953013 119950620A5750 RIB BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 7 SLAT CRACKED IN LOWER AFT CORNER OF SLAT RIB 22 INCHES IB OF OB TRACK. REPAIRED DOUBLER PER MM 57-54-0 FIG 814. FOUND AT HMV. 2L73 4F A3WE 19950721000251995072100025NM 1995 7 21 DL72W953027 119950619A5313 STRINGER BOEING727 727247 138408FNM BS 595 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 595. REMOVED CLIPS, FABRICATED NEW SECTION OF STRINGER AND SPLICE PER SRM 53-10-3. TREATED AND PAINTED PER PS 900-3-6 NR 3. INSTALLED STRINGER SECTIONS, SPLICE AND CLIP PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950721000261995072100026NM 1995 7 21 DL72W953029 119950621A5313 STRINGER BOEING727 727247 138408FNM BS 1180 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 STR 22L CORRODED AT STA 1180. REMOVED DAMAGED STR AND INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19950721000271995072100027NM 1995 7 21 DL72W953031 119950620A5315 FLOORBEAM BOEING727 727247 138408FNM BS 1110 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CABIN FLOORBEAM CORRODED BOTTOM SIDE STA 1110, RBL 12 TO LBL 12 AT NUTPLATES. REMOVED CORROSION PER SRM 51-10-6. REMOVED DAMAGED T-CAP, FABRICATED NEW T-CAP PER SRM 53-10-8. INSTALLED REPAIR PER SRM 53-10-1. 2L73 4F A3WE 19950721000281995072100028NM 1995 7 21 DL72W953032 119950710A5754 RIB BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 3 SLAT RIB CRACKED, I/B OF ACTUATOR ATTACH POINT CRACKED IN RADIUS AT LOWER AFT END OF RIB. INSTALLED DOUBLER PER MM 57-54-0 PG 819. FOUND AT HMV. 2L73 4F A3WE 19950721000291995072100029NM 1995 7 21 DL73E953057 119950709A2530 TRASH BIN BOEING737 737247 138448DNM GALLEY ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11237WA 23185 ON DESCENT, FLT ATTENDANTS REPORTED FUMES IN AFT GALLEY, SMELLED LIKE JET FUEL. EMERGENCY WAS DECLARED, LANDED IN STL WITHOUT INCIDENT. INSPECTION FOUND FUMES TO BE FROM GALLEY TRASH BIN AND CLEANING FLUID RESIDUE. REMOVED TRASH, RETURNED TO SERVICE. 2L72 4F A16WE 19950721000301995072100030NE 1995 7 21 DL73S953056 219950711A751015534 ANTI-ICE DUCT BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE CRACKED A DALAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO11319DL 23091 709138 AFTER TAKEOFF, NR 2 OIL TEMP CLIMBED THROUGH YELLOW ZONE, ENGINE WAS SHUTDOWN WHEN TEMP WENT TO RED. RETURNED TO ATL. FOUND ENGINE ANTI-ICE DUCT CRACKED AND BLOWING HOT AIR ON FUEL HEAT VALVE. THE DUCT AND FUEL HEAT VALVE WERE REPLACED, OPERATION NORMAL. 2L72 4F4 FRTA16WE E2EA 19950721000311995072100031NM 1995 7 21 DL757953030 119950416A5755113N460123 SKIN BOEING757 757232 1384965NM NR 6 SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 23614 ON INITIAL SHOP INSPECTION, MAINTENANCE FOUND 2 SMALL HOLES APPROX 1 INCH IN DIAMETER ON BOTTOM SKIN, LOCATED 4 INCHES FROM T/E. REPAIR WAS ACCOMPLISHED PER SRM 57-70-01 FOR NR 6 SPOILER PANEL. 2L72 4F RTA2NM 19950721000321995072100032NM 1995 7 21 DL757953036 119950704A2497W4216 HARNESS BOEING757 757232 1384965NM FS 700 BURNED A DALAK NONE O OTHER ININSP/MAINT 1 SO11607DL 22814 WHILE TROUBLESHOOTING PROBLEM FOR RT AFT MAIN FUEL BOOST PUMP, A BURNING ODOR WAS REPORTED IN THE AFT CABIN. AIRCRAFT POWER WAS REMOVED AND ODOR INVESTIGATED. FOUND WIRE BUNDLE W4216 AND W4106 SHORTED AND BURNED, WITH 60 WIRED IN BUNDLE W4216 COMPLETELY BURNED THROUGH. DAMAGE WAS LOCATED IN FWD FUSELAGE FS 700, APPARENT CAUSE WAS WIRE CHAFING ON CLAMP. ALL WIRES WERE REPAIRED AND AFFECTED SYSTEMS TESTED NORMAL. 2L72 4F RTA2NM 19950721000331995072100033WP 1995 7 21 DLL13953020 119950702A5320 CLIPS LKHEED1011 10113851 5265010WP BS 1463 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SKIN CLIPS CORRODED IN C2 BB AFT OF STA 1463 BETWEEN STR 33 AND 35. REPAIRED PER SRM 53-13-00 FIG 817. 2L73 4F A23WE 19950721000341995072100034WP 1995 7 21 DLL13953021 119950703A5320 CLIP LKHEED1011 10113851 5265010WP BS 746 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIPS CORRODED FS 746 BETWEEN STR 32 AND 33. REMOVED DAMAGED FORM TO CLIP, FABRICATED CLIP AND SPLICE STRAP, INSTALLED REPAIR PER SRM 53-13-00 FIG 817. 2L73 4F A23WE 19950721000351995072100035WP 1995 7 21 DLL13953022 119950703A5347 SEAT TRACK LKHEED1011 10113851 5265010WP BS 349 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SEAT TRACK CORRODED STA 349. REPLACED SECTION OF TRACK PER SRM 53-21-00 PG 836. 2L73 4F A23WE 19950721000361995072100036WP 1995 7 21 DLL13953023 119950704A5320 CLIP LKHEED1011 10113851 5265010WP FS 480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIP CORRODED STR 33 TO 36 FS 480. REPLACED SKIN CLIP PER SRM 53-12-0 FIG 817. 2L73 4F A23WE 19950721000371995072100037WP 1995 7 21 DLL13953024 119950708A5320 CLIP LKHEED1011 10113851 5265010WP BS 569 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIP CORRODED STA 569 STR 33 TO 36. REPLACED SKIN CLIP PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721000381995072100038WP 1995 7 21 DLL13953025 119950708A5320 CLIP LKHEED1011 10113851 5265010WP BS 849 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIP CORRODED STA 849 BETWEEN STR 31 TO 32. FABRICATED AND PAINTED NEW REPAIR, INSTALLED NEW FORMER TO CLIP REPAIR PER SRM 53-31-00 PG 817. 2L73 4F A23WE 19950721000391995072100039WP 1995 7 21 DLL13953026 119950708A5320 SKIN CLIP LKHEED1011 10113851 5265010WP BS 769 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIP CORRODED STA 769 BETWEEN STR 33 TO 35. CUT AND REMOVED CLIP, DRILLED NEW CLIP AND SPLICE STRAP, INSTALLED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721000401995072100040WP 1995 7 21 DLL13953028 119950709A5320 CLIP LKHEED1011 10113851 5265010WP FS 829 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SKIN CLIPS CORRODED STA 829 STR 31 TO 33. REMOVED CORROSION, TREAT AND PAINTED, FABRICATED NEW FORMER TO SKIN REPAIR, AND INSTALLED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721000411995072100041WP 1995 7 21 DLL13953033 119950706A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 295 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, INSPECTION FOUND THE FLOORBEAM CORRODED AT FS 295 BETWEEN LBL 30 AND RBL 30. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950721000421995072100042WP 1995 7 21 DLL13953059 119950703A5347 SEAT TRACK LKHEED1011 10113851 5265010WP BS 749-846 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SEAT TRACK CORRODED STR 749 TO 846. REMOVED OLD SEAT TRACK, AND DRILLED NEW. INSTALLED TRACK PER SRM 53-21-00 PG 836. 2L73 4F A23WE 19950721000431995072100043WP 1995 7 21 DLL13953060 119950704A5330 TEAR STRAP LKHEED1011 10113851 5265010WP BS 649-669 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND TEAR STRAP DISBONDED STA 649 TO 669 STR 38. TEAR STRAP REMOVED PER ERA 271311-14. 2L73 4F A23WE 19950721000441995072100044WP 1995 7 21 DLL13953061 119950704A5330 TEAR STRAP LKHEED1011 10113851 5265010WP BS 629 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND TEAR STRAP DISBONDED STA 629 STR 34. TEAR STRAP REMOVED PER ERA 271311-14. 2L73 4F A23WE 19950721000451995072100045WP 1995 7 21 DLL13953062 119950710A5320 CLIP LKHEED1011 10113851 5265010WP BS 709 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV FOUND SKIN CLIP CORRODED STA 709 STR 33 TO 36. REMOVED CORRODED CLIP, DRILLED NEW CLIP AND SPLICE, AND INSTALLED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721000461995072100046WP 1995 7 21 DLL13953074 119950712A2150 AIR COND SYSTEM LKHEED1011 10113851 5265010WP CABIN SMOKE ODOR A DALAO OTHER NB FALSE WARNING SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11787DL 193A1126 ON CLIMB, HAD SMOKE DETECTOR IN AFT LAV GO OFF, THEN ALL DETECTORS IN FWD AND AFT CABIN WENT OFF. FLIGHT LANDED HNL. RAN ALL THREE ENGINES PER PFHB AT POWER, ISOLATED EACH BLEED. ALL CHECKED GOOD, NO SMOKE OR ODOR NOTED, RETURNED TO SERVICE. 2L73 4F A23WE 19950721000471995072100047NM 1995 7 21 DLM88953015 119950710A5320 ANGLE DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11973DL 53241 FOUND DURING E-1 LETTER CHECK, KEEL BEAM AFT ANGLE CROSSOVER CRACKED. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950721000481995072100048NM 1995 7 21 DLM88953016 119950710A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11973DL 53241 FOUND DURING E-1 LETTER CHECK, FUSELAGE SKIN CRACKED AT RT NLG STRUT DOOR AFT HINGE. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950721000491995072100049NM 1995 7 21 MWEA95234 119950712A256011320 GIRT BAR DOUG MD88 MD88 3023688NM AFT GALLEY DOOR LACK OF LUBE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 CREW REPORTS, IT WAS VERY DIFFICULT TO DISARM THE AFT GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR. MAINTENANCE CLEANED AND LUBRICATED AFT GALLEY DOOR SLIDE GIRT BAR. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950721000501995072100050WP 1995 7 21 MWEA95235 119950713A3350100865 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP AFT LAV FAILED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 47673 DURING ROUTINE INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOP, FROM ROW 18 AFT. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950721000511995072100051NM 1995 7 21 P5CA9500381 119950630A5415MS2000P62800 HINGE BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON BLOWOUT PANEL HINGE NR PYLON LEFT SIDE. REPLACED HINGE PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950721000521995072100052NM 1995 7 21 P5CA9500382 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1680-1720 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN THE FUSELAGE SKIN LEFT SIDE BETWEEN BS 1680 AND 1720 AT S40L LAP JOINT. REPAIRED PER BOEING SRM 53-30-03. 2L74 4F A20WE 19950721000531995072100053NM 1995 7 21 P5CA9500383 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 1520 BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BEND IN UPPER CHORD AT FLOORBEAM BS 1520 AT LBL 25. STRAIGHTENED PER BOEING SRM 51-40-01 AND 51-10-01. 2L74 4F A20WE 19950721000541995072100054NM 1995 7 21 P5CA9500384 119950630A5321 FLOOR BOEING747 747121 1384871NM BS 1660-1760 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FLOOR COVER SHEET METAL BETWEEN BS 1660 AND 1760 AT RBL 40. REPLACED SKIN PANEL PER BOEING SRM 53-10-23. 2L74 4F A20WE 19950721000551995072100055NM 1995 7 21 P5CA9500385 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1740 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN PANEL AND STRINGER S41L NEAR BS 1740. REPAIRED PER BOEING SRM 53-10-03 AND 51-10-01, STRINGER REPAIR AND SKIN BLENDED WITHIN LIMITS. 2L74 4F A20WE 19950721000561995072100056NM 1995 7 21 P5CA9500386 119950630A2550 ROLLER TRAY BOEING747 747121 1384871NM BS 1740-1760 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND CORROSION IN ROLLER TRAY RBL 35 TO 38 AND LBL 5.5 BETWEEN BS 1740 AND 1760. REPAIRED PER BOEING SRM 53-10-06 AND 51-10-01. 2L74 4F A20WE 19950721000571995072100057NM 1995 7 21 P5CA9500387 119950630A5320 RIB BOEING747 747121 1384871NM FWD CARGO BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN RIB BETWEEN BS 960 AND 980 BETWEEN RBL 24.75 AND RBL 45.5. REPAIRED PER BOEING SRM 53-10-21. 2L74 4F A20WE 19950721000581995072100058NM 1995 7 21 P5CA9500388 119950630A5320 CHORD BOEING747 747121 1384871NM BS 840 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENTS ON UPPER CHORD BETWEEN RBL 45.5 AND LBL 45.5 BS 840. STRAIGHTENED AND SMOOTHED PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950721000591995072100059NM 1995 7 21 P5CA9500389 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 680-700 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND DENTS ON S47L AND S47R BETWEEN BS 680 AND 700. CORROSION REMOVED AND DENTS STRAIGHTENED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721000601995072100060NM 1995 7 21 P5CA9500390 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 680-700 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON S46L BETWEEN BS 680 AND 700. CRACK REPAIRED PER BOEING SRM 53-10-03 FIG 1. 2L74 4F A20WE 19950721000611995072100061NM 1995 7 21 P5CA9500391 119950630A5320 RIB BOEING747 747121 1384871NM BS 700 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON BS 700 RBL 8. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950721000621995072100062NM 1995 7 21 P5CA9500392 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 765 BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BEND ON INTERCOSTAL AT BS 765, BETWEEN LBL 22.75 AND LBL 45.5. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721000631995072100063NM 1995 7 21 P5CA9500393 119950630A5321 FLOOR BOEING747 747121 1384871NM BS 765 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FLOOR AND BEND ON INTERCOSTAL AT BS 765 RBL 24.75 AND RBL 45.5. REPAIRED PER BOEING SRM 53-10-21. 2L74 4F A20WE 19950721000641995072100064NM 1995 7 21 P5CA9500394 119950630A5330 PANEL BOEING747 747121 1384871NM BS 780 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON PLUG PANEL BS 780 ABOVE S46R. REPLACED PANEL PER SRM 53-10-21 AND 51-30-02. 2L74 4F A20WE 19950721000651995072100065NM 1995 7 21 P5CA9500395 119950630A5320 CHORD BOEING747 747121 1384871NM BS 780 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON UPPER CHORD AT THE BL0 BS 780. DAMAGE BLENDED OUT PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721000661995072100066NM 1995 7 21 P5CA9500396 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN BRACKET BS 800 S47L. CORROSION REMOVED PER BOEING SRM 51-10-01 WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721000671995072100067NM 1995 7 21 P5CA9500397 119950630A5321 FLOOR PANEL BOEING747 747121 1384871NM BS 1660 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON FLOOR PANEL BS 1660 TO 1680 ABOVE S40R. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950721000681995072100068NM 1995 7 21 P5CA9500398 119950630A5720 SUPPORT FTG BOEING747 747121 1384871NM WS 669.5 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN RIB SUPPORT FITTING UPPER CHORD AND ANGLE UPPER CHORD LEFT WING WS 669.5. REPAIRED PER BOEING SB 57-2273. 2L74 4F A20WE 19950721000691995072100069NM 1995 7 21 P5CA9500399 119950630A5320 SUPPORTS BOEING747 747121 1384871NM BS 540-560 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON 2 SUPPORTS AT BL0 BETWEEN BS 540 AND 560. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721000701995072100070NM 1995 7 21 P5CA9500400 119950630A5312 BULKHEAD BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON BS 1000 BETWEEN S45L AND S47R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721000711995072100071NM 1995 7 21 SWAA950514 119950705A291050603 VALVE BOEING737 7372H4 138448CNM A-HYD SYST LEAKING A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0757SW 21722 DURING MAINT FERRY FLIGHT AFTER RUDDER CHANGE, AIRCRAFT LOST A-SYSTEM HYDRAULICS. AIRCRAFT RETURNED TO PAE AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND A-SYSTEM SHUTTLE VALVE LEAKING. REPLACED AND SERVICED SYSTEM PER BOEING M/M. 2L72 4F A16WE 19950721000721995072100072 1995 7 21 SWAA950515 419950705A344236140710401 ANTENNA BOEING737 7372H4 138448CNM RADAR INOP A SWAAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0796SW 23055 WEATHER RADAR ANTENNA BECAME INOPERATIVE. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. REPLACED RADAR ANTENNA MOTOR AND OPERATIONAL CHECKED PER BOEING M/M. 2L72 4F A16WE 19950721000731995072100073NM 1995 7 21 SWAA950516 119950707A3244 TIRE BOEING737 7373H4 1384600NM NLG SEPARATION A SWAAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SW07336SW 23940 AFTER TAKEOFF, NUMBER 1 NOSE GEAR TIRE TREAD SEPARATED. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REPLACED BOTH NOSE GEAR WHEEL ASSEMBLIES AND INSPECTED AIRCRAFT FOR DAMAGE PER BOEING M/M. 2L72 4F RTA16WE 19950721000741995072100074SO 1995 7 21 SWIA95595 119950712A323112025262501 RELAY BOX EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT MLG DOORS FAILED A SWIAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM07190SW 120050 LT MAIN GAP DOORS WOULD NOT CLOSE AFTER TAKEOFF, RECYCLED 4 TIMES, BOTH REQUIRED LIGHTS ON WITH GEAR HANDLE IN UP POSITION. REPLACED LDG RELAY BOX SWING GEAR SEVERAL TIMES, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950721000751995072100075NM 1995 7 21 UPS203806 119950711A5320 WEB BOEING727 72730C 1384009NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK EMITTING FROM FASTENER HOLE IN WEB AT STA 259.5 WL 192.5 LBL 21. REPAIRED IAW SRM 53-10-02, 51-30-2, 51-40-02. 2L73 4F A3WE 19950721000761995072100076NM 1995 7 21 UPS203807 119950711A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 910 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER FLANGE FWD SIDE AT STA 910 WL 200 RBL 25-RBL 55. REPAIRED IAW SRM 51-30-2, 51-10-2, 51-20-4, 53-10-8. 2L73 4F A3WE 19950721000771995072100077NM 1995 7 21 UPS203808 119950711A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 312/328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES ON FLOORBEAMS AT STA 312 AND 328, BL 0 TO LBL 60, WL 208. REPAIRED IAW SRM 51-10-2, 51-20-4, 53-10-8, 53-10-1, M/M 51-20-151. 2L73 4F A3WE 19950721000781995072100078NM 1995 7 21 UPS203809 119950711A57546517276 RIB BOEING727 72730C 1384009NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED RIGHT WING NR 5 SLAT ACTUATOR O/B RIB AT FWD END OF SLAT ACTUATOR ROD END ATTACHING RIB. REPLACED IAW SRM 51-10-1. 2L73 4F A3WE 19950721000791995072100079NM 1995 7 21 UPS203810 119950711A5712 RIB BOEING727 72730C 1384009NM WS 171.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED UPPER RIB CHORD AT FWD VENT BOX FWD FLANGE 7 INCHES AFT OF FRONT SPAR ON LEFT WING AT STA 171.5. REPAIRED IAW SRM 51-40-04. 2L73 4F A3WE 19950721000801995072100080NM 1995 7 21 UPS203811 119950711A5315BAC1505100276 FLOORBEAM BOEING727 72730C 1384009NM FS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UNDERSIDE OF UPPER CHORD AT STA 740, BL 0-LBL 25, WL 208.5. REPAIRED IAW SRM 53-10-1, 51-30-5, 51-30-2, 51-10-1. 2L73 4F A3WE 19950721000811995072100081NM 1995 7 21 UPS203812 119950711A5311651862548 FRAME BOEING727 72730C 1384009NM CARGO COMPT CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WEB UPPER SIDE AND END FRAME OF AFT CARGO FLOOR. REPAIRED IAW SRM 51-20-3, 51-40-2, 51-10-1. 2L73 4F A3WE 19950721000821995072100082NM 1995 7 21 UPS203813 119950711A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 640 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 640, RBL 29 TO 60, WL 208, AFT SIDE OF UPPER CHORD. REPAIRED IAW SRM 51-30-2, 51-10-8. 2L73 4F A3WE 19950721000831995072100083NM 1995 7 21 UPS203814 119950711A5311 FRAME BOEING727 72730C 1384009NM BS 640 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND FASTENER HOLES ON TOP OF FRAME AT BS 640 BETWEEN STR 22 TO 21RT. REPAIRED IAW SRM 51-40-3, 53-10-2, 53-10-1, 53-10-2. 2L73 4F A3WE 19950721000841995072100084NM 1995 7 21 UPS203815 119950711A532069164052133 CLIP BOEING727 72730C 1384009NM FS 954 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER TO FORGING ATTACH CLIP IN AFT BAY AT BS 954, WL 154 STR 25L. REPAIRED IAW SRM 51-10-1, 53-10-2, 51-10-6, 51-30-5, 51-30-2, M/M 51-10-151. 2L73 4F A3WE 19950721000851995072100085NM 1995 7 21 UPS203816 119950711A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 900 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER FLANGE AND SUPPORT STRAP AT STA 900 LBL 25 TO LBL 60 WL 200 AFT SIDE. REPAIRED IAW SRM 53-10-1, 53-10-8, 51-30-2, 51-10-1. 2L73 4F A3WE 19950721000861995072100086NM 1995 7 21 UPS203817 119950711A5315 FLOORBEAM BOEING727 72730C 1384009NM FS 1090 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM ON FWD SIDE OF UPPER CHORD AROUND NUTPLATE HOLE AT STA 1090 LBL 60 WL 208. REPAIRED IAW SRM 53-10-1. 2L73 4F A3WE 19950721000871995072100087NM 1995 7 21 UPS203818 119950711A5313BAC1493513 STRINGER BOEING727 72730C 1384009NM FS 400 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON STRINGER 15R AT BS 400. REPAIRED IAW SRM 53-10-3. 2L73 4F A3WE 19950721000881995072100088NM 1995 7 21 UPS203819 119950711A5320651759318 INTERCOSTAL BOEING727 72730C 1384009NM FS 259 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 259 TO 277 WL 208 LBL 11. REPAIRED IAW SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950721000891995072100089NM 1995 7 21 UPS203820 119950711A5320651759321 INTERCOSTAL BOEING727 72730C 1384009NM FS 256 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 256 TO 277 WL 208 RBL 15. REPAIRED IAW SRM 51-10-4, 51-30-2, M/M 32-34-71. 2L73 4F A3WE 19950721000901995072100090NM 1995 7 21 UPS203821 119950711A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION SEAT TRACK AT STA 344 RBL 25 WL 208. REPAIRED IAW SRM 53-10-1, 53-10-5. 2L73 4F A3WE 19950721000911995072100091NM 1995 7 21 UPS203822 119950711A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 678 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION SEAT TRACK FLANGE AT STA 678 RBL 24 WL 208. REPAIRED IAW SRM 51-30-2, 51-10-1, 51-10-6, 53-10-1. 2L73 4F A3WE 19950721000921995072100092NM 1995 7 21 UPS203823 119950711A5530651748428 T-CHORD BOEING727 72730C 1384009NM VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON T-CHORD FOR PANEL 9707 ON VERTICAL FIN AT FIN STA 225.6 RT SIDE. REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950721000931995072100093NM 1995 7 21 UPS203824 119950711A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 344-360 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AT STA 344 TO 360 LBL 62 WL 208. REPAIRED IAW SRM 53-10-5. 2L73 4F A3WE 19950721000941995072100094NM 1995 7 21 UPS203825 119950712A5311 FRAME BOEING727 727247 138408FNM FS 840 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01207UP 21699 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOX FRAME UPPER WEB AT STA 840 RBL 65 CRACKED. REPLACED IAW SRM 51-30-2, M/M 51-20-151, 51-20-21. 2L73 4F A3WE 19950721000951995072100095NM 1995 7 21 UPS203834 119950707A3350 EEL BATTERY BOEING727 72751C 1384015NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01902UP 18898 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT WILL NOT ILLUMINATE WHEN TURNED ON. REPLACED BATTERIES IN BOTH EMERGENCY EXIT LIGHTS. OPS CHECK GOOD. 2L73 4F A3WE 19950721000961995072100096NM 1995 7 21 UPS203836 119950713A5320 FAILSAFE BOEING727 72730C 1384009NM FS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UNDERSIDE OF FAILSAFE 480, STR 25 LT WL 160. REPAIRED IAW SRM 51-40-3. 2L73 4F A3WE 19950721000971995072100097NM 1995 7 21 UPS203837 119950713A5330 SKIN BOEING727 72730C 1384009NM BS 689 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT BS 689 STR 19 RT. REPAIRED IAW EO B727-5330-0509. 2L73 4F A3WE 19950721000981995072100098NM 1995 7 21 UPS203838 119950713A5311 FRAME BOEING727 72730C 1384009NM BS 1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN AFT CARGO BAY BS 1050 STR 26R WL 160, TOP OF FRAME AROUND 2 NUTPLATES. REPAIRED IAW SRM 51-40-3. 2L73 4F A3WE 19950721000991995072100099NM 1995 7 21 UPS203839 119950713A5312 BULKHEAD BOEING727 72730C 1384009NM BS 950 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACK IN BS 950 BULKHEAD AT LBL 15 WL 175. REPAIRED IAW SRM 53-10-9. 2L73 4F A3WE 19950721001001995072100100NM 1995 7 21 UPS203840 119950713A5320 EXPANSION LINK BOEING727 72730C 1384009NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK BUSING HOLE AT RBL 13 BS 740 WL 165. REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950721001011995072100101NM 1995 7 21 UPS203841 119950713A5315BAC1505101167 FLOORBEAM BOEING727 72730C 1384009NM BS 380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION UNDER NUTPLATE STA 380 RBL 48 WL 208 AND LBL 45 TO 62.5 WL 208. REPAIRED IAW SRM 53-10-1, 53-10-8. 2L73 4F A3WE 19950721001021995072100102NM 1995 7 21 UPS203842 119950713A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAM AT STA 277 WL 208 RBL 15 TO 40. REPAIRED IAW SRM 53-10-1, 51-40-4. 2L73 4F A3WE 19950721001031995072100103NM 1995 7 21 UPS203845 119950714A575465172813 RIB BOEING727 72730C 1384009NM NR 5 LE SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SLAT O/B TRACK O/B RIB CORRODED. REPLACED IAW SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950721001041995072100104NM 1995 7 21 UPS203846 119950714A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 64 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT STA 64.0 LBL 30 WL 208. REPLACED IAW EO B727-5310-7190. 2L73 4F A3WE 19950721001051995072100105NM 1995 7 21 UPS203847 119950714A5755651734748 CORE BOEING727 72730C 1384009NM NR 13 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 13 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-62-01. 2L73 4F A3WE 19950721001061995072100106NM 1995 7 21 UPS203848 119950714A575565173481 CORE BOEING727 72730C 1384009NM NR 7 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 7 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-62-01. 2L73 4F A3WE 19950721001071995072100107NM 1995 7 21 UPS203849 119950714A5755651734857 SPOILER BOEING727 72730C 1384009NM NR 5 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950721001081995072100108NM 1995 7 21 UPS203850 119950714A5755651734742 SPOILER BOEING727 72730C 1384009NM WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950721001091995072100109NM 1995 7 21 UPS203851 119950714A5755651734742 CORE BOEING727 72730C 1384009NM NR 2 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 2 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950721001101995072100110NM 1995 7 21 UPS203852 119950714A5755651734742 CORE BOEING727 72730C 1384009NM NR 1 SPOILER DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 SPOILER CORE DAMAGED AND CONTAMINATED. REPLACED IAW M/M 27-61-01. 2L73 4F A3WE 19950721001111995072100111NM 1995 7 21 UPS203853 119950714A5320 ANGLE BOEING727 72730C 1384009NM WS 100 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED ON I/B ATTACH ANGLE AT BOTTOM OF TWO HOLES IN RIGHT WING AT WL 208 FS 100.0. REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950721001121995072100112NM 1995 7 21 UPS203854 119950708A575465162251 SKIN BOEING727 727172C 1384058NM NR 3 LE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01916UP 19808 WHILE IN PHL - MAINTENANCE FOUND NR 3 LEADING EDGE FLAP METAL SKIN ON BACK SIDE DELAMINATED. REPAIRED IAW M/M 27-81-01. 2L73 4F A3WE 19950721001131995072100113NM 1995 7 21 UPS203855 119950714A5320 STRAP BOEING727 72730C 1384009NM BS 519-660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRAP AT BS 519 TO 660, BL 0, WL 201 AROUND NUTPLATE HOLES ON LOWER SIDE. ALSO, AT LBL 2, RBL 2 AT BS 612 TO 628. REPLACED IAW EO B727-5310-7178-A. 2L73 4F A3WE 19950721001141995072100114NM 1995 7 21 UPS203856 119950714A5311 FRAME BOEING727 72730C 1384009NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE OF FRAME AT BS 344 STR 22 RT, WL 177. REPAIRED IAW SRM 51-40-3. 2L73 4F A3WE 19950721001151995072100115NM 1995 7 21 UPS203857 119950714A5320 CREASE BEAM BOEING727 72730C 1384009NM BS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON CREASE BEAM AT BS 1130 WL 208 RBL 64. REPLACED IAW SRM 53-10-1, 51-30-2, 51-20-4. 2L73 4F A3WE 19950721001161995072100116NM 1995 7 21 UPS203858 119950714A5320BAC15061706 STRAP BOEING727 72730C 1384009NM BS 1025-1148 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BL 0 STABILIZER STRAP BS 1025 TO 1148 AROUND NUTPLATES. REPLACED IAW SRM 51-30-8, 51-30-2, 51-20-4, 51-10-6, 51-10-2, 51-10-1. 2L73 4F A3WE 19950721001171995072100117NM 1995 7 21 UPS203859 119950714A575465162275 K-FLAP BOEING727 72730C 1384009NM NR 1 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 1 K-FLAP CORRODED. REPLACED IAW M/M 27-81-01. 2L73 4F A3WE 19950721001181995072100118NM 1995 7 21 UPS203860 119950714A575465162251 ATTACH LUG BOEING727 72730C 1384009NM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 K-FLAP CORROSION ON I/B ATTACH LUG. REPLACED IAW M/M 27-81-01. 2L73 4F A3WE 19950721001191995072100119NM 1995 7 21 UPS203861 119950714A575465162262 ATTACH LUG BOEING727 72730C 1384009NM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 K-FLAP CORROSION ON O/B ATTACH LUG. REPLACED IAW M/M 27-81-01. 2L73 4F A3WE 19950721001201995072100120NM 1995 7 21 UPS203862 119950714A575465172813 RIB BOEING727 72730C 1384009NM NR 4 LE SLAT CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT O/B TRACK I/B RIB AND FITTING CORRODED. REPLACED IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950721001211995072100121NM 1995 7 21 UPS203863 119950714A5315 FLOORBEAMS BOEING727 72730C 1384009NM BS 580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAMS AT BS 580, RBL 49 TO 59, WL 201. REPAIRED IAW B727-5310-7176-A, SRM 53-10-1. 2L73 4F A3WE 19950721001221995072100122NM 1995 7 21 UPS203864 119950714A5320 ANGLE BOEING727 72730C 1384009NM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATES ON FLOORBEAM ANGLE AT BS 600 RBL 49 TO 59 WL 201. REPAIRED IAW SRM 53-10-1, 51-10-2, M/M 51-20-121, 51-30-2. 2L73 4F A3WE 19950721001231995072100123NM 1995 7 21 UPS203865 119950714A5320 SIDE LOAD BEAM BOEING727 72730C 1384009NM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM AT STA 740 WL 170 LBL 34 TO RBL 34. REPAIRED IAW 727-53-1628. 2L73 4F A3WE 19950721001241995072100124NM 1995 7 21 UPS203866 119950714A5754651732214 RIB BOEING727 72730C 1384009NM NR 1 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 1 SLAT ON LT SIDE NR 5 RIB FROM END. REPLACED IAW OHM 57-51-31, SRM 51-30-2. 2L73 4F A3WE 19950721001251995072100125NM 1995 7 21 UPS203867 119950714A5315 FLOORBEAM BOEING727 72730C 1384009NM BS 1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM LOWER CHORD AT BS 1050 WL 199 LBL 31 TO RBL 45. REPLACED IAW SRM 51-30-2 AND EO B727-5310-7183-A. 2L73 4F A3WE 19950721001261995072100126NM 1995 7 21 UPS203868 119950714A5313BAC1498132 STRINGER BOEING727 72730C 1384009NM BS 620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 21R AT BS 620. REPLACED IAW SRM 53-10-3. 2L73 4F A3WE 19950721001271995072100127NM 1995 7 21 UPS203875 119950711A3350 EEL BOEING727 72725C 138400HNM CABIN INOPERABLE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01933UP 19857 WHILE ON GROUND IN CLEVELAND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK NORMAL. 2L73 4F A3WE 19950721001281995072100128WP 1995 7 21 UPS803826 119950712A5330 SKIN DOUG DC8 DC873F 302199FWP NLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACK IN FUSELAGE SKIN AFT LT CORNER ON NOSE LANDING GEAR WHEEL WELL CUTOUT. REPAIRED IAW EO DC8-5330-4154-B. 2L74 4F RT4A25 19950721001291995072100129WP 1995 7 21 UPS803827 119950712A53205753113 TRAP FITTING DOUG DC8 DC873F 302199FWP LT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACK IN LT TRAPEZOIDAL FITTING ON TOP OF LONGERON 24 AT FS 879, 920, 940, 960. REPLACED IAW SRM 51-1-20D, 51-2-0. 2L74 4F RT4A25 19950721001301995072100130WP 1995 7 21 UPS803828 119950712A53203619811 FITTING DOUG DC8 DC873F 302199FWP FS 960 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CORROSION ON LONGERON 24L LOWER SUPPORT FITTING AT BOLT HOLES AT FS 960. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950721001311995072100131WP 1995 7 21 UPS803829 119950712A53204619810 FITTING DOUG DC8 DC873F 302199FWP FS 970 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACKED RT LONGERON T-FITTING AT FS 970. REPLACED IAW SRM 51-1-20D, 51-3-0. 2L74 4F RT4A25 19950721001321995072100132WP 1995 7 21 UPS803830 119950712A5311 FRAME DOUG DC8 DC873F 302199FWP FS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CORROSION ON LT WHEEL WELL MAIN GEAR CHANNEL FRAME AT FS 870 LBL 60. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19950721001331995072100133WP 1995 7 21 UPS803831 119950711A5512 SKIN DOUG DC8 DC873F 302199FWP RT HORIZ STAB LEDAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01867UP 45967 SUPPLEMENTAL MRR - WHILE ON GROUND, MAINTENANCE FOUND DAMAGE TO LEADING EDGE OF RT STABILIZER, DENT 5 INCHES WIDE, 5.5 INCHES TALL, 2 INCHES DEEP WITH 5 INCH VERTICAL CRACK IN CTR, 100 INCHES OUTBOARD FROM FUSELAGE. CUT 5 INCH BY 5 INCH HOLE TO REMOVE DAMAGE FROM L/E. FABRICATED REPAIR DOUBLER IAW DC8-5510-7199A. THIS INTERIM REPAIR TO BE REPLACED AT NEXT C-CHECK. 2L74 4F RT4A25 19950721001341995072100134WP 1995 7 21 UPS803832 119950714A291357155A HYD PUMP DOUG DC8 DC871F 302199DWP NR 2 HYD SYST FAILED A IPXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01703UP 45939 DURING CRUISE AT FL 350, HYD PRESSURE AND FLUID DECREASED, RAN ABNORMAL CHECKLIST. FLUID STOPPED AT AUX LEVEL, LANDED DFW, EMERGENCY DECLARED. REMOVED AND REPLACED RUDDER PUMP, NR 2 ENG PUMP, CASE DRAIN AND SYSTEM FILTERS. SERVICED HYD SYS AND CHANGED CASE DRAIN FILTERS AGAIN. OPENED DEFERRAL TO REPLACE CASE DRAIN AND SYS FILTERS IN 20 HOURS PER M/M 27-24-02. 2L74 4F RT4A25 19950721001351995072100135WP 1995 7 21 UPS803833 119950712A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 WHILE IN FOR B-CHECK, MAINTENANCE FOUND CORROSION ON FUSELAGE SKIN APPROX 12 INCHES FWD OF E AND E COMPARTMENT RIGHT SIDE. REPAIRED IAW EO DC8-5330-7189. 2L74 4F RT4A25 19950721001361995072100136WP 1995 7 21 UPS803835 119950713A53203647117 FITTINGS DOUG DC8 DC873F 302199FWP RT FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01840UP 46140 WHILE IN DALFORT FOR SERVICE, MAINTENANCE FOUND CRACKED RT FITTINGS, 3 ON TOP OF LONG 24, FS 879, 940, 960. REPLACED IAW EO DC8-5310-7191-A. 2L74 4F RT4A25 19950721001371995072100137WP 1995 7 21 UPS803843 119950713A53131415997 LONGERON DOUG DC8 DC871F 302199DWP FS 1650 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 32R AT FS 1650. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950721001381995072100138WP 1995 7 21 UPS803844 119950713A53134641324 LONGERON DOUG DC8 DC871F 302199DWP FS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON END FITTING AT L-32R AT FS 1690. REPLACED IAW SRM 51-1-20D. 2L74 4F RT4A25 19950721001391995072100139NM 1995 7 21 9510755529 119950715A3250 STEERING BOEING757 757251 1384970NM NLG MALFUNCTIONED A ANWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL01529US 23844 DURING INITIAL TAKEOFF POWER APPLICATION AFTER EPR WAS SET, THE AIRCRAFT TURNED HARD RIGHT ON THE RUNWAY. FULL LEFT RUDDER DID NOT CONTROL THE TURN, ALL ENGINE INDICATIONS WERE NORMAL. TAKEOFF WAS ABORTED. NO ASYMMETRY WAS NOTICED DURING TAXI OUT OR IN. RUNUP OF ENGINES TO 1.1 EPR DURING TAXI IN, INDICATED NORMAL FORWARD THRUST. CONTROL OF AIRCRAFT RETURNED TO IDLE POWER. CHECKED RIGGING OF TILLER AND RUDDER STEERING. OPERATIONAL CHECK OF REVERSERS AND BRAKES CHECKED NORMAL. 2L72 4F RTA2NM 19950721001401995072100140EU 1995 7 21 COM3117 119950715A61208210153 PCU SAAB SF340 SF340A 7850100EU RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01344CA15412431 340A025 RT PROPELLER RPM IS SLOW TO ACCELERATE WHEN POWER ADVANCED. REPLACED THE PROPELLER PITCH CONTROL. 2L72 4T RTA52EU 19950721001411995072100141EA 1995 7 21 COM60518 119950714A7931601509197 TRANSDUCER CNDAIRCL600 CL6002B19 EA LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01918CA4300 7018 LEFT ENGINE HAS NO OIL PRESSURE. REPLACED THE PRESSURE TRANSDUCER. 2L72 4F RTA21EA 19950721001421995072100142NM 1995 7 21 DL72E953080 119950715A5343 TRUNNION FITTING BOEING727 727247 138408FNM LT/RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 LIGHT FRETTING CORROSION ON BORES/CAPS AND FACES OF THE LT/RT TRUNNION FITTINGS. LIGHT CORROSION ON LWD BORE OF LT TRUNNION AFT CAP ATTACH BOLT HOLE. REPAIR PER M/M 53-40-0 FIG 811. FOUND A AT HMV. 2L73 4F A3WE 19950721001431995072100143NM 1995 7 21 DL72E953087 119950715A27821U1110 ACTUATOR BOEING727 727247 138408FNM NR 1 LE FLAP FAULTY A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO112826W 21331 ON CLIMB AFTER GEAR RETRACTION, NR 1 L/E KRUGER FLAP DID NOT RETRACT. FLIGHT RETURNED TO DFW. REPLACED NR 1 L/E FLAP ACTUATOR AND S202 POSITION SWITCH, OPERATION NORMAL. 2L73 4F A3WE 19950721001441995072100144NM 1995 7 21 DL72L953063 119950713A5720 ANGLE BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11511DA 21313 FOUND DURING A-2 LETTER CHECK, 1 INCH CRACK NR 11 SPOILER ACTUATOR SUPPORT FITTING I/B ATTACH ANGLE BELOW SUPPORT FITTING MOUNT BOLT. REPAIRED PER SRM 57-50-6 FIG 7. 2L73 4F A3WE 19950721001451995072100145NM 1995 7 21 DL72L953064 119950713A5712 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11511DA 21313 FOUND DURING A-2 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT ACT ATTACH I/B RIB. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721001461995072100146NM 1995 7 21 DL72L953065 119950713A5320 ANGLE BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11511DA 21313 FOUND DURING A-2 LETTER CHECK, CRACK IN ANGLE BL 8 LEFT STATION 1183 ON I/B RADIUS AT BOTTOM OF BULKHEAD SUPPORT ANGLE. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950721001471995072100147NM 1995 7 21 DL72S952935 119950628A5741 FITTING BOEING727 727232 1384082NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 AT HMV, LT FWD TERMINAL PIN BODY FITTING IS CORRODED IN SEVERAL AREAS. REPAIRED PER SRM 57-10-7. 2L73 4F A3WE 19950721001481995072100148NM 1995 7 21 DL72S953046 119950626A5330 SKIN BOEING727 727232 1384082NM FS 682 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 SKIN GOUGED FS 682 BETWEEN STR 21R AND 22R. REPAIRED PER SRM 53-30-3 FIG 3A. 2L73 4F A3WE 19950721001491995072100149NM 1995 7 21 DL72S953047 119950626A5330 SKIN BOEING727 727232 1384082NM VENTRAL STAIR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 AT HMV, FOUND TIME LIMITED REPAIR ON FUSELAGE SKIN AT RT FWD CORNER OF VENTRAL STAIR CUTOUT. INSTALLED NEW REPAIR PER MM 53-30-0 PG 803-804 FIG 802. 2L73 4F A3WE 19950721001501995072100150NM 1995 7 21 DL72S953048 119950627A5510 STRUCTURE BOEING727 727232 1384082NM HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 LIGHTENING HOLE, CRACKED AND BENT ABOVE AND TO THE LEFT OF THE ELEVATOR FEEL COMPUTER. REPAIRED PER SRM 55-10-4 PAGE 3 FIG 2. FOUND AT HMV. 2L73 4F A3WE 19950721001511995072100151NM 1995 7 21 DL72S953049 119950626A5313 STRINGER BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 STR 15L CRACKED AT FWD SIDE OF LT WING L/E ILLUMINATION LIGHT. REPAIRED PER SRM 53-10-3 FIG 2. FOUND AT HMV. 2L73 4F A3WE 19950721001521995072100152NM 1995 7 21 DL72S953050 119950625A5313 STRINGER BOEING727 727232 1384082NM FS 495 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 CORROSION ON STR 28R STA 495 FWD B/B. REPAIRED PER SRM 53-10-3 PG 3. FOUND AT HMV. 2L73 4F A3WE 19950721001531995072100153NM 1995 7 21 DL72S953051 119950703A5330 SKIN BOEING727 727232 1384082NM FS 495 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 CORROSION ON FUS SKIN AT STR 28R STA 495 FWD B/B. REPAIRED PER SRM 53-30-3 FIG 3. FOUND AT HMV. 2L73 4F A3WE 19950721001541995072100154NM 1995 7 21 DL72S953052 119950712A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 NR 3 SLAT COVE SKIN ANGLE CRACKED UNDER TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721001551995072100155NM 1995 7 21 DL72S953053 119950712A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 A .5 AND .25 CRACK ON NR 7 SLAT SUPPORT ANGLE BELOW TAI DUCT. FOUND DURING D-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721001561995072100156NM 1995 7 21 DL72S953075 119950714A33506104789 EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11517DA 21433 DURING LAY OVER, FOUND FWD DOOR ESCAPE SLIDE LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19950721001571995072100157NM 1995 7 21 DL72S953077 119950714A5754 NOSE RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11524DA 21584 FOUND DURING D-2 LETTER CHECK, NR 4 L/E SLAT ACT ATTACH RIB CRACKED 1.75 INCH I/B SIDE. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721001581995072100158NM 1995 7 21 DL72S953081 119950626A5400 SKIN BOEING727 727232 1384082NM NR 2 S-DUCT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV, FOUND CRACK IN SKIN INSIDE NR 2 ENG INLET S-DUCT. REPAIRED PER SRM 54-10-3 FIG 13. 2L73 4F A3WE 19950721001591995072100159NM 1995 7 21 DL72W952932 119950705A5754 RIBS BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND NR 4 L/E SLAT WITH RIB NR 1, 10, 13, 15 CRACKED. REPAIRED CRACKED RIBS PER MM 57-54-0. 2L73 4F A3WE 19950721001601995072100160NM 1995 7 21 DL72W952933 119950704A5754 ANGLE BOEING727 727247 138408FNM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721001611995072100161NM 1995 7 21 DL72W952934 119950705A5754 BRACKET BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 BRACKETS CRACKED, NR 2 KRUEGER FLAP ACTUATOR, O/B SUPPORT BRACKET AND I/B SUPPORT BRACKET. DYE CHECKED, FOUND NO DISCREPANCIES PER PS 900-6-301. 2L73 4F A3WE 19950721001621995072100162NM 1995 7 21 DL72W953079 119950714A5313BAC1498132 STRINGER BOEING727 727247 138408FNM FS 570 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, STR 27 L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER AS PER B-727 SRM 53-10-3. 2L73 4F A3WE 19950721001631995072100163NM 1995 7 21 DL73E953086 119950713A2170 COALESCER BAG BOEING737 737247 138448DNM AFT GALLEY DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11375DL 23602 ON TAKEOFF, HAD SMOKE OF UNKNOWN ORIGIN REPORTED FROM AFT GALLEY THROUGH 1000 FT ON CLIMB. SECURED PACKS, SMOKE ODOR STOPPED. FLIGHT RETURNED TO SLC. RAN ENGINES AT POWER, FOUND ONLY CONDENSATION COMING FROM VENTS. REPLACED COALESCER BAGS, RETURNED TO SERVICE. 2L72 4F A16WE 19950721001641995072100164NM 1995 7 21 DL757953010 119950707A5330 SKIN BOEING757 757232 1384965NM FUSELAGE LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11682DA 26958 FOUND DURING LETTER CHECK, LIGHTNING DAMAGE ON UPPER LT SIDE OF FUSELAGE, STARTING JUST FORWARD OF THE L-2 DOOR AND GOING PAST THE AFT OVER WING EXIT. BURNISHED AND DYE CHECKED ALL STRIKES, EXCEPT AT STATION 1000. OK TO TREAT AND PAINT ALL EXCEPT STA 1000 AND 1040. TREATED AND PAINTED, REWORKED RIVET HOLES AT STA 1000 AND 1040 PER SRM 53-00-01. OK TO INSTALL FASTENERS STA 1000 AND 1040. INSTALLED FASTENERS AND PAINTED REINSTALLED CEILING PANEL. 2L72 4F RTA2NM 19950721001651995072100165NM 1995 7 21 DL757953082 119950622A5751 SKIN 113N710057H BOEING757 757232 1384965NM LT AILERON DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11657DL 5358740 24419 TWO AREAS OF DELAMINATION; ONE AREA IS 1 ACROSS AND 44 FROM THE OUTBOARD END, THE OTHER IS A .5 DELAMINATION 15 FROM THE INBD END. ACCOMPLISHED REPAIRS PER SRM 57-60-01. FOUND DURING SHOP VISIT FOR LEFT WING AILERON. 2L72 4F RTA2NM 19950721001661995072100166WP 1995 7 21 DLL13953037 119950709A5320 CLIP LKHEED1011 10113851 5265010WP FS 549 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIP CORRODED FS 549 STR 34 TO 35. REMOVED DAMAGED FRAME TO SKIN CLIP AND INSTALLED NEW PER 53-12-0 FIG 817. 2L73 4F A23WE 19950721001671995072100167WP 1995 7 21 DLL13953038 119950709A5320 CLIPS LKHEED1011 10113851 5265010WP FS 629 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SKIN CLIP CORRODED FS 629 STR 34 TO 35. REMOVED AND FABRICATED NEW SKIN CLIPS. INSTALLED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721001681995072100168WP 1995 7 21 DLL13953039 119950710A5320 CLIP LKHEED1011 10113851 5265010WP FS 729 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SKIN CLIP CORRODED STA 729 STR 31 TO 35. REMOVED OLD CLIPS AND DRILLED NEW CLIPS AND SPLICES. INSTALLED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721001691995072100169WP 1995 7 21 DLL13953041 119950708A5320 CLIP LKHEED1011 10113851 5265010WP FS 789 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, INSPECTION FOUND THE SKIN CLIP CORRODED AT STA 789 BETWEEN STR 33 AND 35. REMOVED DAMAGED CLIP, INSTALLED NEW PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721001701995072100170WP 1995 7 21 DLL13953042 119950712A5320 CLIP LKHEED1011 10113851 5265010WP FS 809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, INSPECTION FOUND SKIN CLIP CORRODED AT STA 809 BETWEEN STR 30 AND 31. REMOVED DAMAGED CLIP AND INSTALLED NEW PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721001711995072100171WP 1995 7 21 DLL13953043 119950703A5320 CLIP LKHEED1011 10113851 5265010WP FS 669 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, INSPECTION FOUND SKIN CLIPS CORRODED AT STA 669 AFT SIDE BETWEEN STR 34 AND 35. ACCOMPLISHED REPAIRS PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950721001721995072100172WP 1995 7 21 DLL13953044 119950703A5320 CLIP LKHEED1011 10113851 5265010WP FS 669 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, INSPECTION FOUND SKIN CLIP CORRODED AT STA 669 FWD SIDE OF CLIP BETWEEN STR 34 AND 35. ACCOMPLISHED REPAIRS PER SRM 53-12-00 FIG 801. 2L73 4F A23WE 19950721001731995072100173WP 1995 7 21 DLL13953068 119950703A5330 DOUBLER LKHEED1011 10113851 5265010WP FS 1792-1809 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FAIL-SAFE STRAP DISBONDED AFT WASTE TANK COMPT. FAIL-SAFE STRAP DISBONDED AND BULKLED UP BETWEEN FS 1792 AND 1809. REMOVED STRAP DOUBLER AND REMOVED CORROSION, REPAIRED PER SRM 53-31-00. 2L73 4F A23WE 19950721001741995072100174WP 1995 7 21 DLL13953069 119950706A5711 SPAR LKHEED1011 10113851 5265010WP BS 1043 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 STA 1043 WING CTR SECTION INTERMEDIATE SPAR IS CRACKED AT THE UPPER CAP ON THE LT END. REPAIRED PER SRM 57-11-00. 2L73 4F A23WE 19950721001751995072100175WP 1995 7 21 DLL13953070 119950703A5330 SKIN LKHEED1011 10113851 5265010WP FS 509 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FUSELAGE SKIN DENTED FS 509 STRINGER 33 AND 34. REMOVED DAMAGED SKIN, DRILLED UP DOUBLERS FILLER REPAIRED PER ERA 271314-14. FOUND AT HMV. 2L73 4F A23WE 19950721001761995072100176WP 1995 7 21 DLL13953071 119950706A5320 HAT CHANNEL LKHEED1011 10113851 5265010WP CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 HAR CHANNEL AT DOOR OPENING OF LT FIRST CLASS LAV IS CORRODED. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950721001771995072100177WP 1995 7 21 DLL13953072 119950702A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FLOOR SUPPORT CORRODED C-2 B/B FS 1545 LBL 33. REMOVED FIXED FLOOR PANEL, INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00. 2L73 4F A23WE 19950721001781995072100178WP 1995 7 21 DLL13953073 119950702A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 1545 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FLOOR SUPPORT DAMAGED C-2 B/B FS 1545 LBL 50. REMOVED FLOOR SUPPORT, INSTALLED NEW FLOOR SUPPORT PER SRM 53-23-00. FOUND AT HMV. 2L73 4F A23WE 19950721001791995072100179WP 1995 7 21 DLL13953078 119950704A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FLOORBEAM UPPER CAP CORRODED MANY AREAS STA 901 FROM RBL 116 TO LBL 116. ACCOMPLISHED REPAIRS PER SRM 53-21-00 PG 849 FIG 823. FOUND AT HMV. 2L73 4F A23WE 19950721001801995072100180NM 1995 7 21 DLM11953084 119950714A25304110001137 COFFEE MAKER DOUG MD11 MD11 3023602NM GALLEY SMOKING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11803DE 48474 DURING CRUISE, BUSINESS CLASS GALLEY AFT COFFEE MAKER BEGAN TO SMOKE AND POP, THEN WATER STARTED TO LEAK. SHUT OFF POWER AND WATER TO MAKER. DISPENSER WAS INITIALY DEFERRED, THEN REPLACED AT PDX. 2L73 4F RTA22WE 19950721001811995072100181NM 1995 7 21 DLM11953085 119950714A26122215561503 FIRE LOOP DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 2 ENGINE FAULTY A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11810DE 48565 723955 AFTER TAKOFF, HAD FIRE BELL AND LIGHTS FOR NR 2 ENGINE. WARNING CEASED, WHEN POWER WAS REDUCED, RETURNED ATL. REPLACED PYLON LOOP A-HARNESS AND LT AND RT REVERSER LOOP AND B-ASSEMBLIES. ALSO, REPLACED UPPER PYLON FIRE LOOP A AND B. OPERATAION NORMAL. 2L73 4F4 FRTA22WE E24NE 19950721001821995072100182NM 1995 7 21 DLM88953066 119950713A5320 ANGLE DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11959DL 49978 FOUND DURING F-1 LETTER CHECK, KEEL BEAM AFT ANGLE CRACKED, CROSSOVER AFT SIDE OF MLG WHEEL WELL. REPAIRED PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950721001831995072100183NM 1995 7 21 DLM88953076 119950714A5330 SKIN DOUG MD88 MD88 3023688NM LT NOSE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11935DL 49722 FOUND DURING A-1 LETTER CHECK, .5 INCH LONG CRACK FOUND ON FUSELAGE SKIN AT THE AFT HINGE CUTOUT OF LT NOSE WHEEL WELL DOOR. REPAIRED PER SRM 53-05 FIG 62. 2L72 4F RTA6WE 19950721001841995072100184NE 1995 7 21 ERA00010 219950714A8530CP84083 NR 3 CYLINDER DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183075 52020NE RT ENG FAILED A ERAAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 AL031944M 118 19394 BP600421 RT ENGINE EMITTING GRAY SMOKE ON CLIMB FROM ANC. F/F LOW, SPUTTERING AND DETONATION, SHUTDOWN RT ENGINE AND MADE UNEVENTFUL LANDING AT ANC. REPLACED NR 3 CYLINDER AND CHECKED OIL SCREENS. GROUND OPS CHECK GOOD. 2L72 4R4 R A669 5E4 19950721001851995072100185NM 1995 7 21 P5CA9500401 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 540 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN ANGLE ON BS 540 BETWEEN S39R AND S40R. MANUFACTURED NEW ANGLE PER BOEING SRM 51-10-21 AND 51-30-02. 2L74 4F A20WE 19950721001861995072100186NM 1995 7 21 P5CA9500402 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 570 DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DENT ON INTERCOSTAL BS 570 BETWEEN LBL 45 AND RBL 45. REPAIRED PER BOEING SRM 51-40-03 FIG 1. 2L74 4F A20WE 19950721001871995072100187NM 1995 7 21 P5CA9500403 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 620-640 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON UPPER FLOORBEAM IN CARGO COMPARTMENT BETWEEN BS 620 AND 640 NEAR CENTER. REPAIRED PER BOEING SRM 51-40-02 FIG 1. 2L74 4F A20WE 19950721001881995072100188NM 1995 7 21 P5CA9500404 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 640-660 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND CORROSION ON ANGLE BETWEEN BS 640 AND 660, BETWEEN RBL 30 AND RBL 45. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950721001891995072100189NM 1995 7 21 P5CA9500405 119950630A5320 FITTING BOEING747 747121 1384871NM BS 660 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FITTING BS 660 AT RBL 30. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721001901995072100190NM 1995 7 21 P5CA9500406 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 820/840 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S44L BETWEEN BS 820 AND 840. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721001911995072100191NM 1995 7 21 P5CA9500407 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON S37L BS 1000. REPAIRED PER BOEING SRM 53-10-03 AND 51-30-02. 2L74 4F A20WE 19950721001921995072100192NM 1995 7 21 P5CA9500408 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1287 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 ANGLE BROKEN AT BS 1287 UNDER BEAM RBL 112. REPLACED ANGLE PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950721001931995072100193NM 1995 7 21 P5CA9500409 119950630A5330 SKIN BOEING747 747121 1384871NM BS 2160 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR AND DAMAGE IN BULK CARGO WALL AT BS 2160. REPAIRED PER BOEING SRM 51-40-02 FIG 4. 2L74 4F A20WE 19950721001941995072100194NM 1995 7 21 P5CA9500410 119950630A5320 WEB BOEING747 747121 1384871NM BS 1520 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR IN THE WEB BS 1520 BOTTOM TO UPPER CHORD ABOE S48L AND S49L. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950721001951995072100195NM 1995 7 21 P5CA9500411 119950630A5210 HINGE BOEING747 747121 1384871NM R2 DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN R2 DOOR LOWER HINGE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721001961995072100196NM 1995 7 21 P5CA9500412 119950630A5210 STOP BOEING747 747121 1384871NM 3L DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION 3L DOOR STOP 5. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721001971995072100197NM 1995 7 21 P5CA9500413 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 1285 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON BRACKET CONNECTING INTERCOSTAL TO FRAME BS 1285 S26L WL 198. REPAIRED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721001981995072100198NM 1995 7 21 P5CA9500414 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 2230 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION BS 2230 AT BRACKET FROM FRAME TO INTERCOSTAL S26L WL 198. MANUFACTURED NEW PART PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721001991995072100199NM 1995 7 21 P5CA9500415 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1980/1960 OPEN HOLES A P5CAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP23831FT 19648 S46L HAS OPEN HOLES BETWEEN BS 1980 AND 1960. INSTALLED FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950721002001995072100200NM 1995 7 21 P5CA9500416 119950630A5320 CLIP BOEING747 747121 1384871NM BS 1880 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON CLIP BS 1880 S13R. REMOVED CORROSION PER SRM 51-10-01. 2L74 4F A20WE 19950721002011995072100201NM 1995 7 21 P5CA9500417 119950630A5320 CLIP BOEING747 747121 1384871NM BS 1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON CLIP BS 1920 S14R. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002021995072100202NM 1995 7 21 P5CA9500418 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 420 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON INTERCOSTAL BS 420 S30R. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002031995072100203NM 1995 7 21 P5CA9500419 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 480-500 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON INTERCOSTAL BS 480 TO 500 S30R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721002041995072100204NM 1995 7 21 P5CA9500420 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 2140-2200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SEAT TRACK BETWEEN BS 2140 AND 2200 AND LBL 98. REMOVED THE CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002051995072100205NM 1995 7 21 P5CA9500421 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 2140 GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 GOUGES IN SEAT TRACK BS 2140 RBL 11. REPLACED SEAT TRACK PER IAI EO MF-MAN-B47-53-83975. 2L74 4F A20WE 19950721002061995072100206NM 1995 7 21 P5CA9500422 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 2240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SEAT TRACK AT BS 2240 LBL 33. REMOVED THE CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS SRM 53-10-01. 2L74 4F A20WE 19950721002071995072100207NM 1995 7 21 P5CA9500423 119950630A5320 STRAP BOEING747 747121 1384871NM BS 747-760 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN STRAP BETWEEN BS 747 AND 760 ABOVE S36L. MANUFACTURED NEW STRAP PER BOEING SRM 53-10-21 AND 51-30-02. 2L74 4F A20WE 19950721002081995072100208NM 1995 7 21 P5CA9500424 119950630A5320 STRAP BOEING747 747121 1384871NM BS 840 MISINSTALLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 REPAIR NOT PER CURRENT SRM ON STRAP AT BS 840 LT. REPLACED PER BOEING SRM 53-10-21. 2L74 4F A20WE 19950721002091995072100209NM 1995 7 21 P5CA9500425 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 940/960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S36R BETWEEN BS 940 AND 960. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002101995072100210NM 1995 7 21 P5CA9500426 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 860-880 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON INTERCOSTAL AND A DENT ON ANGLE ABOVE INTERCOSTAL AT S34R BETWEEN BS 860 AND 880. REPAIRED PER BOEING SRM 51-40-02 FIG 1. 2L74 4F A20WE 19950721002111995072100211NM 1995 7 21 P5CA9500427 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 760 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR ON S35R BS 760. REPAIRED PER BOEING SRM 53-10-03 FIG 1. 2L74 4F A20WE 19950721002121995072100212NM 1995 7 21 P5CA9500428 119950630A5230 ANGLE BOEING747 747121 1384871NM CARGO DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED ANGLE BULK CARGO DOOR INTERNAL AT AFT LOWER CORNER. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721002131995072100213NM 1995 7 21 P5CA9500429 119950630A5414 SKIN BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK NR 2 PYLON OUTER SKIN NS 221. REPAIRED PER IAI EO MAN-747-54-83978. 2L74 4F A20WE 19950721002141995072100214NM 1995 7 21 P5CA9500430 119950630A5720 FITTING BOEING747 747121 1384871NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION UNDER FITTINGS AT WBL 584 AND 743 RIGHT WING ON LOWER SURFACE SKIN. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721002151995072100215NM 1995 7 21 P5CA9500431 119950630A5720 FITTING BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION UNDER FITTING AT WBL 584. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01. 2L74 4F A20WE 19950721002161995072100216NM 1995 7 21 P5CA9500432 119950630A5320 BRACKETS BOEING747 747121 1384871NM BS 1900-1920 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO BROKEN BRACKETS ATTACHED TO INTERCOSTAL BETWEEN FRAME BS 1900 AND 1920 LBL 25. REPLACED PER BOEING SRM 51-10-23 AND 51-30-02. 2L74 4F A20WE 19950721002171995072100217NM 1995 7 21 P5CA9500433 119950630A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 1900-1920 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR AND CORROSION ON INTERCOSTAL BETWEEN FRAME BS 1900 AND 1920, BETWEEN LBL 7.5 AND LBL 375. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950721002181995072100218NM 1995 7 21 P5CA9500434 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 1900-1920 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN BRACKET ATTACHING INTERCOSTAL BETWEEN BS 1900 AND 1920 BL 0. REPAIRED PER BOEING 51-40-04. 2L74 4F A20WE 19950721002191995072100219NM 1995 7 21 P5CA9500435 119950630A5230 HINGE BOEING747 747121 1384871NM AFT CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN THE LOWER AFT CARGO DOOR HINGE SEGMENTS. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER SRM 53-10-01. 2L74 4F A20WE 19950721002201995072100220NM 1995 7 21 P5CA9500436 119950630A5320 WEB BOEING747 747121 1384871NM BS 2280 OIL CAN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 OIL CAN IN THE WEB AT BS 2280 RIGHT ABOVE S36R AND S38R. REPAIRED PER BOEING SRM 53-10-04. 2L74 4F A20WE 19950721002211995072100221NM 1995 7 21 P5CA9500437 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 2200-2220 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN ANGLE AT BS 2220 TO 2200 S26L WL 198. REMOVED THE CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002221995072100222NM 1995 7 21 P5CA9500438 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 855-860 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION S26R BS 855 TO 860. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002231995072100223NM 1995 7 21 P5CA9500439 119950630A572069B123025 MOUNT BRACKET BOEING747 747121 1384871NM NR 2 SKIRT BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 2 SKIRT FORWARD MOUNTING BRACKET IS BROKEN. INSTALLED NEW FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950721002241995072100224NM 1995 7 21 P5CA9500440 119950630A572069B123026 MOUNT BRACKET BOEING747 747121 1384871NM NR 3 SKIRT BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 3 SKIRT FORWARD MOUNTING BRACKET IS BROKEN. INSTALLED NEW FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950721002251995072100225NM 1995 7 21 P5CA9500441 119950630A5312 LAP SPLICE BOEING747 747121 1384871NM AFT PRESS BLKHD CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO INDICATIONS (LFEC) OF CRACKS OR CORROSION ON AFT PRESSURE BULKHEAD LAP SPLICE. REMOVED CORROSION BETWEEN LAP PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002261995072100226NM 1995 7 21 P5CA9500442 119950630A5210 ANGLE BOEING747 747121 1384871NM NR 4L DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON ANGLE AND BROKEN ANCHOR NUT DOOR NR 4L LOWER SCRUFF. REPLACED ANGLE PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721002271995072100227NM 1995 7 21 P5CA9500443 119950630A5532 LE PANEL BOEING747 747121 1384871NM VERT STAB DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUR DENTS ON VERTICAL FIN LEADING EDGE PANEL. BLENDED OUT DAMAGE PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721002281995072100228NM 1995 7 21 P5CA9500444 119950630A5280 DOOR BOEING747 747121 1384871NM NLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED AND SHEARED RIVET RIGHT NOSE GEAR STRUT DOOR. REPAIRED PER BOEING SRM 51-40-03 FIG 1. 2L74 4F A20WE 19950721002291995072100229NM 1995 7 21 P5CA9500445 119950630A5280 DOOR BOEING747 747121 1384871NM NLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS AND DENTS ON LEFT NOSE GEAR STRUT DOOR. REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950721002301995072100230NM 1995 7 21 P5CA9500446 119950630A5280 DOOR BOEING747 747121 1384871NM NLG DENTED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO DENTS IN THE RIGHT NOSE GEAR DOOR. REPAIRED PER BOEING SRM 52-80-02. 2L74 4F A20WE 19950721002311995072100231NM 1995 7 21 P5CA9500447 119950630A5753 PANEL BOEING747 747121 1384871NM NR 1 TE MIDFLAP SEPARATION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NR 1 MIDFLAP LEADING EDGE PANEL HAS SEPARATION. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950721002321995072100232NM 1995 7 21 P5CA9500448 119950630A524065B162121 BRACKET BOEING747 747121 1384871NM CREW SERV DOOR BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CREW SERVICE DOOR FORWARD BOTTOM SIDE SUPPORT STOP BRACKET BROKEN. REPLACED BRACKET PER BOEING OVERHAUL MANUAL 52-13-11. 2L74 4F A20WE 19950721002331995072100233NM 1995 7 21 P5CA9500449 119950630A5240 SKIN BOEING747 747121 1384871NM CREW SERV DOOR BENT A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CREW SERVICE DOOR AFT LOWER CORNER OUTER SKIN BENT. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950721002341995072100234NM 1995 7 21 P5CA9500450 119950630A5350 SUPPORT BOEING747 747121 1384871NM BS 1394 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN FAIRING SUPPORT AT FUSELAGE RIGHT SIDE AT BS 1394 AREA ABOVE WING. REPLACED SUPPORT PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950721002351995072100235NE 1995 7 21 P5CA9500451 219950716A7260JT9D7A GEAR BOX BOEING747 747132 1384882NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE FROZEN A P5CAD RETURN TO BLOCK O OTHER ININSP/MAINT 1 WP23857FT67748173 20246 662239 A/C PUSHED OUT FOR ENGINE START, NR 4 ENGINE WOULD NOT START. FOUND THAT GEAR BOX WOULD NOT TURN. ENGINE REPLACED. 2L74 4F4 F A20WE E20EA 19950721002361995072100236NM 1995 7 21 P5CA9500452 119950716A3231 CONTROL CABLE BOEING747 747122 1384872NM LT MLG WW BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 DURING POST FLIGHT INSPECTION, FOUND LEFT BODY GEAR DOOR GROUND RELEASE CABLE BROKEN. REPLACED CABLE. 2L74 4F A20WE 19950721002371995072100237NM 1995 7 21 SCNA95147 119950712A33501619 EEL LAMP BOEING727 7272A1 138407FNM L-2 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15286SC 21601 FOUND THE L-2 EMERGENCY SLIDE LIGHT INOPERATIVE. RELAMPED THE L-2 DOOR EMERGENCY SLIDE LIGHT. OPS CHECKED GOOD. 2L73 4F A3WE 19950721002381995072100238NM 1995 7 21 UPS203869 119950717A5313 STRINGER BOEING727 72730C 1384009NM BS 484 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER FLANGE AT BS 484, STR 24 LT WL 157. REPAIRED IAW SRM 53-10-6, 53-10-3, 51-30-2. 2L73 4F A3WE 19950721002391995072100239NM 1995 7 21 UPS203870 119950717A57206516200109 STIFFENER BOEING727 72730C 1384009NM WS 553 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 553 ON L/W L/E. REPLACED IAW SRM 51-30-2, M/M 36-00-01. 2L73 4F A3WE 19950721002401995072100240NM 1995 7 21 UPS203871 119950717A57206516200115 STIFFENER BOEING727 72730C 1384009NM WS 598 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 598 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2. 2L73 4F A3WE 19950721002411995072100241NM 1995 7 21 UPS203872 119950717A57206516200115 STIFFENER BOEING727 72730C 1384009NM WS 594 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED VERTICAL STIFFENER AT FS 594 ON L/W L/E. REPLACED IAW SRM 51-30-2, 51-20-4, 51-10-2. 2L73 4F A3WE 19950721002421995072100242NM 1995 7 21 UPS203873 119950717A571265173335 RIB BOEING727 72730C 1384009NM WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON SLAT TRACK ON O/B SIDE. REPLACED IAW SRM 57-51-31 AND 51-30-2. 2L73 4F A3WE 19950721002431995072100243NM 1995 7 21 UPS203874 119950717A57116595600763 SPAR BOEING727 72730C 1384009NM WS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01918UP 19008 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LOWER FRONT SPAR CHORD AT STA 740 WL 167 LBL 37. REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 19950721002441995072100244NM 1995 7 21 UPS203880 119950717A5320 INTERCOSTAL BOEING727 72730C 1384009NM BS 1110-1130 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED INTERCOSTAL AT BS 1110 TO 1130 RBL 6 WL 152. REPLACED IAW SRM 53-10-2, 51-20-21, 51-10-2, M/M 51-20-00. 2L73 4F A3WE 19950721002451995072100245NM 1995 7 21 UPS203881 119950717A5320 ANGLE BOEING727 72730C 1384009NM BS 296 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SUPPORT ANGLE AT BS 296 LBL 14 WL 180. REPLACED IAW SRM 51-10-6, 53-10-1, 51-30-5, 51-10-2, 51-30-2, 51-20-4. 2L73 4F A3WE 19950721002461995072100246NM 1995 7 21 UPS203882 119950717A5753652962526 END CAP BOEING727 72730C 1384009NM RT TE FOREFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RIGHT WING O/B FOREFLAP I/B END CAP CRACKED ON UPPER SURFACE. REPLACED IAW SRM 51-30-2, 51-10-2. 2L73 4F A3WE 19950721002471995072100247NM 1995 7 21 UPS403883 119950717A5330 SKIN BOEING747 747SR46 NM BS 560 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LOWER FUSELAGE EXTERNAL SKIN DAMAGED AT STA 560 LT SIDE STRINGER 43. REPAIRED IAW SRM 53-30-03. 2L74 4F A20WE 19950721002481995072100248NM 1995 7 21 UPS403884 119950717A5414 SKIN BOEING747 747SR46 NM NR 4 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON OUTER SKIN OF PYLON NR 4 OF ACCESS PANEL AT STA 195, LT. REPAIRED IAW SRM 54-30-03. 2L74 4F A20WE 19950721002491995072100249NM 1995 7 21 UPS403885 119950717A5414 SKIN BOEING747 747SR46 NM NR 4 PYLON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DAMAGE ON OUTER SKIN OF PYLON NR 4 AT STA 210. REPAIRED IAW SRM 54-30-03. 2L74 4F A20WE 19950721002501995072100250WP 1995 7 21 UPS803876 119950714A3260 GEAR IND DOUG DC8 DC873F 302199FWP LANDING GEAR MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01807UP 46007 AFTER TAKEOFF, THE GEAR NOT LATCHED LIGHT ILLUMINATED. PERFORMED THE CHECKLIST AND SHORTLY THEREAFTER THE DOORS NOT LATCHED LIGHT ILLUMINATED, FINISHED CHECKLIST. PROCEEDED TO DESTINATION AT MACH .65. INSPECTED SYSTEM, FOUND NO DEFECTS. LUBED LANDING GEAR AND UPLOCKS. PERFORMED SEVERAL GEAR SWINGS AND OPERATED NORMALLY IAW M/M 32-33-00. 2L74 4F RT4A25 19950721002511995072100251WP 1995 7 21 UPS803877 119950714A33505708458503 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01713UP 46014 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, GROUND CHECKS NORMAL. 2L74 4F RT4A25 19950721002521995072100252 1995 7 21 UPS803878 419950714A256557501131 CONTAINER DOUG DC8 DC871F 302199DWP ESCAPE SLIDE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45979 WHILE ON GROUND, MAINTENANCE FOUND ESCAPE SLIDE CONTAINER CLIP BROKEN. REMOVED AND REPLACED ESCAPE SLIDE CONTAINER. 2L74 4F RT4A25 19950721002531995072100253NM 1995 7 21 UPS803879 119950716A33505106 EEL BATTERY BOEING727 72725C 138400HNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01946UP 19721 WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT FAILS TEST. REPLACED BATTERIES, OPS CHECK OK. 2L73 4F A3WE 19950721002541995072100254EA 1995 7 21 95ZZZX3414 219950624A72613020908 FILLER CAP DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043EA LT ENGINE LOOSE A ASWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP07331SA 3337 PCE51580 CREW FEATHERED LEFT ENGINE IN-FLIGHT DUE TO LOW OIL PRESSURE. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITH LEFT ENGINE AT IDLE POWER AND LANDED. MAINTENANCE PERSONNEL FOUND OIL FILLER CAP ON ENGINE NOT SECURED. 1H72 3T4 T A9EA E4EA 19950721002551995072100255 1995 7 21 95ZZZX3415 419950617A34181675 LIFT DETECTOR DHAV DHC6 DHC6300 EA LT WING LE FAILED A ASWAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP07228SA 253 FLIGHT CREW REPORTED THAT STALL WARNING CAME ON IN-FLIGHT AND REMAINED ON. MAINTENANCE CREW REPLACED INBOARD STALL WARNING SWITCH (LIFT DETECTOR) DUE TO AN INTERNAL SHORT AND AIRCRAFT WAS RELEASED AFTER A SUCCESSFUL TEST FLIGHT. THIS OPERATOR HAS FOUND THIS STALL WARNING SWITCH TO BE SUSCEPTIBLE TO FAILURE ESPECIALLY AFTER PREVIOUS REPAIR. REMOVED SWITCH HAD 570.4 HOURS SINCE PREVIOUS REPAIR BY SAFE FLIGHT. IT IS SUSPECTED THAT MOISTURE CAUSES PREMATURE FAILURES. 1H72 3T A9EA 19950721002561995072100256CE 1995 7 21 95ZZZX3416 119950622A27201015240381 TORQUE SHAFT ARM BEECH 1900 1900D 1154162CE RUDDER LOOSE AS JJBAK NONE O OTHER ININSP/MAINT 1 EA01832CA5573 UE22 RUDDER TORQUE SHAFT ARM, MOUNTING RIVETS (8) LOOSE. 2L72 4T RTA24CE 19950721002571995072100257WP 1995 7 21 95ZZZX3417 119950616A323136548875001 CONTROL VALVE DOUG DC8 DC851 3021920WP MLG DOOR FAILED A TC8AO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23805CK 45649 DFW/YIP - LANDING GEAR WOULD NOT RETRACT. AFTER SEVERAL TRIES, GEAR CAME UP. REMOVED AND REPLACED MAIN GEAR DOOR MANUAL CONTROL VALVE IAW DACA MM 32-4-8. OPS CHECKED GEAR THROUGH SEVERAL CYCLES, SYSTEM OPS CHECKS GOOD IAW 32-7-0. 2L74 4F 4A25 19950721002581995072100258NE 1995 7 21 95ZZZX3418 219950711A7230 COMPRESSOR AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE LT ENGINE FAILED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0942836 200 120525 IAH - FLT 2597 - AFTER TAKEOFF FROM IAH, COCKPIT STARTED TO FILL WITH SMOKE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. AIRCRAFT WAS TEST FLOWN AFTER ENGINE REPLACEMENT WITH NO DISCREPANCIES. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (REF JIC 72-00-00) AND COEX TEST FLIGHT FORM M-630. ENGINE CHECKED IN SHOP AND FOUND EXCESSIVE OIL IN COMPRESSOR SECTION. (X) 2H72 4T4 TRTA53EU E20NE 19950721002591995072100259SO 1995 7 21 C2XA95CL101 119950702A523012023120001 SEAL EMB 120 EMB120RT SO CARGO DOOR RIPPED A C2XAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW0916724 120171 CLE/ABE - FLT 3320 - CABIN LOST PRESSURE AT FL 230. CABIN STABILIZED AT 7,000 FEET DESCENDING THROUGH FL 180. USED MANUAL MODE FOR DESCENT. MAINTENANCE REMOVED AND REPLACED CARGO DOOR SEAL TRIM IAW EMB 120 MM 52-30-01. OPS CHECKED GOOD IAW 21-30-00. AIRCRAFT REETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950721002601995072100260SO 1995 7 21 C2XA95CL102 119950709A32502050000001 POTENTIOMETER EMB 120 EMB120RT SO NOSE GEAR OUT OF ADJUST A AC2XAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW0915725 120173 CLE-CVG - FLT 3263 - DURING TAKEOFF ROLL, EXTREME RIGHT RUDDER PEDAL PRESSURE WAS REQUIRED TO MAINTAIN DIRECTIONAL CONTROL. ONCE AIRBORNE PEDAL STEER INOP LIGHT CAME ON AND COULD NOT EXTINGUISH. RETURNED TO CLEVELAND. MAINTENANCE ADJUSTED STEERING FEEDBACK POTENTIOMETER, OPS CHECKED GOOD. ALL WORK IAW EMB MM 32-50-00. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19950721002611995072100261EU 1995 7 21 C2XA95IA113 119950706A5210S217600101200 PASSENGER DOOR AEROSPATR42 ATR42320 8680930EU FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0942836 200 IAH - DURING A 6C INSPECTION, THE PASSENGER/CREW DOOR WAS FOUND CORRODED IN SEVERAL AREAS BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 19950721002621995072100262EU 1995 7 21 C2XA95IA115 119950709A335044 EEL LAMP AEROSPATR42 ATR42320 8680930EU CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0915818 153 IAH - DURING 1A INSPECTION, FOUND RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED BURNED OUT BULB. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 19950721002631995072100263NM 1995 7 21 CAL950496 119950616A3350 EEL BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0976753 21249 EWR - FLT 0623 - INSPECTION FOUND EMERGENCY EXIT LIGHT AT LEFT AFT SERVICE DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (X) 2L73 4F A3WE 19950721002641995072100264WP 1995 7 21 ORJA9548 119950605A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC987 3022087WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11752RA 49780 FORWARD EMERGENCY DOORS OVERHEAD LAMPS DIM. REMOVED AND REPLACED FORWARD EMERGENCY OVERHEAD LAMPS BATTERY PER ATA 33. OPS CHECK GOOD. (X) 2L72 4F RTA6WE 19950721002651995072100265EU 1995 7 21 VTZA95214 119950701A281014128007402 NEGATIVE G-TANK JETAIRJETSTMJETSTM4101 1500501EU RT WING CRACKED A AVTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA27311UE 41029 IAD/BDL - FLT 6517 - RETURNED TO IAD DUE TO THE RT ENGINE FUEL PRESSURE DROPPING TO ZERO, WITH THE STANDBY PUMP HOLDING 18 PSI. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INVESTIGATED AND FOUND THE RT NEGATIVE G-TANK WAS CRACKED. MAINTENANCE IS CURRENTLY AWAITING A REPAIR SCHEME FROM THE MANUFACTURER. MAINTENANCE REMOVED, REPAIRED, AND REINSTALLED THE RT NEGATIVE G-TANK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950721002661995072100266NE 1995 7 21 WRLA95032 219950629A73107883994 SHUT-OFF VALVE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NR 1 ENGINE FAILED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27274WA 48633 DURING TAXI, CREW OBSERVED 'FADEC MAINTENANCE ALERT' ON NR 1 ENGINE. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL IDENTIFIED AIR/OIL COOLER SHUT-OFF VALVE FAILED. REPLACED SHUT-OFF VALVE. ENGINE GROUND RUN, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F4 FRTA22WE E24NE 19950721002671995072100267NM 1995 7 21 WRLA95033 119950702A2910AVZ4E11504 SHUT-OFF VALVE DOUG MD11 MD11 3023602NM 2/3 HYD SYS FAILED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27280WA 48458 DURING TAXI, CREW RECEIVED 2/3 HYDRAULIC REVERSIBLE MOTOR PUMP DISAGREE ALERT. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING IDENTIFIED 2/3 HYDRAULIC REVERSIBLE MOTOR PUMP SHUT-OFF VALVE INOPERATIVE. REMOVED AND REPLACED SHUT-OFF VALVE. GROUND RUN - NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950721002681995072100268EU 1995 7 21 WTAA950208B 119950611A6120S9413012 O-RING BAG JETSTMJETSTM3101 1500215EU LT ENGINE LEAKING A WTAADE RETURN TO BLOCK ENGINE SHUTDOWN BJKSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FLUID LOSS TXTAXI/GRND HDL 1 WP17419UE 779 SFO - LEFT ENGINE LOW OIL PRESSURE INDICATION REPORTED ACCOMPANIED BY THE REPORT OF SMOKE ODOR IN CABIN DURING TAXI OUT. CREW SECURED LEFT ENGINE AND RETURNED TO GATE. MAINTENANCE FOUND OIL LEAKING AT LEFT ENGINE BETA TUBE O-RINGS AND PROPELLER DOME SEAL. REPLACED O-RINGS AND DOME SEAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19950721002691995072100269EU 1995 7 21 WTAA950210 119950610A3244175K882 TIRE BAG JETSTMJETSTM3101 1500215EU NLG FAILED A WTAAO OTHER O OTHER TXTAXI/GRND HDL 1 WP17428UE 806 FAT - DURING MAINTENANCE TAXI CHECK FOR REPORTED LEFT ENGINE TORQUE FLUCTUATION, LEFT AND RIGHT NOSE TIRE FAILURE OCCURRED AT APPROXIMATELY 60 KNOTS. MAINTENANCE CREW MAINTAINED DIRECTIONAL CONTROL OF AIRCRAFT AND EXITED THE RUNWAY ON HIGH SPEED TAXIWAY. CREW SECURED ENGINES AND NOTIFIED EMERGENCY EQUIPMENT ONCE CLEAR OF RUNWAY. DAMAGE TO NOSEWHEELS, NOSE GEAR AND GEAR DOOR, LEFT PROPELLER AND FUSELAGE NOTED DURING INSPECTION OF AIRCRAFT. REPAIRED DAMAGE AND REPLACED COMPONENTS AS REQUIRED. AIRCRAFT RETURNED TO SERVICE. NOTE, THE SUBJECT NOSE TIRES WERE RETREADED TIRES. (X) 2L72 4T RTA21EU 19950721002701995072100270NE 1995 7 21 WTAA950223 219950629A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT/RT OVERTORQUED A WTAAO OTHER J WARNING INDICATION APAPPROACH 1 WP17280UE 120090 SFO - LEFT AND RIGHT ENGINE OVERTORQUE REPORTED DURING ENCOUNTER WITH AIRCRAFT (B757) WAKE TURBULENCE DURING APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINES, PROPELLER ASSEMBLIES FOR OVERTORQUE CONDITION AND AIRFRAME FOR SEVERE TURBULENCE. NO DEFECTS NOTED. REMOVED PROPELLERS FOR DETAILED INSPECTION. NO DEFECTS REPORTED FOLLOWING PROPELLER ASSEMBLY TEAR-DOWN. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA31SO E20NE 19950721002711995072100271WP 1995 7 21 9510769942 119950711A3260 DOOR LIGHT DOUG DC9 DC932 3022066WP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL013991C 47175 DURING CLIMBOUT FROM YUL, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. CYCLED MAIN GEAR DOORS SEVERAL TIMES, ALL CHECKED OK. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950721002721995072100272WP 1995 7 21 9510779958 119950713A3260 DOOR SWITCH DOUG DC9 DC931 3022065WP LT MLG OUT OF ADJUST A NWAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL01917RW 47175 DURING APPROACH INTO RAP, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. ADJUSTED LEFT MAIN GEAR DOOR SWITCH, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950721002731995072100273WP 1995 7 21 9510789752 119950714A3620 FLAPPER VALVE DOUG DC9 DC941 302207NWP RT TEMP SENSOR LACK OF LUBE A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01752NW 47116 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER DEPARTURE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND FLAPPER VALVE IN RIGHT HIGH TEMPERATURE SENSOR STUCK CLOSED. LUBED SWITCH, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950721002741995072100274WP 1995 7 21 9510799953 119950713A7933 TEMP SENSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D15 52051NE NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01918RW 47158 657545 CLIMBOUT OF MSP, THE NR 1 ENGINE OIL TEMPERATURE WAS FLUCTUATING AND SEEMED TO STABILIZE AT 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR, SYSTEM OPERATION APPEARED TO BE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950721002751995072100275NM 1995 7 21 9510802203 119950715A3150 AURAL WARNING BOEING727 727251 138408HNM FLIGHT DECK SOUNDED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01203US 22543 DURING APPLICATION OF TAKEOFF THRUST WITH FLAPS 5 SELECTED, AURAL WARNING HORN SOUNDED, ABORTED TAKEOFF. SECOND DEPARTURE ATTEMPT WAS NORMAL. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION. 2L73 4F A3WE 19950721002761995072100276WP 1995 7 21 9510819953 119950713A7933 CONNECTOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D15 52051NE NR 1 OIL TEMP MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01918RW 47158 657545 CLIMBING OUT OF MSP, THE NR 1 OIL TEMPERATURE INDICATED 170 DEGREES, THEN BEGAN FLUCTUATING BETWEEN 100 TO 170 DEGREES. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE CANNON PLUG ON THE OIL TEMPERATURE SENSOR, SYSTEM CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950721002771995072100277NM 1995 7 21 9510822204 119950715A3150 AURAL WARNING BOEING727 727251 138408HNM FLIGHT DECK SOUNDED A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01204US 22544 WEAK AURAL WARNING HORN SOUNDED ON TAKEOFF WITH 15 DEGREE FLAP SETTING, ABORTED TAKEOFF. SECOND DEPARTURE WAS NORMAL. MAINTENANCE REPLACED AURAL WARNING HORN UNIT. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950721002781995072100278WP 1995 7 21 9510839874 119950711A7711 EPR TRANSMITTER DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01783NC 48108 696669 NR 2 EPR INDICATION DID NOT REACH THE TARGET EPR ON TAKEOFF ROLL. TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR. SYSTEM CHECKED OK ON RUNUP. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950721002791995072100279NM 1995 7 21 9510842255 119950717A7711 EPR TRANSMITTER BOEING727 727251 138408HNM PWA JT8 JT8D7 52053NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01255US 19974 653411 NR 1 EPR INDICATION DID NOT REACH TARGET EPR ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER AND INDICATOR. SYSTEM CHECKED OK ON RUNUP. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950721002801995072100280SO 1995 7 21 COM11929 119950717A2750 CONNECTOR EMB 120 EMB120RT SO TE FLAPS DIRTY A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01164D 120164 OUTBOARD FLAPS WILL NOT FULLY DEPLOY TO 45 DEGREES. CLEANED MOISTURE FROM FLAP ACTUATOR WIRING CONNECTORS. SYSTEM TEST NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950721002811995072100281EU 1995 7 21 COM31118 119950714A7933MS3470W2255BY CONNECTOR SAAB SF340 SF340A 7850100EU RT PROP GEARBOX CORRODED A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01361CA21575 340A056 RT PROPELLER GEARBOX OIL TEMP IS HIGHER THAN NORMAL. CLEANED CORROSION FROM WING TO FUSELAGE WIRING CONNECTOR 132VP. 2L72 4T RTA52EU 19950721002821995072100282NE 1995 7 21 COM31119 319950623A6114660714200 REAR FACE ROTOL R3544123F13 SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROP HUB CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01344CA5506 5506 DRG549989 340A025 DRG549989 CRACK INDICATION FOUND DURING OVERHAUL INSPECTION OF HUB REAR FACE IAW SF340 SB 61-58 APPENDIX C SCAN B. HUB S/N CW1114 WAS REMOVED FROM FURTHER SERVICE AT THAT TIME. 2L72 4T RTA52EU 6 CP61GL 19950721002831995072100283 1995 7 21 COM31120 319950629A6114660714200 REAR FACE ROTOL R3544123F13 SAAB SF340 SF340A 7850100EU PROP HUB CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01343CA9386 2931 DRG279985 340A024 CRACK INDICATION FOUND DURING UT INSPECTION OF AD 93-19-01. PROPELLER WAS DISASSEMBLED AND HUB S/N 110711 REMOVED FROM SERVICE. 2L72 4T RTA52EU 19950721002841995072100284 1995 7 21 COM31121 319950711A6114660714200 DOWL PIN ROTOL R3544123F13 SAAB SF340 SF340A 7850100EU PROP HUB CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01357CA6522 1456 DRG877084 340A044 CRACK INDICATION FOUND DURING SCHEDULED AD 93-19-01 INSPECTION. PROPELLER WAS DISASSEMBLED AND HUB S/N CW1024 REMOVED FROM SERVICE. 2L72 4T RTA52EU 19950721002851995072100285 1995 7 21 COM60519 419950715A34256229336400 AHRS CNDAIRCL600 CL6002B19 EA NR 1 FAILED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01927CA2377 1355 7031 PILOTS AHRS FAILED, COPILOTS 28V ESS BUS CIRCUIT BREAKER TRIPPED. REPLACED THE NR 1 AHRS. 2L72 4F RTA21EA 19950721002861995072100286EA 1995 7 21 COM60520 119950715A2760 FAULT MESSAGE CNDAIRCL600 CL6002B19 EA FLIGHT SPOILERS ACTIVATED A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01940CA 7048 FLIGHT SPOILERS AND SPOILERONS FAULT MESSAGE ON EICAS. COULD NOT DUPLICATE, CLEARED FAULTS FROM SECU. SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950721002871995072100287NM 1995 7 21 DL72E952874 119950524A57546516221100 RIBS BOEING727 727247 138408FNM RT LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIBS NR 3 AND 4 CRACKED. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950721002881995072100288NM 1995 7 21 DL72E952875 119950518A57546516221100 LE SKIN BOEING727 727247 138408FNM NR 5 LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E OUTER SKIN DENTED. REPAIRED PER SRM 57-50-3 FIG 6. 2L73 4F A3WE 19950721002891995072100289NM 1995 7 21 DL72E952876 119950524A57546516221100 SKIN BOEING727 727247 138408FNM NR 5 LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E SKIN DENTED AT 36 FROM I/B END. REPAIRED PER SRM 57-50-1. 2L73 4F A3WE 19950721002901995072100290NM 1995 7 21 DL72E952877 119950524A57546516221100 RIB BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 12 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804. 2L73 4F A3WE 19950721002911995072100291NM 1995 7 21 DL72E952878 119950524A57546516221100 RIB BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIB NR 2 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804. 2L73 4F A3WE 19950721002921995072100292NM 1995 7 21 DL72E952879 119950524A57546516221100 RIB BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH RIB NR 11 CRACKED. REPAIRED PER SRM 57-54-0 FIG 804. 2L73 4F A3WE 19950721002931995072100293NM 1995 7 21 DL72E952880 119950530A57546516221100 SKIN BOEING727 727247 138408FNM NR 5 LE FLAP OIL CANNED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 OUTER SKIN OIL CANNING AND DENTED 58 INCHES FROM IB END. REPAIRED AS PER 57-50-03 FIG 1 AND IN REFERENCE TO ERA NR 271165-14 FOR NR 5 L/E SLAT, DURING SHOP INSPECTION. 2L73 4F A3WE 19950721002941995072100294NM 1995 7 21 DL72E952881 119950619A57546516221100 RIB BOEING727 727247 138408FNM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 DURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH L/E SUPPORT RIB NR 5 CRACKED. REPAIRED PER SRM 57-54-0 PG 814. 2L73 4F A3WE 19950721002951995072100295NM 1995 7 21 DL72S952868 119950626A5751 SKIN BOEING727 727232 1384082NM RT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 REPAIR UNIDENTIFIED RT O/B AILERON UPPER SKIN HAS PREVIOUS TIME LIMITED REPAIR. INSTALLED PERMANENT REPAIR PER SRM 57-50-5 PG 2. 2L73 4F A3WE 19950721002961995072100296NM 1995 7 21 DL72S952869 119950626A5532 SKIN BOEING727 727232 1384082NM VERT STAB DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 AT HMV, FOUND TIME LIMITED REPAIR RT SIDE VERTICAL STAB SKIN AT TORQUE BOX AREA. INSTALLED PERMANENT REPAIR PER MM 55-30-0 FIG 801. 2L73 4F A3WE 19950721002971995072100297NM 1995 7 21 DL72S952870 119950627A5512 SKIN BOEING727 727232 1384082NM RT HORZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 RT HORIZONTAL STABILIZER I/B EDGE OF UPPER SKIN BENT AND CRACKED WHERE SEAL ATTACHES AT CENTER BOX AREA, BETWEEN FWD AND AFT SPAR. REPAIRED PER SRM 55-10-3 FIG 4. 2L73 4F A3WE 19950721002981995072100298NM 1995 7 21 DL72S952872 119950628A5743 ATTACH FITTING BOEING727 727232 1384082NM LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 LT MLG BEAM HAS CORROSION IN HOLES WHERE O/B ATTACH FITTING BUSHINGS WERE REMOVED. REPAIRED PER SRM 57-40 FIG 1 PG 6 AND 7. 2L73 4F A3WE 19950721002991995072100299NM 1995 7 21 DL72S952885 119950627A5320 WEB BOEING727 727232 1384082NM FS 360 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 WEB CRACKED AT STR 16L STA 360. REPAIRED PER SRM 53-10-4 PG 14. 2L73 4F A3WE 19950721003001995072100300NM 1995 7 21 DL72S952903 119950627A5313 STRINGER BOEING727 727232 1384082NM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION AT STR 28L STA 1050. REPAIRED PER SRM 53-30-3 FIG 1, IDENTIFIED AS A PERMANENT REPAIR PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950721003011995072100301NM 1995 7 21 DL72S952904 119950627A5313 STRINGER BOEING727 727232 1384082NM FS 1148 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION AT STR 28R AFT OF STA 1148 O/B SIDE. REPAIRED AS PER SRM 53-10-3 FIG 1, IDENTIFIED AS PERMANENT REPAIR PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950721003021995072100302NM 1995 7 21 DL72S952907 119950626A5713 STRINGER BOEING727 727232 1384082NM WS 519 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV, FOUND AFT TAB OF VENT BOX STR 11 CRACKED AT WS 519.00. REPAIRED PER M/M 57-13-0. 2L73 4F A3WE 19950721003031995072100303NM 1995 7 21 DL72S952908 119950628A5720 BEAM BOEING727 727232 1384082NM LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV, FOUND LT MLG WALKING BEAM WITH CORROSION IN BORES OF HOLES FOR MLG ATTACH FITTING. REPAIRED PER SRM 57-40 FIG 1 PG 6 AND 7. 2L73 4F A3WE 19950721003041995072100304NM 1995 7 21 DL72S952909 119950629A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV, FOUND FLOORBEAM CORRODED AT STA 1030 RBL 12 LBL 12. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950721003051995072100305NM 1995 7 21 DL72S952910 119950619A5751 SKIN 657273411 BOEING727 727232 1384082NM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA BN7 20745 DURING A SHOP INSPECTION, THE SKIN ON THE LOWER INBD SECTION WAS FOUND TO HAVE SEVERAL DENTS AND ELONGATED HOLES, IN WHICH RIVETS WERE PULLING THROUGH. A SKIN SPLICE REPAIR WAS INSTALLED PER THE M/M 57-51-0 FOR THE LEFT OUTBOARD AILERON. 2L73 4F A3WE 19950721003061995072100306NM 1995 7 21 DL72W952864 119950621A57536521631273A SKIN BOEING727 727247 138408FNM NR 1 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH WEAR ON L/E 17.5 INCHES FROM O/B END. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950721003071995072100307NM 1995 7 21 DL72W952865 119950630A57536521631273A LE SKIN BOEING727 727247 138408FNM NR 1 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH A HOLE IN THE L/E 10.5 INCHES FROM I/B END. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950721003081995072100308NM 1995 7 21 DL72W952866 119950630A57536521631273A SKIN BOEING727 727247 138408FNM NR 1 FOREFLAP HOLE A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV SHOP INSPECTION OF NR 1 F/F, WORN AREA FOUND 11 TO 12 INCHES FORM I/B END OF FLAP. ACCOMPLISHED REPAIRS PER SRM 57-50-4. 2L73 4F A3WE 19950721003091995072100309NM 1995 7 21 DL72W952887 119950622A5315 FLOORBEAM BOEING727 727247 138408FNM FS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 FLOORBEAM CORRODED FS 380 FROM RBL 24 TO CUSP RT. REMOVED CORROSION FROM FLOORBEAM CAP PER SRM 51-10-6. FABRICATED, TREAT AND PAINT REPAIR PARTS PER SRM 53-10-8. 2L73 4F A3WE 19950721003101995072100310NM 1995 7 21 DL72W952888 119950622A5315 FLOORBEAM BOEING727 727247 138408FNM FS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CABIN FLOORBEAM FS 1070, CORROSION AT TRANSVERSAL BEAM AND LBL 64. REPAIRED PER SRM 53-10-8, FOUND AT HMV. 2L73 4F A3WE 19950721003111995072100311NM 1995 7 21 DL72W952889 119950622A5347 SEAT TRACK BOEING727 727247 138408FNM FS 1110 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CABIN FLOOR SEAT TRACKS FS 1110, ATTACH SCREWS CORRODED AT FS 1110 AND RBL 45.5. FOUND AT HMV, ACCOMPLISHED REPAIRS PER SRM 53-20-11. 2L73 4F A3WE 19950721003121995072100312NM 1995 7 21 DL72W952890 119950629A5347 SEAT TRACK BOEING727 727247 138408FNM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 SEAT TRACK CORRODED STA 344 RT SIDE O/B, C53-224-03. REPLACED SEAT TRACK O/B RT SIDE FROM 344 TO 360 PER SRM 53-20-11, FOUND AT HMV. 2L73 4F A3WE 19950721003131995072100313NM 1995 7 21 DL72W952891 119950620A5315 FLOORBEAM BOEING727 727247 138408FNM FS 1110 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 BEAM CORRODED BOTTOM SIDE OF FLOOR SUPPORT AT STA 1110 TO 1130, RBL 24 I/B AND O/B NUTPLATE HOLES. REPAIRED PER SRM 53-20-11, FOUND AT HMV. 2L73 4F A3WE 19950721003141995072100314NM 1995 7 21 DL72W952893 119950622A5347 SEAT TRACK BOEING727 727247 138408FNM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 TRACK CORRODED, LT I/B SEAT TRACK AT FS 344 AND RT I/B SEAT TRACK AT FS 344. REPLACED TRACK PER SRM 51-11-6, FOUND AT HMV. 2L73 4F A3WE 19950721003151995072100315NM 1995 7 21 DL72W952894 119950624A5315 FLOORBEAM BOEING727 727247 138408FNM FS 1090 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND FS 1090 CABIN FLOORBEAM CORRODED AT RBL 45. ACCOMPLISHED REPAIRS PER SRM 53-10-8. 2L73 4F A3WE 19950721003161995072100316NM 1995 7 21 DL72W952897 119950619A5320 ANGLE BOEING727 727247 138408FNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 SUPPORT CORRODED UNDER HINGES FOR PNL 3448R. INSTALLED NEW ANGLE PER SRM 53-30-1, FOUND AT HMV. 2L73 4F A3WE 19950721003171995072100317NM 1995 7 21 DL72W952898 119950625A5720 SUPPORT BOEING727 727247 138408FNM WS 913 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 LT STA 913 UPLOCK SUPPORT FRAME HAS EXISTING TEMP REPAIR. INSTALLED REPAIR PER MM 53-11-0. 2L73 4F A3WE 19950721003181995072100318NM 1995 7 21 DL72W952899 119950619A5755 TE SKIN BOEING727 727247 138408FNM NR 2 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 THE NR 2 SPOILER PANEL T/E HAS DELAMINATED. REMOVED DAMAGED AREA, COMPLETED REPAIR PER SRM 57-50-6 REF 51-40-6, FOUND AT HMV. 2L73 4F A3WE 19950721003191995072100319NM 1995 7 21 DL72W952913 119950703A5330 SKIN BOEING727 727247 138408FNM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 FOUND A LINE OF SMALL NICKS 6 INCHES LONG COMING DOWN FROM AFT LAV SERVICE PAN ON THE FUSELAGE SKIN WITH CORROSION. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-1, FOUND IN ALLOWABLE LIMITS. 2L73 4F A3WE 19950721003201995072100320NM 1995 7 21 DL72W952914 119950703A5330 SKIN BOEING727 727247 138408FNM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 SKIN CORRODED AT STA 720C STR 10 RT. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 53-30-3 FIG 5, TIME LIMITED DOUBLER. 2L73 4F A3WE 19950721003211995072100321NM 1995 7 21 DL72W952915 119950703A5522 SKIN BOEING727 727247 138408FNM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 A .5 INCH CRACK RT ELEVATOR LWR SKIN AFT OF NR 4 BALANCE BOARD. FOUND DURING C-1 LTR CK TPAMM. REPAIRED PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950721003221995072100322NM 1995 7 21 DL72W952916 119950703A5522 SKIN BOEING727 727247 138408FNM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 RT ELEVATOR LWR SKIN CRACKED 1 INCH AT L/E AFT OF NR 4 BALANCE BOARD. FOUND AT C-1 LTR CK. REPAIRED PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950721003231995072100323NM 1995 7 21 DL72W952918 119950629A531165C36279 FRAME BOEING727 727247 138408FNM FS 761 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11292WA 22110 DURING HMV, EDGE DISTANCE COULD NOT BE MAINTAINED ON ONE OF THE FASTENER HOLES THROUGH THE FLOORBEAM UPPER CHORD AT FS 761 ON RT AND LT SIDES. FOUND DURING ACCOMPLISHMENT OF EO 4-61904-3AD. REPAIRED BY PLUGGING THE DISCREPANT HOLES AND CONTINUED EO 61904-3AD. FAA APPROVAL PER FAA ALTERNATE MEANS OF COMPLIANCE LETTER 94-120S-1376 DATED 11-30-94. 2L73 4F A3WE 19950721003241995072100324NM 1995 7 21 DL72W953088 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 595 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 595. ACCOMPLISHED REPAIRS PER SRM 53-10-3. 2L73 4F A3WE 19950721003251995072100325NM 1995 7 21 DL72W953089 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 615 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CORROSION ON S-26L AND SUPPORT ANGLES AT STA 615. REMOVED DAMAGED STRINGER FABRICATED NEW SECTION OF STRINGER SPLICE AND INSTALLED PER SRM 53-10-3. 2L73 4F A3WE 19950721003261995072100326NM 1995 7 21 DL72W953090 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 605 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CORROSION ON S-26L AND SUPPORT ANGLES AT STA 605. FABRICATED NEW SECTION OF STRINGER AND INSTALLED PER SRM 53-10-3, FOUND AT HMV. 2L73 4F A3WE 19950721003271995072100327NM 1995 7 21 DL72W953091 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 585 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 585. FABRICATED NEW SECTION OF STRINGER AND SPLICE AND INSTALLED PER SRM 53-10-3. 2L73 4F A3WE 19950721003281995072100328NM 1995 7 21 DL72W953092 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 628 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND CORROSION DAMAGE TO STR 27R AT FS 628. REMOVED CORRODED SECTION OF STRINGER, REMOVED WEB SECTION, FABRICATED NEW SECTION AND INSTALLED PER SRM 53-10-3. 2L73 4F A3WE 19950721003291995072100329NM 1995 7 21 DL72W953093 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 1030 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 AT HMV, FOUND CORROSION DAMAGE TO STR 28L AT FS 1030. REMOVED CORROSION PER SRM 51-10-6, REMOVED DAMAGED STRINGER, REPAIRED PER SRM 53-10-6 AND INSTALLED. 2L73 4F A3WE 19950721003301995072100330NM 1995 7 21 DL72W953094 119950619A5313 STRINGER BOEING727 727247 138408FNM FS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 STRINGER 28L CORRODED ON O/B SIDE, JUST FWD OF STA 1050. REMOVED DAMAGED SECTION OF STRINGER, FABRICATED NEW SECTION OF STRINGER AND INSTALLED PER SRM 53-10-3, FOUND AT HMV. 2L73 4F A3WE 19950721003311995072100331NM 1995 7 21 DL72W953095 119950622A5315 FLOORBEAM BOEING727 727247 138408FNM BS 380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 FLOORBEAM CAP CORRODED FS 380 FROM RBL 24 TO CUSP RT. REMOVED CORROSION FROM FLOORBEAM CAP PER SMR 51-10-6. REMOVED DAMAGED FLOORBEAM, CUT OUT NEW T-CAP, INSTALLED PER SRM 53-10-6. 2L73 4F A3WE 19950721003321995072100332NM 1995 7 21 DL72W953096 119950714A5313 STRINGER BOEING727 727247 138408FNM BS 570 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 STRINGER 27L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER. INSTALLED REPAIR PER SRM 53-10-3, FOUND AT HMV. 2L73 4F A3WE 19950721003331995072100333NM 1995 7 21 DL733953045 119950215A57536546431279A LE SKIN BOEING737 737347 1384647NM NR 1 FOREFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11309WA 23442 NR 1 FOREFLAP, L/E WORN 14 INCHES FROM O/B END AND 56 INCHES FROM I/B END. REPAIRED PER SRM 57-53-01 FIG 201, AT HMV SHOP INSPECTION. 2L72 4F RTA16WE 19950721003341995072100334NM 1995 7 21 DL757952873 119950628A5315 FLOORBEAM BOEING757 757232 1384965NM FS 760 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 DURING HMV IN ATLANTA, INSPECTION FOUND THE UPPER CAP OF FS 760 FLOORBEAM CORRODED AT LBL 20 RBL 20. ACCOMPLISHED REPAIRS PER SRM 53-30-51 FIG 203. 2L72 4F RTA2NM 19950721003351995072100335NM 1995 7 21 DL757952911 119950625A5414 SKIN BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 NACELLE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 716304 AT HMV, SET UP TO PERFORM TIME LIMITED REPAIR TO THE NACELLE/STRUT SKIN PER ERA 259151-14 CODE 6-54-31. REMOVED FASTENERS AND DYE CHECKED PER PS 900-6-3 NR 1. HFET REMOVAL OF CRACK OK. DRILLED UP AND INSTALLED DOUBLER AND TRIPLER PER ERA 259151-14. 2L72 4F4 FRTA2NM E17NE 19950721003361995072100336NM 1995 7 21 DL757952912 119950629A5720 ATTACH RINGS BOEING757 757232 1384965NM PWA 2037 PW2037 NE LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 716304 AT HMV, THE LT WING LWR SURFACE FUEL TANK ACCESS PLATES ATTACH RINGS ARE DIRTY AND HAVE FRETTING CORROSION. FRETTING CORROSION WAS REMOVED AND AREAS CLEANED. AREA WAS ROTO PEENED PER SRM 57-20-01 FIG 205. REPAIR WAS COMPLETED PER SRM 57-20-01 FIG 205. 2L72 4F4 FRTA2NM E17NE 19950721003371995072100337NM 1995 7 21 DL757952917 119950629A5330146N35318 SKIN BOEING757 757232 1384965NM FS 1473 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 DURING HMV INSPECTION, WHILE ACCOMPLISHING THE PERMANENT REPAIR FOR THE VHF ANTENNA MOUNT PER EO 6-59207-3, INTERFERENCE WAS FOUND WITH A DOUBLER PREVIOUSLY INSTALLED DUE TO CRACKING. TO ACCOMPLISH THE MODIFICATION, THE SKIN WILL BE REPAIRED BY EXTENDING THE DOUBLER AND TRIPLER REQUIRED BY EO 6-59207-3. 2L72 4F RTA2NM 19950721003381995072100338NM 1995 7 21 DL757952929 119950629A5414 SKIN BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11655DL 24395 DURING HMV, NR 2 PYLON STRUT SKIN HFEC SHOWS CRACK INDICATIONS. REMOVED DAMAGE PER SRM 54-51-01. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 54-51-01. 2L72 4F RTA2NM 19950721003391995072100339WP 1995 7 21 DLL10952884 119950627A5521 FRONT SPAR LKHEED1011 10113851 5265010WP LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 LT ELEV, FRONT SPAR CRACKED THROUGH BOTH LAYERS OF SKIN AT LIGHTENING HOLE, JUST INBD OF NR 8 ELEV HINGE. REMOVED REPAIR SECTION OF WEB, FABRICATED NEW WEB PIECES, INSTALLED NEW WEB SECTION. REPAIRED FRONT SPAR CRACK PER SRM 55-21-00 PG 804. INSTALLED LWR SKIN. 2L73 4F A23WE 19950721003401995072100340WP 1995 7 21 DLL10952900 119950702A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 1480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FLOOR SUPPORT CAP CORRODED C2 BB FS 1480 RBL 4. REPAIRED PER SRM 53-23-00 PG 803 TO 804, FOUND AT HMV. 2L73 4F A23WE 19950721003411995072100341WP 1995 7 21 DLL10952901 119950702A5330 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1565-1615 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FAIL-SAFE STRAPS DISBONDED AT FS 1565 TO 1585 STG 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1615 STR 30 TO 29. FAIL-SAFE STRAPS DISBONDED AT FS 1575 STR 36 TO 37. FOUND DURING HMV CORROSION INSP. REPAIRED PER SRM 53-31-00 PG 830 AND SKIN REPLACEMENT. 2L73 4F A23WE 19950721003421995072100342WP 1995 7 21 DLL10952902 119950702A5320 FAIL-SAFE STRAP LKHEED1011 10113851 5265010WP FS 1555/1575 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FAIL-SAFE STRAP DISBONDED AT FS 1555 STR 36 TO 37 AND AT FS 1575 BTWEEN STR 40 TO 41, FOUND AT HMV. REPAIRED PER SRM 53-31-00 PG 830. 2L73 4F A23WE 19950721003431995072100343WP 1995 7 21 DLL10952905 119950627A5320 FORMER LKHEED1011 10113851 5265010WP FS 1163 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 FLOOR PANEL SUPPORT RAIL CRACKED IN RADIUS AT STA 1163 FORMER LBL 104. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19950721003441995072100344WP 1995 7 21 DLL10952920 119950627A5743 TRUNNION FTG LKHEED1011 10113851 5265010WP RT WING CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 OUTBOARD SIDE OF RT TRUNNION FITTING WEB WAS FOUND WITH NUMEROUS AREAS OF SURFACE RUST. REPAIRED PER SRM 51-21-01. 2L73 4F A23WE 19950721003451995072100345WP 1995 7 21 DLL13952906 119950624A5730 SKIN LKHEED1011 10113851 5265010WP LT WING LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 LIGHTNING STRIKE UPPER WING SKIN I/B FWD CORNER. REPAIRED PER 57-32-00 FIG 807. 2L73 4F A23WE 19950721003461995072100346WP 1995 7 21 DLL13952923 119950705A55121524199101 SKIN LKHEED1011 10113851 5265010WP HORZ STAB LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 DURING HANGER INSPECTION, THE LT HORZ STAB WAS FOUND TO HAVE CRACKED RIBS AND L/E PANEL. REPAIRED PER SRM 55-12-00. 2L73 4F A23WE 19950721003471995072100347WP 1995 7 21 DLL13952931 119950705A5315 FLOORBEAM LKHEED1011 10113851 5265010WP FS 669 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 FOUND AT HMV, CORROSION DAMAGE ON FLOORBEAM AT STA 669, C-1 CARGO COMP. REPAIRED PER SRM 53-23-0 FIG 802. 2L73 4F A23WE 19950721003481995072100348NM 1995 7 21 DLM88952882 119950630A5320 ANGLE DOUG MD88 MD88 3023688NM WW KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11942DL 49815 DURING G-1 LTR CHECK, FOUND KEEL BEAM AFT CROSSOVER ANGLE CRACKED. ACCOMPLISHED REPAIRS PER SRM 53-05 FIG 101. 2L72 4F RTA6WE 19950721003491995072100349NM 1995 7 21 DLM88952883 119950630A27525935973501 ACTUATOR ARM DOUG MD88 MD88 3023688NM RT TE FLAP BROKEN A ADALAK NONE O OTHER ININSP/MAINT 1 SO11942DL 49815 FOUND ON ARRIVAL FOR LETTER CHECK, THE RIGHT SIDE INBOARD FLAP INBOARD DRIVE ACTUATOR CASTING CRACKED. REPLACED CASTING ARM AND ACTUATOR. 2L72 4F RTA6WE 19950721003501995072100350NM 1995 7 21 P5CA9500453 119950630A5313 FITTING BOEING747 747121 1384871NM FS 1394 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AND CORROSION IN LONGERON FITTING AT BS 1394, BEFORE WING SLIDE COMPARTMENT ABOVE WING. REMOVED CRACK AND CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950721003511995072100351NM 1995 7 21 P5CA9500454 119950630A5414 SKIN BOEING747 747121 1384871NM NR 1 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON NR 1 PYLON SKIRT NEAR TO RIGHT AFT HYDRAULIC RESERVOIR MOUNTING BOLT. REPAIRED PER BOEING SRM 54-12-02 AND 51-30-02. 2L74 4F A20WE 19950721003521995072100352NM 1995 7 21 P5CA9500455 119950630A5400 ANGLE BOEING747 747121 1384871NM NR 3 PYLON WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 ANGLE WORN AND MISSING FASTENERS IN NR 3 PYLON SKIRT RIGHT FORWARD SIDE. REPAIRED PER BOEING SRM 51-40-01 AND 51-30-02. 2L74 4F A20WE 19950721003531995072100353NM 1995 7 21 P5CA9500456 119950630A5414 SKIN BOEING747 747121 1384871NM NR 4 PYLON WORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 WORN METAL IN RIGHT AFT SIDE NR 4 PYLON SKIRT. REPAIRED PER BOEING SRM 54-10-02 AND 51-30-02. 2L74 4F A20WE 19950721003541995072100354NM 1995 7 21 P5CA9500457 119950630A5312 BLKHD FITTING BOEING747 747121 1384871NM BS 2340-2360 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FITTING BETWEEN BS 2340 AND 2360 S24L AT ATTACH PRESSURE BULKHEAD. CORROSION REMOVED AND TREATED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950721003551995072100355NM 1995 7 21 P5CA9500458 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 1500 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN SEAT BS 1500 LBL 75. REPLACED SEAT TRACK PER BOEING SRM 53-10-05. 2L74 4F A20WE 19950721003561995072100356NM 1995 7 21 P5CA9500459 119950630A5330 SKIN BOEING747 747121 1384871NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED SKIN AT NOSE WHEEL WELL DOOR HINGE CUTOUT RIGHT DOOR FWD HINGE. REPAIRED PER BOEING SRM 53-10-20 AND 51-30-02. 2L74 4F A20WE 19950721003571995072100357NM 1995 7 21 P5CA9500460 119950630A5320 ANGLE BOEING747 747121 1384871NM BS 1800-1820 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON ANGLE BS 1800 TO 1820 RBL 45 AFT CARGO COMPARTMENT. REPAIRED PER BOEING SRM 53-10-23, 51-30-02 AND 53-11-25. 2L74 4F A20WE 19950721003581995072100358NM 1995 7 21 P5CA9500461 119950630A5313 LONGERON BOEING747 747121 1384871NM OVERWING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION AT OVERWING LONGERON LEFT AND RIGHT SIDES. CORROSION REMOVED PER BOEING SRM 51-10-01, TREATED PER 51-10-02. 2L74 4F A20WE 19950721003591995072100359NM 1995 7 21 P5CA9500462 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 1320 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON SEAT TRACK RBL 33 BETWEEN BS 1320 AND 1480. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02. 2L74 4F A20WE 19950721003601995072100360NM 1995 7 21 P5CA9500463 119950630A5340 WEB BOEING747 747121 1384871NM BS 1300/1310 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON THE WEB BETWEEN BS 1300 AND 1310 LBL 33. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02. 2L74 4F A20WE 19950721003611995072100361NM 1995 7 21 P5CA9500464 119950630A5320 WEB BOEING747 747121 1384871NM BS 1420 MISDRILLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 OVAL HOLE IN THE WEB AT BS 1420 LBL 33. REPAIRED PER BOEING SB 53-2224. 2L74 4F A20WE 19950721003621995072100362NM 1995 7 21 P5CA9500465 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM MAIN DECK OVAL HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 OVAL HOLE AT SEAT TRACK TO WEB ATTACHMENT. REPAIRED PER BOEING SB 53-2224, OVERSIZE FASTENER. 2L74 4F A20WE 19950721003631995072100363NM 1995 7 21 P5CA9500466 119950630A5320 BRACKET BOEING747 747121 1384871NM CARGO COMPT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN MAIN CARGO DOOR MANUAL HAND PUMP AFT MOUNTING BRACKET. REPAIRED PER BOEING SRM 51-40-04 AND 51-30-02. 2L74 4F A20WE 19950721003641995072100364NM 1995 7 21 P5CA9500467 119950630A5347 SEAT TRACK BOEING747 747121 1384871NM BS 1910/1890 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON SEAT TRACK AT RBL 25 BETWEEN BS 1910 AND 1890. REPAIRED PER BOEING SRM 53-10-05. 2L74 4F A20WE 19950721003651995072100365NM 1995 7 21 P5CA9500468 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1480 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON S41L BS 1480. REPAIRED PER BOEING SRM 53-10-03. 2L74 4F A20WE 19950721003661995072100366NM 1995 7 21 P5CA9500469 119950630A573065B020931 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 WING PANEL HAS DELAMINATIONS DENTS AND MISSING EDGE. REPAIRED PER BOEING SRM 51-40-06 AND 51-40-09. 2L74 4F A20WE 19950721003671995072100367NM 1995 7 21 P5CA9500470 119950630A5730 PANELS BOEING747 747121 1384871NM WINGS DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATIONS, DENTS AND EDGE DAMAGE ON WING PANELS 672AB, 672CB, 577ET AND 677FT. REPAIRED PER BOEING SRM 51-40-06 AND 51-40-09. 2L74 4F A20WE 19950721003681995072100368WP 1995 7 21 95ZZZX3419 119950710A27611040T1005 ACTUATOR DOUG DC9 DC931 3022065WP SPOILER SYS FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE05982PS 47251 STL - FLT 651 - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG PN 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. CHECK C - 8-16-94 - STL. 2L72 4F A6WE 19950721003691995072100369NM 1995 7 21 95ZZZX3420 119950710A323069141065 TRANSFER CYL BOEING727 727231 1384079NM NLG FAILED A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0554327 20234 ONT - FLT 221 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND NOSE GEAR EXTENDED. FOUND NOSE LANDING GEAR TRANSFER CYLINDER, MFG PN 69-14106-5, WITH INTERNAL MALFUNCTIONS. REPLACED TRANSFER CYLINDER AND NOSE LANDING GEAR, OPERATION CHECKED NORMAL. CHECK C-2 - 9-18-94 - MCI. 2L73 4F A3WE 19950721003701995072100370WP 1995 7 21 95ZZZX3421 119950613A2612427992 CLAMP DOUG DC8 DC851 3021920WP NR 3 ENGINE LOOSE A TWAAK NONE N FALSE WARNING CRCRUISE 1 CE05507DC 45855 DURING CRUISE, EXPERIENCED INTERMITTENT FIRE WARNING ON NR 3 ENGINE WHICH CEASED UPON POWER REDUCTION AND RECURRED DURING DESCENT INTO SJC. INSPECTION REVEALED A CLAMP ON THE COWLING CONTACTING THE FIRE SENSOR ELEMENT. REPOSITIONED CLAMP ON COWLING AND SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 19950721003711995072100371NM 1995 7 21 95ZZZX3422 119950621A5330 SKIN BOEING727 72722C 138400FNM BS 530 DAMAGED A RYNAK NONE O OTHER ININSP/MAINT 1 CE07753AS 19203 A 3 INCH LONG, .5 INCH WIDE VERTICAL GASH OR PUNCTURE AT STA 530, WL 188, RIGHT SIDE OF FUSELAGE, WAS DISCOVERED DURING THE WALK-AROUND INSPECTION IN SAIPAN. DAMAGE REPAIRED IAW SRM 53-30-3, BLIND RIVET REPAIR. PATCH CONSISTED OF A 9 INCH BY 12 INCH AREA SCARF WITH A CENTER AREA OF 1.5 INCH BY 4 INCH. PATCH MATERIAL USED WAS TT 2024.050. 2L73 4F A3WE 19950721003721995072100372EU 1995 7 21 95ZZZX3424 119950701A334003730351K STROBE BAG JETSTMJETSTM3201 1500217EU LOWER DAMAGED A VTZAK NONE C F.O.D. CRCRUISE 1 EA27487UE 906 RDU/IAD - FLT 6190 - DURING CRUISE AT 2109 HRS ON 7-1-95, EXPERIENCED A LIGHTNING STRIKE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT AILERON, THE NR 2 COMM ANTENNA, AND THE LOWER STROBE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF CONTROL NUMBER VTZA95211, AND 95ZZZX3425. (X) 2L72 4T RTA56EU 19950721003731995072100373EU 1995 7 21 95ZZZX3425 119950701A5751137300B446 SKIN BAG JETSTMJETSTM3201 1500217EU RT AILERON DAMAGED A VTZAK NONE C F.O.D. CRCRUISE 1 EA27487UE 906 RDU/IAD - FLT 6190 - DURING CRUISE AT 2109 HRS ON 7-1-95, EXPERIENCED A LIGHTNING STRIKE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT AILERON, THE NR 2 COMM ANTENNA, AND THE LOWER STROBE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF CONTROL NUMBER VTZA95211, AND 95ZZZX3424. (X) 2L72 4T RTA56EU 19950721003741995072100374 1995 7 21 ORJA9547 419950512A256539618991 LANYARD DOUG DC9 DC983 3022083WP FWD DOOR SLIDE BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11832RA 53044 MAIN ENTRY DOOR EMERGENCY SLIDE LANYARD BROKEN. REPLACED FORWARD ENTRY DOOR SLIDE LANYARD. (X) 2L72 4F RTA6WE 19950721003751995072100375WP 1995 7 21 ORJA9549 119950613A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN LOOSE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11876RA 53183 SECTION 4 AND SECTION 5 RIGHT SIDE EMERGENCY FLOOR LIGHTS OUT. RESECURED WIRE ON RIGHT SIDE SECTION 4 AND SECTION 5 FLOOR EMERGENCY LIGHTS. OPS GOOD. (X) 2L72 4F RTA6WE 19950721003761995072100376WP 1995 7 21 ORJA9550 119950620A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11822RA 49932 AFT SECTION OF FLOOR TRACK INOP (EMERGENCY). INSTALLED NEW EMERGENCY FLOOR TRACK LIGHTING SUPPLY POWER PACK. OPS TESTS NORMAL. (X) 2L72 4F A6WE 19950721003771995072100377WP 1995 7 21 ORJA9551 119950617A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11822RA 49932 SECTION 15 THROUGH SECTION 20, RIGHT SIDE EMERGENCY FLOOR LIGHTS OUT. REPLACED POWER PACK BATTERY ON SECTION 15. OPS GOOD. (X) 2L72 4F A6WE 19950721003781995072100378NE 1995 7 21 ORJA9552 219950622A7200 ENGINE DOUG DC9 DC982 3022082WP PWA JT8 JT8D219 52053NE RIGHT FAILED A ORJAK NONE J WARNING INDICATION ININSP/MAINT 1 WP11822RA 49932 IRW - RIGHT ENGINE OIL QUANTITY DECREASED TO 12 QUARTS. TEMPERATURE INCREASED TO 140 DEGREES. REMOVED AND REPLACED 'R' ENGINE PER MD-80 MM 71-00. OPS CHECK GOOD. (X) 2L72 4F4 F A6WE E9NE 19950721003791995072100379 1995 7 21 VTZA95211 419950701A2312101181 ANTENNA BAG JETSTMJETSTM3201 1500217EU LOWER DAMAGED A VTZAK NONE C F.O.D. CRCRUISE 1 EA27487UE 906 RDU/IAD - FLT 6190 - DURING CRUISE AT 2109 HRS ON 7-1-95, EXPERIENCED A LIGHTNING STRIKE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT AILERON, THE NR 2 COMM ANTENNA, AND THE LOWER STROBE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF CONTROL NUMBER 95ZZZX3424, AND 95ZZZX3425. (X) 2L72 4T RTA56EU 19950721003801995072100380EU 1995 7 21 VTZA95215 119950704A77122188406 TQ SIG COND JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE OUT OF CALIB A VTZAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 EA27314UE 41027 IAD/EWR - FLT 6435 - ABORTED TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 92 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950721003811995072100381EU 1995 7 21 9510853245 119950715A3350100865 EEL POWER SUPPLY AIRBUS320 A320211 3930320EU CABIN MALFUNCTIONED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01345NW 399 DURING PREFLIGHT CHECK, THE EMERGENCY PATH LIGHTS ON SEATS ROW 14 TO THE REAR OF THE AIRCRAFT REMAIN ILLUMINATED. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950721003821995072100382EU 1995 7 21 9510863211 119950717A29134205400 HYD PUMP AIRBUS320 A320211 3930320EU NR 1 ENGINE LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01311US130848079 125 DURING CRUISE AT FL 370 APPROXIMATELY ONE HOUR INTO FLIGHT, THE GREEN HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE POWER TRANSFER UNIT AND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WERE DISCONNECTED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CONTINUED TO DTW WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRALUIC PUMP LEAKING. REPLACED THE NR 1 EDP. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950721003831995072100383NE 1995 7 21 P5CA9500471 219950719A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 FAILED A AP5CAE ENGINE SHUTDOWN J WARNING INDICATION ININSP/MAINT 1 WP23850FT581337824 19755 662498 DURING POST EVC, FUEL PUMP AND FUEL CONTROL CHANGE RUNUP ENGINE STALLED AT 1.41 EPR WITH RAPID EGT RISE, ENGINE SHUTDOWN. GROUND REPORTED FIRE IN TAIL PIPE. MOTORED ENGINE, FIRE PUT OUT. FOUND METAL IN TAIL PIPE. ENGINE TO BE CHANGED 2L74 4F4 F A20WE E20EA 19950721003841995072100384NM 1995 7 21 SCNA95148 119950709A3350S106 EEL BATTERIES BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 AFT AIRSTAIR EMERGENCY EXIT LIGHT ON VERY DIM. FOUND BATTERY PACK WITH LOW VOLTAGE AND SOME CORROSION ON TERMINALS. CLEANED TERMINALS AND INSTALLED NEW BATTERIES PER MM 33-50-61, LIGHT TESTED GOOD. 2L73 4F RTA3WE 19950721003851995072100385WP 1995 7 21 SCNA95149 119950714A261172130000010 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 3 LAV FAILED A SCNAK NONE N FALSE WARNING ININSP/MAINT 1 GL15573SC 46905 FOUND NUMBER 3 LAVATORY SMOKE DETECTOR GOING OFF FOR NO APPARENT REASON. REMOVED AND REPLACED NUMBER 3 LAVATORY SMOKE DETECTOR PER MM 26-00. SMOKE DETECTOR TESTED GOOD. 2L73 4F A22WE 19950721003861995072100386WP 1995 7 21 SCNA95150 119950715A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 DURING LINE CHECK, FOUND MID CABIN FLOOR EMERGENCY LIGHTS DIM. REMOVED AND REPLACED MID CABIN POWER SUPPLY IAW MM 33-50-00. LIGHT OPS CHECKED GOOD. 2L73 4F A22WE 19950721003871995072100387NM 1995 7 21 95ZZZM227 119950605A3350A3060719101 EEL STRIP BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07620AA 24578 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 3E-5E LENS WILL NOT STAY IN PLACE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT 3E-5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950721003881995072100388WP 1995 7 21 AAL951064 119950608A3350A3060719103 EEL STRIP DOUG DC9 DC982 3022082WP CABIN FLOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07276AA 49273 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721003891995072100389NM 1995 7 21 AALA951026 119950602A3350A3030398101 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07366AA 25193 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT AFT FLIGHT ATTENDANT STATION AND 36H-37H INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS AT AFT PARTITION AND 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003901995072100390NM 1995 7 21 AALA951030 119950604A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07315AA 22317 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 24 A/B INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR PIN AT 24 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003911995072100391NM 1995 7 21 AALA951033 119950605A3350A3030398101 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07323AA 22324 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 24H INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR PIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003921995072100392NM 1995 7 21 AALA951063 119950608A3350S417N50914 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, LEFT SIDE EMERGENCY EXIT LIGHT IN BUSINESS CLASS CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSY AT LEFT SIDE IN BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003931995072100393WP 1995 7 21 AALA951064 119950608A3350A3060719103 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07276AA 49273 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD LAVATORY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721003941995072100394NM 1995 7 21 AALA951081 119950608A3350A3030398101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071751A 48420 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 7D INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19950721003951995072100395NM 1995 7 21 AALA951084 119950612A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07325AA 22326 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 24HJ INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003961995072100396WP 1995 7 21 AALA951092 119950614A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07131AA 46994 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 27 THROUGH 29 AT RT AISLE INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PASSENGER SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950721003971995072100397WP 1995 7 21 AALA951106 119950617A3350EMBS1392 EEL BATTERY GULTON DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A AALAK NONE L NO TEST DEDESCENT 1 SW07154AA 46709 SFO - FLT NR 28 - DURING DESCENT INTO SFO, EMERGENCY EXIT LIGHTS AT L2 AND R2 DOORS ILLUMINATED. NO OTHER ABNORMAL INDICATIONS NOTED AND AIRCRAFT LANDED SFO WITHOUT INCIDENT. REPLACED L2 AND R2 EMERGENCY EXIT LIGHT BATTERY AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950721003981995072100398NM 1995 7 21 AALA951107 119950617A3350 EEL WIRE BOEING767 767323 1385205NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07359AA 24040 LAX - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LEFT AISLE IN FIRST CLASS CABIN AND HALF OF BUSINESS CLASS CABIN DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT SWITCH IS SELECTED ON. REPAIRED SHORTED WIRE AT LOWER SIDEWALL BY LAST SEAT ON LEFT SIDE OF FIRST CLASS CABIN AND RESECURED LOOSE CONNECTION AT LEFT SIDE OF BUSINESS CLASS CABIN BY FIRST SEAT ROW. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721003991995072100399NM 1995 7 21 AALA951108 119950616A3350 EEL CONNECTORS BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT RT AISLE IN FIRST CLASS CABIN AND BUSINESS CLASS CABIN AND LEFT AISLE IN BUSINESS CLASS CABIN INOPERATIVE. RESECURES EMERGENCY EXIT LIGHT CONNECTORS FOUND DISCONNECTED AT PAX SEAT LOCATIONS 11B AND 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721004001995072100400NM 1995 7 21 AALA951109 119950616A3350A3060720101 EEL CONDUCTOR DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071758B 48527 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN R2 DOOR AND PASSENGER SEAT ROW 7H INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19950721004011995072100401NM 1995 7 21 AALA951110 119950616A3350020182000 EEL BASE BOEING767 767223 1385123NM MID GALLEY BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07316AA 22318 SFO - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN MID GALLEY BROKEN/INOPERATIVE. REPLACED EMERGENCY LIGHT BASE AND LENS AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721004021995072100402EU 1995 7 21 AALA951111 119950618A323071539 SEQ VALVE FOKKERF28 F28MK0100 4990807EU NLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071437B 11427 IAH - FLT 2064 - AFTER TAKEOFF IAH WHEN LANDING GEAR RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. RECYCLED LANDING GEAR TWICE WITH SAME RESULTS. AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRY IAH/DFW. REPLACED NOSE LANDING GEAR SELECTOR SEQUENCE VALVE AND RESTRICTOR. ACCOMPLISHED LEAK CHECK WITH NO DEFECTS FOUND. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950721004031995072100403NM 1995 7 21 AALA951121 119950619A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 9B THROUGH 12B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR BY PASSENGER SEAT ROW S12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950721004041995072100404 1995 7 21 AALA951123 419950614A2565101623111 SLIDE BFGOODRICH BOEING767 767223 1385123NM FWD DOORS SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A3187 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE FLOOR FOUND DETERIORATED. SCRAPPED EMERGENCY EVACUATION SLIDE. (M) 2L72 4F RTA1NM 19950721004051995072100405 1995 7 21 AALA951124 419950619A2565101623111 SLIDE BFGOODRICH BOEING767 767223 1385123NM FWD DOORS SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A3017 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE FLOOR FOUND DETERIORATED AND SLIDE HAD POROSITY LEAKS. SCRAPPED EMERGENCY EVACUATION SLIDE. (M) 2L72 4F RTA1NM 19950721004061995072100406NM 1995 7 21 AALA951131 119950620A3350 EEL CONDUCTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07620AA 24578 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950721004071995072100407NM 1995 7 21 ASAA9510060 119950619A523010608214 DOOR SEAL BOEING737 737290C 138448VNM CARGO DOOR MISSING A ASAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 NM01730AS 22577 ANC - FLT NR 126 - CREW REPORTED LOSS OF PRESSURIZATION DURING CRUISE, PASSENGER OXYGEN MASKS AUTOMATICALLY DEPLOYED. CREW DESCENDED AIRCRAFT TO 10,000 FEET AND SUBSEQUENTLY LANDED WITHOUT INCIDENT. FOUND A LARGE SECTION OF THE AFT LOWER CARGO DOOR SEAL MISSING. REPLACED SEAL, RESTOWED OXYGEN MASKS, PRESSURIZED AIRCRAFT AND OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004081995072100408NM 1995 7 21 AWXA9500388 119950620A5320 STRAP BOEING757 7572S7 1384962NM BS 1681 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - DURING SCHEDULED C3 INSPECTION, FOUND INTERCOSTAL DOUBLER STRAP CRACKED, BS 1681 RBL 12. REMOVED, FABRICATED AND INSTALLED STRAP PER SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19950721004091995072100409NM 1995 7 21 AWXA9500389 119950620A532065456763 FITTINGS BOEING757 7572S7 1384962NM CARGO COMPT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - DURING SCHEDULED C3 INSPECTION, FOUND THRESHOLD STANCHION FITTINGS FOR CARGO NETS CORRODED IN AFT CARGO PIT. REMOVED ADN REPLACED FITTINGS PER SRM 51-40-02. (M) 2L72 4F RTA2NM 19950721004101995072100410NM 1995 7 21 AWXA9500390 119950620A5315 FLOOR BEAM BOEING757 7572S7 1384962NM FS 365 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED IN SEVERAL AREAS, STATION 365 BL 0 TO RBL 40. FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 53-00-51. (M) 2L72 4F RTA2NM 19950721004111995072100411NM 1995 7 21 AWXA9500391 119950620A5315 FLOOR BEAM BOEING757 7572S7 1384962NM STA 377.7 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM TOP CAP CORRODED BEYOND LIMITS AT STATION 377.7 LBL 10. REPAIRED FLOOR BEAM PER SRM 51-70-12. (M) 2L72 4F RTA2NM 19950721004121995072100412NM 1995 7 21 AWXA9500392 119950620A5315 FLOOR BEAM BOEING757 7572S7 1384962NM FS 345 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28906AW 23568 PHX - DURING SCHEDULED C3 INSPECTION, FOUND FLOOR BEAM CORRODED AT FASTENER HOLE, STATION 345 BL 0. REPAIRED PER SRM 51-40-02. (M) 2L72 4F RTA2NM 19950721004131995072100413NM 1995 7 21 AWXA9500394 119950620A335020121 EEL BATT CHARGER BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 6 THROUGH 9. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950721004141995072100414NM 1995 7 21 AWXA9500395 119950622A335058731 EEL STRIP BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERENCY EXIT LIGHTS INOPERATIVE ROW 1 THROUGH ROW 5. REPLACED LIGHT STRIP AT ROW 1, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950721004151995072100415NM 1995 7 21 AWXA9500396 119950622A3350 EEL ASSY BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ROW 7 THROUGH ROW 9 INOPERATIVE. RECONNECTED LIGHTS, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950721004161995072100416NM 1995 7 21 AWXA9500397 119950623A3350900835A EEL BATT PACK BOEING737 7372M8 1384483NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY IN AFT BAG PIT, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950721004171995072100417NM 1995 7 21 AWXA9500400 119950625A33500L3071GEPPL EEL BOEING757 7572G7 1384963NM CABIN DAMAGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS DAMAGED IN SEVERAL AREAS. REMOVED AND REPLACED LIGHTS AS REQUIRED, OPS CEHCK GOOD. (M) 2L72 4F RTA2NM 19950721004181995072100418WP 1995 7 21 CAL950406 119950519A2497 HARNESS DOUG DC10 DC1030 3023501WP FWD CARGO COMPT BURNED A ACALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0912061 47851 FLT 57 - LGW - SEVERAL C/B'S POPPED AND BOTH THE NR 1 AND NR 2 GEN'S HAD NO VOLTS AND NO FREQUENCY WHILE EN ROUTE FROM ORY TO EWR. THE CREW WAS UNABLE TO RESTORE EITHER GEN AND THE A/C WAS DIVERTED TO LGW WHERE IT LANDED W/O INCIDENT. ALL TRIPPED C/B'S WERE ASSOCIATED WITH AC BUS NR 1 AND NR 2 AND WOULD NOT RESET. MX FOUND ALL PIN OUT WIRES SHORTED TO GROUND. THE SHORT WAS TRACED TO A BURNT OUT WIRE BUNDLE IN THE FWD CARGO CEILING AREA. THE WIRING WAS REPAIRED IAW STANDARD PRACTICES CHAP 20 OF MM. OPS CHECK OF THE NR 1 AND NR 2 GEN'S AND ALL ASSOCIATED SYSTEMS WAS GOOD. S/D - MX ALSO FOUND A STICKY LIQUID SUBSTANCE ON C/B'S OF LWR MID PNL. THE C/B'S WERE FREED, AND ANY BROKEN IN PROCESS WERE REPLACED.(M)2L73 4F A22WE 19950721004191995072100419NM 1995 7 21 TSAA9525124 119950607A2530 HOT JUG BOEING737 737297 1384480NM GALLEY SHORTED A TSAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP1370723 21739 FLTN RN 220 - DC CONTROL CIRCUIT BREAKER RESET, AND SMOKE BEGAN TO COME OUT OF UPPER GALLEY AREA. DC CONTROL CIRCUIT BREAKER PULLED AND SMOKE STOPPED. REPLACED CONNECTOR PLUG FOR HOT JUG DUE TO SHORTED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004201995072100420NM 1995 7 21 TSAA9552084 119950602A5230 FRAME BOEING737 737297 1384480NM CARGO DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND FORWARD CARGO DOOR FORWARD FRAME CRACKED 8 INCHES FROM BOTTOM. INSTALLED REPAIR KIT NR 65C31427-2 PER FIG 2 DETAIL 1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004211995072100421NM 1995 7 21 TSAA9552085 119950602A5230 FRAME BOEING737 737297 1384480NM CARGO DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENACNE VISIT, FOUND FORWARD CARGO DOOR FORWARD FRAME CRACKED 18 INCHES UP FROM BOTTOM. REPAIRED PER ECO2594. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004221995072100422NM 1995 7 21 TSAA9553087 119950602A5311 FRAME BOEING737 737297 1384480NM BS 967 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENANCE VISIT, FOUND CRACKED FRAME AT BS 967 INBOARD OF STRINGER 22R. REPAIRED PER ECO2382R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004231995072100423NM 1995 7 21 TSAA9553123 119950606A5330 SKIN BOEING737 737297 1384480NM BS 727 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13726AL 22426 DURING ROUTINE OVERNIGHT CHECK, DISCOVERED FUSELAGE SKIN CRACK 2.25 INCHES LONG AT 2 INCH AFT OF BS 727B, ABOVE STRINGER 16L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004241995072100424NM 1995 7 21 TSAA9557086 119950602A5711 SPAR BOEING737 737297 1384480NM WS 557 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13725AL 22051 DURING HEAVY MAINTENACNE VISIT, EXFOLIATION TYPE OF CORROSION NOTED ON RT WING AFT SIDE OF REAR SPAR INBOARD OF WS 557 AS EVIDENT. REPAIRED PER ECO2590. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950721004251995072100425WP 1995 7 21 AALA950127 119950602A3350MS3124E1415S EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07432AA 49350 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721004261995072100426WP 1995 7 21 AALA950969 119950527A3350A3060719104 EEL STRIP DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07566AA 49348 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FROM ROW 3-6 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 19950721004271995072100427WP 1995 7 21 AALA950975 119950528A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN CORRODED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07474 49649 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BY FORWARD LAVATORY. REPLACED CORRODED SECTION OF WIRING HARNESS. SYSTEM GROUND CHECKED NORMAL. (M) 2L72 4F A6WE 19950721004281995072100428WP 1995 7 21 AALA950976 119950529A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07595AA 53285 DFW - DURING OVERNIGHT CHECK, AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED WIRING AND REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 19950721004291995072100429WP 1995 7 21 AALA951009 119950601A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN CUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW07289AA 49301 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AFT SECTION OF COACH. REPAIRED CUT FLAT WIRE, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721004301995072100430EU 1995 7 21 AALA951031 119950604A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770054 461 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT 2L DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRING AT THE 2L DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950721004311995072100431EU 1995 7 21 AALA951032 119950605A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0777080 626 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT CROSS AISLE BETWEEN DOOR 2L AND 2R INOPERATIVE. REPLACED DAMAGED WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950721004321995072100432NM 1995 7 21 AALA951035 119950602A5330111T3013 SKIN BOEING767 767223 1385123NM FS 955 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FUSELAGE CABIN WING BOX SKIN (UPPER) HAS CORROSION, REMOVED AT STATION 955 LBBL 30, 20, AND 74.81. REPAIRED CORROSION AT STATION 955, LBL 74.81 BY INSTALLING A FILLER STRAP AS SHOWN IN FIGURE. RESTORED SURFACE FINISH TO REWORKED AREA STATION 955 BETWEEN LBL 20, LBL 30. (M) 2L72 4F RTA1NM 19950721004331995072100433NM 1995 7 21 AALA951036 119950605A5330143T3220 SKIN BOEING767 767223 1385123NM FS 742 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - TEAR STRAP ON FUSELAGE SKIN CORROSION OUT OF LIMITS AFTER BLEND-OUT. INSTALL A TAPERED SHIM WET WITH SEALANT AND CORROSION INHIBITING COMPOUND PER B767 SRM AND ENGINEERING MRB 767-935. (M) 2L72 4F RTA1NM 19950721004341995072100434NM 1995 7 21 AALA951037 119950605A5315143T1060 FLOOR BEAM BOEING767 767223 1385123NM FS 478 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. REFINISH BEAM PER B767-SRM. BEAM IS SATISFACTORY FOR CONTINUED SERVICE PER ENGINEERING MRB 767-942. (M) 2L72 4F RTA1NM 19950721004351995072100435NM 1995 7 21 AALA951038 119950605A5414311T1450 SKIN BOEING767 767223 1385123NM LT PYLON GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - LEFT OUTBOARD PYLON SKIN BOTTOM EDGE, HAS GOUGE BEYOND SRM LIMITS AFTER BLEND-OUT. REFINISH BLENDED AREA PER B767-SRM. APPROVED FOR CONTINUED SERVICE PER ENGINEERING MRB 767-946. (M) 2L72 4F RTA1NM 19950721004361995072100436NM 1995 7 21 AALA951039 119950605A5315143T10607 FLOOR BEAM BOEING767 767223 1385123NM FS 500 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FLOOR BEAM CORRODED BEYOND LIMITS SRM AFTER BLEND-OUT. INSTALL ANGLE 0.10 INCH THICK 7075-T6 EXTRUSION WET WITH BMS 5-95 FAY SURFACE SEALANT PER B767 SRM AND ENGINEERING MRB 767-943. (M) 2L72 4F RTA1NM 19950721004371995072100437NM 1995 7 21 AALA951040 119950605A5311146T1216 FRAME BOEING767 767223 1385123NM FS 1417 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FRAME WEB CORRODED BEYOND SRM LIMITS AFTER BLEND-OUT. FABRICATE DOUBLER 0.040 INCH THICK FROM 7075-T6 AND INSTALL WET WITH BMS 5-25 SEALANT PER B767 SRM AND ENGINEERING MRB 767-237. (M) 2L72 4F RTA1NM 19950721004381995072100438NM 1995 7 21 AALA951041 119950605A5313141T3001 STRINGER BOEING767 767223 1385123NM FS 434 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - STRINGER CORRODED UNDER PRODUCTION SPLICE. FABRICATE A NEW SPLICE 3.25 INCHES LONGER. INSTALLED AND FINISH WITH FAY SURFACE SEALANT PER 767 SRM AND ENGINEERING MRB 767-940. (M) 2L72 4F RTA1NM 19950721004391995072100439NM 1995 7 21 AALA951042 119950605A5330143T3220 SKIN BOEING767 767223 1385123NM FS 665 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FUSELAGE SKIN UNDER ANTENNA HAS CORROSION BEYOND SRM LIMITS AFTER BLENDOUT. REFINISH BLENDED AREA PER 767 SRM 53-00-01 FIG 101 AND ENGINEERING MRB 767-238. (M) 2L72 4F RTA1NM 19950721004401995072100440NM 1995 7 21 AALA951044 119950605A5330143T3210 SKIN BOEING767 767223 1385123NM FS 643 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FUSELAGE SKIN FOUND CORRODED. REFINISH BLENDED AREA. FABRICATE AND INSTALL DOUBLER .071 THICK PER 767 SRM 53-00-01 FIGURE 201. APPLY CORROSION INHIBITING COMPOUND TO THE INTERIOR OF REPAIR PER ENGINEERING MRB 767-234. (M) 2L72 4F RTA1NM 19950721004411995072100441NM 1995 7 21 AALA951045 119950602A5330141T3220 SKIN BOEING767 767223 1385123NM FS 368-347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - FUSELAGE SKIN HAS CORROSION. BLEND AND REFINISH PER 767 SRM 53-00-01 FIG 101. BLEND-OUTS ARE SATISFACTORY PER ENGINEERING MRB-933. (M) 2L72 4F RTA1NM 19950721004421995072100442NM 1995 7 21 AALA951046 119950602A5313146T3003 STRINGER BOEING767 767223 1385123NM BS 1307 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07304AA 22310 AFW - STRINGERS ARE CORRODED UNDER THE PRODUCTION SPLICE JUST AFT OF FRAME 1307. REMOVED EXISTING SPLICE. FABRICATE NEW SPLICE 5 INCHES LONGER. REFINISH AND INSTALL REPAIR SPLICE WITH FAY SURFACE SEALANT PER 767 SRM AND ENGINEERING MRB 767-932. (M) 2L72 4F RTA1NM 19950721004431995072100443EU 1995 7 21 AALA951056 119950606A2910 B-NUT FOKKERF28 F28MK0100 4990807EU HYD VALVE LOOSE A AALAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS CRCRUISE 1 SW071406A 11359 BNA - FLT NR 2092 - EN ROUTE DFW/BNA, DURING CRUISE HYDRAULIC SYSTEM 1 LOW QUANTITY INDICATED ON MFDU. HYDRAULIC SYSTEM 1 QUANTITY INDICATED BETWEEN 35 AND 36 PERCENT. DEACTIVATED SYSTEM 1 PUMP 1 AND 2, AND AIRCRAFT PROCEEDED TO BNA. ACCOMPLISHED ALTERNATE FLAP AND LANDING GEAR EXTENSION AND AIRCRAFT LANDED BNA WITHOUT INCIDENT. RESECURED LOOSE 'B' NUT AT NR 1 PRIORITY VALVE. SERVICED HYDRAULIC SYSTEM. HYDRAULIC SYSTEM 1 LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950721004441995072100444WP 1995 7 21 AALA951065 119950606A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07147AA 46702 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT AISLE BETWEEN MID GALLEY AND PASSENGER SEAT ROW 19G INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT 19G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950721004451995072100445WP 1995 7 21 AALA951066 119950607A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07479AA 49654 MIA - DURING OVERNIGHT CHECK, EMEREGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 15 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721004461995072100446NM 1995 7 21 AALA951067 119950605A3297 WIRE BOEING727 727223 1384074NM NLG BROKEN A AALAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW076813 19488 ORD - FLT 1262 - DURING APPROACH TO ORD WHEN LANDING GEAR EXTENDED, NOSE LANDING GEAR RED LIGHT REMAINED ILLUMINATED WITH NO GREEN LIGHT. RECYCLED LANDING GEAR WITH SAME RESULTS. WHILE ACCOMPLISHING A GO-AROUND RED NOSE LANDING GEAR LIGHT EXTINGUISHED AND GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT NOSE LANDING GEAR UP AND LOCKED SWITCH PIN A08. ALSO, REPLACED NOSE LANDING GEAR UP AND LOCKED SWITCH FOUND DEFECTIVE DURING TROUBLESHOOTING. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950721004471995072100447NM 1995 7 21 AALA951102 119950615A5315141T5111 FLOOR BEAM BOEING767 767223 1385123NM FS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - FORWARD FLANGE OF THE CABIN FLOOR BEAM UPPER CHORD CORRODED. DAMAGED AREA FOUND TO BE BEYOND SRM LIMITS AFTER BLENDING. ACCOMPLISHED REPAIRED PER SRM 53-00-51 FIG 202 EXCEPT WITH THE OUTBOARD VERTICAL LEG OF THE REPAIR ANGLE JOGGED DOWN BELOW THE -45 ANGLE AND STOPPED AT THE -92 ANGLE APPROVED BY ENGINEERING PER MRB767-951. (M) 2L72 4F RTA1NM 19950721004481995072100448WP 1995 7 21 AALA951132 119950620A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN OPEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07481AA 49656 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY NR 2 GALLEY INOPERATIVE. REPAIRED WIRE SPLICE IN EMERGENCY FLOOR LIGHTS BY NR 2 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950721004491995072100449WP 1995 7 21 AALA951134 119950621A3350 EEL CONDUCTOR DOUG DC9 DC983 3022083WP CABIN FLOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07591AA 53254 DFW - DURING ACCOMPLISHMENT OF PS CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 19950721004501995072100450NM 1995 7 21 ASAA9510061 119950622A335020131A EEL BATTERY BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 10 AND 11. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004511995072100451NM 1995 7 21 ASAA9510062 119950623A335086210144 EEL BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE FORWARD BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004521995072100452NM 1995 7 21 ASAA9510063 119950625A3350900835A EEL BATT PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004531995072100453NM 1995 7 21 ASAA9540030 119950621A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01771AS 25104 SEA - FLT 110 - CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS INOP AT ROWS 15. FOUND WIRES DISCONNECTED AT ROW 15. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950721004541995072100454NM 1995 7 21 ASAA9540031 119950622A3230 CIRCUIT BREAKER BOEING737 7374Q8 NM LANDING GEAR TRIPPED A ASAAO OTHER O OTHER TOTAKEOFF 1 NM01773AS 25106 SEA - FLT 385 - CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM OAK. USED OVERRIDE TO RETRACT GEAR. FOUND LATCH AND PRESS WARNING CIRCUIT BREAKER TRIPPED. RESET BREAKER. LANDED WITHOUT INCIDENT. PERFORMED MAIN GEAR EXTENSION/RETRACTION TEST AND UNABLE TO DUPLICATE PROBLEM. CYCLED GEAR SEVERAL TIMES AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950721004551995072100455NM 1995 7 21 AWXA9500404 119950629A3350 EEL WIRING BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 20 AND 21. RECONNECTED WIRING, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950721004561995072100456NM 1995 7 21 AWXA9500407 119950630A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 14. RESECURED WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950721004571995072100457NM 1995 7 21 AWXA9500408 119950626A5315 FLOOR BEAM BOEING737 7373G7 1384595NM BS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING SCHEDULED C6 INSPECTION, FOUND MAIN CABIN FLOOR BEAM UPPER CHORD CORRODED, STATION 312 LBL 24 TO LBL 18. REPAIRED FLOOR BEAM PER SRM 53-10-51, FIG 205. (M) 2L72 4F RTA16WE 19950721004581995072100458NM 1995 7 21 AWXA9500409 119950626A5210 DOOR CHORD BOEING737 7373G7 1384595NM BS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING SCHEDULED C6 INSPECTION, FOUND R1 DOOR CHORD CORRODED FROM STATION 312 TO STATION 344. REMOVED CORROSION IAW SRM 53-10-15. (M) 2L72 4F RTA16WE 19950721004591995072100459NM 1995 7 21 AWXA9500410 119950626A5320 FITTING BOEING737 7373G7 1384595NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING SCHEDULED C6 INSPECTION, FOUND L1 DOOR FORWARD GIRT BAR ATTACH FITTING CORRODED. FABRICATED NEW ATTACH FITTING IAW SRM 51-10-02. (M) 2L72 4F RTA16WE 19950721004601995072100460NM 1995 7 21 AWXA9500411 119950626A53471A0870129 SEAT TRACK BOEING737 7373G7 1384595NM RT COCKPIT WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28311AW 24712 PHX - DURING SCHEDULED C6 INSPECTION, FOUND FLIGHT OFFICERS ADJUSTABLE SEAT STOP TRACK WORN BEYOND LIMITS. REMOVED AND REPLACED TRACK ASSEMBLY PER SRM 53-00-52. (M) 2L72 4F RTA16WE 19950721004611995072100461WP 1995 7 21 USAA950583 119950504A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 980 FLOOR BEAM RIGHT LAVATORY, TASK NR C57-53300. INSTALLED FILLER AND SUPPORT ANGLE PER SRM 53-10-14. (M) 2L72 4F A6WE 19950721004621995072100462WP 1995 7 21 USAA950584 119950424A5313 LONGERON DOUG DC9 DC931 3022065WP BS 180 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK AT HI-LOK AT LONGERON 3 LEFT STATION 180. INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19950721004631995072100463WP 1995 7 21 USAA950595 119950504A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19939VJ37940 48120 PIT - DURING SCHEDULED Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK FUSELAGE SKIN RIGHT AFT NOSE GEAR DOOR AFT HINGE AREA. STOP DRILLED CRACK AND INSTALLED DOUBLER PER USAIR TYPICAL REPAIR 53-30-19. (M) 2L72 4F A6WE 19950721004641995072100464NM 1995 7 21 USAA950611 119950615A3230 SENSOR BOEING737 7374B7 1384702NM MLG OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19778AU 24980 CLT - FLT 129 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MLG AIR SAFETY SENSOR TO TARGET CLEARANCE EXCESSIVE. ADJUSTED SENSOR PER MM 32-09-01. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 19950721004651995072100465WP 1995 7 21 95ZZZM228 119950623A335020134 EEL BATTERIES DOUG DC9 DC982 3022082WP AFT CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERIES AND LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9580148. 2L72 4F A6WE 19950721004661995072100466WP 1995 7 21 95ZZZM229 119950610A5311561422924 FRAME DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 FOUND CORROSION AT FS 19 ON FRAME BETWEEN L-29R AND L-31R. FOUND FRAME TO BE OUT OF LIMITS REPAIRED AS PER DOUGLAS FAX FILE NR 268168 GLP 145/95-05-00-001. (M) 2L74 4F 4A25 19950721004671995072100467WP 1995 7 21 95ZZZM230 119950610A5330 SKIN DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19345JW 46042 FOUND CORROSION AT FS 12 ON FRAME AND FUSELAGE SKIN BETWEEN L29R AND 31R. FOUND SKIN AND FRAME BEYOND LIMITS, CUT AREA OF SKIN AND FRAME REPAIR AREA AS PER DOUGLAS FAX NR 268168 GLP 145/95-05-00-001. (M) 2L74 4F 4A25 19950721004681995072100468EU 1995 7 21 95ZZZM231 119950612A792089413016014 O-RINGS BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A NVEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO03933AE 933 FLT NR 4465 - TYS - ON DESCENT THE RIGHT ENGINE OIL PRESSURE LIGHT ILLUMINATED, COCKPIT INDICATOR INDICATED A LOSS OF PRESSURE. THE ENGINE WAS SHUT DOWN BEFORE TOTAL LOSS OF OIL PRESSURE OCCURRED. MAINTENANCE FOUND O-RINGS ON OIL BYPASS VALVE LEAKING. MAINTENANCE REPLACED THE OIL BYPASS VALVE O-RINGS. THE BYPASS VALVE WAS ALSO REPLACED FOR PRECAUTIONARY MEASURES. PERFORMED GROUND RUN NO LEAKS NOTED. (M) 2L72 4T RTA56EU 19950721004691995072100469NM 1995 7 21 ASAA9510056 119950603A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS AT ROW 14 WERE FOUND ON AND REMAINED ON AFTER RESETTING. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004701995072100470NM 1995 7 21 ASAA9510057 119950604A335086210151 EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT TRANSMITTER ON THE PALLET MOD WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004711995072100471NM 1995 7 21 ASAA9510058 119950604A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 SEA - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950721004721995072100472NM 1995 7 21 ASAA9540022 119950515A3350S283T0143 EEL BATT CHARGER BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - L1 DOOR EMERGENCY EXIT IDENTIFIER INOP. MAINTENANCE REPLACED M1132 POWER SUPPLY. (M) 2L72 4F RTA16WE 19950721004731995072100473NM 1995 7 21 ASAA9540025 119950603A3350 EEL WIRING BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 SEA - DURING MAINTENANCE CHECK, THE LAST THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950721004741995072100474NM 1995 7 21 ASAA9540026 119950603A3350 EEL WIRING BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROW 22 AND AFT WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950721004751995072100475NM 1995 7 21 ASAA9540029 119950620A33501619 EEL LAMP BOEING737 7374Q8 NM CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01769AS 25103 SEA - ROW 27 DEF EMERGENCY LIGHT ON BULLNOSE INOP. MAINTENANCE RE-LAMPED. (M) 2L72 4F RTA16WE 19950721004761995072100476NM 1995 7 21 ASAA9540032 119950623A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - ROW NR 9 WHITE FLOOR EMERGENCY LIGHT INOP. MAINTENANCE RECONNECTED LOOSE WIRE. (M) 2L72 4F RTA16WE 19950721004771995072100477 1995 7 21 ASAA9580114 419950517A2565D29982107 EVAC SLIDE DOUG DC9 DC983 3022083WP FWD ENTRY DOOR FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01963AS 53077 OAK - DURING C-CHECK, THE FORWARD ENTRY DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE EVACUATION SLIDE WITH A SERVICEABLE UNIT. (M) 2L72 4F RTA6WE 19950721004781995072100478WP 1995 7 21 ASAA9580123 119950524A33501001191 EEL PORTABLE DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS20666 49925 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004791995072100479WP 1995 7 21 ASAA9580124 119950524A3350251 EEL FUSE DOUG DC9 DC982 3022082WP CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004801995072100480WP 1995 7 21 ASAA9580125 119950524A3260SS092200017019 THROTTLE SWITCH DOUG DC9 DC983 3022083WP FWD PEDESTAL DEFECTIVE A ASAAO OTHER N FALSE WARNING CLCLIMB 1 NM01960AS 53074 SEA - ON ARRIVAL OF FLIGHT NR 375, CREW REPORTED UPON DEPARTURE FROM SFO WHEN THE LANDING GEAR WAS RETRACTED THE GEAR WARNING HORN SOUNDED AND ALL THREE GEAR UNSAFE LIGHTS ON, GEAR APPEARED TO RETRACT NORMALLY. CYCLED LANDING GEAR AND RETRACTION APPEARED NORMAL EXCEPT ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED FOR APPROXIMATELY 30 SECONDS, THEN EXTINGUISHED. FOUND PINS 'V' AND 'Y' OF CONNECTOR P1-1194 SHORTED WITH RIGHT THROTTLE ADVANCED OR RETARDED. REPLACED AND ADJUSTED RIGHT THROTTLE SWITCH ASSEMBLY. (M) 2L72 4F RTA6WE 19950721004811995072100481WP 1995 7 21 ASAA9580128 119950527A33501001191 EEL PORTABLE DOUG DC9 DC982 3022082WP FWD CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS136761396 49925 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004821995072100482WP 1995 7 21 ASAA9580129 119950528A3350RPS1B EEL POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01940AS 49825 PDX - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATAIVE. REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004831995072100483WP 1995 7 21 ASAA9580146 119950621A335060030431 EEL BATTERY PACK DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT OVERWING EXITS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950721004841995072100484WP 1995 7 21 ASAA9580147 119950621A3350 EEL GROUND DOUG DC9 DC983 3022083WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 13 TO 21 WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950721004851995072100485WP 1995 7 21 ASAA9580148 119950623A3350RPS1B EEL PWR SUPPLY DOUG DC9 DC982 3022082WP AFT CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004861995072100486WP 1995 7 21 ASAA9580149 119950624A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004871995072100487WP 1995 7 21 ASAA9580150 119950625A3350RPS1B EEL POWER SUPPLY DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST TXTAXI/GRND HDL 1 NM01944AS 53019 PDX - BLOCK TURN BACK OF FLIGHT 564 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 14 TO 20 WERE FOUND INOPERATIVE DURING TEST. REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950721004881995072100488WP 1995 7 21 ASAA9580151 119950626A335060030431 EEL BATTERY PACK DOUG DC9 DC982 3022082WP TAILCONE DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, TWO EMERGENCY FLOOD LIGHTS IN TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950721004891995072100489EA 1995 7 21 COEA9522202 119950512A4900 DUCT FRCHLDF27 F27F 3373008EA APU OUT OF POSITION A COEAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 NM01222DG 31 FLT 7378 - MSY - DURING CRUISE CREW STARTED THE APU FOR BACKUP AFTER NOTICING THEIR BATTERIES WERE DISCHARGING. AFTER THE APU WAS STARTED THE FIRE WARNING ALARM WENT OFF. CREW ELECTED TO DISCHARGE FIRE BOTTLE. AIRCRAFT LANDED IN MSY WITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVEALED COOLING DUCT FOR HOT SECTION OUT OF ALIGNMENT. ALIGNED DUCT, APU OPS CHECKED GOOD. PLACARDED PER MEL 26-22-3 CAT C DUE TO LACK OF SPARE FIRE BOTTLE. AIRCRAFT RETURNED TO SERVICE. 2H72 4T 7A1 19950721004901995072100490WP 1995 7 21 HAL95082 119950629A27204913801CS17723 CONTROL CABLE DOUG DC9 DC951 3022051WP RUDDER BROKEN A HALAK NONE O OTHER ININSP/MAINT 1 WP13709HA 47764 HNL - FLT NR 526 - DURING MANUAL RUDDER CHECK, APPLIED RIGHT RUDDER PRESSURE AND PEDAL RELEASED AND FREE FLOATED WITH NO TENSION. FOUND RUDDER CABLE 2C BROKEN. SWAGGED BALL END AND TURNBUCKLE END ON 2C AND 1C CABLE. INSTALLED CABLE 2C AND 1C AND TESTED PER MM 27-20-0. SAFETIED, CLOSED UP AND OPERATIONAL CHECKED GOOD. (M) 2L72 4F RTA6WE 19950721004911995072100491EU 1995 7 21 M3HA95013 119950627A33503011151 EEL BATTERY AEROSPATR42 ATR42320 8680930EU CABIN DISCHARGED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13986MH1294 2266 360 HNL - EMERGENCY BATTERY VOLTAGE LOW. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY FOR LIGHTS IAW JIC 33-51-21 RAI 10010-001, OPS CHECK GOOD. (M) 2H72 4T RTA53EU 19950721004921995072100492 1995 7 21 SIMA951791 419950628A342170031109 EADI AEROSPATR42 ATR42300 8680920EU NR 2 FAILED A SIMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21354AT 9104516 354 ORD - FLT 4042 - ON TAXI OUT THE FLIGHT OFFICERS ADI DISPLAY WENT BLANK AND SMOKED UP THE COCKPIT. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 EADI. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950721004931995072100493EU 1995 7 21 SIMA951792 119950628A56107256100502 WINDSCREEN SAAB SF340 340B 7860101EU RT COCKPIT DELAMINATED A SIMAA UNSCHED LANDING O OTHER CRCRUISE 1 SW21589MA 652 340B172 ABI - FLT NR 3579 - FLIGHT OFFICER'S FWD WINDSCREEN DEVELOPED A LARGE BUBBLE WHILE IN FLIGHT. AIRCRAFT DIVERTED TO ABI. CHANGED FLIGHT OFFICER'S WINDSCREEN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950721004941995072100494EU 1995 7 21 SIMA951822 119950701A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU STAIRS FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21420MQ 459 012 ORD - FLT NR 4011 - PASSENGER STAIR/DOOR INTEGRAL EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950721004951995072100495NM 1995 7 21 TAOA069505 119950625A335037067001 EEL BATT PACK MARATHON BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 22043 AFT STAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19950721004961995072100496NM 1995 7 21 TAOA069506 119950625A335090052 EEL BATT BASE BOEING727 727294 1384088NM CABIN INOPERATIVE A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS T4033 22043 WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. LIGHT AT R2/L2 BLINKING. REPLACED BATTERY BASE. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19950721004971995072100497NM 1995 7 21 TWRA9539 119950625A2560 ESCAPE SLIDE BOEING747 747238B 1384828NM COCKPIT OFF TRACK A TWRAK NONE O OTHER TXTAXI/GRND HDL 1 EA15607PE 20011 DURING PREFLIGHT, FLIGHT ENGINEER WAS UNABLE TO LOCK CREW ESCAPE SLIDE IN THE FORWARD POSITION. MAINTENANCE REPOSITIONED HOUSING BACK IN THE TRACK. OPS CHECK OK. (M) 2L74 4F A20WE 19950721004981995072100498EU 1995 7 21 VTZA95210 119950628A76002118846 IEC JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27310UE 41028 FLT NR 6408 - IAD-PWM - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE EGT COMPENSATOR, MAX FUEL FLOW AND DECELERATION SCHEDULE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERAVICE. (M) 2L72 4T RTA41NM 19950721004991995072100499SO 1995 7 21 WTAA950215 119950621A3350F02A250VIA EEL FUSE EMB 120 EMB120RT SO CABIN BLOWN A WTAAK NONE L NO TEST NRNOT REPORTED 1 WP17286UE 120175 SFO - CABIN EMERGENCY FLOOR TRACK LIGHTING REPORTED PARTIALLY INOPERATIVE. MAINTENACNE DEFERRED EMERGENCY LIGHTS PER MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL BY THE REPLACEMENT OF FUSE (F0031). (M) 2L72 4T RTA31SO 19950721005001995072100500EU 1995 7 21 WTAA950217 119950622A32301862F RADIUS ROD BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17430UE 784 SFO - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR RADIUS ROD ASSEMBLY. LANDING GEAR OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950721005011995072100501EU 1995 7 21 WTAA950218 119950623A3260 GEAR LIGHT BAG JETSTMJETSTM3101 1500215EU LT MLG ILLUMINATED A WTAAO OTHER N FALSE WARNING DEDESCENT 1 WP17428UE 806 SFO - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR EXTENSION. CREW CYCLED LANDING GEAR. NORMAL POSITION INDICATIONS RECEIVED FOLLOWING SECOND GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT MAIN GEAR UPLOCK AND DOWNLOCK MICROSWITCHES AND ASSOCIATED WIRING. NO DEFECTS NOTED. LANDING GEAR POSITION INDICATION SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950721005021995072100502EU 1995 7 21 WTAA950219 119950625A3260622800200 SWITCH BAG JETSTMJETSTM3101 1500215EU LT MLG LACK OF LUBE A WTAAO OTHER N FALSE WARNING DEDESCENT 1 WP17428UE 806 STS - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED FOLLOWING GEAR EXTENSION. NORMAL POSITION INDICATIONS RECEIVED FOLLOWING SUBSEQUENT GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO SFO FOR REPAIRS. INSPECTED LEFT MAIN GEAR UPLOCK AND DOWNLOCK MICROSWITCHES AND ASSOCIATED WIRING. NO DEFECTS NOTED. CLEANED AND LUBED LEFT MAIN GEAR UPLOCK AND DOWNLOCK MICROSWITCHES. GEAR POSITION INDICATIONS NORMAL DURING TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950721005031995072100503SO 1995 7 21 WTAA950220 119950624A7540 DUCT LEAK LIGHT EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE ILLUMINATED A WTAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 WP17250YV 120250 SFO - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. CREW SHUTOFF RIGHT ENGINE BLEED AIR VALVE. LIGHT REMAINED ON. CREW SECURED RIGHT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED BLEED AIR SYSTEM, WITH NO EVIDENCE OF AIR LEAK NOTED. DEFERRED RIGHT ENGINE BLEED 'DUCT LEAK' LIGHT PER MEL 36-21-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19950721005041995072100504EU 1995 7 21 WTAA950221 119950625A7333151906002 TRANSMITTER BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RT ENGINE FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17418UE 780 SMF - RT ENGINE FUEL FLOW INDICATION DROPPED TO ZERO DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED RIGHT ENGINE FUEL FLOW METER PER MEL 73-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL WITH THE REPLACEMENT OF THE RIGHT ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHECK SATISFACTORY. (M) 2L72 4T4 TRTA21EU E4WE 19950721005071995072100507CE 1995 7 21 95ZZZX3428 119950621A7110CA183241P FASTENERS BEECH 2000 2000 1152000CE FAILED A ADEBAK NONE O OTHER ININSP/MAINT 1 CE038246S1000 NC18 DURING INSPECTION FOUND VENTRAL FIN DAMAGED. FOUND UPPER COWLING FASTENER HAD COME LOOSE, STRUCK PROPELLER AND WAS THEN THROWN INTO VENTRAL FIN. FASTENER WAS STILL LODGED IN FIN. PROPELLER WAS REMOVED FOR REPAIRS AND FIN REPAIRED PER STRUCTURAL REPAIR MANUAL. 1L72 4T RTA38ACE 19950721005121995072100512CE 1995 7 21 95ZZZX3433 119950601A3244178K235 TIRE LEAR 35 35A 5170602CE NR 1 MLG FAILED AL MLQAA UNSCHED LANDING C F.O.D. CLCLIMB 1 WP05317TT 20831782 317 TIRE SEPARATED ON ROTATION AND INGESTED TO NR 1 ENGINE, FODDING ENGINE. 2L72 4F A10CE 19950721005131995072100513EU 1995 7 21 95ZZZX3434 119950608A273025CT223 QUADRANT HWKSLYDH125 HS125600A 4230158EU ELEV CONTL CORRODED APAJGVAK NONE O OTHER ININSP/MAINT 1 CE09600G 9534 256066 DURING A VISUAL INSPECTION OF THE ELEVATOR QUADRANT, WHILE POWDER WAS NOTED AROUND THE UPPER CONTROL CABLE ATTACH POINT BARREL. REMOVAL OF BOTH CABLES FOUND DEEP CORROSION IN THE CONTROL CABLE ATTACH POINTS ON THE QUADRANT. THE 2400-HOUR, 24- AND 48-MONTH INSPECTIONS CALL OUT FOR AN INSPECTION OF COMPONENTS AND CABLES IN THE HORIZONTAL STABILIZER AREA. NOTHING ABOUT REMOVING CABLES. WITHOUT REMOVING THE CONTROL CABLES AND BARRELS FROM QUADRANT, THIS AREA WOULD NOT BE LOOKED AT. 2L72 4J A3EU 19950721005141995072100514NE 1995 7 21 HAL95073 219950621A7230 COMP BLADES DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE DAMAGED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 OGG - FLT 559 - AFTER LANDING IN MAUI, NR 1 ENGINE FOUND WITH 11 BLADES DAMAGED. LARGEST DAMAGED BLADE WAS .5937 INCH BY .50 INCH LONG. REPLACED LEFT ENGINE ASSEMBLY PER HAWAIIAN AIRLINES STANDARD PRACTICE DC-9, HAL M143 DC-9-50 INSTALLATION REV 59 DATED 1-11-95. (X) 2L72 4F4 F A6WE E2EA 19950721005151995072100515WP 1995 7 21 HAL95076 119950623A3350 EEL BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 8625 48122 INFORMATION FROM M-71 LOG PAGE 148403-1. AFT EMERGENCY FLOOR LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950721005161995072100516WP 1995 7 21 HAL95077 119950623A335060030431 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 11914 47742 HNL - INFORMATION FROM M-71 LOG PAGE 142429-4. OVERHEAD EMERGENCY LIGHTS BETWEEN ROW 6 AND ROW 12 ARE INOPERABLE. REPLACED EMERGENCY BATTERY POWER SUPPLY ABOVE ROW 10R. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950721005171995072100517 1995 7 21 RAIA950631 419950622A34257003360944 COMPUTER AEROSPATR42 ATR42300 8680920EU AVIONICS BAY FAILED A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE032FOR 10492 199 STL - FLT 7230 - NR 2 AHRS FAILED IN-FLIGHT. MAINTENANCE REPLACED NR 2 AHRS COMPUTER. (X) 2H72 4T RTA53EU 19950721005181995072100518WP 1995 7 21 9510879995 119950505A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 37 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 37 FORWARD PRESSURE BULKHEAD AT THE 10 O'CLOCK POSITION NEAR THE RADOME CENTERING PIN. REPAIRED PER EA 99-93550. 2L72 4F A6WE 19950721005191995072100519WP 1995 7 21 9510889995 119950531A5312 BULKHEAD DOUG DC9 DC931 3022065WP AFT CARGO CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT CARGO, AFT BULKHEAD BETWEEN RBL 12 - RBL 36. REPAIRED PER EA 99-192235. 2L72 4F A6WE 19950721005201995072100520WP 1995 7 21 9510899919 119950601A5330 SKIN DOUG DC9 DC932 3022066WP MCD CUTOUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01941N 47450 DURING PERIODIC CHECK, FOUND .50 INCH CRACK IN THE FUSELAGE SKIN EXTENDING FROM THE MAIN CABIN DOOR UPPER AFT DOOR STOP HOLE. REPAIRED PER EA 99-98394. 2L72 4F A6WE 19950721005211995072100521WP 1995 7 21 9510909995 119950603A5415 YOKE DOUG DC9 DC931 3022065WP NR 2 ENGINE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FASTENER HOLE FOR THE RIGHT ENGINE YOKE ISOLATOR MOUNT AT THE FORWARD SPAR. REPAIRED YOKE PER EA 99-93566. 2L72 4F A6WE 19950721005221995072100522WP 1995 7 21 9510919995 119950606A5330 SKIN DOUG DC9 DC931 3022065WP FS 895-915 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE SKIN DOUBLER, LONGERON 23L BETWEEN FS 895 - 915. REPAIRED PER EA 99-92183. 2L72 4F A6WE 19950721005231995072100523WP 1995 7 21 9510929995 119950606A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 110 BULKHEAD FORWARD CAP AT APPROXIMATELY LONGERON 26R IN THE NOSE LANDING GEAR WELL. REPAIRED PER EA 99-92197. 2L72 4F A6WE 19950721005241995072100524NM 1995 7 21 9510932709 119950609A5341 CHORD BOEING727 727225 1384077NM FS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01818EA 22555 DURING PERIODIC CHECK, FOUND CRACKS IN THE WING-TO-BODY RIB UPPER CHORD, BOTH UPPER AND LOWER FORWARD FASTENER HOLES BS 760, LBL 70.5. REPAIRED PER EA 27-98428. 2L73 4F A3WE 19950721005251995072100525WP 1995 7 21 9510949755 119950615A5313 LONGERON DOUG DC9 DC941 302207NWP FS 973 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01755NW 47179 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 30 AFT OF FS 973. REPAIRED PER EA 97-98399. 2L72 4F A6WE 19950721005261995072100526WP 1995 7 21 9510959995 119950615A5330 SKIN DOUG DC9 DC931 3022065WP FS 130 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FUSELAGE SKIN AT FS 130, LEFT SIDE ABOVE THE CUSP. REPAIRED PER EA 99-93534. 2L72 4F A6WE 19950721005271995072100527WP 1995 7 21 9510969995 119950615A5320 SUPPORT DOUG DC9 DC931 3022065WP FS 1087 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 1087 SUPPORT AT LONGERON 24L FORWARD FACE, FORWARD END. REPAIRED PER EA 99-92198. 2L72 4F A6WE 19950721005281995072100528WP 1995 7 21 9510979755 119950617A5330 SKIN DOUG DC9 DC941 302207NWP EXT PWR CAVITY CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01755NW 47179 DURING PERIORIC CHECK, FOUND A CRACK IN THE EXTERNAL POWER RECEPTACLE CAVITY FORWARD LOWER CORNER. REPAIRED PER EA 97-98402. 2L72 4F A6WE 19950721005291995072100529WP 1995 7 21 9510989755 119950620A5313 LONGERON DOUG DC9 DC941 302207NWP FS 794 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01755NW 47179 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 30 AT FS 794. REPAIRED LONGERON AND SKIN PER EA 97-98403. 2L72 4F A6WE 19950721005301995072100530WP 1995 7 21 9510999995 119950628A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 965 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FUSELAGE TO BULKHEAD CLIP AT FS 965 JUST BELOW RADIAL 15. REPAIRED PER EA 99-92296. 2L72 4F A6WE 19950721005311995072100531WP 1995 7 21 9511009997 119950712A5320 FITTING DOUG DC9 DC931 3022065WP FS 587 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING "H" CHECK, FOUND A ONE INCH CRACK IN THE LONGERON 24R, 25R, AND 26R END FITTINGS AT FS 587. REPLACED FITTINGS PER SRM 51-30-2. 2L72 4F A6WE 19950721005321995072100532WP 1995 7 21 9511019964 119950713A5320 FITTING DOUG DC9 DC931 3022065WP FWD SVC DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01912RW 47150 DURING "H" CHECK, FOUND CORROSION ON THE FORWARD SERVICE DOOR JAMB FITTING LOWER FORWARD CORNER. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950721005331995072100533WP 1995 7 21 9511029607 119950713A5320 FITTING DOUG DC9 DC932 3022066WP FS 943 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 943 TIE FITTINGS AT LONGERONS 22R, 26R, AND 28R. REPLACED FITTINGS PER ARM 51-10, 51-30, 53-01. 2L72 4F A6WE 19950721005341995072100534WP 1995 7 21 9511039607 119950713A5320 FITTING DOUG DC9 DC932 3022066WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 604 TIE FITTING AT LONGERON 30. REPLACED FITTING (P/N 5920331-1) PER SRM 53-11. 2L72 4F A6WE 19950721005351995072100535WP 1995 7 21 9511049997 119950713A5320 FRAME DOUG DC9 DC931 3022065WP FS 84 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING "H" CHECK, FOUND CORROSION ON THE FS 84 FRAME FITTING LOWER RIGHT SIDE. REPLACED FITTING PER SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950721005361995072100536WP 1995 7 21 9511059607 119950714A5320 FITTING DOUG DC9 DC932 3022066WP FS 945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FLOOR SUPPORT FITTING AT THE FS 945 FRAME BETWEEN LONGERON 27L-28L. REPLACED FITTING (P/N 5956034-505) PER SRM 51-10 AND 51-30. 2L72 4F A6WE 19950721005371995072100537WP 1995 7 21 9511069907 119950717A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN FAILED A NWAABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01957N 47253 LOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT ENROUTE MEM-MIA. CABIN ALTITUDE REACHED 11,000 FEET AND CAPTAIN DECLARED AN EMERGENCY. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. PRESSURIZATION WAS REGAINED THROUGH MANUAL CONTROL AND FLIGHT CONTINUED TO DESTINATION WITHOUT FURTHER INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950721005381995072100538WP 1995 7 21 9511071147 119950629A3260 INDICATION DOUG DC10 DC1040 3023508WP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING LDLANDING 1 GL01147US 46756 DURING LANDING AT FRA FROM DTW, DID NOT GET GEAR DOWN SAFE INDICATION WHEN HANDLE SELECTED DOWN. RECYCLED GEAR AND GOT SAFE INDICATION. PERFORMED BITE CHECK AND NO FAULTS SHOWN. 2L73 4F A22WE 19950721005391995072100539NE 1995 7 21 9511081226 219950717A7200 ENGINE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2B 30018NE NR 1 FAILED A ANWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL E VIBRATION/BUFFET CLCLIMB 1 GL01226NW 46583 455317 DURING CLIMB, A THUD WAS HEARD FOLLOWED BY NR 1 ENGINE VIBRATION. THE ENGINE WAS SHUT DOWN AND THE FIRE BOTTLES WERE DISCHARGED AFTER A CABIN ATTENDANT NOTED FLAMES COMING FROM THE REAR OF THE ENGINE. NO INDICATION OF DISCHARGE OF EITHER BOTTLE WAS RECEIVED. 75,000 POUNDS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO DTW WHERE AN UNEVENTFUL TWO-ENGINE LANDING WAS ACCOMPLISHED. METAL WAS FOUND IN THE TAILPIPE AND THE AIRCRAFT WAS FERRIED TO MSP WHERE THE ENGINE WAS REPLACED. A FUNCTIONAL CHECK OF THE FIRE EXTINGUISHER SYSTEM FOUND IT TO BE OPERATIONAL AND THE SQUIBS AND FIRE BOTTLES HAD NOT BEEN FIRED. INVESTIGATION IN PROGRESS. 2L73 4F4 F A22WE E23EA 19950721005401995072100540NM 1995 7 21 9511092707 119950717A27821U11032 ACTUATOR BOEING727 727225 1384077NM NR 2/3 LE SLAT FAILED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01816EA1274 1274 22553 DURING CLIMB, LOST ALL "A" SYSTEM HYDRAULIC FLUID ABRUPTLY. REPORTED GRINDING NOISE FROM THE NR 1 ENGINE PRIOR TO LOSS. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 AND NR 3 LEADING EDGE SLAT ACTUATORS. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950721005411995072100541NM 1995 7 21 9511102717 119950719A215032167421 SHUTOFF VALVE BOEING727 7272S7 138407ZNM RT PACK FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 GL01721RC3664112449 22492 AFTER TAKEOFF AT FL 070, COULD NOT REINSTATE AIR CONDITIONING PACK. AIRCRAFT WOULD NOT MAINTAIN PRESSURE WITH ONE PACK OPERATION. JETTISONED 8000 POUNDS OF FUEL AND RETURNED TO RNO WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT PACK SHUT-OFF VALVE. OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950721005421995072100542 1995 7 21 9511115502 419950718A2300 TELEPHONE BOX BOEING757 757251 1384970NM CABIN MALFUNCTIONED A NWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01502US 23190 AT ALTITUDE, THERE WAS A STRONG ELECTRICAL SMOKE SMELL IN THE FIRST CLASS SECTION. THE SMELL WAS ISOLATED TO AN AIRPHONE UNDER-SEAT AUDIO BOX. THE AIRPHONE CIRCUIT BREAKER WAS PULLED AND THE BOX WAS REMOVED AND PLACED IN A PLASTIC BAG IN THE COCKPIT. BOTH CABIN RECIRCULATING FANS WERE TURNED OFF WHEN THE SMELL WAS DETECTED. REPLACED TELEHPONE'S UNDER-SEAT TELEPHONE BOX AND CHORD REELS AT SEATS 1A/B. OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA2NM 19950721005431995072100543NE 1995 7 21 COM31122 319950719A6114660714200 BOLT HOLE INSERT SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROP HUB CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01380CA142343001 340A012 DRG440988 FOUND CRACK IN PROPELLER HUB 109326 AROUND BOLT HOLE INSERT AT NR 3 BLADE PORT DURING S.B. 61-58, APPENDIX C, SCAN B. PROPELLER WAS DISASSEMBLED AND HUB REMOVED FROM SERVICE. 2L72 4T RTA52EU 6 CP61GL 19950721005441995072100544EU 1995 7 21 COM31123 119950718A261072111211000 DETECTOR SAAB SF340 SF340A 7850100EU CARGO FALSE WARN A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01341CA3468 340A021 CARGO SMOKE WARNING ACTIVATED DURING TAKEOFF. REPLACED THE CARGO SMOKE DETECTOR. 2L72 4T RTA52EU 19950721005451995072100545 1995 7 21 COM60521 419950717A3421 ATTITUDE IND CNDAIRCL600 CL6002B19 EA LEFT MALFUNCTIONED A COMAK NONE O OTHER UKUNKNOWN 1 SO01920CA 7022 PILOTS ATTITUDE INDICATOR ALL ONE COLOR, BACKGROUND PURPLE. COULD NOT DUPLICATE. FOUND PFD TO CHECK NORMAL. 2L72 4F RTA21EA 19950721005461995072100546WP 1995 7 21 DHL95801005 119950714A29101053406301 HOSE DOUG DC8 DC873F 302199FWP LT MLG RUPTURED A ADHLAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO01801DH 46033 AFTER LANDING, AIRCRAFT LOST ITS HYDRAULIC FLUID, LEFT BOGGIE TRIM CYLINDER HOSE RUPTURED. REMOVED AND REPLACED HOSE AND BLED PER MM 32-33-1. 2L74 4F RT4A25 19950721005471995072100547EU 1995 7 21 DL31L952041 119950512A7110PW4152 NOSE COWL AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 2 ENGINE DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11838AB7303 676 724912 NR 2 ENG INLET COWL OUTER BARREL COMPOSITE SKIN DELAMINATED. ACCOMPLISHED REPAIRS PER SRM 54-10-00, PG 201. 2L72 4F RTA35EU E24NE 19950721005481995072100548NM 1995 7 21 DL72E952419 119950602A5330 SKIN BOEING727 727247 138408FNM FS 904-946 LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO112829W 21481 FOUND DURING F-1 LETTER CHECK - 3 EACH LIGHTNING STRIKES ON TOP OF FUSELAGE BETWEEN STA 905-946 AND BETWEEN STRINGERS 5 AND 6R. REPAIRED PER SRM 53-04, FIG 38. 2L73 4F A3WE 19950721005491995072100549NM 1995 7 21 DL72E952529 119950606A5320 CLIP BOEING727 727247 138408FNM BS 1166 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND DURING CV-2 VISIT, CORROSION ON FORMER STA 1166 AFT SIDE BETWEEN STRINGERS 29L AND 27L. REPLACED SKIN CLIP. 2L73 4F A3WE 19950721005501995072100550NM 1995 7 21 DL72L952253 119950518A5330 SKIN BOEING727 727232 1384082NM BS 300 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11501DA 21303 FOUND ON CV 2 CHECK, REMOVED 7 INCH BY 8 INCH SECTION OF FUSELAGE SKIN TO FACILITATE MTC. REPAIRED AREA PER SRM 53-30-3, FIG 1. 2L73 4F A3WE 19950721005511995072100551NM 1995 7 21 DL72L953105 119950718A5320 WEB BOEING727 727232 1384082NM BS 1250 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND DURING C-2 LETTER CHECK, .1250 INCH CRACK AT LOWER LIGHTNING HOLE AT STA 1250 LT SIDE, ACCOMPLISHED REPAIRS PER M/M 53-11-0. 2L73 4F A3WE 19950721005521995072100552NM 1995 7 21 DL72L953106 119950718A5754 ANGLE BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND DURING C-2 LETTER CHECK - COVE SKIN ANGLE CRACKED FOR NR 8 L/E SLAT UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721005531995072100553NM 1995 7 21 DL72L953107 119950718A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND DURING C-2 LETTER CHECK - NR 2 L/E SLAT COVE SKIN ANGLE BELOW TAI DUCT CRACKED 1 INCH. REPAIRED ANGLE PER MM 57-54-0, 2L73 4F A3WE 19950721005541995072100554NM 1995 7 21 DL72L953108 119950718A5754 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND DURING C-2 LETTER CHECK - SLAT RIB CRACKED .3750 INCH FOR NR 6 ACTUATOR RIB UPPER FLANGE. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950721005551995072100555NM 1995 7 21 DL72S952236 119950430A5755 SKIN 6517348108A BOEING727 727232 1384082NM NR 7 SPOILER DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 3931N 21150 NR 7 SPOILER PANEL LOWER SURFACE WAS FOUND DENTED FROM TIRE BLOW OUT. REPAIRED PER SRM 57-50-6. 2L73 4F A3WE 19950721005561995072100556NM 1995 7 21 DL72S952239 119950510A57536521634149K PANEL BOEING727 727232 1384082NM NR 2 TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 DURING SHOP INSPECTION, FOUND NR 2 AFT FLAP PANEL L/E HAD WEAR DAMAGE AT 40 INCHES FROM O/B END. REPAIRED PER SRM 57-53-4. 2L73 4F A3WE 19950721005571995072100557NM 1995 7 21 DL72S952856 119950629A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11418DA 21271 COVE SKIN ANGLE CRACKED UNDER NR 3 SLAT TAI DUCT. FOUND DURING B-2 LTR CK. REPAIRED PER 57-54-0, PAR 2. 2L73 4F A3WE 19950721005581995072100558NM 1995 7 21 DL72S952863 119950629A5522 SKIN BOEING727 727232 1384082NM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11418DA 21271 FOUND DURING B-2 LETTER CHECK - HOLE BURNED THROUGH RT O/B ELEVATOR STATIC WICK BASE. REPAIRED PER SRM 55-20-3, FIG 2 SHT 1. 2L73 4F A3WE 19950721005591995072100559NM 1995 7 21 DL72S952871 119950628A5743 BUSHING BOEING727 727232 1384082NM LT MLG BEAM TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 LT MLG BEAM FABROID TORN IN BUSHINGS FOR O/B ATTACH FITTING. REPAIRED PER SRM 57-40, FIG 1. 2L73 4F A3WE 19950721005601995072100560NM 1995 7 21 DL72S952967 119950629A5320 INTERCOSTAL BOEING727 727232 1384082NM BS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION AT SKIN FORWARD OF STA 1070 OUTBOARD STR 28R, INBOARD OF INTERCOASTAL. REPAIR: REPAIRED PER ERA 302065-14. 2L73 4F A3WE 19950721005611995072100561NM 1995 7 21 DL72S952968 119950629A5313 STRINGER BOEING727 727232 1384082NM BS 1070 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION AT STR 28R, OUTBOARD SIDE JUST FORWARD OF STA 1070. REPAIR: REPAIRED PER ERA 302065-14. 2L73 4F A3WE 19950721005621995072100562NM 1995 7 21 DL72S952971 119950627A5313 STRINGER BOEING727 727232 1384082NM BS 480-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION INSIDE STR 27L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14. 2L73 4F A3WE 19950721005631995072100563NM 1995 7 21 DL72S952972 119950627A5330 SKIN BOEING727 727232 1384082NM BS 480-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK, CORROSION ON SKIN OUTBOARD SIDE OF STR 28L BETWEEN STA 480 AND STA 500. REPAIR: REPAIRED PER ERA 302043-14. 2L73 4F A3WE 19950721005641995072100564NM 1995 7 21 DL72S952973 119950627A5313 STRINGER BOEING727 727232 1384082NM BS 480-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 FOUND ON CV2 CHECK CORROSION ON OUTBOARD SIDE OF STR 28L BETWEEN STA 480-500. REPAIR: REPAIRED PER ERA 302043-14. 2L73 4F A3WE 19950721005651995072100565NM 1995 7 21 DL72S953100 119950628A57536521631326 LE SKIN BOEING727 727232 1384082NM NR 4 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 NR 4 FOREFLAP WAS FOUND WITH A TEMPORARY REPAIR ON THE LEADING EDGE 47 INCHES FROM OUTBOARD END. THE DOUBLER WAS REMOVED AND LEADING EDGE REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950721005661995072100566NM 1995 7 21 DL72S953101 119950628A57536521631326 LE SKIN BOEING727 727232 1384082NM NR 4 TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 NR 4 FOREFLAP LEADING EDGE WAS FOUND WORN 46 INCHES FROM INBOARD END. THE LEADING EDGE WAS REPAIRED PER SRM 57504 BY INSTALLING A DOUBLER. 2L73 4F A3WE 19950721005671995072100567NM 1995 7 21 DL72S953102 119950707A5330655838515 SKIN BOEING727 727232 1384082NM BS 950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING HMV INSPECTION, FOUND THE FUSELAGE SKIN BEHIND STRINGER 18A HAD A .3750 INCH CRACK AT BS 948. THE CRACK EMANATES FROM THE LOWER FASTENER ROW OF THE STR 18A ATTACHMENTS AND PROGRESSES DOWNWARD TO EDGE OF THE SKIN. THERE WAS ALSO INDICATION OF A CRACK PROGRESSING UPWARDS FROM THE SAME LOWER FASTENER. THE CRACKS WERE STOP DRILLED AND CRACK CONTAINMENT HAS BEEN VERIFIED BY HFEC, AND AN EXTERNAL STEEL REPAIR DOUBLER WILL BE INSTALLED IN ACCORDANCE WITH BACO TWX DAL-ATL-95-0662RR, DATED JULY 5, 1995. 2L73 4F A3WE 19950721005681995072100568NM 1995 7 21 DL72W952896 119950619A5320 WEB BOEING727 727247 138408FNM FS 795-800 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 WEB CORRODED, FS 795-800. INSTALLED NEW WEB PER SRM 51-40-2. FOUND AT HMV. 2L73 4F A3WE 19950721005691995072100569NM 1995 7 21 DL72W953109 119950718A5532 SKIN BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112820W 21058 FOUND DURING D-2 LETTER CHECK - .75 INCH CRACK IN VERT STAB SKIN RT SIDE JUST AFT OF NR 2 ENG NOSE COWL AT PANEL 9516 . REPAIRED PER M/M 54-30-0, PG 801-802. 2L73 4F A3WE 19950721005701995072100570NM 1995 7 21 DL72W953110 119950718A5754 ANGLE BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112820W 21058 FOUND DURING D-2 LETTER CHECK - ANGLE CRACKED UNDER NR 7 SLAT ANTI-ICE DUCT LOWER AFT END OF SLAT. REPAIRED PER M/M 57-54-0, FIG 805A. 2L73 4F A3WE 19950721005711995072100571NM 1995 7 21 DL733953114 119950710A5320 ANGLE BOEING737 737347 1384647NM BS 807 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112310 23596 FLOOR SUPPORT ANGLE CRACKED ABOVE STR 27L AT STA 807. REMOVED DAMAGED SECTION OF ANGLE, MADE REPAIR PARTS, AND INSTALLED PER SRM 53-00 -53, FIG 201. 2L72 4F RTA16WE 19950721005721995072100572NM 1995 7 21 DL73S953104 119950119A53306545768199 SKIN BOEING737 737232 1384475NM BS 360 DAMAGED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11302DL 23047 DURING LAYOVER IN ATLANTA, THE FUSELAGE SKIN WAS DAMAGED JUST AFT OF STATION 360 AND JUST ABOVE STRINGER 19R WHEN STRUCK BY A BAGGAGE CONTAINER. DAMAGE WAS CUT OUT AND REPAIRED WITH AN EXTERNAL DOUBLER IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIG 1 PER ER/A 300978-14. 2L72 4F RTA16WE 19950721005731995072100573NM 1995 7 21 DL757952257 119950524A5753113N280093SP SKIN BOEING757 757232 1384965NM TE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 NR-664 HOLE ON UPPER AND LOWER SURFACE APPROX 47 INCHES FROM INBD END AND 6 INCHES FROM T/E OF LT AFT FLAP ASSEMBLY. ACCOMPLISHED REPAIRS PER DL ERA 301659-14 AND SRN 57-53-01. 2L72 4F RTA2NM 19950721005741995072100574NM 1995 7 21 DL767952290 119950515A5753 SKIN BOEING767 767232 1385132NM LT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11106DA 22218 PREVIOUS REPAIR TO I/B LOWER SURFACE ON O/B FLAP IS DELAMINATED. WHEN DAMAGED AREA WAS REMOVED, WATER WAS FOUND. ACCOMPLISHED REPAIRS PER SRM 57-53-01. 2L72 4F RTA1NM 19950721005751995072100575NM 1995 7 21 DL767953118 119950620A5754114T410116A SKIN BOEING767 767232 1385132NM NR 12 LE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11107DL 22219 49984 NR 12 SLAT T/E WEDGE HAS TEMPORARY REPAIR 7 INCHES FROM O/B END. N/R NR 896, CHANGED WEDGE PER CMM 57-43-41. N/R NR 7738, T/E WEDGE DENTED 40 INCHES FROM O/B END UPPER SURFACE. CHANGED WEDGE PER CMM 57-43-41. REPAIRS ACCOMPLISHED AT SHOP VISIT. 2L72 4F RTA1NM 19950721005761995072100576NM 1995 7 21 DL76S952287 119950506A5754114T410437SP TE WEDGE BOEING767 767332 1382001NM NR 4 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 000388 T/E WEDGE DENTED TOP SURFACE. INSTALLED WEDGE PER CMM 57-43-55, FOR NR 4 L/E SLAT AT SHOP INSPECTION. 2L72 4F RTA1NM 19950721005771995072100577WP 1995 7 21 DLL10953099 119950613A5755 BEAM 1529102178 LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA HO167 193C1150 DURING INSPECTION, NR 2 RT SPOILER BEAM WAS FOUND TO HAVE A CRACK AT THE ACTUATOR FITTING. BEAM WAS REPLACED AND NEW SKINS AND HONEYCOMB BONDED PER SRM 57-52-00 (REF MFG DWG 1529102). 2L73 4F A23WE 19950721005781995072100578WP 1995 7 21 DLL10953103 119950706A53201553019102 FITTING LKHEED1011 10113851 5265010WP FS 892 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 AT LETTER CHECK ATL, FOUND SUPPORT FITTINGS ON THE GALLEY DOOR WERE CORRODED. THE FITTINGS WERE REPLACED IN ACCORDANCE WITH FAA FORM 8110-3, DATED 07-06-95 TO ACCOMODATE REPAIRS PER DL ERA 271294-14. 2L73 4F A23WE 19950721005791995072100579NE 1995 7 21 DLL10953111 219950718A7260 GEAR BOX M03407AA1031LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE DAMAGED A DALAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO11712DA A985 193C1088 10393 NR 2 ENG OIL FILTER PRESS LITE CAME ON. ON FINAL POWER, IDLE LITE WENT OUT, CAME ON AGAIN. ENGINE SHUT DOWN PER POR. FOUND METAL ON MAIN AND GEAR BOX CHIP DETECTORS, ALSO ON SCAVENGE FILTER. FOUND DAMAGED STEP-SIDE GEAR BOX DPN 727703930 S/N A985. EXTERNAL GEAR BOX DPN 727003020 S/N AM373 WAS ALSO REPLACED. 2L73 4F4 F A23WE E12EU 19950721005801995072100580WP 1995 7 21 DLL13953112 119950703A7110 NOSE COWL LKHEED1011 10113851 5265010WP FS 1705 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND NOSE COWL HAD TIME LIMITED REPAIR. REMOVED OLD ANGLE. DRILLED NEW ANGLE AND INSTALLED PER SRM 54-12-00, FIG 803. 2L73 4F A23WE 19950721005811995072100581WP 1995 7 21 DLL13953115 119950702A5311 FRAME LKHEED1011 10113851 5265010WP FS 1585 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FRAME CORRODED. C2 BB STR 32-33 FS 1585. CLEANED CORROSION, REMOVED OLD DAMAGED PART. INSTALLED NEW REPAIR PER SRM 53-12-00, FIG 817. 2L73 4F A23WE 19950721005821995072100582NM 1995 7 21 DLM88952826 119950627A5330 SKIN DOUG MD88 MD88 3023688NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11961DL 49980 LEFT AFT NOSE GEAR DOOR HAS SMALL CRACK IN DOOR HINGE CUTOUT IN FUSELAGE. FOUND DURING F-1 LETTER CHECK. REPAIRED PER SRM 53-05, FIG 62A. 2L72 4F RTA6WE 19950721005831995072100583NM 1995 7 21 DLM88952857 119950629A5320 ANGLE DOUG MD88 MD88 3023688NM WW KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11905DE 53410 KEEL BEAM AFT ANGLE (W/W AFT JAMB) CRACKED RT SIDE. FOUND DURING C-2 LTR CK TPAMM. REPAIRED PER SRM 53-05, FIG 101. 2L72 4F RTA6WE 19950721005841995072100584NM 1995 7 21 DLM88953083 119950716A2910 HYD RESERVOIR 59369865001 DOUG MD88 MD88 3023688NM LT HYD SYST FAILED A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11904DE EFS21018 53409 IN CRUISE FL 330, LEFT HYD TEMP HI TEMP HI MSG ILLUM. PRESS/ QTY NORMAL. FOLLOWED POM PROC. WHEN LEFT SYSTEM REINSTATED, ZERO HYD PRESS, QTY-19. FOLLOWED LOSS OF HYD SYS PROCEDURES, RETURNED ATL. REPLACED HYD RESERVOIR, LEFT ELEVATOR RETURN CHECK VALVE, AND ELEVATOR BYPASS VALVE, OPERATION NORMAL. 2L72 4F RTA6WE 19950721005851995072100585NM 1995 7 21 DLM88953117 119950424A71105930645509 NOSE COWL 5930645509 DOUG MD88 MD88 3023688NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11965DL 49984 49984 49984 NOSE COWL ACOUSTIC LINER DELAMINATED AT 6:OO POSITION. ALSO SKIN ERODED AROUND AIR SCOOP, REPAIRED PER SRM 54-06, DURING SHOP VISIT. 2L72 4F RTA6WE 19950721005861995072100586EU 1995 7 21 QXEA9500209 119950714A33501312 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 BOI - LEFT OVERWING EMER EXIT LIGHT INOP. BULBS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950721005871995072100587WP 1995 7 21 95ZZZX3435 119950624A29107650332511 PIPE ASSY DOUG DC8 DC851 3021920WP NR 3 HYD PUMP RUPTURED A FXLAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO19508DC 45935 MIA - AFTER TAKEOFF, THERE WAS A LOSS OF HYDRAULIC FLUID AND HYDRAULIC PRESSURE. EXECUTED EMERGENCY CHECK LIST. LANDED MIA WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC PUMP PRESSURE LINE RUPTURED. REPLACED LINE. SERVICED SYSTEM. CHECKED OK ON RUN-UP. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 19950721005881995072100588NM 1995 7 21 95ZZZX3436 119950629A3150 LOGIC CARD BOEING747 747273C 1384896NM E & E COMP NOT SECURED A SRAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO19470EV 20653 MIA - FLT 801 - ON TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON, ABORTED TAKEOFF AND RETURNED TO BASE. FOUND LOGIC CARD LOOSE IN AURAL WARNING LOGIC BOX, RE-INSERTED CARD AND PERFORMED OPS CHECK. GOOD PER BMM CHP31-50-00. 2L74 4F A20WE 19950721005891995072100589WP 1995 7 21 95ZZZX3437 119950626A3244 TIRE DOUG DC8 DC873F 302199FWP RT MLG FAILED A SRAAA UNSCHED LANDING O OTHER CLCLIMB 1 SO19873SJ 46091 RTA/NORFOLK - ON TAKEOFF, TOWER NOTIFIED TWO TIRES BLOWN, AIRCRAFT DIVERTED TO OCEANA FOR LONGER RUNWAY, AIRCRAFT LANDED SAFELY. FOUND NR 7 AND NR 4 TIRES BLOWN AND NR 8 TIRE RECAP CAME OFF, SEVERAL HYDRAULIC LINES BROKEN AND CONDUITS DAMAGED. REPLACED ALL FOUR WHEEL ASSEMBLIES, PN 26014112A, ON RT MAIN GEAR, REPLACED ALL DAMAGED HYDRAULIC LINES AND CONDUITS. ALL ITEMS OPS CHECKED GOOD. INSPECTED AREA FOR DAMAGE BY DEBRIS, NONE FOUND. 2L74 4F RT4A25 19950721005901995072100590SO 1995 7 21 95ZZZX3438 119950626A552035719125 WEIGHT PANEL LKHEED382 382G 526414USO ELEVATOR CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND RIGHT ELEVATOR TIP BALANCE WEIGHT CORRODED. REPLACED ELEVATOR TIP WEIGHT. 2H74 4T A1SO 19950721005911995072100591SO 1995 7 21 95ZZZX3439 119950626A532033563512 SILL LKHEED382 382G 526414USO FS 817 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND RAMP SILL WORN AND CORRODED. REPLACED RAMP SILL. 2H74 4T A1SO 19950721005921995072100592SO 1995 7 21 95ZZZX3440 119950626A53123561081 BULKHEAD LKHEED382 382G 526414USO FS 817 CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND UNDER-FLOOR BULKHEAD UPPER CAP CRACKED. REPLACED UNDER-FLOOR BULKHEAD UPPER CAP. 2H74 4T A1SO 19950721005931995072100593SO 1995 7 21 95ZZZX3441 119950626A53203884943 BEAM LKHEED382 382G 526414USO FUSELAGE CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND BEAM INNER CAP CORRODED. INNER CAP REPLACED. 2H74 4T A1SO 19950721005941995072100594SO 1995 7 21 95ZZZX3442 119950626A53203716032 WEIGHT PANEL LKHEED382 382G 526414USO FS 597 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND LEFT INNER CAP CORRODED. INNER CAP REPLACED. 2H74 4T A1SO 19950721005951995072100595SO 1995 7 21 95ZZZX3443 119950626A53123716032 BLKHD FITTING LKHEED382 382G 526414USO FS 597 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND BULKHEAD LT END FITTING CORRODED. REPLACED END FITTING. 2H74 4T A1SO 19950721005961995072100596SO 1995 7 21 95ZZZX3444 119950626A53203883941 BEAM LKHEED382 382G 526414USO FUSELAGE CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND BEAM OUTER CAP CRACKED. OUTER CAP REPLACED. 2H74 4T A1SO 19950721005971995072100597SO 1995 7 21 95ZZZX3445 119950701A2611 SMOKE LIGHT LKHEED382 382G 526414USO CARGO COMPT ACTIVATED A SRAAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO19912SJ 4388 FLT M405CY - DURING LANDING AT CAMBRIDGE, SMOKE DETECTOR LIGHT CAME ON AND SMOKE WAS VISIBLE IN THE CARGO DEPARTMENT. 2H74 4T A1SO 19950721005981995072100598SO 1995 7 21 95ZZZX3446 119950626A53203897311 INNER CAP LKHEED382 382G 526414USO FS 517.4 CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND LEFT BEAM INNER CAP CRACKED AND CORRODED. REPLACED INNER CAP. 2H74 4T A1SO 19950721005991995072100599SO 1995 7 21 95ZZZX3447 119950626A53203704995 WEIGHT PANEL LKHEED382 382G 526414USO FS 517/FS 597 CORRODED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND CHINE PLATE CORRODED. REPLACED CHINE PLATE. 2H74 4T A1SO 19950721006001995072100600SO 1995 7 21 95ZZZX3448 119950626A711036001515 TRUSS MOUNT LKHEED382 382G 526414USO NR 2 ENG CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19912SJ 4388 DURING C-CHECK, FOUND NR 2 ENGINE TRUSS MOUNT CRACKED AT DIAGONAL BRACE ATTACHMENT CRACKED. REPLACED TRUSS MOUNT. 2H74 4T A1SO 19950721006011995072100601WP 1995 7 21 95ZZZX3449 119950703A5320 FLOOR SUPPORT DOUG DC8 DC862 3021970WP FS 920 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 DURING C-CHECK INSPECTION, FOUND THE RT W/W AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACK AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39. 2L74 4F 4A25 19950721006021995072100602WP 1995 7 21 95ZZZX3450 119950425A573057695832 SLOT DOOR DOUG DC8 DC862 3021970WP RT LE WING CORROSION A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 ON A TYPE SERVICE 'A', FOUND RT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS' HEADS. CUT OUT DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED IAW SRM 57-2-1, FIGURE 2H. 2L74 4F 4A25 19950721006031995072100603WP 1995 7 21 95ZZZX3451 119950703A5753 ANGLE DOUG DC8 DC862 3021970WP RT TE FLAP CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 DURING B-CHECK INSPECTION, THE RT INBOARD FLAP, OUTBOARD, FORMER AND SCISSOR PANEL ATTACHMENT ANGLES FOUND CRACKED IN 2 LOCATIONS, BOTTOM AREA. REMOVED FASTENERS, STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE IAW DER ARW 12565-128. 2L74 4F 4A25 19950721006041995072100604WP 1995 7 21 95ZZZX3452 119950706A5754 SKIN DOUG DC8 DC862 3021970WP LT LE FLAP CORROSION A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 LEFT WING INBOARD SLOT L/E HAS LEVEL 2 CORROSION. REPAIRED IAW SRM 57-2-1. 2L74 4F 4A25 19950721006051995072100605WP 1995 7 21 95ZZZX3453 119950705A5520 FITTING DOUG DC8 DC862 3021970WP LT ELEVATOR CRACKED A AWRAK NONE O OTHER ININSP/MAINT 1 WP251804 45896 DURING PRE-FLIGHT, MAINTENANCE CHECK FOUND LT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0. 2L74 4F 4A25 19950721006061995072100606NM 1995 7 21 AWXA9500414 119950703A5315 FLOORBEAM BOEING757 7572S7 1384962NM FS 1661 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 FOUND DURING C-4 INSPECTION, CORROSION UPPER AND LOWER SURFACE TOP CHORD OF FLOOR BEAM, STA 1661, LBL 24.5 TO LBL 36. REPAIRED FLOORBEAM PER SRM 51-70-12. (X) 2L72 4F RTA2NM 19950721006071995072100607NM 1995 7 21 AWXA9500415 119950703A5315 FLOORBEAM BOEING757 7572S7 1384962NM FS 1661 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 PHX - FOUND DURING C-4 INSPECTION, CORROSION UPPER AND LOWER SURFACE OF TOP CHORD FLOORBEAM STA 1661, LBL 2 TO LBL 22. REPAIRED FLOORBEAM PER SRM 51-70-12. (X) 2L72 4F RTA2NM 19950721006081995072100608NM 1995 7 21 AWXA9500416 119950703A5315 FLOORBEAM BOEING757 7572S7 1384962NM FS 1640 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 PHX - FOUND DURING C-4 INSPECTION, MAIN CABIN FLOORBEAM UPPER CHORD TOP CAP CORRODED, STA 1640, BL ZERO TO RBL 40. REPAIRED BEAM PER 53-00-51. (X) 2L72 4F RTA2NM 19950721006091995072100609SW 1995 7 21 BDHA9500015 119950609A77228972053 EGT RESISTOR SWRNGNSA226 SA226TC 8780404SW RT ENGINE FAILED A BDHAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL15329BA 2006N TC238 MSP - FLT 475 - ON TAKEOFF, CREW NOTED FLUCTUATING EGT ON THE RIGHT ENGINE. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO HANGAR. MAINTENANCE REPLACED THE EGT COMPENSATING RESISTOR AND BOTH CANNON PLUGS TO THE COMP RESISTOR. OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19950721006101995072100610SW 1995 7 21 BDHA9500016 119950616A7931M401144 OIL PRESS SWITCH SWRNGNSA226 SA226TC 8780404SW LT ENGINE INOP A BDHAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL15328BA TC253 MSP - FLT 421 - CREW NOTED THE LEFT OIL PRESSURE WARNING LIGHT STAYED ILLUMINATED AFTER START-UP. MAINTENANCE REPLACED THE OIL PRESSURE WARNING SWITCH AND OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19950721006111995072100611NE 1995 7 21 GRAA9537 219950708A7530 BLEED SENSE LINE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT LOOSE A GRAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP111075T 49724 718220 ON THE 8TH OF JULY, 1995, AIRCRAFT N1075T EXPERIENCED A LOW SPEED TAKEOFF ABORT. AIRCRAFT RETURNED TO GATE AT LAUGHLIN/BULLHEAD CITY, AIRPORT. MAINTENANCE DISCOVERED A MALFUNCTIONING ENGINE COMPRESSOR BLEED AIR VALVE CONTROL SYSTEM CAUSED THE RIGHT ENGINE TO NOT FULLY DEVELOP TAKEOFF RATED POWER. UPON INVESTIGATION, MAINTENANCE DISCOVERED 3 LOOSE BLEED AIR CONTROL SENSE LINES. AFTER TIGHTENING AND RESAFETYING THESE LINES, THE RIGHT ENGINE PERFORMED WITHIN PRESCRIBED PARAMETERS. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F4 FRTA6WE E9NE 19950721006121995072100612NE 1995 7 21 GRAA9538 219950704A7200 ENGINE DOUG DC9 DC915 3022036WP PWA JT8 JT8D7B 52053NE RIGHT FAILED A GRAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP111064T 45778 653485 ON 4TH OF JULY, 1995, AIRCRAFT N1064T EXPERIENCED A TAKEOFF ABORT FROM AMARILLO AIRPORT TEXAS. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. THE ABORT WAS PERFORMED DUE TO THE RIGHT ENGINE NOT BEING ABLE TO ACHIEVE FULL RATED TAKEOFF POWER. MAINTENANCE WAS ROUTED TO THE AIRCRAFT. LINE MAINTENANCE WAS NOT ABLE TO DISCOVER WHAT CAUSED THE MALFUNCTION. THE AIRCRAFT WAS TEST RUN AND STILL COULD NOT ACHIEVE RATED TAKEOFF POWER AND EGT WAS HIGH. MAINTENANCE ROUTED AN ENGINE AND MAINTENANCE PERSONNEL TO PERFORM AN ENGINE CHANGE AND ENGINE TRIM PERFORMED. NO EFFECTS NOTED, OPERATIONAL CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F4 F A6WE E2EA 19950721006131995072100613WP 1995 7 21 ORJA9553 119950628A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 EMERGENCY LIGHTING IN CEILING BETWEEN ROWS 11-16 INOP. REMOVED AND REPLACED EMERGENCY PACK BATTERIES. OPS CHECK GOOD. (X) 2L72 4F RTA6WE 19950721006141995072100614WP 1995 7 21 ORJA9555 119950630A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11876RA 53183 FIRST SECTION OF EMERGENCY LIGHTS SEEMED EXTREMELY WEAK COMPARED TO REST OF THE SYSTEM. REPLACED POWER SUPPLY. GROUND OPS OK. (X) 2L72 4F RTA6WE 19950721006151995072100615WP 1995 7 21 ORJA9557 119950706A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 SEVERAL EMERGENCY LIGHTS IN EMPENNAGE ARE OUT. REPLACED BATTERIES IN RT AFT LAV BATTERY PACK - OPS CHKD GOOD. (X) 2L72 4F RTA6WE 19950721006161995072100616WP 1995 7 21 ORJA9558 119950707A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 OVERHEAD EMERGENCY LIGHTS IN CENTER AISLE AT AFT SERVICE DOOR INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY. (X) 2L72 4F RTA6WE 19950721006171995072100617NM 1995 7 21 PCAA9500230 119950718A2910 'T' FITTING DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYSTEM LOOSE A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA13807EX 292 NR 2 HYDRAULIC SYSTEM WENT TO 0 IN THE AIR. INSPECTED AND FOUND 'T' FITTING LOOSE AFT OF RT OUTBOARD ROLL SPOOILER ACTUATOR. SECURED FITTING. LEAK AND OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950721006181995072100618NM 1995 7 21 TAOA069509 119950629A3350900835A EEL BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS VA4969 22043 EMERGENCY EXIT SIGN AT ROW 3 INOP. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. (X) 0 4 A3WE 19950721006191995072100619NM 1995 7 21 TAOA069607 119950626A3350900835A EEL BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 5314 22043 EMERGENCY EXIT LIGHT AT FORWARD RT OVERWING EXIT INOP. REPLACED BATTERY PACK, OPERATIONAL CHECK OK. (X) 0 4 A3WE 19950721006201995072100620NM 1995 7 21 TAOA069608 119950718A3350900835A BATTERY PACK BELL BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15925TS 21244 EMERGENCY EXIT LIGHT AT ROW 3 ABC INOP. REPLACED BATTERY PACK CHECKS OK. (M) 2L73 4F A3WE 19950721006211995072100621NM 1995 7 21 TAOA079501 119950702A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15919TS 3790 20447 FORWARD LEFT OVERWING EXIT LIGHT WILL NOT TEST. PRELACED BATTERY PACK, OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19950728000011995072800001EA 1995 7 28 95ZZZX3454 119950623A3250711709 LEVER ASSY HEROUX 71300 DHAV DHC6 DHC6300 EA NLG STEERING BROKEN A ASWAO OTHER O OTHER TXTAXI/GRND HDL 1 WP07147SA H693 537 CREW REPORTED NOSEWHEEL STEERING 'POPPED' AFTER TURNING OFF RUNWAY. NOSEWHEEL STEERING WAS LOST. MAINTENANCE CREWS FOUND STEERING LEVER ASSEMBLY BROKEN IN HALF AT FORKED END. 1H72 3T A9EA 19950728000021995072800002 1995 7 28 95ZZZX3455 419950709A34213641 POWER SUPPLY BOEING737 737275 1384485NM COCKPIT FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP282FOR 2157 20958 PHX\MCI - FLT 592 - ONE HOUR OUT OF PHX, THE STANDBY HORIZON FLAGGED AND THE CIRCUIT BREAKER TRIPPED. DUE TO MEL RESTRICTIONS, AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE POWER SUPPLY FAILED. REPLACED POWER SUPPLY AND INDICATOR. AIRCRAFT RETURNED TO SERVICE. REF CONTROL NR AWXA9500421. (X) 2L72 4F A16WE 19950728000031995072800003NE 1995 7 28 95ZZZX3456 219950630A73145009986C FUEL PUMP EMB 120 EMB120RT SO PWA 118 PW118 NE NR 1 ENGINE MALFUNCTIONING A AC2XAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SW09227279313 2790 120177 LRD - FLT 2579 - PILOT REPORTED THAT UPON APPROACH TO LRD, THE NR 1 ENGINE EXPERIENCED A FLAME-OUT. THE AIRCRAFT LANDED AT LRD WITHOUT FURTHER INCIDENT. UPON INSPECTION, THE NR 1 ENGINE DRIVEN FUEL PUMP WAS FOUND TO HAVE A LOOSE DRIVE SHAFT. MAINTENANCE REMOVED AND REPLACED THE FUEL PUMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T4 TRTA31SO E20NE 19950728000041995072800004WP 1995 7 28 95ZZZX3457 119950703A5320 FLOOR SUPPORT DOUG DC8 DC862 3021970WP FS 920 CRACKED ASAARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 DURING B-CHECK INSPECTION, FOUND RIGHT WW AT STA FS 920 AT VERTICAL FLOOR SUPPORT LIGHTING HOLE HAS A CRACK. REMOVED FASTENERS, CUT OUT CRACKED AREA, FABRICATED AND INSTALLED DOUBLER IAW DER ARW 31298-39. 2L74 4F 4A25 19950728000051995072800005NM 1995 7 28 AWXA9500393 119950621A3244 TIRE BOEING737 7372U9 1384498NM NLG FAILED A AWXAO OTHER O OTHER TOTAKEOFF 1 WP28149AW 22575 COS\PHX - FLT 1241 - ON TAKEOFF, A NOSE GEAR BLEW TIRE. AIRCRAFT CONTINUED TO PHX AND LANDED WITHOUT FURTHER PROBLEMS. EMERGENCY TRUCKS WERE CALLED OUT. AIRCRAFT TAXIED TO GATE AFTER LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 2 NOSE WHEEL ASSEMBLIES, PN 26010452, IAW AMW 363. AIRCRAFT INSPECTED AND RETURNED TO SERVICE. (X) 2L72 4F RTA16WE 19950728000061995072800006NM 1995 7 28 AWXA9500401 119950626A275110619264 FLAPS POS IND BOEING737 7373G7 1384595NM TE FLAPS FAILED A AWXAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 WP28307AW 1893 24634 ORD\MDW - FLT 696 - TRAILING EDGE FLAPS WOULD NOT EXTEND FURTHER THAN 17 UNITS DURING DESCENT. AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. CONTRACT MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR PER MM 27 58 41, PGS 401/403. SYSTEM OPS TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA16WE 19950728000071995072800007NM 1995 7 28 AWXA9500418 119950708A2910271N61192 HYD LINE BOEING757 7572S7 1384962NM LT MLG LEAKING A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP28902AW 23322 PHX\JFK - FLT 290 - AIR TURNBACK, DURING CLIMB-OUT, CREW REPORTED EICAS 'L HYD QTY' MESSAGE. CREW VERIFIED QTY WAS DROPPING QUICKLY WITH DECREASING PRESSURE. DURING RETURN TO PHX, CREW REPORTED EICAS 'POWER XFER UNIT' MESSAGE. CREW DECLARED EMERGENCY, LANDING WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED FROM RUNWAY TO GATE. MAINTENANCE REPLACED HIGH PRESSURE DOWNLOCK ACTUATOR LINE AT LT MLG. LEAK CHECK COMPLIED WITH. AIRCRAFT RELEASED FOR SERVICE. (X) 2L72 4F RTA2NM 19950728000081995072800008EU 1995 7 28 AWXA9500420 119950707A2150757A000008 ACM AIRBUS320 A320231 3930325EU NR 2 PACK SEIZED A AWXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 WP28622AW 00403 054 PHX\CMH - FLT 266 - DURING CLIMB OUT, NR 2 PACK FAILED. PILOT STATED THAT PRIOR TO PACK FAIL A STRONG BURNING PLASTIC ODOR WAS NOTICED, BUT DISAPPEARED AFTER PACK SHUT DOWN. PILOT ELECTED TO RETURN TO PHX DUE TO ALTITUTDE RESTRICTION, LANDING WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING WAS ACCOMPLISHED PER AMM 5 51 11, PAGE 601. NO ACTION REQUIRED. MAINTENANCE FOUND ACM TO BE SEIZED. REMOVED AND REPLACED ACM PER AMM 21 52 21. OPS CHECK AND LEAK CHECK, COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950728000091995072800009 1995 7 28 AWXA9500421 419950709A34217057V4 STANDBY HORIZON BOEING737 737275 1384485NM COCKPIT MALFUNCTIONED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP282FOR 20176 20958 PHX\MCI - FLT 592 - ONE HOUR OUT OF PHX, THE STANDBY HORIZON FLAGGED AND THE CIRCUIT BREAKER TRIPPED. DUE TO MEL RESTRICTIONS, AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE POWER SUPPLY FAILED. REPLACED POWER SUPPLY AND INDICATOR. AIRCRAFT RETURNED TO SERVICE. REF CONTROL NR 95ZZZX3455. (X) 2L72 4F A16WE 19950728000101995072800010NM 1995 7 28 AWXA9500422 119950630A3350 EEL CONNECTOR BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 17 THROUGH 21. REPAIRED LOOSE CONNECTION, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000111995072800011NM 1995 7 28 AWXA9500423 119950703A3350 EEL ASSEMBLY BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE ROWS 11 THROUGH 15. RECONNECTED LIGHT ASSEMBLY, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000121995072800012NM 1995 7 28 AWXA9500424 119950705A3350 EEL CONNECTORS BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED SEVERAL LOOSE CONNECTIONS. OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000131995072800013NM 1995 7 28 AWXA9500425 119950706A33500L3071BPEGPL EEL LAMP BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHK, FOUND AFT, 4 EACH, FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BROKEN WIRE AND RELAMPED 2 ASSEMBLIES, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000141995072800014NM 1995 7 28 AWXA9500426 119950706A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28165AW 23626 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 13 ON. REPAIRED BROKEN WIRE AT ROW 13, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000151995072800015NM 1995 7 28 AWXA9500427 119950707A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 14. RECONNECTED LOOSE WIRE, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000161995072800016NM 1995 7 28 AWXA9500428 119950708A3350 EEL ASSY BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28903AW 23323 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND A SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE STARTING AT ROW 27. REPAIRED SECTION OF LIGHTS AT ROW 27, OPS CHECK GOOD. (X) 2L72 4F RTA2NM 19950728000171995072800017NM 1995 7 28 AWXA9500429 119950709A3350900835A EEL BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28180AW 22647 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR AND R1 DOOR SLIDE EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000181995072800018NM 1995 7 28 AWXA9500430 119950710A3350 EEL WIRE BOEING737 737277 1384570NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28180AW 22647 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 14 LT AND ROW 17. REPAIRED BROKEN WIRES AT ROW 14 AND ROW 17, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19950728000191995072800019NM 1995 7 28 AWXA9500431 119950706A5315 FLOORBEAM BOEING757 757225 1384959NM BS 345 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 PHX - DURING SCHEDULED C1 INSPECTION, FOUND FLOORBEAM CORRODED BEYOND CLEAN-UP LIMITS AT STA 345 BL ZERO. INSTALLED REPAIR PER ER 5 53 16 09. (X) 2L72 4F RTA2NM 19950728000201995072800020NM 1995 7 28 AWXA9500432 119950706A5320 ANGLE BOEING757 757225 1384959NM FS 1320-1420 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 PHX - DURING SCHEDULED C1 INSPECTION, FOUND BAG PIT FLOORBOARD SUPPORT STRUCTURE CORRODED FROM STA 1320 TO STA 1420 BETWEEN STR 28 AND STR 29. FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 51 70 11 AND SRM 51 40 02. (X) 2L72 4F RTA2NM 19950728000211995072800021NM 1995 7 28 AWXA9500433 119950706A5315 FLOORBEAM BOEING757 757225 1384959NM BS 377.7 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 PHX - DURING SCHEDULED C1 INSPECTION, FOUND FLOOR BEAM CORRODED AT BS 377.7, LBL 18. INSTALLED REPLACEMENT T-CAP IAW SRM 53 00 51, FIG 203 AND SRM 51 40 00. (X) 2L72 4F RTA2NM 19950728000221995072800022NM 1995 7 28 AWXA9500434 119950706A5315 FLOORBEAM BOEING757 757225 1384959NM BS 377.7 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 PHX - DURING SCHEDULED C1 INSPECTION, FOUND CORROSION ON AFT CORNER OF L1 DOOR THAT EXTENDED UNDER DOORWAY DRAIN PAN AT BS 377.7. REMOVED AND REPLACED T-CAP PER SRM 51 40 00. (X) 2L72 4F RTA2NM 19950728000231995072800023NM 1995 7 28 AWXA9500435 119950706A5347 SEAT TRACK BOEING757 757225 1384959NM BS 365.25 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28907AW 22691 PHX - DURING SCHEDULED C1 INSPECTION, FOUND SEAT TRACK AT RBL 26 BETWEEN STA 365.25 AND STA 418 DAMAGED. REMOVED AND REPLACED SEAT TRACK ASSEMBLY PER SRM 51 40 02. (X) 2L72 4F RTA2NM 19950728000241995072800024NM 1995 7 28 95UAL900045 119950721A3150849704 PSEU BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FLIGHT DECK MALFUNCTIONED A UALAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP29641UA 25091 AIRCRAFT RETURNED TO BLOCKS WITH EICAS AMBER ADVISORY MESSAGE FOR RIGHT OVERWING SLIDE. REPLACED PSEU DUE TO ANNUNCIATOR PANEL LIGHT NOT ACCOMPANYING EICAS ADVISORY MESSAGE. SUSPECT FAULTY DRIVER CARD. 2L72 4F4 FRTA1NM E24NE 19950728000251995072800025NM 1995 7 28 95UAL900046 119950721A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297259U 21406 EMERGENCY SLIDE LIGHTS AT DOORS 1L AND 1R INOP. REPLACED BATTERY PACK FOR THE TWO FWD SLIDE LIGHTS. 2L73 4F4 F A3WE E2EA 19950728000261995072800026NE 1995 7 28 95UAL900047 219950721A7261 OIL QTY BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE DROPPED A UALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29154UA 20103 662764 AFTER REACHING CRUISE ALT NR 4 ENG OIL QTY DROPPED TO JUST ABOVE 1 GAL ON IND, ALL OTHER IND OK. OIL QTY SLOWLY DECREASED TO ZERO AT 5 AND ONE HALF HOURS INTO FLT, THEN PRESS FLUCT. AT 8 HRS, LOW OIL PRESS LIGHT ON, ENGINE SHUTDOWN. 2L74 4F4 F A20WE E20EA 19950728000271995072800027NM 1995 7 28 95UAL900048 119950721A2500 EEL CABLE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299004U 19042 THREE SECTIONS OF EEL LIGHTING INOP MIDDLE OF ACFT. REPLACED EEL LIGHT POWER CABLE, CHECKS NORMAL. 2L72 4F4 F A16WE E2EA 19950728000281995072800028NE 1995 7 28 95UAL900049 219950721A7250774994 TURBINE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 WP297280U 21558 696515 NR 1 ENGINE FAILED ON TAKEOFF AT 90 KTS, LOUD BANG, LOST POWER AND ENGINE RUMBLE AT IDLE. FOUND TURBINE DISINTEGRATED. A CRACKED FUEL NOZZLE AT THE HEAT SHIELD WELD SEAM MELTED THE NOZZLE GUIDE VANES, WHICH WERE THEN LIBERATED AND CAUSED T2 BLADE LIBERATION. 2L73 4F4 F A3WE E2EA 19950728000291995072800029NM 1995 7 28 95UAL900050 119950721A3350 EEL BATTERY PACK BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299030U 19068 RT EXT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY. 2L72 4F4 F A16WE E2EA 19950728000301995072800030NM 1995 7 28 95UAL900053 119950721A5210 RESERVOIR BOEING757 757222 1384956NM PWA 2037 PW2037 NE PAX DOOR DISCHARGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29559UA 26657 PRIOR TO DEPT, LT FWD ENTRY DOOR EMER PWR RESERVOIR PRESSURE THERMALLY DISCHARGED. INSTALLED NEW DISCHARGE KIT AND SERVICED RESERVOIR. 2L72 4F4 FRTA2NM E17NE 19950728000311995072800031WP 1995 7 28 ABXA9500579 119950718A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23984AX 10766 47258 DURING MAINTENANCE CHECK, FOUND COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT BATTERIES IAW DC-9 SUPP MM 33-53-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950728000321995072800032WP 1995 7 28 ABXA9500580 119950717A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC931 3022065WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23907AX 2582 47203 DURING PREDEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTS VERY DIM. REPLACED BATTERIES IAW DC-9 SUPP MM 33-53-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950728000331995072800033NM 1995 7 28 P5CA9500472 119950720A3310 LIGHTS BOEING747 747121 1384871NM FLIGHT DECK SMOKING A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP23831FT 19648 ACRID TYPE SMELL NOTED INITIALLY DURING CLIMB THRU FL 280, 3 MINUTES LATER OBSERVED FAINT SMOKE FROM LEFT GLARESHIELD. TURNED OFF ALL INTSTRUMENT BACK GROUND LIGHTS SMOKE AND ODOR STOPPED, TURNED LIGHTS ON 1 AT A TIME SMOKE AND ODOR DID NOT RETURN. MAINTENANCE AT ORD INSPECTED BEHIND GLARESHIELD, UNABLE TO LOCATE ANY UNITS OVERHEATED. 2L74 4F A20WE 19950728000341995072800034NM 1995 7 28 P5CA9500473 119950630A573065B02077201 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TOP OF LEFT WING DELAMINATED PANEL. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950728000351995072800035NM 1995 7 28 P5CA9500474 119950630A573065B020458 PANEL BOEING747 747121 1384871NM RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATED WING PANEL RIGHT WING. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950728000361995072800036NM 1995 7 28 P5CA9500475 119950630A573065B020922 PANEL BOEING747 747121 1384871NM RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION AND TRAILING EDGE MISSING ON RIGHT WING. 2L74 4F A20WE 19950728000371995072800037NM 1995 7 28 P5CA9500476 119950630A573065B01998201 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION ON LEFT WING OUTBOARD PANEL. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950728000381995072800038NM 1995 7 28 P5CA9500477 119950630A573065B020775 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION ON WING PANEL LEFT WING. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950728000391995072800039NM 1995 7 28 P5CA9500478 119950630A573065B020071 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION AND TRAILING EDGE MISSING LEFT WING. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950728000401995072800040NM 1995 7 28 P5CA9500479 119950630A5320 CLIP BOEING747 747121 1384871NM BS 208 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN TIE CLIP STRINGER S6R BS 2080. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000411995072800041NM 1995 7 28 P5CA9500480 119950630A5320 CLIP BOEING747 747121 1384871NM BS 204 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON TIE CLIP S4R BS 2040. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000421995072800042NM 1995 7 28 P5CA9500481 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1560 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S4R BS 1560. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000431995072800043NM 1995 7 28 P5CA9500482 119950630A5320 CLIP BOEING747 747121 1384871NM BS 1620 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN TIE CLIP AT S6L BS 1620. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000441995072800044NM 1995 7 28 P5CA9500483 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 2040 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN S7L AT BS 2040. REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000451995072800045NM 1995 7 28 P5CA9500484 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 520 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S40R BS 520. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000461995072800046NM 1995 7 28 P5CA9500485 119950630A5320 CLIP BOEING747 747121 1384871NM BS 540 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN CLIP S39R BS 540. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000471995072800047NM 1995 7 28 P5CA9500486 119950630A5330 SKIN BOEING747 747121 1384871NM BS 780-800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 780 AND 800 AT S39R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000481995072800048NM 1995 7 28 P5CA9500487 119950630A5330 SKIN BOEING747 747121 1384871NM BS 820-940 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 820 AND 840 AT S39R. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000491995072800049NM 1995 7 28 P5CA9500488 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 840-860 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION S39R BETWEEN BS 840 AND 860. REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000501995072800050NM 1995 7 28 P5CA9500489 119950630A5320 MOUNT BRIDGE BOEING747 747121 1384871NM BS 2716.6 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK PAST STOP DRILL JUST AHEAD OF AFT APU MOUNT BRIDGE CONNECTION RIGHT AND LEFT SIDE AT BS 2716.6. REPAIRED PER BOEING SRM 51-20-01 AND 51-30-02. 2L74 4F A20WE 19950728000511995072800051NM 1995 7 28 P5CA9500490 119950630A5414 SKIN BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON LOWER EDGE NR 2 PYLON RIGHT SIDE DOOR FAIRING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950728000521995072800052NM 1995 7 28 P5CA9500491 119950630A5330 SKIN BOEING747 747121 1384871NM BS 880-900 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 900 AND 880 S39R. REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000531995072800053NM 1995 7 28 P5CA9500492 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 880-900 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S38R BS 880 TO 900. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000541995072800054NM 1995 7 28 P5CA9500493 119950630A5330 SKIN BOEING747 747121 1384871NM BS 940-980 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 940 AND 980 AT S39R. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000551995072800055NM 1995 7 28 P5CA9500494 119950630A5330 SKIN BOEING747 747121 1384871NM BS 540-560 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 540 AND 560 S39L. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 51-10-02. 2L74 4F A20WE 19950728000561995072800056NM 1995 7 28 P5CA9500495 119950630A5330 SKIN BOEING747 747121 1384871NM BS 760-780 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 760 AND 780 S39L. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000571995072800057NM 1995 7 28 P5CA9500496 119950630A5330 SKIN BOEING747 747121 1384871NM BS 780-800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 780 AND 800 S39L. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000581995072800058NM 1995 7 28 P5CA9500497 119950630A5313 STRINGERS BOEING747 747121 1384871NM BS 820-840 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN STRINGERS S39L AND S40L BETWEEN BS 820 AND 840. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000591995072800059NM 1995 7 28 P5CA9500498 119950630A5330 SKIN BOEING747 747121 1384871NM BS 840-860 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 840 AND 860. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000601995072800060NM 1995 7 28 P5CA9500499 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S40L BS 1000. REPAIRED STRINGER PER BOEING SRM 53-10-03 AND 51-30-02. 2L74 4F A20WE 19950728000611995072800061NM 1995 7 28 P5CA9500500 119950630A5330 SKIN BOEING747 747121 1384871NM BS 500-520 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN SKIN BETWEEN BS 500 AND 520 S39L. CORROSION REMOVED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728000621995072800062NM 1995 7 28 P5CA9500501 119950630A5720 FAIRING BOEING747 747121 1384871NM WS 680 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LOWER FAIRING BROKEN AT WS 680 RIGHT WING REAR SPAR. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000631995072800063NM 1995 7 28 P5CA9500502 119950630A5712 RIB BOEING747 747121 1384871NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS FOUND AT RIGHT WING LEADING EDGE CAVITY FS 800 AND 762 ON RIB UPPER CHORD. REPAIRED PER BOEING SB 57-2116 FIG 6. 2L74 4F A20WE 19950728000641995072800064NM 1995 7 28 P5CA9500503 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1500-1580 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SKIN FROM BS 1500 TO 1580 BETWEEN S18R AND S20R. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000651995072800065NM 1995 7 28 P5CA9500504 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S6L JOINT TO FRAME BS 1000. CORROSION REMOVED PER BOEING SRM 51-10-01, NEW FASTENERS INSTALLED PER 51-30-02. 2L74 4F A20WE 19950728000661995072800066NM 1995 7 28 P5CA9500505 119950630A5320 TEAR STRAP BOEING747 747121 1384871NM BS 1160 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN TEAR STRAP BETWEEN S6R AND S7R AT BS 1160. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000671995072800067NM 1995 7 28 P5CA9500506 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1220 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S4L AT BS 1220 UNDER TIE CLIP. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000681995072800068NM 1995 7 28 P5CA9500507 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S4L AT BS 1200 UNDER TIE CLIP. REMOVED THE CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000691995072800069NM 1995 7 28 P5CA9500508 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1080 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S5L AND TEAR STRAP AT BS 1080. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000701995072800070NM 1995 7 28 P5CA9500509 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1060 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S5L BS 1060. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000711995072800071NM 1995 7 28 P5CA9500510 119950630A5400 BRACKET BOEING747 747121 1384871NM NR 3 PYLON ELONGATED HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON PNEUMATIC DUCT ATTACH BRACKET ON NR 3 NACELLE FIRE WALL NS 195 LEFT SIDE. ALSO, ELONGATED BOLT HOLE AND BADLY CHAFED. REPAIRED PER BOEING SRM 54-10-02. REPLACED FOR ELONGATED HOLE, NOT A LEVEL 2. 2L74 4F A20WE 19950728000721995072800072 1995 7 28 P5CA9500511 419950630A2310 HF TUNER BASE BOEING747 747121 1384871NM RIGHT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HF TUNER BASE CRACKED RIGHT WING TIP. REPLACED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950728000731995072800073NM 1995 7 28 P5CA9500512 119950630A5720 FAIRING BOEING747 747121 1384871NM WS 1240 HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HOLE IN FAIRING FIBER GLASS RIGHT WING LOWER SURFACE WS 1240. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000741995072800074NM 1995 7 28 P5CA9500513 119950630A5730 SKIN BOEING747 747121 1384871NM RT WING TIP SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SKIN IS SEPARTATED ON RIGHT WING TIP LOWER SURFACE NEAR BASE OF HF ANTENNA. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000751995072800075NM 1995 7 28 P5CA9500514 119950630A5330 SKIN BOEING747 747121 1384871NM BS 1480-1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON SKIN BETWEEN BS 1480 AND 1920, S39L AND S39R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-1. 2L74 4F A20WE 19950728000761995072800076NM 1995 7 28 P5CA9500515 119950630A5730 SKIN BOEING747 747121 1384871NM LT WING SWELLING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING OF WING PANEL UPPER WING AT INBOARD HINGE NR 5 SPOILER. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000771995072800077NM 1995 7 28 P5CA9500516 119950630A5730 SKIN BOEING747 747121 1384871NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON LOWER SKIN AT BOOST PUMP ACCESS, LEFT WING. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-30-01. 2L74 4F A20WE 19950728000781995072800078NM 1995 7 28 P5CA9500517 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 460 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN FLOORBEAM CAP BS 460 RBL 85. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950728000791995072800079NM 1995 7 28 P5CA9500518 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 500 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN LOWER CAP FLOORBEAM BETWEEN RBL 11 AND LBL 11 BS 500. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950728000801995072800080NM 1995 7 28 P5CA9500519 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 140 GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 GOUGE ON WEB FLOORBEAM BS 140 RBL 15. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950728000811995072800081NM 1995 7 28 P5CA9500520 119950630A5315 FLOORBEAM BOEING747 747121 1384871NM BS 500 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AND SHEARED RIVET IN LOWER CABIN FLOORBEAM BS 500 RBL 45. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000821995072800082NM 1995 7 28 P5CA9500521 119950630A5411 FRAME BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS ON BOTH SIDES OF LEFT SIDE OF AFT ENGINE MOUNT FRAME NS 222 ON NR 2 NACELLE. REPLACED DOUBLERS PER BOEING SRM 54-30-03 FIG 36. 2L74 4F A20WE 19950728000831995072800083NM 1995 7 28 P5CA9500522 119950630A5522 TE SKIN BOEING747 747121 1384871NM RT ELEVATOR DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SMALL DELAMINATIONS ON RIGHT INBOARD ELEVATOR AT TRAILING EDGES INBOARD AND OUTBOARD EDGES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000841995072800084NM 1995 7 28 P5CA9500523 119950630A540063B10047544 BRACKET BOEING747 747121 1384871NM NR 1 PYLON DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE FWD SKIRT MOUTNING BRACKET NR 1 PYLON. INSTALLED NEW FITTING PER 51-30-02. 2L74 4F A20WE 19950728000851995072800085NM 1995 7 28 P5CA9500524 119950630A540069B1230009 BRACKET BOEING747 747121 1384871NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED FORWARD SKIRT MOUTNING BRACKET NR 4 PYLON. REPLACED FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950728000861995072800086NM 1995 7 28 P5CA9500525 119950630A5720 BRACKET BOEING747 747121 1384871NM WS 1110 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED RIGHT WING TRAILING EDGE FAIRING ANCHOR NUT BRACKET AT WS 1110. REPAIRED PER BOEING SRM 51-30-02 NEW ANGLES. 2L74 4F A20WE 19950728000871995072800087NM 1995 7 28 P5CA9500526 119950630A5320 BRACKET BOEING747 747121 1384871NM BS 1475 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN BRACKET S28R BS 1475. REPAIRED PER BOEING SRM 51-40-03 FIG 4. 2L74 4F A20WE 19950728000881995072800088NM 1995 7 28 P5CA9500527 119950630A5313 STRINGER BOEING747 747121 1384871NM BS 1420 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON S9L BS 1420. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000891995072800089NM 1995 7 28 P5CA9500528 119950630A5320 PRESSURE PAN BOEING747 747121 1384871NM FUSELAGE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION ON APU PRESSURE PAN. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950728000901995072800090NM 1995 7 28 P5CA9500529 119950630A5720 FITTING BOEING747 747121 1384871NM LT WING BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN MOUNT FITTING ON UPPER RIGHT WING PANEL AT LEFT WING NR 4 TRACK FWD MOUNT. MANUFACTURED NEW PANEL PER BOEING SRM 57-10-02, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950728000911995072800091NM 1995 7 28 P5CA9500530 119950704A5754 BRACKET BOEING747 747121 1384871NM NR 14 LE FLAP CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON U-CHANNEL FAIRING ON HINGE BRACKET, INBOARD HINGE OF NR 14 LEADING EDGE FLAP. MANUFACTURED BRACKET PER BOEING SRM 51-20-01, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950728000921995072800092NM 1995 7 28 P5CA9500531 119950704A5320 PRESSURE DECK BOEING747 747121 1384871NM BS 1280-1400 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON PRESSURE DECK WEBS RBL 11 BETWEEN BS 1280 AND 1400 RBL 33 BS 1300 TO 1400. MANUFACTURED AND INSTALLED REINFORCEMENT PER BOEING SRM 53-10-07 FIG 2 DETAIL 2. 2L74 4F A20WE 19950728000931995072800093NM 1995 7 28 P5CA9500532 119950704A5311 FRAME BOEING747 747121 1384871NM BS 1060 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AT BS 1060 FRAME UNDER RIGHT FAIRING. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950728000941995072800094NM 1995 7 28 P5CA9500533 119950704A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 500-520 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS ON INTERCOSTAL AT S30R BETWEEN BS 500 AND 520. MANUFACTURED NEW INTERCOSTAL PER BOEING SRM 53-10-21, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950728000951995072800095NM 1995 7 28 P5CA9500534 119950704A5712 RIB BOEING747 747121 1384871NM WS 850 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON LEFT WING LEADING CAVITY WS 850 FORGED RIB AT THE AFT UPPER LEFT SIDE CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950728000961995072800096NM 1995 7 28 P5CA9500535 119950704A5712 RIB BOEING747 747121 1384871NM WS 960 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED FORGE RIB LEFT WING LEADING EDGE CAVITY WS 960 AFT RIGHT SIDE UPPER CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950728000971995072800097NM 1995 7 28 P5CA9500536 119950704A5712 RIB BOEING747 747121 1384871NM WS 930 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED UPPER LEFT CHORD ON FORGE RIB AT WS 930 LEFT WING LEADING EDGE CAVITY. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950728000981995072800098NM 1995 7 28 P5CA9500537 119950704A5712 RIB BOEING747 747121 1384871NM WS 800 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED FORGED RIB LEFT WING LEADING EDGE CAVITY WS 800. (2 CRACKS ON AFT UPPER LEFT SIDE CHORD). MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03 INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950728000991995072800099NM 1995 7 28 P5CA9500538 119950704A5230 SKIN BOEING747 747121 1384871NM NR 4L DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN SKIN AT NR 4L DOOR LOWER HINGE CUTOUT. REPAIRED BY BLEND OUT, WITHIN LIMITS PER BOEING SRM 52-00-02. 2L74 4F A20WE 19950728001001995072800100NM 1995 7 28 P5CA9500539 119950704A5330 SKIN BOEING747 747121 1384871NM BS 1820-1840 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING ON EXTERNAL SKIN BETWEEN BS 1820 AND 1840 AT S47R. REMOVED FASTENERS FROM SWELLED AREA, REMOVED CORROSION FROM SKIN PER SRM 51-10-01, WITHIN LIMITS PER 53-10-01, INSTALLED FASTENER PER SRM 53-10-01. 2L74 4F A20WE 19950728001011995072800101NM 1995 7 28 P5CA9500540 119950704A5330 SKIN BOEING747 747121 1384871NM BS 1800-1820 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING ON EXTERNAL SKIN BETWEEN BS 1800 AND 1820 AT S50L. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950728001021995072800102NM 1995 7 28 SCNA95152 119950718A3350900835A EEL BATTERY PACK BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 FOUND THE EMERGENCY EXIT LIGHTING ABOVE R-2 DOOR BLINKING REMOVED AND REPLACED R-2 DOOR BATTERY PACK IAW MM 33-50-71, SYSTEM TESTED GOOD. 2L73 4F RTA3WE 19950728001031995072800103NM 1995 7 28 UPS203887 119950717A532065C191217 FITTING BOEING727 72730C 1384009NM FS 941 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN C-CHECK, MAINTENANCE FOUND LINE OF CORROSION BETWEEN FASTENERS STATION 941, RBL 58 TO 59, WL 207 TOP FLANGE OF FRAME FITTING, POSSIBLE CRACK. REPAIRED PER EWO 95-2805 AND UPS EO B727-5310-7200-A. 2L73 4F A3WE 19950728001041995072800104NM 1995 7 28 UPS203888 119950717A321165844055 FITTING BOEING727 72730C 1384009NM LT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF LT MLG FWD TRUNNION BEARING SUPPORT. INSTALLED NEW TRUNNION SUPPORT FITTING IAW MM 32-11-01, MM 32-11-01, MM 32-32-11. 2L73 4F A3WE 19950728001051995072800105NM 1995 7 28 UPS203889 119950717A321165956001664 FITTING BOEING727 72730C 1384009NM RT MLG CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN C-CHECK, MAINTENANCE FOUND CRACK INDICATION DURING INSPECTION OF RT MLG FWD TRUNNION BEARING SUPPORT FITTING. INSTALLED NEW TRUNNION SUPPORT FITTING IAW OHM 32-10-13, MM 32-11-51, MM 32-11-01. 2L73 4F A3WE 19950728001061995072800106NM 1995 7 28 UPS203890 119950717A5755 SKIN BOEING727 72730C 1384009NM NR 13 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01906UP 19314 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 13 SPOILER DELAMINATED ON THE UPPER SURFACE LEADING EDGE AT CENTER HINGE FITTING. REPAIRED WITH FIBERGLASS AND RESIN IAW SRM 57-50-6. 2L73 4F A3WE 19950728001071995072800107NM 1995 7 28 UPS403886 119950720A5311 FRAME BOEING747 747SR46 NM BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION ON OUTER CHORD OF FAIRING FRAME AT BS 960, LBL 07. REPAIRED THE OUTER CHORD OF THE FAIRING FRAME IAW SRM 53-40-04. 2L74 4F A20WE 19950728001081995072800108NM 1995 7 28 UPS403893 119950718A3350 EEL BATTERY PACK BOEING747 747123F NM CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE ON GROUND,MAINTENANCE FOUND EMERGENCY CEILING LIGHT ABOVE CREW LADDER ACCESS INOP. REPLACED BATTERY PACK. 2L74 4F A20WE 19950728001091995072800109WP 1995 7 28 UPS403894 119950718A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01805UP 46117 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. 2L74 4F RT4A25 19950728001101995072800110WP 1995 7 28 UPS403895 119950718A3350 EEL SOCKET DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01803UP 46073 UPON ARRIVAL, CREW REPORTS EMERGENCY LIGHT SOCKET SPRING CONTACT STUCK IN DEPRESSED POSITION. REPAIRED SPRING CONTACT. 2L74 4F RT4A25 19950728001111995072800111NM 1995 7 28 UPS403896 119950718A3350S1356B37 LIGHT BOEING747 747123F NM CABIN FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01677UP 20391 WHILE ON GROUND, MAINTENANCE FOUND CEILING EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY. 2L74 4F A20WE 19950728001121995072800112NM 1995 7 28 UPS403897 119950719A3233 ACTUATOR BOEING747 747123F NM LT MLG INOPERATIVE A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01681UP 19661 CREW REPORTED, LEFT WING DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. LIGHT REMAINED ILLUMINATED AFTER ALTERNATE EXTENSION IAW ABNORMAL CHECKLIST, ATB TO SDF. REPLACED LT WING GEAR ACTUATOR IAW M/M 32-32-01, OPS CHECK GOOD. 2L74 4F A20WE 19950728001131995072800113NM 1995 7 28 UPS403898 119950720A5753 SKIN BOEING727 727185C 138406NNM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE ON GROUND MAINTENANCE FOUND DELAMINATION OF LT I/B T/E FLAP. REPAIRED IAW EO B727-5750-3081. 2L73 4F A3WE 19950728001141995072800114 1995 7 28 9511129952 419950723A34162050011RC ALT INDICATOR DOUG DC9 DC931 3022065WP FLIGHT DECK FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01916RW304425083 47144 DURING CLIMB AT APPROXIMATELY 6,000 FEET, THE NR 1 ALTIMETER AND ALTITUDE ALTERTED OFF FLAGS DISPLAYED. ATTEMPTED RESET OF ALTIMETER, FLAGS RETRACTED THEN RETURNED. FLIGHT RETURNED TO ORIGIN WITHOUT INCIDENT. REPLACED THE NR 1 ALTIMETER INDICATOR, SYSTEM CHECKED OK. 2L72 4F A6WE 19950728001151995072800115NE 1995 7 28 9511132717 219950721A7230 COMPRESSOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01721RC 22492 707907 COMPRESSOR STALLS OCURRED IN THE NR 2 ENGINE ON TAKEOFF, THE TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. THE CREW NOTED A DIRECT CROSSWIND FROM THE LEFT SIDE AT 18 KNOTS. MAINTENANCE REPLACED THE PRBC. NO STALLS NOTED ON SUBSEQUENT RUNUP. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950728001161995072800116 1995 7 28 9511149998 419950723A344220671570153 RADAR TR UNIT DOUG DC9 DC931 3022065WP FLIGHT DECT MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018934E264635 47143 WHILE ENROUTE DTW-DFW, RADAR FAILED TO PAINT KNOWN WEATHER. RADAR TEST OK. RADAR WAS OCCASIONALLY SPOKING AND DOES NOT PAINT GROUND RETURN. DIVERTED TO MEM FOR MAINTENANCE, DUE TO THUNDERSTORMS ENROUTE TO DFW. REPLACED THE RADAR TRANSCEIVER. PERFORMED SYSTEM TEST, CHECKED OK. ALSO, INSPECTED ANTENNA, CHECKED OK. 2L72 4F A6WE 19950728001171995072800117WP 1995 7 28 9511151160 119950723A2120 AIR DISTR DOUG DC10 DC1040 3023508WP CABIN FUMES A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL01160US 46769 DURING TAXI AND ENGINE START, SMOKE AND FUMES WERE DETECTED IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE. VISUALLY CHECKED THE NR 1 AND NR 3 OIL QUANTITIES. PERFORMED ENGINE RUN AND CHECKED AIR CONDITIONING PACK OPERATION. CHECKED OK, AIRCRAFT APPROVED FOR SERVICE. 2L73 4F A22WE 19950728001181995072800118WP 1995 7 28 ABXA9500581 119950719A323127749381 UPLATCH CAM DOUG DC8 DC863 302198AWP LT MLG DOOR WORN A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23817AX 45928 ON INITIAL GEAR RETRACTION AND UPLATCH CHECK, GEAR UNSAFE LIGHT AND GEAR DOOR NOT LATCHED LIGHT WERE ON. CYCLED GEAR SEVERAL TIMES, NO CHANGE. ACCOMPLISHED ABNORMAL PROCEDURES, CONFIRMED LEFT MLG DOOR NOT LATCHED. RESTRICTED AIRSPEED TO .65 MACH AND CONTINUED TO ILN. FOUND GEAR DOOR UPLATCH CAM WORN FOR LEFT GEAR. REPLACED DOOR ROLLER CAM. SYSTEM OPS CHECKED GOOD IAW DC 8 MM. 2L74 4F 4A25 19950728001191995072800119NM 1995 7 28 DL72E953121 119950720A55126520657 PANEL BOEING727 727247 138408FNM RT HORZ STAB DAMAGED A ADALAK NONE O OTHER ININSP/MAINT 1 SO11831WA 21483 UPON ARRIVAL PDX, FOUND ON RIGHT HORZ STAB LOWER SURFACE A CLOSURE PANEL FOR AN ELEV BALANCE PANEL BAY. PANEL 9216 THE FWD THIRD OF PANEL HAD SEPARATED FROM THE ACFT AND EMBEDDED ITSELF INTO THE TAIL CONE. ALSO, FOUND LOWER SKIN DAMAGED ON RIGHT ELEVATOR. DAMAGED PANEL 9206 WAS REPLACED WITH NEW, TAIL CONE REPAIRED PER DL ERA302170-4 AND ELEVATOR LOWER SKIN REPAIRED PER SRM 55-20-2. 2L73 4F A3WE 19950728001201995072800120NM 1995 7 28 DL72L953130 119950720A5320 WEB BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11514DA 21430 FOUND DURING A-1 LETTER CHECK, .3125 INCH CRACK AT LIGHTNING HOLE LT SIDE TOP 2ND HOLE FROM FWD SIDE AFT STAIRWELL WEB. REPAIRED PER SRM 53-11-0 828. 2L73 4F A3WE 19950728001211995072800121NM 1995 7 28 DL72S953120 119950719A3260 SENSOR BOEING727 727232 1384082NM RT MLG OUT OF ADJUST A DALAO OTHER N FALSE WARNING CRCRUISE 1 SO11470DA 20747 AT 31,000 FT RIGHT MAIN GEAR DISAGREEMENT LIGHT ILLUMINATED RED ON FORWARD PANEL, NO OTHER INDICATIONS. FLT CONTINUED WITH GEAR HANDLE UP AS PER POM. PASSED TO MCO DDM AT 0255Z LIGHT EXTINGUISHED PASSING 6000/220 KTS. ADJUSTED RT GEAR UPLOCK SENSOR. CHECKS NORMAL PER MM 32-61-81 PG 403. 2L73 4F A3WE 19950728001221995072800122NM 1995 7 28 DL72S953125 119950720A5754651622296 SKIN BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11542DA 22391 DURING ROUTINE SHOP INSPECTION, NR CARD 7904 WAS WRITTEN DUE TO CRACK IN LOWER SKIN, 9 INCHES FROM O/B EDGE ON NR 6 SLAT. CRACK WAS REPAIRED PER MM 57-54-0 FIG 801. 2L73 4F A3WE 19950728001231995072800123NM 1995 7 28 DL72S953140 119950721A5320651841483 WEB BOEING727 727232 1384082NM BS 294.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11467DA 20744 LT VERTICAL WEB OF NWW HAS 2.0 CRACK BETWEEN STA 294.5 AND STA 285.5, APPROX WL 170. REPAIRED PER DL ERA 302166-14AD. 2L73 4F A3WE 19950728001241995072800124NM 1995 7 28 DL72S953143 119950622A5320651751738 ANGLE BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11405DA 21149 1.0 CRACK IN ANGLE OF FWD BEAM OF THE RT TORQUE BOX, FS 1263. REPAIRED PER DL ERA 301959-14. 2L73 4F A3WE 19950728001251995072800125NM 1995 7 28 DL72S953148 119950711A5320651751737 ANGLE BOEING727 727232 1384082NM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND THE AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER ERA 302109-14AD. 2L73 4F A3WE 19950728001261995072800126NM 1995 7 28 DL72S953150 119950706A5311 FRAME BOEING727 727232 1384082NM FS 950 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 FORWARD FRAME OF C-2 CARGO OPENING FOUND CRACKED. REPAIRED PER DL ERA 302087-14AD. 2L73 4F A3WE 19950728001271995072800127NM 1995 7 28 DL72S953152 119950511A5753652163362 RIB BOEING727 727232 1384082NM NR 4 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 4 MIDFLAP, NR 6354 O/B THRUST BEARING BORE CORRODED. REPAIRED PER SRM 575004, MACHINED BORE AND INSTALLED BUSHING. NR 6320 O/B THRUST BEARING UPPER I/B RETAINER BOLT HOLE CORRODED. REPAIRED PER SRM 575004 FIG 14, MACHINED AND INSTALLED BUSHING. NR 6331 L/E WORN FROM I/B END APPROX 12. REPAIRED PER SRM 575200 FIG 803, INSTALLED FILLER AND DOUBLER. NR 6332 I/B RIB LOWER AFT CORNER CRACKED. REPAIRED PER M/M 575200 TRIMMED DAMAGE AND INSTALLED DOUBLER. REPAIRS ACCOMPLISHED AT SHOP VISIT. 2L73 4F A3WE 19950728001281995072800128NM 1995 7 28 DL72S953160 119950511A5753652163261 SKIN BOEING727 727232 1384082NM NR 2 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 2 MIDFLAP, AFT CORD ANGLE CRACKED 21, 36, AND 55 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 FIG 802 SPLICED IN NEW SECTIONS, NR 6272/6273/6274. ART CORD ANGLE CRACKED 41 FROM O/B END OF FLAP. REPAIRED PER M/M 575200 FIG 802 SPLICED IN NEW SECTION, NR 6275/6526/6537. COVE SKIN CRACKED 32 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 FIG 809. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER, NR 6277. REPAIRS ACCOMPLISHED DURING SHOP VISIT. 2L73 4F A3WE 19950728001291995072800129NM 1995 7 28 DL72S953161 119950512A5753652163262 DOUBLER BOEING727 727232 1384082NM NR 3 MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 NR 3 MIDFLAP, NR 6447 DOUBLER CRACKED IN TWO PLACES AT AFT CHORD ANGLE 29 FROM I/B END. REPAIRED PER M/M 575200 FIG 802. REMOVED AND REPLACED DOUBLER. NR 6449 AFT LOWER SPAR ANGLE DOUBLER IMPROPERLY INSTALLED 40 FROM O/B END. REPAIRED PER M/M 575200 FIG 802, REMOVED AND REPLACED DOUBLER. NR 6421O/B CARRIAGE SUPPORT THRUST BEARING RETAINER, BOTH UPPER BOLT HOLES AND LOWER I/B BOLT HOLE CORRODED AND NR 6423 I/B THRUST BEARING RETAINER, BOTH UPPER BOLT HOLES CORRODED. REPAIRED PER SRM 575004, REAMED AND INSTALLED BUSHINGS. ACCOMPLISHED REPAIRS DURING SHOP VISIT. 2L73 4F A3WE 19950728001301995072800130NM 1995 7 28 DL72S953162 119950722A3350 EEL BATTERY PACK S106 BOEING727 727232 1384082NM L-1 DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11525DA 21585 DURING PREFLIGHT, L-1 DOOR EMERGENCY EXIT SIGN FOUND INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950728001311995072800131NM 1995 7 28 DL72S953164 119950511A5753652163261 FLAP ASSY BOEING727 727232 1384082NM NR 2 MIDFLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 THRUST BEARING BORE RETAINER BOLT HOLES AT I/B END CORRODED, ON NR 2 MIDFLAP ASSEMBLY. REPAIRED PER SRM 57-50-4. 2L73 4F A3WE 19950728001321995072800132NM 1995 7 28 DL72S953168 119950719A5343 BEARINGS BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 BEARINGS, CORRODED NLG LT AND RT ATTACHMENT BEARINGS REPITTED. ACCOMPLISHED REPAIRS PER MM 53-40-0. 2L73 4F A3WE 19950728001331995072800133NM 1995 7 28 DL72S953169 119950719A5343 FITTING BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FITTING CORRODED NLG RT ATTACH FITTING IS CORRODED ON BEARING ON FACE AND PADS. MACHINED RT BORE TO 2.556 TO REMOVE CORROSION. MACHINED SPOTFACES OF FITTING AND CAP TO REMOVE CORROSION LUG THICKNESS. FITTING 1.508 INCH, CAP 1.455 INCH WITHIN M/M 53-40-0 FIG 811. DYE CHECKED, REWORKED AREAS. ROTOPEENED REWORKED AREAS, TREATED AND PAINTED REF M/M 53-40-0. 2L73 4F A3WE 19950728001341995072800134NM 1995 7 28 DL72S953170 119950719A5343 FITTING BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FITTING CORRODED, NLG LT ATTACH FITTING IS CORRODED ON BEARINGS ON FACE AND ON PADS. MACHINED BORE TO 2.625 FOR CORROSION REMOVAL. MACHINED SPOTFACES OF FITTING AND CAP TO REMOVE CORROSION LUG THICKNESS, FITTING 1.499 INCH, CAP 1.434 INCH WITHIN LIMITS OF M/M 53-40-0 FIG 811. DYE CHECKED REWORKED AREAS. ROTOPEENED REWORKED AREAS, TREATED AND PAINTED PER M/M 53-40-0. 2L73 4F A3WE 19950728001351995072800135NM 1995 7 28 DL72S953171 119950720A5343 FITTING BOEING727 727232 1384082NM NLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NOSE LANDING GEAR, ATTACH FITTING RIGHT SIDE AFT HOLE IS CORRODED. REAMED HOLE TO .890 TO REMOVE CORROSION PER M/M 53-40-0. 2L73 4F A3WE 19950728001361995072800136NM 1995 7 28 DL72S953175 119950722A217017805011 SEPARATOR ASSY BOEING727 727232 1384082NM LOWER ACM COMP BURST A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11482DA 20862 ON CLIMBOUT AT FL 2,500, HEARD LOUD BANG FOLLOWED BY VIBRATION AND RISING CABIN ALTITUDE, RETURNED ATL. FOUND LEFT PACK WATER SEPARATOR ASSEMBLY BURST. REPLACED SAME, OPERATION NORMAL. 2L73 4F A3WE 19950728001371995072800137NM 1995 7 28 DL72W953127 119950720A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11296WA 22533 FOUND DURING E-2 LETTER CHECK, 1 INCH CRACK IN VERT STAB STRINGER 8 RT AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19950728001381995072800138NM 1995 7 28 DL72W953128 119950720A5754 ANGLE BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11296WA 22533 NR 2 L/E SLAT COVE SKIN ANGLE CRACKED AT I/B STOP PAD. ITEM FOUND DURING E-2 LETTER CHECK. REPAIRED PER MM 57-54-0 PG 807. 2L73 4F A3WE 19950728001391995072800139NM 1995 7 28 DL72W953129 119950720A5754 DOUBLERS BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11296WA 22533 FOUND DURING E-2 LETTER CHECK, NR 3 L/E SLAT ACT ROD END I/B AND O/B SUPPORT RIB DOUBLERS CRACKED. REPLACED DOUBLERS PER M/M 57-54-0 PG 803 TO 805. 2L73 4F A3WE 19950728001401995072800140NM 1995 7 28 DL72W953131 119950720A3350900835A EEL BATTERY PACK 900542 BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112819W 11081 21057 EMERG LIGHT, F/C BULLNOSE INOP. REPLACED BATTERY AND RACK, OPERATION NORMAL. 2L73 4F A3WE 19950728001411995072800141NM 1995 7 28 DL72W953137 119950705A5753652163492 SKIN BOEING727 727247 138408FNM NR 3 AFT FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11296WA 22533 NR 3 AFT FLAP L/E SKIN WORN AT 21 AND 35 FROM O/B END OF FLAP. REPAIRED PER SRM 57-50-4, FOUND AT SHOP INSPECTION. 2L73 4F A3WE 19950728001421995072800142NM 1995 7 28 DL72W953145 119950623A532065175196 ANGLE BOEING727 7272Q8 138407WNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11831L 21826 1.5 INCH CRACK IN ANGLE OF FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. REPAIRED PER DL ERA 301995-14AD. 2L73 4F A3WE 19950728001431995072800143NM 1995 7 28 DL72W953149 119950708A5320651751737 ANGLE BOEING727 727247 138408FNM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112809W 20581 CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA302097-14AD. 2L73 4F A3WE 19950728001441995072800144NM 1995 7 28 DL72W953151 119950704A5320651751739 ANGLE BOEING727 727247 138408FNM FS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT STA 1263. REPAIRED PER DL ERA 302068-14AD. 2L73 4F A3WE 19950728001451995072800145NM 1995 7 28 DL72W953153 119950620A5753652163395 RETAINERS BOEING727 727247 138408FNM NR 1 MIDFLAP CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 NR 1 MIDFLAP, I/B THRUST BEARING RETAINER, UPPER TWO BOLT HOLES CORRODED. REPAIRED PER SRM 575004 FIG 14 AND ERA302153-14. REAMED AND INSTALLED BUSHINGS, NR CARDS 6671/7220. O/B THRUST BEARING RETAINER UPPER O/B BOLT HOLE CORRODED, REPAIRED PER SRM 575004 FIG 14. REAMED AND INSTALLED BUSHING, NR 6673. REPAIRS ACCOMPLISHED AT SHOP VISIT. 2L73 4F A3WE 19950728001461995072800146NM 1995 7 28 DL757953133 119950719A2530811150417 COFFEE MAKER BOEING757 757232 1384965NM FWD GALLEY SMOKING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11625DL 22915 DURING CRUISE, F/A REPORTED SMOKE COMING OUT OF FORWARD GALLEY COFFEE MAKER. POWER WAS REMOVED AND AS PRECAUTION PORTABLE FIRE EXTINGUISHER WAS USED. COFFEE MAKER WAS REPLACED, OPERATION NORMAL. 2L72 4F RTA2NM 19950728001471995072800147NM 1995 7 28 DL757953135 119950721A5754114N4004165A TE WEDGE BOEING757 757232 1384965NM NR 3 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11639DL 23993 UPON INITIAL INSPECTION, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED PER SRM 57-43-02, FOR NR 3 L/E SLAT PANEL. 2L72 4F RTA2NM 19950728001481995072800148NM 1995 7 28 DL757953141 119950720A5330 SKIN BOEING757 757232 1384965NM FS 1698 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 SKIN AT STA 1698 AND STR 17L SUSTAINED GROUND DAMAGE REQUIRING A 1.5 BY 1.75 CUT OUT. INSTALLED DOUBLER PER DL ERA302169-14. 2L72 4F RTA2NM 19950728001491995072800149NM 1995 7 28 DL767953159 119950505A5754114T410422A TE WEDGE BOEING767 767232 1385132NM NR 4 SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 DURING SHOP INSPECTION, NR 4 L/E SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. WEDGE WAS REPLACED PER SRM 57-43-55. 2L72 4F RTA1NM 19950728001501995072800150NE 1995 7 28 DLL10953163 219950721A7210RB21122B02 GEARBOX LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE FAILED A DALAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 SO111732D AM623 193C1213 010428 NR 2 ENG FAILED 16 MIN AFTER T/O. FOUND GEARBOX FAILED. REPLACED GEAR BOX, OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19950728001511995072800151WP 1995 7 28 DLL10953166 119950706A27401539749 TORQUE TUBE LKHEED1011 10113851 5265010WP HORIZ STAB CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 HORIZONTAL STABILIZER RT UPPER TORQUE TUBE SUPPORT BRACKET WAS FOUND WITH CORROSION ON THE LWR SURFACE OF THE UPPER LUG. CORROSION DOES NOT EXTEND INTO THE PARTING PLANE OF THE TWO BRACKET HALVES. ACCOMPLISHED REPAIRS PER DL ERA 271316-14AD. 2L73 4F A23WE 19950728001521995072800152WP 1995 7 28 DLL10953174 119950722A21507339347 ACM LKHEED1011 10113851 5265010WP AC COMP FAILED A DALAA UNSCHED LANDING JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11722DA 193C1147 SHORTLY AFTER TAKEOFF, SMOKE ALARMS IN AFT CABIN WENT OFF. FLIGHT ATTENDANTS REPORTED SMOKE HAZE IN CABIN, RETURNED LAX. FOUND OIL CONTAMINATION ON NR 2 WATER SEPARATOR BAG. REPLACED BAG AND NR 2 ACM, OPERATION NORMAL. 2L73 4F A23WE 19950728001531995072800153WP 1995 7 28 DLL13953122 119950704A5347 TRACK LKHEED1011 10113851 5265010WP MID GALLEY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND SEAT TRACK CORRODED AT MID GALLEY ATTACH. REMOVED TRACK AND REPLACED PER SRM 53-21-00 PG 836. 2L73 4F A23WE 19950728001541995072800154WP 1995 7 28 DLL13953123 119950706A5315 FLOORBEAM LKHEED1011 10113851 5265010WP CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FLOORBEAM CORRODED, AT LBL 53. REMOVED OLD CAP, TREAT AND PAINTED NEW CAP AND REPAIR ANGLES INSTALLED PER SRM 53-21-00 FIG 828. 2L73 4F A23WE 19950728001551995072800155WP 1995 7 28 DLL13953124 119950706A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 313-331 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FLOOR SUPPORT CORRODED FS 313.0 TO 331.0, RBL 28. REMOVED OLD CHANNEL AND REPLACED PER SRM 53-21-00. 2L73 4F A23WE 19950728001561995072800156WP 1995 7 28 DLL13953134 119950702A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1463 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FLOOR SUPPORT CORRODED C2 B/B STA 1463 STR 35. REMOVED OLD SUPPORT, FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-23-00 FIG 803. 2L73 4F A23WE 19950728001571995072800157WP 1995 7 28 DLL13953154 119950702A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND FLOOR SUPPORT CORRODED C2 B/B FS 1565 LBL 5. REMOVED OLD SUPPORT, FABRICATED NEW SUPPORT AND SPLICES, AND INSTALLED PER SRM 53-23-00 PG 803. 2L73 4F A23WE 19950728001581995072800158WP 1995 7 28 DLL13953155 119950703A7110 NOSE COWL LKHEED1011 10113851 5265010WP BS 1705 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND NOSE COWL CRACKED AT STA 1705, NR 2 INTAKE. REMOVED OLD ANGLE, AND FABRICATED NEW. INSTALLED PER SRM 54-12-00 PG 806. 2L73 4F A23WE 19950728001591995072800159WP 1995 7 28 DLL13953156 119950703A7110 NOSE COWL LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND NOSE COWL CRACKED RT UPPER FWD ACCESS NR 2 INLET. REMOVED FASTENERS FABRICATED REPAIR. DYE CHECKED AND INSTALLED REPAIR PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950728001601995072800160WP 1995 7 28 DLL13953158 119950720A57551529101170 PANEL LKHEED1011 10113851 5265010WP NR 1 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 DURING SHOP INSPECTION NR 1 RT WING SPOILER PANEL WAS FOUND WITH DELAMINATION. PANEL WAS RECONDITIONED PER SRM 57-52-00 AND DRAWING CMM 1529101. 2L73 4F A23WE 19950728001611995072800161NE 1995 7 28 DLM88953119 219950719A7250JT8D219 NR 6 BRG SEAL DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED A DALAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO11974DL17388 53242 718153 RT ENGINE OIL QTY WENT TO ZERO ON DESCENT AT 16000 FEET, FOLLOWED BY LOW OIL PRESSURE LIGHT. SHUT DOWN ENGINE PER POM. REPLACED NR 6 BEARING CARBON SEAL AND SCAVENGE PUMP, OPERATION NORMAL. 2L72 4F4 FRTA6WE E9NE 19950728001621995072800162NM 1995 7 28 DLM88953157 119950721A3397 WIRE DOUG MD88 MD88 3023688NM RT AFT LAV CHAFED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11926DL 49713 F/A REPORTED, SPARKS WITH SMOKE MOMENTARILY IN RT AFT LAV FROM AREA OF FWD MIRROR LIGHT NEXT TO DOOR FRAME, WHEN DOOR CLOSED AND LOCKED. INSPECTION FOUND WIRE FROM DOOR SW CHAFED AND SHORTED TO FRAME FOR THE AFT LAV OCCUPIED SIGN. REMOVED AND TIED BACK WIRE PULLED AND COLLARD C/B FOR AFT LAV OCCUPIED SIGN. WIRE REPAIRED, FWD TO MCO AND PLAC 480194001. 2L72 4F RTA6WE 19950728001631995072800163NM 1995 7 28 DLM88953167 119950614A5330 SKIN DOUG MD88 MD88 3023688NM FS 440-488 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 A 7 INCH WIDE BY 48 INCH LONG BY .1250 DEEP DENT WAS FOUND IN THE FUSELAGE SKIN FROM FS 440 TO FS 488 BETWEEN STR 19R AND STR 20R. NEITHER FRAMES NOR STRINGERS AT THE SUBJECT AREA WAS DAMAGED. THE DAMAGED SKIN IS M/F FROM .050 2024-T3 CLAD. ACCOMPLISHED REPAIRS PER DL ERA 271142-14. 2L72 4F RTA6WE 19950728001641995072800164WP 1995 7 28 MWEA95236 119950718A3350 EEL FUSE DOUG DC9 DC932 3022066WP CABIN FAILED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31301ME 47190 CREW REPORTS, FORWARD FIVE ROWS OF EMERGENCY FLOOR TRACK LIGHTING WILL NOT TEST. MAINTENANCE REPLACED FUSE IN FWD FLOOR TRACK PACK SYSTEM. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950728001651995072800165WP 1995 7 28 MWEA95237 119950720A25607270009 COVER DOUG DC9 DC914 3022034WP TAIL SLIDE OFF HINGE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 DURING ROUTINE INSPECTION, THE TAIL EMERGENCY SLIDE COVER WAS FOUND NOT INSTALLED ON HINGE. MAINTENANCE RESECURED TAIL SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950728001661995072800166WP 1995 7 28 MWEA95238 119950720A5350H2028B CONNECTOR DOUG DC9 DC914 3022034WP TAILCONE CORRODED A MWEAK NONE N FALSE WARNING CRCRUISE 1 GL31800ME 45842 DURING CRUISE, TAIL CONE MISSING LIGHTS WENT ON AND OFF INTERMITTENTLY. THE TAILCONE SWITCH CONNECTORS WERE FOUND CORRODED. CLEANED CORROSION AND OPS CHECKED GOOD. 2L72 4F A6WE 19950728001671995072800167WP 1995 7 28 MWEA95239 119950722A490038025611 APU DOUG DC9 DC932 3022066WP AFT ACCESSORY SMOKING A MWEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31204ME 47680 MAINTENANCE REPORTS, SMOKE IN CABIN WITH ONLY APU RUNNING. MAINTENANCE REMOVED AND REPLACED APU. OPS CHECK GOOD, NO SMOKE IN CABIN. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950728001681995072800168EU 1995 7 28 QXEA9500219 119950721A33501315 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 GEG - OVERHEAD EXIT LIGHT INOP. BULB REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950728001691995072800169NE 1995 7 28 9511165511 219950721A732177910010 FUEL CONTROL BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A ANWAACE ABORTED TAKEOFF ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01511US 23199 16359 DURING TAKEOFF THE NR 1 ENGINE DID NOT REACH FULL TAKEOFF POWER, THE THROTTLES WERE CLOSED, BUT THE ENGINE DID NOT REDUCE TO IDLE. THE NR 1 ENGINE WAS SHUTDOWN AND THE MESSAGES LT ENG SEC CONT AND LT ENG PRI CONT WERE RECEIVED. THE LEFT FUEL CONTROL UNIT WAS REPLACED. LEAK AND OPERATIONAL CHECK OK. 2L72 4F4 FRTA2NM E17NE 19950728001701995072800170NE 1995 7 28 9511176601 219950724A7200 ENGINE BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE NR 4 FLAMED-OUT A NWAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 GL01601US 19778 662615 DURING CRUISE, THE NR 4 ENGINE FLAMED-OUT. RELIGHT WAS OK AND THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. FUEL PRESSURE CHECKED OK AND THE FUEL FILTER WAS REPLACED. GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E20EA 19950728001711995072800171EU 1995 7 28 9511183214 119950723A3250710TS06Y11 TRANSMITTER AIRBUS320 A320211 3930320EU NLG STEERING MALFUNCTIONED A ANWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL01314US 160 AFTER TAKEOFF, THRUST WAS APPLIED, THE AIRCRAFT DRIFTED SLIGHTLY TO THE RIGHT, FULL LEFT RUDDER WAS APPLIED WITH NO RESPONSE. FULL LEFT TILLER WAS APPLIED WITH NO RESPONSE. THE TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETURNED SAFELY TO THE GATE. MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT NOSE STEERING TRANSMITTERS, 1GC AND 2GC. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950728001721995072800172WP 1995 7 28 9511199151 119950723A272037723745503 SHUTOFF VLV DOUG DC9 DC914 3022034WP RUDDER LEAKING A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL018909E 45770 DURING INITIAL CLIMB, EXPERIENCED RIGHT HYDRAULIC SYSTEM FLUID AND PRESSURE LOSS. FLIGHT RETURNED TO ORIGIN WITHOUT FURTHER INCIDENT. THERE WAS NO FURTHER LOSS WITH GEAR EXTENDED. FOUND RUDDER HYDRAULIC POWER SHUTOFF VALVE LEAKING FROM VALVE BODY. REPLACED SHUTOFF VALVE, CHECKED OK. 2L72 4F A6WE 19950728001731995072800173NM 1995 7 28 9511202277 119950723A213310328051 OUT FLOW VALVE BOEING727 727251 138408HNM CABIN MALFUNCTIONED A NWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 GL01277US381182269 21156 CLIMBING THROUGH FL 260, UNABLE TO MAINTAIN AND CONTROL CABIN PRESSURIZATION. MANUALLY DEPLOYED PASSENGER OXYGEN MASK AND DIVERTED TO DCA. MAINTENANCE REPLACED LEFT OUTFLOW VALVE. OPERATIONAL PRESSURIZATION CHECK WAS NORMAL. 2L73 4F A3WE 19950728001741995072800174WP 1995 7 28 9511219755 119950724A2750 TORSION SPRING DOUG DC9 DC941 302207NWP TE FLAPS BENT A NWAAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 GL01755NW 47179 WHILE ON APPROACH FOR LANDING AT MBS, UNABLE TO EXTEND FLAPS FOR LANDING, HANDLE JAMMED IN THE UP POSITION. CONFERRED WITH MAINTENANCE CONTROL, UNABLE TO UNJAM. DECLARED EMERGENCY AND RETURNED TO DTW FOR A NO FLAP LANDING. NO FURTHER INCIDENTS. FOUND FLAP RELEASE TRIGGER BINDING. ALSO, FOUND FLAP HANDLE LATCH TORSION SPRING BENT. INSTALLED NEW TORSION SPRING, CYCLED FLAP HANDLE SEVERAL TIMES, CHECKED OK. 2L72 4F A6WE 19950728001751995072800175NM 1995 7 28 9511222712 119950723A3260 SWITCH BOEING727 7272S7 138407ZNM TAIL SKID LACK OF LUBE A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01712RC 22020 DURING CLIMB UPON GEAR RETRACTION, TAIL SKID INDICATION REMAINED ILLUMINATED. RECYCLED GEAR TO NO AVAIL. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED TAIL SKID INDICATION SWITCH. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950728001761995072800176NM 1995 7 28 95UAL900054 119950725A2560 GIRT BAR BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE SERVICE DOOR LOOSE A UALAK NONE O OTHER ININSP/MAINT 1 WP29916UA 25383 FWD SERVICE DOOR SLIDE GIRT BAR WILL NOT STAY SECURED. REPLACED SLIDE. 2L72 4F4 FRTA16WE E2GL 19950728001771995072800177NM 1995 7 28 95UAL900055 119950725A2560 SLIDE BOTTLE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DOOR LOW PRESS A UALAK NONE O OTHER ININSP/MAINT 1 WP297266U 21413 FLIGHT ATTENDANT REPORTS, SLIDE PRESSURE LOW AT 1L. SERVICED BOTTLE. 2L73 4F4 F A3WE E2EA 19950728001781995072800178NM 1995 7 28 95UAL900056 119950725A3350 EEL BATTERIES BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299068U 19949 ONE COACH EMERGENCY FLASH LIGHT DOES NOT WORK. REPLACED BATTERIES. 2L72 4F4 F A16WE E2EA 19950728001791995072800179NM 1995 7 28 95UAL900057 119950725A3350 EEL BATTERY PACK BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29655UA 25393 EMERGENCY LIGHTS RT SIDE NR 5, 6 AND 7 ARE OUT. REPLACED BATTERY PACK, OPS CHECK NORMAL. 2L72 4F4 FRTA1NM E24NE 19950728001801995072800180NM 1995 7 28 95UAL900058 119950725A3350 EEL BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29612UA 21873 LT EXTERIOR EMERGENCY LIGHTS NR 1 AND NR 5 COUNTING FROM FWD TO AFT IS INOP. REPLACED LAMPS, OPS CHECKS NORMAL. 2L72 4F4 FRTA1NM E3NE 19950728001811995072800181NM 1995 7 28 95UAL900059 119950725A3350 EEL BATTERY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29177UA 24384 CREW REPORTED, UPPER DECK FLOOR EEL LIGHT WOULD NOT ILLUMINATE. REPLACED BATTERY AND CKD OK. 2L74 4F4 FRTA20WE E24NE 19950728001821995072800182NM 1995 7 28 95UAL900060 119950725A2611 SMOKE DETECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE AFT LAV INOPERATIVE A UALAK NONE N FALSE WARNING CRCRUISE 1 WP29510UA 24780 LAVATORY SMOKE ALARM WON'T TURN OFF. DEBRIEF CABIN CREW FOR SPECIFIC LOCATIONS. SMOKE DETECTOR INOP IN AFT LAV, SYSTEM OP CHECKED OK. SUSPECT PASSENGER BLOCKED OFF DETECTOR. 2L72 4F4 FRTA2NM E17NE 19950728001831995072800183WP 1995 7 28 95UAL900061 119950725A27604913802BT15616 CONTROL CABLE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE LT SPOILER BROKEN A UALAK NONE OF OTHER FLT CONT AFFECTED ININSP/MAINT 1 WP291853U 47812 DURING SERVICE OF HYD FLUID, FOUND CABLE OF LT INBD SPOILER BROKEN. REPLACED CABLE AND RERIGGED. 2L73 4F4 F A22WE E23EA 19950728001841995072800184NM 1995 7 28 95UAL900062 119950725A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29509UA 24763 EEL LIGHT COVER LOOSE 2C TO 4C. SECURED LIGHTS AS REQUIRED. 2L72 4F4 FRTA2NM E17NE 19950728001851995072800185NM 1995 7 28 95UAL900064 119950725A2730 PCU 10609263 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT ELEV MALFUNCTIONED A UALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 WP297448U 21902 LANDED ORD UNDER AMBER ALERT, DUE TO HEAVY CONTROL FORCES EXCESSIVE AS IF NO HYDRAULICS. REPLACED RT ELEVATOR POWER CONTROL UNIT. SYSTEM OP CHECKS OK. 2L73 4F4 F A3WE E2EA 19950728001861995072800186SO 1995 7 28 COM11930 119950721A3260922AA27A6PZ72 PROX SENSORS EMB 120 EMB120RT SO NLG OUT OF ADJUST A COMAK NONE N FALSE WARNING CLCLIMB 1 SO01168CA 120168 A-SYSTEM NLG INTRANSIT LIGHT REMAINS ON AFTER LANDING GEAR RETRACTED. ADJUSTED UPLOCK PROXIMITY SENSORS TO M/M SPECIFICATIONS. 2L72 4T RTA31SO 19950728001871995072800187SO 1995 7 28 COM11931 119950721A540012026820001 LATCH ASSY EMB 120 EMB120RT SO LT NACELLE BROKEN A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01200CD 120200 LEFT ENGINE INBD NACELLE LATCH IS BROKEN. REPLACED LATCH. 2L72 4T RTA31SO 19950728001881995072800188SO 1995 7 28 COM11932 119950723A3260922AA2YA6PZ7 PROX SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01257CA 120248 LT MLG A-SYSTEM INTRANSIT LIGHT REMAINS ON DURING FLIGHT. REPLACED DOWN LOCK PROXIMITY SENSOR. 2L72 4T RTA31SO 19950728001891995072800189 1995 7 28 COM11933 419950724A34186225734002 SERVO 6225734002 EMB 120 EMB120RT SO STICK PUSHER DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO011117H121675873 3624 120117 THERE IS NO STICK PUSHER WHEN TESTING STALL WARNING SYSTEM. REPLACED THE STICK PUSHER SERVO MOTORS. 2L72 4T RTA31SO 19950728001901995072800190EA 1995 7 28 COM60522 119950724A323016215103 BRACKET CNDAIRCL600 CL6002B19 EA NLG BENT A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01931CA 7037 NOSE LANDING GEAR WOULD NOT RETRACT. REPLACED NLG WEIGHT ON WHEELS SENSOR BRACKET, WHICH WAS DAMAGED DURING PUSHBACK. 2L72 4F RTA21EA 19950728001911995072800191EA 1995 7 28 COM60523 119950724A276054C54677E01 MANIFOLD CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01927CA2421 7031 GROUND SPOILERS DID NOT DEPLOY. REPLACED THE SPOILER CONTROL MANIFOLD. 2L72 4F RTA21EA 19950728001921995072800192 1995 7 28 COM60524 419950723A34176229820003 DCU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO01937CA2303 7044 EICAS COMP INOP MESSAGE IS ON. REPLACED THE NR 1 DATA CONCENTRATOR UNIT. 2L72 4F RTA21EA 19950728001931995072800193NM 1995 7 28 SWAA950524 119950722A5311 FRAME BOEING737 7372T4 1384492NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B BETWEEN S4 AND 5L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728001941995072800194NM 1995 7 28 SWAA950543 119950722A5312 BLKHD CHORD BOEING737 7372T4 1384492NM BS 1156 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 1156 BULKHEAD LEFT CHORD CRACKED 1.5 INCHES IN LENGTH AND RUNNING VERTICALLY. REPAIRED PER SWA ACO 473-53 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728001951995072800195NM 1995 7 28 SWAA950544 119950722A5320 WEB BOEING737 7372T4 1384492NM APU INLET CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND APU AIR INLET O/B WEB CRACKED 1 INCH LONG WITH A HOLE .25 INCH WIDE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728001961995072800196NM 1995 7 28 SWAA950545 119950722A5311 BELTFRAME BOEING737 7372T4 1384492NM RT AC BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND FAIRING SUPPORT BELT FRAME CRACKED 2 INCHES BELOW AIR DUCT. REPAIRED PER SWA ACO 518-53. 2L72 4F A16WE 19950728001971995072800197NM 1995 7 28 SWAA950546 119950722A5320 CHORD BOEING737 7372T4 1384492NM BS 663.75 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND COMPRESSION CHORDS CRACKED AT BS 663.75, LBL 24.75 AND AT RBL 24.75. REPAIRED PER BOEING DRAWING 691A0032 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728001981995072800198NM 1995 7 28 SWAA950547 119950722A5320 WEB BOEING737 7372T4 1384492NM SERVICE DOORWAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT SERVICE DOORWAY WEB BELOW ASSIST HANDLE CRACKED AT UPPER END. REPAIRED PER SWA ACO 471-53. 2L72 4F A16WE 19950728001991995072800199NM 1995 7 28 SWAA950548 119950722A5712 CHORD BOEING737 7372T4 1384492NM WBL 135.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, FWD OF S2 AT RADIUS. REPAIRED PER SWA ACO 587-57. 2L72 4F A16WE 19950728002001995072800200NM 1995 7 28 SWAA950549 119950722A5320 ANGLE BOEING737 7372T4 1384492NM BS 540 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE CRACKED AT BS 540 AT TOP FAIRING SUPPORT FRAME. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728002011995072800201NM 1995 7 28 SWAA950550 119950722A5320 STRAP BOEING737 7373H4 1384600NM E/E COMP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07319SW 23340 DURING SCHEDULED B/C1 CHECK, FOUND FLOOR BEAM SUPPORT STRAP CRACKED AT RBL 31 IN E AND E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950728002021995072800202NM 1995 7 28 SWAA950551 119950722A5320 FRAME BOEING737 7373H4 1384600NM CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07302SW 22942 DURING SCHEDULED B/C3 CHECK, FOUND FWD CARGO DOOR FRAME CRACKED IN AFT LOWER CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950728002031995072800203NM 1995 7 28 SWAA950552 119950722A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0787SW 22903 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REPAIRED PER BOEING S/B 737-53-1074 AND STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728002041995072800204NM 1995 7 28 SWAA950553 119950722A5320 WEB BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0726SW 21117 DURING SCHEDULED CHECK, FOUND NOSE WHEELWELL LEFT VERTICAL WEB CRACKED 3.1 INCHES, BELOW FWD LEFT ACCESS PANEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950728002151995072800215SO 1995 7 28 95ZZZX3468 119950609A32137873805 AXLE 6549311 PIPER PA32 PA32301 7103207SO RT MLG FAILED A APNSAO OTHER O OTHER LDLANDING 1 AL03818446072 328006012 RIGHT MAIN GEAR AXLE BROKE ON LANDING. CROSSWIND MAY HAVE BEEN A FACTOR. NOTE: AXLE SHIPPED TO PIPER AIRCRAFT FOR FAILURE ANALYSIS. 1L71 3O A3SO 19950728003031995072800303WP 1995 7 28 9511239150 119950718A5350 HANDLE DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR TAILCONE HANDLE AND DROP THE TAILCONE. RERIGGED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950728003041995072800304WP 1995 7 28 9511249964 119950724A5350 HANDLE DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01912RW 47150 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE HANDLE FROM THE CLIPS. ADJUSTED THE HANDLE PER MAINTENANCE MANUAL 53-50-03. 2L72 4F A6WE 19950728003051995072800305WP 1995 7 28 ABXA9500582 119950723A28303119001 DUMP VALVE DOUG DC8 DC863 302198AWP NR 1 ALT STUCK OPEN A ABXAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23814AX 46041 AFTER 5,000 FT, 2.5 PSID, MAIN CARGO DOOR WRN LIGHT ILLUMINATED. LOCKS WERE ENGAGED, MORE WIND NOISE THAN NORMAL. WHEN SELECTED, DUMP CHUTE IND WAS MIDWAY BETWEEN DRAIN AND DOWN. MANUALLY CRANKED CHUTE DOWN; DUMPED APPROX 14,100 LBS. FOUND FUEL DUMPING OUT OF LT CHUTE WHICH WAS UP AND LOCKED. CREW HAD TO TRANSFER ALL FUEL FROM LT WING TO STOP FUEL DUMP. INSPECTED DOOR SEAL, LOCKS, HINGES, ACTUATORS, SWITCHES AND WARNING CIRCUIT. GROUND RAN, AND PRESS TO 4 PSI, NO LEAKS NOTED. CYCLED CARGO DOOR SEVERAL TIMES, OPS CHECKED GOOD IAW DC 8 MM. FOUND SEALANT IN NR 1 ALT DUMP FLAPPER VALVE. REMOVED SEALANT, CLEANED AREA, REFUELED, AND LEAK CHECKED. 2L74 4F 4A25 19950728003061995072800306NE 1995 7 28 ABXA9500583 219950723A732171128713 FUEL CONTROL DOUG DC8 DC863 302198AWP PWA JT3D JT3D3B 52039NE NR 3 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23813AX 46136 669739 CREW SHUTDOWN NR 3 ENGINE DUE TO FLAME-OUT, UNABLE TO RELIGHT. FUEL PSI NORMAL, OIL PSI AND TEMPERATURE NORMAL, 6,450 LBS OF FUEL IN NR 3 MAIN TANK, 0002 Z, ALTITUDE 8,000 FT STRAIGHT AND LEVEL FLIGHT. DRIP STICKED NR 3 MAIN AND SUMPED TANKS, ALL CHECKED OK. SENSE LINES, FCU, P AND D, IGNITION, FUEL SCREENS, ALL CHECKED OK. REPLACED FUEL TEMPERATURE REGULATOR FILTER. PRESSURE CHECKED IN TANK FUEL FEED LINES. RAN ENGINE TO TAKEOFF POWER, PRBC SCHEDULING AND BLEEDS, ALL CHECKED OK IAW DC 8 MM. REPLACED NR 3 FUEL CONTROL AFTER SUBSEQUENT FLIGHT. TRIMMED AND LEAK CHECKED IAW DC 8 MM. 2L74 4F4 F 4A25 1E8 19950728003071995072800307WP 1995 7 28 ABXA9500584 119950724A3260 INDICATOR WIRE DOUG DC9 DC933F 302207AWP LT MLG OPEN A ABXAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL23933AX 47291 DURING CLIMB, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE DURING GEAR RETRACTION. DID NOT ILLUMINATE DURING IDLE FLIGHT WHILE IN DESCENT. FOUND WIRE 1G206024 OPEN. REPLACED WIRE IAW DC-9 WDM 32-61-0. LANDING GEAR SYSTEM OPS CHECKED NORMAL IAW DC-9 SUPP MM 32-60-00. 2L72 4F A6WE 19950728003081995072800308WP 1995 7 28 MWEA95240 119950724A493036011932 ATOMIZER DOUG DC9 DC932 3022066WP APU LEAKING A MWEAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL31401ME 47133 CREW REPORTS WHILE AT GATE IN MKE, THERE WAS A VERY STRONG FUEL SMELL IN CABIN. MAINTENANCE FOUND FUEL LEAKING AT FUEL ATOMIZER ON APU BURNER CAN. REMOVED AND REPLACED ATOMIZER O-RING. LEAK CHECKED GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950728003091995072800309NM 1995 7 28 MWEA95241 119950724A25603952273501 GIRT BAR LATCHES DOUG MD88 MD88 3023688NM AFT GALLEY LACK OF LUBE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 CREW REPORTS, AFT GALLEY SERVICE DOOR SLIDE GIRT BAR STICKS IN THE ARMED POSITION. MAINTENANCE CLEANED AND LUBRICATED GIRT BAR LATCHES. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950728003101995072800310WP 1995 7 28 MWEA95242 119950725A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR DETACHED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31602ME 48133 CREW REPORTS, GALLEY SERVICE DOOR SLIDE COVER NOT SECURE. MAINTENANCE RESECURED SLIDE COVER, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950728003841995072800384CE 1995 7 28 95ZZZX3520 119950708A3222 STRUT CESSNA207 T207A 2073614CE NLG OVERSERVICED A OEZAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP19101EN 20700666 NOSE STRUT OVERSERVICED CAUSING LOSS OF STEERING. TO PREVENT THIS, MAINTENANCE SHOULD SERVICE TO WHAT THE MANUFACTURER STATES AND PERFORM A TAXI TEST. 1H71 3O A16CE 19950728003851995072800385CE 1995 7 28 95ZZZX3521 119950708A711212509271 BAFFLING CESSNA207 T207A 2073614CE PROP GOV AREA MISINSTALLED A OEZAK NONE O OTHER NRNOT REPORTED 1 WP196372H 20700499 BAFFLING WAS IMPROPERLY INSTALLED, JAMMING PROPELLER CONTROL INTERMITTENTLY. MAINTENANCE SHOULD DOUBLE CHECK THEIR WORK ESPECIALLY SINCE THIS AIRPLANE JUST CAME OUT OF AN INSPECTION. 1H71 3O A16CE 19950728004011995072800401WP 1995 7 28 9511259997 119950705A5311 FRAME DOUG DC9 DC931 3022065WP FS 180 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A 3 INCH CRACK IN THE FS 180 FRAME AT LONGERON 9R ABOVE THE SERVICE DOOR. REPAIRED FRAME (P/N 9957874-29) PER EA 99-99931. 2L72 4F A6WE 19950728004021995072800402WP 1995 7 28 9511269997 119950710A5330 SKIN DOUG DC9 DC931 3022065WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND .1250 INCH AND .0625 INCH CRACKS IN THE FUSELAGE SKIN NEAR THE MAIN CABIN DOOR FS 200, LONGERON 14L. REPAIRED SKIN (P/N 5911406-59) PER EA 99-100799. 2L72 4F A6WE 19950728004031995072800403WP 1995 7 28 9511279997 119950712A5320 JAMB DOUG DC9 DC931 3022065WP GALLEY SVC DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND A CRACK IN THE GALLEY SERVICE DOOR JAMB PAN, FORWARD UPPER CORNER. REPAIRED PAN (P/N 5921326-501) PER EA 99-100800. 2L72 4F A6WE 19950728004041995072800404NM 1995 7 28 9511286608 119950713A531365B044832 STRINGER BOEING747 747151 1384891NM FS 1820-1840 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON STR 47L BETWEEN BS 1820 - BS 1840. REPAIRED STRINGER (P/N 65B04483-2) PER EA 66-98658. 2L74 4F A20WE 19950728004051995072800405WP 1995 7 28 9511299964 119950717A5312 BLKHD FITTING DOUG DC9 DC931 3022065WP PRESS BLKHD CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01912RW 47150 DURING H-CHECK, FOUND A ONE INCH CRACK IN THE PRESSURE BULKHEAD WING SPAR TO T-CAP ATTACH FITTING AT LONGERON 24L. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950728004061995072800406WP 1995 7 28 9511309607 119950718A5320 FITTING DOUG DC9 DC932 3022066WP FS 945 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION IN THE INTERCOSTAL TIE FITTING FS 945, LONGERON 29R. REPLACED FITTING (P/N 4912458-501) PER SRM 53-11, SRM 51-10. 2L72 4F A6WE 19950728004071995072800407NM 1995 7 28 9511316608 119950718A5330 SKIN BOEING747 747151 1384891NM FS 1820-1880 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608US 19785 DURING PERIODIC CHECK, FOUND CORROSION AND DISBONDING IN THE FUSELAGE SKIN DOUBLERS AND TRIPLERS BS 1820 - BS 1840 AND BS 1875 - BS 1880 BELOW THE AFT CARGO DOOR SILL. REPAIRED PER EA 66-98647. 2L74 4F A20WE 19950728004081995072800408NM 1995 7 28 9511326608 119950718A5312 BLKHD FITTING BOEING747 747151 1384891NM FS 1480 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608US 19785 DURING PERIODIC CHECK, FOUND CORROSION AND A CRACK IN THE BS 1480 BULKHEAD OUTER CAP FITTING AT APPROXIMATELY STR 33R. REPAIRED FITTING (P/N 65B10084-2) PER EA 66-98223. 2L74 4F A20WE 19950728004091995072800409NM 1995 7 28 9511336608 119950718A5330 SKIN BOEING747 747151 1384891NM FS 1660-1740 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON THE INTERIOR FUSELAGE SKIN BETWEEN BS 1660 - BS 1740, STR 50L - STR 50R. REPAIRED PER EA 66-32459. 2L74 4F A20WE 19950728004101995072800410WP 1995 7 28 9511349607 119950719A5320 FITTING DOUG DC9 DC932 3022066WP FS 579-585 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 30 END FITTING AT FS 579 - FS 585. REPLACED FITTING (P/N 5920331-1). 2L72 4F A6WE 19950728004111995072800411WP 1995 7 28 9511351143 119950720A5320 WEB DOUG DC10 DC1040 3023508WP FS 495 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01133JC 46752 DURING LINE CHECK, FOUND TWO CRACKS IN THE NOSE LANDING GEAR WHEELWELL VERTICAL PANEL PRESSURE WEB BS 495, LEFT SIDE AT Z-63 AND RIGHT SIDE AT Z-62. REPAIRED PER EA 11-98587. 2L73 4F A22WE 19950728004121995072800412NM 1995 7 28 9511366608 119950720A5312 BLKHD CHORD BOEING747 747151 1384891NM FS 2598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON BS 2598 BULKHEAD LOWER CHORD AND WEB STR 46L - STR 49R. REPAIRED PER EA 66-98657. 2L74 4F A20WE 19950728004131995072800413NE 1995 7 28 9511376719 219950726A7200 ENGINE BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 4 FAILED A ANWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01619US 21321 662485 DURING TAKEOFF, THE NR 4 ENGINE EGT WENT TO 950 DEGREES. WHEN POWER WAS REDUCED TO 1.46 EPR, THE EGT REMAINED AT 950 DEGREES. DURING CRUISE, THE NR 4 EGT READ 60 DEGREES HIGHER THAN THE OTHER ENGINES. THE AIRCRAFT DIVERTED TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E20EA 19950728004141995072800414WP 1995 7 28 95UAL900065 119950727A2560 SLIDE LIGHT DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL DOOR 2L MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291828U 46627 AT DEPARTURE TIME, JETWAY OFF, FLT ATTENDANT ADVISED DOOR 2 LEFT SLIDE PRESS LIGHT WOULD NOT TEST. REINSTALLED BATTERY. OPS CHECKED OK. 2L73 4F4 F A22WE E23EA 19950728004151995072800415WP 1995 7 28 95UAL900066 119950727A3350 EEL DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL DOOR R4 INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291828U 46627 PER CREW EMERG FLASHLIGHT AT DOOR 4, RT RED INDICATOR NOT FLASHING. REPLACED FLASHLIGHT ASSY AND BATTERY PACK. OPS CHECKED OK. 2L73 4F4 F A22WE E23EA 19950728004161995072800416NM 1995 7 28 95UAL900067 119950727A3230 UPLOCK ACT 32399 BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE RT MLG MALFUNCTIONED A UALAK NONE J WARNING INDICATION CLCLIMB 1 WP299013U 19051 AFTER GEAR RETRACTION, RT MAIN GEAR INTRANSIT RED LIGHT REMAINED ON. PLACED GEAR HANDLE OFF AND GEAR FELL OUT. TOOK 3 ATTEMPTS TO GET GEAR TO LOCK UP. REPLACED RT UPLOCK ACTUATOR. OPS CHECKS OK. 2L72 4F4 F A16WE E2EA 19950728004171995072800417NM 1995 7 28 95UAL900068 119950727A3350 EEL INVERTER BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29558UA 26654 EMERGENCY LIGHT INVERTER INOP AT OVERWING LOCATION. REPLACED INVERTER. TESTS OK. 2L72 4F4 FRTA2NM E17NE 19950728004181995072800418WP 1995 7 28 95UAL900069 119950727A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291812U 46611 EEL LIGHTS ARE INTERMITTENT ON LT SIDE, ROWS 9-17. REPLACED DAMAGED FEEDER CABLE AT DOOR 2L. 2L73 4F4 F A22WE E23EA 19950728004191995072800419EU 1995 7 28 95UAL900070 119950727A2710 ACTUATOR LUCAS 1659 AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE LT AILERON LEAKING A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29409UA 462 GREEN HYD SYSTEM QTY INDICATION APPROACHED YELLOW BAND, FLIGHT DIVERTED TO DEN. GEAR EXTENDED MANUALLY, LANDED WITHOUT INCIDENT. REPORTED LT INBOARD AILERON ACTUATOR HAD PIN HOLE HYD LEAK ON TOP OF ACTUATOR. REPLACED ACTUATOR. 2L72 4F RTA28NM E40NE 19950728004201995072800420NM 1995 7 28 95UAL900071 119950727A2120 AIR DIST BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN ODOR A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 WP297452U 21906 FLIGHT ATTENDANT NOTED ODD ODOR AND BECAME SLIGHTLY NAUSEOUS UPON TAKEOFF FROM LAS. NOTED TO LESSER EXTENT, SEVERAL TIMES IN CRUISE. RT PACK OVERTEMP AND TRIP ON GROUND AT ORD. CABIN HAD LT BLUE HAZE AND SLIGHT ODOR. PACK DID RESET AFTER COOLING. RESET PACK, AND OPS CHECKS NORMAL. CHECKED 8TH AND 13TH SADDLE COVERS, FOUND NO EVIDENCE OF OIL. UNABLE TO DUPLICATE FAULT. 2L73 4F4 F A3WE E2EA 19950728004211995072800421SO 1995 7 28 BIER950015 119950727A24604981902 MASTER SWITCH PIPER PA31 PA31350 7103110SO CABIN SHORTED B BIEAK NONE H ELECT. POWER LOSS-50 PC TXTAXI/GRND HDL 1 EA213521S5541 317952107 BATTERY WAS DRAINED DOWN TO 22 VOLTS WITH MASTER ELECTRICAL SWITCH IN OFF POSITION. DETERMINED CAUSE WAS MOISTURE BUILD-UP IN SWITCH CAUSING BATTERY DRAIN. COMPLIED WITH PIPER SL 886 BY INSTALLATION OF SEALED SWITCH. 1L72 3O A20SO 19950728004221995072800422SO 1995 7 28 COM11934 119950726A32463006041 WHEEL BFGOODRICH 314461 EMB 120 EMB120RT SO RT MLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO011228 1107273 1720 120228 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO LOW TIRE PRESSURE. WHEEL SHOP VISUAL INSPECTED WHEEL ASSY AND FOUND WHEEL CRACKED AT BOTTOM OF KEY BOSS APPROXIMATELY 1 INCH LONG. SUBASSY HAS BEEN REMOVED FROM SERVICE. 2L72 4T RTA31SO 19950728004231995072800423SO 1995 7 28 COM11935 119950725A29102025000002 SWIVEL EMB 120 EMB120RT SO LT MLG LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO011117H 120117 HYDRAULIC LEAK, LT MLG REPLACED LEAKING BRAKE SWIVEL FITTING. 2L72 4T RTA31SO 19950728004241995072800424SW 1995 7 28 COM20384 119950726A77122719158007 TQ INDICATOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO0127119111401852 AC701 RIGHT ENGINE DOES NOT ACHIEVE REQUIRED TORQUE FOR TAKEOFF. REPLACED RIGHT TORQUE INDICATOR GAUGE. 1L72 4T A8SW 19950728004251995072800425EA 1995 7 28 COM60525 119950726A2760FE210301 SWITCH CNDAIRCL600 CL6002B19 EA QUADRANT DEFECTIVE A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01941CA1910 7050 INBD GROUND SPOILERS ARE UP WHEN AIRCRAFT POWER IS ON. REPLACED THE POWER QUADRANT CAM SWITCH UNIT. 2L72 4F RTA21EA 19950728004261995072800426EA 1995 7 28 COM60526 119950726A27604916403 SECU CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01938CA2156 7046 FLIGHT SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE SPOILER ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19950728004271995072800427NM 1995 7 28 DL72L953176 119950724A5620 WINDOW PA6556705 BOEING727 727232 1384082NM EMERGENCY EXIT MISSING A ADALAK NONE DC INFLIGHT SEPARATION F.O.D. CRCRUISE 1 SO11505DA 21307 MOMENTARY SHUDDER AT FL 350 IN CRZ. SUSPECT NR 1 ENG COMPRESSOR STALL. CHECKED INLET AND EXHAUST. BORESCOPED NR 1 ENG PER MM. RAN ALL 3 ENGS PER PFHB, OPERATION NORMAL. POST-INSPECTION FOUND THE LEFT SIDE OVERWING AFT EMERGENCY EXIT DOOR WITH THE OUTER PANE OF DOOR WINDOW MISSING. EVIDENCE IS INCONCLUSIVE IF ANY PART OF WINDOW PANE WAS INGESTED. A NEW WINDOW WAS INSTALLED FOR RETURN TO SERVICE. 2L73 4F A3WE 19950728004281995072800428NM 1995 7 28 DL72L953182 119950718A5412 FIREWALL PANEL BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 FOUND ON CV2 CK, NR 2 ENG FIREWALL, NR 1 PANEL CRACKED .75 INCH, LT SIDE OF INLET, AND .50 INCH, RT SIDE OF INLET. REPAIR: REPAIRED PER SRM 54-10-3, FIG. 1. 2L73 4F A3WE 19950728004291995072800429NM 1995 7 28 DL72L953193 119950718A5330 SKIN BOEING727 727232 1384082NM BS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 FOUND ON CV2 CK. CORROSION ON SKIN LAP JOINT OUTBOARD OF STR 26R FROM STA 720C-STA 720F. REPAIR: REPAIRED PER ERA 302175-14. 2L73 4F A3WE 19950728004301995072800430NM 1995 7 28 DL72L953198 119950717A5754 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 FOUND ON CV2 CK, CRACK INBD OF ACTUATOR NR 5 SLAT. REPAIR: REMOVED SLAT PER OPN 7005, PEPAIRED PER MM 57-54-0, FIG 804. 2L73 4F A3WE 19950728004311995072800431NM 1995 7 28 DL72S953177 119950724A5753 SKIN BOEING727 727232 1384082NM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11517DA 21433 FOUND DURING F-1 LETTER CHECK - NR 4 L/E FLAP CRACKED OUTBD HINGE CUTOUT. REPAIRED PER MM 57-53-0 PG 802. 2L73 4F A3WE 19950728004321995072800432NM 1995 7 28 DL72S953186 119950725A5720 BRACKET BOEING727 727232 1384082NM LE WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 ATTACH BRACKET CRACKED - NR 1 L/E FLAP ACTUATOR, LOWER CORNER. FOUND AT LTR CHECK, REPAIRED PE MM 57-20-21. 2L73 4F A3WE 19950728004331995072800433NM 1995 7 28 DL72S953187 119950725A5754 SKIN BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 NR 3 L/E SLAT COVE SKIN LOWER ATTACH ANGLE CRACKED BELOW THERMAL ANTI-ICE (TAI) DUCT. FOUND AT LTR CHECK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950728004341995072800434NM 1995 7 28 DL72S953188 119950725A5754 SKIN BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 NR 7 SLAT DOUBLER CRACKED BELOW I/B STOP PAD. FOUND DURING B-2 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950728004351995072800435NM 1995 7 28 DL72S953189 119950725A5320 WEB BOEING727 727232 1384082NM BS 1213 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 1) 1 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 LT. 2) .50 INCH CRACK UPPER END OF VERTICAL TORQUE BOX WEB ABOVE AIRSTAIR CLOSEOUT PANEL STA 1213 RT. FOUND AT B-2 LTR CK. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950728004361995072800436NM 1995 7 28 DL72S953190 119950725A5730 SKIN BOEING727 727232 1384082NM WS 463 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11416DA 21258 2.25 INCH CRACK IN WING L/E SKIN AT WS 463.0 AFT OF NR 5 SLAT ABOVE REFUELING PANEL. FOUND AT B2 LTR CK. REPAIRED PER MM 57-20-21. 2L73 4F A3WE 19950728004371995072800437NM 1995 7 28 DL757953116 119950719A5754114N4002138 TE WEDGE BOEING757 757232 1384965NM NR 10 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11617DL 22907 T/E WEDGE CRACKED AND DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02, DURING SHOP INSPECTION FOR NR 10 L/E SLAT. 2L72 4F RTA2NM 19950728004381995072800438NM 1995 7 28 DL757953179 119950608A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11614DL 22821 RADOME DAMAGED IN NOSE AREA. ON SHOP INSPECTION, FOUND OLD WETLAY UP AND MOISTURE ABOVE LIMITS 40 PERCENT OF SURFACE AREA. REBUILT RADOME FROM BASE RING UP PER S.R.M. 53-10-72 PAINTED AND TESTED, RETURN SERVICABLE UNIT TO STOCK. 2L72 4F RTA2NM 19950728004391995072800439NM 1995 7 28 DL757953180 119950615A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11674DL 25979 UPON INSPECTION RADOME (DL 13) WAS FOUND TO EXCEED MOISTURE LIMITS AT TOP AND RIGHT SIDES CONTAINING AN AREA OF 20 PERCENT OF RADOME SURFACE. ACCOMPLISHED REPAIRS PER SRM 53-10-72. 2L72 4F RTA2NM 19950728004401995072800440NM 1995 7 28 DL767953201 119950725A5610141T480120 WINDOW BOEING767 767232 1385132NM FLT DECK SHATTERED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11101DA 22213 DURING CRUISE, FIRST OFFICER'S NR 1 WINDSHIELD SHATTERED, LANDED MCO. REPLACED WINDOW AND CONTROLLER, GROUND OPERATION NORMAL. 2L72 4F RTA1NM 19950728004411995072800441NM 1995 7 28 DL76S952252 119950430A5754114T410414SP SKIN BOEING767 767332 1382001NM NR 9 LE SLAT DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11135DL 25145 DURING SHOP INSPECTION, NR 9 L/E SLAT T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE. REPAIRS ACCOMPLISHED PER SMR 57-43-55. 2L72 4F RTA1NM 19950728004421995072800442WP 1995 7 28 DLL10952837 119950614A55211524058110 RIBS 1524058110 LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA DL20 193C1139 DURING HMV, SHOP INSPECTION, RT ELEVATOR WAS FOUND WITH CRACKING IN VERTICAL AND DIAGONAL TRUSS MEMBERS OF ELEVATOR RIBS. REPAIRS WERE ACCOMPLISHED PER L011 SB 093-55-018. 2L73 4F A23WE 19950728004431995072800443WP 1995 7 28 DLL10953200 119950725A33505165741 EEL POWER SUPPLY LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11733DS 193C1224 ON LAYOVER, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP IN FWD CABIN. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19950728004441995072800444WP 1995 7 28 DLL13953183 119950706A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FS 1103 RT SIDE FUSE FRAME ATTACH ANGLE AT FLOOR LEVEL CRACKED ON AFT SIDE OF FRAME THROUGH FASTENER HOLE, FABRICATED REPAIR ANGLE. OK TO INSTALL. REPAIRED PER SRM 53-21-00, PAGES 853-855. 2L73 4F A23WE 19950728004451995072800445WP 1995 7 28 DLL13953184 119950702A5320 SUPPORT LKHEED1011 10113851 5265010WP FS 1463 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FLOOR SUPPORT CORRODED C-2 BB FS 1463 RBL 10 TO RT FIXED FLOOR PANEL. ACCOMPLISHED REPAIRS PER SRM 53-23-00, FIG 801 AND 803. 2L73 4F A23WE 19950728004461995072800446NM 1995 7 28 DLM88951456 119950410A52805914984510N DOOR DOUG MD88 MD88 3023688NM NLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11937DL 49810 DURING SHOP INSPECTION, THE NOSE LANDING GEAR RIGHT AFT DOOR PANEL WAS FOUND WITH DAMAGE TO FWD LOWER CORNER OF DOOR. REPAIRED PER SRM 52-05. 2L72 4F RTA6WE 19950728004471995072800447NM 1995 7 28 DLM88953138 119950721A215020495061 TURBINE DOUG MD88 MD88 3023688NM RT ACM FAILED A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO11965DL 49984 AIRCRAFT WOULD NOT MAINTAIN PRESSURE AT FL 250. DIVERTED TO ATL. REPLACED RIGHT ACM, OPERATION NORMAL. 2L72 4F RTA6WE 19950728004481995072800448NM 1995 7 28 DLM88953181 119950723A36101718566 DUCT DOUG MD88 MD88 3023688NM TAIL COMP LEAKING A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO11963DL 49982 ON INITIAL TAKOFF GOT TAIL COMP TEMP HI LIGHT. PER POM RETURNED ATL. FOUND LEFT ACM AIR OUTLET RUBBER DUCT LEAKING. REPLACED DUCT OPERATION NORMAL. 2L72 4F RTA6WE 19950728004491995072800449NM 1995 7 28 DLM88953185 119950725A2420 GENERATOR 947F9453 DOUG MD88 MD88 3023688NM APU FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11913DE UJ2053B 49956 ON CLIMBOUT, NR 2 ENG GENERATOR ON MCO. APU GENERATOR FAILED COULD NOT RESET. DIVERTED ATL. REPLACED APU GENERATOR CONTROL UNIT AND NR 2 ENGINE CSD. OPERATION NORMAL. 2L72 4F RTA6WE 19950728004501995072800450NM 1995 7 28 DLM88953191 119950725A5320 FRAME DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11904DL 49535 DURING C-2 LTR CK, FOUND LEFT WHEELWELL OUTBOARD FWD FRAME WITH 2 INCH CRACK. ACCOMPLISHED REPAIRS PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950728004511995072800451NM 1995 7 28 DLM88953194 119950725A2820120006650 CIRCUIT BREAKER DOUG MD88 MD88 3023688NM RT AC BUS FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11915DL 49546 AFT CENTER FUEL BOOST PUMP C/B POPPED ON ROTATION. RETURNED TO DFW. A PHASE MISSING AT PUMP C/B. REPLACED RT A/C BUS C/B B1-738. 2L72 4F RTA6WE 19950728004521995072800452NM 1995 7 28 UPS203910 119950727A551065175086 CHORD BOEING727 7271A7C 13840X2NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2. 2L73 4F A3WE 19950728004531995072800453NM 1995 7 28 UPS203911 119950727A551065175085 CHORD BOEING727 7271A7C 13840X2NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601. 2L73 4F A3WE 19950728004541995072800454NM 1995 7 28 UPS203912 119950727A551065195326 CHORD BOEING727 7271A7C 13840X2NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD IS CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601. 2L73 4F A3WE 19950728004551995072800455NM 1995 7 28 UPS203913 119950727A5320 ANGLE BOEING727 7271A7C 13840X2NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND TORQUE BOX I/B CHORD ANGLE AT STA 1342, RBL 13, WL 259 CORRODED. REPAIRED IAW E.O. B727-5530-1237, SRM 51-10-2, 51-10-6. 2L73 4F A3WE 19950728004561995072800456NM 1995 7 28 UPS203914 119950727A551065225512 CHORD BOEING727 7271A7C 13840X2NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND CHORD CORRODED. REPLACED IAW SRM 51-30-2, B727-5530-4601. 2L73 4F A3WE 19950728004571995072800457NM 1995 7 28 UPS203915 119950727A5320 ANGLE BOEING727 7271A7C 13840X2NM FS 1362-1380 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND LT UPPER TORQUE BOX BETWEEN F.S. 1362 - 1380, WL 269 ON HORIZONTAL ANGLE CRACKED. REPAIRED IAW SRM 54-10-2, 51-30-2. 2L73 4F A3WE 19950728004581995072800458NM 1995 7 28 UPS203916 119950727A5320 ANGLE BOEING727 7271A7C 13840X2NM BS 1342 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01935UP 20143 WHILE IN NAPLES, ITALY FOR C-CHECK, MAINTENANCE FOUND TORQUE BOX I/B CHORD AT STA 1342, LBL 13, WL 259 CORRODED ANGLE. REPAIRED IAW E.O. B727-5530-1237, SRM 51-10-6, 51-10-2. 2L73 4F A3WE 19950728004591995072800459WP 1995 7 28 UPS803901 119950723A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01836UP 45936 WHILE ON GROUND, MAINTENANCE FOUND LT AFT SERVICE DOOR CUT OUT HAS AFT UPPER RADIUS CRACKED. REPAIRED IAW DC8-5330-4067A. 2L74 4F RT4A25 19950728004601995072800460WP 1995 7 28 UPS803902 119950724A5720 SLOT DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01852UP 46052 WHILE ON GROUND, MAINTENANCE FOUND LEFT WING INBD SLOT-INBD LWR CORNER HAS A 1 INCH CRACK IN IT. REPAIRED AS PER E.O. DC8-5730-7218A. 2L74 4F RT4A25 19950728004611995072800461WP 1995 7 28 UPS803903 119950726A53203619451 FITTING DOUG DC8 DC871F 302199DWP FS 812 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BELT FRAME END FITTING CRACKED AT F.S. 812, LONGERON 21R. REPAIRED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950728004621995072800462WP 1995 7 28 UPS803904 119950726A5320071202XT3 ANGLE DOUG DC8 DC871F 302199DWP FS 781-812 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 3 EACH CRACKED L-ANGLES LOWER SIDE OF CENTER WING BOX, F.S. 781, RBL AND LBL 69 AND F.S. 812, LBL 69. REPAIRED ANGLES PER SRM 53-2-0. 2L74 4F RT4A25 19950728004631995072800463WP 1995 7 28 UPS803905 119950726A57125770123 RIB DOUG DC8 DC871F 302199DWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT WING LEADING EDGE 7 EACH RIBS CRACKED AT STA XFS 835, XFS 817, XFS 804 LOWER, XFS 823, XFS 804 UPPER, XFS 720, AND XFS 763. REPAIRED RIBS PER MM 57-00-00, FIG 801. 2L74 4F RT4A25 19950728004641995072800464WP 1995 7 28 UPS803906 119950726A57125770123 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING OUTBOARD LEADING EDGE 4 EACH UPPER RIBS CRACKED AT STA XFS 735, XFS 791, XFS 811, AND XFS 817. REPAIRED RIBS PER MM 57-00-00, FIG. 801. 2L74 4F RT4A25 19950728004651995072800465WP 1995 7 28 UPS803907 119950726A57525717798502 TAB DOUG DC8 DC871F 302199DWP RT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT INBOARD AILERON OUTBOARD TAB DELAMINATED. REPLACED TAB ASSY PER T/C CL11R-42. 2L74 4F RT4A25 19950728004661995072800466WP 1995 7 28 UPS803908 119950727A5751 SKIN DOUG DC8 DC871F 302199DWP RT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT I/B AILERON LOWER SKIN CRACKED O/B OF I/B HINGE CUTOUT. REPAIRED IAW SRM 57-2-0. 2L74 4F RT4A25 19950728004671995072800467WP 1995 7 28 UPS803909 119950727A575556551672 SKIN DOUG DC8 DC871F 302199DWP NR 3 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING SPOILER NR 3 DELAMINATED AT LOWER SURFACE. REPLACED IAW M/M 27-61-01. 2L74 4F RT4A25 19950728004681995072800468WP 1995 7 28 UPS803917 119950725A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 WHILE ON GROUND, MAINTENANCE FOUND NR 4 PIT FWD UPPER RADIUS HAS .75 INCH CRACK. FABRICATED DOUBLER AS PER SRM 53-2-1, INSTALLED DOUBLER. 2L74 4F RT4A25 19950804000541995080400054NE 1995 8 4 9511386614 219950726A7230 COMPRESSOR BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 3 ENGINE STALLED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL MR OVER TEMP PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01614US 20359 662472 DURING TAKEOFF ROTATION, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH THE EGT GOING TO MAX AND THE ENGINE WAS SHUTDOWN. DUMPED 100,000 LBS OF FUEL AND THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E20EA 19950804000551995080400055NM 1995 8 4 9511392717 119950726A291310605563 HYD PUMP BOEING727 7272S7 138407ZNM B-HYD SYST FAILED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01721RC362282055 22492 AT FL 300, COMPLETE LOSS OF B-SYSTEM HYDRAULIC FLUID AND PRESSURE OCCURRED. A-SYSTEM HYDRAULIC FLUID DECREASED TO 2.2 GALLONS. DECLARED AN EMERGENCY AND DIVERTED TO ATL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 B-SYSTEM HYDRAULIC PUMP AND ASSOCIATED FILTERS. SERVICED SYSTEM AND LEAK CHECK WAS NORMAL. 2L73 4F A3WE 19950804000561995080400056NM 1995 8 4 9511402286 119950727A2781106081917 SWITCH BOEING727 727251 138408HNM NR 4 LE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01286US 21325 DURING DEPARTURE CLIMB UPON FLAP RETRACTION, THE NR 4 LEADING EDGE FLAP DID NOT INDICATE STOWED. RECYCLED FLAPS TO NO AVAIL, FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 4 LEADING EDGE FLAP INDICATION SWITCH S205 INOPERATIVE. REPLACED SWITCH, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950804000571995080400057NM 1995 8 4 9511412288 119950725A3211659864221 TRUNNION BOEING727 727251 138408HNM LT MLG FAILED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US308849471 21376 DURING PREFLIGHT, FOUND THE LEFT MAIN LANDING GEAR AFT TRUNNION SHEARED. MAINTENANCE REPLACED GEAR, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950804000581995080400058NM 1995 8 4 95UAL900072 119950728A3350 EEL LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE DOOR 2R FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29922UA 26642 DOOR 2R EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED LAMP, OPS CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950804000591995080400059NM 1995 8 4 95UAL900073 119950728A3350 EEL BULB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29360UA 24453 EMERGENCY LIGHT INOP OVER SEAT 11DEF. REPLACED LAMP ASSY. 2L72 4F4 FRTA16WE E2GL 19950804000601995080400060NM 1995 8 4 95UAL900074 119950728A323065B8324848 FLEX HOSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE RT MLG FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29180UA 25224 DEPARTING HKG, RIGHT BODY GEAR WOULD NOT RETRACT, HAD GEAR DOOR, GEAR TILT AND GEAR DISAGREE STATUS MESSAGES. REPLACED TILT ACTUATOR HYDRAULIC HOSE. 2L74 4F4 FRTA20WE E24NE 19950804000611995080400061WP 1995 8 4 MWEA95244 119950726A335060030431 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP FWD CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31401ME 47133 DURING ROUTINE INSPECTION, THE FOUR FWD CEILING EMERGENCY LIGHTS WERE VERY DIM DURING TEST. REPLACED FWD CEILING LIGHT BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950804000621995080400062NM 1995 8 4 P4CA9500598 119950701A5311 STUB FRAME BOEING747 747121 1384871NM BS 1394 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS ON DOUBLER AND STUB FRAME AT BS 1394 BETWEEN RBL 98 AND RBL 125. INSTALLED DOUBLER PER BOING SRM 53-10-22. 2L74 4F A20WE 19950804000631995080400063NM 1995 8 4 P5CA9500541 119950726A2841 FUEL INDICATOR BOEING747 747122 1384872NM NR 3 FUEL TANK INOPERATIVE A P5CAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 WP23851FT 19756 DURING TAXI AFTER LANDING, NR 3 ENGINE FLAMED-OUT. CHECKED NR 3 FUEL TANK WITH STICK AND FOUND NO FUEL IN NR 3 TANK, FUEL QUANITY INDICATOR ON PLACARD. FUELED AIRCRAFT ENGINE, RUN OK. 2L74 4F A20WE 19950804000641995080400064NM 1995 8 4 P5CA9500542 119950728A3260 SWITCH BOEING747 747122 1384872NM NLG DIRTY A P5CAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP23854FT 19754 TOP OF CLIMB, RED GEAR WARNING LIGHT ON FORWARD PANEL ON WITH GEAR HANDLE UP AND NORMAL HYDRAULICS. FEO'S ANNUNCIATOR LIGHT SHOWS NOSE GEAR DOWN AND LOCKED IN PRIMARY AND ALTERNATE. CLEANED SWITCHES, PERFORMED OPERATIONAL CHECK OF NOSE GEAR, SYSTEM CHECKED NORMAL. DEFFERED PRIMARY SWITCH PER MEL. 2L74 4F A20WE 19950804000651995080400065NM 1995 8 4 P5CA9500543 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 1200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S4R AT BS 1200. REMOVED AND TREATED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER BOEING SRM 53-10-01. 2L74 4F A20WE 19950804000661995080400066NM 1995 8 4 P5CA9500544 119950701A5320 TIE CLIP BOEING747 747121 1384871NM BS 1160 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN TIE CLIP AT FRAME BS 1160 AT S4R. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000671995080400067NM 1995 8 4 P5CA9500545 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 1120 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S3R AT FRAME BS 1120. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000681995080400068NM 1995 8 4 P5CA9500546 119950701A5320 TIE CLIP BOEING747 747121 1384871NM BS 1200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN TIE CLIP AT S2L, AT FRAME BS 1200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000691995080400069NM 1995 8 4 P5CA9500547 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 1200 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S4L, AT BS 1200. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000701995080400070NM 1995 8 4 P5CA9500548 119950701A5730 SKIN BOEING747 747121 1384871NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 INNER SKIN DELAMINATION AT OUTBOARD BAY UNDER PANEL LEFT WING OUTBOARD MIN FLAP. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950804000711995080400071NM 1995 8 4 P5CA9500549 119950701A5210 SKIN BOEING747 747121 1384871NM DOOR 1 L CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN 1L DOOR LOWER HINGE CUTOUT SKIN, LOWER FORWARD CORNER. REPAIRED PER BOEING SRM 52-00-02. 2L74 4F A20WE 19950804000721995080400072NM 1995 8 4 P5CA9500550 119950701A5400 BRACKET BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED BRACKET NR 2 PYLON SKIRT RETURN MODULE MOUNTING BRACKET LEFT SIDE. MANUFACTURED NEW PART PER SRM 54-12-02, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950804000731995080400073NM 1995 8 4 P5CA9500551 119950701A5312 BULKHEAD BOEING747 747121 1384871NM BS 2360 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK .25 INCH IN LENGTH ON BS 2360, BULKHEAD SKIN BY S46R. REPAIRED PER BOEING SRM 53-10-04, SB 53-2275 AND 53-10-04. 2L74 4F A20WE 19950804000741995080400074NM 1995 8 4 P5CA9500552 119950701A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 600 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED INTERCOSTAL BS 600 S26R. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950804000751995080400075NM 1995 8 4 P5CA9500553 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 1980 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LIGHT SURFACE CORROSION ON S5R AT BS 1980. REMOVED CORROSION PER BOEING SRM 51-01-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000761995080400076NM 1995 8 4 P5CA9500554 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 980-1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON S35L BETWEEN BS 980 AND 1000. REPAIRED PER BOEING SRM 53-10-03. 2L74 4F A20WE 19950804000771995080400077NM 1995 8 4 P5CA9500555 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 520 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON EDGE S30R AT BS 520. REPAIRED PER BOEING SRM 53-10-03. 2L74 4F A20WE 19950804000781995080400078NM 1995 8 4 P5CA9500556 119950701A5320 ANGLE BOEING747 747121 1384871NM BS 980 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN ANGLE ON BS 980 NEAR S43L. REPAIRED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950804000791995080400079NM 1995 8 4 P5CA9500557 119950701A5730 FAIRING BOEING747 747121 1384871NM RT WING MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FIBERGLASS MISSING ON RIGHT WING REAR TRAIILING EDGE, WS UPPER FAIRING LOWER SURFACE AT UPPER FIXED FAIRING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950804000801995080400080NM 1995 8 4 P5CA9500558 119950701A5400 BRACKET BOEING747 747121 1384871NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 2 CRACKS ON NR 2 PYLON SKIRT FORWARD MOUNTING BRACKET. FABRICATED NEW BRACKET PER BOEING SRM 54-50-02. 2L74 4F A20WE 19950804000811995080400081NM 1995 8 4 P5CA9500559 119950701A5280 DOOR BOEING747 747121 1384871NM LT MLG DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT BODY GEAR INBOARD DOOR AFT SIDE UPPER AREA DAMGED. REPAIRED PER BOEING SRM 52-80-02. 2L74 4F A20WE 19950804000821995080400082NM 1995 8 4 P5CA9500560 119950701A5320 BRACKET BOEING747 747121 1384871NM BS 1600-1620 DEFORMED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DEFORMED BRACKET IN CONNECTION TO ANGLE SUPPORT FLOOR PANEL BETWEEN BS 1600 AND 1620 WL 198. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950804000831995080400083NM 1995 8 4 P5CA9500561 119950701A5280 PANEL BOEING747 747121 1384871NM LT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT BODY GEAR SIDE STRUT DOOR UPPER INSPECTION PANEL ABOVE ROD FITTING CRACKED. REPLACED PANEL INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950804000841995080400084NM 1995 8 4 P5CA9500562 119950701A532065B11442907 ANGLE BOEING747 747121 1384871NM LT MLG WW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SIDE ANGLE CRACKED AT MIDDLE AREA. REPLACED PARTS 65B11442-907, 65B11442-17 AND 65B13398-5. 2L74 4F A20WE 19950804000851995080400085NM 1995 8 4 P5CA9500563 119950701A5280 DOOR BOEING747 747121 1384871NM LT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT BODY INBOARD SIDE STRUT DOOR AFT LOWER CORNER CRACKED AND PARTIALLY TORN. REPAIRED PER BOEING SRM 52-80-02. 2L74 4F A20WE 19950804000861995080400086NM 1995 8 4 P5CA9500564 119950701A5280 DOOR BOEING747 747121 1384871NM LT MLG DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE LEFT BODY GEAR INBOARD SIDE STRUT DOOR AFT SIDE AFT UPPER CORNER. REPAIRED PER BOEING SRM 52-80-02. 2L74 4F A20WE 19950804000871995080400087NM 1995 8 4 P5CA9500565 119950701A5320 ANGLES BOEING747 747121 1384871NM FUSELAGE OVAL HOLES A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 OVAL HOLES FOUND ON 2 ANGLES AND 2 WEBS WHILE MODIFYING PER SB 53-2272 DRAWING 62400003 SHEET 91A. REPLACED PARTS, INSTALLED PER DRAWING 62400003 SHEET 91A. 2L74 4F A20WE 19950804000881995080400088NM 1995 8 4 P5CA9500566 119950701A5320 BOLTS BOEING747 747121 1384871NM BS 100 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION AROUND BOLTS AT BS 100 LBL 6. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000891995080400089NM 1995 8 4 P5CA9500567 119950701A5320 SUPPORT BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON Z-SUPPORT AT BS 1240 BETWEEN LBL 40 AND LBL 80. CORROSION REMOVED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804000901995080400090NM 1995 8 4 P5CA9500568 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 740-760 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN S43R BETWEEN BS 740 AND 760. REPAIRED PER 53-10-03 FIG 1. 2L74 4F A20WE 19950804000911995080400091NM 1995 8 4 P5CA9500569 119950701A5311 FRAME BOEING747 747121 1384871NM NR 5R DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FORWARD FRAME LOWER STOP FITTING AREA ENTRY DOOR NR 5. REPAIRED PER BOEING SRM 51-40-02 FIG 1. 2L74 4F A20WE 19950804000921995080400092NM 1995 8 4 P5CA9500570 119950701A532065B079224 FITTING BOEING747 747121 1384871NM BS 434 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED FITTING PN 65B07922-4, AT NR 1R DOOR BS 434 BETWEEN S23R AND S24R. REPLACED PART, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950804000931995080400093NM 1995 8 4 P5CA9500571 119950701A5753 PANEL BOEING747 747121 1384871NM RT INBD TE FLAP SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SEPARATION, RIGHT WING INBOARD AFT FLAP OUTBOARD CORNER. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950804000941995080400094NM 1995 8 4 P5CA9500572 119950701A5330 PANEL BOEING747 747121 1384871NM BS 1200 SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SEPARATION ON AIR CONDITIONING BAY PANEL, BS 1200 LEFT PANEL ADJACENT TO WING ROOT. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950804000951995080400095NM 1995 8 4 P5CA9500573 119950701A5280 DOOR BOEING747 747121 1384871NM RT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED HOLE AND POPPED RIVET RIGHT BODY GEAR GEAR SHOCK STRUT INBOARD DOOR NEAR CAUTION DECAL. REPAIRED PER BOEING SRM 52-80-02. 2L74 4F A20WE 19950804000961995080400096NM 1995 8 4 P5CA9500574 119950701A5280 DOOR BOEING747 747121 1384871NM RT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SMALL CRACK ON AFT INNER EDGE RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR. REPLACED PART. 2L74 4F A20WE 19950804000971995080400097NM 1995 8 4 P5CA9500575 119950701A5280 DOOR BOEING747 747121 1384871NM RT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR FORWARD EXTERNAL SKIN NEAR FIRST HINGE. REPAIRED PER 52-80-02 FIG 1. 2L74 4F A20WE 19950804000981995080400098NM 1995 8 4 P5CA9500576 119950701A5280 DOOR BOEING747 747121 1384871NM RT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR AFT SIDE HAS 6 IN CRACK AND 2 DAMAGED AREAS. REPLACED SEAL, RIB AND ANGLE, INSTALLED PER SRM 51-30-02. 2L74 4F A20WE 19950804000991995080400099NM 1995 8 4 P5CA9500577 119950701A5280 SKIN BOEING747 747121 1384871NM RT MLG DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE TO CORNER SKIN RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR AFT UPPER END. REPAIRED PER BOEING SRM 52-80-02 FIG 1. 2L74 4F A20WE 19950804001001995080400100NM 1995 8 4 P5CA9500578 119950701A5280 SKIN BOEING747 747121 1384871NM RT MLG DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON RIGHT BODY GEAR SHOCK STRUT INBOARD DOOR. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950804001011995080400101NM 1995 8 4 P5CA9500579 119950701A5280 SKIN BOEING747 747121 1384871NM LT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SMALL CRACK AT AFT END CORNER LEFT BODY GEAR WHEEL WELL INBOARD DOOR SKIN. INSTALLED NEW DOOR SKIN PER SRM 51-30-02. 2L74 4F A20WE 19950804001021995080400102NM 1995 8 4 P5CA9500580 119950701A5280 SKIN BOEING747 747121 1384871NM LT MLG DOOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGED LEFT BODY GEAR WHEEL WELL INBOARD DOOR INNER SKIN OUTBOARD SIDE NEAR DOOR ROD FITTING. INSTALLED NEW DOOR SKIN. 2L74 4F A20WE 19950804001031995080400103NM 1995 8 4 P5CA9500581 119950701A5280 SKIN BOEING747 747121 1384871NM LT MLG CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BULGES ALONG SEAM LEFT BODY GEAR WHEEL WELL INBOARD DOOR EXTERNAL SKIN. REMOVED RIVETS, REMOVED CORROSION PER BOEING SRM 51-10-01, TREATED PER 51-10-02, INSTALLED PER SRM 51-30-01. 2L74 4F A20WE 19950804001041995080400104NM 1995 8 4 P5CA9500582 119950701A5280 DOOR BOEING747 747121 1384871NM NLG DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGED FORWARD NOSE GEAR RIGHT DOOR LOWER EDGE. REPAIRED PER SRM 52-80-02. 2L74 4F A20WE 19950804001051995080400105NM 1995 8 4 P5CA9500583 119950701A5753 PANEL BOEING747 747121 1384871NM RT TE FLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 HONEY COMB SEPARATION AND DRILLED HOLES AT INTERNAL SIDE RIGHT WING OUTBOARD AFT FLAP UPPER PANEL. REPAIRED PER BOEING SRM 51-40 06. 2L74 4F A20WE 19950804001061995080400106NM 1995 8 4 P5CA9500584 119950701A5754 FITTING BOEING747 747121 1384871NM RT LE FLAP CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN BOTH HINGES FITTING SIDES RIGHT WING KRUGER LEADING EDGE FLAP NR 15. MANUFACTURED PLATE SUPPORT PER 51-20-01, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950804001071995080400107NM 1995 8 4 P5CA9500585 119950701A5712 RIB BOEING747 747121 1384871NM WS 950 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON LEFT WING LEADING CAVITY WS 950 FORGED RIB AFT UPPER CHORD. REPAIRED PER BOEING SRM 57-20-03. 2L74 4F A20WE 19950804001081995080400108NM 1995 8 4 P5CA9500586 119950701A5280 SEAL BOEING747 747121 1384871NM RT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN RIGHT BODY GEAR SHOCK STRUT OUTBOARD DOOR LOWER EDGE. INSTALLED NEW SEAL AND FASTENERS. 2L74 4F A20WE 19950804001091995080400109NM 1995 8 4 P5CA9500587 119950701A5320 WEB BOEING747 747121 1384871NM BS 1480 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN THE SUPPORTING WEB NR 294C BS 1480 RIGHT. REPAIRED PER 51-40-09. 2L74 4F A20WE 19950804001101995080400110NM 1995 8 4 P5CA9500588 119950701A5720 BRACKET BOEING747 747121 1384871NM LT WING TE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN SUPPORT BRACKET LEFT WING TRAILING EDGE. MANUFACTURED AND REPLACED BRACKET PER BOEING SRM 51-20-01. 2L74 4F A20WE 19950804001111995080400111NM 1995 8 4 P5CA9500589 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON S45R BS 1960 RIGHT SIDE LOWER. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950804001121995080400112NM 1995 8 4 P5CA9500590 119950701A5312 BLKHD PANEL BOEING747 747121 1384871NM BS 1241 PATCH PEELING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FIBERGLASS PANEL PATCH IS PEELING OFF ON BS 1241 LOWER CANTED BULKHEAD. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950804001131995080400113NM 1995 8 4 P5CA9500591 119950701A5720 STIFFENER BOEING747 747121 1384871NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN THE LEFT SIDE TRAILING EDGE STIFFENER, SEAL RIB ASSY LOWER, SRM 57-20-02 FIG 2 INTE 1. REPAIRED PER SRM 51-40-04. 2L74 4F A20WE 19950804001141995080400114NM 1995 8 4 P5CA9500592 119950701A5210 STIFFENER BOEING747 747121 1384871NM NR 2R DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED STIFFENER AT AFT SIDE MAIN DECK ENTRY DOOR 2R CUTOUT LOWER. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950804001151995080400115NM 1995 8 4 P5CA9500593 119950701A5320 WEB BOEING747 747121 1384871NM BS 700 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS FORWARD CARGO BS 700 BETWEEN RBL 45 AND RBL 58 ON WEB. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950804001161995080400116NM 1995 8 4 P5CA9500594 119950701A5720 WEB BOEING747 747121 1384871NM WS 620 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AT AFT AUXILIARY SPAR WEB AT WS 620 AT LOWER SIDE OF STIFFENER. MANUFACTURED NEW PART PER BOEING SRM 57-20-02. 2L74 4F A20WE 19950804001171995080400117NM 1995 8 4 P5CA9500595 119950701A5753 SKIN BOEING747 747121 1384871NM RT TE FOREFLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DELAMINATION RIGHT INBOARD FOREFLAP LOWER SURFACE NEAR INBOARD LINK, MID LINK AND INBOARD ARM. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950804001181995080400118NM 1995 8 4 P5CA9500596 119950701A5321 FLOOR BOEING747 747121 1384871NM BS 1280-1490 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FLOOR BS 1280 TO 1300 LBL 7 TO 14 AND BS 1416 TO 1419 LBL 2 TO 14. REPAIRED PER BOEING SRM 53-10-07. 2L74 4F A20WE 19950804001191995080400119NM 1995 8 4 P5CA9500597 119950701A5400 CHORD BOEING747 747121 1384871NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 EDDY CURRENT INSPECTION PER SB 54-2159, FOUND CRACK IN NR 4 PYLON HORIZONTAL CHORD LEFT SIDE. REAMED HOLE, INSTALLED FREEZE PLUG PER BOEING SB 54-2159, CRACK CLEANED UP. 2L74 4F A20WE 19950804001201995080400120NM 1995 8 4 P5CA9500599 119950701A5313 STRINGER BOEING747 747121 1384871NM BS 2368 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON SIDE OF S46L BS 2368. REPAIRED PER BOEING SRM 53-10-03 FIG 2. 2L74 4F A20WE 19950804001211995080400121NM 1995 8 4 P5CA9500600 119950701A5321 FLOOR BOEING747 747121 1384871NM BS 1660-1680 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TEAR IN FLOOR SKIN BETWEEN BS 1660 AND 1680 LBL 25. MANUFACTURED NEW PART PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950804001221995080400122EU 1995 8 4 QXEA9500225 119950726A3350FDBA56120SNK EEL PLUG FOKKER FOKKERF28 F28MK1000 4990808EU CABIN LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09464US 11063 BOI - EMERGENCY EXIT LIGHT AT 8 A/B INOP. CANNON PLUG RECONNECTED TO POWER SUPPLY AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950804001231995080400123NE 1995 8 4 SWAA950554 219950725A7321 MEC BOEING737 737317 138447PNM GE CFM56 CFM563B1 13802NE NR 2 ENGINE MALFUNCTIONED A SWAAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SW07693AA 23174 AT 35,000 FT, CREW EXPERIENCED NUMBER 2 ENGINE FLAME-OUT. SUCCESSFULLY RESTARTED ENGINE AT 15,000 FT. AIRCRAFT DIVERTED TO ELP AND MADE A NORMAL LANDING. TROUBLESHOT AND BORESCOPED ENGINE, NO DEFECTS NOTED. REPLACED ENGINE FUEL SHUTOFF VALVE, ENGINE MEC AND FUEL PUMP. CHECKED START LEVER SWICTH, CDP LINE AND ALL LINES ON ENGINE. FUEL S/O VALVE: P/N 61163, S/N 128 MEC: P/N 8063208, S/N 60 FUEL PUMP P/N 7086002, S/N 18348. 2L72 4F4 FRTA16WE E2GL 19950804002201995080400220EU 1995 8 4 ERAA9524 119950302A5230112123116 SUPPORT BOLKMS105 BO105S 5626006EU REAR DOOR WONT STOW A ERAAK NONE O OTHER ININSP/MAINT 1 AL03SPARE DOOR SUPPORT WILL NOT STOW PROPERLY, WITHOUT UNREASONABLY BENDING DZUS END. 1G72 3U H3EU 19950804002211995080400221GL 1995 8 4 ERAA9527 219950303A725023038218 NOZZLE VANE 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 1ST STAGE CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03132EH543 543 CAT25334 597 1ST STAGE NOZZLE TRAILING EDGE VANES CRACKED. 1G72 3U3 U H3EU E4CE 19950804002221995080400222GL 1995 8 4 ERAA9528 219950309A725023038218 NOZZLE 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 1ST STAGE CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03131EH334 334 CAT36322 595 TWO ADJACENT CRACKS (AS MARKED) IN VANE 1/4" (6MM) REF PAGE 3-282 TABLE 111-13 ITEM 1 RETURNING NOZZLE 1G72 3U3 U H3EU E4CE 19950804002231995080400223SW 1995 8 4 ERAA9536 119950320A6220412310400107 BEARING 412010406115BELL 412 412 1182202SW M/R WORN A ERAAK NONE O OTHER ININSP/MAINT 1 AL03414EH555 555 A981A1052 33007 BEARINGS ARE WORN BEYOND LIMITS AND UNABLE TO TRACK. 1G72 4U H4SW 19950804002241995080400224GL 1995 8 4 ERAA9578 219950605A7250A6870832 COUPLING BOLKMS105 BO105A EU ALLSN 250C 250C20B 03013GL ENG N2 DEFECTIVE A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03298EH S845 SHAFT UNDERCUT DIMENSIONS; SHAFT INDENTIONS BETWEEN SEAL GROOVES AND BELOW SPLINE END (NOT SCALLOPED END) OD OF SHAFT AT THESE POINTS DIFFER. 1.093" AND 1.104". 1G72 3U3 U H3EU E4CE 19950804002251995080400225GL 1995 8 4 ERAA9579 219950605A7250A6870832 COUPLING BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG N2 DEFECTIVE A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03124EH S559 SHAFT INDENTIONS BETWEEN SEAL GROOVES AND BELOW SPLINE END (NOT SCALLOPED END) - OD OF SHAFT AT THESE POINTS DIFFER. 1.093" AND 1.104". 1G72 3U3 U H3EU E4CE 19950804002261995080400226GL 1995 8 4 ERAA9580 219950605A7250A23038218C505 NOZZLE 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 1ST STAGE CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03427EH454 CAT40423 S554 LOW POWER, VANES CRACKED BEYOND LIMITS, VANES COLLAPSING IN MIDDLE OF VANE. (NOTE: SUPERIOR TURBINE SERVICE LETTER T94-022.) 1G72 3U3 U H3EU E4CE 19950804002271995080400227GL 1995 8 4 ERAA9581 219950606A72506870813 VANE ASSY BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL DIFFUSER STUD BROKE A ERAAK NONE O OTHER ININSP/MAINT 1 AL03297EH S835 DIFFUSSER VANE WAS SENT IN FOR REPAIR BY DALLAS AIRMOTIVE ON ERA POG105627, D/AIRMOTIVE W/O C67418 7/19/94. STUD BROKE AT 30 IN LBS. SEVERAL OTHER STUDS APPEAR TO HAVE WEAK MOLDS. 1G72 3U3 U H3EU E4CE 19950804002281995080400228GL 1995 8 4 ERAA9582 219950606A72506851531 NOZZLE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 4TH STAGE DEFECTIVE A ERAAK NONE O OTHER ININSP/MAINT 1 AL03124EH 559 NOZZLE WAS SENT TO DALLAS AIRMOTIVE FOR OVERHAUL ON ERA P.O. G108745 , D/AIRMOTIVE W/O C67772 . PART HAS -0- HRS TSO AND .007 -.009 SEAL RUNOUT ALL TANG LOCATIONS, WITH NOZZLE IN FIXTURE OR PT SUPPORT. 1G72 3U3 U H3EU E4CE 19950804002291995080400229GL 1995 8 4 ERAA9585 219950609A72616888547 SUMP COVER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG LEAK A ERAAK NONE K FLUID LOSS ININSP/MAINT 1 AL03298EH94 94 S845 PIT ON SMALL O-RING SEAL AREA; OIL LEAK. 1G72 3U3 U H3EU E4CE 19950804002301995080400230GL 1995 8 4 ERAA9586 219950609A7250A6898764 BELLOWS SEAL BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENGINE GROOVED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03298EH94 94 S845 SEAL HAS 93.6 HOURS T.T.. SEAL HAS GROOVES ON CONTACT FACE OF CARBON SEAL. 1G72 3U3 U H3EU E4CE 19950804002311995080400231GL 1995 8 4 ERAA9589 219950614A72506851531 NOZZLE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 4TH STAGE DELAMINATED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03124EH 559 SENT TO D/AIRMOTIVE ON ERA P.O. G108376 FOR OVERHAUL ON D/A WORK ORDER C67743 4/24/95. NOZZLE HAS -0- T.S.O. AND PORTION OF METALIZED AREA OF #4 BLADE TIP PATH DELAMINATED DURING MACHINING. 1G72 3U3 U H3EU E4CE 19950804002681995080400268EU 1995 8 4 9511423225 219950725A7200 ENGINE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CLCLIMB 1 GL01325US 281 731580 DURING CLIMB, THE NR 1 ENGINE EGT REACHED TEMPERATURE OF 935 DEGREES CELSIUS AND STAYED THERE FOR 2 TO 4 SECONDS. THRUST WAS REDUCED AND EGT DROPPED TO YELLOW ZONE BEFORE AGAIN CLIMBING TO RED ZONE FOR 5 SECONDS. THRUST LEVER WAS THEN REDUCED TO IDLE AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO DTW WHERE AN UNEVENTFUL LANDING TOOK PLACE. THEN ENGINE WAS CHANGED AND THE AIRCRAFT WAS DEEMED OK FOR SERVICE. POWERPLANT SERIAL NR 731440 CHANGED TO 731580. 2L72 4F4 FRTA28NM 19950804002691995080400269NE 1995 8 4 9511439925 219950727A7261 OIL FILTER DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 2 ENGINE DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01925US 47472 656868 THE NR 2 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED THE MAIN OIL FILTER TO INSPECT FOR ABNORMAL DEBRIS, NONE FOUND. A NEW OIL FILTER WAS INSTALLED. DURING SUBSEQUENT RUNUP, SYSTEM OPERATION WAS NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950804002701995080400270WP 1995 8 4 9511449152 119950726A7931 OIL PRESS SW DOUG DC9 DC914 3022034WP PWA JT8 JT8D7 52053NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL019811E 45825 657550 THE NR 2 ENGINE FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE DIFFERENTIAL SWITCH AND OIL FILTER. THE REMOVED OIL FILTER WAS INSPECTED FOR CONTAMINANTS, NONE FOUND. DURING RUNUP, THE SYSTEM OPERATION RETURNED TO NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950804002711995080400271NE 1995 8 4 9511459869 219950725A7230 COMPRESSOR DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01778NC 48100 696709 THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE ENGINE. SUBSEQUENT RUNUP AND TEST WERE SATISFACTORY. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950804002721995080400272WP 1995 8 4 9511469160 119950725A5320 FITTING DOUG DC9 DC914 3022034WP FS 642 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND CRACKS IN THE FS 642 RIGHT INBOARD AND OUTBOARD KEEL FITTINGS. REPLACED FITTINGS PER SRM 51-30-1, 51-30-5. 2L72 4F A6WE 19950804002731995080400273WP 1995 8 4 9511479160 119950725A5320 FITTING DOUG DC9 DC914 3022034WP FS 642 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND CORROSION ON THE FS 642 LEFT INBOARD AND OUTBOARD KEEL FITTINGS. REPLACED FITTINGS PER SRM 51-30-1, 51-30-5. 2L72 4F A6WE 19950804002741995080400274WP 1995 8 4 9511489607 119950725A5320 FITTING DOUG DC9 DC932 3022066WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 29L TIE FITTING AT FS 604. REPLACED FITTING (P/N 5920332-1) PER SRM 51-10. 2L72 4F A6WE 19950804002751995080400275NM 1995 8 4 9511492295 119950728A2840 FUEL QTY IND SYS BOEING727 727251 138408HNM NR 2 MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01295US 21506 DURING CLIMBOUT, THE NR 2 FUEL QUANTITY INDICATION DECREASED TO 3,500 LBS FROM 9,000 LBS. DURING RETURN TO BOI, INDICATION RETURNED TO PROPER READING. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED NR 2 FQIS PER MEL 28-11A. 2L73 4F A3WE 19950804002761995080400276SO 1995 8 4 COM11936 119950727A612030005000026 TQ SIG COND EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01205CA13077751 120205 LEFT TORQUE INDICATION ERRATIC. LEFT PROPELLER AUTOFEATHERED. REPLACED THE TORQUE SIGNAL CONDITIONER. 2L72 4T RTA31SO 19950804002771995080400277EU 1995 8 4 COM31125 119950728A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU LT MLG SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01320CA10184371 340A064 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING CLEANING AND VISUAL INSPECTION FOUND INNER RACE HAD SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR OR REPLACEMENT. 2L72 4T RTA52EU 19950804002781995080400278EA 1995 8 4 COM60527 119950724A3150664806 PSEU CNDAIRCL600 CL6002B19 EA COCKPIT FALSE WARNING A COMAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SO01929CA3666 460 7035 INBD ANTI-SKID MESSAGE AND PROXIMITY SYSTEM FAULT MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19950804002791995080400279EA 1995 8 4 COM60528 119950725A3241428853 CONTROL BOX CNDAIRCL600 CL6002B19 EA ANTISKID SYST DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01929CA 7035 ANTI-SKID SYSTEM FAIL, CIRCUIT BREAKER TRIPPED. REPLACED ANTI-SKID CONTROL BOX. 2L72 4F RTA21EA 19950804002801995080400280NM 1995 8 4 DL72K953212 119950726A3350900835A EEL BATTERY BOEING727 727232 1384082NM RT OVERWING DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11410DA 21222 ON LAYOVER HAD RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950804002811995080400281NM 1995 8 4 DL72K953216 119950728A5754 ANGLES BOEING727 727232 1384082NM NR 2/3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 000000 CRACK ON SUPPORT ANGLE ON NR 3 SLAT BELOW TAI DUCT. CRACK BELOW I/B STOP PAD ON NR 2 SLAT. FOUND AT B-1 LTR CHECK, REPAIRED PER MMM 57-54-0. 2L73 4F A3WE 19950804002821995080400282NM 1995 8 4 DL72K953217 119950728A5754 ANGLE BOEING727 727232 1384082NM NR 7/8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 000000 CRACK ON ANGLE NR 7 LE SLAT BELOW ANTI-ICE TUBE. CRACK ON ANGLE BELOW INBD STOP PAD NR 8 SLAT. FOUND AT B-1 LETTER CK, REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950804002831995080400283NM 1995 8 4 DL72L953205 119950705A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 000000 DURING ROUTINE INSPECTION, NR 7865 WAS WRITTEN FOR A DENT IN LT OUTBOARD AILERON UPPER SKIN. DENT WAS REPAIRED PER SRM 57-50-5. 2L73 4F A3WE 19950804002841995080400284NM 1995 8 4 DL72S953195 119950726A2780 ACT BRACKET BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 A .75 INCH CRACK AT NR 3 L/E FLAP ACTUATOR MOUNT BRACKET. FOUND AT B-2 LTR CHECK, REPAIRED PER MM 57-20-21. 2L73 4F A3WE 19950804002851995080400285NM 1995 8 4 DL72S953196 119950726A5754 ANGLE BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 A .25 INCH CRACK COVE SKIN ATTACH ANGLE UNDER ANTI-ICE DUCT AT NR 8 SLAT. FOUND AT B-2 LTR CHECK, REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19950804002861995080400286NM 1995 8 4 DL72S953197 119950726A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11421DA 21274 CRACK UNDER NR 3 SLAT I/B STOP PAD. FOUND AT B-2 LTR CHECK, REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950804002871995080400287NM 1995 8 4 DL72S953206 119950727A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11526DA 21586 000000 CRACK UNDER NR 3 SLAT I/B PAD. FOUND AT D-2 LTR CHECK, REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950804002881995080400288NM 1995 8 4 DL72S953207 119950727A5754 ANGLE BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11526DA 21586 000000 NR 8 SLAT O/B STOP PAD ATTACH ANGLE IS CRACKED PAST PREVIOUS STOP DRILL. FOUND AT D-2 LTR CHECK, REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950804002891995080400289NM 1995 8 4 DL72S953219 119950719A2780 ANGLE BOEING727 727232 1384082NM NR 5 SLAT ACT STOP DRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 000000 NR 5 SLAT ACTUATOR SUPPORT ANGLE ON O/B SIDE HAS CRACK STOP DRILLED. INSTALLED DOUBLER PER M/M 57-54-0 PG 805. 2L73 4F A3WE 19950804002901995080400290NM 1995 8 4 DL72S953223 119950721A7110 INLET BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 TEMP REPAIR OF .8750 INCH CRACK IN NR 2 ENG INLET. REPAIR LOCATED AT 12:20 JUST AFT OF FWD INLET. INSTALLED PERMANENT REPAIR PER MM 54-30-0 PG 801 TO 802. 2L73 4F A3WE 19950804002911995080400291NM 1995 8 4 DL72S953224 119950729A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NR 3 L/E SLAT OB RIB CRACKED AT OB TRACK. ROUTED OUT CRACK AND FABRICATED DOUBLER PER MM 57-54-0 FIG 811. INSTALLED DOUBLER PER MM 57-40-0 FIG 811. 2L73 4F A3WE 19950804002921995080400292NM 1995 8 4 DL72W953202 119950724A5313 STRINGER BOEING727 727247 138408FNM BS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 STRINGER CRACKED, STRINGER 15L BETWEEN STA 720B AND 720C, AFT SIDE OF LIGHT ASSEMBLY. REPAIRED PER SRM 53-10-3, FOUND AT HMV. 2L73 4F A3WE 19950804002931995080400293NM 1995 8 4 DL72W953208 119950727A5754 STIFFNER BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112821W 21059 000000 I/B SPAR STIFFENER CRACKED LWR END AT NR 7 SLAT I/B TRACK. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21 PG 813. 2L73 4F A3WE 19950804002941995080400294NM 1995 8 4 DL72W953214 119950723A5522 TE SKIN BOEING727 727247 138408FNM RT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 000000 RT ELEVATOR LIGHTNING DAMAGE ON O/B CORNER T/E. REPAIRED PER MM 55-20-0 PG 801, FOUND AT HMV. 2L73 4F A3WE 19950804002951995080400295NM 1995 8 4 DL72W953215 119950723A5522 SKIN BOEING727 727247 138408FNM RH ELEV GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 000000 RT ELEVATOR GOUGED, .52 BY .1250 BY .040 ON LWR L/E, 2.5 FT I/B OF OB HINGE. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV. 2L73 4F A3WE 19950804002961995080400296NM 1995 8 4 DL72W953218 119950728A5522 SKIN BOEING727 727247 138408FNM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 000000 RT ELEVATOR HAS 2.5 INCH CRACK AT LWR RT SKIN I/B SIDE. FOUND DURING A-1 LETTER CHECK, REPAIRED PER SRM 55-20-3 PG 9. 2L73 4F A3WE 19950804002971995080400297NM 1995 8 4 DL757953213 119950725A3350 EEL WIRE BOEING757 757232 1384965NM CABIN LOOSE WIRE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11671DN 25332 ON PREFLIGHT, FWD CABIN FLOOR TRACK EMERGENCY LIGHTS ARE INOP. FOUND LOOSE WIRES IN TRACK AT SEAT ROWS 1 TO 2. REPAIRED WIRES, OPERATION NORMAL. 2L72 4F RTA2NM 19950804002981995080400298NM 1995 8 4 DL76L953235 119950729A3830899156612 SENSOR 401900045 BOEING767 767332 1382001NM MID LAVATORIES FAILED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11173DN 1034 24800 AFTER DEPARTING JFK HAD LAV SENSOR FOUL LIGHT WITH F/C RT AFT AND FWD MID LAVATORIES INOP, RETURNED JFK. REPLACED CONTROL MODULE AND SENSORS, OPERATION NORMAL. 2L72 4F RTA1NM 19950804002991995080400299WP 1995 8 4 DLL10953230 119950729A335020131A EEL BATTERY PACK LKHEED1011 10113851 5265010WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11733DS 193C1224 DURING LAYOVER, EMERGENCY LIGHT INOP FWD CABIN RT SIDE. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A23WE 19950804003001995080400300WP 1995 8 4 DLL10953231 119950728A3350RPS1 EEL PWR SUPPLY LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11717DA 193C1096 ON LAYOVER, EMERGENCY TRACK LIGHTS INOP IN D-ZONE. REPLACED POWER SUPPLY AND REPAIRED SHORT IN WIRING AT TRACK BETWEEN R3 AND L3, OPERATION NORMAL. 2L73 4F A23WE 19950804003011995080400301WP 1995 8 4 DLL10953232 119950727A21507339347 PACK LKHEED1011 10113851 5265010WP NR 1 FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO111734D 193C1225 AFTER TAKEOFF, WHEN PACKS TURNED ON THERE WAS A LOUD GRINDING NOISE PLUS SMOKE AND FUMES IN COCKPIT AND CABIN. TURNED OFF NR 1 PACK SMOKE AND FUMES DISSIPATED. NR 1 PACK WAS REPLACED, OPERATION NORMAL. 2L73 4F A23WE 19950804003021995080400302WP 1995 8 4 DLL13953210 119950706A5743 ACT FITTING LKHEED1011 10113851 5265010WP MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 000000 AT HMV, FOUND FITTING CORRODED MLG RETRACT ACT. REAMED HOLES, SPOTFACED AND BLENDED AROUND HOLES. HFEC OF AREA OK. MFG AND PAINTED SHIMS, INSTALLED BUSHINGS PER ERA 271436-14, C/W SRM 57-14-00 FIG 805. 2L73 4F A23WE 19950804003031995080400303WP 1995 8 4 DLL13953211 119950706A5743 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 000000 AT HMV, FOUND FITTING ON MLG RETRACT ACT CORRODED. REAMED HOLES AND BURNISHED AREA. HEFC OF AREA GOOD. MFG AND PAINTED SHIMS, INSTALLED BUSHINGS C/W ERA 271436-14. WORK DONE PER SRM 57-14-00. 2L73 4F A23WE 19950804003041995080400304WP 1995 8 4 DLL13953220 119950727A5744 FITTING LKHEED1011 10113851 5265010WP RT OUTBD AILERONHOLES WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11787DL 193A1126 000000 O/B AILERON, O/B DAMPNER FITTING, HOLES FOR BUSHINGS ARE WORN. FOUND AT D-LETTER CHECK, REPAIRED PER SRM 57-55-00 FIG 808. 2L73 4F A23WE 19950804003051995080400305WP 1995 8 4 DLL16953204 119950727A29101549446105 LINE LKHEED1011 10113853 5265020WP NR 2 ENGINE FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11762DA 193Y1210 000000 A/C DIVERTED INTO JFK WITH C-HYD SYSTEM FAILURE. FOUND LEAKING PRESSURE LINE NR 2 ENG HYD PRESS FILTER IPC, REF 29-11-53 FIG 1 PG 0 ITEM NR 95. INSTALLED NEW LINE AND AS PRECAUTION REPLACED PUMP AND FILTER, OPERATION NORMAL. 2L73 4F A23WE 19950804003061995080400306NM 1995 8 4 DLM88953209 119950728A3320MS3126F1415P CONNECTOR DOUG MD88 MD88 3023688NM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11964DL 49983 000000 WHILE A/C LOCATED GATE A-11 ATL AT 0530 SMELLED SMOKE AND LIGHTING EXTINGUISHED RT SIDE OF CABIN. FOUND CANNON PLUG ROW 17DE BURNT AT OVHD LIGHT AND CEILING PANEL CHARRED. CANNON PULG P1-21-1 AND RECEPTACLE R-12105 WERE REPLACED, OPERATION NORMAL. PLUG AND RECEPTACLE MFG P/N MS3126F1415P AND M3124E14-15S. 2L72 4F RTA6WE 19950804003071995080400307NE 1995 8 4 P5CA9500601 219950729A7230JT9D7A COMPRESSOR BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE STALLED A P5CAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 WP23850FT5431166 19755 662751 NR 3 ENGINE EXPERIENCED AUDIBLE STALL AT TOP OF DESCENT INTO ANC. N1 AND N2 INDICATORS DROPPED WITH STEADY RISE IN EGT SHUTDOWN ENGINE AT 750 DEGREES. RELIGHT OF ENGINE NORMAL ENGINE PERFORMED NORMAL FOR THE REST OF FLIGHT. INSPECTED ENGINE PER MAINTENANCE MANUAL NO ITEMS FOUND OUT OF LIMITS, AIRCRAFT RELEASED. 2L74 4F4 F A20WE E20EA 19950804003081995080400308NE 1995 8 4 P5CA9500602 219950729A7320 CONNECTOR BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CONTAMINATED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23851FT 19756 662231 HUNG START ENGINE NR 2. CLEANED AND SECURED CANNON PLUG ON FUEL CONDITION ACTUATOR, SUBSEQUENT ENGINE STARTS NORMAL. 2L74 4F4 F A20WE E20EA 19950804003091995080400309NE 1995 8 4 P5CA9500603 219950729A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 MALFUNCTIONED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23851FT 19756 662231 AFTER PUSHBACK UNABLE TO START NR 2 ENGINE. SHUTDOWN OTHER OPERATING ENGINES, INSPECTED INSTALLATION OF START VALVE AND FUEL CONDITION ACTUATOR, ALL FOUND NORMAL. START ATTEMPT AT GATE WAS NORMAL. 2L74 4F4 F A20WE E20EA 19950804003101995080400310WP 1995 8 4 QXEA9500191 219950622A72003103051 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NR 1 FAILED A QXEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 NM0926952 AC661 P44305 FCA - NR 1 ENGINE FLAMED-OUT INFLIGHT. AIRCRAFT LANDED IN FCA WITHOUT FURTHER PROBLEM. ENGINE REPLACED IAW MAINT MANUAL. ENGINE GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19950804003111995080400311NM 1995 8 4 UPS 403951 119950729A3350 EEL BULB BOEING747 747123F NM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 WHILE ON GROUND, MAINTENANCE CREW FOUND FWD LWR ENTRANCE DOOR AFT EMER LAMP OUT. RELAMPED, OPS CK NORMAL. 2L74 4F A20WE 19950804003121995080400312WP 1995 8 4 UPS 803921 119950726A2612 FIRE DETECTOR DOUG DC8 DC873F 302199FWP NR 1 ENGINE MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01840UP 46140 WHILE IN CRUISE, NR 1 ENG FIRE DETECTOR SHORT CIRCUIT LIGHT CAME ON MOMENTARILY. ALL OTHER ENGINE INSTRUMENTS NORMAL, OPS CHECKED, FIRE WARNING SYSTEM IAW ED DC8-2610-1268. GROUND RAN AIRCRAFT, SYS CHECKED GOOD. OK FOR SERVICE. 2L74 4F RT4A25 19950804003131995080400313WP 1995 8 4 UPS 803922 119950731A53200717075T1 FITTING DOUG DC8 DC871F 302199DWP FS 420 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, BELT FRAME END FITTING CRACKED AT FS 420 FWD SIDE, LONGERSON 21L LOWER. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003141995080400314WP 1995 8 4 UPS 803923 119950731A53139755803 LONGERON DOUG DC8 DC871F 302199DWP FS 1140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 21L HAS 3 CRACK AT RADIUS FS 1140. REPAIRED LONGERON PER SRM 53-2-5. 2L74 4F RT4A25 19950804003151995080400315WP 1995 8 4 UPS 803924 119950731A57534653423 FITTING DOUG DC8 DC871F 302199DWP RT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, RT FLAP STA 98 FITTING ON INBD SIDE HAS A 1 INCH CRACK. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003161995080400316WP 1995 8 4 UPS 803925 119950731A53200502024T3 JAMB DOUG DC8 DC871F 302199DWP FS 1360 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, X-RAY REVEALS 1 CRACK IN RT T3 DOOR UPPER AFT CORNER FS 1360, UPPER AFT RADIUS OF DOOR JAMB. REPAIRED JAMB PER SRM 53-2-0. 2L74 4F RT4A25 19950804003171995080400317WP 1995 8 4 UPS 803926 119950731A53200327075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 1350 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, FINGER DOUBLER CRACKED AT FS 1350 LONGERON 32R. REPLACED FINGER DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003181995080400318WP 1995 8 4 UPS 803927 119950731A53139754913 LONGERON DOUG DC8 DC871F 302199DWP FS 390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERSON 34R HAS 4 INCH CRACK INBD SIDE FS 390 AND A 15 INCH CRACK FS 200 TO 250. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003191995080400319WP 1995 8 4 UPS 803928 119950731A53139754913 LONGERON DOUG DC8 DC871F 302199DWP FS 190-390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 35L TWO CRACKS, 28 INCHES LONG OUTBD SIDE AND 18 INCHES ON INBD SIDE, FS 190 TO 390. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003201995080400320WP 1995 8 4 UPS 803929 119950731A53139754913 LONGERON DOUG DC8 DC871F 302199DWP FS 340-360 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 36 RT SECTION CRACKED FS 240 TO 360 AND LT SIDE FS 340 TO 360. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003211995080400321WP 1995 8 4 UPS 803930 119950731A53215612298343 SUBFLOOR DOUG DC8 DC871F 302199DWP FS 16 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, COCKPIT SUBFLOOR WEB CORROSION REMOVAL OUT OF LIMITS, FS 16 LBL 48. REPAIRED PER UPS EO DC8-53-1417. 2L74 4F RT4A25 19950804003221995080400322WP 1995 8 4 UPS 803931 119950731A53215612298343 SUBFLOOR DOUG DC8 DC871F 302199DWP FS 16 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, HEAVY CORR ON COCKPIT SUBFLOOR WEB UNDER F/E'S INSTRUMENT PANEL FS 49 TO 15 OUTBD CORNER. REPAIRED PER UPS EO DC8-5310-7208A. 2L74 4F RT4A25 19950804003231995080400323WP 1995 8 4 UPS 803932 119950731A5330 SKIN DOUG DC8 DC871F 302199DWP FS 70-140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR BULGE ON BELLY SKIN FS 70 TO 140 BETWEEN LONGERONS 35L AND 34R. REPLACED BELLY SKIN PANEL FS 70 AND 190 PER SRM 51-1-21. 2L74 4F RT4A25 19950804003241995080400324WP 1995 8 4 UPS 803933 119950731A53135141599712000 LONGERON DOUG DC8 DC871F 302199DWP FS 1558 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 23L HAS HEAVY CORROSION AT FS 1558. REPAIRED LONGERON PER SRM 53-2-2, FIGURE 10. 2L74 4F RT4A25 19950804003251995080400325WP 1995 8 4 UPS 803934 119950731A5313602493 LONGERON DOUG DC8 DC871F 302199DWP FS 1620-1660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, HEAVY CORR AT LONGERON 30R, FS 1620 TO 1660. REPLACED LONGERON SECTION PER 51-1-20D. 2L74 4F RT4A25 19950804003261995080400326WP 1995 8 4 UPS 803935 119950731A532052645716 SPLICE DOUG DC8 DC871F 302199DWP FS 1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, AFT ASSY COMPT HAS HEAVY CORR ON LONGERON SPLICE FS 1560, LONG 30R. REPAIRED PER SRM 53-2-2 FIG 10. 2L74 4F RT4A25 19950804003271995080400327WP 1995 8 4 UPS 803936 119950731A532052645716 SPLICE DOUG DC8 DC871F 302199DWP FS 1540-1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, MODERATE CORR AT LONGERON 32L SPLICE BETWEEN FS 1540 TO 1560. REPAIRED SPLICE PER SRM 53-2-2 FIG 10. 2L74 4F RT4A25 19950804003281995080400328WP 1995 8 4 UPS 803937 119950731A53200327075T6 DOUBLER DOUG DC8 DC871F 302199DWP FS 1620-1680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, INNER DOUBLERS HAVE HEAVY CORR BELOW AFT SERVICED AIR ENTRY DOORS. REPLACED DOUBLERS PER SRM 51-1-20D, AND SRM 51-1-21. 2L74 4F RT4A25 19950804003291995080400329WP 1995 8 4 UPS 803938 119950731A5313975491335N LONGERON DOUG DC8 DC871F 302199DWP FS 390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 35R INBD SIDE HAS 8 INCH CRACK AT FS 390. REPLACED LONGERON SECTION FS 100 TO 390 PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003301995080400330WP 1995 8 4 UPS 803939 119950731A5313577992521N LONGERON DOUG DC8 DC871F 302199DWP FS 120 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 33R CRACKED 1 INCH LONG AT FS 120. REPLACED LONGERON SECTION FS 70 TO 180 PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003311995080400331WP 1995 8 4 UPS 803940 119950731A5313577992519N LONGERON DOUG DC8 DC871F 302199DWP FS 120-180 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01751UP 45915 WHILE IN DALFORT FOR C-CHECK, LONGERON 32R CRACKED 7 INCHES LONG AT FS 120, 140, 160, AND 180. REPLACED LONGERON SECTION FS 20 TO 190 PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003321995080400332NM 1995 8 4 UPS 803941 119950729A3350 EEL BATTERY PACK BOEING727 72727C 138400JNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01915UP 19246 WHILE IN SPRINGFIELD, MAINT FOUND EMERG EXIT LIGHT OVER COCKPIT DOOR INOP. CHANGED BATTERIES. OPS CK OF LIGHT GOOD PER MM 33-50-101. 2L73 4F A3WE 19950804003331995080400333WP 1995 8 4 UPS 803942 119950729A3350570845803 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01811UP 46089 WHILE ON GROUND, MAINTENANCE FOUND EMER EXIT LIGHTS INOP ON PREFLIGHT. REMOVED AND REPLACED EMER BATTERY PACK. 2L74 4F RT4A25 19950804003341995080400334WP 1995 8 4 UPS 803943 119950731A575556551851 SKIN DOUG DC8 DC873F 302199FWP NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND LT WING NR 1 SPOILER DELAM AT LOWER SIDE. REPLACED SPOILER ASSY PER MM 27-61-01. 2L74 4F RT4A25 19950804003351995080400335WP 1995 8 4 UPS 803944 119950731A532036468732 ANGLE DOUG DC8 DC873F 302199FWP RT MLG WW CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND RT WHEEL WELL ANGLE DOUBLER CRACKED AT FWD INBD CORNER, INBD OF SPIDER BRACKET. REPLACED ANGLE PER SRM 51-1-20D. 2L74 4F RT4A25 19950804003361995080400336WP 1995 8 4 UPS 803945 119950731A534754755395 SEAT TRACK DOUG DC8 DC873F 302199FWP FS 863 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND MODERATE TO HEAVY CORR ON NR 7 SEAT TRACK FWD END FS 863. REPLACED TRACK SECTION FS 850 TO 950 PER SRM 53-2-3. 2L74 4F RT4A25 19950804003371995080400337WP 1995 8 4 UPS 803946 119950731A5330063707576 SKIN DOUG DC8 DC873F 302199FWP FS 1700 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND .25 INCH LONG CRACK FWD AND AFT OF RIVET HOLE AT FS 1700 LONGERON 14R TO 15R. REPAIRED PER SRM 53-2-0, FIGURE 1B. 2L74 4F RT4A25 19950804003381995080400338WP 1995 8 4 UPS 803947 119950731A57125770123 LE RIB DOUG DC8 DC873F 302199FWP LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND UPPER LEADING EDGE RIBS CRACKED AT STA XSF 416, XSF 410, XFS 373, XFS 304, AND XFS 310, UPPER AND LOWER. REPAIRED PER MM 57-00-00, FIG 801. 2L74 4F RT4A25 19950804003391995080400339WP 1995 8 4 UPS 803948 119950731A5311561386176 FRAME DOUG DC8 DC873F 302199FWP FS 76 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-MAINT, FOUND FRAME HAS A 2 INCH CRACK AT FS 76, BETWEEN LONGERON 21R TO 24R. REPLACED PER SRM 51-1-21. 2L74 4F RT4A25 19950804003401995080400340SW 1995 8 4 95ZZZW795 119950626A57532726003001 RIB SWRNGNSA227 SA227AC 8780603SW CRACKED G MALAK NONE O OTHER ININSP/MAINT 1 26906 AC654B MSP - DURING SCHEDULED MAINTENANCE, THE LT FLAP I/B END RIB WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE FORWARD END RIB, P/N 27-36004-009, AND AFT END RIB, P/N 27-26-003-001, IAW FAC SRM 57-90-60. REF MALA954515. 2L72 4T RTA8SW 19950804003411995080400341SW 1995 8 4 95ZZZW796 119950626A57532736015010 RIB SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING SCHEDULED MAINTENANCE, THE RT FLAP I/B HINGE CHANNEL, P/N 27-36044-006, WAS FOUND TO BE BENT AND NOSE RIB ASSEMBLIES, P/N 27-36015-010 AND P/N 27-36016-002, WERE FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE PARTS IAW FAC SRM 51-00-00 PAGE 4, 51-46-02, AND 57-90-60. REF 95ZZZW797, MALA954516. 1L72 4T A8SW 19950804003421995080400342SW 1995 8 4 95ZZZW797 119950626A57532736016002 RIB SWRNGNSA227 SA227AC 8780603SW RT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING SCHEDULED MAINTENANCE, THE RT FLAP I/B HINGE CHANNEL, P/N 27-36044-006, WAS FOUND TO BE BENT AND NOSE RIB ASSEMBLIES, P/N 27-36015-010 AND P/N 27-36016-002, WERE FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE PARTS IAW FAC SRM 51-00-00 PAGE 4, 51-46-02, AND 57-90-60. REF MALA954516, 95ZZZW796. 1L72 4T A8SW 19950804003431995080400343SW 1995 8 4 95ZZZW798 119950626A57532731253 RIB SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LT FLAP DOUBLER AND LT RIB WORN AT WS 27. REPAIRS WERE COMPLETED BY REPLACING THE FLAP ROLLER DOUBLER, P/N 27-31141, AND RIB P/N 27-31253, IAW FAC SRM 51-00-00, 57-90-10 AND 57-20-9424. REF MALA954514. 1L72 4T A8SW 19950804003441995080400344WP 1995 8 4 AALA951161 119950628A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07147AA 46702 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RT SIDE OF SERVICE CENTER INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT RT SIDE OF SERVICE CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950804003451995080400345SW 1995 8 4 MALA954510 119950620A32302751000192 UPLOCK HOOK SWRNGNSA227 SA227AC 8780603SW RT MLG BROKEN A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15423MA AC636 FFM - FLT 3074 - AFTER TAKEOFF, NOSE LANDING GEAR WOULD CYCLE PARTIALLY OUT+OF +HEEL WELL. NO GEAR INDICATIONS WOULD ILLUMINATE. THE FLIGHT CONTINUED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT MAIN GEAR UPLOCK. THE SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804003461995080400346SW 1995 8 4 MALA954511 119950624A3260 SWITCHES SWRNGNSA227 SA227AC 8780603SW RT MLG LACK OF LUBE A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15424MA AC639 DTW - FLT 3186 - ON APPROACH, THE RT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. ALL OTHER GEAR INDICATIONS WERE NORMAL. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, MAINTENANCE CLEANED AND LUBED ALL OF THE RT GEAR'S MICROSWITCHES. (W) 1L72 4T A8SW 19950804003471995080400347NM 1995 8 4 MALA954512 119950124A242051608002 GEN CONTL UNIT DHAV DHC8 DHC8102 2809003NM LT FAILED A MALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 GL15852MA 349 DTW - FLT 3029 - ON CLIMBOUT, THE NR 1 GENERATOR FELL OFF LINE. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REPLACED THE LT AC GCU. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804003481995080400348NM 1995 8 4 MALA954513 119950625A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15853MA 353 DTW - FLT 3172 - DURING THE POST FLIGHT INSPECTION, THE CREW FOUND THE PORTABLE EMERGENCY LIGHT ASSEMBLY IN THE COCKPIT TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804003491995080400349SW 1995 8 4 MALA954514 119950626A57532731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE LT FLAP DOUBLER AND LT RIB WORN AT WS 27. REPAIRS WERE COMPLETED BY REPLACING THE FLAP ROLLER DOUBLER, P/N 27-31141, AND RIB P/N 27-31253, IAW FAC SRM 51-00-00, 57-90-10 AND 57-20-9424. REF95ZZZW 1L72 4T A8SW 19950804003501995080400350SW 1995 8 4 MALA954515 119950626A57532736004009 RIB SWRNGNSA227 SA227AC 8780603SW LT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING SCHEDULED MAINTENANCE, THE LT FLAP I/B END RIB WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE FORWARD END RIB, P/N 27-36004-009, AND AFT END RIB, P/N 27-26-003-001, IAW FAC SRM 57-90-60. REF 95ZZZW795. 1L72 4T A8SW 19950804003511995080400351SW 1995 8 4 MALA954516 119950626A57532736044006 CHANNEL SWRNGNSA227 SA227AC 8780603SW RT TE FLAP BENT A MALAK NONE O OTHER ININSP/MAINT 1 GL1526906 AC654B MSP - DURING SCHEDULED MAINTENANCE, THE RT FLAP I/B HINGE CHANNEL, P/N 27-36044-006, WAS FOUND TO BE BENT AND NOSE RIB ASSEMBLIES, P/N 27-36015-010 AND P/N 27-36016-002, WERE FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE PARTS IAW FAC SRM 51-00-00 PAGE 4, 51-46-02, AND 57-90-60. REF 95ZZZW796, 95ZZZW797. 1L72 4T A8SW 19950804003521995080400352SW 1995 8 4 MALA954517 119950627A53112720085 FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 MSP - DURING A SCHEDULED INSPECTION, THE CARGO DOOR AFT FUSELAGE FRAME AT FS 491, WAS FOUND TO BE CRACKED AT THE FS SPRING ATTACH POINT. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING REPAIR DOUBLERS AND FILLER PLATE IAW WITH FAC 53-20-9503. (W) 1L72 4T A8SW 19950804003531995080400353SW 1995 8 4 MALA954519 119950627A3260ML345 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15424MA AC639 DAY - FLT 3004 - ON CLIMBOUT, THE RT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR RETRACTION. THE LIGHT ALSO, DID NOT ILLUMINATE DURING GEAR EXTENSION ON APPROACH TO DTW. MAINTENANCE REPLACED A POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804003541995080400354NM 1995 8 4 MALA954520 119950628A561017180003 WINDOW SEAL DHAV DHC8 DHC8102 2809003NM COCKPIT LOOSE A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15831MA 339 DTW - FLT 3418 - UPON CLIMBOUT, THE PILOT'S SIDE WINDOW SEAL CAME LOOSE. THE AC RETURNED TO DTW. MAINTENANCE RESEALED THE WINDOW SEAL. ALL CHECKS SATISFACTORY. (W) 2H72 4T RTA13NM 19950804003551995080400355WP 1995 8 4 MALA954521 219950629A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT FLAME-OUT A MALAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 GL1526906 AC654B DTW - FLT 3360 - UPON CLIMBOUT, AT 3,000 AGL AND LIGHT RAIN, THE LT ENGINE EXPERIENCED A MOMENTARY FLAME-OUT. THE LT ENGINE IMMEDIATELY RESTARTED. THE ENGINE OPERATED NORMALLY UPON RETURN TO DTW. MAINTENANCE INSPECTED AND GROUND RAN THE ENGINE, NO DISCREPANCIES NOTED. THE ENGINE OPERATED SATISFACTORILY DURING TEST FLIGHT. (W) 1L72 4T4 T A8SW E4WE 19950804003561995080400356NM 1995 8 4 MALA954522 119950629A33506038443 EEL PWR SUPPLY DHAV DHC8 DHC8102 2809003NM CABIN FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15817MA 249 DTW - FLT 3339 - DURING THE PREFLIGHT, THE OVERHEAD AISLE EMERGENCY LIGHT IN THE CABIN WAS BURNED OUT. MAINTENANCE REPLACED THE POWER SUPPLY ASSEMBLY, P/N 60-3844-3. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804003571995080400357SW 1995 8 4 MALA954523 119950628A2432235761 BATTERY SWRNGNSA227 SA227AC 8780603SW LT BATT BOX MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15425MA AC640 LEX - FLT 3376 - EN ROUTE, THE LT BATTERY TEMP WARNING LIGHT ILLUMINATED. THE CREW DISCONNECTED THE LT BATTERY AND THE TEMPERATURE RETURNED TO NORMAL. THE AC RETURNED TO DTW. MAINTENANCE REPLACED THE LT BATTERY. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804003581995080400358SW 1995 8 4 MALA954524 119950628A2431 CONNECTOR SWRNGNSA227 SA227AC 8780603SW LT BATTERY FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15425MA AC640 YNG - FLT 3360 - IN CRUISE, THE LT BATTERY TEMP WARNING LIGHT ILLUMINATED. THE CREW DISCONNECTED THE LT BATTERY AND THE TEMPERATURE CONTINUED TO INDICATE A HIGH TEMPERATURE. THE AC RETURNED TO DTW. MAINTENANCE REPLACED THE CANNON PLUG AT THE BATTERY. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804003591995080400359SW 1995 8 4 MALA954526 119950630A5210 MECHANISM SWRNGNSA227 SA227AC 8780603SW PAX DOOR OUT OF ADJUST A MALAI CABIN DEPRESSURIZATION J WARNING INDICATION CRCRUISE 1 GL152692P AC658B MLI-MSP - FLT 3285 - EN ROUTE AT 16,000, THE PASSENGER DOOR WARNING LIGHT ILLUMINATED. THE CREW DEPRESSURIZED THE AC TO 4.7 PSI DIFFERENTIAL AND THE LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO MSP WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGGING OF THE PASSENGER DOOR BAYONETS AND DOOR WARNING SWITCH. THE SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804003601995080400360WP 1995 8 4 95ZZZX3537 119950703A32227919074721 STRUT DOUG DC9 DC951 3022051WP NLG LOCKED A A4JAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO15920PJ 47677 FLT 220 - AFTER GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON. CYCLED GEAR, ALL INDICATIONS NORMAL. FOUND NOSE LANDING GEAR STRUT HYDRAULICALLY LOCKED. DEPLETED STRUT. SERVICED IAW DOUGLAS DC-9 MM. RETRACTION TEST NORMAL. CYCLES, 6,194. 2L72 4F A6WE 19950804003611995080400361NM 1995 8 4 95ZZZX3538 119950708A8012215N4113 START VALVE BOEING747 747212B 1384886NM NR 3 ENGINE FAILED ALASRAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19745SJ 20888 20888 SJM - FLT 203 - DURING FLIGHT FROM MIAMI TO BOGATA, NR 3 ENGINE START VALVE OPEN LIGHT CAME ON. SHUT DOWN NR 3 ENGINE AS PRECAUTIONARY AND COMPLETED AIR TURN BACK TO MIAMI, AIRCRAFT LANDED AT 655,000 POUNDS. REPLACED NR 3 ENGINE START VALVE PRESSURE SWITCH, PN 215N4113. INDICATION CHECKED GOOD. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION PER BOEING, MM CMT 5-51-39. NO DEFECTS NOTED. 2L74 4F A20WE 19950804003621995080400362WP 1995 8 4 95ZZZX3539 119950320A5610340311030110 WINDSHIELD CVAC 440 440 2422902WP RIGHT CRACKED A FLTAK NONE O OTHER TXTAXI/GRND HDL 1 WP09969N 475 NUC - UPON TAXIING ONTO RAMP IN AN UNPRESSURIZED CONDITION, THE FIRST OFFICER'S WINDSHIELD (OUTER PANE) CRACKED IN THE LOWER RIGHT CORNER. MAINTENANCE FOUND A CRACK IN THE OUTER GLASS RUNNING FROM THE OUTBOARD EDGE IN AN ARC APPROXIMATELY 10.50 INCHES IN LENGTH TO THE BOTTOM EDGE OF THE GLASS. THE WINDSHIELD WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4R 6A6 19950804003631995080400363EA 1995 8 4 95ZZZX3540 119950612A3230155507 UPLOCK ACT MENASCO DHAV DHC7 DHC7102 2802708EA LT MLG FAILED A HNAAK NONE O OTHER APAPPROACH 1 EA07901HA26298 MC137 042 PHL/DCA - FLT 3095 - ON APPROACH, THE LEFT MAIN GEAR WOULD NOT EXTEND, RELEASED GEAR MANUALLY. THE AIRCRAFT CONTINUED INTO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 UPLOCK ACTUATOR AND REAMED THE LOWER BUSHING IN THE UPPER DRAG STRUT. ALSO, REMOVED AND REPLACED FILTERS IN THE RETRACTION ACTUATOR. 2H74 4T A20EA 19950804003641995080400364NM 1995 8 4 95ZZZX3541 119950506A7600 SWITCH DHAV DHC8 DHC8102 2809003NM NR 1 PWR LEVER OUT OF ADJUST A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07979HA 373 EWN/CLT - FLT 3239 - DURING TAKEOFF ROLL, THE ROLL SPOILER GROUND MODE CAUTION LIGHTS ILLUMINATED. CREW ABORTED TAKEOFF WITHOUT INCIDENT. MEL 27-8. AT RON, ADJUSTED NR 1 POWER LEVER ANGLE WITH 2761-S1 AND CLEANED, LUBED AND ADJUSTED NR 2 POWER LEVER ANGLE WITH 2761-S2. 2H72 4T RTA13NM 19950804003651995080400365EA 1995 8 4 95ZZZX3542 219950616A7230 BLADE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA COMPRESSOR DAMAGED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07905HA267249335 070 86392 ORF/DCA - FLT 3003 - ON TAKEOFF, AS POWER APPROACHES 4,200 POUNDS TORQUE & BEYOND, NR 2 ENGINE EXCEEDS 800 DEGREES & LOUD BANGS HEARD. COMPRESSOR STALLS & ENG ROLLS BACK. CREW ABORTED T/O & RETND WITHOUT INCIDENT. REMOVED & REPLACED NR 2 ENG. SUPPLEMENT TO ORIG MRR, 6-16-95. TEAR DOWN RECEIVED FROM AIRWORK 11-30-95, & FND COMPRESSOR'S HOOTING & STALLING CAN BE CONTRIBUTED TO INTERRUPTION OF AIRFLOW IN COMPR ROTOR DUE TO 1ST STAGE BLADE DAMAGE. DAMAGE IS LIKELY RESULTANT OF FOREIGN OBJECT INGESTION DURING LAST T/O RUN IN WHICH COMPR HOOT WAS REPORTED. OTHER CONDITIONS FND DURING EVALUATION ARE SECONDARY TO BLADE DAMAGE WHICH EXCITED STALLING, BUT DID NOT INITATE THE STALL. RE: OPER CNTRL NR HNAA9590519.2H74 4T4 T A20EA E4EA 19950804003661995080400366EA 1995 8 4 95ZZZX3543 119950609A3233154009 ACTUATOR MENASCO DHAV DHC7 DHC7102 2802708EA LT MLG FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07900HA MC049 025 HPN/DCA - FLT 3170 - LEFT MAIN GEAR DID NOT FULLY RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO HPN AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MLG RETRACTION ACTUATOR. 2H74 4T A20EA 19950804003671995080400367EA 1995 8 4 95ZZZX3544 119950612A3230 UPLOCK ACTUATOR DHAV DHC7 DHC7102 2802708EA LT MLG DIRTY A HNAAO OTHER O OTHER APAPPROACH 1 EA07901HA 042 ORF/DCA - FLT 3144 - LEFT MAIN GEAR DID NOT BEGIN TO EXTEND UNTIL NOSE AND RIGHT MAIN WERE DOWN AND LOCKED. EXTENSION WAS SLOW ONCE STARTED. THE AIRCRAFT CONTINUED INTO DCA AND LANDED WITHOUT INCIDENT. CLEANED RESTRICTOR ON UPLOCK ACTUATOR AND OPERATIONAL CHECK GOOD. 2H74 4T A20EA 19950804003681995080400368NE 1995 8 4 95ZZZX3545 219950607A7314025323402 FUEL PUMP DHAV DHC7 DHC7102 2802708EA PWA 120 PW120A NE NR 1 ENGINE FAILED A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA07901HA16661 8108 042 PHL/DCA - FLT 3060 - NR 1 FUEL PRESSURE CAUTION LIGHT ILLUMINATED IN-FLIGHT AND NG DROPPED TO APPROXIMATELY 40 PERCENT. THE ENGINE WAS SHUT DOWN IN-FLIGHT. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 FUEL PUMP AND NR 1 FUEL CONTROL UNIT. 2H74 4T4 T A20EA E20NE 19950804003691995080400369NE 1995 8 4 95ZZZX3546 219950607A732132447531817 FUEL CONTL UNIT DHAV DHC7 DHC7102 2802708EA PWA 120 PW120A NE NR 1 ENGINE FAILED A HNAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA07901HA1647516052 A54048 042 PHL/DCA - FLT 3060 - NR 1 FUEL PRESSURE CAUTION LIGHT ILLUMINATED IN-FLIGHT AND NG DROPPED TO APPROXIMATELY 40 PERCENT. THE ENGINE WAS SHUT DOWN IN-FLIGHT. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 FUEL PUMP AND NR 1 FUEL CONTROL UNIT. 2H74 4T4 T A20EA E20NE 19950804003701995080400370NM 1995 8 4 95ZZZX3547 119950617A6123JV5 ACTUATOR DHAV DHC8 DHC8102 2809003NM COCKPIT BROKEN A HNAAK NONE O OTHER ININSP/MAINT 1 EA07941HA16397 161 AVL/CLT - FLT 3304 - DURING PRE-FLIGHT CHECKS, FOUND THE AUTOFEATHER SYSTEM WOULD NOT ARM. REMOVED AND REPLACED THE ACTUATOR ON POWER LEVER MICROSWITCH 6121-S9. 2H72 4T RTA13NM 19950804003711995080400371NE 1995 8 4 95ZZZX3548 219950707A73217898426009 ECU HAMSTD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE NR 1 ENGINE FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07912HA3065 93030091 40 CHO/BWI - FLT 3201 - ON CLIMB-OUT, NR 1 ENGINE TORQUE UPTRIMMED TO 125 PERCENT. AT FLIGHT IDLE, STILL AT 110 PERCENT. CAPTAIN SHUT ENGINE DOWN IN-FLIGHT. AIRCRAFT DIVERTED TO RIC AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE ELECTRONIC CONTROL UNIT. 2H72 4T4 TRTA13NM E20NE 19950804003721995080400372WP 1995 8 4 95ZZZX3549 119950709A3260PD507756043 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG FAILED A VJ6AO OTHER N FALSE WARNING APAPPROACH 1 SO11901VJ 47275 TPA/ATL - FLT 120 - UPON GEAR EXTENSION, THE LEFT MAIN GEAR DID NOT HAVE A DOWN AND LOCK INDICATION. CAPTAIN DECLARED AN EMERGENCY AND LANDED WITH GEAR DOORS DOWN. NO FURTHER PROBLEMS REPORTED. REPLACED DOWNLOCK SWITCH CANNON PLUG P1-132 AND NEW PINS ON ALL WIRES. PERFORMED GEAR RETRACTION AND EXTENSION. OPS CHECK NORMAL PER MM 32-50. 2L72 4F A6WE 19950804003731995080400373WP 1995 8 4 95ZZZX3563 119950704A3260 IND WIRE DOUG DC9 DC932 3022066WP LT MLG FAILED A VJ6AL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO11901VJ 47275 FLT 198 - HAD AN IMPROPER LANDING GEAR INDICATION ON LEFT MAIN GEAR BEFORE LANDING. REPAIRED THE WIRING AT THE LEFT MAIN GEAR DOWN LIMIT PLUG P-132. OPS CHECK OKAY. 2L72 4F A6WE 19950804003741995080400374SO 1995 8 4 C2XA95CL103 119950711A571312016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0934712 120111 DURING ROUTINE MAINTENANCE INSPECTION, FOUND STR NR 10 CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED STRINGER BY SPLICE JOINT IAW EMBRAER DER APPROVED PROCEDURE EST234/95 AND EST311/95, AND EMB SRM 51-40-02. (X) 2L72 4T RTA31SO 19950804003751995080400375SO 1995 8 4 C2XA95IA116 119950714A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RT WING, RIB 16 UPPER SKIN NR 3 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950804003761995080400376SO 1995 8 4 C2XA95IA117 119950714A573012017291001 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER OUTBOARD SKIN CRACKED AT AFT CORNER OF FUEL CONTROL PANEL CUTOUT, 641AB. MAINTENANCE INSTALLED REPAIR DOUBLER PER EC5730-01031, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950804003771995080400377SO 1995 8 4 C2XA95IA118 119950714A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LT LOWER AFT CABIN SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE LT AFT SECTION OF SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950804003781995080400378SO 1995 8 4 C2XA95IA119 119950714A554012034077001 BRACKET EMB 120 EMB120RT SO LOWER RUDDER 1 RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURINC C-CHECK INSPECTION, FOUND RUDDER 1, SECOND FROM BOTTOM HINGE BEARING, RUSTED. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AND BEARING ASSEMBLY. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TT 11,901.4. TC - 16,783. (X) 2L72 4T RTA31SO 19950804003791995080400379SO 1995 8 4 C2XA95IA120 119950714A572012017056007 SUPPORTS EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LT WING, RIB 16 UPPER, 3 EACH, SKIN SUPPORTS CRACKED. MAINTENANCE REMOVED AND REPLACED SKIN SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA31SO 19950804003801995080400380SO 1995 8 4 C2XA95IA121 119950714A572012017056011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURNG C-CHECK INSPECTION, FOUND LT WING, RIB 15, LOWER NR 1 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 11,901.4. CYCLES, 16,783. (X) 2L72 4T RTA31SO 19950804003811995080400381SO 1995 8 4 C2XA95IA123 119950714A532012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LT WING, RIB 15, LOWER NR 4 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 11,901.4. CYCLES, 16,783. (X) 2L72 4T RTA31SO 19950804003821995080400382EU 1995 8 4 C2XA95IA124 119950717A5320S5397091627200 SUPPORT AEROSPATR42 ATR42320 8680930EU RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0923802 064 IAH - DURING C-CHECK INSPECTION, FOUND TOP FORWARD HORIZONTAL SUPPORT CRACKED BEHIND PANEL 294AR. MAINTENANCE STOP DRILLED CRACK, AND INSTALLED A REPAIR DOUBLER. AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 14,857.5. CYCLES, 18,385. (X) 2H72 4T RTA53EU 19950804003831995080400383EU 1995 8 4 C2XA95IA125 119950717A5720S5397091629300 SUPPORT AEROSPATR42 ATR42320 8680930EU LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0923802 064 IAH - DURING C-CHECK INSPECTION, FOUND MIDDLE HORIZONTAL SUPPORT FRAME CRACKED BEHIND PANEL 293AL. MAINTENANCE STOP DRILLED CRACK, AND INSTALLED A REPAIR DOUBLER. AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 14,857.5. CYCLES, 18,385. (X) 2H72 4T RTA53EU 19950804003841995080400384EU 1995 8 4 C2XA95IA126 119950717A5720S5397091626600 SUPPORT AEROSPATR42 ATR42320 8680930EU RT WING BENT A C2XAK NONE O OTHER ININSP/MAINT 1 SW0923802 064 IAH - DURING C-CHECK INSPECTION, FOUND TOP MIDDLE HORIZONTAL SUPPORT BENT AND CHAFED BEHIND PANEL 294AR. MAINTENANCE INSTALLED A REPAIR DOUBLER, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 14,857.5. CYCLES 18,385. (X) 2H72 4T RTA53EU 19950804003851995080400385EU 1995 8 4 C2XA95IA127 119950717A5720S5397091636300 SUPPORT AEROSPATR42 ATR42320 8680930EU RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0923802 064 IAH - DURING C-CHECK INSPECTION, FOUND RT WING BOX VERTICAL SUPPORT, FRAME 29, CRACKED BEHIND PANEL 296FR. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT, 14,857.5. CYCLES, 18,385. (X) 2H72 4T RTA53EU 19950804003861995080400386EU 1995 8 4 C2XA95IA128 119950717A5720S5721157720100 SUPPORT AEROSPATR42 ATR42320 8680930EU RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0923802 064 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NAVIGATION LIGHT LENSE SUPPORT RIB CRACKED. MAINTENANCE STOP DRILLED CRACK, AND INSTALLED A REPAIR DOUBLER. AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 14,857.5. CYCLES, 18,385. (X) 2H72 4T RTA53EU 19950804003871995080400387WP 1995 8 4 HAL95084 119950629A3350 EEL BULB DOUG DC9 DC951 3022051WP CABIN FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 47742 HNL - INFORMATION FROM M-71 LOG PAGE 148514. THREE SETS OF CABIN EMERGENCY FLOOR LIGHTS ARE OUT. REPLACED 3 EACH EMERGENCY FLOOR LIGHT BULBS. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950804003881995080400388WP 1995 8 4 HAL95087 119950630A3350 EEL BULBS DOUG DC9 DC951 3022051WP CABIN FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - INFORMATION FROM M71 LOG PAGE 148613-2. THREE SETS OF CABIN FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT BULBS. OPERATIONS CHECK GOOD. (X) 2L72 4F A6WE 19950804003891995080400389WP 1995 8 4 HAL95088 119950701A3350 EEL BULBS DOUG DC9 DC951 3022051WP CABIN FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13674MC 47735 HNL - INFORMATION FROM M71 LOG PAGE 149051-3. SIX SETS OF CABIN FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT BULBS. OPERATIONS CHECK GOOD. (X) 2L72 4F A6WE 19950804003901995080400390WP 1995 8 4 HAL95091 119950712A335020131A EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 32446 48122 HNL - INFORMATION FROM M71 LOG PAGE 148957-2. FLOOR EMERGENCY LIGHTS INOPERATIVE FROM THE OVERWING EXITS TO THE AFT OF THE AIRCRAFT CABIN. REPLACED AFT CONTROL MODULE AND BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19950804003911995080400391WP 1995 8 4 HAL95092 119950706A2612 FIRE LOOP DOUG DC10 DC1010 3022110WP NR 1 ENGINE CHAFED A HALAK NONE O OTHER ININSP/MAINT 1 WP13119AA 46519 LAX - INFORMATION FROM LOG PAGE 142093. DURING ENGINE NR 1 LOOP , 'B' FLICKERED ON OVER A ONE MINUTE PERIOD. ACCOMPLISHED ABNORMAL PROCEDURE 1 IN FIRE PROTECTION SECTION OF FCOM. WITH ENGINE 1 LOOPS SWITCH SELECTED TO 'A' LOOP, A SATISFACTORY LOOPS 'A' TEST WAS DONE. FOUND WIRE CHAFED UNDER CLAMP AT 5 O'CLOCK POSITION AFT SECTION. WRAPPED WIRE BUNDLE AND REPLACED CLAMP. CHECKS NORMAL. REMOVED PLACARD. CLEARED MAINTENANCE ITEM CONTROL SHEET. (X) 2L73 4F A22WE 19950804003921995080400392EU 1995 8 4 RAIA950646 119950630A33503011151 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE5512 2045 106 STL - EMERGENCY LIGHTING IN THE CABIN IS INOPERATIVE. MAINTENANCE REPLACED POWER SUPLY AND SOME LIGHT BULBS. (X) 2H72 4T RTA53EU 19950804003931995080400393EU 1995 8 4 RAIA950702 119950706A7722KR123B CONNECTOR WIRE BAG JETSTMJETSTM3201 1500217EU RT ENGINE BROKEN A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03867AE9094 867 FAT - FLT 4746 - RT EGT GAUGE FAILED ON TAXI. MAINTENANCE SOLDERED BROKEN LEAD ON RT ENGINE EGT CONNECTOR. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950804003941995080400394EU 1995 8 4 RAIA950703 119950708A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03338TE7024 7024 932 STL - FLT 7096 - RT ENGINE WOULD NOT MAKE TARGET TORQUE, WOULD ONLY PULL 99 PERCENT RPM. MAINTENANCE ADJUSTED RT ENGINE TORQUE SIGNAL CONDITIONER TO GARRETT DSC SETTING AND PROPELLER GOVERNOR LOW STOP. GROUND RUNS OK. (X) 2L72 4T RTA56EU 19950804003951995080400395EU 1995 8 4 RAIA950704 119950708A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03424TE4537 1375 124 STL - FORWARD EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED FORWARD EMERGENCY BATTERY PACK. (X) 2H72 4T RTA53EU 19950804003961995080400396EU 1995 8 4 RAIA950705 119950708A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE8675 539 106 STL - SMALL SECTION OF FORWARD EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (X) 2H72 4T RTA53EU 19950804003971995080400397SO 1995 8 4 RAIA950706 119950710A3150 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03127AM1588015880 120103 STL - FLT 7452 - TRIM WARNING SOUNDED ON TAKEOFF. MAINTENANCE RESET AURAL WARNING CIRCUIT BREAKER. SYSTEM CHECK GOOD. (X) 2L72 4T RTA31SO 19950804003981995080400398EU 1995 8 4 RAIA950707 119950711A3242215221 BRAKE BAG JETSTMJETSTM3201 1500217EU RT MLG FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03340TE6473 123 939 STL - FLT 7505 - RT BRAKE WILL NOT WORK AFTER FEW APPLICATIONS ON LANDING. MAINTENANCE REPLACED RT BRAKE ASSEMBLY. TAXI CHECK REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19950804003991995080400399EU 1995 8 4 VTZA05215 119950716A77228974694 EGT HARNESS BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27478UE 892 IAD/HVN - FLT 6173 - DURING TAKEOFF AT 1438 HRS ON 7-12-95, RETURNED TO IAD DUE TO THE LEFT ENGINE EGT SHOWING VERY ERRATIC INDICATIONS. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED THE COLD SOLDER JOINT ON THE EGT HARNESS. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950804004001995080400400EU 1995 8 4 VTZA95216 119950710A529791SE13 WIRE BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR BROKEN A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27482UE 897 IAD/SYR - FLT 6343 - DURING CLIMB-OUT AT 1240 HRS ON 7-10-95, RETURNED TO IAD DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED A BROKEN WIRE AT THE PASSENGER DOOR MICROSWITCH. OPS CHECKED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950804004011995080400401EU 1995 8 4 VTZA95217 119950712A77228974694 EGT HARNESS BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27490UE 909 PWM/BOS - FLT 6183 - DURING TAKEOFF AT 1438 HRS ON 7-12-95, RETURNED TO PWM DUE TO THE EGT SHOWING ERRATIC INDICATIONS ON THE LEFT ENGINE. AIRCRAFT LANDED AT PWM WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED THE COLD SOLDER JOINT ON THE EGT HARNESS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950804004021995080400402EU 1995 8 4 VTZA95218 119950709A523014153133417 HANDLE ASSEMBLY JETAIRJETSTMJETSTM4101 1500501EU BAGG DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27302UE 41013 IAD/BDL - FLT 6521 - DURING TAKEOFF AT 1544 HRS ON 7-9-95, ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE FULLY SEATED THE BAGGAGE DOOR HANDLE. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950804004031995080400403EU 1995 8 4 VTZA95219 119950713A7600F323A702561 IEC CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILURE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27309UE 41022 IAD/RDU - FLT 6573 - DURING CLIMB-OUT AT 1055 HRS ON 7-13-95, RETURNED TO IAD DUE TO THE RT IEC FAILING AND IT WOULD NOT RESET. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT T2 CANNON PLUG. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950804004041995080400404NE 1995 8 4 VTZA95220 219950716A7320 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE OUT OF ADJUST A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27309UE 41022 P75015C IAD/TYS - FLT 6160 - DURING TAKEOFF AT 1415 HRS ON 7-16-95, ABORTED TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE MAX FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950804004051995080400405NE 1995 8 4 VTZA95221 219950715A7320 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE NR 2 ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27310UE 41028 P76035C IAD/CHO - FLT 6356 - DURING TAKEOFF AT 0945 ON 7-15-95, ABORTED TAKEOFF DUE TO THE NR 2 ENGINE WOULD NOT MAKE TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RERIGGED RT ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950804004061995080400406EU 1995 8 4 VTZA95222 119950713A3260AIR135022 SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27312UE 41025 TYS/IAD - FLT 6354 - DURING TAKEOFF AT 1430 HRS ON 7-13-95, RETURNED TO TYS DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT WAS THEN FERRIED TO LYH. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT UPLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950804004071995080400407EU 1995 8 4 VTZA95223 119950713A3260T411AL3001C RELAY JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27317UE 41031 IAD/BTV - FLT 6265 - DURING TAKEOFF AT 1216 HRS ON 7-13-95, RETURNED TO IAD DUE TO THE GEAR BEING SELECTED UP AND THE GEAR HANDLE RED LIGHT REMAINED ILLUMINATED. CREW PUT GEAR BACK DOWN AND GOT ALL 3 GREEN DOWNLOCKS AND RED HANDLE LIGHT STILL ILLUMINATED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FLIGHT IDLE BAULK RELAY. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950804004081995080400408EU 1995 8 4 VTZA95224 119950717A793141SG107150G14 OIL PRESS TRANSD BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27494UE 810 IAD/PHL - FLT 6455 - DURING CRUISE AT 0650 HRS ON 7-17-95, RETURNED TO IAD DUE TO THE OIL PRESSURE ON THE LEFT ENGINE BEING ERRATIC. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT OIL PRESSURE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950804004091995080400409WP 1995 8 4 9511509150 119950728A7711 EPR IND DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018909E 45770 655315 NR 1 ENGINE EPR INDICATION WENT TO ZERO ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR. THE SYSTEM CHECKED OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950804004101995080400410WP 1995 8 4 9511519150 119950730A7711 EPR IND DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018909E 45770 655315 NR 1 ENGINE EPR INDICATION WAS BELOW NORMAL ON TAKEOFF, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER, CHECKED THE PT7 SYSTEM FOR LEAKS AND THE INDICATOR FOR ACCURACY. SYSTEM OPERATION WAS NORMAL ON RUNUP. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950804004111995080400411NM 1995 8 4 9511522763 119950731A3260 DOOR WARNING BOEING727 7272M7 138407SNM NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01723RW 21202 DURING CLIMB UPON LANDING GEAR RETRACTION, NOSE GEAR DOOR INDICATIONS REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH PROPER INDICATIONS. DTW MAINTENANCE DEFERRED NOSE LANDING GEAR DOOR WARNING SYSTEM INOPERATIVE PER MEL 32-1. 2L73 4F A3WE 19950804004121995080400412WP 1995 8 4 9511539305 119950728A2612 FIRE DETECTOR DOUG DC9 DC982 3022082WP APU MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01307RC 48086 DURING TAKEOFF, RECEIVED APU FIRE LOOP 'B' WARNING. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE APU FIRE CONTROL UNIT WAS FOUND TO HAVE TOO MUCH RESISTANCE AND WAS REPLACED. AIRCRAFT CHECKED OK FOR SERVICE. 2L72 4F A6WE 19950804004131995080400413WP 1995 8 4 ABXA9500639 119950728A793142D491C PRESS SWITCH DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 1 ENGINE LEAKING A ABXAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 GL23803AX 45917 669379 EIGHTY MINUTES AFTER LEVEL OFF, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL PRESSURE 44 PSI AND OIL TEMPERATURE 100 DEGREES CELSIUS. NOTED NR 1 OIL QTY DECREASING AT RATE OF 1.1 GPH. REDUCED POWER TO IDLE, CONSUMPTION DROPPED TO .6 GPH AT IDLE, OIL PRESSURE LOW LIGHT WAS ON STEADY. ENGINE WAS SECURED AT 1025 Z, TOTAL WINDMILLING TIME 2 HRS 18 MIN AT 20 PSI. FOUND OIL DIFFERENTIAL PRESSURE SWITCH LEAKING. REPLACED DIFFERENTIAL PRESSURE SWITCH AND LOW OIL PRESSURE WARNING SWITCH IAW DC 8 MM. ON GROUND RUN, SYSTEM LEAK AND OPS CHECKED NORMAL. 2L74 4F4 F 4A25 1E8 19950804004141995080400414SO 1995 8 4 BIER950016 119950801A32464090A MAIN WHEEL PIPER PA28 PA28236 7102815SO LT MLG CRACKED B BIEAK NONE O OTHER ININSP/MAINT 1 EA21435952019 288411018 FOUND THREE INCH CRACK ON MAIN WHEEL IN DISHED OUT AREA OPPOSITE THE WHEEL BEAD AREA. 1L71 3O 2A13 19950804004151995080400415SO 1995 8 4 COM11937 119950731A323020647 LINK ROD ERAM 20750 EMB 120 EMB120RT SO NLG FAILED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01200CD157993253 120200 AIRCRAFT ON APPROACH TO FPO, CREW SELECTED GEAR DOWN. THE MLG INDICATED DOWN AND LOCKED AND THE NLG INDICATED UNSAFE. MAINTENANCE INSPECTED THE NLG AND FOUND THE SECONDARY STRUT NOT TO BE FULLY LOCKED, GEAR SAFETY PIN COULD NOT BE INSTALLED. THE SAFETY PIN BUSHING ON THE LINK ROD HAD MIGRATED INTERFERING WITH THE SECONDARY STRUT. MAINTENANCE RESEATED BUSHING AND THE AIRCRAFT WAS FERRIED GEAR DOWN TO THE CLOSEST MAINTENANCE BASE FOR PERMANENT REPAIR. LINK ROD (P/N 20750), WAS REPLACED AND RETRACTION/EXTENSION CHECKS COMPLIED WITH. 2L72 4T RTA31SO 19950804004161995080400416SO 1995 8 4 COM11938 119950731A27503472001001 FLAP CONTL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01267CA6639 120259 OUTBD FLAPS WILL NOT RETRACT. REPLACED THE FLAP CONTROL UNIT. 2L72 4T RTA31SO 19950804004171995080400417SO 1995 8 4 COM11939 119950726A2820 PILOT VALVE EMB 120 EMB120RT SO RT FUEL SYST DEFECTIVE A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01189CA1337011812 120189 SERVICE DOOR WARNING ON CONTINUOUSLY. REPLACED THE RT FUEL VENT PILOT VALVE. 2L72 4T RTA31SO 19950804004181995080400418 1995 8 4 COM31126 419950728A34176224401001 AIR DATA COMP SAAB SF340 SF340A 7850100EU AVIONICS BAY DEFECTIVE A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01358CA9961 654 340A047 INFLIGHT LOST FLIGHT DIRECTOR BARS, RECEIVED RED FLIGHT DIRECTOR WARNING. REPLACED THE AIR DATA COMPUTER. 2L72 4T RTA52EU 19950804004191995080400419EU 1995 8 4 COM31127 119950730A29107229152 TUBING SAAB SF340 SF340A 7850100EU RT MLG CHAFED A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01356CA 340A034 HYDRAULIC FLUID LEAKING FROM RT MLG. REPAIRED CHAFE DAMAGE TO DOWN LOCK HYDRAULIC TUBING. 2L72 4T RTA52EU 19950804004201995080400420EA 1995 8 4 COM60529 119950730A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT/RT TE FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01937CA4656 719 7044 FLAPS FAILED AT ZERO DEGREES. REPLACED THE LT AND RT BPSU. 2L72 4F RTA21EA 19950804004211995080400421NM 1995 8 4 UPS403949 119950801A5711 SPAR WEB BOEING747 747SR46 NM WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND AT WING NR 3, 8 CRACKS AT THE FRONT SPAR WEB, BETWEEN THE INBD AND OUTBD UPPER LINK FITTING. REPAIRED IAW EO B747-5400-6500A. 2L74 4F A20WE 19950804004221995080400422NM 1995 8 4 UPS403950 119950801A5711 SPAR WEB BOEING747 747SR46 NM WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND AT WING NR 2, 6 CRACKS AT THE FRONT SPAR WEB, BETWEEN THE INBD AND OUTBD UPPER LINK FITTING. REPAIRED IAW EO B747-5400-6500A. 2L74 4F A20WE 19950804004231995080400423NM 1995 8 4 UPS403952 119950801A5753 T-CHORD BOEING747 747SR46 NM TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE IN AMSTERDAM FOR C-CK, MAINT FOUND RT OUTBD MIDFLAP ASSY UPPER REAR SPAR T-CHORD (P/N G5BCB532-4), IS CRACKED AND HAS LOCAL CORROSION. REPLACED IAW OHM 57-52-55. 2L74 4F A20WE 19950804004241995080400424WP 1995 8 4 UPS803953 119950729A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01783UP 45973 WHILE ON GROUND IN ORD, MAINTENANCE FOUND 1 INCH CRACK IN FUSELAGE IN POSITION 2. 2L74 4F RT4A25 19950804004251995080400425WP 1995 8 4 UPS803954 119950729A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01750UP 45950 WHILE ON GROUND IN ORD, MAINTENANCE FOUND 3 INCH CRACK ON RIGHT WING JUST OUTBD OF PANEL 520A AND .25 INCH CRACK ON LT FWD NLG WHEEL WELL CUTOUT. REPAIRED IAW EO DC8-5720-7265A, DC8-5330-4154. 2L74 4F RT4A25 19950804004261995080400426WP 1995 8 4 UPS803955 119950731A33505708458503 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01708UP 46048 WHILE ON GROUND IN BWI, MAINTENANCE FOUND EMER LIGHTS DEAD. REMOVED AND REPLACED EMER BATTERY PACK, OPS CK NORMAL. 2L74 4F RT4A25 19950804004271995080400427WP 1995 8 4 UPS803956 119950801A57425753054 FITTING DOUG DC8 DC873F 302199FWP NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-CK, MAINT FOUND .25 INCH CRACK AT NR 2 PYLON AND .75 CRACK AT NR 2 PYLON SUPPORT FITTINGS. REPLACED PER SRM 51-1-20 AND UPS EO DC8-57-580. 2L74 4F RT4A25 19950804004281995080400428WP 1995 8 4 UPS803957 119950801A57535652288505 VANE DOUG DC8 DC871F 302199DWP NR 2 TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CK, MAINT FOUND LT WING NR 2 FLAP VANE DELAM. REPLACED PER MM 27-51-14. 2L74 4F RT4A25 19950804004291995080400429EU 1995 8 4 AALA951104 119950615A3350A3060819104 EEL STRIP FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071439A 11434 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RT 19950804004301995080400430EU 1995 8 4 AALA951105 119950616A3350A3060819103 EEL STRIP FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071409B 11367 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT BY PAX SEAT ROW 11D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT ROW 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RT 19950804004311995080400431NM 1995 8 4 AALA951130 119950620A3350A3060719102 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07897AA 22013 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEATS ROWS 14D THROUGH 18D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PAX SEAT ROWS 14D THROUGH 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A3WE 19950804004321995080400432 1995 8 4 AALA951139 419950622A2565101623111 SLIDE BOEING767 767223 1385123NM ENTRY DOOR SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 LAX - DURING SLIDE SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE HAD NUMEROUS LEAKS AT UPPPER TUBE AND SEAM AREAS. SCRAPPED EMERGENCY EVACUATION SLIDE. (W) 2L72 4F RTA1NM 19950804004331995080400433WP 1995 8 4 AALA951143 119950623A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07271AA 49293 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 21D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PAX SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950804004341995080400434NM 1995 8 4 AALA951145 119950624A3350 EEL CONNECTORS BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS FROM PAX SEAT ROWS 8B TO 12B AND 7H TO 12H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTORS AT PAX SEATS 8B TO 12B AND 7H TO 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950804004351995080400435NM 1995 8 4 AALA951146 119950624A33508100022601 EEL ASSY BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 22B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 22B. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RTA1NM 19950804004361995080400436WP 1995 8 4 AALA951154 119950627A3350A3060719103 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07275AA 49272 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F A6WE 19950804004371995080400437EU 1995 8 4 AALA951163 119950627A2913862536 HYD PUMP FOKKERF28 F28MK0100 4990807EU NR 1 ENGINE FAILED A AALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW071440A 11435 OKC-ORD - FLT 1210 - DURING CRUISE, EXPERIENCED HYDRAULIC QUANTITY LOSS ON SYSTEM 1 AND HYDRAULIC QUANTITY LOW MESSAGE DISPLAYED ON MFDU. AC PROCEEDED TO ORD AND ACCOMPLISHED ALTERNATE LANDING GEAR AND FLAP EXTENSION, LANDING WITHOUT INCIDENT. REPLACED NR 1 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP DUE TO LEAKING O-RING AT PRESSURE LINE. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L72 4F RT 19950804004381995080400438SW 1995 8 4 MALA954496 119950607A33506104781 EEL BULBS SWRNGNSA227 SA227AC 8780603SW CABIN FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15430MA AC710 MSP - DURING WALKAROUND, THE FORWARD EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS HAD TWO BULBS INOPERATIVE. MAINTENANCE REPLACED THE LT AFT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804004391995080400439NM 1995 8 4 MALA954498 119950608A335010005511 EEL LAMP DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15819MA 251 DTW - FLT 3096 - DURING GATE WALKAROUND, MAINTENANCE PERSONNEL NOTED OVERHEAD EMERGENCY LIGHT IN COCKPIT DIMMED RAPIDLY AFTER BEING TURNED ON. MAINTENANCE REPLACED THE LAMP. THE SYSTEM PERFORMED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804004401995080400440EU 1995 8 4 MALA954502 119950610A33506008905 EEL BATT PACK FOKKERF27 F27MK200 4990620EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15278MA 10280 CWA - FLT 3260 - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE OVERHEAD CABIN EVACUATION LIGHTS TO BE DIM. REPAIRS WERE COMPLETED BY REPLACING THE EVACUATION LIGHT BATTERY PACK AT SEAT 3CD. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T A817 19950804004411995080400441NM 1995 8 4 MALA954503 119950609A2913570347 HYDRAULIC PUMP DHAV DHC8 DHC8102 2809003NM RT ENGINE INTERNAL FAULT A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15830MA 337 LEX - FLT 3390 - IN CRUISE, THE NR 2 ENGINE HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED AND THE NR 2 HYDRAULIC QUANTITY AND PRESSURE INDICATIONS WERE AT ZERO. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND RETURNED TO DTW. MAINTENANCE REPLACED THE NR 2 HYDRAULIC PUMP. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804004421995080400442SW 1995 8 4 MALA954504 119950612A57202735112 ANGLE SWRNGNSA227 SA227AC 8780603SW RT WING LOOSE A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 MSP - DURING A SCHEDULED INSPECTION, THE RT I/B WING TO NACELLE LOWER TRANSIT ANGLE HAD LOOSE RIVETS. REPAIRS WERE COMPLETED BY REPLACING THE ANGLE IAW FAC ARP 54-20-9101. (W) 1L72 4T A8SW 19950804004431995080400443NM 1995 8 4 MALA954505 119950615A52108SC0156 GAS SPRING DHAV DHC8 DHC8102 2809003NM PAX FAILED A MALAK NONE O OTHER TXTAXI/GRND HDL 1 GL15816MA 231 MSP - FLT 3408 - AFTER LANDING, FLIGHT ATTENDANT NOTED THAT THE PASSENGER DOOR WAS DIFFICULT TO UNLATCH. MAINTENANCE REPLACED A GAS SPRING ON THE LATCH ACTUATING ROD AND RERIGGED THE DOOR. THE SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804004441995080400444WP 1995 8 4 MALA954506 219950615A726131032172 OIL PUMP SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15426MA AC645 MSP - FLT 3272 - UPON CLIMBOUT, THE LT ENGINE RPM DROPPED TO 45 PERCENT, THE ENGINE STARTED TO NTS AND THE OIL PRESSURE DROPPED TO ZERO. THE ENGINE WAS SHUTDOWN THROUGH STOP AND FEATHER. THE AC RETURNED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE OIL PUMP. ENGINE OPERATED SATISFACTORILY. (W) 1L72 4T3 T A8SW E2WE 19950804004451995080400445 1995 8 4 MALA954507 419950615A612289741016 PROP GOVERNOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE FAILED A MALAO OTHER O OTHER CRCRUISE 1 GL15446MA AC693 FLT 3268 - DURING CRUISE, CREW NOTED A THUMPING NOISE FROM THE RT ENGINE, FOLLOWED BY A LOSS OF 200 RPM. THE FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RT PROP GOVERNOR. THE SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804004461995080400446NM 1995 8 4 MALA954508 119950617A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15826MA 330 DTW - FLT 3066 - DURING PREFLIGHT, CREW NOTED TWO LIGHTS IN THE FLOOR TRACK EMERGENCY LIGHTING SYSTEM TO BE INOPERATIVE. MAINTENANCE REPLACED FOUR FLOOR TRACK EMERGENCY LIGHT BATTERY PACKS. THE SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804004471995080400447NM 1995 8 4 MALA954509 119950620A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15802MA 245 DTW - DURING PREFLIGHT FOR A MAINTENANCE TEST FLIGHT, TWO BULBS IN FLOOR TRACK LIGHTING WERE INOPERATIVE. MAINTENANCE REPLACED AN EMERGENCY LIGHT BATTERY PACK. THE SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T RTA13NM 19950804004481995080400448SW 1995 8 4 MALA954518 119950627A53202722081 DOOR SILL SWRNGNSA227 SA227AC 8780603SW FS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE AFT CARGO DOOR SILL (P/N 27-2208-1) AT FS 438 TO BE CRACKED AT THE RADIUS CUTOUT FOR THE FUSELAGE FRAME. REPAIRS WERE COMPLETED BY INSTALLING REPAIR DOUBLERS IAW FAC ARP 53-30-9507. (W) 1L72 4T A8SW 19950804004491995080400449SW 1995 8 4 MALA954525 119950630A3260ML345 POSITION SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL1527465 AC755B FLT 3271 - MSP - DURING APPROACH, LT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN. THE FLIGHT CONTINUED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MAIN LANDING GEAR UP POSITION SWITCH. THE SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804004501995080400450EU 1995 8 4 MALA954527 119950704A33506008905 EEL BATT PACK FOKKERF27 F27MK200 4990620EU CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15278MA 10280 CWA - DURING SCHEDULED MAINTENANCE, MECHANICS FOUND THE FORWARD EVACUATION LIGHT WOULD ILLUMINATE WHENEVER THE AC POWER AND EVACUATION LIGHT SWITCH WAS SELECTED TO THE OFF POSITION. MAINTENANCE REPLACED THE BATTERY PACK AT CABIN SEAT POSITION ROW 3. SYSTEM OPERATED SATISFACTORILY. (W) 2H72 4T A817 19950804004511995080400451SW 1995 8 4 MALA954528 119950628A2431 CONNECTOR SWRNGNSA227 SA227AC 8780603SW BATT TEMP SYST FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15425MA AC640 YNG - FLT 3360 - IN CRUSIE, THE LT TEMP WARNING LIGHT ILLUMINATED. THE CREW DISCONNECTED THE LT BATTERY AND THE TEMPERATURE CONTINUED TO INDICATE A HIGH TEMPERATURE. THE AC RETURNED TO DTW. MAINTENANCE REPLACED THE CANNON PLUG AT THE BATTERY. SYSTEM OPERATED SATISFACTORILY. (W) 1L72 4T A8SW 19950804004521995080400452NE 1995 8 4 RAIA950701 219950703A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114A 01514NE RT LOW TORQUE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03551HK 41040 STL - FLT 7534 - THE RT ENGINE ONLY ACHIEVED 93 PERCENT TORQUE AS OPPOSED TO 97 PERCENT TARGET TORQUE. MAINTENANCE REMOVED AND REPLACED RT ENGINE AS PER GARRETT TPE33114A MM 72-00-00. POWER RUNS REVEAL ALL PARAMETERS OK. (W) 2L72 4T4 TRTA41NM E18NE 19950804004531995080400453EU 1995 8 4 RAIA950708 119950712A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03337TE 929 CMI - FLT 7439 - THE LT ENGINE WILL NOT MAKE TORQUE. MAINTENANCE ADJUSTED LT ENGINE TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND POWER RUNS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950804004541995080400454EU 1995 8 4 RAIA950709 119950713A29101379305A77 HYD LINE BAG JETSTMJETSTM3201 1500217EU RT ENGINE CHAFED A RAIAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03342TE 954 SBN - FLT 7494 - LOST ALL HYDRAULIC PRESSURE ON RT ENGINE. CREW PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CHAFED HYDRAULIC LINE ON RT ENGINE HYDRAULIC PUMP. (W) 2L72 4T RTA56EU 19950804004551995080400455EU 1995 8 4 RAIA950710 119950713A7931EO32CFR1005SN CONNECTOR AEROSPATR42 ATR42300 8680920EU RT ENGINE DIRTY A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03425TE 125 STL - FLT 7400 - THE RT OIL PRESSURE FLUX 65 TO 45 PSI ON TAKEOFF. MAINTENANCE CLEANED RT OIL PRESSURE TRANSMITTER SWITCH CONNECTOR. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2H72 4T RTA53EU 19950804004561995080400456NE 1995 8 4 RAIA950711 219950713A72612380 OIL QTY AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE RT ENGINE REQD SERVICE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03722TE 220 STL - FLT 7019 - THE RT OIL PRESSURE FLUX ON TAKEOFF. MAINTENANCE SERVICED RT ENGINE WITH OIL. UPON INSPECTION FOR A OIL LEAK, NO LEAK WAS NOTED. ENGINE IS PLACED ON A OIL CONSUMPTION WATCH. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2H72 4T4 TRTA53EU E2ONE 19950804004571995080400457SO 1995 8 4 RAIA950712 119950714A27201206P011401 PRESS SWITCH EMB 120 EMB120RT SO RUDDER FAILED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03125AM 120017 STL - FLT 7251 - BOTH RUDDER INOP LIGHTS ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED RUDDER PRESSURE SWITCH. SYSTEM CHECKED GOOD. (W) 2L72 4T RTA31SO 19950804004581995080400458NE 1995 8 4 RAIA950713 219950716A7200 ENGINE AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE LT OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03721TE 217 STL - FLT 7522 - THE LT ENGINE TORQUE WOULD ONLY MAKE 35 PERCENT TORQUE. MAINTENANCE TRIMMED LT ENGINE. GROUND RUNS REVEALED NORMAL OPERATION. (W) 2H72 4T4 TRTA53EU E2ONE 19950804004591995080400459NE 1995 8 4 RAIA950714 219950714A73207863927 HMU AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LT ENGINE MALFUNCTIONED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03421TE 102 STL - FLT 7126 - LT ENGINE LOW POWER, 28 PERCENT TQ. MAINTENANCE REPLACED LT ENG HYDROMECHANICAL UNIT AS PER PWC MM 72-40-00. GROUNDS RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (W) 2H72 4T4 TRTA53EU E20NE 19950804004601995080400460EU 1995 8 4 RAIA950715 119950716A32609EN1C11HB2BB2 UPLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NLG LACK OF LUBE A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03422AM 856 STL - FLT 7260 - NOSE WHEEL INTRANSIT LIGHT WILL NOT EXTINGUISH AFTER TAKEOFF. MAINTENANCE CLEANED AND LUBED NOSE GEAR UPLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950804005361995080400536NE 1995 8 4 95ZZZX3583 219950713A732189777012 FUEL CONTROL MTSBSIMU2 MU2B36 5780412CE GARRTTTPE331TPE3316252M 01514NE ENGINE FAILED A MCCAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 SW11103RC 673 P20418C ENGINE LOST FUEL FLOW IN CRUISE FLIGHT. ENGINE SHUT-DOWN AND FEATHERED. TROUBLESHOOTING DETERMINED FUEL CONTROL FAILED. THE FUEL CONTROL UNIT HAD APPROXIMATELY 450 HOURS SINCE REPAIR BY WOODWARD. 1H72 3T RTA10SW E2WE 19950804005491995080400549SW 1995 8 4 95ZZZX3598 119950622A55202743042001 FITTING SWRNGNSA227 SA227AC 8780603SW ELEV BRG MT WORN A PNSAK NONE O OTHER ININSP/MAINT 1 AL03640PA10000 AC759B BEARING MOUNT AND CAP WORN AND LOOSE ALLOWS ELEVATOR TO 'BUZZ' IN-FLIGHT. SUSPECT MOUNT AND CAP WERE SLIGHTLY OVERSIZED FROM FACTORY. HAVE OTHER AIRCRAFT IN FLEET WITH MORE THAN TWICE THE HOURS ON THIS PART WITH NO LOOSENESS DETECTED. 1L72 4T A8SW 19950804005541995080400554CE 1995 8 4 95ZZZX3604 119950620A29102607003493 LINE LEAR 25 25D 5170514CE STANDBY HYD RUPTURED A DSCAK NONE K FLUID LOSS NRNOT REPORTED 1 GL25725DM3891 328 PRESS LINE COMING FROM STANDBY HYDRAULIC PUMP AT THE EDGE OF AN819 SLEEVE HAD CRACKED AND RUPTURED CAUSING TOTAL HYD FAILURE. THE OPPOSITE END OF TUBE HAD A SMALL CRACK AT THE SAME LOCATION, BUT HAD NOT RUPTURED. THIS WAS THE SECOND TIME A LINE HAD CRACKED AND RUPTURED. THE LAST OCCASION WAS AT THE CROSS ON PRESS LINE. LEAR JET HAS HEX LINE FOR REPLACEMENT. SUBMITTER SHOULD HAVE A BULLETIN ISSUED. 2L72 4J A10CE 19950804005551995080400555NM 1995 8 4 95ZZZX3605 119950307A532065C3449035 FITTING BOEING737 737205 NM BS 695 LT CRACKED B EE4YK NONE O OTHER ININSP/MAINT 1 SO2373TH 21729 FOUND BS 695, LEFT FRAME LOWER FITTINGS, WITH CRACKS ON WEB RADIUS AND ON THE OUTBOARD VERTICAL FLANGE. NOTE: THIS FITTING ATTACHES TO MAIN LANDING GEAR LINK SUPPORT BEAM TO BODY FRAME. 2L72 4F A16WE 19950804005631995080400563NM 1995 8 4 9511546716 119950728A2612 CONNECTOR BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 4 ENG CONTAMINATED A NWAAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. JM WARNING INDICATION OVER TEMP CRCRUISE 1 GL01616US 21120 689631 DURING CRUISE, THE NR 4 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BOTH TEMPERATURE LOOPS WERE READING FULL SCALE. THE ENGINE WAS SHUT DOWN. THE LEFT FIRE BOTTLE WAS DISCHARGED AND THE FLIGHT CONTINUED TO NRT WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. A METACAL WAS REMOVED FROM THE LOWER FIRE LOOP CONNECTORS AND THE SYSTEM OPERATIONS THEN CHECKED OK. 2L74 4F4 F A20WE E20EA 19950804005641995080400564NM 1995 8 4 9511552705 119950731A3260 TARGET SENSOR BOEING727 727225 1384077NM LT MLG LACK OF LUBE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01802EA 22433 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR INDICATION REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH PROPER INDICATION. BOS MAINTENANCE CLEANED LEFT GEAR TARGET SENSOR AND GREASED UPLOCK HOOK. 2L73 4F A3WE 19950804005651995080400565NM 1995 8 4 DL72S953227 119950731A5754651622294 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 ITEM NR 1, .5 INCH CRACK IN NR 14 RIB. REPAIRED PER M/M 57-54-0. ITEM NR 2, .25 INCH CRACK AT ANTI-ICE DUCT CUTOUT. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT AT SHOP VISIT. 2L73 4F A3WE 19950804005661995080400566NM 1995 8 4 DL72S953228 119950731A5754651622294 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 A .5 INCH CRACK UPPER/FWD END OF RIB NR 10. REPAIRED PER M/M 57-54-0, FOUND AT SHOP VISIT FOR NR 6 L/E SLAT. 2L73 4F A3WE 19950804005671995080400567NM 1995 8 4 DL72S953233 119950730A3350 EEL 1000677 BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11516DA 4026 21432 INTERIOR EMERGENCY EXIT SIGN ABOVE LEFT FWD ENTRY DOOR DID NOT ILLUMINATE ON EMERGENCY EXIT LIGHTS CHECK. REPLACED EMERGENCY EXIT LIGHT ASSY AND BATTERIES. GRD CHECKS OK ON TEST. 2L73 4F A3WE 19950804005681995080400568NM 1995 8 4 DL72S953237 119950628A5753652163396A LE SKIN BOEING727 727232 1384082NM NR 4 TE MIDFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT INBD EDGE OF FLAP. REPAIRED PER SRM 57-52-0 PG 808. 2L73 4F A3WE 19950804005691995080400569NM 1995 8 4 DL72S953238 119950628A5753652163396A LE SKIN BOEING727 727232 1384082NM NR 4 TE MIDFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 DURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH WEAR DAMAGE TO L/E SKIN AT O/B END OF FLAP. REPAIRED PER SRM 57-52-0 PG 808. 2L73 4F A3WE 19950804005701995080400570NM 1995 8 4 DL72S953243 119950731A5320 WEB BOEING727 727232 1384082NM BS 870 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11468DA 20745 A 2.5 AND 1 INCH CRACK BELOW LOAD CONTROL VALVE CUTOUT, BS 870 WEB RT WW. FOUND AT D-1 LTR CK. REPAIRED PER SRM 53-10-9. 2L73 4F A3WE 19950804005711995080400571NE 1995 8 4 DL72S953248 219950731A7200JT8D15 ENGINE BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 3 FAILED A DALAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SO11539DA61680 22385 685565 AT 3,5000 FT NR 3 ENGINE ROLLED BACK TO IDLE AND THEN SHUTDOWN, RETURNED SLC. PERFORMED ENGINE INSPECTION AND RUNUP PER PREFLIGHT HANDBOOK COULD NOT FIND ANY DISCREPANCIES. RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950804005721995080400572NM 1995 8 4 DL72S953249 119950731A3350900835A EEL BATTERY PACK BOEING727 727232 1384082NM CARGO DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11523DA 21583 RT AFT CARGO DOOR EMERG LIGHT INOP. REPLACED BATT PACK M957. OPS CK GOOD. 2L73 4F A3WE 19950804005731995080400573NM 1995 8 4 DL72S953251 119950727A5754 SKIN BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NR 4 L/E SLAT SKIN CRACKED AT I/B TRACK ATTACH POINT. CUT AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER PER MM 57-54-0 PG 821. INSTALLED REPAIR DOUBLER AS PER MM 57-54-0 PG 821 FIG 815, FOUND AT HMV. 2L73 4F A3WE 19950804005741995080400574NM 1995 8 4 DL72S953255 119950731A5620 WINDOW PA6556705AR BOEING727 727232 1384082NM CABIN SHATTERED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 SO11482DA 20862 DURING CRUISE, RIGHT FORWARD OVERING EXIT DOOR WINDOW OUTER PANE SHATTERED AND DEPARTED AIRCRAFT, LANDED DEN. WINDOW WAS REPLACED. REMAINS OF SHATTERED WINDOW ROUTED TO ENGINEERING FOR EVALUATION. 2L73 4F A3WE 19950804005751995080400575NM 1995 8 4 DL72S953256 119950731A3350 EEL CONNECTOR 10617842 BOEING727 727232 1384082NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11494DA 21074 LT OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE DURING MTC CHECK. RELAMPED, NO HELP. RESEATED CANNON PLUG, OPERATION NORMAL. 2L73 4F A3WE 19950804005761995080400576NM 1995 8 4 DL72S953269 119950626A3040518647 CONNECTOR BOEING727 727232 1384082NM LT 1 WINDSHIELD LOOSE A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11518DA 21469 DURING CRUISE, WIRING CONNECTION AT TOP LEFT CORNER OF L-1 WINDSHIELD BEGAN TO SPARK AND BURN. SHUT OFF POWER ARCING STOPPED. FOUND TERMINAL CONNECTION VERY LOOSE. REPLACED TERMINAL DUE TO ARCING DAMAGE. OPERATION NORMAL. 2L73 4F A3WE 19950804005771995080400577NM 1995 8 4 DL72W953258 119950622A5753652163253 MIDFLAP BOEING727 727247 138408FNM NR 2 MIDFLAP CRACKED CHORD A DALAK NONE O OTHER ININSP/MAINT 1 SO11292WA 22110 00000 AFT CHORD CRACKED AT IB AFT FLAP DRIVE ROD CUTOUT. CRACK WAS REPAIRED PER MM 57-52-0 FIG 802, BY STOP DRILLING AND INSTALLING A DOUBLER. FOUND DURING SHOP VISIT FOR NR 2 MIDFLAP. 2L73 4F A3WE 19950804005781995080400578WP 1995 8 4 DLL10953239 119950707A53301503540 SKIN LKHEED1011 10113851 5265010WP FS 1363-1453 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 DURING INSPECTION OF THE LOWER BELLY SKIN AREA, THE LOWER FUSELAGE SKIN FROM FS 1363 TO 1453 WAS FOUND TO HAVE AREAS OF SEVERE CORROSION. ACCOMPLISHED REPAIRS PER DL ERA 270760-14. 2L73 4F A23WE 19950804005791995080400579WP 1995 8 4 DLL10953242 119950711A53301503140 SKIN LKHEED1011 10113851 5265010WP BS 529-983 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THE FORWARD LOWER BELLY SKIN WAS FOUND WITH EXTENSIVE CORROSION BETWEEN FS 529 AND FS 983, STR 29 TO STR 42. ALSO, THERE ARE NUMEROUS EXISTING EXTERNAL REPAIRS ON THE SKIN IN THIS AREA. DUE TO THE EXTENSIVE NATURE OF THE CORROSION AND EXISTING REPAIRS, REPLACEMENT OF LARGE AREA OF THE FORWARD BELLY SKIN WILL BE REQUIRED. ACCOMPLISHED REPAIRS PER DL ERA 271106-14. 2L73 4F A23WE 19950804005801995080400580WP 1995 8 4 DLL10953244 119950627A53301503543 SKIN LKHEED1011 10113851 5265010WP FS 1453-1655 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 FUSELAGE SKIN BETWEEN FS 1453 AND FS 1655 BETWEEN STR 24 AND STR 37 REQUIRES REPLACEMENT, DUE TO EXTENSIVE CORROSION AND NUMEROUS REPAIRS. ACCOMPLISHED REPAIRS PER DL ERA 271107-14. 2L73 4F A23WE 19950804005811995080400581WP 1995 8 4 DLL10953245 119950622A53201520384 SILL LKHEED1011 10113851 5265010WP C-2 DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 C-2 DOOR SURROUND STRUCTURE LOWER SILL OUTER CAP WAS FOUND CORRODED ON THE OUTBOARD HORIZONTAL FLANGE OF THE CAP AT STATION 1625. ACCOMPLISHED REPAIRS PER DL ERA 271113-14. 2L73 4F A23WE 19950804005821995080400582WP 1995 8 4 DLL10953246 119950621A57111503231 SPAR CAP LKHEED1011 10113851 5265010WP FS 1163 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THE CENTER WING FS 1163 INTERMEDIATE SPAR UPPER CAP HAS A CRACK IN THE FWD LEFT AND RIGHT OUTBOARD ENDS. ACCOMPLISHED REPAIRS PER DL ERA 271114-14. 2L73 4F A23WE 19950804005831995080400583WP 1995 8 4 DLL10953247 119950614A53301513977 TRIPLER LKHEED1011 10113851 5265010WP R1 DOOR OPENING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 A CRACK WAS FOUND IN THE AFT EDGE OF THE R-1 DOOR SURROUND TRIPLER BELOW WL 220. ACCOMPLISHED REPAIRS PER DL ERA 271153-14. 2L73 4F A23WE 19950804005841995080400584WP 1995 8 4 DLL10953253 119950726A2120 AIR DISTR LKHEED1011 10113851 5265010WP CABIN ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11722DA 193C1147 ON CLIMBOUT, HAD BURNING ODOR IN CABIN WITH LAV SMOKE DETECTORS ACTIVATED, RETURNED ATL. REPLACED ALL WATER SEPARATOR BAGS AND RAN PACKS OPERATION NORMAL. PERFORMED DUCT CLEANING PER MM 36-00-00 PG 701. OPERATION NORMAL. 2L73 4F A23WE 19950804005851995080400585WP 1995 8 4 DLL13953229 119950704A5320 TEAR STRAP LKHEED1011 10113851 5265010WP STR 38 DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND TEAR STRAP DELAMINATED AT STRINGER 38. REPAIRED PER SRM 53-31-00 PG 803. 2L73 4F A23WE 19950804005861995080400586WP 1995 8 4 DLL13953240 119950620A57111507722 REAR SPAR LKHEED1011 10113851 5265010WP CENTER WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 WHILE ACCOMPLISHING EO 7-59040-3 STRUCTURAL MODIFICATION TO THE REAR SPAR JOINT AT THE BL 115 WING ROOT RIBS, CRACKS WERE FOUND IN THE CENTERWING REAR SPAR WEB TO BL 115 RIB WEB ATTACH ANGLE EMANATING FROM EXISTING ATTACHMENT HOLES. THE CRACKING IS PRESENT ON BOTH THE SPAR WEB AND THE RIB WEB ATTACH FLANGES. ACCOMPLISHED REPAIRS PER DL ERA 270996-14. 2L73 4F A23WE 19950804005871995080400587WP 1995 8 4 DLL13953259 119950711A53201521685101 FITTING LKHEED1011 10113851 5265010WP FS 1501 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 00000 HMV - FRW AND AFT OUTFLOW VALVE SUPPORT FITTINGS CORRODED IN C-2 B/B. REPLACED P/N 1521684-101 AND 1521685-101 FITTINGS, REF DWG 1521682. 2L73 4F A23WE 19950804005881995080400588WP 1995 8 4 DLL15953270 119950623A25302361 CHILLER UNIT LKHEED1011 10113853 5265020WP FWD GALLEY FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11752DA 193W1172 DURING CRUISE, HAD SMOKE ODOR IN F/C GALLEY WITH C/B FOR CHILLER POPPED. CHILLER WAS REPLACED, OPERATION NORMAL. 2L73 4F A23WE 19950804005891995080400589NM 1995 8 4 DLM88953222 119950730A323139567851 LINK DOUG MD88 MD88 3023688NM NLG DOOR BROKEN A DALAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 SO11974DL 53242 ON DEPARTURE FROM SAN, NOTED VIBRATIONS DURING LDG GEAR RETRACTION. FOUND RT NOSE GEAR FWD DOOR LINK BROKEN. REPLACED LINK PER MM 32-22-01 PG 203 TO 204. GEAR RETRACTION NORMAL. 2L72 4F RTA6WE 19950804005901995080400590WP 1995 8 4 MWEA95245 119950731A77208T851B3 EGT BAL RESISTOR DOUG DC9 DC914 3022034WP LT ENGINE FAILED A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31600ME 45725 PILOT REPORTS ON CLIMBOUT FROM MKE, THE LEFT ENGINE EGT WENT DOWN TO 350 AND REMAINED FOR A SHORT TIME, THEN WENT DOWN TO 50 UNTIL RETURN TO MKE. ALL OTHER PARAMETERS NORMAL. MAINTENANCE INSPECTED LEFT ENGINE EGT SYSTEM, TESTED WITH BARFIELD EGT TEST BOX. REPLACED LEFT BALANCING RESISTOR. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950804005911995080400591WP 1995 8 4 MWEA95246 119950731A33105956888503 LIGHT CONT DOUG DC9 DC932 3022066WP COCKPIT INOP A MWEAHD DEACTIVATE SYST/CIRCUITSRETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31502ME 48132 CREW REPORTS WHILE TAXIING OUT FOR TAKEOFF, SMOKE AND FUMES CAME OUT FROM BEHIND THE CENTER PEDESTAL LIGHT CONTROL UNIT. PULLED APPLICABLE CIRCUIT BREAKERS, THE SMOKE STOPPED. RETURNED TO GATE AT DFW. MAINTENANCE CONTROL DEFERRED LIGHTING SYSTEM, A/C RETURNED TO MKE. MAINTENANCE REPLACED CENTER INSTRUMENT PANEL AND PEDESTAL LIGHT CONTROL UNIT. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950804005921995080400592NM 1995 8 4 UPS203969 119950802A5330 SKIN BOEING727 72722C 138400FNM BS 1080 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND BULGE ON BUTT JOINT BS 1080 STR 16 RT. REPAIRED PER SRM 53-30-3 - FIGURE 3.A.J. SHEET 3. 2L73 4F A3WE 19950804005931995080400593NM 1995 8 4 UPS203970 119950802A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 500-520 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND CRACKED SEAT TRACK BBL 45.5 LT, BS 500 THROUGH BS 520. SEAT TRACK REPLACED PER SRM 53-10-5, FIG. 7. 2L73 4F A3WE 19950804005941995080400594NM 1995 8 4 UPS203971 119950802A7120 CONE BOLT BOEING727 72722C 138400FNM NR 2 ENG GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND NR 2 ENGINE, LT FWD MOUNT CONE BOLT NOT SITTING PROPERLY. NEW CONE BOLT INSTALLED AND INSPECTION CARRIED OUT PER E.O. 95-10-003. 2L73 4F A3WE 19950804005951995080400595NM 1995 8 4 UPS203972 119950802A5314 KEEL WEB BOEING727 72722C 138400FNM BS 788-828 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01941UP 19196 WHILE IN SHANNON, IRELAND FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT KEEL BEAM WEB AT BS 790-828 (INNER AND OUTER). OUTER WEB REPAIRED PER SRM 51-40-2, FIGURE 1. INNER WEB REPAIRED PER SRS E.O. 95-10-001. 2L73 4F A3WE 19950804005961995080400596NM 1995 8 4 UPS203973 119950801A291072709 CHECK VALVE BOEING727 72727C 138400JNM HYD SYS INOP A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01909UP 19115 AFTER TAKEOFF, OIL FUMES APPEARED ON FLIGHT DECK. REMOVED AND REPLACED PNEUMATIC CHECK VALVES. RAN PACK. NO ODOR PRESENT. 2L73 4F A3WE 19950804005971995080400597NM 1995 8 4 UPS203974 119950801A2150 PACK BOEING727 72727C 138400JNM LEFT MALFUNCTIONED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01924UP 19115 ON CLIMB-OUT, CREW NOTICED BURNING SMELL ON CLIMB OUT LT COOLING DOOR AUTOMATICALLY OPENED. OPENED BOTH COOLING DOORS AND SMELL SUBSIDED. BOTH PACKS WERE OPERATED AT 115 DEGREES JUST ABOVE GREEN BAND. ON CLIMB-OUT, CPT NOTICED DPU FLAGS. RAN BOTH PACKS AND SELF-TEST ON EFIS. NO DEFECTS OR SMELLS NOTICED. 2L73 4F A3WE 19950804005981995080400598WP 1995 8 4 UPS803958 119950802A5320561228R341 SUB FLOOR DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, HVY. CORR. DAMAGE ON FLT DECK SUB-FLOOR PRESSURE PANEL. REPAIRED PER E.O. DC8-5310-7237-A. 2L74 4F RT4A25 19950804005991995080400599WP 1995 8 4 UPS803959 119950802A533057503223 SKIN DOUG DC8 DC871F 302199DWP BS 1050-1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, HVY. CORR. DAMAGE AND BULGES AT FUSELAGE BELLY SKIN, FS 1050 - 1350. REPLACED PER DAC DRAWING 570322 AND SRM 51-1-20D. 2L74 4F RT4A25 19950804006001995080400600WP 1995 8 4 UPS803960 119950802A531357799139 LONGERON DOUG DC8 DC871F 302199DWP BS 520-540 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, HVY. CORR. AT LONGERON 33R, FS 520-540. REPAIRED PER E.O. DC8-5310-7236-A. 2L74 4F RT4A25 19950804006011995080400601WP 1995 8 4 UPS803961 119950802A532037558242 FITTING DOUG DC8 DC871F 302199DWP BS 280 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MODERATE CORR. ON B/T FITTING, FS 280, BETWEEN LONGERONS 34R-33R (AFT SIDE). REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950804006021995080400602WP 1995 8 4 UPS803962 119950802A53203754023 FITTING DOUG DC8 DC871F 302199DWP BS 300/320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR. AT DOOR FITTING, FS 300 AND 320, BETWEEN LONGERON 33R-A AND 33L. REPLACED PER SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 19950804006031995080400603WP 1995 8 4 UPS803963 119950802A53200327075T6 FITTING DOUG DC8 DC871F 302199DWP BS 1510-1530 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR. AT FINGER DOUBLER FS 1510-1520, LONGERONS 31R-29R. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950804006041995080400604WP 1995 8 4 UPS803964 119950802A53135753744501 LONGERON DOUG DC8 DC871F 302199DWP BS 1270-1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR. AT LONGERSON 31L, FS 1270-1280 AND FS 1350. REPAIRED PER E.O. DC8-5310-7244A AND DC8-5310-7240-A. 2L74 4F RT4A25 19950804006051995080400605WP 1995 8 4 UPS803965 119950802A53203754930 FITTING DOUG DC8 DC871F 302199DWP BS 1200/1205 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR. ON T-FITTINGS, NR 5, FS 1205 AND FS 1200 AND NR 4 FS 1195, LONGERON 33R. REPLACED PER SRM 53-2-0 AND SRM 51-1-20D. 2L74 4F RT4A25 19950804006061995080400606WP 1995 8 4 UPS803966 119950802A5320603057107576 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 1020 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, SHEAR TIE HAS CORR AT FS 1020, BETWEEN LONGERONS 35L-36. REPLACED PER SRM 51-1-20D. 2L74 4F RT4A25 19950804006071995080400607WP 1995 8 4 UPS803967 119950802A53206030571075T6 FITTING DOUG DC8 DC871F 302199DWP BS 160 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, T-FITTING HAS CORR. AFT SIDE OF FS 160, LONGERON 21R. REPLACED SRM 51-1-20D. 2L74 4F RT4A25 19950804006081995080400608WP 1995 8 4 UPS803968 119950802A53115754671 FRAME DOUG DC8 DC871F 302199DWP BS 1140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, CORR. ON BELT FRAME LOWER FWD LIP FS 1140, LONGERON 35L-36. REPAIRED PER DC8-5310-7238-A. 2L74 4F RT4A25 19950804006331995080400633EA 1995 8 4 95ZZZX3631 219950706A7200 ENGINE PIPER PA31T PA31T 7103124SO PWA PT6 PT6A28 EA LEFT POSITION FAILED A XPCAO OTHER Y ENGINE STOPPAGE TOTAKEOFF 1 WP11111KV4542 1840 31T7920035 51939 LEFT ENGINE QUIT ON TAKEOFF. ENGINE SUBJECT TO EVALUATION/CAUSE OF FAILURE BY MANUFACTURER. 1L72 3T4 T A8EA E4EA 19950804006451995080400645EA 1995 8 4 95ZZZX3643 219950711A8550 HOSE PIPER PA60 PA60601P 7106012NM LYC O540 IO540S1A5 41532EA OIL RETURN LOOSE A GXPAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS NRNOT REPORTED 1 GL23601GA 61P0282064 AN OIL RETURN HOSE FROM THE TURBOS CAME LOOSE SPRAYING OIL ONTO THE FIRE DETECTION PROBES. THIS CAUSED THE FIRE WARNING TO ACTIVATE, AND THE PILOT WENT INTO THE CLOSEST AIRPORT. THERE WAS NO DEFECT FOUND WITH THE HOSE OR 'AN' FITTING IT ATTACHED TO. THE HOSE WAS TIGHTENED AND PROBLEM SOLVED. NO RECOMMENDATION FOR CORRECTIVE ACTION. 1M72 3O3 ORTA17WE 1E4 19950804006591995080400659WP 1995 8 4 9511561224 119950630A5330 SKIN DOUG DC10 DC1030 3023501WP FS 808-824 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01224NW 46581 DURING LINE CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 808 - 824, LONGERONS 37L - 38L. REPAIRED SKIN AND LONGERON 38L PER EA 12-99010. 2L73 4F A22WE 19950804006601995080400660WP 1995 8 4 9511579103 119950710A5330 TEAR STRAP DOUG DC9 DC915 3022036WP FS 700 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0193S 47078 DURING H-CHECK, FOUND A CRACK IN THE TEAR STRAP AT FS 700, LONGERON 1. REPAIRED PER EA 91-98412. 2L72 4F A6WE 19950804006611995080400661WP 1995 8 4 9511581155 119950711A5347 TRACK DOUG DC10 DC1040 3023508WP FS 435-450 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE LBL 27.5 SEAT TRACK AT FS 435 - 450. REPAIRED TRACK (P/N ABA 7684-503) PER EA 11-82931. 2L73 4F A22WE 19950804006621995080400662WP 1995 8 4 9511591155 119950714A5315 FLOOR BEAM DOUG DC10 DC1040 3023508WP FS 791 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CRACKS AND CORROSION ON THE FS 791 FLOOR BEAM AT X16, X14. REPAIRED BEAM (P/N ADA 7226-13) PER EA 11-99045. 2L73 4F A22WE 19950804006631995080400663WP 1995 8 4 9511601155 119950715A5330 SKIN DOUG DC10 DC1040 3023508WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD RADIO ALTIMETER MOUNTING RINGS. REPAIRED BOTH PER EA 11-98579. 2L73 4F A22WE 19950804006641995080400664WP 1995 8 4 9511611155 119950719A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1139 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1139, LONGERON 43L - 47L. REPAIRED SKIN (P/N AYB 7065-1) PER EA 11-99040. 2L73 4F A22WE 19950804006651995080400665WP 1995 8 4 9511621155 119950722A5330NDA6276 SKIN DOUG DC10 DC1040 3023508WP FS 1129 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND FINGER DOUBLERS FS 1129 AT LONGERON 48R. REPAIRED PER EA 11-98907. 2L73 4F A22WE 19950804006661995080400666WP 1995 8 4 9511631155 119950722A5315 FLOOR BEAM DOUG DC10 DC1040 3023508WP FS 1178 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND A CRACK IN THE FS 1178 FLOOR BEAM AT RBL 104. REPAIRED BEAM (P/N AEA 0361) PER EA 11-99038. 2L73 4F A22WE 19950804006671995080400667WP 1995 8 4 9511641155 119950724A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1510-1531 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE UNDERWING BARREL SKIN FS 1510 - 1531, LONGERON 51L - 51R. REPAIRED SKIN (P/N AYB 7065) PER EA 11-82926. 2L73 4F A22WE 19950804006681995080400668EU 1995 8 4 95UAL900075 119950801A3350 EEL BATTERY AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29418UA 485 EMERG EXIT LIGHTS BEGAN FLASHING AT DOORS 1L AND 1R AND WERE ON STEADY AT 2L AND 2R. RESET CIDS AND 1L AND 1R WORKED NORMAL, BUT COULD NOT CORRECT 2L AND 2R. REPLACED EMERGENCY POWER UNIT AND BATTERY. TEST OF EPSU REVEALED UNIT OK. 2L72 4F RTA28NM E40NE 19950804006691995080400669NM 1995 8 4 95UAL900076 119950801A3350 EEL CABLE BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29903UA 25003 FIRST CLASS EEL LIGHTING INOP. REPLACED POWER LEADER CABLE FROM INVERTER TO EEL LIGHTING. 2L72 4F4 FRTA16WE E2GL 19950804006701995080400670NM 1995 8 4 95UAL900077 119950801A3350 EEL BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29998UA 22741 RIGHT OVERWING ESCAPE PATH AFT LIGHT NEAR AFT CARGO DOOR INOP. REPLACED LIGHT ASSY. 2L72 4F4 F A16WE E2EA 19950804006711995080400671NM 1995 8 4 95UAL900078 119950801A2560 SLIDE BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE R2 DOOR FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29556UA 26650 RT NR 2 SLIDE PRESSURE WILL NOT TEST IN COCKPIT. REPLACED SLIDE BOTTLE. 2L72 4F4 FRTA2NM E17NE 19950804006731995080400673 1995 8 4 95UAL900080 419950803A2565 SLIDE BFG 7A14371 BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP294718U 19879 SLIDE FAILED AIR RETENTION TEST. SCRAPPED SLIDE. 2L74 4F4 F A20WE E20EA 19950804006741995080400674WP 1995 8 4 ABXA9500585 119950707A5320595296528 DOUBLER DOUG DC9 DC931 3022065WP RT WINDOW FRAME CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF A.D. 90-80-3; S.B. 56-11, X-RAY INDICATED A CRACK IN THE RIGHT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965. 2L72 4F A6WE 19950804006751995080400675WP 1995 8 4 ABXA9500586 119950707A5320595296527 DOUBLER DOUG DC9 DC931 3022065WP LT WINDOW FRAME CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF A.D. 90-18-3; S.B. 56-11, X-RAY INDICATED CRACK IN THE LEFT EYEBROW WINDOW RETAINER. REPLACED DOUBLER IAW DOUGLAS REWORK DRAWING 5952965. 2L72 4F A6WE 19950804006761995080400676WP 1995 8 4 ABXA9500588 119950612A5280ATY54QW ATTACH ROD DOUG DC9 DC931 3022065WP LT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD LANDING GEAR DOOR LATERAL ATTACH ROD, ROD WORN. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804006771995080400677WP 1995 8 4 ABXA9500589 119950613A5280S24312155A BUSHING DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT OUTBOARD LANDING GEAR DOOR LATERAL ATTACH ROD ATTACH PLATE BUSHING WORN. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804006781995080400678WP 1995 8 4 ABXA9500590 119950626A52803924290501 HINGE DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE HALF ON THE WING WORN. REPAIRED IAW DC-9 S.B. 32-244. 2L72 4F A6WE 19950804006791995080400679WP 1995 8 4 ABXA9500591 119950614A5320575468828 DOUBLER DOUG DC9 DC932 3022066WP BS 133 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D 90-80-03; S.B. 56-1, FOUND CRACKS AROUND RIVETS AND EDGE OF DOUBLER AT UPPER AFT CORNER OF RIGHT CLEARVIEW WINDOW. ALSO DISCOVERED A CRACKED RETAINER SKIN AROUND WINDOW AFTER DOUBLER WAS REMOVED. REPAIRED IAW DOUGLAS SERVICE REWORK DRAWING NR 5952965. 2L72 4F A6WE 19950804006801995080400680WP 1995 8 4 ABXA9500592 119950531A78305958775185 TR FAIRING DOUG DC9 DC931 3022065WP LT ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF A.D. 92-22-08, FOUND CRACKED FAIRING ON LOWER THRUST REVERSER BUCKET, INBOARD SIDE, LEFT ENGINE. REPAIRED IAW DC-9 OVERHAUL MANUAL 78-30-1. 2L72 4F A6WE 19950804006811995080400681WP 1995 8 4 ABXA9500593 119950520A52803923161501 BEARING DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR ROD BEARING WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950804006821995080400682WP 1995 8 4 ABXA9500594 119950520A52803923158501 LINK DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINKAGE WORN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD DOOR IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950804006831995080400683WP 1995 8 4 ABXA9500595 119950520A531159356507 FRAME DOUG DC9 DC931 3022065WP FS 699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF A.D. 78-07-05; S.B. 53-131, FOUND LEFT FUSELAGE FRAME STA. 699 CRACKED IN THE UPPER FORWARD FLANGE OUTBOARD POCKET AND SPLICE AREA. REPAIRED FRAME IAW DC-9 S.B. 53-131 AND SERVICE REWORK DRAWING 5935650. 2L72 4F A6WE 19950804006841995080400684WP 1995 8 4 ABXA9500596 119950521A52805910557160 DOOR DOUG DC9 DC931 3022065WP RT MLG DOOR DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR TO HAVE THE FOLLOWING DISCREPANCIES, ACTUATING ROD, ARTICULATING DOOR HINGE, AND ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED DOOR IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950804006851995080400685WP 1995 8 4 ABXA9500597 119950614A52803923167507 ROD DOUG DC9 DC915 3022036WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR LOOSE AT DRIVE LINK. REPLACED ATTACH ROD IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804006861995080400686WP 1995 8 4 ABXA9500598 119950614A5280AN960D716L SHIM DOUG DC9 DC915 3022036WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR CROSS ARM AT DOOR END HAD EXCESSIVE PLAY. RE-SHIMMED CROSS ARM END IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804006871995080400687WP 1995 8 4 ABXA9500599 119950614A52803923167507 LINK DOUG DC9 DC915 3022036WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY AT FORWARD DOOR LINK. REPLACED DOOR LINK IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804006881995080400688WP 1995 8 4 ABXA9500600 119950617A53129911596503 BLKHD FRAME DOUG DC9 DC931 3022065WP FS 110 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C-CHECK INSPECTION, FOUND THE LOWER HORIZONTAL FRAME ON THE AFT SIDE OF 110 BULKHEAD GOUGED AT LONGERON 28L. REPAIRED IAW ABX REA D953-11833-MR. 2L72 4F A6WE 19950804006891995080400689WP 1995 8 4 ABXA9500601 119950622A5330592032339 SKIN DOUG DC9 DC931 3022065WP CENTER FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C-CHECK INSPECTION, FOUND THE FUSELAGE SKIN DAMAGED AT THE PRIMARY STATIC PORT. REPAIRED IAW ABX REA D953-118-41-MR. 2L72 4F A6WE 19950804006901995080400690WP 1995 8 4 ABXA9500602 119950607A533059114023 SKIN DOUG DC9 DC932 3022066WP FS 125 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND FORWARD ENTRY DOOR HOLD OPEN LATCH HITTING FORWARD LOWER CORNER OF LATCH PIN CUTOUT. REPAIRED IAW DC-9 SRM 53-04, FIG. 24 AND ABX REA D953-11777-MR. 2L72 4F A6WE 19950804006911995080400691WP 1995 8 4 ABXA9500603 119950616A57115911300501 SPAR CAP DOUG DC9 DC932 3022066WP XRS 540 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE LEFT WING AFT SPAR UPPER CAP. REPAIRED IAW ABX REA D957-11819-MR. 2L72 4F A6WE 19950804006921995080400692WP 1995 8 4 ABXA9500604 119950616A78303616987501 BRACKET DOUG DC9 DC932 3022066WP BS 110 CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND NR 1 ENGINE THRUST REVERSER CABLE RUN NR 47 CHAFING THROUGH PULLEY BRACKET BELOW COCKPIT PEDESTAL, APPROXIMATELY STA. 110. REPAIRED IAW ABX REA D953-11824-MR. 2L72 4F A6WE 19950804006931995080400693WP 1995 8 4 ABXA9500605 119950615A53305911408125 SKIN DOUG DC9 DC932 3022066WP BS 237-256 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND 9-G NET CHANNEL HAD IMPROPERLY LOCATED HOLES THROUGH THE FINGER DOUBLER AT STA. 237 TO 256 AT LONGERONS NR 1 AND NR 2. REPAIRED IAW ABX REA D953-11796-MR. 2L72 4F A6WE 19950804006941995080400694WP 1995 8 4 ABXA9500606 119950619A5330591970731 SKIN DOUG DC9 DC932 3022066WP BS 794-813 BLENDED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION FOUND, FUSELAGE SKIN, STA. 794 - 813 LEFT SIDE, BLENDED. REPAIRED IAW ABX REA D953-11840-MR. 2L72 4F A6WE 19950804006951995080400695WP 1995 8 4 ABXA9500607 119950618A53205912494501 JAMB DOUG DC9 DC932 3022066WP BS 380-427 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND FORWARD LOWER CARGO DOOR JAMB INTERNAL DOUBLER AND DOOR JAMB PAN CORRODED. REPAIRED IAW ABX REA D953-11776-MR. 2L72 4F A6WE 19950804006961995080400696WP 1995 8 4 ABXA9500608 119950417A524099214001 BEAM DOUG 591053855 DOUG DC9 DC931 3022065WP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23937AX ABXG601 47074 DURING OFF-WING INSPECTION OF FORWARD SERVICE DOOR, DURING COMPLIANCE OF A.D. 81-10-10; S.B. 52-127, FOUND LOWER HORIZONTAL BEAM CRACKED AT AFT FITTING. INSTALLED DASH 3 DOUBLER, DASH 5 DOUBLER AND DASH 87 CLIP IAW DC-9 SERVICE REWORK DRAWING J060167. 2L72 4F A6WE 19950804006971995080400697WP 1995 8 4 ABXA9500609 119950629A53125910130279 SKIN DOUG DC9 DC941 302207NWP AFT PRESS BULK DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 WHILE ACCOMPLISHING A.D. 89-06-04, FOUND THE AFT PRESSURE BULKHEAD CHAFED. REPAIRED IAW ABX REA D953-12012-MR. 2L72 4F A6WE 19950804006981995080400698WP 1995 8 4 ABXA9500610 119950617A5330592032339 SKIN DOUG DC9 DC932 3022066WP FS 313 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION, FOUND FIVE SHARP DENTS IN THE RIGHT FUSELAGE SKIN AT FS 313 AND LONGERONS 24 AND 25R. REPAIRED IAW ABX REA D953-11837-MR. 2L72 4F A6WE 19950804006991995080400699WP 1995 8 4 ABXA9500611 119950619A5330592032339 SKIN DOUG DC9 DC932 3022066WP FS 465-503 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23939AX 47201 DURING C-CHECK INSPECTION FOUND NUMEROUS DENTS, GOUGES AND STATIC DISCHARGE MARKS IN THE RIGHT FUSELAGE SKIN AT FS 465 - 503. REPAIRED IAW ABX REA D953-11829-MR. 2L72 4F A6WE 19950804007001995080400700WP 1995 8 4 ABXA9500612 119950602A531599581841 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 897 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND TWO HOLES INCORRECTLY LOCATED AND ONE HOLE DOUBLE DRILLED AT STA. 897. REPAIRED IAW ABX REA D953-11716-MR. 2L72 4F A6WE 19950804007011995080400701WP 1995 8 4 ABXA9500613 119950602A531599581851 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 977 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND AN EXISTING REPAIR TO THE FLOOR BEAM AT STA. 917 TO BE DAMAGED. REPAIRED IAW ABX REA D953-11698-MR. 2L72 4F A6WE 19950804007021995080400702WP 1995 8 4 ABXA9500614 119950531A53205912494501 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND LEVEL 1 CORROSION AND A REPAIR TO THE LOWER JAMB OF THE FORWARD LOWER CARGO DOOR . REPAIRED IAW ABX REA D953-11672-MR. 2L72 4F A6WE 19950804007031995080400703WP 1995 8 4 ABXA9500615 119950526A5311995821429 FRAME DOUG DC9 DC931 3022065WP BS 897 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND A FRAME IMPROPERLY PLUGGED AND HOLES WITH SHORT EDGE DISTANCE AT STA. 897, LONGERONS 28 AND 29R. REPAIRED IAW ABX REA D953-11619-MR. 2L72 4F A6WE 19950804007041995080400704WP 1995 8 4 ABXA9500616 119950524A53209957906501 JAMB DOUG DC9 DC931 3022065WP BS 427 PUNCTURED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND THE FORWARD LOWER CARGO DOOR JAMB PUNCTURED AND CORRODED AT STA. 427. REPAIRED IAW ABX REA D953-11598-MR. 2L72 4F A6WE 19950804007051995080400705WP 1995 8 4 ABXA9500617 119950523A532049125401 FITTING DOUG DC9 DC931 3022065WP BS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, A BEAM SUPPORT FITTING WAS FOUND CRACKED AT STA. 965L. FITTING WAS REPLACED IAW DC-9 SRM 53-10-5 AND 53-10-2. 2L72 4F A6WE 19950804007061995080400706WP 1995 8 4 ABXA9500618 119950523A52803923167507 ROD DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C- CHECK INSPECTION, WHILE ACCOMPLISHING A.D. 91-22-07; A.S.B. 32-244, FOUND THE LEFT LANDING GEAR FLYING DOOR LINKAGE WORN. REPLACED DRIVE ROD IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950804007071995080400707WP 1995 8 4 ABXA9500619 119950526A52305911412181 SKIN DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND CORROSION HAD BEEN BLENDED OUT OF THE EXTERIOR SURFACE OF THE SKIN ALONG THE LOWER EDGE OF THE FORWARD LOWER CARGO DOOR. REPAIRED IAW ABX REA D953-11690-MR. 2L72 4F A6WE 19950804007081995080400708WP 1995 8 4 ABXA9500620 119950526A53205912528501 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, THE FORWARD UPPER CORNER OF THE AFT LOWER CARGO DOOR JAMB PAN WAS FOUND TO HAVE CORROSION DAMAGE. REPAIRED IAW ABX REA D953-11692-MR. 2L72 4F A6WE 19950804007091995080400709WP 1995 8 4 ABXA9500621 119950527A53305911472485 SKIN DOUG DC9 DC931 3022065WP FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND DAMAGED AT THE AFT EDGE OF THE AFT LOWER CARGO DOOR AT LONGERON 24. REPAIRED IAW ABX REA D953-11616-MR. 2L72 4F A6WE 19950804007101995080400710WP 1995 8 4 ABXA9500622 119950525A532099579061 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, A WEB IN THE FORWARD LOWER CARGO DOOR JAMB WAS FOUND DAMAGED. REPAIRED IAW ABX REA D953-11706-MR. 2L72 4F A6WE 19950804007111995080400711WP 1995 8 4 ABXA9500623 119950530A531359203122 LONGERON DOUG DC9 DC931 3022065WP BS 294/370 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 294 AND STA 370. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950804007121995080400712WP 1995 8 4 ABXA9500624 119950530A53204912583501 SPLICE DOUG DC9 DC931 3022065WP BS 237/257 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND TWO LONGERON SPLICES AT LONGERONS 29L AND 30L CRACKED AT STA. 237 AND 256. REPLACED SPLICES IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950804007131995080400713WP 1995 8 4 ABXA9500625 119950530A531359203191 LONGERON DOUG DC9 DC931 3022065WP BS 313-389 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND LONGERON 29L CRACKED AT STA 313 - STA 389. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950804007141995080400714WP 1995 8 4 ABXA9500626 119950708A57534912322505 STUD DOUG DC9 DC932F 3022067WP RT TE FLAP HINGECRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING COMPLIANCE OF A.D. 79-03-01; S.B. 57-118, FOUND THE RIGHT OUTBOARD FLAP HINGE, INBOARD LOWER ATTACH STUD INDICATED A CRACK BY THE ULTRASONIC INSPECTION. REPLACED STUD IAW DC-9 M.M. 57-40-1. 2L72 4F A6WE 19950804007151995080400715WP 1995 8 4 ABXA9500627 119950616A5530591218820 ANGLE DOUG DC9 DC931 3022065WP VERT STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING C- CHECK INSPECTION WHILE ACCOMPLISHING A.D. 89-08-10; S.B.'S A53-154 AND A53-223, FOUND THE RIGHT DORSAL FIN ATTACH ANGLE CRACKED. REPLACED THE ANGLE IAW DC-9 SRM 53-05-23. 2L72 4F A6WE 19950804007161995080400716WP 1995 8 4 ABXA9500628 119950527A78305958782503 TR LINK PWA 591029431 DOUG DC9 DC941 302207NWP RT ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 47605 47608 DURING COMPLIANCE OF A.D. 75-14-06, A.D. 90-18-03; S.B.'S 78-36, 78-40 AND 78-66, FOUND CRACK INDICATION ON RIGHT ENGINE LOWER INBOARD THRUST REVERSER DRIVER LINK. REPLACED DRIVER LINK IAW DC-9 M.M. 78-31-5. SHOP FINDING: LINK CRACKED. SCRAPPED LINK. 2L72 4F A6WE 19950804007171995080400717WP 1995 8 4 ABXA9500629 119950718A52805910557135 DOOR DOUG DC9 DC932 3022066WP LT MLG DOOR DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR DOOR DELAMINATED. REPLACED DOOR IAW DC-9 M.M. 32-12-1. 2L72 4F A6WE 19950804007181995080400718WP 1995 8 4 ABXA9500630 119950718A5320575468828 DOUBLER DOUG DC9 DC932 3022066WP BS 130 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION, AND COMPLIANCE OF A.D. 90-80-03; S.B. 56-11, REV. 3, FOUND CRACKS AROUND FASTENER 'A', UPPER AFT CORNER OF RIGHT CLEARVIEW WINDOW RETAINER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19950804007191995080400719WP 1995 8 4 ABXA9500631 119950629A528029242891 BUSHING DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE HALF HAD LOOSE BUSHINGS WITHIN THE LOBES. REPLACED BUSHINGS IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804007201995080400720WP 1995 8 4 ABXA9500632 119950712A52803923166502 FITTING DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH A.D. 91-2 2-07; A.S.B. 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR FORWARD LOWER LINK BUSHING WORN. REPLACED FITTING AND BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950804007211995080400721WP 1995 8 4 ABXA9500633 119950711A533059114063 SKIN DOUG DC9 DC932 3022066WP BS 200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH A.D. 94-03-01, FOUND ENTRY DOOR JAMB CUTOUT AFT LOWER CORNER FUSELAGE SKIN REPAIR AND SEAL STRIKER HEAVILY GOUGED. REPAIRED DAMAGED AREA IAW ABX REA D953-12003-MR. INSTALLED NEW LOWER AFT SEAL DEPRESSOR IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19950804007221995080400722WP 1995 8 4 ABXA9500634 119950711A53305911408125 SKIN DOUG DC9 DC932 3022066WP BS 265 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION FOUND FUSELAGE SKIN CORRODED IN AREA WHERE FORWARD ADF LOOP ANTENNA MOUNTS. REPAIRED IAW ABX REA D953-12002-MR. 2L72 4F A6WE 19950804007231995080400723WP 1995 8 4 ABXA9500635 119950714A533059114013 SKIN DOUG DC9 DC932 3022066WP BS 190 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION, FOUND CORROSION ON BELLY SKIN WHERE MARKER BEACON MOUNTS. REPAIRED IAW ABX REA D953-12006-MR. 2L72 4F A6WE 19950804007261995080400726WP 1995 8 4 ABXA9500638 119950716A53205936443 SEAL DEPRESSOR DOUG DC9 DC932 3022066WP BS 912 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C-CHECK INSPECTION, WHILE COMPLYING WITH A.D. 94-03-01, FOUND AN EXISTING REPAIR AT LOWER DOOR JAMB OF AFT LOWER CARGO DOOR. REPAIRED IAW ABX REA D953-12155-MR. 2L72 4F A6WE 19950804007271995080400727WP 1995 8 4 ABXA9500640 119950527A5320591015825 DOUBLER DOUG DC9 DC931 3022065WP AFT LWR CARGO DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING C-CHECK INSPECTION, FOUND THE JAMB DOUBLER AT THE AFT EDGE OF THE AFT LOWER CARGO DOOR AT LONGERON 24 DAMAGED. REPAIRED IAW ABX REA D953-11616-MR. 2L72 4F A6WE 19950804007281995080400728NM 1995 8 4 DL72S953147 119950712A5311651632543 FRAME BOEING727 727232 1384082NM FS 761 INTERFERENCE A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 65163255001 21019 DURING INSTALLATION OF THE MODIFICATION TO THE LT STA 760.95 FRAME, AS REQUIRED PER AD 94-02-04 AND BOEING S/B 727-53-0197, A 0.125 INCH UNIDENTIFIED SHIM, BELOW WL 210 BETWEEN THE FRAME WEB AND THE 65-24546-3 LOWER CHORD OF THE FLOOR BEAM AND THE 69-18474-1 TEE CLIP, WAS FOUND TO CAUSE INTERFERENCE IN INSTALLATION OF THE MODIFICATION. IN ACCORDANCE WITH FAA LETTER 95-1205-907 DATED 18 JULY 1995, ALTERNATE INSTALLATION INSTRUCTIONS WERE PROVIDED. 2L73 4F A3WE 19950804007291995080400729NM 1995 8 4 DL72W953139 119950721A532065678811 GUSSET BOEING727 727247 138408FNM BS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11296WA 6517518 22533 DURING LETTER CHECK INSPECTION, THE RT TORQUE BOX BEAM GUSSET AT FS 1273 WAS FOUND CRACKED. IN ACCORDANCE WITH B727 S/B 53-0129, REV. 4, THE DAMAGED GUSSET WAS REPLACED. 2L73 4F A3WE 19950804007301995080400730NM 1995 8 4 DL72W953261 119950724A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 CRACK IN STRINGER JUST FWD OF LT WING ILLUM. LT BETWEEN 720B AND 720C. INSTALLED REPAIR PER SRM 53-10-3. FOUND AT HMV. 2L73 4F A3WE 19950804007311995080400731NM 1995 8 4 DL72W953262 119950723A5311 FRAME BOEING727 727247 138408FNM FS 1050 PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 FRAME PUNCTURED AT FS 1050 TOP FLANGE ABOVE STR. 27R AND 27L. REPAIRED PER SRM 53-10-4 FIG 27. 2L73 4F A3WE 19950804007321995080400732NM 1995 8 4 DL72W953263 119950728A5713 STRINGER BOEING727 727247 138408FNM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 OUTBOARD SIDE OF WING STR CRACKED AT FS 686.5 IN NR 1 FUEL TANK LT WING. INSTALLED REPAIR PER MM 57-13-0 PG 808. 2L73 4F A3WE 19950804007331995080400733NM 1995 8 4 DL72W953264 119950723A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 VERTICAL WEB INSIDE THE VERTICAL STAB CRACKED AT BASE OF RIB NR 1 AT LT AND RT LOWER CORNERS. REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950804007341995080400734NM 1995 8 4 DL72W953265 119950722A5754 BRACKET BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 NR 2 LE FLAP ACTUATOR AFT ATTACH BRACKETS ARE CRACKED ON ALL 4 CORNERS. REPAIRED PER MM 57-20-21 FIG 807. 2L73 4F A3WE 19950804007351995080400735NM 1995 8 4 DL72W953266 119950722A5754 BRACKET BOEING727 727247 138408FNM NR 1 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 NR 1 LE FLAP ACTUATOR MOUNT BRACKET CRACKED AT UPPER AND LOWER CORNERS. REPAIRED BRACKET PER MM 57-20-21 FIG 807. 2L73 4F A3WE 19950804007361995080400736NM 1995 8 4 DL72W953267 119950724A5313 STRINGER BOEING727 727247 138408FNM FS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 STR 15R CRACKED AT STA 720B AND 720C. REPAIRED PER SRM 55-10-3. 2L73 4F A3WE 19950804007371995080400737NM 1995 8 4 DL72W953268 119950727A5713 STRINGER BOEING727 727247 138408FNM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 00000 RT WING STR. TO RIB CRACKED AT BOLT HOLE AT WS 629. REPAIRED PER MM 57-13-0. FOUND AT HMV. 2L73 4F A3WE 19950804007381995080400738NM 1995 8 4 DL72W953273 119950726A5315 FLOOR BEAM BOEING727 727247 138408FNM BS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND CORROSION ON FLOOR BEAM STA 344 RBL 50. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19950804007391995080400739NM 1995 8 4 DL76L953236 119950731A2780849704 PROX SW 849704 BOEING767 767332 1382001NM LE SLAT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11185DN 778 27961 LEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED AS FLAPS WERE RETRACTED FROM 5 TO 1 DEGREES. CORRECTIVE ACTION: REPLACED PROX SWITCH ELECTRONICS UNIT. BITE AND OPS CHECK NOW OK. 2L72 4F RTA1NM 19950804007401995080400740NM 1995 8 4 DL76L953241 119950731A2782 ACTUATOR 114T01151 BOEING767 767332 1382001NM NR 6 SLAT BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11185DN 27961 LE FLAP ASYMMETRY MSG ILLUMINATED AT 100 FEET AIRBORNE ON TAKEOFF. FLAPS RET PER MAINT CORD. INSTRUCTIONS VISUAL INSP BY F/O REVEALED LE SLATS EXTENDED APROX 6 INCHES FROM UP. RETURNED JFK. FOUND NR 6 SLAT ACTUATOR ROD BROKEN IN HALF PREVENTING FULL RETRACTION. ROD CAUSED DAMAGE TO SLAT T/E WEDGE. REPLACED ACTUATOR AND FERRIED AIRCRAFT TO ATL FOR REPAIRS. 2L72 4F RTA1NM 19950804007411995080400741WP 1995 8 4 DLL10953144 119950606A57531529905102 FITTING LKHEED1011 10113851 5265010WP NR 3 FLAP VANE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 1529117102 193C1139 DURING ACCOMPLISHMENT OF THE FLAP VANE FITTING REWORK PER DELA S.I. 7-65988-12AD, THE NR 3 FLAP VANE INBOARD FITTING LUG WAS FOUND CRACKED. IN ACCORDANCE WITH ALTERNATE MEANS OF COMPLIANCE LETTER ATL ACO DTD. 7/11/95, A REPLACEMENT FITTING WAS FABRICATED AND INSTALLED. 2L73 4F A23WE 19950804007421995080400742NM 1995 8 4 DLM88952767 119950622A5313 STRINGER 2912727 DOUG MD88 MD88 3023688NM BS 1425 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11943DL 49816 STRINGER L-2 CRACKED AT STA 1425. FOUND AT LETTER CHECK, REPAIRED PER SRM 53-02. 2L72 4F RTA6WE 19950804007431995080400743NM 1995 8 4 P5CA9500604 119950803A331065B475281 CARD BOEING747 747122 1384872NM COCKPIT SHORTED A P5CAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP23853FT 19753 ON PREFLIGHT INSPECTION SAW AND SMELLED SMOKE IN THE COCKPIT. DETERMINED THAT SMOKE WAS FROM MASTER DIM AND TEST MODULE. REPLACED CARD CHECKED OK. 2L74 4F A20WE 19950811000011995081100001EU 1995 8 11 9511663223 119950801A5350 PANEL AIRBUS320 A320211 3930320EU LOWER FUSELAGE VIBRATION A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01323US 272 WHILE CLIMBING THROUGH FL 300 AT A SPEED OF MACH 0.78, EXPERIENCED AIRFRAME VIBRATION. SLOWED SPEED TO APPROXIMATELY 0.74 MACH AND VIBRATION WENT AWAY. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE FASTENERS ON A BELLY PANEL. FURTHER TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2L72 4F RTA28NM 19950811000021995081100002WP 1995 8 11 9511679925 119950731A5246 FUEL DOOR DOUG DC9 DC932 3022066WP RIGHT WING OPEN A ANWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL01925US 47472 SLAT DISAGREEMENT LIGHT REMAINED ON AFTER FLAP/SLAT RETRACTION DURING INITIAL CLIMBOUT. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND FUEL PANEL DOOR OPEN WHICH INTERFERRED WITH SLAT TRAVEL. ALSO, FOUND FUEL CAP MISSING. REPLACED CAP, SLAT OPERATION WAS NORMAL ON GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811000031995081100003WP 1995 8 11 9511689916 119950731A3260 DNLOCK SWITCH DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01949N 47560 DURING CLIMBOUT FROM MSP, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND ALL INDICATIONS RETURNED TO NORMAL. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811000041995081100004WP 1995 8 11 9511699916 119950731A3260 UPLOCK SWITCH DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01949N 47566 DURING CLIMBOUT FROM TYS, NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND ALL INDICATIONS RETURNED TO NORMAL. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811000051995081100005NM 1995 8 11 95UAL900081 119950804A5320BACC30M HI-LOC COLLAR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE FLOOR BEAM MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 DURING HMV, FOUND 19 HI-LOC FASTENERS USED TO SECURE AN ATTACHMENT CLIP TO THE FLOORBEAM, MISSING THEIR COLLARS. INSTALLED COLLARS. 2L72 4F4 FRTA16WE E2GL 19950811000061995081100006NM 1995 8 11 P5CA9500605 119950703A5320 ANGLE BOEING747 747121 1384871NM BS 540-560 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN FLOOR ANGLE BETWEEN BS 540 AND 560 LBL 122. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950811000071995081100007NM 1995 8 11 P5CA9500606 119950703A5320 SUPPORT BOEING747 747121 1384871NM BS 2000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN U-SUPPORT, SUPPORTING THE FAIRINGS IN THE UPPER SIDE BS 2000 RBL 87. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950811000081995081100008NM 1995 8 11 P5CA9500607 119950703A5400 ANGLE BOEING747 747121 1384871NM NR 3 PYLON BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN INTERNAL FRAME ANGLE CORNER NR 3 PYLON NS 270. REPAIRED PER BOEING SRM 54-10-02. 2L74 4F A20WE 19950811000091995081100009NM 1995 8 11 P5CA9500608 119950703A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 440-460 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN INTERCOSTAL MAIN DECK BETWEEN FLOORBEAMS BS 440 AND 460 APPROXIMATLY RBL 50. REPLACED INTERCOSTAL INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000101995081100010NM 1995 8 11 P5CA9500609 119950703A5320 SUPPORT BOEING747 747121 1384871NM BS 740 MISSING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 MISSING RISER SUPPORT UPPER DECK BS 740 LEFT SIDE ON FRAME WL 360. INSTALLED RISER PER BOEING SRM 53-10-21 AND 51-30-02. 2L74 4F A20WE 19950811000111995081100011NM 1995 8 11 P5CA9500610 119950703A5320 ANGLE BOEING747 747121 1384871NM WING TO BODY BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN BRACKET NEAR RIGHT BODY GEAR OUTBOARD SHOCK STRUT DOOR BRACKET SUPPORTS BODY TO WING FAIRING. MANUFACTURED NEW BRACKET PER BOEING SRM 51-40-02, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950811000121995081100012NM 1995 8 11 P5CA9500611 119950703A5280 SKIN BOEING747 747121 1384871NM LT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS ON INNER SKIN LEFT BODY GEAR WHEEL WELL INBOARD DOOR. INSTALLED NEW SKIN AND FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000131995081100013NM 1995 8 11 P5CA9500612 119950703A5280 SKIN BOEING747 747121 1384871NM LT MLG DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION UNDER SEAL RETAINER LEFT BODY GEAR WHEEL INBOARD DOOR AFT WEB. INSTALLED NEW WEB SKIN AND FASTENERS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000141995081100014NM 1995 8 11 P5CA9500613 119950703A5320 SHEAR TIE BOEING747 747121 1384871NM BS 520-540 DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGED SHEAR TIE BETWEEN BS 520 AND 540 LBL 65. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950811000151995081100015NM 1995 8 11 P5CA9500614 119950703A5320 STIFFENER BOEING747 747121 1384871NM BS 2240-2280 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN STIFFENERS, 2 BETWEEN BS 2240 AND 2280 LBL 33 AND 56. MANUFACTURED NEW STIFFENERS PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950811000161995081100016NM 1995 8 11 P5CA9500615 119950703A5280 WEB BOEING747 747121 1384871NM LT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON LEFT BODY GEAR SIDE STRUT INBOARD DOOR LOWER WEB. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950811000171995081100017NM 1995 8 11 P5CA9500616 119950703A5280 ANGLE BOEING747 747121 1384871NM LT MLG DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON LEFT BODY GEAR SIDE STRUT INBOARD DOOR UPPER ANGLE. REPLACED ANGLE AND INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000181995081100018NM 1995 8 11 P5CA9500617 119950703A5280 ANGLE BOEING747 747121 1384871NM RT MLG DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON RIGHT BODY GEAR SIDE STRUT INBOARD DOOR UPPER ANGLE. MANUFACTURED NEW ANGLE INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000191995081100019NM 1995 8 11 P5CA9500618 119950703A5280BAC1510932 RETAINER BOEING747 747121 1384871NM RT MLG DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORRODED DOOR SEAL RETAINER RIGHT BODY GEAR SHOCK STRUT DOOR. REPLACED SEAL, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000201995081100020NM 1995 8 11 P5CA9500619 119950703A5320 ANGLE BOEING747 747121 1384871NM BS 1920-1960 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON THE FLOOR PROFILE ANGLE BETWEEN BS 1920 AND 1960, LEFT AND RIGHT SIDES AT BL 55. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01. 2L74 4F A20WE 19950811000211995081100021NM 1995 8 11 P5CA9500620 119950703A5320 BRACKET BOEING747 747121 1384871NM BS 1260 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BRACKET RIGHT WING WHEEL WELL AT CEILING BS 1260 INBOARD SIDE HYDRAULIC LINE CLAMP. MANUFACTURED AND INSTALLED PER BOEING SRM 51-20-01 AND 51-30-02. 2L74 4F A20WE 19950811000221995081100022NM 1995 8 11 P5CA9500621 119950703A5321 FLOOR PANEL BOEING747 747121 1384871NM COCKPIT DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE AND SURFACE CORROSION ON PANEL BETWEEN CAPTAINS SEAT RAILS. MANUFACTURED REPLACEMENT PANEL PER BOEING SRM 51-20-01 AND 51-30-02. 2L74 4F A20WE 19950811000231995081100023NM 1995 8 11 P5CA9500622 119950703A5280 PANEL BOEING747 747121 1384871NM RT MLG DOOR BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN FIBERGLASS ON RIGHT WING GEAR LOWER SHOCK STRUT DOOR AT AFT SIDE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950811000241995081100024NM 1995 8 11 P5CA9500623 119950703A5280 BRACKETS BOEING747 747121 1384871NM RT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO CRACKED BRACKETS, RIGHT WING GEAR LOWER SHOCK STRUT DOOR. MANUFACTURED AND INSTALLED BRACKETS PER BOEING SRM 51-20-01 AND 51-30-02. 2L74 4F A20WE 19950811000251995081100025NM 1995 8 11 P5CA9500624 119950703A5313 STRINGER BOEING747 747121 1384871NM BS 480 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN S38R AT BS 480. REPAIRED PER BOEING SRM 53-10-03 FIG 3. 2L74 4F A20WE 19950811000261995081100026NM 1995 8 11 P5CA9500625 119950703A5320 POST BOEING747 747121 1384871NM BS 440 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN LOWER POST NEAR ATC INSTRUMENT BS 440 BETWEEN S40R AND S41R. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950811000271995081100027NM 1995 8 11 P5CA9500626 119950703A5320 BRACKET BOEING747 747121 1384871NM BS 1241 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SHEARED HI-LOC DUE TO CORRODED BRACKET AT BS 1241 RBL 106. REPLACED BRACKET AND FASTENER PER BOEING SRM 51-20-01 AND 51-30-02. 2L74 4F A20WE 19950811000281995081100028NM 1995 8 11 P5CA9500627 119950703A5330 SKIN BOEING747 747121 1384871NM BS 400 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 NOSE WHEEL WELL BS 400 LEFT AND RIGHT CORNERS CRACKED. REPAIRED PER SB 53-2305. 2L74 4F A20WE 19950811000291995081100029NM 1995 8 11 P5CA9500628 119950703A5730 SKIN BOEING747 747121 1384871NM WS 294-614 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON LOWER SKIN LEFT WING BETWEEN WS 294 AND 614. REMOVED AND TREATED PER BOEING SRM 51-10-01, WITHIN LIMITS PER 57-10-01. 2L74 4F A20WE 19950811000301995081100030NM 1995 8 11 P5CA9500629 119950703A5330 SKIN BOEING747 747121 1384871NM BS 2598 TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SKIN TORN AND PARTLY SEPARATED AT BS 2598 ABOVE STABILIZER FAIRING. REPAIRED PER IAI ENGINEERING ORDER MF-MAN B47-53-83977. 2L74 4F A20WE 19950811000311995081100031NM 1995 8 11 P5CA9500630 119950703A4910 COWLING BOEING747 747121 1384871NM APU CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 APU RIGHT COWLING FORWARD EDGE CRACKED AND 2 RIVETS SHEARED. REPAIRED PER BOEING SRM 51-10-01 AND 51-30-02. 2L74 4F A20WE 19950811000321995081100032NM 1995 8 11 P5CA9500631 119950703A5312 BULKHEAD BOEING747 747121 1384871NM BS 1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON LEFT BS 1350 BULKHEAD, AT BL 76 LOWER CHORD. REWORKED PER BOEING SB 53-23-10 AND SRM 51-10-02. 2L74 4F A20WE 19950811000331995081100033NM 1995 8 11 P5CA9500632 119950703A5320 Z-ANGLE BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT-Z AT BS 1240 BETWEEN LBL 40 AND LBL 80. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950811000341995081100034NM 1995 8 11 P5CA9500633 119950703A5230 SKIN BOEING747 747121 1384871NM FWD CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON FORWARD CARGO DOOR HINGE OUTER SIDE. REMOVED CORROSION PER BOEING SRM 51-10-01 TREATED PER 51-10-02. 2L74 4F A20WE 19950811000351995081100035NM 1995 8 11 P5CA9500634 119950703A5320 WEB BOEING747 747121 1384871NM BS 1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON UPPER CHORD WEB AT BS 1920 RBL 55. REPLACED STRAP INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000361995081100036NM 1995 8 11 P5CA9500635 119950703A532065B071961 FITTING BOEING747 747121 1384871NM BS 1920 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN CONNECTING FITTING TO BS 1920 RIGHT SIDE S40R TO S41R. INSTALLED NEW FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811000371995081100037NM 1995 8 11 P5CA9500636 119950703A5230 HINGE BOEING747 747121 1384871NM FWD CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION LOWER CARGO DOOR EXTERNAL UPPER HINGE SEGMENTS. REMOVED CORROSION PER BOEING SRM 51-10-01, 51-10-02. 2L74 4F A20WE 19950811000381995081100038NM 1995 8 11 P5CA9500637 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1319 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION IN LEFT WING GEAR WHEEL WELL AT BS 1319 LEFT SIDE. REPAIRED PER BOEING SRM 51-40-04 FIG 3. 2L74 4F A20WE 19950811000391995081100039NM 1995 8 11 P5CA9500638 119950703A5312 BLKHD STRINGERS BOEING747 747121 1384871NM BS 400 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 TWO CRACKS AT FORWARD BS 400 BULKHEAD STRINGER S44L AND S44R, AT CORNER AFT O WHEEL WELL AND CRACK AT BS 400 AROUND FASTENER. REPAIRED PER BOEING SB 53-23-05 AND SRM 53-30-03 FIG 35. 2L74 4F A20WE 19950811000401995081100040NM 1995 8 11 P5CA9500639 119950703A5400BACR24N6BL104 EYE BOLTS BOEING747 747121 1384871NM NR 1 PYLON CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 PYLON SKIRT NR 1 SUPPORT ROD EYE BOLTS CORRODED. INSTALLED NEW ROD PER BOEING M/M 20-50-01. 2L74 4F A20WE 19950811000411995081100041NM 1995 8 11 P5CA9500640 119950703A5313 STRINGER BOEING747 747121 1384871NM CABIN CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION IN JOINT S6R TO RIGHT SIDE. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS PER 53-10-01, TREATED PER 51-10-02. 2L74 4F A20WE 19950811000421995081100042NM 1995 8 11 P5CA9500641 119950703A5320 WEB BOEING747 747121 1384871NM BS 1245 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK IN WEB AT BS 1245 RBL 108 RIGHT WING GEAR WHEEL WELL. REPAIRED PER BOEING SRM 53-10-07 FIG 16. 2L74 4F A20WE 19950811000431995081100043NM 1995 8 11 P5CA9500642 119950703A5320 WEB BOEING747 747121 1384871NM BS 1394 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK RIGHT BODY GEAR WHEEL WELL BS 1394 OUTBOARD WALL INNER BOX CAVITY WEB. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950811000441995081100044NM 1995 8 11 P5CA9500643 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1372 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION RIGHT BODY GEAR WHEELWELL BS 1372 OUTBOARD WHEELWELL INNER BOX CAVITY REPAIRED PER IAI E.O. MF-MAN-B47-53-8400. 2L74 4F A20WE 19950811000451995081100045NM 1995 8 11 P5CA9500644 119950703A5320 T-CHORD BOEING747 747121 1384871NM BS 1700-1750 DOUBLE DRILLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BETWEEN BS 1700 AND BS 1750 AT S4L ON THE T-CHORD, FOUND DOUBLE HOLES AND OVAL HOLES. T-CHORD REPLACED WITH NEW PART PER E. O. MF-MAN-B47-53-83972. 2L74 4F A20WE 19950811000461995081100046NM 1995 8 11 P5CA9500645 119950703A5320 T-CHORD BOEING747 747121 1384871NM BS 1950-2000 DOUBLE DRILLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BETWEEN BS 1950 AND BS 2000 ON S4L ON T-CHORD, FOUND DOUBLE HOLES AND OVAL HOLES. REPAIRED PER IAI E.O. MF-MAN-B47-53-83972. 2L74 4F A20WE 19950811000471995081100047NM 1995 8 11 P5CA9500646 119950703A5320 FITTING BOEING747 747121 1384871NM BS 1740 PLUGGED HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BS 1740 S4L ON THE LOWER FORWARD FITTING THAT CONNECTS THE INTERCOSTAL TO THE FRAME ON LEFT SIDE OF THE T-CHORD HAS 2 PLUG HOLES 1.8750 INCHES IN DISTANCE AND SECOND .3750 INCH IN DISTANCE FROM EXISTING HILOCK. INSTALLED STRAP PER IAI E.O. MF-MAN-B47-53-84008. 2L74 4F A20WE 19950811000481995081100048NM 1995 8 11 P5CA9500647 119950703A5320 WEB BOEING747 747121 1384871NM BS 1241 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON PRESSURE DECK WEB BS 1241 RBL 106. TRIMMED AREA TO REMOVE CRACK PER BOEING SRM 53-10-07 FIG 16 DETAIL 2. 2L74 4F A20WE 19950811000491995081100049NM 1995 8 11 P5CA9500648 119950703A5400 BRACKET BOEING747 747121 1384871NM NR 1 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED BRACKET NR 1 PYLON NS 253 INTERNAL ON LEFT WALL. MANUFACTURED NEW BRACKETS PER BOEING SRM 54-10-02. 2L74 4F A20WE 19950811000501995081100050NM 1995 8 11 P5CA9500649 119950703A5230 SEAL GROOVE BOEING747 747121 1384871NM CARGO DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 MAIN SIDE CARGO DOOR FWD INTERIOR SIDE PRESSURE SEAL GROOVE IS DAMAGED AND CRACKED IN 2 PLACES. REPAIRED PER BOEING SRM 51-40-01. 2L74 4F A20WE 19950811000511995081100051NM 1995 8 11 P5CA9500650 119950703A5330 SKIN BOEING747 747121 1384871NM BS 740-760 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS IN FUSELAGE SKIN BETWEEN BS 740 AND 760 S26R. REPAIRED PER BOEING SRM 53-30-03 FIG 1. 2L74 4F A20WE 19950811000521995081100052NM 1995 8 11 UPS203994 119950804A5320651758866 BEAM BOEING727 72727C 138400JNM BS 265 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORR C53-221-01.01-01, AROUND NUTPLATES ON 25 G-BEAM AT STA 265 WL 208 LBL 6 TO RBL 15. CORR REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED 25 G-BEAM DRILLED UP NEW PART, INSTALLED PER SRM 53-10-1, 51-30-2. 2L73 4F A3WE 19950811000531995081100053NM 1995 8 11 UPS203995 119950804A52107075T6 DOOR FRAME BOEING727 72727C 138400JNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND FWD ENTRY DOOR LWR FWD FRAME IS CRACKED. REMOVED DAMAGE, ALODINED AND PRIMED EDGE. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-2, 51-40-3 AND 51-30-2. 2L73 4F A3WE 19950811000541995081100054NM 1995 8 11 UPS203996 119950804A5313BAC1493513 STRINGER BOEING727 72727C 138400JNM BS 400 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND STRINGER 8 LT STA 400 HAS 9 SHEARED FASTENERS GOING THROUGH FRAME AND CRACKS DISPERSING FROM HOLE. REPAIRED STRINGER IAW 53-10-3, 51-30-2. 2L73 4F A3WE 19950811000551995081100055NM 1995 8 11 UPS203997 119950804A53132024T3100 STRINGER BOEING727 72727C 138400JNM BS 760-848 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORROSION C53-224-01.00-02, ON STRINGER 6 LT STA 760 TO 868. CORR REMOVAL WAS OUT OF LIMITS FROM STA 781 TO 768 ON STR 6L. REMOVED DAMAGED AREA FROM BS 781 TO 768, FABRICATED AND INSTALLED REPAIR PARTS. ALL WORK DONE PER SRM 53-10-3, 51-10-2, 51-10-6. ALL OTHER AREAS BETWEEN STA 760 TO 848, WERE WITHIN LIMITS. 2L73 4F A3WE 19950811000561995081100056NM 1995 8 11 UPS203998 119950804A5520M469029 DOUBLER BOEING727 72727C 138400JNM ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORROSION C53-391-01.00-02, ON RT NR 5 BALANCE PANEL ATTACHING DOUBLER. REMOVED, FABRICATED NEW DOUBLER AND INSTALLED PER DWG 65-27917, MM 51-20-00, MM 51-20-21, MM 27-30-21. 2L73 4F A3WE 19950811000571995081100057NM 1995 8 11 UPS203999 119950804A5753 SKIN BOEING727 72727C 138400JNM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND RT WING INBD FOREFLAP HAS 1 DELAM ON UPPER SURFACE AT INBD END. REPAIRED PER SRM 51-40-0. 2L73 4F A3WE 19950811000581995081100058NM 1995 8 11 UPS204000 119950804A5347BAC15201434 SEAT TRACK BOEING727 72727C 138400JNM BS 1067-1071 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORR ON SEAT TRACK BS 1067 TO 1071 RBL 62 WL 208. REMOVED CORR AND FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK, FINISHED INSTALLATION PER SRM 51-10-6, 51-30-2, 51-10-2, MM 51-20-151. 2L73 4F A3WE 19950811000591995081100059NM 1995 8 11 UPS204001 119950804A5720 VENT BOX BOEING727 72727C 138400JNM WS 171.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND RT WING STA 171.5 OB SIDE OF RIB, FWD VENT BOX AFT FLANGE CRACKED. REPAIRED IAW SRM 57-10-4, BY REMOVING AND REPLACING VENT STRINGER TAB. 2L73 4F A3WE 19950811000601995081100060NM 1995 8 11 UPS204002 119950804A5320651759318 INTERCOSTAL BOEING727 72727C 138400JNM BS 259-277 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORR C53-221-01.01-01, ON INTERCOSTAL AT STR 259 TO 277 WL 208 LBL 11. REMOVED CORR, REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL SRM 53-10-1, 51-30-8, 51-20-151 AND 51-30-2. 2L73 4F A3WE 19950811000611995081100061NM 1995 8 11 UPS204003 119950804A53206517593 INTERCOSTAL TEE BOEING727 72727C 138400JNM BS 266 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND CORR ON TEE INTERCOSTAL AT STA 266 LBL 7 TO 11 WL 208. REMOVED AND REPLACED PART IAW SRM. 2L73 4F A3WE 19950811000621995081100062NM 1995 8 11 UPS204004 119950804A53137075T6 STRINGER BOEING727 72727C 138400JNM BS 360 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINT FOUND LFEC INSPECTION SHOWS A 10 PERCENT MATERIAL LOSS AT BS 360 STR. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA, FABRICATED REPAIR PART. INSTALLED COUNTERSUNK FILLERS AND FINAL INSPECTION PER DRAWING 69-62161, SRM 51-30-2, 53-30-2, MM 51-20-151. 2L73 4F A3WE 19950811000631995081100063NM 1995 8 11 UPS204005 119950804A53207075T6 CLIP BOEING727 72727C 138400JNM BS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND SHORT AND MISSING FASTENERS ON FRAME STA 294 LBL 55 WL 280. REMOVED AND REPLACED SHORT FASTENERS AND REPLACED MISSING FASTENERS. FOUND STRINGER CLIP TO BE CRACKED. REMOVED CRACKED STRINGER CLIP AND REPLACED WITH FABRICATED STRINGER CLIP IAW SRM 51-20-1, 51-10-2, 51-30-2 AND 51-30-5. 2L73 4F A3WE 19950811000641995081100064NM 1995 8 11 UPS204006 119950804A53207075T6 WEB BOEING727 72727C 138400JNM BS 1152-1156 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CORR ON WEB STA 1152 TO 1156 LBL 48 WL 208. REMOVED CORR AND FOUND TO BE OUT OF LIMITS SRM 53-10-1. FABRICATED REPAIR PART IAW SRM 51-40-02, SRM 51-30-8 AND 51-30-2. 2L73 4F A3WE 19950811000651995081100065NM 1995 8 11 UPS204007 119950804A5320 WEB BOEING727 72727C 138400JNM BS 746-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND WHILE WORKING EO AND B727-5710-1271-6 FOUND CORR ON LT SIDE PRESSURE BOX AT WL 208 LBL BS 746 TO 760. REMOVED, FABED, NEW PRESSURE WEB USING OLD WEB AT TEMPLATE IAW SRM TO BE INSTALLED AT COMPLETION OF SUBJECT EO. 2L73 4F A3WE 19950811000661995081100066NM 1995 8 11 UPS204008 119950804A53207075T60032 LWR TORQUE BOX BOEING727 72727C 138400JNM BS 1233 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CRACK IN LIGHTENING HOLE IN LWR TORQUE BOX, AT BS 1233 LBL 21 WL 171. STOP DRILLED CRACK, NDI VERIFIED CONTAINMENT, FABED AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2. 2L73 4F A3WE 19950811000671995081100067NM 1995 8 11 UPS204009 119950804A53137075T6 STRINGER BOEING727 72727C 138400JNM BS 390-480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CORR C53-224-01.00-01, ON STRINGER 9 RT STA 390, 400 AND 440 TO 480. REMOVED CORR IAW SRM 53-10-1 AND FOUND AREA AT 396 RT TO BE OUT OF LIMITS. FABED REPAIR PARTS AND INSTALLED IAW SRM 53-10-2, 53-10-3. 2L73 4F A3WE 19950811000681995081100068NM 1995 8 11 UPS204010 119950804A5751 TE WEDGE BOEING727 72727C 138400JNM RT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND RT WING OUTBD AILERON TRAILING EDGE WEDGE HAS PREVIOUS REPAIR DELAMINATING OUTBD END LWR SURFACE AND POTTED ENDS ERODING. REPAIRED RT HAND OUTBD AILERON FOR SRM 51-40-6. ALL WORK DONE PER SRM 51-40-6, SRM 51-30-2, MM 27-10-41 AND 51-80-4. 2L73 4F A3WE 19950811000691995081100069NM 1995 8 11 UPS204011 119950804A554365218204 FITTING BOEING727 72727C 138400JNM RUDDER TAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND LWR RUDDER TAB CONTROL ROD SUPPORT FITTING CORRODED. REMOVED AND REPLACED LWR RUDDER TAB CONTROL ROD SUPPORT FITTING IAW OHM 20-50-01. 2L73 4F A3WE 19950811000701995081100070NM 1995 8 11 UPS204013 119950804A531269201122 BLKHD LINK BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CORROSION ON EXPANSION LINK THAT MOUNTS TO BULKHEAD BS 740 FWD OF LWR CHORD LBL 13. REMOVED AND REPLACED EXPANSION LINK FORK AND BRACKET IAW SRM. 2L73 4F A3WE 19950811000711995081100071NM 1995 8 11 UPS204014 119950804A532069157683 INTERCOSTAL BOEING727 72727C 138400JNM BS 211.8-227.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CORROSION ON INTERCOSTAL BETWEEN BS 211.8 AND BS 227.8 LBL 1.5. REMOVED CORR AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-1. REMOVED INTERCOSTAL AND INSTALLED NEW PART. 2L73 4F A3WE 19950811000721995081100072NM 1995 8 11 UPS204015 119950804A53137075T6 STRINGER BOEING727 72727C 138400JNM BS 538-560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CORROSION C53-224-01.00-01, STRINGER NR 1 STA 538 TO 560. REMOVED CORR FOUND AREA AT 538 TO 560 TO BE OUT OF LIMITS IAW SRM 53-10-1. FABED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3. 2L73 4F A3WE 19950811000731995081100073NM 1995 8 11 UPS204016 119950804A53117075T6 FRAME BOEING727 72727C 138400JNM BS 420 NICKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND NICK IN FRAME STA 420 LBL 60 WL 270. NICK OUT OF LIMITS, CUT OUT DAMAGE, FABED DOUBLER. DOUBLER WILL BE INSTALLED ON NRC 348544. WORK REQ'D IN SAME AREA. ALL WORK DONE IAW SRM 53-10-2 AND 51-40-3. 2L73 4F A3WE 19950811000741995081100074NM 1995 8 11 UPS204017 119950804A5753 SKIN BOEING727 72727C 138400JNM LT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND LT WING INBD FLAP IS DELAMINATING AROUND RUB STRIP INBD END. REMOVED RUB STRIP AND DAMAGED SKIN UNDER RUB STRIP. FINAL INSTALLATION PER SRM 51-40-6, MM 51-51-11. 2L73 4F A3WE 19950811000751995081100075NM 1995 8 11 UPS204018 119950804A5753 SKIN BOEING727 72727C 138400JNM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND RT WING INBD FOREFLAP HAS DELAM ON UPPER SURFACE. REMOVED DISBONDED SKIN AND DELAMINATION OF PREV REPAIR. FINAL REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950811000761995081100076NM 1995 8 11 UPS204019 119950804A575365246759 FITTING BOEING727 72727C 138400JNM LT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND LT WING INBD MIDFLAP INBD YOKE HOUSING HAS CRACK IN BOTTOM OF GOUGE. REMOVED AND REPLACED FITTING PER SRM 51-30-2, OHM 57-52-111, MM 27-51-22. 2L73 4F A3WE 19950811000771995081100077NM 1995 8 11 UPS204020 119950804A5330651757011 PLATE BOEING727 72727C 138400JNM BS 294-304 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND CRACKED MOP SILL AT STA 294 TO 304 LBL 52 WL 208. REMOVED CRACKED MOP SILL, INSTALLED NEW MOP SILL IAW SRM 51-10-1, 51-10-2, 51-20-2, AND MM 51-20-151. 2L73 4F A3WE 19950811000781995081100078NM 1995 8 11 UPS204021 119950804A5751651926012 HINGE FITTING BOEING727 72727C 138400JNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINT FOUND LT WING OB AILERON IB CENTER HINGE FITTING IS CORR ON AFT SIDE. INSTALLED NEW FITTING, WORK DONE IAW SRM 51-30-2. 2L73 4F A3WE 19950811000791995081100079WP 1995 8 11 UPS804023 119950804A53150507075T6 FLOORBEAM WEB DOUG DC8 DC871F 302199DWP FS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01715UP 45915 WHILE IN DALFORT FOR C-CHECK, MAINT FOUND HEAVY CORR ON LOWER SIDE OF VERT WEB FS 80 FWD SIDE OF FLOORBEAM, LT SIDE OF COCKPIT SUBFLOOR AREA. REPLACED VERT WEB PER SRM 51-1-20D. 2L74 4F RT4A25 19950811000801995081100080WP 1995 8 11 UPS804024 119950804A53205612298341 PANEL DOUG DC8 DC873F 302199FWP FS 32-12 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01866UP 45966 WHILE IN DALFORT FOR C-CHECK, MAINT FOUND FLT CABIN SUBFLOOR PRESSURE PANEL HAS HVY CORR AT SKIN JOINT FS 32 TO FS 12 LONGERON 24R. REPAIRED FOR UPS EO DC8-5310-7242-A. 2L74 4F RT4A25 19950811001211995081100121CE 1995 8 11 95ZZZX3731 119950701A5610NAS517320 RETAINER SCREW BEECH MU300 400BEECH CE WINDSHIELD RUSTED A JGVAK NONE O OTHER ININSP/MAINT 1 CE09196KC2936 RJ52 DURING WINDSHIELD SEAL REPLACEMENT, NUMEROUS SCREWS ALONG LOWER PORTION OF WINDSHIELD RETAINER WERE FOUND SEVERELY RUSTED THROUGH APPROXIMATELY 50 PERCENT OF ORIGINAL DIAMETER. SUSPECT CAUSE IS MOISTURE INFILTRATION AROUND RETAINER WHEN SEAL DETERIORATES BETWEEN RETAINER AND WINDSHIELDS. 2H72 4F RTA16SW 19950811001441995081100144WP 1995 8 11 95ZZZW799 119950715A302079588691 DUCT DOUG DC9 DC932 3022066WP LT ENGINE FAILED A VJ6AO OTHER J WARNING INDICATION TOTAKEOFF 1 SO11917VV 47323 BDL-ATL - FLT 449 - ON TAKEOFF, LT ENGINE A LOOP ILLUMINATED, LT OIL STRAINER CLOGGING LIGHT ILLUMINATED, OIL PRESS DROPPED TO 35 PSI, WITH TEMP RAPIDLY RISING THROUGH 120 DEGREES ENGINE OPERATED AT IDLE FOR REMAINDER OF FLIGHT. FOUND NOSE COWL ANTI-ICE DUCT BLOWN WHICH DAMAGED OIL PRESS DIFFERENTIAL SWITCH. REMOVED AND REPLACED ANTI-ICE DUCT AND OIL PRESS SWITCH. 2L72 4F A6WE 19950811001451995081100145NM 1995 8 11 TWRA9540 119950719A33505880 EEL STRIP BOEING747 747136 1384883NM CABIN INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15606FF 20273 UPON PERFORMING EMERGENCY LIGHTS CHECK FOUND GALLEY STRIP BY L4 DOOR INOPERATIVE. REMOVED AND REPLACED GALLEY EGRESS LIGHT STRIP BY L4 DOOR, OPS CHECK OK. (W) 2L74 4F A20WE 19950811001461995081100146NM 1995 8 11 USA950731 119950614A5320 THRESHOLD BOEING737 737301 1384611NM FWD SERVICE DOORCORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 12 INCHES FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001471995081100147NM 1995 8 11 USAA950708 119950601A5315 FLOORBEAM BOEING737 737401 1384701NM BS 947 - 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH STA 947 TO STA 967 RBL 17 INCHES. REPAIRED PER SRM 51-10-1, REPLACED NEW BEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001481995081100148NM 1995 8 11 USAA950709 119950622A5315 FL-ORBEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 INCH DIA AREAS OF CORROSION, STA 328 FLOORBEAM UPPER FLANGE BL 0 TO RBL 56. REPAIRED PER SRM 53-10-51, FIG 205. REPLACED T-CAP LBL 32 TO RBL 56 PER SRM 53-10-51 FIG 205. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001491995081100149NM 1995 8 11 USAA950710 119950622A5320654555541 ANGLE BOEING737 737401 1384701NM BS 937 TO 996 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORROSION 2 INCHES BY 55 INCHES STA 937 TO STA 996 RT. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001501995081100150NM 1995 8 11 USAA950711 119950602A5315 FLOORBEAM BOEING737 737401 1384701NM STA 947 TO 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 4 INCH, 75 PERCENT LOSS STA 947 TO STA 967 RBL 52 INCHES ON FLOORBEAM. REPAIRED PER SRM 51-10-2, INSTALLED NEW BEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001511995081100151NM 1995 8 11 USAA950712 119950622A5320654587512 ANGLE BOEING737 737401 1384701NM BS 940 - 995 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 55 INCHES STA 940 TO STA 995 LT. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001521995081100152NM 1995 8 11 USAA950713 119950601A53156546812170 FLOORBEAM BOEING737 737401 1384701NM BS 967 - 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STA 967 TO STA 986 LBL 17 INCHES. REPAIRED PER SRM 51-10-02, REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW PART. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001531995081100153NM 1995 8 11 USAA950714 119950601A5315 FLOORBEAM BOEING737 737401 1384701NM BS 967 - 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCH BS 967 TO BS 986 RBL 17. REPAIRED PER SRM 51-10-1, REPLACED BEAM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001541995081100154NM 1995 8 11 USAA950715 119950601A531565C333671 FLOORBEAM BOEING737 737401 1384701NM STA 950 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STA 950 LBL 52 INCHES. REPAIRED PER SRM 51-10-02, REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001551995081100155NM 1995 8 11 USAA950726 119950614A53201133022 CHANNEL BOEING737 737301 1384611NM BS 500 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 3 INCH CORROSION, BS 500 PLUS 6 INCHES BL 0. REPLACED CHANNEL WITH NEW CHANNEL SRM 51-10-02. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001561995081100156NM 1995 8 11 USAA950727 119950614A5315 FLOORBEAM BOEING737 737301 1384611NM BS 987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCHES BY 1 INCH OF CORROSION BS 987.0 BL 40 LT T-CAP SECTION OF FLOORBEAM. FABRICATED NEW T-CAP, STRAP AND REPAIR ANGLES AND INSTALLED SAME. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001571995081100157NM 1995 8 11 USAA950728 119950607A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 2 INCHES BY 42 INCHES, STA 344 BL 0 TO LBL 42 INCHES. REMOVED T-CAP SECTION AND REINSTALLED SAME WITH DOUBLER ANGLES AND SPLICE STRAPS. TR 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001581995081100158NM 1995 8 11 USAA950729 119950612A5315 FLOORBEAM BOEING737 737301 1384611NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM 1 INCH BY 12 INCHES STA 328 RBL 6 TO LBL 63. REPLACED UPPER T-CAP, TR 53-10-3. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001591995081100159NM 1995 8 11 USAA950730 119950615A53201123845 ANGLE BOEING737 737301 1384611NM FWD ENTRY DOOR CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19337US 23235 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH, TWO HOLES THROUGH ANGLE CORROSION FORWARD ENTRY DOOR SILL Z-ANGLE. REPLACED Z-ANGLE SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001601995081100160NM 1995 8 11 USAA950734 119950608A5320 FLOOR PAN BOEING737 737301 1384611NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCHES BY 10 INCHES CORROSION AREA ON FLOOR PAN AT LT LAVATORY DUMP CHUTE CUTOUT BS 1016 LBL 5. INSTALLED WEB SKIN REPAIR SRM 51-70-13 FIG 1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001611995081100161NM 1995 8 11 USAA950735 119950605A53206546812175 SUPPORT BOEING737 737301 1384611NM BS 1006-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH AND 1 INCH BY 6 INCH AREA CORRODED TOP OF FLOOR SUPPORT BS 1006 TO 1016, 36 INCHES LBL. FABRICATED NEW WEB AND SUPPORT ANGLE, SRM 51-10-1, SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001621995081100162NM 1995 8 11 USAA950736 119950602A53126546812175 SHIM BOEING737 737301 1384611NM FWD BULKHEAD CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SHIM AT I/B END OF AFT LT LAVATORY FORWARD BULKHEAD WALL SUPPORT HAS CORRODED SCREW HOLE. INSTALLED NEW INTERCOSTAL/SHIM. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001631995081100163NM 1995 8 11 USAA950737 119950605A5315 FLOORBEAM BOEING737 737301 1384611NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORRODED SCREW HOLE FLOORBEAM BS 986.5, 43 INCHES LBL. INSTALLED UPPER T-CAP REPAIR, ENTIRE LENGTH TR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001641995081100164NM 1995 8 11 USAA950738 119950601A53206546812187 INTERCOSTAL BOEING737 737301 1384611NM BS 1006-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA AND 2 CORRODED SCREW HOLES AFT LT LAVATORY DOORWAY, BS 1006 TO 1016. INSTALLED NEW INTERCOSTAL SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001651995081100165NM 1995 8 11 USAA950739 119950609A5347 SEAT TRACK BOEING737 737301 1384611NM BS 340 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION .5 INCH BY 2 INCH, SEAT TRACK STA 340 RBL 45. INSTALLED NEW SECTION OF SEAT TRACK SRM 53-00-52 FIG 202. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001661995081100166NM 1995 8 11 USAA950740 119950531A5320 SUPPORT BOEING737 737301 1384611NM BS 1006 - 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCHES BY 6 INCHES CORRODED AREA, BS 1006 TO 1016 RT AFT LAVATORY DOORWAY FLOOR SUPPORT. INSTALLED NEW INTERCOSTAL SUPPORT SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001671995081100167NM 1995 8 11 USAA950741 119950626A53206546812 SUPPORT BOEING737 737301 1384611NM 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 CORRODED SCREW HOLES, RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 13 INCHES RBL. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW ONE, SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001681995081100168NM 1995 8 11 USAA950742 119950626A5314 KEEL BEAM BOEING737 737301 1384611NM BS 506 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH SQ CORRODED AREA S28R RT KEEL BEAM STA 506 O/B SIDE. INSTALLED REPAIR ANGLE EA 39374. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001691995081100169NM 1995 8 11 USAA950743 119950626A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 986.5 - 1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL, 2 CORRODED SCREW HOLES BS 986.5 TO BS 1006 13 INCHES LBL. FABRICATED NEW INTERCOSTAL SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001701995081100170NM 1995 8 11 USAA950744 119950627A53206546812198 INTERCOSTAL BOEING737 737301 1384611NM BS 967 - 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERCOSTAL, 3 SCREW HOLES CORRODED BS 967 TO 986.5 18 INCHES LBL. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL, SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001711995081100171NM 1995 8 11 USAA950745 119950627A5347 SEAT TRACK BOEING737 737301 1384611NM BS 360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND INTERGRANULAR CORROSION 1 INCH BY 2 INCH SEAT TRACK AT STA 360 RBL 54. FABRICATED NEW SEAT TRACK SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811001721995081100172NM 1995 8 11 USAA950746 119950627A5320 SUPPORT BOEING737 737301 1384611NM BS 986.5 - 1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 CORRODED SCREW HOLES RT AFT LAVATORY FLOOR SUPPORT BS 986.5 PLUS 7 INCHES TO 1006 36 INCHES RBL. FABRICATED NEW SUPPORT SRM 51-10-02 PG 15. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811003051995081100305NM 1995 8 11 9511702288 119950629A5751 SKIN BOEING727 727251 138408HNM RT AILERON DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US 21376 DURING LINE CHECK, FOUND PREVIOUS REPAIR DELAMINATING ON THE RIGHT OUTBOARD AILERON LOWER SURFACE. REPLACED AILERON (P/N 65-21766-58J). 2L73 4F A3WE 19950811003061995081100306NM 1995 8 11 9511712702 119950712A5751 FITTING BOEING727 727225 1384077NM LT AILERON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON SPAR FITTING. REPLACED AILERON (P/N 65-21766-57J). 2L73 4F A3WE 19950811003071995081100307NM 1995 8 11 9511726623 119950725A5755 SKIN BOEING747 747251B 1384892NM NR 7 SPOILER DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01623US 21705 DURING LINE CHECK, FOUND 2 FT BY 3 FT DELAMINATION ON THE NR 7 SPOILER. REPLACED SPOILER (P/N 65B02310-1). 2L74 4F A20WE 19950811003081995081100308NM 1995 8 11 9511732712 119950726A5753 SKIN BOEING727 7272S7 138407ZNM LT TE FLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01712RC 22020 DURING LINE CHECK, FOUND 4 DELAMINATION IN THE LEFT INBOARD TRAILING EDGE FLAP. REPAIRED PER SRM 51-40-6. 2L73 4F A3WE 19950811003091995081100309WP 1995 8 11 9511749991 119950726A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 69 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950811003101995081100310NM 1995 8 11 9511752287 119950726A5320 FITTING BOEING727 727251 138408HNM FS 640-654 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND CORROSION ON THE STR 26R END FITTING AT BS 640 TO 654. REPLACED FITTING PER SRM 51-10-1. 2L73 4F A3WE 19950811003111995081100311WP 1995 8 11 9511769868 119950726A5220 FITTING DOUG DC9 DC951 3022051WP RT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING H-CHECK, FOUND A CRACK IN THE AFT RIGHT OVERWING EXIT LOWER FORWARD SOCKET FITTING. REPLACED FITTING (P/N D 060277-5), PER SRM 53-5 FIG 32A. 2L72 4F A6WE 19950811003121995081100312WP 1995 8 11 9511779607 119950728A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 FRAME FLOOR ATTACH FITTING (P/N 5913700-2), AT RBL 55. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950811003131995081100313WP 1995 8 11 9511789978 119950728A5320 FITTING DOUG DC9 DC931 3022065WP FS 945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 27 END FITTING AT FS 945. REPLACED END FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950811003141995081100314WP 1995 8 11 9511799868 119950801A5230 FITTING DOUG DC9 DC951 3022051WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING H-CHECK, FOUND A .5 INCH CRACK IN THE FORWARD CARGO DOOR LOWER BEAM FORWARD END FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950811003151995081100315NM 1995 8 11 9511805520 119950802A5270 DOOR WARNING BOEING757 757251 1384970NM LT AFT DOOR MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01520US 23208 DURING TAKEOFF ROLL DTW-MEM, LEFT AFT DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT INCIDENT. OPERATIONAL CHECK OK, NO TROUBLE FOUND. 2L72 4F RTA2NM 19950811003161995081100316WP 1995 8 11 ABXA9500641 119950801A7921RU20447A OIL COOLER RROYCE 54210K NIHON YS11 YS11A500 6310416WP RROYCEDART DART54210K 54522EU NR 1 ENGINE CRACKED A ABXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23911AX752 752 21329 2051 21329 NR 1 ENGINE INFLIGHT SHUTDOWN DUE TO LOW OIL PRESSURE, 6 TO 10 PSI. MAINTENANCE FOUND THE NR 1 OIL COOLER LEAKING, CRACKED. REPLACED OIL COOLER IAW ROLLS ROYCE MM 79-20-1. REPLACED NR 1 ENGINE IAW ABX WORK CARD 7202. OPS AND LEAK CHECKED GOOD. 2L72 4T4 T A1PC E5EU 19950811003171995081100317WP 1995 8 11 ABXA9500642 119950804A2150187L100 BELT NIHON YS11 YS11A500 6310416WP AIR COND SYST FRAYED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL23921AX 2117 DURING APPROACH, CREW SMELLED SMOKE. TURNED OFF A/C AND SMELL STARTED TO GO AWAY. INSPECTED AIR CONDITIONING SYSTEM, FOUND SECOND BELT TO COMPRESSOR WORN, FRAYED AND SLIPPING. REPLACED BELT. OPS CHECKED NORMAL IAW ZEE SYSTEMS MM. 2L72 4T A1PC 19950811003181995081100318WP 1995 8 11 ABXA9500643 119950804A2612D237060 FIRE ELEMENT NIHON YS11 YS11A500 6310416WP NR 1 ENGINE SHORTED A ABXAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23921AX 2117 DURING DEPARTURE OUT OF ILN, RECEIVED A LEFT ENGINE FIRE WARNING LIGHT AND BELL. ACCOMPLISHED ENGINE FIRE OVERHEAT CHECKLIST. STILL HAD INDICATION OF FIRE, RETURNED TO ILN FOR LANDING. INSPECTED ENGINE FOR EVIDENCE OF FIRE, NONE FOUND. FOUND FIREWALL ELEMENT SHORTED. REPLACED ELEMENT AT FIREWALL IAW YS-11 MM 26-11-00, OPS CHECKED GOOD. REPLACED NUMBERS ONE THROUGH THREE FIRE BOTTLES AND SQUIBBS. SYSTEM TESTED GOOD IAW YS-11 MM 26-11-0. 2L72 4T A1PC 19950811003191995081100319NM 1995 8 11 DL72L953288 119950805A5754651622296 ANGLE BOEING727 727232 1384082NM NR 6 LE FLAPS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 UPON INSPECTION A CRACK WAS FOUND ON THE LOWER ANGLE BETWEEN THE ACTUATOR RIBS. REPAIRED PER MM 57-54-0 FIG 812. FOUND DURING SHOP INSPECTION FOR NR 6 L/E SLAT. 2L73 4F A3WE 19950811003201995081100320NM 1995 8 11 DL72L953289 119950805A5754651622296 SKIN BOEING727 727232 1384082NM NR 6 LE FLAPS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 UPON INSPECTION A CRACK WAS FOUND IN THE THERMAL ANTI-ICE SKIN BETWEEN THE RIBS O/B FROM THE ACTUATOR RIBS. REPAIRED PER M/M 57-54-0 FIG 803. FOUND DURING SHOP INSPECTION FOR NR 6 L/E SLAT. 2L73 4F A3WE 19950811003211995081100321NM 1995 8 11 DL72L953296 119950728A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND CRACKED AT THE INBD RIB, INBD TRACK ARM IN RADIUS. ALSO, I/B ACTUATOR RIB CRACKED TOP FWD CORNER. REPAIRED PER MM 57-54-0 FIG 805 AND FIG 804. 2L73 4F A3WE 19950811003221995081100322NM 1995 8 11 DL72L953304 119950801A5315 FLOORBEAM BOEING727 727232 1384082NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CORROSION AT FLOORBEAM STA 344 BL 0 THROUGH LBL 60. REPAIRED PER SRM 53-10-8 FIG 10, ID AS PERMANENT REPAIR PER PS 902-5-1 NR 4. 2L73 4F A3WE 19950811003231995081100323NM 1995 8 11 DL72L953305 119950731A5320 TQ BOX BOEING727 727232 1384082NM FS 1235 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, LIGHTENING HOLE CRACKED AT 48 SEC, TORQUE BOX STA 1235 LT SIDE. REPAIRED PER M/M 53-11-0 NR 16 PG 828. 2L73 4F A3WE 19950811003241995081100324NM 1995 8 11 DL72L953306 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 5 BULKHEADS UP FROM ACCESS HOLE 4TH RIB UP. CRACKED AT RIB BULKHEAD ATTACH POINT LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803. 2L73 4F A3WE 19950811003251995081100325NM 1995 8 11 DL72L953307 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CRACK, FOUND INSIDE VERTICAL STABILIZER, 5 BULKHEADS UP FROM ACCESS HOLE 4TH RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT RT SIDE. REPAIRED PER M/M 55-30-O. 2L73 4F A3WE 19950811003261995081100326NM 1995 8 11 DL72L953308 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 4 BULKHEADS UP FROM ACCESS HOLE ON LT SIDE 5TH RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803. 2L73 4F A3WE 19950811003271995081100327NM 1995 8 11 DL72L953309 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE ON RT SIDE 2ND RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803. 2L73 4F A3WE 19950811003281995081100328NM 1995 8 11 DL72L953310 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE AT LT SIDE 3RD RIB UP. CRACKED AT RIB TO BULKHEAD ATTACH POINT. REPAIRED PER M/M 55-30-0 FIG 803. 2L73 4F A3WE 19950811003291995081100329NM 1995 8 11 DL72L953311 119950731A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, CRACK FOUND INSIDE VERTICAL STABILIZER, 2 BULKHEADS UP FROM ACCESS HOLE AT LT SIDE 2ND RIB UP. CRACKED AT BOLT ATTACHED TO BULKHEAD. REPAIRED PER M/M 55-30-0 PG 803. 2L73 4F A3WE 19950811003301995081100330NM 1995 8 11 DL72L953312 119950731A5520 BALANCE BOARD BOEING727 727232 1384082NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, LT ELEVATOR OUTBOARD MOST BALANCE BOARD BAY UPPER BONDED RIB HAS HOLE IN DOUBLER AT O/B END. REPAIRED PER SRM 55-20-3 FIG 3. 2L73 4F A3WE 19950811003311995081100331NM 1995 8 11 DL72S953277 119950720A5311 FRAME BOEING727 727232 1384082NM FS 312 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 FRAME CRACKED IN HALF, STATION 312 RT SIDE AT STR 13 RT. REPAIRED PER SRM 53-10-4, FOUND AT HMV. 2L73 4F A3WE 19950811003321995081100332NM 1995 8 11 DL72S953278 119950803A5720 STIFFENER BOEING727 727232 1384082NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 FOUND DURING C-1 LETTER CHECK, NR 3 SLAT I/B TRACK O/B STIFFENER ANGLE ON WING FRONT SPAR WAS CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813. 2L73 4F A3WE 19950811003331995081100333NM 1995 8 11 DL72S953279 119950803A5720 STIFFENER BOEING727 727232 1384082NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 FOUND DURING C-1 LETTER CHECK, NR 3 SLAT O/B TRACK I/B STIFFENER ANGLE ON WING FRONT SPAR WAS CRACKED. REPLACED STIFFENER PER M/M 57-20-21 PG 813. 2L73 4F A3WE 19950811003341995081100334NM 1995 8 11 DL72S953286 119950804A5311 FRAME BOEING727 727232 1384082NM FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11539DA 22385 FOUND DURING A-2 LETTER CHECK, FUSELAGE FILLET FAIRING ACCESS PANELS 3448 RT AND 3348 LT CORRODED AT HINGE ATTACH POINTS. REPAIRED PER MM 53-30-1. 2L73 4F A3WE 19950811003351995081100335NM 1995 8 11 DL72S953292 119950805A3320 LIGHT BALLAST 036405 BOEING727 727232 1384082NM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11476DA 20753 AFTER STOPPING AT GATE AND DEPLANING, SMOKE STARTED COMING OUT OF OVERHEAD PANEL ABOVE 21A. PULLED ALL CABIN LIGHTING C/BS. FOUND CEILING LIGHT BALLAST BETWEEN 21 AND 22 ABC BURNT UP. DISCONNECTED SAME FWD TOMCO AND PLACED PER MEL 33-00-02. BALLAST WAS SUBSEQUENTLY REPLACED, OPERATION NORMAL. 2L73 4F A3WE 19950811003361995081100336NM 1995 8 11 DL72W953281 119950724A5754 RIB BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 NR 6 SLAT NR 1 RIB CRACKED. REPAIRED PER MM 57-54-0 PG 814, FOUND AT HMV. 2L73 4F A3WE 19950811003371995081100337NM 1995 8 11 DL72W953282 119950724A5754 RIB BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 NR 6 SLAT NR 7 RIB CRACKED. REPAIRED PER MM 57-54-0 PG 814, FOUND AT HMV. 2L73 4F A3WE 19950811003381995081100338NM 1995 8 11 DL72W953283 119950723A5522 SKIN BOEING727 727247 138408FNM LT ELEVATOR LIGHTNING STRIKEA DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 LT ELEVATOR, LIGHTNING DAMAGE L/E TO T/E OB OF TAB. REPAIRED PER SRM 55-20-3 FIG 4, FOUND AT HMV. 2L73 4F A3WE 19950811003391995081100339NM 1995 8 11 DL733953276 119950803A5414 SKIN BOEING737 737347 1384647NM NR 2 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV IN ATL, INSPECTION FOUND THE NR 2 PYLON CHAFED ON THE O/B SIDE AT WING L/E. BURNISHED AREA AND INSTALLED DOUBLER PER SRM 54-50-01 FIG 203. 2L72 4F RTA16WE 19950811003401995081100340NM 1995 8 11 DL733953294 119950803A5210 ATTACH DOOR BOEING737 737347 1384647NM L-1 DOOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV INSPECTION, FOUND L-1 DOOR UPPER GATE FWD SIDE ROD ATTACH LUG BROKEN. REPAIRED ROD ATTACH LUG PER SRM 52-10-02 PG 208 TO 211. 2L72 4F RTA16WE 19950811003411995081100341NM 1995 8 11 DL733953295 119950803A5414 SKIN BOEING737 737347 1384647NM RT PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV, INSPECTION FOUND THE NR 2 PYLON CHAFED ON THE I/B SIDE AT WING L/E. BLENDED WEAR DAMAGE, INSTALLED REPAIR PER SRM 54-50-01 FIG 203. 2L72 4F RTA16WE 19950811003421995081100342NM 1995 8 11 DL733953300 119950802A5414 SKIN BOEING737 737347 1384647NM NR 1 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV, INSPECTION FOUND THE I/B SIDE OF NR 1 PYLON WORN AT WING L/E. BLENDED AREA AND INSTALLED DOUBLER PER DL ERA300634-14 AND SRM 54-50-01 FIG 203. 2L72 4F RTA16WE 19950811003431995081100343WP 1995 8 11 DLL10953285 119950803A33505165741 EEL BATTERY PACK LKHEED1011 10113851 5265010WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11730DA 193C1199 ON LAYOVER, D-SECTION EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A23WE 19950811003441995081100344WP 1995 8 11 DLL13953275 119950704A5320 TEAR STRAP LKHEED1011 10113851 5265010WP FS 549-569 LIFTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND TEAR STRAP LIFTED, C1 BB FS 549 TO 569, STR 25 TO 27. REPAIRED PER SRM 53-31-00 FIG 816. 2L73 4F A23WE 19950811003451995081100345WP 1995 8 11 DLL13953284 119950703A5320 CLIP LKHEED1011 10113851 5265010WP FS 866 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, FOUND CLIPS CORRODED FS 866 FRAME BETWEEN STR 34 TO 35. REPAIRED PER SRM 53-12-00 FIG 817. 2L73 4F A23WE 19950811003461995081100346WP 1995 8 11 DLL13953298 119950805A3350 EEL LKHEED1011 10113851 5265010WP CABIN MALFUNCTIONED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11789DL 193A1142 EMERGENCY LIGHTS FAIL L/O TEST STEPS 13, 14 AND 15, ONLY C-ZONE LIGHTS CAME ON. RESET EMERGENCY LIGHTS, CHARGE C/B'S, TEST OK. 2L73 4F A23WE 19950811003471995081100347NM 1995 8 11 UPS204026 119950807A5754651622193 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01210UP 21697 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 SLAT RIB STRUCTURE BUILD UP FOR ACTUATOR ROD END MOUNT IS CRACKED. REMOVED DAMAGED SLAT AND REPLACED WITH SERVICEABLE SLAT PER MM 27-81-11. 2L73 4F A3WE 19950811003481995081100348NM 1995 8 11 UPS204027 119950807A57207075T6 FITTING BOEING727 727247 138408FNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01210UP 21697 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LOWER IB T/E SUPPORT BEAM FOR NR 8 SPOILER SUPPORT FITTING IS CRACKED AND HAS SEVERAL LOOSE FASTENERS. REMOVED CRACKED SUPPORT FITTING, FABRICATED REPAIR PARTS IAW B 727-5710-7222-A. 2L73 4F A3WE 19950811003491995081100349NM 1995 8 11 UPS204028 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 756-796 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05,00-01), ON FUEL CELL UPPER SKIN FROM 756 TO 796 RBL 32 TO 45 WL 203. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003501995081100350NM 1995 8 11 UPS204029 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 857-860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00-01), ON FUEL CELL UPPER SKIN FROM BS 857 TO 860 RBL 66 TO 69. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003511995081100351NM 1995 8 11 UPS204030 119950807A5330 SKIN BOEING727 72727C 138400JNM BS 761-765 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00-01), ON FUEL CELL UPPER SKIN BS 761 TO 765 RBL 11 TO 17. REMOVED CORROSION AND BLENDED AREA, SHOT PEENED AREA, ALODINED AND PRIMED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003521995081100352NM 1995 8 11 UPS204031 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 837-870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (CS53-224-05.00-01), ON FUEL CELL UPPER SKIN BS 837-870 LBL 25 TO 45. REPAIRED IAW UPS EO NR 727-57-1116. 2L73 4F A3WE 19950811003531995081100353NM 1995 8 11 UPS204032 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 804-860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (CS53-224-05.00-01), ON FUEL CELL SKIN UPPER SURFACE BS 804 TO 860 LBL 47 TO 62 WL 203. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003541995081100354NM 1995 8 11 UPS204033 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 759/761 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION WHILE WORKING FUSE 82 ON TOP SIDE OF FUEL CELL SKIN AT BS 759 AND 761 RBL 67 WL 206. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003551995081100355NM 1995 8 11 UPS204034 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 780-800 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF FUEL CELL SKIN BS 780 TO 800 LBL 47 TO 62. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003561995081100356NM 1995 8 11 UPS204035 119950807A53202024T3 FLOOR BOEING727 72727C 138400JNM BS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT INBOARD DOG HOUSE FLOOR TO BE CRACKED AT BS 294 LBL 25. REPAIRED IAW SRM 51-40-02 AND 51-30-2. 2L73 4F A3WE 19950811003571995081100357NM 1995 8 11 UPS204036 119950807A5347 SEAT TRACK BOEING727 72727C 138400JNM BS 1130-1138 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 1130 TO 1138 RBL 45 WL 208. REMOVED, FABRICATED, REPLACED SEAT TRACK IAW SRM 53-10-1, M/M 51-30-2. 2L73 4F A3WE 19950811003581995081100358NM 1995 8 11 UPS204037 119950807A5347BAC15201432 SEAT TRACK BOEING727 72727C 138400JNM BS 360-365 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK BS 360 TO 365 LBL 23 WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-10-2, 51-10-6, MM 51-20-151 SRM 51-30-2. 2L73 4F A3WE 19950811003591995081100359NM 1995 8 11 UPS204038 119950807A57127075T6 RIB BOEING727 72727C 138400JNM WS 171.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W STA 171.5 UPPER RIB CHORD CRACKED AT STRINGER 5 TO 20 ATTACH POINT. REMOVED FASTENERS AND CUT OUT DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-2, 51-30-2. 2L73 4F A3WE 19950811003601995081100360NM 1995 8 11 UPS204039 119950807A53307075T6 SKIN BOEING727 72727C 138400JNM BS 740-870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON FUEL CELL UPPER SKIN BS 740 TO 870 RBL 47 TO 62. REPAIRED IAW UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003611995081100361NM 1995 8 11 UPS204040 119950807A5330 SKIN BOEING727 72727C 138400JNM BS 760-870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON FUEL CELL UPPER SKIN BS 760 TO 870 BL 0 LBL 25. REMOVED CORROSION PER UPS EO NR 727-57-1416. 2L73 4F A3WE 19950811003621995081100362NM 1995 8 11 UPS204041 119950807A53157075T6 FLOORBEAM BOEING727 72727C 138400JNM BS 344 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON PREVIOUS SPLICE REPAIRS OF FLOORBEAM BS 344 LBL 35 RBL 14 AND 23 WL 208. INSTALLED NEW UPPER FLOORBEAM IAW SRM 53-10-8 AND 51-30-2, 53-10-1. 2L73 4F A3WE 19950811004241995081100424SO 1995 8 11 95ZZZX3815 119950717A3221 SUPPORT PIPER PA34 PA34220T 7103420SO NLG STA 49.7 CRACKED A MNTAK NONE O OTHER ININSP/MAINT 1 NM038239D2340 348333001 DURING INSPECTION OF SB983, FOUND SUPPORT CRACKED. THIS AIRCRAFT HAS NOT BEEN SUBJECT TO HARD LANDING, BUT WAS FOUND CRACKED. THE OLD STYLE SUPPORT IS VERY WEAK. NEW STYLE MUCH BETTER. SUBMITTER SUGGESTS MANDATORY COMPLIANCE. 1L72 3O A7SO 19950811004261995081100426NE 1995 8 11 95ZZZX3817 219950718A853040698 PISTON BEECH 18 E18S 1151006CE PWA R985 R985AN14B 52008NE NR 6 CYLINDER CRACKED A VLLAK NONE K FLUID LOSS ININSP/MAINT 1 GL059669N 717 BA382 JP206207 AFTER POST-FLIGHT INSPECTION, PILOT REPORTED OIL DRIPPING FROM NR 6 CYLINDER EXHAUST STACK. REMOVED CYLINDER, FOUND NR 6 PISTON CRACKED SPANWISE ACROSS PISTON TOP CAUSING OIL TO DRAIN OUT EXHAUST STACK. THERE WERE NO OTHER SIGNS OF DAMAGE TO CYLINDER OR LINK ROD. 1L72 3R3 R A765 5E1 19950811004311995081100431NM 1995 8 11 95ZZZW801 119950613A3350RPS1B EEL CHARGER BOEING737 7372B7 1384560NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19281AU 23114 BWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS. REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER. REF USAA950608. 2L72 4F A16WE 19950811004321995081100432NM 1995 8 11 CAL950477 119950530A5312 BLKHD DOUBLER BOEING727 727225 1384077NM BS 1183 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW098886Z 21855 DEN - INSPECTION FOUND CORROSION ON ANGLE DOUBLER AT STA 1183 PRESSURE BULKHEAD BEAM. A DOUBLER WAS FABRICATED AND INSTALLED PER BOEING DRAWING 69-60242. (W) 2L73 4F A3WE 19950811004331995081100433NM 1995 8 11 CALA950478 119950530A5320 CHORD BOEING727 727225 1384077NM BS 294 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW098886Z 21855 DEN - INSPECTION FOUND CORROSION ON THE NLG CHORD AT STA 294L WL 148. A REPAIR WAS INSTALLED PER SRM 51-40-4. (W) 2L73 4F A3WE 19950811004341995081100434NM 1995 8 11 USAA950603 119950608A2742AR7077M3 ACTUATOR BOEING737 7373B7 1384580NM STAB TRIM FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19385US 22958 PIT - FLT 1662 - AFTER DEPARTURE, CREW WAS UNABLE TO TRIM STABLIZER WITH THE YOKE SWITCHS. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED STAB TRIM MAIN ELECTRIC ACTUATOR. OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950811004351995081100435NM 1995 8 11 USAA950604 119950609A2613 SENSOR BOEING737 7373B7 1384580NM NR 2 ENGINE MISALIGNED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19521AU 23856 SAN - FLT 1152 - ON CLIMBOUT, NR 2 ENGINE OVERHEAT LIGHT CAME ON. THROTTLE REDUCED TO IDLE AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO SAN WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPOSITIONED CORE ENGINE DETECTOR. RAN ENGINE AT TAKEOFF AND CLIMB SETTINGS, LIGHT REMAINED OFF. (W) 2L72 4F RTA16WE 19950811004361995081100436NM 1995 8 11 USAA950605 119950524A33503114981 EEL SOCKET BOEING737 7372B7 1384560NM CABIN CORRODED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19269AU 22881 CLE - THE RT FORWARD SLIDE LIGHT INOPERATIVE. MAINTENANCE FOUND SOCKET ASSEMBLY CORRODED. REPLACED SOCKET ASSEMBLY, OPS CHECKED GOOD. (W) 2L72 4F A16WE 19950811004371995081100437NM 1995 8 11 USAA950608 119950613A3350 EEL WIRING BOEING737 7372B7 1384560NM CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19281AU 23114 BWI - FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AT ROW 1C FLOOR LIGHTS. REPLACED FORWARD FLOOR EMERGENCY LIGHTS BATTERY CHARGER. REF 95ZZZW801. 2L72 4F A16WE 19950811004381995081100438NM 1995 8 11 USAA950624 119950313A5313 STRINGER BOEING737 7372B7 1384560NM BS 948.8 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19268AU 22880 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 6 INCHES CORROSION S27L BS 948.8. REPAIRED PER SRM 53-10-8. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950811004391995081100439NM 1995 8 11 USAA950625 119950328A5315 BEAM BOEING737 7372B7 1384560NM BS 948 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19268AU 22880 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1.5 INCH CORRODED AREAS AROUND CLIP NUT HOLES, BS 948 LBL 11 TO RBL 49, CABIN FLOORBEAM. REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950811004401995081100440NM 1995 8 11 USAA950626 119950313A5313 STRINGER BOEING737 7372B7 1384560NM BS 847 - 867 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19268AU 22880 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCHES CORROSION S21R BS 847 TO 867. REPAIRED PER SRM 53-10-3 DETAIL 7. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (W) 2L72 4F A16WE 19950811004411995081100441NM 1995 8 11 USAA950642 119950618A323365446259 ACTUATOR BOEING737 737201 1384454NM NLG FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19234US 22274 BWI - FLT 1120 - UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR. (W) 2L72 4F A16WE 19950811004421995081100442NM 1995 8 11 USAA950644 119950626A5230 SEALS BOEING737 7373B7 1384580NM CARGO DOORS LOOSE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19376US 22955 BWI - FLT 7004 - UNABLE TO PRESSURIZE AC AFTER TAKEOFF. FLIGHT RETURNED TO BWI WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE FOUND DOOR SEALS ON BOTH CARGO DOORS OUT OF CHANNELS. SECURED SEALS, AC PRESSURIZED NORMALLY. (W) 2L72 4F RTA16WE 19950811004431995081100443NM 1995 8 11 USAA950645 119950627A2613 SENSOR BOEING737 7373B7 1384580NM LT ENGINE FAILED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19391US 23313 MCO - FLT 1018 - ON CLIMBOUT, LT WING BODY OVERHEAT LIGHT ILLUMINATED. FLIGHT RETURNED TO MCO WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE PYLON OVERHEAT SENSOR. (W) 2L72 4F RTA16WE 19950811004441995081100444NM 1995 8 11 USAA950646 119950629A2910 HYD LINE BOEING737 737301 1384611NM B-HYD SYST LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19340US 23237 CLT - FLT 1702 - ON CLIMBOUT, B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED AND QUANTITY LEVEL BEGAN TO DROP. FLIGHT RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE CHANGED B-SYSTEM HYDRAULIC ELECTRIC PUMP LINE FROM ACCUM TO B-SYSTEM RETURN MODULE AND REPLACED B-SYSTEM ENGINE PUMP. (W) 2L72 4F RTA16WE 19950811004451995081100445NM 1995 8 11 USAA950647 119950618A3350 EEL BATT PACK BOEING757 757225 1384959NM CABIN DISCHARGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19609AU 22205 LGA - FLT 505 - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, OPERATION OF LIGHTS CHECKED GOOD. (W) 2L72 4F RTA2NM 19950811004461995081100446EU 1995 8 11 USAA950651 119950627A2612 FIRE WIRE FOKKERF28 F28MK0100 4990807EU APU CHAFED A USAAAF UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 EA19894US 11379 PIT - FLT 348 - AFTER TAKEOFF, THE APU FIRE LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BOTTLES AND THE LIGHT EXTINGUISHED. FLIGHT RETURNED TO PIT. MAINTENANCE FOUND THE APU FIRE DETECTION WIRE CHAFED THROUGH. THE DETECTION ELEMENT, FIRE BOTTLE AND FIRE WIRE WAS REPLACED. OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950811004471995081100447EU 1995 8 11 USAA950652 219950629A753232145525 PRSOV BOEING737 737401 1384701NM CFMINTCFM56 CFM563B2 13802EU LT ENGINE LEAKING A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA19421US 23988 RIC - FLT 2151 - ON CLIMBOUT, NR 1 ENGINE FIRE WARNING LIGHT AND OVERHEAT LIGHT ILLUMINATED, NR 1 ENGINE WAS SHUTDOWN. CREW FIRED THE BOTTLES INTO NR 1 ENGINE AND DIVERTED TO RIC WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE PRSOV DUE TO LEAK AT SHAFT SEAL. GROUND RUN LEAK CHECK GOOD. (W) 2L72 4F4 FRTA16WE E21EU 19950811004481995081100448NM 1995 8 11 USAA950653 119950702A21307638102 PRESS CONTROLLER BOEING737 7373B7 1384580NM CABIN FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19518AU 23704 MCO - FLT 738 - CABIN ALTITUDE STARTED CLIMBING AT 9OO FPM AND REACHED 10,000 FT CABIN ALTITUDE, ALERT HORN SOUNDED. FLIGHT DIVERTED TO MCO WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PRESSURE CONTROLLER, PRESSURE SELECTOR, AND OUTFLOW VALVE. OPS CHECK NORMAL. (W) 2L72 4F RTA16WE 19950811004491995081100449NM 1995 8 11 USAA950716 119950622A5315 FLOORBEAM BOEING737 737401 1384701NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 30 INCHES STA 986 LBL, 12 INCHES TO FRAME. REPAIRED PER EA 39362, T-CAP SECTION REPLACED PER EA 39362. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004501995081100450NM 1995 8 11 USAA950717 119950622A5315 FLOORBEAM BOEING737 737401 1384701NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 INCH BY .75 INCH AREA OF CORROSION, STA 986.5 FLOORBEAM UPPER WEB RBL 4. REPAIRED PER SRM 53-60-51 FIG 201, DOUBLER INSTALLED PER SRM 53-60-51 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004511995081100451NM 1995 8 11 USAA950718 119950622A5315 FLOORBEAM BOEING737 737401 1384701NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCH STA 986 RBL, 25 INCHES TO FRAME. REPLACED T-CAP PER EA 39362, REPAIRED PER EA 39362. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004521995081100452NM 1995 8 11 USAA950719 119950622A5315 FLOORBEAM BOEING737 737401 1384701NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .75 BY .75 AREA OF CORROSION STA 986.5 FLOORBEAM WEB RBL 43. REPAIRED PER SRM 53-60-51 FIG 201, DOUBLER INSTALLED PER SRM 53-60-51 FIG 201. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004531995081100453NM 1995 8 11 USAA950720 119950602A5315 FLOORBEAM BOEING737 737401 1384701NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19419US 23986 INT - DURING Q-1 CHECK VISUAL INSPECTION FOUND APPROX 1 INCH BY 7 INCH AREA CORRODED STA 312 ON FLOORBEAM BL 0 RBL 7. REPAIRED PER TR 53-10-03, CUT OUT CORRODED SECTION OF UPPER T-CAP AND SPLICED IN NEW SECTION. THERE WAS LESS THAN ONE POUND ADDED FOR REPAIR. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004541995081100454 1995 8 11 USAA950721 419950613A2564R0680101 NR 2 ASPIRATOR BOEING727 727247 138408FNM LIFE RAFT FAILED A USAAK NONE O OTHER ININSP/MAINT 1 EA19749US 21393 CLT - THE NR 2 ASPIRATOR ON LIFE RAFT, SERIAL NR TJ260 FAILED TEST. MAINTENANCE REPLACED THE SLIDE ASPIRATORS. OPERATIONS CHECKED GOOD. (W) 2L73 4F A3WE 19950811004551995081100455NM 1995 8 11 USAA950725 119950629A5320 INTERCOSTAL BOEING737 737301 1384611NM BS 312 - 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19334US 23231 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 16 INCH CORROSION BS 312 TO BS 328 RBL 12. REPLACED WITH PREFAB INTERCOSTAL SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (W) 2L72 4F RTA16WE 19950811004561995081100456NM 1995 8 11 USAA950747 119950705A2130 PRESSURIZATION BOEING737 7374B7 1384702NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19775AU 24933 DCA - FLT 1454 - UNABLE TO PRESSURIZE AC. FLIGHT RETURNED TO DCA WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE PRESSURIZED AC WITH APU AND BOTH ENGINES. AC PRESSURIZED NORMALLY. (W) 2L72 4F RTA16WE 19950811004571995081100457NM 1995 8 11 USAA950748 119950708A2910 HYDRAULIC LINE BOEING737 737201 1384454NM RT MLG LEAKING A USAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 EA19240AU 22355 ROC - FLT 2274 - UPON GEAR RETRACTION ON TAKEOFF, A-SYSTEM QUANTITY WENT TO ZERO AND A-SYSTEM LOW PRESSURE LIGHTS CAME ON. FLIGHT RETURNED TO ROC WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING AT RT MAIN GEAR UPLOCK CYCLINDER. REPLACED LINE. (W) 2L72 4F A16WE 19950811004581995081100458EU 1995 8 11 USAA950750 119950708A2150220348024 EEL PACK FOKKERF28 F28MK0100 4990807EU LT FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19899US 11399 CLT - FLT 166 - AT APPROX FL 301, THE LT PACK WENT OUT MAKING A LOUD NOISE. CREW DECIDED TO DIVERTED TO CLT. MAINTENANCE REPLACED THE LT PACK ASSEMBLY, OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950811004591995081100459EU 1995 8 11 USAA950751 119950709A29106607P98D SWITCH FOKKERF28 F28MK0100 4990807EU NR 1 HYD SYST FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA19861US 11297 CLT - FLT 446 - ON TAKEOFF, CREW RECEIVED AN ALERT MESSAGE OF A NR 1 HYDRAULIC SYSTEM FAILURES. CAPTAIN DECLARED AN EMERGENCY AND LANDED IN CLT. MAINTENANCE FOUND THE NR 1 ENGINE, NR 1 HYDRAULIC PRESSURE SWITCH CONTACTS FAULTY AND RPLACED THE SWITCH. OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950811004601995081100460EU 1995 8 11 USAA950752 119950711A2130 VALVE FOKKERF28 F28MK0100 4990807EU RT LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19863US 11303 RDU - FLT 109 - THE CABIN PRESSURE WOULD NOT CLIMB WITH ALTITUDE. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO RDU. MAINTENANCE INSTALLED A NEW VALVE AT THE RT SIDE EXTERNAL AIR CONNECTION. OPERATIONS CHECKED GOOD. (W) 2L72 4F RT 19950811005091995081100509EU 1995 8 11 95ZZZX3872 119950524A2150365A32285802 BRACKET AEROSPSA365 AS365N2 8680815EU AIR COND CRACKED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM705 6429 AIR CONDITIONING BRACKET CRACKED. REMOVED AND REPLACED BRACKET. 1G72 3U RTH10EU 19950811005101995081100510EU 1995 8 11 95ZZZX3873 119950605A2822P94C16606 PUMP AEROSPSA365 AS365N2 8680815EU FUEL BOOST INOPERATIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM719 20907 6429 BOOST PUMP INOPERATIVE. REMOVED AND REPLACED BOOST PUMP. 1G72 3U RTH10EU 19950811005111995081100511EU 1995 8 11 95ZZZX3874 119950422A5210365A25313821 ROD AEROSPSA365 AS365N2 8680815EU CABIN RT BROKE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM672 6429 ROD BROKE AT CENTER BOLT HOLE. REMOVED AND REPLACED ROD. 1G72 3U RTH10EU 19950811005121995081100512EU 1995 8 11 95ZZZX3875 119950428A7400HE402D GENERATOR AEROSPSA365 SA365N 8680669EU HE GENERATOR INOPERATIVE A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365SJ 9039 6018 H. E. GENERATOR INOPERATIVE. 1G72 3U H10EU 19950811005131995081100513EU 1995 8 11 95ZZZX3876 119950316A6520350A33215300 LAMIFICATION SNIAS 350 AS350BA 8680817EU T/R UNBONDED A HCMAK NONE O OTHER ININSP/MAINT 1 WP13642BH292 2495 LAMIFICATION DELAMINATED AND UNBONDED. 1G71 3U NCH9EU 19950811005141995081100514EU 1995 8 11 95ZZZX3877 119950529A6410355A09103600 BEARING SNIAS 350 AS350BA 8680817EU T/R HALF SHELL WORN A HCMAK NONE O OTHER ININSP/MAINT 1 WP13752BH423 2510 HALF SHELL BEARING WORN BEYOND LIMITS. 1G71 3U NCH9EU 19950811005161995081100516NM 1995 8 11 9511812771 119950803A21317612608 CONTROLLER BOEING727 7272M7 138407SNM FLIGHT DECK MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01742RW22930313 21952 AFTER LEVEL OFF AT FL 240 WITH SINGLE PACK OPERATION, LEFT CABIN ALTITUDE CONTINUED A 200 FPM CLIMB. UNABLE TO CONTROL BY ALTERNATE MEANS. FLIGHT JETTISONED 10,000 LBS OF FUEL, DIVERTED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED AUTO PRESSURE CABIN CONTROLLER. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950811005171995081100517NE 1995 8 11 9511822252 219950704A7532 PRBC BOEING727 727251 138408HNM PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01255US 19971 653978 NR 1 ENGINE HAD LOW FREQUENCY VIBRATION AT POWER SETTINGS ABOVE 70 PERCENT N2. FLIGHT RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PRBC AND TESTED THE ENGINE. ENGINE PERFORMANCE WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950811005181995081100518WP 1995 8 11 9511839928 119950804A3260 UPLOCK SWITCH DOUG DC9 DC931 3022065WP RT MLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018921E 45836 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO YYC AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR UPLOCK SWITCH. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811005191995081100519WP 1995 8 11 9511849150 119950802A3150 SWITCH DOUG DC9 DC914 3022034WP HORIZ STAB FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018908E 45749 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL AT 1.4 EPR. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED THE HORIZONTAL STABILIZER SWITCH (S1-141) AND FLAP SWITCH (S1-159). OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811005201995081100520WP 1995 8 11 9511859753 119950803A21311313082 CONTROLLER DOUG DC9 DC941 302207NWP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01753NW1118311183 47117 LOSS OF AUTO PRESSURIZATION OCCURRED AFTER TAKEOFF. FOUND CABIN PRESSURE AUTO/MANUAL CIRCUIT BREAKER POPPED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RESET CIRCUIT BREAKER. REGAINED CABIN PRESSURIZATION THROUGH MANUAL CONTROL. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED PRE-PRESSURE CONTROLLER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811005211995081100521 1995 8 11 9511869923 419950804A3420 COMPASS DOUG DC9 DC932 3022066WP RT COCKPIT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01927RC 47469 FIRST OFFICER'S COMPASS FLAGGED ON HSI AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. SYSTEM OPERATED NORMALLY DURING GROUND CHECK. DISCREPANCY COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950811005221995081100522NE 1995 8 11 95UAL900082 219950809A7200 ENGINE AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE NR 1 FLAME-OUT A UALAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION NRNOT REPORTED 1 WP29404UA 450 V10020 NUMBER ONE ENGINE FLAMED-OUT IN FLIGHT. 2L72 4F RTA28NM E40NE 19950811005231995081100523NE 1995 8 11 95UAL900083 219950721A7260804277 CARBON SEAL BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 4 GEARBOX CHIPPED A UALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29154UA 20103 662764 AFTER REACHING CRUISE ALT NR 4 ENG OIL QTY DROPPED TO JUST ABOVE 1 GAL ON IND, ALL OTHER IND OK. OIL QTY SLOWLY DECREASED TO ZERO AT 5.5 HOURS INTO FLT, THEN PRESS FLUCT, AT 8 HRS LOW OIL PRESS LIGHT CAME ON AND ENGINE SHUTDOWN. CSD CARBON SEAL LOCATED ON THE MAIN GEARBOX WAS FOUND TO BE DAMAGED. CARBON SEAL WAS REPLACED. 2L74 4F4 F A20WE E20EA 19950811005241995081100524NM 1995 8 11 DL72S953316 119950806A3350 EEL BATTERY PACK 6013211 BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11411DA 21223 AFT LEFT AND RIGHT SERVICE DOOR EMERGENCY SLIDE LIGHT INOP. SECURED BATTERY PACK AT M983 POWER SUPPLY. 2L73 4F A3WE 19950811005251995081100525NM 1995 8 11 DL72S953330 119950720A5313 STRINGER BOEING727 727232 1384082NM BS 720 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 STR CRACKED BETWEEN STA 720B AND 720C STR 15L FWD AND AFT OF LIGHT BOX. REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19950811005261995081100526NM 1995 8 11 DL72S953332 119950721A5320 CHANNEL BOEING727 727232 1384082NM BS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 TOP OF VERT U-SUPPORT CHANNELS, UNDER CABIN FLOOR, ARE WORN AT TOP AND ATTACH BOLT WASHERS AT RBL 24 AND 52 STA 720D AND 24 LBL. SUPPORTS CAME FROM B/B. INSTALLED PER SRM 53-10-9. 2L73 4F A3WE 19950811005271995081100527NM 1995 8 11 DL72S953333 119950725A5330 PANEL SUPPORT BOEING727 727232 1384082NM BS 780-800 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 PANEL SUPPORT CORRODED BETWEEN STA 780 TO 800 LBL 8.0. FABRICATED NEW SECTION PER M/M 53-30-1 PG 807 TO 808. INSTALLED REPAIR PER MM 53-30-1 PG 807 AND FIG 804, FOUND AT HMV. 2L73 4F A3WE 19950811005281995081100528NM 1995 8 11 DL72W953302 119950806A2782269002914 ACTUATOR BOEING727 727247 138408FNM NR 3 SLAT FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO112822W 21327 FLT 1400 CALLED EMERGENCY APPROACH INTO SFO, A HYD SYST LEAKING RAPIDLY. CREW FREE FEEL LANDING GEAR TO ACCOMPLISH LDG GEAR EXTENSION. MTC TOWED A/C TO GATE AND FOUND NR 3 LEADING EDGE SLAT ACTUATOR END BLOWN /SEPERATED FROM PISTON. ACTUATOR END REMOVAL AND REPLACEMENT OF ACTUATOR COMPLIED WITH. GEAR SWING ACCOMPLISHED, SYST OPS CHECK NORMAL. 2L73 4F A3WE 19950811005291995081100529NM 1995 8 11 DL72W953320 119950724A575465162255A LE SKIN BOEING727 727247 138408FNM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 CORNER MISSING L/E OF O/B END, NR 3 L/E KRUGER FLAP. REPAIRED PER M/M 57-53-0 FIG 803, DURING SHOP VISIT. 2L73 4F A3WE 19950811005301995081100530NM 1995 8 11 DL73E953301 119950806A33501619 EEL BULB BOEING737 737247 138448DNM RT OVERWING FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11381DL 23608 AFT OVERWING RT SLIDE EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK NORMAL. FOUND AT LAYOVER. 2L72 4F A16WE 19950811005311995081100531NM 1995 8 11 DL73S953297 119950806A33501619 EEL BULB BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11310DA 23082 EXTERIOR EMERGENCY LIGHT INOP AT L2 DOOR. RELAMPED, OPERATION NORMAL. 2L72 4F RTA16WE 19950811005321995081100532 1995 8 11 DL73S953299 419950806A3421 ADI 7725005005 BOEING737 737232 1384475NM LT COCKPIT INOP A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11322DL 6K2607 23094 CAPT ADI INOP WITH ALT FLAG, ROLL LIGHT ILLUMINATED. TEST SWITCH RESULTED IN INDICATOR SPINNING AT HIGH SPEED IN ROLL DIRECTION, AUX GYRO NO HELP. AIR TURNBACK TO ATL AT 1420. C/A REPLACED CAPT ADI, FUNCTIONS NORMAL. 2L72 4F RTA16WE 19950811005331995081100533NM 1995 8 11 DL76S953315 119950806A3350 EEL BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11130DL 24080 OVERHEAD EMERGENCY WALKWAY LIGHTS INOP AT 39F, 47C AND 28C. RELAMPED, OPERATIONAL OK. 2L72 4F RTA1NM 19950811005341995081100534WP 1995 8 11 DLL13953173 119950706A5320 ANGLE LKHEED1011 10113851 5265010WP BS 349 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 LOWER SUPPORT BEAM ATTACHED TO PRESSURE DECK CRACKED AT RBL 84 FS 349.1. REPLACED ANGLES, TEATED AND PAINTED. REINSTALLED FLOORBEAM SUPPORT STRUT PER SRM 53-21-00 PG 829. 2L73 4F A23WE 19950811005351995081100535WP 1995 8 11 DLL13953322 119950706A57121647070 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 LT/RT WING RIB UPPER CAPS AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPLACED CAP PER ERA 271319-14AD. 2L73 4F A23WE 19950811005361995081100536WP 1995 8 11 DLL13953325 119950720A5312 BLKHD SKIN LKHEED1011 10113851 5265010WP BS 1365 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 FOUND THAT 65 FASTENER HOLES WERE TOOL DAMAGED AT FS 1365 BULKHEAD, STR 22 TO STR 47. ACCOMPLISHED REPAIRS PER DL ERA 271346-14. REPAIRED PER ERA 271346-14. 2L73 4F A23WE 19950811005371995081100537WP 1995 8 11 MWEA95247 119950807A3350 EEL SIGN DOUG DC9 DC915 3022036WP FWD GALLEY DETACHED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31900ME 45841 THE EMERGENCY EXIT LIGHT SIGN CAME OFF THE WALL, NEXT TO THE FWD GALLEY SERVICE DOOR. MAINTENANCE INSTALLED NEW SIGN. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811005381995081100538NM 1995 8 11 P5CA9500651 119950703A5320 BRACKET BOEING747 747121 1384871NM APU COMPT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED APU AFT MOUNT SUPPORT ROD MOUNTING BRACKET IS CRACKED BOTH SIDES. REPAIRED PER BOEING SRM 51-20-02. 2L74 4F A20WE 19950811005391995081100539NM 1995 8 11 P5CA9500652 119950703A5730 SKIN BOEING747 747121 1384871NM RT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON LOWER RIGHT WING SKIN BETWEEN WBS 254 AND 614. REMOVED CORROSION PER BOEING SRM 57-10-01. 2L74 4F A20WE 19950811005401995081100540NM 1995 8 11 P5CA9500653 119950703A7110 COWL BOEING747 747121 1384871NM NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK WITH STOP HOLE ON EXTERIOR SURFACE O, NR 2 LEFT COWLING, UNDER CSD OIL FILL PANEL. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950811005411995081100541NM 1995 8 11 P5CA9500654 119950703A5530 ANGLE BOEING747 747121 1384871NM VERT STAB CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON VERTICAL STABILIZER AT STA 232.5 LEFT ANGLE ON NUTPLATE STRIP. REPAIRED PER BOEING SRM 51-40-04. 2L74 4F A20WE 19950811005421995081100542NM 1995 8 11 P5CA9500655 119950703A532065B0723206 FIITING BOEING747 747121 1384871NM BS 1240 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS AND CORROSION ON FITTINGS TO S1L AND S1R, BS 1240. REPLACED FITTINGS INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811005431995081100543NM 1995 8 11 P5CA9500656 119950703A532065B0723206 FITTING BOEING747 747121 1384871NM 1240 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKS ON S3L, BS 1240 FWD SIDE. REPLACED FITTING PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811005441995081100544NM 1995 8 11 P5CA9500657 119950703A5330 SKIN BOEING747 747121 1384871NM BS 520 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AROUND FASTENER AT BS 520 S43R. REPAIRED PER BOEING SRM 53-30-03 FIG 47 SHEET 3. 2L74 4F A20WE 19950811005451995081100545NM 1995 8 11 P5CA9500658 119950703A5280 DOOR BOEING747 747121 1384871NM LT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK LEFT WING LANDING GEAR UPPER HALF DOOR FWD SIDE EDGE. REPAIRED PER BOEING SRM 51-40-03. 2L74 4F A20WE 19950811005461995081100546NM 1995 8 11 P5CA9500659 119950703A7110 COWLING BOEING747 747121 1384871NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON NR 3 ENGINE LEFT COWLING INTERIOR. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950811005471995081100547NM 1995 8 11 P5CA9500660 119950703A7110 BRACKET BOEING747 747121 1384871NM NR 3 ENGINE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN HOLDING BRACKET FOR SUPPORT ROD NR 3 ENGINE LEFT COWLING. MANUFACTURED BRACKET PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950811005481995081100548NM 1995 8 11 P5CA9500661 119950703A7110 COWLING BOEING747 747121 1384871NM NR 3 ENGINE DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 DAMAGE ON NR 3 ENGINE LEFT FAN COWL EXTERIOR SKIN. REPAIRED PER BOEING SRM 54-30-03. 2L74 4F A20WE 19950811005491995081100549NM 1995 8 11 P5CA9500662 119950703A7110 COWLING BOEING747 747121 1384871NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON NR 3 ENGINE RIGHT COWLING INTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950811005501995081100550NM 1995 8 11 P5CA9500663 119950703A7110 COWLING BOEING747 747121 1384871NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION AND LOOSE RIVETS ON NR 3 ENGINE COWLING, RIGHT EXTERIOR SURFACE SKIN. REMOVED CORROSION PER BOEING SRM 51-10-01, WITHIN LIMITS. REPLACED LOOSE RIVETS. 2L74 4F A20WE 19950811005511995081100551NM 1995 8 11 P5CA9500664 119950703A7110 COWLING BOEING747 747121 1384871NM NR 2 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON INTERIOR SURFACE SKIN OF NR 2 ENGINE RIGHT COWLING. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950811005521995081100552NM 1995 8 11 P5CA9500665 119950703A7110 COWLING BOEING747 747121 1384871NM NR 2 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON RIVET HEADS AND SHEARED RIVETS ON THE EXTERIOR SURFACE OF NR 2 LEFT COWLING. REPLACED RIVETS PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811005531995081100553EU 1995 8 11 QXEA9500241 119950807A3350MGG1280 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 PDX - EXIT SIGN AT ROW 8 IS DIM. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950811005891995081100589EU 1995 8 11 95ZZZX3913 119950413A7933646600251 PROBE SNIAS 350 AS350B2 8680813EU OIL TEMP ERRATIC A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH840 4652 2804 PROBE UNIT ERRATIC AND CAUSING OIL TEMPERATURE FLUCTUATIONS. 1G71 3U H9EU 19950811005901995081100590EU 1995 8 11 95ZZZX3914 119950503A6520350A33215000 BALL JOINT SNIAS 350 AS350B2 8680813EU T/R WORN A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH915 M189440 2804 BALL JOINT HAS EXCESSIVE AXIAL PLAY IN BEARING. 1G71 3U H9EU 19950811005911995081100591EU 1995 8 11 95ZZZX3915 119950516A6730SC50711 SERVO SNIAS 350 AS350B2 8680813EU T/R LEAKING A HCMAK NONE K FLUID LOSS ININSP/MAINT 1 WP13972BH974 386 2804 SERVO LEAKING BAD IN OUTPUT AREA. 1G71 3U H9EU 19950811005921995081100592EU 1995 8 11 95ZZZX3916 119950516A65207704411 SEAL SNIAS 350 AS350B2 8680813EU T/R BOX LEAKS A HCMAK NONE K FLUID LOSS ININSP/MAINT 1 WP13972BH974 2804 SEAL WORN BEYOND LIMITS. LEAKS BAD. 1G71 3U H9EU 19950811005931995081100593 1995 8 11 95ZZZX3917 419950613A3416066030510000 ENCODER SNIAS 350 AS350B2 8680813EU COCKPIT DEFECTIVE A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH989 74450 2804 ENCODER HAS INACCURATE ALTITUDE ENCODING. 1G71 3U H9EU 19950811005941995081100594EU 1995 8 11 95ZZZX3918 119950215A6310350A35110421 GIMBAL HOUSING SNIAS 350 AS350B2 8680813EU LT EAR MOUNT DAMAGED A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH542 2263 2804 LEFT EAR MOUNT COMPRESSOR PIVOT POINT GROUND DOWN. 1G71 3U H9EU 19950811005951995081100595EU 1995 8 11 95ZZZX3919 119950215A6310350A35110500 GIMBAL RING SNIAS 350 AS350B2 8680813EU ENG/XMSN BEARING UNBONDEDA HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH542 2804 BUSH BEARING WAS SPINNING OR UNBONDING AND TURNING. 1G71 3U H9EU 19950811005961995081100596EU 1995 8 11 95ZZZX3920 119950215A6310350A35110203 COUPLING SNIAS 350 AS350B2 8680813EU GIMBAL BORE WORN A HCMAK NONE O OTHER ININSP/MAINT 1 WP13972BH542 2804 COUPLING BORES WORN. 1G71 3U H9EU 19950811006011995081100601SW 1995 8 11 95ZZZX3925 119950616A6210222015500105 BLADE BELL 222 222 1182122SW M/R DOUBLER SEPARATEA YC6AO OTHER D INFLIGHT SEPARATION CRCRUISE 1 EA25969YC3428 AMR06066 47081 OUTBOARD UPPER SPAN DOUBLER SEPARATED FROM BLADE IN-FLIGHT. DOUBLER WAS REPLACED 2/91. TT SINCE REPAIR, 820 HRS. 1G72 3U H9SW 19950811006021995081100602CE 1995 8 11 95ZZZW802 119950706A3310 LIGHT WIRE CESSNA402 402C 207590RCE COCKPIT FAILED A GUUAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO192615Z 402C0110 MIA-MHN - FLT 102 - BURNING SMELL IN COCKPIT WITH LIGHTS AT FULL INTENSITY. AC RETURNED TO MIA WITHOUT INCIDENT. TROUBLESHOT, FOUND BURNT WIRE AT CIRCUIT BOARD SWITCH. CLEANED AREA AND RESOLDERED WIRE. OPERATIONAL CHECK GOOD. 1L72 3O A7CE 19950811006031995081100603CE 1995 8 11 95ZZZW803 119950709A324030146 CALIPER BEECH 99 C99 1154006CE MLG LOCKED UP A GUUAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO19131GP U225 MIA-DAB - FLT 393 - THE NR 4 MAIN TIRE BRAKE LOCKED UP ON TAXI OUT. REMOVED AND REPLACED NR 4 BRAKE CALIPER, BLED AND SERVICED SYSTEM. RELEASED AC. 1L72 3T A14CE 19950811006041995081100604CE 1995 8 11 95ZZZW804 119950713A3220 CLEVIS BEECH 99 C99 1154006CE NLG SHEARED A GUUAO OTHER O OTHER LDLANDING 1 SO19216EE U206 FLT 102 - NOSE GEAR COLLAPSED ON LANDING. INSPECTED AND DETERMINED NOSE ACTUATOR ROD END CLEVIS TO HAVE SHEARED AT BASE OF SHANK. REMOVED AND REPLACED ACTUATOR, NOSE TRUNNION AND SUBSEQUENT SHEET METAL REPAIRS IN PROGRESS. 1L72 3T A14CE 19950811006051995081100605EA 1995 8 11 95ZZZW805 219950715A7261 OIL SYST BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE OVER SERVICED A GUUAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO19198GA UB5 MIA-ELH - FLT 465 - SMOKE IN CABIN, AC RETURNED TO MIA WITHOUT FURTHER INCIDENT. DETERMINED RT ENGINE TO BE OVER SERVICED. DRAINED OIL TO PROPER LEVEL. AC WAS TEST FLOWN WITH SATISFACTORY RESULTS AND RELEASED FOR SERVICE. 2L72 4T4 TRTA24CE E4EA 19950811006061995081100606CE 1995 8 11 95ZZZW806 119950713A3260 WARNING HORN BEECH 99 C99 1154006CE LANDING GEAR INOP A GUUAK NONE P NO WARNING INDICATION APAPPROACH 1 SO19216EE U206 FPO-FLL - FLT 472 - GEAR WARNING HORN INOP. FERRIED AC TO PRINCIPLE MAINTENANCE BASE. SWUNG GEAR SEVERAL TIMES ON JACKS. GEAR HORN DOOR AND GEAR RIGGING ALL CHECK NORMAL IAW MM 32-30-60 AND 32-60-00. 1L72 3T A14CE 19950811006071995081100607CE 1995 8 11 95ZZZW807 119950622A3260404EN16 SWITCH BEECH 99 C99 1154006CE RT MLG INTERMITTENT A GUUAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 SO197209W U224 MCO-MIA - FLT 396 - THE RT GEAR GREEN DOWN LOCK INDICATOR DOES NOT ILLUMINATE UNTIL APPROX 5 TO 30 SECONDS AFTER THE GEAR IS DOWN. REMOVED AND REPLACED RT DOWN LOCK SWITCH, GEAR SWING GOOD. AC RELEASED. 1L72 3T A14CE 19950811006081995081100608WP 1995 8 11 AALA951142 119950623A3350 EEL WIRE DOUG DC10 DC1010 3022110WP CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07147AA 46702 LAX - FLT 161 - AT THE GATE DURING PS CHECK, UNABLE TO TURN OFF EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN AND FORWARD SERVICE CENTER. WATER WAS LEAKING FROM SERVICE CENTER TRASH BIN, CREATING WIRING SHORT. REPLACED FORWARD SERVICE CENTER TRASH BIN AND DRIED CARPETS AND WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950811006091995081100609WP 1995 8 11 AALA951208 119950707A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07162AA 46943 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE OF FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTORS AT LT AISLE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (W) 2L73 4F A22WE 19950811006101995081100610NM 1995 8 11 ASAA950035 119950627A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01778AS 25110 SEA - CHECK, TRACK LIGHTS INOP ROWS 18 TO 22. MAINTENANCE RECONNECTED LIGHTS. (W) 2L72 4F RTA16WE 19950811006111995081100611NM 1995 8 11 ASAA9510064 119950701A3350900835A EEL BATT PACK BOEING737 7372X6C 1384552NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ON AT ROWS 14 AND 15. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950811006121995081100612NM 1995 8 11 ASAA9510065 119950704A33508621014 EEL BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (W) 2L72 4F A16WE 19950811006131995081100613NM 1995 8 11 ASAA9510066 119950708A335020131A EEL BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, TWO WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 5. REPLACED BATTERY AND LIGHTS OPERATED NORMAL. (W) 2L72 4F RTA16WE 19950811006141995081100614NM 1995 8 11 ASAA9510067 119950711A526065596422 GOVERNOR BOEING737 737290C 138448VNM AFT AIRSTAIR DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 SEA - DURING C-CHECK, THE AFT AIRSTAIR FAILED THE EMERGENCY EXTENSION TIME CHECK. REPLACED CENTRIFUGAL GOVERNOR AND OPERATED WITHIN EMERGENCY EXTENSION TIME LIMITS. (W) 2L72 4F A16WE 19950811006151995081100615NM 1995 8 11 ASAA9510068 119950711A5315 FLOORBEAM BOEING737 737290C 138448VNM BS 328 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER CHORD FLANGE OF THE FLOORBEAM AT BS 328 BETWEEN RBL 14.5 TO 60. PERFORMED INTERIM REPAIR PER EA 5310-1367 AND BOEING TELEX ASA-SEA 95-0438RR. (W) 2L72 4F A16WE 19950811006161995081100616NM 1995 8 11 ASAA9510069 119950711A5315 FLOORBEAM BOEING737 737290C 138448VNM BS 727B CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS 22577 SEA - DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER FORWARD FLANGE OF THE FLOORBEAM AT BS 727B AT LBL 4.00. PERFORMED INTERIM REPAIR PER EA 5310-01365 AND BOEING TELEX ASA-SEA 950429RR. (W) 2L72 4F A16WE 19950811006171995081100617NM 1995 8 11 ASAA9540034 119950627A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - CHECK, AFT TWO RED TRACK LIGHTS INOP. MAINTENANCE RECONNECTED LIGHTS. (W) 2L72 4F RTA16WE 19950811006181995081100618NM 1995 8 11 ASAA9540036 119950630A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 12 WERE FOUND INOPERATIVE. REPAIRED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F RTA16WE 19950811006191995081100619NM 1995 8 11 ASAA9540037 119950704A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - CHECK, AFT THREE TRACK LIGHTS INOP. MAINTENANCE RECONNECTED WIRING. (W) 2L72 4F RTA16WE 19950811006201995081100620NM 1995 8 11 ASAA9540038 119950704A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01771AS 25104 SEA - CHECK, LAST 2 FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED WIRES. (W) 2L72 4F RTA16WE 19950811006211995081100621NM 1995 8 11 ASAA9540039 119950705A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - CHECK, AFT THREE TRACK LIGHTS INOP. MAINTENANCE RECONNECTED LIGHTS. (W) 2L72 4F RTA16WE 19950811006221995081100622 1995 8 11 ASAA9580154 419950628A2565D37013115 SLIDE DOUG DC9 DC983 3022083WP L1 DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 SFO - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (W) 2L72 4F RTA6WE 19950811006231995081100623NE 1995 8 11 ASAA9580155 219950630A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE NR 1 FAILED A ASAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NM01963AS 53077 716728 ANC - AIR TURN BACK OF FLT NR 180, NR 1 ENGINE FAILED DURING CLIMB-OUT PASSING 2500 FEET. ENGINE FAILURE CHECKLIST WAS COMPLIED WITH AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. VENDOR TEARDOWN REVEALED 8TH STAGE COMPRESSOR STATOR VANE FATIGUE FRACTURE AT INNER AND OUTER SHROUDS. (M) 2L72 4F4 FRTA6WE E9NE 19950811006241995081100624WP 1995 8 11 ASAA9580159 119950707A2530416000139 COFFEE MAKER DOUG DC9 DC983 3022083WP NR 3 GALLEY MALFUNCTIONED A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM01961AS 53075 ANC - FLT 107 - FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE ODOR IN GALLEY NR 3 DURING CRUISE. DEACTIVATED GALLEY POWER AND ODOR DISSIPATED. OPERATED ALL AFT GALLEY APPLIANCES AND UNABLE TO DUPLICATE ODOR. REPLACED NR 3 GALLEY COFFEE MAKER AND NO EVIDENCE OF OVERHEATING FOUND. (W) 2L72 4F RTA6WE 19950811006251995081100625WP 1995 8 11 ASAA9580160 119950708A335041B004AD07G3 BATTERY DOUG DC9 DC982 3022082WP TAILCONE DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EXIT LIGHTS OVER EVACUATION SLIDE WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950811006411995081100641SW 1995 8 11 95ZZZX3941 119950522A2435230790001 GENERATOR SWRNGNSA226 SA226TB 8780406SW LT ENG START/GENBEARING FAILED A C2SAE ENGINE SHUTDOWN EH VIBRATION/BUFFET ELECT. POWER LOSS-50 PC CRCRUISE 1 CE01193CS820 T300 EN ROUTE, LEFT STARTER/GENERATOR WENT INOPERATIVE. AFTER 30-40 MINUTES, THE LEFT ENGINE STARTED A VIBRATION AND WAS SHUT DOWN. FOUND REAR BEARING OF STARTER/GENERATOR WAS DISINTEGRATED. 1L72 4T A5SW 19950811006541995081100654WP 1995 8 11 9511879989 119950619A5312 BLKHD WEB DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018944E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER WEB OF THE AFT PRESSURE BULKHEAD AT THE T-CHORD FS 996, APPROXIMATELY 8 OUTBOARD OF RADIALS 22L AND 22R. REPAIRED WEB (P/N 5910130-65) PER EA 99-94812. 2L72 4F A6WE 19950811006551995081100655WP 1995 8 11 9511889150 119950714A5330 SKIN DOUG DC9 DC914 3022034WP FS 942-964 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 942 TO 964 LONGERONS 20L TO 20R. REPAIRED SKIN (P/N 5910228-19), PER EA 91-100809. 2L72 4F A6WE 19950811006561995081100656WP 1995 8 11 9511899150 119950714A5322 SUPPORT DOUG DC9 DC914 3022034WP FS 229-296 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND CORROSION ON THE CENTER FLOOR SUPPORT BETWEEN FS 229 TO 296. REPAIRED SUPPORT (P/N 5910137-9) PER EA 91-100826. 2L72 4F A6WE 19950811006571995081100657WP 1995 8 11 9511909997 119950715A5313 LONGERON DOUG DC9 DC931 3022065WP FS 570 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018933E 47142 DURING H-CHECK, FOUND 2 INCH CRACK IN LONGERON 29L AT FS 570. REPAIRED LONGERON (P/N 5920319-504), PER EA 99-97107. 2L72 4F A6WE 19950811006581995081100658NM 1995 8 11 9511912702 119950718A5753 SKIN BOEING727 727225 1384077NM TE FOREFLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE RIGHT INBOARD FOREFLAP TRAILING EDGE. REPLACED FLAP (P/N 65-21630-188A), PER CITEXT 20-2750-1-9801. 2L73 4F A3WE 19950811006591995081100659WP 1995 8 11 9511929964 119950719A5412 WEB DOUG DC9 DC931 3022065WP PYLON OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01912RW 47150 DURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB LEFT AND RIGHT SIDES. REPAIRED WEB (P/N 9912243-81,-4) PER EA 99-100828. 2L72 4F A6WE 19950811006601995081100660WP 1995 8 11 9511939150 119950719A5330 SKIN DOUG DC9 DC914 3022034WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN FS 200 BETWEEN LONGERONS 14L TO 15L. REPAIRED SKIN (P/N 5911406-7), PER EA 91-100820. 2L72 4F A6WE 19950811006611995081100661NM 1995 8 11 9511942287 119950720A5320 CHORD BOEING727 727251 138408HNM BS 1178 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1178 TENSION CHORD UPPER SURFACE FROM LBL 8 TO RBL 12 WATER LINE 208. REPAIRED CHORD (P/N 65-31773-1), PER EA 22-98929. 2L73 4F A3WE 19950811006621995081100662WP 1995 8 11 9511951155 119950721A5320 CLIP DOUG DC10 DC1040 3023508WP FS 979 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01155US 46764 DURING PERIODIC CHECK, FOUND CORROSION ON THE T-CLIP AT FS 979 BETWEEN LONGERONS 44R AND 45R. REPAIRED CLIP (P/N ADA 0252-7), PER EA 11-98910. 2L73 4F A22WE 19950811006631995081100663WP 1995 8 11 9511969150 119950721A5713 LONGERON DOUG DC9 DC914 3022034WP LT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018908E 45749 DURING H-CHECK, FOUND CORROSION ON LEFT WING STR 11 AT XRS 78 TO 88 AND RIGHT WING STR 14, 15, 17, AND 18 FROM XRS 65 TO 109. REPAIRED ALL PER EA 91-100821. 2L72 4F A6WE 19950811006641995081100664NM 1995 8 11 9511972287 119950724A5314 KEEL BEAM BOEING727 727251 138408HNM FS 950-970 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND CORROSION IN THE KEEL BEAM CHORDS STR 29L AND 29R, FLANGE COMMON TO THE FUSELAGE SKIN FS 950F TO 970. REPAIRED STRINGERS (P/N 65-56441-3, -4), PER EA 22-98940, 22-98941. 2L73 4F A3WE 19950811006651995081100665NM 1995 8 11 9511982287 119950726A5342 CHORD BOEING727 727251 138408HNM FS 1343-1360 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT VERTICAL STABILIZER TO BODY CHORD FOR THE NR 2 ENGINE BS 1343 AND 1360 RESPECTIVELY. REPAIRED CHORD (P/N 65-17555-1577), PER EA 22-98944. 2L73 4F A3WE 19950811006661995081100666NM 1995 8 11 9511992287 119950727A5320 STRAP BOEING727 727251 138408HNM FS 1090 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR INTERNAL BEAR STRAP BS 1090. REPAIRED STRAP (P/N 65-54593-2), PER EA 22-98942. 2L73 4F A3WE 19950811006671995081100667NM 1995 8 11 9512002287 119950727A5311 FRAME BOEING727 727251 138408HNM FS 930 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND TWO, .5 INCH CRACKS IN THE BS 930 FRAME ABOVE STR 14R AND 14L. REPAIRED FRAME (P/N 65-16336-6), PER EA 22-98927 AND EA 22-98926 RESPECTIVELY. 2L73 4F A3WE 19950811006681995081100668NM 1995 8 11 9512012287 119950727A5311 FRAME BOEING727 727251 138408HNM FS 1365 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01287US 21375 DURING PERIODIC CHECK, FOUND A .75 INCH CRACK IN THE BS 1365 WEB FRAME RIGHT SIDE. REPAIRED FRAME (P/N 65-17555-1576), PER EA 22-98947. 2L73 4F A3WE 19950811006691995081100669WP 1995 8 11 9512029868 119950802A5230 FITTING DOUG DC9 DC951 3022051WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING. 2L72 4F A6WE 19950811006701995081100670WP 1995 8 11 9512039969 119950802A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR NR 4 AND NR 5 BEAMS FORWARD END FITTINGS. REPLACED FITTINGS PER SRM 51-30-5 PG 1. 2L72 4F A6WE 19950811006711995081100671NM 1995 8 11 9512042280 119950803A5523 SKIN BOEING727 727251 138408HNM ELEVATOR TAB DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01280US 21159 DURING LINE CHECK, FOUND DELAMINATION IN THE RIGHT ELEVATOR TAB, OUTBOARD END. REPLACED TAB (P/N 65-72799-72K), PER MM 27-30-87. 2L73 4F A3WE 19950811006721995081100672NM 1995 8 11 9512052203 119950803A5755 SKIN BOEING727 727251 138408HNM NR 1 SPOILER DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01203US 22543 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE NR 1 SPOILER UPPER SKIN. REPLACED SPOILER (P/N 65-17347-81A). 2L73 4F A3WE 19950811006731995081100673WP 1995 8 11 9512069917 119950804A5720 SKIN DOUG DC9 DC932 3022066WP RT FIXED VANE DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01967N 47573 DURING H-CHECK, FOUND DELAMINATION IN THE RIGHT WING CENTER FIXED VANE. REPAIRED PER EA 99-97628. 2L72 4F A6WE 19950811006741995081100674WP 1995 8 11 9512079917 119950805A5320 JAMB DOUG DC9 DC932 3022066WP CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01967N 47573 DURING H-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB. REPAIRED JAMB PER EA 99-97626. 2L72 4F A6WE 19950811006751995081100675WP 1995 8 11 9512089917 119950805A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01967N 47573 DURING H-CHECK, FOUND CORROSION ON THE INNER SKIN JUST BELOW THE RIGHT FORWARD OVERWING EMERGENCY EXIT. REPAIRED SKIN PER EA 99-97624. 2L72 4F A6WE 19950811006761995081100676NM 1995 8 11 9512096718 119950805A323069B803586 DNLOCK ACT BOEING747 747251F 1384898NM RT MLG LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 GL01618US2078215376 21122 AFTER GEAR EXTENSION, THE RIGHT WING RED GEAR LIGHT ILLUMINATED. ALSO, THE RIGHT WING GEAR FAILED TO INDICATE DOWN AND LOCKED IN PRIMARY AND ALTERNATE POSITION. CREW FOLLOWED COCKPIT OPERATING MANUAL AND LANDED AIRCRAFT WITHOUT FURTHER INCIDENTS. MAINTENANCE REPLACED THE DOWNLOCK ACTUATOR AND PERFORMED SWING OPERATION. CHECK WAS NORMAL. CONTROL NUMBER 812096718 CHANGED TO 9512096718. 2L74 4F A20WE 19950811006771995081100677NM 1995 8 11 9512102295 119950806A7931 OIL PRESS SW BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01295US 21506 696501 THE NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED, THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE LOW OIL PRESSURE AND DIFFERENTIAL PRESSURE SWITCHES. THE MAIN OIL FILTER WAS INSPECTED FOR CONTAMINANTS, NONE FOUND. SYSTEM OPERATION CHECKED OK ON RUNUP. THE AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950811006781995081100678 1995 8 11 9512116633 419950806A34417883450041 INS BOEING747 747227B 1384888NM NR 1/2 MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CRCRUISE 1 GL01633US386111 22234 AFTER TAKEOFF ORD, THE NR 2 INS WARNING LIGHT ILLUMINATED WITHOUT ACTION/MALFUNCTION CODES. ALSO, THE NR 1 INS HAD CODE 3 MODE 26 WITH INTERMITTENT CREW FLIGHT/HSI WARNING FLAGS. INS TRANSFER WAS SUCCESSFUL, DUMPED 139,000 LBS OF FUEL AND DIVERTED TO MSP. REPLACED THE NR 1 AND NR 2 INS NAVIGATION UNIT AND TEST WAS NORMAL. 2L74 4F A20WE 19950811006791995081100679NM 1995 8 11 9512126717 119950723A5751 SKIN BOEING747 747251F 1384898NM RT AILERON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01617US 21121 DURING PERIODIC CHECK, FOUND CRACKING AND DELAMINATION IN THE RIGHT WING OUTBOARD AILERON INBOARD AFT CORNER. REPAIRED PER SRM 51-40-09, FIG 16 AND DWG 65B02154. 2L74 4F A20WE 19950811006801995081100680 1995 8 11 9512133220 419950723A2211 COMPUTER AIRBUS320 A320211 3930320EU NR 1 MALFUNCTIONED A NWAAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION DEDESCENT 1 GL01320US 213 WHILE PASSING THROUGH 20,000 FEET IN DESCENT INTO SEA, RECEIVED 'F/CTL ELAC 1 FAULT', ACCOMPANIED BY A 5 TO 10 DEGREE ROLL LEFT AND RIGHT. ATTEMPTED RESET, NO HELP. AIRCRAFT LANDED WITHOUT INCIDENT IN SEA. MAINTENANCE RESET ELEVATOR AILERON COMPUTER NR 1. OPERATIONAL CHECK OK. BOTH PITCH AND ROLL SIDE STICK TRANSDUCERS AND ELAC 1 WERE REPLACED. 2L72 4F RTA28NM 19950811006811995081100681NM 1995 8 11 95UAL900026 119950630A2750 VALVE 6523552 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE TE FLAPS MALFUNCTIONED A UALAK NONE JF WARNING INDICATION FLT CONT AFFECTED LDLANDING 1 WP297281U 21559 A/C EXPERIENCED ASYMMETRIC FLAP EXTENSION UPON LANDING. REPLACED INBD FLAP VALVE, LT FWD BEARING ON THE ELEPHANT EAR. FOUND PINION GEAR ON THE VALVE WORN. 2L73 4F4 F A3WE E2EA 19950811006821995081100682WP 1995 8 11 ABXA9500644 119950803A32607000010101 SWITCH DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23939AX 47201 DURING APPROACH TO ILN, DID NOT GET GREEN LIGHT FOR NOSE GEAR. RECYCLED TWICE AND RECEIVED GREEN LIGHT. MAINTENANCE DID NOT VERIFY. CLEANED AND RESEATED PLUG, REPLACED SWITCH AND BULBS AS A PRECAUTIONARY MEASURE IAW DC-9 MM 32-60-1. PERFORMED GEAR SWING IAW DC-9 32-30-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950811006831995081100683CE 1995 8 11 BIER950018 119950809A534704102352 SEAT TRACK CESSNA150 152 2071835CE RT OUTBD CORROSION B BIEAK NONE O OTHER ININSP/MAINT 1 EA21757ZR5132 15280138 DURING COMPLIANCE WITH AD87-20-03 R2, FOUND SEVERE CORROSION IN/ON COPILOT RT OB SEAT TRACK TO APPROX HALF THICKNESS OF TRACK. CORROSION WAS PROGRESSING INTO FLOOR PAN. 1H71 3O NT3A19 19950811006841995081100684NM 1995 8 11 DHLA9572005 119950804A7711JG298A5 EPR GAUGE BOEING727 727228 NM NR 1 MALFUNCTIONED A TDHLAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01720DH 19544 DURING TAKEOFF ROLL, LOST NR 1 EPR INDICATION, ALL OTHER PARAMETERS NORMAL. RECEIVED AUTO PACK TRIP, ABORTED TAKEOFF. RAN NR 1 ENGINE TO TAKEOFF POWER, ALL INDICATONS NORMAL. RESUMED SCHEDULED FLIGHT PLAN. 2L73 4F A3WE 19950811006851995081100685NM 1995 8 11 DL72E953336 119950718A5330 SKIN BOEING727 727247 138408FNM FS 660-680 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11283WA 21485 DUE TO GROUND DAMAGE, THE RIGHT SIDE OF THE FUSELAGE SUSTAINED DAMAGE. STRINGER 21R WAS SEVERED, THE SKIN DAMAGE WAS CUTOUT BETWEEN FS 660 TO FS 680 TO THE DIMENSIONS 22.5 FORE-AFT BY 20 UP AND DOWN. THE DAMAGED SECTION OF 21R HAS BEEN REMOVED FROM FS 650 TO FS 680. IN ACCORDANCE WITH B727 SRM 53-10-3 FIGURE 1, B727 SRM 53-10-4, FIGURE 11 AND FIG 12, AND B727 SRM 53-30-3, FIGURE 3A, THE DAMAGED AREAS WERE REPAIRED. 2L73 4F A3WE 19950811006861995081100686NM 1995 8 11 DL72L953314 119950807A2130 PRESS SW BOEING727 727232 1384082NM CABIN MALFUNCTIONED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11507DA 21309 CABIN ALT WARNING HORN WOULD NOT RESET WITH BUTTON. AUTO AND STBY PRESSURIZATION INOP. FWD CABIN ALT WARNING SYS TO MCO 21-00-14. 2L73 4F A3WE 19950811006871995081100687NM 1995 8 11 DL72L953334 119950727A5753 SHIM BOEING727 727232 1384082NM TE FLAP MIGRATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 DURING INSPECTION, A LAMINATED SHIM INSTALLED ON THE LEFT WING, INBD T/E FLAP, INBD TRACK WAS FOUND TO HAVE MIGRATED GREATER THAN THE 0.25 LIMIT SPECIFIED PER DAL SI 4-58662-12AD. IN COMPLIANCE WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED AND THE ATTACHMENTS WILL BE RETORQUED. 2L73 4F A3WE 19950811006881995081100688NM 1995 8 11 DL72L953338 119950730A533065182195 SKIN BOEING727 727232 1384082NM FS 379 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11502DA 21304 DURING INSPECTION, AN APPROXIMATE 4.25 BY 3.25 CUTOUT WAS MADE IN THE SKIN TO REMOVE DAMAGE FROM GOUGE. MAINTAINING SCHEDULE OF THE A/C, A TIME LIMITED REPAIR WILL BE INSTALLED AND THE PERM REPAIR WILL BE ACCOMPLISHED AT NEXT HMV IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 1. 2L73 4F A3WE 19950811006891995081100689NM 1995 8 11 DL72L953354 119950807A5330 SKIN BOEING727 727232 1384082NM FS 1010 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 DURING CV-2 INSPECTION, TWO CUTOUTS WERE MADE IN THE BELLY SKIN AFT OG THE SKIN SPLICE AT STA 1010. THE RT CUTOUT IS O/B OF STR 28R AND MEASURES 3.5 BY 4.5. THE LT CUTOUT EXTENDS FROM STR 30 TO SEVERAL INCHES O/B OF STR 29L AND MEASURES 4.75 BY 8 AND WILL REQUIRE DTA. IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 3A, THE CORROSION WAS CUTOUT FOR COMPLETE DAMAGE REMOVAL. REPAIRS ACCOMPLISHED IAW DL ERA 302267-14. 2L73 4F A3WE 19950811006901995081100690NM 1995 8 11 DL72L953355 119950721A5330 SKIN BOEING727 727232 1384082NM FS 700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11503DA 21305 DURING CV-2 INSPECTION, CORROSION WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 700 AND OUTBD OF STRINGER 28L. DAMAGE REMOVAL RESULTED IN A 2 BY 2 CUTOUT. DUE TO THE PROXIMITY TO AN EXISTING REPAIR, THE FACT THAT THE SKIN IS A SSI ITEM AND THE PROXIMITY TO THE INSPECTION AREA OF BACO S/B 727-53-A0203, THE DAMAGE REMOVAL WAS IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 1. ACCOMPLISHED REPAIRS PER DL ERA 302177-14. 2L73 4F A3WE 19950811006911995081100691NM 1995 8 11 DL72S952189 119950514A5311 FRAME BOEING727 727232 1384082NM FS 970 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 FRAME 970, CORROSION FWD SIDE BETWEEN STR 28R AND 27R. REPAIRED PER MM 53-11-0 PG 825. 2L73 4F A3WE 19950811006921995081100692NM 1995 8 11 DL72S953252 119950718A5311 FRAME BOEING727 727232 1384082NM FS 1352 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 THE NR 2 ENGINE STA 1352 FWD COWLING MATING SURFACE RING FLANGE IS BADLY WORN. REMOVED RING LOCATED, DRILLED NEW RING AND INSTALLED NEW RING PER MM 53-11-0, FOUND AT HMV. 2L73 4F A3WE 19950811006931995081100693NE 1995 8 11 DL72S953317 219950807A7230 COMPRESSOR BLADE BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FRACTURED A DALAE ENGINE SHUTDOWN XC ENGINE FLAMEOUT F.O.D. CRCRUISE 1 SO11541DA43204 22387 700344 DURING CRUISE, FL 370, NR 1 ENGINE STALLED AND FLAMED OUT. THERE WAS SOME SMOKE ODOR IN CABIN FOLLOWING FLAME-OUT. LANDED SLC. FOUND METAL IN TAILPIPE AND BLEED AIR MANIFOLD. ENGINE WAS REPLACED AND ROUTED TO SHOP. SUPPLEMENT: FRACTURED 7TH STAGE COMPRESSOR BLADE FOUND AT ENGINE SHOP DISASSEMBLY. VERY LIGHT FOD NOTED AT FRACTURE INITIATION SITE ON BLADE L/E. DAMAGE THROUGHOUT DOWNSTREAM STAGES OF THE HPC. 2L73 4F4 F A3WE E2EA 19950811006941995081100694NM 1995 8 11 DL72S953326 119950807A5754 LE RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 A .5 INCH CRACK ON SLAT NOSE RIB RADIUS JUST O/B OF ACTUATOR BOLT. FOUND AT F-1 LTR CK AND REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950811006951995081100695NM 1995 8 11 DL72S953327 119950807A5754 LE RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 DURING LETTER CK F1, NR 6 L/E SLAT NR 2 L/E RIB CRACKED AT AFT FLANGE. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19950811006961995081100696NM 1995 8 11 DL72S953328 119950807A5754 SKIN BOEING727 727232 1384082NM NR 6/7 SLATS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 NR 6 SLAT PANEL CRACKED BELOW ANTI-ICE DUCT. NR 7 SLAT PANEL CRACKED BELOW ANTI-ICE DUCT. FOUND DURING F-1 LTR CK AND REPAIRED PER MM 57-50-3. 2L73 4F A3WE 19950811006971995081100697NM 1995 8 11 DL72S953329 119950807A5522 SKIN BOEING727 727232 1384082NM LT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11546DA 22677 LT ELEVATOR SKIN CRACKED LOWER I/B END. FOUND AT F-1 LTR CK AND REPAIRED PER SRM 55-20-3. 2L73 4F A3WE 19950811006981995081100698NM 1995 8 11 DL72S953337 119950707A5330 SKIN BOEING727 727232 1384082NM FS 480-500 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING CV-2 INSPECTION, THE SKIN WAS FOUND DAMAGED IN TWO PLACES ALONG STA 480 TO 500. ONE WAS FOUND AT STR 28L AND THE OTHER NEAR STR 27L. THE DAMAGE WAS REMOVED TO LEAVE TWO CUTOUTS MEASURING 17 BY 2.5 AND 16.375 BY 1.125. AN EXISTING REPAIR IS LOCATED JUST AFT AND INBD OF THE NEW CUTOUTS. THE OLD CUTOUT IS 1.5 BY .875. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 3, THE PREVIOUS REPAIR WAS REMOVED AND A DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE NEW CUTOUTS. ALSO, STRS 27L AND 28L HAVE BEEN REPAIRED PER B727 SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950811006991995081100699NM 1995 8 11 DL733953335 119950721A53306545775594 SKIN BOEING737 737347 1384647NM FS 765 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO112310 23596 DURING HMV INSPECTION, THE SKIN WAS FOUND DENTED AT FS 765 JUST BELOW THE STRINGER 20R LAP SPLICE. IN ACCORDANCE WITH B737-300 SRM 53-00-01, FIG 202, THE DAMAGED SECTION WILL BE CUT OUT AND AN EXTERNAL REPAIR DOUBLER WILL BE INSTALLED. 2L72 4F RTA16WE 19950811007001995081100700NM 1995 8 11 DL73E952575 119950612A5210 SKIN BOEING737 737247 138448DNM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11376DL 23603 FOUND ON LTR CK, L1 DOOR LOWER HINGE CUTOUT LWR AFT CORNER .3125 INCH CRACK. REPAIRED PER SRM 52-00-3. 2L72 4F A16WE 19950811007011995081100701NM 1995 8 11 DL73E952576 119950612A5542 SKIN BOEING737 737247 138448DNM RUDDER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11376DL 23603 FOUND ON LTR CK, DAMAGE TO TRAIL EDGE RUDDER. REPAIRED PER SRM 55-40-5 FIG 1. 2L72 4F A16WE 19950811007021995081100702NM 1995 8 11 DL73S952203 119950519A5542 SKIN BOEING737 737232 1384475NM RUDDER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11329DL 23101 RUDDER DELAMINATED AT TOP LEFT SIDE T/E NEXT TO PREV REPAIR. ACCOMPLISHED REPAIRS PER SRM 51-40-9 FIG 1 AND ERA 301817-14. 2L72 4F RTA16WE 19950811007031995081100703NM 1995 8 11 DL73S952204 119950519A5755 SKIN BOEING737 737232 1384475NM NR 6 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11329DL 23101 NR 6 SPOILER UPPER SURFACE DELAMINATED. REPAIRED PER SRM 57-50-5 FIG 5. FOUND AT M1 LTR CK. 2L72 4F RTA16WE 19950811007041995081100704NM 1995 8 11 DL73S952205 119950519A5230 DOOR BOEING737 737232 1384475NM CARGO COMPT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11329DL 23101 FWD B/B DOOR PAN CRACKED AT FWD AND AFT CORNERS INSIDE RADIUS. REPAIRED PER DL ERA 301812-14. 2L72 4F RTA16WE 19950811007051995081100705NM 1995 8 11 DL757952083 119950512A5230 CORNER BOEING757 757232 1384965NM BAGG DOOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11616DL 22823 AFT REAR BAG BIN DOOR, FWD BOTTOM CORNER DAMAGED. REPAIRED PER SRM 52-30-01. FOUND AT LTR CHECK. 2L72 4F RTA2NM 19950811007061995081100706NM 1995 8 11 DL767952038 119950510A5751 SKIN BOEING767 767232 1385132NM LT AILERON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11106DA 22218 INBOARD END OF OUTBOARD AILERON HAS CONDENSATION ON LOWER SKIN SURFACE, DUE TO WATER INGESTION. ACCOMPLISHED REPAIRS PER SRM 57-60-02. FOUND AT LETTER CHECK. 2L72 4F RTA1NM 19950811007071995081100707NM 1995 8 11 DL76L952711 119950620A5753 SKIN BOEING767 767332 1382001NM RT TE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11179DN 25144 O/B FLAP LOWER SURFACE DELAMINATED JUST I/B OF O/B FLAP TRACK FAIRING. REPAIRED PER SRM 52-53-01. FOUND AT LETTER CHECK. 2L72 4F RTA1NM 19950811007081995081100708NM 1995 8 11 DL76L953319 119950807A2432 CHARGER 425404 BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE BATTERY COMPT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11180DN 0980 25985 700344 MAIN BATTERY CHARGER EICAS STATUS MESSAGE OCCURED AFTER T/O JFK - DIVERTED TO BOSTON. REPLACED MAIN BATTERY CHARGER AND INSPECTED BATTERY GRD CABLE FOR CORROSION, NONE FOUND. BATTERY CHARGER OPS CKS. NML PER M/M PERFORMED OVERWEIGHT LNDNG INSP AND OVERWATER 1 CK. 2L72 4F4 FRTA1NM E24NE 19950811007091995081100709NM 1995 8 11 DL76L953357 119950804A2120 AIR DIST BOEING767 767332 1382001NM FWD GALLEY SMOKE ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11184DN 27111 DURING CRUISE, THE ON/OFF LIGHT ON CHILLER IN FWD GALLEY WAS FLICKERING. SMOKE COMING OUT OF VENT ABOVE CIRCUIT BREAKERS. ALL NORMAL WHEN GALLEY POWER SHUTDOWN. OPERATION OF FWD CHILLER FOUND NORMAL. OPENED AND CHECKED C/B PANEL IN FWD GALLEY AND FOUND ALL OK, NO EVIDENCE OF SMOKE OR BURNED WIRES. RETURNED TO SERVICE. 2L72 4F RTA1NM 19950811007101995081100710NM 1995 8 11 DL76S953356 119950804A2120 AIR DISTR BOEING767 767332 1382001NM CABIN SMOKE ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11138DL 25409 AFTER T/O, F/A REPORTED LIGHT ODOR OF SMOKE THROUGHOUT CABIN. ALSO, HEAT EMITTING FROM AREA AROUND SEAT 1F, LOWER HALF OF SIDEWALL. CHECKED ALL LIGHT BALLASTS IN AREA, NO PROBLEM FOUND. RAN PACKS AND INSPECTED AREA AROUND SEAT 1F, NO PROBLEM NOTED. RETURNED TO SERVICE. 2L72 4F RTA1NM 19950811007111995081100711NM 1995 8 11 DL76S953358 119950805A2710251T141311 CABLE QUADRANT BOEING767 767332 1382001NM LT WING CRACKED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO11118DL 23277 ON TAXI OUT FOR TAKEOFF, WITH FLAPS AT 15 DEGREES, DURING FLT CONTROL CHECK THE AILERONS WERE BINDING, THEN STUCK FULL DEFLECTION RIGH WING DOWN. AC RETURNED TO BLOCK AND FOUND LEFT LATERAL CENTRAL CONTROL ACTUATOR WITH CABLE QUADRANT BROKEN. REPLACED QUADRANT, OPERATION CHECK NORMAL PER MM 27-11-18. 2L72 4F RTA1NM 19950811007121995081100712WP 1995 8 11 DLL10951655 119950416A3020 ANTI-ICE RING LKHEED1011 10113851 5265010WP NR 2 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 NR 2 ENGINE INLET ANTI-ICE RING DIMPLE SKIN IS CRACKED AT 1030 POSITION. REPAIRED PER SRM 54-34-00 FIG 804. 2L73 4F A23WE 19950811007131995081100713WP 1995 8 11 DLL10951678 119950420A5311 FORMER LKHEED1011 10113851 5265010WP BS 1103 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 FORMER CRACKED AT STA 1103 LT SIDE W/L 198, JUST UNDER FLOOR LEVEL. REPAIRED PER SRM 53-12-00 FIG 816. FOUND AT HMV. 2L73 4F A23WE 19950811007141995081100714WP 1995 8 11 DLL10951710 119950425A5320 TEAR STRAP LKHEED1011 10113851 5265010WP BS 1393 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 TEAR STRAP DISBONDED FS 1393 BETWEEN STRGR 34 TO 35. REPAIRED DURING ACCOMPLISHMENT OF LOWER SKIN REPLACEMENT FS 1363 TO FS 1453, BETWEEN STRINGERS 31 AND 36, PER DL ERA 270691-14. 2L73 4F A23WE 19950811007151995081100715WP 1995 8 11 DLL10951812 119950416A5510 STIFFENERS LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331G. REPAIRED PER SRM 55-12-00 FIG 803, FOUND AT HMV. 2L73 4F A23WE 19950811007161995081100716WP 1995 8 11 DLL10951931 119950506A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP BS 689 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 C-1 B/B FLOOR SUPPORT CORRODED AT LBL3 FS 689. REPAIRED PER SRM 53-23-04. FOUND AT HMV. 2L73 4F A23WE 19950811007171995081100717WP 1995 8 11 DLL10951992 119950412A5311 FRAME LKHEED1011 10113851 5265010WP BS 1792 GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 STA 1792 FRAME GOUGED ON RT SIDE APPROX AT STRINGERS 23 AND 24. INSTALLED DOUBLER PER SRM 53-12-0 FIG 804. 2L73 4F A23WE 19950811007181995081100718WP 1995 8 11 DLL10952009 119950416A5510 STIFFENERS LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 INTERNAL STIFFENERS CRACKED RT HORIZ LE PANEL 341F. REPAIRED PER SRM 55-12-00 FIG 803. FOUND AT HMV. 2L73 4F A23WE 19950811007191995081100719WP 1995 8 11 DLL10952010 119950416A5510 STIFFENERS LKHEED1011 10113851 5265010WP LT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11719DA 193C1135 INTERNAL STIFFENERS CRACKED LT HORIZ LE PANEL 331D. REPAIRED PER SRM 55-12-00 FIG 803. 2L73 4F A23WE 19950811007201995081100720WP 1995 8 11 DLL10952623 119950614A5311 FRAME LKHEED1011 10113851 5265010WP FS 629/649 DOUBLE DRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FUSELAGE FRAME FS 629 AT STR 32 AND FS 649 AT STR 32 FOUND WITH DOUBLE DRILLED HOLE. ACCOMPLISHED REPAIR PER SRM 53-31-00. 2L73 4F A23WE 19950811007211995081100721WP 1995 8 11 DLL10952663 119950614A5311 FRAME LKHEED1011 10113851 5265010WP FS 569/589 DOUBLE DRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 AT HMV, FUSELAGE FRAME FS 569 AT STR 36 AND FS 589 AT FS 33 FOUND WITH DOUBLE DRILLED HOLE. REPAIRED PER SRM 53-31-00 FIG 818. 2L73 4F A23WE 19950811007221995081100722WP 1995 8 11 DLL13953172 119950708A5743 FITTING LKHEED1011 10113851 5265010WP LT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, LEFT MLG RETRACT ACTUATOR FITTING ATTACH POINT ON AIRCRAFT STRUCTURE FOUND WITH CORROSION DAMAGE. REPAIRED PER SRM 57-14-00 STEPS 2 TO 6. 2L73 4F A23WE 19950811007231995081100723WP 1995 8 11 DLL13953203 119950708A5720 FITTING LKHEED1011 10113851 5265010WP RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AT HMV, RT MLG RETRACT ACTUATOR FITTING ATTACH POINT ON AIRCRAFT STRUCTURE FOUND WITH CORROSION DAMAGE. REPAIRED PER SRM 57-14-00 STEPS 2 TO 6. 2L73 4F A23WE 19950811007241995081100724WP 1995 8 11 DLL13953321 119950801A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 LT/RT WING RIB LOWER CAP AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPAIRED PER DL ERA 271518-14AD. FOUND AT HMV. 2L73 4F A23WE 19950811007251995081100725WP 1995 8 11 DLL13953341 119950703A5330 SKIN LKHEED1011 10113851 5265010WP FS 651 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 A 1.625 BY 1.375 BY 0.128 DENT WAS FOUND IN THE FUSELAGE SKIN AT FS 651, BETWEEN STGR 27R AND STGR 28R. ACCOMPLISHED REPAIRS PER DL ERA 271295-14. 2L73 4F A23WE 19950811007261995081100726WP 1995 8 11 DLL13953342 119950801A5712 RIB LKHEED1011 10113851 5265010WP WS 503 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE LT WING RIB UPPER CAP AT IWS 503 HAS SEVERAL CRACKS IN THE ATTACH TABS. DUE TO STRUCTURAL CONSTRAINTS IT IS DESIRABLE TO REPLACE THE UPPER CAP RATHER THAN REPAIR SUBJECT DAMAGED PART. REPAIRED PER DL ERA 271522-14AD. 2L73 4F A23WE 19950811007271995081100727WP 1995 8 11 DLL13953345 119950720A53301507533101 TRIPLER LKHEED1011 10113851 5265010WP GALLEY DR CUTOUTCORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE FUSELAGE LWR GALLEY DOOR TRIPLER SURROUND STRUCTURE WAS FOUND WITH SEVERE CORROSION LOCATED IN THE LWR AFT CORNER OF THE DOOR CUTOUT. FOUND AT HMV, AND REPAIRED IAW DL ERA 271379-14. 2L73 4F A23WE 19950811007281995081100728WP 1995 8 11 DLL13953347 119950714A53301503541217 SKIN LKHEED1011 10113851 5265010WP FS 1453-1753 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE AFT LOWER BELLY SKIN WAS FOUND TO BE CORRODED AT SEVERAL LOCATIONS BETWEEN FS 1453 AND FS 1753, BETWEEN STRINGERS 30 AND 36. THE FUSELAGE SKIN PANEL BETWEEN FS 1453 AND FS 1575 AND BETWEEN THE LAP JOINT AT STRINGER 24 AND STRINGER 31 IS HEAVILY CORRODED. A RUN-OUT TAB OF THE C-2 DOOR OUTER DOUBLER, AT FS 1535 BETWEEN STRINGERS 26 AND 27 WAS HEAVILY CORRODED. DUE TO THE EXTENSIVE LEVEL OF CORROSION, REPLACEMENT OF LARGE AREAS OF THE AFT SKIN IS REQUIRED. REPAIRS ACCOMPLISHED PER DL ERA 271342-14. 2L73 4F A23WE 19950811007291995081100729WP 1995 8 11 DLL13953348 119950726A53301608990 SKIN LKHEED1011 10113851 5265010WP FS 1655 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AN UNIDENTIFIED EXTERNAL SKIN REPAIR WAS REMOVED FROM FS 1655, BETWEEN STRINGERS 24 AND 25. THE REPAIR CONSISTED OF A CUTOUT APPROX 4.5 BY 4.25, A 0.032 2024-T3 DOUBLER, .070 TRIPLER AND .090 FILLER. INSTALLED PERMANENT REPAIR PER DL ERA 271459-14. FOUND AT HMV. 2L73 4F A23WE 19950811007301995081100730WP 1995 8 11 DLL13953349 119950721A53301503140155 SKIN LKHEED1011 10113851 5265010WP FS 539-983 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE FWD LWR BELLY SKIN WAS FOUND WITH EXTENSIVE CORROSION BETWEEN FS 529 AND FS 983 AND STRINGER 29 AND STRINGER 42. DUE TO THE EXTENSIVE NATURE OF THE CORROSION AND EXISTING REPAIRS, REPLACEMENT OF LARGE AREAS OF THE FWD BELLY SKIN WILL BE REQUIRED. ACCOMPLISHED REPAIRS PER DL ERA 271311-14. 2L73 4F A23WE 19950811007311995081100731WP 1995 8 11 DLL13953350 119950706A5330 SKIN LKHEED1011 10113851 5265010WP FS 349-409 CREASED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 DURING HMV INSPECTION, THE FUSELAGE SKIN AFT OF THE L1 DOOR AT WL 200 FROM FS 349 TO FS 409 WAS FOUND WITH A CREASE. THE MAXIMUM DEPTH OF THE CREASE IS .045, AND THERE IS NO DAMAGE TO THE UNDERLYING STRUCTURE. ACCOMPLISHED REPAIRS PER DL ERA 271317-14. 2L73 4F A23WE 19950811007321995081100732WP 1995 8 11 DLL13953351 119950721A53301503492147 SKIN LKHEED1011 10113851 5265010WP FS 328 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE FUSELAGE SKIN WAS FOUND SLIGHTLY BULGED AROUND THE LBL 22 FS 328 NLG W/W CORNER. UPON FURTHER INSPECTION, THERE WAS SLIGHT CORROSION FOUND ON THE INNER CUTOUT DOUBLER. THE CORROSION WAS REMOVED PER SRM PROCEDURES. AFTER REMOVAL OF THE EXISTING CORNER DOUBLERS A 1.5 INCH LONG CRACK WAS FOUND EXISTING IN BOTH THE OUTER FUSELAGE SKIN AND THE INNER CUTOUT DOUBLER. THE CRACK RUNS FWD FROM THE NLG W/W CUTOUT EDGE, THROUGH FASTENER AND ENDS IN A .3125 INCH DIA STOP DRILL. REPAIRED PER DL ERA 271415-14AD. FOUND AT HMV. 2L73 4F A23WE 19950811007331995081100733WP 1995 8 11 DLL13953352 119950706A53121646545 BULKHEAD LKHEED1011 10113851 5265010WP FS 328 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 AFTER ACCOMPLISHMENT OF THE PERMANENT REPAIR PER ER/A226723-14, LAC DWG 1646545 AND EO 7-53207-3AD WAS ISSUED TO ACCOMPLISH REINFORCEMENT OF THE FS 328 CANTED BULKHEAD STRUCTURE ON DELTA'S ENTIRE L1011 FLEET. AFTER INSPECTION OF THE EXISTING MODIFICATIONS INSTALLED ON THE FS 328 BULKHEAD DURING HMV ON 7/95, IT WAS FOUND THAT THE EXTERNAL MODIFICATION PARTS ON THE RT SIDE DEVIATED FROM THE EO MODIFICATION. REPAIR APPROVAL PER DL ERA 271315-14AD. 2L73 4F A23WE 19950811007341995081100734WP 1995 8 11 DLL17951738 119950404A57121527275 RIB LKHEED1011 10113853 5265020WP LANDING GEAR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11764DA 193H1202 DURING HMV, THE A HOLE IN THE MLG ATTACH RIB WAS OVERSIZED TO REMOVE CORROSION. ACCOMPLISHED REPAIRS PER DL ERA 270587-14. 2L73 4F A23WE 19950811007351995081100735 1995 8 11 DLM88953318 419950807A3442 RADAR 20414440403 DOUG MD88 MD88 3023688NM PWA JT8 JT8D15A 52051NE NOSE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11990DL 53342 700344 WEATHER RADAR SYSTEM HAD AN ANTENNA FAULT, ENROUTE TO ATL. FLT DIVERTED TO MGM DUE TO WEATHER. REPLACED R/T UNIT AND ANTENNA. 2L72 4F4 FRTA6WE E2EA 19950811007361995081100736WP 1995 8 11 MWEA 95249 119950717A5330 SKIN DOUG DC9 DC914 3022034WP BS 737 GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, FOUND GOUGE IN BELLY SKIN .040 DEEP JUST RIGHT OF LONGERON 30 STA 737. MAINTENANCE REPAIRED SKIN IAW SRM 53-05 FIG 38 VIEW H. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007371995081100737WP 1995 8 11 MWEA 95258 119950725A5320 ANGLE DOUG DC9 DC914 3022034WP BS 867 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, THE EXTERIOR ANGLE AT STA 867 FUSELAGE TO VERTICAL STABILIZER ATTACH POINT WAS FOUND CRACKED 1.5 IN LENGTH. MAINTENANCE FABRICATED NEW ANGLE AND INSTALLED IAW SRM 53-09 FIG 23. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007381995081100738WP 1995 8 11 MWEA 95259 119950808A3350 EEL DOUG DC9 DC914 3022034WP FWD GALLEY INOP A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31400ME 45727 DURING ROUTINE INSPECTION, THE EMERGENCY LIGHTING IN GALLEY WAS INOP. MAINTENANCE ADJUSTED LIGHT SOCKETS. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007391995081100739WP 1995 8 11 MWEA95248 119950711A53207075T6 ANGLE DOUG DC9 DC914 3022034WP BS 210 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, THE CUSP ANGLE AT STA 210 LONGERON 18R WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED ANGLE IAW SRM 53-05 FIG 55 AND DAC DRAWING 9910078. REPAIR ANGLE FABRICATED FROM 7075-T6. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007401995081100740WP 1995 8 11 MWEA95250 119950718A5313L27779224 LONGERON DOUG DC9 DC914 3022034WP BS 786L CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, LONGERON 17L WAS FOUND CRACKED AT STA 786. MAINTENANCE REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-02 FIG 2 PAGE 2A. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007411995081100741WP 1995 8 11 MWEA95251 119950718A5313L27779203 LONGERON DOUG DC9 DC914 3022034WP BS 786 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, LONGERON 13R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 53-02. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007421995081100742WP 1995 8 11 MWEA95252 119950718A5313L2777948 LONGERON DOUG DC9 DC914 3022034WP BS 766 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, LONGERON 14L WAS FOUND CRACKED AT STA 766. MAINTENANCE REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-02. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007431995081100743WP 1995 8 11 MWEA95253 119950718A5313L27779221 LONGERON DOUG DC9 DC914 3022034WP BS 786 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE MAINTENANCE, LONGERON 16R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 53-02. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007441995081100744WP 1995 8 11 MWEA95254 119950718A5313L27779224 LONGERON DOUG DC9 DC914 3022034WP BS 786 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, LONGERON 17R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED SECTION OF LONGERON IAW SRM 53-02. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007451995081100745WP 1995 8 11 MWEA95255 119950719A5330 SKIN DOUG DC9 DC914 3022034WP BS 756 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, THE SKIN WAS FOUND CRACKED APPROXIMATELY .75 IN LENGTH AT STA 756, LONGERON 7R. MAINTENANCE INSTALLED PLUG REPAIR IAW SRM 53-04 FIG 38 VIEW 1. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007461995081100746WP 1995 8 11 MWEA95256 119950720A5330 SKIN DOUG DC9 DC914 3022034WP BS 756 GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, THE SKIN WAS FOUND GOUGED AT STA 756 AND LONGERON 12L. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 53-04 FIG 38 VIEW G. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007471995081100747WP 1995 8 11 MWEA95257 119950721A531599115957 FLOORBEAM DOUG DC9 DC914 3022034WP STA 200 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 DURING ROUTINE INSPECTION, THE FLOORBEAM AT STA 200 WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE INSTALLED NEW SECTION OF EXTRUSION IAW SRM 53-01 FIG 2 AND 4. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950811007481995081100748NM 1995 8 11 P5CA9500666 119950703A5320 CLIPS BOEING747 747121 1384871NM BS 2060-2080 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORRODED FASTENERS AND CLIPS AT MAIN DECK WINDOWS BETWEEN BS 2060 AND 2080. REPLACED CLIPS AND FASTENERS PER BOEING MAINT MANUAL 56-21-01. 2L74 4F A20WE 19950811007491995081100749NE 1995 8 11 P5CA9500667 219950703A7240 TURBINE CASE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 662570 ENGINE NR 2 S-FLANGE AT 2 O'CLOCK IS CRACKED IN TWO PLACES ONE ON THE OD AND ONE FROM RAIL TO CASE OF TURBINE. REPAIRED PER 72-53-01 2L74 4F4 F A20WE E20EA 19950811007501995081100750NM 1995 8 11 P5CA9500668 119950703A7110 COWL FRAME BOEING747 747121 1384871NM NR 4 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACKED FRAME 3RD HOOK NR 4 ENGINE RIGHT MAIN COWL UPPER. REPAIRED PER BOEING SRM 54-30-03. 2L74 4F A20WE 19950811007511995081100751NM 1995 8 11 P5CA9500669 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION FUSELAGE SKIN EXTERNAL AND INTERIOR, BS 1000 BETWEEN S38L AND S40L. REPAIRED PER EO B747-53-84022-A40-010. 2L74 4F A20WE 19950811007521995081100752NM 1995 8 11 P5CA9500670 119950703A7110 COWLING BOEING747 747121 1384871NM NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FORWARD EDGE NR 3 ENGINE RIGHT COWLING EXTERIOR SURFACE SKIN. REPAIRED PER BOEING SRM 54-30-03. 2L74 4F A20WE 19950811007531995081100753NM 1995 8 11 P5CA9500671 119950703A5320 CHORD BOEING747 747121 1384871NM NLG WW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON CHORD RIGHT SIDE NOSE WHEEL CORNER. REPAIRED PER BOEING DRAWING 141U1098 (SB 53-2272). 2L74 4F A20WE 19950811007541995081100754NM 1995 8 11 P5CA9500672 119950703A4980 EXHAUST BELLOW BOEING747 747121 1384871NM APU CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 APU EXHAUST BELLOW BENT AND CRACKED. REPLACED BELLOW. 2L74 4F A20WE 19950811007551995081100755NM 1995 8 11 P5CA9500673 119950703A5755 SPOILER BOEING747 747121 1384871NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK AT SKIN NEAR PCU FITTING ON NR 7 SPOILER RIGHT WING. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950811007561995081100756NM 1995 8 11 P5CA9500674 119950703A5320 CHORD BOEING747 747121 1384871NM BS 1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON LOWER FLANGE OF THE LOWER CHORD LANDING GEAR BEAM, AT BS 1350 LEFT AND RIGHT. REWORKED PER BOEING SB 53-2310 WITHIN LIMITS. 2L74 4F A20WE 19950811007571995081100757NM 1995 8 11 P5CA9500675 119950703A5753 SKIN BOEING747 747121 1384871NM LT TE AFT FLAP SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT WING OUTBOARD FLAP UPPER SURFACE 2 POINTS OF SEPARATION. REPAIRED PER BOEING SRM 51-40-06. 2L74 4F A20WE 19950811007581995081100758NM 1995 8 11 P5CA9500676 119950703A5330 SKIN BOEING747 747121 1384871NM CARGO DR CUTOUT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON AFT BULK CARGO DOOR CUTOUT, AT INTERNAL LOWER FORWARD CORNER. REPAIRED PER BOEING SRM 51-40-10. 2L74 4F A20WE 19950811007591995081100759NM 1995 8 11 P5CA9500677 119950703A532065B0466750 FITTING BOEING747 747121 1384871NM BS 1820 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CRACK ON FITTING AT BS 1820 S40R. REPLACED FITTING, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811007601995081100760NM 1995 8 11 P5CA9500678 119950703A5330 SKIN BOEING747 747121 1384871NM CARGO DR CUTOUT CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SURFACE CORROSION ON HI-LOCK HEADS, ON EXTERNAL SKIN MAIN SIDE CARGO DOOR CUTOUT. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950811007611995081100761NM 1995 8 11 P5CA9500679 119950703A5720 BRACKET BOEING747 747121 1384871NM WS 1168 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 BROKEN BRACKET RIGHT WING LEADING EDGE CAVITY WS 1168. MANUFACTURED PART PER BOEING SRM 51-20-02, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950811007621995081100762NM 1995 8 11 P5CA9500680 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1800-1860 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING IN FUSELAGE SKIN RIGHT SIDE BETWEEN BS 1860 AND 1800 S47R. SWELLING AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950811007631995081100763NM 1995 8 11 P5CA9500681 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1940 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING AND PROTRUDING RIVETS IN FUSELAGE SKIN, AT BS 1940 BETWEEN S47L AND S51L. REWORKED AREA AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED PER 51-30-02. 2L74 4F A20WE 19950811007641995081100764NM 1995 8 11 P5CA9500682 119950703A5720 ANGLE BOEING747 747121 1384871NM WS 630 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 RIGHT WING LEADING EDGE CAVITY WS 630 RIB TO LEADING EDGE CONNECTION ANGLE IS CRACKED. REPLACED ANGLE MANUFACTURED PER BOEING SRM 51-20-02, INSTALLED 51-30-02. 2L74 4F A20WE 19950811007651995081100765NM 1995 8 11 P5CA9500683 119950703A5312 BULKHEAD BOEING747 747121 1384871NM BS 1000 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION UNDER BOLTS BS 1000 LEFT SIDE. SURFACE CORROSION REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS. 2L74 4F A20WE 19950811007661995081100766NM 1995 8 11 P5CA9500684 119950703A5320 ANGLE BOEING747 747121 1384871NM BS 1320-1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT ANGLE FOR FLOOR MAIN DECK WL 178 LEFT SIDE BETWEEN BS 1320 AND 1350. REPLACED SUPPORT ANGLE, INSTALLED PER BOEING SRM 51-30-02. 2L74 4F A20WE 19950811007671995081100767NM 1995 8 11 P5CA9500685 119950703A5320 ANGLE BOEING747 747121 1384871NM BS 1240-1260 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 CORROSION ON SUPPORT ANGLE FOR FLOOR, BETWEEN BS 1240 AND 1260 LBL 100. REPLACED ANGLE PER BOEING SRM. 2L74 4F A20WE 19950811007681995081100768NM 1995 8 11 P5CA9500686 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1940 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING ON EXTERNAL SKIN AT BS 1940 S47R. REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHIN LIMITS, INSTALLED FASTENERS PER 51-30-02. 2L74 4F A20WE 19950811007691995081100769NM 1995 8 11 P5CA9500687 119950703A5330 SKIN BOEING747 747121 1384871NM BS 1789-1800 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 SWELLING IN FUSELAGE SKIN BETWEEN BS 1780 AND 1800 AT S49R. AREA REWORKED AND TREATED PER BOEING SRM 51-10-02, WITHING LIMITS, INSTALLED FASTENERS PER 51-30-01. 2L74 4F A20WE 19950811007701995081100770NM 1995 8 11 P5CA9500688 119950803A532065B083566 SUPPORT PLATE BOEING747 747122 1384872NM BS 1350 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED SUPPORT PLATE BS 1350 RBL 72, RIGHT BODY GEAR BAY. REPLACED SUPPORT PLATE. 2L74 4F A20WE 19950811007711995081100771NM 1995 8 11 P5CA9500689 119950803A5330 SKIN BOEING747 747122 1384872NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DURING INSPECTION PER AD 94-12-09, 6 HOLES CRACKED S19R BS 526 TO BS 534, 5 HOLES CRACKED BS 546 TO BS 551, 5 HOLES CRACKED BS 625 TO BS 630. REPAIRED PER BOEING SB 747-53-2307. 2L74 4F A20WE 19950811007721995081100772NM 1995 8 11 P5CA9500690 119950803A5330 SKIN BOEING747 747122 1384872NM FUSELAGE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DURING INSPECTION PER AD 94-12-09, 7 HOLES CRACKED S19L BS 527.5 TO BS 535, 6 HOLES CRACKED BS 547 TO BS 553.5, 3 RIVET HOLES CRACKED BS 571 TO BS 573.5, 1 RIVET HOLE CRACKED BS 592, 3 RIVET HOLES CRACKED BS 668 TO 671. REPAIRED PER BOEING SB 747-53-2307. 2L74 4F A20WE 19950811007731995081100773NM 1995 8 11 P5CA9500691 119950803A532065B105053 FITTING BOEING747 747121 1384871NM BS 1480 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 LEFT BODY LANDING GEAR RETRACT ACTUATOR UPPER FITTING CRACKED, BS 1480 BULKHEAD. REPLACED FITTING. 2L74 4F A20WE 19950811007741995081100774NM 1995 8 11 P5CA9500692 119950809A5522 SKIN BOEING747 747121 1384871NM LT ELEVATOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 LEFT INBOARD ELEVATOR TRAILING EDGE CRACKED, UPPER AND LOWER SURFACE APPROXIMATLY 36 TO 40 INCHES FROM INBOARD END. REPAIRED PER BOEING SRM 51-40-14. 2L74 4F A20WE 19950811007751995081100775NM 1995 8 11 P5CA9500693 119950809A5313 STRINGER BOEING747 747121 1384871NM BS 1820-1850 MISDRILLED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 FOUND AT BS 1820 TO BS 1850, S34L UPPER SIDE OF HAT CHANNEL HAS 32 HOLES .5 INCH APART AND 11 HOLES UPPER SIDE OF HAT CHANNEL IN SPLICE AREA AT BS 1890. REPLACED STRINGER PER EA 5310-0-01. 2L74 4F A20WE 19950811007761995081100776NM 1995 8 11 P5CA9500694 119950809A5313 STRINGER BOEING747 747121 1384871NM BS 1740-1890 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 S34L FROM BS 1740 TO SPLICE ARE AT BS 1890 HAS LIGHT CORROSION ON LOWER UPPER SECTION OF HAT CHANNEL, NO PROTECTIVE COATING ON STRINGER. STRINGER REPLACED FOR OTHER DAMAGE. 2L74 4F A20WE 19950811007771995081100777NM 1995 8 11 P5CA9500695 119950809A5313 STRINGER BOEING747 747121 1384871NM BS 1852 ELONGATED HOLE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 S34L ELONGATED HOLE AT BS 1852. STRINGER REPLACED. 2L74 4F A20WE 19950811007781995081100778NM 1995 8 11 P5CA9500696 119950809A5313 STRINGER BOEING747 747121 1384871NM BS 1778 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 S34L CRACKED IN RADIUS, BS 1778 AT OLD SET MARK. REPLACED STRINGER. 2L74 4F A20WE 19950811007791995081100779NM 1995 8 11 P5CA9500697 119950809A5350 RADOME BOEING747 747121 1384871NM FWD FUS DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 RADOME HAS AREAS OF ERROSION AND APPROXIMATELY 2 BY 2 AREA OF DELAMINATION. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950811007801995081100780NM 1995 8 11 P5CA9500698 119950809A5400 FAIRING BOEING747 747121 1384871NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 NR 3 PYLON LOWER AFT FAIRING CRACKED ON RIGHT SIDE AND HAS LOOSE AND MISSING FASTENERS ON BOTH SIDES. REPAIRED PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950811007811995081100781NM 1995 8 11 P5CA9500699 119950809A5751 TE SKIN BOEING747 747121 1384871NM RT AILERON SEPARATING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 RIGHT OUTBOARD AILERON TRAILING EDGE SEPARATING INBOARD APROXIMATELY 6 TO 10 INCHES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950811007821995081100782NM 1995 8 11 P5CA9500700 119950809A5753 LE SKIN BOEING747 747121 1384871NM RT TE FOREFLAP GOUGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 RIGHT OUTBOARD FLAP, FOREFLAP OUTBOARD END LEADING EDGE IS GOUGED IN 3 PLACES. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950811007831995081100783EU 1995 8 11 QXEA9500242 119950808A25305001021005 COFFEE JUG LATCH FOKKERF28 F28MK1000 4990808EU GALLEY LOOSE A QXEAA UNSCHED LANDING O OTHER CLCLIMB 1 NM09466US 11075 PDX - LATCH ON COFFEE JUG FALLS DOWN ON ROTATION. COFFEE JUG FELL OUT AND STRUCK PASSENGER. SAFETY CATCH WAS REPLACED AND A ADDITIONAL CATCH WAS INSTALLED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950811007841995081100784EU 1995 8 11 QXEA9500243 119950808A3350 EEL WIRE FOKKER FOKKERF28 F28MK1000 4990808EU CABIN DISCONNECTED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 BOI - EMERGENCY EXIT LIGHT ON SEAT 8B INOP. POWER WIRE WAS RECONNECTED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950811007851995081100785EU 1995 8 11 QXEA9500244 119950808A3350MGG1280 EEL BULBS FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 GEG - EXIT LIGHT INOP AT ROW 8 A/B. BULBS WERE REPLACED ON FORWARD SIDE AND REPLACED CIRCUIT BOARD ON AFT SIDE OF EXIT SIGN. LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950811007861995081100786NM 1995 8 11 SWAA950555 119950730A5312 BLKHD SKIN BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0782SW 22731 DURING SCHEDULED C1 CHECK, FOUND 1 CRACK AT BS 178, BULKHEAD BETWEEN WL 218 AND S2L. REPAIRED PER SWA RA 1-253-1320. 2L72 4F A16WE 19950811007871995081100787NM 1995 8 11 SWAA950556 119950730A3260 PROX SENSOR BOEING737 7372H4 138448CNM RT MLG INOP A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0785SW 22826 AFTER GEAR RETRACTION, RIGHT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND LIGHT EXTINGUISHED, THEN ILLUMINATED AGAIN. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED GEAR PROXIMITY SENSOR, RIGHT GEAR UPLOCK SWITCH AND SEALS AT PRIORITY VALVE PER BOEING M/M. 2L72 4F A16WE 19950811007881995081100788NM 1995 8 11 SWAA950557 119950729A33506113211 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND CABIN FLOOR TRACK LIGHTING INOP. REPLACED AFT BATTERY PACK AND REWIRED TRACK LIGHTING PER BOEING M/M. 2L72 4F A16WE 19950811007891995081100789NM 1995 8 11 SWAA950558 119950804A5330 SKIN BOEING737 7373H4 1384600NM BS 727D CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07321SW 23342 DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKS AT LEFT FUSELAGE JUST FWD AND BELOW EMERGENCY OVERWING EXIT LIGHT UNDER T/E FLAPS AT BS 727D, AT S23LT AND RT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950811007901995081100790NM 1995 8 11 SWAA950559 119950804A5240 SKIN BOEING737 7373A4 1384585NM FWD SERV DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07679AA 23291 DURING SCHEDULED C-CHECK, FOUND FWD SERVICE DOOR HINGE CUTOUT CRACKED, LOWER AREA. REPAIRED PER SWA RA 1-352-224. 2L72 4F RTA16WE 19950811007911995081100791NM 1995 8 11 SWAA950560 119950804A2782654465109 ACTUATOR BOEING737 7372T4 1384492NM NR 2 LE SLAT FAILED A SWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SW07130SW 22699 AFTER TAKEOFF, NUMBER 2 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 L/E SLAT ACTUATOR PER BOEING M/M. 2L72 4F A16WE 19950811007921995081100792NE 1995 8 11 SWAA950561 219950805A723065737694 COMPRESSOR BOEING737 7372H4 138448CNM PWA JT8 JT8D9 52048NE NR 2 ENGINE STALLED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0750SW 21447 687796 DURING CLIMBOUT, EXPERIENCED NUMBER 2 ENGINE COMPRESSOR STALL. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED NUMBER 2 ENGINE PER BOEING M/M. 2L72 4F4 F A16WE E2EA 19950811007931995081100793NE 1995 8 11 SWAA950562 219950806A7230 FAN BLADES BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE NR 2 ENGINE DAMAGED A SWAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW07515SW 25154 DURING CLIMBOUT, EXPERIENCED BIRD STRIKE TO NUMBER 2 ENGINE. AIRCRAFT RETURNED TO HRL AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND 6 FAN BLADE TIPS BENT. REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F4 FRTA16WE E2GL 19950811007941995081100794NM 1995 8 11 SWAA950563 119950801A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0782SW 22731 DURING SCHEDULED C2 CHECK, FOUND WEB CRACKED AT FASTENER HOLE IN UPPER RIGHT CORNER OF BS 178 BULKHEAD. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950811007951995081100795NM 1995 8 11 SWAA950564 119950729A5330 SKIN BOEING737 7372T4 1384492NM BS 530/534 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 534 AND 530, AT S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950811007961995081100796NM 1995 8 11 SWAA950565 119950729A5330 SKIN BOEING737 7373A4 1384585NM FWD FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07680AA 23505 DURING SCHEDULED C-CHECK, FOUND FUSELAGE SKIN DOUBLER CRACKED JUST BEHIND RADOME AT 12 O'CLOCK POSITION. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950811007971995081100797NM 1995 8 11 SWAA950566 119950731A33501000079 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0761SW 21970 DURING SCHEDULED A1 CHECK, FOUND RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950811007981995081100798NM 1995 8 11 SWAA950567 119950803A33506104781 EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0787SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS AT FWD ENTRY AND FWD SERVICE DOORS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950811007991995081100799NM 1995 8 11 SWAA950568 119950730A335020131A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRYWAY EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY CHARGER AND BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950811008001995081100800NM 1995 8 11 SWAA950569 119950731A3350 EEL BOEING737 7373H4 1384600NM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07366SW 26577 DURING SCHEDULED B/C1 CHECK, FOUND FOUR CABIN TRACK LIGHTS INOP. REPLACED LIGHTS PER BOEING M/M. 2L72 4F RTA16WE 19950811008011995081100801NM 1995 8 11 SWAA950570 119950803A3350 EEL BOEING737 7375H4 138449DNM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07508SW 24185 DURING SCHEDULED SERVICE CHECK, FOUND ONE CABIN TRACK LIGHT INOP. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2L72 4F RTA16WE 19950811008021995081100802NM 1995 8 11 UPS204042 119950808A532065175861 INTERCOSTAL BOEING727 72727C 138400JNM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 277 TO 294, WL 208 LBL 11. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW SRM 51-30-2 AND 53-10-1. 2L73 4F A3WE 19950811008031995081100803NM 1995 8 11 UPS204043 119950808A5320651759369 INTERCOSTAL BOEING727 72727C 138400JNM BS 295-303 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL BS 295 TO 303 LBL 11 WL 208. REPLACED NEW PART IAW 51-30-5, 51-30-8. 2L73 4F A3WE 19950811008041995081100804NM 1995 8 11 UPS204044 119950808A5313BAC1498142 STRINGER BOEING727 72727C 138400JNM BS 308 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STR 21 FLANGE AT BS 308 LBL 54 WL 220. REPAIRED IAW SRM 53-10-1, 53-10-3. 2L73 4F A3WE 19950811008051995081100805NM 1995 8 11 UPS204045 119950808A53137075T6 STRINGER BOEING727 72727C 138400JNM BS 415 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STR 25 TOP OF FLANGE, BS 415 RBL 30 WL 155. REPLACED STRINGER PER SRM 53-10-3. 2L73 4F A3WE 19950811008061995081100806NM 1995 8 11 UPS204047 119950808A53207075T6 STRAP BOEING727 72727C 138400JNM BS 380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON 380 FRAME STRAP AT BS 380 LBL 12 RBL 12 WL 148. FABRICATED NEW REPAIR ANGLE AND INSTALLED WITH FASTENERS IAW SRM 51-40-3, 51-10-6 AND 53-10-1. 2L73 4F A3WE 19950811008071995081100807NM 1995 8 11 UPS204048 119950808A53207075T6 ANGLE BOEING727 72727C 138400JNM BS 441 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND REPAIR ANGLE TO BE CORRODED AND GOUGED AT BS 441 STR 26R. FABRICATED NEW REPAIR ANGLES AND INSTALLED WITH FASTENERS IAW SRM 51-30-2 AND 51-20-1. 2L73 4F A3WE 19950811008081995081100808NM 1995 8 11 UPS204049 119950808A5313BAC1498113 STRINGER BOEING727 72727C 138400JNM BS 360-380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 1 BETWEEN STA 360 AND 380. FABRICATED STRINGER AND SPLICE PARTS IAW SRM 53-10-3. ALL OTHER WORK DONE IAW SRM 53-10-1, 51-30-2, 51-10-02, 51-10-6 AND MM 51-20-151. 2L73 4F A3WE 19950811008091995081100809NM 1995 8 11 UPS204050 119950808A5522652563931 SKIN BOEING727 72727C 138400JNM LT ELEV CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LEFT ELEVATOR I/B STATIC WICK BASE. REPLACED SKIN IAW 51-30-2, 55-20-1 AND 55-20-3. 2L73 4F A3WE 19950811008101995081100810NM 1995 8 11 UPS204051 119950808A575369207734 RIB BOEING727 72727C 138400JNM RT TE MIDFLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SUPPORT RIB ON THE R/W I/B MIDFLAP IN THE TRAILING EDGE COVE 53 INCHES FROM THE O/B END. INSTALLED NEW RIB IAW SRM 51-101 AND 51-30-2. 2L73 4F A3WE 19950811008111995081100811NM 1995 8 11 UPS204052 119950808A5320 BEAM BOEING727 72727C 138400JNM BS 760-860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM STA 760 TO 860 RBL 25 WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646. 2L73 4F A3WE 19950811008121995081100812NM 1995 8 11 UPS204053 119950808A5320 BEAM BOEING727 72727C 138400JNM BS 760-860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM STA 760 TO 860, BLO WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646. 2L73 4F A3WE 19950811008131995081100813NM 1995 8 11 UPS204054 119950808A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 760-860 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BEAM STA 760 TO 860 LBL 45 WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646. 2L73 4F A3WE 19950811008141995081100814NM 1995 8 11 UPS204055 119950808A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 720 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 720, RBL 45, 50, RBL 22, 35, WL 208. FABRICATED FLOORBEAM T-CHORD IAW SRM 53-10-8, 51-30-2, 51-10-02 AND MM 51-20-151. 2L73 4F A3WE 19950811008151995081100815NM 1995 8 11 UPS204056 119950808A5347BAC15201430 SEAT TRACK BOEING727 72727C 138400JNM BS 344-360 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AROUND NUTPLATE HOLES BS 344 TO 360 LBL 55 WL 208. REPAIRED IAW SRM 53-10-01, SRM 51-30-2. 2L73 4F A3WE 19950811008161995081100816NM 1995 8 11 UPS204057 119950808A5347BAC15201434 SEAT TRACK BOEING727 72727C 138400JNM BS 640-660 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK AT BS 640 TO 660 RBL 45 WL 208. REPAIRED IAW SRM 53-10-5, 53-10-1, 51-10-6. 2L73 4F A3WE 19950811008171995081100817NM 1995 8 11 UPS204058 119950808A5313BAC1493531 STRINGER BOEING727 72727C 138400JNM BS 400 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND STRINGER TO FRAME ATTACHMENT POINT CRACKED ON STRINGER NR 9 LT, BS 400. FABRICATED NEW PARTS AND INSTALLED PARTS WITH FASTENERS IAW SRM 51-30-2, 53-10-3. 2L73 4F A3WE 19950811008181995081100818NM 1995 8 11 UPS204059 119950808A552169144011 RIB BOEING727 72727C 138400JNM LT ELEVATOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND ELEVATOR NOSE RIB AT STA 208.16 TO BE CORRODED ON LT ELEVATOR. REPLACED NOSE RIB IAW SRM 51-30-2. 2L73 4F A3WE 19950811008191995081100819WP 1995 8 11 95ZZZX3954 119950618A5270 WARNING LIGHT DOUG DC9 DC932 3022066WP AIRSTAIR DOOR ILLUMINATED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11530MD 47260 BDL/ATL - FLT 449 - AIRCRAFT RETURNED TO BDL DUE TO AFT AIRSTAIRS LIGHT CAME ON THE ANNUNCIATOR PANEL. 2L72 4F A6WE 19950811008201995081100820 1995 8 11 95ZZZX3955 419950627A344220852680104 CONNECTOR DOUG DC9 DC932 3022066WP RADAR IND LOOSE A VJ6AA UNSCHED LANDING O OTHER CRCRUISE 1 SO11936VV 47397 RDU - FLT 298 - EN ROUTE, EXPERIENCED SPOTS ON THE RADAR INDICATOR. AIRCRAFT RETURNED TO ATL DUE TO BAD WEATHER, RADAR REQUIRED FOR FLIGHT THROUGH KNOWN WEATHER. FOUND CANNON PLUG ON THE BACK OF THE ANTENNA EXTREMELY LOOSE, RECONNECTED AND REPLACED RADAR INDICATOR AS PRECAUTIONARY. 2L72 4F A6WE 19950811008211995081100821WP 1995 8 11 95ZZZX3956 119950706A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11937VV 45774 ATL/MIA - FLT 591 - RETURNED TO ATL BECAUSE THE A/C WOULD NOT PRESSURIZE. RESECURED THE E AND E DOOR. 2L72 4F A6WE 19950811008221995081100822NE 1995 8 11 95ZZZX3957 219950624A7261MS9388331 OIL CAP PACKING BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE FAILED A RIVAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17307AS 22000 AIRCRAFT DIVERTED TO FLL DUE TO INDICATED LOSS OF OIL IN NR 3 ENGINE. OIL QUANTITY INDICATOR STABILIZED AT 1.5 GA., TEMP AND PRESS OK (NO ENGINE SHUT-DOWN). FOUND PACKING BLOWN OUT AT SERVICE CAP AND REPLACED. LEAK CK OK. 2L73 4F4 F A3WE E2EA 19950811008231995081100823NE 1995 8 11 95ZZZX3958 219950625A753069565082 DUCT SHIMS BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A RIVAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO178866E 20628 ON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON, THROTTLE BACK LIGHT WENT OUT. RETURNED TO MIA, FOUND AIR LEAK IN AREA OF 13TH STAGE SUPPLY DUCT MOUNT FLANGE. REPLACED SHIMS IN DUCT FLANGE. ENGINE RUN-UP TO TAKEOFF POWER AND LEAK CK FOUND OK. 2L73 4F4 F A3WE E2EA 19950811008241995081100824CE 1995 8 11 95ZZZX3959 119950428A2120 AIR DISTR BEECH 1900 1900C 1154161CE CABIN ODOR A MASAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW01140YV UC140 PIT - AFTER TAKEOFF, CREW NOTICED AN ODOR AND HAZE IN THE CABIN AND COCKPIT. AFTER SHUTTING OFF BLEEDS, ODOR SUBSIDED. AIRCRAFT RETURNED TO GATE IN PIT. MAINTENANCE INSPECTED ENVIRONMENTAL SYSTEM AND RAN A.C. WITH BLEEDS ON AND PRESSURIZED. NO DEFECTS NOTED. RETURNED TO SERVICE. 2L72 4T RTA24CE 19950811008251995081100825EA 1995 8 11 95ZZZX3960 219950709A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RIGHT FAILED A XZWAAE UNSCHED LANDING ENGINE SHUTDOWN BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 WP07259AF119723054 UB55 PCE32108 AT FL 21,000, SMOKE BEGAN TO FILL THE CABIN. SELECTED RIGHT BLEED-OFF TO CLEAR SMOKE. OBSERVED OIL PRESSURE NR 2 ENGINE DROPPING TO 85 PSI. REDUCED ENGINE POWER TO 1,000 POUNDS TORQUE. OIL PRESSURE CONTINUED TO DROP AND ENGINE WAS SHUT DOWN WHEN OIL PRESSURE REACHED 60 PSI. SINGLE ENGINE LANDING ACCOMPLISHED AT PSP. MAINTENANCE INVESTIGATION REVEALED LARGE QUANTITY OF OIL IN COMPRESSOR SECTION, OIL QUANTITY MORE THAN 5 QUARTS LOW. ENGINE TO BE REMOVED FOR REPAIR. 2L72 4T4 TRTA24CE E4EA 19950811008261995081100826EU 1995 8 11 95ZZZX3961 119950606A261251271107 FIRE LOOP FOKKERF27 F27MK500 4990629EU LT ENGINE CONTAMINATED A MTNAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 SO05724FE 10677 AFTER TAKEOFF, LEFT ENGINE FIRE WARNING LIGHT CAME ON. THE FIRE BOTTLES WERE SHOT AND THE ENGINE SHUT DOWN. AFTER LANDING WHILE TAXIING BACK TO THE RAMP, THE LIGHT WENT OUT. AFTER AN INSPECTION, THE MECHANIC FOUND NO EVIDENCE OF A FIRE. AFTER TROUBLESHOOTING, THE MECHANIC FOUND MOISTURE IN THE DETECTION WIRE. THERE HAD BEEN A GREAT DEAL OF RAIN IN THE AREA PRIOR TO THE FLIGHT. 2H72 4T A817 19950811008271995081100827NE 1995 8 11 95ZZZX3962 219950624A7261A53209111 O-RING BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE CUT A GLBAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0196UX 3261 UE96 ISN - AFTER TAKEOFF, CREW OBSERVED AN OIL PRESSURE FLUCTUATION ON THE RIGHT ENGINE. THE ENGINE WAS SHUT DOWN FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN OIL LEAK CAUSED BY A CUT O-RING. SERVICED ENGINE WITH 4 QUARTS OIL AND LEAK CHECKED OK. 2L72 4T4 TRTA24CE E26NE 19950811008281995081100828WP 1995 8 11 95ZZZX3963 219950607A7200 ENGINE LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LEFT MALFUNCTIONED A AOQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA1153GH 7293 3521 304 P74814 ISP - AFTER TAKEOFF, CABIN AND COCKPIT FILLED WITH SMOKE (ENGINE OIL FUMES). EMERGENCY ACTIONS WERE TAKEN AND AIRCRAFT RETURNED TO ISP WITHOUT INCIDENT. BORESCOPE INSPECTION OF ENGINE COMPRESSOR SECTION REVEALED OIL PRESENT IN THE NR 4 AND NR 5 BEARING CARBON SEAL CAVITY. ENGINE TEAR DOWN WILL BE REQUIRED. FINAL REPORT TO FOLLOW. LANDINGS, 6,624. 2L72 4F4 F A10CE E6WE 19950811008291995081100829NE 1995 8 11 95ZZZX3964 319950623A61117900961 LE SHEATH HAMSTD SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE NR 3 BLADE SEPARATED A NVEAEA ENGINE SHUTDOWN UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO03244AE9104 4907 340B244 864238 JAN - FLT 4596 - RIGHT ENGINE TO FLUX 7 PERCENT DURING CLIMB FOLLOWED BY MINOR VIBS. CREW SELECTED TORQUE-MOTOR-LOCKOUT, BUT DID NOT CURE PROBLEM. CREW SHUT DOWN RIGHT ENGINE AND SAFELY RETURNED TO JACKSON. INSPECTION REVEALED THE RIGHT NR 3 PROPELLER BLADE WAS MISSING A 14 INCH SECTION OF LEADING EDGE SHEATH. SHORT PIECE FOUND IN RIGHT ICE SHIELD. REPLACED RIGHT NR 3 BLADE. FERRIED TO BNA FOR ICE SHIELD REPAIR. 2L72 4T RTA52EU 6 CP11NE 19950811008301995081100830 1995 8 11 95ZZZX3965 419950621A23709806019001 CVR DHAV DHC6 DHC6300 EA AFT FUSELAGE INOPERATIVE A KPVAK NONE O OTHER ININSP/MAINT 1 WP13712PV 610 696 COCKPIT VOICE RECORDER WILL NOT TEST. 1H72 3T A9EA 19950811008311995081100831 1995 8 11 95ZZZX3966 419950621A23709806019001 CVR DHAV DHC6 DHC6300 EA AFT FUSELAGE INOPERATIVE A KPVAK NONE O OTHER ININSP/MAINT 1 WP13703PV 1476 434 COCKPIT VOICE RECORDER WILL NOT TEST. 1H72 3T A9EA 19950811008321995081100832WP 1995 8 11 95ZZZX3967 119950505A7921 OIL COOLER INLET SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE LEAKING A BSAAO OTHER J WARNING INDICATION APAPPROACH 1 NM05115BS 6417 TC324 P54125 OIL PRESSURE DROPPED ON FINAL APROACH ON LEFT ENGINE. ENGINE WAS SHUT DOWN AFTER LANDING. OIL LEAK IN OIL COOLER INLET RING. PILOT NOTICED OIL PRESSURE STARTING TO DROP ON FINAL APPROACH. PRESSURE DROPPED TO 5 PSI AFTER LANDING ENGINE WAS SHUT DOWN. LEFT ENGINE WAS REMOVED AND REPLACED. 1L72 4T4 T A8SW E4WE 19950811008331995081100833CE 1995 8 11 95ZZZX3968 119950611A323399388001 ACTUATOR BEECH 99 99 1154002CE RT MLG LEAKING A FFSAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AL0159CA 0431 U87 LOSS OF HYDRAULUIC FLUID THROUGH THE LEAKING PACKING IN THE RIGHT MAIN GEAR ACTUATOR RESULTED IN AN UNCOMMANDED LANDING GEAR EXTENSION DURING CRUISE. USE OF THE MANUAL EXTENSION PUMP WAS REQUIRED TO GET 3 GREEN GEAR DOWN LIGHTS PRIOR TO LANDING. 1L72 3T A14CE 19950811008341995081100834NE 1995 8 11 95ZZZX3969 319950616A6111 PROP BLADE 7825016 SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE LT ENGINE SEPARATED A NVEABE EMER. DESCENT ENGINE SHUTDOWN ED VIBRATION/BUFFET INFLIGHT SEPARATION CRCRUISE 1 SO03250AE8359 3111 1093 340B250 869064 MIA - FLT 5725 - CREW REPORTS LEFT ENGINE VIBRATION IN-FLIGHT, SHUT ENGINE DOWN IN-FLIGHT. FOUND BLADE SHEATH SEPARATED FROM LEFT PROPELLER BLADE. REPLACED PROPELLER BLADE. 2L72 4T RTA52EU 6 CP11NE 19950811008351995081100835 1995 8 11 95ZZZX3970 419950624A3418693733921 STALL WARN MOD BOEING737 7372T4 1384492NM STALL WARN SYST MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 ITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPED SHAKER. EMERGENCY DECLARED. RETURNED TO ITO. LANDING NORMAL. REPLACED STALL WARN MOD AND AOA SENSOR, FUNCTIONAL CHECK IAW MM 27-32-0 OK. WINDSHEAR BITE CHECK OK. AIRCRAFT RETURNED TO SERVICE. REFERENCE CONTROL NR TSAA9534126. 2L72 4F A16WE 19950811008361995081100836WP 1995 8 11 95ZZZX3971 119950614A532057727864 JAMB DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15795FT 46103 MAIN CARGO DOOR LOWER AFT DOOR, THRESHOLD HAS A CRACK. REPAIRED CRACKED CORNER FILLET AT MAIN CARGO DOOR JAMB, AFT LOWER CORNER IAW TIMCO REO DC08-53-1567. 2L74 4F RT4A25 19950811008371995081100837WP 1995 8 11 95ZZZX3972 119950614A532057727864 JAMB DOUG DC8 DC863F 302198FWP CARGO DOOR CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15959R 46143 MAIN CARGO DOOR LOWER AFT DOOR, THRESHOLD HAS A CRACK. REPAIRED CRACKED CORNER FILLET AT MAIN CARGO DOOR JAMB, AFT LOWER CORNER IAW TIMCO REO DC08-53-1565. 2L74 4F 4A25 19950811008381995081100838EA 1995 8 11 95ZZZX3973 119950717A5512C6TP10017 SKIN DHAV DHC6 DHC6300 EA RT HORIZ STAB CRACKED AS SCIAK NONE O OTHER ININSP/MAINT 1 WP19238SA29886 389 UPON STRIPPING OF PAINT ON THE HORIZONTAL STABILIZER, A SERIES OF SMALL CRACKS WAS DETECTED ON THE UPPER SKIN RIGHT SIDE OF THE HORIZONTAL STABILIZER. THERE WERE 5 CRACKS RANGING IN SIZE FROM .5 INCH TO 5.5 INCHES LOCATED BETWEEN STA 91.25 AND STA 113.25. THE SKIN WAS FOUND TO HAVE BEEN PULLED AWAY FROM THE INTERNAL RIB. THE STABILIZER WAS REMOVED FROM THE AIRCRAFT AND A SERVICEABLE UNIT INSTALLED. 1H72 3T A9EA 19950811008391995081100839NM 1995 8 11 95ZZZX3974 119950618A57116545320 SPAR CHORD BOEING737 737214 138446RNM WS 120.5-140.5 CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15460AT49618 20158 MCO - ON 6-18-95 APPROXIMATELY 21:00 LOCAL, INSPECTION FOUND A CRACK AT THE LEFT WING FRONT SPAR UPPER CHORD BETWEEN FRONT SPAR STATION (FSS) 120.5 AND (FSS) 140.5 (20 INCHES IN LENGTH) ON AIRCRAFT. T.A.T. 49617.5. T.A.C. 60930. THE CRACK WAS FOUND DURING THE REPETITIVE INSPECTION REQUIRED BY AD 88-11-04, AND PERFORMED IAW SB 737-57A1081, REV 10, DATED JULY 16, 1987. BOEING ENGINEERING WAS CONTACTED FOR FURTHER ACTION. 2L72 4F A16WE 19950811008411995081100841WP 1995 8 11 95ZZZX3976 119950720A2913AS66411LS666 HYD PUMP DOUG DC9 DC932 3022066WP LT ENGINE FAILED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11912VV 47359 FLT 574 - AFTER TAKEOFF, LEFT HYDRAULIC TEMP HIGH LIGHT CAME ON. AIRCRAFT RETURNED TO ATLANTA. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. P/N AS66411LS, S/N OFF 165614, S/N ON 179506. OPS CHECK GOOD, NO LEAKS FOUND IAW MM CHAPTER 29-10-5. 2L72 4F A6WE 19950811008441995081100844EU 1995 8 11 AALA950741 119950425A5313 STRINGER FOKKERF28 F28MK0100 4990807EU FS 25016-25516 DISBONDED A AALAK NONE O OTHER ININSP/MAINT 1 SW071462C 2821 11482 TULE - THE FOLLOWING STRINGERS IN ZONE 310 DISBONDED, STA 25016 - STA 25516. LEFT STRINGERS (21 EACH) NR 7 THROUGH NRS 17, 19, 20, 21A, AND NR 23 THROUGH NR 30. RIGHT STRINGERS (15 EACH) NR 45 THROUGH NRS 52, 53A, 55, 56, 58, 60, 61, 62, AND 64. TOTAL CYCLES, 2,111. INSTALLED INTERNAL NESTED ANGLES AND RIVETS ON STRINGERS PER ESO 51000, DATED 3-30-95, 4-7-95, AND 4-12-95. (X) 2L72 4F RT 19950811008451995081100845EU 1995 8 11 AALA950743 119950425A5330 DOUBLER FOKKERF28 F28MK0100 4990807EU FS 26025 DISBONDED A AALAK NONE O OTHER ININSP/MAINT 1 SW071462C 2821 11482 TULE - LEFT SKIN DOUBLER DISBONDED ON TAIL SECTION, STA 26025 BETWEEN STR 21 TO STR 22. INSTALLED FASTENER REPAIR PER ESO 51000, DATED 3-30-95, ITEM NR 1. TOTAL CYCLES, 2,111. (X) 2L72 4F RT 19950811008461995081100846EU 1995 8 11 AALA950745 119950425A5330 DOUBLER FOKKERF28 F28MK0100 4990807EU FS 26026 DISBONDED A AALAK NONE O OTHER ININSP/MAINT 1 SW071462C 2821 11482 TULE - RIGHT SKIN DOUBLER DISBONDED ON TAIL SECTION, STA 26026 BETWEEN STR 52 TO STR 54. INSTALLED REPAIR FASTENERS PER ESO 51000, DATED 3-30-95, ITEM NR 1 AND ATTACHED DRAWING. TOTAL CYCLES 2,111. (X) 2L72 4F RT 19950811008471995081100847EU 1995 8 11 AALA950749 119950425A5330 SKIN FOKKERF28 F28MK0100 4990807EU FS 12975/13550 DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW071462C 2821 11482 SKIN DAMAGED LOWER SURFACE, STA 12975 AND STA 13550 BETWEEN FALSE SPAR AND STR 2.60. INSTALLED DOUBLER PER ESO 51000, DATED 3-10-95. TOTAL CYCLES, 2,111. (X) 2L72 4F RT 19950811008481995081100848WP 1995 8 11 AALA950970 119950528A3260833703 SENSOR ELDEC DOUG DC9 DC983 3022083WP NLG DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0776201 53291 DFW - FLT 0619 - AFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, ALL GREEN GEAR INDICATING LIGHTS WENT OUT. NOSE GEAR RED INDICATING LIGHT REMAINED ILLUMINATED. GEAR DOOR OPEN LIGHT WAS OUT. LOWERING THE GEAR HANDLE RESULTED IN NORMAL INDICATION FOR GEAR DOWN. RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NOSE GEAR UP/DOWNLOCK SENSOR. PERFORMED REQUIRED INSTALLATION AND OPERATION CHECKS INCLUDING NOSE GEAR SWING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA6WE 19950811008491995081100849NM 1995 8 11 AALA950973 119950528A3350 EEL WIRE BOEING727 727223 1384074NM CABIN NEED REPAIR A AALAK NONE L NO TEST ININSP/MAINT 1 SW07893AA 22009 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD SECTION OF MAIN CABIN DIM. REPAIRED EMERGENCY EXIT FLOOR PATH WIRING AT FORWARD SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950811008501995081100850NM 1995 8 11 AALA950978 119950530A3350A3060712101 EEL STRIP BOEING727 727227 1384078NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07729AA 20736 DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED 10 FEET OF EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19950811008511995081100851NM 1995 8 11 AALA951011 119950601A3350A3060719101 EEL STRIP BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07691AA 25697 JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHT STRIP BROKEN AT SEAT 1. REPAIRED LIGHT STRIP, SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950811008521995081100852WP 1995 8 11 AALA951028 119950604A3350A3060719104 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07485AA 49678 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19950811008531995081100853EU 1995 8 11 AALA951083 119950606A2910 O-RING FOKKERF28 F28MK0100 4990807EU NR 1 POSITION LEAKING A AALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW071460A 11480 MCI/DFW - FLT 0739 - EN ROUTE DURING CRUISE, NR 1 HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN TO DECREASE. AIRCRAFT PROCEEDED TO DFW AND ACCOMPLISHED ALTERNATE FLAP AND ALTERNATE LANDING GEAR EXTENSION, LANDING WITHOUT INCIDENT. REPLACED O-RING ON NR 1 HYDRAULIC PUMP PRESSURE DISCONNECT. PRECAUTIONARY REPLACED HYDRAULIC FILTERS AND SERVICED SYSTEM. ACCOMPLISHED LEAK AND GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RT 19950811008541995081100854WP 1995 8 11 AALA951090 119950613A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07583AA 53160 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 16 FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT, ROW 7. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19950811008551995081100855NM 1995 8 11 AALA951091 119950615A3350 EEL WIRE DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071767A 48598 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROW 8D AND L2 DOOR INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F RTA22WE 19950811008561995081100856WP 1995 8 11 AALA951149 119950626A3350A3060719104 EEL STRIP DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07599AA 53289 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA6WE 19950811008571995081100857NM 1995 8 11 ASAA9540028 119950616A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01778AS 25110 ANC - CHECK - FLOOR TRACK EMERGENCY LIGHTS BETWEEN ROWS 15 AND 18 INOP. MAINTENANCE RE-CONNECTED WIRING. (X) 2L72 4F RTA16WE 19950811008581995081100858NM 1995 8 11 ASAA9540033 119950623A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01778AS 25110 SEA - PILOT REPORT - FLOOR TRACK LIGHTS OUT BETWEEN ROWS 19 AND 21. MAINTENANCE CONNECTED WIRE HARNESS AT ROW 21. (X) 2L72 4F RTA16WE 19950811008591995081100859EU 1995 8 11 C2XA95IA102 119950615A5320S53970919202 BRACKET AEROSPATR42 ATR42320 8680930EU WING/FUS CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914822 163 IAH - DURING C-CHECK INSPECTION, FOUND RT UPPER FWD WING TO FUSELAGE FAIRING BRACKET CRACKED OTBD, PANEL 291AL. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. TT 13,049.3. TC 14,220. (X) 2H72 4T RTA53EU 19950811008601995081100860EU 1995 8 11 C2XA95IA103 119950615A2720SA414A4 BEARING AEROSPATR42 ATR42320 8680930EU UPPER RUDDER RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914822 163 IAH - DURING C-CHECK INSPECTION, FOUND UPPER RUDDER BEARING BLEEDING RUST. MAINTENANCE REMOVED AND REPLACED THE BEARING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT 13,049.3. CYCLES, 14,220. (X) 2H72 4T RTA53EU 19950811008611995081100861NM 1995 8 11 PCAA9500227 119950523A2931 CONNECTOR DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYST DIRTY A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13830EX 155 NR 1 HYDRAULIC PRESSURE INDICATED 1400 PSI IN-FLIGHT. UPON LANDING, PRESSURE RETURNED TO 3000 PSI. CLEANED INDICATOR CANNON PLUG. GROUND RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19950811008621995081100862 1995 8 11 PCAA9500231 419950627A2312 VHF UNIT DHAV DHC8 DHC8102 2809003NM RADIO RACK LOOSE A PCAAO OTHER O OTHER NRNOT REPORTED 1 EA13831EX11407 160 CREW REPORTED LOSS OF ALL VHF COMMUNICATIONS. AIRCRAFT LANDED IN BOS WITHOUT INCIDENT. BOS MAINTENANCE FOUND RADIO ELECTRONICS UNIT UNSECURED. SECURED UNIT IN RACK. OPERATIONALLY CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950811008631995081100863 1995 8 11 RAIA950633 319950623A61408659567 SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03875JX7866 875 STL - FLT 7498 - RIGHT BETA LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT BETA LIGHT SWITCH. (X) 2L72 4T RTA56EU 19950811008641995081100864EU 1995 8 11 SIMA951721 119950621A3350301210 EEL ASSY AEROSPATR42 ATR42300 8680920EU PAX STAIRS INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21250AA 250 ORD - FLT 4351 - DURING DEBOARD, PILOT REPORTED EMERGENCY LIGHT ON PASSENGER STAIR WAS INOPERATIVE. MTX RAI LIGHT ASSY SYSTEM, OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950811008651995081100865 1995 8 11 TSAA9534126 419950624A34182566A21 AOA SENSOR BOEING737 7372T4 1384492NM STALL WARN SYST MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13807AL 23443 ITO/HNL - FLT 437 - PILOT REPORT. DURING TAKEOFF, ROLL 'WINDSHEAR INOP' LIGHT CAME ON. TAKEOFF CONTINUED, AND AFTER BECOMING AIRBORNE, STICK SHAKER BEGAN. AIRSPEED APPROXIMATELY 140 KNOTS TO 150 KNOTS. MOVING STALL WARNING SWITCH TO 'TEST' POSITION STOPPED SHAKER. EMERGENCY DECLARED. RETURNED TO ITO. LANDING NORMAL. REPLACED STALL WARN MOD AND AOA SENSOR, FUNCTIONAL CHECK IAW MM 27-32-0 OK. WINDSHEAR BITE CHECK OK. AIRCRAFT RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX3970. (X) 2L72 4F A16WE 19950811008661995081100866NM 1995 8 11 TWRA9538 119950620A5320BACR30US14K55 BOLT BOEING747 747212B 1384886NM BS 1241 SHEARED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15618FF 21937 DURING 'D' SERVICE, FOUND BOLT SHEARED IN ANGLE FORGED FITTING LOCATED AT STA 1241. REMOVED AND REPLACED BOLT. (X) 2L74 4F A20WE 19950811008671995081100867EU 1995 8 11 VTZA95201 119950619A77221379273H EGT CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE DIRTY A VTZAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 EA27496UE 900 IAD/HVN - FLT 6173 - DURING TAKOFF AT 1730 HRS ON 6-19-95, ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE DROPPED OFF DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE CANNON PLUGS ON THE LEFT EGT COMP RESISTOR. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950811008681995081100868EU 1995 8 11 VTZA95204 119950617A7600P323A702561 CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE BENT PINS A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27322UE 41058 IAD/BOS - FLT 6418 - DURING CLIMB-OUT AT 1105 HRS ON 6-17-95, RETURNED TO IAD DUE TO LEFT IEC FAILING IN-FLIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE STRAIGHTENED BENT PINS ON CANNON PLUG AT FIREWALL. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950811008691995081100869EU 1995 8 11 VTZA95212 119950630A3260ATG135020 SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG FAILURE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27325UE 41063 IAD/ORF - FLT 6462 - DURING TAKEOFF AT 1630 HRS ON 6-30-95, RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED LEFT WEIGHT-ON-WHEEL SWITCH. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950811008701995081100870EU 1995 8 11 VTZA95213 119950630A3230M4001256 RELAY JETAIRJETSTMJETSTM4101 1500501EU AVIONICS RACK FAILED A VTZAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA27325UE 41063 CHO/IAD - FLT 6270 - DURING CLIMB-OUT AT 100 HRS ON 6-30-95, THE LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. AIRCRAFT PROCEEDED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT AOG SLAVE RELAY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950811008711995081100871GL 1995 8 11 WTAA950208A 319950611A61147503503AF DOME SEAL BAG JETSTMJETSTM3101 1500215EU ROTOL R333 R333482F12 GL LT PROPELLER LEAKING A WTAADE RETURN TO BLOCK ENGINE SHUTDOWN BJKSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FLUID LOSS TXTAXI/GRND HDL 1 WP17419UE 779 LEFT ENGINE LOW OIL PRESSURE INDICATION REPORTED ACCOMPANIED BY THE REPORT OF SMOKE ODOR IN CABIN DURING TAXI OUT. CREW SECURED LEFT ENGINE AND RETURNED TO GATE. MAINTENANCE FOUND OIL LEAKING AT LEFT ENGINE BETA TUBE O-RINGS AND PROPELLER DOME SEAL. REPLACED O-RINGS AND DOME SEAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 6 CP61GL 19950811008721995081100872NE 1995 8 11 YIEA00195 219950517A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE RIGHT FLAMED OUT ALAYIEAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 GL23814AA100264722 31 299G033 PILOT REPORTED WHILE ACFT LEVEL AT CRUISE ALTITUDE 27,000 FEET AND AIRSPEED MACH. .70, RT ENGINE FLAMED OUT AFTER LIGHTNING FLASH ON RT SIDE OF ACFT. ACFT DESCENDED TO 20,000 FEET AND ENGINE SUCCESSFULLY RESTARTED. ENG OPERATION NORMAL AFTER THAT. ACFT/ENG FUEL AND IGNITION SYSTEMS CHECKED FOR DISCREPANCIES, NONE FOUND. ENGINE WAS INSPECTED FOR FOD OR DAMAGE TO COMPRESSOR AND FAN WITH NONE FOUND. ENG BLEED AND GUIDE VANE SYS INSPECTED FOR DISCREPANCIES WITH NONE FOUND. ENG GROUND RUN AND PERFORMANCE CHECKED IAW GE MM. ALL ENG PARAMETERS MET. ACFT RETURNED TO SERVICE. IT IS BELIEVED UNSTABLE AIR IN VICINITY OF LIGHTNING AND THUNDERSTORMS CAUSE OF ENG FLAME-OUT. NO FURTHER ACTION REQUIRED.(X) 2L72 4F4 F A7EU E7EA 19950811008741995081100874NE 1995 8 11 9512149853 219950806A7230 COMPRESSOR DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01762NC 47710 688767 NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE ENGINE AND PERFORMED A GROUND RUN-UP. THE ENGINE SYSTEMS CHECKED OK. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950811008751995081100875NM 1995 8 11 9512155529 119950809A29133508806 HYD PUMP BOEING757 757251 1384970NM LT ENGINE FAILED A NWAAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01529US22809449 23844 DURING CRUISE, THE LT HYD ENG PUMP AND LT ENG HYD OVERHEAT MESSAGES DISPLAYED AND THE PRESSURE LIGHT AND OVERHEAT LIGHT ILLUMINATED. AFTER 30 SECONDS THE OVERHEAT LIGHT WENT OUT, HYDRAULIC PRESSURE AND QUANTITY WERE NORMAL. THE ENGINE PUMP SWITCH WAS TURNED OFF. AFTER TEN MINUTES THE HYDRAULIC QUANTITY DECREASED AND THE LT HYD SYS PRESS MESSAGE AND LIGHT CAME ON. HYDRAULIC PRESSURE REMAINED NORMAL. WHEN FLAPS 1 DEGREE WAS SELECTED ON APPROACH, POWER XFER UNIT MESSAGE APPEARED AND THE LT HYDRAULIC PRESSURE WENT TO ZERO. ALTERNATE FLAP AND GEAR EXTENSION PROCEDURES WERE USED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE HYDRAULIC PUMP AND SYSTEM FILTERS. SYSTEM CHECK WAS NORMAL. 2L72 4F RTA2NM 19950811008761995081100876NM 1995 8 11 95UAL900085 119950810A2612 FIRE WARNING BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE WHEEL WELL MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29608UA 21869 WHEEL WELL FIRE LIGHT ILLUMINATED IN FLIGHT, LOWERED LANDING GEAR AND LIGHT WENT OUT. A/C RETURNED TO FIELD UNDER AMBER ALERT, NO EVIDENCE OF FIRE FOUND. REPLACED CARD SYSTEM, OPS CHECKS OK. NO FAULT FOUND WITH CARD, UNABLE TO DUPLICATE. 2L72 4F4 FRTA1NM E3NE 19950811008771995081100877NM 1995 8 11 95UAL900086 119950810A53136547977502 STRINGER BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE BS 660 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29363UA 24532 STRINGER 17R CRACKED 1.5 INCHES AT STATION 660. REPAIRED PER SRM 51-70-12. 2L72 4F4 FRTA16WE E2GL 19950811008781995081100878SO 1995 8 11 COM11942 119950803A323019803 RETRACT MECH EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01200C 120200 RIGHT MLG INTRANSIT LIGHTS REMAIN ON WITH LANDING GEAR RETRACTED. FOUND LOCK WASHER ON RIGHT MLG RETRACT ACTUATOR DEFECTIVE. ADJUSTED RIGHT RETRACT ACTUATOR TO M/M SPECIFICATIONS AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950811008791995081100879SO 1995 8 11 COM11943 119950807A2432167556 BATTERY EMB 120 EMB120RT SO BATT COMPT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01463CA6572 170 120267 BATTERY OVERHEAT WARNING AFTER TAKEOFF. FLIGHT RETURNED TO RDU. REPLACED AIRCRAFT BATTERY. 2L72 4T RTA31SO 19950811008801995081100880SO 1995 8 11 COM11944 119950804A3260922AA2YA6YZ722 SENSOR EMB 120 EMB120RT SO LT MLG DAMAGED A COMAO OTHER N FALSE WARNING LDLANDING 1 SO01241CA 120211 DURING LANDING, LEFT MLG INDICATED UNSAFE ON A-SYSTEM AND SAFE ON B-SYSTEM. REPLACED DAMAGED PROXIMITY SENSOR FOR A SYSTEM DOWNLOCK. 2L72 4T RTA31SO 19950811008811995081100881NE 1995 8 11 COM11945 219950807A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A COMAK NONE O OTHER ININSP/MAINT 1 SO01257CA 3672 120248 115325 RIGHT PROPELLER COULD NOT BE ROTATED BY HAND. REPLACED RIGHT ENGINE. 2L72 4T4 TRTA31SO E20NE 19950811008821995081100882SO 1995 8 11 COM11946 119950804A7333M259884908 O-RING EMB 120 EMB120RT SO RT ENGINE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01259CA 120252 FUEL LEAK RIGHT ENGINE. REPLACED O-RING ON FUEL FLOW TRANSMITTER. 2L72 4T RTA31SO 19950811008831995081100883SO 1995 8 11 COM11947 119950808A4900M610628023 RELAY EMB 120 EMB120RT SO E/E BAY MALFUNCTIONED A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01168CA 120168 DURING PUSH BACK THE AIRCRAFT FILLED WITH SMOKE. APU AUTO SHUT DOWN. INSPECTED APU AND FOUND NO DEFECTS. REPLACED RELAY KO 194 FOR TROUBLESHOOTING. 2L72 4T RTA31SO 19950811008841995081100884SO 1995 8 11 COM11948 119950808A527012042482001 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01264CA 120262 CARGO DOOR WARNING TAKEOFF. TAKEOFF ABORTED. ADJUSTED CARGO DOOR MICROSWITCH STRIKER. 2L72 4T RTA31SO 19950811008851995081100885NE 1995 8 11 COM31129 319950803A611466071425 HUB ROTOL R3544123F13 SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROPELLER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01341CA9450 3229 DRG150986 340A021 DRG150986 DURING OVERHAUL INSPECTION MULTIPLE CRACK INDICATIONS WERE FOUND DURING ULTRASONIC INSPECTION (IAW SB 61-58 APPENDIX C, SCAN B) HUB S/N 110502 WAS DISASSEMBLED AND REMOVED FROM SERVICE. 2L72 4T RTA52EU 6 CP61GL 19950811008861995081100886EU 1995 8 11 COM31130 119950805A2610M8372396K1005N CONNECTOR SAAB SF340 SF340A 7850100EU RT NACELLE DEFECTIVE A COMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01341CA 340A021 RIGHT TAIL PIPE HOT LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. ENGINE WAS SHUT DOWN AND LIGHT EVENTUALLY WENT OUT. FLIGHT RETURNED TO CVG. REPLACED WIRING CONNECTOR 162VP. 2L72 4T RTA52EU 19950811008871995081100887EU 1995 8 11 COM31131 119950807A61201103P0620 PRESS SWITCH SAAB SF340 SF340A 7850100EU LT/RT ENGINE DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01357CA5283 697 340A044 AUTO COARSEN WARNING ON CWP. FLIGHT RETURNED TO EVV. REPLACED THE AUTO COARSEN P3 PRESSURE SWITCHES. 2L72 4T RTA52EU 19950811008881995081100888EU 1995 8 11 COM31132 119950805A7931IPTE551000200 OIL PRESS TRANS SAAB SF340 SF340A 7850100EU RT PROP G BOX DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01158CA8469 126 340A158 RIGHT PROPELLER GEARBOX INDICATED ZERO OIL PRESSURE. FLIGHT RETURNED TO CVG. REPLACED OIL PRESSURE TRANSDUCER. 2L72 4T RTA52EU 19950811008901995081100890 1995 8 11 COM31134 419950808A61228210163 PROP GOVERNOR SAAB SF340 SF340A 7850100EU RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01357CA1259944 340A044 RIGHT PROPELLER VERY SLOW COMING OUT OF FEATHER. THE OVERSPEED TEST DID NOT FUNCTION NORMAL. REPLACED THE RIGHT PROPELLER OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950811008911995081100891EA 1995 8 11 COM60533 119950809A2910601R7530117 HYD LINE CNDAIRCL600 CL6002B19 EA RT SPOILERON LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01915CA 7013 HYDRAULIC LEAK NOTICED RIGHT WING SPOILERON AREA. REPLACED RIGHT SPOILERON HYDRAULIC LINE ASSY WHICH WAS LEAKING FROM SWAGE FITTING. 2L72 4F RTA21EA 19950811008921995081100892EA 1995 8 11 COM60534 119950808A7830 TR UNIT CNDAIRCL600 CL6002B19 EA RT ENGINE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01916CA 7014 AFTER TAKEOFF, WHEN RIGHT THRUST REVERSER ARM SWITCH SET TO OFF, THE RIGHT T/R UNSAFE MESSAGE CAME ON. ACFT RETURNED TO FIELD. THRUST REVERSER WAS STOWED AND SECURED AND SYSTEM PLACED ON DEFERRED MAINT LIST. 2L72 4F RTA21EA 19950811008931995081100893NM 1995 8 11 MWEA95260 119950808A25605917689103 SLIDE COVER DOUG MD88 MD88 3023688NM FWD ENT DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31701ME 49760 CREW REPORTS FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. MAINTENANCE RESECURED FORWARD ENTRANCE SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950811008941995081100894NM 1995 8 11 P5CA9500701 119950809A5751 TE SKIN BOEING747 747121 1384871NM RT AILERON SEPARATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 RIGHT OUTBOARD AILERON TRAILING EDGE SEPERATED OUTBOARD OF NR 2 STATIC WICK. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950811008951995081100895WP 1995 8 11 SCNA95151 119950715A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15151SY 48295 FOUND THE AFT CABIN EMERGENCY FLOOR LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT CABIN POWER SUPPLY PER MM 33-51-01. LIGHTS TESTED GOOD. 2L73 4F A22WE 19950811008961995081100896WP 1995 8 11 SCNA95153 119950719A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 DURING LINE CHECK FOUND THE MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED MID CABIN POWER SUPPLY IAW MM 33-50-00. LIGHTS CHECKED GOOD. 2L73 4F A22WE 19950811008971995081100897WP 1995 8 11 SCNA95154 119950721A3350DC26F14195 EEL CONNECTOR DOUG DC10 DC1010 3022110WP OVERWING SHORTED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 FOUND THE OVERWING (OVERHEAD) EMERGENCY LIGHTS INTERMITTENT. CONNECTOR PI-2069 WAS FOUND INTERNALLY SHORTING WHEN CONNECTED TO THE EMERGENCY LIGHT BATTERY PACK. REMOVED AND REPLACED CONNECTOR PI-2069 AND LIGHTS CHECKED GOOD. 2L73 4F A22WE 19950811008981995081100898NM 1995 8 11 SCNA95155 119950724A335057761 EEL BATTERY BOEING727 727282 2F0R NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 FOUND THE ZONE 5 EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY AT ZONE 5 AND FLOOR TRACK LIGHTING TESTED GOOD PER MM 33-50-01. 2L73 4F RTA3WE 19950811008991995081100899NM 1995 8 11 SCNA95156 119950724A3350S106 EEL BATTERY BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 FOUND THE OVERHEAD EMERGENCY LIGHT AT SEAT 11 INOPERATIVE. REMOVED AND REPLACED BATTERIES IN OVERHEAD EMERGENCY LIGHT AND UNIT TESTED GOOD. 2L73 4F RTA3WE 19950811009001995081100900NM 1995 8 11 SCNA95157 119950725A3350900835A EEL BATTERY BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 FOUND THE EMERGENCY EXIT AISLE SIGN BETWEEN THE L-2 AND R-2 DOOR TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1095 AT THE AFT EMERGENCY AISLE EXIT SIGN IAW MM 33-50-22. SIGN TESTED GOOD. 2L73 4F RTA3WE 19950811009011995081100901NM 1995 8 11 SCNA95159 119950730A793142D107A1 OIL PRESS SWITCH BOEING727 7272A1 138407FNM NR 3 ENGINE LEAKING A SCNAE ENGINE SHUTDOWN K FLUID LOSS UKUNKNOWN 1 GL15286SC 21601 WHILE EN ROUTE THE NR 3 ENGINE OIL QUANTITY BEGAN TO DECREASE. THE ENGINE WAS SHUTDOWN, AND ALL INDICATIONS WERE NORMAL. A LEAK WAS FOUND AT THE LOW OIL PRESSURE SWITCH AND THE UNION BELOW THE SWITCH. THE SWITCH AND PACKINGS AT THE UNION WERE REPLACED, AND THE ENGINE LEAK CHECKED GOOD. 2L73 4F A3WE 19950811009021995081100902WP 1995 8 11 SCNA95160 119950730A3350P4010049 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A SCNAK NONE L NO TEST CLCLIMB 1 GL15573SC 46905 THE FORWARD LEFT AND RIGHT EMERGENCY FLOOR LIGHTS ILLUMINATED SHORTLY AFTER TAKEOFF. THE EMERGENCY LIGHTS WERE FOUND SHORTED DUE TO A RIGHT FORWARD LAV LEAKING FLUID. THE EMERGENCY BATTERY PACKS WERE REPLACED AND THE LIGHTS TESTED GOOD. 2L73 4F A22WE 19950811009031995081100903NM 1995 8 11 SCNA95161 119950726A335090054200 EEL POWER SUPPLY BOEING727 7272A1 138407FNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK POWER SUPPLY AND BATTERY PACK (M1086). PERFORMED EMERGENCY EXIT LIGHT TEST AND LIGHTS TESTED GOOD PER MM 33-50-22. 2L73 4F A3WE 19950811009041995081100904NM 1995 8 11 SCNA95162 119950731A3350S106 EEL BATTERIES BOEING727 727227 1384078NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 FOUND THE AFT AIRSTAIR EMERGENCY FLOOD LIGHTS DIM. REMOVED AND REPLACED BATTERIES AND LIGHTS TESTED GOOD PER MM 33-50-01. 2L73 4F A3WE 19950811009051995081100905NM 1995 8 11 SCNA95163 119950803A2750MX1116852A FLAP DRIVE MOTOR BOEING727 7272A1 138407FNM OTBD FLAP DRIVE LEAKING A SCNAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL15286SC 21601 AFTER ENGINE START AND TAXI THE A-SYSTEM HYDRAULIC QUANTITY DROPPED FROM FULL TO 2 GALLONS. THE OUTBOARD FLAP DRIVE MOTOR WAS FOUND LEAKING WITH THE ENGINES RUNNING AND FLAPS IN THE DOWN POSITION. REMOVED AND REPLACED THE FLAP DRIVE MOTOR PER MM 27-51-62. OPERATIONS TESTED GOOD WITH NO LEAKS NOTED. 2L73 4F A3WE 19950811009061995081100906NM 1995 8 11 UPS404102 119950807A5753 LE SKIN BOEING747 747123 1384873NM LT TE MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND MAINTENANCE FOUND LT WING, INBD MID FLAP LEADING EDGE INBD SECTION HAS A HOLE APPROX 1 INCH DIAMETER AND A CRACK EMANATING FROM IT THAT IS APPROX 10 - 12 INCHES LONG. REPAIRED PER SRM 747-51-40-9. 2L74 4F A20WE 19950811009071995081100907NM 1995 8 11 UPS404103 119950807A5730 PANEL BOEING747 747123 1384873NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND MAINTENANCE FOUND LEFT WING FLYING PANEL INBD TRAILING EDGE NEXT TO FUSELAGE HAS 14 INCH CRACK (TOP OF WING). REMOVED PANEL. DRILLED HOLES IN NEW PANEL AND STARTED INSTALLATION. FINISHED INSTALLATION OF NEW PANEL AS PER M/M 57-22-01. 2L74 4F A20WE 19950811009081995081100908WP 1995 8 11 UPS804104 119950808A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01808UP 46008 WHILE ON GROUND MAINTENANCE FOUND EMERERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK. 2L74 4F RT4A25 19950818000011995081800001EU 1995 8 18 9512163204 219950808A7530 VBV AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL01304US 40 31686 DURING CLIMB, NR 2 ENGINE EGT REACHED 890 DEGREES AND NEVER COOLED BELOW 850 DEGREES. THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE VBV AND A SHEARED FLEX SHAFT WERE REPLACED. GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L72 4F4 FRTA28NM 19950818000021995081800002NE 1995 8 18 9512171152 219950809A7530 OVERRIDE VALVE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP LDLANDING 1 GL01152US 46761 686114 DURING LANDING ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WHILE IN REVERSE THRUST. THE EGT WENT TO 910 DEGREES AND THE ENGINE WAS SHUTDOWN. THE ENGINE WAS INSPECTED AND THE 3.0 BLEED OVERRIDE SOLENOID VALVE WAS REPLACED. GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L73 4F4 F A22WE E20EA 19950818000031995081800003NM 1995 8 18 9512182290 119950808A361065224462 DUCT BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 3 ENGINE LEAKING A NWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL01290US 21387 695275 ON DESCENT TO MSP, THE NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED MOMENTARILY. A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED ON NR 2 ENGINE. THE FLIGHT CONTINUED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. A LEAK WAS FOUND IN THE NR 3 START BLEED AIR DUCT. MAINTENANCE REPLACED THE DUCT AND CHECKED THE SYSTEM FOR LEAKS, NONE FOUND. OPERATIONAL CHECKS WERE OK, AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950818000041995081800004NE 1995 8 18 ABXA9500656 219950808A7200 ENGINE DOUG DC8 DC861 3021952WP PWA JT3D JT3D3B 52039NE NR 4 FAILED A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 GL23845AX 46157 669184 NR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO ENGINE FAILURE. EGT MAXIMUM TEMPERATURE WAS 760 DEGREES CELSIUS. NR 4 ENGINE WAS SECURED IAW EMERGENCY PROCEDURE CHECKLIST. AIRCRAFT RETURNED TO ILN. REMOVED AND REPLACED ENGINE. TRIMMED DURING GROUND RUN IAW DC 8 MM. 2L74 4F4 F 4A25 1E8 19950818000051995081800005WP 1995 8 18 ABXA9500657 119950808A3350 EEL WIRE DOUG DC8 DC863 302198AWP CABIN BROKEN A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23822AX 46079 EMERGENCY EXIT LIGHTS 'DISARM' LIGHT DOES NOT ILLUMINATE, WHEN DISARM SWITCH IS PLACED IN THE DISARM CHECK POSITION. LIGHT COMES ON WHEN SWITCH IS RELEASED TO THE 'DISARM' POSITION. FOUND BROKEN TERMINAL ON EMERGENCY DISARM LIGHT SWITCH. REPAIRED BROKEN WIRE TERMINAL. ALL SYSTEMS OPS CHECKED GOOD IAW DC 8 MM. 2L74 4F 4A25 19950818000061995081800006NM 1995 8 18 P5CA9500702 119950811A5313 STRINGER BOEING747 747124 1384874NM BS 480 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 ON WALK AROUND FOUND POPPED FASTENERS AT BS 480, STRINGERS 44 AND 47. ALSO, FOUND CRACKED STRINGER AND CORROSION. REPAIRED PER BOEING SRM 53-30-03. 2L74 4F A20WE 19950818000071995081800007NM 1995 8 18 UPS204060 119950811A532065453134 CLIP BOEING727 72727C 138400JNM BS 294 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED STRINGER CLIP STA 294 STR 2L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-5, 51-30-2. 2L73 4F A3WE 19950818000081995081800008NM 1995 8 18 UPS204061 119950811A53307075T6 SKIN BOEING727 72727C 138400JNM BS 1243 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK AT LOWER TORQUE BOX BS 1243, LBL 21 WL 169. INSTALLED FABRICATED PART, WORK DONE IAW SRM 51-30-2, 51-10-1, 51-40-2, 51-10-2, MM 51-20-1 AND SRM 51-30-6. 2L73 4F A3WE 19950818000091995081800009NM 1995 8 18 UPS204062 119950811A531266147361 BLKHD LINK BOEING727 72727C 138400JNM BS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK THAT MOUNTS TO BULKHEAD BS 740 FWD OF LWR CHORD RBL 13. REPLACED EXPANSION LINK IAW SRM 51-30-2 AND SRM 51-10-1. 2L73 4F A3WE 19950818000101995081800010NM 1995 8 18 UPS204063 119950811A53302024T3063 SKIN BOEING727 72727C 138400JNM BS 294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION IN SKIN LAP STR 24L BS 294. REPAIRED SKIN LAP IAW SRM 53-30-3 AND UPS EO B727-5330-0509Q. 2L73 4F A3WE 19950818000111995081800011NM 1995 8 18 UPS204064 119950811A53302024T3 SKIN BOEING727 72727C 138400JNM BS 298/318 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION IN SKIN LAP STR 24R, BETWEEN BS 298 AND BS 318. FABRICATED, INSTALLED FILLER AND DOUBLER, WORK DONE IAW SRM 53-30-1, 53-30-3. 2L73 4F A3WE 19950818000121995081800012NM 1995 8 18 UPS204065 119950811A5320ALUM7075T6068 STRINGER TIE BOEING727 72727C 138400JNM BS 400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT STRINGER TIE AND SUPPORT ANGLE, STA 400 STRINGER 28 RBL 7 WL 148. CORROSION REMOVAL ON SUPPORT WAS WITHIN LIMITS, STRINGER TIE WAS OUT-OF-LIMITS. REMOVED STR TIE, FABRICATED AND INSTALLED NEW STRINGER TIE AT BS 400, STR 28R, IAW SRM 53-10-2, 51-10-4, 51-10-6, 53-10-1. 2L73 4F A3WE 19950818000131995081800013NM 1995 8 18 UPS204066 119950811A53117075T6050ALUM FRAME BOEING727 72727C 138400JNM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FRAME, STA 360 LBL 25 TO LBL 30 WL 155. FABRICATED AND INSTALLED REPAIR PART PER SRM 51-40-3, 53-10-1, 51-10-6. 2L73 4F A3WE 19950818000141995081800014NM 1995 8 18 UPS204067 119950811A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 1110 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK ON SHEAR TIE AT STA 1110 STR 1 AND 2 LT. REMOVED, FABRICATED AND REPLACED SHEAR TIE AT STA 1110 BETWEEN STR 1 AND 2 LEFT IAW SRM 51-10-01. 2L73 4F A3WE 19950818000151995081800015NM 1995 8 18 UPS204068 119950811A53132024T3 STRINGER BOEING727 72727C 138400JNM BS 1125 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER AT STA 1125 STR 2 LT. FABRICATED NEW PARTS AND INSTALLED WITH FASTENERS IAW SRM 51-30-2, 53-10-3, 51-20-4. 2L73 4F A3WE 19950818000161995081800016NM 1995 8 18 UPS204069 119950811A5313BAC1493574 STRINGER BOEING727 72727C 138400JNM BS 730-740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER AT STA 730 TO 740. FABRICATED J-ANGLE REPAIR DOUBLER. INSTALLED PER SRM 51-30-2, 51-20-4, 53-10-3, 51-30-4, 53-10-2. 2L73 4F A3WE 19950818000171995081800017NM 1995 8 18 UPS204070 119950811A5315BAC1505100246 FLOORBEAM BOEING727 72727C 138400JNM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATES HOLES, STA 328 LBL 2 TO 50 WL 208. REPAIRED FLOORBEAM IAW SRM 53-10-8 AT STA 328 LBL 4-50 2L 208. 2L73 4F A3WE 19950818000181995081800018NM 1995 8 18 UPS204071 119950811A57506593155119 FITTING BOEING727 72727C 138400JNM NR 4 HOUSING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 CARRIAGE HOUSING CORRODED AT BEARING MATING SURFACE. REMOVED AND REPLACED CARRIAGE HOUSING IAW SRM 51-30-2. 2L73 4F A3WE 19950818000191995081800019NM 1995 8 18 UPS204072 119950811A57506593155119 FITTING BOEING727 72727C 138400JNM NR 3 HOUSING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION AND CRACK ON NR 3 CARRIAGE HOUSING. REMOVED AND REPLACED NR 3 CARRIAGE HOUSING IAW SRM 51-30-2. 2L73 4F A3WE 19950818000201995081800020NM 1995 8 18 UPS204073 119950811A574465192474 FITTING BOEING727 72727C 138400JNM RT TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W I/B MIDFLAP I/B CARRIAGE SUPPORT FITTING WAS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-30-2. 2L73 4F A3WE 19950818000211995081800021NM 1995 8 18 UPS204074 119950811A574465192474 FITTING BOEING727 72727C 138400JNM RT TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W I/B MIDFLAP O/B CARRIAGE SUPPORT FITTING WAS CORRODED. REMOVED AND REPLACED FITTING IAW 727 SRM 51-30-2. 2L73 4F A3WE 19950818000221995081800022NM 1995 8 18 UPS204075 119950811A5712652466628 RIB BOEING727 72727C 138400JNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W INBD MIDFLAP, OB CENTER TRACK RIB FITTING WAS CRACKED. INSTALLED NEW TRACK RIB FITTING IAW SRM 51-30-2 AND SRM 51-10-1. 2L73 4F A3WE 19950818000231995081800023NM 1995 8 18 UPS204076 119950811A575165931551031 SUPPORT FITTING BOEING727 72727C 138400JNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND L/W I/B AILERON HAS CORROSION IN FASTENER HOLES ON I/B LOWER SIDE OF SUPPORT FITTING. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-30-2. 2L73 4F A3WE 19950818000241995081800024NM 1995 8 18 UPS204105 119950811A5347BAC51201430 SEAT TRACK BOEING727 72727C 138400JNM BS 760-850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND SEAT TRACK AT BS 760 TO 850 RBL 65 TO BE CORRODED ON BOTTOM FLANGE. FABRICATED REPLACEMENT TRACK PER SRM 51-10-2 AND INSTALLED TRACK PER SRM 51-30-2. 2L73 4F A3WE 19950818000251995081800025NM 1995 8 18 UPS204106 119950811A575369207734 SUPPORT RIB BOEING727 72727C 138400JNM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK SUPPORT RIB IN THE R/W I/B MIDFLAP TRAILING EDGE COVE 52 INCHES FROM THE I/B END. INSTALLED NEW RIB IAW SRM 51-30-5, 51-10-1, 51-30-2. 2L73 4F A3WE 19950818000261995081800026NM 1995 8 18 UPS204107 119950811A5315BAC14902773071 FLOORBEAM BOEING727 72727C 138400JNM BS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 312, LBL 0 LBL 29. FABRICATED REPAIR PARTS AND INSTALLED PER SMR 53-10-8. 2L73 4F A3WE 19950818000271995081800027NM 1995 8 18 UPS204108 119950811A5320 STIFFENER BOEING727 72727C 138400JNM BS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION RT PRESSURE BOX FORMED STIFFENER AT BS 740 TO BE CRACKED, FORWARD STIFFENER. FABRICATED PART AND INSTALLED ALL PART IAW SRM 51-20-1, 51-10-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950818000281995081800028NM 1995 8 18 UPS204109 119950811A571365C2613912 STRINGER BOEING727 72727C 138400JNM WS 546.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND STRINGER 9 UPPER CRACKED AT 546.5 ON LEFT WING. INSTALLED REPAIR IAW EO B727-5710-0314-F. 2L73 4F A3WE 19950818000291995081800029WP 1995 8 18 UPS8040100 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 816.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 816.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0. 2L74 4F RT4A25 19950818000301995081800030WP 1995 8 18 UPS8040101 119950811A5320 WEB DOUG DC8 DC873F 302199FWP FS 190-200 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND WEB CRACK AT ACCESS HOLE CLOSURE WEB BETWEEN FRAME STA 190 AND 200 AT LONG 16R. ROUTED CRACK THAT TERMINATED AT .25 STOP DRILL IAW SRM 53-2-0, INSTALLED DOUBLER IAW SRM 53-2-0 AND 51-1-21. 2L74 4F RT4A25 19950818000311995081800031WP 1995 8 18 UPS804077 119950811A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT FLOORBEAM SUPPORT FITTING CORRODED ON INNER SERVICE AT FLOORBEAM ST 1340. REMOVED CORROSION PER SRM 51-1-8, FABRICATED, DRILLED AND INSTALLED DOUBLER PER SRM 53-2-0. 2L74 4F RT4A25 19950818000321995081800032WP 1995 8 18 UPS804078 119950811A5347 SEAT TRACKS DOUG DC8 DC873F 302199FWP BS 1330/1370 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND STA 1370, BLO SEAT TRACK SPLICES AND BOTH SEAT TRACKS ARE CORRODED ON UNDERSIDE. ALSO, AT 6 STA 1330. REMOVED, FABRICATED AND INSTALLED SEAT TRACK SPLICE. CLEANED AND TREATED LOWER ENDS OF SEAT TRACKS PER SRM 51-1-8. 2L74 4F RT4A25 19950818000331995081800033WP 1995 8 18 UPS804079 119950811A5320 SHEAR TIE DOUG DC8 DC873F 302199FWP BS 1340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND STA 1340 AT STR 31L, SHEAR TIE HAS HEAVY CORROSION. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-4-1 AND 51-1-21. 2L74 4F RT4A25 19950818000341995081800034WP 1995 8 18 UPS804080 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 747.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD WING, STA XFS 747.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00 PG 801. 2L74 4F RT4A25 19950818000351995081800035WP 1995 8 18 UPS804081 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 785.0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00 PG 801. 2L74 4F RT4A25 19950818000361995081800036WP 1995 8 18 UPS804082 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 672.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E AT STA XFS 672.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00. 2L74 4F RT4A25 19950818000371995081800037WP 1995 8 18 UPS804083 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 785.0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT LWR END. REPAIRED IAW MM 57-00-00. 2L74 4F RT4A25 19950818000381995081800038WP 1995 8 18 UPS804084 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 760.0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 760.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00. 2L74 4F RT4A25 19950818000391995081800039WP 1995 8 18 UPS804085 119950811A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 680 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ACC COMPT STA 680 LBL 48 SEAT TRACK SUPPORT ANGLE WAS CRACKED. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 53-4-3 AND 51-1-20D. 2L74 4F RT4A25 19950818000401995081800040WP 1995 8 18 UPS804086 119950811A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 680 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ACC COMPT STA 680 RBL 24 SEAT TRACK SUPPORT ANGLE WAS CRACKED. FABRICATED AND INSTALLED SUPPORT ANGLE IAW SRM 53-4-3 AND 51-1-20D. 2L74 4F RT4A25 19950818000411995081800041WP 1995 8 18 UPS804087 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 810 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 810.0 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000421995081800042WP 1995 8 18 UPS804088 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 797.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 797.5 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000431995081800043WP 1995 8 18 UPS804089 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 791.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000441995081800044WP 1995 8 18 UPS804090 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 791.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000451995081800045WP 1995 8 18 UPS804091 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 766.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-00-00. 2L74 4F RT4A25 19950818000461995081800046WP 1995 8 18 UPS804092 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 766.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000471995081800047WP 1995 8 18 UPS804093 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 610.0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 610.0 WAS CRACKED AT THE AFT LWR END. REPAIRED PER SRM 57-2-0. 2L74 4F RT4A25 19950818000481995081800048WP 1995 8 18 UPS804094 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 566.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 566.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM 57-20-0. 2L74 4F RT4A25 19950818000491995081800049WP 1995 8 18 UPS804095 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 728.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 728.75 WAS CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-20-0. 2L74 4F RT4A25 19950818000501995081800050WP 1995 8 18 UPS804096 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB STA XFS 660.0 WAS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0. 2L74 4F RT4A25 19950818000511995081800051WP 1995 8 18 UPS804097 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 641.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 641.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0. 2L74 4F RT4A25 19950818000521995081800052WP 1995 8 18 UPS804098 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 653.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 653.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0. 2L74 4F RT4A25 19950818000531995081800053WP 1995 8 18 UPS804099 119950811A5712 RIB DOUG DC8 DC873F 302199FWP WS 778.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 778.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0. 2L74 4F RT4A25 19950818000571995081800057SO 1995 8 18 95ZZZX3999 119950629A3230 ROD END PIPER PA31 PA31350 7103110SO RT MLG ACTUATOR FAILED A JIKAO OTHER O OTHER CLCLIMB 1 WP013BT 317752172 PILOT REPORTED THE RIGHT MAIN GEAR WOULD NOT UNLOCK AND RETRACT. MAINTENANCE FOUND FOLLOWING DISCREPANCIES: THE MAIN GEAR ACTUATOR ROD END (PN IS NOT LISTED IN EITHER FIGURE 39 OR FIGURE 106 OF THE IPC) HAD COME APART (BALL RETAINERS AND BALL SEPARATED FROM HOUSING) AND HAD BROKEN AT THE TOP THREAD. THE TELESCOPING ROD UPPER ROD END (PN 452-383) ALSO HAD BROKEN AT THE TOP THREAD, AND THE LOCK ROD ATTACH FORK (PN 41789-00) WAS FROZEN. 1L72 3O A20SO 19950818000581995081800058SO 1995 8 18 95ZZZX4000 119950629A52804752932 HINGE 4752930 PIPER PA31 PA31 7103102SO MLG LT INBD DOORBROKEN A JIKAO OTHER J WARNING INDICATION CLCLIMB 1 WP016733L 31636 AFTER GEAR RETRACTION, LEFT INBOARD DOOR REMAINED OPEN AND GEAR UNSAFE LIGHT REMAINED ON. FOUND THE FORWARD HINGE HAD BROKEN IN RADIUS. THIS HINGE IS THE IMPROVED TYPE INSTALLED IAW AD 80-26-05 AND PIPER SB 682 TO PREVENT CRACKING. AIRCRAFT TOTAL TIME 14,876. 1L72 3O A20SO 19950818000591995081800059SO 1995 8 18 95ZZZX4001 119950703A52804752932 HINGE 4752930 PIPER PA31 PA31350 7103110SO MLG RT INBD DOORBROKEN A JIKAO OTHER J WARNING INDICATION CLCLIMB 1 WP01600TS 317305047 AFTER GEAR RETRACTION, RIGHT INBOARD DOOR REMAINED OPEN AND GEAR UNSAFE LIGHT REMAINED ON. FOUND THE FORWARD HINGE HAD BROKEN IN RADIUS. ALSO FOUND BEARING (PRESSED INTO HINGE) WORN AND HAD EXCESSIVE PLAY. THIS HINGE IN THE IMPROVED TYPE INSTALLED IAW WITH AD 80-26-05 AND PIPER SB 682 TO PREVENT CRACKING. SECOND INCIDENT IN RECENT MEMORY (REF MOD 6-29-95). 1L72 3O A20SO 19950818000601995081800060SO 1995 8 18 95ZZZX4002 119950621A3233452729 ROD END 3579702 PIPER PA32 PA32R300 7103213SO NLG ACTUATOR BROKEN A JIKAO OTHER O OTHER NRNOT REPORTED 1 WP018929C 32R7680144 THIS REPORT FULFILLS THE REQUIREMENTS OF FAR 135.415(A)(12). AIRCRAFT EXPERIENCED AN UNCOMMANDED NLG EXTENSION DURING FLIGHT. NOSE GEAR LOCKED DOWN. WHEN SELECTED, BOTH MAINS LOCKED DOWN WITHOUT DIFFICULTY. UPON LANDING, EXAMINATION DETERMINED THE NOSE GEAR ACTUATOR ROD END HAD BROKEN IN THE SECOND THREAD FROM THE HEAD (BALL END). PREVIOUS CRACK WAS EVIDENCED. 1L71 3O A3SO 19950818000741995081800074SO 1995 8 18 95ZZZX4016 119950726A3230AN625 BOLT PIPER PA28 PA28R180 7102809SO NLG DRAG LINK MISINSTALLED A DTEAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL254590J 28R30463 CONTRARY TO AC 43-16 ALERT, JUNE, 1993 ISSUE AND PSB SM, FIGURE 7A-2, THE UPPER NOSE GEAR DRAG LINK TO ENGINE MOUNT ATTACHMENT BOLTS WERE INSTALLED BACKWARDS AND WASHER ARRANGEMENT INCORRECT. 1L71 3O 2A13 19950818000931995081800093NE 1995 8 18 95ZZZX4035 219950713A725070BM031070 MODULE 3 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL0526492902 289 1066 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. 1G71 3U3 U H9EU E19EU 19950818000941995081800094EU 1995 8 18 95ZZZX4036 119950703A2913704A3410006 PUMP SNIAS 350 AS350B 8680801EU HYD SHAFT SHEARED A ILNAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP133610T 1279 DURING CHECK RIDE, AIRCRAFT EXPERIENCED LOSS OF HYDRAULIC POWER. INSPECTED HYDRAULIC SYSTEM, FOUND SHEARED HYDRAULIC PUMP SPLINED SHAFT TO PULLEY. REMOVED AND REPLACED HYDRAULIC PUMP. 1G71 3U H9EU 19950818000981995081800098NE 1995 8 18 95ZZZX4040 219950604A725070BM035400 MODULE 3 SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL056052C1408 9253 2586 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. 1G71 3U3 U H9EU E19EU 19950818000991995081800099NE 1995 8 18 95ZZZX4041 219950713A725070BM031070 MODULE 3 SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL056080R1306 128 2685 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. 1G71 3U3 UNCH9EU E19EU 19950818001001995081800100NE 1995 8 18 95ZZZX4042 219950531A725070BMO31070 MODULE 3 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL056015S2053 809 1884 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. SECOND OCCURRENCE IN 300 HOURS. 1G71 3U3 U H9EU E19EU 19950818001011995081800101NE 1995 8 18 95ZZZX4043 219950710A725070BMO31070 MODULE 3 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL05579551386 772 1538 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. 1G71 3U3 U H9EU E19EU 19950818001021995081800102NE 1995 8 18 95ZZZX4044 219950719A725070BMO31070 MOUDLE 3 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL05579582394 772 1512 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRES DISASSEMBLY AND CLEANING. 1G71 3U3 U H9EU E19EU 19950818001031995081800103WP 1995 8 18 USAA950606 119950614A3244 TIRE DOUG DC9 DC931 3022065WP LT MLG FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19937VJ 48117 DCA-BWI - FLT 1178 - THE LT MAIN TIRE BLEW ON TAKEOFF, FLIGHT DIVERTED DUE TO THE GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT O/B WHEEL ASSEMBLY (P/N 3910063507. SPIN CHECKS GOOD. (W) 2L72 4F A6WE 19950818001041995081800104WP 1995 8 18 USAA950616 119950621A793142D1091A OIL PRESS SW DOUG DC9 DC931 3022065WP NR 1 ENGINE LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19984VJ 47207 BUF - FLT 1463 - CAPTAIN RECEIVED AN OIL STRAINER CLOG LIGHT, IT DID NOT EXTINGUISH WHEN THE ENGINE WAS THROTTLED BACK TO IDLE. THE LT ENGINE WAS THEN SHUTDOWN AND THE FLIGHT DIVERTED TO BUF. FLIGHT LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 14 MINUTES. MAINTENANCE REPLACED THE NR 1 ENGINE OIL PRESSURE DIFFERENTAIL PRESSURE SWITCH. LEAK CHECKED NORMAL. (W) 2L72 4F A6WE 19950818001051995081800105WP 1995 8 18 USAA950619 119950624A2130 PRESSURIZATION DOUG DC9 DC981 3022081WP CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19801US 48037 CLT - FLT 514 - ON TAKEOFF, THE AC FAILED TO PRESSURIZE. FLIGHT RETURNED TO CLT. MAINTENANCE PERFORMED BITE CHECKS ON THE CONTROLLERS. ALL CHECKED GOOD. (W) 2L72 4F A6WE 19950818001061995081800106WP 1995 8 18 USAA950620 119950616A5313 LONGERON DOUG DC9 DC931 3022065WP BS 680 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19955VJ 47593 IND - DURING SCHEDULED SID INSPECTION REF: PSE 53.09.009 AND 53.09.010, FOUND A 1 INCH CRACK IN LONGERON 3L AT STATION 680. CUT OUT DAMAGE AND INSTALLED SPLICE REPAIR PER USAIR EA 39338 AND SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950818001071995081800107WP 1995 8 18 USAA950627 119950527A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1076 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA STR 1076 LONGERON 14R ON BELTFRAME. BLENDED OUT CHAFED AREA, TREATED/PRIME, INSTALLED DOUBLER REPAIR UNDER FLANGE PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950818001081995081800108WP 1995 8 18 USAA950628 119950528A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1059 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA AT STA 1059 LONGERON 20R ON BELTFRAME. BLENDED OUT AREA, TREATED AND PRIMED INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950818001091995081800109WP 1995 8 18 USAA950629 119950525A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1059 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2.5 INCH CHAFED AREA AT STA 1059 LONGERON 14R BELTFRAME. BLENDED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950818001101995081800110WP 1995 8 18 USAA950636 119950515A5320591014211 JAMB DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION TO FWD CARGO DOOR JAMB WEB FWD LOWER CORNER AT STA 362.500 CPCP TASK C51-53300. CUT OUT CORRODED AREA AND INSTALLED NEW SECTION OF WEB AND INSTALLED DOUBLER PER USAIR EA 30429. (W) 2L72 4F A6WE 19950818001111995081800111WP 1995 8 18 USAA950641 119950523A53201719673 ANGLE DOUG DC9 DC931 3022065WP BS 255 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 6 INCH AREA PANEL NR 20 IN SUPPORT ANGLE AT STA 255, CENTER LINE, AREA PREVIOUSLY REWORKED. CPCP TASK NR C58-53303. SPLICED IN NEW SECTION OF ANGLE PER USAIR TYPICAL REPAIR 53-10-21A. (W) 2L72 4F A6WE 19950818001121995081800112WP 1995 8 18 USAA950672 119950525A5330 SKIN DOUG DC9 DC981 3022081WP BS 465-484 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK BETWEEN STA 465 AND 484 LONGERON 24R TO 25R SKIN. CUT OUT DAMAGED SKIN AND INSTALLED A FLUSH REPAIR PER USAIR EA 30543. (W) 2L72 4F A6WE 19950818001131995081800113WP 1995 8 18 USAA950673 119950525A5330 SKIN DOUG DC9 DC981 3022081WP BS 389-408 LIGHTNING STRIKEA USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LIGHTNING STRIKES FROM STA 389 TO 408 BETWEEN LONGERONS 28R AND 29R SKIN. INSTALLED INTERNAL DOUBLERS 4 INCH BY 6.5 AND 4 INCHES BY 8 INCHES PER SRM 53-04 VIEW E. (W) 2L72 4F A6WE 19950818001141995081800114WP 1995 8 18 USAA950674 119950525A5320 JAMB DOUG DC9 DC981 3022081WP CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AFT CARGO DOOR JAMB BEAM. PREVIOUS REWORK, CPCP TASK C57-53300. SPLICED IN NEW JAMB BEAM SECTION PER SRM 53-05 FIG 63. (W) 2L72 4F A6WE 19950818001151995081800115WP 1995 8 18 USAA950675 119950525A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 313-370 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION BETWEEN STA 313 TO 370 RT I/B SEAT TRACK, PREVIOUS REWORK. CPCP TASK C58-53306. CUT OUT CORRODED AREA AND SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG L/F. (W) 2L72 4F A6WE 19950818001161995081800116WP 1995 8 18 USAA950676 119950525A53475936663501 TIE DOWN RAIL DOUG DC9 DC981 3022081WP BS 1007-1155 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION BETWEEN STA 1007 TO 1155 RT TIE DOWN RAIL IN AFT CARGO, PREVIOUS REWORK. CPCP TASK C57-53300. SPLICED IN NEW SECTION OF TIE DOWN RAIL PER USAIR TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950818001171995081800117WP 1995 8 18 USAA950677 119950525A5347 TIE DOWN TRACK DOUG DC9 DC981 3022081WP BS 1155-1211 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AFT CARGO LT SIDE BETWEEN STA 1155 TO 1211, PREVIOUS REWORK. CPCP TASK C57-53300, TIE DOWN TRACK. CUT OUT CORRODED AREA, INSTALLED FILLER AND DOUBLER PER USAIR TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950818001181995081800118WP 1995 8 18 USAA950678 119950525A5347 TIE DOWN RAIL DOUG DC9 DC981 3022081WP BS 655-712 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECITON, FOUND LEVEL 1 CORROSION BETWEEN STA 655 TO 712 LT SIDE TIE DOWN RAIL FWD CARGO. PREVIOUS REWORK NOT A CPCP TASK. CLEANED CORROSION AND INSTALLED DOUBLER REPAIR STRAP PER USAIR TYPICAL REPAIR 53-20-09A. (W) 2L72 4F A6WE 19950818001191995081800119WP 1995 8 18 USAA950679 119950525A5320 JAMB DOUG DC9 DC981 3022081WP FWD CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION FWD CARGO DOOR JAMB PAN. CORROSION TASK NR C51-53300, PREVIOUSLY REWORKED. REMOVED CORROSION AND SPLICED IN NEW SECTION OF PAN PER SRM 53-05 FIG 44. (W) 2L72 4F A6WE 19950818001201995081800120WP 1995 8 18 USAA950680 119950525A5347 TIE DOWN RAIL DOUG DC9 DC981 3022081WP BS 617-655 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT CARGO TIE DOWN RAIL STA 617 TO 655 LONGERON 28L. CORROSION TASK C51-53300. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-20-09 FIG 1. (W) 2L72 4F A6WE 19950818001211995081800121WP 1995 8 18 USAA950681 119950525A5320 FLANGE DOUG DC9 DC981 3022081WP BS 1380-1401 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION BETWEEN STA 1380 AND 1401 LONGERON 25R TO LONGERON 30 TAIL INTERIOR FLANGE. CORROSION TASK C58-53301. REMOVED CORROSION AND INSTALLED REPAIR ANGLE DOUBLERS PER SRM 53-01 FIG 2. (W) 2L72 4F A6WE 19950818001221995081800122WP 1995 8 18 USAA950682 119950525A5315991556171 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT FLOORBEAM TOP FLANGE RT LAV STA 1338 CORROSION TASK NR C58-53300. REMOVED AND REPLACED TOP FLOOR ANGLE AND INSTALLED BEAM SPLICE PER USAIR TYPICAL REPAIR 53-10-14. (W) 2L72 4F A6WE 19950818001231995081800123WP 1995 8 18 USAA950684 119950525A531599581883 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AROUND 2 HOLES IN FLOORBEAM RT LAV. CORROSION TASK NR C58-53300. REMOVED CORROSION AND INSTALLED FILLER, STRAP AND ANGLE REPAIR PER USAIR TYPICAL REPAIR 53-10-19. (W) 2L72 4F A6WE 19950818001241995081800124WP 1995 8 18 USAA950685 119950525A5315 FLOORBEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION IN FLOORBEAM WEB AT STA 1338 RT O/B. CORROSION TASK C58-53305. CUT OUT CORRODED AREA AND INSTALLED WEB REPAIR PER SRM 53-05 FIG 79 SHT 1. (W) 2L72 4F A6WE 19950818001251995081800125WP 1995 8 18 USAA950686 119950525A5320 WINDOW PAN DOUG DC9 DC981 3022081WP BS 902 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .5 INCH CRACK IN LOWER WINDOW PAN STA 902 RT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (W) 2L72 4F A6WE 19950818001261995081800126WP 1995 8 18 USAA950687 119950525A5330 SKIN DOUG DC9 DC981 3022081WP BS 845 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND BURNISH MARK, GOUGED .18 INCH DEEP AT STA 945 LONGERON 9R IN SKIN. INSTALLED DOUBLER INTERNAL REPAIR PER SRM 53-04 FIG 38. (W) 2L72 4F A6WE 19950818001271995081800127WP 1995 8 18 USAA950688 119950525A5311 BELTFRAME DOUG DC9 DC981 3022081WP BS 1322 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND BELTFRAME CRACKED .75 INCH LONG AT STA 1332 LONGERON 17L. REMOVED CRACKED SECTION OF BELTFRAME AND SPLICED PER SRM 53-03 FIG 32. (W) 2L72 4F A6WE 19950818001281995081800128WP 1995 8 18 USAA950689 119950525A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 200/248 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND SEAT TRACK AT STA 200 AND 248 RT O/B WORN BEYOND LIMITS PER SRM 53-05 FIG 4B. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (W) 2L72 4F A6WE 19950818001291995081800129WP 1995 8 18 USAA950690 119950525A5320 DOOR JAMB DOUG DC9 DC981 3022081WP BS 210 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND CRACK 1.5 INCH LONG AT STA 210 AND LONGERON 15L IN DOOR JAMB MEMBRANE WEB. CUT OUT DAMAGED WEB AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 53-01 FIG 2 SHT 4. (W) 2L72 4F A6WE 19950818001301995081800130WP 1995 8 18 USAA950691 119950525A5313 LONGERON DOUG DC9 DC981 3022081WP BS 237 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND CRACK .75 INCH AT STA 237 ON LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950818001311995081800131WP 1995 8 18 USAA950692 119950525A53305911409 SKIN DOUG DC9 DC981 3022081WP BS 229-246 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND SKIN DENTED AND DAMAGED BEYOND LIMITS BETWEEN STA 229 AND 246 LONGERONS 15L AND 18L. CUT SKIN PANEL AND SPLICED IN NEW SECTION PER SRM 53-04 FIG 6 AND USAIR EA 30336. (W) 2L72 4F A6WE 19950818001321995081800132WP 1995 8 18 USAA950693 119950525A5313 LONGERON DOUG DC9 DC981 3022081WP BS 408 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .625 INCH CRACK STA 408 ON LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (W) 2L72 4F A6WE 19950818001331995081800133WP 1995 8 18 USAA950694 119950525A5330 SKIN DOUG DC9 DC981 3022081WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.25 INCH CRACK STA 1437 LT SIDE BELOW LONGERON 3L IN FUSELAGE SKIN. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (W) 2L72 4F A6WE 19950818001341995081800134WP 1995 8 18 USAA950695 119950525A5400 ANGLE DOUG DC9 DC981 3022081WP BS 1480 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK IN THE STA 1480 UPPER PYLON ATTACH ANGLE RT SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER TO ANGLE PER SRM 54-04 FIG 10 SHT 3. (W) 2L72 4F A6WE 19950818001351995081800135WP 1995 8 18 USAA950696 119950525A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1463 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.5 INCH CRACK AT STA 1463 LT SIDE VERTICAL STAB TO FUSELAGE ATTACH ANGLE. CUT OUT CRACKED SECTION OF ANGLE, INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-05 FIG 23A AND USAIR EA NR 19449. (W) 2L72 4F A6WE 19950818001361995081800136WP 1995 8 18 USAA950697 119950525A5312 BLKHD ANGLE DOUG DC9 DC981 3022081WP BS 1338 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK IN ANGLE AT STA 1338 TOP CENTER OF AFT PRESSURE BULKHEAD FWD SIDE. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER SRM 53-01 PG 9. (W) 2L72 4F A6WE 19950818001371995081800137WP 1995 8 18 USAA950698 119950525A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1401/1418 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND HOLE CHAFED IN LONGERON 8R AT STA 1401 AND 1418. CUT OUT CHAFED SECTION AND INSTALLED NEW SECTION OF LONGERON. SPLICED PER USAIR TYPICAL REPAIR 53-10-17. (W) 2L72 4F A6WE 19950818001381995081800138WP 1995 8 18 USAA950699 119950525A5330 SKIN DOUG DC9 DC981 3022081WP BS 1380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .3125 INCH CRACK STA 1380 LT SIDE ABOVE LONGERON 14L IN FUSELAGE SKIN. CUT OUT AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 18. (W) 2L72 4F A6WE 19950818001391995081800139WP 1995 8 18 USAA950724 119950630A2150SRL92E INDICATOR DOUG DC9 DC981 3022081WP RT PACK INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19805US 48053 PHL - FLT 260 - AFTER TAKEOFF, THE RT AIR CONDITIONING PACK FAILED CAUSING THE AC TO LOSE PRESSURIZATION. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE RT AIR CONDITIONING SUPPLY PRESSURE INDICATOR SYSTEM. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950818001401995081800140WP 1995 8 18 USAA950753 119950710A2913 PUMP DOUG DC9 DC981 3022081WP RIGHT LEAKING A USAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19805US 48053 IND - FLT 977 - AT FL 350, THE RT HYDRAULIC PRESSURE LIGHT ILLUMINATED AND THE HYDRAULIC QUANTITY DROPPED TO ZERO. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN IND. MAINTENANCE REPLACED THE HYDRAULIC PUMP AND FILTERS. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950818001411995081800141NE 1995 8 18 95ZZZX4045 319950801A61124E30171 DEICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RT PROPELLER MISSING A JJBAK NONE O OTHER DEDESCENT 1 EA01855CA1958 UE61 HJ188A RIGHT PROPELLER MISSING DEICE BOOT BLADE, S/N UNKNOWN. FURTHER INSPECTION FOUND 3 SEPARATE CRACKS IN LEADING EDGE OF 2 BLADES, S/N UNKNOWN. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL. 2L72 4T RTA24CE 5 CP10NE 19950818001421995081800142CE 1995 8 18 95ZZZX4046 119950725A261224409015 FIRE LOOP BEECH 1900 1900C 1154161CE RT ENGINE BROKEN A AMWAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 CE07163AM UC163 FLT 5626 - ON CLIMB-OUT, THE RIGHT FIRE WARNING ILLUMINATED, PULLED FIRE T-HANDLE AND LIGHT EXTINGUISHED. RETURNED TO FIELD ON LEFT ENGINE. MAINTENANCE FOUND AFT FIRE LOOP BROKEN, REPLACED LOOP, OPS CHECKED NORMAL. 2L72 4T RTA24CE 19950818001431995081800143NE 1995 8 18 95ZZZX4047 219950802A73203031829 AIR SENSE LINE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE RT ENGINE FAILED A MASAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0142YV 6682 UE42 114050 LAX/SMX - AIRCRAFT DEPARTED. APPROXIMATELY 10 MINUTES INTO FLIGHT AT 10,000 FEET, RT ENGINE STARTED TO SURGE IN POWER AND TORQUE DROPPED TO ZERO WITHIN 10 SECONDS. ALL OTHER PARAMETERS NORMAL. FLIGHT CREW SECURED RIGHT ENGINE AND DIVERTED TO BFL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED RT ENGINE AND FOUND P4 LINE TO P3 FILTER BROKEN. INSTALLED NEW P4 LINE. PERFORMED GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA24CE E26NE 19950818001441995081800144EA 1995 8 18 95ZZZX4048 219950704A7250 GAS GENERATOR BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE FAILED A AMWAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE07119YV1588451 UC119 GG97316 MCI/SLN - EN ROUTE, LEFT ENGINE FAILED AND CREW DIVERTED TO FOE. REMOVED AND REPLACED GAS GENERATOR AND POWER SECTION. GG TSO 51 HRS., 15,884 TT, PS S/N 32472, TSSV 1602, TT 8781. HSK S/N 72A912. TSN 1667, TSSV 1602. TEAR DOWN REPORT SHOWED NR 1 BEARING HAD FAILED. INSPECTED AIRCRAFT FOR LIGHTNING STRIKE, NONE WAS FOUND. 2L72 4T4 TRTA24CE E4EA 19950818001451995081800145EA 1995 8 18 95ZZZX4049 219950623A7250 GAS GENERATOR BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE FAILED A AMWAAE UNSCHED LANDING ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE07119YV10001 UC119 32573 FLT 5630 - CREW REPORTED SMOKE IN COCKPIT FOLLOWED BY LT ENGINE OIL LIGHT. CREW SHUT DOWN LEFT ENGINE AND RETURNED TO FIELD AT FYV. REMOVED AND REPLACED ENGINE. RECORDS SHOWED ENGINE HAD 54 HOURS SINCE IT CAME OUT OF SHOP FOR REAR HUB REPLACEMENT. GAS GENERATOR HAD 2528 T.S.S.V. TEAR DOWN REPORT STATED NR 1 BEARING HAD FAILED. 2L72 4T4 TRTA24CE E4EA 19950818001461995081800146EA 1995 8 18 95ZZZX4050 219950614A7250 GAS GENERATOR BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE SEIZED A AMWAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE07119YV UC119 32026 FYV - FLT 5635 - ON CLIMB AFTER TAKEOFF, LEFT ENGINE SHUT DOWN MAINTENANCE, FOUND POWER SECTION AND GAS GENERATOR SEIZED. REMOVED AND REPLACED GAS GENERATOR AND POWER SECTION. POWER SECTION HAD 2533 HOURS SINCE SHOP VISIT. GAS GENERATOR HAD 75 HOURS SINCE SHOP VISIT. AT TEAR DOWN, NR 1 BEARING FOUND TO HAVE FAILED. 2L72 4T4 TRTA24CE E4EA 19950818001471995081800147NM 1995 8 18 95ZZZX4051 119950621A33501000677 EEL BOEING727 727227 1384078NM R-2 DOOR INOPERATIVE A MZZAK NONE L NO TEST ININSP/MAINT 1 WP13864266000 21364 GUM - THE R-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING B-CHECK. THE R-2 DOOR EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED PER MM 33-50-101 AND OPERATION CHECKED GOOD. 2L73 4F A3WE 19950818001491995081800149NM 1995 8 18 BJNA95701 119950721A33506104791 EEL BATTERY PACK BOEING737 737214 138446RNM CABIN DISCHARGED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11457TM 7959 20156 RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY UNIT IAW BMM 33-51-31, OPS CHECKS OK. THIS CLEARS DMI NR 073. (X) 2L72 4F A16WE 19950818001501995081800150WP 1995 8 18 CKSA95083 119950704A2910AN818 B-NUT DOUG DC8 DC861 3021952WP NR 2 ENGINE LOOSE A CKSAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL23817CK49543 45887 SFO - ON TAKEOFF, HYDRAULIC CAME DOWN AND GEAR TOOK LONGER THAN NORMAL TO RETRACT. CONTINUED TO CLIMB OUT, THE HYD FLUID LEVEL CONTINUED TO COME DOWN CONFIRMING A LOSS OF HYD FLUID OR PRESS. CHECKLIST, THE LOSS STOPPED. DECLARED A HYD EMERGENCY, DUMPED FUEL. HYD FLUID STAYED ABOVE STANDPIPE AND AUXILIARY PUMP PRESSURE WAS NORMAL. FOUND LOOSE B-NUT AT PRESSURE OUTLET OF NR 2 ENG DRIVEN PUMP, RESECURED B-NUT, SERVICED RESERVOIR IAW DC-8 MM CHAPTER 12-30-1, BLEED HYD SYSTEM, RAN NR 2 AND NR 3 ENGINES. NO LEAKS NOTED AT THIS TIME. (X) 2L74 4F 4A25 19950818001511995081800151WP 1995 8 18 CKSA95085 119950711A2612244E54G210 FIRE LOOP DOUG DC8 DC8F55 3021928WP NR 4 ENGINE FAILED A CKSAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 GL236161C55829 45856 EINN - FIRE INDICATION ON NR 4 ENGINE AFTER TAKEOFF. SHUT ENGINE DOWN IAW F.O.M. SHOT BOTH FIRE AGENT BOTTLES ON RIGHT WING, FIRE INDICATION CONTINUED, RETURNED TO AIRPORT. REMOVED AND REPLACED FORWARD OUTBOARD FIRE LOOP PER DC-8 MM 26-2-1. FIRE LOOP OPS CHECKS GOOD PER DC-8 MM 26-2-0. REMOVED AND REPLACED BOTH RIGHT WING BOTTLES PER DC-8 MM 26-4-1. (X) 2L74 4F 4A25 19950818001521995081800152WP 1995 8 18 CKSA95088 119950711A3260 CONNECTOR DOUG DC8 DC863 302198AWP NOSE GEAR UNSECURED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23781AL79529 45926 KTOL - UPLATCH CHECK FAILED, DOORS NOT LATCHED LIGHT ON IN UPLATCH AND WITH GEAR UP. ABNORMAL PROCEDURES COMPLIED WITH. FOUND NOSE GEAR LOCK SWITCH CONNECTOR NOT SECURED. CLEANED AND RESECURED CANNON PLUG. OPS CHECK GOOD ON GROUND IAW MM CHAPTER 32. NO DEFECTS NOTED DURING GEAR SWING. (X) 2L74 4F 4A25 19950818001531995081800153NE 1995 8 18 GRAA9539 219950718A72617584654 OIL FILTER DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE NR 2 ENGINE DIRTY A GRAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP111075T 49724 718220 ON JULY 18, 1995, AIRCRAFT N1075T BLOCKED OUT AT IFP AIRPORT AND AT STATIC ENGINE RUN-UP THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. AIRCRAFT N1075T RETURNED TO THE RAMP WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND INSTALLED A NEW OIL FILTER ON NR 2 ENGINE. MAINTENANCE PERFORMED AN OPERATIONAL AND LEAK CHECK OF NR 2 ENGINE. NR 2 ENGINE OPERATED NORMALLY, NO DEFECTS NOTED. AIRCRAFT N1075T WAS RETURNED TO SERVICE. (X) 2L72 4F4 FRTA6WE E9NE 19950818001541995081800154NM 1995 8 18 IXKA9500023 119950726A2913371380 HYDRAULIC PUMP VICKERS 371380 BOEING727 727251 138408HNM NR 1 ENGINE FAILED A IXKAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 EA25264US MX351237 19983 TPA/ATL - FLT 59 - IN-FLIGHT, LOST A-HYDRAULIC FLUID. AIRCRAFT RETURNED TO TPA. REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND FILTERS. OPS CHECK AND RAN NR 1 ENGINE, CHECK OK PER MM 29-11-33. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP AND FILTERS, PRECAUTIONARY, AND OPS CHECK OK PER MM 29-11-33. (X) 2L73 4F A3WE 19950818001551995081800155NE 1995 8 18 IXXA199568 219950725A73149477 FUEL PUMP DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 2 ENGINE LOW OUTPUT A IXXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 GL23786AL 10650 46121 671244 HUF - DURING DESCENT AT AROUND 10,000 FEET, NR 3 ENGINE FLAMED OUT. ENGINE SHUT-DOWN PROCEDURES WERE ACCOMPLISHED. ON THE GROUND IN HUF, DETERMINED THE ENGINE WOULD LIGHT OFF, BUT HANG AT AROUND 40 PERCENT N2 RPM. TROUBLESHOOTING INDICATED THE OUTPUT OF THE ENGINE DRIVEN FUEL PUMP WAS INSUFFICIENT. THE ENGINE DRIVEN FUEL PUMP WAS REPLACED, AND ENGINE OPERATION RETURNED TO NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F4 F 4A25 1E8 19950818001561995081800156WP 1995 8 18 IXXA199569 119950725A3040 WINDSHIELD DOUG DC8 DC863F 302198FWP COCKPIT SMOKE ODOR A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23784AL 46135 KNGU/BIKF - BETWEEN KNGU AND BIKE, AN ELECTRICAL SMELL AND A SMALL AMOUNT OF SMOKE WERE NOTED COMING FROM THE FIRST OFFICER'S WINDSHIELD AREA. IN KNGU, NO SOURCE COULD BE DETERMINED FOR THE SMELL. THE WINDSHIELD HEAT WAS DEFERRED AS A PRECAUTION FOR FURTHER TROUBLESHOOTING. (X) 2L74 4F 4A25 19950818001571995081800157WP 1995 8 18 SRAA79503 119950708A2612 FIRE CONNECTOR DOUG DC8 DC873F 302199FWP NR 3 ENGINE DIRTY A SRAAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO19873SJ 46091 DUBAI - FLT 192 - DURING FLIGHT, NR 4 ENGINE FIRE AURAL WARNING CAME ON, SHUT DOWN ENGINE AND WARNING LIGHT EXTINGUISHED. WHEN FIRE HANDLE WAS PULLED DOWN, NR 4 ENGINE SHORT CIRCUIT LIGHT CAME ON, AIRCRAFT LANDED IN DUBAI WITHOUT INCIDENTS. INSPECTED NR 4 ENGINE, FOUND NO FIRE OCCURRED. INSPECTED FIRE LOOP, FOUND EVIDENCE OF OIL AT CANNON PLUG, REMOVED OIL AND OPS CHECKED GOOD. (X) 2L74 4F RT4A25 19950818001581995081800158SO 1995 8 18 SRAA79508 119950717A3244 TIRES LKHEED382 382G 526414USO NLG BAD A SRAACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 SO19909SJ 4763 CHS - FLT ADY1 - ON TAKEOFF AT 60 KNOTS, EXPERIENCED NOSE WHEEL SHIMMY. AT 80 KNOTS, TAKEOFF WAS REJECTED. FOUND BOTH NOSE WHEEL TIRES WERE BAD. REPLACED BOTH NOSE WHEEL ASSEMBLIES, OPS CHECKED PER MM, CHAPTER 32. (X) 2H74 4T A1SO 19950818001591995081800159GL 1995 8 18 SRAA79509 219950718A7320670854 ROD END LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 3 ENGINE BROKEN A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19909SJ 4763 CHARLESTON - FLT ADY2 - DURING FLIGHT, NR 3 ENGINE WENT TO FULL POWER HIGH, FUEL FLOW, T.I.T., AND TORQUE WOULD NOT RESPOND TO THROTTLE MOVEMENT. SHUT DOWN NR 3 ENGINE. FOUND ROD END AT COORDINATOR TO FUEL CONTROL UNIT SEPARATED FROM ROD. REPLACED ROD ASSEMBLY AND RIGGED UNIT. OPS CHECKED GOOD PER MM, CHAPTER 73. (X) 2H74 4T4 T A1SO E282 19950818001601995081800160SO 1995 8 18 SRAA79510 119950718A3230 RETRACT MECH LKHEED382 382G 526414USO RT MLG LACK OF LUBE A SRAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19921SJ 4586 ANC - FLT 1951 - AFTER TAKEOFF, RT MLG WOULD NOT COME UP WHEN HANDLE SELECTED TO RETRACT POSITION. COMPLETED AIR TURN BACK TO ANC. JACKED UP AIRCRAFT, FOUND DIRT ACCUMULATED ON BALLSCREWS, REMOVED DIRT, ADJUSTED FORWARD LOWER SHOES, RIGHT AFT LOWER AND UPPER SHOES, LUBED FORWARD AND AFT BALLSCREWS. OPS CHECKED GOOD DURING RETRACTION TEST. (X) 2H74 4T A1SO 19950818001611995081800161NE 1995 8 18 TAOA07903 219950725A7314243600 FUEL PUMP BOEING727 727225 1384077NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE FAILED A TAOAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 EA15918TS 2339 9573 20445 655361 BOSTON - NR 3 ENGINE SHUT DOWN ON TAKEOFF AT 375 FEET AGL. RETURNED TO BOSTON TO GATE. WINDMILLING OIL PRESSURE - 20 PSI FOR 14 MINUTES. REPLACED NR 3 FUEL PUMP PER MM 73-11-1 - NORMAL RUN. FUEL PUMP SHAFT SHEARED. FUEL CONTROL UNIT CHANGED - PRECAUTIONARY. (X) 2L73 4F4 F A3WE E2EA 19950818001621995081800162WP 1995 8 18 USAA950655 119950526A5330 SKIN DOUG DC9 DC931 3022065WP BS 89 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 EACH, .1250 INCH CRACKS IN FUSELAGE SKIN AT STA 89 NEAR RT NOSE GEAR DOOR. INSTALLED MFG NEW SKIN REPAIR PER SRM 53-01, FIGURE 2, SHEET 3. (X) 2L72 4F A6WE 19950818001631995081800163WP 1995 8 18 USAA950656 119950526A5330 SKIN DOUG DC9 DC931 3022065WP BS 100 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .1875 INCH CRACK IN FUSELAGE SKIN AT STA 100 AFT OF RT NOSE GEAR DOOR AFT HINGE. INSTALLED MFG NEW SKIN AND INSTALLED REPAIR PER SRM 53-01, FIGURE 2, SHEET 3. (X) 2L72 4F A6WE 19950818001641995081800164WP 1995 8 18 USAA950657 119950601A5313 LONGERON DOUG DC9 DC931 3022065WP BS 965 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION FOUND .1250 INCH CRACK IN RIGHT NAV LONGERON 17R STA 965. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (X) 2L72 4F A6WE 19950818001651995081800165WP 1995 8 18 USAA950658 119950601A5531 RIB DOUG DC9 DC931 3022065WP VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK AT VERTICAL STAB L.E. BOTTOM 7TH RIB. INSTALLED NESTED DOUBLER REPAIR PER SRM 55-01. (X) 2L72 4F A6WE 19950818001661995081800166WP 1995 8 18 USAA950659 119950601A5313 LONGERON DOUG DC9 DC931 3022065WP BS 639 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L AT STA 637. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2. (X) 2L72 4F A6WE 19950818001671995081800167WP 1995 8 18 USAA950660 119950601A5312 BLKHD ANGLE DOUG DC9 DC931 3022065WP BS 996 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK TOP C/L ANGLE ABOVE AFT PAX ENTRY DOOR ON FWD SIDE OF PRESSURE DOME, STA 996. INSTALLED ANGLE AND DOUBLER REPAIR PER SRM 53-01, FIGURE 2. (X) 2L72 4F A6WE 19950818001681995081800168WP 1995 8 18 USAA950661 119950601A532099234847 WEB DOUG DC9 DC931 3022065WP BS 180 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND 12 INCH CRACK IN STA 180 WEB 9923484-7. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER DAC DWG 9923484. (X) 2L72 4F A6WE 19950818001691995081800169WP 1995 8 18 USAA950662 119950601A5320 BELT BEAM DOUG DC9 DC931 3022065WP BS 107 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 CRACKS, .1250 INCH EACH, IN STA 207, LT SIDE TOP OF BOTTOM WINDOW BELT BEAM. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 36. (X) 2L72 4F A6WE 19950818001701995081800170WP 1995 8 18 USAA950663 119950601A5320 MEMBRANE DOUG DC9 DC931 3022065WP BS 617 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND 2 INCH CRACK IN CUSP MEMBRANE, STA 617, LONGERON 18L. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X) 2L72 4F A6WE 19950818001711995081800171WP 1995 8 18 USAA950664 119950601A5313 LONGERON DOUG DC9 DC931 3022065WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L, STA 160. INSTALLED SPLICE REPAIR OF LONGERON PER SRM 53-02, FIGURE 2, VIEW BB. (X) 2L72 4F A6WE 19950818001721995081800172WP 1995 8 18 USAA950665 119950601A5320 SUPPORT DOUG DC9 DC931 3022065WP BS 237 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND CORROSION, STA 237, FLOOR SUPPORT CENTER, LT SIDE. FABRICATED NEW SUPPORT AND SPLICED IN ANGLE REPAIR PER USAIR TYPICAL REPAIR 53-10-21A. (X) 2L72 4F A6WE 19950818001731995081800173WP 1995 8 18 USAA950666 119950601A5320 CLIP DOUG DC9 DC931 3022065WP BS STA 598 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN FORWARD CARGO FLOOR SUPPORT CLIP, STA 598, LONGERON 27L. MFG NEW CLIP AND INSTALLED PER SRM 53-01. (X) 2L72 4F A6WE 19950818001741995081800174WP 1995 8 18 USAA950667 119950601A5320 MEMBRANE DOUG DC9 DC931 3022065WP BS 596 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN CUSP MEMBRANE, STA 596, LONGERON 18R. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X) 2L72 4F A6WE 19950818001751995081800175WP 1995 8 18 USAA950668 119950601A5400 ANGLE DOUG DC9 DC931 3022065WP BS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LEFT PYLON TOP ATTACH ANGLE AT STA 980. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 54-04, FIGURE 10. (X) 2L72 4F A6WE 19950818001761995081800176WP 1995 8 18 USAA950669 119950601A5320 PAN DOUG DC9 DC931 3022065WP BS 180-205 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION FOUND LEVEL 1 CORROSION AT GALLEY FLOOR PAN, STA 180 TO STA 205, RT SIDE, PREVIOUS REWORK. REF: CRCP TASK C46-53303. INSTALLED NEW SECTION OF FLOOR SUB-PAN PER SRM 53-01. (X) 2L72 4F A6WE 19950818001771995081800177WP 1995 8 18 USAA950670 119950601A5320 ANGLE DOUG DC9 DC931 3022065WP BS 983 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19983VJ32966 48159 PIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL 1 CORROSION CPCP TASK NR C58-53300, LT LAV THRESHOLD ANGLE, STA 983, PREVIOUS REWORK. INSTALLED DOUBLER REPAIR PER SRM 53-01. (X) 2L72 4F A6WE 19950818001781995081800178WP 1995 8 18 USAA950671 119950525A5320 MEMBRANE DOUG DC9 DC981 3022081WP BS 1287-1367 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.75 INCH CRACK, STA 1287 - STA 1367, RT SIDE CUSP MEMBRANE. CUT OUT SECTION OF CUSP MEMBRANE AND INSTALLED SPLICE REPAIR PER SRM 53-05, FIGURE 97. (X) 2L72 4F A6WE 19950818001791995081800179WP 1995 8 18 USAA950700 119950525A5330 SKIN DOUG DC9 DC981 3022081WP FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH CRACK FWD UPPER CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY). INSTALLED EXTERNAL DOUBLER AND FILLER REPAIR PER SRM 53-05, FIGURE 25A AND USAIR, EA 30427. (X) 2L72 4F A6WE 19950818001801995081800180WP 1995 8 18 USAA950701 119950525A5730 SKIN DOUG DC9 DC981 3022081WP RT WING LE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US3757537575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .6250 INCH CRACK IN RT WING LEADING EDGE OUTBOARD OF VORTILON. STOP DRILLED CRACK AND INSTALLED DOUBLER AND SUPPORT ANGLE REPAIR PER SRM 57-068, FIGURE 9. (X) 2L72 4F A6WE 19950818001811995081800181WP 1995 8 18 USAA950702 119950525A5320 INTERCOSTAL DOUG DC9 DC981 3022081WP BS 886/905 MISDRILLED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND INTERCOSTAL AND DOUBLER MISDRILLED AT STA 886 AND STA 905, LONGERON 16L. FABRICATED AND HEAT TREATED NEW SECTION OF INTERCOSTAL AND INSTALLED DOUBLERS PER SRM 53-01, SRM 51-10-2A. (X) 2L72 4F A6WE 19950818001821995081800182WP 1995 8 18 USAA950703 119950525A5313 LONGERON DOUG DC9 DC981 3022081WP BS 237-427 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACKS AT ATTACH POINTS IN LONGERON 17L AT STA 237, 256, 275, 294, 313, 332, 370, AND 427. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2A. (X) 2L72 4F A6WE 19950818001831995081800183WP 1995 8 18 USAA950704 119950525A5320 PAN DOUG DC9 DC981 3022081WP BS 946 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN UPPER FWD CORNER OF WINDOW PAN AT STA 946 LT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-30-06. (X) 2L72 4F A6WE 19950818001841995081800184WP 1995 8 18 USAA950705 119950525A5320 PAN DOUG DC9 DC981 3022081WP BS 886 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK UPPER FORWARD CORNER STA 886, LT WINDOW PAN. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) 2L72 4F A6WE 19950818001851995081800185WP 1995 8 18 USAA950706 119950525A5320 PAN DOUG DC9 DC981 3022081WP BS 929 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN WINDOW PAN STA 929 UPPER FWD CORNER RT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) 2L72 4F A6WE 19950818001861995081800186WP 1995 8 18 USAA950707 119950525A5320 PAN DOUG DC9 DC981 3022081WP BS 888 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN WINDOW PAN UPPER FWD CORNER AT STA 888 RT. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-06. (X) 2L72 4F A6WE 19950818001871995081800187WP 1995 8 18 USAA950722 119950602A335060030451LB EEL POWER SUPPLY DOUG DC9 DC931 3022065WP CABIN DEFECTIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19936VJ 48116 CLE - THE FORWARD CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONS CHECKED GOOD. (X) 2L72 4F A6WE 19950818001881995081800188WP 1995 8 18 USAA950733 119950525A5320 MEMBRANE DOUG DC9 DC981 3022081WP BS 1268-1307 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19809US37575 48041 PIT - DURING Q-5 CHECK INSPECTION, FOUND 2.50 INCH CRACK STA 1268 - STA 1307, LT SIDE CUSP MEMBRANE. CUT OUT SECTION OF CUSP MEMBRANE AND SPLICED IN REPAIR PER SRM 53-05, FIGURE 97. (X) 2L72 4F A6WE 19950818001891995081800189 1995 8 18 VTZA05242 419950730A342504134004 AHRS JETAIRJETSTMJETSTM4101 1500501EU FWD E/E BAY MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27303UE 41015 LYN/ROA - FLT 6911 - DURING CLIMB-OUT, RETURNED TO LYH DUE TO THE NR 1 AHRS FAILURE. AIRCRAFT RETURNED TO LYH WITH NO FURTHER INCIDENTS. MAINTENANCE RERACKED THE AHRS COMPUTER. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950818001901995081800190EU 1995 8 18 VTZA94241 119950729A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGG DOOR DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27315UE 41033 LGA/IAD - FLT 6322 - DURING CLIMB-OUT AT 0830 HRS ON 7-29-95, RETURNED TO LGA DUE TO THE REAR BAGGAGE DOOR LIGHT ILLUMINATING ON CLIMB-OUT. AIRCRAFT RETURNED TO LGA WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE BAGGAGE DOOR MICROSWITCHES. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950818001911995081800191EU 1995 8 18 VTZA95236 119950729A2424 GEN CONTL UNIT BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA27491UE 911 IAD/PHL - FLT 6227 - DURING CRUISE ON 7-29-95, RETURNED TO IAD DUE TO THE LT GENERATOR FAILING IN-FLIGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE GCU. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001921995081800192EU 1995 8 18 VTZA95237 119950728A32336158E ACTUATOR BAG JETSTMJETSTM3201 1500217EU NOSE GEAR FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27486UE 905 IAD/LGA - FLT 6380 - DURING CLIMB-OUT AT 0945 HRS ON 7-28-95, RETURNED TO IAD DUE TO THE NOSE GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NOSE GEAR RETRACTION ACTUATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001931995081800193EU 1995 8 18 VTZA95238 119950730A27505148YMK83NP SELECTOR SW BAG JETSTMJETSTM3201 1500217EU TE FLAPS FAILED A AVTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27475UE 850 IAD/ROAD - FLT 6499 - DURING APPROACH AT 1400 HRS ON 7-30-95, THE FLAPS WERE SELECTED TO 10 DEGREES AND THEN MOVED TO 35 DEGREES UNCOMMANDED. AIRCRAFT LANDED AT ROA WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FLAP SELECTOR SWITCH AND REPAIRED A BROKEN WIRE TO SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001941995081800194EU 1995 8 18 VTZA95239 119950730A244013711636 GPU DOOR BAG JETSTMJETSTM3201 1500217EU NOSE ACCESS MISSING A VTZAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA27490UE 909 BOS/PWM - FLT 6398 - DURING POST-FLIGHT WALKAROUND AT 1836 HRS ON 7-30-95, FLIGHT CREW DISCOVERED THE GPU DOOR HAD SEPARATED FROM THE AIRCRAFT DURING FLIGHT. MAINTENANCE REPLACED GPU DOOR. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001951995081800195EU 1995 8 18 VTZA95240 119950731A7933CAD6R12S3SF80 CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 EA27475UE 850 IAD/ROA - FLT 6499 - DURING CLIMB-OUT AT 1250 HRS ON 7-31-95, RETURNED TO IAD DUE TO THE LT OIL TEMPERATURE BEING ERRATIC. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE OIL TEMP BULB CONNECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001961995081800196NE 1995 8 18 VTZA95243 219950801A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RIGHT FAILED A VTZAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27313UE 41026 P76008 ORF/IAD - FLT 6517 - DURING LANDING ROLL-OUT AT 0710 HRS ON 8-1-95, THE RT ENGINE SHUT DOWN. AIRCRAFT TAXIED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE DECELERATION SCHEDULE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950818001971995081800197EU 1995 8 18 VTZA95244 119950731A2432BTCA520 BATTERY BAG JETSTMJETSTM3201 1500217EU FWD E/E COMPT OVERTEMP A VTZAH DEACTIVATE SYST/CIRCUITS MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 EA27490UE 909 PHL/IAD - FLT 6197 - DURING TAXI FOR TAKEOFF AT 2330 ON 7-31-95, RETURNED TO THE GATE DUE TO THE RT MAIN BATTERY INDICATING AN OVERTEMP CONDITION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT MAIN BATTERY. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950818001981995081800198WP 1995 8 18 VTZA95245 219950801A732189778025 FUEL CONTL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE331* 01514WP RT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27473UE 828 IAD/PHL - FLT 6455 - DURING CLIMB-OUT AT 0645 ON 8-1-95, RETURNED TO IAD DUE TO THE RT ENGINE ONLY MAKING 60 PERCENT TORQUE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL CONTROL. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E2WE 19950818001991995081800199NE 1995 8 18 Y2PA95010 219950726A7320 PT2 DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE LT/RT ENGINE PLUGGED A Y2PAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL23196US 47155 P657575 ELP - ON TAKEOFF, N1 INDICATION WAS 85 PERCENT ON BOTH ENGINES WHEN EPR INDICATION WAS 1.93. INSPECTED AND FOUND PT-2 PROBES ON 'BOTH' ENGINES PLUGGED WITH 'MUD' FROM WASP'S NESTS. REMOVED OBSTRUCTIONS, AND RAN ENGINES. OPERATIONAL CHECKED GOOD. (X) 2L72 4F4 F A6WE E2EA 19950818002001995081800200NM 1995 8 18 9512192285 119950809A7931ST104Z TRANSMITTER BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01285US6747 4626 21324 696558 NR 3 ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO ON TAKEOFF ROLL, TAKEOFF WAS ABORTED. THE AIRCRAFT RETURNED TO THE GATE. A REPLACEMENT OIL PRESSURE TRANSMITTER WAS INSTALLED. SYSTEM OPERATION RETURNED TO NORMAL. THE AIRCRAFT RESUMED REVENUE SERVICE. 2L73 4F4 F A3WE E2EA 19950818002011995081800201NM 1995 8 18 9512202716 119950810A324026011825 BRAKE BOEING727 7272S7 138407ZNM LT MLG MALFUNCTIONED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL01720RC4769 694 22491 DURING LANDING ROLLOUT, THE NR 2 MAIN LANDING GEAR TIRE ASSEMBLY LOCKED UP. SMOKE WAS EMITTING FROM THE WHEEL WELL. FIRE RESCUE CALLED OUT TO FOLLOW AIRCRAFT TO THE GATE. NO EVIDENCE OF FIRE. MAINTENANCE REPLACED THE NR 2 BRAKE ASSEMBLY AND NR 1 AND NR 2 TIRES. 2L73 4F A3WE 19950818002021995081800202NM 1995 8 18 9512215517 119950813A2751 INDICATION BOEING757 757251 1384970NM TE FLAPS MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01517US 23205 UPON EXTENDING FLAPS TO POSITION NR 1 FOR LANDING IN PDX, RECEIVED TE FLAP DISAGREE MESSAGE AND TRAILING EDGE WARNING LIGHT. FLAPS DID NOT MOVE OUT OF UP POSITION, CREW DECLARED AN EMERGENCY. PERFORMED ALTERNATE FLAP EXTENSION PROCEDURE, LANDED WITHOUT INCIDENT. VISUAL AND OPERATIONAL CHECK OF FLAP SYSTEM CHECKED NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA2NM 19950818002031995081800203NE 1995 8 18 95UAL900087 219950814A726170R654 OIL FILTER BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 2 ENGINE LEAKING A UALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29180UA 25224 717657 THE NR 2 ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND PRESSURE. OIL FILTER HOUSING COVER LEAK CAUSED BY A FAILED HELICOIL. MODIFIED COVER, REPLACED BOLT AND HELICOIL WITH STUD AND NUT. 2L74 4F4 FRTA20WE E24NE 19950818002041995081800204NM 1995 8 18 95UAL900089 119950814A3520 OXYGEN MASKS BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DEPLOYED A UALAO OTHER O OTHER CLCLIMB 1 WP29325UA 23957 SHORTLY AFTER DEPARTURE COS, FLIGHT EXPERIENCED DEPLOYMENT OF ALL OXYGEN MASKS. MASKS DROPPED DUE TO PACKS BEING OFF DURING TAKEOFF. SYSTEM OPERATED PROPERLY. 2L72 4F4 FRTA16WE E2GL 19950818002051995081800205NM 1995 8 18 95UAL900090 119950815A2910 PACKING LTV ARLINGTO401602723 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE A-HYD SYST FAILED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP297263U 21410 LANDED LGA UNDER AMBER ALERT DUE TO LOSS OF A-SYSTEM HYDRAULIC. REPLACED ELEVATOR FEEL COMPUTER UNIT FILTER PACKING P/N NAS161216. 2L73 4F4 F A3WE E2EA 19950818002061995081800206SO 1995 8 18 COM11949 119950810A2121EVAC2322C2 COOLING FAN EMB 120 EMB120RT SO RT PACK FAILED A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01256CA10321 120245 DURING TAXI, RT A/C PACK PRODUCED SMOKE IN CABIN. PACK FAILED AND DUCT LEAK INDICATOR ON. REPLACED THE RT GROUND COOLING FAN. 2L72 4T RTA31SO 19950818002071995081800207SO 1995 8 18 COM11950 119950808A5330120278875001 SKIN EMB 120 EMB120RT SO FUSELAGE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01255C 10686 120238 UPON REMOVAL OF THE VHF-2 ANTENNA, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED BETWEEN THE NUTPLATES FOR MOUNTING THE ANTENNA. THE SKIN WAS REPAIRED PER EMB 120 SRM 53-20-01 PG 204 TO 208. 2L72 4T RTA31SO 19950818002081995081800208NE 1995 8 18 COM11951 219950809A72503034954D TURBINE PRATT PW118 EMB 120 EMB120RT SO PWA 118 PW118 NE HAMSTD14RF 14RF9 NE ENGINE FAILED A COMAO OTHER O OTHER ININSP/MAINT 1 SO01257C 14185 115325 120248 115325 910521 POWER TURBINE WOULD NOT ROTATE ON PREFLIGHT WALK AROUND. REMOVED AND REPLACED ENGINE. ALSO, REMOVED POWER TURBINE AND DISSEMBLED. FOUND 2ND STAGE PT STATOR INNER SEAL RETAINING RIUETS AND PLATES FLOATING FREELY BETWEEN 2ND STAGE STATOR AND ROTOR. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 19950818002091995081800209SW 1995 8 18 COM20385 119950810A2910SS1008F000D154Y HOSE ASSY SWRNGNSA227 SA227AC 8780603SW NLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01703CA AC703 HYDRAULIC LEAK, NOSE LANDING GEAR AREA. REPLACED DEFECTIVE RETRACT ACTUATOR UP HYDRAULIC LINE. 1L72 4T A8SW 19950818002101995081800210EA 1995 8 18 COM60535 119950810A27604916403 CONTROL LEVER CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAK NONE O OTHER CRCRUISE 1 SO01924CA3101 1053 7026 FLIGHT SPOILERS FAULT MESSAGE, DURING FLIGHT SPOILERS OPERATED NORMALLY. REPLACED THE SPOILER CONTROL LEVER ASSY. 2L72 4F RTA21EA 19950818002111995081800211EA 1995 8 18 COM60536 119950810A3010124112450 LEAK SENSOR CNDAIRCL600 CL6002B19 EA LT WING DEFECTIVE A COMAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CRCRUISE 1 SO01946CA247 247 7072 ANTI-ICE DUCT MESSAGE AFTER 20 MINUTES OF USE, EICAS INDICATED LT WING. STANDBY SYSTEM OPERATES NORMAL. REPLACED DUCT LEAK SENSORS 527WK, 519WK, 525WK, 515WK. 2L72 4F RTA21EA 19950818002121995081800212EA 1995 8 18 COM60537 119950810A301011513361 CONTROLLER CNDAIRCL600 CL6002B19 EA WING ANTI-ICE DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01938CA2254 7046 WING ANTI-ICE SENSOR CAUTION MESSAGE DURING TEST. REPLACED THE TEMP CONTROLLER. 2L72 4F RTA21EA 19950818002131995081800213NM 1995 8 18 DL72K953382 119950812A2612790378 FIRE LOOP BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A DALAF ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SO11479DA 20756 696623 FIRE WARNING INFLT ON NR 1 ENG, NO OTHER INDICATIONS OF FIRE. SHUTDOWN ENG AND FIRED BOTH BOTTLES, LANDED LGA. DETERMINED IT WAS FALSE WARNING, NO EVIDENCE OF FIRE. FOUND FAULTY FIRE LOOP, REPLACED SAME. OPERATION NORMAL. 2L73 4F4 F A3WE E2EA 19950818002141995081800214NM 1995 8 18 DL72L953361 119950801A5754 SKIN BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11505DA 21307 FOUND ON CV2 CHECK, .5 CRACK AT NR 3 SLAT INNER SKIN BELOW THERMAL ANTI-ICE TUBE. REPAIRED PER M/M 57-54-0 PG 807A. 2L73 4F A3WE 19950818002151995081800215NM 1995 8 18 DL72S953346 119950808A5320 ANGLE BOEING727 727232 1384082NM BS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11403DA 21147 FOUND DURING E-2 LETTER CHECK, .25 INCH VISIBLE CRACK LT SIDE 1183 BL 8 ANGLE OUTBD SIDE. REPAIRED PER M/M 53-11-0 PAR 9. 2L73 4F A3WE 19950818002161995081800216NM 1995 8 18 DL72S953359 119950809A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11409DA 21153 NR 7 SLAT COVE SKIN SUPPORT ANGLE HAS .5 CRACK BELOW THERMAL ANTI-ICE DUCT. FOUND DURING E-1 LTR CK TPAMM, REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950818002171995081800217NM 1995 8 18 DL72S953360 119950809A7110 SKIN BOEING727 727232 1384082NM NR 2 ENG CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11409DA 21153 NR 2 ENGINE INLET HOUSING CRACKED .5 RT SIDE AT PANEL 9524. FOUND DURING E-1 LTR CK TPAMM, REPAIRED PER MM 54-30-00. 2L73 4F A3WE 19950818002181995081800218NM 1995 8 18 DL72S953375 119950811A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11400DA 21144 FOUND DURING E-2 LETTER CHECK, NR 2 SLAT ACT ROD END ATTACH RIB CRKD .5 INCH I/B WEB, NR 3 SLAT ACT ROD END ATTACH RIB CRKD .25 INCH O/B WEB. REPAIRED PER M/M 57-54-0 PG 803 TO 804. 2L73 4F A3WE 19950818002191995081800219NM 1995 8 18 DL72S953376 119950811A5320 WEB BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11400DA 21144 FOUND DURING E-2 LETTER CHECK, LIGHTENING HOLE CRACKED .25 INCH AT STA 1263 LT LOWER. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19950818002201995081800220NM 1995 8 18 DL72S953377 119950811A5320 FRAME BOEING727 727232 1384082NM R2 DOOR OPENING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11400DA 21144 FOUND DURING E-2 LETTER CHECK, R-2 DOOR OPENING FRAME HAS .75 INCH CRACK AT FWD UPPER STOP PAD CASTING. INSTALLED DOUBLER PER M/M 53-13-0 PG 808. 2L73 4F A3WE 19950818002211995081800221NM 1995 8 18 DL72S953379 119950811A5532 SKIN BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11400DA 21144 FOUND DURING E-2 LETTER CHECK, .5 INCH CRACK EXTENDING FROM RIVET AT PNL 9523. REPAIRED PER MM 54-30-0. 2L73 4F A3WE 19950818002221995081800222NM 1995 8 18 DL72W953353 119950808A2530 COFFEE MAKER BOEING727 727247 138408FNM AFT GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11295WA 22532 COFFEE MAKER AND AFT FACING OVEN IN AFT GALLEY GIVING OFF INTENSE ODOR, HOT PLASTIC SMELL. SHUT OFF COFFEE MAKER AND OVEN, GOT RID OF ODOR. REMOVED PLASTIC BAGS FROM UNDER COFFEE MAKER AND FROM SIDE OF OVEN FOOD RACK. COFFEE MAKER AND OVEN OPN NORMAL WITH NO ODOR. 2L73 4F A3WE 19950818002231995081800223NM 1995 8 18 DL72W953362 119950804A5347 SEAT TRACK BOEING727 727247 138408FNM BS 1110-1130 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND SEAT TRACK CORRODED AT RBL 28 FROM STA 1110 TO 1130. REPLACED SEAT TRACK PER 53-20-11. 2L73 4F A3WE 19950818002241995081800224NM 1995 8 18 DL72W953363 119950724A5311 FRAME BOEING727 727247 138408FNM BS 930 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND FRAME AT STA 930 LEFT CRACKED 6 INCHES ABOVE STR 14L. REPAIRED PER SRM 53-10-4 FIG 25. 2L73 4F A3WE 19950818002251995081800225NM 1995 8 18 DL72W953364 119950723A5320 WEB BOEING727 727247 138408FNM BS 1278 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND WEB CRACKED AT STA 1278 IN 48 SECTION, LOWER INSP HOLE. REPAIRED PER MM53-11-0 PAGE 832. 2L73 4F A3WE 19950818002261995081800226NM 1995 8 18 DL72W953365 119950723A7110 SUPPORT RING BOEING727 727247 138408FNM BS 1352 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND NR 2 ENG COWL SUPPORT RING WORN. REPAIRED PER M/M 53-11-0 PAGE 801. 2L73 4F A3WE 19950818002271995081800227NM 1995 8 18 DL72W953366 119950725A5241 SKIN BOEING727 727247 138408FNM R2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND R-2 DOOR SKIN CRACKED AT THE LOWER FWD CORNER. REPAIRED PER M/M 52-14-0 NR 7. 2L73 4F A3WE 19950818002281995081800228NM 1995 8 18 DL72W953367 119950723A5414 SKIN BOEING727 727247 138408FNM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND TEMP REPAIRED INSTALLED RIGHT SIDE AFT AND ABOVE PANEL 9516. REPAIRED PER MM 53-30-0 PAGE 801 AND 802. 2L73 4F A3WE 19950818002291995081800229NM 1995 8 18 DL72W953368 119950723A5330 SKIN BOEING727 727247 138408FNM BS 1223 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 RBL 12. REPAIRED PER MM 53-30-0 PAGE 804. 2L73 4F A3WE 19950818002301995081800230NM 1995 8 18 DL72W953369 119950723A5330 SKIN BOEING727 727247 138408FNM FS 1223 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 ALONG STR 27R. REPAIRED PER MM 53-30-0 PAGE 804. 2L73 4F A3WE 19950818002311995081800231NM 1995 8 18 DL72W953370 119950723A5330 SKIN BOEING727 727247 138408FNM FS 1223 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV, FOUND TEMP REPAIR INSTALLED AT FS 1223 STR 27L. REPAIRED PER MM 53-30-0 PAGE 804. 2L73 4F A3WE 19950818002321995081800232NM 1995 8 18 DL72W953374 119950811A5754651622295 RIBS BOEING727 727247 138408FNM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112822W 21327 DURING SHOP INSPECTION FOR NR 3 L/E SLAT, CRACKS WERE FOUND IN THE L/E SUPPORT RIBS ON INBD AND OTBD SIDES OF ACTUATOR SUPPORT FITTING. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950818002331995081800233NM 1995 8 18 DL733953372 119950802A5320 FRAME BOEING737 737347 1384647NM C2 DOOR CUTOUT TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV, THE C2 CARGO DOOR FWD CUTOUT FRAME LOWER COVER PLATE WAS FOUND TO BE BENT AND TORN WITH SHEARED RIVETS AND WOOD JAMMED BETWEEN FRAME AND COVER. A REPAIR WAS FABRICATED PER SRM 53-60-15 AND THE COVER WAS REINSTALLED. 2L72 4F RTA16WE 19950818002341995081800234NM 1995 8 18 DL733953378 119950803A5713 STRINGER BOEING737 737347 1384647NM WS 453 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV, STR 3 WAS FOUND TO BE CRACKED INSIDE RT WING TANK AT STA 453.00 UPPER STRINGER. THE DAMAGED AREA WAS CUT OUT AND REPAIR DOUBLERS WERE DRILLED UP AND INSTALLED AS PER ERA 302259-14 REF SRM 57-20-03. 2L72 4F RTA16WE 19950818002351995081800235NM 1995 8 18 DL76S953386 119950809A2530 GALLEY BOEING767 767332 1382001NM CABIN ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11131DN 24852 DURING CRUISE, FLIGHT ATTENDANT REPORTED INTERMITTENT BURNING ODOR JUST FWD OF MID GALLEY ON RT SIDE. ODOR AND FREQUENCY WORSENED, DEACTIVATED POWER IN MID GALLEY, SMELL DISSIPATED. CEILING PANELS WERE LOWERED, AREA INSPECTED AND GALLEY EQUIPMENT TURNED ON. NO ODOR OR BURNING NOTED, RETURNED TO SERVICE. 2L72 4F RTA1NM 19950818002361995081800236NM 1995 8 18 DLM11953373 119950808A33506044113 EEL BATTERY PACK DOUG MD11 MD11 3023602NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11803DE 48474 EMERGENCY LIGHTS AFT OF SEAT 46 ARE STROBING. REPLACED AFT EMERGENCY BATTERY PACK. EMERGENCY LIGHTS AT 2AB, 3AB, 14G, 49AB, AFT 2 IN FWD GALLEY, RT SIDE ARE INOP. RELAMPED. 2L73 4F RTA22WE 19950818002371995081800237NM 1995 8 18 DLM88953371 119950810A2910 LINE DOUG MD88 MD88 3023688NM RT HYD SYS LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO11981DL 53268 RIGHT HYD SYSTEM FAILED DURING SLAT EXTENTION ON DESCENT. MANUALLY EXTENDED LANDING GEAR, LANDED ATL. FOUND PRESSURE LINE FROM RT FILTER MODULE LEAKING. REPLACED LINE, OPERATION NORMAL. 2L72 4F RTA6WE 19950818002381995081800238WP 1995 8 18 MWEA95261 119950809A53479957871 SEAT TRACK DOUG DC9 DC914 3022034WP FLIGHT COMPT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31500ME 45711 DURING C-CHECK INSPECTION, THE CAPTAINS LEFT AND RIGHT AFT SEAT TRACKS WERE FOUND TO BE WORN AT THE LOCK PIN HOLES. MAINTENANCE INSTALLED STRAP REPAIR TO THE LEFT AND RIGHT SEAT TRACKS IAW SRM 53-05, FIG 28 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950818002391995081800239WP 1995 8 18 MWEA95262 119950811A2560113313 EVAC SLIDE DOUG DC9 DC932 3022066WP PAX DOOR FELL OFF A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 CREW REPORTS, MAIN ENTRANCE DOOR EVACUATION SLIDE FELL OFF, WHEN DOOR OPENED AT GATE. MAINTENANCE RESECURED SLIDE AND COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950818002401995081800240WP 1995 8 18 MWEA95263 119950813A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER CRCRUISE 1 GL31501ME 47132 CREW REPORTS, THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF IN FLIGHT. MAINTENANCE RESECURED GALLEY DOOR SLIDE COVER. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950818002411995081800241EU 1995 8 18 QXEA9500245 119950808A33506008905 EEL PWR SUPPLY FOKKER FOKKERF28 F28MK1000 4990808EU CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 PDX - SEVERAL EVAC LIGHTS INOP. BATTERY POWER SUPPLY ABOVE SEAT 6A REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818002421995081800242EU 1995 8 18 QXEA9500246 119950810A33501820 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 GEG - LIGHT IN EMERGENCY EXIT SIGN OVER LEFT OVERWING EXIT IS OUT. BULB WAS REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818002431995081800243NM 1995 8 18 QXEA9500247 119950811A2611473054 DETECTOR DHAV DHAV DHC8 DHC8102 2809003NM CARGO COMPT MALFUNCTIONED A QXEAO OTHER N FALSE WARNING CRCRUISE 1 NM09821PH 104 PDX - NR 1 CARGO SMOKE WARNING LIGHT INTERMITTENTLY ILLUMINATES. VERIFIED THAT THERE WAS NO SMOKE IN CARGO COMPARTMENT. NR 1 SMOKE DETECTOR WAS REPLACED AND TESTED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950818002441995081800244EU 1995 8 18 QXEA9500248 119950811A3350 EEL WIRE FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 GEG - EVACUATION LIGHT ON SEAT 6B INOP. BROKEN WIRE AT LIGHT REPAIRED. LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818002451995081800245EU 1995 8 18 QXEA9500249 119950812A3350387 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09464US 11063 GEG - 28V EGRESS LIGHT AT MAIN CABIN DOOR WON'T ILLUMINATE. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818002461995081800246EU 1995 8 18 QXEA9500250 119950812A32321252515 ACTUATOR FOKKER FOKKERF28 F28MK1000 4990808EU RT MLG DOOR SPLIT A QXEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NM09801PH 11097 BOI - UTILITY HYDRAULIC SYSTEM LOST PRESSURE AND QUANTITY ON GEAR EXTENSION INTO SUN VALLEY AIRPORT. AIRCRAFT RETURNED TO BOI AND LANDED WITHOUT FURTHER PROBLEM. RIGHT MAIN GEAR DOOR FORWARD ACTUATOR WAS FOUND SPLIT. ACTUATOR WAS REPLACED AND BOTH UTILITY SYSTEM PUMPS. HYDRAULIC SYSTEM WAS SERVICED AND BLEED. GEAR SWING PERFORMED AND DOOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818002471995081800247NM 1995 8 18 UPS204111 119950812A5320 WEB BOEING727 72727C 138400JNM BS 1263 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TORQUE BOX WEB AT BS 1263, WL 150, RBL 18. MAINTENANCE REPAIRED THE WEB IAW SRM 51-40-2. 2L73 4F A3WE 19950818002481995081800248NM 1995 8 18 UPS204112 119950812A5311 FRAME BOEING727 72727C 138400JNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT BS 760, LBL 67, WL 212. MAINTENANCE REPAIRED IAW SRM 51-10-1, 51-20-4, AND 51-30-2. 2L73 4F A3WE 19950818002491995081800249NM 1995 8 18 UPS204113 119950812A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 900 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM WEB AFT SIDE AT STA 900, RBL 2 TO RBL 23, WL 201 TO 203. MAINTENANCE REPAIRED IAW 53-10-1. 2L73 4F A3WE 19950818002501995081800250NM 1995 8 18 UPS204114 119950812A5751 FITTING BOEING727 72727C 138400JNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON L/W O/B AILERON CENTER, I/B BEARING BLOCK ATTACH CASTING, ATTACHING BEARING BLOCK TO AILERON. MAINTENANCE REMOVED AND REPLACED PER SRM 51-30-2. 2L73 4F A3WE 19950818002511995081800251NM 1995 8 18 UPS204115 119950812A5712 RIB BOEING727 72727C 138400JNM NR 6 SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 SLAT I/B TRACK SUPPORT FITTINGS AND RIBS CRACKED BEYOND STOP DRILL. MAINTENANCE REMOVED AND REPLACED THE RIBS PER SRM 51-30-2. 2L73 4F A3WE 19950818002521995081800252NM 1995 8 18 UPS204116 119950812A5347 SEAT TRACK BOEING727 72727C 138400JNM BS 740-760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 740 TO 760 LBL 45 WL 208. MAINTENANCE INSTALLED NEW PARTS PER SRM 51-10-02, 51-20-04, 51-10-1, 51-30-2 AND OHM 20-44-04. 2L73 4F A3WE 19950818002531995081800253NM 1995 8 18 UPS204117 119950812A5720 CHORD BOEING727 72727C 138400JNM WS 232.2 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER SURFACE OF THE LOWER WING IN SPAR STIFFENER STR 5. MAINTENANCE REPAIRED IAW 727-57-1424. 2L73 4F A3WE 19950818002541995081800254NM 1995 8 18 UPS404110 119950812A3350 EEL BOEING747 747123 1384873NM CABIN DIM A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND IN SDF, MAINTENANCE FOUND EMERGENCY LIGHT IN CREW SERVICE DOOR FRAME IS DIM. MAINTENANCE RELAMPED EMERGENCY EXIT AT RT FLIGHT DECK SERVICE DOOR. 2L74 4F A20WE 19950818002551995081800255NM 1995 8 18 UPS404118 119950812A3350 EEL BOEING747 747123 1384873NM CABIN DIM A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND, MAINTENANCE FOUND CREW SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE CLEANED THE CONNECTOR, LIGHT OPS CK OK. 2L74 4F A20WE 19950818003071995081800307WP 1995 8 18 9512221150 119950811A7830 TR UNIT DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01150US 46759 686151 DURING TAKEOFF ROLL, THE NR 1 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. THE REVERSER WAS DEACTIVATED AND PLACED ON MEL. 2L73 4F4 F A22WE E20EA 19950818003081995081800308NE 1995 8 18 9512239912 219950813A7310 FUEL HEAT VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL01961N 47406 657587 NR 1 ENGINE FUEL HEAT VALVE OPENED IN FLIGHT AND COULD NOT BE CLOSED WITH NORMAL PROCEDURES. THE ENGINE OIL TEMPERATURE EXCEEDED RECOMMENDED LIMITS, THE COM PROCEDURES WERE FOLLOWED AND A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE WITH A SERVICEABLE UNIT. SUBSEQUENT RUNUP AND CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950818003091995081800309NM 1995 8 18 9512242201 119950813A5241 GALLEY DOOR BOEING727 727251 138408HNM CABIN NOT LATCHED A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 GL01201US 22154 MSP-DFW - DURING CLIMB, A LOUD SHRILL NOISE BEGAN EMANATING FROM THE LEFT AFT GALLEY DOOR, NO PRESSURIZATION DISCREPANCIES WERE NOTED. DUMPED 3,000 LBS OF FUEL AND DIVERTED TO MCI WITHOUT FURTHER INCIDENT. PRESSURIZED AIRCRAFT PER MM 21-30-00, PGS 502 TO 503. NO TROUBLE WAS FOUND. 2L73 4F A3WE 19950818003101995081800310WP 1995 8 18 9512259978 119950811A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE HANDLE FROM THE CLIPS. ALSO, FOUND THAT THE UPPER LATCHES RELEASED PRIOR TO THE LOWER LATCHES AND THAT THE TAILCONE FAILED TO DROP. ADJUSTED TAILCONE PER MM 53-50-3, FUNCTIONAL CHECK OK. 2L72 4F A6WE 19950818003111995081800311WP 1995 8 18 9512269160 119950809A5350 CLIP DOUG DC9 DC914 3022034WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. REPLACED AND ADJUSTED THE AFT CLIP, CHECKED OK. 2L72 4F A6WE 19950818003121995081800312WP 1995 8 18 9512279978 119950810A5220 EMERGENCY EXIT DOUG DC9 DC931 3022065WP LT OVERWING OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE LEFT AFT OVERWING EMERGENCY EXIT. RERIGGED DOOR PER MM 52-21-0, CHECKED OK. 2L72 4F A6WE 19950818003131995081800313WP 1995 8 18 9512289178 119950812A5720 FENCE DOUG DC9 DC914 3022034WP LT WING SEPARATED A NWAAK NONE D INFLIGHT SEPARATION DEDESCENT 1 GL013310L 45705 DTW-DSM - DURING DESCENT, THE LEFT WING LEADING EDGE FENCE SEPARATED FROM THE AIRCRAFT. NO ENGINE OR CONTROL DISCREPANCIES NOTED, LANDED DSM WITHOUT FURTHER INCIDENT. REPLACED AND RESEALED LEFT WING FENCE. INSPECTED NR 1 ENGINE AND LEFT WING TRAILING EDGE FOR FOD, NO TROUBLE FOUND. 2L72 4F A6WE 19950818003141995081800314WP 1995 8 18 ABXA9500670 119950814A335060030431 EEL BATTERY PACK DOUG DC9 DC932F 3022067WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23904AX 1771 47040 DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INOP. REPLACED THE EMERGENCY LIGHTING BATTERY PACK. OPS CHECKED GOOD IAW DC-9 SUPP MM 33-54-0. 2L72 4F A6WE 19950818003151995081800315WP 1995 8 18 ABXA9500671 119950814A335060030431 EEL POWER SUPPLY DOUG DC9 DC941 302207NWP CABIN DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23975AX 1771 47512 DURING SERVICE CHECK, EMERGENCY LIGHTS STAYED ON WHEN SWITCH PLACED IN OFF POSITION. REPLACED EMERGENCY EXIT LIGHT SUPPLY IAW DC-9 SUPP MM 33-54-0. OPS CHECKED GOOD. 2L72 4F A6WE 19950818003161995081800316SO 1995 8 18 COM11952 119950813A2400 POWER WIRE EMB 120 EMB120RT SO GALLEY FAILED A COMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01255CA 120238 STRONG SMELL OF ELECTRICAL BURNING IN COCKPIT AREA. FOUND BURNED GALLEY POWER WIRE. SECURED POWER TO GALLEY BY PULLING BREAKERS AND PLACED ON DEFERRED MAINT LIST. 2L72 4T RTA31SO 19950818003171995081800317SO 1995 8 18 COM11953 119950813A2751 FLAP WARNING EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO01159CA 120159 WHEN FLAPS SELECTED TO 15 DEGREES DURING APPROACH ASYMMETRY WARNING CAME ON. COULD NOT DUPLICATE PROBLEM. CYCLED FLAPS 20 TIMES WITH NO MALFUNCTION. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19950818003181995081800318SO 1995 8 18 COM11954 119950813A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG WORN A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01267CA8730 8613 120259 WHEN LANDING GEAR SELECTED UP, THE LT MLG INDICATED INTRANSIT. CYCLED GEAR AND ALL INDICATIONS NORMAL. REPLACED THE LT MLG RETRACT ACTUATOR. 2L72 4T RTA31SO 19950818003191995081800319EA 1995 8 18 COM20386 119950814A274283962 ACTUATOR 70621 CNDAIRCL600 CL6002B19 EA HORZ STAB FAILED A COMAK NONE J WARNING INDICATION CRCRUISE 1 SO01932CA3340 147 7038 STABILIZER CHANNEL 1 INOP STATUS MESSAGE ON CIRCUIT BREAKER TRIPPED. REPLACED THE HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT. 2L72 4F RTA21EA 19950818003201995081800320EA 1995 8 18 COM20387 119950814A2751 FLAP INDICATION CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01946CA 7072 FLAP FAULT MESSAGE ON EICAS, ZERO FLAPS LANDING. COULD NOT DUPLICATE PROBLEM. SYSTEM TEST NORMAL AND ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19950818003211995081800321EA 1995 8 18 COM20388 119950813A2750855D1004 BPSU CNDAIRCL600 CL6002B19 EA LT/RT FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01918CA3145 3145 7018 FLAPS FAILED WHEN SELECTED TO 20 DEGREES. REPLACED THE LT AND RT FLAP BRAKE AND POSITION SENSOR UNITS. 2L72 4F RTA21EA 19950818003221995081800322EU 1995 8 18 COM31135 119950813A3230AIR131330 SPRING SAAB SF340 SF340A 7850100EU LT MLG BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01359CA 340A053 LANDING GEAR EXTENSION ASSIST SPRING ON LT MLG IS BROKEN. REPLACED ASSISTOR SPRING. 2L72 4T RTA52EU 19950818003231995081800323EU 1995 8 18 COM31136 119950814A3260D49410001 DOWN/LOCK IND SAAB SF340 SF340A 7850100EU NLG INOP A COMAO OTHER P NO WARNING INDICATION CRCRUISE 1 SO01340SF11716571 340A014 NOSE LANDING GEAR DOWN AND LOCKED INDICATOR IS INOP. REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. 2L72 4T RTA52EU 19950818003241995081800324WP 1995 8 18 MWEA95264 119950814A33506011777 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP RT NACELLE DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31501ME 47132 DURING SERVICE CHECK, RIGHT ENGINE NACELLE LIGHT WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED EMERGENCY NACELLE LIGHT POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950818003251995081800325NM 1995 8 18 P5CA9500703 119950814A5414 SKIN BOEING747 747124 1384874NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 SKIN CRACK AT NR 4 PYLON, FORWARD ACCESS DOOR CUTOUT 1.75 INCH LONG, TERMINATES AT FASTENER. REPAIRED PER BOEING SRM 54-30-03 FIG 17B. 2L74 4F A20WE 19950818003261995081800326NM 1995 8 18 SCNA95164 119950803A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 22559 THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND BLINKING. REPLACED BATTERY IN THE EMERGENCY LIGHT, UNIT TESTED GOOD. 2L73 4F A3WE 19950818003271995081800327WP 1995 8 18 SCNA95165 119950805A2740418575 TRIM BRAKE MOTOR DOUG DC10 DC1015 3022118WP RT HORIZ STAB CRACKED A SCNAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 GL15152SY 48289 DURING TAXI OUT, ALL HYDRAULIC FLUID FROM SYSTEM 3 WAS LOST. AIRCRAFT RETURNED TO THE GATE. THE RIGHT HYDRAULIC HORIZONTAL STABILIZER TRIM BRAKE MOTOR CASING WAS FOUND CRACKED. REMOVED AND REPLACED TRIM BRAKE MOTOR AND ACCOMPLISHED LEAK CHECKS AND SERVICING. 2L73 4F A22WE 19950818003281995081800328NM 1995 8 18 SCNA95166 119950808A323065404676 LOCK ACTUATOR BOEING727 727282 2F0R NM NOSE GEAR BROKEN A SCNAO OTHER J WARNING INDICATION DEDESCENT 1 GL15281SC 21949 NOSE GEAR DID NOT EXTEND DURING GEAR EXTENSION, A-SYSTEM HYDRAULIC INDICATIONS WERE NORMAL. NOSE GEAR WAS EXTENDED MANUALLY. NOSE GEAR LOCK ACTUATOR WAS FOUND BROKEN. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR AND PERFORMED EMERGENCY EXTENSION CHECK AND RESET MANUAL EXTENSION SYSTEM PER MM 32-33-11. 2L73 4F RTA3WE 19950818003291995081800329NM 1995 8 18 SCNA95167 119950808A335057761 EEL BATTERY PACK BOEING727 727259 138408JNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE FORWARD MIDDLE EMERGENCY PATH LIGHTING INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND LIGHTING TESTED GOOD PER MM 33-50-01. 2L73 4F A3WE 19950818003301995081800330WP 1995 8 18 SCNA95168 119950812A261172130000002 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 8 LAV MALFUNCTIONED A SCNAK NONE N FALSE WARNING UKUNKNOWN 1 GL15573SC 46905 THE SMOKE DETECTOR IN LAVATORY NUMBER 8 WENT OFF TWICE FOR NO APPARENT REASON. REMOVED AND REPLACED NUMBER 8 LAV SMOKE DETECTOR AND UNIT TESTED GOOD. 2L73 4F A22WE 19950818003311995081800331NM 1995 8 18 SCNA95169 119950811A27512061121 POSITION IND BOEING727 727227 1384078NM TE FLAPS MALFUNCTIONED A SCNAO OTHER N FALSE WARNING CLCLIMB 1 GL15275AF 22092 DURING FLAP RETRACTION FROM 15 DEGREES TO 5 DEGREES THE OUTBOARD TRAILING EDGE FLAPS STAYED AT 15 DEGREES. ALTERNATE PROCEDURES WERE USED TO RETRACT FLAPS. CHECKED THE FLAPS, FLAP DRIVE SYSTEM, CONTROL SYSTEM, FOLLOW UP SYSTEM, OPERATION OF BYPASS VALVES, AND OPERATED FLAPS WITH NO DEFECTS NOTED. REPLACED THE OUTBOARD FLAP POSITION INDICATOR AS A PRECAUTIONARY MEASURE. 2L73 4F A3WE 19950818003321995081800332CE 1995 8 18 95ZZZX4052 119950610A321051410061 PIN CESSNA402 402C 207590RCE LT MLG SHEARED A FAHAO OTHER O OTHER LDLANDING 1 SO1926371 402C0327 UPON LANDING IN CAPE HATIAN, HAITI, THE LEFT MLG TORQUE LINK, UPPER SCISSOR PIN SHEARED CAUSING AIRCRAFT TO VEER OFF THE RUNWAY. INSPECTED IAW CESSNA MM, CHAPTER 5-50-00, PAGES 1 AND 2A, AND PAGE 4, NR 2F. REMOVED AND REPLACED UPPER SCISSOR ASSEMBLY. 1L72 3O A7CE 19950818003331995081800333NM 1995 8 18 95ZZZX4053 119950717A572065114212 SUPPORT FITTING BOEING707 707369C 1383661NM WBL 59.24 CRACKED A FWTAK NONE O OTHER ININSP/MAINT 1 SO19725FW5511626109 20085 DURING ROUTINE B-CHECK INSPECTION, A CRACK WAS FOUND IN THE SUPPORT, AFT RIB WING BL 59.24. THE CRACK IS APPROXIMATELY 10 INCHES LONG. 2L74 4F 4A26 19950818003341995081800334NE 1995 8 18 95ZZZX4054 219950709A7200 ENGINE BOEING757 75723APF 1384966NM RROYCERB211 RB211535E4 54555NE RIGHT FLAMED OUT A CLCAO OTHER X ENGINE FLAMEOUT APAPPROACH 1 SO19571CA 24456 BOG - FLT 092/09 - RIGHT ENGINE FLAME-OUT ON FINAL APPROACH TO BOG, WITH A NORMAL RESTART. TROUBLESHOT PER MM 71-05-00. NO DISCREPANCIES FOUND ON RIGHT ENGINE. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F4 FRTA2NM E12EU 19950818003351995081800335 1995 8 18 95ZZZX4055 419950527A25624523050 ELT TRAY ARTEX 1004 BEECH 1900 1900D 1154162CE AFT FUSELAGE CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01830CA756 53656 UE19 DURING DETAILED PHASE NR 6 INSPECTION, ELT MOUNTING TRAY WAS DISCOVERED AS BEING CRACKED. UNIT WAS REPLACED WITH A NEW ELT ASSEMBLE. 2L72 4T RTA24CE 19950818003361995081800336 1995 8 18 95ZZZX4056 419950609A25624523050 ELT TRAY ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE BROKEN A JJBAK NONE O OTHER ININSP/MAINT 1 EA01832CA2765 UE22 DURING SCHEDULED MAINTENANCE AND ELT BATTERY TIME CHANGE, ELT MOUNTING TRAY WAS DISCOVERED BROKEN. REMOVED AND REPLACED MOUNTING TRAY AND BATTERY PACK. 2L72 4T RTA24CE 19950818003371995081800337 1995 8 18 95ZZZX4057 419950520A25621183400021 ELT HARNESS ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER NRNOT REPORTED 1 EA01834CA309 UE25 ELT TRANSMITS CONSTANTLY - FOUND REMOTE SWITCH HARNESS SHORTED AND UNIT WAS WET. REMOVED AND REPLACED BATTERY PACK, PN 452-0130, AND REMOTE SWITCH HARNESS, PN 118-340002-1. 2L72 4T RTA24CE 19950818003381995081800338 1995 8 18 95ZZZX4058 419950603A25621104 ELT MOUNT ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE BROKEN A JJBAK NONE O OTHER ININSP/MAINT 1 EA01852CA1356 52397 UE55 DURING DETAILED PHASE NR 6 INSPECTION, FOUND ELT MOUNT AND FACE PLATE BROKEN. REPLACED ELT WITH NEW UNIT. 2L72 4T RTA24CE 19950818003391995081800339CE 1995 8 18 95ZZZX4059 119950702A32606046H39 RELAY BEECH 1900 1900C 1154161CE CABIN FAILED A MASAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW01155YV UC155 DURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LT MAIN INDICATOR LAMP AND FLAP MOTOR RELAY. AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL NR MASA 9515. 2L72 4T RTA24CE 19950818003401995081800340NM 1995 8 18 AALA950039H 119950628A5315141T511 FLOORBEAM BOEING767 767223 1385123NM BS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - CORROSION FOUND ON FORWARD FLANGE OF CABIN FLOORBEAM UPPER CHORD AT STA 287. REPAIRED PER MRB 767-951 AND SRM 53-00-51. TST 35,774. CYCLES, 6,431. (X) 2L72 4F RTA1NM 19950818003411995081800341NM 1995 8 18 AALA950041H 119950628A5280141T691034 DOOR BOEING767 767223 1385123NM NLG DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - DAMAGE ON INNER SURFACE OF LT FORWARD NLG DOOR IN CRITICAL AREA. REPAIRED PER MRB 767-948. SRM 51-70-05 WITH 2 EXTRA PLIES. TST 35,774. CYCLES, 6,431. (X) 2L72 4F RTA1NM 19950818003421995081800342NM 1995 8 18 AALA950042H 119950628A5347141T512120 SEAT TRACK BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - UPPER FLANGE OF TRACK HAS CORROSION OUT OF LIMITS. BLENDED AND REFINISHED. APPROVED PER MRB 767-949. TST 35,774. CYCLES, 6,431. (X) 2L72 4F RTA1NM 19950818003431995081800343EU 1995 8 18 AALA951148 119950626A3231 DOOR STOP FOKKERF28 F28MK0100 4990807EU LT MLG OUT OF ADJUST A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071411G 11369 DFW - FLT 0776 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, LT MLG MESSAGE APPEARED ON MFDU. RECYCLED LANDING GEAR WITH SAME RESULTS. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. ADJUSTED LT MLG DOOR STOP. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19950818003441995081800344NM 1995 8 18 AALA951155 119950623A5330146T3240 SKIN BOEING767 767223 1385123NM FS 1314 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - LOWER FUSELAGE SKIN OUTER SURFACE UNDERNEATH VHF ANTENNA CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED ANTENNA WITH NEW FASTENERS. APPROVED BY ENGINEERING PER MRB 767-967. TST 41,944.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003451995081800345NM 1995 8 18 AALA951156 119950623A5347143T52109 SEAT TRACK BOEING767 767223 1385123NM BS 788 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FOUND CORROSION ON THE SEAT TRACK OUTBOARD FLANGE AT LBL 11 AND ON THE INBOARD FLANGE AT RBL 11. FLAP PEENED BLENDED AREAS. PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-957. TST 41,944.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003461995081800346NM 1995 8 18 AALA951158 119950623A5320146T10432 DOOR FRAME BOEING767 767223 1385123NM FS 1270 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FOUND CORROSION ON THE FORWARD SIDE OF THE VERTICAL LEG OF THE INNER CHORD. ALODINED BLENDED AREA AND REINSTALLED FASTENERS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-958. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003471995081800347NM 1995 8 18 AALA951159 119950623A5320 SILL BOEING767 767223 1385123NM BS 1270 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - INNER CHORD CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REINSTALLED FASTENERS WITH SHIM AS REQUIRED AFTER ALODING BLENDED AREAS. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-959. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003481995081800348NM 1995 8 18 AALA951160 119950623A5320146T10433 STRAP BOEING767 767223 1385123NM FS 1270 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FAIL SAFE STRAP LOCATED ON THE FORWARD SIDE OF THE AFT CARGO DOOR CUT-OUT CORRODED JUST BELOW 533R AND JUST BELOW 532R. BOTH EXCEEDED SRM LIMITS AFTER BLENDING. ROTOPEENED, PRIMED, AND PAINTED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE BY ENGINEERING WITH NOTED CONDITION PER MRB 767-960. TST 41,944.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003491995081800349NM 1995 8 18 AALA951167 119950623A5315141T5113 FLOORBEAM BOEING767 767223 1385123NM FS 325 LBL 23 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERING PER MRB 767-953. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003501995081800350NM 1995 8 18 AALA951169 119950623A5315141T5113 FLOORBEAM BOEING767 767223 1385123NM BS 325 RBL 57 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FLOORBEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED A REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED AND PAINTED. REPAIR ACCOMPLISHED. APPROVED BY ENGINEERING PER MRB 767-954. TST 41,944.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003511995081800351NM 1995 8 18 AALA951170 119950623A5315141T5112 FLOORBEAM BOEING767 767223 1385123NM FS 303 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED REPAIR STRAP. APPROVED BY ENGINEERING PER MRB 767-955. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003521995081800352NM 1995 8 18 AALA951171 119950623A5315141T5114 FLOORBEAM BOEING767 767223 1385123NM FS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FLOORBEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF-HARD STAINLESS STEEL. PRIMED AREA. APPROVED BY ENGINEERING PER MRB 767-956. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003531995081800353NM 1995 8 18 AALA951172 119950623A5313146T3003 STRINGER BOEING767 767223 1385123NM FS 1263-1285 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - STRINGER CORRODED AROUND FASTENER HOLES. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-961. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003541995081800354NM 1995 8 18 AALA951173 119950623A5330146T3240 SKIN STRAP BOEING767 767223 1385123NM FS 1540 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - TEAR STRAP CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-963. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003551995081800355NM 1995 8 18 AALA951174 119950623A5311 FRAME BOEING767 767223 1385123NM FS 1307 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FOUND AND BLENDED OUT CORROSION ON AFT CARGO FRAME WEB JUST BELOW INNER CHORD AT LBL 32. BLEND OUT GOES ALL OF THE WAY THROUGH THE WEB. FABRICATED AND INSTALLED REPAIR STRAP USING .040 INCH 7075-T6 ALUMINUM PRIMED REPAIR STRAP. APPROVED BY ENGINEERING AND ACCOMPLISHED PER MRB 767-966. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003561995081800356NM 1995 8 18 AALA951175 119950623A5230140T2633 FITTING BOEING767 767223 1385123NM CARGO DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07302AA 22308 AFW - FOUND INTERNAL CORROSION ON THE TEE FITTING LOCATED NEXT TO THE AFT FASTENER HOLE. TRIMMED OUT DISCREPANT AREA. APPLIED ALODINE AND PRIMED. FABRICATED AND INSTALLED FILLER, SHIM, AND STRAP USING 7075-T6 ALUMINUM. PRIMED AND PAINTED. ACCOMPLISHED AND APPROVED BY ENGINEERING PER MRB 95C062. TST 41,966.02. CYCLES, 13,544. (X) 2L72 4F RTA1NM 19950818003571995081800357NM 1995 8 18 AALA951182 119950630A2422100201021000 INVERTER BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07366AA 25193 LHR - FLT 0096 - EN ROUTE ORD/MXP, ELECTRICAL SMOKE OF UNKNOWN SOURCE WAS DETECTED IN THE CABIN. AIR INTERRUPTED AND LANDED LHR WITHOUT INCIDENT. REPLACED STATIC INVERTER PER MM24-33-03-04. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950818003581995081800358NM 1995 8 18 AALA951184 119950702A3350 EEL TERMINAL BOEING727 727223 1384074NM AFT STAIRS DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07859AA 21086 MIA - DURING OVERNIGHT CHECK, FOUND AFT STAIRS EMERGENCY LIGHT INOPERATIVE. REPLACED GROUND TERMINAL END. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950818003591995081800359NM 1995 8 18 AALA951185 119950704A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07335AA 22333 SFO - DURING OVERNIGHT CHECK, FOUND LOWER CEILING RIGHT EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY EXIT SIGN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950818003601995081800360NM 1995 8 18 AALA951187 119950704A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07633AA 24591 DFW - DURING OVERNIGHT CHECK, FOUND L3 DOOR EMERGENCY EXIT IDENTIFIER MARKER INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY EXIT IDENTIFIER MARKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950818003611995081800361NM 1995 8 18 AALA951188 119950704A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07321AA 22322 SFO - DURING OVERNIGHT CHECK, EMERGENCY SEAT LIGHTS ON LEFT SIDE OF ROW 31 FOUND INOPERATIVE. REPLACED CONNECTOR AT SEAT ROW 33. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950818003621995081800362NM 1995 8 18 AALA951233 119950712A324626045611 WHEEL BENDIX BOEING727 727223 1384074NM NR 2 POSITIION FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07871AA 21383 MIA - FLT 0993 - UPON ARRIVAL AT THE GATE IN MIA, NR 2 MAIN WHEEL WAS DISCOVERED FLAT AND MISSING APPROXIMATELY 50 PERCENT OF THE INBOARD WHEEL HALF WITH STONE DEFLECTOR BENT AND SCORING TO NR 2 BRAKE. REPLACED NR 1 AND NR 2 MAIN WHEEL AND TIRE ASSEMBLIES. ALSO, REPLACED STONE DEFLECTOR AND NR 2 BRAKE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950818003631995081800363NM 1995 8 18 AALA951234 119950712A33508100022601 EEL BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07353AA 24034 SFO - FLT 0035 - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT IN BUSINESS CLASS CABIN RT SIDE FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN BUSINESS CLASS CABIN RT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950818003641995081800364NM 1995 8 18 AALA951235 119950712A3350S283T0231 EEL INVERTER BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739356 24037 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING IN MID-GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTING INVERTER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950818003651995081800365WP 1995 8 18 CAL950487 119950614A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW0914889 49118 EWR - FLT 0346 - INSPECTION FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 19-31 INOPERATIVE. MAINTENANCE FOUND WIRING TO LIGHTS BROKEN. THE WIRES WERE SPLICED AND OPERATION OF THE LIGHTS CHECKED GOOD. (X) 2L72 4F A6WE 19950818003661995081800366WP 1995 8 18 CAL950488 119950615A2913AS66411LS666 HYD PUMP DOUG DC9 DC932 3022066WP NR 2 ENGINE LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0912514163946712 48113 MIA - FLT 1626 - WHEN EXTENDING FLAPS AND SLATS ON APPROACH TO FLL, THE RT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST. THE AIRCRAFT WAS DIVERTED TO MIA, AS A PRECAUTION, FOR THE LONGER RUNWAY AND LANDED SAFELY WITH SLATS ONLY. MAINTENANCE FOUND THE RT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD. (X) 2L72 4F A6WE 19950818003671995081800367WP 1995 8 18 CAL950497 119950617A3260800403 PROX CONTROL BOX DOUG DC9 DC932 3022066WP MLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW091452447728 47539 IAH - FLT 1536 - THE LEFT GEAR UNSAFE LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK AFTER DEPARTING IAH. CYCLING THE GEAR AND REPEATING THE UPLATCH CHECK GAVE NO CHANGE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE LANDING GEAR PROXIMITY SWITCH CONTROL BOX WAS REMOVED AND REPLACED. A CHECK OF THE LT MLG UPLATCH SENSOR SHOWED PROPER CLEARANCE. SEVERAL GEAR RETRACTIONS AND EXTENSIONS WERE PERFORMED AND ALL GEAR INDICATIONS WERE NORMAL. (X) 2L72 4F A6WE 19950818003681995081800368NM 1995 8 18 CAL950548 119950621A243225582003 BATTERY BOEING737 737217 1384464NM BATT COMPT FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW0913234153 145 19888 GSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTNANCE FOUND THE ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE BATTERY CHARGER WAS REPLACED AS A PRECAUTIONARY MEASURE. THE CHARGING SYSTEM WAS CHECKED AND NO DISCREPANCIES WERE FOUND. SUPPLEMENT - THE SDR STATUS HAS BEEN CHANGED TO OPEN PENDING RESULTS OF SHOP REPORT ON BATTERY. SUPPLEMENT - INVESTIGATION REVEALED THE BATTERY HAD EXPERIENCED THERMAL RUNAWAY. THE VENDOR EXAMINED THE CHARGER AND FOUND NO FAULTS THAT COULD HAVE CONTRIBUTED TO BATTERY FAILURE. (X) 2L72 4F A16WE 19950818003691995081800369WP 1995 8 18 CAL950552 119950626A5320 JAMB DOUG DC9 DC932 3022066WP AFT VENTRAL DOORCRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093350645574 47765 HOU - INSPECTION FOUND THE AFT VENTRAL DOOR JAMB HAD A 2 INCH CRACK ON THE FORWARD SIDE OF LEFT CORNER. REPAIRED PER SRM 53-08, FIGURE 29. (X) 2L72 4F A6WE 19950818003701995081800370NM 1995 8 18 CAL950553 119950621A2432 BATTERY BOEING737 737217 1384464NM E/E COMPT FAILED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW09132341919715497 19888 GSO - FLT 1551 - A FAINT ELECTRICAL SMELL WAS OBSERVED IN THE COCKPIT AND CABIN DURING TAXI IN AT GSO. THE AIR STARTED TO CLEAR AFTER THE PACKS AND BLEEDS WERE TURNED OFF. MAINTENANCE FOUND ACFT BATTERY BURNED. THE BATTERY WAS REMOVED AND REPLACED. THE BATTERY CHARGER WAS REPLACED AS A PRECAUTIONARY MEASURE. CHARGING SYS CHECKED AND NO DISCREPANCIES FOUND. SDR WILL REMAIN OPEN PENDING SHOP FINDINGS ON BATTERY CHARGER. SUPPLEMENT - INVESTIGATION REVEALED THE BATTERY HAD EXPERIENCED THERMAL RUNAWAY. THE VENDOR EXAMINED THE CHARGER AND FOUND NO FAULTS THAT COULD HAVE CONTRIBUTED TO BATTERY FAILURE. (X) 2L72 4F A16WE 19950818003711995081800371WP 1995 8 18 CAL950554 119950707A2530 OVEN DOUG DC10 DC1030 3023501WP FWD GALLEY DIRTY A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0968060 47850 EWR - FLT 0041 - THE FORWARD GALLEY CENTER OVEN EMITTED SMOKE MOMENTARILY WHILE AT CRUISE. MAINTENANCE FOUND HEATING ELEMENTS AND BOTTOM OF OVEN CONTAMINATED WITH GREASE AND OIL. THE OVEN WAS CLEANED. OVEN OPERATION CHECKED GOOD WITH NO SMOKE PRODUCED AND NO OTHER DISCREPANCIES FOUND. (X) 2L73 4F A22WE 19950818003721995081800372NM 1995 8 18 CALA950505 119950602A5313 STRINGER BOEING727 727232 1384082NM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND STRINGER 27R CORRODED IN FORWARD BAG PIT AT STA 740. THE STRINGER WAS REPAIRED IAW SRM 51-10-6, SRM 51-10-3, AND SRM 51-20-4. (X) 2L73 4F A3WE 19950818003731995081800373NM 1995 8 18 CALA950506 119950602A5321 FLOOR BOEING727 727232 1384082NM BS 620 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND THE FORWARD BAG PIT CENTER FLOOR CORRODED AT STA 620. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-40-3 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818003741995081800374NM 1995 8 18 CALA950512 119950602A5313 STRINGER BOEING727 727232 1384082NM BS 675 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND CORROSION ON LOWER SURFACE OF STRINGER 28L IN FORWARD BAG PIT AT STA 675. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818003751995081800375NM 1995 8 18 CALA950524 119950625A2910 LINE BOEING737 737217 1384464NM NR 2 ENGINE CHAFED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW0914233 19887 DFW - FLT 1648 - LOSS OF A-SYSTEM HYD QUANTITY. REQUIRED BRAKE REPLACEMENT TO REMOVE FROM RUNWAY DUE TO OVERTEMP ON LANDING. FOUND LINE ON NR 2 ENGINE DRIVEN PUMP CHAFED. REPLACED LINE, FLUSHED, OPERATION AND LEAK CHECKED SYSTEM. REMOVED AND REPLACED NR 1, 2, 3, AND 4 BRAKES DUE TO OVERTEMP ON LANDING. (X) 2L72 4F A16WE 19950818003761995081800376WP 1995 8 18 CALA950590 119950712A499038025611 APU DOUG DC9 DC932 3022066WP AFT FUSELAGE LOW OIL A CALAOH OTHER DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 SW0927522263304270 47524 MSY - FLT 1529 - THE APU OIL PRESSURE LOW LIGHT BEGAN TO ILLUMINATE INTERMITTENTLY IN-FLIGHT. THE APU WAS SHUT DOWN. MAINTENANCE FOUND THE APU OIL LEVEL LOW. THE APU WAS SERVICED TO FULL. (X) 2L72 4F A6WE 19950818003771995081800377NE 1995 8 18 CALA950591 219950712A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE NR 2 FAILED A CALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW09138811962716874 48045 717369 MCO - FLT 0554 - THE NR 2 ENGINE FAILED WITH A LOUD POP AND FLAME SEEN IN THE EXHAUST DURING TAKEOFF ROLL AT 60 KNOTS. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. (X) 2L72 4F4 F A6WE E9NE 19950818003781995081800378NM 1995 8 18 EIAA9514 119950423A2820 VALVE BOEING747 747212B 1384886NM NR 4 CROSSFEED CLOSED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV 20712 JFK - LOG PAGE A 7103 - NR 4 ENGINE WILL NOT CROSSFEED. FOUND NR 4 CROSSFEED VALVE IN CLOSED POSITION. SECURED VALVE OPEN AS REQUIRED PER MEL 28-5 DDPG. ITEM TO CONTINUE ON DMI NR 743. VERIFIED VALVE OPEN BY TRANSFERRING FUEL BETWEEN TANK 3 AND 4 MAIN. (X) 2L74 4F A20WE 19950818003791995081800379NM 1995 8 18 EIAA9517 119950419A535065B079306 RADOME BOEING747 747212B 1384886NM FWD FUSELAGE DENTED A EIAAO OTHER C F.O.D. CLCLIMB 1 NM09485EV 20712 BRU - LOG PAGE A3720 - ON CLIMB-OUT OEJN AT 5,900 FEET AGL, A LOUD BANG WAS HEARD AT NOSE OF AIRPLANE. ON INVESTIGATION AFTER LANDING AT EBBR, FOUND EVIDENCE OF BIRD STRIKE ON NOSE AND RADOME - FRONT OF RADOME CRUSHED. REPLACED RADOME - CHECKED OKAY. BRITISH AIRWAYS LOANER. BIRD STRIKE MAINTENANCE PRACTICES ACCOMPLISHED PER MM 05-51-14. NO MORE DAMAGE FOUND. (X) 2L74 4F A20WE 19950818003801995081800380NM 1995 8 18 EIAA9518 119950514A5230 VENT DOOR HANDLE BOEING747 747132 1384882NM CARGO DOOR NOT SECURED A EIAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09481EV 19896 JFK - LOG PAGE A3752 - AFT CARGO LIGHT ILLUMINATED ON TAKEOFF ROLL ALONG WITH CARGO DOOR ANNUNCIATOR LIGHT ON PILOTS CLEAR SHIELDS. ABNORMAL CHECKLIST COMPLETED AND LANDING WAS UNEVENTUAL. FOUND LOWER AFT CARGO DOOR VENT DOOR RELEASE HANDLE OPEN. RESECURED HANDLE AND OPERATED HANDLE NUMEROUS TIMES. LIGHT OPERATED NORMALLY IAW MM 52-34-0. OPERATION OF AFT CARGO DOOR VENT DOOR HANDLE AND TRIGGER ASSY AND INDICATION SYSTEM ALL CHECKED OK. (X) 2L74 4F A20WE 19950818003811995081800381CE 1995 8 18 MASA9515 119950702A32601864 LAMP BEECH 1900 1900C 1154161CE COCKPIT FAILED A MASAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW01155YV UC155 DURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LT MAIN INDICATOR LAMP AND FLAP MOTOR RELAY. AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL 95ZZZX4059. (X) 2L72 4T RTA24CE 19950818003821995081800382EU 1995 8 18 SIMA951921 119950711A323024589000 UPLOCK BOX AEROSPATR72 ATR72212 EU NLG FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21253AT 652 253 ORD - FLT 4003 - DURING CLIMB-OUT, PILOT SUSPECTED NOSE GEAR WAS NOT FULLY RETRACTED (PRIMARY NOSE GEAR PREVIOUSLY HELD). CREW DID NOT GET INDICATION ON SECONDARY PANEL. RETURNED TO ROD WHERE MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX AND PERFORMED GEAR CHECKS. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950818003831995081800383EU 1995 8 18 SIMA951931 119950712A2432501122804 BATTERY SAAB SF340 SF340A 7850100EU BATT COMPT DISCHARGED A SIMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW21112AE 781 6502 340A112 DFW - FLT 3946 - EMERGNECY POWER LIGHT ILLUMINATED. AIRCRAFT TURNED BACK TO DFW. REMOVED AND INSTALLED EMERGENCY BATTERY. OPERATIONS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19950818003841995081800384SO 1995 8 18 SRAA79502 119950706A2150203430 COOLING TURBINE LKHEED382 382B 5264104SO FLT DECK FAILED A SRAAH DEACTIVATE SYST/CIRCUITS O OTHER CRCRUISE 1 SO19907SJ 4248 FLT 1002 - DURING FLIGHT, COOLING TURBINE CHATTERS AND EMITS BAD ODORS, DEACTIVATE SYSTEM FOR THE REMAINING FLIGHT. REPLACED COOLING TURBINE, OPS CHECKED GOOD PER LOCKHEED MM CMT 21. (X) 2H74 4T A1SO 19950818003851995081800385WP 1995 8 18 95ZZZM232 119950629A3244 TIRE DOUG DC9 DC981 3022081WP NR 1/2 BLOWN A USAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA19803US 48035 MCO - FLT NR 1136 - UPON TAXIING FOR DEPARTURE, THE LEFT BRAKE SEIZED. SUBSEQUENTLY, THE NR 1 TIRE WENT FLAT. CAPTAIN DECIDED TO RETURN TO THE GATE. MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY, AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES P/N 32935. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950818003861995081800386 1995 8 18 95ZZZM233 319950727A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE LT PROPELLER MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01854CA969 UE60 LEFT PROP, BLADE S/N UNKNOWN, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE. SUBMITTER STATES THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. (M) 2L72 4T RTA24CE 19950818003871995081800387 1995 8 18 95ZZZM234 319950727A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE RT PROPELLER MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01839CA1318 UE36 RIGHT PROP, BLADE S/N 317MA, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, SUBMITTER STATES THE PROBLEM LIES WITH THE PAINT BEING APPLIED. THE BLADES PRIOR TO BOOT INSTALLATION. (M) 2L72 4T RTA24CE 19950818003881995081800388 1995 8 18 95ZZZM235 319950727A61124E30171 DE-ICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE LT PROPELLER MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01846CA1167 UE49 LEFT PROP, BLADE S/N 373MA, MISSING DE-ICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, IT WAS APPARENT, SUBMITTER STATES, THAT THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. (M) 2L72 4T RTA24CE 19950818003891995081800389CE 1995 8 18 95ZZZM236 119950727A3260951F04 LIGHT BULB BEECH 1900 1900D 1154162CE NLG FAILED A JJBAO OTHER P NO WARNING INDICATION DEDESCENT 1 EA01852CA UE55 NOSE LANDING GEAR ANNUNCIATOR MODULE BULBS FAILED TO ILLUMINATE ON EXTENSION. INSPECTION OF MODULE FOUND P/N 951-F04 BULBS FAILED. (M) 2L72 4T RTA24CE 19950818003901995081800390EU 1995 8 18 95ZZZM237 119950711A52107015006200A NITROGEN CYL 7015600001 AIRBUS300 A300B4203 3930306EU L2 DOOR INOP A P2RAO OTHER O OTHER ININSP/MAINT 1 WP2314976 6386 271 DOOR L-2 FAILED TO OPEN DURING MINI-EVAC. MAINTENANCE REPLACED L2 DOOR ASSIST ACTUATING MECHANISM IAW MM. OPERATIONAL CHECK NORMAL. RESULT SATISFACTORY. 2L72 4F A35EU 19950818003911995081800391NM 1995 8 18 95ZZZM238 119950712A7540 BLEED AIR WARN DORNERDO32 DO328100 2996000NM COCKPIT ACTIVATED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07423JS 3032 FLT NR 4023 - CREW REJECTED TAKEOFF AFTER RECEIVING BLEED AIR SHUTOFF VALVE CAS MESSAGE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CONDUCTED AN OPERATIONAL CHECK OF THE SYSTEM IAW DO328MM 36-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 19950818003921995081800392WP 1995 8 18 95ZZZM239 219950718A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT/RT MALFUNCTIONED A VNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07845JS 769 FLIGHT NR 4032 - AIRCRAFT RETURNED TO GATE AFTER FLIGHT CREW NOTICED TORQUE FLUCTUATION BOTH ENGINES PRIOR TO TAKEOFF. PIT/MX CONDUCTED ENGINE GROUND RUNS IAW MM 71-00-00. OPS CHECK GOOD. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19950818003931995081800393EU 1995 8 18 95ZZZM240 119950718A3230 BYPASS PIN BAG JETSTMJETSTM3101 1500215EU LANDING GEAR TRIPPED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07836JS 732 FLIGHT 4114 - AIRCRAFT RETURNED TO GATE AFTER FLIGHT CREW WAS UNABLE TO RETRACT LANDING GEAR. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DAY/MX INSPECTED AIRCRAFT AND DISCOVERED MAIN LANDING GEAR EMERGENCY EXTENSION BYPASS PIN TRIPPED, RESET PIN IAW MM 32-00-00. CONDUCTED A LANDING GEAR RETRACT TEST, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19950818003941995081800394 1995 8 18 95ZZZM241 319950724A61124E30171 DE-ICE BFGOODRICH BEECH 1900 1900D 1154162CE RT PROP MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01844CA1351 UE45 DE-ICE BOOT NOT MAINTAINING BOND TO PROPELLER BLADE. ONE BOOT SEPARATED IN FLIGHT FROM BLADE S/N 409MA. BOOT WAS INSTALLED AT OVERHAUL BY HARTZELL ON 11/18/94 NEW BOOT WAS INSTALLED IAW CHAPTER 30 OF BEECH MANUAL. (M) 2L72 4T RTA24CE 19950818003951995081800395EA 1995 8 18 95ZZZM242 219950705A73203032125 P3 LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE CRACKED A AMWAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0780ZR UC80 COMING OUT OF OMA LEFT ENGINE LOST TORQUE, CREW SHUT DOWN LEFT ENGINE AND RETURNED TO OMA. MAINTENANCE FOUND P3 LINE CRACKED. REPLACED LINE OPS CHECKED NORMAL. (M) 2L72 4T4 TRTA24CE E4EA 19950818003961995081800396WP 1995 8 18 95ZZZM243 119950711A323047783031 RETRACT PIN DOUG 5759145506 DOUG DC8 DC863 302198AWP RT MLG SHEARED A ARRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15951R 5870 P2184 46092 FLT NR 003 31J-KCLT, DURING GEAR RETRACTION AFTER TAKEOFF FELT A HUGE THUD WITH AIRCRAFT SHUDDER. RESULTING INDICATIONS WERE RED GEAR UNSAFE LIGHT AND RED DOOR UNLATCHED LIGHT ON MAIN AND NOSE GEAR. LIGHTS OUT WITH GEAR HANDLE UP. PROCEEDED WITH EMERGENCY CHECK LIST PRIOR TO RETURNING TO 31J. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG RETRACT PIN SHEARED. REMOVED AND REPLACED RT MLG RETRACT PIN, DOWN LOCK SWITCH, AND CONNECTOR. GEAR RETRACTION WAS SATISFACTORY PER MM CHAPTER 32. 2L74 4F 4A25 19950818003971995081800397WP 1995 8 18 95ZZZM244 119950706A27403648166501 SPROCKET ASSY DOUG DC8 DC871 302199AWP HORIZ STAB SHEARED RIVETS A RRXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP158177U 45983 FLT NR 001 - KOAK-KSMF - WHILE EN ROUTE TO KSMF HORIZONTAL STAB JAMMED. CREW ADVISED TO RETURN TO KOAK. AIRCRAFT RETURNED TO KOAK. MAINTENANCE FOUND SHEAR RIVETS ON UPPER SPROCKET SHEARED. REMOVED AND REPLACED HORIZONTAL STAB SPROCKET ASSEMBLY IAW MM 27-42-09. OPS CHECK GOOD. NO LEAKS NOTED. (M) 2L74 4F 4A25 19950818003981995081800398WP 1995 8 18 95ZZZM245 119950708A2612 FIRE LOOP DOUG DC8 DC863 302198AWP NR 3 ENGINE DISCONNECTED A RRXAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 WP15797AL 46163 FLT 010 - KDAY-KSJC - ON CLIMB-OUT PASSING FL 240 NR 3 ENGINE FIRE LIGHT ILLUMINATED AND FIRE BELL SOUNDED. NR 3 PNEUMATIC SWITCH WAS TURNED OFF WITH NO CHANGE. ALL OTHER INDICATIONS NORMAL. SHUT ENGINE DOWN PER ENGINE FIRE CHECK LIST. LIGHT AND BELL WENT OUT WHEN FUEL LEVER WAS SHUT OFF. KSJC MX CHECKED ENGINE AIR, FUEL, AND HYDRAULICS FOR LEAKS DURING GROUND RUN. NONE NOTED. CLEANED FIRE LOOP CONNECTORS AND FOUND UPPER LOOP CONNECTOR GROUND WIRE OFF GROUNDING STUD. REPLACED CONNECTOR ON GROUND AN RECONNECTED GROUND WIRE. NR 3 ENGNE CHECKS NORMAL, OK FOR SERVICE. 2L74 4F 4A25 19950818003991995081800399 1995 8 18 95ZZZM246 319950718A6140YD4N RELAY DHAV DHC8 DHC8102 2809003NM NR 1 PROP FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07979HA4026 373 FLT NR 3236 - LYH-DCA - WHILE PERFORMING AUTOFEATHER TEST ON PREFLIGHT CHECK, THE NR 1 TORQUE INDICATOR DOES NOT INCREASE WHEN 'TEST' SWITCH IS SELECTED. CLEANED THE 7700-P3 CONNECTOR AND REMOVED AND REPLACED THE 6121-K3 RELAY AS A PRECAUTION. 2H72 4T RTA13NM 19950818004001995081800400NM 1995 8 18 95ZZZM247 119950719A323282970018011 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07921HA14414754 0426 089 FLT 3017 - TPA-TLH - AFTER GEAR WAS SELECTED UP, THE LEFT MAIN FORWARD GEAR DOOR OPENED UP AFTER GEAR RETRACTION. RECYCLED GEAR AND THE DOOR CLOSED. CONTINUED ON TO TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR FORWARD DOOR ACTUATOR. 2H72 4T RTA13NM 19950818004011995081800401NM 1995 8 18 95ZZZM248 119950719A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07975HA1188211874 85 176 FLT NR 3111 - PHL-LYH - ON APPROACH TO LYH, SELECTED GEAR DOWN AND GEAR FAILED TO EXTEND. THREE UNSAFE LIGHTS WERE ILLUMINATED. THE CREW PERFORMED THE ALTERNATE EXTENSION AND LANDED IN LYH WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. 2H72 4T RTA13NM 19950818004021995081800402NM 1995 8 18 95ZZZM249 119950720A771230005000046 TSEU SIMMONDS DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE MALFUNCTION A HNAACD ABORTED TAKEOFF RETURN TO BLOCK JR WARNING INDICATION PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA07912HA3014 3014 4266 40 FLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONTROL AND THE NR 1 ENGINE T1.8 SENSOR. 2H72 4T RTA13NM 19950818004031995081800403NM 1995 8 18 95ZZZM250 119950720A77123034652 SENSOR PWA DHAV DHC8 DHC8102 2809003NM NR 1 ENG T1.8 MALFUNCTION A HNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA07912HA2494824948 00463 40 FLT 3409 - FLL-TPA - WHILE ATTEMPTING TO SET TAKEOFF POWER, NR 1 ENGINE TORQUE DID NOT COME UP AND PROPELLER WENT INTO FEATHER. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR ELECTRONIC CONTROL AND THE NR 1 ENGINE T1.8 SENSOR. 2H72 4T RTA13NM 19950818004041995081800404NE 1995 8 18 95ZZZM251 219950716A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT DEFECTIVE A NVEAK NONE B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO03177AE 340B177 785369 FLT NR 7910 - BNA - CREW REPORTED A SMOKE LIKE SMELL IN THE COCKPIT. THIS AIRCRAFT WAS ON A FUNCTIONAL CHECK FLIGHT FOR A DUEL PROP REMOVAL. HANGAR MECHANICS FOUND OIL IN THE 'A' SUMP OF THE RT ENGINE. FURTHER TROUBLESHOOTING FOUND RT ENGINE TO BE DEFECTIVE. 2L72 4T4 TRTA52EU E8NE 19950818004051995081800405WP 1995 8 18 95ZZZM252 119950726A3350 EEL DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11917VV 47323 EMERGENCY FLOOD LIGHTS OVER FORWARD FLIGHT ATTENDANT SEAT TO ILLUMINATED SLIDES AND RI LIGHT STAYS ON. PLACED EMERGENCY EXTERIOR LIGHTS ON MEL 33.20. 2L72 4F A6WE 19950818004061995081800406WP 1995 8 18 95ZZZM253 119950726A3260 CONNECTOR DOUG DC9 DC932 3022066WP NLG UPLOCK LOOSE A VJ6AO OTHER P NO WARNING INDICATION DEDESCENT 1 SO11909VJ 47322 FLT 120 - TPA-ATL - ON APPROACH TO ATL DID NOT HAVE GEAR WARNING HORN. FOUND CANNON PLUG LOOSE ON NOSE GEAR UPLOCK SWITCH. CLEANED CANNON PLUG AND SECURED. ALL GEAR LIGHTS OPERATE NORMALLY IAW MM 32-60. 2L72 4F A6WE 19950818004071995081800407WP 1995 8 18 95ZZZM254 119950706A5242 DOOR DOUG DC9 DC932 3022066WP E/E COMPT NOT SECURED A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11937VV 45774 FLT NR 591 - ATL-MIA - RETURNED TO ATL BECAUSE THE AIRCRAFT WOULD NOT PRESSURIZE. RESECURED THE E/E DOOR. (M) 2L72 4F A6WE 19950818004081995081800408CE 1995 8 18 95ZZZM255 119950714A24301013647151 POWER PANEL BEECH 1900 1900C 1154161CE RIGHT MALFUNCTIONED A PLGAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 NE05823BE UB66 FLT 4306 RETURNED TO BOS DUE TO A RIGHT HAND GENERATOR TIE LIGHT FOLLOWED BY ABNORMAL BUSS VOLTAGE PROBLEMS. THE AIRCRAFT RETURNED TO BOS WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REPLACED THE RIGHT HAND DC POWER PANEL AND BOTH GENERATOR CONTROL UNITS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19950818004091995081800409NM 1995 8 18 95ZZZM256 119950612A7920AS43013154 PACKING BOEING757 75723APF 1384966NM PRESSURE FILTER BROKEN A CLCAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19571CA 24456 FLT 044 - MRCO - ON CLIMB-OUT, LEFT ENGINE OIL QUANTITY ZERO. OIL PRESSURE LOW, 16 PSI. ENGINE WAS SHUTDOWN. FOUND PRESSURE FILTER HOUSING PACKING BROKEN, REPLACED PER MM 79-21-07. RESERVICED ENGINE. RUNUP, OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19950818004101995081800410WP 1995 8 18 95ZZZM257 119950707A541457530101 PLANK DOUG DC8 DC863F 302198FWP NR 1 PYLON CRACK A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING PREFLIGHT, FOUND CRACK ON NR 1 PYLON OUTBOARD SIDE LOWER PLANK STATION YN 277.8. REMOVED FASTENERS IN AREA FABRICATE DOUBLER FROM 7075-T6 .125 AND TRIPLERS FROM 7075-T6 .190 AND .160, LOCATE DRILL UP. TREATED AND PRIMED AND INSTALLED IAW DOUGLAS NR GLP01505 AND FILE NR 273426. 2L74 4F 4A25 19950818004111995081800411WP 1995 8 18 95ZZZM258 119950714A541457530111 PLANK DOUG DC8 DC863F 302198FWP NR 1 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING PREFLIGHT, FOUND CRACK AT NR 1 INTERMEDIATE PYLON PLANK, PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABRICATE NEW DOUBLER AND TRIPLER, TREATED, PRIMED AND INSTALLED IAW DAC GL PO 1505. 2L74 4F 4A25 19950818004121995081800412WP 1995 8 18 95ZZZM259 119950705A540037530272 FITTING DOUG DC8 DC863F 302198FWP NR 1 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 AFTER REMOVING NR 1 PYLON INTERMEDIATE PLANK FOR REPAIR, FOUND A CRACKED TEE FITTING ON THE INBOARD SIDE OF PYLON AT YN 336.750. REMOVED FITTING, FABRICATED NEW FITTING AS PER DOUGLAS DRAWING NR 5753022, TEE FITTING NR 3753027-2 UNDER DOUGLAS AT AUTHORIZATION FILE C1-P63-ATM/056 DATED 07-06-95. INSTALLED TEE FITTING IAW SRM 51-3-0.. 2L74 4F 4A25 19950818004131995081800413WP 1995 8 18 95ZZZM260 119950710A523047778651 FITTING DOUG DC8 DC863F 302198FWP MAIN CARGO DOOR CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19661AV 45969 DURING REPAIRS ON MAIN CARGO DOOR ACT SUPPORT FITTING, FOUND THE SIDE SUPPORT BRACKET CRACKED. REMOVED CRACKED FITTING, FABRICATED NEW FITTING AUTHORIZED BY DAC FILE C1-P63-15M/060 DATE JULY 10, 1995 IAW DRAWING 4777865 LOCATE DRILLED UP, TREATED PRIME AND INSTALLED IAW SRM 51-3-0. 2L74 4F 4A25 19950818004141995081800414NM 1995 8 18 95ZZZM261 119950715A3310BACC18ZSR CIRCUIT BREAKER BOEING747 747246F NM UPPER DECK FELL APART A SRAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO19740SJ 22477 CREW REPORTED THAT THE UPPER DECK CREW REST READING LIGHT CIRCUIT BREAKER FELL APART AND SMOKED. CREW REST LIGHT WAS ALSO SMOKING. SECURED LIGHT OFF AND LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER AND LAMP ASSY PER MM CH 24 AND 33. 2L74 4F A20WE 19950818004151995081800415NM 1995 8 18 ASAA9510070 119950712A5315 FLOOR BEAM BOEING737 737290C 138448VNM BS 520 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01730AS38605 22577 SEA- DURING C-CHECK, CORROSION WAS FOUND ON THE UPPER FORWARD FLANGE OF THE FLOOR BEAM AT BS 520, RBL 9.50, 15.375 AND 20. PERFORMED INTERIM REPAIR PER EA 5310-01371 AND BOEING TELEX ASA-SEA-95-0440RR. (M) 2L72 4F A16WE 19950818004161995081800416SO 1995 8 18 C2XA95IA129 119950725A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 15, AND NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M0 2L72 4T RTA31SO 19950818004171995081800417SO 1995 8 18 C2XA95IA130 119950725A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 15, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004181995081800418SO 1995 8 18 C2XA95IA131 119950725A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 16, NR 2, NR 3, AND NR 4 UPPER SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004191995081800419SO 1995 8 18 C2XA95IA132 119950725A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 21, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004201995081800420SO 1995 8 18 C2XA95IA133 119950725A572012017060009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 19, NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004211995081800421SO 1995 8 18 C2XA95IA134 119950725A572012017056011 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 15, NR 3 LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004221995081800422SO 1995 8 18 C2XA95IA135 119950725A572012017056013 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004231995081800423SO 1995 8 18 C2XA95IA136 119950725A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004241995081800424SO 1995 8 18 C2XA95IA137 119950725A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004251995081800425SO 1995 8 18 C2XA95IA138 119950725A572012017057006 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 16, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004261995081800426SO 1995 8 18 C2XA95IA139 119950725A572012017062013 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 20, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004271995081800427SO 1995 8 18 C2XA95IA140 119950725A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 20, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004281995081800428SO 1995 8 18 C2XA95IA141 119950725A572012017062013 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004291995081800429SO 1995 8 18 C2XA95IA143 119950725A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 22, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004301995081800430SO 1995 8 18 C2XA95IA144 119950725A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE LEFT INBOARD AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRACK SECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004311995081800431SO 1995 8 18 C2XA95IA145 119950725A5720124350003 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, PRESSURE REFUEL SHUTOFF VALVE SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004321995081800432SO 1995 8 18 C2XA95IA146 119950725A571312016079002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 8, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND AFFECTED PORTION OF THE STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB FAX NR EST .234/95. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004331995081800433SO 1995 8 18 C2XA95IA147 119950725A571312016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE AFFECTED PORTION OF THE STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB FAX NR EST .234/95. THE AIRCRAFT WAS THE APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004341995081800434SO 1995 8 18 C2XAIA142 119950725A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0919704 120086 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950818004351995081800435WP 1995 8 18 ORJA9560 119950724A33500105606003 EEL MODULE DOUG DC9 DC983 3022083WP CABIN INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11834RA 53124 EMERGENCY AISLE LIGHTS, ONE SECTION INOP. REMOVED AND REPLACED EMERGENCY LIGHTING LAMP MODULE ASSY. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 19950818004361995081800436WP 1995 8 18 ORJA9561 119950718A5320 JAMB DOUG DC9 DC982 3022082WP E/E DOOR CUTOUT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11840RA 49424 CORROSION NUMEROUS PLACES ON E/E BAY DOOR CUTOUT SURROUND JAMB. REMOVED CORROSION, TREAT AND PRIME PER DOUGLAS SRM 5110-3 AND 3B. (M) 2L72 4F A6WE 19950818004371995081800437WP 1995 8 18 ORJA9562 119950717A53205936469IN BRACKET DOUG DC9 DC982 3022082WP CARGO DR CUTOUT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11840RA 49424 AFT CARGO COMPARTMENT DOOR CUTOUT HAS CORROSION ON BRACKET IN THE AFT LOWER CORNER. REMOVED AFT CARGO COMPARTMENT DOOR AFT LOWER CORNER BRACKET AND INSTALLED NEW ONE IAW MD-80-SRM 51-60-0, 51-30-5. (M) 2L72 4F A6WE 19950818004381995081800438WP 1995 8 18 ORJA9563 119950718A5320 BRACKET DOUG DC9 DC982 3022082WP CARGO DR CUOUT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11840RA 49424 MID CARGO PIT DOOR CUTOUT HAS CORROSION ON BRACKET IN LOWER AFT CORNER. REMOVED CORROSION IN REF 53-05. (M) 2L72 4F A6WE 19950818004391995081800439WP 1995 8 18 ORJA9564 119950717A532059364692N BRACKET DOUG DC9 DC982 3022082WP CARGO DR CUTOUT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11840RA 49424 AFT CARGO COMPARTMENT DOOR CUTOUT HAS CORROSION ON BRACKET IN THE FWD LOWER CORNER. REMOVED AFT CARGO COMPARTMENT DOOR FORWARD LOWER CORNER BRACKET AND INSTALLED NEW BRACKET IAW MD 80 SRM 51-60-0 AND 51-30-5. (M) 2L72 4F A6WE 19950818004401995081800440WP 1995 8 18 ORJA9565 119950718A5320 BRACKET DOUG DC9 DC982 3022082WP CARGO DR CUT OUTCORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11840RA 49424 MID CARGO PIT DOOR CUTOUT HAS CORROSION ON BRACKET IN LOWER FORWARD CORNER. REMOVED CORROSION IN REF 53-05. (M) 2L72 4F A6WE 19950818004411995081800441CE 1995 8 18 PLGA71495G1 119950714A243051538001A GCU BEECH 1900 1900C 1154161CE RIGHT MALFUNCTIONED A PLGAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 NE05823BE UB66 FLT 4306 RETURNED TO BOS DUE TO A RIGHT HAND GENERATOR TIE LIGHT FOLLOWED BY ABNORMAL BUSS VOLTAGE PROBLEMS. THE AIRCRAFT RETURNED TO BOS WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REPLACED THE RIGHT HAND DC POWER PANEL AND BOTH GENERATOR CONTROL UNITS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19950818004421995081800442NE 1995 8 18 PLGA71595G1 219950715A72506038T39P05 BLADE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE STG 1 ROTOR FAILED A PLGACD ABORTED TAKEOFF RETURN TO BLOCK M OVER TEMP TOTAKEOFF 1 NE05343BE 340A101 367385 BOS\BGR - FLT 4570 - DURING TAKEOFF, THE CREW HEARD A LOUD BANG WHEN CTOT WAS TURNED OFF. THE TAKEOFF WAS ABORTED. THE CREW NOTED THE RIGHT ENGINE ITT REMAINED AT 1000 DEGREES AFTER RETARDING THE POWER LEVERS. AFTER TURNING OFF THE RUNWAY, THE ENGINE SHUT DOWN UNCOMMANDED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACED THE ENGINE. THIS SDR IS TO CLOSE OUT AN OPEN SDR DATED 7-15-95 FOR FLT 4570, BOS TO BGR IN WHICH THE FLIGHT CREW HEARD A LOUD BANG WHEN CTOT WAS SELECTED OFF. TEAR-DOWN INSPECTION OF THE ENGINE REVEALED FAILURE OF A STGI GG ROTOR BLADE BELOW THE BLADE PLATFORM. (X) 2L72 4T4 TRTA52EU E8NE6 19950818004431995081800443NM 1995 8 18 TSAA9552138 119950710A5230 FRAME BOEING737 7372S5C 1384499NM CARGO DOOR CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, APPROXIMATE 1.5 INCHES LONG CRACK FOUND ON FWD CARGO DOOR AFT FRAME (INNER) AS EVIDENT. REPLACED FRAME PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004441995081800444NM 1995 8 18 TSAA9553134 119950710A5311 FRAME BOEING737 7372S5C 1384499NM BS 460 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING MAINTENANCE VISIT, CRACK APPROXIMATELY 3.5 INCHES LONG FOUND ON FUSELAGE LOWER LOBE LEFT SIDE FRAME STATION 460 AS EVIDENT BTW STRINGER 21L AND STRINGER 22L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004451995081800445NM 1995 8 18 TSAA9553135 119950710A5311 FRAME BOEING737 7372S5C 1384499NM BS 480 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, CRACK APPROXIMATELY 3.5 INCHES LONG FOUND ON FUSELAGE LOWER LOBE, LEFT SIDE FRAME STATION 480 AS EVIDENT BETWEEN STRINGER 21L AND STRINGER 22L. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004461995081800446NM 1995 8 18 TSAA9553137 119950710A5311 FRAME BOEING737 7372S5C 1384499NM BS 530 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND FRAME CRACKED AT BS 530, STRINGER R23R. REPAIRED PER SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004471995081800447NM 1995 8 18 TSAA9553139 119950710A5347 SEAT TRACK BOEING737 7372S5C 1384499NM BS 344 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, CABIN SEAT TRACK AT STATION 344 RIGHT, 2ND TRACK FROM THE WALL, A LUG PORTION MISSING. REPAIRED PER ECO2605. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004481995081800448NM 1995 8 18 TSAA9553141 119950711A5320 VERT SUPPORT BOEING737 7372S5C 1384499NM AC COMPT CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON LEFT VERTICAL SUPPORT WEB, INSIDE EXTERNAL AIR COND ACCESS COMPARTMENT. REPAIRED PER ECO2588. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004491995081800449NM 1995 8 18 TSAA9553142 119950711A5330 SKIN BOEING737 7372S5C 1384499NM BS 908 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENACNE VISIT, FOUND CORROSION BULGE AT BS 908 MINUS 1 INCH AND STRINGER 23L. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004501995081800450NM 1995 8 18 TSAA9553143 119950711A5347 SEAT TRACK BOEING737 7372S5C 1384499NM CABIN CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FATIGUE/STRESS CRACKS FOUND ON SEAT TRACK (O/B ONE) ON FLOOR PANEL NR F-9 AS EVIDENT. REPAIRED PER SRM 53-10-5 FIG 7. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004511995081800451NM 1995 8 18 TSAA9553144 119950711A5347 SEAT TRACK BOEING737 7372S5C 1384499NM CABIN CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURNG HEAVY MAINTENANCE VISIT, CORROSION FOUND ON SEAT TRACK LOCATED AT PANEL NR F-11 (O/B ONE) BETWEEN TRACK HOLD DOWN FASTENERS AS EVIDENT. CLEAN AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004521995081800452NM 1995 8 18 TSAA9553145 119950711A5320 STIFFENER BOEING737 7372S5C 1384499NM BS 1128 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, VERTICAL STIFFENER APU TORQUE BOX AFT SIDE OF APU INLET BS 1128 HAS STRESS CORROSION. REPLACED STIFFENER PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004531995081800453NM 1995 8 18 TSAA9553147 119950711A53206546579540 CHORD BOEING737 7372S5C 1384499NM BS 1109 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, LOWER RIGHT CHORD BS 1109 APU TORQUE BOX CORRODED. REPLACED CHORD PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004541995081800454NM 1995 8 18 TSAA9553148 119950711A5320 SUPPORT BOEING737 7372S5C 1384499NM BS 847-947 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, SURFACE CORROSION ON FLOOR SUPPORT STRIP ABOVE 25R, BS 847 TO BS 947. REPAIRED PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004551995081800455NM 1995 8 18 TSAA9553149 119950711A53206546579510 STIFFENER BOEING737 7372S5C 1384499NM BS 1128 EXFOLIATED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, VERTICAL STIFFENER BS 1128 FWD SIDE EXFOLIATED. REPLACED STIFFENER PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004561995081800456NM 1995 8 18 TSAA9553150 119950711A5313 STRIGNER BOEING737 7372S5C 1384499NM BS 1124 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND STRINGER 17AR AT BS 1124 LOWR FLANGE CORRODED. REPAIRED PER SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004571995081800457NM 1995 8 18 TSAA9553151 119950711A5330 SKIN BOEING737 7372S5C 1384499NM APU DOOR CUTOUT CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND FUSELAGE SKIN BY THE APU DOR HINGE CUTOUT (FWD AND AFT) CRACKED. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004581995081800458NM 1995 8 18 TSAA9553154 119950711A5330 SKIN BOEING737 7372S5C 1384499NM BS 1064 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION BULGE AT S20L LAP JOINT AND BS 1064. OPENED LAP JOINT, REMOVED CORROSION AND CLOSED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004591995081800459NM 1995 8 18 TSAA9553155 119950711A5313 STRINGER BOEING737 7372S5C 1384499NM BS 927 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON STRINGER 26L AT BS 927 PLUS 4 INCHES. REPAIRED PER ECO2599. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004601995081800460NM 1995 8 18 TSAA9553156 119950711A4910 APU INLET BOEING737 7372S5C 1384499NM BS 1088 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION AROUND APU INLET DUCT CUTOUT AT BS 1088. REPAIRED PER ECO 198OR6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004611995081800461NM 1995 8 18 TSAA9553157 119950711A5330 SKIN BOEING737 7372S5C 1384499NM BS 787 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON THE FUSELAGE SKIN BETWEEN S-24L AND S-25L AT BS 787. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004621995081800462NM 1995 8 18 TSAA9555127 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 81. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004631995081800463NM 1995 8 18 TSAA9555128 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENACNE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT VERTICAL STABILIZER REAR SPAR AT FS 86. REPAIRED PER ECO2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004641995081800464NM 1995 8 18 TSAA9555129 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 201. REPAIRED PER ECO 2509 PART II. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004651995081800465NM 1995 8 18 TSAA9555130 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURNG HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 195. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004661995081800466NM 1995 8 18 TSAA9555131 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 158. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004671995081800467NM 1995 8 18 TSAA9555132 119950710A5531 REAR SPAR BOEING737 7372S5C 1384499NM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON LEFT VERTICAL STABILIZER REAR SPAR AT FS 132. REPAIRED PER ECO2509 PART 2. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004681995081800468NM 1995 8 18 TSAA9555133 119950710A5510 BEAM BOEING737 7372S5C 1384499NM RT HORIZ STAB TECORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON RT HORIZONTAL STABILIZER LOWER T/E BEAM AT STRINGER 125, ELS 76.45. REPAIRED PER ECO1584R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004691995081800469NM 1995 8 18 TSAA9555152 119950711A5511 RIB BOEING737 7372S5C 1384499NM RT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, RIGHT HORIZONTAL STABILIZER LOWER CHORD OF RIB AT BALANCE PANEL AREA STRINGER 221.5 HAS EXFOLIATION CORROSION. REPLACED PANEL PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004701995081800470NM 1995 8 18 TSAA9555153 119950710A5511 RIB BOEING737 7372S5C 1384499NM RT HORIZ STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, RIGHT HORIZONTAL STABILIZER LOWER CHORD OF RIB AT BALANCE PANEL AREA STRINGER 166.3 HAS EXFOLIATION CORROSION. CLEANED AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004711995081800471NM 1995 8 18 TSAA9556140 119950711A5320 WINDOW FRAME BOEING737 7372S5C 1384499NM CABIN CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, WINDOW FRAME AT 13R EXFOLIATION CORROSION NOTED ON THE FWD LOWER CORNER. REPAIRED PER SRM 56-20-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004721995081800472NM 1995 8 18 TSAA9557136 119950710A5720 FASTENERS BOEING737 7372S5C 1384499NM LT WING LOOSE A TSAAK NONE K FLUID LOSS ININSP/MAINT 1 WP13802AL 22148 DURING HEAVY MAINTENANCE VISIT, FUEL LEAK AT LEFT WING INBOARD SKATE ANGLE FASTENERS. REPAIRED PER ECO1699 DEV A. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950818004731995081800473WP 1995 8 18 USAA950609 119950617A3260 INDICATION DOUG DC9 DC931 3022065WP GEAR DOORS MALFUNCTIONED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19978VJ 47371 CLT - FLT NR 1187 - RETURN TO FIELD DUE TO AN INDICATION THAT THE GEAR DOOR WAS OPEN. JACKED AIRCRAFT, CHECKED ALL LANDING GEAR INDICATION SWITCHES AND MECH. NO DEFECTS NOTED. CYCLED GEAR. ALL INDICATIONS GOOD. (M) 2L72 4F A6WE 19950818004741995081800474WP 1995 8 18 USAA950648 119950629A3240500432114 BRAKE ASSY DOUG DC9 DC981 3022081WP LEFT FAULTY A USAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA19803US 48035 MCO - FLT NR 1136 - UPON TAXIING FOR DEPARTURE, THE LEFT BRAKE SEIZED. SUBSEQUENTLY, THE NR 1 TIRE WENT FLAT. CAPTAIN DECIDED TO RETURN TO THE GATE. MAINTENANCE REPLACED THE NR 1 BRAKE ASSEMBLY, AND THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES P/N 32935. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950818004751995081800475WP 1995 8 18 USAA950650 119950627A323029170031 SPRING DOUG DC9 DC931 3022065WP LANDING GEAR MISSING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19923VJ 48143 BWI - FLT 0589 - ON TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO BWI. MAINTENANCE REPLACED THE ASSIST SPRING. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950818004761995081800476WP 1995 8 18 USAA950754 119950715A3222 O-RING DOUG DC9 DC981 3022081WP NLG STRUT FAULTY A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19828US 48028 FLT NR 0417 - TPA - THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. THE GEAR WAS RECYCLED THREE TIMES BUT GEAR STILL WOULD NOT RETRACT. FLIGHT DIVERTED TO TPA. MAINTENANCE REPLACED O-RING AT THE NOSE STRUT SCHRADER VALVE. THE STRUT WAS SERVICED AND THE GEAR CYCLED. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950818004771995081800477EU 1995 8 18 VTZA95231 119950721A3233AIR864961 RETRACTION JACK JETAIRJETSTMJETSTM4101 1500501EU RT MAIN FAILURE A VTZAO OTHER J WARNING INDICATION APAPPROACH 1 EA27312UE 41025 FLT NR 6462 - EWR-IAD - DURING APPROACH AIRCRAFT LEFT MAIN GEAR DID NOT EXTEND UNTIL ACTUATED A SECOND TIME. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT MAIN GEAR RETRACTION JACK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950818004781995081800478EU 1995 8 18 VTZA95232 119950721A3233AIR864961 RETRACTION JACK JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27314UE 41027 FLT NR 6500 - PWM-IAD - DURING CLIMB-OUT RETURNED TO PWM DUE TO THE RIGHT MAIN LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. AIRCRAFT LANDED AT PWM WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT MAIN GEAR RETRACTION JACK. AIRCRAFT WAS RELEASED ADN APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950818004791995081800479EU 1995 8 18 VTZA95233 119950721A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27484UE 899 FLT NR 6565 - IAD-GSO - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950818004801995081800480EU 1995 8 18 VTZA95234 119950723A243523095002 STARTER GEN JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A VTZAB EMER. DESCENT EH VIBRATION/BUFFET ELECT. POWER LOSS-50 PC CRCRUISE 1 EA27322UE 41058 FLT 6409 - PWM-IAD - DURING CRUISE DIVERTED TO BOS DUE TO THE LEFT GENERATOR FALLING OFF LINE FOLLOWED BY ENGINE VIBRATION. THE ENGINE WAS NOT SHUT DOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT BOS WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT STARTER GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950818004811995081800481EU 1995 8 18 VTZA95235 119950725A21302758A000 PRESSURE SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27370MT 800 FLT NR 6326 - IAD-ROC - DURING TAKEOFF ABORTED THE TAKEOFF DUE TO THE RIGHT AIR OFF LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE AIR OFF PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950818004821995081800482WP 1995 8 18 WRLA95037 119950725A335058785 EEL DOUG DC10 DC1030 3023501WP CABIN BROKEN A WRLAK NONE L NO TEST ININSP/MAINT 1 EA273024W 48318 DURING PREFLIGHT, CREW NOTED ESCAPE PATH LIGHT FLOOR LIGHT STRIP, 'A' ZONE RIGHT FORWARD CENTER PARTITION AREA INOPERATIVE. REMOVED AND REPLACED LIGHT STRIPS, LAMPS AND HARNESSES. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A22WE 19950818004831995081800483NE 1995 8 18 Y2PA95009 219950814A7260667488 GEARBOX DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE ENGINE FAILED A Y2PAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23197US AA0153 47154 655239 PIA - SHUT DOWN THE ENGINE. DECLARED AN EMERGENCY WITH CHI CENTER, REQUESTED VECTORS TO THE NEAREST AIRPORT. MADE AND UNSCHEDULED LANDING AT PIA. REPLACED THE MAIN ENGINE ACCESSORY GEAR BOX. (M) 2L72 4F4 F A6WE E2EA 19950818004841995081800484WP 1995 8 18 95ZZZM262 119950713A5230 SEAL DOUG DC8 DC863F 302198FWP MAIN CARGO DOOR LEAKING A ARWAB EMER. DESCENT O OTHER CLCLIMB 1 SO19441J 45988 AIR TURN BACK WITH 4 TC'S ON, CABIN CLIMB AT 1,000 FT/MIN WHEN AIRCRAFT REACHED 20,000 FEET CARGO DOOR SEAL LEAKING, CABIN WENT TO 11,000 FEET. INSTALLED NEW BACKUP SEAL ON ENTIRE MAIN CARGO DOOR AFTER AIRCRAFT WAS LEAK CHECKED AT BLAST FENCE WITH SMOKE CANISTERS. PRESSURIZED AIRCRAFT IAW MM 21-30. NO LEAKS NOTED ON MAIN CARGO DOOR. 2L74 4F 4A25 19950818004851995081800485WP 1995 8 18 95ZZZM263 119950425A573057695832 SLOT DOOR DOUG DC8 DC862 3021970WP RT WING LE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 ON A-CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. REMOVED SLOT DOOR L/E. CUT OUT DAMAGED AREAS, FABRICATED ADN INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E. 2L74 4F 4A25 19950818004861995081800486WP 1995 8 18 95ZZZM264 119950425A573057695831 SLOT DOOR DOUG DC8 DC862 3021970WP LT WING LE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 ON A-CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL 2 CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE. REMOVED SLOT DOOR L/E SECTION, CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW SRM 57-2-1 FIG 2H. REINSTALLED SLOT DOOR L/E. 2L74 4F 4A25 19950818004871995081800487WP 1995 8 18 95ZZZM265 119950703A5522 SKIN DOUG DC8 DC862 3021970WP LT ELEVATOR CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 LEFT ELEVATOR LOWER SKIN HAS LEVEL 2 CORROSION AT XE 195.33. SKIN SECTION REMOVED. FABRICATED NEW SKIN USING OLD AS TEMPLATE. INSTALLED NEW SKIN SECTION IAW SRM 55-2-0, 51-1-8 AND 51-1-21. REBALANCED ELEVATOR IAW SRM 51-4-4, DC8 SB 27-185 AND DOUGLAS FAX FILE NR 272283. 2L74 4F 4A25 19950818004881995081800488WP 1995 8 18 95ZZZM266 119950705A5520 FITTING DOUG DC8 DC862 3021970WP LT ELEVATOR CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 DURING PREFLIGHT MAINTENANCE CHECK, FOUND LEFT ELEVATOR OUTBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED LEFT OUTBOARD HINGE FITTING IAW MM 55-50-0. 2L74 4F 4A25 19950818004891995081800489WP 1995 8 18 95ZZZM267 119950529A5522 TE SKIN DOUG DC8 DC862 3021970WP LT ELEVATOR CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 FOUND LEVEL 2 CORROSION LEFT ELEVATOR OUTBOARD STATIC WICK ATTACH POINT. REMOVED LEFT ELEVATOR. REMOVED DAMAGED T/E SECTION. FABRICATED AND INSTALLED NEW T/E SECTION IAW SRM 51-1-21A. INSTALLED NEW STATIC WICK BASE IAW MM 23-60-00. REINSTALLED ELEVATOR AFTER BALANCING. 2L74 4F 4A25 19950818004901995081800490WP 1995 8 18 95ZZZM268 119950703A53135613861329 LONGERON DOUG DC8 DC862 3021970WP FS 208 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 POPPED RIVET HEADS AND SKIN BULGE AT FS 208.00 AT LONGERON 28R. REMOVED SECTION OF LONGERON 28R AND TWO INTERCOSTALS. FOUND LEVEL 2 CORROSION ON L-28R. REPLACED 20 INCH SECTION OF L-28R AND REINSTALLED INTERCOSTALS PICKING EXISTING HOLES IAW SRM 53-2-2 AND 51-1-21. 2L74 4F 4A25 19950818004911995081800491WP 1995 8 18 95ZZZM269 119950618A323156496992 DOOR DOUG DC8 DC873F 302199FWP NLG LACK OF LUBE A DHLAAJ UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CLCLIMB 1 SO01803DH 46123 SUSPECT NOSE GEAR LANDING DOOR DID NOT CLOSE ON TAKEOFF, LOUD RUMBLING SOUND AND HEAVY VIBRATION IN NOISE GEAR AREA. PERFORMED FUEL DUMP ABNORMAL PROCEDURE FOR LANDING. FOUND RIGHT GEAR DOOR DOWN, PERFORMED INSPECTION, UNLOCK PIN STICKING, CLEANED AND LUBED OPS CHECKS OK IAW MM 32-22-01. 2L74 4F RT4A25 19950818004921995081800492WP 1995 8 18 95ZZZM270 119950620A291076140312090 PIPE ASSY DOUG DC8 DC873F 302199FWP BS 938-980 CHAFED A DHLAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01805DH 46125 DURING CRUISE OBSERVED HYDRAULIC QUANTITY LOSS TO AUX LEVEL. PERFORMED ALL APPLICABLE ABNORMAL PROCEDURES AND CONTINUED FLIGHT. LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT ON ARRIVAL. FOUND 2 LINES (1 FLEX, 1 HARD) CHAFFING AND SPRAYING UNDER PRESSURE IN AND AT RUDDER SYSTEM PUMP. INSTALLED FLEX LINES AS INTERIM REPAIR IAW 20-01-01 DMI NRE273. 2L74 4F RT4A25 19950818004931995081800493EU 1995 8 18 95ZZZM271 119950530A3246 WHEEL BEARING BFGOODRICH 31485 BAG JETSTMJETSTM3101 1500215EU LT MLG DEFECTIVE A VNAAK NONE O OTHER ININSP/MAINT 1 GL07834JS 726 DURING A TIRE CHANGE IN LYN, A MAINTENANCE TECHNICIAN NOTICED SOME DAMAGE TO THE LEFT MAIN WHEEL ASSY. UPON REMOVAL OF THE WHEEL ASSY THEY ALSO NOTICED DAMAGE TO BRAKE ASSY AND WHEEL BEARINGS. MAINTENANCE REPLACED LEFT MAIN WHEEL, WHEEL BEARINGS, AND BRAKE ASSY IAW MM 32-40-00 AND REPLACED LEFT MLG AXLE WHICH WAS DAMAGED AS A RESULT OF BEARING FAILUE IAW MM 32-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950818004941995081800494NM 1995 8 18 95ZZZM272 119950617A2781H1010262 SWITCH BOEING727 7272Q9 138448MNM NR 6 LE SLAT LACK OF LUBE A DHLACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01740DH 21930 DURING TAKEOFF ROLL, BEFORE AIRSPEED CALL OUT, AMBER LEADING EDGE FLAP LIGHT FLICKERED. DURING TAXI BACK NR 6 LEADING EDGE SLAT GREEN LIGHT FLICKERED OFF AND ON, ON SECOND OFFICERS PANEL. CLEANED AND SECURED NR 6 LEADING EDGE SLAT POSITION INDICATOR SWITCH. OPS CHECKED OK PER MM 27-8-0. 2L73 4F RTA3WE 19950818004951995081800495NM 1995 8 18 95ZZZM273 119950706A77143039242 PULSE PICKUP DORNERDO32 DO328100 2996000NM RT ENG DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07424JS 3033 FLT NR 4007 - PIT-CHO - CREW NOTICED A FLUCTUATION IN RT ENGINE NH INDICATOR. ELECTED TO RETURN TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED A DEFECTIVE NH TRANSMITTER. REPLACED TRANSMITTER IAW MM 71-00-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950818004961995081800496NM 1995 8 18 95ZZZM274 119950611A24358160121 STARTER/GEN DORNERDO32 DO328100 2996000NM LT ENG DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07424JS 150 3033 FLT 4162 - AFTER TAKEOFF LEFT GENERATOR OVERHEAT CAPTION ILLUMINATED, AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED LEFT STARTER/GENERATOR IAW MM 24-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 19950818004971995081800497NE 1995 8 18 95ZZZM275 219950714A7261693905 OIL CAP DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE ENGINE SERVICEABLE A VJ6AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11901VJ 47275 657466 FLT NR 134 - FLL-ATL - AFTER TAKEOFF THE FLIGHT CREW NOTICED THE OIL QUANTITY DROP TO 4 QTS. THEY RETURNED TO FLL. MAINTENANCE FOUND A LOOSE OIL CAP. RESERVICED AND SECURED THE CAP, THE FLIGHT PROCEEDED WITHOUT FURTHER DELAY. (M) 2L72 4F4 F A6WE E2EA 19950818004981995081800498WP 1995 8 18 95ZZZM276 119950716A3350 EEL WIRE DOUG DC9 DC932 3022066WP COCKPIT FAILED A VJ6AK NONE O OTHER TXTAXI/GRND HDL 1 SO11917VV 47323 IN ATL, EMERGENCY LIGHTING SYSTEM WOULD NOT COME ON WITH FLIGHT DECK SWITCH. MAINTENANCE FOUND WIRE SHORTED ON SWITCH ASSY. REPAIRED WIRE PER MM 33. 2L72 4F A6WE 19950818004991995081800499WP 1995 8 18 95ZZZM277 119950715A5242 LATCH DOUG DC9 DC932 3022066WP E/E DOOR NOT SECURED A VJ6AA UNSCHED LANDING O OTHER TOTAKEOFF 1 SO11903VJ 47261 FLT NR 481 - IAD-MCO - AT TAKEOFF FLT CREW NOTICED E/E DOOR LIGHT CAME ON. CREW RETURNED TO IAD. MAINTENANCE SECURED DOOR LATCH AND DISPATCHED FOR CONTINUED SERVICE. 2L72 4F A6WE 19950818005001995081800500WP 1995 8 18 95ZZZM278 119950718A2731 RELAY TERMINALS DOUG DC9 DC932 3022066WP ELEV TRIM DIRTY A VJ6AA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO11937VV 45774 FLT 190 - ATL-FLL - AIR RETURN TO ATL DUE TO THE PRIMARY AND SECONDARY TRIM INOP IN NOSE DOWN POSITION. CLEANED STUDS NR 1503 AND 1511 PRIMARY TRIM RELAY TERMINALS. OPS CHECK GOOD PER MM 27-00. PRIMARY AND SECONDARY TRIM CHECK GOOD. 2L72 4F A6WE 19950818005011995081800501NM 1995 8 18 AALA951122 119950620A256031073105 SLIDE LATCH BOEING727 727223 1384074NM FWD DOORS FRAYED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A2216 ORD - DURING SHOP VISIT, EMERGENCY EVACUATION SLIDE LATCH ASSY FOUND FRAYED. REPLACED EMERGENCY EVACUATION SLIDE LATCH ASSY DURING REPAIR PROCESS. (M) 2L73 4F A3WE 19950818005021995081800502NM 1995 8 18 AALA951147 119950626A2560 BOTTLE BOEING727 727223 1384074NM AFT DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A2614 ORD - DURING SLIDE SHOP RECEIVING INSPECTION, EMERGENCY EVACUATION SLIDE P/N CBB3335, FOUND WITH LOW BOTTLE PRESSURE. REPLACED EMERGENCY EVACUATION SLIDE BOTTLE. (M) 2L73 4F A3WE 19950818005031995081800503 1995 8 18 AALA951165 419950629A2564D23835201 RAFT AIRCRUISERS BOEING727 727223 1384074NM CABIN OVERHEAD SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 649 LAX - DURING SHOP TEST DEPLOYMENT, LIFE RAFT FAILED LEAK CHECK DUE TO LARGE AREA LEAK BETWEEN UPPER AND LOWER TUBES. SCRAPPED LIFE RAFT. (M) 2L73 4F A3WE 19950818005041995081800504 1995 8 18 AALA951166 419950629A2564D23835201 RAFT AIRCRUISERS BOEING727 727223 1384074NM CABIN OVERHEAD SCRAPPED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 607 LAX - DURING SHOP TEST DEPLOYMENT, LIFE RAFT FAILED LEAK CHECK DUE TO DEGENERATION OF FABRIC. SCRAPPED LIFE RAFT. (M) 2L73 4F A3WE 19950818005051995081800505 1995 8 18 AALA951176 419950629A256531073105 SEAM AIRCRUISERS BOEING727 727223 1384074NM SLIDE SEPARATING A AALAK NONE O OTHER ININSP/MAINT 1 SW07889AA A2709 21527 ORD - DURING SLIDE SHOP RECEIVING INSPECTION, EMERGENCY EVACUATION SLIDE, P/N 31073105, SEAMS AT BOTTLE HOLDER FOUND SEPARATING. REGLUED AND PATCHED BOTTLE HOLDER SEAMS DURING SHOP REPAIR PROCESS. (M) 2L73 4F A3WE 19950818005061995081800506NM 1995 8 18 AALA951181 119950630A5240 ASSIST BOTTLE BOEING727 72723 1384004NM L4 DOOR REQ'D SERVICE A AALAK NONE O OTHER ININSP/MAINT 1 SW071909 19184 MIA - DURING OVERNIGHT CHECK, L4 EMERGENCY EXIT DOOR ASSIST BOTTLE HAD A LOW PRESSURE READING. SERVICED L4 EMERGENCY EXIT DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950818005071995081800507NM 1995 8 18 AALA951248 119950714A33508100022601 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07369AA 25196 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7B TO 12B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 7B AND 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950818005081995081800508EU 1995 8 18 AALA951249 119950715A3350 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0790070 513 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE IN FIRST CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF RIGHT AISLE IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950818005091995081800509EU 1995 8 18 AALA951250 119950715A33507024092007 EEL ASSY AIRBUS300 A300B4605R 3930308EU L3 DOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0790070 513 MAI - DURING OVERNIGHT CHECK, EMERGENCY LIGHT AT L3 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950818005101995081800510NM 1995 8 18 CAL950595 119950714A3234 LEVER ASSY BOEING727 727243 138408DNM GEAR HANDLE LACK OF LUBE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0917402 21265 FLT NR 0618 - FLL - WHEN GEAR WAS EXTENDED FOR LANDING AT FLL ALL THREE GREEN AND ALL THREE RED GEAR LIGHTS WERE ILLUMINATED AND THE TAIL SKID LIGHT WAS ON. THE RED DOOR LIGHT AND DOORS LIGHT ON SECOND OFFICERS PANEL WERE OUT. THE GEAR WAS CYCLED AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE GEAR LEVER WAS NOT FULLY RETRACTING. THE GEAR HANDLE/LEVER ASSY WAS CLEANED AND LUBRICATED. ALL POSITION SWITCHES WERE CHECKED AND FOUND TO BE OPERATING NORMALLY. AN OPERATIONAL CHECK OF THE GEAR SYSTEM WAS GOOD. (M) 2L73 4F RTA3WE 19950818005111995081800511NM 1995 8 18 CAL950601 119950717A2910 HYD LINE BOEING727 727243 138408DNM 'A' HYD SYSTEM LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0958414 22166 FLT NR 0423 - LAX - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE EN ROUTE FROM IAH TO LAX. THE HYDRAULIC FLUID SHUTOFF VALVES WERE CLOSED FOR THREE MINUTES AND THE AIRCRAFT LANDED SAFELY AT LAX. MAINTENANCE FOUND A HYDRAULIC LINE IN THE 'A' SYSTEM LEAKING. THE HYDRAULIC LINE WAS REPAIRED WITH A NEW SLEEVE AND B-NUT. THE HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (M) 2L73 4F RTA3WE 19950818005121995081800512NM 1995 8 18 CAL950605 119950710A5530 SHEAR TIE BOEING727 727224 1384076NM VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974842187 22450 GSO - INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 157, STRINGER 9R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16812. (M) 2L73 4F A3WE 19950818005131995081800513NM 1995 8 18 CAL950606 119950710A5530 SHEAR TIE BOEING727 727224 1384076NM VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974842187 22450 GSO - INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 25, STRINGER 7R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16811. (M) 2L73 4F A3WE 19950818005141995081800514NM 1995 8 18 CAL950607 119950710A5530 SHEAR TIE BOEING727 727224 1384076NM VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097974842187 22450 GSO - INSPECTION FOUND A .75 INCH CRACK IN SHEAR TIE AT VERTICAL STABILIZER STATION 25, STRINGER 10R. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BAC DRAWING 65-16881. (M) 2L73 4F A3WE 19950818005151995081800515SW 1995 8 18 MALA954529 119950707A79312719153001 OIL PRESS TRANS SWRNGNSA227 SA227AC 8780603SW LT ENG INTERNAL FAULT A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL152692P AC658B FLT 3304 - ON CLIMB-OUT FROM MSP, THE LEFT OIL PRESSURE GAUGE READ ABNORMALLY HIGH. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT OIL PRESSURE TRANSDUCER. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950818005161995081800516NE 1995 8 18 MALA954531 219950709A73207863916L27 HMU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15864MA 363 FLT 3169 - IN CRUISE FLIGHT, THE LEFT ENGINE EXHIBITED FLUCTUATIONS IN FUEL FLOW, NH, AND TORQUE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT HMU. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T4 TRTA13NM E20NE 19950818005171995081800517 1995 8 18 MALA954532 419950710A34226226136002 DIR GYRO SWRNGNSA227 SA227AC 8780603SW NR 2 MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15445MA AC687 FLT 3213 - ON CLIMB-OUT FROM MSP, THE FIRST OFFICERS HSI AND CAPTAINS RMI HEADING INDICATOR STUCK. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 DIRECTIONAL GYRO. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950818005181995081800518SW 1995 8 18 MALA954533 119950710A3260 POSITION IND SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15430MA AC710 FLT 3253 - ON APPROACH TO MSP, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GEAR POSITION INDICATOR WAS REPLACED AS A PRECAUTION. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (M) 1L72 4T A8SW 19950818005191995081800519SW 1995 8 18 MALA954534 119950711A32302751016003 ACTUATORS SWRNGNSA227 SA227AC 8780603SW RT MLG OUT OF ADJUST A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL1526906 AC654B FLT 3395 - ON CLIMB-OUT FROM YXU, THE RIGHT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AND THE HYDRAULIC PRESSURE FLUCTUATED AFTER THE GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED TO DTW WITH ITS GEAR DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE RIGHT LANDING GEAR ACTUATORS. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950818005201995081800520EU 1995 8 18 MALA954535 119950712A33506008905 EEL BATTERY PACK FOKKERF27 F27MK200 4990620EU CABIN DISCHARGED A MALAO OTHER O OTHER ININSP/MAINT 1 GL15278MA 10280 DURING A MAINTENANCE WALKAROUND IN CWA, FOUR FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT SEAT 3DE. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T A817 19950818005211995081800521NM 1995 8 18 MALA954536 119950712A32607002537 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15824MA 327 FLT 3409 - ON APPROACH TO DTW, THE INTRANSIT LIGHT ON THE GEAR HANDLE DID NOT ILLUMINATE UPON GEAR EXTENSION. MAINTENANCE REPLACED THE ADVISORY CONTROL UNIT. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950818005221995081800522SW 1995 8 18 MALA954537 119950711A57532731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL152692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP ROLLER DOUBLER WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER IAW ARP 57-10-9207 AND ARP 57-20-9424. (M) 1L72 4T A8SW 19950818005231995081800523SW 1995 8 18 MALA954538 119950711A57532731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL152692P AC658B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT FLAP ROLLER DOUBLER TO BE WORN. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT FLAP ROLLER DOUBLER IAW ARP 57-10-9207 AND 57-20-9424. (M) 1L72 4T A8SW 19950818005241995081800524NM 1995 8 18 MALA954539 119950710A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15828MA 333 FLT NR 3390 - DURING THE PREFLIGHT IN DTW, THE CREW NOTED THAT SEVERAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD COAT CLOSET BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950818005251995081800525NE 1995 8 18 MALA954540 219950710A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LEFT MALFUNCTIONED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15828MA 333 FLT NR 3390 - ON APPROACH TO LEX, THE CREW NOTED AND OIL SMELL IN THE CABIN. NO WARNING LIGHT WAS NOTED ON THE ANNUNCIATOR PANEL, AND THE DUCT TEMPERATURE WAS NORMAL. THE CREW PERFORMED QUICK REFERENCE PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN LEX. MAINTENANCE REPLACED THE LEFT ENGINE. AN INVESTIGATION IS CONTINUING. (M) 2H72 4T4 TRTA13NM E20NE 19950818005261995081800526NM 1995 8 18 MALA954544 119950717A2510 SEAT TRACKS DHAV DHC8 DHC8102 2809003NM COCKPIT WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15822MA 326 DURING A C-CHECK INSPECTION AT BNA, MAINTENANCE FOUND THE SEAT TRACK HOLES ON THE PILOTS AND CO-PILOTS SEATS WORN. REPAIRS WERE COMPLETED BY INSTALLING WEAR STRIPS ON THE PILOTS, P/N 85310067-055, 53, AND CO-PILOTS, P/N 85310061-055, 061, SEAT TRACKS IAW SB 8-53-53. (M) 2H72 4T RTA13NM 19950818005271995081800527NM 1995 8 18 MALA954545 119950717A531385310984 STRINGER DHAV DHC8 DHC8102 2809003NM BS 182 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15822MA 326 DURING A C-CHECK INSPECTION IN BNA, MAINTENANCE NOTED CORROSION TO STRINGER 31, P/N 85310984, AT STATION 182, FRAME 31. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW RD 53-925 AND SRM 51-10-100. (M) 2H72 4T RTA13NM 19950818005281995081800528NM 1995 8 18 MALA954546 119950717A533085310026 SKIN DHAV DHC8 DHC8102 2809003NM BS 167-182 DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15822MA 326 DURING C-CHECK INSPECTION IN BNA, MAINTENANCE FOUND A DENTED AND GOUGED SKIN PANEL, P/N 85310026, BETWEEN STATIONS X167.00 AND 182.OO. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW RD8-53-1601. (M) 2H72 4T RTA13NM 19950818005291995081800529SW 1995 8 18 MALA954549 119950719A32302751000385 HOOK ASSY SWRNGNSA227 SA227AC 8780603SW LT MLG CRACKED A MALAO OTHER O OTHER CLCLIMB 1 GL1526863 AC650B DLT 3492 - AFTER TAKEOFF FROM STC, THE LEFT MAIN LANDING GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE PROBLEM RECURRED AFTER THE CREW CYCLED THE GEAR. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UPLOCK HOOK ASSY. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950818005301995081800530WP 1995 8 18 ORJA9556 119950703A32302178824503 CONTROL CABLE DOUG DC9 DC982 3022082WP NLG FRAYED A ORJAO OTHER J WARNING INDICATION CLCLIMB 1 WP11823RA133179025 49889 RNO - ON TAKEOFF FROM SEA, LANDING GEAR WOULD NOT RETRACT, COMPLIED WITH ABNORMAL PROCEDURE. PUSHED GEAR HANDLE RELEASE AND GEAR RETRACTED NORMALLY WITH NO ELEC GROUND SHIFT PROBLEMS. FOUND ANTI-RETRACTION CABLE FRAYED. REMOVED AND REPLACED CABLE. OPS CHECK NORMAL PER MM 32-31-01. (M) 2L72 4F A6WE 19950818005311995081800531WP 1995 8 18 ORJA9559 119950715A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11840RA 49424 AFT EMERGENCY LIGHTS IN EMPENNAGE INOP. REPLACED BATTERIES. OPS CHECK GOOD. (M) 2L72 4F A6WE 19950818005321995081800532EU 1995 8 18 PLGA62995G 119950629A3244175K882 TIRE TREAD GOODYEAR SAAB SF340 340B 7860101EU NLG MISSING A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE05353BE 40201113 340B242 AFTER TAKEOFF FROM DCA THE CREW NOTED A NOISE WHICH CEASED AS THE NOSE GEAR RETRACTED. THE AIRCRAFT CONTINUED TO BOS WHERE A PRECAUTIONARY FLYBY WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE RIGHT HAND NOSE TIRE HAD EXPERIENCED SEPARATION OF THE CENTER TREAD APPROXIMATELY QUARTER AROUND THE TIRE. THE TAXI LIGHT HOUSING WAS ALSO BROKEN AND MISSING. MAINTENANCE REMOVED AND REPLACED THE WHEEL ASSY AND DEFERRED THE TAXI LIGHT PER THE MEL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950818005331995081800533CE 1995 8 18 PLGA71095G 119950710A54001149800221 KEEL WEB BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05810BE UB48 DURING INSPECTION THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE TWO CRACKS ON THE FORWARD FLANGE. BOTH CRACKS RAN VERTICALLY ON THE FLANGE. ONE CRACK WAS BETWEEN THE TWO CENTER ATTACH RIVETS APPROXIMATELY 1 INCH IN LENGTH. THE 2ND CRACK WAS LOCATED NEXT TO THE THREE LOWER HI-LOCK ATTACH FASTENERS APPROXIMATELY 3 INCHES IN LENGTH. THE KEEL WAS REPAIRED IAW AERODESIGN ENGINEERING REPORT NR 1507, DATED 6/2/95 AND FAA FORM 8110-3. THE KEEL WEB IS TO BE REPLACED NO LATER THAN 1/4/96 WITH REINSPECTIONS EVERY 45 DAYS UNTIL REPLACEMENT. (M) 2L72 4T RTA24CE 19950818005341995081800534NE 1995 8 18 PLGA71195J1 219950815A7261 STATIC SEAL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE A-SUMP EXCESS CLEARANCEA PLGAO OTHER O OTHER CRCRUISE 1 NE05741BA1331619 340A090 367411 HIGH OIL TEMPERATURE, OIL PRESSURE FLUCTUATION AND LOSS IS BELIEVED TO BE THE RESULT OF EXCESSIVE CLEARANCE BETWEEN THE NR 3 LABRYNTH SEAL AND ITS ASSOCIATED STATIC SEAL, THE A-SUMP SUPPORT SEAL, WHICH CAUSED SUMP AIRFLOWS INSUFFICIENT TO PREVENT EXCESSIVE LOSS OF OIL INTO THE MAIN FRAME/COMPRESSOR. (M) 2L72 4T4 TRTA52EU E8NE6 19950818005351995081800535CE 1995 8 18 PLGA71395G1 119950713A29101013880175 HYDRAULIC HOSE BEECH 1900 1900C 1154161CE RT MLG LEAKING A PLGAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 NE05818BE UB61 BOS - ON APPROACH THE LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW PUMPED THE GEAR DOWN, LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED BY BOS MAINTENANCE AND FERRIED GEAR DOWN TO ALB. ALB MAINTENANCE REPLACED THE HYDRAULIC PRESSURE HOSE TO THE RIGHT ACTUATOR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19950818005361995081800536CE 1995 8 18 PLGA716951 119950716A54001149800212 KEEL WEB BEECH 1900 1900C 1154161CE RT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE053067X UB67 DURING RIGHT ENGINE CHANGE THE NACELLE INBOARD UPPER KEEL WEB (P/N 114-980021-2) WAS FOUND TO BE CRACKED ON THE FORWARD FLANGE. THE CRACK WAS APPROXIMATELY 4 INCHES IN LENGTH RUNNING VERTICALLY BETWEEN THE ATTACHMENT RIVETS ON THE FORWARD FLANGE. THE KEEL WAS REPAIRED IAW AERODESIGN ENGINEERING REPORT 1507-5 AND FAA FORM 8110-3 DATED 6/2/95. THE KEEL WEB IS TO BE REPLACED NO LATER THAN 1/10/95. (M) 2L72 4T RTA24CE 19950818005371995081800537CE 1995 8 18 PLGA716952 119950716A54001149800221 KEEL WEB BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05808BE UB45 DURING A WING INSPECTION, THE LEFT ENGINE NACELLE OUTBOARD UPPER KEEL WEB (P/N 114-980022-1) WAS FOUND TO HAVE ONE CRACK ON THE FORWARD FLANGE. THE CRACK RAN VERTICALLY BETWEEN THE FORWARD ATTACHING RIVETS. THE KEEL WEB WAS REPAIRED IAW AERODESIGN ENGINEERING REPORT NR 1507 DATED 6/2/95 AND FAA FORM 8110-3. THE KEEL WEB IS TO BE REPLACED NO LATER THAN 1/4/96 WITH REINSPECTIONS EVERY 45 DAYS UNTIL REPLACEMENT. (M) 2L72 4T RTA24CE 19950818005381995081800538 1995 8 18 RAIA950716 419950717A3416066306202 ALTIMETER BAG JETSTMJETSTM3201 1500217EU NR 1 FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03424AM5414 865 STL - 7061 - NR 1 ALTIMETER STICKING. MAINTENANCE REPLACED NR 1 ALTIMETER. PITOT/STATIC LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950818005391995081800539EU 1995 8 18 RAIA950717 119950718A29104484D275 CHECK VALVE BAG JETSTMJETSTM3201 1500217EU RT HYD SYSTEM CRACKED A RAIAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03342TE6369 954 JLN - FLT 7067 - HYDRAULIC PRESSURE FELL TO ZERO, LANDING GEAR WOULD NOT EXTEND, PERFORMED EMERGENCY GEAR EXTENSION AND LANDED. MAINTENANCE REPLACED RT HYDRAULIC ISOLATION CHECK VALVE. RESET GEAR BYPASS PIN, GROUND RUNS REVEALED NO LEAKS SYSTEM OK. (M) 2L72 4T RTA56EU 19950818005401995081800540EU 1995 8 18 RAIA950718 119950716A3350311701 EEL BATT PACK BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03434AM5474 887 STL - EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY. (M) 2L72 4T RTA56EU 19950818005411995081800541EU 1995 8 18 RAIA950719 119950716A3150350A52005009 COMPUTER AEROSPATR72 ATR72202 8680940EU INSTR PNL MALFUNCTIONED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03721TE1820 217 STL - FLT 714 - AFTER ENGINE START SMOKE FILLED THE COCKPIT. UPON INSPECTION MAINTENANCE RESET MULTI-FUNCTION COMPUTER NR 1B SYSTEM. SYSTEM TEST REVEALED NO SMOKE. (M) 2H72 4T RTA53EU 19950818005421995081800542EU 1995 8 18 RAIA950720 119950717A2150NSA931321350 CIRCUIT BREAKER AEROSPATR72 ATR72202 8680940EU RT PACK TRIPPED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CE03723TE6934 283 STL - FLT 7014 - IN HOTEL MODE WITH BOTH PACKS OFF, CABIN FILLS WITH SMOKE. MAINTENANCE RESET RT PACK VALVE CIRCUIT BREAKER. GROUND TEST REVEALED NORMAL OPERATION. (M) 2H72 4T RTA53EU 19950818005431995081800543NM 1995 8 18 WRLA95034 119950717A4900R1965453 DOOR DOUG MD11 MD11 3023602NM APU INLET BINDING A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27275WA 48631 DURING TAXI, CAPTAIN NOTED APU INLET DOOR WOULD NOT CLOSE. CAPTAIN ELECTED TO RETURN TO GATE FOR MAINTENANCE TROUBLE-SHOOTING. AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL TROUBLE-SHOOTING DETERMINED THAT APU INLET DOOR LINKAGE BINDING. DOOR LINKAGE WAS CLEANED AND LUBED. OPS CHECK PERFORMED WITH NO FAULT. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F RTA22WE 19950818005441995081800544NM 1995 8 18 AWXA9500413 119950705A261213003100 FIRE LOOP BOEING737 737275 1384485NM APU FAILED A AWXAAF UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 WP282FOR 20958 PHX - FLT 742 - ELP TO LAS DURING CRUISE, APU FIRE LIGHT AND BELL CAME ON. APU PREVIOUSLY PLACARDED, FIRE EXTINGUISHING SYSTEM INOP. CREW PULLED FIRE HANDLE AND WARNINGS CEASED. CREW ELECTED TO RETURN TO PHX. MAINTENANCE FOUND LOOP-M 334 OUT OF TOLERANCE, REPLACED M 334 AND CLEANED PLUG D 4816. SYSTEM OPS CHECKED OK, AC RETURNED TO SERVICE. (W) 2L72 4F A16WE 19950818005451995081800545EU 1995 8 18 AWXA9500419 219950707A7200 ENGINE BOEING737 7373Y0 1384671NM CFMINTCFM56 CFM563B2 13802EU NR 2 MALFUNCTIONED A AWXAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 WP282FOR 23747 PHX-ABQ - FLT 205 - ON TAKEOFF, THE E2 EGT REACHED 940 FOR 45 SECONDS, THE NR 2 TRUST LEVER WENT TO FIREWALL AND N1 2 PERCENT LESS THAN TARGET. AFTER REDUCING POWER ESTABLISHED IN CLIMB, THE NR 2 N2 STARTED INCREASING AND REACHED APPROXIMATELY 103 PERCENT BEFORE SWITCHING AUTO THROTTLE OFF. PILOT RETURNED AC TO PHX WITHOUT FURTHER INCIDENT. MX PERFORMED TAKEOFF SIMULATION, BLEEDS ON PACKS ON, PMC'S ON, AUTO/THROTTLE ACTIVATED NR 2 ENGINE, ACHIEVED TAKEOFF POWER TARGET WITH ALL PARAMETERS WITHIN LIMITS AND MATCHED WITH NR 1 ENGINE. SWITCHED PMC'S OFF, ALL PARAMETERS STABLE. NR 2 ENGINE HAD 1 INCH CUSHION FROM FIREWALL AT TAKEOFF POWER SETTING. (W) 2L72 4F4 FRTA16WE E21EU 19950818005461995081800546NM 1995 8 18 AWXA9500436 119950711A2913MX342087 HYD PUMP BOEING757 7572S7 1384962NM LT ENGINE LEAKING A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28901AW 23321 PHX-JFK - FLT 294 - EN ROUTE PILOT REPORTED, EICAS MESSAGE 'LT ENGINE HYD PUMP FAULT' AND ASSOCIATED OVERHEAD SWITCH FAULT. EICAS MESSAGE FOR LOW QUANTITY LT SYS HYD APPREARED. DURING DESCENT INTO JFK, THE T/E FLAPS STUCK BETWEEN 0 AND 1 UNIT, AFTER SELECTING 1 UNIT. ALTERNATE FLAP DRIVE METHOD USED, FLAPS DID NOT RESPOND. GEAR HANDLE SELECTED DOWN, GEAR DID NOT RESPOND, GEAR WAS MANUALLY EXTENDED. MAINTENANCE REPLACED LEAKING LT HYD PUMP AND FLUSHED SYSTEM. OPERATIONAL AND LEAK CHECK GOOD. MAINTENANCE RESET FLAP/SLAT ELECTRONIC UNIT, OPERATIONAL CHECK GOOD. LANDING GEAR EXTENDED MANUALLY DUE TO LOSS OF LT HYD QTY, NO ACTION REQUIRED PER BOEING MM. (W) 2L72 4F RTA2NM 19950818005471995081800547NM 1995 8 18 AWXA9500447 119950715A2520 ANGLE BOEING737 73733A 1384673NM FWD ATT SEAT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND FORWARD ATTENDANT SEAT LOWER SUPPORT ANGLE CORRODED. REPAIRED PER ER 3-53-41-06. (W) 2L72 4F RTA16WE 19950818005481995081800548NM 1995 8 18 AWXA9500448 119950715A5320 STRAP BOEING737 73733A 1384673NM BS 312/328 WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND STABILIZER STRAP WORN THROUGH IN TWO PLACES BETWEEN BOTTOM OF FLOORBEAM AT STA 312 AND STA 328. REPAIRED PER SRM 53-10-51. CLEARANCE CHECK OK. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005491995081800549NM 1995 8 18 AWXA9500449 119950715A5320 SHEAR TIE BOEING737 73733A 1384673NM BS 380 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND FRAME SHEAR TIE AT STA 380 BL 0 CRACKED. REPAIRED PER SRM 53-40-07. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005501995081800550NM 1995 8 18 AWXA9500450 119950715A5320 FRAME BOEING737 73733A 1384673NM RT COCKPIT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND F/O'S NR 1 WINDOW FRAME CRACKED AT UPPER O/B CORNER. REPAIRED PER ER 53-31-03. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005511995081800551NM 1995 8 18 AWXA9500451 119950715A5320 ANGLE BOEING737 73733A 1384673NM AFT PIT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND AFT PIT CENTER PANEL LT VERTICAL SUPPORT ATTACH FLANGE CRACKED AT BOTTOM. REPLACED ANGLE PER SRM 51-40-02. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005521995081800552NM 1995 8 18 AWXA9500452 119950715A5320 ANGLE BOEING737 73733A 1384673NM BS 380-400 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND INTERCOSTAL UPPER L-ANGLE CRACKED BETWEEN STA 380 AND STA 400 BL 0. REMOVED, FABRICATED AND REPLACED L-ANGLE PER SRM 51-40-02 AND 53-30-51. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005531995081800553NM 1995 8 18 AWXA9500453 119950715A5330 SKIN BOEING737 73733A 1384673NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW29740 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND FUSELAGE SKIN AT AVIONICS EXHAUST COOLING CUTOUT CRACKED. INSTALLED FABRICATED INTERNAL DOUBLER PER EO 53-30-13. TOTAL CYCLES 22943. (W) 2L72 4F RTA16WE 19950818005541995081800554NM 1995 8 18 AWXA9500454 119950715A5320 DOOR SILL BOEING737 73733A 1384673NM AFT CARGO CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28164AW 23625 PHX - DURING SCHEDULED C10 INSPECTION, FOUND AFT CARGO DOOR SILL FRAME WEB CORRODED BEYOND LIMITS IN SEVERAL PLACES AT FASTENER HOLES. REPLACED WEB PER SRM 51-10-02 AND SRM 51-40-02. (W) 2L72 4F RTA16WE 19950818005551995081800555NM 1995 8 18 AWXA9500455 119950717A3350900835A EEL BATT PACK BOEING737 7372M8 1384483NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FWD AISLE L1 DOOR AND R1 DOOR EMERGENCY EXIT LIGHTS FLICKERED. REMOVED AND REPLACED BATTERY PACK AND CHARGER, OPS CHECK GOOD. (W) 2L72 4F A16WE 19950818005561995081800556NM 1995 8 18 AWXA9500456 119950718A3350276005 EEL FUSE BOEING737 7373S3 1384711NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH ROW 22. REPLACED FUSE IN AFT RT BATTERY PACK ASSEMBLY. OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950818005571995081800557NM 1995 8 18 AWXA9500457 119950718A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 15 THROUGH 21. RESECURED LOOSE WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950818005581995081800558NM 1995 8 18 AWXA9500458 119950720A3350 EEL ASSEMBLY BOEING757 7572G7 1384963NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE, ROW 26 THROUGH ROW 32. RECONNECTED LOWER LIGHT ASSEMBLY AT ROW 32, OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950818005591995081800559NM 1995 8 18 AWXA9500459 119950720A3350 EEL WIRE BOEING737 7372A6 138448BNM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28145AW 20194 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND BROKEN WIRE ON EMERGENCY EXIT LIGHT AT ROW 2. REPAIRED WIRE, OPS CHECK GOOD. (W) 2L72 4F A16WE 19950818005601995081800560EU 1995 8 18 AWXA9500460 119950722A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28633AW 082 PHX - DURING ROUTINE MAINTENANCE CHECK, LT FWD EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950818005611995081800561NM 1995 8 18 AWXA9500461 119950722A3350276005 EEL FUSE BOEING757 7572G7 1384963NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN. RECONNECTED SEVERAL LIGHT ASSY'S AND REPLACED FUSE IN BATTERY CHARGER ASSEMBLY IN AFT RT GALLEY. OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950818005621995081800562NM 1995 8 18 AWXA9500462 119950722A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28306AW 24633 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEATS 2 TO 5ABC. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950818005631995081800563NM 1995 8 18 AWXA9500463 119950723A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 12 THROUGH 23. RECONNECTED WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950818005641995081800564EU 1995 8 18 RAIA950721 119950719A3260900EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03422AM 856 STL - FLT 7508 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH. MAINTENANCE REPLACED NOSE GEAR UPLOCK SWITCH AND COMPLIED WITH SB 32-JA 891142. GEAR SWINGS REVEALED NORMAL OPERATION. (W) 2L72 4T RTA56EU 19950818005651995081800565EU 1995 8 18 RAIA950722 119950717A3242AC63740 MAXERAT BAG JETSTMJETSTM3201 1500217EU RT BRAKE FAULTY A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03340TE 939 STL - FLT 7082 - ON ROLLOUT, CAPTAIN'S AND FO'S BRAKE BECAME INOP. BOTH BRAKES WORK NORMAL WHEN EMERGENCY BRAKE IS USED. MAINTENANCE REPLACED RT BRAKE MAXERAT PER J32 MM 324000. TAXI CHECK REVEALED NORMAL BRAKING SYSTEM. (W) 2L72 4T RTA56EU 19950818005661995081800566WP 1995 8 18 RAIA950723 219950719A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT MALFUNCTIONED A RAIAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CE03431AM 881 STL - FLT 7436 - LOW POWER BOTH ENGINES. MAINTENANCE REPLACED RT ENGINE PER GARRETT MM AND LT ENGINE BLEED AIR GASKETS. GROUND POWER RUNS REVEALED NORMAL OPERATION AND ALL ENGINE PARAMETERS. (W) 2L72 4T4 TRTA56EU E4WE 19950818005671995081800567EU 1995 8 18 RAIA950724 119950717A3240DAS21592 0-RING BAG JETSTMJETSTM3201 1500217EU LT MLG BRAKE WORN A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03435AM 889 STL - THE LT BRAKE GRABBING AND RELEASING WITH PRESSURE APPLIED. MAINTENANCE REPLACED O-RING ON LT BRAKE MAXERAT UNIT. TAXI CHECK AND LEAK CHECK GOOD. (W) 2L72 4T RTA56EU 19950818005681995081800568EU 1995 8 18 RAIA950725 119950714A3242AH54450 BRAKE BAG JETSTMJETSTM3201 1500217EU RT MLG WORN A RAIAK NONE O OTHER ININSP/MAINT 1 CE03971JX 971 FAT - THE LT BRAKE GRABS DURING SLOW TAXI. MAINTENANCE REPLACED LT BRAKE ASSY. TAXI CHECK NORMAL. (W) 2L72 4T RTA56EU 19950818005691995081800569EU 1995 8 18 RAIA950726 119950716A3240 BRAKE SYST BAG JETSTMJETSTM3201 1500217EU RT MLG BRAKE LOW FLUID A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03340TE 939 STL - THE RT BRAKE INOP. MAINTENANCE SERVICED CAPTAIN'S RT BRAKE MASTER CYLINDER (P/N ACM26810) WITH HYDRAULIC FLUID. TAXI CHECK AND LEAK CHECK GOOD. (W) 2L72 4T RTA56EU 19950818005701995081800570EU 1995 8 18 RAIA950727 119950717A3350167006 EEL BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03721TE 217 STL - SOME EMERGENCY ESCAPE PATH LIGHTING IN THE CABIN FLOOR ARE OUT. MAINTENANCE REPLACED LIGHT BULBS FOR EMERGENCY LIGHTING. (W) 2H72 4T RTA53EU 19950818005711995081800571EU 1995 8 18 RAIA950728 119950719A33507012210 EEL BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE 283 STL - AFT SERVICE DOOR EXIT LIGHT HAS BURNED OUT BULBS. MAINTENANCE REPLACED LIGHT BULBS. (W) 2H72 4T RTA53EU 19950818005721995081800572EU 1995 8 18 RAIA950729 119950720A5270915E13 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03429AM 879 STL - FLT 7442 - PAX DOOR LIGHT CAME ON. MAINTENANCE ADJUSTED PAX DOOR MICROSWITCH. SYSTEM CHECK OF DOOR REVEALED NORMAL INDICATIONS AND OPERATION. (W) 2L72 4T RTA56EU 19950818005731995081800573NE 1995 8 18 RAIA950730 219950723A73203105900 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114A 01514NE NR 1 ENG OUT OF ADJUST A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03551HK 41040 STL - FLT 7514 - THE NR 1 ENGINE LOW TORQUE. ADJUSTED FUEL SCHEDULE. (W) 2L72 4T4 TRTA41NM E18NE 19950818005741995081800574WP 1995 8 18 RAIA950731 219950723A732089778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 1 ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03860AE 860 SFO - FLT 4286 - THE NR 1 ENGINE LOW TORQUE. ADJUSTED FUEL CONTROL MAX FUEL ADJUSTMENT. (W) 2L72 4T4 TRTA56EU E4WE 19950818005751995081800575EU 1995 8 18 RAIA950732 119950721A3250A1424D ISOLATION VALVE BAG JETSTMJETSTM3201 1500217EU NLG STEERING FAULTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03872AE 872 SFO - FLT 4721 - DURING CLIMB, LANDING GEAR CONTROL C/B TRIPPED. REPLACED STEERING ISOLATION VALVE. (W) 2L72 4T RTA56EU 19950818005761995081800576EU 1995 8 18 RAIA950733 119950721A7712310385 STRAIN GAUGE BAG JETSTMJETSTM3201 1500217EU NR 1 FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03433AM 885 STL - FLT 7366 - THE NR 1 SURGING AND TORQUE INDICATOR PEGGGED. REPLACED NR 1 ENG STRAIN GAUGE. (W) 2L72 4T RTA56EU 19950818005771995081800577NE 1995 8 18 RAIA950734 219950721A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 2 LOW PWR A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03426TE 228 MSN - FLT 7173 - THE NR 2 ENGINE LOW POWER. REMOVED AND REPLACED NR 2 ENGINE. (W) 2H72 4T4 TRTA53EU E20NE 19950818005781995081800578EU 1995 8 18 RAIA950735 119950723A2150NAS55208D CLAMP AEROSPATR72 ATR72202 8680940EU NR 2 PACK LOOSE A RAIAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE 283 STL - FLT 7019 - THE NR 2 PACK EMITTED SMOKE IN CABIN. SECURED CLAMP ON TURBO FAN. (W) 2H72 4T RTA53EU 19950818005791995081800579EU 1995 8 18 RAIA950736 119950723A3243ACM26810 BRAKE SYST BAG JETSTMJETSTM3201 1500217EU RT COCKPIT REQD SERVICE A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03430AM 880 FIRST OFFICERS RT BRAKE INOP. BLEED AND SERVICED MASTER CYLINDER (P/N ACM26810). (W) 2L72 4T RTA56EU 19950818005801995081800580EU 1995 8 18 RAIA950737 119950725A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU NR 2 ENGINE OUT OF ADJUST A RAIAA UNSCHED LANDING O OTHER TOTAKEOFF 1 CE03436AM 891 STL - FLT 7510 - THE NR 2 ENGINE WOULD NOT MAKE TARGET TORQUE. RECALIBRATED TORQUE SIGNAL CONDITIONER. (W) 2L72 4T RTA56EU 19950818005811995081800581SO 1995 8 18 RAIA950738 119950723A3240396512 VALVE EMB 120 EMB120RT SO BRAKE SYST INTERMIT A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03124AM 120016 MOMENTARILY LOST BRAKES ON TAXI. REPLACED BRAKE CONTROL VALVE. (W) 2L72 4T RTA31SO 19950818005821995081800582EU 1995 8 18 RAIA950739 119950723A33503011210 EEL AEROSPATR42 ATR42300 8680920EU SERVICE DOOR INOP A RAIAK NONE L NO TEST TXTAXI/GRND HDL 1 CE032FOR 176 EMERGENCY LIGHT AT SERVICE DOOR INOP. REPLACED LIGHT. (W) 2H72 4T RTA53EU 19950818005841995081800584NE 1995 8 18 95ZZZX4061 219950713A725070BMO31070 MODULE 3 SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE MOD 3 REAR BEARING COKED A HXSAK NONE O OTHER ININSP/MAINT 1 AL056015S2053 809 1884 ENGINE NOT PASSING OIL FLOW CHECK DUE TO COKING IN THE REAR BEARING OF MODULE 3. REQUIRED DISASSEMBLY AND CLEANING. 1G71 3U3 U H9EU E19EU 19950818005961995081800596GL 1995 8 18 95ZZZX4073 219950810A732323007506 GOVERNOR BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTION ALAELOAO OTHER R PARTIAL RPM/PWR LOSS DEDESCENT 1 AL0386TA 36 1647 CAE822365 FROM CRUISE, A LOW POWER DESCENT INITIATED. WHEN POWER APPLIED, ENGINE RPM DECREASED. PILOT ENTERED AUTOROTATION, POWER REAPPLIED AND ENGINE FLAME-OUT OCCURRED. ENGINE RE-STARTED AND 95 PERCENT N2, BUT WHEN POWER APPLIED FOR LANDING, ENGINE FLAME-OUT. AUTOROTATION LANDING MADE. TROUBLESHOOTING FOUND PT GOVERNOR MALFUNCTION AND WAS REPLACED. FLIGHT CHECK NORMAL. 1G71 3U3 U H2SW E4CE 19950818005971995081800597SW 1995 8 18 95ZZZX4074 119950720A291070010H000A180 LINE BELL 206 206B 1181511SW HYD PUMP LEAKING A DCGAK NONE K FLUID LOSS ININSP/MAINT 1 WP1337741 1695 LOSS OF HYDRAULIC BOOST DUE TO HYDRAULIC FLUID LEAKING FROM SMALL HOLE ON PRESSURE LINE FROM HYDRAULIC PUMPS TO FILTER HEAD. INTERNAL BREAKDOWN DUE TO RUBBER SWELLING. REPLACED PRESSURE LINE. OPS CHECK OK. 1G71 3U H2SW 19950818005991995081800599CE 1995 8 18 95ZZZX4076 119950724A24324076 BATTERY SAFT LEAR 24 24 5170302CE TAILCONE OVERHEAT A KKFAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP NRNOT REPORTED 1 GL23555LB 177 BATTERY 140 DEGREES AND 160 DEGREES WARNING LIGHT ILLUMINATED. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED NR 2 BATTERY WITH SERVICEABLE UNIT. 2L72 4J A10CE 19950818006081995081800608 1995 8 18 9512509853 419950811A34174013243901 AIR DATA COMP DOUG DC9 DC951 3022051WP E/E COMPARTMENT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01762NC5363 473 47710 CAPTAIN'S ALTIMETER RED FLAG APPEARED ON TAKEOFF ROLL, ABORTED TAKEOFF AT 80 KNOTS. AIRCRAFT RETURNED TO THE GATE. REPLACED AIR DATA COMPUTER, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950818006091995081800609WP 1995 8 18 9512519978 119950814A5220 EMERGENCY EXIT DOUG DC9 DC931 3022065WP RT OVERWING WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE RIGHT FORWARD OVERWING EMERGENCY EXIT. REPLACED THE DOOR. 2L72 4F A6WE 19950818006101995081800610WP 1995 8 18 9512529857 119950814A5350 RELEASE MECH DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01766NC 47739 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE TAILCONE, CHECKED OK. 2L72 4F A6WE 19950818006111995081800611NE 1995 8 18 9512536637 219950813A7532 BLEED VALVE 7371092 BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 3 ENGINE MALFUNCTIONED A NWAACE ABORTED TAKEOFF ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP TOTAKEOFF 1 GL01637US 04838 23548 715190 DURING TAKEOFF THE NR 3 ENGINE EXPERIENCED A FIRE WARNING WITH THE NACELLE TEMPERATURES GOING INTO THE RED AND AT 115 KNOTS TAKEOFF WAS ABORTED. THE EGT HAD GONE TO 715 DEGREES FOR 15 SECONDS AND A BORESCOPE INSPECTION WAS PERFORMED. THE HIGH STAGE BLEED VALVE WAS FOUND PARTIALLY OPEN AND WAS LOCKED CLOSED. UNDER INVESTIGATION. 2L74 4F4 F A20WE E3NE 19950818006121995081800612WP 1995 8 18 95UAL900063 119950725A271019697 PULLEY DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL AILERON CONTROL FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP291839U 46633 DURING ACCOMPLISHMENT OF AILERON CONTROL SYSTEM FRICTION CHECK, THERE WAS AN ADVERSE SPOILER DEPLOYMENT. REPLACED RT AILERON CABLE TURNAROUND PULLEY. 2L73 4F4 F A22WE E23EA 19950818006131995081800613WP 1995 8 18 95UAL900091 119950815A5620AAA7010501 OUTER WINDOW DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN CRACKED A UALAA UNSCHED LANDING O OTHER ININSP/MAINT 1 WP291838U 46632 A/C DIVERTED DUE TO CRACKED OUTER PAIN ON CABIN WINDOW. REPLACED WINDOW. DC-10 FLEET IS BEING INSPECTED, AND SUSPECT WINDOWS REPLACED. 2L73 4F4 F A22WE E23EA 19950818006141995081800614NM 1995 8 18 95UAL900092 119950815A27801267627 FLAP CONTL UNIT BOEING747 747422 1384935NM PWA 4056 PW4056 NE NR 3 LE FLAP MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29185UA16417 25395 LEFT INBOARD LEADING EDGE FLAPS WOULD NOT RETRACT AFTER TAKEOFF. LEADING EDGE FLAP SYSTEM WAS OP CHECKED FOR DISCREPANCIES, NONE WERE FOUND. THE CENTER FLAP CONTROL UNIT WAS REPLACED, AS A PRECAUTION. ALSO, AS A FURTHER PRECAUTION, THE NR 3 LEFT HAND LEADING EDGE FLAP DRIVE UNIT WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 19950818006151995081800615NM 1995 8 18 95UAL900093 119950815A492038420722 TURBINE WHEEL ALLIED SIGNA98CK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE APU FAILED A UALAK NONE O OTHER CRCRUISE 1 WP297273U4992 15436 21420 APU TURBINE WHEEL SEPARATED INTO TWO HALVES. FAILURE DUE TO A CASTING FLAW AT THE MIDDLE OF THE TURBINE WHEEL. 2L73 4F4 F A3WE E2EA 19950818006161995081800616NM 1995 8 18 95UAL900094 119950815A4930976000 FLOW DIVIDER ALLIED SIGNA36038791 BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE APU MALFUNCTIONED A UALAF ACTIVATE FIRE EXT. A FLAME/FIRE ININSP/MAINT 1 WP29157UA261396663 P493C 20106 A/C HAD APU TAILPIPE FIRE WHILE AT GATE. REPLACED APU. FLOW DIVIDER (P/N 976000) IN FUEL CONTROL FOUND TO BE STICKING AND THE BLEED DOWN VALVE (P/N 36037) WAS FAILING TO DUMP EXCESS FUEL. 2L74 4F4 F A20WE E20EA 19950818006171995081800617NM 1995 8 18 95UAL900095 119950816A3350 EEL CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29542UA 25276 EEL LIGHT INOP AT MID LAV. FOUND EEL CONNECTOR LOOSE RESECURED. 2L72 4F4 FRTA2NM E17NE 19950818006181995081800618WP 1995 8 18 95UAL900096 119950816A3350 EEL POWER CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291824U 46623 EEL LIGHTING FROM SEATS 9AB TO 18AB INOP. REPLACED POWER CABLE. 2L73 4F4 F A22WE E23EA 19950818006191995081800619WP 1995 8 18 95UAL900097 119950816A5620AAA7010501 WINDOW PANE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN CRACKED A UALAA UNSCHED LANDING O OTHER CRCRUISE 1 WP291839U 46633 OUTER PANE OF PASSENGER WINDOW AT SEAT 11J DEPARTED A/C. REPLACED WINDOW. WINDOW FAILED DUE TO IN-PLANE CRACKING. UA IS CURRENTLY INSPECTING THE FLEET TO FIND OTHER SUSPECT WINDOWS AND REPLACING THEM. 2L73 4F4 F A22WE E23EA 19950818006201995081800620WP 1995 8 18 ABXA9500672 119950814A322057714071 BRACE DOUG 57153545535NDOUG DC8 DC861 3021952WP BS 52 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23848AX 2507 060 46032 DURING POST FLIGHT WALK-AROUND, FOUND A CRACK IN THE LEFT SIDE BRACE OF THE NOSE LANDING GEAR, JUST BELOW THE DOOR ATTACH POINT. REPLACED THE LEFT SIDE BRACE IAW DC-8 MM 32-21-3, OPS CHECKED NORMAL. 2L74 4F 4A25 19950818006211995081800621WP 1995 8 18 ABXA9500673 119950814A3040 DE-ICE NIHON YS11 YS11A500 6310416WP RT WINDSHIELD MALFUNCTIONED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23911AX 2051 WINDSHIELD DE-ICE GREEN LIGHTS DID NOT COME ON IN LOW, THE RIGHT LIGHT COMES ON. LATER IN FLIGHT, CYCLED ON AND OFF. POSSIBLE ASSOCIATED INTERMITTENT SMOKE ODOR. RAN AIRCRAFT AT ILN, OPERATED WINDSHIELD DE-ICE FOR ABOUT FIVE MINUTES. SYSTEM OPS CHECKED GOOD IAW YS-11 MM, NO SMOKE OR ODOR NOTED. 2L72 4T A1PC 19950818006221995081800622NM 1995 8 18 DL72S953383 119950813A5330 SKIN BOEING727 727232 1384082NM BS 344 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11478DA 20755 DURING INSPECTION, FOUND FUSELAGE SKIN CRACKED BETWEEN 3 RIVET HOLES AT FS 344 BETWEEN STRINGERS 22L AND 23L. REPAIRED PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 19950818006231995081800623NM 1995 8 18 DL72S953385 119950813A2782 ACTUATOR BOEING727 727232 1384082NM NR 4 SLAT FAILED A DALAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11492DA 21061 AT CRUISE LOSS A-HYD SYS QTY AND PRESS NR 4 SLAT DID NOT EXTEND ON LANDING. REPLACED NR 4 SLAT ACTUATOR, NR 1 AND 2 ENG DRIVEN HYD PUMPS AND FILTERS. 2L73 4F A3WE 19950818006241995081800624NM 1995 8 18 DL72S953390 119950721A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1070 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 1070 FLOORBEAM RBL 40 TO 60 HAS CORROSION. REMOVED CORROSION PER SRM 51-10-6, FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. REMOVED DAMAGED SECTION, REPAIRED PER SRM 53-10-8 PG 1. FOUND AT HMV. 2L73 4F A3WE 19950818006251995081800625NM 1995 8 18 DL72S953391 119950814A5754 WEB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND DURING B-1 LETTER CHECK, NR 7 SLAT ACT ROD END WEB CRACKED .5 INCH I/B WEB. REPAIRED PER MM 57-54-0 PG 803. 2L73 4F A3WE 19950818006261995081800626NM 1995 8 18 DL72S953392 119950814A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND DURING B-1 LETTER CHECK, NR 6 L/E SLAT O/B STOP PAD ANGLE CRACKED O/B END. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950818006271995081800627NM 1995 8 18 DL72S953393 119950814A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 FOUND DURING B-1 LETTER CHECK, .5 INCH CRACK NR 3 SLAT COVE ANGLE BELOW ANTI-ICE DUCT. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950818006281995081800628NM 1995 8 18 DL72S953394 119950814A3350 EEL BATTERY PACK S106 BOEING727 727232 1384082NM AFT AIRSTAIR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11536DA 22049 DURING LAYOVER, FOUND EMERGENCY LIGHTS ABOVE AFT AIRSTAIR INOP. REPLACED BATTERY OPERATION NORMAL. 2L73 4F A3WE 19950818006291995081800629NM 1995 8 18 DL72S953402 119950806A5754651622296 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11537DA 22073 NR 6 L/E SLAT HAD A CRACK IN THE LOWER SKIN ATTACH ANGLE. CRACK WAS REPAIRED PER M/M 57-54-0 FIG 809A. FOUND AT SHOP INSPECTION. 2L73 4F A3WE 19950818006301995081800630NE 1995 8 18 DL757953389 219950814A7200PW2037 ENGINE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11684DA8231 27104 727102 ON CLIMBOUT, CVG HAD LT ENG COMPRESSOR STALLS FOLLOWED BY LOW OIL PRESSURE EICAS MSG ENG SHUTDOWN. MTC REPORTED EGT 691 FOR 37 SEC METAL IN TAIL PIPE. ENGINE WAS REPLACED AND ROUTED TO SHOP. 2L72 4F4 FRTA2NM E17NE 19950818006311995081800631WP 1995 8 18 DLL10953339 119950808A21501505449129 DUCT LKHEED1011 10113851 5265010WP NR 2 PACK RUPTURED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO11728DA 193C1173 ON LANDING, SMOKE NOTICED IN COCKPIT AND CABIN. NR 2 TURBINE BYPASS DOOR, FULL HOT IN AUTO OR MANUAL. THE C-AREA OVERHEAT CAME ON, FOLLOWED BY B-AREA. SHUTOFF NR 2 AND 3 PACKS. ACM DISCHARGE TEMPS OVER 96 FOR BOTH PACKS. THE NR 2 FLOW CONTROL C/B POPPED. FOUND DUCT BLOWN FROM NR 2 ACM AND WATER SEPARATOR. LOCKED OUT FLOW CONTROL PER MEL. 2L73 4F A23WE 19950818006321995081800632NE 1995 8 18 DLL10953384 219950813A7530AC66670 VALVE SHROUD LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE BROKEN A DALAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO11727DA 010657 193C1167 010657 ON SHORT FINAL HAD NR 2 FIRE WARNING BOTH LOOPS, SHUTDOWN PER POM. DID NOT FIRE BOTTLE, NO SECONDARY INDICATIONS. FOUND HP BLEED VALVE DUCT SHROUD BROKEN. SUSPECT WHEN THROTTLES PULLED BACK FOR DESCENT, BLEED VALVE OPENS AND DUMPS HOT AIR UNDER CORE COWLS. REPLACED DUCT AND VALVE, OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19950818006331995081800633NM 1995 8 18 DLM88953323 119950730A5330 SKIN DOUG MD88 MD88 3023688NM BS 207-215 PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11950DL 49881 SKIN PUNCTURE ON RT SIDE EXTENDING FROM FS 207 TO FS 215 AND FROM LONGERON 19 TO 20. GROUND DAMAGE REPAIRED PER DL ERA 2715008-14. 2L72 4F RTA6WE 19950818006341995081800634WP 1995 8 18 MWEA95265 119950815A335060030431 EEL POWER SUPPLY DOUG DC9 DC914 3022034WP AFT RT LAV DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31500ME 45711 DURING SERVICE CHECK, WHEN BATTERY SWITCH SHUTOFF THE RIGHT AFT AND TAIL COMPARTMENT LIGHTS ILLUMINATE. MAINTENANCE REMOVED AND REPLACED AFT RT POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950818006351995081800635NM 1995 8 18 SCNA95170 119950810A2611PC1604 BATTERIES BOEING727 7272J4 1384006NM LAVS DISCHARGED A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15288SC 20765 THE FORWARD AND AFT LEFT LAVATORY SMOKE DETECTOR EMITTED A CHIRPING SOUND WHILE EN ROUTE. REMOVED AND REPLACED BATTERIES IN THREE LAV SMOKE DETECTORS AND OPS CHECK DETECTORS PER MM 26-00-00. 2L73 4F RTA3WE 19950818006361995081800636NM 1995 8 18 UPS204119 119950814A5720 CHORD BOEING727 72727C 138400JNM BS 759/761 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TOPSIDE OF PLUS CHORD AT BS 759 AND 761 RBL 68 WL 206. REPAIRED IAW EO B727-5710-1271 AND UPS EO B727-5710-7298-A. 2L73 4F A3WE 19950818006371995081800637NM 1995 8 18 UPS204120 119950814A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-03) ON FLOORBEAM AT BS 1110 RBL 46 TO 52 WL 208. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED PER B727-5310-7278A. 2L73 4F A3WE 19950818006381995081800638NM 1995 8 18 UPS204121 119950814A5755 SPOILER BOEING727 72727C 138400JNM NR 14 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND SPOILER NR 14 X-RAY VIEWS NR 3, 4, 5 AND 6 SHOW CORE DAMAGE AND CONTAMINATION. MAINTENANCE REPAIRED IAW SRM 57-50-6 AND SRM 57-50-6. 2L73 4F A3WE 19950818006391995081800639NM 1995 8 18 UPS204122 119950814A5720 STIFFENER BOEING727 72727C 138400JNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER ON RT L/E AT APF 99 486 JUST O/B OF NR 6 SLAT I/B TRACK. MAINTENANCE REPLACED THE CRACKED STIFFENER IAW SRM 51-30-2, MM 27-81-00. 2L73 4F A3WE 19950818006401995081800640NM 1995 8 18 UPS204123 119950814A5754 RIB BOEING727 72727C 138400JNM LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 SLAT O/B TRACK I/B SUPPORT FITTING TO BE CRACKED. MAINTENANCE REPLACED RIB, WORK DONE IAW SRM 51-30-02, 51-10-01, 57-51-51, AND MM 27-81-00. 2L73 4F A3WE 19950818006411995081800641NM 1995 8 18 UPS204124 119950814A5713 STRINGER BOEING727 72727C 138400JNM WS 232.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-571-01.02-01) ON UPPER SURFACE FORWARD STRINGER S-5 AT WING STATION 232.5. MAINTENANCE FABRICATED REPAIR PARTS PER MM 28-10-0, SRM 57-20-2 AND 51-20-4. 2L73 4F A3WE 19950818006421995081800642NM 1995 8 18 UPS204125 119950814A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-224-01.05-01) ON FLOORBEAM AT BS 640 LBL 5 TO 33 WL 208. MAINTENANCE FOUND THE CORROSION REMOVAL WAS OUT OF LIMITS AND REMOVED THE DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW UPS EO B727-5310-7313-A. 2L73 4F A3WE 19950818006431995081800643NM 1995 8 18 UPS204126 119950814A5712 RIB BOEING727 72727C 138400JNM WS 546.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK AT RT WING RIB AT WS 546.5. MAINTENANCE REMOVED AND INSTALLED A NEW RIB IAW EO B727-5710-13256. 2L73 4F A3WE 19950818006441995081800644NM 1995 8 18 UPS204127 119950814A5530 FITTING BOEING727 72727C 138400JNM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE TENSION TIE RIB AFT SHEAR FITTING VERTICAL BOLT HOLES HAVE CORROSION IN BORES. MAINTENANCE REMOVED THE CORROSION, REPLACED THE BUSHING DUE TO MISALIGNMENT. ALL WORK WAS PERFORMED BY BOEING PER CONTRACT 6-1171-TA-377 AND SB 727-55-56. 2L73 4F A3WE 19950818006451995081800645NM 1995 8 18 UPS204128 119950814A5510 HINGE FITTING BOEING727 72727C 138400JNM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE LT NR 5 BALANCE PANEL FITTING TO BE CORRODED. MAINTENANCE REPLACED THE LT BALANCE PANEL HINGE FITTING IAW SRM 51-30-2 AND SRM 51-30-5. 2L73 4F A3WE 19950818006461995081800646NM 1995 8 18 UPS204129 119950814A5313 STRINGER BOEING727 72727C 138400JNM BS 850 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 18L BS 850 RBL 70.5 WL 192. MAINTENANCE REPAIRED PER UPS EO B727-5310-7314-A. 2L73 4F A3WE 19950818006471995081800647NM 1995 8 18 UPS204130 119950814A5712 RIB BOEING727 72727C 138400JNM WS 546.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE RT WING RIB AT WS 546.5 WAS CRACKED AT S-6 LOWER AND S-9 UPPER. MAINTENANCE REPLACED THE RIB IAW UPS EO B727-5710-1325-6 AND MM 28-10-00. 2L73 4F A3WE 19950818006481995081800648NM 1995 8 18 UPS204131 119950816A5311 FRAME BOEING727 72727C 138400JNM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 660 FRAME HAS A 2 INCH CRACK AT WL 174, LBL 58. MAINTENANCE FABRICATED DOUBLER AND INSTALLED IAW SRM 51-30-2 AND SRM 51-40-3. 2L73 4F A3WE 19950818006491995081800649NM 1995 8 18 UPS204132 119950816A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SHEAR TIE AT BS 680 BETWEEN STR 25 AND STR 24L. MAINTENANCE FABRICATED NEW PARTS AND INSTALLED. THE WORK WAS DONE IAW SRM 53-10-4. 2L73 4F A3WE 19950818006501995081800650NM 1995 8 18 UPS204133 119950816A5320 SUPPORT BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON PRESSURE BOX SUPPORT AT BS 740 TO 74L LBL 70.5 WL 210. MAINTENANCE FABRICATED AND INSTALLED NEW PARTS PER SRM 51-10-6, 53-10-1, 51-20-1, 51-40-2, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950818006511995081800651NM 1995 8 18 UPS204134 119950816A5320 STIFFENER BOEING727 72727C 138400JNM BS 1213 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TRANSVERSE BEAM IN AFT AIR STAIR AREA AT STA 1213 LBL 15 RBL 15 WL 167. MAINTENANCE REMOVED AND INSTALLED NEW TRANSVERSE BEAM IAW SRM 51-30-2 AND 51-10-2. 2L73 4F A3WE 19950818006521995081800652NM 1995 8 18 UPS204135 119950816A5313 STRINGER BOEING727 72727C 138400JNM BS 600-620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.0P0-01) ON STRINGER NR 5 RT 600 TO 620. MAINTENANCE FABRICATED AND INSTALLED NEW REPAIR PARTS PER SRM 3-10-3. 2L73 4F A3WE 19950818006531995081800653NM 1995 8 18 UPS204136 119950816A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON TOP AND BOTTOM OF FLOORBEAM AROUND NUTPLATE HOLES AT STA 680 RBL 60 TO 65 LBL 11 WL 208. MAINTENANCE INSTALLED NEW CHORD AND SPLICED. ALL WORK WAS PERFORMED IAW SRM 530-10-1, 53-10-8, 51-10-1, 51-30-2. 2L73 4F A3WE 19950818006541995081800654NM 1995 8 18 UPS204137 119950816A5754 END CAP BOEING727 72727C 138400JNM LT TE FOREFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING OUTBOARD FOREFLAP INBOARD END CAP WAS CORRODED AND GOUGED UPPER SURFACE. MAINTENANCE REPLACED L/W O/B FOREFLAP INBOARD END CAP PER SRM 51-30-2. 2L73 4F A3WE 19950818006551995081800655NM 1995 8 18 UPS204138 119950816A5320 BEAM BOEING727 72727C 138400JNM BS 1213 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TRANSVERSE BEAM IN AFT AIRSTAIR AREA AT STA 1213 LBL 15, RBL 15, WL 175. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1, REMOVED TRANSVERSE BEAM AND INSTALLED A NEW TRANSVERSE BEAM PER SRM 51-30-2. 2L73 4F A3WE 19950818006561995081800656NM 1995 8 18 UPS204139 119950816A5320 STIFFENER BOEING727 72727C 138400JNM BS 1213 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER END OF VERTICAL STIFFENER AT STA 1213 LBL 5 WL 174. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED PER SRM 51-30-2 BOEING DRAWING 65-25992. 2L73 4F A3WE 19950818006571995081800657NM 1995 8 18 UPS204140 119950816A5313 STRINGER BOEING727 72727C 138400JNM BS 363 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LT STRINGER NR 19 AT STA 363 AND 370 WL 190. MAINTENANCE REPAIRED PER SRM 53-10-1 AND 53-10-3. 2L73 4F A3WE 19950818006581995081800658NM 1995 8 18 UPS204141 119950816A5320 EXTRUSION BOEING727 72727C 138400JNM BS 228/233 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON PEDESTAL CHANNELS AT STA 228 LBL 12-29, WL 208-210 AND STA. 233 LBL 12-29 WL 208-210. MAINTENANCE FABRICATED SEAT PEDESTAL IAW SRM 51-20-1 AND INSTALLED PARTS PER SRM 51-30-2. 2L73 4F A3WE 19950818006591995081800659NM 1995 8 18 UPS204142 119950816A5230 FRAME BOEING727 72727C 138400JNM CARGO DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON AFT CARGO DOOR FWD FRAME UNDER RELEASE CABLE BRACKET. ALSO, AREA 3 ABOVE NR 3 STOP PIN FITTING. MAINTENANCE REMOVED CORRODED FRAME AND REPLACED WITH NEW FRAME IAW SRM 51-10-1, 51-10-2, 51-30-5, 51-20-4, MM 51-20-151, AND SRM 51-30-2. 2L73 4F A3WE 19950818006601995081800660NM 1995 8 18 UPS204143 119950816A5330 SKIN BOEING727 72727C 138400JNM BS 266/267/268 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK INDICATIONS AT BS 266, 267, 268, RT LWR ROW OF FASTENERS ON UPPER SILL FRAME EXTERIOR SKIN OF FLIGHT DECK. MAINTENANCE FABRICATED DOUBLER REPAIR AND MADE FINAL INSTALLATION PER SRM 51-20-04, 53-30-3, 51-30-2. 2L73 4F A3WE 19950818006611995081800661NM 1995 8 18 UPS204144 119950816A5313 STRINGER BOEING727 72727C 138400JNM BS 362-370 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT STRINGER NR 25 AT STA 362 TO 370, RBL 30 WL 154. MAINTENANCE REMOVED THE DAMAGED SECTION AND SPLICED IN A REPAIR SECTION IAW SRM 53-10-3. 2L73 4F A3WE 19950818006621995081800662NM 1995 8 18 UPS204145 119950816A5320 STRINGER TIE BOEING727 72727C 138400JNM BS 362 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT STRINGER TIE STA 362 RBL 25 STRINGER NR 26. MAINTENANCE CLEANED THE CORROSION PER SRM 53-10-1. REMOVED STRINGER TIE AND INSTALLED NEW STRINGER TIE PER SRM 510-30-2. 2L73 4F A3WE 19950818006631995081800663NM 1995 8 18 UPS204146 119950816A5330 SKIN BOEING727 72727C 138400JNM BS 297 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SKIN BELOW STRINGER 22R WITH BLUE WATER STAINS AND PEELING PAINT AT STA 297 B5301. MAINTENANCE FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 53-20-1, 53-30-2, 51-10-1 AND 51-20-2. 2L73 4F A3WE 19950818006641995081800664NM 1995 8 18 UPS204147 119950816A5330 SKIN BOEING727 72727C 138400JNM BS 1034 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SKIN LAP AT STA 1034 STR 4 RT. MAINTENANCE REMOVED CORROSION IAW SRM 51-10-6, REPAIRED SKIN LAP IAW SRM 53-30-1, 51-10-2, 51-30-2, 51-30-8, 53-30-2 AND 53-30-3. 2L73 4F A3WE 19950818006651995081800665NM 1995 8 18 UPS204148 119950816A5313 STRINGER BOEING727 72727C 138400JNM BS 1110-1135 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER AT STA 1110 TO 1135 STR 15 LT. MAINTENANCE REMOVED CORROSION IAW SRM 51-10-6 AND REWORKED IAW SRM 53-10-1. REPAIRED STRINGER 15 LT IAW SRM 53-10-2, STRINGER TIE AT 1110. ALSO, REPAIRED AND INSTALLED IAW SRM 51-20-1 AND 51-30-02. 2L73 4F A3WE 19950818006661995081800666NM 1995 8 18 UPS204149 119950816A5320 MOP SILL BOEING727 72727C 138400JNM PAX DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON MOP SILL AND FWD ENTRY SILL SUPPORT. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-2, 51-20-4, 51-30-2, 53-10-1 AND MM 51-20-151. 2L73 4F A3WE 19950818006671995081800667NM 1995 8 18 UPS204150 119950816A5320 EXPANSION LINK BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT BS 740 AND BUSHING RBL 25 WL 207. MAINTENANCE FABRICATED NEW EXPANSION LINK AND INSTALLED IAW SRM 51-10-1, AND 51-30-2. 2L73 4F A3WE 19950818006681995081800668NM 1995 8 18 UPS204151 119950816A5320 EXPANSION LINK BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON EXPANSION LINK AT BS 740 BL 0 WL 207. MAINTENANCE FABRICATED NEW EXPANSION LINK AND INSTALLED IAW SRM 51-10-1, AND 51-30-2. 2L73 4F A3WE 19950818006691995081800669NM 1995 8 18 UPS204152 119950816A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 668 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TOP AND BOTTOM FWD FLOORBEAM AROUND NUTPLATE HOLES AT STA 668 RBL 16 TO 60, 65 WL 208. MAINTENANCE BLENDED AWAY CORROSION AND INSTALLED A REPAIR ANGLE IAW SRM 51-10-6, 53-10-01. 2L73 4F A3WE 19950818006701995081800670NM 1995 8 18 UPS204154 119950816A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TOP AND BOTTOM FWD FLOORBEAM AT STA 640 LBL 45 TO RBL 65 WL 208. MAINTENANCE REPAIRED THE FLOORBEAM IAW UPS EO 727-53-1654. 2L73 4F A3WE 19950818006711995081800671NM 1995 8 18 UPS204155 119950816A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TOP AND BOTTOM FWD FLOORBEAM AROUND NUTPLATE HOLES AT STA 400 RBL 15 TO 45 WL 208. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-10-8 AND 53-10-1. 2L73 4F A3WE 19950818006721995081800672NM 1995 8 18 UPS204156 119950816A5531 SPAR CHORD BOEING727 72727C 138400JNM VERT STAB CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE VERTICAL FIN MID SPAR CHORD WAS CHAFED AT ACCESS PANEL 9602 CROSS BRACE, RT. MAINTENANCE REMOVED AND REPAIRED IAW UPS EO 727-55-0292. 2L73 4F A3WE 19950818006731995081800673NM 1995 8 18 UPS204157 119950816A5753 FITTING BOEING727 72727C 138400JNM NR 4 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION RUST ON THE FWD ATTACH FITTING FOR THE NR 4 FLAP TRACK. MAINTENANCE REMOVED THE CORRODED FITTING AND REPLACED WITH NEW FITTING IAW MM 27-51-31, SRM 51-30-2 AND MM 27-51-31. 2L73 4F A3WE 19950818006741995081800674NM 1995 8 18 UPS204158 119950816A5753 RIB FITTING BOEING727 72727C 138400JNM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE R/W I/B MIDFLAP O/B TRACK I/B RIB FITTING WAS CRACKED IN 2 PLACES. MAINTENANCE REMOVED THE CRACKED FITTING AND INSTALLED NEW RIB FITTINGS IAW SRM 51-30-2. 2L73 4F A3WE 19950818006751995081800675NM 1995 8 18 UPS204159 119950816A5744 YOKE HOUSING BOEING727 72727C 138400JNM LT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND L/W I/B MIDFLAP O/B YOKE HOUSING IS CRACKED. MAINTENANCE REMOVED THE GIMBAL MOUNTING ECCENTRIC AND INSTALLED A NEW MOUNTED ECCENTRIC. 2L73 4F A3WE 19950818006761995081800676NM 1995 8 18 UPS204160 119950816A5754 RIB BOEING727 72727C 138400JNM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 1 K-FLAP RIB WAS PITTED AROUND THE CONDUIT MOUNT BOLTS, O/BSIDE. MAINTENANCE FROZE PLUG HOLES AND INSTALLED REPAIR STRAPS IAW SRM 51-30-2, 57-50-1 AND 51-10-6. 2L73 4F A3WE 19950818006771995081800677NM 1995 8 18 UPS204161 119950816A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 227.8 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACKED SHEAR TIE AT STRINGER 15 RT AFT SIDE OF STA 277.8 WL 225. MAINTENANCE REPAIRED IAW SRM 51-10-1 AND 51-40-2. 2L73 4F A3WE 19950818006781995081800678NM 1995 8 18 UPS204162 119950816A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 312 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AROUND NUTPLATE HOLES AT STA 312 LBL 45 TO 60 WL 208. MAINTENANCE REPAIRED THE FLOORBEAM IAW SRM 53-10-8, 51-10-6 AND 53-10-1. 2L73 4F A3WE 19950818006791995081800679NM 1995 8 18 UPS204163 119950816A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 305-310 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 305 TO 310 LBL 30 WL 208. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-30-2 AND 51-20-4. 2L73 4F A3WE 19950818006801995081800680NM 1995 8 18 UPS204164 119950816A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 312-328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 312 TO 328 LBL 30 WL 208. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-30-2 AND 51-20-4. 2L73 4F A3WE 19950818006811995081800681NM 1995 8 18 UPS204165 119950816A5320 INTERCOSTAL BOEING727 72727C 138400JNM BS 328-344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 328 TO 344 LBL 30 WL 208. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-30-2, 51-10-1 AND 51-10-2. 2L73 4F A3WE 19950818006821995081800682NM 1995 8 18 UPS204166 119950816A5347 SEAT TRACK BOEING727 72727C 138400JNM BS 760-848 PITTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE SEAT TRACK RBL 45 AT STA 760 TO 848 WL 208 IS BADLY PITTED AND HAS BROKEN TEETH. MAINTENANCE FABRICATED A NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-8, 51-30-5, 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950818006831995081800683NM 1995 8 18 UPS204167 119950816A5320 WEB BOEING727 72727C 138400JNM BS 1223 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE CENTER AIRSTAIR WEB WAS CORRODED AT BS 1223 BETWEEN LBL 20 AND RBL 20 WL 163. MAINTENANCE FABRICATED AND INSTALLED NEW AIRSTAIR PER SRM 51-10-2, 51-30-2 AND 51-20-1. 2L73 4F A3WE 19950818006841995081800684NM 1995 8 18 UPS204168 119950816A5320 CHANNELS BOEING727 72727C 138400JNM BS 1223 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE LT AND RT U-CHANNEL CRACKED AT STA 1223 RBL AND LBL 20.54 WL 163. ALSO, STA 1220 RT RBL 20.5 WL 163 IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED NEW U-CHANNEL PER SRM 51-20-1 AND 5-30-2. 2L73 4F A3WE 19950818006851995081800685NM 1995 8 18 UPS204169 119950816A5753 RIB BOEING727 72727C 138400JNM LT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE LEFT WING I/B MIDFLAP O/B TRACK I/B RIB IS CRACKED. MAINTENANCE INSTALLED NEW RIBS IAW SRM 51-30-2. 2L73 4F A3WE 19950818006861995081800686NM 1995 8 18 UPS204170 119950816A5753 SUPPORT BOEING727 72727C 138400JNM TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE O/B MIDFLAP O/B BACK SUPPORT FOR DRUM IS CORRODED. MAINTENANCE REPAIRED PER SRM 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950818006871995081800687NM 1995 8 18 UPS204171 119950816A5320 SHEAR TIE BOEING727 72727C 138400JNM BS 294.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACKED SHEAR TIE ON FRAME 294.5, JUST ABOVE STR 21R RBL 52. MAINTENANCE REPAIRED PER SRM 51-40-2. 2L73 4F A3WE 19950818006881995081800688NM 1995 8 18 UPS204172 119950813A3350 EEL BOEING747 747123 1384873NM UPPER DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND IN ANC, MAINTENANCE FOUND THE UPPER DECK ESCAPE DOOR HAS AN INOP FWD EMERGENCY LIGHT. MAINTENANCE RELAMPED, OPS CK GOOD. 2L74 4F A20WE 19950818007071995081800707SW 1995 8 18 95ZZZX4099 119950627A6410206016201127 BLADE 206011810125BELL 206 206L1 1182107SW BLADE TIP PAINT PEEL B ALGRK NONE O OTHER ININSP/MAINT 1 SW035756N294 CS6485 45546 ROUTINE INSPECTION FOUND PAINT PEELING OFF BLADE. SUSPECT CAUSE - POOR PREPARATION BEFORE PAINTING. 1G71 3U H2SW 19950818007091995081800709NE 1995 8 18 95ZZZX4101 219950624A7250 TURBINE BOEING727 727259 138408JNM PWA JT8 JT8D17R 52049NE NR 1 ENGINE FAILED A UHVACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 SO17203AV19519 22474 707152 KMIA/SVMC - FLT KYC203 - ON POWER RUN-UP FOR TAKEOFF KMIA, APPROXIMATE 1.6 EPR, NR 1 ENGINE BEGAN TO VIBRATE. REJECTED TAKEOFF, AND MONITORED ENGINE. EGT 500, N1 28 PERCENT, N2 52 PERCENT. UPON INSPECTION AT GATE, FOUND TURBINE FAILURE. ENGINE IS BEING REPLACED. TURBINE FAILURE UNDER FURTHER INVESTIGATION. (X) 2L73 4F4 F A3WE E2EA 19950818007101995081800710NM 1995 8 18 95ZZZX4102 119950619A5230 DOOR BOEING727 72723 1384004NM CARGO COMPT NOT CLOSED A UHVAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO171993 18449 KFLL/KGPT - FLT KYC630 - AIR TURN BACK. AIRCRAFT WOULD NOT HOLD CABIN PRESSURE, ISOLATED ALL SYSTEMS. RETURNED TO KFLL. UPON MAINTENANCE INSPECTION, FOUND DEBRIS IN AFT CARGO DOOR SILL, AND DOOR NOT LOCKED CLOSE. DOOR SWITCH STUCK CLOSED. INSPECTED DOOR AND FRAME, OPS CHECK OKAY. PLACED AFT CARGO DOOR WARNING ON DMI 3-2, PER MEL 52-4. RETURNED AIRCRAFT TO SERVICE. (X) 2L73 4F A3WE 19950818007111995081800711WP 1995 8 18 95ZZZX4103 119950708A53121505220 BULKHEAD LKHEED1011 10113851 5265010WP BS 1363 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA38719 193A1012 ACCOMPLISHED AD 95-12-24. DISCOVERED CRACKS ON RIGHT LOWER OUTBOARD SECTION OF FS 1363 BULKHEAD BY VISUAL INSPECTION. PERFORMED BOLT HOLE EDDY CURRENT INSPECTION IAW SB 093-53-268. TWO CRACKS WERE FOUND ON THE BULKHEAD CAP AT BL 42.5. LOCKHEED NOTIFIED AND REPAIRS IN WORK. (X) 2L73 4F A23WE 19950818007121995081800712WP 1995 8 18 95ZZZX4104 219950630A732189737527A9 FUEL CNTRL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3312UA 01514WP LT ENGINE MALFUNCTIONED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO03915AE 915 BNA - FLT 4684 - EN ROUTE TO TUP, LEFT ENGINE TORQUE STUCK AT 60 PERCENT. AIRCRAFT RETURNED TO BNA, SHUT DOWN LT ENGINE ON APPROACH AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LT FUEL CONTROL. (X) 2L72 4T3 TRTA56EU E3WE 19950818007131995081800713NE 1995 8 18 95ZZZX4105 219950704A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67 52043NE LEFT FAILED A NVEAE ENGINE SHUTDOWN Y ENGINE STOPPAGE APAPPROACH 1 SO03160DD4798 SH3723 106014 BWI - FLT 4923 - CREW AND PASSENGERS HEARD LOUD SOUND. CAPTAIN THEN NOTICED THE LEFT ENGINE EGT WAS 800 DEGREES WITH THE TORQUE DECREASING. LEFT POWER LEVER WAS PULLED BACK AND THE EGT STAYED AT 800 DEGREES, LEFT ENGINE WAS SHUT DOWN. AIRCRAFT WAS ON FINAL APPROACH INTO BWI. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED THE LEFT ENGINE. (X) 2H72 4T4 T A41EU E26NE 19950818007141995081800714SO 1995 8 18 ASOA95016 119950712A3260604EN16 SWITCH EMB 110 EMB110P1 3260122SO MLG OUT OF ADJUST A ASOAO OTHER N FALSE WARNING APAPPROACH 1 SO11904FB 110411 SPS/DFW - FLT 7455 - DURING APPROACH FROM SPS/DFW, THE CREW REPORTED THE RIGHT MAIN GEAR LIGHT WAS SLOW TO ILLUMINATE AND REQUESTED EMERGENCY VEHICLES TO STAND BY DURING LANDING. LANDING WAS MADE SAFELY AND WITHOUT INCIDENT AT DFW. ADJUSTED RIGHT MAIN GEAR DOWNLOCK MICROSWITCH. TEST FLIGHT DETERMINED PROPER OPERATION AND ACFT RETURNED TO SERVICE. (X) 1L72 4T A21SO 19950818007151995081800715EA 1995 8 18 ASOA95017 219950714A7200 ENGINE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA RIGHT FAILED A ASOAA UNSCHED LANDING T ENGINE CASE PENETRATION CLCLIMB 1 SO11901FB293662470 110397 57004 DFW/TXK - FLT 7457 - AFTER TAKEOFF, RIGHT ENGINE AUTO SHUT DOWN. FLIGHT RETURNED TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. ENGINE WAS CONFIRMED TO HAVE LOST SOME PIECES WHICH EXITED THROUGH THE EXHAUST AND BURNER CANS. NO PIECES EXITED THROUGH THE COWLING. REMOVED AND REPLACED THE RIGHT ENGINE. S/N ON 57236. REMOVED AND REPLACED THE RIGHT PROP ASSEMBLY. S/N ON BU11997. OPERATIONAL AND LEAK CHECKS GOOD ON ENGINE AND PROP ASSEMBLY. THIS MRR REMAINS OPEN PENDING TEAR DOWN REPORT. (X) 1L72 4T4 T A21SO E4EA 19950818007161995081800716SO 1995 8 18 ASOA95018 119950714A361038E966A PRESS REG EMB 120 EMB120RT SO LT WING DEFECTIVE A ASOAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 SO11275AS 120234 MCN/ATL - FLT 7219 - DURING FLIGHT, LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED. THE LEFT ENGINE WAS SHUT DOWN AND SECURED PER POH PROCEDURES, AND THE CREW MADE A SUCCESSFUL SINGLE ENGINE LANDING SAFELY IN ATL. REMOVED AND REPLACED THE LEFT DE-ICE PRESSURE REGULATOR. S/N OFF PE2120, S/N ON RF1842. OPERATIONAL AND LEAK CHECK GOOD IAW/MM. (X) 2L72 4T RTA31SO 19950818007171995081800717WP 1995 8 18 CAL950494 119950617A3230 UNLOCK CYLINDER DOUG DC10 DC1030 3023501WP NLG JAMMED A ACALAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 SW0968065 46590 FRA - FLT 0059 - THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM FRA. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO FRA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A .1875 INCH DIAMETER BOLT JAMMED IN THE UNLOCK CYLINDER AT THE PIVOT POINT. THE BOLT WAS REMOVED. AN INSPECTION FOUND NO EVIDENCE OF DAMAGE OR MISSING BOLTS. (X) 2L73 4F A22WE 19950818007181995081800718NM 1995 8 18 CAL950501 119950602A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND A 2.25 INCH CRACK IN RADIUS OF NR 3 SLAT INBOARD TRACK INBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-2 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007191995081800719NM 1995 8 18 CAL950502 119950602A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF THE NR 3 SLAT OUTBOARD TRACK OUTBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-50-3, SRM 51-40-3, AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007201995081800720NM 1995 8 18 CAL950503 119950602A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND 13 CRACKS RUNNING FROM FASTENER HOLES IN LEFT SECTION 41 SKIN PANEL. THE CRACKS RANGED IN LENGTH FROM 0.25 INCH TO 0.009 INCH. THE EXISTING DOUBLER WAS REMOVED AND THE DAMAGED AREAS WERE CUT OUT. FILLERS AND DOUBLERS WERE INSTALLED IAW SRM 51-30-2 AND SRM 51-30-3. (X)E 2L73 4F A3WE 19950818007211995081800721NM 1995 8 18 CAL950504 119950602A5320 SUPPORT BOEING727 727232 1384082NM FS 540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - THE FORWARD BAG PIT FLOOR SUPPORT JUST FORWARD OF STA 540 AND ABOVE STR 29L HAD CORROSION ON UPPER AND LOWER SURFACE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-6, SRM 51-40-3, AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007221995081800722NM 1995 8 18 CAL950508 119950602A5754 RIBS BOEING727 727232 1384082NM LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND 2 LOWER LEADING EDGE INBOARD SLAT RIBS CRACKED AT ACTUATOR. THE CRACKS WERE APPROXIMATELY .75 INCH LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007231995081800723NM 1995 8 18 CAL950509 119950602A5330 SKIN BOEING727 727232 1384082NM SECTION 41 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND 3 CRACKS RUNNING FROM FASTENER HOLES IN SECTION 41 SKIN PANEL ON RT SIDE OF FUSELAGE. THE CRACKS WERE APPROXIMATELY .25 INCH LONG. THE EXISTING DOUBLER WAS REMOVED AND THE DAMAGED SKIN WAS CUT OUT. FILLERS AND DOUBLERS WERE INSTALLED IAW SRM 53-30-2 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007241995081800724NM 1995 8 18 CAL950510 119950602A5330 SKIN BOEING727 727232 1384082NM BS 580 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER HOLE, BS 580, LAP SEAM 26L. THE DAMAGED AREA WAS REMOVED AND REPAIRED. DOUBLER, FILLER, AND SHIM WERE INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007251995081800725NM 1995 8 18 CAL950511 119950602A5330 SKIN BOEING727 727232 1384082NM BS 720 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND FUSELAGE SKIN CRACKED THROUGH RIVET HOLES BETWEEN STA 720 AND STA 720A AT CENTERLINE ON LOWER FUSELAGE. THE CRACK WAS 2.5 INCHES LONG. THE DAMAGED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3. (X) 2L73 4F A3WE 19950818007261995081800726NM 1995 8 18 CAL950519 119950605A5320 T-ANGLE BOEING737 737130 1384435NM FS 277.8 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097721564951 19032 31J - CORROSION WAS FOUND ON THE T-ANGLE ABOVE THE NOSE WHEELWELL ACCESS PANEL AT FS 227.8, LT SIDE. THE T-ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED USING FILLERS AND DOUBLERS IAW SRM 53-10-8. (X) 2L72 4F A16WE 19950818007271995081800727WP 1995 8 18 CAL950520 119950617A5311995823879 BELT FRAME DOUG DC9 DC982 3022082WP BS 1309 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW098387239604 49120 HOU - INSPECTION FOUND CORROSION AT LOWER AND UPPER FLANGES OF BELT FRAME AT STA 1309 FROM LONGERON 28L TO LONGERON 28R IN THE AFT BAGGAGE BIN. THE CORRODED SECTION OF BELT FRAME WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-03, FIGURE 2A. (X) 2L72 4F A6WE 19950818007281995081800728NM 1995 8 18 CAL950521 119950623A5280 SEAL BOEING727 727227 1384078NM NLG DOOR BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0976752 21248 MCO - FLT 1978 - AIRCRAFT RETURNED TO AIRPORT DUE TO NLG DOOR INDICATION AND AIR NOISE. MAINTENANCE FOUND SEAL AT LEADING EDGE OF DOOR LOOSE AND JAMMING UNDER DOOR WHEN CLOSED. RESECURED SEAL AND PERFORMED EXTENSION AND RETRACTION TEST OF DOOR AND GEAR, OPERATION CHECKED GOOD. (X) 2L73 4F A3WE 19950818007291995081800729NM 1995 8 18 CAL950531 119950623A213089812621 REGULATOR BOEING727 727232 1384082NM NR 3 ENGINE INOPERATIVE A CALAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW09277831870517150 20638 LAX - FLT 0418 - AIRCRAFT LOST CABIN PRESSURE WHILE AT 33,000 FEET EN ROUTE FROM SFO TO LAX. CABIN PRESSURE COULD NOT BE CONTROLLED IN STAND-BY A.C. OR D.C. MODES AND RT PACK COULD NOT BE RESET. OXY MASKS DEPLOYED AND AIRCRAFT WAS DIVERTED TO LAX WHERE IT LANDED WITHOUT INCIDENT. BOTH THE HIGH PRESSURE REGULATOR AND HIGH PRESSURE MODULATING VALVE WERE REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. OPERATION OF THE RT PACK AND MIX VALVE CHECKED GOOD. DECAY CHECK WAS PERFORMED IAW MM 5-12-71 AND PRESSURE WAS WITHIN LIMITS. THE OUTFLOW VALVE WAS REPLACED AS A PRECAUTIONARY MEASURE. ALSO NOTED BY MAINTENANCE ALL OXY MASKS HAD DEPLOYED. OXY MASKS WERE STOWED AND OXY BOTTLES SERVICED TO FULL. (X) 2L73 4F A3WE 19950818007301995081800730NE 1995 8 18 CAL950533 219950702A7321796067 FUEL CONTROL DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0983873247402850 49121 709856 EWR - FLT 0400 - THE NR 2 ENGINE PARAMETERS BEGAN TO FLUCTUATE WHEN CLIMB POWER WAS SELECTED. THE AUTO THROTTLE WAS DISCONNECTED, BUT THE PROBLEM REMAINED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL CONTROL UNIT (FCU) AT FAULT. THE NR 2 FCU WAS REMOVED AND REPLACED. THE NR 2 ENGINE WAS TRIMMED IAW MM 71-00-00 AND ALL PARAMETERS WERE NORMAL. (X) 2L72 4F4 F A6WE E9NE 19950818007311995081800731WP 1995 8 18 CAL950534 119950703A4930360800010 FUEL CONTROL DOUG DC9 DC982 3022082WP APU INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW09819NY13735258 49479 SLC - FLT 0288 - WHILE OPERATING THE APU AT CRUISE WITH THE LEFT GENERATOR SYSTEM PLACARDED INOPERATIVE, THE APU RPM SLOWLY INCREASED THROUGH 104 PERCENT TO 105 PERCENT AND THEN SHUT DOWN. THE AIRCRAFT WAS DIVERTED TO SLC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE APU AND ALL PARAMETERS WERE WITHIN LIMITS. THE APU WAS RESTARTED SEVERAL TIMES AND RAN AT 103 PERCENT DURING ALL RUNS. THE APU CONTINUED TO HAVE PROBLEMS ON A SUBSEQUENT FERRY FLIGHT. THE APU FUEL CONTROL UNIT WAS REMOVED AND REPLACED AND OPERATION OF THE APU CHECKED NORMAL. (X) 2L72 4F A6WE 19950818007321995081800732WP 1995 8 18 CAL950536 119950529A5320 SUPPORT DOUG DC9 DC982 3022082WP FS 180 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09477AC39162 48062 31J - INSPECTION FOUND THE FLOOR SUPPORT STRUCTURE CORRODED AT STA 180. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01. (X) 2L72 4F A6WE 19950818007331995081800733WP 1995 8 18 CAL950547 119950623A53503913359501 CABLES DOUG DC9 DC932 3022066WP TAIL CONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0933506 47765 HOU - THE TAIL CONE WOULD NOT RELEASE WHEN INTERIOR HANDLE WAS PULLED. THE CABLES WERE ADJUSTED IAW MM 53-50-3. (X) 2L72 4F A6WE 19950818007341995081800734NM 1995 8 18 CALA950507 119950607A5313 STRINGER BOEING727 727232 1384082NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND CORROSION ON STRINGER LOWER SURFACE AFT SIDE OF STA 720 FRAME IN FORWARD LOWER CARGO AREA. THE CORRODED SECTION WAS REMOVED AND A STRINGER AND STRINGER SPLICE WERE INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X) 2L73 4F A3WE 19950818007351995081800735NM 1995 8 18 CALA950513 119950602A5313 STRINGER BOEING727 727232 1384082NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778364939 20638 GSO - INSPECTION FOUND CORROSION ON STR 28R IN FORWARD BAG PIT AT STA 720. A REPAIR SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, SRM 51-30-2, AND SRM 51-20-4. (X) 2L73 4F A3WE 19950818007361995081800736NE 1995 8 18 IXXA199561 219950630A7240 BEARING DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 3 ENGINE DAMAGED A IXXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23786AL 10042 46121 671357 EINN/DTW - IN CRUISE BETWEEN EINN AND DTW, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED WITH NORMAL PRESSURE, BUT OIL TEMP CLIMBED SOMEWHAT ABOVE THE NORMAL RANGE. WHEN THE THROTTLE WAS RETARDED, THE BYPASS LIGHT REMAINED ON, ENGINE WAS PRECAUTIONARILY SHUT DOWN. INSPECTION OF THE ENGINE ON THE GROUND IN DTW REVEALED BEARING-TYPE METAL IN THE SCREEN. SHOP TEAR DOWN OF THE ENGINE CONFIRMED NR 4 BEARING DETAIL 2 WAS DAMAGED AND THAT ITS CAGE HAD FAILED. (X) 2L74 4F4 F 4A25 1E8 19950818007371995081800737WP 1995 8 18 IXXA199563 119950629A3610D17D87 DUCT CLAMP DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 3 ENGINE FAILED A IXXAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL2321CX 45955 671321 LPLA/KWRI - IN CRUISE BETWEEN LPLA AND KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED WITH NORMAL ENGINE PARAMETERS OBSERVED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE FIRE BOTTLES DISCHARGED. THE FIRE WARNING EXTINGUISHED AND THE ENGINE MAINTAINED 39 PSI WINDMILLING OIL PRESSURE. INSPECTION ON THE GROUND AT KWRI REVEALED A FAILED CLAMP ON THE 9TH STAGE PNEUMATIC BLEED DUCT. THE CLAMP WAS REPLACED AND THE SYSTEM LEAK-CHECKED. THE FIRE BOTTLES WERE REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F4 F 4A25 1E8 19950818007381995081800738WP 1995 8 18 IXXA199565 119950630A2612D5020 FIRE DETECTOR DOUG DC8 DC862 3021970WP NR 3 ENGINE MALFUNCTIONED A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL2321CX 45955 KWRI - ON DEPARTURE OUT OF KWRI, A NR 3 ENGINE FIRE WARNING WAS EXPERIENCED. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO KWRI FOR MAINTENANCE. WINDMILLING OIL PRESSURE WAS 30 PSI. INSPECTION AT KWRI REVEALED AN INTERMITTENTLY BAD LOWER FIRE DETECTOR ELEMENT. THE FIRE DETECTOR ELEMENT WAS REPLACED, AND THE ENGINE RUN EXTENSIVELY ON THE GROUND TO VERIFY THE REPAIR. THERE WAS NO RECURRING FALSE FIRE WARNING. THE AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950818007391995081800739WP 1995 8 18 IXXA199566 119950706A2780436392218 CONTL VALVE DOUG DC8 DC871F 302199DWP LE FLAPS SEAL EXTRUDED A IXXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23828BX 45993 DFW/TOL - DURING CRUISE BETWEEN DFW AND TOL, THE AIRCRAFT EXPERIENCED AN HYDRAULIC SYSTEM FAILURE OF BOTH PRESSURE AND QUANTITY. AFTER AN UNEVENTFUL LANDING, MAINTENANCE FOUND THE RIGHT HYDRAULIC MANIFOLD SLOT CONTROL VALVE O-RING EXTRUDED BETWEEN THE MANIFOLD AND THE VALVE. MAINTENANCE REPLACED THE O-RING, SERVICED THE HYDRAULIC SYSTEM, RAN THE AIRCRAFT, ALL SYSTEMS OPERATIONALLY CHECKED GOOD IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F RT4A25 19950818007401995081800740WP 1995 8 18 IXXA199567 119950719A3297 WIRE DOUG DC8 DC862 3021970WP RT MLG FAILED A IXXAO OTHER N FALSE WARNING CLCLIMB 1 GL2361CX 46142 WSAP - ON DEPARTURE DURING UPLATCH CHECK, THE GEAR LIGHT STAYED ON WITH THE MAIN GEAR DOOR LIGHT OUT. THE LANDING GEAR WAS CYCLED ONCE, AND THE UPLATCH CHECK WAS SUCCESSFUL. INSPECTION OF THE SYSTEM IN RJTY REVEALED AN INTERMITTENT GROUND WIRE ON THE RT MLG UPLATCH SWITCH. AN OPERATIONAL CHECK OF THE LANDING GEAR WAS ACCOMPLISHED WITH NORMAL OPERATION NOTED ON SIX RETRACTIONS. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F 4A25 19950818007411995081800741EU 1995 8 18 PAYA95A4029 119950628A5210 DOOR STEP AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174204G16759 061 PASSENGER DOOR STEP FRAME CRACKED, THREE AREAS. REPAIRED IAW SRM. (X) 2H72 4T RTA53EU 19950818007421995081800742EU 1995 8 18 PAYA95A4030 119950628A5320 THRESHOLD AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174204G16759 061 PASSENGER DOOR THRESHOLD CORRODED. REPLACED THRESHOLD. (X) 2H72 4T RTA53EU 19950818007431995081800743EU 1995 8 18 PAYA95A4031 119950712A3233D227090001 ACTUATOR AEROSPATR42 ATR42300 8680920EU NLG DEFECTIVE A PAYAO OTHER O OTHER APAPPROACH 1 EA174209G 129 CREW HEARD NOISE IN NLG WELL ON GEAR EXTENSION AND REPORTED NLG SLOW TO EXTEND. ROD END BEARING FOUND LOOSE IN MOUNT ALLOWING LATERAL MOVEMENT WHEN IN USE. REMOVED AND REPLACED ACTUATOR IAW JIC. 2H72 4T RTA53EU 19950818007441995081800744WP 1995 8 18 9512299160 119950719A5743 FITTING DOUG DC9 DC914 3022034WP LT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR SIDE BRACE ATTACH FITTING LUG. REPAIRED FITTING (P/N 5919289-521) PER EA 91-97104. 2L72 4F A6WE 19950818007451995081800745WP 1995 8 18 9512309160 119950725A5312 BLKHD WEB DOUG DC9 DC914 3022034WP FS 817 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD WEB AT FS 817 AT THE 3 O'CLOCK AND 5 O'CLOCK POSITIONS. REPAIRED WEB PER EA 91-101064. 2L72 4F A6WE 19950818007461995081800746NM 1995 8 18 9512312702 119950726A5330 SKIN BOEING727 727225 1384077NM FS 720 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN RAM AIR INLET LIP BS 720B - 720C AT STR 28L. REPAIRED SKIN (P/N 65-54590-5) PER EA 27-97784. 2L73 4F A3WE 19950818007471995081800747NM 1995 8 18 9512322702 119950727A5315 FLOOR BEAM BOEING727 727225 1384077NM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM BETWEEN LBL 27 - 51. REPAIRED BEAM (P/N 65-20838-16) PER EA 27-98938. 2L73 4F A3WE 19950818007481995081800748NM 1995 8 18 9512332702 119950727A5313 STRINGER BOEING727 727225 1384077NM FS 560 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON STR 27R AT BS 560. REPAIRED STRINGER (P/N 65-56236-102) PER EA 27-97786. 2L73 4F A3WE 19950818007491995081800749WP 1995 8 18 9512349160 119950801A5330 SKIN DOUG DC9 DC914 3022034WP FS 490 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND A ONE INCH CRACK IN THE FUSELAGE SKIN FS 490 AT LONGERON 29R. REPAIRED SKIN (P/N 5911418-1) PER EA 91-97105. 2L72 4F A6WE 19950818007501995081800750NM 1995 8 18 9512352702 119950801A5312 BLKHD STIFFENER BOEING727 727225 1384077NM FS 287 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 287 NOSE LANDING GEAR WHEELWELL VERTICAL STIFFENER AT RBL 30. REPAIRED STIFFENER (P/N 65-18414-36) PER EA 27-98936. 2L73 4F A3WE 19950818007511995081800751NM 1995 8 18 9512362702 119950801A5320 DOOR JAMB BOEING727 727225 1384077NM FS 950 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR JAMB OUTER CHORD FS 950E AT STR 27R. REPAIRED CHORD (P/N 65-561-25) PER EA 27-98924. 2L73 4F A3WE 19950818007521995081800752WP 1995 8 18 9512379160 119950802A5330 SKIN DOUG DC9 DC914 3022034WP FS 170 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 170 BETWEEN LONGERONS 28L - 28R. REPAIRED SKIN (P/N 5911401-1) PER EA 91-97109. 2L72 4F A6WE 19950818007531995081800753NM 1995 8 18 9512382702 119950802A5314 KEEL BEAM BOEING727 727225 1384077NM FS 950 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION AND CRACKS ON THE KEEL BEAM CHORD STR 29R AT BS 950E. REPAIRED STRINGER (P/N 65-56441-4) PER EA 27-98928. 2L73 4F A3WE 19950818007541995081800754NM 1995 8 18 9512392702 119950802A5320 SHEAR TIE BOEING727 727225 1384077NM FS 1263 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND A CRACK IN THE BS 1263 SHEAR TIE BETWEEN STR 11L - 12L. REPAIRED SHEAR TIE (P/N 65-17504-27) PER EA 27-98950. 2L73 4F A3WE 19950818007551995081800755NM 1995 8 18 9512402702 119950802A5320 SHEAR TIE BOEING727 727225 1384077NM FS 1263 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND A CRACK IN THE BS 1263 SHEAR TIE BETWEEN STR 11R - 12R. REPAIRED SHEAR TIE (P/N 65-17504-28) PER EA 27-98951. 2L73 4F A3WE 19950818007561995081800756NM 1995 8 18 9512412702 119950804A5320 SIDE PANEL BOEING727 727225 1384077NM FS 346 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE NOSE LANDING GEAR WHEELWELL LEFT SIDE PANEL CHORD AT BS 346. REPAIRED CHORD (P/N 65-19861-7) PER EA 27-98954. 2L73 4F A3WE 19950818007571995081800757WP 1995 8 18 9512429969 119950808A5241 FITTING DOUG DC9 DC931 3022065WP GALLEY SVC DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND A CRACK IN THE FORWARD GALLEY SERVICE DOOR LOWER BEAM FORWARD END. REPAIRED BEAM AND REPLACED THE FITTING (P/N 3953686-1) PER SRM 52-05, FIG.25. 2L72 4F A6WE 19950818007581995081800758NM 1995 8 18 9512432702 119950808A5315 FLOOR BEAM BOEING727 727225 1384077NM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018877Z 21450 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM LOWER CHORD FROM LBL 38 - RBL 20. REPAIRED CHORD (P/N 65-20838-17) PER EA 27-97788. 2L73 4F A3WE 19950818007591995081800759WP 1995 8 18 9512449608 119950809A5322 FITTING DOUG DC9 DC932 3022066WP FS 916 CORROCED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 916 RIGHT SIDE FLOOR FITTING. REPLACED FITTING (P/N 4911383-501) PER SRM 51-01. 2L72 4F A6WE 19950818007601995081800760WP 1995 8 18 9512459969 119950809A5320 FITTING DOUG DC9 DC931 3022065WP FS 160 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND CORROSION ON THE FS 160 FITTING FORWARD OF THE GALLEY SERVICE DOOR. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950818007611995081800761WP 1995 8 18 9512469946 119950810A5320 FITTING DOUG DC9 DC931 3022065WP FS 110 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 25L END FITTING AT FS 110. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950818007621995081800762WP 1995 8 18 9512479601 119950810A5320 FITTING DOUG DC9 DC932 3022066WP FS 579 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION IN THE FS 579 FRAME FITTING AT LONGERON 18L. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19950818007631995081800763WP 1995 8 18 9512489969 119950811A5312 BLKHD FITTING DOUG DC9 DC931 3022065WP FS 756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND A CRACK IN THE FS 756 BULKHEAD TO RIGHT KEEL ATTACH FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950818007641995081800764WP 1995 8 18 9512499868 119950813A5320 FITTING DOUG DC9 DC951 3022051WP FS 1164 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING H-CHECK, FOUND A CRACK IN THE FS 1164 DOOR JAMB UPPER LEFT STOP FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19950818007651995081800765NE 1995 8 18 COM31137 319950817A6114660714200 HUB ROTOL R3544123F13 SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROPELLER CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01347CA7899 2970 DRG130185 340A028 DRG130185 DURING ULTRASONIC INSPECTION OF PROP HUB S/N 110935, SEVERAL FLAWS WERE DETECTED WHILE PERFORMING SB 61-58 APPENDIX C SCAN B. PROPELLER WAS DISASSEMBLED AND HUB WAS REMOVED FROM SERVICE. 2L72 4T RTA52EU 6 CP61GL 19950818007661995081800766NM 1995 8 18 DL72S953403 119950815A3350 EEL RPS1B BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11544DA 2688 22493 AFT STRIP OF CABIN EMERGENCY FLOOR LIGHTS INOP. REPAIRED SHORT AT FLOOR STRIP AND REPLACED POWER SUPPLY. OPERATION NORMAL. 2L73 4F A3WE 19950818007671995081800767NM 1995 8 18 DL72S953407 119950815A533065545661 SKIN BOEING727 727232 1384082NM FS 580 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 DURING HMV INSPECTION, CORROSION DAMAGE WAS FOUND JUST AFT OF FS 580, OUTBD OF STR 28-L. THE DAMAGE WAS REMOVED RESULTING IN A 19 INCH X 1.75 INCH CUTOUT AND IS 7 INCHES FROM AN EXISTING INTERNAL DOUBLER. IN ACCORDANCE WITH FAA/DER APPROVAL DATED 15 AUG 1995, A FILLER WAS INSERTED IN THE CUTOUT AND A DOUBLER AND TRIPLER WERE INSTALLED WITH THE DOUBLER OVERLAPPING INTO THE EXTERNAL AREA OF THE EXISTING INTERNAL REPAIR. 2L73 4F A3WE 19950818007681995081800768NM 1995 8 18 DL72W953401 119950815A3230 SENSOR 189929 BOEING727 727247 138408FNM LT MLG FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO112811W 20649 LANDING GEAR FAILED TO RETRACT ALL HYD SYS NML - REPLACED FAULTY M831 SENSOR AND DAMAGED WIRES AT SAME SENSOR. OPERATION NORMAL. 2L73 4F A3WE 19950818007701995081800770WP 1995 8 18 DLL13953395 119950815A57201527479108 ATTACH TEE LKHEED1011 10113851 5265010WP WS 503 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 DURING AIRCRAFT HEAVY MTC VISIT, THE RIB TO TORQUE BOX VERTICAL ATTACH TEE ON THE RT WING AT IWS 503 WAS FOUND CRACKED AT SEVERAL TYPICAL LOCATIONS. THE REPLACEMENT OF THE TEE IS COVERED IN S/B 093-57-207. THE TEE HAS BEEN REPAIRED PER THIS S/B. 2L73 4F A23WE 19950818007711995081800771WP 1995 8 18 DLL13953396 119950815A3211SPS70718V814 ATTACH BOLTS LKHEED1011 10113851 5265010WP MLG IMPROPER PART A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11786DL 193A1123 DURING AIRCRAFT HEAVY MTC VISIT, IT WAS FOUND THAT A/C 786 WAS NOT LISTED IN THE ISSUED EFFECTIVITY IN REGARDS TO TEN BOLTS THROUGH THE VERTICAL LEG OF THE LT AND RT WING MLG ATTACH FITTINGS. THE BOLTS HAVE BEEN REPLACED WITH APPROVED SUBSTITUTES PER S/B 093-57-148. 2L73 4F A23WE 19950818007721995081800772WP 1995 8 18 DLL13953397 119950815A2910000AE5616T0510 HOSE LKHEED1011 10113851 5265010WP NR 2 ENGINE LEAKING A DALAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11781DL 193A1003 HYD SYSTEM B-QUANTITY DOWN TO .6250 INCH, TURN ON ATM, TURN OFF ENG PUMP. QUANTITY CONTINUED TO DROP 1/2, TURNED OFF ATM. FOUND PRESSURE LINE FROM B1 PUMP LEAKING. REPLACED LINE AND LEAK CKD OK - HAD TO WAIT FOR PART FROM LGA. 2L73 4F A23WE 19950818007741995081800774WP 1995 8 18 DLL17953399 119950815A2810N38260 FUEL CAP LKHEED1011 10113853 5265020WP LT WING WORN A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11766DA 193H1207 ONE HOUR INTO FLIGHT, PASSENGER NOTICED LIQUID LEAKING FROM VICINITY OF LT OVERWING INBD FUEL CAP. F/O VERIFIED FUEL LEAKING AND CAP SECURE. CAPT AND FLT CONTROL CONCURRED TO RETURN TO ATL. REPLACED NR 1 TANK GRAVITY FILL CAP. LEAK CK GOOD. 2L73 4F A23WE 19950818007751995081800775NM 1995 8 18 MWEA95266 119950816A36105712152180 CLAMP DOUG MD88 MD88 3023688NM TAIL COMPT LOOSE A MWEAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL31601ME 49762 PILOT REPORTS AFTER LEVELING OFF, THE TAIL COMPARTMENT TEMP HI LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE. LIGHT WENT OUT WHEN RIGHT THROTTLE AND RIGHT PACK WERE SHUT OFF. LIGHT REMAINED OFF WITH THROTTLE BACK TO NORMAL AND RIGHT PACK SHUT OFF. RETURNED TO MKE. MAINTENANCE FOUND CLAMP LOOSE ON CROSSFEED VALVE. ALSO, TROUBLESHOT AND FOUND FAULTY TEMP SWITCH. CHANGED SWITCH. RAN ENGINES. OPS AND LEAK CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950818007761995081800776NM 1995 8 18 P5CA9500704 119950817A5711 SPAR BOEING747 747122 1384872NM WS 1555 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIGHT WING FRONT SPAR LOWER RABBET AREA WS 1555 T-CHORD CORRODED. REPAIRED PER BOEING SRM 57-30-03. 2L74 4F A20WE 19950818007771995081800777NE 1995 8 18 P5CA9500705 219950817A7200JT9D7A ENGINE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 MALFUNCTIONED A P5CAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 WP23831FT311524960 19648 662378 NR 1 ENGINE AUTO DECELERATION WITHOUT THROTTLE MOVEMENT, SLOW ENGINE RESPONSE 40 MINUTES INTO FLIGHT, PRECAUTIONARY SHUT DOWN. RESTARTED ENGINE IN-FLIGHT, ALL NORMAL AFTER RESTART. INSPECTED TAIL PIPE AND BLEEDS FOR FOD, PULLED 8TH STAGE CHECK VALVE AND DUCT INSPECTED FOR BLADE DAMAGE, INSPECTED 8TH STAGE CHECK VALVE AND DUCT, CHECKED THE SUMP OF THE FUEL CONTROL FOR WATER, CHECKED BURNER SENSE LINE, C/W DECAY CHECK OF PRECOOLER, CHECKED CHIP DETECTORS, NO DEFECTS FOUND, GROUND RUN OK. 2L74 4F4 F A20WE E20EA 19950818007781995081800778NM 1995 8 18 QXEA9500251 119950813A3260 INDICATION DHAV DHC8 DHC8102 2809003NM RT MLG MALFUNCTIONED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09828PH 287 GEG - RIGHT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. LANDING GEAR WAS RECYCLED AND RIGHT MAIN INDICATED DOWN. AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. AIRCRAFT FERRIED TO PDX FOR REPAIR. COULD NOT DUPLICATE PROBLEM AFTER MANY GEAR SWINGS. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950818007791995081800779NM 1995 8 18 QXEA9500252 119950815A335082410162007 EEL CONTROL BOX DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09825PH 213 PDX - EMERGENCY LIGHTING REMAINS ON WITH EMERGENCY LIGHTING SWITCH OFF. LIGHT CONTROL BOX REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950818007801995081800780 1995 8 18 QXEA9500253 419950814A31005223120005 AMPLIFIER FOKKERF28 F28MK1000 4990808EU RADIO RACK POPPED BREAKER A QXEAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM09454US 11107 GEG - FLIGHT CREW NOTICED SMOKE IN COCKPIT, SMELL AND VISUALLY WHILE AWAITING PUSHBACK. INSTRUMENT AMPLIFIER CIRCUIT BREAKER POPPED. INSTRUMENT AMPLIFIER REPLACED AND AMPLIFIER OPS CHECKED GOOD. NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950818007811995081800781SO 1995 8 18 SWIA95597 119950713A3010 REG VLV GASKET EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT DE-ICE FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07207SW 120266 FIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LIST, AFTER 3 MINUTES BEGAN PRECAUTIONARY ENGINE SHUT DOWN CHECK LIST WITH ENGINE AT FLIGHT IDLE AS RT ENGINE PROP WAS FEATHERED, DUCT LIGHT WENT OUT. TROUBLESHOT SYSTEM, FOUND GASKET FOR RT DEICE PRESSURE REGULATING VALUE BLOWN, INSTALLED NEW GASKET, RAN ENGINE, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950818007821995081800782SO 1995 8 18 SWIA95598 119950714A275012025262501 CONTL MECH EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS OUT OF ADJUST A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07190SW 120050 ON DEPARTURE AFTER GEAR UP SELECTED AND NORMAL GEAR RETRACTOR LIGHT SEQUENCES, LOUD RUMBLING SOUND FROM FRONT OF PLANE OCCURRED DUE TO GEAR DOORS NOT CLOSING. RETURNED TO FIELD. REPLACED RELAY BOX, CYCLED GEAR 25 TO 30 TIMES, AND IT FUNCTIONED PROPERLY. 2L72 4T4 TRTA31SO E20NE 19950818007831995081800783EA 1995 8 18 SWIA95599 119950714A2750 CONTL MECH CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAPS MALFUNCTIONED A SWIAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 NM07410SW 7066 FLAPS FAIL MESSAGE, FLAP FAILED AT 18 DEGREES. CONTACTED SGU MAIN CONTROL. DIVERTED TO MSO. RESET FECU CIRCUIT BREAKER FLAPS FAIL MESSAGE, CLEANED FLAPS, OPS CKS NORMAL. 2L72 4F4 FRTA21EA E15NE 19950818007841995081800784EA 1995 8 18 SWIA95600 119950715A2750 FECU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAPS MALFUNCTIONED A SWIAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 NM07410SW 7066 FLAP FAIL MESSAGE AT FLAP RETRACTION AFTER TAKEOFF, FLAPS INOP, COMPLETED FLAPS UP LANDING. RESET FECU ON FLAP CON CHAN 1 AND CHAN 2, OPS CKS NORMAL. 2L72 4F4 FRTA21EA E15NE 19950818007851995081800785SO 1995 8 18 SWIA95601 119950716A2750 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM07190SW 120050 SHORTLY AFTER TAKEOFF WITH FLAPS SET 15 DEGREES, A FLAP ASYMMETRY OCCURRED, OUTBD FLAPS. CLEANED OUTBD FLAPS CANNON PLUG CONNECTION AND RERACKED FLAP COMPUTER. OPS CKS GOOD ON GROUND. 2L72 4T4 TRTA31SO E20NE 19950818007861995081800786GL 1995 8 18 SWIA95602 319950716A6110P65253220307 PROPELLER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP HARTZLHCB3T HCB3TN5 GL RT ENGINE MALFUNCTIONED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM0726902 3052 AC657 RT ENGINE HAS 10 TO 15 PERCENT T2 FLUCTUATIONS, 3 TO 5 PERCENT RPM FLUCTUATIONS, RETURNED TO PSP. REMOVED AND REPLACED RT PROP IAW MM 61-15-00. 1L72 4T4 T A8SW E4WE 6 CP15EA 19950818007871995081800787SO 1995 8 18 SWIA95603 119950718A27223211001003 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER MALFUNCTIONED A SWIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 NM07203SW11033 120240 RT RUDDER STIFF INFLIGHT NO UNWANTED YAW, RUDDER CENTERS NORMALLY, RUDDER TRIM SEEMS INHIBITED ALTHOUGH IT WORKS, TURNING OFF BLUE RUDDER SYSTM SOLVES STIFF RUDDER PEDAL PROBLEM, NO ANNUNICATOR INFLIGHT WITH BOTH RUDDER SYSTEMS TURNED OFF. PERFORMED RUDDER OVERBOOST, CHECK FOUND GOOD, INSPECTED RUDDER PCU AND ACTUATOR EXTENDS, FOUND NO DISCREPANCIES, OPS RUDDER SYSTEM IN ALL CONFIGURATIONS, COULD NOT DUPLICATE, SUSPECT BAD SOLENOID ON PCU, REPLACED RUDDER PCU, REPLACED BLUE SYSTEM RUDDER ACTUATOR. OPS CKS GOOD ON GROUND, NO LEAKS NOTED, PER MM 27-22-02. 2L72 4T4 TRTA31SO E20NE 19950818007881995081800788SO 1995 8 18 SWIA95604 119950718A6123 CONNECTOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTO FEATHER SYSDIRTY A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07204SW 120243 AUTO FEATHER DID NOT ARM DURING TAKEOFF ROLL, ABORTED TAKEOFF. CLEANED SIGNAL CONDITIONER CANNON PLUGS, GROUND OPS CKS GOOD, SEE F/L 80101. 2L72 4T4 TRTA31SO E20NE 19950818007891995081800789SO 1995 8 18 SWIA95605 119950720A6123141CC1AY1 RELAY EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTO FEATHER SYSFAILED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07204SW 120243 AUTO FEATHER WOULD NOT ARM ON TAKEOFF ROLL, ABORTED TAKEOFF. REPLACED AUTO FEATHER ARM RELAY, RAN ENGINES, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950818007901995081800790SW 1995 8 18 SWIA95606 119950721A79312719153001 OIL PRESS TRANS SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07184SW AC647 RT OIL PRESSURE GAUGE WENT TO ZERO AFTER TAKEOFF. REPLACED RT OIL PRESS TRANSUCER, RAN RT ENGINE, OPS CKS GOOD, NO LEAKS NOTED. 1L72 4T4 T A8SW E4WE 19950818007911995081800791SW 1995 8 18 SWIA95607 119950721A8200 AWI SYST SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT/RT ENGINE MALFUNCTIONED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 NM0726974 AC664 DURING TAKEOFF, AWI WAS TURNED ON, GOT BOTH LIGHTS BUT NO TORQUE RISE ON EITHER ENGINE. OPS CKS AWI SYSTEM ON GROUND, FOUND TO BE OPS NORMALLY AT THIS TIME. 1L72 4T4 T A8SW E4WE 19950818007921995081800792SO 1995 8 18 SWIA95608 119950723A6123K0039 RELAY EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE AUTO FEATHER SYSFAILED A SWIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NM07190SW 120050 RT PROP FEATHERED ON TAKEOFF ROLL. REMOVED AND REPLACED K0039 AND K0161 RELAYS WITH A NEW UNIT, AUTO FEATHER TESTS GOOD, GROUND RAN ENGINE TO TAKEOFF POWER, OPS CKS NORMAL. 2L72 4T4 TRTA31SO E20NE 19950818007931995081800793SW 1995 8 18 SWIA95609 119950723A77122719158007 TQ INDICATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RIGHT MALFUNCTIONED A SWIAK NONE O OTHER CRCRUISE 1 NM072699Y AC666 RT ENGINE TORQUE STICKS AT 20 PERCENT. REMOVED AND REPLACED RT TORQUE GAUGE, OPS CKS GOOD. 1L72 4T4 T A8SW E4WE 19950818007941995081800794SW 1995 8 18 SWIA95610 119950725A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT MLG OUT OF ADJUST A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM0727297 AC735 AFTER TAKEOFF IN LAX, LT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND LIGHT STILL INDICATED UNSAFE, APPROX 20 SECONDS AFTER GEAR HANDLE SELECTED UP, LT GEAR LIGHT ILLUMINATED GREEN, WHEN GEAR HANDLE SELECTED TO DOWN POSITION, NORMAL INDICATION 3 GREEN LIGHTS, DURING THIS JACKED AIRCRAFT, LUBED GREASED POINTS OF LT GEAR, ADJUSTED ACTUATORS IN 1 FULL TURN, PER MM 32-30-00, CYCLED GEAR 10 TIMES, OPS CKS GOOD. 1L72 4T4 T A8SW E4WE 19950818007951995081800795 1995 8 18 SWIA95611 419950728A34182744049027 SERVO SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP STICK PUSHER MALFUNCTIONED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM072685L AC648 STICK PUSHER ENGAGED FOUR TIMES ON CLIMB-OUT OF BUR NO AURAL WARNING OR SAS FAULT OBSERVED. REPLACED SAS CLUTCH SERVO, OPS CKS GOOD, IAW MM 27-30-44, SEE F/L 11547. 1L72 4T4 T A8SW E4WE 19950818007961995081800796SW 1995 8 18 SWIA95612 119950730A3234 SELECTOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LDG HANDLE OUT OF ADJUST A SWIAO OTHER O OTHER CLCLIMB 1 NM072698C AC665 AFTER TAKEOFF, LANDING HANDLE COULD NOT BE RELEASED FOR RETRACTION, OVERRIDE BUTTON WOULD NOT RELEASE IT EITHER, FINALLY IT RELEASED AFTER 5 MINUTES OF SHAFTING THE HANDLE AND PRESSING THE OVERRIDE BUTTON SIMULTANEOULSY. FOUND LOWER MOUNT SCREW FOR CLEAN HANDLE JAMMING UP OVERRIDE BUTTON, REMOVED LONG SCREW AND INSTALLED SHORT SCREW, OPS CKS GOOD, SEE F/L 12343. 1L72 4T4 T A8SW E4WE 19950818007971995081800797NM 1995 8 18 UPS204173 119950817A5313 STRINGER BOEING727 72727C 138400JNM BS 400 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND A GOUGE IN STR 5 LT STA. 400 (UPON CLEANING GOUGE FOUND STRINGER TO BE CRACKED). MAINTENANCE INSTALLED FABRICATED REPAIR PART IAW SRM 53-10-1, 51-30-2, 51-30-3. 2L73 4F A3WE 19950818007981995081800798NM 1995 8 18 UPS204174 119950817A5313 STRINGER BOEING727 72727C 138400JNM BS 420 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND A GOUGE IN STRINGER NR 6 LT STA 420. UPON CLEANING, FOUND STRINGER TO BE CRACKED. MAINTENANCE FABRICATED AND INSTALLED NEW STRINGER IAW SRM 53-10-1, 53-10-3, 53-10-4, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19950818007991995081800799NM 1995 8 18 UPS204175 119950817A5313 STRINGER BOEING727 72727C 138400JNM BS 380-440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8 LT STA 380-440. MAINTENANCE FABRICATED AND INSTALLED NEW STRINGER IAW SRM 51-10-6, 53-10-3, 51-10-1, 51-10-2 AND 51-30-2. 2L73 4F A3WE 19950818008001995081800800NM 1995 8 18 UPS204176 119950817A5313 STRINGER BOEING727 72727C 138400JNM BS 380-420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 8 RT BS 380-420. MAINTENANCE FABRICATED AND INSTALLED NEW STRINGER IAW SRM 53-10-6, 53-10-3, 51-10-2, 51-30-2, 51-30-5, AND 51-10-4. 2L73 4F A3WE 19950818008011995081800801NM 1995 8 18 UPS204177 119950817A5315 FLOOR BEAM BOEING727 72727C 138400JNM BS 380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AROUND NUT PLATE HOLES STA 380 RBL 45-60 AND LBL 45-65, WL 208. MAINTENANCE FABRICATED AND INSTALLED NEW REPAIR STRAP AND ANGLE IAW E.O. B727-5310-7283A, SRM 51-10-6, 51-10-2, AND 51-30-2. 2L73 4F A3WE 19950818008021995081800802NM 1995 8 18 UPS204178 119950817A5753 SPAR BOEING727 72727C 138400JNM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND R/W I/B MIDFLAP LOWER AFT SPAR CHORD CRACKED AT I/B AFT FLAP DRUM ROD CUTOUT. MAINTENANCE REPAIRED IAW SRM 57-50-02, 57-10-1, 51-30-02. 2L73 4F A3WE 19950818008031995081800803NM 1995 8 18 UPS204179 119950817A5711 SPAR BOEING727 72727C 138400JNM WS 221 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LT WING UPPER REAR SPAR CHORD AT WS 221 INBD OF TRUNNION FITTING. MAINTENANCE REPAIRED IAW E.O. 95-2880. 2L73 4F A3WE 19950818008041995081800804NM 1995 8 18 UPS204180 119950817A5744 CARRIAGE SPINDLE BOEING727 72727C 138400JNM TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE INSIDE SPINDLE ON NR 5 CARRIAGE. MAINTENANCE REMOVED AND REPLACED THE FLAP CARRIAGE IAW MM 27-51-03. 2L73 4F A3WE 19950818008051995081800805NM 1995 8 18 UPS204181 119950817A5347 SEAT TRACK BOEING727 72727C 138400JNM CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE SEAT TRACK FLANGE LBL 45 ON THE TOP STA 344-380, 560-640, ON BOTTOM STA 420-480 WL 208. MAINTENANCE REPAIRED THE SEAT TRACK IAW 51-30-02, 51-10-01, 51-30-08, 51-10-02 AND MM 51-20-15. 2L73 4F A3WE 19950818008061995081800806NM 1995 8 18 UPS204182 119950817A5751 FITTING BOEING727 72727C 138400JNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON L/W O/B AILERON LOCKOUT SUPPORT FITTING ON UPPER SURFACE AROUND BOLT HOLE THAT ATTACHES TO QUADRANT. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-10-6. 2L73 4F A3WE 19950818008071995081800807NM 1995 8 18 UPS204183 119950817A5751 FITTING BOEING727 72727C 138400JNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK ON THE L/W I/B AILERON I/B BALANCE BAY RIB CHORD. MAINTENANCE FABRICATED NEW CHORD AND INSTALLED IAW SRM 51-30-2, 51-10-1 AND 51-10-2. 2L73 4F A3WE 19950818008081995081800808NE 1995 8 18 UPS804233 219950810A7200 ENGINE DOUG DC8 DC871F 302199DWP GE CFM56 CFM562C1 13802NE NR 1 ENGINE MALFUNCTION A IPXAO OTHER Y ENGINE STOPPAGE DEDESCENT 1 SO01707UP 45907 692186 PILOT REPORTED NR 1 ENGINE SHUTDOWN DUE BANG AND N1, N2 AND F/F ALL CUT BACK. A/C ENGINE SHUTDOWN IAW QRH PROCEDURES. REPLACED NR 1 ENGINE PER TC 1001, 1002, 1003. OPS RUN AND LEAKS CHECK OK. PN CFM56-2-C1. 2L74 4F4 FRT4A25 E2GL 19950818008091995081800809EU 1995 8 18 95ZZZX4106 119950609A5541 RIB BAG BAE146BAE146100A 1500260EU RUDDER LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 MISSING AND LOOSE RIVETS IN RUDDER BOTTOM RIB (1). REMOVED AND REPLACED NR 1 RIB ON BOTTOM OF RUDDER IAW BAE 146 SRM AND REPAIR INSTRUCTION HC554H9005. 2H74 4F RTA49EU 19950818008101995081800810EU 1995 8 18 95ZZZX4107 119950606A2710 GUST DAMPENER BAG BAE146BAE146300A 1500267EU AILERONS FAILED A A6WAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31615AW E3141 DEN - FLT 357 - ON CONTROL CHECK, FOUND AILERON VERY STIFF TO MOVE EITHER RIGHT OR LEFT ESPECIALLY NEAR CENTER POSITION. FOUND THE RIGHT AILERON GUST DAMPER ROD END ON THE AILERON SIDE FROZEN. SENT A REPLACMENT DAMPER TO DEN. 2H74 4F RTA49EU 19950818008111995081800811EU 1995 8 18 95ZZZX4108 119950607A2710P311450002 GUST DAMPENER BAG BAE146BAE146300A 1500267EU AILERONS FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW DBPBAEA193 E3141 DEN - FLT 366 - ON CONTROL CHECK, FOUND AILERONS VERY STIFF TO MOVE EITHER RIGHT OR LEFT, ESPECIALLY NEAR CENTER POSITION. FOUND ROD END BEARING BAD AT RIGHT AILERON GUST DAMPER. REMOVED AND REPLACED RIGHT GUST DAMPER IAW MM 27-70-11. AILERON DISCONNECTED FOR TROUBLESHOOTING, RECONNECTED DISCONNECT SYSTEM IAW 27-11-34. CONTROLS TEST FREE. S/N OFF DBPBAEA193, S/N ON DBP.BAEA65. 2H74 4F RTA49EU 19950818008121995081800812EU 1995 8 18 95ZZZX4109 119950603A3234HTE210014 ACTUATOR BAG BAE146BAE146100A 1500260EU MLG SELECTOR VLVFAILED A A6WAO OTHER J WARNING INDICATION APAPPROACH 1 GL31246SS 781HB177H E1003 CRW - FLT 272 - ATTEMPTED GEAR EXTENSION, GEAR DID NOT MOVE. RED LIGHT IN GEAR HANDLE. SHORTLY THEREAFTER, GREEN HYD SYSTEM HI-TEMP LIGHT ILLUMINATED. CHARTERED MAINTENANCE TO THE AIRCRAFT. REPLACED THE GEAR SELECTOR VALVE ACTUATOR. 2H74 4F RTA49EU 19950818008131995081800813EU 1995 8 18 95ZZZX4110 119950603A5720 BOLT BAG BAE146BAE146100A 1500260EU LT WING LOOSE A A6WAK NONE K FLUID LOSS ININSP/MAINT 1 GL31463AP E1063 ATW - LEFT WING REAR SPAR ROOT JOINT FITTING AT RIB 2, BOLT 'A' IS LOOSE AND LEAKING. REMOVED AND REPLACED BOLT 'A' AT LEFT WING REAR SPAR JOINT FITTING. BOLT HEAD HAS BEEN SEALED AT 1440. W/C GENERATED FOR LEAK CHECK W/C 5020. 2H74 4F RTA49EU 19950818008141995081800814EU 1995 8 18 95ZZZX4111 119950426A5313 STRINGER BAG BAE146BAE146300A 1500267EU BS 29.54 DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31616AW E3145 ATW - C/W E.O. E95/005/653. ORIGINAL ISSUE ON LT AND RT FRAME 29 STRINGERS AT STA 25.94 FOUND DAMAGED. REPAIRED RT FRAME 29 STRINGER AT STA 29.54 IAW E.O. E95/005/653. ORIGINAL ISSUE. REPAIRED LT FRAME 29 STRINGER AT STA 25.94 IAW E.O. E95/005/653. ORIGINAL ISSUE AND AVRO FAX NR DJR/RJ0592-95. 2H74 4F RTA49EU 19950818008151995081800815EU 1995 8 18 95ZZZX4112 119950424A2750 OPERATING RODS BAG BAE146BAE146200A 1500266EU LT TE FLAP BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31294UE E2107 ATW - LEFT INBOARD FLAP TRACK COVER, INBOARD PAIR OF OPERATING RODS FOUND BROKEN WHEN FLAPS WERE RETRACTING. REPLACED FLAP TRACK COVER AND RODS. 2H74 4F RTA49EU 19950818008161995081800816NE 1995 8 18 95ZZZX4113 219950424A7310216362035 FUEL MANIFOLD BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE CRACKED A AA6WAK NONE O OTHER ININSP/MAINT 1 GL31616AW1763 1777P E3145 ATW - FOUND CRACK INDICATION ON 5TH SCALLOP OF RIGHT FUEL MANIFOLD, NR 1 ENGINE. P/N 2-163-620-35, S/N 1777P. AIRCRAFT IN HEAVY CHECK, MAINIFOLD TO BE REPLACED. 2H74 4F4 FRTA49EU E6NE 19950818008171995081800817NE 1995 8 18 95ZZZX4114 219950417A7310216362036 FUEL MANIFOLD BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NR 4 ENGINE CRACKED A AA6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP15230807 83E012 E1063 ATW - NR 4 ENGINE, LEFT FUEL MANIFOLD CRACKED, FOUND ON INSPECTION. REPLACED FUEL MANIFOLD. 2H74 4F4 FRTA49EU E6NE 19950818008181995081800818EU 1995 8 18 95ZZZX4115 119950504A5320 STIFFENER BAG BAE146BAE146300A 1500267EU FRAME 29 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 ATW - STIFFENER CRACKED AT FRAME 29 (POSITION 25.94 LT). C/W EO E95/005/653. ORIGINAL ISSUE AT LT STA 25.94 ON FRAME 29. 2H74 4F RTA49EU 19950818008191995081800819EU 1995 8 18 95ZZZX4116 119950504A5531 RIB BAG BAE146BAE146300A 1500267EU VERT STABILIZER CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 RIGHT SIDE OF VERTICAL STABILIZER, RIB 1, STABILIZER TO FUSELAGE CLOSURE ANGLE HAS 2 INCH CRACK THROUGH FASTENER AT FORWARD EDGE OF VERTICAL STABILIZER. REPAIRED IAW BAE REPAIR DRAWING HC550H9004 AND FAX REF KW/0863-91. 2H74 4F RTA49EU 19950818008201995081800820EU 1995 8 18 95ZZZX4117 119950504A5320 STIFFENER BAG BAE146BAE146300A 1500267EU FRAME 29 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 STIFFENER CRACKED AT FRAME 29 (POSITION 25.94 RT) C/W EO E95/005/653 ORIGINAL ISSUE, RT STA 25.94 ON FRAME 29. 2H74 4F RTA49EU 19950818008211995081800821EU 1995 8 18 95ZZZX4118 119950708A5330 SKIN BAG BAE146BAE146200A 1500266EU FWD FUSELAGE BIRD STRIKE A A6WAA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL31609AW E2070 DEN - FLT 353 - EN ROUTE, BIRD STRIKE ON NOSE OF AIRCRAFT. AIR RETURN. INSPECTED AIRCRAFT IAW BAE MM 05-50-21. BIRD STRIKE INSPECTION. NO DEFECTS NOTED ON AIRCRAFT OR ENGINES. 2H74 4F RTA49EU 19950818008221995081800822EU 1995 8 18 95ZZZX4119 119950621A5414 SKIN BAG BAE146BAE146100A 1500260EU NR 3 PYLON CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 NR 3 ENGINE PYLON - PRE-COOLER DUCT RIVETS LOOSE AND SKIN CRACKED AFT OF SHOULDER COWL. REMOVED DUCT ASSY. REPAIRED CRACK IAW PS-1 REPAIR DRAWING NR HC711H9006, REINSTALLED DUCT ASSY. 2H74 4F RTA49EU 19950818008231995081800823EU 1995 8 18 95ZZZX4120 119950620A5400HC712H0041000 BOLT BAG BAE146BAE146100A 1500260EU NR 2 PYLON CRACKED A AA6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 NR 2 ENGINE YOKE TO PYLON BOLT, LEFT TOP TO BE REMOVED FOR MAINTENANCE INSPECTION OF CRACK INDICATION ON THREAD RUN-OUT AREA. REF: P/N HC712H0041-000. SSI 54-00-123. CARD NR 268. REPLACED NR 2 ENGINE YOKE TO PYLON BOLT AT LEFT TOP POSITION. 2H74 4F RTA49EU 19950818008241995081800824EU 1995 8 18 95ZZZX4121 119950620A5400HC574H003620D BOLT BAG BAE146BAE146100A 1500260EU NR 3 PYLON CRACKED A AA6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 NR 3 PYLON - LOWER RT BOLT, P/N HC574H0036-20D, REQUIRES REMOVAL FOR VERIFICATION OF CRACK INDICATIONS, REF SSI 57-20-174. REMOVED AND REPLACED RT LOWER NR 3 PYLON BOLT, P/N HC574H0036-200, IAW A.M.M. 2H74 4F RTA49EU 19950818008251995081800825EU 1995 8 18 95ZZZX4122 119950616A5210 SKIN BAG BAE146BAE146100A 1500260EU PASSENGER DOOR DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 LEFT REAR PASSENGER DOOR OUTER SKIN HAS A 1 INCH LONG SCRAPE AT THE BOTTOM AFT CORNER (WITH DOOR CLOSED). INSPECTED SCRAPED AREA AT LOWER AFT CORNER OF REAR PASSENGER DOOR. DAMAGED AREA FOUND TO BE MINOR. TREATED DAMAGED AREA AND REPAINTED. 2H74 4F RTA49EU 19950818008261995081800826EU 1995 8 18 95ZZZX4123 119950615A2750 BOLT BAG BAE146BAE146100A 1500260EU NR 4 TE FLAP FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 BY MT AND PT METHODS OF NDT, FOUND UPPER CARRIAGE-TO-LEVER PIN ASSY CRACKED IN THE HEAD-TO-SHANK RADIUS. (NR 4 RT CARRIAGE.) REF: SSI 57-55-129. REMOVED AND REPLACED OUTBOARD BOLT ON NR 4 RT FLAP TRACK CARRIAGE (UPPER CARRIAGE-TO-LEVER PIN). 2H74 4F RTA49EU 19950818008271995081800827EU 1995 8 18 95ZZZX4124 119950614A5541 RIBS BAG BAE146BAE146100A 1500260EU RUDDER BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 RUDDER RIBS 2 AND 3 ARE CRACKED AND BROKEN. REPAIRED RIBS 2 AND 3 ON BOTTOM OF RUDDER IAW 146 SRM 55-40-11 AND SRM 51-71-11 STANDARD PRACTICES. 2H74 4F RTA49EU 19950818008281995081800828EU 1995 8 18 95ZZZX4125 119950614A5730 SKIN BAG BAE146BAE146100A 1500260EU RT WING CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 RIGHT FUSELAGE IS CHAFED WHERE UNDER WING PANEL SEALS RUB ON FUSELAGE. LOCATED BETWEEN FRAME 32 AND FRAME 33A ABOVE CABIN WINDOWS. SSI NR 53-20-159D. INSPECTED AND BLENDED OUT, ALCROMED AND REPRIMED. PERFORMED EO E92/045/653. ORIGINAL REVISION GENERATED WORK CARD FOR CHAFE OVER FRAME 33 THAT RUNS FORE AND AFT AT .003 INCH FOR 7.50 INCHES (REF W/C 6014) AND REF W/C 6016 FOR ND. 2H74 4F RTA49EU 19950818008291995081800829EU 1995 8 18 95ZZZX4126 119950613A2750 PIN BAG BAE146BAE146100A 1500260EU TE FLAPS FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 LEFT NR 3 LOWER FLAP TRACK CARRIAGE TO SCREW JACK TRUNNION PIN FAILED N.D.T. NOTE: SEVERAL INDICATIONS IN PIN-TO-FLANGE RADIUS. REMOVED AND REPLACED LEFT NR 3 LOWER FLAP TRACK CARRIAGE TO SCREW JACK TRUNNION PIN IAW A.M.M. 2H74 4F RTA49EU 19950818008301995081800830EU 1995 8 18 95ZZZX4127 119950612A2420 ACT BOLT BAG BAE146BAE146100A 1500260EU RUDDER DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 AFT UPPER RUDDER ACTUATOR BOLT IS GALLED AND SCORED. SSI 55-40-105 (INSTALLED BAD BOLT TO FOM). REMOVED AND REPLACED BOLT AND SAFTIED. 2H74 4F RTA49EU 19950818008311995081800831EU 1995 8 18 95ZZZX4128 119950612A2720 ACT BOLT BAG BAE146BAE146100A 1500260EU RUDDER DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 AFT LOWER RUDDER ACTUATOR BOLT IS PITTED AND SHANK IS SCORED. SSI 55-40-105. REMOVED AND REPLACED AFT LOWER RUDDER ACTUATOR BOLT IAW AMM. 2H74 4F RTA49EU 19950818008321995081800832EU 1995 8 18 95ZZZX4129 119950508A5320 INTERCOSTAL BAG BAE146BAE146300A 1500267EU CABIN CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 FORWARD VEST, INTERCOSTAL IN FRONT OF F/A SEAT CORRODED. REMOVED AND REPLACED INTERCOSTAL AND SUPPORT MEMBER WITH ASSOCIATED GUSSET PLATES IN FORWARD VEST FRAME 15 - FRAME 18, IN FRONT OF THE F/A SEAT IAW SRM. 2H74 4F RTA49EU 19950818008331995081800833EU 1995 8 18 95ZZZX4130 119950504A3610 AIR VALVE BAG BAE146BAE146200A 1500266EU NR 1 ENGINE STUCK A A6WAO OTHER J WARNING INDICATION CRCRUISE 1 GL31607AW E2052 DEN - FLT 366 - NR 1 ENGINE AIR VALVE STUCK OPEN AT ALTITUDE. CLEANED POPPET VALVE - NO FIX, REPLACED THE VALVE. 2H74 4F RTA49EU 19950818008341995081800834EU 1995 8 18 95ZZZX4131 119950508A2710 CABLES BAG BAE146BAE146300A 1500267EU AILERON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31611AW E3120 AILERON INTERCONNECT CABLES CORRODED AT WING ROOT PULLEY. REMOVED AND REPLACED AILERON INTERCONNECT CABLES PER BAE 146 MM. WORK CARD GENERATED FOR AILERON DISCONNECT TO BE RESET AND INTERCONNECT CABLES TO BE RIGGED W/C 2149. 2H74 4F RTA49EU 19950818008351995081800835EU 1995 8 18 95ZZZX4132 119950508A3610 DUCT VALVES BAG BAE146BAE146300A 1500267EU APU MALFUNCTIONED A A6WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31616AW E3145 DEN - FLT 381 - RIGHT ZONE HIGH-TEMP LIGHT ILLUMINATED IN-FLIGHT. NO LEAKS NOTED IN THE SPINE AREAS. FOUND A LEAK IN THE APU AIR SUPPLY DUCT TO THE Y-DUCT SUPPLYING THE 2 MANIFOLDS. BOTH DUCT RELIEF VALVES NEED TO BE REPLACED. PLACED APU AIR ON MEL. REPLACED THE DUCT RELIEF VALVES. THE FLIGHT CREW FOUND THERE WERE THREE EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE ASSOCIATED POWER SUPPLY. 2H74 4F RTA49EU 19950818008361995081800836EU 1995 8 18 95ZZZX4133 119950508A3350 EEL BAG BAE146BAE146300A 1500267EU CABIN INOPERATIVE A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31616AW E3145 DEN - FLT 381 - RIGHT ZONE HIGH-TEMP LIGHT ILLUMINATED IN-FLIGHT. NO LEAKS NOTED IN THE SPINE AREAS. FOUND A LEAK IN THE APU AIR SUPPLY DUCT TO THE Y-DUCT SUPPLYING THE 2 MANIFOLDS. BOTH DUCT RELIEF VALVES NEED TO BE REPLACED. PLACED APU AIR ON MEL. REPLACED THE DUCT RELIEF VALVES. THE FLIGHT CREW FOUND THERE WERE THREE EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED THE ASSOCIATED POWER SUPPLY. 2H74 4F RTA49EU 19950818008371995081800837NE 1995 8 18 95ZZZX4134 219950514A7320216362035 MANIFOLD BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NR 4 ENGINE DIRTY A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS 1637 E1003 DURING SCHEDULED ET INSPECTION OF THE NR 4 ENGINE FUEL MANIFOLDS, FOUND INDICATION OF SOOT AT THE SCALLOPS. REPLACED BOTH NR 4 ENGINE FUEL MANIFOLDS. A/C TT 6445 - LEFT. 2H74 4F4 FRTA49EU E6NE 19950818008381995081800838NE 1995 8 18 95ZZZX4135 219950514A7320216362036 MANIFOLD BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NR 4 ENGINE DIRTY A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS 1031P E1003 DURING SCHEDULED ET INSPECTION OF THE NR 4 ENGINE FUEL MANIFOLDS, FOUND INDICATION OF SOOT AT THE SCALLOPS. REPLACED BOTH NR 4 ENGINE FUEL MANIFOLDS. A/C TT 9434 - RIGHT. 2H74 4F4 FRTA49EU E6NE 19950818008391995081800839EU 1995 8 18 95ZZZX4136 119950513A2730 CONTROLS BAG BAE146BAE146200A 1500266EU ELEVATOR OSCILLATED A AA6WAO OTHER O OTHER CLCLIMB 1 GL31610AW E2082 DEN - FLT 365 - AIRCRAFT EXPERIENCED A PITCH OSCILLATION ON CLIMB-OUT FROM MLI IN FREEZING PRECIPITATION AT FL 210 AND 250 KNOTS. INSPECTION A/C AND C/W BAE OSCILLATION INCIDENT CHECKLIST. NO DEFECTS NOTED. 2H74 4F RTA49EU 19950818008401995081800840NE 1995 8 18 95ZZZX4137 219950509A7320216362036 MANIFOLD BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 2 ENGINE CRACKED A AA6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW10468 529 E2070 DURING ROUTINE MAINTENANCE, FOUND NR 2 ENGINE LEFT FUEL MANIFOLD HAD EVIDENCE OF A FIRE AND AN INDICATION OF A CRACK. REPLACED THE MANIFOLD. 2H74 4F4 FRTA49EU E6NE 19950818008411995081800841 1995 8 18 95ZZZX4138 419950515A2565D31050 ESCAPE SLIDE BAG BAE146BAE146300A 1500267EU LT AFT DOOR MALFUNCTIONED A AA6WAK NONE L NO TEST ININSP/MAINT 1 GL31615AW11333 0518 E3141 LEFT AFT DOOR ESCAPE SLIDE DUE A SCHEDULED DEPLOYMENT BUT DID NOT DEPLOY CORRECTLY, IT WENT AFT OF THE FUSELAGE. REPLACED SLIDE. 2H74 4F RTA49EU 19950818008421995081800842EU 1995 8 18 95ZZZX4139 119950711A3411 PITOT TUBE BAG BAE146BAE146300A 1500267EU NR 1 PLUGGED A A6WAK NONE O OTHER NRNOT REPORTED 1 GL31615AW E3141 NR 1 A/S INDICATOR INOPERATIVE. FOUND NR 1 PITOT TUBE AT HEAD PLUGGED, BLEW OUT FROM INSTRUMENT TO HEAD. OPS AND LEAK CHECKED GOOD. 2H74 4F RTA49EU 19950818008431995081800843 1995 8 18 95ZZZX4140 419950710A3414WL106AMA20 AIRSPEED IND BAG BAE146BAE146200A 1500266EU LEFT MALFUNCTIONED A A6WACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL31606AW20335 AG789 E2033 ATW - FLT 300 - CAPTAIN'S AIRSPEED INDICATOR READ ZERO ON TAKEOFF ROLL AT 80 KNOT SPEED CHECK, FIRST OFFICER'S WAS OK. ABORTED TAKEOFF AND RETURNED TO THE GATE. ATW MAINTENANCE PUMPED UP PITOT SYSTEM AND AIRSPEED READ NORMAL, MAINTENANCE CTL DECIDED TO REPLACE INDICATOR AS A PRECAUTION. ABORTED SECOND TAKEOFF WITH SAME PROBLEM, SWAPPED AIRCRAFT. 2H74 4F RTA49EU 19950818008441995081800844EU 1995 8 18 95ZZZX4141 119950525A5320 STIFFENER BAG BAE146BAE146300A 1500267EU BS 25.94 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31614AW E3132 LEFT AND RIGHT FRAME 29 STIFFENERS CRACKED AT STA 25.94 E.O. E95/005/653. ORIGINAL ISSUE NEEDS TO BE C/W. REPAIRED CRACKED STIFFENERS IAW E.O. E95/005/653, ORIGINAL ISSUE. REPAIR DRAWINGS AW-53-20-9506-06. 2H74 4F RTA49EU 19950818008451995081800845EU 1995 8 18 95ZZZX4142 119950518A2910HTE9531101 ISO VALVE BAG BAE146BAE146200A 1500266EU LEFT ENGINE FAILED A A6WAO OTHER J WARNING INDICATION CRCRUISE 1 GL31609AW15264 785VB137 E2070 ORD - FLT 372 - YELLOW HYDRAULIC HI-TEMP WARNING LIGHT CAME ON, 25 MINUTES INTO FLIGHT, LIGHT WENT OUT APPROXIMATELY 10 MINUTES LATER. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP ISO VALVE. OPS AND LEAK CHECK GOOD. S/N OFF 785VB137. S/N ON 1185VB154. 2H74 4F RTA49EU 19950818008461995081800846EU 1995 8 18 95ZZZX4143 119950418A5260C14648 RAIL BAG BAE146BAE146200A 1500266EU AIRSTAIR DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 ATW - FORWARD AIRSTAIR INBOARD RAIL FORWARD END, CORRODED BEYOND LIMITS. REMOVED AND REPLACED FORWARD AIRSTAIR INBOARD RAIL. 2H74 4F RTA49EU 19950818008471995081800847EU 1995 8 18 95ZZZX4144 119950408A3350 EEL WIRE BAG BAE146BAE146300A 1500267EU CABIN LOOSE A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31616AW E3145 DEN - FLT 366 - FLOOR TRACK LIGHTING, ROW 10 - ROW 20 INOPERATIVE. FOUND LOOSE WIRE AT ROW 10, REPAIRED, OPS CHECKED GOOD. 2H74 4F RTA49EU 19950818008481995081800848EU 1995 8 18 95ZZZX4145 119950404A5320 INTERCOSTAL BAG BAE146BAE146300A 1500267EU CARGO BAY BENT A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 INTERCOSTAL RIB BETWEEN FRAME 20 AND FRAME 21, RT LOWER SIDE, FORWARD CARGO BAY, BENT. REPLACED INTERCOSTAL RIB PER FAX DJH/RJ0504-95 DATED 4-5-95. 2H74 4F RTA49EU 19950818008491995081800849EU 1995 8 18 95ZZZX4146 119950403A3234HTE210014 SELECTOR VLV ACT BAG BAE146BAE146100A 1500260EU LANDING GEAR MALFUNCTIONED A A6WAO OTHER J WARNING INDICATION APAPPROACH 1 GL31246SS5275 891GB160 E1003 ORD - FLT 349 - GEAR HANDLE SELECTED DOWN 3 TIMES BEFORE GEAR DROPPED. RED HANDLE LIGHT CAME ON. REMOVED AND REPLACED ELECTRICAL GEAR SELECTOR VALVE ACTUATOR C/W BAE MM SUPPLEMENT PAGE 32-30-17. S/N OFF 8916B160. S/N ON 7816B177/H. 2H74 4F RTA49EU 19950818008501995081800850EU 1995 8 18 95ZZZX4147 119950401A5720 CLEAT BAG BAE146BAE146300A 1500267EU LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 LEFT WING TRAILING EDGE STRUCTURE BETWEEN RIBS 7 AND 8 HAS A CRACKED CLEAT ATTACHING STIFFENER TO THE REAR FALSE SPAR. REMOVED AND REPLACED CLEAT BETWEEN LEFT WING TRAILING EDGE BETWEEN RIBS 7 AND 8 IAW BAE 146-300 SRM. 2H74 4F RTA49EU 19950818008511995081800851EU 1995 8 18 95ZZZX4148 119950331A5720 FALSE SPAR BAG BAE146BAE146300A 1500267EU LT WING CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 LEFT WING TRAILING EDGE FALSE SPAR HAS A 2.50 INCH CRACK AT THE INBOARD LIFT SPOILER CENTER HINGE POINT. STOP DRILLED CRACK. C/W PLATE REPAIR OVER LEFT WING TRAILING EDGE OF FALSE SPAR JUST INBOARD OF LIFT SPOILER CENTER HINGE POINT IAW REPAIR DRG HC572H9036 AND BAE 146-300 SRM. 2H74 4F RTA49EU 19950818008521995081800852EU 1995 8 18 95ZZZX4149 119950330A5260 RAILS BAG BAE146BAE146300A 1500267EU AIR STAIR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 INNER AIR STAIR RAIL (AFT STAIRS) AFT END, CORRODED. REPLACED INNER AIR STAIR RAIL (TRACK ONLY) ON AFT STAIRS. 2H74 4F RTA49EU 19950818008531995081800853EU 1995 8 18 95ZZZX4150 119950330A5320 SILL BAG BAE146BAE146300A 1500267EU SERVICE DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 AFT SERVICE DOOR SILL PLATE HAS SOME CORROSION. REPLACED AFT RT SILL PLATE. 2H74 4F RTA49EU 19950818008541995081800854EU 1995 8 18 95ZZZX4151 119950330A5260 TREAD PLATE BAG BAE146BAE146300A 1500267EU AIRSTAIR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 FORWARD AIRSTAIRS, 4TH TREAD PLATE FROM BOTTOM, CORRODED. REMOVED AND REPLACED 4TH FROM BOTTOM TREAD PLATE. ALSO, REMOVED AND REPLACED AFT TREAD PLATE SUPPORT BRACKET DUE TO BEING CORRODED. 2H74 4F RTA49EU 19950818008551995081800855EU 1995 8 18 95ZZZX4152 119950329A2710B6038081 ROD END BAG BAE146BAE146300A 1500267EU AILERON CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 LEFT INNER AILERON TRIM TAB ROD, SUSPECT CRACKED FERRULE, NEEDS CLEANING, STRIPPING AS NECESSARY. REMOVED AND REPLACED ROD END. 2H74 4F RTA49EU 19950818008561995081800856EU 1995 8 18 95ZZZX4153 119950327A2710 CABLES BAG BAE146BAE146300A 1500267EU AILERONS CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 AILERON INTERCONNECT CABLES HAVE SIGNS OF CORROSION AT BOTH WING ROOT PULLEYS ON LT AND RT SIDES. ALSO, ALL 4 PULLEYS HAVE RUST DEPOSITS. REMOVED AND REPAIRED BOTH CENTER SECTIONS OF AILERON INTERCONNECT CABLE CIRCUITS PER MM. REMOVED ALL 4 PULLEYS AND CLEANED RUST DEPOSITS. REINSTALLED PULLEYS AND TENSIONED CABLES PER MM. FUNCTION TEST OF DISCONNECT SYSTEM OK. REF: WC 5005. 2H74 4F RTA49EU 19950818008571995081800857EU 1995 8 18 95ZZZX4154 119950324A5320 FIREWALL BAG BAE146BAE146300A 1500267EU APU CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 FOUND APU BAY FORWARD WALL CRACK ABOVE EXHAUST PIPE LOOKING FROM ECS BAY. REMOVED AND REPLACED APU FIREWALL. ALL WORK ACCOMPLISHED IAW BAE DRAWING P/N HC260H9000 AND PARTS SUPPLIED IN MOD KIT P/N HCM36179A-A01. EXISTING TITANIUM DISHING RE-USED IN LIEU OF MISDRILLED SUPPLIED INNER SKIN. BOLT HOLES IN SKIN DYE CHECKED FOR CRACKS. 2H74 4F RTA49EU 19950818008581995081800858WP 1995 8 18 95ZZZX4155 119950713A3222 OLEO SEALS DOUG DC9 DC931 3022065WP NLG STRUT STICKING A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05977Z 47249 STL - FLT 246 - AFTER TAKEOFF, LANDING GEAR HANDLE WAS LOCKED IN THE DOWN POSITION. FOUND NOSE LANDING GEAR OLEO STICKING IN THE COMPRESSED POSITION. REPLACED NOSE LANDING GEAR SEALS, MFG KIT P/N A03772REVH. NOSE GEAR OPERATION CHECKED NORMAL. CHECK C - 6-30-94 - STL. 2L72 4F A6WE 19950818008591995081800859WP 1995 8 18 95ZZZX4156 119950530A5313 LONGERON DOUG DC9 DC931 3022065WP BS 218 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05976Z 47248 STL - DURING OP-15, FOUND .1250 INCH CRACK IN LONGERON 29R, STA 218. REPAIRED BY REPLACING LONGERON PER SRM 51-10-0, PAGES 1 AND 2, AND STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 66,307 HOURS; 81,239 CYCLES. 2L72 4F A6WE 19950818008601995081800860WP 1995 8 18 95ZZZX4157 119950622A5320 DOOR OPENING DOUG DC9 DC915 3022036WP BS 750 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05975Z 47035 STL - DURING SPECIAL CHECK, FOUND A ONE-INCH CRACK IN AFT CARGO BIN BOTTOM AT AFT CORNER OF DOOR OPENING, WHICH WAS ALSO BENT, STA 750. REPAIRED PER EMLR 65708. AIRCRAFT TOTAL TIME: 60,441 HOURS; 77,859 CYCLES. 2L72 4F A6WE 19950818008611995081800861EU 1995 8 18 SIMA952082 119950727A324650092361 WHEEL 5010488 SAAB SF340 340B 7860101EU NR 3 CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21595MA3587 JAN920445 340B216 LAW - LAW SHOP - WHEEL ASSY WAS REMOVED FROM AIRCRAFT IN LAW AND SENT TO WHEEL SHOP. THE WHEEL ASSY HAS A .50 INCH CRACK ON FLANGE OF INNER WHEEL ASSY. THE INNER WHEEL ASSY HAS BEEN REMOVED FROM SERVICE. CRACK WAS FOUND DURING NDT INSPECTION ON 7-31-95. PART TOTAL CYCLES 3767. (X) 2L72 4T RTA52EU 19950818008621995081800862EU 1995 8 18 SIMA952101 119950729A3350 EEL WIRING SAAB SF340 SF340A 7850100EU CABIN LOOSE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21119AE 340A119 DFW - FLT 3519 - F/A'S EMERGENCY LIGHT SWITCH IS INOPERATIVE. INSPECTED AND REPAIRED LOOSE WIRING AT THE SWITCH. AIRCRAFT RETURNED TO SERVICE. (X0 2L72 4T RTA52EU 19950818008631995081800863EU 1995 8 18 SIMA952111 119950730A2622892480 FIRE BOTTLE AEROSPATR72 ATR72212 EU CABIN MALFUNCTIONED A SIMAK NONE O OTHER CLCLIMB 1 SW21410AT2481 211293 410 CRP - FLT 3833 - THE AFT FIRE EXTINGUISHER DISCHARGED IN THE OVERHEAD BIN AFTER TAKEOFF. REASON FOR DISCHARGE IS UNKNOWN. REPLACED FIRE EXTINGUISHER. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2754. (X) 2H72 4T RTA53EU 19950818008641995081800864EU 1995 8 18 SIMA952112 119950730A29109302631001 HYD LINE SAAB SF340 SF340A 7850100EU HYD MANIFOLD FAILED A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW21114SB 340A114 DFW - FLT 3888 - AIRCRAFT LOST HYDRAULIC PRESSURE AFTER LANDING. REMOVED AND INSPECTED SUPPLY MANIFOLD PRESSURE LINE SYSTEM. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19950818008651995081800865EU 1995 8 18 SIMA952151 119950803A3260D49410001 CONTROL BOX SAAB SF340 SF340A 7850100EU LANDING GEAR FAILED A SIMAO OTHER N FALSE WARNING APAPPROACH 1 SW21107AE4217 1760687 340A107 DFW - FLT 7615 - NO LANDING GEAR INDICATION. REMOVED AND INSPECTED LANDING GEAR CONTROL BOX. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 4614. (X) 2L72 4T RTA52EU 19950825000011995082500001WP 1995 8 25 9512559880 119950813A3232 ACTUATOR DOUG DC9 DC951 3022051WP NLG FAILED A NWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01675MC 47651 VIBRATION AND NOISE FROM NOSE GEAR AREA OCCURRED ON GEAR RETRACTION AFTER TAKEOFF. NOSE GEAR AND RED UNSAFE LIGHT ALSO ILLUMINATED. RECYCLED GEAR SEVERAL TIMES AND LIGHT REMAINED ON. PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND RETURNED TO RDU. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND DAMAGE TO FORWARD NOSE GEAR DOOR, RELEASE ACTUATOR, AND DOOR STOP CABLE. IT IS SUSPECTED THAT THE DOOR RELEASE ACTUATOR HAD FAILED. REPLACED CABLE, ACTUATOR, AND REPAIRED DOOR. INSPECTED NOSE GEAR PROXIMITY SENSOR FOR ADJUSTMENT AND SECURITY. ALL CHECKED GOOD. PERFORMED RETRACTION TEST OF NOSE GEAR SEVERAL TIMES. NO PROBLEMS WERE FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825000021995082500002 1995 8 25 9512569940 419950813A22102589445933 YAW DAMPER DOUG DC9 DC932 3022066WP AUTO PILOT MALFUNCTIONED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL013322L448808 47031 DURING CLIMB THROUGH 26,000 FEET WITH AUTO-PILOT ENGAGED, THE AIRCRAFT SUDDENTLY YAWED TO ONE SIDE THEN THE OTHER. DISCONNECTED AUTO-PILOT AND PROBLEM CONTINUED. SWITCHED RUDDER CONTROL MANUAL; YAWING CEASED. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT DIVERTED TO TYS. NOTE: NUMEROUS RUDDER TRIM CHANGES WERE REQUIRED DURING CONTINUATION OF FLIGHT TO MAINTAIN CENTERED POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE YAW DAMPER ACTUATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825000031995082500003 1995 8 25 95UAL900098 419950818A2397 HARNESS BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN ARCED A UALAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29642UA 25092 FOUND WIRE BUNDLE ARCING ALONG SIDEWALL FLOOR BETWEEN SEATS 2A AND 3A. FOUND CHAFED WIRES DUE TO CONTACT WITH SIDE WALL GRILL. REPAIRED WIRES. SYSTEM OPS CHECKS OK. 2L72 4F4 FRTA1NM E24NE 19950825000041995082500004WP 1995 8 25 ABXA9500645 119950731A53125910163259 BLKHD T CAP DOUG DC9 DC932F 3022067WP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING COMPLIANCE OF A.D. 89-06-04 AND 89-16-12; A.S.B. A53-231 AND A53-232, FOUND AFT PRESSURE BULKHEAD CRACKED AT LONGERON 16L. REPLACED T-CAP IAW DC-9 S.B. A53-231. 2L72 4F A6WE 19950825000051995082500005WP 1995 8 25 ABXA9500646 119950731A57115911301503 SPAR DOUG DC9 DC931 3022065WP WS 164 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTION, FOUND THE RIGHT WING REAR SPAR CAP CRACKED AT THE LOWER FLAP HINGE ATTACH STUDS, STA 164. REPAIRED IAW ABX EA AD-57-03904-MR. 2L72 4F A6WE 19950825000061995082500006WP 1995 8 25 ABXA9500647 119950712A56105644324 RETAINER DOUG DC9 DC931 3022065WP COCKPIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03, FOUND THE LEFT OVERHEAD WINDOW OUTER RETAINER CRACKED. REPAIRED IAW EA AD-56-03239-MA. 2L72 4F A6WE 19950825000071995082500007WP 1995 8 25 ABXA9500648 119950724A55319911881 RIB DOUG DC9 DC931 3022065WP VERT STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTION, SEVERAL RIBS WERE FOUND CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPAIRED OR REPLACED RIBS IAW DC-9 SUPP., SRM DRAWING K05159, AND DC-9 SRM 51-30-5, 51-30-2 AND 51-30-3. 2L72 4F A6WE 19950825000081995082500008WP 1995 8 25 ABXA9500649 119950718A53205910130225 GUSSETT DOUG DC9 DC931 3022065WP AFT FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTI0N, FOUND A CRACK IN THE GUSSET OF THE VENTRAL DOOR JAMB, RIGHT SIDE, FORWARD EDGE. REPAIRED IAW ABX REA D953-12213-MR. 2L72 4F A6WE 19950825000091995082500009WP 1995 8 25 ABXA9500650 119950725A5311995821429 FRAME DOUG DC9 DC931 3022065WP BS 897 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTION, A FUSELAGE FRAME AT STA 897 BETWEEN LONGERONS 30 AND 29 R WAS FOUND WITH IMPROPERLY DRILLED HOLES. REPAIRED IAW ABX REA D953-12219-MR. 2L72 4F A6WE 19950825000101995082500010WP 1995 8 25 ABXA9500651 119950719A5311991224672 FRAME DOUG DC9 DC931 3022065WP BS 1059 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C - CHECK INSPECTION, FOUND THE FUSELAGE FRAME AT STA 1059, LONGERON 5L, GOUGED. REPAIRED IAW ABX REA D953-12144-MR. 2L72 4F A6WE 19950825000111995082500011WP 1995 8 25 ABXA9500652 119950701A783059587821 LINK DOUG 591029415 DOUG DC9 DC931 3022065WP LEFT CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23948AX 47455 47065 DURING COMPLIANCE OF A.D. 75-14-06; A.D. 90-18-03; S.B.'S 78-36, 78-38, 78-40 AND 78-66, FOUND NR 2 LOWER LEFT DRIVER LINK HAD A CRACK INDICATION. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 78-30-1. SHOP FINDINGS: LINK CORRODED AND PITTED BEYOND LIMITS. LINK WAS SCRAPPED. 2L72 4F A6WE 19950825000121995082500012WP 1995 8 25 ABXA9500653 119950621A521059100817 SKIN DOUG DC9 DC941 302207NWP MAIN ENTRY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 DURING PRE-FLIGHT INSPECTION, FOUND THE MAIN ENTRY DOOR HAD A ONE INCH CRACK ON THE LOWER FORWARD CORNER AND A DEEP GOUGE FIVE INCHES ABOVE IT. REPAIRED IAW ABX REA D952-11953-MR. 2L72 4F A6WE 19950825000131995082500013WP 1995 8 25 ABXA9500654 119950725A533059100853 SKIN DOUG DC9 DC941 302207NWP FS 190 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING SEVERE WEATHER AND VERY HIGH WINDS, THE CREW ENTRANCE STAIRS WERE BLOWN AGAINST THE FUSELAGE PUNCTURING A HOLE IN THE SKIN BELOW THE ENTRANCE DOOR. TEMPORARY REPAIR DONE IAW ABX REA D953-12257-MR. 2L72 4F A6WE 19950825000141995082500014WP 1995 8 25 ABXA9500655 119950725A533059100853 SKIN DOUG DC9 DC941 302207NWP FS 190 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23971AX 47497 DURING AIRCRAFT OUTBASED OPERATION IN OKC, THE FUSELAGE WAS DAMAGED BY THE CREW ENTRANCE STAIRS DURING SEVERE WEATHER. THE DAMAGE TO THE FUSELAGE WAS TEMPORARILY REPAIRED PER ABX REA D953-12257-MR. TEMPORARY REPAIR REPLACED 07-25-95 BY PERMANENT REPAIR IAW ABX REA\ND953-12265-MR. 2L72 4F A6WE 19950825000151995082500015WP 1995 8 25 ABXA9500658 119950716A533059114273 SKIN DOUG DC9 DC932 3022066WP BS 945 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C - CHECK INSPECTION, FOUND FUSELAGE SKIN DAMAGED AT STA 945, LONGERON 15L - 16L. REPAIRED IAW ABX REA D953-12128-MR. 2L72 4F A6WE 19950825000161995082500016WP 1995 8 25 ABXA9500659 119950715A53205910158 JAMB DOUG DC9 DC932 3022066WP BS 937 BLENDED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23903AX 47427 DURING C - CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND AFT CARGO DOOR JAMB HAD EXCESSIVE BLEND OUT AT FS 937 AT THE NR 1 DOOR STOP. REPAIRED IAW ABX REA D953-12131-MR. 2L72 4F A6WE 19950825000171995082500017WP 1995 8 25 ABXA9500660 119950712A5280S2210370P4101 BUSHING DOUG DC9 DC932 3022066WP BS 111 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 47426 DURING C - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THAT THE OUTBOARD GEAR DOOR ACTUATOR ROD END BUSHING WAS WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950825000181995082500018NE 1995 8 25 ABXA9500661 219950702A7240767197 CASE PWA JT8D15 DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23953AX 701003 47608 701003 DURING COMPLIANCE OF A. D. 87-11-7; A.S.B. 5676, REV. 6, FOUND THE NR 2 ENGINE COMBUSTION CHAMBER OUTER CASE CRACKED AT THE 11 O'CLOCK POSITION. REPLACED NR 2 ENGINE IAW ABX JOB CARD 7001. 2L72 4F4 F A6WE E2EA 19950825000191995082500019WP 1995 8 25 ABXA9500662 119950803A276039545571 LINK DOUG DC9 DC933F 302207AWP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING COMPLIANCE OF A.D. 85-01-03; S.B.'S 27-288, 27-229, EAAD 27-32091, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED LEFT OUTBOARD SPOILER DRIVE LINK ISW DC-9 SUPP. M.M. 27-61-1. 2L72 4F A6WE 19950825000201995082500020WP 1995 8 25 ABXA9500663 119950726A5753995760015 ANGLE DOUG DC9 DC941 302207NWP WS 360 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950825000211995082500021WP 1995 8 25 ABXA9500664 119950726A5753995760019 ANGLE DOUG DC9 DC941 302207NWP WS 360 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION, FOUND LEFT FLAP ATTACH ANGLE FOR OUTBOARD HINGE CRACKED INSIDE THE FLAP. REPLACED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950825000221995082500022WP 1995 8 25 ABXA9500665 119950722A52803923166501 FITTING DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR LINK ASSEMBLY HAD EXCESSIVE PLAY. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950825000231995082500023WP 1995 8 25 ABXA9500666 119950722A3231NAS1304 BOLT DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION AND COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT OUTBOARD MAIN LANDING GEAR DOOR ARM ASSEMBLY HAD EXCESSIVE PLAY. REPLACED BOLT IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19950825000241995082500024WP 1995 8 25 ABXA9500667 119950725A278099193984 FITTING DOUG DC9 DC941 302207NWP WS 137 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION, FOUND RIGHT WING SLAT ACTUATING MECHANISM INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19950825000251995082500025WP 1995 8 25 ABXA9500668 119950725A575459225001 LE SKIN DOUG DC9 DC941 302207NWP NR 1 SLAT DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION, FOUND DENT IN LEADING EDGE OF THE NR 1 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A. 2L72 4F A6WE 19950825000261995082500026WP 1995 8 25 ABXA9500669 119950726A575459225331 LE SKIN DOUG DC9 DC941 302207NWP NR 3 SLAT DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING C - CHECK INSPECTION, FOUND DENT IN THE LEADING EDGE OF THE NR 3 SLAT ON THE LEFT WING. REPAIRED IAW DC-9 SRM 57-03, FIG. 14A. 2L72 4F A6WE 19950825000271995082500027WP 1995 8 25 ABXA9500674 119950817A2150SZ2430041 PULLEY NIHON YS11 YS11A500 6310416WP AIR CONDITIONER WARPED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23911AX 2051 UNDEFINED SMOKE ODOR IN THE COCKPIT DURING LAST PORTION OF CLIMB TO 10,000 FEET. GRADUALLY WENT AWAY AFTER TEN MINUTES. UNABLE TO IDENTIFY OR ISOLATE SOURCE. FOUND AIR CONDITIONING DRIVE PULLEY WARPED AND CORRODED CAUSING DRIVE BELT TO BURN IN A SHORT PERIOD OF TIME. REPLACED JACK SHAFT AND PULLEY. 2L72 4T A1PC 19950825000281995082500028NM 1995 8 25 DL72L953408 119950727A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11504DA 21306 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH L/E SUPPORT RIBS NR 7 AND NR 10 CRACKED AT THE LOWER END AND LOWER ATTACH ANGLE CRACKED 38 INCHES FROM I/B END. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950825000291995082500029NM 1995 8 25 DL72S953419 119950718A53116572741 FRAME BOEING727 727232 1384082NM FS 1090 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 THE UPPER LEG OF THE C-3 DOOR CUTOUT FORWARD FRAME WAS FOUND CORRODED AT STA 1090, OUTBOARD OF STRINGER 27R. THE DAMAGE WAS REMOVED AND REPAIRED PER B727 SRM 51-40-3, FIGURE 1. 2L73 4F A3WE 19950825000301995082500030NM 1995 8 25 DL72W953406 119950816A2613355944255 ELEMENT BOEING727 727247 138408FNM LWR AFT BODY SHORTED A DALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11294WA 22112 ON TAKEOFF OUT OF ORF, HAD THE LOWER/AFT BODY OVERHEAT ILLUM. FOLLOWED PROCEDURES, LIGHT STAYED ILLUM. ISOLATED THE NR 1, NR 2, NR 3 ENG PNEUMATICS, LIGHT REMAINED ILLUM. OFF-LANDED IN CAE. FOUND RT OVERHEAT DET M365 SEC 48 SHORTED. REPLACED SAME, RAN ENGINES, OPERATION NORMAL. 2L73 4F A3WE 19950825000311995082500031NM 1995 8 25 DL72W953410 119950816A5533 VENTRAL WEB BOEING727 727247 138408FNM BS 1245/1225 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112816W 20872 FOUND DURING E-1 LETTER CHECK - LIGHTNING HOLE HAS CRACK LT VENTRAL WEB STA 1245 - LT VENTRAL WEB HAS CRACK AT TOP OF WEB AT STA 1225. REPAIRED PER MMM 53-11-0 PG 828 - 832. 2L73 4F A3WE 19950825000321995082500032NM 1995 8 25 DL72W953411 119950816A5520 SKIN BOEING727 727247 138408FNM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112816W 20872 FOUND DURING E-1 LETTER CHECK - 1 INCH HOLE ON BOTTOM SKIN OF RT ELEVATOR. REPAIRED PER MM 55-20-3. 2L73 4F A3WE 19950825000331995082500033NM 1995 8 25 DL72W953420 119950809A533065545502 SKIN BOEING727 727247 138408FNM FS 720 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 AT HMV, DURING ACCOMPLISHMENT OF PERMANENT REPAIRS TO FUSELAGE SKIN PER DL ERA 256356-14AD. TO FACILITATE MAINTENANCE, AN ADDITIONAL AREA OF SKIN WAS REPLACED AT FS 680 AND 720A +15, PER DL ERA 302240-14. 2L73 4F A3WE 19950825000341995082500034NM 1995 8 25 DL72W953422 119950731A5330651842014 SKIN BOEING727 727247 138408FNM FS 355 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 A DENT WAS FOUND IN THE UPPER FORWARD CORNER OF AN EXISTING REPAIR AT FS 335 AND STRINGER 24R (REF ER/A 215945-14). THE SECTION WAS TRIMMED OUT AND A DOUBLER WAS INSTALLED PER DL ERA 302205-14. 2L73 4F A3WE 19950825000351995082500035NM 1995 8 25 DL733953425 119950802A5320 SUPPORT RAIL BOEING737 737347 1384647NM FS 815 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11311WA 23597 AT HMV, INSPECTION FOUND HEAVY CORROSION ON CENTER FLOOR SUPPORT RAIL AT FS 815. REPAIRED PER SRM 53-00-53. 2L72 4F RTA16WE 19950825000361995082500036NM 1995 8 25 DL73S953409 119950814A5330 SKIN BOEING737 737232 1384475NM FS 935 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11319DL 23091 FUSELAGE SKIN AT FS 935 BETWEEN STR 21 AND 22, SUSTAINED PUNCTURE DAMAGE FROM GROUND EQUIPMENT. REPAIRED PER DL ERA 302319-14 AND SRM 53-10-3 FIG 1 FOR DAMAGE TO FS 935 FRAME. 2L72 4F RTA16WE 19950825000371995082500037NM 1995 8 25 DL73S953413 119950815A554265C258411 SKIN BOEING737 737232 1384475NM RUDDER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11319DL 23091 RUDDER HAS TEMPORARY REPAIR ON UPPER RT SIDE SKIN. REPAIRED DAMAGE AS PER SRM 55-40-5 WITH REF TO 51-40-15. 2L72 4F RTA16WE 19950825000381995082500038NM 1995 8 25 DL73S953418 119950817A53306573741 SKIN BOEING737 737232 1384475NM FS 360-380 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313DL 23085 GROUND SERVICE EQUIPMENT CAUSED 2 X 4 INCH TEAR IN FUSELAGE SKIN FROM FS 360 - 380, STRINGER 19R TO 20R. SKIN WAS TRIMMED OUT AND REPAIRED PER DL ERA 302313-14. 2L72 4F RTA16WE 19950825000391995082500039NM 1995 8 25 DL73S953421 119950810A57146545410223 FLOOR BEAM BOEING737 737232 1384475NM WING CTR SECT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11304DL 23076 THE BL0.07 FLOOR BEAM OF THE WING CENTER SECTION IS COMPLETELY CRACKED. THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 2.0 INCHES IN LENGTH IN THE SAME LOCATION. THE ORIGINAL 65-45410-104 ANGLE IS REINSTALLED TO REPAIR DAMAGE. REPAIRS ACCOMPLISHED PER DLA ERA 302296-14. 2L72 4F RTA16WE 19950825000401995082500040NM 1995 8 25 DL757953414 119950815A5730 PANEL BOEING757 757232 1384965NM WS 313.5 LE DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11627DL 22917 RT WING FIXED L/E AT WS 313.5 HAS DAMAGE AND FIXED L/E PANEL RT WING WS 459.5 HAS DAMAGE. REPAIRED AS PER ERA 302136-14 PER PERMANENT INSTRUCTIONS AND PER SRM 57-70-07. REPAIRS ACCOMPLISHED AT SPECIAL MTC VISIT. 2L72 4F RTA2NM 19950825000411995082500041NM 1995 8 25 DL757953423 119950816A2910000AE9616T0252 HOSE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE RUPTURED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11643DL 23997 716577 LOST LEFT HYDRAULIC SYSTEM ON APPROACH, QUANITY WENT TO ZERO. FOUND ENGINE DRIVEN PUMP PRESSURE LINE RUPTURED. REPLACED LINE AND PUMP. 2L72 4F4 FRTA2NM E17NE 19950825000421995082500042WP 1995 8 25 DLL13953415 119950815A5330 SKIN LKHEED1011 10113851 5265010WP FS 769 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11787DL 193A1126 A SMALL DENT WAS FOUND ON THE FUSELAGE SKIN ABOVE AN OLD EASTERN AIRLINES REPAIR LOCATED AT FS 769 NEAR STR 51. THE DENT HAS BEEN CUT OUT AND THE OLD REPAIR REMOVED. THE NEW CUTOUT MEASURES 4 X 2 INCHES. AN EXTERNAL REPAIR DOUBLER AND TRIPLER HAVE BEEN INSTALLED PER DL ERA 271571-14. 2L73 4F A23WE 19950825000431995082500043WP 1995 8 25 DLL13953416 119950815A57121647070 RIB LKHEED1011 10113851 5265010WP WS 503 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE LT AND RT WING RIB UPPER CAPS AT IWS 503 WERE FOUND WITH SEVERAL CRACKS IN THE TYPICAL LOCATIONS AT THE ATTACH TABS AT AIRCRAFT HMV. THESE CAPS WILL BE REPLACED PER DL ERA 271522-14. 2L73 4F A23WE 19950825000441995082500044NM 1995 8 25 DLM88953417 119950815A5330 SKIN DOUG MD88 MD88 3023688NM FS 522-541 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11996DL 53363 THE SUBJECT AIRCRAFT WAS DAMAGED BY GROUND EQUIPMENT RESULTING IN TWO PUNCTURES. THE TWO HOLES MEASURED 3.75 X 2 INCHES AND 1.5 X 1.5 INCHES. IN ADDITION, THE FORMER SKIN ATTACH ANGLE LOCATED AT FS 541 ABOVE STR 22R IS DAMAGED ON THE SKIN ATTACH FLANGE AND REQUIRES REPAIR. REPAIRS WERE ACCOMPLISHED PER DL ERA 271193-14. 2L72 4F RTA6WE 19950825000451995082500045NM 1995 8 25 P5CA9500706 119950818A5730 PANEL BOEING747 747122 1384872NM RIGHT WING ERODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 RIGHT WING UPPER SURFACE FOUND ERODED. FIBERGLASS REPAIR REQUIRED FROM WING ROOT TO WING TIP. REPAIRED PER BOEING SRM 51-40-09 FINISH RESTORED. 2L74 4F A20WE 19950825000461995082500046NM 1995 8 25 P5CA9500707 119950818A5730 SKIN BOEING747 747122 1384872NM LEFT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 LEFT WING UPPER SKIN RABBET AREA 3, BULGE ON LEADING EDGE SKIN AT WS 685 AFT OF LEADING EDGE FLAP. CORROSION REMOVED AND AFFECTED AREA RE-PROTECTED WITH 0.050 INCH MATERIAL, REMOVAL WITHIN LIMITS PER BOEING SRM 57-30-01 PAGE 2. 2L74 4F A20WE 19950825000471995082500047NM 1995 8 25 P5CA9500708 119950818A5412 STRAP BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACK ON NR 3 PYLON ENGINE AFT MOUNT SUPPORT BULKHEAD AT THE 6 O'CLOCK POSITION. FABRICATED NEW STRAP AND INSTALLED PER BOEING SRM 51-40-00. 2L74 4F A20WE 19950825000481995082500048NM 1995 8 25 P5CA9500709 119950818A5412 STRAP BOEING747 747122 1384872NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACK ON NR 4 PYLON ENGINE AFT MOUNT SUPPORT BULKHEAD AT THE 6 O'CLOCK POSITION. FABRICATED NEW STRAP AND INSTALLED PER BOEING SRM 51-40-00. 2L74 4F A20WE 19950825000491995082500049NM 1995 8 25 P5CA9500710 119950818A5400 STIFFENER BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACKED STIFFENER, NR 3 PYLON NACELLE, STATION 180 INBOARD SIDE, REPAIRED PER BOEING SRM 54-1003 FIG. 15. 2L74 4F A20WE 19950825000501995082500050NM 1995 8 25 P5CA9500711 119950818A5720AND101411401 STIFFENER BOEING747 747122 1384872NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 CRACKED RIB STIFFENER, RIGHT WING INBOARD AILERON, INBOARD SUPPORT. INSTALLED NEW STIFFENER PER BOEING SRM 51-40-00 AND DRAWING 65B08150-2- ITEM 9. 2L74 4F A20WE 19950825000511995082500051NM 1995 8 25 P5CA9500712 119950818A21216054572 FAN BOEING747 747122 1384872NM FWD CARGO FAILED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 NR 1 RECIRCULATION FAN INOPERATIVE. FAN BLADE FOUND CRACKED AND LODGED INTO FAN HOUSING BARREL. REPLACED, BENCH CHECK OK, AND REINSTALLED. 2L74 4F A20WE 19950825000521995082500052NM 1995 8 25 P5CA9500713 119950818A284060B40037807 HARNESS BOEING747 747122 1384872NM NR 3 MAIN TANK LOW RESISTANCE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 NR 3 MAIN FUEL QUANTITY INDICATOR ERRATIC AT CRUISE ALTITUDE, QTY ROLLS UP ABOUT DOUBLE THE AMOUNT OF FUEL AND THEN ROLLS BACK WITH PRESS TO TEST BUTTON. TROUBLESHOT SYSTEM, FOUND READINGS BELOW M/M REQUIREMENTS, REPLACED TANK HARNESS ASSY AND TESTED PER BOEING MAINTENANCE MANUAL 28-40-01. 2L74 4F A20WE 19950825000531995082500053NM 1995 8 25 QXEA9500255 119950817A3350400005130003 EEL SWITCH DHAV DHAV DHC8 DHC8102 2809003NM FA PANEL MALFUNCTIONED A QXEAK NONE O OTHER CRCRUISE 1 NM09840PH 74 PDX - EMERGENCY LIGHTS CAME ON AND WENT OUT TWO OR THREE TIMES IN-FLIGHT FOR ABOUT 10-20 SECONDS. EMERGENCY LIGHT SWITCH ON, FLIGHT ATTENDANTS PANEL WAS REPLACED, AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950825000541995082500054NM 1995 8 25 QXEA9500256 119950817A33508GH00247308 EEL BULB DORNER DORNERDO32 DO328100 2996000NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09335PH 3013 PDX - AFT CABIN EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825000551995082500055NM 1995 8 25 SCNA95171 119950815A335057761 EEL BATTERY PACK BOEING727 727282 2F0R NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE AFT BATTERY PACK AND LIGHTS, OPS CHECKED NORMAL. 2L73 4F RTA3WE 19950825000561995082500056NE 1995 8 25 SWIA95613 219950729A73133037941 FUEL NOZZLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE FAILED A SWIAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 NM07224SW 120294 LT ENGINE FAILURE AT ROTATION RETURNED FOR LANDING. FOUND O-RINGS FOR NR 10 FUEL NOZZLE SPLIT. INSTALLED NEW O-RINGS RAN ENGINE, FLAMED OUT, INSTALLED, SERVICED NR 10 NOZZLE AND NEW TUBE. RAN ENGINE AT 100 PECENT TORQUE FOR 5 MINUTES. OPS CKS GOOD, NO LEAKS FOUND. 2L72 4T4 TRTA31SO E20NE 19950825000571995082500057SW 1995 8 25 SWIA95614 119950801A32332751016003 ACTUATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT MAIN FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0727297 AC735 LT MAIN GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LT MAIN LANDING GEAR OUTBD ACTUATOR IAW MM 32-10-20. CYCLED GEAR NUMEROUS TIMES, ALL INDICATIONS GOOD. 1L72 4T4 T A8SW E4WE 19950825000581995082500058NE 1995 8 25 SWIA95615 219950802A73213035659 FUEL CONTROL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE FAILED A SWIAO OTHER O OTHER CRCRUISE 1 NM07224SW4591 4591 120294 RT TORQUE UNCOMMANDED INCREASE AND DECREASE WITH LITTLE OR NO POWER LEVER INPUT. INSTALLED SERVICEABLE HMU AND T1.8 SENSOR. 2L72 4T4 TRTA31SO E20NE 19950825000591995082500059SO 1995 8 25 SWIA95616 119950803A3231 RETRACT MECH EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG DOORS MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07196SW 120151 RT GEAR DOORS WOULD NOT CLOSE AFTER TAKEOFF. CYCLED SEVERAL TIMES, RETURNED TO JAC. INSPECTED PROX SWITCHES, CONDUIT AND GAPS, PERFORMED GEAR SWINGS. PROBLEM COULD NOT BE DUPLICATED. SYSTEM OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950825000601995082500060NM 1995 8 25 9471W8PA 119950711A3260106122615 SWITCH MENASCO 6573761110 BOEING737 7373B7 1384580NM RT MLG FAILED A W8PAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03947WP C90557 23376 LANDING GEAR CONFIGURATION WARNING HORN ON IN-FLIGHT DURING CLIMB-OUT. USED OVERRIDE TO RETRACT GEAR. AIRCRAFT RETURNED TO COS. TROUBLESHOT WARNING SYSTEM. AIRCRAFT FERRIED GEAR DOWN TO DIA. REPLACED AIR SAFETY SWITCH, PERFORMED GEAR SWING AND RETURNED AIRCRAFT TO SERVICE. (X) 2L72 4F RTA16WE 19950825000611995082500061NM 1995 8 25 95ZZZX4158 119950512A531365564418 STRINGER BOEING727 7272J7 138400ENM BS 950 CORRODED A S4FAK NONE O OTHER ININSP/MAINT 1 WP07128NA47276 20879 IN THE PROCESS OF COMPLYING WITH SB 53-159, BELLY SKIN REPLACEMENT STRINGER P/N 65-56441-8 WAS FOUND CORRODED ALONG TOP SIDE. STRINGER WAS REPAIRED. SUBMITTER STATED CAUSE OF CORROSION WAS EITHER MOISTURE BUILD-UP OR LACK OF FINISH ON THE PART. 2L73 4F A3WE 19950825000621995082500062NM 1995 8 25 95ZZZX4159 119950512A5313655612910 STRINGER BOEING727 7272J7 138400ENM NR 2 CARGO DOOR CORRODED A S4FAK NONE O OTHER ININSP/MAINT 1 WP07128NA47275 20879 IN THE PROCESS OF COMPLYING WITH SB 53-159 BELLY SKIN REPLACEMENT, SOME CORROSION WAS FOUND ON LEFT SIDE OF STRINGER PN 65-56129-10. THE STRINGER HAD TO BE REPLACED. THIS STRINGER RUNS ALONG THE LOWER END OF NR 2 CARGO DOOR. SUBMITTER STATED CAUSE OF THIS CORROSION IS WATER AND DEBRIS LAYING INSIDE THE CHANNEL. 2L73 4F A3WE 19950825000631995082500063NM 1995 8 25 95ZZZX4160 119950510A5310 STRUCTURE BOEING727 7272J7 138400ENM FS 320-361 CORRODED A S4FAK NONE O OTHER ININSP/MAINT 1 WP07128NA 20879 DURING A C-CHECK INSPECTION, FOUND SEVERAL STRINGERS AND DOUBLERS CORRODED IN LOWER BELLY AREA FROM STA 320 - STA 360. INTERNAL DOUBLER CORRODED ON SKIN PANEL STA 351 TO STA 360, STR 27L TO STR 27R. STRINGER SEGMENT CORRODED STA 351 TO STR 360, STR 26R. FRAME TO TEE CHORD SHEAR TIE CORRODED STA 328R BELOW STR 28. RIGHT SUBFRAME CORRODED WHERE FLANGE MEETS LOWER TEE CHORD STA 320, STR 28. DEFECTS COULD BE MOISTURE AS PARTS ARE IN CLOSED AREA. 2L73 4F A3WE 19950825000641995082500064NM 1995 8 25 95ZZZX4162 119950510A53126516317199 BLKHD WEB BOEING727 7272J7 138400ENM FS 351.2 CORRODED A S4FAK NONE O OTHER ININSP/MAINT 1 WP07128NA47276 20879 DURING A C-CHECK INSPECTION, CORROSION WAS FOUND AT STA 351.2 FORWARD BULKHEAD WEB SHEAR TIE AND ADJACENT AREA. AS THE CORROSION WAS FOUND IN NUMEROUS AREAS, THE BULKHEAD WEB WAS REPLACED. THE REPAIR WAS ACCOMPLISHED WITH THE HELP OF BOEING AIRCRAFT COMPANY. AS THIS IS A CLOSED AREA, THE CORROSION WOULD BE FOUND ONLY AT THE TIME THE LOWER SKIN PANEL WAS REMOVED. 2L73 4F A3WE 19950825000651995082500065 1995 8 25 95ZZZX4163 319950727A61124E30171 DEICE BOOT BFGOODRICH BEECH 1900 1900D 1154162CE LEFT PROPELLER MISSING A JJBAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA01853CA2391 UE56 LEFT PROPELLER, BLADE, SERIAL NUMBER UNKNOWN, MISSING DEICE BOOT. PROPELLER AND BLADES WERE OVERHAULED BY HARTZELL AT WHICH TIME NEW BOOTS WERE INSTALLED. UPON INSPECTION OF BLADE, SUBMITTER STATED THE PROBLEM LIES WITH THE PAINT BEING APPLIED TO THE BLADES PRIOR TO BOOT INSTALLATION. 2L72 4T RTA24CE 19950825000661995082500066 1995 8 25 95ZZZX4164 419950612A25621104 ELT ARTEX BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER NRNOT REPORTED 1 EA01860CA675 51804 UE134 ELT TRANSMITS CONSTANTLY, UNABLE TO SILENCE. REMOVED AND REPLACED ELT ASSEMBLY. UNIT REMOVED WET. 2L72 4T RTA24CE 19950825000671995082500067 1995 8 25 95ZZZX4165 419950512A25621104 ELT ARTEX BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER ININSP/MAINT 1 EA01847CA1007 52414 UE52 DURING DETAILED INSPECTION, DISCOVERED ELT INOPERATIVE. UNIT WAS CONTAMINATED WITH WATER AND MOUNTING TRAY WAS CRACKED. REMOVED AND REPLACED ELT ASSEMBLY. 2L72 4T RTA24CE 19950825000681995082500068 1995 8 25 95ZZZX4166 419950624A25621104 ELT ARTEX BEECH 1900 1900D 1154162CE AFT FUSELAGE WET A JJBAK NONE O OTHER NRNOT REPORTED 1 EA01847CA250 53357 UE52 ELT TRANSMITS CONTINUOUSLY. REMOVED AND REPLACED ELT ASSEMBLY. UNIT REMOVED WAS CONTAMINATED WITH WATER. 2L72 4T RTA24CE 19950825000691995082500069CE 1995 8 25 95ZZZX4167 119950603A573011412003573 SKIN BEECH 1900 1900D 1154162CE LT WING DELAMINATED A MASAK NONE O OTHER CRCRUISE 1 SW01135YV UE135 DURING AIRCRAFT REPOSITIONING FLIGHT FROM BRADFORD, PA TO JAMESTOWN, NY, PILOT FELT VIBRATION IN AIRFRAME. AIRCRAFT LANDED WITHOUT INCIDENT. DURING POST-FLIGHT INSPECTION, FOUND LT INBOARD WING PANEL (TOP) HAD STARTED TO DELAMINATE. REMOVED AND REPLACED PANEL AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950825000701995082500070CE 1995 8 25 95ZZZX4168 119950622A5720MS20426AD RIVETS BEECH 1900 1900D 1154162CE RT WING LOOSE A MASAK NONE K FLUID LOSS ININSP/MAINT 1 SW01155ZV95 UE155 RIVETS LOCATED IN RT WING OUTBOARD OF NACELLE TOP SPAR AREA LOOSE CAUSING FUEL LEAK. VERY COMMON OCCURRENCE WITH APPROXIMATELY A 6-10 RIVET LENGTH ALONG TOP WING SPAR. 2L72 4T RTA24CE 19950825000711995082500071NM 1995 8 25 95ZZZX4169 119950710A77143039242 PULSE PICK-UP DORNERDO32 DO328100 2996000NM LT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07426JS 3038 FLT 4151 - DURING FLIGHT, LT ENGINE NH GAUGE BECAME ERRATIC, CREW INSTRUCTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT/MX REPLACED LT ENGINE NH PULSE PICK-UP IAW MM 77-00-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825000721995082500072NM 1995 8 25 95ZZZX4170 119950711A7603 POWER LEVERS DORNERDO32 DO328100 2996000NM COCKPIT OUT OF ADJUST A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07426JS 3038 FLT 4254 - CREW REJECTED TAKEOFF. BOTH POWER LEVERS STUCK AT FLIGHT IDLE GATE, WOULD NOT ADVANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT/MX ADJUSTED FLIGHT IDLE LOCK-OUT MECHANISM IAW MM 76-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825000731995082500073NM 1995 8 25 95ZZZX4171 119950702A7603 POWER LEVER DORNERDO32 DO328100 2996000NM RIGHT LACK OF LUBE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL07426JS 3038 FLT 4253 - CREW ABORTED TAKEOFF BECAUSE RIGHT POWER LEVER SEIZED IN A POSITION OF APPROXIMATELY 20 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. PIT/MX INSPECTED AIRCRAFT, NOTICED RIGHT POWER LEVER PRIMARY LOW PITCH LOCK-OUT WAS BINDING - LUBRICATED LOCK-OUT MECHANISM IAW STANDARD MAINTENANCE PRACTICES. OPS GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825000741995082500074NM 1995 8 25 95ZZZX4172 119950710A6120C60023 CSU DORNERDO32 DO328100 2996000NM LT PROPELLER DEFECTIVE A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07430JS 11405007 3044 FLT 4269 - AFTER TAKEOFF, SETTING CLIMB POWER, COULD NOT MATCH TORQUE WITHOUT SPLIT BETWEEN CONDITION LEVER POSITIONS. LEFT C.L. AT FULL STOP. CREW ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DAY/MX INSPECTED AIRCRAFT AND DISCOVERED A FAULTY CONSTANT SPEED LIMIT. REPLACED LT C.S.U. IAW MM 61-21-03. OPS CHECKED GOOD IAW MM 61-00-06. TEST FLIGHT GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825000751995082500075WP 1995 8 25 95ZZZX4173 119950718A2530811150413M COFFEE MAKER DOUG DC9 DC932 3022066WP FWD GALLEY OVERHEATING A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11911VV 47285 ATL - FLT 166 - SMOKE IN COCKPIT ON APPROACH TO ATL. FOUND TO BE FORWARD GALLEY COFFEE MAKER OVERHEATING. REMOVED COFFEE MAKER AND PLACED ON MEL. 2L72 4F A6WE 19950825000761995082500076WP 1995 8 25 95ZZZX4174 119950725A24258DW84LBA1 VOLT/AMP METER DOUG DC9 DC932 3022066WP COCKPIT FAILED A VJ6AH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO11529MD 47262 ATL/IAD - FLT 454 - WHEN ON FINAL APPROACH, DECLARED AN EMERGENCY DUE TO THE VOLT/AMP METER HAVING AN ELECTRICAL FAULT AND SMOKING ON THE FLIGHT DECK. REPLACED VOLT/AMP METER. 2L72 4F A6WE 19950825000771995082500077WP 1995 8 25 95ZZZX4175 119950721A5743 ATTACH FITTING DOUG DC8 DC871F 302199DWP LT MLG CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15801GP 46039 DURING B-CHECK, THE LEFT MLG ATTACH FITTING WAS FOUND WITH A SUBSTANTIAL CRACK. AIRCRAFT REMOVED FROM SERVICE. SUPPLEMENTAL REPORT TO FOLLOW. 2L74 4F RT4A25 19950825000781995082500078CE 1995 8 25 95ZZZX4176 119950618A3260 INDICATOR BULBS BEECH 99 C99 1154006CE RT MLG/NLG FAILED A GUUAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO192225H U227 ATL/ANB - FLT 604 - PILOT REPORT: RIGHT MAIN NOSE GEAR LIGHT WOULD NOT ILLUMINATE, HAD TO MANUALLY EXTEND LANDING GEAR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED INDICATOR BULBS, SWING GEAR, AND RELEASED AIRCRAFT. 1L72 3T A14CE 19950825000791995082500079SO 1995 8 25 95ZZZX4177 119950608A2160CY1221073 TEMP CONTL COMP BARBERCOL LKHEED1329 1329 5263102SO FS 598 INOPERATIVE A DVYAK NONE O OTHER ININSP/MAINT 1 WP23888WT600 302023Y 5070 FOLLOW-UP OF SDR RELATING TO PRESSURIZATION PROBLEM, DIFFICULTY TRACED TO TEMP CONTROL BOX LOCATED IN AFT EQUIPMENT AREA. CONTROLLER REPLACED. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2L74 4J 2A15 19950825000821995082500082NM 1995 8 25 95ZZZX4180 119950706A7930 OIL BYPASS WIRE BOEING747 7472B4B 138481BNM NR 1 ENGINE DEFECTIVE A MEAFEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15203AE 21098 DURING CLIMB, ENGINE NR 1 OIL FILTER BYPASS LIGHT ILLUMINATED, REDUCING THRUST LEVER TO NEAR IDLE, LIGHT WENT DIM AND OUT THEN FLICKERED ON-OFF. ENGINE SHUT DOWN AND RETURNED TO BASE. ENGINE OIL CHANGED, PRESSURE FILTER REPLACED, ALL CHIP DETECTORS CHECKED SATISFACTORY, GROUND RUN PERFORMED. ALL PARAMETERS NORMAL EXCEPT FILTER BYPASS FLICKERS AT 90 PERCENT N2, CONFIRMED WIRING DEFECT. 2L74 4F RTA20WE 19950825000831995082500083NM 1995 8 25 AALA951177 119950629A3350A3060719103 EEL STRIP BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07663AM 25297 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950825000841995082500084NM 1995 8 25 AALA951186 119950703A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07697AN 26977 DFW - DURING OVERNIGHT CHECK, FOUND L1 DOOR FORWARD EMERGENCY EXIT IDENTIFIER MARKER INOPERATIVE. REPAIRED BROKEN WIRE ON EMERGENCY EXIT IDENTIFIER MARKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950825000851995082500085NM 1995 8 25 AALA951203 119950706A3350A3060719101 EEL STRIP BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07698AN 26980 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT CABIN FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GOUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950825000861995082500086NM 1995 8 25 AALA951210 119950707A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07670AA 25335 DFW - DURING OVERNIGHT CHECK, EMERGENCY PATH LIGHTS FROM L2 DOOR TO OVERWING EMERGENCY EXITS FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY PATH LIGHT WIRE AT L2 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950825000871995082500087NM 1995 8 25 AALA951212 119950708A3350 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07663AM 25297 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT ROW 3 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950825000881995082500088EU 1995 8 25 AALA951229 119950709A2910 B-NUT FOKKERF28 F28MK0100 4990807EU NR 1 HYD SYST LOOSE A AALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW071474D 11520 BNA - FLT 0580 - EN ROUTE DFW/BNA DURING CRUISE, HYDRAULIC SYTEM NR 1 LOW QUANTITY INDICATION ON MFDU. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT PROCEEDED TO BNA, LANDING WITHOUT INCIDENT. RESECURED LOOSE B-NUT AT LT THRUST REVERSER CONTROL VALVE STOW LINE. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK AND SYSTEM GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19950825000891995082500089EU 1995 8 25 COEA9572002 119950501A57301301303901 DOUBLER FOKKERF27 F27MK500 4990629EU WS 7200, 7900 CRACKED AS COEAK NONE O OTHER ININSP/MAINT 1 NM01720FE45887 10464 DURING SIP 57-30-05, THE FOLLOWING WAS FOUND. RIGHT WING FUEL TANK ACCESS COVER NR 153 DOUBLER ASSEMBLY, COMMON TO THE LOWER SKIN PANEL INSTALLATION, WAS FOUND CRACKED AT RT WING STA 7200 (3.0 MM) AND 7900 (1.4 MM). REPAIRS WERE ACCOMPLISHED IAW FOKKER F27 SB 57-46 REPAIR SCHEME IV, KIT W FOR STA 7200 AND X FOR STA 7900. TAC, 68,035. (X) 2H72 4T A817 19950825000901995082500090WP 1995 8 25 ORJA9566 119950725A335041B004AD073 EEL BATT PACK EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11879RA 53185 AFT OVER THE WING DOOR EXITS EMERGENCY LAMPS INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK OK. (X) 2L72 4F RTA6WE 19950825000911995082500091EU 1995 8 25 USAA950643 219950619A7200 ENGINE BOEING737 7374B7 1384702NM CFMINTCFM56 CFM563B2 13802EU LEFT FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA19432US16979 24554 DAB - FLT 1202 - LEFT ENGINE LOST POWER CLIMBING THROUGH 15,000 FEET. FLIGHT CREW ACCOMPLISHED ENGINE SHUT DOWN AND RETURNED TO DAB WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT ENGINE. (X) 2L72 4F4 FRTA16WE E21EU 19950825000921995082500092WP 1995 8 25 95268 119950818A2560375321321 CLIP DOUG DC9 DC932 3022066WP FWD GALLEY SLIDEBROKEN A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31501ME 47132 CREW REPORTS, GALLEY DOOR EVACUATION SLIDE LOOSE. MAINTENANCE INSTALLED NEW INNER SLIDE CUP RETAINER CLIP. REINSTALLED EVACUATION SLIDE, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950825000931995082500093WP 1995 8 25 9512579978 119950728A5412 WEB DOUG DC9 DC931 3022065WP FS 965 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING H-CHECK, FOUND OIL CANNING ON THE PYLON BULKHEAD WEB, RIGHT SIDE FS 965. REPAIRED BULKHEAD (P/N 9912243-81) PER EA 99-100832. 2L72 4F A6WE 19950825000941995082500094WP 1995 8 25 9512589604 119950815A5753 SKIN DOUG DC9 DC932 3022066WP RT TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT FLAP NR 2 TRAILING EDGE SEGMENT. REPAIRED PER SRM 51-70-2. 2L72 4F A6WE 19950825000951995082500095WP 1995 8 25 9512599860 119950816A5523 SKIN DOUG DC9 DC951 3022051WP ELEVATOR TAB DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01769NC 47757 DURING L-CHECK, FOUND DELAMINATION ON THE RIGHT ELEVATOR, RIGHT CONTROL TAB LOWER SKIN. REPLACED TAB PER MM 27-30-0, CODE 3, PG 515 TO 517, MG PART NUMBER 5910413-501N. 2L72 4F A6WE 19950825000961995082500096WP 1995 8 25 9512601227 119950808A5751 SKIN DOUG DC10 DC1030 3023501WP RT AILERON DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01227NW 46969 DURING PERIODIC CHECK, DAMAGE WAS FOUND ON THE RIGHT HAND OUTBOARD AILERON LOWER SKIN PANEL DUE TO CORROSION ALONG THE LEADING EDGE OF SKIN PANEL ARC 1113. REPLACED SKIN PANEL PER EA 12-98992, MFG PART NUMBER NRC 6041-506. 2L73 4F A22WE 19950825000971995082500097WP 1995 8 25 9512611161 119950803A5312 BULKHEAD DOUG DC10 DC1040 3023508WP FS 515 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01161US 46770 DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE BULKHEAD AT FS 515, STR 27R AND LONGERON 27L. REPLACED WEB PER EA 11-98526 AND INSTALLED DOUBLER PER EA 11-98525. 2L73 4F A22WE 19950825000981995082500098WP 1995 8 25 9512621161 119950802A5320 SUPPORT DOUG DC10 DC1040 3023508WP FS 495 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01161US 46770 DURING T-CHECK, A CRACK WAS FOUND ON THE FLOOR SUPPORT AT FS 495 RBL 24 TO 26. INSTALLED REPAIR STRAP PER EA 11-99021, MFG PART NUMBER 0048-33. 2L73 4F A22WE 19950825000991995082500099WP 1995 8 25 9512631161 119950728A5511 SPAR CAP DOUG DC10 DC1040 3023508WP HORIZ STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01161US 46770 DURING INSPECTION OF THE RIGHT HORIZONTAL SPAR CAP, A CRACK WAS FOUND AT THE FORWARD FLANGE AT STA XFS 82. INSTALLED REPAIR PER EM 5511-01014 AND EA 11-99036. 2L73 4F A22WE 19950825001001995082500100WP 1995 8 25 9512641161 119950810A5315 FLOORBEAM DOUG DC10 DC1040 3023508WP FS 1887 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01161US 46770 DURING T-CHECK, CRACKS WERE FOUND AT THE NUTPLATE HOLES ON THE FS 1887 FLOORBEAM UPPER CHORD FLANGE AT RBL 26. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER EA 11-99176, MFG PART NUMBER AGA 3793-19. 2L73 4F A22WE 19950825001011995082500101WP 1995 8 25 9512669903 119950815A7712 TQ IND DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01953N 47083 653954 THE NR 2 N1 INDICATOR FAILED ON TAKEOFF ROLL, THE TAKEOFF WAS ABORTED. THE N1 INDICATOR WAS PLACED ON MEL AND THE FLIGHT RESUMED ITS SCHEDULED ROUTE. SUBSEQUENT REPLACEMENT OF THE INDICATOR RESTORED NORMAL SYSTEM OPERATION. 2L72 4F4 F A6WE E2EA 19950825001021995082500102NE 1995 8 25 9512679755 219950813A7321 FUEL CONTROL DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01755NW 47179 676199 DURING CLIMB, THE NR 2 ENGINE N1, N2, AND EPR INDICATORS WERE FLUCTUATING. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL ASSEMBLY AND TESTED THE ENGINE. ENGINE PERFORMANCE WAS SATISFACTORY, THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950825001031995082500103NM 1995 8 25 9512682282 119950816A5210507945177 DOOR BOEING727 727251 138408HNM MAIN CABIN NOT CLOSED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01282US183033680 21161 DURING CLIMB DTW-ORD, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE AND THAT A LOUD AIR LEAK EXISTED AT THE MAIN CABIN DOOR. RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE DOOR WAS NOT FULLY CLOSED. OPERATIONAL AND PRESSURE CHECK OK. 2L73 4F A3WE 19950825001041995082500104NM 1995 8 25 9512692282 119950816A5210 DOOR BOEING727 727251 138408HNM MAIN CABIN NOT CLOSED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01282US 21161 DURING CLIMB DTW-ORD, FOUND THAT THE AIRCRAFT WOULD NOT PRESSURIZE AND THAT A LOUD AIR LEAK EXISTED AT THE MAIN CABIN DOOR. RETURNED TO DTW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE DOOR WAS NOT FULLY CLOSED. OPERATIONAL AND PRESSURE CHECK OK. 2L73 4F A3WE 19950825001051995082500105NM 1995 8 25 9512702708 119950817A3260 SWITCH BOEING727 727225 1384077NM TAIL SKID LACK OF LUBE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01817EA 22554 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, TAIL SKID INDICATION REMAINED ILLUMINATED. RECYCLED GEAR WITH PROPER INDICATIONS. MAINTENANCE CLEANED TAIL SKID SWITCH. 2L73 4F A3WE 19950825001061995082500106 1995 8 25 9512719955 419950817A3422 DIR GYRO DOUG DC9 DC931 3022065WP NR 2 MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01922RW 47182 FIRST OFFICER'S COMPASS FLAG APPEARED DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 2 DIRECTIONAL GYRO AND RMI. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825001071995082500107WP 1995 8 25 9512729872 119950819A3260 CONNECTORS DOUG DC9 DC951 3022051WP MLG DOOR SW CONTAMINATED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01781NC 48121 ON FINAL APPROACH, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. RECYCLED GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND CLEANED BOTH CANNON PLUGS. CYCLED GEAR DOOR SEVERAL TIMES. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825001081995082500108WP 1995 8 25 9512739872 119950820A3231 ROLLER DOUG DC9 DC951 3022051WP RT MLG DOOR LOOSE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01781NC 48121 ON APPROACH INTO DTW, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED, RECYCLED GEAR WITH NO HELP. ACCOMPLISHED EMERGENCY GEAR EXTENSION PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT MAIN GEAR DOOR ROLLER NOT SECURED PROPERLY, TIGHTENED ROLLER ASSEMBLY TO RIGHT MAIN GEAR DOOR. ALSO, REPLACED LEFT MAIN GEAR DOOR DUE TO DAMAGE INCURRED. OPERATIONAL CHECK OK ON GEAR SWING, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825001091995082500109NM 1995 8 25 9512742203 119950804A5752 TAB BOEING727 727251 138408HNM LT AILERON DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01203US 3676 22543 DURING PERIODIC CHECK, FOUND OUTBOARD LEFT AILERON TAB DELAMINATED. REPLACED AILERON TAB, MFG PART NUMBER 65-21726-41K. 2L73 4F A3WE 19950825001101995082500110WP 1995 8 25 9512759160 119950725A5220 STOP FITTING DOUG DC9 DC914 3022034WP LT EMER EXIT DR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 69639 45744 DURING H-CHECK, FOUND LEFT OVERWING EMERGENCY EXIT DOOR UNSERVICEABLE. SHOP FOUND CRACKED INNER PAN AT STOP NR 14, CRACK AT STOP FITTING NR 1, AND UPPER INBOARD CORNER BETWEEN BEAMS NR 2 AND NR 3 GOUGED. REPAIRED PER NWA EA 99-098720 AND SRM 52-05 AND 52-01, MFG PART NUMBER 5910159-31. 2L72 4F A6WE 19950825001111995082500111NM 1995 8 25 95FDEA01113 119950815A532065453132 STR CLIP BOEING727 72725 1384006NM BS 660 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 DAMAGED STR CLIP BS 660 STR 2R. REMOVED AND REPLACED STR CLIP 2R PER FEDEX SRM 51-30-2. 2L73 4F A3WE 19950825001121995082500112NM 1995 8 25 95FDEA01114 119950815A53157075T6 FLOOR BEAM BOEING727 72725 1384006NM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION 72C235-02 ON FLOOR BEAM BS 560 RBL 4-23 WL 208. REMOVED AND REPLACED UPPER T-CHORD PER FEDEX SRM 51-30-08. 2L73 4F A3WE 19950825001131995082500113NM 1995 8 25 95FDEA01115 119950815A53137075T3 STRINGER BOEING727 72725 1384006NM BS 660 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 WHILE REMOVING STR CLIP 2R, DAMAGED STR BS 660. REMOVED AND REPLACED DAMAGED STR 2R FROM BS 670-690 PER SRM 53-10-3. 2L73 4F A3WE 19950825001141995082500114NM 1995 8 25 95FDEA01116 119950815A575365246588 SPAR BOEING727 72725 1384006NM RT TE FOREFLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 R/W I/B FOREFLAP I/B END POTTING COMPOUND MISSING. REMOVEDUPPER SKIN SURFACE OF FLAP, FOUND L/E SPAR CORRODED. REMOVED CORRODED SPAR AND REPLACED WITH NEW SPAR. LAYED UP SKIN REPAIRS. ALL WORK DONE IAW FEDEX SRM 51-40-6, 51-30-2 AND FEDEX MM 51-20-151, 51-51-11. 2L73 4F A3WE 19950825001151995082500115NM 1995 8 25 95FDEA01117 119950815A5315BAC1505100617 FLOOR BEAM BOEING727 72725 1384006NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION 72C285-02 ON FLOOR BEAM BS 480 RBL 34 - LBL 22 WL208. REMOVED AND REPLACED FLOOR BEAM UPPER T-CHORD FROM BS480 RBL 35 - LBL 35 WL 208 PER SRM 53-10-8. 2L73 4F A3WE 19950825001161995082500116NM 1995 8 25 95FDEA01118 119950815A53117075T6050 FRAME BOEING727 72725 1384006NM BS 1070 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CRACK IN FRAME STA 1070 STR 27L. REMOVED DAMAGED AREA OF FRAME, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950825001171995082500117NM 1995 8 25 95FDEA01119 119950815A53207075T2 SHEAR TIE BOEING727 72725 1384006NM BS 1148 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CRACKED SHEAR TIE BS 1148 WL 151 LBL 9.5. REMOVED AND REPLACED SHEAR TIE BS 1148 WL 151 LBL 9.5 PER SRM 51-30-2. 2L73 4F A3WE 19950825001181995082500118NM 1995 8 25 95FDEA01120 119950815A5313BAC1498147 STRINGER BOEING727 727227 1384078NM BS 1174 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 CRACKED STR AND RIVETS PULLING THROUGH STR 29R BS 1174 WL 154. CUT OUT DAMAGED SECTION OF STR AND REPAIRED PER SRM 53-10-03 FIG 1. 2L73 4F A3WE 19950825001191995082500119NM 1995 8 25 95FDEA01121 119950815A53117075T6 FRAME BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CRACK IN FRAME BS 720 RBL 4 WL 153. REPAIRED FRAME AT BS 720 RBL 4 WL 153 AS PER FEDEX SRM 51-40-2. 2L73 4F A3WE 19950825001201995082500120NM 1995 8 25 95FDEA01122 119950815A53302024T3 SKIN BOEING727 727227 1384078NM BS 1119 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 DENT ON INNER SKIN SURFACE AT BS 1119 LBL 4 (BETWEEN STR 29L-30L). FOUND DENT TO BE OUT OF LIMITS, REMOVED DAMAGE, FABRICATED REPAIR PLATE OUT OF 2024-T3, .071 X 8 INCH X 12 INCH, M459214 AND INSTALLED AS PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825001211995082500121NM 1995 8 25 95FDEA01123 119950815A53117075T6 FRAME BOEING727 727227 1384078NM BS 680 DOUBLE DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25489FE 21492 DOUBLE HOLE IN FRAME AT STR CLIP ON STR 5R AT BS 680. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-4. 2L73 4F A3WE 19950825001221995082500122NM 1995 8 25 95FDEA01124 119950815A5311 FRAME BOEING727 727227 1384078NM BS 520 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 IN THE FWD CARGO BAG THE UPPER FLANGE AT FRAME IS CRACKED AT BS 520 RBL 42 WL 165. FABRICATED REPAIR DOUBLER AND REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 19950825001231995082500123NM 1995 8 25 95FDEA01126 119950815A5311TPN7075T6 FRAME BOEING727 727233 138408ANM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME STA 660 BETWEEN STR 23-25R. REMOVED AND REPLACED DAMAGE TO FRAME STA 660 STR 23-25R PER FEDEX 51-40-3, REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F RTA3WE 19950825001241995082500124NM 1995 8 25 95FDEA01128 119950815A53117075T6 FRAME BOEING727 727233 138408ANM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME, STA 680 RT BETWEEN STR 20-25R. REMOVED DAMAGE FROM FRAME STA 680R STR 20-25R. REPAIRED PER FEDEXSRM 51-40-3. 2L73 4F RTA3WE 19950825001251995082500125NM 1995 8 25 95FDEA01129 119950815A53117075T6 FRAME BOEING727 727233 138408ANM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME STA 500 RT BETWEEN STR 22-23R. REPAIRED DENTED FRAME BS 500 RT BETWEEN STR 22-23R IAW FEDEX SRM 51-40-3. 2L73 4F RTA3WE 19950825001261995082500126NM 1995 8 25 95FDEA01130 119950815A53117075T6 FRAME BOEING727 727233 138408ANM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME STA 520 LT BETWEEN STR 23-24L. REPAIRED DENT ON FRAME STA 520 LT BETWEEN STR 23-24L IAW FEDEX SRM 51-40-3. 2L73 4F RTA3WE 19950825001271995082500127NM 1995 8 25 95FDEA01131 119950815A5313 STRINGER BOEING727 727233 138408ANM BS 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME, STA 600 LT BETWEEN STR 23-25L. REPAIRED DENT ON FRAME BS 600 BETWEEN STR 23-25L PER FEDEX SRM 51-40-3. 2L73 4F RTA3WE 19950825001281995082500128NM 1995 8 25 95FDEA01132 119950815A5330 SKIN BOEING727 727227 1384078NM BS 1046 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 AREA OF CORROSION ON INNER SKIN AT BS 1046 JUST ABOVE STR 28R. FABRICATED REPAIR DOUBLER AND INSTALLED, WORK DONE PER SRM 53-30-3. 2L73 4F A3WE 19950825001291995082500129NM 1995 8 25 95FDEA01133 119950815A5330 SKIN BOEING727 727227 1384078NM BS 1214-1221 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 DENT AT BS 1214-1221 BETWEEN STR 24-25R. DENT IS 7 INCHES X 5.5 INCHES X .250 INCH DEEP. RECONTOURED DENT TO WITHIN LIMITS. WORK PER SRM 51-40-2. 2L73 4F A3WE 19950825001301995082500130NM 1995 8 25 95FDEA01134 119950816A53117075T6 FRAME BOEING727 727233 138408ANM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENTS ON FRAME STA 680 LT BETWEEN STR 22-25. CUT OUTDAMAGE AND REPAIRED PER SRM 51-40-03. 2L73 4F RTA3WE 19950825001311995082500131 1995 8 25 95FDEA01135 419950817A34217725431001 ADI BOEING727 72722C 138400FNM LT FLIGHT DECK FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25102FE 19193 CAPTAIN'S ADI FAILED DURING CLIMB OUT IN NORMAL POSITION, AND ALSO FAILED IN AUXILIARY POSITION. REPLACED CAPTAIN'S ADI. OPS CK NORMAL ON GROUND. 2L73 4F A3WE 19950825001321995082500132NM 1995 8 25 95FDEA01136 119950818A5754 BONDING JUMPER BOEING727 72725 1384006NM LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION ON BULLNOSE BONDING JUMPER ON K-FLAP I/B UPPER ATTACH POINT. REMOVED CORROSION AND RELOCATED BONDING JUMPER ON K-FLAP PER FEDEX DRAWING SR37-57-010 RMB. 2L73 4F A3WE 19950825001331995082500133NM 1995 8 25 95FDEA01137 119950817A53117075T6 FRAME BOEING727 727233 138408ANM BS 700 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENTS ON FRAME BS 700 BETWEEN STR 23 TO 25L. REMOVED DAMAGE AND REPAIRED PER SRM 51-40-03. 2L73 4F RTA3WE 19950825001341995082500134NM 1995 8 25 95FDEA01138 119950817A5754 BONDING JUMPER BOEING727 727227 1384078NM NR 5 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON NR 5 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER ATTACH POINT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AREA AND REPAIRED PER SRM 57-50-03. 2L73 4F A3WE 19950825001351995082500135NM 1995 8 25 95FDEA01139 119950818A53207075T6 SHEAR TIE BOEING727 727227 1384078NM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON SHEAR TIE BS 700 STR 26 AND 27 RIGHT. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGE AREA AND REPAIRED PER SRM 53-10-04. 2L73 4F A3WE 19950825001361995082500136NM 1995 8 25 95FDEA01140 119950818A53207075T6 CHORD BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 BS 760 LBL 70.5 WL 208, 1 EA FWD, LOWER HOLE IN CHORD IS CRACKED. REPAIRED PER FEDEX EA 7-5710-25565. 2L73 4F A3WE 19950825001371995082500137NM 1995 8 25 95FDEA01141 119950818A55107075T6 BEAM BOEING727 727227 1384078NM LT HORIZ STAB ELONGATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 BOLT HOLE ON LT HORIZONTAL STAB TRAILING EDGE BEAM AT NR 2 RUB BLOCK IS ELONGATED. REMOVED HORIZONTAL STAB TRAILING EDGE BEAM, FABRICATED AND INSTALLED PARTS PER FEDEX EA 7-5510-25555. 2L73 4F A3WE 19950825001381995082500138NM 1995 8 25 95FDEA01142 119950818A52302024T3 SKIN BOEING727 727233 138408ANM NR 3 CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 NR 3 CARGO DOOR OUTER SKIN IS DENTED 5.5, AFT OF FWD EDGE 21.5 UP FROM LOWER EDGE. REPAIRED NR 3 CARGO DOOR OUTER SKIN DENT, BY INSTALLING EXTERNAL REPAIR IAW FEDEX SRM 52-00-03. 2L73 4F RTA3WE 19950825001391995082500139NM 1995 8 25 95FDEA01143 119950818A55222024T3 SKIN BOEING727 727233 138408ANM RT ELEVATOR LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 LIGHTNING STRIKE ON RT ELEVATOR ON TRAILING EDGE AT THE OUTBOARD STATIC WICK BASE. REPAIRED LIGHTNING STRIKE ON RT ELEVATOR ON TRAILING EDGE AT THE OUTBOARD STATIC WICK BASE, IAW FEDEX SRM 52-00-03 AND 51-80-7. 2L73 4F RTA3WE 19950825001401995082500140NM 1995 8 25 95FDEA01144 119950818A53302024T3 SKIN BOEING727 727233 138408ANM BS 324 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 SKIN DENTED INWARD AT BS 324, BETWEEN STR 3L AND 4L. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 53-30-03. 2L73 4F RTA3WE 19950825001411995082500141NM 1995 8 25 95FDEA01145 119950818A3412 TAT GAUGE BOEING727 727223 1384074NM FLIGHT DECK MALFUNCTIONED A FDEAK NONE O OTHER TOTAKEOFF 1 SO25265FE 21671 TAT GAUGE INDICATED NORMAL UNTIL LIFT OFF AT WHICH TIME TEMP ROLLED BACK TO APPROX 75 CELSIUS. OFF FLAG OUT OF VIEW, TURNING PITOT HEAT DID NOT AFFECT INDICATIONS. 2L73 4F A3WE 19950825001421995082500142NM 1995 8 25 95FDEA11127 119950815A53117075T6 FRAME BOEING727 727233 138408ANM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FOUND DENT ON FRAME, STA 660 LT BETWEEN STR 23-25L. TRIMMED OUT AND REMOVED DENT ON FRAME STA 660L STR 23-25L. REPAIRED FRAME PER FEDEX SRM 51-40-3. 2L73 4F RTA3WE 19950825001431995082500143EA 1995 8 25 BIER950020 219950818A8530 STUDS PIPER PA28 PA28RT201 7102818SO LYC O360 IO360C1C6 41514EA NR 4 CYL SHEARED B BIEAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA218368H 1306 28R8118062 L1847036A DURING TAKEOFF, PILOT NOTICED VIBRATION/PWR LOSS, AN UNEVENTFUL LANDING WAS MADE. DURING PRELIM INSP, FOUND 5 OF THE 8 CYL HOLD DN STUDS FOR THE NR 4 CYL HAD SHEARED, LEAVING CYL LOOSELY MOUNTED ON ENG. FURTHER INSP REVEALED CRACK IN CASE AROUND AREA OF REAR UPPER THROUGH STUD. ENG WAS MATTITUCK OVERHAUL. 1L71 3O3 O 2A13 1E10 19950825001441995082500144EU 1995 8 25 COM31138 119950820A243523080031 STARTER GEN SAAB SF340 SF340A 7850100EU LT ENGINE INOPERATIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01146CA19314700 340A146 ON TAXI OUT, THE LT ENGINE FAILED TO SHOW ANY RPM DURING START ATTEMPT. REMOVED AND REPLACED STARTER/GENERATOR. 2L72 4T RTA52EU 19950825001451995082500145NE 1995 8 25 COM31139 219950819A7200CT75A2 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT OVERTEMP A COMACD ABORTED TAKEOFF RETURN TO BLOCK M OVER TEMP TOTAKEOFF 1 SO01356CA200282804 340A034 367169 NR 1 ENGINE ITT EXCEEDED 930 DEGREES DURING TAKEOFF. THE OUTSIDE AIR TEMPERATURE 89 DEGREES, TQ 105 PERCENT, ITT 940 DEGREES FOR 3 SECONDS. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY. 2L72 4T4 TRTA52EU E8NE6 19950825001461995082500146EA 1995 8 25 COM60538 119950820A80128989308 START VALVE CNDAIRCL600 CL6002B19 EA RT ENGINE INOPERATIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01912CA5776 7011 THE RIGHT ENGINE WILL NOT ROTATE DURING START ATTEMPT. REMOVED AND REPLACED THE START VALVE. 2L72 4F RTA21EA 19950825001471995082500147EA 1995 8 25 COM60539 119950820A3350100865 EEL POWER SUPPLY CNDAIRCL600 CL6002B19 EA CABIN INOPERATIVE A COMAK NONE O OTHER ININSP/MAINT 1 SO01931CA3760 7037 THE EMERGENCY LIGHT BY THE CABIN DOOR IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT. 2L72 4F RTA21EA 19950825001481995082500148EA 1995 8 25 COM60540 119950817A2913PV304448 HYD PUMP CNDAIRCL600 CL6002B19 EA LT ENGINE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01933CA3243 7040 THE LT ENGINE DRIVEN HYDRAULIC PUMP IS LEAKING FLUID. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP. 2L72 4F RTA21EA 19950825001491995082500149NM 1995 8 25 DL72L953426 119950817A5754 ANGLE BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 A 2 INCH CRACK IN NR 5 SLAT COVE SKIN ATTACH ANGLE O/B END. FOUND DURING C-2 LTR CK. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19950825001501995082500150NM 1995 8 25 DL72S953427 119950818A3350 EEL LAMP BOEING727 727232 1384082NM R2 DOOR INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11468DA 20745 FOUND ON L/O EMERGENCY LIGHT PATH, LIGHT OUT AND LENS MISSING R2 DOOR. REPLACED LAMP HOLDER, BULB AND LENS. OPS CK GOOD. 2L73 4F A3WE 19950825001511995082500151NM 1995 8 25 DL72S953430 119950624A5753652163261 SPAR BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 THE NR 2 MIDFLAP AFT LOWER SPAR RAIL CRACKED 56 FROM I/B END OF FLAP. REPAIRED PER M/M 575200 P807, SPLICED IN NEW SECTION OF SPAR RAIL. FOUND AT SHOP VISIT. 2L73 4F A3WE 19950825001521995082500152NM 1995 8 25 DL72S953432 119950818A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11420DA 21273 FOUND DURING B-2 LETTER CHECK, NR 3 SLAT COVE SKIN ANGLE CRACKED UNDER THERMAL ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950825001531995082500153NM 1995 8 25 DL72S953433 119950818A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 FOUND DURING B-1 LETTER CHECK, NR 2 SLAT COVE SKIN ANGLE CRACKED UNDER THERMAL ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950825001541995082500154NM 1995 8 25 DL72S953434 119950818A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 FOUND DURING B-1 LETTER CHECK, NR 2 SLAT COVE SKIN ANGLE CRACKED AT INBOARD END. REPAIRED PER MM 57-54-0 PG 807A. 2L73 4F A3WE 19950825001551995082500155NM 1995 8 25 DL72S953435 119950818A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 FOUND DURING B-1 LETTER CHECK, NR 2 SLAT ACTUATOR O/B UPPER MOUNT BROKEN. REPAIRED PER MM 57-42-0 PG 812 TO 813. 2L73 4F A3WE 19950825001561995082500156NM 1995 8 25 DL72S953436 119950818A5330 SKIN BOEING727 727232 1384082NM BELOW L3 WINDOW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11534DA 22047 FOUND DURING B-1 LETTER CHECK, .5 CRACK AT LWR AFT CORNER OF L3 WINDOW OPENING. REPAIRED PER SRM 53-30-3 FIG 8. 2L73 4F A3WE 19950825001571995082500157NM 1995 8 25 DL72W953441 119950818A2782269002914 ACTUATOR BOEING727 7272Q8 138407WNM NR 4 SLAT RUPTURED A DALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11831L 21826 AT 5,000 FLT ON DEPT, SYS-A HYD LOW PRESS LIGHT ILLUM WITH FWD PANEL SYS A-LIGHT. SYS-A HYD QTY AND PRESS INDICATES ZERO. EMERGENCY CHECK LIST COMPLETED AND FUEL DUMPED, RETURNED TO DFW. FOUND NR 4 SLAT ACT RUPTURED. REPLACED ACT AND SERVICED HYD TO FULL. NR 4 SLAT ACT LEAKS AND OPN CKS GOOD. NO OTHER LEAKS DETECTED. 2L73 4F A3WE 19950825001581995082500158NE 1995 8 25 DL76L953447 219950819A7230PW4060 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11176DN15115 25061 724158 NUMBER 1 ENGINE HAD 2 COMPRESSOR STALLS AT TOP OF CLIMB. LOST LEFT HYDRAULIC SYSTEM FLUID AND OIL QUANTITY WENT TO ZERO. ENGINE WAS SHUTDOWN, AIRCRAFT RETURNED FRA. FOUND TURBINE CASE COOLING TUBING BROKEN, HYDRAULIC PRESSURE LINE LEAKING AT HYDRAULIC PUMP, OIL PRESSURE LINE BROKEN, AND METAL IN TAILPIPE. ENGINE WAS REPLACED, ROUTED TO SHOP FOR REPAIRS. 2L72 4F4 FRTA1NM E24NE 19950825001591995082500159WP 1995 8 25 DLL13953437 119950818A2410 IDG 729640 LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11783DL 388R 193A1009 010563 AFTER DEPARTURE, NR 1 GEN DIFF FAULT LIGHT CAME ON WITH APU ON MCO, RETURNED FLT TO LAX. FOUND METAL IN SCAVENGE FILTER OF NR 1 IDG. REPLACED IDG, OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19950825001601995082500160WP 1995 8 25 DLL15953446 119950817A33505165741 EEL POWER SUPPLY LKHEED1011 10113853 5265020WP FLT DECK FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11753DA 193W1189 DURING LAYOVER, COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19950825001611995082500161WP 1995 8 25 MWEA95267 119950818A256039522735501 BAR LATCH DOUG DC9 DC914 3022034WP FWD GALLEY DOOR DIRTY A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31600ME 45725 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LATCH SPRING IS BROKEN. MAINTENANCE FOUND SPRING OK, BUT LATCH WAS DIRTY. CLEANED AND LUBRICATED LATCH. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950825001621995082500162WP 1995 8 25 MWEA95269 119950819A3350S103 EEL BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31602ME 48133 MAINTENANCE FOUND DURING TRANSIT CHECK, THE FWD EMERGENCY EXIT CEILING LIGHTS INOP. REMOVED AND REPLACED NICAD BATTERIES IN FWD CABIN POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950825001631995082500163NM 1995 8 25 QXEA9500254 119950817A7712311627002 TQ HARNESS DORNERDO32 DO328100 2996000NM NR 2 ENGINE FAILED A QXEALE ABORTED APPROACH ENGINE SHUTDOWN O OTHER APAPPROACH 1 NM09336PH 3014 PDX - NR 2 ENGINE SURGED FROM FLIGHT IDLE WHILE ON SHORT FINAL, GO AROUND EXECUTED. ENGINE SURGED AGAIN 30 PERCENT TORQUE TO 70 PERCENT ON DOWN LEG. NR 2 ENGINE SHUTDOWN PER EMERGENCY CHECKLIST. AIRCRAFT LANDED SINGLE ENGINE WITHOUT INCIDENT. ENGINE HARNESS REPLACED AND NP PROBE REPLACED. ENGINE OPS CHECKED GOOD ON GROUND RUN, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950825001641995082500164SW 1995 8 25 QXEA9500257 119950818A2430AM363C524 CURRENT LIMITER SWRNGN SWRNGNSA227 SA227AC 8780603SW COCKPIT LOOSE A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09380PH AC582 PDX - AIRCRAFT RETURNED TO FIELD DUE TO ELECTRICAL SMELL IN COCKPIT. FOUND 225 AMP CURRENT LIMITER NUT WAS LOOSE AND LIMITER SHOWED SIGNS OF HEAT. CURRENT LIMITER WAS REPLACED AND MOUNTING POINT WAS CHECKED FOR DAMAGE, NONE NOTED. LIMITER OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950825001651995082500165EU 1995 8 25 QXEA9500258 119950819A33506008905 EEL POWER SUPPLYFOKKER FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 BOI - OVERWING EXIT EMERGENCY LIGHT INOP. BATTERY POWER SUPPLY AND LIGHT OPS CHECKED GOOD. 2L72 4F RTA20EU 19950825001661995082500166NM 1995 8 25 QXEA9500259 119950819A335082410162007 EEL CONTROL BOX DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONED A QXEAK NONE L NO TEST CRCRUISE 1 NM09840PH 74 PDX - EMERGENCY LIGHTS COME ON IN FLIGHT WHEN SWITCH IS CYCLED TO OFF AND BACK TO ARM. EMERGENCY LIGHT CONTROL BOX WAS REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950825001671995082500167EU 1995 8 25 QXEA9500260 119950820A3231H61C0722623 VALVE FOKKER FOKKERF28 F28MK1000 4990808EU NLG DOOR MALFUNCTIONING A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09468US 11095 PDX - NOSE GEAR RED LIGHT REMAINED ON LONGER THAN NORMAL FOLLOWING GEAR RETRACTION. NOSE GEAR EXTENSION IS NORMAL. ONE WAY RESTRICTOR REPLACED IN NOSE GEAR DOOR LINE. 2L72 4F RTA20EU 19950825001681995082500168NM 1995 8 25 SWAA950571 119950813A2931 PRESS IND BOEING737 7372H4 138448CNM B-HYD SYS INOP A SWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW0792SW 22964 EN ROUTE TO MDW, EXPERIENCED B-SYSTEM PRESSURE DROP. AIRCRAFT DIVERTED TO IND AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND PRESSURE INDICATOR INOP, DEFERRED INDICATOR AND CONTINUED PER MEL 29-3. 2L72 4F A16WE 19950825001691995082500169NM 1995 8 25 SWAA950572 119950814A2612 FIRE CONTL PNL BOEING737 7372H4 138448CNM COCKPIT MALFUNCTIONED A SWAADF RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SW0751SW 21448 AFTER TAKEOFF, EXPERIENCED APU FIRE WARNING. CREW ACTIVATED APU FIRE BOTTLE, FIRE WARNING LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO LBB AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE CONTROL PANEL AND FIRE DETECTION UNIT PER BOEING M/M. 2L72 4F A16WE 19950825001701995082500170NM 1995 8 25 SWAA950573 119950814A3246594 BEARING BOEING737 7373H4 1384600NM NR 1 MLG WHEEL FAILED A SWAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW07605SW 27956 WHILE TAXIING, CREW NOTED A BRAKE DRAGGING SENSATION, AIRCRAFT RETURNED TO GATE. INSPECTED AND FOUND DAMAGE TO LEFT MAIN GEAR AXLE AND NUMBER 1 WHEEL AND BRAKE ASSEMBLY. REPLACED LEFT MAIN GEAR INNER CYLINDER, NUMBER 1 AND 2 WHEEL/BRAKE ASSEMBLIES AND ANTI-SKID TRANSDUCERS PER BOEING M/M. 2L72 4F RTA16WE 19950825001711995082500171NE 1995 8 25 SWAA950574 219950817A7200 ENGINE BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 1 FAILED A SWAAE ENGINE SHUTDOWN Y ENGINE STOPPAGE DEDESCENT 1 SW07387SW 26602 720244 DURING DESCENT INTO ELP, EXPERIENCED NUMBER 1 ENGINE FAILURE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT ELP. INSPECTED AND FOUND NUMBER 1 ENGINE TOWER SHAFT FAILURE. REMOVED AND REPLACED ENGINE ASSEMBLY PER BOEING M/M. 2L72 4F4 FRTA16WE E2GL 19950825001721995082500172NM 1995 8 25 SWAA950575 119950818A3246594 BEARING BOEING737 7373H4 1384600NM NR 3 MLG WHEEL FAILED A SWAAO OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 SW07309SW 22948 ON TAKEOFF FROM LBB, NUMBER 3 MAIN GEAR WHEEL ASSEMBLY SEPARATED FROM BRAKE ASSEMBLY. AIRCRAFT MADE AN UNEVENTFUL LANDING AT ABQ. INSPECTED AND FOUND THE REASON FOR SEPARATION WAS DUE TO FAILED WHEEL BEARING. REPLACED NUMBER 3 AND 4 MAIN GEAR WHEEL ASSEMBLIES, NUMBER 3 BRAKE ASSEMBLY AND ANTI-SKID TRANSDUCER PER BOEING M/M. 2L72 4F RTA16WE 19950825001731995082500173NM 1995 8 25 SWAA950576 119950818A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500 PLUS 6, STRINGER 23R AT BS 860 STRINGER 26L BETWEEN BS 909 AND 916 STRINGER 24R AND AT BS 330 STRINGER 25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001741995082500174NM 1995 8 25 SWAA950577 119950818A5320 CLIP BOEING737 7373H4 1384600NM BS 500 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 500D, S19R. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001751995082500175NM 1995 8 25 SWAA950578 119950818A5320 DOOR FRAME BOEING737 7373H4 1384600NM BS 492 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR AFT FRAME CRACKED AT BS 492 RBL 39 WL 162. REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001761995082500176NM 1995 8 25 SWAA950579 119950818A5330 SKIN BOEING737 7373H4 1384600NM BS 867-887 DAMAGE A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CHAFING DAMAGE FROM BS 867 TO 887 BETWEEN S2 LT AND RT. REPAIRED PER TRAMCO EWO 95-0497 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001771995082500177NM 1995 8 25 SWAA950580 119950818A5330 SKIN BOEING737 7373H4 1384600NM BS 316 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 316 BELOW S17L AND AT BS 332 BETWEEN S19 AND 20L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001781995082500178NM 1995 8 25 SWAA950581 119950818A5315 FLOORBEAM BOEING737 7373H4 1384600NM BS 294/1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 1016 LBL 5 WL 208 AND AT BS 294 AT LBL12 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001791995082500179NM 1995 8 25 SWAA950582 119950818A5754 TE SKIN BOEING737 7373H4 1384600NM NR 3 SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND NUMBER 3 SLAT LOWER T/E SKIN CRACKED AT I/B END. REPAIRED PER BOEING DRAWING 65C30133 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001801995082500180NM 1995 8 25 SWAA950583 119950818A5330 SKIN BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07313SW 23335 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 178 WL 189 BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND TRAMCO EWO 95-0494. 2L72 4F RTA16WE 19950825001811995082500181NM 1995 8 25 SWAA950584 119950818A5320 PANEL BOEING737 7373H4 1384600NM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07310SW 22949 DURING SCHEDULED A2 CHECK, FOUND NOSE WHEEL WELL CEILING PANEL OPENING CRACKED 2.125 AT AFT INBOARD RADIUS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001821995082500182NM 1995 8 25 SWAA950585 119950818A5320 DOOR FRAME BOEING737 7375H4 138449DNM CARGO DOOR DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO DOOR FWD AND AFT LOWER FRAME WEBS DAMAGED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001831995082500183NM 1995 8 25 SWAA950586 119950818A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 312 LBL 14. REPAIRED PER SWA RA 1-553-1327 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001841995082500184NM 1995 8 25 SWAA950587 119950818A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947 LBL 10 AND 5 AT BS 986.5 LBL 15 AND RBL 6. REPAIRED PER SWA RA 1-553-1329 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001851995082500185NM 1995 8 25 SWAA950588 119950818A5320 T-CHORD BOEING737 7375H4 138449DNM BS 539 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND A/C RAM AIR INLET WEB T-CHORD CRACKED JUST BELOW UPPER DRAG ANGLE AT BS 539. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001861995082500186NM 1995 8 25 SWAA950589 119950818A5320 CASTING BOEING737 7373H4 1384600NM FWD ENTRY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07320SW 23341 DURING SCHEDULED C1 CHECK, FOUND CRACK IN UPPER FWD CORNER OF FWD ENTRY DOOR LOWER CAM PLATE SUPPORT CASTING. REPAIRED PER SWA RA 1-353-1331 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001871995082500187NM 1995 8 25 SWAA950590 119950818A5320 STRAP BOEING737 7375H4 138449DNM E/E COMPT BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW07513SW 24190 DURING SCHEDULED B/C CHECK, FOUND RIGHT O/B FLOORBEAM STRAP AT FWD END OF E AND E COMPT BROKEN. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001881995082500188NM 1995 8 25 SWAA950591 119950818A5315 FLOORBEAM BOEING737 7375H4 138449DNM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5 RBL 42 AND 45. REPAIRED PER SWA RA 1-553-1325 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001891995082500189NM 1995 8 25 SWAA950592 119950818A5320 ANGLE BOEING737 7375H4 138449DNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07501SW 24178 DURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD SUPPORT ANGLE CRACKED AT BS 727 RBL 3. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950825001901995082500190NM 1995 8 25 SWAA950593 119950815A5330 SKIN BOEING737 7372T4 1384492NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07129SW 22340 DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950825001911995082500191NM 1995 8 25 UPS204184 119950818A5730 SKIN BOEING727 72727C 138400JNM WS 743-745 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF LOWER FUEL CELL SKIN STA 743 TO 745 LBL 19 TO 45 WL 169. MAINTENANCE REPAIRED IAW SRM 57-30-1 AND EO 727-53-1649. 2L73 4F A3WE 19950825001921995082500192NM 1995 8 25 UPS204185 119950818A5730 SKIN BOEING727 72727C 138400JNM WS 209 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W UPPER SKIN LOWER SURFACE CORRODED AT REAR SPAR CHORD WS 209. MAINTENANCE REPAIRED IAW EO 727-57-1426. 2L73 4F A3WE 19950825001931995082500193NM 1995 8 25 UPS204217 119950818A5312 BLKHD ANGLE BOEING727 72727C 138400JNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BULKHEAD ANGLE AT BS 680 RBL 6 TO RBL 25 WL 19L. MAINTENANCE REMOVED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-2, 51-10-1 AND MM 51-20-151, MM 51-20-21. 2L73 4F A3WE 19950825001941995082500194NM 1995 8 25 UPS204218 119950818A5312 BLKHD ANGLE BOEING727 72727C 138400JNM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BULKHEAD ANGLE AT BS 680 LBL 25 TO RBL 25 OUT OF LIMITS. MAINTENANCE REMOVED ANGLE, FABRICATED AND INSTALLED NEW ANGLE. ALL WORK WAS DONE IAW SRM 53-10-1, 51-30-2, 51-10-1 AND MM 51-20-21, MM 51-20-151. 2L73 4F A3WE 19950825001951995082500195NM 1995 8 25 UPS204219 119950818A5320 STRAP BOEING727 72727C 138400JNM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STABILIZATION STRAP ON BL 0 AT RBL 2 WL 199 13S 540, 600, 620. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-1, 51-30-2. 2L73 4F A3WE 19950825001961995082500196NM 1995 8 25 UPS204220 119950818A5315 FLOORBEAM BOEING727 72727C 138400JNM BS 480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DOUBLE HOLES AND CORROSION ON FLOORBEAM AND NUTPLATE HOLES AT STA 480 RBL 25 TO 65 WL 208. MAINTENANCE REPAIRED IAW UPS EO B727-5310-7318A. 2L73 4F A3WE 19950825001971995082500197NM 1995 8 25 UPS204221 119950818A5753 FLAP CARRIAGE BOEING727 72727C 138400JNM TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 FLAP CARRIAGE INSIDE SPINDLE. MAINTENANCE REMOVED AND REPLACED THE FLAP CARRIAGE ASSY. 2L73 4F A3WE 19950825001981995082500198NM 1995 8 25 UPS204222 119950818A5753 FLAP CARRIAGE BOEING727 72727C 138400JNM TE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 2 FLAP CARRIAGE INSIDE SPINDLE. MAINTENANCE REMOVED AND REPLACED THE SPINDLE. 2L73 4F A3WE 19950825001991995082500199NM 1995 8 25 UPS204223 119950818A5753 FITTING BOEING727 72727C 138400JNM RT TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RIGHT WING O/B MIDFLAP, O/B CARRIAGE SUPPORT FITTING CORRODED. MAINTENANCE REPAIRED IAW SRM 51-30-2. 2L73 4F A3WE 19950825002001995082500200NM 1995 8 25 UPS204224 119950818A5754 BULLNOSE BOEING727 72727C 138400JNM NR 1 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 1 K-FLAP BULLNOSE HAS PITTING AROUND O/B ATTACH LUG. MAINTENANCE REMOVED AND REPLACED BULLNOSE PER MM 27-81-01. 2L73 4F A3WE 19950825002011995082500201NM 1995 8 25 UPS204225 119950818A5754 K-FLAP BOEING727 72727C 138400JNM NR 2 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 2 K-FLAP CENTER LUG CORRODED AROUND UPPER AND LOWER BOLTS. MAINTENANCE REPLACED THE NR 2 K-FLAP IAW MM 27-80-00. 2L73 4F A3WE 19950825002021995082500202NM 1995 8 25 UPS204226 119950818A5754 K-FLAP BOEING727 72727C 138400JNM NR 3 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 3 K-FLAP I/B LUG UPPER BOLT HAS CORROSION AROUND THE NUT. MAINTENANCE REPLACED THE NR 3 K-FLAP PER MM 27-80-00. 2L73 4F A3WE 19950825002031995082500203NM 1995 8 25 UPS204227 119950818A5754 K-FLAP BOEING727 72727C 138400JNM NR 4 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 K-FLAP O/B LUG PITTED AROUND UPPER AND LOWER BOLTS. MAINTENANCE REMOVED AND REPLACED NR 4 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19950825002041995082500204NM 1995 8 25 UPS204228 119950818A5754 K-FLAP BOEING727 72727C 138400JNM NR 5 PITTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP I/B LUG IS PITTED AROUND BOLTS AND EDGE LUG. MAINTENANCE REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19950825002051995082500205NM 1995 8 25 UPS204229 119950818A5754 K-FLAP BOEING727 72727C 138400JNM NR 6 PITTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 K-FLAP CENTER LUG PITTED ON LOWER I/B HOLE AND UPPER O/B HOLE. MAINTENANCE REMOVED AND REPLACED NR 6 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19950825002061995082500206NM 1995 8 25 UPS204230 119950818A5751 SKIN BOEING727 72727C 138400JNM LT AILERON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DENT AND POSSIBLE CRACK ON LEFT WING O/B AILERON UPPER SURFACE 24.5 FROM O/B END. MAINTENANCE REMOVED THE DAMAGED AREA AND FABRICATED REPAIR PARTS IAW SRM 51-80-4, MM 27-10-31, AND SRM 57-50-5. 2L73 4F A3WE 19950825002071995082500207NM 1995 8 25 UPS204231 119950818A5743 TRUNNION BOEING727 72727C 138400JNM WS 221 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE LT WING TRUNNION FITTING WS 221 WL 185 WHILE WORKING. MAINTENANCE INSTALLED NEW TRUNNION IAW SRM 51-32-4, 51-30-5, 51-30-8, AND 51-20-4. 2L73 4F A3WE 19950825002081995082500208NM 1995 8 25 UPS204232 119950818A5743 TRUNNION BOEING727 72727C 138400JNM RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TRUNNION SUPPORT FITTING AROUND HOLES FOR THE TRUNNION BEARING. MAINTENANCE REPLACED WITH NEW FITTING IAW UPS EO 727-57-1426. 2L73 4F A3WE 19950825002091995082500209NM 1995 8 25 UPS404276 119950818A3350 EEL BOEING747 747123 1384873NM CREW DOOR INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND, MAINTENANCE FOUND CREW SERVICE DOOR EMERGENCY EXIT LIGHTS FOR SLIDE INOP, DEFERED MEL 33-13. 2L74 4F A20WE 19950825002101995082500210WP 1995 8 25 UPS804234 119950818A3240 CONTL VLV DOUG DC8 DC873F 302199FWP LT MLG BRAKES FAILED A IPXAK NONE O OTHER TXTAXI/GRND HDL 1 SO01840UP 46140 WHILE ON TAXI OUT IN DFW, LT BRAKES FAILED DUE TO BROKEN ARM AT BRAKE CONTROL VALVE. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE. 2L74 4F RT4A25 19950825002111995082500211WP 1995 8 25 UPS804277 119950818A3350 EEL BULB DOUG DC8 DC873F 302199FWP CABIN FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01803UP 46073 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT WILL NOT DISARM PROPERLY. REPLACED EMERGENCY LIGHT DISARM BULB. OPS CHECK SYSTEM NORMAL IAW M/M 33-50-00. 2L74 4F RT4A25 19950825002121995082500212WP 1995 8 25 UPS804278 119950819A33506012235 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01748UP 45948 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS WOULD NOT DISARM. REPLACED EMERGENCY BATTERY PACK, SYS CHECKS OK. 2L74 4F RT4A25 19950825002131995082500213NM 1995 8 25 95FDEA01073 119950804A2910 HYD LINES BOEING727 72721C 138400MNM NLG FAILED A FDEAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25143FE 19136 A-SYS FAILURE UPON GEAR RETRACTION, QTY ZERO, PRESS ZERO, RED PAGE COMPLIED WITH. APPROXIMATELY 5 MINS FLT TIME WITH FLUID SHUTOFF, PUMPS ON, 9 MINS WITH THEM OFF. HYDRAULIC PUMPS RAN 1 MIN PRIOR TO TURNING THEM OFF. FOUND HOLE IN RETRACT LINE IN NOSE GEAR. REPLACED RETRACT AND EXTEND FLEX LINES. INSPECTED AND REPLACED NR 1 AND NR 2 ENG HYD PUMP CASE DRAIN FILTERS AND BOTH PRESS FILTERS ON A MODULE. NO CONTAMINATION FOUND, LEAK CK GOOD. SVC HYD SYS TO FULL, OK FOR SERVICE. 2L73 4F A3WE 19950825002141995082500214NM 1995 8 25 95FDEA01074 119950804A5753652163479 SKIN BOEING727 72725 1384006NM LT TE FLAP DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 L/W I/B AT FLAP DENTED LWR SURFACE 56 FROM I/B END. L/W I/B AFT FLAP REPAIRED IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950825002151995082500215NM 1995 8 25 95FDEA01075 119950804A57536521630173 SKIN BOEING727 72725 1384006NM LT TE FOREFLAP PUNCTURE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 L/W I/B FOREFLAP HAS A PUNCTURE ON UPPER SURFACE 64 FROM I/B END. L/W I/B FOREFLAP WAS REPAIRED I/W FEDEX SRM 51-40-6. 2L73 4F A3WE 19950825002161995082500216NM 1995 8 25 95FDEA01076 119950805A2611 SMOKE DETECTOR BOEING727 727225 1384077NM CARGO COMPT MALFUNCTIONED A FDEAO OTHER N FALSE WARNING UKUNKNOWN 1 SO25462FE 22550 INTERMITTENT MAIN CARGO SMOKE INDICATION. INDICATOR LIGHT NR 5 WAS ON FOR 2 SECONDS AND THEN WENT OUT. TESTED SYS ANDCHECKED GOOD. CHECKED M/CARGO SMOKE DETECTORS 5 TIMES. NOINDICATIONS OF A PROBLEM, OK FOR SERVICE. 2L73 4F A3WE 19950825002171995082500217 1995 8 25 95FDEA01077 419950809A256510608453 ESCAPE SLIDE BOEING727 72725 1384006NM PAX DOOR TORN GIRT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 FORWARD ENTRY DOOR ESCAPE SLIDE GIRT IS TORN 1.5 PER TC 72C247-00 THIS REQUIRES REPLACEMENT. REPLACED FORWARD ENTRY DOOR ESCAPE SLIDE ASSY IAW FEDEX MM 25-60-13. 2L73 4F A3WE 19950825002181995082500218NM 1995 8 25 95FDEA01078 119950809A53157075T6 FLOOR BEAM BOEING727 72725 1384006NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C235-02) ON FASTENER HOLES AT BS 344 LBL 33-57WL 208 DOUBLE DRILLED HOLE AT BS 344 LBL 51 WL 208. REPAIRED FLOOR BEAM IAW FEDEX SRM 53-10-1 AND FEDEX DWG NR SR 27-53-007. 2L73 4F A3WE 19950825002191995082500219NM 1995 8 25 95FDEA01079 119950809A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 693-704 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C235-02) ON SEAT TRACK BS 693-704 RBL 46 WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK FROM STA 690-740 IAW SRM 51-10-1, 51-30-2, ANDFEDEX MM 51-20-2, 57-20-01. 2L73 4F A3WE 19950825002201995082500220NM 1995 8 25 95FDEA01080 119950809A57542024T3 BRACKET BOEING727 72725 1384006NM NR 6 LE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 RIGHT WING NR 6 SLAT O/B TRACK TO T/E SKIN MOUNTING BRACKETCRACKED. FABRICATED REPLACEMENT BRACKET IAW FEDEX DWG 69-17497-1, FEDEX SRM 51-20-1. REPLACED CRACKED BRACKET WITH FABRICATED BRACKET IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950825002211995082500221NM 1995 8 25 95FDEA01081 119950810A2613 OVERHEAT WARNING BOEING727 727233 138408ANM LWR BODY MALFUNCTIONED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25278FE 22345 DURING CLIMB, AFTER SETTING CLIMB POWER, LOWER AFT BODY OVERHEAT LIGHT CAME ON. RAN CHECKLIST 'C'. LIGHT EXTINGUISHEDWITH RETARD OF NR 1 THROTTLE, RETURNED TO MEM. REMOVED ANDREPLACED APU KEEL BEAM FIRE LOOP. MEG BOTH LOOPS, CHECK OK. INSTALL APU, OPS CHECK GOOD. INSPECTED PNEUMATIC DUCTS IN KEEL BEAM AREA, CHECK GOOD. RAN ENG, CK NORMAL. RAN PACKS WITH A/C CLOSED UP FOR SEVERAL HOURS, NO OVERHEAT NOTED. OK TO CONTINUE. 2L73 4F RTA3WE 19950825002221995082500222NM 1995 8 25 95FDEA01065 119950802A2621 FIRE BOTTLE BOEING727 7272S2F 1384O81NM APU DISCHARGED A FDEAFH ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25215FE 22936 GDL - APU LEFT ON THROUGH T/O AND CLIMBOUT, FIRE WARNING LIGHT AND BELL AT APPROX FL 190 TO 200. FIRE HANDLE PULLED, LIGHT WENT OUT IMMEDIATELY AND BOTTLE DISCHARGED. ALL PROCEDURES IN RED TAB'S COMPLIED WITH, FIRE WARNING CIRCUIT TESTEDAND CHECKED GOOD. APU LIGHT WAS NOT ON AT THE TIME OF FIREINDICATION DUE TO AUTO SHUTDOWN. COULD NOT RUN APU DUE TO FIRE BOTTLE DISCHARGED, AND BOTTLE NOT IN STOCK AT GDL STATION. DEFERRED APU FIRE PROTECTION/DETECTION SYSTEM PER MEL 26-11 (A)(M) APU NOT TO BE USED UNTIL FIRE BOTTLE REPLACEMENT. CHANGED APU FIRE BOTTLES AS PER MM 26-23-1 PG 401. 2L73 4F A3WE 19950825002231995082500223EU 1995 8 25 95FDEA00951 119950713A5210 MECHANISM AIRBUS310 A310203 EU CABIN DOOR NOT LATCHED A FDEAI CABIN DEPRESSURIZATION J WARNING INDICATION CLCLIMB 1 SO25402FE 203 AT FL 220, RECEIVED ECAM WARNING L FWD DOOR NOT CLOSED. ALSO, GOT AUDIBLE WARNING FROM DOOR SIREN. A/C WAS DEPRESSURIZED AND WARNING CONTINUED. DURING DESCENT THROUGH 15,000, ECAM AND AUDIBLE WARNING CLEARED ITSELF. A/C WAS UNPRESSURIZED AT 15,000, WHEN PROBLEM CLEARED. INSPECTED CLOSE AND LOCK MECH OF L-1 ENTRY DOOR, NO FAULTS. DOOR OPENED AND CLOSEDNORMAL. CHECKED FOR FAIR, ALL NORMAL. OK TO CONTINUE FLIGHT PER MEL 52-8. CLOSED AND LOCK WARNING DEF, MX PROC 52-8 C/W CONT NR 0713034, EXP 7-23-95. 2L72 4F RTA35EU 19950825002241995082500224NM 1995 8 25 UPS204025 119950807A575365246367 RIB BOEING727 727247 138408FNM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01210UP 21697 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT O/B FOREFLAP CENTER LINK TO TRACK ATTACH BOLT IS CHAFING ON MIDFLAP CUTOUT RIB. FOUND CHAFED AREA TO HAVE CRACK REMOVED AND REPLACED RIB PER SRM 51-30-2. 2L73 4F A3WE 19950825002351995082500235EA 1995 8 25 95ZZZX4191 219950715A8530LW12967 CYLINDER PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA NR 1 WORN OUT A VLWAO OTHER K FLUID LOSS NRNOT REPORTED 1 GL053590N 319 318052148 L226668A OIL BLOWN OVERBOARD IN-FLIGHT (APPROX 3 QUARTS LOW). RESEARCH FOUND THE NR 1 CYLINDER LOW ON COMPRESSION. THE CYLINDER WAS FOUND WORN OUT AT THE UPPER ONE-THIRD AREA. CHROME PLATING IS WORN THROUGH. BOTH COMPRESSION RINGS WERE FOUND DESTROYED, SHATTERED INTO SEVERAL PIECES. SUBMITTER RECOMMENDS NOT ALLOWING CHROMED CYLINDER TO BE PUT ON AIRCRAFT ENGINES AS A WAY TO PREVENT PROBLEMS LIKE THIS. 1L72 3O3 O A20SO E14EA 19950825002581995082500258NE 1995 8 25 REXA95043 319950530A6110 PROPELLER SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE RT ENGINE DAMAGED A REXAK NONE C F.O.D. TXTAXI/GRND HDL 1 SO25325PX DRG704986 340A051 RIGHT PROPELLER HAS A ROCK STRIKE ON LEADING EDGE, RIGHT FORWARD EMERGENCY EXIT HAS PUNCTURE FROM A ROCK STRIKE, THREE DENTS, PUNCTURE BETWEEN RIGHT FORWARD EMERGENCY EXIT AND ICE SHIELD. REPLACED PROPELLER, INSTALLED SERVICEABLE RIGHT FORWARD EMERGENCY EXIT. MADE THREE 1 INCH CUT-OUTS IN RIGHT SKIN AT FS 301.0, FS 301.7, AND FS 304.0. FABRICATED DOUBLER AND TRIPLER AND INSTALLED THE MIAW SAAB DOCUMENT NR 72YFS0853. (X) 2L72 4T RTA52EU 6 CP61GL 19950825002601995082500260WP 1995 8 25 9512651221 119950818A5312 BULKHEAD DOUG DC10 DC1030 3023501WP FS 1841 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 46579 DURING PERIODIC CHECK, A PUNCTURE HOLE WAS FOUND IN THE AFT BULKHEAD OF THE CENTER CARGO COMPARTMENT AT FS 1841 RBL 2. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-01. 2L73 4F A22WE 19950825002611995082500261WP 1995 8 25 9512769966 119950818A2160 ANTICIPATOR DOUG DC9 DC931 3022065WP LT PACK MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL019330 47138 LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED WHEN POWER WAS APPLIED AT START OF TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED ANTICIPATOR AND THERMOSTAT, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825002621995082500262WP 1995 8 25 9512779989 119950816A2130 DUCT DOUG DC9 DC931 3022065WP RT PACK DISCONNECTED A NWAAB EMER. DESCENT O OTHER CRCRUISE 1 GL018945E 47181 LOSS OF CABIN PRESSURIZATION OCCURRED AT 29,000 FEET, CABIN ALTITUDE CLIMBED TO 11,000 FEET. INITIATED EMERGENCY DESCENT PROCEDURES AND PRESSURE WAS REGAINED AT 17,000 FEET. CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. OXYGEN MASKS DID NOT DEPLOY. FOUND RIGHT PACK FLEX DUCT FORWARD OF COLD AIR CHECK VALVE DISCONNECTED AND CLAMP MISSING. REPLACED CLAMP AND INSTALLED NEW FLEX DUCT. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825002631995082500263NM 1995 8 25 95UAL900099 119950821A2720 PCU BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE RUDDER MALFUNCTIONED A UALAO OTHER O OTHER TOTAKEOFF 1 WP29937UA 26668 ON ROTATION FROM ONT AT 128 KTS, SHARP RAPID LEFT YAW, NO RUDDER INPUT FELT ON RUDDERS, LASTED FOR 2 SECONDS, FELT LIKE ENGINE LOSS. REPLACED RUDDER PCU, ACCOMPLISHED MAX POWER RUN ON BOTH ENGINES, NO FAULTS FOUND. NO FAULT FOUND WITH PCU, UNABLE TO DUPLICATE. 2L72 4F4 FRTA16WE E2GL 19950825002641995082500264NE 1995 8 25 95UAL900100 219950821A7230 COMPRESSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE STALLED A UALAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29576UA 26690 726693 LEFT ENGINE COMPRESSOR STALL ON TAKEOFF OUT OF EWR AT 1,000 FT, HEARD ONE BANG. ENGINE INDICATIONS DID NOT CHANGE. DURING REMAINDER OF FLIGHT, ALL ENG OPERATIONS NORMAL. ENGINE WAS BORESCOPED AND FOUND WITHIN LIMITS, ACCOMPLISHED HIGH POWER RUN, ACCELERATION AND DECELERATION CHECKS AND ALL PARAMETERS WITHIN LIMITS. CHECKED ENGINE INLET, EXHAUST AND CHIP DETECTOR, NO DISCREPENCIES FOUND. 2L72 4F4 FRTA2NM E17NE 19950825002651995082500265NM 1995 8 25 95UAL900101 119950821A5200 ASSIST BOTTLES BOEING757 757222 1384956NM PWA 2037 PW2037 NE 2 RT, 4 LT/RT DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29578UA 26694 DOOR ASSIST BOTTLES FOR NR 2 RT, NR 4 LT AND NR 4 RT WERE FOUND FLAT. REPLACED DOOR ASSIST BOTTLES AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING. 2L72 4F4 FRTA2NM E17NE 19950825002661995082500266NM 1995 8 25 95UAL900102 119950821A520080330035600U ASSIST BOTTLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE 4 RT DOOR RUPTURED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29582UA 26702 DOOR ASSIST BOTTLE FOR DOOR NR 4 RT FOUND EMPTY. REPLACED DOOR ASSIST BOTTLE AND ISOLATED CAUSE AS MATERIAL DEFECT. UAL HAS A RECOVERY PLAN AND IS CORRECTING. 2L72 4F4 FRTA2NM E17NE 19950825002671995082500267NM 1995 8 25 95UAL900103 119950821A3350 EEL CONNECTOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29618UA 21878 EMERGENCY EEL LIGHT INOP, RIGHT FWD AISLE. REPLACED POWER STRIP CONNECTOR, CHECKS NORMAL. 2L72 4F4 FRTA1NM E3NE 19950825002681995082500268NM 1995 8 25 95UAL900104 119950821A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN MISSING A UALAK NONE O OTHER ININSP/MAINT 1 WP297278U 21425 EMERGENCY EXIT LIGHT IN AFT ENTRYWAY MISSING. REPLACED LIGHT ASSY, CHECKS OK. 2L73 4F4 F A3WE E2EA 19950825002691995082500269NM 1995 8 25 95UAL900105 119950821A2700 FLIGHT CONTROLS BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AIRFRAME YAW RIGHT A UALAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 WP297289U 21567 RETURNED TO THE FIELD UNDER AMBER ALERT DUE TO A HARD YAW TO THE RIGHT ON TAKEOFF. BEFORE ROTATION DURING TAKEOFF ROLL, AIRCRAFT FELT AS IF RT MAIN TIRE BLEW OR NR 3 ENGINE FAILED. VIBRATION ALSO FELT. ONCE AIRBORNE, EVERYTHING NORMAL. ACCOMPLISHED A GENERAL CHECK OF FLIGHT CONTROLS, BRAKE SYS, ENGINES (PERFORMANCE AND ACCELERATION). NO DEFECTS. TEST FLIGHT COMPLETED. ALL SYSTEMS OPERATED NORMALLY. 2L73 4F4 F A3WE E2EA 19950825002701995082500270WP 1995 8 25 ABXA9500675 119950818A33505708458503 EEL BATTERY PACK DOUG DC8 DC862 3021970WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23802AX 46134 COCKPIT EMERGENCY LIGHTS FAILED DURING A-1 CHECK. REPLACED EMERGENCY LIGHTING BATTERY PACK. SYSTEM OPS CHECKED GOOD IAW DC 8 MM. 2L74 4F 4A25 19950825002711995082500271WP 1995 8 25 ABXA9500676 119950820A335060030431 EEL POWER SUPPY DOUG DC9 DC932 3022066WP CABIN DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23985AX 47522 DURING C-CHECK INSPECTION, FOUND THE EMERGENCY LIGHTS ILLUMINATE WHEN THE SHIPS POWER IS TURNED OFF. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY IAW DC-9 SUPP MM 33-53-00. OPS CHECKED GOOD. 2L72 4F A6WE 19950825002721995082500272SO 1995 8 25 COM11955 119950821A2913MPEV30082B HYDRAULIC PUMP EMB 120 EMB120RT SO LT NACELLE LEAKING A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01156CA7474 296 120156 FLIGHT CREW REPORTED, LEFT ELECTRIC HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED ELECTRIC HYDRAULIC PUMP WITH SERVICEABLE UNIT. 2L72 4T RTA31SO 19950825002731995082500273EA 1995 8 25 COM60541 119950821A276054C54677E01 MANIFOLD CNDAIRCL600 CL6002B19 EA GROUND SPOILERS INOPERATIVE A COMAK NONE J WARNING INDICATION LDLANDING 1 SO01918CA4051 7018 OUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REMOVED AND REPLACED GROUND SPOILER MANIFOLD WITH SERVICEABLE UNIT. 2L72 4F RTA21EA 19950825002741995082500274EA 1995 8 25 COM60542 119950821A8097 WIRE CNDAIRCL600 CL6002B19 EA LT ENGINE CHAFED A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01926CA 7027 LEFT ENGINE WILL NOT ROTATE WHEN START SWITCH IS SELECTED. CIRCUIT BREAKER POP'S AND WILL NOT RESET. REPAIRED CHAFED WIRE AT JB11. 2L72 4F RTA21EA 19950825002751995082500275NM 1995 8 25 DL72L953443 119950820A3350334701748 EEL ASSY BOEING727 727232 1384082NM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11505DA 21307 OVERHEAD EMERGENCY LIGHT IN FWD CABIN INOP. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL. 2L73 4F A3WE 19950825002761995082500276NM 1995 8 25 DL72S951221 119950322A575465162256A BULLNOSE BOEING727 727232 1384082NM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 CRACK AT I/B BULLNOSE HINGE ATTACH POINT, NR 4 KRUGER FLAP. REPAIRED PER SRM 57-50-3 PG 32. 2L73 4F A3WE 19950825002771995082500277NM 1995 8 25 DL72S951410 119950311A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11528DA 21702 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKS IN L/E RIBS NR 9 AND 10. CRACKING WAS ON THE INNER SKIN OUTBOARD OF THE OUTBOARD ACTUATOR ATTACH SUPPORT RIB, CRACK IN LOWER SKIN AT 5 FROM THE OUTBOARD END OF SLAT. ALSO, A CRACK IN THE UPPER CORNER OF OPENING IN SPAR FOR THE ANTI-ICE TEE DUCT. ACCOMPLISHED REPAIRS PER MM 57-54-0. 2L73 4F A3WE 19950825002781995082500278NM 1995 8 25 DL72S953445 119950820A3350 EEL CONNECTOR 1001141 BOEING727 727232 1384082NM AFT AIRSTAIR CORRODED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11406DA 21150 AFT AIRSTAIR WELL OVERHEAD EMERGENCY LIGHT WILL NOT TEST. CLEANED CORROSION FROM CONNECTIONS AND RELAMPED, OPERATION NORMAL. 2L73 4F A3WE 19950825002791995082500279NM 1995 8 25 DL757953453 119950630A7110314N311053B COWL BOEING757 757232 1384965NM ENGINE HEAT DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING SHOP VISIT AT REPAIR STATION EZ2R812K, ENGINE FAN COWL PANEL WAS REPAIRED FOR HEAT DAMAGE AT THE LOWER END INTERIOR SKIN, AFT END LOWER CORNER. DELAMINATION ACROSS PANEL TO WITHIN 10 INCHES OF FWD EDGE AND A PUNCTURE AREA OF 3 BY 1.5 INCHES AT MID PANEL NEAR 10 O'CLOCK POSITION. EXTERIOR SKIN HAS HEAT DAMAGE IN EDGE PLIES AT LOWER END OF PANEL. ACCOMPLISHED REPAIRS PER SRM 54-21-01, 54-21-04 AND DRAWING NR 3143111. 2L72 4F RTA2NM 19950825002801995082500280NM 1995 8 25 DL757953454 119950801A7110314N311054B PANEL BOEING757 757232 1384965NM ENGINE HEAT DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO11647DL 24218 DURING SHOP VISIT AT REPAIR STATION EZ2R812K, ENGINE FAN COWL WAS REPAIRED FOR HEAT DAMAGE ON INTERIOR SKIN AT LOWER FWD END. A 2 SQ FT AREA OF HONEY COMB WAS REMOVED AND REPLACED PER DRAWING 314N3111, SRM 54-21-01 AND 54-21-04. 2L72 4F RTA2NM 19950825002811995082500281WP 1995 8 25 DLL10953444 119950815A5520 WEB LKHEED1011 10113851 5265010WP LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11729DA 193C1180 FOUND AT L/C ATL, ELEVATOR BALANCE WEIGHT SUPPORT WEB CRACKED AND FASTENERS LOOSE AT ATTACH TO UPPER STAB SURFACE, LOCATED LT ELEVATOR MOST OUTBD ACCESS PANEL. REMOVED DAMAGED BALANCE WEIGHT WEB AND DRILLED UP REPLACEMENT PART. INSTALLED NEW SUPPORT WEB. 2L73 4F A23WE 19950825002821995082500282NM 1995 8 25 DLM88953442 119950820A5310 STRUCTURE DOUG MD88 MD88 3023688NM FUSELAGE DAMAGED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11980DL 53267 A/C DAMAGED BY RAMP PERSONNEL RT SIDE 2 FT FWD OF WATER SERVICE PANEL 8 INCHES BELOW FLOOR LINE. REPAIRED PER SRM 53-04 PG 218A. 2L72 4F RTA6WE 19950825002831995082500283WP 1995 8 25 MWEA95270 119950818A2560113313 EVAC SLIDE DOUG DC9 DC914 3022034WP FWD GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL3180ME 45795 CREW REPORTS, FWD GALLEY DOOR EVACUATION SLIDE CAME OFF ITS MOUNT. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950825002841995082500284NM 1995 8 25 P5CA9500714 119950522A2840 FUEL QTY IND BOEING747 747122 1384872NM NR 3 ENGINE MALFUNCTIONED A P5CAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 WP23851FT 19756 AT FLIGHT LEVEL 33.0 SMOOTH AIR NR 3 ENGINE HAD LOUD BANG WITH FIRE BALL GOING FORWARD SHUTDOWN ENGINE. ON GROUND FOUND FUEL TANK EMPTY PLACARDED FUEL QUANTITY SYSTEM. 2L74 4F A20WE 19950825002851995082500285WP 1995 8 25 SCNA95172 119950818A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15152SY 48289 COCKPIT EMERGENCY LIGHT SYSTEM FAILED SELF-TEST. THE AFT CABIN EMERGENCY POWER SUPPLY WAS REPLACED AND THE SYSTEM TESTED GOOD. 2L73 4F A22WE 19950825002861995082500286WP 1995 8 25 SCNA95173 119950819A3350EMBS1392 EEL POWER SUPPLY DOUG DC10 DC1015 3022118WP CABIN FAULTY A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15152SY 48289 COCKPIT EMERGENCY LIGHT SYSTEM FAILED SELF-TEST. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY POWER SUPPLY AND THE SYSTEM TESTED GOOD PER MM 33-51-01. 2L73 4F A22WE 19950825002871995082500287NM 1995 8 25 SCNA95174 119950820A33501102832 EEL BATTERIES BOEING727 727227 1384078NM AFT AIRSTAIR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE AFT AIRSTAIR EMERGENCY LIGHT BATTERIES AND THE LIGHT CHECKED GOOD IAW MM 33-50-61. 2L73 4F A3WE 19950825002881995082500288NM 1995 8 25 UPS204279 119950821A5320 SPLICE BOEING727 72727C 138400JNM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE BL ZERO FRAME AT STATION 600, LBL 2 AND WL 199. MAINTENANCE FABRICATED THE REPAIR PARTS AND INSTALLED IAW UPS EO B727-5310-7277-A. 2L73 4F A3WE 19950825002891995082500289NM 1995 8 25 UPS204280 119950821A5720 CHORD BOEING727 72727C 138400JNM STA 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER CHORD AT STATION 740 AND RBL 25 TO LBL 25. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW UPS EO B727-5210-7332-A. 2L73 4F A3WE 19950825002901995082500290NM 1995 8 25 UPS204281 119950821A5320 CHORD BOEING727 72727C 138400JNM BS 950 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND OUTER CHORD BETWEEN STRINGER 9 TO 810 RIGHT. THE INDICATION IS PRESENT FOR THE FULL LENGTH AT THIS AREA. MAINTENANCE REPLACED THE DAMAGED AREA IAW UPS EO B727-5310-3012. 2L73 4F A3WE 19950825002911995082500291NM 1995 8 25 UPS204282 119950821A5743 TRUNNION FTG BOEING727 72727C 138400JNM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION UNDER THE TRUNNION FITTING OF THE LEFT WING SPAR CHORD. MAINTENANCE REMOVED AND INSTALLED NEW TRUNNION FITTING PER MM 32-11-00 AND 32-11-01. 2L73 4F A3WE 19950825002921995082500292NM 1995 8 25 UPS204283 119950821A5755 FITTING BOEING727 72727C 138400JNM NR 7 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 7 SPOILER FITTING. MAINTENANCE REMOVED AND REPLACED THE NUMBER 7 SPOILER FITTING PER SRM 1-30-2. 2L73 4F A3WE 19950825002931995082500293NM 1995 8 25 UPS204284 119950821A5320 WEB BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE WEB AT STATION 740, LBL 60 AND WL 198. MAINTENANCE REPAIRED DAMAGED AREA IAW UPS EO B727-5710-7331-A. 2L73 4F A3WE 19950825002941995082500294NM 1995 8 25 UPS204285 119950821A5320 EXPAND LINK BOEING727 72727C 138400JNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01939UP 19532 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE EXPANSION LINK AND BUSING AT STATION 740, RBL 25 AND WL 207. MAINTENANCE REMOVED AND INSTALLED A NEW LINK IAW SRM 51-10-2, 53-10-1 AND 51-30-2. 2L73 4F A3WE 19950825002951995082500295NM 1995 8 25 UPS204286 119950818A3350 EEL BOEING727 72725C 138400HNM FLIGHT DECK MALFUNCTION A IPXAK NONE L NO TEST TOTAKEOFF 1 SO01946UP 19721 PILOT REPORTED DURING TAKEOFF ROLL, ENCOUNTERED SEVERAL HARD BUMPS, EMERGENCY LIGHTS ILLUMINATED AND REMAINED ILLUMINATED IN ARMED POSITION. CHECKED OPERATION OF EMERGENCY LIGHTS AND FOUND OPERATION NORMAL AT PRESENT. 2L73 4F A3WE 19950825002961995082500296NM 1995 8 25 UPS204287 119950819A3350 EEL BATTERIES BOEING727 727185C 138406NNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01940UP 19826 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS OVER FLIGHT DECK AND FWD ENTRY DOOR INOP. REPLACED BATTERIES, OPS CHECK OK. 2L73 4F A3WE 19950825002971995082500297WP 1995 8 25 UPS804235 119950821A5755 SKIN DOUG DC8 DC871F 302199DWP NR 1 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK ON THE LOWER SURFACE OF THE LEFT HAND WING NR 1 SPOILER. MAINTENANCE REPAIRED THE SPOILER PER SRM 51-1-9. 2L74 4F RT4A25 19950825002981995082500298WP 1995 8 25 UPS804236 119950821A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 857 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN LEFT HAND LONGERON 24, UPPER VERTICAL FLANGE AT STATION 857. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2. 2L74 4F RT4A25 19950825002991995082500299WP 1995 8 25 UPS804237 119950821A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 1440 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 2 INCH CRACK IN THE SHEAR TIE AT STATION 1440 AND LONGERON 33L TO 34L. MAINTENANCE REPAIRED THE SHEAR TIE PER SRM 53-2-0. 2L74 4F RT4A25 19950825003001995082500300WP 1995 8 25 UPS804238 119950821A5320 SPLICE DOUG DC8 DC871F 302199DWP BS 1490 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SPLICE STRAP AT STATION 1490 AND LONGERON 32L. MAINTENANCE REPLACED THE SPLICE PER SRM 51-1-21. 2L74 4F RT4A25 19950825003011995082500301WP 1995 8 25 UPS804239 119950821A5712 LE RIB DOUG DC8 DC873F 302199FWP WS 691 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING LEADING EDGE UPPER RIB AT STATION XFS 691. MAINTENANCE REPAIRED THE RIB PER SRM 57-00-00 FIGURE 801. 2L74 4F RT4A25 19950825003021995082500302WP 1995 8 25 UPS804240 119950821A5744 FITTING DOUG DC8 DC873F 302199FWP NR 4 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING NR 4 SPOILER OUTBOARD ATTACH FITTING. MAINTENANCE REPLACED THE FITTING WITH SPOILER ASSEMBLY PER MM 27-61-01. 2L74 4F RT4A25 19950825003031995082500303WP 1995 8 25 UPS804241 119950821A5320 WEB DOUG DC8 DC873F 302199FWP BS 1580 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE WEBBING AT STATION 1580, AFT OF FLOOR SUPPORT ATTACH ANGLE LEFT HAND SIDE IN AFT ACCY COMPARTMENT. MAINTENANCE REPAIRED THE WEB PER SRM 53-2-0. 2L74 4F RT4A25 19950825003041995082500304WP 1995 8 25 UPS804242 119950821A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK ON THE FUSELAGE SKIN UPPER RADIUS OF THE LEFT AFT SERVICE DOOR CUTOUT. MAINTENANCE REPAIRED THE DAMAGE PER UPS EO DC8-5330-7309-A. 2L74 4F RT4A25 19950825003051995082500305WP 1995 8 25 UPS804243 119950821A5245 DOOR DOUG DC8 DC873F 302199FWP LT PACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS UNDER THE LEFT AFT PACK COOLING DOOR LOWER AFT CORNER. MAINTENANCE REPAIRED THE DAMAGED AREA PER UPS EO DC8-5330-4732-A. 2L74 4F RT4A25 19950825003061995082500306WP 1995 8 25 UPS804244 119950821A5712 LE RIB DOUG DC8 DC873F 302199FWP WS 822.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 822.5, AT THE AFT LOWER END. MAINTENANCE REMOVED THE FASTENERS AND STOP DRILLED THE CRACK PER MM 57-00-00 FIGURE 801. HFEC STOP DRILL CRACK TERMINATION. REPAIRED PER MM 57-00-00 FIGURE 801. 2L74 4F RT4A25 19950825003071995082500307WP 1995 8 25 UPS804245 119950821A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP NR 2 PIT DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER FORWARD CORNER OF THE NR 2 PIT DOOR ON THE RIGHT HAND SEAT TRACK. MAINTENANCE REMOVED THE CORRODED SECTION OF THE TRACK, FABRICATED REPLACEMENT AND INSTALLED SECTION OF TRACK PER SRM 51-3-0, 53-1-0, AND 51-3-0. 2L74 4F RT4A25 19950825003081995082500308WP 1995 8 25 UPS804246 119950821A5720 AUX SPAR CAP DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSON ON THE LEFT HAND LOWER AUX SPAR CAP AT OUTBOARD HOLES. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND LOWER AUX SPAR CAP IAW SRM 51-01-20. 2L74 4F RT4A25 19950825003091995082500309WP 1995 8 25 UPS804247 119950821A5712 RIB DOUG DC8 DC873F 302199FWP WS 304 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE AFT END OF THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 304. MAINTENANCE STOP DRILLED THE CRACK, REPAIRED AND PRIMED PER SRM 57-2-0 FIGURE 1 AND 51-8-1. 2L74 4F RT4A25 19950825003101995082500310WP 1995 8 25 UPS804248 119950821A5712 RIB DOUG DC8 DC873F 302199FWP WS 729 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LEADING EDGE RIB AT THE AFT END OF THE LEFT HAND LEADING EDGE WING AT STA 729. MAINTENANCE STOP DRILLED THE CRACK AND REPAIRED THE RIB PER SRM 57-2-0 FIGURE 1, TREATED AND PRIMED PER SRM 51-8-1. 2L74 4F RT4A25 19950825003111995082500311WP 1995 8 25 UPS804249 119950821A5730 SKIN DOUG DC8 DC873F 302199FWP WS 703.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE SCREW HEAD AT THE RIGHT HAND WING, OUTBOARD LEADING EDGE LOWER SKIN AT STATION XFS 703.5. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED THE FILLER AND DOUBLER AND INSTALLED PER SRM 57-2-1. 2L74 4F RT4A25 19950825003121995082500312WP 1995 8 25 UPS804250 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEADS AT THE RIGHT HAND CUSP AT STATION 360. MAINTENANCE REMOVED THE OLD FITTING, DRILLED AND FASTENED THE NEW FITTING IAW SRM 51-1-20 AND 51-3-0. 2L74 4F RT4A25 19950825003131995082500313WP 1995 8 25 UPS804251 119950821A5712 RIB DOUG DC8 DC873F 302199FWP WS 297.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT UPPER END OF THE LEFT HAND WING LEADING EDGE RIB AT STATION 297.5. MAINTENANCE REPAIRED THE DAMAGED AREA IAW SRM 57-2-0. 2L74 4F RT4A25 19950825003141995082500314WP 1995 8 25 UPS804252 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION AROUND THE FASTENERS AT THE END OF THE FRAME AT STATION 960 AND STRINGER 22R. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20. 2L74 4F RT4A25 19950825003151995082500315WP 1995 8 25 UPS804253 119950821A5320 DOOR FRAME DOUG DC8 DC873F 302199FWP NR 2 PIT DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME LOWER FORWARD CORNER OF THE NR 2 PIT DOOR PLATE. MAINTENANCE REMOVED THE CORRODED WEB, FABRICATED AND INSTALLED A NEW WEB PER SRM 51-1-8. 2L74 4F RT4A25 19950825003161995082500316WP 1995 8 25 UPS804254 119950821A5712 RIB DOUG DC8 DC873F 302199FWP WS 596.0 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT END OF THE UPPER LEADING EDGE RIB ON THE LEFT HAND WING LEADING EDGE AT STATION XFS 596.0. MAINTENANCE STOP DRILLED THE CRACK AND FABRICATED THE REPAIR PARTS IAW SRM 53-2-0 AND INSTALLED PARTS PER SRM 53-2-0 AND 51-1-21. 2L74 4F RT4A25 19950825003171995082500317WP 1995 8 25 UPS804255 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE ATTACH POINT TO FRAME AT STATION 1690 AND LONGERON 30R. MAINTENANCE REMOVED THE FITTING PER SRM 51-1-21 AND INSTALLED THE REPLACEMENT FITTING IAW SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 19950825003181995082500318WP 1995 8 25 UPS804256 119950821A5320 WEB DOUG DC8 DC873F 302199FWP BS 008 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A 4 INCH CRACK IN THE WEB AT THE COURIER SUBFLOOR AT STATION 008 RBL 46. MAINTENANCE STOP DRILLED THE CRACK AND REPAIRED THE WEB PER SRM 53-3-3 AND 53-2-0. 2L74 4F RT4A25 19950825003191995082500319WP 1995 8 25 UPS804257 119950821A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1040 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME CAP AT STATION 1040 AND L36 AND L35L TO L35R. MAINTENANCE REMOVED THE CORROSION PER SRM 51-1-8, FABRICATED AND INSTALLED DOUBLER PER SRM 51-1-8 AND 53-2-0. 2L74 4F RT4A25 19950825003201995082500320WP 1995 8 25 UPS804258 119950821A5711 SPAR DOUG DC8 DC873F 302199FWP WS 1 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE 3 O'CLOCK POSITION TOP VIEW LOOKING DOWN RIGHT HAND FRONT SPAR LOWER CAP FORWARD T-ANGLE, IN FURTHEST INBOARD HOLD AT STATION XFS 1.000, .020 DEEP. MAINTENANCE ENLARGED THE HOLE IAW SRM 57-2-6 FIGURE 4. HFEC INSPECTION AFTER REWORK CRACK NOTED. INSTALLED REPAIR IAW SRM 57-2-6 FIGURE 4. 2L74 4F RT4A25 19950825003211995082500321WP 1995 8 25 UPS804259 119950821A5711 SPAR DOUG DC8 DC873F 302199FWP WS 33.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE 7 O'CLOCK POSITION TOP VIEWING DOWN OF THE LEFT HAND FRONT SPAR, LOWER SPAR FORWARD T-ANGLE. FASTENERS HOLE AT STATION XFS 33.50L GREATER THAN .020 INCHES IN DEPTH. MAINTENANCE ENLARGED THE HOLE IAW SRM 57-2-6 FIGURE 4. HFEC INSPECTION AFTER REWORK REPAIR, NO CRACK NOTED. INSTALLED REPAIR IAW SRM 57-2-6. 2L74 4F RT4A25 19950825003221995082500322WP 1995 8 25 UPS804260 119950821A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1020 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT SIDE OF THE FRAME AT STATION 1020 AND STRINGER 34R. MAINTENANCE REMOVED THE CORROSION, FABRICATED AND INSTALLED THE REPAIR ANGLE PER SRM 53-2-0 FIGURE 2B, 51-1-21. 2L74 4F RT4A25 19950825003231995082500323WP 1995 8 25 UPS804261 119950821A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1020 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT SIDE OF THE FRAME AT STATION 1020 AND STRINGER 33L. MAINTENANCE REMOVED THE CORROSION, FABRICATED AND INSTALLED THE REPAIR ANGLE PER SRM 53-2-0, FIGURE 2B AND 51-1-21. 2L74 4F RT4A25 19950825003241995082500324WP 1995 8 25 UPS804262 119950821A5347 SEAT TRACK DOUG DC8 DC873F 302199FWP CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN CABIN SEAT TRACK AT THE LAV AREA AT STATION RBL 59. MAINTENANCE REMOVED THE CORRODED SECTION OF THE SEAT TRACK, FABRICATED THE SECTION OF TRACK AND INSTALLED PER SRM 53-2-3, 53-7-3, FIGURE 3 AND SRM 53-2-3. 2L74 4F RT4A25 19950825003251995082500325WP 1995 8 25 UPS804263 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEVERAL FASTENERS ON THE FRAME AT STATION 960 AND STRINGER 22L. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 53-4-1. 2L74 4F RT4A25 19950825003261995082500326WP 1995 8 25 UPS804264 119950821A5320 INTERCOSTAL DOUG DC8 DC873F 302199FWP BS 980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A LARGE CRACK AFT END OF THE BULKHEAD TIE INTERCOSTAL AND CORROSION ON THE FORWARD END AT STATION 980 TO 1000 STRINGER 32L. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19950825003271995082500327WP 1995 8 25 UPS804265 119950821A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 180 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 180 AND LONGERON 31R. MAINTENANCE REMOVED THE DOUBLER, SPLICE ANGLES, FABRICATED THE REPLACEMENT DOUBLER AND INSTALLED PER SRM 53-4-1, 51-1-8, 51-1-20 AND 51-1-14. 2L74 4F RT4A25 19950825003281995082500328WP 1995 8 25 UPS804266 119950821A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 55 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD AIRCRAFT COMPARTMENT FINGER DOUBLER AT STATION 55 AND LONGERON 31R. MAINTENANCE REMOVED THE FINGER DOUBLER, FABRICATED AND INSTALLED THE FINGER DOUBLER IAW SRM 53-3-3 FIGURE 1 AND SRM 51-1-21. 2L74 4F RT4A25 19950825003291995082500329WP 1995 8 25 UPS804267 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1691 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND THE AFT FUSELAGE END FITTING WAS CRACKED AND CORRODED AT STATION 1691 AND LONGERON 28L. MAINTENANCE REMOVED THE FITTING PER SRM 51-1-20 AND INSTALLED THE NEW FITTING PER SRM 51-1-20 AND 51-3-0. 2L74 4F RT4A25 19950825003301995082500330WP 1995 8 25 UPS804268 119950821A5320 SPLICE DOUG DC8 DC873F 302199FWP BS 1050 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SPLICE AT STATION 1050 AND LONGERON 31R. MAINTENANCE REMOVED AND REPLACED THE SPLICE FITTING PER SRM 51-1-20D, 51-3-0 AND 51-1-11. 2L74 4F RT4A25 19950825003311995082500331WP 1995 8 25 UPS804270 119950821A5347 FITTING DOUG DC8 DC873F 302199FWP BS 1520 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FLOORBEAM TO SEAT TRACK SUPPORT FITTING AT STATION 1520, BL 0 AND WL 202. MAINTENANCE REMOVED AND REPLACED THE FITTING WITH HI-LOC PER SRM 51-1-20D. 2L74 4F RT4A25 19950825003321995082500332WP 1995 8 25 UPS804271 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1700 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE END FITTING AT STATION 1700 AND LONGERON 35R. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20 AND 53-1-0. 2L74 4F RT4A25 19950825003331995082500333WP 1995 8 25 UPS804272 119950821A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1691 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE END FITTING AT STATION 1691 AND LONGERON 36. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950825003341995082500334WP 1995 8 25 UPS804273 119950821A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1645 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE LONGERON AT STATION 1645 TO 1700 AND LONGERON 35R. MAINTENANCE CUT OUT DAMAGED AREA, INSTALLED REPLACEMENT LONGERON PER SRM 53-2-2 AND FABRICATED REPAIR SPLICE AND INSTALLED PER SRM 53-1-22, 51-1-20D. 2L74 4F RT4A25 19950825003351995082500335WP 1995 8 25 UPS804274 119950821A5712 RIB DOUG DC8 DC873F 302199FWP WS 385.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK AT THE LOWER SPANWISE INTERCOSTAL AT THE RIGHT HAND WING LEADING EDGE RIB AT STATION XFS 385.25. MAINTENANCE REPAIRED THE RIB IAW SRM 51-2-0. 2L74 4F RT4A25 19950825003361995082500336WP 1995 8 25 UPS804275 119950821A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT FUSELAGE SKIN AT STATION 1690 TO 1700 BETWEEN LONGERON 35L AND 36. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-2-1. 2L74 4F RT4A25 19950825003371995082500337NM 1995 8 25 95UAL900042 119950717A2612 FIRE WARNING BOEING777 777222 1385219NM PWA PW4077PW4077 NE APU MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29768UA 26919 APU FIRE DETECTION SYSTEM FAILED FIRE OVERHEAT TEST. UNABLE TO DUPLICATE FAULT, PROBLEM HAS NOT REOCCURRED. 2L72 4F4 FRTT0001SE E46NE 19950825003601995082500360EA 1995 8 25 95ZZZX4233 119950806A3230 RETRACT MECH DHAV DHC7 DHC7102 2802708EA LT MLG MALFUNCTIONED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07900HA 025 DCA/ORF - FLT 3025 - AFTER DEPARTURE, LEFT MAIN GEAR FAILED TO SHOW UP AND LOCKED. CYCLED GEAR. ALL INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED TO ORF WITHOUT INCIDENT. INSPECTED THE LEFT MAIN GEAR, NO VISUAL DISCREPANCIES NOTED AT THIS TIME. (X) 2H74 4T A20EA 19950825003611995082500361EA 1995 8 25 95ZZZX4234 219950808A73203035279 P3 LINE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA NR 4 ENGINE BROKEN A HNAAA UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 EA07905HA31120 070 SBY/DCA - FLT 3268 - AFTER TAKEOFF, NR 4 ENGINE BEGAN TO SPOOL DOWN. THE AIRCRAFT TURNED BACK TO SBY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE P3 LINE BETWEEN THE GAS GENERATOR CASE AND FUEL CONTROL. 2H74 4T4 T A20EA E4EA 19950825003621995082500362NM 1995 8 25 95ZZZX4235 119950808A3260864202 UPLOCK SENSORS ELDEC DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07980HA3833 376 DCA/GSO - FLT 3118 - ALL AMBER GEAR DOOR LIGHTS REMAINED ILLUMINATED AFTER RETRACTION. CENTER AND AFT GEAR DOORS COULD BE SEEN OPEN. CYCLED GEAR, AND GEAR RETRACTED AS NORMAL. AIRCRAFT CONTINUED ON TO GSO WITHOUT INCIDENT. REMOVED AND REPLACED ALL UPLOCK SENSORS. PSEU CHECKED GOOD, CHECKED ALL FILTER INDICATORS, ALL CHECKED GOOD. 2H72 4T RTA13NM 19950825003631995082500363NM 1995 8 25 95ZZZX4236 119950807A33506013211X EEL BATTERY DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07975HA14441 SBY75 176 EWN/CLT - FLT 3207 - DURING PRE-FLIGHT WALK-AROUND, FOUND MID-CABIN OVERHEAD EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED 3351-PS4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. REFERENCE CONTROL NR 95ZZZX4237. 2H72 4T RTA13NM 19950825003641995082500364NM 1995 8 25 95ZZZX4237 119950807A33506104791X EEL POWER SUPPLY DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07975HA15543 PS006 176 EWN/CLT - FLT 3207 - DURING PRE-FLIGHT WALK-AROUND, FOUND MID-CABIN OVERHEAD EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED 3351-PS4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. REFERENCE CONTROL NR 95ZZZX4236. 2H72 4T RTA13NM 19950825003651995082500365NM 1995 8 25 95ZZZX4238 119950803A3260M390166105L RELAY DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07980HA3794 376 DCA/GSO - FLT 3118 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, THE GEAR RETRACTED, BUT ALL DOOR LIGHTS REMAINED ON. GEAR DOORS REMAINED OPEN. THE AIRCRAFT TURNED BACK TO DCA AND LANDED WITHOUT INCIDENT. PERFORMED PSEU TEST. REMOVED AND REPLACED THE RELAY 3261-K8. TEST FLIGHT SATISFACTORY. 2H72 4T RTA13NM 19950825003661995082500366NM 1995 8 25 95ZZZX4239 119950731A3260864202 SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE N FALSE WARNING DEDESCENT 1 EA07942HA16693 163 CRW/DCA - FLT 3075 - THE NOSE LANDING GEAR CYCLES WHEN THE GEAR HANDLE IS SELECTED DOWN. ALTERNATE EXTENSION PROCEDURES WERE FOLLOWED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE GEAR DOWNLOCK PROXIMITY SENSOR. 2H72 4T RTA13NM 19950825003671995082500367NM 1995 8 25 95ZZZX4240 119950730A33506104791X EEL BATTERY GRIMES DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07938HA17361 PS008 152 PHL/DCA - FLT 3257 - DURING PRE-FLIGHT WALK-AROUND, FOUND TWO FORWARD RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY AND BASE. REFERENCE CONTROL NR 95ZZZX4241. 2H72 4T RTA13NM 19950825003681995082500368NM 1995 8 25 95ZZZX4241 119950730A33506013211X EEL BASE GRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07938HA310 SBY106 152 PHL/DCA - FLT 3257 - DURING PRE-FLIGHT WALK-AROUND, FOUND TWO FORWARD RED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY AND BASE. REFERENCE CONTROL NR 95ZZZX4240. 2H72 4T RTA13NM 19950825003691995082500369NM 1995 8 25 95ZZZX4242 119950729A33506013211X EEL BATT PACKS GRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07927HA13172 ORF43 117 PHN/BWI - FLT 3260 - DURING PRE-FLIGHT WALK-AROUND, FOUND NUMEROUS INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY BATTERY PACKS AT LOCATIONS PS6 AND PS3. 2H72 4T RTA13NM 19950825003701995082500370NM 1995 8 25 95ZZZX4243 119950728A3260YD4N RELAY DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07980HA3750 376 HPN/PHL - FLT 3158 - WHEN THE GEAR WAS SELECTED UP AFTER TAKEOFF, THREE AMBER LIGHTS STAYED ON WITH GEAR UP. CREW SELECTED THE GEAR DOWN, TURNED BACK AND LANDED IN HPN WITHOUT INCIDENT. REMOVED AND REPLACED THE 3261-K13 RELAY. ALSO, REMOVED AND REPLACED THE PSU AS A PRECAUTION. 2H72 4T RTA13NM 19950825003711995082500371NM 1995 8 25 95ZZZX4244 119950728A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA07980HA3750 106 376 HPN/PHL - FLT 3158 - WHEN THE GEAR WAS SELECTED UP AFTER TAKEOFF, THREE AMBER LIGHTS STAYED ON WITH GEAR UP. CREW SELECTED THE GEAR DOWN, TURNED BACK AND LANDED IN HPN WITHOUT INCIDENT. REMOVED AND REPLACED THE 3261-K13 RELAY. ALSO, REMOVED AND REPLACED THE PSU AS A PRECAUTION. 2H72 4T RTA13NM 19950825003721995082500372NM 1995 8 25 95ZZZX4245 119950727A3260YD4N RELAY DHAV DHC8 DHC8102 2809003NM GEAR DOOR LIGHTSFAILED A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07980HA3745 376 GON/BWI - FLT 3157 - ON GEAR RETRACTION, ALL 3 GEAR DOOR LIGHTS STAYED ON. AFTER CYCLING THE GEAR, THE LIGHTS GO OUT. AIRCRAFT CONTINUED ON TO BWI WITHOUT INCIDENT. REMOVED AND REPLACED 3261-K9 AND 3261-K11 RELAYS. REFERENCE CONTROL NR 4246. 2H72 4T RTA13NM 19950825003731995082500373NM 1995 8 25 95ZZZX4246 119950727A3260DSC1822 RELAY DHAV DHC8 DHC8102 2809003NM GEAR DOOR LIGHTSFAILED A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07980HA3745 376 GON/BWI - FLT 3157 - ON GEAR RETRACTION, ALL 3 GEAR DOOR LIGHTS STAYED ON. AFTER CYCLING THE GEAR, THE LIGHTS GO OUT. AIRCRAFT CONTINUED ON TO BWI WITHOUT INCIDENT. REMOVED AND REPLACED 3261-K9 AND 3261-K11 RELAYS. REFERENCE CONTROL NR 95ZZZX4245. 2H72 4T RTA13NM 19950825003741995082500374NM 1995 8 25 95ZZZX4247 119950803A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07823EX 377 CLT/HHH - FLT 3174 - UPON DEPARTURE, THE GEAR WOULD NOT RETRACT. THE AIRCRAFT TURNED BACK AND LANDED IN CLT WITHOUT INCIDENT. CLOSED THE ALTERNATE RELEASE DOOR. 2H72 4T RTA13NM 19950825003751995082500375WP 1995 8 25 95ZZZX4248 119950721A323047713921C RETRACT PIN 57531185543 DOUG DC8 DC862 3021970WP LT MLG SHEARED A RRXAO OTHER J WARNING INDICATION CLCLIMB 1 WP15990CF887 904 46048 KEWR/KBWI - FLT 118 - AFTER TAKEOFF OUT OF KEWR, THE DOORS, LIGHT, AND LANDING GEAR UNSAFE LIGHT STAYED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE AND LIGHTS STAYED ILLUMINATED. HYDRAULIC PRESSURE AND QTY NORMAL. NORMAL LANDING MADE AT KBWI. MAINTENANCE FOUND LT MLG RETRACT PIN SHEARED. FERRIED TO KMCN FOR REPAIR. (SUP-INFO TO FOLLOW). 2L74 4F 4A25 19950825003761995082500376WP 1995 8 25 95ZZZX4249 119950714A5720 PROBE COVERS DOUG DC8 DC873F 302199FWP LT/RT WING CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 LEFT WING FUEL PROBE COVERS NR 5, NR 23, NR 13 AND RIGHT WING FUEL PROBE COVERS NR 6, NR 19, NR 21, AND NR 8 HAVE CRACKS. REPAIRED CRACKED LEFT WING FUEL PROBE COVERS NR 5, NR 23, NR 13, AND RIGHT WING FUEL PROBE COVERS NR 6, NR 19, NR 21, AND NR 8 IAW TIMCO REO DC08-57-1576. 2L74 4F RT4A25 19950825003771995082500377WP 1995 8 25 95ZZZX4250 119950714A5341 FILLET PANEL DOUG DC8 DC873F 302199FWP CENTER WING CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 CENTER WING FILLET PANEL NR 161K HAS AREAS OF CORROSION AND BARE METAL. REPAIRED CORRODED CENTER WING FILLET PANEL NR 161K IAW TIMCO REO DC8-53-1577. 2L74 4F RT4A25 19950825003781995082500378WP 1995 8 25 95ZZZX4251 119950714A5341 FILLET PANELS DOUG DC8 DC873F 302199FWP CENTER WING DELAMINATED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 CENTER WING FILLET PANELS NR 161-F AND NR 162-G HAVE AREAS OF DELAMINATION AND BARE METAL. REPAIRED DELAMINATED CENTER WING FILLET PANELS NR 161-F AND NR 162-G IAW TIMCO REO DC08-53-1574. 2L74 4F RT4A25 19950825003791995082500379WP 1995 8 25 95ZZZX4252 119950714A5320 SUPPORT FITTING DOUG DC8 DC873F 302199FWP BS 900 CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 THE SUPPORT FITTING ON LONGERON 24 LEFT AT FRAME STATION 900 HAS A CRACK ON THE INBOARD FACE. REPAIRED CRACKED SUPPORT FITTING ON LONGERON 24 LEFT AT FRAME STATION 900 IAW TIMCO REO DC08-53-1587. 2L74 4F RT4A25 19950825003801995082500380WP 1995 8 25 95ZZZX4253 119950714A5230 SKIN DOUG DC8 DC873F 302199FWP CARGO DOOR CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 THE LOWER CENTER EXTERNAL SKIN HAS A CRACK AT THE BOTTOM DOOR JAMB OF THE FORWARD DOOR IN THE AFT CARGO COMPARTMENT. REPAIRED THE CRACKED LOWER CENTER EXTERNAL SKIN AT THE BOTTOM DOOR JAMB OF THE FORWARD DOOR IN THE AFT CARGO COMPARTMENT IAW TIMCO REO DC08-53-1586. 2L74 4F RT4A25 19950825003811995082500381WP 1995 8 25 95ZZZX4254 119950714A5730 SKIN DOUG DC8 DC873F 302199FWP WS 69.5 CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 THE LEFT WING AT STA 69.5, LOWER SKIN AND SPAR, HAS CRACK INDICATIONS IN HOLES A, C, D, AND NR 1. REPAIRED HOLES NR A, NR C, NR D, AND NR 1, THAT HAD CRACK INDICATIONS ON THE LOWER SKIN AND SPAR ON THE LEFT WING AT STA 69.5 IAW TIMCO REO DC08-57-1583. REFERENCE CONTROL NR 95ZZZX4255. 2L74 4F RT4A25 19950825003821995082500382WP 1995 8 25 95ZZZX4255 119950714A5711 SPAR DOUG DC8 DC873F 302199FWP WS 69.5 CRACKED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15792FT 46046 THE LEFT WING AT STA 69.5, LOWER SKIN AND SPAR, HAS CRACK INDICATIONS IN HOLES A, C, D, AND NR 1. REPAIRED HOLES NR A, NR C, NR D, AND NR 1, THAT HAD CRACK INDICATIONS ON THE LOWER SKIN AND SPAR ON THE LEFT WING AT STA 69.5 IAW TIMCO REO DC08-57-1583. REFERENCE CONTROL NR 95ZZZX4254. 2L74 4F RT4A25 19950825003831995082500383NE 1995 8 25 95ZZZX4256 219950804A7261 FILTER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE DIRTY A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE05919TW 49368 ICT - FLT 65 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1206, DUE TO HIGH OIL PRESSURE AND INCREASING OIL TEMPERATURE. REPLACED ENGINE OIL FILTER AND ENGINE OIL PRESSURE RELIEF VALVE. ENGINE OPERATION AND LEAK CHECK NORMAL. ENGINE TOTAL TIME: 21,726 HOURS; 10,984 CYCLES. OP-16 - 8-17-94 - MCI. 2L72 4F4 F A6WE E9NE 19950825003841995082500384NM 1995 8 25 95ZZZX4257 119950801A793165B90115169 OIL VENT LINE BOEING747 747131 1384881NM NR 3 ENGINE LOOSE A TWAAOE OTHER ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0593108 19674 JFK - FLT 903 - DURING CRUISE, SHUT DOWN NR 3 ENGINE, SN 4285, DUE TO OIL LOSS, FOUND VENT LINE TO OIL PRESSURE TRANSMITTER LEAKING. REPLACED VENT LINE, MFG PN 65B90115-169. ENGINE OPERATION AND LEAK CHECK WAS NORMAL. ENGINE TOTAL TIME 65,051 HOURS AND 13,468 CYCLES. CHECK C2 - 1-29-95 - MCI. 2L74 4F A20WE 19950825003851995082500385NE 1995 8 25 95ZZZX4258 219950731A7314378200 FUEL PUMP DOUG DC9 DC931 3022065WP PWA JT8 JT8D7A 52053NE NR 1 ENGINE MALFUNCTIONED A TWAAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 CE05985Z 47491 STL - FLT 340 - DURING CLIMB, SHUT DOWN NR 1 ENGINE, SN 2143, DUE TO ENGINE SURGED AND THROTTLE WOULD NOT CONTROL ENGINE POWER. REPLACED ENGINE FUEL PUMP, MFG PN 378200 AND FUEL CONTROL. MFG PN 743602-4. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME 39,260 HOURS AND 41,358 CYCLES. CHECK C - 3-1-95 - STL. REFERENCE CONTROL NR 95ZZZX4259. 2L72 4F4 F A6WE E2EA 19950825003861995082500386NM 1995 8 25 95ZZZX4260 119950726A7830 TR UNIT BOEING747 747131 1384881NM NR 1 ENGINE MALFUNCTIONED A TWAAECD ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE0593107 19673 STL - FLT 720 - DURING TAKEOFF, SHUT DOWN NR 1 ENGINE, SN 4173, DUE TO UNCOMMANDED THRUST LEVER MOVEMENT TO IDLE AND REVERSER OPERATING LIGHT ILLUMINATION FOR FIVE SECONDS. CHECKED ENGINE CONTROL SYSTEM AND OPERATION WAS NORMAL. DEACTIVATED THRUST REVERSER PER MEDP. ENGINE TOTAL TIME: 77,759 HOURS; 13,914 CYCLES. CHECK C-3 - 10-29-94 - JFK. 2L74 4F A20WE 19950825003871995082500387NM 1995 8 25 CAL950645 119950803A5330 SKIN BOEING727 727243 138408DNM DOOR CUT-OUT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093441536801 22167 DEN - INSPECTION FOUND THE L-1 DOOR LOWER HINGE ARM FUSELAGE CUT-OUT WITH A 0.04 INCH CRACK IN SKIN. REPAIRED IAW ECRA 5310-03145. (X) 2L73 4F RTA3WE 19950825003881995082500388NM 1995 8 25 CAL950646 119950803A5320 ANGLES BOEING727 727243 138408DNM BS 1263 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093441536801 22167 DEN - INSPECTION FOUND .50 INCH CRACKS IN ANGLES AT STA 1263 UNDER AFT AIRSTAIR ACTUATOR ON RT SIDE. REPAIRED PER SRM 51-40-3. (X) 2L73 4F RTA3WE 19950825003891995082500389NE 1995 8 25 CAL950649 219950808A7314384300 FUEL PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE LEAKING A ACALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914814206799888 49112 DFW - FLT 0140 - THE NR 1 FUEL QUANTITY DECREASED FROM 6500 TO 1350 WITHIN 15 MINUTES WHILE ENROUTE FROM LAS TO IAH. THE CROSSFEED PROCEDURE WAS USED AND THE NR 2 FUEL QUANTITY DECREASED FASTER THAN FUEL QTY DISPLAYS COULD INDICATE. THE AIRCRAFT WAS DIVERTED TO DFW FOR AN UNEVENTFUL LANDING. AFTER LANDING, PERSONNEL ON THE GROUND REPORTED FUEL LEAKING FROM THE NR 1 ENGINE. PASSENGERS WERE DEPLANED ON THE TAXIWAY AS A PRECAUTIONARY MEASURE. MAINTENANCE FOUND THE FITTING FOR FUEL INLET PRESSURE LINE BLOWN OUT OF MANIFOLD ON NR 1 ENGINE FUEL PUMP. THE NR 1 ENGINE FUEL PUMP WAS REMOVED AND REPLACED IAW MM 73-12-01. LEAK AND OPERATIONAL CHECKS WERE NORMAL. (X) 2L72 4F4 F A6WE E9NE 19950825003901995082500390WP 1995 8 25 CAL950650 119950808A4930360800010 FUEL CONTROL GARRTT 3812761M DOUG DC9 DC981 3022081WP APU INOPERATIVE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW09168845986 810 P402 48074 EWR - FLT 0210 - THE APU AUTO SHUT-DOWN WHILE THE APU GENERATOR WAS POWERING THE LEFT BUS DURING CLIMB THROUGH FL 290. THE APU WAS RESTARTED AFTER DESCENDING TO FL 230. WHILE CLIMBING BACK THROUGH FL 270, THE APU RPM APPROACHED 108 PERCENT WITH FREQUENCY IN EXCESS OF 420 CPS. THE AIRCRAFT WAS DESCENDED BACK TO FL 230 WHERE THE FLIGHT WAS COMPELTED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL UNIT. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A6WE 19950825003911995082500391CE 1995 8 25 S2YA950001 119950428A55331294400613 ANGLE BEECH 1900 1900D 1154162CE FS 557.50 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13891SK2594 UE89 DURING AN INSPECTION, MAINTENANCE FOUND A 1.50 INCH CRACK ON THE ATTACH ANGLES OF BOTH THE LT AND RT VENTRAL FINS. THE LOCATION IS BELOW THE AFT PRESSURE BULKHEAD, FS 557.50 AND IS CAUSED BY THE LACK OF SHIMMING AT THE SKIN OVERLAP. THE CRACKS WERE REPAIRED. (X) 2L72 4T RTA24CE 19950825003921995082500392CE 1995 8 25 S2YA950003 119950512A24201143800331 VOLT/FREQ METER BEECH 1900 1900D 1154162CE OVERHEAD PANEL KNOB MISSING A S2YAK NONE O OTHER ININSP/MAINT 1 GL13801SK3014 UE80 THE PUSH-TO-READ VOLT BUTTON ON THE A.C. VOLT/FREQUENCY METER EASILY BREAKS OFF OR BECOMES LOOSE AND FALLS OFF. SUBMITTER SUGGESTED THE DESIGN NEEDS TO BE IMPROVED. THREE INSTANCES OF THIS PROBLEM HAS OCCURRED ON DIFFERENT AIRCRAFT ON FLEET. (X) 2L72 4T RTA24CE 19950825003931995082500393NE 1995 8 25 S2YA950004 219950608A7532311701101 COMP BLEED VALVE BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE LT ENGINE MALFUNCTIONED A S2YAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 GL1379SK 3271 UE79 PCE114188 THE CREW EXPERIENCED A VIBRATION ON TAKEOFF AND DURING CLIMB-OUT FOLLOWED BY A LOUD POP AND A YAW TO THE LEFT AS THEY WERE CLIMBING THROUGH 7,000 FEET ASL, THE LT PROP RPM WAS NOTICED TO DEVIATE AT THAT TIME. THE CREW RETURNED TO MKE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT ENGINE BLEED VALVE AS A PRECAUTION DUE TO POSSIBLY STICKING. (X) 2L72 4T4 TRTA24CE E26NE 19950825003941995082500394CE 1995 8 25 S2YA950011 119950601A291011455012017 HYD FILL LINE BEECH 1900 1900D 1154162CE LT WING LEAKING A S2YAK NONE K FLUID LOSS ININSP/MAINT 1 GL1381SK 3119 UE81 FOUND HYRAULIC HAND PUMP SUCTION LINE CHAFING AGAINST THE LT SIDE OF THE AIR CYCLE MACHINE EXHAUST DUCT AT ZONE 511. MAINTENANCE REPAIRED THE LINE AND SUBMITTER IS IN THE PROCESS OF CHECKING THE REST OF FLEET. (X) 2L72 4T RTA24CE 19950825003951995082500395CE 1995 8 25 S2YA950012 119950611A61207101 SWITCH BEECH 1900 1900D 1154162CE PROP SWITCH FAILED A S2YAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL1385SK 3164 UE85 THE PROP SYNCROPHASER BECAME INOP DUE TO AN ON/ON SWITCH BEING USED INSTEAD OF AN ON/OFF SWITCH. BEECH IS USING A THREE-POLE SWITCH AND THE ONE BARE UNPROTECTED TERMINAL HAS POWER SWITCHED TO IT WHEN YOU THINK IT IS SELECTED TO THE OFF POSITION. THIS HAS OCCURRED ON FOUR OTHER AIRCRAFT. (X) 2L72 4T RTA24CE 19950825003961995082500396CE 1995 8 25 S2YA950014 119950628A284011438904029 FUEL SENSOR BEECH 1900 1900D 1154162CE RT TANK FAILED A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13901SK2938 UE90 AFTER TAKEOFF, RIGHT COLLECTOR TANK 'LOW' ANNUNCIATOR ILLUMINATED. THE CREW DECIDED TO RETURN TO MKE AND MEL'D THE SYSTEM. THE FLIGHT NUMBER WAS 1834.2. MAINTENANCE LATER TROUBLESHOT THE SYSTEM AND REMOVED AND REPLACED THE FUEL LEVEL SENSOR. (X) 2L72 4T RTA24CE 19950825003971995082500397NM 1995 8 25 95ZZZM279 119950715A3234574205 SEL VALVE DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION TOTAKEOFF 1 EA07975HA15357 405 176 FLT 3434 - BWI-CHO - ON TAKEOFF, THE NOSE GEAR DID NOT RETRACT, THE DOORS REMAINED OPEN AND NOSE GEAR REMAINED UNSAFE FOR 20 SECONDS. THE AIRCRAFT CONTINUED ON TO CHO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE PROXIMITY SENSOR FOR THE NOSE GEAR DRAG STRUT. (M) 2H72 4T RTA13NM 19950825003981995082500398NM 1995 8 25 95ZZZM280 119950715A3260864202 PROX SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION TOTAKEOFF 1 EA07975HA15364 5143 176 FLT 3434 - BWI-CHO - ON TAKEOFF, THE NOSE GEAR DID NOT RETRACT, THE DOORS REMAINED OPEN AND NOSE GEAR REMAINED UNSAFE FOR 20 SECONDS. THE AIRCRAFT CONTINUED ON TO CHO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE PROXIMITY SENSOR FOR THE NOSE GEAR DRAG STRUT. (M) 2H72 4T RTA13NM 19950825003991995082500399NM 1995 8 25 95ZZZM281 119950714A33506013211X EEL BATTERY GRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07926HA14041 ORF21 114 FLT 3082 - PHF-DCA - DURING PREFLIGHT WALKAROUND, FOUND FIRST TWO RED FLOOR LEVEL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT 3352-PS1. (M) 2H72 4T RTA13NM 19950825004001995082500400NM 1995 8 25 95ZZZM282 119950714A33506104791X EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07926HA18816 PS033 114 FLT 3082 - PHF-DCA - DURING PREFLIGHT WALKAROUND, FOUND FIRST TWO RED FLOOR LEVEL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT 3352-PS1. (M) 2H72 4T RTA13NM 19950825004011995082500401NM 1995 8 25 95ZZZM283 119950714A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07975HA1366912393 189 176 FLT NR 3103 - BWI TO HPN - ON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW CYCLED THE GEAR DOWN, RETURNED TO BWI AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROXIMITY SENSING ELECTRONIC UNIT. 2H72 4T RTA13NM 19950825004021995082500402NM 1995 8 25 95ZZZM284 119950718A323382970018009 ACTUATOR DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA072FOR 9148 0223 070 FLT 3064 - PBI-TPA - LEFT FORWARD MAIN GEAR DOOR REMAINED OPEN AFTER TAKEOFF. AIRCRAFT CONTINUED ON TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MAIN FORWARD GEAR DOOR ACTUATOR. 2H72 4T RTA13NM 19950825004031995082500403CE 1995 8 25 95ZZZM285 119950301A27501005240731 MOTOR BEECH 1900 1900D 1154162CE TE FLAPS FAILED A AMASAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW01113YV UE113 DEPARTED MONTROSE, PASSENGER COMPLAINED OF SMOKE IN CABIN. PILOT CALLED AN INFLIGHT EMERGENCY. RETURNED TO GATE WITHOUT INCIDENT. MECHANIC FOUND FLAP MOTOR AND WIRES BURNED. MEL'D FLAPS. PERFORMED GROUND RUN USING ALL ENVIRONMENTAL CHECKS TO ENSURE THERE WOULD NOT BE CONTINUING PROBLEM. PERFORMED TEST FLIGHT ALSO. NO FURTHER DISCREPANCIES WERE FOUND. (M) 2L72 4T RTA24CE 19950825004041995082500404EA 1995 8 25 95ZZZM286 119950628A77123039478 TQ SIG COND UNIT DHAV DHC8 DHC8311 1386006EA RT ENGINE FAILED A AMASAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW01436AW7090 336 FLT NR 7538 - ON DEPARTURE OUT OF DEN AT 200 FEET AGL THE RT ENGINE AUTOFEATHERED UNCOMMANDED, POWER WAS PULLED BACK ON THE RT ENGINE, AND THE SHUTDOWN AND SECURED THE CREW THEN RETURNED TO DEN. THE FDR DATA WAS DOWN LOADED BY MX PERSONNEL AND SENT TO PWA PER DHC8311 MM. PWA REVIEWED AND REPORTED ACTUAL OVER TQ OF RT ENG TO BE 145.40 PERCENT. THE PROP WAS REMOVED PER HAMSTD MM FOR INSPECTION. THE RT RGB CHIP DETECT AND SCAVENGE FILTER INSPECTED PER PWA MANUAL AND FOUND OK. THE RT ENG TQ PROBE TSCU WAS CHANGED, GROUND RUNS PERFORMED. GROUND RUN CHECK GOOD. TEST FLT PERFORMED, TEST FLT SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950825004051995082500405NM 1995 8 25 95ZZZM287 119950717A5711 SPAR BOEING737 737214 138446RNM FS 120.5-140.5 CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15460AT2770627706 20158 ON 6/18/95 AT MCO APPROXIMATELY 2100 LOCAL, INSPECTION FOUND A CRACK AT LEFT WING FRONT SPAR UPPER CHORD BETWEEN FRONT SPAR STATION FS 140.5 (20 INCHES). TOTAL AIRCRAFT TIME 49,617.5, TOTAL AIRCRAFT CYCLES 60,930. THE CRACK WAS FOUND DURING THE REPETITIVE INSPECTION REQUIRED BY AD-11-04, AND PERFORMED IAW SERVICE BULLETIN 737-57A1081 REVISION 10, DATED JULY 16, 1987. A RECORDS INSPECTION REVEALED THAT CRACK HAD BEEN REPAIRED IAW SB 57A1081 BY PAMCORP ON 10/13/93. RETURNED AIRCRAFT TO SERVICE. 2L72 4F A16WE 19950825004061995082500406NM 1995 8 25 95ZZZM288 119950708A7714MS9386112 PACKING DHAV DHC8 DHC8102 2809003NM NR 1 ENG DETERIORATED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15828MA 333 FLT 3106 - DURING CRUISE EN ROUTE FROM DTW TO YOW, THE CREW NOTED OILY SMOKE COMING FROM THE BLEED AIR SYSTEM. THE CREW SHUT DOWN BOTH BLEEDS AND RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 N1 PROB O-RINGS. THE SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950825004071995082500407WP 1995 8 25 CAL950608 119950719A3260 DOWNLOCK DOUG DC9 DC982 3022082WP RT MLG INOPERATIVE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0983873 49121 FLT NR 0364 - EWR - THE RIGHT MLG RED UNSAFE LIGHT ILLUMINATED WHILE ON APPROACH TO EWR. ABNORMAL PROCEDURES WERE COMPLIED WITH DURING A GO AROUND AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK SENSOR AT FAULT. THE DOWNLOCK SENSOR AND CANNON PLUG WAS REMOVED AND REPLACED. LANDING GEAR INDICATIONS TESTED GOOD. (M) 2L72 4F A6WE 19950825004081995082500408WP 1995 8 25 CAL950609 119950720A25308101220000B OVEN DOUG DC9 DC982 3022082WP GALLEY INOPERATIVE A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW098387020273 48056 FLT NR 0762 - EWR - AN OVEN IN FIRST CLASS GALLEY BEGAN TO SMOKE WHILE IN FLIGHT. THE SMOKE WAS ACCOMPANIED BY A CRACKING SOUND AND THE POWER LIGHT FLICKERING. THE SMOKE CEASED AFTER PULLING THE OVEN CIRCUIT BREAKER AND SHUTTING OFF THE GALLEY POWER. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 1 FIRST CLASS GALLEY OVEN WAS FOUND AT FAULT. THE OVEN WAS REMOVED AND REPLACED. OPERATION OF THE OVEN CHECKED GOOD WITH NO DISCREPANCIES NOTED. (M) 2L72 4F A6WE 19950825004091995082500409WP 1995 8 25 CAL950611 119950723A3230580236 CONTROL CABLE DOUG DC10 DC1010 3022110WP LANDING GEAR BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0968046 47800 FLT NR 0970 - NGO - THE LANDING GEAR WOULD NOT RETRACT WHEN GEAR WAS SELECTED TO UP POSITION AFTER TAKEOFF FROM NGO. THE AIRCRAFT WAS RETURNED TO NGO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE PUSH-PULL CABLE BEHIND THE GEAR SELECTOR HANDLE BROKEN. THE CABLE WAS REMOVED AND REPLACED. THE CABLE WAS ADJUSTED AND OPERATION CHECKED GOOD IAW MM 32-31-02. (M) 2L73 4F A22WE 19950825004101995082500410NM 1995 8 25 MALA954530 119950708A7714AS3209110 PACKING DHAV DHC8 DHC8102 2809003NM NR 1 ENG DETERIORATED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15828MA 333 FLT 3106 - DURING CRUISE EN ROUTE FROM DTW TO YOW, THE CREW NOTED OILY SMOKE COMING FROM THE BLEED AIR SYSTEM. THE CREW SHUT DOWN BOTH BLEEDS AND RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 N1 PROBE O-RINGS. THE SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950825004111995082500411SW 1995 8 25 MALA954541 119950715A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15430MA AC710 FLT 3027 - ON APPROACH TO MSP, THE CREW DIDN'T RECEIVE A DOWN AND LOCKED INDICATION FROM THE NOSE GEAR POSITION AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR TWICE BEFORE A DOWN AND LOCKED INDICATION WAS RECEIVED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH NOSE GEAR DOWNLOCK SWITCHES. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950825004121995082500412SW 1995 8 25 MALA954542 119950717A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG OUT OF ADJUST A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL1526863 AC650B FLT NR 3460 - IN CRUISE FLIGHT TO MSP, THE LEFT GEAR INTRANSIT LIGHT ILLUMINATED IN LIGHT TURBULENCE WITH THE GEAR UP AND LOCKED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED A POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950825004131995082500413WP 1995 8 25 MALA954543 219950717A723031070511 COMPRESSOR SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP RT ENGINE FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15424MA AC639 DURING AN ENGINE INSPECTION IN MSP, MAINTENANCE NOTED THAT THE RIGHT ENGINE COMPRESSOR SEAL WAS DETERIORATED. REPAIRS WERE COMPLETED BY REPLACING THE SEAL, P/N 3107051-1, IAW GARRETT ENGINE MAINTENANCE MANUAL REFERENCES 72-00-00, 72-10-01, 72-10-06, 71-10-09, THROUGH 72-10-13. (M) 1L72 4T3 T A8SW E2WE 19950825004141995082500414NM 1995 8 25 MALA954547 119950717A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15822MA 326 DURING A C-CHECK INSPECTION IN BNA, MAINTENANCE FOUND THE FORWARD INTERIOR AND EXTERIOR EMERGENCY LIGHTS TO BE INOPERATIVE. REPAIRS WERE COMPLETED BY REPLACING THE BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950825004151995082500415NM 1995 8 25 MALA954548 119950719A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15864MA 363 DURING A MAINTENANCE WALKAROUND IN DTW, THE COCKPIT EMERGENCY LAMP ASSEMBLY WAS FOUND TO BE INOPERATIVE. REPAIRS WERE COMPLETED BY REPLACING THE COMPONENT. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950825004161995082500416NE 1995 8 25 SIMA952044 219950723A7200 ENGINE AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE RIGHT FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21263AT3221 263 127065 ICT - FLT 3746 - AFTER TAKEOFF, LOST POWER TO NR 2 ENGINE, AND FIRE WARNING. CREW ACTIVATED FIRE BOTTLE AND RETURNED TO ICT. MAINTENANCE REPLACED THE NR 2 ENGINE. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19950825004171995082500417NE 1995 8 25 USAA950755 219950708A7321 FUEL CONTROL BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE MALFUNCTIONED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 EA19523AU 23858 SYR - FLT 1518 - EN ROUTE BTV TO PIT, NR 2 ENGINE FLAMED OUT DURING FUEL CROSSFEED, RIGHT PUMPS OFF, LEFT PUMPS ON, CROSSFEED OPEN. FLIGHT CREW ACCOMPLISHED INFLIGHT RESTART AND DIVERTED TO SYR. SINGLE ENGINE TIME WAS 7 MINUTES. MAINTENANCE REPLACED AUX FUEL CONTROL UNIT, NR 2 ENGINE MEC AND FUEL PUMP. ACCOMPLISHED FUEL SYSTEM VACUUM FEED TEST. OPS CHECKED GOOD. (M) 2L72 4F4 FRTA16WE E2GL 19950825004181995082500418NM 1995 8 25 USAA950756 119950711A7933 OIL TEMP TRANS BOEING737 737301 1384611NM RT ENG FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA19577US 23742 PHL - FLT 385 - HIGH OIL TEMPERATURE ON TAKEOFF FROM PHL. CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE OIL TEMPERATURE TRANSMITTER. (M) 2L72 4F RTA16WE 19950825004191995082500419NM 1995 8 25 USAA950757 119950712A521066109013 HINGE COVER BOEING737 737301 1384611NM MAIN ENTRANCE DRLEAKING A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19573US 23560 SAN - FLT 1412 - ON CLIMB-OUT, SQUEAL WAS HEARD OUT OF THE L1 DOOR. AT FL 330 IN CRUISE, CABIN PRESSURE BEGAN TO CLIMB. FLIGHT RETURNED TO SAN WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FORWARD ENTRY DOOR TOP HINGE COVER. (M) 2L72 4F RTA16WE 19950825004201995082500420EU 1995 8 25 VTZA95225 119950719A612089548115 PROP PITCH CONTL JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE MALFUNCTIONED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27309UE 41022 FLT 6345 - IAD-LGA - ABORTED TAKEOFF DUE TO THE LEFT ENGINE ONLY MAKING 80 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE PROP PITCH CONTROL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950825004211995082500421EU 1995 8 25 VTZA95226 119950719A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27495UE 818 FLT 6247 - IAD-BGM - ABORTED TAKEOFF DUE TO THE LEFT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RECALIBRATED THE TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950825004221995082500422EU 1995 8 25 VTZA95230 119950719A2751TY176004A TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU RT TE FLAP FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27302UE 41013 FLT 6577 - IAD-JFK - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE FLAP ASYMMETRY LIGHT ILLUMINATING DURING CLIMB-OUT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950825004231995082500423WP 1995 8 25 WRLA95036 119950718A33505863108 EEL DOUG DC10 DC1030 3023501WP CABIN BROKEN A WRLAK NONE L NO TEST ININSP/MAINT 1 EA273024W 48318 DURING PREFLIGHT, FLIGHT CREW NOTED EMERGENCY ESCAPE PATH LIGHT STRIP, RIGHT SIDE FORWARD 'A' ZONE INOPERATIVE. REPAIRED BROKEN WIRING TO STRIP CONNECTOR. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A22WE 19950825004241995082500424EU 1995 8 25 WTAA950224 119950705A5610 WINDSHIELD BAG JETSTMJETSTM3101 1500215EU RT COCKPIT BIRD STRIKE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 WP17331CA 793 LAX - BIRD STRIKE REPORTED ABOVE FLIGHT OFFICERS WINDSHIELD ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950825004251995082500425SO 1995 8 25 WTAA950225 119950705A5270JS5 SWITCH ROLLER EMB 120 EMB120RT SO RT FUEL DOOR OUT OF ADJUST A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17280UE 120090 LAX - SERVICE DOOR WARNING ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED INBOARD FUEL SERVICE DOOR MICROSWITCH ROLLER. DOOR WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950825004261995082500426NE 1995 8 25 WTAA950226 219950705A73203038046 TUBE ASSY EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE AIR LEAK A WTAAO OTHER O OTHER CRCRUISE 1 WP17285UE 120153 SFO - RT ENGINE TORQUE DROPPED TO ZERO IN FLIGHT. ENGINE REPORTED UNRESPONSIVE TO ENGINE CONTROL CHANGES. CREW DECLARED EMERGENCY AND CONTINUED TO STATION WITHOUT INCIDENT. MAINTENANCE DISCOVERED LEAKING PNEUMATIC PRESSURE SENSING TUBE ASSEMBLY FROM OVERSPEED GOVERNOR TO HMU. REPLACED TUBE ASSEMBLY. ENGINE GROUND CHECKED NORMAL, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19950825004271995082500427SO 1995 8 25 WTAA950227 119950706A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17453UE 120148 RNO - TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA31SO 19950825004281995082500428SO 1995 8 25 WTAA950228 119950709A3150 AURAL WARNING EMB 120 EMB120RT SO COCKPIT SOUNDED A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17453UE 120148 SFO - AUTOFEATHER AURAL WARNING SOUNDED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. UNABLE TO DUPLICATE DISCREPANCY. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950825004291995082500429EU 1995 8 25 WTAA950229 119950711A261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU BAGGAGE COMPT MALFUNCTIONED A WTAAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP17402UE 734 FAT - BAGGAGE COMPARTMENT SMOKE DETECTOR ACTIVATED AT GATE AFTER PASSENGERS WERE BOARDED. NO SMOKE DETECTED IN BAGGAGE COMPARTMENT. PROBLEM FOUND TO BE FALSE ACTIVATION OF DETECTOR. MAINTENANCE REPLACED SMOKE DETECTOR. SYSTEM OPERATIONAL CHECK NORMAL AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950825004301995082500430SO 1995 8 25 WTAA950230 119950716A3230922FS2A6NZ735 PROX SENSOR EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17284UE 120145 FAT - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR SHOCK ABSORBER PROXIMITY SENSOR. GEAR EXTENSION AND RETRACTION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950825004311995082500431EU 1995 8 25 WTAA950231 119950712A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3101 1500215EU LT ENG OUT OF ADJUST A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17425UE 798 SEA - LEFT ENGINE FAILED TO OBTAIN REQUIRED TAKEOFF TORQUE. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT ENGINE TORQUE SIGNAL CONDITIONER. ENGINE OBTAINS TARGET TORQUE DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950825004321995082500432NM 1995 8 25 95ZZZM289 119950709A3010320115 ANTI-ICE VLV BOEING727 727225 1384077NM LT WING INOP A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA258880Z 23303 21453 FLT NR 10, MCO-EWR - AFTER TAKEOFF PASSING 10,000 FEET, LOWER AFT BDY OVERHEAT, NR 1 WING ANTI-ICE VALVE LIGHTS CAME ON, STANDBY LIGHTS ILLUMINATED. NR 1 WING BLEED VALVE, NR 1 PK VALVE AND LE VALVE CIRCUIT BREAKERS POPPED. NR 1 ENGINE SHUT DOWN PRECAUTIONARY. AIRCRAFT RETURNED TO MCO. REMOVED AND REPLACED BLOWN 13TH STAGE DUCT AND WING ANTI-ICE VALVE FROM NR 1 ENGINE, LEAK CHECK OK AS PER MM 30-10-00. FOUND WIRES, C/P'S DAMAGED TO FLW CONT MODULE S/O VALVES TO STANDBY PUMP AND TAI FOR WING SENSOR OUT NR 1 ENGINE REWIRED AND INSTALLED NEW C/P'S ON VALVES, PUMP SENSOR. OPS CHECK AND INSPECTED OK AS PER MM 72-10-01. (M) 2L73 4F A3WE 19950825004331995082500433WP 1995 8 25 95ZZZM290 119950706A3260PDS077S6043 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG OPERATIONAL A VJ6AL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO11905VJ 47378 FLT NR 286 - ATL-MCO - UPON LANDING GEAR EXTENSION ON APPROACH TO MCO THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. FLIGHT CREW AND ATC CONFIRMED GEAR EXTENSION AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND LOOSE CANNON PLUG ON DOWNLOCK SWITCH. RESECURED AND CLEARED OPERATIONAL CHECKS OK. 2L72 4F A6WE 19950825004341995082500434WP 1995 8 25 95ZZZM291 119950718A2612 FIRE WIRE DOUG DC8 DC8F54 3021926WP NR 1 ENGINE LOOSE A ATC8AO OTHER N FALSE WARNING CLCLIMB 1 GL23802CK 45679 UPON ROTATION NR 1 ENGINE FIRE WARNING WENT OFF. COMPLETED APPROPRIATE CHECKLIST. DUE TO BEING ON 3 ENGINE FERRY, WAS NOW ON 2 ENGINES. DECLARED EMERGENCY, RETURNED TO HUF. TROUBLESHOT, FOUND NO FIRE BUT INDICATION ONLY. FOUND WIRE PULLED FROM AFT OUTBOARD COWL CANNON PLUG. INSTALLED NEW PIN, GROUND TEST SEVERAL TIMES, OK FOR SERVICE IAW MM 26-2-0. (M) 2L74 4F 4A25 19950825004351995082500435WP 1995 8 25 95ZZZM292 119950723A2530 OVEN DOUG DC9 DC982 3022082WP AFT GALLEY SMOKING A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05909TW 49170 PHX - DURING CRUISE, AFT GALLEY FORWARD OVEN EMITTED SMOKE. SHUT OFF OVEN, SMOKE DISSIPATED. FOUND CHARRED PAPER FROM FOOD CONTAINER. CLEANED OVEN AND OPERATION CHECK NORMAL. 2L72 4F A6WE 19950825004361995082500436NE 1995 8 25 95ZZZM293 219950721A7261 OIL FILTER LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 ENGINE DIRTY A TWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 CE0515017 193B1063 DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4806, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION. FOUND CARBON IN OIL FILTER. REPLACED OIL FILTER, DRAINED AND REPLENISHED ENGINE OIL. ENGINE OIL FILTER DIFFERENTIAL PRESSURE SYSTEM CHECKED NORMAL. ENGINE TOTAL TIME 49,276, TOTAL CYCLES 16,099. 2L73 4F4 F A23WE A12EU 19950825004371995082500437NE 1995 8 25 95ZZZM294 219950723A73217436025 FUEL CONTROL DOUG DC9 DC934 302207EWP PWA JT8 JT8D15 52051NE RT ENGINE FAILED A TWAAO OTHER O OTHER DEDESCENT 1 CE05928L 48124 DURING DESCENT SHUT DOWN RIGHT ENGINE, S/N 1605, DUE TO ENGINE DID NOT REDUCE TO IDLE WHEN THRUST LEVER WAS MOVED TO IDLE POSITION. FOUND FUEL CONTROL HAD INTERNAL MALFUNCTION. REPLACED FUEL CONTROL, MFG P/N 743602-5. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME 27,452, TOTAL CYCLES 23,975. 2L72 4F4 FRTA6WE E2EA 19950825004381995082500438NM 1995 8 25 95ZZZM295 119950720A793135674033001 OIL PRESS TRANS BOEING747 747131 1384881NM NR 2 ENGINE FAILED A TWAAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 CE0593107 19673 DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4144, DUE TO OIL PRESSURE FLUCTUATION AND LOW OIL QUANTITY. FOUND OIL PRESSURE TRANSMITTER, MFG P/N 35674403-3001, CRACKED. REPLACED OIL PRESSURE TRANSMITTER. ENGINE LEAK CHECKED AND OPERATION CHECKED NORMAL. ENGINE TOTAL TIME 70,948, TOTAL CYCLES 13,869. 2L74 4F A20WE 19950825004391995082500439NE 1995 8 25 95ZZZM296 219950725A7250836201 TURBINE BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT ENGINE FAILED A TWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE05906TW 49160 1218 AFTER TAKEOFF SHUT DOWN RIGHT ENGINE, DUE TO LOUD BANG AND N1 ROLLED BACK TO 62 PERCENT. FOUND METAL PARTICLES IN EXHAUST PIPE. REPLACED RIGHT ENGINE. ENGINE OPERATION CHECKED NORMAL. S/D INVESTIGATION INTO ENGINE STALL AND METAL IN EXHAUST PIPE, REVEALED FIRST STAGE TURBINE BLADE, P/N 836201, RELEASED OUTER PORTION OF AIRFOIL DUE TO FATIGUE CRACK. ENGINE WAS REPAIRED AND RETURNED TO SERVICE. (M) 2L72 4F4 F A6WE E9NE 19950825004401995082500440NE 1995 8 25 95ZZZM297 219950718A7320 EEC BOEING767 767231 1385131NM PWA JT9 JT9D7R4D 52054NE RT ENGINE OUT OF ADJUST A TWAAO OTHER O OTHER TXTAXI/GRND HDL 1 CE05605TW 22568 DURING HOLDING PATTERN RIGHT ENGINE DID NOT RESPOND TO THROTTLE AND ENGINE ROLLED BACK TO IDLE. TURNED OFF EEC. CHECKED ENGINE OPERATION AND ADJUSTED ENGINE IDLE. ENGINE OPERATION CHECKED NORMAL. 2L72 4F4 FRTA1NM E3NE 19950825004411995082500441NM 1995 8 25 95ZZZM298 119950717A2530888011 FOOD CART BOEING767 767231 1385131NM GALLEY FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05602TW 22565 DURING CRUISE, FOOD CART S/N 3212, HAD ELECTRICAL MALFUNCTION AND EMITTED STRONG FUMES. DISCONNECTED FOOD CART. REPLACED FOOD CART, MFG P/N 88801-1, CHECKED GALLEY ELECTRICAL, AND OPERATION WAS NORMAL. 2L72 4F RTA1NM 19950825004421995082500442WP 1995 8 25 95ZZZM299 119950703A32601HE1912 SWITCH CVAC 440 440 2422902WP RT MLG DEFECTIVE A SPAAO OTHER N FALSE WARNING APAPPROACH 1 WP0773157 312 DURING APPROACH INTO LAS WHEN LANDING GEAR SELECTED DOWN, THE RED GEAR UNLOCKED LIGHT REMAINED ON WITH ALL THREE GEAR SAFE LIGHTS ILLUMINATED. THE RT MAIN GEAR DOWNLOCK SWITCH WAS FOUND DEFECTIVE. THE SWITCH WAS REPLACED AND ADJUSTED PER THE CV-580 MM. 2L72 4R 6A6 19950825004431995082500443WP 1995 8 25 95ZZZM300 119950707A3350 EEL CVAC 440 440 2422902WP CABIN INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP0773153 179 DURING UNSCHEDULED MAINTENANCE, THE FORWARD EMERGENCY EXIT LIGHT AND ALL EXTERIOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. CLEANED CORROSION, INCREASED TENSION ON BASE CONTACT AREA OF BATTERY FOR FORWARD INTERIOR EMERGENCY EXIT LIGHT. REPLACED BURNED OUT LAMPS, CLEANED LIGHT BULB SOCKETS AND CLEANED BATTERY PACK CONNECTION FOR ALL EXTERIOR EMERGENCY EXIT LIGHTS. SUBSEQUENT SYSTEM CHECKS WERE SATISFACTORY. 2L72 4R 6A6 19950825004441995082500444NM 1995 8 25 AALA951211 119950706A5754114T410555 TE SKIN BOEING767 767223 1385123NM NR 5 SLAT DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW07335AA 22333 SFO - DURING OVERNIGHT CHECK, NR 5 LEADING EDGE SLAT FOUND WITH DELAMINATION AT MOST INBOARD AREA AT TRAILING EDGE WHICH WAS BEYOND SRM LIMITS. REPLACED NR 5 LEADING EDGE SLAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825004451995082500445WP 1995 8 25 ASAA9580170 119950727A78307936907603 HYD LINE DOUG DC9 DC982 3022082WP LT TR UNIT BROKEN A ASAAO OTHER BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TXTAXI/GRND HDL 1 NM01932AS 49233 SFO - FLT NR 232 - AFTER LANDING, FLIGHT ATTENDANTS REPORTED FUMES/VAPOR IN CABIN. CREW NOTED LEFT HYDRAULIC QUANTITY AT 'O' ENTERING TAXI WAY. ACCOMPLISHED EMERGENCY EVACUATION OF PASSENGERS ON TAXI WAY WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH BROKEN. HYDRAULIC FLUID MIGRATED INTO APU INLET CAUSING FUMES/VAPOR IN CABIN. REPLACED HYDRAULIC LINE, HYDRAULIC CASE DRAIN FILTERS AND WATER SEPARATOR COALESCERS, SERVICED AND BLED HYDRAULIC SYSTEM. (M) 2L72 4F A6WE 19950825004461995082500446WP 1995 8 25 CAL950485 119950614A213010315411 RELIEF VALVE DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A ACALABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 SW092750923079 47798 FLT NR 1173 - IAH - THE AIRCRAFT EXPERIENCED RAPID DECOMPRESSION DURING CLIMB-OUT OF MSY. AN EMERGENCY DESCENT WAS PERFORMED AND THE OXYGEN MASKS DROPPED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE AFT POSITIVE PRESSURE RELIEF VALVE AT FAULT. THE RELIEF VALVE WAS REMOVED AND REPLACED AND OPERATION CHECKED NORMAL. IT WAS DISCOVERED THAT BOTH AFT LAV OXYGEN MASKS HAD NOT DEPLOYED. A DROP CHECK OF MASKS WAS PERFORMED AND OPERATION WAS ALL NORMAL. THE MASKS WERE RESTOWED. (M) 2L72 4F A6WE 19950825004471995082500447WP 1995 8 25 CAL950490 119950514A2420DC62E16SM1SM CONNECTOR DOUG DC9 DC982 3022082WP APU CONTAMINATED A ACALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW0910801 49127 EWR - FLT 0305 - WHILE APU WAS POWERING THE LT BUS, WITH LT GENERATOR PLACARDED INOPERATIVE & THE RT GENERATOR COVERING RT BUS, BOTH GENERATORS DROPPED OFF LINE ON TAKEOFF FROM EWR. THE LOSS OF GENERATOR WAS ACCOMPANIED BY ILLUMINATION OF THE APU GENERATOR FEEDER FAULT LIGHT. POWER COULD NOT BE RESTORED. AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY ON EMERGENCY POWER. MX FOUND OIL IN THE APU FEEDER CABLE FIREWALL DISCONNECT PLUG P1-1110. PLUG WAS REMOVED AND CLEANED. APU GENERATOR WAS POWERED AND ALL CHECKED GOOD. LT GENERATOR PLACARD WAS CLEARED BY REPLACING LT ENGINE RELAY. ALL ENGINES WERE RUN & OPERATION OF ALL GENERATORS CHKED GOOD. SUPPLEMENT - INSP BY MX FND NO SOURCE OF OIL LEAKAGE.(X) 2L72 4F A6WE 19950825004481995082500448WP 1995 8 25 CAL950515 119950621A3350 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912811 49265 FLT NR 0299 - EWR - INSPECTION FOUND THE INTERIOR EMERGENCY EXIT LIGHTS AT ROW 6-9 AND AT ENTRANCE TO COCKPIT DOOR INOPERATIVE. THE BATTERIES AT ROW 7 AND IN THE FORWARD OVERHEAD CEILING COMPARTMENT WERE REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19950825004491995082500449WP 1995 8 25 CAL950516 119950622A3350 EEL WIRING DOUG DC9 DC981 3022081WP CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0913881 48045 FLT NR 0323 - EWR - INSPECTION FOUND SEVERAL SECTIONS OF EMERGENCY AISLE PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND BROKEN WIRING AT SEVERAL LOCATIONS. THE WIRING WAS SPLICED AND A NEW HARNESS WAS INSTALLED AT REAR ENTRY DOOR. OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (M) 2L72 4F A6WE 19950825004501995082500450NM 1995 8 25 CAL950518 119950601A5320 PRESSURE PANEL BOEING737 737130 1384435NM NLG WW CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097721564951 19032 31J - THE NOSE WHEEL WELL PRESSURE BULKHEAD WAS FOUND WITH A CORROSION BULGE 1 INCH IN DIAMETER, AT THE AFT FORWARD OUTBOARD CORNER OF THE LEFT ACCESS PANEL BETWEEN THE SKIN AND INVERTED 'T'. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03128, REV IR. (M) 2L72 4F A16WE 19950825004511995082500451WP 1995 8 25 CAL950522 119950623A335060030451 EEL POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0993875 49125 FLT NR 0302 - DCA - OVERHEAD EMERGENCY LIGHTS ROW 28 AND 29 INOP. REPLACED POWER SUPPLY. OPERATION OF OVERHEAD LIGHTING RESTORED. (M) 2L72 4F A6WE 19950825004521995082500452NM 1995 8 25 CAL950523 119950624A3350 EEL SOCKET BOEING727 727227 1384078NM CABIN SHORTED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0976753 21249 FLT NR 0623 - EWR - LAST EIGHT ROWS, L2, R2 AND AFT AIRSTAIR EMERGENCY LIGHTS INOPERATIVE. TROUBLE SHOT TO AFT LEFT EXIT SIGN, REMOVED AND REPLACED SHORTED SOCKET ASSY. OPERATION OF THE EMERGENCY LIGHTING WAS RESTORED. (M) 2L73 4F A3WE 19950825004531995082500453WP 1995 8 25 CAL950525 119950626A2840 CIRCUIT BREAKER DOUG DC9 DC982 3022082WP RT AC BUS BROKEN A CALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0916802 49222 FLT NR 0611 - GSO - AIRCRAFT DIVERTED DUE TO INFLIGHT FAILURE OF THE FUEL QUANTITY INDICATION SYSTEM. FOUND RIGHT AC BUS B PHASE CIRCUIT BREAKER BROKEN AND POPPED. REPLACED CIRCUIT BREAKER. FUEL QUANTITY INDICATION RESTORED. (M) 2L72 4F A6WE 19950825004541995082500454NM 1995 8 25 CAL950527 119950628A2910 HYD LINE BOEING737 737222 1384473NM NLG WORN A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0910236 19937 FLT NR 1728 - CLE - THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IND. BOTH THE RED AND GREEN LIGHTS REMAINED ON. WHEN THE GEAR HANDLE WAS PLACED DOWN, THE RED LIGHT EXTINGUISHED. THE HYDRAULIC QUANTITY GAUGE DROPPED TO .8 GALS. THE AIRCRAFT WAS RETURNED TO IND WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE TO THE NOSE GEAR LOCK ACTUATOR WORN THROUGH. THE LINE WAS REMOVED AND REPLACED. OPERATIONAL AND LEAK CHECKS WERE GOOD. (M) 2L72 4F A16WE 19950825004551995082500455WP 1995 8 25 CAL950535 119950704A335060030431 EEL BATT CHARGER DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0971828 49488 FLT NR 0204 - EWR - THE EMERGENCY LIGHTS IN FIRST CLASS CEILING AND ROWS 28-29 CEILING WERE FOUND INOPERATIVE. THE BATTERY CHARGER FOR THE FIRST CLASS CEILING LIGHTS WAS REMOVED AND REPLACED. THE BATTERIES FOR THE CEILING LIGHTS AT ROWS 28-29 WERE REPLACED. OPERATION OF THE EMERGENCY CEILING LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19950825004561995082500456WP 1995 8 25 CAL950566 119950707A801297941011 STARTER VALVE DOUG DC9 DC983 3022083WP NR 2 ENGINE INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09938MC315322527 49525 FLT NR 0664 - LAS - THE RIGHT ENGINE START VALVE LIGHT CAME ON DURING CLIMB-OUT OF LAS AND WAS FOLLOWED SHORTLY AFTERWARDS BY THE RIGHT ENGINE FIRE WARNING ACTIVATING. THE RIGHT ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE RIGHT ENGINE START VALVE HAD FAILED OPEN WITH RESULTANT DAMAGE TO THE STARTER. THE STARTER VALVE AND STARTER WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2L72 4F RTA6WE 19950825004571995082500457WP 1995 8 25 CAL950592 119950712A3260 SWITCH DOUG DC9 DC932 3022066WP GEAR HANDLE STICKING A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW0933506 47765 FLT NR 1474 - IND - WHEN FLAPS WERE EXTENDED TO 25 DEGREES WITH GEAR EXTENDED AND THREE GREEN INDICATIONS, THE GEAR WARNING INDICATED GEAR NOT DOWN AND LOCKED ON APPROACH TO IND. THE FLAPS WERE PUT BACK TO FIVE DEGREES AND THE LANDING GEAR WAS CYCLED. WHEN THE FLAPS WERE EXTENDED BEYOND 15 DEGREES AGAIN, THE WARNING HORN SOUNDED. THE X33 CIRCUIT BREAKER WAS PULLED AFTER GEAR WAS CONFIRMED DOWN AND LOCKED. THEN WITH FLAPS AT 40 DEGREES, THE GROUND PROXIMITY WARNING SYSTEM ACTIVATED. THE LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE LANDING GEAR HANDLE SWITCH STICKING. THE SWITCH WAS CLEANED AND LUBRICATED. THE SWITCH WAS OPERATED SEVERAL TIMES AND ALL CHECKED GOOD PER MM 32-60-0. (M) 2L72 4F A6WE 19950825004581995082500458WP 1995 8 25 CAL950594 119950714A2612 FIRELOOP DOUG DC9 DC982 3022082WP LT ENGINE CHAFED A CALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW0933817 49371 FLT NR 0499 - IAH - THE LEFT ENGINE 'A' LOOP FIRE DETECTION LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO IAH. THE ENGINE WAS BROUGHT TO IDLE AND THE AIRCRAFT LANDED AT IAH. THE ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES WERE DISCHARGED AFTER LANDING. MX FOUND NO EVIDENCE OF FIRE. CHAFED WIRES WERE FOUND ON THE LEFT ENGINE FIRELOOP. THE WIRES WERE INSULATED AND SECURED. IN ADDITION, A PRBC LINE WAS FOUND LOOSE AND BLOWING ABOVE PYLON LOOP. THE PRBS LINE WAS SECURED. THE ENGINES WERE RUN AT TAKEOFF POWER FOR FIVE MINUTES AND NO DEFECTS WERE NOTED. BOTH ENGINE FIRE BOTTLES WERE REPLACED. (M) 2L72 4F A6WE 19950825004591995082500459WP 1995 8 25 CAL950598 119950715A3350EMBS1392 EEL BATT CHARGER DOUG DC10 DC1030 3023501WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW091406263010 47863 FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BATTERY CHARGER WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. (M) 2L73 4F A22WE 19950825004601995082500460WP 1995 8 25 CAL950599 119950715A3350EMSE299 EEL BATTERY DOUG DC10 DC1030 3023501WP L-1 DOOR DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09140621617711395 47863 FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BATTERY CHARGER WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. (M) 2L73 4F A22WE 19950825004611995082500461WP 1995 8 25 CAL950600 119950715A3350EMSE299 EEL BATTERY DOUG DC10 DC1030 3023501WP LT OVERWING DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09140621691 90 47863 FLT NR 0012 - LAX - THE EMERGENCY LIGHTS WOULD NOT TEST DURING A PREFLIGHT CHECK. MAINTENANCE FOUND THE L-1 DOOR AND LEFT OVERWING BATTERY PACKS INOPERATIVE. THE FORWARD CENTER BATTERY CHARGER WAS ALSO FOUND INOPERATIVE. BOTH OF THE BATTERY PACKS AND THE BATTERY CHARGER WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD. (M) 2L73 4F A22WE 19950825004621995082500462WP 1995 8 25 CAL950602 119950718A3260 SWITCH DOUG DC9 DC982 3022082WP LANDING GEAR INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW09478AC 48063 FLT NR 0603 - CLE - ALL LANDING GEAR RED LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE UP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO CLE, ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LEVER SWITCH AT FAULT. THE SWITCH WAS REMOVED AND REPLACED IAW MM 32-60-00, PAGE 201. OPERATION AND INDICATIONS CHECKED GOOD DURING GEAR SWING. (M) 2L72 4F A6WE 19950825004631995082500463WP 1995 8 25 CAL950603 119950718A3260MS250081 SWITCH DOUG DC9 DC982 3022082WP PEDESTAL INOPERATIVE A CALAO OTHER N FALSE WARNING CRCRUISE 1 SW0918835 49439 FLT NR 0117 - LAX - ALL THREE RED GEAR UNSAFE LIGHTS ILLUMINATED WHILE IN FLIGHT. THE GEAR WAS CYCLED, BUT THE LIGHTS DID NOT EXTINGUISH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE S1-319 LEFT THROTTLE SWITCH IN THE PEDESTAL AT FAULT. THE SWITCH WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD. (M) 2L72 4F A6WE 19950825004641995082500464NM 1995 8 25 CKSA95084 119950704A3260 CONNECTIONS BOEING727 727223 1384074NM LT MLG DIRTY A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL236816 71520 19491 CVG - ON GEAR RETRACTION WITH THE GEAR LEVER IN THE UP POSITION LEFT MAIN GEAR RED AND GREEN LIGHTS STAYED ON. ALL OTHER INDICATIONS WERE NORMAL. GEAR EXTENSION AND RETRACTION OPERATED NORMAL. CLEANED CONNECTIONS ON LANDING GEAR ACCESSORY UNIT. OPS CHECKED NORMAL IAW B727 MM CHAP 32-09-121. (M) 2L73 4F A3WE 19950825004651995082500465NM 1995 8 25 IXKA9500022 119950709A302065234941 DUCT BOEING727 727225 1384077NM NR 1 ENGINE BLOWN A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA258880Z 21453 FLT NR 10, MCO-EWR - AFTER TAKEOFF PASSING 10,000 FEET, LOWER AFT BDY OVERHEAT, NR 1 WING ANTI-ICE VALVE LIGHTS CAME ON, STANDBY LIGHTS ILLUMINATED. NR 1 WING BLEED VALVE, NR 1 PK VALVE AND LE VALVE CIRCUIT BREAKERS POPPED. NR 1 ENGINE SHUT DOWN PRECAUTIONARY. AIRCRAFT RETURNED TO MCO. REMOVED AND REPLACED BLOWN 13TH STAGE DUCT AND WING ANTI-ICE VALVE FROM NR 1 ENGINE, LEAK CHECK OK AS PER MM 30-10-00. FOUND WIRES, C/P'S DAMAGED TO FLW CONT MODULE S/O VALVES TO STANDBY PUMP AND TAI FOR WING SENSOR OUT NR 1 ENGINE REWIRED AND INSTALLED NEW C/P'S ON VALVES, PUMP SENSOR. OPS CHECK AND INSPECTED OK AS PER MM 72-10-01. (M) 2L73 4F A3WE 19950825004661995082500466EU 1995 8 25 JBXA950301 119950320A3246201072699 SPACER FOKKERF28 F28MK0100 4990807EU LT MLG MISSING A JBXAK NONE D INFLIGHT SEPARATION LDLANDING 1 GL31103ML4560 11444 UPON LANDING IN RDU IT WAS NOTED THAT THE R2 MAIN TIRE AND WHEEL ASSY WAS MISSING FROM THE AIRCRAFT. THE AXLE NUT WAS ATTACHED TO THE AXLE AND THE BRAKE ASSY WAS IN PLACE. DURING A TIRE CHANGE THE PREVIOUS NIGHT, THE SPACER HAD BEEN OMITTED DURING REINSTALLATION. 2L72 4F RT 19950825004671995082500467EU 1995 8 25 SIMA952043 119950723A33503011210 EEL AEROSPATR72 ATR72212 EU PAX DOOR DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21440AM 440 ORD - FLT NR 4021 - CREW REPORTS PASSENGERS EMERGENCY EXIT DOOR LIGHT INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004681995082500468EU 1995 8 25 SIMA952051 119950724A33503011151 EEL BATT PACK 3011180 AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21235RM 2928 235 MQT - DURING PS-2 CHECK, MAINTENANCE FOUND THE LEFT AND RIGHT AFT EMERGENCY EXIT, RIGHT AFT GROUND ILLUMINATION, AND THE 2ND, 4TH, AND 6TH EMERGENCY FLOOR LIGHTS REMAIN ON WITH SWITCH IN THE OFF POSITION. MAINTENANCE REMOVED AND REPLACED LIGHT BATTERY PACK. SYSTEM OPERATION CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004691995082500469EU 1995 8 25 SIMA952052 119950724A3350 EEL BULB SAAB SF340 340B 7860101EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21297AE 340B297 DFW - FLT NR 3531 - CREW REPORTS EMERGENCY EXIT SIGN P/N 2LA00593600M00, AT SEAT 8A HAS BULB OUT. MAINTENANCE REPLACED SIGN ASSEMBLY AND RELEASED AIRCRAFT FOR SERVICE. (M) 2L72 4T RTA52EU 19950825004701995082500470EU 1995 8 25 SIMA952062 119950725A3350 EEL WIRE AEROSPATR42 ATR42300 8680920EU PAX DOOR FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21423MQ 030 ORD - FLT NR 4339 - EMERGENCY STAIR LIGHT ON PASSENGER DOOR INOPERATIVE. REPAIRED WIRES ON PASSENGER DOOR. RETURNED AIRCRAFT TO SERVICE. (M) 2H72 4T RTA53EU 19950825004711995082500471NE 1995 8 25 SIMA952071 219950726A7530310848501 SWITCHING VALVE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LT ENG STICKING A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21266AT 266 121068 MKG - FLT NR 4108 - ELECTRICAL SMOKE LIGHT ILLUMINATED DURING TAXI. SMOKE SMELL WAS PRESENT IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. MAINTENANCE FOUND NR 1 ENG P.2.5/P.30 SWITCHING VALVE STUCK IN P3.0 POSITION. SWITCHING VALVE WAS REPLACED. SYSTEM OPERATIONS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19950825004721995082500472EU 1995 8 25 SIMA952081 119950727A7714MS9386112 O-RING PWA 3033509 AEROSPATR72 ATR72212 EU RT ENG NICKED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW21274AT 274 DFW - FLT 3542 - AFTER LANDING, DURING TAXI, AIRCRAFT CABIN FILLED WITH SMOKE. SMOKE ORIGINATED FROM MIDDLE OF CABIN. NO COCKPIT INDICATION. MAINTENANCE REMOVED AND REPLACED O-RING ON NL PROBE SYSTEM. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004731995082500473EU 1995 8 25 SIMA952091 119950728A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21423MQ 030 ORD - FLT 4258 - FLOOR PROXIMITY LIGHTS IN ROW 6 ARE INOPERATIVE. MAINTENANCE REMOVED AND INSTALLED BATTERY PACKS AT 3WL, 15WL, AND 18WL. SYSTEM OPERATIONS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004741995082500474EU 1995 8 25 SIMA952141 119950802A61303037785 PROP BRAKE AEROSPATR42 ATR42300 8680920EU RT ENG MELTED A SIMAFE ACTIVATE FIRE EXT. ENGINE SHUTDOWN A FLAME/FIRE TXTAXI/GRND HDL 1 SW21216AT7391 1266 283 216 ORD - FLT 4371 - DURING TAXI OUT FLT ATTENDANT REPORTED A FIRE FROM NR 2 ENGINE. BOTH ENGINES WERE SHUTDOWN, FIRE BOTTLES WERE DISCHARGED AND PASSENGERS WERE EVACUATED USING EMERGENCY PROCEDURES. MX FOUND PROP BRAKE SEIZED AND MELTED DOWN. PROP BRAKE WAS REMOVED AND REPLACED. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004751995082500475EU 1995 8 25 SIMA952142 119950802A3350852516R12B10PNF EEL CONNECTOR AEROSPATR72 ATR72212 EU PAX DOOR BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21369AT 369 DFW - CABIN DOOR, TOP STEP CONNECTOR HAS ALL WIRES PULL OUT WITH ASSOCIATED EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW CONNECTOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825004761995082500476NE 1995 8 25 UF6A950612 219950628A7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE RIGHT FAILED A UF6AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE03851AW5443 2020 SBN - FLT NR 5116 - NR 2 ENGINE LOW OIL PRESSURE LIGHT ON THE CWP ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED THE NR 2 ENGINE. (M) 2L72 4T4 TRTA27NM E2ONE 19950825004771995082500477EU 1995 8 25 UF6A950701 119950702A61207863364 PCU BAG ATP ATP EU LT ENG FAULTY A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 CE03858AW5619 ATPC0115 2035 ORD - FLT 5015 - LEFT PROP WOULD NOT FEATHER ON ENGINE SHUTDOWN. MAINTENANCE REPLACED THE PROP CONTROL UNIT. (M) 2L72 4T RTA27NM 19950825004781995082500478NE 1995 8 25 UF6A950702 219950710A7532311171202 BLEED VLV BAG ATP ATP EU PWA PW120 PW126A NE RT ENG FAILED A UF6AA UNSCHED LANDING O OTHER CLCLIMB 1 CE03852AW6295 2021 ORD - FLT NR 5029 - ON CLIMB-OUT, RIGHT ENGINE TORQUE DECREASED TO 78 PERCENT. MAINTENANCE REPLACED THE BLEED VALVE. (M) 2L72 4T4 TRTA27NM E2ONE 19950825004791995082500479 1995 8 25 USAA950758 419950717A344220412170416 RT UNIT BOEING737 737301 1384611NM FWD FUS INOPERATIVE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19356US 23559 CLT - FLT 0249 - RETURN TO FIELD DUE TO AN INOPERATIVE WEATHER RADAR. MAINTENANCE REPLACED THE RADAR R/T. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA16WE 19950825004801995082500480NM 1995 8 25 USAA950790 119950707A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCHES BY 18 INCHES TOTAL AREA OF SURFACE CORROSION FLOOR BEAM STATION 986.5 AT RBL 5 TO LBL 45. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. CUT OUT UPPER FLANGE OF ENTIRE LENGTH OF FLOOR BEAM AND INSTALLED NEW T-CAP. NOT MORE THAN ONE POUND ADDED WT FOR REPAIR. REPAIRED PER EA 39521. (M) 2L72 4F RTA16WE 19950825004811995082500481NM 1995 8 25 USAA950791 119950630A5320 ANGLE BOEING737 737401 1384701NM BS 727-787 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 727 TO BS 787 ABOVE S-26 R ON TRANSITION ANGLE. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. SPLICED IN NEW SECTION OF TRANSITION ANGLE. REPAIRED PER SRM 53-60-53. (M) 2L72 4F RTA16WE 19950825004821995082500482NM 1995 8 25 USAA950792 119950627A532065C34059U3 INTERCOSTAL BOEING737 737401 1384701NM BS 949 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA, BS 949, RBL 16 ON INTERCOSTAL. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REMOVED AND REPLACED CORRODED INTERCOSTAL WITH NEW IDENTICAL PART. REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19950825004831995082500483NM 1995 8 25 USAA950793 119950630A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 344 BL 0 TO LBL 10 ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. CUTOFF TOP OF FLOOR BEAM AND INSTALLED NEW 'T' CAP. REPAIRED PER TR 53-10-03. (M) 2L72 4F RTA16WE 19950825004841995082500484NM 1995 8 25 USAA950794 119950630A5320654583448 INTERCOSTAL BOEING737 737401 1384701NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION LB 11 BS 328 TO BS 344 ON INTERCOSTAL. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPAIRED PER SERM 51-10-2. (M) 2L72 4F RTA16WE 19950825004851995082500485NM 1995 8 25 USAA950795 119950705A5320 ANGLE BOEING737 7373B7 1384580NM BS 867-947.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU27298 23512 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 6 FOOT CORROSION BS 867 TO BS 947.5 ON TRANSITION ANGLE. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. REPLACED TRANSITION ANGLE, REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19950825004861995082500486NM 1995 8 25 USAA950796 119950706A532065C3184779 INTERCOSTAL BOEING737 737401 1384701NM BS 987 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH SQUARE TOTAL AREA, BETWEEN BS 967-987 RBL 16 ON INTERCOSTAL. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-03. (M) 2L72 4F RTA16WE 19950825004871995082500487NM 1995 8 25 USAA950797 119950706A53201124784 ANGLE BOEING737 737401 1384701NM BS 955 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 955 TO 995 LBL 50 ON Z-ANGLE. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED Z-ANGLE, REPAIRED PER SRM 51-10-02. (M) 2L72 4F RTA16WE 19950825004881995082500488NM 1995 8 25 USAA950798 119950627A53201137899 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 5 INCH TOTAL AREA OF SURFACE CORROSION STATION 947 TO 967, LBL 16 ON INTERCOSTAL. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REMOVED DEFECTIVE PART AND INSTALLED NEW. REPAIRED PER SRM 51-10-02. (M) 2L72 4F RTA16WE 19950825004891995082500489NM 1995 8 25 USAA950799 119950630A5320 SILL BOEING737 737401 1384701NM SERVICE DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 40 INCH AREA OF SURFACE CORROSION FORWARD SERVICE DOOR SILL 'Z' ANGLE. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REMOVED CORRODED 'Z' ANGLE REPLACED 'Z' ANGLE. REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19950825004901995082500490NE 1995 8 25 WRLA95039 219950802A7412106216301 EXCITER UNIT DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE NR 1 ENGINE FAILED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27275WA 48631 DURNG TAXI, CREW EXPERIENCED A NR 1 ENGINE 'A' IGNITION FAILURE. CAPTAIN ELECTED TO RETURN TO GATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED ENGINE NR 1 IGNITION 'A' EXCITER UNIT. RTS CHECK PERFORMED, NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F4 FRTA22WE E24NE 19950825004911995082500491NM 1995 8 25 95ZZZM301 119950719A28207G1106 SWITCH BOEING737 737301 1384611NM RIGHT FAILED A USAAA UNSCHED LANDING O OTHER APAPPROACH 1 EA19585US 23930 MCO - FLT NR 0119 - AIRCRAFT DIVERTED DUE TO THE CENTER TANK FUEL PUMP FAILING. MAINTENANCE REPLACED THE CENTER BOOST PUMP AND RIGHT PRESSURE SWITCH. OPERATIONS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19950825004921995082500492NM 1995 8 25 AALA951257 119950712A5754 SKIN BOEING767 767323 1385205NM NR 4 SLAT DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07372AA 25199 AFW - FOUND NR 4 SLAT HAS A GOUGE WORN INTO LOWER SKIN SURFACE. DYE PENETRANT CHECKED, TAP TESTED AND RESTORED SURFACE FINISH PER ENGINEERING MRB 767-976. (M) 2L72 4F RTA1NM 19950825004931995082500493NM 1995 8 25 AALA951261 119950714A5311146T1207 FRAME BOEING767 767223 1385123NM BS 1219 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07320AA 22321 AFW - FOUND WEB OF FRAME AT STATION 1219 BL 0 CRACKED. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER FROM 0.032 7075-T6 ALUMINUM AND INSTALLED WET WITH BMS5-95 SEALANT, ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB 767-972. (M) 2L72 4F RTA1NM 19950825004941995082500494NM 1995 8 25 AALA951262 119950714A5414311T1450 SKIN BOEING767 767223 1385123NM LT PYLON WORN A AALAK NONE O OTHER ININSP/MAINT 1 SW07320AA 22321 AFW - FOUND A GROOVE WORN IN THE LEFT PYLON INBOARD AND OUTBOARD SIDE SKINS. BOTH GROOVES WERE CAUSED BY AN ANGLE ON THE THRUST REVERSER RUBBING ON THE SIDE SKINS. BLENDED AND REFINISHED GROOVES. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-975. (M) 2L72 4F RTA1NM 19950825004951995082500495NM 1995 8 25 AALA951264 119950714A5315 FLOOR BEAM BOEING767 767223 1385123NM BS 266 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07320AA 22321 AFW - FOUND FLOOR BEAM CORROSION, REMOVAL BEYOND SRM LIMITS. ALODINE BLENDED AREA. FILL BLEND OUT WITH BMS-592. FABRICATE A REPAIR STRAP FROM .050 301 HALF HARD STAINLESS AND INSTALL WET PER ENGINEERING MRB 767-970. 2L72 4F RTA1NM 19950825004961995082500496NM 1995 8 25 AALA951266 119950714A5320146T63291 CORNER BOEING767 767223 1385123NM CARGO DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07320AA 22321 AFW - FOUND CORROSION AROUND A NUT PLATE HOLE IN THE INNER FLANGE OF THE LOWER FORWARD CORNER PIECE OF THE BULK CARGO DOOR. FOUND BEYOND SRM LIMITS AFTER BLENDING. TREATED, PRIMED AND PAINTED AREA. REINSTALLED NUT PLATE, APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-974. (M) 2L72 4F RTA1NM 19950825004971995082500497NM 1995 8 25 AALA951274 119950718A5330 SKIN BOEING727 727227 1384078NM BS 535-540 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TUL - STRINGER 26L, RIVETS PULLING, 1 INCH CRACK AT STATION 535 TO 540. REPAIRED PER SRM 53-30-3 PGS 76-80. (M) 2L73 4F A3WE 19950825004981995082500498NM 1995 8 25 AALA951275 119950718A5510652298772 BEAM BOEING727 727227 1384078NM RT HORIZ STAB TECORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION ON RT TRAILING EDGE HORIZONTAL STABILIZER BEAM. REPLACED TRAILING EDGE BEAM TOP OF HORIZONTAL STABILIZER, RT TRAILING EDGE. (M) 2L73 4F A3WE 19950825004991995082500499NM 1995 8 25 AALA951276 119950718A5347 SEAT TRACK BOEING727 727227 1384078NM BS 1063-1070 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION ON SEAT/GALLEY TIE DOWN TRACK, STATION 1063-1070, LEFT INBOARD SIDE. INSTALLED NEW TRACK PER SRM 53-10-5. (M) 2L73 4F A3WE 19950825005001995082500500NM 1995 8 25 AALA951277 119950718A5320 SPLICE BOEING727 727227 1384078NM BS 675 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION LEFT STRINGER 27L, STATION 675. REPLACED STRINGER SPLICE PER SRM 51-10-1 PG 4. (M) 2L73 4F A3WE 19950825005011995082500501NM 1995 8 25 AALA951278 119950613A5347 SEAT TRACK BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - THE OUTER HORIZONTAL FLANGE OF SEAT TRACK CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REFINISHED BLENDED AREA PER SRM 53-00-52 FIG 101. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-949. (M) 2L72 4F RTA1NM 19950825005021995082500502NM 1995 8 25 AALA951280 119950612A5315 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07330AA 22330 AFW - FLOOR BEAM AT STATION 347 RBL 48 TO RBL 78 HAS CORRODED BEYOND SRM LIMITS. BLENDED OUT CORROSION, ALODINED BLENDED AREAS. FILLED WITH BMS 5-92. FABRICATED STAINLESS STRAP. PRIMER COATED AND INSTALLED REPAIR STRAP WET. (M) 2L72 4F RTA1NM 19950825005031995082500503NM 1995 8 25 AALA951282 119950724A5330 SKIN BOEING727 727227 1384078NM BS 682-684 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION ON FUSELAGE SKIN, BEYOND LIMITS, STATION 682-684 BL 6 INCHES L TO 8 INCHES L. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3. (M) 2L73 4F A3WE 19950825005041995082500504NM 1995 8 25 AALA951283 119950724A5720 DOUBLER BOEING727 727227 1384078NM RT WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION ON RT PRIMARY HEAT EXCHANGER PLENUM DOUBLER. INSTALLED DOUBLER PER SRM 57-30-3 FIG 10. (M) 2L73 4F A3WE 19950825005051995082500505NM 1995 8 25 AALA951284 119950724A5320 RIVETS BOEING727 727227 1384078NM BS 300-328 FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND SKIN LAP 24R RIVETS PULLING, 1 HEAD SHEARED STATION 300-328. REMOVED CORRODED SKIN LAP. INSTALLED DOUBLER PER SRM 53-30-3 PG 76 THROUGH 80B. (M) 2L73 4F A3WE 19950825005061995082500506NM 1995 8 25 AALA951285 119950724A5330 SKIN BOEING727 727227 1384078NM BS 350-360 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND CORROSION IN SKIN LAP, RIVETS PULLING. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 35-30-3 PG 80A. (M) 2L73 4F A3WE 19950825005071995082500507NM 1995 8 25 AALA951286 119950724A5320 STRAP BOEING727 727227 1384078NM BS 720 DISBONDED A AALAK NONE O OTHER ININSP/MAINT 1 SW07716AA 20608 TULE - FOUND BONDED STRAP DISBONDED AT 720C BL 0. REPAIRED STRAP PER SRM 51-40-2, PG 1-6. REPAIRED SKIN PER SRM 53-30-3 PG 8. (M) 2L73 4F A3WE 19950825005081995082500508WP 1995 8 25 AALA951294 119950722A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07410AA 49321 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY ILLUMINATED. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950825005091995082500509NM 1995 8 25 AALA951325 119950722A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07370AA 25197 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT PATH LIGHTS AT SEAT 17B INOPERATIVE. RECONNECTED CONNECTOR AT SEAT 17B TO FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825005101995082500510WP 1995 8 25 AALA951326 119950723A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN MIS INSTALLED A AALAK NONE LN NO TEST FALSE WARNING ININSP/MAINT 1 SW07290AA 49302 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM OVERWING EXIT TO FORWARD GALLEY CYCLING ON AND OFF. REVERSED POLARITY IN EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19950825005111995082500511NM 1995 8 25 AALA951327 119950723A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07322AA 22323 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 35H AND INOPERATIVE. REPLACED PINS ON SEAT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825005121995082500512WP 1995 8 25 AALA951328 119950723A3350A3060698101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07154AA 46709 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS ON RIGHT BUSINESS SECTION OF CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR ON RIGHT SIDE OF BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19950825005131995082500513NM 1995 8 25 AALA951329 119950723A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT 9-12AB, 25-31AB, AND 7-12HJ INOPERATIVE. RESECURED CONNECTORS AT SAME LOCATIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825005141995082500514NM 1995 8 25 AALA951333 119950725A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM 8B TO 12B INOPERATIVE. RECONNECTED CONNECTOR AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825005151995082500515EU 1995 8 25 AALA951334 119950725A3350 EEL HARNESS AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077082A 643 JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS FROM SEAT 13AB TO 20AB INOPERATIVE. REPLACED CONNECTING HARNESS BETWEEN WALL PLUGS AND TRACK LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950825005161995082500516NM 1995 8 25 AALA951335 119950725A3350 EEL WIRE DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071758B 48527 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AFT OF R2 DOOR INOPERATIVE. INSTALLED NEW WIRING BETWEEN R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19950825005171995082500517NM 1995 8 25 AALA951336 119950726A2530 CART BOEING767 767223 1385123NM GALLEY DEFECTIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07330AA 22330 LHR - FLT NR 0116 - AFTER TAKEOFF AN ACRID ODOR WAS REPORTED IN THE MID GALLEY AREA ACCOMPANIED BY A TRACE OF SMOKE. SECURED GALLEY POWER AND ODOR DISSIPATED ALONG WITH SMOKE. LANDED LHR WITHOUT INCIDENT. REPLACED WARMING CART, NO ODOR OR SMOKE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950825005181995082500518NM 1995 8 25 USAA950749 119950705A3350900835A EEL BATT PACK BOEING737 7372B7 1384560NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19287AU 23134 CLE - INTERIOR OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED BATTERY PACK AND CHARGER ASSEMBLY. (M) 2L72 4F A16WE 19950825005191995082500519NM 1995 8 25 USAA950759 119950720A3260 CIRCUIT BREAKER BOEING737 7374B7 1384702NM LANDING GEAR FAILED A USAAO OTHER N FALSE WARNING DEDESCENT 1 EA19429US 24551 LGA - FLT 2235 - THE 'NOSE GEAR UNSAFE' LIGHT ILLUMINATED WHEN THE POWER WAS BROUGHT TO IDLE. VISUALLY VERIFIED GEAR POSITION AND PERFORMED TOWER FLYBY. FLIGHT CREW FOUND AIR/GRD RELAY AND LANDING GEAR LIGHTS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. INDICATION WAS NORMAL. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CIRCUIT BREAKER. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA16WE 19950825005201995082500520NM 1995 8 25 USAA950761 119950719A2822568126713005 PUMP BOEING737 737301 1384611NM LEFT FAILED A USAAA UNSCHED LANDING O OTHER APAPPROACH 1 EA19585US 23930 MCO - FLT NR 0119 - AIRCRAFT DIVERTED DUE TO THE CENTER TANK FUEL PUMP FAILING. MAINTENANCE REPLACED THE CENTER BOOST PUMP AND RIGHT PRESSURE SWITCH. OPERATIONS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19950825005211995082500521NE 1995 8 25 USAA950764 219950722A7261 FILTERS BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE CLOGGED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA19528AU 24410 SFO - FLT NR 1426 - CREW RECEIVED AN OIL FILTER BYPASS LIGHT ON THE NR 2 ENGINE. THE CAPTAIN PULLED THE RIGHT ENGINE BACK TO IDLE WITH NO RESULT. FLIGHT CREW SHUTDOWN THE NR 2 ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FORWARD SCAVENGE MCD SCREEN CLOGGED. THE SCREEN WAS CLEANED. THE MAIN ENGINE OIL PRESSURE AND SCAVENGE FILTERS WERE REPLACED. OPERATIONS AND LEAK CHECKED GOOD. (M) 2L72 4F4 FRTA16WE E2GL 19950825005221995082500522NM 1995 8 25 USAA950767 119950718A2761654456115 ACTUATOR BOEING737 737201 1384454NM NR 6 SPOILER LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19247US 22754 BOS - FLT NR 0284 - ON TAKEOFF, THE MASTER CAUTION LIGHT ILLUMINATED. THE HYDRAULIC SYSTEM 'A' PRESSURE WAS FLUCTUATING ABOVE ZERO, AND THE HYDRAULIC SYSTEM 'A' QUANTITY REACHED ZERO. FLIGHT RETURNED TO BOS. MAINTENANCE REPLACED THE NR 6 SPOILER ACTUATOR DUE TO LEAKAGE. OPERATIONS CHECKED GOOD. (M) 2L72 4F A16WE 19950825005231995082500523NM 1995 8 25 USAA950774 119950707A2131 CONTROLLER BOEING737 7373B7 1384580NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19517AU 23703 CLT - FLT 0549 - THE CAPTAIN REPORTED PRESSURIZATION FAILURE. THE FLIGHT RETURNED TO CLT. MAINTENANCE PRESSURIZED THE AIRCRAFT TO 6 PSID. NO LEAKS WERE NOTED. THE PRESSURIZATION CONTROLLER WAS REPLACED AS A PRECAUTION. (M) 2L72 4F RTA16WE 19950825005241995082500524EU 1995 8 25 USAA950775 119950728A3231 LOCK FOKKERF28 F28MK0100 4990807EU LT MLG DOOR BROKEN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19860US 11295 MSP - FLT 0232 - THE LEFT LANDING GEAR DOOR DID NOT LOCK UPON GEAR RETRACTION. THE GEAR WAS CYCLED TWICE BUT THE LIGHT WOULD NOT EXTINGUISH. MAINTENANCE INSTALLED A NEW DOOR LOCK ON THE LEFT GEAR DOOR. OPERATIONS CHECKED GOOD. (M) 2L72 4F RT 19950825005251995082500525 1995 8 25 USAA950777 419950801A34426225132108 RADAR TR UNIT BOEING737 7373B7 1384580NM FWD FUS FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19532AU 24479 CLT - FLT 1409 - FLIGHT EXPERIENCED RADAR FAILURE DURING CLIMB-OUT. THE FLIGHT RETURNED TO CLT. MAINTENANCE REPLACED THE RADAR R/T. OPERATIONS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19950825005261995082500526NM 1995 8 25 USAA950779 119950728A3350 EEL BATT PACK BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 BOS - THE EMERGENCY FLOOR LIGHTING FAILED. MAINTENANCE RELAMPED SEVERAL LIGHTS AND REPLACED TWO BATTERY PACKS. OPERATIONS TESTED GOOD. (M) 2L72 4F RTA1NM 19950825005271995082500527NM 1995 8 25 USAA950780 119950731A2910 HYD LINE BOEING757 757225 1384959NM RT MLG LEAKING A USAAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA19608AU 22204 LAX - FLT 0412 - AT 23,000 FEET, THE LEFT HYDRAULIC QUANTITY LIGHT ILLUMINATED. THE CAPTAIN DECLARED AN EQUIPMENT EMERGENCY WHEN IN RANGE OF LAX. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DOWNLOCK ACTUATOR PRESSURE LINE ON THE RIGHT GEAR. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA2NM 19950825005281995082500528NM 1995 8 25 USAA950784 119950802A2780 FLAP CONTROL BOEING757 757225 1384959NM LE FLAPS MALFUNCTIONED A USAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 EA19609AU 22205 DCA - FLT 0450 - THE CREW HAD DECLARED AND EMERGENCY DUE TO A LE FLAP ASYMMETRY PROBLEM. (M) 2L72 4F RTA2NM 19950825005291995082500529NM 1995 8 25 USAA950788 119950705A5320 STRAP BOEING737 7373B7 1384580NM BS 860 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU27298 23512 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 3 INCH CORROSION ON STRAP AT BS 860. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. REPLACED STRAP, REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19950825005301995082500530NM 1995 8 25 USAA950789 119950706A532065C3184779 INTERCOSTAL BOEING737 737401 1384701NM BS 967-987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US19660 23885 INT - DURING Q-3 CHECK VISUAL, FOUND CORROSION 1 INCH TOTAL AREA BETWEEN BS 967-987 LBL 16 ON INTERCOSTAL. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-3. (M) 2L72 4F RTA16WE 19950825005311995082500531WP 1995 8 25 95ZZZM302 119950719A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-11 AND 20-22. REPLACED BATTERY PACK AT ROWS 9-11 AND BATTERIES AT ROWS 20-22. LIGHTS OPERATED NORMALLY. 2L72 4F RTA6WE 19950825005321995082500532NM 1995 8 25 95ZZZM303 119950731A3260806002 UPLOCK CARD BOEING737 7373G7 1384595NM LT MLG MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 23782 MDW-LAS - FLT 403 - DURING CLIMB THE LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED WITH THE HANDLE IN THE UP POSITION. HANDLE WAS RECYCLED WITH THE SAME RESULT. CREW ELECTED TO RETURN TO MDW AND LANDED WITHOUT FURTHER INCIDENT. OVERWEIGHT INSPECTION WAS NOT REQUIRED. MAINTENANCE REPLACED THE LT UPLOCK SENSOR AND UPLOCK GEAR CARD. OPS TEST NORMAL PER BMM 32-61-00, PAGE 107. 2L72 4F RTA16WE 19950825005331995082500533NM 1995 8 25 95ZZZM304 119950726A2133322684003 OUTFLOW VLV BOEING737 7372E3 NM CABIN MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28138AW 04810002 22792 PHX-LAX - FLT 15 - ON CLIMB-OUT AIRCRAFT LOST RT PACK, CREW WAS UNABLE TO PRESSURIZE CABIN. LEFT PACK WAS ON MEL. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER PROBLEMS. MAINTENANCE REPLACED FWD OUTFLOW VALVE AND E/E COOLING EXHAUST VALVE PER MM 21-58-31, PAGE 401. PRESSURIZED AND TESTED PER MM 5-51-91, CHECK 5. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA16WE 19950825005351995082500535NM 1995 8 25 ASAA9510071 119950718A335086210144 EEL BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE BULKHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950825005361995082500536NM 1995 8 25 ASAA9510072 119950730A33508731002142 EEL ASSY BOEING737 737290C 138448VNM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER 'EXIT TO REAR' LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F A16WE 19950825005371995082500537WP 1995 8 25 ASAA9580163 119950719A335060030431 EEL BATT PACK DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 9-11 AND 20-22. REPLACED BATTERY PACK AT ROWS 9-11 AND BATTERIES AT ROWS 20-22. LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005381995082500538WP 1995 8 25 ASAA9580164 119950720A33501001191 EEL ASSY DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01945AS 49643 LAX - DURING MAINTENANCE CHECK, THE L-1 PORTABLE EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005391995082500539WP 1995 8 25 ASAA9580165 119950720A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19-22. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005401995082500540WP 1995 8 25 ASAA9580166 119950720A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19-22 AND ADJACENT TO AFT GALLEY. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950825005411995082500541WP 1995 8 25 ASAA9580167 119950721A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01958AS 53024 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGNCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROWS 19-22. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005421995082500542WP 1995 8 25 ASAA9580168 119950723A33506011779 EEL PWR SUPPLY DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01963AS 53077 LAX - DURING MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005431995082500543WP 1995 8 25 ASAA9580171 119950730A33501001191 PORTABLE EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01965AS7095 53079 SFO - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950825005441995082500544NM 1995 8 25 AWXA9500290 119950515A2150PN56697 VLV BOEING737 7373Y0 1384671NM E/E COOLING INOPERATIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP282FOR 4181 23747 PHX-SNA - FLT 661 - AIR TURNBACK, CREW UNABLE TO PRESSURIZE AIRCRAFT ON CLIMB-OUT. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED E/E COOLING VLV. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950825005451995082500545NM 1995 8 25 AWXA9500465 119950726A215028420 COOLING EXH VLV BOEING737 7372E3 NM E/E COMPT MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28138AW 6 22792 PHX-LAX - FLT 15 - ON CLIMB-OUT AIRCRAFT LOST RT PACK, CREW WAS UNABLE TO PRESSURIZE CABIN. LEFT PACK WAS ON MEL. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER PROBLEMS. MAINTENANCE REPLACED FWD OUTFLOW VALVE AND E/E COOLING EXHAUST VALVE PER MM 21-58-31, PAGE 401. PRESSURIZED AND TESTED PER MM 5-51-91, CHECK 5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950825005461995082500546EU 1995 8 25 AWXA9500466 119950726A326021891241 PROX SENSOR AIRBUS320 A320231 3930325EU NLG FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28635AW 092 PHX-SEA - FLT 840 - DURING TAKEOFF, THE NOSE GEAR DOORS DID NOT COME UP. GEAR WAS CYCLED AND APPEARED UP AND LOCKED. AFTER GEAR AND DOORS WERE UP AND LOCKED, LANDING GEAR DISAGREE AND LANDING CONTROL ECAM MESSAGE APPEARED. FWD PANEL HAD RED CENTER, UNSAFE TRIANGLE ILLUMINATED. AIRCRAFT RETURNED TO PHX, LANDING UNEVENTFULLY. MAINTENANCE FOUND NOSE LANDING GEAR SENSOR 13GA TO BE FAULTED. REMOVED AND REPLACED SENSOR 13GA. OPERATIONAL CHECK GOOD ON GROUND PER AMM 32-31-00, PAGE 509/519. NO FAULTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19950825005471995082500547NM 1995 8 25 AWXA9500467 119950719A5230 SKIN BOEING737 73733A 1384673NM AFT CARGO DOOR DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND AFT CARGO DOOR DENTED AT MIDDLE OF DOOR OUTER SKIN. INSTALLED REPAIR DOUBLE PER SRM 52-00-01. (M) 2L72 4F RTA16WE 19950825005481995082500548NM 1995 8 25 AWXA9500468 119950719A321065461409 TEE BOLT BOEING737 73733A 1384673NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND LEFT MAIN LANDING GEAR DRAG STRUT TEE BOLT CORRODED. REPLACED TEE BOLT PER OHM 32-16-01. (M) 2L72 4F RTA16WE 19950825005491995082500549NM 1995 8 25 AWXA9500469 119950719A321065461067 BRACE ASSY BOEING737 73733A 1384673NM RT MLG WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND RT MAIN STRUT, LOWER SIDE BRACE UNIVERSAL ASSY WORN AT ATTACH BOLT BUSHING. REMOVED AND REPLACED LOWER SIDE OF UNIVERSAL BRACE ASSY PER OHM 32-16-1. (M) 2L72 4F RTA16WE 19950825005501995082500550NM 1995 8 25 AWXA9500470 119950719A321065461409 TEE BOLT BOEING737 73733A 1384673NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 17981 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND RT MAIN LANDING GEAR DRAG STRUT TEE BOLT CORRODED, AND BUSHING SURFACE CHIPPED. REPLACED TEE BOLT PER OHM 32-16-01. (M) 2L72 4F RTA16WE 19950825005511995082500551NM 1995 8 25 AWXA9500471 119950719A321165633789 TRUNNION LINK BOEING737 73733A 1384673NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 3228 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND RT MAIN LANDING GEAR TRUNNION LINK CORRODED ON LUG FACES. REPLACED TRUNNION LINK PER AWA TASK CARD 4M32018. (M) 2L72 4F RTA16WE 19950825005521995082500552NM 1995 8 25 AWXA9500472 119950719A3211654611317 TRUNNION PIN BOEING737 73733A 1384673NM RT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW AGM790 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND RT MAIN LANDING GEAR TRUNNION LINK PIN CORRODED ON BEARING SURFACE AND THREADS. REPLACED TRUNNION LINK PIN PER AWA TASK CARD R4M32018. (M) 2L72 4F RTA16WE 19950825005531995082500553NM 1995 8 25 AWXA9500473 119950719A3211656337811 TRUNNION LINK BOEING737 73733A 1384673NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW 3715 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND LEFT MAIN LANDING GEAR TRUNNION LINK CORRODED ON BEARING FACE AND SURFACE. REPLACED TRUNNION LINK PER AWA TASK CARD R4M32018. (M) 2L72 4F RTA16WE 19950825005541995082500554NM 1995 8 25 AWXA9500474 119950719A3211654611321 TRUNNION PIN BOEING737 73733A 1384673NM LT MLG CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28175AW A1151 23634 PHX - DURING SCHEDULED C11 INSPECTION, FOUND LEFT MAIN LANDING GEAR TRUNNION PIN CORRODED. REPLACED TRUNNION PIN PER AWA TASK CARD R4M32018. (M) 2L72 4F RTA16WE 19950825005551995082500555NM 1995 8 25 AWXA9500476 119950717A5320 DOOR STOP BOEING737 737277 1384570NM R2 DOOR CUTOUT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND R1 DOOR STOP LUG CUTOUT CRACKED. ROUTED OUT CRACK AND INSTALLED REPAIR DOUBLER PER ER 3-52-10-10. (M) 2L72 4F RTA16WE 19950825005561995082500556NM 1995 8 25 AWXA9500477 119950717A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND FLOOR BEAM CORRODED AT SCREW HOLES, STATION 312, BLO 0 TO RBL 6. REPLACED SECTION OF FLOOR BEAM PER SRM 53-10-9, FIG 5. (M) 2L72 4F RTA16WE 19950825005571995082500557NM 1995 8 25 AWXA9500478 119950717A5320 THRESHOLD BOEING737 737277 1384570NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND L1 DOOR THRESHOLD CHORD FASTENER HOLES CORRODED. REMOVED AND REPLACED L1 DOOR THRESHOLD CHORD PER SRM 51-10-1 AND 51-30-2. (M) 2L72 4F RTA16WE 19950825005581995082500558NM 1995 8 25 AWXA9500479 119950717A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND FLOOR BEAM AT BS 328 RBL 45 CORRODED ON UPPER CHORD. INSTALLED REPAIR ANGLE PER SRM 51-40-4, FIG 2. (M) 2L72 4F RTA16WE 19950825005591995082500559NM 1995 8 25 AWXA9500480 119950717A5320 THRESHOLD BOEING737 737277 1384570NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND R2 DOOR THRESHOLD INNER CHORD CORRODED IN SEVERAL PLACES BETWEEN BS 967 AND 986.5. REMOVED CORROSION PER SRM 51-10-6, FOUND AREA PREVIOUSLY REPAIRED. REINSTALLED REPAIR ANGLE PER SRM 51-40-4. (M) 2L72 4F RTA16WE 19950825005601995082500560NM 1995 8 25 AWXA9500481 119950717A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 267-294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - DURING SCHEDULED C7 INSPECTION, FOUND FLOOR BEAM CORRODED AT STATION 294 RBL 45. REMOVED AND REPLACED FLOOR BEAM 'T' CAP FROM RBL 24 TO RBL 48, STATION 267 TO STATION 294 PER SRM 51-10-1, SRM 51-30-2 AND SRM 51-40-4. (M) 2L72 4F RTA16WE 19950825005611995082500561NM 1995 8 25 AWXA9500483 119950728A5315 FLOOR BEAM BOEING737 737275 1384485NM BS 1016 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP282FOR 20958 PHX - DURING SCHEDULED C8 INSPECTION, FOUND MAIN FLOOR BEAM AT STATION 1016 BL 0 CORRODED BEYOND LIMITS. INSTALLED REPAIR ANGLE AND REPAIRED PER SRM 51-40-4, FIGURE 1. (M) 2L72 4F A16WE 19950825005621995082500562NM 1995 8 25 AWXA9500487 119950731A3260106122629 UPLOCK SENSOR BOEING737 7373G7 1384595NM LT MLG FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 23782 MDW-LAS - FLT 403 - DURING CLIMB THE LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED WITH THE HANDLE IN THE UP POSITION. HANDLE WAS RECYCLED WITH THE SAME RESULT. CREW ELECTED TO RETURN TO MDW AND LANDED WITHOUT FURTHER INCIDENT. OVERWEIGHT INSPECTION WAS NOT REQUIRED. MAINTENANCE REPLACED THE LT UPLOCK SENSOR AND UPLOCK GEAR CARD. OPS TEST NORMAL PER BMM 32-61-00, PAGE 107. (M) 2L72 4F RTA16WE 19950825005631995082500563 1995 8 25 C2XA95CL109 419950608A3442MI585353 RADAR PEDESTAL AEROSPATR42 ATR42320 8680930EU NOSE FAILED A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW09148197610 1015 156 FLT NR 3650 - EWR - WEATHER RADAR FAILED ON CLIMB-OUT. AIRCRAFT RETURNED TO EWR. MAINTENACNE REMOVED AND REPLACED WEATHER RADAR PEDESTAL IAW ATR JIC 344111. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950825005641995082500564SO 1995 8 25 C2XA95IA148 119950729A553012015734002 DRAG ANGLE EMB 120 EMB120RT SO VERT STAB CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917728 120182 IAH - DURING A SCHEDULED MAINTENANCE CHECK, THE RIGHT DRAG ANGLE, ON THE VERTICAL STABILIZER, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005651995082500565SO 1995 8 25 C2XA95IA149 119950731A534712026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005661995082500566SO 1995 8 25 C2XA95IA150 119950731A534712026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005671995082500567SO 1995 8 25 C2XA95IA151 119950802A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005681995082500568SO 1995 8 25 C2XA95IA152 119950802A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005691995082500569SO 1995 8 25 C2XA95IA153 119950802A572012017056013 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950825005701995082500570NM 1995 8 25 TAOA079502 119950713A2611824PY SMOKE DETECTOR BOEING727 727225 1384077NM FWD LAV MALFUNCTIONED A TAOAK NONE N FALSE WARNING ININSP/MAINT 1 EA15923TS 065A 20441 FORWARD LAVATORY SMOKE DETECTOR WILL NOT SHUT OFF. REPLACED FORWARD LAVATORY SMOKE DETECTOR. OPS CHECKED OK. (M) 2L73 4F A3WE 19950825005901995082500590NM 1995 8 25 95ZZZX4280 119950714A335007912 EEL SOCKET BRUCE BR20137372GFBOEING737 7372P6 NM CABIN INOP A A6XAK NONE L NO TEST ININSP/MAINT 1 SO132FOR 21612 DURING INSPECTION, FOUND THE EMERGENCY PASSENGER LIGHTING SYSTEM WHITE LIGHT INOP BETWEEN ROWS 1 AND 2. BAD SOCKET WAS FOUND AND REPLACED. OPS CHECKED GOOD. 2L72 4F RTA16WE 19950825005921995082500592NM 1995 8 25 95ZZZX4282 119950720A335008163023410 EEL COVER BRUCE BR2013737GG BOEING737 7372P6 NM FORWARD MISSING A A6XAK NONE O OTHER ININSP/MAINT 1 SO132FOR 21677 DURING AN INSPECTION, THE EMERGENCY FLOOR LIGHTING AT FORWARD GALLEY WAS MISSING APPROXIMATELY A 10 INCH STRIP PLASTIC COVER DUE TO PASSENGER STEPPING ON IT. INSTALLED AND SECURED FLOOR STRIP. FLOOR LIGHT OPS CHECKED GOOD PER M/M 33. 2L72 4F RTA16WE 19950825006271995082500627NE 1995 8 25 9512692294 219950818A7321 FUEL CONTROL BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01294US 21505 700272 NR 2 ENGINE HAD A LOW FREQUENCY VIBRATION AT POWER SETTING ABOVE 65 PERCENT N2. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. THE ENGINE WAS INSPECTED AND BORESCOPED, NO DISCREPANCIES NOTED. MAINTENANCE REPLACED THE FUEL CONTROL UNIT RESTRICTOR TUBE WITH A SERVICEABLE UNIT. THE ENGINE WAS RUN UP AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. CORRECTED COPY: CHANGED A/C TT AND A/C TC. 2L73 4F4 F A3WE E2EA 19950825006281995082500628NM 1995 8 25 9512786716 119950822A5320 SUPPORT BOEING747 747251F 1384898NM CARGO DOOR LATCHCRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01616US 21120 DURING PERIODIC CHECK, THE LEFT AND RIGHT NOSE CARGO DOOR PORTAL LATCH NR 4 SUPPORT FITTING AT LBL 70 AND RBL 70 WERE FOUND CRACKED. THE (P/N 65B13044-3), 4 SUPPORT FITTINGS WERE FOUND WITH A CRACK THROUGH THE VERTICAL AND HORIZONTAL FLANGES, MADE REPAIR PER EA 67-51752. 2L74 4F A20WE 19950825006291995082500629EU 1995 8 25 9512793215 119950820A3830D3817101000000 WATER LINE AIRBUS320 A320211 3930320EU AFT RIGHT LAV RUPTURED A NWAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01315US 171 DURING CLIMBOUT FROM MIA, THE RIGHT AFT LAVATORY DEVELOPED AN UNCONTROLLABLE WATER LEAK. AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AFT RIGHT LAV WATER SUPPLY LINE. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950825006301995082500630EU 1995 8 25 9512803240 119950820A2421740119E IDG AIRBUS320 A320211 3930320EU NR 2 ENGINE OVERHEAT A NWAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 GL01340NW138843571 372 DURING CRUISE, THE NR 2 ENGINE IDG TEMPERATURE INCREASED TO 183 DEGREES CELCIUS. DISCONNECTED NR 2 IDG AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG AND IDG OIL COOLER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950825006311995082500631EU 1995 8 25 9512813246 119950819A2920 B-NUT AIRBUS320 A320211 3930320EU YELLOW HYD SYS LOOSE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL01346NW 400 DURING TAKEOFF ROLL, RECEIVED HYD YELLOW RESERVOIR LOW LEVEL MESSAGE. TAKEOFF WAS ABORTED AT APPROXIMATELY 50 KNOTS. MAINTENANCE TIGHTENED LOOSE B-NUT ON THE YELLOW SYSTEM ACCUMULATOR. SERVICED YELLOW HYDRAULIC SYSTEM TO FULL. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950825006321995082500632EU 1995 8 25 9512823242 119950817A31503957900612 EIU AIRBUS320 A320211 3930320EU NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01342NW12210263 381 DURING CRUISE AT FL 390, RECEIVED ENG 1 EIU FAULT WITH ACCOMPANIED LOSS OF AUTO THRUST. ALSO, RECEIVED AIR PACK 1 AND 2 FAULT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND DESCENDED TO 10,000 FEET MSL. AIRCRAFT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE INTERFACE UNIT. 2L72 4F RTA28NM 19950825006331995082500633NM 1995 8 25 9512832712 119950822A3231 RETRACT MECH BOEING727 7272S7 138407ZNM NLG DOORS OUT OF ADJUST A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01712RC 22020 DURING DEPARTURE CLIMB UPON GEAR RETRACTION, NOSE LANDING GEAR DOOR INDICATION REMAINED ILLUMINATED. RECYCLED GEAR TO NO AVAIL, FLIGHT DIVERTED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED LEFT NOSE GEAR DOOR NOT FAIRED. RIGGED NOSE LANDING GEAR DOORS AND PERFORMED GEAR SWING, NO DISCREPANCIES NOTED. 2L73 4F A3WE 19950825006341995082500634EU 1995 8 25 9512843212 219950819A7320 HMU AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01312US 152 31676 DURING CLIMBOUT, VIBRATION FROM NR 1 ENGINE WAS FELT THROUGHOUT THE AIRCRAFT ACCOMPANIED BY FLUCTUATIONS IN FUEL FLOW N1, AND THROTTLE POSITION ON ECAM INDICATION. POWER WAS REDUCED, BUT ENGINE PERFORMANCE WAS STILL ERRATIC. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. THE HMU WAS REPLACED AND POWER ASSURANCE CHECK PERFORMED AND THE AIRCRAFT WAS DEEMED OK FOR SERVICE. 2L72 4F4 FRTA28NM 19950825006351995082500635EU 1995 8 25 9512853215 119950819A2612 FIRE LOOP AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 2 ENGINE MALFUNCTIONED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL01315US 171 31685 DURING TAKEOFF WITH ENG NR 2 FIRE LOOP 'B' FAULT INDICATION ON MEL, RECEIVED NR 2 ENGINE FIRE WARNING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DTW WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE NR 2 PYLON LOOP 'B' AND CORE LOOP SUPPORT WERE REPLACED. THE SYSTEMS CHECKED OK AND THE AIRCRAFT WAS DEEMED READY FOR SERVICE. 2L72 4F4 FRTA28NM 19950825006361995082500636NM 1995 8 25 9512865526 119950820A49405198586 STARTER BOEING757 757251 1384970NM APU FAILED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01526US 23620 DURING CRUISE AND WITH THE NR 1 ENGINE IDG ON MEL, THE APU SHUTDOWN DUE TO LOSS OF OIL. THE AIRCRAFT DIVERTED TO JNU WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE IDG AND APU STARTER WERE REPLACED AND BOTH SYSTEM CHECKED OK. 2L72 4F RTA2NM 19950825006371995082500637NM 1995 8 25 95FDEA01146 119950808A5320 ANGLE BOEING727 727227 1384078NM BS 227.5 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON BOTH THE VERTICAL AND HORIZONTAL INTERNAL FLANGES OF THE BS 227.5 LOWER CHORD ANGLE. THE CORROSION IS LOCATED JUST TO THE LEFT OF BL 0. FABRICATED REPAIR DOUBLER PER ESO11782, 8-8-95 AND EA 7-5310-25381, 8-4-95. 2L73 4F A3WE 19950825006381995082500638NM 1995 8 25 95FDEA01147 119950807A5720 ANGLE BOEING727 727233 138408ANM WS 656.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 RT WING WS 656.5, S12 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. HFEC CONFIRMED CRACK RUNS FROM FASTENER HOLE TO AFT EDGE OF ANGLE. INSTALLED REPAIR ANGLES PER SRM 57-10-4 PG 37 FIG 11, REF SB 727-57A159. 2L73 4F RTA3WE 19950825006391995082500639NM 1995 8 25 95FDEA01148 119950808A5720 ANGLE BOEING727 727233 138408ANM WS 656.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 RT WING WS 656.5 S13 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALL REPAIR ANGLES PER SRM 57-10-4 AND SB 57A 159 FIG 18. 2L73 4F RTA3WE 19950825006401995082500640NM 1995 8 25 95FDEA01149 119950808A5720 ANGLE BOEING727 727233 138408ANM WS 656.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25254FE 20936 RT WING WS 656.6 S14 LWR ANGLE CRACKED AT RIB ATTACH FASTENER. STOP DRILLED END OF CRACK. HFEC CONFIRMED CRACK ENDS AT STOP DRILL. INSTALLED REPAIR ANGLES PER SRM 57-10-4 AND SB 727-57A 159 FIG 18. 2L73 4F RTA3WE 19950825006411995082500641NM 1995 8 25 95FDEA01150 119950821A53207075T6 WEB BOEING727 727227 1384078NM BS 791 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 AREA OF CORROSION ON LOWER WEB OF DELTA BEAM, OUTER SURFACE AT BS 791 LBL 5. REPAIRED AREA OF CORROSION ON LOWER WEB OF DELTA BEAM, OUTER SURFACE AT BS 791 PER FEDEX SRM 51-40-2 FIG 1. 2L73 4F A3WE 19950825006421995082500642NM 1995 8 25 95FDEA01151 119950821A5311 FRAME BOEING727 727227 1384078NM BS 520 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 IN THE FWD CARGO BAY, THE UPPER FLANGE OF FRAME IS CRACKED AT BS 520 LBL 2 WL 154 AND RBL 14 WL 154. FABRICATED DOUBLER, CUT OUT DAMAGE, REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 19950825006431995082500643NM 1995 8 25 95FDEA01152 119950821A5320 SHEAR TIE BOEING727 727227 1384078NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON SHEAR TIE BS 720 BETWEEN STR 27 LT AND RT. REMOVED, FABRICATED AND REPLACED SHEAR TIE SRM 53-10-4. 2L73 4F A3WE 19950825006441995082500644NM 1995 8 25 95FDEA01153 119950821A5320 CHORD BOEING727 727227 1384078NM BS 720 DOUBLE DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25489FE 21492 DOUBLE HOLE IN LOWER CHORD OF FLOORBEAM BS 720F LBL 46 WL 201. OVERSIZED HOLE AND INSTALLED HI-LOC PER ENGINEERING REQUEST. 2L73 4F A3WE 19950825006451995082500645NM 1995 8 25 95FDEA01154 119950821A5347 SEAT TRACK BOEING727 727227 1384078NM BS 538-550 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 SEAT TRACK CORRODED ALONG RT FLANGE BS 538 TO 550 RBL 25 WL 208.5. REMOVED, MACHINE SHOP FABRICATED AND INSTALLED SEAT TRACK FROM BS 480 TO 550. 2L73 4F A3WE 19950825006461995082500646NM 1995 8 25 95FDEA01155 119950821A5347 TRACK BOEING727 727227 1384078NM BS 344-423 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 SEAT TRACK CORRODED OUT OF LIMITS BS 344 TO 423 LBL 25 WL 208.5. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM BS 344 TO 480, WORK PER SRM 51-10-1. 2L73 4F A3WE 19950825006471995082500647NM 1995 8 25 95FDEA01156 119950821A53302024T3 SKIN BOEING727 727233 138408ANM BS 491 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 LIGHTNING STRIKE AT BS 491 STR 17R. REPAIRED LIGHTNING STRIKE AT BS 491 STR 17R IAW FEDEX SRM 53-30-3, FILLET SEALED PATCH AND PAINTED. 2L73 4F RTA3WE 19950825006481995082500648NM 1995 8 25 95FDEA01157 119950821A53302024T3071 SKIN BOEING727 727227 1384078NM BS 720 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21496 UPON REMOVAL OF LT WING PIE SECTION. FOUND CHAFING SPOT 2 INCHES LONG BY 1 INCH WIDE AND .081 DEEP ON STR 19L AT LAP SEAM, STA 720D PLUS 11. REPAIRED DAMAGE PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825006491995082500649NM 1995 8 25 95FDEA01158 119950822A3610 DUCT DOUG MD11 MD11F 3023600NM NR 2 ENGINE LEAKING A FDEAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO25606FE 48602 NR 2 ENG FIRE WARNING ON CLIMBOUT FROM EWR, ALL ENG EGT'S OK, NO OTHER ABNORMAL INDICATIONS ON NR 2 EXCEPT AUDIO/VISUAL FIRE WARNING, PERFORMED ENG FIRE SHUTDOWN CKLIST, DID NOT HAVE TO USE FIRE BOTTLE. REMOVED AND REPLACED NR 2 ENG FCDU, FOUND 11TH STAGE DUCT LEAKING AT CLAMP IN AREA OF RT UPPER LOOP JUNCTION, REPLACED SEALS AND RE-INSTALLED DUCT SECTION. METERED FIRE DETECTION RESPONDERS. ALL SHOW GOOD, A/C OK FOR SERVICE. 2L73 4F RTA22WE 19950825006501995082500650NM 1995 8 25 95FDEA01159 119950821A3230 RETRACT MECH BOEING727 72721C 138400MNM NLG LACK OF LUBE A FDEAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 SO25144FE 19137 CDG - UPON GEAR EXTENTION LT AND RT MAIN GEAR INDICATED DOWN AND LOCKED WITH GREEN LIGHTS, NOSE GEAR RED LIGHT ILLUMINATED, DID NOT HEAR ANY INDICATION THAT NOSE WHEEL EXTENDED. LUBRICATED NOSE GEAR ASSY PER MM 12-21-11, PERFORMED TEST NOTE GEAR RETRACTION AND EXTENSION, ALL NORMAL, 8 SEC FOR GEAR EXTENTION. INSPECTED LOCK ACTUATING ROD AND LOCK MECHANISM FOUND ALL OK, A/C OK FOR SERVICE. 2L73 4F A3WE 19950825006511995082500651NM 1995 8 25 95FDEA01160 119950822A532065453132 CLIP BOEING727 727233 138408ANM BS 910 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CRACKED STR CLIP AT BS 910 STR 5R. REMOVED AND REPLACED STR CLIP AT BS 910 STR 5R. 2L73 4F RTA3WE 19950825006521995082500652NM 1995 8 25 95FDEA01161 119950822A57112024T3 SPAR BOEING727 727227 1384078NM RT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21493 NR 6 SLOT CRACKED IN SPAR AT TAI TUBE CUTOUT. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS IAW SRM 57-20-1, 51-30-2 AND FEDEX EA 7-5710-25579. 2L73 4F A3WE 19950825006531995082500653NM 1995 8 25 95UAL900106 119950823A3350 LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP297455U 21909 EMERGENCY EXIT LIGHT INOP AT AIRSTAIRS DOOR. REPLACED LIGHT AND POWER CABLE ASSEMBLY, CHECKS OK. 2L73 4F4 F A3WE E2EA 19950825006541995082500654NM 1995 8 25 95UAL900107 119950823A3350M1136 BATTERY BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29904UA 25004 EMERGENCY ESCAPE PATH LIGHTING ROW 4 TO ROW 14 AND LEFT HAND AND RIGHT HAND OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACKS, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950825006551995082500655WP 1995 8 25 ABXA9500677 119950822A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC932 3022066WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23984AX 10766 47258 DURING SERVICE CHECK, FOUND COCKPIT EMERGENCY LIGHTING VERY DIM. REPLACED BATTERIES IN THE EMERGENCY LIGHTING BATTERY PACK IAW DC-9 SUPP MM 33-53-00. 2L72 4F A6WE 19950825006561995082500656NM 1995 8 25 DL72E953449 119950821A5720 ANGLE BOEING727 727247 138408FNM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND DURING D-1 LETTER CHECK, TORQUE BOX O/B SUPPORT ANGLE CRACKED ACTUATOR MOUNT NR 4 L/E FLAP. REPAIRED PER MM 57-20-21. 2L73 4F A3WE 19950825006571995082500657NM 1995 8 25 DL72K953451 119950817A5311 FRAME BOEING727 727232 1384082NM BS 990 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 FOUND ON CV2 CHECK, CUT STA 990 FRAME AND FAIL-SAFE CHORD FOR ACCESS TO REPAIR STR 29L, REF NRC 256. REPAIRED FRAME AND CHORD PER MM 53-12-0 PG 806 AND 807, REPAIRED CHORD PER SRM 51-40-3. 2L73 4F A3WE 19950825006581995082500658NM 1995 8 25 DL72K953452 119950814A5720 ANGLE BOEING727 727232 1384082NM WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 A .75 INCH CRACK BELOW NR 8 SLAT TAI ON SUPPORT ANGLE. REPAIRED PER M/M 57-54-0 PG 807A, FOUND AT LETTER CHECK. 2L73 4F A3WE 19950825006591995082500659NM 1995 8 25 DL72K953467 119950816A5240 SKIN BOEING727 727232 1384082NM LT SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 FOUND ON CV2 CK, FED LOWER CORNER OF LT AFT SERVICE DOOR OUTER SKIN CRACKED. REPAIRED PER M/M 52-11-01. 2L73 4F A3WE 19950825006601995082500660NM 1995 8 25 DL72K953468 119950814A5522 ELEVATOR BOEING727 727232 1384082NM RT ELEVATOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 FOUND ON CV CK, DENT TOP SIDE OF RT ELEVATOR OB SIDE .5 BY .3125, .1875 DEEP. REPAIRED PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19950825006611995082500661NM 1995 8 25 DL72S953460 119950727A53306554590 SKIN BOEING727 727232 1384082NM FS 680-715 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 DURING OVERHAUL INSPECTION, EXTENSIVE CORROSION WAS FOUND ON THE SKIN ALONG STRINGER 28R AT STATIONS 680, 689, AND 715. REPAIRED IN ACCORDANCE WITH BACO S/B 727-53A0203, R2, A SKIN SPLICE FROM STA 680 TO STA 715 BETWEEN STRS 26L AND 26R WAS INSTALLED. 2L73 4F A3WE 19950825006621995082500662NM 1995 8 25 DL72W953461 119950814A5330651842012 SKIN BOEING727 727247 138408FNM FS 259-312 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING OVERHAUL INSPECTION, THE LOWER FUSELAGE SKIN PANEL BETWEEN BS 259.50 AND BS 312 AT STRINGER 20R HAD TO BE TRIMMED TO REMOVE CORROSION DAMAGE TO THE SKIN BELOW THE FWD LAV SERVICE DOOR. REPAIRED IN ACCORDANCE WITH FAA/DER FORM 8110-3, DATED 08-14-95, AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. 2L73 4F A3WE 19950825006631995082500663NM 1995 8 25 DL757953472 119950725A271015277005 CONTROL BOEING757 757232 1384965NM RT AILERON BINDING A DALAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO11614DL 22821 ON TAXI OUT FOR TAKEOFF DURING FLIGHT CONTROL CHECK, RIGHT AILERON BECAME STUCK IN FULL UP POSITION. RETURNED TO BLOCK, FOUND RT INBOARD PCA INPUT LEVER RESTRICTED. REPLACED UNIT, OPERATION NORMAL. SHOP INSPECTION OF PCA FOUND SPRING (P/N 1527725) MISSING. THIS ALLOWED THE WASHER (P/N 1527729) TO FALL OUT OF POSITION AND JAM THE SLIDE ASSEMBLY (P/N 1527721). 2L72 4F RTA2NM 19950825006641995082500664NM 1995 8 25 DL76S953471 119950821A2611 SMOKE DETECTOR BOEING767 767332 1382001NM AFT LAVATORIES ACTIVATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11134DL 25123 DURING CRUISE, SMOKE DETECTORS IN THE AFT LAVATORIES ACTIVATED. FLT ATTENDANT NOTED HIGH PITCH NOISE IN GALLEY AND LIGHT ODOR. CHECKED OVENS, COFFEE MAKERS AND LIGHT BALLASTS, NO PROBLEMS NOTED. REPLACED BATTERIES IN SMOKE DETECTORS, RETURNED TO SERVICE. 2L72 4F RTA1NM 19950825006651995082500665WP 1995 8 25 DLL13953324 119950713A53121505220 BULKHEAD 1505220 LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 AT LETTER CHECK DURING INSPECTION OF FS 1363 BULKHEAD, FOUND BULKHEAD CAP WITH DAMAGE. REPLACED CAP FROM LBL 80 TO RBL 80 PER DL ERA 271374AD. 2L73 4F A23WE 19950825006661995082500666NE 1995 8 25 P5CA9500715 219950822A73217480004 FUEL CONTROL BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE MALFUNCTIONED A P5CAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 WP23830FT 72459 19642 685859 DURING CLIMBOUT EXPERIENCED SLUGGISH ENGINE RESPONSE NR 4 ENGINE AT FL 210. CLIMBING THROUGH FL 290 HEARD AUDIBLE STALL AND OBSERVED SUBSEQUENT TOTAL LOSS OF ENGINE POWER. ALL PARAMETERS DROPPED OFF INCLUDING EGT. RELIGHT OF ENGINE WAS NORMAL AND ENGINE PERFORMANCE REMAINED NORMAL DURING RETURN TO JFK. INSPECTED INLET/EXHAUST AND BLEEDS, BORESCOPED ENGINE 8TH, 9TH, 14TH, AND 15TH STAGE COMPRESSORS, BORESCOPED 1ST AND 2ND STAGE TURBINES, NO DAMAGE. REMOVED AND REPLACED FUEL CONTROL UNIT AND TT2 SENSOR. 2L74 4F4 F A20WE E20EA 19950825006671995082500667WP 1995 8 25 UPS804318 119950819A3350 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01783UP 45973 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS. 2L74 4F RT4A25 19950825006681995082500668WP 1995 8 25 9512879872 119950821A3232 ACTUATOR DOUG DC9 DC951 3022051WP LT MLG DOOR SLOW A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01781NC 48121 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. COMPLETED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT STAYED ON. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND TARGET ARM SLIDING OFF EDGE OF LEFT DOOR ROLLER. ADJUSTED TO CENTER OF ROLLER. ALSO ADJUSTED ROLLER ASSEMBLY AND SENSOR. FOUND LEFT DOOR SLOW TO CLOSE. REPLACED DOOR ACTUATOR. NOTE: ALSO REPLACED THE LEFT DOOR ASSEMBLY AND RIGHT DOOR SKID PLATE DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825006691995082500669WP 1995 8 25 9512889883 119950822A3260 PROX CONTROL DOUG DC9 DC951 3022051WP NLG MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01671MC 47660 NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PROXIMITY CONTROL UNIT AND DOWNLOCK SENSOR. CYCLED GEAR SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950825006701995082500670NM 1995 8 25 95FDEA01162 119950822A5530AND101341201 STRINGER BOEING727 727227 1384078NM VERT FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 STR NR 8R IS CRACKED IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2. REPAIRED STR NR 8R IN VERTICAL FIN BAY NR 8 AT FIN STA 151.2 IAW FEDEX SRM 55-30-4. 2L73 4F A3WE 19950825006711995082500671NM 1995 8 25 95FDEA01163 119950822A5330M459214 SKIN BOEING727 727227 1384078NM BS 689-688 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON (INTERIOR) SKIN AT BUTT JOINT BS 680-688 BETWEEN STR 26-27R. REPAIRED CORROSION ON SKIN AT BUTT JOINT BS 680-688 BETWEEN STR 26-27R AS PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825006721995082500672NM 1995 8 25 95FDEA01164 119950822A5530AND101341204 STRINGER BOEING727 727227 1384078NM VERT FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 NR 8R STR IS CRACKED IN VERTICAL FIN BAY NR 8 FIN STA 180 WHERE STR ATTACHES TO WEB. REPAIRED NR 8R STR IN VERTICAL FIN, BAY NR 8, FIN STA 180. FEDEX SRM 55-30-4 FIG 1. 2L73 4F A3WE 19950825006731995082500673NM 1995 8 25 95FDEA01165 119950822A5315 FLOORBEAM BOEING727 72725 1384006NM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C235-02), ON FLOORBEAM BOTTOM SIDE OF UPPER FLANGE BS 660 RBL 50 WL 208. 2L73 4F A3WE 19950825006741995082500674NM 1995 8 25 95FDEA01166 119950822A57117075T6 SPAR BOEING727 72725 1384006NM WS 250 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 WHILE WORKING CUST ID NR0579, FOUND CORROSION ON REAR SPAR LOWER CHORD L/W STA 250. REPAIRED LOWER REAR SPAR CHORD IAW FEDEX EA 7-5710-25573 AT WS 224.5. 2L73 4F A3WE 19950825006751995082500675NM 1995 8 25 95FDEA01168 119950822A575465162262 SKIN BOEING727 72725 1384006NM NR 2 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION UNDER DATA PLATE NR 2 K-FLAP. REMOVED AND REPLACED NR 2 K-FLAP PER FEDEX MM 57-53-0. 2L73 4F A3WE 19950825006761995082500676NM 1995 8 25 95FDEA01169 119950822A575465163262 BONDING JUMPER BOEING727 72725 1384006NM NR 5 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION ON NR 5 K-FLAP I/B UPPER BONDING JUMPER ATTACH POINT. REMOVED AND REPLACED NR 5 K-FLAP PER FEDEX MM 27-01-01. 2L73 4F A3WE 19950825006771995082500677NM 1995 8 25 95FDEA01170 119950822A575465162252 SKIN BOEING727 72725 1384006NM NR 4 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION ON NR 4 K-FLAP O/B UPPER GROUND WIRE ATTACH POINT. REMOVED AND REPLACED NR 4 K-FLAP PER FEDEX MM 27-81-1. 2L73 4F A3WE 19950825006781995082500678NM 1995 8 25 95FDEA01171 119950822A53302024T3071 SKIN BOEING727 72725 1384006NM BS 444 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 LIGHTNING STRIKE BS 444 BETWEEN FASTENER ON STR 4L. FOUND LIGHTNING STRIKE DAMAGE TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825006791995082500679NM 1995 8 25 95FDEA01172 119950822A5754651622716 BULLNOSE BOEING727 72725 1384006NM NR 6 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION ON NR 6 K-FLAP O/B BULLNOSE ACTUATING ROD LOWER ATTACH POINT AT BULLNOSE. REMOVED AND REPLACED NR 6 K-FLAP PER FEDEX MM 27-81-01. 2L73 4F A3WE 19950825006801995082500680NM 1995 8 25 95FDEA01173 119950822A5314155PH KEEL BEAM BOEING727 72725 1384006NM BS 990-1050 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION AROUND FASTENER ON KEEL BEAM AT BS 990-1010 AND BS 1030-1050, S29R. CORROSION REMOVAL WAS OUT OF LIMITS, OVERSIZED FASTENER HOLES TO REMOVE CORROSION, FABRICATED FREEZE PLUGS AND REPAIR ANGLES, INSTALLED ALL WORK DONE PER TRAMCO EWO NR 95-2968, EA 7-5310-25588. 2L73 4F A3WE 19950825006811995082500681NM 1995 8 25 95FDEA01174 119950822A5320 SHEAR TIE BOEING727 72725 1384006NM BS 1203 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 SHEAR TIE CRACKED AT BS 1203, WL 249, RBL 66. REPAIRED SHEAR TIE PER EWO 95-2953, BS 1203, RBL 66, WL 249. 2L73 4F A3WE 19950825006821995082500682NM 1995 8 25 95FDEA01175 119950822A53302024T3 SKIN BOEING727 72725 1384006NM BS 1135 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 DENT IN FUSELAGE SKIN BS 1135 BETWEEN 2R - 3R. REMOVED DAMAGED SKIN AND REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825006831995082500683NM 1995 8 25 95FDEA01176 119950823A57116595600763 SPAR BOEING727 72725 1384006NM WS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION ON LOWER WING SPAR CHORD AT STA 740, LBL 16, WL 168. ACCOMPLISHED REPAIR OF LOWER 740 CHORD AND SKIN IAW FEDEX EA 7-5710-25579. 2L73 4F A3WE 19950825006841995082500684NM 1995 8 25 95FDEA01177 119950823A552165174412 RIB BOEING727 72725 1384006NM NR 6 ELEV HINGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 POSSIBLE CRACK ON THE NR 6 ELEVATOR HINGE RIB UPPER SURFACE BETWEEN THE 2ND AND 3RD RIVET FORWARD FROM THE T/E BEAM. NDI VERIFIED CRACK, REMOVED AND REPLACED NR 6 ELEVATOR HINGE RIB PER FEDEX MM 27-30-21, SRM 51-30-02, EA 7-5510-25592A. 2L73 4F A3WE 19950825006851995082500685NM 1995 8 25 95FDEA01178 119950728A53302024T3063 SKIN BOEING727 727233 138408ANM BS 1030 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 GOUGE IN SKIN AT STA 1030 AFT CARGO DOOR SKIN CUT OUT BETWEEN STR 23-24R (MARKED) OUT OF LIMITS PER FEDEX SRM 53-30-1 FIG 1. REPAIRED SKIN IAW FEDEX SRM 53-30-3. 2L73 4F RTA3WE 19950825006861995082500686NM 1995 8 25 95FDEA01179 119950728A53207075T6120 BRACKET BOEING727 727233 138408ANM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25264FE 21626 CORROSION ON STR TO FRAME BRACKET BS 950E, RBL 6, STR 29R, WL 138.5. REMOVED CORRODED BRACKET, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW FEDEX SRM 51-20-1, 51-30-2. 2L73 4F RTA3WE 19950825006871995082500687NM 1995 8 25 95FDEA01180 119950823A5511 RIB BOEING727 727227 1384078NM LT HORIZ STAB CRACK A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FLOOR BEAM CORRODED AT BS 460, RBL 12 - 23, WL 208.5. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1 AND 53-10-08. 2L73 4F A3WE 19950825006881995082500688NM 1995 8 25 95FDEA01181 119950823A5347 SEAT TRACK BOEING727 727227 1384078NM BS 495-535 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 SEAT TRACK CORRODED ALONG FLANGES BS 495-535 AND BS 615, BL 0, WL 208.5. REMOVED, FABRICATED AND INSTALLED SEAT TRACK BS 480-630 PER SRM 53-10-5. 2L73 4F A3WE 19950825006891995082500689NM 1995 8 25 95FDEA01182 119950823A5313BAC1498 STRINGER BOEING727 727227 1384078NM BS 496 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION IN FWD CARGO BAY. THERE IS CORROSION ON STR 28R AT BS 496. REPAIRED CORRODED STR 28R AT BS 496 PER FEDEX SRM 53-10-3. REPAIRED CORRODED SKIN FROM NRO 067 AT BS 496 , RBL 7 PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950825006901995082500690NM 1995 8 25 95FDEA01183 119950823A5320 SHEAR TIE BOEING727 727227 1384078NM BS 970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION (71C709-02) ON SHEAR TIE LOWER FLANGE BS 970, RBL 3, FWD AND AFT SIDE OF FRAME AFT CARGO BAY. INSTALLED NEW SHEAR TIE OR BS 970 PER SRM 53-10-2. 2L73 4F A3WE 19950825006911995082500691NM 1995 8 25 95FDEA01184 119950823A53302024T3 SKIN BOEING727 727227 1384078NM BS 480-500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 BS 480-500 STR 28R-26R. THERE ARE DEEP GOUGES, DENTS AND A SMALL BULGE ON EXTERIOR SKIN. REPAIRED CORRODED SKIN AT BS 496, RBL 7 PER FEDEX SRM 53-30-5. 2L73 4F A3WE 19950825006921995082500692NM 1995 8 25 95FDEA01185 119950823A5313BAC1498143 STRINGER BOEING727 727233 138408ANM BS 804 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 DRILL STARTS IN STR 4-5R, BS 804. REPAIRED IAW FEDEX SRM 53-10-3, STR 4-5R, BS 804. 2L73 4F RTA3WE 19950825006931995082500693WP 1995 8 25 95FDEA01186 119950812A5313 LONGERON DOUG DC10 DC1030F 3023504WP BS 152-154 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 RUSTY FASTENERS IN LWR CENTER CARGO COMPT UNDER FLOOR SPACE AT FS 152-154L, LONGERONS 45-47L. REMOVED FASTENERS, BURNISHED OUT CORROSION, FABRICATED ANGLE AND INSTALLED IAW EO 8-5310-25134. 2L73 4F RTA22WE 19950825006941995082500694WP 1995 8 25 95FDEA01187 119950801A5312 BULKHEAD DOUG DC10 DC1030F 3023504WP BS 1156 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 WING CTR SECT FUEL TANK BLKHD STA 1156 HAS INTERGRANULAR CORROSION AT VERTICAL STIFFENER O/B OF OPENING PNL143CZ, FWD FACE, LWR AREA. REMOVED CORROSION FROM AFFECTED AREA IAW DC10 SRM 51-21-01. THICKNESS LIMIT CK'D OK. ALONDINED AND PAINTED AFFECTED AREA IAW DC10 SRM 51-21-01. 2L73 4F RTA22WE 19950825006951995082500695WP 1995 8 25 95FDEA01188 119950804A5510ALC750212 T ANGLE DOUG DC10 DC1030F 3023504WP RT HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 RT STAB L/E 2ND RIB, O/B SECTION UPPER WEB T-CHORD IS CRACKED, ENTIRE LENGTH INSIDE. REMOVED T-ANGLE, INSTALLED NEW PART ALC7502-12, FEDEX SRM 51-00-01. 2L73 4F RTA22WE 19950825006961995082500696WP 1995 8 25 95FDEA01189 119950804A5510ALC750211 T ANGLE DOUG DC10 DC1030F 3023504WP LT HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 LEFT STAB L/E 2ND RIB, REMOVED SECTION O/B WEB UPPER T-CHORD IS CRACKED ON INSIDE. REMOVED T-CHORD, INSTALLED NEW T-CHORD P/N ALC-7502-11, PER SRM 51-00-01. 2L73 4F RTA22WE 19950825006971995082500697WP 1995 8 25 95FDEA01190 119950730A5510 T-CHORD DOUG DC10 DC1030F 3023504WP LT HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 LT/STAB L/E 2ND REMOVED SECTION O/B WEB LWR T-CHORD IS CRACKED ON INSIDE 6. STOP DRILLED CRACK, FABRICATED SHIMS AND REPAIRED ANGLE AS PER EA 8-5510-25132. 2L73 4F RTA22WE 19950825006981995082500698WP 1995 8 25 95FDEA01192 119950727A5754ARH01742 BRACKET DOUG DC10 DC1030F 3023504WP RT LE SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 RIGHT WING O/B SLAT DRIVE OUTER BRACKET CRACKED, LOWER FWD FLANGE RADIUS. REMOVED AND REPLACED BRACKET WITH NEW BRACKET MODIFIED TO EO 8-2780-7-2319C SPEC. MM 27-83-02 (REF TO CONTROL ITEM 4, PART NR 4). 2L73 4F RTA22WE 19950825006991995082500699WP 1995 8 25 95FDEA01194 119950816A5320 ANGLE DOUG DC10 DC1030F 3023504WP BS 1795-1835 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 INSIDE AFT CARGO COMPT STA 1795-1835, LONGERON 44L, NESTING ANGLE AND ATTACHING WEB TO CARGO DOOR LOWER TORQUE BOX HAS CORROSION - LEVEL 2. REMOVED AND REPLACED NESTING ANGLE AND ATTACH WEB. 2L73 4F RTA22WE 19950825007001995082500700WP 1995 8 25 95FDEA01195 119950816A5320 FITTING DOUG DC10 DC1030F 3023504WP BS 1790 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25303FE 46802 INSIDE AFT CARGO COMPT - FWD LOWER CORNER OF DOOR SILL - LONGERON 41 - END FITTING AT STA 1790 IS CORRODED - LEVEL 2. INSTALLED NEW FITTING. 2L73 4F RTA22WE 19950825007011995082500701NM 1995 8 25 95FDEA01196 119950824A523070750090 DOUBLER BOEING727 727233 138408ANM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 MAIN CARGO DOOR SIDE FRAME IS GOUGED ON AFT LOWER FRAME. REPAIRED MAIN CARGO AFT LOWER SIDE FRAME IAW FEDEX SR 27-52-009. 2L73 4F RTA3WE 19950825007021995082500702NM 1995 8 25 95FDEA01197 119950824A5315BAC1505100617 FLOOR BEAM BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 THE UPPER CHORD OF THE BS 480, FLOOR BEAM IS CORRODED OUT OF LIMITS AT RBL 12, WL 208.5. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-10-08, FIG 3. 2L73 4F A3WE 19950825007031995082500703EU 1995 8 25 COM31140 119950822A32317232110623 CONTROL CABLE SAAB SF340 SF340A 7850100EU RT MLG DOOR BROKEN A COMAK NONE J WARNING INDICATION ININSP/MAINT 1 SO01320CA 340A064 RIGHT INBOARD MAIN GEAR DOOR WOULD NOT RETRACT AFTER GEAR EXTENSION. ACTION: FOUND RELEASE CABLE ON TELESCOPING ROD, BROKEN, REPLACED CABLE WITH SERVICEABLE UNIT. 2L72 4T RTA52EU 19950825007041995082500704 1995 8 25 COM31141 419950822A61228210163C GOVERNOR SAAB SF340 SF340A 7850100EU RT ENGINE INOPERATIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01357CA10233 340A044 RIGHT PROPELLER COMES OUT OF FEATHER VERY SLOW. ACTION: FERRIED AIRCRAFT TO CVG, FOUND RIGHT PROPELLER OVERSPEED GOVERNOR BAD. REMOVED AND REPLACED GOVERNOR WITH SERVICEABLE UNIT. 2L72 4T RTA52EU 19950825007051995082500705EA 1995 8 25 COM60543 119950822A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA CARGO BAY ACTIVATED A COMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO01933CA 7040 CARGO SMOKE WARNING ON TAXI OUT. ARMED AND FIRED BOTTLES. ACTION: FOUND LIVE BIRDS (300 CANARIES IN CAGES) HAD CAUSED DETECTORS TO ACTIVATE; REMOVED AND REPLACED FIRE BOTTLES AND SQUIBS WITH SERVICEABLE UNITS. 2L72 4F RTA21EA 19950825007061995082500706NE 1995 8 25 P5CA9500716 219950822A75307477555 ENGINE VANE CONT BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE MALFUNCTIONED A P5CAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23830FT 94614 19642 685859 AT TAKEOFF, UNABLE TO REACH TARGET BEFORE HITTING STOPS. REPLACED ENGINE VANE CONTROL. 2L74 4F4 F A20WE E20EA 19950825007071995082500707NE 1995 8 25 P5CA9500717 219950824A7261JT9D7A ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 OIL LEAKING A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP23852FT633922848 19757 662326 DURING CLIMB-OUT, LOSS OF OIL IN NR 1 ENGINE SHUT DOWN ENGINE. FOUND OIL TO BE COMING OUT TAIL PIPE, ENGINE CHANGED. 2L74 4F4 F A20WE E20EA 19950825007081995082500708SW 1995 8 25 QXEA9500261 119950821A3230727425 CIRCUIT BREAKER SWRNGN SWRNGNSA227 SA227AC 8780603SW LANDING GEAR TRIPPED A QXEAK NONE O OTHER CLCLIMB 1 NM09383PH AC590 BOI - FLIGHT CREW HAD TO USE OVERRIDE TO GET GEAR TO COME UP. GEAR EXTENSION WAS NORMAL. LANDING GEAR CONTROL CIRCUIT BREAKER WAS REPLACED AND GEAR HANDLE, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19950825007091995082500709EU 1995 8 25 QXEA9500262 119950821A33501820 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 GEG - SEVERAL OVERHEAD EMERGENCY LIGHTS INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950825007101995082500710EU 1995 8 25 QXEA9500263 119950823A3350MGG1280 EEL BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 GEG - CENTER ISLE OVERHEAD EXIT SIGN IS INOP WITH EMERGENCY LIGHT ARMED. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950825007111995082500711EU 1995 8 25 QXEA9500264 119950823A33505515900003 EEL PANEL FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 PDX - EXIT SIGN ABOVE COCKPIT DOOR IS INOP. LIGHT PANEL REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950825007121995082500712NM 1995 8 25 UPS204319 119950823A3260 INDICATOR BOEING727 727180C 138406GNM MAIN GEAR INOP A IPXAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO01921UP 19874 PILOT REPORTED RIGHT MAIN GEAR DOWN AND LOCKED GREEN INDICATING LIGHT DID NOT COME ON AFTER GEAR EXTENDED. CHECKED LIGHT BULBS AFTER RECYCLING GEAR, AND FOUND BOTH NOT WORKING. REPLACED ONE BULB AND INDICATOR WORKED. MAINTENANCE REPLACED BOTH BULBS, AND R-13 (RIGHT MAIN GEAR DOWNLOCK DELAY) AS A PRECAUTION. PINNED AND CYCLED GEAR SEVERAL TIMES. CHECKS OK AS PER MM 32-61-21. 2L73 4F A3WE 19950825007131995082500713WP 1995 8 25 UPS804289 119950823A5330 SKIN DOUG DC8 DC871F 302199DWP BS 1540 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FUSELAGE SKIN AT STATION 1540 AND LONGERON 33R - 34R. MAINTENANCE REPAIRED PER UPS EO DC8-53-1445. 2L74 4F RT4A25 19950825007141995082500714WP 1995 8 25 UPS804290 119950824A5755 SKIN DOUG DC8 DC873F 302199FWP NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND DELAMINATION AT THE INBOARD LOWER SIDE OF THE LEFT WING, NR 1 SPOILER. MAINTENANCE REPLACED THE SPOILER IAW MM 27-61-01. 2L74 4F RT4A25 19950825007151995082500715WP 1995 8 25 UPS804291 119950824A5755 SKIN DOUG DC8 DC873F 302199FWP NR 4 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER INBOARD SIDE LEFT WING NR 4 SPOILER. MAINTENANCE REPLACED THE SPOILER PER MM 27-61-01. 2L74 4F RT4A25 19950825007161995082500716WP 1995 8 25 UPS804292 119950824A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 35 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE ANGLE STIFFENER ON THE LAVATORY FLOOR AT STATION 35 AND RBL 45. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE PART PER SRM 53-3-1, 53-3-3 AND 51-1-21. 2L74 4F RT4A25 19950825007171995082500717WP 1995 8 25 UPS804293 119950824A5320 CASTING DOUG DC8 DC873F 302199FWP BS 1460 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEAD ON THE LEFT CUSP AT STATION 1460 AFT TOP. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 51-1-20. 2L74 4F RT4A25 19950825007181995082500718WP 1995 8 25 UPS804294 119950824A5320 CASTING DOUG DC8 DC873F 302199FWP BS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BOTH SIDES OF CASTING AT THE RIGHT CUSP AT STATION 560. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 5 1-1-20D. 2L74 4F RT4A25 19950825007191995082500719WP 1995 8 25 UPS804295 119950824A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 80 - 100 AT LONGERON 31R. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE FINGER DOUBLER IAW SRM 51-1-20 AND 51-1-20D. 2L74 4F RT4A25 19950825007201995082500720WP 1995 8 25 UPS804296 119950824A5320 CASTING DOUG DC8 DC873F 302199FWP BS 620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AROUND THE BOLT HEAD AT RIGHT CUSP, STATION 620. MAINTENANCE REMOVED AND REPLACED THE CASTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950825007211995082500721WP 1995 8 25 UPS804297 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT THE RIGHT CUSP AROUND BOLT HEADS AT STATION 600. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950825007221995082500722WP 1995 8 25 UPS804298 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT RIGHT CUSP AROUND THE BOLT HEAD AT STATION 640. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950825007231995082500723WP 1995 8 25 UPS804299 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT RIGHT CUSP AROUND BOLT HEADS AT STATION 660. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19950825007241995082500724WP 1995 8 25 UPS804300 119950824A5220 FITTING DOUG DC8 DC873F 302199FWP BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN DECK FRAME 420 RIGHT FLOOR FITTING AT CUSP AROUND ATTACH BOLTS. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE FITTING PER SRM 51-1-20. 2L74 4F RT4A25 19950825007251995082500725WP 1995 8 25 UPS804301 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE CASTING AT LEFT CUSP AT STATION 420. MAINTENANCE REMOVED, FABRICATED AND INSTALLED THE FITTING IAW SRM 51-1-20, 53-1-0 AND 51-3-0. 2L74 4F RT4A25 19950825007261995082500726WP 1995 8 25 UPS804302 119950824A5712 LE RIB DOUG DC8 DC873F 302199FWP WS 520.168 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE AFT UPPER END OF THE RIGHT WING LEADING EDGE RIB AT STATION XS520.168. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED AND INSTALLED THE ANGLE PER SRM 53-2-0. 2L74 4F RT4A25 19950825007271995082500727WP 1995 8 25 UPS804303 119950824A5320 WEB DOUG DC8 DC873F 302199FWP STA 367-380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN DECK 21 RIGHT BETWEEN FRAME 360 - 380 AT STATION 367 - 380. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED AND INSTALLED PER SRM 53-01-0 AND 53-2-5. 2L74 4F RT4A25 19950825007281995082500728WP 1995 8 25 UPS804304 119950824A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 960-980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FINGER DOUBLER AT STATION 960 - 980 AND RBL 62. MAINTENANCE FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-4-1, 51-1-8 AND 51-1-21. 2L74 4F RT4A25 19950825007291995082500729WP 1995 8 25 UPS804305 119950824A5320 SPLICE DOUG DC8 DC873F 302199FWP BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER SPLICE 31L BETWEEN FRAME 600 - 620. MAINTENANCE REMOVED THE SPLICE, FABRICATED AND INSTALLED THE SPLICE IAW SRM 51-1-20 AND 53-4-1. 2L74 4F RT4A25 19950825007301995082500730WP 1995 8 25 UPS804306 119950824A5311 FUSELAGE DOUG DC8 DC873F 302199FWP BS 1120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 1120 BETWEEN LONGERON 33R AND 34R. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7306-A. 2L74 4F RT4A25 19950825007311995082500731WP 1995 8 25 UPS804307 119950824A5754 SKIN DOUG DC8 DC873F 302199FWP RT TE SLOT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT INBOARD WING SLOT OUTBOARD END UPPER SURFACE. MAINTENANCE REMOVED THE ANGLE REPAIR, STOP DRILLED, REPAIRED AND REINSTALLED PER SRM 51-3-0, 57-2-0, AND 51-1-20. 2L74 4F RT4A25 19950825007321995082500732WP 1995 8 25 UPS804308 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1220 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FITTING ACROSS THE FASTENER C-3 AFT AT DOOR OPENING LOWER AT STATION 1220. MAINTENANCE REMOVED AND REPLACED THE FITTING AND FASTENERS IAW SRM 51-1-20D. 2L74 4F RT4A25 19950825007331995082500733WP 1995 8 25 UPS804310 119950824A5730 SKIN DOUG DC8 DC873F 302199FWP WS 635-667 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD LEADING EDGE LOWER SKIN BETWEEN STATION XFS 635.0 - XFS 667.0. MAINTENANCE TRIMMED OUT THE CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 57-2-1. 2L74 4F RT4A25 19950825007341995082500734WP 1995 8 25 UPS804311 119950824A5320 ANGLE DOUG DC8 DC873F 302199FWP WS 640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT WING FORWARD OF THE FORWARD SPAR WING TO BODY ANGLE AT STATION 640 - 680. MAINTENANCE REMOVED THE ANGLE, FABRICATED AND INSTALLED PER SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19950825007351995082500735WP 1995 8 25 UPS804312 119950824A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 855-920 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN LONGERON 24R AT STATION 855 - 867 AND STA 919 - 920. MAINTENANCE REMOVED AND REPLACED THE LONGERON IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19950825007361995082500736WP 1995 8 25 UPS804313 119950824A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TOP FORWARD CORNER OF THE RIGHT FORWARD SERVICE DOOR ON THE FUSELAGE SKIN. MAINTENANCE CUT OUT THE DAMAGED AREA PER UPS EO DC8-5330-7308-A. 2L74 4F RT4A25 19950825007371995082500737WP 1995 8 25 UPS804314 119950824A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FITTING AT STATION 1140 AND LONGERON 33R. MAINTENANCE REMOVED AND REPLACED THE FITTING PER SRM 51-1-20D AND 51-1-8. 2L74 4F RT4A25 19950825007381995082500738WP 1995 8 25 UPS804315 119950824A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1540 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 33L AT STATION 1540. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2. 2L74 4F RT4A25 19950825007391995082500739WP 1995 8 25 UPS804316 119950824A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1540-1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 29R AT STATION 1540 - 1560. MAINTENANCE REPAIRED THE LONGERON PER SRM 53-2-2. 2L74 4F RT4A25 19950825007401995082500740WP 1995 8 25 UPS804317 119950824A5754 SKIN DOUG DC8 DC873F 302199FWP RT LE SLOT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIGHT WING OUTBOARD MID-SLOT PANEL. MAINTENANCE REPLACED THE SLOT PANEL PER MM 27-80-02. 2L74 4F RT4A25 19950825007411995082500741WP 1995 8 25 UPS804320 119950823A5330 SKIN PANEL DOUG DC8 DC871F 302199DWP BS 1350 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE BELLY SKIN AT STATION 1350 - 1490. MAINTENANCE REPLACED THE SKIN PANEL PER SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19950825007421995082500742WP 1995 8 25 UPS804321 119950823A5330 SKIN DOUG DC8 DC871F 302199DWP BS 160 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE SKIN AT STATION 160 - 190 AND LONGERONS 34L - 35R. MAINTENANCE REPLACED THE BELLY SKIN PANEL PER SRM 51-1-20D, 51-1-21 AND 51-1-14. 2L74 4F RT4A25 19950825007431995082500743WP 1995 8 25 UPS804322 119950823A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34R AT STATION 80 - 187. MAINTENANCE REPLACED THE LONGERON PER SRM 51-1-20D. 2L74 4F RT4A25 19950825007441995082500744WP 1995 8 25 UPS804323 119950823A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 100-187 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 36 AND ON THE END FITTING AT STATION 100 - 187. MAINTENANCE REPLACED THE LONGERON AND END FITTING PER SRM 51-1-20D, 2L74 4F RT4A25 19950825007451995082500745WP 1995 8 25 UPS804324 119950823A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1360-1460 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 35R AT STATION 1360 - 1460. MAINTENANCE REPLACED THE LONGERON PER SRM 51-1-20D. 2L74 4F RT4A25 19950825007461995082500746WP 1995 8 25 UPS804325 119950823A5311 FRAME DOUG DC8 DC871F 302199DWP BS 120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE BELT FRAME LOWER LIP AT STATION 120 AND LONGERON 35L - 35R. MAINTENANCE REPAIRED THE FRAME PER SRM 53-2-0. 2L74 4F RT4A25 19950825007471995082500747WP 1995 8 25 UPS804326 119950823A5330 SKIN DOUG DC8 DC871F 302199DWP BS 1155 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SKIN AT STATION 1155 AND LONGERON 33R. MAINTENANCE REPAIRED THE SKIN PER UPS EO DC8-5330-7345-A. 2L74 4F RT4A25 19950825007481995082500748WP 1995 8 25 UPS804327 119950824A5320 WEB DOUG DC8 DC873F 302199FWP BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01804UP 46004 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE MAIN LANDING GEAR WHEELWELL CEILING WEB AT STATION 960 AND LONGERON 22L. MAINTENANCE REPAIRED THE DAMAGE PER UPS EO DC8-5310-7346-A. 2L74 4F RT4A25 19950825007491995082500749WP 1995 8 25 UPS804328 119950824A5330 SKIN DOUG DC8 DC871F 302199DWP BS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE SKIN AT STATION 1240 AND LONGERON 36. MAINTENANCE REPAIRED THE SKIN PER UPS EO DC8-5330-7351-A. 2L74 4F RT4A25 19950825007501995082500750WP 1995 8 25 UPS804329 119950823A5330 SKIN DOUG DC8 DC871F 302199DWP BS 35 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE SKIN AT STATION 35 AND LONGERON 31R. MAINTENANCE REPAIRED PER UPS EO DC8-5330-7343-A. 2L74 4F RT4A25 19950825007511995082500751WP 1995 8 25 UPS804331 119950824A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1445-1460 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 31R AT STATION 1445 - 1460. MAINTENANCE REPAIRED THE LONGERON PER UPS EO DC8-5310-7352-A. 2L74 4F RT4A25 19950901000011995090100001EU 1995 9 1 9512893205 119950822A2760 SPOILER AIRBUS320 A320211 3930320EU RIGHT WING FLOATING A ANWAAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 GL01305US 41 DURING ROTATION, NOTICED A SLIGHT ROLL MOMENT AT APPROXIMATELY 1,000 FEET. RECEIVED F/CTL GND SPOILER FAULT. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE NOTED THAT THE RIGHT GROUND SPOILER INDICATED A FOUR INCH DEFLECTION ON THE LOWER ECAM. RESET RIGHT GROUND SPOILER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950901000021995090100002 1995 9 1 9513046603 419950823A34417883450041 INS BOEING747 747151 1384891NM NR 3 MALFUNCTIONED A NWAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL01603US 19780 AFTER TAKEOFF WITH NR 3 INS ON MEL, THE NR 1 INS WENT OUT OF TOLERANCE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 50,000 LBS OF FUEL, RETURNED TO HNL AND LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE REPLACED NR 1 INS AND PERFORMED FUNCTIONAL CHECK, UNIT TESTED NORMAL. 2L74 4F A20WE 19950901000031995090100003NM 1995 9 1 95FDEA01198 119950824A2612 FIRE DETECTOR DOUG MD11 MD11F 3023600NM NR 2 ENGINE MALFUNCTIONED A FDEAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25606FE 48602 NRT - CLIMBING THROUGH FL 200, NR 2 FIRE WARNING ILLUMINATED WITH THE THROTTLE PULLED TO IDLE FIRE WARNING LIGHT IN HANDLE AND START SW WENT AWAY, RETURNED RJAA. NR 2 FDCU FAULT REVIEW, UP RIGHT FIRE DET ASSY-A AND LOOP-A FAULT REMOVED WIRE TERMINALS FROM RESPONDER AND CLEAN AND REMOVED DIRTY FOD CLAMPS. NR 2 FDCU R-T-S TEST PASSED PER MM 26-11-02, TOTAL RESISTANCE READS 1,465K OHMS. 2L73 4F RTA22WE 19950901000041995090100004NM 1995 9 1 95FDEA01199 119950824A3260 SWITCH WIRE BOEING727 727227 1384078NM RT MLG DOOR FAILED A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25477FE 21394 RT MLG DOOR LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT, 3 TIMES. REMOVED AND REPLACED WIRING FROM D752 TO SPLICES SP578 AND SP576. REMOVED AND REPLACED D752 FOR RT MLG DOOR LOCK SW. FUNCTIONAL CHECKS GOOD PER FEDEX MM 32-62-11. 2L73 4F A3WE 19950901000051995090100005WP 1995 9 1 ABXA9500678 119950824A33504TL1110B EEL SWITCH DOUG DC9 DC941 302207NWP COCKPIT DEFECTIVE A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23990AX 47493 DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTS INTERMITTENT IN TEST. REPLACED THE EMERGENCY LIGHT SWITCH AND OPS CHECKED GOOD IAW DC-9 SUPP MM 33-53-00. 2L72 4F A6WE 19950901000061995090100006NM 1995 9 1 DL72K953500 119950815A5315 FLOORBEAM BOEING727 727232 1384082NM BS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 FOUND ON CV2 CHECK, CORROSION AROUND FASTENER HOLES FLOORBEAM UPPER SURFACE STA 344 LBL 45 RBL 13. REPAIRED PER SRM 53-10-8 FIG 10. 2L73 4F A3WE 19950901000071995090100007NM 1995 9 1 DL72S953462 119950822A531265C15764120 BLKHD DOUBLER BOEING727 727232 1384082NM BS 1183 TRIMMMED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11493DA 21062 DURING ACCOMPLISHMENT OF BACO S/B 727-53-0055, R9, REINFORCEMENT OF THE BS 1183 BULKHEAD AS MANDATED BY AD 90-06-09. WHILE ACCOMPLISHING MODIFICATION TO THE BS 1183 LT AFT DOOR FRAME, THE DOUBLER WAS TRIMMED INADVERTENTLY. IN ACCORDANCE WITH BACO TWX-DAL-ATL-95-0762RR DATED 03 AUG 1995, THE IMPROPERLY INSTALLED DOUBLER WAS AUTHORIZED TO BE TRIMMED. 2L73 4F A3WE 19950901000081995090100008NM 1995 9 1 DL72S953474 119950818A5743 TRUNNION BOEING727 727232 1384082NM LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 AT HMV, LEFT MLG FWD TRUNNION FTG CORRODED IN HOLES. REWORKED PER MM 57-43-0 AND PS 900-4 NR 5. 2L73 4F A3WE 19950901000091995090100009NM 1995 9 1 DL72S953475 119950822A5753 BUSHING BOEING727 727232 1384082NM NR 4 FLAP TRACK MISALIGNED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 AT HMV, FOUND LT FITTING FOR NR 4 FLAP TRACK MISALIGNED. REPLACED BUSHING PER MM 57-42-0 PG 814. 2L73 4F A3WE 19950901000101995090100010NM 1995 9 1 DL72S953476 119950823A5755 ANGLE BOEING727 727232 1384082NM LT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 AT HMV, FOUND ANGLE CRACKED INBD LWR CORNER OF INBD GRND SPOILER MOUNT BOX. REPAIRED PER MM 57-55-0 PG 805. 2L73 4F A3WE 19950901000111995090100011NM 1995 9 1 DL72S953496 119950820A5347 SEAT TRACK BOEING727 727232 1384082NM FS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 FWD CABIN SEAT TRACK, RT SIDE STA 400 OB, AND 470 OB, REMOVED CORR PER SRM 51-10-6. STA 470 WITHIN LIMITS PER SRM 53-10-1 FIG 3, STA 400 OUT OF LIMITS PER SRM 53-10-1 FIG 3. ALSO, FS 400 SHOWS EVIDENCE OF PREVIOUS CORROSION REMOVAL. PREPARED NEW SEAT TRACK SECTION PER MM 53-20-11 FIG 802. INSTALLED SEAT TRACK AS PER MM 53-20-11 FIG 802. 2L73 4F A3WE 19950901000121995090100012NM 1995 9 1 DL72S953497 119950820A53475342021060 SEAT TRACK BOEING727 727232 1384082NM STA 1090 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 SEAT TRACK AFT CABIN CORRODED RT SIDE OB TRACK STA 1090. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED CORROSION BETWEEN STA 1090 TO 1110 WITHIN LIMITS PER SRM 53-10-1 FIG 1. REMOVED PIGTAIL STA 1110 TO 1130, BEGAN REPLACEMENT OF TRACK PER MM 53-20-11 FIG 802. OK TO TREAT AND PAINT 1090 TO 1110, INSTALLED TRACK 1110 TO 1130. TREATED AND PAINTED SEAT TRACK STA 1090 TO 1110, AS PER PS 900-3-6. 2L73 4F A3WE 19950901000131995090100013NM 1995 9 1 DL757953458 119950821A7830 REVERSER PANEL HAD18952 BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11685DA 235871 27588 727151 DURING THRU/SERVICING CHECK, FOUND A 6 INCH BY 8 INCH HOLE BURNED THROUGH RT INBOARD REVERSER COLDSTREAM ACOUSTIC PANEL JUST AFT OF INTAKE FOR PNEUMATICS HEAT EXCHANGER COLD AIR AT THE 11 O'CLOCK POSITION. FOUND IMMERSION THERMOCOUPLE BACKED OUT OF MOUNTING HOLE, ALLOWING JET OF HOT AIR TO BURN HOLE IN PANEL. REINSTALLED THERMOCOUPLE AND SAFTIED, FERRIED AC TO ATL WHERE INBOARD REVERSER HALF WAS REPLACED AND ROUTED TO SHOP FOR REPAIRS. 2L72 4F4 FRTA2NM E17NE 19950901000141995090100014NM 1995 9 1 DL76S953466 119950823A335020131A EEL BATTERY PACK BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11117DL 23276 EMER LIGHTS AT AFT ENTRANCE DOORS AND AFT SECTION OF COACH TRACK LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L72 4F RTA1NM 19950901000151995090100015WP 1995 9 1 DLL10953491 119950821A2530120000125 WIRE LKHEED1011 10113851 5265010WP NR 2 OVEN BURNED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO111732D 193C1213 NR 2 OVEN 'B' PHASE FEEDER WIRES AND TERMINAL BLOCK BURNED. RETERMINATED WIRES AND REPLACED OVEN. FLT ATTENDANT REPORTED OVEN OVERHEATING. 2L73 4F A23WE 19950901000161995090100016WP 1995 9 1 DLL13953455 119950822A2720 ROD END 428007 LKHEED1011 10113851 5265010WP RUDDER BROKE A DALAK NONE O OTHER ININSP/MAINT 1 SO11787DL 1902 193A1126 DURING FLT CONTROL CHECK JUST PRIOR TO DEPARTURE, UPPER CONTROL SURFACE DAMPER ON RUDDER BROKE AT ITS ROD END AND DAMAGED SHEET METAL COVER AND ACCESS DOOR ASSY. REPLACED DAMPENER AND ATTACH FITTING ON RUDDER, FLT CONTROL CHECK NORMAL. 2L73 4F A23WE 19950901000171995090100017WP 1995 9 1 DLL13953469 119950821A57431591922 ACTUATOR FITTING LKHEED1011 10113851 5265010WP MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE RT AN LT MLG ACTUATOR ATTACH FITTING WERE FOUND WITH AREAS OF CORROSION. CORROSION WAS REMOVED FROM THE SURROUNDING AREA AND HOLE BORES OF HOLES 1, 2, 3, 4, 17 AND 19 ON THE LT FITTING. ALSO, HOLES 1, 2, 19 AND 18 ON THE RT FITTING. THE HOLES WILL BE REAMED AND BUSHED PER STANDARD SRM PRACTICES AND DL ERA 271413-14 REV B. 2L73 4F A23WE 19950901000181995090100018WP 1995 9 1 DLL13953470 119950821A53201634985 ANGLE LKHEED1011 10113851 5265010WP FS 1043 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11786DL 193A1123 THE WING TO FUSELAGE JOINT FAIL-SAFE ANGLE AFT HOLE OF THE RT UPPER ROOT JOINT AT FS 1043, WAS OVERSIZED TO REMOVE A CRACK INDICATION. THE HOLE WILL BE TREATED FOR CORROSION AND RETURNED TO SERVICE PER DL ERA 271375-14AD. 2L73 4F A23WE 19950901000191995090100019WP 1995 9 1 DLL13953489 119950823A5312 BLKHD ANGLE LKHEED1011 10113851 5265010WP AFT PRESS DOME CRACKED A ADALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11781DL 193A1003 0000 RAPID DEPRESSURIZATION 33,000 FEET, SOURCE UNKNOWN. LOUD BANG, UNABLE TO REGAIN CONTROL OF PRESSURIZATION. ABLE TO HOLD CABIN ALTITUDE TO 7,000 AT A/C ALTITUDE OF 14,000, RETURNED TO LAX. FOUND AFT PRESSURE P-DOME CHORD ANGLE THAT ATTACHED P-DOME TO FUSELAGE STRUCTURE FRACTURED BETWEEN STRINGER NR 10 AND NR 55. CRACK LENGTH WAS APPROXIMATELY 12 FEET, UNDER INVESTIGATION. 2L73 4F A23WE 19950901000201995090100020 1995 9 1 DLL14953463 419950822A22204016608401 MACH FEEL MOTOR LKHEED1011 1011385115 5265015WP AUTO FLT SYST FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11736DY 193C1227 DURING DEPARTURE APPROX 14,000 FT AND 280 KTS MACH FEEL, 1 AND 2 LIGHTS FAILED. LATER MACH TRIM 2 FAILED, RETURNED ATL. REPLACED BOTH MACH FEEL MOTORS, OPERATION NORMAL. 2L73 4F A23WE 19950901000211995090100021NM 1995 9 1 DLM88953501 119950819A2910AS15508240 HYD HOSE DOUG MD88 MD88 3023688NM TAIL COMP LEFT MISROUTED A DALAO OTHER KJHFLUID LOSS WARNING INDICATION ELECT. POWER LOSS-50 PC APAPPROACH 1 SO11995DL 53362 ON APPROACH TO LGA, THE LEFT GEN DROPPED OFF LINE WITH CROSSTIE LOCKOUT MSG ON EOAP. APU WAS STARTED WOULD NOT GO ON BUS. ALSO, HAD LEFT HYDRAULIC SYSTEM LOOSE PRESSURE AND FLUID. FOUND GENERATOR FEEDER CABLES SHORTED TO LEFT HYDRAULIC PRESSURE LINE FROM PUMP TO FILTER MODULE. THE CHAFING OCCURED JUST ABOVE THE FILTER MODULE. REPLACED HYD LINE, FILTER AND PUMP. REPAIRED BURNED A, B, C FEEDER CABLES FROM R5-2 TO S3-280, OPERATION NORMAL. 2L72 4F RTA6WE 19950901000221995090100022WP 1995 9 1 MWEA95271 119950823A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP FWD GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31602ME 48133 CREW REPORTS, GALLEY EVACUATION SLIDE COVER FELL OFF AT GATE. MAINTENANCE RESECURED GALLEY EVAC SLIDE COVER AND REMOVED A/C TO SERVICE. 2L72 4F A6WE 19950901000231995090100023NM 1995 9 1 P5CA9500718 119950824A5350 RADOME BOEING747 747121 1384871NM NOSE DELAMINATED A P5CAK NONE O OTHER APAPPROACH 1 WP23832FT 20347 NOSE RADOME HIT BY BIRD ON LANDING. THE TOP SECTION BS 114, 9 INCH DIAMETER OF DELAMINATION, NO BROKEN SKIN INSIDE OR OUT. ENGINEERING REVIEWED OK FOR FLIGHT TO MAINTENANCE BASE FOR RADOME REPLACEMENT. 2L74 4F A20WE 19950901000241995090100024EU 1995 9 1 QXEA9500265 119950824A3350 EEL WIRE FOKKER FOKKERF28 F28MK1000 4990808EU CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09803PH 11031 BOI - FORWARD THREE SEGMENTS OF FLOOR PROXIMITY LIGHTING ARE INOP. REPAIRED GROUND WIRE AT BATTERY PACK CANNON PLUG. FLOOR PROXIMITY LIGHTING OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19950901000251995090100025WP 1995 9 1 QXEA9500266 219950824A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RIGHT FAILED A QXEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 NM0926952 AC661 P44308 FCA - RIGHT ENGINE FAILED ON APPROCH TO FCA. AIRCRAFT LANDED IN FCA WITHOUT FURTHER PROBLEM. RIGHT ENGINE REPLACED I/A/W MAINTENANCE MANUAL AND OPS CHECKED GOOD ON GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. AWAITING ENGINE TEARDOWN FOR CAUSE. 1L72 4T4 T A8SW E4WE 19950901000261995090100026NM 1995 9 1 QXEA9500267 119950824A2121 FAN DORNERDO32 DO328100 2996000NM AVIONICS FAILED A QXEAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM09335PH 3013 SEA - BURNING ELECTICAL ODOR IN COCKPIT AFTER TAKEOFF. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT FURTHER PROBLEMS. ODOR TRACED TO AVIONICS FAN AND FAN FAIL CAS MESSAGE WAS ANNUNCIATED DURING THE COURSE OF TROUBLESHOOTING. FAN PLACED ON MEL 21-6. 2H72 4T RTA45NM 19950901000271995090100027NM 1995 9 1 SCNA95175 119950822A3350900542 EEL BATTERY PACK BOEING727 7272A1 138407FNM RT OVERWING DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE EXTERIOR RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE DIM. REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY AT M956, THE LIGHT TESTED GOOD. 2L73 4F A3WE 19950901000281995090100028WP 1995 9 1 95ZZZW808 119950619A3230 LOWER STOP CABLE DOUG DC9 DC931 3022065WP LOWER NLG BROKEN A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19965VJ 47374 DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION. ALL INDICATIONS WERE NORMAL. FLIGHT RETURNED TO DCA. MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK. OPERATIONS CHECKED GOOD. REF USAA950617, 95ZZZW809, 95ZZZW810. 2L72 4F A6WE 19950901000291995090100029WP 1995 9 1 95ZZZW809 119950619A3230 SPRING TENSION DOUG DC9 DC931 3022065WP LOWER NLG BROKEN A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19965VJ 47374 DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION. ALL INDICATIONS WERE NORMAL. FLIGHT RETURNED TO DCA. MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK. OPERATIONS CHECKED GOOD. REF USAA950617, 95ZZZW808, 95ZZZW810. 2L72 4F A6WE 19950901000301995090100030WP 1995 9 1 95ZZZW810 119950619A3230 DOOR LINK DOUG DC9 DC931 3022065WP FORWARD BROKEN A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19965VJ 47374 DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION. ALL INDICATIONS WERE NORMAL. FLIGHT RETURNED TO DCA. MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK. OPERATIONS CHECKED GOOD. REF USAA950617, 95ZZZW808, 95ZZZW809. 2L72 4F A6WE 19950901000311995090100031WP 1995 9 1 95ZZZW811 119950629A2913 PRESS FILTER DOUG DC9 DC981 3022081WP RT INOPERATIVE A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19827US 48049 MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FILTER. OPERATIONS CHECKED GOOD. REF USAA950649, 95ZZZW812, 95ZZZW813. 2L72 4F A6WE 19950901000321995090100032WP 1995 9 1 95ZZZW812 119950629A2912 DRAIN FILTER DOUG DC9 DC981 3022081WP RT INOPERATIVE A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19827US 48049 MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FILTER. OPERATIONS CHECKED GOOD. REF USAA950649, 95ZZZW811, 95ZZZW813. 2L72 4F A6WE 19950901000331995090100033WP 1995 9 1 95ZZZW813 119950629A2912 RTN LINE FILTER DOUG DC9 DC981 3022081WP RT INOPERATIVE A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19827US 48049 MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FILTER. OPERATIONS CHECKED GOOD. REF USAA950649, 95ZZZW811, 95ZZZW12. 2L72 4F A6WE 19950901000341995090100034WP 1995 9 1 ASAA9580152 119950627A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950901000351995090100035WP 1995 9 1 ASAA9580153 119950628A5210 MECHANISM DOUG DC9 DC982 3022082WP L1 DOOR BINDING A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01936AS 49363 SEA - FLT 530 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT LOCK CLOSED. FREED AND LUBRICATED THE INTERLOCK MECHANISM AND DOOR OPERATED NORMALLY. (W) 2L72 4F A6WE 19950901000361995090100036WP 1995 9 1 ASAA9580156 119950701A33501001191 EEL ASSY DOUG DC9 DC983 3022083WP L1 DOOR MALFUNCTIONED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01975AS 53451 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR PORTABLE EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH UNLESS SWITCH ON LIGHT CYCLED. REPLACED L1 DOOR PORTABLE EMERGENCY EXIT LIGHT AND OPERATED NORMALLY. (W) 2L72 4F RTA6WE 19950901000371995090100037WP 1995 9 1 ASAA9580157 119950704A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, THE AFT QUARTER OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. FOUND WIRE PULLED OUT OF SPLICE AT TRACK, RECRIMPED WIRING AND LIGHTS OPERATED NORMALLY. (W) 2L72 4F A6WE 19950901000381995090100038WP 1995 9 1 ASAA9580158 119950706A33501001191 EEL ASSY DOUG DC9 DC982 3022082WP L1 DOOR DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01940AS 49825 LAX - DURING A8 CHECK, THE FORWARD L-1 PORTABLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (W) 2L72 4F A6WE 19950901000391995090100039EU 1995 9 1 AWXA9500437 119950711A3350 EEL CONNECTOR AIRBUS320 A320231 3930325EU CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28637AW 099 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT ROW OF EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED CONNECTOR ON WALL AT AFT ROW, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950901000401995090100040NM 1995 9 1 AWXA9500438 119950712A3350 LIGHT BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHT BROKEN AT ROW 10. REINSTALLED LIGHT, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950901000411995090100041NM 1995 9 1 AWXA9500439 119950713A335020121A EEL BATT CHARGER BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN. REPLACED RT BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950901000421995090100042EU 1995 9 1 AWXA9500440 119950713A3350321452 EEL BATTERY AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28627AW 66 PHX - DURING ROUTINE MAINTENANCE CHECK, RT MID CABIN BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY, OPS CHECK GOOD. (W) 2L72 4F RTA28NM 19950901000431995090100043NM 1995 9 1 AWXA9500441 119950715A7722 EGT BOEING737 7373S3 1384711NM NR 2 ENGINE HIGH A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28313AW 23712 CMH - FLT 843 - THE NR 2 ENGINE HIGH EGT OCCURRED DURING TAKEOFF AND CLIMB, TEMP REACHED 936 DEGREES FOR 11 SECONDS. CREW RETURNED AC TO CMH AND LANDED UNEVENTFULLY. MX PERFORMED ENGINE PERFORMANCE GROUND RUN AND AVIONICS PERFORMED TEST OF EGT HARNESS, NO FAULTS WERE NOTED ON EITHER TEST. MX ELECTED TO DERATE BOTH ENGINES TO B1 POWER. AC RELEASED FOR FURTHER SERVICE. (W) 2L72 4F RTA16WE 19950901000441995090100044NM 1995 9 1 AWXA9500442 119950714A3350 EEL BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND NUMEROUS EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED LIGHTS FROM 3L TO 16L, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950901000451995090100045 1995 9 1 AWXA9500443 419950716A2250 EEL WIRING BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 THROUGH ROW 18. RESECURED LOOSE WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950901000461995090100046NM 1995 9 1 AWXA9500444 119950714A5315 FLOORBEAM BOEING737 7372M8 1384483NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28141AW 21955 PHX - DURING SCHEDULED C6 INSPECTION, FOUND FLOORBEAM WEB CRACKED, STA 639 RBL 64 BELOW STR 17. REPAIRED CRACK PER ER 2 53 14 35A. (W) 2L72 4F A16WE 19950901000471995090100047NM 1995 9 1 AWXA9500445 119950714A5730 SKIN BOEING737 7372M8 1384483NM WS 103.5 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28141AW 21955 PHX - DURING SCHEDULED C6 INSPECTION, WING STA 103.5 O/B AFT TWO FASTENERS D AND E, FAILED LFEC INSPECTION. REPAIRED CRACKED FASTENER HOLE PER ER 2 57 33 02. (W) 2L72 4F A16WE 19950901000481995090100048NM 1995 9 1 AWXA950714 119950714A5311 FRAME BOEING737 7372M8 1384483NM BS 639 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28141AW 21955 PHX - DURING SCHEDULED C6 INSPECTION, FOUND MAIN FRAME CRACKED AT STA 639, RT SIDE JUST BELOW EMERGENCY EXIT DOOR LOWER SILL. REPAIRED CRACK PER ER 2 53 14 35A. (W) 2L72 4F A16WE 19950901000491995090100049WP 1995 9 1 USAA950617 119950619A3230 UPPER STOP CABLE DOUG DC9 DC931 3022065WP UPPER BROKEN A USAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 EA19965VJ 47374 DCA - FLT 481 - UPON RETRACTING THE GEAR, A LOUD NOISE WAS HEARD AROUND THE NOSE GEAR AREA FOLLOWED BY A VIBRATION. ALL INDICATIONS WERE NORMAL. FLIGHT RETURNED TO DCA. MAINTENANCE REPLACED THE UPPER NOSE LANDING GEAR DOOR STOP CABLE, THE LOWER CABLE, SPRING TENSION AND FORWARD NOSE LANDING GEAR DOOR LINK. OPERATIONS CHECKED GOOD. REF 95ZZZW808, 95ZZZW809, 95ZZZW810. 2L72 4F A6WE 19950901000501995090100050WP 1995 9 1 USAA950630 119950522A53129912243501 BULKHEAD DOUG DC9 DC931 3022065WP BS 965 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND .5 INCH CRACK AND BUCKLING AT 965 RT BULKHEAD BETWEEN LONGERON 17R AND 18R FLOOR LEVEL. SPLICED IN NEW WEB SECTION FROM LONGERON 18R TO 17R PER SRM 53-03 FIG 19 AND USAIR EA 30491. (W) 2L72 4F A6WE 19950901000511995090100051WP 1995 9 1 USAA950631 119950523A5330 SKIN DOUG DC9 DC931 3022065WP BS 208 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND GOUGED OUT OF LIMITS AT STA 208 FROM LONGERON 1L TO AND BETWEEN LONGERON 1R AND LONGERON 2R. BURNISHED AREA AND INSTALLED TWO DOUBLERS PER SRM 53-04 FIG 38 NR 4 EFG. (W) 2L72 4F A6WE 19950901000521995090100052WP 1995 9 1 USAA950632 119950523A5320 BEAM DOUG DC9 DC931 3022065WP RT MLG WW CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 1.5 INCH BY .050 DEEP CHAFE AFT FACE OF BEAM OF RT WING SHELF INBED OF THE SERVICE INTERPHONE JACK IN RT MLG WW. ROUTED OUT DAMAGED AREA AND INSTALLED A DOUBLER REPAIR PER SRM 53-01. (W) 2L72 4F A6WE 19950901000531995090100053WP 1995 9 1 USAA950633 119950525A5311 FRAME DOUG DC9 DC931 3022065WP BS 1076 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY .5 INCH CHAFED AREA OUT OF LIMITS ON BELTFRAME STA 1076 LONG 14L. CUT OUT DAMAGED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 2A. (W) 2L72 4F A6WE 19950901000541995090100054WP 1995 9 1 USAA950634 119950525A5230 SKIN DOUG DC9 DC931 3022065WP FWD CARGO DOOR DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 2 INCH BY 10 INCH DENT FWD CARGO DOOR EXTERIOR SKIN UNDER DOOR HANDLE. INSTALLED DOUBLER REPAIR PER SRM 52-05 FIG 30. (W) 2L72 4F A6WE 19950901000551995090100055WP 1995 9 1 USAA950635 119950530A5330 SKIN DOUG DC9 DC931 3022065WP BS 256-280 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 4815W PIT - DURING Q-t/CX-5 INSPECTION, FOUND 2 , 20 INCH BY 6 INCH BY .375 INCH DEEP DENTS AND 1.5 INCH CRACK BETWEEN STA 256 TO 294 AND LONGERON 20R AND 21R APPROX STA 280. CUT OUT DAMAGED AREA AND INSTALLED FILLER DOUBLER AND TAPERED SHIMS PER USAIR EA NR 30552. (W) 2L72 4F A6WE 19950901000561995090100056WP 1995 9 1 USAA950649 119950629A2913AS66411LS666 PUMP DOUG DC9 DC981 3022081WP RT INOPERATIVE A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19827US 48049 MCO - FLT 944 - EN ROUTE, AC LOST THE RT HYDRAULIC QUANTITY. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PRESSURE LINE FILTER, THE CASE DRAIN FILTER AND HYDRAULIC SYSTEM RETURN LINE FILTER. OPERATIONS CHECKED GOOD. REF 95ZZZW811, 95ZZZW812, 95ZZZW813. 2L72 4F A6WE 19950901000571995090100057WP 1995 9 1 USAA950732 119950607A2560 SLIDE DOUG DC9 DC982 3022082WP TAIL CONE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19824US 49143 BDL - THE TAIL CONE WAS INADVERTENTLY RELEASED. THE EVACUATION SLIDE FAILED TO DEPLOY. MAINTENANCE REINSTALLED THE TAIL CONE AND PERFORMED AN ADJUSTMENT TEST, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD. (W) 2L72 4F A6WE 19950901000761995090100076CE 1995 9 1 95ZZZX4331 119950728A323050810354 GUIDE ROD BEECH 99 B99 1154004CE LT MLG DOWNLOCK BROKEN A ATIMAK NONE O OTHER TXTAXI/GRND HDL 1 NM07950AA U159 AIRCRAFT WAS TAXIING WHEN THE LEFT GEAR FOLDED UP. THE AIRCRAFT WAS JACKED UP BY MAINTENANCE PERSONNEL AND THEY FOUND THE DOWNLOCK SPRING GUIDE ROD BROKEN IN TWO. THE SPRING GUIDE ATTACHES BETWEEN THE DOWNLOCK HOOK (PN 50-810338-1) AND THE MLG ACTUATOR (PN 99-810057-651). SEE BEECHCRAFT B-99 PARTS MANUAL, FIGURE 201, ITEMS 8, 31, AND 33 FOR BREAKDOWN. THIS ALLOWED THE OVERCENTER LOCK (PN 50-810338-1) TO WORK FREE AND THE GEAR TO FOLD. DAMAGE WAS TO THE LEFT ENGINE (PROP STRIKE) AND LEFT WING TIP. AIRCRAFT IS CURRENTLY AOG FOR REPAIRS. TSO CYCLES, 440. 1L72 3T A14CE 19950901000901995090100090NM 1995 9 1 95ZZZX4345 119950709A2844 FUEL PRESS WARN DORNERDO32 DO328100 2996000NM COCKPIT ACTIVATED A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07328JS 3030 FLT 4147 - CREW ABORTED TAKEOFF AFTER RECEIVING FUEL LOW PRESSURE - C.A.S. MESSAGE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK ON THE SYSTEM IAW DO328 MM 28-00-00, COULD NOT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950901000911995090100091CE 1995 9 1 95ZZZX4346 119950702A27506046H39 RELAY BEECH 1900 1900C 1154161CE TE FLAPS FAILED A MASAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW01155YV UC155 DURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LEFT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED HIS APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN INDICATOR LAMP AND FLAP MOTOR RELAY. AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL NR SW019515. 2L72 4T RTA24CE 19950901000921995090100092WP 1995 9 1 CAL950637 119950803A3260 POSTION SENSOR DOUG DC9 DC982 3022082WP NLG OUT OF ADJUST A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0918835 49439 IAH - FLT 0664 - THE AIRCRAFT HAD A BRIEF HISTORY OF THE NLG RED UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. MAINTENANCE FOUND THE NOSE GEAR UP/DOWN POSITION SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED PER MM 32-60-05 AND OPERATION CHECKED GOOD. THE AIRCRAFT HAS FLOWN OVER 10 FLIGHTS WITHOUT A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. (X) 2L72 4F A6WE 19950901000931995090100093WP 1995 9 1 CAL950638 119950801A3350 EEL GROUND WIRE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0972824 49824 CLE - INSPECTION FOUND THE LT AND RT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE DURING 'A' CHECK. THE GROUND WIRE AT STUD IN FRAME SECTION WAS FOUND READING 20,000 OHMS. THE TERMINAL END WAS REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHTS CHECKED GOOD. (X) 2L72 4F A6WE 19950901000941995090100094WP 1995 9 1 CAL950642 119950722A3350VR4D EEL BATTERIES DOUG DC9 DC932 3022066WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09541NY 45793 HOU - INSPECTION FOUND THE FIRST CLASS AND FORWARD COACH OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THE BATTERIES DISCHARGED. THE BATTERIES WERE CHARGED AND OPERATION OF THE OVERHEAD EMERGENCY LIGHTS WAS RESTORED. (X) 2L72 4F A6WE 19950901000951995090100095NM 1995 9 1 CAL950647 119950803A5330 SKIN BOEING727 727243 138408DNM BS 950B GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW093441536801 22167 DEN - A GOUGE MEASURING 1.25 INCHES LONG BY 0.05 INCH WIDE BY 0.046 INCH DEEP WAS FOUND IN SKIN 5.5 INCHES FORWARD OF STA 950B AT STR 29L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 3 AND ECRA 5330-02308. (X) 2L73 4F RTA3WE 19950901000961995090100096NM 1995 9 1 CAL950648 119950802A5210 FRAME BOEING727 727243 138408DNM L-2 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093441536801 22167 DEN - INSPECTION FOUND A .75 INCH CRACK IN UPPER AFT CORNER OF L-1 DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW ECRA 552C062. (X) 2L73 4F RTA3WE 19950901000971995090100097NM 1995 9 1 CAL950652 119950723A335020131A EEL BATTERY PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0969311 23362 HOU - THE R-2 DOOR OVERHEAD EMERGENCY EXIT SIGN BATTERY PACK FAILED THE 15 MINUTE DURATION TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT SIGN WAS RESTORED. (X) 2L72 4F RTA16WE 19950901000981995090100098NM 1995 9 1 CAL950653 119950723A335020131A EEL BATTERY PACK BOEING737 7373T0 1384582NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0969311 23362 HOU - THE AFT CABIN EMERGENCY AISLE LIGHTING BATTERY PACK FAILED THE 15 MINUTE DURATION TEST. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY AISLE LIGHTING WAS RESTORED. (X) 2L72 4F RTA16WE 19950901000991995090100099NM 1995 9 1 EIAA9537 119950808A3244 TIRES BOEING747 747273C 1384896NM NR 11/12 BLOWN A EIAAK NONE O OTHER LDLANDING 1 NM09471EV 20651 HKG - NR 11 AND NR 12 TIRES FOUND TO BLOWN ON LANDING IN VHHH. (M) 2L74 4F A20WE 19950901001001995090100100 1995 9 1 ORJA9567 419950725A3442 ANTENNA DOUG DC9 DC983 3022083WP RADAR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11836RA 53046 MINOR CORROSION ON FORWARD AND AFT FACE OF RADAR DISH. REMOVED CORROSION AND TREATED PER REFERENCE 51-10-3. (X) 2L72 4F RTA6WE 19950901001011995090100101WP 1995 9 1 ORJA9568 119950726A5320 THRESHOLD DOUG DC9 DC983 3022083WP CARGO COMPT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11836RA 53046 FORWARD PIT DOOR THRESHOLD CORRODED. TREATED AND PRIMED AREAS OF CORROSION. REMOVAL PER SRM 51-10-3. (X) 2L72 4F RTA6WE 19950901001021995090100102WP 1995 9 1 ORJA9569 119950802A32608326098002 PROX BOX DOUG DC9 DC987 3022087WP LT MLG INOPERATIVE A ORJAO OTHER N FALSE WARNING APAPPROACH 1 WP11750RA 49777 WHEN LANDING GEAR WAS LOWERED NO LIGHT CAME ON, ON LEFT MAIN. WHEN NOSE AND RIGHT BECAME GREEN, LEFT BECAME RED. EMERGENCY EXTENSION PROCEDURE ACCOMPLISHED. LEFT MAIN REMAINED RED. REMOVED AND REPLACED PROX BOX PER MM CHAP 32. OPS CHECK NORMAL. (M) 2L72 4F RTA6WE 19950901001031995090100103EU 1995 9 1 PLGA725952G 119950726A52307252300041 SEAL SAAB SF340 340B 7860101EU CARGO DOOR TORN A PLGAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 NE05352BE 340B239 YYZ/IAD - FLT 4897 - AT 23,000 FEET CRUISE ALTITUDE, THE CABIN ALTITUDE WARNING SYSTEM SOUNDED. THE CREW PERFORMED AN EMERGENCY DESCENT LANDING IN IAD WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THE CARGO DOOR SEAL HAD COME LOOSE AND WAS TORN. IAD MAINTENANCE SECURED THE SEAL AND DEFERRED THE PRESSURIZATION PER THE MEL AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T RTA52EU 19950901001041995090100104NE 1995 9 1 PLGA72595G1 219950727A72305036TAP02 ROD END SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE FAILED A PLGACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 NE05346BE 340A150 367510 YHZ/BOS - FLT 4733 - DURING TAKEOFF ROLL, RIGHT ENGINE TORQUE AND NP INDICATION DROPPED WITH AN INCREASE IN ITT. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT WHERE TROUBLESHOOTING REVEALED THE ROD END TO THE INLET GUIDE VANE LINK HAD FAILED ALLOWING THE GUIDE VANES TO CLOSE. MAINTENANCE REPLACED THE CONTROL LINK AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2L72 4T4 TRTA52EU E8NE6 19950901001051995090100105CE 1995 9 1 SW019515 119950702A32601864 INDICATOR LAMP BEECH 1900 1900C 1154161CE LT MLG FAILED A MASAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW01155YV UC155 DURING APPROACH INTO PITTSBURGH, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A LEFT MAIN DOWN AND LOCK INDICATION. AFTER PILOT ABORTED HIS APPROACH, FLAPS WERE SELECTED UP, BUT REMAINED IN 'LANDING' POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN INDICATOR LAMP AND FLAP MOTOR RELAY. AIRCRAFT WAS THEN RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX4346. (X) 2L72 4T RTA24CE 19950901001061995090100106NM 1995 9 1 WRLA95038 119950726A24305D00245150 RCCB DOUG MD11 MD11 3023602NM DC EMERGENCY PWRTRIPPED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27273WA 48519 DURING TAXI-OUT, CAPTAIN NOTED REMOTE CONTROL CIRCUIT BREAKER ALERT. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL SHUT DOWN ENGINE AND PERFORMED RETURN TO SERVICE TEST. OPS CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19950901001071995090100107WP 1995 9 1 9512909998 119950817A5220 DOOR PAN DOUG DC9 DC931 3022065WP LT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND LEFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT UPPER AFT STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31. 2L72 4F A6WE 19950901001081995090100108WP 1995 9 1 9512919998 119950817A5220 DOOR PAN DOUG DC9 DC931 3022065WP RT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND RIGHT AFT EMERGENCY EXIT DOOR PAN CRACKED AT LOWER FORWARD END. REPLACED DOOR, MFG PART NUMBER 5910159-31. 2L72 4F A6WE 19950901001091995090100109WP 1995 9 1 9512929998 119950817A5220 DOOR PAN DOUG DC9 DC931 3022065WP RT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND RIGHT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT UPPER FORWARD STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31. 2L72 4F A6WE 19950901001101995090100110WP 1995 9 1 9512939998 119950817A5220 DOOR PAN DOUG DC9 DC931 3022065WP LT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND LEFT AFT FORWARD EMERGENCY EXIT DOOR PAN CRACKED AT LOWER FORWARD STOP. REPLACED DOOR, MFG PART NUMBER 5910159-31. 2L72 4F A6WE 19950901001111995090100111WP 1995 9 1 9512949991 119950817A5330 SKIN DOUG DC9 DC931 3022065WP FS 965 DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK, FOUND SKIN DAMAGE AT PRESSURE CAP AT UPPER PYLON SPAR CAP FS 965 RIGHT SIDE. REPAIRED PYLON SPAR CAP PER EA 99-1102703. 2L72 4F A6WE 19950901001121995090100112WP 1995 9 1 9512959969 119950817A5220 DOOR PAN DOUG DC9 DC931 3022065WP LT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT DOOR PAN CRACKED AT TOP EDGE FORWARD SUPPORT AREA. STOP DRILLED CRACK, FABRICATED DOUBLER, AND INSTALLED DOUBLER AND WEB PER EA 99-09711. 2L72 4F A6WE 19950901001131995090100113WP 1995 9 1 9512969163 119950819A5220 DOOR FLANGE DOUG DC9 DC914 3022034WP LT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND LEFT OVERWING EMERGENCY EXIT DOOR CRACKED AT AFT LOCKING PIN FLANGE. REPAIRED CRACK PER SRM 52-05 FIG 51 VIEW H. PERMANENT REPAIR WILL BE ACCOMPLISHED AT NEXT PERIODIC CHECK. 2L72 4F A6WE 19950901001141995090100114WP 1995 9 1 9512979994 119950821A5414 SKIN DOUG DC9 DC931 3022065WP RT PYLON DAMAGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018979E 47328 DURING ACCEPTANCE CHECK, FOUND RIGHT PYLON TRAILING EDGE SECTION LOWER SKIN TO SECOND RIB WITH ELEVEN LOOSE FASTENERS AT END OF RIB. REPAIRED LOWER SKIN SECTION PER EA 99-094743 AND SRM 51-30-2. 2L72 4F A6WE 19950901001151995090100115WP 1995 9 1 9512989991 119950821A5320 PRESS PANEL DOUG DC9 DC931 3022065WP FS 83 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK, FOUND COCKPIT PRESSURE PANEL CRACKED AT FS 83. FABRICATED DOUBLER AND INSTALLED PER EA 99-102726. 2L72 4F A6WE 19950901001161995090100116WP 1995 9 1 9512999991 119950821A5313 STRINGER DOUG DC9 DC931 3022065WP FS 207 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK, FOUND LONGERON 15L TO FRAME ATTACHMENT STRAP CRACKED AT FS 207. FABRICATED FILLER AND DOUBLER AND INSTALLED PER EA 99-094137. 2L72 4F A6WE 19950901001171995090100117WP 1995 9 1 9513009984 119950817A5754 BRACKET DOUG DC9 DC932 3022066WP RT INBD FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01894US 47383 DURING LINE MAINTENANCE CHECK, FOUND RIGHT INBOARD FLAP FAIRING INBOARD SIDE BRACKET CRACKED. STOP DRILLED CRACK PER EA 99-096778. PERMANENT REPAIR WILL BE ACCOMPLISHED WITHIN 30 CALENDAR DAYS FROM 17 AUG 95. 2L72 4F A6WE 19950901001181995090100118WP 1995 9 1 9513019946 119950822A5330 SKIN DOUG DC9 DC931 3022065WP FS 148-150 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK, FOUND SKIN CRACKED BETWEEN FS 148 AND 150, LONGERON 27L. FABRICATED DOUBLER AND INSTALLED PER EA 99-102752 AND SRM 53-04 FIG 8. 2L72 4F A6WE 19950901001191995090100119WP 1995 9 1 9513029163 119950822A5312 BULKHEAD DOUG DC9 DC914 3022034WP AFT FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AROUND PERIMETER OF PLUG DOOR OPENING. STOP DRILLED CRACK AT LOWER LEFT RADIAL NR 16. REPAIRED RIGHT UPPER RADIAL PER SB 53-127. 2L72 4F A6WE 19950901001201995090100120WP 1995 9 1 9513039163 119950822A5330 SKIN DOUG DC9 DC914 3022034WP FS 585-642 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND THREE SKIN CRACKS AT FS 585, FS 623 AND FS 642. REPAIRED PER EA 91-097634 SEC 1 AND SEC 2, PERMANENT REPAIR WILL BE ACCOMPLISHED IN ONE YEAR FROM 24 AUG 95. 2L72 4F A6WE 19950901001211995090100121EU 1995 9 1 95FDEA01200 119950825A3411 PITOT SYST AIRBUS310 A310200 3930310EU LT/RT DIRTY A FDEAA UNSCHED LANDING I FLT. ATTITUDE INST. TOTAKEOFF 1 SO25401FE 501 ON T/O AT ONT, BOTH AIRSPEED INDICATORS BECAME ACTIVE AND CK'D AT 80 KTS AT 200 FT ABOVE GRD. AIRSPEED DROPPED OFF ON APPROACH A/S WAS 40 TO 60 KTS BELOW PFD SPEED, NO OTHER PRESSURE GAUGES WAS ALT OR VSI WERE EFFECTED BOTH A/S INDICATORS SHOWED THE PROBLEM. FLUSHED STANDBY TOTAL PRESSURE SYS PER 34-1000 PG 302, LEAKED CK OF STANDBY PITOT SYS PER 34-10-0 P 548 AND 549 NORMAL. 2L72 4F RTA35EU 19950901001221995090100122NM 1995 9 1 95FDEA01201 119950825A5315BAC1505100617 FLOORBEAM BOEING727 72725 1384006NM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C235-02), ON FLOORBEAM UPPER FLANGE BS 620 RBL 8 TO 17 WL 208. REMOVED AND REPLACED UPPER FLOORBEAM T-CHORD BS 620 LBL 15 RBL 34 PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19950901001231995090100123NM 1995 9 1 95FDEA01202 119950828A712065C8067891 FITTING BOEING727 7272S2F 1384O81NM CTR ENGINE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 CENTER ENGINE REAR SUPPORT FITTING ASSEMBLY IS BADLY CORRODED. REMOVED AND REPLACED CENTER ENGINE REAR SUPPORT FITTING IAW FEDEX SRM 51-30-2, 51-30-4 AND FEDEX MM 71-21-1. 2L73 4F A3WE 19950901001241995090100124NM 1995 9 1 95FDEA01203 119950828A57556517348107A TE SKIN BOEING727 7272S2F 1384O81NM NR 5 SPOILER DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25215FE 22936 DELAM ON TRAILING EDGE OF NR 5 SPOILER. REPAIRED NR 5 SPOILER IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950901001251995090100125NM 1995 9 1 95FDEA01204 119950828A53207075T6 DELTA BEAM WEB BOEING727 727232 1384082NM BS 790 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 IN THE LOWER A/C BAY AT BS 790 RBL 5 WL 148 THERE IS CORROSION ON THE DELTA BEAM WEB. REMOVED DAMAGED SECTION. FABRICATED REPAIR DOUBLER & FILLER PER FEDEX SRM 51-40-02. INSTALLED DOUBLER & FILLER PER FEDEX SRM 51-30-02. APPLIED SKYDROL RESISTANT FINISH & APPLIED 2PS 3 TO CLEANED AREAS, ON DELTA BEAM WEB. 2L73 4F A3WE 19950901001261995090100126NM 1995 9 1 95FDEA01205 119950828A53117075T3 FRAME BOEING727 727227 1384078NM BS 560 CRACK A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 IN THE FWD CARGO BAY THE UPPER FLANGE OF FRAME IS CRACKED AT BS 560 RBL 2, WL 154. REPAIRED UPPER FLANGE OF FRAME AT BS 560 RBL 2 WL 154 IAW SRM 51-40-3. 2L73 4F A3WE 19950901001271995090100127NM 1995 9 1 95FDEA01206 119950827A532065562399 SPLICE BOEING727 727227 1384078NM BS 648-664 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON STR 26R BS 648-664 AND ON STR SPLICE HAT AT BS 680. REMOVED CORROSION WITHIN DAMAGE LIMITATION ON STR AND REPLACED STR SPLICE HAT AT BS 680 STR 26R ALL WORK IAW SRM 51-40-3. 2L73 4F A3WE 19950901001281995090100128NM 1995 9 1 95FDEA01207 119950828A5210M4592142024T3 GATE BEAM BOEING727 727233 138408ANM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FWD ENTRY DOOR LOWER GATE BEAM IS CRACKED AT FWD CORNER STOP FITTING, APPROX 1 INCH LENGTH. REPAIRED CRACK IN FWD ENTRY DOOR LOWER GATE BEAM IAW FEDEX EA 7-3210-25602. 2L73 4F RTA3WE 19950901001291995090100129NM 1995 9 1 95FDEA01208 119950828A5330M4391082024T3125SKIN BOEING727 727233 138408ANM BS 620 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 BS 620 STR 24R AND 25R THERE IS A LIGHTNING STRIKE ON EXTERIOR SKIN. BLENDED OUT LIGHTNING STRIKE, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-30-1. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER AND FILLER, ALL WORK WAS DONE IAW FEDEX SRM 53-30-3, 53-30-1. 2L73 4F RTA3WE 19950901001301995090100130NM 1995 9 1 95FDEA01209 119950828A5315BAC1505106617 FLOORBEAM BOEING727 727233 138408ANM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CORROSION ON TOP CHORD OF BS 1110 FLOORBEAM RBL 8 TO 55 LBL 47 TO 55 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1110 RBL 8 LBL 55 WL 208. TOP CHORD WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED TOP CHORD OF 1110 FLOORBEAM FROM LBL 17.5 TO RBL 76 WL 208 PER FEDEX SRM 53-1-8. 2L73 4F RTA3WE 19950901001311995090100131NM 1995 9 1 95FDEA01210 119950828A53157075T6 FLOORBEAM BOEING727 727233 138408ANM BS 1030 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CORROSION (72C237-02), ON TOP CHORD OF BS 1030 FLOORBEAM RBL 9 TO 22 LBL 51.5 WL 208. MECHANICALLY REMOVED CORROSION FROM TOP CHORD OF FLOORBEAM AT BS 1030 RBL 9 TO 22 LBL 51.5 AREA WAS OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED TOP CHORD OF FLOORBEAM AT BS 1030 LBL 51.5 WL 208 PER FEDEX EA 7-5310-25603. 2L73 4F RTA3WE 19950901001321995090100132NM 1995 9 1 95FDEA01211 119950826A5315BAC1518388 FLOORBEAM BOEING727 727233 138408ANM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CORROSION ON TOP CHORD OF FLOORBEAM BS 1070 AT LBL 13 LBL 47.5 TO 54 RBL 15 TO 52 WL 208. CUT OUT DAMAGED UPPER CHORD OF FLOORBEAM FROM LBL 65 RBL 65 AND REPAIRED PER SRM 53-10-08 FIG 3. 2L73 4F RTA3WE 19950901001331995090100133NM 1995 9 1 95FDEA01212 119950822A5347BAC1529792 SEAT TRACK BOEING727 727233 138408ANM BS 1050-1090 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CORROSION ENTIRE LENGTH OF I/B FLANGE OF SEAT TRACK BS 1050 TO 1090 WL 208 LBL 45. FOUND CORROSION TO GO ALL THE WAY THROUGH THE SEAT TRACK. REMOVED CORRODED TRACK, INSTALLED NEW TRACK. 2L73 4F RTA3WE 19950901001341995090100134NM 1995 9 1 95FDEA01213 119950828A53302024T3 SKIN BOEING727 727227 1384078NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION (71C209-02), ON SKIN BS 950F PLUS 12 TO 974, BETWEEN STR 29 AND 30R AFT CARGO BAY. CUT OUT DAMAGED AREAS OF SKIN FROM BS 950F PLUS 12 TO 974, BETWEEN STR 29 AND 30R. REPAIRED CUT OUT AREAS IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950901001351995090100135NM 1995 9 1 95FDEA01214 119950826A531465C80006206 KEEL BEAM BOEING727 727227 1384078NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 CORROSION ON O/B FLANGE OF STR 29R BS 950E KEEL BEAM. DURING CORROSION REMOVAL DISCOVERED A CRACK RUNNING CLEAR THROUGH KEEL BEAM LOWER FLANGE FROM RADIUS TO RADIUS, AT BS 950E PLUS 3.5 STR 29R CRACK WAS 1.5 LONG. CUT OUT SKIN FOR ACCESS AND REMOVED KEEL BEAM FROM BS 950 TO 980. REPLACED KEEL BEAM AND REPAIRED SKIN CUT OUT PER SRM 53-30-3 FIG 3 AND FEDEX EA 7-5310-25557. 2L73 4F A3WE 19950901001361995090100136NM 1995 9 1 95FDEA01215 119950828A53157075T6 FLOORBEAM BOEING727 727227 1384078NM BS 1110 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 WHILE WORKING NR O652 DISCOVERED DAMAGE TO FLOORBEAM WEB AT BS 1110 BL 0 WL 207. PREVIOUSLY CAUSED DURING INSTALLATION OF HAYES CARGO MOD. REPAIRED FLOORBEAM PER FEDEX EA 7-5310-25620. 2L73 4F A3WE 19950901001371995090100137WP 1995 9 1 ABXA9500679 119950824A7933715447 OIL TEMP REG DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 4 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN M OVER TEMP CRCRUISE 1 GL23801AX 46077 669266 NR 4 ENGINE OIL TEMPERATURE WENT UP TO AND STAYED AT 140 DEGREES. INCREASED POWER FROM CRUISE TO MCT, TEMPERATURE DECREASED TO 134 DEGREES AFTER 15 MINUTES. CREW SECURED THE NR 4 ENGINE, SECURE TIME WAS 0515 Z, WINDMILLING OIL PRESSURE WAS 25 PSI. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM AT ILN. REPLACED NR 4 OIL TEMPERATURE REGULATOR AND TEMP BULB IAW DC 8 MM CHAPTER 79. ENGINE OPS CHECKED GOOD ON GROUND RUN. 2L74 4F4 F 4A25 1E8 19950901001381995090100138EU 1995 9 1 COM31142 119950825A2750 CONTROL SYSTEM SAAB SF340 SF340A 7850100EU TE FLAPS OUT OF ADJUST A COMAK NONE O OTHER UKUNKNOWN 1 SO01358CA 340A047 FLAP WARNING ON CWP ACTIVATED. RIGGED THE FLAP CONTROL SYSTEM IAW M/M SPECIFICATIONS AND AIRCRAFT TO SERVICE. 2L72 4T RTA52EU 19950901001391995090100139EU 1995 9 1 COM31143 119950827A61201103P0620 SWITCH SAAB SF340 SF340A 7850100EU LT PROP DEFECTIVE A COMAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01342CA4236 275 340A023 AUTO COARSEN WARNING DURING TAKEOFF. REPLACED THE AUTO COARSEN ARMING P3 PRESSURE SWITCH. 2L72 4T RTA52EU 19950901001401995090100140NE 1995 9 1 COM31144 219950826A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT MALFUNCTIONED A COMAK NONE O OTHER UKUNKNOWN 1 SO01342CA962 962 340A023 384102L LEFT ENGINE WILL NOT ACHIEVE 100 PERCENT TORQUE. REPLACED THE LT ENGINE. 2L72 4T4 TRTA52EU E8NE6 19950901001411995090100141NM 1995 9 1 DL72L953492 119950824A3350334102486 EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11505DA40188 21307 DURING LAYOVER C-2, CARGO EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19950901001421995090100142NM 1995 9 1 DL72S953478 119950817A7110 INLET BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND NR 2 INLET DUCT, DOGHOUSE CRACKED AT THE 12 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 13. 2L73 4F A3WE 19950901001431995090100143NM 1995 9 1 DL72S953479 119950823A5713 STRINGER BOEING727 727232 1384082NM WS 686 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND STRINGER CRACKED RT WING STA 686 FWD STRINGER. REPAIRED PER M/M 57-13-0 PG 808. 2L73 4F A3WE 19950901001441995090100144NM 1995 9 1 DL72S953480 119950823A5743 TRUNNION BOEING727 727232 1384082NM RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND RT MLG TRUNNION FITTING CORRODED INSIDE HOLES. REPAIRED PER M/M 57-43-0. 2L73 4F A3WE 19950901001451995090100145NM 1995 9 1 DL72S953481 119950823A5754 BRACKET BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND I/B MOUNT BRACKET CRACKED FOR THE NR 5 L/E FLAP ACTUATOR. REPAIRED PER 57-20-21. 2L73 4F A3WE 19950901001461995090100146NM 1995 9 1 DL72S953482 119950823A5744 TRUNNION BOEING727 727232 1384082NM NR 6 FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND I/B TRUNNION MOUNT BRACKET CRACKED ON NR 6 FLAP ACTUATOR. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950901001471995090100147NM 1995 9 1 DL72S953483 119950823A5343 ATTACH FITTING BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND NOSE LANDING GEAR RT PIVOT ATTACH POINT FITTINGS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1. 2L73 4F A3WE 19950901001481995090100148NM 1995 9 1 DL72S953484 119950823A5343 ATTACH FITTING BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND NOSE LANDING GEAR LT PIVOT ATTACH POINTS CORRODED ON MATING FLANGES AND INSIDE OF HOLES. REPAIRED PER SRM 53-40-1. 2L73 4F A3WE 19950901001491995090100149NM 1995 9 1 DL72S953493 119950824A5754651622295 LE RIBS BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH SEVERAL CRACKED L/E RIBS. ACCOMPLISHED REPAIRS PER MM 57-54-0. 2L73 4F A3WE 19950901001501995090100150NM 1995 9 1 DL72S953494 119950824A5754651622374 RIBS BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11495DA 21075 DURING SHOP INSPECTION, NR 7 L/E SLAT WAS FOUND WITH NR 2 L/E RIB CRACKED IN LOWER AFT CORNER. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950901001511995090100151NM 1995 9 1 DL72S953504 119950807A5753652163233 SPAR BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NR 2 MIDFLAP, AFT LOWER SPAR CHORD IS CRACKED 37, 52 INCHES FROM I/B END OF FLAP AND 43 INCHES FROM O/B END OF FLAP. REPAIRED PER M/M 57520 PG 802 AND 807, INSTALLED DOUBLERS. FOUND AT HMV SHOP VISIT. 2L73 4F A3WE 19950901001521995090100152NM 1995 9 1 DL72S953507 119950824A5400 S-DUCT BOEING727 727232 1384082NM EMPENNAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 FWD EDGE OF UPPER S-DUCT INNER SKIN CRACKED AT APPROX 6 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3 FIG 9. 2L73 4F A3WE 19950901001531995090100153NM 1995 9 1 DL72S953508 119950820A5713 STRINGER BOEING727 727232 1384082NM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 LT WING UPPER STRINGER TO RIB STA 686.5 STR NR 13 CRACK INDICATION HFEC. REPAIRED PER MM 57-13-0 PG 808. FOUND AT HMV. 2L73 4F A3WE 19950901001541995090100154NM 1995 9 1 DL72S953509 119950818A5755 ANGLE BOEING727 727232 1384082NM LT SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 I/B LWR CORNER OF I/B GROUND SPOILER MOUNT BOX, ANGLE IS CRACKED. REPAIRED PER MM 57-55-0 PG 805. 2L73 4F A3WE 19950901001551995090100155NM 1995 9 1 DL72S953510 119950820A5400 S-DUCT BOEING727 727232 1384082NM CTR ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 INNER SKIN OF THE FWD SECTION OF S-DUCT IS BENT AND CRACKED AT APPROX 12 O'CLOCK POSITION. REPAIRED PER SRM 54-10-3. 2L73 4F A3WE 19950901001561995090100156NM 1995 9 1 DL72S953511 119950820A5744 BRACKET BOEING727 727232 1384082NM LT LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 NR 2 KRUEGER FLAP ACTUATOR BRACKET CRACKED AT RADIUS. REPAIRED PER 57-20-21 PG 811. FOUND AT HMV. 2L73 4F A3WE 19950901001571995090100157NM 1995 9 1 DL72S953512 119950820A5713 STRINGER BOEING727 727232 1384082NM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 LT WING UPPER STR TO RIB WS 686.5 STR NR 10 CRACKED. REPAIRED PER MM 57-13-0 PG 802. FOUND AT HMV. 2L73 4F A3WE 19950901001581995090100158NM 1995 9 1 DL72S953513 119950826A5754651622199 LE RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED L/E RIB AT THE ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 804. 2L73 4F A3WE 19950901001591995090100159NM 1995 9 1 DL72S953516 119950826A5522657278420 SKIN BOEING727 727232 1384082NM RT ELEVATOR CREASED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 AT HMV, FOUND RT ELEVATOR LOWER SKIN PANEL NR 4 FROM THE I/B END WITH CREASE. REPAIRED PER SRM 55-20-3 FIG 5. 2L73 4F A3WE 19950901001601995090100160NM 1995 9 1 DL72S953519 119950826A3350328 EEL BULB BOEING727 727225 1384077NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO118875Z 21293 10615 DURING LAYOVER, AFT EMERGENCY EXIT LIGHT OVER F/A SEAT INOP. RELAMPED LIGHT, OPERATION NORMAL. 2L73 4F A3WE 19950901001611995090100161NM 1995 9 1 DL76L953498 119950824A213121173889 CONTROLLER 1305027 BOEING767 767332 1382001NM CABIN MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11182DN 702188 25987 DURING CRUISE, COULD NOT CONTROL CABIN PRESSURE IN EITHER AUTO 1 OR AUTO 2, DIVERTED BOS. RAN BITE CHECK AS PER FIM, NUMBER 2 AC POWER FAULT, RESET, ALL CHECK NORMAL. REPLACED NUMBER 2 CONTROLLER AND ALT SELECT ON MODE CONTROL PANEL, UNRELIABLE TEST. REPLACED MODE SELECT PANEL, RAN BITE CHECK AS PER FIM, ALL OPERATION NORMAL AND RETURNED TO SERVICE. 2L72 4F RTA1NM 19950901001621995090100162NM 1995 9 1 DL76L953499 119950825A3350 EEL BULB OL3071BPEGPLBOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11183DN 27110 DURING S/C, FOUND 2 LAMPS INOP AT FWD CROSS AISLE PATH LIGHT. RELAMPED, OPERATION NORMAL. 2L72 4F RTA1NM 19950901001631995090100163NM 1995 9 1 DL76S953488 119950824A33501317 EEL BULB BOEING767 767332 1382001NM RT OVERWING FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11122DL 23436 FOUND RT OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED, OPERATION NORMAL. 2L72 4F RTA1NM 19950901001641995090100164 1995 9 1 DLL17953506 419950825A2220 MOTOR 4016608401 LKHEED1011 10113853 5265020WP MACH FEEL INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11769DL 389252 193H1218 AFTER TAKEOFF MACH FEEL CHANNEL 1 AND 2 FAILED, RETURNED ATL. REPLACED NR 1 AND NR 2 CHANNEL MACH FEEL MOTORS, OPERATION NORMAL. 2L73 4F A23WE 19950901001651995090100165NM 1995 9 1 DLM11953505 119950825A3350CMA8A113 EEL BULB DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11805DE 48476 FLOOR TRACK LIGHTS INOP AT SEAT 1E AND FWD LEFT GALLEY. RELAMPED. 2L73 4F RTA22WE 19950901001661995090100166NM 1995 9 1 DLM88953457 119950822A55235930497502 TAB DOUG MD88 MD88 3023688NM ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11908DL 49539 DURING SHOP INSPECTION, ELEVATOR TAB WAS RESTORED PER DRAWING 5930497 AND REPAIRED PER SRM 55-04 AND 51-70-2. 2L72 4F RTA6WE 19950901001671995090100167NM 1995 9 1 DLM88953473 119950822A2170 SEPARATOR BAGS 21D101 DOUG MD88 MD88 3023688NM CABIN DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11964DL 49983 DURING CLIMBOUT, STRONG ODOR ENTERED CABIN, SMELLED OILY. WHEN HP BLEEDS WERE OFF ODOR CLEARED, RETURNED ATL. REPLACED WATER SEPARATOR BAGS. INSP ENG BLEED CAPS, EMPTIED HYD OVERFLOW BOTTLE. RAN ENGS, ALL CKS OK. 2L72 4F RTA6WE 19950901001681995090100168NM 1995 9 1 DLM88953525 119950824A3350RPS1 EEL POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11917DE 49958 DURING PREFLIGHT, FOUND FORWARD CABIN EMERGENCY FLOOR TRACK LIGHTS FAIL TO TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L72 4F RTA6WE 19950901001691995090100169NM 1995 9 1 DLM88953526 119950822A2730 CONTROL CABLE DOUG MD88 MD88 3023688NM ELEVATOR DISCONNECTED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO11935DL 49722 WHILE TAXIING OUT DURING FLT CONTROL CHECK, PILOT REPORTED ELEVATOR CONTROL FELT ABNORMAL. RETURNED TO BLOCK AND FOUND HORIZONTAL STAB TRIM CABLE TURNBUCKLE UNDONE AT THE ELEVATOR FEEL FORCE LIMITER. REATTACHED CABLE, CHECKED OPERATION PER MM 27-30-00, OPERATION NORMAL. 2L72 4F RTA6WE 19950901001701995090100170NM 1995 9 1 SCNA95176 119950823A33503005931 EEL BATTERY PACK BOEING727 7272J4 1384006NM RT OVERWING DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE, DURING A FUNCTIONAL TEST. CHARGED BATTERY PACK AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19950901001711995090100171NM 1995 9 1 SCNA95177 119950823A335065801211 EEL CONNECTOR BOEING727 7272J4 1384006NM CABIN LOOSE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 THE FORWARD OVERHEAD AISLE EXIT SIGN WAS FOUND INOPERATIVE, DURING FUNCTIONAL TEST. RESEATED THE CANNON PLUG ON EXIT SIGN AND THE LIGHT TESTED GOOD. 2L73 4F RTA3WE 19950901001721995090100172NM 1995 9 1 SCNA95178 119950825A3350900542 EEL BATTERY PACK BOEING727 7272A1 138407FNM RIGHT OVERWING DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE EXTERIOR RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M956 PER MM 33-50-22, LIGHT TESTED GOOD. 2L73 4F A3WE 19950901001731995090100173NM 1995 9 1 UPS204332 119950823A3230 RETRACT MECH BOEING727 72727C 138400JNM NLG MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01914UP 19246 PILOT REPORTED, NOSE GEAR DOOR AND NOSE GEAR WOULD NOT COME DOWM ON FIRST ATTEMPT. RECYCLE, NOSE GEAR DOOR LIGHTS CAME ON AND NOSE GEAR CAME DOWN, INDICATING DOWN AND LOCKED. LUBED NOSE GEAR, PERFORMED GEAR RETRACTION THROUGH SEVERAL CYCLES. CK OK IAW M/M 12-21-11. 2L73 4F A3WE 19950901001741995090100174NM 1995 9 1 UPS204333 119950825A335037067001 EEL BATTERIES BOEING727 727247 138408FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01208UP 21701 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. 2L73 4F A3WE 19950901001751995090100175NM 1995 9 1 UPS204334 119950824A5522 LE SKIN BOEING727 72725C 138400HNM LT ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01932UP 19856 WHILE ON GROUND, MAINTENANCE FOUND REF D97427 LT ELEVATOR L/E 2 CRACKED. REPAIRED LT REV IAW 55-20-3 FIG 4. CALCULATED REPAIR WEIGHT TO BE 20 GRAMS AT O MOMENT, REPAIR WEIGHT WITHIN SRM 57-80-7. 2L73 4F A3WE 19950901001761995090100176WP 1995 9 1 UPS804269 119950828A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 980 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT MLG WHEEL WELL AFT PRESSURE BULKHEAD, B/S 980 AT LONGERON 31R CORRODED BEYOND LIMITS. REPAIR BULKHEAD B/S 980 AT LONGERON 31R IAW DC8-5310-7307A. 2L74 4F RT4A25 19950901001771995090100177WP 1995 9 1 UPS804309 119950828A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1040 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME B/S 1040 CORRODED AT LONGERON 34R. CUT OUT CORROSION DAMAGE, FABRICATED AND INSTALLED ANGLE AND FILLER IAW DC8-5310-7303A. 2L74 4F RT4A25 19950901001781995090100178WP 1995 9 1 UPS804335 119950828A5210561540389 DOOR FRAME DOUG DC8 DC871F 302199DWP PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01706UP 46056 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FWD ENTRY DOOR AFT FRAME SEGMENT CRACKED ABOVE BAYONETTE. REPAIRED PER UPS EO. 2L74 4F RT4A25 19950901001791995090100179NM 1995 9 1 95FDEA01083 119950804A5315 FLOORBEAM BOEING727 727227 1384078NM BS 530 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON FLOORBEAM STA 530 BETWEEN 5 AND 6 SEAT TRACKS.CORROSION WAS CUT OUT OF UPPER AFT FLANGE OF BEAM. DOUBLERS, REPAIR ANGLES AND FILLER WERE INSTALLED PER ESO 11782 DATE 8-03-95 REF NR1127. 2L73 4F A3WE 19950901001801995090100180NM 1995 9 1 95FDEA01084 119950809A5330 SKIN BOEING727 727227 1384078NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWR CARGO STA 720 BLO LEVELING COMPOUND SEPARATING FROM SKIN. REMOVED LEVELING COMPOUND AND REMOVED CORROSION PER SRM 87-10-6, TREATED PER SRM 59-10 MATERIAL REMOVED BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 PAGE 519. 2L73 4F A3WE 19950901001811995090100181NM 1995 9 1 95FDEA01085 119950809A5315 FLOORBEAM BOEING727 727227 1384078NM FS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON MAIN CABIN FLOORBEAM STA 344 RBL 24 TO LBL 65.REMOVED CORROSION PER SRM 51-20-6 CORROSION REMOVAL BEYOND LIMITS. INSTALLED SPLICE REPAIR ON TEE CHORD IAW ATTACHED JOB PROGRESS FROM SRM 51-10-1 AND 51-40-4 PAGE 942. 2L73 4F A3WE 19950901001821995090100182NM 1995 9 1 95FDEA01086 119950808A5315 FLOORBEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON UNDERSIDE OF TOP FLANGE OF FLOORBEAM STA 344, AROUND NUT CLIPS FROM BLL 12 TO BLR 12. REMOVED CORROSION, REMOVED AND REPLACED TOP TEE CHORD AND INSTALLED SPLICE REPAIR ON TEE CHORD IAW ATTACHED JOB PROGRESS FORM 51-10-1 OF SRM, 51-40-4 FIG 1 OF SRM. 2L73 4F A3WE 19950901001831995090100183NM 1995 9 1 95FDEA01087 119950809A5320 DOOR FRAME BOEING727 727227 1384078NM BS 450 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 LEVELING COMPOUND AFT OF E AND E DOOR CUTOUT AFT FRAME IS LOOSE. REMOVED LEVELING COMPOUND CORROSION FOUND ON DOOR CUTOUT FRAME. FRAME AT BS 450 REMOVED AND REPLACED WITH NEW FRAME PER SRM 51-10-1. 2L73 4F A3WE 19950901001841995090100184NM 1995 9 1 95FDEA01088 119950808A5315 FLOORBEAM BOEING727 727227 1384078NM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 FWD CARGO STA 620L BOTTOMSIDE OF MAIN CARGO FLOORBEAM LBL 48 CORROSION AROUND NUTPLATE. REMOVED NUTPLATE AS PER SRM 51-10-1. REMOVED CORROSION AS PER SRM 51-10-6, CORROSION REMOVED APPROX 50 PERCENT MATERIAL REMAINING. INSTALLED DOUBLERPER EA 7-5310-25380 8/4/98. 2L73 4F A3WE 19950901001851995090100185NM 1995 9 1 95FDEA01089 119950808A5315 FLOORBEAM BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON FLOORBEAM AT STA 480 UNDER NR 5 SEAT TRACK. REMOVED CORROSION AS PER SRM 51-20-11, CORROSION REMOVED BEYOND LIMITS. INSTALLED DOUBLER PER EA 7-5310-25380 8/4/95. 2L73 4F A3WE 19950901001861995090100186NM 1995 9 1 95FDEA01090 119950808A5320 ANGLE BOEING727 727227 1384078NM BS 227.5 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON BOTH VERTICAL AND HORIZANTAL INTERNAL FLANGES AT BS 227.5 LOWER CHORD ANGLE. CORROSION IS LOCATED JUST TOTHE LEFT OF BLLO. FABRICATED REPAIR DOUBLER PER EA 7-5310-25381 8/4/95. 2L73 4F A3WE 19950901001871995090100187NM 1995 9 1 95FDEA01091 119950811A5330 SKIN BOEING727 72725 1384006NM BS 1330 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CRACK IN SKIN AT PREVIOUS REPAIR, BS 1330 LBL 35 WL 163 ON LT SIDE OF AIRSTAIR CUTOUT. REMOVED AND REPLACED REPAIR PERFEDEX SRM 53-30-3. 2L73 4F A3WE 19950901001881995090100188NM 1995 9 1 95FDEA01092 119950811A5347694121 SEAT TRACK BOEING727 72725 1384006NM BS 848-950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C236-02) FOUND ON SEAT TRACK BS 950 TO 848 RBL25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 950 TO 848 RBL 25 WL 208 PER FEDEX SRM 51-30-2. 2L73 4F A3WE 19950901001891995090100189NM 1995 9 1 95FDEA01093 119950811A5347BAC1520241 SEAT TRACK BOEING727 72725 1384006NM BS 744-788 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION (72C236-02), AROUND SEAT TRACK BS 774 TO 788 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK BS 774 TO 788 LBL 25 WL 208 PER FEDEX SRM 51-30-2. 2L73 4F A3WE 19950901001901995090100190NM 1995 9 1 95FDEA01094 119950812A2613 CONNECTOR BOEING727 72722C 138400FNM OVERHEAT LOOP LOOSE A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING UKUNKNOWN 1 SO25106FE 19201 LWR AFT BODY OVERHEAT ILLUMINATED IN FLT, COMPLIED WITH ABNORMAL PROCEDURES. LIGHT WENT OUT AND STAYED OUT AFTER TURNING OFF RIGHT PACK AND CLOSING NR 3 BLEED VALVE. RAN ENGINESAND APU LEAKED CHECK RIGHT PACK AND AIR CONDITION BAY. FOUND SEVERAL CLAMPS LEAKING AND FOUND PLUG ON OVERHEAT LOOP BAD ON LT SIDE AIRSTAIR. REPLACED PLUG D1806, TIGHTEN CLAMPS IN RIGHT AIR CONDITION BAY, LEAK AND OPS CHECK GOOD. 2L73 4F A3WE 19950901001911995090100191NM 1995 9 1 95FDEA01095 119950812A261365249203 DETECTION UNIT BOEING727 727233 138408ANM E/E COMPT FAILED A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING CLCLIMB 1 SO25220FE 20934 FSD - ON CLIMBOUT PASSING 15,000 MSL, THE LOWER AFT BODY OVERHEAT LIGHT STARTED FLASHING. BLEEDS WERE NR 1 ON, LT PACKON, NR 2 RT ON, RT PACK ON, NR 3 OFF, OVERHEAT LIGHT EXTINGUISHED WITHIN 5 SECONDS OF TURNING NR 3 BLEED ON AND SYSTEM TESTED GOOD. NO FURTHER ACTION TAKEN, LEFT BOTH PACKS ON WITH NR 1, 2 RT AND 3 BLEEDS ON. REPLACED FIRE AND OVERHEAT DECTECTOR CONTROL BOX PER MM, OPS CHECKS GOOD. 2L73 4F RTA3WE 19950901001921995090100192NM 1995 9 1 95FDEA01096 119950811A52102024T3063 SKIN BOEING727 727227 1384078NM ENTRY DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25477FE 21394 FWD ENTRY DOOR HAS A LARGE DENT IN AFT EDGE OF SKIN, AFT LOWER CORNER. REPAIRED FWD ENTRY DOOR, LARGE DENT IN AFT EDGEIN SKIN AFT LOWER CORNER PER FEDEX SRM 52-00-3, 52-00-2, 51-30-8, 51-10-2, 51-30-2, 52-10-1. 2L73 4F A3WE 19950901001931995090100193NM 1995 9 1 95FDEA01097 119950814A5280 FRAME DOUG MD11 MD11F 3023600NM RT CTR GEAR DOORCRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25604FE 48460 RT/CENTER GEAR DOOR, 1B FWD CORNER ON INSIDE FRAME CRACKED APPROX 2. VERIFIED CRACK W/EDDY CURRENT, REMOVED DAMAGED SECTION OF DOOR FRAME, INSTALLED NEW SECTION OF FRAME (P/N AW87376-2) PER 53-00-7. 2L73 4F RTA22WE 19950901001941995090100194NM 1995 9 1 95FDEA01098 119950814A5312NCA6244515 BLKHD SKIN DOUG MD11 MD11F 3023600NM BS 62 DAMAGED A FDEAK NONE O OTHER LDLANDING 1 SO25604FE 48460 EA 1-5330-24396 SPLICE REPAIRED SKIN AT STA 62 LONGERON 36 TO 48 LT AND RT. PERMANENT REPAIR EA 1-5310-25112 REPAIRED PRESSURE BULKHEAD AT BS 595. 2L73 4F RTA22WE 19950901001951995090100195NM 1995 9 1 95FDEA01099 119950814A7110AJC756445 COWL WEB DOUG MD11 MD11F 3023600NM NR 2 ENGINE CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25604FE 48460 NR 2 ENG INTERNAL NOSE COWL FWD BULKHEAD WEB AND LOWER CHORD IS CRACKED AT 4 O'CLOCK POS APPROX 1, PANEL 362GR. REMOVED AND REPLACED LOWER CHORD WEB PER SRM 51-00-00 (P/N AJC7564-45). 2L73 4F RTA22WE 19950901001961995090100196NM 1995 9 1 95FDEA01100 119950813A5315 FLOORBEAM BOEING727 727227 1384078NM BS 400 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 CORROSION ON MAIN CABIN FLOORBEAM STA 400 AT RBL 24, FOUND WHEN FLOOR TRACK WAS REMOVED. ROUTED OUT DAMAGED AREA, INSTALLED DOUBLER WITH INTERCOSTAL PER 53-10-5. 2L73 4F A3WE 19950901001971995090100197NM 1995 9 1 95FDEA01101 119950812A5320 SUPPORT BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25482FE 21464 STR 26R IS CORRODED AT STA 480. REMOVED SECTION OF FLOOR SUPPORT RT STA 480 TO 495 FOM. REMOVED CORRODED STR 26R SPLICE AT STA 480, TREATED WITH ALODINE 1200 PER SRM 51-10-2, DRILLED NEW SPLICE, ALODINE 1200 TREATED, PRIMED. ALL FASTENERS THROUGH THE SKIN INSTALLED WET. FINISHED INSTALLATION OFSPLICE PER 51-30-1, INSTALLED FLOOR SUPPORT. 2L73 4F A3WE 19950901001981995090100198WP 1995 9 1 95FDEA01102 119950814A3260806125 PROX SWITCH DOUG DC10 DC1010F 3022111WP LT MLG LOOSE A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2568058 46705 LT MLG IND LIGHT REMAINED RED AFTER INT RETRACTION, BOTH PANELS. GEAR WAS RECYCLED PER PG 2-6-2 OF OTHER EMERGENCY ANDABNORMAL PROCEDURE HANDBOOK AND BOTH REMAINED RED. ONE MORE RECYCLE WAS ACCOMP WITH THE SAME RESULTS. FLT CONTINUED AT 260 KTS OR LESS FOR THE REMAINDER OF FLT PER CKLIST. FUELCONSUMPTION AND DRAG IND THAT THE GEAR WAS UP, LIGHTS REMAINED ON THROUGHOUT FLT, LIGHTS SHOWED GREEN EACH TIME. FOUNDPROX SW TARGET LOOSE, REPLACE SAME, FOUND EXCESSIVE GAP BETWEEN TARGET AND PROX SW ADJ SAME PER 32-34-03. DURING T/S FE LDG IND WENT INOP. REMOVED AND REPLACED PROX ELECTRONIC UNIT. BITE CK SAME, ALL POS CK NORMAL, PERFORMED GEAR SW ANDALL IND NORMAL. OK FOR SERVICE. 2L73 4F A22WE 19950901001991995090100199NM 1995 9 1 95FDEA01103 119950815A5315 FLOORBEAM BOEING727 7272S2F 1384O81NM BS 344 DOUBLE DRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 WHILE WORKING NR O0070, FOUND MECHANICAL DAMAGE AND DOUBLE HOLES IN FLOORBEAM BS 344 RBL 35 TO 55 WL 208. REMOVED EXISTING FLOORBEAM, REPAIRED AND INSTALLED FABRICATED FLOORBEAM AT BS 344 WL 208 RBL 35 TO 55 PER FEDEX SRM 51-10-1, 53-10-2. 2L73 4F A3WE 19950901002001995090100200NM 1995 9 1 95FDEA01104 119950815A532065453132 CLIP BOEING727 72725 1384006NM BS 660 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 DAMAGED STR CLIP BS 660 STR 2R. REMOVED AND REPLACED STR CLIP 2R PER FEDEX SRM 51-30-2. 2L73 4F A3WE 19950901002011995090100201NM 1995 9 1 95FDEA01105 119950815A53157075T6 FLOORBEAM BOEING727 72725 1384006NM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 CORROSION 72C235-02, ON FLOORBEAM BS 560 RBL 4 TO 23 WL 208. REMOVED AND REPLACED UPPER T-CHORD PER FEDEX SRM 51-30-08. 2L73 4F A3WE 19950901002021995090100202NM 1995 9 1 95FDEA01106 119950815A53137075T6 STRINGER BOEING727 72725 1384006NM BS 660 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 WHILE REMOVING STR CLIP 2R DAMAGED STR BS 660. REMOVED ANDREPLACED DAMAGED STR NR 2R FROM BS 670 TO 690 PER SRM 53-10-3. 2L73 4F A3WE 19950901002031995090100203NM 1995 9 1 95FDEA01107 119950815A575365246588 SPAR BOEING727 72725 1384006NM RT TE FOREFLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25156FE 18289 R/W I/B FOREFLAP I/B END POTTING COMPOUND MISSING. REMOVED UPPER SKIN SURFACE OF FLAP, FOUND L/E SPAR CORRODED. REMOVED CORRODED SPAR AND REPLACED WITH NEW SPAR LAID UP SKIN REPAIRS, ALL WORK DONE IAW FEDEX SRM 51-40-6, 51-30-2 AND FEDEX MM 51-20-151 AND 51-51-11. 2L73 4F A3WE 19950901002041995090100204NM 1995 9 1 95FDEA01108 119950713A5347652363762 SEAT TRACK BOEING727 727223 1384074NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 CORROSION TOP LT FLANGE OF NR 3 TRACK LBL 25 STA 740. THE NR 3 TRACK STA 740 IS OUT OF LIMITS 53-10-1 PG 616. REPLACED SEAT TRACK PER SRM 53-10-5. 2L73 4F A3WE 19950901002051995090100205NM 1995 9 1 95FDEA01109 119950718A5320 RIB CHORD BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 FS 760 RT RIB CHORD UPPER VERTICAL FLANGE FWD UPPER FASTENER HOLE AND FWD LOWER FASTENER HOLE HAVE CRACKS UP AND DOWN FROM HOLES. REMOVED END OF CRACK PER 51-10-1, NFRC INSP SPOTFREE OF CRACK REMOVED, REPAIRED BY INSTALLING DOUBLER PER EO 7-5710-7-23084 PART 1 AND 3 PER SB 727-S7-0112 REV 4. 2L73 4F A3WE 19950901002061995090100206NM 1995 9 1 95FDEA01110 119950720A5347 SEAT TRACK BOEING727 727227 1384078NM BS 740 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 SEAT TRACK WORN STA 740 LBL 45. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-10-5 PG 1 TO 4. 2L73 4F A3WE 19950901002071995090100207NM 1995 9 1 95FDEA01111 119950722A5313 STRINGER BOEING727 727227 1384078NM BS 490-500 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 STR 28R IS CORRODED IN 2 PLACES BETWEEN STA 490 TO 500. REPAIRED DAMAGED AREA PER SRM 53-30-3 PG 140 AND 53-10-3 PG 1. 2L73 4F A3WE 19950901002081995090100208NM 1995 9 1 95FDEA01112 119950724A5313 STRINGER BOEING727 727227 1384078NM BS 530-540 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25480FE 21462 STR 7R CRACKED IN 2 PLACES BETWEEN STA 530 TO 540R. INSTALLED STR REPAIR AS PER SRM 53-10-3. 2L73 4F A3WE 19950901002091995090100209NM 1995 9 1 95FDEA01125 119950815A5315BAC150529222 FLOOR BEAM BOEING727 7272S2F 1384O81NM BS 344 DOUBLE DRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25203FE 22925 WHILE WORKING NRO0070 FOUND MECHANICAL DAMAGE AND DOUBLE HOLES IN FLOOR BEAM BS 344 RBL 35 - 55 WL 208. REMOVED EXISTING FLOOR BEAM, REPAIRED AND INSTALLED FABRICATED FLOOR BEAM AT BS 344 WL 208 RBL 35 - 55 PER FEDEX SRM 51-10-1, 53-10-2. MFG P/N M446204. 2L73 4F A3WE 19950901002461995090100246NE 1995 9 1 9513059965 219950826A7310 FUEL HEAT VLV DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01911RW 47149 656091 NR 1 ENGINE FUEL HEAT INDICATOR ILLUMINATED IN CRUISE. THE ENGINE OIL TEMPERATURE EXCEEDED RECOMMENDED LIMITS, A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED AND THE FLIGHT DIVERTED TO TYS LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE, INSPECTED THE CHIP DETECTORS, AND CHANGED THE ENGINE OIL AND FILTER. NO ABNORMAL DEBRIS WAS NOTED. THE ENGINE WAS RUNUP, CHECKED OK, AND SCHEDULED FOR REINSPECTION IN 50 FLIGHT HOURS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950901002471995090100247NM 1995 9 1 9513062275 119950826A3260 SWITCH BOEING727 727251 138408HNM RT MLG DIRTY A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01275US 21154 DURING APPROACH AFTER GEAR EXTENSION, RIGHT MAIN GEAR UNSAFE INDICATION ILLUMINATED. DURING GO-AROUND, INDICATION CEASED. AFTER GEAR RETRACTION INDICATION REMAINED EXTINGUISHED. DURING SUBSEQUENT EXTENSION, ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED RIGHT MAIN LANDING GEAR INDICATION SWITCH, OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950901002481995090100248WP 1995 9 1 9513079854 119950828A3231 LINK DOUG DC9 DC951 3022051WP NLG DOORS BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01763NC 47716 VIBRATION FROM NOSE GEAR AREA OCCURRED AFTER GEAR RETRACTION, DURING CLIMBOUT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR RELEASE ACTUATOR LINK BROKEN. REPLACED RIGHT NOSE GEAR DOOR RELEASE ACTUATOR AND DOOR, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901002491995090100249WP 1995 9 1 9513089906 119950825A3260 DNLOCK SWITCH DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01956N 47252 ON APPROACH INTO DTW, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED AND FLAPS AT 25 DEGREES. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND EMERGENCY EQUIPMENT WAS CALLED TO MEET FLIGHT ON LANDING AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR DOWNLOCK SWITCH. ALSO, REPAIRED RIGHT MAIN GEAR DOOR AND REPLACED BOTH MAIN GEAR DOOR SKID PLATES DUE TO DAMAGE INCURRED. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901002501995090100250WP 1995 9 1 9513099908 119950815A3231 RETRACT MECH DOUG DC9 DC931 3022065WP NLG DIRTY A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01958N 47254 NOSE LANDING GEAR DOOR DID NOT CLOSE ON GEAR RETRACTION, RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDENT. INSPECTED AND RELATCHED RIGHT NOSE GEAR DOOR, CLEANED DEBRIS FROM BUNGEE CYLINDER. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901002511995090100251NE 1995 9 1 9513106309 219950825A7230 COMPRESSSOR BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 3 ENGINE STALLED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN MR OVER TEMP PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01669US 24224 717673 DURING ROTATION, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH HIGH EGT AND WAS SHUTDOWN. THE AIRCRAFT RETURNED TO TPE WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED AND THE ENGINE WAS REPLACED. 2L74 4F4 FRTA20WE E24NE 19950901002521995090100252NM 1995 9 1 95FDEA01216 119950822A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 HEAVY CORROSION LOWER FLANGE OF UPPER LOBE FLOORBEAM STA 1110 RBL 28 TO 30 IN AFT CARGO COMPT CEILING, NR 0993. 2L73 4F A3WE 19950901002531995090100253NM 1995 9 1 95FDEA01217 119950822A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 CORROSION IN UPPER LOBE FLOORBEAM, UPPER FWD FLANGE STA 1110 RBL 48 TO 60, NR 0996. 2L73 4F A3WE 19950901002541995090100254NM 1995 9 1 95FDEA01218 119950822A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 CORROSION TOP AFT FLANGE ON STA 1110 FLOORBEAM, LOWER SIDE AT FASTENER HOLES RBL 35 TO 40 AFT CARGO CEILING, NR 0994. 2L73 4F A3WE 19950901002551995090100255NM 1995 9 1 95FDEA01219 119950823A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 560 CORRODED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25105FE 19194 BS 560 LBL 29 TO 32 MAIN CARGO, FOUND CORROSION ON TOP LEG OF FLOORBEAM BETWEEN LT INBD AND LT CENTER CARGO TIE-DOWN TRACKS. REMOVED CORROSION INSTALLED REPAIR PER 53-10-8 PG 31 TO 48. 2L73 4F A3WE 19950901002561995090100256NM 1995 9 1 95FDEA01220 119950828A5712 RIB BOEING727 72722C 138400FNM WS 738.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 LT WING AT STA 738.5 INSIDE SURGE TANK, RIB CRACKED IN RADIUS AT AFT STR LOWER ATTACHMENT, NR 1023. INSTALLED DOUBLER ON RIB STA 738.5 L/LT WING, REF SRM 57-10-5. 2L73 4F A3WE 19950901002571995090100257WP 1995 9 1 ABXA9500680 119950826A3297 WIRE DOUG DC9 DC941 302207NWP NLG UPLOCK LOOSE A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23957AX 47759 NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT WENT OUT. FOUND UPLOCK SENSOR GROUND WIRE LOOSE. SECURED GROUND WIRE, OPS CHECKED PROX SENSORS AND UNSAFE LIGHT IAW DC-9 SUPP MM 32-60-1. DURING GEAR SWING, ALL INDICATIONS OPS CHECKED GOOD IAW DC-9 SUPP MM 32-10-00. 2L72 4F A6WE 19950901002581995090100258WP 1995 9 1 ABXA9500681 119950827A6123CRFP29 FEATHER PUMP ROTOL R209440452 NIHON YS11 YS11A500 6310416WP RROYCEDART DART54210K 54522EU ROTOL R2094 R209440 EU NR 2 PROP FAILED A ABXAA UNSCHED LANDING O OTHER CRCRUISE 1 GL23915AX6865 6864 DRG181699 2062 21327 DRG18169 NR 2 ENGINE SHUTDOWN FOR PRACTICE IN FLIGHT TRAINING. UNABLE TO RELIGHT, DID NOT COME OUT OF FEATHER. FOUND FEATHER PUMP INOP. REPLACED NR 2 FEATHER PUMP IAW YS-11 MM 61-20-2 AND ABX WORKCARD 6102, OPS CHECKED GOOD. 2L72 4T4 T A1PC E5EU 6 CP2EU 19950901002591995090100259EU 1995 9 1 COM31145 119950827A2731MS276456A BEARING SAAB SF340 SF340A 7850100EU RT ELEV TRIM WORN A ACOMAK NONE E VIBRATION/BUFFET CRCRUISE 1 SO01357CA 340A044 DURING FLIGHT, VERY NOTICEABLE VIBRATION IN CONTROL YOKE. AILERONS SEEM TO HAVE DELATED RESPONSE TO RT ROLL INPUT COMMAND. INSPECTED AILERON CONTROL SYSTEM AND FOUND NO DEFECTS. REPLACED WORN BEARINGS ON RT ELEVATOR TRIM TAB. 2L72 4T RTA52EU 19950901002601995090100260EU 1995 9 1 COM31146 119950828A3150004WS00 WEU SAAB SF340 SF340A 7850100EU AVIONICS BAY DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01359CA3399 854 340A053 CABIN PRESSURE WARNING ON CWP, DURING TAKEOFF. REPLACED THE WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19950901002611995090100261EU 1995 9 1 COM31147 119950829A2820AV16B2117B1 VALVE SAAB SF340 SF340A 7850100EU FUEL CROSS FEED FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01344CA23856 340A025 THE FUEL CROSS-FEED VALVE WILL NOT CLOSE, CIRCUIT BREAKER TRIPPED. REPLACED THE FUEL CROSS-FEED VALVE. 2L72 4T RTA52EU 19950901002621995090100262EA 1995 9 1 COM60544 119950828A1420 CONNECTOR CNDAIRCL600 CL6002B19 EA RT TE FLAP DAMAGED A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01917CA5501 7017 FLAPS FAIL MESSAGE ON EICAS, DURING TAXI. REPAIRED DAMAGED WIRE AT THE RT BPSU WIRING CONNECTOR. 2L72 4F RTA21EA 19950901002631995090100263EA 1995 9 1 COM60545 119950901A5210 HANDLE CNDAIRCL600 CL6002B19 EA PAX DOOR NOT STOWED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01912CA AC7011 DURING CRUISE FLIGHT, RECEIVED INBOARD COOL STATUS MESSAGE. FOUND EXTERNAL PAX DOOR HANDLE NOT STOWED PROPERLY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA21EA 19950901002641995090100264EA 1995 9 1 COM60546 119950829A361032895902 VALVE 35602310 CNDAIRCL600 CL6002B19 EA LT ENGINE NOT CLOSING A COMAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO01932CA3519 7038 LEFT ENGINE 14TH STAGE DUCT LEAK WARNING MESSAGE, INFLIGHT ENGINE SHUTDOWN AND DIVERTED TO TLH. PROBLEM COULD NOT BE DUPLICATED ON GROUND, THE BLEED AIR SHUT-OFF VALVE WAS NOT CLOSING FULLY AND WAS REPLACED, THE BLEED LEAK DETECTOR LOOP WAS ALSO REPLACED AS A PRECAUTION. 2L72 4F RTA21EA 19950901002651995090100265NM 1995 9 1 P5CA9500720 119950829A5753 SKIN BOEING747 747122 1384872NM NR 3 TE FLAP PUNCTURE A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 PUNCTURE LEFT WING INBOARD MIDFLAP LOWER SURFACE OUTBOARD OF NR 3 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950901002661995090100266NM 1995 9 1 P5CA9500721 119950829A5753 LE SKIN BOEING747 747122 1384872NM NR 4 FOREFLAP PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 PUNCTURE LEFT WING INBOARD FOREFLAP LEADING EDGE AT NR 4 FLAP TRACK. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950901002671995090100267NM 1995 9 1 P5CA9500722 119950829A5711 SPAR CHORD BOEING747 747122 1384872NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 CORROSION AT LES 777 LEFT WING LEADING EDGE CAVITY LOWER FRONT SPAR CHORD. REMOVED CORROSION PER BOEING SRM 51-10-01 WITHIN LIMITS PER 51-10-01. 2L74 4F A20WE 19950901002681995090100268NM 1995 9 1 P5CA9500723 119950829A5712 LE RIB BOEING747 747122 1384872NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 CRACKED LEADING EDGE RIB AT SUPPORT FOR GROUP 3 LEADING EDGE PDU INTERCOSTAL INBOARD END, BS 938.45 WS 294. REPAIRED PER BOEING TELEX 32-9430 PAO-SIN-95-0006RE, RI-PA57-018. 2L74 4F A20WE 19950901002691995090100269NM 1995 9 1 P5CA9500724 119950829A5400 FAIRING MOUNT BOEING747 747122 1384872NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23850FT 19755 PYLON NR 2 INBOARD SIDE FAIRING MOUNT IS CRACKED. REPAIRED PER BOEING SRM 54-10-00. 2L74 4F A20WE 19950901002701995090100270EA 1995 9 1 95ZZZX4347 119950421A6123 AUTOFEATHER DHAV DHC8 DHC8311 1386006EA RT ENGINE MALFUNCTIONED A MASAO OTHER J WARNING INDICATION CRCRUISE 1 SW01431AW 284 DURING CRUISE AT 16,000 FEET WITH POWER AT APPROX 45 PERCENT TORQUE, CREW SELECTED AUTOFEATHER ARMED AND WHEN CONDITION LEVERS ADVANCED FROM MIN RPM TO MAX RPM TO RT ENGINE, EXPERIENCED AUTOFEATHER CONDITION. CREW SELECTED AUTOFEATHER OFF AND ENGINE RETURNED TO NORMAL PARAMETER. ACFT LANDED UNEVENTFULLY AT RAP. PERFORMED MAINTENANCE GROUND RUN IN RAP WITH AUTOFEATHER OFF. FERRIED AIRCRAFT TO GJT FOR INVESTIGATION. DOWNLOADED FDR AND FOUND ALL ENGINE PARAMETERS NORMAL FOR AUTOFEATHER OPERATION. PERFORMED GROUND RUN-UP AND OPS CHECK OF AUTOFEATHER SYSTEM. ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19950901002711995090100271SO 1995 9 1 95ZZZX4348 119950422A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A AMASAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW01221YV 120221 PHX - ON APPROACH, AIRCRAFT ENCOUNTERED AN OUTBOARD FLAP ASSEMETRIC FAULT. THE FLAP ANNUNCIATOR SHOWED NO PROBLEM, AND THAT ALL FLAPS WERE AT 45 DEGREES, HOWEVER, UPON LANDING, THE RT OUTBOARD FLAP WAS NOTED TO BE AT APPROX 10 DEGREES. FLAP WAS RETURNED TO 'UP' POSITION AND VERIFIED FOR FERRY TO FMN. AFTER 2 DAYS OF EXTENSIVE TROUBLESHOOTING, NO ELECTRICAL DISCREPANCIES WERE FOUND. THE RT OUTBOARD FLAP ACTUATOR WAS REPLACED. AIRCRAFT TEST FLOWN WITH NO PROBLEMS REPORTED AND DISPATCHED. 2L72 4T RTA31SO 19950901002721995090100272NM 1995 9 1 ASAA9510075 119950816A53136547693501 STRINGER BOEING737 737298C 1384490NM BS 767-787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS33055 20794 SEA - DURING C-CHECK, CORROSION FOUND ON A PREVIOUS STRAP REPAIR ON THE OUTBOARD FLANGE OF S27L BETWEEN BS 767 AND BS 787. REMOVED CORROSION PER EA 5310-01376 AND BOEING TELEX ASA-DEA-95-0503RR. (X) 2L72 4F RTA16WE 19950901002731995090100273NM 1995 9 1 ASAA9540045 119950817A524069177652 LINK BOEING737 7374Q8 NM R1 DOOR HINGE LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01773AS 25106 SFL- FLT 113 - UNABLE TO OPEN R1 DOOR FROM OUTSIDE OF AIRCRAFT DURING CATERING. FOUND TOP DOOR HINGE TO BE DRY OF LUBRICANT; LUBED TOP HINGE AND DOOR OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19950901002741995090100274NM 1995 9 1 BJNA95801 119950807A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 1016 DENTED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FUSELAGE AFT BULKHEAD WEB DUE TO DENT AT BS 1016 BETWEEN STIFFENERS NR 6 LEFT AND NR 7 LEFT IAW SRM 53-10-4, FIG 12. (M) 2L72 4F A16WE 19950901002751995090100275NM 1995 9 1 BJNA95802 119950807A5330 SKIN BOEING737 7372H4 138448CNM BS 727 CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FUSELAGE SKIN DUE TO CRACK AT BS 727 BETWEEN STRINGER NR 20 AND STRINGER NR 19 RIGHT IAW DRAWING NR CEX3-53-1 DATED JULY 15, 1995, DOCUMENTED ON FAA FORM 8110-3. (M) 2L72 4F A16WE 19950901002761995090100276NM 1995 9 1 BJNA95803 119950807A5315BAC1518399 FLOOR BEAM BOEING737 7372H4 138448CNM BS 1006 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 1006 WL 208.1 BETWEEN BL 0 TO LBL 23 IAW SRM 53-10-9, FIG 7. (M) 2L72 4F A16WE 19950901002771995090100277NM 1995 9 1 BJNA95804 119950807A5315BAC1505100246 FLOOR BEAM BOEING737 7372H4 138448CNM BS 328 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM WEB DUE TO CORROSION AT BS 328 WL 200 BETWEEN LBL 52 TO LBL 64 IAW SRM 51-40-2, FIG 1. (M) 2L72 4F A16WE 19950901002781995090100278NM 1995 9 1 BJNA95805 119950807A5315BAC1518399 FLOOR BEAM BOEING737 7372H4 138448CNM BS 967 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 967 WL 208.1 BETWEEN LBL 1 TO LBL 16 IAW SRM 53-10-9, FIG 7. (M) 2L72 4F A16WE 19950901002791995090100279NM 1995 9 1 BJNA95806 119950807A5313BAC1498150 STRINGER BOEING737 7372H4 138448CNM BS 903-913 CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPLACED SPLICE IN RIGHT STRINGER NR 4 DUE TO CRACK BETWEEN BS 903 TO BS 913 IAW SRM 51-10-1, 51-30-2 AND 51-20-1. (M) 2L72 4F A16WE 19950901002801995090100280NM 1995 9 1 BJNA95807 119950807A5713 STRINGER BOEING737 7372H4 138448CNM LT WING CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED LEFT WING DUE TO CRACK AT WBL 227 UPPER STRINGER NR 11 AND STRINGER NR 12 ON THE RIB ATTACHMENT FLANGE IAW CASINO DWG NR CEX3-57-4, DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3. 2L72 4F A16WE 19950901002811995090100281NM 1995 9 1 BJNA95808 119950807A5315BAC1505100246 FLOOR BEAM BOEING737 7372H4 138448CNM BS 277 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM WWEB DUE TO CORROSINO AT BS 277 WL 194 BETWEEN LBL 9.50 TO LBL 12.50 IAW SRM 51-40-2, FIG 1. (M0 2L72 4F A16WE 19950901002821995090100282NM 1995 9 1 BJNA95809 119950807A5313 STRINGER BOEING737 7372H4 138448CNM BS 1035-1045 CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED STRINGER NR 9 LEFT DUE TO CRACK BETWEEN BS 1035 TO BS 1045 IAW SRM 53-10-3, FIG2. (M) 2L72 4F A16WE 19950901002831995090100283NM 1995 9 1 BJNA95810 119950807A5315BAC1518399 FLOOR BEAM BOEING737 7372H4 138448CNM BS 947.5 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 947.5 WL 208.1 RBL 7 TO RBL 54 IAW SRM 53-10-9, FIG 2. (M) 2L72 4F A16WE 19950901002841995090100284NM 1995 9 1 BJNA95811 119950807A5315BAC1505100246 FLOOR BEAM BOEING737 7372H4 138448CNM BS 344 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 344 WL 208.1 BETWEEN LBL 12 TO LBL 58 IAW SRM 53-10-9, FIG 5. (M) 2L72 4F A16WE 19950901002851995090100285NM 1995 9 1 BJNA95812 119950807A5315BAC1505100246 FLOOR BEAM BOEING737 7372H4 138448CNM BS 312 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FLOOR BEAM UPPER CHORD DUE TO CORROSION AT BS 312 WL 208.1 BETWEEN LBL 18 TO RBL 5 IAW SRM 53-10-9, FIG 5. (M) 2L72 4F A16WE 19950901002861995090100286NM 1995 9 1 BJNA95813 119950807A5320654580532 CHORD BOEING737 7372H4 138448CNM BS 267 CORRODED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPLACED CHORD SECTION DUE TO CORROSION ON NOSE GEAR TORQUE BOX AT BS 267 WL 144 BETWEEN LBL 20 TO RBL 20 IAW SRM 51-10-1 AND 51-30-2. (M) 2L72 4F A16WE 19950901002871995090100287NM 1995 9 1 BJNA95814 119950807A5713 STRINGER BOEING737 7372H4 138448CNM LT WING CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED LEFT WING DUE TO CRACK AT WBL 279.5 UPPER STRINGER NR 9 ON THE RIB ATTACHMENT FLANGE IAW CASINO DRAWING NR CEX3-57-3 DATED JULY 20, 1995, DOCUMENTED ON FAA FORM 8110-3. (M) 2L72 4F A16WE 19950901002881995090100288NM 1995 9 1 BJNA95815 119950807A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 294.5 CRACKED A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM57970 20336 REPAIRED FUSELAGE BULKHEAD WAS DUE TO CRACKS AT BS 294.5 LBL 3.5 TO LBL 9.5 AND RBL 5 TO RBL 11 BETWEEN WL 172.5 TO WL 150.5 IAW FAX BOEING M-7272-953780 DATED JULY 21, 1995 AND SKETCH CIN FAAX952195 1/1, DOCUMENTED ON FAA FORM 8110-3. (M) 2L72 4F A16WE 19950901002891995090100289EU 1995 9 1 C2XA95IA182 119950815A33503011206 EEL AEROSPATR42 ATR42320 8680930EU RT EXTERIOR INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0926826 172 IAH - DURING AN A-CHECK INSPECTION, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 19950901002901995090100290 1995 9 1 MALA95455 419950726A34526226523008 TRANSPONDER SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15158MC AC762B DTW - FLT 3318 - AFTER DEPARTURE, CREW NOTED THE ALTITUDE ENCODING TRANSPONDER WAS INDICATING 3,300 FEET HIGHER THAN THEIR ACTUAL ALTITUDE. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE TRANSPONDER CONTROL UNIT. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901002911995090100291NM 1995 9 1 MALA954550 119950722A24317504341 WARNING PANEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15828MA 333 DTW - FLT 3106 - DURING CLIMB-OUT, 'AUX BATTERY HOT' LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAUTION LIGHT PANEL. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901002921995090100292SW 1995 9 1 MALA954551 119950723A213110234010 PRESS CONTROL SWRNGNSA227 SA227AC 8780603SW CABIN FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15439MA AC722 DTW - FLT 3338 - DURING DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROL. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901002931995090100293SW 1995 9 1 MALA954552 119950723A7930PT06E84S BYPASS CONN SWRNGNSA227 SA227AC 8780603SW RT ENGINE FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1526906 AC654B DTW - FLT 3094, DURING CLIMB-OUT, THE RT ENGINE BYPASS LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPAIRED TWO OPEN CONTACTS IN THE RT BYPASS VALVE CANNON PLUG. THE SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901002941995090100294SW 1995 9 1 MALA954553 119950723A3260 WARNING LIGHT SWRNGNSA227 SA227AC 8780603SW GEAR DOOR MALFUNCTIONED A MALAK NONE N FALSE WARNING APAPPROACH 1 GL15442MA AC725 DTW - FLT 3312 - DURING APPROACH, THE 'GEAR DOOR POSITION' WARNING LIGHT ILLUMINATED. THE LIGHT FLICKERED, THEN EXTINGUISHED DURING ROLL-OUT. AFTER EXTENSIVE TROUBLESHOOTING AND INSPECTION, MAINTENANCE PERSONNEL WERE UNABLE TO DUPLICATE THE DISCREPANCY. (X) 1L72 4T A8SW 19950901002951995090100295NM 1995 9 1 MALA954554 119950724A5330 SKIN DHAV DHC8 DHC8102 2809003NM NOSE BIRD STRIKE A MALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL15829MA 335 MQT - FLT 3188 - DURING TAKEOFF, AIRCRAFT RECEIVED A BIRD STRIKE TO THE NOSE BELOW THE CAPTAIN'S WINDSHIELD. THE AIRCRAFT RETURNED TO MQT WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED A BIRD STRIKE INSPECTION; NO DEFECTS WERE NOTED. ALL SYSTEMS PERFORMED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901002961995090100296SW 1995 9 1 MALA954556 119950729A32602782186017 INDICATOR SWRNGNSA227 SA227AC 8780603SW LANDING GEAR FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL1560NE AC760B FNT - FLT 3440 - DURING APPROACH, CREW DID NOT GET A GREEN 'GEAR DOWN AND LOCKED' INDICATION WHEN THE GEAR WAS SELECTED DOWN. AFTER A VISUAL INSPECTION BY ATC PERSONNEL ON THE GROUND, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR INDICATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901002971995090100297NM 1995 9 1 MALA954558 119950731A5313 STRINGER DHAV DHC8 DHC8102 2809003NM BS 151.6-167 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15826MA 330 BNA - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND CORROSION ON STR L30 BETWEEN FRAME STATION 151.6 AND FRAME STATION 167.0. THEY REMOVED THE CORROSION IAW SRM 51-10-00, AND FABRICATED AND INSTALLED A REPAIR PART IAW SRM 53-10-21. (X) 2H72 4T RTA13NM 19950901002981995090100298NM 1995 9 1 MALA954559 119950731A5313 STRINGER DHAV DHC8 DHC8102 2809003NM BS 167-182 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15826MA 330 BNA - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CORROSION ON STR L28 BETWEEN FRAME STATION 16.0 AND FRAME STATION 182.0. THEY REMOVED THE CORROSION IAW SRM 51-10-00, AND FABRICATED AND INSTALLED A REPAIR PART IAW SRM 53-10-21. (X) 2H72 4T RTA13NM 19950901002991995090100299SW 1995 9 1 MALA954561 119950801A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND WEAR ON THE RT FLAP WALKING BEAM ROLLER DOUBLER. THEY REPLACED THE DOUBLER WITH A SERVICEABLE DOUBLER IAW FAIRCHILD SRM 57-90-10. (X) 1L72 4T A8SW 19950901003001995090100300SW 1995 9 1 MALA954562 119950801A5320 FLANGE SWRNGNSA227 SA227AC 8780603SW FS 254.52 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .125 INCH CRACK AT THE RT CONSTANT SECTION INNER FLANGE RADIUS, FS 254.52 AND APPROXIMATELY WL 70.65. THEY REPAIRED THE CRACK BY STOP DRILLING IT AND FABRICATING, PREPPING, AND INSTALLING A DOUBLER AND A STIFFENER IAW FAIRCHILD SRM 53-90-20. (X) 1L72 4T A8SW 19950901003011995090100301SW 1995 9 1 MALA954563 119950801A5320 FLANGE SWRNGNSA227 SA227AC 8780603SW BS 145.95 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .5 INCH CRACK AT RT CONSTANT SECTION INNER FLANGE RADIUS FS 145.95 AND APPROXIMATELY WL 70.65. THEY STOP DRILLED THE CRACK AND FABRICATED, PREPPED, AND INSTALLED A DOUBLER AND STIFFENER IAW FAIRCHILD SRM 53-90-20. (X) 1L72 4T A8SW 19950901003021995090100302SW 1995 9 1 MALA954564 119950801A5320 FLANGE SWRNGNSA227 SA227AC 8780603SW FS 159.24 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .125 INCH CRACK AT THE RT CONSTANT SECTION INNER FLANGE RADIUS FS 159.24 AND APPROXIMATELY WL 70.65. THEY STOP DRILLED THE CRACK AND FABRICATED, PREPPED, AND INSTALLED A DOUBLER AND STIFFENER IAW FAIRCHILD SRM 53-90-20. (X) 1L72 4T A8SW 19950901003031995090100303SW 1995 9 1 MALA954565 119950801A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND WEAR ON THE LT FLAP WALKING BEAM ROLLER DOUBLER. THEY REPLACED THE DOUBLER WITH A SERVICEABLE DOUBLER IAW FAIRCHILD SRM 57-90-10. (X) 1L72 4T A8SW 19950901003041995090100304SW 1995 9 1 MALA954566 119950801A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND THE LT NACELLE INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT SEVERAL RIVET HOLES ON THE FORWARD END. THEY REPLACED THE FORWARD 20 INCHES OF THE ANGLE AND INSTALLED A DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD SRM 51-00-00 AND ARP 54-20-9101. (X) 1L72 4T A8SW 19950901003051995090100305NM 1995 9 1 MALA954568 119950801A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15831MA 339 MSP - DURING PRE-FLIGHT, CREW NOTED SEVERAL FLOOR TRACK EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE LT FORWARD EMERGENCY LIGHTING BATTERY PACK. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901003061995090100306NM 1995 9 1 MALA954569 119950801A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15848MA 346 DTW - FLT 3051 - DURING APPROACH, LANDING GEAR WOULD NOT EXTEND. THE CREW RECYCLED THE GEAR. THE PROBLEM REMAINED. THE CREW USED THE ALTERNATE EXTENSION SYSTEM AND THE GEAR LOCKED DOWN. THE FLIGHT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR SELECTOR VALVE. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901003071995090100307NM 1995 9 1 MALA954570 119950802A335010005511 EEL LAMP DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15852MA 349 DTW - DURING PRE-FLIGHT, CREW NOTED THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE LIGHT ASSEMBLY WITH A SERVICEABLE ONE. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901003081995090100308NM 1995 9 1 MALA954571 119950728A5522 TE SKIN DHAV DHC8 DHC8102 2809003NM LT/RT ELEV CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15846MA 344 MSP - DURING A LIGHTNING STRIKE INSPECTION, MAINTENANCE PERSONNEL NOTED CRACKS IN THE LT AND RT ELEVATOR TRAILING EDGES AT THE STATIC WICKS. THEY REPAIRED THE CRACKS BY COMPLYING WITH DH8 SB 8-55-19, 'INCREASED SKIN AND RIB THICKNESS.' ALL WORK WAS PERFORMED IAW WITH SB, DHC SRM 18-3, AND DHC SRM 55-20-61. (X0 2H72 4T RTA13NM 19950901003091995090100309SW 1995 9 1 MALA954572 119950803A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL152692P AC658B LAF - FLT 3416 - DURING APPROACH, CREW NOTED THE RT MAIN LANDING GEAR INTRANSIT LIGHT DID NOT ILLUMINATE. MAINTENANCE PERSONNEL CLEANED THE RT MLG INTRANSIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901003101995090100310SW 1995 9 1 MALA954574 119950805A2612MS2517115 BOOT SWRNGNSA227 SA227AC 8780603SW RT ENGINE WORN A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15446MA AC693 MSP - FLT 3218 - ON CLIMB-OUT, RIGHT ENGINE FIRE LIGHT BEGAN TO FLICKER. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED A RUBBER BOOT FOR THE FIRE DETECTOR LOCATED AT THE ENGINE CASE. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901003111995090100311SW 1995 9 1 MALA954576 119950807A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW CARGO COMPT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15428MA AC646 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND AFT CARGO DOOR FUSELAGE FRAME CRACKED AT THE ACTUATOR ATTACH POINT HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, DOUBLER, AND FILLER IAW FAC ARP 53-20-9503. (X) 1L72 4T A8SW 19950901003121995090100312NM 1995 9 1 MALA954577 119950807A3350 EEL WIRE DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15826MA 330 DTW - FLT 3191 - DURING PRE-FLIGHT, EXIT LIGHT NEAR THE MAIN PASSENGER DOOR WAS FOUND INOPERATIVE. REPAIRS WERE COMPLETED BY RESECURING A GROUNDING WIRE FOR THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19950901003131995090100313SW 1995 9 1 MALA954578 119950807A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15439MA AC722 DTW - FLT 3357 - ON APPROACH, LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. ALL TESTS WERE NORMAL. THE AIRCRAFT CONTINUED TO DTW. MAINTENANCE CLEANED AND LUBED THE INTRANSIT SWITCHES. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901003141995090100314SW 1995 9 1 MALA954579 119950809A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG FAILED A MALAO OTHER O OTHER APAPPROACH 1 GL15434MA AC717 MSP - FLT 3027 - ON APPROACH, LT GEAR INTRANSIT LIGHT WAS VERY DIM WHEN ILLUMINATED DURING GEAR EXTENSION. THE INDICATION LIGHT ILLUMINATED NORMALLY WHEN TESTED. MAINTENANCE REPLACED THE LEFT INBOARD UPPER GEAR POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950901003151995090100315NM 1995 9 1 MALA954580 119950811A533085310026 SKIN DHAV DHC8 DHC8102 2809003NM BS 167-182 DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15824MA 327 BNA - DURING C-CHECK INSPECTION, MAINTENANCE NOTED A DENT IN THE FUSELAGE BETWEEN STR 32R AND STR 31R, STA X167 AND STA X182. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER PER RD8-53-1627. (X) 2H72 4T RTA13NM 19950901003161995090100316EU 1995 9 1 PLGA8995G1 119950809A3240 STATOR CLIP SAAB SF340 340B 7860101EU NR 3 BRAKE FAILED A PLGAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 NE05348BE 340B190 BGR - FLT 4969 - AFTER T/O, CREW NOTED RAPID LOSS OF HYD FLUID LEVEL IND. ACFT RETND, LANDING SAFELY. ACFT STOPPED ON RUNWAY WHERE PAX DEPLANED & ACFT TOWED TO GATE. MX OBSERVED NR 3 WHEEL AT APPROX 45 DEGREE ANGLE TO AXLE. MX RPLD NR 3 WHEEL & BRAKE, RESERVICED HYD SYS & RETND ACFT TO SERV. SHOP INVEST REVEALED FAILURE OF BRAKE OUTER STATOR (PN 5012637) INNER CLIPS. CLIPS BROKE FREE FROM CARB DISK CAUSING INNER BRNG CONE TO SEPARATE FROM WHEEL HALF. FAILURE ALLOWED WHEEL HALF TO ERODE BRAKE HSNG CAUSING HYD FLUID LOSS. SDR CLOSES SDR OF 8-9-95 WHERE FAIL OF NR 3 BRAKE OUTER STATOR INNER CLIPS CAUSED FAIL OF WHEEL HALF & BRAKE HSNG. AD952205 AMEND 39-9412 EFFECTIVE FOR INSP OF STATOR CLIP DAMAGE. (X) 2L72 4T RTA52EU 19950901003171995090100317CE 1995 9 1 SW019514 119950609A32601003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG FAILED A MASAO OTHER P NO WARNING INDICATION APAPPROACH 1 SW01158YV UC158 DURING APPROACH INTO CLARKSBURG, WV, PILOT SELECTED LANDING GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19950901003181995090100318NM 1995 9 1 TAOA089503 119950811A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS P2841 20445 FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOPERABLE. REPLACED BATTERY PACK FOR FORWARD ENTRY AISLE EMERGENCY EXIT SIGN. OPS CHKS OK. (X) 2L73 4F A3WE 19950901003191995090100319NM 1995 9 1 TAOA089504 119950813A2611 SMOKE DETECTOR BOEING727 727227 1384078NM LT LAVATORY MALFUNCTIONED A TAOAO OTHER N FALSE WARNING CRCRUISE 1 EA15559PE 21041 AFT LEFT LAV SMOKE DETECTOR SOUNDED, CIRCUIT BREAKER PULLED, NO FIRE. RESET CIRCUIT BREAKER, RESET TEST BUTTON TO 'OFF' THEN OPERATED TEST SEVERAL TIMES. OPS CHKD OK. (X) 2L73 4F A3WE 19950901003261995090100326NM 1995 9 1 AWXA9500524 119950811A3350 EEL CONNECTOR BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 18 THROUGH ROW 22. RESECURED LIGHT CONNECTOR AT ROW 18, OPS CHECK OK. (W) 2L72 4F RTA16WE 19950901003271995090100327NM 1995 9 1 AWXA9500525 119950811A3350 EEL WIRE BOEING757 7572G7 1384963NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 30 THROUGH 33. REPAIRED BROKEN WIRING, OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950901003281995090100328NM 1995 9 1 AWXA9500526 119950811A3350 EEL FUSE BOEING757 7572G7 1384963NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 20 THROUGH ROW 25. REPLACED PICO FUSE, OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950901003291995090100329NM 1995 9 1 AWXA9500527 119950813A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE IN BACK OF CABIN. RECONNECTED WIRE, OPS CHECK GOOD. (W) 2L72 4F RTA16WE 19950901003301995090100330NM 1995 9 1 AWXA9500528 119950813A3350 EEL CONNECTOR BOEING757 7572G7 1384963NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT CABIN AND FROM ROW 17 THROUGH ROW 25. REPAIRED WIRE IN AFT CABIN AND RESECURED LOOSE CONNECTOR AT ROW 17. OPS CHECK GOOD. (W) 2L72 4F RTA2NM 19950901003311995090100331NE 1995 9 1 AWXA9500530 219950814A7200 ENGINE BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 1 MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28902AW 23322 PHX - FLT 91 - ON TAKEOFF, THE LT EEC LIGHT AND LT ENGINE LIMITER LIGHT ILLUMINATED AFTER NR 1 ENG START, UMSR ISSUED. REDUCED TAKEOFF EPR OF 1.54, THE NR 1 ENG EGT ENTERED CAUTION RANGE OF 805 DEGREES. FUEL FLOW ON NR 1 ENG 1400 LBS HIGHER THAN NR 2 ENG. AC RETURNED TO PHX WITHOUT FURTHER PROBLEMS. MX REMOVED AND REPLACED THE NR 1 ENG PER AWA TASK CARD R5M71601. ENGINE TEST RUNS GOOD AND AC RETURNED TO SERVICE. (W) 2L72 4F4 FRTA2NM E12EU 19950901003321995090100332NM 1995 9 1 AWXA9500532 119950810A5330 SKIN BOEING737 7372U9 1384498NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW40737 22575 PHX - DURING SCHEDULED C10 INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT AFT EDGE OF COOLING FAN EXHAUST CUTOUT. REPAIRED PER EO 53 30 13. TOTAL CYCLES 31827. (W) 2L72 4F RTA16WE 19950901003331995090100333NM 1995 9 1 AWXA9500533 119950810A321165461131 TRUNNION BOEING737 7372U9 1384498NM RT MLG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW40737 22575 PHX - DURING SCHEDULED C10 INSPECTION, FOUND CRACK IN RT TRUNNION LINK PIN FWD LUG. REMOVED AND REPLACED TRUNNION PIN IAW 32 11 11. TOTAL CYCLES 31827. (W) 2L72 4F RTA16WE 19950901003341995090100334NM 1995 9 1 AWXA9500534 119950810A5330 SKIN BOEING737 7372U9 1384498NM BS 1156 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW40737 22575 PHX - DURING SCHEDULED C10 INSPECTION, FOUND CRACK IN FUSELAGE SKIN AT BS 1156 STR 2L TO STR 3L. REPAIRED PER EO 53 30 06. TOTAL CYCLES 31827. (W) 2L72 4F RTA16WE 19950901003351995090100335NM 1995 9 1 AWXA9500539 119950810A5311 FRAME BOEING737 7372U9 1384498NM BS 328 WORN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW40737 22575 PHX - DURING SCHEDULED C10 INSPECTION, FOUND FRAME AT BS 328 HAS WEAR MARKS ON TOP OF FRAME WHERE E AND E DOOR HAS BEEN HITTING FRAME. REPAIRED FRAME IAW SRM 51 40 3 FIG 1. TOTAL CYCLES 31827. (W) 2L72 4F RTA16WE 19950901003361995090100336NM 1995 9 1 AWXA9500540 119950810A5313 STRINGER BOEING737 7372U9 1384498NM BS 1006 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW40737 22575 PHX - DURING SCHEDULED C10 INSPECTION, FOUND EXFOLIATED CORROSION ON STRINGERS 28L TO 28R AT STA 1006. COMPLETED STRINGER REPAIR PER SRM 53 10 3. TOTAL CYCLES 31827. (W) 2L72 4F RTA16WE 19950901003371995090100337WP 1995 9 1 USAA950637 119950526A5320 ANGLE DOUG DC9 DC931 3022065WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT GALLEY NR 2 FLOOR SUPPORT FROM CENTER LINE TO I/B SEAT TRACK RT AT STA 200, PREVIOUS REWORK. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE SECTION PER SRM 53-11. (W) 2L72 4F A6WE 19950901003381995090100338WP 1995 9 1 USAA950638 119950526A5320 ANGLE DOUG DC9 DC931 3022065WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF LEVEL 1 CORROSION IN FLOOR SUPPORT STA 200, RUNNNG FROM CENTER LINE LT TO O/B SEAT TRACK, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE PER SRM 53-11. (W) 2L72 4F A6WE 19950901003391995090100339WP 1995 9 1 USAA950639 119950526A5320 ANGLE DOUG DC9 DC931 3022065WP BS 200-235 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION 2 INCH BY 14 INCH AREA STA 200 TO 235, LT OF CENTER LINE IN FLOOR SUPPORT ANGLE, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 53-11. (W) 2L72 4F A6WE 19950901003401995090100340WP 1995 9 1 USAA950640 119950526A5320 ANGLE DOUG DC9 DC931 3022065WP BS 160-218 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19981VJ 48157 PIT - DURING Q-4/CX-5 INSPECTION, FOUND LEVEL 1 CORROSION AT STA 160 TO 218 CENTER LINE OF A/C, AREA PREVIOUSLY REWORKED. CPCP TASK NR C46-53303. FABRICATED AND INSTALLED NEW SECTION OF FLOOR SUPPORT ANGLE PER SRM 53-11. (W) 2L72 4F A6WE 19950901003411995090100341WP 1995 9 1 USAA950654 119950705A5350 TAILCONE DOUG DC9 DC931 3022065WP AFT FUSELAGE DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19996VJ 47335 IAD - THE AFT TAILCONE WAS INADVERTENTLY DEPLOYED. THE TAILCONE DID NOT FALL AWAY ENOUGH TO PULL THE ESCAPE SLIDE OUT OF THE PACK TO DEPLOY. MAINTENANCE REPAIRED THE DAMAGED CONE TIP AND REINSTALLED THE TAILCONE. (W) 2L72 4F A6WE 19950901003461995090100346CE 1995 9 1 95ZZZX4353 119950809A28100823400110 BULKHEAD CESSNA402 402B 207590PCE RT TIP TANK CRACKED A AOEZAK NONE K FLUID LOSS ININSP/MAINT 1 WP19971589181 402B0544 PILOT FOUND FUEL LEAKING FROM RIGHT TIP TANK. FOUND BULKHEAD COLLAPSED AND CRACKED. FOUND CRACK IN AFT FUEL TANK NEAR BULKHEAD. SUGGEST MAINTENANCE TAKE CAREFUL LOOK AT THIS AREA SINCE THIS IS 3RD FAILURE IN TWO YEARS IN 3 DIFFERENT AIRPLANES. 1L72 3O A7CE 19950901003611995090100361EU 1995 9 1 95ZZZX4368 119950619A793153408 TRANSDUCER AEROSPSA365 SA365N 8680669EU NR 2 ENGINE OIL FLUCTUATES A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365SJ230 1035 6018 NR 2 ENGINE OIL PRESSURE FLUCTUATES. REMOVED AND REPLACED PRESSURE TRANSMITTER. 1G72 3U H10EU 19950901003621995090100362EU 1995 9 1 95ZZZX4369 119950709A6320579060 BALL JOINT AEROSPSA365 AS365N2 8680815EU TRANSMISSION CRACKED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM761 7942 6429 YELLOW BALL JOINT BULGED. OTHER THREE BADLY CRACKED AND WORKING. REMOVED AND REPLACED BALL JOINTS. 1G72 3U RTH10EU 19950901003631995090100363EU 1995 9 1 95ZZZX4370 119950709A6320579060 BALL JOINT AEROSPSA365 AS365N2 8680815EU TRANSMISSION CRACKED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM761 7959 6429 YELLOW BALL JOINT BULGED. OTHER THREE BADLY CRACKED AND WORKING. REMOVED AND REPLACED BALL JOINTS. 1G72 3U RTH10EU 19950901003641995090100364EU 1995 9 1 95ZZZX4371 119950709A6320579060 BALL JOINT AEROSPSA365 AS365N2 8680815EU TRANSMISSION CRACKED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM761 7960 6429 YELLOW BALL JOINT BULGED. OTHER THREE BADLY CRACKED AND WORKING. REMOVED AND REPLACED BALL JOINTS. 1G72 3U RTH10EU 19950901003651995090100365EU 1995 9 1 95ZZZX4372 119950709A6320579060 BALL JOINT AEROSPSA365 AS365N2 8680815EU TRANSMISSION BULGED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM761 7941 6429 YELLOW BALL JOINT BULGED. OTHER THREE BADLY CRACKED AND WORKING. REMOVED AND REPLACED BALL JOINTS. 1G72 3U RTH10EU 19950901003661995090100366EU 1995 9 1 95ZZZX4373 119950619A6220365A31185802 FREQ ADAPTER AEROSPSA365 AS365N2 8680815EU M/R SPLIT A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM343 7862 6429 YELLOW FREQUENCY ADAPTER HAS SPLIT CASING. REMOVED AND REPLACED. 1G72 3U RTH10EU 19950901003701995090100370SO 1995 9 1 95ZZZX4377 219950803A731428729 PUMP AIRBORNE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO FUEL SYSTEM BEARING WORN APACWTAK NONE O OTHER ININSP/MAINT 1 GL05663AA33 2J64 402C0123 FUEL PUMP REPLACED DUE TO LOW PRESSURE. THIS IS THE 3RD FAILURE IN 160 HOURS, ALL OVERHAULED BY RAPCO FLEET SUPPORT. PILOT FOUND METAL FLAKES IN FUEL SAMPLE FROM SUMP DRAIN. DISASSEMBLED PUMP AND FOUND BEARING FAILED. REPLACED WITH NEW AIRBORNE PUMP. 1L72 3O3 O A7CE E8CE 19950901003921995090100392WP 1995 9 1 9513119161 119950826A2910 HYD LINE DOUG DC9 DC914 3022034WP RT HYD SYST CRACKED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL018905E 45746 ON DESCENT INTO BHM, RIGHT HYDRAULIC SYSTEM PRESSURE BEGAN FLUCTUATING BETWEEN 1,500 AND 3,000 PSI AND QUANTITY WENT TO ZERO. PRECAUTIONARY COCKPIT OPERATING MANUAL PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. DAMAGE TO LEFT MAIN GEAR DOOR WAS INCURRED. FOUND AUXILIARY HYDRAULIC PUMP FILTER HOUSING LINE CRACKED. ALSO, FOUND RUDDER SHUTOFF VALVE CRACKED AND LEAKING. REPLACED AUXILIARY PUMP FILTER HOUSING AND LINE, RUDDER POWER SHUTOFF VALVE, AND LEFT MAIN GEAR DOOR DUE TO DAMAGE. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901003931995090100393WP 1995 9 1 9513129910 119950824A324295607887 BRAKE DOUG DC9 DC931 3022065WP LT MLG SEIZED A NWAAO OTHER O OTHER LDLANDING 1 GL01960N 57180185 47256 LEFT BRAKE SEIZED ON LANDING INTO EWR. AIRCRAFT CLEARED RUNWAY, BUT WAS UNABLE TO TAXI FORWARD. AIRCRAFT WAS TOWED TO THE GATE. FOUND BINDING IN NR 1 BRAKE ASSEMBLY AND REPLACED BRAKE. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901003941995090100394WP 1995 9 1 9513139102 119950827A2450 CIRCUIT BREAKER DOUG DC9 DC915 3022036WP RT AC BUS FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0192S 47064 DURING CLIMBOUT FROM DTW, AUTO-PILOT DROPPED OFF LINE, CAPTAIN'S RMI FLAGGED, FORWARD AND AFT FUEL BOOST PUMP CIRCUIT BREAKERS POPPED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND RIGHT AC BUS PHASE A CIRCUIT BREAKER BROKEN AND REPLACED THE CIRCUIT BREAKER. ALSO, RESET BOOST PUMP CIRCUIT BREAKERS. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950901003951995090100395EU 1995 9 1 95FDEA01221 119950829A213182010B040901 CONTROLLER AIRBUS310 A310203 EU NR 2 FAILED A AFDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25411FE 359 AFTER T/O, A/C TEMP WENT EXTREMELY HIGH AND THE PRESS CONTROLLER NR 2 FAILED. SWITCHED AUTOMATICALLY TO NR 1, WHICH DIDN'T CONTROL THE CABIN EITHER. MANUAL PRESS WAS TRIED AND DIDN'T WORK EITHER. NR 2 AFT, FWD AND MANUAL PRESS VALVES WOULD NOT EVEN MOVE AT TOUCHDOWN. VALVES SEEMED TO BE UNJAMMED, TEMPERATURE WENT TO FULL COLD AND THE COCKPIT FULL OF FOG. CABIN PRESS BEFORE TOUCHDOWN WAS MINUS 3,000 FT EVENTHOUGH LANDING ELEVATION WAS PLUS 20 FT, V/S ZERO AND DELTA PRESSURE WAS BLINKING AND SHOWING 8.6 PSI. REMOVED AND REPLACED NR 1 PRESS CONTROLLER. BITE TESTED BOTH NR 1 AND NR 2 SYS, PERFORMED PRESS SYS FUNCTIONAL CK NORMAL PER MM 21-30-00. 2L72 4F RTA35EU 19950901003961995090100396NM 1995 9 1 95FDEA01222 119950830A53302024T3 SKIN BOEING727 727233 138408ANM BS 490 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 WHILE WORKING NR 0412, FOUND LIGHTNING STRIKES AND DEEP GOUGES TO BE OUT OF LIMITS AT BS 490 STR 27R WL 149. REPAIRED DAMAGE AT BS 490 STR 27R WL 149, PER FEDEX SRM 53-30-3. 2L73 4F RTA3WE 19950901003971995090100397NM 1995 9 1 95FDEA01223 119950830A53137075T6 STRINGER BOEING727 727227 1384078NM BS 625 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25489FE 21492 FWD CARGO BAY HAD CORROSION ON STR 27R AT BS 625. REMOVED AND REPLACED DAMAGED AREA OF STA 625 STR 27R PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950901003981995090100398NM 1995 9 1 95FDEA01224 119950830A71102024T3071 COWL BOEING727 727233 138408ANM NR 1 ENGINE DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 NR 1 ENG NOSE COWL DENTED AT 6 O'CLOCK POSITION. DENT OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 54-10-3. 2L73 4F RTA3WE 19950901003991995090100399NM 1995 9 1 95FDEA01225 119950830A52302024T3063 SKIN BOEING727 727233 138408ANM NR 3 CARGO DOOR PUNCTURE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 LARGE PUNCTURE AT RIVET LOCATION ON NR 3 CARGO DOOR INTERNAL SKIN, BS 1138 WL 169 RBL 86. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 52-00-3. 2L73 4F RTA3WE 19950901004001995090100400NM 1995 9 1 95FDEA01226 119950829A53302024T3 SKIN BOEING727 727232 1384082NM BS 1243 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 DENT WITH CREASE FOUND IN SKIN AT BS 1243 WL 143 ON RIGHT SIDE OF A/C BETWEEN STR 22R AND 23R. 2L73 4F A3WE 19950901004011995090100401NM 1995 9 1 95FDEA01227 119950830A53137075T6 STRINGER BOEING727 727232 1384082NM BS 404 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CRACK STRINGER AT BS 404 STR 2R. ACCOMPLISHED STR REPAIR AT BS 404 STR 2R PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950901004021995090100402NM 1995 9 1 P5CA9500725 119950829A270165B821062 LIMITER SPRING BOEING747 747121 1384871NM LT CONTROL WHEELBROKEN A P5CAK NONE O OTHER CRCRUISE 1 WP23831FT 19648 FIRST OFFICER'S CONTROL WHEEL HAS 2 DEGREES PLAY BEFORE GETTING ANY AILERON MOVEMENT. CAPTAIN'S CONTROL WHEEL OK. FOUND AILERON CONTROL LOAD LIMITER TORSION SPRING BROKEN. REMOVED AND REPLACED LOAD LIMITER PER BOEING MAINTENANCE MANUAL 27-11-05. 2L74 4F A20WE 19950901004031995090100403WP 1995 9 1 SCNA95179 119950821A3350EMBS1392 EEL BATTERY PACK DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15572SC 46977 EMERGENCY LIGHT FAILED TEST FROM COCKPIT. REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMERGENCY BATTERY PACK AND THE SYSTEM TESTED GOOD PER MM 33-51-01. 2L73 4F A22WE 19950901004041995090100404NM 1995 9 1 SWAA950594 119950820A335020131A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW0752SW 21533 DURING SCHEDULED SERVICE CHECK, FOUND MAIN ENTRY AND SERVICE DOORS OUTSIDE EMERGENCY EXIT LIGHTS WEAK. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950901004051995090100405NM 1995 9 1 SWAA950595 119950821A335020131A EEL BATTERY BOEING737 7372H4 138448CNM CABIN DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD SERVICE DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M. 2L72 4F A16WE 19950901004061995090100406NM 1995 9 1 SWAA950596 119950819A33506104791 EEL POWER SUP BOEING737 7372T4 1384492NM FWD CARGO INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED POWER SUPPLY PER BOEING M/M. 2L72 4F A16WE 19950901004071995090100407NM 1995 9 1 SWAA950597 119950816A33506104789 EEL CHARGER BOEING737 7372T4 1384492NM FWD ENTRY INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER PER BOEING M/M. 2L72 4F A16WE 19950901004081995090100408NM 1995 9 1 SWAA950598 119950817A3350 EEL BOEING737 7372T4 1384492NM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07702ML 22054 DURING SCHEDULED SERVICE CHECK, FOUND ALL EMERGENCY EXIT LIGHTS INOP. REPLACED FWD FLOOR TRACK BATTERY HOUSING, AFT FLOOR TRACK BATTERY PACK, AFT SERVICE DOOR PORTABLE LIGHT ASSEMBLY, RELAMPED FLOOR TRACK LIGHTS AND EXIT SIGNS PER BOEING M/M. 2L72 4F A16WE 19950901004091995090100409NM 1995 9 1 SWAA950599 119950824A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0729SW 21340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKS AT BS 178 BULKHEAD WEB AT LBL 5.7 AND RBL 5.7, ALONG SIDE I/B ROW OF FASTENER HOLES BETWEEN WL 207 AND 218. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950901004101995090100410NM 1995 9 1 SWAA950600 119950825A32306552811113 RETRACT MECH BOEING737 7372H4 138448CNM LANDING GEAR MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0791SW 22963 AFTER TAKEOFF, CREW WAS UNABLE TO RAISE LANDING GEAR POSITION LEVER PAST THE OFF POSITION TO RETRACT GEAR. AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING. AIRCRAFT WAS MX FERRIED TO MDW WHERE THEY RIGGED THE GROUND SHIFT CABLE AND REPLACED THE LANDING GEAR ACCESSORY UNIT. 2L72 4F A16WE 19950901004111995090100411NM 1995 9 1 SWAA950601 119950825A261280600031 FIRE LOOP BOEING737 7372H4 138448CNM APU MALFUNCTIONED A SWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0751SW 21448 DURING CLIMBOUT, CREW EXPERIENCED APU FIRE WARNING AND THE APU WAS OFF. FIRE BOTTLE WAS ACTIVATED AND THE FIRE WARNING LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND NOTED NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED APU FIRE DETECTION LOOP M717 AND FIRE BOTTLE PER BOEING M/M. 2L72 4F A16WE 19950901004121995090100412NM 1995 9 1 SWAA950602 119950828A3230189929 SENSOR BOEING737 7373G7 1384595NM LANDING GEAR FAILED A SWAAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW07690SW 23787 AFTER TAKEOFF, LANDING GEAR POSITION LEVER WOULD NOT MOVE PAST OFF POSITION. GEAR POSITION INDICATED GEAR DOWN AND LOCKED. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FERRIED AIRCRAFT TO PHX. REPLACED GROUND SHIFT SENSOR AND PC LOGIC CARD PER BOEING M/M. 2L72 4F RTA16WE 19950901004131995090100413NM 1995 9 1 SWAA950603 119950825A5330 SKIN BOEING737 7372H4 138448CNM BS 720 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0786SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND 3 SKIN CRACK ALONG S25L AT BS 720. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950901004141995090100414NM 1995 9 1 SWAA950604 119950828A5315 FLOORBEAM BOEING737 7373H4 1384600NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07676SW 23288 DURING SCHEDULED B/C1 CHECK, FOUND FLOORBEAM STRAP CRACKED AT BS 344, JUST O/B AND ABOVE BATTERY. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19950901004151995090100415WP 1995 9 1 95ZZZM305 119950804A3260801801 DOWNLOCK SWITCH 7919074721 DOUG DC9 DC951 3022051WP NLG INOPERATIVE A A4JAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO15920PJ CPT603 47677 FLT 1818 - ON APPROACH, NOSE LANDING GEAR UNSAFE LIGHT CAME ON. WENT AROUND AND CYCLED GEAR. ALL INDICATIONS NOW NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH. GEAR OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19950901004161995090100416NM 1995 9 1 95ZZZM306 119950710A323069141065 TRANS CYLINDER BOEING727 727231 1384079NM NLG MALFUNCTIONED A ATWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0554327 20234 ONT - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND NOSE GEAR EXTENDED. FOUND NOSE LANDING GEAR TRANSFER CYLINDER, MFG P/N 69-14106-5, WITH INTERNAL MALFUNCTIONS. REPLACED TRANSFER CYLINDER AND NOSE LANDING GEAR OPERATION CHECKED NORMAL. (M) 2L73 4F A3WE 19950901004171995090100417WP 1995 9 1 95ZZZM307 119950710A27611040T1005 ACTUATOR DOUG DC9 DC931 3022065WP AUTO SPOILER FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 CE05982PS 47251 STL - DURING LANDING, SMOKE APPEARED IN COCKPIT. FOUND AUTO GROUND SPOILER ACTUATOR, MFG P/N 1040T100-5, HAD OVERHEATED CAUSING SMOKE. REPLACED AUTO GROUND SPOILER ACTUATOR AND OPERATION CHECKED NORMAL. (M) 2L72 4F A6WE 19950901004181995090100418WP 1995 9 1 ASAA9580161 119950715A5240 STRIKER/ROLLER DOUG DC9 DC982 3022082WP R1 DOOR BINDING A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01941AS 49925 PDX - PRIOR TO DEPARTURE OF FLIGHT 490, CREW REPORTED THE R1 DOOR WOULD NOT CLOSE. RELEASED THE STRIKER AND ROLLER ASSY AND DOOR OPERATED NORMALLY. (M) 2L72 4F A6WE 19950901004191995090100419WP 1995 9 1 ASAA9580169 119950727A5240 GUST LOCK DOUG DC9 DC983 3022083WP R1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01973AS 53449 SEA - AFTER ARRIVAL OF FLT 547 - CREW REPORTED THE R1 DOOR GUST LOCK WOULD NOT ENGAGE PROPERLY. LUBED GUST LOCK MECHANISM AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950901004201995090100420WP 1995 9 1 ASAA9580172 119950731A5210 MECHANISM DOUG DC9 DC982 3022082WP FWD ENTRY DOOR OUT OF SEQUENCE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01956AS 48079 SAN - PRIOR TO DEPARTURE OF FLT 325, GROUND CREW REPORTED FORWARD ENTRY DOOR WOULD NOT CLOSE PROPERLY. INSPECTED DOOR AND FOUND TO BE OUT OF SEQUENCE. CYCLED DOOR AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950901004211995090100421NM 1995 9 1 AWXA9500475 119950728A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 15 THROUGH ROW 21 EMERGENCY EXIT LIGHTS INOPERATIVE. REINSTALLED LOOSE WIRES, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004221995090100422NM 1995 9 1 AWXA9500484 119950729A3350900835A EEL POWER SUPPLY BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 21 AND ROW 23. REMOVED AND REPLACED POWER PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004231995090100423NM 1995 9 1 AWXA9500485 119950729A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN UNATTACHED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE JUST AFT OF OVERWING EXITS. REATTACHED WIRES AT ROW 14, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004241995090100424NM 1995 9 1 AWXA9500486 119950731A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE ROW 14 THROUGH ROW 18. REPAIRED WIRING, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004251995090100425NM 1995 9 1 AWXA9500488 119950731A3350 EEL ASSY BOEING757 7572G7 1384963NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 30 TO AFT OF AIRCRAFT. RECONNECTED NUMEROUS LIGHTS FROM ROW 30 AFT, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950901004261995090100426NM 1995 9 1 AWXA9500489 119950731A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 20 AND ROW 21. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004271995090100427NM 1995 9 1 AWXA9500490 119950801A3350 EEL CONNECTOR BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATAIVE IN CABIN. RECONNECTED LOOSE CONNECTOR AT ROW 14, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004281995090100428NM 1995 9 1 AWXA9500491 119950802A3350S417N50911 EEL ASSY BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28313AW 23712 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT OF AIRCRAFT. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004291995090100429NM 1995 9 1 AWXA9500493 119950804A2410727702E IDG ASSY BOEING757 7572G7 1384963NM NR 1 ENGINE FAILED A AWXAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 WP28909AW A0146 24522 PHX - FLT NR 11 - ON FLIGHT FROM JFK TO LAS, THE APU SHUTDOWN FOR LACK OF OIL. SINCE THE NR 1 ENG IDG WAS PLACARDED INOPERATIVE, THE PILOT ELECTED TO DIVERT AIRCRAFT TO PHX. MAINTENANCE REMOVED AND REPLACED THE NR 1 INTEGRATED DRIVE GENERATOR ASSY. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19950901004301995090100430NM 1995 9 1 AWXA9500495 119950805A3350BAC1522452714 EEL ASSY BOEING737 7373S3 1384711NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 16 THROUGH ROW 20. REMOVED AND REPLACED LIGHT ASSEMBLY AT ROW 16. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004311995090100431NM 1995 9 1 AWXA9500498 119950805A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28165AW 23626 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT TWO FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004321995090100432NM 1995 9 1 AWXA9500499 119950806A3350 EEL WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28905AW 23567 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE BETWEEN ROW 18 AND ROW 30. REPAIRED BROKEN WIRE AT R3 DOOR, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950901004331995090100433NM 1995 9 1 AWXA9500500 119950807A33509005242 EEL PWR SUPPLY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MANTENANCE CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950901004341995090100434 1995 9 1 C2XA95CL104 419950726A3441426871 CONTROL EMB 120 EMB120RT SO ANTI-SKID INTERMITTENT A C2XAK NONE O OTHER TXTAXI/GRND HDL 1 SW09157256639 209 120173 FLT NR 3363 - IND-CLE - CAPTAINS BRAKES FAILED DURING TAXI, FIRST OFFICERS WORKED NORMAL. MAINTENANCE REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW EMB MM 32-42-03. OPS CHECKED GOOD. (M) 2L72 4T RTA31SO 19950901004351995090100435SO 1995 9 1 C2XA95CL105 119950727A79313022871 OIL PRESS REG EMB 120 EMB120RT SO LT ENG OUT OF ADJUST A C2XAD RETURN TO BLOCK O OTHER CRCRUISE 1 SW0931711 120107 FLT NR 3357 - CLE - CRUISE FLIGHT LEFT ENGINE OIL PRESSURE ROSE TO 68/69 PSID, AS PER QRH REDUCED POWER TO 40 PERCENT, OIL PRESSURE REMAINED AT 66/68 PSID FOR REMAINDER OF FLIGHT. MAINTENANCE REMOVED TWO WASHERS FROM OIL PRESSURE REGULATOR IAW PWA 72-01-50 AND 72-00-00. RAN ENGINE OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950901004361995090100436SO 1995 9 1 C2XA95CL106 119950729A5610NP1513111 WINDSHIELD EMB 120 EMB120RT SO CAPTAINS SHATTERED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0927716 8841211460 120128 FLT NR 3267 - CLE - CAPTAINS WINDSHIELD SHATTERED IN FLIGHT ABOUT 1700 FEET ALTITUDE. MAINTENANCE REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW EMB 120MM 56-10-01. OPS CHECKED AND LEAK CHECKED GOOD IAW EMB 120MM 21-30-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950901004371995090100437 1995 9 1 C2XA95CL107 419950803A34426227337001 RT UNIT EMB 120 EMB120RT SO RADAR FAILED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW09167029053 1161 120078 FLT NR 3265 - CLE-CVG - RADR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD IAW EMB MM 34-41-00, 34-41-01, 34-41-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950901004381995090100438 1995 9 1 C2XA95CL108 419950803A34426227338002 CONTROL PANEL EMB 120 EMB120RT SO RADAR MALFUNCTIONED A C2XAA UNSCHED LANDING O OTHER CRCRUISE 1 SW09167025286 2112 120078 FLT NR 3265 - CLE-CVG - RADAR WILL NOT PAINT. AIRCRAFT RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED RADAR RECIEVER/TRANSMITTER AND CONTROL PANEL. OPS CHECKED GOOD IAW EMB MM 34-41-00, 34-41-01, 34-41-02. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950901004391995090100439EU 1995 9 1 C2XA95CL110 119950802A5230S5237640120200 SEAL AEROSPATR42 ATR42320 8680930EU FWD CARGO DOOR RUPTURED A C2XAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW0915823 165 FLT NR 3690 - EWR-BTV - AT FL 190 ENCOUNTERED EXCESSIVE CABIN ALTITUDE, PERFORMED EMERGENCY DESCENT. MAINTENANCE REMOVED AND REPLACED FORWARD CARGO DOOR SEAL IAW ATR JIC 52-31-40 RAI 10000-002. OPS AND PRESSURE CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950901004401995090100440NE 1995 9 1 C2XA95CL111 219950802A72003037223 SEAL AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 ENGINE LEAKING A C2XAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SW0915816 105 120982 FLT NR 3555 - MHT-EWR - NR 1 ENGINE OIL PRESSURE FLUCTUATION WITH CCAS ACTIVATION, SHUT DOWN ENGINE ACCORDING TO CHECKLIST. MAINTENANCE RESEALED TRANSFER TUBES TO 6 AND 7 BEARING HOUSING AND DRESSED AIR/OIL SEPARATOR SEAL FACE IAW PRATT AND WHITNEY M/M 72-20-00. ALL OPS CHECKS GOOD ON RUNS, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE 8/4/95. (M) 2H72 4T4 TRTA53EU E20NE 19950901004411995090100441SO 1995 9 1 C2XA95IA179 119950808A532012014226001 CROSS BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND THE CROSS BEAM BETWEEN FRAMES 35 TO 38, TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CROSSBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901004421995090100442SO 1995 9 1 C2XA95IA180 119950808A532012004449001 T-CAP EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND THE T-CAP AT FRAME 40 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-CAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901004431995090100443WP 1995 9 1 CAL950615 119950710A5350 CLIPS DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0993875 49125 HOU - THE INTERIOR TAILCONE RELEASE REQUIRED EXCESSIVE FORCE TO PULL FROM CLIPS. THE RELEASE HANDLE CLIPS WERE ADJUSTED TO WITHIN SPECIFICATION PER MM 53-53-00. (M) 2L72 4F A6WE 19950901004441995090100444NM 1995 9 1 CAL950616 119950718A5315 FLOORBEAM BOEING727 727232 1384082NM BS 410 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW094579364936 20647 STATION 31J - CORROSION WAS FOUND ON THE MAIN CABIN FLOORBEAM AT BS 410. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-8 AND 51-10-1. (M) 2L73 4F A3WE 19950901004451995090100445NM 1995 9 1 CAL950617 119950715A5330 SKIN BOEING727 727232 1384082NM BS 445 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094579364936 20647 STATION 31J - INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT BS 445, S19L AND THERE WAS CORROSION AT THE FASTENERS. THE CRACKED AND CORRODED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M) 2L73 4F A3WE 19950901004461995090100446NM 1995 9 1 CAL950619 119950727A2530 COFFEEMAKER BOEING727 727224 1384076NM GALLEY SMOKING A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0979746 22449 FLT NR 0538 - EWR - SMOKE WAS OBSERVED COMING FROM THE VICINITY OF THE AFT GALLEY COFFEEMAKER WHILE IN FLIGHT. THE COFFEEMAKER WAS TURNED OFF AND THE SMOKE CEASED. MAINTENANCE FOUND BURNT PAPER AT THE BACK OF THE COFFEEMAKER. THE AREA WAS CLEANED FREE OF THE DEBRIS. THERE WAS NO TROUBLE FOUND WITH THE COFFEEMAKER. 2L73 4F A3WE 19950901004471995090100447WP 1995 9 1 CAL950620 119950728A323039370301 LINK DOUG DC9 DC982 3022082WP RT MLG BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0983872 49120 FLT 1419 - EWR - THE RIGHT MLG WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR DOOR OPEN LIGHT AND THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED. ABNORMAL PROCEDURES WERE ACCOMPLISHED, BUT THE LIGHTS DID NOT EXTINGUISH. THE AIRCRAFT WAS RETURNED TO EWR AND LANDED WITH NORMAL GEAR INDICATIONS. MAINTENANCE FOUND THE RT MLG ACTUATOR ROD LOWER ATTACH LINK BROKEN/DETACHED. THE LOWER ATTACH LINE WAS REMOVED AND REPLACED. OPERATION AND INDICATIONS CHECKED NORMAL DURING A GEAR RETRACTION. (M) 2L72 4F A6WE 19950901004481995090100448 1995 9 1 CAL950621 419950727A22104030952906 COUPLER BOEING737 7373T0 1384582NM YAW DAMPER RATE GYRO FAILEDA ACALAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DEDESCENT 1 SW0914341 23579 FLT 0131-MEX-THE YAW DAMPER WENT FULL SCALE RT WITH RUDDER MOVEMENT TO THE RT AT APPROX 11,000 FT WITH AIRSPEED BETWEEN 180 AND 170. THE YAW DAMPER WAS TURNED OFF AND RUDDER WENT BACK TO NORM. THE AUTOPILOT ACCY UNIT WAS REMOVED DURING T/S AND TESTED GOOD PER MM 22-11-36. THE YAW DAMPER COUPLER WAS REPLACED AS A PRECAUTION. ALSO, THE RUDDER PCU AND STANDBY RUDDER PCU WERE BOTH R/R. OPS OF BOTH UNITS CHKD GOOD. S/D - FAILURES BEEN ATTRIBUTED TO THE YAW DAMPER COUPLER WHICH WAS FOUND TO HAVE A FAULTY RATE GYRO. NO TROUBLE WAS FOUND WITH THE STANDBY RUDDER PCU. THE RUDDER PCU DID NOT PASS ACCEPTANCE TEST, BUT NO DISCREPANCIES WERE FOUND THAT COULD HAVE LEAD TO YAW DAMPER ANOMALY. (M) 2L72 4F RTA16WE 19950901004491995090100449NE 1995 9 1 CAL950622 219950727A7230 NR 3 BEARING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE FAILED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0934838 49634 708460 FLT NR 0204 - STL - THE NR 1 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED DURING CLIMB-OUT. THE CHECK LIST WAS COMPLIED WITH, BUT THE LIGHT REMAINED ILLUMINATED. ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT WAS DIVERTED TO STL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. TEARDOWN REVEALED A NR 3 BEARING FAILURE, ANTI-ROTATION BEARING PINS FAILED. (M) 2L72 4F4 F A6WE E9NE 19950901004501995090100450NE 1995 9 1 CAL950628 219950730A7250 CARBON SEAL BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 2 ENGINE BROKEN A CALAE ENGINE SHUTDOWN KJMFLUID LOSS WARNING INDICATION OVER TEMP CRCRUISE 1 SW0933785304548488 20640 700787 FLL - FLT 0443 - THE NR 2 ENGINE OIL TEMPERATURE CLIMBED INTO THE RED ZONE WHILE EN ROUTE FROM EWR TO FLL. THE TEMPERATURE RISE WAS ACCOMPANIED BY A DROP IN OIL PRESSURE AND QUANTITY AND ILLUMINATION OF THE NR 2 ENGINE OIL BYPASS LIGHT. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED AT FLL WITHOUT INCIDENT. THE NR 2 ENGINE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - SHOP FINDINGS REVEALED NR 5 CARBON SEAL, SEAL RING, AND HEATSHIELD BROKEN AND WORN. (X) 2L73 4F4 F A3WE E2EA 19950901004511995090100451EU 1995 9 1 95ZZZM308 119950110A2620 FIRE BOTTLE WIRE BAG BAE146BAE146200A 1500266EU NR 4 ENGINE CHAFED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31609AW E2070 NR 4 ENGINE, BARE WIRE ON WIRE BUNDLE GOING TO RIGHT FIRE BOTTLE LOCATED IN PANEL 442AR CHAFING ON TIE WRAP ON ANOTHER WIRE BUNDLE. INSPECT WIRE 4HK365 AND FOUND PTFE INSULATION DAMAGED BUT FOUND KAPTON TAPE TO BE UNDAMAGED. REPAIRED BY INSTALLATION OF HIGH TEMP HEAT SHRINK TUBING IAW WIRING MANUAL STAN PRAC 20-44-04. DAMAGE OF INSULATION WAS APPROX 8 INCHES FROM CANNON PLUG. 2H74 4F RTA49EU 19950901004521995090100452NE 1995 9 1 95ZZZM309 219950725A7310216362035 MANIFOLD BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE DIRTY A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FOUND EVIDENCE OF SOOT IN THE RT REAR COWL AREA OF NR 1 ENGINE. RIGHT MANIFOLD FAILED ET. REPLACED RT MANIFOLD ASSY ON NR 1 ENGINE. 2H74 4F4 FRTA49EU E6NE 19950901004531995090100453EU 1995 9 1 95ZZZM310 119950717A3234HTE94904 HYD SELECTOR VLV BAG BAE146BAE146300A 1500267EU LANDING GEAR FAILED A A6WAO OTHER J WARNING INDICATION APAPPROACH 1 GL31614AW E3132 GEAR FAILED TO EXTEND WHEN SELECTED. WENT TO EMERGENCY AND GEAR EXTENDED. LANDED WITHOUT INCIDENT. SENT REPLACEMENT VALVE AND ACTUATOR TO DEN. REPLACED VALVE AND ACTUATOR. 2H74 4F RTA49EU 19950901004541995090100454EU 1995 9 1 95ZZZM311 119950211A2420 GEN CONTL UNIT BAG BAE146BAE146300A 1500267EU NR 1 OFF LINE A A6WAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION APAPPROACH 1 GL31615AW E3141 NR 1 AC BUS AND ESS AC BUS OFF LINE OCCURRED APPROX 200 FEET PRIOR TO TOUCHDOWN. AIRCRAFT IN LANDING CONFIGURATION APU WAS OPERATIONAL AT THE TIME. RESET NR 1 GCU BUS RESET, GROUND RAN, OPS CHECKS GOOD. AIRCRAFT 73 MINUTES LATE INBOUND DUE TO HEADWINDS. (M) 2H74 4F RTA49EU 19950901004551995090100455EU 1995 9 1 95ZZZM312 119950419A5320 STIFFENER BAG BAE146BAE146200A 1500266EU BS 25.94 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31608AW E2049 BOTH INBOARD (LT/RT) STIFFENERS AT STATION 25.94 ON FRAME 29 IN HYD BAY ARE CRACKED. REPAIR STIFFENERS IAW EO E95/005/653. COMPLIED EO E95/005/653 ORIGINAL ISSUE AT LT/RT STATION 25.94 ON FRAME 29 STIFFENERS. (M) 2H74 4F RTA49EU 19950901004561995090100456EU 1995 9 1 95ZZZM313 119950609A5753HC579L0053000 BOLT BAG BAE146BAE146100A 1500260EU NR 4 FLAP TRACK DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 LEFT NR 4 FLAP TRACK CROSS HEAD TO LINK CAP BOLT IS BAD AND NEEDS REPLACED. FAILED INSPECTION CHECK. INSTALLED NEW LEFT NR 4 FLAP TRACK CROSS HEAD TO LIND CAP BOLT AS REQUIRED. 2H74 4F RTA49EU 19950901004571995090100457EU 1995 9 1 95ZZZM314 119950524A5320 SILL BAG BAE146BAE146300A 1500267EU PAX DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31614AW E3132 FORWARD PASSENGER DOOR LOWER SILL TO FLOOR FLANGE SILL CORRODED, FRAME 15-18. DRILLED OUT CORROSION, CONFIRMED AREA FREE FROM CRACKS AND CORROSION VIA NDT (DOC ON ANOTHER W/C) REPROTECTED AREA, PRIMED AND REPAINTED. (M) 2H74 4F RTA49EU 19950901004581995090100458NM 1995 9 1 95ZZZM315 119950728A2897106182721 HARNESS BOEING737 737297 1384480NM NR 1 FUEL TANK FAILED A ZZDAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 SO15462AT27706 22631 ON APPROACH TO CVG THE CREW OF FLIGHT 700 OBSERVED THE NR 1 FUEL QUANTITY SYSTEM GIVING AN ERRATIC INDICATION. THE CAPTAIN DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED THE ERRATIC INDICATION WAS CAUSED BY CONDENSATION BUILDUP ON THE NR 1 TANK FUEL QUANTITY PROBES. SUMPED TANK. DID NOT CORRECT DISCREPANCY. FUEL QUANTITY SYSTEM TEST SET INDICATED THAT THE NR 1 TANK FUEL QUANTITY HARNESS WAS DEFICIENT. REPLACED HARNESS. SUBSEQUENT FUEL QUANTITY CHECK TESTED GOOD. FUELED NR 1 TANK WITH NO DIFFICULTIES NOTED. (M) 2L72 4F A16WE 19950901004591995090100459EU 1995 9 1 95ZZZM316 119950403A5320 STIFFENER BAG BAE146BAE146300A 1500267EU FUSELAGE CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 FOUND CORROSION ON FRAME 29 STIFFENERS AT RT STATION 25.94 AND LEFT STATIONS 25.94, 31.13 AND 36.62. COMPLIED WITH EO E95/005/653 ORIG ISSUE ON FRAME 29 STIFFENERS AT RT STATION 25.94 AND LEFT STATIONS 25.94, 31.13 AND 36.62 TO REMOVED CORROSION. 2H74 4F RTA49EU 19950901004601995090100460EU 1995 9 1 95ZZZM317 119950411A2720 FRICTION BRAKE BAG BAE146BAE146300A 1500267EU RUDDER OUT OF ADJUST A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW E3122 IN EITHER DIRECTION THE RUDDER WOULD NOT RETURN TO CENTER, THE CAPTAINS AND FLIGHT OFFICERS RUDDER PEDALS INPUTS HAVE SAME EFFECT. ADJUSTED RUDDER CABLE COMPENSATOR FRICTION BRAKE. (M) 2H74 4F RTA49EU 19950901004611995090100461WP 1995 9 1 95ZZZM318 119950802A2612244F70G36 SENSOR WIRE DOUG DC8 DC851 3021920WP NR 1 ENG BROKEN A FXLAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO19507DC 45855 IN CLIMB-OUT OF BOG, RECEIVED FIRE WARNING ON NR 1 ENGINE. SHUT DOWN ENGINE, RETURNED TO BOG AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED GROUND WIRE BROKEN AT SENSOR ON LEFT AFT DOOR. REPAIRED GROUND WIRE TO SENSOR. SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A25 19950901004621995090100462SO 1995 9 1 C2XA95IA177 119950808A572012017057015 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901004631995090100463SO 1995 9 1 C2XA95IA178 119950808A532012009846001 CROSSBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND CROSSBEAM AT FRAME 16 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CROSSBEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901004641995090100464NM 1995 9 1 CAL950623 119950728A29106517844239 HYD LINE BOEING727 727243 138408DNM 'A' HYD SYSTEM CRACKED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0958414 22166 FLT NR 0566 - IAH - THE 'A' SYSTEM HYDRAULIC QUANTITY INDICATED ZERO IN FLIGHT. THE 'A' SYSTEM PUMPS WERE SHUT OFF, THE CHECKLIST WAS COMPLIED WITH, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE HYDRAULIC PRESSURE LINE TO THE 'A' SYSTEM MODULE CRACKED. THE LINE WAS REPLACED AND LEAK CHECKS WERE GOOD. (M) 2L73 4F RTA3WE 19950901004651995090100465NM 1995 9 1 CAL950624 119950728A3260656021123 ACCESSORY UNIT BOEING727 727243 138408DNM LANDING GEAR INOPERATIVE A ACALAO OTHER N FALSE WARNING CLCLIMB 1 SW09344152639 22167 FLT NR 0334 - IAH - THE LEFT MLG RED AND GREEN LIGHTS ON THE FORWARD PANEL REMAINED ILLUMINATED AFTER TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHTS REMAINED ON WITH THE SECOND OFFICERS PANEL INDICATING NORMAL. A VISUAL INSPECTION FOUND THE GEAR RETRACTED. MAINTENANCE FOUND THE LANDING GEAR ACCESSORY UNIT AT FAULT. THE LG ACCESSORY UNIT WAS REPLACED AND OPERATION OF THE UNIT CHECKED GOOD. (M) 2L73 4F RTA3WE 19950901004661995090100466NE 1995 9 1 CAL950629 219950731A7250 TURBINE BOEING727 727243 138408DNM PWA JT8 JT8D9 52048NE NR 3 ENGINE FAILED A CALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SW0917407590181129 21270 674242 EWR - FLT 0177 - THE NR 3 ENGINE AUTO SHUT-DOWN DURING CLIMB-OUT OF EWR. THE SHUT-DOWN WAS ACCOMPANIED BY A LOUD BANG AND VIBRATION. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - SHOP FINDINGS REVEALED THE FAILURE OF TWO FIRST STAGE TURBINE BLADES AT THE AIRFOIL AREA. THE FAILED BLADES SUFFERED FROM INTERNAL METAL DEFICIENCY. (X) 2L73 4F4 FRTA3WE E2EA 19950901004671995090100467NM 1995 9 1 CKSA95087 119950627A53307775D6 SKIN BOEING727 727223 1384074NM FUSELAGE PUNCTURED A CKSAK NONE O OTHER ININSP/MAINT 1 GL236812 71865 19487 KBOS - SKIN PUNCTURE, FOUND ON POST FLIGHT IN BOS. PUNCTURE IS APPROXIMATELY 1 INCH LONG BY .1250 INCH WIDE, AND LOCATED APPROXIMATELY 36 INCHES AFT OF THE AFT CARGO DOOR. ACCOMPLISHED FUSELAGE EXTERNAL SKIN REPAIR IAW SRM 53-30-3. (M) 2L73 4F A3WE 19950901004681995090100468EU 1995 9 1 COEA9572001 119950427A53205215012401 FITTING FOKKERF27 F27MK500 4990629EU BS 7961 CRACKED AS COEAK NONE O OTHER ININSP/MAINT 1 NM01720FE45887 10464 DURING THE ACCOMPLISHMENT OF ROUTINE D-CHECK WORKCARD 00-153, THE FOLLOWING WAS FOUND, FUSELAGE FRAME STATION 7961, CENTER WING STATION 1040 LEFT, REF F27 IPC 53-40-01, FIG 01, PG 1. FUSELAGE FRAME P/N 5215-012-401. THE CENTER WING FWD ATTACH FITTING P/N 5215-012-401 WAS FOUND TO HAVE SURFACE LEVEL 1 CORROSION AT THE FOUR O'CLOCK POSITION OF HOLE CIRCUMFERENCE. CORROSION WAS REMOVED BY REAMING HOLE TO OVERSIZE. REPAIRED CRACK BY SPOT FACING THE FWD SIDE OF THE FITTING WITH INSTALLATION OF NEW .015 BUSHING PER FOKKER F27 SB 57-51 AND FILLER PER FOKKER RLD APPROVED INSTRUCTIONS. (M) 2H72 4T A817 19950901004691995090100469NM 1995 9 1 F3LA95014 119950720A793356B17D OIL TEMP BULB BOEING737 737201 1384454NM RT ENGINE FAILED A F3LAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03214AU 20214 OMA - AIR TURNBACK, FLIGHT CREW REPORTED HIGH OIL TEMPERATURE INDICATED ON RIGHT ENGINE. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO OMAHA. UPON ARRIVAL IN OMAHA, MAINTENANCE REPLACED THE OIL TEMPERATURE SENSING BULB, CHECKED AND CLEANED ELECTRICAL CONNECTIONS. THE AIRCRAFT GROUND CHECKED OK AND WAS FERRIED TO DENVER. IN DENVER, MAINTENANCE DISASSEMBLED AND CHECKED CONNECTORS AND WIRING BETWEEN THE OIL TEMPERATURE SENSING BULB AND THE OIL TEMPERATURE INDICATOR, AND CHECKED OK. PERFORMED OPERATIONAL CHECK OF ENGINE AND CHECKED OK. (M) 2L72 4F A16WE 19950901004701995090100470WP 1995 9 1 HAL95096 119950731A335026XN3359 EEL POWER PACK DOUG DC9 DC951 3022051WP COCKPIT DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13601AP 9149 47658 HNL - COCKPIT EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY LIGHT POWER PACK. OPERATIONS CHECK OK. (M) 2L72 4F A6WE 19950901004711995090100471WP 1995 9 1 HAL95097 119950802A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN DISCONNECTED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13601AP 47658 HNL - SECTION OF FLOOR EMERGENCY LIGHTS INOPERABLE. RECONNECTED WIRE 7-10. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950901004721995090100472WP 1995 9 1 HAL95098 119950805A3350 EEL BULB DOUG DC9 DC951 3022051WP OVERWING FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 47662 HNL - RIGHT OVERWING EMERGENCY LIGHTS INOPERABLE. RELAMPED, OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950901004731995090100473WP 1995 9 1 HAL95100 119950805A3350 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 47662 HNL - FORWARD AISLE EMERGENCY CEILING LIGHTS VERY DIM. REPLACED EMERGENCY CEILING LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950901004741995090100474WP 1995 9 1 IXXA199570 119950810A21105614845517 CABIN COMPRESSOR DOUG DC8 DC863F 302198FWP NR 2 FAILED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23906R 46087 BETWEEN IAH AND BRO, THE NR 2 CABIN COMPRESSOR STALLED AND CREATED LOUD NOISE AND OILY FUMES IN THE COCKPIT. MAINTENANCE DETERMINED THAT THE CABIN COMPRESSOR HAD SEIZED. THE NR 2 CABIN COMPRESSOR WAS DEFERRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2L74 4F 4A25 19950901004751995090100475WP 1995 9 1 IXXA199571 119950804A57435611425 ATTACH FITTING DOUG DC8 DC871F 302199DWP LT MLG CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23827BX7252411928 45971 DURING C-CHECK, THE LEFT MLG ATTACH FITTING WAS FOUND TO BE CRACKED. A CRACK IN EXCESS OF 2.5 INCHES WAS LOCATED IN THE BOTTOM OF LUG 'D' OF THE ATTACH FITTING. (SEE SB 57-94, VIEW JJ). THE ATTACH FITTING WAS REPLACED IAW THE DC-8 SRM, MM, AND DOUG INSTALLATION GUIDE. ATI JOBCARD 74201, BRAKE PLUMBING CHECK, WAS ACCOMPLISHED. (M) 2L74 4F RT4A25 19950901004761995090100476EU 1995 9 1 M3HA95014 119950810A335060001 EEL WIRE AEROSPATR42 ATR42320 8680930EU PAX DOOR BROKEN A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13983MA1687 243 308 HNL - FLT 704 - DURING C1P7 INSPECTION, THE PASSENGER STAIR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT SOCKET. OPERATIONAL TEST GOOD. (M) 2H72 4T RTA53EU 19950901004771995090100477NM 1995 9 1 MZZA9543 119950806A291065178444440 HYD TUBE BOEING727 727224 1384076NM 'A' HYD SYSTEM LEAKING A MZZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP1379745 22448 FLT NR 956 - GUM - EN ROUTE FROM TKK TO PNI NR 1 ENGINE 'A' HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP WAS TURNED OFF. PRESSURE STABILIZED AT 3000 PSI AND QUANTITY DECREASED TO 1/2 GALLONS. ABNORMAL CHECKLIST AND PROCEDURES COMPLIED WITH. DIVERTED TO GUM. FOUND PRESSURE SUPPLY LINE FROM 'A' SYSTEM MODULE WITH LEAKING 'B' NUT. INSTALLED SERVICEABLE LINE AND UNION. PERFORMED OPERATIONAL AND LEAK CHECK. (M) 2L73 4F A3WE 19950901004781995090100478NE 1995 9 1 REXA95046 219950519A7200CT75A2 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RIGHT MALFUNCTIONED A REXAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 SO25406BH18376 340A074 GEE367282KU LOST RIGHT ENGINE OIL PRESSURE, CWP VERIFIED BY GAUGE, SHUTENGINE DOWN. INSPECTED ENGINE FOUND TO BE WITHIN OVER SERVICE LIMIT TABLE 206 GE MM OK FOR SERVICE OR 10 ADDITIONAL FLIGHT HOURS. (M) 2L72 4T4 TRTA52EU E8NE6 19950901004791995090100479EU 1995 9 1 REXA95047 119950801A3230L38710SA SWIVEL SAAB SF340 SF340A 7850100EU LT MAIN GEAR LEAKING A REXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25324PX 340A048 AFTER TAKEOFF HYD WARNING MAIN ACCUM WENT TO ZERO HYD QTY WENT TO ZERO. REMOVED AND REPLACED LEFT SWIVEL AT DOWNLOCK ACTUATOR, BLEED SWIVEL SERVICED HYD RESERVOIR PERFORMED GEAR SWING. (M) 2L72 4T RTA52EU 19950901004801995090100480NM 1995 9 1 TSAA9529158 119950805A2910 HYD LINE BOEING737 737297 1384480NM LT MLG RUPTURED A TSAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP1370724 21740 FLT 63 - HNL-LIH - 500 FEET AFTER DEPARTURE, A SYSTEM FAILED. REPLACED LEFT MLG UPLOCK ACTUATOR LINE DUE TO RUPTURE. CHECKED NR 1 AND NR 2 ENGINE CASE DRAW FILTERS FOR CONTAMINATION. RAN NR 1 AND NR 2 ENGINE LEAK CHECK CASE DRAIN FILTERS AND HYDRAULIC LINE INSTALLATION. CYCLED ALL FLIGHT CONTROLS. REPLENISHED HYDRAULIC FLUID. OPS CHECK OK. (M) 2L72 4F A16WE 19950901004811995090100481NM 1995 9 1 TWRA9541 119950726A33509008 EEL BATTERY PACK BOEING747 747282B 1384860NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15610FF 20501 AT R4 DOOR PASSAGEWAY BOTH EXIT SIGNS (FWD AND AFT) ARE INOPERATIVE. REPLACED BATTERY PACK AFT OF R4 DOOR EMERGENCY LIGHTS, OPS CHECK OK. (M) 2L74 4F A20WE 19950901004821995090100482NE 1995 9 1 TWRA9542 219950727A7530747955 VANE CONTROL BOEING747 747131 1384881NM PWA JT9 JT9D7A 52054NE NR 1 ENG MALFUNCTIONED A TWRAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 EA15608FF 19672 DURING CRUISE AT FL 35.0, NR 1 ENGINE FLAMED OUT UNABLE TO RESTART DESCENDED TO 24,000 FEET RESTARTED ENGINE. NO ENGINE RESPONSE TO THRUST LEVER MOVEMENT SHUT DOWN ENGINE RETURNED TO JFK. FOUND NR 1 ENGINE EVC AT FAULT. REMOVED AND REPLACED EVC, OPS CHECK NORMAL DURING TESTS. (M) 2L74 4F4 F A20WE E20EA 19950901004831995090100483NM 1995 9 1 TWRA9543 119950727A5210 DOOR SILL BOEING747 747238B 1384828NM MAIN CABIN DIRTY A TWRAK NONE O OTHER ININSP/MAINT 1 EA15614FF 20534 R1 MAIN ENTRY DOOR WOULD NOT GO INTO AUTOMATIC. FOUND DEBRIS IN SILL, REMOVED DEBRIS AND CLEANED SILL. DOOR OPS NORMAL IN ALL MODES. (M) 2L74 4F A20WE 19950901004841995090100484NM 1995 9 1 TWRA9544 119950726A3350 EEL WIRE BOEING747 747282B 1384860NM CABIN SHORTED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15610FF 20501 UPPER DECK EGRESS LIGHTS AT SEATS AND COCKPIT INOPERATIVE. REPLACED SHORTED EGRESS FEED. REPLACED WIRING TO EXIT EGRESS SIGN IN COCKPIT. OPS CHECK OK. (M) 2L74 4F A20WE 19950901004851995090100485NM 1995 9 1 TWRA9545 119950726A3350 EEL WIRE BOEING747 747282B 1384860NM CABIN BROKEN A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15610FF 20501 C-ZONE EGRESS LIGHTS RIGHT SIDE INOPERATIVE. REPLACED BROKEN GROUND WIRE AT BATTERY PACK, OPS CHECK OK (M) 2L74 4F A20WE 19950901004861995090100486NM 1995 9 1 TWRA9546 119950726A3350 EEL WIRING STRIP BOEING747 747282B 1384860NM CABIN SHORTED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15610FF 20501 D-ZONE EGRESS LIGHTS RIGHT SIDE INOPERATIVE. REPLACED SHORTED DAMAGED EGRESS STRIP, REPAIRED FLOOR WIRING, OPS CHECK OK. (M) 2L74 4F A20WE 19950901004871995090100487SO 1995 9 1 WTAA950235 119950725A3260922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO NLG INOPERATIVE A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17453UE 120148 PSP - NOSE LANDING GEAR 'A' SYSTEM RED INDICATION LIGHT AND 'B' SYSTEM GREEN INDICATION LIGHT REMAINED ILLUMINATED FOLLOWING GEAR RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND DOWNLOCK 'A' SYSTEM INDICATION TO BE FAULTY (DOWN LOCK SENSOR). SWAPPED 'A' AND 'B' SYSTEM SENSOR PER SNL 120-032-0015 AND DEFERRED 'B' SYSTEM PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE CLEARED DEFERRAL WITH THE REPLACEMENT OF THE NOSE GEAR 'A' DOWNLOCK PROXIMITY SENSOR. (M) 2L72 4T RTA31SO 19950901004881995090100488EU 1995 9 1 WTAA950236 119950727A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU LT MLG FAILED A WTAAO OTHER N FALSE WARNING DEDESCENT 1 WP17428UE 806 VIS - LEFT MAIN LANDING GEAR 'RED' UNSAFE LIGHT REMAINED ILLUMINATED FOLLOWING GEAR EXTENSION. NORMAL POSITION INDICATIONS RECEIVED FOLLOWING SUBSEQUENT GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR DOWN LOCK MICROSWITCH. GEAR POSITION INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950901004891995090100489EU 1995 9 1 95ZZZM319 119950726A553013708F1 HINGE BAG JETSTMJETSTM3201 1500217EU VERT STAB CRACKED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03931AE6971 931 LIT - UPON REMOVAL OF RUDDER ASSY, DURING HEAVY MAIN BASE VISIT, UPPER VERTICAL STABILIZER TO RUDDER HINGE HAD FATIGUE CRACKING AROUND THE CENTER LUG OF THE HINGE. REMOVED AND REPLACED HINGE. 2L72 4T RTA56EU 19950901004901995090100490EU 1995 9 1 95ZZZM320 119950729A3240 BRAKE SAAB SF340 340B 7860101EU RT MLG SMOKING A NVEAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO03250AE 340B250 FLT NR 4917 - PIT - DURING TAXI INTO GATE, FLIGHT ATTENDANT REPORTED TO THE CAPTAIN THAT THE RT MAIN LANDING GEAR WAS SMOKING. AIRCRAFT STOPPED, EMERGENCY PERSONNEL WAS NOTIFIED, CREW THEN ACTIVATED ENGINE FIRE BOTTLES AND EVACUATED PASSENGERS FROM AIRCRAFT. RIGHT MAIN LANDING BRAKE WAS EXTINGUISHED NO INJURIES WERE REPORTED. (M) 2L72 4T RTA52EU 19950901004911995090100491NE 1995 9 1 95ZZZM321 219950728A7314358200 FUEL PUMP BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE NR 1 ENGINE FAILED A RYNAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 CE07428EX 19097 NR 1 ENGINE FAILED AFTER TAKEOFF, RETURNED TO BWI, UPON LANDING THE NR 3 MAIN LANDING GEAR TIRE BLEW. REPLACED THE NR 1 ENGINE FUEL PUMP, FUEL CONTROL AND THE NR 3 AND NR 4 MAIN TIRE ASSEMBLIES, OPS CHECKED GOOD. (M) 2L73 4F4 F A3WE E2EA 19950901004971995090100497WP 1995 9 1 95ZZZM327 119950110A5320 FITTING DOUG DC9 DC932 3022066WP FS 756 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE KEEL BEAM FITTING AT FS 756 WAS CRACKED IN THE LEFT WW. REMOVED AND REPLACED THE FITTING IAW DC9 SRM 51-30-2 AND 51-30-1. N/R NR 027N1/0668. 2L72 4F A6WE 19950901004981995090100498WP 1995 9 1 95ZZZM328 119950108A5311 FRAME DOUG DC9 DC932 3022066WP FS 522/541 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME BETWEEN LONGERON 28L AND 28R WAS FOUND CORRODED AT FS 522 AND 541. FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-10-3. N/R NR 027N1/0447 AND 0448. 2L72 4F A6WE 19950901004991995090100499WP 1995 9 1 95ZZZM329 119950106A5330 SKIN DOUG DC9 DC932 3022066WP FS 1025 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE SKIN AT FS 1025 AND LONGERON 23L IS CORRODED. FABRICATED AND INSTALLED SKIN REPAIRS IAW DC9 SRM 53-10-1, 53-01, 51-10-3 AND 51-30-2. N/R NR 027N1/0421. 2L72 4F A6WE 19950901005001995090100500WP 1995 9 1 95ZZZM330 119950104A5314 KEEL BEAM DOUG DC9 DC932 3022066WP CENTER WING CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE CENTER WING KEEL AREA HAS EXTENSIVE CORROSION DAMAGE ON THE RT SIDE. FABRICATED AND INSTALLED REPAIRS FOR THE CENTER WING KEEL PANEL AND LONGERONS 29 LT AND RT IAW DC9 SRM 51-10-3, 51-30-0, 53-31-0 AND 51-10-2A. N/R NR 027N1/-391. 2L72 4F A6WE 19950901005051995090100505SO 1995 9 1 C2XA5IA176 119950808A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005061995090100506SO 1995 9 1 C2XA95IA154 119950802A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 2, AND NR 3 SKIN SUPPORTS CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005071995090100507SO 1995 9 1 C2XA95IA155 119950802A572012017057017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 6 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005081995090100508SO 1995 9 1 C2XA95IA156 119950802A572012017057005 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 4 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005091995090100509SO 1995 9 1 C2XA95IA157 119950802A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING NR 3 SKIN SUPPORT AT RIB NR 16 CRACKED, LOWER SKIN. MAINTENANCE REMOVED AND REPLACED THE SUPPORT AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005101995090100510SO 1995 9 1 C2XA95IA158 119950802A572012017059009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 18. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005111995090100511SO 1995 9 1 C2XA95IA159 119950802A572012017060011 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER FORWARD SKIN SUPPORT CRACKED AT RIB NR 19. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005121995090100512SO 1995 9 1 C2XA95IA160 119950802A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING NR 4 SKIN SUPPORT CRACKED AT RIB NR 21 UPPER. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005131995090100513SO 1995 9 1 C2XA95IA161 119950802A572012017066031 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT NR 3 CRACKED AT RIB NR 25. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005141995090100514SO 1995 9 1 C2XA95IA162 119950802A572012017066037 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORTS NR 4 AND NR 5 CRACKED AT RIB NR 25. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005151995090100515SO 1995 9 1 C2XA95IA163 119950802A532012020235005 BRACKET EMB 120 EMB120RT SO AFT CABIN CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD BRACKET FOR CARGO DOOR COUNTER BALANCE TORSION RODS CRACKED. MAINTENANCE REMOVED AND REPLACED THE BRACKET, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005161995090100516SO 1995 9 1 C2XA95IA164 119950803A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916710 120106 IAH - DURING C-CHECK INSPECTION, FOUND RT WING UPPER NR 2 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005171995090100517EU 1995 9 1 C2XA95IA165 119950803A3350335189 EEL POWER WIRE AEROSPATR42 ATR42320 8680930EU PAX DOOR BROKEN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0914804 069 IAH - DURING 2A CHECK INSPECTION, FOUND LEFT AFT EXTERIOR EMERGENCY FLOOR LIGHT INOPERATIVE AT PASSENGER/CREW ENTRY DOOR. MAINTENANCE REPAIRED WIRING AT UPPER STEP AREA, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19950901005181995090100518SO 1995 9 1 C2XA95IA166 119950808A572012017056013 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER SKIN SUPPORT NR 2 CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005191995090100519SO 1995 9 1 C2XA95IA167 119950808A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005201995090100520SO 1995 9 1 C2XA95IA168 119950808A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005211995090100521SO 1995 9 1 C2XA95IA169 119950808A572012017057007 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005221995090100522SO 1995 9 1 C2XA95IA170 119950808A572012017062013 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 1 UPPER SKIN SUPPORT CRACKED AT RIB NR 21. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005231995090100523SO 1995 9 1 C2XA95IA171 119950808A572012017056013 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2, AND NR 4 SKIN SUPPORTS CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005241995090100524SO 1995 9 1 C2XA95IA172 119950808A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005251995090100525SO 1995 9 1 C2XA95IA173 119950808A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 5 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005261995090100526SO 1995 9 1 C2XA95IA174 119950808A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005271995090100527SO 1995 9 1 C2XA95IA175 119950808A572012017057008 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0947722 120166 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER NR 2 SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950901005281995090100528NM 1995 9 1 EIAA9534 119950723A3350 EEL WIRE BOEING747 747212B 1384886NM CABIN BROKEN A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09482EV 20713 SBGR - RIGHT SIDE EMERGENCY LIGHTS C-ZONE INOP. NO PASSENGERS ALLOWED IN C-ZONE. ALTERNATE LIGHTS INOPERATIVE TRANSFERRED TO DMI NR 746 PER MEL 33-16-1. REPAIRED WIRING AT SEATS 22, 25, 27 AND 30. AIRCRAFT RIGHT EMERGENCY LIGHTS OPERATIONAL CHECK PER MM 33-50-00 CLEARED DMI NR 476. (M) 2L74 4F A20WE 19950901005321995090100532WP 1995 9 1 95ZZZM338 119950106A5320 SPLICE DOUG DC9 DC932 3022066WP FS 813/889/945 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO BAY LONGERON 30 WAS FOUND WITH 3 IMPROPER SPLICES WITH CORROSION AT FS 813, 889 AND 945. FABRICATED AND INSTALLED 3 NEW SPLICES IAW DC9 SRM 53-02, 52-00. N/R NR 027A1/-0169. 2L72 4F A6WE 19950901005331995090100533WP 1995 9 1 95ZZZM339 119950104A5311 FRAME DOUG DC9 DC932 3022066WP FS 465 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME AT FS 465 BETWEEN LONGERON 29R AND LONGERON 30 ON INTERCOSTALS AND GUSSET WAS FOUND TO BE CORRODED. FABRICATED AND INSTALLED REPAIR ANGLES AND DOUBLERS FOR THE FRAME, GUSSETS, AND INTERCOSTALS IAW DC9 SRM 51-102, 53-03-02A, 51-10-2 AND 51-30-5. N/R NR 027A1/0120. 2L72 4F A6WE 19950901005341995090100534WP 1995 9 1 95ZZZM340 119950104A5311 FRAME DOUG DC9 DC932 3022066WP FS 446 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FUSELAGE FRAME UPPER CHORD AT FS 446 BETWEEN LONGERON 25R AND LONGERON 30 WAS FOUND CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED A REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-03-02A, 51-10-4, AND DPS 10.225 OF PARA F. N/R NR 207A1/0119. 2L72 4F A6WE 19950901005351995090100535WP 1995 9 1 95ZZZM341 119950110A5320 ANGLE DOUG DC9 DC932 3022066WP FS 200 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE UPPER CUSP AT THE R-1 DOOR ENTRY WAS FOUND TO BE EXTENSIVELY CORRODED AT FS 200. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-05, 51-10-3, 51-30-1, 51-20-0 AND MM20-30-1. N/R NR 027N1/0658. 2L72 4F A6WE 19950901005361995090100536WP 1995 9 1 95ZZZM342 119950108A5311 FRAME DOUG DC9 DC932 3022066WP FS 332 TO 503 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11936VV 47397 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FORWARD CARGO COMPARTMENT FRAMES ARE CORRODED AT FS 332 THROUGH 503 BETWEEN LONGERONS 28R AND 28L. FABRICATED AND INSTALLED REPAIR MEMBERS AND DOUBLERS IAW DC9 SRM 53-03, 51-10-2A, AND 51-10-3. N/R NR'S 027N1/0449, 0450, 0451, 0452, 0454, 0455, AND 0456. 2L72 4F A6WE 19950901005371995090100537WP 1995 9 1 95ZZZM343 119950122A5313 LONGERON DOUG DC9 DC932 3022066WP FS 200 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 23 AT FS 200 WAS FOUND CRACKED. FABRICATED AND INSTALLED REPAIR MEMBERS IAW DC9 SRM 53-02, 51-10-3 AND 51-30-2. 2L72 4F A6WE 19950901005381995090100538WP 1995 9 1 95ZZZM344 119950124A5311 FRAME DOUG DC9 DC932 3022066WP FS 522 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 522 AT LONGERON 28L WAS FOUND WITH CORROSION. FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4, AND 53-10-1. N/R NR 027N1/0632. 2L72 4F A6WE 19950901005391995090100539WP 1995 9 1 95ZZZM345 119950122A5342 LE SKIN DOUG DC9 DC932 3022066WP VERT STAB CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP INLAKE CITY, FLORIDA, THE VERTICAL STABILIZER L/E WAS FOUND WITH 5 CRACKED STIFFENERS. FABRICATED AND INSTALLED NEW STIFFENERS IAW DC9 SRM 55-02 AND MM 51-00. N/R NR027N1/0598. 2L72 4F A6WE 19950901005401995090100540WP 1995 9 1 95ZZZM346 119950124A5311 FRAME DOUG DC9 DC932 3022066WP FS 541 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE TEFLON STRIP ON THE UPPER FLOOR FRAMES AT FS 541. FABRICATED AND INSTALLED FRAME REPAIRS IAW DC9 SRM 53-03-2A, 51-10-3, AND 51-10-2A. N/R NR 027N1/0658. 2L72 4F A6WE 19950901005411995090100541WP 1995 9 1 95ZZZM347 119950124A5311 FRAME DOUG DC9 DC932 3022066WP FS 1019 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND UNDER THE NUTPLATES ON THE FLOOR FRAME AT FS 1019 PRESSURE DOME. FABRICATED AND INSTALLED PRESSURE DOME FLOOR FRAME REPAIRS IAW DC9 SRM 53-05 AND 51-10-3. N/R NR 027N1/0643. 2L72 4F A6WE 19950901005421995090100542WP 1995 9 1 95ZZZM348 119950124A5311 FRAME DOUG DC9 DC932 3022066WP FS 560 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FRAME SEGMENT AT FS 560 AT LONGERON 28L WAS FOUND CORRODED. FABRICATED AND INSTALLED A NEW FRAME SEGMENT IAW DC9 SRM 51-10-2A, 51-10-4 AND 53-10-1. N/R NR 027N1/0633. 2L72 4F A6WE 19950901005431995090100543WP 1995 9 1 95ZZZM349 119950124A5320 FRAME DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A 1 INCH CRACK WAS FOUND IN THE AFT CARGO DOOR FRAME. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 52-03, 51-10-4, AND 51-30-5. N/R NR 027N1/0710. 2L72 4F A6WE 19950901005441995090100544WP 1995 9 1 95ZZZM350 119950114A5330 SKIN DOUG DC9 DC932 3022066WP FS 275 DENTED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .052 IN DEPTH DENT WAS FOUND IN THE FUSELAGE (PRESSURIZED) SKIN FS 275. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04 FIG 38. N/R NR 027N1/0281. 2L72 4F A6WE 19950901005451995090100545WP 1995 9 1 95ZZZM351 119950113A5330 SKIN DOUG DC9 DC932 3022066WP FS 332 DENTED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .027 INCH DEPTH DENT WAS FOUND AT FS 332 BETWEEN LONGERONS 23L AND 24L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-04, 51-30-2 AND 51-10-4. N/R NR 027N1/0131. 2L72 4F A6WE 19950901005461995090100546WP 1995 9 1 95ZZZM352 119950113A5330 SKIN DOUG DC9 DC932 3022066WP FS 945 DENTED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A .023 INCH DEPTH DENT WAS FOUND AT FS 945 AND LONGERON 26L. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 53-04 AND 51-30-2. N/R NR 027N1/0127. 2L72 4F A6WE 19950901005471995090100547WP 1995 9 1 95ZZZM353 119950113A5330 SKIN DOUG DC9 DC932 3022066WP FS 867-900.5 DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A LIFE LIMITED REPAIR WAS FOUND BETWEEN LONGERON 27L AND 28R AT FUSELAGE STATION 867 TO FS 900.5. FABRICATED AD INSTALLED FUSELAGE (PRESSURIZED) SKIN REPAIRS IAW DC9 SRM 51-10-3 AND 53-04 AND AERO CORP EO 95-111 REV IR DATED 2/1/95 FAA FORM 8110-3 DATED 2/15/95. N/R NR 027A1/0135. 2L72 4F A6WE 19950901005481995090100548WP 1995 9 1 95ZZZM354 119950115A5311 FRAME DOUG DC9 DC932 3022066WP FS 870 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CRACKS WERE FOUND PROGRESSED BEYOND THE STOP DRILL IN THE LOWER FRAME AT FS 870 ABOVE LONGERONS 29 LT AND RT AND 28R. FABRICATED AND INSTALLED NEW LOWER FRAME IAW DC9 SRM 51-10-3, 53-03 AND 51-10-2A. N/R NR 027N1/0383. 2L72 4F A6WE 19950901005491995090100549WP 1995 9 1 95ZZZM355 119950115A5320 RIB DOUG DC9 DC932 3022066WP FS 813 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE LOWER RIB AT FS 813 LONGERON 27L TO LONGERON 27R WAS FOUND CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-03, 51-10-2A AND 51-30-3. N/R NR 027N1/0381. 2L72 4F A6WE 19950901005501995090100550WP 1995 9 1 95ZZZM356 119950113A5311 FRAME DOUG DC9 DC932 3022066WP FS 218 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11937VV 45774 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FRAME BETWEEN LONGERONS 24R AND 26R AT FS 218. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-2A, 53-03, 53-01, 51-10-4 AND 51-10-3. N/R NR 027A1/0145. 2L72 4F A6WE 19950901005561995090100556NM 1995 9 1 AWXA9500501 119950806A5320 EXTRUSION BOEING737 7373G7 1384595NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - DURING SCHEDULED C7 INSPECTION, FOUND CORROSION IN AREA OF LEFT AFT LAV, UPPER CHORD OF BS 986.5 LBL 43 AROUND NUT PLATE HOLE. REPAIR ANGLE INSTALLED PER ER 3-53-16-27. (M) 2L72 4F RTA16WE 19950901005571995090100557NM 1995 9 1 AWXA9500502 119950806A5330 SKIN BOEING737 7373G7 1384595NM BS 340 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - DURING SCHEDULED C7 INSPECTION, FOUND FUSELAGE SKIN CRACKED IN LIGHTNING STRIKE REWORK AREA AT STATION 340 STRINGER 25R. REPAIRED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 19950901005581995090100558NM 1995 9 1 AWXA9500503 119950806A5330 SKIN BOEING737 7373G7 1384595NM BS 265 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - DURING SCHEDULED C7 INSPECTION, FOUND FUSELAGE SKIN CRACKED IN LIGHTNING STRIKE REWORK AREA AT STATION 265 BETWEEN STRINGER 24R AND STRINGER 25R. REPAIRED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 19950901005591995090100559NM 1995 9 1 AWXA9500504 119950806A5330 SKIN BOEING737 7373G7 1384595NM BS 280 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28155AW 23777 PHX - DURING SCHEDULED C7 INSPECTION, FOUND THREE SMALL CRACKS IN FUSELAGE SKIN AT STATION 280 BETWEN S 24R AND S 25R LIGHTNING STRIKE AREA. REPAIRED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 19950901005601995090100560NM 1995 9 1 AWXA9500506 119950805A783017310211 TR DOOR BOEING737 737277 1384570NM NR 2 ENG OUT OF ADJUST A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 78023 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND NR 2 ENGINE UPPER T/R BUCKET DOOR BUMPERS DO NOT HAVE FULL CONTACT. WELDED PER ER 2-78-32-02. (M) 2L72 4F RTA16WE 19950901005611995090100561NM 1995 9 1 AWXA9500507 119950805A53476065497178T6511 SEAT TRACK BOEING737 737277 1384570NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND AFT GALLEY SEAT TRACK ATTACH POINTS CORRODED ON UNDER SIDE OF FLOOR BOARD AT ATTACH HOLES, BS 986.5 TO 1016, WL 208.1. REMOVED AND REPLACED SEAT TRACK EXTRUSION AT RBL 30 PER SRM 51-30-2. (M) 2L72 4F RTA16WE 19950901005621995090100562NM 1995 9 1 AWXA9500508 119950805A531385311026105 STRINGER BOEING737 737277 1384570NM BS 945 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND STRINGER 27R BS 947 CORRODED. REMOVED AND REPLACED STRINGER 27R SECTION FROM BS 945 TO 957 PER SRM 53-10-3, FIG 1. (M) 2L72 4F RTA16WE 19950901005631995090100563NM 1995 9 1 AWXA9500509 119950805A575365464285 FLAP TRACK BOEING737 737277 1384570NM NR 2 TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION,FOUND NR 2 FLAP TRACK CORRODED AT AFT SPAR PARTING SURFACE. REMOVED AND REPLACED FLAP TRACK ASSY PER BMM 27-51-151, PAGE 406. (M) 2L72 4F RTA16WE 19950901005641995090100564NM 1995 9 1 AWXA9500510 119950805A5330 SKIN BOEING737 737277 1384570NM R2 DOOR CUTOUT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT, UPPER FORWARD CORNER UPPER HINGE CUTOUT. FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR PER SRM 53-30-3, FIGURE 21A. (M) 2L72 4F RTA16WE 19950901005651995090100565NM 1995 9 1 AWXA9500511 119950805A532065C352421 DOOR FRAME BOEING737 737277 1384570NM CARGO COMPT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND FORWARD CARGO DOOR CUTOUT FRAME CRACKED AT STATION 440 STOP 5. REMOVED AND REPLACED FRAME PER BOEING DRAWING 65C35244 AND SRM 51-10-1. (M) 2L72 4F RTA16WE 19950901005661995090100566NM 1995 9 1 AWXA9500512 119950805A3230658005110 DRAG BRACE BOEING737 737277 1384570NM NLG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 465 22648 DURING SCHEDULED C-15 INSPECTION, FOUND NOSE GEAR 'A' FRAME CRACKED BY DOOR CRANK ARMS. REMOVED AND REPLACED NLG 'A' FRAME (DRAG BRACE) PER AWA TASK CARD R4N32003. (M) 2L72 4F RTA16WE 19950901005671995090100567NE 1995 9 1 AWXA9500513 219950805A7230537131 FAN INLET CASE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 1 ENG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND NR 1 ENGINE IGV CASE CRACKED AT WELD AT 10:00 POSITION. WELDED CRACK PER ER 2-72-23-02B. (M) 2L72 4F4 FRTA16WE E2EA 19950901005681995090100568NM 1995 9 1 AWXA9500519 119950808A3350 EEL ASSY BOEING757 7572G7 1384963NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 25 TO AFT. REPAIRED LIGHTS, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950901005691995090100569WP 1995 9 1 9513149607 119950424A5752 TAB DOUG DC9 DC932 3022066WP RT AILERON DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND APPROXIMATELY FOUR SQUARE INCHES OF DELAMINATION ON THE RIGHT AILERON CONTROL TAB LOWER SKIN. REMOVED AND REINSTALLED TAB IAW MM 27-10-1. MFG. PART NUMBER 5910047-2. 2L72 4F A6WE 19950901005701995090100570WP 1995 9 1 9513159929 119950712A5313 LONGERON DOUG DC9 DC931 3022065WP FS 813 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018923E 45838 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN LONGERON 30 AT FS 813. REPAIRED LONGERON PER EA 99-97390. 2L72 4F A6WE 19950901005711995090100571WP 1995 9 1 9513169929 119950713A5330 SKIN DOUG DC9 DC931 3022065WP FS 197 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018923E 45838 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN FS 197 AT LONGERON 22L. REPAIRED SKIN PER EA 99-94700. 2L72 4F A6WE 19950901005721995090100572WP 1995 9 1 9513179969 119950725A5220 FRAME DOUG DC9 DC931 3022065WP EMER EXIT DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING PERIODIC CHECK, FOUND A CRACK IN THE OVERWING EMERGENCY EXIT DOOR PAN ADJACENT TO THE NR 14 STOP FITTING. REPAIRED PAN (P/N 5913195-1) PER EA 99-98720. 2L72 4F A6WE 19950901005731995090100573WP 1995 9 1 9513189929 119950727A5320 DOUBLER DOUG DC9 DC931 3022065WP PAX DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018923E 45838 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR CUTOUT, LOWER INTERNAL DOUBLER BENEATH THE SEAL DEPRESSOR. REPAIRED PER EA 99-94734. 2L72 4F A6WE 19950901005741995090100574WP 1995 9 1 9513199868 119950815A5313 LONGERON DOUG DC9 DC951 3022051WP FS 860-870 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01777NC 47787 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 860 - 870. REPAIRED LONGERON (P/N 5924878-503) PER EA 98-100854. 2L72 4F A6WE 19950901005751995090100575WP 1995 9 1 9513201221 119950816A5753 VANE DOUG DC10 DC1030 3023501WP LT TE FLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 16272 46579 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE LEFT WING OUTBOARD FLAP VANE LOWER SURFACE. REPLACED VANE. MFG. P/N NRC6068-513. 2L73 4F A22WE 19950901005761995090100576WP 1995 9 1 9513211221 119950816A5753 VANE DOUG DC10 DC1030 3023501WP LT TE FLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 16275 46579 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE LEFT WING INBOARD FLAP VANE UPPER SURFACE. REPLACED VANE. MFG. P/N NRC6062-519. 2L73 4F A22WE 19950901005771995090100577WP 1995 9 1 9513229969 119950817A5220 FRAME DOUG DC9 DC931 3022065WP EMER EXIT DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING H-CHECK, FOUND A CRACK IN THE LEFT FORWARD OVERWING EMERGENCY EXIT DOOR PAN. REPAIRED PAN (P/N 5913195-1) PER EA 99-97116. 2L72 4F A6WE 19950901005781995090100578WP 1995 9 1 9513239998 119950818A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING. 2L72 4F A6WE 19950901005791995090100579WP 1995 9 1 9513249968 119950825A5755 SKIN DOUG DC9 DC931 3022065WP LT SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019332 6046 47264 DURING A-CHECK, FOUND A 7 INCH CRACK IN THE LEFT INBOARD SPOILER LOWER SKIN. REPLACED SPOILER. MFG. P/N 5910055-515. 2L72 4F A6WE 19950901005801995090100580WP 1995 9 1 9513259163 119950825A5711 SPAR WEB DOUG DC9 DC914 3022034WP RT WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING AFT SPAR WEB AT THE NR 2 STOP HINGE, LOWER INBOARD ATTACH STUD. REPAIRED PER EA 91-97631. 2L72 4F A6WE 19950901005811995090100581WP 1995 9 1 9513269163 119950825A5330 SKIN DOUG DC9 DC914 3022034WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND TWO CRACKS IN THE FUSELAGE SKIN AT THE MAIN CABIN DOOR CUTOUT FS 200 BETWEEN LONGERONS 12L - 14L. REPAIRED SKIN PER EA 91-102773. 2L72 4F A6WE 19950901005821995090100582WP 1995 9 1 9513279886 119950826A5230 FITTINGS DOUG DC9 DC951 3022051WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01600TR 47783 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE FORWARD CARGO DOOR LOWER FITTINGS. REPLACED FITTINGS PER SRM 51-30-02, -05. 2L72 4F A6WE 19950901005831995090100583WP 1995 9 1 9513289953 119950826A5320 FITTINGS DOUG DC9 DC931 3022065WP FS 168-200 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND CORROSION ON FRAME FITTINGS FORWARD AND AFT OF THE GALLEY SERVICE DOOR FS 168 AND FS 200. REPLACED FITTINGS PER SRM 51-10-04. 2L72 4F A6WE 19950901005841995090100584NM 1995 9 1 9513296716 119950826A5751 SKIN BOEING747 747251F 1384898NM RT AILERON DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01616US 21120 DURING PERIODIC CHECK, FOUND DELAMINATION ON RIGHT OUTBOARD AILERON UPPER SURFACE WS 1508. REPAIRED PER SRM 51-40-14, PART 4, FIG. 9. 2L74 4F A20WE 19950901005851995090100585EA 1995 9 1 COM60547 119950830A2611473052 DETECTOR CNDAIRCL600 CL6002B19 EA CARGO MALFUNCTIONED A COMAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 SO01933CA3315 7040 CARGO SMOKE WARNING DURING TAXI, FIRE BOTTLES WERE DISCHARGED. REPLACED THE CARGO COMPARTMENT SMOKE DETECTOR AND FIRE BOTTLES, FALSE WARNING, NO INDICATION OF SMOKE OR FIRE. 2L72 4F RTA21EA 19950901005861995090100586NM 1995 9 1 DL72S953520 119950827A3350S106 EEL BATTERY PACK BOEING727 727232 1384082NM AFT AIRSTAIR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11532DA 22045 10615 DURING LAYOVER, FOUND THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT INOP. RELAMPED, CLEANED CONNECTIONS AND REPLACED BATTERY PACK. OPERATION NORMAL. 2L73 4F A3WE 19950901005871995090100587NM 1995 9 1 DL72S953521 119950827A3350BR9279108 EEL SIGN BOEING727 727232 1384082NM CABIN BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 EMERGENCY EXIT LIGHT FOUND BROKEN AND HANGING ON SIDEWALL PANEL SEAT ROW 20ABC. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL. 2L73 4F A3WE 19950901005881995090100588NM 1995 9 1 DL72S953523 119950724A5753652163234 DOUBLER BOEING727 727232 1384082NM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NR 3 MID-FLAP DURING HMV. SHOP INSP WAS FOUND TO HAVE AFT CORD SPAR DOUBLER CRACKED IN TWO PLACES, 19 INCHES AND 22 INCHES, FROM INBOARD END. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950901005891995090100589NM 1995 9 1 DL72S953524 119950724A5753652163234 AFT SPAR BOEING727 727232 1384082NM NR 3 TE MID FLAPCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11493DA 21062 NR 3 MID-FLAP DURING HMV. SHOP INSPECTION WAS FOUND TO HAVE AFT SPAR CORD CRACKED 56 INCHES FROM INBOARD END. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19950901005901995090100590NM 1995 9 1 DL72S953530 119950828A5754 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 NR 6 SLAT HAS .50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950901005911995090100591NM 1995 9 1 DL72S953531 119950828A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 CRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP. 2L73 4F A3WE 19950901005921995090100592NM 1995 9 1 DL72S953536 119950829A5230 SKIN BOEING727 727232 1384082NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11521DA 21472 C-2 DOOR SKIN CRACKED IN 2 PLACES AT UPPER EDGE 15 INCHES FWD OF AFT CORNER. REPAIRED PER SRM 52-00-3, FIG 3. 2L73 4F A3WE 19950901005931995090100593NM 1995 9 1 DL72S953538 119950829A3350RBS1 EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST LDLANDING 1 SO11470DA 20747 EMERGENCY TRACK LIGHTS INOP IN F/C CABIN, REPLACED PACK AND BATTERIES, FOUND LIGHT ASSEMBLY AT SEAT 2AB SHORTED. REMOVED LIGHT AND FWD LIGHT AT 2AB TO MCO PER MEL 33-00-17. REPLACED LIGHT ASSEMBLY AT SEAT 2AB. OPERATION NORMAL. 2L73 4F A3WE 19950901005941995090100594NM 1995 9 1 DL72S953544 119950829A5720 STIFFENER BOEING727 727232 1384082NM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 FOUND ON F-1 LETTER CHECK - FRONT SPAR STIFFENERS CRACKED AT NR 4 LEADING EDGE SLAT, INBOARD TRACK ROLLER BOX. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950901005951995090100595NM 1995 9 1 DL72S953545 119950829A3260 SWITCHES BOEING727 727232 1384082NM NLG DOOR DIRTY A DALAK NONE N FALSE WARNING APAPPROACH 1 SO11400DA 21144 ON APPROACH, NOSE GEAR DOOR LIGHTS ON FORWARD PANEL AND FLIGHT ENGINEER'S PANEL TOOK EXCEPTIONALLY LONG, 30-50 SECONDS, TO EXTINGUISH. CORRECTIVE ACTION. CLEANED DEBRIS FROM NOSE LANDING GEAR DOOR SWITCHES. CKS OK. NO MRR. REJECTED. 08-31-05 GT 595. 2L73 4F A3WE 19950901005961995090100596NM 1995 9 1 DL72S953547 119950828A53306517530 SKIN BOEING727 727232 1384082NM FS 1323 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11521DA 21472 DURING CV3 IN ATL, THE FUSELAGE SKIN WAS DENTED IN TWO PLACES AT FUSELAGE STATION 1323, STR 21L. IN ACCORDANCE WITH B727 SRM 53-30-3, FIGURE 3, AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. 2L73 4F A3WE 19950901005971995090100597NM 1995 9 1 DL72S953548 119950828A5312 BLKHD STIFFENER BOEING727 727232 1384082NM FS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11521DA 21472 AT CV3 IN ATL, A CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 8. THE CRACK WAS 1 INCH LONG. REPAIRED DAMAGE PER DL ERA 302413-14AD. AUTHORIZED BY B727-53-0175 REV. 2. 2L73 4F A3WE 19950901005981995090100598NM 1995 9 1 DL72S953549 119950829A5320651751737 BEAM BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 AT A LETTER CHECK IN TPA, A .50 INCH CRACK WAS FOUND IN THE UPPER TRANSVERSE BEAM GUSSET ANGLE AT F.S. 1273. ALSO, A .75 INCH CRACK IN THE ACCOMPANYING UPPER TRANSVERSE BEAM AT F.S. 1273. THE DAMAGED PARTS WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129 REV. 4. 2L73 4F A3WE 19950901005991995090100599NM 1995 9 1 DL72S953550 119950818A2761 ACTUATOR BOEING727 727232 1384082NM NR 13 SPOILER LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 ITEM: SPOILER ACTUATOR SUPPORT FITTING LOOSE INBD LOWER BOLT AT NR 13 SPOILER. REPAIRED FITTING PER MM 57-42-0 REV D. 2L73 4F A3WE 19950901006001995090100600NM 1995 9 1 DL72S953552 119950819A5320 ANGLE BOEING727 727232 1384082NM BS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11420DA 21273 AT LETTER CHECK IN TPA, THE UPPER CHORD AT RBL 20 RUNNING FORE/AFT IN THE AFT VENTRAL STAIRWAY TORQUE BOX WAS FOUND CRACKED AT STA 1273. THE INBOARD END OF THE FLOOR SUPPORT ANGLE AT STA 1273 HAD AN APPROX. 3 INCH CRACK AND THE FRAME BEAM HAD A 4 INCH LONG CRACK IN THE INBOARD END. THE AFT SUPPORT ANGLE WILL BE REPLACED TO FACILITATE INSTALLATION. THIS REPAIR WILL BE ACCOMPLISHED IN ACCORDANCE WITH S/B 727-53-0129, REV. 4. 2L73 4F A3WE 19950901006011995090100601NM 1995 9 1 DL733953551 119950822A5320 INTERCOSTAL BOEING737 737347 1384647NM R1 DOOR FRAME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11312WA 23598 AT HMV IN ATL, THE R1 DOOR FRAME INTERCOSTAL WAS FOUND CRACKED IN THE TYPICAL MANNER SHOWN IN S/B 737-53A1108, REV. 5. THIS REPAIR WAS ACCOMPLISHED IN PER AND IN ACCORDANCE WITH S/B 737-53A1108, REV. 5. 2L72 4F RTA16WE 19950901006021995090100602NM 1995 9 1 DL73E953561 119950825A3350 EEL BOEING737 737247 138448DNM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11244WA 23518 ON PRE-FLIGHT, FOUND EMERGENCY TRACK LIGHTS INOP AT SEAT ROWS 10 TO 15, FOUND SHORTED WIRES IN TRACK. REPAIRED WIRES, OPERATION NORMAL. ALSO, HAD FWD GALLEY AND BOTH AFT GALLEY DOORS EMERGENCY LIGHTS INOP. REPLACED FWD GALLEY LIGHT ASSEMBLY AND LENS. FOUND LEADS SHORTED TO GROUND AT AFT DOOR LIGHTS, REPAIRED WIRES OPERATION NORMAL. 2L72 4F A16WE 19950901006031995090100603NM 1995 9 1 DL757953532 119950829A3350767 EEL BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO11636DL 0 23763 AFT LEFT EMERGENCY LIGHT BEHIND FILLET PANEL INOP. RELAMPED, OPERATION NORMAL. 2L72 4F RTA2NM 19950901006041995090100604NM 1995 9 1 DL757953565 119950827A2450TB5012 TERMINAL BOEING757 757232 1384965NM P6-3 PANEL BURNED A DALAK NONE O OTHER ININSP/MAINT 1 SO11604DL 22811 DURING L/O, FWD EQUIP COOLING FAN C/B POPPED WITH NUMEROUS UNASSOCIATED MTC AND STATUS MSGS. FOUND TERMINAL STRIP TB5012 IN P6-3 PANEL AND BOTH TERMINALS NR 1 PHASE WIRE BURNED. REPLACED TB5012 AND COVER WITH MFG P/N MS27212-3-3 AND MS18029-353. REPLACED WIRE TERMINALS. ALL CHECKS NORMAL. 2L72 4F RTA2NM 19950901006051995090100605WP 1995 9 1 DLL10953517 119950815A5520 SUPPORT WEB LKHEED1011 10113851 5265010WP RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11729DA 193C1180 FOUND AT U-CK - RT ELEVATOR OUTBOARD BALANCE WEIGHT SUPPORT WEB CRACKED. VERIFIED BY DYE PENETRANT INSP. CORR - REMOVED OLD SUPPORT WEB AND DRILLED UP NEW WEB. COMPLETED INSTALLATION OF NEW WEB. INSTALLED WEIGHT. 2L73 4F A23WE 19950901006061995090100606WP 1995 9 1 DLL10953527 119950828A53121554950 BLKHD FITTINGS LKHEED1011 10113851 5265010WP AFT P DOME CRACKED A ADALAK NONE O OTHER ININSP/MAINT 1 SO11716DA 193C1095 DURING ACCOMPLISHMENT OF AN INSPECTION FOR THE AFT PRESSURE BULKHEAD, THE STR 58 AND STR 61 FITTINGS WERE FOUND TO BE CRACKED. THE FITTINGS ARE TO BE RELEASED ON A TIME LIMITED BASIS AND WILL BE REPLACED WITHIN 150 FLIGHT CYCLES, PER DL ERA 271719-14. 2L73 4F A23WE 19950901006071995090100607WP 1995 9 1 DLL10953535 119950829A2150 PACK 7339347 LKHEED1011 10113851 5265010WP NR 3 SMOKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO111734D UNKNOWN 193C1225 SMOKE IN AFT CABIN DURING FLT - ISOLATED NR 3 PACK AND APPEARED TO CLEAR - PACK TEMPS NORMAL. CORR. ACTN. CHKD ALL 3 A/C PACKS AND OK. RAN SYSTEMS ON GROUND WITH NO ODORS OR VISIBLE POLLUTANTS IN CABIN. RENDERED NR 3 PACK INOP PER MEL 21-51-07A AND PLACED ON MCO AND PLACARD. 2L73 4F A23WE 19950901006081995090100608WP 1995 9 1 DLL10953546 119950829A2120 DUCT 7339308 LKHEED1011 10113851 5265010WP AIR COND COMPT CRACKED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO111734D 920178 193C1225 DURING CLIMB-OUT THROUGH FL 220, A MUFFLED BANG WAS HEARD. AFT OVERFLOW VALVE WENT FULL CLOSED AND FWD VALVE SLOWLY WENT CLOSED. AS AIRCRAFT CLIMBED THROUGH FL 280, LEVEL AT FL 350 CBN, CLIMB AT 100 FPM. UNLATCHED COOL AIR OVRBD SWITCH. DESCENDED TO FL 240 BEFORE CABIN RATE WOULD DESCEND. FOUND SEAL DISCONNECTED BETWEEN NR 2 WATER SEPARATOR Y-DUCT AND THE AFT GROUND A/C CHECK VALVE. NR 2 SEPARATOR WAS CRACKED. REPLACED NR 2 SEPARATOR AND DUCT ASSY. RAN ENGINES AND NR 2 PACK, OPERATION AND LEAK CHECK GOOD. 2L73 4F A23WE 19950901006091995090100609NE 1995 9 1 DLL13953534 219950827A7261727706605 OIL PUMP LKHEED1011 10113851 5265010WP RROYCERB211 RB211* 54555NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11783DL 193A1009 AFTER TAKOFF, HAD SMOKE AND OIL SMELL IN CABIN, WITH SMOKE DETECTORS ACTIVATED, RETURNED ATL. FOUND NR 2 ENGINE WITH OIL IN INTAKE. REPLACED OIL PUMP IN MAIN GEAR BOX PERFORMED DUCT BURN-OUT, RETURNED TO SERVICE . 2L73 4F4 F A23WE A12EU 19950901006101995090100610NM 1995 9 1 DLM88953528 119950828A5320 STRIKER DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11910DE 53419 ONE INCH CRACK AT MLG W/W AFT O/B STRIKER. FOUND AT C-1 LTR CK. REPAIRED PER SRM 53-05, FIG 81A. 2L72 4F RTA6WE 19950901006111995090100611NM 1995 9 1 DLM88953529 119950828A5320 STRIKER ANGLE DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11910DE 53419 CRACK, .1250 INCH, ON MLG W/W AFT O/B STRIKER. FOUND AT C-1 LTR CK. REPAIRED PER SRM 53-05, FIG 81A. 2L72 4F RTA6WE 19950901006121995090100612WP 1995 9 1 SCNA95180 119950829A3350110049 EEL BATT CHARGER DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15571SC 46645 THE LEFT, AFT CABIN EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY PATH LIGHTING BATTERY CHARGER IAW MM 33-50-00 AND LIGHTS TESTED GOOD. 2L73 4F A22WE 19950901006131995090100613SW 1995 9 1 SWIA95617 119950813A2911223002 ACCUMULATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP HYD SYST FAILED A SWIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM0727278 AC732 WHEN RETRACTING THE LANDING GEAR AFTER TAKEOFF, BOTH HYD LIGHTS ILLUMINATED AND HYD PRESSURE DROPPED TO ZERO. RETURN FOR LANDING. AFTER EMERGENCY GEAR EXTENSION, FOUND THE HYD ACCUMULATOR CRACKED. REPLACED ACCUMULATOR. SERVICED SYSTEM. RAN LT AND RT ENGINES, BLED AND RESERVICED. OPS AND LEAK CK GOOD. 1L72 4T4 T A8SW E4WE 19950901006141995090100614NE 1995 9 1 SWIA95618 219950814A73213035659 FUEL CONTROL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE FAILED A ASWIAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07224SW 120294 LT ENGINE FAILURE AT 2,500 FEET WITH CLIMB POWER. RETURNED TO LAX. TORQUE FLUXUATED 65 TO 84 THEN TO 101. REPLACED HMU FUEL CONTROL, IAW MM 73-21-00, OPS CKS GOOD, NO LEAKS NOTED. 2L72 4T4 TRTA31SO E20NE 19950901006151995090100615SW 1995 9 1 SWIA95619 119950825A2720 CABLES SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RUDDER OUT OF ADJUST A SWIAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 NM072685L AC648 ON ROTATION, A/C REQUIRES EXCESSIVE RT RUDDER AND WITH RUDDERS NEUTRAL, RUDDER IS DEFLECTED. FOUND RUDDER CABLE TENSIONS LOW AND TRAVEL INCORRECT. SET CABLES TO CORRECT TENSION AND ALSO SET RUDDER TO CORRECT TRAVEL. OP CK GOOD. 1L72 4T4 T A8SW E4WE 19950901006161995090100616NE 1995 9 1 SWIA95620 219950828A7261 OIL SYST EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE REQD SERVICE A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07207SW 120266 AFTER ROTATION, RT OIL PRESSURE FLUCTUATED TO AROUND 40 PSI AND OIL AURAL WARNING SOUNDED. OIL PRESSURE IMMEDIATELY RETURNED AND MAINTAINED NORMAL PSI. SERVICED RT ENGINE OIL, 3 QTS. INSPECTED ENGINE, NO LEAKS FOUND. FILTER BYPASS PINS NOT POPPED, TRANSMITTER WIRING AND CANNON PLUG OK. PERFORMED ENGINE RUN UP, OIL PRESSURE INDICATION NORMAL. 2L72 4T4 TRTA31SO E20NE 19950901006171995090100617NM 1995 9 1 UPS204338 119950829A53207075T6 HAT CHANNEL BOEING727 72751C 1384015NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON PANEL SUPPORT AT FORWARD LAV STA 344, RBL 18, WL 208-UNDERSIDE. REMOVED AND INSTALLED NEW FABRICATED HAT CHANNEL. WORK DONE I/A/W SRM'S 53-10-1, 51-30-2. 2L73 4F A3WE 19950901006181995090100618NM 1995 9 1 UPS204339 119950829A5755 SKIN BOEING727 72751C 1384015NM NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 1 SPOILER HAS 2 AREAS OF DELAMINATION ON LOWER SURFACE AT THE INBOARD FORWARD CORNER AND ON THE OUTBOARD EDGE OF THE CENTER FITTING. REMOVED DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 57-50-1, 51-40-6. 2L73 4F A3WE 19950901006191995090100619NM 1995 9 1 UPS204340 119950831A5753 TE WEDGE BOEING727 72751C 1384015NM TE MID FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE HAS ONE DELAMINATION ON UPPER SURFACE 23 INCHES FROM INBOARD END. CUT OUT DAMAGE AREA, APPLIED FIBERGLASS, AND COMPLETED REPAIRS PER SRM 51-40-6, MM 51-20-151. 2L73 4F A3WE 19950901006201995090100620NM 1995 9 1 UPS204341 119950829A57532024T6 SKIN BOEING727 72751C 1384015NM LT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEADING EDGE INBOARD AFT FLAP, INBOARD CENTER TRACK CUT-OUT IS CRACKED. CONTAINED CRACK BY STOP DRILLING AND VERIFIED BY NDI. FABRICATED REPAIR PARTS AND INSTALLED. WORK DONE I/A/W SRM 57-50-4, 51-30-2. 2L73 4F A3WE 19950901006211995090100621NM 1995 9 1 UPS204342 119950829A57537075T73511 LOWER CHORD BOEING727 72751C 1384015NM TE MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBOARD MID-FLAP, INBOARD AFT FLAP ACTUATING CUT-OUT LOWER CHORD IS CRACKED. REMOVED AND INSTALLED NEW FABRICATED PARTS. WORK DONE I/A/W SRM 51-30-2, 51-40-4. 2L73 4F A3WE 19950901006221995090100622NM 1995 9 1 UPS204343 119950829A574466137463 FITTING BOEING727 72751C 1384015NM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 HINGE BEARING BLOCK ON LT WING, OUTBOARD AILERON TO BE WORN AND HAVE EXCESSIVE PLAY, BACK AND FORTH, SIDE TO SIDE. (NOTE UPON REMOVAL OF BEARING BLOCK FOUND FITTING CORRODED). REMOVED AND INSTALLED NEW FITTING. WORK DONE I/A/W SRM'S 51-30-2, 51-30-5. 2L73 4F A3WE 19950901006231995090100623NM 1995 9 1 UPS204344 119950829A53302024T3 SKIN BOEING727 72751C 1384015NM FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK INDICATION NOTED LT WINDSHIELD, UPPER SILL, LOWER AFT RIVET APPROX 8 O'CLOCK POSITION. CUT OUT DAMAGE AND REPAIRED PER SRM 53-30-3. 2L73 4F A3WE 19950901006241995090100624NM 1995 9 1 UPS204345 119950829A575465162261 BONDING JUMPER BOEING727 72751C 1384015NM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP OUTBOARD BONDING JUMPER UPPER ATTACH POINT IS PITTED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-50-1, CUT OUT DAMAGE AND REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19950901006251995090100625NM 1995 9 1 UPS204346 119950829A53137075T6 STRINGER BOEING727 72751C 1384015NM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 20 PERCENT MATERIAL LOSS AT BS 360, 3 INCHES TO THE RIGHT ON STR 1 MARKED BY NDI. REPAIRED PER E.O. B727-5310-1371E, SRM'S 51-10-2, 51-30-8, 51-20-4, AND 51-30-2. 2L73 4F A3WE 19950901006261995090100626NM 1995 9 1 UPS204350 119950831A575465217506A BULLNOSE BOEING727 72751C 1384015NM NR 5 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01905UP 18946 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP BULLNOSE CRACKED AT OUTBOARD LUG ATTACH POINT, INBOARD FASTENERS HOLES. REMOVED CRACKED BULLNOSE AND INSTALLED NEW BULLNOSE PER SRM 51-30-2, 51-30-8, M.M. 27-81-00. 2L73 4F A3WE 19950901006271995090100627NM 1995 9 1 UPS404351 119950831A5313 STRINGER BOEING747 747123 1384873NM BS 982 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND END OF STR 47R ON BSTA 902 IS CORRODED, CORROSION IS OUT OF LIMITS, ACC. SRM 53-10-01, FIG. 1, NOTE-B. REPAIRED STRINGER FROM 970 TO BSTA 984 ACC. SRM. 53-10-03, FIG. I, DETAIL I, MATERIAL EXISTING STRINGER IS 0.90 INCH 7075T6. 2L74 4F A20WE 19950901006281995090100628NM 1995 9 1 UPS404352 119950831A5414 SKIN BOEING747 747123 1384873NM NR 4 PYLON DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PYLON NR 4 NAC: STA 225, SKIN DAMAGED BY WEAR ON TOP OF PYLON, OUTBOARD SIDE. SKIN REPAIRED ACC: S.R.M. 54-30-03 FIG 17A. 2L74 4F A20WE 19950901006291995090100629WP 1995 9 1 UPS804336 119950829A57305769589 SKIN DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 1 PYLON CUT OUT AT WING LEADING EDGE HAS A 4 INCH CRACK. REPAIRED PER SRM 57-2-1A, FIG. 1, AND UPS E.O. DC8-57-371. 2L74 4F RT4A25 19950901006301995090100630WP 1995 9 1 UPS804337 119950829A52305645357 FRAME DOUG DC8 DC871F 302199DWP NR 2 CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01709UP 45914 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 BELLY DOOR HAS A 5.75 INCH LONG CRACK AT LOWER FRAME. REPAIRED FRAME PER U.P.S. E.O. DC8-5230-7357-A. 2L74 4F RT4A25 19950901006311995090100631WP 1995 9 1 UPS804347 119950831A33505708454503 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE ON GROUND WHILE DOING A PRE-DEPARTURE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. ATA 25-60-00. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK - OPS CK'D SYSTEM SATISFACTORY. 2L74 4F RT4A25 19950901006321995090100632WP 1995 9 1 UPS804348 119950829A3260 CONNECTOR DOUG DC8 DC871F 302199DWP GEAR DOOR DIRTY A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01808UP 46008 PILOT REPORTED DOORS NOT LATCHED LIGHT ON AFTER TAKEOFF. RECYCLE GEAR AND OK. PERFORMED PULL TEST OF DOORS, OPS CK GOOD. CLEARED CANNON PLUGS ON DOOR SWITCHES. 2L74 4F RT4A25 19950901006331995090100633WP 1995 9 1 UPS804349 119950816A3260 IND LIGHT DOUG DC8 DC873F 302199FWP RT MLG MALFUNCTIONED A IPXAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO01810UP 46008 PILOT REPORTED RIGHT LANDING GEAR DID NOT INDICATE SAFE WHEN HANDLE LOWERED. COMMENT NOTED BY MX. 2L74 4F RT4A25 19950908000011995090800001WP 1995 9 8 9513309607 119950823A5312 BULKHEAD DOUG DC9 DC932 3022066WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK, FOUND HORIZONTAL STIFFENER TO FRAME CRACKED AT FS 996 AFT PRESSURE BULKHEAD. FABRICATED AND INSTALLED REPAIR ANGLE PER EA 96-098097. 2L72 4F A6WE 19950908000021995090800002WP 1995 9 8 9513319163 119950823A5330 SKIN DOUG DC9 DC914 3022034WP FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND FUSELAGE SKIN AT AFT SIDE OF FORWARD ENTRY DOOR CRACKED AT THIRD AND FOURTH DOOR STOPS. ACCOMPLISHED TEMPORARY REPAIR PER EA 91-102773. 2L72 4F A6WE 19950908000031995090800003WP 1995 9 8 9513329163 119950824A5315 FLOORBEAM DOUG DC9 DC914 3022034WP FS 817 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND FLOORBEAM AT LEFT LAVATORY CORRODED AT FS 817. REPAIRED PER EA 91-102775. 2L72 4F A6WE 19950908000041995090800004WP 1995 9 8 9513339163 119950824A5312 BULKHEAD DOUG DC9 DC914 3022034WP FS 642 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND AFT PIT FORWARD BULKHEAD LOWER CHORD CORRODED IN SEVERAL AREAS AT FS 642 BETWEEN LONGERONS 28L AND 28R. SPLICED IN NEW SECTION OF T-CHORD PER EA 91-097635. 2L72 4F A6WE 19950908000051995090800005WP 1995 9 8 9513349163 119950824A5330 SKIN DOUG DC9 DC914 3022034WP FS 585-642 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018906E 45747 DURING H-CHECK, FOUND FUSELAGE SKIN CRACKED AT FS 585, 623 AND 642 BETWEEN LONGERONS 1R AND 2R AT FASTENERS IN FRAME CLIP. FABRICATED AND INSTALLED DOUBLER PER EA 91-097634. 2L72 4F A6WE 19950908000061995090800006EU 1995 9 8 9513353226 119950830A2421740119E GENERATOR AIRBUS320 A320211 3930320EU NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01326US1195411954 282 DURING TAKEOFF ROLL, RECEIVED ELEC IDG 2 OIL LOW PRESSURE MESSAGE. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 40 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 IDG, LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950908000071995090800007EU 1995 9 8 9513363250 119950827A29234205602 HYD PUMP AIRBUS320 A320211 3930320EU LT MLG WW FAILED A NWAAO OTHER J WARNING INDICATION DEDESCENT 1 GL01350NA9120 9120 418 DURING DESCENT INTO DTW, RECEIVED HYD B-SYS LOW PRESSURE INDICATION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP, CASE DRAIN, AND PRESSURE FILTERS. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950908000081995090800008NM 1995 9 8 9513372712 119950831A3260 INDICATION BOEING727 7272S7 138407ZNM NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01712RC 22020 DURING CLIMB AFTER GEAR RETRACTION, NOSE LANDING GEAR DOOR INDICATIONS REMAINED ILLUMINATED WITH GEAR HANDLE IN UP POSITION. WHEN GEAR HANDLE IN OFF POSITION, TAILSKID INDICATION ILLUMINATED AS WELL. RECYCLED LANDING GEAR TO NO AVAIL AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED NOSE LANDING GEAR AND TAILSKID INDICATION. 2L73 4F A3WE 19950908000091995090800009NM 1995 9 8 9513382712 119950831A3260MS250111 INDICATION SW BOEING727 7272S7 138407ZNM NLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01712RC 22020 DURING CLIMB AFTER LANDING GEAR RETRACTION, NOSE LANDING GEAR DOOR INDICATIONS REMAINED ILLUMINATED. ASSOCIATED WIND NOISE WITH INDICATION AND RECYCLED LANDING GEAR TO NO AVAIL. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NOSE LANDING GEAR DOORS AND INDICATION WIRING, NO TROUBLE FOUND. REPLACED BOTH NOSE LANDING GEAR DOOR INDICATION SWITCHES, OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950908000101995090800010NM 1995 9 8 95FDEA01231 119950831A5315 FLOORBEAM BOEING727 727233 138408ANM BS 380 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 BS 380 RBL 26 TO 32, MAIN CARGO FLOORBEAM UPPER FLANGE IS CRACKED AND CORRODED. REMOVED CRACKED AND CORRODED SECTION OF UPPER FLANGE OF BS 380 RBL 16.75 AND 35.25 RBL, FLOORBEAM. FABRICATED DOUBLER PER SRM 53-10-8 PG 2A. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8 PG 2A. 2L73 4F RTA3WE 19950908000111995090800011WP 1995 9 8 ABXA9500682 119950829A326056487405503 ROLLER DOUG DC8 DC863 302198AWP LT MLG DOOR OUT OF ADJUST A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23818AX 46075 WHILE PERFORMING A MISSED APPROACH, THE LEFT MLG DOOR INDICATED UNLOCKED. RECYCLED GEAR AND INDICATION WAS STILL UNLOCKED, DEFERRED IAW DC 8 MEL 32-14. FOUND LEFT MLG DOOR UPLATCH ROLLER TO BE OUT OF ADJUSTMENT. ADJUSTED AND TESTED DOOR IAW DC 8 MM CHAPTER 32. INDICATION OPS CHECKED GOOD. 2L74 4F 4A25 19950908000121995090800012WP 1995 9 8 ABXA9500683 119950831A25102657621 SPRING DOUG DC8 DC863 302198AWP CAPT SEAT BROKEN A ABXAO OTHER O OTHER CRCRUISE 1 GL23811AX 46113 CAPTAIN'S SEAT WOULD NOT STAY LOCKED IN POSITION, KEPT SLIDING BACK. FOUND SPRING TO LOCKPIN BROKEN. REPLACED SPRING IAW DC 8 MM CHAPTER 25, SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950908000131995090800013WP 1995 9 8 MWEA95272 119950829A531259101639XX BLKHD SKIN DOUG DC9 DC915 3022036WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 TWO CRACKS IN AFT PRESSURE BULKHEAD SKIN AT RECEPTACLE HOLE, APPROXIMATLY 1 O'CLOCK POSITION .25 INCH AND .75 INCH LONG. STOP DRILLED CRACK AND INSTALLED REPAIR TO THE TWO CRACKS IAW SVC RWK 5934886-509. 2L72 4F A6WE 19950908000141995090800014WP 1995 9 8 MWEA95273 119950829A531259101639N BLKHD SKIN DOUG DC9 DC915 3022036WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 CRACK IN AFT PRESSURE BULKHEAD SKIN AT 6 O'CLOCK POSITION BELOW PLUG DOOR JAMB 1.083 LONG. REMOVED EXITING REPAIR, VERIFIED LENGTH OF CRACK AND INSTALLED REPAIR IAW 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950908000151995090800015WP 1995 9 8 MWEA95274 119950829A533059114111 SKIN DOUG DC9 DC915 3022036WP FS 256 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT SIDE OF FUSELAGE, STATION 256 AT LONGERON SKIN 25 IS SHARPLY DENTED 1.5 INCH LONG. INSTALLED REPAIR IAW SRM 53-04 FIG 38 SHEET 21. 2L72 4F A6WE 19950908000161995090800016WP 1995 9 8 MWEA95275 119950829A533059114061 SKIN DOUG DC9 DC915 3022036WP FS 164 CRACK A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 CRACK IN FUSELAGE SKIN APPROX 1.5 INCH LONG, AT PASSENGER DOOR UPPER FORWARD CORNER AT STATION 164. CUT OUT DAMAGE, FABRICATED AND INSTALLED PLUG, DOUBLER AND TRIPLER PER SRM 53-05 FIG 26. 2L72 4F A6WE 19950908000171995090800017WP 1995 9 8 MWEA95276 119950829A533059114092 SKIN DOUG DC9 DC915 3022036WP FS 280 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 FUSELAGE SKIN DAMAGED ON RIGHT SIDE OF FUSELAGE NEAR AOA VANE AT STATION 280. REMOVED DAMAGED SKIN AND SPLICED IN NEW SKIN ON RIGHT SIDE, PER XYX DRAWING 53-147 AND TELEX SVC-ORD-0151/PDG. 2L72 4F A6WE 19950908000181995090800018WP 1995 9 8 MWEA95277 119950829A53472914913 SEAT TRACK DOUG DC9 DC915 3022036WP FS 200 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT OUTBOARD SEAT TRACK MODERATELY CORRODED AT STATION 200. REPAIRED IAW SRM 53-05 FIG 4, AT FACTORY SPLICE. 2L72 4F A6WE 19950908000191995090800019WP 1995 9 8 MWEA95278 119950829A53472772660 SEAT TRACK DOUG DC9 DC915 3022036WP FS 200 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 RIGHT INBOARD SEAT TRACK MODERATELY CORRODED AT STATION 200. REPAIRED IAW SRM 53-05 FIG 4, AT FACTORY SPLICE. 2L72 4F A6WE 19950908000201995090800020WP 1995 9 8 MWEA95279 119950829A531199115153 FRAME DOUG DC9 DC915 3022036WP FS 160 MISDRILLED A MWEAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL31300ME 45718 FUSELAGE FRAME AT STATION 160 HAS A .75 INCH HOLE IN UPPER RADIUS, 3 INCHES OUTBOARD OF LONGERON 4R. INSTALLED REPAIR IAW DOUGLAS TELEX JSS DTD, 16 AUG 95 AND PDG DTD 17 AUG 95. 2L72 4F A6WE 19950908000211995090800021WP 1995 9 8 MWEA95280 119950829A5210591412159N PAN DOUG DC9 DC915 3022036WP PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 PASSENGER DOOR PAN IS CRACKED APPROXIMATELY .6250 INCH ON AFT PORTION OF BEAM NR 8. REPAIRED CRACK IAW SRM 52-05 FIG 18A. 2L72 4F A6WE 19950908000221995090800022NM 1995 9 8 SWAA950605 119950819A5320 ANGLE BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SCHEDULED 1/4 D-CHECK, FOUND CHORD CRACKED IN AFT EDGE AT I/B FASTENER OF 18A CHORD ANGLE, LEFT MAIN WHEEL WELL, BS 727 S18A. INSTALLED CHORD ANGLE REPAIR PER DRAWING 65-29228. 2L72 4F A16WE 19950908000231995090800023NM 1995 9 8 SWAA950606 119950819A5320 NLG PANEL BOEING737 7372H4 138448CNM BS 277 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SCHEDULED 1/4 D-CHECK, FOUND NOSE WHEEL WELL CEILING CRACKED AT SPRING ATTACH POINT, BS 277 RBL 10. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950908000241995090800024NM 1995 9 8 SWAA950607 119950819A5312 BLKHD T-CHORD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SCHEDULED 1/4 D-CHECK, FOUND TWO CRACKS AT T-CHORD BS 178 BULKHEAD AFT SIDE, WL 184, ONE I/B AND ONE O/B. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950908000251995090800025NM 1995 9 8 SWAA950608 119950819A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, RBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950908000261995090800026NM 1995 9 8 SWAA950609 119950819A5312 BLKHD STRAP BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0751SW 21448 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB AND STRAP CRACKS AT BS 178 BULKHEAD, INBOARD ROW OF FASTENERS, LBL 5.7 FROM WL 184 TO 201. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950908000271995090800027NM 1995 9 8 SWAA950610 119950830A274091238071 RELAY BOEING737 7373H4 1384600NM STABILIZER FAILED A SWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07601WN 27695 MAIN STABILIZER TRIM WAS INOPERATIVE, OVERRIDE USED TO OPERATE SYSTEM. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED MAIN STABILIZER TRIM RELAY PER BOEING M/M. 2L72 4F RTA16WE 19950908000281995090800028NM 1995 9 8 SWAA950611 119950830A3350 EEL BOEING737 7375H4 138449DNM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07507SW 24184 FOUND 2 EMERGENCY FLOOR TRACK LIGHTS INOP. RELAMPED AND RECONNECTED LIGHTS PER BOEING M/M. 2L72 4F RTA16WE 19950908000291995090800029NM 1995 9 8 SWAA950612 119950830A3350 EEL BATTERY BOEING737 7375H4 138449DNM AFT GALLEY DISCHARGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07508SW 24185 AFT GALLEY EMERGENCY LIGHT REMAINS ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED LIGHT BATTERY PACK PER BOEING M/M. 2L72 4F RTA16WE 19950908000321995090800032SW 1995 9 8 95ZZZX4401 119950721A6230206010335001 LEVER ASSY 206010350021BELL 206 206B3 1181506SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW03116AL 791 2389 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001 SPACERS, 4 EACH, 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH, NAS 6605D64 BOLTS, 1 EACH, 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 790.7. 1G71 3U H2SW 19950908000331995090800033SW 1995 9 8 95ZZZX4402 119950721A6230206010336005 LINK IDLER 206010350021BELL 206 206B3 1181506SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW03116AL 791 2389 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001 SPACERS, 4 EACH, 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH, NAS 6605D64 BOLTS, 1 EACH, 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 790.7. 1G71 3U H2SW 19950908000401995090800040SW 1995 9 8 95ZZZX4409 119950721A6230206010335001 LEVER ASSY 206010350021BELL 206 206B 1181511SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032299U 596 3415 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001 SPACERS, 4 EACH, 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH, NAS 6605D64 BOLTS, 1 EACH, 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 596.1 1G71 3U H2SW 19950908000411995090800041SW 1995 9 8 95ZZZX4410 119950721A6230206010336005 LINK IDLER 206010350021BELL 206 206B 1181511SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032299U 596 3415 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001 SPACERS, 4 EACH, 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH, NAS 6605D64 BOLTS, 1 EACH, 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 596.1 1G71 3U H2SW 19950908000451995090800045SW 1995 9 8 95ZZZX4414 119950801A2612209075395001 FIRE DET UNIT BELL 214 214ST 1182106SW NR 2 ELECT BAY FAULTY A ALGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW03391AL6775 12131 28103 WHILE IN LEVEL FLIGHT, NR 2 ENGINE FIRE LIGHT ILLUMINATED. PERFORMED CLEARING TURN TO CHECK FOR SMOKE. NO SMOKE WAS NOTED. FOLLOWED EMERGENCY CHECKLIST AND RETURNED TO BASE. TROUBLESHOT SYSTEM. FOUND FIRE CONTROL UNIT UNSERVICEABLE. REPLACED FIRE CONTROL UNIT. 2G72 4U H10SW 19950908000531995090800053EU 1995 9 8 95ZZZX4422 119950627A33506035501 EEL BATT PACK BAG BAE146BAE146200A 1500266EU CABIN DISCHARGED A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31293UE 1363 E2097 DEN - FLT 353 - FLOOR TRACK LIGHTING FROM ROW 2 TO ROW 8 IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM. OPS CHECK GOOD. S/N OFF 1363. S/N ON 36. 2H74 4F RTA49EU 19950908000541995090800054EU 1995 9 8 95ZZZX4423 119950528A2750676801007 COMPUTER BAG BAE146BAE146200A 1500266EU TE FLAPS FAILED A A6WAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 GL31293UE DRG121687 E2097 ATW - FLT 307 - FLAP INOP AND FLAP FAULT LIGHTS ILLUMINATED ON APPROACH TO ATW WITH FLAPS STUCK AT 24 DEGREES, WHEN FLAPS 33 SELECTED. REMOVED AND REPLACED FLAP COMPUTER. 2H74 4F RTA49EU 19950908000551995090800055CE 1995 9 8 95ZZZX4424 119950712A78101299500001 EXHAUST STACK BEECH 1900 1900D 1154162CE LT ENGINE CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW01131YV958 UE131 LEFT ENGINE OUTBOARD EXHAUST STACK CRACKED ABOUT 1.50 INCHES LONG AT BLAST TUBE EXHAUST PORT. CRACK AT WELD BEAD PROGRESSING CIRCUMFERENTIALLY AROUND TUBE. REMOVED AND REPLACED EXHAUST STACK. 2L72 4T RTA24CE 19950908000561995090800056CE 1995 9 8 95ZZZX4425 119950712A323311438004111 ACTUATOR BEECH 1900 1900D 1154162CE RT MLG FAILED A MASAK NONE K FLUID LOSS ININSP/MAINT 1 SW01131YV958 0235A UE131 HYDRAULIC MAIN GEAR ACTUATOR ON RIGHT MAIN GEAR LEAKING FLUID FROM THREADED PISTON HOUSING NEAR FORWARD BOSS. REMOVED AND REPLACED MAIN GEAR ACTUATOR WITH NEW SERVICEABLE ACTUATOR PER BEECH MM, OPERATIONAL AND LEAK CHECK GOOD. 2L72 4T RTA24CE 19950908000571995090800057NM 1995 9 8 95ZZZX4426 119950619A3350 EEL WIRE BRUCE BR20137372GFBOEING737 737247 138448DNM CABIN BROKEN A A6XAK NONE L NO TEST ININSP/MAINT 1 SO134510W 19607 DURING AN INSPECTION, FOUND 2 BULBS OUT IN 4-BULB RED LIGHT GROUP OF THE TRACKING LIGHTING, PN BR9279110, AT ROW 22. FOUND BROKEN WIRE IN SOCKET. SPLICED AS REQUIRED PER MM 3350 AND OPS CHECKED. 2L72 4F A16WE 19950908000581995090800058EU 1995 9 8 AALA951378 119950804A2910AS1005D101006 UNION TEE FOKKERF28 F28MK0100 4990807EU NR 1 HYD SYS BROKEN A AAALAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW071435D 11425 DFW - FLT 1598 - EN ROUTE CRP/DFW DURING CRUISE, HYDRAULIC SYSTEM LOW QUANTITY MESSAGE ON MFDU. AIRCRAFT PROCEEDED TO DFW, ACCOMPLISHED ALTERNATE LANDING GEAR AND FLAP PROCEDURES AND LANDED DFW WITHOUT INCIDENT. REPLACED BROKEN FITTING UNDER CABIN FLOOR FOR HYDRAULIC SYSTEM 1. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19950908000591995090800059EU 1995 9 8 AWXA9500464 119950725A3230 LGCIU AIRBUS320 A320232 3930326EU NR 1/2 FAILED A AWXAO OTHER J WARNING INDICATION DEDESCENT 1 WP28639AW 471 PHX/CMH - FLT 825 - ON DESCENT, CREW EXPERIENCED CLASS 1 FAULT FOR NR 2 LANDING GEAR CONTROL INTERFACE UNIT (LGCIU). A/C LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED THE NR 1 AND NR 2 LGCIU'S PER AMM 32 31 91 AND AMM 32 69 00. BYTE TEST OK. A/C RETURNED TO SERVICE. (X) 2L72 4F RTA28NM 19950908000601995090800060NM 1995 9 8 CAL950529 119950628A2910 PLATE GASKET BOEING757 757224 1384958NM LT HYD SYST LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0918112 27302 IAH - FLT 0193 - THE LEFT ENGINE DRIVEN PUMP AND ELECTRIC PUMP LOST PRESSURE WHILE ON APPROACH TO IAH. THE PRESSURE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE LT HYDRAULIC SYSTEM PRESSURE LIGHT, THE RUDDER RATIO LIGHT, AND THE HYDRAULIC QUANTITY LIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RRCA SOLENOID VALVE LEAKING AT THE PLATE GASKET. THE PLATE GASKET WAS REMOVED AND REPLACED AND LEAK CHECKS WERE GOOD. (X) 2L72 4F RTA2NM 19950908000611995090800061NM 1995 9 8 CAL950593 119950713A3241423071 ANTI-SKID CONTL BOEING727 727225 1384077NM LANDING GEAR INOPERATIVE A CALAO OTHER O OTHER LDLANDING 1 SW098886Z1753 21855 EWR - FLT 0223 - WHEN FIRST APPLYING THE BRAKES ON LANDING AT EWR, THERE WAS LITTLE BRAKING AVAILABLE. ALL GAUGE PRESSURES WERE NORMAL. MAXIMUM APPLICATION OF BRAKES WAS REQUIRED TO BRING THE AIRCRAFT TO A STOP. ALL FOUR ANTI-SKID TRANSDUCERS CHECKED GOOD. AN ANTI-SKID TEST WAS PERFORMED PER MM 32-42-01, PAGE 501, AND ALL CIRCUIT FUNCTION CHECKS FAILED. THE ANTI-SKID CONTROL BOX WAS REMOVED AND REPLACED. A BITE TEST AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19950908000621995090800062WP 1995 9 8 CAL950596 119950715A2420947F9452 GEN CONTL PNL DOUG DC9 DC982 3022082WP RT SYSTEM INOPERATIVE A CALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW09168083841632094 49262 GSO - FLT 0402 - THE RIGHT CSD OIL TEMP WENT OFF SCALE HIGH AFTER TAKEOFF FROM MCO. THE CSD WAS DISCONNECTED AND THE APU WAS STARTED TO POWER THE RIGHT AC BUS. THE APU GENERATOR FREQUENCY STARTED FLUCTUATING FULL SCALE DEFLECTION BOTH WAYS. THE APU GENERATOR WAS SHUT DOWN WHILE CLIMBING THROUGH 27,000 FEET. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. THE APU GENERATOR CONTROL PANEL WAS REPLACED AND OPERATION CHECKED GOOD. IN ADDITION, THE RIGHT CSD, GENERATOR, AND CSD OIL COOLER WERE REPLACED DUE TO THE CSD FAILURE. (X) 2L72 4F A6WE 19950908000631995090800063CE 1995 9 8 S2YA950002 119950503A521012951410517 CTR BAL ARM BEECH 1900 1900D 1154162CE AIRSTAIR DOOR CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL1391SK 595 UE91 THE CENTERBALANCE ARM WAS FOUND BENT. HAVE REPLACED 14 OF THE DASH 17 TYPES AND, SO FAR, 2 OF THE DASH 33 NEW DESIGNS BETWEEN 13 AIRCRAFT. 2L72 4T RTA24CE 19950908000641995090800064CE 1995 9 8 S2YA950005 119950515A571211412003327 RIB BEECH 1900 1900D 1154162CE WS 83.00 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL1391SK 2340 UE91 DURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 83.00 TO HAVE CRACKED ON THE BOTTOM PORTION BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS. THE CRACKS WERE APPROXIMATELY 3 INCHES AND 1 INCH LONG EXTENDING FROM THE CENTER OF THE RIB REINFORCEMENT, P/N 114-120033-15, WHICH WAS ALSO CRACKED TOP AND BOTTOM. A REPAIR WAS MADE. (X) 2L72 4T RTA24CE 19950908000651995090800065CE 1995 9 8 S2YA950006 119950515A57121141200323 RIB BEECH 1900 1900D 1154162CE WS 69.00 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL1391SK 2340 UE91 DURING AN INSPECTION, MAINTENANCE FOUND THE LT WING CENTER MID-RIB AT WS 69.00 TO HAVE A CRACK 1.5 INCHES LONG ON THE TOP PORTION NEXT TO THE LOWER MOUNT HOLE OF THE MANUAL HYDRAULIC RESERVOIR BLEED VALVE, PN 114-388012-1. A REPAIR WAS MADE PER THE BEECH SRM. (X) 2L72 4T RTA24CE 19950908000661995090800066 1995 9 8 S2YA950007 419950518A3442 CONNECTOR BEECH 1900 1900D 1154162CE CENTER PEDESTAL LOOSE A S2YAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL13145SK188 UE145 THE CREW REPORTED THEIR RADAR FAULTED SEVERAL TIMES DURING AN ATTEMPTED FERRY FLIGHT AND THEN FAILED. THEY THEN TURNED BACK TO THEIR ORIGINATION BECAUSE OF WEATHER CONDITIONS. MAINTENANCE RESEATED THE CANNON PLUGS AT THE COLLINS WX RADAR CONTROL PANEL, PN 622839K013. OPS CHECK GOOD. (X) 2L72 4T RTA24CE 19950908000671995090800067CE 1995 9 8 S2YA950008 119950519A535011441009527 RADOME BEECH 1900 1900D 1154162CE FS 30.00 LEAKS A S2YAK NONE O OTHER ININSP/MAINT 1 GL13148SK11 UE148 THE RADOME TO FUSELAGE MOUNT AREA AT FS 30.00 HAD TO BE SEALED TO PREVENT PREMATURE RADAR FAILURES DUE TO MOISTURE. AS THE RADAR TRANSIT/RECEIVER IS HIGHLY SUSCEPTIBLE TO ANY WATER. WE HAVE HAD MULTIPLE FAILURES DUE TO THIS PROBLEM. THE REST OF FLEET WAS SEALED AND CHECKED PERIODICALLY FOR LEAKS. A FLEXIBLE BUTYL SEALANT WAS USED. (X) 2L72 4T RTA24CE 19950908000681995090800068CE 1995 9 8 S2YA950009 119950519A32221148200261 AXLE 114820021601BEECH 1900 1900D 1154162CE NLG INCORRECT DIA A AS2YAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL13148SK11 408A95 UE148 DISCOVERED BOTH INNER AND OUTER WHEEL BEARINGS, PN 13899, WERE FROZEN IN PLACE ON NLG STRUT ASSY AXLE SHAFT, PN 114-820026-1, WHILE TRYING TO REMOVE THE NOSE WHEEL AND TIRE ASSY. ATTEMPTED DRY ICE AND HEATING OF THE BEARING RACE TO FACILITATE REMOVAL, TO NO AVAIL. REMOVED THE WHEEL BY MACHINING A NOTCH IN THE OUTER BEARING RACE AND REMOVING THE ROLLERS THEN HAD TO CUT OFF BOTH THE INNER BEARING RACES FROM THE AXLE. (X) 2L72 4T RTA24CE 19950908000691995090800069CE 1995 9 8 S2YA950010 119950520A215011412005267 ACM INLET DUCT BEECH 1900 1900D 1154162CE LT WING IMPROPER INSTL A S2YAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL13148SK11 UE148 FOUND THE AIR CYCLE MACHINE INLET DUCT INSTALLED BACKWARDS ON THE BOTTOM OF THE LT WING PANEL WELD ASSEMBLY. REMOVED AND REINSTALLED THE LOUVER IN THE PROPER POSITION. THIS HAD ALSO OCCURRED ON AIRCRAFT S/N UE-145, BOTH FROM THE FACTORY. (X) 2L72 4T RTA24CE 19950908000701995090800070CE 1995 9 8 S2YA950013 119950622A3010131823E10D1300 DEICE SUPP LINE BEECH 1900 1900D 1154162CE VERT STABILIZER CHAFED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13148SK237 UE148 FOUND THE TAIL DEICE SUPPLY LINE CHAFED AT THE POINT OF EXIT FROM THE CLEAR PLASTIC ROUTING 'PROTECTION' TUBE. THE LOCATION IS THE BASE OF THE VERTICAL STABILIZER, LOWER ZONE 331. THE LINE WAS REPAIRED AND REST OF THE FLEET IS BEING CHECKED. (X) 2L72 4T RTA24CE 19950908000711995090800071CE 1995 9 8 S2YA950015 119950707A24371013842331 VOLT/AMMETER BEECH 1900 1900D 1154162CE OVERHEAD PANEL STICKING A S2YAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1387SK 3110 UE87 MKE - FLT 1091.1 - AFTER FLIGHT CREW TOOK OFF, THEY NOTICED THE D.C. AMMETER STAYED AT ABOUT 60 AMPS. THEY DECIDED TO TURN BACK TO MKE TO HAVE MAINTENANCE CHECK IT. MAINTENANCE DETERMINED IT WAS A STICKING GAUGE MOVEMENT. VOLT/AMMETER WAS REPLACED. (X) 2L72 4T RTA24CE 19950908000721995090800072EU 1995 9 8 SIMA952061 119950725A33507239410803 EXIT SIGN SAAB SF340 340B 7860101EU CABIN BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21592MA 340B199 DFW - FLT 3753 - EMERGENCY EXIT SIGN OVER SEAT 8A IS INOPERATIVE. REMOVED AND REPLACED EXIT SIGN OVER SEAT 8A DUE TO BROKEN WIRE GOING INTO ASSEMBLY. (X) 2L72 4T RTA52EU 19950908000731995090800073NM 1995 9 8 TAOA079504 119950730A2612 FIRE WARNING BOEING727 727254 138408LNM WHEELWELL ACTIVATED A TAOAO OTHER J WARNING INDICATION CLCLIMB 1 EA15916TS 20437 FLT 6602 - AT 5,000 FEET, 250 KNOTS, WHEELWELL WARNING LIGHTS CAME ON WITH FIRE BELL. LIGHT WENT OUT WHEN GEAR DOORS OPENED. INSPECTION OF WHEELWELL AREA REVEALED NO EVIDENCE OF FIRE. SUSPECT HOT BRAKES IN THE WHEELWELL AREA ACTIVATED THE FIRE WARNING SYSTEM. FIRE WARNING SYSTEM AND LOOPS IN THE WHEELWELL AREA WERE INSPECTED AND TESTED IAW 26-80-00. SYSTEM TESTED NORMAL. (X) 2L73 4F A3WE 19950908000741995090800074NM 1995 9 8 USAA950760 119950714A2410 TEMP BULB BOEING737 737301 1384611NM NR 1 ENG CSD FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19589US 23934 OKC - FLT 1409 - THE NR 1 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED. THE CSD WAS DISCONNECTED AND FLIGHT DIVERTED TO OKC. MAINTENANCE REPLACED THE TEMPERATURE BULB. OPERATIONS CHECKED GOOD. (X) 2L72 4F RTA16WE 19950908000751995090800075EU 1995 9 8 USAA950778 219950728A7200 ENGINE BOEING737 7373B7 1384580NM CFMINTCFM56 CFM563B2 13802EU NR 2 FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19374US22281 22953 720931 DEN - FLT 0021 - BOTH ENGINES OVER TEMP ON TAKEOFF. FLIGHT RETURNED TO DENVER. MAINTENANCE INSPECTED ENGINES. FERRIED AIRCRAFT TO PIT. REPLACED NR 2 ENGINE ASSEMBLY, INSPECTED NR 1 ENGINE FOR AREA B EXCURSION. FOUND THE REASON TO BE PERFORMANCE DETERIORATION. OK FOR SERVICE. (M) 2L72 4F4 FRTA16WE E21EU 19950908000761995090800076NM 1995 9 8 USAA950785 119950705A5320 BRACKET BOEING737 737301 1384611NM BS 792 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU27298 23512 INT - DURNG 'Q-1' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION ON BRACKET AT BS 792, S-23L AND S-24L. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. BURNISHED TOP BRACKET AND REPLACED BOTTOM BRACKET, REPAIRED PER SRM 51-10-2. (X) 2L72 4F RTA16WE 19950908000771995090800077NM 1995 9 8 USAA950786 119950706A5320 ANGLE BOEING737 737301 1384611NM BS 787-847 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU27298 23512 INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND .75 INCH BY 1 INCH SEVERAL PLACES CORRODED BS 787 TO BS 847 ON FLOOR ANGLE. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. REPLACED ANGLE, REPAIRED PER SRM 51-10-02. (X) 2L72 4F RTA16WE 19950908000781995090800078NM 1995 9 8 USAA950787 119950706A5320 ANGLE BOEING737 737301 1384611NM BS 947.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19558AU27298 23512 INT - DURING 'Q-1' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 3 FOOT CORROSION ON ANGLE AT BS 947.5. CORROSION TASK NR: C53-208-01. CORROSION LEVEL: 2. FABRICATED NEW ANGLE REF DRAWING NR 65-49616, REPAIRED PER BOEING DRAWING 65-49616. (X) 2L72 4F RTA16WE 19950908000791995090800079EU 1995 9 8 VTZA95227 119950720A2750TY175802A SELECTOR JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27323UE 41059 IAD/PVD - FLT 6215 - DURING TAKEOFF AT 1220 HRS ON 7-20-95, ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SOUNDING ON THE TAKEOFF ROLL AT 80 KNOTS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FLAP SELECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950908000801995090800080EU 1995 9 8 VTZA95228 119950720A324091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PARKING BRAKE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27323UE 41059 IAD/DAY - FLT 6290 - DURING TAKEOFF AT 1800 HRS ON 7-20-95, ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SOUNDING ON THE TAKEOFF ROLL AT 70 KNOTS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE PARKING BRAKE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950908000811995090800081EU 1995 9 8 VTZA95229 119950720A2751TY176004A TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU TE FLAPS OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27323UE 41059 IAD/DAY - FLT 6290 - DURING TAKEOFF AT 1900 HRS ON 7-20-95, ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SOUNDING ON THE TAKEOFF ROLL AT 70 KNOTS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED ALL OF THE FLAP POSITION TRANSDUCERS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950908000821995090800082WP 1995 9 8 9513399908 119950830A3260 DOOR SWITCH DOUG DC9 DC931 3022065WP RT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01958N 47254 DURING APPROACH INTO PIT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EMERGENCY GEAR EXTENSION PROCEDURES WERE ACCOMPLISHED AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOOR SWITCH AND ADJUSTED LEFT DOOR SWITCH. REPLACED MAIN GEAR DOOR SKID PLATES DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908000831995090800083 1995 9 8 9513409951 419950827A34542587567 RMI COMPASS DOUG DC9 DC932 3022066WP INST PANEL MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL019347 464087804 45827 LOSS OF NR 2 COMPASS INDICATOR OCCURRED DURING INITIAL SPOOL UP ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 2 RMI. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908000841995090800084NE 1995 9 8 9513416717 219950830A7200 ENGINE BOEING747 747251F 1384898NM PWA JT9 JT9D7F 52054NE NR 4 FAILED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01617US 21121 89472 EN ROUTE IAH-LAX, THE NR 4 ENGINE WAS SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT, RISING OIL TEMPERATURE AND DECREASING OIL QUANTITY. CREW FOLLOWED COCKPIT OPERATING MANUAL AND RETURNED FLIGHT TO IAH WITHOUT FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 4 ENGINE AND TEST WAS NORMAL. 2L74 4F4 F A20WE E20EA 19950908000851995090800085 1995 9 8 95FDEA01232 219950901A7250 PWA JT8D174 BOEING727 727233 138408ANM NR 2 ENGINE FAILED A FDEACDEFABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN ACTIVATE FIRE EXT. TYAENGINE CASE PENETRATION ENGINE STOPPAGE FLAME/FIRE TOTAKEOFF 1 SO25285FE 22622 ABORTED T/O DUE TO SEVERE VIBRATION FROM NR 2 ENG, LOUD BANG FOLLOWED BY ENG FAIL LIGHT AND NR 2 LOW OIL PRESSURE BYPASS LIGHT. NR 2 FIRE HANDLE PULLED AND BOTH FIRE BOTTLES USED. ALSO, LOSS OF OIL PRESSURE, PER CONVERSATION WITH CREW AT SITE. DISCONNECTED ENG NR 2 PER WORK CARD 70T0002 STEPS 1 A 1X, REMOVED NR 2 ENG PER WORK CARD 70T0002. REMOVED AND REPLACED NR 2 ENG FWD ISOLATORS PER MM 71-24-1G. REPLACEMENT OF FIRE BOTTLES SEE LOG PAGE 140150, SEE A/C MX LOG 140148 FOR FWD ISOLATOR REPLACEMENT INSTALLED NR 2 ENG PER WORK CARD 70T0002. OPS AND LEAK CHECK GOOD, OK FOR SERVICE. REQUIRED ITEM INSPECTION COMPLIED WITH. 2L73 4F RTA3WE 19950908000861995090800086NM 1995 9 8 95FDEA01233 119950831A3150692482725 CIRCUIT CARD BOEING727 727227 1384078NM FLIGHT DECK FAILED A FDEAC ABORTED TAKEOFF N FALSE WARNING TXTAXI/GRND HDL 1 SO25489FE 21492 T/O ABORTED AT 110 KTS, BECAUSE OF WARNING LIGHT, ALT ALERT, 3 REVERSERS, ALL GEAR WARNING LIGHTS GEAR PANEL. REMOVED AND REPLACED MASTER DIM AND TEST MODULE CARD. 2L73 4F A3WE 19950908000871995090800087NM 1995 9 8 95FDEA01234 119950901A53302024T3063 SKIN BOEING727 727232 1384082NM BS 1333 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FASTENERS AT BS 1333 ON SKIN HAS 11 PULLED THROUGH FASTENER WL 257, LT SIDE ON SKIN EDGE. REMOVED DAMAGED SKIN AT BS 1333 WL 257 LT, FABRICATED DOUBLER, FILLER AND TAPERED SHIM, SCOTCH BRITE, ALODINE AND PRIMED. INSTALLED AS PER FEDEX 54-30-3, 51-20-1. 2L73 4F A3WE 19950908000881995090800088NM 1995 9 8 95FDEA01235 119950901A53117075T6050 FRAME BOEING727 727232 1384082NM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED AT BS 680 BETWEEN STR 25 AND 23R. REPAIRED FRAME AT BS 680 BETWEEN STR 25 AND 23R, PER SRM 51-40-3 FEDEX. 2L73 4F A3WE 19950908000891995090800089NM 1995 9 8 95FDEA01236 119950901A53117075T6050 FRAME BOEING727 727232 1384082NM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED ON TOP BS 660 BETWEEN STR 25 AND 22L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 660 BETWEEN STR 25 AND 22L, IAW FEDEX SRM 51-10-3. 2L73 4F A3WE 19950908000901995090800090NM 1995 9 8 95FDEA01237 119950901A5347694121 SEAT TRACK BOEING727 727233 138408ANM BS 890 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION (72C207-00), ON SEAT TRACK BS 890 LBL 45 WL 208.5 IN WELL OF SEAT TRACK. REPLACED EXPANSION LINK SEAT TRACK BS 852 TO 870. REMOVED CORROSION AT STA 870 TO 890, .004 TO .005 MATERIAL IN AREA 1 BY 20 ORIGINAL THICKNESS, .100 WITHIN LIMITS IAW FEDEX SRM 53-10-1, 51-10-1, 51-10-2 AND MM 51-20-0. 2L73 4F RTA3WE 19950908000911995090800091NM 1995 9 8 95FDEA01238 119950901A5347694121 SEAT TRACK BOEING727 727233 138408ANM BS 741.5 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION (72C207-00), ON SEAT TRACK FLANGE BS 741.5 TO 757.5 LBL 25 WL 208. REMOVED CORRODED SEAT TRACK EXPANSION LINK, POSITIONED AND INSTALLED NEW SEAT TRACK EXPANSION LINK, LOCATED HOLES AND SECURED WITH FASTENERS IAW FEDEX SRM 53-10-1, 51-10-1, 51-10-2 AND FEDEX MM 51-20-0. 2L73 4F RTA3WE 19950908000921995090800092NM 1995 9 8 95FDEA01239 119950901A5347BAC1520841 SEAT TRACK BOEING727 727233 138408ANM BS 752-852 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION (72C207-00), ON SEAT TRACK BS 752 TO 852 LBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK PER FEDEX SRM 51-30-2, 51-10-1, 51-30-4, 51-10-2. 2L73 4F RTA3WE 19950908000931995090800093NM 1995 9 8 95FDEA01240 119950830A5315 FLOORBEAM BOEING727 727233 138408ANM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 CORROSION STA 620 LBL 12 CABIN FLOORBEAM. INSTALLED DOUBLER ASSY PER SRM 53-10-6 FIG 8. 2L73 4F RTA3WE 19950908000941995090800094NM 1995 9 8 95FDEA01241 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 FLOORBEAM UPPER CAP WHERE FLOORBEAM MOUNTS IS CORRODED AROUND SCREW HOLES BETWEEN 5 AND 6 SEAT TRACKS STA 1070. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 19950908000951995090800095NM 1995 9 8 95FDEA01242 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 TOP FLANGE OF FLOORBEAM AT STA 600 CORRODED BEYOND SRM LIMIT RBL 46.5 APPROX. CUT OUT DAMAGE, REPAIRED PER SRM 53-10-8 PG 44 TO 48. DAMAGE CUT OUT WAS 1 BY 1.5. 2L73 4F RTA3WE 19950908000961995090800096NM 1995 9 8 95FDEA01243 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25233FE 20936 CORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 1110 FROM 3 TO 20 RBL. REPAIRED PER SRM 51-10-6. 2L73 4F RTA3WE 19950908000971995090800097NM 1995 9 8 95FDEA01244 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 STA 1110 FLOORBEAM IS CORRODED ON TOP AND BOTTOM OF UPPER CAP AREA, WHERE FLOOR BOARDS MOUNT BETWEEN NR 5 AND NR 6 SEAT TRACKS. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 19950908000981995090800098NM 1995 9 8 95FDEA01245 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 CORROSION ON BOTTOM OF CABIN FLOORBEAM AROUND FLOOR BOARD ATTACH HOLES AT STA 1110 BETWEEN RBL 22.5 AND RBL 46. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 19950908000991995090800099NM 1995 9 8 95FDEA01246 119950901A5315 FLOORBEAM BOEING727 727233 138408ANM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20936 CORROSION ON TOP AND BOTTOM OF FLOORBEAM AROUND MOUNT HOLES AT STA 1070 BETWEEN RBL 22.5 AND RBL 46. REPAIRED PER SRM 53-10-8. 2L73 4F RTA3WE 19950908001001995090800100NM 1995 9 8 95FDEA01247 119950901A5311 FRAME BOEING727 72722C 138400FNM BS 540 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 FRAME BENT AND CRACKED STA 540 AT STR 7 TO 6R. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 51-10-4 PG 3 AND 4. 2L73 4F A3WE 19950908001011995090800101NM 1995 9 8 95FDEA01248 119950901A5311 FRAME BOEING727 72722C 138400FNM BS 520 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 520. REMOVED DAMAGED AREA OF FRAME AND INSTALLED REPAIR PER SRM 51-40-3 PG 1 TO 4. 2L73 4F A3WE 19950908001021995090800102NM 1995 9 8 95FDEA01249 119950901A5311 FRAME BOEING727 72722C 138400FNM BS 500 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 500. REMOVED DAMAGED AREA INSTALLED DOUBLER PER 51-40-3 PG 3. 2L73 4F A3WE 19950908001031995090800103WP 1995 9 8 95FDEA01250 119950905A5520NLC6041516 STRUCTURE DOUG DC10 DC1010 3022110WP RT ELEVATOR DAMAGED A FDEAK NONE O OTHER UKUNKNOWN 1 SO2568051 STRUCTURAL FAILURE ON RT ELEVATOR UPPER SURFACE, APPROX 3 INCHES LONG BY 3 INCHES WIDE AND HAD COLLAPSED APPROX .5 INCHES, DOES NOT APPEAR TO BE FROM IMPACT. THIS GOES ACROSS 4 RIBS AND IS LOCATED APPROX 2 FEET FROM O/B END OF ELEVATOR. ITEM FOUND DURING B-CHECK MX. REMOVED AND REPLACED O/B ELEVATOR IAW MM 27-20-02, PERFORMED ELEVATOR CHECK PER MM 27-30-02 PG 601 TO 603. 2L73 4F A22WE 19950908001041995090800104NE 1995 9 8 95UAL900043 219950717A7314 O-RING BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 FUEL PUMP FAILED A UALAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP297265U 21412 696565 SHUTDOWN NR 1 ENGINE DUE TO LOSS OF OIL QUANTITY. FOUND DAMAGED FUEL PUMP SHAFT O-RING, REPLACED O-RING SYSTEM, OP CHECKS OK. 2L73 4F4 F A3WE E2EA 19950908001051995090800105NM 1995 9 8 95UAL900108 119950824A5230 DOOR BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CARGO COMPT NOT LATCHED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP299022U 19060 AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF AND AIRCRAFT WOULD NOT PRESSURIZE. FOUND DOOR OPEN ON ARRIVAL, CHECKED LATCHES AND THEY OPERATED NORMAL, OVER CENTERED GOOD. NO PREVIOUS HISTORY. 2L72 4F4 F A16WE E2EA 19950908001061995090800106NM 1995 9 8 95UAL900109 119950828A261217051 FIRE LOOP BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 MALFUNCTIONED A UALAF ACTIVATE FIRE EXT. J WARNING INDICATION TXTAXI/GRND HDL 1 WP299070U 19951 656062 AFTER TAXI OUT, THE NR 2 FIRE WARNING LIGHT CAME ON AND TWO FIRE BOTTLES WERE DISCHARGED. LIGHT REMAINED ON, PASSENGERS EVACUATED BY SLIDES. FOUND FIRE LOOP M337 HAS A SHORT BETWEEN PINS 4 AND 6 IN CONNECTOR D992. REPLACED LOOP SYSTEM, OPS CHECKS OK. 2L72 4F4 F A16WE E2EA 19950908001071995090800107WP 1995 9 8 95UAL900110 119950828A5620AAA7010501 WINDOW DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN CRACKED A UALAK NONE L NO TEST CLCLIMB 1 WP291838U 46632 RETURNED TO FIELD WITH A CRACKED AND DELAMINATED PASSENGER WINDOW. REPLACED PASSENGER WINDOW 18J. THE DC-10 FLEET IS BEING INSPECTED AND SUSPECT WINDOWS ARE BEING REPLACED. 2L73 4F4 F A22WE E23EA 19950908001081995090800108NM 1995 9 8 95UAL900111 119950828A29136506606 HYD PUMP BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE ENGINE FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29615UA 21876 RETURNED TO FIELD UNDER AMBER ALERT WITH NR TWO SYSTEM HYDRAULIC FAILURE. FOUND ENGINE DRIVEN PUMP FAILED. REPLACED PUMP. CHECKS O.K. 2L72 4F4 FRTA1NM E3NE 19950908001091995090800109NM 1995 9 8 95UAL900112 119950830A2150 PACK BOEING777 777222 1385219NM PWA PW4077PW4077 NE RIGHT FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29777UA 26916 AIRCRAFT LOST RIGHT A/C PACK, AS RESULT OF ROUTE CHANGE. AIRCRAFT DIVERTED INTO LHR FOR FUEL. 2L72 4F4 FRTT0001SE E46NE 19950908001101995090800110NM 1995 9 8 95UAL900113 119950830A2910 RESERVOIRS BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE LT/RT DEPRESSURIZED A UALAA UNSCHED LANDING JW WARNING INDICATION INADEQUATE Q C CRCRUISE 1 WP29956UA 26704 DIVERTED TO SLC UNDER AMBER ALERT, DUE TO TWO INOP HYDRAULIC PUMPS. BOTH HYDRAULIC RESERVOIRS WERE DEPRESSURIZED FOR MAINTENANCE WORK AND WERE INADVERTENTLY LEFT DEPRESSURIZED. REMOVED DEPRESSURIZATION TOOLS AND SYSTEM OPS CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950908001111995090800111NM 1995 9 8 95UAL900114 119950901A5240 HINGE BOEING757 757222 1384956NM PWA 2037 PW2037 NE SERVICE DOOR BROKEN A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29509UA 24763 RETURNED TO ORD, DUE TO LEFT OVERWING SLIDE DEPLOYED LIGHT AND OVERWING DOOR MESSAGE. A BROKEN HINGE AND IMPROPER LATCHING OF THE SERVICE DOOR AFT OF THE SLIDE COMPARTMENT ACTIVATED THE DOOR SWITCH, WHICH CAUSED THE DOOR OPEN LIGHT. REPLACED HINGE. 2L72 4F4 FRTA2NM E17NE 19950908001121995090800112NE 1995 9 8 95UAL900115 219950901A7321 FUEL CONTROL HAMSTD 7436023 BOEING727 727222 1384073NM PWA JT8 JT8D17 52049NE LT ENGINE MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP297255U 92357 21402 ABORTED TAKEOFF AT 90 KNOTS WHEN A/C VEERED TO THE LEFT WITH FULL RIGHT RUDDER APPLIED. REPLACED THE FUEL CONTROL UNIT. THE FCU WAS OVERHAULED, BUT A SPECIFIC CAUSE OF FAILURE COULD NOT BE DETERMINED. 2L73 4F4 F A3WE E2EA 19950908001131995090800113WP 1995 9 8 MEJA9508001 219950804A7261MS51830201 INSERT SWRNGNSA227 SA227AT 8780610SW GARRTTTPE331TPE33111U 01514WP LT ENGINE STRIPPED E AMEJAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW17544UP AT544 P44209 FLT 2586 - BIS-FSD - LOST OIL PRESSURE ON LEFT ENGINE, SHUTDOWN ENGINE AND ELECTED TO LAND AT ABR. MAINTENANCE FOUND STRIPPED INSERT FOR OIL BYPASS BOLT. REPLACED INSERT IN ACCORDANCE WITH THE GARRETT MAINTENANCE MANUAL. PERFORMED RUNUP AND LEAK CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A5SW E4WE 19950908001141995090800114SW 1995 9 8 MEJA9508002 119950804A3230ML1092 LIMIT SWITCH SWRNGNSA227 SA227AT 8780610SW LT MLG FAILED E AMEJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW17560UP AT560 MAF - LEFT MAIN GEAR WOULD NOT FULLY RETRACT ON TAKEOFF, ATTEMPTED 4 GEAR CYCLES WITH NO LUCK. A NORMAL LANDING WAS MADE AT THE DEPARTURE POINT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED THE LEFT MAIN GEAR LANDING GEAR UP LIMIT SWITCH. INSTALLED NEW SWITCH PART NUMBER ML1092 AND PERFORMED GEAR SWING IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL 32-30-00. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19950908001151995090800115WP 1995 9 8 MWEA95281 119950901A25603552273501 GIRT BAR LATCH DOUG DC9 DC915 3022036WP FWD ENTRANCE DIRTY A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31300ME 45718 CREW REPORTS, FORWARD ENTRANCE DOOR EVACUATION SLIDE GIRT BAR IS HARD TO REMOVE AND INSTALL. MAINTENANCE CLEANED AND LUBED GIRT BAR LATCHES. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950908001161995090800116WP 1995 9 8 MWEA95282 119950901A3260 SWITCH WASHER DOUG DC9 DC915 3022036WP RT MLG LOOSE A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31900ME 45841 PILOT REPORTS, ON CLIMBOUT THE RIGHT GEAR RED UNSAFE LIGHT WOULD NOT EXTINGUISH, PERFORMED QRH PROCEDURES, RETURNED TO MKE. MAINTENANCE FOUND RIGHT UPLATCH SWITCH STRIKER WASHER LOOSE, STRIKER HAD JUMPED WASHER. SECURED WASHER, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950908001171995090800117NM 1995 9 8 MWEA95283 119950902A3350600304031 EEL PWR SUPPLY DOUG MD88 MD88 3023688NM CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31701ME 49760 DURING R-CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS REPORTED VERY DIM BETWEEN ROWS 15 AND 18. MAINTENANCE REMOVED AND REPLACED FLOOR TRACK LIGHTING BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950908001181995090800118NM 1995 9 8 P5CA9500726 119950831A5245 DOOR BOEING747 747122 1384872NM NR 1 PACK DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23854FT 19754 NR 1 PACK HEAT EXCANGER ACCESS DOOR HAS AN AREA OF DELAMINATION. REMOVED AND HOT BOND REPAIRED PANEL PER BOEING SRM 51-40-12, REINSTALLED PANEL. 2L74 4F A20WE 19950908001191995090800119NE 1995 9 8 P5CA9500727 219950904A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 FLAME-OUT A P5CAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 WP23850FT519951256 19755 685616 DURING CRUISE FL 370, NR 1 ENGINE FLAMED-OUT, ENGINE SHUTDOWN PROCEDURE ACCOMPLISHED. DESCENDED TO FL 350 IN FLIGHT START PER AOM ENGINE PERFORMANCE NORMAL. CHECKED ENGINE INTAKE AND EXHAUST, FUEL PUMP PRESSURE CHECKED, CONDITION MOTOR CHECKED, AND WATER CONTAMINATION CHECKED PER MAINTENANCE MANUAL 71-00-42. ALL CHECKED GOOD AIRCRAFT RELEASED. 2L74 4F4 F A20WE E20EA 19950908001201995090800120WP 1995 9 8 SCNA95181 119950901A2560141111001 TEST LIGHT BATT DOUG DC10 DC1015 3022118WP R 2 DOOR DISCHARGED A SCNAK NONE L NO TEST UKUNKNOWN 1 GL15151SY 48295 THE R-2 DOOR SLIDE INTEGRITY TEST LIGHT DID NOT ILLUMINATE WHEN PRESSED. REMOVED AND REPLACED TEST BATTERIES, AND SLIDE TESTED GOOD. 2L73 4F A22WE 19950908001211995090800121NM 1995 9 8 UPS404353 119950901A3350 EEL LAMP BOEING747 747123 1384873NM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK, LT DOOR SILL EMERGENCY LIGHT INOP. RELAMPED, OPS CK OK. 2L74 4F A20WE 19950908001221995090800122NM 1995 9 8 UPS404357 119950904A3350 EEL LAMP BOEING747 747123 1384873NM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01675UP 20390 WHILE ON GROUND, MAINTENANCE FOUND 1 EMER LIGHT BURNED OUT, AFT O/H ABOVE FLT RECORDER. RELAMPED AS REQ'D, OPS CK GOOD. 2L74 4F A20WE 19950908001231995090800123NM 1995 9 8 UPS404358 119950829A5320 WEB PLATE BOEING747 747123 1384873NM BS 1620-1640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND WEB PLATE ON RBL 11.33 STA 1620 AND 1640, CORRODED AND CRACKED. CORROSION AND CRACK OUT OF LIMITS ACC SRM 53-10-01. REPLACED WEB IAW SRM 51-10-01, AT BS 1620 TO 1640 RBL 11.33. 2L74 4F A20WE 19950908001241995090800124NM 1995 9 8 UPS404359 119950829A5412 BLKHD WEB BOEING747 747123 1384873NM NR 2 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PYLON NR 2 CRACKED, ON THE AFT BULKHEAD LWR SIDE WEB. CRACK WAS OUT OF LIMITS ACC SRM 54-10-01 FIG 1 PAGE 4. WEB HAS BEEN REPAIRED ACC SRM 51-40-02. 2L74 4F A20WE 19950908001251995090800125WP 1995 9 8 UPS804354 119950901A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01851UP 46051 WHILE ON GROUND, MAINTENANCE FOUND EMERG BATTERY PACK HAD LOW VOLTAGE. THE LIGHT WOULD COME ON AND THEN DIM AND GO OUT. REPLACED BATTERY PACK, CHECK OK. 2L74 4F RT4A25 19950908001261995090800126WP 1995 9 8 UPS804355 119950901A2910 HYD LINE DOUG DC8 DC873F 302199FWP RUDDER PUMP CHAFED A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01868UP 45968 PILOT REPORTED, HYD FLUID LOSS. FOUND STANDBY RUDDER PUMP PRESSURE LINE CHAFED AND REPLACED IAW MM 29-00-00. 2L74 4F RT4A25 19950908001271995090800127WP 1995 9 8 UPS804356 119950902A2915 RELIEF VALVE DOUG DC8 DC873F 302199FWP HYD SYST LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO01752UP 45968 PILOT REPORTED, HYD FLUID LOSS. PRESSURE AFTER LANDING, AIR BRAKES WERE USED. AUX PUMP PRODUCED NO PRESSURE, BUT FLUID QUANTITY DECREASED. FOUND RT GEAR BOGIE UNLOCK PRESS RELIEF VALVE LEAKING. CAPPED OFF BOGIE UNLOCK CYLINDER HYD LINES AT STRUT MANIFOLD. PLACED ON MEL 32-6 ON M97762, LEAKING RELIEF VALVE REMOVED. 2L74 4F RT4A25 19950908001281995090800128EU 1995 9 8 WWMA950061 119950903A3241140041 TRANSDUCER SAAB SF340 340B 7860101EU MLG ANTI-SKID DEFECTIVE A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 WP15306AE 340B306 FLT 5090 - BPT-DFW - AFTER LANDING PILOT APPLIED THE BRAKES AND THE ANTI-SKID LIGHT CAME ON. THE CONTROL TOWER REPORTED SMOKE, THE ANTI-SKID WAS TURNED OFF AND THE BRAKES WORKED NORMALLY. UPON INVESTIGATION MAINTENANCE INSPECTED THE NR 4 BRAKE AND REPLACED THE NR 4 ANTI-SKID TRANSDUCER IAW SAAB AMM 32-40-50. ALL OPERATIONAL CHECKS GOOD, NO FURTHER PROBLEMS. 2L72 4T RTA52EU 19950908001291995090800129CE 1995 9 8 7289596CK 119950729A77142CM9ABE6 TACH GENERATOR LEAR 23 23LEAR 5170102CE LT ENGINE FAILED A KKFAA UNSCHED LANDING O OTHER CRCRUISE 1 GL2396CK 23016 LEFT TACHOMETER FAILED IN-FLIGHT. AIRCRAFT RETURNED TO YIP. REPAIRED CANNON PLUG. OPS CHECKED GOOD. (X) 1L72 4J A5CE 19950908001301995090800130NE 1995 9 8 89955LL 219950809A73238005004 GOVERNOR LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE LT ENGINE MALFUNCTION A KKFAO OTHER K FLUID LOSS CLCLIMB 1 GL235LL 735 697932 183 251334 LEFT ENGINE SURGED ON CLIMB-OUT. OVERSPEED GOVERNOR FOUND LEAKING AT SPLIT LINE. REPLACED OVERSPEED GOVERNOR WITH SERVICEABLE UNIT, OPS AND LEAK CHECKED GOOD. (X) 2L72 4J4 J A10CE 1E16 19950908001421995090800142SO 1995 9 8 95ZZZX4439 119950807A2910159H1016519P8 LINE GULSTMG159 G159 3952202SO LT HYD PUMP OUT RUPTURED A BTVAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 GL23812CC 129 DURING FLIGHT, THE SUBJECT HYDRAULIC LINE RUPTURED CAUSING LOSS OF ALL MAIN SYSTEM HYDRAULIC FLUID. THE FLIGHT CREW DECLARED AN EMERGENCY, BLEW THE LANDING GEAR DOWN USING THE EMERGENCY GEAR EXTENSION SYSTEM, AND MADE AN UNEVENTFUL LANDING AT YIP. REF: OPER CONTROL NR BTVR626C080395. 2L72 4T 1A17 19950908001451995090800145SO 1995 9 8 95ZZZX4442 119950810A7810LW10162 RISER PIPER PA31 PA31350 7103110SO NR 6 CYL EXH FAILED A TIMAE ENGINE SHUTDOWN JR WARNING INDICATION PARTIAL RPM/PWR LOSS CRCRUISE 1 NM07700TS 318152157 FLT 9922 - ON AUGUST 10, 1995, FLIGHT 9922 EXPERIENCED A LOSS OF MANIFOLD PRESSURE AND A RAPID RAISE IN CHT ON THE LEFT ENGINE. THE FLIGHT WAS OUTBOUND FROM COLORADO SPRINGS ABOUT FORTY MILES WHEN POWER WAS LOST. MAINTENANCE FOUND THE EXHAUST RISER COMING FROM THE NR 6 CYLINDER (PN/LW-10162 TOTAL TIME ON FAILED COMPONENT IS UNKNOWN) HAD ERODED THROUGH CAUSING THE LOSS OF MANIFOLD PRESSURE, THE EXHAUST GASES WERE BLOWING ACROSS THE CHT PROBE WHICH IS ALSO LOCATED ON THE NR 6 CYLINDER CAUSING THE RAPID RISE IN CHT. THE EXHAUST RISER ASSY FOR NRS 2, 4, 6 CYLINDERS WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1L72 3O A20SO 19950908001551995090800155EU 1995 9 8 SIMA952312 119950819A5280S52871300500699 DOOR AEROSPATR42 ATR42300 8680920EU LT MLG MISSING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21423MQ 030 UPON AIRCRAFT ARRIVAL AT OHARA, NOTED THE LEFT MAIN LANDING GEAR BIFOLD DOOR WAS TORN AWAY FROM AIRCRAFT. ACFT TT 1832. (X) 2H72 4T RTA53EU 19950908001781995090800178WP 1995 9 8 95ZZZX4471 219950819A7230S9413529 O-RING LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP LT ENGINE CUT A XMRAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW218LA 124 P74387 DCA - EN ROUTE FROM DCA TO 029, FLIGHT CREW TURNED TEMP CONTROLLER TO WARM. LIGHT SMOKE THEN ENTERED CABIN. FLIGHT CREW THEN TURNED TEMP CONTROLLER TO FULL COLD, INCREASED CABIN ALTITUDE AND TURNED OFF LT BLEED AIR. SMOKE CLEARED AND OPERATIONS WERE CONTINUED. UPON LANDING AT 029, CREW NOTED A LARGE AMOUNT OF OIL ON ENGINE AND COWLING AND PUDDLING ON GROUND. CORRECTIVE ACTION WAS TAKEN BY REPLACING, PN S9413-529, O-RING. GROUND RUN AND SUBSEQUENT FLIGHTS PROVED NO FURTHER DEFECTS. 2L72 4F4 F A10CE E6WE 19950908001881995090800188CE 1995 9 8 95ZZZX4481 119950817A32601VA20 SWITCH CESSNA402 402CESSNA 207590KCE MLG SQUAT FAILED A OEZAK NONE O OTHER NRNOT REPORTED 1 WP193500T11285 4020113 SQUAT SWITCH FAILED CAUSING LANDING GEAR TO NOT RETRACT. 1L72 3O A7CE 19950908001951995090800195WP 1995 9 8 9513429612 119950613A5512 SKIN DOUG DC9 DC932 3022066WP HORIZ STAB CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT HORIZONTAL STABILIZER UPPER AFT SKIN, LOWER SURFACE OF THE STRINGER NR 3 LAP FLANGE. REPAIRED PER EA 96-98094. 2L72 4F A6WE 19950908001961995090800196NM 1995 9 8 9513432204 119950822A5753652163476 SKIN BOEING727 727251 138408HNM TE FLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 9151 22544 DURING PERIODIC CHECK, FOUND INBOARD AFT FLAP DELAMINATED AND SPLIT. REPLACED FLAP. 2L73 4F A3WE 19950908001971995090800197NM 1995 9 8 9513442204 119950822A5755651734781A SKIN BOEING727 727251 138408HNM NR 2 SPOILER DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 6576 22544 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE LEFT WING NR 2 SPOILER UPPER SKIN. REPLACED SPOILER. 2L73 4F A3WE 19950908001981995090800198NM 1995 9 8 9513452204 119950822A57556517348107A SKIN BOEING727 727251 138408HNM NR 5 SPOILER DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 6576 22544 DURING PERIODIC CHECK, FOUND DELAMINATION IN THE LEFT WING NR 5 SPOILER UPPER SKIN. REPLACED SPOILER. 2L73 4F A3WE 19950908001991995090800199WP 1995 9 8 9513469760 119950826A5320 BRACKET DOUG DC9 DC941 302207NWP FS 1114 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01760NW 47288 DURING LINE CHECK, FOUND A CRACK IN THE SHEAR CLIP ANGLE, FS 1114 AT LONGERON 15L. REPAIRED CLIP (P/N 9912246-43) PER EA 97-100866. 2L72 4F A6WE 19950908002001995090800200WP 1995 9 8 9513479998 119950828A5320 FITTING DOUG DC9 DC931 3022065WP FS 579 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018934E 47143 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 29R AND 30 END FITTINGS AT FS 579. REPLACED FITTINGS PER SRM 51-10-3. 2L72 4F A6WE 19950908002011995090800201WP 1995 9 8 9513489946 119950828A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT T-CAP TIE FITTING, FS 604 AT LONGERON 30. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950908002021995090800202WP 1995 9 8 9513499953 119950828A57535919217502 HINGE DOUG DC9 DC931 3022065WP NR 3 FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 37635 47158 DURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE STUD HOLES. REPLACED HINGE PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19950908002031995090800203NM 1995 9 8 9513506716 119950830A5522 SKIN BOEING747 747251F 1384898NM RT ELEVATOR DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01616US 21120 DURING PERIODIC CHECK, FOUND PREVIOUS FIBERGLASS REPAIR DELAMINATED ON THE RIGHT OUTBOARD ELEVATOR, 8 FORWARD OF THE TRAILING EDGE. REPAIRED PER SRM 51-40-12. 2L74 4F A20WE 19950908002041995090800204WP 1995 9 8 9513519105 119950830A57555910055516 SKIN DOUG DC9 DC915 3022036WP RT SPOILER DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0195S 8639 47205 DURING LINE CHECK, FOUND DELAMINATION IN THE RIGHT INBOARD SPOILER. REPLACED SPOILER PER CITEXT 90-2760-1-9901. 2L72 4F A6WE 19950908002051995090800205NM 1995 9 8 9513522204 119950830A5220 CASTING BOEING727 727251 138408HNM EMERGENCY EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 22544 DURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT AFT EMERGENCY EXIT LATCH OPENING FRAME. REPLACED CASTING. 2L73 4F A3WE 19950908002061995090800206WP 1995 9 8 9513539963 119950831A7312 FUEL HEAT VALVE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE MALFUNCTIONED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01913RW 47171 657133 NR 2 ENGINE FUEL HEAT SYSTEM CYCLED ON INTERMITTENTLY WHILE SELECTED OFF. OIL TEMPERATURE EXCEEDED NORMAL LIMITS AND A PRECAUTIONARY ENGINE SHUTDOWN WAS ACCOMPLISHED. THE FLIGHT RETURNED TO MEM LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE AND CHANGED THE ENGINE OIL AND FILTER. SYSTEM OPERATION WAS SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950908002071995090800207WP 1995 9 8 9513549869 119950830A7932 OIL QTY IND SYS DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE MALFUNCTIONED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL01778NC 48100 649188 CLIMBING OUT OF DTW, NR 2 ENGINE OIL QUANTITY INDICATION BEGAN DECREASING RAPIDLY. NOTING A RISE IN OIL TEMPERATURE, THE CREW DECIDED TO PERFORM A PRECAUTIONARY SHUTDOWN OF THE ENGINE. THE FLIGHT RETURNED TO DTW FOR AN UNEVENTFUL LANDING. THE OIL TEMPERATURE SYSTEM OPERATION CHECKED NORMAL. THE OIL QUANTITY INDICATION SYSTEM HAD MALFUNCTIONED, IT WAS PLACED ON MEL AND THE AIRCRAFT CONTINUED IN SERVICE. SUBSEQUENT REPLACEMENT OF THE OIL QUANTITY TRANSMITTER RESTORED NORMAL SYSTEM OPERATION. 2L72 4F4 F A6WE E2EA 19950908002081995090800208EU 1995 9 8 9513553204 119950831A2923 HYD PUMP AIRBUS320 A320211 3930320EU BLUE HYD SYST FAILED A NWAAO OTHER J WARNING INDICATION CRCRUISE 1 GL01304US 40 DURING CRUISE RECEIVED HYD-B ELEC PUMP LOW PRESSURE MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP. OPS AND LEAK CHECKED OK. 2L72 4F RTA28NM 19950908002091995090800209NE 1995 9 8 9513561155 219950903A73217426005 FUEL CONTROL DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 GL01155US33912384 46764 686152 TOP OF DESCENT, NR 2 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE AND CONTINUED LANDING. BORESCOPED, PERFORMED PRECISION TRIM AND REPLACED ENGINE CONTROL. 2L73 4F4 F A22WE E20EA 19950908002101995090800210NM 1995 9 8 9513572202 119950831A324140835 TRANSDUCER BOEING727 727251 138408HNM LT MLG MALFUNCTIONED A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 GL01202US422707579 22155 AFTER LANDING, TOWER REPORTED SMOKE EMITTING FROM LEFT MAIN GEAR. FIRE DEPARTMENT INSPECTED AND FOUND NR 2 TIRE FLAT. AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED NR 1 TIRE, NR 2 BRAKE, TIRE AND ANTI-SKID TRANSDUCER. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950908002111995090800211NE 1995 9 8 9513586636 219950831A7200 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 4 FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01636US 23547 15180 EN ROUTE JFK-NRT, THE NR 4 ENGINE OIL PRESSURE WENT TO ZERO AND OIL QUANTITY PEGGED OFF SCALE. CREW FOLLOWED COCKPIT OPERATING MANUAL, SHUTDOWN NR 4 ENGINE AND DIVERTED TO MSP WITHOUT FURTHER INCIDENTS. MAINTENANCE REPLACED THE ENGINE AND TEST WAS NORMAL. 2L74 4F4 F A20WE E3NE 19950908002121995090800212WP 1995 9 8 9513591156 119950903A7830 TR DRIVE CABLE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 2 ENGINE BROKEN A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01156US 46765 686143 DURING TAKEOFF, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. REMOVED BROKEN DRIVE CABLE, INSTALLED LOCKOUT PLATES AND DEFERRED PER MEL 78-1A. 2L73 4F4 F A22WE E20EA 19950908002131995090800213NM 1995 9 8 9513602285 119950830A7711 EPR IND BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01285US 21324 696474 NR 1 ENGINE EPR INDICATION FLUCTUATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND PERFORMED A RUNUP, NO DISCREPANCIES NOTED. AIRCRAFT TURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950908002141995090800214NM 1995 9 8 9513612769 119950901A2612 FIRE WARNING BOEING727 7272M7 138407SNM NR 2 ENGINE ACTIVATED A NWAAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 GL01729RW 21742 DURING DEPARTURE CLIMB, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED FOR 1.5 SECONDS DURATION. ALL OTHER INDICATIONS WERE NORMAL. JETTISONED 3,000 LBS OF FUEL AND RETURNED TO TPA WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION UNDER INVESTIGATION. 2L73 4F A3WE 19950908002151995090800215WP 1995 9 8 9513629161 119950831A5280 DOOR DOUG DC9 DC914 3022034WP LT MLG DAMAGED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018905E 45746 LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED, RECYCLED GEAR WITH SAME RESULTS. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND FLIGHT RETURNED TO ATL, LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN INBOARD GEAR DOOR, RIGGED AND CYCLED DOORS SEVERAL TIMES. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908002161995090800216 1995 9 8 9513636306 419950830A2330 VIDEO CONSOLE BOEING747 747451 1384940NM CABIN FAILED A NWAAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL01666US 23821 DURING FLIGHT, A PASSENGER SPILLED A LARGE AMOUNT OF WATER ON THE ARMREST OF SEAT 10JK. THEN, DURING THE DEPLANING OF PASSENGERS, THE ARMREST STARTED EMITTING A SMALL AMOUNT OF WHITE SMOKE. FLIGHT ATTENDANT USED HALON FIRE EXTINGUISHER ON ARMREST AND SMOKING CEASED. MAINTENANCE REPLACED VIDEO CONSOLE, THE SEAT ELECTRICAL BOX AND THE UNDERSEAT ELECTRICAL BOX. OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19950908002171995090800217EU 1995 9 8 95FDEA01251 119950905A213182010B040901 CONTROLLER AIRBUS300 A300F4605R 3930327EU CABIN FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25411FE 359 KUL - ON CLIMBOUT, NR 1 PRESSURE CONT FAILED, NR 2 PRESS CONT COULD NOT CONTROL CABIN. IAW ECAM PROCEDURES SELECTED MANUAL CONTROL, UNABLE TO STOP CABIN RATE OF CLIMB/DECENT. CABIN PRESS DISPLAY ON ECAM SHOWED OUTFLOW VALVE NR 1 AFT CYCLING RANDOMLY. EME DESCENT ACCOMP, TURNBACK. SWAPPED NR 1 AND NR 2 AFT OUTFLOW VALVES, PERFORMED AUTO AND MANUAL CONTROL TEST ON BOTH SYS IAW A-310 MM 21-30-00, ALL TEST NORMAL. NR 2 CABIN PRESS SYS CONSIDERED INOP DUE TO OUTFLOW VALVE FLUX. DEFERRED PER MEL 21-44 CONTROL NR 0904005 CAT 'C' EXP 9-14-95, MXP C/W SYS NR 2 REG DEACTIVATED. REMOVED AND REPLACED NR 1 PRESS CONTROLLER AS PRECAUTIONARY MEASURE, CONTROLLER BITE CHECK NORMAL. 2L72 4F RTA35EU 19950908002181995090800218NM 1995 9 8 95FDEA01252 119950830A5320 ANGLE BOEING727 727223 1384074NM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 SIDEWALL SLANT PANEL ATTACHMENT IS CORRODED AT RT CREASE ANGLE ATTACHMENT JUST AFT OF STA 620, LWR AFT CORNER AREA OF DOOR CUTOUT. INSTALLED NEW SLANT PANEL ATTACH SUPPORT ANGLE AFT OF STA 620 RT, PER SRM 51-40 PAGE 1. 2L73 4F A3WE 19950908002191995090800219NM 1995 9 8 95FDEA01253 119950901A5313 STRINGER BOEING727 72722C 138400FNM BS 460 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 MAIN CARGO, NR 7L STR AT STA 460 CRACKED. CUTOUT CRACKED STR SECTION. REPAIRED PER SRM 53-10-3 PAGE 7, FUSELAGE STR REPAIR. 2L73 4F A3WE 19950908002201995090800220NM 1995 9 8 95FDEA01254 119950905A533065C139132 SKIN BOEING727 727233 138408ANM BS 1010-1090 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 FUSELAGE SKIN PANEL IS SEVERELY NICKED AND GOUGED FROM BS 1010 TO 1090 STR 20 TO 26R, REQUIRING REPLACEMENT OF PANEL. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 20 TO 26R, IAW FEDEX SRM 51-30-2, BAC DRW 65-54583 AND EA NR 7-5300-25594. 2L73 4F RTA3WE 19950908002211995090800221NM 1995 9 8 95FDEA01255 119950905A53306554583136 SKIN BOEING727 727233 138408ANM BS 1010-1183 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 LOWER 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM 1010 TO 1183 STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 26 LT AND RT, IAW FEDEX SRM 51-30-2, BAC DRAWING 6554583 SHT 4 AND EA NR 7-5300-25594. 2L73 4F RTA3WE 19950908002221995090800222NM 1995 9 8 95FDEA01256 119950905A53306554583186 SKIN BOEING727 727233 138408ANM BS 950-1010 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 LWR 46 SECTION SKIN IS SEVERELY GOUGED AND NICKED, REQUIRING REPLACEMENT OF SKIN PANEL FROM BS 950 TO 1010, STR 26 LT AND RT. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND INSTALLED NEW AT BS 950 TO 1010 STR 25 LT AND RT, IAW FEDEX SRM 51-30-2, BAC DRAWING NR 65-54581, FEDEX EA 7-5300-25394. 2L73 4F RTA3WE 19950908002231995090800223NM 1995 9 8 95FDEA01257 119950905A53157075T6 FLOORBEAM BOEING727 727233 138408ANM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25271FE 22036 CORROSION (71C709-02), ON LOWER FLANGE OF FLOORBEAM AT BS 1070 RBL 7 WL 200. CORROSION WAS FOUND TO BE OUT OF LIMITS ON LOWER FLANGE OF FLOORBEAM AT BS 1070, RBL 1 TO 16 AND RBL 50, PER FEDEX SRM 53-10-1. REPAIRED LOWER FLANGE OF FLOORBEAM AT BS 1070 LBL 27 TO RBL 55 WL 200, PER FEDEX SRM 53-10-8 FIG 8. 2L73 4F RTA3WE 19950908002241995090800224NM 1995 9 8 95FDEA01258 119950905A5315BAC150529222 FLOORBEAM BOEING727 727233 138408ANM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 WHILE ACCESSING FOR REPAIR ON CARD NR O102, DISCOVERED THE UPPER CHORD OF 344 BEAM TO BE CORRODED BEYOND LIMITS AT RBL 30 LBL 45 WL 208. THE CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED ENTIRE UPPER CHORD, FABRICATED NEW CHORD AND INSTALLED ALL WORK PER FEDEX SR 27-53-007. 2L73 4F RTA3WE 19950908002251995090800225NM 1995 9 8 95FDEA01259 119950905A5347BAC1520841 SEAT TRACK BOEING727 727233 138408ANM BS 758-852 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION (72C207-00), ON LONG BEAM FLANGE AND FASTENER HOLES AT BS 758 TO 852 RBL 25 WL 208.1. CORROSION REMOVAL WAS OUT OF LIMITS ON SEAT TRACK. REPLACED SEAT TRACK, REPAIRED SEAT TRACK FLANGE, ALL WORK DONE IAW EA NR 7-5310-25652. 2L73 4F RTA3WE 19950908002261995090800226NM 1995 9 8 95FDEA01260 119950905A5347BAC1520792 SEAT TRACK BOEING727 727233 138408ANM BS 870-893 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25263FE 21625 CORROSION (72C207-00), ON SEAT TRACK BS 870 TO 893 RBL 45 WL 208.5. THE CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER FEDEX SRM 53-10-1. 2L73 4F RTA3WE 19950908002271995090800227WP 1995 9 8 ABXA9500685 119950905A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23955AX 8877 47619 DURING PREFLIGHT INSPECTION, FOUND THE FLIGHT COMPARTMENT EMERGENCY LIGHTS VERY DIM. REPLACED THE BATTERIES IN THE SUPPLY PACK IAW DC-9 SUPP MM 33-53-00, OPS CHECKED NORMAL. 2L72 4F A6WE 19950908002281995090800228WP 1995 9 8 ABXA9500686 119950905A32607910105 TERMINAL STRIP DOUG DC9 DC931 3022065WP RT MLG DIRTY A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23943AX 47528 AFTER TAKEOFF FROM OKC, THE RIGHT GEAR UNSAFE LIGHT WAS ILLUMINATED. RECYCLED GEAR, NO HELP AND GEAR UPLATCH WAS UNSATISFACTORY TOO. CLEANED GROUND WIRE, CANNON PLUG AND TERMINAL STRIP. OPS CHECKED GEAR IAW DC-9 SUPP MM 32-60-00. OPS CHECKED GOOD AT THIS TIME. 2L72 4F A6WE 19950908002291995090800229WP 1995 9 8 ABXA950684 119950831A56105613219502 SLIDING WINDOW DOUG DC9 DC941 302207NWP COCKPIT OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23975AX 47512 DURING POST FLIGHT INSPECTION, FOUND FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. CLEANED TRACK, REPOSITIONED OPERATING ASSEMBLY AT TOP OF WINDOW AND LUBRICATED. OPS CHECKED GOOD IAW DC-9 MM. 2L72 4F A6WE 19950908002301995090800230SO 1995 9 8 COM11957 119950831A301044E202A SEPARATOR EMB 120 EMB120RT SO WING DE-ICE BROKEN A COMAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO01137H 15918 120137 NR 2 ENGINE DUCT LEAK WARNING CAME ON DURING CLIMB, AIRCRAFT RETURNED TO MCO. REPLACED BROKEN WING DE-ICE BLEED AIR WATER SEPARATOR. 2L72 4T RTA31SO 19950908002311995090800231EA 1995 9 8 COMA0544 119950901A3350BJ10017001 EEL LENSE CNDAIRCL600 CL6002B19 EA CABIN BROKEN A COMAK NONE O OTHER ININSP/MAINT 1 SO01929CA 7035 LOWER EMERGENCY LIGHT ON MAIN PASSENGER DOOR HAS A BROKEN LENSE AND DOES NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. 2L72 4F RTA21EA 19950908002321995090800232EU 1995 9 8 COMA1137 119950903A33506104781 EEL BATTERY PACK SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01359CA 340A053 AFT LT FUSELAGE AND AFT MOST RT CABIN OVERHEAD EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK NUMBER 24LN. 2L72 4T RTA52EU 19950908002331995090800233SO 1995 9 8 COMA1956 119950901A7931311489201 VALVE EMB 120 EMB120RT SO PWA 118 PW118A NE NR 1 ENGINE STUCK A COMAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01159A 12059 115571 DURING FLIGHT, THE NR 1 ENGINE OIL PRESSURE DECREASED TO 52 PSI, ALONG WITH SOUND OF RELAYS CLICKING IN PILOTS SIDE PANEL. WHILE THE PROPELLER WAS IN FEATHER OIL PRESSURE RETURNED TO 60 PSI. REMOVED AND REPLACED THE P2.5 SWITCHING VALVE. 2L72 4T4 TRTA31SO E20NE 19950908002341995090800234EA 1995 9 8 COMA60543 119950830A2760270003 PCU CNDAIRCL600 CL6002B19 EA RT SPOILER DEFECTIVE A COMAK NONE F FLT CONT AFFECTED UKUNKNOWN 1 SO01924CA3516 2017 7026 FLIGHT SPOILER FAULT MESSAGE ON EICAS. REPLACED THE RT INBD SPOILER POWER CONTROL UNIT. 2L72 4F RTA21EA 19950908002351995090800235NM 1995 9 8 DL72S953539 119950826A5320 ANGLE BOEING727 727232 1384082NM BS 740-780 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 ANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780, CORRODED WHERE HINGES ATTACH FOR PANEL 3348L. FOUND DURING HMV AND REPAIRED PER MM 53-30-1 PG 807 TO 808. 2L73 4F A3WE 19950908002361995090800236NM 1995 9 8 DL72S953540 119950817A5531 RIB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 CRACK INSIDE VERTICAL STABILIZER, RIGHT SIDE 4TH BAY UP, 7TH RIB FROM TOP. CRACK FOUND AT HMV, REPAIRED PER MM 53-30-0 PG 802. 2L73 4F A3WE 19950908002371995090800237NM 1995 9 8 DL72S953542 119950830A3350012209069 EEL BULB BOEING727 727232 1384082NM RT OVERWING FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11493DA 21062 RT CENTER OVERWING EMERG LIGHT, AFT BULB INOP. RELAMPED, OPERATION NORMAL. 2L73 4F A3WE 19950908002381995090800238NM 1995 9 8 DL72S953543 119950830A3350334202395 EEL SOCKET BOEING727 727232 1384082NM CABIN WORN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11493DA 21062 LEFT FWD DOOR SLIDE LIGHT INOP. REPLACED WORN LIGHT SOCKET, OPERATION NORMAL. 2L73 4F A3WE 19950908002391995090800239NM 1995 9 8 DL72S953553 119950830A5754 SKIN BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED .3750 INCH UNDER TAI DUCT ON NR 2 SLAT. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4. 2L73 4F A3WE 19950908002401995090800240NM 1995 9 8 DL72S953554 119950830A5754 SKIN BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING A-1 LETTER CHECK, FOUND COVE SKIN SUPPORT ANGLE CRACKED 1 INCH FROM O/B END ON NR 4 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950908002411995090800241NM 1995 9 8 DL72S953555 119950830A5720 STIFFENER BOEING727 727232 1384082NM LT WING LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING A-1 LETTER CHECK, FOUND I/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. O/B SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 3 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950908002421995090800242NM 1995 9 8 DL72S953556 119950830A5720 STIFFENER BOEING727 727232 1384082NM LT WING LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11492DA 21061 DURING A-1 LETTER CHECK, O/B LEADING EDGE SPAR STIFFENER HAS 1.5 INCH CRACK AT NR 2 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950908002431995090800243NM 1995 9 8 DL72S953560 119950827A531165163255001 FRAME BOEING727 727232 1384082NM FS 760/783 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11515DA 21431 DURING HMV IN ATL, SEVERAL HOLES IN THE INBOARD FRAME FLANGE WERE OVERSIZED AT FS 760.95 AND FS 783.95, IN BOTH RT AND LT SIDE WHILE ACCOMPLISHING EO 4-61904-3AD. THE HOLES WERE AUTHORIZED OVERSIZED PER S/B 727-53-0197 REV 2. 2L73 4F A3WE 19950908002441995090800244NM 1995 9 8 DL72S953563 119950823A532069678811 CHORD BOEING727 727225 1384077NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 DURING LETTER CHECK IN TPA, THE UPPER CHORD AT RBL 20 RUNNING FORE/AFT IN THE VENTRAL STAIRWAY TORQUE BOX WAS FOUND CRACKED AT STA 1273. THE INBOARD END OF THE FORWARD SUPPORT ANGLE AT STA 1273 HAS AN APPROX 3 INCH CRACK AND THE FRAME BEAM HAS AN APPROX 4 CRACK IN THE INBOARD END. DAMAGED PARTS WILL BE REPAIRED AND REPLACED IN ACCORDANCE WITH S/B 727-53-0129 REV 4. 2L73 4F A3WE 19950908002451995090800245NM 1995 9 8 DL72S953566 119950831A5754651622199 RIB BOEING727 727232 1384082NM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11411DA 21223 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH NR 6 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950908002461995090800246NM 1995 9 8 DL72S953573 119950830A5312 BULKHEAD BOEING727 727232 1384082NM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 INSIDE VENTRAL STABILIZER AT STA 1303, BULKHEAD LOWER VERTICAL WALL ABOVE S-DUCT HAS CRACK AT LT CORNER. CRACK WAS FOUND AT HMV, REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950908002471995090800247NM 1995 9 8 DL72S953574 119950826A5320 ANGLE BOEING727 727232 1384082NM BS 740-780 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 ANGLE CORRODED, A/C BAY DOOR ATTACH TEE FROM STA 740 TO 780 CORRODED WHERE HINGES ATTACH FOR PANEL NR 3448. CORROSION WAS FOUND AT HMV, REPAIRED PER M/M 53-30-1 PG 807 AND 808. 2L73 4F A3WE 19950908002481995090800248NM 1995 9 8 DL72S953575 119950830A5530 BLKHD BOEING727 727232 1384082NM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 CRACK INSIDE VERTICAL STABILIZER AT STA 1303 BULKHEAD LOWER RT CORNER, VENTRAL WALL ABOVE S-DUCT HAS CRACK. CRACK WAS FOUND AT HMV, REPAIRED BY INSTALLING DOUBLER PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950908002491995090800249NM 1995 9 8 DL72S953577 119950821A5720 ACT ATTACH BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 5 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LWR O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. CRACK WAS FOUND AT HMV. 2L73 4F A3WE 19950908002501995090800250NM 1995 9 8 DL72S953578 119950822A5720 ACT ATTACH BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 6 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. 2L73 4F A3WE 19950908002521995090800252NM 1995 9 8 DL72S953586 119950829A5713 STRINGER BOEING727 727232 1384082NM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 WING UPPER STRINGER TO RIB WS 686.5 STRINGER NR 5 IS CRACKED. STOP DRILLED CRACK PER M/M 57-13-0 PG 802. FABRICATED REPAIR PARTS AND INSTALLED PER M/M 57-13-00 PG 802. 2L73 4F A3WE 19950908002531995090800253NM 1995 9 8 DL72S953587 119950820A5713 STRINGER BOEING727 727232 1384082NM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 LEFT WING UPPER STRINGER TO RIB WS 629 STRINGER NR 3 CRACKED. FABRICATED AND INSTALLED PARTS PER M/M 57-13-00 FIG 804. CRACK WAS FOUND AT HMV. 2L73 4F A3WE 19950908002541995090800254NM 1995 9 8 DL72S953590 119950624A5753652163262 SPAR RAIL BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11489DA 21019 FASTENER ELONGATED ON LOWER SURFACE T/E SEAL RETAINER ATTACH ANGLE, LOWER AFT SPAR ANGLE. REPAIR DOUBLER CRACKED, APPROX 2 INCH CRACK IN AFT SPAR RAIL, 56 INCHES FROM I/B END OF FLAP. ALL THREE AREAS WERE REPAIRED BY REPLACING SPLICING IN NEW SPAR RAIL AS PER REF MM 57-52-0 FIG 802, FOR NR 3 MIDFLAP ASSEMBLY. FOUND DURING SHOP VISIT. 2L73 4F A3WE 19950908002551995090800255NM 1995 9 8 DL72W953562 119950824A532065175186 ANGLE BOEING727 727247 138408FNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11293WA 22111 DURING LETTER CHECK IN TPA, A CRACK WAS FOUND IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THE DAMAGED PARTS WERE REPLACED IN ACCORDANCE WITH S/B 727-53-0129 REV 4. 2L73 4F A3WE 19950908002561995090800256NM 1995 9 8 DL72W953580 119950901A5754 DOUBLER BOEING727 727247 138408FNM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 PREVIOUS DOUBLER REPAIR CRACKED BENEATH NR 7 L/E SLAT I/B DOWN STOP PAD. CRACK WAS FOUND AT F-1 LTR CHECK. REPLACED DOUBLER PER MM 57-54-0. 2L73 4F A3WE 19950908002571995090800257NM 1995 9 8 DL72W953581 119950901A3520 OXYGEN MASKS BOEING727 727247 138408FNM CABIN FAILED TEST A DALAK NONE L NO TEST ININSP/MAINT 1 SO11295WA 22532 REF OPER 6821 - DURING O/2 DROP CHECK, MASK PANELS DID NOT OPEN AT SEATS 2AB, 13ABC, AND 28DEF. FOUND AT F-1 LTR CHECK. REPLACED PSU PANELS, OPERATION NORMAL. 2L73 4F A3WE 19950908002581995090800258NM 1995 9 8 DL73S953559 119950823A5330654576972 SKIN BOEING737 737232 1384475NM BS 379 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11325DL 23097 DURING HMV IN ATL, THE SKIN LOCATED AT THE COOLING DUCT CUTOUT AT BS 379 BL 0, WAS FOUND CRACKED IN THE AFT EDGE OF THE CUTOUT. THE CRACK WILL BE REPAIRED IN ACCORDANCE WITH S/B 737-53-1117 REV 1. 2L72 4F RTA16WE 19950908002591995090800259WP 1995 9 8 DLL13953585 119950902A33505165741 EEL POWER SUPPLY LKHEED1011 10113851 5265010WP L4 DOOR INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11784DA 193A1038 L4 DOOR EMERGENCY LIGHT INOP. REPLACED EMER LIGHT BATT PACK, DAL P/N 337001090 SN NR 54051. 2L73 4F A23WE 19950908002601995090800260WP 1995 9 8 DLL17953558 119950830A33500L3071BPEGPL EEL BULB LKHEED1011 10113853 5265020WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11767DA 193H1209 EMERGENCY FLOOR TRACK LIGHTS WERE INOP AT SEATS 12C AND 32C. RELAMPED. ALSO, EMERGENCY FLOOR TRACK LIGHTS WERE INOP AT SEATS 12G AND 30G. REPLACED HOLDERS, BULBS AND MODULES. 2L73 4F A23WE 19950908002611995090800261NM 1995 9 8 DLM88953557 119950830A5320 RIB DOUG MD88 MD88 3023688NM KEEL BEAM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11916DE 53421 DURING B-2 LETTER CHECK, FOUND MLG W/W KEEL BEAM CROSSOVER RIB CRACKED. REPAIRED PER MM FIG 101. 2L72 4F RTA6WE 19950908002621995090800262NM 1995 9 8 DLM88953572 119950831A5320 FRAME DOUG MD88 MD88 3023688NM RT MLG CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11974DL 53242 A 3 INCH CRACK IN O/B FWD FRAME OF MLG DOOR CUTOUT. CRACK WASB FOUND AT E-1 LTR CKECK. REPAIRED PER SRM 53-05 FIG 78A. 2L72 4F RTA6WE 19950908002631995090800263NM 1995 9 8 DLM88953583 119950901A5400 ANGLE DOUG MD88 MD88 3023688NM NR 1 ENG PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11951DL 49882 A .75 INCH CRACK IN REPAIR ANGLE UPPER ATTACH ANGLE ON NR 1 ENG PYLON AT AFT END. CRACK WAS FOUND AT F-2 LTR CK. REPLACED ANGLE PER SRM 54-04A PG 17 FIG 4. 2L72 4F RTA6WE 19950908002641995090800264NM 1995 9 8 DLM88953584 119950902A5610 WINDSHIELD 5887275501 DOUG MD88 MD88 3023688NM CENTER SHATTERED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11928DL 92014H06686049715 CENTER WINDSHIELD SHATTERED INFLT, DIVERTED TO ATL. REPLACED WINDSHIELD, OPERATION NORMAL. 2L72 4F RTA6WE 19950908002651995090800265WP 1995 9 8 MWEA95284 119950905A5350 FAIRING DOUG DC9 DC914 3022034WP RT WING BENT A MWEAK NONE O OTHER UKUNKNOWN 1 GL31800ME 45842 PILOT REPORTS ON WALK-AROUND IN ATLANTA, THE RIGHT OUTBD MOVEABLE VANE TRACK FAIRING WAS BENT UPWARD. MAINTENANCE IN ATL REMOVED FAIRING, AIRCRAFT WAS FERRIED TO MKE. NEW FAIRING WAS INSTALLED, A/C RETURNED TO SERVICE. 2L72 4F A6WE 19950908002661995090800266WP 1995 9 8 SCNA95182 119950902A261172130000002 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP MID GALLEY FAILED A SCNAK NONE N FALSE WARNING UKUNKNOWN 1 GL15573SC 46905 SMOKE DETECTOR IN MID GALLEY CEILING WAS INTERMITTENTLY SOUNDING. REPLACED SMOKE DETECTOR WHICH WAS CAUSING ALARM SOUND, NEW DETECTOR OPS CHECKED GOOD PER MM 26-16-00. 2L73 4F A22WE 19950908002671995090800267WP 1995 9 8 9513659855 119950902A5350 LATCHES DOUG DC9 DC951 3022051WP TAILCONE REQ ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS; INADEQUATE FORCE WAS SUBSEQUENTLY REQUIRED TO DROP THE TAILCONE. ADJUSTED THE CLIPS AND LATCHES. CHECKED OK. 2L72 4F RTA6WE 19950908002681995090800268WP 1995 9 8 9513669852 119950905A5280591498551N DOOR DOUG DC9 DC951 3022051WP NLG DAMAGED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01761NC4851848518 47709 A LOUD BANG OCCURRED FROM NOSE LANDING GEAR AREA DURING GEAR RETRACTION AFTER TAKEOFF. RECYCLED GEAR WITH SAME RESULTS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND LEFT NOSE GEAR DOOR BRACKET BENT AND DAMAGE TO DOOR. REPLACED LEFT NOSE GEAR DOOR. RIGGED AND CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908002691995090800269WP 1995 9 8 9513679908 119950904A52805910161118N DOOR DOUG DC9 DC931 3022065WP RT MLG DAMAGED A NWAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL01958N 374648712 47254 ON APPROACH INTO BNA, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. GO-AROUND PROCEDURES FOR MISSED APPROACH WERE ACCOMPLISHED AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED. AIRCRAFT LANDED WITHOUT INCIDENT. RIGHT MAIN GEAR DOOR SKID PLATE WAS REPLACED AND AIRCRAFT FERRIED TO ATL. REPLACED RIGHT MAIN GEAR DOOR. RIGGED AND FUNCTIONALLY CHECKED BOTH LEFT AND RIGHT MAIN GEAR DOORS. ALL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908002701995090800270WP 1995 9 8 9513689929 119950902A2751 CIRCUIT BREAKER DOUG DC9 DC931 3022065WP LT INST TRNSFMR POPPED A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL018923E 45838 DURING APPROACH INTO DTW, FLAPS INDICATED AN ASYMMETRICAL CONDITION ON FLAP EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND ACCOMPLISHED AN UNEVENTFUL LANDING USING SLATS ONLY. FOUND LEFT INSTRUMENT TRANSFORMER CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER, CYCLED FLAPS SEVERAL TIMES AND ALL INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950908002711995090800271SO 1995 9 8 COM11958 119950905A315080055711 TO WARNING UNIT EMB 120 EMB120RT SO AVIONICS DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01463CA7853 120267 TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF, CIRCUIT BREAKER WAS TRIPPED. REPLACED THE AUDIO WARNING UNIT. 2L72 4T RTA31SO 19950908002721995090800272EU 1995 9 8 COMA31138 119950905A2910GP848430621 CONRTOL VLV SAAB SF340 SF340A 7850100EU NLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01359CA21927 340A053 HYDRAULIC FLUID LEAKING IN NOSE LANDING GEAR AREA. REPLACED THE LANDING GEAR CONTROL VALVE. 2L72 4T RTA52EU 19950908002731995090800273NM 1995 9 8 P5CA9500728 119950809A5753 FAIRING BOEING747 747122 1384872NM NR 1 FLAP PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 PUNCTURE IN NR 1 TRAILING EDGE FLAP MOVABLE FAIRING. FIBERGLASS REPAIR COMPLETED PER BOEING SRM 51-40-09 2L74 4F A20WE 19950908002741995090800274NM 1995 9 8 P5CA9500729 119950809A5755 TE SKIN BOEING747 747122 1384872NM NR 7 SPOILER DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATION AT LOWER TRAILING EDGE AREA OF NR 7 SPOILER. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950908002751995090800275NM 1995 9 8 P5CA9500730 119950809A5753 FAIRING BOEING747 747122 1384872NM NR 8 CANOE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATION OF NR 8 CANOE FAIRING AT BOTTOM. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950908002761995090800276NM 1995 9 8 P5CA9500731 119950809A5412 BULKHEAD BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 NR 3 PYLON BULKHEAD AT NACELLE STA 221 CRACKED AT OUTBOARD FORWARD AND AFT FACES. REPLACED BULKHEAD ANGLES AND STRAPS. 2L74 4F A20WE 19950908002771995090800277NM 1995 9 8 P5CA9500732 119950809A5320 PRESS DECK BOEING747 747122 1384872NM GEAR WHEEL WELL CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION ON PRESSURE DECK FLOOR ABOVE LANDING GEAR SELECTOR VALVE. REMOVED CORROSION, FOUND WITHIN LIMITS PER BOEING SRM 3-10-01, DOUBLER INSTALLED PER SRM 51-40-06. 2L74 4F A20WE 19950908002781995090800278NM 1995 9 8 P5CA9500733 119950809A5754 SKIN BOEING747 747122 1384872NM NR 16 LE FLAP CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACK ON NR 16 KRUEGER FLAP AFT SIDE OUTBOARD LOWER EDGE. REPAIRED PER BOEING SRM. 2L74 4F A20WE 19950908002791995090800279NM 1995 9 8 P5CA9500734 119950809A572065B12725103 SUPPORT BOEING747 747122 1384872NM WS 970 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 BROKEN SUPPORT LINK FOR RIGHT WING LOWER LEADING EDGE PANEL, AT LES 970. REPLACED LINK. 2L74 4F A20WE 19950908002801995090800280NM 1995 9 8 P5CA9500736 119950809A361065B902651 PRECOOLER BOEING747 747122 1384872NM NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 PRECOOLER COVER ON NR 3 ENGINE HAS CRACK 1 INCH, ALONG ITS LOWER CORNER. REPAIRED PER BOEING SRM. 2L74 4F A20WE 19950908002811995090800281NM 1995 9 8 P5CA9500737 119950809A5730 COVER PANEL BOEING747 747122 1384872NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED COVER PANEL AT OUTBOARD END OF INBOARD TRAILING EDGE FLAP COVER AREA. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950908002821995090800282NM 1995 9 8 P5CA9500738 119950809A5730 TE WEDGE BOEING747 747122 1384872NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATED FIBERGLASS TRAILING EDGE WEDGE SECTION OUTBOARD OF OUTBOARD TRAILING EDGE FLAP AND INBOARD OF NR 1 PYLON TRAILING EDGE FAIRING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950908002831995090800283NM 1995 9 8 P5CA9500739 119950809A5720 STIFFENER BOEING747 747122 1384872NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED INBOARD AILERON INBOARD SUPPORT RIB STIFFENER AT UPPER END. REPLACED FITTING PER BOEING SRM 51-40-00. 2L74 4F A20WE 19950908002841995090800284NM 1995 9 8 P5CA9500740 119950809A5320 T-CHORD BOEING747 747122 1384872NM BS 880 SHEARED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 SHEARED T-CHORD AT BS 880, BETWEEN MIDDLE 2 ROLLER TRACKS FORWARD CARGO COMPARTMENT. REPLACED T-CHORD AND STIFFENERS PER BOEING SRM 51-40-00. 2L74 4F A20WE 19950908002851995090800285 1995 9 8 PRCA9500735 419950809A34451267485SW PDU BOEING747 747122 1384872NM RT WING BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED MOUNT LUG NR 1 RIGHT LEADING EDGE PDU. REPLACED PDU PER BOEING MAINTENANCE MANUAL 27-81-03. 2L74 4F A20WE 19950908002861995090800286NM 1995 9 8 SWAA950613 119950906A5315 FLOOR BEAM BOEING737 7373H4 1384600NM E/E COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FLOOR BEAM CRACKED IN E/E COMPARTMENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANAUL. 2L72 4F RTA16WE 19950908002871995090800287NM 1995 9 8 SWAA950614 119950903A5313 STRINGER BOEING737 7372T4 1384492NM RT MLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.25 INCHES, RIGHT WHEELWELL. REPAIRED PER SWA ACO 640-53. 2L72 4F A16WE 19950908002881995090800288NM 1995 9 8 SWAA950615 119950903A5313 STRINGER BOEING737 7372T4 1384492NM AFT BLKHD CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07721WN 22697 DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.5 INCHES, AT AFT BULKHEAD. REPAIRED PER SWA ACO 640-53. 2L72 4F A16WE 19950908002891995090800289NM 1995 9 8 SWAA950616 119950904A3350 EEL BOEING737 7375H4 138449DNM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07507SW 24184 FOUND FLOOR TRACK LIGHTING TORN UP AT ROW 6 AND SEVERAL LIGHTS INOP. REPAIRED TRACK LIGHTING AND REPLACED LIGHTS PER BOEING M/M. 2L72 4F RTA16WE 19950908002901995090800290NE 1995 9 8 SWAA950617 219950904A7230 FAN BLADES BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE BENT A SWAAA UNSCHED LANDING C F.O.D. TOTAKEOFF 1 SW07394SW 27380 ON TAKEOFF, EXPERIENCED BIRDSTRIKE TO NR 2 ENGINE CAUSING VIBRATION. AIRCRAFT RETURNED TO SFO AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION AND FOUND TWO ENGINE FAN BLADES BENT. REPLACED BLADES AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F4 FRTA16WE E2GL 19950908002911995090800291NM 1995 9 8 SWAA950618 119950903A2781 SENSOR BOEING737 7372H4 138448CNM NR 1 LE FLAP INOP A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0790SW 22905 DURING CLIMB-OUT, NR 1 KRUGER FLAP TRANSIT LIGHT REMAINED ILLUMINATED. AIRCRAFT DIVERTED INTO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED NR 1 KRUGER FLAP POSITION SENSOR PER BOEING M/M. 2L72 4F A16WE 19950908002921995090800292NM 1995 9 8 SWAA950619 119950831A21307110033 OUTFLOW VLV BOEING737 7373H4 1384600NM CABIN MALFUNCTIONED A ASWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW07392SW 27379 AT 35,000 FEET, EXPERIENCED CABIN ALTITUDE ALERT WARNING. CREW WAS UNABLE TO CONTROL CABIN PRESSURE USING STANDBY OR MANUAL MODES. INITIATED EMERGENCY DESCENT TO 15,000 FEET WHERE CREW REGAINED CONTROL OF PRESSURE. AIRCRAFT MADE AN UNEVENTFUL LANDING AT SJC. INSPECTED AND PERFORMED PRESSURE CONTROL TEST WITH NO DEFECTS NOTED. REPLACED MAIN OUTFLOW VALVE, O/H PRESSURE CONTROL PANEL AND PRESSURE CONTROLLER PER BOEING M/M. 2L72 4F RTA16WE 19950908002931995090800293NM 1995 9 8 UPS203508 119950607A2913 HYD PUMP BOEING727 72721C 138400MNM 1/2 B HYD SYS MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION DEDESCENT 1 SO01934UP 19135 (SUPPLEMENTAL MRR) PILOT REPORTED THAT AT BEGINNING OF DESCENT WHEN THRUST LEVERS WERE BROUGHT TO IDLE, THE SYSTEM 'B' HYDRAULIC LIGHTS ON F/O PANEL ILLUMINATED. BOTH SYS 'B' PUMP LOW PRESS LIGHTS ON F/O PANEL ILLUMINATED AND SYSTEM QUANTITY DROPPED TO ZERO. LOSS OF SYSTEM 'B' CHECKLIST WAS ACCOMPLISHED AND EMERGENCY DECLARED. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED NR 2 SYSTEM 'B' ELECTRIC PUMP. REPLACED BR 1 SYSTEM 'B' PUMP, RAN BOTH PUMPS, OPS AND LEAK CK OK. 2L73 4F A3WE 19950908002941995090800294NM 1995 9 8 UPS204360 119950905A33501000679 EEL BOEING727 72722C 138400FNM CABIN MALFUNCTION A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01930UP 19096 WHILE ON GROUND AT CGN, MAINTENANCE FOUND DURING TESTING, LIGHTS GOING DIM RAPIDLY. MAINTENANCE REPLACED ASSY, F/C GOOD. 2L73 4F A3WE 19950908002951995090800295NM 1995 9 8 UPS40434 119950907A5311 FRAME BOEING747 747123 1384873NM BS 2040 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STR 29 AT BS 2040 LT CORRODED AT FRAME LOCATION. NO CORROSION FOUND IN STRINGER, BUT A CRACK ON FRAME WEB AT DESCRIBED LOCATION, DUE TO CORROSION. STOP-DRILLED CRACK AND REMOVED CORROSION ACC SRM 51-10-01 AND REPAIRED WEB ACC SRM 53-10-04, FIG 39. 2L74 4F A20WE 19950908002961995090800296NM 1995 9 8 UPS404362 119950907A5720 D-BEAM BOEING747 747123 1384873NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT WING WBL 470 D-BEAM CRACKED IN FRONT OF PYLON 3. D-BEAM REPAIRED ACC SRM 57-30-04. 2L74 4F A20WE 19950908002971995090800297NM 1995 9 8 UPS404363 119950907A5347 SEAT TRACK BOEING747 747123 1384873NM BS 2000-2060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2160 - BS 2000 RBL 98 WEB PANEL AND SEAT TRACK CORRODED. REPAIRED WEB PANEL IAW SRM 51-40-02, FIG 1. REPLACED SEAT TRACK IAW SRM 51-10-01. 2L74 4F A20WE 19950908002981995090800298NM 1995 9 8 UPS42810 119950329A3350 EEL BOEING747 747123F NM FLIGHT DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 (SUPPLEMENTAL MRR) MAINTENANCE REPORTED UPPER RT PASSENGER CABIN EMERGENCY LIGHT INOP. REPLACED EMER LIGHT. OPS CK GOOD. 2L74 4F A20WE 19950908002991995090800299WP 1995 9 8 UPS804361 119950905A3297 WIRE DOUG DC8 DC871F 302199DWP GEAR DOOR SWITCHSEPARATED A IPXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01797UP 45897 PILOT REPORTED AIR TURN BACK AS GEAR RETRACTION DOOR NOT LATCHED LIGHT REMAINED ILLUMINATED. FOLLOWED CHECK LIST. RECYCLED GEAR. NO HELP. FOUND WIRE 376D24 SEPARATED FROM TERMINAL STRIP S339, REPAIRED WIRE. DOOR WARNING LIGHT SYS. OPS CHECK NORMAL. ALSO, REPLACED DOOR WARNING LIGHT SWITCHES. 2L74 4F RT4A25 19950908003001995090800300NM 1995 9 8 95ZZZM362 119950804A323065461084 WALKING BEAM BOEING737 7373G7 1384595NM LT MLG WORN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 575 23782 LAS - FLT 131 - DURING CLIMB WITH GEAR HANDLE SELECTED UP, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED. CREW VERIFIED THE GEAR DID NOT RETRACT BY VISUAL INSPECTION. GEAR SELECTED DOWN WITH THREE GREEN SAFE LIGHTS ILLUMINATED. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING COMPLIED WITH. MAINTENANCE REPLACED TRUNNION PIN, WALKING BEAM, MLG ACTUATOR, MLG ARM ASSY, AND MLG UPLOCK ACTUATOR. NO DEFECTS NOTED ON RETRACTION TEST, LEAK CHECK AND OPERATIONAL CHECK. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA16WE 19950908003011995090800301NM 1995 9 8 95ZZZM363 119950804A323365491027 ACTUATOR BOEING737 7373G7 1384595NM LT MLG WORN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 1801953 23782 LAS - FLT 131 - DURING CLIMB WITH GEAR HANDLE SELECTED UP, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED. CREW VERIFIED THE GEAR DID NOT RETRACT BY VISUAL INSPECTION. GEAR SELECTED DOWN WITH THREE GREEN SAFE LIGHTS ILLUMINATED. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING COMPLIED WITH. MAINTENANCE REPLACED TRUNNION PIN, WALKING BEAM, MLG ACTUATOR, MLG ARM ASSY, AND MLG UPLOCK ACTUATOR. NO DEFECTS NOTED ON RETRACTION TEST, LEAK CHECK AND OPERATIONAL CHECK. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA16WE 19950908003021995090800302NM 1995 9 8 95ZZZM364 119950804A323065610912 ARM ASSY BOEING737 7373G7 1384595NM LT MLG WORN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 9010 23782 LAS - FLT 131 - DURING CLIMB WITH GEAR HANDLE SELECTED UP, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED. CREW VERIFIED THE GEAR DID NOT RETRACT BY VISUAL INSPECTION. GEAR SELECTED DOWN WITH THREE GREEN SAFE LIGHTS ILLUMINATED. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING COMPLIED WITH. MAINTENANCE REPLACED TRUNNION PIN, WALKING BEAM, MLG ACTUATOR, MLG ARM ASSY, AND MLG UPLOCK ACTUATOR. NO DEFECTS NOTED ON RETRACTION TEST, LEAK CHECK AND OPERATIONAL CHECK. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA16WE 19950908003031995090800303NM 1995 9 8 95ZZZM365 119950804A323065448106 UPLOCK ACTUATOR BOEING737 7373G7 1384595NM LT MLG WORN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW DA3085 23782 LAS - FLT 131 - DURING CLIMB WITH GEAR HANDLE SELECTED UP, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED. CREW VERIFIED THE GEAR DID NOT RETRACT BY VISUAL INSPECTION. GEAR SELECTED DOWN WITH THREE GREEN SAFE LIGHTS ILLUMINATED. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING COMPLIED WITH. MAINTENANCE REPLACED TRUNNION PIN, WALKING BEAM, MLG ACTUATOR, MLG ARM ASSY, AND MLG UPLOCK ACTUATOR. NO DEFECTS NOTED ON RETRACTION TEST, LEAK CHECK AND OPERATIONAL CHECK. AIRCRAFT RELEASED FOR SERVICE. 2L72 4F RTA16WE 19950908003041995090800304NE 1995 9 8 95ZZZM366 219950808A7200 ENGINE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE RIGHT OVERTEMP A AWXAO OTHER M OVER TEMP CLCLIMB 1 WP28509DC 23636 COS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED BOTH ENGINES. (M) 2L72 4F4 FRTA16WE E2GL 19950908003051995090800305NE 1995 9 8 95ZZZM367 219950810A7532ETPU100026 TPU BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 1 ENG FAILED A AWXAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 WP28902AW BX326228 23322 PHX-LAX - FLT NR 20 - CREW ABORTED TAKEOFF DUE TO HIGH EGT ON NR 1 ENGINE. OAT 101 DEGREES, EPR 1.66, EGT 852 DEGREES AND CLIMBING. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENG TRANSIENT PRESSURE UNIT (TPU) PER BMM 75-32-15. NO FAULTS NOTED. AS A PRECAUTIONARY MEASURE, THE NR 1 ENGINE EPR TRANSMITTER WAS ALSO REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF RECORD NR AWX9500516. 2L72 4F4 FRTA2NM E12EU 19950908003061995090800306NM 1995 9 8 95ZZZM368 119950802A2910 O-RING DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYS FAILED A SABAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 SO05883CC 162 FLT NR 5007 - EN ROUTE FROM CLT TO CVG ENCOUNTERED A NR 1 HYDRAULIC FAILURE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. THE AIRCRAFT LANDED UNEVENTFULLY AT CLT AND WAS TOWED BACK TO THE GATE AFTER ENGINE SHUTDOWN. MAINTENANCE PERSONNEL TROUBLESHOT THE SYSTEM AND FOUND A HYDRAULIC LEAK COMING FROM A CRUSHED O-RING ON A T-FITTING REDUCER ON A LINE GOING TO THE HYDRAULIC FILTER IN THE ELFT WHEEL WELL. MAINTENANCE REMOVED AND REPLACED THE O-RING AND SERVICED THE NR 1 HYDRAULIC SYSTEM AND THE SYSTEM LEAK CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950908003071995090800307WP 1995 9 8 95ZZZM369 119950715A2612 FIRE WARNING DOUG DC8 DC873F 302199FWP NR 4 ENG MALFUNCTIONED A SRAAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SO19874SJ 46149 AT TOP OF DESCENT INTO BOMBAY, NR 4 ENGINE WAS SHUTDOWN DUE TO FIRE WARNING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET RELAYS AND INSPECTED WIRING SYSTEM. OPS CHECKED GOOD ON GROUND. AT DEPARTURE, PROBLEM REOCCURRED, AIRCRAFT RETURNED TO BLOCK, SECURED NR 4 ENGINE LOWER FIRE LOOP AND WARNING INDICATION EXTINGUISHED. TROUBLESHOT SYSTEM AND UNABLE TO DUPLICATE PROBLEM. 2L74 4F RT4A25 19950908003081995090800308SO 1995 9 8 95ZZZM370 119950803A61206794188 ROD LKHEED382 382G 526414USO NR 1 ENG BROKEN A SRAAO OTHER O OTHER LDLANDING 1 SO19921SJ 4586 ON LANDING FOR FLIGHT 1973 AT AET, NR 1 PROPELLER FAILED TO REVERSE, LOW PITCH STOPS DID NOT RETRACT. FOUND INTERMEDIATE PROP CONTROL ROD BROKEN, REPLACED ROD AND PERFORMED OPS CHECK PER MM CHAP 76. 2H74 4T A1SO 19950908003091995090800309WP 1995 9 8 95ZZZM371 119950717A26128990992 FIRE LOOP DOUG DC8 DC873F 302199FWP NR 4 ENGINE SHORTED A SRAAO OTHER N FALSE WARNING DEDESCENT 1 SO19874SJ 46149 ON LANDING AT DUBAI, NR 4 ENGINE FIRE LIGHT AND BELL CAME ON. RESET CIRCUIT BREAKER BELL AND LIGHT STAYED ON AIRCRAFT. LANDED WITHOUT INCIDENTS. FOUND SHORT BETWEEN PIN V AND PIN P AT FIREWALL CANNON PLUG, ISOLATED PROBLEM TO AFT FIRE LOOP. REPLACED LOOP, SYSTEM OPS CHECKED GOOD. 2L74 4F RT4A25 19950908003101995090800310NM 1995 9 8 95ZZZM372 119950816A5320 ATTACH FINGER BOEING737 7372T4 1384492NM BS 1016 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, DISCOVERED EXFOLIATION CORROSION ON BS 1016 ATTACH FINGER AT STRINGER 17R. REPAIRED PER SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003111995090800311WP 1995 9 8 95ZZZM373 119950721A5730 SKIN DOUG DC8 DC862 3021970WP WS 70.9 LE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191803 45895 LEFT LEADING EDGE AFT LOWER SKIN CRACKED INBOARD OF NR 2 ENGINE PYLON AT WING STATION XS1 70.900 AT AFT ROW OF ATTACH FASTENERS, 1.5 INCH CRACK. STOP DRILLED CRACK, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED 5 INCH BY 7 INCH 7075-T6 .071 INCH DOUBLER IAW SRM 57-2-0. 2L74 4F 4A25 19950908003121995090800312NM 1995 9 8 95ZZZM374 119950804A3350 EEL BATT PACK BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19373US 22952 CLT - THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK. 2L72 4F RTA16WE 19950908003131995090800313WP 1995 9 8 95ZZZM375 119950812A3350 EEL DOUG DC9 DC932 3022066WP TAIL COMPT INOP A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11912VV 47359 AFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT. REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33. (M) 2L72 4F A6WE 19950908003171995090800317NM 1995 9 8 AWXA9500492 119950804A3211654611312 TRUNNION PIN BOEING737 7373G7 1384595NM LT MLG WORN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28160AW 450 23782 LAS - FLT 131 - DURING CLIMB WITH GEAR HANDLE SELECTED UP, LT MAIN GEAR UNSAFE LIGHT ILLUMINATED. CREW VERIFIED THE GEAR DID NOT RETRACT BY VISUAL INSPECTION. GEAR SELECTED DOWN WITH THREE GREEN SAFE LIGHTS ILLUMINATED. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. OVERWEIGHT LANDING COMPLIED WITH. MAINTENANCE REPLACED TRUNNION PIN, WALKING BEAM, MLG ACTUATOR, MLG ARM ASSY, AND MLG UPLOCK ACTUATOR. NO DEFECTS NOTED ON RETRACTION TEST, LEAK CHECK AND OPERATIONAL CHECK. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RTA16WE 19950908003181995090800318NE 1995 9 8 AWXA9500505 219950805A7230537131 FAN INLET CASE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PHX - DURING SCHEDULED C-15 INSPECTION, FOUND NR 2 ENGINE IGV CASE CRACKED AT WELD AT 1:00 TO 3:00 POSITION AND 11:00 POSITION. WELDED CRACK PER ER 2-72-23-02B. (M) 2L72 4F4 FRTA16WE E2EA 19950908003191995090800319NM 1995 9 8 AWXA9500514 119950805A78105553598 EXHAUST STRUTS BOEING737 737277 1384570NM NR 1 ENGINE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 PXH - DURING SCHEDULED C-15 INSPECTION, FOUND NR 1 ENGINE EXHAUST STRUTS (4 EACH) CRACKED AT LEADING EDGES. WELDED CRACKS PER PWA ENGINE MANUAL 72-54-02, REPAIR NR 03. (M) 2L72 4F RTA16WE 19950908003201995090800320NE 1995 9 8 AWXA9500515 219950808A7200 ENGINE BOEING737 73733A 1384673NM GE CFM56 CFM563B1 13802NE LEFT OVERTEMP A AWXAO OTHER M OVER TEMP CLCLIMB 1 WP28509DC 23636 COS - DURING CLIMB, CREW REPORTED BOTH ENGINES EXCEEDED ALLOWABLE EGT LIMITS, E1 GOING TO 980 DEGREES AND E2 TO 960 DEGREES. CREW CONTINUED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED AND REPLACED BOTH ENGINES. (M) 2L72 4F4 FRTA16WE E2GL 19950908003211995090800321NM 1995 9 8 AWXA9500516 119950810A77117898301 EPR TRANSMITTER BOEING757 7572S7 1384962NM NR 1 ENG MALFUNCTIONED A AWXAC ABORTED TAKEOFF M OVER TEMP TOTAKEOFF 1 WP28902AW 83082039 23322 PHX-LAX - FLT NR 20 - CREW ABORTED TAKEOFF DUE TO HIGH EGT ON NR 1 ENGINE. OAT 101 DEGREES, EPR 1.66, EGT 852 DEGREES AND CLIMBING. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENG TRANSIENT PRESSURE UNIT (TPU) PER BMM 75-32-15. NO FAULTS NOTED. AS A PRECAUTIONARY MEASURE, THE NR 1 ENGINE EPR TRANSMITTER WAS ALSO REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19950908003221995090800322NM 1995 9 8 AWXA9500517 119950808A3350900835A EEL POWER SUPPLY BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE IN FWD CABIN. REMOVED AND REPLACED POWER SUPPLY AT FWD CABIN POSITION. OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950908003231995090800323NM 1995 9 8 AWXA9500518 119950808A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH 21. RESECURED WIRING AT ROWS 17 AND 19. SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003241995090800324NM 1995 9 8 AWXA9500520 119950808A3350 EEL WIRING BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT TRACK LIGHTING INOPERATIVE AT ROWS 7, 8, 22 AND 23. RESECURED BROKEN WIRES AT NUMEROUS ROWS. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003251995090800325NM 1995 9 8 AWXA9500521 119950809A3350 EEL CONNECTOR BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE FROM ROW 18 TO ROW 21. RESECURED LOOSE CONNECTOR, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003261995090800326NM 1995 9 8 AWXA9500522 119950809A3350 EEL WIRING BOEING737 73733A 1384673NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE AFT OF ROW 13. RESECURED WIRE AT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003271995090800327NE 1995 9 8 AWXA9500523 219950812A73208062530 FFG BOEING757 7572S7 1384962NM RROYCERB211 RB211535E4 54555NE NR 1 ENG FAILED A AWXAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 WP28902AW 1999013 23322 PHX - FLT 696 - AT ROTATION, THE NR 1 ENGINE EGT WENT TO 878 DEGREES. CREW RETARDED THRUST LEVER TO KEEP EGT BELOW RED LINE. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENG FFG. LEAK AND OPERATION CHECKS NORMAL. AIRCRAFT RELEASED FOR FURTHER SERVICE. (M) 2L72 4F4 FRTA2NM E12EU 19950908003281995090800328SW 1995 9 8 BDHA9500017 119950705A26125708A WIRE SWRNGNSA226 SA226TC 8780404SW LT ENGINE FAILED A BDHAK NONE L NO TEST ININSP/MAINT 1 GL15328BA TC253 FSD - FLT 434 - CREW REPORTED THE LEFT ENGINE FIRE WARNING LIGHT WOULD NOT TEST ON PREFLIGHT. THE SYSTEM WAS INSPECTED AND THE WIRE TO THE ENGINE OIL COOLER DUCT FIRE DETECTOR WAS OPEN. THE WIRE WAS REPAIRED AND THE SYSTEM OPERATED NORMAL. THE AIRCRAFT WAS RELEASED. (M) 2L72 4T RTA8SW 19950908003291995090800329NM 1995 9 8 F3LA95015 119950731A3241 ANTI-SKID CONTL BOEING737 737201 1384454NM LT MLG FAILED A F3LAO OTHER O OTHER LDLANDING 1 NM03217US 20215 BZN - UPON LANDING, FLIGHT CREW REPORTED LOSS OF LEFT MAIN LANDING GEAR BRAKES. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM AND PERFORMED AN OPERATIONAL CHECK. SYSTEM CHECKED OK. A FAULT WAS FOUND ON THE ANTI-SKID MODULE TEST AND THE LEFT OUTBOARD ANTI-SKID BRAKE SYSTEM WAS PLACARDED PER MEL 32-2. S/D MAINTENANCE REPLACED THE ANTI-SKID CONTROL UNIT ON THE LEFT OUTBOARD ANTI-SKID BRAKE AND SYSTEM CHECKED OK. (M) 2L72 4F A16WE 19950908003301995090800330NM 1995 9 8 IXKA9500024 119950805A323069181941 ACT FITTING BOEING727 727251 138408HNM NLG SHEARED A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25264US 19983 AFTER TAKEOFF, FLT NR 58, ATL TO PBI, UNABLE TO RAISE NOSE LANDING GEAR. RETURNED TO ATLANTA. UPON INSPECTION OF NOSE WHEEL WELL, FOUND NOSE LANDING ACTUATOR FITTING SHEARED. REMOVED AND REPLACED NLG LOCK ACTUATOR FITTING AND REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR. PERFORMED GEAR SWING AND OPS CHECK PER MM 32-33-0 AND MM 32-33-11. (M) 2L73 4F A3WE 19950908003311995090800331EU 1995 9 8 REXA95049 119950802A33501317 EEL SAAB SF340 SF340A 7850100EU CABIN INOP A REXAK NONE L NO TEST TXTAXI/GRND HDL 1 SO25406BH 340A074 EMERGENCY OVERHEAD LIGHT INOP 2A. REMOVED AND REPLACED EMERGENCY OVERHEAD LIGHT, OPS CHECK GOOD. (M) 2L72 4T RTA52EU 19950908003321995090800332NM 1995 9 8 TSAA9555159 119950816A5510 BEAM BOEING737 7372T4 1384492NM LT HORIZ STAB TECORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 145. REPAIRED PER ECD 1584R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003331995090800333NM 1995 9 8 TSAA9555160 119950816A5510 BEAM BOEING737 7372T4 1384492NM LT HORIZ STAB TECORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 176.64. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003341995090800334NM 1995 9 8 TSAA9555161 119950816A5510 BEAM BOEING737 7372T4 1384492NM LT HORIZ STAB TECORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE EXFOLIATION CORROSION NOTED AT ES 149.12. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003351995090800335NM 1995 9 8 TSAA9555162 119950816A5510 BEAM BOEING737 7372T4 1384492NM LT HOR STAB TE CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM UPPER SURFACE FILIFORM CORROSION NOTED AT ES 94.07. REPAIRED PER ECO 1584R3. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003361995090800336NM 1995 9 8 TSAA9557164 119950816A5730 SKIN BOEING737 7372T4 1384492NM RT WING CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13808AL 23445 DURING HEAVY MAINTENANCE VISIT, RT WING LOWER EXTERIOR SURFACE EXFOLIATION CORROSION NOTED JUST AFT OF NR 6 SLAT TELESCOPING DUCT. REPAIRED EPR ECO 1684R6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950908003371995090800337NM 1995 9 8 USAA950843 119950804A3350RPS1B EEL BATT CHARGER BOEING737 7373B7 1384580NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19373US 22952 CLT - THE AFT EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PACK. (M) 2L72 4F RTA16WE 19950908003381995090800338WP 1995 9 8 WRLA95040 119950803A2830AV16B1926C FUEL DUMP VALVE DOUG DC10 DC1030 3023501WP LT/RT FAILED A WRLAA UNSCHED LANDING O OTHER CRCRUISE 1 EA272FOR 47956 WHILE EN ROUTE TO SBCF, A PASSENGER SUFFERED A MEDICAL EMERGENCY. CAPTAIN ELECTED TO DUMP FUEL AND DIVERT TO SAN JUAN BUT NEITHER DUMP VALVE WOULD OPEN DURING BEGINNING OF DESCENT. CREW PERFORMED TROUBLESHOOTING PROCEDURES BUT STILL UNSUCCESSFUL IN DUMPING FUEL. CAPTAIN ELECTED TO RETURN TO MIAMI. ARRIVED MIAMI WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REMOVED AND REPLACED BOTH DUMP VALVES. OPS CHECK PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F A22WE 19950908003401995090800340NM 1995 9 8 95ZZZM380 119950823A3230 RETRACT MECH BOEING727 727259 138408JNM NLG LACK OF LUBE A UHVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17203AV 22474 FLT NR DKYC9318, AFTER TAKEOFF FROM KMIA THE NOSE LANDING GEAR P/N 65163424 WOULD NOT RETRACT. CYCLED GEAR SEVERAL TIMES, NO HELP. AIRCRAFT RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. LUBRICATED NOSE GEAR. JACKED AIRCRAFT AND CYCLED GEAR NUMEROUS TIMES PER MM 32-33-0. OPERATIONALLY CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 19950908003411995090800341WP 1995 9 8 95ZZZM381 119950810A335058531 EEL CABLE DOUG DC9 DC934 302207EWP CABIN FAILED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05936L 47711 STL - DURING CRUISE, EGRESS LIGHTS, FROM SEAT ROW 8 TO ROW 14, CAME ON. CYCLED EMERGENCY LIGHT SWITCH TO OFF, TO ARMED, EXTINGUISHED LIGHTS. FOUND OPEN FEEDER CABLE, MFG P/N 5853-1. REPLACED FEEDER CABLE AND LIGHT OPERATION CHECKED NORMAL. (M) 2L72 4F RTA6WE 19950908003421995090800342NM 1995 9 8 95ZZZM382 119950816A2150 DUCT BOEING727 727231 1384079NM CABIN LOOSE A TWAAO OTHER O OTHER CLCLIMB 1 CE0554325 20232 STL - AFTER TAKEOFF SMOKE WAS REPORTED EXITING SIDEWALL SEAT ROWS 10 AND 11, RIGHT SIDE. VISUALLY CHECKED AREA. REMOVED SIDEWALL AND FOUND THREE INCH AIR CONDITIONING DUCT CONNECTOR LOOSE CAUSING CONDENSATION TO EXIT DUCT. REINSTALLED DUCT CONNECTOR. OPERATED AIR CONDITIONING SYSTEM AND ALL CHECKED NORMAL. (M) 2L73 4F A3WE 19950908003431995090800343WP 1995 9 8 95ZZZM383 119950717A793042D1091A FILTER BYPASS SW DOUG DC9 DC983 3022083WP NR 2 ENGINE FAILED A TWAAO OTHER N FALSE WARNING CRCRUISE 1 CE052FOR 49575 MCI - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO OIL FILTER BYPASS LIGHT CAME ON. REPLACED OIL FILTER AND OIL FILTER BYPASS SWITCH, MFG P/N 42D109-1A. ENGINE OPERATION CHECKED NORMAL. 2L72 4F RTA6WE 19950908003441995090800344NM 1995 9 8 95ZZZM384 119950820A3230656021117 ACCESSORY UNIT BOEING727 727231 1384079NM LANDING GEAR FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0552310 19829 STL - AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT MOVE TO LANDING GEAR UP POSITION. USED LANDING GEAR OVERRIDE PROCEDURES TO RETRACT LANDING GEAR. FOUND LANDING GEAR ACCESSORY UNIT, MFG P/N 65-60211-17, WITH INTERNAL MALFUNCTION. REPLACED LANDING GEAR ACCESSORY UNIT. LANDING GEAR OPERATION CHECKED NORMAL. (M) 2L73 4F A3WE 19950908003451995090800345NE 1995 9 8 95ZZZM385 219950813A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE NR 2 FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 CE05932L 47669 2119 DFW - DURING DESCENT SHUT DOWN NR 2 ENGINE, DUE TO HIGH OIL TEMPERATURE AND LOW OIL QUANTITY. FOUND ENGINE HAD INTERNAL OIL LEAK. REPLACED NR 2 ENGINE. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME 49,375, TOTAL CYCLES 54,671. 2L72 4F4 F A6WE E2EA 19950908003461995090800346NM 1995 9 8 95ZZZM386 119950727A278210617921 ACTUATOR BOEING727 727259 138408JNM NR 1 SLAT LEAKING A UHVAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO17203AV 22474 FLT NR XKYC202 - SVMC-KMIA - HYDRAULIC SYSTEM 'A' FAILURE EN ROUTE. ABNORMAL CHECKLIST USED. FLUID LEVEL INCREASED UPON NORMAL GEAR EXTENSION. LANDED AND TAXIED TO GATE UNDER OWN POWER. UPON MAINTENANCE INSPECTION FOUND NR 1 SLAT ACTUATOR LEAKING AT RETRACT SWIVEL. REPLACED SLAT ACTUATOR SWIVEL SEALS, BOTH NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS AND FILTERS. SERVICED AND BLED HYDRAULIC SYSTEMS. LEAK CHECK OK. JACKED AIRCRAFT, CYCLED LANDING GEAR SEVERAL TIMES. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 19950908003471995090800347 1995 9 8 BUFA9516 419950731A34525222703013 XPONDER COLLINS DOUG DC8 DC862 3021970WP NR 1/2 INOP A BUFAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 CE05924BV 45920 FLT NR BVA924 - MIA-IAH - ATC XPONDER'S 1 AND 2 AND MODE C INOP. RETURNED TO MIA. REMOVED AND REPLACED ATCRT BOTH SYSTEMS, S/N 6615 AND 2860, OP CHECKED WITH ATTACHED TEST BOX IAW 34-42-00. (M) 2L74 4F 4A25 19950908003481995090800348WP 1995 9 8 BUFA9717 119950802A5245 DOOR DOUG DC8 DC861 3021952WP AIR COND COMPT NOT CLOSED A BUFAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE05915BV 45981 FLT MRX793 - SBKP-SPIM - UNABLE TO PRESSURIZE AIRCRAFT, RETURNED TO SBKP. FOUND AIRCRAFT AIR COND DOOR OPEN. OPS CHECKED DOOR AND CLOSED DOOR IAW MM 52-00. (M) 2L74 4F 4A25 19950908003591995090800359EU 1995 9 8 M3HA95015 119950811A24301030032 SENSOR AUXILEC AEROSPATR42 ATR42320 8680930EU NR 2 DC GEN WET A M3HAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP13983MA1693 8466241 308 HNL - FLT NR 702 - NR 2 DC GENERATOR FAILED DURING CLIMB-OUT. REPLACED SENSOR, HALL EFFECT. (M) 2H72 4T RTA53EU 19950908003601995090800360NM 1995 9 8 P2EA95005 119950727A5320 BEAM BOEING737 737222 1384473NM BS 227.8 CORROSION A P2EAK NONE O OTHER ININSP/MAINT 1 CE05209US 19548 FLT NR 119 - MCI - DURING NOSE WHEEL WELL INSPECTION PER EO 953753A010, MAINTENANCE FOUND CORROSION ABOVE NOSE WHEEL WELL APPROXIMATLEY STATION 227.8. MAINTENANCE REMOVED AND REPLACED STRUCTURAL BEAM. LEVEL 2 REPORT WILL BE FILED WITH BOEING AND FAA WILL ALSO BE COPIED. (M) 2L72 4F A16WE 19950908003611995090800361EU 1995 9 8 REXA95051 119950811A32325ENI6N95 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU NLG BROKEN A REXAO OTHER J WARNING INDICATION CLCLIMB 1 SO25300PX 652 LANDING GEAR WILL NOT RETRACT. REPAIRED BROKEN WIRES ON NOSE OLEO SWITCH AND RESET PIN ON RELEASE VALVE. PERFORMED GEAR SWINGS. OPS CHECK GOOD. (M) 2L72 4T RTA21EU 19950908003621995090800362EU 1995 9 8 SIMA952331 119950821A2710S2711008800020 CRANK BEARING AEROSPATR42 ATR42300 8680920EU LT AILERON LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21242AT 242 MQT - DURING MAINTENANCE INSPECTION, THE LEFT WING AILERON CRANK ASSEMBLY WAS FOUND TO HAVE A LOOSE BEARING. MAINTENANCE REMOVED AND REPLACED THE CRANK ASSEMBLY. SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950908003631995090800363EU 1995 9 8 SIMA952332 119950821A2720S272819600000 CONTROL ROD AEROSPATR42 ATR42300 8680920EU RUDDER CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21242AT 242 MQT - DURING MAINTENANCE INSPECTION, THE RUDDER TRIM CONTROL ROD WAS FOUND TO BE CORRODED INTERNALLY. MAINTENANCE REMOVED AND REPLACED ROD, SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950908003641995090800364EU 1995 9 8 SIMA952341 119950822A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU COMPT MALFUNCTIONED A SIMACDF ABORTED TAKEOFF RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TOTAKEOFF 1 SW21301AE A2987 340B301 SGF - FLT NR 4186 - DURING TAKEOFF ROLL, THE AFT SMOKE DETECTOR LIGHT ILLUMINATED, THE TAKEOFF WAS ABORTED AND THE AFT CARGO FIRE BOTTLE WAS DISCHARGED. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF HEAT OR FIRE, REPLACED AFT SMOKE DETECTOR AND FIRE BOTTLE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950908003651995090800365NE 1995 9 8 TWRA9548 219950814A7250 TURBINE BOEING747 747130 1384880NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE FAILED A ATWRAE ENGINE SHUTDOWN TA ENGINE CASE PENETRATION FLAME/FIRE CLCLIMB 1 EA15603FF 19746 685854 EXPERIENCED SEVERE VIBRATION CLIMBING THROUGH 14,000 FEET. ACCOMPLISHED THE ENGINE FIRE SEVERE DAMAGE OR SEPARATION CHECKLIST 2.21.1 NR 1 ENGINE. FOUND NR 1 ENGINE WITH LPT FAILURE. REMOVED ENGINE, S/N 685854, INSTALLED S/N 6857837 PER WIC 71-002. THIS IS AN UNCONTAINED TURBINE FAILURE. (M) 2L74 4F4 F A20WE E20EA 19950908003661995090800366NM 1995 9 8 TWRA9550 119950726A217025TD47 COALESCER BAG BOEING747 747130 1384880NM FLIGHT DECK DIRTY A TWRAG O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15603FF 19746 DURING CRUISE, FLIGHT CREW EXPERIENCED FUEL FUMES IN THE COCKPIT THROUGH OUT THE FLIGHT. OXYGEN WAS USED INTERMITTENTLY. UPON LANDING MAINTENANCE INSPECTED THE AIRCRAFT AND NO LEAKS WERE NOTED. FOLLOWING REPLACEMENT OF THE COALESCER FILTERS, THE ITEM WAS CLEARED. (M) 2L74 4F A20WE 19950908003671995090800367NM 1995 9 8 USAA50784 119950802A2750 RETRACT MECH BOEING757 757225 1384959NM TE FLAPS OUT OF ADJUST A USAAO OTHER J WARNING INDICATION DEDESCENT 1 EA19609AU 22205 DCA - FLT 0450 - THE CREW HAD DECLARED AN EMERGENCY DUE TO A FLAP ASYMMETRY PROBLEM. MAINTENANCE RESET THE TRIP INDICATORS ON THE LEFT AND RIGHT FLAP TORQUE TUBE ACTUATORS. THE FLAPS WERE CYCLED. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA2NM 19950908003681995090800368WP 1995 9 8 USAA950772 119950725A21505910244125 DUCT DOUG DC9 DC931 3022065WP RT PACK BLOWN A USAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 EA19941VJ 47054 LGA - FLT NR 0329 - DURING CLIMB, FLIGHT EXPERIENCED A RAPID DECOMPRESSION. AN EMERGENCY WAS DECLARED AND A DESCENT WAS MADE TO 10,000 FEET. CABIN PRESSURE DID NOT RAISE ABOVE 14,000 FEET PRE-EMPTING THE OXYGEN MASKS TO DEPLOY. THE FLIGHT DIVERTED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE DUCT ASSEMBLY ON THE RIGHT PACK. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950908003691995090800369NM 1995 9 8 USAA950844 119950718A5320 DOUBLER BOEING737 737301 1384611NM BS 794 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL AREAS OF CORROSION APPROXIMATELY 2 INCHES IN DIAMETER BS 794 S-22 R TO S-24 R INNER DOOR FRAME DOUBLER. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. FABRICATED NEW DOUBLER AND INSTALLED SAME. REPAIRED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19950908003701995090800370NM 1995 9 8 USAA950845 119950719A5320 ANGLE BOEING737 737301 1384611NM BS 807 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 4 INCH ATTACH ANGLE CORRODED, BS 807 RBL 17.5. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. FABRICATED NEW ANGLE AND INSTALLED, REPAIRED PER DRAWING 65-46551. (M) 2L72 4F RTA16WE 19950908003711995090800371NM 1995 9 8 USAA950846 119950801A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 985.6 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 12 INCH AND .5 INCH BY 14 INCH CORROSION, BS 985.6 AT LBL 43 INCHES - RBL 30 INCHES ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED T-CAP ON FLOOR BEAM, REPAIRED PER TR 53-10-05. (M) 2L72 4F RTA16WE 19950908003721995090800372NM 1995 9 8 USAA950850 119950718A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US2704327043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DIAMETER CORROSION, STATION 967 LBL 6, ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REMOVED DAMAGED FLOOR BEAM CAP AND SPLICED IN LOCAL MFGD CAP AND SPLICED ANGLES AND DOUBLERS. REPAIR PER SRM 53-00-51. (M) 2L72 4F RTA16WE 19950908003731995090800373WP 1995 9 8 Y2PA950011 119950712A571299574651 RIB DOUG DC9 DC915F 3022037WP LT WING BROKEN A Y2PAK NONE O OTHER ININSP/MAINT 1 GL23194US63189 47016 YIP - DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS NOTED THAT THE LEFT WING OUTBOARD SPOILER SUPPORT UPPER RIB ASSEMBLY WAS BROKEN, AND A SECTION OF THE RIB WAS MISSING. REMOVED AND REPLACED RIB ASSEMBLY. NEW RIB WAS PROCURED PRE-DRILLED AND THE HOLES DID NOT ALIGN WITH EXISTING STRUCTURE. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED PER USA JET AIRLINES, INC ENGINEERING AUTHORIZATION NR 95-57-01. THIS DATA WAS DESIGNED AND DER APPROVED BY FLIGHT VEHICLES INC ENGINEERING AUTHORIZATION NR 95-53-9549, AND ASSOCIATED FAA FORM 8110-3. (M) 2L72 4F A6WE 19950908003751995090800375NM 1995 9 8 AWXA9500529 119950811A2133392268631 REGULATOR BOEING737 737277 1384570NM NR 1 ENG INOPERATIVE A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28189AW P823 22656 CMH - FLT 407 - ON CLIMB, CREW REPORTED THE NR 1 ENGINE BLEED WENT TO 90 PSI AND THE LEFT PACK SHUT DOWN. DUE TO APU BEING INOPERATIVE, CREW RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATOR. LEAK AND OPERATIONAL CHECK NORMAL. AIRCRAFT RELEASED FOR FURTHER SERVICE. (M) 2L72 4F RTA16WE 19950908003761995090800376NM 1995 9 8 AWXA9500531 119950815A2613 LOOP CONNECTOR BOEING737 737277 1384570NM AFT PRESS BLKHD SHORTED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28184AW 22651 PHX - FLT 15 - ON CLIMB-OUT OF PHX, THE LT WING TO BODY OVERHEAT LIGHT ILLUMINATED. CREW CLOSED THE LT ENGINE BLEED WITH NO CHANGE. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER INCIDENT. NO OVER WEIGHT LANDING WAS REQUIRED. MX REPAIRED SHORT AT LOOP CONNECTOR AFT OF PRESSURE BULKHEAD. OPS CHECK OK. REMOVED AND REPLACED APU LOAD CONTROL VALVE P/N 10948661, PER MM CHAPTER 49. (M) 2L72 4F RTA16WE 19950908003771995090800377NM 1995 9 8 AWXA9500535 119950810A5315 FLOOR BEAM BOEING737 7372U9 1384498NM BS 294.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW 22575 PHD - DURING SCHEDULED C-10 INSPECTION, FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 294.5 RBL 13 TO RBL 53. REMOVED AND REPLACED T-CAP AT STATION 294.5 IAW SRM 51-30-02. (M) 2L72 4F RTA16WE 19950908003781995090800378NM 1995 9 8 AWXA9500536 119950810A5315 FLOOR BEAM BOEING737 7372U9 1384498NM BS 328 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW 22575 PHX - DURING SCHEDULED C-10 INSPECTION, FOUND DEEP CUTS IN FLOOR BEAM UPPER SURFACE OF UPPER CHORD, BS 328 RBL 24 TO RBL 44. REPAIRED FLOOR BEAM T-CAP AT STATION 328 IAW SRM 51-40-4. (M) 2L72 4F RTA16WE 19950908003791995090800379NM 1995 9 8 AWXA9500537 119950810A5315 FLOOR BEAM BOEING737 7372U9 1384498NM BS 344 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW 22575 PHX - DURING SCHEDULED C-10 INSPECTION, FOUND CRACK IN FLOOR BEAM UPPER CHORD AT FASTENER HOLE, BS 344 LBL 8. REPAIRED FLOOR BEAM IAW SRM 53-10-7. (M) 2L72 4F RTA16WE 19950908003801995090800380NM 1995 9 8 AWXA9500538 119950810A5320 THRESHOLD BOEING737 7372U9 1384498NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28149AW 22575 PHX - DURING SCHEDULED C-10 INSPECTION, FOUND L1 DOOR THRESHOLD CHORD CORRODED. REMOVED AND REPLACED THRESHOLD CHORD IAW SRM 51-10-1 AND SRM 51-30-2. (M) 2L72 4F RTA16WE 19950908003811995090800381NM 1995 9 8 AWXA9500550 119950815A3350900835A EEL BATT PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT EMERGENCY EXIT LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL. (M) 2L72 4F A16WE 19950908003821995090800382NM 1995 9 8 AWXA9500551 119950815A3350 EEL PINS BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE IN AFT SECTION OF AIRCRAFT. RECONNECTED PINS OF LIGHT ASSEMBLY AT ROW 20, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003831995090800383NM 1995 9 8 AWXA9500552 119950815A3350 EEL WIRING BOEING757 7572G7 1384963NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 28 THROUGH ROW 35. REINSTALLED TRACK LIGHTING WIRES AS REQUIRED. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950908003841995090800384NM 1995 9 8 AWXA9500554 119950816A3350 EEL BATT PACK BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT MID SECTION EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT R2 DOOR. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950908003851995090800385NM 1995 9 8 AWXA9500555 119950816A335020131A EEL BATT PACK BOEING757 7572S7 1384962NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28901AW 23321 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R3 DOOR EXTERIOR AND MIDDLE EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950908003861995090800386NM 1995 9 8 AWXA9500556 119950816A335020131A EEL BATT PACK BOEING757 7572S7 1384962NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28905AW 23567 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT L4 DOOR AND AFT LT AISLE. REMOVED AND REPLACED AFT LT BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950908003871995090800387NM 1995 9 8 AWXA9500557 119950817A3350 EEL WIRING BOEING737 7373S3 1384711NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 THROUGH ROW 20. RECONNECTED WIRING IN TWO PLACES. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950908003881995090800388EU 1995 9 8 AWXA9500558 119950818A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, EMERGENCY EXIT LIGHT SYSTEM FAILED TEST. REMOVED AND REPLACED FORWARD LEFT BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950908003891995090800389NM 1995 9 8 CAL950665 119950726A5320 T-ANGLE BOEING727 727243 138408DNM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09579PE41584 21662 STATION 31J - INSPECTION FOUND CORROSION ON T-ANGLE AT BS 500, STRINGER 26R. A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2L73 4F RTA3WE 19950908003901995090800390NM 1995 9 8 CAL950666 119950730A5753652165127 FITTING BOEING727 727243 138408DNM LT TE FLAP CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09579PE41584 21662 THE LEFT INBOARD FLAP TRACK FORWARD SUPPORT FITTING WAS FOUND CORRODED IN THE INBOARD RADIUS FOR THE TRUNNION PIN. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW MM 27-51-31. (M) 2L73 4F RTA3WE 19950908003911995090800391NM 1995 9 8 CAL950667 119950726A5330 SKIN BOEING727 727243 138408DNM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09579PE41584 21662 STATION 31J - INSPECTION FOUND A 1 INCH CRACK IN THE LEFT FORWARD FUSELAGE SKIN AT THE FORWARD END OF THE L-1 DOOR LOWER HINGE CUTOUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M) 2L73 4F RTA3WE 19950908003921995090800392NM 1995 9 8 CAL950669 119950727A5315 FLOORBEAM BOEING727 727243 138408DNM BS 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09579PE41584 21662 STATION 31J - THE AFT PIT WAS FOUND CORRODED ON THE BOTTOM OF THE CABIN FLOORBEAM AT BS 1130, LBL 60 TO RBL 60. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PRIMED. A STRAP WAS FABRICATED AND INSTALLED IAW ECRA 5710-01675, REV IR AND AERO CORP ENGINEERING 95-180, REV IR. (M) 2L73 4F RTA3WE 19950908003931995090800393WP 1995 9 8 CAL950705 119950815A29107936913685 HYD LINE DOUG DC9 DC982 3022082WP RT HYD SYSTEM LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0935888 49117 FLT NR 0317 - DCA - THE RIGHT HYDRAULIC QUANTITY DECREASED 4 QUARTS WHILE IN FLIGHT FROM EWR TO DCA. MAINTENANCE FOUND THE HYDRAULIC BRAKE PRESSURE LINE IN THE RT WHEEL WELL LEAKING. THE LINE WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. SYSTEM LEAK CHECKS WERE GOOD. (M) 2L72 4F A6WE 19950908003941995090800394WP 1995 9 8 CAL950706 119950808A5350 CLIPS DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0916806 49260 HOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT 45 POUNDS. THE HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. (M) 2L72 4F A6WE 19950908003951995090800395WP 1995 9 8 CAL950707 119950803A55435910257503 SKIN DOUG DC9 DC982 3022082WP RUDDER TAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - DURING INSPECTION, FOUND THREE DENTS ON RIGHT SIDE OF RUDDER TAB. THE DENTS WERE REPAIRED PER SRM 55-04 AND 55-40-1. (M) 2L72 4F A6WE 19950908003961995090800396WP 1995 9 8 CAL950708 119950806A57545922500509 SKIN DOUG DC9 DC982 3022082WP NR 1 LE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - DURING INSPECTION, FOUND A 3 INCH CRACK IN NR 1 SLAT SKIN ON THE LOWER SIDE. THE SLAT WAS REPAIRED IAW ECRA 5750-02346. (M) 2L72 4F A6WE 19950908003971995090800397WP 1995 9 8 CAL950709 119950803A5330 SKIN DOUG DC9 DC982 3022082WP BS 207-256 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - DURING INSPECTION, FOUND SEVERAL DENTS IN SKIN AT STATION 207 TO 256, LONGERONS 15, 16, AND 17. THE DENTS WERE REPAIRED IAW ECRA 5330-02309. (M) 2L72 4F A6WE 19950908003981995090800398WP 1995 9 8 CAL950710 119950803A57539936837503 TE PANEL DOUG DC9 DC982 3022082WP NR 1 TE FLAP DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - INSPECTION FOUND THE LOWER TRAILING EDGE PANEL DELAMINATED JUST OUTBOARD OF NR 1 FLAP HINGE. THE PANEL WAS REPAIRED PER SRM 51-90-0. (M) 2L72 4F A6WE 19950908003991995090800399WP 1995 9 8 CAL950711 119950803A5311 BELTFRAME DOUG DC9 DC982 3022082WP BS 636 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - INSPECTION FOUND CORROSION ON BELTFRAME IN AFT CARGO BIN AT STATION 636. THE BELTFRAME WAS REPAIRED BY REMOVING CORROSION IAW SRM 53-01, FIGURE 1. (M) 2L72 4F A6WE 19950908004001995090800400WP 1995 9 8 CAL950712 119950802A55435955545503 TE SKIN DOUG DC9 DC982 3022082WP RUDDER TAB DELAMINATED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - INSPECTION FOUND THE UPPER TRAILING EDGE OF RUDDER TAB DELAMINATED THE RUDDER TAB WAS REPAIRED IAW SRM 55-04. (M) 2L72 4F A6WE 19950908004011995090800401WP 1995 9 8 CAL950713 119950803A5311 BELTFRAME DOUG DC9 DC982 3022082WP BS 598 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680630477 49260 HOU - INSPECTION FOUND CORROSION ON BELTFRAME IN MID CARGO BIN AT STATION 598. THE BELTFRAME WAS REPAIRED BY REMOVING CORROSION IAW SRM 53-01, FIGURE 1. (M) 2L72 4F A6WE 19950908004021995090800402WP 1995 9 8 CAL950715 119950809A5320 DOUBLER DOUG DC9 DC932 3022066WP BS 639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A 3 INCH CRACK IN DOUBLER AT STATION 639R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 12. (M) 2L72 4F A6WE 19950908004031995090800403WP 1995 9 8 CAL950716 119950813A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568176 47111 IAH - DURING INSPECTION, FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD AIRSTAIR DOOR CUTOUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 57A. (M) 2L72 4F A6WE 19950908004041995090800404WP 1995 9 8 CAL950717 119950813A5320 BEAM DOUG DC9 DC932 3022066WP BS 160-200 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568176 47111 IAH - DURING INSPECTION, FOUND CORROSION ON LONGITUDINAL BEAM AT FORWARD AIRSTAIR CUTOUT BETWEEN STATION 160 AND 200. THE LONGITUDINAL BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-00. (M) 2L72 4F A6WE 19950908004051995090800405NM 1995 9 8 USAA950763 119950719A5610571762315 WINDOW BOEING727 727247 138408FNM COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19749US 21393 LGA - FLT 0599 - THE CAPTAINS SLIDING WINDOW CRACKED. CAPTAIN TURNED OFF THE WINDSHIELD HEAT AND RETURNED TO LGA. MAINTENANCE REPLACED THE CAPTAINS SLIDING WINDOW. OPERATIONS CHECKED GOOD. (M) 2L73 4F A3WE 19950908004061995090800406NE 1995 9 8 USAA950771 219950725A7200 ENGINE DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE NR 1 FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19814US 48094 708513 ATL - FLT 1194 - THE CREW RECEIVED AN EXCESSIVE FUEL FLOW INDICATION ON THE LEFT ENGINE. A PASSING AIRCRAFT NOTICED AND EXCESSIVE CONTRAIL OUT OF THE LEFT ENGINE. CREW SHUTDOWN THE LEFT ENGINE. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE ASSY. OPERATIONS CHECKED GOOD. (M) 2L72 4F4 F A6WE E9NE 19950908004071995090800407WP 1995 9 8 USAA950773 119950721A2560 SLIDE DOUG DC9 DC981 3022081WP TAIL CONE MALFUNCTIONED A USAAK NONE O OTHER ININSP/MAINT 1 EA19802US 48036 DCA - WHILE INSPECTING THE TAIL AREA FOR FUEL FUMES, THE TAILCONE WAS INADVERTENTLY DEPLOYED. THE TAIL SLIDE DID NOT DEPLOY. THE SLIDE WAS RERIGGED WITH THE TAIL CONE LANYARD TO DETERMINE THE REASON FOR THE SLIDE NOT DEPLOYING. MAINTENANCE RERIGGED THE SLIDE THEN RECHECKED IT FOR PROPER INSTALLATION. (M) 2L72 4F A6WE 19950908004081995090800408NE 1995 9 8 USAA950781 219950727A7200 ENGINE BOEING727 727214 138407RNM PWA JT8 JT8D15 52051NE NR 1 FAILED A USAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 EA19754US 21958 PHL - FLT NR 1876 - AT 4000 FEET, THE AIRCRAFT LOST OIL PRESSURE AND QUANTITY FOR THE NR 1 ENGINE. THE ENGINE WAS SHUTDOWN AND AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NR 1 ENGINE. OPERATIONS CHECKED GOOD. (M) 2L73 4F4 F A3WE E2EA 19950908004091995090800409EU 1995 9 8 USAA950782 119950802A2130 PRESSURIZATION FOKKERF28 F28MK4000 4990810EU CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19496US 11169 CLT - FLT 0741 - RETURN TO CLT DUE TO THE AIRCRAFT NOT ABLE TO BE PRESSURIZED. MAINTENANCE PRESSURE CHECKED THE CABIN AND CHECKED THE MANUAL AND AUTO CONTROLLER. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA20EU 19950908004101995090800410WP 1995 9 8 USAA950783 119950802A2120 AIR DISTR DOUG DC9 DC981 3022081WP CABIN ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19803US 48035 CLT - FLT NR 0207 - THE FLIGHT ATTENDANT REPORTED SMELLING SMOKE AND FUMES IN THE CABIN. THE CREW ELECTED TO DIVERT TO CLT. MAINTENANCE CHECKED ALL OVERHEAD PANEL LIGHTS, BALLASTS AND OXYGEN. RAN ENGINE AND APU AT POWER. MX CHECKED THE ACM OILS, TAIL COMPARTMENT, GALLEY AREA, FORWARD/AFT FEEDER CABLES AND E/E COMPARTMENT AFT BAG BIN AREA. NO FAULTS FOUND. (M) 2L72 4F A6WE 19950908004111995090800411NM 1995 9 8 USAA950847 119950706A53206546812186 INTERCOSTAL BOEING737 737301 1384611NM BS 958 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CORROSION AROUND NUT PLATES (TOTAL APPROXIMATELY .25 INCH BY 6 INCHES), BS 958 RBL 8 INCHES. CORROSION TASK NR C51-107-02, CORROSION LEVEL 2. REMOVED INTERCOSTAL AND INSTALLED NEW, REPAIRED PER SRM 51-10-02. (M) 2L72 4F RTA16WE 19950908004121995090800412NM 1995 9 8 USAA950848 119950711A53206546812186 INTERCOSTAL BOEING737 737301 1384611NM BS 989 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUT PLATE HOLES, LOWER SIDE INTERCOSTAL BS 989 RBL 17. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-30-02. (M) 2L72 4F RTA16WE 19950908004131995090800413NM 1995 9 8 USAA950849 119950713A53206546812185 INTERCOSTAL BOEING737 737301 1384611NM BS 996-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19338US27043 23234 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUT PLATE HOLES, BS 996-BS 1006 LBL 13. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. REMOVED AND REPLACED INTERCOSTAL BS 986-BS 1006. REPAIRED PER SRM 51-10-2 AND SRM 51-40-2. (M) 2L72 4F RTA16WE 19950915000011995091500001WP 1995 9 15 REXA95044 219950711A732189737519 FUEL CONTROL BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RT ENGINE FAILED A REXAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 SO25658BA3701 658 P42069C POWER CONTROL FOR RIGHT ENGINE WAS UNCONTROLLABLE. WITH ANY LITTLE MOVEMENT OF THE POWER LEVER, THE TORQUE WOULD FLUCTUATE UP TO 90 PERCENT TORQUE TO EITHER SIDE. REMOVED AND REPLACED RIGHT FCU IAW GMM AND PERFORMED GROUND RUNS. OK FOR SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19950915000121995091500012WP 1995 9 15 9513699994 119950831A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018978E 47327 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE FORWARD CARGO DOOR LOWER FITTINGS, FORWARD AND AFT. REPLACED FITTINGS PER SRM 51-30-2. 2L72 4F A6WE 19950915000131995091500013WP 1995 9 15 9513709953 119950831A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FRAME AND FITTING LOCATED IN THE UPPER FORWARD ACCESS NR 1. REPLACED THE FITTING. 2L72 4F A6WE 19950915000141995091500014WP 1995 9 15 9513719604 119950902A5343 FITTING DOUG DC9 DC932 3022066WP MLG ACTUATOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION TO THE LEFT MAIN LANDING GEAR RETRACT SUPPORT FITTING. REPLACED FITTING PER CITEXT 90-3211-1-9902. 2L72 4F A6WE 19950915000151995091500015WP 1995 9 15 9513729604 119950903A5320 FITTING DOUG DC9 DC932 3022066WP FS 700 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FITTING LOCATED AT FS 700 IN THE RIGHT MAIN LANDING GEAR WHEEL WELL. REPLACED FITTING PER SRM 51-10-03. 2L72 4F A6WE 19950915000161995091500016WP 1995 9 15 9513739603 119950903A5320 FITTING DOUG DC9 DC932 3022066WP FS 851 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FRAME TO FLOORBEAM LOWER ATTACH FITTING, FS 851. REPLACED FITTING PER SRM 51-10-3. 2L72 4F A6WE 19950915000171995091500017NM 1995 9 15 9513742284 119950825A5330 PANELS BOEING727 727251 138408HNM FUSELAGE MISSING A NWAAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 GL01284US 21323 EXPERIENCED VIBRATION DURING THE FLIGHT FROM PHL-DTW, ESPECIALLY IN THE MID CABIN. CONTINUED TO DTW WITHOUT FURTHER INCIDENT. FOUND THAT PANEL NR 3351 WAS MISSING, THE ROTATING BEACON AND SEVERAL ADDITIONAL PANELS WERE DAMAGED. REPLACED AND REPAIRED THE PANELS AND ROTATING BEACON. 2L73 4F A3WE 19950915000181995091500018NM 1995 9 15 95FDEA01261 119950906A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 480-600 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 WL 208.5 BL 0, REF FEDEX SRM 53-10-5. 2L73 4F A3WE 19950915000191995091500019NM 1995 9 15 95FDEA01262 119950906A53209086044 CLIP BOEING727 727232 1384082NM BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP, IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950915000201995091500020NM 1995 9 15 95FDEA01263 119950906A53117075T6050 FRAME BOEING727 727232 1384082NM BS 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950915000211995091500021NM 1995 9 15 95FDEA01264 119950906A53117075T6071 FRAME BOEING727 727232 1384082NM BS 720 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950915000221995091500022NM 1995 9 15 95FDEA01265 119950908A55302024T3050 WEB BOEING727 727232 1384082NM VERTICAL STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 1303 WEB IN BAY NR 1 AT VERTICAL FIN IS CRACKED LT LOWER CORNER. REPAIRED CRACK AT 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015. 2L73 4F A3WE 19950915000231995091500023NM 1995 9 15 95FDEA01266 119950908A532069436951 SKIN SUPPORT BOEING727 727232 1384082NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FOUND CORROSION WHILE WORKING NR O858 FUSELAGE 00117 SKIN SUPPORT (P/N 69-43695-1), OF BS 740 WL 145 TO 150 BETWEEN STR 28 AND 27L. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 51-10-1, 53-10-1. 2L73 4F A3WE 19950915000241995091500024NM 1995 9 15 95FDEA01267 119950908A53117075T6003 FRAME BOEING727 727232 1384082NM BS 720 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD, FRAME DENTED AND GOUGED ON TOP BS 720C AT STR 23 TO 24R. GOUGE FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME AT BS 720C STR 23 TO 24R, PER SRM 51-40-3. 2L73 4F A3WE 19950915000251995091500025NM 1995 9 15 95FDEA01268 119950908A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 344-480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN SEAT TRACK AT BS 344 TO 480 WL 208.5 BL 0. REMOVED CORROSION FROM SEAT TRACK BS 347 TO 415 BL 0 AND IT WAS FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. ALODINE AND PRIMED SEAT TRACK BS 347 TO 415 BL 0. ACCOMPLISHED SEAT TRACK REPAIR FROM BS 450 TO 480 IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950915000261995091500026NM 1995 9 15 95FDEA01269 119950908A53302024T3050 SKIN BOEING727 727232 1384082NM BS 420 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 WHILE WORKING CARD NR 7-3520-7-3313A PT 2, COCKPIT 00017. REMOVED STR 20R FOR OXYGEN MOD AND FOUND CORROSION ON SKIN AT BS 420 UNDER STR 20R, OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED DAMAGED SKIN PER FEDEX SRM 53-10-3 FIG 4. 2L73 4F A3WE 19950915000271995091500027EU 1995 9 15 95FDEA01270 119950908A2910 O-RING AIRBUS310 A310200 3930310EU GREEN HYD SYST FAILED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25413FE 512 WRI 29-10-287 ON DEPARTURE FROM SJC, GREEN SYSTEM HYDRAULIC QUANTITY WAS LOST. REPLACED O-RING ON GREEN SYSTEM HIGH PRESSURE MANIFOLD, RESERVICED HYD SYS PER MM 12-12-28, OK FOR SERVICE. 2L72 4F RTA35EU 19950915000281995091500028NM 1995 9 15 95FDEA01271 119950907A5347BAC1520841 SEAT TRACK BOEING727 72722 1384002NM BS 760-850 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 CORRODED SEAT TRACK AND FASTENERS AT STA 760 TO 850 LBL 25. REMOVED AND REPLACED SEAT TRACK. ALL WORK DONE IAW FEDEX SRM 53-10-1 AND FEDEX MM 53-20-12. 2L73 4F A3WE 19950915000291995091500029NM 1995 9 15 95FDEA01272 119950907A53207075T6 STIFFENER BOEING727 72722 1384002NM BS 312 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 GOUGE IN FLOORBEAM VERTICAL STIFFENER STA 312 RBL 52 WL 207. REMOVED AND FABRICATED FLOORBEAM VERTICAL STIFFENER. ALL WORK DONE IAW FEDEX SRM 53-20-1. 2L73 4F A3WE 19950915000301995091500030NM 1995 9 15 95UAL900030 119950703A2400BACC18AC15 CIRCUIT BREAKER BOEING777 777222 1385219NM PWA PW4077PW4077 NE P110 PANEL DAMAGED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP29767UA 26918 A/C RETURNED TO FIELD WITH LEFT ENGINE EEC AND BLEED PROBLEMS. REPLACED CIRCUIT BREAKER AND WIRE. PER BOEING ANALYSIS THE SCREW HOLDING THE WIRES IN THE CIRCUIT BREAKER WAS CROSS THREADED AND WAS NOT HOLDING THE WIRES SECURE. 2L72 4F4 FRTT0001SE E46NE 19950915000311995091500031NM 1995 9 15 95UAL900118 119950907A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297284U 21562 AFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19950915000321995091500032NM 1995 9 15 95UAL900119 119950908A2910 FITTING BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE A HYD SYST LOOSE A UALAO OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 WP29918UA 25385 LANDED UNDER AMBER ALERT DUE TO A-SYSTEM HYDRAULIC QUANTITY LOW. FOUND NR 1 ENGINE HYDRAULIC PUMP OUTLET FITTING LOOSE. REPLACED O-RING ON FITTING AND TIGHTENED FITTING. CHECKED AND REPLACED CASE DRAIN AND PRESSURE FILTERS. RAN ENGINE NO LEAKS FOUND. 2L72 4F4 FRTA16WE E2GL 19950915000331995091500033WP 1995 9 15 95UAL900120 119950908A7933 GROUND WIRE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 ENGINE CONTAMINATED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP291858U 46987 HKG - AN UNPLANNED STOP WAS MADE AFTER SHUTTING DOWN NR 3 ENGINE, DUE TO HIGH OIL TEMPERATURE. REPLACED WIRE E553B18N, BAD GROUND AND CORRECTED HYD LEAK. FLUID CONTAMINATED THE GROUND BRACKET WHICH CAUSED INTERMITTENT GROUND. INSTALLED WIRE AND BRACKET PER MM. 2L73 4F4 F A22WE E23EA 19950915000341995091500034NM 1995 9 15 95UAL900121 119950908A33501317 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29533UA 25073 EMERGENCY ESCAPE PATH LIGHTING INOP ROW NR 16. RELAMPED, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950915000351995091500035WP 1995 9 15 ABXA9500687 119950907A32607000010101 SWITCH DOUG DC9 DC932 3022066WP LT MLG DEFECTIVE A ABXAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL23903AX 47427 LEFT GEAR UNSAFE LIGHT INOP DURING RETRACTION AND EXTENTION. TESTED OK, RECYCLED GEAR AND PROBLEM REMAINED. REPLACED DOWNLOCK SWITCH ON LEFT GEAR. POSITION AND WARNING SYSTEM OPS CHECKED GOOD IAW DC-9 MM 32-60-00. PIN RETENTION POOR ON PINS 5 AND 7 OF PLUG P1-130. REPLACED PINS 5 AND 7 ON PLUG PER WDM 32-61-00, OPS CHECK WAS GOOD. 2L72 4F A6WE 19950915000361995091500036NM 1995 9 15 DL72K953620 119950905A53306572743 SKIN BOEING727 727232 1384082NM BS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 THE SKIN BETWEEN S-28 LT AND S-28 RT AT STA 720 WAS FOUND TO BE CORRODED. THE DAMAGE WAS REMOVED AND A DOUBLER WAS INSTALLED PER DL ERA 302443-14AD. 2L73 4F A3WE 19950915000371995091500037NM 1995 9 15 DL72K953627 119950901A532065175176 VERT STIFFENER BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 DURING CV-2 IN TPA, THE RT TORQUE BOX VERTICAL STIFFENER ANGLE AT STA 1263 WAS FOUND CRACKED. THE VERTICAL STIFFENER ANGLE WAS REPLACED IN ACCORDANCE WITH S/B 727-53-0129 REV 4. 2L73 4F A3WE 19950915000381995091500038NM 1995 9 15 DL72K953629 119950829A5522 SKIN BOEING727 727232 1384082NM RT ELEVATOR DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11410DA 21222 FOUND ON CV2 CHECK, SEVERAL DENTS AND GOUGES AT TOP SIDE OF RT ELEVATOR O/B END. REPAIRED PER SRM 55-20-3 FIG 4, O/B DENT ONLY. THE I/B DENTS WITHIN LIMITS PER SRM 55-20-1. 2L73 4F A3WE 19950915000391995091500039NM 1995 9 15 DL72L953596 119950904A5630PA6556705AR WINDOW BOEING727 727232 1384082NM LT EMER EXIT BROKEN A DALAK NONE D INFLIGHT SEPARATION CRCRUISE 1 SO11505DA 21307 PREFLIGHT CHECK, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT HATCH WINDOW OUTER PANE BROKEN. REPLACED WITH SERVICEABLE DOOR FOR RETURN TO SERVICE. SDR UNDER INVESTIGATION. 2L73 4F A3WE 19950915000401995091500040NM 1995 9 15 DL72S953568 119950831A35304566M37B PBE MASK BOEING727 727232 1384082NM CABIN DEFECTIVE A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO11522DA 21582 DURING PREFLIGHT, FWD CABIN PBE WAS FOUND PARTIALLY OPEN. REPLACED PBE ASSEMBLY. 2L73 4F A3WE 19950915000411995091500041NM 1995 9 15 DL72S953602 119950903A5754 SKIN BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816. 2L73 4F A3WE 19950915000421995091500042NM 1995 9 15 DL72S953607 119950905A3350334102486 EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11519DA 21470 DURING LAYOVER, RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK, OPS CKS NORMAL. 2L73 4F A3WE 19950915000431995091500043NM 1995 9 15 DL72S953609 119950819A5210 FRAME BOEING727 727232 1384082NM L2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV, FOUND L2 DR FRAME CRACKED IN LWR RADIUS OF UPPER HINGE CUTOUT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 52-40-2. 2L73 4F A3WE 19950915000441995091500044NM 1995 9 15 DL72S953610 119950820A5754 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND NR 4 SLAT RIB CRACKED .5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814. 2L73 4F A3WE 19950915000451995091500045NM 1995 9 15 DL72S953614 119950905A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 FOUND ON A-1 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950915000461995091500046NM 1995 9 15 DL72S953615 119950904A3221651767631 TRUNNION BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11519DA 21470 DURING LTR CHECK, FOUND NOSE GEAR LEFT AFT TRUNNION BOLT BORE CORRODED. OPENED HOLE TO .9385, HFEC CK OK. REAMED HOLE PER M/M 53-40-0, MACHINED BUSHINGS TO SIZE AND TREATED. TREATED, PAINTED BOLT BORES AND INSTALLED BUSHINGS PER M/M 53-40-0. 2L73 4F A3WE 19950915000471995091500047NM 1995 9 15 DL72S953626 119950901A5311 FRAME BOEING727 727232 1384082NM BS 784 MISDRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 WHILE ACCOMPLISHING EO 4-61904-3AD AT HMV IN ATL, 2 OVERSIZED HOLES WERE DISCOVERED IN THE RT OVERWING EXIT FRAME AT STA 784. THE DOUBLER WAS MODIFIED TO REMOVE THE TWO HOLES FROM THE MODIFICATION, IN ACCORDANCE WITH BACO TWX DAL-ATL-95-0883RR DTD 8-31-95. 2L73 4F A3WE 19950915000481995091500048NM 1995 9 15 DL72S953628 119950706A5330 SKIN BOEING727 727232 1384082NM BS 259.5-294.5 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11522DA 21582 DURING A LAYOVER IN CMH, THE SKIN FROM FS 259.5 TO 294.5 WAS DENTED FROM CONTACT WITH A SERVICE TRUCK. THE PERMANENT REPAIR WILL BE INSTALLED IN ACCORDANCE WITH B727 SRM 53-10-4, FRAME STA 278, 53-10-3 FIG 2, STR 20R, 53-10-4 FIG 11, FRAME 294, 53-30-3 FIG 24, SKIN. 2L73 4F A3WE 19950915000491995091500049NM 1995 9 15 DL72S953634 119950301A5751 SKIN 652176633 BOEING727 727232 1384082NM LT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11418DA 246 21271 FASTENERS PULLED THROUGH SKIN AT 2ND TAB HINGE FITTING FROM INBRD, UPPER SKIN OF LEFT OUTBOARD AILERON. REPAIRED DURING SHOP VISIT`PER SRM 57-50-5 FIG 3. 2L73 4F A3WE 19950915000501995091500050NM 1995 9 15 DL72S953637 119950820A5754 SKIN BOEING727 727232 1384082NM NR 6 SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820. 2L73 4F A3WE 19950915000511995091500051NM 1995 9 15 DL72S953638 119950819A5754 SKIN BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND NR 5 SLAT RIVET MISSING IN LWR T/E SKIN O/B OF O/B TRACK. SKIN WORN AT FENCE ATTACHMENT AND WORN THIN AT BOLT HOLE ON LWR T/E SKIN. REF NR CARD 1148, BURNISHED WORN AREA. DIE PENETRANT INSP SHOWS CRACK AT 3 FENCE ATTACH HOLES. FABRICATED AND DRILLED DOUBLER PER MM 57-54-0. 2L73 4F A3WE 19950915000521995091500052NM 1995 9 15 DL72S953639 119950821A5754 SKIN BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0. 2L73 4F A3WE 19950915000531995091500053NM 1995 9 15 DL72W953600 119950904A2150 VALVE 39854021 BOEING727 727247 138408FNM RT PACK STUCK A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11291WA P3564 22109 A/C UNABLE TO MAINTAIN PRESSURIZATION CLIMBING THROUGH FLT LEVEL 300. DESCENDED TO FLT LEVEL 190, FOUND RT PACK INOP. OFF LANDED IN ABQ DUE TO NOT ENOUGH FUEL TO REACH DFW AT FTL LEVEL 190. FOUND RT PACK VALVE STUCK IN CLOSED POSITION. REPLACE VALVE, OPERATION NORMAL. 2L73 4F A3WE 19950915000541995091500054NM 1995 9 15 DL73S953594 119950904A3350BPS73 EEL POWER SUPPLY BOEING737 737232 1384475NM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11307DL 23079 DURING LAYOVER, L-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY OPERATION NORMAL. 2L72 4F RTA16WE 19950915000551995091500055NM 1995 9 15 DL73S953595 119950904A523010608211 SEAL BOEING737 737232 1384475NM CARGO DOOR FAILED A DALAB EMER. DESCENT O OTHER CRCRUISE 1 SO11309DL 23081 FL 330 CABIN STARTED CLIMBING 2,000 FPM, EMERGENCY DESCENT TO 10,000 FT. FOUND FWD CARGO DOOR SEAL BLOWN OUT. REPLACED SEAL RETURNED TO SERVICE. 2L72 4F RTA16WE 19950915000561995091500056NM 1995 9 15 DL73S953625 119950622A5330 SKIN BOEING737 737232 1384475NM R-1 DOORWAY CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11311DL 23083 DURING A LETTER CHECK IN TPA, A CRACK WAS FOUND IN THE R-1 DOORWAY IN THE LOWER AFT CORNER APPROXIMATELY 1.4 INCH LENGTH. THE CRACK WILL BE REPAIRED IN ACCORDANCE WITH B737-200 SRM 53-30-3 FIGURE 26. 2L72 4F RTA16WE 19950915000571995091500057NM 1995 9 15 DL757953567 119950831A2612 PRESS SWITCH S453T201T BOEING757 757232 1384965NM CARGO COMPT FAILED A DALAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO11603DL 05340F1 22810 DURING PUSHBACK, NR 1 BTL CARGO FIRE EXT DISCHARGE WAS ILLUMINATED. DURING TOW INTO GATE NR 2 BTL DISCHARGE ILLUMINATED AND WAS ACCOMPANIED WITH CARGO BTL 1 AND CARGO BTL 2 EICAS MESSAGE. REPLACED NR 1 CARGO FIRE EXT BOTTLE AND FOUND PRESSURE SWITCH FAULTY. 2L72 4F RTA2NM 19950915000581995091500058NM 1995 9 15 DL757953603 119950830A5414 SKIN BOEING757 757232 1384965NM RT PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11616DL 22823 DURING HMV, FOUND NR 2 PYLON SKIN CRACKED ON OUTBD SIDE, JUST AFT OF NAC STA 107.70. REPAIRED PER SRM 54-51-01 PG 206 TO 210. 2L72 4F RTA2NM 19950915000591995091500059NM 1995 9 15 DL757953617 119950906A5754114N4005178A TE WEDGE BOEING757 757232 1384965NM NR 7 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11658DL 24420 UPON INSPECTION, HAIL DAMAGE WAS FOUND TO THE T/E WEDGE. NEEDED TO C/W AD 90-23-06. REPAIRED BOTH ITEMS PER SRM 57-43-02 FIG 202, FOR NR 7 L/E SLAT PANEL. 2L72 4F RTA2NM 19950915000601995091500060NM 1995 9 15 DL76S953605 119950904A3350767 EEL BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11130DL 24080 DURING LAYOVER, RIGHT AND LEFT AFT ESCAPE SLIDE LIGHT OUT. RELAMPED, LIGHT CHECKS GOOD. 2L72 4F RTA1NM 19950915000611995091500061WP 1995 9 15 DLL10953593 119950903A3350BPS73 EEL BATTERY PACK LKHEED1011 10113851 5265010WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11716DA 193C1095 DURING LAYOVER, FOUND EMERGENCY BATTERY PACK AT C-2 DOOR POPS BREAKER. REPLACED EMERGENCY LIGHT BATTERY PACK AT L-2 DOOR, OPERATION NORMAL. 2L73 4F A23WE 19950915000621995091500062WP 1995 9 15 DLL10953597 119950830A5330 SKIN LKHEED1011 10113851 5265010WP BS 600 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11729DA 193C1180 THE FUSELAGE SKIN WAS FOUND DENTED DURING LINE INSPECTION BETWEEN STA 589 AND 609, STRINGERS 26 AND 27. THE DENT IS AUTHORIZED FOR SERVICE UNTIL DTA LIMITS HAS BEEN MET. THEN A PERMANENT REPAIR WILL BE INSTALLED, PER DL ERA 267421-14 REV B. 2L73 4F A23WE 19950915000631995091500063WP 1995 9 15 DLL10953598 119950830A53131550247 LONGERON LKHEED1011 10113851 5265010WP BS 983 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11729DA 193C1180 THE SUBJECT AIRCRAFT WAS FOUND WITH DAMAGE TO THE LOWER RT SIDE OF THE STA 983 BULKHEAD. THE ATTACHED FUSELAGE TO WING LONGERON WAS FOUND COMPLETELY SEVERED. FURTHER INSPECTION FOUND CRACKS IN THE ADJACENT SKIN. LONGERON WILL BE REPLACED AND THE SKIN WILL BE REPAIRED PER DL ERA 271648-14 REV B. 2L73 4F A23WE 19950915000641995091500064WP 1995 9 15 DLL10953604 119950902A335020121 EEL POWER SUPPLY LKHEED1011 10113851 5265010WP L-2 DOOR FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11716DA 193C1095 LOG - EMERGENCY EXIT OVERHEAD AISLE LIGHT, LEFT SIDE B/C FWD LIGHT INOP. POPS BREAKER CB-3 ON BATTERY PACK PWR SUPPLY AT L-2 DOOR. REPLACED FLOOR TRACK BATTERY POWER SUPPLY, CKS OK. 2L73 4F A23WE 19950915000651995091500065WP 1995 9 15 DLL10953611 119950904A5320 FLOOR SUPPORT LKHEED1011 10113851 5265010WP FS 295 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11715DA 193C1092 ATL - DURING LTR CK, FLOOR SUPPORT CRACKED FS 295 RBL 40 CORRODED. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 51-10-05. 2L73 4F A23WE 19950915000661995091500066WP 1995 9 15 DLL10953618 119950905A53201554952102 STRINGER SPLICE LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT P-DOME STR SPLICE FITTING PER SI 7-66332-12 AND VA 30620, STRINGER 10 FITTING WAS FOUND TO BE CRACKED. THE SUBJECT FITTING WILL BE RELEASED ON A TIME LIMITED BASIS AND REPAIRED BY REPLACING WITH A SERVICEABLE PART, WITHIN 150 FLIGHT CYCLES OF ISSUANCE. 2L73 4F A23WE 19950915000671995091500067WP 1995 9 15 DLL10953619 119950905A5313154947101 STRINGER SPLICE LKHEED1011 10113851 5265010WP FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTING PER SI 7- 66332-12 AT STR 58 FITTING, WAS FOUND TO BE CRACKED. THE FITTING WILL BE RELEASED ON A TIME LIMITED BASIS AND REPLACED WITHIN 150 FLIGHT CYCLES FROM DATE OF ISSUANCE. 2L73 4F A23WE 19950915000681995091500068WP 1995 9 15 DLL10953630 119950903A5312 FITTING LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11713DA 193C1089 COMPLYING WITH AD T95-18-52, DL INSPECTION SI 7-66332-12, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 4 AND NR 8. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915000691995091500069WP 1995 9 15 DLL10953631 119950828A53121554947 FITTING LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 COMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED, AT STRINGERS NR 8, 10, 56, 58 AND 61. FITTINGS WERE REPLACED. 2L73 4F A23WE 19950915000701995091500070WP 1995 9 15 DLL10953644 119950831A53121554947 FITTINGS LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 COMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS AT STRINGERS NR 5, 10 AND 61 CRACKED. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915000711995091500071WP 1995 9 15 DLL10953645 119950831A53121554947 FITTING LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 8, 10 AND 58. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT PER DL ERA 271733-14AD REV D. 2L73 4F A23WE 19950915000721995091500072WP 1995 9 15 DLL10953647 119950825A53121554947 FITTING LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11730DA 193C1199 COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS CRACKED AT STRINGERS NR 5 AND NR 58. FITTINGS SCHEDULED FOR REPLACEMENT PER DL ERA 272720-14. 2L73 4F A23WE 19950915000731995091500073WP 1995 9 15 DLL12953646 119950831A5312 FITTING LKHEED1011 1011385115 5265015WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11724DA 193C1151 COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTING CRACKED AT STRINGER NR 58. THE FITTING WAS SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915000741995091500074WP 1995 9 15 DLL13953599 119950904A3350516574 EEL POWER PACK LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11784DA 193A1038 DURING LAYOVER, L-4 DOOR EMERGENCY LIGHT POWER SUPPLY POPS C/B. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2L73 4F A23WE 19950915000751995091500075WP 1995 9 15 DLL13953616 119950905A53111506582 FRAME LKHEED1011 10113851 5265010WP BS 1605 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11790DL 193A1143 DURING INSPECTION, FOUND FUSELAGE FRAME CRACKED AT STA 1605, STR 14. DAMAGE IS TYPICAL TO THAT DESCRIBED IN FAA AD 95-10-17 AND LAC S/B 093-53-A271. REPAIR IS BEING ACCOMPLISHED PER DAL SI 7-69903-12AD. 2L73 4F A23WE 19950915000761995091500076WP 1995 9 15 DLL13953621 119950905A5311 FRAME LKHEED1011 10113851 5265010WP BS 1645 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11790DL 193A1143 A 1.25 INCH CRACK WAS FOUND AT FS 1645 FRAME ATTACHMENT TO THE WL 289 LONGERON, STRINGER 14. ALSO, THREE ADDITIONAL HOLES WERE ADDED THROUGH THE FRAME INNER CAP, BETWEEN WL 295 AND WL 300. THE FRAME WAS REPAIRED PER FIG 8 OF SI 7-69903-12AD AND THE THREE HOLES HAVE BEEN PLUGGED WITH AD RIVETS, PER DL ERA 271769-14 REV A. 2L73 4F A23WE 19950915000771995091500077WP 1995 9 15 DLL13953648 119950903A5312 FITTING LKHEED1011 10113851 5265010WP AFT P-DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 COMPLYING WITH INSPECTION SI 7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTING CRACKED AT STRINGER NR 11. SCHEDULED THE FITTING REPLACEMENT PER DL ERA 271759-14. 2L73 4F A23WE 19950915000781995091500078NM 1995 9 15 DLM11953608 119950905A3350349201652 EEL BULB DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11805DE 48476 DURING LAYOVER, EMERGENCY FLOOR TRACK LIGTHS AT 40AB TO 47AB OUT. RETERMINATED BROKEN WIRE, RELAMPED AND OPERATION NOW NORMAL. 2L73 4F RTA22WE 19950915000791995091500079NM 1995 9 15 DLM88953601 119950904A2133 OUTFLOW VALVE 20219742 DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11988DL 111400 53339 DURING DEPARTURE, BOTH AUTO PRESSURIZATION CONTROLLERS FAILED AND BOTH CONTROLLERS FAULT AC MOTOR. VERIFY CHECK, NO FAULTS. REPLACED OUTFLOW VALVE ACTUATOR GEARBOX AND AC MOTORS, CHECKS GOOD PER MM CHECK. 2L72 4F RTA6WE 19950915000801995091500080WP 1995 9 15 MWEA95285 119950906A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31602ME 48133 CREW REPORTS, GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. MAINTENANCE RESECURED GALLEY DOOR EVACUATION SLIDE COVER AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915000811995091500081WP 1995 9 15 MWEA95286 119950907A33506003043 EEL POWER SUPPLY DOUG DC9 DC914 3022034WP CABIN FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31500ME 45711 DURING SERVICE CHECK, THE GALLEY AREA EMERGENCY LIGHTS WOULD NOT COME ON WHEN AC BUSES ARE TURNED OFF. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915000821995091500082NM 1995 9 15 P5CA9500735 119950809A27801267485SW PDU BOEING747 747122 1384872NM NR 1 LE FLAP BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED MOUNT LUG NR 1 RIGHT LEADING EDGE PDU. REPLACED PDU PER BOEING MAINTENANCE MANUAL 27-81-03. 2L74 4F A20WE 19950915000831995091500083NE 1995 9 15 P5CA9500741 219950908A7250JT9D7A TURBINE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE FAILED A P5CAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 WP23830FT519122191 19642 685859 JFK - ON CLIMBOUT, NR 4 ENGINE EXPERIENCED A COMPRESSOR STALL AT CONSTANT SPEED, ALTITUDE 17,000 MAX EGT 856, ENGINE SHUTDOWN. SECOND STAGE TURBINE FAILURE, FOUND METAL IN TAIL PIPE. ENGINE CHANGED. 2L74 4F4 F A20WE E20EA 19950915000841995091500084NM 1995 9 15 P5CA9500742 119950809A5400 FAIRING BOEING747 747122 1384872NM NR 4 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED FAIRING NR 4 STRUT FORWARD. REPAIRED PER BOEING SRM. 2L74 4F A20WE 19950915000851995091500085NM 1995 9 15 P5CA9500743 119950809A5730 SKIN BOEING747 747122 1384872NM LT WING CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION FOUND AROUND RIVET HEAD, TOP OF LEFT WING BETWEEN FRONT AND REAR SPARS. CLEANED CORROSION WITHIN LIMITS PER BOEING SRM 51-30-03. 2L74 4F A20WE 19950915000861995091500086NM 1995 9 15 P5CA9500744 119950809A5730 TE PANEL BOEING747 747122 1384872NM LT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED AND DELAMINATED FIBERGLASS PANEL, LEFT WING TRAILING EDGE OUTBOARD OF INBOARD AILERON. REPAIRED PER BOEING SRM. 2L74 4F A20WE 19950915000871995091500087NM 1995 9 15 P5CA9500745 119950809A5730 TE PANEL BOEING747 747122 1384872NM LT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATED FIBERGLASS PANEL LEFT WING TRAILING EDGE OUTBOARD OF OUTBOARD AILERON, PCU UPPER ACCESS PANEL. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000881995091500088NM 1995 9 15 P5CA9500746 119950809A5730 PANEL BOEING747 747122 1384872NM LT WING LE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATED FIBERGLASS PANEL LEFT WING LEADING EDGE UPPER PANEL INBOARD OF NR 2 PYLON. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000891995091500089NM 1995 9 15 P5CA9500747 119950809A5730 TE PANEL BOEING747 747122 1384872NM RT WING DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATED WING TRAILING EDGE PANEL FORWARD OF THE INBOARD AILERON RIGHT WING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000901995091500090NM 1995 9 15 P5CA9500748 119950809A5730 TE PANEL BOEING747 747122 1384872NM RT WING CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED PANEL RIGHT WING UPPER TRAILING EDGE, FORWARD OF NR 8 SPOILER PANEL. REPAIRED PER SRM 51-40-09. 2L74 4F A20WE 19950915000911995091500091NM 1995 9 15 P5CA9500749 119950809A5753 SKIN BOEING747 747122 1384872NM RT TE MIDFLAP PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 SMALL PUNCTURE HOLE IN RIGHT WING INBOARD MIDFLAP FORWARD OF NR 5 CANOE FAIRING. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000921995091500092NM 1995 9 15 P5CA9500750 119950809A5753 LE SKIN BOEING747 747122 1384872NM RT TE FOREFLAP PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 PUNCTURE RIGHT WING OUTBOARD FOREFLAP AT OUTBOARD LEADING EDGE. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000931995091500093NM 1995 9 15 P5CA9500751 119950809A5753 SKIN BOEING747 747122 1384872NM RT TE MIDFLAP DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATION ON RIGHT WING INBOARD MIDFLAP, OUTBOARD UPPER PANEL. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000941995091500094NM 1995 9 15 P5CA9500752 119950809A5753 SPAR BOEING747 747122 1384872NM RT TE MIDFLAP CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION ON RIGHT WING INBOARD MIDFLAP REAR SPAR UPPER T-CHORD, APPROXIMATELY WBL 230. CORROSION REMOVED AND SURFACE REPROTECTED PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950915000951995091500095NM 1995 9 15 P5CA9500753 119950809A5730 PANEL BOEING747 747122 1384872NM RT WING LE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACK RIGHT WING LOWER LEADING EDGE PANEL JUST OUTBOARD OF NR 3 PYLON, LES 740. REPAIRED PER BOEING SRM 51-40-09. 2L74 4F A20WE 19950915000961995091500096NM 1995 9 15 P5CA9500754 119950809A5755 TE PANEL BOEING747 747122 1384872NM NR 7/8 SPOILERS CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 LIGHT CORROSION ON TRAILING EDGES OF NR 7 AND NR 8 SPOILER PANELS. REMOVED CORROSION AND REPROTECTED SURFACES PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950915000971995091500097NM 1995 9 15 P5CA9500755 119950809A5730 PANEL BOEING747 747122 1384872NM WS 758 LE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION RIGHT WING LOWER LEADING EDGE SURFACE APPROXIMATLEY WS 758. REMOVED CORROSION WITHIN LIMITS PER BOEING SRM 57-30-01, REPROTECTED SURFACE. 2L74 4F A20WE 19950915000981995091500098NM 1995 9 15 P5CA9500756 119950809A5711 SPAR BOEING747 747122 1384872NM WS 1520 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION BULGE AT RIGHT WING FRONT SPAR LOWER CHORD AT WS 1520. REPAIRED PER BOEING SRM 57-30-03 FIG 9. 2L74 4F A20WE 19950915000991995091500099NM 1995 9 15 P5CA9500757 119950809A5753 CANOE FAIRING BOEING747 747122 1384872NM NR 7 DELAMINATION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 DELAMINATION AND PUNCTURE NR 7 CANOE FAIRING. REPAIRED PER BOEING SRM. 2L74 4F A20WE 19950915001001995091500100NM 1995 9 15 P5CA9500758 119950809A5320 PRESS DECK BOEING747 747122 1384872NM BS 1325 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION AT BS 1325 RIGHT OUTBOARD PRESSURE DECK FLOOR, OUTBOARD LOWER CHORD JOINT. CORROSION REMOVED WITHIN LIMITS PER BOEING SRM 53-10-01, INSTALLED DOUBLER WHERE MATERIAL WAS REMOVED AS PER BOEING SRM 51-40-02. 2L74 4F A20WE 19950915001011995091500101NM 1995 9 15 P5CA9500759 119950809A5320 STIFFENER BOEING747 747122 1384872NM BS 1350 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORRODED STIFFENER IN LEFT BODY GEAR WHEEL WELL, BS 1350 AT LBL 87. REMOVED CORROSION WITHIN LIMITS OF BOEING SRM 51-10-01 FIG 1. 2L74 4F A20WE 19950915001021995091500102NM 1995 9 15 P5CA9500760 119950809A540065B9072611 BRACKETS BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED LATCH SUPPORT BRACKETS, 2ND AND 4TH FROM FRONT ON NR 3 PYLON INBOARD TRAILING EDGE DOOR. REPLACED BRACKETS. 2L74 4F A20WE 19950915001031995091500103NM 1995 9 15 P5CA9500761 119950809A498065B987051 EXHAUST LINER BOEING747 747122 1384872NM APU CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 SEVERAL CRACKS APU EXHAUST LINER. REPLACED LINER. 2L74 4F A20WE 19950915001041995091500104NM 1995 9 15 P5CA9500762 119950809A2520 LADDER BOEING747 747122 1384872NM MAIN DECK CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CRACKED UPPER DECK ACCESS LADDER AT PULLEY LOCATION. REPAIRED LADDER. 2L74 4F A20WE 19950915001051995091500105NM 1995 9 15 P5CA9500763 119950809A5230 ANGLE BOEING747 747122 1384872NM CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION ON ANGLE ON AFT CARGO DOOR, FORWARD OF NEGATIVE PRESSURE RELIEF VALVE CUTOUT. REPLACED ANGLE. 2L74 4F A20WE 19950915001061995091500106NM 1995 9 15 P5CA9500764 119950809A7800 EXHAUST BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662663 CRACKS ON NR 1 ENGINE ON R-FLANGE, TWO-THIRTY AND S-FLANGE AT 2 O'CLOCK POSITION. WELD REPAIRED PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-01. 2L74 4F4 F A20WE E20EA 19950915001071995091500107NM 1995 9 15 P5CA9500765 119950809A7800 EXHAUST BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662575 CRACKS ON NR 2 ENGINE R-FLANGE AT FIVE O'CLOCK POSITION, S-FLANGE AT 3 LOCATIONS BETWEEN SIX-THIRTY AND SEVEN-THIRTY POSITION. WELD REPAIRED PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-01. 2L74 4F4 F A20WE E20EA 19950915001081995091500108NM 1995 9 15 P5CA9500766 119950809A7800 EXHAUST CASE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662628 CRACKS ON NR 3 ENGINE RT FLANGE AT FOUR THIRTY, S-FLANGE AT FIVE O'CLOCK AND SIX THIRTY. WELD REPAIRED PER PRATT AND WHITNEY MANINTENCE MANUAL 72-53-01. 2L74 4F4 F A20WE E20EA 19950915001091995091500109NM 1995 9 15 P5CA9500767 119950809A5320 L-CHORD BOEING747 747122 1384872NM BS 1283-1333 CORROSION A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 CORROSION ON LT OUTBOARD LONGERON L-CHORD, BS 1283 TO BS 1333. REPAIRED PER BOEING TELEX PAO-SIN-95-0002RE. 2L74 4F A20WE 19950915001101995091500110EA 1995 9 15 95ZZZX4499 219950806A73208061328 FUEL CONTROL BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT ENGINE OUT OF ADJUST A GPPAL ABORTED APPROACH O OTHER APAPPROACH 1 CE09317BH 1948436 UB32 PS32234 GSO - FLT 2135 - APPROACH INTO COLUMBUS FROM GSO, EXPERIENCED DIRECTIONAL CONTROL PROBLEMS. GO-AROUND WAS INITIATED ON NEXT APPROACH, SAME DIFFICULTIES. GO-AROUND INITIATED, EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. RE-RIGGED LOW PITCH STOP AND FUEL CONTROL ON NR 2 ENGINE. WORK DONE BY GPX MAINTENANCE. AIRCRAFT TEST FLIGHT SATISFACTORY. RETURNED TO SERVICE. (X) 2L72 4T4 TRTA24CE E4EA 19950915001111995091500111CE 1995 9 15 95ZZZX4500 119950812A79311013890233 OIL PRESS TRANS BEECH 1900 1900C 1154161CE RT ENGINE FAILED A GPPAK NONE N FALSE WARNING CLCLIMB 1 CE09318BH UB33 ON CLIMB CHECK, RT OIL PRESSURE FLUCTUATING BETWEEN 30-50 PSI. SUBSEQUENTLY, WENT TO OPSI WITHOUT ILLUMINATION OF OIL PRESSURE LIGHT. GPX MAINTENANCE REPLACED TRANSDUCER, GROUND RUN CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. 2L72 4T RTA24CE 19950915001121995091500112WP 1995 9 15 95ZZZX4501 119950824A3260833703 UPLOCK SENSOR DOUG DC9 DC981 3022081WP LT MLG MALFUNCTIONED A A4JAO OTHER N FALSE WARNING CLCLIMB 1 SO15817SJ 48051 UPON GEAR RETRACTION, LEFT MAIN LANDING GEAR UNSAFE LIGHT CAME ON. CYCLED GEAR, LIGHT WENT OUT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED LEFT MLG UPLOCK SENSOR. OPERATIONAL TEST NORMAL. 2L72 4F A6WE 19950915001131995091500113NM 1995 9 15 95ZZZX4502 119950818A243131920002 SENSOR MARATHON 31920002 DORNERDO32 DO328100 2996000NM RT BATTERY FAILED A EQGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW19328LS 266 3025 DFW - AIRCRAFT WAS IN CRUISE AFTER DEPARTING, AND THE RIGHT BATTERY OVERHEAT CAME ON. RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. FOUND RIGHT BATTERY SENSOR BAD. REPLACED RIGHT BATTERY SENSOR IAW MARATHON AND DORNIER MM. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19950915001141995091500114GL 1995 9 15 95ZZZX4503 219950722A73213300588 FUEL CNTRL UNIT CVAC 340 34030 2422702WP ALLSN 501D 501D13H 03004GL LT ENGINE FAILED A SPAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP0773301 6048 80 501616 DEN/BIL - FLT 8072 - THE LT ENGINE WAS SHUT DOWN DUE TO RPM FLUCTUATION FROM 13,000 RPM TO 15,000 RPM. AIRCRAFT RETURNED TO DEN. THE LT FUEL CONTROL UNIT WAS REPLACED. SUBSEQUENT GROUND RUNS AND TEST FLIGHT WERE SATISFACTORY. 2L72 4R4 T 6A6 E282 19950915001151995091500115GL 1995 9 15 95ZZZX4504 219950726A72506886407 WHEEL BELL 206 206L 1181522SW ALLSN 250C 250C30P 03013GL FIRST STAGE CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11121NH2495 1989 X129082 46610 DURING INSPECTION OF FIRST STAGE NOZZLE, FOUND FIRST STAGE WHEEL CRACKED AT THE INNER RING. CRACK PROGRESSES TOWARD THE SPLINED SHAFT. THIS HAS BEEN THE FIRST OCCURRENCE OF FIRST STAGE TURBINE WHEEL BEING CRACKED AT THIS LOCATION. 1G71 3U3 U H2SW E1GL 19950915001171995091500117EU 1995 9 15 AALA951290 119950723A532053777080200 DOOR FRAME AIRBUS300 A300B4605R 3930308EU BS 1876 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW0780058 466 TULE - FRAME 28A BETWEEN STR 19 AND STR 20 LT FRAME CRACKED. REMOVED AND REPLACED DOOR FRAME SECTION PER SRM 53-14-13-2. T.S.T. 19,702.17. CYCLES, 7,880. (X) 2L72 4F RTA35EU 19950915001181995091500118NM 1995 9 15 AALA951380 119950804A5313 STRINGER BOEING767 767223 1385123NM BS 1316 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07307AA 22313 AFW - STRINGER CORRODED BEYOND SRM LIMITS AT STA 1316. REQUESTED AUTHORIZATION FROM ENGINEERING TO REMOVE 5 INCHES OFF 39R (STA 1312 TO STA 1317) AND EXTEND STR SPLICE AT STA 1307 AFT TO STA 1323.5. T.S.T. 40,223.25. CYCLES, 12,808. (X) 2L72 4F RTA1NM 19950915001191995091500119NM 1995 9 15 AALA951384 119950804A5313146T300311 STRINGER BOEING767 767223 1385123NM BS 1299 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07307AA 22313 AFW - STRINGER CORRODED BEYOND SRM LIMITS. REQUESTED AUTHORIZATION FROM ENGINEERING TO REMOVE 5 INCHES OF STR 36L (1304.5 TO 1299.5) AND EXTEND STR SPLICE AT STA 1307 FORWARD TO STA 1294.5. T.S.T. 40,223.25. CYCLES, 12,808. (X) 2L72 4F RTA1NM 19950915001201995091500120NM 1995 9 15 AALA951386 119950804A5313146T300317 STRINGER BOEING767 767223 1385123NM BS 1307 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07307AA 22313 AFW - REMOVED 6 INCHES OF STR 39L DUE TO CORROSION. REQUESTED AUTHORIZATION FROM ENGINEERING TO EXTEND STRINGER SPLICE 6 INCHES AFT OF STA 1313. FABRICATED AND INSTALLED SPLICE. APPROVED BY ENGINEERING PER MRB 767-982. T.S.T. 40,223.25. CYCLES, 12,808. (X) 2L72 4F RTA1NM 19950915001211995091500121NM 1995 9 15 AALA951387 119950803A5320143T15902 CHORD BOEING767 767223 1385123NM BS 540 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07307AA 22313 AFW - UPPER SURFACE OF FAIL-SAFE CHORD. AFTER REMOVING CORROSION, FOUND BEYOND SRM LIMITS. BLENDED AND ROTOPEENED AREA. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERING PER MRB 767-986. T.S.T. 40,223.25. CYCLES, 12,808. (X) 2L72 4F RTA1NM 19950915001221995091500122NM 1995 9 15 AALA951388 119950803A5320140T10433 STRAP BOEING767 767223 1385123NM BS 1270 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07307AA 22313 AFW - FAIL SAFE STRAP CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ROTOPEENED, TREATED, PRIMED, AND PAINTED. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-980. T.S.T. 40,223.23. CYCLES, 12,808. (X) 2L72 4F RTA1NM 19950915001231995091500123EU 1995 9 15 AALA951403 119950809A3350A3030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0777080 626 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT L2/R2 DOORS CROSS AISLE FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT L2/R2 DOORS CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA35EU 19950915001241995091500124EU 1995 9 15 AALA951406 119950809A24502XN CIRCUIT BREAKER AIRBUS300 A300B4605R 3930308EU NR 2 AC BUS DEFECTIVE A AALAA UNSCHED LANDING O OTHER CRCRUISE 1 SW0780058 466 SJU - FLT 0412 - EN ROUTE STT/JFK DURING CRUISE, AC BUS NR 2 OFF LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AC BUS CIRCUIT BREAKER (DASH 2XN). SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 19950915001251995091500125NM 1995 9 15 AALA951436 119950814A5753113T2311 SKIN BOEING767 767323 1385205NM TE FLAP CHAFED A AALAK NONE O OTHER ININSP/MAINT 1 SW07374AA 25201 AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS. BLENDED DYE-CHECKED ALODINED, PRIMED, FILLED WITH BMS 5-28 SEALANT AND PAINTED AREA PER ENGINEERING MRB 767-287. T.S.T. 14,105. CYCLES, 2,184. (X) 2L72 4F RTA1NM 19950915001261995091500126NM 1995 9 15 AALA951437 119950814A5315111T5008 FLOORBEAM BOEING767 767323 1385205NM BS 800/840 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07374AA 25201 AFW - FLOORBEAM IS BEYOND SRM LIMITS AFTER BLEND OUT OF CORROSION AND GOUGES. FLAP PEEN, BLEND, DYE-CHECK, ALODINE, PRIME, FILL WITH BMS 5-28 SEALANT AND PAINT PER ENGINEERING MRB 767-988. T.S.T. 14,105. CYCLES, 2,184. (X) 2L72 4F RTA1NM 19950915001271995091500127EU 1995 9 15 AALA951447 119950814A492038005141 ENGINE GARRTT FOKKERF28 F28MK0100 4990807EU APU COMPT DEFECTIVE A AALAF ACTIVATE FIRE EXT. J WARNING INDICATION DEDESCENT 1 SW071433B P175 11418 DTW - FLT 1374 - DURING DESCENT INTO DFW, APU FIRE WARNING FOLLOWED BY APU AUTO SHUTDOWN. DISCHARGED APU FIRE BOTTLE AND AIRCRAFT LANDED DTW WITHOUT INCIDENT. PLACARDED APU AND APU FIRE EXTINGUISHING SYSTEM. SUBSEQUENTLY, REPLACED APU AT ORD ON SAME DATE. REPLACED APU FIRE BOTTLE. ACCOMPLISHED LEAK AND SYSTEM GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RT 19950915001281995091500128NM 1995 9 15 AALA951478 119950818A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07652AA 24610 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT AFT OF CENTER GALLEY FOUND INOPERATIVE. RESECURED LOOSE CONNECTOR AFT OF CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19950915001291995091500129NM 1995 9 15 AALA951479 119950818A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07352AA 24033 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT SIDE OF FIRST CLASS AND BUSINESS CLASS FOUND INOPERATIVE. RESECURED LOOSE CONNECTOR IN FIRST CLASS, RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950915001301995091500130NM 1995 9 15 AALA951480 119950818A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07368AA 25195 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RT SIDE OF COACH FOUND INOPERATIVE. REPAIRED CONNECTOR ON RT SIDE OF COACH. SYTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950915001311995091500131 1995 9 15 AALA951481 419950817A2565101651300 SLIDE BFGOODRICH BOEING767 767323 1385205NM ENTRY DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07368AA A4362 25195 LAX - DURING SLIDE SHOP RECEIVING INSPECTION, FOUND HOLE ABOVE LEFT RELIEF VALVE EMERGENCY EVACUATION SLIDE. REPAIRED SLIDE, SLIDE CHECKS GOOD. (X) 2L72 4F RTA1NM 19950915001321995091500132NM 1995 9 15 AALA951485 119950819A2613358050 OVER TEMP UNIT FENWAL BOEING727 727223 1384074NM E/E COMPT DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW07710AA 8646 22467 SJU - FLT 1879 - EN ROUTE MIA/CUR DURING CRUISE, LOWER AFT BODY HEAT LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY CHECK LIST AND DIVERTED INTO SJU AND LANDED WITHOUT INCIDENT. REPLACED OVER TEMP ALARM CONTROL UNIT. INSPECTED DUCTS, RAN ENGINES, AND ACCOMPLISHED ALL CHECKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19950915001331995091500133NM 1995 9 15 AALA951529 119950821A3350 EEL WIRE BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07363AA 24044 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT SIDE OF BUSINESS CLASS FOUND INOPERATIVE. REPAIRED WIRING AT 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950915001341995091500134NM 1995 9 15 AALA951530 119950823A3350P4010051127 EEL MODULE DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST CRCRUISE 1 SW071767A 48598 DFW - DURING CRUISE, THE EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATED. CYCLED SWITCH, NO HELP. LANDED DFW WITHOUT INCIDENT. REPLACED FIRST CLASS RIGHT SIDE LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F RTA22WE 19950915001351995091500135NM 1995 9 15 AALA951531 119950824A33508100022002 EEL STRIP BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07369AA 25196 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED TWO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AND AN INVERTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950915001361995091500136NM 1995 9 15 AALA951532 119950824A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07354AA 24035 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS AT ROW 2-7B INOPERATIVE. CONNECTED LOOSE PINS IN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19950915001371995091500137SO 1995 9 15 C2XA95IA196 119950823A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, A/C RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001381995091500138SO 1995 9 15 C2XA95IA197 119950823A572012017056021 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, A/C RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001391995091500139SO 1995 9 15 C2XA95IA198 119950823A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001401995091500140SO 1995 9 15 C2XA95IA199 119950823A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 5 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001411995091500141SO 1995 9 15 C2XA95IA200 119950823A572012017056021 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001421995091500142SO 1995 9 15 C2XA95IA201 119950823A572012017057007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001431995091500143SO 1995 9 15 C2XA95IA202 119950823A572012017057006 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001441995091500144EU 1995 9 15 C2XA95IA203 119950823A3234F96GA0102 GEAR HANDLE AEROSPATR42 ATR42320 8680930EU COCKPIT FAULTY A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926826 172 IAH - FLT 2768 - LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE ASSEMBLY, PERFORMED EXTENSION/RETRACTION CHECK, AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19950915001451995091500145SO 1995 9 15 C2XA95IA204 119950823A572012017059015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND THE NR 2 LOWER SKIN SUPPORT FOR LEFT WING RIB 18 CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES, 19,430. (X) 2L72 4T RTA31SO 19950915001461995091500146SO 1995 9 15 C2XA95IA205 119950823A571312016086001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING STR 10 CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF THE STRINGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. REFERENCE EMBRAER FAXES EST 243/95 AND EST 376/95 FOR REPAIR PROCEDURES. A/C TT - 13,674.8 HRS. CYCLES - 19,430. (X) 2L72 4T RTA31SO 19950915001471995091500147SO 1995 9 15 C2XA95IA206 119950823A572012017059019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LT WING RIB 18 LOWER NR 1 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED AFFECTED SKIN SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT - 13,674.8 HRS. CYCLES - 19,430. (X) 2L72 4T RTA31SO 19950915001481995091500148EU 1995 9 15 C2XA95IA207 119950825A5230S52376114200 FITTING AEROSPATR42 ATR42320 8680930EU CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914804 069 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR ACTUATOR TO CARGO DOOR FORWARD ATTACH FITTING WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT - 14,967.4 HRS. CYCLES, 18,408. (X) 2H72 4T RTA53EU 19950915001491995091500149EU 1995 9 15 C2XA95IA208 119950825A5210S5217600100200 PASSENGER DOOR AEROSPATR42 ATR42320 8680930EU AFT FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914804 069 IAH - DURING C-CHECK INSPECTION, THE PASSENGER/CREW ENTRY DOOR WAS FOUND CORRODED. MAINTENANCE REMOVED THE DOOR, REPAIRED THE AFFECTED AREAS, AND REINSTALLED THE DOOR. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. A/C TT - 14,967.4 HRS. CYCLES, 18,408. (X) 2H72 4T RTA53EU 19950915001501995091500150EU 1995 9 15 C2XA95IA209 119950825A2731NTA1425140 TRIM TAB BEARING AEROSPATR42 ATR42320 8680930EU RT ELEVATOR RUSTED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914804 069 IAH - DURING C-CHECK INSPECTION, RT ELEVATOR TRIM TAB OUTBOARD BEARING WAS FOUND BLEEDING RUST. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT - 14,967.4 HRS. CYCLES, 18,408. (X) 2H72 4T RTA53EU 19950915001511995091500151EU 1995 9 15 C2XA95IA210 119950825A5320S53971402221 STIFFENER AEROSPATR42 ATR42320 8680930EU LOWER FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914804 069 IAH - DURING C-CHECK INSPECTION, THE STIFFENER ON FRAME 27A WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT - 14,967.4 HRS. CYCLES, 18,408. (X) 2H72 4T RTA53EU 19950915001521995091500152NE 1995 9 15 C2XA95IA211 319950826A6111SFA13M10AB BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE RT PROP NR 2 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW091783114050627 185 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 2 BLADE FAILED THE SHEAR WAVE ULTRASONIC INSPECTION. THE PROPELLER BLADE WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS APPROVED FRO RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001531995091500153NE 1995 9 15 C2XA95IA212 319950826A6111SFA13M10AB BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE RT PROP NR 3 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW099384014350878 271 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001541995091500154NE 1995 9 15 C2XA95IA213 319950826A6111SFA13G10AB BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE LT PROP NR 3 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914832119995420 187 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001551995091500155NE 1995 9 15 C2XA95IA214 319950826A6111SFA13M10A BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE RT PROP NR 1 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0921837106214044 202 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RT PROPELLER NR 1 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001561995091500156NE 1995 9 15 C2XA95IA215 319950826A6111SFA13M10A BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE RT PROP NR 2 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0921837142832430 202 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RT PROPELLER NR 2 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001571995091500157NE 1995 9 15 C2XA95IA216 319950827A6111SFA13M10A BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE RT PROP NR 4 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW09148329716 4869 187 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE RIGHT PROPELLER NR 4 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001581995091500158NE 1995 9 15 C2XA95IA217 319950826A6111SFA13M10A BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE LT PROP NR 3 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917810110364222 093 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LT PROPELLER NR 3 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001591995091500159NE 1995 9 15 C2XA95IA218 319950826A6111SFA13M10A BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF5 NE LT PROP NR 2 FAILED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0917810129887068 093 IAH - DURING ACCOMPLISHMENT OF AD T95-18-51, THE LEFT PROPELLER NR 2 BLADE FAILED THE ULTRASONIC SHEAR WAVE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BLADE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2H72 4T RTA53EU 6 CP7NE 19950915001601995091500160NE 1995 9 15 VTZA95260 219950814A732031059003 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27313UE 41026 P76008 AID/LGA - FLT 6530 - DURING TAKEOFF AT 1910 HRS ON 8-14-95, ABORTED TAKEOFF DUE TO RT ENGINE UNABLE TO MAKE TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED TT2 BIAS, MAX POWER, AND DECELERATION SCHEDULE IAW MM CHAPTER 72. PERFORMED ENGINE RUNS, OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19950915001611995091500161WP 1995 9 15 VTZA95261 219950815A73208937527 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27490UE 909 P66088 JFK/IAD - FLT 6473 - DURING TAKEOFF AT 1400 HRS ON 8-15-95, ABORTED TAKEOFF DUE TO LT ENGINE TORQUE ROLLED BACK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 10706 IAW MEL 76-1. MAINTENANCE LATER CLEARED DMI NR 10706 BY ADJUSTING SCREW 'X' ON THE FUEL CONTROL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E3WE 19950915001621995091500162WP 1995 9 15 VTZA95262 219950821A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RIGHT MALFUNCTIONED A VTZAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 EA27480UE 12352 894 P66030A IAD/CRW - FLT 6377 - DURING TAKEOFF AT 1300 HRS ON 8-21-95, ABORTED TAKEOFF DUE TO THE RT ENGINE NOT MAKING TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO LYH FOR AN ENGINE CHANGE ON 8-22-95. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. AIRCRAFT IS IN LYH AWAITING ENGINE CHANGE. LYH MAINTENANCE LATER COMPLETED ENGINE CHANGE ON 8-22-95. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E3WE 19950915001631995091500163EU 1995 9 15 VTZA95263 119950822A771231024562 SIGNL CONDITIONR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CLCLIMB 1 EA27478UE 892 P66183 IAD/ELM - FLT 6212 - DURING TAKEOFF AT 1220 HRS ON 8-22-95, ABORTED TAKEOFF DUE TO RT ENGINE NOT MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E3WE 19950915001641995091500164EU 1995 9 15 VTZA95264 119950822A7722 EGT WIRE BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27478UE 892 IAD/ROC - FLT 6326 - DURING TAKEOFF AT 1220 HRS ON 8-22-95, ABORTED TAKEOFF DUE TO THE LT ENGINE TEMPS OUT BEFORE MAKING TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED WIRE TO ZONE 2 CONNECTOR FROM EGT COMP RESISTOR MODULAR POSITION. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950915001651995091500165EU 1995 9 15 VTZA95265 119950823A2510168676 LAP BELT BAG JETSTMJETSTM3201 1500217EU COPILOT OUT OF ADJUST A VTZAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27482UE 897 BOS/SWF - FLT 6584 - DURING TAXI AT 0800 HRS ON 8-23-95, RETURNED TO GATE DUE TO THE F/O'S SHOULDER HARNESS WOULD NOT RELEASE TO PULL OUT AND PUT ON. MAINTENANCE TIGHTENED RELEASE CABLE ADJUSTMENT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950915001661995091500166EU 1995 9 15 VTZA95266 119950824A2432BTCA520 MAIN BATTERY BAG JETSTMJETSTM3201 1500217EU NOSE EQUIP BAY OVERHEATED A VTZAK NONE J WARNING INDICATION LDLANDING 1 EA27479UE 893 IAD/EWR - FLT 6435 - DURING THE LANDING PHASE AT 1815 HRS ON 8-24-95, EXPERIENCED A NR 2 BATTERY OVERHEAT. AIRCRAFT COMPLETED LANDING AND TAXIED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NR 2 BATTERY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19950915001671995091500167WP 1995 9 15 VTZA95268 219950824A7320 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110U 01514WP RT ENGINE OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27479UE 893 P66283 IAD/HPN - FLT 6281 - DURING CLIMB-OUT AT 0700 HRS ON 8-24-95, RETURNED TO IAD DUE TO THE RT ENGINE MAX RPM OF 97.5 PERCENT WITH A TORQUE DROP OF APPROXIMATELY 20 PERCENT ON CLIMB-OUT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE SPEED LEVER ON THE FUEL CONTROL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA56EU E4WE 19950915001681995091500168EU 1995 9 15 VTZA95270 119950825A32347177011 GEAR SELECTOR JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27310UE 41028 IAD/JFK - FLT 6501 - DURING CLIMB-OUT AT 1715 HRS ON 8-25-95, RETURNED TO IAD DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP, AND THE GEAR HANDLE LIGHT STAYED ILLUMINATED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE GEAR SELECTOR HANDLE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950915001691995091500169EU 1995 9 15 VTZA95271 119950826A3230AIR132254 SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27310UE 41028 DAY/IAD - FLT 6460 - DURING CLIMB-OUT AT 1500 HRS ON 8-26-95, RETURNED TO DAY DUE TO THE LANDING GEAR NOT RETRACTING WHEN SELECTED UP. AIRCRAFT LANDED AT DAY WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE NLG WEIGHT-ON-WHEEL MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950915001701995091500170EU 1995 9 15 VTZA95272 119950827A3260ARG135022 SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27301UE 41012 IAD/EWR - FLT 6403 - DURING CLIMB-OUT AT 2024 HRS ON 8-27-95, RETURNED TO IAD DUE TO THE LANDING GEAR SELECTOR HANDLE LIGHT ILLUMINATING WITH THE GEAR UP AND LOCKED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LT MLG STANDBY UPLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950915001711995091500171WP 1995 9 15 9513649156 119950814A2740 PRIMARY TRIM DOUG DC9 DC914 3022034WP COCKPIT MALFUNCTIONED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED UKUNKNOWN 1 GL018915E 45832 PRIMARY TRIM WOULD NOT OPERATE IN NOSE UP POSITION WITH YOKE SWITCHES, FUNCTIONED PROPERLY FROM SUITCASE HANDLES. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. OPERATIONAL CHECK WAS NORMAL ON GROUND. DISCREPANCY COULD NOT BE DUPLICATED, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915001721995091500172WP 1995 9 15 9513759872 119950906A3260 DOOR ROLLER DOUG DC9 DC951 3022051WP LT MLG OUT OF ADJUST A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01781NC 48121 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND LEFT MAIN GEAR DOOR ROLLER OUT OF ADJUSTMENT. READJUSTED DOOR ROLLER ASSEMBLY, OPERATIONAL CHECK OK ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915001731995091500173EU 1995 9 15 9513763203 119950906A2910 O-RING AIRBUS320 A320211 3930320EU NR 1 ENGINE FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01303US 34 DURING DESCENT, RECEIVED HYD 'G' RSVR LOW LEVEL MESSAGE. AN EMERGENCY WAS DECLARED AND EQUIPMENT CALLED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RING ON NR 1 ENGINE PRESSURE FITTING. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950915001741995091500174EU 1995 9 15 9513773217 119950905A2120 AIR DISTRIBUTION AIRBUS320 A320211 3930320EU CABIN SMOKE A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01317US 197 DURING CLIMBOUT FROM SAN, HEARD A BANG AND FELT A THUMP, VISUAL CHECK REVEALED NO DISCREPANCIES. APPROXIMATELY 1.5 HOURS LATER, FLIGHT ATTENDANT REPORTED SMALL CLOUD OF SMOKE JUST OUTSIDE THE FORWARD LAVATORY, A STRONG ELECTRICAL SMELL WAS NOTED. AN EMERGENCY WAS DECLARED, EQUIPMENT CALLED OUT, AND THE AIRCRAFT DIVERTED TO ICT WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE TROUBLESHOOTING AND VISUAL INSPECTION REVEALED NO DISCREPANCIES. 2L72 4F RTA28NM 19950915001751995091500175WP 1995 9 15 9513789853 119950905A5350 CLIPS DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19950915001761995091500176NM 1995 9 15 9513792704 119950908A3231 RETRACT MECH BOEING727 727225 1384077NM NLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01801EA 22432 DURING DEPARTURE CLIMB UPON LANDING GEAR RETRACTION, NOSE LANDING GEAR DOOR UNSAFE INDICATIONS REMAINED ILLUMINATED. VERIFIED DOORS WERE OPEN, FLIGHT RETURNED TO MSP WITHOUT FURTHER INCIDENT. MAINTENANCE RIGGED THE NOSE LANDING GEAR DOORS PER MAINTENANCE MANUAL, OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950915001771995091500177NM 1995 9 15 95FDEA01273 119950908A5313 STRINGER BOEING727 727233 138408ANM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25223FE 20935 CABIN, STR END CRACKED 15R BETWEEN 720B AND 720C FWD OF LIGHT ASSY NR 1401. STOP DRILLED CRACK PER SRM 53-10-2, INSTALLED REPAIR PART PER SRM 53-10-3. 2L73 4F RTA3WE 19950915001781995091500178WP 1995 9 15 95FDEA01274 119950905A5412ANB702515 BULKHEAD DOUG DC10 DC1030F 3023504WP NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 NR 1 PYLON AFT SPHERICAL BEARING SUPPORT BULKHEAD YN 417.212, HAS A 10 INCH CRACK AT I/B INSIDE RADIUS. CRACK WAS DISCOVERED BY AN INSPECTOR WHILE PERFORMING THE SB 54-74 INSPECTIOIN. THE NR 3 PYLON WAS INSPECTED AND NO CRACKING WAS EVIDENT. CRACK APPEARS TO HAVE ORIGINATED AT ZN 55.692 AND PROPAGATED DOWNWARDS TO ZN 44.705. REMOVED AND REPLACED THE BULKHEAD. 2L73 4F RTA22WE 19950915001791995091500179NM 1995 9 15 95FDEA01275 119950906A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 CORROSION ON TOP OF FLOOR BEAM C/L TO LBL 24 STA 560, MAIN CARGO LOBE. REMOVED CORROSION AND REPAIRED FLOORBEAM PER SRM 53-10-5 PG 31 TO 48. 2L73 4F A3WE 19950915001801995091500180WP 1995 9 15 95FDEA01276 119950822A5280ANB72872 FRAME DOUG DC10 DC1030F 3023504WP CTR GEAR DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 RT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C. 2L73 4F RTA22WE 19950915001811995091500181WP 1995 9 15 95FDEA01277 119950822A5280ANB73871 FRAME DOUG DC10 DC1030F 3023504WP CTR GEAR DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 LT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C. 2L73 4F RTA22WE 19950915001821995091500182WP 1995 9 15 95FDEA01278 119950824A5520 FITTING DOUG DC10 DC1030F 3023504WP LT ELEVATOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 LT DETACHABLE ELEVATOR, AFT BAYONET LATCH ASSY LOOSE IN FITTING, WORN C/W SB 55-9 AND EA NR 8-5520-25165. OPEN SKIN, REPLACED FITTINGS AND LATCHES. SKIN AND PANELS OPS CHECK OK. 2L73 4F RTA22WE 19950915001831995091500183WP 1995 9 15 95FDEA01279 119950824A5520 FITTING DOUG DC10 DC1030F 3023504WP RT ELEVATOR WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 RT DETACHABLE ELEVATOR'S BAYONET LATCHES ARE LOOSE, WORN FITTINGS C/W S/B 55-9 AND EA NR 8-5520-25164. REPLACED FITTINGS AND LATCHES, OPENED AND CLOSED SKIN AND SEAL EDGES. ELEV OPS CHECK OK. 2L73 4F RTA22WE 19950915001841995091500184WP 1995 9 15 95FDEA01280 119950824A5753 FITTING DOUG DC10 DC1030F 3023504WP RT TE FLAP LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 RT WING O/B FLAP I/B SUPPORT FITTING TO REAR SPAR IS SUSPECTED LOOSE, MEASURED GAP 0.003. REMOVED O/B FLAP AND INSPECTED SUPT FITTING HOLES FOR CRACKS, NO DEFECTS NOTED. INSTALLED NEW STUDS AND PLI WASHERS AS PER MM 20-20-01 PG 202. REINSTALLED FLAP, FITTINGS AND SEALED. 2L73 4F RTA22WE 19950915001851995091500185WP 1995 9 15 95FDEA01281 119950902A5543 SKIN DOUG DC10 DC1030F 3023504WP RUDDER TAB LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25310FE 48299 LIGHTNING STRIKE, TOP OF UPPER RUDDER TAB RT SIDE, APPROX .25 INCH HOLE BURNED THROUGH ALUMINUM SKIN. FABRICATED DOUBLER PER SRM 55-00-01, WEIGHT CHANGE PLUS 1.502. RESTAMPED PLACARD TO ACTUAL WT OF RUDDER AS REQ SRM 55-40-02, PRIMED AND PAINTED PER SRM 51-21-02. 2L73 4F RTA22WE 19950915001861995091500186NM 1995 9 15 95UAL900123 119950911A3350 EEL STRIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29202UA 24717 EEL LIGHTS BROKEN LOOSE FROM FLOOR TRACK. RESECURED STRIP. 2L72 4F4 FRTA16WE E2GL 19950915001871995091500187NM 1995 9 15 95UAL900124 119950911A24322434930B BATTERY BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE BATTERY COMPT FAILED A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29937UA 26668 DIVERTED TO OAK AND LANDED UNDER AMBER ALERT, DUE TO SMOKE IN THE CABIN. REPLACED STORAGE BATTERY AND CHARGER, CHARGER CHECKS OK. BATTERY CHARGER WIRING ON A/C CHECKED OK. SUBMITTER STATES, SOURCE OF SMOKE LIKELY DUE TO BATTERY. 2L72 4F4 FRTA16WE E2GL 19950915001881995091500188NM 1995 9 15 95UAL900125 119950911A3350 EEL BATTERY BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP294728U 19925 DOOR MOUNTED EMERGENCY LIGHTS AT SEVERAL MAIN ENTRY DOORS INOP. REPLACED CONNECTOR, BATTERY PACK AND REPAIRED DAMAGED SPLICE. 2L74 4F4 F A20WE E20EA 19950915001891995091500189SO 1995 9 15 COMA9511959 119950907A73123039173 FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE CRACKED A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01137H 14011 120137 115270 FUEL LEAKING FROM RIGHT ENGINE NACELLE. REMOVED AND REPLACED RIGHT ENGINE FUEL HEATER WITH SERVICEABLE UNIT. 2L72 4T4 TRTA31SO E20NE 19950915001901995091500190EU 1995 9 15 COMA9531148 119950906A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU MAIN WHEEL R1 SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01347C AUG930545 340A028 MECHANIC REMOVED WHEEL ASSY DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950915001911995091500191EU 1995 9 15 COMA9531149 119950906A32465009237 INNER RACE 5010488 SAAB SF340 SF340A 7850100EU MAIN WHEEL R1 SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01158C MAR89D668 340A158 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING VISUAL INSPECTION FOUND INNER RACE SPUN. SUBASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950915001921995091500192 1995 9 15 COMA9531150 419950907A34176224401001 AIR DATA COMP SAAB SF340 SF340A 7850100EU AVIONICS RACK INOPERATIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01359CA17161 340A053 CAPTAINS AIRSPEED INDICATOR WAS SPINNING ON TAKEOFF ROLL. REMOVED AND REPLACED AIR DATA COMPUTER WITH SERVICEABLE. 2L72 4T RTA52EU 19950915001931995091500193EU 1995 9 15 COMA9531151 119950907A61208542M2 COMPUTER SAAB SF340 SF340A 7850100EU AUTO-COARSEN INOPERATIVE A COMAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 SO01342CA4697 340A023 DURING TAKEOFF ROLL, AUTO-COARSEN WARNING LIGHT ON CENTRAL WARNING PANEL CAME ON, ABORTED TAKEOFF. REMOVED AND REPLACED AUTO-COARSEN COMPUTER WITH SERVICEABLE UNIT. 2L72 4T RTA52EU 19950915001941995091500194NM 1995 9 15 DL72S953591 119950820A5754 RIB BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814. 2L73 4F A3WE 19950915001951995091500195NM 1995 9 15 DL72S953633 119950906A5754 RIB BOEING727 727232 1384082NM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807. 2L73 4F A3WE 19950915001961995091500196NM 1995 9 15 DL72S953636 119950907A5754 ANGLE BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 6 SLAT, .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A. 2L73 4F A3WE 19950915001971995091500197NM 1995 9 15 DL72S953641 119950908A5754651622373 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 DURING SHOP INSPECTION, NR 2 L/E SLAT WAS FOUND WITH SUPPORT RIB NR 2, 20 INCH CRACK. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19950915001981995091500198NM 1995 9 15 DL72S953642 119950908A5754651622373 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 DURING SHOP INSPECTION, NR 2 L/E SLAT WAS FOUND WITH RIB NR 5 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950915001991995091500199NM 1995 9 15 DL72S953643 119950906A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11419DA 21272 DURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLAT. 2L73 4F A3WE 19950915002001995091500200NM 1995 9 15 DL72S953655 119950909A3350 EEL BULB 81 BOEING727 727232 1384082NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11470DA 20747 DURING LAYOVER, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOP. C/A RELAMPED BOTH BULBS, OPERATION NORMAL. 2L73 4F A3WE 19950915002011995091500201NM 1995 9 15 DL72S953656 119950909A3350900835A EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11470DA 20747 DURING LAYOVER, FOUND C-2 CARGO DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950915002021995091500202NM 1995 9 15 DL72S953658 119950818A5744 FITTING BOEING727 727232 1384082NM NR 2 SPOILER LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 THE NR 2 SPOILER ACTUATOR SUPPORT FITTING LOWER TWO ATTACH BOLTS, AT REAR SPAR ARE VERY LOOSE IN MOUNT LUGS. REPAIRED PER MM 57-42-00 PG 804 STEP D. 2L73 4F A3WE 19950915002031995091500203NM 1995 9 15 DL72W953667 119950905A3350 EEL WIRES BOEING727 727247 138408FNM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11291WA 22109 DURING LAYOVER, FLOOR ESCAPE PATH LIGHTS INOP AT ROWS 11 TO 20. FOUND BROKEN WIRE IN TRACK, SPLICED WIRE AND OPERATION NORMAL. 2L73 4F A3WE 19950915002041995091500204NM 1995 9 15 DL757953651 119950908A2913 PUMP 731966 BOEING757 757232 1384965NM HYD SYSTEM FAILED A DALAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO11666DN MX507103 25034 PRIOR TO TAKEOFF, ELECTRICAL PUMP OVERHEAT LIGHT ILLUMINATED, FOLLOWED BY A LOSS OF ALL LEFT HYD QUANTITY. MAINTENANCE INSPECTION FOUND FLUID LEAKING OUT OF PUMP SPLINE DRAIN. THE FLUID LEAKED INTO ELECTRICAL PORTION OF PUMP AND NOTICED ARCING AND A BURNING SMELL. PUMP WAS REPLACED, OPERATION NORMAL. 2L72 4F RTA2NM 19950915002051995091500205WP 1995 9 15 DLL15953653 119950909A32331535927105 ACTUATOR 1535927105 LKHEED1011 10113853 5265020WP LT MLG CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11756DR M0414 193Y1185 THE C-HYDRAULIC SYSTEM FAILED WHEN GEAR EXTEND FOR LANDING. FOUND MLG ACTUATOR HOUSING CRACKED. REPLACED MLG ACTUATOR PER MM 32-32-01, OPS AND LEAK CHECK OK. 2L73 4F A23WE 19950915002061995091500206WP 1995 9 15 DLL15953663 119950909A323311523107105 ACTUATOR LKHEED1011 10113853 5265020WP LT MLG BROKEN A DALAO OTHER J WARNING INDICATION APAPPROACH 1 SO11756DR 193Y1185 ON APPROACH, WHEN GEAR LOWERED GOT IN TRANS AND LT GEAR DOOR LIGHTES, NO GREEN LIGHT FOR LEFT GEAR. CYCLED GEAR GOT NORMAL INDICATION, LANDED CVG. FOUND LEFT MLG JURY BRACE ACTUATOR BROKEN. REPLACED SAME, OPERATION NORMAL. 2L73 4F A23WE 19950915002071995091500207WP 1995 9 15 DLL16953652 119950908A3350RPS1 EEL POWER SUPPLY LKHEED1011 10113853 5265020WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11760DH 0315 193Y1194 DURING SERVICE CHECK, AFT CABIN FLOOR TRACK LIGHTS INOP. REPLACED AFT BATTERY AND POWER SUPPLY. 2L73 4F A23WE 19950915002081995091500208WP 1995 9 15 MWEA 95296 119950905A3350S103D EEL BATTERY DOUG DC9 DC914 3022034WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, THE EMERGENCY EXIT LIGHTS ABOVE RIGHT EMERGENCY EXIT AND THE COCKPIT EMERGENCY EXIT LIGHTS WERE VERY DIM DURING TEST. MAINTENANCE REPLACED BATTERIES IN FWD BATTERY PACK, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002091995091500209WP 1995 9 15 MWEA 95298 119950909A52109915565159 ANGLE DOUG DC9 DC932 3022066WP AFT ENT DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31501ME 47132 DURING C-CHECK, FOUND AFT ENTRANCE DOOR HAD 3 CRACKS INTERNALLY. THE FITTING ON RIGHT END FRAME APPROX 1 INCH LENGTH, THE RIGHT CENTER STOP AREA LOWER HORIZONTAL ATTACH ANGLE APPROX .75 INCH LENGTH, AND THE RIGHT HAND PAN STA Z35.0, .25 INCH AT ONE FASTENER. MAINTENANCE REPLACED ANGLES ON END FRAME AND CENTER STOP AREAS IAW SRM 51-30-2. THE PAN WAS REPAIRED WITH DOUBLER IAW 52-01 FIG 2 SHT 3 OF SRM. REINSTALLED DOOR, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002101995091500210WP 1995 9 15 MWEA95287 119950905A5532 SKIN DOUG DC9 DC914 3022034WP VERT STAB ERRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, THE VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER THE LEFT FWD HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 51-10-2A, 51-30-2, 51-30-5, 55-30-0. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002111995091500211WP 1995 9 15 MWEA95288 119950905A5311 FRAME DOUG DC9 DC914 3022034WP BS 897 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3145725 45725 DURING INSPECTION, FOUND FORMER AT STA 897 AND L16R CRACKED AT UPPER AND LOWER EDGES. MAINTENANCE REMOVED AND REPLACED FORMER IAW SRM 53-01 PG 1. ALSO, FABRICATED AND INSTALLED NEW FITTING IAW DAC DRWG 3959083. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002121995091500212WP 1995 9 15 MWEA95289 119950905A5311 FORMER DOUG DC9 DC914 3022034WP BS 880 CRACK A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, FOUND FORMER AT STA 880 AND L17R HAS A CRACK EMANATING FROM HOLE TO EDGE OF FORMER. MAINTENANCE INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002131995091500213WP 1995 9 15 MWEA95290 119950905A531327779225 LONGERON DOUG DC9 DC914 3022034WP BS 908 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, FOUND LONGERON 16L CRACKED AT STA 908 AFT ACCESSORY COMPARTMENT. MAINTENANCE REMOVED AND REPLACED LONGERON SECTION AT STA 908 WITH (P/N 27779225) IAW SRM 53-10-4 FIG 8 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002141995091500214WP 1995 9 15 MWEA95291 119950905A53152912758 FLOORBEAM DOUG DC9 DC914 3022034WP BS 817 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, THE FLOORBEAM AT STA 817 WAS FOUND MODERATELY CORRODED IN 3 AREAS. MAINTENANCE REPLACED UPPER BEAM CAP IAW SRM 53-30 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002151995091500215WP 1995 9 15 MWEA95292 119950905A53465917717 FITTING DOUG DC9 DC914 3022034WP AFT ENGINE MOUNTCRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, FOUND FITTING FOR AFT UPPER ENGINE MOUNT CRACKED AT STA 859. MAINTENANCE FABRICATED NEW FITTING IAW DAC DRAWING 5917717 AND INSTALLED IAW SRM 53-01 PG 1. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002161995091500216WP 1995 9 15 MWEA95293 119950905A5320 PRESS PANEL DOUG DC9 DC914 3022034WP BS 83 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, FOUND CRACK STA 83 IN NOSE GEAR WELL PRESSURE PANEL RUNNING UNDER CUSP ANGLE ON BOTH LEFT AND RIGHT SIDES OF GEARWELL. MAINTENANCE INSTALLED REPAIR DOUBLER, .020 CRES MATERIAL IAW SB 53-187 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002171995091500217WP 1995 9 15 MWEA95294 119950905A532039164311 SPLICE DOUG DC9 DC914 3022034WP BS 897 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, FOUND LONGERON SPLICE 13R AT STA 897 CRACKED IN TWO PLACES. MAINTENANCE REMOVED AND REPLACED LONGERON SPLICE 39164311, IAW SRM 53-10. 2L72 4F A6WE 19950915002181995091500218WP 1995 9 15 MWEA95295 119950905A5532 SKIN DOUG DC9 DC914 3022034WP VERT STAB ERRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER LEFT AFT HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 55-30-0 FIG 7, 55-01 FIG 4 SHT 2. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002191995091500219NM 1995 9 15 MWEA95297 119950908A25605956953403 SLIDE COVER DOUG MD88 MD88 3023688NM AFT GALLEY DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31701ME 49760 CREW REPORTS, COVER FOR AFT GALLEY DOOR EVACUATION SLIDE FELL OFF. MAINTENANCE REINSTALLED AFT GALLEY DOOR EVACUATION SLIDE COVER AND RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950915002201995091500220WP 1995 9 15 MWEA95299 119950910A3350 EEL SOCKETS DOUG DC9 DC932 3022066WP CABIN DIRTY A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31501ME 47132 DURING C-CHECK, FOUND EMERGENCY EXIT LIGHTS ABOVE AFT FLIGHT ATTENDANTS SEAT VERY DIM. MAINTENANCE CLEANED LIGHT SOCKETS AND LENS, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915002211995091500221WP 1995 9 15 MWEA95300 119950910A5530 ANGLE DOUG DC9 DC932 3022066WP VERT STAB CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31501ME 47132 DURING C-CHECK, FOUND RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED BETWEEN AND EXTENDING BEYOND TWO FASTENERS NEAR AFT SPAR OF VERTICAL STABILIZER. 2L72 4F A6WE 19950915002221995091500222NE 1995 9 15 P5CA9500768 219950909A7200JT9D7A ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 FLAMED-OUT A P5CAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 WP23850FT56723711 19755 685654 DURING LEVEL OFF FL 370, THE NR 4 ENGINE FLAMED-OUT. RESTART AT FL 190, ENGINE OPERATED NORMAL FOR REMAINDER OF FLIGHT. TROUBLESHOOTING PER MAINTENANCE MANUAL 71-00-42 PG 118. ALL ITEMS FOUND NORMAL, AIRCRAFT RELEASED. 2L74 4F4 F A20WE E20EA 19950915002231995091500223NM 1995 9 15 P5CA9500769 119950913A2710 AILERON CONTROLS BOEING747 747122 1384872NM RIGHT LOCKED OUT A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23850FT 19755 DURING DEPARTURE, RIGHT OUTBOARD AILERON WAS LOCKED OUT. RETURNED TO BLOCKS, RECYCLED FLAPS AND OPERATION NORMAL. 2L74 4F A20WE 19950915002241995091500224NM 1995 9 15 UPS204365 119950907A2910 HYD LINE BOEING727 727247 138408FNM NR 2 B-PUMP FAILED A IPXAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO01209UP 21698 BTB - PILOT REPORTED, DURING TAXI OUT FOR T/O THE NR 2 B-PUMP LOW PRESSURE LIGHT CAME ON, FOLLOWED BY THE NR 1 B-PUMP LOW PRESSURE LIGHT, 2 MIN LATER. THEN THE B SYSTEM PRESSURE DROPPED TO ZERO. THE BRAKE PRESSURE DROPPED TO 1,000 PSI, ACCUMULATOR PRECHARGE AND THE A-SYSTEM QUANTITY DROPPED STEADILY 70, MAINTAINED 2.5 GALLONS. THE B-SYSTEM QUANTITY DROPPED TO 1.5 GALLONS FROM FULL AND HELD STEADY. BRAKE EFFECTIVENESS STEADILY DETERIOATED UNTIL ALL BRAKE ACTION WAS LOST. FOUND PRESSURE LINE ON B-PUMP NR 2 BLOWN. REPLACED LINE, LEAK CHECKS OK. OPERATED BRAKES AND ASSOCIATED HYD SYSTEMS, NO DEFECTS NOTED AND SERVICED HYD SYSTEM. 2L73 4F A3WE 19950915002251995091500225NM 1995 9 15 UPS204367 119950911A5313 STRINGER BOEING747 747123 1384873NM BS 1500-1520 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT STR 33 BETWEEN 'B' STA 1500 TO 1520, CORRODED AND CRACKED. CORROSION AND CRACK ARE OUT OF LIMITS PER SRM 53-10-07. REMOVED DAMAGE STR PARTS FROM 'B' STA 1510 TO 1530 AND REPAIRED ACC SRM 53-10-03 FIG 1. 2L74 4F A20WE 19950915002261995091500226NM 1995 9 15 UPS204368 119950911A5313 STRINGER BOEING747 747123 1384873NM BS 1940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND AT 'B' STA 1940 RT SIDE STRINGER 34 CORRODED AND CRACKED. CORROSION AND CRACK WHERE OUT OF LIMITS PER SRM 53-10-07. REPAIRED STR 34 AT 'B' STA 1940 PER SRM 53-10-03 FIG 2. 2L74 4F A20WE 19950915002271995091500227NM 1995 9 15 UPS804364 119950906A4900 APU BOEING757 75724APF 1384969NM EMPENNAGE MALFUNCTION A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01422UP 25324 PILOT REPORTED, A/C DID AIR TURNBACK DUE TO APU AUTO-SHUTDOWN IN FLIGHT. THIS LEFT A/C WITH ONLY ONE OPERATING GENERATOR DUE TO LEFT ENGINE GENERATOR BEING ON DEFERRAL (M-97875). BITE CHECKED APU, FOUND REVERSE FLOW SHUTDOWN FAULT WITH NO LRU FAULTS. REPLACED LEFT ENG IDG IAW MM 24-11-1, OPS CKS OK AND THIS CLEARED M 97875. REPLACED APU SURGE BLEED VALVE IAW MM 49-53-1 AND APU FLOW SENSOR MODULE IAW MM 49-53-8, OPS CHECKS OK. 2L72 4F RTA2NM 19950915002281995091500228WP 1995 9 15 UPS804366 119950909A2121 FAN DOUG DC8 DC871F 302199DWP COCKPIT FAILED A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO01703UP 45939 PILOT REPORTED, ELECTRICAL SMOKE SMELL IN COCKPIT ON APPROACH TO SDF. TURNING OFF RECIRC FAN CLEARED SMELL. T/S AND FOUND RECIRC FAN MOTOR HAD BURNED UP AND WOULD NOT RESET. DEFERRED RECIRC FAN ORDER MEL 21-16. 2L74 4F RT4A25 19950915002291995091500229WP 1995 9 15 UPS804369 119950911A57535652287505 VANE DOUG DC8 DC871F 302199DWP LT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT WING TRAILING EDGE INBD FLAP, INBD FLAP VANE DELAMINATED ON LOWER SURFACE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950915002301995091500230WP 1995 9 15 UPS804370 119950911A531597540222 FLOORBEAM DOUG DC8 DC871F 302199DWP FS 340 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FLOORBEAM END FITTING CRACKED AT FS 340, LONGERON 21 RT. REPLACED FITTING PER SRM 51-1. 2L74 4F RT4A25 19950915002311995091500231WP 1995 9 15 UPS804371 119950911A57125770123 LE RIB DOUG DC8 DC871F 302199DWP RT WING CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE RIBS, 3 EA CRACKED AT WS XFS 346, XFS 397 UPPER, AND XFS 416 UPPER. REPAIRED RIBS PER SRM 57-2-0. 2L74 4F RT4A25 19950915002321995091500232WP 1995 9 15 UPS804372 119950911A57535701152502 VANE DOUG DC8 DC871F 302199DWP RT TE FLAP DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING NR 4 FLAP VANE DELAMINATED ON INBD LOWER SURFACE. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19950915002331995091500233WP 1995 9 15 UPS804373 119950911A53115772958 FRAME DOUG DC8 DC871F 302199DWP FS 220-240 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 2 BELT FRAMES CRACKED AT FS 220 AND 240, BETWEEN LONGERONS 334 TO 34R. REPAIRED FRAMES PER SRM 53-2-0. 2L74 4F RT4A25 19950915002341995091500234WP 1995 9 15 UPS804374 119950911A532010322424T3 DOUBLER DOUG DC8 DC871F 302199DWP FS 450 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 450 FINGER DOUBLER CRACKED BETWEEN LONGERONS 31L AND 31R. REPLACED DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19950915002381995091500238NM 1995 9 15 DL757953250 119950731A49007321387009 CONNECTOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE APU INLET DOOR LOOSE A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO11683DA14260 27103 APU QUIT INFLIGHT WITH APU FAULT LIGHT. NR 2 IDG WAS ON MCO/PLAC AS INOPERATIVE, RETURNED TO ATL. APU EEC FAULTS APU INLET DOOR. REPLACED DOOR ACTUATOR, NO HELP. MANUALLY OPENED DOOR AND RESEATED CANNON PLUG. APU START AND OPERATION NORMAL. NR 2 IDG CONTROL PANEL WAS REPLACED, OPERATION NORMAL. 2L72 4F4 FRTA2NM E17NE 19950915002391995091500239EU 1995 9 15 REXA95036 119950429A53477253799378 SEAT TRACK SAAB SF340 340B 7860101EU FS 638 CORRODED A REXAK NONE O OTHER ININSP/MAINT 1 SO25365PX 340B265 LAV CENTER SEAT TRACK FS 638 HAS MAJOR CORROSION DAMAGE LOWER FLANGE. CUT CENTER TRACK AT FS 620 REMITTING BACK TO FS 686 DRILLED UP NEW SEAT TRACK SECTION AND DOUBLER AND INSTALLED REPAIR PART IAW SRM 53-70-60. (Z) 2L72 4T RTA52EU 19950915002401995091500240EU 1995 9 15 REXA029 119950303A261251653151 FIRE CONTL UNIT BAG JETSTMJETSTM3101 1500215EU RT ENGINE MALFUNCTIONED A REXAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO25332PX 702 RIGHT ENGINE FIRE LIGHT ILLUMINATED, SECURED ENGINE AND COMPLIED WITH CHECK LIST. REMOVED AND REPLACED FIRE DETECTOR CONTROL UNIT, JAW JSMM 26-10-15, FUNCTIONAL CHECK DONE IHW JSMM 26-10-0, OPS CHECK GOOD. (Z) 2L72 4T RTA21EU 19950915002411995091500241EU 1995 9 15 REXA95037 119950501A301029S7D514104 BOOT SAAB SF340 SF340A 7850100EU LT WING TORN A REXAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SO25323PX 340A046 SHUT LEFT ENGINE DOWN DUE TO VIBRATION. VIBRATION CAUSED BY LEFT WING O/B DE-ICE BOOT TORN AND SEPERATED FROM WING. RESECURED BOOT TO WING AND DEFERRED DE-ICE BOOT SYSTEM UNTIL BOOT CAN BE REPLACED. NO DEFECTS NOTED WITH THE LEFT ENGINE. (Z) 2L72 4T RTA52EU 19950915002421995091500242NE 1995 9 15 REXA95038 219950511A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT BIRD STRIKE A REXAK NONE C F.O.D. UKUNKNOWN 1 SO25106PX 340A106 BIRD FOUND ON LEFT OIL COOLER ON POST FLIGHT. REMOVED AND REPLACED LEFT ENGINE IAW AMM 71-00-00 DUE TO BIRD INGESTION. (Z) 2L72 4T4 TRTA52EU E8NE6 19950915002431995091500243EU 1995 9 15 REXA95039 119950512A3241 ANTI-SKID SYST SAAB SF340 SF340A 7850100EU MLG MALFUNCTIONED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25922MA 340A077 ON TAXI INTO GATE, LOST BRAKE'S. TURNED ANTI-SKID OFF, BRAKES RETURNED. CHECKED AND CLEANED ALL ELECTRICAL CONNECTORSREF AMM 32-43-00. NO FAULTS DETECTED, OPS CHECKED GOOD ACFT OK FOR SERVICE. (Z) 2L72 4T RTA52EU 19950915002441995091500244EU 1995 9 15 REXA95040 119950512A324114004120 ANTI-SKID SYST SAAB SF340 SF340A 7850100EU RT MLG BROKEN A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25922MA 340A077 LOST BRAKES WHEN TAXIING INTO RAMP. TURNED OF ANTI-SKID BRAKES, RETURNED. REMOVED AND REPLACED LT I/B AND O/B TRANSDUCER. REMOVED AND REPLACED I/B AND O/B HUB CAPS, BOTH CLIPS WERE BROKEN. ACFT OK FOR SERVICE. (Z) 2L72 4T RTA52EU 19950915002451995091500245WP 1995 9 15 REXA95041 219950409A72003103301 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A REXAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 SO25316PX 687 P63082 LT ENGINE FAILED IN FLIGHT. REMOVED AND REPLACED LT ENGINEIAW JS MM 71-00-00 OPS AND LEAK CHECK GOOD. (Z) 2L72 4T4 TRTA21EU E4WE 19950915002461995091500246EU 1995 9 15 REXA95042 119950518A3350N1112201 EEL WIRE SAAB SF340 SF340A 7850100EU CABIN FAILED A REXAK NONE L NO TEST ININSP/MAINT 1 SO25407BH 340A078 EMERGENCY LIGHT NR 7 CIRCUIT BREAKER OUT, WON'T RESET. REPAIRED WIRE TO RAYCHEM CONNECTOR AND RESET NR 7 CIRCUIT BREAKER, CHECKED SYSTEM IAW AMM. (Z) 2L72 4T RTA52EU 19950915002471995091500247EU 1995 9 15 REXA95029 119950303A261251653151 FIRE CONTL UNIT BAG JETSTMJETSTM3101 1500215EU RT ENGINE MALFUNCTIONED A REXAE ENGINE SHUTDOWN N FALSE WARNING APAPPROACH 1 SO25332PX 702 RIGHT ENGINE FIRE LIGHT ILLUMINATED, SECURED ENGINE AND COMPLIED WITH CHECK LIST. REMOVED AND REPLACED FIRE DETECTOR CONTROL UNIT, JAW JSMM 26-10-15, FUNCTIONAL CHECK DONE IHW JSMM 26-10-0, OPS CHECK GOOD. (Z) 2L72 4T RTA21EU 19950915002481995091500248NM 1995 9 15 95FDEA1046 119950728A5313BAC1498131 STRINGER BOEING727 727232 1384082NM BS 739 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25497FE 20866 CORROSION FWD BAY, ON STR 27L AT BS 739 IN BILGE, ACCESS IS REQ. ACCESSED REPAIR AREA, REMOVED CORRODED END OF STR, FABRICATED AND INSTALLED REPAIR PARTS AT BS 739 WL 145 STR 27L PER FEDEX SRM 53-10-3 AND RESTORED ACCESSED ITEMS TO NORMAL CONFIGURATION. 2L73 4F A3WE 19950915002491995091500249NE 1995 9 15 95FDEAOO604 219950523A7250 TURBINE BOEING727 727233 138408ANM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A FDEAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 SO25263FE 21625 MAX T10 POWER, AFTER GEAR RETRACT. NR 2 ENGINE TURBINE FAILED HIGH N1, 700 DEGED EGT. REMOVED AND REPLACED NR 2 ENGINE. 2L73 4F4 FRTA3WE E2EA 19950915002501995091500250NM 1995 9 15 95FDEAOO734 119950616A5311 FRAME BOEING727 72722C 138400FNM BS 560 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 DENTED FRAME AT BS 560, STR 6 RT. REPAIRED DENTED FRAME IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19950915002511995091500251NM 1995 9 15 95FDEAOO735 119950616A532070750T6 SHEAR TIE BOEING727 72722C 138400FNM BS 640 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 CRACKED AND DAMAGED SHEAR TIE AT BS 640, LT STR 8. REPAIRED DAMAGED SHEAR TIE IAW FEDEX EA 7-5310-24654. 2L73 4F A3WE 19950915002521995091500252NM 1995 9 15 95FDEAOO736 119950616A5315BAC150529222 FLOORBEAM BOEING727 72722C 138400FNM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 NRO-777, CORROSION ON TOP CHORD OF FLOORBEAM AT BS 344 RBL 20 TO LBL 60 WL 208 STR 8. REMOVED TOP CHORD FLOORBEAM AT BS 344 RBL 70 TO LBL 70 WL 208 STR 8, IAW FEDEX REPAIR DRAWING NR SR27-53-007, DUE TO TOP CHORDS OF FLOORBEAM OUT OF LIMITS. 2L73 4F A3WE 19950915002531995091500253NM 1995 9 15 95FDEAOO737 119950616A53207075T6 ANGLE BOEING727 72722C 138400FNM BS 310-343 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 NRO-777, CORROSION AROUND NUTPLATES ON FORWARD ENTRY DOOR AT BS 310 TO 343 LBL 62 WL 309. REMOVED CORRODED SUPPORT AT BS 310 TO 343 LBL 62 WL 309, IAW FEDEX SRM 51-IC-1. 2L73 4F A3WE 19950915002541995091500254NM 1995 9 15 95FDEAOO738 119950616A5347BAC15201434 SEAT TRACK BOEING727 72722C 138400FNM BS 344-349 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 NRO-780, CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 344 TO BS 349 LBL 58 WL 208.1, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-01. INSTALLED NEW ONE. 2L73 4F A3WE 19950915002551995091500255NM 1995 9 15 95FDEAOO739 119950616A5347BAC15201434 SEAT TRACK BOEING727 72722C 138400FNM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 NRO-781, CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1. REMOVED CORROSION ON SEAT TRACK FLANGE AT BS 360 LBL 60 WL 208.1, IAW FEDEX SRM 53-10-01. 2L73 4F A3WE 19950915002561995091500256NM 1995 9 15 95FDEAOO740 119950616A53117075HTT6 FRAME BOEING727 72722C 138400FNM BS 380 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25104FE 19198 (NRO 783) MECHANICAL DAMAGE TO FRAME AT BS 380, STR 7 L/H WL 280 CORRECTIVE ACTION FOUND DAMAGE TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED FRAME AT STATION 380 STR 7 L/H WL 280 PER FEDEX SRM 53-10-4 . 2L73 4F A3WE 19950915002591995091500259CE 1995 9 15 95ZZZX4508 119950812A326063210075 SWITCH CESSNA402 402C 207590RCE RT UPLOCK OUT OF RIG A SQFAK NONE N FALSE WARNING ININSP/MAINT 1 SO175736C 402C0031 PILOT REPORTED WITH THE GEAR IN THE UP POSITION, THE RED UNSAFE LIGHT FAILED TO EXTINGUISH. AIRCRAFT JACKED AND GEAR OPERATED. FOUND RT GEAR UPLOCK SWITCH NEEDED ADJUSTMENT. SWITCH ADJUSTED IAW SECTION 32 OF THE CESSNA SM. GEAR OPERATED SEVERAL MORE TIMES, OPERATION NORMAL. AIRCRAFT TEST FLOWN, OPERATION NORMAL. 1L72 3O A7CE 19950915002941995091500294NM 1995 9 15 95ZZZX4543 119950611A3810417T200815 SUPPORT ROD O1261014211 BOEING767 76735H 1385208NM WATER TANK BROKEN B GJPYK NONE K FLUID LOSS ININSP/MAINT 1 WP33800CZ5729 5729 ADCN3 26389 THE CREW REPORTED THERE WAS WATER LEAKAGE. AFT-FLIGHT CHECK FOUND FOUR RODS FOR LEFT WATER TANK SUPPORT BROKEN AND THE SUPPORT CRACKED. THE AIR TUBE BESIDE THE WATER TANK WAS PRESSED OUT OF SHAPE. RECOMMEND TO REPLACE THE FOUR RODS AND REPAIR THE WATER TANK SUPPORT AS WELL AS THE AIR TUBE. 2L72 4F RTA1NM 19950915003001995091500300NE 1995 9 15 95ZZZX4549 219950704A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67 52043NE LT ENGINE FAILED A NVEAE ENGINE SHUTDOWN Y ENGINE STOPPAGE APAPPROACH 1 SO03160DD SH3723 106014 BWI - STA 4923 - CREW REPORTS - CREW AND PASSENGERS HEARD LOUD SOUND. CAPTAIN THEN NOTICED THE LT ENGINE EGT WAS 800 DEGREES WITH THE TORQUE DECREASING. LT POWER LEVER WAS PULLED BACK AND THE EGT STAYED AT 800 DEGREES, LT ENGINE WAS SHUT DOWN. AIRCRAFT WAS ON FINAL APPROACH INTO BWI. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. 2H72 4T4 T A41EU E26NE 19950915003011995091500301NM 1995 9 15 95ZZZX4550 119950727A2760 SPOILER BOEING737 737214 138446RNM NR 7 REQUIRED ADJ A BJNAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP11457TM 20156 EKO - FLT 457 - AIRCRAFT ROLLED RIGHT 6 DEGREES AT 270 KIAS UPON INITIAL APP. OF SPEED BRAKE. ADJUSTED NR 7 SPOILER PANEL PER BMM 27-61-11. 2L72 4F A16WE 19950915003061995091500306WP 1995 9 15 9513809612 119950628A5320 DOUBLER DOUG DC9 DC932 3022066WP FS 917 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT CARGO DOOR JAMB DOUBLER FS 917. REPAIRED DOUBLER (P/N 5910158-25) PER EA 96-98092. 2L72 4F A6WE 19950915003071995091500307WP 1995 9 15 9513819612 119950628A533059114015 SKIN DOUG DC9 DC932 3022066WP FS 165 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE INNER FUSELAGE SKIN AT FS 165 LBL 5. REPAIRED SKIN (P/N 5911401-5), PER EA 96-98098. 2L72 4F A6WE 19950915003081995091500308WP 1995 9 15 9513829612 119950706A5320 DOUBLER DOUG DC9 DC932 3022066WP FS 427 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE MAIN CAIN RING PAN WINDOW BELT DOUBLERS, FS 427 AT LONGERON 14L AND FS 851 AT LONGERON 12L. REPAIRED BOTH (P/N 5912285-1), PER EA 96-98099. 2L72 4F A6WE 19950915003091995091500309WP 1995 9 15 9513839612 119950808A5312 BLKHD WEB DOUG DC9 DC932 3022066WP FS 1143 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A ONE INCH CRACK IN THE RUDDER SUPPORT CANTED BULKHEAD WEB AT FS 1143. REPAIRED WEB (P/N 9911842-101), PER EA 96-98122. 2L72 4F A6WE 19950915003101995091500310NM 1995 9 15 9513842704 119950814A5314 KEEL BEAM BOEING727 727225 1384077NM FS 950-1010 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01801EA 22432 DURING H-CHECK, FOUND CORROSION ON THE KEEL BEAM CHORDS STRINGERS 29R AND 29L FROM BS 950E TO 1010. REPAIRED STRINGERS (P/N 65-56441-4), PER EA 27-99059. 2L73 4F A3WE 19950915003111995091500311NM 1995 9 15 9513852704 119950825A5330 SKIN BOEING727 727225 1384077NM FS 490 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01801EA 22432 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN BS 490 BETWEEN STRINGERS 27L AND 27R. REPAIRED SKIN PER EA 27-99060. 2L73 4F A3WE 19950915003121995091500312WP 1995 9 15 9513861221 119950825A5330 SKIN DOUG DC10 DC1030 3023501WP FS 1690-1701 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 46579 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1690 TO 1701 AT LONGERON 52. REPAIRED SKIN PER EA 12-99028. 2L73 4F A22WE 19950915003131995091500313WP 1995 9 15 9513871221 119950825A5713 LONGERON DOUG DC10 DC1030 3023501WP WS 358 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 46579 DURING PERIODIC CHECK, FOUND A CRACK IN THE RIGHT WING STRINGER 41 AT XORS 358. REPAIRED STRINGER (P/N ARB 2541-2), PER EA 12-99032. 2L73 4F A22WE 19950915003141995091500314NM 1995 9 15 9513882204 119950828A5315 FLOORBEAM BOEING727 727251 138408HNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 22544 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1130 FLOOR BEAM UPPER CHORD. REPAIRED BEAM (P/N 65-20838-16), PER EA 22-99070. 2L73 4F A3WE 19950915003151995091500315WP 1995 9 15 9513891221 119950828A5330 SKIN DOUG DC10 DC1030 3023501WP FS 2000 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 46579 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 2000 FROM LONGERON 45R TO 46R. REPAIRED SKIN (P/N AJC 7164-502), PER EA 12-99212. 2L73 4F A22WE 19950915003161995091500316NM 1995 9 15 9513902704 119950830A5313 STRINGER BOEING727 727225 1384077NM BS 985 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01801EA 22432 DURING H-CHECK, FOUND CORROSION INSIDE STRINGER 30 AT BS 985. REPAIRED STRINGER (P/N 65-58387-3), PER EA 27-99063. 2L73 4F A3WE 19950915003171995091500317NM 1995 9 15 9513912704 119950830A5712 RIB BOEING727 727225 1384077NM BS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01801EA 22432 DURING H-CHECK, FOUND TWO CRACKS IN THE WING TO BODY UPPER RIB CHORD BS 760 RBL 70.5. REPAIRED PER EA 27-98961. 2L73 4F A3WE 19950915003181995091500318WP 1995 9 15 9513929922 119950831A5341 FITTING DOUG DC9 DC932 3022066WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING H-CHECK, FOUND CRACKS IN THE WING TO FUSELAGE ATTACH FITTING, RIGHT AND LEFT SIDES FS 604. REPAIRED FITTINGS (P/N 5910465-33, -34), PER EA 99-97123. 2L72 4F A6WE 19950915003191995091500319WP 1995 9 15 9513939922 119950901A5330 SKIN DOUG DC9 DC932 3022066WP FS 1076-1087 CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING H-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1076 TO 1087 BETWEEN LONGERONS 17L TO 18L. REPAIRED SKIN (P/N 5912870-501), PER EA 99-94921. 2L72 4F A6WE 19950915003201995091500320WP 1995 9 15 9513949922 119950901A5311 FRAME DOUG DC9 DC932 3022066WP FS 541 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING H-CHECK, FOUND CORROSION ON THE FS 541 FLOOR SUPPORT FRAME BETWEEN LONGERON 29L TO 29R. REPAIRED FRAME PER EA 99-97124. 2L72 4F A6WE 19950915003211995091500321WP 1995 9 15 9513951143 119950904A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1661-1681 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01133JC 46752 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1661 TO 1681, LONGERON 51L TO 51R AT THE ANTI-COLLISION LIGHT. REPAIRED SKIN PER EA 11-98921. 2L73 4F A22WE 19950915003221995091500322WP 1995 9 15 9513969946 119950905A5312 BULKHEAD DOUG DC9 DC931 3022065WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION BETWEEN THE LONGERON 29L AND 30 ATTACH CASTINGS AND THE FS 756 BULKHEAD. REPLACED BOTH CASTINGS PER SRM 51-01 AND DWG 3911418. 2L72 4F A6WE 19950915003231995091500323WP 1995 9 15 9513979970 119950905A5311 FRAME DOUG DC9 DC931 3022065WP FS 622 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019334 47247 DURING H-CHECK, FOUND CRACKS IN THE FS 622 FRAME ATTACH FITTINGS INBOARD OF LONGERON 24L. REPLACED FITTINGS PER SRM 51-10-02, 51-10-03, 51-30-0. 2L72 4F A6WE 19950915003241995091500324WP 1995 9 15 9513981143 119950905A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1721-1741 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01133JC 46752 DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1721 TO 1741, LONGERONS 51R TO 52 AT THE VHF ANTENNA. REPAIRED SKIN PER EA 11-67705. 2L73 4F A22WE 19950915003251995091500325WP 1995 9 15 9513999953 119950906A5320 FITTING DOUG DC9 DC931 3022065WP FS 758-760 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 758 TO 760. REPLACED END FITTING PER SRM 53-02 FIG 12. 2L72 4F A6WE 19950915003261995091500326WP 1995 9 15 9514009955 119950906A5341 FITTING DOUG DC9 DC931 3022065WP FS 598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING H-CHECK, FOUND CORROSION ON THE ATTACH FITTING BETWEEN THE FS 598 FRAME AND THE CENTER WING FORWARD SPAR. REPLACED THE FITTING PER SRM 51-30-1. 2L72 4F A6WE 19950915003271995091500327NM 1995 9 15 9514012285 119950903A7711 EPR IND BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01285US 21324 696474 NR 1 ENGINE EPR INDICATION FAILED TO REACH TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND CHECKED THE SYSTEM. SYSTEM OPERATION WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950915003281995091500328 1995 9 15 9514025507 419950908A2565D31038186 EVAC SLIDE BOEING757 757251 1384970NM DOOR 1L WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01507US284832932 23196 DURING OVERHAUL IN SHOP, THE EVACUATION SLIDE FROM DOOR 1L WAS FOUND WITH A HOLE WORN IN THE SILL TUBE. REPAIRED PER 25-66-01 PG 606-1 AND OVERHAULED SLIDE. WEAR CAUSED BY CHAFING AGAINST IPC REF 52-11-53-02 ITEM 129A. 2L72 4F RTA2NM 19950915003291995091500329NE 1995 9 15 9514036730 219950909A75307479555 EVC BOEING747 7472J9F 1384806NM PWA JT9 JT9D7F 52054NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01630US2975 21668 62629 DURING TAKEOFF, THE NR 1 ENGINE SLOW TO ACCELERATE WITH HIGH EGT AT 700 DEGREES. CREW FOLLOWED OPERATING MANUAL AND ABORTED TAKEOFF AT 40 KNOTS. MAINTENANCE REPLACED THE NR 1 ENGINE EVC, GROUND RUN TRIMMED, OPERATION AND LEAK CHECK TESTED NORMAL. 2L74 4F4 FRTA20WE E20EA 19950915003301995091500330WP 1995 9 15 9514049851 119950910A2131 CONTROLLER DOUG DC9 DC951 3022051WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01760NC 47708 AIRCRAFT FAILED TO AUTO PRESSURIZE AFTER TAKEOFF, CABIN ALTITUDE CLIMBED AT A RATE OF 2,000 FPM. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915003311995091500331WP 1995 9 15 9514059912 119950909A3231 STOP CABLE DOUG DC9 DC931 3022065WP NLG DOOR BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01962N 47406 LOUD NOISE WITH MODERATE VIBRATION OCCURRED FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR LINK AND STOP CABLE BROKEN. ALSO, DAMAGE TO DOOR WAS INCURRED. REPLACED LINK, CABLE, AND DOOR AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915003321995091500332WP 1995 9 15 9514069912 119950910A3231 DOOR LINK DOUG DC9 DC931 3022065WP NLG BROKEN A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01962N 47406 A LOUD NOISE WITH MODERATE VIBRATION OCCURRED FROM NOSE GEAR AREA AFTER TAKEOFF AND GEAR RETRACTION. FLIGHT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LEFT FORWARD NOSE GEAR DOOR LINK BROKEN AND DOOR GOUGED. ALSO, FOUND LEFT LOWER DOOR STOP CABLE BROKEN. REPLACED LEFT DOOR LINK, CABLE, AND DOOR. ALSO, REPLACED NOSE GEAR ACTUATING CYLINDER AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915003331995091500333WP 1995 9 15 9514079971 119950908A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAG O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 GL019335 47337 LOSS OF CABIN PRESSURIZATION OCCURRED DURING CLIMB THROUGH 29,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT THE CABIN, DESCENT WAS MADE TO 26,000 FEET AND PRESSURIZATION WAS REGAINED THROUGH MANUAL CONTROL. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT AND ACCOMPLISHED UNEVENTFUL LANDING. REPLACED THE CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915003341995091500334WP 1995 9 15 9514089971 119950908A3520 OXYGEN MASK DOUG DC9 DC931 3022065WP CABIN FAILED TO DEPLOYA NWAAG O2 MASK DEPLOYED J WARNING INDICATION CLCLIMB 1 GL0193335 47337 DURING OXYGEN MASK DEPLOYMENT DUE TO LOSS OF CABIN PRESSURIZATION, MASKS AT ROW 14 AND RIGHT AFT LAVATORY FAILED TO DEPLOY. ADJUSTED BOTH SYSTEMS TO PROPER LIMITS. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915003351995091500335WP 1995 9 15 9514099102 119950908A246092057802 TRANSFER RELAY DOUG DC9 DC915 3022036WP DC EMERGENCY PWRMALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0192S 47064 AFTER TAKEOFF, BOTH A AND B PHASE FUEL BOOST PUMP CIRCUIT BREAKERS POPPED, IN CONJUNCTION WITH LOSS OF SEVERAL AIRCRAFT COMPONENTS INCLUDING COMMUNICATIONS. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED DC CROSSTIE RELAY (R2-27) AND NR 1 AND NR 2 TRANSFORMER RECTIFIERS. ALSO, SWAPPED GENERATOR CONTROL PANELS, ALL WITH NO HELP. REPLACED DC EMERGENCY POWER TRANSFER RELAY (R2-19). SYSTEM CHECKED OK AND AIRCRAFT RETRUNED TO SERVICE. 2L72 4F A6WE 19950915003361995091500336NM 1995 9 15 95FDEA01282 119950901A5311 FRAME BOEING727 72722C 138400FNM BS 500 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 NR 0413 UPPER LOBE FRAME BENT 3 INCHES ABOVE RT FLOOR LINE STA 500. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER 51-40-3 PG 3. 2L73 4F A3WE 19950915003371995091500337NM 1995 9 15 95FDEA01283 119950907A5311 FRAME BOEING727 72722C 138400FNM BS 480 BENT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25105FE 19194 CORROSION LOWER SIDE OF FWD FLANGE STA 480 FLOOR FRAME RBL 3 TO 6. REMOVED CORROSION INSTALLED REPAIR PER 53-10-8 FIG 5 PG 31. 2L73 4F A3WE 19950915003381995091500338NM 1995 9 15 95FDEA01284 119950906A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 480-600 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN SEAT TRACK AT BS 480 TO 600 WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AT BS 480 TO 600 BL 0 WL 208.5. FABRICATED NEW SEAT TRACK AND INSTALLED AT BS 480 TO 600 BL 0 WL 208.5, REF FEDEX SRM 53-10-5. 2L73 4F A3WE 19950915003391995091500339NM 1995 9 15 95FDEA01285 119950906A53209086044 CLIP BOEING727 727232 1384082NM BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION STR CLIP BS 1166 STR 15L. REMOVED CORRODED STR CLIP AT BS 1166 STR 15L AND INSTALLED NEW STR CLIP AT BS 1166 STR 15L IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950915003401995091500340NM 1995 9 15 95FDEA01286 119950906A53117075T6050 FRAME BOEING727 727232 1384082NM BS 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED ON TOP AT BS 600 BETWEEN STR 26 TO 23L. ALSO, FACTORY SPLICE IS DENTED. REPAIRED FRAME AT BS 600 BETWEEN STR 26 TO 23L PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950915003411995091500341NM 1995 9 15 95FDEA01287 119950906A53117075T6071 FRAME BOEING727 727232 1384082NM BS 720 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY, FRAME DENTED AT BS 720C BETWEEN STR 25 TO 24L. REPAIRED DENTED FRAME AT BS 720C BETWEEN STR 24 TO 25L PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950915003421995091500342NM 1995 9 15 95FDEA01288 119950908A55302024T3050 WEB BOEING727 727232 1384082NM VERTICAL FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 1303 WEB IN BAY NR 1 IN VERTICAL FIN IS CRACKED LT LWR CORNER. REPAIRED CRACK IN 1303 WEB IN BAY NR 1 OF VERTICAL FIN LT LOWER CORNER, PER FEDEX DRAWING SR 27-53-015. 2L73 4F A3WE 19950915003431995091500343NM 1995 9 15 95FDEA01289 119950908A532069436951 SKIN SUPPORT BOEING727 727232 1384082NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY FOUND WHILE WORKING NR 0338 FUSELAGE 00117 SKIN SUPPORT AT BS 740 WL 145 TO 150 BETWEEN STR 28 TO 27L. CORROSION WAS FOUND TO BE OUT OF LIMITS. REMOVED OLD SKIN SUPPORT AND REPLACED WITH NEW SKIN SUPPORT IAW SRM 51-10-1, 53-10-1. 2L73 4F A3WE 19950915003441995091500344NM 1995 9 15 95FDEA01290 119950908A53117075T6003 FRAME BOEING727 727232 1384082NM BS 720 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD FRAME DENTED AND GOUGED ON TOP BS 720C AT STR 23 TO 24R. GOUGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED FRAME AT BS 720C STR 23 TO 24R, PER SRM 51-40-3. 2L73 4F A3WE 19950915003451995091500345NM 1995 9 15 95FDEA01291 119950908A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 344-480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN SEAT TRACK AT BS 344 AND 480 WL 208.5 BL 0. REMOVED CORROSION FROM SEAT TRACK BS 347 TO 415 BL 0 AND FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1. ALODINE AND PRIMED SEAT TRACK BS 347 TO 415 BL 0. ACCOMPLISHED SEAT TRACK REPAIR FROM BS 450 TO 480, IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950915003461995091500346NM 1995 9 15 95FDEA01292 119950912A572065185385 CHORD BOEING727 72722 1384002NM BS 870 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25195FE 19144 NR 0232 043. CORROSION C53-132-2(1) ON STA 870 LOWER CHORD LBL 70, 38-41, RBL 20, WL 156. REMOVED AND REPLACED BS 870 LOWER CHORD, LBL 70, WL 156 PER FEDEX EA 7-5710-29709. 2L73 4F A3WE 19950915003471995091500347NM 1995 9 15 95FDEA01293 119950911A532069436835 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY BS 720B STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND SHEAR TIE STA 720B STR 26 TO 27R WL 148 CORRODED BEYOND LIMITS PER FEDEX SRM 727 53-10-1. REMOVED AND REPLACED NEW SHEAR TIE. 2L73 4F A3WE 19950915003481995091500348NM 1995 9 15 95FDEA01294 119950911A53207075T6 SHEAR TIE BOEING727 727232 1384082NM BS 700 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY BS 700 STR 27 TO 28R ON THE SHEAR TIE. REMOVED DAMAGED SHEAR TIE AND INSTALLED FABRICATED SHEAR TIE. FOUND SHEAR TIE CORRODED OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950915003491995091500349NM 1995 9 15 95FDEA01295 119950911A53207075T6 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY BS 720A STR 27 TO 28R WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE BS 720A STR 27 TO 28R WL 148. FABRICATED, DRILLED, ALODINED, PRIMED, PAINTED AND INSTALLED SHEAR TIE PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950915003501995091500350NM 1995 9 15 95FDEA01296 119950911A5313655623612 STRINGER BOEING727 727232 1384082NM BS 680-720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FOUND WHILE WORKING NR 0450 ON STR 28L BS 680 TO 720 WL 145. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED STR 28L BS 680 TO 720 PLUS 3 WL 145. 2L73 4F A3WE 19950915003511995091500351NM 1995 9 15 95FDEA01297 119950911A53302024T3100 SKIN BOEING727 727232 1384082NM BS 580-600 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 WHILE WORKING NR 0448, FOUND CORROSION ON SKIN UNDER INTERCOSTAL AND LEVELING COMPOUND BS 580 TO 600 LBL 7 WL 147.5. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SKIN AT BS 580 TO 600 LBL 7 WL 147.5 IAW SRM 53-30-3. 2L73 4F A3WE 19950915003521995091500352NM 1995 9 15 95FDEA01298 119950911A532069436835 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY BS 720C STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND SHEAR TIE BS 720C STR 26 TO 27R WL 148 CORRODED BEYOND LIMITS PER FEDEX SR 727 53-10-1. REMOVED AND REPLACED SHEAR TIE. 2L73 4F A3WE 19950915003531995091500353NM 1995 9 15 95FDEA01299 119950911A53207075T6 WEB BOEING727 727232 1384082NM BS 344 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION ON WEB AT BS 344 WL 207 AND 208 RBL 6 LBL 46 AFT AND FWD SIDE, FOUND WHILE WORKING NR 0827 AFTER REMOVAL OF FLOORBEAM. REMOVED CORROSION ON WEB AT BS 344 WL 207 AND 208 RBL 6 LBL 46 AFT AND FWD SIDE, FOUND TO BE OUT OF LIMITS AT LBL 27-43. FABRICATED AND INSTALLED DOUBLER PER SRM FEDEX 51-40-2 AT LBL 27-43. 2L73 4F A3WE 19950915003541995091500354NM 1995 9 15 95FDEA01300 119950911A5751 TE WEDGE BOEING727 727232 1384082NM RT AILERON DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 RT WING O/B AILERON WEDGE HAS CREASED DENT ON UPPER SURFACE AND 2 DISBONDS ON T/E. REPAIRED RT WING O/B AILERON WEDGE IAW FEDEX SRM 51-40-6 AND 51-40-10. 2L73 4F A3WE 19950915003551995091500355NM 1995 9 15 95FDEA01301 119950911A53207075T6 STR CLIP BOEING727 727232 1384082NM BS 660 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON STR CLIP AT BS 660 STR 26R ON BILGE. REMOVED STR CLIP AT BS 660 STR 26R AND FOUND CORROSION OUT OF LIMITS PER FEDEX SRM 53-10-1. INSTALLED FAB STR CLIP AT BS 660 STR 26R. 2L73 4F A3WE 19950915003561995091500356NM 1995 9 15 95FDEA01302 119950911A53117075T6 FRAME BOEING727 727232 1384082NM BS 700 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY FRAME DENTED AT BS 700 BETWEEN STR 25 AND 22R. REMOVED DAMAGED PART OF FRAME AT BS 700 BETWEEN STR 22 AND 25R. INSTALLED REPAIR DOUBLER IAW FEDEX SRM 51-40-3. 2L73 4F A3WE 19950915003571995091500357NM 1995 9 15 95FDEA01303 119950911A53117075T6 FRAME BOEING727 727232 1384082NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FWD BAY DENTED AT BS 500 BETWEEN STR 26 TO 22R. REPAIRED DENTED FRAME AT BS 500 STR 26 TO 22R, PER FEDEX SRM 51-40-2. 2L73 4F A3WE 19950915003581995091500358NM 1995 9 15 95FDEA01304 119950911A53207075T6050 STRINGER CLIP BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON STR CLIP AT BS 720C AND 720B AT STR 26R. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED STR CLIP AT BS 720C AND 720B AT STR 26R. 2L73 4F A3WE 19950915003591995091500359NM 1995 9 15 95FDEA01305 119950911A53207075T6 STRINGER CLIP BOEING727 727232 1384082NM BS 660 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON STR CLIP AT BS 660 AT STR 26L. ACCESSED AREA, REMOVED CLIP AND CLEANED AREA. DRILLED FAB CLIP DEBURRED AND ALODINED AREA. PAINTED AREA, CLIP AND FASTENED INTO PLACE. CORROSION ON STR CLIP FOUND OUT OF LIMIT PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950915003601995091500360NM 1995 9 15 95FDEA01306 119950911A53207075T6 STRINGER CLIP BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON STR CLIP AT BS 720C AT STR 26L. REMOVED CLIP TO ACCESS AREA, FOUND CORROSION ON CLIP. DRILLED FAB CLIP ALODINED, PRIMED AND FASTENED INTO PLACE. CORROSION ON STR CLIP FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 STR 26L BS 720C. 2L73 4F A3WE 19950915003611995091500361NM 1995 9 15 95FDEA01307 119950911A532065159406 STIFFENER BOEING727 727232 1384082NM BS 740 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON VERTICAL STIFFENER AT BS 740 BL 0 WL 150. REMOVED CORRODED STIFFENER AND REPLACED NEW STIFFENER BS 740 BL 0 WL 150. 2L73 4F A3WE 19950915003621995091500362NM 1995 9 15 95FDEA01308 119950911A53137075T6032 STRINGER BOEING727 727232 1384082NM BS 1111 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION STR 4R BS 1111. THE CORROSION WAS FOUND TO BE OUT OF LIMITS. INSTALLED CHANNEL REPAIR AT BS 1111 STR 4L IAW SRM 53-10-3 AND 53-10-1. 2L73 4F A3WE 19950915003631995091500363NM 1995 9 15 95FDEA01309 119950911A5315BAC14902734 FLOORBEAM BOEING727 727232 1384082NM BS 344 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN FLOORBEAM AT BS 344 WL 208.5 RBL 4 LBL 51. REMOVED DAMAGED PORTION OF FLOORBEAM AND INSTALLED REPAIR PARTS AT BS 344 WL 208 RBL 10 LBL 70, PER FEDEX DRAWING SR 27-53-007. 2L73 4F A3WE 19950915003641995091500364NM 1995 9 15 95FDEA01310 119950911A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION IN SEAT TRACK AT BS 720 TO 720F WL 208.5 BL 0. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW FABRICATED SEAT TRACK AT BS 720 TO 720F WL 208.5 BL 0. 2L73 4F A3WE 19950915003651995091500365EU 1995 9 15 DL31L953665 119950910A2433F11QB3121D TRANSFORMER/REC AIRBUS310 A310324 3930206EU E/E COMP FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11837AB 674 DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN FLIGHT DECK. ESSENTIAL BUSS TRANSFORMER RECTIFIER FAILED 2 HOURS INTO FLIGHT AND ESS T/R AMPS DROPPED FROM 2 TO 4. DIVERTED FLIGHT TO YJT. REPLACED TRANSFORMER RECTIFIER, OPERATION NORMAL. 2L72 4F RTA35EU 19950915003661995091500366NM 1995 9 15 DL72S953668 119950820A5754 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807. 2L73 4F A3WE 19950915003671995091500367NM 1995 9 15 DL72S953669 119950906A5754 RIB BOEING727 727232 1384082NM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 NR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807. 2L73 4F A3WE 19950915003681995091500368NM 1995 9 15 DL73S953678 119950906A2761654496112 ACTUATOR BOEING737 737232 1384475NM NR 1 SPOILER CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO11326DL 23098 DURING APPROACH, LOST A-SYSTEM HYDRAULIC QTY AND PRESS. FOUND NR 1 SPOILER ACTUATOR CRACKED. REPLACED ACTUATOR, AS PRECAUTION REPLACED PUMP AND FILTER AND OPERATION NORMAL. 2L72 4F RTA16WE 19950915003691995091500369NM 1995 9 15 DL767953660 119950910A3350 EEL BULB BOEING767 767232 1385132NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11108DL 22220 10615 EMERGENCY EXIT LIGHT FWD OF C2 DOOR INOP. RELAMPED AND OPS NORMAL. 2L72 4F RTA1NM 19950915003701995091500370NM 1995 9 15 DL767953661 119950910A33500L3071BPEGPL EEL BULB BOEING767 767232 1385132NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11108DL 22220 10615 F/C FWD CROSS AISLE AREA PATH LIGHT AND MID GALLEY RT AISLE AREA LIGHT OUT. RELAMPED AND OPS NORMAL. 2L72 4F RTA1NM 19950915003711995091500371WP 1995 9 15 DLL10953518 119950827A2150 AIR COND LKHEED1011 10113851 5265010WP CABIN ODOR A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11725DA 193C1162 10615 STRONG PETRO/CHEMICAL ODOR IN A/C BLEED, CLOSED NR 2 PACK AND NR 2 ENG ISOLATION VALVE, ODOR DIMINISHED. EXTENSIVE INSPECTION AND OPERATIONAL CHECKS COULD NOT DETERMINE SOURCE OF ODOR. DUE TO HISTORY OF ODOR IN CABIN, REPLACED WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT. 2L73 4F A23WE 19950915003721995091500372WP 1995 9 15 DLL10953679 119950906A2150 AIR COND LKHEED1011 10113851 5265010WP CABIN ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11713DA 193C1089 DURING CLIMBOUT, ALL AFT LAVATORY SMOKE DETECTORS ACTIVATED WITH ODOR PRESENT IN AFT CABIN. RAN PACKS IN ALL MODES, COULD NOT DUPLICATE AND RETURNED TO SERVICE. 2L73 4F A23WE 19950915003731995091500373WP 1995 9 15 DLL13953680 119950908A3610 PNEUMATIC SYS LKHEED1011 10113851 5265010WP NR 2 ENGINE ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11787DL 193A1126 DURING CLIMBOUT, HAD SMOKE ODOR IN CABIN WITH SEVERAL LAV SMOKE DETECTORS GOING OFF. ISOLATED ODOR TO NR 2 PNEUMATIC SYSTEM, DEACTIVATED NR 2 ISOLATION VALVE, PLACED ON MCO. 2L73 4F A23WE 19950915003741995091500374WP 1995 9 15 DLL14953659 119950910A3350 EEL BATTERY PACK RPS1 LKHEED1011 1011385115 5265015WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO111738D 6338 193C1234 DURING LAYOVER, EMERGENCY TRACK LIGHT INOP IN BUSINESS CLASS CABIN. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19950915003751995091500375NM 1995 9 15 DLM88953662 119950910A33507715AS15 EEL BULB DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11901DE 53378 10615 EMER PATH LIGHT INOP AT SEAT 20D AND 24D. RELAMPED, OPS CHECK GOOD. 2L72 4F RTA6WE 19950915003761995091500376NM 1995 9 15 DLM88953676 119950901A2150 AIR COND DOUG MD88 MD88 3023688NM TAIL COMP ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11967DL 53116 DURING TAKEOFF, CABIN FILLED WITH SMOKE ODOR AND CONTINUED AFTER ATTEMPTING TO SWAP PACKS. RETURNED TO TYS AND PERFORMED GROUND RUN, COULD NOT DUPLICATE. PERFORMED DUCT BURNOUT, REPLACED WATER SEPARATOR BAGS AND RETURNED TO SERVICE. 2L72 4F RTA6WE 19950915003771995091500377NM 1995 9 15 DLM88953677 119950902A2150 AIR COND DOUG MD88 MD88 3023688NM CABIN ODOR A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11920DE 53423 DURING TAKEOFF, HAD SMOKE ODOR IN CABIN. RETURNED TO MCI AND PERFORMED VISUAL ACFT INSP, NO LEAKS NOTED. RAN PACKS AND COULD NOT DUPLICATE. RETURNED A\C TO SERVICE. 2L72 4F RTA6WE 19950915003781995091500378NM 1995 9 15 UPS204375 119950909A57536521630173 FOREFLAP BOEING727 72762C 138402CNM LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01913UP 19245 WHILE ON GROUND, MAINTENANCE FOUND LEFT HAND I/B FOREFLAP DAMAGED. REMOVED LEFT HAND INBOARD FOREFLAP PER MM 27-51-01 PG 404 PAR G, H, I,. INSTALLED PER MM 27-51-01 PG 408 PAR G, H, K, ON (P/N 65-21630-187)(S/N BN498), OFF (P/N 65-21630-173)(S/N BN3). 2L73 4F A3WE 19950915003791995091500379NM 1995 9 15 UPS204376 119950909A5753 SKIN BOEING727 72725C 138400HNM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01949UP 1917 WHILE ON GROUND, MAINTENANCE FOUND LEFT MIDFLAP DELAMINATED MIDDLE TRAILING EDGE 2 PLACES O/B FLAP. DEFERRED PER D-98013 INTERM REPAIR PER 57-50-1. 2L73 4F A3WE 19950915003801995091500380NM 1995 9 15 UPS204381 119950911A3350 EEL BATTERY PACK BOEING727 72727C 138400JNM CABIN INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01908UP 19114 WHILE ON GROUND, MAINTENANCE FOUND PASSENGER ENTRANCE DOOR EMER EXIT LIGHT FAILS TEST. REPLACED 2 S-106 BATTERIES AND OPS OK. 2L73 4F A3WE 19950915003811995091500381NM 1995 9 15 UPS404377 119950910A5753 SKIN BOEING747 747123 1384873NM RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD FLAP FWD SIDE, 2 INCH BY 6 INCH DELAM SECTION. REPAIRED FLAP ROCK GUARD AND PAINTED IAW SRM 51-40-06. 2L74 4F A20WE 19950915003821995091500382NM 1995 9 15 UPS404378 119950910A5753 SKIN BOEING747 747123 1384873NM RT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD FLAP SECTION, AFT FLAP SECTION FWD SIDE, 1 INCH BY 4 INCH DELAM SECTION JUST AFT OF NR 6 CANOE. REPAIRED ROCK GUARD ON FLAP AND PAINTED IAW SRM 51-40-06. 2L74 4F A20WE 19950915003831995091500383NM 1995 9 15 UPS404379 119950911A5753 SKIN BOEING747 747123 1384873NM LT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND, MAINTENANCE FOUND LT WING INBOARD FLAP, AFT SECTION FWD SIDE, 2 INCH BY 4 INCH AREA OF DELAMINATION JUST AFT OF NR 3 CANOE. REPAIRED FLAP ROCK GUARD PER SRM 51-40-06. 2L74 4F A20WE 19950915003841995091500384NM 1995 9 15 UPS404380 119950911A5330 SKIN BOEING747 747123 1384873NM BS 2420 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE ON GROUND, MAINTENANCE FOUND LOWER FUSELAGE HAS A 3 INCH CRACK, APPROX STA 2420 AT 7 O'CLOCK POS. THE CRACK IS ALONG EDGE OF SKIN LAP. REPAIRED PER SRM 53-30-03. 2L74 4F A20WE 19950915003851995091500385NM 1995 9 15 UPS404384 119950912A5320 WEB BOEING747 747123 1384873NM BS 1620-1640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND WEB PLATE ON RBL 11.33 STA 1620 TO 1640 CORRODED AND CRACKED. CORROSION AND CRACK OUT OF LIMITS ACC SRM 53-10-01. REPLACED WEB IAW SRM 51-10-01, AT BS 1620 TO 1640 RBL 11.33. 2L74 4F A20WE 19950915003861995091500386NM 1995 9 15 UPS404385 119950912A5315 FLOORBEAM BOEING747 747123 1384873NM BS 2220 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2220 RBL 65 CORROSION IN TOP FLANGE OF FLOORBEAM. CORROSION ON UPPER CHORD OUT OF LIMITS ACC SRM 53-10-01. REPLACED UPPER CHORD FROM RBL 44 TO RBL GD ACC SRM 53-10-07. 2L74 4F A20WE 19950915003871995091500387NM 1995 9 15 UPS404386 119950912A5315 FLOORBEAM BOEING747 747123 1384873NM BS 2140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND THE FUSELAGE FLOORBEAM BADLY CORRODED AT STA 2140 RBL 33. RENEWED FLOORBEAM AT STA 2140 RBL 11 TO RBL 99 ACC SRM 53-10-01. 2L74 4F A20WE 19950915003881995091500388NM 1995 9 15 UPS404387 119950912A5313 STRINGER BOEING747 747123 1384873NM BS 1965 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACKS IN STRINGER UNDER STRINGER END FITTING BS 1965, S-30 LT. REMOVED DAMAGED PART OF STRINGER FROM BS 1965 TO BS 1985 AND REPAIRED STRINGER ACCORDING SRM 53-10-03 FIG 1. 2L74 4F A20WE 19950915003891995091500389NM 1995 9 15 UPS404388 119950912A5315 FLOORBEAM BOEING747 747123 1384873NM BS 2240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 2140 RBL 95 TO RBL 105 FLOORBEAM CORRODED. CORROSION AT FLOORBEAM RBL 95 TO RBL 105 STA 2140 OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM ACC 53-10-07. 2L74 4F A20WE 19950915003901995091500390WP 1995 9 15 UPS804382 119950912A53204619610 FITTING DOUG DC8 DC871F 302199DWP FS 390 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON FITTING HAS HEAVY CORROSION FS 390, LONGERON 36. REPLACED FITTING PER SMR 51-1-20D. 2L74 4F RT4A25 19950915003911995091500391WP 1995 9 15 UPS804383 119950912A53115772958 FRAME DOUG DC8 DC871F 302199DWP FS 380 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BELT FRAME AT FS 380, LONGERON 33L TO 34L CRACKED 3 INCHES LONG. REPAIRED FRAME PER SRM 53-2-0. 2L74 4F RT4A25 19950915004331995091500433WP 1995 9 15 9514101221 119950825A5311 FRAME DOUG DC10 DC1030 3023501WP FS 1975 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01221NW 46579 DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 1975 FRAME T-LONGERON 50L AND 50R. REPAIRED THE FRAME (P/N AGA3183), PER EA 12-98997. 2L73 4F A22WE 19950915004341995091500434WP 1995 9 15 9514119853 119950907A5343 FITTING DOUG DC9 DC951 3022051WP MLG ATTACH CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR FITTING SIDE BRACE LUG. REPLACED FITTING. 2L72 4F A6WE 19950915004351995091500435WP 1995 9 15 9514129946 119950907A5320 CASTING DOUG DC9 DC931 3022065WP FS 756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING BETWEEN THE FS 756 BULKHEAD AND LONGERON 29L IN THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED CASTING PER SRM 51-03. 2L72 4F A6WE 19950915004361995091500436WP 1995 9 15 9514139946 119950907A5320 CASTING DOUG DC9 DC931 3022065WP FS 691 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE ATTACH CASTING LOCATED AT FS 691, LEFT OF THE CENTER LINE IN THE LEFT MAIN LANDING GEAR WHEEL WELL. REPLACED CASTING PER SRM 51-01. 2L72 4F A6WE 19950915004371995091500437WP 1995 9 15 9514149970 119950908A5720 FITTING DOUG DC9 DC931 3022065WP WS 161 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019334 47247 DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING TRAILING EDGE CAP FITTING AT STATION XTE 161.708. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19950915004381995091500438NM 1995 9 15 9514156624 119950909A5400 FITTING BOEING747 747251B 1384892NM NR 3 STRUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING PERIODIC CHECK, FOUND A CRACK IN THE NR 3 STRUT DIAGONAL BRACE FORWARD ATTACH FITTING. REPLACED FITTING. 2L74 4F A20WE 19950915004391995091500439EU 1995 9 15 9514163221 119950911A271031073110 SERVO AIRBUS320 A320211 3930320EU LT AILERON FAULTED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01321US1229912299 262 DURING CLIMBOUT, RECEIVED ELAC 1 FAULT AND ATTEMPTED RESET WITH NO HELP. LEFT AILERON INDICATES BOTH B AND G AMBER AND RIGHT AILERON INDICATES G AMBER. WITH LEFT AILERON HYDRAULIC SERVO CONTROL SYSTEM PREVIOUSLY ON MEL, THE DECISION WAS MADE TO RETURN TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE LEFT AILERON GREEN INBOARD SERVO CONTROL. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19950915004401995091500440EU 1995 9 15 9514173206 219950909A7532 VBV SENSOR AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01306US 60 731363 DURING CLIMB AT 10,000 FEET, RECEIVED ECAM MESSAGE ENG 2 COMPRESSOR VANE ACCOMPANIED WITH NO RAPID THROTTLE MOVEMENT. AIRCRAFT RETURNED TO DTW DUE TO LACK OF PARTS IN SJU TO ADDRESS THE PROBLEM. THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE VBV SENSOR WAS REPLACED. LEAK AND OPERATIONAL CHECK OK. 2L72 4F4 FRTA28NM 19950915004411995091500441WP 1995 9 15 9514189922 119950908A5350 LATCHES DOUG DC9 DC932 3022066WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LATCHES. ADJUSTED THE TAILCONE RELEASE SYSTEM AND CHECKED OK. 2L72 4F A6WE 19950915004421995091500442NE 1995 9 15 9514191156 219950911A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 3 ENGINE STALLED A NWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 GL01156US 46765 686148 TOP OF DESCENT, NR 3 ENGINE COMPRESSOR STALLED AND WAS SHUTDOWN. ENGINE WAS RESTARTED AND LANDED WITHOUT FURTHER INCIDENT. THE ENGINE WAS INSPECTED, BORESCOPED AND AN INFLIGHT BLEED CHECK IS SCHEDULED. THE PRBD, EVC REMOVAL AND PRECISION TRIM IS ON DEFERRAL. 2L73 4F4 F A22WE E20EA 19950915004431995091500443WP 1995 9 15 9514209972 119950911A215032185831 CONTROL VALVE DOUG DC9 DC931 3022065WP RT PACK MALFUNCTIONED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL019336 4270397 47338 DURING CLIMBOUT, RIGHT AIR CONDITIONING PACK BEGAN SMOKING AND THEN WENT TO FULL HOT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED TEMPERATURE CONTROL VALVE AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950915004441995091500444NM 1995 9 15 9514215521 119950912A2130 CONTROL VALVE BOEING757 757251 1384970NM LEFT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01521US 23209 THE LEFT ENGINE BLEED VALVE CLOSED SHORTLY AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE AND FLIGHT RETURNED TO MSP. REPLACED THE LEFT REVERSE FLOW CONTROLLER VALVE AND BLEED CONFIGURATION CIRCUIT CARD. SYSTEM CHECK DURING ENGINE RUNUP WAS NORMAL. 2L72 4F RTA2NM 19950915004451995091500445WP 1995 9 15 9514229993 119950912A7933 OIL TEMP SENSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL018986E 47402 666676 DURING CLIMBOUT, NR 1 ENGINE OIL TEMPERATURE INDICATION MOVED INTO THE CAUTION RANGE, FLUCTUATED, AND THEN GAVE A MAXIMUM TEMPERATURE INDICATION. A PRECAUTIONARY SHUTDOWN WAS ACCOMPLISHED AND THE FLIGHT RETURNED TO DTW LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR AND TESTED THE SYSTEM. SYSTEM OPERATIONAL WAS SATISFACTORY AND THE AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950915004461995091500446WP 1995 9 15 95FDEA01311 119950909A5400AUB7031503 SPAR WEB DOUG DC10 DC1030F 3023504WP NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 NR 1 ENG PYLON UPPER SPAR WEB CRACKED AT O/B CORNER, APPROX 5 INCHES. REMOVED AND REPLACED SPAR WEB. 2L73 4F RTA22WE 19950915004471995091500447NM 1995 9 15 95FDEA01312 119950912A5320 CHORD BOEING727 72722 1384002NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 CORROSION FOUND ON HORIZONTAL CHORD AT RBL 16.5 TO 20 WL 191.5. REPAIRED CORRODED AREA PER EA 7-5310-25687. 2L73 4F A3WE 19950915004481995091500448NM 1995 9 15 95FDEA01313 119950912A532065317731 CHORD BOEING727 72722 1384002NM BS 1176.9 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 CORROSION ON REINFORCEMENT CHORD STA 1176.9 RBL 55 WL 208. REMOVED PARTS, SECONDARY STRUCTURE AND REMOVED CORRODED REINFORCEMENT CHORD. INSTALLED NEW CHORD AND SECONDARY STRUCTURE. ALL WORK DONE IAW FEDEX SRM 53-10-1, 51-30-2. REPLACED CHORD BS 1176.9 LBL 65 RBL 55. 2L73 4F A3WE 19950915004491995091500449NM 1995 9 15 95FDEA01314 119950908A53302024T3 SKIN BOEING727 72722 1384002NM BS 1372-1389 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 STRINGER 9L STA 1372 TO 1389 PILLOWING SKIN. REMOVED DAMAGE SECTION OF SKIN AND REPAIRED IAW FEDEX SRM 53-30-3, 51-30-2. 2L73 4F A3WE 19950915004501995091500450NM 1995 9 15 95FDEA01315 119950912A5330651755630 SKIN BOEING727 72722 1384002NM BS 1352-1420 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 STR 9R STA 1352 TO 1420 PILLOWING SKIN. REMOVED AND REPLACED 30 INCHES OF SKIN AND REPAIRED SKINS BOTH FWD AND AFT OF STA 1365.5 STR 9R, PER FEDEX SRM 53-30-3, 51-30-2. 2L73 4F A3WE 19950915004511995091500451NM 1995 9 15 95FDEA01316 119950908A53207075T6 FLOOR SUPPORT BOEING727 72722 1384002NM BS 840 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25147FE 19080 FLOOR SUPPORT FLANGE AT STA 840 LBL 24 WL 208 HAS INTERGRANULAR CORROSION THAT IS OUT OF LIMITS. FABRICATED REINFORCEMENT STRAP PER EWO NO 95-3069. 2L73 4F A3WE 19950915004521995091500452NM 1995 9 15 95FDEA01317 119950912A5753 SKIN BOEING727 72725 1384006NM RT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 RT WING O/B MIDFLAP HAS DISBOND AT I/B CORNER UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP I/B CORNER UPPER SURFACE, IAW FEDEX SRM 57-50-01 AND 51-40-06. 2L73 4F A3WE 19950915004531995091500453NM 1995 9 15 95FDEA01318 119950912A5753 SKIN BOEING727 72725 1384006NM RT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 RT WING O/B MIDFLAP HAS DISBOND, 28 INCHES FROM I/B UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP, 28 INCHES FROM I/B END UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06. 2L73 4F A3WE 19950915004541995091500454NM 1995 9 15 95FDEA01319 119950912A5753 SKIN BOEING727 72725 1384006NM RT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 RT WING O/B MIDFLAP HAS DISBOND, 70 INCHES FROM O/B END UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP, 70 INCHES FROM O/B END UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06. 2L73 4F A3WE 19950915004551995091500455NM 1995 9 15 95FDEA01320 119950912A5753 SKIN BOEING727 72725 1384006NM RT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 RT WING O/B MIDFLAP HAS DISBOND AT O/B CORNER ON UPPER SURFACE. REPAIRED RT WING O/B MIDFLAP O/B CORNER UPPER SURFACE IAW FEDEX SRM 57-50-01, 51-40-06. 2L73 4F A3WE 19950915004561995091500456NM 1995 9 15 95FDEA01321 119950912A5753 SKIN BOEING727 72725 1384006NM RT TE AFT FLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 LT WING O/B AFT FLAP 2 INCHES FROM O/B END HAS DISBOND, LOWER SURFACE. REPAIRED LT WING O/B AFT FLAP 2 INCHES FROM O/B END IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950915004571995091500457NM 1995 9 15 95FDEA01322 119950912A5755 SKIN BOEING727 72725 1384006NM NR 11 SPOILER DISBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 NR 11 SPOILER HAS DISBONDED AREA OF LOWER SKIN AT HINGE DOUBLER. REPAIRED NR 11 SPOILER LOWER SKIN IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950915004581995091500458NM 1995 9 15 95FDEA01323 119950912A5755 SKIN BOEING727 72725 1384006NM NR 12 SPOILER DISBONDED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 NR 12 SPOILER HAS LARGE DISBONDED AREA OF LOWER SKIN. REPAIRED NR 12 SPOILER LOWER SKIN IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950915004591995091500459NM 1995 9 15 95FDEA01324 119950912A5753 RUB STRIP BOEING727 72725 1384006NM LT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 LT WING O/B MIDFLAP UPPER I/B RUB STRIP DISBONDED. LT WING O/B MIDFLAP UPPER I/B RUB STRIP WAS REPAIRED PER FEDEX MM 51-51-11. 2L73 4F A3WE 19950915004601995091500460NM 1995 9 15 95FDEA01325 119950912A53302024T3050 SKIN BOEING727 727233 138408ANM BS 1195-1205 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 DENT ON EXTERNAL SKIN SURFACE, BS 1195 TO 1205 STR 24R. REPAIRED DENT, REF SRM 53-30-2. 2L73 4F RTA3WE 19950915004611995091500461NM 1995 9 15 95FDEA01326 119950912A53202024T3 SHEAR TIE BOEING727 727233 138408ANM BS 1010 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORRODED SHEAR TIE AT BS 1010 RBL 9 WL 138. REMOVED DAMAGE IN A .5 INCH BY 6 INCH AREA AND FABRICATED REPAIR PART ALODINED, PRIMED AND INSTALLED REPAIR IAW FEDEX SRM 53-10-4. 2L73 4F RTA3WE 19950915004621995091500462NM 1995 9 15 95FDEA01327 119950912A574065216500 BONDING JUMPER BOEING727 727232 1384082NM NR 3 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION (75C002-00), NR 3 K-FLAP TO BULLNOSE I/B BONDING JUMPER LOWER ATTACH POINT. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED NR 3 K-FLAP IAW EA 7-5710-25636 SR 27-57-010. 2L73 4F A3WE 19950915004631995091500463NM 1995 9 15 95FDEA01328 119950912A53302024T3090 SKIN BOEING727 727232 1384082NM BS 1173-1176 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 DENT IN SKIN BS 1173 TO 1176 BETWEEN STR 16 AND 17R, .5 BY .5 BY .045 OUT OF LIMITS PER SRM. DENT WAS FOUND TO BE OUT OF LIMITS. CUTOUT DAMAGED SKIN AND REPAIRED IAW SRM 53-30-3. 2L73 4F A3WE 19950915004641995091500464NM 1995 9 15 95FDEA01329 119950912A532069471112 INTERCOSTAL BOEING727 727232 1384082NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON PRESS GUSSET AT BS 740 BL 0 WL 145, BETWEEN KEEL BEAMS. DISCOVERED WHILE WORKING FUSELAGE 00188 NR 0561. PRESS GUSSET AT BS 740 BL 0 WL 145 FOUND TO BE CORRODED BEYOND LIMITS, PER FEDEX SRM 55-10-1. REMOVED AND REPLACED PRESS GUSSET PER FEDEX SRM 51-30-2. 2L73 4F A3WE 19950915004651995091500465NM 1995 9 15 95FDEA01330 119950912A532065562392 SPLICE BOEING727 727232 1384082NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION (71C209-02), ON STR TERMINATION SPLICE STR 27L BS 680. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED STR SPLICE AT BS 680 STR 27L. 2L73 4F A3WE 19950915004661995091500466NM 1995 9 15 95FDEA01331 119950912A532069436833 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY BS 720C STR 25R AND 26R WL 148 ON THE SHEAR TIE. REMOVED AND REPLACED SHEAR TIE AT BS 720C STR 25 TO 26R WL 148, ALDOINED, PRIMED, AND PAINTED. CORROSION ON SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950915004671995091500467NM 1995 9 15 95FDEA01332 119950912A532065562392 SPLICE BOEING727 727232 1384082NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FOUND WHILE WORKING NR 0460 ON STR SPLICE AT BS 680 AT STR 28R WL 145. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED OLD STR SPLICE AND REPLACED WITH NEW STR SPLICE AT BS 680 STR 28R. 2L73 4F A3WE 19950915004681995091500468EU 1995 9 15 DL31L953675 119950911A2120 AIR DISTR AIRBUS310 A310324 3930206EU AFT GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11843AB 689 ELECTRICAL RUBBER INSULATION BURNED SMELL IN AFT GALLEY ABOUT 01.45 BEFORE LANDING, NO SMOKE NOTICED. THOUGHT TO COME FROM CEILING AREA. PULLED AFT GALLEY C/BS AND TURNED ALL GALLEY SWS OFF. TURNED OFF NAV LIGHTS. OPERATED ALL OVENS, REMOVED COFFEE MAKERS AND CHECKED PADSAND WIRING. OPENED OVERHEAD PANELS AND CHECKED WIRING BALLASTAND TUBES. WITH AIR COND ON OPERATED SYSTEMS, ALL OK. 2L72 4F RTA35EU 19950915004691995091500469NM 1995 9 15 DL72S953640 119950819A5320 BLKHD BOLTS BOEING727 727232 1384082NM BS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND MOUNT BOLTS WORN FWD CARGO BULKHEAD AT FS 720D VERTICAL SUPPORT BEAMS ATTACH POINT AT STR 26L AND 26R. REPAIRED PER SRM 53-10-9 FIG 9. 2L73 4F A3WE 19950915004701995091500470NM 1995 9 15 DL72S953649 119950820A5754 WEB BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805. 2L73 4F A3WE 19950915004711995091500471NM 1995 9 15 DL72S953670 119950911A5754651622296 ANGLE BOEING727 727225 1384077NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 CRACK AT L ANGLE UNDER TAI DUCT. REPAIRED PER M/M 57-54-9 FIG 805A. FOUND AT SHOP INSPECTION FOR NR 6 L/E SLAT PANEL. 2L73 4F A3WE 19950915004721995091500472NM 1995 9 15 DL72S953673 119950911A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11485DA 20865 FOUND ON A2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT OUTBD STOP PAD. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950915004731995091500473NM 1995 9 15 DL72S953674 119950911A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11485DA 20865 FOUND ON A2 LETTER CHECK, NUMBER 2 SLAT COVE SKIN ATTACH ANGLE IS CRACKED AT INBD STOP PAD. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950915004741995091500474NM 1995 9 15 DL72S953684 119950909A5754651622373 PANEL BOEING727 727232 1384082NM NR 2 SLAT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING SHOP INSPECTION, FOUND LEADING EDGE SLAT DAMAGED ON OUTBOARD END. REPAI RED DAMAGE PER THE 727 SRM 57-50-3 FIG 1, FOR NR 2 L/E SLAT PANEL. 2L73 4F A3WE 19950915004751995091500475NM 1995 9 15 DL767953672 119950911A3350 EEL BULB BOEING767 767232 1385132NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11108DL 22220 LEFT AFT ENTRY DOOR EMER SLIDE LIGHT INOP. REPLACED LAMP AND CLEANED LIGHT ASSY, CHECK'S NORM. 2L72 4F RTA1NM 19950915004761995091500476WP 1995 9 15 DLL10953686 119950828A5312 FITTING LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11714DA 193C1090 COMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 5 AND NR 10. FITTINGS WERE SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915004771995091500477WP 1995 9 15 DLL10953687 119950829A5312 FITTING LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11715DA 193C1092 COMPLYING WITH DL INSPECTION SI 7-66332-12, AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 8 AND NR 58. FITTINGS WERE SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915004781995091500478WP 1995 9 15 DLL10953688 119950825A5312 FITTINGS LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 COMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52, AFT P-DOME TO STRINGER SPLICE FITTINGS WERE FOUND CRACKED AT STRINGERS NR 8 AND NR 58. FITTINGS WERE SCHEDULED FOR REPLACEMENT. 2L73 4F A23WE 19950915004791995091500479NM 1995 9 15 DLM88953671 119950911A3233 ACTUATOR 59370365505 DOUG MD88 MD88 3023688NM RT MLG LEAKING A DALAO OTHER K FLUID LOSS LDLANDING 1 SO11917DL 8603 49573 AT FLT LEVEL 350 NOTICED RIGHT HYD SYS QTY 6, SHUTDOWN RIGHT HYDRAULIC PUMP. WHEN PUMP TURNED BACK ON, THERE WAS NO SYS PRESS. FOUND RT MAIN GEAR RETRACT ACTUATOR CYLINDER LEAKING. REPLACED CYLINDER, OPERATION NORMAL. 2L72 4F RTA6WE 19950915004801995091500480NM 1995 9 15 SCNA95183 119950910A3350S106 BATTERIES BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM. REPLACED THE EMERGENCY EXIT LIGHT BATTERIES AND LIGHT OPS CHECKED GOOD PER MM 33-50-01. 2L73 4F RTA3WE 19950915004811995091500481NM 1995 9 15 SCNA95184 119950909A335065795991 EEL BULBS BOEING727 7272A1 138407FNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE R1 DOOR EMERGENCY EXIT SIGN WAS FOUND TO HAVE 2 BULBS INOPERATIVE. THE EXIT SIGN WAS RELAMPED AND TESTED PER MM 33-50-01. 2L73 4F A3WE 19950915004821995091500482NM 1995 9 15 SCNA95185 119950910A33501102833 EEL POWER PACK BOEING727 727282 2F0R NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE FORWARD CABIN CEILING MOUNTED EMERGENCY AREA LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE OVERHEAD EMERGENCY AREA LIGHT POWER PACK IAW MM 33-50-81 AND THE LIGHT TESTED GOOD. 2L73 4F RTA3WE 19950915004831995091500483WP 1995 9 15 SCNA95186 119950906A53302024T3 SKIN DOUG DC10 DC1015 3022118WP BS 1761 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15152SY 48289 THE FUSELAGE SKIN WAS FOUND BULGING AND CRACKED WITH A PULLED FASTENER AT FRAME STATION 1761 BETWEEN LONGERON 47R AND 48R, JUST BELOW THE CENTER CARGO DOOR CUTOUT. THE BULGE WAS CAUSED BY CORROSION BETWEEN THE FUSELAGE SKIN AND THE UNDERLYING TITANIUM TEARSTRAP. THE DAMAGED SKIN WAS CUTOUT, A FILLER AND DOUBLER INSTALLED PER DC-10 SRM, VOLUME 1 CHAPTER 53-20-00 FIGURE 6. 2L73 4F A22WE 19950915004861995091500486NM 1995 9 15 95ZZZM390 119950806A21301296942 THERMOSTAT BOEING737 7373G7 1384595NM LEFT FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28302AW 753 24009 LAS-SNA - FLT NR 1855 - DURING CLIMB THE CABIN ALTITUDE BEGAN CLIMBING RAPIDLY. CREW UNABLE TO CONTROL WITH MANUAL OR STANDBY. LEFT BLEED INDICATED 0 PSI. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TWELVE INCHES OF AFT CARGO DOOR SEAL HANGING OUT OF DOOR. MAINTENANCE ALSO FOUND NR 1 ENG MUSCLE AIR LINE AT PRSOV LEAKING. REINSTALLED AFT CARGO DOOR SEAL AND REPLACED NR 1 ENGINE MUSCLE AIR LINE AND 450 DEGREE THERMOSTAT. REF AWXA9500494. 2L72 4F RTA16WE 19950915004871995091500487NM 1995 9 15 95ZZZM391 119950806A5230 DOOR SEAL BOEING737 7373G7 1384595NM CARGO COMPT FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28302AW 24009 LAS-SNA - FLT NR 1855 - DURING CLIMB THE CABIN ALTITUDE BEGAN CLIMBING RAPIDLY. CREW UNABLE TO CONTROL WITH MANUAL OR STANDBY. LEFT BLEED INDICATED 0 PSI. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TWELVE INCHES OF AFT CARGO DOOR SEAL HANGING OUT OF DOOR. MAINTENANCE ALSO FOUND NR 1 ENG MUSCLE AIR LINE AT PRSOV LEAKING. REINSTALLED AFT CARGO DOOR SEAL AND REPLACED NR 1 ENGINE MUSCLE AIR LINE AND 450 DEGREE THERMOSTAT. REF AWXA9500494. 2L72 4F RTA16WE 19950915004881995091500488NM 1995 9 15 AWXA9500494 119950806A2130106494060080 LINE BOEING737 7373G7 1384595NM NR 1 ENG FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28302AW 24009 LAS-SNA - FLT NR 1855 - DURING CLIMB THE CABIN ALTITUDE BEGAN CLIMBING RAPIDLY. CREW UNABLE TO CONTROL WITH MANUAL OR STANDBY. LEFT BLEED INDICATED 0 PSI. CREW RETURNED AIRCRAFT TO LAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TWELVE INCHES OF AFT CARGO DOOR SEAL HANGING OUT OF DOOR. MAINTENANCE ALSO FOUND NR 1 ENG MUSCLE AIR LINE AT PRSOV LEAKING. REINSTALLED AFT CARGO DOOR SEAL AND REPLACED NR 1 ENGINE MUSCLE AIR LINE AND 450 DEGREE THERMOSTAT. (M) 2L72 4F RTA16WE 19950915004891995091500489NM 1995 9 15 AWXA9500559 119950820A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTING INOPERATIVE FROM ROW 17 THROUGH ROW 19. REPAIRED WIRE WITH NEW TERMINAL, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950915004901995091500490NM 1995 9 15 AWXA9500560 119950820A335020131A EEL BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950915004911995091500491NM 1995 9 15 AWXA9500565 119950821A3230273N20032 DOWNLOCK ACT BOEING757 757225 1384959NM LT MLG FAILED A AWXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28914AW DA00134 22208 PHX - FLT NR 292 - DURING CRUISE, THE EICAS MESSAGE L HYD QTY ILLUMINATED. HYDRAULIC QUANTITY WAS .42 AND DROPPED TO .10 ON FINAL APPROACH. LEFT ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED. PUMP WAS TURNED OFF. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT MLG DOWNLOCK ACTUATOR LEAKING FROM SWIVEL END. REMOVED AND REPLACED ACTUATOR PER BMM 32-32-01 AND 32-32-02. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19950915004921995091500492NM 1995 9 15 AWXA9500573 119950821A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH ROW 21. RESECURED LOOSE WIRE AT ROW 21, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950915004931995091500493NM 1995 9 15 AWXA9500574 119950822A33501012721 EEL ASSY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28181AW 22648 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED SEAT LIGHT ASSEMBLY AT ROW 5, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950915004941995091500494NM 1995 9 15 AWXA9500575 119950822A335020131A EEL BATTERY PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 12 THROUGH ROW 19. REMOVED AND REPLACED BATTERY PACK AT ROW 18 LT, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19950915004951995091500495NM 1995 9 15 AWXA9500576 119950823A33501000679 EEL ASSY BOEING737 7372M8 1384483NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CEHCK, FOUND EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE AT L2 DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F A16WE 19950915004961995091500496NM 1995 9 15 AWXA9500577 119950823A335020131A EEL BATTERY PACK BOEING757 7572G7 1384963NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT ROW 24 RT OVERHEAD. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950915004971995091500497NM 1995 9 15 AWXA9500578 119950824A3350 EEL CONNECTORS BOEING737 7373G7 1384595NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT 1B. REATTACHED CONNECTORS, OPS CHECK GOOD PER BMM. (M) 2L72 4F RTA16WE 19950915004981995091500498NM 1995 9 15 AWXA9500579 119950824A335020131A EEL BATTERY PACK BOEING757 7572G7 1384963NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28910AW 24523 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT POSITION M734. REMOVED AND REPLACED PACK M734, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19950915004991995091500499NM 1995 9 15 AWXA9500580 119950825A5315 FLOORBEAM BOEING737 7373G7 1384595NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING SCHEDULED C7 INSPECTION, FOUND FOUR AREAS OF CORROSION BEYOND LIMITS ON UPPER CHORD AT STATION 986.5, RBL 3.54 TO RBL 18.32. REMOVED DAMAGED SECTION OF FLOORBEAM. REPLACED EXTRUSION AND SPLICE ANGLES PER SRM 53-00-51, FIG 202. (M) 2L72 4F RTA16WE 19950915005001995091500500NM 1995 9 15 AWXA9500581 119950825A321165C313326 TRUNNION BOEING737 7373G7 1384595NM RT MLG DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28160AW 23782 DURING SCHEDULED C7 INSPECTION, FOUND RT MAIN LANDING GEAR FORWARD TRUNNION BEARING MISSING RIVETS. REPLACED FORWARD TRUNNION BEARING ASSEMBLY. (M) 2L72 4F RTA16WE 19950915005011995091500501EU 1995 9 15 AWXA9500582 119950825A3350 EEL WIRING AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28625AW 064 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. REPAIRED SECTION OF BROKEN WIRING BY SEAT FLOOR TRACK, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950915005021995091500502EU 1995 9 15 AWXA9500583 119950827A3350 EEL WIRING AIRBUS320 A320231 3930325EU CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28636AW 098 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT 24 LT. REPAIRED BROKEN WIRE THAT WAS BROKEN OFF CANNON PLUG AT ROW 24, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950915005031995091500503NM 1995 9 15 AWXA9500584 119950826A3350 EEL BOEING737 737277 1384570NM CABIN LOOSE A AWXAA UNSCHED LANDING O OTHER TOTAKEOFF 1 WP28185AW 22652 PHX-LAX - FLT NR 24 - ON TAKEOFF, THE LT AFT OVER DOOR EMERGENCY EXIT LIGHT FIXTURE FELL OUT INJURING THE NR 3 FLIGHT ATTENDANT. AIRCRAFT RETURNED TO PHX WITHOUT FURTHER PROBLEMS. MAINTENANCE TRIMMED CEILING PANEL TO BETTER FACILITATE LIGHT HOUSING AND REINSTALLED LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950915005041995091500504NM 1995 9 15 AWXA9500585 119950816A5330 SKIN BOEING737 737277 1384570NM BS 360 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 LAS - FLT NR 134 - DURING RON INSPECTION, MAINTENANCE FOUND AREA OF DAMAGE ON FUSELAGE SKIN 4 INCHES AFT OF STATION 360 LEFT SIDE OF AIRCRAFT. MAINTENANCE REPAIRED DAMAGE IAW SRM 53-30-3, FIGURE 1. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RTA16WE 19950915005051995091500505 1995 9 15 AWXA9500586 419950827A2330IFDA1109100 SEAT GROUP ASSY BOEING737 7373G7 1384595NM SEAT 10C INOPERATIVE A AWXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28307AW 24634 CMH - FLT NR 401 - PASSENGER REPORTED SMOKE SMELL COMING FROM FLIGHT LINK SET ON SEAT 10C. SYSTEM WAS DEACTIVATED AND PLACED ON DMI 50748. CONTRACT MAINTENANCE REMOVED AND REPLACED SEAT GROUP ASSY BOX. SYSTEM TESTED, NO FAULTS FOUND. DMI CLEARED AND AIRCRAFT REMAINS IN SERVICE. (M) 2L72 4F RTA16WE 19950915005061995091500506WP 1995 9 15 HALA95108 119950816A3350 EEL CONTACTS DOUG DC9 DC951 3022051WP COCKPIT DIRTY A HALAK NONE L NO TEST ININSP/MAINT 1 WP13699HA 47763 COCKPIT EMERGENCY LIGHTS DO NOT TEST. CLEANED CONTACTS ON BULB. OPERATIONS CHECK GOOD. (M) 2L72 4F A6WE 19950915005071995091500507WP 1995 9 15 HALA95109 119950817A33506011777 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 1526 47764 HNL - RIGHT EXTERIOR EMERGENCY LIGHT LIGHT DOES NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950915005081995091500508WP 1995 9 15 HALA95111 119950822A5531 LE RIBS DOUG DC9 DC951 3022051WP VERT STAB CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13601AP 47658 IN C-CHECK, UPON REMOVAL OF VERTICAL STABILIZER LEADING EDGE FOR DPM 119846, 3 ADDITIONAL CRACKS FOUND IN RIBS LEFT SIDE NR 2, NR 7 AND NR 8 FROM BOTTOM. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 55-02 FIG 19. (M) 2L72 4F A6WE 19950915005091995091500509WP 1995 9 15 HALA95112 119950822A5531 L/E RIBS DOUG DC9 DC951 3022051WP VERT STAB CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13601AP 47658 IN C-CHECK, FOUND CRACKS ON VERTICAL STABILIZER LEADING EDGE RIBS ZFS = 142 AND 148, RIGHT LOWER ENDS. REMOVED CRACKED VERTICAL STABILIZER LEADING EDGE RIBS, ZFS = 142 AND 148 PER SRM 53-05-84. FABRICATED, TREATED AND PRIMED REPAIR ANGLES PER SRM 51-10-02, 51-10-03 AND INSTALLATION COMPLETE PER 53-03-84. (M) 2L72 4F A6WE 19950915005101995091500510WP 1995 9 15 HALA95114 119950828A33501001191 EEL DOUG DC9 DC951 3022051WP CABIN BROKEN A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 FLT NR 281 - FORWARD ENTRANCE EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950915005111995091500511EU 1995 9 15 M3HA95017 119950822A3350 EEL CONNECTOR AEROSPATR42 ATR42320 8680930EU CABIN BROKEN A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13985MA 358 HNL - EMERGENCY EXIT TRACK LIGHTS, SIDE EXIT LIGHTS OUT. FOUND CONNECTOR ON EMERGENCY BATTERY PACK BROKEN. REPLACED EMERGENCY BATTERY PACK, P/N 3011151, S/N 2110. (M) 2H72 4T RTA53EU 19950915005121995091500512EU 1995 9 15 RAIA950838 119950821A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE5023 2042 119 STL - AFT CENTER EMERGENCY LIGHT DOES NOT WORK. MAINTENANCE REPLACED BATTERY PACK IN ROW 10CD. (M) 2H72 4T RTA53EU 19950915005131995091500513NE 1995 9 15 RAIA950839 219950825A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LEFT MALFUNCTIONED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE032FOR 13704 176 STL - FLT NR 7524 - ELECTRICAL SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE. ENGINE PERFORMANCE RUNS REVEALED ALL ENGINE PARAMETERS TO BE NORMAL. NO SMOKE NOTED. (M) 2H72 4T4 TRTA53EU E20NE 19950915005141995091500514 1995 9 15 RAIA950840 419950826A34526226523007 ATC CONTROLLER AEROSPATR42 ATR42300 8680920EU COCKPIT FAILED A RAIAD RETURN TO BLOCK O OTHER CRCRUISE 1 CE03424TE12690 124 STL - FLT NR 7154 - LOST BOTH ATC TRANSPONDERS. MAINTENANCE REPLACED ATC CONTROLLER. TRANSPONDER CHECK REVEALED NORMAL OPERATION. (M) 2H72 4T RTA53EU 19950915005151995091500515EU 1995 9 15 RAIA950841 119950823A3240 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU LEFT REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03424AM 865 STL - FLIGHT OFFICERS LEFT BRAKE INOP, NO PRESSURE SHOWN ON GAUGE. MAINTENANCE SERVICED BOTH FLIGHT OFFICERS BRAKE MASTER CYLINDERS, P/N ACM26810. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005161995091500516EU 1995 9 15 RAIA950842 119950823A3240ACM2626810 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU LEFT REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03431AM9569 881 STL - FLT NR 7421 - ANTI-SKID SYSTEM RELEASES PRESSURE ON BRAKES ENOUGH TO WHERE NORMAL BRAKING IS QUESTIONABLE. MAINTENANCE BLEED BRAKES, SERVICED CAPTAINS MASTER CYLINDERS. TAXI CHECK OK. (M) 2L72 4T RTA56EU 19950915005171995091500517EU 1995 9 15 RAIA950843 119950824A3240 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU RUDDER PDLS REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03431AM9569 881 STL - FLT NR 7311 - MINIMUM BRAKE PRESSURE APPLIED, ANTI-SKID ACTIVATED AND DURING NORMAL BRAKING TAXIING TO GATE. MAINTENANCE SERVICED ALL FOUR MASTER CYLINDERS P/N ACM 26810, TO LIMITS AS REQUIRED. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005181995091500518EU 1995 9 15 RAIA950844 119950818A3240215221 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU MAIN WHEELS REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03338TE6421 932 STL - PARKING BRAKE DOES NOT HOLD AIRCRAFT STILL ABOVE 30 PERCENT TQ. MAINTENANCE BLEED BRAKES, PARKING BRAKE CHECK GOOD, LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005191995091500519EU 1995 9 15 RAIA950845 119950824A3240 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU LEFT REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03339TE 935 STL - FLT NR 7429 - LEFT BRAKE VERY WEAK. MAINTENANCE SERVICED LEFT BRAKE MASTER CYLINDER P/N ACM 26810. (M) 2L72 4T RTA56EU 19950915005201995091500520EU 1995 9 15 RAIA950846 119950824A3240215221 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU LT MLG REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03338TE9496 932 STL - FLT NR 7397 - BRAKES SEEM WEAK. MAINTENANCE BLEED LEFT BRAKE. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005211995091500521EU 1995 9 15 RAIA950847 119950826A21708323715 WATER SOCKS BAG JETSTMJETSTM3201 1500217EU LT/RT DIRTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03429AM9562 879 STL - FLT NR 7433 - BLEEDS SMELL. MAINTENANCE REPLACED BOTH PACKS WATER SOCKS. SYSTEM CHECKS GOOD. (M) 2L72 4T RTA56EU 19950915005221995091500522EU 1995 9 15 RAIA950848 119950828A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU NR 1 ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03343TE6461 6461 955 STL - FLT NR 7390 - ON TAKEOFF ROLL NR 1 ENGINE DID NOT MAKE TORQUE AND TTL DID NOT BYPASS FUEL-EGT WENT TO 670 DEGREES. MAINTENANCE RECALIBRATED LEFT ENGINE SIGNAL CONDITIONER. DEFERRED LT TTL AS PER MEL 76-2 CAT C. GROUND RUNS CHECK OK. (M) 2L72 4T RTA56EU 19950915005231995091500523NM 1995 9 15 95ZZZM392 119950823A361032144463 HIGH STAGE VLV BOEING737 73733A 1384673NM NR 2 ENG FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP28169AW 794 23630 PHX-COS - FLT NR 412 - AIR TURNBACK, LT AND RT ENGINE BLEED TRIP LIGHT ILLUMINATED DURING BLEEDS OFF TAKEOFF. LEFT BLEED TRIP RESET AFTER RELIEVING PRESSURE/TEMPERATURE BY ACTIVATING THE ASSOCIATED ANTI-ICE VALVES. RT ENGINE BLEED WOULD NOT RESET. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FAN AIR VALVE IAW MM 36-11-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-15, AND THE NR 2 ENGINE BLEED AIR REGULATOR PER MM 36-10-11. ALL OPS AND LEAK CHECKS GOOD. REF AWXA9500572. 2L72 4F RTA16WE 19950915005241995091500524NM 1995 9 15 95ZZZM393 119950823A36101074922 BLEED REGULATOR BOEING737 73733A 1384673NM NR 2 ENG FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP28169AW 1385 23630 PHX-COS - FLT NR 412 - AIR TURNBACK, LT AND RT ENGINE BLEED TRIP LIGHT ILLUMINATED DURING BLEEDS OFF TAKEOFF. LEFT BLEED TRIP RESET AFTER RELIEVING PRESSURE/TEMPERATURE BY ACTIVATING THE ASSOCIATED ANTI-ICE VALVES. RT ENGINE BLEED WOULD NOT RESET. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FAN AIR VALVE IAW MM 36-11-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-15, AND THE NR 2 ENGINE BLEED AIR REGULATOR PER MM 36-10-11. ALL OPS AND LEAK CHECKS GOOD. REF AWXA9500572. 2L72 4F RTA16WE 19950915005251995091500525NE 1995 9 15 95ZZZM394 219950811A7321743602 FUEL CONTROL BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 3 ENGINE MALFUNCTIONED A MYWAE ENGINE SHUTDOWN O OTHER NRNOT REPORTED 1 SO19806MA 845 22437 79315 NR 3 ENGINE IN FLIGHT SHUT DOWN AT FL 350. ACCOMPLISHED EMERGENCY ENGINE SHUT DOWN PROCEDURES. AFTER SHUT DOWN, ENGINE WINDMILLED FOR 30 MINUTES, OIL PRESSURE 15-20 PSI. REMOVED AND REPLACED NR 3 ENGINE FUEL FILTER AND FUEL CONTROL. (M) 2L73 4F4 F A3WE E2EA 19950915005261995091500526WP 1995 9 15 95ZZZM395 119950620A5313 LONGERON LKHEED1011 10113851 5265010WP FS 1565-1585 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION, LONGERON 39 IS CORRODED BETWEEN FS 1565 AND 1585 INSIDE OF C2 COMPARTMENT, LOWER LOBE. REMOVED DAMAGED AREA, TREATED, AND FABRICATED AND INSTALLED REPAIR PER SRM 53-13-00. 2L73 4F A23WE 19950915005271995091500527WP 1995 9 15 95ZZZM396 119950620A5313 LONGERON LKHEED1011 10113851 5265010WP FS 1585-1625 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION, C2 COMPARTMENT LOWER LOBE LONGERON 39 IS CORRODED FROM FS 1585 TO FS 1625. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED REPAIR PER SRM 53-13-00. (M) 2L73 4F A23WE 19950915005281995091500528WP 1995 9 15 95ZZZM397 119950620A5347 SEAT TRACK LKHEED1011 10113851 5265010WP FS 1605-1625 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19765BE 193P1105 LEVEL 2 CORROSION, C2 COMPARTMENT LEFT SEAT TRACK IS CORRODED BETWEEN FS 1605 AND FS 1625 55 INCHES LBL. REMOVED DAMAGED AREA, TREATED, FABRICATED AND INSTALLED REPAIR PER SRM 53-13-00. (M) 2L73 4F A23WE 19950915005291995091500529NM 1995 9 15 95ZZZM399 119950819A32226527147RTR STRUT CYLINDER BOEING707 707321C 138367BNM NLG CRACKED A MIRAK NONE K FLUID LOSS ININSP/MAINT 1 SO19722GS 1823FJ61 19373 AFTER NORMAL LANDING AT SAN JOSE, COSTA RICA, WHILE PERFORMING PREFLIGHT INSPECTION, CREW DISCOVERRED NOSE LANDING GEAR OLEO STRUT FLAT AND EVIDENCE OF HEAVY HYDRAULIC LEAK. FURTHER INSPECTION REVEALED NLG OUTER CYLINDER WAS CRACKED FROM THE TOP TO THE BOTTOM OF THE CYLINDER. THE NLG HAD ONLY 10 HOURS AND 5 LANDINGS SINCE OVERHAUL. NLG RETURNED TO REPAIR AGENCY FOR TEARDOWN INSPECTION TO DETERMINE THE CAUSE OF FAILURE. (M) 2L74 4F 4A26 19950915005301995091500530NM 1995 9 15 95ZZZM400 119950825A2910106010918 HYDRAULIC LINE BOEING707 707323C 138367DNM NR 3 ENG CRACKED A MIRAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO19751MA 19582 TNCC-KMIA - HYDRAULIC FAILURE THIS LEG. REPLACED PRESSURE LINE AND FITTING AT NR 3 ENGINE PYLON, PERFORMED GROUNDED. OPS CHECKED NORMAL AS PER MM 29-00. 2L74 4F 4A26 19950915005311995091500531NE 1995 9 15 95ZZZM401 219950824A7200 ENGINE BOEING707 707323C 138367DNM PWA JT3D JT3D3B 52039NE NR 2 FAILED A MIRAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 SO19751MA 19582 645783 SBKP-TNCC - THIRTY FIVE MINUTES AFTER TAKEOFF SEVERE COMPRESSOR STALLS NR 2 ENGINE. PRECAUTIONARY SHUTDOWN AT 2400Z. AT PILOTS DISCRETION (CHECKED WEATHER AT ALL AIRPORTS EN ROUTE, VISION FLIGHT RULES ALLTHE WAY) DECIDED TO CONTINUE TO TNCC FOR MAINTENANCE HELP. IN COMMUNICATION WITH FLIGHT FOLLOWING, RE-RELEASED TO TNCC, ADVISED ATC. INSPECTED NR 2 ENGINE FOUND ALL BLADES ON C2 DESTROYED, EVIDENCE OF METAL AT EXHAUST. ACCOMPLISHED THREE ENGINE FERRY PREPARATION IAW MILLION AIR FORM T-199 ITEMS NUMBER FROM 1 THROUGH 32. 2L74 4F4 F 4A26 1E8 19950915005321995091500532NE 1995 9 15 95ZZZM402 219950813A7320665038061446 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE FAILED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO03184AE 340B184 785216 FLT NR 4553 - BNA - WHILE CLIMBING THROUGH FL 190, LEFT ENGINE TEMPERATURE INCREASED FROM 860 TO 870. CAPTAIN SHUTDOWN ENGINE AND RETURNED TO BNA. REPLACED LEFT ENGINE HMU. (M) 2L72 4T4 TRTA52EU E8NE 19950915005331995091500533NE 1995 9 15 95ZZZM403 219950617A72107757612 GEAR BOX HAMSTD 6044T35P10 SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE FAILED A NVEAEA ENGINE SHUTDOWN UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 SO03218AE UDGA0617 340B218 785304 FLT NR 7895 - LIT - RIGHT PROP RPM FLUCTUATED, THE PGB OIL PRESSURE ROSE TO 200 PSI. CREW SHUT DOWN RIGHT ENGINE. SAFELY DIVERTED TO LITTLE ROCK. DETERMINED RIGHT PROPELLER GEARBOX HAD FAILED. COMPLIED WITH RIGHT ENGINE CHANGE. 2L72 4T4 TRTA52EU E8NE 19950915005341995091500534WP 1995 9 15 95ZZZM404 119950810A5730 SKIN DOUG DC8 DC8F54 3021926WP WS 75 CRACKED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1957FB 45669 DURING B-CHECK, MAINTENANCE FOUND A 1.5 INCH CRACK ON RIGHT WING UPPER SURFACE SKIN AT STATION 75.312. CUT OUT CRACK SECTION, INSTALLED TWO .75 INCH FILLER AND 2 FOOT BY 1 FOOT EXTERNAL DOUBLER IAW SRM 57-2-1, FIG 39. 2L74 4F 4A25 19950915005351995091500535WP 1995 9 15 95ZZZM405 119950810A5730 SKIN DOUG DC8 DC8F54 3021926WP WS 90 CRACKED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1957FB 45669 DURING B-CHECK, MAINTENANCE FOUND A .5 INCH CRACK ON LEFT WING UPPER SURFACE SKIN AT STATION 90.0. CUT OUT CRACK SECTION, INSTALLED 1.5 INCH FILLER AND 10 INCH BY 8 INCH EXTERNAL DOUBLER IAW SRM 57-2-1, FIG 20. 2L74 4F 4A25 19950915005361995091500536NM 1995 9 15 ASAA9510079 119950825A53156546811502 FLOOR BEAM BOEING737 737298C 1384490NM BS 1006 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS33055 20794 SEA - DURING C-CHECK, FOUND CORROSION ON FLOOR BEAM AT STATION 1006. REMOVED CORROSION AND REPAIRED PER ASA EA 5310-01381. (M) 2L72 4F RTA16WE 19950915005371995091500537NM 1995 9 15 ASAA9540040 119950728A5210 BEARING BOEING737 7374Q8 NM L2 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01774AS 25107 ANC - FLT 53 - FLIGHT ATTENDANT COMPLAINED THAT THE LEFT AFT ENTRY DOOR (L2) IS HARD TO CLOSE AND MAKES A GRINDING NOISE. MAINTENANCE CLEANED AND LUBED STUCK UPPER DOOR HINGE ROLLER BEARING, DOOR OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950915005381995091500538NM 1995 9 15 AWXA9500566 119950813A5320 INTERCOSTAL BOEING737 73733A 1384673NM BS 500 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28165AW 23626 PHX - DURING SCHEDULED C-10 CHECK, FOUND FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN STATION 500 AND STATION 520 BL 0. FABRICATED AND INSTALLED NEW INTERCOSTAL PER SRM 51-10-02 AND SRM 51-40-02. (M) 2L72 4F RTA16WE 19950915005391995091500539NM 1995 9 15 AWXA9500572 119950823A361032895624 FAN AIR VLV BOEING737 73733A 1384673NM NR 2 ENG FAILED A AWXAA UNSCHED LANDING GJ MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 WP28169AW 12520 23630 PHX-COS - FLT NR 412 - AIR TURNBACK, LT AND RT ENGINE BLEED TRIP LIGHT ILLUMINATED DURING BLEEDS OFF TAKEOFF. LEFT BLEED TRIP RESET AFTER RELIEVING PRESSURE/TEMPERATURE BY ACTIVATING THE ASSOCIATED ANTI-ICE VALVES. RT ENGINE BLEED WOULD NOT RESET. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FAN AIR VALVE IAW MM 36-11-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-05, THE NR 2 ENGINE HIGH STAGE VALVE PER MM 36-10-15, AND THE NR 2 ENGINE BLEED AIR REGULATOR PER MM 36-10-11. ALL OPS AND LEAK CHECKS GOOD. (M) 2L72 4F RTA16WE 19950915005401995091500540NM 1995 9 15 CIHA044H 119950804A323165239491 LINK BOEING727 727223 1384074NM LT MLG DOOR CRACKED A C1HAK NONE O OTHER ININSP/MAINT 1 WP236821 7056970569 19496 LEFT MAIN GEAR DOOR FORWARD LINK BULKHEAD TO DOOR HAS A CRACK OVER 6 INCHES LONG FORWARD SIDE OF LINK PIVOT BOLT HOLE. REPLACED LINK ASSY P/N 65-23949-1. (M) 2L73 4F A3WE 19950915005411995091500541EU 1995 9 15 RAIA950740 119950723A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST TXTAXI/GRND HDL 1 CE03423TE146451424 119 STL - CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED BATTERY PACK. (M) 2H72 4T RTA53EU 19950915005421995091500542EU 1995 9 15 RAIA950742 119950725A3242215221 BRAKES BAG JETSTMJETSTM3201 1500217EU LT/RT MLG WEAK A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03435AM 889 BRAKES WEAK AND CATCHING DURING TAXI. REPLACED BOTH LEFT AND RIGHT BRAKES. LEFT BRAKE TIME SINCE OVERHAUL 773, RIGHT BRAKE TIME SINCE OVERHAUL 1607. (M) 2L72 4T RTA56EU 19950915005431995091500543SO 1995 9 15 RAIA950743 119950725A3350D366D4001 EEL BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03127AM159981734 120103 STL - EMERGENCY PATH LIGHTING DOES NOT TEST LIGHTS INOP. MAINTENANCE REPLACED FWD EMERGENCY BATTERY PACK. (M) 2L72 4T RTA31SO 19950915005441995091500544 1995 9 15 RAIA950744 419950728A3442MI5853505 RT UNIT AEROSPATR72 ATR72202 8680940EU RADAR FAILED A RAIAO OTHER O OTHER CRCRUISE 1 CE03721TE5127 217 STL - FLT 7130 - RADAR INOP. MAINTENANCE REPLACED RADAR RECEIVER/TRANSMITTER. GROUND TEST GOOD. (M) 2H72 4T RTA53EU 19950915005451995091500545EU 1995 9 15 RAIA950745 119950727A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR DIRTY A RAIAO OTHER P NO WARNING INDICATION CLCLIMB 1 CE03859AE121013601 859 STL - FLT 4774 - GEAR INTRANSIT LIGHT WOULD NOT ILLUMINATE AND TRIPPED GEAR POSITION CIRCUIT BREAKER. MAINTENANCE CLEANED AND LUBED NOSE GEAR UPLOCK SWITCH AND RESET CIRCUIT BREAKER. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19950915005461995091500546SO 1995 9 15 RAIA950746 119950730A3350D36604001 EEL POWER SUPPLY EMB 120 EMB120RT SO CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03125AM 120017 STL - EMERGENCY LIGHTING INOP, FORWARD SECTION AND MIDDLE SECTION. MAINTENANCE REPLACED EMERGENCY TRACK LIGHTING POWER SUPPLIES. (M) 2L72 4T RTA31SO 19950915005471995091500547EU 1995 9 15 RAIA950749 119950727A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE9832 1898 102 STL - MAINTENANCE FOUND EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (M) 2H72 4T RTA53EU 19950915005481995091500548EU 1995 9 15 RAIA950801 119950802A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03339TE 935 STL - FLT NR 7496 - EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED BOTH FORWARD AND AFT EMERGENCY LIGHTS BATTERIES. (M) 2L72 4T RTA56EU 19950915005491995091500549EU 1995 9 15 RAIA950802 119950803A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE7706 102 STL - MAINTENANCE FOUND EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERIES. (M) 2H72 4T RTA53EU 19950915005501995091500550EU 1995 9 15 RAIA950804 119950803A3242AC63742 MAXARET BAG JETSTMJETSTM3201 1500217EU LT MLG FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03422AM9307 856 STL - LEFT BRAKE GRABS. MAINTENANCE REPLACED LEFT MAXARET UNIT ON LEFT BRAKE. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005511995091500551EU 1995 9 15 RAIA950805 119950808A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03339TE9362 9362 935 STL - FLT NR 7456 - LEFT ENGINE TORQUE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19950915005521995091500552CE 1995 9 15 S2YA950016 119950808A2720 BOOST SYSTEM BEECH 1900 1900D 1154162CE RUDDER MALFUNCTIONED A S2YACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 GL13118SK UE108 DURING TAKEOFF ROLL OF FLIGHT NR 1120 THE CREW FELT LEFT RUDDER DEFLECTION AND VERIFIED THE RUDDER BOOST SYSTEM WAS MALFUNCTIONING. THEY ABORTED TAKEOFF, RETURNED TO MKE AND MAINTENANCE DEFERRED THE SYSTEM. SUBMITTER STATES, CONTACTED OPERATOR THIS WAS NOT A FULL DEFLECTION. (M) 2L72 4T RTA24CE 19950915005531995091500553 1995 9 15 S2YA950017 419950808A34426228394013 RADAR CONTL PNL BEECH 1900 1900D 1154162CE CENTER PEDESTAL INOP A S2YAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING O OTHER CLCLIMB 1 GL13118SK1581 958 UE108 AFTER THE FLIGHT CREW DEPARTED ON FLIGHT NR 1822, THE WEATHER RADAR BECAME INOPERATIVE IN ALL MODES. THEY RETURNED TO MKE AND MAINTENANCE REPLACED THE RADAR CONTROL PANEL AND CLEARED THE DISCREPANCY. (M) 2L72 4T RTA24CE 19950915005541995091500554CE 1995 9 15 S2YA950018 119950814A261224412886 FIRE LOOP BEECH 1900 1900D 1154162CE RT ENGINE SHORTED A S2YAEAF ENGINE SHUTDOWN UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 GL13901SK1654 UE90 THE FLIGHT CREW HAD A RIGHT ENGINE FIRE INDICATION IN FLIGHT AFTER DEPARTING MKE ON FLIGHT NR 1026. THEY PROCEEDED TO SHUT DOWN THE RIGHT ENGINE IN FLIGHT AND DISCHARGED THE RT ENGINE FIRE BOTTLE. THEY DECLARED AN EMERGENCY, MADE A TURNBACK IN FLIGHT AND LANDED. THEY EVACUATED THE AIRCRAFT THROUGH THE AIRSTAIR DOOR. MAINTENANCE VERIFIED IT TO BE A FALSE FIRE INDICATION CAUSED BY A FAULTY FORWARD FIRE DETECTION LOOP. (M) 2L72 4T RTA24CE 19950915005551995091500555CE 1995 9 15 S2YA950019 119950816A2430 GENERATOR BEECH 1900 1900D 1154162CE RIGHT OFF LINE A S2YAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL13148SK UE148 AFTER THE FLIGHT CREW LEFT MKE ON FLT NR 1124, THEY FOUND THAT THE RT DC GENERATOR WAS OFF LINE. THEY PROCEEDED TO TURN BACK TO MKE. MAINTENANCE PARALLELED THE GENERATOR CIRCUIT PER BEECH MM AND OPS CHECK GOOD. (M) 2L72 4T RTA24CE 19950915005561995091500556CE 1995 9 15 S2YA950020 119950818A571211412003327 RIB BEECH 1900 1900D 1154162CE WS 83 CRACKED A S2YAK NONE O OTHER ININSP/MAINT 1 GL13801SK UE80 DURING AN SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT WING CENTER MID RIB AT WS 83.00 TO HAVE A CRACK AT THE TOP APPROXIMATELY FIVE INCHES ACROSS. THE CRACK WAS LOCATED BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS AND A REPAIR WAS MADE. THE RIB REINFORCMENT P/N NR 114-12003315 WAS ALSO CRACKED ON TOP. THIS IS THE FIFTH REPAIR AND IT IS LIKELY THE REST OF OUR FLEET WILL HAVE THE SAME PROBLEM DUE TO INSUFFICENT ENGINEERING. (M) 2L72 4T RTA24CE 19950915005571995091500557NM 1995 9 15 TAOA089506 119950823A335090052 EEL BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 22043 RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK AND BASE ASSEMBLY. OPS CHECKED OK PER MM 33-50. (M) 0 4 A3WE 19950915005581995091500558NM 1995 9 15 TWRA9551 119950814A3350BE50047001 EEL BUFFER MOD BOEING747 747212B 1384886NM CABIN INOPERATIVE A TWRAK NONE L NO TEST CRCRUISE 1 EA15616FF 21939 DURING CRUISE, EMERGENCY EXIT EGRESS LIGHTS BEGAN TO BLINK IN C-ZONE BY 2-R M.E.D. UPON LANDING, MAINTENANCE REPLACED BUFFER MODULE, RE-LAMPED BULBS AND CHANGED ALL POWER PACKS. OPS CHECK OK. (X) 2L74 4F A20WE 19950915005591995091500559NM 1995 9 15 TWRA9552 119950826A2150719238 ACM BOEING747 747121 1384871NM NR 2 ACM FAILED A TWRAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA15609FF 20354 BLOCK TURNBACK, DUE TO SMOKE IN CABIN. UPON RETURNING TO GATE, MAINTENANCE FOUND NR 2 AIR CYCLE MACHINE HAD FAILED. REMOVED AND REPLACED THE NR 2 AIR CYCLE MACHINE, OPS CHECK OK. (M) 2L74 4F A20WE 19950915005601995091500560 1995 9 15 WTAA950247 319950821A6140865966 BETA PRESS BAG JETSTMJETSTM3101 1500215EU RT ENGINE FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17423UE 799 PDX - RIGHT ENGINE BETA LIGHT FAILED TO EXTINGUISH ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED RT ENGINE BETA PRESSURE SWITCH. BETA SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950915005611995091500561EU 1995 9 15 95ZZZM406 119950816A7331415G107100G14 FUEL XMITTER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP COCKPIT FAULTY A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03859AE2893 859 66065 SAN - FLT NR 4745 - RT FUEL LOW PRESSURE INDICATION DROPPED DOWN INTO THE YELLOW. MAINTENANCE REPLACED RT FUEL INDICATOR AND TRANSMITTER. (M) 2L72 4T4 TRTA56EU E4WE 19950915005621995091500562 1995 9 15 ASAA9580162 419950716A2565D29984103 EVAC SLIDE DOUG DC9 DC983 3022083WP TAILCONE DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01963AS 53077 ANC - DURING GROUND SERVICING, THE EMERGENCY HANDLE ON THE AFT ENTRY DOOR WAS INADVERTENTLY PULLED WHICH JETTISONED THE TAILCONE. THE TAILCONE EMERGENCY EVACUATION SLIDE DID NOT DEPLOY AND THERE WAS NO DAMAGE TO THE TAILCONE. REINSTALLED THE TAILCONE AND REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. THE CAUSE FOR FAILURE OF THE EMERGENCY EVACUATION SLIDE TO DEPLOY WAS IMPROPER INSTALLATION OF THE AUTOMATIC DEPLOYMENT LANYARD. THE LANYARD WAS NOT PROPERLY INSERTED THROUGH THE GIRT TAB THUS FAILING TO DISCHARGE THE INFLATION BOTTLE. (M) 2L72 4F RTA6WE 19950915005631995091500563SO 1995 9 15 ASOA95021 119950826A7931APT79100080D OIL PRESS TRANS EMB 120 EMB120RT SO LT ENGINE DEFECTIVE A ASOAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO11242AS 120069 INBOUND ATL-FAY, CAPTAIN ADVISED THAT APPROXIMATELY 50 MILES OUT THE LEFT ENGINE OIL PRESSURE PEGGED. THE CAPTAIN ELECTED TO SHUT DOWN THE ENGINE AND DECLARE AN EMERGENCY. LANDING WAS MADE IN FAY SAFELY AND WITHOUT INCIDENT. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915005641995091500564WP 1995 9 15 HALA95101 119950809A335060030431 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 10222 47662 HNL - FORWARD EMERGENCY LIGHT PACK INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950915005651995091500565WP 1995 9 15 HALA95103 119950810A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN SHORTED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 47662 HNL - WHEN CHECKING EMERGENCY POWER, NO OVERHEAD LIGHT CAME ON IN CABIN. REPAIRED SHORTED WIRING AND REPLACED LAMPS. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950915005661995091500566WP 1995 9 15 HALA95104 119950811A3350 EEL BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13699HA 47763 HNL - FORWARD CEILING EMERGENCY LIGHTS INOPERABLE. REPLACED EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19950915005671995091500567EU 1995 9 15 M3HA95016 119950817A33503011151 EEL BATTERY AEROSPATR42 ATR42320 8680930EU CABIN DISCHARGED A M3HAK NONE L NO TEST ININSP/MAINT 1 WP13985MA 2569 358 HNL - TRACK LIGHTS FORWARD OF ROW 3 INOP. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY FOR LIGHTS IAW JIC 33-51-21 RAI 10010-001, OPS CHECK GOOD. (M) 2H72 4T RTA53EU 19950915005681995091500568NM 1995 9 15 PCAA9500232 119950717A291082970010121 HYD LINE DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYSTEM FAILED A PCAAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 EA13831EX1154613248 160 NR 1 HYD SYSTEM QUANTITY INDICATION DROPPED TO 0 FOLLOWED BY NR 1 PRESS INDICATION SYSTEM DROPPING TO 0. TROUBLESHOT, FOUND LINE FROM ANTI-SKID CONTROL VALVE TO PRESSURE MANIFOLD CRACKED, INSTALLED FLEX LINE, NEW ENGINE DRIVEN PUMP AND CASE DRAIN MANIFOLD. SERVICED AND BLED NR 1 SYSTEM IAW M/M. GROUND TEST OK. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19950915005691995091500569NE 1995 9 15 PCAA9500235 219950720A73103038454 FUEL FILTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE CLOGGED A PCAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA13821EX1207813820 173 120939 NR 2 FUEL FILTER BYPASS LIGHT ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED. REMOVED AND REPLACED HIGH AND LOW PRESSURE FILTERS, BYPASS SWITCH, RAN ENGINE, OPS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA13NM E20NE 19950915005701995091500570EU 1995 9 15 RAIA950806 119950808A7712 CONNECTOR AEROSPATR42 ATR42300 8680920EU RT ENGINE DIRTY A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03426TE 228 STL - FLT NR 7176 - RT TORQUE IN FLIGHT UP TO 120 PERCENT BOTH ANALOG AND DIGITAL FUEL FLOW NORMAL. MAINTENANCE CLEANED ALL RT ENGINE WIRING HARNESS P/N 311198201, CANNON PLUGS. GROUND RUNS REVEALED NORMAL ENGNIE PARAMETERS. (M) 2H72 4T RTA53EU 19950915005711995091500571EU 1995 9 15 RAIA950807 119950809A21708323715 WATER SOCK BAG JETSTMJETSTM3201 1500217EU LT/RT DIRTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03342TE6516 1385 954 STL - NR 7083 - EXCESSIVE STEAM OR SMOKE COMING FROM RT PACK. MAINTENANCE REPLACED BOTH WATER SOCKS AND DRAINED OIL FROM COOLING TURBINE LEFT AND RT. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19950915005721995091500572 1995 9 15 RAIA950808 319950808A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03432AM5818 883 STL - FLT NR 7416 - LEFT BETA LIGHT WILL NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED LEFT BETA SWITCH. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005731995091500573 1995 9 15 RAIA950809 319950808A61403997049005 BETA LINE BAG JETSTMJETSTM3201 1500217EU LT ENGINE AIRLOCK A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03432AM5818 883 STL - FLT NR 7314 - LEFT BETA LIGHT WILL NOT EXTINGUISH ON TAKEOFF. MAINTENANCE BLEED OIL LINE TO BETA SWITCH AND REMOVED AIRLOCK. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005741995091500574 1995 9 15 RAIA950810 419950808A61228974106 GOVERNOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03432AM5818 444 883 STL - FLT NR 7430 - LEFT BETA LIGHT WOULD NOT EXTINGUISH ON TAKEOFF. MAINTENANCE REPLACED LEFT PROPELLER GOVERNOR. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005751995091500575 1995 9 15 RAIA950811 319950809A61408659567 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03432AM5818 883 STL - FLT NR 7466 - LEFT BETA LIGHT WOULD NOT EXTINGUISH ON TAKEOFF. MAINTENANCE REPLACED LEFT BETA SWITCH. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005761995091500576EU 1995 9 15 RAIA950812 119950809A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03343TE9540 9540 955 JLN - FLT NR 7060 - RT ENGINE DOES NOT MAKE TORQUE. MAINTENANCE ADJUSTED RT ENGINE TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SHEET. GROUND POWER RUNS REVEALED NORMAL ENGINE PARAMETERS. (M) 2L72 4T RTA56EU 19950915005771995091500577SO 1995 9 15 RAIA950813 119950808A3244 TIRE EMB 120 EMB120RT SO LT MLG BLOWN A RAIAO OTHER O OTHER LDLANDING 1 CE03124AM 120016 STL - NR 7503 - ON LANDING, LOST LEFT BRAKES, TOOK FULL LEFT RUDDER INPUT TO STAY ON RUNWAY. MAINTENANCE REPLACED BOTH LEFT WHEELS P/N 31446, NO SKID MARKS NOTED. (M) 2L72 4T RTA31SO 19950915005781995091500578EU 1995 9 15 RAIA950814 119950808A3240AC66867 CONTROL VALVE BAG JETSTMJETSTM3201 1500217EU LT MLG BRAKE FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03435AM8328 2221 889 STL - FLT NR 7413 - LEFT BRAKE GRABS. MAINTENANCE REPLACED BRAKE CONTROL VALVE. TAXI CHECK REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19950915005791995091500579EU 1995 9 15 RAIA950815 119950808A3244AHA1752 TIRE AEROSPATR72 ATR72202 8680940EU LT MLG LOW PRESS A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03723TE398 283 STL - FLT NR 7012 - LEFT OUTBOARD BRAKE PIN ALMOST FLUSH PULLS HARD LEFT BRAKING WITH OR WITHOUT ANTI-SKID. MAINTENANCE INSPECTED WEAR INDICATORS AND FOUND TO BE WITHIN LIMITATIONS OF MM. SERVICED LEFT MAIN TIRES. (M) 2H72 4T RTA53EU 19950915005801995091500580EU 1995 9 15 RAIA950816 119950809A3240AH54450 BRAKE BAG JETSTMJETSTM3201 1500217EU LT/RT MLG REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03875JX2864 875 STL - FLT NR 7036 - BRAKES WEAK AT HIGH SPEED PEDAL FIRM BUT BRAKES APPEAR WEAK. MAINTENANCE INSPECTED BRAKES AND BLED BOTH BRAKES. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005811995091500581EU 1995 9 15 RAIA950817 119950811A3244 TIRE BAG JETSTMJETSTM3201 1500217EU LT MLG FIRE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK A FLAME/FIRE TOTAKEOFF 1 CE03875JX 875 STL - FLT NR 7104 - LEFT MAIN TIRE FIRE ON TAKEOFF. MAINTENANCE INSPECTED LEFT MAIN WHEEL WELL, PERFORMED DETAILED VISUAL INSPECTION OF STRUT, WING. REPLACED LEFT MAIN WHEEL, BRAKE AND MAXARET. OPERATION AND LEAK CHECK OK. (M) 2L72 4T RTA56EU 19950915005821995091500582WP 1995 9 15 RAIA950818 219950813A7320A218C14 RPM SCREW BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03425AM8353 2253 870 66145 STL - FLTN RN 7318 - RT ENGINE SLOW TO ACCELERATE, ACHIEVED ONLY 60 PERCENT TQ. MAINTENANCE ADJUSTED RT ENGINE TAKEOFF RPM SCREW X. GROUND PERFORMANCE RUNS REVEALED NORMAL OPERATION. ALL ENGINE PARAMETERS NORMAL. (M) 2L72 4T4 TRTA56EU E4WE 19950915005831995091500583EU 1995 9 15 RAIA950819 119950813A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03430AM 880 66152 STL - FLT NR 7512 - RT ENGINE WOULD NOT MAKE TARGET TORQUE. ADJUSTED RT TORQUE SIGNAL CONDITIONER TO GARRETT DSC SETTING, GROUND POWER RUNS CHECK OK. ALL ENGINE PARAMETERS NORMAL. (M) 2L72 4T4 TRTA56EU E4WE 19950915005841995091500584NE 1995 9 15 RAIA950821 219950815A7320310465701 CONNECTOR AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE RT ENG DIRTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03722TE 220 124410R SGF - FLT NR 7008 - RT ENGINE SLOW TO SPOOL, DID NOT ACHIEVE TAKEOFF TORQUE. MAINTENANCE CLEANED RT ENGINE ECU CANNON PLUG FROM OIL RESIDUAL. GROUND RUNS CHECK NORMAL, COULD NOT DUPLICATE DISCREPANCY. (M) 2H72 4T4 TRTA53EU E2ONE 19950915005851995091500585EU 1995 9 15 RAIA950822 119950816A7331696219 FUEL INDICATOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP COCKPIT FAULTY A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03859AE2893 859 66065 SAN - FLT NR 4745 - RT FUEL LOW PRESSURE INDICATION DROPPED DOWN INTO THE YELLOW. MAINTENANCE REPLACED RT FUEL INDICATOR AND TRANSMITTER. (M) 2L72 4T4 TRTA56EU E4WE 19950915005861995091500586EU 1995 9 15 RAIA950824 119950817A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03422AM9974 5999 856 66298 JLN - FLT NR 7064 - RT ENGINE FAILED TO ACHIEVE TARGET TORQUE. MAINTENANCE ADJUSTED RT TORQUE SIGNAL CONDITIONER AS PER GARRETT DCS SETTINGS. GROUND POWER RUNS REVEALED ALL ENGINE PARAMETERS TO BE NORMAL. (M) 2L72 4T4 TRTA56EU E4WE 19950915005871995091500587EU 1995 9 15 RAIA950825 119950816A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03429AM9499 4929 879 DEC - FLT NR 7301 - RT ENGINE DID NOT MAKE TARGET TORQUE, ENGINE AT 650 IS ONLY PRODUCING 90 PERCENT. MAINTENANCE ADJUSTED RT ENGINE TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTINGS. POWER CHECK GOOD ON GROUND RUN. (M) 2L72 4T RTA56EU 19950915005881995091500588EU 1995 9 15 RAIA950826 119950817A77129AA1108118 TQ SENSING LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 CE03972JX8241 2141 972 66076 LAX - FLT NR 4763 - LEFT ENGINE OIL PRESSURE ERRATIC. MAINTENANCE REPLACED LEFT ENGINE NEGATIVE TORQUE SENSING OIL LINE. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19950915005891995091500589WP 1995 9 15 RAIA950831 219950818A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RIGHT FAILED A RAIAO OTHER A FLAME/FIRE CRCRUISE 1 CE03425AM8379 2312 870 66145 CMI - FLT NR 7440 - RT ENGINE FAILED. MAINTENANCE REPLACED RT ENGINE. PERFORMED DETAILED VISUAL INSPECTION OF ALL ENGINE ACCESSORIES. (M) 2L72 4T4 TRTA56EU E4WE 19950915005901995091500590EU 1995 9 15 RAIA950833 119950817A2150S2158111901600 LINE AEROSPATR72 ATR72202 8680940EU RT/LT PACK LOOSE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE7104 283 STL - FLT NR 7120 - SMOKE IN COCKPIT AND CABIN. MAINTENANCE REPAIRED WATER LINES AT RT AND LEFT PACKS. SYSTEM TEST OK. (M) 2H72 4T RTA53EU 19950915005911995091500591EU 1995 9 15 RAIA950834 119950821A33503011151 EEL BATT PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE2444 119 STL - FLT NR 7136 - AFT CENTER EMERGENCY LIGHT DOES NOT WORK WITHOUT BATTERY POWER ON. MAINTENANCE REPLACED BATTERY PACK FOR EMERGENCY LIGHT. SYSTEM CHECK GOOD ON TEST. (M) 2H72 4T RTA53EU 19950915005921995091500592EU 1995 9 15 RAIA950836 119950902A3242AC63742 MAXARET BAG JETSTMJETSTM3201 1500217EU RT MLG FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03436AM9363 891 STL - BRAKES GRAB DURING TAXI CAUSING AIRCRAFT TO SHUDDER. MAINTENANCE REPLACED RT MAXARET UNIT. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19950915005931995091500593WP 1995 9 15 RAIA950837 219950822A7320A218C14 RPM SCREW BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG OUT OF ADJ A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03434AM8234 2134 887 66139 STL - FLT NR 7067 - LEFT ENGINE TORQUE DROPPED FROM 80 PERCENT TO 40 PERCENT. MAINTENANCE ADJUSTED LEFT ENGINE MAX RPM. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T4 TRTA56EU E4WE 19950915005941995091500594WP 1995 9 15 USAA950769 119950713A335020131A EEL BATTERY PACK DOUG DC9 DC931 3022065WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19971VJ 47051 CLT -FLT NR 1437 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19950915005951995091500595WP 1995 9 15 USAA950770 119950725A3350 EEL WIRE DOUG DC9 DC931 3022065WP CABIN CHAFING A USAAK NONE L NO TEST ININSP/MAINT 1 EA19963VJ 47508 BWI - FLT 0589 - THE EMERGENCY LIGHTS WERE POPPING THE CIRCUIT BREAKER. MAINTENANCE REPAIRED WIRES THAT WERE FOUND TO BE CHAFING IN THE CEILING OF THE AFT LAVATORY AGAINST THE WATER LINE. (M) 2L72 4F A6WE 19950915005961995091500596WP 1995 9 15 USAA950776 119950727A3350 EEL BATTERIES DOUG DC9 DC931 3022065WP CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19969VJ 47421 PIT - FLT 0519 - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSTALLED NEW BATTERIES IN THE POWER PACK. (M) 2L72 4F A6WE 19950915005971995091500597NM 1995 9 15 USAA950839 119950803A5210 STRAP BOEING737 737201 1384454NM PAX DOOR UNSECURE A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19229US 21818 PIT - FLT 0281 - THE REAR PASSENGER DOOR WAS CLOSED WITH THE SAFETY STRAP OUTSIDE. AIRCRAFT RETURNED TO PIT. MAINTENANCE SECURED THE RIGHT REAR SERVICE DOOR SAFETY STRAP IN THE HOLDER. NO DAMAGE WAS NOTED TO THE DOOR OR FUSELAGE. (M) 2L72 4F A16WE 19950915005981995091500598SO 1995 9 15 WTAA950245 119950815A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17455UE 120163 ACV, TAKEOFF FLAP WARNING ACTIVATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT OUTBOARD ACTUATOR. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915005991995091500599NE 1995 9 15 WTAA950246 219950818A7321 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17122AM 120013 RDD - RIGHT ENGINE NH REPORTED AT 106 PERCENT ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. PERFORMED ENGINE GROUND RUNS. ALL ENGINE PARAMETERS REPORTED NORMAL WITH EEC OFF AND ON. ENGINE OVERSPEED TEST OPERATIONAL CHECK NORMAL. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19950915006101995091500610WP 1995 9 15 95ZZZM417 119950826A3350EA1D21D15 EEL BATT PACKS DOUG DC9 DC932 3022066WP COCKPIT DISCHARGED A VJ6AK NONE L NO TEST TXTAXI/GRND HDL 1 SO11915VV 47443 FLT NR 485 - PHF-ATL - COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOP UPON CREW LEAVING THE AIRCRAFT IN ATL. MAINTENANCE REPLACED BATTERY PACKS P/N EA1D131D15 AND 6012231. OPS CHECKED OK. 2L72 4F A6WE 19950915006111995091500611WP 1995 9 15 95ZZZM418 119950616A53505644530501 DOOR DOUG DC8 DC862 3021970WP TAILCONE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND CORROSION AROUND TAILCONE LOWER DOOR. MECHANICALLY REMOVED CORROSION. TREATED AND PRIMED AREA. FABRICATED AND INSTALLED DOUBLER IAW DER DWG ARW 950051-6037. 2L74 4F 4A25 19950915006121995091500612WP 1995 9 15 95ZZZM419 119950409A5330 SKIN DOUG DC8 DC862 3021970WP FS 1300 DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 ON C-CHECK FOUND, 9 INCHES BY 9.5 INCHES TEMP REPAIR AT FS 1300 L26R, UPPER AFT CORNER OF 'D' BELLY DOOR CUTOUT. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED DOUBLERS IAW DAC DWG SR 08530019. (M) 2L74 4F 4A25 19950915006131995091500613WP 1995 9 15 95ZZZM420 119950615A5512565174763 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAS CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT T/E. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED. (M) 2L74 4F 4A25 19950915006141995091500614WP 1995 9 15 95ZZZM421 119950615A5320 DOUBLER DOUG DC8 DC862 3021970WP CARGO DR CUTOUT DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND IN PROPER REPAIR ON THE LOWER FORWARD CARGO COMPARTMENT AFT DOOR CUTOUT AT LOWER FWD SAB CORNER. REMOVED IN PROPER REPAIR, FABRICATED DOUBLERS USE CLAD 7075-TL 125 AND .090 TREATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 51-1-21, 51-3-0, 51-1-20D AND DRAWING SR 08530019. 2L74 4F 4A25 19950915006151995091500615WP 1995 9 15 95ZZZM422 119950427A5751 SKIN DOUG DC8 DC862 3021970WP RT AILERON DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND 26 INCHES BY 12 INCHES TEMP REPAIR ON RT INBOARD AILERON LOWER SURFACE. REMOVED PREVIOUS SKIN PANEL FROM XA 542.00 TO XW 563.00 CUT REAR SPAR FOR ACCESS. INSTALLED NEW SKIN PANEL AND INSTALLED REPAIR DOUBLERS ON REAR SPAR IAW DER DWG ARW 950051-0484. 2L74 4F 4A25 19950915006161995091500616WP 1995 9 15 95ZZZM423 119950616A5320 PRESS FLOOR DOUG DC8 DC862 3021970WP BS 182 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND UNDERSIDE OF COCKPIT PRESSURE FLOOR WITH LEVEL 2 CORROSION AT FS 182 LBL 44. CUT OUT CORRODED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW DER DWG ARW 950051-4066. 2L74 4F 4A25 19950915006171995091500617WP 1995 9 15 95ZZZM424 119950703A5730 SKIN DOUG DC8 DC862 3021970WP CENTER WING CORRODED A ARWAO OTHER Z SIGNIFICANT FAILURE REPORT ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON WING CENTER SECTION UPPER SKIN PANEL SPLICE DOUBLER AT XCW 0.000 FS 780. MECHANCICALLY REMOVED CORROSION. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DER DWG ARW 950051-5296. 2L74 4F 4A25 19950915006181995091500618WP 1995 9 15 95ZZZM425 119950409A5330 SKIN DOUG DC8 DC862 3021970WP FS 290 DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND TEMP REPAIR AT FS 290.00 L26R AT TOILET DUMP ACCESS. REMOVED TEMP REPAIR. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-5011. 2L74 4F 4A25 19950915006191995091500619WP 1995 9 15 95ZZZM426 119950616A5330 SKIN DOUG DC8 DC862 3021970WP BS 225-270 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL TWO CORROSION INSIDE FORWARD ACCESSORY COMPARTMENT ON L27R BETWEEN FS 225 AND 270. REMOVED CORROSION. FABRICATED AND INSTALLED FILLER AND DOUBLER, IAW DER DWG ARW 950051-0566. MFG AND INSTALLED LONGERON IAW DAC DWG 5613861510. 2L74 4F 4A25 19950915006201995091500620WP 1995 9 15 95ZZZM427 119950612A5330 SKIN DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON SKIN UNDER AFT END 'C' BELLY DOOR SILL PROTECTOR. REMOVED SCUFF PLATE. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER IAW SRM 51-1-8 AND 5-1-16 PER DER DWG ARW 950051-5100. 2L74 4F 4A25 19950915006211995091500621WP 1995 9 15 95ZZZM428 119950615A5730 SKIN DOUG DC8 DC862 3021970WP RT WING CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND RT WING UPPER LEADING EDGE BETWEEN NR 3 AND NR 4 ENGINES AREAS OF BULGING SKIN CORROSION LEVEL 2 SMALL CRACKS. REMOVED CORROSION FOUND BEYOND LIMITS IAW SRM 57-2-0 CUT OUT DAMAGE SECTION, FABRICATED DOUBLER AND FILLER IAW DER 950051-1098 TREATED PRIMED AND INSTALLED IAW DER ARW 950051-1098. 2L74 4F 4A25 19950915006221995091500622WP 1995 9 15 95ZZZM429 119950615A55125644330101 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB LECORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 FOUND DURING C-CHECK, LEFT HORIZONTAL STABLE INBOARD FROM XAR TO XFS 178 HAS LEVEL II CORROSION ON UPPER SIDE AROUND ATTACH FASTENERS. CUT OUT CORRODED AREA, FABRICATED DOUBLERS AND FILLERS IAW DER ARW 950051-0966 AND SRM 57-2-1 FIG 38 DAC 274118/G1P1518. 2L74 4F 4A25 19950915006231995091500623NE 1995 9 15 C2XA95CL112 219950816A7250 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE LEFT FAILED A AC2XAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SW0914822146419650 120531 163 120531 FLT NR 3852 - EWR-MVY - DURING FLIGHT NR 1 ENGINE FIRE WARNING ACTIVATED. THE NR 1 AND NR 2 FIRE BOTTLES WERE DISCHARGED. MAINTENANCE INSPECTED ENGINE, SUSPECT POWER TURBINE FAILURE. REMOVED AND REPLACED NR 1 ENGINE AND NR 1 AND NR 2 FIRE BOTTLES IAW TASK CARD NR 72-00-00 AND 26-21-71. 2H72 4T4 TRTA53EU E20NE 19950915006241995091500624SO 1995 9 15 C2XA95IA183 119950822A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO LT WING OUTBD CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 2, NR 3, NR 4 AND NR 5 SKIN SUPPORTS CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006251995091500625SO 1995 9 15 C2XA95IA184 119950822A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO LT WING OUTBD CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER NR 2, AND NR 3 SKIN SUPPORTS CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006261995091500626SO 1995 9 15 C2XA95IA185 119950822A572012017056019 SKIN SUPPORT EMB 120 EMB120RT SO RT WING OUTBD CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 5 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006271995091500627SO 1995 9 15 C2XA95IA186 119950822A572012017056005 SKIN SUPPORT EMB 120 EMB120RT SO RT WING OUTBD CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING UPPER NR 3 SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006281995091500628SO 1995 9 15 C2XA95IA187 119950822A572012017057017 SKIN SUPPORT EMB 120 EMB120RT SO RT WING OUTBD CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 2 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006291995091500629SO 1995 9 15 C2XA95IA188 119950822A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 16. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006301995091500630SO 1995 9 15 C2XA95IA189 119950822A572012017056021 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 3 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006311995091500631SO 1995 9 15 C2XA95IA190 119950822A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND RT WING NR 4 LOWER SKIN SUPPORT CRACKED AT RIB NR 15. MAINTENANCE REMOVED AND REPLACED THE SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006321995091500632SO 1995 9 15 C2XA95IA191 119950822A532012015374001 ANGLE EMB 120 EMB120RT SO FIN TO FUSE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FIN TO FUSELAGE ATTACH (DRAG) ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950915006331995091500633SO 1995 9 15 C2XA95IA192 119950823A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND CABIN FLOOR LEFT SEAT TRACK CORRODED FORWARD OF GALLEY. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915006341995091500634SO 1995 9 15 C2XA95IA193 119950823A534712015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND CABIN SIDEWALL LEFT SEAT TRACK CORRODED AT FORWARD END. REMOVED AND REPLACED AFFECTED PORTION OF TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915006351995091500635SO 1995 9 15 C2XA95IA194 119950823A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND CABIN FLOOR LEFT SEAT TRACK CORRODED. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915006361995091500636SO 1995 9 15 C2XA95IA195 119950823A534712015597003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0959708 120098 IAH - DURING C-CHECK INSPECTION, FOUND CABIN RT SIDEWALL SEAT TRACK CORRODED. REMOVED AND REPLACED AFFECTED PORTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950915006371995091500637NM 1995 9 15 USAA950838 119950706A3350900835A EEL BATT PACK BOEING737 7372B7 1384560NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19267AU 22879 CLE - THE CABIN CEILING EXIT SIGN, FOR THE OVERWING EMERGENCY EXIT, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2L72 4F A16WE 19950915006381995091500638NM 1995 9 15 USAA950841 119950806A2750251N41351 SHAFT BOLT 251N405039 BOEING757 757225 1384959NM NR 1 TE FLAP SHEARED A AUSAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 EA19600AU 445 22192 SFO - FLT NR 0851 - THE FLAPS WERE FROZEN AT 15 DEGREES AND WOULD NOT RETRACT. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO SFO. MAINTENANCE FOUND A BOLT ON THE FLAP TRANSMISSION. OPERATIONS CHECKED NORMAL. (M) 2L72 4F RTA2NM 19950915006391995091500639WP 1995 9 15 USAA950842 119950805A3350 EEL BATTERIES DOUG DC9 DC981 3022081WP COCKPIT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19801US 48037 DCA - THE COCKPIT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2L72 4F A6WE 19950915006401995091500640EU 1995 9 15 WIMA951712 119950620A3230C24589000 UPLOCK BOX AEROSPATR72 ATR72212 EU RT MLG FAILED A SIMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW21377AT2790 5473 377 YHZ - FLT 4398 - RT MLG SHOWED UNLK ON BOTH INDICATION PANELS, RETURNED TO YHZ. MAINTENANCE PINNED GEAR THEN ISSUED MEL. DEAD HEADED AIRCRAFT TO ALB. MAINTENANCE REMOVED AND INSPECTED UPLOCK BOX SYSTEM. OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950915006411995091500641NM 1995 9 15 TWRA9535 119950622A335086210066 EEL BATT PACK BOEING747 747259B NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND EVAC LIGHTS BATTERY PACK DEPLEATED AT ROW 50ABC. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK. (M) 2L74 4F RTA20WE 19950915006421995091500642NM 1995 9 15 TWRA9536 119950622A335087310012 EEL BOEING747 747259B NM CABIN INOP A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND EVAC LIGHT MISSING AT ROW 60A. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2L74 4F RTA20WE 19950915006431995091500643NM 1995 9 15 TWRA9537 119950622A335087310012 EEL BOEING747 747259B NM CABIN INOP A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND EVAC LIGHT AT ROW 19A BROKEN. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK OK. (M) 2L74 4F RTA20WE 19950915006441995091500644NM 1995 9 15 95FDEA01333 119950913A2740 MOTOR BOEING727 727233 138408ANM STAB TRIM FAILED A FDEAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SO25258FE 20940 A/P AND CRUISE STABILIZER TRIM ACTUATOR CIRCUIT BREAKER TRIPPED IN DESCENT. DISCONNECTED A/P. RESET CIRCUIT BREAKER, IT TRIPPED SECOND TIME. REMOVED AND REPLACED CRUISE TRIM MOTOR. OPS CK GOOD. 2L73 4F RTA3WE 19950915006451995091500645WP 1995 9 15 95FDEA01334 119950913A5400 SPAR DOUG DC10 DC1030F 3023504WP NR 1 PYLON CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 NR 1 PYLON UPPER SPAR RT CHORD, AFT 16, HAS RUST ON TOP OF HORIZONTAL FLANGE AND INBOARD SIDE OF TOP VERTICAL FLANGE. CLEANED AND TREATED CORROSION PER SRM 51-21-01, PAGE 36. 2L73 4F RTA22WE 19950915006461995091500646NM 1995 9 15 95FDEA01335 119950913A2780 RETRACT MECH BOEING727 72722 1384002NM NR 7 LE FLAP MALFUNCTIONED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25150FE 19141 DURING CLIMBOUT FROM MEM, WHEN RETRACTING FLAPS FROM 2 DEGREES TO ZERO, LED NR 7 WOULD NOT RETRACT. RECYCLED FLAPS FROM 2 DEGREES TO ZERO THREE TIMES, BUT LED NR 7 REMAINED EXTENDED EACH TIME. INSPECTED ACT INST AND SWS, ALL CK GOOD. SUSPECT AIR IN SYS, CYCLED FLAPS SEVERAL TIMES. ALL IND GOOD. OK FOR SERVICE. 2L73 4F A3WE 19950915006471995091500647NM 1995 9 15 95FDEA01336 119950913A2782 ACTUATOR BOEING727 72722 1384002NM NR 7 LE FLAP MALFUNCTIONED A FDEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 SO25150FE 19141 DURING CLIMBOUT FROM MEM WHEN RETRACTING FLAPS FROM 2 DEGREES TO ZERO, NR 7 SLAT RETRACT, RECYCLED FROM 2 TO ZERO 3 TIMES, BUT NR 7 SLAT REMAINED EXTENDED. REMOVED NR 7 SLAT ACTUATOR, CAPPED LINES. INSTALLED NR 7 SLAT ACT PER MM 27-81-32, OPS AND LEAK CK GOOD. OK FOR SERVICE. RII C/W NR 313. 2L73 4F A3WE 19950915006481995091500648 1995 9 15 95UAL900126 419950913A2565 SLIDE BF GOODRICH 7A14401 BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE L5 DOOR LEAKING A UALAK NONE L NO TEST ININSP/MAINT 1 WP294720U G1003 19881 DOOR 5 LT SLIDE FAILED POROSITY TEST DURING PROOF PRESSURE TEST AT OVERHAUL. SLIDE SCRAPPED. 2L74 4F4 F A20WE E20EA 19950915006491995091500649 1995 9 15 95UAL900127 419950913A2565 SLIDE BF GOODRICH 7A14181 BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE L3 DOOR TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29156UA G193 20105 DOOR 3 LEFT SLIDE, INTERNAL OUTBOARD BULKHEAD DAMAGE - TOP HINGE TAPE HAS 2.75 INCH TEAR. THE BOTTOM HINGE TAPE HAS A 2.25 INCH TEAR. THE TOP BULKHEAD HAS 2.75 INCH SEPARATION. THE BOTTOM BULKHEAD HAS 2.25 INCH SEPARATION. SLIDE ASSY SENT TO VENDOR FOR REPAIR. 2L74 4F4 F A20WE E20EA 19950915006501995091500650NM 1995 9 15 95UAL900129 119950913A3350 EEL BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297294U 21572 EMERGENCY LIGHT ABOVE AFT END OF VENTRAL STAIRS INOPERATIVE. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19950915006511995091500651NM 1995 9 15 95UAL900130 119950914A3350 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29533UA 25073 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW NR 16. RELAMPED. CHECKS O.K. 2L72 4F4 FRTA2NM E17NE 19950915006521995091500652NM 1995 9 15 95UAL900131 119950914A3350 EEL BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29605UA 21866 DOOR NR 2 LEFT, EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLY. CHECKS O.K. 2L72 4F4 FRTA1NM E3NE 19950915006531995091500653NM 1995 9 15 95UAL900132 119950914A3350 EEL STRIP BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29646UA 25283 EMERGENCY ESCAPE PATH LIGHTING INOP AT AFT GALLEY BETWEEN DOORS NR 2 LEFT AND NR 2 RIGHT. REPLACE LIGHT STRIP. CHECKS O.K. 2L72 4F4 FRTA1NM E24NE 19950915006541995091500654WP 1995 9 15 95UAL900133 119950914A49003602883 COOLING ASSY DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL APU PACKING WORN A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291834U742 742 47966 STRONG OIL SMELL IN AIRCRAFT, BELIEVE COMING FROM APU. REPLACED C-1, STATOR, RING AND COOLING FAN ASSEMBLY. 2L73 4F4 F A22WE E23EA 19950915006551995091500655WP 1995 9 15 ABXA9500737 119950913A27603644322509 DRIVE LINK DOUG DC8 DC863 302198AWP LT SPOILER FAILED A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23811AX 46113 DURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LT SPOILER SWITCH WAS BROKEN. REPLACED LINKS AND SWITCH IAW DC 8MM. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950915006561995091500656WP 1995 9 15 ABXA9500738 119950913A27603654073 LINK DOUG DC8 DC863 302198AWP LT SPOILER FAILED A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23811AX 46113 DURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LT SPOILER SWITCH WAS BROKEN. REPLACED LINKS AND SWITCH IAW DC 8MM. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950915006571995091500657WP 1995 9 15 ABXA9500739 119950913A27603654072 LINK DOUG DC8 DC863 302198AWP LT SPOILER FAILED A ABXAO OTHER J WARNING INDICATION APAPPROACH 1 GL23811AX 46113 DURING GEAR EXTENSION ON APPROACH, THE SPOILER EXTEND LIGHT ILLUMINATED; NO BUFFET WAS FELT. EXTENDED SPOILERS MANUALLY, LIGHT REMAINED ON AFTER THEY WERE RETRACTED. FOUND LT MOST INBOARD SPOILER PANEL DRIVE LINK AND OUTBOARD TOP DRIVE LINK BROKEN. ALSO, LT SPOILER SWITCH WAS BROKEN. REPLACED LINKS AND SWITCH IAW DC 8MM. SYSTEM OPS CHECKED GOOD. 2L74 4F 4A25 19950915006581995091500658SO 1995 9 15 COMA9511960 119950912A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAK NONE J WARNING INDICATION CLCLIMB 1 SO01117H 152327870 120117 LEFT MLG FAILED TO RETRACT. RETRACTION SUCCESSFUL ON SECOND ATTEMPT. REPLACED THE LT MLG RETRACT ACTUATOR. 2L72 4T RTA31SO 19950915006591995091500659EU 1995 9 15 COMA9531152 119950912A2450A2043C PDU SAAB SF340 SF340A 7850100EU RIGHT DEFECTIVE A COMAK NONE H ELECT. POWER LOSS-50 PC UKUNKNOWN 1 SO01343CA1528010 340A24 LEFT MAIN ELECTRICAL BUS WILL NOT COME ON LINE. REPLACED THE RT POWER DISTRIBUTION UNIT. 2L72 4T RTA52EU 19950915006601995091500660EU 1995 9 15 COMA9531153 119950911A2710DA5623A41 BEARING SAAB SF340 SF340A 7850100EU LT AILERON WORN A COMAK NONE E VIBRATION/BUFFET UKUNKNOWN 1 SO01158CA 340A158 SHUDDER FELT THROUGH CONTROL YOKE DURING INFLIGHT TURNS. REPLACED LT AILERON BEARINGS. 2L72 4T RTA52EU 19950915006611995091500661EA 1995 9 15 COMA9560547 119950910A2913PV304448 PUMP CNDAIRCL600 CL6002B19 EA RT ENGINE LEAKING A COMAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO01918CA2905 1129 7018 RIGHT HYDRAULIC PUMP IS LEAKING HYDRAULIC FLUID. REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP. 2L72 4F RTA21EA 19950915006621995091500662NM 1995 9 15 DL72S952587 119950613A5521657278419 SPAR BOEING727 727232 1384082NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING SHOP INSPECTION, THE LOWER FORWARD SPAR CAP WAS FOUND CRACKED 8 FEET FROM THE INBOARD EDGE. THE SPAR WAS REPAIRED PER SRM 55-20-5. 2L73 4F A3WE 19950915006631995091500663NM 1995 9 15 DL72S953632 119950820A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 UPON HMV, FOUND .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A. 2L73 4F A3WE 19950915006641995091500664NM 1995 9 15 DL72S953685 119950912A3350 BATTERY PACK 900835A BOEING727 727232 1384082NM EMERGENCY LIGHTSDISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11419DA 40471997 21272 LT AND RT LOWER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS EACH SIDE. RT SIDE CKS NORMAL. LT SIDE FORWARD TO MCO. 2L73 4F A3WE 19950915006651995091500665WP 1995 9 15 DLL10953699 119950906A5312 FITTING LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 COMPLYING WITH DL INSPECTION SI 7-66332-12 AND AD T95-18-52. AFT P-DOME TO STRINGER SPLICE FITTING WAS FOUND CRACKED AT STRINGER NR 10. SCHEDULED FITTING FOR REPLACEMENT PER DL ERA 271811-14AD. 2L73 4F A23WE 19950915006661995091500666WP 1995 9 15 DLL12953700 119950831A5312 BLKHD WEB LKHEED1011 1011385115 5265015WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11724DA 193C1151 WHILE REPLACING A LEFT WHEELWELL FIBERGLASS PANEL ATTACH ANGLE LOCATED ON THE FS 1363 BULKHEAD, A 1.5 INCH CRACK WAS FOUND ON THE FS 1363 BULKHEAD WEB UNDER THE PANEL ATTACH ANGLE. THE DAMAGE WAS REPAIRED PER SRM 53-11-00, PG 949 . 2L73 4F A23WE 19950915006671995091500667WP 1995 9 15 DLL13953691 119950131A7110LJ21744 NOSE COWL LKHEED1011 10113851 5265010WP ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11781DL 193A1003 DURING INSPECTION, A DENT WAS DISCOVERED IN THE EXTERIOR SKIN AT THE 5 0'CLOCK POSITION OF ENGINE NOSE COWL. COWL WAS ROUTED TO SHOP WHERE DAMAGE WAS REPAIRED PER SRM 54-31-00. 2L73 4F A23WE 19950915006681995091500668 1995 9 15 DLL16953682 419950912A34174031800902 AIR DATA COMP LKHEED1011 10113853 5265020WP NR 2 FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO11760DH 193Y1194 MACH TRIM CH 2 FAILED. MACH FEEL CH 2 FAIL. OVSPD CLACKER SOUNDED FOR NO REASON. COULD NOT SILENCE. HAD TO PULL CIRCUIT BREAKER. F/O A/S-ALT-RAD ALT AND VSI OFF FLAGS ALL SIMULTANEOUSLY APPEARED WITH INSTR COMP. ALT SCOREBOARD PRESENT. NO WIND READ OUT ON NR 2/3 INS. ALSO, ATS CH 2 FAILED IN-FLIGHT. WINDSHEAR COMPTR ANNUNC LITE ILLUM. FOUND NR 2 AIR DATA COMPUTER FAILED. REPLACED SAME AND LEAK CK AND TEST IS OK. 2L73 4F A23WE 19950915006691995091500669WP 1995 9 15 DLL17953692 119950903A7110 COWL 1512222110 LKHEED1011 10113853 5265020WP NR 2 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA EO195 193H1206 AT HMV, NR 2 ENGINE RT COWL PANEL WAS FOUND WITH WEAR DAMAGE AT LOWER FORWARD CORNER OF PANEL. ACCOMPLISHED REPAIRS PER SRM 51-50-01, FIG 2. 2L73 4F A23WE 19950915006701995091500670NM 1995 9 15 DLM88953683 119950912A5311 FRAME DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11938DL 49811 FOUND ON F2 LETTER CK, FORWARD OUTBD FRAME OF RT W/W OPENING IS CRACKED 2 INCHES. REPAIRED PER SRM 53-05. 2L72 4F RTA6WE 19950915006711995091500671WP 1995 9 15 MWEA95301 119950912A2560113313 EVAC SLIDE DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 CREW REPORTS UPON ARRIVAL TO THE A/C IN THE MORNING, THEY FOUND THE FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE HAD FALLEN OFF DOOR. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950915006721995091500672NM 1995 9 15 P5CA9500770 119950913A2720NAS13514H20P BOLTS BOEING747 747122 1384872NM UPPER RUDDER SHEARED A P5CAO OTHER J WARNING INDICATION APAPPROACH 1 WP23853FT 19753 ON APPROACH, NR 1 HYDRAULIC SYSTEM SHOWED DECREASING QUANTITY, WENT TO ZERO AFTER LANDING. TOWED AIRCRAFT FROM RUNWAY DUE TO LOSS OF NOSE WHEEL STEERING. FOUND SHEARED BOLTS RETAINING FILTER ON UPPER RUDDER PACKAGE. REPLACED BOLTS, LEAK CHECK OK. 2L74 4F A20WE 19950915006731995091500673NM 1995 9 15 UPS204397 119950913A33501000677 EEL BOEING727 72722C 138400FNM CABIN MALFUNCTION A IPXAK NONE L NO TEST CLCLIMB 1 SO01942UP 19101 PILOT REPORTED EMERGENCY, CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. CYCLED EMERGENCY LIGHT SWITCH NUMEROUS TIMES. COULD NOT DUPLICATE. REPLACED EMERGENCY LIGHT OVER ENTRANCE DOOR, PRECAUTIONARY. 2L73 4F A3WE 19950915006741995091500674NM 1995 9 15 UPS204398 119950913A2613 OVERHEAT WIRE BOEING727 72727C 138400JNM NR 1 STRUT CHAFED A IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01914UP 19246 PILOT REPORTED ENGINE NR 1 STRUT LIGHT ILLUMINATED IN FLIGHT. ENGINE NR 1 WAS SHUT DOWN, WHEN LIGHT WOULD NOT EXTINGUISH LIGHT OFF AFTER SHUT DOWN. FOUND WIRE NR W902-20 AT CONNECTOR DM9526B CHAFED THROUGH AT CONNECTOR BARREL. REPAIRED WIRE AS REQUIRED. RAN NR 1 ENGINE WITH STRUT. PANELS REMOVED. NO AIR LEAKS FOUND. NR 1 CKS GOOD. PER MM 26-14-12 AND WDM 26-14-01. 2L73 4F A3WE 19950915006751995091500675NM 1995 9 15 UPS204411 119950914A3350 EEL BATTERY BOEING727 7272A1 138407FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01213UP 21341 WHILE ON GROUND, MAINTENANCE FOUND BOTH EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERIES IN COCKPIT, LT ASSY, AND REPLACED FORWARD ENTRY LIGHT ASSY. OPS CKS OK. S/N OFF 72254. S/N ON 4663. 2L73 4F A3WE 19950915006761995091500676NM 1995 9 15 UPS404390 119950913A5313 STRINGER BOEING747 747123 1384873NM BS 1740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STRINGER END CRACKED AND CORRODED AT BSTA 1740, RT SIDE STR 32 (UNDER SPLICE). REPAIRED STR 32 AT BSTA 1740, RT PER SRM 53-10-03. 2L74 4F A20WE 19950915006771995091500677NM 1995 9 15 UPS404391 119950913A5315 FLOORBEAM BOEING747 747123 1384873NM BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT FLOORBEAM BETWEEN LBL 98 AND LBL 75, STA 1580. FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM IAW SRM 53-10-07, FIG 12, FROM LBL 98 TO 75, STA 1580. 2L74 4F A20WE 19950915006781995091500678NM 1995 9 15 UPS404392 119950913A5311 FRAME BOEING747 747123 1384873NM BS 1640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR-C CHECK, MAINTENANCE FOUND FRAME CRACKED ON TOP OF BSTA 1640 NEAR STR 29 (JUST ABOVE STRINGER CLIP). CRACK IN FRAME AT BSTA 1640 NEAR STR 29 RT, REPAIRED PER SRM 51-40-03, FIG 7. 2L74 4F A20WE 19950915006791995091500679NM 1995 9 15 UPS404399 119950914A261121561 SMOKE DETECTOR BOEING747 747123 1384873NM MAIN DECK CARGO INOPERATIVE A IPXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01675UP 20390 SUPPLEMENTAL MRR - PILOT REPORTED, ENGINE MAIN DECK CARGO FIRE AND SMOKE LIGHT NR 3 ILLUMINATED, WHILE AT FL 390. INITIATED UPS EMER PROCEDURE. WITH PACKS OFF AND A/C COMPLETELY PRESSURIZED AND PASSING THROUGH 10,000 FT, LIGHT EXTINGUISHED. NO SMOKE OR FIRE WAS EVER VISIBLE TO CREW. REPLACED BOTH 3A AND 3B SMOKE DETECTORS. ALSO, REPLACED AMPLIFIER AS PRECAUTIONARY, OPS CK GOOD PER MM 26-14-00. 2L74 4F A20WE 19950915006801995091500680NM 1995 9 15 UPS404405 119950914A5315 FLOORBEAM BOEING747 747123 1384873NM BS 1500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CORROSION AT THE FLOOR BEAM BETWEEN LBL 98 AND LBL 75, STA 1500. FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPLACED FLOORBEAM IAW SRM 53-10-07, FIG 12, AT LBL 75 TO 98 AT BS 1500. 2L74 4F A20WE 19950915006811995091500681NM 1995 9 15 UPS404406 119950914A5315 FLOORBEAM BOEING747 747123 1384873NM BS 460 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BS 460 STR 13A RT FLOORBEAM HAS CRACK ON FORWARD FACE OF WEB 1 INCH LONG AT THE UPPER SIDE OF THE WEB. CRACK OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FLOORBEAM WEB ACC SRM 53-10-07, FIG 11, AT BS 460, STR 13A RBL 90. 2L74 4F A20WE 19950915006821995091500682NM 1995 9 15 UPS404407 119950914A5315 FLOORBEAM BOEING747 747123 1384873NM BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FLOORBEAM CORRODED RBL 33.99, STA 1580 FLOORBEAM OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FLOORBEAM IAW SRM 53-10-07, FIG 12, AT 33.99 RBL STA 1580. 2L74 4F A20WE 19950915006831995091500683NM 1995 9 15 UPS404408 119950914A5311 FRAME BOEING747 747123 1384873NM BS 2702 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND APU COMPT FRAME CRACKED 1.5 INCHES LONG, LT SIDE AT BS 2702 WL 313. CRACK OUT OF LIMITS ACC SRM 53-10-01. REPAIRED FRAME AT BS 2702 WL 313 IAW SRM 51-40-03, FIG 3. 2L74 4F A20WE 19950915006841995091500684NM 1995 9 15 UPS404409 119950914A5313 STRINGER BOEING747 747123 1384873NM BS 2140-2160 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND BETWEEN STA 2140 - 2160, STR 27 RT CORROSION AND CRACKS. REMOVED CORROSION AND STOP DRILLED CRACKS ACC TO SRM 51-10-01. REPAIRED STRINGER ACC TO SRM 53-10-03, FIG 2. 2L74 4F A20WE 19950915006851995091500685NM 1995 9 15 UPS404410 119950914A5313 STRINGER BOEING747 747123 1384873NM BS 982 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STR 67R ON BSTA 982 IS CORRODED. CORROSION IS OUT OF LIMITS ACC SRM 53-10-01, FIG 1, DETAIL 1. REMOVED CORRODED PART AT BSTA 970 AND REPAIRED STRINGER ACC SRM 53-10-03, FIG 1 DETAIL 1. MATERIAL EXISTING STRINGER IS 0.090 INCH 7075T6. 2L74 4F A20WE 19950915006861995091500686WP 1995 9 15 UPS804393 119950913A533057552713 SKIN DOUG DC8 DC871F 302199DWP FS 220-340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGES ON FUSELAGE SKIN FS 220-340, LONGERONS 34R-36. REPLACED BELLY SKIN PANEL FROM FS 190-450 PER DAC DRAWING 5755271. 2L74 4F RT4A25 19950915006871995091500687WP 1995 9 15 UPS804394 119950913A53139754913 LONGERON DOUG DC8 DC871F 302199DWP FS 240-360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT 3 EACH LONGERONS. LONGERON 34R, FS 240-360. LONGERON 35R, FS 260-360. LONGERON 36, FS 250-330. REPLACED LONGERON SECTIONS PER SRM 51-1-20D. 2L74 4F RT4A25 19950915006881995091500688WP 1995 9 15 UPS804395 119950913A53203754930 FITTING DOUG DC8 DC871F 302199DWP FS 340 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 LOWER T-LOCK FITTING CORROSION REMOVAL OUT OF LIMITS. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950915006891995091500689WP 1995 9 15 UPS804396 119950913A573057695897 SKIN DOUG DC8 DC871F 302199DWP WS 304 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01755UP 46055 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE INNER SKIN CRACKED .50 INCH LONG AT STA XFS 304. REPAIRED SKIN PER UPS E.O. DC8-57-0593. 2L74 4F RT4A25 19950915006901995091500690WP 1995 9 15 UPS804400 119950914A53204640871 FITTING DOUG DC8 DC873F 302199FWP FS 1690 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON LONGERON 33L FITTING, FS 1690. REPLACED FITTING PER SM 51-1-20D, SRM 51-1-21 AND SRM 51-3-0. 2L74 4F RT4A25 19950915006911995091500691WP 1995 9 15 UPS804401 119950914A53151257075T6 FLOOR BEAM DOUG DC8 DC873F 302199FWP FS 1620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON AFT SIDE OF FLOORBEAM AND FITTING, FS 1620 LT CUSP. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19950915006921995091500692WP 1995 9 15 UPS804402 119950914A53115722956 FRAME DOUG DC8 DC873F 302199FWP FS 1640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION DAMAGE AT FWD SIDE OF BOLT FRAME DOUBLER FS 1640, FROM LONGERONS 25R-27R. REPLACED FRAME DOUBLER PER SRM 51-1-20D. 2L74 4F RT4A25 19950915006931995091500693WP 1995 9 15 UPS804403 119950914A534774529523 SEAT TRACK DOUG DC8 DC873F 302199FWP CABIN CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT NR 7 SEAT TRACK FWD END OF COMPARTMENT NR 15 AND AFT END OF COMPARTMENT NR 14. REPLACED SEAT TRACK PLUGS PER SRM 53-2-3. 2L74 4F RT4A25 19950915006941995091500694WP 1995 9 15 UPS804404 119950914A5330SR08530025 SKIN DOUG DC8 DC873F 302199FWP SERV DR CUTOUT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND AFT SERVICE DOOR FWD LOWER CORNER ON FUSELAGE SKIN CUT OUT IS CRACKED. REPAIRED PER UPS EO DC8-5310-7402-A. 2L74 4F RT4A25 19950915007081995091500708CE 1995 9 15 95ZZZX4611 119950825A2450 INVERTER HARNESS BEECH 90 E90 1152914CE AC BUS MISWIRED ASAVIBAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO131UC LW140 DURING AN INSPECTION, A DUAL FEEDER BUS CONFORMITY TEST WAS PERFORMED. THE INVERTER POWER HARNESS WAS FOUND WIRED TO THE WRONG BUSS (LT WIRED TO RT, AND VICE VERSA). SHOULD THE 325-AMP ISOLATION LIMITER BECOME OPEN, BOTH INVERTERS WOULD FAIL. THIS IS SECOND MODEL 90 THAT HAS BEEN WIRED IMPROPERLY. A ONE-TIME INSPECTION OF THE INVERTER SYSTEM BY REMOVING ONE 325-AMP LIMITER AT A TIME AND CHECKING INVERTER OPERATION WHICH WOULD SHOW THE MISWIRING PROBLEM IF BOTH INVERTERS FAILED, NR 1 INVERTER SHOULD FAIL ONLY WHEN NR 1 LIMITER IS REMOVED. SIMILAR RESULTS FOR NR 2 LIMITER REMOVAL. 1L72 3T 3A20 19950922000011995092200001NM 1995 9 22 9514232203 119950913A324021147AC DEBOOSTER VALVE BOEING727 727251 138408HNM LT MLG BRAKE FAILED A NWAAK NONE O OTHER LDLANDING 1 GL01220US1065 344 22543 DURING LANDING, THE NR 1 BRAKE SEIZED AND CAUSED NR 1 TIRE TO DEFLATE. MAINTENANCE REPLACED THE NR 1 BRAKE, TIRE AND DEBOOSTER VALVE. OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19950922000021995092200002WP 1995 9 22 9514249949 119950912A5312 BLKHD FITTING DOUG DC9 DC931 3022065WP FS 604 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 604 BULKHEAD END CAP AT LONGERON 24L. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19950922000031995092200003NM 1995 9 22 9514252279 119950913A5343 TRUNNION BOEING727 727251 138408HNM NLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01279US 21158 DURING PERIODIC CHECK, FOUND CORROSION ON THE UPPER RIGHT NOSE GEAR TRUNNION FITTING. REPLACED FITTING (P/N 65-17676-40), PER SRM 51-10-01 PG 4 PARA 4. 2L73 4F A3WE 19950922000041995092200004WP 1995 9 22 9514269953 119950911A5350 RELEASE SYST DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. ADJUSTED THE CLIPS AND RELEASE, SYSTEM CHECKED OK. 2L72 4F A6WE 19950922000051995092200005NE 1995 9 22 9514272292 219950913A7230 COMPRESSOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01292US 21503 696502 SUSPECTED COMPRESSOR STALL OCCURRED IN NR 3 ENGINE DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND NO DISCREPANCIES WERE NOTED. ON RUNUP, ENGINE PERFORMANCE WAS SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19950922000061995092200006NM 1995 9 22 95FDEA01337 119950914A2910 HYD LINE BOEING727 72725 1384006NM NR 2 ENGINE CHAFED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25154FE 18287 BOTH SYS-A HYD LOW PRESS LIGHTS CAME ON WITH AUDIBLE PRESS SURGES. A-SYS PRESS IND ZERO, FULL QTY IND AND OPERATED 3 MIN WITH LIGHTS ON. FOUND NR 2 ENG PUMP PRESS LINE CHAFED THROUGH BECAUSE OF MISROUTING. REMOVED AND REPLACED NR 2 HYD PUMP PRESS LINE AND REROUTED SAME. INSPECTED NR 1 AND 2 ENG CASE DRAIN FILTERS, PER MM 29-11-41, NO CONTAMINATION. REPLACED BOTH CASE DRAIN FILTERS PER MM 29-11-41. SERVICED HYD TO FULL AND REMOVED AND REPLACED A-SYS PRESS FILTER, LEAK CK GOOD PER MM 29-11-62. COMPLIED WITH SPECIAL INSPECTION MM 29-11-0 PAGE 101K. RAN NR 1 AND NR 2 ENG, LEAK CK GOOD. OK FOR SERVICE. 2L73 4F A3WE 19950922000071995092200007WP 1995 9 22 MWEA95302 119950913A7711 EPR WIRE DOUG DC9 DC932 3022066WP COCKPIT BROKEN A MWEACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL31302ME 47102 CREW REPORTS AT START OF TAKEOFF ROLL, LEFT ENGINE EPR GAUGE FLUCTUATES ABOVE 1.8 EPR. AIRCRAFT RETURNED TO GATE. MAINTENANCE LEAK CHECKED PT2 AND PT7 LINES AND NO LEAK FOUND. WIRE 'D' FROM EPR TRANSMITTER WAS FOUND BROKEN JUST ABOVE RUDDER PEDALS. REPAIRED WIRE, RAN ENGINES AND OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922000081995092200008 1995 9 22 MWEA95303 219950913A72205910297503 INLET BULLET DOUG DC9 DC914 3022034WP LT ENGINE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31600ME 45725 DURING INSPECTION, THE LEFT ENGINE NOSE INLET BULLET WAS FOUND CRACKED AT MOUNT BOLTS. MAINTENANCE REMOVED AND REPLACED NOSE INLET BULLET. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922000091995092200009WP 1995 9 22 SCNA95187 119950914A3350EMSE300 EEL POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15572SC 46977 THE FORWARD CABIN CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED FORWARD CABIN POWER SUPPLY AND BATTERY. CEILING EMERGENCY LIGHTS TEST GOOD. 2L73 4F A22WE 19950922000101995092200010NM 1995 9 22 UPS404421 119950915A5311 FRAME BOEING747 747123 1384873NM BS 1860 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1860 RT AT STR 13 TO 14 RT. FOUND DENTS OUT OF LIMIT ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 UPS EFN NR 747-53-0733. 2L74 4F A20WE 19950922000111995092200011NM 1995 9 22 UPS404422 119950915A5311 FRAME BOEING747 747123 1384873NM BS 1760 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1760 RT AT STR 10 AND 11 RT. FOUND DENTS OUT OF LIMITS ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 AND UPS EFN NR 747-53-0733. 2L74 4F A20WE 19950922000121995092200012NM 1995 9 22 UPS404423 119950915A5311 FRAME BOEING747 747123 1384873NM BS 1800 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DAMAGE FRAME AT BS 1800 RT AT STR 10 AND 11 RT. FOUND DENTS OUT OF LIMITS ACC SRM 53-10-01. REPAIRED PER DRW NR 2H101392 REV 2 AND UPS EFN NR 747-53-0733. 2L74 4F A20WE 19950922000131995092200013NM 1995 9 22 UPS404424 119950915A5320 T-CHORD BOEING747 747123 1384873NM BS 560 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FWD LOWER CARGO COMP T-CHORD CRACKED AT 'B' STA 560 LBL 48 AND AT 'B' STA 560 LBL 27 WL 120. REPLACED T-CHORD ACC SRM 53-10-07, CHORD REPAIRED ACC UPS EFN 747-53-0729. 2L74 4F A20WE 19950922000141995092200014NM 1995 9 22 UPS404425 119950915A5315 FLOORBEAM BOEING747 747123 1384873NM BS 2200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND INTERNAL BODY STA 2200 RBL 33 TO RBL 75 FLOORBEAM BADLY CORRODED. REWORKED CORROSION ACC SRM 51-10-01 AND REPLACED UPPER CHORD ACC SRM 53-10-07. 2L74 4F A20WE 19950922000151995092200015NM 1995 9 22 UPS404426 119950915A5320 REVEAL BOEING747 747123 1384873NM BS 2240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER REVEAL DOOR 5 RT AT STA 2240. REPAIRED UPPER REVEAL DOOR ACC UPS EO 747-53-0730. 2L74 4F A20WE 19950922000161995092200016WP 1995 9 22 UPS804412 119950915A335019022 EEL BATTERY DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01744UP 45944 WHILE ON GROUND MAINTENANCE FOUND EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK ASSY. SUSPECT BATTERIES DEAD, REASON UNKNOWN. OPS GOOD AFTER REMOVED AND REPLACED. 2L74 4F RT4A25 19950922000171995092200017WP 1995 9 22 UPS804413 119950915A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 80 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT STA 80 LBL 59 CHORD ANGLE HAS HEAVY CORROSION AT O/B END. CUT OUT DAMAGE, FABRICATED T-CHORD, REPAIR ANGLE AND INSTALLED PER UPS EO DC8 5310-7325A. 2L74 4F RT4A25 19950922000181995092200018WP 1995 9 22 UPS804414 119950915A532037584952 FITTING DOUG DC8 DC873F 302199FWP FS 1240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 1240 LONG 35R AFT INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-10 AND 51-1-20D. 2L74 4F RT4A25 19950922000191995092200019WP 1995 9 22 UPS804415 119950915A532036471171N FITTING DOUG DC8 DC873F 302199FWP BS 960 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FRAME FITTING B/S 960 IN RT WHEEL WELL ABOVE LONG 24R IS CORRODED AND CRACKED. REMOVED AND REPLACED FITTING AT B/S 960 IN RT WHEEL WELL PER SRM 53-2-0 FIG 8. 2L74 4F RT4A25 19950922000201995092200020WP 1995 9 22 UPS804416 119950915A53205779912 SPLICE DOUG DC8 DC873F 302199FWP FS 200-220 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND SPLICE IS CRACKED ON STRINGER 31L BETWEEN FRAME 200 AND 220. REMOVED SPLICE AND INSTALLED NEW SPLICE IAW SRM 53-2-2 AND 51-1-10. 2L74 4F RT4A25 19950922000211995092200021WP 1995 9 22 UPS804417 119950915A5330 SKIN DOUG DC8 DC873F 302199FWP FS 140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 140 LONG 31R AFTER CORROSION REMOVAL, SKIN WAS FOUND TO BE BEYOND ALLOWABLE LIMITS PER SRM 53-2-0 ON NR 289954. CUT OUT DAMAGED AREA PER SRM 53-2-1, FABRICATED AND INSTALLED PARTS ACCORDING WITH SRM 53-2-1. 2L74 4F RT4A25 19950922000221995092200022WP 1995 9 22 UPS804418 119950915A5330 PANEL DOUG DC8 DC873F 302199FWP FS 880-900 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MAIN CABIN CENTER SECTION PRESSURE PANEL HAS EXFOLIATION CORROSION AT FS 880 TO 900. REMOVED DAMAGED SECTION IAW SRM 53-0-0. RADIUSED CORNER, INSTALLED REPAIR SPLICE IAW UPS EO DC8 5310-7338A. 2L74 4F RT4A25 19950922000231995092200023WP 1995 9 22 UPS804419 119950915A5315 FLOORBEAM DOUG DC8 DC873F 302199FWP BS 850 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FS 850 LBL 50 FLOORBEAM HAD CORROSION IN FWD LWR CORNER, AFTER FASTENERS CORROSION AND DAMAGED CHORD WERE REMOVED. WEB WAS FOUND IN LIMITS AND PROTECTIVE TREATED CHORD WAS SUBMITTED TO ENG. REMOVED DAMAGED AREA, FABBED AND INSTALLED REPAIR PARTS PER UPS EO DC8 5310-7340A. 2L74 4F RT4A25 19950922000241995092200024WP 1995 9 22 UPS804420 119950915A5330 PANEL DOUG DC8 DC873F 302199FWP BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01806UP 46006 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MAIN CABIN CENTER SECTION PRESSURE PANEL HAS EXFOLIATION CORROSION AT FS 960 RBL 69. REMOVED DAMAGED SECTION OF PAN IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR IAW UPS EO DC8 5310-7339A. 2L74 4F RT4A25 19950922000251995092200025NM 1995 9 22 DLM90953313 119950806A3000 STRAKE DE-ICE 59650831 DOUG MD90 MD9030 3023690NM LT FWD FUS FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11901DA 53381 EWR - FLT 0282 - AFT ANTI-ICE FAULT MSG IN-FLIGHT WHEN USING ANTI-ICE. APPROACHING GATE 46B NOTICED A LARGE AMOUNT OF WHITE SMOKE ON LEFT SIDE OF AIRCRAFT. LEFT STRAKE OVERHEATED CAUSING PAINT TO CHAR AND BLISTER OFF. LEFT STRAKE CIRCUIT BREAKERS TRIPPED. FOUND LEFT STRAKE BURNED, REPLACED LEFT STRAKE, CONTROLLER AND THREE CIRCUIT BREAKERS. TESTS OK PER 30-13-00. (X) 2L72 4F RTA6WE 19950922000261995092200026NE 1995 9 22 DLL16953199 219950725A7320 FUEL FLOW REG FFR104MK1 LKHEED1011 10113853 5265020WP RROYCERB211 RB211* 54555NE NR 1 ENGINE FAILED A DALAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO11759DA B2053 193Y1176 014708 DURING CRUISE FL 370, NR 1 ENGINE DID NOT RESPOND TO THROTTLE THEN FLAMED OUT, RESTARTED ON SECOND ATTEMPT, THEN FLAMED OUT AGAIN ON SHORT FINAL AT ORY. PER FIM 71-80-00, REPLACED NR 1 FUEL FLOW REGULATOR, OPERATION NORMAL. 2L73 4F4 F A23WE A12EU 19950922000271995092200027NM 1995 9 22 DL733953126 119950712A5414 SKIN BOEING737 737347 1384647NM GE CFM56 CFM56* 13802NE NR 2 PYLON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112310 23596 720387 AT HMV, INSP FOUND THE O/B SIDE OF NR 2 PYLON WORN AT WING L/E AREA. ACCOMPLISHED REPAIRS PER SRM 54-50-01 PG 219. 2L72 4F4 FRTA16WE E2GL 19950922000281995092200028NE 1995 9 22 95UAL900029 219950630A7510 ANTI ICE VLV BOEING777 777222 1385219NM PWA PW4077PW4077 NE RT ENGINE INOP A UALAK NONE J WARNING INDICATION ININSP/MAINT 1 WP29777UA 26916 RIGHT ENGINE ANTI-ICE VALVE INOP. 2L72 4F4 FRTT0001SE E46NE 19950922000291995092200029NM 1995 9 22 95UAL900044 119950717A32307341736002 TILT ACTUATOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE RT MLG FAILED A UALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP29769UA 26921 AFTER TAKEOFF RIGHT MLG DOOR WOULD NOT CLOSE, RETURNED TO FIELD. *S/D* FOUND RT MLG TRUCK TILT ACTUATOR BYPASSING. REPLACED SAME, SWUNG GEAR OPERATES NORMAL. 2L72 4F4 FRTT0001SE E46NE 19950922000301995092200030NM 1995 9 22 95UAL777001 119950602A3230 RETRACT MECH BOEING777 777222 1385219NM PWA PW4077PW4077 NE LANDING GEAR MALFUNCTIONED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP29767UA 26918 ON TAKEOFF GEAR WOULD NOT RETRACT, WOULD RAISE WITH OVER RIDE SWITCH. 2L72 4F4 FRTT0001SE E46NE 19950922000701995092200070 1995 9 22 9514289970 419950912A3414B020081104 AIRSPEED IND DOUG DC9 DC931 3022065WP LT COCKPIT MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL019334 399322600 47247 CAPTAIN'S AIRSPEED INDICATOR WAS FROZEN AT 150 KNOTS ON TAKEOFF, THEN DROPPED TO 60 KNOTS. FLIGHT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S AIRSPEED INDICATOR AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950922000711995092200071NM 1995 9 22 9514296623 119950916A2420 RELAY BOEING747 747251B 1384892NM E/E BAY MALFUNCTIONED A NWAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01623US 21705 THIRTY MINUTES INTO FLIGHT ESSENTIAL BUS POWER LIGHT ILLUMINATED. THE PROBLEM CONTINUED ON AND OFF FOR SEVERAL MINUTES AND GOT WORSE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 55,000 LBS OF FUEL AND RETURNED TO LAX. MAINTENANCE REPLACED R79 RELAY, RAN ALL FOUR ENGINES IN IDLE POWER AND WITH POWER FOR ABOUT 15 MINUTES, COULD NOT DUPLICATE PROBLEM. 2L74 4F A20WE 19950922000721995092200072NM 1995 9 22 9514302203 119950906A3150 AURAL WARNING BOEING727 727251 138408HNM COCKPIT SOUNDED A NWAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL01203US 22543 DURING INITIAL POWER-UP FOR TAKEOFF, TAKEOFF AURAL WARNING HORN SOUNDED, ABORTED DEPARTURE. CHECKED FLIGHT CONTROL SETTINGS AND PERFORMED TAKEOFF WARNING CHECK. OPERATIONAL CHECK NORMAL AND FLIGHT DEPARTED WITHOUT FURTHER INCIDENT. 2L73 4F A3WE 19950922000731995092200073NM 1995 9 22 9514312204 119950914A2740 STAB TRIM BOEING727 727251 138408HNM COCKPIT OUT OF POSITION A NWAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL01204US 22544 WHEN POWER WAS ADVANCED FOR TAKEOFF, CONFIGURATION AURAL WARNING HORN SOUNDED, ABORTED DEPARTURE. RESET STABILIZER TO 3.1 UNITS AND SYSTEM CHECKED NORMAL. 2L73 4F A3WE 19950922000741995092200074NM 1995 9 22 9514326638 119950914A3244 TIRE BOEING747 747251B 1384892NM RT MLG FAILED A NWAAO OTHER O OTHER LDLANDING 1 GL01638US 23549 DURING LANDING, THE RIGHT BODY GEAR NR 12 TIRE BLEW. THE CREW WAS ABLE TO TAXI THE AIRCRAFT TO THE GATE AREA. FOUND DAMAGE TO THE RIGHT BODY GEAR STRUT DOOR AND STRUCTURE AREA OF THE BODY GEAR. MAINTENANCE REPLACED NR 11 AND NR 12 MAIN WHEEL ASSEMBLIES AND ANTI-SKID CONTROL VALVE. REPAIRED DAMAGED STRUCTURE, PERFORMED FUNCTIONAL CHECK AND CHECK WAS NORMAL. 2L74 4F A20WE 19950922000751995092200075NM 1995 9 22 95FDEA01338 119950915A5313655623620 STRINGER BOEING727 727232 1384082NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON STR 27R BS 740 ACCESS IS REQUIRED, FWD BAY STR 27R BS 680 TO 740. REMOVED AND REPLACED WITH NEW STR, CORROSION WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950922000761995092200076NM 1995 9 22 95FDEA01339 119950915A5314655642210 KEEL BEAM BOEING727 727232 1384082NM BS 920 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON KEEL BEAM AROUND BUCKTAILS AT CRACKED PAINT, BS 920C TO 720E IN BILGE ACCESS IS REQUIRED, RT KEEL BEAM. REMOVED KEEL BEAM BS 720 TO 740, STR 28R AND REPLACED WITH NEW KEEL BEAM. 2L73 4F A3WE 19950922000771995092200077NM 1995 9 22 95FDEA01340 119950915A55102024T3 CHORD BOEING727 727232 1384082NM HORIZ STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 RT LOWER T/E CHORD, HORIZONTAL STAB, 3 RUBSTRIP FASTENERS HAVE PULLED THROUGH BETWEEN ELEVATOR STATIONS. REPAIRED LOWER T/E CHORD IAW FEDEX EA 7-5510-25695. 2L73 4F A3WE 19950922000781995092200078NM 1995 9 22 95FDEA01341 119950915A5347BAC1520792 SEAT TRACK BOEING727 727232 1384082NM BS 690-740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND CORROSION, MECHANICAL DAMAGES IN SEAT TRACK AT BS 690 TO 740 WL 208.5 LBL 25. REMOVED CORRODED SEAT TRACK FROM BS 690 TO 740 WL 208.5 LBL 25. INSTALLED FABRICATED SEAT TRACK FROM BS 690 TO 740 WL 208.5 LBL 25. 2L73 4F A3WE 19950922000791995092200079NM 1995 9 22 95FDEA01342 119950915A5347BAC15201430 SEAT TRACK BOEING727 727232 1384082NM BS 381-406 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 FOUND MECHANICAL DAMAGE ON SEAT TRACK AT BS 381 WL 208.5 RBL 63. ACCOMPLISHED SEAT TRACK REPAIR AT BS 381 TO 406 WL 208.5 RBL 63, PER SRM 53-10-5. REMOVED DAMAGED WEBS AND MOPSILL BS 360 TO 440 WL 208 RBL 64 TO 70. FAB NEW WEBS AND INSTALLED NEW MOPSILL PER FEDEX DRAWING 65-56153. 2L73 4F A3WE 19950922000801995092200080NM 1995 9 22 95FDEA01343 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION, FWD BAY FOUND WHILE WORKING FUSELAGE 159 NR 460 SHEAR TIES FROM FRAME AT BS 720F WL 149 AND 150, BETWEEN STR 27 TO 28L ON 720 FRAME. FOUND CORROSION TO BE OUT OF LIMITS AND REPAIRED SHEAR TIE AT BS 720F STR 27 TO 28L IAW SRM 53-10-4. 2L73 4F A3WE 19950922000811995092200081NM 1995 9 22 95FDEA01344 119950915A531465564229 KEEL BEAM BOEING727 727232 1384082NM BS 720-740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION 71C209-02, ON KEEL BEAM BS 720 TO 740 STR 28L. REMOVED KEEL BEAM AT STR 28L BS 720 TO 740 AND REPLACED WITH KEEL BEAM. 2L73 4F A3WE 19950922000821995092200082NM 1995 9 22 95FDEA01345 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720C STR 27 TO 28R WL 148 ON THE SHEAR TIE. CORROSION FOUND TO BE OUT LIMITS. REMOVED AND REPAIRED DAMAGED SHEAR TIE PER SRM 53-10-4. 2L73 4F A3WE 19950922000831995092200083NM 1995 9 22 95FDEA01346 119950915A53207057T6080 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720R STR 26 TO 27R WL 148 ON THE SHEAR TIE. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4 FIG 15. 2L73 4F A3WE 19950922000841995092200084NM 1995 9 22 95FDEA01347 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 700 STR 28 LT AND RT WL 148 ON THE SHEAR TIE. REPLACED SHEAR TIE AT BS 700 STR 28 LT AND RT WL 148 PER FEDEX SRM 53-10-4. THE CORROSION REMOVED WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950922000851995092200085NM 1995 9 22 95FDEA01348 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY, BS 720B STR 28 LT AND RT WL 148 ON SHEAR TIE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, BS 720B STR 28 LT AND RT WL 148 PER FEDEX 53-10-3. FABRICATED SHEAR TIE AND INSTALLED PER FEDEX 53-10-4 SRM. 2L73 4F A3WE 19950922000861995092200086NM 1995 9 22 95FDEA01349 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720B STR 27 AND 28R WL 148 ON THE SHEAR TIE. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED SHEAR TIE AT BS 720B STR 27 TO 28R WL 148 IAW SRM 53-10-4. 2L73 4F A3WE 19950922000871995092200087NM 1995 9 22 95FDEA01350 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720C STR 28 LT AND RT WL 148 ON THE SHEAR TIE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED SHEAR TIE AT BS 720C STR 28 LT AND RT WL 148, FABRICATED REPAIR PART AND INSTALLED PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950922000881995092200088NM 1995 9 22 95FDEA01351 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720B STR 27 TO 28L WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE, BS 720B STR 27 TO 28L AND REPAIRED PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950922000891995092200089NM 1995 9 22 95FDEA01352 119950915A53207075T6 INTERCOSTAL BOEING727 727232 1384082NM BS 700-720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 700 TO 720 STR 28L WL 148 ON THE INTERCOSTAL WEB. INTERCOSTAL WEB CORRODED BEYOND LIMITS IAW FEDEX SRM 53-10-1. REMOVED AND REPLACED INTERCOSTAL, BS 700 TO 720 STR 28L WL 148. 2L73 4F A3WE 19950922000901995092200090NM 1995 9 22 95FDEA01353 119950915A53207075T6071 SHEAR TIE BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION IN FWD BAY, BS 720C STR 27 TO 28L WL 148 ON THE SHEAR TIE. REMOVED CORRODED SHEAR TIE BS 720C STR 27 TO 28L WL 148 AND REPAIRED PER FEDEX SRM 53-10-4. SHEAR TIE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950922000911995092200091NM 1995 9 22 95FDEA01354 119950915A53207075T6040 INTERCOSTAL BOEING727 727232 1384082NM BS 680-700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FOUND WHILE WORKING NR 0460 ON INTERCOSTAL BS 680 TO 700 RBL 13.5 WL 145. REMOVED INTERCOSTAL BETWEEN BS 680 TO 700 RBL 13.5 WL 145, WORK DONE PER FEDEX SRM 51-30-2. DAMAGE WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950922000921995092200092NM 1995 9 22 95FDEA01355 119950915A5313BAC1498137 STRINGER BOEING727 727232 1384082NM BS 680-723 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FOUND WHILE WORKING NR 0460 ON STR 28R BS 680 TO 723 WL 145. REMOVED CORROSION ON STR 28R BS 680 TO 723 WL 145, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPLACED STR PER FEDEX SRM 51-10-1. 2L73 4F A3WE 19950922000931995092200093NM 1995 9 22 95FDEA01356 119950915A53302024T3 SKIN BOEING727 72725 1384006NM BS 848.95 LIGHTNING STRIKEA FDEAK NONE C F.O.D. ININSP/MAINT 1 SO25508FE 18279 LIGHTNING STRIKE BS 848.95 LBL 1, CROW DOUBLE STRIKE. DAMAGED WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950922000941995092200094NM 1995 9 22 95FDEA01357 119950915A53302024T3 SKIN BOEING727 72725 1384006NM BS 860 LIGHTNING STRIKEA FDEAK NONE C F.O.D. ININSP/MAINT 1 SO25508FE 18279 LIGHTNING STRIKE BS 860 STR 1L. DAMAGE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950922000951995092200095NM 1995 9 22 95FDEA01358 119950915A5753 SKIN BOEING727 72725 1384006NM LT TE MIDFLAP DISBOND A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 LT WING I/B MIDFLAP T/E LWR SURFACE, 6 FEET FROM I/B END HAS DISBOND. REPLACED DELAMINATION 6 FEET FROM I/B AND ON THE LT WING I/B MIDFLAP T/E LOWER SURFACE IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19950922000961995092200096NM 1995 9 22 95FDEA01359 119950915A5330 SKIN BOEING727 72725 1384006NM BS 847 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION ON INTERIOR SKIN, BS 847 WL 214 BETWEEN STR 16 TO 17R. REMOVED STR SPLICE FOR ACCESS STR 16R BS 825 TO 850, BLENDED CORROSION ON INTERIOR SKIN BS 847 WL 214 RT IN 1 INCH BY 1 INCH AREA. ORIG THICKNESS .200, REMOVED .018, REMOVAL IS WITHIN LIMITS IAW FEDEX SRM 53-10-1. REINSTALLED STR SPLICE, ALODINED AND PRIMED BARE METAL AREAS. ALL WORK PER FEDEX SRM 51-10-7, 53-30-1, 51-30-2. 2L73 4F A3WE 19950922000971995092200097NM 1995 9 22 95FDEA01360 119950915A5347 SEAT TRACK BOEING727 72725 1384006NM BS 380-420 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION (72C235-02), ON SEAT TRACK BS 380 TO 420 LBL 24 WL 208. REMOVED CORROSION ON SEAT TRACK, OUT OF LIMITS IAW FEDEX 53-10-1. REMOVED AND REPLACED DAMAGED SEAT TRACK FROM BS 380 TO 420 LBL 24 WL 208 IAW PER FEDEX SRM 53-10-5. 2L73 4F A3WE 19950922000981995092200098NM 1995 9 22 95FDEA01361 119950915A5315 FLOORBEAM BOEING727 72725 1384006NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION (72C235-02), ON BEAM BS 480 LBL 12 TO 36 WL 208. REPAIRED UPPER CHORD OF FLOORBEAM BS 480 RBL 15 LBL 36 PER FEDEX SRM 53-10-8, ALODINED, PRIMERED AND PAINTED. FOUND CORROSION OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19950922000991995092200099NM 1995 9 22 95FDEA01362 119950915A5511 RIB BOEING727 72725 1384006NM RT HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 RT HORIZONTAL STAB NR 5 HINGE SUPPORT FITTING CRACKED AT LOWER TRAILING EDGE BEAM ATTACH POINT. REMOVED WIPER PLATES TO GAIN ACCESS TO RT HORIZONTAL STAB HINGE SUPPORT RIB. REPAIRED RIB IAW FEDEX SRM 55-10-4 AND REINSTALLED WIPER PLATES IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950922001001995092200100EA 1995 9 22 COMA950551 119950916A2750D3899926WC98SN CONNECTOR CNDAIRCL600 CL6002B19 EA RT TE FLAP DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01915CA 7013 FLAPS FAILED, WHEN SELECTED TO 20 DEGREES. REPAIRED DEFECTIVE WIRING CONNECTOR AT RT BPSU. 2L72 4F RTA21EA 19950922001011995092200101SO 1995 9 22 COMA9511961 119950916A2150 PACK EMB 120 EMB120RT SO RIGHT MALFUNCTIONED A COMAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01156CA 120156 RT DUCT LEAK WARNING ACTIVATED WHILE RUNNING A/C PACKS ON APU BLEED AIR AND NOTED SOME SMOKE IN CABIN. PLACED RT A/C PACK ON DEFERRED MAINTENANCE LIST. ACFT CONTINUED SERVICE. 2L72 4T RTA31SO 19950922001021995092200102SO 1995 9 22 COMA9511962 119950911A532012020235001 BRACKET EMB 120 EMB120RT SO CARGO DOOR CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01159A 14620 120159 THE CARGO DOOR LIFTING MECHANISM TORSION BAR FORWARD SUPPORT ATTACH BRACKET WAS FOUND CRACKED. THE BRACKET WAS REPLACED WITH SUBSTITUTE PART OF THICKER MATERIAL (P/N 120-20235-005), PER AERODESIGN REPORT NR 1397-1, DATED 2-15-95. 2L72 4T RTA31SO 19950922001031995092200103SO 1995 9 22 COMA9511963 119950914A612078249024 PCU LINKAGE EMB 120 EMB120RT SO LT ENGINE WORN A COMAK NONE O OTHER UKUNKNOWN 1 SO01268CA8284 719 120262 LEFT ENGINE DID NOT SHUTDOWN WHEN CONDITION LEVER SELECTED TO FUEL OFF. FOUND THE PROPELLER PITCH CONTROL LINKAGE TO BE WORN AND REPLACED THE PCU. 2L72 4T RTA31SO 19950922001041995092200104SO 1995 9 22 COMA9511964 119950916A213122201T011400 CONTROLLER EMB 120 EMB120RT SO CABIN DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01244CA6940 461 120217 AFTER TAKEOFF, CABIN PRESSURE WAS RISING OUT OF CONTROL, SWITCHED TO MANUAL CONTROL WITH SAME RESULTS. AIRCRAFT RETURNED TO BHM. REPLACED THE ELECTRONIC PRESSURE CONTROLLER. 2L72 4T RTA31SO 19950922001051995092200105SO 1995 9 22 COMA9511965 119950915A612078249024 PCU EMB 120 EMB120RT SO HAMSTD14RF 14RF9 NE RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01130G 75192 120130 901102 RT PROPELLER FEATHERED DURING TAKEOFF. FDR DATA INDICATED TORQUE REACHED 132 PERCENT. REPLACED PROPELLER DUE TO OVER TORQUE AND REPLACED PROPELLER PITCH CONTROL FOR UNCOMMANDED FEATHERING. 2L72 4T RTA31SO 6 CP11NE 19950922001061995092200106EU 1995 9 22 COMA9531154 119950916A5610 WINDSHIELD SAAB SF340 SF340A 7850100EU RIGHT BIRD STRIKE A COMAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO01358CA 340A047 BIRD STRIKE ON RT WINDSHIELD AREA. PERFORMED BIRD STRIKE INSPECTION IAW INSPECTION PROGRAM, NO DEFECTS FOUND AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19950922001071995092200107NE 1995 9 22 COMA9531155 319950918A6114660714200 PROPELLER HUB SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE BOLT HOLE CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01341CA6334 1496 340A021 DRG172884 DURING ULTRASONIC INSP OF HUB REAR FACE, A FLAW WAS INDICATED AT THE BOLT HOLE ADJACENT TO BLADE PORT NR 3. PROPELLER WAS DISSEMBLED, HUB (S/N CW1044) AND REMOVED FROM SERVICE. 2L72 4T RTA52EU 6 CP61GL 19950922001081995092200108NE 1995 9 22 COMA9531156 219950917A72605078T36P01 SEAL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE LEAKING A COMAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01342CA 340A023 SMOKE WAS OBSERVED COMING FROM LEFT ENGINE STARTER/GENERATOR COOLING VENT. REPLACED THE STARTER/GENERATOR DRIVE OIL SEAL. 2L72 4T4 TRTA52EU E8NE6 19950922001091995092200109EU 1995 9 22 COMA9531157 119950913A76005308211 QUADRANT LOCK SAAB SF340 SF340A 7850100EU COCKPIT MALFUNCTIONED A COMAK NONE O OTHER UKUNKNOWN 1 SO01357CA172431629 340A044 CONDITION LEVERS FRICTION LOCK DOES NOT HOLD SUFFICIENTLY. REPLACED THE CONTROL QUADRANT. 2L72 4T RTA52EU 19950922001101995092200110EU 1995 9 22 COMA9531158 119950913A7931M8372395R08036 CONNECTOR SAAB SF340 SF340A 7850100EU RT PGB DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01158CA 340A158 RT PROPELLER GEAR BOX OIL PRESSURE INDICATOR WAS FLUCTUATING BETWEEN 30 AND 200 PSI. REPLACED THE PGB OIL PRESSURE TRANSDUCER WIRING CONNECTOR. 2L72 4T RTA52EU 19950922001111995092200111 1995 9 22 COMA9560548 419950913A34406222855011 RADIO ALTIMETER CNDAIRCL600 CL6002B19 EA NR 1 DEFECTIVE A COMAK NONE O OTHER LDLANDING 1 SO01934CA11200 7042 SPOILERS DEPLOY NORMALLY DURING LANDING, BUT THEN STOW AND REDEPLOY AGAIN. REPLACED THE NR 1 RADIO ALTIMETER. 2L72 4F RTA21EA 19950922001121995092200112EA 1995 9 22 COMA9560549 119950914A2913PV304448 HYD PUMP CNDAIRCL600 CL6002B19 EA RT ENGINE LEAKING A COMAK NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 SO01932CA3573 7038 RT ENGINE DRIVEN HYDRAULIC PUMP IS LEAKING. REPLACED RT HYDRAULIC PUMP. 2L72 4F RTA21EA 19950922001131995092200113 1995 9 22 COMA9560550 419950914A3418 STALL COMPUTER CNDAIRCL600 CL6002B19 EA E/E COMPT MALFUNCTIONED A COMAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SO01914CA 7012 STALL FAIL CAUTION MESSAGE AFTER TAKEOFF AND REMAINED ON AT ALL AIR SPEEDS. RESET CHANNEL NR 1 AND NR 2 OF STALL PROTECTION COMPUTER AND SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950922001141995092200114NM 1995 9 22 MWEA95304 119950917A335060030431 EEL POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31601ME 49762 DURING INSPECTION, FOUND FWD SECTION OF EMERGENCY CEILING LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED FWD BATTERY POWER SUPPLY. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19950922001151995092200115NM 1995 9 22 UPS204428 119950913A3232 ACTUATOR BOEING727 72725C 138400HNM RT MLG DOOR MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION CRCRUISE 1 SO01937UP 19302 PILOT REPORTED, THAT RIGHT MAIN GEAR DOOR LIGHT CAME ON WHEN GEAR HANDLE WAS PLACED IN OFF. LANDING GEAR RECYCLED WITH NO EFFECT. MAINTENANCE REPLACED THE RIGHT MAIN DOOR ACTUATOR. 2L73 4F A3WE 19950922001161995092200116NM 1995 9 22 UPS204430 119950915A3350 EEL CB BOEING727 72722C 138400FNM FLIGHT DECK OPEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE ON THE GROUND, CREW FOUND EMERGENCY EXIT LIGHT IN COCKPIT IS ON IN ARMED POSITION. FOUND EMERGENCY EXIT LIGHT BATTERY CHARGER CB OPEN. RESET AND NO FURTHER PROBLEMS NOTED. OPERATIONAL TEST GOOD PER MM 33-50-01. 2L73 4F A3WE 19950922001171995092200117NM 1995 9 22 UPS204438 119950918A5260 WEB BOEING727 727108C 1384039NM BS 1217 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK EMANATING FROM THE LIGHTENING HOLE OF THE LEFT HAND AIRSTAIR WEB AT STATION 1217 AND WL 184. MAINTENANCE REPAIRED THE DAMAGE PER SRM 51-40-2. 2L73 4F A3WE 19950922001181995092200118NM 1995 9 22 UPS204439 119950918A5320 CLIP BOEING727 727108C 1384039NM BS 1166 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGER CLIP AT STATION 1166 AND STRINGER 22R. MAINTENANCE REMOVED THE STRINGER CLIP, FABRICATED NEW STRINGER AND INSTALLED PER SRM 51-20-1 AND 51-30-2. 2L73 4F A3WE 19950922001191995092200119NM 1995 9 22 UPS204440 119950918A5320 SILL BOEING727 727108C 1384039NM BS 304 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE MOPSILL AT STATION 304 TO 344, RBL 61 AND WL 208. MAINTENANCE REMOVED THE CORROSION, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-1, 53-10-2 AND 51-30-2. 2L73 4F A3WE 19950922001201995092200120NM 1995 9 22 UPS204441 119950918A5753 SKIN BOEING727 727108C 1384039NM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION IN THE RIGHT WING INBOARD FOREFLAP ALONG THE LEADING EDGE INBOARD END LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER MM 51-20-151, 51-40-6. 2L73 4F A3WE 19950922001211995092200121NM 1995 9 22 UPS204442 119950918A5753 TE SKIN BOEING727 727108C 1384039NM RT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP UPPER AND LOWER TRAILING EDGE SURFACES, AT NR 1 AFT FLAP CARRIAGES. MAINTENANCE REPLACED THE TRAILING EDGE WEB. 2L73 4F A3WE 19950922001221995092200122NM 1995 9 22 UPS204443 119950918A5753 TE WEDGE BOEING727 727108C 1384039NM RT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE RIGHT WING INBOARD MIDFLAP TRAILING EDGE WEDGE, AT THE UPPER SURFACE NR 3 AFT FLAP CARRIAGE AND LOWER SURFACE AT THE NR 4. MAINTENANCE REPLACED THE TRAILING EDGE WEDGE. 2L73 4F A3WE 19950922001231995092200123NM 1995 9 22 UPS204444 119950918A5753 DOUBLER BOEING727 727108C 1384039NM RT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AT THE SEAM DOUBLER ON THE RIGHT WING INBOARD FOREFLAP LOWER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREAS, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-51-11, 51-40-6. 2L73 4F A3WE 19950922001241995092200124NM 1995 9 22 UPS204445 119950918A5753 SKIN BOEING727 727108C 1384039NM RT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION AND MULTIPLE DENTS ALONG THE LOWER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIRS PER SRM 51-40-6. 2L73 4F A3WE 19950922001251995092200125NM 1995 9 22 UPS204446 119950918A5753 SKIN BOEING727 727108C 1384039NM RT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE RIGHT WING INBOARD AFT FLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950922001261995092200126NM 1995 9 22 UPS204447 119950918A5753 TE WEDGE BOEING727 727108C 1384039NM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE INBOARD END UPPER SURFACE OF THE TRAILING EDGE WEDGE, ON THE LEFT WING INBOARD MIDFLAP. MAINTENANCE REMOVED THE DAMAGED AREA, APPLIED FIBERGLASS AND COMPLETED THE REPAIR PER SRM 51-40-6. 2L73 4F A3WE 19950922001271995092200127NM 1995 9 22 UPS204448 119950918A5753 SKIN BOEING727 727108C 1384039NM LT TE AFT FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD AFT FLAP UPPER SURFACE CENTER. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED FIBERGLASS REPAIR AND INSTALLED PER SRM 51-40-6. 2L73 4F A3WE 19950922001281995092200128NM 1995 9 22 UPS204449 119950918A5753 TE WEDGE BOEING727 727108C 1384039NM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON THE LEFT WING OUTBOARD MIDFLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED GLASS REPAIR AND INSTALLED IAW SRM 51-40-6. 2L73 4F A3WE 19950922001291995092200129NM 1995 9 22 UPS204450 119950918A5312 BLKHD SUPPORT BOEING727 727108C 1384039NM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AT THE HORIZONTAL ANGLE OF THE 680 BULKHEAD SUPPORT, LBL 13 RBL 17 AND WL 198. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-20-1, 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950922001301995092200130NM 1995 9 22 UPS204451 119950918A5511 SPAR CHORD BOEING727 727108C 1384039NM LT HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HAND HORIZONTAL STABILIZER LOWER AFT SPAR CHORD AT STAB STATION 170. MAINTENANCE STOP DRILLED THE CRACK, NDT VERIFIED CONTAINMENT, FABRICATED REPAIR ANGLE DOUBLER. 2L73 4F A3WE 19950922001311995092200131NE 1995 9 22 UPS404432 219950916A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 3 MALFUNCTIONED A IPXAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SO01674UP 20100 PILOT REPORTED, ON FINAL APPROACH WITH ALL ENGINES AT IDLE, NR 3 ENGINE SURGED TO 1.25 EPR, N1 80 PLUS PERCENT N1 AND HIGH FUEL FLOW. ENGINE WAS SHUTDOWN. 2L74 4F4 F A20WE E20EA 19950922001321995092200132NM 1995 9 22 UPS404437 119950918A5330 SKIN BOEING747 747123 1384873NM BS 2598 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01672UP 20324 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND A DEEP DENT IN THE FUSELAGE SKIN JUST INBOARD FWD OF AFT JACKPOINT BODY STATION 2598. MAINTENANCE CHECKED THE DENT PER SRM 53-30-01 AND FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER AT STA 2598 AROUND JACKPOINT PER SRM 53-30-03 FIGURE 1A. 2L74 4F A20WE 19950922001331995092200133WP 1995 9 22 UPS804427 119950913A2910 SLOT VALVE DOUG DC8 DC873F 302199FWP HYD SYST LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01867UP 45967 PILOT REPORTED, AFTER FLAP RETRACTION THEY LOST HYDRAULIC FLUID. PROPER CHECKLIST ACCOMPLISHED, DISCUSSED OPTIONS, COORDINATED WITH FLIGHT CONTROL AND CONTINUED TO OAKLAND. PILOT DECLARED EMERGENCY WITH BAY APPROACH AS A PRECAUTION. EXTENDED GEAR MANUALLY AND WAS ABLE TO GET APPROACH FLAPS, LANDING FLAPS AND LANDED NORMALLY. MAINTENANCE RESEALED THE SLOT CHECK VALVE, RESERVICED SYSTEM LEAK AND OPS CHECK GOOD ON A 20 MIN ENGINE RUN. CYCLED AILERONS RUDDER AND FLAPS NUMEROUS TIMES AND NO LEAKS NOTED. 2L74 4F RT4A25 19950922001341995092200134WP 1995 9 22 UPS804429 119950914A3350 EEL METER DOUG DC8 DC873F 302199FWP CABIN MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01811UP 46089 WHILE ON THE GROUND, MAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY PACK METER SHOWING ON, WHEN EMERGENCY LIGHTS WERE OFF. A/C BATTERY PACK METER NEEDS TO BE DEACTIVATED AND PLACARDED. MAINTENANCE DEACTIVED THE METER PER WDM 33-50-01, OK TO CONTINUE SERVICE. INSTALLED DEACTIVED STICKER PER 34-21-04, EFIS WDM FOR FURTHER INFO. 2L74 4F RT4A25 19950922001351995092200135WP 1995 9 22 UPS804431 119950915A3350 EEL BATTERIES DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01744UP 45944 WHILE ON THE GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE BATTERY PACK ASSEMBLY. SUSPECT BATTERIES DEAD, REASON UNKNOWN. OPS GOOD AFTER REMOVED AND REPLACED. 2L74 4F RT4A25 19950922001361995092200136WP 1995 9 22 UPS804433 119950916A3297 WIRE DOUG DC8 DC873F 302199FWP LANDING GEAR FAULTY A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01806UP 46006 PILOT REPORTED, ON RETRACTION GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED, USED CHECK LIST AND RECYCLED GEAR. WHEN GEAR RETRACTED, THE DOOR NOT LATCHED AND THE GEAR NOT LATCHED WERE ILLUMINATED. ALSO, ALT GEAR DOOR INDICATOR INDICATED RIGHT GEAR DOOR. RECYCLED GEAR ONCE AGAIN, THE DOOR AND GEAR NOT LATCHED LIGHTS EXTINGUISHED. PERFORMED UP LATCH CHECK AND THE GEAR NOT LATCHED LT AND RT DOOR WARNING ILLUMINATED. PROCEEDED AT 230 KTS DUE TO ALT GEAR DOOR LIGHT ILLUMINATED. MAINTENANCE REPAIRED FAULTY WIRING. 2L74 4F RT4A25 19950922001371995092200137WP 1995 9 22 UPS804434 119950918A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE AFT ASSEMBLY COMPARTMENT FLOORBEAM END FITTING AT STATION 1580. MAINTENANCE REPLACED THE FITTING PER SRM 51-3-0. 2L74 4F RT4A25 19950922001381995092200138WP 1995 9 22 UPS804435 119950918A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE BOLT FRAME AT STATION 1580 AND LONGERON 21L UPPER SIDE. MAINTENANCE REPAIRED THE FRAME PER SRM 53-2-0 FIGURE 2. 2L74 4F RT4A25 19950922001391995092200139WP 1995 9 22 UPS804436 119950918A5210 BRACKETS DOUG DC8 DC873F 302199FWP FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE EVACUATION SLIDE MOUNT BRACKETS. MAINTENANCE FABRICATED AND REPLACED THE BRACKETS PER SRM 51-1-4 AND 51-1-21. 2L74 4F RT4A25 19950922001401995092200140NM 1995 9 22 95FDEA00825 119950622A53207075T6 SHEAR TIE BOEING727 727225 1384077NM BS 950 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25461FE 22548 CORROSION ON SHEAR TIE AND FRAME AT BS 950 RBL 10 TO 15 WL 150. REPLACED AFTER CUT OUT, PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950922001411995092200141NM 1995 9 22 95FDEA00836 119950628A53302024T3030 SKIN BOEING727 72722 1384002NM BS 410 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 GOUGE LESS THAN .004 INCH DEEP IN SKIN AT BS 410 WL 156 LT SIDE. FOUND GOUGE TO BE OUT OF LIMITS, REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AT BS 410 WL 156 LT SIDE IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950922001421995092200142NM 1995 9 22 95FDEA00837 119950628A53202024T3 TIE BOEING727 72722 1384002NM FS 823 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 WEB TO FRAME TIE FOUND TO BE CRACKED AT STA 823 RBL 67 WL 208. REMOVED FRAME TIE AT STA 823 RBL 67 WL 208 FABRICATED NEW TIE ALODINED AND PRIMED, INSTALLED PER FEDEX SRM 51-20-1 AND SRM 51-10-2. 2L73 4F A3WE 19950922001431995092200143NM 1995 9 22 95FDEA00838 119950628A53302024T3063 SKIN BOEING727 72722 1384002NM BS 461 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 DENT APPROXIMATELY .100 INCH DEEP IN SKIN AT BS 461 WL 210 RT SIDE. CUT OUT DENT AT BS 461 WL 210 AND FABRICATED A REPAIR DOUBLER AND INSTALLED AS PER FEDEX SRM 53-30-3 FIG 1. 2L73 4F A3WE 19950922001441995092200144NM 1995 9 22 95FDEA00839 119950628A53302024T3090 SKIN BOEING727 72722 1384002NM BS 523 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 FORWARD CARGO BAY DOORWAY CUT OUT BS 523 BETWEEN STR 22 AND 23R, 2 EACH GOUGES MAXIMUM DEPTH OF .030 INCH. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 53-30-3, AT FWD CARGO BAY DOORWAY CUT OUT BS 523 BETWEEN STR 22 AND 23R. 2L73 4F A3WE 19950922001451995092200145NM 1995 9 22 95FDEA00840 119950628A5313BAC1493513 STRINGER BOEING727 72722 1384002NM BS 380 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 POSSIBLE CRACKS ON STR 24L BS 380. REMOVED DAMAGED STR, FABRICATED REPAIR PARTS AND INSTALLED IAW FEDEX SRM 53-10-3. 2L73 4F A3WE 19950922001461995092200146NM 1995 9 22 95FDEA00841 119950628A5313 STRINGER BOEING727 72722 1384002NM BS 380 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 STR 23L IS CRACKED AT STA 380. REMOVED AND REPLACED STR 23L STA 360-384 IAW FEDEX SRM 53-10-3. 2L73 4F A3WE 19950922001471995092200147NM 1995 9 22 95FDEA00842 119950628A53117075T6050 FRAME BOEING727 72722 1384002NM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 CRACKED FRAME AT BS 1090 STR 27L. REMOVED AND REPLACED FRAME BS 1090 STR 24-27L AND TREATED IAW FEDEX SRM 57-40-03, FEDEX MM 51-20-31 AND 51-20-21. 2L73 4F A3WE 19950922001481995092200148NM 1995 9 22 95FDEA00843 119950628A53117075T6 FRAME BOEING727 72722 1384002NM BS 1070 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 CRACKED FRAME AT BS 1070 STR 27L. REMOVED AND REPLACED FRAME AT BS 1070 STR 24-27L AND TREATED IAW FEDEX SRM 51-40-03, FEDEX MM 51-20-31 AND 51-20-21. 2L73 4F A3WE 19950922001491995092200149NM 1995 9 22 95FDEA00844 119950628A5311 FRAME BOEING727 72722 1384002NM BS 1030 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 FOUND FIGURE EIGHT HOLE IN FRAME FLANGE AT STA 1030 STR 27R. TRIMMED OUT DAMAGED PORTION OF FRAME, FABRICATED REPAIR PART AND INSTALLED WET WITH SEAL AS PER SRM 51-40-3. 2L73 4F A3WE 19950922001501995092200150NM 1995 9 22 95FDEA00845 119950628A532065189553 FITTING BOEING727 72722 1384002NM BS 351 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 STA 351, CORROSION ON STR 26R DOG BONE FITTING. REMOVED AND REPLACED STR 26R STA 351. FITTING IAW FEDEX SRM 51-30-2. 2L73 4F A3WE 19950922001511995092200151NM 1995 9 22 95FDEA00846 119950628A53117075T6 FRAME BOEING727 72722 1384002NM BS 1130 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 AFT CARGO BAY BS 1130 STR 27L, FRAME IS CRACKED. CUT OUT DAMAGE AND REPAIR PER SRM 51-40-3. 2L73 4F A3WE 19950922001521995092200152NM 1995 9 22 95FDEA00847 119950628A531465C80006104 KEEL BEAM BOEING727 72722 1384002NM BS 953 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 RIGHT KEEL BEAM CORRODED, BS 953, RBL 6, WL 156. CUT ACCESS HOLE IN SKIN, REMOVED AND REPLACED KEEL BEAM THEN REPAIRED HOLE IN SKIN. REF: TCO EWO NR 95-2710 AND SRM 53-30-3 FIG 3. 2L73 4F A3WE 19950922001531995092200153NM 1995 9 22 95FDEA00848 119950628A571165185385 SPAR BOEING727 72722 1384002NM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 CORROSION FOUND ON UPPER REAR SPAR CHORD BS 870 AT RBL 20 AND LBL 10. REMOVED AND REPLACED UPPER REAR SPAR CHORD AT BS 870 PER EA NR 95-2684 AND DWG NR 65C21531-2. 2L73 4F A3WE 19950922001541995092200154NM 1995 9 22 95FDEA00849 119950628A532065C52828 POST BOEING727 72722 1384002NM NR 2 WINDOW CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25180FE 18867 RIGHT NR 2 WINDOW CUT OUT DOUBLER IS CRACKED IN THE UPPER AFT RADIUS. REPAIRED CRACK IN DOUBLER IAW EO 7-5330-7-3354 PART 5. 2L73 4F A3WE 19950922001551995092200155NM 1995 9 22 95FDEA00850 119950606A523065266803 FITTING BOEING727 72725C 138400HNM CARGO DOOR CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 UPPER LOBE CARGO DOOR: CARGO DOOR AFT CAM SUPPORT FITTING CRACKED BETWEEN 2ND AND 3RD RIVET IN WEB AT INBD ROW OF FASTENERS. REMOVED AND REPLACED CASTING PER ESO 11782 FEDEX EA NR 7-5230-25056. 2L73 4F A3WE 19950922001561995092200156NM 1995 9 22 95FDEA00851 119950607A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25134FE 19852 CORROSION ON TOP OF FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE, BS 360 RBL 20-22. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM. BLEND OUT AREA IS 2.0 INCHES X 1.0 INCH X .075 INCH DEEP, PER SRM 51-10-6 GUIDELINES. INSTALLED REPAIR STRAP PER ESO 11782 DATED 6-13-95. APPLIED LPS-3/DINITROL AVB TO REWORK AREA. REPAIR ACCOMPLISHED PER EA 7-5310-25029 DATED 6-13-95. 2L73 4F A3WE 19950922001571995092200157NM 1995 9 22 95FDEA00852 119950621A5320 CASTING BOEING727 72725C 138400HNM BS 620 CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 LIGHT CORROSION ON HEAVY CARGO DOOR CASTING STA 620 ON UNDERSIDE OF LEG, AFT SIDE OF 620 INCLUDING CORRODED GOUGE. HFEC'D AREA, APPROXIMATELY A 1.50 INCH CRACK, RUNS INTO RADIUS MARKED ENDS. INSTALLED DOUBLER REPAIR PER ESO 11782. INSTALLED DOUBLER PER FEDEX EA 7-5310-25041. 2L73 4F A3WE 19950922001581995092200158NM 1995 9 22 95FDEA00853 119950607A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 360 CORRODED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 FS 360 RBL 19-20. CORROSION ON FLOORBEAM AROUND FLOORBOARD ATTACH SCREW HOLE. REPAIRED PER AA ESO 11782 FEDEX EA NR 7-5310-25029. 2L73 4F A3WE 19950922001591995092200159NM 1995 9 22 95FDEA00854 119950607A5711 SPAR WEB BOEING727 72725C 138400HNM CENTER WING CORRODED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 CENTER WING BOX AFT SPAR WEB SKIN AT UPPER CHORD HAS FOUR EACH FASTENERS WITH POPPED HEADS AND ONE READY TO POP, TOTAL FIVE. WEB SKIN IS BULGED AT APPROX RBL 50. REMOVED RIVETS AND CUT OUT TOP PORTION OF WEB OUT TO REMOVE CORROSION ON UPPER SPAR. INSTALLED DOUBLER REPAIR PER ESO 11782 DATED 6-9-95. BEAD SEALED DOUBLER. REPAIR DONE FROM FEDEX EA 7-5710-25012. 2L73 4F A3WE 19950922001601995092200160NM 1995 9 22 95FDEA00855 119950620A5315 FLOORBEAM BOEING727 72725C 138400HNM FS 344 CORRODED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 FS 344 LBL 6-14 CORROSION ON TOP LEG OF FLOORBEAM. INSTALLED FLOORBEAM CAP PER 53-10-8. 2L73 4F A3WE 19950922001611995092200161NM 1995 9 22 95FDEA00856 119950607A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25134FE 19852 CORROSION ON TOP OF LEG ON FLOORBEAM (TOP LEG) STA 480 RBL 18-20. BLENDED OUT CORROSION ON TOP LEG OF FLOORBEAM, BLENDED OUT AREA 2.0 INCHES X .75 INCH WIDE, AT A DEPTH OF .045 INCH EXCEEDING SRM LIMITS. INSTALLED STRAP REPAIR PER ESO 11782 DATED 6-13-95 EA NR 7-5310-25028. 2L73 4F A3WE 19950922001621995092200162NM 1995 9 22 95FDEA00857 119950608A5320 FITTING BOEING727 72725C 138400HNM BS 870 CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 RIGHT STA 870 CRACK ABOVE STR 10 EXTENDING UNDER SPLICE PLATE - AFT SIDE OF 870 FORGING. REPAIRED BS 870 TERMINAL FITTING AS PER BOEING SB 727-53-0. 2L73 4F A3WE 19950922001631995092200163NM 1995 9 22 95FDEA00858 119950608A523065266803 FITTING BOEING727 72725C 138400HNM CARGO DOOR CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25134FE 19852 MAIN CARGO DOOR AFT CAM SUPPORT FITTING CRACKED. REPLACED FITTING WITH 65-26680-5 IN PLACE OF ORIGINAL - 3 FITTINGS OBSOLETE PER EA NR 7-5230-25056. 2L73 4F A3WE 19950922001641995092200164NM 1995 9 22 95FDEA00860 119950630A2910 HYD FLUID BOEING727 727233 138408ANM A-HYD SYST LOST A FDEAC ABORTED TAKEOFF K FLUID LOSS TOTAKEOFF 1 SO25262FE 21624 ON DEPARTURE FROM ROC, A/C LOST ALL A-SYSTEM HYD QTY. 2L73 4F RTA3WE 19950922001651995092200165NM 1995 9 22 95FDEA00861 119950630A3260 IND LIGHT BOEING727 727227 1384078NM NLG MALFUNCTIONED A FDEAO OTHER P NO WARNING INDICATION LDLANDING 1 SO25496FE 21670 DID NOT GET NOSE GEAR LIGHT DURING NORMAL EXTENSION, RECYCLED AND TESTED AND DID NOT CHECK NORMAL, WENT AROUND AND ON GROUND, THE NOSE GEAR LIGHT TESTED NORMAL, LEFT GEAR DOWN IN PATTERN AND LANDED. INSPECTED NOSE GEAR POSITION SWITCH AND FOUND WATER IN CANNON PLUG, CLEANED MOISTURE FROM CANNON PLUG - CHECKED LINKAGE FOR DEFECTS, FOUND NONE, SYS GROUND CHECK NORMAL. 2L73 4F A3WE 19950922001661995092200166NM 1995 9 22 95FDEA00862 119950630A3260656021132 GEAR MODULE BOEING727 727227 1384078NM NLG MALFUNCTIONED A FDEAO OTHER P NO WARNING INDICATION LDLANDING 1 SO25496FE 21670 NOSE WHEEL GEAR LIGHT WOULD NOT GIVE DOWN AND LOCKED INDICATION AFTER PUTTING GEAR HANDLE DOWN. THE TEST WOULD NOT TEST NORMAL. NOSE GEAR BULB WORKED NORMALLY. DOWN AND LOCKED VERIFIED BY VIEWING PORT AND RUNNING THE CHECKLIST. REMOVED AND REPLACED LANDING GEAR ELECTRICAL/ELECTRONIC MODULE. OPS TEST PER MM 32-09-121 PAGE 401 AND TESTED PER 32-09-121 PAGE 501. ALL SYSTEM CHECKS NORMAL. 2L73 4F A3WE 19950922001671995092200167NM 1995 9 22 95FDEA00863 119950630A3260 GEAR INDICATION BOEING727 727227 1384078NM NOSE GEAR MALFUNCTIONED A FDEAO OTHER P NO WARNING INDICATION LDLANDING 1 SO25496FE 21670 ON LANDING INTO OAK, DID NOT GET NOSE GEAR LIGHT, DOWN AND LOCKED. 2L73 4F A3WE 19950922001681995092200168NM 1995 9 22 95FDEA00864 119950701A57542024T3 SKIN BOEING727 72725C 138400HNM NR 1 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25127FE 19719 CORROSION (75C002-00) NR 1 K-FLAP DATA PLATE. REPAIRED CORROSION DAMAGE AT NR 1 K-FLAP DATA PLATE AND RELOCATED DATA PLATE IAW FEDEX SRM 57-50-3 AND SRM 27-57-010. 2L73 4F A3WE 19950922001691995092200169NM 1995 9 22 95FDEA00865 119950701A5347BAC15201430 SEAT TRACK BOEING727 72725C 138400HNM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25127FE 19719 SEAT TRACK WL 208, LBL 45, STA 560, HAS CORROSION IN WELL. REMOVED AND REPLACED SEAT TRACK. 2L73 4F A3WE 19950922001701995092200170NM 1995 9 22 DL73S953564 119950818A53156545410515 FLOORBEAM BOEING737 737232 1384475NM BS 663 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11325DL 23097 DURING HMV IN ATL, THE CABIN FLOORBEAM WAS FOUND CRACKED INTHE OP FLANGE AT STA 663, BL 0. THE UPPER CAP OF THE FLOORBEAM IS CRACKED COMPLETELY THROUGH THE HORIZONTAL FLANGE. ANOTHER CRACK EXISTED IN THE WEB JUST FWD OF THE DAMAGED CAP. THESE CRACKS WILL BE REPAIRED PER S/B 737-57-1210. 2L72 4F RTA16WE 19950922001951995092200195WP 1995 9 22 95FDEA01363 119950915A2700APH72C25 ARM DOUG DC10 DC1030F 3023504WP FLIGHT CONTROLS CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 UPON DISASSEMBLY OF CONTROLS, ARM AP NR 7202-5 WAS FOUND CRACKED AT SPLINE SHAFT MOUNT END. CRACK ORIGINATED IN CLAMP UP BOLT PLANE AND FOLLOWS GRAIN OF PART LENGTH. THIS CONDITION FOUND ON 2 OF ARMS FROM THIS A/C AND THE ARMS WERE REPLACED. 2L73 4F RTA22WE 19950922001961995092200196WP 1995 9 22 95FDEA01364 119950917A5340ANB7253501 FITTING DOUG DC10 DC1030F 3023504WP RT TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 RT I/B FLAP I/B ACTUATOR ATTACHMENT TO FUSELAGE BOLTS NOT SECURED. CHECKED BARREL NUTS FOR WEAR, FOUND ACT LOWER ATTACH FITTING CRACKED AT LOWER BOLT HOLES. 2L73 4F RTA22WE 19950922001971995092200197EU 1995 9 22 95FDEA01365 119950915A2611CG7G011 SMOKE DET AIRBUS310 A310203 EU COCKPIT MALFUNCTIONED A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25413FE 400 SIN - AVIONICS SMOKE WARNING ON FINAL, WITH ECAM WARNING. PILOT CONFIRMED NO SMOKE WITH SNIFFER FAN AND NO WARN ON OVERHEAD. REMOVED AND REPLACED COCKPIT SMOKE DET 13WA AND OPS CHECKS GOOD PER 310 TSM 26-15-00. 2L72 4F RTA35EU 19950922001981995092200198NM 1995 9 22 95FDEA01366 119950918A5321 FLOOR BOEING727 72725C 138400HNM BS 344 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UNAUTHORIZED REPAIR INSTALL ON FLOOR, BS 344 LBL 38. REMOVED AND REPLACED REPAIR PER DRAWING NR SR27-53-007, NR O857. 2L73 4F A3WE 19950922001991995092200199NM 1995 9 22 95FDEA01367 119950915A5330 SKIN BOEING727 72725C 138400HNM BS 1138 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 HOLE IN STR 9R AND CRACKED AT STA 1138, CUT OUT DAMAGED PART OF STR 9R AND FUSE SKIN THAT WAS DAMAGED ALONG WITH STR. INSTALLED FLUSH DOUBLER AND STR REPAIR PER 53-30-8. ARRIVED IN TUL IN THIS CONDITION. 2L73 4F A3WE 19950922002001995092200200NM 1995 9 22 95FDEA01368 119950915A5330 SKIN BOEING727 72725C 138400HNM BS 440 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 OUTSIDE FUSELAGE STA 440 STR 17R THERE IS A BULGE IN THE SKIN NR 00073. LFEC SHOWS CORROSION IN EXCESS OF 20 PERCENT MATERIAL LOSS. REMOVED CORROSION AND FABRICATED DOUBLER PER SRM 53-30-3. 2L73 4F A3WE 19950922002011995092200201NM 1995 9 22 95FDEA01369 119950916A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION ON MAIN CABIN FLOORBEAM STA 400 AT LBL 35. 2L73 4F A3WE 19950922002021995092200202NM 1995 9 22 95FDEA01370 119950914A5230CST65961571 CASTING BOEING727 72725C 138400HNM CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION ON MAIN CARGO DOOR CASTING, 7 PLACES LOCATED BETWEEN 6TH AND 7TH LATCHES. 2L73 4F A3WE 19950922002031995092200203NM 1995 9 22 95FDEA01371 119950918A5314 KEEL BEAM BOEING727 727233 138408ANM BS 950-1000 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORROSION IN THE AFT CARGO BAG, CORROSION ON O/B FLANGE OF STR 29R KEEL BEAM AT BS 950F TO 970 BS 976, 982, 989 AND 990 TO 1000. REMOVED AND REPLACED KEEL BEAM PER FEDEX EA 7-5310-25768 AND EWO 95-3091. 2L73 4F RTA3WE 19950922002041995092200204NM 1995 9 22 95FDEA01372 119950918A5314 KEEL BEAM BOEING727 727233 138408ANM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORROSION IN THE AFT CARGO BAG, CORROSION ON KEEL BEAM STR 29L BS 950E PLUS 5 TO 950E PLUS 13 AND AT BS 950L PLUS 12. REMOVED CORROSION AND TREATED AREA PER EA 7-5310-25771 AND EWO 95-3089. 2L73 4F RTA3WE 19950922002051995092200205NM 1995 9 22 95FDEA01373 119950918A53157075T6 FLOORBEAM BOEING727 727233 138408ANM BS 312 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORROSION ON FLOORBEAM BS 312 LBL 4, 19, 45 WL 208 AROUND NUTPLATE HOLES. REPAIRED CORRODED AREA ON FLOORBEAM BS 312 LBL 19 WL 208 AROUND NUTPLATE HOLES PER FEDEX 53-10-8 FIG 7. REMOVED CORROSION ON BS 312 FLOORBEAM LBL 4 AND 45 WL 208, FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. 2L73 4F RTA3WE 19950922002061995092200206NM 1995 9 22 95FDEA01374 119950918A5730 SKIN BOEING727 727233 138408ANM BS 826 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORROSION ON UPPER SKIN OF WING CENTER SECTION BS 826 BETWEEN STR 80 TO 70 RBL 50. BLENDED CORROSION NDI VERIFICATION OF CORROSION REMOVAL. REMOVAL OF MATERIAL WITHIN LIMITS, WORN PER EA 7-5710-25770. 2L73 4F RTA3WE 19950922002071995092200207NM 1995 9 22 95FDEA01375 119950918A5320 SHEAR TIE BOEING727 727233 138408ANM BS 970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25268FE 21673 CORRODED SHEAR TIE AT BS 970 RBL 8 WL 138. FABRICATED AND INSTALLED SHEAR TIES PER SRM 53-10-4. 2L73 4F RTA3WE 19950922002081995092200208NM 1995 9 22 95FDEA01376 119950918A5311BAC14302763 FRAME BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY, BS 720E WL 150 RBL 4, 6 AND 11, LBL 5, 7 AND 13 ON BILGE FRAME. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS PER FEDEX SRM 53-10-1, REMOVED CORRODED FRAME. 2L73 4F A3WE 19950922002091995092200209NM 1995 9 22 95FDEA01377 119950918A5320694368311 SHEAR TIE BOEING727 727232 1384082NM BS 680 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION (71C209-02), ON SHEAR TIE BS 680 STR 25 TO 26R WL 150. REMOVED CORROSION FROM SHEAR TIE BS 680 STR 25 TO 26R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 680 STR 25 TO 26R. 2L73 4F A3WE 19950922002101995092200210NM 1995 9 22 95FDEA01378 119950918A5320694368310 SHEAR TIE BOEING727 727232 1384082NM BS 680 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION (71C209-02), ON SHEAR TIE BS 680 STR 26 TO 27R WL 148. REMOVED CORROSION FROM SHEAR TIE BS 680 STR 26 TO 27R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE AT BS 680 STR 26 TO 27R. 2L73 4F A3WE 19950922002111995092200211NM 1995 9 22 95FDEA01379 119950918A53136556236620 STRINGER BOEING727 727232 1384082NM BS 680 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION ON STR 27L AT VARIOUS LOCATIONS FROM BS 680 TO 740 WL 145. REMOVED CORROSION ON STR 27L FROM BS 680 TO 740 AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED STR 27L FROM BS 680 TO 740 AND INSTALLED NEW STR 27L FROM 680 TO 740. 2L73 4F A3WE 19950922002121995092200212 1995 9 22 95FDEA01380 419950919A3441 IRU AIRBUS310 A310203 EU NR 1 FAILED A FDEAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO25404FE 233 THE NR 1 IRU FAILED, SHOWS IRS WARNING AND NR 1 F/D FAILED AT SAME TIME, REPEAT WRITE UP. SWAPPED NR 1 AND NR 3 IRS, NR 1 AND NR 3 IRS ALIGNED NORMAL. DEFER NR 3 IRS PER MEL 34-10 CAT C ITEM CONTROL 0919014, EXP 9-29-95. A/C DOWNGRADED TO CAT 2, MOCCC NOTIFIED, NEED (P/N 461600-0800-0801). 2L72 4F RTA35EU 19950922002131995092200213NM 1995 9 22 95FDEA01381 119950918A532065453135 CLIP BOEING727 72722 1384002NM BS 400 MIS MFG A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25188FE 19081 THERE IS NO RADIUS AT STR CLIP CUTOUT, BS 400 STR 5R. REMOVED AND REPLACED STR CLIP AT BS 400 STR 5R. 2L73 4F A3WE 19950922002141995092200214NM 1995 9 22 95FDEA01382 119950918A532065453136 CLIP BOEING727 72722 1384002NM BS 420 MIS MFG A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 THERE IS NO RADIUS AT STR CLIP CUTOUT, BS 420 STR 5 TO 6R. REMOVED AND REPLACED STR CLIPS AT BS 420 STR 5 TO 6R. 2L73 4F A3WE 19950922002151995092200215NM 1995 9 22 95FDEA01383 119950918A53207075T6 SHEAR TIE BOEING727 72722 1384002NM BS 312 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 FOUND CRACKED SHEAR TIE STA 312L BETWEEN STR 22 TO 23L, DOG HOUSE. REMOVED CRACKED SHEAR TIE AT BS 312 BETWEEN STR 22 TO 23L AND INSTALLED REPLACEMENT SHEAR TIE WET WITH SEALANT. 2L73 4F A3WE 19950922002161995092200216NM 1995 9 22 95FDEA01384 119950918A53117075T6 FRAME BOEING727 72722 1384002NM BS 1070 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HFEC INSP EXHIBITS CRACK EMITTING FROM HOLE ON BS 1070 FRAME ON THE O/B SIDE UPPER OF STR 27L. REPAIRED CRACK IN FRAME AT BS 1070 O/B SIDE OF STR 27L, WORK DONE IAW PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950922002171995092200217NE 1995 9 22 95FDEA01385 219950919A7200 ENGINE BOEING747 747245F 1384897NM PWA JT9 JT9D70A 52054NE NR 3 FLAMED-OUT A FDEAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO25636FE 21764 WHILE AT FL 410 ENCOUNTED SEV TURB, ENG 2 WENT TO IDLE AND NR 3 FLAMED-OUT, COULD NOT MX ALT OR A/S DESC TO FL 280. ENG NR 2 CAME BACK AFTER 2 MIN AND NR 3 WAS RESTARTED. PER CREW BRIEF THIS WAS RELATED TO TURBULANCE. INSPECTED BOTH INLET AND EXHAUST, PER DEBRIEF WITH I/B CREW BOTH RAN OK FOR LAST HOUR OF FLT. 2L74 4F4 F A20WE E3NE 19950922002181995092200218NE 1995 9 22 95FDEA01386 219950918A7230 COMPRESSOR BOEING747 747245F 1384897NM PWA JT9 JT9D70A 52054NE NR 1 ENGINE STALLED A FDEAE ENGINE SHUTDOWN RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 SO25638FE 21841 JFK-FRA - EN ROUTE AT FL 330 1408Z, NR 1 ENG EXPERIENCED A COMPRESSOR STALL. AFTER 2 MILD BUMPS, THE ENG PARA WOUND DOWN, NO OVERTEMP PRESENT. AFTER CHECKLIST PROCEDURE NORMAL FLT WAS ACCOMP. IN CRUISE AT FL 370, NR 1 ENG FLAMEOUT. AFTER PERFORMING CHECKLIST, DUE TO PREVIOUS ENG STALL AND PROXIMITY TO FRA, WE STARTED TO SHUTDOWN NR 1 ENG. THREE ENG LANDING PERFORMED, NO FURTHER INCIDENT. T/S NR 1 ENG PER MM 71-00-00, CHECKED ALL FUEL FILTERS, NO CONTAMINATION FOUND. RAN ENG, ALL PARA NORMAL. LEAK CHECK PERFORMED, NONE FOUND. RETURNED TO SERV AS PER P/P ENG. 2L74 4F4 F A20WE E3NE 19950922002191995092200219WP 1995 9 22 95UAL900134 119950918A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291824U 46623 EEL LIGHTING, FIRST CLASS RIGHT SIDE INOPERATIVE. REPLACED FEEDER CABLE, CHECKS NORMAL. 2L73 4F4 F A22WE E23EA 19950922002201995092200220NE 1995 9 22 95UAL900135 219950918A7230 BLADES BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 2 ENGINE DAMAGED A UALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29604UA 21865 707507 NR TWO ENGINE EXPERIENCED COMPRESSOR STALL IN STEADY STATE CLIMB. RETARDED THROTTLE TO IDLE AND USED POWER ON LANDING. ENGINE WAS BORESCOPED AND LOW PRESSURE COMPRESSOR BLADES WERE FOUND DAMAGED. ENGINE WAS REMOVED AND ROUTED TO THE SHOP. 2L72 4F4 FRTA1NM E3NE 19950922002211995092200221NE 1995 9 22 95UAL900136 219950918A732178017013 EEC BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 1 ENGINE MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29604UA 609 21865 707510 ABORTED TAKEOFF DUE TO NR 1 ENGINE EEC LIGHT. ELECTRONIC ENGINE CONTROL WAS REPLACED PER FAULT ISOLATION MANUAL, SYSTEM CHECKED O.K. CONTROL WAS BENCH CHECKED IN THE SHOP WITH NO FAULTS FOUND. SUSPECT LOOSE CONNECTION WHEN INSTALLED. 2L72 4F4 FRTA1NM E3NE 19950922002221995092200222NM 1995 9 22 95UAL900137 119950918A5270 SWITCH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE DOOR OUT OF ADJUST A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29904UA 25004 ABORTED TAKEOFF AT 90 KNOTS, DUE TO DOOR WARNING LIGHT. ADJUSTED DOOR SWITCH PER MM. 2L72 4F4 FRTA16WE E2GL 19950922002231995092200223NM 1995 9 22 95UAL900138 119950918A2613 OVERHEAT WARNING BOEING747 747422 1384935NM PWA 4056 PW4056 NE ENGINE ACTIVATED A UALAEAJ ENGINE SHUTDOWN UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 WP29191UA 26880 727333 SHORTLY AFTER TAKEOFF, RECEIVED EICAS MESSAGE OF NACELLE ENGINE OVERHEAT AND FIRE DETECTOR OVERHEAT. 2L74 4F4 FRTA20WE E24NE 19950922002241995092200224NE 1995 9 22 95UAL900139 219950918A7261804660 OIL PUMP SHAFT BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE FAILED A UALAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP294717U 19878 663080 THE NR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE. MAIN OIL PUMP DRIVE SHAFT FAILED. REPLACED ENGINE. 2L74 4F4 F A20WE E20EA 19950922002251995092200225NM 1995 9 22 95UAL900140 119950918A29001192113 ACTUATOR DOWTY 1U11928 BOEING747 747422 1384935NM PWA 4056 PW4056 NE LT MLG DOOR FAILED A UALAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP29171UA 102993 24322 LANDING GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. AIRCRAFT LOST NR 4 HYDRAULIC SYSTEM AND RETURNED TO FIELD. LANDING GEAR LOWERED MANUALLY. REPLACED LEFT WING GEAR INBOARD DOOR ACTUATOR. 2L74 4F4 FRTA20WE E24NE 19950922002261995092200226NM 1995 9 22 95UAL900141 119950919A3350 EEL LAMP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29369UA 24538 EMERGENCY EXIT LIGHT INOP ROW 1CD BULLNOSE. RELAMPED, OPS CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19950922002271995092200227WP 1995 9 22 95UAL900142 119950919A3350 EEL CONNECTOR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291812U 46611 LT EEL LIGHTS IN FIRST CLASS SECTION INOPERATIVE. RESEATED EEL POWER CONNECTOR BY FORWARD LT CLOSET AREA, CHECKS OK. 2L73 4F4 F A22WE E23EA 19950922002281995092200228NM 1995 9 22 95UAL900143 119950919A2710BACC2A6B00754 CONTROL CABLE BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE LT AILERON DAMAGED A AUALAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP29993UA 22383 AILERON CABLE ABSA-1 WAS FOUND WITH ONE STRAND OF CABLE INTACT. DAMAGED LOCATED ALONG THE AFT SPAR OF THE LEFT WING UNDER THE MLG WALKING BEAM OUTBOARD ATTACH POINT. THE CABLE WAS MISROUTED BETWEEN AN ADJACENT PULLEY BRACKET AND WING AFT SPAR VERTICAL STIFFENER. LOCATION OF DAMAGE AROUND WBL 160. REMOVED AND REPLACED PULLEY BRACKET WHICH WAS DAMAGED FROM SAWING ACTION. REMOVED AND REPLACED CABLE. 2L72 4F4 F A16WE E2EA 19950922002291995092200229NM 1995 9 22 DL72L953709 119950912A5315 FLOORBEAM BOEING727 727232 1384082NM BS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 400 RBL 33. REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19950922002301995092200230NM 1995 9 22 DL72L953710 119950912A5315 FLOORBEAM BOEING727 727232 1384082NM BS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 400 RBL 1. REF NR 90, REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19950922002311995092200231NM 1995 9 22 DL72L953725 119950917A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1050 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM STA 1050 AT SCREW HOLES TOP AND BOTTOM LBL 60 TO LBL 12. REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19950922002321995092200232NM 1995 9 22 DL72L953726 119950912A5315 FLOORBEAM BOEING727 727232 1384082NM BS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FOUND ON CV2 CHECK, CORROSION ON FLOORBEAM AT STA 400 RBL 54. REPAIRED AS PER M/M 53-20-4. 2L73 4F A3WE 19950922002331995092200233NM 1995 9 22 DL72S953690 119950913A57546516224101 ANGLE BOEING727 727232 1384082NM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING SHOP INSPECTION, NR 1 L/E SLAT LOWER COVE SKIN SUPPORT ANGLE WAS FOUND CRACKED. REPAIRED PER MM 57-54-0 FIG 812. 2L73 4F A3WE 19950922002341995092200234NM 1995 9 22 DL72S953693 119950914A5754651622373 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING SHOP INSPECTION, FOUND RIB NR 9 AND NR 14 CRACKED. REPAIRED PER MM 57-54-0 FIG 814, NR 2 L/E SLAT. 2L73 4F A3WE 19950922002351995092200235NM 1995 9 22 DL72S953695 119950914A5754 BRACKET BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 6 KRUEGER FLAP ACTUATOR BRACKET IS CRACKED AT I/B LOWER FWD CORNER. REPAIRED PER M/M 57-20-21. 2L73 4F A3WE 19950922002361995092200236NM 1995 9 22 DL72S953697 119950913A3350081691 EEL BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11470DA 20747 FOUND ON A/C LAYOVER CHECK, EMERGENCY FLOOR TRACK LIGHTS INOP AND OR LENS COVER MISSING AT ROWS 10, 11, 17, 19 AND 31. REPLACED SOCKET AND OR BULBS AND COVERS AS NECESSARY. 2L73 4F A3WE 19950922002371995092200237NM 1995 9 22 DL72S953706 119950914A3350 EEL BATTERY 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11494DA 21074 EMERGENCY LIGHTS INOP AFT AISLE EXIT SIGN. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19950922002381995092200238NM 1995 9 22 DL72S953711 119950915A5754651622373 RIB BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING SHOP INSPECTION, FOUND NR 2 L/E SLAT WITH RIB NR 20 CRACKED. REPAIRED PER MM 57-54-0 FIG 14. 2L73 4F A3WE 19950922002391995092200239NM 1995 9 22 DL72S953733 119950909A5754 WEB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 060294 DURING HMV, FOUND NR 6 SLAT I/B WEB AT DE-ICE TUBE CRACKED. REPAIRED ANGLE PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950922002401995092200240NM 1995 9 22 DL72W953704 119950914A5754 ANGLE BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112819W 21057 FOUND ON B2 LETTER CHECK, CRACK IN NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950922002411995092200241NM 1995 9 22 DL757953724 119950917A3350OL3071BPEGPL EEL BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11661DN 24972 EMERGENCY LIGHT AT SEAT 7AB, LAST WHITE LIGHT ON THE PATH IS INOP. RELAMPED, CHECKS NORMAL. 2L72 4F RTA2NM 19950922002421995092200242NM 1995 9 22 DL76L953696 119950913A3350 EEL BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11182DN 25987 AFT MOST FUSELAGE EMERGENCY LIGHT INOP ON LEFT SIDE. RELAMPED, OPS CHECK GOOD. 2L72 4F RTA1NM 19950922002431995092200243NM 1995 9 22 DL76L953716 119950916A3210161T111034 LANDING GEAR BOEING767 767332 1382001NM RT MLG FRACTURED A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO11172DN 24775 DURING TAXI FOR TAKOFF, RIGHT MAIN LANDING GEAR COLLAPSED AS AIRCRAFT WAS MAKING TURN TO RUNWAY. LANDING GEAR TRUNNION OUTER CYLINDER FAILED AT THE AFT TRUNNION AREA AND DIAGONALLY ACROSS THE MAIN GEAR STRUT. THE STRUT PUNCTURED THE WING UPPER SURFACE AND AIRCRAFT CAME TO REST ON THE RIGHT ENGINE. WING STRUCTURE, ENGINE AND PYLON SUSTAINED SUBSTANTIAL DAMAGE, UNDER INVESTIGATION. 2L72 4F RTA1NM 19950922002441995092200244WP 1995 9 22 DLL14953708 119950915A3230155193 PRIORITY VALVE LKHEED1011 1011385115 5265015WP LT MLG FAILED A DALAK NONE KJ FLUID LOSS WARNING INDICATION LDLANDING 1 SO11740DA 193C1244 THE C-HYDRAULIC SYSTEM FELL TO .25 FULL WHEN GEAR EXTENDED. FOUND LT MLG PHASE CONTROL VALVE, PRIORITY VALVE END CAP SHEARED. REPLACED PRIORITY VALVE, LEAK CHECK OK. 2L73 4F A23WE 19950922002451995092200245WP 1995 9 22 DLL17953707 119950907A5315 FLOORBEAM LKHEED1011 10113853 5265020WP BS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 DURING HMV, FS 901 FLOOR SUPPORT BEAM CORRODED AT LBL 49, 60, AND RBL 49, 70. REPLACED BEAM CAP PER SRM 53-21-00 PG 849 TO 852. 2L73 4F A23WE 19950922002461995092200246WP 1995 9 22 DLL17953723 119950907A5315 FLOORBEAM LKHEED1011 10113853 5265020WP BS 846 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 DURING HMV, UPPER SURFACE OF FLOORBEAM AND SUPPORT ANGLE CORRODED AT FS 846 AT RBL 40. REPAIRED PER SRM 53-21-00 PG 849 TO 852. 2L73 4F A23WE 19950922002471995092200247NM 1995 9 22 DLM88953705 119950914A5400 ANGLE DOUG MD88 MD88 3023688NM NR 1 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11909DL 49540 FOUND ON B2 LETTER CHECK, CRACK IN ATTACH ANGLE UPPER AFT END, NR 1 PYLON .75 INCH. REPAIRED PER MM 54-04A. 2L72 4F RTA6WE 19950922002481995092200248NM 1995 9 22 DLM88953718 119950916A3350 EEL WIRE DOUG MD88 MD88 3023688NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11998DL 53370 EMERGENCY LIGHT AT SEAT 25D IS INOP. REPAIRED BROKEN WIRE ON TRACK LIGHT, CHECKS GOOD. 2L72 4F RTA6WE 19950922002491995092200249NM 1995 9 22 DLM88953720 119950917A2910AE7055381 HOSE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11910DE 53419 726918 ACFT DIV TO MCO, RIGHT HYD SYS QUANTITY DECREASED RAPIDLY TOWARDS ZERO, PRESS FOLLOWED. FOLLOWED RIGHT HYD SYS FAILURE PROCEDURE. REPLACED NR 2 ENGINE HYD PRESSURE LINE, OPERATION NORMAL. 2L72 4F4 FRTA6WE E9NE 19950922002501995092200250NM 1995 9 22 DLM88953722 119950916A5240 BOLT DOUG MD88 MD88 3023688NM SERVICE DOOR SHEARED A DALAK NONE O OTHER ININSP/MAINT 1 SO11956DL 49887 AFT LEFT SERVICE DOOR INSIDE HANDLE INOP. FOUND INTERIOR HANDLE RETAINING BOLT SHEARED. INSTALLED NEW BOLT DOOR OPN NML REF IPC 52-40-11-03 ITEM 720. 2L72 4F RTA6WE 19950922002511995092200251WP 1995 9 22 MWEA95305 119950913A5320 RIB DOUG DC9 DC914 3022034WP BS 474 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING INSPECTION, THE RT FWD ADF ANTENNA ATTACH RIB STRUCTURE WAS FOUND CRACKED, APPROX 2 INCHES LENGTH AT STA 474 LONGERON 20R. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 53-01 FIG 2 SHEET 2, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922002521995092200252 1995 9 22 MWEA95306 419950915A256513621225 EVAC SLIDE DOUG DC9 DC914 3022034WP TAILCONE DEPLOYED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING INSPECTION, TAIL EVACUATION SLIDE INADVERTENTLY DEPLOYED WHILE INSTALLING. MAINTENANCE INSTALLED NEW TAIL EVACUATION SLIDE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922002531995092200253WP 1995 9 22 MWEA95307 119950917A5230 SKIN DOUG DC9 DC914 3022034WP FWD CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 80ME DURING INSPECTION, THE FWD CARGO DOOR SKIN WAS FOUND CRACKED ON FWD LOWER CORNER APPROX .75 INCH LENGTH. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 52-05 FIG 4 PG 5, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922002541995092200254NM 1995 9 22 P5CA9500771 119950917A3230 RETRACT MECH BOEING747 747123 1384873NM LANDING GEAR MALFUNCTIONED A P5CAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 WP23858FT 20109 AFTER SUCCESSFUL LANDING GEAR RETRACTION, BOTH LT AND RT WING LANDING GEAR CAME OUT OF THE WHEEL WELLS. BOTH GEAR FULLY LOCKED IN THE DOWN POSITION AND BOTH DOORS REMAINED OPEN, RETURNED TO HKG. CHECKED RIGGING AND CABLE TENSIONS OF WING GEAR SELECTOR VALVE, WING GEAR SELECTOR VALVE QUADRANT, WING GEAR DOOR OPERATED SEQUENCE VALVE ALTERNATE GEAR EXTENSION ELECTRIC MOTORS AND CABLES. ALL CHECKS FOUND SATISFACTORY WITHIN MAINTENANCE MANUAL LIMITS. ACCOMPLISHED GEAR SWING, COULD NOT DUPLICATE CONDITION AND AIRCRAFT RELEASED. 2L74 4F A20WE 19950922002551995092200255NM 1995 9 22 P5CA9500772 119950919A7800 EXHAUST STRUT BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 662457 DURING B-CHECK INSPECTION, FOUND CRACKS AT EXHAUST STRUT POSITIONS 2, 3, 4, 5, 12 AND 15. ENGINE SCHEDULED FOR 100 HOUR REPEAT INSPECTIONS PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-53-02. 2L74 4F4 F A20WE E20EA 19950922002561995092200256SO 1995 9 22 SWIA95621 119950901A3230 RETRACT MECH EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG LACK OF LUBE A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07217SW 120286 RT MAIN WOULD NOT RETRACT, CYCLED 3 TIMES. LUBRICATED RT MLG MAIN BRAKE ATTACH POINTS, SWUNG GEAR SEVERAL TIMES AND OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19950922002571995092200257SO 1995 9 22 SWIA95622 119950905A3233 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG OUT OF ADJUST A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07217SW 120286 RT MLG WOULD NOT RETRACT, CYCLED 3 TIMES. ADJUSTED RT MLG ACTUATOR IAW MM 32-32-10. 2L72 4T4 TRTA31SO E20NE 19950922002581995092200258 1995 9 22 SWIA95623 319950905A6140 NP INDICATION EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT PROP FLUCTUATES A SWIAK NONE O OTHER CLCLIMB 1 NM07221SW 120290 RT NP INDICATION FLUCTUATES INTERMITTENTLY. RAN A/C AND FOUND RT PROP FLUCTUATES .2 TO .5 PERCENT. FOUND WITHIN MM LIMITS AND OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19950922002591995092200259SO 1995 9 22 SWIA95624 119950906A32301953500001 DN LOCK ACT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07217SW 120286 AFTER TAKEOFF, RT MAIN GEAR STAYED DOWN, RETURNED FOR LANDING AT LAX. REPLACED RT GEAR SEQUENCE VALUE, LEAK AND OPS CKS GOOD. FAILED TEST FLIGHT, FOUND RT DOWN LOCK ACTUATOR SLOW TO UNLOCK GEAR. INSTALLED SERVICEABLE UNIT AND OPS CKS GOOD. CYCLED LANDING GEAR ON TEST FLIGHT, ALL SYST EMS NORMAL. 2L72 4T4 TRTA31SO E20NE 19950922002601995092200260NM 1995 9 22 UPS204453 119950915A33501000677 EEL BOEING727 72727C 138400JNM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01908UP 11914 WHILE ON GROUND MAINTENANCE, FOUND EMERGENCY EXIT LIGHT ON FORWARD ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. 2L73 4F A3WE 19950922002611995092200261NM 1995 9 22 UPS204454 119950915A3350 EEL BOEING727 72731C 1384011NM CABIN MALFUNCTION A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01922UP 19231 PILOT REPORTED, EMERGENCY EXIT LIGHTS ILLUMINATED ON TAXI OUT WITH ARMING SWITCH ARMED. LIGHT WENT OUT WHEN SWITCH PLACED IN OFF POSITION, THEN ON WHEN ARMED. RESECURED EMERGENCY EXIT LIGHT ASSY, CHECK OK. 2L73 4F A3WE 19950922002621995092200262WP 1995 9 22 UPS804452 119950914A5230 SKIN DOUG DC8 DC871F 302199DWP NR 3 CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01730UP 46030 WHILE ON GROUND, MAINTENANCE FOUND NR 3 PIT DOOR SKIN CRACKED UPPER AFT CORNER. REMOVED AND REPLACED BROKEN DOUBLER PER SRM 52-2-0. 2L74 4F RT4A25 19950922002631995092200263NM 1995 9 22 9501W8PA 119950815A7830106122628 STOW PROX SWITCH BOEING737 737301 1384611NM NR 2 TR UNIT OUT OF ADJUST A W8PAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03301AU 23229 FLT NR 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M) 2L72 4F RTA16WE 19950922002641995092200264WP 1995 9 22 95ZZZM430 119950614A5330 SKIN DOUG DC8 DC862 3021970WP BS 902-980 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LIGHT CORROSION AT EXTERIOR FUSELAGE SKIN CUSP LINE AT FS 902-980 AT L21R. REMOVED CORROSION PER SRM 51-18 FOUND TO BE BEYOND LIMITS LEVEL 2 CORROSION. FABRICATED AND INSTALLED REPAIR PARTS IAW DER DWG ARW 950051-5065. 2L74 4F 4A25 19950922002651995092200265WP 1995 9 22 95ZZZM431 119950615A551257696005 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF LEFT HORIZ STAB L/E OUTBOARD FROM XH 285.00 TO XFS 178.00. CUTOUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0969 SRM 51-3-0. 2L74 4F 4A25 19950922002661995092200266WP 1995 9 22 95ZZZM432 119950613A5720 TRAP PANEL DOUG DC8 DC862 3021970WP WS 19 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL 2 CORROSION LEFT WING UPPER SURFACE TRAPEZOID PANEL BETWEEN AFT SPAR AND XW 19.00. FABRICATED AND INSTALLED NEW PANEL AS PER ORIGINAL IAW DER DWG ARW 950051-0203. 2L74 4F 4A25 19950922002671995092200267WP 1995 9 22 95ZZZM433 119950615A5512 SKIN DOUG DC8 DC862 3021970WP RT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK, FOUND LEVEL 2 CORROSION AROUND ATTACH FASTENERS ON UPPER SURFACE OF RT HORIZONTAL STABILIZER LEADING EDGE OUTBOARD FROM XFS 178.00 TO XH 285.00. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DER DWG ARW 950051-0968. 2L74 4F 4A25 19950922002681995092200268WP 1995 9 22 95ZZZM434 119950620A531356138627 LONGERON DOUG DC8 DC862 3021970WP BS 208-270 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND L31R AND FINGER DOUBLER BETWEEN FS 208.00 AND 270.00 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED L31R AND FINGER DOUBLER BETWEEN FS 208.00 AND 270.00 IAW SRM 51-1-2 AND 51-2-0. 2L74 4F 4A25 19950922002691995092200269WP 1995 9 22 95ZZZM435 119950615A5512 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STAB TIP WITH LEVEL 2 CORROSION. REMOVED DAMAGED SKIN PANELS, FABRICATED, TREATED AND INSTALLED NEW PANELS IAW SRM 51-1-8, 51-1-21 PG 20-25 AND 55-1-0. 2L74 4F 4A25 19950922002701995092200270WP 1995 9 22 95ZZZM436 119950615A5512 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, LOWER SKIN SURFACE AT TRAILING EDGE BETWEEN XE 272.00 TO STABILIZER TIP WITH LEVEL 2 CORROSION. REPLACED PANEL IAW SRM 51-1-21 PG 20-25 AND SRM 55-1-0. 2L74 4F 4A25 19950922002711995092200271WP 1995 9 22 95ZZZM437 119950615A532045976431 FITTING DOUG DC8 DC862 3021970WP FS 235 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND FLOOR BEAM TO FUSELAGE FRAME ATTACH FITTING AT RIGHT FS 235 WITH LEVEL 2 CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F 4A25 19950922002721995092200272WP 1995 9 22 95ZZZM438 119950615A5730 SKIN DOUG DC8 DC862 3021970WP WS 566 LE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND THE LEFT WING LEADING EDGE WITH CORROSION AT STATION XFS 566. REMOVED FASTENERS, REMOVED CORROSION, FOUND LEVEL 2 CORROSION FABRICATED DOUBLER IAW 57-2-1 TREATED AND PRIMED IAW 51-1-8 INSTALLED FILLERS AND DOUBLER IAW SRM 57-2-1, 51-1-21 AND 51-1-21A. 2L74 4F 4A25 19950922002731995092200273WP 1995 9 22 95ZZZM439 119950615A5320 SUPPORT DOUG DC8 DC862 3021970WP FUSELAGE CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LEFT W/W FAIRING SUPPORT FRAME BENEATH REVERSER PUMP WITH LEVEL 2 CORROSION. FABRICATED NEW SUPPORT USED 7075-T6.063 IAW 51-1-0 TREATED WITH ALODINE AND F.R. PRIMER IAW 51-1-8 INSTALLED NEW SUPPORT AS PER SRM 51-1-21 AND SRM 53-1-0. 2L74 4F 4A25 19950922002741995092200274WP 1995 9 22 95ZZZM440 119950615A5330 SKIN DOUG DC8 DC862 3021970WP FS 862 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND FS 862 JUST FORWARD OF LEFT MLG DOOR (BELLY FAIRINGS) HAS A 4 INCH BY 3 INCH TEMP REPAIR. FABRICATED NEW SKIN AS PER ORIGINAL USED CLAD 7075-T6 .050 DRILLED HOLES TREATED AREAS WITH ALODINE AND F.R. PRIMER IAW SRM 51-1-8 INSTALLED NEW SKIN WITH FASTENERS IAW SRM 51-1-21. 2L74 4F 4A25 19950922002751995092200275EU 1995 9 22 95ZZZM441 119950821A21704935C123 WATER SEPARATOR JETAIRJETSTMJETSTM4101 1500501EU RT WING ROOT DIRTY A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27323UE 41059 FLT NR 6590 - IAD-RDU - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE CREW REPORTING FUEL SMELL IN COCKPIT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE WATER SEPARATOR SOCK AND THE COLD AIR UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE NR VTZA95256. 2L72 4T RTA41NM 19950922002761995092200276NM 1995 9 22 95ZZZM442 119950823A801138315212 AIRTURB STARTER BOEING737 737297 1384480NM NR 1 ENGINE MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13726AL 22426 NR 1 ENGINE START VALVE OPEN LIGHT INFLIGHT. THE AIRCRAFT WAS RETURNED TO HNL AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE STARTER SHUTOFF VALVE, AIRTURBINE STARTER AND STARTER ADAPTER. GRO OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REFERENCE TSAA9580166. 2L72 4F A16WE 19950922002771995092200277WP 1995 9 22 95ZZZM443 119950615A5512565174763 SKIN DOUG DC8 DC862 3021970WP LT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND LEFT SIDE HORIZONTAL STABILIZER, UPPER SKIN HAD CORROSION LEVEL 2 FROM XE 219.979 TO XE 312.500 AT TRAILING EDGE. REMOVED PANEL AND ROUTED TO OUTSIDE SERVICE. PANEL WAS RESKINNED AND REINSTALLED. 2L74 4F 4A25 19950922002781995092200278WP 1995 9 22 95ZZZM444 119950615A5320 DOUBLER DOUG DC8 DC862 3021970WP CARGO DR CUTOUT DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING C-CHECK INSPECTION, FOUND IMPROPER REPAIR ON THE LOWER FORWARD CARGO COMPARTMENT AFT DOOR CUTOUT AT LOWER FORWARD SAB CORNER. REMOVED IMPROPER REPAIR, FABRICATED DOUBLERS USE CLAD 7075-TL 125 AND .090 TREATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 51-1-21, 51-3-0, 51-1-20D AND DRAWING SR 08530019. 2L74 4F 4A25 19950922002791995092200279NE 1995 9 22 EIAA9536 219950808A7230 COMPRESSOR BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 2 ENGINE STALLED A EIAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 NM09485EV 7381 20712 662220 BBR - NR 2 ENGINE COMPRESSOR STALLED WITH PARAMETERS EPR 1.34, N1 92 PERCENT, N2 90 PERCENT, EGT 800 DEGREES CELSIUS, FLIGHT LEVEL 290. OIL QUANTITY RAPIDLY DECREASED, PERFORMED ENGINE SHUT DOWN PROCEDURES AND SECURED ENGINE. PARAMETERS AFTER SHUT DOWN N1 30.5 PERCENT, N2 25.5 PERCENT, EGT 18 DEGREES CELSIUS OIL QUANTITY 0 OIL TEMP 70 DEGREES CELSIUS, OIL PRESS 0. DID NOT ATTEMPT TO RESTART DUE TO ZERO OIL QUANTITY. REMOVED AND REPLACED NR 2 ENGINE AS PER F7201 RUN UP COMPLIED WITH MM 72-00-00. (M) 2L74 4F4 F A20WE E20EA 19950922002801995092200280NE 1995 9 22 EIAA9538 219950811A7200 ENGINE BOEING747 747273C 1384896NM PWA JT9 JT9D7J 52054NE NR 4 MALFUNCTIONED A EIAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 NM09471EV 78 20651 662889 JFK - ENGINE EGT STARTED TO RAPIDLY RISE AFTER DESCENT FROM FL 370. SHUT DOWN FUEL AND WAITED COUPLE MINUTES AND MADE WINDMILLING START AND TEMPERATURE RISING PAST 550 DEGREES CELSIUS AND ABORTED START. WAITED TO FL 250 AND MADE WINDMILLING START OK. TEMPS NEVER EXCEEDED LIMITS. ENGINE OPERATED NORMALLY FOR REMAINDER OF FLIGHT. REMOVED NR 4 ENGINE PER WORK CARDS 9724001, 9724002, 9724003 AND 9724007. OPS CHECKS OK. (M) 2L74 4F4 F A20WE E20EA 19950922002811995092200281NE 1995 9 22 EIAA9539 219950815A7200 ENGINE BOEING747 747121 1384871NM PWA JT9 JT9D7J 52054NE NR 4 FLAMED OUT A EIAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 NM09473EV 2580 19657 662247 DURING CLIMB-OUT FROM JFK PASSING FL 33.2, MACH .81, 290 KNOTS, NR 4 ENGINE FLAMED OUT, IT WAS X-FEEDING FROM NR 2 MAIN TANK AT THE TIME, ALL OTHER PARAMETERS WERE NORMAL, ACCOMPLISHED SHUT DOWN CHECKLIST AND IN FLIGHT CHECKLIST. ENGINE RESTARTED NORMALLY, ALL PARAMETERS NORMAL. CHECKED NR 4 ENGINE INLET AND EXHAUST FOR DAMAGE. FOUND NONE. CHECKED 3.5 BLEED FOUND NORMAL, DISCONNECTED STARTER DUCT FOUND NO METAL PARTICLES. REMOVED NR 4 MAIN FUEL FILTER, FOUND NO CONTAMINATION PER FIM 71-01. AIRCRAFT DISPATCHED FOR FURTHER OPS. (M) 2L74 4F4 F A20WE E20EA 19950922002821995092200282NM 1995 9 22 MZZA95044 119950814A2910AE2463513J0604 HOSE BOEING727 727224 1384076NM NR 2 ENGINE RUPTURED A MZZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP1379745 22448 FLT NR 965 - GUM - LOST 'A' SYSTEM HYDRAULIC AFTER TAKEOFF. QUANTITY DROPPED TO ZERO. MANUAL GEAR EXTENTION PERFORMED. MAINTENANCE FOUND A BROKEN PRESSURE HYDRAULIC LINE COMING FROM NR 2 ENGINE HYDRAULIC PUMP INSIDE STAIRWELL AREA. REPLACED LINE. ALSO, FOUND NR 1 ENGINE HYDRAULIC PUMP BURNED UP. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP ASSEMBLY, CHECKED SYSTEM 'A' MODULE AND CASE DRAIN FILTERS. ALL FOUND CLEAN. RAN ENGINE CYCLED FLIGHT CONTROL AND ALL CHECKED GOOD WITH NO LEAKS. (M) 2L73 4F A3WE 19950922002831995092200283CE 1995 9 22 PLGA812951G 119950812A3230IN4005 DIODE BEECH 1900 1900C 1154161CE LANDING GEAR FAILED A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE0515503 UC72 LGA - FLT NR 4654 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LGA LANDING WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR FERRY FLIGHT TO ALB MAINTENANCE BASE FOR REPAIRS. ALB MAINTENANCE REMOVED AND REPLACED TWO LINE DIODES AT THE HYDRAULIC POWER PACK SELECTOR VALVE, PERFORMED SEVERAL GEAR SWINGS AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19950922002841995092200284EU 1995 9 22 PLGA81895G1 119950818A61202100600002 CONNECTOR PIN C821452 SAAB SF340 SF340A 7850100EU RT PCU CABLE FAILED A PLGAO OTHER O OTHER APAPPROACH 1 NE05748BA 340A149 FLTN 4787 - ON FINAL INTO PWM, THE RIGHT PROP RPM DROPPED TO 1160 WITH THE CONDITION LEVER AT MAX. ON THE GROUND, THE CREW WAS UNABLE TO FEATHER THE PROPELLER WITH THE CONDITION LEVER. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND FOUND THAT THE BALL JOINT CONNECTOR RETAINING PIN HAD FAILED AND ALLOWED THE BALL JOINT TO SEPARATE FROM THE CONTROL CABLE. MAINTENANCE REPLACED THE BALL JOINT CONNECTOR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA52EU 19950922002851995092200285NM 1995 9 22 TSAA9580166 119950823A801297910211 STARTER SO VLV BOEING737 737297 1384480NM NR 1 ENGINE MALFUNCTIONED A TSAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13726AL 22426 NR 1 ENGINE START VALVE OPEN LIGHT ON INFLIGHT. THE AIRCRAFT WAS RETURNED TO HNL AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE STARTER SHUTOFF VALVE, AIRTURBINE STARTER AND STARTER ADAPTER. GRO OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950922002861995092200286NM 1995 9 22 USAA950765 119950723A21307110025 PANEL BOEING737 7374B7 1384702NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19428US 24550 LGA - FLT NR 8076 - EN ROUTE BOS TO CLT, THE CABIN ALTITUDE HORN SOUNDED AND THE CABIN PRESSURIZATION WAS CLIMBING. CAPTAIN DECIDED TO DIVERT TO LGA. MAINTENANCE REPLACED THE CABIN PRESSURE SELECT PANEL, PRESSURE CONTROLLER AND OUTFLOW VALVE. (M) 2L72 4F RTA16WE 19950922002871995092200287EU 1995 9 22 USAA950766 119950721A2150 PACK FOKKERF28 F28MK0100 4990807EU LEFT FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19890US 11365 PIT - FLT 0317 - UPON CLIMB-OUT, THE CAPTAIN REPORTED THAT HE SHUT THE AIR CONDITIONING PACK OFF AND WAS RETURNING TO PIT. MAINTENANCE REPLACED THE LEFT COOLING PACK. OPERATIONS CHECKED GOOD. (M) 2L72 4F RT 19950922002881995092200288EU 1995 9 22 USAA950768 119950722A5270 STRIKER FOKKERF28 F28MK4000 4990810EU CARGO DOOR OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19478US 11227 PHF - FLT NR 1297 - AFTER TAKEOFF FROM PHF, CREW RECEIVED A CARGO DOOR LIGHT. CAPTAIN ELECTED TO RETURN TO PHF. MAINTENANCE ADJUSTED THE AFT CARGO DOOR WARNING SWITCH STRIKER. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA20EU 19950922002891995092200289EU 1995 9 22 USAA950852 119950713A5320 WEB FOKKERF28 F28MK4000 4990810EU LT MLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19477AU21366 11226 PIT - DURING FC-6 CHECK INSPECTION, FOUND .5 INCH CRACK FORWARD VERTICAL WEB IN NLG WHEEL WELL LOWER LIGHTENING HOLE. INSTALLED DOUBLER REPAIR PER SRM 53-02-01 FIG 8. (M) 2L72 4F RTA20EU 19950922002901995092200290EU 1995 9 22 USAA950853 119950720A5330 SKIN FOKKERF28 F28MK4000 4990810EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19477AU21366 11226 PIT - DURING FC-6 CHECK INSPECTION, FOUND DENT 3MM DEEP AND 1 INCH IN DIAMETER FUSELAGE SKIN 6 INCHES BELOW AFT WATER SERVICE PANEL BETWEEN STRINGER 9 AND 10. INSTALLED DOUBLER REPAIR PER SRM 53-02. (M) 2L72 4F RTA20EU 19950922002911995092200291EU 1995 9 22 USAA950895 119950812A3350 EEL FOKKERF28 F28MK4000 4990810EU CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19498US 11181 CLT - THE OVERHEAD EMERGENCY LIGHTING COMES ON WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE TROUBLESHOT THE EVACUATION LIGHTING SYSTEM. OPERATIONS WERE FOUND TO BE NORMAL. (M) 2L72 4F RTA20EU 19950922002921995092200292WP 1995 9 22 VTZA95247 219950803A732089778025 FUEL CONTL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27495UE 818 P66182 FLT NR 6383 - CMH-IAD - DURING TAKEOFF, ABORTED THE TAKEOFF DUE TO THE ENGINE DID NOT MAKE TARGET TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED SCREW X ON THE FUEL CONTROL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950922002931995092200293GL 1995 9 22 VTZA95248 319950801A6197 HARNESS JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR36B5JFR36C1103GL LT PROP HEAT FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27321UE 41045 FLT NR 6506 - LYH-CHO - DURING CLIMB-OUT, RETURNED TO LYH DUE TO THE LEFT PROP HEAT FAILING. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 21935 IAW MEL 61-1. MAINTENANCE LATER CLEARED DMI NR 21935 BY REPLACING THE PROP HEATER LEAD HARNESS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 6 CP15NE 19950922002941995092200294EU 1995 9 22 VTZA95249 119950807A7714AG34 TACH GENERATOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27488UE 907 FLT NR 6282 - IAD-HPN - DURING CLIMB-OUT RETURNED TO IAD DUE TO LEFT ENGINE RPM DROPPED TO ZERO ON CLIMB-OUT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LEFT TACH GEN. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950922002951995092200295EU 1995 9 22 VTZA95250 119950807A3260ATG135022 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27311UE 41029 FLT NR 6573 - IAD-RDU - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE RED GEAR HANDLE LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED UP. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN UPLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950922002961995092200296EU 1995 9 22 VTZA95251 119950810A3260ATG135022 UPLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU LT MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27317UE 41031 FLT NR 900 - LYH-ROA - DURING CLIMB-OUT RETURNED TO LYH DUE TO THE LEFT RED GEAR HANDLE LIGHT REMAINING ILLUMINATED WHEN GEAR SELECTED UP. AIRCRAFT RETURNED TO LYH WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN UPLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950922002971995092200297EU 1995 9 22 VTZA95252 119950811A24221B3501B13 INVERTOR BAG JETSTMJETSTM3201 1500217EU NOSE EQUIP BAY FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27474UE 849 FLT NR 6495 - MDT-IAD - TAKEOFF WAS ABORTED, DUE TO THE RIGHT INVERTOR FAILING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT MAIN INVERTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950922002981995092200298NE 1995 9 22 VTZA95253 219950817A7530S2L226 O-RING JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27307UE 41021 P75020C FLT NR 6330 - IAD-PIT - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT DUCT FAIL LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE O-RINGS ON THE LEFT ENGINE BLEED DUCT COUPLING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA41NM E18NE 19950922002991995092200299EU 1995 9 22 VTZA95254 119950820A324091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PARKING BRAKE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27302UE 41013 FLT NR 6202 - MDT-IAD - ABORTED THE TAKEOFF DUE TO THE CONFIGURATION WARNING SOUNDING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE PARKING BRAKE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950922003001995092200300EU 1995 9 22 VTZA95256 119950821A21501718D000 COLD AIR UNIT JETAIRJETSTMJETSTM4101 1500501EU RT WING ROOT FAILURE A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA27323UE 41059 FLT NR 6590 - IAD-RDU - DURING CLIMB-OUT RETURNED TO IAD DUE TO THE CREW REPORTING FUEL SMELL IN COCKPIT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE WATER SEPARATOR SOCK AND THE COLD AIR UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950922003011995092200301EU 1995 9 22 VTZA95257 119950822A76006945059010 T2 SENSOR JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27314UE 41027 FLT NR 6193 - IAD-JFK - DURING CLIMB-OUT MADE AN UNSCHEDULED LANDING AND RETURNED TO GATE DUE TO THE LEFT ENGINE IEC FAILED ON TAKEOFF CLIMB-OUT. MAINTENANCE REPLACED LEFT ENGINE T2 SENSOR AND PERFORMED ENGINE RUNS. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950922003021995092200302EU 1995 9 22 VTZA95259 119950823A73301103P171 LOW PRESS SW BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27489UE 908 P66214A FLT NR 6258 - IAD-ALB - DURING CLIMB-OUT, MADE AN UNSCHEDULED LANDING BACK TO IAD DUE TO LEFT ENGINE IGNITION LIGHT COMING ON IN FLIGHT (AUTO IGNITION). AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED RELAY AND PRESSURE SWITCH AND MAF WAS SATISFACTORY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19950922003031995092200303WP 1995 9 22 95ZZZM445 119950817A3231510361 LINK DOUG DC8 DC861 3021952WP NLG DOOR STICKING A FXLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO1929UA 46159 AFTER TAKEOFF SDQ, RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RELEASE PIN STICKING IN FORWARD RT DOOR LINK ASSY. REPLACED LINK EPR MM 32-22-2. RETURNED AIRCRAFT TO SERVICE. 2L74 4F 4A25 19950922003041995092200304NM 1995 9 22 95ZZZM446 119950822A2530B006781 CONTROLLER BOEING747 747131 1384881NM SERVING CART SMOKING A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0553116 20321 JFK - FLT NR 803 - DURING CRUISE, SMOKE AND ELECTRICAL ODOR EMITTED FROM AFT GALLEY E-1 SERVING CART CONTROLLER, MFG P/N B006781. TURNED OFF CONTROLLER AND OPENED CIRCUIT BREAKERS. REPLACED THE E-1 CART CONTROLLER AND OPERATION CHECKED NORMAL. 2L74 4F A20WE 19950922003051995092200305WP 1995 9 22 95ZZZM447 119950802A5347 SEAT TRACK DOUG DC9 DC931 3022065WP BS 200-266 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 67006 47134 STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4. 2L72 4F A6WE 19950922003061995092200306EU 1995 9 22 AWXA9500541 119950816A5320 SUPPORT AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CABIN FLOOR STRUCTURE CORRODED IN SEVERAL AREAS ON TOP SURFACE OF 'I' BEAM UPPER CHORD, FRAME 17 TO FRAME 19 Y 254. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-11-14. (M) 2L72 4F RTA28NM 19950922003071995092200307EU 1995 9 22 AWXA9500542 119950816A5320 SUPPORT AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON FLOOR BEAM SUPPORT FROM FRAME 16 TO FRAME 20 AT Y 254. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER PER SRM 53-11-14. (M) 2L72 4F RTA28NM 19950922003081995092200308EU 1995 9 22 AWXA9500543 119950816A5315 FLOOR BEAM AIRBUS320 A320231 3930325EU CABIN CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEVERAL AREAS OF CORROSION ON TOP SURFACE OF CABIN FLOOR 'I' BEAM UPPER CHORD FROM FRAME 17 TO FRAME 19 AT Y 1292. INSTALLED NEW FLOOR BEAM SECTION PER SRM 51-72-11 AND SRM 51-42-21. (M) 2L72 4F RTA28NM 19950922003091995092200309EU 1995 9 22 AWXA9500544 119950816A5320 SUPPORT AIRBUS320 A320231 3930325EU CARGO COMPT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT LEFT FLOOR SUPPORT AT FRAME 29 CRACKED AT RIVET. REPAIRED IAW ER 32-53-26-28. (M) 2L72 4F RTA28NM 19950922003101995092200310EU 1995 9 22 AWXA9500545 119950816A5320 SUPPORT AIRBUS320 A320231 3930325EU CABIN CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR BOARD AFT SUPPORT STRUCTURE AT FR 65 CRACKED AND DEFORMED AT FASTENER HOLE. REPAIRED IAW ER 32-53-26-29. (M) 2L72 4F RTA28NM 19950922003111995092200311EU 1995 9 22 AWXA9500546 119950816A5230D5237119000251 CASTING AIRBUS320 A320231 3930325EU CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT DOOR HANDLE CASTING CRACKED AT FORWARD UPPER MOUNT BOLT LUG. REPAIRED PER ER 32-52-30-05. (M) 2L72 4F RTA28NM 19950922003121995092200312EU 1995 9 22 AWXA9500547 119950816A5230D5237119000251 CASTING AIRBUS320 A320231 3930325EU CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT CARGO COMPARTMENT DOOR FRAME CRACKED, AFT LOWER CORNER AT HANDLE. REPAIRED PER ER 32-52-30-05. (M) 2L72 4F RTA28NM 19950922003131995092200313EU 1995 9 22 AWXA9500548 119950816A5320 SUPPORT AIRBUS320 A320231 3930325EU CABIN CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28625AW 064 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT FR 31 CRACKED AND BENT, CENTER OF AIRCRAFT. REPAIRED IAW ER 32-53-26-27. (M) 2L72 4F RTA28NM 19950922003141995092200314NE 1995 9 22 AWXA9500549 219950816A7532 LOCK PIN AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 1 ENGINE LOOSE A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28624AW 55 PHX-YVR - FLT NR 815 - AIR TURNBACK DUE TO NR 1 ENGINE BLEED FAULT. BLEED WENT TO OVERHEAT CONDITION TWO MINUTES AFTER SELECTED ON. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND SAFETY WIRE BROKEN AND LOCK PIN BACKED OUT OF FAN AIR VALVE. REINSTALLED PIN AND SAFETIED. RAN ENGINE, TEMPERATURE 185 DEGREES CELSIUS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F4 FRTA28NM E311NE 19950922003151995092200315NM 1995 9 22 AWXA9500562 119950818A2612894093 FIRE LOOP BOEING737 737275 1384485NM NR 1 ENGINE FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP282FOR 4361 20922 PHX-IAH - FLT NR 273 - DURING CRUISE AT FL 330, NR 1 FIRE HANDLE LIGHT ILLUMINATED WITH FIRE WARNING BELL. NR 1 ENGINE WAS SHUTDOWN IAW QRH PROCEDURES, BOTH FIRE BOTTLES WERE DISCHARGED. LIGHT WENT OUT FOR APPROXIMATELY THREE MINUTES AND THEN WENT ON AND OFF SPORADICALLY. AIRCRAFT DIVERTED TO MAF, LIGHT REMAINED OUT FOR REMAINDER OF FLT. AIRCRAFT LANDED UNEVENTFULLY. MX REPLACED RT AND LT ENG FIRE BOTTLES IAW MM 26-21-11, CARD R4L26001. OPS CHECK OK PER A4L26003. ALSO, PLACED NR 1 ENGINE NORMAL POSTION ON MEL 26-02 UNTIL AIRCRAFT ARRIVED AT PHX BASE MAINTENANCE. PHX MAINTENANCE REPLACED NR 1 ENGINE LOWER FIRE DETECTION SYSTEM. OPS CHECK GOOD. MEL REMOVED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19950922003161995092200316EU 1995 9 22 PAYA95A4032 119950731A5712 RIB AEROSPATR42 ATR42300 8680920EU LT WING CHAFED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174210G 149 LEFT WING RIB NR 30 CHAFED AT THE STROBE POWER SUPPLY MOUNTING LOCATION. REPAIRED IAW AN 8110-3. (M) 2H72 4T RTA53EU 19950922003171995092200317EU 1995 9 22 PAYA95A4033 119950731A5210 SKIN AEROSPATR42 ATR42300 8680920EU PAX DOOR CORRODED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174210G 149 PASSENGER DOOR SKIN, INNER SURFACE, FOUND CORRODED. REPAIRED IAW SRM. (M) 2H72 4T RTA53EU 19950922003181995092200318EU 1995 9 22 PAYA95A4034 119950731A5210 STEP FRAME AEROSPATR42 ATR42300 8680920EU PAX DOOR CRACKED A PAYAK NONE O OTHER ININSP/MAINT 1 EA174210G 149 PASSENGER DOOR STEP FRAME CRACKED IN TWO PLACES. REPAIRED IAW SRM. (M) 2H72 4T RTA53EU 19950922003191995092200319EU 1995 9 22 PAYA95A4035 119950814A3260C24589000 UPLOCK BOX AEROSPATR42 ATR42300 8680920EU NLG MALFUNCTIONED A PAYAO OTHER N FALSE WARNING APAPPROACH 1 EA174208G 086 FLT NR 7728 - BWI-JFK - WITH LANDING GEAR UP, THE LEFT MAIN AND NOSE GEAR TRANSIT LIGHTS CYCLED THREE TIMES WITH AN ASSOCIATED HYDRAULIC SURGE. REPLACED NOSE GEAR UPLOCK BOX. (M) 2H72 4T RTA53EU 19950922003201995092200320EU 1995 9 22 PAYA95A4036 119950815A3260D227870001 PROX HARNESS AEROSPATR42 ATR42300 8680920EU NLG MALFUNCTIONED A PAYAO OTHER N FALSE WARNING APAPPROACH 1 EA174208G 086 FLT NR 7753 - JFK-ORF - WITH LANDING GEAR UP, THE NOSE TRANSIT LIGHT INTERMITTENTLY CAME ON WITH AN ASSOCIATED HYDRAULIC SURGE. REPLACED NOSE GEAR SECONDARY PROXIMITY HARNESS. (M) 2H72 4T RTA53EU 19950922003211995092200321EU 1995 9 22 SIMA952161 119950804A29109302630001 LINE SAAB SF340 340B 7860101EU HYD BAY RUPTURED A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21588MA 340B169 FSM - FLT NR 3523 - LOST MAIN HYDRAULIC PRESSURE IN FLIGHT. PILOT MANUALLY SELECTED GEAR DOWN USING ALTERNATE MEANS. MAINTENANCE REPLACED RUPTURED HYD LINE. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19950922003221995092200322EU 1995 9 22 SIMA952191 119950806A3241AN35A SCREWS AEROSPATR72 ATR72212 EU ANTI-SKID VALVE BROKEN A SIMAO OTHER K FLUID LOSS DEDESCENT 1 SW21369AT 369 CRP - FLT NR 3857 - BLUE AND GREEN HYDRAULIC SYSTEM LOW LEVEL LIGHT ON INFLIGHT, LANDING GEAR EXTENDED MANUALLY, ZERO FLAPS LANDING. CFR CALLED OUT. (M) 2H72 4T RTA53EU 19950922003231995092200323EU 1995 9 22 SIMA952201 119950808A33503011210 EEL AEROSPATR42 ATR42300 8680920EU PAX DOOR BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21427MQ 451 091 ORD - FLT NR 4369 - WHILE DOING THE INITIAL INSPECTION OF THE AIRCRAFT, THE CREW NOTED THE PASSENGER STAIR EMERGENCY LIGHT WAS INOP. MAINTENANCE FOUND A PIN CONNECTOR DAMAGED ON THE LIGHT ASSY. MAINTENANCE REPLACED THE LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950922003241995092200324EU 1995 9 22 SIMA952231 119950811A33503011210 EEL AEROSPATR42 ATR42300 8680920EU PAX DOOR DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21420MQ 601 012 RFD - DURING PS-2 CHECK, MAINTENANCE FOUND THE PASSENGER/CREW DOOR EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE PASSENGER/CREW DOOR EMERGENCY LIGHT IAW JIC 33-51-24. EMERGENCY LIGHT SYSTEM OPS CHECKED GOOD, IAW JIC 33-50-00. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950922003251995092200325EU 1995 9 22 SIMA952291 119950817A27108618M2 LINEAR ACTUATOR SAAB SF340 SF340A 7850100EU AILERONS OUT OF ADJUST A ASIMAO OTHER EF VIBRATION/BUFFET FLT CONT AFFECTED DEDESCENT 1 SW21109AE 340A109 OKC - FLT NR 3553 - DESCENT FOR LANDING INTO OKC, AIRCRAFT EXPERIENCED SEVERE ROLL RIGHT. CREW RECOVERED AND CONTINUED FOR AN UNEVENTFUL LANDING. FOLLOWING LANDING WHEN CREW RESET THE GUST LOCK, IT WAS NOTED THAT THE AILERONS WERE IN A DISCONNECT CONFIGURATION. ADJUSTED AILERON DISCONNECT ACTUATOR. CONDUCTED SATISFACTORY TEST FLIGHT. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4T RTA52EU 19950922003261995092200326EU 1995 9 22 USAA950762 219950720A7323GD501 GOVERNOR FOKKERF28 F28MK0100 4990807EU RROYCESPEY SPEY55515 54521EU LT ENGINE LEAKING A USAALA ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA19898US 11398 11398 SRQ - FLT NR 0139 - DURING A GO-AROUND PROCEDURE DUE TO THUNDERSTORMS, THE LEFT ENGINE WOULD NOT PRODUCE SELECTED THRUST. CAPTAIN DECIDED TO DIVERT TO SRQ WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP SHAFT GOVERNOR. LEAK CHECKED GOOD. (M) 2L72 4F4 FRT E2EU 19950922003271995092200327WP 1995 9 22 USAA950851 119950726A5530 ANGLE DOUG DC9 DC931 3022065WP VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19933VJ71857 47216 PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN VERTICAL STAB ATTACH ANGLE VERTICAL LEG AFT END LEFT SIDE. INSTALLED DOUBLER REPAIR 14 INCHES IN LENGTH PER SRM 53-05 FIG 23A. (M) 2L72 4F A6WE 19950922003281995092200328EU 1995 9 22 USAA950854 119950712A5313 STRINGER FOKKERF28 F28MK0100 4990807EU BS 3870 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19855US13185 11283 PIT - DURING C-CHECK INSPECTION, FOUND 2 INCH CRACK AND STRINGER NR 68R APPROXIMATELY 4 INCHES AFT OF STATION 3870. INSTALLED SPLICE REPAIR PER SRM 51-70-06 REPAIR NR 5 PG 206. (M) 2L72 4F RT 19950922003291995092200329NM 1995 9 22 USAA950897 119950818A335020121 EEL BATTERY PACK BOEING737 737301 1384611NM CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19334US 23231 LGA - THE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTING BATTERY PACK FOR ROW 12 TO 16. OPERATIONS CHECKED GOOD. (M) 2L72 4F RTA16WE 19950922003301995092200330NM 1995 9 22 USAA950898 119950820A5210 DOOR BOEING737 7373B7 1384580NM PAX DOOR NOT CLOSED A USAAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 EA19511AU 23594 JAX - FLT NR 8645 - RETURN TO JAX DUE TO THE MAIN CABIN DOOR NOT BEING CLOSED PROPERLY. THE CAPTAIN DID NOT RECEIVE ANY LIGHTS IN THE COCKPIT PRIOR TO DEPARTURE THAT THE DOOR WAS NOT CLOSED. MAINTENANCE INSPECTED THE DOOR. NO DEFECTS NOTED. (M) 2L72 4F RTA16WE 19950922003311995092200331NE 1995 9 22 USAA950902 219950813A7260 OIL SLEEVES BOEING757 757225 1384959NM RROYCERB211 RB211535E43754555NE UPPER/LOWER LEAKING A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19618AU 22210 MCI - FLT NR 0675 - CAPTAIN DIVERTED TO MCI DUE TO HIGH OIL CONSUMPTION ON THE LEFT ENGINE. THE ENGINE WAS NOT SHUT DOWN. FLIGHT LANDED SAFELY. MAINTENANCE FOUND A CUT SEAL ON THE LEFT ENGINE HIGH SPEED GEAR BOX RADIAL DRIVE SHAFT. THE ASSEMBLY WAS RESEALED AND THE UPPER AND LOWER OIL SEALING SLEEVES WERE REPLACED. NO LEAKS NOTED. (M) 2L72 4F4 FRTA2NM E12EU 19950922003321995092200332SO 1995 9 22 WTAA950237 119950721A7334M8372386R1005N CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE FUEL PRESS SW LOOSE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17453UE 120148 SFO - LEFT ENGINE FUEL LOW PRESSURE LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED LEFT FUEL LOW PRESSURE LIGHT PER MEL 73-35-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY REPLACED ELECTRICAL CONNECTOR AT LEFT FUEL LOW PRESSURE SWITCH. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2L72 4T4 TRTA31SO E20NE 19950922003331995092200333SO 1995 9 22 WTAA950238 119950721A282012008735 FUEL LINE EMB 120 EMB120RT SO LEFT WING LEAKING A WTAACD ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TOTAKEOFF 1 WP17453UE 120148 SFO - LEFT ENGINE REPORTED TORQUE LIMITED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED LEFT FUEL MOTIVE FLOW SYSTEM PER MEL 28-21-3. AIRCRAFT RETURNED TO SERVICE, MAINTENANCE SUBSEQUENTLY REPLACED LEAKING MOTIVE FLOW LINE IN LEFT WING FUEL BAY. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA31SO 19950922003341995092200334SO 1995 9 22 WTAA950239 119950726A3150 TAKEOFF WARNING EMB 120 EMB120RT SO TRIM SYSTEM ACTIVATED A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17122AM 120013 SFO - TAKEOFF TRIM WARNING ACTIVATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED TRIM SYSTEM. NO DEFECTS NOTED. ACCOMPLISHED OPERATIONAL CHECK OF TRIM SYSTEM AND AURAL WARNING UNIT. ALL CHECKS NORMAL. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19950922003351995092200335NE 1995 9 22 WTAA950240 219950801A7320M8372386R1203N CONNECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE DIRTY A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17201YW 120201 SBP - RT ENGINE EEC FAILED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED EEC PER MEL 73-21-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL. MAINTENANCE CLEANED ELECTRICAL CONNECTOR AT RIGHT ENGINE NL SPEED PROBE. (M) 2L72 4T4 TRTA31SO E20NE 19950922003361995092200336EU 1995 9 22 WTAA950241 119950806A7110 COWL BAG JETSTMJETSTM3101 1500215EU RT ENGINE BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17417UE 794 LAX - BIRD STRIKE REPORTED AT RIGHT ENGINE COWL. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950922003371995092200337SO 1995 9 22 WTAA950242 119950806A2750 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A AWTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17280UE 120090 SFO - FLAP ASYMMETRY REPORTED WHEN TRANSITIONING INTO CRUISE CONFIGURATION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE DISCREPANCY ON GROUND. REPLACED FLAP CONTROL UNIT AND FLAP ANNUNCIATOR PANEL FOR PRECAUTIONARY REASONS. AIRCRAFT RETURNED TO SERVICE. REMOVED AND COMPONENTS WERE INSPECTED AND BENCH CHECKED WITH NO DISCREPANCIES NOTED. COMPONENTS RETURNED TO STOCK. (M0 2L72 4T RTA31SO 19950922003381995092200338 1995 9 22 WTAA950244A 419950808A2350MS21353351 PTT SWITCH BAG JETSTMJETSTM3101 1500215EU FO'S CONTRL YOKESHORTED A WTAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP17402UE 734 FAT - EN ROUTE FAT TO SFO, FLIGHT OFFICERS INTERCOM TRANSMISSIONS REPORTED INTERMITTENTLY TRANSMITTING ON COMM RADIO FREQUENCY WITH PTT SWITCH SELECTED TO INTERCOM. AIRCRAFT RETURNED TO STATION. AVIONICS REPLACED FLIGHT OFFICERS PTT SWTICH AND FLIGHT OFFICERS CONTROLLER (STATION BOX). FLIGHT OFFICERS COMMUNICATIONS SYSTEM OPERATIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950922003391995092200339 1995 9 22 WTAA950244B 419950808A2350B692229 CONTROLLER BAG JETSTMJETSTM3101 1500215EU COCKPIT INTERMITTENT A WTAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP17402UE 734 FAT - EN ROUTE FAT TO SFO, FLIGHT OFFICERS INTERCOM TRANSMISSIONS REPORTED INTERMITTENTLY TRANSMITTING ON COMM RADIO FREQUENCY WITH PTT SWITCH SELECTED TO INTERCOM. AIRCRAFT RETURNED TO STATION. AVIONICS REPLACED FLIGHT OFFICERS SWITCH AND FLIGHT OFFICERS CONTROLLER (STATION BOX). FLIGHT OFFICERS COMMUNICATION SYSTEM OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950922003401995092200340 1995 9 22 WTTAA950243 419950807A23509970054 PTT SWITCH BAG JETSTMJETSTM3101 1500215EU FO'S CNTRL YOKE SHORTED A WTAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP17402UE 734 FAT - EN ROUTE FAT TO SMF, FLIGHT OFFICERS INTERCOM TRANSMISSIONS REPORTED TRANSMITTING ON COMM RADIO FREQUENCY WITH PTT SWITCH SELECTED TO INTERCOM. AIRCRAFT RETURNED TO STATION. AVIONICS REPAIRED SHORTED WIRE AT FLIGHT OFFICERS PTT SWITCH. INTERPHONE SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19950922003411995092200341NM 1995 9 22 95ZZZM448 119950822A3230 BOLT BOEING727 727231 1384079NM LANDING GEAR WORN A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0552310 19829 FLT NR 556 - STL - AFTER TAKEOFF, LANDING GEAR LEVER WAS LOCKED. USED OVERRIDE PROCEDURES TO RETRACT LANDING GEAR. FOUND WORN BOLT FOR LANDING GEAR SAFETY SWITCH SENSOR ACTUATOR. REPLACED BOLT AND LANDING GEAR OPERATION CHECKED NORMAL. 2L73 4F A3WE 19950922003421995092200342NM 1995 9 22 95ZZZM449 119950822A2530888011 SERVING CART BOEING767 767231 1385131NM GALLEY SMOKING A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05605TW 22568 JFK - FLT NR 740 - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR. TURNED OFF AND DISCONNECTED CART, MFG P/N 88801-1. FOUND MALFUNCTIONING HEATING PLATES. REPLACED SERVING CART AND OPERATION CHECKED NORMAL. 2L72 4F RTA1NM 19950922003431995092200343WP 1995 9 22 95ZZZM450 119950822A3231S2210370P9157 BUSHING DOUG DC9 DC982 3022082WP LT MLG DOOR MISSING A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05920TW 49369 MCI - FLT 179 - DURING CLIMB, LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND LEFT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED. VERIFIED LANDING GEAR WAS DOWN AND DOOR REMAINED OPEN. FOUND LEFT MAIN LANDING GEAR DOOR ACTUATOR BUSHING, MFG P/N S2210370P9-157, MISSING. INSTALLED BUSHING AND LANDING GEAR AND LANDING GEAR DOOR OPERATION CHECKED NORMAL. 2L72 4F A6WE 19950922003441995092200344NM 1995 9 22 95ZZZM451 119950714A5320 DECK BOEING727 727231 1384079NM LT MLG WW CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055433162690 20309 MCI - DURING C-CHECK, FOUND TWO CRACKS, EACH APPROXIMATELY ONE INCH LONG, IN LEFT MLG WHEELWELL CEILING PRESSURE DECK AFT OUTBOARD CORNER, FORWARD OF 950 BULKHEAD, LBL 56 AND 58. REPAIRED BY INSTALLING DOUBLER PER ARA 9372. TOTAL CYCLES 42,177. 2L73 4F A3WE 19950922003451995092200345NM 1995 9 22 95ZZZM452 119950714A5330 SKIN BOEING727 727231 1384079NM FS 720 WORN A TWAAK NONE O OTHER ININSP/MAINT 1 CE055434938173 21968 MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .030 TO .015, STRINGER 17R TO 19R, AND STRINGER 17L TO 19L, FS 720E TO 720F. ALSO, WORN APPROXIMATELY .040, STRINGER 19. REPAIRED PER ARA 9354. TOTAL CYCLES 24,723. 2L73 4F A3WE 19950922003461995092200346WP 1995 9 22 95ZZZM453 119950804A5753 FITTING DOUG DC9 DC932 3022066WP RT TE FLAP CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05997Z 47029 MCI - DURING OP-15 FOUND RIGHT WING RS AFT FLAP CENTER HINGE FITTING MOUNT AREA REAR SPAR WEB, CRACKED .75 INCH IN EYEBROW AT UPPER OUTBOARD HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SB 57-179 AND DRAWING J060272-502. 2L72 4F A6WE 19950922003471995092200347NM 1995 9 22 95ZZZM454 119950714A5530 SKIN BOEING727 727231 1384079NM VERT STAB CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055434938173 21968 MCI - DURING OP-17, FOUND A ONE INCH CRACK IN SKIN ON VERTICAL STABILIZER LEFT SIDE AT BASE, FS 1330. STOP DRILLED CRACK PER SRM 51-10-1, AND REPAIRED PER ARA9370A. TOTAL CYCLES 24,723. 2L73 4F A3WE 19950922003481995092200348WP 1995 9 22 95ZZZM455 119950802A5313 LONGERON DOUG DC9 DC931 3022065WP BS 945-996 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 47134 STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. 2L72 4F A6WE 19950922003491995092200349WP 1995 9 22 95ZZZM456 119950802A5313 LONGERON DOUG DC9 DC931 3022065WP BS 945-996 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 47134 STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. 2L72 4F A6WE 19950922003501995092200350EA 1995 9 22 95ZZZM457 119950720A2430 RELAY A701AD DHAV DHC6 DHC6300 EA LT STARTER/GEN FAILED A ASMPAK NONE O OTHER ININSP/MAINT 1 WP1328SP CC37583 601 LEFT REVERSE CURRENT CUTOUT RELAY MAIN CONTACTORS REMAINED CLOSED AFTER ENGINE SHUTDOWN CAUSING THE STARTER/GENERATOR TO MOTOR CONTINOUSLY UNTIL THE MOTOR WAS DAMAGED FROM EXCESSIVE HEAT. THE LEFT ENGINE STARTER/GENERATOR AND REVERSE CURRENT CUTOUT RELAY WERE BOTH REPLACED. POST INSPECTION OF CUTOUT RELAY REVEALED THAT THE MAIN CONTACTORS WERE NOT BURNED AND FUSED. HOWEVER, THE 'E' TYPE EXTERNAL RETAINING SNAP RING THAT SECURES THE MAIN MOVEABLE CONTACTS ASSEMBLY WAS FOUND BROKEN. THUS ALLOWING THE MAIN CONTACTS TO CONNECT WITH THE STATIONARY CONTACTS. THIS PROVIDED CONTINUOUS POWER TO THE STARTER/GENERATOR, DAMAGING IT. 1H72 3T A9EA 19950922003541995092200354CE 1995 9 22 95ZZZM461 119950717A57301181100471 LE SKIN BEECH 1900 1900C 1154161CE LT WING DENTED A GLBAK NONE O OTHER TXTAXI/GRND HDL 1 CE0155668 UC138 SPW - LEFT OUTBOARD WING LEADING EDGE DAMAGED BY A TRACTOR. THE DAMAGE WAS REMOVED AND A SLUSH DOUBLER INSERT WAS INSTALLED IAW BEECH SRM. 2L72 4T RTA24CE 19950922003551995092200355NM 1995 9 22 ASAA9510073 119950812A335020131A EEL BATTERY BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON SEAT PALLET 5-8 WERE FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950922003561995092200356NM 1995 9 22 ASAA9510074 119950812A33506012541 EEL BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950922003571995092200357NM 1995 9 22 ASAA9540041 119950803A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LIGHTS AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950922003581995092200358NM 1995 9 22 ASAA9540042 119950803A3350S417N5048 EEL ASSY BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE FORWARD RED EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950922003591995092200359NM 1995 9 22 ASAA9540043 119950807A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 SEA - DURING MAINTENANCE CHECK, THE MID CABIN EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRING CONNECTION IN FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950922003601995092200360NM 1995 9 22 ASAA9540044 119950810A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01771AS 25104 SEA - FLOOR TRACK LIGHTS INOP ROWS 15-18. MAINTENANCE RECONNECTED WIRE HARNESS AT ROW 18. (M) 2L72 4F RTA16WE 19950922003611995092200361NM 1995 9 22 ASAA9540046 119950817A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01771AS 25104 SEA - FLT NR 486 - DURING PREFLIGHT, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15-18. FOUND SPLIT IN WIRE AT DISCONNECT, RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950922003621995092200362WP 1995 9 22 ASAA9580173 119950801A33501001191 EEL DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01938AS3730 49365 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON LAMP WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003631995092200363WP 1995 9 22 ASAA9580174 119950801A33506011779 EEL POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS17453 49925 PDX - DURING MAINTENANCE CHECK, THE AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003641995092200364WP 1995 9 22 ASAA9580175 119950802A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 15 AND 16 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003651995092200365WP 1995 9 22 ASAA9580176 119950803A33501001191 EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01960AS15221 53074 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003661995092200366WP 1995 9 22 ASAA9580177 119950805A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003671995092200367WP 1995 9 22 ASAA9580178 119950805A3350S103 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 10 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003681995092200368WP 1995 9 22 ASAA9580179 119950807A33500105610001 EEL SOCKET DOUG DC9 DC982 3022082WP CABIN SHORTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 PDX - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 2 SHORTED LAMP SOCKETS AND REPLACED F1 FUSE IN POWER SUPPLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003691995092200369WP 1995 9 22 ASAA9580180 119950807A3350S103 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01947AS 53020 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003701995092200370WP 1995 9 22 ASAA9580181 119950807A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003711995092200371WP 1995 9 22 ASAA9580182 119950810A3350 EEL TERMINAL DOUG DC9 DC983 3022083WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 LAX - PRIOR TO DEPARTURE OF FLIGHT 256 - CREW REPORTED THE FORWARD 4 EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. SECURED LOOSE TERMINAL AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003721995092200372WP 1995 9 22 ASAA9580183 119950813A335060030431 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN ILLUMINATED WHEN AIRCRAFT DEPOWERED. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003731995092200373WP 1995 9 22 ASAA9580184 119950814A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01957AS 49126 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003741995092200374WP 1995 9 22 ASAA9580186 119950815A335060030431 EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 25 TO 29 REMAIN ILLUMINATED WITH ELECTRIC POWER OFF. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19950922003751995092200375WP 1995 9 22 ASAA9580187 119950816A335041B004AD07G3 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REPLACED THE BATTERIES AND SIGN OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950922003761995092200376NM 1995 9 22 CAL950668 119950727A5511 SPAR CAP BOEING727 727243 138408DNM LT HORIZ STAB CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09579PE41584 21662 STA 31J - INSPECTION FOUND THE LEFT HORIZONTAL STABILIZER UPPER OUTBOARD SPAR CAP HAD INTERGRANULAR CORROSION. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 55-10-5, DETAIL 1. (M) 2L73 4F RTA3WE 19950922003771995092200377WP 1995 9 22 CAL950698 119950813A3244 TIRE DOUG DC9 DC932 3022066WP RT MLG BLOWN A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0912508 47797 FLT NR 549 - IAH - THE NR 3 RIGHT MLG TIRE BLEW ON TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE TIRE CASING CAUSED DAMAGE TO THE RT WING INBOARD TRAILING EDGE FLAP AND FLAP ACCESS DOOR AND THE NR 2 ENGINE C1 AND C2 FAN ASSEMBLIES. THE RT WING FLAP ACCESS DOOR WAS REMOVED AND REPLACED. THE RT WING INBOARD TRAILING EDGE FLAP WAS REPAIRED BY INSTALLING A DOUBLER IAW SRM 57-01, FIGURE 4, SHEET 2. THE C1 AND C2 FAN ASSEMBLIES WERE REPLACED. BOTH THE NR 3 AND NR 4 RT MLG TIRE/WHEEL ASSEMBLIES WERE REMOVED AND REPLACED PER MM 32-40-00. (M) 2L72 4F A6WE 19950922003781995092200378NE 1995 9 22 EIAA9535 219950726A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7A 52054NE NR 3 FLAMED OUT A AEIAAO OTHER X ENGINE FLAMEOUT NRNOT REPORTED 1 NM09481EV 19896 MNL - NR 3 ENGINE FLAMED OUT FL 390 IN TURBULENCE AND HEAVY RAIN, FUEL TEMP 5 DEGREES CELSIUS, EPR 1.40 LGN NR 2 ON SMALL ACC TAT-23M .89 IAS 261, ANTI-ICE ON RELIGHT EGT TO PLUS 1000 DEGREES FOR TWO SECONDS. ECRA 662274-72-001 REVISION A ACCOMPLISHED. NO DEFECTS NOTED AT THIS TIME PER MM 72-00-00, PAGES 221 THROUGH 244, LOGPAGE F09141. (M) 2L74 4F4 F A20WE E20EA 19950922003791995092200379CE 1995 9 22 95ZZZM462 119950706A521011451402813 BRACKET BEECH 1900 1900C 1154161CE AIRSTAIR DOOR LOOSE A GLBAK NONE O OTHER ININSP/MAINT 1 CE01167GL9499 UC167 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER ATTACH BRACKET LOOSE AND THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1. 2L72 4T RTA24CE 19950922003801995092200380CE 1995 9 22 95ZZZM463 119950702A5330 SKIN BEECH 1900 1900C 1154161CE DORSAL FIN CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01734GL19242 UB34 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 2 SKIN CRACKS AT THE INTERSECTION OF THE DORSAL FIN AND THE REAR PRESSURE BULKHEAD. CRACKS WERE STOP DRILLED AND REINFORCED IAW BEECH 1900 SRM. 2L72 4T RTA24CE 19950922003811995092200381CE 1995 9 22 95ZZZM464 119950701A521011451402813 BRACKET BEECH 1900 1900C 1154161CE AIRSTAIR DOOR LOOSE A GLBAK NONE O OTHER ININSP/MAINT 1 CE01734GL19227 UB34 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER BRACKET LOOSE. THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1. 2L72 4T RTA24CE 19950922003821995092200382CE 1995 9 22 95ZZZM465 119950630A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT NACELLE CRACKED A AGLBAK NONE O OTHER ININSP/MAINT 1 CE01152GL5498 330 UC152 SPW - DURING ROUTINE VISUAL INSPECTION OF AREA 'A' IAW AD95-02-18, THE RT ENGINE TRUSS WAS FOUND CRACKED. THE TRUSS WAS REMOVED AND REPLACED WITH A SERVICEABLE TRUSS. (M) 2L72 4T RTA24CE 19950922003831995092200383GL 1995 9 22 95ZZZM466 319950621A6111 BLADE BEECH 1900 1900C 1154161CE HARTZLHCB4M HCB4M GL RT PROP NICKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01123UE170862468 UC123 FW1158 GRI - ON WALK AROUND, THE PILOT FOUND A NICK ON ONE BLADE OF RT PROP. MAINTENANCE DETERMINED THAT THE NICK WAS OUT OF LIMITS AND CHANGED THE PROPELLER. 2L72 4T RTA24CE 6 CP56GL 19950922003841995092200384CE 1995 9 22 95ZZZM467 119950620A3244 TIRE BEECH 1900 1900C 1154161CE NLG SEPARATED A GLBAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 CE01174GL 84 0661 UC174 SQI - AFTER TAKEOFF, CREW REPORTED A VERY SEVERE NOSE WHEEL SHIMMY. AS A PRECAUTION, THE AIRCRAFT WAS DIVERTED TO SPI WHERE IT MADE AN UNEVENTFUL LANDING. MAINTENANCE NOTED THAT THE RECAP TREAD WAS GONE. THE NOSE WHEEL ASSY, P/N 11480013, CHANGED ALONG WITH A NOSE WHEEL WELL INSPECTION. NO DEFECTS NOTED. 2L72 4T RTA24CE 19950922003851995092200385CE 1995 9 22 95ZZZM468 119950615A521011451402813 BRACKET BEECH 1900 1900C 1154161CE AIRSTAIR DOOR LOOSE A GLBAK NONE O OTHER ININSP/MAINT 1 CE0198GL 14077 UC98 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE AIRSTAIR DOOR SNUBBER BRACKET LOOSE. THE ATTACH BRACKET WAS REMOVED AND REPLACED WITH BEECH KIT 114-4032-1. 2L72 4T RTA24CE 19950922003861995092200386CE 1995 9 22 95ZZZM469 119950614A5270MD3211Q1 SWITCH BEECH 1900 1900C 1154161CE CABIN DOOR OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE0160UE 16338 UC60 TVC - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURNBACK DUE TO AN UNSAFE CABIN DOOR INDICATION. AN UNEVENTFUL LANDING WAS ACCOMPLISHED, AFTERWHICH MAINTENANCE ADJUSTED THE DOOR MICROSWITCH. 2L72 4T RTA24CE 19950922003901995092200390EU 1995 9 22 95ZZZM473 119950813A2130 RELAY FOKKERF28 F28MK4000 4990810EU LEFT FAULTY A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19498US 11181 CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. THE CAPTAIN DECIDED TO RETURN TO CLT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE. REFERENCE NR USAA950896. 2L72 4F RTA20EU 19950922003911995092200391EU 1995 9 22 AALA950946 119950517A217020D102 COALESCER AIRBUS300 A300B4605R 3930308EU LT ACM CONTAMINATED A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0714053 420 MIA - FLT 1815 - AFTER TAKEOFF DURING CLIMB-OUT, ODOR NOTED IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RT COALESCER BAGS DUE TO LEFT BAG CONTAMINATED WITH HYDRAULIC FLUID. CLEANED HYDRAULIC FLUID RESIDUE FROM WHEEL WELL AREA. NO HYDRAULIC LEAKS NOTED. ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950922003921995092200392NM 1995 9 22 AALA951293 119950721A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07849AA 20990 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 24 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTORS BY PASSENGER SEAT ROW 7 AND PASSENGER SEAT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950922003931995092200393NM 1995 9 22 AALA951324 119950723A3350A3030398101 EEL CONNECTOR BOEING727 727227 1384078NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07723AA 20731 BWI - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS SECTION INOPERATIVE. RECONNECTED CONNECTOR AT FIRST CLASS GALLEY BULKHEAD, AND AT AFT END OF LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950922003941995092200394NM 1995 9 22 AALA951331 119950724A3350 EEL FEEDER BOEING727 727227 1384078NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07729AA 20736 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS TO COACH FEEDER INOPERATIVE. REPLACED FEEDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19950922003951995092200395NM 1995 9 22 AALA951357 119950731A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07618AA 24526 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING IN FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPAIRED BROKEN WIRING AT SIDEWALL IN FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950922003961995092200396NM 1995 9 22 AALA951375 119950806A3350A3060720101 EEL CONDUCTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07610AA 24486 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID GALLEY INOPERATIVE. REPLACED FLAT CONDUCTOR AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950922003971995092200397EU 1995 9 22 AALA951395 119950808A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0714065 508 JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEATS 15AB TO 21AB INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHTS FROM LIGHT TRACK TO WALL CONNECTOR BY PASSENGER SEAT 21AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950922003981995092200398NM 1995 9 22 AALA951405 119950810A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07360AA 24041 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 2B AND 7B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT ROW 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19950922003991995092200399NM 1995 9 22 AALA951424 119950815A3350A3060698101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07657AM 24615 BWI - FLT NR 2030 - DURING OVERNIGHT CHECK, EMEREGNCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 2 THROUGH 17 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 2. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19950922004001995092200400EU 1995 9 22 SIMA952351 119950823A33502012001 EEL POWER SUPPLY AEROSPATR72 ATR72212 EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT3362 733 263 CMH - FLT NR 4336 - FORWARD CABIN EMERGENCY EXIT SIGNS WON'T ILLUMINATE. REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950922004011995092200401NM 1995 9 22 TAOA089509 119950830A3350900835A EEL BATT PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 9228 20441 OVERHEAD EMERGENCY LIGHT AT ROW 16 INOP. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19950922004021995092200402NM 1995 9 22 TAOA089510 119950831A3350900835A EEL BATT PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 4791 22043 CEILING EMERGENCY EXIT LIGHT INOPERABLE AT ROW 4. REPLACED BATTERY PACK FOR CEILING EMERGENCY EXIT LIGHT AT ROW 4. OPS CHECKS OK. (M) 0 4 A3WE 19950922004031995092200403NM 1995 9 22 TWRA9553 119950902A35106350A34CCC OXYGEN BOTTLE BOEING747 747136 1384883NM FWD CARGO COMPT DEPLETED A TWRAA UNSCHED LANDING O OTHER TOTAKEOFF 1 EA15606FF 20273 AFTER TAKEOFF CREW OXYGEN WENT TO ZERO PSI. AIRCRAFT RETURNED TO GATE AT LAX. REPLACED OXYGEN BOTTLE. NO LEAKS FOUND AIRCRAFT DEPARTED. (M) 2L74 4F A20WE 19950922004041995092200404EU 1995 9 22 USAA950602 119950613A3230 ACTUATOR FOKKERF28 F28MK0100 4990807EU LT MLG OUT OF ADJUST A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19866US 11310 PIT - FLT 0753 - UPON GEAR RETRACTION, CREW RECEIVED AN INDICATION THAT THE RIGHT MAIN GEAR WAS NOT RETRACTED. FLIGHT RETURNED TO PIT. MAINTENANCE ADJUSTED THE DOWNLOCK ACTUATOR. (M) 2L72 4F RT 19950922004051995092200405EU 1995 9 22 USAA950896 119950813A2130 VALVE FOKKERF28 F28MK4000 4990810EU LEFT FAULTY A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19498US 11181 CLT - FLT NR 0690 - THE AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF. THE CAPTAIN DECIDED TO RETURN TO CLT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE AIR CONDITIONING S/O RELAY AND THE RATE CONTROL VALVE. (M) 2L72 4F RTA20EU 19950922004061995092200406NM 1995 9 22 USAA950904 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US18051 23886 CLT - DURING 'MQ-4' VISUAL CHECK INSPECTION, FOUND A 2 INCH BY 2 INCH CORRODED AREA LOCATED AT BS 344 BETWEEN BL 24 LT AND BL 8 RT. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED NEW 'T' CAP AND REPAIR ANGLES AND STRAPS AND FILTERS, REPAIRED BY SRM 53-10-03 AND SRM 51-70-13. (M) 2L72 4F RTA16WE 19950922004071995092200407NM 1995 9 22 USAA950905 119950730A5330 SKIN BOEING737 7373B7 1384580NM BS 294.5-328 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US 23319 CLT - DURING A Q-1 CHECK INSPECTION, FOUND A CRACK 14 INCHES BY 32 INCHES, BETWEEN STATION 294.5 AND 328, STRINGER 19R AND 22R. DOUBLER INSTALLED (PREVIOUS REPAIR). (M) 2L72 4F RTA16WE 19950922004081995092200408NM 1995 9 22 USAA950906 119950730A5330 SKIN BOEING737 7373B7 1384580NM BS 360-400 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US27459 23319 CLT - DURING A Q-1 CHECK INSPECTION, FOUND A 25 INCH BY 6.5 INCH CRACK (PREVIOUS REPAIR) LOCATED BETWEEN STATION 360 AND STATION 400, S-20R AND S-21R. DOUBLER INSTALLED (PREVIOUS REPAIR). 2L72 4F RTA16WE 19950922004091995092200409NM 1995 9 22 USAA950907 119950730A5330 SKIN BOEING737 7373B7 1384580NM BS 887-907 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19397US 23319 CLT - DURING A Q-1 CHECK INSPECTION, FOUND A 1 INCH SMALL HOLE (PREVIOUS REPAIR) BETWEEN STATION 887 TO STATION 907, 4 INCHES ABOVE S-22L. PATCH INSTALLED (PREVIOUS REPAIR). (M) 2L72 4F RTA16WE 19950922004101995092200410NM 1995 9 22 USAA950910 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US18051 23886 CLT - DURING 'MQ-4' VISUAL CHECK INSPECTION, FOUND NUMEROUS AREAS OF CORROSION AROUND FLOOR BOARD 17 INCHES ATTACH HOLES. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED NEW T-CAP, REPAIR ANGLES, STRAPS AND FILTERS. REPAIRED BY TRM 53-10-03 AND SRM 51-70-12. (M) 2L72 4F RTA16WE 19950922004111995092200411NM 1995 9 22 USAA950911 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US19507 23886 CLT - DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A 3.5 INCH CRACK ON STATION 520 EXTENDING 1.8 INCHES OUTBOARD AND 1.7 INCHES INBOARD OF LBL 45.5 OF FLOOR BEAM. INSTALLED REPAIR DOUBLERS, RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 39548. (M) 2L72 4F RTA16WE 19950922004121995092200412NM 1995 9 22 USAA950912 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US19507 23886 CLT- DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A 1.9 INCH CRACK ON STA 520 EXTENDING 1 INCH INBOARD AND .9 INCH OUTBOARD OF RBL 45.5 OF FLOOR BEAM. INSTALLED REPAIR DOUBLER AND RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 39548. (M) 2L72 4F RTA16WE 19950922004131995092200413NM 1995 9 22 USAA950913 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US19507 23886 CLT - DURING A Q-4 EDDY CURRENT CHECK, INSPECTION FOUND A .9 INCH CRACK ON STATION 520 EXTENDING OUTBOARD FROM LBL 24.75 OF FLOOR BEAM. INSTALLED REPAIR DOUBLERS, RADIUS FILLERS AND NEW VERTICAL ANGLE PER EA 34548. (M) 2L72 4F RTA16WE 19950922004141995092200414NM 1995 9 22 USAA950925 119950720A5313 STRINGER BOEING737 737201 1384454NM BS 947.5-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19225US42176 21667 INT - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND 4 INCH BY 2 INCH CORRODED AREA BETWEEN STATION 947.5 AND 967 AT S-26L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M) 2L72 4F A16WE 19950922004151995092200415NM 1995 9 22 USAA950926 119950720A5313 STRINGER BOEING737 737201 1384454NM BS 967-986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19225US42176 21667 INT - DURING 'CD-6' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BETWEEN STATION 967 AND 986.5 AT S-27L. INSTALLED REPAIR SPLICES. REPAIRED PER SRM 53-10-3. (M) 2L72 4F A16WE 19950922004161995092200416NM 1995 9 22 USAA950927 119950728A5313 STRINGER BOEING737 737201 1384454NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19237US38466 22353 ROA - DURING 'BX CHECK' VISUAL INSPECTION, FOUND 13 .125 INCH LONG STRINGER CORRODED FUSELAGE STATION 967 JUST TO THE LEFT OF WATER TANK. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIRED PER SRM 53-10-3 FIG 1 FUSELAGE STRINGER REPAIR S-14-28. (M) 2L72 4F A16WE 19950922004171995092200417NE 1995 9 22 USAA9509901 219950811A7230UL29556 FAN BLADES BOEING757 757225 1384959NM RROYCERB211 RB211535E43754555NE NR 1 ENGINE DAMAGED A USAAA UNSCHED LANDING C F.O.D. CRCRUISE 1 EA19618AU 22210 LAX - FLT NR 1898 - AT 131 KNOTS, A BIRD WAS INGESTED INTO THE NR 1 ENGINE CAUSING A LOSS OF POWER AND NOTICEABLE ENGINE VIBRATION. IT WAS DECIDED TO DIVERT TO LAX. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NR 19 AND NR 20 FAN BLADES. OPERATIONS CHECKED GOOD. (M) 2L72 4F4 FRTA2NM E12EU 19950922004181995092200418WP 1995 9 22 VTZA95267 219950824A73103986B000 FF CONTROL VLV BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP LT ENG FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27496UE 900 P66009 FLT NR 6379 - IAD-SYR - ABORTED THE TAKEOFF DUE TO THE LEFT ENGINE TORQUE AND EGT SPIKING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENACNE FOUND THE LEFT ENGINE FUEL FLOW STUCK IN THE ON POSITION. MAINTENANCE REPLACED THE FLOW CONTROL VALVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T3 TRTA56EU E3WE 19950922004191995092200419NM 1995 9 22 9514336310 119950908A7931 PRESSURE SWITCH BOEING747 747451 1384940NM PWA 4056 PW4056 NE NR 3 ENGINE MALFUNCTIONED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL N FALSE WARNING CLCLIMB 1 GL01670US 24225 717667 DURING CLIMB, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN, 130,000 LBS OF FUEL WAS DUMPED, THE AIRCRAFT DIVERTED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH AND OIL FILTER. OPERATIONAL CHECK OK. 2L74 4F4 FRTA20WE E24NE 19950922004201995092200420WP 1995 9 22 9514349931 119950916A7933 OIL TEMP SENSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL0190S 47244 657381 MSP - DURING CLIMBOUT, NR 2 ENGINE OIL TEMPERATURE INDICATION EXCEEDED RECOMMENDED LIMITS AND THEN BECAME UNSTABLE. FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TEMPERATURE SENSOR AND TIGHTENED LOOSE WIRING HARNESS GROUND CONNECTORS, FOUND ON THE TOP OF THE ENGINE. SYSTEM OPERATION WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A6WE E2EA 19950922004211995092200421WP 1995 9 22 9514359953 119950914A7332 FUEL PRESS SW DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK JN WARNING INDICATION FALSE WARNING TOTAKEOFF 1 GL01918RW 47158 666308 WHEN TAKEOFF POWER WAS APPLIED, THE NR 2 ENGINE INLET FUEL PRESSURE LOW WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE SYSTEM WAS PLACED ON MEL AND AIRCRAFT CONTINUED IN SERVICE. SUBSEQUENT REPLACEMENT OF THE LOW FUEL PRESSURE SWITCH CORRECTED SYSTEM DISCREPANCY. 2L72 4F4 F A6WE E2EA 19950922004221995092200422WP 1995 9 22 9514369921 119950918A3260 UNSAFE LIGHT DOUG DC9 DC932 3022066WP RT MLG ILLUMINATED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01943N 47647 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CLEANED, LUBED UPLATCH MECHANISMS, ADJUSTED DOOR ROLLER AND CYCLED GEAR NUMEROUS TIMES. ALL INDICATIONS CHECKED NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950922004231995092200423WP 1995 9 22 9514379970 119950913A3231 RETRACT MECH DOUG DC9 DC931 3022065WP RT MLG OUT OF ADJUST A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL019334 47247 HOU - RIGHT MAIN LANDING GEAR DOOR WAS OPEN AND SCRAPPED ON LANDING. THE GEAR DOOR OPEN LIGHT WAS NOT ILLUMINATED. FOUND RIGHT MAIN GEAR SEQUENCE PUSH/PULL TELESCOPING TUBE BINDING. REPLACED AND ADJUSTED SEQUENCE CABLE AND HOUSING, CLEANED ASSEMBLY. ALSO, REPLACED THE RIGHT MAIN GEAR DOOR SWITCH AND THE RIGHT MAIN GEAR DOOR, DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950922004241995092200424NM 1995 9 22 95FDEA01387 119950918A5343 AFT TRUNNION BOEING727 72725C 138400HNM FS 740 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 LEFT WING FRONT SPAR FORWARD TERMINAL PIN JOINT HOLE CRACKED AFT FORWARD. LEVELED AND SHORED A/C IAW SRM 51-50-1. CUT LOWER CHORD ANGLE AND WEB IAW BOEING DWG 65C29064. REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGLE IAW BOEING DWG 65C29064. 2L73 4F A3WE 19950922004251995092200425WP 1995 9 22 MWEA95309 119950913A5320 INTERCOSTAL DOUG DC9 DC914 3022034WP BS 642.6 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31700ME 45696 DURING INSPECTION, FOUND CRACKED INTERCOSTAL AT STA 642, 6 INCHES LEFT OF CENTERLINE AT FLOORBEAM LEVEL. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 53-01 PG 9 AND 53-01 FIG 2 SHEET 4. 2L72 4F A6WE 19950922004261995092200426WP 1995 9 22 MWEA95310 119950916A53209915565157 ANGLE DOUG DC9 DC932 3022066WP DOOR FRAME CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, FOUND 3 CRACKED FITTINGS ON AFT ENTRANCE DOOR FRAME, INTERNAL STRUCTURE. MAINTENANCE REMOVED AND REPLACED FITTINGS WITH NEW DOUGLAS PARTS IAW DAC DRAWING 9915565. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922004271995092200427WP 1995 9 22 MWEA95311 119950916A335060030431 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP FWD CABIN MALFUNCTIONED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, THE CABIN EMERGENCY LIGHTS OVER ROWS 1 THROUGH 14 WERE VERY DIM. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY FOR OVERHEAD EMERGENCY LIGHTS. OP CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922004281995092200428WP 1995 9 22 MWEA95312 119950918A5320591143278 ANGLE DOUG DC9 DC932 3022066WP BS 1075 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, FOUND FRAME ATTACH ANGLE CRACKED AT STA 1075, LONGERON 2R. MAINTENANCE REMOVED AND REPLACED ANGLE WITH DOUGLAS PART IAW SRM 53-01. 2L72 4F A6WE 19950922004291995092200429WP 1995 9 22 MWEA95313 119950918A53205911432877 ANGLE DOUG DC9 DC932 3022066WP BS 1076 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, THE ATTACH ANGLE AT STA 1076 LONGERON 2L WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE WITH DOUGLAS PART IAW SRM 53-01. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922004301995092200430WP 1995 9 22 MWEA95314 119950918A5311S2777930 FRAME DOUG DC9 DC932 3022066WP BS 1076 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING C-CHECK, FOUND FRAME CRACKED IN 2 PLACES AT FUS STA 1076, LONGERON 2 LT AND 2 RT. MAINTENANCE SPLICED IN NEW SECTION OF FRAME IAW SRM 53-02 FIG 32. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922004311995092200431WP 1995 9 22 MWEA95315 119950918A5754 SKIN DOUG DC9 DC932 3022066WP NR 1 LE SLAT PUNCTURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31204ME 47680 DURING INSPECTION, THE RT NR 1 SLAT RECEIVED A 2 INCH DIAMETER PUNCTURE HOLE, WHEN INADVERTENTLY STRIKING WORK STAND. MAINTENANCE INSTALLED 30 DAY TEMPORARY PATCH REPAIR IAW DOUGLAS APPROVAL AND SRM 57-09 FIG 10A. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19950922004321995092200432NM 1995 9 22 SCNA95188 119950917A3350582214 EEL POWER SUPPLY BOEING727 727282 2F0R NM CABIN MALFUNCTIONED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE LEFT AFT TRACK LIGHTING WAS FOUND TO BE DIM WHEN CHECKED. REMOVED AND REPLACED POWER SUPPLY M9204 AND PERFORMED OPERATIONAL TEST IAW MM 33-50-01 PAGE 501, LIGHTS CHECKED GOOD. 2L73 4F RTA3WE 19950922004331995092200433NM 1995 9 22 SCNA95189 119950917A33501000677 EEL BOEING727 727225 1384077NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 22559 THE L-1 PORTABLE EMERGENCY EXIT LIGHT REMAINED ON WHEN SWITCH TURNED TO OFF POSITION. REMOVED AND REPLACED L-1 PORTABLE EMERGENCY EXIT LIGHT PER MM 33-50-101, LIGHT TESTED GOOD. 2L73 4F A3WE 19950922004381995092200438SW 1995 9 22 95ZZZX5052 119950828A6720 BOOT BELL 206 206L4 1182110SW T/R PC GRBOX AIR BOUND A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH 52076 WHEN APPLYING PRESSURE TO TAIL ROTOR PEDALS, IT BOUNCES BACK BY ITSELF (FEEDBACK). THE TAIL ROTOR GEARBOX PITCH CHANGE MECHANISM PROTECTIVE BOOT BECOMES AIR BOUND. RELIEVED AIR PRESSURE IN BOOT. 1G71 3U NCH2SW 19950922004391995092200439SW 1995 9 22 95ZZZX5053 119950823A2510 BELT BELL 206 206L4 1182110SW SEAT EXCESS WEAR A NYBAK NONE O OTHER ININSP/MAINT 1 EA11123NH 52076 EXCESSIVE WEAR, BELTS APPEAR TO BE INSTALLED INCORRECTLY. DURING PROLONGED USE OF SEAT BELTS, THE INERTIA REEL TENDS TO FOLD THE SEAT BELT, THEN, INADVERTENTLY, ROTATING THE BELT. REMOVED BELT AND REINSTALLED NEW BELT. 1G71 3U NCH2SW 19950922004881995092200488WP 1995 9 22 ORJA9534 119950515A5101 AIRFRAME DOUG DC9 DC987 3022087WP STRUCTURE BIRD STRIKE A ORJAO OTHER C F.O.D. TOTAKEOFF 1 WP11750RA 49777 ON TAKEOFF, ACFT SUFFERED A BIRD STRIKE. C/W BIRD STRIKE INSPECTION PER MM 05-51-08 PG 601 REF CC1, NR 4 AND NR 5. NO OTHER DEFECTS NOTED. (X) 2L72 4F RTA6WE 19950922004891995092200489 1995 9 22 9514382716 419950919A22102588880901 COUPLER BOEING727 7272S7 138407ZNM LWR YAW DAMPER FAILED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01720RC3202810835 22491 DURING CLIMBOUT IN CLEAN CONFIGURATION, FLIGHT CONTROLS FELT HEAVY WITH INTERMITTENT VIBRATION IN RUDDER PEDALS. VIBRATION NOT ASSOCIATED WITH ENGINES OR AIRSPEED (230-310 KIAS). AT APPROACH SPEEDS NO NOTICEABLE VIBRATION, FLIGHT RETURNED TO TPA WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL FLIGHT CONTROLS AND ENGINES WITH NO FINDINGS. PERFORMED BITE CHECK ON LOWER YAW DAMPER COUPLER AND UNIT FAILED. REPLACED LOWER YAW DAMPER COUPLER. 2L73 4F A3WE 19950922004901995092200490WP 1995 9 22 95FDEA01393 119950909A5400AUB1031503 SPAR WEB DOUG DC10 DC1030F 3023504WP NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 NR 1 ENG PYLON UPPER SPAR WEB CRACKED AT OUTBOARD CORNER (APPROX 5). REMOVED AND REPLACED SPAR WEB. REPAIRED PER EA 8-5410-20129. REPLACED NR 1 PYLON AFT BULKHEAD FITTING AND REPAIRED UPPER WEB. SEE EA FOR DETAILS. 2L73 4F RTA22WE 19950922004911995092200491NM 1995 9 22 95FDEA01394 119950919A531365C2553357 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 NR 0398 (PATTERN CARD 72C235-02) CRACK IN STR 15L AT FASTENER. FORWARD SIDE OF ICE LIGHT BETWEEN FUSELAGE STA 720B - 720C. STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-10-3, FIG 2. 2L73 4F A3WE 19950922004921995092200492NM 1995 9 22 95FDEA01395 119950919A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CORROSION ON TOP OF UPPER LOBE FLOOR BEAM STA 344, RBL 2-6. 2L73 4F A3WE 19950922004931995092200493NM 1995 9 22 95FDEA01396 119950915A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 STR 9R HAD HOLE AND CRACK AND ONE FAST HOLE WITH EXISTING MISDRILL CAUSED DAMAGE IN FUSELAGE SKIN (A/C CAME IN WITH THIS COND). STR DAMAGE AND FUSELAGE SKIN DAMAGE WAS CUT OUT AND STR SPLICE 9 .050 INCH DOUBLER ON SKIN WAS INSTALLED, PER SRM 53-30-3, FIG 9, NR 0224. 2L73 4F A3WE 19950922004941995092200494NM 1995 9 22 95FDEA01397 119950918A5541 RIB BOEING727 72725C 138400HNM RUDDER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UPPER RUDDER THRUST HINGE, LOWER LT SIDE. RIB IS CRACKED BETWEEN FASTENERS. REMOVED 6 EACH FASTENERS - HFEC CHECKED. VERIFIED CRACK FROM HOLE-TO-HOLE, AFT ROW. INSTALLED DOUBLER PER FEDEX EA 7-5510-25773 DATED 9-15-95. PAINTED ALL AREAS EFFECTED FOR WATER-TIGHT SEAL. 2L73 4F A3WE 19950922004951995092200495NM 1995 9 22 95FDEA01398 119950919A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 420 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 ON NR 0234, CORROSION ON FLOOR BEAM IN MAIN CARGO STA 420 RBL 20. CORROSION REMOVED BEYOND LIMITS. CUT OUT AREA AND INSTALLED .090 INCH DOUBLERS AND FILLER PER SRM 53-11-8, FIG 8. 2L73 4F A3WE 19950922004961995092200496NM 1995 9 22 95FDEA01399 119950919A2612 FIRE LOOP DOUG MD11 MD11F 3023600NM NR 2 ENGINE MALFUNCTIONED A FDEAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 SO25607FE 48547 DEPARTING 10,000 MSL, NR 2 ENG FIRE ALERT SOUNDED. AS THROTTLE NR 2 WAS RETARDED TO IDLE, THE FIRE INDICATOR WENT OUT. LEFT NR 2 ENG IN IDLE, FIRE ALERT DID NOT RECUR. RETURNED TO ANC. PLACED ALUMINUM FOIL ON DUCT CLAMPS FOR POWER RUN. FOUND SOME OF THE CLAMPS LOOSE. TIGHTEN AND LEAK CHECKED. TROUBLESHOT PER FIM MANUAL 26-11-00. REMOVED AND REPLACED LOOP HARNESS P/N 4220812-000 AND FIRE DETECTOR LOOP P/N 224-9741-511. REMOVED AND REPLACED LOOP 'B' HARNESS P/N 420811-000. REMOVED AND REPLACED HARNESS P/N 420584-0000. REMOVED AND REPLACED LOWER TURBINE FIRE DETECTOR P/N 224-9742-505. RAN ENG AGAIN, OK FOR SERVICE. 2L73 4F RTA22WE 19950922004971995092200497WP 1995 9 22 95FDEA1392 119950905A5412AUB70251115 BULKHEAD DOUG DC10 DC1030F 3023504WP NR 1 PYLON CRACKED A AFDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 NR 1 PYLON AFT SPHERICAL BEARING SUPPORT BULKHEAD, YN 417.212, HAS A 10 INCH CRACK AT INBOARD INSIDE RADIUS. CRACK WAS DISCOVERED BY AN INSPECTOR WHILE PERFORMING THE SB 54-74 INSPECTION. THE NR 3 PYLON WAS ALSO INSPECTED AND NO CRACKING WAS EVIDENT. CRACK APPEARS TO HAVE ORIGINATED AT ZN 55.692 AND PROPAGATED DOWNWARDS TO ZN 44.705. REMOVED AND REPLACED THE BULKHEAD PER EA 8-5410-20129. (NOTE: THIS IS THE FINAL C/A). 2L73 4F RTA22WE 19950922004981995092200498NM 1995 9 22 DL72S953729 119950918A5754 RIB BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND ON HMV RIB WEB AT TAI, TUBE CRACKED AT NR 6 SLAT INBOARD WEB. REPAIRED RIB PER M/M 57-54-0, FIG 805. 2L73 4F A3WE 19950922004991995092200499NM 1995 9 22 DL72S953730 119950918A5754 ACTUATOR MOUNT BOEING727 727232 1384082NM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND AT HMV, NR 4 SLAT MAIN ACTUATOR MOUNT CRACKED AT PREVIOUSLY REPAIRED AREA. REPAIRED PER M/M 57-54-0, FIG 804A. 2L73 4F A3WE 19950922005001995092200500NM 1995 9 22 DL72S953740 119950906A5753652163384A SKIN BOEING727 727232 1384082NM NR 4 TE MIDFLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING SHOP INSPECTION, NR 4 MID-FLAP WAS FOUND WITH WEAR DAMAGE TO LEADING EDGE SKIN, AT THE OUTBOARD 9 OF FLAP. REPAIRED PER MM 57-52-0, FIG 803. 2L73 4F A3WE 19950922005011995092200501NM 1995 9 22 DL72S953744 119950909A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND DURING HMV, NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED CRACK PER M/M 57-54-0, FIG 812. 2L73 4F A3WE 19950922005021995092200502NM 1995 9 22 DL72S953745 119950909A5754 RIB BOEING727 727232 1384082NM NR 8 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND DURING HMV - NR 8 SLAT NR 13 RIB IS CRACKED IN RADIUS. FABRICATED REPAIR PER M/M 57-54-0, FIG 805. 2L73 4F A3WE 19950922005031995092200503NM 1995 9 22 DL72S953748 119950918A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND DURING HMV - NR 6 SLAT, CRACKED ANGLE BETWEEN DE-ICE TUBE AND FARTHEST ROLLER TRACK. REPAIRED PER M/M 57-54-0, FIG 812. 2L73 4F A3WE 19950922005041995092200504NM 1995 9 22 DL72S953751 119950919A3350 EEL 1000677 BOEING727 727232 1384082NM COCKPIT INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11490DA 3874 21020 COCKPIT EMERGENCY LIGHT INOP. REPLACED RACK, OPS NORMAL. 2L73 4F A3WE 19950922005051995092200505NM 1995 9 22 DL72S953752 119950919A3350 EEL 900542 BOEING727 727232 1384082NM CARGO DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11490DA UNKNOWN 21020 EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. NEEDS RACK M957 FWD TO MCO AND PLAC. REPLACED RACK, OPERATION NORMAL. 2L73 4F A3WE 19950922005061995092200506NM 1995 9 22 DL72S953754 119950619A5753652163262 PANEL BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 THE INBOARD AFT PUSHROD CUT-OUT HAS A CRACK AT INBOARD AFT CORNER. REPAIRED PER M/M 57-52-0, PAGE 819. FOR NR 3 MID-FLAP PANEL DURING SHOP INSPECTION. 2L73 4F A3WE 19950922005071995092200507NM 1995 9 22 DL73S953736 119950916A57546546423280AK SKIN BOEING737 737232 1384475NM NR 4 LE FLAP DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11305DL 23077 DURING SHOP INSPECTION, NR 4 LEADING EDGE SLAT WAS FOUND WITH DENT TO LEADING EDGE SKIN AT 10 FROM THE OUTBOARD END, REPAIRED PER SRM 57-50-3, FIG 1. 2L72 4F RTA16WE 19950922005081995092200508NM 1995 9 22 DL767953734 119950918A3350 EEL 1317 BOEING767 767232 1385132NM OVERWING INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11104DA 22216 AFT LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED AFT LEFT OVERWING EMERGENCY LIGHT. LIGHT OPS CHECK NORMAL. 2L72 4F RTA1NM 19950922005091995092200509NM 1995 9 22 DL76L953732 119950919A3350344003361 EEL BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11182DN 25987 EMERGENCY FLOOR TRACK LIGHT TO SEAT 20F INOP. REPAIRED WIRING AND REPLACED BULB. OPS NOW NORMAL. 2L72 4F RTA1NM 19950922005101995092200510WP 1995 9 22 DLL10953714 119950916A3350201314 EEL BATTERY PACK LKHEED1011 10113851 5265010WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11733DS 193C1224 ON LAYOVER, FOUND FWD CABIN EMERGENCY EXIT PATH LIGHTS FAILED TEST. REPLACED BATTERY AND POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19950922005111995092200511WP 1995 9 22 DLL17953737 119950919A5753 SKIN LKHEED1011 10113853 5265020WP NR1 TE FLAP VANECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 AT HMV, LEFT WING NR 1 FLAP VANE WAS FOUND WITH UPPER SKIN CRACKED ALONG A RIB AT 40 INCHES FROM INBD END. REPAIRED PER SRM 57-53-00. 2L73 4F A23WE 19950922005121995092200512WP 1995 9 22 DLL17953738 119950919A5753 SKIN LKHEED1011 10113853 5265020WP NR1 TE FLAP VANEDAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH HEAVY WEAR DAMAGE TO OUTER SKIN AT THE INBD END OF VANE. REPAIRED PER SRM 57-53-00, FIG 805. 2L73 4F A23WE 19950922005131995092200513WP 1995 9 22 DLL17953739 119950919A5753 SKIN LKHEED1011 10113853 5265020WP NR1 TE FLAP VANEDENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 AT HMV, LT WING NR 1 FLAP VANE WAS FOUND WITH DENTED SKIN ON INNER SKIN PANEL. INSTALLED REPAIR DOUBLERS PER SRM 51-50-01. 2L73 4F A23WE 19950922005141995092200514NM 1995 9 22 DLM88953728 119950918A2910AS15308254 HOSE DOUG MD88 MD88 3023688NM RT HYD SYST LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11904DL 49535 060294 LOST RT HYD SYS OTY THEN PRESSURE AFTER FLAPS WERE RETRACTED ON TAKEOFF. RETURNED TO ATL. GEAR WAS EXTENDED USING ALT EXTEND. REPLACED RT SYSTEM FILTER MODULE PRESSURE LINE. LEAK CKS GOOD, DL/PN 299201294. 2L72 4F RTA6WE 19950922005151995092200515NM 1995 9 22 DLM88953747 119950919A33200200956006 SOCKET DOUG MD88 MD88 3023688NM CABIN FAILED A DALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11956DL 49887 AN ELECTRICAL BURNING ODOR REPORTED BY PASSENGER AND F/A S BETWEEN ROWS 20-27. FOUND SIDEWALL LIGHT BALLAST SOCKETS AT ROW 23DE BURNED. DEACTIVATED LIGHT FOR RETURN TO SERVICE, SOCKETS WERE REPLACED. 2L72 4F RTA6WE 19950922005161995092200516NM 1995 9 22 P5CA9500773 119950921A2710DL1326M119 ACTUATOR BOEING747 747122 1384872NM RT AILERON FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23850FT 19755 OFF BLOCKS ON FLIGHT CONTROL CHECK RIGHT OUTBOARD AILERON LOCKED OUT WITH FLAPS DOWN. REPLACED AILERON LOCK-OUT ACTUATOR. 2L74 4F A20WE 19950922005171995092200517NM 1995 9 22 P5CA9500774 119950920A5350 FAIRING BOEING747 747122 1384872NM BS 1239 BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 LEFT LOWER WING TO BODY FAIRING 191KL BROKEN AND DELAMINATED. APPROX STATION 1239 AFT UPPER CORNER. REPAIRED AREA I/A/W SRM 51-40-15. 2L74 4F A20WE 19950922005181995092200518NM 1995 9 22 UPS204457 119950920A5720 ANGLE BOEING727 727185C 138406NNM NR 3 SKATE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE NR 3 SKATE ANGLE IN 2 PLACES ON INBOARD SIDE. MAINTENANCE STOP DRILLED THE CRACK NDI VERIFIED AND INSTALLED DOUBLER IAW SRM 51-40-2. 2L73 4F A3WE 19950922005191995092200519NM 1995 9 22 UPS204458 119950920A5320 FITTING BOEING727 727185C 138406NNM BS 870 PITTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND THE AILERON PCU MOUNT FITTING PITTED AT THE ATTACH POINTS AND CONTROL LINKAGES. MAINTENANCE REMOVED THE DAMAGED FITTING, INSTALLED NEW FITTING ONTO AIRCRAFT AND INSTALLED CABLES AND TORQUE TUBES PER MM 27-10-91. 2L73 4F A3WE 19950922005201995092200520NM 1995 9 22 UPS204459 119950920A5755 SKIN BOEING727 727185C 138406NNM NR 5 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE NR 5 SPOILER AT THE FORWARD OUTBOARD CORNER ON BOTH UPPER AND LOWER SKINS. MAINTENANCE REPLACED SPOILER IAW UPS NRC 364863. 2L73 4F A3WE 19950922005211995092200521NM 1995 9 22 UPS204460 119950920A5210 GATE BEAM BOEING727 727185C 138406NNM PAX DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR LOWER GATE BEAM AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE CRACKED LOWER GATE BEAM AND SECURED WITH FASTENERS IAW SRM 51-30-2 AND SRM 51-10-1. 2L73 4F A3WE 19950922005221995092200522NM 1995 9 22 UPS204461 119950920A5753 TE WEDGE BOEING727 727185C 138406NNM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE OF THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE LEFT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6. 2L73 4F A3WE 19950922005231995092200523NM 1995 9 22 UPS204462 119950920A5753 TE WEDGE BOEING727 727185C 138406NNM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED SKIN ON THE UPPER AND LOWER SKINS, FINAL REPAIRS PER SRM 51-40-6. 2L73 4F A3WE 19950922005241995092200524NM 1995 9 22 UPS204463 119950920A5753 TE WEDGE BOEING727 727185C 138406NNM RT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REPAIRED THE RIGHT WING INBOARD MID-FLAP TRAILING EDGE WEDGE IAW SRM 51-40-6. 2L73 4F A3WE 19950922005251995092200525NM 1995 9 22 UPS204464 119950920A5753 TE WEDGE BOEING727 727185C 138406NNM RT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SKIN ON THE RIGHT WING OUTBOARD MID-FLAP TRAILING EDGE WEDGE. MAINTENANCE REMOVED THE DAMAGED AREA, CLEANED AND REPAIRED AREA PER SRM 51-40-6. 2L73 4F A3WE 19950922005261995092200526NM 1995 9 22 UPS204465 119950920A5753 SKIN BOEING727 727185C 138406NNM LT TE FOREFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE UPPER SURFACE AND LOWER SURFACE OF THE LEFT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE UPPER AND LOWER SURFACES OF THE LEFT WING INBOARD FORE FLAP IAW SRM 51-40-6. 2L73 4F A3WE 19950922005271995092200527NM 1995 9 22 UPS204466 119950920A5312 DOUBLER BOEING727 727185C 138406NNM BS 875 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE ACCESS PANEL DOUBLER AT STATION 875, LBL 55 AND WL 165. MAINTENANCE REMOVED THE CORRODED DOUBLER, FABRICATED A NEW DOUBLER, AND INSTALLED PER SRM 51-10-2, 51-30-5 AND 51-30-2. 2L73 4F A3WE 19950922005281995092200528NM 1995 9 22 UPS204467 119950920A5320 CHORD BOEING727 727185C 138406NNM BS 294.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT MID-CHORD AT STATION 294.5 - 312, LBL 15 AND WL 170. MAINTENANCE REMOVED CORROSION BEYOND LIMITS, REMOVED AND REPLACED THE CHORD, FINAL INSTALLATION PER SRM 51-30-2, 53-10-1 AND 56-40-00. 2L73 4F A3WE 19950922005291995092200529NM 1995 9 22 UPS204468 119950920A5753 TE WEDGE BOEING727 727185C 138406NNM RT TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN C-CHECK, MAINTENANCE FOUND DELAMINATION ON THE LOWER SURFACE OF THE RIGHT WING OUTBOARD FORE FLAP. MAINTENANCE REMOVED THE CORROSION AND TRAILING EDGE WEDGE, REPAIRED THE CORE AND INSTALLED NEW WEDGE PER SRM 51-40-6. 2L73 4F A3WE 19950922005301995092200530NM 1995 9 22 UPS204469 119950920A5320 INTERCOSTAL BOEING727 727108C 1384039NM BS 803 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND THE NUT PLATES AT STATION 803, RBL 6 AND WL 148. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRM 53-10-1, 51-10-6 AND 51-30-2. 2L73 4F A3WE 19950922005311995092200531NM 1995 9 22 UPS204470 119950920A5320 CHORD BOEING727 727108C 1384039NM BS 334 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 334 AND 335 AND LBL 14.5. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2. 53-10-1 AND MM 51-20-4. 2L73 4F A3WE 19950922005321995092200532NM 1995 9 22 UPS204471 119950920A5320 CHORD BOEING727 727108C 1384039NM BS 324 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER NOSE CHORD AT STATION 324, 340, 346, RBL 14.5 AND WL 166. MAINTENANCE REPLACED THE CHORD IAW SRM 51-10-2, 51-10-6, 51-30-2, 53-10-1 AND 51-20-4. 2L73 4F A3WE 19950922005331995092200533NM 1995 9 22 UPS204472 119950920A5313 STRINGER BOEING727 727108C 1384039NM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 7L STATION 1110 - 1176. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. 2L73 4F A3WE 19950922005341995092200534NM 1995 9 22 UPS204473 119950920A5313 STRINGER BOEING727 727108C 1384039NM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4R AT STATION 1110 - 1180. MAINTENANCE REMOVED THE DAMAGED AREA, FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-2, 51-10-6, 53-10-3, 51-30-2. 2L73 4F A3WE 19950922005351995092200535NM 1995 9 22 UPS204474 119950920A5313 STRINGER BOEING727 727108C 1384039NM BS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5L AND STATION 1130 - 1180. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED PER SRM 53-10-3, 53-10-2, 51-30-3, 51-10-2 AND 51-10-6. 2L73 4F A3WE 19950922005361995092200536NM 1995 9 22 UPS204475 119950920A5753 SKIN BOEING727 727108C 1384039NM TR TE FORE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DELAMINATION ON UPPER SURFACE RUB STRIP OF THE RIGHT WING INBOARD FORE FLAP. MAINTENANCE REPAIRED THE DAMAGED AREA IAW SRM 51-40-6. 2L73 4F A3WE 19950922005371995092200537NM 1995 9 22 UPS204476 119950920A5510 STIFFENER BOEING727 727108C 1384039NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT INBOARD CLOSURE WEB INSIDE ACCESS PANEL 9205 AREA AT UPPER END OF WEB WHERE AFT INTERSPAR WEB ATTACHING BRACKET IS MOUNTED. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1. 2L73 4F A3WE 19950922005381995092200538NM 1995 9 22 UPS204477 119950920A5510 STIFFENER BOEING727 727108C 1384039NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HORIZONTAL STABILIZER AFT INTERSPAR WEB INBOARD ATTACHING BRACKET INSIDE ACCESS PANEL AREA 9206. MAINTENANCE FABRICATED NEW STIFFENER AND INSTALLED IAW SRM 51-30-2 AND 55-10-1. 2L73 4F A3WE 19950922005391995092200539NM 1995 9 22 UPS204478 119950920A5510 STIFFENER BOEING727 727108C 1384039NM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK ON THE LEFT HORIZONTAL STABLIZER WEB STIFFENER AT STATION 54 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2. 2L73 4F A3WE 19950922005401995092200540NM 1995 9 22 UPS204479 119950920A5510 STIFFENER BOEING727 727108C 1384039NM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 64 ON THE UPPER SIDE OF STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW PER SRM 57-30-2. 2L73 4F A3WE 19950922005411995092200541NM 1995 9 22 UPS204480 119950920A5510 STIFFENER BOEING727 727108C 1384039NM HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE LEFT HORIZONTAL STABILIZER WEB STIFFENER AT STAB STATION 73 ON THE UPPER SIDE OF THE STIFFENER. MAINTENANCE REMOVED THE CRACKED STIFFENER AND REPLACED WITH NEW IAW SRM 57-30-2. 2L73 4F A3WE 19950922005421995092200542NM 1995 9 22 UPS204481 119950920A5754 RIB BOEING727 727108C 1384039NM NR 6 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE RIB OF THE NR 6 SLAT ATTACH ROD END ATTACH POINT. MAINTENANCE REMOVED THE CRACKED RIB AND REPLACED WITH A NEW RIB IAW SRM 51-30-2, 51-30-8 AND 51-30-5. 2L73 4F A3WE 19950922005431995092200543NM 1995 9 22 UPS204483 119950920A5711 SPAR WEB BOEING727 727108C 1384039NM LT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT WING FRONT SPAR CENTER TANK ACCESS DOOR CUTOUT ON THE OUTER SURFACE. MAINTENANCE REMOVED THE DAMAGED AREA, REPAIRED AND INSTALLED PER SRM 57-30-3 AND UPS EO 727-57-1630. 2L73 4F A3WE 19950922005441995092200544NM 1995 9 22 UPS204484 119950920A5320 SPLICE BOEING727 727108C 1384039NM BS 380 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE TOP OF FRAME AT STATION 380 AND STRINGER 26R - 25R. MAINTENANCE REPLACED THE FRAME SPLICE IAW SRM 53-10-1, 53-10- 2 AND 51-10-6. 2L73 4F A3WE 19950922005451995092200545NM 1995 9 22 UPS204485 119950920A5313 STRINGER BOEING727 727108C 1384039NM BS 294.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 16 AT STATION 294.5, LBL 59 AND WL 217. MAINTENANCE REMOVED AND REPLACED PART OF THE STRINGER IAW UPS EO B727-5310-1259F. 2L73 4F A3WE 19950922005461995092200546NM 1995 9 22 UPS204486 119950920A5315 FLOOR BEAM BOEING727 727108C 1384039NM BS 500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AROUND THE NUTPLATE HOLE FORWARD LOWER SIDE OF THE UPPER CHORD ON THE FLOOR BEAM AT STATION 500, LBL 55 - 57 AND WL 208. MAINTENANCE REPAIRED THE FLOOR BEAM IAW SRM 53-10-8. 2L73 4F A3WE 19950922005471995092200547NM 1995 9 22 UPS204487 119950920A5510 BEAM BOEING727 727108C 1384039NM HORIZ STAB TE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LEFT HORIZONTAL TRAILING EDGE BEAM EXTERIOR SURFACE AT STAB STATION 225.54 AND 182.5. MAINTENANCE CUTOUT THE DAMAGED SECTION AND SPLICED IN NEW SECTION IAW SRM 55-10-6. 2L73 4F A3WE 19950922005481995092200548NM 1995 9 22 UPS204489 119950920A5313 STRINGERS BOEING727 727108C 1384039NM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN VARIOUS SPOTS ON STRINGER 5, 6, 7, 8 AT STATION 277 - 294, LBL 29 - 47 AND WL 268 - 287. MAINTENANCE REPLACED STRINGERS 7 AND 8L ON UPS EO 5310-1259F, STRINGERS 5 AND 6L WERE REMOVED AND REPLACED IAW SRM. 2L73 4F A3WE 19950922005491995092200549NM 1995 9 22 UPS504490 119950918A3260 BULB BOEING757 75724APF 1384969NM LT MLG FAILED A IPXAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO01432UP 25463 PILOT REPORTED ON APPROACH TO RUNWAY 27 AT SAN ON GEAR DOWN LANDING CHECKLIST COMMAND, THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. AIRCRAFT MISSED THE APPROACH AND VECTORED TO RUN GEAR DISAGREE CHECKLIST. NNC PAGE NR 63. RAN CHECKLIST, NO INDICATION CHANGE, DIVERTED AFTER TALKING TO FLIGHT OPS AND MMOC - BACK TO KONT. FLEW LOW PASS TO CONFIRM GEAR INDICATION. DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE FOUND 2 EACH BURNED OUT 387 BULBS IN LEFT MAIN LANDING GEAR DOWN INDICATOR, LIGHT CHECK SYSTEM OPERATES NORMAL. 2L72 4F RTA2NM 19950922005501995092200550WP 1995 9 22 UPS804455 119950920A5311 FRAME DOUG DC8 DC873F 302199FWP BS 62 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FRAME AT STATION 62 BETWEEN LONGERONS 17L - 21L. MAINTENANCE REPLACED FRAME PER SRM 51-1-20D. 2L74 4F RT4A25 19950922005511995092200551WP 1995 9 22 UPS804456 119950920A5320 FITTING DOUG DC8 DC873F 302199FWP BS 52 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE END FITTING AT STATION 52 AND LONGERON 8L. MAINTENANCE REPLACED THE FITTING PER SRM 51-1-21. 2L74 4F RT4A25 19950922005521995092200552EU 1995 9 22 WWMA9500063 119950914A32507805106 UNIVERSAL JOINT SAAB SF340 340B 7860101EU NLG STEERING FAILED A WWMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP15338SB 340B338 DURING TAXI, THE NOSE WHEEL STEERING BECAME INEFFECTIVE IN A TURN TO THE LEFT. UPON INVESTIGATION, MAINTENANCE FOUND STEERING UNIVERSAL JOINT IN GEARBOX (LEFT SIDE COCKPIT SIDE PANEL) FAILED. REMOVED AND REPLACED BOTH UNIVERSAL JOINTS ON STEERING LINK IAW AMM 32-50-10. AIRCRAFT TAXI CHECK GOOD. THIS IS THE THIRD OCCURRENCE OF THIS PART FAILURE IN THE PAST MONTH, ALL ON DIFFERENT AIRCRAFT. 2L72 4T RTA52EU 19950922005531995092200553EU 1995 9 22 WWMA9500064 119950914A3240AC66868 BRAKE VALVE BAG JETSTMJETSTM3201 1500217EU LT MLG DEFECTIVE A WWMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP15962AE 962 FOOT BRAKES REQUIRE MAXIMUM PRESSURE (STANDING ON THEM TO GET 1500-1600 PSI ON BRAKE PRESSURE GAUGE). BRAKES WILL NOT HOLD AIRCRAFT AT TAKEOFF POWER AND REQUIRE EXCESSIVE PEDAL APPLICATION TO GET BRAKE PRESSURE. UPON INVESIAGATION, MAINTENANCE REPLACED THE LEFT BRAKE ASSEMBLY AND PRESSURE REDUCING VALVE IAW AMM 32-40-17. AIRCRAFT TAXI CHECK GOOD. NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19950922005661995092200566SO 1995 9 22 95ZZZX5114 119950828A52804205907 HINGE PIPER PA31 PA31310 7103103SO MLG DOOR CRACKED A JIKAK NONE O OTHER ININSP/MAINT 1 WP017434L 31822 LEFT MAIN GEAR OUTBOARD DOOR'S FORWARD HINGE WAS FOUND CRACKED IN THE RADIUS DURING A STANDARD INSPECTION. AN AD AND SUBSEQUENT DEFECTS HAVE BEEN NOTED ON THE INBOARD GEAR DOOR HINGES, BUT THIS IS THE FIRST CRACKED OUTBOARD DOOR HINGE FOUND BY THIS OPERATOR. 1L71 3O RTA20SO 19950922005781995092200578CE 1995 9 22 95ZZZX5126 119950828A32305143122 UPLOCK HOOK CESSNA402 402C 207590RCE LT MLG WELL CRACKED A SQFAK NONE O OTHER ININSP/MAINT 1 SO175736C 402C0031 PILOT REPORTED GEAR WOULD NOT STAY IN UP POSITION. IN INSPECTION, FOUND LEFT MAIN GEAR UPLOCK HOOK CRACKED. 1L72 3O A7CE 19950929000031995092900003NE 1995 9 29 9514392255 219950920A7261 OIL FILTER BOEING727 727251 138408HNM PWA JT8 JT8D7B 52053NE NR 1 ENGINE DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01255US 19974 655396 NR 1 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL FILTER, AIRCRAFT WAS RUNUP AND SYSTEM CHECKED OK. 2L73 4F4 F A3WE E2EA 19950929000041995092900004NM 1995 9 29 95FDEA01400 119950921A5320BAC1498152 SPLICE BOEING727 727232 1384082NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION (71C209-02), ON STR SPLICE BS 680 STR 27R WL 148. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STR SPLICE AT BS 680 STR 27R WL 148 IAW SRM 53-10-1. 2L73 4F A3WE 19950929000051995092900005NM 1995 9 29 95FDEA01401 119950921A5315BAC14902885 FLOORBEAM BOEING727 72722 1384002NM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (72C235-02), AROUND FASTENER HOLE ON BS 660 FLOORBEAM RBL 19 WL 208. REMOVED DAMAGE AT BS 660 FLOORBEAM RBL 19 WL 208 AND INSTALLED REPAIR PER FEDEX SRM 53-10-08 FIG 8. REMOVED .046 MATERIAL FROM ORIGINAL .125 THICKNESS FLANGE, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 57-10-01. 2L73 4F A3WE 19950929000061995092900006NM 1995 9 29 95FDEA01402 119950921A53302024T3 SKIN BOEING727 72725 1384006NM BS 910 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 LIGHTNING STRIKE STA 910 BETWEEN STR 1 TO 2L. SKIN AND TEAR STRAP DAMAGE WAS BEYOND REPAIRABLE LIMITS PER FEDEX SRM 53-30-1. INSTALLED SKIN AND TEAR STRAP REPAIR IAW FEDEX SRM 53-30-3 AND 53-30-4 BS 910 BETWEEN STR 1 TO 2L. 2L73 4F A3WE 19950929000071995092900007NM 1995 9 29 95FDEA01403 119950921A5311 FRAME BOEING727 72725 1384006NM BS 312 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CRACK IN FRAME EMANATING FROM TOOLING HOLE AT BS 312 LBL 47 WL 175. REMOVED CRACKED FRAME AT BS 312 LBL 47 WL 175. RELEVELED NEW FRAME, DRILLED, ALODINED, PRIMED AND INSTALLED PER FEDEX SRM 51-20-1, 51-10-02, 51-30-02. 2L73 4F A3WE 19950929000081995092900008NM 1995 9 29 95FDEA01404 119950920A532066118096 CLIP BOEING727 72725 1384006NM BS 1166 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 WHILE PERFORMING INSPECTION PER EO 7-5310-7-2354, NOTED CRACK INDICATION IN LOWER HOLE STR 28L BS 1166. FURTHER INSPECTION REVEALED CRACK WAS LIMITED TO STR CLIP ONLY. REMOVED AND REPLACED STR CLIP REF SRM 51-30-2. 2L73 4F A3WE 19950929000091995092900009NM 1995 9 29 95FDEA01405 119950921A5320 FAIL-SAFE BOEING727 72725 1384006NM BS 337 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CRACKED FAIL-SAFE ON BS 337 FRAME WL 171 LBL 50. REMOVED CRACKED FAIL-SAFE ON BS 337 FRAME, FABRICATED NEW FAIL-SAFE, TRIMMED, BACK DRILLED, ALODINED, PRIMERED, AND PAINTED IAW FEDEX SRM 53-10-2, 51-30-2 AND MM 51-20-2, INSTALLED WET WITH SEALANT. 2L73 4F A3WE 19950929000101995092900010WP 1995 9 29 95UAL900145 119950807A2781 DISAGREE LIGHT DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL LE FLAPS ILLUMINATED A UALALA ABORTED APPROACH UNSCHED LANDING N FALSE WARNING LDLANDING 1 WP291838U 46632 LAX - SLAT DISAGREE LIGHT ON, DURING APPROACH STICK SHAKER ACTIVATED AND A/C DIVERTED TO LAS. OPERATIONALLY CHECKED SLATS AND FLAPS, BITE CHECKED PROXIMITY ELECTRONICS UNIT, ALL CHECKED OKAY. SUBSEQUENT MONITORING OF AIRCRAFT HAS PRODUCED NO REOCCURANCE. 2L73 4F4 F A22WE E23EA 19950929000111995092900011NE 1995 9 29 95UAL900146 219950922A73211680654 MEC BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE NR 1 ENGINE FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP29948UA 1033 26691 856341 ABORTED TAKEOFF AT 110 KNOTS DUE TO NR 1 ENGINE AUTO-RETARDED TO 82 PERCENT. REPLACED THE MAIN ENGINE CONTROL. THE CAUSE OF THE POWER REDUCTION IS ATTRIBUTED TO A FAILED ROTABLE VARIABLE DIGITAL TRANSDUCER. 2L72 4F4 FRTA16WE E2GL 19950929000121995092900012NM 1995 9 29 95UAL900147 119950922A3350 EEL CABLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29506UA 24627 EMERGENCY ESCAPE PATH LIGHT STRIP INOP FROM ROW 24 TO 32. REPLACED FEEDER CABLE, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19950929000131995092900013 1995 9 29 95UAL900148 419950922A34174040800906 ADC BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 2 INTERMITTANT A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29613UA 21874 ATC FAULT LIGHT AND MESSAGE DISPLAYED. RETURNED TO LAX. FIRST OFFICER'S INSTRUMENTS RETURNED TO NORMAL IN DESCENT, BUT RUDDER RATIO AND AILERON LOCKOUT MESSAGES REMAINED. REPLACED NR TWO AIR DATA COMPUTER AND PERFORMED HI-RANGE LEAK CHECK. CHANGED CIRCUIT BREAKER AS PRECAUTIONARY. 2L72 4F4 FRTA1NM E3NE 19950929000141995092900014WP 1995 9 29 95UAL900149 119950922A3350 EEL BATTERY PACK DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291854U 47813 OVERWING EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY PACK. 2L73 4F4 F A22WE E23EA 19950929000151995092900015WP 1995 9 29 ABXA9500740 119950919A25105641031501 SEAT DOUG DC8 DC861 3021952WP RT COCKPIT LACK OF LUBE A ABXAK NONE O OTHER CRCRUISE 1 GL23842AX 46015 FIRST OFFICER'S SEAT WOULD NOT REMAIN LATCHED IN POSITIONS SELECTED, FORWARD AFT POSITIONS. LATCH PINS NOT FULLY ENGAGING IN TRACK. LUBED TRACKS, LATCH PINS AND SEAT OPS CHECKED GOOD PER DC8 MM. 2L74 4F 4A25 19950929000161995092900016SO 1995 9 29 COMA11968 119950917A528012012347001 LATCH EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMAK NONE O OTHER UKUNKNOWN 1 SO01164D 120164 RIGHT MAIN LANDING GEAR DOOR LATCH IS BROKEN. REPLACED BROKEN LATCH. 2L72 4T RTA31SO 19950929000171995092900017SO 1995 9 29 COMA9511496 119950917A21632154834342 SENSOR EMB 120 EMB120RT SO RT DUCT DEFECTIVE A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01256CA 120245 RT DUCT OVERHEAT WARNING, WARNING REMAINED ON WHEN THE TEMPERATURE WAS SELECTED TO FULL COLD. REPLACED THE DUCT OVER TEMPERATURE SENSOR. 2L72 4T RTA31SO 19950929000181995092900018NE 1995 9 29 COMA9511967 219950918A7310ST3367010 O-RINGS EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENIGNE LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01196CA1123 1123 120196 FUEL LEAKING FROM THE LEFT ENGINE NACELLE. REPLACED THE FUEL NOZZLES TRANSFER TUBE O-RINGS. 2L72 4T4 TRTA31SO E20NE 19950929000191995092900019SO 1995 9 29 COMA9511969 119950921A731210718D FUEL HEATER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LEAKING A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO01267CA11229372 120259 FUEL IS LEAKING FROM THE LEFT ENGINE NACELLE. REPLACED LEAKING FUEL HEATER ASSEMBLY ON THE LEFT ENGINE. 2L72 4T4 TRTA31SO E20NE 19950929000201995092900020SO 1995 9 29 COMA9511970 119950920A27523082001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO011117H4813 1652 120117 FLAP CONTROL FAULT. REPLACED THE LEFT NACELLE FLAP ACTUATOR. 2L72 4T RTA31SO 19950929000211995092900021SO 1995 9 29 COMA9511971 119950919A2450MS2740116 RELAY EMB 120 EMB120RT SO RELAY RACK DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01258CA 120247 DURING FLIGHT, THE RIGHT 115 VOLT AC BUS LIGHT ILLUMINATES. REPLACED K00006 EMERGENCY BUS SENSOR RELAY. 2L72 4T RTA31SO 19950929000221995092900022SW 1995 9 29 COMA9520389 119950925A243051509002B GCU SWRNGNSA227 SA227AC 8780603SW LEFT FAILED A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01704C 1429925 AC704 LEFT GENERATOR WILL NOT COME ON LINE. RESET HAS NO EFFECT. REPLACED THE LT GENERATOR CONTROL UNIT. 1L72 4T A8SW 19950929000231995092900023SW 1995 9 29 COMA9520390 119950926A21211250151 FAN MOTOR SWRNGNSA227 SA227AC 8780603SW CABIN OVERHEATED A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01457CA4317 2391 AC694 DURING DEPLANNING, ELECTRICAL ODOR AND SMOKE OBSERVED COMING FROM A/C VENT. REPLACED DEFECTIVE AIR CONDITIONING SYSTEM ELECTRIC MOTOR. 1L72 4T A8SW 19950929000241995092900024WP 1995 9 29 COMA9520391 219950926A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LEFT FAILED A COMAK NONE O OTHER ININSP/MAINT 1 SO01459AM 2484 AC700 44564 LEFT PROPELLER VERY HARD TO TURN. REPLACED LEFT ENGINE. 1L72 4T4 T A8SW E4WE 19950929000251995092900025EU 1995 9 29 COMA9531159 119950919A77127086M60G10 ECU SAAB SF340 SF340A 7850100EU LT ENGINE DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01361CA24549390 340A056 DURING FLIGHT, THE LEFT ENGINE TORQUE INDICATION FLUCTUATES. REPLACED THE LEFT ENGINE ELECTRONIC CONTROL UNIT. 2L72 4T RTA52EU 19950929000261995092900026EU 1995 9 29 COMA9531160 119950920A243523080031 STARTER GEN SAAB SF340 SF340A 7850100EU LT ENGINE FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01358CA15171676 340A047 DURING START SEQUENCE, THE LEFT ENGINE DOES NOT ROTATE. REPLACED THE LT ENGINE STARTER/GENERATOR. 2L72 4T RTA52EU 19950929000271995092900027EA 1995 9 29 COMA9560552 119950921A2760FE210008 QUADRANT CNDAIRCL600 CL6002B19 EA COCKPIT DEFECTIVE A COMAK NONE O OTHER LDLANDING 1 SO01931CA 7037 DURING LANDING, GROUND LIFT DUMP DEPLOYS NORMALLY, THEN RETRACTS AND REDEPLOYS. REPLACED THE THROTTLE QUADRANT. 2L72 4F RTA21EA 19950929000281995092900028EA 1995 9 29 COMA9560553 119950920A274283963 TRIM ACTUATOR CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01931CA977 151 7037 HORIZONTAL STABILIZER CHANNEL NR 2 WILL NOT ENGAGE. REPLACED THE STABILIZER TRIM ACTUATOR. 2L72 4F RTA21EA 19950929000291995092900029EA 1995 9 29 COMA9560554 119950920A2750865D1007 PDU CNDAIRCL600 CL6002B19 EA TE FLAPS CRACKED A COMAK NONE O OTHER APAPPROACH 1 SO01924CA4991 653 7026 FLAPS FAILED TO OPERATE AT 45 DEGREES. REPLACED CRACKED POWER DRIVE UNIT. 2L72 4F RTA21EA 19950929000301995092900030NM 1995 9 29 DL72S953763 119950908A5320 DOUBLER BOEING727 727232 1384082NM GRND AIR CONNECTDAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND TEMPORARY REPAIR DOUBLER ON PNEUMATIC GROUND AIR CONNECTOR CUTOUT AFT INBOARD CORNER. FABRICATED NEW DOUBLER PER M/M 53-30-0 PGS 803 AND 804. 2L73 4F A3WE 19950929000311995092900031NM 1995 9 29 DL72S953767 119950909A5741 FITTING BOEING727 727232 1384082NM LT WING CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND LT AFT WING ATTACH BODY FITTING WAS CORRODED AT 6 O'CLOCK POSITION. REPAIRED PER SRM 57-10-7. 2L73 4F A3WE 19950929000321995092900032NM 1995 9 29 DL72S953768 119950909A5754 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 4 SLAT RIB CRACKED O/B RIB OF O/B TRACK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950929000331995092900033NM 1995 9 29 DL72S953769 119950909A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 3 SLAT, RIB NR 9 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950929000341995092900034NM 1995 9 29 DL72S953770 119950909A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 3 SLAT, RIB NR 7 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950929000351995092900035NM 1995 9 29 DL72S953771 119950909A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 3 SLAT, RIB NR 6 CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950929000361995092900036NM 1995 9 29 DL72S953772 119950909A5754 RIB BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, NR 8 SLAT, RIB NR 6 FOUND CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19950929000371995092900037NM 1995 9 29 DL72S953774 119950913A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND LT ELEVATOR SKIN CRACKED APPROX 1.5 INCH CRACK IN UPPER SKIN I/B END NEAR LEADING EDGE. REPAIRED PER SRM 55-20-3. 2L73 4F A3WE 19950929000381995092900038NM 1995 9 29 DL72S953775 119950915A5210 BEAM BOEING727 727232 1384082NM FWD ENTRY DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND FWD ENTRY DOOR LOWER HORIZONTAL BEAM CRACKED AT AFT CORNER. REPAIRED PER M/M 52-11-01 PG 805. 2L73 4F A3WE 19950929000391995092900039NM 1995 9 29 DL72S953776 119950918A5754 RIB BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 3 SLAT HAS CRACK IN LOWER SURFACE OF NR 3 RIB FROM I/B END. REPAIRED PER MM 57-54-0 FIG 805. 2L73 4F A3WE 19950929000401995092900040NM 1995 9 29 DL72S953777 119950918A5754 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 4 SLAT HAS CRACK AT ACTUATOR ATTACH O/B RIB. REPAIRED PER MM 57-54-0 FIG 804. 2L73 4F A3WE 19950929000411995092900041NM 1995 9 29 DL72S953778 119950919A5754 RIB BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND NR 8 SLAT, RIB NR 13 WAS CRACKED IN RADIUS. REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19950929000421995092900042NM 1995 9 29 DL72S953779 119950920A5531 RIB BOEING727 727232 1384082NM VERT FIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND ON VERTICAL FIN 4TH RIB DOWN FROM ACCESS HOLE STA 6.372 RIB NR 6 CHORD ANGLE CRACKED AT STR 7 LEFT. REPAIRED PER M/M 55-30-0 PG 802. 2L73 4F A3WE 19950929000431995092900043NM 1995 9 29 DL72S953784 119950906A5753652163261 DOUBLER BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV INSPECTION, THE NR 2 MIDFLAP WAS FOUND CRACKED AFT SPAR RAIL REPAIR DOUBLER AT ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0, CRACKED AT 21 INCHES AND 56 INCHES FROM I/B END. 2L73 4F A3WE 19950929000441995092900044NM 1995 9 29 DL72S953785 119950906A5753652163261 SKIN BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING HMV INSPECTION, FOUND NR 2 MIDFLAP WAS FOUND TO HAVE COVE SKIN CRACKED AT I/B ACTUATOR CUTOUT. REPAIRED PER M/M 57-52-0 PAGE 819. 2L73 4F A3WE 19950929000451995092900045NM 1995 9 29 DL733953788 119950913A5520 SKIN BOEING737 737347 1384647NM LT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313WA 23599 10607 DURING HMV INSPECTION, FOUND LT ELEVATOR TOP SURFACE DAMAGE LOCATED 6 INCHES FROM TRAILING EDGE BETWEEN STATION 39 AND STATION 66.5. REPAIRED PER SRM 55-20-01 REF 51-70-17. 2L72 4F RTA16WE 19950929000461995092900046NM 1995 9 29 DL733953789 119950914A5522 SKIN BOEING737 737347 1384647NM LT ELEV DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313WA 23599 10607 DURING HMV INSPECTION, FOUND EXISTING REPAIR IN POOR CONDITION ON LT ELEVATOR LOWER SURFACE T/E, 30 INCHES FROM O/B END. REPAIRED PER ERA 271896-14. 2L72 4F RTA16WE 19950929000471995092900047NM 1995 9 29 DL76S953786 119950908A7110314T1210408 COWL BOEING767 767332 1382001NM NR 1 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11131DN 24852 THE AFT FRAME AT THE LOWER END OF THE RT CORE COWL WAS WORN. THE DAMAGE WAS REPAIRED PER SRM 54-41-02. 2L72 4F RTA1NM 19950929000481995092900048NE 1995 9 29 DLL13953794 219950917A7200 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO11787DL 193A1126 010612 DUE TO HISTORY OF SMOKE AND OIL SMELL IN AIRCRAFT CABIN, NR 2 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR REPAIRS. 2L73 4F4 F A23WE E12EU 19950929000491995092900049WP 1995 9 29 DLL17953782 119950908A5311 FRAME LKHEED1011 10113853 5265020WP BS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 DURING HMV, 1363 BULKHEAD FRAME AT APPROX WL 160 ON RT SIDE IS CRACKED AT THE SECOND FASTENER FROM BOTTOM FWD ROW. INSTALLED REPAIR AS PER SRM 53-11-00 FIG 843. 2L73 4F A23WE 19950929000501995092900050NM 1995 9 29 DLM88953780 119950920A5330 SKIN DOUG MD88 MD88 3023688NM FWD FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11966DL 53115 DURING E-2 LETTER CHECK, FOUND SKIN CRACKED AT LT NLG STRUT DOOR AFT HINGE CUTOUT. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950929000511995092900051NM 1995 9 29 DLM88953781 119950920A5330 SKIN DOUG MD88 MD88 3023688NM FWD FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11966DL 53115 DURING E-2 LETTER CHECK, FOUND SKIN CRACKED AT RT NLG STRUT DOOR AFT HINGE CUTOUT. REPAIRED PER SRM 53-05 FIG 62A. 2L72 4F RTA6WE 19950929000521995092900052NM 1995 9 29 P5CA9500775 119950922A5512 PANEL BOEING747 747122 1384872NM HORIZ STAB DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 LEFT HAND HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL, JUST OUTBOARD OF ELEVATOR ACTUATOR DELAMINATED THREE PLACES. REPAIRED PANEL IAW 51-40-06. 2L74 4F A20WE 19950929000531995092900053NM 1995 9 29 P5CA9500776 119950922A5730 SKIN BOEING747 747122 1384872NM RT WING LE DETERIORATING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 RIGHT HAND WING LEADING EDGE BOTTOM AT ROOT, PREVIOUS REPAIR DETERIORATING TO COMPOSITE CORE. REPAIRED RIGHT HAND WING LEADING EDGE BOTTOM AT ROOT PER SRM 51-40-12. 2L74 4F A20WE 19950929000541995092900054NM 1995 9 29 P5CA9500777 119950922A5330 SKIN BOEING747 747122 1384872NM FS 759-800 CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 CORROSION LOWER FUSELAGE SKIN STA 750 TO 800. REMOVED CORRODED AREA AND REPAIRED IAW SRM 53-30-03. 2L74 4F A20WE 19950929000551995092900055NM 1995 9 29 SCNA95190 119950919A3350106178317 EEL BOEING727 727227 1384078NM CABIN FAULTY A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE OVERHEAD EMERGENCY LIGHT NEAR THE R-1 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-01, LIGHT TESTED GOOD. 2L73 4F A3WE 19950929000561995092900056NM 1995 9 29 SWAA950635 119950919A5320 SPLICES BOEING737 7372H4 138448CNM BS 905/907/360 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORROSION AT BS 905, LBL 21.5 WL 168, BS 907, S5R AND BS 360, S4L AND S14L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000571995092900057NM 1995 9 29 SWAA950636 119950919A5313 STRINGER BOEING737 7372H4 138448CNM BS 639/747/767 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 747, BS 767 S9R AND AT BS 639 S3L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000581995092900058NM 1995 9 29 SWAA950637 119950919A5320 ANGLE BOEING737 7372H4 138448CNM BS 570 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 42 TO 55 WL 170. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000591995092900059NM 1995 9 29 SWAA950638 119950919A5311 FRAMES BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 663 S4R, BS 500 LBL 2 WL 155, BS 344 LBL 46 WL 170 AND BS 294 WL 209 RBL 55. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000601995092900060NM 1995 9 29 SWAA950639 119950919A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 707-727 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM LOWER O/B FLANGE CORRODED AT BS 707 TO 727, LBL 7 WL 149. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000611995092900061NM 1995 9 29 SWAA950640 119950919A5314 KEEL BEAM BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM FASTENER HOLE CORROSION AT LBL 5.5, AT BS 673.75, 677, 687.5, 692.25, 706.75 AND 708.25. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000621995092900062NM 1995 9 29 SWAA950641 119950919A5330 SKIN BOEING737 7372H4 138448CNM BS 963 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 963, BETWEEN 20 AND 21L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000631995092900063NM 1995 9 29 SWAA950642 119950919A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 842 TO 857 BETWEEN 26R AND 27L, BS 480 BETWEEN S27 AND 28R AND AT BS 306 ABOVE S25L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000641995092900064NM 1995 9 29 SWAA950643 119950919A5320 CHORD BOEING737 7372H4 138448CNM BS 726 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND T-CHORD CRACKED AT AFT CARGO BAY, BS 726 RBL 8.5 WL 203. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000651995092900065NM 1995 9 29 SWAA950644 119950919A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 1156 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND GOUGE IN FWD SIDE OF BS 1156 BULKHEAD AND ON ADJOINING WEB BEHIND RT CENTER SECTION HINGE. REPAIRED PER TRAMCO EWO 95-0560 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000661995092900066NM 1995 9 29 SWAA950645 119950919A5320 WINDOW POST BOEING737 7372H4 138448CNM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND COCKPIT NUMBER 1 WINDOW POST CRACKED AT UPPER AFT CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000671995092900067NM 1995 9 29 SWAA950646 119950919A5320 MOPSILL BOEING737 7372H4 138448CNM AFT SERVICE DOORCORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOOR MOPSILL CORRODED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000681995092900068NM 1995 9 29 SWAA950647 119950919A5315 FLOORBEAMS BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0755SW 21593 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947 WL 208 RBL 10 TO 16, BS 294 LBL 15 RBL 9 WL 208 AND BS 360 RBL 14 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19950929000691995092900069NM 1995 9 29 SWAA950648 119950921A2170 CANISTER BOEING737 7372H4 138448CNM LT AC BAY LEAKING A SWAAD RETURN TO BLOCK O OTHER CLCLIMB 1 SW0720SW 21337 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE USING AUTO, MANUAL OR STANDBY MODES. AIRCRAFT RETURNED TO ABQ AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND LEFT WATER SEPARATOR BAG CANISTER LEAKING. REINSTALLED CANISTER AND O-RINGS PER M/M. 2L72 4F A16WE 19950929000731995092900073WP 1995 9 29 95ZZZX5142 119950909A334025307222 SWITCH LKHEED1011 10113851 5265010WP COCKPIT FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE0511004 193B1016 LAX - FLT 119 - DURING APPROACH WHEN LIGHTS WERE TURNED ON, SMOKE EMITTED FROM EXTERIOR LIGHT CONTROL PANEL. TURNED OFF LIGHTS AND SMOKE DISSIPATED. FOUND LIGHT SWITCH, MFG PN 25307-222, HAD OVERHEATED. REPLACED SWITCH AND OPERATION CHECKED NORMAL. CHECK C-8C - 8-6-95 - JFK. 2L73 4F A23WE 19950929000741995092900074NM 1995 9 29 95ZZZX5143 119950910A7930A008032 PRESSURE SWITCH BOEING727 727231 1384079NM NR 2 ENGINE MALFUNCTIONED A TWAAO OTHER N FALSE WARNING CRCRUISE 1 CE0554338 20843 DTW - FLT 267 - DURING POWER CHANGE AT LEVEL OFF, NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE SN 3989. REPLACED NR 2 ENGINE OIL BYPASS PRESSURE SWITCH, MFG PN A00803-2 AND OIL FILTER ELEMENT, MFG PN 7578678. ENGINE RUN-UP OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 50,538 HOURS; 34,442 CYCLES. CHECK C-3 - 10-7-94 - MCI. 2L73 4F A3WE 19950929000751995092900075WP 1995 9 29 95ZZZX5144 119950901A3260H146 DOWNLOCK SWITCH DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE05988Z 47134 STL - FLT 693 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED NOSE LANDING GEAR GREEN, LOCKED LIGHT DID NOT ILLUMINATE. CYCLED LANDING GEAR AND GREEN LOCKED LIGHT ILLUMINATED. FOUND DEFECTIVE NOSE GEAR DOWNLOCK SWITCH, MFG PN H14-6. REPLACED NOSE GEAR DOWNLOCK SWITCH AND LANDING GEAR LIGHTS, OPERATION CHECKED NORMAL. CHECK C - 8-4-95 - STL. 2L72 4F A6WE 19950929000761995092900076WP 1995 9 29 95ZZZX5145 119950902A3260H146 SWITCH DOUG DC9 DC915 3022036WP RT MLG DOOR MALFUNCTIONED A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05970Z 45772 STL - FLT 582 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR AND DOOR LIGHT WAS SLOW TO EXTINGUISH. FOUND DEFECTIVE RIGHT MAIN LANDING GEAR DOOR SWITCH, MFG H14-6. REPLACED RIGHT MAIN LANDING GEAR DOOR SWITCH AND DOOR LIGHT, OPERATION CHECKED NORMAL. CHECK C - 6-24-94 - STL. 2L72 4F A6WE 19950929000771995092900077WP 1995 9 29 95ZZZX5146 119950802A5313 LONGERON DOUG DC9 DC931 3022065WP BS 945-996 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 47134 STL - DURING OP-15, FOUND CORROSION ON LONGERON 28L, STA 945 TO STA 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, SRM 51-30-2, AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 67,006 HOURS; 73,957 CYCLES. 2L72 4F A6WE 19950929000781995092900078NM 1995 9 29 95ZZZX5147 119950822A3230 BOLT BOEING727 727231 1384079NM LANDING GEAR WORN A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE0552310 19829 STL - FLT 556 - AFTER TAKEOFF, LANDING GEAR LEVER WAS LOCKED. USED OVERRIDE PROCEDURES TO RETRACT LANDING GEAR. FOUND WORN BOLT FOR LANDING GEAR SAFETY SWITCH SENSOR ACTUATOR. REPLACED BOLT AND LANDING GEAR, OPERATION CHECKED NORMAL. CHECK C - 8-8-95 - MCI. 2L73 4F A3WE 19950929000791995092900079NM 1995 9 29 95ZZZX5148 119950830A3230 RETRACT MECH BOEING727 727231 1384079NM NLG LACK OF LUBE A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0554341 21628 SLC - FLT 777 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NLG DID NOT EXTEND. CYCLED LANDING GEAR AND NOSE GEAR EXTENDED AND LOCKED. LUBRICATED NLG, INSPECTED NLG AND DOORS, ALL APPEARED NORMAL. CHECK C-1 - 11-21-94 - MCI. 2L73 4F A3WE 19950929000801995092900080NM 1995 9 29 95ZZZX5149 119950830A323065404676 LOCK ACTUATOR BOEING727 727231 1384079NM NLG MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0554341 21628 STL - FLT 264 - DURING APPROACH, NOSE LANDING GEAR DID NOT EXTEND UNTIL MAIN LANDING GEAR WAS DOWN AND LOCKED. FOUND LOCK RELEASE ACTUATOR, MFG PN 65-40467-6, HAD INTERNAL MALFUNCTION. REPLACED NLG LOCK RELEASE ACTUATOR AND NLG OPERATION CHECKED NORMAL. CHECK C-1 - 11-21-94 - MCI. 2L73 4F A3WE 19950929000811995092900081NE 1995 9 29 95ZZZX5150 219950824A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7A 52053NE NR 2 FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 CE05976Z 47248 CLE - FLT 384 - DURING DESCENT, SHUT DOWN NR 2 ENGINE, SN 2161, DUE TO LOW OIL PRESSURE LIGHT ILLUMINATION AND DECREASING OIL QUANTITY. FOUND OIL LEAK AT NR 1 BEARING AND METAL PARTICLES IN OIL SCREEN. CHANGED NR 2 ENGINE. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 48,251 HOURS; 54,637 CYCLES. CHECK C- 7-3-95 - STL. 2L72 4F4 F A6WE E2EA 19950929000821995092900082NM 1995 9 29 95ZZZX5151 119950904A3260864202 PROX SENSOR ELDEC DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07907HA27498 011 PHL/SBY - FLT 3185 - AFTER GEAR RETRACTION, LEFT MAIN GEAR DOOR LIGHTS STAYS ILLUMINATED. DOORS APPEAR FULLY CLOSED BY VISUAL INSPECTION. AIRCRAFT CONTINUED ON TO SBY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED PROXIMITY SENSOR. 2H72 4T RTA13NM 19950929000831995092900083NM 1995 9 29 95ZZZX5152 119950828A5260 VALVE DHAV DHC8 DHC8102 2809003NM AIRSTAIR DOOR LACK OF LUBE A HNAAK NONE O OTHER ININSP/MAINT 1 EA07906HA 009 TLH/TPA - FLT 3087 - DURING PRE-FLIGHT WALK-AROUND, FLIGHT ATTENDANT COULD NOT OPEN MAIN EXIT DOOR. LUBED AIRSTAIR DOOR SEAL PRESSURE VALVE. 2H72 4T RTA13NM 19950929000841995092900084NM 1995 9 29 95ZZZX5153 119950825A6123 AUTOFEATHER SW DHAV DHC8 DHC8102 2809003NM NR 1/2 DIRTY A HNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA07925HA 111 MCO/TLH - FLT 3092 - ON TAKEOFF ROLL, AUTOFEATHER WOULD NOT ARM WHEN POWER LEVERS ADVANCED TO TAKEOFF SETTINGS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. CLEANED NR 1 AND NR 2 AUTOFEATHER MICROSWITCHES. 2H72 4T RTA13NM 19950929000851995092900085NM 1995 9 29 95ZZZX5154 119950821A33506013211X EEL BATTERY GRIMES DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07928HA158808952 ORF148 120 TPA/JAX - FLT 3451 - DURING PRE-FLIGHT WALK-AROUND, FOUND 2 RED FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY AT SEATS 1DF. 2H72 4T RTA13NM 19950929000861995092900086NM 1995 9 29 95ZZZX5155 119950823A322288051 INNER CYLINDER ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07930HA18437 0091WH 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000871995092900087NM 1995 9 29 95ZZZX5156 119950823A322088357 ARM ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07930HA18437 DCL159 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000881995092900088NM 1995 9 29 95ZZZX5157 119950823A322288121 PISTON ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07930HA18437 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000891995092900089NM 1995 9 29 95ZZZX5158 119950823A322288321 AXLE ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07930HA18437 DCL167 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000901995092900090NM 1995 9 29 95ZZZX5159 119950823A324688283 UPPER BEARINGS ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07930HA18437 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000911995092900091NM 1995 9 29 95ZZZX5160 119950823A324688221 LWR BEARINGS ROTOL DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE J WARNING INDICATION CLCLIMB 1 EA07930HA18437 126 LYN/PHL - FLT 3230 - AFTER TAKEOFF, UPON GEAR RETRACTION, THE WOW CAUTION LIGHT ILLUMINATED AND THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND BOTH LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. AFTER FERRYING TO SBY, THE NOSE LANDING GEAR LOWER BEARING WAS FOUND TO BE BINDING AND STICKING. REMOVED AND REPLACED THE NLG INNER CYLINDER, TRAIL ARM, PISTON, AXLE, UPPER AND LOWER BEARINGS, AND ASSOCIATED SEALS. 2H72 4T RTA13NM 19950929000921995092900092NE 1995 9 29 95ZZZX5161 319950829A6111E10950K BLADE BEECH 1900 1900D 1154162CE HARTZLHCE4A HCE4A3A NE RT ENGINE CRACKED A AJJBAK NONE O OTHER ININSP/MAINT 1 EA01841CA3325 722 581MA UE40 HJ139A RIGHT PROPELLER BLADE, SN 518MA, DE-ICE BOOT PARTIALLY MISSING AND LEADING EDGE CRACKED IN AREA OF BOOT OPERATION. REMOVED AND REPLACED PROPELLER WITH ZERO TIME OVERHAULED UNIT. (CRACK NOTED WAS IN LEADING EDGE ABRASION STRIP. THIS IS SECOND FAILURE OF THIS TYPE REPORTED BY OPERATOR.) 2L72 4T RTA24CE 5 CP10NE 19950929000931995092900093 1995 9 29 95ZZZX5162 419950825A2565C17760101 GAUGE GARRTT A30466102133AIRBUS300 A300B4203 3930306EU R1 DOOR SLIDE OUT OF TOLERANCEA P2RAK NONE O OTHER ININSP/MAINT 1 WP2314976 2075 271 DURING MAINTENANCE CHECK, FOUND R-1 DOOR SLIDE PRESSURE GAUGE READING HIGH BEYOND LIMIT. REMOVED AND REPLACED R1 DOOR SLIDE/RAFT ASSY PER MM. RESULTS SATISFACTORY. 2L72 4F A35EU 19950929000951995092900095WP 1995 9 29 CAL950778 119950801A2612 FIRE LOOP DOUG DC10 DC1010 3022110WP NR 2 ENGINE INOPERATIVE A CALAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0968043 46902 NRT - FLT 0962 - THE NR 2 ENGINE B-LOOP FIRE WARNING LIGHT ILLUMINATED DURING CLIMB-OUT OF NRT. THE NR 2 ENGINE WAS SHUT DOWN, BOTH FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT WAS RETURNED TO NRT WHERE IT LANDED WITHOUT INCIDENT. THERE WAS NO EVIDENCE OF FIRE FOUND. THE NR 2 ENGINE LOWER CORE COWL FIRE LOOP ELEMENT WAS REPLACED AND THE B-LOOP FIRE WARNING SYSTEM TESTED GOOD. BOTH ENGINE FIRE BOTTLES WERE REPLACED. (X) 2L73 4F A22WE 19950929000961995092900096WP 1995 9 29 CAL950780 119950901A2910 PACKING DOUG DC9 DC982 3022082WP HYD TRNSF VALVE LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914810 49264 PHX - FLT 0165 - THE LT HYDRAULIC QUANTITY DROPPED AND WAS FOLLOWED SHORTLY AFTERWARDS BY A DROP OF THE RT HYDRAULIC QUANTITY WHILE EN ROUTE FROM IAH TO SFO. BOTH HYDRAULIC QUANTITY GAUGES READ 2 QUARTS. THE AIRCRAFT WAS DIVERTED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC TRANSFER VALVE LEAKING. THE PACKING FOR THE HYDRAULIC TRANSFER VALVE WAS REPLACED. IN ADDITION, FOUR LOOSE FITTINGS AT THE LEFT WHEELWELL PTU VALVE WERE TIGHTENED. THE LEFT AND RIGHT HYDRAULIC SYSTEMS WERE SERVICED AND OPERATIONAL AND LEAK CHECKS WERE GOOD. (X) 2L72 4F A6WE 19950929000971995092900097WP 1995 9 29 CAL950781 119950901A2750 CONTROL CABLE DOUG DC10 DC1010 3022110WP LT TE FLAP BROKEN A CALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SW0968047 47801 GUM - FLT 0962 - THE FLAP DISAGREE LIGHT ILLUMINATED AND THE AIRCRAFT EXPERIENCED A SLIGHT LEFT ROLL DURING FLAP EXTENSION ON APPROACH TO GUM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBD FLAP FOLLOW-UP CABLE 98B CORRODED AND BROKEN. THE FLAP FOLLOW-UP CABLE WAS REPLACED IAW MM 27-51-00 AND OPERATION CHECKED GOOD. (X) 2L73 4F A22WE 19950929000981995092900098WP 1995 9 29 CAL950783 119950902A2820 FUEL COUPLING DOUG DC9 DC932 3022066WP RT WING LEAKING A CALAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SW0970542 47535 IAH - FLT 1230 - THE LEFT MAIN FUEL QUANTITY BEGAN TO DECREASE AS FUEL WAS TRANSFERRED FROM CENTER TANK AFTER TAKEOFF FROM IAH. THE LEFT FUEL QUANTITY STEADILY AND RAPIDLY DECREASED. THE CROSS-FEED WAS OPENED IN AN ATTEMPT TO BURN RT MAIN FUEL, BUT THE LT FUEL QUANTITY CONTINUED TO DECREASE. FUEL WAS REPORTED COMING FROM THE LT WING. THE CROSS-FEED WAS CLOSED AND THE ACFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT WING INBD FUEL COUPLING LOOSE AND LEAKING FUEL. THE COUPLING PACKINGS WERE REPLACED AND THE COUPLING WAS RECONNECTED AND SAFTIED. LEAK CHECKS WERE GOOD. ALL FUEL BOOST PUMPS OPERATED NORMALLY AND NO LEAKS WERE NOTED. (X) 2L72 4F A6WE 19950929000991995092900099NM 1995 9 29 CAL950784 119950902A323065404676 LOCK ACTUATOR BOEING727 727224 1384076NM NLG INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW09667345050612196 20663 EWR - FLT 0434 - THE NLG FAILED TO EXTEND ON APPROACH TO EWR, THE GEAR WAS CYCLED DURING A 'GO AROUND' AND THE NOSE GEAR EXTENDED NORMALLY. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-33-11. AN EXTENSION/RETRACTION TEST WAS PERFORMED IAW MM 32-33-0 AND NO DEFECTS WERE NOTED. (X) 2L73 4F A3WE 19950929001001995092900100NM 1995 9 29 CAL950787 119950903A331069482725 TEST MODULE BOEING727 727243 138408DNM FLIGHT COMPT INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW09579PE16406 21662 IAH - FLT 0423 - SEVERAL WARNING LIGHTS ILLUMINATED DURING TAKEOFF FROM IAH. THE TERRAIN WARNING, AUTOPILOT DISENGAGE, WINDSHEAR, ALL THREE ENGINE OIL LIGHTS, HYDRAULIC LIGHT, AILERON, RUDDER, AND ELEVATOR LIGHTS, AND MASTER WARNING LIGHT ALL ILLUMINATED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE M833 AND M981 MASTER DIM AND TEST MODULES WERE REMOVED AND REPLACED. IN ADDITION, THE MASTER DIM AND TEST SWITCH WERE REPLACED. AN OPERATIONAL CHECK OF ALL WARNING LIGHTS WAS NORMAL (X) 2L73 4F RTA3WE 19950929001011995092900101 1995 9 29 CAL950790 419950905A34189654020003 AOA SENSOR DOUG DC10 DC1030 3023501WP LEFT INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW096806032129 47850 FCO - FLT 0041 - THE STALL WARNING SYSTEM ACTIVATED AFTER SLATS WERE RETRACTED DEPARTING FCO. THE SLAT/FLAPS WERE DROPPED THREE TIMES, BUT THE WARNING CONTINUED. THE FLAP/SLAT INDICATOR DISAGREE LIGHT ALSO ILLUMINATED. THE AIRCRAFT WAS RETURNED TO FCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBD FLAP POSITION TRANSMITTER SHAFT FROZEN AND THE CANNON PLUG WAS CORRODED. THE TRANSMITTER AND CANNON PLUG WERE REMOVED AND REPLACED. THE LEFT AOA SENSOR WAS ALSO FOUND AT FAULT. THE LEFT AOA SENSOR WAS REMOVED AND REPLACED. AT/SC AND AOA SELF-TESTS WERE PERFORMED PER MM 22-33-01 AND OPERATION CHECKED NORMAL. (X) 2L73 4F A22WE 19950929001021995092900102WP 1995 9 29 CAL950791 119950905A2130ABM7012505 VALVE DOUG DC10 DC1030 3023501WP CABIN STUCK A CALAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091506968439 46584 IAH - FLT 0010 - THE AIRCRAFT LOST PRESSURIZATION AT 11,000 FEET AFTER TAKEOFF FROM IAH. THE LOSS OF PRESSURE WAS ACCOMPANIED BY A LOUD BANG AND CREW WAS UNABLE TO CONTROL THE CABIN. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CONDITION AIR RELIEF/GROUND CHECK VALVE STUCK OPEN. THE VALVE WAS RESEATED. THE CABIN WAS PRESSURIZED AND ALL CHECKED NORMAL WITH NO LEAKS FOUND. (X) 2L73 4F A22WE 19950929001031995092900103EU 1995 9 29 RAIA950849 119950829A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03424AM6815 1573 865 CMI - FLT 7437 - RIGHT ENGINE WOULD NOT MAKE TAKEOFF TORQUE BY 5 PERCENT. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER PER GARRETT DSC SETTINGS AND ADJUSTED EGT COMPENSATOR. GROUND RUNS REVEALED NORMAL OPERATION. AIRCRAFT TT 10,091.0. (X) 2L72 4T RTA56EU 19950929001041995092900104EU 1995 9 29 RAIA950850 119950829A3240 BRAKE FLUID BAG JETSTMJETSTM3201 1500217EU LEFT LOW A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03424AM10091 865 STL - FLT 7431 - FIRST OFFICER'S LEFT BRAKE PEDAL VERY MUSHY, SHOWS NO PRESSURE WHERE FULLY DEPRESSED. MAINTENANCE REFILLED FIRST OFFICER'S BRAKE MASTER CYLINDER, PN ACM26810, BLED BRAKE. TAXI CHECK OF BRAKING SYSTEMS REVEALED NORMAL OPS. AIRCRAFT TT, 10,091.2. (X) 2L72 4T RTA56EU 19950929001051995092900105SO 1995 9 29 RAIA950851 119950827A2150EVAC2322C2 FAN EMB 120 EMB120RT SO LT PACK FAULTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03124AM117427321 120016 STL - FLT 7210 - LEFT PACK PUTS OUT SMOKE IN COCKPIT. MAINTENANCE REPLACED LEFT PACK GROUND COOLING FAN. SYSTEM CHECK GOOD. AIRCRAFT TT, 19,593.0. (X) 2L72 4T RTA31SO 19950929001061995092900106EU 1995 9 29 RAIA950852 119950828A3242AC69596 MAXERATE BAG JETSTMJETSTM3201 1500217EU LT MLG FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03431AM2453 224 881 STL - FLT 7060 - LEFT BRAKE ANTI-SKID BYPASSES FLUID UPON MAIN BRAKE APPLICATION. MAINTENANCE REPLACED LEFT MAXERATE. TAXI AND LEAK CHECK GOOD. AIRCRAFT TT, 9616.0. (X) 2L72 4T RTA56EU 19950929001071995092900107EU 1995 9 29 RAIA950853 119950829A21708323715 WATER SOCK BAG JETSTMJETSTM3201 1500217EU LT PACK DIRTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03433AM9365 581 885 STL - FLT 7104 - SUPPLEMENT - EXCESSIVE OIL SMELLING SMOKE FROM FLOWS. MAINTENANCE REPLACED LT PACK WATER SOCK. SYSTEM CHECK GOOD. (X) 2L72 4T RTA56EU 19950929001081995092900108EU 1995 9 29 RAIA950854 119950831A215032149602 VALVE AEROSPATR72 ATR72202 8680940EU RT PACK FAILED A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE03722TE5143 1217 220 STL - FLT 7525 - CABIN FILLED UP WITH SMOKE. MAINTENANCE REPLACED RT PACK VALVE ASSY. GROUND RUNS CHECK GOOD. AIRCRAFT TT, 8969.0. (X) 2H72 4T RTA53EU 19950929001091995092900109EU 1995 9 29 RAIA950855 119950831A215022051201 ACM AEROSPATR72 ATR72202 8680940EU RT PACK FAULTY A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03722TE6284 1795 220 STL - SUPPLEMENT - FA SMELLED SMOKE IN CABIN. MAINTENANCE REPLACED RT SIDE AIR CYCLING MACHINE. GROUND CHECK GOOD. AIRCRAFT TT, 8976.0. (X) 2H72 4T RTA53EU 19950929001101995092900110EU 1995 9 29 RAIA950856 119950827A33503011151 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03426AM101441820 874 STL - FIRST EIGHT EMERGENCY FLOOR LIGHTS INOP. MAINTENANCE REPLACED FWD EMERGENCY LIGHT BATTERY. AIRCRAFT TT 10,144.0. (X) 2L72 4T RTA56EU 19950929001111995092900111WP 1995 9 29 RAIA950857 219950831A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LEFT MALFUNCTIONED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03425AM8961 2591 870 66162 STL - FLT 7440 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE. GROUND PERFORMANCE RUNS REVEALED NORMAL PARAMETERS AND LEAKS CHECK GOOD. AIRCRAFT TT 9814.0. ENGINE TT 8691.0. (X) 2L72 4T4 TRTA56EU E4WE 19950929001121995092900112WP 1995 9 29 RAIA950902 219950902A732189778027 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03428AM9689 3711 877 66116 DEC - FLT 7303 - LEFT TORQUE 70 PERCENT. MAINTENANCE REPLACED LEFT FCU. GROUND RUNS REVEALED NORMAL OPERATION. AIRCRAFT TT, 9723.0. ENGINE TT, 8974. (X) 2L72 4T4 TRTA56EU E4WE 19950929001131995092900113EU 1995 9 29 RAIA950904 119950904A527091SE13 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03425AM9814 870 STL - FLT 7470 - PASSENGER DOOR CAP LIGHT ILLUMINATED. MAINTENANCE ADJUSTED PASSENGER DOOR CENTER MICROSWITCH. SYSTEM CHECK GOOD. AIRCRAFT TT, 9814.0. (X) 2L72 4T RTA56EU 19950929001141995092900114NE 1995 9 29 TSAA9572165 219950822A7200 ENGINE BOEING737 7372M6C 1384708NM PWA JT8 JT8D15 52051NE NR 2 FAILED A TSAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP13805AL 21809 702833 HUL - FLT 940 - P/R 1 - NR 2 ENGINE FAILED AT 1,000 FEET WITH THROTTLE VIBRATION. RETURNED FOR LANDING AFTER SOP. THE AIRCRAFT RETURNED TO HUL, AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. ACCOMPLISHED ENGINE MOUNT INSPECTION, PHASE 2, PER FORM M-148, AND NR 2 ENGINE ASSY REPLACED PER M-211, M-212, M-213, M-214, AND M-215. AIRCRAFT RETURNED TO SERVICE. ENGINE CYCLES, 28,632. (X) 2L72 4F4 FRTA16WE E2EA 19950929001151995092900115EU 1995 9 29 VTZA95284 119950908A3244AHA1837 TIRE JETAIRJETSTMJETSTM4101 1500501EU NLG OUT OF ROUND A VTZAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 EA27301UE 41012 IAD/EWR - FLT 6410 - DURING THE CLIMB-OUT PHASE OF THE TAKEOFF AT 1,315 HRS ON 9-8-95, RETURNED TO IAD DUE TO A VIBRATION DURING THE RETRACTION OF THE LANDING GEAR. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NOSE TIRES DUE TO THEM BEING OUT OF ROUND. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950929001161995092900116EU 1995 9 29 VTZA95286 119950909A3234AIR87390 SELECTOR VALVE JETAIRJETSTMJETSTM4101 1500501EU LANDING GEAR MALFUNCTIONED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27315UE 41033 EWR/IAD - FLT 6371 - DURING THE INITIAL CLIMB-OUT PHASE OF THE TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. AIRCRAFT RETURNED AND LANDED AT EWR WITH NO FURTHER INCIDENTS. MAINTENANCE RESET THE LANDING GEAR AND FLAP EMERGENCY SELECTOR VALVES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19950929001171995092900117NM 1995 9 29 95FDEA00423 119950410A5320ANB7309 SPLICE PLATE DOUG MD11 MD11F 3023600NM WS 118 GOUGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25614FE 48528 CENTER WING TO RT LOWER WING LONGITUDINAL SPLICE PLATE HAS A WEAR MARK APPROX 5 FEET IN LENGTH, WITH L/E TIP OF SPLICE PLATE WORN APPROX 90 PERCENT OF MATERIAL THICKNESS AT XCW118 INTERSECTING FUSE STA 1156. C/W EA 1-5710-24326 WING OUBT TO CENTER, SPLICE PLATE BLEND OUT (RT). 2L73 4F RTA22WE 19950929001181995092900118NM 1995 9 29 95FDEA00424 119950419A2612 FIRE LOOP BOEING727 727233 138408ANM NR 1 ENGINE OUT OF POSITION A FDEAH DEACTIVATE SYST/CIRCUITS N FALSE WARNING UKUNKNOWN 1 SO25221FE 20932 NR 1 ENG STRUT O/H LIGHT CAME ON. BLEED AIR WAS BEING USED FOR PACK. OPS AFTER AIR WAS TURNED OFF, O/H LIGHT EXTINGUISHED, ACCOMP ENG STRUT O/H LIGHT ON CKLST. ESTABLISH PACK OPS USING NR 2 BLEED. OPENED NR 1 STRUT ACCESS PANELS, FOUND AFT UPPER LOOP IN CONTACT WITH LOWER LOOP BRACKET, REPOSITIONED. ALSO, FOUND LOOPS CONN LOOSE AT FUSELAGE, RE-TIGHTENED AND RE-SAFETIED. RAN ENG PER JRH A DIF POWER SETTING. NO LEAKS, NO LIGHT, GND OPS CK GOOD. RE-INSTALLED STRUT ACCESS PANELS. 2L73 4F RTA3WE 19950929001191995092900119NM 1995 9 29 95FDEA00443 119950422A3231ANB7216504 RETRACT MECH DOUG MD11 MD11F 3023600NM RT MLG DOOR OUT OF ADJUST A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25609FE 48549 ON GEAR RETRACTION, BOTH RT MAIN IND REMAINED RED, CYCLED GEAR AND GOT BOTH LT AND RT INDICATIONS RED. ALL GREEN IN DOWN POS, RECYCLED GEAR AND GOT SAME INDICATIONS, AFTER 3 MINUTES LT GEAR RETURNED TO NORMAL. THIS SEQUENCE OCCURED TWICE, CONTINUED FLT TO NRT. RT GEAR IND RED AND IND PINS ON TOP OF WINGS WERE NORMAL NO VIBRATION FLT OR YAW. FOUND DAMAGE ON L/B EDGE FWD AND AFT OF FAIRNIG OF THE RT MLG RAMP DOOR ASSY, AT GATE. INSP RIGGING CONDITION AND PERFORMED RIGGING OF ROD LINKAGE, WITH DOOR INPUT FOLLOW-UP FOR DOOR CONTROL RT AND RIGGING DOOR LATCH RT. LANDING GEAR HAD EXTEND AND RETRACT CHECK ON LIFTING CONDITION PER MM 32-00-00, FOUND GOOD. COMPLIED RII. 2L73 4F RTA22WE 19950929001201995092900120WP 1995 9 29 95FDEA00444 119950424A3233ARG73765509 CYLINDER DOUG DC10 DC1030 3023501WP LT MLG FAILED A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25312FE 48300 AFTER TAKEOFF HYD SYS NR 3 ELEV LIGHT CAME ON SECOND OFFICERS PANEL IN CONJUNCTION WITH LOUD BANG AND CORRESPONDING LOSS OF SYS NR 3 HYD QTY (DOWN TO ONE GAL) APPROPRIATE EMERGENCY PROCEDURE CHECKLIST WERE RUN. REMOVED AND REPLACED LEFT MAIN LANDING GEAR RETRACT CYLINDER, AND FIELD WORK BY BF GOODRICH REPLACING LOWER EYE BUSHINGS AS PER MM 32-33-01, ALL SYS GROUND CHECKED NORMAL. 2L73 4F A22WE 19950929001211995092900121NM 1995 9 29 95FDEA00445 119950502A5243 DOOR BOEING727 727277 138408SNM HYD COMPT MISSING A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25243FE 21480 ACFT ARRIVED AT JFK WITH HYD SERVICE DOOR MISSING AND SLIGHT FAIRING DAMAGE. REPLACED MISSING HYD SERVICE DOOR AND MADE TEMPORARY REPAIR ON FAIRINGS. 2L73 4F RTA3WE 19950929001221995092900122NE 1995 9 29 95FDEA00446 219950502A7200 ENGINE BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE NR 1 FAILED A FDEAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION DEDESCENT 1 SO25103FE 19199 DURING FLT HAD NR 1 LOW OIL PRESS/FILTER BYPASS LIGHT WITH 46 PSI OIL PRESS NR 1 ENG SHUTDOWN AS PER RED TABS. LIGHT CAME ON AT START OF DESCENT. MINOR VIBRATION NOTED DURING FLIGHT, BUT ALL INDICATIONS NORMAL UNTIL LIGHT CAME ON. FOUND METAL IN THE OIL SYSTEM. REMOVED AND REPLACED NR 1 ENGINE. 2L73 4F4 F A3WE E2EA 19950929001231995092900123NM 1995 9 29 95FDEA00447 119950425A53302024T4050 SKIN BOEING727 72725 1384006NM BS 207 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25155FE 18288 DOUBLE HOLE IN SKIN BELOW F/O'S NR 1 WINDOW BS 207 RBL 31 WL 243. REPAIRED DOUBLE HOLE IN SKIN BELOW F/O'S NR 1 WINDOW BS 207 RBL 31 WL 243 IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950929001241995092900124NM 1995 9 29 95FDEA00448 119950425A53302074T3050 SKIN BOEING727 72725 1384006NM BS 420-440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 420 TO 440 AT STR 216 TWO POSSIBLE CRACKS IN SKIN. TRIMMED OUT DAMAGED ON SKIN AT STA 430 STR 216, FABRICATED, DRILLED UP, ALODINED, PRIMED, AND INSTALLED DOUBLER AND FILLER. ALL WORK ACCOMPLISHED IAW FEDEX SRM 727-100 (53-30-3) FUNCTIONAL TESTS CHECK GOOD PER FEDEX MM 34-22-24, 34-21-71, 34-52-0, AND 23-51-11. 2L73 4F A3WE 19950929001251995092900125NM 1995 9 29 95FDEA00449 119950425A53202024T3100 LWR CHORD BOEING727 72725 1384006NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON LOWER 740 CHORD AT WL 170, RBL 28. BLENDED AND REMOVED CORROSION ON LOWER 740 CHORD AT WL 170 RBL 28. ORIGINAL THICKNESS OF MATERIAL .0270, REMOVED .083 MATERIAL 1.0 BY 2.0 OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED 740 CHORD PER EA 7-5710-24587. 2L73 4F A3WE 19950929001261995092900126NM 1995 9 29 95FDEA00450 119950425A5311 FRAME BOEING727 72725 1384006NM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION IN THE FWD CARGO BAY THERE IS CORROSION UNDER FLANGE OF FRAME AT BS 660, RBL 25, WL 156. CORROSION FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1 UNDER FRAME FLANGE AT BS 660 RBL 25 WL 156. REPAIRED FRAME PER FEDEX SRM 57-46-3 AND 53-10-2. 2L73 4F A3WE 19950929001271995092900127NM 1995 9 29 95FDEA00451 119950425A5347BAC1520843 SEAT TRACK BOEING727 72725 1384006NM BS 570 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION IN THE FWD CARGO BAY IN CARGO SEAT TRACK AT BS 570 LBL 18 WL 156. REMOVED AND REPLACED CARGO SEAT TRACK FROM BS 520 TO 580 LBL 18 WL 156 IN FWD CARGO BAY PER FEDEX SRM 53-10-5. 2L73 4F A3WE 19950929001281995092900128NM 1995 9 29 95FDEA00452 119950425A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 620-640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON SEAT TRACK AT BS 620 TO 640 BLO WL 208 HAD MECH DAMAGE AT BS 614. REMOVED AND REPLACED SEAT TRACK FROM BS 600 TO 720 WL 208 BL0. 2L73 4F A3WE 19950929001291995092900129NM 1995 9 29 95FDEA00453 119950425A53207075T6 WEB BOEING727 72725 1384006NM BS 850 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK IN LONGITUDINAL WEB BS 850 LBL 45 WL 200. REPAIRED CRACK IN LONGITUDINAL WEB AT BS 850 LBL 45 WL 200 PER FEDEX SRM 51-40-2 AND 51-10-1. 2L73 4F A3WE 19950929001301995092900130NM 1995 9 29 95FDEA00454 119950425A5347BAC1520792 SEAT TRACK BOEING727 72725 1384006NM BS 545-560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) ON SEAT TRACK BS 545 TO 560 BL0 WL 208 AND BS 480 TO 494. REMOVE AND REPLACED NEW SEAT TRACK FROM BS 480 TO 600 BL0 WL 208 AS PER FEDEX SRM 53-10-1 AND 53-10-5. 2L73 4F A3WE 19950929001311995092900131NM 1995 9 29 95FDEA00455 119950426A5347BAC1520792AL SEAT TRACK BOEING727 72725 1384006NM BS 496 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) ON SEAT TRACK BS 496 RBL 25 WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 480 TO 510 RBL 25 WL 208 PER FEDEX SRM 53-10-05 AND 53-10-01. 2L73 4F A3WE 19950929001321995092900132NM 1995 9 29 95FDEA00456 119950425A53476010452 SEAT TRACK BOEING727 72725 1384006NM BS 1130-1176 BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 INBOARD SEAT TRACK AT POSITION WHERE FWD STANTION ATTACHED TO FLOOR (10L) IS BROKEN. REMOVED AND REPLACED SEAT TRACK AT POSITION WHERE FWD STANTION ATTACHES TO FLOOR (10L) BS 1130 TO 1176 WL 208 LBL 24.75. 2L73 4F A3WE 19950929001331995092900133NM 1995 9 29 95FDEA00457 119950425A5313BAC1498142 STRINGER BOEING727 72725 1384006NM BS 1165 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON STR 22L, BS 1165. REPAIRED STR 22L AT BS 1165 PER FEDEX SRM 53-10-3 FIG 1. 2L73 4F A3WE 19950929001341995092900134NM 1995 9 29 95FDEA00458 119950425A53202024T3125 FITTING BOEING727 72725 1384006NM BS 870 SEPARATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 SUSPECT INDICATIONS FOUND AT BS 870 RT TERMINAL FITTING DURING UT INSP. REQUIRE REMOVAL OF FWD AND AFT SPLICE PLATES TO VERIFY INDICATIONS WITH HFEC. REPAIRED WEB SEPARATION IN BS 870 RT TERMINAL FITTING IAW FEDEX EA 7-5310-24491. 2L73 4F A3WE 19950929001351995092900135NM 1995 9 29 95FDEA00459 119950425A5312M368996 BULKHEAD BOEING727 72725 1384006NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 2 CRACKS IN 950 BULKHEAD LBL 5 AND RBL 5 WL 174. REPAIRED CRACKS IN 950 BLUKHEAD AT LBL 5 AND RBL 5 WL 174 PER FEDEX SRM 53-10-9 FIG 2. 2L73 4F A3WE 19950929001361995092900136NM 1995 9 29 95FDEA00460 119950425A5313BAC1498142 STRINGER BOEING727 72725 1384006NM BS 1030 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACKED STR 22L, BS 1030. CUT OUT DAMAGED AREA FABRICATED REPAIR PARTS, INSTALLED REPAIR PARTS NET WITH SEAL AND INSTALLED FASTENERS, ALL WORK DONE IN ACCORDANCE WITH FEDEX SRM 53-10-3 AT BS 1030 STR 22L. MFG P/N M377459, BAC1498132, M424422. 2L73 4F A3WE 19950929001371995092900137NM 1995 9 29 95FDEA00461 119950425A53207075T6071 SHEAR TIE BOEING727 72725 1384006NM BS 1148 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON SHEAR TIE BS 1148, LBL 22, WL 153. REMOVE AND REPLACED SHEAR TIE AT BS 1148, LBL 22, WL 153 AS PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19950929001381995092900138NM 1995 9 29 95FDEA00462 119950425A5311TH143860 FRAME BOEING727 72725 1384006NM BS 1110 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 DAMAGED FRAME AT WL 300, STA 1110, STR 2L PLUS 2 INCHES. REMOVED DAMAGED AREA FROM FRAME AT WL 300 STA 1110 STR 2L, FABRICATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-4 PG 2. 2L73 4F A3WE 19950929001391995092900139NM 1995 9 29 95FDEA00463 119950425A53122024T3080 BULKHEAD BOEING727 72725 1384006NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK IN 950 BULKHEAD LBL 41, WL 182. REPAIRED CRACK IN 950 BULKHEAD AT LBL 41 WL 182 IAW FEDEX 727 SRM 53-10-9. 2L73 4F A3WE 19950929001401995092900140NM 1995 9 29 95FDEA00464 119950425A53207075T6 FAILSAFE CHORD BOEING727 72725 1384006NM BS 1110 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACKED FAILSAFE CHORD BS 1110 STR 24L. REPAIRED CRACKED FAILSAFE CHORD AT BS 1110 STR 24L AS PER FEDEX SRM 51-40-4. 2L73 4F A3WE 19950929001411995092900141NM 1995 9 29 95FDEA00465 119950425A53302024T3080 SKIN BOEING727 72725 1384006NM BS 294.5 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 294.5 BETWEEN STR 24L AND 25L, THERE IS A LIGHTNING STRIKE. BLENDED AREA BS 294.5 BETWEEN STR 24L TO 25L AND FABRICATED DOUBLER, INSTALLED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950929001421995092900142NM 1995 9 29 95FDEA00466 119950425A5315BAC15123396 FLOORBEAM BOEING727 72725 1384006NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) ON FLOORBEAM AT BS 680 RBL 10 WL 208. REMOVED AND REPLACED TOP CHORD ON FLOORBEAM AT BS 680 LBL 10 TO RB 15, WL 208 PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19950929001431995092900143NM 1995 9 29 95FDEA00467 119950425A53302024T3 SKIN BOEING727 72725 1384006NM BS 460-520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 460-520 BETWEEN STR 20R TO 21R THERE IS A DENT IN SKIN THAT OIL CANS. CUT OUT DAMAGED AREA FABRICATED REPAIR DOUBLER ALODINE AND PRIMERED, INSTALLED WET WITH SEALANT, INSTALLED FASTENERS IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950929001441995092900144NM 1995 9 29 95FDEA00468 119950425A53122024T3 BLKHD WEB BOEING727 72725 1384006NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK IN 950 BULKHEAD RBL 22 WL 166. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 166 PER FEDEX SRM 53-10-9. 2L73 4F A3WE 19950929001451995092900145NM 1995 9 29 95FDEA00469 119950425A53122024T3 BLKHD WEB BOEING727 72725 1384006NM BS 950 CARCKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK IN 950 BULKHEAD RBL 22 WL 183. REPAIRED CRACK IN 950 BULKHEAD RBL 22 WL 183 PER FEDEX SRM 53-10-9. 2L73 4F A3WE 19950929001461995092900146NM 1995 9 29 95FDEA00470 119950425A53117075T6 FRAME BOEING727 72725 1384006NM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACKED FRAME AT BS 1090 LBL 22 UNDER FLOOR TO SIDEWALL SUPPORT WL 150. REPAIRED CRACKED FRAME PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950929001471995092900147NM 1995 9 29 95FDEA00471 119950425A53302024T3050 SKIN BOEING727 72725 1384006NM BS 251.6 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 251.6 STR 22R, POSSIBLE CRACK IN SKIN AT FASTENER. REPAIRED CRACK IN SKIN PER FEDEX SRM 53-30-3 BS 251.6 STR 22R. 2L73 4F A3WE 19950929001481995092900148NM 1995 9 29 95FDEA00472 119950425A575165192596 HINGE BOEING727 72725 1384006NM RT AILERON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 RT WING O/B AILERON, OTBD CENTER HINGE FITTING CRACKED. REMOVED CRACKED FITTING, INSTALLED NEW FITTING. 2L73 4F A3WE 19950929001491995092900149NM 1995 9 29 95FDEA00473 119950425A53207075T6 STIFFENER BOEING727 72725 1384006NM BS 254 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 254 WL 173, RBL 25 HORIZONTAL STIFFENER IS CORRODED. BLENDED OUT AND REMOVED CORROSION, CUT AND TRIMMED OFF FLANGE. FABRICATED A NEW REPAIR PART, ALODINED, PRIMED, PAINTED PART, INSTALLED PART WET WITH SEALANT. ALL WORK ACCOMPLISHED IAW FEDEX (EA 7-5310-24450) AT BS 254 WL 173 RBL 25 HORIZONTAL STIFFENER. 2L73 4F A3WE 19950929001501995092900150NM 1995 9 29 95FDEA00474 119950425A5347 SEAT TRACK BOEING727 72725 1384006NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSIN ON SEAT TRACK BS 48 RBL 45 WL 208. ALSO, AT BS 578 RBL 45 SHEARED FASTENER AT 480 RBL 45. REMOVED AND REPLACED SEAT TRACK AT RBL 45, WL 208 BS 480 TO 580 IAW FEDEX SRM 53-10-5. ALSO, REPLACED SHEARED FASTENER AT RBL 45, BS 480 REINSTALL AND REMOVED ANGLE AT WEB. 2L73 4F A3WE 19950929001511995092900151NM 1995 9 29 95FDEA00475 119950425A53207075T6 WEB BOEING727 72725 1384006NM BS 254-259 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION UNDER WEB 254 TO 259 RBL 48 WL 224. REMOVED CORRODED DOUBLER STA 254 TO 259 RBL 48 WL 224, FABRICATED NEW DOULBER, ALODINED, PRIMED, INSTALLED. 2L73 4F A3WE 19950929001521995092900152NM 1995 9 29 95FDEA00476 119950425A53302024T3 SKIN BOEING727 72725 1384006NM BS 1183-1342 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION AND GOUGE ON SKIN BS 1183 TO 1342 STR 20 TO 27L. REMOVED CORROSION FROM SKIN AND INSTALLED DOUBLER OVER AREA WHERE SKIN WAS REMOVED DUE TO GOUGE. IAW FEDEX SRM 53-30-3. 2L73 4F A3WE 19950929001531995092900153NM 1995 9 29 95FDEA00477 119950425A53157075T6M400877 FLOORBEAM BOEING727 72725 1384006NM BS 660 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION IN THE FWD CARGO BAY THERE IS CORROSION ON LOWER FLANAGE OF FLOORBEAM AT NUTPLATE LOCATION BS 660 RBL 14 WL 200. BLENDED AND REMOVED CORROSION ON FLOORBEAM, ORIGINAL THICKNESS OF MATERIAL 133 REMOVED .027 5 BY 1 AREA, FLOORBEAM, OUT OF LIMITS PER FEDEX (53-10-1) FABRICATED AND INSTALLED A STRAP, PER FEDEX EA 7-5310-24461. 2L73 4F A3WE 19950929001541995092900154NM 1995 9 29 95FDEA00478 119950425A5347BAC1520 TRACK BOEING727 72725 1384006NM BS 559 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON SEAT TRACK BS 559 LBL 45 WL 208 AND BS 620 TO 628. ALSO, BS 641 AND 601. REPLACED SECTION OF SEAT TRACK FROM BS 550 TO 650 LBL 45 WL 208 IAW FEDEX SRM 53-10-5. 2L73 4F A3WE 19950929001551995092900155NM 1995 9 29 95FDEA00479 119950425A53137075T6BAC1498142STRINGER BOEING727 72725 1384006NM BS 990 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACKED STR 6L AT BS 990 WL 288. REPAIRED STR 6L AT BS 990 WL 288 PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19950929001561995092900156NM 1995 9 29 95FDEA00480 119950425A53157075T6 FLOORBEAM BOEING727 72725 1384006NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION AROUND FLOORBOARD FASTENER HOLES ON UNDERSIDE OF THE FLOORBEAM AT STA 1110 RBL 9 TO RBL 44. FOUND CORROSION BEYOND LIMITS. REPAIRED 1110 FLOORBEAM PER EA 7-53-10-24462. 2L73 4F A3WE 19950929001571995092900157NM 1995 9 29 95FDEA00481 119950425A5315BAC1505100246 FLOORBEAM BOEING727 72725 1384006NM BS 312 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) ON 312 FLOORBEAM WL 208 LBL 3, 23 AND 48. CORROSION FOUND BEYOND LIMITS. REPLACED FLOORBEAM BS 312 WL 208 RBL 4.5 TO LBL 55 PER EA 7-5310-24463. 2L73 4F A3WE 19950929001581995092900158NM 1995 9 29 95FDEA00482 119950425A53157075T6063 FLOORBEAM BOEING727 72725 1384006NM BS 480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) UNDER FLANGE OF FLOORBEAM BS 480 LBL 27, 43 AND RBL 48 WL 208. REMOVED CORROSION, DETERMINED TO BE OUT OF LIMITS. REPAIRED AFFECTED AREAS PER EA 7-5310-24479. 2L73 4F A3WE 19950929001591995092900159NM 1995 9 29 95FDEA00483 119950425A5320BAC1505100617 CHORD BOEING727 72725 1384006NM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION (72C235-02) ON FLOORBEAM AT BS 620 LBL 31 AND LBL 42 WL 208 AND RBL 10-13. REMOVED AND REPLACED FLOORBEAM UPPER CHORD AT BS 620 RBL 35 TO LT OUTBOARD END. FABRICATED CHORD AND REPLACED AS PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19950929001601995092900160NM 1995 9 29 95FDEA00484 119950425A53207075T6063 CHORD BOEING727 72725 1384006NM BS 259 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 259 WL 172 LBL 27 CHORD CORRODED. REMOVED CORROSION ON CHORD, OUT OF LIMITS PER FEDEX SRM 53-10-1. DRILLED ALODINED PRIMED AND INSTALLED REPAIR STRAP PER FEDEX EA 7-5310-24483. 2L73 4F A3WE 19950929001611995092900161NM 1995 9 29 95FDEA00485 119950425A53302024T3090 SKIN BOEING727 72725 1384006NM BS 360 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 360 STR 246 THERE IS A GOUGE ON EXTERIOR SKIN. FOUND GOUGE TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED DAMAGED AREA AT BS 360 STR 246 IAW FEDEX EO 7-5330-7-23196 PART 5 AND DRAWING 69-62161. 2L73 4F A3WE 19950929001621995092900162NM 1995 9 29 95FDEA00486 119950425A532065184175 STIFFENER BOEING727 72725 1384006NM BS 294.5 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CORROSION ON HORZ STIFFENER HORIZ FLANGE AT BS 294.5 TO 15 INCHES LBL 10 TO RBL 10 WL 182. REMOVED AND REPLACED HORIZONTAL STIFFENER AT BS 294.5 LBL 10 TO RBL 10 WL 183. 2L73 4F A3WE 19950929001631995092900163NM 1995 9 29 95FDEA00487 119950425A5530040 FRAME BOEING727 72725 1384006NM VERT FIN DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 L/T VERTICAL FIN FRAME AT LBL 11 FIN STA 267 WL 420 UNDER PANEL 9601 HAS A FASTENER THAT HAS PULLED THROUGH. REPAIRED AREA ON L/T VERTICAL FIN FRAME AT LBL 11 FINE STA 267 WL 420 IAW EA 7-5510-24465. 2L73 4F A3WE 19950929001641995092900164NM 1995 9 29 95FDEA00488 119950425A52307075T6 FRAME BOEING727 72725 1384006NM CARGO DOOR GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 MAIN CARGO DOOR AFT FRAME LOWER SECTION IS GOUGED ON INNER RADIUS APPROXIMATELY 75 PERCENT OF MATERIAL THICKNESS, BS 620 LBL 60 WL 218. REPAIRED DAMAGE OF MAIN CARGO DOOR AFT FRAME LOWER SECTION ON INNER RADIUS AT BS 620, LBL 60 WL 218 IAW EA 7-5230-24523. 2L73 4F A3WE 19950929001651995092900165NM 1995 9 29 95FDEA00489 119950425A532065453132 CLIP BOEING727 72725 1384006NM BS 828 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 MECHANICAL DAMAGE ON STR CLIP AT BS 828 STR 7R. REMOVED AND REPLACED STR CLIP AT BS 828 STR 7R ALL WORK DONE IAW FEDEX DRAWING 65-163282. 2L73 4F A3WE 19950929001661995092900166NM 1995 9 29 95FDEA00490 119950425A53302024T3 SKIN BOEING727 72725 1384006NM BS 350 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 BS 350 BETWEEN STR 22 TO 23R THERE IS A DEEP GOUGE ON EXTERIOR SKIN. REPAIRED GOUGE ON EXTERIOR SKIN IAW FEDEX SRM 53-30-3 FIG 1 LOC BS 350 STR 22 TO 23R. 2L73 4F A3WE 19950929001671995092900167NM 1995 9 29 95FDEA00491 119950425A532065C36281 GUSSET BOEING727 72725 1384006NM BS 825.95 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 FRAME GUSSET CRACKED ON INBOARD ROW OF FASTENERS FROM BOTTOM OF GUSSET TO FIRST FASTENER IN ROW STA 825.95, RBL 66.5 WL 197. REMOVED CRACKED FRAME GUSSET AT BS 825 R/T AND INSTALLED NEW GUSSET IAW FEDEX EA 7-5310-24522. 2L73 4F A3WE 19950929001681995092900168NM 1995 9 29 95FDEA00492 119950425A531165C36281 FRAME BOEING727 72725 1384006NM BS 825 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK INDICATION IN SECOND HOLE BELOW FLOOR L/T FRAME AT BS 825. REPAIRED FRAME AT BS 825 L/T IAW FEDEX EA 7-5310-24522. 2L73 4F A3WE 19950929001691995092900169NM 1995 9 29 95FDEA00493 119950425A53112024T3 FRAME BOEING727 72725 1384006NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK INDICATION IN FIRST HOLE ABOVE FLOOR L/T FRAME BS 760. REPAIRED FRAME AT BS 760 L/T IAW FEDEX EA 7-5310-24533. 2L73 4F A3WE 19950929001701995092900170NM 1995 9 29 95FDEA00494 119950425A5311TPN2024T35HT090 FRAME BOEING727 72725 1384006NM BS 848.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 CRACK INDICATION IN THE FIRST AND SECOND FASTENER HOLES BELOW THE FLOOR IN THE R/T FRAME AT BS 848.5. REPAIRED R/T FRAME AT BS 848.5 IAW FEDEX EA 7-5310-24522. 2L73 4F A3WE 19950929001711995092900171NM 1995 9 29 95FDEA00495 119950425A53306545800218 SKIN BOEING727 72725 1384006NM BS 177 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 UPON REMOVAL OF RADOME, FOUND DAMAGE TO SKIN AT BS 177 WL 242 RBL 10 TO LBL 9. REMOVED AND REPLACED SKIN AT BS 177 WL 242 RBL 10 TO LBL 9. 2L73 4F A3WE 19950929001721995092900172NM 1995 9 29 95FDEA00496 119950425A532065C352828 DOUBLER BOEING727 72725 1384006NM WINDOW FRAME CRACK A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 R/T NR 2 WINDOW HAS A CRACK IN THE UPPER QUADRANT OF THE UPPER AFT RADIUS IN THE DOUBLER, CRACK IS NOT CONTAINED. REPAIRED CRACK IN UPPER AFT RADIUS OF R/T NR 2 WINDOW UPPER QUADRANT PER FEDEX EO 7-5330-7-3354 PT 5. 2L73 4F A3WE 19950929001731995092900173NM 1995 9 29 95FDEA00497 119950425A53207075T6 TERMINAL FITTING BOEING727 72725 1384006NM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 SUSPECT INDICATIONS FOUND AT BS 870 L/T TERMINAL FITTING DURING UT INSP, REQUIRES REMOVAL OF FWD AND AFT SPLICE PLATES TO VERIFY INDICATIONS WITH HFEC. REPAIRED BS 870 TERMINAL FITTING LT IAW FEDEX EA 7-5310-24490 AND 7-5310-24491. 2L73 4F A3WE 19950929001741995092900174NM 1995 9 29 95FDEA00498 119950425A53117075T6 FRAME BOEING727 72725 1384006NM BS 804 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25155FE 18288 FRAME IS CRACKED AT BS 804 WL 209 LBL 67 TO 71.REMOVED AND REPLACED FRAME SECTION AT BS 804 LBL 67 TO 71 WL 199 TO 31. 2L73 4F A3WE 19950929001751995092900175NM 1995 9 29 95FDEA00499 119950502A5754 BONDING STRAP BOEING727 72721C 138400MNM NR 1 LE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25144FE 19137 NR 1 K-FLAP O/B LOWER BONDING VAMPER UPPER ATTACH POINT IS CORRODED. CLEANED AND TREATED PER EWO NR 95-2426, CORROSION ON NR 1K-FLAP O/B LOWER BONDING VAMPER ATTACH POINT AS WELL AS FEDEX EA 7-5750-24438. 2L73 4F A3WE 19950929001761995092900176NM 1995 9 29 95FDEA00500 119950502A52107075T6060 DOOR FRAME BOEING727 72721C 138400MNM PAX DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25144FE 19137 AFT ENTRY DOOR L/T SIDE FRAME PREVIOUS REPAIRED CRACK ISN'T CONTAINED AT STOP DRILL (2 PLACES). REMOVED DAMAGED AREA FROM WL 218 TO 239, FABRICATED AND INSTALLED NEW SEGMENT OF FRAME AND SPLICE DOUBLERS PER FED EX SRM 51-40-3. 2L73 4F A3WE 19950929001771995092900177WP 1995 9 29 95ZZZX5164 119950908A2612 FIRE LOOP DOUG DC8 DC863 302198AWP NR 4 ENGINE DIRTY A RRXAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP15964R 46000 KAUS/KDAY - FLT 107 - AFTER TAKEOFF, NR 4 ENGINE FIRE WARNING SOUNDED. THE CREW DISCHARGED FIRE AGENT AND SHUT DOWN NR 4 ENGINE. N964R RETURNED TO KAUS. MAINTENANCE FOUND WATER IN THE FIRE LOOP ELECTRICAL CONNECTOR. MAINTENANCE DRIED AND RESECURED THE ELECTRICAL CONNECTOR ON THE FIRE LOOP AND CHANGED THE FIRE BOTTLE AND SQUIBS. ALL SYSTEMS OPERATED NORMALLY ON GROUND CHECK. 2L74 4F 4A25 19950929001781995092900178WP 1995 9 29 95ZZZX5165 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 218 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAMP SEAM CORROSION, LT TOP FS 218. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001791995092900179WP 1995 9 29 95ZZZX5166 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 301 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION, LT TOP FS 301. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001801995092900180WP 1995 9 29 95ZZZX5167 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 344 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION, LT TOP FS 344. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001811995092900181WP 1995 9 29 95ZZZX5168 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 586-616 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION, LT TOP FS 586 TO FS 616. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001821995092900182WP 1995 9 29 95ZZZX5169 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 720-802 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION, LT TOP FS 720 TO STA 802. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001831995092900183WP 1995 9 29 95ZZZX5170 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 301 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 RIGHT WING ILLUMINATION LIGHT CORRODED STA 301. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001841995092900184WP 1995 9 29 95ZZZX5171 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 330-350 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION, LT SIDE FS 330 TO FS 350. REPAIRED IAW SRM 12-56. 2L74 4R 6A3 19950929001851995092900185WP 1995 9 29 95ZZZX5172 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 NR 5 LT WINDOW LOWER FRAME CORRODED. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001861995092900186WP 1995 9 29 95ZZZX5173 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 NR 7 LT WINDOW UPPER FRAME CORRODED. REPAIRED IAW SM 12-51. 2L74 4R 6A3 19950929001871995092900187WP 1995 9 29 95ZZZX5174 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 NR 8 LT WINDOW UPPER FRAME CORRODED. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001881995092900188WP 1995 9 29 95ZZZX5175 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 NR 9 LT WINDOW FWD AND LWR FRAME CORRODED. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001891995092900189WP 1995 9 29 95ZZZX5176 119950818A5320 DOOR FRAME DOUG DC6 DC6A 3021706WP CARGO COMPT CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 REAR CARGO LWR DOOR FRAME CORRODED. REPLACED LWR DOOR FRAME ASSY. 2L74 4R 6A3 19950929001901995092900190WP 1995 9 29 95ZZZX5177 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP BS 801-843 CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 HEAVY CORROSION TOP RT SIDE OF FS 810 TO FS 843. REPLACED SKIN SECTION. 2L74 4R 6A3 19950929001911995092900191WP 1995 9 29 95ZZZX5178 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 BOTTOM SKIN LWR RT BELLY AFT OF LWR BAGGAGE DOOR CORRODED. REPLACED SKIN SECTION. 2L74 4R 6A3 19950929001921995092900192WP 1995 9 29 95ZZZX5179 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 NR 1 RT WINDOW LWR FRAME CORRODED. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001931995092900193WP 1995 9 29 95ZZZX5180 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 HEAVY CORROSION 3 FEET BELOW NR 1 RT WINDOW. REPAIRED IAW SRM 12-55. 2L74 4R 6A3 19950929001941995092900194WP 1995 9 29 95ZZZX5181 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 RT WING ILLUMINATION LIGHT HAS HEAVY CORROSION. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001951995092900195WP 1995 9 29 95ZZZX5182 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CORRODED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 LAP SEAM CORROSION ABOVE AND FWD OF RT WING ILLUMINATION LIGHT. REPAIRED IAW SRM 12-55. 2L74 4R 6A3 19950929001961995092900196WP 1995 9 29 95ZZZX5183 119950818A5320 WINDOW FRAME DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 RIGHT 2ND TO LAST WINDOW FRAME HAS CRACKS TOP AFT CORNER AND LWR CENTER. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001971995092900197WP 1995 9 29 95ZZZX5184 119950818A5330 SKIN DOUG DC6 DC6A 3021706WP CABIN CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19870TA25491 45518 RIGHT 3RD TO LAST WINDOW LWR FWD CORNER HAS CRACKS AND CORROSION. REPAIRED IAW SRM 12-51. 2L74 4R 6A3 19950929001981995092900198NE 1995 9 29 95ZZZX5185 219950406A7230 DIFFUSER BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 3 ENGINE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11766AT 21999 21999 IND - NR 3 ENGINE HAS A CRACK IN THE OUTER DIFFUSER DUCT. NR 3 ENGINE WAS REMOVED AND REPLACED. 2L73 4F4 F A3WE E2EA 19950929001991995092900199NE 1995 9 29 95ZZZX5186 219950429A7200 ENGINE BOEING727 727208 138407WNM PWA JT8 JT8D9A 52048NE NR 1 DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11780AT 22295 688224 IND - NR 1 ENGINE HAS C1 AND C2 FAN DAMAGE. REMOVED AND REPLACED NR 1 ENGINE. 2L73 4F4 FRTA3WE E2EA 19950929002001995092900200NE 1995 9 29 95ZZZX5187 219950419A7200 ENGINE BOEING727 727227 1384078NM PWA JT8 JT8D9A 52048NE NR 1 DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11779AT 22091 707121 IND - NR 1 ENGINE REQUIRES REPLACEMENT DUE TO BURNER CAN SHIFT AND DAMAGE. NR 1 ENGINE REMOVED AND REPLACED. 2L73 4F4 F A3WE E2EA 19950929002011995092900201 1995 9 29 95ZZZX5188 419950729A25652552032 SLIDE LKHEED1011 1011385115 5265015WP CABIN INFLATED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11194AT 2674 193B1230 JFK - NR 1L SLIDE BLOWN (SLIDE ACCIDENTALLY BLOWN - DOOR AND SLIDE OPERATED NORMALLY). REMOVED AND REPLACED NR 1L SLIDE/RAFT IAW MM 25-61-01. 2L73 4F A23WE 19950929002021995092900202WP 1995 9 29 95ZZZX5189 119950714A2560 GIRT BAR LKHEED1011 10113851 5265010WP CABIN BROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11191AT 193C1084 LAX - R3 DOOR SLIDE ACCIDENTLY DEPLOYED DUE TO GIRT BAR TUBE BROKEN. REPLACED SLIDE. 2L73 4F A23WE 19950929002031995092900203WP 1995 9 29 95ZZZX5190 119950708A28202850301 SHUT-OFF VALVE LKHEED1011 10113851 5265010WP FUEL TANK INOPERATIVE A AAMTAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 GL11188AT 000197 193C1078 DTW - DURING CLIMB THROUGH 26,000 FEET, NR 3 ENGINE TANK VALVE FLOW BAR LIGHT WENT OUT WHICH WAS ASSOCIATED WITH NR 3 ENGINE FLAMING OUT. ENGINE WINDMILL FOR 20 MINUTES OIL PRESS. REPLACED NR 3 ENGINE FUEL TANK SHUT-OFF VALVE IAW MM 28-24-15 AND VALVE SWITCH WAS ALSO REPLACED. SYSTEM TEST OK. 2L73 4F A23WE 19950929002041995092900204 1995 9 29 95ZZZX5191 419950629A25652513217 SLIDE BOEING727 727264 138408MNM DOOR LEAKING A AMTAK NONE O OTHER ININSP/MAINT 1 GL11764AT 000463 22984 IND - RIGHT NR 1 SLIDE IS ZERO PSI. REPLACED R-1 DOOR SLIDE, OK FOR SERVICE. 2L73 4F A3WE 19950929002051995092900205NM 1995 9 29 95ZZZX5192 119950622A26122610015 FIRE DET MODULE BOEING727 727264 138408MNM COCKPIT FAILED A AMTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL11764AT 577 22984 STL - AFTER TAKEOFF WHEN ENGINE POWER WAS RETARDED TO CLIMB EPR, BOTH MASTER F/W LIGHTS ILLUMINATED AND F/W BELL ACTIVATED WITHOUT ANY FIRE. RETURNED TO STL. REMOVED AND REPLACED FIRE DETECTION AND WARNING MODULE. OPS CHECK AND F/W SYSTEM TESTS GOOD ON GROUND. 2L73 4F A3WE 19950929002061995092900206NM 1995 9 29 95ZZZX5193 119950609A2130 CONNECTOR BOEING727 7272Q8 138407WNM CABIN LOOSE A AMTAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11776AT 21608 MCO - ON CLIMB-OUT, COULD NOT MAINTAIN CABIN ALTITUDE. RETURNED TO MCO. CLEANED AND RESEATED CABIN PRESS. CONTROLLER SYSTEM CANNON PLUG. OPS CHECK OK. 2L73 4F A3WE 19950929002071995092900207WP 1995 9 29 95ZZZX5194 119950621A2150 DUCT PLUG LKHEED1011 10113851 5265010WP AIR COND BAY MISSING A AMTAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL11193AT 193C1071 BOS - ON CLIMB-OUT, OVERHEAT LIGHT ON B-LOOP STAYS ON. SINGLE LOOP SELECTED. AREA OVERHEAT LIGHT OFF WHEN PACK FLOW CONTROL VALVE CLOSED. RETURN TO BOS. FOUND PLUG MISSING FROM DUCT FWD OF NR 2 PACK VALVE. RE-INSTALLED PLUG AND RAN NR 2 PACK. ALL CHECKS OK. 2L73 4F A23WE 19950929002081995092900208NM 1995 9 29 95ZZZX5195 119950601A2612 FIRE LOOP BOEING727 727227 1384078NM AFT BODY OUT OF POSITION A AMTAO OTHER N FALSE WARNING CLCLIMB 1 GL11769AT 21998 MCD - ON CLIMB-OUT GOING THROUGH FL 290, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, C/W ABNORMAL PROCEDURES. CLEANED ELECTRICAL CONNECTOR ON FIRE LOOP (AFT BODY). RESPOSITIONED AFT BODY FIRE LOOP. TESTS OK. 2L73 4F A3WE 19950929002091995092900209WP 1995 9 29 95ZZZX5196 119950608A52703151003 SWITCH BOX LKHEED1011 10113851 5265010WP DOOR WARNING INOPERATIVE A AMTAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 GL11181AT 445 193L1125 IND - ON TAKEOFF, NUMEROUS DOOR WARNING LIGHTS ILLUMINATED. RETURNED TO IND. REMOVED AND REPLACED PROXIMITY SWITCH CARD J-27, J-24 SWITCH BOX. 2L73 4F A23WE 19950929002101995092900210NM 1995 9 29 95ZZZX5197 119950522A33503322045 EEL BATTERY BOEING757 7572Q8 1384972NM CABIN DISCHARGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11755AT827 24965 MDW - ON DAILY SERVICE CHECK, FOUND AFT AISLE LIGHTS (EMERGENCY) WOULD NOT ILLUMINATE. REMOVED AND REPLACED AFT POWER SUPPLY PER 33 IN MM. OPS CHECK GOOD. 2L72 4F RTA2NM 19950929002111995092900211NM 1995 9 29 95ZZZX5198 119950605A3610 BLEED LINE BOEING727 7272B7 138407LNM NR 2 ENGINE BROKEN A AMTAA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL11762AT 22162 IND - ON CLIMB, NR 2 ENGINE LOW POWER. WITH THROTTLES ALIGNED AND NR 1 AND NR 3 N1'S AT 92 PERCENT, NR 2 EPR DROPPED TO 1.5 EPR AND N1 AT 82 PERCENT. RETURNED TO IND. FOUND 13TH STAGE BLEED VALVE LINE BROKEN AT UPPER END. REMOVED AND REPLACED BLEED LINE. ACCOMPLISHED BLEED VALVE CHECK AND ENGINE OPS CHECK OK. 2L73 4F A3WE 19950929002121995092900212WP 1995 9 29 95ZZZX5199 119950730A21502150314 ACM LKHEED1011 10113851 5265010WP AIR COND BAY FAILED A AMTAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL11197AT 826536 193P1082 HNL - ON THE GROUND, THE NR 1 AIR CONDITIONING PACK MAKES A LOUD RUMBLE AND WHINING NOISES, SMOKE IN AFT CABIN AND FLIGHT DECK. SECURED PACK. ALL TEMPS WITHIN NORMAL RANGE. NO OVERHEAT LIGHTS. DEFERRED PER MEL 21-51-01. REMOVED AND REPLACED NR 1 ACM. SYSTEM LEAK CHECK AND OPS CHECK NORMAL. 2L73 4F A23WE 19950929002131995092900213WP 1995 9 29 95ZZZX5200 119950530A5330 SKIN LKHEED1011 10113851 5265010WP BS 983 CORRODED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11193AT 1071 DURING C-3 CHECK, SKIN CORROSION WAS DETECTED FS 983 BETWEEN STR 33 AND STR 34. A SECTION OF SKIN, 7 FEET BY 4 FEET, WAS REPLACED AT FS 983 BETWEEN STR 33 AND STR 34 PER SRM 53-31-00, FIGURE 826. 2L73 4F A23WE 19950929002141995092900214NE 1995 9 29 95ZZZX5201 219950828A7261 B-NUT DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE NR 1 ENGINE LOOSE A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE05929L 47174 IAH - FLT 309 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 2123, DUE TO DECREASING OIL QUANTITY. FOUND OIL LINE B-NUT LOOSE ABOVE OIL FILTER. TORQUED B-NUT, SERVICED ENGINE OIL. ENGINE LEAK CHECKED AND OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 36,069 HOURS; 35,139 CYCLES. CHECK C - 9-18-94 - STL. 2L72 4F4 F A6WE E2EA 19950929002151995092900215NM 1995 9 29 MALA954588 119950819A523085230400 SKIN DHAV DHC8 DHC8102 2809003NM CARGO DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15828MA 333 BNA - DURING A C-CHECK INSPECTION, THE CARGO DOOR SKIN HAD IMPACT DAMAGE AT STA 2110 AND STA X554. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A DOUBLER IAW RD8-52-188. (X) 2H72 4T RTA13NM 19950929002161995092900216NM 1995 9 29 MALA954589 119950819A534785320490 SEAT TRACK DHAV DHC8 DHC8102 2809003NM LT INBOARD CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15828MA 333 BNA - DURING A C-CHECK INSPECTION, CORROSION WAS FOUND ON THE LEFT INBOARD SEAT TRACK A STA X231. REPAIRS WERE COMPLETED BY SPLICING IN A NEW SECTION OF TRACK IAW RD8-53-1491. (X) 2H72 4T RTA13NM 19950929002171995092900217SW 1995 9 29 MALA954590 119950820A57302731321SE0202 SKIN SWRNGNSA227 SA227AC 8780603SW WS 197 DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL1560NE AC760B MSP - DURING A SCHEDULED INSPECTION, THE RIGHT LOWER WING SKIN WAS FOUND DENTED AT WS 197.00. REPAIRS WERE COMPLETED BY INSTALLING A SURFACE DOUBLER AW FAC SRM 57-90-20. (X) 1L72 4T A8SW 19950929002181995092900218NE 1995 9 29 MALA954593 219950818A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LEFT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15866MA 366 DTW - FLT 3005 - IN CRUISE FLIGHT, THE NR 1 ENGINE TORQUE BEGAN TO ERRATICALLY SURGE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT ENGINE. INVESTIGATION IS CONTINUING. (X) 2H72 4T4 TRTA13NM E20NE 19950929002191995092900219SW 1995 9 29 MALA954595 119950820A54002735025067 FORMER SWRNGNSA227 SA227AC 8780603SW NAC STA 120 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 MSP - DURING A SCHEDULED INSPECTION, THE LT INBD FORMER, PN 27-35025-067, AND STR, PN 27-35041-012, WERE FOUND CRACKED AT NACELLE STA 120.00. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW FAC LAR NR 95-MALA-225. (X) 1L72 4T A8SW 19950929002201995092900220SW 1995 9 29 MALA954601 119950823A324631418 WHEEL SWRNGNSA227 SA227AC 8780603SW NLG OUT OF BALANCE A MALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL1563NE AC763B YQT - FLT 3087 - ON CLIMB-OUT, THE AIRCRAFT EXPERIENCED A VIBRATION UNTIL SHORTLY AFTER THE GEAR WAS UP AND LOCKED. THE AIRCRAFT RETURNED TO YQT. MAINTENANCE REPLACED THE NOSE WHEEL/TIRE ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 1L72 4T A8SW 19950929002211995092900221SW 1995 9 29 MALA954604 119950827A52102724044010 CORNER SWRNGNSA227 SA227AC 8780603SW PASSENGER DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR LOWER FORWARD CORNER CRACKED AT THE NUTPLATE GAS SPRING ATTACH PLATE. REPAIRS WERE COMPLETED BY REPLACING THE LOWER FORWARD PASSENGER DOOR CORNER IAW FAC MM 51-00-00 AND MM 51-40-01. (X) 1L72 4T A8SW 19950929002221995092900222SW 1995 9 29 MALA954605 119950827A54002735001 ANGLE SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT THE 10TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 54-20-9101. (X) 1L72 4T A8SW 19950929002231995092900223SW 1995 9 29 MALA954606 119950827A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT NACELLE INBOARD WING TO NACELLE ATTACH ANGLE CRACKED AT THE 9TH RIVET HOLE OF THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X) 1L72 4T A8SW 19950929002241995092900224SW 1995 9 29 MALA954607 119950827A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW CARGO COMPT CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15445MA AC687 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE AFT CARGO DOOR FRAME AT FS 491.00 HAD A RADIAL CRACK IN THE GAS STRUT ATTACH HOLE AREA. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, FILLER AND DOUBLER IAW ARP 53-20-9503. (X) 1L72 4T A8SW 19950929002251995092900225SW 1995 9 29 MALA954614 119950831A53202722085 FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 MSP - DURING A SCHEDULED INSPECTION, FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 491 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, PLATE, AND FILLER IAW ARP 53-20-9503. (X) 1L72 4T A8SW 19950929002261995092900226SW 1995 9 29 MALA954615 119950831A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW BS 438 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 MSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 438 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20-9503. (X) 1L72 4T A8SW 19950929002271995092900227SW 1995 9 29 MALA954616 119950901A5730 SKIN SWRNGNSA227 SA227AC 8780603SW LT WING LE DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423MA AC636 MSP - DURING PRE-FLIGHT INSPECTION, THE CREW NOTED A BIRD STRIKE DENT ON THE LEFT WING EXTENSION. MAINTENANCE PERSONNEL REPAIRED THE WING DENT BY REMOVING A 11.75 INCH SECTION OF LEADING EDGE SKIN AND REPLACING IT WITH A FLUSH PATCH AND REPAIR SPLICE IAW FAIRCHILD SRM 57-90-20. (X) 1L72 4T A8SW 19950929002281995092900228WP 1995 9 29 NOCA0795 119950818A3350 EEL DOUG DC9 DC983 3022083WP CABIN INOP A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15183NA 49808 DURING PERFORMANCE OF DAILY CHECK 8-17-95 AT JFK, FOUND EMERGENCY EGRESS LIGHT INOP BY SEATS 28 DEF AND 31 DEF. RESECURED WIRES AND TRACK COVERS. OPS CHECK OKAY. (X) 2L72 4F RTA6WE 19950929002291995092900229NE 1995 9 29 SRAA99504 219950908A7200 ENGINE DOUG DC8 DC873F 302199FWP GE CFM56 CFM562C1 13802NE NR 4 FLAMED OUT A SRAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 SO19875SJ 46063 SEATTLE/TOLEDO - FLT 807 - DURING FLIGHT, NR 4 ENGINE FLAMED OUT AT FL 37.0. SHUT DOWN ENGINE, DESCENDED TO FL 21.0, AND RE-STARTED ENGINE, ALL PARAMETERS CHECKED NORMAL. PERFORMED VISUAL INSPECTION TO THE INLET AND EXHAUST. NO DAMAGE NOTED, INSPECT FUEL FILTER, FOUND NO DEFECTS. (X) 2L74 4F4 FRT4A25 E2GL 19950929002301995092900230NE 1995 9 29 SRAA99505 219950911A73207344441 TT2 SENSOR BOEING747 747212B 1384886NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE FAILURE A SRAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SO19745SJ 20888 MIA - FLT 102 - ON DESCENT, NR 2 ENGINE STALLED, EGT WENT TO 780 DEGREES, FUEL FLOW NORMAL, NO RESPONSE TO THROTTLE, MOVED THROTTLE START LEVER TO CUT-OFF POSITION. AFTER ALTITUDE AND EGT STABILIZED, RE-LIT ENGINE, ALL PARAMETERS CHECKED NORMAL. REPLACED TT2 SENSOR, PERFORMED ENGINE RUN-UP, OPS CHECKED GOOD PER MM CHAPTER 71. (X) 2L74 4F4 F A20WE E20EA 19950929002311995092900231NM 1995 9 29 TAOA099501 119950903A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15922TS 9839 20415 OVERHEAD EMERGENCY LIGHT AT FWD CPR AREA INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19950929002321995092900232NM 1995 9 29 TAOA099502 119950903A33500325012 EEL LENS COVER BRUCE BOEING727 727225 1384077NM CABIN MISSING A TAOAK NONE O OTHER ININSP/MAINT 1 EA15922TS 20415 ROW 16 EMERGENCY LIGHT LENS COVER MISSING. REPLACED LENS COVER. OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19950929002331995092900233NM 1995 9 29 TAOA099505 119950911A3350900835A EEL BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15924TS 20175 21041 RIGHT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK ASSEMBLY. OPS CHECK OK PER MM 33-50-0. (X) 2L73 4F A3WE 19950929002341995092900234NM 1995 9 29 9514402281 119950817A7331 POWER SUPPLY BOEING727 727251 138408HNM PWA JT8 JT8D15 52051NE FUEL FLOW FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01281US 21160 DURING TAKEOFF, ALL THREE ENGINE FUEL FLOW INDICATORS WERE INOPERATIVE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL FLOW POWER SUPPLY AND SYSTEM OPERATION RETURNED TO NORMAL. 2L73 4F4 F A3WE E2EA 19950929002351995092900235NE 1995 9 29 9514412707 219950820A7200 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 3 MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01816EA 22553 696537 DURING TAKEOFF, NR 3 ENGINE DID NOT REACH TARGET EPR. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO DISCREPANCIES. AN ENGINE PERFORMANCE RUN VERIFIED THAT FULL TAKEOFF THRUST WAS AVAILABLE. AIRCRAFT CONTINUTED IN SERVICE. 2L73 4F4 F A3WE E2EA 19950929002361995092900236WP 1995 9 29 9514429162 119950922A2740 BRAKE SWITCH DOUG DC9 DC914 3022034WP HORIZONTAL STAB MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018907E 45748 AFTER TAKEOFF, PRIMARY TRIM SWITCH ON CAPTAIN'S YOKE WAS INOPERATIVE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED STABILIZER BRAKE SWITCH AT AFT PEDESTAL. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002371995092900237WP 1995 9 29 9514439881 119950921A3220 TORQUE LINKS DOUG DC9 DC951 3022051WP NLG FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 GL01676MC 47652 DURING TAKEOFF ROLL, EXCESSIVE VIBRATION FROM NOSE GEAR AREA WAS EXPERIENCED. ABORTED TAKEOFF AT APPROXIMATELY 30 KNOTS AND RETURNED TO GATE. REPLACED THE UPPER AND LOWER NOSE GEAR TORQUE LINKS AND BUSHINGS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002381995092900238WP 1995 9 29 9514449945 119950921A2780 RETRACT MECH DOUG DC9 DC931 3022065WP LE FLAPS MALFUNCTIONED A NWAAL ABORTED APPROACH FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 GL018925E 45840 DURING SLAT EXTENSION ON APPROACH INTO MSP, SLAT EXTEND LIGHT BEGAN FLICKERING, THEN EXTINGUISHED AND SLAT DISAGREEMENT LIGHT ILLUMINATED. PERFORMED MISSED APPROACH AND CAPTAIN DECLARED AN EMERGENCY. SUCCESSFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT WITH FLAPS AT 40 DEGREES AND NO SLATS. CYCLED SLATS AND FLAPS SEVERAL TIMES AND DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002391995092900239WP 1995 9 29 9514459104 119950924A2810 FUEL SYS DOUG DC9 DC915 3022036WP LT WING VENTING A NWAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL0194S 47204 AFTER TAKEOFF, FUEL BEGAN VENTING FROM LEFT WING. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PERFORMED BOOST PUMP CHECK VALVE BACKFLUSH PROCEDURE PER MM 28-20-0. FUEL TRANSFER CHECK WAS OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002401995092900240WP 1995 9 29 9514469307 119950922A2421 GENERATOR DOUG DC9 DC982 3022082WP LEFT FAILED A NWAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 GL01309RC 48088 LEFT AC GENERATOR DROPPED OFF LINE AFTER TAKEOFF. ALSO AUTO PRESSURIZATION SYSTEM WAS INOPERATIVE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED LEFT AC GENERATOR AND CSD. ALSO, REPLACED CABIN PRESSURE CONTROLLER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002411995092900241WP 1995 9 29 9514479970 119950919A2131 CONTROLLER DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019334 47247 AFTER TAKEOFF, AUTO-PRESSURIZATION SYSTEM FAILED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND AMPLIFIER. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002421995092900242WP 1995 9 29 9514489945 119950924A2781 INDICATION DOUG DC9 DC931 3022065WP LE FLAPS MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL018925E 45840 DURING APPROACH INTO MSP, AFTER SLATS AND FLAPS WERE EXTENDED FOR LANDING, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTENDED LIGHT. SLATS WERE VISUALLY CONFIRMED TO BE IN EXTENDED POSITION AND AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. REPLACED SWITCH S1-298 AND CONNECTORS P1-373, P1-374. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19950929002431995092900243NM 1995 9 29 95FDEA01406 119950923A2910 LINES BOEING727 727225 1384077NM B-HYD SYST CHAFED A FDEAO OTHER J WARNING INDICATION DEDESCENT 1 SO25469FE 21581 THE B-SYS LOSS NR 1 PUMP IND LOW PRESS, 20 SEC LATER PRESS ZERO, QTY ZERO. CREW REPORTED B-SYS SHUTOFF BEFORE QTY DROPPED. REMOVED AND REPLACED NR 1 AND NR 2 B-SYS CASE DRAIN FILTERS. NO METAL CONTAMINATION FOUND FLL-1365, FILTERS LEAK CK'D OK. FOUND SUPPLY AND CASE DRAIN LINES AT B-PUMP NR 1 CHAFED AND LEAKING. REMOVED AND REPLACED BOTH LINES, LEAK CK'D AND NO LEAKS FOUND. SERVICED HYD QTY IAW MM 29-12-0. 2L73 4F A3WE 19950929002441995092900244NE 1995 9 29 95UAL900117 219950906A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 FLAMEOUT A UALAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 WP294724U 19875 662797 NR 2 ENGINE FLAMEOUT AT FLIGHT LEVEL 370 AND ENGINE RELIT AT FLIGHT LEVEL 350. ACCOMPLISHED FLAMEOUT PROCEDURES. REPLACED NR 2 ENGINE FUEL FILTER AND SUMPED THE A/C FUEL TANKS. NO PROBLEMS NOTED, CAUSE UNKNOWN. 2L74 4F4 F A20WE E20EA 19950929002451995092900245WP 1995 9 29 95UAL900150 119950925A4910 APU INLET DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL AFT FUSELAGE DIRTY A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP291831U 46630 PUNGENT ODOR - SMOKE IN AIRCRAFT (PNEUMATICS SUPPLIED BY APU ONLY). WITH ENGINES RUNNING, IT BECAME WORSE. PROBLEM WAS NOT RELATED TO THE APU. CLEANED APU INLET AREA DUE TO FUEL, OIL AND SKYDROL CONTAMINATION. REPLACED ALL THREE COALESER BAGS. NO ADDITIONAL COMMENTS. 2L73 4F4 F A22WE E23EA 19950929002461995092900246NM 1995 9 29 95UAL900151 119950925A3350 EEL JUMPER BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN BROKEN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29174UA 24381 FLOOR EEL INOP IN E-ZONE RT AISLE AT ROWS 46 TO 52. REPLACED BROKEN JUMPER AT ROW 52. 2L74 4F4 FRTA20WE E24NE 19950929002471995092900247WP 1995 9 29 95UAL900152 119950925A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291839U 46633 EEL LIGHTING STRIP IN RT AISLE OF FIRST CLASS CABIN WILL NOT ILLUMINATE. REPLACED FEEDER CABLE AT DOOR 1 R. 2L73 4F4 F A22WE E23EA 19950929002481995092900248NM 1995 9 29 95UAL900153 119950925A2120 AIR DISTR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE COCKPIT ODOR A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP297452U 21906 PER CREW, SLIGHT BURNING ODOR IN COCKPIT, PLASTIC LIKE SMELL, MOST NOTICABLE NEAR NR 1 CSD TEMP INDICATOR. INTERMITTENT AND ONLY ON RT SIDE OF COCKPIT. INSPECTED AREA BEHIND FLIGHT ENGINEER S-PANEL AND FOUND NOTHING THAT WOULD HAVE CAUSED THE ODOR. NO SUBSEQUENT COMMENTS. 2L73 4F4 F A3WE E2EA 19950929002491995092900249SO 1995 9 29 COMA9511972 119950921A27523082001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO011117H11110300 120117 DURING LANDING, FLAP CONTROL FAULT WARNING. REPLACED THE NACELLE FLAP ACTUATOR. 2L72 4T RTA31SO 19950929002501995092900250EU 1995 9 29 COMA9531161 119950925A32465009237 INNER RACE SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01361C 9806 9806 340A056 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL SUBASSY IS BEING SENT TO ABS FOR SECOND REPAIR AND REMOVED FROM SERVICE. 2L72 4T RTA52EU 19950929002511995092900251EU 1995 9 29 COMA9531162 119950925A324650092371 INNER RACE SAAB SF340 SF340A 7850100EU LT MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 3362 340A140 MECHANIC REMOVED WHEEL ASSY FROM A/C DUE TO TIRE WORN TO LIMITS. DURING INSPECTION FOUND INNER RACE SPUN. WHEEL ASSY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19950929002521995092900252EU 1995 9 29 COMA9531163 119950922A33506104781 EEL BATTERY PACK SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01320CA 340A064 FLOOR PROXIMITY EMERGENCY LIGHTING AT ROW 5 IS INOP. REPLACED EMERGENCY LIGHTING BATTERY PACK. 2L72 4T RTA52EU 19950929002531995092900253NE 1995 9 29 COMA9531164 319950923A6110 PROPELLER SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE LEFT MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01359CA 340A053 276684 DURING FINAL APPROACH, THE LT PROPELLER RPM WAS 100 RPM LOW. REPLACED THE LT PROPELLER ASSY. 2L72 4T RTA52EU 6 CP61GL 19950929002541995092900254WP 1995 9 29 DHL95802004 119950920A3240 BRAKES DOUG DC8 DC873 302199CWP RT MLG GRABBING A TDHLACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01802DH 46076 REJECTED TAKEOFF, SUSPECTED FLAT TIRE OR BRAKE GRABBING. INSPECTED RIGHT TIRES AND BRAKE, NO FAULTS NOTED AND THE BRAKES OPERATE NORMALLY. 2L74 4F RT4A25 19950929002551995092900255 1995 9 29 P5CA9500778 419950923A23106223371002 HF COUPLER BOEING747 747122 1384872NM NR 2 FAILED A P5CAO OTHER O OTHER CRCRUISE 1 WP23850FT 19755 DUE TO RAPID INCREASE IN CABIN ALTITUDE WHEN NR 2 HF SYSTEM KEYED, PASSENGER MASKS DEPLOYED AND OXYGEN ACTIVATED. REPLACED HF COUPLER, STOWED ALL MASKS AND RESET 02 FLOW CONTROL. 2L74 4F A20WE 19950929002561995092900256NM 1995 9 29 P5CA9500779 119950924A2720 LIMITER BOEING747 747123 1384873NM RUDDER INTERMITTENT A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23858FT 20109 DURING PUSHBACK, RUDDER RATIO LIGHT CAME ON. FOUND RUDDER TRAVEL LIMITED. ACTUATED TEST SWITCH ON UPPER RUDDER CONTROL UNIT, LIGHT EXTINGUISHED AND BOTH RUDDERS MOVE FULL TRAVEL. 2L74 4F A20WE 19950929002571995092900257 1995 9 29 P5CA9500780 419950924A2312 PANEL BOEING747 747132 1384882NM VHF 1/2 MALFUNCTIONED A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23857FT 20246 WHILE IN POSITION AND HOLDING FOR TAKEOFF, EXPERIENCED FAILURE OF VHF NR 1 AND VHF NR 2. DISCONNECTED ELECTRONICS BAY AUDIO SELECTOR PANEL PLACARDED AND DISPATCHED. 2L74 4F A20WE 19950929002581995092900258NM 1995 9 29 P5CA9500781 119950924A80117265746 STARTER BOEING747 747123 1384873NM NR 4 ENGINE FAILED A P5CAE ENGINE SHUTDOWN J WARNING INDICATION TXTAXI/GRND HDL 1 WP23859FT 20326 ORD - ON TAXI, NR 4 ENGINE STARTER LIGHT CAME ON. SHUTDOWN ENGINE AND CLOSED BLEED VALVE. FOUND STARTER FAILED, SHEARED COUPLER AND BLOWN DUCT. REPLACED DAMAGED UNITS AND STARTER SHUTOFF VALVE. 2L74 4F A20WE 19950929002591995092900259NM 1995 9 29 P5CA9500782 119950922A5532 PANEL BOEING747 747122 1384872NM VERT STAB PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 HOLE IN AFT WEB OF VERTICAL STABILIZER AT THE OPENING FOR THE UPPER RUDDER ACTUATOR. REMOVED DAMAGED AREA AND REPAIRED PER BOEING SRM 51-40-3. 2L74 4F A20WE 19950929002601995092900260NM 1995 9 29 P5CA9500783 119950922A5280 DOUBLER BOEING747 747122 1384872NM RT MLG DOOR CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 CRACKED DOUBLER, RIGHT WING GEAR FLYING DOOR LEADING EDGE. REPAIRED PER BOEING SRM 52-80-00. 2L74 4F A20WE 19950929002611995092900261NM 1995 9 29 P5CA9500784 119950922A7820 CASCADE VANE BOEING747 747122 1384872NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 NR 3 ENGINE OUTBOARD NR 5 CASCADE VANE HAS CORROSION AND BROKEN VANE. BLENDED BROKEN VANE AND CORRODED SURFACE PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950929002621995092900262NM 1995 9 29 P5CA9500785 119950922A7820 CASCADE VANE BOEING747 747122 1384872NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 NR 3 ENGINE, OUTBOARD NR 7 AND NR 8 CASCADE VANES CORRODED. REMOVED CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950929002631995092900263NM 1995 9 29 P5CA9500786 119950922A7820 CASCADE VANE BOEING747 747122 1384872NM NR 3 ENGINE CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 NR 3 ENGINE, INBOARD NR 15 AND 17 CASCADE VANE CORRODED. BLENDED OUT CORROSION PER BOEING SRM 51-10-01. 2L74 4F A20WE 19950929002641995092900264NM 1995 9 29 P5CA9500787 119950922A2621 BRACKET BOEING747 747122 1384872NM NR 3 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 NR 3 PYLON FIRE EXTINGUISHER BOTTLE AT SUPPORT BRACKET CRACKED, ON INBOARD END. MANUFACTURED AND INSTALLED REPAIR PARTS PER BOEING SRM 54-11-03. 2L74 4F A20WE 19950929002651995092900265NM 1995 9 29 P5CA9500788 119950922A5400 BRACKET BOEING747 747122 1384872NM NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 SUPPORT BRACKET CRACKED, NR 3 ENGINE BLEED AIR RELIEF VALVE, 9 O'CLOCK POSITION. WELD REPAIRED PER BAC5975. 2L74 4F A20WE 19950929002661995092900266WP 1995 9 29 SCNA95193 119950920A2560199821001 SLIDE INDICATOR DOUG DC10 DC1010 3022110WP R3 DOOR FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46905 THE R-3 DOOR SLIDE WOULD NOT TEST. REPLACED THE R-3 DOOR TEST INDICATOR AND SLIDE TESTED GOOD PER MM 25-61-03. 2L73 4F A22WE 19950929002671995092900267 1995 9 29 SCNA95194 419950920A25655WD230500203 SLIDE DOUG DC10 DC1010 3022110WP L3 DOOR FAULTY A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46905 THE L-3 DOOR SLIDE WOULD NOT TEST. REPLACED THE L-3 DOOR SLIDE IAW MM 25-61-01 AND THE SLIDE TESTED GOOD. 2L73 4F A22WE 19950929002681995092900268NM 1995 9 29 UPS204491 119950922A5744 BOLTS BOEING727 727185C 138406NNM NR 3 FLAP TRACK SHEARED A AIPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE NR 3 FLAP TRACK SPOILER BEAM BOLTS WERE SHEARED. MAINTENANCE REMOVED AND INSTALLED NEW BOLTS, FABRICATED NEW SHIM AND INSTALLED. ALL WORK DONE IAW MM 27-51-31-AND 51-30-2. 2L73 4F A3WE 19950929002691995092900269NM 1995 9 29 UPS204492 119950922A5210 SEAL DEPRESSOR BOEING727 727185C 138406NNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOORWAY SEAL DEPRESSOR BELOW LOWER HINGE CUTOUT. MAINTENANCE REMOVED THE OLD SEAL DEPRESSOR, FABRICATED NEW SEAL DEPRESSOR AND INSTALLED PER SRM 51-10-2, 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950929002701995092900270NM 1995 9 29 UPS204493 119950922A5210 FRAME BOEING727 727185C 138406NNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR AFT FRAME AT THE LOWER AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR AFT FRAME PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1. 2L73 4F A3WE 19950929002711995092900271NM 1995 9 29 UPS204494 119950922A5210 GATE BEAM BOEING727 727185C 138406NNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER GATE BEAM IN THE OUTBOARD RADIUS. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR UPPER GATE BEAM PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1, 51-20-1 AND MM 51-20-151. 2L73 4F A3WE 19950929002721995092900272NM 1995 9 29 UPS204495 119950922A5210 FRAME BOEING727 727185C 138406NNM FWD ENTRY DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE FORWARD FRAME ON THE FORWARD ENTRY DOOR AT THE LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR FORWARD FRAME PER SRM 51-10-1 AND 51-20-1. 2L73 4F A3WE 19950929002731995092900273NM 1995 9 29 UPS204496 119950922A5210 GATE BOEING727 727185C 138406NNM FWD ENTRY DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION IN THE FORWARD ENTRY DOOR LOWER GATE AT CENTER ROD ATTACHING POINT. MAINTENANCE REMOVED AND REPLACED THE FWD ENTRY DOOR LOWER GATE PER SRM 51-10-2, 51-30-2, 51-20-4, 51-10-1 AND 51-20-1 AND MM 51-20-151. 2L73 4F A3WE 19950929002741995092900274NM 1995 9 29 UPS204497 119950922A5751 FITTING BOEING727 727185C 138406NNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED A NEW FITTING IAW SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 19950929002751995092900275NM 1995 9 29 UPS204498 119950922A5751 FITTING BOEING727 727185C 138406NNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT WING OUTBOARD AILERON, OUTBOARD CENTER BEARING SUPPORT FITTING ON THE AILERON. MAINTENANCE REMOVED AND INSTALLED NEW FITTING IAW SRM 51-30-2. 2L73 4F A3WE 19950929002761995092900276NM 1995 9 29 UPS204499 119950922A5730 SKIN BOEING727 727185C 138406NNM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE ON THE UPPER SIDE OF THE TOP SKIN AT STATION 870, RBL 45 TO 65 WL 190. MAINTENANCE BLENDED OUT THE CORROSION, FLAP PEENED AREA IAW OHM, TREATED AND INSTALLED REPAIR STRAP IAW UPS EO 727-57-1648. 2L73 4F A3WE 19950929002771995092900277NM 1995 9 29 UPS204500 119950922A5730 UPPER SKIN BOEING727 727185C 138406NNM BS 868-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE THE BOTTOM SIDE OF UPPER SKIN AT STATION 868 TO 870, RBL 63 LBL 63. MAINTENANCE COMPLIED WITH UPS EO 727-57-1648. 2L73 4F A3WE 19950929002781995092900278NM 1995 9 29 UPS204501 119950922A5320 INTERCOSTAL BOEING727 727108C 1384039NM BS 277-294 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE INTERCOSTAL AT STA 277 TO 294 WL 208. MAINTENANCE REPLACED THE DAMAGED AREA IAW SRM 51-30-2, 51-10-2, 51-10-6 AND 51-20-6. 2L73 4F A3WE 19950929002791995092900279NM 1995 9 29 UPS204502 119950922A5220 LOWER FRAME BOEING727 727108C 1384039NM LT OVERWING EXITCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE LOWER SEAL OF THE LEFT HAND AFT OVERWING EXIT HATCH. MAINTENANCE REMOVED THE LOWER AFT FRAME AND SEAL FORMERS, INSTALLED NEW FRAME AND SEAL FORMER. INSTALLATION IAW SRM 51-30-2, 53-30-01, AND 52-20-1. 2L73 4F A3WE 19950929002801995092900280NM 1995 9 29 UPS204503 119950922A5511 RIB BOEING727 727108C 1384039NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE HORIZONTAL STABILIZER RIGHT HAND INBOARD CLOSURE WEB, INSIDE ACCESS HOLE 9223 AREA, FWD WEB UPPER END WHERE THE WEB ATTACHING BRACKET IS MOUNTED AND EXTENDING 16 INCHES FWD. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW CLOSURE WEB IAW SRM. 2L73 4F A3WE 19950929002811995092900281NM 1995 9 29 UPS204504 119950922A5744 FITTING BOEING727 727108C 1384039NM NR 3 FLAP TRACK CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND A CRACK IN THE TRACK ATTACH POINT, LEFT WING NR 3 FLAP TRACK INBOARD AFT ATTACH FITTING AT SPOILER SUPPORT BEAM. MAINTENANCE REMOVED THE CRACKED ATTACH FITTING, INSTALLED A NEW ATTACH FITTING PER SRM 51-30-2, MM 27-51-31. 2L73 4F A3WE 19950929002821995092900282NM 1995 9 29 UPS204505 119950922A5311 FRAME BOEING727 727108C 1384039NM BS 360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FASTENER HOLES, COMMON TO FRAME AT STATION 360 LBL 48 WL 165, BS 360 LBL 45 WL 165, BS 360 LBL 35 WL 158 AND BS 360 RBL 21 WL 151. MAINTENANCE REPAIRED PER UPS EO 727-53-1667. 2L73 4F A3WE 19950929002831995092900283NM 1995 9 29 UPS204506 119950922A5320 DOUBLER BOEING727 727108C 1384039NM BS 307.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE DOUBLER AT STATION 307.5 TO STA 316, LBL 12.5 WL 181 TO 169. MAINTENANCE REMOVED TRIPLER AND REMOVED CORROSION ON TRIPLER. CORROSION FOUND BEYOND LIMITS, FABRICATED NEW DOUBLER AND TRIPLER, FINAL INSTALLATION PER SRM 51-10-6, 51-30-2, 51-20-4, MM 51-20-0 AND UPS 727-53-1671. 2L73 4F A3WE 19950929002841995092900284NM 1995 9 29 UPS204507 119950922A5511 RIB CHORD BOEING727 727108C 1384039NM RT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE RIGHT HAND HORIZONTAL STABILIZER, INBOARD UPPER CLOSURE WEB CHORD FROM APPROXIMATELY 11.5 TO 24.75 AFT OF HORIZONTAL STABILIZER FRONT SPAR. MAINTENANCE REMOVED, FABRICATED AND REPLACED THE CHORD IAW SRM. 2L73 4F A3WE 19950929002851995092900285NM 1995 9 29 UPS204513 119950922A33501000679 EEL BOEING727 72722C 138400FNM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST TOTAKEOFF 1 SO01942UP 19101 PILOT REPORTED, ON TAKEOFF ROLL EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR AND FWD ENTRY DOOR ILLUMINATED. CYCLED SWITCHES ON OVERHEAD PANEL, UNDER COVER, NO CHANGE AND HAD TO TURN OFF FOR LIGHTS TO EXTINGUISH. FOUND EMERGENCY LIGHT C/B POPPED, RESET D/B. FOUND COCKPIT ENTRY DOOR LIGHT ASSY INOP. REMOVED AND REPLACED COCKPIT ENTRY DOOR EMERGENCY LIGHT ASSY AND OPS CHECKS GOOD. 2L73 4F A3WE 19950929002861995092900286NM 1995 9 29 UPS204514 119950922A3350 EEL BATTERY PACK BOEING727 72722C 138400FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01915UP 19101 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT ABOVE CONTROL CABIN DOOR WILL NOT ILLUMINATED WITH EMERGENCY EXIT LIGHT SWITCH ON. EMERGENCY EXIT LIGHT ASSY BATTERIES REPLACED AND LIGHTS CHECKED SERVICEABLE. 2L73 4F A3WE 19950929002871995092900287NM 1995 9 29 UPS204516 119950923A5753 SKIN BOEING727 72762C 138402CNM LT TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01912UP 19244 WHILE ON GROUND, MAINTENANCE FOUND LEFT INBOARD MIDFLAP TRAILING EDGE DELAMINATED IN SEVERAL PLACES. REPAIRED DELAMINATION IAW B-727 SRM 51-40-6 PAGE 20. 2L73 4F A3WE 19950929002881995092900288NM 1995 9 29 UPS204517 119950925A5320 BEAM BOEING727 727247 138408FNM BS 1040-1060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01208UP 21701 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-06.00-1), LBL 65, STA 1040 TO 1060 WL 208.2 AT NUTPLATES FOR DOOR SILL AT CREASE BEAM. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CREASE BEAM, INSTALLED NEW CREASE BEAM, SEALED AND PAINTED PER SRM 51-10-1, 51-30-2 AND 51-10-2. 2L73 4F A3WE 19950929002891995092900289NM 1995 9 29 UPS40415 119950923A5753 TE CORNER BOEING747 747123 1384873NM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01675UP 20390 WHILE ON GROUND, MAINTENANCE FOUND RIGHT INBOARD MIDFLAP RIGHT HAND TRAILING EDGE CORNER HAS CRACK. ACCOMPLISHED COMPOSITE REPAIR REF SRM 51-40-09. 2L74 4F A20WE 19950929002901995092900290NE 1995 9 29 UPS404508 219950921A7261 COVER PLATE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE LEAKED A IPXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01673UP 20325 PILOT REPORTED TWO HOURS INTO FLIGHT, NR 3 ENGINE OIL QUANTITY INDICATED 3.5 GALLON OIL LOSS. ENGINE WAS SHUTDOWN WITH 1 GALLON REMAINING. OIL TEMPERATURE AND PRESSURE NORMAL. MAINTENANCE FOUND OIL LEAK AT OIL PUMP COVER PLATE LOCATED ON ENGINE GEARBOX NR 3 ENGINE. REMOVED AND REPLACED PACKING ON COVER PLATES, BAGGED ALL OIL DRAIN LINES, RAN ENGINE. OPS AND LEAK CHECK GOOD. 2L74 4F4 F A20WE E20EA 19950929002911995092900291NM 1995 9 29 UPS404512 119950922A5522 TE SKIN BOEING747 747121 1384871NM LT HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01682UP 20349 WHILE ON GROUND, MAINTENANCE FOUND 2 LT HORIZONTAL STAB T/EDGE CRACKED. 2L74 4F A20WE 19950929002921995092900292WP 1995 9 29 UPS804509 119950921A3230 RETRACT MECH DOUG DC8 DC871F 302199DWP NLG MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01772UP 46072 PILOT REPORTED ON FIRST AND SECOND ATTEMPTS TO LOWER GEAR, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE. DURING THIRD ATTEMPT ALL 3 LIGHTS GREEN AND HEARD VERY LOUD SOUND IN NOSEWHEEL AREA. MAINTENANCE LUBED THE NOSE GEAR AND RELAMPED NOSE INDICATOR. RETRACTED AND EXTENDED NOSE GEAR SEVERAL TIMES, ALL CHECK NORMAL. 2L74 4F RT4A25 19950929002931995092900293WP 1995 9 29 UPS804510 119950921A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01806UP 46006 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT DID NOT OPERATE. MAINTENANCE REPLACED THE BATTERY PACK AND LIGHT OPS GOOD. THE OFF (P/N 60-1223-3), (S/N 188) AND ON (P/N 5708458-503), (S/N FT002). 2L74 4F RT4A25 19950929002941995092900294WP 1995 9 29 UPS804511 119950921A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01811UP 46089 WHILE ON GROUND, MAINTENANCE FOUND EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND OPS CHECK GOOD. THE OFF AND ON (P/N 5708458-503), S/N ON FTL 182 AND S/N ON FTL 231. 2L74 4F RT4A25 19950929002951995092900295WP 1995 9 29 UPS804518 119950925A533097558781 SKIN DOUG DC8 DC873F 302199FWP FS 400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGE ON FUSELAGE SKIN AND DOUBLER, STA 400 LONGERON 36. REPAIRED PER UPS EO DC8-5330-7427-A. 2L74 4F RT4A25 19950929002961995092900296WP 1995 9 29 UPS804519 119950925A5311561378415 FRAME DOUG DC8 DC873F 302199FWP FS 67 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME STA 67, BETWEEN LONGERONS 17L TO 21L. REPAIRED PER UPS EO DC8-5310-7429-A. 2L74 4F RT4A25 19950929002971995092900297WP 1995 9 29 UPS804520 119950925A531156138579 FRAME DOUG DC8 DC873F 302199FWP FS 77 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME STA 77, BETWEEN LONGERONS 17L TO 21L. REPAIRED PER UPS EO DC8-5310-7428-A. 2L74 4F RT4A25 19950929002981995092900298WP 1995 9 29 UPS804521 119950925A5311561237617 FRAME DOUG DC8 DC873F 302199FWP FS 52 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LOWER FWD SIDE OF BELT FRAME FS 52, LBL 52 AND FLOORBEAM. REPAIRED PER UPS EO DC8-5310-6902-A. 2L74 4F RT4A25 19950929002991995092900299NE 1995 9 29 9514495523 219950921A7230 COMPRESSOR BOEING757 757251 1384970NM PWA 2037 PW2037 NE NR 1 ENGINE STALLED A NWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01523US 23617 16371 DURING CLIMB, THE NR 1 ENGINE COMPRESSOR STALLED ACCOMPANIED BY POWER LOSS AND YAW TO THE LEFT. ENGINE RECOVERED SHORTLY THEREAFTER WITH NORMAL INDICATIONS. AIRCRAFT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. METAL WAS FOUND IN THE TAILPIPE AND THE ENGINE WAS CHANGED. 2L72 4F4 FRTA2NM E17NE 19950929003001995092900300EU 1995 9 29 9514503214 119950922A7933 OIL TEMP WIRE AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 ENGINE CHAFED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL01314US 160 31408 DURING CLIMB, THE NR 1 ENGINE OIL TEMPERATURE GAUGE INDICATED HIGH. ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. CHAFED WIRES IN THE PYLON SECTION WERE FOUND AND REPAIRED. ENGINE WAS RUN AND LEAK CHECKED OK. AIRCRAFT DEEMED OK FOR SERVICE. 2L72 4F4 FRTA28NM 19950929003011995092900301NE 1995 9 29 9514512295 219950925A7261 SCAVENGE LINE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE BROKEN A NWAAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 GL01295US 21506 696501 NR 1 ENGINE WAS SHUTDOWN AFTER THE OIL SUPPLY HAD BEEN DEPLETED, DUE TO A LEAK AT THE NR 6 BEARING SCAVENGE LINE. THE FLIGHT CONTINUED TO ITS PLANNED DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BROKEN SCAVENGE LINE AND INSPECTED THE ENGINE FOR DAMAGE, NON FOUND. THE SUBSEQUENT RUNUP AND LEAK CHECK WERE SATISFACTORY. 2L73 4F4 F A3WE E2EA 19950929003021995092900302NM 1995 9 29 9514522202 119950921A26121011C FIRE WARNING BOEING727 727251 138408HNM NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01202US9862 9862 22155 DURING TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS, ENGINE FIRE WARNING HORN SOUNDED WITH NO VISUAL INDICATIONS. ABORTED TAKEOFF WITHOUT FURTHER INCIDENT. DETERMINED FALSE WARNING INDICATION AND MAINTENANCE REPLACED NR 1 ENGINE TEST POWER UNIT. OPERATIONAL CHECK WAS NORMAL. 2L73 4F A3WE 19950929003031995092900303NM 1995 9 29 95FDEA01407 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1640 RBL 34 TO 76, UPPER AND LOWER SURFACES HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED FLOORBEAM IAW B747 SRM 51-10-1. 2L74 4F A20WE 19950929003041995092900304NM 1995 9 29 95FDEA01408 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1720 RBL 75 HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED FLOORBEAM IAW B747 SRM 53-10-7. 2L74 4F A20WE 19950929003051995092900305NM 1995 9 29 95FDEA01409 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1800 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1800 RBL 76 TO 119, UPPER CHORD HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED SECTION OF FLOORBEAM UPPER CHORD AND REPAIRED IAW B747 SRM 51-40-04. 2L74 4F A20WE 19950929003061995092900306NM 1995 9 29 95FDEA01410 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1640 LBL 34 TO 76 UPPER CHORD HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED SECTION OF FLOORBEAM IAW B747 SRM 51-40-04. 2L74 4F A20WE 19950929003071995092900307NM 1995 9 29 95FDEA01411 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1660 BL 0 RBL 119, UPPER AND LOWER SURFACES HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED FLOORBEAM IAW B747 SRM 51-10-1. 2L74 4F A20WE 19950929003081995092900308NM 1995 9 29 95FDEA01412 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1740 LBL 60 HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-10-01. 2L74 4F A20WE 19950929003091995092900309NM 1995 9 29 95FDEA01413 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOOR BEAM AT BS 1720 BL 0 - RBL 119 UPPER CHORD HAD CORROSION. CIRCUMSTANCES UNK. R/R FLOOR BEAM IAW B747 SRM 51-10-01. 2L74 4F A20WE 19950929003101995092900310NM 1995 9 29 95FDEA01414 119950919A5315 FLOORBEAM BOEING747 747245F 1384897NM BS 1800 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK FLOORBEAM AT BS 1800 LBL 85 TO 90 UPPER CHORD HAD CORROSION, CIRCUMSTANCES UNK. REMOVED DAMAGED AREA, FABRICATED REPAIR SPLICE IAW B747 SRM 51-40-04, INSTALLED FLOORBEAM T-CHORD IAW B747 SRM 51-40-4 AND INSTALLED REPAIR SPLICE IAW B747 SRM 51-40-04. 2L74 4F A20WE 19950929003111995092900311NM 1995 9 29 95FDEA01415 119950919A5347 SEAT TRACK BOEING747 747245F 1384897NM BS 1710-1740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK SEAT TRACK, LOWER SURFACE AT BS 1710 TO 1740, LBL 99 LOWER SURFACE HAD CORROSION, CIRCUMSTANCES UNK. REMOVED AND REPLACED SEAT TRACK IAW B747 SRM 51-10-01. 2L74 4F A20WE 19950929003121995092900312NM 1995 9 29 95FDEA01416 119950919A5347 SEAT TRACK BOEING747 747245F 1384897NM BS 1800 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25641FE 20827 MAIN CARGO DECK SEAT TRACK BS 1800 RBL 99, CIRCUMSTANCES UNK. REMOVED DAMAGED SECTION, FABRICATED, INSTALLED REPAIR SPLICE AND NEW SEAT TRACK IAW B747 SRM 53-10-05. 2L74 4F A20WE 19950929003131995092900313NM 1995 9 29 DL72S953791 119950921A3350 EEL BATTERY PACK 900835A BOEING727 727232 1384082NM CARGO DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11497DA 4074 21077 DURING LAYOVER, EMERGENCY LIGHT AT C-2 CARGO DOOR INOP. REPLACED BATTERY PACK M957, OPERATION NORMAL. 2L73 4F A3WE 19950929003141995092900314NM 1995 9 29 DL72S953795 119950816A5753652163261 SPAR BOEING727 727232 1384082NM LT TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 DURING SHOP VISIT, FOUND THE NR 2 MIDFLAP AFT SPAR RAIL CRACKED 21 INCHES AND 56 INCHES FROM I/B END OF FLAP. REPAIRED PER M/M57-52-0. 2L73 4F A3WE 19950929003151995092900315NM 1995 9 29 DL72S953799 119950922A5754 ANGLE BOEING727 727232 1384082NM NR 1 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11538DA 22076 FOUND ON A2 LETTER CHECK, NR 1 SLAT COVE SKIN ANGLE CRACKED AT THE OUTBOARD STOP PAD. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950929003161995092900316NM 1995 9 29 DL72S953800 119950922A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11538DA 22076 FOUND ON A2 LETTER CHECK, NUMBER 7 SLAT COVE SKIN ANGLE CRACKED .25 INCH IN UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950929003171995092900317NM 1995 9 29 DL72S953803 119950921A5720 ANGLE BOEING727 727232 1384082NM WING TE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ANGLE CRACKED, WING TRAILING EDGE BELOW NR 8 SPOILER ATTACH BRACKET FOR ACTUATOR. STOP DRILLED CRACK, INSTALLED REPAIR PER M/M 57-20-22 PG 809. 2L73 4F A3WE 19950929003181995092900318NM 1995 9 29 DL72S953811 119950924A3350900835A EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11483DA 20863 DURING EMERGENCY LIGHTS TEST, FOUND EXIT LIGHTS ABOVE BOTH WING EMERGENCY EXITS WERE INOP. REPLACED BATTERY PACK M1086 AND LIGHTS NOW TEST GOOD. 2L73 4F A3WE 19950929003191995092900319NM 1995 9 29 DL72S953814 119950908A5531 RIB BOEING727 727232 1384082NM VERTICAL FIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, FOUND VERTICAL FIN INTERIOR STATION 1303 RIB CRACKED AT BOTTOM. DYE CHECKED AND REPAIRED PER SRM 53-10-4. 2L73 4F A3WE 19950929003201995092900320NM 1995 9 29 DL733953820 119950914A5320 SKIN CLIPS BOEING737 737347 1384647NM FS FRAME 807 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11313WA 23599 DURING HMV, THE SKIN CLIPS WERE FOUND TO BE PITTED BETWEEN STRS 28L AND 28R. THE DAMAGED CLIPS WERE REMOVED AND A REPAIR WAS INSTALLED, ALL PER SRM 53-00-07 FIG 203. 2L72 4F RTA16WE 19950929003211995092900321NM 1995 9 29 DL73S953793 119950922A2170 COALESCER BAGS 213201808 BOEING737 737232 1384475NM LT/RT PACKS DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11323DL 23095 SLC - RETURNED DUE TO SMOKE IN CABIN. SMOKE APPEARED TO DISSIPATE WHEN GALLEY PWR AND GASPER FAN ARE TURNED OFF. SMOKE DID REMAIN IN THE CABIN AND SMELLED TO BE ELECTRICAL IN NATURE. BOTH FRONT AND AFT LAV SMOKE DETECTORS WENT OFF SHORTLY AFTER WE SMELLED THE SMOKE. MAINT CHECKED OVENS, COFFEE MARKERS, CABIN AND LAVS AND ALL FOUND NORMAL. RAN ENGS TO T/O POWER FOR 5 MIN WITH PACKS ON, NO ODORS NOTED. AC HAD BEEN DE-ICED IN DEN, FLUID IN PACK AREA SLIGHT SMELL. REPLACED COALESCER BAGS AND WITH BOTH PACKS ON RUN, NO ODORS. 2L72 4F RTA16WE 19950929003221995092900322NM 1995 9 29 DL73S953810 119950923A33501619 EEL BULB BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11334DL 23105 DURING LAYOVER, RT AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT FAIL TEST. REPLACED BULB, OPERATION NORMAL. 2L72 4F RTA16WE 19950929003231995092900323NM 1995 9 29 DL767953796 119950922A3350 EEL TRACK BOEING767 767232 1385132NM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11108DL 22220 DURING LAYOVER, EMERGENCY TRACK LIGHT DAMAGED NEAR AFT LEFT LAV. FOUND WIRE BROKEN UNDER TRACK. REPAIRED WIRES, OPS CHECK NORMAL. 2L72 4F RTA1NM 19950929003241995092900324NM 1995 9 29 DL767953809 119950924A5754114T410518A SKIN BOEING767 767232 1385132NM NR 8 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 HAIL DAMAGE TO UPPER SURFACE OF NR 7 L/E SLAT. REPLACED WEDGE PER CMM 57-43-61. 2L72 4F RTA1NM 19950929003251995092900325NM 1995 9 29 DL76L953804 119950922A2410 IDG 755359 BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO11176DN L0117 25061 724691 DURING CRUISE, HAD RT GENERATOR DRIVE LIGHT. PER POM DISCONNECTED DRIVE, STARTED APU AND AFTER 20 MIN HAD APU LOW OIL STATUS MSG WITH AUTO SHUTDOWN, DIVERTED DUB. REPLACED NR 2 IDG, SERVICED APU WITH OIL AND RETURNED TO SERVICE. 2L72 4F4 FRTA1NM E24NE 19950929003261995092900326WP 1995 9 29 DLL10953805 119950922A335051066 EEL MODULE LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11725DA 193C1162 DURING LAYOVER CHECK OF EMERGENCY PATH LIGHTS, D-ZONE WOULD NOT ILLUMINATE ON EITHER SIDE WITH POWER OFF TEST. REPLACED INVERTER MODULE AT POWER SUPPLY 8. 2L73 4F A23WE 19950929003271995092900327NM 1995 9 29 DLM88953798 119950922A5320 DOUBLER DOUG MD88 MD88 3023688NM LT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11903DL 49534 DURING D1 LETTER CHECK, FOUND DOUBLER CRACKED AT MLG W/W AFT FRAME T-ANGLE O/B CORNER. REPAIRED PER SRM 53-05. 2L72 4F RTA6WE 19950929003281995092900328NM 1995 9 29 DLM88953801 119950923A3350337201956 EEL LENS DOUG MD88 MD88 3023688NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11936DL 49723 FLOOR TRACK AT SEAT 38D, BULB AND COVER MISSING. REPLACED FLOOR TRACK LIGHT, LENS AND OPS NORMAL. 2L72 4F RTA6WE 19950929003291995092900329WP 1995 9 29 MWEA95316 119950922A2611 SMOKE DETECTOR DOUG DC9 DC932 3022066WP LAVATORY FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31502ME 48132 LEFT HAND SMOKE DETECTOR INOP UPON TESTING WARNING FUNCTION. REMOVED AND REPLACED SMOKE DETECTOR AND OPS CHECK GOOD. 2L72 4F A6WE 19950929003301995092900330 1995 9 29 MWEA95317 419950923A2565113316DME EVAC SLIDE DOUG DC9 DC932 3022066WP PAX DOOR LOW PRESSURE A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31401ME 2434 47133 MAIN DOOR SLIDE FOUND LOW ON PRESSURE. REMOVED AND REPLACED CABIN DOOR SLIDE WITH A SERVICEABLE UNIT. 2L72 4F A6WE 19950929003311995092900331WP 1995 9 29 MWEA95318 119950923A2622466040 PORTABLE FIRE-X DOUG DC9 DC932 3022066WP CABIN BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 FORWARD CABIN HALON FIRE EXTINGUISHER HANDLE BROKE IN HALF, AS THE FLIGHT ATTENDANT WAS CHECKING IT OVER PRIOR TO FLIGHT. REMOVED AND REPLACED WITH A SERVICEABLE EXTINGUISHER. 2L72 4F A6WE 19950929003321995092900332WP 1995 9 29 MWEA95319 119950923A524199115793 DOOR BEAM DOUG DC9 DC932 3022066WP GALLEY DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31202ME 47672 GALLEY SERVICE DOOR UPPER HORIZONTAL BEAM CRACKED .6250 INCH, AT FORWARD END OF THE OUTER RADIUS. REMOVED DOOR AND REPAIRED CRACK IAW SERVICE REWORK DRAWING 5939988. REINSTALLED DOOR, OPS AND PRESSURE CHECKED. 2L72 4F A6WE 19950929003331995092900333WP 1995 9 29 MWEA95320 119950923A5280 SKIN DOUG DC9 DC932 3022066WP NLG DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31202ME 47672 SKIN AROUND LEFT AFT NOSE GEAR DOOR AFT HINGE HAS A PROGRESSING CRACK THROUGH 2 STOP DRILLS. INSTALLED DOUBLER AROUND NOSE GEAR HINGE POINT IAW SRM 53-05 FIGURE 62. 2L72 4F A6WE 19950929003341995092900334WP 1995 9 29 MWEA95321 119950924A3350 EEL DOUG DC9 DC932 3022066WP CABIN DIM A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31502ME 48132 FORWARD OVERWING EXIT EMERGENCY LIGHTS DIM ON LEFT AND RIGHT SIDES. OPS CHECKED EMERGENCY LIGHT SYSTEM AND FOUND ALL LIGHTS TO WORK. 2L72 4F A6WE 19950929003351995092900335WP 1995 9 29 MWEA95322 119950924A2622466040 PORTABLE FIRE-X DOUG DC9 DC932 3022066WP CABIN LEAKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31203ME 4304 47672 FORWARD FLIGHT ATTENDANT'S PORTABLE HALON FIRE EXTINGUISHER, FOUND LEAKED DOWN TO ZERO. REPLACED THE FIRE EXTINGUISHER WITH A SERVICEABLE UNIT. 2L72 4F A6WE 19950929003361995092900336WP 1995 9 29 MWEA95323 119950926A25605917689103 SLIDE COVER DOUG DC9 DC914 3022034WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 45795 GALLEY DOOR SLIDE COVER CAME OFF WHEN OPENED FOR CATERING TRUCK. REPOSITIONED SLIDE IN HOLDER AND REINSTALLED THE DOOR SLIDE COVER. 2L72 4F A6WE 19950929003371995092900337NM 1995 9 29 SCNA95196 119950921A253041600015 COFFEE MAKER BOEING727 727225 1384077NM GALLEY FAILED A SCNAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 GL15282SC 22558 COFFEE MAKER BEGAN SMOKING IN GALLEY. THE CIRCUIT BREAKER WAS PULLED FOR THE COFFEE MAKER AND THE SMOKE CEASED. REMOVED AND REPLACED COFFEE MAKER AND NEW UNIT TESTED GOOD. 2L73 4F A3WE 19950929003381995092900338NM 1995 9 29 UPS204523 119950926A3350 EEL CB BOEING727 72722C 138400FNM CABIN TRIPPED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01942UP 19101 WHILE ON GROUND, MAINTENANCE PREFLIGHT CREW FOUND EMERGENCY LIGHTS CHARGER C/B POPPED. A/C 214 COVERED FLT W/E PHL. 2L73 4F A3WE 19950929003391995092900339NM 1995 9 29 UPS204524 119950921A3350 EEL BOEING727 727247 138408FNM CABIN DIM A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01208UP 21701 EMERGENCY EXIT LIGHTS ARE DIM WITH SWITCH IN OFF POS. TRANSFERRED TO NRC 374590. 2L73 4F A3WE 19950929003401995092900340WP 1995 9 29 UPS804522 119950926A5330SR08530021 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01894UP 46094 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND AFT SERVICE DOOR FWD LOWER CORNER ON FUSELAGE SKIN CUTOUT IS CRACKED. REPAIRED PER UPS EO DC8-5310-7402-A. 2L74 4F RT4A25 19950929003411995092900341CE 1995 9 29 818956LL 119950819A212166001122 BLOWER ELECTROMECH LEAR 25 25D 5170514CE CABIN FAILED A KKFAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL236LL 668 256 COCKPIT FILLED WITH SMOKE AFTER DEPARTING BWI. PILOT SHUT OFF CABIN BLOWER FAN. SMOKE STOPPED. CABIN CLEARED. REPLACED CABIN BLOWER FAN WITH SERVICEABLE UNIT. OPS CHECKED GOOD. 2L72 4J A10CE 19950929003421995092900342NM 1995 9 29 95ZZZX5202 119950905A612030005000024 TSCU PRECISION DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE FAILED A HNAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA072FOR 12609 1017 073 PBY/TPA - FLT 3031 - ON TAKEOFF, THE NR 1 ENGINE PROPELLER FEATHERED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR CONTROL UNIT AND CLEANED BOTH TSCU CONNECTORS. 2H72 4T RTA13NM 19950929003431995092900343NM 1995 9 29 95ZZZX5203 119950905A3260MS3476L833P CONNECTOR DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA072FOR 22376 070 MIA/JAX - FLT 3053 - EN ROUTE TO JAX, THE WEIGHT-ON-WHEELS LIGHT ILLUMINATED, THE GEAR WARNING HORN SOUNDED, THE ROLL OUTBOARD GROUND AND GROUND SPOILER CAUTION LIGHT ILLUMINATED AND THE APU INLET DOOR WOULD NOT OPEN. REMOVED AND REPLACED LEFT OUTBOARD WEIGHT-ON-WHEELS CANNON PLUG AT LANDING GEAR JUNCTION TO NACELLE. 2H72 4T RTA13NM 19950929003471995092900347SO 1995 9 29 95ZZZX5207 119950816A760367639011 CONTROL CABLE PIPER PA32 PA32R300 7103213SO THROTTLE BROKEN APAJIKAA UNSCHED LANDING O OTHER CLCLIMB 1 WP011333H14391 32R7780154 AFTER TAKEOFF, PILOT FOUND THAT THROTTLE MOVEMENT INEFFECTIVE AND HE COULD NOT REDUCE POWER (ENGINE WAS AT FULL TAKEOFF POWER). PILOT RETURNED TO AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE THROTTLE CABLE HAD WORN COMPLETELY THROUGH APPROXIMATELY 3 INCHES FROM THE SWAGED FITTING AT THE ENGINE END OF THE CABLE. THE WIRE ROPE IS CONTAINED IN A HOUSING, AND DUE TO THE FACT THAT BOTH END FITTINGS ARE SWAGED ONTO THE WIRE ROPE, IT IS NOT POSSIBLE TO ACCESS THE CABLE TO INSPECT IT FOR WEAR. 1L71 3O A3SO 19950929003491995092900349CE 1995 9 29 95ZZZX5209 119950915A2820414000153 TRANSFER PUMP DUKES CESSNA401 401A 207590DCE RT OTBD NAC LEAKING A VOXAEO ENGINE SHUTDOWN OTHER AK FLAME/FIRE FLUID LOSS TXTAXI/GRND HDL 1 NM03401WD226 9161 401A0011 AIRCRAFT LANDED AND DURING TAXI OUT, PILOT NOTICED GLOW NEAR RT NACELLE AREA. TOWER REPORTED SUSPECT FIRE. PILOT SHUT DOWN, EXITED AIRCRAFT. FIRE WAS EXTERNAL UNDER WING. FIRE EXTINGUISHED ON ITS OWN. NO DAMAGE TO AIRCRAFT FOUND ON FOLLOW-UP INSPECTION. DUKES PUMP DRAIN LINE IN INTERMEDIATE AREA, PUMP LEAKING FROM DRAIN LINE. EXHAUST IGNITED FUEL ON WING. PUMP WAS CHANGED AT THIS TIME. 1L72 3O A7CE 19950929003941995092900394NE 1995 9 29 95ZZZX5256 219950826A7200 ENGINE BEECH 200 B200 1152922CE PWA PT6 PT6A42 52043NE POWER SECTION FAILED A ACECAEA ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 EA051PD BB908 PCE93722 ENGINE FAILED DURING LEVEL CRUISE FLIGHT AT 13,000 FEET MSL. NO WARNING OR INDICATION OF A PROBLEM PRIOR TO SUDDEN POWER LOSS. SECURED ENGINE AND LANDED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. ENGINE IS TO BE RETURNED TO MANUFACTURER FOR INSPECTION AND REPAIR. DAMAGE APPEARS TO BE EXTENSIVE. THIS REPORT WILL BE AMENDED WHEN CAUSE OF FAILURE IS DETERMINED. 1L72 4T4 T A24CE E4EA 19950929003991995092900399EU 1995 9 29 RAIA950901 119950904A77123034486 CONNECTOR AEROSPATR42 ATR42300 8680920EU LT ENGINE DIRTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE032FOR 199 STL - FLT 7128 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE CLEANED LEFT EEC CANNON PLUG. AIRCRAFT TT, 11,503.0. ENGINE TT, 121,021.0. (X) 2H72 4T RTA53EU 19950929004001995092900400EU 1995 9 29 RAIA950905 119950903A2121EVAC2423FD COOLING FAN AEROSPATR42 ATR42300 8680920EU LT PACK FAILED A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE032FOR 6069 6069 176 STL - FLT 7001 - NR 1 PACK FAULTS WITH ELECT SMOKE MASTER. MAINTENANCE REPLACED NR 1 GROUND COOLING FAN. AIRCRAFT TT, 12,613.0. (X) 2H72 4T RTA53EU 19950929004651995092900465NM 1995 9 29 UPS404525 119950923A5753 CORNER BOEING747 747SR46 NM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE ON GROUND, MAINTENANCE FOUND RT I/B MIDFLAP COVE LIP OB CORNER CRACKED AND DELAMINATED. ACCOMPLISHED COMPOSITE REPAIR REF SRM 51-40-09. 2L74 4F A20WE 19950929004661995092900466NM 1995 9 29 UPS404526 119950924A5753 SKIN BOEING747 747SR46 NM RT TE MIDFLAP PUNCTURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01680UP 20923 WHILE ON GROUND, MAINTENANCE FOUND RT I/B MIDFLAP LOWER SURFACE HAS TWO HOLES AT 2 FEET AND 5 FEET FROM THE I/B, COVE LIP AREA. ACCOMPLISHED COMPOSITE REPAIR PER SRM 51-40-09. 2L74 4F A20WE 19950929004671995092900467 1995 9 29 95ZZZW820 319950818A61401379049H403 STUB PIPE BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03341TE 950 STL - FLT 7321 - THE RT ENGINE DID NOT MAKE TORQUE, RT BETA FLICKERING. MAINTENANCE REPLACED RT ENGINE STUB PIPE AND BETA SWITCH. GROUND POWER RUNS CHECK OK. REF RAIA950830. 2L72 4T RTA56EU 19950929004681995092900468EU 1995 9 29 RAIA950803 119950801A2150 LT PACK BAG JETSTMJETSTM3201 1500217EU CABIN SMOKING A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03433AM 885 STL - THE LT PACK PUTS OUT SMOKE. MAINTENANCE PERFORMED GROUND RUNS, NO SMOKE NOTED. (W) 2L72 4T RTA56EU 19950929004691995092900469NE 1995 9 29 RAIA950827 219950819A72612380 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RIGHT LOW SERVICE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03423TE 119 120627 STL - FLT 7542 - THE RIGHT ENGINE LOW OIL PRESSURE. MAINTENANCE INSPECTED RT ENGINE FOR OIL LEAKS, NON NOTED. MAINTENANCE SERVICED RT ENGINE WITH OIL. GROUND RUNS CHECK OK. (W) 2H72 4T4 TRTA53EU E20NE 19950929004701995092900470EU 1995 9 29 RAIA950828 119950820A7722KJA6T17F26SN CONNECTOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE DIRTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03337TE 929 BRL - FLT 7057 - THE RT SRL INOP. MAINTENANCE CLEANED CONNECTOR ON RT SRL COMPUTER. PERFORMED AUTO START AND TEST OF SYSTEM CHECK OK. (W) 2L72 4T RTA56EU 19950929004711995092900471EU 1995 9 29 RAIA950829 119950820A7933CA06R12S3SF80 CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03337TE 929 STL - FLT 7454 - THE LT OIL TEMP GAUGE BEGAN TO FLUTTER. MAINTENANCE REPLACED LT OIL TEMP BULB CONNECTOR. OPS CHECK GOOD ON GROUND RUN TEST. (W) 2L72 4T RTA56EU 19950929004721995092900472 1995 9 29 RAIA950830 319950818A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03341TE 950 STL - FLT 7321 - THE RT ENGINE DID NOT MAKE TORQUE, RT BETA FLICKERING. MAINTENANCE REPLACED RT ENGINE STUB PIPE AND BETA SWITCH. GROUND POWER RUNS CHECK OK. REF 95ZZZW820. 2L72 4T RTA56EU 19950929004731995092900473EU 1995 9 29 RAIA950832 119950820A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03337TE 929 STL - FLT 7454 - ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED ALL EMERGENCY LIGHTING BATTERIES. SYSTEM CHECK GOOD ON TEST. (W) 2L72 4T RTA56EU 19950929005571995092900557WP 1995 9 29 95ZZZX5313 219950607A7250 SEAL LEAR 35 35A 5170602CE GARRTTTFE731TFE73122B 01518WP NR 4-5 FAILED A AOQAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA1153GH 304 P74814 ISP - AFTER TAKEOFF, CABIN AND COCKPIT FILLED WITH SMOKE (ENGINE OIL FUMES). EMERGENCY ACTIONS WERE TAKEN AND AIRCRAFT RETURNED TO ISP WITHOUT INCIDENT. BORESCOPE INSPECTION OF ENGINE COMPRESSOR SECTION REVEALED OIL PRESENT IN THE NR 4 AND NR 5 BEARING CARBON SEAL CAVITY. OIL LEAKAGE PAST THE NR 4 AND NR 5 AIR/OIL SEALS RESULTED IN SMOKE IN THE CABIN. BOTH THE NR 4 AND NR 5 SEALS WERE REPLACED AND THE NR 5 SEAL AREA SCAVENGE CAPABILITY IMPROVED WITH THE INCORPORATION OF SB 72-3540. THE ENGINE HAS BEEN REASSEMBLED AND HAS DEMONSTRATED ACCEPTABLE PERFORMANCE/FUNCTION ON TEST CELL AND RETURNED TO SERVICE. 2L72 4F4 F A10CE E6WE 19950929005671995092900567WP 1995 9 29 95ZZZX5323 119950115A2720 RUDDER PEDAL DOUG DC9 DC932 3022066WP COCKPIT CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11935VV 47534 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A CRACK WAS FOUND IN THE CAPTAIN'S LEFT RUDDER PEDAL AFT, INBD BOLT HOLE DURING INSP ON SB 27-209, AD 82-04-02. REMOVED AND REPLACED THE RUDDER PEDAL IAW SB 27-209 AND AD 82-04-02. N/R NR 027A1/0153. 2L72 4F A6WE 19950929005681995092900568WP 1995 9 29 95ZZZX5324 119950103A5541 RIB DOUG DC9 DC932 3022066WP RUDDER CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11935VV 47534 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND RUDDER RT SIDE RIB NR 17 FWD OF EXISTING REPAIR HAS 1 EACH CRACK. FABRICATED AND INSTALLED REPAIR MEMBERS FOR CRACKED RIB IAW DC9 SRM 55-03, FIG 12, AND SB 55-23. N/R NR 027A1/0133. 2L72 4F A6WE 19950929005761995092900576WP 1995 9 29 95ZZZX5332 119950801A5313 LONGERON DOUG DC9 DC932 3022066WP FS 389 DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11935VV 47534 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND LEFT FS 389, LONGERON 20 HAS IMPROPER REPAIR. REMOVED NON-STANDARD REPAIRS. FABRICATED AND INSTALLED REPAIRS FOR LONGERON IAW DC9 SR 53-04 AND SRM 51-10-4. N/R NR 027N1/0445. 2L72 4F A6WE 19950929005781995092900578WP 1995 9 29 95ZZZX5334 119950509A5313 LONGERON DOUG DC9 DC932 3022066WP BS 160-180 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE E AND E COMPARTMENT, LONGERON 22, BETWEEN STA 160 TO STA 180, LOWER LEG. REMOVED DAMAGED LONGERON AND REPAIRED IAW E.O. 95-159. N/R NR 027F1-0007. 2L72 4F A6WE 19950929005791995092900579WP 1995 9 29 95ZZZX5335 119950509A5313 LONGERON DOUG DC9 DC932 3022066WP FS 332-450 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE FWD CARGO COMPARTMENT, LONGERON 29L FROM FS 332 TO FS 450. INSTALLED NEW LONGERON, FS 332-FS 450 AND FS 332-FS 294, AND INSTALLED NEW SPLICES IAW DC9 SRM 53-02. N/R NR 027N1-0135. 2L72 4F A6WE 19950929005801995092900580WP 1995 9 29 95ZZZX5336 119950509A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 200 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LATERAL CABIN FLOOR SUPPORT BS 200 FROM BL ZERO TO RBL 22 AF 13. FABRICATED PART IAW SRM 53-11-1. ALODINE AND PRIMED PART IAW SRM 51-10. DRILLED PART AND DEBURRED PART AND INSTALLED IAW SRM 53-11. N/R NR 027D1-4046. 2L72 4F A6WE 19950929005811995092900581WP 1995 9 29 95ZZZX5337 119950509A5311 FRAME DOUG DC9 DC932 3022066WP BS 1089 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE RT AFT FS 1089 S-11 LEVEL FRAME WHICH WAS BLEEDING OUT BETWEEN ANGLE AND FRAME AT CANTED BULKHEAD TIE INTO FRAME. DOT 1. REMOVED ANGLES IAW SRM 51 TO GAIN ACCESS TO CORROSION. REMOVED CORROSION, FOUND FRAME WEB OUT OF LIMITS IAW SRM 51. FABRICATD REPAIR DOUBLER, TREATED AND PRIMED METAL. REINSTALLED ANGLES, DOUBLERS. N/R NR 027D1-4072. 2L72 4F A6WE 19950929005821995092900582WP 1995 9 29 95ZZZX5338 119950509A5313 LONGERON DOUG DC9 DC932 3022066WP FS 332-450 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE FWD CARGO COMPT. LONGERON NR 30L FROM FS 332 TO FS 450. INSTALLED NEW LONGERON FS 294-FS 450 IAW DC9 SRM 53-02. INSTALLED NEW SPLICES IAW DC9, SRM 53-02. N/R NR 027N1-0135. 2L72 4F A6WE 19950929005831995092900583WP 1995 9 29 95ZZZX5339 119950509A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 220 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LONGITUDINAL CABIN FLOOR SUPPORT, BS 220 AT LBL 14. FABRICATED NEW FLOOR SUPPORT IAW DC9 SRM 51. DRILLED HOLES AND DEBURRED IAW SRM 51. ALODINED AND PRIMED IAW DC9 SRM 51, INSTALLED IAW DC9 SRM 51-30 AND SRM 51-30. N/R NR 027D1-4046. 2L72 4F A6WE 19950929005841995092900584WP 1995 9 29 95ZZZX5340 119950509A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 200 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE LATERAL CABIN FLOOR SUPPORT BS 200 FROM RBL 22 TO RBL 44. FABRICATD NEW PART, DRILLED HOLES AND DEBURRED, ALODINE AND PRIMED, AND INSTALLED NEW PART IAW SRM 51-10-2, 3, 4. N/R NR 027D1-4046. 2L72 4F A6WE 19950929005851995092900585WP 1995 9 29 95ZZZX5341 119950506A5330 SKIN DOUG DC9 DC932 3022066WP BS 148 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND A BULGE IN THE SKIN AT FS 148, LT SIDE , JUST BELOW LONGERON 18. CUT OUT DAMAGED AREA AND FABRICATE PARTS IAW DC9 53-04. INSTALLED REPAIR IAW SRM 53-04. N/R NR 027F1-0027. 2L72 4F A6WE 19950929005861995092900586WP 1995 9 29 95ZZZX5342 119950509A5320 FITTING DOUG DC9 DC932 3022066WP BS 218 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND AT THE FUSELAGE FRAME BS 218 AND UNDER FLOOR AT RBL 55, BOLT WAS RUSTY. REMOVED EXISTING SPLICE, FITTING AND AIR DUCT. ORDERED NEW FITTINGS, FABRICATED NEW CUSP SPLICE, HEAT TREATED TO 7025, DRILLED AND DEBURRED, ALODINED, PRIMED AND INSTALLED NEW FITTINGS. CUSP SPLICE AND IAR DUCT ALL IAW 51-31-12. N/R NR 027D1 4046. 2L72 4F A6WE 19950929005871995092900587WP 1995 9 29 95ZZZX5343 119950506A5330 SKIN DOUG DC9 DC932 3022066WP FS 210 DENTED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A DENT IN THE SKIN WAS FOUND AT FS 210, RT, BETWEEN LONGERON 18 AND LONGERON 17 AND 0.122 INCH DEEP. THIS IS CONDITION NR 2. CUT OUT DAMAGED AREA, FABRICATED 2 INCH FILLER PLATES, 2 INCHES BY .050 INCH, DOUBLER, 5 INCHES BY .063 INCH. DRILLED HOLES, COUNTERSUNK AND DEBURRED, ALODINED AND PRIMED, INSTALLED AND SEALED IAW 51-20. N/R NR 027E10027. 2L72 4F A6WE 19950929005881995092900588WP 1995 9 29 95ZZZX5344 119950518A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 180 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND IN THE E AND E COMPARTMENT, FS 180, BL 20L, UPPER FLOOR BEAM WEB AND L-ANGLE CRACKED. REMOVED ANGLE, FABRICATED NEW ANGLE AND INTERCOSTAL REPAIRS AND INSTALLED IAW DC9 SRM CHAPTER 51-10-02 AND CHAPTER 53-05, FIGURE 100. FS 180, BL 20L. N/R NR 027D1-0225. 2L72 4F A6WE 19950929005891995092900589WP 1995 9 29 95ZZZX5345 119950509A5313 STRINGER DOUG DC9 DC932 3022066WP BS 1143 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11941VV 47666 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FOUND ON THE RT AFT FUSELAGE CANTED BULKHEAD AREA, STA 1143, STR 9, EXFOLIATED BEYOND LIMITS. REMOVED 18.025 INCHES OF EXFOLIATED LONGERON, FABRICATED REPAIR LONGERON OF 7075T6-.063. FABRICATED REPAIR SPLICES OF 7075-T6.063 IAW SRM 53-02. ALODINE AND PRIME PARTS IAW SRM 51-10-03, FAY SURFACE SEAL PARTS IAW SRM 51-20-0. N/R NR 027D1-4072. 2L72 4F A6WE 19950929005901995092900590WP 1995 9 29 95ZZZX5346 119950123A5313 LONGERON DOUG DC9 DC932 3022066WP FS 503-520 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11938VV 47442 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE FWD CARGO LONGERON 30 WAS CORRODED OUT 25 PERCENT OF MATERIAL THICKNESS AT FS 508. REMOVED AND REPLACED LONGERON 30 FROM FS 503 TO FS 520 IAW DC9 SRM 51-40-4 AND SRM 51-30-05. N/R NR 027A1/0220. 2L72 4F A6WE 19950929005921995092900592WP 1995 9 29 95ZZZX5348 119950119A5320 FITTING DOUG DC9 DC932 3022066WP FS 718 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11938VV 47442 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA FOUND INSIDE THE MAIN CABIN AT FS 718, LONGERON 19 FRAME (RT) FITTING IS CRACKED FWD AND AFT SIDES, ONE 1 INCH FWD AND ONE 1 INCH AFT. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, SRM 51-30-01, SB53-131 AND D.A.C. DWG 5935650. N/R NR 027A1/0201 AND 0202. 2L72 4F A6WE 19950929005931995092900593WP 1995 9 29 95ZZZX5349 119950122A5330 SKIN DOUG DC9 DC932 3022066WP FS 125-157 DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11938VV 47442 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE REPAIR AT FS 125 TO FS 157 IS A NON-STANDARD REPAIR. FABRICATED AND INSTALLED NEW SKIN FILLERS AND DOUBLERS IAW DC9 SRM 53-04, FIG 12B, AND SRM 51-20-0. N/R NR 027A1/0234. 2L72 4F A6WE 19950929005951995092900595WP 1995 9 29 95ZZZX5351 119950118A5330 SKIN DOUG DC9 DC932 3022066WP FS 237-541 DENTED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11938VV 47442 UPON A SCHEDULED INSPECTION A AERO CORP IN LAKE CITY, FLORIDA, THE EXTERNAL SKIN WAS FOUND WITH NUMEROUS DENTS, FROM FS 237 TO FS 541, FROM LONGERON 17R TO LONGERON 25R. REMOVED DAMAGED SECTION OF SKIN. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW DC9 SRM 53-04, SRM 51-30-2, AND SRM 51-20-0. N/R NR'S 027N1/0399, 0400, 0401, 0403, 0404, 0405, 0406, 0407, 0408, AND 0409. 2L72 4F A6WE 19950929005961995092900596WP 1995 9 29 95ZZZX5352 119950119A5312 ANGLE DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11938VV 47442 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND THE MAIN CABIN COMPARTMENT AFT PRESSURE BULKHEAD ATTACH ANGLE IS CRACKED AT APPROXIMATELY 10 O'CLOCK POSITION, RT SIDE. FABRICATED AND INSTALLED PRESSURE BULKHEAD REPAIRS IAW DC9 SRM 53-05-89. N/R NR 927N1/0454. 2L72 4F A6WE 19950929005971995092900597WP 1995 9 29 95ZZZX5353 119950329A5313 LONGERON DOUG DC9 DC932 3022066WP FS 218 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11940VV 47523 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 25L AT FS 218.0 WAS FOUND CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9, SRM 53-02, FIG 2. N/R NR 027N1/0072. 2L72 4F A6WE 19950929005981995092900598WP 1995 9 29 95ZZZX5354 119950329A5320 DOUBLER DOUG DC9 DC932 3022066WP FS 541.0 DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11940VV 47523 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A NON-CONFORMING REPAIR WAS FOUND AT FS 541.0. REMOVED OLD REPAIR. FABRICATED AND INSTALLED NEW DOUBLER AND FILLERS IAW AERO CORP E.O. 95-141, REV IR, DATED 4-25-95. 2L72 4F A6WE 19950929005991995092900599WP 1995 9 29 95ZZZX5355 119950331A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP FS 280 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11940VV 47523 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, THE FLOOR BEAM AT FS 180.0, LBL 20.2, WAS FOUND CRACKED. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-05 AND SRM 51-10-2. 2L72 4F A6WE 19950929006001995092900600WP 1995 9 29 95ZZZX5356 119950329A5320 DOUBLER DOUG DC9 DC932 3022066WP FS 832 DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11940VV 47523 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, A NON-CONFORMING REPAIR WAS FOUND AT FS 832 LONGERON 23R. REMOVED NON-CONFORMING REPAIR. FABRICATED AND INSTALLED A NEW DOUBLER AND SHIMS IAW DC9 SRM 53-04 AND AERO CORP E.O. 95-141 REV. IR DATED 4-7-95. N/R NR 027T1/0003. 2L72 4F A6WE 19950929006011995092900601NM 1995 9 29 CAL950489 119950616A521080330035 ASSIST BOTTLE BOEING757 757224 1384958NM L-1 DOOR LOW PRESSURE A CALAK NONE O OTHER ININSP/MAINT 1 SW09131102076 27300 EWR - THE EMRGENCY ASSIST L-1 DOOR BOTTLE WAS FOUND WITH ZERO PRESSURE DURING SERVICE CHECK. THE EMERGENCY ASSIST DOOR BOTTLE WAS REMOVED AND REPLACED PER MM 52-11-00. (X) 2L72 4F RTA2NM 19950929006021995092900602 1995 9 29 CAL950631 419950801A2565100502115 SLIDE DOUG DC9 DC982 3022082WP GALLEY DOOR LOW PRESSURE A CALAK NONE O OTHER ININSP/MAINT 1 SW0969826218936564 49486 IAH - FLT 0291 - INSPECTION FOUND THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WITH LOW PRESSURE DURING A PRE-FLIGHT CHECK. THE AFT GALLEY DOOR EMERGENCY EVACUATION SLIDE WAS REMOVED AND REPLACED. (X) 2L72 4F A6WE 19950929006031995092900603NM 1995 9 29 DLM90951824 119950427A242128B5274 GENERATOR DOUG MD90 MD9030 3023690NM NR 1/2 ENGINE OIL LEAK A DALAO OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO11902DA 53382 DURING CRUISE, RT AS POWER FAULT ILLUMINATED ALONG WITH OIL PRESSURE FAULT. STARTED APU, THEN LEFT GENERATOR AC POWER FAULT CAME ON WITH LEFT GENERATOR AND OIL PRESSURE STATUS LIGHT, THEN LEFT GENERATOR TRIPPED OFF LINE. LANDED EWR, FOUND BOTH GENERATORS WITH LOW OIL, EVIDENCE OF LEAKAGE IN ENGINE COWL. SERVICED GENERATORS AND FOUND LEFT GENERATOR FILTER BOWL HOUSING CRACKED AND THE RT GENERATOR PRESSURE SERVICING PORT LEAKING. REPLACED BOTH GENERATORS. 2L72 4F RTA6WE 19950929006041995092900604NM 1995 9 29 95FDEA01417 119950925A53302024T3 SKIN BOEING727 72722 1384002NM BS 360-480 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 THERE ARE 24 LIGHTNING STRIKES ON SKIN, BS 360 TO 480 STR 23 TO 26R. REMOVED DAMAGE AND REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19950929006051995092900605NM 1995 9 29 95FDEA01418 119950925A575420240080 SKIN BOEING727 72722 1384002NM NR 6 LE SLAT GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 THE NR 6 SLAT L/E HAS SMALL GOUGES APPROX 28 INCHES FROM O/B END. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED ON NR 6 SLAT L/E APPROX 28 INCHES FROM O/B END IAW FEDEX SRM 57-50-1, 57-50-3, DWG 65-17302. 2L73 4F A3WE 19950929006061995092900606NM 1995 9 29 95FDEA01419 119950925A53217075T6 FLOOR PANEL BOEING727 72722 1384002NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION AROUND FLOOR PANEL FASTENER HOLE AT STA 312 LBL 45 WL 208. REPAIRED PER FEDEX SRM 53-10-8 FIG 7. 2L73 4F A3WE 19950929006071995092900607NM 1995 9 29 95FDEA01420 119950925A5315BAC150529 FLOOR BEAM BOEING727 72722 1384002NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION AROUND FLOOR PANEL FASTENER HOLES AT FLOORBEAM STA 344 WL 208 RBL 19 LBL 55. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-02. REMOVED AND REPLACED 344 BEAM UPPER CHORD FROM SKIN TO SKIN PER FEDEX DRAWING NR SR 8753-007. 2L73 4F A3WE 19950929006081995092900608NM 1995 9 29 95FDEA01421 119950925A5320BAC150043 FLOOR SUPPORT BOEING727 72722 1384002NM BS 277-295 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORRODED INTERCOSTAL STA 277 TO 295 RBL 13 WL 208. REMOVED AND REPLACED INTERCOSTAL FLOOR SUPPORT, STA 277 TO 295 RBL 13 WL 208. 2L73 4F A3WE 19950929006091995092900609NM 1995 9 29 95FDEA01422 119950925A532065198614 NOSE CHORD BOEING727 72722 1384002NM BS 294.5 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION EMANATING FROM BULGING LEVELING COMPOUND ON LOWER RT NOSE CHORD, BS 294.5 PLUS 17 RBL 17 WL 145. REMOVED AND REPLACED RT NOSE CHORD, BS 284.5 PLUS 17 TO 351 RBL 17 WL 145 IAW BAC DRAWING NR 6515724. 2L73 4F A3WE 19950929006101995092900610NM 1995 9 29 95FDEA01424 119950926A5315BAC1518338 FLOOR BEAM BOEING727 72722 1384002NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (72C235-02), ON TOP CHORD AND WEB OF BS 720 FLOORBEAM, RBL 13 TO 22, 47.5 TO 55, WL 206 TO 208. 2L73 4F A3WE 19950929006111995092900611NM 1995 9 29 95FDEA01425 119950926A53117075T6071 FRAME BOEING727 72722 1384002NM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HFEC INSP EXHIBITS CRACK EMANATING FROM HOLE ON BS 1090 FRAME, O/B SIDE UPPER OF STR 27L. REPAIRED CRACKED FRAME AT BS 1090, O/B SIDE UPPER OF STR 27L PER FEDEX SRM 51-40-3 FIG 1. 2L73 4F A3WE 19950929006121995092900612NM 1995 9 29 95FDEA01426 119950926A53302024T3080 SKIN BOEING727 72722 1384002NM BS 227 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 DENT IN SKIN AT NOSE ACCESS DOOR, BS 227 RBL 5. REPAIRED DENT PER FEDEX SRM 53-30-3, AT BS 227 RBL 5 FUSELAGE SKIN. 2L73 4F A3WE 19950929006131995092900613NM 1995 9 29 95FDEA01427 119950926A53117075T6 FRAME BOEING727 72725 1384006NM BS 660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION FOUND ON FRAME, STA 660 WL 156 LBL 26 AROUND NUTPLATE. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGE AND REPAIRED PER FEDEX EA NR 7-5310-25826. 2L73 4F A3WE 19950929006141995092900614WP 1995 9 29 95FDEA01428 219950926A75301555M23G01 DUCT DOUG DC10 DC1030F 3023504WP NR 1 ENGINE FAILED A FDEAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO25322FE 47908 DURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 DEGREES HIGHER THAN ENG NR 2 AND NR 3. AT APPROX 300 FEET NR 1 FIRE WARNING AND BELL RECEIVED. ACCOMP EMERGENCY CHECKLIST, DUMPED FUEL, DECLARED EMERGENCY AND RETURNED TO ANC. MX DISCOVERED THE 14TH STAGE CROSSOVER DUCT FAILED AND IT WAS REPLACED ALONG WITH BOTH REVERSER HALVES. ALSO, REPLACED WERE 2 FUEL NOZZLE TUBES. 2L73 4F RTA22WE 19950929006151995092900615NE 1995 9 29 COMA9511973 219950925A7230 COMPRESSOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FOD DAMAGE A COMAK NONE C F.O.D. ININSP/MAINT 1 SO011105G 1191 120105 115522 DURING PREFLIGHT INSPECTION, FOUND COMPRESSOR BLADE DAMAGE ON RT ENGINE. REPLACED ENGINE. 2L72 4T4 TRTA31SO E20NE 19950929006161995092900616SO 1995 9 29 COMA9511974 119950925A243523080013 STARTER GEN EMB 120 EMB120RT SO RT ENGINE FAILED A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01189CA4914 170 120189 THE RT ENGINE WOULD NOT START, NO ROTATION. REPLACED THE STARTER/GENERATOR. 2L72 4T RTA31SO 19950929006171995092900617EA 1995 9 29 COMA9560556 119950924A2760 ECU CNDAIRCL600 CL6002B19 EA SPOILER MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01940CA 7048 DURING LIFT OFF, OUTBOARD GROUND LIFT DUMP INDICATED DEPLOYED. ALSO, AMBER MESSAGE ON EICAS AND FLIGHT CONTROL PAGE INDICATED DEPLOYED, ACFT RETURNED TO FIELD. RESET THE SPOILER ELECTRONIC CONTROL UNIT AND SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19950929006181995092900618 1995 9 29 SCNA95197 419950922A2565141111001 BATTERIES DOUG DC10 DC1010 3022110WP L1 DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15907WA 46946 THE L-1 DOOR SLIDE TESTED WEAK. THE SLIDE INTEGRITY TEST BATTERIES WERE FOUND WEAK. REPLACED BATTERIES AND SLIDE TESTED GOOD. 2L73 4F A22WE 19950929006191995092900619NM 1995 9 29 SCNA95198 119950923A335008167120 EEL WIRE BOEING727 7272J4 1384006NM CABIN DAMAGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 LEFT SIDE FORWARD SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REPAIRED SPLICE AT AFT SECTION OF FORWARD TRACK AND LIGHTING TESTED GOOD PER MM 33-50-01. 2L73 4F RTA3WE 19950929006201995092900620NE 1995 9 29 9514532295 219950925A7261 TUBE BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE BROKEN A NWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01295US 21506 96501 EN ROUTE TO DTW, THE NR 1 ENGINE OIL QUANTITY DECREASING AND LOW OIL PRESSURE INDICATION ILLUMINATED. SHUT DOWN NR 1 ENGINE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BROKEN OIL TUBE FROM NR 6 SCAVENGE PUMP. REPLACED TUBE. LEAK CHECK WAS NORMAL. 2L73 4F4 F A3WE E2EA 19950929006211995092900621NM 1995 9 29 95FDEA01429 119950927A53302024T3071 SKIN BOEING727 727232 1384082NM BS 650 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 EA 7-5330-25397 CORRECTIONS FOR DENT IN FUSELAGE SKIN/CARGO DOOR DOUBLER (LOGBOOK ENTRY REQUIRED) MACH NR 53-30/686. REMOVED DAMAGED STR 24L, RECONTOURED DENT, INSPECTED FOR CRACKS NONE FOUND. FABRICATED STR AND DOUBLER REPAIR AND INSTALLED REPAIR PARTS AT BS 650, STR 23-24L PER SRM 53-10-3, 53-30-3, 51-40-1 AND FEDEX EA 7-5310-25787. INSPECTION SCUFF MARK AT BS 490, STR 23L. BLENDED AREA, INSPECTED AT CRACKS, NONE FOUND. NO FURTHER ACTION REQUIRED AT BS 490, STR 23L PER SRM 53-30-1. 2L73 4F A3WE 19950929006221995092900622NM 1995 9 29 95FDEA01430 119950923A5315 FLOOR BEAM BOEING727 72723 1384004NM BS 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 HEAVY CORROSION AT F/B SCREW HOLES STA 400, LBL 35 ON FLOOR BEAM TOP SIDE. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA PER SRM 53-10-8. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8, PG 45 - 48. 2L73 4F A3WE 19950929006231995092900623NM 1995 9 29 95FDEA01431 119950926A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION OF FLOOR TRACK AT LBL 45 AT BS 360, 400-420 AND 380. REMOVED SECTION OF FLOOR BEAM STATION 360 - 420 AND INSTALLED NEW FLOOR TRACK FROM STA 360-420 PER SRM 51-10-5. 2L73 4F A3WE 19950929006241995092900624NM 1995 9 29 95FDEA01432 119950921A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 MAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 277-53-007. 2L73 4F A3WE 19950929006251995092900625NM 1995 9 29 95FDEA01433 119950927A533065C141291 SKIN BOEING727 727232 1384082NM BS 680-740 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY, ON AND UNDER BONDED DOUBLER AT BL 0, BS 720-726 AT VARIOUS BODY STAT, IT IS DISBONDED, ALSO, (ACCESS IS REQUIRED). REMOVED AND REPLACED BELLY SKIN FROM BS 680-740, STR 26 LT AND RT ALL WORK DOWN IAW FEDEX EA 7-5300-25764 AND DRAWING NR 65-54577. 2L73 4F A3WE 19950929006261995092900626NM 1995 9 29 95FDEA01434 119950926A53157075T6071 FLOOR BEAM BOEING727 72722 1384002NM BS 328 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON FLOOR BEAM STA 328, WL 208, LBL 18 - 45. REMOVED CORROSION AND TREATED BS 328, WL 208, LBL 45. FOUND CORROSION AT BS 328, WL 208, LBL 18 OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR. ALL PER FEDEX SRM 53-10-8, 53-10-1, 53-10-2. 2L73 4F A3WE 19950929006271995092900627NM 1995 9 29 95FDEA01435 119950926A53157075T6 FLOOR BEAM BOEING727 72722 1384002NM BS 600 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (72C235-02) AND BARE METAL ON TOP CHORD AND WEB OF THE BS 600 FLOOR BEAM RBL 2-55 AND LBL 2-48, WL 202-208. REMOVED CORROSION AT BS 600, RBL 2-55 AND LBL 2-43, WL 202-208, RBL 11 - 41 WERE FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNESS WAS .125 INCH. MATERIAL REMOVED WAS .040 INCH AT RBL 41 AND 100 PERCENT AT RBL 11. REPAIRED BOTH AREAS PER FEDEX SRM 53-10-8 - ALODINED AND PRIMED ALL BARE METAL. 2L73 4F A3WE 19950929006281995092900628NM 1995 9 29 95FDEA01436 119950926A53117075T6 FRAME BOEING727 72722 1384002NM BS 970 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HOLE ON BS 970, RT FRAME ON THE INBOARD SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION (FIGURED AND SHAPED). CUT OUT DAMAGE ON UPPER FLANGE OF FRAME AT STR 27R, BS 970, RT AREA. CUT OUT WAS .50 INCH BY 1 INCH. FABRICATED REPAIR PART AND INSTALLED AS PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950929006291995092900629NM 1995 9 29 95FDEA01437 119950926A53117075T6 FRAME BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING ON EO 7-5310-7-2354E1, A CRACK WAS FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L. REPAIRED CRACK FOUND ON FRAME AT TOOLING HOLE LOCATED AT BS 1050, LBL 22.5 ABOVE STR 27L AS PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19950929006301995092900630NM 1995 9 29 95FDEA01438 119950927A53117075T6 FRAME BOEING727 72725 1384006NM BS 620 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 POSSIBLE CRACK FOUND IN FRAME AT STA 620, RBL 60, WL 190. CONFIRMED CRACK. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX EA NR 7-5310-25817. 2L73 4F A3WE 19950929006311995092900631NM 1995 9 29 95FDEA01439 119950927A53117075T6 FRAME BOEING727 72725 1384006NM BS 580 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION FOUND ON FRAME AT STA 580, WL 156-172, LBL 26-45 AROUND NUT PLATES (MARKED). REMOVED CORROSION ON FRAME BS 580, STR 24 LT. FABRICATED NEW SPLICE PLATE. TREATED REWORKED AREA AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5310-25825. 2L73 4F A3WE 19950929006321995092900632NM 1995 9 29 95FDEA01440 119950927A53117075T6 FRAME BOEING727 72725 1384006NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION ON UPPER CHORD BS 950, WL 208, RBL 12, 45 AND LBL 25. FOUND ADDITIONAL CORROSION AT LBL 11. REMOVED CORROSION FROM ALL AREAS. FOUND AREAS AT LBL 11, 25 TO BE WITHIN LIMITS. AREA AT RBL 12, 48 WERE FOUND OUT OF LIMITS. REPAIRED AREAS AT RBL 12 AND 48 PER FEDEX EA 7-5310-25837. 2L73 4F A3WE 19950929006331995092900633NM 1995 9 29 95FDEA01441 119950927A53117075T6 FRAME BOEING727 72725 1384006NM BS 211 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION ON INSIDE SKIN AND NOSE DOOR CUT OUT FRAME AT BS 211, LBL 19, WL 172. FOUND ADDITIONAL CORROSION ON WEB BETWEEN BS 203-219, LBL 15, ON L-ANGLE FOR SAME WEB, ON WEB FOR FRAME AT BS 211, LBL 16. FABRICATED NEW WEB AND L-ANGLE FOR BS 203-219, LBL 15, AND NEW WEB FOR FRAME FOR BS 211, LBL 16 THEN INSTALLED ALL NEW PARTS. REPAIRED CORRODED T-CHORD PER FEDEX EA NR 7-5310-25819. 2L73 4F A3WE 19950929006341995092900634NM 1995 9 29 95FDEA01442 119950927A57112024T3 SPAR BOEING727 72725 1384006NM WS 331.7-339.7 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 WHILE WORKING CUST ID NR0443, FOUND CORROSION EVIDENCE ON LT WING FRONT UPPER SPAR CHORD UPPER SURFACE AT SIX FASTENER HOLES, LES 331.7 - LES 339.7. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW FEDEX SRM 57-30-4 AND EA NR 7-5710-25816. AT L/E STA 331.7 TO L/E STA 339.7 ON UPPER SPAR CHORD UPPER SURFACE. 2L73 4F A3WE 19950929006351995092900635NM 1995 9 29 95FDEA01443 119950927A53107075T6 FRAME BOEING727 72725 1384006NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION FOUND ON BS 740 FRAME AT LBL 3. DISCOVERED ADDITIOINAL CORROSION FROM STR 1L - 3L. MECHANICALLY REMOVED CORROSION FROM FRAME FLANGE. CUT OUT DAMAGED SKIN AT BS 742, LBL 3. REPAIRED FRAME AND SKIN PER FEDEX EA NR 7-5310-25835. 2L73 4F A3WE 19950929006361995092900636NM 1995 9 29 95FDEA01444 119950927A53302024T3 SKIN BOEING727 72725 1384006NM BS 211 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25508FE 18279 CORROSION (71C113-02) ON INSIDE SKIN AND NOSE DOOR CUT OUT FRAME BS 211, RBL 19, WL 172. REMOVED FASTENERS FOR T-CHORD EXT SKIN BS 211 FRAME AND WEB. CLEAN AND TREATED CORROSION, ALODINED, PRIMED AND RE-INSTALLED FASTENERS. REMOVED DOOR CUT OUT FRAME WEB, FABRICATED NEW WEB, ALODINED, PRIMED AND INSTALLED. WORK DONE IAW SRM 53-10-1. 2L73 4F A3WE 19950929006371995092900637NM 1995 9 29 95UAL900154 119950927A5230 LATCHES BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CARGO DOOR OUT OF RIG A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP299063U 19944 A/C RETURNED TO FIELD WITH AFT CARGO DOOR LIGHT, UNABLE TO PRESSURIZE A/C. AFT CARGO DOOR WAS FOUND OPEN. THE LATCHES APPEARED SECURE, BUT THE DOOR WAS OUT RIG. 2L72 4F4 F A16WE E2EA 19950929006381995092900638NM 1995 9 29 95UAL900155 119950927A3300 EEL BATTERY PACK BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299071U 19952 EMERGENCY LIGHTS INOP ON LEFT SIDE EXTERIOR OF AIRCRAFT. REPLACED BATTERY PACK. 2L72 4F4 F A16WE E2EA 19950929006391995092900639NM 1995 9 29 95UAL900156 119950927A3350 EEL BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29389UA 24664 EMERGENCY LIGHTS AT RIGHT HAND OVER WING EXIT AND AT CLASS DIVIDER ARE INOP. REPLACED BATTERY PACK. 2L72 4F4 FRTA16WE E2GL 19950929006401995092900640WP 1995 9 29 95UAL900157 119950928A2120 AIR DISTR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN ODOR A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP291823U 46622 PUNGENT ODOR, SMOKE IN AIRCRAFT 0N ENGINE PNEUMATICS AT HIGH ENGINE POWER. 2L73 4F4 F A22WE E23EA 19950929006411995092900641NM 1995 9 29 95UAL900158 119950928A26121061096217 FIRE DETECTOR BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE APU INOPERATIVE A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29993UA 22383 CREW DIVERTED EN ROUTE AND LANDED UNDER AMBER ALERT DUE TO APU FIRE WARNING INDICATION. DISCHARGED BOTTLE. REPLACED FIRE DETECTORS. ALSO, REPLACED FIRE BOTTLE, SQUIB AND INDICATOR DISK. CHECKS O.K. 2L72 4F4 F A16WE E2EA 19950929006421995092900642NM 1995 9 29 95UAL900159 119950928A7830D5114 CONNECTOR BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE ENGINE LOOSE A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29389UA 24664 ABORTED TAKEOFF AT 80 KNOTS DUE TO A REVERSER LIGHT. FOUND LOOSE CONNECTOR, RESET THE ENGINE ACCESSORY UNIT, AND REPLACED THE CONTROL VALVE MODULE. 2L72 4F4 FRTA16WE E2GL 19950929006431995092900643NM 1995 9 29 95UAL900160 119950928A2161 TEMP CONTROLLER GARRETT 5483766 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN FAILED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP297274U O1263762 21421 LEFT PACK MIX VALVE STUCK IN FULL COLD - CAUSED PACK TRIP WITH SMOKE IN COCKPIT AND CABIN. THIS INCIDENT OCCURRED ON AUGUST 7, BUT WAS NOT REPORTED THROUGH THE NORMAL CHANNELS. REPLACED CABIN TEMPERATURE CONTROLLER. COMPONENT CHECKED OKAY IN SHOP. 2L73 4F4 F A3WE E2EA 19950929006441995092900644WP 1995 9 29 ABXA9500688 119950612A57305758386 SKIN DOUG DC8 DC863 302198AWP WS 69.5 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND MOD ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-16-05, SB 57-88, FOUND LEFT WING LOWER SKIN AT XCW 69.5, HOLES A, C, F, I, 4 AND 5 HAVE CRACK LIKE INDICATIONS NOTED BY HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED IAW ABX REA D857-11369-MR. 2L74 4F 4A25 19950929006451995092900645WP 1995 9 29 ABXA9500689 119950518A57305858386 SKIN DOUG DC8 DC863 302198AWP WS 69.5 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, WHILE COMPLYING WITH AD 90-16-05, SB 57-88, FOUND LOWER WING SKIN, RIGHT SIDE AT STATION XCW 69.5 HAD CRACK INDICATIONS. REPAIRED SKIN IAW ABX REA D857-11370-MR. 2L74 4F 4A25 19950929006461995092900646WP 1995 9 29 ABXA9500690 119950602A523057799133 SKIN DOUG DC8 DC863 302198AWP BS 520 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FORWARD LOWER CARGO COMPARTMENT AFT DOOR SKIN HAD A DENT AND WAS GOUGED. REPAIRED IAW ABX REA D853-11372-MR. 2L74 4F 4A25 19950929006471995092900647WP 1995 9 29 ABXA9500691 119950531A53115615747511 FRAME DOUG DC8 DC863 302198AWP BS 180 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FRAME CRACKED AT FS 180 BETWEEN L35L AND L36. REPAIRED FUSELAGE FRAME IAW ABX REA D853-11373-MR. 2L74 4F 4A25 19950929006481995092900648WP 1995 9 29 ABXA9500692 119950712A52305615775127 SKIN DOUG DC8 DC863 302198AWP L2 DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND THAT PREVIOUS REPAIR ON SKIN OF L2 DOOR, LOWER FORWARD CORNER IS NOT IAW DAC DRAWING SR08530021. REPAIRED IAW DAC DRAWING SR08530021 AND ABX REA D853-11634-MR. 2L74 4F 4A25 19950929006491995092900649WP 1995 9 29 ABXA9500693 119950714A572056440111 ANGLE DOUG DC8 DC863 302198AWP BS 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE ATTACH ANGLE OF REAR SPAR AT FS 857, RBL 46.00. REPAIRED IAW ABX REA D853-11643-MR. 2L74 4F 4A25 19950929006501995092900650WP 1995 9 29 ABXA9500694 119950706A53205643394 DOUBLER DOUG DC8 DC863 302198AWP BS 920-940 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE RIGHT AND LEFT SIDES OF THE MAIN CABIN WINDOW FRAME AT FS 920 - 940. REPAIRED WINDOW DOUBLERS IAW ABX REA D853-11644-MR. 2L74 4F 4A25 19950929006511995092900651WP 1995 9 29 ABXA9500695 119950705A53205643394 DOUBLER DOUG DC8 DC863 302198AWP BS 1250 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE LEFT WINDOW DOUBLER AT STATION 1250. REPAIRED IAW ABX REA D853-11645-MR. 2L74 4F 4A25 19950929006521995092900652WP 1995 9 29 ABXA9500696 119950622A5753575117120 PLATE DOUG DC8 DC863 302198AWP LT TE FLAP WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT INBOARD FLAP, INBOARD HINGE, OUTBOARD FITTING PLATE WORN. REPAIRED IAW ABX REA D857-11652-MR. 2L74 4F 4A25 19950929006531995092900653WP 1995 9 29 ABXA9500697 119950621A5753575117120 FITTING DOUG DC8 DC863 302198AWP LT TE FLAP WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND INBOARD HINGE FITTING AT INBOARD FLAP WORN. REPAIRED IAW ABX REA D857-11653-MR. 2L74 4F 4A25 19950929006541995092900654WP 1995 9 29 ABXA9500698 119950628A5320975044891 CUSP DOUG DC8 DC863 302198AWP BS 1480 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT STATION 1480, LONGERON 21R. REPAIRED CUSP IAW ABX REA D853-11655-MR. 2L74 4F 4A25 19950929006551995092900655WP 1995 9 29 ABXA9500699 119950816A532097596121 ANGLE DOUG DC8 DC863 302198AWP BS 1020 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP ANGLE, RIGHT SIDE, AT STATION 1020, LONGERON 22R. REPAIRED CUSP ANGLE IAW ABX REA D853-11656-MR. 2L74 4F 4A25 19950929006561995092900656WP 1995 9 29 ABXA9500700 119950628A5320975044889 CUSP DOUG DC8 DC863 302198AWP BS 1280-1300 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT LONGERON 21L, STATION 1280 - 1300. REPAIRED CUSP IAW ABX REA D853-11657-MR. 2L74 4F 4A25 19950929006571995092900657WP 1995 9 29 ABXA9500701 119950628A532097596111 CUSP DOUG DC8 DC863 302198AWP BS 1045 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON CUSP AT STATION 1045, LONGERON 21L. REPAIRED CUSP IAW ABX REA D853-11658-MR. 2L74 4F 4A25 19950929006581995092900658WP 1995 9 29 ABXA9500702 119950706A575356527963 RIB DOUG DC8 DC863 302198AWP LT TE FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT INBOARD END RIB WEB DAMAGED. REPAIRED IAW ABX REA D857-11662-MR. 2L74 4F 4A25 19950929006591995092900659WP 1995 9 29 ABXA9500703 119950706A575056527964 RIB DOUG DC8 DC863 302198AWP RT TE FLAP DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND RIGHT INBOARD END RIB WEB DAMAGED. REPAIRED IAW ABX REA D857-11662-MR. 2L74 4F 4A25 19950929006601995092900660WP 1995 9 29 ABXA9500704 119950713A533057595121 SKIN DOUG DC8 DC863 302198AWP BS 1170 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FUSELAGE SKIN AT LONGERON 21R, STATION 1170 CRACKED. REPAIRED IAW ABX REA D853-11663-MR. 2L74 4F 4A25 19950929006611995092900661WP 1995 9 29 ABXA9500705 119950706A53137075T6511 LONGERON DOUG DC8 DC863 302198AWP BS 500-520 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND L36 CORRODED BETWEEN FS 500 AND FS 520. REPAIRED IAW ABX REA D853-11668-MR. 2L74 4F 4A25 19950929006621995092900662WP 1995 9 29 ABXA9500706 119950801A53133759529 LONGERON DOUG DC8 DC863 302198AWP BS 1080-1120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON LONGERON 9R AT STATION 1080 - 1120. REPAIRED IAW ABX REA D853-11673-MR. 2L74 4F 4A25 19950929006641995092900664WP 1995 9 29 ABXA9500708 119950628A53145750043501 KEEL BEAM DOUG DC8 DC863 302198AWP BS 660 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE HORIZONTAL FLANGES OF THE FORWARD KEEL TEE. REPAIRED IAW ABX REA D853-11886-MR. 2L74 4F 4A25 19950929006651995092900665WP 1995 9 29 ABXA9500709 119950724A52305649820 CORNER DOUG DC8 DC863 302198AWP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AND CRACKS IN THE FORWARD CORNER OF THE AFT DOOR OF THE AFT CARGO COMPARTMENT. REPAIRED AFT DOOR IAW ABX REA D853-11921-MR. 2L74 4F 4A25 19950929006661995092900666WP 1995 9 29 ABXA9500710 119950707A53115779772509 FRAME DOUG DC8 DC863 302198AWP BS 1020 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1020, LONGERON 33 - 34R. REPAIRED FRAME IAW ABX REA D853-11923-MR. 2L74 4F 4A25 19950929006671995092900667WP 1995 9 29 ABXA9500711 119950825A53115612161501 FRAME DOUG DC8 DC863 302198AWP BS 1890 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE LOWER FRAME AT STATION 1890, FROM LONGERON 28R - 28L. REPAIRED IAW ABX REA D853-11926-MR. 2L74 4F 4A25 19950929006681995092900668WP 1995 9 29 ABXA9500712 119950808A531397596274 LONGERON DOUG DC8 DC863 302198AWP BS 1050-1350 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON LONGERON 36 AT STATION 1050 - 1350. REPAIRED IAW ABX REA D853-11929-MR. 2L74 4F 4A25 19950929006691995092900669WP 1995 9 29 ABXA9500713 119950717A532056163067 JAMB DOUG DC8 DC863 302198AWP LT MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LEFT MAIN LANDING GEAR DOOR FORWARD JAMB ZEE CRACKED. REPAIRED MAIN LANDING GEAR DOOR FORWARD JAMB ZEE IAW ABX REA D853-11938-MR. 2L74 4F 4A25 19950929006701995092900670WP 1995 9 29 ABXA9500714 119950726A53205643394 DOUBLER DOUG DC8 DC863 302198AWP BS 1500 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE WINDOW DOUBLER AT FS 1500R. REPAIRED WINDOW DOUBLER IAW ABX REA D853-11941-MR. 2L74 4F 4A25 19950929006711995092900671WP 1995 9 29 ABXA9500715 119950801A528056163075 CHANNEL DOUG DC8 DC863 302198AWP LT MLG DOOR CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND ZEE CHANNEL ON THE LEFT MAIN LANDING GEAR DOOR CHAFED. REPAIRED CHANNEL IAW ABX REA D852-12160-MR. 2L74 4F 4A25 19950929006721995092900672WP 1995 9 29 ABXA9500716 119950720A531170750 FRAME DOUG DC8 DC863 302198AWP BS 1640 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1640, BETWEEN LONGERON 26L AND 27L. REPAIRED IAW ABX REA D853-12163-MR. 2L74 4F 4A25 19950929006731995092900673WP 1995 9 29 ABXA9500717 119950718A5311561214665 FRAME DOUG DC8 DC863 302198AWP BS 17 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT YCS 17.00, LONGERON 6R. REPAIRED FUSELAGE TAIL SECTION FRAME IAW ABX REA D853-12166-MR. 2L74 4F 4A25 19950929006741995092900674WP 1995 9 29 ABXA9500718 119950731A531197549219 FRAME DOUG DC8 DC863 302198AWP BS 1200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1200, LONGERON L1. REPAIRED FRAME IAW ABX REA D853-12172-MR. 2L74 4F 4A25 19950929006751995092900675WP 1995 9 29 ABXA9500719 119950728A531156402293 FRAME DOUG DC8 DC863 302198AWP BS 1400 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46615 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND FRAME AT STATION 1400, LONGERON 36, CRACKED AND CORRODED. REPAIRED FRAME IAW ABX REA D853-12167-MR. 2L74 4F 4A25 19950929006761995092900676WP 1995 9 29 ABXA9500720 119950808A531197510533 FRAME DOUG DC8 DC863 302198AWP BS 1660-1670 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT FS 1667. REPAIRED IAW ABX REA D853-12183-MR. 2L74 4F 4A25 19950929006771995092900677WP 1995 9 29 ABXA9500721 119950808A5320975105911 INTERCOSTAL DOUG DC8 DC863 302198AWP BS 1660-1670 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE INTERCOSTAL AT FS 1667, LONGERON 23L. REPAIRED INTERCOSTAL IAW ABX REA D853-12183-MR. 2L74 4F 4A25 19950929006781995092900678WP 1995 9 29 ABXA9500722 119950731A5320575196117 ANGLE DOUG DC8 DC863 302198AWP BS 920 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME ANGLE AT STATION 920, LONGERONS 1 - 2R. REPAIRED FRAME ANGLE IAW ABX REA D853-12190-MR. 2L74 4F 4A25 19950929006791995092900679WP 1995 9 29 ABXA9500723 119950801A531156402323 FRAME DOUG DC8 DC863 302198AWP BS 1460 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT AFT PIT STATION 1460, LONGERON 34L TO 35R. REPAIRED FRAME IAW ABX REA D853-12195-MR. 2L74 4F 4A25 19950929006801995092900680WP 1995 9 29 ABXA9500724 119950801A53117075T6 FRAME DOUG DC8 DC863 302198AWP BS 1000 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE FRAME AT STATION 1000, LONGERON 35L - 35R. REPAIRED FRAME IAW ABX REA D853-12204-MR. 2L74 4F 4A25 19950929006811995092900681WP 1995 9 29 ABXA9500725 119950802A5330 PLATING DOUG DC8 DC863 302198AWP BS 1670 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND EXISTING REPAIR AT STATION 1670, LONGERONS 21L AND 17L. REPAIRED IAW ABX REA D853-12278-MR. 2L74 4F 4A25 19950929006821995092900682WP 1995 9 29 ABXA9500726 119950802A52402024T3 DOOR DOUBLER DOUG DC8 DC863 302198AWP FS 156 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND GROUND PNEUMATIC DOOR INTERNAL DOUBLER CRACKED. REPAIRED IAW ABX REA D853-12283-MR. 2L74 4F 4A25 19950929006831995092900683WP 1995 9 29 ABXA9500727 119950817A53205754924505 DOUBLER DOUG DC8 DC863 302198AWP BS 1050-1350 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND INTERNAL DOUBLER AT STATION 1050 - 1350 DAMAGED. REPAIRED INTERNAL DOUBLER IAW ABX REA D853-12310-MR. 2L74 4F 4A25 19950929006841995092900684WP 1995 9 29 ABXA9500728 119950804A531370750 LONGERON DOUG DC8 DC863 302198AWP BS 90 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND LONGERON 22L AT STATION 90 HAD A NON-STANDARD REPAIR. REPAIRED LONGERON IAW ABX REA D853-12311-MR. 2L74 4F 4A25 19950929006851995092900685WP 1995 9 29 ABXA9500729 119950808A53117075T6 FRAME DOUG DC8 DC863 302198AWP BS 1360 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT LOWER FLANGE AT STATION 1360, LONGERON 36. REPAIRED IAW ABX REA D853-12322-MR. 2L74 4F 4A25 19950929006861995092900686WP 1995 9 29 ABXA9500730 119950804A523056553163 DOOR PAN DOUG DC8 DC863 302198AWP C2 DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT C-2 DOOR PAN. REPAIRED C-2 DOOR PAN IAW ABX REA D852-12338-MR. 2L74 4F 4A25 19950929006871995092900687WP 1995 9 29 ABXA9500731 119950805A53157075T6511 FLOOR BEAM DOUG DC8 DC863 302198AWP BS 1700 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING D - CHECK AND AND ACCEPTANCE INSPECTIONS, FOUND CORROSION AT AFT SIDE OF FLOOR BEAM AT STATION 1700, LONGERON 31. REPAIRED FLOOR BEAM IAW ABX REA D853-12343-MR. 2L74 4F 4A25 19950929006881995092900688WP 1995 9 29 ABXA9500732 119950622A53205644011 ANGLE DOUG DC8 DC861 3021952WP BS 857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23841AX 45908 DURING C - CHECK INSPECTION FOUND CORROSION ON FLANGE SHEAR WEB ATTACH ANGLE AT STATION 857, LBL 28 AND RBL 28. REPAIRED IAW ABX REA D853-11888-MR. 2L74 4F 4A25 19950929006891995092900689WP 1995 9 29 ABXA9500733 119950719A57207075T6 DOUBLER DOUG DC8 DC861 3021952WP BS 852 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23841AX 45908 DURING C - CHECK INSPECTION FOUND CORROSION ON DOUBLER AT STATION 852 AT XCW 4L AND XCW 6R ON CENTER WING SECTION. REPAIRED IAW ABX REA D857-11890-MR. 2L74 4F 4A25 19950929006901995092900690WP 1995 9 29 ABXA9500734 119950719A53205642235129 ANGLE DOUG DC8 DC861 3021952WP BS 810 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23841AX 45908 DURING C - CHECK INSPECTION DISCOVERED CORROSION ON UPPER WEB ATTACH ANGLE AT STATION 810. REPAIRED IAW ABX REA D853-11911-MR. 2L74 4F 4A25 19950929006911995092900691WP 1995 9 29 ABXA9500735 119950719A523056453163 DOOR PAN DOUG DC8 DC861 3021952WP C2 DOOR CORROSION A ABXAK NONE O OTHER ININSP/MAINT 1 GL23841AX 45908 DURING C - CHECK INSPECTION, FOUND CORROSION ON THE C-2 DOOR PAN. REPAIRED IAW ABX REA D852-11915-MR. 2L74 4F 4A25 19950929006921995092900692WP 1995 9 29 ABXA9500736 119950628A57205643130 DOUBLER DOUG DC8 DC861 3021952WP WS 0.00 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23841AX 56908 DURING C - CHECK INSPECTION, FOUND CORROSION ON UPPER JOINT DOUBLER AT XWC-0.00, STRINGER 4L. REPAIRED IAW ABX REA D857-11900-MR. 2L74 4F 4A25 19950929006931995092900693WP 1995 9 29 ABXA9500741 119950524A53205912285515 RETAINER DOUG DC9 DC941 302207NWP BS 680 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION, FOUND THE LEFT WINDOW SEAL RETAINER CRACKED IN THE UPPER FORWARD CORNER AT FS 680. REPAIRED IAW ABX REA D953-11589. 2L72 4F A6WE 19950929006941995092900694WP 1995 9 29 ABXA9500742 119950529A53202024T3040 INTERCOSTAL DOUG DC9 DC941 302207NWP BS 37-44 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION, FOUND THE UPPER SIDE CRACKED ON AN INTERCOSTAL, BETWEEN FS 37 AND FS 44. REPLACED INTERCOSTAL IAW DC-9 SRM, CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19950929006951995092900695WP 1995 9 29 ABXA9500743 119950515A531299122437 BLKHD ANGLE DOUG DC9 DC941 302207NWP BS 1041 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, LOWER ATTACH ANGLE FASTENER HOLES OVERSIZED ON THE LEFT SIDE. REPLACED ATTACH ANGLE IAW DC-9 SRM, CHAPTER 51-30-4. 2L72 4F A6WE 19950929006961995092900696WP 1995 9 29 ABXA9500744 119950607A5312991224397 BLKHD FASTENER DOUG DC9 DC941 302207NWP FS 1041 MISLOCATED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION, FOUND THE BULKHEAD AT FS 1041, VERTICAL BRACE, LOWER FASTENER, HAD IMPROPER EDGE DISTANCE ON THE LEFT SIDE. REPAIRED BRACE IAW ABX REA D953-11754. 2L72 4F A6WE 19950929006971995092900697WP 1995 9 29 ABXA9500745 119950606A32313927498503N DOOR ARM DOUG DC9 DC941 302207NWP BS 775 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY ON FLYING DOOR ARM. REPLACED RIGHT MAIN LANDING GEAR DOOR ARM ASSEMBLY AND BEARINGS IAW DC-9 M.M., CHAP. 32-10-6. 2L72 4F A6WE 19950929006981995092900698WP 1995 9 29 ABXA9500746 119950711A32314923281501 BEARINGS DOUG DC9 DC941 302207NWP BS 775 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D - CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR ACTUATING ROD ASSEMBLY HAD WORN BEARINGS. REPLACED ACTUATING ROD END AND BEARINGS IAW DC-9 M.M., CHAPTER 32-10-6. 2L72 4F A6WE 19950929006991995092900699WP 1995 9 29 ABXA9500747 119950927A324026014122 BRAKE DOUG DC8 DC863 302198AWP NR 8 LEAKING A ABXAK NONE AK FLAME/FIRE FLUID LOSS TXTAXI/GRND HDL 1 GL23814AX 34 46041 NR 8 BRAKE ASSEMBLY HAD MINOR FIRE ON ARRIVAL. EXTINGUISHED FIRE ON NR 8 BRAKE ASSEMBLY. FIRE WAS ATTRIBUTED TO HYDRAULIC FLUID LEAK ON BRAKE ASSEMBLY. REPLACED NR 8 BRAKE ASSEMBLY AND MAIN WHEEL ASSEMBLY. 2L74 4F 4A25 19950929007001995092900700SO 1995 9 29 COMA9511975 119950927A282012008718005 TUBE ASSY EMB 120 EMB120RT SO LT NACELLE CRACKED A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01137H 120137 FUEL LEAKING FROM LT ENGINE NACELLE. REPLACED CRACKED VENT VALVE FLOW LINE IN LT NACELLE. 2L72 4T RTA31SO 19950929007011995092900701EU 1995 9 29 COMA9531165 119950926A61218210163 GOVERNOR SAAB SF340 SF340A 7850100EU LT PROP DEFECTIVE A COMAK NONE O OTHER APAPPROACH 1 SO01320CA7656 11 340A064 LT PROPELLER RPM DROPS TO 1370 DURING FINAL APPROACH. REPLACED THE PROPELLER OVERSPEED GOVERNOR. 2L72 4T RTA52EU 19950929007021995092900702EA 1995 9 29 COMA9560557 119950926A7997601R5790015 HARNESS CNDAIRCL600 CL6002B19 EA RT ENGINE SHORTED A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01927CA4523 7031 RIGHT ENGINE LOW OIL PRESSURE WARNING DURING TAKEOFF. OIL PRESSURE GAUGE INDICATED NORMAL PRESSURE. REPLACED THE RT ENGINE PURPLE WIRING HARNESS. 2L72 4F RTA21EA 19950929007031995092900703EA 1995 9 29 COMA9560558 119950927A274070604 TCU CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA4441 1016 7017 STABILIZER TRIM DISCONNECTED DURING FLIGHT, COULD NOT RE-ENGAGE EITHER CHANNEL. REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2L72 4F RTA21EA 19950929007041995092900704EA 1995 9 29 COMA9560559 119950927A3250864806 STEERING CNDAIRCL600 CL6002B19 EA NLG FAILED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01912CA2746 508 7011 NOSE WHEEL STEERING FAILED, WOW INPUT AND WOW OUTPUT MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19950929007051995092900705 1995 9 29 COMA9560560 419950927A34178220372115 ADC CNDAIRCL600 CL6002B19 EA NR 1 DEFECTIVE A COMAK NONE J WARNING INDICATION CRCRUISE 1 SO01912CA1836 50 7011 EFIS COMP MESSAGE DURING FLIGHT. REPLACED THE NR 1 AIR DATA COMPUTER. 2L72 4F RTA21EA 19950929007061995092900706NM 1995 9 29 DL72S953808 119950924A3340 ACL WIRE G9325A1 BOEING727 727232 1384082NM FUSELAGE SHORTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11515DA 3472 21431 ON CLIMB-OUT, UPPER FUSELAGE ANTI-COLLISION LIGHT FELL OUT OF MOUNT AND CAUSED POWER WIRES TO SHORT, WITH RESULTING SPARKS AND SMOKE IN CABIN. FLT RETURNED TO CAE. FOUND DAMAGED WIRES ON LIGHT ASSEMBLY. REMOVED ASSEMBLY, SECURED WIRES, PLACED ON MCO. LIGHT ASSEMBLY WAS REPLACED, OPERATION NORMAL. 2L73 4F A3WE 19950929007071995092900707NM 1995 9 29 DL72S953818 119950925A7110 COWLING 6519645211 BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA DL27 22493 DURING A SHOP INSPECTION, THE UPPER FRAME ANGLE WAS FOUND TO BE CRACKED. A REPAIR WAS INSTALLED PER THE S.R.M. 54-10-3. FOR NR 2 ENGINE LEFT FORWARD COWL PANEL. 2L73 4F A3WE 19950929007081995092900708NM 1995 9 29 DL72S953819 119950926A57516572734104 SPAR BOEING727 727232 1384082NM RT AILERON CRACKED A ADALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 DURING INSPECTION, RT WING AILERON WAS FOUND WITH REAR SPAR CRACKED. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19950929007091995092900709NM 1995 9 29 DL72S953826 119950926A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11469DA 20746 FOUND DURING C-1 LETTER CHECK - 1.25 INCH CRACK IN RIB ON NR 7 SLAT I/B OF I/B TRACK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19950929007101995092900710NM 1995 9 29 DL72S953827 119950926A5330 SKIN BOEING727 727232 1384082NM BS 1308 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11469DA 20746 FOUND DURING C-1 LETTER CHECK - .75 INCH HOLE IN 48 SEC TORQUE BOX SKIN RT STA 1308 - .3750 INCH CRACK IN 48 SEC TORQUE BOX SKIN AT LIGHTNING HOLE STA 1235 RT. REPAIRS MADE PER M/M 53-11-0, PGS 802 - 832, AND 833. 2L73 4F A3WE 19950929007111995092900711NM 1995 9 29 DL72S953828 119950926A5754 DOUBLER BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11469DA 20746 FOUND DURING C-1 LETTER CHECK - DOUBLER UNDERNEATH I/B STOP PAD NR 7 SLAT IS CRACKED. REPAIRED PER MM 57-54-0 PAR 12. 2L73 4F A3WE 19950929007121995092900712NM 1995 9 29 DL72S953831 119950910A5530 WEB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 AT HMV, FOUND LOWER LEFT CORNER CRACKED VERT WEB INSIDE VERT STAB AT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950929007131995092900713NM 1995 9 29 DL72S953832 119950910A5530 WEB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 AT HMV, FOUND LOWER RT CORNER CRACKED VERT WEB INSIDE VERT STAB STA 1303. REPAIRED PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19950929007141995092900714NM 1995 9 29 DL73S953838 119950908A71106585378395 COWL BOEING737 737232 1384475NM ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11330DL 23102 DURING SHOP VISIT, ENGINE NOSE COWL ASSEMBLY WAS RESTORED PER CMM 65-85378. OUTER SKIN DENTED AT 5:30 POSITION. REPAIRED PER SRM 51-40-2. 2L72 4F RTA16WE 19950929007151995092900715NM 1995 9 29 DL757953829 119950926A3350 EEL BULB BOEING757 757232 1384965NM CABIN MISSING A DALAK NONE L NO TEST ININSP/MAINT 1 SO11639DL 23993 TRACK LIGHTING AT 30ABC OUT OF TRACK. REPLACED LIGHT BULB AND LENS COVER. OPS CK GOOD. 2L72 4F RTA2NM 19950929007161995092900716NM 1995 9 29 DL767953821 119950926A5754114T410225A TE WEDGE BOEING767 767232 1385132NM LT TE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 SLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55. 2L72 4F RTA1NM 19950929007171995092900717NM 1995 9 29 DL767953822 119950926A5754114T411317 TE WEDGE BOEING767 767232 1385132NM LT TE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11114DL 22226 SLAT WAS SENT TO SHOP FOR REPLACEMENT OF T/E WEDGE DUE TO HAIL DAMAGE. WEDGE WAS INSTALLED ACCORDING TO THE CMM 57-43-55. 2L72 4F RTA1NM 19950929007181995092900718NM 1995 9 29 DL767953823 119950921A5754114T410427A SKIN BOEING767 767232 1385132NM NR 4 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11114DL 000246 22226 HAIL DAMAGE TO UPPER SURFACE OF NR 4 L/E SLAT. THE TRAILING EDGE WEDGE WAS REPLACED PER CMM 57-43-55. THE PART NUMBER OF THE NEW WEDGE IS 114T4114-17. THIS IS THE TERMINATING ACTION FOR A.D. 93-14-19. 2L72 4F RTA1NM 19950929007191995092900719NM 1995 9 29 DL767953824 119950923A5754114T410529A TE WEDGE BOEING767 767232 1385132NM NR 4 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11114DL 000246 22226 THE WEDGE OF THE SLAT WAS DENTED DUE TO HAIL DAMAGE. THE WEDGE WAS REPLACED PER THE CMM 57-43-61. THE WEDGE REPLACEMENT IS THE TERMINATING ACTION FOR A.D. 93-14-19. 2L72 4F RTA1NM 19950929007201995092900720NM 1995 9 29 DL767953825 119950921A5754114T411119 TE WEDGE BOEING767 767232 1385132NM NR 1 LE SLAT DENTED A DALAK NONE C F.O.D. ININSP/MAINT 1 SO11114DL 22226 HAIL DAMAGE OCCURRED TO UPPER SURFACE OF T/E WEDGE. REPLACED WEDGE IN C/W C.M.M.57-43-41. 2L72 4F RTA1NM 19950929007211995092900721NM 1995 9 29 DL76L953843 119950909A3350 EEL WIRE BOEING767 767332 1382001NM CABIN SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11177DN 25122 EMERGENCY FLOOR TRACK LIGHTS INOP FROM ROW 13 TO 23 BOTH LEFT AND RIGHT SIDES OF A/C. REPAIRED SHORTED WIRE AT 12AB SIDEWALL AND REPLACED FUSE IN M9009 AND M9009 POWER SUPPLIES. OPERATION NORMAL. 2L72 4F RTA1NM 19950929007221995092900722NM 1995 9 29 P5CA9500789 119950928A361069B401425 DUCT BOEING747 747124 1384874NM LT WING FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23855FT 19733 ON PUSH-BACK, LT WING OVERHEAT LIGHT AND FORWARD CARGO OVERHEAT LIGHT CAME ON. REPLACED FAILED DUCT BETWEEN NR 1 AND NR 2 PYLON. 2L74 4F A20WE 19950929007231995092900723NM 1995 9 29 UPS204527 119950928A5320 BRACKET BOEING727 727185C 138406NNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON DELTA BEAM FORWARD ATTACH ANGLE BS 740 LBL 6 TO RBL 6, WL 155. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW 727 SRM 51-10-01, 51-10-2, 53-10-1, 51-30-2. 2L73 4F A3WE 19950929007241995092900724NM 1995 9 29 UPS204528 119950928A5320 LOAD BEAM BOEING727 727185C 138406NNM BS 740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SIDE LOAD BEAM STA 740, RBL 40 TO LBL 40, WL 170. REMOVED BEAM CHORD AND REPLACED WITH NEW CHORD IAW 727 SRM 51-10-2, 51-10-6, 51-30-2. 2L73 4F A3WE 19950929007251995092900725NM 1995 9 29 UPS204529 119950928A57307075T6 SKIN BOEING727 727185C 138406NNM WS 190-224.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING UPPER SKIN HAS CORROSION AND AN 8 INCH CRACK FROM RWS 190 TO 224.5 AT AFT SPAR. CUTOUT DAMAGED SKIN, FABRICATED, INSTALLED REPAIR DOUBLERS, PER UPS E.O. B727-5730-7416. 2L73 4F A3WE 19950929007261995092900726NM 1995 9 29 UPS204530 119950928A57112024T3 SPAR WEB BOEING727 727185C 138406NNM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE REMOVED CENTER CELL REAR SPAR WEB FOR ACCESS OF 870 TENSION STRAP. AFTER WEB REMOVAL, FOUND CORROSION ON WEB TO BE OUT OF LIMITS PER SRM 57-10-1. REPLACED BS 870 WEB PER SRM 51-30-2, 51-10-1, 51-10-2, 51-10-6, 51-30-5, 51-20-4 AND MM 51-20-151. 2L73 4F A3WE 19950929007271995092900727NM 1995 9 29 UPS204531 119950928A5521659561313 RIB BOEING727 727185C 138406NNM NR 1 ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 1 ELEVATOR HINGE SUPPORT RIB CRACKED IN THREE PLACES ON UPPER CHORD. REMOVED AND INSTALLED NEW SUPPORT RIB. WORK DONE IAW SRM 51-30-2 MM 27-20-1, MM 27-30-05, MM 27-30-81, MM 27-30-61, MM 27-30-00. 2L73 4F A3WE 19950929007281995092900728NM 1995 9 29 UPS204532 119950928A575465162268A SLAT BOEING727 727185C 138406NNM NR 5 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP ATTACH LUGS ARE CORRODED AT LUG MOUNT BOLTS OUT OF LIMITS. REMOVED AND REPLACED NR 5 K-FLAP PER MM 27-81-1 AND MM 27-81-00. 2L73 4F A3WE 19950929007291995092900729NM 1995 9 29 UPS204533 119950928A57111252024T0 SPAR CHORD BOEING727 727185C 138406NNM WS 130-224.5 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-02) RT WING UPPER SPAR CHORD IS CORRODED FROM WS 130 TO 224.5 AND GOING UNDER TRUNNION FITTING. REMOVED AND REPAIRED RT WING SPAR CHORD IAW UPS E.O. B727-5710-7410-A. 2L73 4F A3WE 19950929007301995092900730NM 1995 9 29 UPS204534 119950928A57112024T3511 SPAR CHORD BOEING727 727185C 138406NNM WS 180-184 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-581-03.00E-01) LT WING LOWER SPAR CHORD IS CORRODED AT WS 180 TO 184 IN HEEL OF CHORD. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS, REPAIRED PER UPS E.O. B727-5710-7411-A. 2L73 4F A3WE 19950929007311995092900731NM 1995 9 29 UPS204535 119950928A531365185602 STRINGER BOEING727 727185C 138406NNM WS 226-230 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 STRINGER (LOWER) RWS 226-230, LOCATED ON TOP SIDE OF BOTTOM HORIZONTAL LEG OUT OF LIMITS. REMOVED AND REPLACED STRINGER PER E.O. 757-57-1641. UPON REMOVAL OF STRINGER, FOUND DAMGED SHEAR TIE AND ANGLE. REMOVED AND REPLACED SHEAR TIE AND ANGLE IAW SRM 51-30-2. 2L73 4F A3WE 19950929007321995092900732NM 1995 9 29 UPS204536 119950928A53307075T6 SKIN BOEING727 727185C 138406NNM BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE ACCESSING 870 PRESSURE SEAL RETAINER, CORROSION UPPER SIDE OF TOP SKIN STA 870, LBL 45-65, WL 190. REMOVED CORROSION, REPAIRED SKIN PER USP E.O. 727-57-1648. 2L73 4F A3WE 19950929007331995092900733NM 1995 9 29 UPS204537 119950928A5312 BULKHEAD BOEING727 727185C 138406NNM BS 1183 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE WORKING FUSELAGE 13/CL2-115-01, A 3 INCH CRACK ON THE 1183 BULKHEAD, RBL 8, WL 181 - 2L 178. INSTALLED REPAIRS IAW E.O. B727-5311-0635B. 2L73 4F A3WE 19950929007341995092900734NM 1995 9 29 UPS204538 119950928A5720BAC15141493 CHORD BOEING727 727185C 138406NNM BS 740 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER CHORD BS 740 LBL 10 TO LBL 13 WL 165. REMOVED AND REPLACED BS 740 LOWER CHORD PER UPS E.O. B727-5710-7431 AND SRM 51-30-2, 51-20-4. 2L73 4F A3WE 19950929007351995092900735NM 1995 9 29 UPS204539 119950928A57202024T351 CHORD BOEING727 727185C 138406NNM BS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (SSID W-1A) ON EXTERIOR OF LOWER CHORD AT BS 870 RBL 41. WHILE REMOVING WEB, FOUND CORROSION ON LOWER SIDE OF CHORD BEYOND LIMITS. REPLACED LOWER CHORD. WORK DONE IAW E.O. B727-5710-7413-A. 2L73 4F A3WE 19950929007361995092900736NM 1995 9 29 UPS204540 119950928A5343658818956 TRUNNION FITTING BOEING727 727185C 138406NNM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND, AFTER REMOVING NOSE LANDING GEAR ON CARD 364793, BOTH RT AND LT NOSE TRUNNION FITTINGS CORRODED BEYOND LIMITS. REMOVED AND INSTALLED NEW FITTINGS. WORK DONE IAW SRM 51-10-2, 51-10-6, 53-10-1, 51-20-1, 51-30-5, 51-30-5, MM 32-33-0 AND E.O. B727-5310-3954B. 2L73 4F A3WE 19950929007371995092900737NM 1995 9 29 UPS204541 119950928A5755651922225 HINGE FITTING BOEING727 727185C 138406NNM NR 9 SPOILER CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 9 SPOILER SUPPORT FITTING IS CORRODED. REMOVED AND INSTALLED NEW FITTING WORK DONE IAW SRM 51-30-2 AND MM 27-51-131 AND MM 27-62-91. 2L73 4F A3WE 19950929007381995092900738NM 1995 9 29 UPS204542 119950928A571165162346 SPAR CHORD BOEING727 727185C 138406NNM WS 228 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON RT LOWER BEAM SPAR CHORD HORIZONTAL FLANGE AT WING STA 228. REMOVED CORROSION AND FOUND OT OF LIMITS. CUT OUT DAMAGE AREA OF SPAR CHORD AND SHEAR TIE, FABRICATED REPAIRS AND INSTALLED PER SRM 51-30-10, 51-30-2, E.O. B727-5710-7434-A. 2L73 4F A3WE 19950929007391995092900739NM 1995 9 29 UPS204543 119950928A5320BAC15061706 CHORD BOEING727 727108C 1384039NM BS 1110 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION BS 1110, WL 199 BL 0 ON THE STABILIZATION STRAP (CHORD) AROUND THE NUT PLATES. REMOVED CORROSION PER SRM 53-10-1. REMOVED DAMAGED SECTION, FABRICATED REPLACEMENT CHORD AND INSTALLED PER SRM 51-30-2 AND SRM 51-10-1. 2L73 4F A3WE 19950929007401995092900740NM 1995 9 29 UPS204544 119950928A53306519185056 SKIN BOEING727 727108C 1384039NM BS 1070-1080 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.06-03) ON INTERIOR SKIN STA 1070-1090 STR 10-14 RT FROM UNDER WINDOW CASTING AND REPAIR DOUBLERS. REPLACED WINDOW FRAME PER SRM 51-10-1, 51-10-2, 51-10-6, 51-30-2, 53-10-4 AND 51-20-4. 2L73 4F A3WE 19950929007411995092900741NM 1995 9 29 UPS204545 119950928A53137075T6 STRINGER BOEING727 727108C 1384039NM BS 1110-1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-03) ON STRINGER 1 STA 1110-1130. CORROSION MECHANICALLY REMOVED IAW SRM 51-10-6. REPAIRED STR 1 STA 1110-1130 IAW SRM 53-10-3. 2L73 4F A3WE 19950929007421995092900742NM 1995 9 29 UPS204546 119950928A531565163169 FLOOR BEAM BOEING727 727108C 1384039NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON FLOOR BEAM STA 344 LBL 60-RBL 60 WL 208. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6. REPAIRED FLOOR BEAM IAW SRM5 1-30-2, 51-10-2, 53-10-8. 2L73 4F A3WE 19950929007431995092900743NM 1995 9 29 UPS204547 119950928A5752652173624K TRIM TAB BOEING727 727108C 1384039NM RT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING I/B AILERON TAB IS DELAMINATED AT T/E (MARKED). REPLACED RT WING AILERON TAB IAW SRM 51-80. 2L73 4F A3WE 19950929007441995092900744NM 1995 9 29 UPS204548 119950928A551165168825 RIB BOEING727 727108C 1384039NM LT HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LOWER LT HORIZONTAL STAB RIB CHORD HAS A CRACK AT STA STA 8.00 (MARKED AT FRONT SPAR WEB). REMOVED AND REPLACED RIB CHORD AT LT STAB STA 8.00 PER SRM 51-10-1 AND SRM 51-30-2. 2L73 4F A3WE 19950929007451995092900745NM 1995 9 29 UPS204549 119950928A575465172838 RIB BOEING727 727108C 1384039NM NR 5 TE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON NR 5 SLAT 23 INCHES FROM O/B END (4TH RIB FROM O/B END, MARKED). REMOVED AND REPLACED 4TH RIB FROM O/B END OF NR 5 SLAT IAW SRM 51-30-2, 51-30-5. 2L73 4F A3WE 19950929007461995092900746NM 1995 9 29 UPS204550 119950928A5320 CLIP BOEING727 727108C 1384039NM BS 400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) BS 400 STR 19L ON STRINGER CLIP. REPLACED CLIP IAW SRM 51-10-6, 51-30-2 SRM 51-20-4. 2L73 4F A3WE 19950929007471995092900747NM 1995 9 29 UPS204551 119950928A53132024T3 STRINGER BOEING727 727108C 1384039NM BS 660-680 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-0.1-08-01) ON STR 6L STA 660-680. REPAIRED IAW SRM 53-10-3, 51-10-2, 51-10-3. 2L73 4F A3WE 19950929007481995092900748NM 1995 9 29 UPS204552 119950928A5311707T56 FRAME BOEING727 727108C 1384039NM BS 804 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND FRAME CRACKED AT STRINGER TO FRAME ATTACH POINT BS 804 STRINGER 14 RT. REPAIRED FRAME PER SRM 51-40-3. 2L73 4F A3WE 19950929007491995092900749NM 1995 9 29 UPS204553 119950928A575465172913 RIB BOEING727 727108C 1384039NM NR 3 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 3 SLAT, RIB JUST I/B OF TAI T-DUCT, CRACKED AT FWD CORNER. REMOVED AND REPLACED NR 3 SLAT RIB JUST I/B OF TAI T-DUCT IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950929007501995092900750NM 1995 9 29 UPS204554 119950928A575465172677 WEB BOEING727 727108C 1384039NM NR 4 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 7.25. REMOVED AND REPLACED NR 4 SLAT RIB AT SLAT STA 7.25 IAW SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19950929007511995092900751NM 1995 9 29 UPS204555 119950928A5754651627113 FITTING BOEING727 727108C 1384039NM NR 2 LE FLAP CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON UPPER FWD SIDE OF NR 2 K-FLAP OUTBOARD MOUNTING LUG WHILE WORKING NR 360298 (WINGS 203). REMOVED AND REPLACED NR 2 K-FLAP OUTBOARD MOUNTING FITTING PER SRM 51-30-2 AND MM 27-81-01. 2L73 4F A3WE 19950929007521995092900752NM 1995 9 29 UPS204556 119950928A53117075T6071 FRAME BOEING727 727108C 1384039NM BS 227.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-221-01.03-01) ON BACKSIDE OF WEB AT BS 227.8 LBL 41 WL 224. MECHANICALLY REMOVED CORROSION IAW SRM 51-10-6. REPAIRED WEB FRAME IAW SRM 51-40-2. 2L73 4F A3WE 19950929007531995092900753NM 1995 9 29 UPS204557 119950928A53302024T3 SKIN BOEING727 727108C 1384039NM BS 460-464 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND DISHED FASTENERS 4 EA AT BS460 - 464 519R (NOTE: ACCOMPLISHED NDI INSPECTION OF LAP PER E.O. B727-5330-0509. FOUND MATERIAL LOSS AT BS 461 - 476). ACCOMPLISHED REPAIR PER E.O. B727-5330-0509 AND SRM 53-30-3. 2L73 4F A3WE 19950929007541995092900754NM 1995 9 29 UPS204558 119950928A53126516306122 BLKHD ANGLE BOEING727 727108C 1384039NM BS 227.8 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 RBL 38 WL 199 AFT SIDE OF BULKHEAD ON SUPPORT ANGLE. REMOVED CORROSION MECHANICALLY IAW SRM 53-10-1. REMOVED AND REPLACED ANGLE (STIFFENER) IAW SRM 51-30-2, 51-10-1. 2L73 4F A3WE 19950929007551995092900755NM 1995 9 29 UPS204559 119950928A575465172676 RIB BOEING727 727108C 1384039NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB IN NR 5 SLAT 8 INCHES FROM I/B END (3RD RIB IN FROM I/B END MARKED). REPLACED RIB IAW SRM 51-30-2. 2L73 4F A3WE 19950929007561995092900756NM 1995 9 29 UPS204560 119950928A5753652163328 FLAP BOEING727 727108C 1384039NM RT TE MID FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING O/B MID-FLAP TO HAVE CRACKS AND CORROSION THROUGHOUT FLAP. MID-FLAP WAS REPLACED PER MM 27-51-11. 2L73 4F A3WE 19950929007571995092900757NM 1995 9 29 UPS204561 119950928A53302024T3080 SKIN BOEING727 727108C 1384039NM BS 829 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.01-02) ON SKIN AND LAP AT BS 829 STR 4 RT (ACCESS REQUIRED). MECHANICALLY REMOVED CORROSION IAW SRM 53-10-1. REPAIRED SKIN LAP IAW SMR 53-30-3. 2L73 4F A3WE 19950929007581995092900758NM 1995 9 29 UPS204562 119950928A5311 FRAME BOEING727 727108C 1384039NM BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION BS 420 STR 23R ON TOP AND FWD SIDE OF FRAME. FABRICATED AND INSTALLED REPAIR DOUBLER TO FRAME IAW 727 SRM 51-40-3. 2L73 4F A3WE 19950929007591995092900759NM 1995 9 29 UPS204563 119950928A5313 STRINGER BOEING727 727108C 1384039NM BS 680-700 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STR 6R FROM ST 680 - 700. CUT OUT DAMAGED SECTION OF STRINGER AND SPLICED IN NEW SECTION IAW 727 SRM 53-10-3. 2L73 4F A3WE 19950929007601995092900760NM 1995 9 29 UPS204564 119950928A5311 FRAME BOEING727 727108C 1384039NM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01) ON FRAME 344 BETWEEN STRINGER 1 TO STRINGER 8R. REPAIRED 344 FRAME IAW SRM 51-40-3. 2L73 4F A3WE 19950929007611995092900761NM 1995 9 29 UPS204565 119950928A551165382052 SPAR BOEING727 727108C 1384039NM RT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK MAINTENANCE FOUND AND REPLACED RT STAB UPPER FRONT SPAR CHORD DUE TO CORROSION AND CRACKS. INSTALLED NEW FRONT SPAR CHORD PER SRM 51-30-2. 2L73 4F A3WE 19950929007621995092900762NM 1995 9 29 UPS204566 119950928A571365C2613916 STRINGER BOEING727 727108C 1384039NM WS 629 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LEFT WING STRINGER NR 4 IS CRACKED AT WS 629.0. STOP DRILLED CRACK, INSTALL REPAIR KIT PER E.O. B727-5710-0314F. 2L73 4F A3WE 19950929007631995092900763NM 1995 9 29 UPS204567 119950928A571365C2613916 STRINGER BOEING727 727108C 1384039NM WS 656.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT WING UPPER STRINGER 14 AT WS 656-5 IS CRACKED. CUT OUT DAMAGE AREA. ALSO, STOP DRILL FINISH INSTALLATION OF KIT PER E.O. B727-5710-0314. 2L73 4F A3WE 19950929007641995092900764NM 1995 9 29 UPS204568 119950928A5315BAC150539042 FLOOR BEAM BOEING727 727108C 1384039NM FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CUT OUT DAMAGED PORTION OF FLOOR BEAM. FABRICATED NEW TOP CHORD AND INSTALLED. ALL WORK DONE IAW SRM 51-30-2, 51-40-2 AND 51-40-4. 2L73 4F A3WE 19950929007651995092900765NM 1995 9 29 UPS204569 119950928A5320 WEB BOEING727 727108C 1384039NM BS 350 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) AT BS 350 ON THE WEB AFT SIDE LBL 61 WL 181 TO 188. REPAIRED IAW SRM 53-10-1, 51-10-6, 51-40-2. 2L73 4F A3WE 19950929007661995092900766NM 1995 9 29 UPS204570 119950928A5313 STRINGER BOEING727 727108C 1384039NM BS 990-1050 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 4 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN NEW SECTION IAW SRM 53-10-3. 2L73 4F A3WE 19950929007671995092900767NM 1995 9 29 UPS204571 119950928A5313 STRINGER BOEING727 727108C 1384039NM BS 990-1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 5 LT STA 990 - 1050. CUT OUT DAMAGED SECTION OF STRINGER BETWEEN BS 990 - 1050 AND SPLICED IN A NEW SECTION IAW SRM 53-10-3. 2L73 4F A3WE 19950929007681995092900768NM 1995 9 29 UPS204572 119950928A5313 STRINGER BOEING727 727108C 1384039NM BS 990-1050 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND BARE METAL ON STRINGER 6 LT, STA 990 - 1050. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN A NEW SECTION IAW SRM 53-10-3 BETWEEN BS 990 - 1050. 2L73 4F A3WE 19950929007691995092900769NM 1995 9 29 UPS204573 119950928A5313BAC1498161 STRINGER BOEING727 727108C 1384039NM BS 1130-1180 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 3 LT STA 1130 - 1180. REPAIRED STRINGER PER SRM 53-10-3. 2L73 4F A3WE 19950929007701995092900770NM 1995 9 29 UPS204574 119950928A5311 FRAME BOEING727 727108C 1384039NM BS 350 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) BS 350 STR 22L ON AFT SIDE OF FRAME. REPAIRED FRAME IAW SRM 51-10-6, 53-10-1, 53-30-2, 51-40-2. 2L73 4F A3WE 19950929007711995092900771NM 1995 9 29 UPS204575 119950928A53117075T6 FRAME BOEING727 727108C 1384039NM BS 574-580 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01) ON MCD SHEAR WEB AT STA 574 TO 580 WL 208, LBL 60. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER. FINAL INSTALLATION PER SRM 51-10-2, 51-10-6, 53-10-11, 51-40-2, 51-30-2. 2L73 4F A3WE 19950929007721995092900772NM 1995 9 29 UPS204576 119950928A5312BAC15061706 BLKHD ANGLE BOEING727 727108C 1384039NM BS 227.8 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-111-01.00-01) STA 227.8 LBL 40 WL 186 AFT SIDE OF BULKHEAD, SUPPORT ANGLE CORRODED BEYOND LIMITS. REMOVED CORRODED AREA, INSTALLED REPAIR PER SRM 51-40-4. 2L73 4F A3WE 19950929007731995092900773NM 1995 9 29 UPS204577 119950928A53157075T6 FLOOR BEAM BOEING727 727108C 1384039NM BS 640 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53224-01.00-1) ON FLOOR BEAM, FLOORBOARD HOLES BS 640, RBL 32, 37, 41, 49, WL 208. REMOVED CORROSION, FOUND OUT OF LIMITS, CUT DAMAGE CHORD SECTION, FABRICATED CHORD SECTION. FINAL INSTALLATION PER SRM 53-10-1, 51-30-2. 2L73 4F A3WE 19950929007751995092900775WP 1995 9 29 95ZZZM475 119950812A3350 EEL WIRE DOUG DC9 DC932 3022066WP TAIL COMPT SHORTED A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11912VV 47359 AFT SECTION OF EPL'S AND TAIL COMPARTMENT EMERGENCY LIGHTS INOP. FOUND WIRING SHORTED BEHIND PANEL IN TAIL COMPARTMENT. REPAIRED WIRING AND REPLACED FUSES IN BATTERY CHARGER IAW MM CH 33. 2L72 4F A6WE 19950929007761995092900776CE 1995 9 29 95ZZZM476 119950812A5400 BRACKET BEECH 1900 1900C 1154161CE RT NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV12676 UC119 DURING THE AND INSPECTION, FOUND CRACK IN THE TOP FORWARD TOP OUTBOARD COWLING ATTACH BRACKET. WELDED CRACK AND RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19950929007771995092900777CE 1995 9 29 95ZZZM477 119950812A5400 BRACKET BEECH 1900 1900C 1154161CE LT NACELLE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07119YV12676 UC119 DURING AREA 'A' INSPECTION, LEFT INBOARD TOP FORWARD COWL ATTACH BRACKET WAS FOUND TO HAVE A SMALL CRACK. WELDED CRACK AND RETURNED TO SERVICE. 2L72 4T RTA24CE 19950929007781995092900778CE 1995 9 29 95ZZZM478 119950802A575335165050259 FLAP BEECH 1900 1900C 1154161CE RT WING CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07160AM8184 UC160 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND 10 INCH FROM O/B EDGE 3.5 INCH FROM TRAILING EDGE. REPAIRED WITH PATCH 4 INCH BY 5 INCH. (M) 2L72 4T RTA24CE 19950929007791995092900779CE 1995 9 29 95ZZZM479 119950812A575335165050258 FLAP BEECH 1900 1900C 1154161CE LT WING CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV 2342 UC137 DURING ROUTINE MAINTENANCE, A .5 INCH CRACK WAS FOUND INBOARD OF ATTACH POINT. REPAIRED WITH PATCH. (M) 2L72 4T RTA24CE 19950929007801995092900780EU 1995 9 29 AALA951164 119950628A3230DSB1102 SENSOR ELDEC AIRBUS300 A300B4605R 3930308EU RT MLG DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0718066 509 SJU - FLT 1786 - AFTER TAKEOFF ANU, LANDING GEAR WOULD NOT RETRACT IN SYSTEM 2. SELECTED SYSTEM 1 AND LANDING GEAR RETRACTED NORMALLY. AIRCRAFT PROCEEDED SJU AND LANDED WITHOUT INCIDENT. PLACARDED LANDING GEAR SYSTEM 2. SUBSEQUENTLY REPLACED RT MAIN LANDING GEAR SYSTEM 2 PROXIMITY DETECTION SENSOR 12GA AND ACCOMPLISHED BITE CHECK OF POSITION DETECTION UNIT WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (M) 2L72 4F RTA35EU 19950929007811995092900781EU 1995 9 29 AALA951251 119950712A3230DSB1102 PROXIMITY ELDEC AIRBUS300 A300B4605R 3930308EU RT MLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0790070 513 MIA - FLT NR 0799 - AFTER T/O SJU, UNABLE TO RAISE LANDING GEAR LEVER FROM NEUTRAL TO UP POSITION WITH SYS 1 SELECTED. SELECTED SYS 2 AND LANDING GEAR RETRACTED NORMALLY. A/C PROCEEDED TO MIA AND LANDED W/O INCIDENT. PLACARDED SYS 1 AND WHEN A/C DEPARTED MIA, PROBLEM REPEATED. A/C RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY BOX DUE TO FAILED BITE CHK. ACCOMPLISHED FUNCTIONAL CHECK FLT AND PROBLEM REPEATED. REPLACED SUPPORT BRACKET AND TARGET AT RT MAIN LANDING GEAR BOGIE BEAM. SYS GROUND CHK NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHK FLT AND LANDING GEAR OP CHECKED NORMAL USING SYS 1 AND SYS. REMOVED PLACARD FOR SYS 1 AND A/C RETURNED TO SERVICE. (M) 2L72 4F RTA35EU 19950929007821995092900782EU 1995 9 29 AALA951295 119950722A293053942100021PC0A INDICATOR AIRBUS300 A300B4605R 3930308EU GREEN HYD SYSTEMLEAKING A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW0714056 463 MIA - FLT NR 1292 - EN ROUTE PAP DURING CRUISE, GREEN HYDRAULIC SYSTEM LOW LEVEL INDICATION ON ECAM AND OVERHEAD PANEL. AIRCRAFT PROCEEDED TO MIA, ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND LANDED MIA WITHOUT INCIDENT. REPLACED HYDRAULIC CLOG INDICATOR AT HIGH PRESSURE FILTER FOR MANIFOLD FLIGHT CONTROL. ACCOMPLISHED LEAK AND SYSTEM GROUND CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19950929007831995092900783NE 1995 9 29 AALA951379 219950805A72501337M13G03 TUBE AIRBUS300 A300B4605R 3930308EU GE CF6 CF680C2A5 NE NR 2 ENGINE BROKEN A AALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW0780058 466 ORD - FLT NR 915 - AFTER TAKEOFF ORD, DURING CLIMB-OUT, NR 2 ENGINE FIRE LIGHT ILLUMINATED WITH WARNING ON ECAM. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NR 2 ENGINE HIGH PRESSURE COOLING TUBE AT 3 O'CLOCK POSITION. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN TO HIGH POWER WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F4 FRTA35EU E13NE 19950929007841995092900784EU 1995 9 29 AALA951446 119950811A2910AS1005D101006 HYD UNION TEE FOKKERF28 F28MK0100 4990807EU NR 1 HYD SYSTEM BROKEN A AALAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SW071411G 11369 ORD - FLT NR 0393 - DURING DESCENT INTO ORD, LOST ALL HYDRAULIC FLUID IN SYSTEM 1. ACCOMPLISHED ALTERNATE LANDING GEAR AND FLAP EXTENSIONS AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. REPLACED BROKEN 'T' FITTING UNDER CABIN FLOOR FOR HYDRAULIC SYSTEM 1. SERVICED HYDRAULIC SYSTEM AND ACCOMPLISHED LEAK CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19950929007851995092900785NM 1995 9 29 AALA951484 119950816A2840728800291 DRIPSTICK KAISER BOEING727 727227 1384078NM RT CTR FUEL TANKDEFECTIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07726AA 20733 MSY - FLT 0958 - WHILE EN ROUTE PTY, DURING CRUISE, A FAINT ODOR OF FUEL AT THE MID-SECTION OF THE CABIN WAS NOTED BY A FLIGHT ATTENDANT. THE ODOR BECAME STRONGER AND AIRCRAFT WAS DIVERTED TO MSY AND LANDED WITHOUT INCIDENT. A FUEL LEAK WAS CONFIRMED UNDER THE FORWARD PART OF THE FUSELAGE. AIRCRAFT WAS FERRIED TO TUL FOR REPAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. REPLACED DRIPSTICK ASSEMBLY. ALSO, AS PRECAUTIONARY REPLACED BOTH AIR CONDITIONING SYSTEMS WATER SEPARATOR BAGS. (M) 2L73 4F A3WE 19950929007861995092900786WP 1995 9 29 CAL950723 119950817A2612 FIRE LOOP DOUG DC9 DC982 3022082WP NR 1 ENGINE INOPERATIVE A CALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 SW0914890 49114 FLT NR 0114 - IAH - THE NR 1 ENGINE LOOP 'A' AND FIRE DETECT LOOP LIGHT ILLUMINATED WHILE ON DESCENT INTO IAH AT 15,000 FEET. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND BOTH FIRE BOTTLES WERE DISCHARGED. THE NR 1 ENGINE WAS SHUT DOWN. THE RED HANDLE LIGHT REMAINED ON FOR 10 MINUTES TO LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 1 ENGINE 'A' FIRE DETECTION LOOP WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. IN ADDITION, BOTH ENGINE FIRE BOTTLES WERE REPLACED. (M) 2L72 4F A6WE 19950929007871995092900787WP 1995 9 29 CAL950724 119950807A5312 JAMB DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .5 INCH CRACK IN LEFT LOWER CORNER OF DOOR JAMB AT AFT PRESSURE BULKHEAD. THE DOUBLER WAS REPAIRED IAW EA 653A006. (M) 2L72 4F A6WE 19950929007881995092900788WP 1995 9 29 CAL950725 119950811A5320 DOUBLERS DOUG DC9 DC932 3022066WP FWD BAGG BIN CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND CORROSION UNDER DOUBLERS AT FORWARD BAGGAGE BIN THRESHOLD. THE REPAIR DOUBLERS WERE REMOVED AND THE CORROSION WAS CLEANED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-05. (M) 2L72 4F A6WE 19950929007891995092900789WP 1995 9 29 CAL950726 119950814A5320 WEB DOUG DC9 DC932 3022066WP BS 996 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND WEB CORRODED AT RT LAV, STATION 996. THE SURFACE CORROSION WAS REMOVED. A NEW WEB AND SKIN CLIP WERE INSTALLED IAW ECRA 653C249. (M) 2L72 4F A6WE 19950929007901995092900790WP 1995 9 29 CAL950727 119950816A5350 CABLES DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0914810 49264 HOU - THE PASSENGER AFT ENTRANCE DOOR TAILCONE RELEASE PULLS LOW AT NINE POUNDS. THE AFT PASSENGER ENTRY DOOR TAILCONE RELEASE SYSTEM CABLES WERE ADJUSTED PER MM 53-53-00. (M) 2L72 4F A6WE 19950929007911995092900791WP 1995 9 29 CAL950728 119950816A5350S2274640 CLIP DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0914810 49264 HOU - THE TAILCONE INTERIOR RELEASE HANDLE PULLS LOW FROM CLIPS. THE INTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00. (M) 2L72 4F A6WE 19950929007921995092900792WP 1995 9 29 CAL950732 119950818A2520TA1201 RECEPTACLE DOUG DC9 DC931 3022065WP CABIN BURNED A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW0914564 47490 FLT NR 1579 - FLL - THE CREW REPORTED AN ODOR IN MID CABIN PRIOR TO LANDING AT FLL. MAINTENANCE FOUND PSU RECEPTACLE BETWEEN ROW 12-14 RT BURNED. THE RECEPTACLE AND PSU WERE REMOVED AND REPLACED. THE READING LIGHTS, CALL SWITCH, AND PASSENGER WARNING SIGNS CHECKED GOOD. (M) 2L72 4F A6WE 19950929007931995092900793WP 1995 9 29 CAL950735 119950820A29107912641861 HYDRAULIC LINE DOUG DC9 DC932 3022066WP LT WHEEL WELL LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0917557 47424 FLT NR 1542 - IAH - ALL HYDRAULIC FLUID IN THE LEFT SYSTEM WAS LOST DURING APPROACH TO IAH. THE PRESSURE AND QUANTITY DROPPED TO ZERO. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE IN LEFT WHEEL WELL LEAKING. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACED THE FLEX LINE WITHIN 1200 FLIGHT HOURS OR 500 FLIGHTS, WHICHEVER COMES FIRST. (M) 2L72 4F A6WE 19950929007941995092900794WP 1995 9 29 CAL950736 119950820A49703812761 OIL PRESS LIGHT DOUG DC9 DC982 3022082WP APU MALFUNCTIONED A CALAO OTHER N FALSE WARNING CRCRUISE 1 SW0969803177643324 49229 FLT NR 0200 - IAH - WHILE OPERATING THE APU IN FLIGHT, WITH THE LEFT GENERATOR PLACARDED INOPERATIVE, THE APU LOW OIL PRESSURE LIGHT ILLUMINATED. THE APU WAS SHUT DOWN AND THE FLIGHT WAS COMPLETED WITHOUT ANY FURTHER PROBLEM. MAINTENANCE CHECKED THE APU OIL LEVEL AND FOUND IT TO BE FULL. THE APU WAS STARTED AND RAN WITHOUT FAULT. THE FAILURE COULD NOT BE DUPLICATED. (M) 2L72 4F A6WE 19950929007951995092900795WP 1995 9 29 CAL950737 119950814A5400 CHANNEL DOUG DC9 DC932 3022066WP NR 1 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091250746100 47788 IAH - INSPECTION FOUND TWO 'Z' CHANNELS CRACKED AT TOP OF CANNON PLUG COMPARTMENT OF NR 1 ENGINE PYLON. THERE WERE THREE CRACKS MEASURING 4.125 INCHES, 1.5 INCHES AND 1.25 INCHES LONG. TWO NEW 'A' CHANNELS WERE FABRICATED AND INSTALLED IAW SRM 54-10-0, PAGE 2, FIGURE 1. (M) 2L72 4F A6WE 19950929007961995092900796NE 1995 9 29 CAL950740 219950821A7230737314 BLADE LOCK DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE FRACTURED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW09838723223 49120 709804 FLT NR 149 - PHL - THE NR 1 ENG FAILED WHILE IN FLIGHT AT 31,000 FEET. THE ENGINE INDICATIONS AFTER FAILURE WERE, EGT 800, N1 20 PERCENT, N2 49 PERCENT, AND OIL PRESSURE AT 8 PSI. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO PHL WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. TEARDOWN REVEALED A C10 BLADE LOCK FRACTURE AS THE PRIMARY CAUSE OF THE ENGINE FAILURE. (M) 2L72 4F4 F A6WE E9NE 19950929007971995092900797WP 1995 9 29 CAL950741 119950809A5330 SKIN DOUG DC9 DC932 3022066WP BS 143-173 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .5 INCH CRACK AND CORROSION IN SKIN BETWEEN STATION 143 AND 173 AT LONGERON 30. THE AREA WAS REPAIRED IAW ECRA 5330-02310. (M) 2L72 4F A6WE 19950929007981995092900798WP 1995 9 29 CAL950742 119950809A5314 KEEL BEAM DOUG DC9 DC932 3022066WP BS 622 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM AT STATION 622R. THE CRACKED AREA WAS TRIMMED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 12. (M) 2L72 4F A6WE 19950929007991995092900799WP 1995 9 29 CAL950743 119950809A5314 KEEL BEAM DOUG DC9 DC932 3022066WP BS 639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .5 INCH CRACK IN KEEL BEAM AT STATION 639L. A DOUBLER PLATE WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 12. (M) 2L72 4F A6WE 19950929008001995092900800NM 1995 9 29 CAL950752 119950824A2910651782111 HYD MODULE BOEING727 727227 1384078NM 'A' HYD SYSTEM LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0915774 21242 FLT NR 0299 - EWR - THE 'A' HYD SYSTEM OVERHEAT LIGHT ILLUMINATED IN FLIGHT. THE 'ABNORMAL' PROCEDURES WERE COMPLIED WITH, BUT HAD NO EFFECT. A RETURN TO EWR WAS INITIATED AND ON FINAL APPROACH THE 'A' SYSTEM PRESSURE WENT TO 500 PSI ACCOMPANIED BY ILLUMINATION OF BOTH HYDRAULIC 'A' SYSTEM LOW PRESSURE LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE 'A' SYSTEM HYDRAULIC MODULE LEAKING. THE MODULE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. (M) 2L73 4F A3WE 19950929008011995092900801WP 1995 9 29 CAL950753 119950808A5330 SKIN DOUG DC9 DC932 3022066WP BS 1038 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .25 INCH CRACK IN LEFT FUSELAGE SKIN AT STATION 1038, LONGERON 1. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2. (M) 2L72 4F A6WE 19950929008021995092900802WP 1995 9 29 CAL950754 119950808A5330 SKIN DOUG DC9 DC932 3022066WP BS 1038 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753165802 45847 HOU - INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038, ABOVE RT PYLON. THE CRACKED SKIN WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 18. (M) 2L72 4F A6WE 19950929008031995092900803WP 1995 9 29 CAL950761 119950827A3230 ANTI-RETRACT LVR DOUG DC9 DC932 3022066WP NLG OUT OF RIG A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0918544 47219 FLT NR 9873 - STA 31J - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM 31J (AERO CORP). THERE WAS NO GROUND SHIFT TO AIRBORNE. THE AIRCRAFT WAS RETURNED TO 31J WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE GROUND SENSE AND ANTI-RETRACTION LEVER IAW MM 32-23-1 AND OPERATION CHECKED GOOD. IN ADDITION, THE NLG POSITION INTERLOCK SWITCH WAS REMOVED AND REPLACED. A GEAR SWING WAS PERFORMED IAW MM 32-30 AND OPERATION CHECKED GOOD. (M) 2L72 4F A6WE 19950929008041995092900804WP 1995 9 29 CAL950762 119950823A5400 SKIN DOUG DC9 DC932 3022066WP NR 2 PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0914524 47539 HOU - INSPECTION FOUND A .5 INCH CRACK IN SKIN ON TOP SIDE OF NR 2 ENGINE PYLON. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-02. (M) 2L72 4F A6WE 19950929008051995092900805NM 1995 9 29 CAL950769 119950829A2750652355936 TRANSMISSION BOEING727 727232 1384082NM TE FLAPS INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09523PE222997004 20646 FLT NR 0219 - EWR - THE OUTBOARD TRAILING EDGE FLAPS FAILED TO EXTEND ON APPROACH TO EWR. USE OF FLAP ALTERNATE DRIVE SYSTEM WAS NO HELP. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OUTBOARD NR 8 FLAP TRANSMISSION AT FAULT. THE NR 8 FLAP TRANSMISSION WAS REMOVED AND REPLACED PER MM 27-51-41 AND OPERATION CHECKED GOOD. (M) 2L73 4F A3WE 19950929008061995092900806NE 1995 9 29 VTZA95273 219950830A7320NAS62038D BOLT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE MISSING A AVTZAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 EA27307UE 41021 P75039 FLT NR 6341 - IAD-LGA - DURING TAXI, RETURNED TO GATE DUE TO THE LEFT ENGINE CONDITION LEVER WILL NOT COME OUT OF TAXI POSITION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND CONDITION LEVER ROD END BOLT MISSING AT FUEL CONTROL CONNECTION. REPLACED BOLT AND AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA41NM E18NE 19950929008071995092900807EU 1995 9 29 VTZA95275 119950831A77208972605 TRANSDUCER BAG JETSTMJETSTM3201 1500217EU NR 2 ENGINE FAILED A VTZAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27473UE 828 FLT NR 6173 - IAD-HVN - DURING TAKEOFF ROLL, ABORTED THE TAKEOFF DUE TO THE NR 2 ENGINE BYPASSED (TTL) AT 88 PERCENT TORQUE WITH TARGET TORQUE BEING 90-93 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DELTA P OVER P TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950929008081995092900808EU 1995 9 29 VTZA95276 119950831A527091SE13 SWITCH BAG JETSTMJETSTM3201 1500217EU BAGGAGE POD OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27472UE 823 FLT NR 0906 - LYH-CHO - DURING CLIMB-OUT, RETURNED TO LYH DUE TO THE POD DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE DOOR MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19950929008091995092900809EU 1995 9 29 VTZA95277 119950830A7330696219 TRIPLE GAUGE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP COCKPIT FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER CLCLIMB 1 EA27484UE 899 FLT NR 6365 - IAD-ROC - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT FUEL PRESSURE INDICATION FLUCTUATING AFTER TAKEOFF. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE TRIPLE GAUGE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T3 TRTA56EU E3WE 19950929008101995092900810EU 1995 9 29 VTZA95278 119950901A2751TY176004A POS TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU LT TE FLAP FAILED A VTZABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27313UE 41026 FLT NR 6483 - IAD-CHS - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE FLAP ASYMMETRY WARNING. FLIGHT CREW DECLARED AN EMERGENCY AND PERFORMED AN EMERGENCY DESCENT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE LEFT FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950929008111995092900811EU 1995 9 29 VTZA95279 119950831A2751TY176004A POS TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU RT TE FLAP DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27323UE 41059 FLT NR 6416 - IAD-CHS - DURING CRUISE RETURNED TO IAD DUE TO THE FLAP ASYMMETRY WARNING SOUNDING IN FLIGHT. FLIGHT CREW TRIED RESETTING BUT COULD NOT GET IT TO RESET. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED AND CHECKED RIGGING ON RIGHT FLAP TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950929008121995092900812EU 1995 9 29 VTZA95281 119950901A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27315UE 41033 FLT NR 6462 - EWR-IAD - ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE BAGGAGE DOOR WARNING MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19950929008131995092900813 1995 9 29 95ZZZM480 419950725A34256229682002 DISPLAY UNIT BEECH 1900 1900D 1154162CE LEFT INOPERATIVE A GLBAA UNSCHED LANDING I FLT. ATTITUDE INST. TOTAKEOFF 1 CE01101UX957 410 UE101 FAR - THE CREW ELECTED AN AIR TURNBACK AFTER A RIGHT SIDE DISPLAY UNIT AND EFIS FAILURE. FOLLOWING AN UNEVENTFUL LANDING, MAINTENANCE RERACKED THE DISPLAY UNIT AND A GROUND CHECK WAS SATISFACTORY. (M) 2L72 4T RTA24CE 19950929008141995092900814SO 1995 9 29 95ZZZM481 119950818A215022045402 COOLING TURBINE EMB 120 EMB120 3260201SO RIGHT SMOKING A GLBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE01293UX2129 120293 MOT - DURING FLIGHT, THE CREW REPORTED A RIGHT ENVIR FAIL LIGHT, SMOKE ALARM, AND SMOKE IN THE CABIN. THE SMOKE SMELLED LIKE OIL. THE RIGHT PACK WAS SHUTOFF AND THE SMOKE CLEARED. MAINTENANCE OPERATED THE RIGHT PACK AND COULD NOT DUPLICATE THE DISCREPANCY. 2L72 4T RTA31SO 19950929008151995092900815 1995 9 29 95ZZZM482 419950816A34131143800353 VSI BEECH 1900 1900C 1154161CE INST PANEL FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01159GL 640 W29297HA UC159 DUL - THE CREW ELECTED AN AIR TURNBACK AFTER THE NR 2 VSI FAILED. FOLLOWING AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE UNIT WHICH TESTED SATISFACTORILY. 2L72 4T RTA24CE 19950929008161995092900816CE 1995 9 29 95ZZZM483 119950815A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RIGHT CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0145GL 4467 469 UC45 ESC - DURING THE ROUTINE TRUSS INSPECTION REQUIRED BY AD95-02-18, A .75 INCH CRACK WAS FOUND NEAR THE LINSEED OIL PLUG OF THE INBOARD AREA 'A' OF THE RIGHT TRUSS. THE TRUSS WAS REPAIRED IAW BEECH KIT 129-9006, REPAIR NR 2. 2L72 4T RTA24CE 19950929008171995092900817CE 1995 9 29 95ZZZM484 119950809A7997 WIRE BEECH 1900 1900C 1154161CE LT ENGINE BROKEN A GLBAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE01123UE13966 UC123 GRI - THE CREW ELECTED AN AIR TURNBACK AFTER NOTING THAT THE LEFT OIL PRESSURE GAUGE FLUCTUATED BETWEEN 60-90 PSI IN CRUISE. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE SOLDERED BROKEN WIRES ON A CANNON PLUG AT THE PRESSURE TRANSDUCER. SYSTEM WAS OPS CHECKED SATISFACTORILY. 2L72 4T RTA24CE 19950929008181995092900818EA 1995 9 29 95ZZZM485 219950808A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LEFT OIL LEAK A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 CE0179GL UC79 PCE32523 ORD - ON FINAL APPROACH, THE CREW NOTED FAINT SMOKE WAS ENTERING THE CABIN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE DETERMINED THAT THE LEFT ENGINE HAD AN INTERNAL OIL LEAK. THE ENGINE WAS REPLACED AND TESTED SATISFACTORILY. 2L72 4T4 TRTA24CE E4EA 19950929008191995092900819EA 1995 9 29 95ZZZM486 219950731A7313MS937116 NOZZLE GASKET BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE LEAKING A AGBLAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 NM0784GL 45 45 UC84 DEN - THE CREW ELECTED AN AIR TURNBACK WHEN THE LEFT ENGINE LOST POWER IN FLIGHT AND TORQUE DROPPED TO 1000 AT FULL POWER. MAINTENANCE FOUND SEVERAL FUEL NOZZLE GASKETS (MS937116) LEAKING. ALL FUEL NOZZLES AND GASKETS WERE CHANGED AND LEAKED CHECKED GOOD. A POWER RUN WAS SATISFACTORY. 2L72 4T4 TRTA24CE E4EA 19950929008201995092900820CE 1995 9 29 95ZZZM487 119950808A712012991003279 TRUSS BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01101UE 3007 UC101 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE OUTER LEFT ENGINE TRUSS CRACKED AT UPPER WELD ON COWL ATTACH BRACKET ON TUBE, APPROXIMATELY .5 INCH LONG ON OUTER AND .125 INCH LONG ON INNER. BOTH CRACKS WERE REPAIRED IAW BEECH KIT NR 129-9006. 2L72 4T RTA24CE 19950929008211995092900821CE 1995 9 29 95ZZZM488 119950729A3260101381006 UPLOCK SWITCH BEECH 1900 1900C 1154161CE NLG WW DEFECTIVE A GLBAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 CE0155594 UC145 FOD - THE CREW ELECTED TO DIVERT TO SPW AFTER THEY COULD NOT GET A GEAR SAFE LIGHT INDICATION ON APPROACH TO FOD. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE INSTALLED A NEW UPLOCK SWITCH AND CYCLED THE GEAR. ALL INDICATIONS WERE SATISFACTORY. 2L72 4T RTA24CE 19950929008221995092900822 1995 9 29 95ZZZM489 419950727A34426227337001 RECEIVER/TRANS BEECH 1900 1900C 1154161CE NOSE INTERMITTENT A GLBAA UNSCHED LANDING O OTHER TOTAKEOFF 1 CE0145GL 1328 UC45 DVL - THE CREW ELECTED AN AIR TURNBACK AFTER THE WEATHER RADAR PICTURE SHRUNK AND THE HORIZONTAL WAS INTERMITTENT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED FOLLOWED BY THE REPLACEMENT OF THE RADAR R/T. 2L72 4T RTA24CE 19950929008231995092900823CE 1995 9 29 95ZZZM490 119950724A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01166GL 5906 1034 UC166 ESC - DURING INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED. THE .5 INCH CRACK WAS CENTERED AT THE OIL PLUG ON THE UPPER LEFT FORWARD LEG. A WELD REPAIR WAS ACCOMPLISHED IAW BEECH REPAIR KIT NR 129-9006-1 REPAIR NR 2. 2L72 4T RTA24CE 19950929008241995092900824CE 1995 9 29 95ZZZM491 119950719A3297 WIRE BEECH 1900 1900C 1154161CE RT MLG BROKEN A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0167UE 7872 UC67 DEN - THE CREW ELECTED AN AIR TURNBACK AFTER THE LANDING GEAR RELAY BREAKER POPPED. THE GEAR WAS EXTENDED MANUALLY FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REPAIRED BROKEN WIRE AT SQUAT SWITCH. REPLACED SQUAT SWITCH P/N 44EN49-6 AND K-3 RELAY P/N MS2417LD1. GEAR TESTED SATISFACTORILY. 2L72 4T RTA24CE 19950929008251995092900825CE 1995 9 29 95ZZZM492 119950719A3230571203 MOTOR BEECH 1900 1900C 1154161CE LT MLG FAILED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE0167UE 7868 UC67 GRI - THE CREW ELECTED AN AIR TURNBACK AFTER REPEATED LANDING GEAR RELAY CIRCUIT BREAKER FAILURES. THE GEAR WAS EXTENDED MANUALLY FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR MOTOR (P/N 571203 S/N 1060A) AND PRESSURE SWITCH (P/N 570383 S/N 0201). THE GEAR WAS SUCCESSFULLY CYCLED THREE TIMES. 2L72 4T RTA24CE 19950929008261995092900826EU 1995 9 29 C2XA95IA220 119950906A5210 SKIN AEROSPATR42 ATR42320 8680930EU PAX DOOR CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926826 172 IAH - DURING C-CHECK INSPECTION, THE PAX/CREW ENTRY DOOR WAS FOUND TO BE CORRODED ON THE INNER SKIN. MAINTENANCE REMOVED THE DOOR (P/N S5217600101200), REPAIRED THE DOOR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EA 5210-01006, AND REINSTALLED THE DOOR. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19950929008271995092900827SO 1995 9 29 C2XA95IA224 119950911A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008281995092900828SO 1995 9 29 C2XA95IA225 119950911A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008291995092900829SO 1995 9 29 C2XA95IA226 119950911A572012017056017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008301995092900830SO 1995 9 29 C2XA95IA227 119950911A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008311995092900831SO 1995 9 29 C2XA95IA228 119950911A572012017056021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008321995092900832SO 1995 9 29 C2XA95IA229 119950911A572012017056013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008331995092900833SO 1995 9 29 C2XA95IA230 119950911A572012017056021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008341995092900834SO 1995 9 29 C2XA95IA231 119950911A572012017057008 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008351995092900835SO 1995 9 29 C2XA95IA232 119950911A572012017059019 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 20, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008361995092900836SO 1995 9 29 C2XA95IA233 119950911A572012017059019 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008371995092900837SO 1995 9 29 C2XA95IA234 119950911A572012017057007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008381995092900838SO 1995 9 29 C2XA95IA235 119950911A572012017059015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008391995092900839SO 1995 9 29 C2XA95IA236 119950911A572012017059017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008401995092900840SO 1995 9 29 C2XA95IA237 119950911A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 3 SKIN SUPPORT, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008411995092900841SO 1995 9 29 C2XA95IA238 119950911A572012017057005 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008421995092900842SO 1995 9 29 C2XA95IA239 119950911A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008431995092900843WP 1995 9 29 CAL950729 119950816A5350 CABLES DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0914810 49264 HOU - THE TAILCONE INTERIOR RELEASE PULLS HIGH AT 68 POUNDS. THE TAILCONE INTERIOR RELEASE SYSTEM CABLES WERE ADJUSTED PER MM 53-53-00. (M) 2L72 4F A6WE 19950929008441995092900844WP 1995 9 29 CAL950730 119950816A5350S2274640 CLIP DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A CALAK NONE O OTHER ININSP/MAINT 1 SW0914810 49264 HOU - THE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW FROM CLIPS AT 16 POUNDS. THE TAILCONE EXTERIOR RELEASE HANDLE CLIPS WERE ADJUSTED PER MM 53-53-00. (M) 2L72 4F A6WE 19950929008451995092900845WP 1995 9 29 CAL950738 119950811A52403917853503 BEAM DOUG DC9 DC982 3022082WP AFT SERVICE DOORCRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091481030710 49264 HOU - INSPECTION FOUND A 2 INCH CRACK ON LEFT SIDE OF BEAM AT AFT SERVICE DOOR. REMOVED AND REPLACED BEAM IAW SRM 51-60-0. (M) 2L72 4F A6WE 19950929008461995092900846WP 1995 9 29 CAL950739 119950811A5280SB093201893 DOOR DOUG DC9 DC982 3022082WP LT MLG CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091481030710 49264 HOU - INSPECTION FOUND A 2.5 INCH CRACK IN AFT EDGE OF LEFT MLG DOOR. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 28. (M) 2L72 4F A6WE 19950929008471995092900847NM 1995 9 29 CAL950746 119950823A2720591005015 PWR CONTROL UNIT BOEING727 727232 1384082NM RUDDER INOPERATIVE A ACALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SW09523PE38872 20646 FLT NR 0354 - SJU - WHILE CRUISING AT FL 280 THE AIRCRAFT BEGAN A 'FISHTAILING' MOTION. THE AIRCRAFT WAS SLOWED TO APPROXIMATELY 270 AND BOTH YAW DAMPERS WERE CYCLED OFF, BUT THIS DID NOT CORRECT THE PROBLEM. THE AIRCRAFT WAS RETURNED TO SJU. MAINTENANCE FOUND THE UPPER RUDDER POWER CONTROL UNIT AT FAULT. THE UPPER RUDDER PCU WAS REMOVED AND REPLACED PER MM 27-20-141, PAGE 201. AN OPERATIONAL TEST AND ADJUSTMENT OF THE SYSTEM WAS PERFORMED PER MM 27-20-141, PAGES 206-210 AND THE SYSTEM FUNCTIONED NORMALLY. (M) 2L73 4F A3WE 19950929008481995092900848NM 1995 9 29 IXKA9500025 119950829A2612FRF651253508 PLUG BOEING727 727251 138408HNM NR 2 ENG DAMAGED A IXKAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 EA25264US 19983 ON DESCENT INTO EWR, NR 2 ENGINE FIRE HANDLE INDICATED A FIRE WARNING. BOTH BOTTLE DISCHARGED, LIGHT REMAINED ON. LANDED AT EWR WITHOUT INCIDENT. FOUND NR 2 ENGINE FIRE SENSE PLUG (D1490) MISSING INSULATION IN PLUG. SYSTEM CHECKED NORMAL AS PER MM 26-11-00. (M) 2L73 4F A3WE 19950929008491995092900849 1995 9 29 ORJA9570 419950731A3442 RADAR DISH DOUG DC9 DC982 3022082WP FWD FUS CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11841RA 49421 MINOR SURFACE CORROSION ON FORWARD AND AFT FACE OF RADAR DISH. REMOVED CORROSION IAW SRM 51-10-2. TREATED IAW SRM 51-10-3. (M) 2L72 4F A6WE 19950929008501995092900850WP 1995 9 29 ORJA9571 119950731A5720 FAIRING DOUG DC9 DC982 3022082WP LT WING CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11841RA 49421 LEFT WING TIP UNDER LOGO LIGHT FAIRING TOP AND BOTTOM HAS CORROSION. CLEANED CORROSION FROM LEFT WING TIP LOGO LIGHT FAIRING IAW SRM 51-10-3. (M) 2L72 4F A6WE 19950929008511995092900851WP 1995 9 29 ORJA9572 119950802A2550 HOLD DOWN RAIL DOUG DC9 DC982 3022082WP BAGGAGE COMPT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11841RA 49421 CORROSION ON TOP OF AND BELOW BAGGAGE HOLD DOWN RAIL APPROXIMATELY 6 INCHES IN BACK OF AND FORWARD OF BAGGAGE DOOR. REPAIRED REF SRM 51-10-2. (M) 2L72 4F A6WE 19950929008521995092900852SW 1995 9 29 95ZZZM493 119950907A52102724150 COVER SWRNGNSA227 SA227AC 8780603SW PAX CRACKED A MALAO OTHER O OTHER ININSP/MAINT 1 GL15438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LOWER FORWARD PASSENGER DOOR CORNER (P/N 27-24044) AND LOWER FORWARD PASSENGER DOOR COVER (P/N 27-24150) CRACKED IN RADIUS. THEY REPLACED THE CRACKED PARTS IAW FAIRCHILD SRM 51-00-00. REF NR MALA954626. 1L72 4T A8SW 19950929008531995092900853CE 1995 9 29 95ZZZM494 119950831A324611480013 WHEEL BFGOODRICH 3B1426 BEECH 1900 1900D 1154162CE NOSE GEAR BROKEN A AJJBAO OTHER O OTHER TXTAXI/GRND HDL 1 EA01841CA3925 0511 UE40 DURING TAXI ONTO RUNWAY A STEERING PROBLEM WAS NOTED. INSPECTION OF NOSE GEAR BY MAINTENANCE, REVEALED THAT THE INNER HALF OF NOSE WHEEL WAS BROKEN AROUND THE COMPLETE RADIUS OF WHEEL. NOSE WHEEL AND TIRE REPLACED. (M) 2L72 4T RTA24CE 19950929008541995092900854NM 1995 9 29 95ZZZM495 119950823A3350900542 EEL BATT CHARGER BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND BATTERY CHARGER, LIGHTS OPERATED NORMALLY. REF ASAA9510077. 2L72 4F A16WE 19950929008551995092900855WP 1995 9 29 95ZZZM496 119950710A5530591218836 ANGLE DOUG DC9 DC931 3022065WP BS 1076 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. REF USAA950883. 2L72 4F A6WE 19950929008561995092900856NM 1995 9 29 ASAA9510076 119950823A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 17. REPLACED BATTERY PACK AND LIGHTS NORMALLY. (M) 2L72 4F A16WE 19950929008571995092900857NM 1995 9 29 ASAA9510077 119950823A3350900835A EEL BATTERY PACK BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND BATTERY CHARGER, LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19950929008581995092900858NM 1995 9 29 ASAA9510078 119950824A335086210144 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EXIT LIGHT WOULD NOT EXTINGUISH AFTER TEST. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950929008591995092900859NM 1995 9 29 ASAA9510080 119950826A335020131A EEL BATTERIES BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND MID EMERGENCY EXIT FLOOR TRACK LIGHTING TRANSMITTERS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES, AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950929008601995092900860NM 1995 9 29 ASAA9510081 119950827A33508731002142 EEL ASSEMBLY BOEING737 737298C 1384490NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950929008611995092900861NM 1995 9 29 ASAA9540047 119950824A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01771AS 25104 OAK - FLT NR 486 - DURING PREFLIGHT, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15-17. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950929008621995092900862NM 1995 9 29 ASAA9540048 119950829A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - FLT NR 413 - EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 11 AND 12 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROWS 11 AND 12, LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19950929008631995092900863WP 1995 9 29 ASAA9580190 119950823A33501001191 PORTABLE EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01973AS17693 53449 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950929008641995092900864WP 1995 9 29 ASAA9580191 119950825A3350014597101 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01948AS 53021 SEA - PRIOR TO DEPARTURE OF FLT 116, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 6 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES, AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19950929008651995092900865WP 1995 9 29 ASAA9580193 119950828A3350 EEL TERMINAL DOUG DC9 DC982 3022082WP TAILCONE LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01941AS 49925 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE TAILCONE WAS FOUND INTERMITTENT. SECURED LOOSE TERMINAL ON LIGHT SOCKET AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19950929008661995092900866EU 1995 9 29 C2XA95IA219 119950906A5712S5721158200100 RIB AEROSPATR42 ATR42320 8680930EU RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926826 172 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LEADING EDGE RIB NR 30 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED RIB USING A DOUBLER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19950929008671995092900867SO 1995 9 29 C2XA95IA221 119950911A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008681995092900868SO 1995 9 29 C2XA95IA222 119950911A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008691995092900869SO 1995 9 29 C2XA95IA223 119950911A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916723 120169 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19950929008701995092900870SW 1995 9 29 MALA954622 119950906A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD LOWER FORWARD WING SKIN-TO-NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M) 1L72 4T A8SW 19950929008711995092900871SW 1995 9 29 MALA954623 119950906A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT OUTBOARD UPPER FORWARD WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAIRCHILD ARP 54-20-9101. (M) 1L72 4T A8SW 19950929008721995092900872SW 1995 9 29 MALA954624 119950906A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE RT FLAP WALKING BEAM ROLLER DOUBLER WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M) 1L72 4T A8SW 19950929008731995092900873SW 1995 9 29 MALA954625 119950906A57532731141001 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE LEFT FLAP WALKING BEAM ROLLER DOUBLER TO BE WORN NEAR LIMITS. THEY REPLACED THE DOUBLER IAW FAIRCHILD ARP 57-20-9424. (M) 1L72 4T A8SW 19950929008741995092900874SW 1995 9 29 MALA954626 119950907A52102724044 CORNER SWRNGNSA227 SA227AC 8780603SW PAX CRACKED A MALAO OTHER O OTHER ININSP/MAINT 1 GL15438MA AC721B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LOWER FORWARD PASSENGER DOOR CORNER (P/N 27-24044) AND LOWER FORWARD PASSENGER DOOR COVER (P/N 27-24150) CRACKED IN RADIUS. THEY REPLACED THE CRACKED PARTS IAW FAIRCHILD SRM 51-00-00. (M) 1L72 4T A8SW 19950929008751995092900875NM 1995 9 29 MALA954627 119950907A324021565 BRAKE DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15866MA 366 FLIGHT 3429 - DURING TAXI FROM GATE AT DTW, THE CREW NOTED A SHUDDER FROM THE RT MAIN GEAR WHEN BRAKE PRESSURE WAS APPLIED . THEY TESTED THE ANTI-SKID SYSTEM, WHICH CAUSED THE RT BRAKE TO RELEASE WITH PRESSURE STILL APPLIED. MAINTENANCE PERSONNEL REPLACED THE LT AND RT MAIN GEAR BRAKE ASSEMBLIES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19950929008761995092900876SW 1995 9 29 MALA954628 119950908A77142719157003 RPM IND SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1526863 AC650B FLT NR 3241 - AFTER TAKEOFF FROM MSP, THE LEFT ENGINE RPM INDICATION ROSE TO 103 PERCENT. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT RPM INDICATOR GAUGE. (M) 1L72 4T A8SW 19950929008771995092900877SW 1995 9 29 MALA954629 119950909A2435230790001 STARTER SWRNGNSA227 SA227AC 8780603SW RT ENGINE FAILED A MALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 GL1526863 AC650B FLT NR 3208 - AFTER TAKEOFF FROM MSP, THE RT GENERATOR FELL OFF LINE. WHILE ATTEMPTING TO BRING THE RT GENERATOR ON LINE, THE LEFT GENERATOR FELL OFF LINE. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT GENERATOR AND GCU. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950929008781995092900878SW 1995 9 29 MALA954630 119950910A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL152693C AC659B FLT NR 3017 - DURING APPROACH TO DTW, THE RT MLG IN TRANSIT LIGHT DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. MAINTENANCE PERSONNEL CLEANED THE RT MAIN GEAR INDICATION MICROSWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19950929008791995092900879NM 1995 9 29 USAA950607 119950614A3230 RETRACT MECH BOEING757 757225 1384959NM LANDING GEAR MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19609AU 22205 LAX - FLT NR 0527 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE CAPTAIN DECIDED TO RETURN TO LAX. MAINTENANCE ADJUSTED THE 'NOSE GEAR NOT COMPRESSED' SENSORS. GEAR RETRACTION AND INDICATION TEST GOOD. SERVICED NOSE STRUT. REPLACED THE RIGHT TRACK POSITIONER ACTUATOR. GEAR RETRACTION TEST PERFORMED GOOD. (M) 2L72 4F RTA2NM 19950929008801995092900880WP 1995 9 29 USAA950874 119950622A5320 CLIP DOUG DC9 DC931 3022065WP BS 945 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 3 INCH CRACK AT STATION 945 SKIN CLIP AT LONGERON 45L AND 16. REPLACED SECTION OF SKIN CLIP PER SRM 51-10-04. (M) 2L72 4F A6WE 19950929008811995092900881WP 1995 9 29 USAA950875 119950622A5320 CLIP DOUG DC9 DC931 3022065WP BS 995 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN STATION 945 SKIN CLIPS BETWEEN LONGERON 14R AND 15R AND BETWEEN 15R AND 16R. REPLACED SECTION OF SKIN CLIPS PER SRM 51-10-04. (M) 2L72 4F A6WE 19950929008821995092900882WP 1995 9 29 USAA950876 119950623A5330 SKIN DOUG DC9 DC931 3022065WP BS 985 PUNCTURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND .25 INCH SKIN PUNCTURE STATION 985 AT LONGERON 17 R. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 12B. (M) 2L72 4F A6WE 19950929008831995092900883WP 1995 9 29 USAA950877 119950622A5330 SKIN DOUG DC9 DC931 3022065WP BS 996 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 6 INCHES BY 8 INCHES TEMPORARY REPAIR STATION 996 AT LONGERON 17R IN SKIN. REMOVED TEMPORARY REPAIR. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 17. (M) 2L72 4F A6WE 19950929008841995092900884WP 1995 9 29 USAA950878 119950623A53479957855 TRACK DOUG DC9 DC931 3022065WP BS 110-140 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 2 INCH WEAR IN PILOTS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK STATION 110-140. INSTALLED DOUBLERS PER DOUGLAS DRAWING 9957855. (M) 2L72 4F A6WE 19950929008851995092900885WP 1995 9 29 USAA950879 119950623A53479957855 TRACK DOUG DC9 DC931 3022065WP BS 110-140 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 20 INCH BY 20 INCH FIRST OFFICERS FORWARD AND AFT INBOARD AND OUTBOARD SEAT TRACK WORN STATION 110-140. INSTALLED DOUBLER REPAIRS PER DOUGLAS DRAWING 995-7855. (M) 2L72 4F A6WE 19950929008861995092900886WP 1995 9 29 USAA950880 119950622A5531 RIB DOUG DC9 DC931 3022065WP VERT STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURNIG Q-3/CX-2 INSPECTION, FOUND 1 INCH CRACK AT VERTICAL STABILIZER LEADING EDGE LOWER RT RIB. INSTALLED DOUBLER REPAIR PER SRM 52-01. (M) 2L72 4F A6WE 19950929008871995092900887WP 1995 9 29 USAA950881 119950622A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1076 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME AT STATION 1076 LONGERON 20R. INSTALLED SPLICE REPAIR PER SRM 53-03 FIG 26 - 3 SPLICE. (M) 2L72 4F A6WE 19950929008881995092900888WP 1995 9 29 USAA950882 119950622A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1059 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH BY 2 INCH CHAFE IN BELTFRAME STATION 1059 AT LONGERON 22R. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 26. (M) 2L72 4F A6WE 19950929008891995092900889WP 1995 9 29 USAA950883 119950710A5530591118835 ANGLE DOUG DC9 DC931 3022065WP BS 1076 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 2 INCH CRACKS IN ATTACH ANGLES INNER VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLES LEFT AND RT AT STATION 1076. REPAIRED ATTACH ANGLES PER SRM 53-05 FIG 90 AND USAIR EO 5388X223. (M) 2L72 4F A6WE 19950929008901995092900890WP 1995 9 29 USAA950884 119950710A5320 CLIPS DOUG DC9 DC931 3022065WP BS 637/658 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND TWO 3 INCH CRACKS IN SKIN CLIPS AT STATION 637 LONGERON 26L AND STATION 658 LONGERON 25L. INSTALLED ANGLE DOUBLERS PER SRM 53-03 PAGE 51. (M) 2L72 4F A6WE 19950929008911995092900891NM 1995 9 29 USAA950909 119950730A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US18051 23886 CLT - DURING 'MQ-4' VISUAL CHECK, INSPECTION FOUND A 2 INCH BY 2 INCH CORRODED AREA ON FLOOR BEAM, LOCATED AT BS 312, BETWEEN BL 38LT AND BL 38RT. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED NEW 'T' CAP AND REPAIR ANGLES, STRAPS AND FILTERS REPAIRED BY TRM 53-10-03 AND SRM 51-70-13. (M) 2L72 4F RTA16WE 19950929008921995092900892NM 1995 9 29 USAA950944 119950815A5347 FLOOR TRACK BOEING737 737301 1384611NM BS 737-797 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19342US26115 23511 INT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AND .5 BY 1 INCH CORROSION AT NUT PLATE BS 737 TO BS 797. FABRICATED NEW FLOOR TRACK AND INSTALLED, REPAIRED PER SRM 53-00-53. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008931995092900893NM 1995 9 29 USAA950945 119950809A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19342US26115 23511 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT STATION 986 BL ZERO TO LBL 20 INCHES ON FLOOR BEAM. INSTALLED REPAIR DOUBLERS, REPAIRED PER TR 53-10-01A. (M) 2L72 4F RTA16WE 19950929008941995092900894NM 1995 9 29 USAA950946 119950830A5320 ANGLE BOEING737 737301 1384611NM BS 294.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19342US26115 23511 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH CORRODED AREA BS 294.5 ON Z ANGLE. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008951995092900895NM 1995 9 29 USAA950947 119950829A5320 ANGLE BOEING737 737301 1384611NM BS 857-787 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19342US26115 23511 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 25 INCH CORROSION AT BS 857 TO BS 787 ON FLOOR SUPPORT ANGLE. INSTALLED NEW SUPPORT ANGLE SECTION INCLUDING DOUBLER AND FILLER. ALSO, COMPLETED JOGGLE MOD AT STATION 852 SRM 53-00-53 FIG 202. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008961995092900896NM 1995 9 29 USAA950948 119950830A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 13 INCH CORROSION BS 312 RBL 7 INCHES THROUGH RBL 20 INCHES ON FLOOR BEAM T-CAP. REPAIRED PER SRM 737-400 53-10-51 FIG 206 PAGE 224. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008971995092900897NM 1995 9 29 USAA950949 119950830A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 14 INCH CORRODED BS 328 RBL 28-42 ON FLOOR BEAM. SPLICED IN NEW SECTION OF T-CAP. REPAIRED 737-300/400 TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008981995092900898NM 1995 9 29 USAA950950 119950807A53206545834611 INTERCOSTAL BOEING737 737401 1384701NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 26 INCH BY .5 INCH CORROSION AT BS 328-344 RBL 12 INCHES ON INTERCOSTAL. REPAIRED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-02 PG 16. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929008991995092900899NM 1995 9 29 USAA950951 119950830A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 40 INCHES STATION 344 LBL 24 INCHES - RBL 24 INCHES. REPLACED SECTION OF T-CAP. REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009001995092900900NM 1995 9 29 USAA950953 119950808A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US1926619266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE CORRODED SPOTS (.5 INCH BY 2 INCHES EACH) BS 967, RBL 19, RBL 31, RBL 43 ON FLOOR BEAM. CUT OUT CORRODED SECTIONS ON AFT SIDE OF UPPER T-CAP, AND INSTALLED REPAIR ANGLES AND FILLERS. REPAIRED PER SRM 53-30-51 FIG 202. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009011995092900901NM 1995 9 29 USAA950954 119950804A53206545834256 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND FOUR .5 INCH BY 1 INCH CORRODED SPOTS BS 312 TO BS 328, RBL 12 CABIN FLOOR INTERCOSTAL. REPLACED WITH NEW PART, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009021995092900902NM 1995 9 29 USAA950955 119950804A53206545834255 INTERCOSTAL BOEING737 737401 1384701NM BS 294.5-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH BY 1 INCH CORRODED SPOTS BS 294.5 TO BS 312, RBL 12 CABIN FLOOR INTERCOSTAL. INSTALLED NEW PART, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009031995092900903NM 1995 9 29 USAA950956 119950811A53206546812169 INTERCOSTAL BOEING737 737401 1384701NM BS 967-987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 16 BS 967 TO BS 987 ON INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009041995092900904NM 1995 9 29 USAA950957 119950810A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 986.5 RBL 18 TO LBL 50. CUT OFF UPPER FLANGE AND INSTALLED NEW T-CAP. CORROSION TASK NR C53-107-02, CORROSION LEVEL. (M) 2L72 4F RTA16WE 19950929009051995092900905NM 1995 9 29 USAA950958 119950810A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, BS 947 LBL 4 TO RBL 4. CUT OFF UPPER FLANGE INSTALLED NEW T-CAP. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009061995092900906NM 1995 9 29 USAA950959 119950810A532065C807351 ANGLE BOEING737 737401 1384701NM SERVICE DR SILL CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOTS OF CORROSION Z-ANGLE AT RIGHT AFT SERVICE DOOR SILL. REPAIRED PER SRM 51-10-2. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19950929009071995092900907NM 1995 9 29 USAA950960 119950810A53206552878533 ANGLE BOEING737 737401 1384701NM ENTRY DR SILL CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH SPOT OF CORROSION Z-ANGLE AT LEFT AFT ENTRY DOOR SILL. REPAIRED PER SRM 53-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009081995092900908NM 1995 9 29 USAA950961 119950810A53206546812170 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER SPOT OF CORROSION RBL 17 BS 947-BS 967. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009091995092900909NM 1995 9 29 USAA950962 119950810A53206546812169 INTERCOSTAL BOEING737 737401 1384701NM BS 967-987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19420US19266 23987 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION, RBL 16 BS 967 TO 987 INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19950929009101995092900910WP 1995 9 29 95ZZZM497 119950826A211071130625 CONNECTOR DOUG DC8 DC862 3021970WP NR 2 TURBO COMPRLOOSE A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19802BN 45909 AFTER DEPARTING MIA, CREW WAS UNABLE TO PRESSURIZE ABOVE 3.2 PSI DIFF WITH 4 T/C'S OPERATING. AIRCRAFT RETURNED TO MIAMI. FOUND NR 2 T/C DISCHARGE DUCT CONNECTOR SEPARATED. REMOVED AND REPLACED SEALS AT CONNECTOR AND RESECURED CONNECTOR. OPS CHECK NORMAL ON PRESSURIZATION CHECK. (M) 2L74 4F 4A25 19950929009111995092900911WP 1995 9 29 95ZZZM498 119950831A5330 SKIN DOUG DC8 DC863F 302198FWP FS 500-520 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19441J 45988 DURING PREFLIGHT, FOUND EVIDENCE OF CORROSION BETWEEN FS 500 AND FS 520 BETWEEN L-28R AND L-29R. OPEN UP SKIN, CUT OUT AREA OF CORROSION AND FABRICATE REPAIR DOUBLER AND FINGER DOUBLERS AS PER DWG NR 30942-14. INSTALLED DOUBLERS AND FILLERS AS PER DWG NR ARW 30942-14. (M) 2L74 4F 4A25 19950929009121995092900912WP 1995 9 29 95ZZZM499 119950831A282211230311 PUMP DOUG DC8 DC871 302199AWP NR 4 MAIN TANK FAILED A ARRXAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 WP158087U PE3126K 45977 FLT NR 016 - KPHX-KTUS - ON TAKEOFF ROLL, ALL THREE PHASES OF THE NR 4 FUEL FEED PUMP OPENED. ON CLIMB-OUT NR 4 ENGINE FLAMED OUT. ONCE ATTAINED STABLE FLIGHT, NR 4 ENGINE WAS RESTARTED. MAINTENANCE REMOVED AND REPLACED THE NR 4 FUEL FEED PUMP. AN OPERATIONAL CHECK OF THE FUEL FEED SYSTEM AND NR 4 ENGINE GROUND RUN WAS GOOD. (M) 2L74 4F 4A25 19950929009131995092900913WP 1995 9 29 95ZZZM500 119950828A3241 CONTROL BOX DOUG DC8 DC873F 302199FWP ANTI-SKID SYS LOOSE A RRXAO OTHER O OTHER LDLANDING 1 WP15870TV 46086 FLT EWW262 - KMIA-KFLL - ON LANDING ROLL OUT AT KFLL, THE BRAKES FADE WITH ANTI-SKID ON. MAINTENANCE RESECURED THE ANTI-SKID CONTROL BOX. TESTED THE ANTI-SKID SYSTEM PER MM CHAPTER 32-43-0. NO DEFECTS WERE NOTED. (M) 2L74 4F RT4A25 19950929009141995092900914WP 1995 9 29 95ZZZM501 119950825A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 980 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO19427FB5995719140 45684 DURING C-CHECK, MAINTENANCE FOUND CORROSION ON THE FUSELAGE EXTERIOR SKIN RIGHT SIDE AT STATION 980, AROUND THE CABIN WINDOW IN THE LINE OF WINDOW ATTACHMENT FASTENERS. REMOVED ALL CORROSION AND BLENDED TO A 63 MICRO-INCH FINISH AND INSTALLED A .160 7075-T6 REPAIR DOUBLER IAW EO 9506242. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19950929009151995092900915WP 1995 9 29 95ZZZM502 119950825A5330 SKIN DOUG DC8 DC8F54 3021926WP FUSELAGE CRACKED A FXLAK NONE O OTHER ININSP/MAINT 1 SO19427FB5995719140 45684 DURING C-CHECK, MAINTENANCE FOUND A 1.25 INCH CRACK ON OUTER SKIN OF RIGHT AFT SERVICE DOOR AT FUSELAGE TOP AFT CORNER. CUT OUT CRACKED OUTER SKIN, INSTALLED A REPAIR DOUBLER AND TRIPLER IAW DOUGLAS DRAWING NR SRO 8530021. (M) 2L74 4F 4A25 19950929009161995092900916NM 1995 9 29 95ZZZM503 119950720A801135057165 STARTER BOEING737 7373M8 1384615NM NR 1 ENGINE FAILED A MRKAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AL03681MA 24376 RETURNED TO GATE, NR 1 ENGINE WOULD NOT ROTATE. REPLACED NR 1 STARTER DUE TO SHEARED SHAFT. ENGINE STARTS NORMALLY, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19950929009171995092900917NM 1995 9 29 95ZZZM504 119950820A801232896302 START VALVE BOEING737 7372X6C 1384552NM NR 2 ENGINE FAILED A MRKAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AL03673MA 23124 NR 2 ENGINE START VALVE WOULD NOT ENGAGE, RETURNED TO GATE. DMI START VALVE AND MANUAL START IN MDW AND MSP. 2L72 4F RTA16WE 19950929009181995092900918WP 1995 9 29 95ZZZM505 119950819A2120325628505 CLAMP DOUG DC8 DC861 3021952WP RAM AIR DUCT BROKEN A FXLAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 SO1927UA 45942 AFTER TAKEOFF MIA, EXPERIENCED LOUD NOISE AND VIBRATION IN NOSE LANDING GEAR AREA. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE CONDENSER RAM AIR DUCT DISCONNECTED DUE TO A BROKEN CLAMP. RE-INSTALLED DUCT, REPLACED CLAMP, PERFORMED OVERWEIGHT INSPECTION AND RETURNED AIRCRAFT TO SERVICE. (M) 2L74 4F 4A25 19950929009191995092900919WP 1995 9 29 95ZZZM506 119950902A32301523042109 PIN 1504964 LKHEED1011 10113851 5265010WP LT MLG ACT CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA21943 408TDA 193A1012 WHILE PERFORMING ROUTINE MAINTENANCE, MECHANIC FOUND LEFT MLG RETRACT ACTUATOR PIN CRACKED AT AFT HOUSING. MLG PIN WAS REMOVED AND REPLACED IAW 32-11-27. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A23WE 19950929009201995092900920NM 1995 9 29 AALA951541 119950825A5315141T5114 FLOOR BEAM BOEING767 767223 1385123NM CABIN CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - FLOOR BEAM IN CABIN CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301.5 HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB 767-990. (M) 2L72 4F RTA1NM 19950929009211995092900921NM 1995 9 29 AALA951542 119950825A5313140T0115 STRINGER BOEING767 767223 1385123NM BS 417 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - FOUND STRINGER 37L CORRODED BETWEEN STATION 399 AND 434. DAMAGE IS WITHIN 20 INCHES OF A STRINGER SPLICE. REPAIRED PER SRM 53-00-03-2 FIG 202. APPROVED BY ENGINEERING PER MRB 767-996. (M) 2L72 4F RTA1NM 19950929009221995092900922EU 1995 9 29 AWXA9500567 119950318A5230D5237119000000 HANDLE CASTING AIRBUS320 A320231 3930325EU FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO DOOR HANDLE MOUNTING CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-72-11. (M) 2L72 4F RTA28NM 19950929009231995092900923EU 1995 9 29 AWXA9500568 119950318A5330 SKIN AIRBUS320 A320231 3930325EU FRAME 60-61 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN DAMAGED BETWEEN FRAME 60 AND FRAME 61, INBOARD OF STRINGER 43 RT. FABRICATED FILLER/DOUBLER REPAIR PER SRM 53-00-11. (M) 2L72 4F RTA28NM 19950929009241995092900924EU 1995 9 29 AWXA9500570 119950328A5320 RAIL AIRBUS320 A320231 3930325EU BS 254 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 254 BETWEEN FRAME 16 AND FRAME 18 CORRODED AT SCREW HOLES. REPAIRED PER SRM 53-11-14. (M) 2L72 4F RTA28NM 19950929009251995092900925EU 1995 9 29 AWXA9500571 119950328A5320 RAIL AIRBUS320 A320231 3930325EU BS 1292 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28627AW 66 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL MINUS 1292 BETWEEN FRAME 16 AND FRAME 20 CORRODED. FABRICATED AND INSTALLED RAIL PER SRM 51-42-11. (M) 2L72 4F RTA28NM 19950929009261995092900926EU 1995 9 29 AWXA9500587 119950318A5320 RAIL AIRBUS320 A320231 3930325EU FR 16 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 1292 BETWEEN FRAME 16 AND FRAME 20 CORRODED. REPAIRED PER SRM 51-72-11. (M) 2L72 4F RTA28NM 19950929009271995092900927EU 1995 9 29 AWXA9500588 119950318A5347 SEAT TRACK AIRBUS320 A320231 3930325EU FR 20 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK ON RAIL AT MINUS 1292 BETWEEN FRAME 20 AND FRAME 21 CORRODED. REPAIRED PER SRM 51-72-11. (M) 2L72 4F RTA28NM 19950929009281995092900928EU 1995 9 29 AWXA9500589 119950318A5347 SEAT TRACK AIRBUS320 A320231 3930325EU BS 265 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK ON RAIL AT 265 BETWEEN FRAME 20 AND FRAME 21 CORRODED. REPAIRED PER SRM 51-72-11. (M) 2L72 4F RTA28NM 19950929009291995092900929EU 1995 9 29 AWXA9500590 119950318A5320 RAIL AIRBUS320 A320231 3930325EU FR 20 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28628AW 67 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL AT MINUS 254 FRAME 20 CORRODED. REPAIRED PER SRM 53-11-14. (M) 2L72 4F RTA28NM 19950929009301995092900930EU 1995 9 29 AWXA9500594 119950830A3350321452 EEL POWER SUPPLY AIRBUS320 A320231 3930325EU CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW 091 PHX - DURING ROUTINE MAINTENANCE CHECK, LEFT MID CABIN EMERGENCY EXIT LIGHT POWER SUPPLY FAILED TEST. REMOVED AND REPLACED LEFT MID CABIN POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19950929009311995092900931SW 1995 9 29 BDHA9500018 119950824A6120 PROP GOVERNOR SWRNGNSA226 SA226TC 8780404SW RT ENGINE OUT OF ADJUST A BDHAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL15229AM TC305 MSP - FLT 447 - RIGHT ENGINE WAS SURGING WHEN SET TO TAKEOFF POWER. AIRCRAFT RETURNED TO HANGER AND MAINTENANCE ADJUSTED THE PROP GOVERNOR LOW SETTING. RUN UP TEST WAS SATISFACTORY, AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19950929009321995092900932WP 1995 9 29 BUFA9718 119950830A2422 WIRE DOUG DC8 DC861 3021952WP STATIC INVERTER FAILED A BUFAA UNSCHED LANDING O OTHER CLCLIMB 1 CE05161DB 45980 FLT GAC801 - MIA-CCS - STANDBY HORIZON TUMBLING 90 DEGREES NOSE UP 25 DEGREES BANK DURING INITIAL AND NORMAL CLIMB AFTER TAKEOFF, RETURNED TO MIA. REPAIRED WIRING AT PIN C OF STATIC INVERTER, SYSTEM OPS CHECK GOOD IAW DMM 34-28-0. (M) 2L74 4F 4A25 19950929009331995092900933WP 1995 9 29 BUFA9719 119950901A79215294332 OIL COOLER PWA 5294332 DOUG DC8 DC861 3021952WP NR 4 ENGINE LEAKING A BUFAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS NRNOT REPORTED 1 CE05915BV 597D 45981 FLT 0X0401 - MIA-POS - SHUT DOWN NR 4 ENGINE IN FLIGHT DUE TO LOW OIL PRESSURE AND LOW OIL QUANTITY. NO EMERGENCY DECLARED. REMOVED AND REPLACED NR 4 ENGINE FUEL HEAT OIL COOLER. RUN ENGINE, OPS CHECK GOOD. LEAK CHECK GOOD IAW MM 72-00. (M) 2L74 4F 4A25 19950929009341995092900934WP 1995 9 29 BUFA9720 119950904A79215294332 OIL COOLER PWA 5294332 DOUG DC8 DC861 3021952WP NR 4 ENGINE LEAKING A BUFAO OTHER JK WARNING INDICATION FLUID LOSS NRNOT REPORTED 1 CE05915BV 90157 45981 FLT 0X0701 - TPP-GAS - NR 4 ENGINE HAD LOSS OF OIL PRESSURE AND QUANTITY, WIND MILL OK PRESSURE WAS 20 PSI. REMOVED AND REPLACED NR 4 ENGINE HEAT OIL COOLER. RUN ENGINE, OPS CHECK GOOD. LEAK CHECK GOOD IAW MM72-00. (M) 2L74 4F 4A25 19950929009351995092900935WP 1995 9 29 HALA95117 119950821A5311 FRAME DOUG DC9 DC951 3022051WP BS 1305 CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13601AP 47658 SBA - AN .5 INCH BY .5 INCH AREA OF EXFOLIATION EXISTS ON FRAME FLANGE AT STATION 1305 STRINGER 14R. REMOVED CORROSION PER SRM 51-10-3. MATERIAL LOSS OUT OF LIMITS PER SRM 53-01 FIG 1. FABRICATED ANGLES AND FILLER PER SRM 53-01 FIG 2, ALODINED, PRIMED AND INSTALLED PER 53-01. (M) 2L72 4F A6WE 19950929009361995092900936NM 1995 9 29 IXKA9500026 119950906A2197 WIRE BOEING727 727230 1384080NM RT PACK BROKEN A IXKAA UNSCHED LANDING O OTHER CLCLIMB 1 EA25357KP 20675 FLT NR 31 - EWR-MDW - AFTER TAKEOFF, COULD NOT MAINTAIN CABIN PRESSURE, RT PACK INOP. AIRCRAFT RETURNED TO EWR. FOUND NR 3 ENGINE 13TH STAGE MOD VALVE NOT OPENING WHEN RT PACK TURNED ON. REMOVED AND REPLACED 13TH STAGE MOD VALVE PER MM 36-12-42. NO HELP. FURTHER TROUBLE SHOOTING FOUND BROKEN WIRE ON RT PACK SWITCH. REPAIRED WIRE AND OPS CHECK OK AS PER MM 21-31-0. (M) 2L73 4F A3WE 19950929009371995092900937WP 1995 9 29 IXXA199573 119950816A275237741721 ACT FLAP CRANK DOUG DC8 DC863 302198AWP RT TE FLAP BROKEN A AIXXAA UNSCHED LANDING O OTHER CLCLIMB 1 GL23788AL 45999 DURING NORMAL FLAP RETRACTION ON DEPARTURE OUT OF BDL, THE RIGHT HAND FLAP APPEARED TO STICK AT 18 DEGREES WITH THE AIRCRAFT TENDING TO ROLL TO THE LEFT AT A LOWER FLAP SETTING. FLAP ASYMMETRY WOULD APPEAR AGAIN ABOVE FLAPS 25. THE AIRCRAFT RETURNED TO BDL FOR MAINTENANCE. INSPECTION ON THE GROUND REVEALED A BROKEN FLAP CRANK ASSEMBLY (P/N 37741721) ON THE RT INBOARD ACTUATOR. THE CRANK ASSEMBLY AND FLAP ACTUATOR WERE REPLACED. (M) 2L74 4F 4A25 19950929009381995092900938NE 1995 9 29 IXXA199574 219950823A7200 ENGINE DOUG DC8 DC871 302199AWP GE CFM56 CFM56* 13802NE NR 1 FLAMED OUT A IXXAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL23820BX 46065 692334 ON DESCENT INTO TOL, NR 1 ENGINE FLAMED OUT AT 31,000 FEET WHEN THE THROTTLE WAS RETARDED. THE ENGINE RE-LIT AND OPERATED NORMALLY AFTER COMPLETION OF POWER LOSS CHECKLIST. INSPECTION ON THE GROUND IN TOL IDENTIFIED NO DEFECTS. THE FUEL FILTER WAS CHECKED AND FOUND TO BE SERVICEABLE. IT WAS REPLACED AS A PRECAUTION. THE ENGINE WAS RUN AND FOUND TO OPERATE NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F4 F 4A25 E2GL 19950929009391995092900939NM 1995 9 29 MRKA9559 119950828A3350862101401 EEL BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 EMERGENCY LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 19950929009401995092900940NM 1995 9 29 MRKA9560 119950828A3350862101401 EEL BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 EMERGENCY LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 19950929009411995092900941NM 1995 9 29 MRKA9565 119950828A335001617844 EEL BATT CHARGER BOEING737 7372X6C 1384552NM RT OVERWING INOP A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 BATTERY CHARGER INOP, WILL NOT CHARGE. REMOVED AND REPLACED BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M) 2L72 4F RTA16WE 19950929009421995092900942 1995 9 29 ORJA9554 419950808A2565D29984103 ESCAPE SLIDE DOUG DC9 DC983 3022083WP TAILCONE MALFUNCTIONED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11832RA 53044 TAILCONE WAS ACCIDENTALLY DEPLOYED. SLIDE DEPLOYED NORMALLY, HOWEVER, IT DID NOT INFLATE. SLIDE WAS REPLACED, TAILCONE REPAIRED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19950929009431995092900943WP 1995 9 29 ORJA9573 119950811A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC987 3022087WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11752RA 49780 EMERGENCY LIGHTING TRACK FLOOR LAMPS WILL NOT ILLUMINATE AT ROW 3 AND ROW 25. RELAMPED BOTH. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 19950929009441995092900944WP 1995 9 29 ORJA9574 119950819A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 RNO - POST FLIGHT CHECK SHOWED SEVERAL EMERGENCY FLOOR LIGHTS INOP. REPAIRED BROKEN WIRE ON EMERGENCY PATH LIGHTING SYSTEM, OPS NORMAL. (M) 2L72 4F RTA6WE 19950929009451995092900945EU 1995 9 29 PLGA81795G1 119950926A2910 HYD LINE SAAB SF340 SF340A 7850100EU LT ENGINE FAILED A PLGAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. JA WARNING INDICATION FLAME/FIRE TXTAXI/GRND HDL 1 NE05742BA 340A092 PHL - FLT NR 4426 - DURING TAXI, THE FLIGHT CREW EXPERIENCED A LEFT TAIL PIPE HOT LIGHT FOLLOWED BY A LEFT BLEED LEAK LIGHT. THE LEFT BLEED WAS OPEN IN AUTO AND CROSSOVER BLEED VALVE WAS OPEN. FLAMES WERE CONFIRMED AT WHICH POINT BOTH ENGINE WERE SECURED. THE FIRE BOTTLE DISCHARGED AND THE AIRCRAFT EVACUATED. INVESTIGATION FOUND DAMAGE WHICH WAS CONSISTENT WITH FIRE INVOLVING M/L 5606 HYDRAULIC FLUID FROM A FAILED HYDRAULIC LINE. (M) 2L72 4T RTA52EU 19950929009461995092900946EA 1995 9 29 PLGA827951G 119950827A3260750122001 SWITCH PHOENIX 1143800415 BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA RT MLG INTERMITTENT A PLGAO OTHER N FALSE WARNING APAPPROACH 1 NE05817BE3508 3508 159 UB52 LGA- FLT NR 4732 ON APPROACH THE RT MLG DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. DURING ABNORMAL CHECKLIST PROCEDURES THE DOWN AND LOCKED LIGHT ILLUMINATED. THE AIRCRAFT LANDED IN LGA WITHOUT INCIDENT. THE AIRCRAFT WAS THEN INSPECTED AND DETERMINDED TO BE SAFE FOR FERRY FLIGHT TO ALB. ALB MAINTENANCE REMOVED AND REPLACED THE RT MLG ACTUATOR AS THE GEAR LIGHT SWITCH WAS DETERMINED TO BE INTERMITTENT. (M) 2L72 4T4 TRTA24CE E4EA 19950929009471995092900947EU 1995 9 29 PLGA94951G 119950904A5270725220017 SHOOT-BOLT SAAB SF340 SF340A 7850100EU CREW HATCH WORN A PLGAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NE05345BE 340A108 FLT NR 4471 - TAKEOFF FROM BOS, THE CREW HATCH WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. TROUBLE SHOOTING FOUND THE SHOOT-BOLT WORN AT THE MICRO-SWITCH ACTUATING POINT. MAINTENANCE REPLACED THE SHOOT-BOLT AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA52EU 19950929009481995092900948EU 1995 9 29 REXA95048 119950807A33205104WW LIGHT BULB SAAB SF340 340B 7860101EU CABIN FAILED A REXAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO25365PX 340B265 WINDOW LIGHTS 8C NEON LIGHT STRIP SHORT CIRCUITED. AREA AROUND PLUG IN LOOKS BURNED. DEFERRED IAW MEL 33-20-1 AUTHORIZATION NR 10029. (M) 2L72 4T RTA52EU 19950929009491995092900949EU 1995 9 29 REXA95053 119950821A2700 CONTROL WHEEL BAG JETSTMJETSTM3101 1500215EU COCKPIT STUCK A AREXAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 SO25304PX 663 LANDING AT GTR, CONTROL WHEEL GOT STUCK AND HAD TO FORCE FOR OUT GO-AROUND TO UNSTICK IT. IN PATTERN AT GTR CONTROL WHEEL HARD TO MOVE LEFT, RIGHT, FORWARD AND BACK. REF AML'S 344376, 344377, 344380, 344381, 344383 AND 344383 FOR INSPECTION OF AIRCRAFT AND DISCREPANCIES FOUND AND CORRECTED. NO DISCREPANCIES FOUND THAT WOULD JUSTIFY THIS PROBLEM. NO DISCREPANCY WAS NOTED ON THE FERRY FLIGHT FROM GTR TO MEMPHIS. AIRCRAFT WAS RELEASED FOR A TEST FLIGHT WHICH WAS SATISFACTORY. (M) 2L72 4T RTA21EU 19950929009501995092900950EU 1995 9 29 SIMA952391 119950827A33503011210 EEL AEROSPATR72 ATR72212 EU PAX DOOR INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT2258 458 419 263 ORD - FLT NR 4127 - PASSENGER DOOR STAIR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY AND REPAIRED CANNON PLUG AT TOP OF STAIRS. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950929009511995092900951EU 1995 9 29 SIMA952392 119950827A3246L45449 BEARING TIMKEN L45449 AEROSPATR42 ATR42300 8680920EU NLG SEIZED A SIMAO OTHER O OTHER TXTAXI/GRND HDL 1 SW21424MQ145046731 045 ORD - FLT 4016 - UPON ARRIVAL IN ORD, NR 1 NOSE TIRE WAS FOUND TO BE FLAT. DURING TIRE ASSY REMOVAL, INNER BEARING WAS SEIZED AND OVERHEATED ON THE AXLE. MAINTENANCE REPLACED THE NOSE GEAR (P/N 022698100). OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950929009521995092900952EU 1995 9 29 SIMA952451 119950902A2161 TEMP CONTROLLER AEROSPATR72 ATR72212 EU CABIN FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21355AT 355 FLT NR 3935 - FSM - FLIGHT ATTENDANTS REPORTED SMOKE SMELL AND HIGH PITCHED WHINE, FLIGHT DIVERTED TO FSM, RECIRC FAN TURNED OFF. CREW DECLARED EMERGENCY FOR PRIORITY HANDLING. MAINTENANCE INSPECTED AND DETERMIND FAULT WITH LEFT AUTO TEMP CONTROL SYSTEM. SYSTEM WAS DEFERRED. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2H72 4T RTA53EU 19950929009531995092900953EU 1995 9 29 SIMA952491 119950906A33503011151 EEL BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21223AT 3281 223 ORD - FLT NR 4263 - FORWARD HALF OF EMERGENCY LIGHTS STAY ON. REPLACED BATTERY PACK 10WL. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19950929009541995092900954WP 1995 9 29 USAA950885 119950710A5314 KEEL BEAM DOUG DC9 DC931 3022065WP BS 637 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND 2 INCH CRACK RT SIDE OF KEEL BEAM RIB. INSTALLED ANGLE DOUBLER REPAIRS PER SRM 53-03 FIG 12. (M) 2L72 4F A6WE 19950929009551995092900955WP 1995 9 29 USAA950886 119950622A5312 BLKHD PANEL DOUG DC9 DC931 3022065WP BS 995 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND STATION 965 BULKHEAD LOWER PORTION 1 INCH CRACK IN PANEL. CUT OUT DAMAGED AREA AND FABRICATED NEW PANEL AND INSTALLED PER SRM 53-03 FIG 19. (M) 2L72 4F A6WE 19950929009561995092900956WP 1995 9 29 USAA950887 119950621A5330 SKIN DOUG DC9 DC931 3022065WP BS 813 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFED .014 INCH DEEP 5 INCHES BY 1 INCH STATION 813 AT LONGERON 26R UNDER FILLET PANEL. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 37. (M) 2L72 4F A6WE 19950929009571995092900957WP 1995 9 29 USAA950888 119950621A5330 SKIN DOUG DC9 DC931 3022065WP BS 813 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND SKIN CHAFE .014 BY .018 INCH DEEP 5 INCHES BY 1 INCH AT STATION 813 AND LONGERON 26L UNDER FILLET PANEL. INSTALLED DOUBLERS PER SRM 53-04 FIG 37. (M) 2L72 4F A6WE 19950929009581995092900958WP 1995 9 29 USAA950889 119950621A5754 WEB DOUG DC9 DC931 3022065WP RT LE FLAP CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND .75 INCH CRACK IN WEB OF RHS FLAP AT XFS341. INSTALLED .090 INCH FILLER AND .063 INCH 7075T6 DOUBLER PER SRM 57-01 AND USAIR EA 30788. (M) 2L72 4F A6WE 19950929009591995092900959WP 1995 9 29 USAA950890 119950622A5330 SKIN DOUG DC9 DC931 3022065WP BS 996 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND DENT IN FUSELAGE SKIN 3 INCHES BY 2.5 INCHES BY .187 INCH DEEP AT STATION 996 LONG 18R. INSTALLED .032 INCH TITANIUM DOUBLER PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19950929009601995092900960WP 1995 9 29 USAA950891 119950621A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 180-200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 20 INCHES BY 20 INCHES STATION 180-200, FROM RT SIDE WALL SUB FLOOR BEAM. CLEANED CORROSION AND SPLICED IN FILLER AND DOUBLER PER SRM 51-10-2. (M) 2L72 4F A6WE 19950929009611995092900961WP 1995 9 29 USAA950892 119950622A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 2 INCH BY 2 INCH STATION 980 LEFT LAV INBOARD SCREW HOLE IN FLOOR BEAM. CUT OUT DAMAGED AREA AND INSTALLED FILLERS AND DOUBLER PER SRM 53-10-19. (M) 2L72 4F A6WE 19950929009621995092900962WP 1995 9 29 USAA950893 119950710A5311 FRAME DOUG DC9 DC931 3022065WP BS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND LEVEL 2 CORROSION AT BELTFRAME 20 INCHES BY 2 INCHES BETWEEN LONGERON 27L AND 27R AT STATION 980 (CORROSION TASK REF C51-53300). CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER SRM 53-03 PG 4A FIG 2A. (M) 2L72 4F A6WE 19950929009631995092900963WP 1995 9 29 USAA950894 119950622A5311 FRAME DOUG DC9 DC931 3022065WP BS 980 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19982VJ33241 48158 PIT - DURING Q-3/CX-2 INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH RIGHT LAV STATION 980 FLOOR BEAM AROUND SCREW HOLES IN FLOOR BEAM. CUT OUT DAMAGE AND INSTALLED FILLERS AND DOUBLERS PER SRM 53-05 FIG 20D. (M) 2L72 4F A6WE 19950929009641995092900964WP 1995 9 29 USAA950900 119950817A3244 TIRE DOUG DC9 DC931 3022065WP LT MLG FAILED A USAAO OTHER O OTHER CLCLIMB 1 EA19937VJ 48117 PIT - FLT 1637 - ON TAKEOFF, THE LEFT MAIN OUTBOARD TIRE BLEW. MOST OF THE TIRE WAS INGESTED INTO THE LEFT ENGINE. ON APPROACH BACK TO PIT, THE CREW RECEIVED A GEAR UNSAFE LIGHT. THE CAPTAIN DID A MISSED APPROACH AND CYCLED THE GEAR. WITH THE UNSAFE LIGHT STILL ON, CAPTAIN DID A FLYBY OF THE TOWER TO VERIFY THAT THE GEAR WAS DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 TIRE AND WHEEL ASSEMBLY (P/N 3910063507) DUE TO A BLOWN CAP. SPIN CHECK WAS GOOD. (M) 2L72 4F A6WE 19950929009651995092900965EU 1995 9 29 USAA950914 119950823A2420X00043409 CURRENT SENSOR FOKKERF28 F28MK0100 4990807EU LT EQUIP COMPT FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19854US 11282 PIT - FLT 967 - DURING CLIMB-OUT FROM PIT, CREW RECEIVED A STALL WARNING FAULT MESSAGE. CREW WAS ADVISED TO RETURN TO FIELD FOR REPAIRS. NON EMERGENCY AND NO OTHER INCIDENTS. REPLACED VARIOUS COMPONENTS WITH NO HELP. FINAL FIX WAS REPLACEMENT OF LEFT A/C CURRENT SENSOR. RCN 53007. (M) 2L72 4F RT 19950929009661995092900966EU 1995 9 29 USAA950919 119950827A33506040681 EEL BATTERY PACK FOKKERF28 F28MK0100 4990807EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19892US 11372 CLT - FLT NR 2416 - EXTERIOR EMERGENCY LIGHTS INOP. ISOLATED TO BATTERY PACK SUPPLYING THE AFT EXTERIOR LIGHTS. PRECAUTIONARY PROCEDURE TAKEN, MEL'D SYSTEM. REPLACED BATTERY PACK. (M) 2L72 4F RT 19951006000011995100600001WP 1995 10 6 95ZZZX5357 119950331A5313 LONGERON DOUG DC9 DC932 3022066WP FS 140-160 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11940VV 47523 UPON A SCHEUDLED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, LONGERON 25L FROM FS 160.0 TO FS 140.0 WAS FOUND CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIRS IAW DC9 SRM 53-02, FIGURE 2. N/R NR 027N1/0093. 2L72 4F A6WE 19951006000021995100600002WP 1995 10 6 95ZZZX5358 119950825A5330 SKIN LKHEED1011 10113851 5265010WP FS 1565-1545 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO19305GB 193P1127 LEVEL 2 CORROSION/C-2 CARGO COMPARTMENT, FUSELAGE SKIN CORROSION AT FS 1565-FS 1545, STR 29-STR 30. REMOVED CORROSION, TREATED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 53-31-00. 2L73 4F A23WE 19951006000031995100600003NM 1995 10 6 95ZZZX5359 119950721A33501000679 EEL BOEING737 737247 138448DNM CABIN INOPERATIVE A USVAK NONE L NO TEST ININSP/MAINT 1 SO19305VA 21091 19606 DURING AMPLIFIED PRE-FLIGHT, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED UNIT, OPS CHK GOOD. 2L72 4F A16WE 19951006000041995100600004NM 1995 10 6 95ZZZX5360 119950708A3350BR96442 EEL LENSE BRUCE BR2013P BOEING737 737247 138448DNM CABIN MISSING A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 FOUND 1 OF 2 FORWARD RED LENSE FOR FLOOR TRACK EMERGENCY LIGHTS MISSING. REMOVED AND REPLACED FLOOR TRACK SOCKET LAMP, RED LENSE (SECOND FROM FRONT OF A/C LTS. CHECK GOOD). 2L72 4F A16WE 19951006000051995100600005NM 1995 10 6 95ZZZX5361 119950531A33501060021101 EEL BATTERY BOEING737 737247 138448DNM CABIN DISCHARGED A USVAK NONE L NO TEST ININSP/MAINT 1 SO19308VA 19613 BOTH EXTERNAL EMERGENCY EXIT LIGHTS INOP, LEFT SIDE OF AIRCRAFT. TROUBLESHOT TO LOW BATTERY PACK. CHARGED BATTERY IAW B737 MM 33-51-0. 2L72 4F A16WE 19951006000061995100600006CE 1995 10 6 95ZZZX5362 119950408A3213654100042 GEAR PISTON 6541000804 CESSNA500 550 2076604CE RT MLG MISMANUFACTURED A COZAK NONE O OTHER ININSP/MAINT 1 WP27116K 5214 176 5500149 DURING ROUTINE INSPECTION OF RT MLG, THE SAFETY WIRE ON THE WHEEL HEAT SHIELD WAS FOUND BROKEN. FURTHER INSPECTION FOUND THE DISTANCE BETWEEN THE WHEEL KEYWAY LINERS AND THE MAIN GEAR SCISSOR LOWER ATTACH POINT WAS VERY CLOSE AND RUBBING ON LANDING AND HIGH SPEED TAXI. A CHECK BETWEEN THE LT AND RT MLG SHOWED THE DISTANCE BETWEEN THE LINERS AND GEAR SCISSORS WAS .145 INCH ON THE RT, AND .298 INCH ON THE LT. THE GEAR PISTON BOSS AREA WHERE THE BRAKE MOUNTS WERE NOT MANUFACTURED TO THE CORRECT SPECIFICATIONS. A NEW PISTON AND AXLE ASSEMBLY WAS INSTALLED AND THERE IS NOW A CLEARANCE OF .312 INCH BETWEEN THE LINERS AND GEAR SCISSORS. THE PISTON AND AXLE ASSY WAS SENT TO CESSNA, WICHITA, KS FOR EVALUATION. 1L72 4F A22CE 19951006000071995100600007NM 1995 10 6 95ZZZX5363 119950717A2934001A29A0752000 FLOAT DORNERDO32 DO328100 2996000NM HYD RESERVOIR PUNCTURED A EQGAK NONE N FALSE WARNING ININSP/MAINT 1 SW19335LS369 3035 CAS - DURING PRE-FLIGHT, CREW REPORTED CAS MESSAGE, HYD AUXILIARY QUANTITY LOW. AIRCRAFT WAS FERRIED TO HOT MAINTENANCE BASE. MECHANIC FOUND AUXILIARY RESERVOIR FLOAT HAD A HOLE IN IT. REMOVED AND REPLACED AUXILIARY RESERVOIR FLOAT ASSEMBLY. PERFORMED OPS CHECK OF SYSTEM. ALL CHECKS NORMAL. NO LEAKS NOTED. AIRRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19951006000081995100600008NM 1995 10 6 95ZZZX5364 119950809A5610SPSD0328231 WINDOW DORNERDO32 DO328100 2996000NM LT COCKPIT SHATTERED A EQGAA UNSCHED LANDING O OTHER CRCRUISE 1 SW19335LS543 231 3035 DFW - AFTER DEPARTING, AIRCRAFT WAS IN CRUISE AT 31,000 FEET AND PILOT HEARD A LOUD NOISE. THE CAPTAIN'S OUTER PANE WINDOW HAD SHATTERED, BUT REMAINED INTACT. THE PILOT DESCENDED AND RETURNED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CAPTAIN'S WINDOW IAW THE DORNER MM, OPS CHECKS NORMAL, AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19951006000091995100600009SW 1995 10 6 95ZZZX5365 119950725A3610J416A8555 CHECK VALVE FRCHLDSA227 SA227DC 3377521SW RT ENGINE STUCK OPEN A EQGAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 SW19850LS DC850B CREW REPORTED LOW SUCTION LIGHT ON ANNUNCIATOR AND SUCTION GAUGE READ ZERO WITH RIGHT ENGINE RUNNING. AIRCRAFT WAS FERRIED TO HOT MAINTENANCE BASE. MECHANIC REMOVED AND REPLACED THE RT ENGINE CHECK VALVE. OPS CHECKED GOOD, ENGINE RUN PERFORMED, ALL CHECKS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T RTA18SW 19951006000281995100600028WP 1995 10 6 AALA951389 119950807A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07586AA 53249 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR IN AFT CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19951006000291995100600029NM 1995 10 6 AALA951393 119950808A33501703663 EEL CONTACT BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07389AA 27449 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 21H FOUND INOPERATIVE. REPLACED BROKEN CONTACT AT SEAT 21H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951006000301995100600030WP 1995 10 6 AALA951404 119950809A3350A3060719102 EEL STRIP DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0776202 53292 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 16D TO 20D FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 16D AND 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA6WE 19951006000311995100600031NM 1995 10 6 AALA951425 119950813A3350A3060720101 EEL CONDUCTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07687AA 25695 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT LAVATORY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY AFT LAVATORY. SYTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19951006000321995100600032NM 1995 10 6 AALA951426 119950814A3350A3060698101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07681AA 25338 EWR - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19951006000331995100600033NM 1995 10 6 AWXA9500553 119950816A3350 EEL WIRE BOEING737 737301 1384611NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28325AW 23260 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE AT 5ABC. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19951006000341995100600034NM 1995 10 6 P9IA95002 119950714A2560732203 DOOR CONSOLCNTRLS7322C3 BOEING727 727231 1384079NM RAFT/COMPT JAMMED A P9IAK NONE O OTHER ININSP/MAINT 1 SO037431861392 962 20051 DURING DITCHING DEMONSTRATION, FORWARD OVERHEAD RAFT COMPARTMENT DOOR JAMMED ON OPENING. FOUND INERTIA REEL JAMMED. SEVERAL TEETH BROKEN ON GEARS. (X) 2L73 4F A3WE 19951006000351995100600035EU 1995 10 6 PLGA725951G 119950725A2710 CONTROL MECH BAC 146 AVRO146RJ70A1500095EU AILERON SYSTEM DECOUPLED A PLGAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NE05833BE E1224 JFK - FLT 4838 - DURING FINAL APPROACH SEGMENT, ACFT ENCOUNTERED WAKE TURBULENCE FROM PRECEDING AIRBUS A340. ACFT ROLLED 35 DEG TO LEFT & AUTOPILOT DISCONNECTED. PILOT APPLIED CORRECTIVE INPUT AT WHICH POINT AILERONS DECOUPLED (SYS SPLIT). ROLL CORRECTED & FLT CONTINUED LANDING WITHOUT INCIDENT. MX PERFORMED ALL FUNCTIONAL & OPERATIONAL CHECKS WITH NO DEFECTS FND. ACFT RETURNED TO SERV. SDR IS TO CLOSE OUT SDR OF 7-25-95 IN WHICH WAKE TURBULANCE ENCOUNTERED CAUSING AILERON SYS TO DECOUPLE. INVEST FND NO DEFECTS WITH INTERCONNECT UNIT. TESTING PERFORMED WITH NEW UNIT & UNIT INSTALLED AT TIME OF INCIDENT, ALL WITHIN DESIGN REQUIREMENTS. ORIG INTERCONNECT STRUT REINSTALLED & ACFT RETNED TO SERV.(X) 2H74 4F RTA49EU 19951006000361995100600036NE 1995 10 6 RAIA950741 219950726A7260 CHIP LIGHT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE NR 2 ENGINE ILLUMINATED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03554HK54 41067 76082 NR 2 ENGINE CHIP LIGHT ILLUMINATED. PERFORMED INSPECTION AND REQUIREMENTS OF ENGINE MM. OBTAINED OIL SOAP SAMPLE. ACFT TT, 54.0. (X) 2L72 4T4 TRTA41NM E18NE 19951006000371995100600037EU 1995 10 6 RAIA950820 119950813A52306FS11551 HANDLE JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR NOT SECURE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03554HK185 41067 STL - FLT 7073 - CARGO DOOR LIGHT ILLUMINATED. MAINTENANCE CYCLED CARGO DOOR HANDLE. OPERATION OF SYSTEM CHECK OK. ACFT TT, 185.0. (X) 2L72 4T RTA41NM 19951006000381995100600038NE 1995 10 6 REXA95050 219950811A7210J221P035 O-RING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE CUT A REXAEA ENGINE SHUTDOWN UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 SO25369PX 340B295 CEE785373 RIGHT ENGINE OIL PRESSURE FLUCTUATION FOLLOWED BY CWP CAPTION IN-FLIGHT. FOLLOWED BY ENGINE SHUT-DOWN PROCEDURES AS CALLED FOR IN EMERGENCY CHECK LIST. FOUND BAD O-RING ON RIGHT BB AXIS SEAL. REINSTALLED O-RING ON BB AXIS SEAL. GROUND RUN CHECKS GOOD. (X) 2L72 4T4 TRTA52EU E8NE 19951006000391995100600039EU 1995 10 6 SIMA952241 119950812A2621404028 FIRE BOTTLE SAAB SF340 SF340A 7850100EU NR 1 ENGINE DISCHARGED A SIMACF ABORTED TAKEOFF ACTIVATE FIRE EXT. N FALSE WARNING TOTAKEOFF 1 SW21115SB156981551 80513EK 340A115 DFW - FL 3883 - NR 1 ENGINE FIRE WARNING DURING TAKEOFF ROLL, ABORTED TAKEOFF AND BLEW THE FIRE BOTTLE. CALLED OUT CFR, FIRE LIGHT EXTINGUISHED. FUNCTION CHECK FIRE INDICATION IAW SAAB 340 AMM 26-11-00. NO DEFECTS NOTED. GROUND RAN A/C, ENG TEMP 750, NO FIRE FAULT NOTED AND REPLACED NR 1 ENGINE FIRE BOTTLE IAW AMM 26-71-20. AIRCRAFT RETURNED FOR SERVICE. PART TOTAL CYCLES, 17,301. (X) 2L72 4T RTA52EU 19951006000401995100600040EU 1995 10 6 SIMA952292 119950817A32465010488 MAIN WHEEL ASSY SAAB SF340 340B 7860101EU LT MLG CRACKED A SIMAK NONE O OTHER TXTAXI/GRND HDL 1 SW21344SB2504 66 MAY931238 340B344 DFW - FLT 3514 - LT INBOARD WHEEL ASSY CRACKED AT BEAD. (TIRE BLOWN). FOUND AFTER AIRCRAFT LANDED AT DFW AND TAXIED TO THE GATE. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2,696. (X) 2L72 4T RTA52EU 19951006000411995100600041EU 1995 10 6 SIMA952311 119950819A33506013211 EEL POWER SUPPLY SAAB SF340 SF340A 7850100EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW2198MQ 3270 989 19169 340A098 DFW - FLT 3961 - EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS OF ILLUMINATION. MAINTENANCE REPLACED POWER SUPPLY. SYSTEM OPS CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 3,713.0. (X) 2L72 4T RTA52EU 19951006000421995100600042NM 1995 10 6 TAOA079505 119950731A3350900835A EEL BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 20441 EMERGENCY LIGHTS AT ROW 15 CEILING AND ROW 21 CEILING INOPERABLE. REPLACED BATTERY PACK FOR ROW 15 AND ROW 21 CEILING EMERGENCY LIGHTS - CKS OK. S/N ROW 15 - 11725. S/N ROW 21 - T3921. (X) 2L73 4F A3WE 19951006000431995100600043NM 1995 10 6 TAOA089501 119950801A3350900835A BATTERY PACK GRIMES BOEING727 727225 1384077NM EMERGENCY LIGHTSDISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15922TS P2793VA5440 20415 EMERGENCY LIGHTS AT CEILING OVERWING AND AT AFT OF LIFE RAFT COMPARTMENT FOUND INOPERABLE. REPLACED BATTERY PACKS FOR EMERGENCY LIGHTS - OPS CK OK. (X) 2L73 4F A3WE 19951006000441995100600044NM 1995 10 6 TAOA089502 119950806A2611 SMOKE DETECTOR BOEING727 727227 1384078NM AFT LAV DIRTY A TAOAK NONE N FALSE WARNING CRCRUISE 1 EA15924TS 21041 AFT LAV LEFT SIDE SMOKE DETECTOR CAME ON IN-FLIGHT. NO SMOKE PRESENT. CLEANED CONNECTOR AT DETECTOR - OPS CHECKED NORMAL PER SELF-TEST. (X) 2L73 4F A3WE 19951006000451995100600045NM 1995 10 6 TAOA089505 119950818A3350900835A EEL BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15924TS 21041 RIGHT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK - OPS CHECK OK PER MM 33-50. (X) 2L73 4F A3WE 19951006000461995100600046NM 1995 10 6 TAOA089507 119950825A3350900835A EEL BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15924TS 18142K 21041 RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK FOR RT FORWARD OVERWING EMERGENCY EXIT LIGHT - OPS CHKS OK. (X) 2L73 4F A3WE 19951006000471995100600047NM 1995 10 6 TWRA9549 119950813A3350BC50047001 EEL BUFFER MOD BOEING747 747212B 1384886NM CABIN INOPERATIVE A TWRAK NONE L NO TEST CRCRUISE 1 EA15616FF 21939 DURING CRUISE, EMERGENCY EXIT EGRESS LIGHTS BEGAN TO BLINK IN C-ZONE BY 2-R M.E.D. UPON LANDING, MAINTENANCE REPLACED THE BUFFER MODULE. OPS CHECK OK. (X) 2L74 4F A20WE 19951006000481995100600048NM 1995 10 6 UIEA9503 119950824A783065B9462228 TR DUCT BOEING747 747230B 1384889NM NR 4 ENGINE CHAFED A UIEAAE UNSCHED LANDING ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CLCLIMB 1 EA15508MC 21644 DURING CLIMB-OUT, NR 4 PYLON VALVE CLOSE LIGHT CAME ON FOLLOWED BY HI-STAGE OPEN LIGHT, FOLLOWED BY FIRE WARNING ALMOST FULL SCALE. FIRE WARNING AND HI-STAGE OPEN LIGHT WENT OUT WHEN THROTTLE PULLED BACK. DUMP FUEL, AIR TURN BACK. FOUND REVERSER BLEED AIR DUCT CHAFING AGAINST REVERSER GROUND AIR DUCT. REPLACED DUCTS. OPERATES NORMAL. (X) 2L74 4F A20WE 19951006000491995100600049NM 1995 10 6 USVA8951 119950809A3350079123 EEL LENSE BRUCE BR2013P BOEING737 737247 138448DNM CABIN MISSING A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 EMERGENCY FLOOR LEVEL TRACK LIGHTING MISSING ONE RED LENSE. REPLACED LENSE. (X) 2L72 4F A16WE 19951006000501995100600050NM 1995 10 6 USVA8952 119950809A3350CM3071 EEL BOEING737 737247 138448DNM CABIN INOPERATIVE A USVAK NONE L NO TEST ININSP/MAINT 1 SO19305VA 19606 DURING INSPECTION, FOUND WHITE FLOOR TRACK LIGHT AT ROW 21 INOPERATIVE. REMOVED AND REPLACED FLOOR TRACK LIGHT IAW 33-51-122. OPS CHECK GOOD. (X) 2L72 4F A16WE 19951006000511995100600051NM 1995 10 6 USVA8953 119950811A3350079123 EEL LENSE BRUCE BR2013P BOEING737 737247 138448DNM CABIN MISSING A USVAK NONE L NO TEST ININSP/MAINT 1 SO19305VA 19606 EMERGENCY FLOOR TRACK LIGHTING MISSING ONE WHITE LENSE. (X) 2L72 4F A16WE 19951006000521995100600052EU 1995 10 6 VTZA95246 119950805A7600 CONNECTOR WIRE JETAIRJETSTMJETSTM4101 1500501EU LT CHAFED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27326UE 41064 IAD/DAY - FLT 6292 - DURING TAKEOFF AT 1245 HRS ON 8-5-95, ABORTED TAKEOFF DUE TO THE LT IEC, PN 21188406, FAILED ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED A CHAFED WIRE TO THE TT2 CANNON PLUG. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951006000531995100600053EU 1995 10 6 VTZA95255 119950818A7921L86023281 OIL COOLER JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 EA27324UE 41017 TYS/IAD - FLT 6175 - DURING CRUISE AT 2000 HRS ON 8-18-95, RETURNED TO TYS DUE TO THE LT ENGINE LOSING OIL PRESSURE IN-FLIGHT. AIRCRAFT LANDED AT TYS WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE OIL COOLER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951006000541995100600054EU 1995 10 6 VTZA95258 119950823A5270 WARN SYSTEM JETAIRJETSTMJETSTM4101 1500501EU BAGG DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27324UE 41017 IAD/EWR - DURING TAKEOFF AT 1220 HRS ON 8-23-95, ABORTED TAKEOFF TO EWR DUE TO BAGGAGE DOOR WARNING ILLUMINATED, AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED BAGGAGE DOOR MICROSWITCH AND RESET WARNING SYSTEM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951006000551995100600055EU 1995 10 6 VTZA95269 119950825A523014152060427 DOOR JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE BAY NOT LATCHED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27324UE 41017 IAD/LGA - FLT 6341 - DURING TAKEOFF AT 1130 HRS ON 8-25-95, ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR LIGHT ILLUMINATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RELATCHED THE BAGGAGE DOOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951006000561995100600056WP 1995 10 6 9514539865 119950921A5350 RELEASE CABLE DOUG DC9 DC951 3022051WP TAILCONE OUT OF POSITION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01774NC 47776 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ALSO, FOUND THAT THE UPPER LEFT PULLEY WAS MISSING THE RETAINER PIN AND THE CABLE HAD JUMPED THE PULLEY AND WAS UNDAMAGED. REINSTALLED CABLE AND REPLACED THE PIN. ADJUSTED THE RELEASE SYSTEM AND HANDLE CLIPS, CHECKED OK. 2L72 4F A6WE 19951006000571995100600057WP 1995 10 6 9514549604 119950602A5330 SKIN DOUG DC9 DC932 3022066WP FS 370-427 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB SKIN FS 370 TO 427, BENEATH THE SCUFF PLATE. REPAIRED SKIN (P/N 5911412), PER EA 99-97600. 2L72 4F A6WE 19951006000581995100600058WP 1995 10 6 9514559604 119950727A5330 SKIN DOUG DC9 DC932 3022066WP FS 1121-1168 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01604NW 47222 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT FUSELAGE SKIN FRAME FS 1121 TO 1168, LONGERONS 9L TO 16L. REPLACED SKIN (P/N 5910228-209), PER EA 99-97603. 2L72 4F A6WE 19951006000591995100600059WP 1995 10 6 9514569612 119950810A5210 ANGLE DOUG DC9 DC932 3022066WP AFT ENTRY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01612NW 47436 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2 INCH CRACK IN THE AFT ENTRY DOOR PAN, LOWER CENTER BEAM ATTACH ANGLE AND VERTICAL ANGLE. REPAIRED PER EA 96-100274. 2L72 4F A6WE 19951006000601995100600060WP 1995 10 6 9514579922 119950829A5412 BLKHD WEB DOUG DC9 DC932 3022066WP PYLON CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED PER EA 99-100864. 2L72 4F A6WE 19951006000611995100600061WP 1995 10 6 9514589953 119950831A5313 LONGERON DOUG DC9 DC931 3022065WP FS 570 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT THE FS 570 SPLICE. REPAIRED SPLICE (P/N 5920319-504), PER EA 99-97125. 2L72 4F A6WE 19951006000621995100600062WP 1995 10 6 9514591143 119950905A5320 ANTENNA MT RINGS DOUG DC10 DC1040 3023508WP FUSELAGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01133JC 46752 DURING PERIODIC CHECK, FOUND CORROSION ON BOTH PAIRS OF RADIO ALTIMETER ANTENNA MOUNTING RINGS. REPAIRED RINGS (AYB 7022, AYB 7053), PER EA 11-98920. 2L73 4F A22WE 19951006000631995100600063WP 1995 10 6 9514609970 119950908A5320 CUSP DOUG DC9 DC931 3022065WP FS 965-966 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019334 47247 DURING H-CHECK, FOUND CORROSION ON THE RIGHT CUSP BETWEEN FS 965 TO 966. REPAIRED PER EA 99-102778. 2L72 4F A6WE 19951006000641995100600064WP 1995 10 6 9514619955 119950909A5220 PAN DOUG DC9 DC931 3022065WP RT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING H-CHECK, FOUND A CRACK IN THE RIGHT FORWARD OVERWING EMERGENCY EXIT DOOR PAN. REPAIRED PAN (P/N 5913195-1), PER EA 99-103273. 2L72 4F A6WE 19951006000651995100600065NM 1995 10 6 9514626624 119950909A5414 SKIN BOEING747 747251B 1384892NM NR 1 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING PERIODIC CHECK, FOUND A .25 INCH CRACK IN THE NR 1 PYLON INBOARD SKIN AT NACELLE STATION 175, WATER LINE 151. REPAIRED SKIN PER EA 66-99085. 2L74 4F A20WE 19951006000661995100600066WP 1995 10 6 9514639949 119950913A5280 CASTING DOUG DC9 DC931 3022065WP RT MLG DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND 4 INCH CRACK IN THE RIGHT MAIN LANDING GEAR WHEEL WELL DOOR HINGE ATTACH CASTING AT THE LOWER OUTBOARD FLANGE. REPLACED CASTING PER SRM 51-01. 2L72 4F A6WE 19951006000671995100600067WP 1995 10 6 9514649955 119950913A5313 LONGERON DOUG DC9 DC931 3022065WP FS 580 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING H-CHECK, FOUND A 6 INCH CRACK IN LONGERON 29L AT THE FS 580 SPLICE. REPAIRED SPLICE (P/N 5920319-504), PER EA 99-103274. 2L72 4F A6WE 19951006000681995100600068WP 1995 10 6 9514659955 119950913A5330 SKIN DOUG DC9 DC931 3022065WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING H-CHECK, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN, FS 200 AT THE MAIN CABIN DOOR JAMB PSE 53.09.031. REPAIRED SKIN (P/N 5911406-5), PER EA 99-100868. 2L72 4F A6WE 19951006000691995100600069NM 1995 10 6 9514662279 119950913A5343 TRUNNION FITTING BOEING727 727251 138408HNM NLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01279US 21158 DURING PERIODIC CHECK, FOUND CORROSION ON THE NOSE LANDING GEAR UPPER RIGHT TRUNNION FITTING. REPLACED FITTING (P/N 65-17676-40), PER SRM 51-10-01 PG 4 PARA 4. 2L73 4F A3WE 19951006000701995100600070WP 1995 10 6 9514679853 119950913A5343 FITTING DOUG DC9 DC951 3022051WP LT MLG CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND A CRACK IN THE LEFT MAIN LANDING GEAR FITTING, LOWER INBOARD AND OUTBOARD BOLT HOLES. REPLACED FITTING PER CITEXT 09-5740-1-0006. 2L72 4F A6WE 19951006000711995100600071WP 1995 10 6 9514689953 119950913A5313 LONGERON DOUG DC9 DC931 3022065WP FS 945 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND A ONE INCH CRACK IN LONGERON 17R, FS 945 BOTH FRAME ATTACH POINTS. REPAIRED LONGERON (P/N 5911427-9), PER EA 99-100870. 2L72 4F A6WE 19951006000721995100600072NM 1995 10 6 9514696624 119950914A5753 SKIN BOEING747 747251B 1384892NM TE MIDFLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING PERIODIC CHECK, FOUND A PREVIOUS REPAIR CRACKED AND DISBONDING ON THE RIGHT WING INBOARD MIDFLAP LOWER FORWARD PANEL, WBL 210. REPAIRED PANEL (P/N 65B08426-202), PER EA 66-80179. 2L74 4F A20WE 19951006000731995100600073WP 1995 10 6 9514709853 119950914A5210 FITTING DOUG DC9 DC951 3022051WP AFT ENTRY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR LOWER HORIZONTAL BEAM END FITTING. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951006000741995100600074NM 1995 10 6 9514716624 119950915A5730 SKIN BOEING747 747251B 1384892NM WS 1309 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING PERIODIC CHECK, FOUND CORROSION ON THE RIGHT WING LOWER SKIN FORWARD OF THE FRONT SPAR, FS 1309 AT THE LEADING EDGE TENSION ROD FITTING PAD. REPAIRED PAD PER EA 66-99086. 2L74 4F A20WE 19951006000751995100600075WP 1995 10 6 9514729853 119950915A5743 HINGE DOUG DC9 DC951 3022051WP NR 2 FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 18289 47710 DURING H-CHECK, FOUND CORROSION ON THE NR 2 FLAP FORWARD HINGE FITTING AT THE UPPER STUD HOLES. REPLACED HINGE (P/N 5919218-505), PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19951006000761995100600076WP 1995 10 6 9514739949 119950921A7120 MOUNT DOUG DC9 DC931 3022065WP RT ENGINE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT ENGINE AFT MOUNT. REPLACED MOUNT PER MM 71-20-2. 2L72 4F A6WE 19951006000771995100600077WP 1995 10 6 9514749955 119950915A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01922RW 47182 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19951006000781995100600078WP 1995 10 6 9514759853 119950913A5220 RELEASE MECH DOUG DC9 DC951 3022051WP RT EMER EXIT OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO RELEASE THE RIGHT AFT OVERWING EMERGENCY EXIT DOOR. ADJUSTED THE EXIT DOOR PER MM 52-21-10 STEP G, CHECKED OK. 2L72 4F A6WE 19951006000791995100600079WP 1995 10 6 9514769105 119950916A5350 CLIPS DOUG DC9 DC915 3022036WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL0195S 47205 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19951006000801995100600080WP 1995 10 6 9514779914 119950921A5247 DOOR DOUG DC9 DC931 3022065WP APU MISSING A NWAAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 GL01964N 47416 GRR-DTW - ON ARRIVAL, FOUND THE RIGHT SIDE APU DOOR AND FUEL SHROUD DRAIN MAST WERE MISSING, WITH DAMAGE TO THE APU DOOR JAMB. THE FLIGHT CREW REPORTED NO EFFECT EN ROUTE. REPLACED THE APU DOOR, DRAIN MAST AND REPAIRED THE DOOR JAMB. 2L72 4F A6WE 19951006000811995100600081EU 1995 10 6 9514783229 119950927A2710D9550001900700 CONTROLLER AIRBUS320 A320211 3930320EU FLIGHT DECK MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL01329NW 306 DURING CRUISE, EXPERIENCED SEVERAL UNCOMMANDED AILERON ROLLS. THE RIGHT AILERON APPEARED TO MOVE ON THE ECAM PICTORIAL WHILE THE LEFT WAS STABLE. ALSO, RECEIVED ELAC 1 FAULT. AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S SIDESTICK ASSEMBLY AND REPLACED THE PITCH AND ROLL TRANSDUCERS ON THE FIRST OFFICER'S SIDESTICK ASSEMBLY. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951006000821995100600082WP 1995 10 6 9514799980 119950925A3260 SWITCH DOUG DC9 DC931 3022065WP LT MLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL019344 47440 DLH - DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED FOR LANDING. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. REPLACED THE LEFT MAIN GEAR DOOR SWTICH AND CYCLED GEAR DOORS SEVERAL TIMES. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006000831995100600083WP 1995 10 6 9514809926 119950807A3150 SWITCH DOUG DC9 DC932 3022066WP T/O WARNING MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01926NW 47425 TAKEOFF WARNING HORN SOUNDED WHEN THROTTLES WERE ADVANCED FOR TAKEOFF. CYCLED FLAPS AND SPEED BRAKES, NO HELP. ABORTED TAKEOFF AT 10 TO 20 KNOTS AND RETURNED TO GATE. REPLACED TAKEOFF WARNING SWITCH. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006000841995100600084WP 1995 10 6 9514819882 119950902A2781 WARNING LIGHT DOUG DC9 DC951 3022051WP TE FLAPS ILLUMINATED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01670MC 47659 MSP - ON FINAL APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED. SLATS WERE VISUALLY CONFIRMED TO BE EXTENDED AND NO ROLL WAS NOTICED. EXECUTED GO-AROUND AND LANDED SAFELY WITHOUT INCIDENT ON SECOND ATTEMPT. CYCLED FLAPS AND SLATS SEVERAL TIMES AND DISCREPANCY COULD NOT BE DUPLICATED ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006000851995100600085NM 1995 10 6 95FDEA01445 119950928A3230 SENSOR BOEING727 727227 1384078NM RT MLG FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO25479FE 21461 DURING T/O WITH WEIGHT OFF LDG GEAR, LDG GEAR LEVER LATCH FAILED TO RELEASE, CB ON P6-3 WERE IN. UPON RETRACTING FLAPS IAW CHECKLIST FROM 5 TO 2 DEGREES, RECEIVED A T/O WARNING HORN. GEAR REMAIN DOWN ON THE GRD, RT MAIN IND LT FLASHES. REMOVED AND REPLACED BOTH AIR AND GROUND SENSING SENSORS (M831, M832), IAW MFG MM 32-0-221. OPS TESTED GOOD AND OK FOR RETURN TO SERVICE. OFF (PN 1899-15), ON (SN 163996), POS AIR REA 02. 2L73 4F A3WE 19951006000861995100600086NM 1995 10 6 95FDEA01446 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1090 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 22 WL 149. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000871995100600087NM 1995 10 6 95FDEA01447 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1110 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 LBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000881995100600088NM 1995 10 6 95FDEA01448 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1110 DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 RBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000891995100600089NM 1995 10 6 95FDEA01449 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1010 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1010 RBL 24 WL 146. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000901995100600090NM 1995 10 6 95FDEA01450 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1090 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 RBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000911995100600091NM 1995 10 6 95FDEA01451 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1090 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000921995100600092NM 1995 10 6 95FDEA01452 119950928A5311 FRAME BOEING727 727225 1384077NM BS 1190 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THERE IS MECHANCIAL DAMAGE ON UPPER FLANGE OF FRAME AT BS 1190 RBL 20 WL 151. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. 2L73 4F A3WE 19951006000931995100600093NM 1995 10 6 95FDEA01453 119950928A5330 SKIN BOEING727 72725C 138400HNM PAX DOOR CUTOUT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CRACK IN SKIN AT FWD EDGE OF ENTRY DOOR CUTOUT JUST BELOW STR 7L. REPAIRED PER ESO 11782 DATED 9-15-95 AND EA 7-5330-25765 DATED 9-18-95. 2L73 4F A3WE 19951006000941995100600094NM 1995 10 6 95FDEA01454 119950928A5320 CASTING BOEING727 72725C 138400HNM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UPPER LOBE FLOOR, FOUND CORROSION ON 9G NET FLOOR ANCHOR STA 360 LT LBL 24. INSTALLED NEW NET ANCHOR CASTING PER SRM 51-10-1 EA 7-5320-25815 DATED 9-25-95. 2L73 4F A3WE 19951006000951995100600095NM 1995 10 6 95FDEA01455 119950928A5320 CASTING BOEING727 72725C 138400HNM BS 460-487 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 THE 9G NET CASTING HAS HEAVY CORROSION, JUST I/B OF RBL 45 SEAT TRACK AND CRACKED STA 460 TO 487. FABRICATED NEW SUPPORT PER EA 7-5320-25815 DATED 9-25-95. INSTALLED FITTING 9G AT RBL 45 IAW ESO 11782 DATED 9-15-95 AND SRM 51-10-1. 2L73 4F A3WE 19951006000961995100600096NM 1995 10 6 95FDEA01456 119950927A5311 FRAME BOEING727 72725C 138400HNM BS 870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 BS 870 TERMINAL FITTING AFT ROW 2ND FASTENER HOLE ABOVE STR 10R HAS CRACK IND, AT 12 O'CLOCK ON O/B SIDE OF O/B FLANGE, RT SIDE FUSELAGE. CRACK IN FRAME STA 870 RT JUST ABOVE STR 10R CRACK IND IS BETWEEN THE 3RD AND 4TH FASTENER ABOVE STR 10R. INSTALLED DOUBLERS PER SB 727-53-0194-NSC2 AND NR JOB FROM NR 0724. REF NR 0724 PGS 1 AND 2 JOB PROGRESS FORMS THIS REPAIR. 2L73 4F A3WE 19951006000971995100600097WP 1995 10 6 95FDEA01457 119950928A5512ALC72812 SKIN DOUG DC10 DC1030F 3023504WP RT HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25301FE 46800 RIGHT HORIZONTAL STABILIZER, UPPER AFT SKIN PANEL CRACKED AT I/B AFT CORNER O/B OF THE OPERATION BULKHEAD, CRACK LENGTH .6250 INCH. REPAIRED UPPER AFT SKIN STAB PANEL PER EA NR 8-5510-25166. INSTALLED AND SEALED ALL ACCESS AND L/E PANELS AS REQ IAW MM 55-10-02. 2L73 4F RTA22WE 19951006000981995100600098NM 1995 10 6 95FDEA01458 119950926A3240 BRAKE ASSY DOUG MD11 MD11F 3023600NM MLG DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25611FE MUO150N 416EA526 REFERENCE NR 7015 - DURING REPLACEMENT OF WORN TIRE AND WHEEL ASSY ON POS NR 3, FOUND ROTORS ON BRAKE ASSY DAMAGED. ROTORS NR 3, 4 AND 5 ARE DELAMINATED. STATORS NR 3 AND NR 5 ARE SHOWING SIGNS OF DELAMINATION, POSSIBLY DUE TO CHEMICAL CONTAMINATION, SOAPS AND DEGREASES. REMOVED BROKEN BRAKE ASSY, REF 32-43-20. INSTALLED BRAKE ASSY PER MM 32-43-01. C/W BRAKE TEMP MM TIRE PRESS IND MM 52-40-00, 700-804. C/W BRAKE TEMP IND CHECK MM 32-40-00, 700-802. 2L73 4F RTA22WE 19951006000991995100600099WP 1995 10 6 ABXA9500748 119950928A793356B3D OIL TEMP SENSOR DOUG DC8 DC862 3021970WP NR 4 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 GL23801AX 46077 DURING CRUISE, NR 4 ENGINE OIL TEMP INDICATION INCREASED TO 140 DEGREES CELSIUS. ENGINE OIL PRESSURE AND ALL OTHER ENGINE PARAMETERS REMAINED NORMAL. ENGINE THRUST WAS INCREASED TO MAX CRUISE AND OIL TEMP REMAINED HIGH. ENGINE THRUST WAS REDUCED TO IDLE AND OIL TEMP REMAINED HIGH. ENGINE WAS SHUTDOWN AND THEN RESTARTED 10 MINUTES LATER, WHEN THE OIL TEMP SUDDENLY DROPPED TO 75 DEGREES CELSIUS. OIL TEMP INDICATION WAS NORMAL FOR REMAINDER OF FLIGHT. REPLACED NR 4 ENGINE OIL TEMP SENSOR IAW DC8 MM, CHAPTER 79. ENGINE WAS GROUND RUN AND OPS CHECK WAS GOOD. 2L74 4F 4A25 19951006001001995100600100WP 1995 10 6 ABXA9500749 119950928A3230 RETRACT MECH DOUG DC9 DC941 302207NWP LANDING GEAR MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23965AX 47498 ILN - AFTER TAKEOFF WITH GEAR SELECTOR UP, ALL THREE UNSAFE LIGHTS AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED. ALL THREE GEARS APPEARED TO REMAIN DOWN. RECYCLED GEAR, RETRACTED NORMALLY WITH NORMAL INDICATIONS. JACKED AIRCRAFT AND PERFORMED SIX GEAR RETRACTIONS AND INDICATIONS WERE NORMAL. CHECKED RIGGING OF LANDING GEAR, CONTROL VALVE AND EMERGENCY EXTENSION AND ALL CHECKED OK IAW DC9 SUPPLEMENTAL MM, CHAPTER 32. 2L72 4F A6WE 19951006001011995100600101NE 1995 10 6 DL31L953844 219950927A7230 COMPRESSOR AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 2 ENGINE STALLED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO11837AB 674 724910 DURING TAXI OUT, NR 2 ENGINE HAD OFF IDLE STALL, RETURNED TO BLOCK. ENGINE WAS REPLACED AND ROUTED TO SHOP. 2L72 4F RTA35EU E24NE 19951006001021995100600102NM 1995 10 6 DL72E953853 119950927A3231 RETRACT MECH BOEING727 727247 138408FNM LDG GEAR DOORS MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11282WA 21484 CVG - DURING CLIMBOUT ABOVE 350 KTS AT 17,000 FT, LANDING GEAR DOOR MASTER AND ALL GEAR RED INDICATORS WERE MOMENTARILY FLASHING, ACCOMPANIED BY BRIEF BUFFECTING OF AIRCRAFT. THE ACFT RETURNED TO CVG. JACKED A/C AND RAN GEAR, ALL NORMAL. TIGHTENED AIR GROUND SENSE ARM, RETURNED TO SERVICE. 2L73 4F A3WE 19951006001031995100600103NM 1995 10 6 DL72S953839 119950906A711065196472 COWL BOEING727 727232 1384082NM NR 2 ENGINE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING HMV, NR 2 ENGINE RT AFT COWL PANEL WAS FOUND WITH TOP SIDE SKIN RIVETS ALONG LONGERON ARE SHORT OF EDGE DISTANCE. ALSO, TOP EDGE OF COWL IS WORN. REPAIRED PER SRM 54-10-3 FIG 6. 2L73 4F A3WE 19951006001041995100600104NM 1995 10 6 DL72S953846 119950923A33501001141 EEL BOEING727 727232 1384082NM AFT AIRSTAIR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11467DA 20744 AFT AIRSTAIR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED LIGHT ASSEMBLY AND BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19951006001051995100600105NM 1995 10 6 DL72W953841 119950927A3350 EEL 1001141 BOEING727 727247 138408FNM AFT STAIRWAY INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO112813W 20869 AFT STAIRWAY EMERGENCY LIGHT INOP. REPLACED BATTERIES, NO HELP. FWD TO MCO AND PLACARD. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL. 2L73 4F A3WE 19951006001061995100600106NM 1995 10 6 DL757953845 119950918A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE COLLAPSED A DALAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 SO11667DN 25035 FLL - CLIMBING THROUGH 18,000 FT, HEARD LOUD BAND AND THUMP IN THE NOSE AREA. ACFT RETURNED AND FOUND RADOME DAMAGED. INDICATION IS THAT RADOME COLLAPSED AT A SUSPECTED AREA OF DELAMINATION. RADOME WAS ROUTED TO SHOP FOR REPAIRS. 2L72 4F RTA2NM 19951006001071995100600107WP 1995 10 6 DLL15953840 119950927A33505165741 EEL POWER SUPPLY LKHEED1011 10113853 5265020WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11756DR 193Y1185 DURING TEST, R-2 EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED POWER SUPPLY, CHECKS OK. 2L73 4F A23WE 19951006001081995100600108NM 1995 10 6 DLM90953852 119950927A3350 EEL WIRE DOUG MD90 MD9030 3023690NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11905DA 53385 DURING TEST, LAST 12 EMERGENCY FLOOR TRACK LIGHTS ARE INOP. FOUND LOOSE POWER WIRE IN TRACK. RECONNECTED WIRE, OPERATION NORMAL. 2L72 4F RTA6WE 19951006001091995100600109WP 1995 10 6 MWEA95324 119950928A5330 SKIN DOUG DC9 DC932 3022066WP BS 465 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31501ME 47132 WHILE ACCOMPLISHING A VISUAL INSPECTION OF THE LOWER FUSELAGE SKIN IAW AD 85-03-08, A 1.5 INCH CRACK WAS FOUND AT STA 465 AND LONGERON 30. INSTALLED TEMPORARY REPAIR IAW SB A53-188 AND DAC DRAWING SB 09530188. 2L72 4F A6WE 19951006001101995100600110WP 1995 10 6 MWEA95325 119950927A793162644B REGULATOR DOUG DC9 DC932 3022066WP LT ENGINE INTERMITTENT A MWEACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL31602ME 48133 DURING TAKEOFF AT APPROXIMATELY 100 KTS, THE LEFT ENGINE OIL PRESSURE WAS SLIGHTLY ABOVE 80 PSI. ABORTED TAKEOFF, RETURNED TO BLOCK. REPLACED REGULATOR PER MM 79-32 AND ADJUSTED TO PROPER LIMITS. RUN UP, LEAK AND OPS CHECK GOOD. 2L72 4F A6WE 19951006001111995100600111WP 1995 10 6 MWEA95326 119950927A7931 OIL PRESS WIRE DOUG DC9 DC932 3022066WP LT ENGINE BROKEN A MWEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31602ME 48133 TEN MINUTES INTO FLIGHT, LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE AND ALL OTHER INDICATIONS WERE NORMAL. TWENTY MINUTES INTO FLIGHT, LEFT ENGINE OIL PRESSURE DROPPED TO ZERO AND OIL PRESSURE LOW LIGHT AND OTHER INDICATIONS NORMAL. ACFT RETURNED TO MKE. FOUND WIRES BROKEN INSIDE THE INSULATION AT THE OIL PRESSURE TRANSMITTER ELECTRICAL CONNECTOR. REMOVED AND REPLACED THE CONNECTOR, OPS CHECKED GOOD. 2L72 4F A6WE 19951006001121995100600112NM 1995 10 6 P5CA9500790 119950929A760065B8270328 SWITCH MODULE BOEING747 747124 1384874NM CONTROL STAND FAILED A P5CAD RETURN TO BLOCK Y ENGINE STOPPAGE TXTAXI/GRND HDL 1 WP23855FT 19733 AFTER ENGINE START, TAXI AND DURING FLIGHT ENGINEER CHECK, SHUT OFF NR 4 ENGINE FUEL BOOST PUMPS AND ENGINE SHUTDOWN. REPLACED START LEVER CONTROL STAND SWITCH MODULE PER MAINTENANCE MANUAL 76-11-02. 2L74 4F A20WE 19951006001131995100600113NM 1995 10 6 SCNA95200 119950919A55202024T3 DOUBLER BOEING727 727282 2F0R NM RT ELEVATOR CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15281SC 21949 DURING C-CHECK, A CRACKED DOUBLER WAS FOUND ON THE RIGHT ELEVATOR REAR SPAR JUST ABOVE THE CONTROL ROD. REMOVED CRACKED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW B727 SRM 55-26-01. 2L73 4F RTA3WE 19951006001141995100600114EU 1995 10 6 95ZZZX5384 119950912A3230 T-HANDLE STBROSSD3 SD360 8100606EU LANDING GEAR OUT OF POSITION A SABAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05747HH SH3747 CLT\AGS - FLT 5132 - FLIGHT HAD JUST TAKEN OFF. FLIGHT CREW SELECTED GEAR UP, BUT, THE LANDING GEAR DID NOT RETRACT. THE CREW SELECTED GEAR DOWN AND RETURNED TO CLT FOR AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL WERE DISPATCHED TO TROUBLESHOOT THE PROBLEM. THE EMERGENCY LANDING GEAR EXTENSION T-HANDLE WAS FOUND IN THE PULLED POSITION. THE HANDLE WAS RESET AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T A41EU 19951006001151995100600115WP 1995 10 6 95ZZZX5385 119950905A7933 OIL TEMP IND DOUG DC9 DC932 3022066WP NR 1 ENGINE MALFUNCTIONED A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 SO11529MD 47262 ATL/FLL - FLT 515 - FLIGHT MADE AN AIR RETURN TO ATL DUE TO NR 1 ENGINE HIGH OIL TEMP AT 150 DEGREES. ENGINE SHUT DOWN IN-FLIGHT AND CAPTAIN DECLARED EMERGENCY. RAN ENGINE AT POWER, OPS CHECK GOOD AFTER CHECKING ALL WIRING AND CONNECTORS. CHANGED OIL AND FILTER, NO ABNORMALITIES NOTED. CLEANED GROUND STUD (906) MM 79-23, 79-33, AND WD 79-33-00. ALSO, REMOVED AND REPLACED GROUND TERMINAL WITH NEW ONE. 2L72 4F A6WE 19951006001161995100600116 1995 10 6 95ZZZX5386 419950904A221025866891 CONTROLLER DOUG DC9 DC932 3022066WP AUTOPILOT MALFUNCTIONED A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11931VV 47674 JAN/ATL - FLT 494 - AUTOPILOT HEADING SELECT SWITCH SHORTED OUT WITH SMOKE IN-FLIGHT. REPLACED AUTOPILOT CONTROLLER, OPS CHECKED NORMAL PER MM 22-10. 2L72 4F A6WE 19951006001171995100600117WP 1995 10 6 95ZZZX5387 119950907A5242 DOOR DOUG DC9 DC932 3022066WP E/E COMPT NOT LATCHED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11930VV 47723 ATL/DTW FLT 444 - ELECTRICAL COMPARTMENT DOOR CAME OPEN IN-FLIGHT, RETURNED TO GATE. SECURED E & E DOOR, OPS CHECKED ANNUNCIATOR LIGHT, OPS CHECKED OK. 2L72 4F A6WE 19951006001181995100600118NM 1995 10 6 95ZZZX5388 119950708A5320 SUPPORT BOEING737 7373T0 1384582NM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND CORROSION ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT BILGE AREA AT BS 500 - BS 500A, RBL 24. THE CORROSION WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-01. (X) 2L72 4F RTA16WE 19951006001191995100600119NM 1995 10 6 95ZZZX5389 119950707A5320 CHANNEL BOEING737 7373T0 1384582NM BS 952-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOOR SUPPORT CHANNEL IN AFT GALLEY AREA AT STA 952 - STA 967, RBL 18. THE CORROSION WAS REMOVED AND A SUPPORT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-01. (X) 2L72 4F RTA16WE 19951006001201995100600120CE 1995 10 6 95ZZZX5390 119950909A273008150972 ACTUATOR ASSY CESSNA402 402C 207590RCE ELEV PITCH SYST FAILED ASAGUUAA UNSCHED LANDING EF VIBRATION/BUFFET FLT CONT AFFECTED CLCLIMB 1 SO1969SC 43 04 402C0041 MHH/FLL - FLT 446 - AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A PITCH UP, PITCH DOWN, AND SEVERE VIBRATION. THE AIRCRAFT DIVERTED TO FPO AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO FPO TO REMOVE AND REPLACE THE ELEVATOR PITCH TRIM ACTUATOR. THE ROLL PINS (2) HAD VIBRATED OUT OF THE ELEVATOR PITCH TRIM ACTUATOR. 1L72 3O A7CE 19951006001211995100600121NE 1995 10 6 95ZZZX5391 219950825A7261625926 ADAPTER BOEING747 747131 1384881NM PWA JT9 JT9D20 52054NE NR 4 ENGINE FAILED A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0593119 20083 ATH - FLT 880 - DURING CRUISE, SHUT DOWN NR 4 ENGINE, SN 4178, DUE TO LOW OIL QUANTITY. FOUND OIL LEAK AT ANGLE GEARBOX OIL SCAVENGE LINE ADAPTER, MFG PN 625926. REPLACED OIL SCAVENGE LINE ADAPTER. ENGINE LEAK CHECKED AND OPERATION NORMAL. ENGINE TOTAL TIME: 78,763 HOURS; 13,798 CYCLES. CHECK C-2 - 10-19-94 - MCI. 2L74 4F4 F A20WE E20EA 19951006001221995100600122NM 1995 10 6 CAL950580 119950630A5320 DOUBLER BOEING737 7372C0 1384488NM BS 727A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .25 INCH CRACK AT UPPER FORWARD FASTENER ON DOUBLER REPAIR AT BS 727A, S17L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 25, PAGE 87. (X) 2L72 4F A16WE 19951006001231995100600123NM 1995 10 6 CAL950581 119950630A5313 STRINGER BOEING737 7372C0 1384488NM BS 727A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND .25 INCH CRACKS AT THREE FASTENERS ON BOTTOM ROW OF STR 14R AT STA 727A. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L72 4F A16WE 19951006001241995100600124NM 1995 10 6 CAL950582 119950630A5330 TEAR STRAP BOEING737 7372C0 1384488NM BS 727A CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .50 INCH CRACK IN TEAR STRAP AT FASTENER HOLE BELOW STR 14, LT STA 727A. A TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L72 4F A16WE 19951006001251995100600125NM 1995 10 6 CAL950583 119950630A5330 SKIN BOEING737 7372C0 1384488NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER STA 727A, S10R. THE CRACKED AREA OF SKIN WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19951006001261995100600126NM 1995 10 6 CAL950584 119950701A5720 WEBBING BOEING737 737219 1384469NM WS 139 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - THE RIGHT WING CENTER INBOARD OF STA 139 HAD WEBBING WITH CRACKS AROUND FASTENER HOLES. THE CRACKS WERE .25 INCH LONG. THE CRACKED AREAS WERE REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-40-6. (X) 2L72 4F A16WE 19951006001271995100600127NM 1995 10 6 CAL950585 119950701A5712 RIB BOEING737 737219 1384469NM WS 738 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF RT RIB AT LOWER FORWARD ATTACH HOLE, STA 738. THE CRACK WAS STOP-DRILLED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-10-5. (X) 2L72 4F A16WE 19951006001281995100600128NM 1995 10 6 CAL950586 119950701A5754 INTERCOSTAL BOEING737 737219 1384469NM NR 2 SLAT TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL OF NR 2 SLAT INBOARD SLAT TRACK, AT SLAT TRACK ATTACH FITTING AREA. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19951006001291995100600129NM 1995 10 6 CAL950587 119950701A5730 SKIN BOEING737 737219 1384469NM LT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - A .50 INCH CRACK WAS FOUND IN LT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUT-OUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (X) 2L72 4F A16WE 19951006001301995100600130NM 1995 10 6 CAL950588 119950701A5754 INTERCOSTAL BOEING737 737219 1384469NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - THE NR 6 SLAT INTERIOR HAD TWO EACH INTERCOSTALS CRACKED AT INBOARD SLAT TRACK ATTACH FITTING. EACH CRACK WAS APPROXIMATELY .50 INCH LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-50-3. (X) 2L72 4F A16WE 19951006001311995100600131NM 1995 10 6 CAL950589 119950701A5754 RIB BOEING737 737219 1384469NM NR 3 LE SLAT TRKCORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024852104 20344 GSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT THE NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS CLEANED UP AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3 AND SRM 51-30-2. (X) 2L72 4F A16WE 19951006001321995100600132NM 1995 10 6 CAL950597 119950717A2910 HYD LINE BOEING737 7372C0 1384488NM NR 2 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914245 20074 EWR - FLT 1216 - THE A-SYSTEM HYDRAULIC FLUID DROPPED IN-FLIGHT. THE NR 2 A-HYDRAULIC PUMP WAS TURNED OFF AND THE QUANTITY WAS MAINTAINED AT THREE-FOURTHS GALLON WITH PRESSURE HOLDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN A-SYSTEM HYDRAULIC PRESSURE LINE LEAKING. THE PRESSURE LINE WAS REPLACED AND THE HYDRAULIC SYSTEM WAS SERVICED. A LEAK CHECK WAS PERFORMED WITH THE ENGINE RUNNING AND NO DEFECTS WERE NOTED. (X) 2L72 4F A16WE 19951006001331995100600133NM 1995 10 6 CAL950625 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 986.50 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097035224487 23590 YVR - INSPECTION FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 986.50. THE FLOORBEAM WAS REPAIRED PER ECRA 5310-03139. (X) 2L72 4F RTA16WE 19951006001341995100600134NM 1995 10 6 CAL950626 119950711A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 948 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097035224487 23590 YVR - INSPECTION FOUND THE FLOORBEAM CORRODED AT BS 948, BETWEEN LBL 6 AND RBL 4. REPAIRED PER ECRA 5310-03141. (X) 2L72 4F RTA16WE 19951006001351995100600135NM 1995 10 6 CAL950627 119950725A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096931130313 23362 HOU - INSPECTION FOUND A 1 INCH CRACK IN CABIN FLOORBEAM AT BS 520, RBL 45.5. THE FLOORBEAM WAS REPAIRED IAW ECRA 5320-01208. (X) 2L72 4F RTA16WE 19951006001361995100600136NM 1995 10 6 CAL950670 119950706A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION IN AND AROUND CLIP NUT HOLES OF CABIN FLOORBEAM AT STA 328, BL ZERO TO RBL 55. A FILLER AND ANGLE REPAIR WAS INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001371995100600137NM 1995 10 6 CAL950671 119950708A5512 SKIN BOEING737 7373T0 1384582NM RT HORIZ STAB DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND A 3 INCH BY 1.5 INCH BY .25 INCH DEEP DENT IN RT HORIZONTAL STABILIZER LEADING EDGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-10-01. (X) 2L72 4F RTA16WE 19951006001381995100600138NM 1995 10 6 CAL950672 119950708A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM BS 947-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND SURFACE AND INTERGRANULAR CORROSION ON FLOOR SUPPORT ANGLE IN AFT GALLEY AREA AT BS 947-967, LBL 17. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-02. (X) 2L72 4F RTA16WE 19951006001391995100600139NM 1995 10 6 CAL950673 119950708A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND SURFACE AND INTERGRANULAR CORROSION ON FLOORBEAM IN AFT GALLEY AREA AT BS 947, LBL 10 TO RBL 14. THE CORROSION WAS REMOVED IAW SRM 51-10-02. A NEW FLOORBEAM WAS TREATED AND INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001401995100600140NM 1995 10 6 CAL950674 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND SURFACE CORROSION ON TOP OF FLOORBEAM IN AFT LAV AREA AT BS 986, RBL 18 TO LBL 28. THE CORROSION WAS REMOVED. AN ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001411995100600141NM 1995 10 6 CAL950675 119950708A5330 SKIN BOEING737 7373T0 1384582NM BS 727-747 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND A 1 INCH LONG BY 0.075 INCH DEEP DENT IN UPPER FUSELAGE ROLLED SKIN BETWEEN BS 727B AND BS 747, STR 14R AND STR 15R. DOUBLERS WERE FABRICATED IAW SRM 51-40-00 AND SRM 51-20-01 AND THEN INSTALLED IAW SRM 53-00-01. (X) 2L72 4F RTA16WE 19951006001421995100600142NM 1995 10 6 CAL950676 119950707A5320 SUPPORT BOEING737 7373T0 1384582NM BS 540 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND A .50 INCH CRACK IN CABIN FLOOR SUPPORT AT BS 540, RBL 1, WL 208. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-40-04. (X) 2L72 4F RTA16WE 19951006001431995100600143NM 1995 10 6 CAL950677 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOORBEAM AT AFT LAV AREA AT STA 986, BL 43R. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-46-02. (X) 2L72 4F RTA16WE 19951006001441995100600144NM 1995 10 6 CAL950678 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION IN AND AROUND CLIP NUT HOLES OF CABIN FLOORBEAM AT STA 344, RLB 12 TO LBL 55. THE CORROSION WAS REMOVED AND A T-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001451995100600145NM 1995 10 6 CAL950680 119950706A5320 ANGLE BOEING737 7373T0 1384582NM FS 294-312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON CABIN FLOOR SUPPORT ANGLE BETWEEN BS 294.5 AND BS 312, RBL 14. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-01. (X) 2L72 4F RTA16WE 19951006001461995100600146NM 1995 10 6 CAL950682 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 294.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOORBEAM AT BS 294.5 FROM BL ZERO TO LBL 40, WL 208. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-00. (X) 2L72 4F RTA16WE 19951006001471995100600147NM 1995 10 6 CAL950683 119950707A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION IN AND AROUND NUT HOLES OF CABIN FLOORBEAM AT STA 312, BL ZERO TO LBL 55, WL 208.1. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001481995100600148NM 1995 10 6 CAL950684 119950706A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 312, BL ZERO TO RBL 55. THE CORROSION WAS REMOVED. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-00-58. (X) 2L72 4F RTA16WE 19951006001491995100600149NM 1995 10 6 CAL950685 119950709A5315 FLOORBEAM BOEING737 7373T0 1384582NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND CORROSION AT CLIP NUT HOLES OF FLOORBEAM AT STA 312, LBL 1 AND LBL 8. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5310-01102. (X) 2L72 4F RTA16WE 19951006001501995100600150NM 1995 10 6 CAL950687 119950707A5312 BLKHD ANGLE BOEING737 7373T0 1384582NM BS 986-1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOOR AND BULKHEAD DIAGONAL SUPPORT BEAMS AT BS 986 - BS 1016. THE CORRODED PART WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-30-02. (X) 2L72 4F RTA16WE 19951006001511995100600151NM 1995 10 6 CAL950688 119950706A5230 FRAME BOEING737 7373T0 1384582NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND A 4 INCH CRACK IN FORWARD CARGO DOOR FORWARD BOTTOM CORNER FRAME. THE CRACK WAS STOP-DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 52-30-02. (X) 2L72 4F RTA16WE 19951006001521995100600152NM 1995 10 6 CAL950691 119950709A5313 STRINGER BOEING737 7373T0 1384582NM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON STR 26L AT BS 500C. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-00-3 AND SRM 51-30-02. (X) 2L72 4F RTA16WE 19951006001531995100600153NM 1995 10 6 CAL950692 119950709A5313 STRINGER BOEING737 7373T0 1384582NM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON STR 26L AT BS 500A. THE CORRODED SECTION OF STRINGER WAS REMOVED. A STRINGER SECTION AND REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-00-03 AND SRM 53-00-02. (X) 2L72 4F RTA16WE 19951006001541995100600154NM 1995 10 6 CAL950693 119950706A5210 SKIN BOEING737 7373T0 1384582NM R-1 DOOR TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND OUTSIDE SKIN OF R-1 DOOR TORN AT BOTTOM HINGE POINT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L72 4F RTA16WE 19951006001551995100600155NM 1995 10 6 CAL950696 119950709A5320 STRAP BOEING737 7373T0 1384582NM BS 772 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND CORROSION ON STRAP FOR NUTPLATES IN AFT CARGO COMPARTMENT AT FLOOR CENTERLINE, STA 772. A STRAP WAS FABRICATED AND INSTALLED AND THE NUTPLATES WERE REPLACED IAW SRM 51-10-01 AND SRM 51-30-02. (X) 2L72 4F RTA16WE 19951006001561995100600156NM 1995 10 6 CAL950700 119950707A5312 BLKHD ANGLE BOEING737 7373T0 1384582NM BS 308 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON LAV BULKHEAD SUPPORT ANGLE AND STRAP AT BS 308 FROM LBL 12 TO LBL 45, WL 208. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-06. (X) 2L72 4F RTA16WE 19951006001571995100600157NM 1995 10 6 CAL950702 119950708A5320 CHANNEL BOEING737 7373T0 1384582NM BS 967-986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOOR SUPPORT CHANNEL IN AFT GALLEY AREA AT STA 967 - STA 986, RBL 18. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-02. THE FLOOR SUPPORT CHANNEL WAS REPLACED IAW ECRA 5320-01270. (X) 2L72 4F RTA16WE 19951006001581995100600158NM 1995 10 6 CAL950703 119950707A5230 SKIN BOEING737 7373T0 1384582NM AFT CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND A .50 INCH CRACK IN AFT CARGO DOOR INTERIOR SKIN. THE CRACK WAS LOCATED AT THE LIGHTENING HOLE, 22 INCHES ROM TOP OF DOOR AND 14 INCHES FROM FORWARD END OF DOOR. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-01. (X) 2L72 4F RTA16WE 19951006001591995100600159NM 1995 10 6 CAL950704 119950705A5330 SKIN BOEING737 7373T0 1384582NM BS 789 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - FLT MIDD - INSPECTION FOUND CORROSION AT FOUR NUTPLATES OF AFT CARGO DOOR JAMB SKIN PANEL AT STA 789, STR 23R - STR 25R. THE RIVETS WERE DRILLED OUT IAW SRM 51-30-2 AND THE NUTPLATES WERE REPLACED IAW SRM 51-10-1. (X) 2L72 4F RTA16WE 19951006001601995100600160NM 1995 10 6 CAL950718 119950814A5753 STRUTS BOEING737 7373T0 1384582NM RT TE FLAPS BROKEN A ACALAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 SW0976355 23593 BOS - FLT 1246 - TWO TO THREE UNITS OF LEFT WING DOWN WERE REQUIRED TO KEEP WINGS LEVEL AT FLAPS 1, 5, AND 10. MAINTENANCE FOUND THE RT WING CENTER OUTBOARD FLAP TRACK FAIRING STRUTS BROKEN WITH CAM TRACK DAMAGED AND THE PUSHROD FOR AFT FLAP BEARING BROKEN. THE STRUTS, CAM TRACK, AND PUSHROD WERE REMOVED AND REPLACED IAW MM 27-51-52. THE OUTBOARD FLAP FAIRING WAS INSTALLED AND RIGGED IAW MM 27-51-52. OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F RTA16WE 19951006001611995100600161NM 1995 10 6 CAL950734 119950820A323069355003 UPLOCK ACTUATOR BOEING737 7373T0 1384582NM RT MLG INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09143412351 23579 BUF - FLT 0640 - THE RT MLG GAVE AN UNSAFE GEAR INDICATION WHEN GEAR WAS EXTENDED ON APPROACH TO BUF. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND A TOWER FLY-BY WAS CONDUCTED. THE GEAR WAS CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG UPLOCK ACTUATOR AT FAULT. THE UPLOCK ACTUATOR WAS REMOVED AND REPLACED. THE GEAR WAS SWUNG SEVERAL TIMES AND OPERATION CHECKED GOOD. (X) 2L72 4F RTA16WE 19951006001621995100600162NM 1995 10 6 CAL950745 119950822A29136507606 HYD PUMP BOEING737 7372C0 1384488NM NR 2 ENGINE LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW097324313069843 20072 GSO - FLT 1275 - THE A-SYSTEM HYDRAULIC QUANTITY DECREASED TO ZERO DURING CLIMB-OUT OF GSO. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM LOW PRESSURE LIGHTS. A MANUAL GEAR AND FLAP EXTENSION WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F A16WE 19951006001631995100600163NM 1995 10 6 CAL950777 119950831A215039606411 FLOW CONTL VLV BOEING737 737247 138448DNM LT A/C PACK INOPERATIVE A ACALAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SW091424668663 20129 CLE - FLT 1244 - THE AIRCRAFT LOST PRESSURIZATION AT 31,000 FEET AND ALL OXYGEN MASKS DEPLOYED WHILE EN ROUTE FROM DAY TO EWR. 'ABNORMAL' PROCEDURES WERE FOLLOWED, BUT THE CABIN PRESSURE WAS UNCONTROLLABLE. THE AIRCRAFT WAS DIVERTED TO CLE AND WHILE ON APPROACH, THE CABIN PRESSURIZATION WORKED NORMALLY IN STAND-BY. MAINTENANCE FOUND LT A/C PACK NOT FUNCTIONING. THE LT FLOW CONTROL VALVE WAS REMOVED AND REPLACED AND LT A/C CHECKED GOOD. IN ADDITION, THE CABIN PRESSURE CONTROLLER WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. A DECAY CHECK WAS PERFORMED AND FELL WITHIN LIMITS. THE OXYGEN MASKS WERE RESTOWED. (X) 2L72 4F A16WE 19951006001641995100600164NM 1995 10 6 CAL950782 119950902A29136507506 HYD PUMP BOEING737 737291 138448WNM NR 1 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW091725225149192 20362 GSO - FLT 1495 - THE A-HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE A-HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. (X) 2L72 4F A16WE 19951006001651995100600165WP 1995 10 6 CAL950785 119950902A49203812761 APU DOUG DC9 DC982 3022082WP TAIL INOPERATIVE A CALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW0914840236135315 49580 FLT NR 356 - EWR - THE APU WAS IN USE PRIOR TO TAKEOFF FROM EWR, BUT WAS SHUT DOWN BEFORE TAKING THE RUNWAY. SMOKE ENTERED THE CABIN MOMENTARILY AFTER TAKEOFF. THE SMOKE DISSIPATED AND THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. THE APU WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L72 4F A6WE 19951006001661995100600166NM 1995 10 6 CAL950799 119950907A3232731414 ACTUATOR BOEING727 727232 1384082NM LT MLG DOOR LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW091777917091 20634 CUN - FLT 0774 - THE A-HYDRAULIC SYSTEM QUANTITY BEGAN TO SLOWLY DECREASE WHILE EN ROUTE FROM IAH TO SJO. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE A-HYDRAULIC SYSTEM WAS STABILIZED WITH BOTH A-PUMPS OFF. THE AIRCRAFT WAS DIVERTED TO CUN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOOR ACTUATOR LEAKING. THE DOOR ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19951006001671995100600167NM 1995 10 6 CAL950802 119950828A5320 WEB BOEING737 737217 1384464NM NLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 GSO - INSPECTION FOUND A 1 INCH CRACK IN NOSE WHEELWELL UPPER WEB AT THE INBOARD AFT CORNER ON LT SIDE AND CORROSION FOUND AT THE INBOARD FORWARD CORNER ON LT SIDE. THE WEB AREA WAS REPAIRED IAW EA 5310-02452 AND BAC DRAWING 65C35749. (X) 2L72 4F A16WE 19951006001681995100600168NM 1995 10 6 CAL950807 119950911A2910 HYD LINE BOEING737 737291 138448WNM A-HYD SYST LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0917252 20362 GSO - FLT 1867 - THE AIRCRAFT WAS RETURNED TO GSO AFTER LOSING THE A-HYDRAULIC SYSTEM IN-FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO OUTBOARD SPOILER PANEL IN LT WING OUTBOARD OF GEAR LEAKING. THE FLEX LINE WAS REPLACED. IN ADDITION, BOTH ENGINE DRIVEN HYDRAULIC PUMPS WERE REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM WAS SERVICED AND THE FLIGHT CONTROLS WERE CYCLED SEVERAL TIMES WITH BOTH ENGINES OPERATING AND OPERATION CHECKED GOOD WITH NO LEAKS NOTED. (X) 2L72 4F A16WE 19951006001691995100600169NM 1995 10 6 CAL950821 119950916A291357186 HYD PUMP BOEING727 727227 1384078NM NR 1 ENGINE INOPERATIVE A CALAO OTHER J WARNING INDICATION CRCRUISE 1 SW097675251211 21248 MSY - FLT 1528 - THE NR 1 HYDRAULIC B-PUMP LOW PRESSURE LIGHT ILLUMINATED IN-FLIGHT. 'ABNORMAL' PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 B-SYSTEM HYDRAULIC ELECTRIC DRIVEN PUMP HAD FAILED. THE PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L73 4F A3WE 19951006001701995100600170NM 1995 10 6 CAL950822 119950917A2782269002911 ACTUATOR BOEING727 727243 138408DNM NR 8 LE SLAT INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09579PE17958 21662 EWR - FLT 1900 - THE NR 8 LEADING EDGE SLAT WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE FLAPS WERE CYCLED WITH NO EFFECT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 8 LEADING EDGE SLAT ACTUATOR AT FAULT. THE NR 8 LEADING EDGE SLAT ACTUATOR WAS REMOVED AND REPLACED. THE LEADING EDGE SLATS WERE CYCLED SEVERAL TIMES PER MM 27-81-32, PAGE 406, AND OPERATION CHECKED GOOD. (X) 2L73 4F RTA3WE 19951006001711995100600171EU 1995 10 6 COEA9570201 119950905A3610AC61552 COMPRESSOR FOKKERF27 F27MK600 4990706EU RT ENGINE LEAKING A COEAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 NM01702FE 9 N7289 10350 DURING CRUISE OF REPOSITIONING FLIGHT TO MAF, RT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN ENGINE PRECAUTIONARY AND LANDED IN TCC WITHOUT INCIDENT. EMERGENCY MAINTENANCE CHECKED GEARBOX OIL CONTENT AND SERVICED. ENGINE RAN, OPS AND LEAK CHECK GOOD. OIL LEVEL CHECKED OKAY. AIRCRAFT RELEASED FOR FLIGHT. UPON ARRIVAL INTO MAF, EMPIRE MAINTENANCE INSPECTED GEARBOX AND FOUND A LARGE AMOUNT OF OIL IN THE RT MOISTURE SEPARATOR. MAINTENANCE PLACARDED RT COMPRESSOR PER MEL 36-10-1. RT COMPRESSOR REMOVED AND REPLACED IN DFW, OPS AND LEAK CHECK GOOD. (X) 2H72 4T A817 19951006001811995100600181WP 1995 10 6 9514829990 119950905A5400 ANGLE DOUG DC9 DC931 3022065WP FS 1104 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018950E 47186 DURING LINE CHECK, FOUND A CRACK IN THE LEFT PYLON UPPER SKATE ANGLE FS 1104. REPAIRED ANGLE PER EA 99-99246. 2L72 4F A6WE 19951006001821995100600182NM 1995 10 6 9514836719 119950908A5311 FRAME BOEING747 747251F 1384898NM FS 1460 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01619US 21321 DURING LINE CHECK, FOUND 3 CRACKS IN THE BS 1460 FRAME WEB BETWEEN STRINGERS 28R TO 29R. REPAIRED WEB (P/N 65B01891-26), PER EA 67-98246. 2L74 4F A20WE 19951006001831995100600183WP 1995 10 6 9514849104 119950912A5533 ANGLE DOUG DC9 DC915 3022036WP DORSAL FIN CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194S 47204 DURING B-CHECK, FOUND A CRACK IN THE DORSAL FIN ATTACH ANGLE AT LONGERON 2L. REPAIRED ANGLE (P/N 5939711-1), PER EA 91-99249. 2L72 4F A6WE 19951006001841995100600184NM 1995 10 6 9514852714 119950912A5320 WEB BOEING727 7272S7 138407ZNM FS 1156-1166 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01718RC 22344 DURING C-CHECK, FOUND CORROSION IN THE SHEAR WEB LOCATED AT BS 1156 TO 1166, LBL 54 TO 60. REPAIRED WEB (P/N 65-19604), PER EA 27-98247. 2L73 4F A3WE 19951006001851995100600185WP 1995 10 6 9514869957 119950913A5711 SPAR CAP DOUG DC9 DC931 3022065WP WS 319 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01915RW 47139 DURING LINE CHECK, FOUND A CRACK IN THE RIGHT WING REAR SPAR CAP AT XRS 319. REPAIRED CAP (P/N 5911300-502), PER EA 99-99248. 2L72 4F A6WE 19951006001861995100600186WP 1995 10 6 9514879921 119950918A5330 SKIN DOUG DC9 DC932 3022066WP DOOR JAMB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01943N 47647 DURING B-CHECK, FOUND A .5 INCH CRACK IN THE FORWARD AIRSTAIR DOOR JAMB SKIN, LOWER AFT CORNER. REPAIRED DOOR JAMB PER EA 99-99068. 2L72 4F A6WE 19951006001871995100600187WP 1995 10 6 9514889855 119950919A5415 FITTING DOUG DC9 DC951 3022051WP PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND A 1.25 INCH CRACK IN THE RIGHT PYLON FITTING LOCATED FORWARD AND INBOARD OF THE UPPER AFT PYLON STRAP. REPLACED FITTING PER SRM 51-01 PARA 1C AND 51-30. 2L72 4F A6WE 19951006001881995100600188WP 1995 10 6 9514899989 119950922A5230 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018945E 47181 DURING LINE CHECK, FOUND A CRACK IN THE UPPER AFT CARGO DOOR STOP FITTING, FORWARD CARGO DOOR JAMB. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951006001891995100600189NE 1995 10 6 9514905509 219950928A7261 GASKET BOEING757 757251 1384970NM PWA 2037 PW2037 NE LT ENGINE LEAKING A NWAAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 GL01509US 23198 716425 LEFT ENGINE WAS LOSING OIL AT APPROXIMATELY ONE QUART PER 16 MINUTES. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. FOUND GASKETS PINCHED ON NR 5 BEARING COVER. REPLACED GASKETS ON NR 5 BEARING HOUSING COVER AND ON NR 5 BEARING SCAVENGE TUBE. 2L72 4F4 FRTA2NM E17NE 19951006001901995100600190EU 1995 10 6 9514913217 219950927A73211459M55P17 ECU AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 1 ENGINE MALFUNCTIONED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING O OTHER CRCRUISE 1 GL01317US14128 197 731193 DURING CRUISE AT FL 390, THE AUTO THROTTLE TRIPPED OFF AND THE NR 1 ENGINE N1 SPEED ACCELERATED TO 102 PERCENT FOR 41 MINUTES. CYCLING OF THE THRUST LEVER WAS NO HELP, DESCENDED TO A LOWER ALTITUDE AND SHUT NR 1 ENGINE DOWN. AFTER ALLOWING THE ENGINE TO COOL, PERFORMED RESTART AND ALL INDICATIONS WERE NORMAL. AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE CONTROL UNIT AND OPERATIONAL CHECK OK. 2L72 4F4 FRTA28NM 19951006001911995100600191NM 1995 10 6 95FDEA01459 119950925A5320 FLANGE BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UPPER MAIN CARGO, CORROSION ON BOTTOM SIDE OF THE FWD FLANGE STA 480 RBL 5. REMOVED CORROSION AT LOCATIONS PER SRM 51-10-01, INSTALLED REPAIR IAW SRM 53-10-8 FIG 5 AND 51-40-2. 2L73 4F A3WE 19951006001921995100600192NM 1995 10 6 95FDEA01460 119950925A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UPPER LOBE FLOOR, CORROSION ON UNDERSIDE OF FLOORBEAM LT STA 480 BETWEEN BL 0 AND LBL 24. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED REPAIR IAW 53-10-8 FIG 5 AND 51-40-2. 2L73 4F A3WE 19951006001931995100600193NM 1995 10 6 95FDEA01461 119950928A5330 SKIN BOEING727 72725C 138400HNM BS 310-318 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION BETWEEN SKINS IN CORNER OF FWD ENTRY DOOR CUTOUT, FWD UPPER CORNER APPROX STA 310 TO 318, CORNER OF DOOR AND PROCEEDS FWD TO APPROX STA 303 AREA. REPAIRED PER EA 7-5330-25765 DATED 9-18-95. 2L73 4F A3WE 19951006001941995100600194NM 1995 10 6 95FDEA01462 119950928A5313 STRINGER BOEING727 72725C 138400HNM BS 460-484 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 FASTENERS PULLED THROUGH SIDE OF STR 24R STA 460 TO 484. REMOVED FASTENERS AND REPAIRED STR PER SRM 51-10-3. 2L73 4F A3WE 19951006001951995100600195NM 1995 10 6 95FDEA01463 119950929A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 312 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION TOP SIDE OF FLOORBEAM STA 312 LBL 35. REPAIR PER SRM 53-10-2. 2L73 4F A3WE 19951006001961995100600196NM 1995 10 6 95FDEA01464 119950930A3230 LOCK SOLENOID BOEING727 727225 1384077NM LANDING GEAR MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25469FE 21581 REPEAT WRITE UP - ON INITIAL RETRACTION, GEAR WOULD NOT COME UP, SEVERAL ATTEMPTS WITH NO SUCCESS. RED TAB CHECKLIST RAN, LANDING GEAR LEVER LATCH FAILED TO RELEASE RESULTING IN LATCH BEING RAISED, AND GEAR RETRACTED. FOUND LANDING GEAR CONTROL LEVER LOCK SOLENOID BAD. REMOVED AND REPLACED LOCK SOLENOID PER MM 32-31-16, CHECKS NORMAL. ALSO, RAN GEAR RETRACTION AND EXTENSION WHILE A/C ON JACKS, OPS GOOD. 2L73 4F A3WE 19951006001971995100600197NM 1995 10 6 95FDEA01465 119950930A3230656021123 ACCESSORY UNIT BOEING727 727233 138408ANM LANDING GEAR FAILED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25263FE 21625 LANDING GEAR WON'T RETRACT. TROUBLESHOT IAW MM 33-31-11 PG 101 AND 501. TRACED PROBLEM TO LANDING GEAR ACCESSORY UNIT. REMOVED AND REPLACED MLG ACCESSORY UNIT, OPS CHECKED GOOD AS PER MM. 2L73 4F RTA3WE 19951006001981995100600198WP 1995 10 6 95FDEA01466 119950930A5400 SPAR WEB DOUG DC10 DC1010F 3022111WP NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568054 47808 THE NR 1 PYLON CENTER SPAR WEB WAS FOUND CRACKED. CRACK EMANATED FROM LAST LIGHTENING HOLE DIAGONALLY TO THE I/B AFT CORNER ATTACH BOLT HOLE, CRACK TERMINATES AT EXISTING FASTENER HOLE. FABRICATED AND INSTALLED REPAIR PER SRM 54-00-01 PAGE 11. 2L73 4F A22WE 19951006001991995100600199WP 1995 10 6 ABXA9500750 119950929A291023722886 O-RINGS DOUG DC8 DC862 3021970WP HYD FILTER LEAKING A ABXAO OTHER K FLUID LOSS CRCRUISE 1 GL23802AX 46134 GENERAL HYDRAULIC SYSTEM FLUID QUANTITY BEGAN DECREASING IN FLIGHT. ACCOMPLISHED HYDRAULIC PRESSURE OR FLUID LOSS CHECKLIST. DURING APPROACH WITH AUX PUMP ON, QUANTITY STOPPED DECREASING HALFWAY BETWEEN FULL AND STANDPIPE. NO FURTHER FLUID LOSS WAS NOTED. REPLACED LEFT AILERON HYDRAULIC SYSTEM FILTER O-RINGS IAW DC8 MM CHAPTER 29. DURING ENGINE GROUND RUN, LEAK CHECK WAS GOOD. 2L74 4F 4A25 19951006002001995100600200 1995 10 6 DHL95801006 419950928A34525222703011 TRANSPONDER DOUG DC8 DC873F 302199FWP E/E BAY INOPERATIVE A TDHLAJA DUMP FUEL UNSCHED LANDING O OTHER CRCRUISE 1 SO01801DH 46033 BRU - AFTER TAKEOFF, TRANSPONDER WAS REPORTED AS INOP BY ATC. REMOVED AND REPLACED ATC TRANSPONDER RT AND CONTROL HEAD IAW MM 34-53-0, OPS CHECK OK. 2L74 4F RT4A25 19951006002011995100600201EU 1995 10 6 DL31L953866 119950930A3610 FLEX LINE 10828071 AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 2 ENGINE BLOWN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11837AB 674 717728 DURING CLIMBOUT, NR 2 ENG BLEED TEMP INCREASED TO 260 DEGREES CELSIUS. BLEED VALVE CLOSED AND FAULTED, DID NOT RESET AND RETURNED TO JFK. FOUND FLEX LINE TO FAN AIR VALVE BLOWN. REPLACED LINE, OPERATION NORMAL. 2L72 4F RTA35EU E24NE 19951006002021995100600202NM 1995 10 6 DL72E953854 119950929A3350RPS1 EEL POWER SUPPLY BOEING727 727247 138408FNM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112824W 21329 FLOOR EMERGENCY EXIT LIGHTS INOP AFT OF ROW 26. FOUND PWR SUPPLY BAD FOR AFT EMERGENCY TRACK LIGHTING. REPLACED SAME EMERGENCY LIGHTS, NOW TEST NORMAL. 2L73 4F A3WE 19951006002031995100600203NM 1995 10 6 DL72L953875 119950927A5320 WEB BOEING727 727232 1384082NM BS 1225 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 DURING CV2 CHECK, FOUND .25 INCH CRACK AT LIGHTNING HOLE, INBD VERT WEB RT STA 1225. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19951006002041995100600204NM 1995 10 6 DL72S953836 119950927A5320 WEB BOEING727 727232 1384082NM BS 1323 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11535DA 22048 DURING B-1 LTR CHECK, FOUND 48 SEC TORQUE BOX WEB IS CRACKED AT LIGHTENING HOLE, STA 1323 LT. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951006002051995100600205NM 1995 10 6 DL72S953847 119950928A5753 LE SKIN 652163383 BOEING727 727232 1384082NM NR 1 TE MIDFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA DL10 21431 DURING SHOP INSPECTION, NR 1 MIDFLAP L/E SKIN WAS FOUND WITH WEAR DAMAGE AT THE O/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 803. 2L73 4F A3WE 19951006002061995100600206NM 1995 10 6 DL72S953855 119950821A5753652163261 SPAR BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 DURING SHOP INSPECTION, NR 2 MIDFLAP HAS A CRACKED AFT SPAR CHORD 22 FT AND 53 FROM I/B END OF FLAP AND A CRACK AT I/B ACTUATOR CUTOUT. SPLICED IN NEW SECTIONS OF AFT SPAR CHORD AND INSTALLED DOUBLERS, PER MM 57-52-00 PG 807. 2L73 4F A3WE 19951006002071995100600207NM 1995 10 6 DL72S953858 119950929A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING F-1 LETTER CHECK, FOUND NR 7 L/E SLAT COVE SKIN ANGLE CRACKED BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19951006002081995100600208NM 1995 10 6 DL72S953859 119950929A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING F-1 LETTER CHECK, FOUND NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19951006002091995100600209NM 1995 10 6 DL72S953872 119950920A3221 ATTACH MOUNT BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 NOSE LANDING GEAR LEFT ATTACH MOUNT CORRODED. CLEANED BOLT HOLES, MACHINED BORE TO 2.617, REMOVED CORROSION AND ROTOPEENED. TREATED, MANUFACTURED BUSHINGS, CAD BUSHING AND INSTALLED BUSHINGS PER MM 53-40-0. 2L73 4F A3WE 19951006002101995100600210NM 1995 10 6 DL72S953873 119950921A3221 TRUNNION BOEING727 727232 1384082NM NLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 NOSE GEAR RT TRUNNION BORE CORRODED. CLEANED ATTACH BOLT HOLES, MACHINED BORE TO 2.525 TO REMOVE CORROSION. ROTOPEENED, TREATED, PRIMED, MFG BUSHINGS AND INSTALLED BUSHINGS PER MM 53-40-0. 2L73 4F A3WE 19951006002111995100600211NM 1995 10 6 DL72S953874 119950921A3211 FITTING BOEING727 727232 1384082NM RT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 RT MLG FWD TRUNNION FITTING INSIDE FACES CORRODED. ALSO, EVIDENCE OF CORROSION UNDER BUSHINGS. REMOVED BUSHINGS AND CORROSION, BORED HOLES, SPOTFACED HOLES WITHIN MM 57-43-0 LIMITS. MACHINED LOWER O/B BUSHINGS PER DRAWING NR 69-49502-7 AND MM 57-43-0 PG 403 NR 2. CADPLATED, ROTOPEENED, TREATED, PRIMED, INSTALLED BUSHINGS. MANUFACTURED, TREATED AND INSTALLED FILLERS. APPLIED TOP COAT, BMS 3-23 AND BMS 3-26 PER PS 900-2 NR 4. 2L73 4F A3WE 19951006002121995100600212NM 1995 10 6 DL72W953842 119950928A3350900835A EEL PACK BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112821W 21059 RIGHT FWD OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK NORMAL. 2L73 4F A3WE 19951006002131995100600213NM 1995 10 6 DL757953849 119950928A5754 TE WEDGE 114N4004165ABOEING757 757232 1384965NM NR 3 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11605DL A10157 22812 DURING A SHOP INSPECTION, THE TRAILING EDGE WEDGE WAS FOUND TO BE DELAMINATED. A NEW WEDGE WAS INSTALLED PER SRM 57-42-02, ON NR 3 L/E SLAP PANEL. 2L72 4F RTA2NM 19951006002141995100600214NM 1995 10 6 DL757953857 119950929A335020131A EEL BATTERY PACK BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11649DL 24389 R1 EXIT SIGN AND SLIDE LIGHT WERE INOP. REPLACED BATTERY PACK. 2L72 4F RTA2NM 19951006002151995100600215WP 1995 10 6 DLL10953851 119950928A3350 EEL POWER PACK 516574 LKHEED1011 10113851 5265010WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11720DA 37740 193C1136 DURING L/O CK, FOUND EMERGENCY LIGHTS OUT AT MID GALLEY, CROSS AISLE. REPLACED POWER PACK PS9. 2L73 4F A23WE 19951006002161995100600216NE 1995 10 6 DLL10953861 219950928A7260 GEARBOX M06157 LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 3 ENGINE FAILED A DALAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO11727DA AM619 193C1167 10360 ENGINE NR 3 FLAMED-OUT AT FLIGHT LEVEL 370, WINDMILL AT N3 26 PERCENT. ATTEMPTED RELIGHT, ENGINE LIGHT OFF. THROTTLE MOVEMENT HAD NO EFFECT ON EPR, TGT, N1, N2, N3 AS IF FUEL CONTROL HAD LET GO. REPLACED MAIN GEARBOX DUE TO INTERNAL FAILURE. 2L73 4F4 F A23WE A12EU 19951006002171995100600217NM 1995 10 6 DLM11953869 119950930A3350CM77839 EEL BULB DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11803DE 48474 SEVERAL EMERGENCY FLOOR TRACK LIGHTS ARE NOT LIGHTING UP. RELAMPED LIGHTS, CKS GOOD. 2L73 4F RTA22WE 19951006002181995100600218NM 1995 10 6 P5CA0900794 119950929A5320 DRAIN PANEL BOEING747 747121 1384871NM FWD LAV CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 FOUND CORRODED WASHERS, WHICH ARE BULGING SKIN AT FORWARD LAV SERVICE PANEL DRAIN CUTOUT. REPLACED CORRODED WASHERS IAW SRM 51-10-01 AND REPAIRED PANEL IAW SRM 51-10-01. 2L74 4F A20WE 19951006002191995100600219NM 1995 10 6 P5CA9500791 119950929A5522 TE SKIN BOEING747 747121 1384871NM LT ELEVATOR DEBONDED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 DEBONDED ELEVATOR, LEFT HAND INBOARD ELEV TRAILING EDGE. REPAIRED WITH POTTING COMPOUND AND FIBERGLASS OVERLAY IAW SRM 51-41-00. PRIMED AND PAINTED IAW SRM 51-24-11. 2L74 4F A20WE 19951006002201995100600220NM 1995 10 6 P5CA9500792 119950929A498065B987051 LINER BOEING747 747121 1384871NM APU CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 CRACKED APU EXHAUST PIPE INNER LINER. REMOVED AND REPLACED LINER IAW MM 49-81-03. 2L74 4F A20WE 19951006002211995100600221NM 1995 10 6 P5CA9500793 119950929A323165B733247 CLEVIS ASSY BOEING747 747121 1384871NM LT MLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 LANDING GEAR DOOR FITTING BROKEN AND CRACKED. REMOVED AND REPLACED CLEVIS ASSEMBLY ON LEFT HAND MAIN BODY GEAR OUTBOARD DOOR IAW MM 20-11-27. 2L74 4F A20WE 19951006002221995100600222NM 1995 10 6 P5CA9500795 119950929A7110 FAN COWL BOEING747 747121 1384871NM NR 2 ENGINE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 DELAMINATION AND PUNCTURE OF NR 2 ENGINE RIGHT FAN COWL. REPAIRED IAW SRM 51-40-06. 2L74 4F A20WE 19951006002231995100600223NM 1995 10 6 P5CA9500796 119950929A5280 DOOR BOEING747 747121 1384871NM LT MLG PUNCTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 PUNCTURED LEFT HAND WING GEAR, LOWER OUTBOARD FLYING DOOR INNER SKIN. REPAIRED AND PAINTED AREA IAW SRM 51-40-15. 2L74 4F A20WE 19951006002241995100600224NM 1995 10 6 P5CA9500797 119950929A5242 SKIN BOEING747 747121 1384871NM E/E DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 SURFACE CORROSION OF CENTER E AND E DOOR INNER SKIN. REMOVED SURFACE CORROSION WITH NEGLIGIBLE MATERIAL LOSS AND REPAIRED IAW 51-10-01. 2L74 4F A20WE 19951006002251995100600225NM 1995 10 6 P5CA9500798 119950929A5242 FAIRING BOEING747 747121 1384871NM E/E DOOR BULGING A P5CAK NONE O OTHER ININSP/MAINT 1 WP23832FT 20347 BULGING FAIRING BEHIND CTR E AND E DOOR. REMOVED FAIRING AND FOUND SHIM MISSING. INSTALLED SHIM AND INSTALLED FAIRING IAW SRM 51-30-02. 2L74 4F A20WE 19951006002261995100600226NM 1995 10 6 P5CA9500799 119950928A528065B101543 HINGE BOEING747 747122 1384872NM RT MLG DOOR BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23854FT 19754 DURING WALK-AROUND, FOUND RIGHT HAND FORWARD MAIN GEAR DOOR FORWARD UPPER HINGE BROKEN. REPLACED UPPER HINGE HALF IAW MM 32-12-00. 2L74 4F A20WE 19951006002271995100600227NE 1995 10 6 P5CA9500800 219950930A7200 ENGINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 FAILED A P5CAEA ENGINE SHUTDOWN UNSCHED LANDING JY WARNING INDICATION ENGINE STOPPAGE CRCRUISE 1 WP23851FT 19756 662964 THE NR 3 OIL PRESS LIGHT CAME ON, CONFIRMED OIL PRESS LOSS BELOW 40 PSI, SHUTDOWN ENGINE. REPLACED ENGINE IAW POLAR WORK CARD M7100-002A. 2L74 4F4 F A20WE E20EA 19951006002281995100600228NE 1995 10 6 SWAA950649 219950924A7310629198 FUEL LINE BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 2 RUPTURED A SWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW0795SW 23054 DURING TAKEOFF ROLL APPROACHING 60 KNOTS, EXPERIENCED NUMBER 2 ENGINE POWER DROP. ABORTED TAKEOFF AND RETURNED TO GATE. INSPECTED AND REPLACED FUEL SUPPLY LINE FROM P AND D VALVE TO RIGHT NOZZLE. OPS AND LEAK CHECKED OK PER BOEING M/M. 2L72 4F4 F A16WE E2EA 19951006002291995100600229NE 1995 10 6 SWAA950650 219950916A7261 SEAL BOEING737 7373H4 1384600NM GE CFM56 CFM563B1 13802NE NR 1 FAILED A SWAAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SW07342SW 24133 EXPERIENCED NUMBER 1 ENGINE OIL PRESSURE DROP AND THE CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT LANDED AT AMA WITHOUT INCIDENT. REPLACED OIL SEAL, LEAK CHECKED AND PERFORMED POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F4 FRTA16WE E2GL 19951006002301995100600230NM 1995 10 6 UPS204578 119950927A33501000677 EEL BATTERY PACK BOEING727 72725C 138400HNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01933UP 19857 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT BATTERY PACK DIM. REMOVED AND REPLACED BATTERY LIGHT PACK. 2L73 4F A3WE 19951006002311995100600231NM 1995 10 6 UPS204579 119950927A5755 TE SKIN BOEING727 72725C 138400HNM NR 6 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01931UP 19858 WHILE ON GROUND, MAINTENANCE FOUND NR 6 SPOILER LT WING DELAMINATED ON TRAILING EDGE. REMOVED AND REPLACED NR 6 GROUND SPOILER (P/N 65-17348-108A) (S/N 5758) ON, (P/N 65-17348-55) (S/N 6307) OFF. 2L73 4F A3WE 19951006002321995100600232NM 1995 10 6 UPS204581 119950929A572065185385 UPPER CHORD BOEING727 727185C 138406NNM WS 870 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON 870 UPPER CHORD, LBL 35 AND RBL 25 WL 190. REMOVED AND REPLACED IAW EO B727-5710-7412A. 2L73 4F A3WE 19951006002331995100600233NM 1995 10 6 UPS204582 119950929A53207075T6 BRACKET BOEING727 727185C 138406NNM BS 344 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BROKEN CHANNEL SUPPORT BRACKET, STA 344 RBL 53 WL 207, UNDER HAT CHANNEL. REMOVED AND REPLACED CRACKED HAT CHANNEL SUPPORT BRACKET PER SRM 51-30-2, 51-20-1, 51-10-02 AND 51-20-04. 2L73 4F A3WE 19951006002341995100600234NM 1995 10 6 UPS204583 119950929A575165212919 TE WEDGE BOEING727 727185C 138406NNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01954UP 19827 WHILE IN FOR C CHECK MAINTENANCE FOUND RT WING OUTBOARD AILERON TRAILING EDGE WEDGE HAS WATER CONTAMINATION, IS CORRODED AND HAS A PREVIOUS REPAIR IS DELAMINATED. REMOVED AND INSTALLED NEW WEDGE IAW SRM 51-80-1, 51-80-4, 51-80-6 MM 27-10-41 ANS SRM 51-30-2. 2L73 4F A3WE 19951006002351995100600235NM 1995 10 6 UPS204584 119950929A5315 FLOORBEAM BOEING727 727108C 1384039NM BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK MAINTENANCE FOUND CORROSION ON UPPER CHORD OF FLOOR BEAM BS 680, RBL 10, 16, 59. TRIMMED OUT UPPER CHORD FROM RBL 12 TO RBL 70 AND SPLICED IN NEW CHORD SECTION IAW 727 SRM 53-10-8. 2L73 4F A3WE 19951006002361995100600236NM 1995 10 6 UPS204585 119950929A53157075T6 FLOORBEAM BOEING727 727108C 1384039NM BS 640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK MAINTENANCE FOUND CORROSION (C53-224-06.00-01) ON BEAM UNDER NUT PLATE AT BS 640, LBL 47, WL 208. REMOVED CORROSION BY BLENDING, FABRICATED STRAP AND DOUBLER FINAL REPAIRS PER SRM 51-10-6, 51-10-2, 51-10-1 AND EO 727-53-1668. 2L73 4F A3WE 19951006002371995100600237NM 1995 10 6 UPS204586 119950929A5313BAC1493213 STRINGER BOEING727 727108C 1384039NM BS 323 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.00-01), STR 4L STA 323, 344 TO 348. REPAIR WAS MADE. 2L73 4F A3WE 19951006002381995100600238NM 1995 10 6 UPS204587 119950929A53157075T6 FLOORBEAM BOEING727 727108C 1384039NM BS 400 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01), ON FLOORBEAM STA 400 RBL 25 TO RBL 60 WL 208, LOWER SIDE OF UPPER CHORD. REMOVED CORROSION, FOUND OUT OF LIMIT, REMOVED DAMAGE AREA, FABRICATED T-CHORD. FINAL INSTALLATION PER SRM 53-10-8, 53-30-2, 51-10-6 AND 53-10-1. 2L73 4F A3WE 19951006002391995100600239NM 1995 10 6 UPS204588 119950929A575465162267B SKIN BOEING727 727108C 1384039NM NR 2 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND AND REPLACED NR 2 K-FLAP DUE TO CONDITION AND CORROSION. THE NR 2 K-FLAP WAS FOUND TO BE CORRODED OUT OF LIMITS. REPLACED NR 2 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19951006002401995100600240NM 1995 10 6 UPS204589 119950929A5754202473 BOLT BOEING727 727108C 1384039NM NR 5 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 5 SLAT IS CRACKED AT O/B GUIDE HOOK, UPPER ATTACH BOLT. REPAIRED NR 5 SLAT PER SRM 57-50-03. 2L73 4F A3WE 19951006002411995100600241NM 1995 10 6 UPS204590 119950929A575465162268A FLAP BOEING727 727108C 1384039NM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP. REPLACED NR 5 K-FLAP PER MM 27-81-01. 2L73 4F A3WE 19951006002421995100600242NM 1995 10 6 UPS204591 119950929A5753652466858 TE WEDGE BOEING727 727108C 1384039NM RT TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND RT WING, I/B MIDFLAP T/E WEDGE SPAR CORROSION. REPLACED RT WING, I/B MIDFLAP T/E WEDGE PER SRM 51-10-1, 51-30-2. 2L73 4F A3WE 19951006002431995100600243NM 1995 10 6 UPS204592 119950929A5754 RIB BOEING727 727108C 1384039NM NR 4 LE SLAT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 4 SLAT RIB CRACKED AT SLAT STA 48.25. REPAIRED RIB IAW 727 SRM 57-50-3. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER. 2L73 4F A3WE 19951006002441995100600244NM 1995 10 6 UPS204593 119950929A5743651929613 TRUNION FITTING BOEING727 727108C 1384039NM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON INNER SURFACE OF ATTACH FITTING, AROUND HOLES WHERE BEARING SUPPORT MATES, FWD TRUNNION. REPLACED TRUNNION FITTING PER SRM 51-30-2, 51-10-2, 51-20-4. 2L73 4F A3WE 19951006002451995100600245NM 1995 10 6 UPS204594 119950929A5343 TRUNNION FTGS BOEING727 727108C 1384039NM NLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LEFT AND RIGHT NOSE LANDING GEAR TRUNNION FITTINGS CORRODED BEYOND LIMITS. REMOVED AND REPLACED LEFT AND RIGHT NLG TRUNNION FITTINGS AND STIFFENERS IAW UPS EO B727-5310-3954B AND BOEING REPAIR DRAWING 65-88189. 2L73 4F A3WE 19951006002461995100600246NM 1995 10 6 UPS204595 119950929A532065956001723 CHORD BOEING727 727108C 1384039NM BS 740 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AND CRACKS ON 740 CHORD RBL 45 WL 200. REMOVED CORROSION AND REPAIRED PER EO B727-5710-7409A. 2L73 4F A3WE 19951006002471995100600247NM 1995 10 6 UPS204596 119950929A53212024T3 FLOOR BOEING727 727108C 1384039NM RT DOGHOUSE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND UPON REMOVAL OF LT AND RT DOGHOUSE FLOORS, BOTH LT AND RT HAND FLOORS HAVE NUMEROUS CRACKS. INSTALLED FABRICATED FLOOR REPAIRS PER SRM 51-20-1, 51-40-2, 51-30-2. 2L73 4F A3WE 19951006002481995100600248NM 1995 10 6 UPS204597 119950929A53157075T6 FLOORBEAM BOEING727 727108C 1384039NM BS 380 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01), ON FLOORBEAM AROUND NUTPLATE HOLES LOWER AFT SIDE OF UPPER CHORD STA 380 RBL 55 TO 58 WL 208. REPAIRED FLOORBEAM PER UPS EO B727-5310-7415-A. 2L73 4F A3WE 19951006002491995100600249NM 1995 10 6 UPS204598 119950929A5320 SILL BOEING727 727108C 1384039NM CARGO DOOR CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON MAIN CARGO DOOR INTERNAL THRESHOLD STA 620 LBL 67 WL 208 LOWER SIDE OF SHEAR WEB. BLENDED OUT CORROSION, INSTALLED NUTPLATE DOUBLER IAW EO 727-53-1675. 2L73 4F A3WE 19951006002501995100600250NM 1995 10 6 UPS204599 119950929A553165174301 RIB BOEING727 727108C 1384039NM ELEV STA 50.05 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT HORIZ STAB NR 2 T/E SUPPORT RIB, AT ELEV STA 50.05 IS CRACKED ON LOWER SURFACE. REPLACED CRACKED SUPPORT RIB PER SRM 51-30-2, 51-30-5, 51-10-2. 2L73 4F A3WE 19951006002511995100600251NM 1995 10 6 UPS204600 119950929A574465999091664 SUPPORT BOEING727 727108C 1384039NM LT TE MIDFLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT WING I/B MIDFLAP I/B ACTUATING CABLE PULLEY GOUGED. PULLEY SUPPORT FITTING ASSY CORRODED EXTENSIVELY. REPLACED PULLEY SUPPORT ASSY IAW OHM 20-50-03, 57-52-01. 2L73 4F A3WE 19951006002521995100600252NM 1995 10 6 UPS204601 119950929A5315 FLOORBEAM BOEING727 727108C 1384039NM BS 560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION FORWARD CARGO BAY IN NUTPLATE HOLES IN THE LOWER FLANGE OF THE 560 FLOORBEAM RBL 5 TO RBL 58 WL 201. BLENDED CORROSION IAW 727-53-1669. 2L73 4F A3WE 19951006002531995100600253NM 1995 10 6 UPS204602 119950929A5313 STRINGER BOEING727 727108C 1384039NM BS 618-164 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01-68-01), ON AND AROUND FASTENERS ON STRINGER 4R STA 618 TO 624. REPAIRED STRINGER PER SRM 53-10-1, 53-10-3, 51-10-2, 53-10-4, 51-30-2 AND MM 51-20-151. 2L73 4F A3WE 19951006002541995100600254NM 1995 10 6 UPS204603 119950929A5315 FLOORBEAM BOEING727 727108C 1384039NM BS 1130 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION AROUND NUTPLATE HOLES BS 1130, RBL 25 TO 45 WL 208, FLOORBEAM JUST FORWARD OF PRESSURE WEB. BLENDED OUT CORROSION IAW 727 SRM 51-10-6. 2L73 4F A3WE 19951006002551995100600255NM 1995 10 6 UPS204604 119950929A5320 FITTING BOEING727 727108C 1384039NM TIE RIB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON AFT VERTICAL BOLT HOLE FLANGE LOWER SURFACE ON TENSION TIE RIB. REMOVED CORROSION AND INSTALLED DNW BUSHINGS PER 51-10-6. 2L73 4F A3WE 19951006002561995100600256NM 1995 10 6 UPS204605 119950929A5320 FITTING BOEING727 727108C 1384039NM TIE RIB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN AFT VERTICAL BOLT HOLES, AT TENSION TIE SHEAR FITTING. REMOVED CORROSION, REMOVED AND REPLACED BUSHINGS PER SRM 51-10-6 EO 727-55-0294. 2L73 4F A3WE 19951006002571995100600257NM 1995 10 6 UPS204606 119950929A5755651734862 PANEL BOEING727 727108C 1384039NM NR 8 SPOILER CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 8 SPOILER HAS WATER CONTAMINATION. REPLACED NR 8 SPOILER PANEL WITH NEW PANEL PER MM 27-62-01. 2L73 4F A3WE 19951006002581995100600258NM 1995 10 6 UPS204607 119950929A57556517347 CORE BOEING727 727108C 1384039NM NR 14 SPOILER CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 14 SPOILER HAS WATER CONTAMINATION INTERNAL AND CORE DAMAGE. REPAIRED SPOILER PER SRM 51-40-6. 2L73 4F A3WE 19951006002591995100600259NM 1995 10 6 UPS204608 119950929A5755651734748 CORE BOEING727 727108C 1384039NM NR 12 SPOILER CONTAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND NR 12 SPOILER HAS WATER CONTAMINATION INTERNAL. REPAIRED SPOILER PER SRM 51-40-06. 2L73 4F A3WE 19951006002601995100600260NM 1995 10 6 UPS204609 119950929A5533651678719 FITTING BOEING727 727108C 1384039NM LT LOWER CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION LT LOWER SPLICE BEAM UPPER AND LOWER SHEAR FITTINGS. REPLACED PER SRM 51-30-2, MM 51-20-21, 51-20-00, 51-20-21. 2L73 4F A3WE 19951006002611995100600261NM 1995 10 6 UPS204646 119951001A5753 TE SKIN BOEING727 72730C 1384009NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01917UP 19310 WHILE ON GROUND MAINTENANCE, FOUND LEFT INBD FLAP TRAILING EDGE HAS DELAMINATION. REPAIRED TRAILING EDGE FLAP PER SRM 727-51-40-6. 2L73 4F A3WE 19951006002621995100600262WP 1995 10 6 UPS804580 119950927A33505708458503 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01801UP 46101 WHILE ON GROUND, MAINTENANCE FOUND ON F/E'S PREFLIGHT EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK, CKS OK. ON (S/N FTL 008), OFF (S/N 107) (P/N 5708458-503). 2L74 4F RT4A25 19951006002631995100600263WP 1995 10 6 UPS804610 119951002A5313975491333N LONGERON DOUG DC8 DC873F 302199FWP FS 220-320 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 36, LT AND RT SIDES CRACKED AT FS 220 TO 320. REPLACED LONGERON SECTION PER SRM 51-1-20D. 2L74 4F RT4A25 19951006002641995100600264WP 1995 10 6 UPS804611 119950929A53205753133502N FITTING DOUG DC8 DC873F 302199FWP FS 920 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 920. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006002651995100600265WP 1995 10 6 UPS804612 119951002A532036471171 FITTING DOUG DC8 DC873F 302199FWP FS 960 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 960. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006002661995100600266WP 1995 10 6 UPS804613 119951002A532036410042N FITTING DOUG DC8 DC873F 302199FWP FS 879 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 879. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006002671995100600267WP 1995 10 6 UPS804614 119951002A532036469562N FITTING DOUG DC8 DC873F 302199FWP FS 940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON 24R, BATH TUB FITTING CRACKED AT FS 940. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006002681995100600268WP 1995 10 6 UPS804616 119951002A5511 RIB DOUG DC8 DC871F 302199DWP HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND I/B RIB CRACKED ON I/B LEADING EDGE OF RT HORIZ STAB. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 55-2-0. 2L74 4F RT4A25 19951006002691995100600269WP 1995 10 6 UPS804617 119951002A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 442.185 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT STA XS 442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACK IAW SRM 57-2-0. 2L74 4F RT4A25 19951006002701995100600270WP 1995 10 6 UPS804618 119951002A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 448.581 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT STA XS 448.581 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACKED IAW SRM 51-2-0. 2L74 4F RT4A25 19951006002711995100600271WP 1995 10 6 UPS804619 119951002A5512 SKIN DOUG DC8 DC871F 302199DWP RT HORZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SKIN CRACKED AND APPEARS TO HAVE CORROSION O/B L/E AT I/B END OF RT HORZ STAB. INSTALLED REPAIR PER SRM 55-2. 2L74 4F RT4A25 19951006002721995100600272WP 1995 10 6 UPS804620 119951002A5730 SKIN DOUG DC8 DC871F 302199DWP WS 765-766 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E LOWER SKIN STA XFS 765.0 TO 766.5 HAS EXFOLIATION AND INTERGRANULAR CORROSION. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-20, 51-1-21. 2L74 4F RT4A25 19951006002731995100600273WP 1995 10 6 UPS804621 119951002A5311 FITTING DOUG DC8 DC871F 302199DWP BS 460 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATED CORROSION ON AFT SIDE OF FRAME FITTING, LONGERON 21L STA 460. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19951006002741995100600274WP 1995 10 6 UPS804622 119951002A5712 RIB DOUG DC8 DC871F 302199DWP WS 628.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING OUTBOARD L/E RIB AT STA XFS 628.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0. 2L74 4F RT4A25 19951006002751995100600275WP 1995 10 6 UPS804623 119951002A5311 FITTING DOUG DC8 DC871F 302199DWP FS 35 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND STA 35 AT RT CUSP FRAME TO CUSP TIE FITTING HAS HEAVY CORROSION AROUND FASTENER HOLE. REMOVED AND INSTALLED NEW FITTING IAW SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 19951006002761995100600276WP 1995 10 6 UPS804624 119951002A5320 SPLICE FITTING DOUG DC8 DC871F 302199DWP BS 1270 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1270 LONG 34L, SPLICE FITTING CORRODED BEYOND LIMITS. INSTALLED NEW FITTING AT STA 1270 LONG 34L IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006002771995100600277WP 1995 10 6 UPS804625 119951002A5320 SPLICE FITTING DOUG DC8 DC871F 302199DWP BS 1270 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CORRODED BEYOND LIMITS, STA 1270 LONG 34R. REPLACED SPLICE FITTING, STA 1270 LONG 34R IAW SRM 51-2-20D. 2L74 4F RT4A25 19951006002781995100600278WP 1995 10 6 UPS804626 119951002A5320 SUPPORT DOUG DC8 DC871F 302199DWP FS 99 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND PRESSURE FLOOR SUPPORT CHORD BS 99 CORRODED BEYOND LIMITS, AT VARIOUS LOCATIONS FROM LBL 70 TO RBL 70. FABRICATED AND INSTALLED NEW CHORD PER SRM 51-1-21. 2L74 4F RT4A25 19951006002791995100600279WP 1995 10 6 UPS804627 119951002A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1160 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING AT FRAME 1160, WHERE IT ATTACHES TO THE CUSP LT SIDE HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D. 2L74 4F RT4A25 19951006002801995100600280WP 1995 10 6 UPS804628 119951002A5311 FRAME DOUG DC8 DC871F 302199DWP BS 220 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATION CORROSION ON LWR FLANGE OF FRAME STA 200 LONG 35L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER DC8 SRM 53-2-0. TREATED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER DC8 SRM 53-2-0, 53-2-0 FIG 2 AND 51-1-21. 2L74 4F RT4A25 19951006002811995100600281WP 1995 10 6 UPS804629 119951002A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 45-65 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT FS 45 TO 65 RBL 16 TO 24, FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED AND FABRICATED FINGER DOUBLER IAW SRM 53-3-1 AND INSTALLED PER SRM 51-1-21. 2L74 4F RT4A25 19951006002821995100600282WP 1995 10 6 UPS804630 119951002A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 25-45 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT FS 25 TO 45 RBL 16 TO 24, FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED AND FABRICATED NEW FINGER DOUBLER IAW SRM 53-3-1 AND 53-1-0, INSTALLED DOUBLER IAW SRM 51-2-21. 2L74 4F RT4A25 19951006002831995100600283WP 1995 10 6 UPS804631 119951002A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 420 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34L STA 420. INSTALLED REPLACEMENT LONGERON PER SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006002841995100600284WP 1995 10 6 UPS804644 119951002A5330 SKIN DOUG DC8 DC873F 302199FWP FS 335 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND THE AFT LOWER CORNER OF THE A-CROSS SLIDE DOOR CUTOUT HAS CRACK DAMAGE. REPAIRED PER UPS EO DC8-5310-7439-A. 2L74 4F RT4A25 19951006002851995100600285WP 1995 10 6 UPS804645 119951002A53205772850 ANGLE DOUG DC8 DC873F 302199FWP FS 380 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE AT DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 380 BELT FRAME FLOOR SUPPORT ANGLE CRACKED AT LONGERON 33R. WELDED CRACK PER UPS 10225. 2L74 4F RT4A25 19951006002871995100600287SW 1995 10 6 95ZZZX5457 119950830A6230206010335001 LEVER ASSY 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW031075Y 273 45378 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. WORN PARTS TT, 272.7. 1G71 3U H2SW 19951006002881995100600288SW 1995 10 6 95ZZZX5458 119950830A6230206010336005 LINK IDLER 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW031075Y 273 45378 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH, 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. WORN PARTS TT, 272.7. 1G71 3U H2SW 19951006003031995100600303GL 1995 10 6 95ZZZX5473 219950724A72306896888 SCROLL 23005250 BELL 206 206L3 1182108SW ALLSN 250C 250C30P 03013GL FORWARD SIDE FOREIGN OBJECT B ALGRK NONE O OTHER ININSP/MAINT 1 SW03359AL 367 AP23328 51461 CAE895538 UPON AIR LOGISTICS BORESCOPE INSPECTION, FOUND CERAMIC BEAD LODGED IN AIR SLOT ON INTERNAL PART OF SCROLL. 1G71 3U3 U H2SW E1GL 19951006003501995100600350NE 1995 10 6 9514926627 219950929A7532 BLEED VALVE 7880461 BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE MALFUNCTIONED A NWAAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 GL01627US 13376 21709 702029 DURING CLIMB, THE NR 3 ENGINE NACELLE TEMPERATURE PEAKED AND THE ENGINE FIRE WARNING ACTIVATED. THE ENGINE WAS SHUTDOWN, THE FIRE BOTTLES WERE DISCHARGED, AND THE AIRCRAFT RETURNED TO NRT WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. THE HIGH STAGE BLEED VALVE AND CONTROLLER WERE REPLACED AND A RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19951006003511995100600351NE 1995 10 6 9514933231 219950928A7200 ENGINES AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE LT/RT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01331NW 318 DURING TAKEOFF ROLL, THE ENGINES WERE NOT ACCELERATING EVENLY. TAKEOFF WAS ABORTED AT APPROXIMATELY 10 TO 15 KNOTS. MAINTENANCE INSPECTION REVEALED NO DISCREPANCIES. ENGINES OPERATIONAL CHECK OK. 2L72 4F4 FRTA28NM E29NE 19951006003521995100600352WP 1995 10 6 9514949310 119950924A3260 SENSOR DOUG DC9 DC982 3022082WP LT MLG DOOR LOOSE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01313RC 48091 MSP - DURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. CONTINUED FLIGHT TO SMF AND UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES FOR LANDING. RIGHT GEAR DOOR WAS DAMAGED DURING LANDING ROLL AND FOUND LEFT MAIN GEAR DOOR SENSOR FASTENER MISSING. INSTALLED FASTENER, REPLACED RIGHT MAIN GEAR DOOR AND LEFT MAIN GEAR DOOR SKID PLATE. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006003531995100600353WP 1995 10 6 9514959973 119951001A7711 EPR IND/TRANS DOUG DC9 DC931 3022065WP LT ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL019337 47346 DURING TAKEOFF ROLL, LEFT ENGINE EPR WAS FROZEN AT 1.6 TO 1.7. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED LEFT ENGINE EPR INDICATOR AND TRANSMITTER. OPERATIONAL CHECK OK ON ENGINE RUN AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006003541995100600354 1995 10 6 9514969973 219951001A7320 PT7 TUBE DOUG DC9 DC931 3022065WP LT ENGINE BROKEN A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL019337 47346 DURING TAKEOFF ROLL, LEFT ENGINE EPR DECAYED TO APPROXIMATELY 1.6. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED BROKEN PT7 LINE ON LEFT ENGINE. OPERATIONAL CHECK OK ON ENGINE RUN AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006003551995100600355WP 1995 10 6 9514971153 119951001A3620 PNEU IND LOOP DOUG DC10 DC1040 3023508WP NR 2 FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CRCRUISE 1 GL01153US 46762 DURING CRUISE, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO HNL. FOUND THE NR 2 LOOP BAD, DEFERRED PER MEL 36-10A. 2L73 4F A22WE 19951006003561995100600356NM 1995 10 6 95FDEA01467 119950925A53207075T6 FAIL-SAFE CHORD BOEING727 727232 1384082NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21018 CORROSION FWD BAY ON TOP SIDE OF BS 740 FAIL-SAFE CHORD LBL 9 TO LBL 14. ALSO, 4 FASTENERS UNDERSIDE, 2 AT STR 27L AND 2 AT STR 27R, ACCESS IS REQUIRED. REMOVED CORROSION ON FAIL-SAFE CHORD BS 740 FROM LBL 18 RBL 16, FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED REPAIR PARTS, DRILLED, ALODINED, PRIMED AND INSTALLED IAW FEDEX EA 7-5310-25785. 2L73 4F A3WE 19951006003571995100600357NM 1995 10 6 95FDEA01468 119950925A532069648411 GUSSET BOEING727 727232 1384082NM BS 740 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25499FE 21019 CORROSION FWD BAY ON PRESS GUSSET AT BS 740 AT KEEL BEAM, STR 28R WL 145. REMOVED CORROSION FROM PRESS GUSSET AT BS 740 STR 28R AND FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED GUSSET AND INSTALLED NEW GUSSET, BS 740 STR 28R. FUNCTIONAL CHECK PER MM FEDEX 21-56-0, 28-22-0 AND 27-82-31. 2L73 4F A3WE 19951006003581995100600358NM 1995 10 6 95FDEA01469 119951002A53117075T6 FRAME BOEING727 727227 1384078NM BS 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FRAME BENT AND CRACKED AT BS 500 STR 25L. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-03. 2L73 4F A3WE 19951006003591995100600359NM 1995 10 6 95FDEA01470 119951002A53117075T6 FRAME BOEING727 727225 1384077NM BS 312 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CRACKED FRAME AT BS 312 LBL 45 WL 173 NEAR STR 22L. REMOVED CRACKED FRAME AT BS 312 LBL 45 WL 173 AND INSTALLED NEW FRAME. 2L73 4F A3WE 19951006003601995100600360NM 1995 10 6 95FDEA01471 119951002A53117075T6 FRAME BOEING727 727225 1384077NM BS 700 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 FRAME DENTED AT BS 700 RBL 32 WL 160 AND CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PART, ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR PART PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951006003611995100600361NM 1995 10 6 95FDEA01472 119951002A53137075T6 STRINGER BOEING727 727225 1384077NM BS 525/528/530 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STR 3 PLACES, BS 525, 528 AND 530 LBL 15 WL 150. MECHANICALLY REMOVED CORROSION ON STR 27 BS 525 TO 530 LBL 15 WL 150, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND 53-10-0. REPAIRED STR 7 AT BS 525 TO 530 LBL 15 WL 150 PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951006003621995100600362NM 1995 10 6 95FDEA01473 119951002A53117075T6 FRAME BOEING727 72722 1384002NM BS 990 DAMAGED HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HOLE ON BS 990 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 990 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1. 2L73 4F A3WE 19951006003631995100600363NM 1995 10 6 95FDEA01474 119951002A53117075T6 FRAME BOEING727 72722 1384002NM BS 1010 DAMAGE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 HOLE ON BS 1010 RT FRAME ON THE I/B SIDE OF STR 27R IS NOT INSPECTABLE DUE TO GEOMETRIC CONFIGURATION, FIG 8 SHAPED. REPAIRED HOLE IN BS 1010 RT FRAME ON I/B SIDE OF STR 27R PER FEDEX SRM 51-40-3 FIG 1. 2L73 4F A3WE 19951006003641995100600364WP 1995 10 6 95FDEA01475 119951002A5280 GEAR DOOR DOUG DC10 DC1030F 3023504WP CTR MLG CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25305FE 47870 CENTER LINE GEAR L/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED ANGLE PER SRM 51-00-00 VOL 1 PAR 2 SEC 3. 2L73 4F RTA22WE 19951006003651995100600365WP 1995 10 6 95FDEA01476 119951002A5280 DOOR DOUG DC10 DC1030F 3023504WP CTR MLG CRACKED A FDEAK NONE O OTHER UKUNKNOWN 1 SO25305FE 47870 CENTER LINE GEAR R/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED FRAME PER SRM 51-00-00 VOL 1 PAR 2 SEC C. 2L73 4F RTA22WE 19951006003661995100600366EU 1995 10 6 95UAL900162 119951002A3230 RETRACT MECH AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE NLG MALFUNCTIONED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP29417UA 483 AT FL 330 MACH .80, EXPERIENCED A LOUD BANG WITH RED NOSE GEAR WARNING AND UNCOMMANDED NOSE GEAR EXTENSION. SLOWED AIRCRAFT AND GEAR RETRACTED. 2L72 4F RTA28NM E40NE 19951006003671995100600367WP 1995 10 6 95UAL900163 119951002A5754ARB7105501 FILLET DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 1 LE SLAT MISSING A UALAK NONE D INFLIGHT SEPARATION ININSP/MAINT 1 WP291855U 47837 ON ARRIVAL AT NRT, FOUND LEFT SLAT NR 1 DAMAGED AND FILLET MISSING. REPLACED FILLET. INSPECTED AREA AND REPAIRED MINOR DAMAGE TO SLAT. RELEASED COAT 3-8065 TO PERFORM A ONE TIME FLEET INSPECTION OF SLAT FILLET ATTACHMENTS. 2L73 4F4 F A22WE E23EA 19951006003681995100600368NM 1995 10 6 95UAL900164 119951002A2613 WIRE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE BODY OVERHEAT CHAFED A UALAK NONE N FALSE WARNING CLCLIMB 1 WP297269U 21416 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. LIGHT WENT OUT WITH ALL 3 ENGINES AT IDLE DURING DESCENT. FOUND CHAFED WIRES AT FWD DISCONNECT FOR DETECTOR M365, SEC 48 OVERHEAT DETECTOR. REPAIRED PER MM, PRESSURIZED DUCTS AND MOTORED ENGINE FOR LEAKS AND NO LEAKS FOUND. 2L73 4F4 F A3WE E2EA 19951006003691995100600369NE 1995 10 6 95UAL900165 219951002A7261 OIL QUANTITY BOEING777 777222 1385219NM PWA PW4077PW4077 NE NR 2 ENGINE DEPLETED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP29770UA 26925 777015 CREW REPORTED, NR 2 ENG OIL QTY DROPPED TO 5 QTS AND LOST 2 QTS IN A HALF HOUR. NR 2 ENGINE REDUCED TO IDLE, DIVERTED TO DORVAL, MONTREAL AND LANDED UNDER AMBER ALERT. 2L72 4F4 FRTT0001SE E46NE 19951006003701995100600370NM 1995 10 6 95UAL900166 119951002A3350 EEL INVERTER BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29524UA 24977 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW NR 9 THROUGH NR 16. REPLACED INVERTER, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951006003711995100600371NM 1995 10 6 95UAL900167 119951002A2613 OVERHEAT LOOP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE LWR AFT BODY FAILED A UALAK NONE N FALSE WARNING CLCLIMB 1 WP297269U 21416 LOWER AFT BODY HEAT LIGHT ILLUMINATED ON CLIMBOUT. LIGHT OUT WITH NR 1 THROTTLE AT IDLE AND LEFT PACK OFF. LEFT DUCT PRESSURE SHOWS 10 PSI. FOUND KEEL BEAM LOOP RESISTANCE OUT OF LIMITS. REPLACED KEEL BEAM LOOP AND TESTED PER MM, TESTED NORMAL. 2L73 4F4 F A3WE E2EA 19951006003731995100600373EU 1995 10 6 COMA951166 119951002A2450H2042C PDU SAAB SF340 SF340A 7850100EU LT DEFECTIVE A COMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO01343CA171642181 340A024 AFTER TAKEOFF, LEFT MAIN ELECTRICAL BUS FAILED. REPLACED THE LT POWER DISTRIBUTION UNIT. 2L72 4T RTA52EU 19951006003741995100600374EU 1995 10 6 COMA951168 119950929A56107256100502 WINDSHIELD SEAL SAAB SF340 SF340A 7850100EU RIGHT FAILED A COMAA UNSCHED LANDING O OTHER CRCRUISE 1 SO01356CA9606 3497 340A034 LOUD POP SOUND FOLLOWED BY HIGH AIR FLOW SOUND IN COPILOTS WINDSHIELD AREA. THE PRESSURIZATION REMAINED NORMAL. REPLACED COPILOTS WINDSHIELD BECAUSE OF DEFECTIVE SEAL. 2L72 4T RTA52EU 19951006003751995100600375SO 1995 10 6 COMA9511976 119950929A26123033515 FIRE LOOP EMB 120 EMB120RT SO NR 2 DEFECTIVE A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01463CA8663 887 120267 DURING FLIGHT, THE NR 2 FIRE DETECTOR INOP WARNING ILLUMINATED. REPLACED DEFECTIVE RT ENGINE FIRE DETECTION LOOP. 2L72 4T RTA31SO 19951006003761995100600376SO 1995 10 6 COMA9511977 119950929A27523082001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP LEAKING A COMAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 SO01156CA1133 120156 HYDRAULIC FLUID LEAKING FROM LT NACELLE FLAP AREA. REPLACED LEAKING NACELLE FLAP ACTUATOR. 2L72 4T RTA31SO 19951006003771995100600377SO 1995 10 6 COMA9511978 119950928A575312022884003 BRACKET EMB 120 EMB120RT SO RT TE FLAP CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01161CA 120143 RT OUTBOARD FLAP MOVABLE PANEL, ROLLER SUPPORT BRACKET IS CRACKED. REPLACED CRACKED SUPPORT BRACKET. 2L72 4T RTA31SO 19951006003781995100600378SO 1995 10 6 COMA9511979 119951001A6123M61D628023 RELAY EMB 120 EMB120RT SO E/E COMP DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01267CA 120259 DURING TAKEOFF ROLL, AUTOFEATHER SYSTEM DID NOT ARM. REPLACED RELAYS K0039 AND K0161, SYSTEM TEST NORMAL. 2L72 4T RTA31SO 19951006003791995100600379EA 1995 10 6 COMA9560561 119950928A274083963 TRIM CONTL UNIT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01932CA2154 326 7038 STABILIZER TRIM FAILS WHEN FLAPS SELECTED TO 45 DEGREE. REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2L72 4F RTA21EA 19951006003801995100600380EA 1995 10 6 COMA9560562 119950928A2760 CAUTION MESSAGE CNDAIRCL600 CL6002B19 EA GROUND SPOILERS ACTIVATED A COMAK NONE N FALSE WARNING CRCRUISE 1 SO01912CA 7011 OUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS FLIGHT SPOILERS FAULT MESSAGE. THE PROBLEM COULD NOT BE DUPLICATED AND CLEARED FAULT MESSAGES FROM SECU. AIRCRAFT RELEASED FOR TEST FLIGHT AND NO FURTHER DISCREPANCIES NOTED. 2L72 4F RTA21EA 19951006003811995100600381EA 1995 10 6 COMA9560563 119950927A3240158861 VALVE CNDAIRCL600 CL6002B19 EA PARKING BRAKE DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01940CA3001 2121 7048 BRAKE SHUTOFF VALVE AND ANTISKID FAIL MESSAGE ON EICAS. REPLACED THE PARKING BRAKE SHUTOFF VALVE. 2L72 4F RTA21EA 19951006003821995100600382NM 1995 10 6 DL72L953881 119950930A5320651751738 ANGLE BOEING727 727232 1384082NM BS 1263 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 THERE IS A .3750 CRACK ON THE RIGHT FORWARD AIRSTAIR TORQUE BOX ANGLE AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-0708, WHICH REQUIRES INSPECTION PER S/B 53-0129. 2L73 4F A3WE 19951006003831995100600383NM 1995 10 6 DL72S953877 119950926A5753 SHIM BOEING727 727232 1384082NM RT TE FLAP MISALIGNMENT A DALAK NONE O OTHER ININSP/MAINT 1 SO11532DA 22045 DURING ROUTINE INSECTION, THE LAMINATED SHIM INSTALLED ON THE RIGHT WING I/B FLAP TRACK WAS FOUND TO HAVE MIGRATED FROM LEFT TO RIGHT. COMPLYING WITH AD 90-07-05, THE MIGRATED SHIM WILL BE RELOCATED, REINSTALLED AND THE ATTACHMENTS WILL BE RETORQUED. INSPECTIONS PER SI 4-58662-12AD WILL BE CONTINUED. 2L73 4F A3WE 19951006003841995100600384NM 1995 10 6 DL72S953878 119950917A531165163255001 FRAME BOEING727 727232 1384082NM FS 760.95 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING ACCOMPLISHMENT OF EO 4-61904-3AD, SEVERAL HOLES IN THE INBOARD FRAME FLANGE AT FS 760.95, BOTH RT AND LT SIDES WERE OVERSIZED THROUGH THE STRAP, FRAME, AND MODIFICATION ANGLE. ONE HOLE ON THE LEFT HAND SIDE HAS BEEN OVERSIZED TO 0.403 DIA AND REQUIRES THE INSTALLATION OF A BUSHING. 2L73 4F A3WE 19951006003851995100600385NM 1995 10 6 DL72S953879 119950922A5311651632581 FRAME BOEING727 727232 1384082NM FS 760.95 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11544DA 22493 DURING THE ACCOMPLISHMENT OF DAL EO 4-58560-3AD, IT WAS NOTICED BY MAINTENANCE THAT THE FRAME REINFORCEMENT STRAP ON THE OUTER CHORD OF STA 760.95 FRAM, WAS DOUBLE DRILLED AT THREE LOCATIONS PRIOR TO THIS HEAVY MAINTENANCE VISIT. MAINTENANCE OVERSIZED THE HOLES TO CLEAN UP THE DAMAGE. THE UPPER TWO OVERSIZED HOLES ARE THROUGH THE STRAP AND FRAME AND ARE 0.500 INCH AND 0.437 INCH DIAMETER. THE LOWER HOLE IS ONLY THROUGH THE STRAP AND IS 0.437 INCH DIAMETER. NO DAMAGE HAS BEEN DONE TO THE SKIN. 2L73 4F A3WE 19951006003861995100600386NM 1995 10 6 DL72S953880 119950912A5712 RIB BOEING727 727232 1384082NM BS 760.95 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING THE ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DETECTED IN A FASTENER HOLE IN THE VERTICAL FLANGE OF THE RIB CHORD AT BS 760.95. REMOVAL OF THE CRACK IN THE RIB CHORD RESULTED IN THE INADVERTENT OVERSIZING OF THE FUSELAGE SKIN AT THIS LOCATION, AS WELL AS AN ADJACENT FASTENER. THE BS 760.95 FRAME WAS NOT OVERSIZED. 2L73 4F A3WE 19951006003871995100600387NM 1995 10 6 DL72S953882 119950909A5330 SKIN BOEING727 727232 1384082NM BS 1090 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 THE FUSELAGE SKIN AT STA 1090 IS CRACKED IN TWO PLACES. A .75 INCH CRACK EXISTS ALONG STR 1 AND A .25 INCH CRACK EMANATES FROM THE FIRST FASTENER HOLE RIGHT OF THE CENTERLINE. THIS FASTENER HOLE IS THE FORWARD MOST FASTENER FOR THE DOGHOUSE FAIRING ATTACH ANGLE. THESE 2 CRACK SITES ARE .75 INCH APART CIRCUMFERENTIAL, AND THE CRACKS RUN LONGITUDINALLY. ACCOMPLISHED REPAIRS PER ERA 232051-14AD. 2L73 4F A3WE 19951006003881995100600388NM 1995 10 6 DL72S953884 119950822A5320 FRAMES BOEING727 727232 1384082NM EMER EXIT MISDRILLED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 DURING ACCOMPLISHMENT OF SI 4-61904-12AD, MAINTENANCE DISCOVERED THAT THE FRAMES AT STA 760.95 LT AND RT AND STA 783.95 LT AND RT HAVE OPEN PILOT HOLES IN THE WEB ABOVE STR 17. THE HOLES WHICH ARE ATTACH POINTS FOR INSULATION BLANKETS, HAVE BEEN INSPECTED AND FOUND CRACK FREE. THE HOLES WILL BE INSPECTED UNTIL THE MODIFICATION PER EO 4-61904-3AD IS ACCOMPLISHED ON EACH FRAME. 2L73 4F A3WE 19951006003891995100600389NM 1995 10 6 DL72S953885 119950831A551065241892 BEAM BOEING727 727232 1384082NM RT HORIZ STAB TECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 THE LOWER TRAILING EDGE BEAM ON THE RT HORIZONTAL STABILIZER WAS FOUND CRACKED APPROXIMATELY 2 INCHES FROM THE OUTBOARD END OF THE BEAM. ACCOMPLISHED REPAIRS PER ERA 302395-14. 2L73 4F A3WE 19951006003901995100600390NM 1995 10 6 DL72S953886 119950822A5312 BULKHEAD BOEING727 727232 1384082NM BS 1183 FASTENER SUB A DALAK NONE O OTHER ININSP/MAINT 1 SO11515DA 21431 WHILE ACCOMPLISHING EO 4-40130-3AD, AFT ENTRY DOORWAY AND BODY STATION 1183 BULKHEAD REINFORCEMENT, SEVERAL FASTENERS CALLED FOR BY THE DRAWING, COULD NOT BE INSTALLED DUE TO FRAME INTERFERENCE. THESE FASTENERS WILL BE SUBSTITUTED TO FACILITATE THE MODIFICATION, APPROVAL PER DL ERA 302368-14AD. 2L73 4F A3WE 19951006003911995100600391NM 1995 10 6 DL73S953870 119951001A335020131A EEL BATTERY PACK BOEING737 737232 1384475NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11316DL 23088 EMERGENCY LIGHTS ON LEFT HAND AFT DOOR ARE INOP. REPLACED BATTERY PACK, CKS GOOD. 2L72 4F RTA16WE 19951006003921995100600392NM 1995 10 6 DL73S953871 119951001A33501317 EEL BULB BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11316DL 23088 FOUND EMERGENCY AISLE LIGHT INOP AT 21ABC. RELAMPED, CKS GOOD. 2L72 4F RTA16WE 19951006003931995100600393NM 1995 10 6 DLM88953897 119951001A56105887275501 WINDSHIELD DOUG MD88 MD88 3023688NM FLT DECK FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11970DL 43173 DURING CLIMBOUT AT 5,000 FT, HEARD LOUD POP FROM CENTER WINDSHIELD AND THEN LOUD AIR RUSHING NOISE. FLIGHT RETURNED OAK. REPLACED CENTER WINDSCREEN. 2L72 4F RTA6WE 19951006003941995100600394WP 1995 10 6 MWEA95327 119951001A5320591015839 DOOR JAMB DOUG DC9 DC914 3022034WP AFT CARGO CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND AFT CARGO DOOR JAMB CORRODED UNDER DOOR CUTOUT PAN. REMOVED CORROSION AND INSTALLED SECTION OF DOOR PAN IAW 53-05 FIG HH SHT 4, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006003951995100600395WP 1995 10 6 MWEA95328 119951001A5347S2772660 SEAT TRACK DOUG DC9 DC914 3022034WP BS 217 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND MODERATE CORROSION ON NR 2 SEAT TRACK AT STA 217. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-30-5, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006003961995100600396WP 1995 10 6 MWEA95329 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 786 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND FRAME IN AFT CARGO COMPT STA 786 LONGERON 30, WAS CORRODED. 2L72 4F A6WE 19951006003971995100600397WP 1995 10 6 MWEA95330 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 680 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, THE FRAME AT STA 680 LONGERON 30 IN AFT CARGO COMPT, WAS FOUND CORRODED. MAINTENANCE BLENDED CORROSION AND INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 2A, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006003981995100600398WP 1995 10 6 MWEA95331 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 661 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, THE FRAME AT STA 661 LONGERON 30 IN AFT CARGO COMPT, WAS FOUND CORRODED. MAINTENANCE BLENDED CORROSION AND INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 2A SHT 1, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006003991995100600399WP 1995 10 6 MWEA95332 119951001A53152777897 FLOORBEAM DOUG DC9 DC914 3022034WP CABIN CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND FLOORBEAM AT STA 256, 275, 408, AND 465 CHAFED FROM FLOOR CENTER PANELS. MAINTENANCE FABRICATED AND INSTALLED WEAR STRIP REPAIR IAW SRM 53-05 FIG 20A, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004001995100600400WP 1995 10 6 MWEA95333 119951001A5320991007813 ANGLE DOUG DC9 DC914 3022034WP FWD SERVICE DOORCORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND MODERATE CORROSION IN GALLEY SERVICE DOOR JAMB FORWARD LOWER POCKET, HORIZONTAL BEAM. MAINTENANCE BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS. INSTALLED ANGLE REPAIR IAW SRM 53-05 FIG 55, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004011995100600401WP 1995 10 6 MWEA95334 119951001A53135914562 LONGERON DOUG DC9 DC914 3022034WP BS 661 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, LONGERON 30 AT STA 661 WAS FOUND CORRODED BEYOND LIMITS UNDER FLANGE AT FRAME ATTACH POINT. MAINTENANCE REMOVED AND REPLACED LONGERON IAW SRM 53-01 PG 1, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004021995100600402WP 1995 10 6 MWEA95335 119951001A5320 FITTING DOUG DC9 DC914 3022034WP BS 562 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, IN THE KEEL BEAM AREA AN ATTACH FITTING WAS FOUND CORRODED AT STA 562. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004031995100600403WP 1995 10 6 MWEA95336 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 525/544 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND FRAMES AT STA 525 AND 544 CRACKED ON OUTBD END LT SIDE OF KEEL AREA. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIRS IAW SRM 53-02 FIG 12, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004041995100600404WP 1995 10 6 MWEA95337 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 566 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND FRAME AT STA 566 IN KEEL AREA CORRODED BEYOND LIMITS. MAINTENANCE BLENDED CORROSION AND INSTALLED ANGLE REPAIR IAW SRM 53-03 FIG 12. 2L72 4F A6WE 19951006004051995100600405WP 1995 10 6 MWEA95338 119951001A5311 FRAME DOUG DC9 DC914 3022034WP BS 503/525/544 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, 3 FRAMES WERE FOUND CRACKED IN KEEL BEAM AREA AT STA 503, 525, 544, ALL ON OUTBD AND RT SIDE. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIRS IAW SRM 53-03 FIG 12. 2L72 4F A6WE 19951006004061995100600406WP 1995 10 6 MWEA95339 119951001A532099115573 INTERCOSTAL DOUG DC9 DC914 3022034WP BS 150 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, FOUND INTERCOSTAL CRACKED AT STA 150 RT SIDES, JUST FWD OF GALLEY SERVICE DOOR 54 ABOVE CUSP LINE. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 53-01 FIG 2 SHT 4, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004071995100600407WP 1995 10 6 MWEA95340 119951001A5320 INTERCOSTAL DOUG DC9 DC914 3022034WP BS 286 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, THE AFT CARGO COMPARTMENT FLOOR SUPPORT INTERCOSTAL WAS FOUND CRACKED AT STA 810 LONGERON 286 AND 28R. MAINTENANCE FABRICATED AND INSTALLED NEW INTERCOSTAL FROM 2024-T2 .050 MATERIAL IAW SRM 53-10-3 FIG 3 AND 53-01, PG 1, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004081995100600408WP 1995 10 6 MWEA95341 119951001A2560 GIRT BAR MOUNT DOUG DC9 DC914 3022034WP TAIL SLIDE LOOSE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, THE TAIL EVACUATION SLIDE GIRT BAR WAS FOUND LOOSE ON RIGHT MOUNT. MAINTENANCE TIGHTENED RIGHT SIDE GIRT BAR MOUNT AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006004091995100600409NM 1995 10 6 SCNA95201 119950925A33505878 EEL WIRING BOEING727 727282 2F0R NM CABIN DAMAGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE IN THE FORWARD SECTION OF THE CABIN. A BROKEN FEEDER WIRE WAS FOUND DAMAGED. REPAIRED WIRE AND THE EMERGENCY PATH LIGHTING TESTED GOOD. 2L73 4F RTA3WE 19951006004101995100600410NM 1995 10 6 SCNA95202 119950930A33501002243 EEL BOEING727 727225 1384077NM CABIN INOPERATIVE A SCNAK NONE O OTHER ININSP/MAINT 1 GL15282SC 22558 THE AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-61 AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951006004111995100600411NM 1995 10 6 SCNA95203 119950929A3350900542 EEL BATT CHARGER BOEING727 7272J4 1384006NM L-2 DOOR FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15285SC 21676 THE L-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER, LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951006004121995100600412NM 1995 10 6 UPS404615 119951003A5320 INTERCOSTAL BOEING747 747121 1384871NM BS 1420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACKS IN THE REINFORCING ANGLE AT BS 9360 BETWEEN STR 59 TO STR 8. MAINTENANCE REPAIRED ANGLE IAW SRM 51-40-03. 2L74 4F A20WE 19951006004131995100600413NM 1995 10 6 UPS404636 119951003A5312 CHANNEL BOEING747 747121 1384871NM BS 140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CHANNEL W/200 RT SIDE OF CENTER VERTICAL BEAM CRACKED AT LOWER POSITION. MAINTENANCE PRESSURE BULKHEAD CHANNEL BELOW W/200 RT SIDE OF CENTER VERTICAL BEAM. CRACK OUT OF LIMITS IAW SRM 53-10-01, REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004141995100600414NM 1995 10 6 UPS404637 119951003A5320 FITTING BOEING747 747121 1384871NM BS 2360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND STRINGER END FITTING OF STR S1 STA 236O IS CORRODED. MAINTENANCE REMOVED CORROSION, OUT OF LIMITS, REPLACED FITTING IAW SRM 51-30-05/02. 2L74 4F A20WE 19951006004151995100600415NM 1995 10 6 UPS404638 119951003A5330 SKIN BOEING747 747121 1384871NM WS 499 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK AT UPPER SKIN OF D-BEAM. MAINTENANCE REPAIRED SKIN AT WS 499 IAW SRM 57-30-04 FIGURE 2. 2L74 4F A20WE 19951006004161995100600416NM 1995 10 6 UPS404639 119951003A5320 SHEAR TIE BOEING747 747121 1384871NM BS 1880 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIE ON FRAME CRACKED AT BS 1880 RT, BETWEEN STRINGER 48 TO 49. MAINTENANCE REPAIRED IAW SRM 53-10-04 FIGURE 3. 2L74 4F A20WE 19951006004171995100600417NM 1995 10 6 UPS404640 119951003A5320 SHEAR TIE BOEING747 747121 1384871NM BS 1820 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN SHEAR TIE AT BS 1820 LT, STR 45 AND 46. MAINTENANCE REPAIRED IAW SRM 53-10-04 FIGURE 3. 2L74 4F A20WE 19951006004181995100600418NM 1995 10 6 UPS404641 119951003A5312 BULKHEAD BOEING747 747121 1384871NM BS 2160 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SMALL CRACKS ON BS 2160 BULKHEAD AT RBL 53, 10 INCHES ABOVE CARGO FLOOR AND RBL 37, 5 INCHES ABOVE CARGO FLOOR. MAINTENANCE REPAIRED IAW SRM 51-40-02. 2L74 4F A20WE 19951006004191995100600419NM 1995 10 6 UPS404642 119951003A3270 TAIL SKID BOEING747 747121 1384871NM STA 2580 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND PERMANENT REPAIR OF TAIL SKID DAMAGED AT STA 2580 STRINGER 47R. MAINTENANCE MADE A PERMANENT REPAIR IAW SRM 53-30-03. 2L74 4F A20WE 19951006004201995100600420NM 1995 10 6 UPS404643 119951003A5330 SKIN BOEING747 747121 1384871NM BS 2520 DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND DENT AT LAP SPLICE ON LT LOWER SIDE STA 2520. MAINTENANCE REPAIRED IAW SRM 53-30-03. 2L74 4F A20WE 19951006004211995100600421NM 1995 10 6 UPS404648 119950930A5330 SKIN BOEING747 747SR46 NM NR 4 DOOR CUTOUTCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01689UP 20133 WHILE ON GROUND, MAINTENANCE FOUND NR 4 LT DOOR LOWER HINGE CUTOUT IS CRACKED, VERIFIED WITH EDDY CURRENT. MAINTENANCE REMOVED PANEL, DRILLED OUT RIVETS AND STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 52-10-02. THE WORK WAS PERFORMED IAW EO B747-5210-74684. 2L74 4F A20WE 19951006004221995100600422NM 1995 10 6 UPS404649 119951003A5311 FRAME BOEING747 747121 1384871NM BS 1780 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FRAME WEB DEFORMED AND STIFFENERS CRACKED ON BS 1780 UPPER SIDE, AFT CARGO COMPARTMENT BETWEEN LBL 30 AND RBL 30. MAINTENANCE REMOVED DAMAGED SECTION AND STIFFENERS, FOUND TO BE OUT OF LIMITS AND REPAIRED IAW SRM 51-40-02 AND 51-30-02. 2L74 4F A20WE 19951006004231995100600423NM 1995 10 6 UPS404650 119951003A5311 FRAME BOEING747 747121 1384871NM BS 1900 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER FLANGE OF FRAME AT BS 1900 S42 LT NEAR SIDE GUIDE. MAINTENANCE REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004241995100600424NM 1995 10 6 UPS404651 119951003A5313 STRINGER BOEING747 747121 1384871NM BS 2000 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN THRESHOLD STRINGER IN BULK CARGO COMPARTMENT, AT BS 2000 RBL 52. MAINTENANCE FOUND THE DAMAGE TO BE OUT OF LIMITS, REMOVED CRACKED SECTION OF STRINGER AND REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004251995100600425NM 1995 10 6 UPS404652 119951003A5311 FRAME BOEING747 747121 1384871NM BS 2060 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN FRAME JUST UNDER FLOOR STRUCTURE, BS 2060 LBL 54. MAINTENANCE REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004261995100600426NM 1995 10 6 UPS404653 119951003A5311 FRAME BOEING747 747121 1384871NM BS 2080 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER FLANGE OF FRAME, BS 2080 LBL 53. MAINTENANCE REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004271995100600427NM 1995 10 6 UPS404654 119951003A5311 FRAME BOEING747 747121 1384871NM BS 2000 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND FRAME AND REINFORCEMENT ANGLE CRACKED ON BS 2000 LBL 54 UNDER FLOOR STRUCTURE. MAINTENANCE REPAIRED CRACK IAW SRM 51-40-03. 2L74 4F A20WE 19951006004281995100600428NM 1995 10 6 UPS404655 119951003A5311 FRAME BOEING747 747121 1384871NM BS 1960 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND CRACK IN REINFORCEMENT ANGLE UNDER FRAME UPPER FLANGE, BS 1960 LBL 55. THE CRACK WAS FOUND OUT OF LIMITS. MAINTENANCE REPAIRED IAW SRM 51-40-03. 2L74 4F A20WE 19951006004291995100600429NM 1995 10 6 UPS404656 119950930A3260 SWITCH BOEING727 72721C 138400MNM RT MLG DOOR OUT OF ADJUST A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01934UP 19135 DURING CLIMBOUT, THE RT MAIN GEAR DOOR ANNUNCIATOR LIGHT ILLUMINATED, AFTER POSITIONING THE GEAR HANDLE TO THE OFF POSITION. MAINTENANCE CYCLED THE LANDING GEAR AND THE RT MAIN LIGHT ILLUMINATED AGAIN WITH THE GEAR. ADJUSTED AND TESTED DOOR SWITCH PER MM 32-62-11, OPS NORMAL. 2L73 4F A3WE 19951006004301995100600430WP 1995 10 6 UPS804632 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP FS 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FS 1000 L31 LT AND L31 RT. AFTER CORROSION REMOVAL, FRAME CAP WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT CAP IAW SRM 51-1-8 AND 51-1-20. 2L74 4F RT4A25 19951006004311995100600431WP 1995 10 6 UPS804633 119951003A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP BS 270-280 MISINSTALLED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 270 TO 280 MCD FRAME HAS 2 INTERCOSTAL AT LONGERON 12 AND BETWEEN LONGERON 13 AND 14 LT. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, 51-1-20. 2L74 4F RT4A25 19951006004321995100600432WP 1995 10 6 UPS804634 119951003A5320 SUPPORT DOUG DC8 DC871F 302199DWP BS 70 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLIGHT DECK ENTRY WAY, STA 70 RBL 10 FLOOR SUPPORT INTERCOSTAL CRACKED AT THE AFT END. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-1-21. 2L74 4F RT4A25 19951006004331995100600433WP 1995 10 6 UPS804657 119951003A5320 SUPPORT DOUG DC8 DC871F 302199DWP BS 70 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLIGHT DECK ENTRYWAY, STA 70 RBL 10 FLOOR SUPPORT INTERCOSTAL CRACKED AT AFT END. MAINTENANCE REMOVED ANGLE FABRICATED AND INSTALLED IAW SRM 51-1-21. 2L74 4F RT4A25 19951006004341995100600434WP 1995 10 6 UPS804658 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON ATTACH FITTING SEVERELY CORRODED AND PITTED, STA 1740 LONG 222. MAINTENANCE REMOVED AND REPLACED IAW SRM 51-3-8 AND 51-1-20A. 2L74 4F RT4A25 19951006004351995100600435WP 1995 10 6 UPS804659 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON ATTACH FITTING SEVERELY CORRODED AND PITTED, LONGERON 21L STA 1740. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-3-8 AND 51-1-20A. 2L74 4F RT4A25 19951006004361995100600436WP 1995 10 6 UPS804660 119951003A5313 STRINGER DOUG DC8 DC871F 302199DWP BS 1740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 22L AT FRAME 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER AND FABRICATED REPLACEMENT STRINGER, LOCATED AND INSTALLED IAW SRM 53-5-1. 2L74 4F RT4A25 19951006004371995100600437WP 1995 10 6 UPS804661 119951003A5313 STRINGER DOUG DC8 DC871F 302199DWP BS 1740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 20L AT STATION 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER AND FABRICATED REPLACEMENT STRINGER, LOCATED AND INSTALLED IAW SRM 53-5-1. 2L74 4F RT4A25 19951006004381995100600438WP 1995 10 6 UPS804662 119951003A5313 STRINGER DOUG DC8 DC871F 302199DWP BS 1740 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 21L AT STA 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER, FABRICATED REPLACEMENT STRINGER AND INSTALLED IAW SRM 53-5-1. 2L74 4F RT4A25 19951006004391995100600439WP 1995 10 6 UPS804663 119951003A5320 FRAME FTG DOUG DC8 DC871F 302199DWP BS 440 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATED CORROSION ON FWD SIDE OF FRAME FITTING IN MAIN CABIN, STA 440 LONG 21L. MAINTENANCE REMOVED AND REPLACED FITTING PER DCI SRM 51-1-21D AND 51-3-1. 2L74 4F RT4A25 19951006004401995100600440WP 1995 10 6 UPS804664 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND C-3 FITTING AT LONGERON 33R, FLS 1200 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 53-1-0. 2L74 4F RT4A25 19951006004411995100600441WP 1995 10 6 UPS804665 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 100/120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT, EXFOLIATED AND SURFACE CORROSION ON AND IN LONGERON 34R STA 100 TO 120. 2L74 4F RT4A25 19951006004421995100600442WP 1995 10 6 UPS804666 119951003A5712 RIB DOUG DC8 DC871F 302199DWP WS 810 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING OUTBOARD L/E RIB, STA XFS 810.00 IS CRAKCED AT THE AFT UPPER RIVET. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 57-2-0 AND 51-1-20D. 2L74 4F RT4A25 19951006004431995100600443WP 1995 10 6 UPS804667 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP FS 782 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN EXFOLIATED CORROSION ON BOTTOM OF INTERCOSTAL FWD FITTING, STA 782 LONG 18L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004441995100600444WP 1995 10 6 UPS804668 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 390 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CRACKED, STA 390 LONGERON 28L. MAINTENANCE FABRICATED SPLICE FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006004451995100600445WP 1995 10 6 UPS804669 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 390 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CORRODED BEYOND LIMITS, LONGERON 32L AT STA 390. MAINTENANCE FABRICATED SPLICE FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951006004461995100600446WP 1995 10 6 UPS804670 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME FITTING CORRODED, STA 1120 WHERE LT FRAME ATTACHES TO THE CUSP. MAINTENANCE REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19951006004471995100600447WP 1995 10 6 UPS804671 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP BS 920 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON THE FWD SIDE OF FRAME, STA 920 ABOVE LONG 20L. MAINTENANCE REMOVED SURFACE CORROSION, TREATED AND PRIMED AREA PER SRM 51-1-8. 2L74 4F RT4A25 19951006004481995100600448WP 1995 10 6 UPS804672 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 721 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 31R BS 721, SEVERELY CORRODED. MAINTENANCE REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED NEW ONE PER SRM 53-4-1 AND 51-1-21. 2L74 4F RT4A25 19951006004491995100600449WP 1995 10 6 UPS804673 119951003A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 749 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E, STA XFS 749 UPPER L/E RIB CRACKED AT AFT END. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-2 AND 51-1-20D. 2L74 4F RT4A25 19951006004501995100600450WP 1995 10 6 UPS804674 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 759 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME 759 RT, WHERE ATTACHED TO TOP OF OUTER WING SECTION HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED FITTING PER SRM 51-1-21. 2L74 4F RT4A25 19951006004511995100600451WP 1995 10 6 UPS804675 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1230 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 1230 FRAME FITTING LONGERON 33R AND 34R, SEVERELY CORRODED. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004521995100600452WP 1995 10 6 UPS804676 119951003A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 647.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT OUTBD WING L/E RIB AT STA XFS 647.5, CRACKED AT THE AFT UPPER END. MAINTENANCE FABRICATED AND INSTALLED NEW REPAIR ANGLES IAW SRM 57-2-0 AND 51-1-21. 2L74 4F RT4A25 19951006004531995100600453WP 1995 10 6 UPS804677 119951003A5320 SUPPORT DOUG DC8 DC871F 302199DWP BS 180 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND C1 CARGO COMPARTMENT FLOORBEAM SUPPORT, STA 180 RT CORRODED OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004541995100600454WP 1995 10 6 UPS804678 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1160 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1160 LONGERON 27L HAS HEAVY CORROSION. DAMAGED AREA CUT OUT ON NR 297388, INSTALLED REPAIR PARTS IAW DC8-53-1464 AND SRM 51-1-20D. 2L74 4F RT4A25 19951006004551995100600455WP 1995 10 6 UPS804679 119951003A5712 LE RIB DOUG DC8 DC871F 302199DWP WS 353 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E, STA XFS 353.0 UPPER L/E RIB CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-2-0 AND 51-1-20D. 2L74 4F RT4A25 19951006004561995100600456WP 1995 10 6 UPS804680 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1160 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME ATTACH FITTING CRACKED AND CORRODE, STA 1160 LONG 34R. MAINTENANCE INSTALLED REPAIR SPLICE IAW SRM 52-2-0 FIGURE 20 AND 51-1-20D. 2L74 4F RT4A25 19951006004571995100600457WP 1995 10 6 UPS804681 119951003A5315 FLOORBEAM DOUG DC8 DC871F 302199DWP BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLOORBEAM SEVERELY CORRODED, BS 1580 LBL 45 TO 60. MAINTENANCE REPAIRED IAW EO DC-8-5310-7441A. 2L74 4F RT4A25 19951006004581995100600458WP 1995 10 6 UPS804682 119951003A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP BS 1030-1140 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SEAT TRACK FS 1030 TO 1140 CORRODED BEYOND LIMITS AND STRESS CRACKED. MAINTENANCE REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION IAW SRM 53-2-3 FIGURE 14. 2L74 4F RT4A25 19951006004591995100600459WP 1995 10 6 UPS804683 119951003A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER CORRODED BS 870 AT LONGERON 31R. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-3-1 FIGURE 1. 2L74 4F RT4A25 19951006004601995100600460WP 1995 10 6 UPS804684 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 68 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32R FS 68 CRACKED AND CORRODED. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT LONGERON PER SRM 53-31 FIGURE 2, 51-1-21 AND 51-1-21D. 2L74 4F RT4A25 19951006004611995100600461WP 1995 10 6 UPS804685 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 27/53 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 31R HAS EXFOLIATION CORROSION BEYOND LIMITS, BS 27 AND 53. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-3-1 FIGURE 2, 51-1-21 AND 51-1-21D. 2L74 4F RT4A25 19951006004621995100600462WP 1995 10 6 UPS804686 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1020 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION, FS 1020 LONG 33R TO 33L. AFTER CORROSION REMOVAL FRAME CAP WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED CAP, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-4-1 AND 53-2-0 AND INSTALLED CAP IAW SRM 51-1-21. 2L74 4F RT4A25 19951006004631995100600463WP 1995 10 6 UPS804687 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1060 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION, FS 1060 LONG 33R TO 33L. AFTER CORROSION REMOVAL FRAME CAP WAS FOUND TO BE BEYOND LIMITS. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-4-1, 53-2-0 AND 51-1-8. 2L74 4F RT4A25 19951006004641995100600464WP 1995 10 6 UPS804688 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 960 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON FITTING BETWEEN UPPER WEB AND SKIN, LT MLG W/W STA 960. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIGURE 8. 2L74 4F RT4A25 19951006004651995100600465WP 1995 10 6 UPS804689 119951003A5720 STIFFENER DOUG DC8 DC871F 302199DWP RT WING CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING ROOT JUST I/B OF I/B SPOILER T/E VERTICAL STIFFENER IS CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW PART IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004661995100600466WP 1995 10 6 UPS804690 119951003A5320 SPLICE DOUG DC8 DC871F 302199DWP BS 1270 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1270 LONG 35R SPLICE FITTING, CRACKED AND CORRODED. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004671995100600467WP 1995 10 6 UPS804691 119951003A5712 RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING T/E LOWER MOST INBOARD RIB AT WING ROOT, CRACKED AT THE BOTTOM FLANGE. MAINTENANCE REPAIRED IAW SRM 57-2-0 FIGURE 1. 2L74 4F RT4A25 19951006004681995100600468WP 1995 10 6 UPS804692 119951003A5720 ANGLE DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPAR WEB ATTACH ANGLE CRACKED ON O/B SLOT AREA, RT WING. MAINTENANCE FABRICATED REPLACEMENT ANGLE IAW SRM 54-3-2 AND REMOVED AND REPLACED PER SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19951006004691995100600469WP 1995 10 6 UPS804693 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND ATTACH FITTING FRAME 680 LT, WHERE ATTACHED TO CENTER WING HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-3-0. 2L74 4F RT4A25 19951006004701995100600470WP 1995 10 6 UPS804694 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 680 FRAME TO CENTER WING TANK FITTING RBL 65 TO 70, HAS HEAVY CORROSION AND CAN BE SEEN FROM CABIN UNDER FLOOR. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20. 2L74 4F RT4A25 19951006004711995100600471WP 1995 10 6 UPS804695 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 204 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT LONGERON 28L STA 204 SPLICE CRACKED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE PER SRM 51-1-20D, 51-1-21 AND 51-1-11. 2L74 4F RT4A25 19951006004721995100600472WP 1995 10 6 UPS804696 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1150 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 1150 FRAME FITTING, LONGERON 33R TO 34R IS SEVERELY CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0. 2L74 4F RT4A25 19951006004731995100600473WP 1995 10 6 UPS804697 119951003A5712 RIB DOUG DC8 DC871F 302199DWP WS 322 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E AT STA XFS 322.0 THE UPPER L/E RIB, CRACKED AT THE AFT END. MAINTENANCE REPAIRED RIB IAW SRM 57-2-0. 2L74 4F RT4A25 19951006004741995100600474WP 1995 10 6 UPS804698 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1241 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1241 LONG 35R INTERCOSTAL ATTACH FITTING IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004751995100600475WP 1995 10 6 UPS804699 119951003A5320 WEB DOUG DC8 DC871F 302199DWP BS 860 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND WEB CORRODED AT STA 860, WHERE CENTER WING BOX MEETS WITH W/W PRESSURE PANEL BETWEEN RBL 24, 2ND AND 3RD SEAT TRACK FROM RT SIDE OF FUSELAGE. MAINTENANCE REPAIRED WEB IAW SRM 53-2-0, FABRICATED AND INSTALLED VERTICAL STIFFENER AND END CLIP PER SRM 53-1-0. 2L74 4F RT4A25 19951006004761995100600476WP 1995 10 6 UPS804700 119951003A5712 RIB DOUG DC8 DC871F 302199DWP WS 6.225 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT WS 6.225 CRACKED AT THE AFT LOWER END. MAINTENANCE FABRICATED REPAIR AND INSTALLED IAW SRM 57-2-0 AND 51-1-20D. 2L74 4F RT4A25 19951006004771995100600477WP 1995 10 6 UPS804701 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 98 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHOVEL FITTING CORRODED AT LONGERON 36 FS 98. MAINTENANCE REMOVED AND REPLACED SHOVEL FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004781995100600478WP 1995 10 6 UPS804702 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 118 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT CORROSION AROUND NUT, LONG 36 STA 118. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED AND INSTALLED LONGERON SPLICE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006004791995100600479WP 1995 10 6 UPS804703 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 480-500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 29L CORRODED AT STA 480 TO 500. MAINTENANCE CUT OUT THE DAMAGED AREA PER SRM 53-2-2 FIGURE 10, SPLICED IN NEW SECTION. 2L74 4F RT4A25 19951006004801995100600480WP 1995 10 6 UPS804704 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 500 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 35 CORRODED BEYOND LIMITS AT FS 500. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW SRM 53-2-2, 51-1-20D AND 53-2-2. 2L74 4F RT4A25 19951006004811995100600481WP 1995 10 6 UPS804705 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED AT STA 1420 LONG 33L TO 36. MAINTENANCE REMOVED DAMAGED FRAME, FABRICATED REPLACEMENT SEGMENT AND INSTALLED REPAIR SPLICE IAW SRM 53-4-1. 2L74 4F RT4A25 19951006004821995100600482WP 1995 10 6 UPS804706 119951003A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED, STA 1420 LONG 36 TO 34R. MAINTENANCE REMOVED THE CORRODED FRAME SEGMENT AND FABRICATED REPLACEMENT IAW SRM 53-4-1, AND INSTALLED PER SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951006004831995100600483WP 1995 10 6 UPS804707 119951003A5320 INTERCOSTAL DOUG DC8 DC871F 302199DWP BS 1245 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERCOSTAL, STA 1245 LONG 33R HAS CORROSION AROUND THE NUTPLATE. MAINTENANCE REMOVED, FABRICATED AND REPLACED INTERCOSTAL STA 1245 LONG 33R IAW SRM 53-4-1 AND 51-1-20. 2L74 4F RT4A25 19951006004841995100600484WP 1995 10 6 UPS804708 119951003A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1220 GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1220 LONGERON 33R, WEB WAS GOUGED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. MAINTENANCE COMPLIED WITH EO DC8-5310-7450A, FOR PERMANENT REPAIR. 2L74 4F RT4A25 19951006004851995100600485WP 1995 10 6 UPS804709 119951003A5320 FITTING DOUG DC8 DC871F 302199DWP BS 754 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 759 LONGERON 19R, INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. MAINTENANCE REMOVED FITTING, RECEIVED AND INSTALLED IAW SRM 51-1-20D AND DRAWING 3379874. 2L74 4F RT4A25 19951006004861995100600486WP 1995 10 6 UPS804710 119951003A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE FRAME STA 120 LONG 36, HAS CORROSION UNDER DOUBLER ON FWD SIDE OF FRAME. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PARTS IAW SRM 53-2-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006004871995100600487WP 1995 10 6 UPS804711 119951003A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1240 LONG 36, INTERNAL DOUBLER BULGED AND CORRODED. MAINTENANCE REPLACED EXTERNAL FUSELAGE SKIN PER DRAWING 5750322, SRM 51-1-21, 51-1-20D, 51-3-0 AND UPS EO DC8-5310-7442A. 2L74 4F RT4A25 19951006004901995100600490NM 1995 10 6 9514985501 119950925A5320 FITTING BOEING757 757251 1384970NM FS 336 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01501US 23190 DURING T-CHECK, FOUND CORROSION ON THE LAVATORY MOUNT FITTING BS 336 AT LBL 20. REPLACED FITTING. 2L72 4F RTA2NM 19951006004911995100600491WP 1995 10 6 9514999607 119950929A3222 STRUT DOUG DC9 DC932 3022066WP NLG REQD SERVICE A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01607NW 47232 DURING CLIMB, LANDING GEAR WOULD NOT RETRACT, CREW FOLLOWED PROCEDURE AND LANDING GEAR RETRACTED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. UPON INSPECTION FOUND NOSE STRUT FLAT. SERVICED NOSE STRUT AND AIRCRAFT APPROVED FOR SERVICE. 2L72 4F A6WE 19951006004921995100600492NM 1995 10 6 9515006716 119950930A2782126344171 ACTUATOR BOEING747 747251F 1384898NM NR 1 LE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01616US74133 21120 SFO-ANC - EN ROUTE, THE NR 1 LEADING EDGE DEVICE IN TRANSIT LIGHT ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND DIVERTED TO SEA. MAINTENANCE REPLACED THE LEADING EDGE FLAP DEVICE ACTUATOR AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L74 4F A20WE 19951006004931995100600493WP 1995 10 6 9515019864 119950925A5350 BLOCK/LATCH DOUG DC9 DC951 3022051WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING L-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND SUBSEQUENTLY DROP THE TAILCONE. ALSO, FOUND THE UPPER LEFT CABLE BLOCK WORN AND THE LOWER LEFT LATCH WITH EXCESSIVE PLAY. REPLACED BLOCK, LATCH, ADJUSTED THE RELEASE SYSTEM AND HANDLE CLIPS, CHECKED OK. 2L72 4F A6WE 19951006004941995100600494NM 1995 10 6 9515026730 119950929A2782126344171 ACTUATOR BOEING747 7472J9F 1384806NM NR 1 LE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01630US15271 21668 DURING CRUISE, THE NR 1 WING LEADING EDGE DEVICE IN TRANSIT LIGHT ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, DUMPED 20,000 LBS OF FUEL AND DIVERTED TO SEA. MAINTENANCE REPLACED THE LEFT WING OUTBOARD ROTARY ACTUATOR AND PERFORMED CHECK. UNIT CHECKED NORMAL. 2L74 4F RTA20WE 19951006004951995100600495NM 1995 10 6 9515032278 119950929A278140173 SWITCH BOEING727 727251 138408HNM NR 4 LE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 GL01278US 21157 MDW - ON FLAP EXTENSION, DID NOT GET A BLUE LIGHT AT FIVE DEGREES FLAP. THE LEADING EDGE FLAP PANEL INDICATED THE NR 4 FLAP DID NOT EXTEND. VISUAL INSPECTION IN FLIGHT INDICATED THE FLAP TO BE DOWN. AIRCRAFT DIVERTED TO ORD DUE TO A LONGER RUNWAY AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE NR 4 LEADING EDGE FLAP POSITION SWITCH AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19951006004961995100600496NE 1995 10 6 9515049929 219951001A7320 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE LOW POWER A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL018923E 45838 DURING TAKEOFF, THE NR 1 ENGINE DID NOT REACH TAKEOFF POWER. ABORTED TAKEOFF AND RETURNED TO THE GATE. RERIGGED AND TRIMMED BOTH ENGINES AND OPERATIONAL CHECK GOOD. 2L72 4F4 F A6WE E2EA 19951006004971995100600497NM 1995 10 6 95UAL900169 119951004A3211 TRUNNIONS BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE LT MLG REQD SERVICE A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP294727U 19883 LEFT WING GEAR DOOR REMAINED DOWN UPON GEAR RETRACTION, GEAR DID NOT FULLY RETRACT. LEFT WING GEAR FORWARD AND AFT TRUNNIONS WERE DISASSEMBLED AND REASSEMBLED PER MAINTENANCE MANUAL. 2L74 4F4 F A20WE E20EA 19951006004981995100600498NM 1995 10 6 95UAL900170 119951004A575465B1412714 SUPPORT ROD ASSY BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 20 LE FLAP FAILED A UALAK NONE O OTHER ININSP/MAINT 1 WP29156UA 20105 SUPPORT ROD ASSY WAS FOUND FAILED AFTER FLIGHT. THERE WAS RESULTANT DAMAGE TO THE NR 20 LEADING EDGE VARIABLE CAMBER FLAP. SUPPORT, ROD ASSY AND VARIABLE CAMBER FLAP ASSY WERE REPLACED. FAILURE OF THE SUPPORT ROD WAS INITIATED BY FRETTING DAMAGE WITH A INSULATION CLAMP ON THE ADJACENT PNEUMATIC DUCT. 2L74 4F4 F A20WE E20EA 19951006004991995100600499NM 1995 10 6 95UAL900171 119951004A2700 CONTROLS BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RUDDER/AILERON OUT OF TRIM A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP297298U 21893 UNPLANNED STOP IN DEN, ABNORMAL TRIM INDICATIONS DURING CLIMBOUT AND CRUISE, WITH INCREASING AIRSPEED .82M FL 310 UP TO 3 UNITS OF RUDDER AND 0 UNITS OF AILERON, OR 3 UNITS OF AILERON AND 0 UNITS OF RUDDER. CHECKED FUEL LOAD UPON ARRIVAL AT DENVER, FUEL IMBALANCE OF 4,500 LBS BETWEEN TANKS 1 AND 3, MM 27-00-25 ATTRIBUTES FUEL IMBALANCE AS SOURCE OF OUT OF TRIM. 2L73 4F4 F A3WE E2EA 19951006005001995100600500NM 1995 10 6 95UAL900172 119951004A3150 WARNING PANEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE COCKPIT MALFUNCTIONED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP297258U 21405 BURNING SMELL IN COCKPIT. REPLACED AURAL WARNING PANEL. COMPONENT SHOP FOUND NO EVIDENCE OF OVERHEAT OR BURNING. NO FURTHER REPORTS OF SMELL IN COCKPIT. 2L73 4F4 F A3WE E2EA 19951006005011995100600501 1995 10 6 MWEA95342 419951003A256513621225 EVAC SLIDE DOUG DC9 DC932 3022066WP TAIL LOW PREASURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 4037 47133 DURING SERVICE CHECK, THE TAIL EVACUATION SLIDE PRESSURE WAS FOUND LOW, 2400 PSI. MAINTENANCE REMOVED AND REPLACED TAIL EVACUATION SLIDE IAW DC9 MM, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006005021995100600502NM 1995 10 6 95ZZZX5520 119950816A27825006288G ROTARY ACTUATOR BOEING757 757236 NM RT WING SLAT DEFECTIVE B GJPYO OTHER F FLT CONT AFFECTED NRNOT REPORTED 1 WP33770BE D448 24119 WHEN OPERATED DURING FLIGHT 3555, 'LE SLAT DISAGREE' MESSAGE DISPLAYED. THE LE SLAT COULD NOT BE EXTENDED. FOUND THE ROTARY ACTUATOR AT THE RT WING TIP HAD DEFECT. AS MAINTENANCE HAD NO REPAIR PARTS, THE FLIGHT WAS CANCELLED. OPERATOR SENT MAINTENANCE PEOPLE TO REPAIR THE FAULT. CHANGED THE ROTARY ACTUATOR, CK OK. 2L72 4F RTA2NM 19951006005131995100600513GL 1995 10 6 95ZZZX5531 319950906A6111C13019 CLAMP DHAV DHC6 DHC6300 EA HARTZLHCB3T HCB3TN3 GL BLADE CRACKED AS ERAAK NONE O OTHER ININSP/MAINT 1 AL03 165972885 EF1921 BU6834 PROPELLER INSPECTION REVEALED BLADE CLAMP CRACKED. 1H72 3T A9EA 6 CP15EA 19951006005311995100600531EU 1995 10 6 YIEA00295 119950906A5320AN426AD5 RIVETS AMD FALC20FALCON 2720302EU SKIN DOUBLER WORN A YIEAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AA1207 067 DURING INSPECTION, THE AIRCRAFT WAS FOUND TO HAVE SEVERAL RIVETS LOOSE IN THE AREA OF THE SKIN DOUBLER, INSTALLED AS PART OF THE CABIN DOOR, STC SA2490S0. FURTHER INSPECTION REVEALED DEFECTIVE 'UPSET' HEADS ON MANY OF THE RIVETS INSTALLED DURING THIS MODIFICATION. FOUND NO EVIDENCE OF STRUCTURAL FAILURE. SUBMITTER FEELS THIS IS A CASE OF IMPROPER INSTALLATION TECHNIQUE DURING THE MODIFICATION. TO CORRECT THIS, THE DEFECTIVE RIVETS WERE REMOVED AND REPLACED WITH NEW. SUBMITTER'S ESTIMATION IS THAT APPROXIMATELY 30 PERCENT OF THE TOTAL NUMBER OF RIVETS USED TO ATTACH THIS DOUBLER REQUIRED REPLACEMENT. (X) 2L72 4F A7EU 19951006005781995100600578NM 1995 10 6 95FDEA01477 119950921A5711 SPAR BOEING727 72725C 138400HNM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 RIVET HEAD POPPED AND CORROSION ON OUTSIDE OF CENTER TANK REAR SPAR JUST FWD OF STA 870 RT, RBL 50. REMOVED CORR - MATERIAL THICKNESS BEYOND MM LIMIT. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER AA ESO 11782. AWAITING FEDEX EA. 2L73 4F A3WE 19951006005791995100600579NM 1995 10 6 95FDEA01478 119950923A5315 FLOOR BEAM BOEING727 72723 1384004NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 UPPER LOBE FLOOR STA 480 LT CORROSION ON UNDERSIDE OF FLOOR BEAM BETWEEN LBL 24 AND LBL 45 AROUND FASTENER HOLES. REMOVED CORROSION NR 7 ABOVE LOCATION PER SRM 51-10-06. CORROSION REMOVED BEYOND LIMITS, REPAIRED CORRODED FLOOR BEAM PER 53-10-8 FIG 5. 2L73 4F A3WE 19951006005801995100600580NM 1995 10 6 95FDEA01479 119950923A5312 BLKHD WEB BOEING727 72723 1384004NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 AFT CARGO COMP FS 950 BLKD UPPER FLANGE AND WEB CORRODED BETWEEN RBL 24 - 54. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 FIG 2, SRM 51-10-9. 2L73 4F A3WE 19951006005811995100600581NM 1995 10 6 95FDEA01480 119950925A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION BOTTOM OF FLOOR BEAM JUST I/B OF RBL 25 SEAT TRACK STA 480. REMOVED PORTION OF CORRODED BEAM - FABRICATED AND INSTALLED DOUBLER PER 53-10-8 FIG 5 OF SRM. 2L73 4F A3WE 19951006005821995100600582NM 1995 10 6 95FDEA01481 119950925A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 STA 640, RBL 5 UPPER FLANGE OF FLOOR BEAM HAS EXFOLIATION CORROSION PILLOWED AND BLOWN OUT - REMOVED CORROSION AND INSTALLED DOUBLER REPAIR WITH 7075-T6 EXTRUSIONS AND A 15-5 STAINLESS STEEL STRAP, CAD PLOTED AND HEAT TREATED TO 180-200 RSI, TREATED AND PRIMED ALL SURFACES AS REQ'D. INSTALLED WITH FASTENERS AND FAYING SURFACE SEALER PER SRM 53-10-8. 2L73 4F A3WE 19951006005831995100600583NM 1995 10 6 95FDEA01483 119950926A5330 SKIN BOEING727 72725C 138400HNM BS 1130 MISMFG A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25135FE 19853 TWO FASTENERS INSTALLED IN ONE HOLE, THROUGH SHEAR TIE STA 1130, O/B OF STR 29L. REMOVED DAMAGE FROM FASTENERS AT STA 1130 O/B OF STR 29L. INSTALLED DOUBLER OF AFT FUSE BELLY SKIN PER SRM 53-30-3. 2L73 4F A3WE 19951006005841995100600584NM 1995 10 6 95FDEA01484 119950926A5330 SKIN BOEING727 72725C 138400HNM BS 1150 MISMFG A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25135FE 19853 AFT CARGO BELLY SKIN AT STA 1150, STA 29 - 2 EA HOLES HAVE 2 FASTENERS IN ONE HOLE. REMOVED DAMAGED FASTENERS, INSTALLED DOUBLER ON SKIN PER SRM 53-30-3. 2L73 4F A3WE 19951006005851995100600585NM 1995 10 6 95FDEA01485 119951003A5330 SKIN BOEING727 72725C 138400HNM BS 1160 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 DOUBLER CRACKED AT RIVET STA 1160 O/B OF STR 26R. REMOVED DAMAGED SKIN AT SKIN LAP STA 1149 - 1163, STR 26R PER SRM 53-30-3 FIG 5. INSTALLED REPAIR DOUBLER FROM STA 1140 - 1167 STR 26R PER SRM 53-30-3, PAGES 20-25. 2L73 4F A3WE 19951006005861995100600586NM 1995 10 6 95FDEA01486 119951003A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION IN LOWER FLANGE OF FLOOR BEAM BS 1110, BL 0 - 48 RT, IN AFT CARGO COMP. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED ANGLES AND STRAP PER ESO 11782, INSTALLED SAME PER ESO 11782, EA NR 7-5310-25188. 2L73 4F A3WE 19951006005871995100600587NM 1995 10 6 95FDEA01487 119951003A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 CORROSION IN AFT CARGO COMP FS 1110 FLOOR BEAM LOWER FLANGE BL 16L TO 30L. REMOVED CORRODED AREA PER SRM 51-10-6, FABRICATED FILLER AND DOUBLER PER ESO 11782, INSTALLED FILLER AND DOUBLER PER ESO 11782 AND SRM 51-10-6, 51-40-2. EA NR 7-5310-25810. 2L73 4F A3WE 19951006005881995100600588NM 1995 10 6 95FDEA01488 119951004A5741 FITTING PIN BOEING727 72725C 138400HNM RT WING CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 RIGHT WING REAR SPAR BODY FITTING FWD AND REAR BUSHINGS WORN, BODY FITTING PIN FLANGE CORRODED. INSTALLED NEW RT WING REAR SPAR BODY FITTING PIN PER SRM 51-10-1 PG 4, REPLACED FWD AND REAR BUSHINGS PER 51-10-1 PG 4, ESO 11782 AND FEDEX EA NR 7-5310-25827. 2L73 4F A3WE 19951006005891995100600589NM 1995 10 6 95FDEA01489 119950916A5313 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 CRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT BOX BETWEEN STA 720B AND 720G. STOP DRILLED CRACK IN STR 15L AT FASTENER AFT OF ICE LIGHT. HFEC AROUND STOP DRILL, NO CRACKS FOUND PER NDT MANUAL. INSTALLED REPAIR PER SRM 53-10-3 / 7075-T6 .040 INCH, SRM 53-10-2. 2L73 4F A3WE 19951006005901995100600590NM 1995 10 6 95FDEA01490 119950920A5313 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 MAIN CARGO INTERIOR STRUCTURE. STR 16R CRACKED IN OUTER FLANGE, AFT OF STA 720B FRAME, FWD OF ICE LIGHT HOUSING. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER SRM 53-10-3 FIG 2. 2L73 4F A3WE 19951006005911995100600591NM 1995 10 6 95FDEA01491 119950921A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 MAIN CARGO INTERIOR, CORROSION ON TOP OF STA 344 FLOOR BEAM UPPER CHORD, BETWEEN RBL 2 - 14. REMOVED CORROSION, INSTALLED REPLACEMENT CHORD AND SPLICE ANGLES PER STANDARD REPAIR DRAWING MANUAL SR 27-53-007. 2L73 4F A3WE 19951006005921995100600592NM 1995 10 6 95FDEA01492 119950925A5330 SKIN BOEING727 727227 1384078NM BS 303 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25483FE 21465 FORWARD LT FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUT OUT. FS 303, STR 13L. CRACK LENGTH .480 INCH INITIAL MEASUREMENT. NDT VERIFIED CRACK END IN FASTENER HOLE. COUNTER BORED FUSELAGE OUTER SKIN AT FASTENER HOLE. ROUTED OUT CRACK AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3, FIG 11 AND BOEING SB 53-727-53-0198, REV I FIG 4. 2L73 4F A3WE 19951006005931995100600593NM 1995 10 6 95FDEA01493 119951004A5320 SHEAR TIE BOEING727 72722 1384002NM BS 1070 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING KEEL BEAM NR0389, FOUND CORROSION ON THE SHEAR TIE AT BS 1070 BETWEEN STR 29 AND STR 28L AFTER REMOVING SEAL FOR ACCESS OF AREA. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED SHEAR TIE, DOUBLER, AND FILLER, ALODINED, PRIMED AND PAINTED AS REQ, SEALED PARTS, REPAIRED SHEAR TIE PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19951006005941995100600594NM 1995 10 6 95FDEA01494 119951003A5311 FRAME BOEING727 727227 1384078NM BS 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FRAME CRACKED UNDER FLOOR SUPPORT, BS 600 ABOVE STR 28L LBL 10. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951006005951995100600595NM 1995 10 6 95FDEA01495 119951003A5311 FRAME BOEING727 727227 1384078NM BS 640 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FRAME CRACKED UNDER FLOOR SUPPORT, BS 640, STR 27R, RBL 18. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951006005961995100600596NM 1995 10 6 95FDEA01496 119951004A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CORROSION (C53-224-01) AROUND FASTENER HOLES ON TOP CHORD OF BEAM BS 344, RBL 16-LBL 60, WL 208. REMOVED UPPER T-CHORD, FIXED NEW CHORD IN PLACE AND DRILLED, REMOVED DEBURRED, ALODINED, PRIMED AND INSTALLED WET WITH SEALANT. ALL WORK DONE IAW FEDEX SR 27-53-007, AT BS 344, RBL 16 - LBL 60, WL 208. 2L73 4F A3WE 19951006005971995100600597NM 1995 10 6 95FDEA01497 119951004A5313 STRINGER BOEING727 727227 1384078NM BS 480 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 STR 22R PUNCTURED BS 480 PLUS 8.5 INCHES. REMOVED DAMAGED SECTION OF STR 22R, BS 480 PLUS 8.5 INCHES. FABRICATED REPAIR PARTS AND INSTALLED WET WITH SEALANT IAW FEDEX 727 SRM 53-10-3, FIG 1. 2L73 4F A3WE 19951006005981995100600598NM 1995 10 6 95FDEA01498 119951004A532065453132 CLIP BOEING727 727227 1384078NM BS 440 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CRACKED STR CLIP NR 1 AT BS 440. REMOVED CRACKED STR CLIP AT BS 440 STR 1. BACK DRILLED NEW CLIP AND INSTALLED WET WITH FAYING SURFACE SEALANT IAW FEDEX SRM 51-30-2, 51-10-1 AND MM 51-30-0. 2L73 4F A3WE 19951006005991995100600599NM 1995 10 6 95FDEA01499 119951004A532065453132 CLIP BOEING727 727227 1384078NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CRACKED STRINGER CLIPS AT STA 950C, STR 6 AND 7R. REMOVED CRACKED STR CLIPS AT BS 950C, STR 6 AND 7R. BACK DRILLED NEW STR CLIPS AND INSTALLED WET WITH FAYING SURFACE SEALANT IAW FEDEX SRM 51-30-2, 51-10-1 AND FEDEX MM 51-30-0. 2L73 4F A3WE 19951006006001995100600600NM 1995 10 6 95FDEA01500 119951004A532065453132 CLIP BOEING727 727227 1384078NM BS 750 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 MECH DAMAGE FOUND ON STR CLIP AND AT STA 750F, STR 7R. REMOVED DAMAGED STR CLIP AT STA 950F, STR 7R. BACK DRILLED NEW CLIP AND INSTALLED WET WITH FAYING SURFACE SEALANT IAW FEDEX SRM 51-30-2, 51-10-1, MM 51-30-0. 2L73 4F A3WE 19951006006011995100600601NM 1995 10 6 95FDEA01501 119951004A5311 FRAME BOEING727 727225 1384077NM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 THE UPPER FLANGE OF FRAME IS CRACKED AT BS 1090 STA 27R. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND REPAIRED UPPER FLANGE OF FRAME AT BS 1090 STR 27R PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951006006021995100600602NM 1995 10 6 95FDEA01502 119951004A5311 FRAME BOEING727 727225 1384077NM BS 1050 PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 IN THE AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AND HAS A DOUBLE HOLE AT BS 1050, RBL 19, WL 148. REPAIRED UPPER FLANGE OF FRAME AT BS 1050, RBL 19, WL 148 PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951006006031995100600603NM 1995 10 6 95UAL900173 119951005A2751AL4500351 SWITCH BOEING757 757222 1384956NM PWA 2037 PW2037 NE TE FLAPS FAILED A UALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 WP29521UA 24891 ON FINAL, WHEN FLAPS SELECTED FROM 20-25 DEGREES, TRAILING EDGE FLAP DISAGREE LIGHT CAME ON. FLAPS STOPPED AT 20 DEGREES AND WOULD NOT MOVE. LANDED WITH FLAPS 20 DEGREES. REPLACED TRAILING EDGE ALTERNATE FLAP SWITCH ASSEMBLY AND CIRCUIT CARD. FLAPS WERE CYCLED SEVERAL TIMES. CHECKS O.K. 2L72 4F4 FRTA2NM E17NE 19951006006041995100600604NM 1995 10 6 95UAL900174 119951005A3350 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29550UA 25398 EMERGENCY EXIT LIGHT INOP AT ROW 17. RELAMPED. CHECKS O.K. 2L72 4F4 FRTA2NM E17NE 19951006006051995100600605WP 1995 10 6 95UAL900175 119951005A5415 FITTING DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE NR 3 ENGINE CRACKED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291858U 46987 NR 3 ENGINE PYLON FWD MOUNT TRUSS FITTING ASSY, PRIOR TO FURTHER FLIGHT, REPLACE AT LEAST ONE TRUSS FITTING ACCT RT FITTING PREVIOUSLY CRACKED AND REPAIRED. LT FITTING CRACKED AT HORIZ FLANGE INBD BOLT HOLE. 2L73 4F4 F A22WE E23EA 19951006006061995100600606WP 1995 10 6 ABXA9500751 119951002A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC931 3022065WP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23949AX 309 47325 DURING PRE-FLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE NICAD BATTERIES IN THE EMERGENCY LIGHT POWER SUPPLY PACK IAW DC-9 SUPP. M.M. 33-53-0. 2L72 4F A6WE 19951006006071995100600607WP 1995 10 6 ABXA9500752 119951002A335041B004AD07G3 EEL BATTERY GRIMES 60030431 DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23970AX 47494 DURING MAINTENANCE CHECK, FOUND THE EMERGENCY LIGHTS INOP. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 SUPP. M.M. 33-53-0. OPS CHECKED GOOD. 2L72 4F A6WE 19951006006081995100600608WP 1995 10 6 ABXA9500753 119951002A7920519516 OIL LINE DOUG DC9 DC933F 302207AWP PWA JT8 JT8D11 52044NE LT ENGINE LEAKING A ABXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL23930AX 47363 666772 LEFT ENGINE SHUT DOWN FOR FLUCTUATING OIL PRESSURE AND ZERO QUANTITY INDICATION. TOTAL WINDMILL TIME WAS LESS THAN 1.5 MINUTES. REPLACED TWO OIL LINES OFF THE FUEL/OIL COOLER TO GEAR BOX IAW DC-9 M.M. 79-20. LEAK CHECKED GOOD. 2L72 4F4 F A6WE E2EA 19951006006091995100600609WP 1995 10 6 ABXA9500754 119951004A3260801801 SENSOR DOUG DC9 DC931 3022065WP NLG DEFECTIVE A ABXAK NONE N FALSE WARNING TOTAKEOFF 1 GL23942AX 47522 AFTER TAKEOFF, DURING UPLATCH CHECK, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. CYCLED GEAR. NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. REPLACED NOSE DOWNLOCK SENSOR IAW DC-9 SUPP. M.M. 32-60-1. OPS CHECKED GOOD. 2L72 4F A6WE 19951006006101995100600610NE 1995 10 6 ABXA9500755 219951004A7261581167 RELIEF VALVE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 2 ENGINE NICKED A ABXAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 GL23815AX 46097 669403 DURING CRUISE, NT 2 ENGINE OIL PRESSURE DROPPED TO 5 P.S.I. NR 2 ENGINE WAS SHUTDOWN. INSPECTED NR 2 ENGINE OIL FILTER AND NO DISCREPANCIES WERE FOUND. REPLACED OIL FILTER ASSEMBLY I/A/W DC8 MM. REPLACED ENGINE OIL RELIEF VALVE AND ADJUSTED THE OIL PRESSURE I/A/W DC8 MM AND PWA MM, CHAPTER 72. GROUND RAN ENGINE AND ALL INDICATIONS WERE GOOD. NO LEAKS WERE NOTED. 2L74 4F4 F 4A25 1E8 19951006006111995100600611WP 1995 10 6 MWEA95343 119951002A53209958231501 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 897-937 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 DURING C-CHECK INSPECTION, FOUND THE AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN STATION 897 AND 937 JUST INBD OF DOOR JAMB HAS CORROSION. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006006121995100600612WP 1995 10 6 MWEA95344 119951002A335060030431 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN FAILED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31502ME 2655 48132 DURING C-CHECK INSPECTION, FOUND EMERGENCY LIGHTS OVER BOTH LT AND RT FWD EMERGENCY EXITS ARE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006006131995100600613WP 1995 10 6 MWEA95345 119951002A523059101413 SKIN DOUG DC9 DC932 3022066WP FWD CARGO DOOR CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 DURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR HANDLE CHAFING ON DOOR SKIN AT CUTOUT. MAINTENANCE INSTALLED REPAIR DOUBLER ON SKIN PER SRM 52-05, FIG. 30. A/C RETURNED TO SERVICE. 2L72 4F A6WE 19951006006141995100600614WP 1995 10 6 MWEA95346 119951002A52109915565159 ANGLE DOUG DC9 DC932 3022066WP AFT STAIR DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 DURING C-CHECK INSPECTION, FOUND THE AFT VENTRAL STAIR DOOR HAS A SUPPORT ANGLE CRACKED AT THE MID-SPAN. MAINTENANCE REMOVED AND REPLACED ANGLE AS PER SRM 51-30-2 AND SRM 51-30-3. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006006151995100600615WP 1995 10 6 MWEA95347 119951002A53205912528501 DOOR JAMB DOUG DC9 DC932 3022066WP AFT CARGO COMPT CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31502ME 48132 DURING C-CHECK INSPECTION, FOUND THE AFT CARGO DOOR JAMB LOWER PAN CRACKED WITH CORROSION NEAR CENTER STOP. MAINTENANCE REPLACED LOWER PAN PER SRM 53-05, FIG. 44. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951006006161995100600616WP 1995 10 6 MWEA95348 119951003A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP FWD CABIN FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31401ME 47133 CREW REPORTED PASSENGER ENTRANCE DOOR SLIDE COVER FELL OFF. MAINTENANCE RESECURED SLIDE COVER. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951006006171995100600617NM 1995 10 6 SWAA950651 119950925A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07373SW 26581 DURING SCHEDULED C2/C4 CHECK, FOUND GOUGE UNDER FWD ENTRY DOOR AT AFT CORNER MEASURING 5 INCH BY .250 INCH BY .018 INCH DEEP. REPAIRED PER SWA RA 1-353-1370. 2L72 4F RTA16WE 19951006006181995100600618NM 1995 10 6 SWAA950652 119950928A5330 SKIN BOEING737 7373H4 1384600NM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07329SW 23693 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT BS 727D BELOW STRINGER 20L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951006006191995100600619NM 1995 10 6 SWAA950653 119950928A5330 SKIN BOEING737 7375H4 138449DNM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07508SW 24185 DURING SCHEDULED 1/2 C-CHECK, FOUND PREVIOUS FUSELAGE SKIN REPAIR DOUBLER AT AFT ENTRY DOORWAY WITH SEVERAL DISCREPANCIES. REPAIRED PER SWA RA 1-553-1371. 2L72 4F RTA16WE 19951006006201995100600620NM 1995 10 6 SWAA950654 119950929A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0750SW 21447 DURING SCHEDULED 1/2 C CHECK, FOUND FUSELAGE SKIN CRACKED AT LEFT SIDE, 2ND PASSENGER WINDOW FROM FRONT AT TOP FWD CORNER RIVET HEAD. REPAIRED PER SWA RA 1-253-1372 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951006006211995100600621NM 1995 10 6 SWAA950655 119950928A5320 WEB BOEING737 7375H4 138449DNM BS 794.3 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07508SW 24185 DURING SCHEDULED 1/2 C-CHECK, FOUND WEB GOUGED AND CRACKED FWD OF AFT CARGO DOOR AT BS 794.3 FROM S25R TO 24R. REPAIRED PER SWA RA 1-553-1371. 2L72 4F RTA16WE 19951006006221995100600622NM 1995 10 6 UPS204647 119950930A3350 EEL BATT PACK BOEING727 72725C 138400HNM ENTRY DOOR LOOSE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01933UP 19857 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT OVER COCKPIT DOOR MUST BE BANGED ON TO MAKE WORK. FOUND BATT PACK LOOSE. CLEANED DOOR CONTACT PINS AND RESECURED BATT PACK. OPS CK NORMAL MM 33-50-00. 2L73 4F A3WE 19951006006231995100600623NM 1995 10 6 UPS204744 119951005A2170 COALESCER BAGS BOEING727 72731C 1384011NM A/C PACK DIRTY A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01925UP 19230 WHILE IN JACKSON, MS, A BURNING SMELL OCCURRED ON TAKEOFF ROLL. MAINTENANCE CHANGED LT AND RT WATER SEPARATOR COALESCERS PER MM 21-51-34. 2L73 4F A3WE 19951006006241995100600624WP 1995 10 6 UPS204745 119951005A2560 EVAC SLIDE DOUG DC8 DC871F 302199DWP EMER EXIT SLIDE UNSECURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE ON GROUND, MAINTENANCE FOUND ENTRY DOOR EVAC SIDE GIRTH BAR FAILED TO LATCH. MAINTENANCE RE-PACKED EVAC SLIDE. 2L74 4F RT4A25 19951006006251995100600625NM 1995 10 6 UPS204746 119951005A3350 EEL BOEING747 747123 1384873NM MAIN DECK INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 20100 WHILE ON GROUND, MAINTENANCE FOUND FWD CREW ENTRY EMER LT AND EMER LT FWD OF CREW LADDER (MAIN DECK CEILING) INOP. MAINTENANCE INSTALLED LIGHT AND BATTERY PACK. OPS CK OK. 2L74 4F A20WE 19951006006261995100600626WP 1995 10 6 UPS204747 119951005A3260 CONNECTOR DOUG DC8 DC871F 302199DWP NLG LOOSE A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01755UP 46055 ON DEPARTURE FOR CLEVELAND, PILOT REPORTED THAT ON UPLATCH CHECK, NOSE EXTENSION W/GEAR NOT LATCHED LIGHT ILLUMINATED. UPLATCH CHECK PASSED ON THIRD ATTEMPT. MAINTENANCE FOUND THE PLUG NOT LATCHED ON SW LOOSE. RESECURED, LUBED NOSE GEARS AS A PRECAUTION. CHECKED PER MM 32-60-00, PAGE 201. 2L74 4F RT4A25 19951006006271995100600627NM 1995 10 6 UPS404733 119951004A5313 STRINGER BOEING747 747121 1384871NM BS 340/400 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SEVERAL CRACKS ON STR 6 LT AT BS 340/400 BY HFEC INSP. MAINTENANCE INSTALLED REPAIR DOUBLER ACC SB53-2253R2 AND DWR 65B28212-1 AND -2 PER UPS E.O. B747-5330-7466. 2L74 4F A20WE 19951006006281995100600628NM 1995 10 6 UPS404734 119951004A5320 SHEAR TIES BOEING747 747121 1384871NM BS 1720 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIES CRACKED AT BS 1720 RT BETWEEN STR 47/48 AND STR 48/49. MAINTENANCE FOUND CRACK OUT OF LIMITS AND REPAIRED IAW SRM 53-10-01, 53-10-04, FIGURE 3. 2L74 4F A20WE 19951006006291995100600629NM 1995 10 6 UPS404735 119951004A5320 SHEAR TIES BOEING747 747121 1384871NM BS 1700 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND SHEAR TIES CRACKED AND CORRODED ON BS 1700 BETWEEN STRINGER 51 LT AND STRINGER 51 RT BETWEEN STRINGER 47 AND 46, RT AND BETWEEN STRINGER 48 AND 49 RT. MAINTENANCE FOUND CRACKS AND CORROSION OUT OF LIMITS AND REPAIRED SHEAR TIES IAW SRM 53-10-01 AND 53-10-04. 2L74 4F A20WE 19951006006301995100600630NM 1995 10 6 UPS404736 119951004A5730 SKIN BOEING747 747121 1384871NM WS 780 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01683UP 0353 WHILE IN AMSTERDAM FOR C-CHECK, MAINTENANCE FOUND RT WING LOWER SKIN CORRODED. REMOVED CORRODED PAD-UP AT LES STA 780. MAINTENANCE REPAIRED IAW UPS E.O. 747-57-0291. 2L74 4F A20WE 19951006006311995100600631WP 1995 10 6 UPS804712 119951004A5311 FRAME DOUG DC8 DC873F 302199FWP FS 260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELTFRAME, FS 260 BETWEEN LONGERONS 35L-35R. REPAIRED IAW DC8-5310-7474A. 2L74 4F RT4A25 19951006006321995100600632WP 1995 10 6 UPS804713 119951004A5320 FITTING DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND B/T FITTING HAS HEAVY CORROSION AND CRACKED AT STA. 270, L33A-33BR. REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006006331995100600633WP 1995 10 6 UPS804714 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 260-360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INNER DOUBLER AT STA 260-360, LONGERONS 35L-38A. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006006341995100600634WP 1995 10 6 UPS804715 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 360-400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT INNER DOUBLER, FS 360-400, LONGERON 35L-30R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006006351995100600635WP 1995 10 6 UPS804716 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 220-260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT INNER SKIN DOUBLER AT FS 220-260 LONGERON 35L-30R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006006361995100600636WP 1995 10 6 UPS804717 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 200-220 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON ANTENNA DOUBLER BETWEEN FS 200-220, LONGERONS 35L-35R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006006371995100600637WP 1995 10 6 UPS804718 119951004A5330 SKIN DOUG DC8 DC873F 302199FWP BS 190-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELLY SKIN PANEL AT FS 190-450. MAINTENANCE REPLACED BELLY SKIN PANEL PER SRM 51-1-20D AND SRM 51-1-21. 2L74 4F RT4A25 19951006006381995100600638WP 1995 10 6 UPS804719 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 230-320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION AT FINGER DOUBLER FS 220-320, LONGERON 31L. MAINTENANCE REPLACED DOUBLER SECTION STA. 210-350 IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006006391995100600639WP 1995 10 6 UPS804720 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 190-200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER, FS 190-200, LONGERON 31L. MAINTENANCE REPLACED DOUBLER SECTION IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951006006401995100600640WP 1995 10 6 UPS804721 119951004A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 260-300 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERONS 34L FS 260-300 L34RT BOTH CRACKED AND HEAVILY CORRODED. MAINTENANCE REPLACED LONGERON SECTIONS IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006006411995100600641WP 1995 10 6 UPS804722 119951004A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 488 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT AILERON ACCESS PANEL NR 5H DOUBLER CRACKED AT STA. 488. REPAIRED IAW UPS E.O. DC8-5750-7469-A. 2L74 4F RT4A25 19951006006421995100600642WP 1995 10 6 UPS804723 119951004A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 1660 BELT FRAME LOWER LIP AT LONGERON 36 HAS INTERGRANULAR CORROSION. MAINTENANCE REPLACED FRAME SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19951006006431995100600643WP 1995 10 6 UPS804724 119951004A5320 FITTING DOUG DC8 DC873F 302199FWP BS 870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION (53-224-05.00-01) BS 870 BODY FORGING WL 191 RBL 71 (MARKED). MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-30-1, AND E.O. B727-5310-7454-A. 2L74 4F RT4A25 19951006006441995100600644WP 1995 10 6 UPS804725 119951004A5730 SKIN DOUG DC8 DC873F 302199FWP WING CTR SECTIONCORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP OF UPPER FUEL CELL SKIN BS 746-770 RBL 25-45 WL 203 (MARKED). MAINTENANCE REPAIRED WING CENTER SECTION UPPER FUEL CELL SKIN PER UPS E.O. 727-57-1653. 2L74 4F RT4A25 19951006006451995100600645WP 1995 10 6 UPS804726 119951004A5713 STRINGER DOUG DC8 DC873F 302199FWP BS 350-360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON WEB CONNECTING BS 350 AND 360, WL 198 (STRINGER 19), LBL 60. MAINTENANCE REMOVED CORROSION FOUND OUT OF LIMITS, CUT OUT THE DAMAGED AREA, FABRICATED NEW WEB AND STIFFENERS AND INSTALLED IAW SRM 51-30-2, 53-10-1. 2L74 4F RT4A25 19951006006461995100600646WP 1995 10 6 UPS804727 119951004A3231 PULLEY QUADRANT DOUG DC8 DC873F 302199FWP NLG DOOR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND NOSE DOOR PULLY QUADRANT CORRODED. MAINTENANCE REMOVED AND REPLACED WITH NEW QUADRANT IAW MM 32-33-51, 32-31-51 AND 32-22-01. 2L74 4F RT4A25 19951006006471995100600647WP 1995 10 6 UPS804728 119951004A5320 STRAP DOUG DC8 DC873F 302199FWP BS 504-658 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE FORWARD CARGO BAY AROUND NUTPLATE HOLES ON THE BL ZERO STAB. STRAP. STA 504-658, LBL 2-RBL 2 WL 201. MAINTENANCE REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED THE DAMAGED PARTS, FABRICATED AND INSTALLED NEW PARTS IAW SRM 53-10-1 AD E.O. 95-30-22. 2L74 4F RT4A25 19951006006481995100600648WP 1995 10 6 UPS804729 119951004A5315 FLOOR BEAM DOUG DC8 DC873F 302199FWP CARGO BAY CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND CORROSION FORWARD CARGO BAY IN NUTPLATE HOLES IN THE LOWER FLANGE OF THE S40 FLOOR BEAM LBL 17-RBL 58 WL 201. MAINTENANCE BLENDED CORROSION AND FOUND OUT OF LIMITS, CUT FLOOR BEAM LOWER FLANGE AND REPAIRED IAW E.O. B727-5310-7452-A. 2L74 4F RT4A25 19951006006491995100600649WP 1995 10 6 UPS804730 119951004A5313 STRINGER DOUG DC8 DC873F 302199FWP BS 355 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND STR 20 BS 355 TO BE CORRODED, RT. MAINTENANCE CLEANED CORROSION, FOUND OUT OF LIMITS, REPAIRED IAW SRM 53-10-3 AND 53-10-1. 2L74 4F RT4A25 19951006006501995100600650WP 1995 10 6 UPS804731 119951004A5510 SPLICE BEAM DOUG DC8 DC873F 302199FWP HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND THE LT UPPER SPLICE BEAM AND THE UPPER AND LOWER SHEAR FITTINGS CORRODED AT APPROX RUDDER STA 212.87-220.870. MAINTENANCE REMOVED AND REPLACED SPLICE ASSY AND UPPER AND LOWER SHEAR FITTINGS IAW BOEING DRAWING 65-16788 AND SRM 51-30-2. 2L74 4F RT4A25 19951006006511995100600651WP 1995 10 6 UPS804732 119951004A5541 RIB DOUG DC8 DC873F 302199FWP RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01818UP 46108 WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BOTH HOLES IN UPPER RUDDER, UPPER THRUST LINK SUPPORT RIB CRACKED WHERE THE BOLTS GO THROUGH THE SPLICE BEAM. MAINTENANCE REMOVED AND REPLACED THE RIB ASSY IAW SRM 51-30-2 AND MM 27-20-21, 27-20-101, AND 27-20-141. 2L74 4F RT4A25 19951006006521995100600652WP 1995 10 6 UPS804737 119951004A5315 FLOOR BEAM DOUG DC8 DC871 302199AWP BS 1640 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLOOR BEAM STA 1640 RBL 29.5 TO BE OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-1-20 AND DC8-53-1463. 2L74 4F 4A25 19951006006531995100600653WP 1995 10 6 UPS804738 119951004A5312 BLKHD ANGLE DOUG DC8 DC871 302199AWP CTR WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE CENTER WING LOWER SURFACE LT AFT CORNER BULKHEAD ATTACH ANGLE CRACKED. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND 51-3-0. 2L74 4F 4A25 19951006006541995100600654WP 1995 10 6 UPS804739 119951004A5320 INTERCOSTAL DOUG DC8 DC871 302199AWP BS 980-1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL CORRODED AT STA 980 TO 1000 LONGERON 30R. MAINTENANCE FABRICATED INTERCOSTAL PER UPS DC8-53-1465, INSTALLED FABRICATED INTERCOSTAL IAW SRM 51-1-20. 2L74 4F 4A25 19951006006551995100600655WP 1995 10 6 UPS804740 119951004A5311 FRAME DOUG DC8 DC871 302199AWP BS 180 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FORWARD SIDE OF THE FRAME CRACKED, LONGERON 34R AT STA. 180. MAINTENANCE INSTALLED FRAME REPAIR IAW SRM 53-2-0, FIGURE 2. 2L74 4F 4A25 19951006006561995100600656WP 1995 10 6 UPS804741 119951004A5311 FRAME DOUG DC8 DC871 302199AWP BS 1260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME FORMER CORRODED AT STA 1260 BETWEEN LONGERONS 35L AND 35R. MAINTENANCE FABRICATED REPLACEMENT SECTION AND INSTALLED IAW SRM 53-2-02B AND 53-4-1, FIGURE 51 AT STA 1260. 2L74 4F 4A25 19951006006571995100600657WP 1995 10 6 UPS804742 119951004A5311 FRAME DOUG DC8 DC871 302199AWP BS 1260 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME 1260 BETWEEN LONGERONS 35L AND 35R IS OUT OF LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-2-0 AND 51-1-20. 2L74 4F 4A25 19951006006581995100600658WP 1995 10 6 UPS804743 119951004A5311 FRAME DOUG DC8 DC871 302199AWP BS 99 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD SPLICE FITTING CORRODED AT STA 99 AS SEEN THROUGH PANEL 90B. MAINTENANCE FABRICATED SPLICE AND INSTALLED IAW SRM 51-1-20D, 51-1-20, 51-1-21, AND DC8-53-1476. 2L74 4F 4A25 19951006006591995100600659WP 1995 10 6 UPS804748 119951005A5315 FLOOR BEAM DOUG DC8 DC871F 302199DWP BS 1560 EXFOLIATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FLOOR BEAM UPPER CAP EXFOLIATED AT LBL 3.0 TO LBL 6.0 AT STA. 1560. MAINTENANCE CUT OUT THE DAMAGED SECTION, FABRICATED REPAIR ANGLE AND FILLER AND INSTALLED PER DC8-5310-7446A. 2L74 4F RT4A25 19951006006601995100600660WP 1995 10 6 UPS804749 119951005A5315 FLOOR BEAM DOUG DC8 DC871F 302199DWP BS 1600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FLOOR BEAM AT STA 1600 RBL 40 LOWER SIDE OF HORIZ. FLANGE WAS BEYOND LIMITS AFTER CORROSION REMOVAL. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER DC8-5310-7457A. 2L74 4F RT4A25 19951006006611995100600661WP 1995 10 6 UPS804750 119951005A5311 FRAME DOUG DC8 DC871F 302199DWP BS 99 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD CRACKED BELOW SPLICE, STA 99 AT WBL 4750 AS SEEN THROUGH PANEL 90B. MAINTENANCE INSTALLED LOWER CAP WBL ANGLE CHORD REPAIR AT STA 99 PER DHC SK 798-093 REV A (RT SIDE). 2L74 4F RT4A25 19951006006621995100600662WP 1995 10 6 UPS804751 119951005A5311 FRAME DOUG DC8 DC871F 302199DWP BS 1240 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1240 LONGERON 36 FRAME CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REPAIRED FRAME IAW DHC SK 798-179. 2L74 4F RT4A25 19951006006631995100600663NM 1995 10 6 UPS804752 119951005A5315 FLOOR BEAM BOEING727 727108C 1384039NM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON THE FLOOR BEAM AT STA 328, LBL 33 WL 208. ALSO, HAS MECHANICAL DAMAGE LBL 54, WL 208. MAINTENANCE REPAIRED THE FLOOR BEAM IAW SRM 53-10-8, FIGURE 7. 2L73 4F A3WE 19951006006641995100600664NM 1995 10 6 UPS804753 119951005A3230 UPLOCK HOOK BOEING727 727108C 1384039NM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND THE LT UPLOCK HOOK HAS EXCESSIVE PLAY. MAINTENANCE FOUND THE UPLOCK TO BE CORRODED, REMOVED UPLOCK ASSY AND REPLACED WITH NEW PART IAW MM 32-32-51, 32-32-61, 32-32-0. 2L73 4F A3WE 19951006006651995100600665NM 1995 10 6 UPS804754 119951005A5330 SKIN BOEING727 727108C 1384039NM BS 272-275 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272-275, LBL 56, WL 209-213. MAINTENANCE REMOVED THE CORROSION, WAS FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER, PERFORMED FINAL REPAIR IAW SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2. 2L73 4F A3WE 19951006006661995100600666NM 1995 10 6 UPS804755 119951005A5320 WEB BOEING727 727108C 1384039NM BS 600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND SUPPORT WEB TO BE CRACKED AT BS 600, LBL 7, WL 300. MAINTENANCE REPAIRED AREA IAW EO B727-53-1683. 2L73 4F A3WE 19951006006671995100600667NM 1995 10 6 UPS804756 119951005A5315 FLOOR BEAM BOEING727 727108C 1384039NM BS 420 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BEAM STA 420 LBL 0 TO LBL 24 AND LBL 45 - LBL 65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED CORROSION ON UPPER CHORD OF FLOOR BEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. MAINTENANCE REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM PER UPS EO B727-5310-7455A. 2L73 4F A3WE 19951006006681995100600668NM 1995 10 6 UPS804757 119951005A5315 FLOOR BEAM BOEING727 727108C 1384039NM BS 420 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM AT STA 420 RBL 45-65, WL 208 LOWER SIDE OF UPPER CHORD. MAINTENANCE REMOVED THE CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. MAINTENANCE REPAIRED IAW UPS EO B727-5310-7455A. 2L73 4F A3WE 19951006006691995100600669NM 1995 10 6 UPS804758 119951005A5511 RIB BOEING727 727108C 1384039NM EMPENNAGE CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM AT APPROX RUDDER STA 128.765 LT. MAINTENANCE REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW TRAMCO EWO 95-3072. 2L73 4F A3WE 19951006006701995100600670CE 1995 10 6 95ZZZM507 119950816A3297 WIRE BEECH 99 C99 1154006CE GEAR HORN CHAFED A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19216EE U206 FLT NR 472 - FPO-FLL - LANDING GEAR WARNING HORN ON AND OFF IN FLIGHT. TROUBLESHOT SYSTEM TO SHORT IN CENTER FLOOR PC BOARD HOLDER AREA, ZONE 143. REPAIRED CHAFED WIRE. OPS CHECK GOOD ON JACKS, TEST FLIGHT SATISFACTORY AIRCRAFT RELEASED TO SERVICE. (M) 1L72 3T A14CE 19951006006711995100600671WP 1995 10 6 95ZZZM508 119950902A2720160009 PRESS REG VLV DOUG DC8 DC862 3021970WP RUDDER INOP A RIAAJA DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET NRNOT REPORTED 1 SO191805 45899 DURING FLT NR EE1100 AT LEVEL 31,000 AIRCRAFT EXPERIENCED RUDDER VIBRATION, AIRCRAFT DESCENDED TO FLIGHT LEVEL 11,000 DUMPED FUEL AND REDUCED AIRSPEED TO 210 KNOTS AT WHICH TIME VIBRATION CEASED. AIRCRAFT WAS DIVERTED TO JFK FOR INSPECTION/TROUBLESHOOTING. AT JFK REPLACED RUDDER PRESSURE REGULATOR AND RELIEF VALVE. (M) 2L74 4F 4A25 19951006006721995100600672WP 1995 10 6 95ZZZM509 119950824A3260833703 UPLOCK SENSOR DOUG DC9 DC981 3022081WP LT MLG INTERMITTENT A A4JAO OTHER N FALSE WARNING CLCLIMB 1 SO15817SJ 48051 UPON GEAR RETRACTION, LEFT MAIN LANDING GEAR UNSAFE LIGHT CAME ON. CYCLED GEAR, LIGHT WENT OUT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED LEFT MLG UPLOCK SENSOR. OPERATIONAL TEST NORMAL. (M) 2L72 4F A6WE 19951006006731995100600673 1995 10 6 95ZZZM510 419950831A34216224565001 VERT GYRO BEECH 1900 1900D 1154162CE COCKPIT INOP A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE01100UX 4415 UE100 FAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M) 2L72 4T RTA24CE 19951006006741995100600674 1995 10 6 95ZZZM511 419950831A34256229681001 EHSI BEECH 1900 1900D 1154162CE COCKPIT INOP A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE01100UX 791 UE100 FAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M) 2L72 4T RTA24CE 19951006006751995100600675CE 1995 10 6 95ZZZM512 119950824A77141143800075 N1 INDICATOR BEECH 1900 1900C 1154161CE RT ENGINE OUT OF ADJUST A GLBAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 CE0187GL 8408129 UC87 DEN - THE CREW ELECTED AN AIR TURN BACK AFTER OBSERVING THE RT ENGINE AT 104 PERCENT AND 2700 LBS TORQUE WOULD NOT MAKE REQUIRED TORQUE. THE CREW ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE CALIBRATED THE TORQUE SYSTEM, THE ITT SYSTEM, COMPRESSOR WASHED THE ENGINE, AND REPLACED THE N1 INDICATOR. THE ENGINE RUN WAS SATISFACTORY. (M) 2L72 4T RTA24CE 19951006006761995100600676EA 1995 10 6 95ZZZM513 219950830A7200 ENGINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LEFT FAILED A GLBAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 CE01122GL1518 538 UC122 PCE32546 ORD-BRL - FLT NR 5927 - THE LEFT ENGINE FAILED AND WAS SECURED. THE CREW DIVERTED TO GBC ON SINGLE ENGINE AND COMPLETED AND UNEVENTFUL LANDING. MAINTENANCE CHANGED ENGINES. SUSPECT BEARING FAILURE. (M) 2L72 4T4 TRTA24CE E4EA 19951006006771995100600677CE 1995 10 6 95ZZZM514 119950831A712012991003779 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01123UE 2007 UC123 SPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RT ENGINE TRUSS CHAFED IN AREA 'B' AS DESCRIBED IN BEECH SB 2255R7 AND AD 95-02-18, THE DAMAGE WAS REPAIRED IAW REPAIR NR 2 OF BEECH KIT 129-9006-1. (M) 2L72 4T RTA24CE 19951006006781995100600678CE 1995 10 6 95ZZZM515 119950830A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01174GL3746 UC174 SPW - DURING THE ROUTINE VISUAL INSPECTION REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED IN AREA 'A'. THE TRUSS WAS CHANGED AND ENGINE FUNCTIONAL TEST WAS SATISFACTORY. 2L72 4T RTA24CE 19951006006791995100600679CE 1995 10 6 95ZZZM516 119950830A5610 WINDSHIELD BEECH 1900 1900D 1154162CE FUSELAGE BIRD STRIKE A GLBAA UNSCHED LANDING C F.O.D. CLCLIMB 1 CE01101UX UE101 SPW - DURING CLIMB-OUT AFTER DEPARTURE, THE CREW ENCOUNTERED A BIRD STRIKE. THE CREW ELECTED A PRECAUTIONARY AIR TURN BACK. AFTER AN UNEVENTFUL LANDING, MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION. NO FINDINGS WERE FOUND. (M) 2L72 4T RTA24CE 19951006006801995100600680NM 1995 10 6 95ZZZM517 119950911A6123954215B653323 SWITCH DHAV DHC8 DHC8102 2809003NM AUTOFEATHER SYSTFAILED A HNAAK NONE N FALSE WARNING CLCLIMB 1 EA07925HA19374 111 FLT NR 3031 - TPA-JAX - THE AUTOFEATHER ARM LIGHT FLICKERED ON AND OFF SEVERAL TIMES DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDENT. GROUND RUN UP WAS COMPLIED WITH IN JAX AND THE AUTOFEATHER OPERATED NORMALLY. COULD NOT DUPLICATE THE PROBLEM. AT RON, THE AUTOFEATHER SELECT SWITCH WAS REMOVED AND REPLACED. (M) 2H72 4T RTA13NM 19951006006811995100600681NM 1995 10 6 95ZZZM518 119950911A3260841005 PSEU DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAK NONE N FALSE WARNING CRCRUISE 1 EA072FOR 10212 132 070 FLT NR 3053 - MIA-JAX - NOSE GEAR GREEN AND RED LIGHTS AND GEAR HANDLE LIGHT ILLUMINATED IN FLIGHT. AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROXIMITY SENSING ELECTRONIC UNIT. (M) 2H72 4T RTA13NM 19951006006821995100600682NM 1995 10 6 AALA951356 119950730A3350P4010051126 EEL MODULE BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07879AA 21391 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM PAX SEAT ROW 15 AFT INOPERATIVE. AIRCRAFT MAINTENANCE FERRY RDU/MIA. REPLACED EMERGENCY FLOOR LIGHT CONTROL MODULE AM1059. ALSO, REPAIRED WIRES FOUND CHAFED BEHIND RT AFT SERVICE DOOR PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951006006831995100600683NM 1995 10 6 AALA951374 119950805A3350A3060722 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07865AA 21370 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION (M) 2L73 4F A3WE 19951006006841995100600684EU 1995 10 6 AALA951416 119950725A2460CR3 DIODE FOKKERF28 F28MK0100 4990807EU HEAT SINK DEFECTIVE A AALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SW071442E 11437 SWF - FLT NR 0428 - EN ROUTE ORD-ALB - DURING CRUISE, EMERGENCY DC BUS FAIL INDICATION ON MULTI FUNCTION DISPLAY UNIT. AIRCRAFT DIVERTED TO SWF AND LANDED WITHOUT INCIDENT. REPLACED CR3 BLOCKING DIODE ON HEAT SINK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19951006006851995100600685EU 1995 10 6 AALA951482 119950818A3350 EEL WIRE FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071402K 11353 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT WIRING ON LOOSE CEILING PANEL BETWEEN FORWARD GALLEY BROKEN. REPAIRED EMERGENCY LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19951006006861995100600686NM 1995 10 6 AALA951483 119950818A33505013CW EEL ASSEMBLY BOEING727 727223 1384074NM GALLEY DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07886AA 21525 RDU - DURING OVERNIGHT CHECK, FOUND THE FORWARD AND AFT GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED LIGHT ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951006006871995100600687NM 1995 10 6 AALA951534 119950825A5320 SPLICE BOEING767 767223 1385123NM BS 1307 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - STRINGER 39L SPLICE AT STATION 1307 CORRODED. FABRICATE NEW LONGER STRINGER SPLICE. INSTALLED SPLICE WET WITH SAME FASTENER TYPE AND PATTERN PER ENGINEERING MRB 767-1007. (M) 2L72 4F RTA1NM 19951006006881995100600688NM 1995 10 6 AALA951535 119950825A5314 KEEL BEAM BOEING767 767223 1385123NM BS 1011 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - KEEL BEAM PANEL FLANGE CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ROTOPEENED BLENDED AREAS. REFINISHED BLENDED AREA PER SRM 53-50-12 FIG 101. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-999. (M) 2L72 4F RTA1NM 19951006006891995100600689NM 1995 10 6 AALA951536 119950825A5320 SPLICE BOEING767 767223 1385123NM BS 434 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - STRINGER 38L FOUND CORRODED IN FORWARD CARGO. STRINGER TRIMMED BACK SEVEN INCHES TO REMOVE CORROSION. FABRICATED AND INSTALLED NEW SPLICE FROM .040 INCH MATERIAL IDENTICAL TO THE OLD PIECE EXCEPT THE NEW PIECE WAS LONGER BY THE AMOUNT REMOVED FROM THE STRINGER END. APPROVED BY ENGINEERING PER MRB 767-997. (M) 2L72 4F RTA1NM 19951006006901995100600690NM 1995 10 6 AALA951537 119950825A5313146T3240 STRINGER BOEING767 767223 1385123NM BS 1307-1329 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - STRINGER 39R CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. REFINISHED BLENDED AREAS PER SRM 53-00-03 FIG 101. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-995. (M) 2L72 4F RTA1NM 19951006006911995100600691NM 1995 10 6 AALA951538 119950825A5315141T5110 FLOOR BEAM BOEING767 767223 1385123NM BS 266 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - FLOOR BEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 AND A HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MBB 767-991. (M) 2L72 4F RTA1NM 19951006006921995100600692NM 1995 10 6 AALA951539 119950825A5314 KEEL BEAM BOEING767 767223 1385123NM BS 1012 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - LEFT PANEL FLANGE OF KEEL BEAM CORRODED. AFTER BLENDING FOUND BEYOND SRM LIMITS. ROTOPEENED AND ALODINED BLENDOUT. REFINISHED AREA PER SRM 53-50-12 FIG 101. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MBB 767-1002. (M) 2L72 4F RTA1NM 19951006006931995100600693NM 1995 10 6 AALA951540 119950825A5730 SKIN BOEING767 767223 1385123NM CTR WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07308AA 22314 AFW - CORROSION FOUND ON CENTER WING UPPER SKIN AT AFT DRAINS. REMOVED FASTENERS IN CORRODED AREAS AND REMOVED CORROSION. EDDY CHECKED BLENDED AREAS AND FASTENER HOLES. NO CRACKS FOUND. SPOT FACED FASTENER HOLES. ROTOPEENED BLENDED AREAS. INSTALLED FASTENERS. ALODINED AND PRIMED, APPLIED FUEL BARRIER TOP COAT AND DYNOL ACCOMPLISHED PER ENGINEERING PER MRB767-993. (M) 2L72 4F RTA1NM 19951006006941995100600694NM 1995 10 6 AALA951543 119950824A5753 SKIN BOEING767 767323 1385205NM TE AFT FLAP CHAFED A AALAK NONE O OTHER ININSP/MAINT 1 SW07371AA 25198 AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS IN TWO AREAS. BLENDED SHARP EDGES, EDDY CURRENT CHECKED FILLED WITH BMS 5078 TYPE 3 AND ADJUSTED SEAL RETAINER PER ENGINEERING MRB 767-100. (M) 2L72 4F RTA1NM 19951006006951995100600695NM 1995 10 6 AALA951544 119950824A5753 SKIN BOEING767 767323 1385205NM TE AFT FLAP CHAFED A AALAK NONE O OTHER ININSP/MAINT 1 SW07371AA 25198 AFW - FLAP NOSE SKIN IS CHAFED BEYOND SRM LIMITS IN TWO AREAS. BLENDED SHARP EDGES, EDDY CURRENT CHECKED, FILLED WITH BMS 5-28 TYPE 3 AND ADJUSTED SEAL RETAINER PER ENGINEERING MRB 767-100. (M) 2L72 4F RTA1NM 19951006006961995100600696NM 1995 10 6 AALA951553 119950826A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN FLOOR NEED RESECURING A AALAK NONE L NO TEST ININSP/MAINT 1 SW07613AA 24489 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT ROW 8D THROUGH 15D. SECURED CONNECTOR. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951006006971995100600697NM 1995 10 6 AALA951556 119950821A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS ON THE LEFT SIDE OF BUSINESS CLASS INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT 12B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006006981995100600698NM 1995 10 6 AALA951557 119950828A3350S283T0231 EEL INVERTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT INVERTOR AND LEFT GALLEY CROSS AISLE LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006006991995100600699NM 1995 10 6 AALA951558 119950828A3350 EEL PIN BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 JFK - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS ON RIGHT AISLE BETWEEN SEATS 24H THROUGH 37H INOPERATIVE. SECURED EMERGENCY EXIT FLOOR PATH LIGHT PIN AT 5702 VT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006007001995100600700NM 1995 10 6 AALA951560 119950822A3350A3060719101 EEL STRIP BOEING757 757223 1384957NM CABIN SHORTED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07697AN 26977 ORD - FLT NR 416 - EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951006007011995100600701NM 1995 10 6 AALA951570 119950829A3260 SWITCH WIRE BOEING727 727223 1384074NM NLG BROKEN A AALAK NONE N FALSE WARNING CLCLIMB 1 SW07874AA 21386 MIA - FLT NR 1111 - AFTER TAKEOFF MCO WHEN LANDING GEAR RETRACTED, UNSAFE NOSE LANDING GEAR INDICATION WITH ALL HYDRAULIC PRESSURE NORMAL. AIRCRAFT PROCEEDED MIA AND LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE SPLICE TO NOSE LANDING GEAR LOCK SWITCH. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951006007021995100600702 1995 10 6 AALA951575 419950903A34174045053912 ADC HONEYWELL FOKKERF28 F28MK0100 4990807EU E/E COMPT DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071451N 93071646 11460 ORD - FLT NR 2085 - AFTER TAKEOFF ORD DURING CLIMB-OUT, LOST LEFT EFIS AIRSPEED INDICATION FOLLOWED BY NR 1 FLIGHT AUGMENTATION PANEL FAULTS. UNABLE TO RESET AND AIRCRAFT RETURNED TO ORD, LANDING WITHOUT INCIDENT. REPLACED NR 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19951006007031995100600703NM 1995 10 6 AWXA9500599 119950906A523010608211 SEAL BOEING737 737277 1384570NM FWD CARGO DOOR TORN A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28185AW 22652 LAS - 552 - PHX/SMF - PRESSURIZATION FAILED IN AUTO MODE. CREW ELECTED TO DIVERT AIRCRAFT TO LAS, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MASSIVE LEAK ABOVE RT WING UNDERNEATH THE WING TO BODY FAIRING, AND THE CARGO DOOR SEAL TORN IN TWO PLACES. MAINTENANCE RESEALED .5 INCH SQUARE HOLE UNDER WING TO BODY FAIRING (RT AFT), AND REPLACED FORWARD CARGO DOOR SEAL. CABIN PRESSURE CHECK OK, NO LEAKS NOTED AS PER MM 5-51-91. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951006007041995100600704NM 1995 10 6 AWXA9500600 119950904A335020131A EEL BATT PACKS BOEING757 7572S7 1384962NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28902AW 23322 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT L1, L4, R2 AND R3 DOORS. REMOVED AND REPLACED BATTERY PACKS AT M737, M734, M733 AND M731. OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951006007051995100600705NM 1995 10 6 AWXA9500601 119950907A33501000679 EEL ASSEMBLY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28180AW 22647 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE OVER THE L1 DOOR. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951006007061995100600706NM 1995 10 6 AWXA9500602 119950907A335020131A EEL BATT PACK BOEING757 757225 1384959NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28913AW 22207 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT R3 DOOR. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951006007071995100600707NM 1995 10 6 AWXA9500604 119950908A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHT WIRE BROKEN AT ROW 18. REPINNED WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951006007081995100600708NM 1995 10 6 AWXA9500605 119950911A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 18 AND ROW 20. RECONNECTED PINS AT SEATS 20 AND 18, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951006007091995100600709NM 1995 10 6 AWXA9500606 119950911A3350900835A EEL BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR AND R1 DOOR LOWER EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951006007101995100600710EU 1995 10 6 AWXA9500607 119950908A5320 RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND T-CAP AT RAIL MINUS 1292 CORRODED FROM FRAME 16 TO FRAME 20. REMOVED AND REPLACED RAIL IAW SRM 51-22-00 AND SRM 51-42-11. (M) 2L72 4F RTA28NM 19951006007111995100600711EU 1995 10 6 AWXA9500608 119950908A5320 RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND T-CAP AT RAIL MINUS 254 CORRODED FROM FRAME 16 TO FRAME 20. REMOVED AND REPLACED RAIL IAW SRM 53-11-14. (M) 2L72 4F RTA28NM 19951006007121995100600712EU 1995 10 6 AWXA9500609 119950908A5320 RAIL AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND DUMMY RAIL 254 CORRODED FROM FRAME 20 FORWARD TO APPROXIMATELY 8 INCHES FORWARD OF FRAME 16. REPAIRED IAW SRM 53-11-14, FIGURE 202. (M) 2L72 4F RTA28NM 19951006007131995100600713EU 1995 10 6 AWXA9500611 119950908A5320 T-CAP AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND T-CAP AT RAIL 252 CORRODED AT FRAME 20. REMOVED AND REPLACED T-CAP PER SRM 51-72-11. (M) 2L72 4F RTA28NM 19951006007141995100600714EU 1995 10 6 AWXA9500612 119950908A5313 LONGERON AIRBUS320 A320231 3930325EU FUSELAGE CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND T-CAP AT RAIL 1292 CORRODED FROM FRAME 16 TO FRAME 20. REMOVED AND REPLACED LONGERON RAIL PER SRM 51-22-00 AND SRM 51-42-11. (M) 2L72 4F RTA28NM 19951006007151995100600715WP 1995 10 6 IXXA199575 119950830A3231510361 LINK ASSY DOUG DC8 DC863F 302198FWP NLG DOORS OUT OF ADJUST A IXXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 GL23786AL 46121 ON CLIMB-OUT OF ATL, WITH LANDING GEAR RETRACTED AND ALL INDICATIONS NORMAL, NOSE GEAR DOOR VIBRATION WAS EXPERIENCED AT 250 KNOTS. THE AIRCRAFT WAS SLOWED TO 230 KTS, THE GEAR WAS CYCLED, AND AN UPLATCH CHECK WAS PERFORMED. ALL INDICATIONS WERE NORMAL, BUT DOOR BUFFETING CONTINUED. THE FLIGHT PROCEEDED TO TOL AT 230 KNOTS WITH THE GEAR EXTENDED. EN ROUTE, DOOR BUFFETING CEASED. ALL NOSE GEAR DOORS WERE CLOSED ON ARRIVAL AT TOL. MAINTENANCE INSPECTED AND RIG-CHECKED THE NLG DOORS AND DOOR LINKS, ADDING SPACERS TO THE RT FORWARD LINK. THE NOSE GEAR WAS OPS CHECKED IAW THE DC-8 MM 32-22-1, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951006007161995100600716NM 1995 10 6 MALA954613 119950829A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15830MA 337 FLT NR 3022 - DURING THE PREFLIGHT IN DTW, THE FIRST TWO RED FLOOR TRACK LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951006007171995100600717NE 1995 10 6 PLGA83195TJ 219950830A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 FAILED A PLGAO OTHER J WARNING INDICATION APAPPROACH 1 NE05350BE593 340B197 785379 FLT NR 4891 - ON LANDING APPROACH TO IAD CREW OBSERVED NR 2 ENGINE CHIP LIGHT ILLUMINATION. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. TECHNICIAN REMOVED THE ENGINE OIL FILTER AND CONFIRMED PRESENCE OF METAL CHIPS SIZE AND QUANTITY ABOVE ALLOWABLE LIMITS. THE ENGINE WAS REMOVED AND REPLACED IAW APPLICABLE CHAPTERS OF THE GE AND SAAB MAINTENANCE MANUALS. 2L72 4T4 TRTA52EU E8NE 19951006007181995100600718SO 1995 10 6 SRAA79512 119950803A61206794188 ROD LKHEED382 382G 526414USO NR 1 ENGINE BROKEN A SRAAO OTHER O OTHER LDLANDING 1 SO19921SJ 4586 AET - FLT NR 1973 - ON LANDING, NR 1 PROPELLER FAILED TO REVERSE, LOW PITCH STOPS DID NOT RETRACT. FOUND INTERMEDIATE PROP CONTROL ROD BROKEN. REPLACED ROD AND PERFORMED OPS CHECK PER MM CHAPTER 76. (M) 2H74 4T A1SO 19951006007191995100600719WP 1995 10 6 SRAA80195 119950804A3350 EEL BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A SRAAK NONE L NO TEST ININSP/MAINT 1 SO19873SJ 46091 WHILE ON THE GROUND, MAINTENANCE PERSONNEL FOUND EMERGENCY EXIT LIGHT WOULD NOT TURN ON. FOUND BATTERY PACK HAS NO POWER. REPLACED BATTERY PACK, OPS CHECKED GOOD. (M) 2L74 4F RT4A25 19951006007201995100600720SO 1995 10 6 SRAA80295 119950806A2613 TEMP SENSOR LKHEED382 382E 526413USO RT WING FAILED A SRAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO19923SJ 4301 AFTER TAKEOFF FROM LUTTON, RIGHT WING OVERHEAT LIGHT ILLUMINATED, AIRCRAFT COMPLETED AIR TURN BACK TO LUTTON. PERFORMED DUCT PRESSURE CHECK ON THE ANTI-ICE SYSTEM. NO LEAKS NOTED, INSPECT TEMP SENSOR FOUND FAULTY REPLACED SENSOR, SYSTEM OPS CHECKED GOOD. (M) 2H74 4T A1SO 19951006007211995100600721SO 1995 10 6 SRAA99503 119950902A5320 BOW BEAM LKHEED382 382G 526414USO BS 537 CRACKED A SRAAK NONE O OTHER ININSP/MAINT 1 SO19918SJ 4208 POST FLIGHT INSPECTION, FOUND RIGHT WHEEL WELL AT FUSELAGE STATION 537, HAD BAD BOW IN SKIN AREA. FOUND RIGHT BOW BEAM AT FUSELAGE STATION 537, WATER LEVEL 170 CRACKED. REPAIRED BOW BEAM IAW SRM CHAPTER 53-40-12-B. (M) 2H74 4T A1SO 19951006007221995100600722NM 1995 10 6 USAA950908 119950818A5311 FRAME BOEING737 737301 1384611NM FRAME 360 DAMAGED A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19558AU 23512 CLT - DURING AN UNSCHEDULED MAINTENANCE CHECK INSPECTION, FOUND A DEEP CUT BY TOOLING WHEEL LOCATED AT FRAME 360, S-4 RT TO S-4 LT. INSTALLED REPAIR DOUBLE SECTION. (X) 2L72 4F RTA16WE 19951006007231995100600723NM 1995 10 6 USAA950921 119950823A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19507AU27606 23382 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON NUT PLATE HOLES ON TOP OF FLOOR BEAM CAP, BS 986.5 RBL 23-37 AND LBL 20-42. INSTALLED NEW CAP ON FLOOR BEAM (ENTIRE LENGTH). REPAIRED PER TR 53-10-05. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951006007241995100600724NM 1995 10 6 USAA950922 119950804A5320 ANGLE BOEING737 7373B7 1384580NM BS 950-999 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19507AU27606 23382 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 40 INCHES CORRODED AREA ON 'Z' ANGLE AT LEFT AFT ENTRY DOOR FRAME STATION 950 TO STATION 999. REPLACED 'Z' ANGLE AND FABRICATED NEW WEB UNDER ANGLE. REPAIRED PER SRM 51-10-2. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19951006007251995100600725NM 1995 10 6 USAA950923 119950725A5313 STRINGER BOEING737 7373B7 1384580NM STA 315-324 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19507AU27606 23382 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 9 INCH CORRODED AREA ON STRINGER S-28 L STATION 315 TO STATION 324. SPLICED IN NEW STRINGER, REPAIRED PER SRM 53-00-03, FIG 201. CORROSION TASK NR C53-202-01. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951006007261995100600726NM 1995 10 6 USAA950924 119950804A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 986.5 - 992 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19507AU27606 23382 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA AT CABIN BS 986.5 - 992 LBL 36 - LBL ON INTERCOSTAL. REPLACED INTERCOSTAL, SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951006007271995100600727NM 1995 10 6 95ZZZM519 119950902A5755654645123 SKIN BOEING737 737214 138446RNM NR 8 SPOILER DELAMINATED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO15460AT 20158 NR 8 SPOILER DELAMINATED LOWER SURFACE APPROXIMATELY 612 SQUARE INCHES. REPLACED SPOILER PANEL. (M) 2L72 4F A16WE 19951006007281995100600728NM 1995 10 6 AWXA9500591 119950829A7931 OIL PRESS IND BOEING757 757225 1384959NM LT ENGINE MALFUNCTIONED A AWXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 WP28914AW 22208 PHX-LAS - FLT NR 91 - EN ROUTE TO LAS THE LT ENGINE WAS SHUT DOWN DUE TO LOW OIL PRESSURE INDICATION. AIRCRAFT CONTINUED TO LAS AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE PERFORMED INSPECTION OF LEFT ENGINE OIL FILTERS, AND CHECKED AND CLEANED OIL PRESSURE SWITCH CONNECTORS. ALL CHECKS OK. PERFORMED BVCU BITE, NO FAULTS NOTED. INSPECTED CHIP DETECTORS ON ENGINE GEAR BOX. NO METAL NOTED. EICAS BITE CHECK OK. BPCU BITE CHECK NORMAL. NO FAULTS NOTED. SWAPPED OIL PRESSURE TRANSMITTER WITH NR 2 ENGINE FOR TROUBLESHOOTING. PERFORMED ENGINE RUN AT IDLE POWER AND THREE QUARTERS POWER. NO ANOMALIES NOTED DURING RUNS OR TAXI. ALL PARAMETERS NORMAL. NO FAULTS NOTED. A/C RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19951006007291995100600729EU 1995 10 6 AWXA9500610 119950908A5320 SUPPORT BEAM AIRBUS320 A320231 3930325EU L2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND L2 DOOR THRESHOLD SUPPORT BEAM AT SIDEWALL CORRODED AT TWO ATTACH HOLES OF FRAME 68. REPAIRED PER AWA ER 32-53-17-03. (M) 2L72 4F RTA28NM 19951006007301995100600730EU 1995 10 6 AWXA9500613 119950908A5313 LONGERON AIRBUS320 A320231 3930325EU RAIL 765 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND T-CAP AT RAIL 765 CORRODED AT FRAME 20 FORWARD OF OUTBOARD SEAT TRACK. INSTALLED NEW LONGERON IAW SRM 51-72-11 ADN 51-42-11. (M) 2L72 4F RTA28NM 19951006007311995100600731EU 1995 10 6 AWXA9500614 119950908A5230 FITTING AIRBUS320 A320231 3930325EU FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FWD CARGO DOOR EXTERIOR HANDLE MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING PER AWA ER 32-52-30-05B. (M) 2L72 4F RTA28NM 19951006007321995100600732EU 1995 10 6 AWXA9500615 119950908A5230 FITTING AIRBUS320 A320231 3930325EU AFT CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT CARGO DOOR EXTERIOR HANDLE MOUNT FITTING CRACKED. REPAIRED PER AWA ER 32-52-30-05C. (M) 2L72 4F RTA28NM 19951006007331995100600733EU 1995 10 6 AWXA9500616 119950908A5320 THRESHOLD PLATE AIRBUS320 A320231 3930325EU R1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND R1 DOOR THRESHOLD ENTRY PLATE ATTACHMENT NUT PLATE HOLES CORRODED. INSTALLED REPLACEMENT THRESHOLD EXTRUSION PER SRM 51-72-00, PAGE 1 AND SRM 51-72-11, PAGE 1, 2. (M) 2L72 4F RTA28NM 19951006007341995100600734EU 1995 10 6 AWXA9500617 119950908A5320 ATTACH BEAM AIRBUS320 A320231 3930325EU BS 1295 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28629AW 076 PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT LAV AND GALLEY AREA FLOOR SUPPORT SEAT TRACK ATTACH BEAM CORRODED AT FASTENER HOLE AT FRAME 67 LBL 48 Y 1295. REPAIRED PER AWA ER 32-53-17-02A. (M) 2L72 4F RTA28NM 19951006007351995100600735NM 1995 10 6 CAL950679 119950707A5320 SUPPORT BOEING737 7373T0 1384582NM BS 540 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - INSPECTION FOUND A 1.5 INCH CRACK IN CABIN FLOOR SUPPORT AT BS 540, LBL 51, WL 208. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS FABRICATED AD INSTALLED IAW SRM 53-10-09. (M) 2L72 4F RTA16WE 19951006007361995100600736NM 1995 10 6 CAL950681 119950707A5315 FLOOR BEAM BOEING737 7373T0 1384582NM AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - INSPECTION FOUND INTERGRANULAR CORROSION ON FLOOR BEAM IN AFT LAV AT WL 208. THE CORRODED SECTION OF FLOOR BEAM WAS CUT OUT. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW ECRA 5310-01102. (M) 2L72 4F RTA16WE 19951006007371995100600737NM 1995 10 6 CAL950689 119950705A5320 FLOOR SUPPORT BOEING737 7373T0 1384582NM BS 727-793 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - INSPECTION FOUND CORROSION AT NUT PLATES ON FLOOR SUPPORT INBOARD OF STRINGER 26L IN AFT CARGO COMPARTMENT AT BS 727E-793. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-10-01 AND 51-30-02. (M) 2L72 4F RTA16WE 19951006007381995100600738NM 1995 10 6 CAL950690 119950705A5320 ANGLE BOEING737 7373T0 1384582NM BS 794 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432430220 23375 DHN - INSPECTION FOUND CORROSION ON ANGLE IN AFT CARGO BILGE AREA AT STATION 794, ABOVE STRINGER 26R. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. (M) 2L72 4F RTA16WE 19951006007391995100600739WP 1995 10 6 CAL950804 119950827A5313 LONGERON DOUG DC9 DC932 3022066WP BS 945-960 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091452463881 47539 HOU - INSPECTION FOUND CORROSION ON LONGERON 26L BETWEEN STATION 945-960. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE INSTALLED IAW SRM 51-30-2. (M) 2L72 4F A6WE 19951006007401995100600740WP 1995 10 6 CAL950805 119950824A5712 RIB DOUG DC9 DC932 3022066WP WS 501 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091452463881 47539 HOU - INSPECTION FOUND THREE .25 INCH CRACKS IN WING LEADING EDGE RIB AT STATION XRS 501. A DOUBLER, FILLER, AND CLIP WERE FABRICATED AND INSTALLED IAW ECRA 5720-01260. (M) 2L72 4F A6WE 19951006007411995100600741WP 1995 10 6 CAL950812 119950827A5320 ANGLE DOUG DC9 DC982 3022082WP BS 46 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD SIDE OF ANGLE AT NOSE WHEEL WELL FORWARD RIGHT SIDE STATION 46 DOOR JAMB. THE ANGLE WAS REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 4. (M) 2L72 4F A6WE 19951006007421995100600742WP 1995 10 6 GRAA9540 119950716A3350 EEL LENS DOUG DC9 DC987 3022087WP CABIN BROKEN A GRAAK NONE O OTHER ININSP/MAINT 1 WP111075T 49724 AT IFP, WHEN PASSENGERS WERE DEBOARDING, ONE EACH EMERGENCY LIGHT LENS WAS BROKEN. THE EMERGENCY LIGHT WAS DEFERRED IAW MEL 33-24. ON THE 25TH OF JULY, THE LENS WAS REPLACED AND THE DMI WAS CLOSED. (M) 2L72 4F RTA6WE 19951006007431995100600743WP 1995 10 6 GRAA9541 119950906A213121171802 CONTROLLER DOUG DC9 DC987 3022087WP E/E COMPARTMENT MALFUNCTIONED A GRAAO OTHER J WARNING INDICATION CRCRUISE 1 WP111075T 49724 WHILE FLYING AT 35,000 FEET OVER ROCK SPRINGS WYOMING, A/C WAS OPERATING ON THE STANDBY AUTO PRESSURE CONTROLLER WHEN THE AIRCRAFT BEGAN TO LOSE CABIN PRESSURE. THE PILOT BEGAN TO DESCEND THE A/C AND SWITCHED TO THE PRIMARY AUTO PRESSURE CONTROLLER AND CONTINUED TO SALT LAKE CITY, UTAH. UPON ARRIVAL INTO SALT LAKE, MAINTENANCE TROUBLESHOT THE SYSTEM AND THE STANDBY AUTO PRESSURE CONTROLLER FAILED THE TEST. MAINTENANCE DMI'D THE SYSTEM IAW MEL 21-24. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951006007441995100600744SW 1995 10 6 MALA954581 119950813A52102724043035 CORNER FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR DENTED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, THE PASSENGER DOOR LOWER FRAME WAS FOUND TO BE DENTED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER FRAME, P/N 27-24044-009, STRAIGHT FRAME, P/N 27-24043-003, AND STRAIGHT FRAME, P/N 27-24043-035 IAW FAC SRM 51-00-00 PAGE 4 PART FOR PART REPLACEMENT, 51-40-51, 51-40-02 STANDARD PRACTICES. (M) 1L72 4T A8SW 19951006007451995100600745NM 1995 10 6 MALA954582 119950810A3350 EEL DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15849MA 347 DURING A PREFLIGHT INSPECTION IN DTW, THE CREW NOTED THAT NUMEROUS FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE RESET THE EMERGENCY FLOOR TRACK LIGHTING CIRCUIT BREAKER. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951006007461995100600746NM 1995 10 6 MALA954583 119950811A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15849MA 347 DURING THE PREFLIGHT IN DTW, THE FLIGHT ATTENDANT REPORTED THAT SEVERAL FLOOR TRACK LIGHTS WERE INOP. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT FORWARD BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951006007471995100600747SW 1995 10 6 MALA954584 119950814A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 438.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15158MC AC762B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME, FS 438.060, TO BE CRACKED AT THE GAS SPRING ATTACH LUG HOLE. REPAIRS WERE COMPLETED BY INSTALLING REPAIR DOUBLERS IAW FAC ARP 53-20-9503 AND LAR 95-MALA-216. (M) 1L72 4T A8SW 19951006007481995100600748SW 1995 10 6 MALA954585 119950816A57532731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW RT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER IAW FAC 57-10-9207 AND ARP 57-20-9024. (M) 1L72 4T A8SW 19951006007491995100600749NM 1995 10 6 MALA954586 119950818A33506104781 EEL BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15831MA 339 FLT NR 3407 - DURING THE PREFLIGHT IN DTW, THE CREW NOTED THAT THE EMERGENCY EXIT SIGN BY SEAT 1E DIDN'T ILLUMINATE. MAINTENANCE REPLACED THE LOWER WARDROBE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951006007501995100600750SW 1995 10 6 MALA954591 119950818A2432235761 BATTERY SWRNGNSA227 SA227AC 8780603SW LEFT WING FAILED A MALAO OTHER J WARNING INDICATION CRCRUISE 1 GL15425MA AC640 FLT NR 3245 - IN CRUISE FLIGHT TO MSP, THE LEFT BATTERY HOT LIGHT ILLUMINATED. THE CREW DISCONNECTED THE BATTERY AND CONTINUED TO MSP. MAINTENANCE REPLACED THE LEFT BATTERY. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007511995100600751SW 1995 10 6 MALA954592 119950821A5297 WIRE SWRNGNSA227 SA227AC 8780603SW CARGO DOOR BROKEN A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL152693C AC659B FLT NR 3356 - ON CLIMB-OUT FROM DTW, THE CARGO DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE RESECURED A BROKEN WIRE AT THE TOP OF THE DOOR. SYSTEM OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19951006007521995100600752SW 1995 10 6 MALA954594 119950821A52102724158007 BELLCRANK SWRNGNSA227 SA227AC 8780603SW CABIN DOOR WORN A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15159MC AC728B FLT NR 3213 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT AND RIGHT UPPER BAYONET BELLCRANK ASSY. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007531995100600753SW 1995 10 6 MALA954596 119950821A32602782186057 INDICATOR SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15439MA AC722 FLT NR 3240 - ON APPROACH TO MSP, THE RIGHT MAIN GEAR INTRANSIT LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LANDING GEAR INDICATOR. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007541995100600754NM 1995 10 6 MALA954597 119950822A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15849MA 347 FLIGHT 3442 - DURING THE PREFLIGHT IN DTW, THE EMERGENCY LIGHT IN THE COCKPIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951006007551995100600755SW 1995 10 6 MALA954598 119950822A54002735112032 ANGLE SWRNGNSA227 SA227AC 8780603SW LEFT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B DURING A SCHEDULED INSPECTION IN MSP, THE LEFT INBOARD WING TO NACELLE TRANSIT ANGLE WAS CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101. (M) 1L72 4T A8SW 19951006007561995100600756SW 1995 10 6 MALA954599 119950822A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 491.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1527465 AC755B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FUSELAGE/CARGO DOOR LEFT FRAME CRACKED AT GAS STRUT MOUNT POST HOLE AT FS 491.060. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 53-20-9503. (M) 1L72 4T A8SW 19951006007571995100600757SW 1995 10 6 MALA954600 119950822A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15436MA AC719 FLT 3186 - ON APPROACH TO DTW, THE RIGHT INTRANSIT LIGHT DIDN'T ILLUMINATE DURING GEAR EXTENSION. MAINTENANCE CLEANED THE GEAR POSITION SWITCHES. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007581995100600758SW 1995 10 6 MALA954602 119950824A7931 OIL PRESS TRANS SWRNGNSA227 SA227AC 8780603SW RT ENGINE MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15159MC AC728B FLT NR 3075 - ON CLIMB-OUT FROM MSP, THE CREW NOTED THAT THE RIGHT OIL PRESSURE GAUGE WAS FLUCTUATING ERRATICALLY BETWEEN 10 PSI AND 100 PSI. ALL OTHER INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED GROUND RUNS AT CRUISE POWER FOR SEVERAL MINUTES BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. MAINTENANCE ALSO INSPECTED THE TRANSMITTER CANNON PLUG AND ASSOCIATED WIRING WITH NO DISCREPANCIES NOTED. THE TRANSMITTER WAS REPLACED FOR PRECAUTIONARY MEASURES. SYSTEM OPERATED SATISFACTORILY DURING GROUND RUNS. (M) 1L72 4T A8SW 19951006007591995100600759NE 1995 10 6 MALA954603 219950824A732043M03108NM03108NROTARY SWITCH DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15866MA 366 FLIGHT 3005 - IN CRUISE FLIGHT TO BMI, THE ENGINE INDICATIONS FOR THE NR 1 ENGINE BEGAN TO FLUCTUATE WITH THE ECU ON. THE CREW TURNED OFF THE ECU AND THE INDICATIONS STABILIZED. THE AIRCRAFT RETURNED DTW. MAINTENANCE REPLACED AN ENGINE TRIM SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T4 TRTA13NM E20NE 19951006007601995100600760SW 1995 10 6 MALA954609 119950826A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15424MA AC639 FLT NR 3019 - ON APPROACH TO DTW, THE LEFT GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. THE CREW RECYCLED THE GEAR AND A NORMAL INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR OUTBOARD INDICATION SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007611995100600761SW 1995 10 6 MALA954610 119950827A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW LT MLG FAILED A MALAK NONE O OTHER APAPPROACH 1 GL15438MA AC721B FLT NR 3255 - ON APPROACH TO MSP, THE LEFT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING THE GEAR RETRACTION. MAINTENANCE REPLACED THE LEFT INBOARD DOWN AND LOCKED SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951006007621995100600762SW 1995 10 6 MALA954611 119950829A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 491 TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M) 1L72 4T A8SW 19951006007631995100600763WP 1995 10 6 USAA950800 119950718A5320 FRAME DOUG DC9 DC931 3022065WP AFT VENTRAL DOORCRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19987VJ70957 47210 PIT - DURING RON CHECK, FOUND A 2 INCH CRACK AT AFT VENTRAL DOOR LEFT SIDE ABOVE TOP LEFT DOOR STOP. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 30. (M) 2L72 4F A6WE 19951006007641995100600764WP 1995 10 6 USAA950801 119950718A5320 JAMB DOUG DC9 DC931 3022065WP VENTRAL DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19987VJ70957 47210 PIT - DURING RON CHECK MAINTENANCE, FOUND A 1.5 INCH CRACK IN THE TOP LEFT CORNER OF THE VENTRAL DOOR JAM. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 29. (M) 2L72 4F A6WE 19951006007651995100600765WP 1995 10 6 USAA950802 119950706A53205912494501 JAMB DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US36727 48099 IND - DURING CX-6 CHECK INSPECTION, FOUND 1 INCH SQUARE AREA OF CORROSION WITH .125 INCH CRACK IN FORWARD CARGO DOOR JAM LOWER PAN. ACCOMPLISHED DOUBLER REPAIR PER USAIR EA 30892 AND SRM 53-05 FIG NR 44. (M) 2L72 4F A6WE 19951006007661995100600766WP 1995 10 6 Y2PA950012 119950830A27514916554501 GUIDE BAR DOUG DC9 DC915F 3022037WP RT TE FLAP VANE WORN A Y2PAK NONE O OTHER ININSP/MAINT 1 GL23198US42814 47045 YIP - DURING ROUTINE INSPECTION, SEVERE CHAFFING WAS NOTED ON THE RIGHT WING INBOARD FLAP MOVEABLE VANE, FORWARD GUIDE BAR. REPLACED RIGHT MOVEABLE VANE GUIDE BAR AND CHECKED THE RIGGING PER THE DC9 MM CHAPTER 27-51. (M) 2L72 4F A6WE 19951006007671995100600767NM 1995 10 6 CAL950537 119950613A5320 CHORD BOEING737 737130 1384435NM LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091420964151 19026 STA 31J - INSPECTION FOUND A 14 INCH CRACK IN THE LEFT MLG WHEEL WELL AFT BULKHEAD LOWER CIRCUMFERENTIAL ANGLE (PREVIOUSLY STOP DRILLED). THE CHORD WAS REPLACED IAW SERVICE BULLETIN 737-53-1088 AND ECRA 5310-03133. (M) 2L72 4F A16WE 19951006007681995100600768NM 1995 10 6 CAL950539 119950613A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT RBL 5-10.5, WL 208, STATION 986.5. REMOVED CORRODED SECTION OF CHORD AND REPAIRED WITH NEW CHORD SPLICE PER SRM 53-60-51, MM 51-21-41, 51-21-99, AND 51-10-02. (M) 2L72 4F RTA16WE 19951006007691995100600769NM 1995 10 6 CAL950540 119950613A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON FLOOR BEAM AT BS 344, LBL 15 TO RBL 5. REMOVED CORRODED CHORD AND INSTALLED NEW CHORD IAW SRM 51-20-01, 51-40-02, 51-40-08, 51-70-09, AND MM 51-21-41. (M) 2L72 4F RTA16WE 19951006007701995100600770NM 1995 10 6 CAL950541 119950613A5320 INTERCOSTAL BOEING737 7373T0 1384582NM BS 312-328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON INTERCOSTAL FROM BS 312-328, LBL 12, WL 208. THE CORRODED SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-10-02, 51-21-41, 51-21-99, AND 51-10-2. (M) 2L72 4F RTA16WE 19951006007711995100600771NM 1995 10 6 CAL950542 119950613A5320 BEAM BOEING737 7373T0 1384582NM BS 1006-1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON BEAM AT STATION 1006-1016, LBL 7, WL 208. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 19951006007721995100600772NM 1995 10 6 CAL950543 119950613A5320 INTERCOSTAL BOEING737 7373T0 1384582NM BS 1011-1013 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON BOTTOM INTERCOSTAL AT STATION 1011-1013, WL 208, RBL 6. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-2 AND 51-40-2. (M) 2L72 4F RTA16WE 19951006007731995100600773NM 1995 10 6 CAL950544 119950613A5315 CHORD BOEING737 7373T0 1384582NM BS 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON FLOOR BEAM UPPER CHORD AT BS 1016, WL 208, RBL 16-23. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 19951006007741995100600774NM 1995 10 6 CAL950545 119950613A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 294.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION AND ELONGATED HOLES ON TOP OF FLOOR BEAM CHORD AT BS 294.5, LBL 19 TO RBL 9, WL 208. THE CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51, 51-40-02, 51-20-01, 51-40-08, AND 51-70-09. (M) 2L72 4F RTA16WE 19951006007751995100600775NM 1995 10 6 CAL950546 119950613A5320 BEAM BOEING737 7373T0 1384582NM BS 996-1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096031231288 23363 PAE - INSPECTION FOUND CORROSION ON BEAM AT STATION 996-1006, LBL 10, WL 208. REMOVED AND REPLACED BEAM IAW SRM 51-40-02. (M) 2L72 4F RTA16WE 19951006007761995100600776NM 1995 10 6 CAL950549 119950616A3230654654321 UPLOCK FITTING BOEING737 7373T0 1384582NM BS 685 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0963305 23356 YVR - INSPECTION FOUND THE LEFT MLG FORWARD ATTACH LUG (BODY LUG AT STATION 685) CORRODED IN AND AROUND THE BORE. THE BORE WAS REAMED, UNEVEN AREAS WERE REAMED, AND FACES SPOTFACED. SHOT PEENED AND FABRICATED AND INSTALLED REPAIR SLEEVE. SPOTFACED FILLERS, FABRICATED AND INSTALLED. (M) 2L72 4F RTA16WE 19951006007771995100600777NM 1995 10 6 CAL950550 119950616A3230654654322 UPLOCK FITTING BOEING737 7373T0 1384582NM BS 685 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0963305 23356 YVR - THE RIGHT MLG FORWARD UPLOCK BODY LUG, STATION 685, WAS FOUND CORRODED. BORE REAMED, BLENDED UNEVEN AREAS, AND FACES SPOTFACED. SHOT PEENED AND FABRICATED AND INSTALLED REPAIR SLEEVE. SPOT FACED FILLERS AND FABRICATED AND INSTALLED. (M) 2L72 4F RTA16WE 19951006007781995100600778NM 1995 10 6 CAL950551 119950612A534750D5328185 CARGO TRACK BOEING737 7373T0 1384582NM BS 460-480 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096330530305 23356 YVR - INSPECTION FOUND A 20 INCH CRACK IN FORWARD CARGO FLOOR TRACK AT STATION 460-480, RBL 14. THE TRACK WAS REPLACED AND SPLICED PER DRAWING 50D53-28185 AND ECRA 5320-01387. (M) 2L72 4F RTA16WE 19951006007791995100600779NM 1995 10 6 CAL950555 119950630A5311 FRAME BOEING737 7372C0 1384488NM BS 460 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND THE FRAME AT BS 460 CRACKED BETWEEN S22L AND S21L AND BETWEEN S21L AND S20L. BOTH CRACKS WERE .5 INCH LONG. A NEW FRAME AND SPLICE WERE INSTALLED IAW B737 DRAWING 65C25113-7. (M) 2L72 4F A16WE 19951006007801995100600780NM 1995 10 6 CAL950556 119950630A5311 FRAME BOEING737 7372C0 1384488NM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 500. A NEW FRAME AND FASTENERS WERE INSTALLED IAW B737 DRAWING 65C25113-A AND SRM 51-30-2. (M) 2L72 4F A16WE 19951006007811995100600781NM 1995 10 6 CAL950557 119950630A5313 STRINGER BOEING737 7372C0 1384488NM BS 355 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND STRINGER 22R CORRODED AT BS 355. A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-30-2. (M) 2L72 4F A16WE 19951006007821995100600782NM 1995 10 6 CAL950558 119950630A5311 FRAME BOEING737 7372C0 1384488NM BS 420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 420 BETWEEN S20L AND S21L AND A .5 INCH CRACK IN FRAME AT BS 420 S22L. REPAIR WAS INSTALLED IAW BOEING DRAWING 65C25113A AND SRM 51-30-2. (M) 2L72 4F A16WE 19951006007831995100600783NM 1995 10 6 CAL950559 119950630A5311 FRAME BOEING737 7372C0 1384488NM BS 400 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 400 BETWEEN S20L AND S21L. A NEW FRAME AND FASTENERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C25113-A AND SRM 51-30-2. (M) 2L72 4F A16WE 19951006007841995100600784NM 1995 10 6 CAL950560 119950630A5320 SUPPORT BOEING737 7372C0 1384488NM BS 887-907 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND CORROSION ON FLOOR SUPPORT PANEL ABOVE S25L BETWEEN BS 887 AND BS 907. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M) 2L72 4F A16WE 19951006007851995100600785NM 1995 10 6 CAL950561 119950630A5320 FLOOR SUPPORT BOEING737 7372C0 1384488NM BS 540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK IN CABIN FLOOR SUPPORT AND ANGLE AT BS 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M) 2L72 4F A16WE 19951006007861995100600786NM 1995 10 6 CAL950562 119950630A5320 INTERCOSTAL BOEING737 7372C0 1384488NM BS 847-867 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND CORROSION ON INTERCOSTAL FLANGE AT STATION 847-867 BELOW STRINGER 24. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (M) 2L72 4F A16WE 19951006007871995100600787NM 1995 10 6 CAL950564 119950630A5511 RIB BOEING737 7372C0 1384488NM LT HORIZ STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK IN INBOARD SIDE NR 5 RIB FROM THE FRONT OF THE LEFT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 55-10-4, AND 51-10-1. (M) 2L72 4F A16WE 19951006007881995100600788NM 1995 10 6 CAL950565 119950630A5330 SKIN BOEING737 7372C0 1384488NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT FORWARD ENTRY DOOR LOWER FRAME SKIN. THE SKIN WAS REPAIRED IAW ECRA 5330-02294 AND BAC DRAWING 65C27257. (M) 2L72 4F A16WE 19951006007891995100600789NM 1995 10 6 CAL950568 119950630A5330 SKIN BOEING737 7372C0 1384488NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN ON RIGHT SIDE AT STATION 727 BELOW S18. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING 65C28086 AND SERVICE BULLETIN 737-53-1077. (M) 2L72 4F A16WE 19951006007901995100600790NM 1995 10 6 CAL950569 119950630A5311 FRAME BOEING737 7372C0 1384488NM BS 639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK THROUGH INBOARD CHORD AND WEB OF STATION 639 FRAME AT STRINGER 16R. A NEW CHORD AND WEB WERE INSTALLED PER BOEING DRAWING 65C31658. (M) 2L72 4F A16WE 19951006007911995100600791NM 1995 10 6 CAL950570 119950630A5320 STRINGER TIES BOEING737 7372C0 1384488NM BS 597 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND STRINGER TIES AT STATION 597 STRINGERS 5R, 4R, AND 4L CRACKED. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (M) 2L72 4F A16WE 19951006007921995100600792NM 1995 10 6 CAL950571 119950630A5320 ANGLE BOEING737 7372C0 1384488NM BS 291-294 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK IN RT OUTBOARD STIFFENER ANGLE AT STATION 291 TO 294. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-0. (M) 2L72 4F A16WE 19951006007931995100600793NM 1995 10 6 CAL950572 119950630A5320 TEAR STRAP BOEING737 7372C0 1384488NM BS 752 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .5 INCH CRACK IN TEAR STRAP AT FASTENER HOLE RT STATION 752 BELOW STRINGER 14. A NEW TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M) 2L72 4F A16WE 19951006007941995100600794NM 1995 10 6 CAL950573 119950630A5320 WEB BOEING737 7372C0 1384488NM BS 947 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A 2 INCH CRACK IN WEB AT BS 947 FORWARD OF R-2 DOOR. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M) 2L72 4F A16WE 19951006007951995100600795NM 1995 10 6 CAL950575 119950630A5320 STRINGER TIES BOEING737 7372C0 1384488NM BS 767 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND STRINGER TIES CRACKED AT STATION 767 STRINGERS 4L AND 5L. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2L72 4F A16WE 19951006007961995100600796NM 1995 10 6 CAL950576 119950630A5320 STRINGER TIES BOEING737 7372C0 1384488NM BS 685 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF THE STRINGER TIES AT STRINGERS 5R, 2L, 3L, AND 4L, STATION 685. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2L72 4F A16WE 19951006007971995100600797NM 1995 10 6 CAL950577 119950630A5320 WEB BOEING737 7372C0 1384488NM BS 638-663 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .5 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 638 AND 663L. A WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M) 2L72 4F A16WE 19951006007981995100600798NM 1995 10 6 CAL950578 119950630A5320 STRINGER TIES BOEING737 7372C0 1384488NM BS 702 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF TWO STRINGER TIES AT STRINGERS 4L AND 4R, STATION 702. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M) 2L72 4F A16WE 19951006007991995100600799NM 1995 10 6 CAL950579 119950630A5320 WEB BOEING737 7372C0 1384488NM BS 616-639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091424168543 20070 GSO - INSPECTION FOUND A .75 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 616 AND 639L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M) 2L72 4F A16WE 19951006008001995100600800NM 1995 10 6 CAL950632 119950801A3350 EEL WIRING BOEING727 727232 1384082NM CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0977780 20635 IAH - FLT NR 0650 - INSPECTION FOUND SEVERAL SECTION OF CABIN EMERGENCY AISLE LIGHTING INOPERATIVE. MAINTENANCE REPAIRED BROKEN AISLE LIGHTING WIRING AND OPERATION OF THE EMERGENCY AISLE LIGHTS WAS RESTORED. (M) 2L73 4F A3WE 19951006008011995100600801NM 1995 10 6 CAL950634 119950731A52306546921528 DOOR BOEING737 7373T0 1384582NM CARGO COMPT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091231331757 23364 CLE - INSPECTION FOUND A 2 INCH CRACK IN FORWARD CARGO DOOR, ZONE 209. AN REINFORCEMENT ANGLE WAS INSTALLED ON THE CARGO DOOR IAW DRAWING SA005-5230-01027. (M) 2L72 4F RTA16WE 19951006008021995100600802 1995 10 6 CAL950635 419950731A2210 TRANSDUCER BOEING737 7372C0 1384488NM E/E COMPT INOPERATIVE A CALAO OTHER F FLT CONT AFFECTED CLCLIMB 1 SW0910242 20071 FLT NR 1405 - ATL - THE AIRCRAFT HAD A SLIGHT YAW AFTER TAKEOFF FROM EWR. THE RANGE OF THE YAW GREW AS SPEED INCREASED. THE YAWING STOPPED AFTER THE YAW DAMP SWITCH WAS POSITIONED TO OFF. MAINTENANCE FOUND THE RUDDER PCU 'B' POSITION TRANSDUCER OPEN. THE TRANSDUCER WAS REMOVED AND REPLACED IAW MM 22-11-51, PAGE 501. OPERATIONAL CHECKS WERE GOOD WITH NO OTHER DEFECTS FOUND. (M) 2L72 4F A16WE 19951006008031995100600803NM 1995 10 6 CAL950640 119950802A5321 FLOOR BOEING737 7373T0 1384582NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096931130313 23362 HOU - INSPECTION FOUND A 48 INCH BY 2 INCH AREA OF THE CABIN CENTER FLOOR STRUCTURE CORRODED AT STATION 312. THE AREA WAS REPAIRED PER SRM 53-10-51, FIGURE 205. (M) 2L72 4F RTA16WE 19951006008041995100600804NM 1995 10 6 CAL950643 119950802A5330 SKIN BOEING737 7373T0 1384582NM BS 1006 TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW0969311 23362 HOU - THE FUSELAGE SKIN WAS TORN WHEN CONTACTED BY A STAND WHILE AIRCRAFT WAS IN D-CHECK MAINTENANCE. THE TEAR WAS LOCATED AT STATION 1006, STRINGER 4R-5R. THE SKIN WAS REPAIRED IAW ECRA 5330-02306. (M) 2L72 4F RTA16WE 19951006008051995100600805NM 1995 10 6 CAL950651 119950731A3350 EEL BATTERY BOEING727 727243 138408DNM R-1 DOOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0934415 22167 DEN - INSPECTION FOUND EMERGENCY EXIT LIGHT AT THE R-1 DOOR INOPERATIVE. THE BATTERY WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (M) 2L73 4F RTA3WE 19951006008061995100600806NM 1995 10 6 CAL950654 119950805A5311 FRAME BOEING737 737214 138446RNM BS 460 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423964964 19920 GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STATION 460L AND STRINGERS 21L-22L. CUT OUT DAMAGE AND INSTALLED A NEW FRAME, CHORD AND SPLICES IAW SRM 51-30-2 AND BOEING DRAWING 65C25113. (M) 2L72 4F A16WE 19951006008071995100600807NM 1995 10 6 CAL950656 119950805A5311 FRAME BOEING737 737214 138446RNM BS 420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423964964 19920 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 420L BETWEEN STRINGERS 20L-21L. THE DAMAGE WAS CUT OUT AND A NEW FRAME, CHORD, AND SPLICES WERE INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 65C25113. (M) 2L72 4F A16WE 19951006008081995100600808NM 1995 10 6 CAL950657 119950805A5241 FRAME BOEING737 737214 138446RNM GALLEY DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423964964 19920 GSO - INSPECTION FOUND A .75 INCH CRACK IN FORWARD GALLEY DOOR LOWER SIDE OF FRAME AT LOWER FORWARD STOP FITTING. THE CRACKED SEGMENT OF FRAME WAS REMOVED. A NEW SEGMENT WAS INSTALLED PER ECRA 5240-01089 AND BAC DRAWING 69-69680. (M) 2L72 4F A16WE 19951006008091995100600809NM 1995 10 6 CAL950658 119950805A5315 FLOOR BEAM BOEING737 737214 138446RNM BS 250 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091423964964 19920 GSO - INSPECTION FOUND CORROSION ON FLOOR BEAM UNDER COCKPIT FLOOR PANEL AT STATION 250, BBL 0. A WEB AND FILLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-40-4. (M) 2L72 4F A16WE 19951006008101995100600810NM 1995 10 6 CAL950659 119950805A5311 FRAME BOEING737 737214 138446RNM BS 639 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09142396496464964 19920 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 639R, STRINGER 16. REMOVED CRACKED UPPER CHORD AND FRAME WEB AND INSTALLED REPAIR PARTS IAW BOEING DRAWING NR 65C31658 AND SRM 51-30-2. (M) 2L72 4F A16WE 19951006008111995100600811NM 1995 10 6 CAL950661 119950805A5311 FRAME BOEING737 737214 138446RNM BS 440L CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09142396496464964 19920 GSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STATION 440L BETWEEN STRINGERS 19L-20L. THE CRACKED FRAME SECTION WAS CUT OUT. A NEW FRAME AND CHORD SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING NR 65C27113. (M) 2L72 4F A16WE 19951006008121995100600812NM 1995 10 6 CAL950719 119950808A3350 EEL BATTERY BOEING727 727232 1384082NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916784 20639 DEN - THE RIGHT SIDE ESCAPE HATCH EXIT SIGN BATTERY PACK FAILED CAPACITY TEST. THE BATTERY WAS REMOVED AND REPLACED. (M) 2L73 4F A3WE 19951006008131995100600813NM 1995 10 6 CAL950720 119950808A3350 EEL BATTERY BOEING727 727232 1384082NM EXIT SIGN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916784 20639 DEN - THE LEFT SIDE ESCAPE HATCH EXIT SIGN BATTERY PACK FAILED CAPACITY TEST. THE BATTERY WAS REMOVED AND REPLACED. (M) 2L73 4F A3WE 19951006008141995100600814NM 1995 10 6 CAL950721 119950808A3350 EEL BATTERY BOEING727 727232 1384082NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916784 20639 DEN - THE AIRSTAIR FIXED EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. THE BATTERY WAS REMOVED AND REPLACED. (M) 2L73 4F A3WE 19951006008151995100600815NM 1995 10 6 CAL950722 119950808A33506104789 EEL BATTERY BOEING727 727232 1384082NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916784 20639 DEN - THE FORWARD EMERGENCY EXIT SLIDE BATTERY PACK FAILED CAPACITY TEST. THE BATTERY WAS REMOVED AND REPLACED. (M) 2L73 4F A3WE 19951006008161995100600816 1995 10 6 CAL950760 419950826A34449650376079 GPWS COMPUTER BOEING727 727232 1384082NM E/E RACK INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW09523PE26347 20646 FLT NR 0219 - EWR - THE GPWS SOUNDED AT 300 FEET WITH FLAPS SET AT 30 DEGREES WHILE ON APPROACH TO EWR. A 'GO AROUND' WAS PERFORMED AND ON THE NEXT APPROACH THERE WAS NO GPWS WARNING WITH THE SAME CONDITIONS. THE GPWS COMPUTER WAS REMOVED AND REPLACED IAW MM 34-52-11 AND SYSTEM OPERATION CHECKED GOOD. (M) 2L73 4F A3WE 19951006008171995100600817WP 1995 10 6 CAL950792 119950905A25308101280000B OVEN DOUG DC10 DC1030 3023501WP GALLEY DIRTY A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0968065 46590 FLT NR 0050 - FRA - THE FORWARD GALLEY OVEN NEXT TO LEFT AISLE BEGAN PRODUCING SMOKE IN FLIGHT. THE SMOKE CEASED SHORTLY AFTER OVEN POWER WAS REMOVED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND FOOD CONTAMINATING THE HEATING ELEMENT OF THE FORWARD GALLEY OVEN AT POSITION 308. THE OVEN WAS PLACARDED INOPERATIVE. (M) 2L73 4F A22WE 19951006008181995100600818WP 1995 10 6 CAL950803 119950827A5313 LONGERON DOUG DC9 DC932 3022066WP BS 937-945 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091452463881 47539 HOU - INSPECTION FOUND CORROSION ON LONGERONS 26L TO 28L IN AFT BAGGAGE BIN BETWEEN STATION 937-945. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE REPLACED IAW SRM 51-30-2. (M) 2L72 4F A6WE 19951006008191995100600819WP 1995 10 6 CAL950808 119950829A5712 RIB DOUG DC9 DC982 3022082WP LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A 1 INCH CRACK IN RIB AT LEFT WING LEADING EDGE OUTBOARD OF NR 9 SLAT TRACK. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-01 AND 51-30-5. (M) 2L72 4F A6WE 19951006008201995100600820WP 1995 10 6 CAL950809 119950828A5320 CUSP MEMBRANE DOUG DC9 DC982 3022082WP BS 1287-1309 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A 6 INCH CRACK ON CUSP MEMBRANE BETWEEN STATION 1287 AND 1309 ON RT SIDE. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05. (M) 2L72 4F A6WE 19951006008211995100600821WP 1995 10 6 CAL950810 119950828A5720 DOUBLER DOUG DC9 DC982 3022082WP LT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A .5 INCH CRACK IN LEFT WING LEADING EDGE SPLICE DOUBLER BETWEEN NR 5 AND NR 6 SLAT TRACKS. THE AREA WAS REPAIRED IAW ECRA 5710-01645. (M) 2L72 4F A6WE 19951006008221995100600822WP 1995 10 6 CAL950811 119950828A5320 GUSSET DOUG DC9 DC982 3022082WP BS 993 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A .75 INCH CRACK IN RADIUS OF GUSSET AT STATION 993 IN RT WHEEL WELL AFT OF FUEL FEED. THE CRACK WAS STOP DRILLED AND A STACKED DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (M) 2L72 4F A6WE 19951006008231995100600823WP 1995 10 6 CAL950813 119950827A5320 ANGLE DOUG DC9 DC982 3022082WP BS 46 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD SIDE OF ANGLE AT NOSE WHEEL WELL FORWARD LEFT SIDE STATION 46 DOOR JAMB. THE ANGLE WAS REPAIRED IAW SRM 53-01, FIGURE 2, SHEET 4. (M) 2L72 4F A6WE 19951006008241995100600824NM 1995 10 6 CAL950827 119950905A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 986.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND CORROSION ON FLOOR BEAM AT STATION 986.5 FROM BL 0 TO ABOUT 12 INCHES LEFT OF BL 0 AND 14 INCHES RIGHT OF BL 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-51. (M) 2L72 4F RTA16WE 19951006008251995100600825NM 1995 10 6 CAL950828 119950814A5400313A1355649 CHANNEL BOEING737 7373T0 1384582NM LT PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432528791 23455 HOU - INSPECTION FOUND A 10 INCH CRACK IN LEFT PYLON SPAR WEB CHANNEL ON INBOARD EDGE AT STATION 305-315. THE AREA WAS REPAIRED IAW SRM 51-10-02 AND IN REF TO BOEING DRAWING NR 313A1355. (M) 2L72 4F RTA16WE 19951006008261995100600826NM 1995 10 6 CAL950829 119950905A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND CORROSION ON FLOOR BEAM AROUND SCREW HOLES IN AREA OF RIGHT SIDE FLOOR TRACKS AT STATION 328. A NEW FLOOR BEAM SECTION WAS SPLICED IN PER SRM 53-10-51, FIGURE 205. (M) 2L72 4F RTA16WE 19951006008271995100600827WP 1995 10 6 95ZZZM520 119950912A5320 ANGLE LKHEED1011 10113851 5265010WP FS 1363 CRACKED A WRNAK NONE O OTHER ININSP/MAINT 1 SO05311EA39150 193A1012 DURING NORMAL SERVICING OF ATM, MAINTENANCE NOTICED A CRACK LOCATED AT FS 1363 WL 147 (APPROXIMATELY) ON THE RIGHT SIDE. ANGLE 1561639-101 REPAIRED IAW SRM 53-11-00 FIG 822. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A23WE 19951006008281995100600828WP 1995 10 6 95ZZZM521 119950907A323136548875001 VALVE DOUG DC8 DC863F 302198FWP LT MLG DOOR FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19661AV 45969 TWENTY MINUTES INTO FLIGHT FROM MIA, LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. COULD NOT EXTINGUISH LIGHT, AIRCRAFT RETURNED TO MIA WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING DETERMINED MLG DOOR 'J' HANDLE TO BE INTERNALLY BYPASSING (MLG DOOR CONTROL VALVE). REMOVED AND REPLACED VALVE. OPS CHECKED NORMAL. (M) 2L74 4F 4A25 19951006008291995100600829WP 1995 10 6 AALA951597 119950905A3350A3060720204 EEL CONDUCTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07274AA 49271 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951006008301995100600830EU 1995 10 6 AALA951617 119950910A3350A3030398101 EEL CONNECTOR FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071412A 11370 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19951006008311995100600831NM 1995 10 6 AALA951625 119950911A3350A3060819104 EEL STRIP BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07843AA 20984 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 16D AND 19D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 16D AND 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951006008321995100600832WP 1995 10 6 CAL950538 119950626A5320 JAMB DOUG DC9 DC932 3022066WP AFT VENTRAL DOORCRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093350645574 47765 HOU - A ONE INCH CRACK WAS FOUND IN THE AFT VENTRAL DOOR JAMB BEHIND THE TOP RIGHT DOOR STOP. THE DOOR JAMB WAS REPAIRED IAW ECRA 653C0116. (M) 2L72 4F A6WE 19951006008331995100600833NM 1995 10 6 CAL950744 119950816A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 986-1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432031637 23371 IAH - INSPECTION FOUND CORROSION ON FLOOR BEAM OF L-2 DOOR THRESHOLD AT STATION 986-1006. THE AREA WAS REPAIRED IAW SRM 51-40-01. (M) 2L72 4F RTA16WE 19951006008341995100600834NM 1995 10 6 CAL950748 119950810A5313 STRINGER BOEING737 737217 1384464NM BS 947.5-986 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223072995 19884 MIA - INSPECTION FOUND CORROSION ON STRINGER 27R IN AFT BILGE INTERIOR AREA FROM STATION 947.5 TO 986. THE CORRODED AREA WAS CUT OUT. FILLER AND SPLICES WERE FABRICATED AND INSTALLED PER SRM 53-10-3. (M) 2L72 4F A16WE 19951006008351995100600835NM 1995 10 6 CAL950749 119950818A5313 STRINGER BOEING737 737217 1384464NM BS 947.5-967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223072995 19884 MIA - INSPECTION FOUND CORROSION ON STRINGER 27L FROM STATION 947.5 TO 967. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-3. (M) 2L72 4F A16WE 19951006008361995100600836NM 1995 10 6 CAL950755 119950816A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 1016 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432031637 23371 IAH - INSPECTION FOUND CORROSION ON TOP OF FLOOR BEAM AT STATION 1016, LBL 5.5. THE FLOOR BEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 202 AND ECRA 5310-03151. (M) 2L72 4F RTA16WE 19951006008371995100600837NM 1995 10 6 CAL950756 119950816A5320 ANGLE BOEING737 7373T0 1384582NM BS 1014 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432031637 23371 IAH - INSPECTION FOUND WALL SUPPORT ANGLE CORRODED AT STATION 1014, RBL 4.54. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-2. (M) 2L72 4F RTA16WE 19951006008381995100600838NM 1995 10 6 CAL950757 119950816A5320 ANGLE BOEING737 7373T0 1384582NM BS 1014 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432031637 23371 IAH - INSPECTION FOUND WALL SUPPORT ANGLE CORRODED AT STATION 1014, LBL 4.54. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-2. (M) 2L72 4F RTA16WE 19951006008391995100600839NM 1995 10 6 CAL950758 119950819A5320 ANGLES BOEING737 7373T0 1384582NM BS 967 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432031637 23371 IAH - INSPECTION FOUND CORROSION ON FLOOR BEAM SUPPORT ANGLES AT STATION 967 AND RBL 18.0, RBL 5.0, LBL 4.5, AND LBL 27.5. THE FLOOR SUPPORT ANGLES WERE REPAIRED IAW SRM 53-00-51 AND ECRA 5310-03152. (M) 2L72 4F RTA16WE 19951006008401995100600840NM 1995 10 6 CAL950765 119950828A3230 PROX SENSOR BOEING737 737217 1384464NM LANDING GEAR INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0912230 19884 FLT NR 1580 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR/GROUND PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REPLACED AND GEAR RETRACTION WAS NORMAL. OTHER GROUND SENSE FUNCTIONS ALSO CHECKED GOOD. (M) 2L72 4F A16WE 19951006008411995100600841NM 1995 10 6 CAL950775 119950830A2910AS116080264 HYD HOSE BOEING737 7373T0 1384582NM 'B' HYD SYSTEM RUPTURED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0912327 23457 FLT NR 0133 - IAH - THE 'B' HYDRAULIC SYSTEM WAS LOST AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC FLEX HOSE BETWEEN 'B' ELECTRIC PUMP AND PRESSURE HYDRAULIC MODULE RUPTURED. THE FLEX HOSE WAS REPLACED. LEAK AND OPERATIONAL CHECKS AFTER HYDRAULIC SYSTEM SERVICING WERE GOOD. (M) 2L72 4F RTA16WE 19951006008421995100600842NM 1995 10 6 CAL950776 119950830A2780 RETRACT MECH BOEING737 7373T0 1384582NM NR 2 SLAT BINDING A CALAO OTHER F FLT CONT AFFECTED DEDESCENT 1 SW0914325 23455 CLE - FLT 1567 - THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL 30 DEGREES TO THE LT AND THEN 30 DEGREES TO THE RT WHILE ON DESCENT INTO CLE. AUTOPILOT WAS ON AND THE YAW DAMPENER AT TIME OF OCCURRENCE SHOWED FULL LEFT. AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. THE SDR WILL REMAIN OPEN FOR PART INFO PENDING CORRECTIVE ACTION. SUPPLEMENT - A READING OF THE FLIGHT DATA RECORDER REVEALED ACFT ONLY ROLLED 3 DEGREES TO THE LT AND THE CAPTAIN OVER-CORRECTED 9 DEGREES TO THE RT. ENGINEERING CONCLUDED NR 2 SLAT WAS BINDING AND AUTOPILOT WORKED PROPERLY COMPENSATING FOR THE ROLL. NR 2 SLAT WAS ADJUSTED. BOEING HAS ASSUMED INVESTIGATION. A 60-DAY HISTORY SINCE THIS OCCURRENCE REVEALED NO REPEATS. (X) 2L72 4F RTA16WE 19951006008431995100600843NE 1995 10 6 CAL950779 219950901A7260 O-RING BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE LEAKING A CALAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0970352 23590 721238 FLT NR 1534 - IAH - THE NR 2 ENGINE WAS SHUT DOWN IN FLIGHT AS A PRECAUTIONARY MEASURE DUE TO THE OIL QUANTITY DROPPING TO ZERO. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING AT NR 2 ENGINE CHIP DETECTOR. THE CHIP DETECTOR O-RINGS WERE REPLACED. THE OIL SYSTEM WAS SERVICED AND NO LEAKS WERE NOTED DURING ENGINE RUN. (M) 2L72 4F4 FRTA16WE E2GL 19951006008441995100600844NM 1995 10 6 CAL950788 119950905A2613 HARNESS BOEING737 737217 1384464NM NR 2 ENGINE CHAFED A CALAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW0913234 19888 FLT NR 1588 - EWR - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED ON APPROACH TO EWR. THE NR 2 ENGINE WAS SHUT DOWN AND BOTH LEFT AND RIGHT FIRE BOTTLES WERE DISCHARGED. THE LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY ANOTHER EIGHT MINUTES AND THEN EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 2 ENGINE OVERHEAT WIRE HARNESS WAS FOUND CHAFED AT THE FUEL HEAT VALVE. THE WIRE HARNESS WAS REPAIRED AND SECURED. IN ADDITION, BOTH FIRE BOTTLES WERE REMOVED AND REPLACED. (M) 2L72 4F A16WE 19951006008451995100600845NM 1995 10 6 CAL950793 119950906A4920 GASKET GARRTT Q38042861 BOEING737 7373T0 1384582NM APU BURNER CAN LEAKING A CALAF ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SW0969333 P60208 23571 FLT NR 0220 - CLE - THE APU WAS STARTED ON SHORT FINAL INTO CLE, THEN ON LANDING ROLL OUT THE APU FIRE WARNING ACTIVATED. THE APU WAS SHUT DOWN AND THE FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING CEASED. THE FIRE DEPARTMENT WAS ALERTED AND OBSERVED NO FIRE OR SMOKE. MAINTENANCE INSPECTED THE APU EXHAUST, ELEVATOR, AND RUDDER WITH NO EVIDENCE OF FIRE NOTED. MAINTENANCE FOUND A LEAK AT THE APU BURNER CAN GASKET. A NEW GASKET WAS INSTALLED ON THE BURNER CAN. THE APU WAS RUN SEVERAL TIMES WITH PACKS OPERATING AND NO PROBLEMS WERE NOTED. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 19951006008461995100600846NM 1995 10 6 CAL950795 119950828A5312 BLKHD CHORD BOEING737 737217 1384464NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 GSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD RIGHT OUTBOARD CHORD AT STRINGER 18A. THE RIGHT OUTBOARD CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638. (M) 2L72 4F A16WE 19951006008471995100600847NM 1995 10 6 CAL950796 119950828A5320 BEAM BOEING737 737217 1384464NM BS 251.6 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 GSO - INSPECTION FOUND THE RIGHT NOSE WHEEL WELL STATION 251.6 VERTICAL SUPPORT BEAM AND ATTACHING WEB CORRODED. THE RIGHT VERTICAL BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. THE CORRODED ANGLES AND FRAME WEB WERE REPAIRED IAW SRM 51-40-1 AND 51-40-2. (M) 2L72 4F A16WE 19951006008481995100600848NM 1995 10 6 CAL950797 119950828A5313 STRINGER BOEING737 737217 1384464NM BS 1006 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 GSO - INSPECTION FOUND CORROSION ON FORWARD LOWER AND UPPER AFT END OF STRINGER 26R AT STATION 1006. THE STRINGER WAS REMOVED AND A NEW STRINGER AND SPLICE WERE INSTALLED IAW SRM 53-10-3, FIGURE 1. (M) 2L72 4F A16WE 19951006008491995100600849NM 1995 10 6 CAL950798 119950828A5312 BLKHD CHORD BOEING737 737217 1384464NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 GSO - INSPECTION FOUND A 1.5 INCH CRACK IN BS 727 BULKHEAD LEFT OUTBOARD CHORD AT STRINGER 18A. THE CHORD WAS REMOVED AND REPLACED IAW EA 5310-01638, OPERATION NR 2. (M) 2L72 4F A16WE 19951006008501995100600850NM 1995 10 6 CAL950800 119950909A2612 FIRE LOOP BOEING737 7373T0 1384582NM NR 2 ENGINE INOPERATIVE A CALAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SW0917344 23582 FLT NR 0655 - IAH - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF IAH. THE NR 2 ENGINE WAS SHUT DOWN AND THE RIGHT FIRE BOTTLE WAS DISCHARGED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 2 ENGINE 'B' SYSTEM FIRE DETECTION CORE LOOP WAS FOUND AT FAULT. THE NR 2 ENGINE CORE LOOP WAS REPLACED. THE NR 2 ENGINE WAS RUN AND OPERATION OF THE FIRE DETECTION SYSTEM CHECKED NORMAL PER MM 26-21-00. THE RIGHT FIRE BOTTLE WAS REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 19951006008511995100600851NM 1995 10 6 CAL950801 119950828A5311 FRAME BOEING737 737217 1384464NM BS 664 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091323471080 19888 INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE FRAME AT RIGHT BS 664, WL 191.5, STRINGER 18A SHEAR BEAM. THE AREA WAS REPAIRED IAW ECRA 5310-03156 AND IAW BAC SERVICE BULLETIN 737-53-1082, REV 3, FIG 1. (M) 2L72 4F A16WE 19951006008521995100600852NM 1995 10 6 CAL950814 119950913A3244 TIRE BOEING737 7373T0 1384582NM LT MLG FAILED A CALAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW0914325 23455 FLT NR 0216 - ORD - THE LEFT MLG NR 1 TIRE THREW ITS TREAD ON TAKEOFF FROM PHX DESTINED FOR EWR. THE CREW WAS NOTIFIED OF THE TIRE DAMAGE AND ELECTED TO DIVERT TO ORD DUE TO THE WEATHER CONDITIONS IN EWR. THE AIRCRAFT LANDED AT ORD WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE NR 1 TIRE CAP WAS GONE, BUT THE TIRE WAS STILL INFLATED. THERE WERE DENTS IN THE LEFT INBOARD AFT FLAP AND THERE WAS DAMAGE TO BOTH THE LEFT GEAR INNER AND CENTER DOORS. THE NR 1 AND NR 2 TIRE/WHEEL ASSEMBLIES WERE REMOVED AND REPLACED. THE LEFT INBOARD AFT FLAP WAS REMOVED AND REPLACED. THE LEFT GEAR INNER AND CENTER DOORS WERE REMOVED AND PLACED ON CDL. (M) 2L72 4F RTA16WE 19951006008531995100600853NM 1995 10 6 CAL950824 119950905A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 947 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND CORROSION ON FLOOR BEAM AT STATION 947 10 INCHES TO THE LEFT AND RIGHT OF BL 0. A REPAIR WAS INSTALLED IAW SRM 53-00-51. (M) 2L72 4F RTA16WE 19951006008541995100600854NM 1995 10 6 CAL950825 119950907A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 312 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND PASSENGER CABIN FLOOR BEAM CORRODED AROUND SEVERAL SCREW HOLES AT STATION 312. A DOUBLER AND FILLER REPAIR WERE INSTALLED PER SRM 53-10-51. (M) 2L72 4F RTA16WE 19951006008551995100600855NM 1995 10 6 CAL950826 119950905A5320 ANGLE BOEING737 7373T0 1384582NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND A 'Z' ANGLE CORRODED ON BOTTOM SIDE NEAR MIDDLE OF R-2 ENTRY. THE 'Z' ANGLE WAS REMOVED AND REPLACED PER SRM 51-10-2. (M) 2L72 4F RTA16WE 19951006008561995100600856NM 1995 10 6 CAL950830 119950902A5414 SKIN BOEING737 7373T0 1384582NM NR 2 NACELLE CRACK A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND A .75 INCH CRACK IN NACELLE STRUT SKIN OF NR 2 ENGINE AT PANEL 5824 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBELR WAS INSTALLED IAW ECRA 5430-01204. (M) 2L72 4F RTA16WE 19951006008571995100600857WP 1995 10 6 ORJA9576 119950809A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11821RA 49931 ALL FIRST CLASS EMERGENCY CEILING LAMPS, ROWS 11-16 EMERGENCY CEILING LAMPS AND ROWS 23-26 EMERGENCY CALLING LAMPS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERIES IN ALL 3 CORRESPONDING BATTERY PACKS. ALL THREE OPS CHECK GOOD. (M) 2L72 4F A6WE 19951006008581995100600858WP 1995 10 6 ORJA9577 119950908A32462601483 BOLT BENDIX 26088911 DOUG DC9 DC983 3022083WP NR 1 MAIN WHEEL BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11836RA 5044 53046 NR 1 M/W ASSEMBLY, THROUGH BOLT SHEAR. REMOVED AND REPLACED NR 1 M/W ASSEMBLY DUE TO THROUGH BOLT SHEAR PER MM CHAP 32. (M) 2L72 4F RTA6WE 19951006008591995100600859WP 1995 10 6 ORJA9578 119950907A3260 BULBS DOUG DC9 DC982 3022082WP LT/RT MLG FAILED A ORJAO OTHER P NO WARNING INDICATION APAPPROACH 1 WP11841RA 49421 LAX - RIGHT LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. SWITCHED LEFT AND RIGHT LANDING GEAR INDICATOR ASSEMBLIES. NEITHER LEFT OR RIGHT WOULD ILLUMINATE AFTER SWITCHING GEAR EMERGENCY EXTENSION LEVER IS PULLED. FOUND FOUR BURNED OUT LAMPS IN LEFT AND RIGHT MLG INDICATOR LIGHTS. RELAMPED AND OPS CHECK OK. RESET EMERGENCY EXTENSION LEVER PER MM PRESSURIZED, GEAR DOOR CLOSED. OPS AND IND CHECKED OK. GEAR PADS ON DOORS FOUND OK. (M) 2L72 4F A6WE 19951006008601995100600860NE 1995 10 6 ORJA9579 219950909A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE LEFT VIBRATING A ORJAO OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 WP11871RA 49788 725441 NR 1 ENGINE VIBRATIONS. REMOVED AND REPLACED NR 1 ENGINE DUE TO VIBRATIONS PER MM 71-00-00. LEAK AND OPS CHECK NORMAL. TRIMMED ENGINE PER MM 71-00-00. OPS CHECK NORMAL (M) 2L72 4F4 FRTA6WE E9NE 19951006008611995100600861NM 1995 10 6 USAA950963 119950818A5313 STRINGER BOEING737 737201 1384454NM BS 967 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19247US35278 22754 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER CORROSION FOUND UNDER STRINGER 27L AT STATION 967. REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3. (M) 2L72 4F A16WE 19951006008621995100600862EU 1995 10 6 USAA950964 219950831A7200 ENGINE BOEING737 737301 1384611NM CFMINTCFM56 CFM563B2 13802EU LEFT FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA19354US22291 23557 7211786 PHL - FLT NR 0803 - ON CLIMB-OUT FROM PHL, PASSING THROUGH 7500, NR 1 ENGINE FAILED. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO PHL. LANDING WAS WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REPLACED THE LEFT ENGINE ASSEMBLY. (M) 2L72 4F4 FRTA16WE E21EU 19951006008631995100600863NE 1995 10 6 USAA950965 219950901A7260717000 N2 GEAR BOX BOEING737 7372B7 1384560NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE OIL LOSS A USAAAE UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CLCLIMB 1 EA19270AU162654402 22882 709201 LGA - FLT NR 0152 - NR 1 ENGINE LOSING OIL QUANTITY ON CLIMB-OUT FROM LGA. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO LGA. SET WAS APPROXIMATELY 10 MINUTES. MAINTENANCE REPLACED LEFT ENGINE N2 GEAR BOX ASSEMBLY. (M) 2L72 4F4 F A16WE E2EA 19951006008641995100600864EU 1995 10 6 VTZA9292 119950914A3230184925 UPLOCK SPRING BAG JETSTMJETSTM3201 1500217EU RT MLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27486UE 905 IAD-PHL - FLT NR 2229 - DURING TAKEOFF, RETURNED TO IAD DUE TO THE RIGHT MAIN GEAR INTRANSIT LIGHT REMAINING ILLUMINATED AFTER RETRACTION. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE UPLOCK SPRING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951006008651995100600865EU 1995 10 6 VTZA95290 119950914A3260622800200 SWITCH BAG JETSTMJETSTM3201 1500217EU NOSE GEAR OUT OF ADJUST A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27487UE 906 FLT NR 6250 - ABE-IAD - DURING APPROACH, THE NOSE GEAR DOWN AND LOCKED INDICATION WAS INOP AND THE INTRANSIT INDICATION REMAINED ILLUMINATED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE NOSE GEAR DOWN AND LOCKED MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951006008661995100600866EU 1995 10 6 VTZA95291 119950908A527014153211109 STRIKER JETAIRJETSTMJETSTM4101 1500501EU BAGG DOOR BROKEN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27315UE 41033 FLT NR 6433 - IAD-EWR - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE STRIKER ON THE FORWARD DOOR WARNING MICROSWITCH BROKEN. MAINTENANCE OPENED DMI NR 17241 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 17241 ON 9-13-95 BY REPLACING THE MICROSWITCH STRIKER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951006008671995100600867EU 1995 10 6 95ZZZM522 119950830A2913PV304426 HYD PUMP BAG JETSTMJETSTM3101 1500215EU LT/RT ENGINE MALFUNCTIONED A REXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25309PX 676 ON REPOSITION FLIGHT TO TUP LOST LEFT HYD PUMP AND RIGHT PUMP INTERMITTENT. UPON LANDING FOUND HYDRAULIC LINE RUPTURED. FOUND RUPTURED HYD PRESSURE LINE IN LEFT ENGINE NACELLE AND REPLACED LINE. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS AS A PRECAUTION DUE TO LOSS OF HYDRAULIC FLUID. (M) 2L72 4T RTA21EU 19951006008681995100600868NM 1995 10 6 95ZZZM523 119950906A3260H1010154 UPLOCK SWITCH BOEING707 707330C 138367GNM LT MLG FAILED A CLCACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO19707HE 20124 FLIGHT NR 043 - OUT OF MIAMI, ON START OF TAKEOFF ROLL, GEAR UNSAFE LIGHT COMES ON AND LEFT GEAR DOWN AND LOCK GOES OUT. ABORTED TAKEOFF. FOUND LEFT MAIN GEAR UPLOCK SWITCH AT FAULT. REPLACED SWITCH AND OPS CHECKED NORMAL PER MM 32-6-0. (M) 2L74 4F 4A26 19951006008691995100600869NM 1995 10 6 95ZZZM524 119950824A32449560571B TIRE BOEING707 707330C 138367GNM NR 2/ NR 6 FAILED A CLCAO OTHER O OTHER ININSP/MAINT 1 SO19707HE 20124 FLT NR 044 - MIA - ON LANDING BLEW NR 2 AND NR 6 TIRES. REPLACED NR 2 AND NR 6 TIRES PER MM 32-3-41. REPLACED NR 1 AND NR 5 IAW GMM 0521-4C. ANTI-SKID SYSTEM CHECKED NORMAL. (M) 2L74 4F 4A26 19951006008701995100600870EU 1995 10 6 AALA951569 119950828A2133566920 OUTFLOW VALVE FOKKERF28 F28MK0100 4990807EU AVIONICS COMPT DEFECTIVE A AALAABGIUNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED CABIN DEPRESSURIZATION J WARNING INDICATION CRCRUISE 1 SW071418A 11397 CVT - FLT NR 1886 - EN ROUTE CLE/DFW DURING CRUISE AT FL 350, LOST CABIN PRESSURIZATION. ACCOMPLISHED EMERGENCY DESCENT AND ALL PASSENGER OXYGEN MASKS DROPPED SUCCESSFULLY. AIRCRAFT DIVERTED TO CVG AND LANDED WITHOUT INCIDENT. PLACARDED BOTH OUTFLOW VALVES INOPERATIVE AND PLACARDED PASSENGER OXYGEN SYSTEM INOPERATIVE AND AIRCRAFT PROCEEDED DFW AT LOWER ALTITUDE. REPLACED AVIONICS COOLING OUTFLOW VALVE. RESTOWED ALL PASSENGER OXYGEN MASKS AND REPLACED OXYGEN GENERATORS. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19951006008711995100600871NM 1995 10 6 AALA951589 119950903A33501703663 EEL CONTACT BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07324AA 22325 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONTACT AT PASSENGER SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006008721995100600872NM 1995 10 6 AALA951590 119950903A33501721651 EEL CONNECTOR BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE S AFFECT SYSTEMS ININSP/MAINT 1 SW07380AN 25449 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROW 36H AND AFT GALLEY INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 42H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006008731995100600873WP 1995 10 6 AALA951591 119950903A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07577AA 53154 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 30 AND 33 INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951006008741995100600874WP 1995 10 6 AALA951592 119950904A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07160AA 46710 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT SIDE OF SERVICE CENTER INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT LEFT SIDE OF SERVICE CENTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19951006008751995100600875EU 1995 10 6 AALA951596 119950905A2433F11QB3121 TRANS/RECTIFIER LUCAS AIRBUS300 A300B4605R 3930308EU NR 2 POSITION DEFECTIVE A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0714053 420 MIA - FLT NR 0916 - AFTER TAKEOFF BOG DURING CLIMB-OUT, ECAM ADVISORY ELECTRICAL DC PAGE TRANSFORMER RECTIFIER 2 SHOWED 31 VOLTS AND ZERO AMPS. ORANGE LINE TO NORMAL DC BUS AND BURNING ODOR NOTED COCKPIT. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 TRANSFORMER RECTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951006008761995100600876WP 1995 10 6 AALA951598 119950906A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07162AA 46943 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT LEFT SIDE OF 'C' LIFT ON FLOOR BOARD INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT SIGN CONNECTOR AT LEFT SIDE OF 'C' LIFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19951006008771995100600877NM 1995 10 6 AALA951618 119950910A3350P4010051112 EEL MODULE BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07338AA 22335 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE FROM PASSENGER SEAT ROW 31 AFT INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONTROL MODULE FOR RIGHT AISLE AFT CABIN AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951006008781995100600878NM 1995 10 6 BJNA95901 119950913A33501012721 EEL BULB BOEING737 737214 138446RNM CABIN FAILED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11457TM 20156 ROW 20 LEFT SIDE EMERGENCY EXIT LIGHT MISSING. REMOVED AND REPLACED MISSING EMERGENCY EXIT LIGHT IAW BSWP 20. OPSCHECKS GOOD THIS STATION. (M) 2L72 4F A16WE 19951006008791995100600879WP 1995 10 6 IXXA199576 119950915A3260 CONNECTOR DOUG DC8 DC871 302199AWP LT MLG DOOR CONTAMINATED A IXXAO OTHER N FALSE WARNING CLCLIMB 1 GL23824BX 45946 ON TAKEOFF OUT OF ONT, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. CYCLING THE LANDING GEAR EXTINGUISHED THE DOOR WARNING LIGHT. IN TOL, TROUBLESHOOTING REVEALED A HIGH RESISTANCE IN THE LEFT MLG DOOR UPLATCH SWITCH CIRCUIT CAUSED BY A CONTAMINATED ELECTRIAL CONNECTOR. THE ELECTRICAL CONNECTOR WAS CLEANED, RESTORING THE NORMAL OPERATION OF THE DOOR UPLATCH SWITCH. (M) 2L74 4F 4A25 19951006008801995100600880WP 1995 10 6 IXXA199577 119950915A2121X702256D FAN DOUG DC8 DC862 3021970WP LEFT FAILED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL2321CX 45955 DURING FLIGHT BETWEEN PJON AND PHNL, THE LEFT RECIRCULATION FAN PRODUCED FUMES WHICH WERE THEN CIRCULATED INTO THE AIRCRAFT. THE RECIRCULATION FAN WAS DEFERRED AND SCHEDULED FOR REPLACEMENT. (M) 2L74 4F 4A25 19951006008811995100600881EU 1995 10 6 PAYA95A4037 119950903A3234F96GA0102 SELECTOR AEROSPATR42 ATR42300 8680920EU LANDING GEAR INTERMITTENT A PAYAO OTHER J WARNING INDICATION APAPPROACH 1 EA174209G 129 JFK-PIT - FLT NR 7791 - UPON SELECTING LANDING GEAR DOWN, THE TRANSIT LIGHTS CAME ON AND OFF FIVE TIMES WITH AN ASSOCIATED HYDRAULIC SURGE. THEREAFTER, THE GEAR EXTENDED NORMALLY. REPLACED LANDING GEAR SELECTOR. THE AIRCRAFT WAS RELEASED IAW THE MEL AT PIT AND REPOSITIONED TO PNE FOR REPAIR. (M) 2H72 4T RTA53EU 19951006008821995100600882NM 1995 10 6 PCAA9500236 119950831A3230101655 ROLLER DHAV DHC8 DHC8102 2809003NM RT MLG SEIZED A PCAAO OTHER J WARNING INDICATION APAPPROACH 1 EA13819EX 016 ROO - RIGHT LANDING GEAR FAILED TO EXTEND. ALTERNATE GEAR EXTENSION USED. CYCLED GEAR, FOUND RIGHT GEAR UPLOCK ROLLER FROZEN. REPLACED ROLLER IAW MM, CYCLED SEVERAL TIMES. OPS CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19951006008831995100600883EU 1995 10 6 REXA95054 119950830A29101379305A77 PRESSURE HOSE BAG JETSTMJETSTM3101 1500215EU LT ENGINE RUPTURED A REXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25309PX 676 ON REPOSITION FLIGHT TO TUP, LOST LEFT HYD PUMP AND RIGHT PUMP INTERMITTENT. UPON LANDING FOUND HYDRAULIC LINE RUPTURED. FOUND RUPTURED HYD PRESSURE LINE IN LEFT ENGINE NACELLE AND REPLACED LINE. REMOVED AND REPLACED LEFT AND RIGHT HYDRAULIC PUMPS AS A PRECAUTION DUE TO LOSS OF HYDRAULIC FLUID. (M) 2L72 4T RTA21EU 19951006008841995100600884EU 1995 10 6 REXA95055 119950904A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU AVIONICS COMPT MALFUNCTION A REXACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO25360PX 340B220 ON TAKEOFF AT APPROXIMATELY 90 KTS AVIONICS SMOKE LIGHT ON CWP CAME ON. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. OPS CHECK GOOD. (M) 2L72 4T RTA52EU 19951006008851995100600885EU 1995 10 6 REXA95056 119950904A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG INOPERATIVE A REXAL ABORTED APPROACH N FALSE WARNING LDLANDING 1 SO25658BA 658 GEAR EXTENSION WASN'T ACCOMPLISHED ON FIRST TRY (NOSE GEAR RED). READMITTED AND GOT THREE GREENS. INSPECTED AIRCRAFT FOR FERRY FLIGHT. INCORPORATED SB 32-JA891142, PT 1. REMOVAL AND REPLACEMENT OF NOSE LANDING GEAR DOWN LOCK MICROSWITCH. PERFORMED GEAR SWINGS AND SYSTEM GROUND CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4T RTA21EU 19951006008861995100600886EU 1995 10 6 REXA95057 119950906A33506104781 EEL BATTERY SAAB SF340 SF340A 7850100EU CABIN DISCHARGED A REXAK NONE L NO TEST ININSP/MAINT 1 SO25106PX 340A106 EMERGENCY LIGHTS WILL NOT STAY ON DURING PREFLIGHT TESTING. NO DEFECTS NOTED WITH EMERGENCY LIGHTS AND THE AIRCRAFT WAS RELEASED FOR SERVICE AFTER THE BATTERIES WERE CHARGED DURING THE FERRY FLIGHT FROM FYV TO MEM. (M) 2L72 4T RTA52EU 19951006008871995100600887EU 1995 10 6 SIMA95251 119950908A29109302631001 HYD LINE SAAB SF340 340B 7860101EU LT NLG WW LEAKING A SIMAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW21594MA10934379 340B212 FLT NR 3883 - LAWTON - DURING TAXI FOR TAKEOFF, CREW OBSERVED HYD QUANTITY GOING TO ZERO, SHUT ENGINES DOWN. MAINTENANCE FOUND HYD FLUID LEAKING FROM AREA LEFT SIDE NLG WHEEL WELL AREA. HYDRAULIC LINE P/N 9302631-001 WAS LEAKING FLUID BETWEEN BRAIDED LINE AND FITTING AND ON LINE. REPLACED LINE, SERVICED HYD SYSTEM PER AMM AND CHECK FOR LEAKS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19951006008881995100600888EU 1995 10 6 SIMA95252 119950909A33503012000 EEL BATTERY AEROSPATR72 ATR72212 EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21345AT6135 1150 300 345 ORD - FLT NR 4057 - EMERGENCY LIGHT ON FLOOR INOP. REMOVED AND INSPECTED BATTERY PACK 61WL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951006008891995100600889EU 1995 10 6 SIMA952541 119950911A2710S2711001400100 LEVER AEROSPATR42 ATR42300 8680920EU RT AILERON FAILED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21433MQ 151 MQT - DURING INSPECTION OF AILERON SYSTEM IAW ZL-644-GVI-10000-001, MAINTENANCE FOUND THE RIGHT WING AILERON LEVER AT RIB 7 HAD EXCESSIVE PLAY. MAINTENANCE REMOVED AND REPLACED THE LEVER, SYSTEM OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951006008901995100600890EU 1995 10 6 SIMA952542 119950911A33503012000 EEL BATTERY AEROSPATR72 ATR72212 EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21345AT6135 1150 345 ORD - FLT 4340 - EMERGENCY LIGHTS STAY ON. REMOVED AND INSPECTED PACK 73WL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951006008911995100600891EU 1995 10 6 SIMA952552 119950912A33503012000 EEL BATTERY PACK AEROSPATR72 ATR72212 EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21248AT4421 636 341 248 ORD - FLT NR 4171 - TWO EMERGENCY FLOOR LIGHTS INOP. REMOVED AND INSPECTED BATTERY PACK FOR ONE 73WL EMERGENCY LIGHT AND DEFERRED OTHER LIGHT AS PER MEL. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951006008921995100600892NM 1995 10 6 TAOA099503 119950904A3350900835A EEL BATT PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS UA5221 20445 OVERHEAD EMERGENCY LIGHT AT CPR MASK AREA INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951006008931995100600893NM 1995 10 6 TAOA099504 119950910A335037067001 EEL BATT PACK MARATHON BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15922TS 20415 OVERHEAD EMERGENCY LIGHT AT ROW 9 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951006008941995100600894EU 1995 10 6 VTZA95287 119950907A7900SYLC4522453 ACTUATOR JETAIRJETSTMJETSTM4101 1500501EU RT ENG FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27307UE 41021 FLT NR 6207 - IAD-MHT - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE CAPTAIN COULD NOT CLOSE RIGHT OIL COOLER DOOR, AND ENGINE COULD NOT MAINTAIN MINIMUM TEMPERATURE WITH INCREASED ALTITUDE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT OIL COOLER ACTUATOR. (M) 2L72 4T RTA41NM 19951006008951995100600895EU 1995 10 6 VTZA95288 119950908A527014153211109 STRIKER JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR BROKEN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27315UE 41033 FLT NR 6433 - IAD-EWR - ABORTED THE TAKEOFF DUE TO THE BAGGAGE DOOR WARNING LIGHT ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE STRIKER ON THE FORWARD DOOR WARNING MICROSWITCH BROKEN. MAINTENANCE OPENED DMI NR 17241 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 17241 ON 9-13-95 BY REPLACING THE MICROSWITCH STRIKER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951006008961995100600896EU 1995 10 6 VTZA95289 119950911A527091SE13 SWITCHES BAG JETSTMJETSTM3201 1500217EU PAX DOOR DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27481UE 895 FLT RN 6499 - IAD-ROA - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING IN FLIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED PASSENGER DOOR AND CLEANED THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951006008971995100600897SO 1995 10 6 WTAA950248 119950822A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP INTERMITTENT A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17280UE 120090 SFO - FLAP CONTROL FAULT REPORTED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. UPON FLAP RETRACTION INBOARD PAIR REMAINED AT 15 DEGREES WHILE OUTBOARD AND NACELLE FLAPS RETRACTED NORMALLY. MAINTENANCE ELECTRICAL CONNECTORS AT INBOARD FLAP ACTUATORS. FLAP SYSTEM OPERATIONAL CHECK NORMAL. PROBLEM REOCCURED ON SUBSEQUENT TAKEOFF ATTEMPT. MAINTENANCE REPLACED LEFT INBOARD FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951006008981995100600898EU 1995 10 6 WTAA950249 119950811A6120897410 PROP GOVERNOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE OUT OF ADJUST A WTAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 WP17428UE 806 FAT - RIGHT ENGINE TORQUE DROPPED OFF DURING TAKEOFF ROLL DUE TO POSSIBLE FUEL BYPASSING. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED RIGHT ENGINE TTL SYSTEM PER MEL 76-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY RIGHT PROP RPM (SCREW X). PERFORMED ENGINE GROUND RUN, ALL PARAMETERS NORMAL. CLEARED PREVIOUSLY DEFERRED ITEM. (M) 2L72 4T RTA21EU 19951006008991995100600899NE 1995 10 6 WTAA950250 219950823A7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT REQ'D A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17284UE 120145 SMF - AFTER DEPARTURE, RIGHT ENGINE OIL PRESSURE FLUCTUATION REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT ENGINE NO EVIDENCE OF OIL LEAKAGE NOTED. SERVICED ENGINE WITH 4 QUARTS OF OIL. OIL PRESSURE INDICATIONS NORMAL ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19951006009001995100600900EU 1995 10 6 WTAA950251 119950824A32609005EN38 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU NLG BROKEN A WTAAK NONE O OTHER APAPPROACH 1 WP17425UE 798 ACV - NOSE LANDING GEAR RED INTRANSIT LIGHT FAILED TO ILLUMINATE WHEN LANDING GEAR WAS EXTENDED. MAINTENANCE REPAIRED BROKEN WIRE AT NOSE LANDING GEAR UPLOCK MICROSWITCH. LANDING GEAR INDICATION SYSTEM OPERATIONAL CHECK NORMAL AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951006009011995100600901SO 1995 10 6 WTAA950253 119950827A7712 TQ IND EMB 120 EMB120RT SO LT ENG MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17453UE 120148 ACV - LEFT TORQUE INDICATION ROSE TO LIMIT AT ACCELERATED RATE DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE REPORTED DISCREPANCY DURING ENGINE GROUND RUNS. ALL ENGINE INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951006009021995100600902EU 1995 10 6 WTAA950254 119950828A5610 WINDSHIELD BAG JETSTMJETSTM3101 1500215EU COCKPIT BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17427UE 811 SEA - CREW REPORTED BIRD STRIKE AT AIRCRAFT NOSE AND WINDSCREEN AREA. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AREA. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951006009031995100600903EU 1995 10 6 WTAA950255 119950904A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG FAILED A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17418UE 780 LAX - NOSE LANDING GEAR GREEN INDICATION LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE REPLACED NOSE LANDING GEAR DOWN LOCK MICROSWITCH. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR DOWN LOCK MICROSWITCH. GEAR INDICATION NORMAL DURING GEAR RETRACTION TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951006009041995100600904EU 1995 10 6 WTAA950256A 119950905A5270MS1610615 SWITCH BAG JETSTMJETSTM3101 1500215EU POD DOOR WORN A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17425UE 798 IPL - POD DOOR LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. DEFERRED POD DOOR CAPTION PER MEL 52-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL WITH THE POD DOOR MICORSWITCH AND STRIKER. (M) 2L72 4T RTA21EU 19951006009051995100600905EU 1995 10 6 WTAA950256B 119950905A527031518217 STRIKER PLATE BAG JETSTMJETSTM3101 1500215EU POD DOOR WORN A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17425UE 798 IPL - POD DOOR LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT WITHOUT INCIDENT. DEFERRED POD DOOR CAPTION PER MEL 52-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED THE DEFERRAL WITH THE POD DOOR MICROSWITCH AND STRIKER. (M) 2L72 4T RTA21EU 19951006009061995100600906EU 1995 10 6 WTAA950257 119950906A261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU CARGO BAY MALFUNCTIONED A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17428UE 806 FAT - SMOKE DETECTOR CAPTION ILLUMINATED INTERMITTENTLY IN FLIGHT. NO EVIDENCE OF SMOKE REPORTED IN CABIN. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SMOKE DETECTOR. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951006009071995100600907EU 1995 10 6 WTAA950258 119950906A5730 SKIN BAG JETSTMJETSTM3101 1500215EU LT WING BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17428UE 806 FAT - BIRD STRIKE REPORTED AT LEFT WING ROOT AREA. MAINTENANCE INSPECTED AIRCRAFT IAW JETSTREAM 3101 MM. NO DAMAGE NOTED AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951006009081995100600908SO 1995 10 6 WTAA950259 119950911A5330 SKIN EMB 120 EMB120RT SO FUSE NOSE BIRD STRIKE A WTAAK NONE C F.O.D. APAPPROACH 1 WP17120AM 120012 ACV - BIRD STRIKE REPORTED AT RIGHT SIDE OF AIRCRAFT NOSE SECTION. MAINTENANCE INSPECTED AIRCRAFT. NO DEFECTS OR DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951006009091995100600909SO 1995 10 6 WTAA950260 119950912A5350 RADOME EMB 120 EMB120RT SO FWD FUS BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17453UE 120148 SMF - BIRD STRIKE REPORTED ON RIGHT FORWARD RADOME AREA. PERFORMED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951013000011995101300001 1995 10 13 9515069992 419951005A3418861FG4 TRANSDUCER DOUG DC9 DC931 3022065WP LT/RT INOPERATIVE A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01896OE157 157 45869 DURING CLIMB, WITH FLAPS SET AT 15 DEGREES, THE STALL WARNING AND STICK SHAKER ACTIVATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT AOA TRANSDUCERS, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951013000021995101300002NM 1995 10 13 9515082277 119950930A5270 SWITCH BOEING727 727251 138408HNM AFT AIRSTAIRS MALFUNCTIONED A NWAAO OTHER N FALSE WARNING TOTAKEOFF 1 GL01277US 21156 MSP-MIA, DURING TAKEOFF, THE AMBER AFT AIRSTAIR WARNING LIGHT ILLUMINATED AND REMAINED ON. AFTER COMMUNICATION BETWEEN THE FLIGHT CREW, DISPATCH, AND MAINTENANCE THE FLIGHT CONTINUED TO MIA. EMERGENCY EQUIPMENT WAS CALLED OUT, BUT NOT USED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE UPLOCK SWITCH, CHECKED OK. 2L73 4F A3WE 19951013000031995101300003EU 1995 10 13 9515093223 119951003A2910 CONNECTION AIRBUS320 A320211 3930320EU LT MLG DOOR LOOSE A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01323US 272 DURING DESCENT, RECEIVED HYD 'G' RSVR LO LVL MESSAGE. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE WHERE MAINTENANCE FOUND A LOOSE B-NUT AT THE LEFT HAND MAIN LANDING GEAR DOOR LATCH. TIGHTENED B-NUT, LEAK CHECK OK. 2L72 4F RTA28NM 19951013000041995101300004WP 1995 10 13 9515109984 119951005A3150 TO WARNING SW DOUG DC9 DC932 3022066WP COCKPIT MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01984US 47383 WHEN ADVANCING POWER FOR TAKEOFF, TAKEOFF WARNING HORN SOUNDED WITH FLIGHT SURFACES IN CORRECT POSITION. THE TAKEOFF WAS ABORTED. REPLACED THE TAKEOFF WARNING SWITCH, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951013000051995101300005NM 1995 10 13 95FDEA01503 119951005A5320 TORQUE BOX BOEING727 727225 1384077NM RIGHT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 THE RT TORQUE BOX IS CRACKED BEYOND THE DOUBLER IN THE FWD RADIUS OF THE SUPPORT ANGLE, JUST BELOW THE VERTICAL ACTUATOR SUPPORT, TEMP REPAIR INSTALLED AND LOGBOOK ENTRY REQ. REPAIRED RT TORQUE BOX PER EA 7-5310-25836. 2L73 4F A3WE 19951013000061995101300006NM 1995 10 13 95FDEA01504 119951005A5521 FITTING BOEING727 727227 1384078NM RT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 RT ELEVATOR AFT SPAR AT CONTROL TAB CUTOUT SUPPORT FITTING CRACKED. REMOVED RT ELEVATOR CONTROL TAB CUTOUT SUPPORT FITTING, REPAIRED CRACK IN ELEVATOR REAR SPAR PER FEDEX SRM 51-40-3. REPLACED NEW RT ELEVATOR CONTROL TAB CUTOUT SUPPORT FITTING. RECALCULATED ELEVATOR REPAIR MOMENT, NEW MOMENT IS 127.91 IAW FEDEX SRM 51-80-7. 2L73 4F A3WE 19951013000071995101300007NM 1995 10 13 95FDEA01505 119951005A5311 FRAME BOEING727 727227 1384078NM BS 520 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FRAME BENT WITH POSSIBLE CRACK AT BS 520 STR 25R. CUT OUT DAMAGE, FABRICATED DOUBLER AND INSTALLED PER FEDEX SRM 51-40-03. 2L73 4F A3WE 19951013000081995101300008NM 1995 10 13 95FDEA01506 119951005A5754 TE WEDGE BOEING727 727227 1384078NM NR 7 LE SLAT TORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 NR 7 SLAT T/E WEDGE IS TORN ABOVE I/B GUIDEHOOK. REPAIRED NR 7 SLAT T/E WEDGE IAW EA NR 7-5710-25887. 2L73 4F A3WE 19951013000091995101300009NM 1995 10 13 95FDEA01508 119951006A5270 WARNING LIGHT BOEING727 727227 1384078NM CARGO DOOR ILLUMINATED A FDEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25489FE 21492 AT FLT 330 MACH .80, THE MCD LIGHT ANNUNCIATOR LIGHT ILLUMINATED, WENT OUT BRIEFLY CAME BACK ON. A/C WAS HOLDING PRESS GOOD. C/W DOOR ANNUNCIATOR, CKLIST AND DIVERTED TO DEN. AFTER DEPRESS LIGHT WENT OUT CARGO DOOR LOCK ANNUNCIATOR INOP. DEFER PER MEL 52-4A, CATEGORY A, CONTROL NR 1006012, EXP 10-8-95. CARGO DOOR WARNING SYS OPS CK OK PER MM 52-70-09. INBOUND CREW REPORTED NO PROBLEMS WITH DOOR WARNING LIGHT. 2L73 4F A3WE 19951013000101995101300010NM 1995 10 13 95FDEA01509 119951006A2150 PACK BOEING727 727225 1384077NM RIGHT MALFUNCTIONED A FDEAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 SO25468FE 21452 ON CLIMBOUT, FLT ENG NOTICED FLUX OF 30 TO 40 DEGREES IN R/PACK TEMP AND ABNORMAL LOW R/BLEED PRESS. ALMOST SIMULTANEOUSLY ENG NR 3 OVERHEAT LIGHT ON FLT ENG'S PANEL ILLUMINATED. R/PACK WAS SHUTDOWN AND R/BLEED CLOSED. THE NR 3 ENG STRUT OVERHEAT LIGHT WENT OUT IMMEDIATELY. RAN ALL 3 ENG AT 80 PERCENT AND BOTH PACKS. CND MALFUNCTION, OK FOR SERVICE. 2L73 4F A3WE 19951013000111995101300011NM 1995 10 13 95FDEA01510 119951007A2910 HYD LINE BOEING727 72725C 138400HNM NR 2 SPOILER BROKEN A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25136FE 19855 DURING CRUISE FL 290, A/C LOST SYS A-HYD, NO APPARENT REASON. FOUND NR 2 SPOILER PRESS LINE BROKE. REMOVED AND REPLACED PRESS LINE, REMOVED CASE DRAIN FILTERS AND PRESS FILTERS, NO CONTAMINATION FOUND. INSTALLED NEW CASE DRAIN FILTERS PER MM 29-11-41, PRESS FILTERS PER MM 29-22-62, SERVICED HYD SYS PER MM 12-12-00, NO LEAK FOUND AND OK FOR SERVICE. 2L73 4F A3WE 19951013000121995101300012NM 1995 10 13 95UAL900176 119951006A3350 EEL BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP299040U 19078 FIRST CLASS EEL LIGHTS INOP. REPLACED EEL LIGHTS. 2L72 4F4 F A16WE E2EA 19951013000131995101300013NM 1995 10 13 95UAL900177 119951006A2760 PICKUP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE SPOILER OUT OF ADJUST A UALAO OTHER O OTHER NRNOT REPORTED 1 WP297280U 21558 AILERON CONTROL IS SLUGGISH WITH EXCESSIVE DEADBAND EITHER SIDE OF NEUTRAL. ACFT HAS PRONOUNCED LEFT ROLLING TENDENCY AT LOW SPEEDS AND RIGHT ROLLING TENDENCY AT HIGH SPEEDS. ALSO, ACFT ROLLS LEFT WITH SPEED BRAKES EXTENDED. ADJUSTED SPOILER PICKUP PER MM 27-60-13. 2L73 4F4 F A3WE E2EA 19951013000141995101300014NE 1995 10 13 95UAL900178 219951006A72508DT2SETS T2 BLADE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FRACTURED A UALAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 WP297286U 18110 21564 696578 NR 3 ENGINE FAILURE LIGHT ON DURING TAKEOFF ROLL. SEVERE VIBRATION AT IDLE N1 19 PERCENT, N2 50 PERCENT. REPLACED ENGINE. THE T-2 BLADE FAILURE WAS DUE TO IMPACT DAMAGE, LEADING TO HIGH CYCLE FATIGUE CRACK AND RESULTANT FAILURE. SEVERE DOWNSTREAM DAMAGE IN THE N1 TURBINE AND EXHAUST CASE. 2L73 4F4 F A3WE E2EA 19951013000151995101300015NM 1995 10 13 95UAL900179 119951009A3231 RETRACT MECH BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE LT MLG DOOR MALFUNCTIONED A UALAJA DUMP FUEL UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 WP294714U 19876 LEFT BODY GEAR DOOR WOULD NOT CLOSE, DUMPED FUEL, BOTH PRIMARY AND SECONDARY SHOWED OPEN. ALSO, AIRCRAFT VIBRATED. PER CREW, WITH GEAR DOWN, GEAR DOOR LIGHTS WERE OUT, PRIMARY AND SECONDARY, WITH GEAR RETRACTED, LEFT GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AND FELT VIBRATION. 2L74 4F4 F A20WE E20EA 19951013000161995101300016NM 1995 10 13 95UAL900180 119951009A3350 EEL BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN LOOSE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29608UA 21869 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 10. SECURED LIGHT, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951013000171995101300017NM 1995 10 13 95UAL900181 119951009A3350 EEL CABLE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29609UA 21870 EMERGENCY ESCAPE PATH LIGHTING INOP AT CROSS AISLE. REPLACED POWER FEEDER CABLE, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951013000181995101300018NM 1995 10 13 95UAL900182 119951009A3350 EEL LAMP BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN INOP A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29604UA 21865 EMERGENCY EXIT LIGHT INOP ROW 32. REPLACED LAMP, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951013000191995101300019NM 1995 10 13 95UAL900183 119951009A3350 EEL BATTERY BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29655UA 25393 EMERGENCY ESCAPE PATH LIGHTING INOP ON THE LEFT SIDE IN FIRST CLASS. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA1NM E24NE 19951013000201995101300020NE 1995 10 13 95UAL900184 219951009A7200 ENGINE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK JE WARNING INDICATION VIBRATION/BUFFET TOTAKEOFF 1 WP297270U 21417 CREW ABORTED TAKEOFF DUE TO VIBRATION AND LOSS OF FUEL FLOW. CREW TRIED TO REAPPLY POWER AND LOST N1 ALSO. LOGBOOK READS: NR 1 ENG VIBRATION AND DROPPING FUEL FLOW ON TAKEOFF. CHECKED OIL SCREEN, FUEL FILTER, AND FCU INLET FUEL FILTER, COMPRESSOR BLEED VALVE ACCELERATION, AND MAX EGT. WITH ALL ENGINES AT TAKEOFF POWER 2.13 EPR, THE N1'S ALIGNED AT 97.0 PERCENT. RETURNED ENGINE TO SERVICE (NR 1 ENGINE REPLACED ON 10-22-95 DUE TO RECURRING VIBRATION). 2L73 4F4 F A3WE E2EA 19951013000211995101300021WP 1995 10 13 ABXA9500756 119950912A5320992348423 GUSSET DOUG DC9 DC941 302207NWP BS 180 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTENING HOLE GUSSET PLATE CRACKED AT FLOORBEAM STA 180. REPLACED GUSSET IAW DC-9 SRM 51-30-5 AND ENGINEERING MEMO 95-01. 2L72 4F A6WE 19951013000221995101300022WP 1995 10 13 ABXA9500757 119950909A53209915558236 ANGLE DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER, BETWEEN LONGERONS 16L TO 17L. REPAIRED IAW DC-9 SUPP DRAWING NR K05159. 2L72 4F A6WE 19951013000231995101300023WP 1995 10 13 ABXA9500758 119950911A53209915558236 ANGLE DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 15R TO 16R. REPLACED ANGLE IAW DC-9 SUPP SRM DRAWING NR K05159. 2L72 4F A6WE 19951013000241995101300024WP 1995 10 13 ABXA9500759 119950911A53209915558236 ANGLE DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE UPPER AND LOWER ATTACH ANGLES ON THE APB STIFFENER AT LONGERON 15R. REPAIRED IAW DC-9 SUPP DRAWING NR K05159. 2L72 4F A6WE 19951013000251995101300025WP 1995 10 13 ABXA9500760 119950908A53209915558233 ANGLE DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND A CRACK IN THE ATTACH ANGLE ON APB STIFFENER BETWEEN LONGERONS 12L TO 13L. REPLACED ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19951013000261995101300026WP 1995 10 13 ABXA9500761 119950913A5320995823869 TIE DOUG DC9 DC941 302207NWP BS 1056 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DAMAGED AREA IN THE RADIUS OF THE SHEAR TIE STA 1056 ABOVE LONGERON 12L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19951013000271995101300027WP 1995 10 13 ABXA9500762 119950913A53205956030 SUPPORT DOUG DC9 DC941 302207NWP BS 465 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND CRACKED FLOOR SUPPORT ON FRAME 465 AT LONGERON 29R. REPAIRED FLOOR SUPPORT IAW SUPP MM DRAWING NR K05018. 2L72 4F A6WE 19951013000281995101300028WP 1995 10 13 ABXA9500763 119950913A57525910051501 TAB DOUG DC9 DC941 302207NWP LT AILERON DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND LEFT AILERON TRIM TAB DELAMINATED. REPLACED TRIM TAB IAW DC-9 MM 27-10-5. 2L72 4F A6WE 19951013000291995101300029WP 1995 10 13 ABXA9500764 119950914A575259100471 TAB DOUG DC9 DC941 302207NWP LT AILERON DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND LEFT AILERON CONTROL TAB DELAMINATED. REPLACED TAB IAW DC-9 MM 27-10-2. 2L72 4F A6WE 19951013000301995101300030WP 1995 10 13 ABXA9500765 119950920A57535910041501 VANE DOUG DC9 DC941 302207NWP LT TE FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FIXED VANE DELAMINATED. REPLACED FIXED VANE IAW DC-9 MM 27-51-3. 2L72 4F A6WE 19951013000311995101300031WP 1995 10 13 ABXA9500766 119950914A5330592032379 SKIN DOUG DC9 DC941 302207NWP BS 294-351 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND TWO COLD WORKED AREAS BETWEEN STATION 294 AND 351 AT LONGERONS 20 TO 22R. REPAIRED IAW ABX REA D953-12805-MR. 2L72 4F A6WE 19951013000321995101300032WP 1995 10 13 ABXA9500767 119950914A53125910130277 BLKHD SKIN DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND A 2.125 INCH CRACK AT AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-12807-MR. 2L72 4F A6WE 19951013000331995101300033WP 1995 10 13 ABXA9500768 119950915A533059248034 SKIN DOUG DC9 DC941 302207NWP BS 712 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON SKIN AT STATION 712, BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-10808-MR. 2L72 4F A6WE 19951013000341995101300034WP 1995 10 13 ABXA9500769 119950914A5330592032379 SKIN DOUG DC9 DC941 302207NWP BS 256 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT STATION 256 BETWEEN LONGERONS 18R AND 19R. REPAIRED IAW ABX REA D953-12810-MR. 2L72 4F A6WE 19951013000351995101300035WP 1995 10 13 ABXA9500770 119950915A5330592032379 SKIN DOUG DC9 DC941 302207NWP BS 360 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AT STATION 360 AT LONGERON 23R. REPAIRED IAW ABX REA D953-12812-MR. 2L72 4F A6WE 19951013000361995101300036WP 1995 10 13 ABXA9500771 119950918A5330592032379 SKIN DOUG DC9 DC941 302207NWP BS 473 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND SKIN DENTED AND CREASED AT STATION 473 BETWEEN LONGERONS 20R AND 21R. REPAIRED IAW ABX REA D953-12817-MR. 2L72 4F A6WE 19951013000371995101300037WP 1995 10 13 ABXA9500772 119950918A5330591142739 SKIN DOUG DC9 DC941 302207NWP BS 1067 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND TWO CRACKS IN THE SKIN AT STATION 1067. REPAIRED IAW ABX REA D953-12818-MR. 2L72 4F A6WE 19951013000381995101300038WP 1995 10 13 ABXA9500773 119950918A53135924878501 LONGERON DOUG DC9 DC941 302207NWP BS 794 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND CORROSION ON LONGERON 30, STA 794. REPAIRED IAW ABX REA D953-12820-MR. 2L72 4F A6WE 19951013000391995101300039WP 1995 10 13 ABXA9500774 119950918A533059248763 SKIN DOUG DC9 DC941 302207NWP BS 786 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN GOUGED AT STA 786 UNDER LONGERON 30. REPAIRED IAW ABX REA D953-12820-MR. 2L72 4F A6WE 19951013000401995101300040WP 1995 10 13 ABXA9500775 119950919A533059114003 SKIN DOUG DC9 DC941 302207NWP FWD FUS WRINKLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND SKIN WRINKLED JUST AFT OF NOSE LANDING GEAR DOOR JAMB ON THE LEFT SIDE. REPAIRED IAW ABX REA D953-12886-MR. 2L72 4F A6WE 19951013000411995101300041WP 1995 10 13 ABXA9500776 119950919A5320991150985 CAP DOUG DC9 DC941 302207NWP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER T-CAP AT STATION 110 BETWEEN LONGERONS L26L TO L27L AND L26R TO L27R. REPAIRED IAW ABX REA D953-12890-MR. 2L72 4F A6WE 19951013000421995101300042WP 1995 10 13 ABXA9500777 119950920A5330592032379 SKIN DOUG DC9 DC941 302207NWP BS 427-475 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX 47498 DURING C-CHECK INSPECTION, FOUND MULTIPLE DENTS, GOUGES AND CREASES ON THE FUSELAGE SKIN AFT OF FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT. REPAIRED IAW ABX REA D953-12891-MR. 2L72 4F A6WE 19951013000431995101300043WP 1995 10 13 ABXA9500778 119950916A524099115823 DOOR FRAME DOUG DC9 DC931 3022065WP FS 170 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING COMPLIANCE OF AD'S 81-10-10, 90-18-03, SB'S 52-125 AND 52-127, FOUND FORWARD SERVICE DOOR BOTTOM BEAM HAD VISUAL AND EDDY CURRENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0. 2L72 4F A6WE 19951013000441995101300044WP 1995 10 13 ABXA9500779 119950916A524099115803 DOOR FRAME DOUG DC9 DC931 3022065WP FS 170 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03, SB'S 52-125 AND 52-127, FOUND FORWARD SERVICE DOOR, SECOND FROM THE TOP BEAM HAD VISUAL AND EDDY CURENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0. 2L72 4F A6WE 19951013000451995101300045WP 1995 10 13 ABXA9500780 119950916A524099115793 DOOR FRAME DOUG DC9 DC931 3022065WP FS 170 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23949AX 47325 DURING COMPLIANCE OF AD'S 81-10-10 AND 90-18-03, SB'S 52-125 AND 52-127, FOUND THE FORWARD SERVICE DOOR UPPER BEAM HAD VISUAL AND EDDY CURRENT CRACK INDICATIONS. REPLACED SERVICE DOOR AND ADJUSTED IAW DC-9 MM 52-41-0. 2L72 4F A6WE 19951013000461995101300046WP 1995 10 13 ABXA9500781 119950926A52805910557159 DOOR DOUG DC9 DC933F 302207AWP LT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE LUGS WORN AND ONE LUG MISSING A BUSHING. REPLACED OUTBOARD DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19951013000471995101300047WP 1995 10 13 ABXA9500782 119950926A32313923167507 ROD ENDS DOUG DC9 DC933F 302207AWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD ENDS WORN. REPLACED DRIVER ROD IAW DC-9 OH MANUAL 32-10-6. 2L72 4F A6WE 19951013000481995101300048WP 1995 10 13 ABXA9500783 119950602A531599115951 FLOORBEAM DOUG DC9 DC941 302207NWP FS 200 CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A FLOORBEAM CHAFED AT FS 200 IN THE MAIN CABIN. REPAIRED FLOORBEAM AT FS 200 IAW ABX REA D953-11699-MR. 2L72 4F A6WE 19951013000491995101300049WP 1995 10 13 ABXA9500784 119950602A532099581561 WINDOW BELT DOUG DC9 DC941 302207NWP FS 541-636 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WINDOW BELT SECTION FROM FS 541 TO FS 636 HAD SHORT RIVET EDGE DISTANCE ON ONE FASTENER. REPLACED WINDOW BELT SECTION IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND REPAIRED SHORT EDGE DISTANCE AREA IAW ABX REA D953-11707-MR. 2L72 4F A6WE 19951013000501995101300050WP 1995 10 13 ABXA9500818 119951006A25105641031533 SEAT DOUG DC8 DC863 302198AWP RT COCKPIT DEFECTIVE A ABXAK NONE O OTHER CRCRUISE 1 GL23817AX 45928 FIRST OFFICER'S SEAT WILL NOT LOCK IN EITHER THE FWD OR AFT POSITION. REPLACED FIRST OFFICER'S SEAT IAW DC8 MM, CHAPTER 25. OPS CHECK OF SEAT ADJUSTMENTS WERE GOOD. 2L74 4F 4A25 19951013000511995101300051EA 1995 10 13 COMA9506056 119951003A3350852D100MD51 EEL SIGN CNDAIRCL600 CL6002B19 EA RT SERVICE DOOR INOPERATIVE A COMAK NONE L NO TEST TXTAXI/GRND HDL 1 SO01917CA4606 2985 7017 FLAPS FAIL MESSAGE, WHEN FLAPS SELECTED TO 30 DEGREES. REPLACED THE LT INBD FLAP SECTION OUTER ACTUATOR. 2L72 4F RTA21EA 19951013000521995101300052EU 1995 10 13 COMA951169 119951003A32307232360151 UP LOCK SPRING SAAB SF340 SF340A 7850100EU LT MLG BROKEN A COMAK NONE J WARNING INDICATION CLCLIMB 1 SO01380CA 340A012 WHEN LANDING GEAR RETRACTED, INTRANSIT INDICATOR REMAINED ON. REPLACED BROKEN UPLOCK SPRING ON LT MLG. 2L72 4T RTA52EU 19951013000531995101300053EU 1995 10 13 COMA951170 119951004A6120 OVERSPEED SYST SAAB SF340 SF340A 7850100EU LT PROP NO TEST A COMACD ABORTED TAKEOFF RETURN TO BLOCK L NO TEST TOTAKEOFF 1 SO01359CA 340A053 LT PROPELLER OVERSPEED SYSTEM DOES NOT TEST. COULD NOT DUPLICATE, SYSTEM TEST NORMAL AND ACFT CONTINUED SERVICE. 2L72 4T RTA52EU 19951013000541995101300054SO 1995 10 13 COMA9511980 119951003A27503472001001 FCU EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO011117H1838 199 120117 FLAP DISAGREEMENT WARNING SOUNDED WHEN FLAPS SELECTED TO 15 DEGREES. AIRCRAFT DIVERTED, DUE TO RUNWAY LENGTH. REPLACED THE FLAP CONTROL UNIT. 2L72 4T RTA31SO 19951013000551995101300055SO 1995 10 13 COMA9511981 119951005A323012038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01156CA8566 1848 120156 WHEN LANDING GEAR SELECTED TO UP, THE A-SYSTEM DISAGREEMENT LIGHTS ILLUMINATED. CYCLED LANDING GEAR WITH SAME RESULTS. REPLACED THE LANDING GEAR CONTROL BOX. 2L72 4T RTA31SO 19951013000561995101300056EA 1995 10 13 COMA9560564 119951004A2750860D10018A FECU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01917CA2182 100 7017 WHEN FLAPS SELECTED UP AFTER TAKEOFF, FLAPS FAIL MESSAGE ON EICAS. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19951013000571995101300057NM 1995 10 13 DL72E953905 119951003A5754 ANGLE BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING A-1 LETTER CHECK, FOUND .25 INCH CRACK NR 7 L/E SLAT COVE SKIN ATTACH ANGLE AT I/B STOP PAD. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951013000581995101300058NM 1995 10 13 DL72E953906 119951003A5754 ANGLE BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 DURING A-1 LETTER CHECK, FOUND 2 INCH CRACK NR 2 L/E SLAT COVE SKIN ATTACH ANGLE AT O/B STOP PAD. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951013000591995101300059NM 1995 10 13 DL72E953915 119951004A5754 ANGLE BOEING727 727247 138408FNM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11283WA 21485 DURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951013000601995101300060NM 1995 10 13 DL72L953893 119951002A5754 BRACKET BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11501DA 21303 DURING D-1 LETTER CHECK, FOUND NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED AT UPPER AND LWR CORNERS, I/B SIDE. REPAIRED PER M/M 57-20-21 PAR 12. 2L73 4F A3WE 19951013000611995101300061NM 1995 10 13 DL72L953924 119951003A3350RPS1 EEL PWR SUPPLY BOEING727 727232 1384082NM CABIN FAILED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO11511DA 21313 DURING DEPARTURE CHECK, EMERGENCY TRACK LIGHT IN FWD CABIN DO NOT TEST. REPLACED BATTERY PACK M9026, OPERATION NORMAL. 2L73 4F A3WE 19951013000621995101300062NM 1995 10 13 DL72L953930 119950929A5313 STRINGER BOEING727 727232 1384082NM BS 990 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11506DA 21308 DURING CV-2 CHECK, STA 990 FRAME WAS CUT TO FACILITATE MTC OF STRINGER 29L REF NR 95. REPAIRED PER M/M 53-12-0 PG 806 AND 807 FIG 805. 2L73 4F A3WE 19951013000631995101300063NM 1995 10 13 DL72P953937 119950926A573065877421 SKIN BOEING727 727225 1384077NM LWR WING CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO118891Z 21860 DURING INSPECTION OF THE LOWER WING SKIN PER EO 4-37113-3, CORROSION WAS DISCOVERED ON THE AFT SKIN BETWEEN S-5C AND S-3C AT APPROXIMATELY LBL 30 AND RBL 30. MTC REPORTS A MINIMUM REMAINING THICKNESS OF .067 AT THE RT DAMAGE AREA AND A MINIMUM REMAINING THICKNESS OF .122 AT THE LT DAMAGE AREA. THE SUBJECT LOWER SKIN IS MANUFACTURED FROM 0.563 2024-T351 WITH A LOCAL THICKNESS OF 0.220 AND SKIN PADS OF 0.390. FINAL CLEANUP DIMENSIONS ARE APPROXIMATELY 16 INCHES FWD TO AFT, BY 6 INCHES I/B TO O/B ON THE RT SIDE AND 6 INCHES FWD TO AFT BY 5 INCHES I/B TO O/B ON THE LT SIDE. REPAIRS ACCOMPLISHED PER DL ERA 302540-14AD. 2L73 4F A3WE 19951013000641995101300064NM 1995 10 13 DL72S953856 119950930A5754 FLAP 65162255A BOEING727 727232 1384082NM NR 3 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA BN1408 21432 DURING INSPECTION, FOUND NR 3 KRUEGER FLAP WITH TIME LIMITED REPAIR AT O/B GATE HINGE CUTOUT. REPAIRED PER MM 57-53-0. 2L73 4F A3WE 19951013000651995101300065NM 1995 10 13 DL72S953865 119950930A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON OVERSIZED HOLE A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 UPON INSPECTION, AN OVERSIZED HOLE WAS FOUND IN SKIN OF LEFT O/B AILERON. REPAIRED PER SRM 57-51-0 PG 801. 2L73 4F A3WE 19951013000661995101300066NM 1995 10 13 DL72S953883 119951002A5610 WINDOW 58935734 BOEING727 727232 1384082NM FLT DECK, R4 ARCING A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11470DA A15233017 20747 AT FL 330 HAD BURNING OR SOLVENT TYPE ODOR. THE PROBLEM WAS INTERMITTENT, DECIDED TO DIVERT LAS. FOUND R4 WINDOW ARCING WHEN WINDOW HEAT WAS ON. DEACTIVATED WINDOW HEAT, PLACED ON MCO AND WINDOW WAS REPLACED. 2L73 4F A3WE 19951013000671995101300067NM 1995 10 13 DL72S953888 119950623A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH RIBS NR 11 AND NR 13 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951013000681995101300068NM 1995 10 13 DL72S953889 119950623A5754651622295 RIBS BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACKING IN THE I/B AND O/B SUPPORT RIBS, FOR BOTH I/B AND O/B SLAT TRACK ATTACH FITTINGS. ACCOMPLISHED REPAIRS PER MM 57-54-0. 2L73 4F A3WE 19951013000691995101300069NM 1995 10 13 DL72S953890 119950623A5754651622295 HEAT SHIELD BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11470DA 20747 DURING SHOP INSPECTION, NR 3 L/E SLAT WAS FOUND WITH CRACK IN HEAT SHIELD AT RIVETS BETWEEN RIBS NR 5, 6, 7, 10 AND 11. REPAIRED PER MM 57-54-0 FIG 814. 2L73 4F A3WE 19951013000701995101300070NM 1995 10 13 DL72S953903 119950925A5753652163262 SPAR BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 AFT SPAR CHORD WAS FOUND CRACKED 33, 54 AND 61 FROM IB END OF NR 3 MIDFLAP. THE DAMAGED SECTION WAS REPLACED AND SPLICED IN PER MM 57-50-00. 2L73 4F A3WE 19951013000711995101300071NM 1995 10 13 DL72S953907 119951003A3350 EEL BATTERY PACK 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11403DA 21147 RIGHT CENTER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19951013000721995101300072NM 1995 10 13 DL72S953914 119950613A57206521796111A FAIRING BOEING727 727232 1384082NM WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11497DA 21077 AFT MOUNT HOLES ENLARGED, WELDED AS PER MM 57-52-0 2. CRACK IN CLOSEOUT PANEL UNDER GUIDE PIN. REPAIRED PER SRM 51-40-2. REPAIRS FOUND AT SHOP INSP FOR AFT O/B FLAP TRACK FAIRING. 2L73 4F A3WE 19951013000731995101300073NM 1995 10 13 DL72S953920 119950925A5720651622174 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11536DA 22049 THE NR 5 L/E SLAT, LOWER T/E ATTACH ANGLE CRACKED AT RIB NR 9. REPAIRED PER M/M 57-54-0 PAGE 807A. 2L73 4F A3WE 19951013000741995101300074NM 1995 10 13 DL72S953923 119951003A5754 SKIN BOEING727 727232 1384082NM NR 4 SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 UPON HMV, FOUND SKIN WORN ON SECTION OF SKIN UNDER LIFT FENCE NR 4 SLAT. REPAIRED PER MM 57-54-0 PG 817. 2L73 4F A3WE 19951013000751995101300075NM 1995 10 13 DL72S953927 119951006A5754 COVE ANGLE BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11520DA 21471 DURING F-1 LTR CHECK, FOUND NR 8 SLAT COVE ANGLE CRACKED BELOW ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951013000761995101300076NM 1995 10 13 DL72S953941 119950926A5753652163358 LE SKIN BOEING727 727232 1384082NM NR 3 TE MIDFLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING SHOP INSP, NR 3 MIDFLAP WAS FOUND WITH I/B L/E SKIN WORN. REPAIRED LEADING EDGE PER MM 57520, BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER. 2L73 4F A3WE 19951013000771995101300077NM 1995 10 13 DL72S953942 119950925A5753652163358 SKIN BOEING727 727232 1384082NM NR 4 TE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING SHOP INSP, NR 4 MIDFLAP L/E SKIN WORN AT O/B END OF FLAP. REPAIRED PER MM 57520 BY REMOVING DAMAGED AREA AND INSTALLING A DOUBLER AND FILLER. 2L73 4F A3WE 19951013000781995101300078NM 1995 10 13 DL72W953887 119951002A52306557140514 DOOR BOEING727 727247 138408FNM C 1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11291WA 22109 AFT FRAME SECTION CRACKED AT AFT TORQUE TUBE CRANK ARM CUTOUT OF C-1 DOOR. REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19951013000791995101300079NM 1995 10 13 DL72W953921 119951005A3350900542 EEL BATTERIES BOEING727 7272Q8 138407WNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11831L 21826 OVERWING EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19951013000801995101300080 1995 10 13 DL73E953899 419951003A3418861CAK AOA SENSOR BOEING737 737247 138448DNM LEFT BROKEN A DALAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SO11239WA 23187 ON LIFT-OFF, THE STICK SHAKER ACTIVATED AND DID NOT STOP UNTIL TOUCHDOWN. FOUND LEFT AOA SENSOR BROKEN OFF FROM A/C. REPLACED LEFT AOA, OPS CKS GOOD. 2L72 4F A16WE 19951013000811995101300081NM 1995 10 13 DL73S953938 119951003A5330 SKIN BOEING737 737232 1384475NM BS 940 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11325DL 23097 A BAGGAGE CART STRUCK THE AIRCRAFT RESULTING IN DAMAGE TO THE SKIN, S-23L AND S-24L AT APPROXIMATELY STA 940. THE SKIN CUTOUT EXTENDS FWD AND AFT FROM STA 925 TO STA 947 AND IS LOCATED BETWEEN S-22L AND S-24L. THE SKIN AND STRINGER WILL BE REPAIRED PER B737-200 SRM AND DL ERA 302583-14. 2L72 4F RTA16WE 19951013000821995101300082NM 1995 10 13 DL757953904 119951003A2121 FAN 6067723 BOEING757 757232 1384965NM RIGHT FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11608DA 25324 22815 DURING CRUISE, HAD AN ELECTRICAL BURNING SMELL IN CABIN. UTILITY BUSES TURNED OFF AND SMELL WENT AWAY. FOUND RT RECIRC FAN MOTOR WINDINGS BURNT, FWD TO MCO. REPLACED FAN, OPERATION NORMAL. 2L72 4F RTA2NM 19951013000831995101300083NM 1995 10 13 DL757953931 119951007A5210 LATCHING MECH BOEING757 757232 1384965NM RT PAX DOOR OUT OF RIG A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11653DL 24393 000 CLIMBING THROUGH 2500 FT, CENTER ENTRY DOOR LIGHT ILLUMINATED. DOOR HANDLE WAS HELD CLOSED BY FLIGHT ATTENDANT TO PREVENT IT MOVING TO OPEN POSITION. INSPECTED 2 RT DOOR, FOUND UNLATCHING FORCE BELOW MINIMUMS. ADJUSTED PER MM 52-11-00 DOOR LATCHING FORCE WITHIN LIMITS. 2L72 4F RTA2NM 19951013000841995101300084NM 1995 10 13 DL76L953901 119951003A3350 EEL POWER SUPPLY BPS73 BOEING767 767332 1382001NM CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11176DN 9007 25061 EMERGENCY TRACK LIGHTS AFT CABIN LT SIDE INOP. REPLACED POWER SUPPLY M9010 AND REPOSITIONED TRACK, CHECKS OK. 2L72 4F RTA1NM 19951013000851995101300085NE 1995 10 13 DL76L953925 219951006A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11181DN17755 25986 724178 FOUND METAL ON CHIP DETECTORS AND OIL SCREEN. REPLACED ENGINE, ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19951013000861995101300086NM 1995 10 13 DL76L953928 119951006A3350337201959 EEL ASSY BOEING767 767332 1382001NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11181DN 25986 EMERGENCY TRACK LIGHT LOOSE RT SIDE, RT AFT LAV. REPLACED TRACK LIGHT ASSY, OPS CKS OK. 2L72 4F RTA1NM 19951013000871995101300087NM 1995 10 13 DL76S953876 119951002A3350 EEL LAMPS OL3071BPEGPLBOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11116DL 23275 ON LAYOVER, FOUND PATH LIGHTS OUT AT SEATS 11AB, 38AB. REPLACED LAMPS, BOTH LIGHTS CK NORMAL. 2L72 4F RTA1NM 19951013000881995101300088NM 1995 10 13 DL76S953919 119951003A3350 EEL LAMP L3071BPEGPL BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11120DL 23279 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. LOCATED AFT OF R2 ENTRANCE DOOR. RELAMPED, CHECKS GOOD. 2L72 4F RTA1NM 19951013000891995101300089NM 1995 10 13 DL76S953922 119951005A3350 EEL BULB 0L3071BPEGPLBOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11117DL 23276 ON LAYOVER, EMERGENCY PATH LIGHT OUT AT ROW 21F. RELAMPED, OPERATION NORMAL. 2L72 4F RTA1NM 19951013000901995101300090WP 1995 10 13 DLL14953916 119951004A335008163000625 EEL TRACK LKHEED1011 1011385115 5265015WP CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11736DY 193C1227 EMERGENCY TRACK LIGHT AT 12C IS MISSING. REPLACED TRACK AND LENS ASSEMBLY, CKS GOOD. 2L73 4F A23WE 19951013000911995101300091WP 1995 10 13 DLL14953918 119951004A3350 EEL BATTERY PACK 5165741 LKHEED1011 1011385115 5265015WP CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO111739D 61495 193C1237 AT DEPARTURE, EMERGENCY LIGHT AFT LT C/B POPPED. REPLACED EMERGENCY LIGHT BATTERY PACK, CKS OK. 2L73 4F A23WE 19951013000921995101300092NM 1995 10 13 DLM88953834 119950926A3350BR9279103 EEL DOUG MD88 MD88 3023688NM AFT STAIRS INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11911DL 49542 DURING INSPECTION, AFT AIRSTAIR EMERGENCY LIGHT FOUND INOP. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL. 2L72 4F RTA6WE 19951013000931995101300093NM 1995 10 13 DLM88953909 119951004A56105912290505 WINDSHIELD DOUG MD88 MD88 3023688NM LT COCKPIT CRACKED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11977DL 53258 DURING CRUISE, CAPTAINS WINDSHIELD STARTED TO ARC, THEN CRACKED. A/C DIVERTED TO ATL. REPLACED WINDSHIELD. 2L72 4F RTA6WE 19951013000941995101300094NM 1995 10 13 DLM88953917 119951004A3020 ICE DUCT 13277505 DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE BLOWN A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 SO11987DL 53338 718248 ON TAKEOFF, GOT RT ENG FIRE LOOP 'B' MSG FOLLOWED BY RT ENG ANTI-ICE MSG AND RT ENG VLV MSG. THEN FIRE WARNING CAME ON, WARNING CX BY RETARDING THROTTLE. FOUND RT ENG COWL ANTI-ICE DUCT 759102250 BLOWN, BRACKET 719201023 AND WIRING NEAR DUCT DAMAGED. ALSO, INSIDE OF COWL NEAR DUCT DAMAGED. 2L72 4F4 FRTA6WE E9NE 19951013000951995101300095NM 1995 10 13 DLM88953926 119951006A5320 STRIKER DOUG MD88 MD88 3023688NM RT MLG DOOR JAMBCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11997DL 53364 DURING D-1 LETTER CHECK, FOUND RT WW AFT DOOR JAMB STRIKER CRACKED 1 INCH. REPAIRED PER SRM 53-05 FIG 81A. 2L72 4F RTA6WE 19951013000961995101300096NM 1995 10 13 DLM90953929 119951006A2421 GENERATOR 1B1892 DOUG MD90 MD9030 3023690NM NR 2 ENGINE FAILED A DALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 SO11901DA 107 53381 INFLIGHT 310 FL, RIGHT GEN FAILED WITH R GEN OFF AND R AC PWR FAULT ON, OAP LT ALREADY ON MCO. NEEDS RT VSCF, REMOVED RT VSCF, INSTALLED NEW VSCF, RAN ENG TEST NORMAL. METERED OIL TEMP SENSOR AND WIRES FROM CONVERTER TO GEN, ALL NORMAL. 2L72 4F RTA6WE 19951013000971995101300097NM 1995 10 13 P5CA9500801 119951006A291068B01544175 HYD LINE BOEING747 747122 1384872NM NR 2 PACK CRACKED A P5CAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP23854FT 19754 SMOKE/VAPOR IN COCKPIT, SMELLS OF BURNT SKYDROL, DISSIPATED AFTER 10 TO 12 MINUTES. CREW DONNED OXYGEN MASKS AND RETURNED LANDING OVERWEIGHT WITH LOW SINK RATE. FOUND HYDRAULIC LEAK AND CRACKED HYDRAULIC RETURN LINE NR 2 PACK AREA. SUSPECT INGESTION INTO AIR CONDITIONING SYSTEM. REPAIRED WITH TEMPORARY LINE IAW MM 20-11-05, OVERWEIGHT INSPECTION COMPLIED WITH. 2L74 4F A20WE 19951013000981995101300098NM 1995 10 13 P5CA9500802 119951002A5230A290K09089 RESERVOIR BOEING747 747121 1384871NM CARGO DOOR RUPTURED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23830FT 19642 UPON ARRIVAL VCP, UNABLE TO OPEN SIDE CARGO DOOR. WHILE ATTEMPTING TO TROUBLESHOOT DOOR HYDRAULIC PROBLEM, DOOR HYDRAULIC RESERVOIR RUPTURED. FOUND BENT LINE CAPPED WHICH CAUSED RUPTURE. REPLACED RESERVOIR IAW MM 52-35-00. 2L74 4F A20WE 19951013000991995101300099NM 1995 10 13 P5CA9500803 119951005A2841 FUEL GAUGE BOEING747 747123 1384873NM NR 2 MALFUNCTIONED A P5CAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP23859FT 20326 MAO-GRU - DURING CLIMBOUT, NR 2 FUEL QUANTITY GAUGE DECREASED FROM 26,000 LBS TO 8,800 LBS IN A 10 MINUTE PERIOD. THE NR 2 BOOST PUMPS WERE TURNED OFF AND NR 2 ENGINE CROSSFED FROM OTHER TANKS AND QUANTITY CONTINUED TO DECREASE TO 4,800 LBS. SUSPECTED FUEL LEAK AND RETURNED TO MAO. COMPARED ARRIVAL FUEL TO STICK READINGS, NO ERROR. CHECKED FOR FUEL LEAKS, NO SIGN OF FUEL LEAK DURING PRESS CHECK OF FUEL SYSTEMS. REFUELED AIRCRAFT, RECHECKED STICK READINGS, DISPATCHED AIRCRAFT. 2L74 4F A20WE 19951013001001995101300100NM 1995 10 13 P5CA9500804 119951007A29102720021 CHECK VALVE BOEING747 747122 1384872NM NR 3 HYD ADP FAILED A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23850FT 19755 DURING CONTROL CHECK ON TAXI OUT, NR 3 HYDRAULIC PRESS LIGHT ILLUMINATED WITH SUBSEQUENT LOSS OF TOTAL SYSTEM QUANTITY. DEPRESSURIZED SYSTEM AND RETURNED TO BLOCKS. FOUND NR 3 HYDRAULIC CHECK VALVE FAILED, VALVE CRACKED AT THREADS. REMOVED REMAINING THREADED SECTION, INSPECTED MODULE THREADS, INSTALLED NEW CHECK VALVE. LEAK AND OP CHECK NORMAL PER MM 29-11-40. 2L74 4F A20WE 19951013001011995101300101WP 1995 10 13 SCNA95208 119951005A5311NEA6014 FRAME DOUG DC10 DC1010 3022110WP BS 1505 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46905 DURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE AFT FACE OF STATION 1505 FRAME LOWER CAP AT APPROXIMATELY BS 78. THE FRAME WAS REPAIRED IAW SUN COUNTRY ENGINEERING ORDER 53-5155-1. 2L73 4F A22WE 19951013001021995101300102WP 1995 10 13 SCNA95209 119951005A5312AEA00243 BLKHD STIFFENER DOUG DC10 DC1010 3022110WP BS 1521 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46905 DURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE VERTICAL STIFFENER ATTACHED TO THE FORWARD SIDE OF THE STATION 1521 BULKHEAD AT APPROXIMATELY BS 78. THE VERTICAL STIFFENER WAS REPAIRED IAW SUN COUNTRY ENGINEERING ORDER 53-5154-1. 2L73 4F A22WE 19951013001031995101300103WP 1995 10 13 SCNA95210 119951005A5320AEA00246 INTERCOSTAL DOUG DC10 DC1010 3022110WP BS 1505 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46905 DURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE INTERCOSTAL AT STATION 1505, APPROXIMATELY BS 78. REMOVED AND REPLACED THE INTERCOSTAL AT STATION 1505 IAW SRM 51-33-01. 2L73 4F A22WE 19951013001041995101300104 1995 10 13 SWIA95625 419950911A3418 CONTROL PANEL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE STALL WARNING DIRTY A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07214SW 120280 AFTER T/O, INADVERTENT STICK SHAKER, TURNED OFF NR 2 SYSTEM AND RETURNED TO LAX. FOUND SYSTEM NR 2 TEST TO BE STICKING. REMOVED, CLEANED AND REINSTALLED STALL WARNING CONTROL PANEL. OPS CK GOOD. 2L72 4T4 TRTA31SO E20NE 19951013001051995101300105EA 1995 10 13 SWIA95626 119950914A8012 START VLV LIGHT CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT ENGINE ILLUMINATED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07406SW 7030 RT ENGINE START LIGHT ON AND RT ENGINE START EICAS MESSAGE ON, CLIMBING THROUGH 15,000 FT. PROBLEM INTERMITTENT ON ABOUT 60 PERCENT OF THE TIME. PROBLEM APPEARED THROTTLE SENSITIVE. RETARDING RT THROTTLE, LIGHT GOES OUT AND ADVANCING THROTTLE LIGHT COMES ON, ABOVE 12,000 FT. REPAIRED CHAFED WIRE AT START VALVE. GROUND RUN CK GOOD. 2L72 4F4 FRTA21EA E15NE 19951013001061995101300106SW 1995 10 13 SWIA95627 119950919A3213 UP LIMIT SW SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NLG MALFUNCTIONED A SWIAD RETURN TO BLOCK O OTHER CLCLIMB 1 NM07685AV AC685 NOSE WHEEL WOULD NOT LOCK IN UP POSITION. REPLACED NOSE GEAR UP LIMIT SWITCH. NOSE GEAR WOULD CYCLE AFTER GEAR RETRACTION. REPLACED GEAR SECTION VALVE IN LT WHEEL. OPS CKS GOOD AND NO LEAKS NOTED. 1L72 4T4 T A8SW E4WE 19951013001071995101300107SW 1995 10 13 SWIA95628 119950928A2710 CONTL CABLES SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP AILERONS OUT OF ADJUST A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM0726974 AC664 DURING PREFLIGHT CONTROL CHECK, FOUND EXCESSIVE PLAY IN CONTROLS, COPILOT WOULD MOVE WHILE CAPT WOULD REMAIN STATIONARY. INSPECTED AILERON CABLES FROM CONTROL COLUMN TO BELL CRANK, FOUND NORMAL. FOUND CABLE TENSION TO BE BELOW, ADJUSTED CABLES TO CORRECT TENSION AND OP CK GOOD. 1L72 4T4 T A8SW E4WE 19951013001081995101300108WP 1995 10 13 SWIA95629 219951001A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LEFT MALFUNCTIONED A SWIAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 NM072726N AC727 ON DESCENT, LT ENGINE STARTED LOOSING POWER. WITH POWER LEVER AT THE FWD STOP THE ENGINE WOULD ONLY MAKE 2.5 PERCENT TORQUE. AS WE APPROACHED TO LAND AT 100 FT WITH BOTH POWER LEVER AT FLIGHT IDLE, THE LT ENGINE STARTED TO POWER UP ON ITS OWN AT APPROX 65 TO 70 PERCENT TORQUE. INSPECTED LT ENGINE RIGGING AT FUEL CONTROL PPC PROP GOV AND FUEL SHUTOFF, ALL FOUND SECURED AND NO INTERFERENCE DURING MOVEMENT. ALL RIGGING PARAMETERS CORRECT, CHECKED P2T2 FOR DAMAGE, FOD NONE FOUND. RAN LT ENGINE ALL POWER CONFIGURATION, ALL PARAMETERS NORMAL. SRL TEMP CKS GOOD, AP AND TORQ LIMITS TEST GOOD, NO UNSUAL ENGINE PERFORMANCE. 1L72 4T4 T A8SW E4WE 19951013001091995101300109SO 1995 10 13 SWIA95630 119951002A3610 BLEED AIR LINE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT ENGINE LOOSE A SWIAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07214SW 120280 LT DUCT LEAK LIGHT CAME ON AND WOULD NOT EXTINGUISH, SHUTDOWN LT ENGINE AND RETURNED TO LAX. FOUND BLEED AIR LOOSE ON 18 PSI REGULATOR. TIGHTENED LINE, PERFORMED ENGINE POWER, OPS CKS GOOD AND NO LEAKS NOTED. 2L72 4T4 TRTA31SO E20NE 19951013001101995101300110NM 1995 10 13 UPS204759 119951004A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01933UP 19857 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208. ALSO, HAS MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED FLOORBEAM PER 727 SRM 53-10-8 FIGURE 7 AND EO 727-53-1686. 2L73 4F A3WE 19951013001111995101300111NM 1995 10 13 UPS204760 119951009A5315 FLOORBEAM BOEING727 727108C 1384039NM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON FLOORBEAM STA 328 LBL 33 WL 208 AND MECHANICAL DAMAGE LBL 54 WL 208. REPAIRED IAW SRM 53-10-8 AND B727-53-1686. 2L73 4F A3WE 19951013001121995101300112NM 1995 10 13 UPS204761 119951009A5330 SKIN BOEING727 727108C 1384039NM BS 272-275 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON SKIN AT BS 272 TO 275, LBL 56 WL 209 TO 213. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. TRIMMED OUT DAMAGE AREA, FABRICATED REPAIR DOUBLER, FINAL REPAIR PER SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2, EO B727-5330-7453A. 2L73 4F A3WE 19951013001131995101300113NM 1995 10 13 UPS204762 119951009A5541 RIB BOEING727 727108C 1384039NM RUD STA 128 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION IN BORE FOR BOTTOM BUSHING AND O/B FACE ON UPPER THRUST RIB LUG FOR LOWER SPLICE BEAM, AT APPROX RUDDER STA 128 TO 765 LT. REMOVED CORROSION AND OVERSIZE BORE, INSTALLED OVERSIZED BUSHING IAW EO 727-55-0302. 2L73 4F A3WE 19951013001141995101300114NM 1995 10 13 UPS204763 119951009A5531 MID SPAR BOEING727 727108C 1384039NM VERT FIN CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND RT VERT FIN MID SPAR UPPER FLANGE HAS BROKEN FASTENER HOLE. REMOVED DAMAGE, FABRICATED, INSTALLED REPAIR ANGLES PER SRM 51-30-2 UPS EO 727-55-0303. 2L73 4F A3WE 19951013001151995101300115NM 1995 10 13 UPS204764 119951009A5711 SPAR BOEING727 727108C 1384039NM FSS 200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT WING L/E LOWER FRONT SPAR CHORD AT FSS 200. MECHANICALLY REMOVED CORROSION, REWORK OUT OF LIMITS IAW SRM 57-10, FRONT SPAR LOWER CHORD REPAIRED IAW UPS EO 727-57-1642. 2L73 4F A3WE 19951013001161995101300116NM 1995 10 13 UPS204765 119951009A57206516200104 STIFFENER BOEING727 727108C 1384039NM FSS 475 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 475, ON THE I/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED STIFFENER AT FSS 475, I/B SIDE NR 6 SLAT I/B TRACK IAW SRM 51-30-2. 2L73 4F A3WE 19951013001171995101300117NM 1995 10 13 UPS204766 119951009A57206516200103 STIFFENER BOEING727 727108C 1384039NM FSS 480 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND VERTICAL STIFFENER AT FSS 480, ON O/B SIDE OF NR 6 SLAT I/B TRACK IS CRACKED. REMOVED AND REPLACED CRACKED STIFFENER IAW SRM 51-30-2 AT FSS 480. 2L73 4F A3WE 19951013001181995101300118NM 1995 10 13 UPS204767 119951009A5744652177613 FITTING BOEING727 727108C 1384039NM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING O/B AILERON LOCKOUT FITTING HAS CORROSION PITS IN LOWER SURFACE NEXT TO BELL CRANK. REPLACED FITTING IAW SRM 51-30-2, MM 27-10-131, 27-10-121. 2L73 4F A3WE 19951013001191995101300119NM 1995 10 13 UPS204768 119951009A574465261187 FITTING BOEING727 727108C 1384039NM LT AILERON CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION LT WING I/B AILERON TURNAROUND FITTING. REPLACED FITTING IAW SRM 51-30-2. 2L73 4F A3WE 19951013001201995101300120NM 1995 10 13 UPS204769 119951009A5530652330070 SHEAR TIE BOEING727 727108C 1384039NM VERT STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT VERTICAL STABILIZER SHEAR TIE FITTING, AT FIN STA 204 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED FITTING ON RT VERTICAL STAB AT FIN STA 204 IAW SRM 51-30-2. 2L73 4F A3WE 19951013001211995101300121NM 1995 10 13 UPS204770 119951009A553065233009291 SHEAR TIE BOEING727 727108C 1384039NM VERT STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON BOTH LT AND RT VERTICAL STABILIZER SHEAR TIES, AT FWD END OF RIB NR 9 AT FIN STA 180.6 INSIDE VERTICAL FIN TUNNEL. REMOVED AND REPLACED LT AND RT SHEAR TIES IAW 727 SRM 51-30-2. 2L73 4F A3WE 19951013001221995101300122NM 1995 10 13 UPS204771 119951009A5530652330069 SHEAR TIE BOEING727 727108C 1384039NM VERT STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON VERTICAL FIN SHEAR TIE FITTING, AT FIN STA 204 LT SIDE FORWARD END OF RIB NR 10 INSIDE TUNNEL, FOUND WHILE WORKING TAIL 227 CI 360676. REMOVED SHEAR TIE FITTING AT FIN STA 204 LT SIDE. REPLACED SHEAR TIE IAW WRM 51-30-2. 2L73 4F A3WE 19951013001231995101300123NM 1995 10 13 UPS204772 119951009A5711 SPAR BOEING727 727108C 1384039NM WS 571 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON INDICATIONS ON UPPER REAR SPAR ON LT WING AT WS 571. REMOVED CORROSION IAW 57-10-1, REPAIRED SPAR IAW SRM 57-10-6. 2L73 4F A3WE 19951013001241995101300124NM 1995 10 13 UPS204773 119951009A532065228672728 PRESSURE PANELS BOEING727 727108C 1384039NM NR 3120-3121 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON PANELS BETWEEN GASKET SEAL ON PRESSURE PANELS 3120 AND 3121. REMOVED AND REPLACED PANELS IAW SRM 51-30-2. 2L73 4F A3WE 19951013001251995101300125NM 1995 10 13 UPS204774 119951009A575465162251 FLAP BOEING727 727108C 1384039NM NR 3 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE REPLACED NR 3 K-FLAP, DUE TO CONDITION AND CORROSION. REMOVED AND REPLACED NR 3 K-FLAP IAW MM 27-81-01. 2L73 4F A3WE 19951013001261995101300126NM 1995 10 13 UPS204775 119951009A5315 FLOORBEAM BOEING727 727108C 1384039NM BS 600 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION FWD CARGO BAY IN THE NUTPLATE HOLES, LOWER FLANGE OF THE 600 FLOORBEAM LBL 16 RLB 58 WL 201. REPAIRED BS 600 FLOORBEAM IAW UPS EO B727-5310-7463-A. CORROSION REWORK WAS OUT OF LIMTS IAW SRM 53-10-1. 2L73 4F A3WE 19951013001271995101300127NM 1995 10 13 UPS204776 119951009A5531 SPAR BOEING727 727108C 1384039NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON LT SIDE VERTICAL FIN FRONT SPAR FROM FIN STA 108.8 TO 6.372. CORROSION OUT OF LIMITS, REPAIRED LT SPAR CHORD IAW UPS EO B727-5530-7473-A. 2L73 4F A3WE 19951013001281995101300128NM 1995 10 13 UPS204777 119951009A5531 SPAR BOEING727 727108C 1384039NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON RT SIDE VERT FIN UPPER FLANGE ON FRONT SPAR ENTIRE LENGTH STA 6.372 TO 180.6. CORROSION OUT OF LIMITS, REPAIRED RT SPAR CHORD IAW UPS EO B727-5530-7473-A. 2L73 4F A3WE 19951013001291995101300129NM 1995 10 13 UPS204778 119951009A5512 SKIN BOEING727 727108C 1384039NM HORIZ STAB DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND DAMAGE AROUND FASTENERS AT APPROX STAB STA 32.08 TO 44.00 ON LT HORIZONTAL STAB UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW EO B727-5510-7485-A. 2L73 4F A3WE 19951013001301995101300130NM 1995 10 13 UPS204779 119951009A5554657278810 FITTING BOEING727 727108C 1384039NM RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND UPPER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 212 TO 208. REMOVED UPPER RUDDER, INSTALLED REPLACEMENT RUDDER IAW MM 27-20-01. 2L73 4F A3WE 19951013001311995101300131NM 1995 10 13 UPS204780 119951009A5554652229815 FITTING BOEING727 727108C 1384039NM RUDDER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND LOWER RUDDER CENTER RUDDER HINGE SUPPORT FITTING IS CRACKED AT RUD STA 178 LT SIDE 3RD FASTENER FROM TOP. REMOVED RUDDER, INSTALLED SERVICEABLE RUDDER IAW MM 27-20-01. 2L73 4F A3WE 19951013001321995101300132NM 1995 10 13 UPS204781 119951010A553065233001112 SHEAR TIE BOEING727 727108 NM VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C55-395-10-00-01) ON BOTH LT AND RT FWD SHEAR TIES INSIDE VERTICAL FIN TUNNEL AT FIN STA 87.0 UPPER END OF RIBS NR 5. MECHANICALLY REMOVED CORROSION. REWORK OUT-OF-LIMITS IAW SRM 55-50-00. REMOVED AND REPLACED SHEAR TIES IAW SRM 51-30-2. 2L73 4F RTA3WE 19951013001331995101300133NM 1995 10 13 UPS204788 119951009A551165382025 SPAR BOEING727 727108C 1384039NM LT HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE ON GROUND, MAINTENANCE FOUND CORROSION BETWEEN LT HORIZONTAL STAB UPPER REAR SPAR CHORD AND SKIN AT STAB STA 215. REMOVED REAR SPAR CHORD, INSTALLED NEW SPAR CHORD AND FABRICATED RELATED PARTS, INSTALLATION PER SRM 51-30-02 SRM 51-21-31, 51-31-31, 55-10-3, EO B727-8510-7484-A/727-55-0300. 2L73 4F A3WE 19951013001341995101300134NM 1995 10 13 UPS504786 119951007A5751 SKIN BOEING757 75724APF 1384969NM RT AILERON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01408UP 23730 WHILE ON GROUND, MAINTENANCE FOUND RT AILERON O/B END LWR SURFACE HAS DOUBLER DELAMINATED. REPAIRED IAW B757-5760-6676. 2L72 4F RTA2NM 19951013001351995101300135WP 1995 10 13 UPS804787 119951008A531257726383335 BLKHD BEAM DOUG DC8 DC873F 302199FWP AFT PRESS BLKHD CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01815UP 46002 (SUPPLEMENTAL MRR) WHILE ON GROUND, MAINTENANCE FOUND AFT PRESSURE BULKHEAD J-BEAMS NR 3 AND NR 4 CRACKED AT CENTER LINE. NR 3 J-BEAM CRACK LENGTH = 3.1250 INCHES, P/N 5772638-33; NR 4 J-BEAM CRACK LENGTH = 3.0 INCHES, P/N 5772638-35. REPAIRED PER E.O. DC8-5310-6598-B. 2L74 4F RT4A25 19951013001761995101300176 1995 10 13 95ZZZX5599 419950803A6122200302 PROP GOVERNOR DHAV DHC3 DHC3 2800202EA HARTZLHCB3T HCB3TN3 GL COCKPIT TO GOV SEIZES A AGJRAK NONE O OTHER ININSP/MAINT 1 NM01904221300 152 BU3988 AIRPLANE MODIFIED PER SERV AERO STC SA3777NM WITH INSTALLATION OF PT6A-135 ENGINE. THE PROPELLER CONTROL REGULARLY BECOMES FROZEN WHEN THE ENGINE IS SHUT DOWN AND BECOMES COLD, THEN LOOSENS UP WHEN THE ENGINE IS STARTED AND WARMS UP. IN THIS CASE, THE CONTROL BECAME FROZEN AND IMMOVEABLE DURING FLIGHT. SUBMITTER STATES THIS IS A RECURRING PROBLEM WITH ALL AIRPLANES INCORPORATING THIS ENGINE MODIFICATION. CONTROLS OF AIRCRAFT QUALITY SHOULD BE INCORPORATED INTO THE MODIFICATION. NOTE: FIRE SLEEVE HAD BEEN INSTALLED ON CONTROL TO PREVENT HEAT DAMAGE, BUT WAS NOT EFFECTIVE. 1H71 3R A815 6 CP15EA 19951013002171995101300217SO 1995 10 13 95ZZZX5640 219950914A7414M3816 CAPACITOR SLICK 6320 CESSNA414 414A 2075907CE CONT O520 TSIO520NB 17040SO LOCK RING CORRODED A CRJAK NONE O OTHER NRNOT REPORTED 1 CE01135BG105 414A0419 519078 MAGNETO FAILED, REMOVED AND DISASSEMBLED AND FOUND SEVERE CORROSION ON DISTRIBUTOR GEAR, PN M-3056, ROTOR GEAR, PN 3828, POINT SET M3081 AND CAPACITOR, PN M-3816. CAUSE OF FAILURE WAS LOCK RING HOLDING PIG TAIL ON CAPACITOR TERMINAL HAD CORRODED AND SPLIT LETTING PIG TAIL CONTACT HOUSING AND SHORTING OUT POINTS. SUBMITTER STATED IT IS CLEAR THIS IS BEING CAUSED BY PRESSURIZATION OF MAGNETOES OFF TURBOCHARGER. PRESSURIZATION LINES SHOULD BE REMOVED. 1L72 3O3 O A7CE E8CE 19951013002211995101300221SO 1995 10 13 95ZZZX5644 119950905A6120B24914 PITCH CHANGE ROD PIPER PA31 PA31350 7103110SO NR 1 ENG PROP SEVERED A AWVBAC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL0159829 317652081 SECOND BEFORE ROTATION, A LOUD BANG AND LOSS OF POWER ON NR 1 ENGINE OCCURRED. PROPELLER WENT INTO FEATHER. INSPECTION OF NR 1 ENGINE, NO DEFECTS FOUND, BUT ENG WOULD NOT TURN MORE THAN 600 RPM. PROPELLER WOULD NOT COME OUT OF FEATHER. REPLACED PROPELLER. NR 1 ENG CHECKED OUT NORMAL. TEAR DOWN OF PROP REVEALED THE PTICH CHANGE ROD WAS SEVERED JUST AFT OF PISTON, PN B-3237, RETAINING FLANGE CROSSING PROP TO ABRUPTLY GO INTO FEATHER. PITCH CHANGE ROD BEING FORWARDED TO HARTZELL FOR FURTHER INVESTIGATION. PROP TSO, 274.00 HRS. 1L72 3O A20SO 19951013002231995101300223SO 1995 10 13 95ZZZX5646 219950908A85206419311075 THROUGH-BOLT CESSNA414 414 2075908CE CONT O520 TSIO520N 17040SO FRONT TOP BROKEN A MOXAK NONE O OTHER ININSP/MAINT 1 EA23616RM3848 712 4140375 22826R WHILE DOING AN INSPECTION, FOUND THE FRONT TOP THROUGH-BOLT BROKEN AT THE THREADED AREA LEFT SIDE OF ENGINE NR 6 CYLINDER. FOUND THE BROKEN END OF THE BOLT WITH THE NUT ON IT, IN THE ENGINE COMPARTMENT. NO RECORD OF BOLT CHANGE. 1L72 3O3 ORTA7CE E8CE 19951013002241995101300224SO 1995 10 13 95ZZZX5647 119950731A32464046 WHEEL PARKERHANFIN GULSTMG44 G44 3951502SO LT MLG FAILED A PNSAO OTHER O OTHER TOTAKEOFF 1 AL0317481 1360 AIRCRAFT WAS ON TAKEOFF ROLL WITH TAIL WHEEL OFF THE GROUND WHEN THE LT WHEEL LET GO. PILOT HEARD LOUD SNAP AND THE HUB CAP BLEW OFF. CHOPPED POWER AND BRAKED. WHEEL WENT CROOKED, SNAPPED BOTTOM BRAKE FITTINGS AND PILOT LOST THE LT BRAKE, GROUND LOOPED, SNAPPED OFF LT FLOAT, BENT LT WING TIP AFT OF SPAR. 1H72 3I O A734 19951013002321995101300232EU 1995 10 13 95FDEA01511 119951009A5230 FITTING AIRBUS310 A310203 EU CARGO DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 LOWER AFT CARGO DOOR ACTUATOR FITTING IS CRACKED AT AFT DRAIN HOLE JUST FWD OF FRAME 62, CRACK IS .102 INCH LONG GOING FWD AND O/B, REF EO 6-5310-7-3301. REPAIRED PER EO 6-5310-7-3301 PART 2, INSTALLED CEILING PANEL. 2L72 4F RTA35EU 19951013002331995101300233NM 1995 10 13 95FDEA01512 119951009A531465C339901 KEEL BEAM BOEING727 72722 1384002NM BS 1077-1085 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 LT/KEEL BEAM IS CRACKED AND CORRODED FROM BS 1077 TO 1085. REPAIRED LT/KEEL BEAM THAT WAS CRACKED AND CORRODED FROM BS 1077 TO 1085 AS PER ENGINEERING EO 7-5310-7-2356 REV C PART 4. UPON FASTENER INSTALLATION FOUND STR 29L TO HAVE DRILL START OUT OF LIMITS. REMOVED AND REPLACED STR SECTION PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951013002341995101300234NM 1995 10 13 95FDEA01513 119951009A5330 SKIN BOEING727 727233 138408ANM BS 1342.4 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 WORKING FASTENERS AT BS 1342.4 STR 8 TO 12R. CUT OUT DAMAGE SKIN, FABRICATED FILLERS AND DOUBLERS. ALODINED AND PRIMED SEALED AND INSTALLED WITH FASTENERS WET WITH SEALANT PER FEDEX SRM 54-30-3. 2L73 4F RTA3WE 19951013002351995101300235NM 1995 10 13 95FDEA01514 119951009A5330 SKIN BOEING727 727233 138408ANM BS 1342.4 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 WORKING FASTENERS AT BS 1342.4 STR 8 TO 14L. CUT OUT DAMAGED SKIN, FABRICATED FILLERS AND DOUBLER, ALODINED AND PRIMED. SEALED REPAIR PARTS AND INSTALLED WITH FASTENERS WET WITH SEALANT PER FEDEX SRM 54-30-3. 2L73 4F RTA3WE 19951013002361995101300236NM 1995 10 13 95FDEA01515 119951009A5330 SKIN BOEING727 727233 138408ANM BS 1218 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 CRACK FOUND IN SKIN AT BS 1218 WL 138.5 RBL 10. STOP DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER ON SKIN, ALL WORK DONE PER FEDEX SRM 53-30-2 AND 51-10-1. 2L73 4F RTA3WE 19951013002371995101300237NM 1995 10 13 95FDEA01516 119951009A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 LOWER FWD CARGO DOOR HAS MULTIPLE LIGHTNING STRIKES ALONG LOWER OUTER SKIN. REPAIRED 10 AREAS OF LIGHTNING STRIKES ALONG OUTER SKIN OF FWD CARGO DOOR LOWER, BS 560 TO 620 3.23 INCHES UP FROM BOTTOM OF DOOR, PER FEDEX SRM 52-00-2, 52-00-3 AND 53-30-3. 2L73 4F A3WE 19951013002381995101300238NM 1995 10 13 95FDEA01517 119951009A5320 SHEAR TIE BOEING727 727225 1384077NM BS 1166 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 AFT CARGO BAY, THERE IS CORROSION ON SHEAR TIES ON AFT SIDE OF FRAME AT BS 1166 RBL 4 LBL 18 WL 150. REMOVED AND REPLACED CORROSION ON SHEAR TIES BS 1166 RBL 4 LBL 18 WL 150, PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19951013002391995101300239NM 1995 10 13 95FDEA01518 119951009A5330 SKIN BOEING727 727225 1384077NM BS 481 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON SKIN UNDER LEVELING COMPOUND AT BS 481, BL 0 WL 150 (C53-113-0161). REPAIRED CORRODED AREA PER FEDEX EA 7-5310-25902 AND SRM 53-10-4. 2L73 4F A3WE 19951013002401995101300240NM 1995 10 13 95FDEA01519 119951009A5313 STRINGER BOEING727 727225 1384077NM BS 530 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STRINGER AT BS 530 LBL 23 WL 151. REMOVED DAMAGE, FABRICATED SPLICE, FILLER AND INSTALLED PER SRM 53-10-3. 2L73 4F A3WE 19951013002411995101300241NM 1995 10 13 95FDEA01520 119951009A5311 FRAME BOEING727 727227 1384078NM BS 580 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 BS 580 ABOVE STR 28R FRAME CRACKED UNDER FLOOR SUPPORT. STOP DRILLED CRACK, FABRICATED PATCH DRILLED IN PLACE REMOVED DEBURRED, ALODINED PRIMED AND PAINTED. INSTALLED WET WITH SEALANT AT BS 580 STR 28R, ALL WORK DONE IAW FEDEX SRM 53-10-2, 51-40-3. 2L73 4F A3WE 19951013002421995101300242NM 1995 10 13 95FDEA01521 119951006A5311 FRAME BOEING727 727227 1384078NM BS 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FRAME CRACKED UNDER FLOOR SUPPORT ABOVE STR 28R BS 600. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951013002431995101300243NM 1995 10 13 95FDEA01522 119951009A5530 STRINGER BOEING727 727227 1384078NM VERT STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 THE NR 8 STR CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6. CUT OUT CRACKED AREA OF NR 8 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 55-30-4. 2L73 4F A3WE 19951013002441995101300244NM 1995 10 13 95FDEA01523 119951009A5530 STRINGER BOEING727 727227 1384078NM VERT STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 THE NR 9 STR CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6. CUT OUT CRACKED AREA OF NR 9 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW FEDEX SRM 55-30-4. 2L73 4F A3WE 19951013002451995101300245NM 1995 10 13 95FDEA01524 119951009A5530 STRINGER BOEING727 727227 1384078NM VERT STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 THE NR 9 STRINGER CRACKED ON LT SIDE OF VERTICAL FIN AT STA 180.6. CUT OUT CRACKED AREA OF NR 9 STR ON LT SIDE VERTICAL FIN AT FIN STA 180.6, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW FEDEX SRM 55-30-4. 2L73 4F A3WE 19951013002461995101300246NM 1995 10 13 95FDEA01525 119951009A5530 STRINGER BOEING727 727227 1384078NM VERT STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 THE NR 9 STRINGER CRACKED ON RT SIDE OF VERTICAL FIN AT FIN STA 157.2. CUT OUT CRACKED AREA OF NR 9 STR ON RT SIDE OF VERTICAL FIN AT FIN STA 157.2, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 55-30-4. 2L73 4F A3WE 19951013002471995101300247NM 1995 10 13 95FDEA01526 119951009A5315 FLOORBEAM BOEING727 727227 1384078NM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CORROSION ON TOP OF BEAM, BS 360 LBL 8 WL 208. REMOVED CORRODED SECTION OF FLOORBEAM LBL 6 TO 9 BS 360. FABRICATED REPAIR PARTS, ALODINED, PRIMED, PAINTED AND INSTALLED PARTS PER FEDEX SRM 53-10-8 FIG 5. 2L73 4F A3WE 19951013002481995101300248NM 1995 10 13 95FDEA01527 119951009A5313BAC1498146 STRINGER BOEING727 727225 1384077NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON STR AT BS 740 LBL 23 WL 150. CORROSION ON STR AT BS 740 LBL 23 WL 150 OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951013002491995101300249NM 1995 10 13 95FDEA01528 119951009A551065245712 BEAM BOEING727 727225 1384077NM RT HORIZ STAB CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION (73C032-03), ON THE T/E AFT UPPER CHORD AT STAB STA 206 AND STA 161 RIGHT HORZ STAB. REMOVED AND REPLACED T/E AFT UPPER CHORD ON RIGHT HORZ STAB, ALL WORK DONE IAW. 2L73 4F A3WE 19951013002501995101300250NM 1995 10 13 95FDEA01529 119951009A5320651758866 BEAM BOEING727 727225 1384077NM BS 264 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25464FE 21288 CORROSION ON 25G BEAM, BS 264 LBL 4 WL 208. REMOVED FLOOR PANELS FOR ACCESS, REMOVED AND REPLACED CORRODED 25G BEAM, BS 264 LBL 4 WL 208. INSTALLED NEW 25G BEAM BS 204 LBL 4 WL 208. REINSTALLED FLOOR PANELS. 2L73 4F A3WE 19951013002511995101300251NE 1995 10 13 95UAL900185 219951010A72611163P0052 OIL FILTER BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 2 ENGINE DIRTY A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP297288U 21566 696515 OIL FILTER BYPASS LIGHT NR 2 CAME ON. OIL PRESSURE NORMAL 45-47 PSI. LIGHT WENT OUT AS THROTTLE REDUCED, BUT CAME BACK ON AT THE NEW SETTING. STAYED ON AT IDLE THRUST. SHUT DOWN NR 2 ENGINE AND RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE: A SMALL AMOUNT OF DEBRIS WAS FOUND IN THE OIL FILTER. REPLACED OIL FILTER AND BYPASS SWITCH AND CLEANED LP 5 AND LP 6 RESTRICTOR FITTINGS. 2L73 4F4 F A3WE E2EA 19951013002521995101300252NE 1995 10 13 95UAL900186 219951010A7230 COMPRESSOR BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LT ENGINE STALLED A UALAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP29611UA 21872 709608 LEFT ENGINE HAD A COMPRESSOR STALL AT FL 390. AIR TEMP MINUS 25 DEGREES. ENGINE ANTI-ICE ON. DESCENDED TO FL 310 AND ALL OPERATIONS NORMAL. NO LIMITS WERE EXCEEDED. ENGINE WAS BORESCOPED AND CHECKED PER MM 71-00-35. NO FAULTS WERE FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. NO ENGINE PROBLEMS WITH STALLING HAVE BEEN NOTED. 2L72 4F4 FRTA1NM E3NE 19951013002531995101300253NE 1995 10 13 95UAL900188 219951010A731437820178 FUEL PUMP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1 ENGINE FAILED A UALAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 WP297459U 6183 21913 696649 NR 1 ENGINE ROLL-BACK 1500 FEET AGL. HAD N1, N2 ROTATION. NO FUEL FLOW ON RESTART CK LIST, RETURNED TO OHARE. LANDED UNEVENTFULLY. EXCESSIVELY WORN SPLINES IN THE FUEL PUMP DRIVE CAUSED FUEL PUMP TO FAIL AND STARVE THE ENGINE. REPLACED PUMP. 2L73 4F4 F A3WE E2EA 19951013002541995101300254NM 1995 10 13 95UAL900189 119951010A2913 HYD PUMP BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE B-HYD SYST FAILED A UALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP297945U 21899 CREW REPORTS, LOSS OF B-SYSTEM HYD FLUID. LANDED ABQ UNDER AMBER ALERT. CHECKED ON GROUND, HAD APPROX 2 GAL B-SYSTEM FLUID LEFT. OUTBOARD B-SYSTEM PUMP SEAL BLOWN. REPLACED BOTH B-SYSTEM PUMPS AND CASE DRAIN FILTERS. 2L73 4F4 F A3WE E2EA 19951013002551995101300255NM 1995 10 13 95UAL900190 119951010A2530 CIRCUIT BREAKERS BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE GALLEY HOT A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29995UA 22399 AFTER PUSH-BACK ON ENGINE START, HAD A HOT ELECTRICAL SMELL FROM GALLEY AREA. SMELL CAME FROM AREA OF CIRCUIT BREAKERS ON FORWARD WALL OF AFT GALLEY. WALL WAS WARM PER FLIGHT ATTENDANT. ALL CIRCUIT BREAKERS PULLED AND COLLARED. OPENED CEILING PANELS, LOOKED AT AREA BEHIND CIRCUIT BREAKERS FOR ELECTRICAL SHORT, FOUND NONE. RE-SET BREAKERS AND COULD NOT SMELL ANYTHING. OPERATED CHILLERS, RAN ENGINE, AND TAXIED. NO ABNORMAL ODORS NOTICED. 2L72 4F4 F A16WE E2EA 19951013002561995101300256NM 1995 10 13 95UAL900191 119951010A551069398801 CHANNEL BOEING737 737322 1384676NM CFMINTCFM56 CFM563B2 13802EU HORIZ STAB CRACKED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29338UA 24242 HORIZONTAL STABILIZER CENTER SECTION, LEFT U-CHANNEL OF BOX WEB ASSEMBLY CRACKED. REPLACED LEFT U-CHANNEL OF BOX WEB ASSEMBLY. 2L72 4F4 FRTA16WE E21EU 19951013002571995101300257NM 1995 10 13 95UAL900192 119951010A3350 EEL BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE EXTERIOR FUS INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29932UA 26658 EXTERIOR EMERGENCY LIGHT INOP ON THE FUSELAGE JUST FWD OF THE AFT PIT. RELAMPED, CHECKED OPERATION AND FOUND OK. 2L72 4F4 FRTA16WE E2GL 19951013002581995101300258NM 1995 10 13 95UAL900193 119951010A3350 EEL BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29348UA 24252 EEL LIGHTS INOP ROWS 11 TO 17. REPLACED BATTERY PACK, OPS CHECKED OK. 2L72 4F4 FRTA16WE E2GL 19951013002591995101300259WP 1995 10 13 ABXA9500785 119950526A53205910142505 PAN DOUG DC9 DC941 302207NWP FS 370-442 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR PAN DENTED AND BOWED. ALSO, THERE WERE SOME DOUBLE DRILLED RIVET HOLES. REPAIRED FORWARD LOWER DOOR JAMB PAN IAW ABX REA D953-11714-MR. 2L72 4F A6WE 19951013002601995101300260WP 1995 10 13 ABXA9500786 119950614A53205912492501 PAN DOUG DC9 DC941 302207NWP FS 200 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR JAMB PAN DENTED AT BAYONET FITTING. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11734-MR. 2L72 4F A6WE 19951013002611995101300261WP 1995 10 13 ABXA9500787 119950602A57135912156159 STRINGER DOUG DC9 DC941 302207NWP WS 200 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEFT WING STRINGER NR 26 HAD PREVIOUS REPAIR AT XRS 200 THAT WAS NOT IAW THE SRM. REPAIRED LEFT WING STRINGER IAW ABX REA D957-11735-MR. 2L72 4F A6WE 19951013002621995101300262WP 1995 10 13 ABXA9500788 119950602A532099234847 INTERCOSTAL DOUG DC9 DC941 302207NWP FS 180 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN INTERCOSTAL AT FS 180 AND BL 0 TO LBL 22 HAD AN IMPROPER REPAIR. REPAIRED IAW ABX REA D953-11736-MR. 2L72 4F A6WE 19951013002631995101300263WP 1995 10 13 ABXA9500789 119950612A53205912492501 PAN DOUG DC9 DC941 302207NWP FS 200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE SERVICE DOOR PAN REQUIRED REPAIR DUE TO ACCOMPLISHMENT OF CUSP ANGLE REPAIRS. REPAIRED SERVICE DOOR PAN IAW ABX REA D953-11737-MR. 2L72 4F A6WE 19951013002641995101300264WP 1995 10 13 ABXA9500790 119950622A571159113011 SPAR CAP DOUG DC9 DC941 302207NWP WS 164 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUS REPAIR ON THE RIGHT WING REAR SPAR AT WS 164.0. REMOVED REPAIR, INSPECTED AREA IAW ASB 57-146. REPAIRED AREA IAW ABX REA D957-11745-MR. 2L72 4F A6WE 19951013002651995101300265WP 1995 10 13 ABXA9500791 119950612A53125910130281 BLKHD WEB DOUG DC9 DC941 302207NWP FS 1072 CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD CHAFED ON THE LEFT SIDE BELOW THE LOWER FIRE EXTINGUISHER BOTTLE. REPAIRED AFT PRESSURE BULKHEAD WEB IAW ABX REA D953-11758-MR. 2L72 4F A6WE 19951013002661995101300266WP 1995 10 13 ABXA9500792 119950607A553059144073 FITTING DOUG DC9 DC941 302207NWP VERT STAB GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT ATTACH FITTINGS ON THE VERTICAL STABILIZER GOUGED AT HORIZONTAL STABILIZER JACKSCREW GIMBAL ATTACH POINTS. REPAIRED FITTINGS IAW ABX REA D955-11779-MR. 2L72 4F A6WE 19951013002671995101300267WP 1995 10 13 ABXA9500793 119950606A532099115311 WINDOW BELT DOUG DC9 DC941 302207NWP FS 389 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, WHILE REPLACING THE WINDOW BELT PANEL AT FS 389, FOUND THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE. REPAIRED WINDOW BELT IAW ABX REA D953-11780-MR. 2L72 4F A6WE 19951013002681995101300268WP 1995 10 13 ABXA9500794 119950718A5330591970733 SKIN DOUG DC9 DC941 302207NWP FS 993 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND MULTIPLE DAMAGED AND CORRODED AREAS ON THE AFT LOWER CARGO COMPARTMENT DOOR JAMB. REPAIRED DOOR JAMB IAW ABX REA D953-11800-MR. 2L72 4F A6WE 19951013002691995101300269WP 1995 10 13 ABXA9500795 119950718A5320591015837 DOOR JAMB DOUG DC9 DC941 302207NWP FS 993 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LOWER CARGO DOOR INTERNAL WEB ON THE DOOR JAMB CORRODED. REPAIRED AFT LOWER CARGO DOOR JAMB WEB IAW ABX REA D953-11804-MR. 2L72 4F A6WE 19951013002701995101300270WP 1995 10 13 ABXA9500796 119950613A532099115311 WINDOW BELT DOUG DC9 DC941 302207NWP FS 465 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND DURING REPLACEMENT OF WINDOW BELT PANEL, THAT THE UPPER AND LOWER AFT CORNER FASTENER HOLES HAD SHORT EDGE DISTANCE AT FS 465R. REPAIRED WINDOW BELT PANEL IAW ABX REA D953-11822-MR. 2L72 4F A6WE 19951013002711995101300271WP 1995 10 13 ABXA9500797 119950630A541459114271 LE SKIN DOUG DC9 DC941 302207NWP RT ENGINE PYLON CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A PREVIOUS REPAIR CORRODED AT THE LEADING EDGE OF THE RIGHT ENGINE PYLON. REPAIRED IAW ABX REA D953-11882-MR. 2L72 4F A6WE 19951013002721995101300272WP 1995 10 13 ABXA9500798 119950620A532099105035 WEB DOUG DC9 DC941 302207NWP FS 1041 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, WHILE REPLACING THE LEFT CUSP WEB AT FS 1041, THE WEB WAS CUT SHORT OF REQUIRED INSTALLATION UNDER THE FRAME FOOT, STA 1041 LEFT SIDE. REPAIRED CUSP WEB IAW ABX REA D953-11947-MR. 2L72 4F A6WE 19951013002731995101300273WP 1995 10 13 ABXA9500799 119950623A532099119903 JAMB DOUG DC9 DC941 302207NWP FS 1165 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AND RIGHT VENTRAL STAIRWAY JAMBS CRACKED AT EXISTING REPAIRS. REPAIRED VENTRAL STAIRWAY JAMBS IAW ABX REA D953-11964-MR. 2L72 4F A6WE 19951013002741995101300274WP 1995 10 13 ABXA9500800 119950627A53205956879501 JAMB DOUG DC9 DC941 302207NWP FS 200 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD ENTRY DOOR JAMB INNER SKIN CRACKED AT LONGERON 11L. REPAIRED ENTRY DOOR JAMB INNER SKIN IAW ABX REA D953-11995-MR. 2L72 4F A6WE 19951013002751995101300275WP 1995 10 13 ABXA9500801 119950711A532099115351 WINDOW BELT DOUG DC9 DC941 302207NWP FS 756 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WINDOW BELT AT FS 756 HAD PREVIOUS CORROSION BLEND OUTS THAT WERE BEYOND SRM LIMITS. REPAIRED RIGHT WINDOW BELT SECTION NR 27R IAW ABX REA D953-12047-MR. 2L72 4F A6WE 19951013002761995101300276WP 1995 10 13 ABXA9500802 119950712A57535912596501 HINGE FITTING DOUG DC9 DC941 302207NWP LT TE FLAP WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT OUTBOARD FLAP HINGE FITTING BEARING HOLE ELONGATED. REPAIRED IAW ABX REA D927-12127-MR. 2L72 4F A6WE 19951013002771995101300277WP 1995 10 13 ABXA9500803 119950605A57435924841507 TRUNNION FITTING DOUG DC9 DC941 302207NWP LT MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT MAIN LANDING GEAR TRUNNION FITTING CORRODED AT THE FORWARD ATTACH LUG. REPLACED TRUNNION FITTING IAW ABX EA SB57-03131-MA. 2L72 4F A6WE 19951013002781995101300278WP 1995 10 13 ABXA9500804 119950607A533059248763 SKIN DOUG DC9 DC941 302207NWP FS 794-879 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT LOWER CARGO COMPARTMENT FORWARD EXTERIOR SKIN FROM LONGERON 26L TO 26R CORRODED FROM FS 794 TO FS 879. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-104, 51-30-2 AND 51-30-5 AND PFEA D953-9883. 2L72 4F A6WE 19951013002791995101300279WP 1995 10 13 ABXA9500805 119950518A53305910228196 SKIN DOUG DC9 DC941 302207NWP FS 1197-1244 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244, CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19951013002801995101300280WP 1995 10 13 ABXA9500806 119950516A553259121669 SKIN DOUG DC9 DC941 302207NWP VERT STAB GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT VERTICAL STABILIZER SKIN GOUGED UNDER THE LOWER HORIZONTAL STABILIZER FAIRING. REPLACED VERTICAL STAB SKIN IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19951013002811995101300281WP 1995 10 13 ABXA9500807 119950617A531359197079 LONGERON DOUG DC9 DC941 302207NWP FS 879-1031 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CORRODED BETWEEN FS 879 AND FS 1031. REPLACED LONGERON 30 SECTION IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951013002821995101300282WP 1995 10 13 ABXA9500808 119950607A53135924878501 LONGERON DOUG DC9 DC941 302207NWP FS 794 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 BLENDED. CORROSION WAS BEYOND SRM LIMITS AT FS 794. REPLACED LONGERON 30 IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-5 AND 51-10-4. 2L72 4F A6WE 19951013002831995101300283WP 1995 10 13 ABXA9500809 119950515A53305910228183 SKIN DOUG DC9 DC941 302207NWP FS 1197-1231 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE PANEL FROM FS 1197 TO 1231 CORRODED BELOW THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19951013002841995101300284WP 1995 10 13 ABXA9500810 119950510A53305910228195 SKIN DOUG DC9 DC941 302207NWP FS 1197-1244 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1244 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19951013002851995101300285WP 1995 10 13 ABXA9500811 119950508A561059124151 EYEBROW WINDOW DOUG DC9 DC941 302207NWP FS 133.4 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CAPTAIN'S EYEBROW WINDOW DELAMINATED. REPLACED CAPTAIN'S EYEBROW WINDOW IAW DC-9 MM CHAPTER 56-10-4. 2L72 4F A6WE 19951013002861995101300286WP 1995 10 13 ABXA9500812 119950511A5400991550015 ANGLE DOUG DC9 DC941 302207NWP FS 1152 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT PYLON WEB UPPER ATTACH ANGLE CRACKED. REPLACED UPPER WEB ATTACH ANGLE IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951013002871995101300287WP 1995 10 13 ABXA9500813 119950627A532059570945 SEAL DEPRESSOR DOUG DC9 DC941 302207NWP FS 200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FORWARD ENTRY DOOR SEAL DEPRESSOR DAMAGED AT LONGERON 10L. REPLACED SEAL DEPRESSOR IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19951013002881995101300288WP 1995 10 13 ABXA9500814 119950522A53305910228184 SKIN DOUG DC9 DC941 302207NWP FS 1197-1231 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN PANEL FROM FS 1197 TO FS 1231 CORRODED UNDER THE RAIN GUTTER. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2L72 4F A6WE 19951013002891995101300289WP 1995 10 13 ABXA9500815 119950524A533059134213 SKIN DOUG DC9 DC941 302207NWP FS 101 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUSLY INSTALLED RIGHT SKIN DOUBLER CRACKED AT AFT HINGE OF RIGHT NOSE LANDING GEAR AFT DOOR. REPLACED SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-10-2. 2L72 4F A6WE 19951013002901995101300290WP 1995 10 13 ABXA9500816 119950522A541299122438 PYLON BLKHD DOUG DC9 DC941 302207NWP FS 1041 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT PYLON BULKHEAD CRACKED SEVERAL PLACES AT FS 1041. REPLACED BULKHEAD WEB IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND DOUGLAS DRAWING NR 9912243. 2L72 4F A6WE 19951013002911995101300291WP 1995 10 13 ABXA9500817 119950629A53125910130387N BLKHD TEE DOUG DC9 DC941 302207NWP FS 1072 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER T-CAP GOUGED IN TWO PLACES AT LONGERON 30. REPLACED LOWER T-CAP SECTIONS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951013002921995101300292WP 1995 10 13 ABXA9500819 119951006A33101495 BULB DOUG DC9 DC932F 3022067WP PILOTS MAP LIGHTFAILED A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23904AX 47040 CAPTAIN'S MAP LIGHT HEATED UP TO THE POINT THAT IT COULD NOT BE TOUCHED. THE PLASTIC HEATED AND CAUSED FUMES IN THE COCKPIT. REPLACED BULB AND OPERATED LIGHT FOR 30 MINUTES, NO FUMES OR EXCESS HEAT NOTED. 2L72 4F A6WE 19951013002931995101300293NM 1995 10 13 SCNA95229 119951005A335010617837 EEL BOEING727 727259 138408JNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE FORWARD LEFT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951013002941995101300294NM 1995 10 13 SCNA95230 119951005A335010617837 EEL BOEING727 727259 138408JNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE AFT RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RESEATED CANNON PLUG ON LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951013002951995101300295NM 1995 10 13 SCNA95231 119951005A335010617837 EEL BOEING727 727259 138408JNM CABIN FAILED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 THE FORWARD RIGHT OVERWING EXIT DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. RESEATED CANNON PLUG ON LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951013002961995101300296NM 1995 10 13 SCNA95232 119951005A3350900835A EEL BATTERY PACK BOEING727 727259 138408JNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE AFT OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CLEANED CORROSION ON BATTERY CONTACTS AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951013002971995101300297NM 1995 10 13 SCNA95233 119951005A33501619 EEL BULB BOEING727 727259 138408JNM L 1 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE L-1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED THE L-1 DOOR EMERGENCY SLIDE LIGHT AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951013002981995101300298 1995 10 13 95UAL900128 419950913A2565 SLIDE BF GOODRICH 7A14312 BOEING747 747222B 1384904NM PWA JT9 JT9D7R4G2 52054NE R3 DOOR TORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29151UA G198 23736 DOOR 3 RT INTERNAL BULKHEAD DAMAGE - TOP HINGE TAPE HAS 2 INCH TEAR AND TOP BULKHEAD HAS 2 INCH SEPARATION. SLIDE SENT TO VENDOR FOR REPAIR. 2L74 4F4 FRTA20WE E3NE 19951013002991995101300299NM 1995 10 13 95UAL900122 119950907A532065B0028312 DOUBLERS BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE BS 340 CRACKED A UALAK NONE O OTHER UKUNKNOWN 1 WP29161UA 21352 THE 65B00283-1, 65B00283-2 DOUBLERS WERE FOUND TO HAVE CRACKS EMANATING FROM THE INBOARD EDGE. THE DOUBLERS WERE PREVIOUSLY INSTALLED BY THE PRIOR OWNER. UAL REPLACED DOUBLERS AND REINFORCED AREA PER BOEING SERVICE BULLETIN 747-53-2112 PER EVA G95-6196. 2L74 4F4 F A20WE E20EA 19951013003001995101300300 1995 10 13 95UAL900187 419951010A2565D31039202 SLIDE BOEING757 757222 1384956NM NR 2 DOOR WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29 DURING TIME CONTROLLED OVERHAUL OF A NR 2 DOOR SLIDE, WEAR WAS FOUND IN THE GIRT FABRIC PASSING THROUGH THE INFLATION TUBE. THIS TYPE OF WEAR HAS BEEN NOTED BEFORE AND IS CAUSED BY THE GIRT ATTACH LANYARD. RETURNED UNIT TO VENDOR FOR REPAIR. (X) 2L72 4F RTA2NM 19951013003591995101300359NE 1995 10 13 95ZZZX5714 219950825A7200 ENGINE BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE NR 2 MAKING METAL A AGDGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW13911LT2000 7503 18009 SHORTLY AFTER TAKEOFF, A NR 2 ENGINE CHIP LIGHT ILLUMINATED. AN UNEVENTFUL PRECAUTIONARY SINGLE ENGINE LANDING WAS MADE. FURTHER INVESTIGATION REVEALED SMALL METAL PARTICLES ON BOTH MAGNETIC PLUGS AND BOTH ELECTRONIC CHIP DETECTORS. THE FILTER ALSO HAD EVIDENCE OF METAL CONTAMINATION. THE ENGINE WAS REMOVED FROM SERVICE WITH 2,000 HOURS TOTAL TIME. 1G72 3U3 UNCH13EU E19EU 19951013003621995101300362WP 1995 10 13 9515119980 119951007A56105912290501 WINDSHIELD DOUG DC9 DC931 3022065WP LEFT CRACKED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL019344 15937 47440 MSP-YQR - DURING CRUISE AT FL 350, 0.78 MACH, THE CAPTAIN'S OUTER WINDSHIELD PANEL CRACKED. RETURNED TO MSP PER DISPATCH AND MAINTENANCE CONTROL DIRECTION. REPLACED THE CAPTAIN'S WINDSHIELD AND WINDOW HEAT CONTROLLER, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951013003631995101300363NM 1995 10 13 9515122771 119951005A3220 TORQUE LINK BOEING727 7272M7 138407SNM NLG DISCONNECTED A NWAAO OTHER E VIBRATION/BUFFET LDLANDING 1 GL01742RW 21952 DURING LANDING ROLLOUT, SEVERE VIBRATION FROM NOSE WHEEL AND STEERING BECAME INOPERATIVE. AIRCRAFT WAS TOWED TO GATE. MAINTENANCE FOUND NOSE GEAR TORQUE LINK DISCONNECTED AND GROUND SHIFT ARM BENT. REPLACED UPPER TORQUE LINK AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19951013003641995101300364EU 1995 10 13 9515133204 119951006A2910 LINE AIRBUS320 A320211 3930320EU RT MLG WW LEAKING A NWAACD ABORTED TAKEOFF RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL01304US 40 DURING TAKEOFF ROLL, RECEIVED HYD 'Y' RSVR LO LVL MESSAGE. TAKEOFF WAS ABORTED AT 60 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPAIRED A LEAKING HYDRAULIC LINE IN THE RIGHT MAIN LANDING GEAR WHEEL WELL. LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951013003651995101300365WP 1995 10 13 9515149603 119950927A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 23R ATTACH FITTING AT FS 996. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951013003661995101300366WP 1995 10 13 9515159946 119950927A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 26L END FITTINGS AT FS 996. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19951013003671995101300367WP 1995 10 13 9515169758 119950927A5311 FRAME DOUG DC9 DC941 302207NWP FS 756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01758NW 47286 DURING LINE CHECK, FOUND A 2.5 INCH VERTICAL CRACK IN THE FS 756, MAIN FRAME INBOARD AFT FLANGE. REPAIRED FRAME (P/N 9923436-1), PER EA 97-103285. 2L72 4F A6WE 19951013003681995101300368WP 1995 10 13 9515179967 119950927A5753 HINGE FTG DOUG DC9 DC931 3022065WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 19488 47263 DURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE BEARING RETAINER PLATE FASTENER HOLES. REPLACED HINGE FITTING (P/N 5919217-502), PER CITEXT 09-5740-1-9800. 2L72 4F A6WE 19951013003691995101300369WP 1995 10 13 9515189613 119950928A5753 FITTING DOUG DC9 DC932 3022066WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613NW 47438 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT FLAP NR 1 WEDGE UPPER OUTBOARD FORWARD CORNER FITTING. REPLACED FITTING PER DWG 5912992 AND SRM 51-30, 51-10. 2L72 4F A6WE 19951013003701995101300370WP 1995 10 13 9515199967 119950928A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND A CRACK IN THE FS 996 FLOORBEAM END FITTING AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19951013003711995101300371WP 1995 10 13 9515209613 119950929A5753 FITTING DOUG DC9 DC932 3022066WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613NW 47438 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT FLAP NR 3 WEDGE INBOARD T-FITTING. REPLACED FITTING PER SRM 51-30, 51-10. 2L72 4F A6WE 19951013003721995101300372WP 1995 10 13 9515219946 119950930A5320 FITTING DOUG DC9 DC931 3022065WP FS 980-996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS AND CORROSION IN THE FS 980 TO 996 FLOORBEAM END FITTINGS, LEFT AND RIGHT SIDES. REPLACED ALL FOUR FITTINGS PER SRM 51-01. 2L72 4F A6WE 19951013003731995101300373NM 1995 10 13 9515222712 119951008A5210 GUIDE ARM BOEING727 7272S7 138407ZNM CABIN DOOR OUT OF ADJUST A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01712RC 22020 DTW-YUL - DURING CLIMB, AT APPROXIMATELY 5,000 TO 6,000 FEET, THE CREW HEARD A POP SOUND FROM THE MAIN CABIN DOOR AND THE AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. RERIGGED THE DOOR GUIDE ARM AND OPERATIONAL CHECK OK. 2L73 4F A3WE 19951013003741995101300374NE 1995 10 13 9515231148 219951006A7261 DE-OILER SHAFT DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 3 ENGINE FAILED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL01148US 46757 686181 DURING CRUISE, THE NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED, OIL QUANTITY WENT TO ZERO AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED, NO FUEL WAS DUMPED. THE DE-OILER SHAFT WAS FOUND SHEARED AND THE AIRCRAFT WAS FERRIED TO MSP WHERE THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19951013003751995101300375NM 1995 10 13 9515246611 119951003A5320 FITTINGS BOEING747 747251B 1384892NM FS 1301/1309 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611US 20356 DURING PERIODIC CHECK, FOUND CORROSION IN THE LBL 120 TO 125 OVERWING LONGERON AT THE FORWARD AND AFT UPLOCK SUPPORT CASTINGS, BS 1301 AND 1309. REPLACED FITTINGS (P/N 65B01332-7, 65B01331-15), PER SRM 53-10-01 FIG 1. 2L74 4F A20WE 19951013003761995101300376WP 1995 10 13 9515259991 119951002A5320 FITTING DOUG DC9 DC931 3022065WP FS 69 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN BOTH FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTINGS. REPLACED FITTINGS PER SRM 51-01. 2L72 4F A6WE 19951013003771995101300377NM 1995 10 13 9515262710 119951008A3242 BRAKES BOEING727 727225 1384077NM LT MLG ON FIRE A NWAAO OTHER A FLAME/FIRE UKUNKNOWN 1 GL01820EA 22557 AFTER LANDING AND PARKED AT THE GATE, GROUND CREW ADVISED THAT THE LEFT MAIN LANDING GEAR WAS ON FIRE. EMERGENCY EQUIPMENT WAS CALLED OUT, BUT NOT REQUIRED. MAINTENANCE REPORTED GREASE FIRE ON THE NR 1 BRAKE. REPLACED THE NR 1 BRAKE AND TIRE. CAUSE FOR EXCESSIVE GREASE UNDER INVESTIGATION. 2L73 4F A3WE 19951013003781995101300378 1995 10 13 9515279943 419951007A3418 AOA TRANSDUCERS DOUG DC9 DC931 3022065WP LT/RT MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 GL011308T 47315 DURING TAKEOFF AT APPROXIMATELY 180 TO 190 KNOTS, STALL WARNING SYSTEM ACTIVATED, CONTINUED TAKEOFF AND CLIMB. AIRCRAFT RETURNED TO MEM, LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT ANGLE OF ATTACK TRANSDUCERS, LEFT FLAP TRANSMITTER AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951013003791995101300379NE 1995 10 13 9515289956 219951010A7261 OIL CAP SEAL DOUG DC9 DC931 3022065WP PWA JT8 JT8D15 52051NE NR 1 ENGINE DAMAGED A NWAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL01923RW 47183 657142 NR 1 ENGINE OIL QUANTITY WAS DECREASING IN FLIGHT, ENGINE WAS RETARDED TO IDLE POWER. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. OIL LOSS WAS CAUSED BY A DAMAGED OIL CAP SEAL. MAINTENANCE REPLACED THE OIL CAP O-RING AND RAN THE ENGINE TO CHECK FOR LEAKS, NO LEAKS NOTED. 2L72 4F4 F A6WE E2EA 19951013003801995101300380NM 1995 10 13 95FDEA01530 119951010A5311 FRAME BOEING727 72725C 138400HNM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133 19851 AFT CARGO FLOOR CRACK IN FRAME AROUND TOOLING HOLE STA 1090 JUST ABOVE STR 27L. BELT FRAME REPAIR ACCOMPLISHED PER SRM 51-40-3 AND DOUBLER INSTALLED. 2L73 4F A3WE 19951013003811995101300381NM 1995 10 13 95FDEA01531 119951010A5311 FRAME BOEING727 72725C 138400HNM BS 1070-1090 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 THE AREA ABOVE CARGO DOOR, CORROSION ON FRAME BETWEEN STA 1070 TO 1090 RT BELOW STR 18R. 2L73 4F A3WE 19951013003821995101300382NM 1995 10 13 95FDEA01532 119951010A5347 SEAT TRACK BOEING727 727233 138408ANM CABIN CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 REMOVED CORROSION AROUND FASTENER HOLES, FLOOR PANEL. THE CORROSION WAS FOUND UNDER SEAT TRACK. REMOVED SEAT TRACK, ORIGINAL THICKNESS ON LONGITUDINAL BEAM .090 UPPER HORIZONTAL FLANGE, FOUND TO BE OUT OF LIMITS MAX ALLOWABLE 10 PERCENT. REMOVED FROM .017 TO .019 ON 10 AREAS APPROX 1 BY 1.5. 2L73 4F RTA3WE 19951013003831995101300383NM 1995 10 13 95FDEA01533 119951010A5313 STRINGER BOEING727 72722 1384002NM BS 385 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION ON STR 26R STA 385 RT, E-BAY. REMOVED DAMAGED AREA OF STR 26R FROM BS 377 TO 393 AND REPAIRED PER FEDEX SRM 53-10-3. ALODINED AND PRIMED ALL EFFECTED AREAS. 2L73 4F A3WE 19951013003841995101300384EU 1995 10 13 95FDEA01534 119951010A4980A4987040000200 MUFFLER AIRBUS310 A310203 EU APU CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25403FE 230 APU EXHAUST ACOUSTIC INTERNAL LINER IS CRACKING AND DETERIORATED THROUGHOUT DUCT, PIECES AS LARGE AS 4 INCH BY 10 INCH ARE MISSING. REMOVED AND REPLACED APU EXHAUST MUFFLER AS PER AMM 49-81-15. 2L72 4F RTA35EU 19951013003851995101300385WP 1995 10 13 95FDEA01535 119951010A3260 PROX SENSOR DOUG DC10 DC1030F 3023504WP LT MLG DEFECTIVE A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25310FE 48299 LT MAIN IND UNSAFE, BOTH PANELS WITH GEAR HANDLE UP. INITIALLY GEAR WENT UP SAFE, BUT AFTER ABOUT 5 SECONDS THE RED LIGHT CAME BACK ON, THIS OCCURRED ON TWO OCCASIONS. FOUND LT/MLG DOWN LOCK SENSOR WIRES DEFECTIVE. REMOVED AND REPLACED POSITION PROXIMITY SENSOR AND CONDUIT PER 32-61-03, CK'D SYS PER TAFI 32-30-00, CK'S OK. 2L73 4F RTA22WE 19951013003861995101300386NE 1995 10 13 95UAL900194 219951011A72301B5129 BEARING BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE SPALLED A UALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP29579UA 26697 726560 LEFT ENGINE OIL FILTER BYPASS INDICATION ILLUMINATED AND OIL TEMPERATURE, PRESSURE AND QUANTITY REMAINED NORMAL. OIL PRESSURE BEGAN TO RISE AND THEN DROPPED TO ZERO. ENGINE WAS SHUTDOWN, TEMP AND QUANTITY REMAINED STEADY. GROUND INSPECTION FOUND METAL IN THE SCREEN AND ON CHIP DETECTORS. ENGINE WAS REMOVED AND SHOP FOUND NUMBER ONE BEARING SPALLED. 2L72 4F4 FRTA2NM E17NE 19951013003871995101300387NE 1995 10 13 DHL95720005 219951005A7200 ENGINE BOEING727 727228 NM PWA JT8 JT8D7B 52053NE NR 1 OVERTEMP A TDHLAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO01720DH 19544 649605 DURING ROTATION, NR 1 EGT WENT INTO RED, PULLED THRUST LEVER BACK TO 1.85 EPR TO KEEP EGT OUT OF RED. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00. 2L73 4F4 F A3WE E2EA 19951013003881995101300388NM 1995 10 13 MWEA95349 119951006A335060030431 EEL POWER SUPPLY DOUG MD88 MD88 3023688NM CABIN INOP A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31701ME 1195 49760 DURING SERVICE CHECK, FOUND AISLE CEILING EMERGENCY LIGHTS AT ROWS 22 THROUGH 25 DID NOT COME ON DURING TEST. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA6WE 19951013003891995101300389WP 1995 10 13 MWEA95350 119951011A3350P401004 EEL BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31502ME 48132 CREW REPORTED FORWARD CABIN EMERGENCY FLASHLIGHT DOES NOT FLASH THE TEST LIGHT. MAINTENANCE REMOVED AND REPLACED BATTERY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951013003901995101300390WP 1995 10 13 MWEA95351 119951013A3350P4010021 EEL BATTERIES DOUG DC9 DC914 3022034WP CABIN DISCHARGED A MWEAK NONE L NO TEST NRNOT REPORTED 1 GL31400ME 45727 CREW REPORTS, FWD EMERGENCY FLASHLIGHT AT FLT ATTENDANT STA HAS WEAK CHARGE. MAINTENANCE REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951013003911995101300391WP 1995 10 13 MWEA95352 119951013A25605917689103 SLIDE COVER DOUG DC9 DC932 3022066WP GALLEY DOOR FELL OFF A MWEAK NONE O OTHER ININSP/MAINT 1 GL31602ME 48133 DURING SERVICE CHECK, FOUND FWD GALLEY SERVICE DOOR EVACUATION SLIDE COVER HAD FALLEN OFF. MAINTENANCE REINSTALLED EVAC SLIDE COVER AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951013003921995101300392WP 1995 10 13 MWEA95353 119951008A5532591213071 SKIN DOUG DC9 DC915 3022036WP VERT STAB CHAFED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING CORROSION TASK INSPECTION OF VERTICAL STABILIZER, FOUND THE LEFT HAND FORWARD SKIN CHAFED UNDER HORIZONTAL STABILIZER FAIRING. MAINTENANCE REMOVED AND REPLACED SKIN IAW 55-01 PG 1, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951013003931995101300393WP 1995 10 13 MWEA95354 119951008A531127779306 FRAME DOUG DC9 DC915 3022036WP BS 786 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31900ME 45841 DURING CORROSION TASK INSPECTION OF AFT CARGO BAY, FOUND LIGHT CORROSION TO AFT FACE OF FRAME BETWEEN LONGERON 39R AND 29L, STA 786. MAINTENANCE INSTALLED REPAIR DOUBLER IAW SRM 53-03, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951013003941995101300394NM 1995 10 13 P5CA9500805 119951010A2720382200012 PCU BOEING747 747122 1384872NM RUDDER CRACKED A P5CAK NONE K FLUID LOSS ININSP/MAINT 1 WP23852FT 19757 DURING SYDNEY GROUND TIME, OBSERVED HYDRAULIC FLUID COMING FROM UPPER RUDDER POWER CONTROL UNIT. FOUND TWO INCH CRACK IN FILTER HOUSING. REPLACED POWER CONTROL UNIT IAW MM 27-21-17. 2L74 4F A20WE 19951013003951995101300395NM 1995 10 13 SCNA95234 119951006A3350S106 EEL BATTERIES BOEING727 7272J4 1384006NM COCKPIT DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15288SC 20765 THE COCKPIT DOOR OVERHEAD EMERGENCY LIGHT TESTED VERY DIM. REMOVED AND REPLACED BATTERIES AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951013003961995101300396NM 1995 10 13 SWAA950656 119951002A5320 POST BOEING737 7373H4 1384600NM COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07686SW 23175 DURING SCHEDULED CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH. REPAIRED PER SWA RA 1-A53-1156. 2L72 4F RTA16WE 19951013003971995101300397NM 1995 10 13 95FDEA01536 119951011A5312 BULKHEAD BOEING727 727227 1384078NM BS 1183 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART, INSTALLED NEW ANGLE PER SRM 51-10-1. 2L73 4F A3WE 19951013003981995101300398NM 1995 10 13 95FDEA01537 119951011A5230 SKIN BOEING727 727233 138408ANM CARGO DOOR DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25165FE 21671 NR 3 CARGO DOOR OUTER SKIN LWR FWD CORNER IS DENTED BEYOND ALLOWABLE LIMITS OF FEDEX SRM 52-00-2. REPAIRED LWR FWD CORNER ON NR 3 CARGO DOOR PER FEDEX SRM 52-00-3. 2L73 4F RTA3WE 19951013003991995101300399NM 1995 10 13 95FDEA01538 119951011A5313 STRINGER BOEING727 727227 1384078NM BS 1070 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 DRILL START / DOUBLE HOLE AT AFT SIDE OF 1070 FRAME ON STR 7L (LOWER SIDE OF STR). BLENDED DAMAGED STR AND FABRICATED REPAIR PARTS. BS 1070, STR 7L. INSTALLED PARTS AND FASTENER WET WITH SEALANT IAW FEDEX 727 SRM 53-10-3 FIG 3. 2L73 4F A3WE 19951013004001995101300400WP 1995 10 13 ABXA9500820 119951011A25105641031521 SEAT DOUG DC8 DC863 302198AWP RT COCKPIT UNLOCKED A ABXAK NONE O OTHER CRCRUISE 1 GL23817AX 45928 FIRST OFFICER'S SEAT WILL NOT LOCK IN THE FORWARD OR AFT POSITION NEAR THE FORWARD END OF THE SEAT TRACK. ADJUSTED FIRST OFFICER'S SEAT ROLLERS I/A/W DC8 MM, CHAPTER 25. LUBRICATED SEAT ROLLERS AND LATCHING MECHANISM. OPS CHECK OF LATCHING MECHANISM WAS GOOD. 2L74 4F 4A25 19951013004011995101300401NE 1995 10 13 ABXA9500821 219951010A7200 ENGINE DOUG DC9 DC941 302207NWP PWA JT8 JT8D11 52044NE RIGHT SEIZED A ABXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL23979AX47339162 47492 676157 RIGHT ENGINE SEIZED ON TAKEOFF ROLL. TAKEOFF ABORTED. REPLACED RIGHT ENGINE. 2L72 4F4 F A6WE E2EA 19951013004021995101300402NM 1995 10 13 DL72E953943 119951001A5753652163234 SPAR BOEING727 727247 138408FNM LT TE MID FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 NR 3 MID FLAP DURING HMV INSPECTION FOUND A CRACKED AFT SPAR CORD 19 INCHES FROM I/B END AND A CRACKED DOUBLER 37 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0 NRC38851 (2) AFT SPAR CORD WAS CRACKED 41 INCHES FROM O/B END. REPAIRED PER M/M 57-52-0. NRC 8852. 2L73 4F A3WE 19951013004031995101300403NM 1995 10 13 DL72E953945 119951009A7110 STRINGER 6519507249 BOEING727 727247 138408FNM NR 1 ENG COWL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W K33573 21329 DURING A HANGAR INSPECTION, A CRACK WAS DISCOVERED IN THE FWD STRINGER OF THE NR 1 ENGINE LWR COWL. A REPAIR WAS INSTALLED PER THE S.R.M. 51-40-3. 2L73 4F A3WE 19951013004041995101300404NM 1995 10 13 DL72E953965 119951002A5330 SKIN BOEING727 727247 138408FNM FS 1148 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 DEFERRED FROM NR 15. WORKED AT HMV, 6 INCHES LONG BY 2 INCHES WIDE, DENTED/SCRATCHED AREA LWR RT FUSELAGE SKIN STA 1148 BETWEEN STR 19R AND 20R. REPAIRED PER SRM 53-30-03. 2L73 4F A3WE 19951013004051995101300405NM 1995 10 13 DL72E953967 119951002A5320 WEB BOEING727 727247 138408FNM BS 913.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 WORKED AT HMV. PERFORM PERMANENT REPAIR, CRACK STA 913.5 LT, PER M/M 53-11-00, PG 816. REMOVED AND INSTALLED REPAIR PER M/M 53-11-00. 2L73 4F A3WE 19951013004061995101300406NM 1995 10 13 DL72E953968 119951003A5720 VENT BOX TAB BOEING727 727247 138408FNM WS 686 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 TAB CRACKED. VENT BOX TAB CRACKED STA. 686.5 AT HOLE MARKED NR 4. WORKED AT HMV. REPAIRED TAB PER M/M 57-13-00. 2L73 4F A3WE 19951013004071995101300407NM 1995 10 13 DL72E953969 119951003A5754 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 NR 4 SLAT-RIB NR 2 CRACKED. WORKED AT HMV. REPAIRED PER M/M 57-40-00, FIG 805. 2L73 4F A3WE 19951013004081995101300408NM 1995 10 13 DL72E953970 119951003A5520 SUPPORT BOEING727 727247 138408FNM RT ELEV CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 RT ELEVATOR-HINGE SUPPORT FRAME CRACKED AT BOLT, INSIDE 3RD BALANCE BAY FROM O/B END, WORKED AT HMV. REPAIRED PER SRM 55-10-04, FIG 6. 2L73 4F A3WE 19951013004091995101300409NM 1995 10 13 DL72E953971 119951003A5713 STRINGER BOEING727 727247 138408FNM LT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 HFEC CHECKED ON STR-TO-RIB HOLES SHOWS CRACK INDICATION ON STRINGER NR 10 AND NR 14 AT W.S. 656.5. WORKED AT HMV. INSTALLED REPAIR DOUBLER PER M/M 57-13-00. 2L73 4F A3WE 19951013004101995101300410NM 1995 10 13 DL72E953972 119951003A5754 HEAT SHIELD BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 NR 6 SLAT-INTERIOR HEAT SHIELD CRACKED BETWEEN RIBS 11 AND 12. WORKED AT HMV. REPAIRED PER M/M 57-54-00, PG 804A. 2L73 4F A3WE 19951013004111995101300411NM 1995 10 13 DL72E953973 119951003A5754 RIB BOEING727 727247 138408FNM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 NR 5 SLAT-RIB NR 20 CRACKED UNDER LEADING EDGE AT NUTPLATE. WORKED AT HMV. REPAIRED PER M/M 57-54-00. 2L73 4F A3WE 19951013004121995101300412NM 1995 10 13 DL72E953974 119951003A5720 VENT BOX TAB BOEING727 727247 138408FNM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 REF OPN 8602 AD HFEC INSP OF RT OUTER WING UPPER STRINGER-TO-RIB CRACK INDICATED FWD VENT BOX AFT TAB W.S. 686.5, MARKED NR 2. 2L73 4F A3WE 19951013004131995101300413NM 1995 10 13 DL72S953933 119951006A5754 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 RIB CRACKED-NR 2 SLAT RIB MARKED NR 11 CRACKED AT LOWER ATTACH ANGLE. CORRECTION-FABRICATED REPAIR PER M/M 57-54-0, PG 805. 2L73 4F A3WE 19951013004141995101300414NM 1995 10 13 DL72S953949 119950925A5330 SKIN BOEING727 727232 1384082NM BS 710/720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 EO144 HEAVY CORROSION WAS FOUND JUST FORWARD OF STA 720 AND OUTBOARD OF STR 28R AND, ALSO, AFT OF STA 710 AND OUTBOARD OF STR 27L. THERE ARE THREE EXISTING DOUBLERS IN THIS REPAIR AREA. THIS ER/A WILL REMOVE THE DAMAGED SECTION OF SKIN AND REPAIR THE DAMAGE WITH A SKIN SPLICE. REPAIRS ACCOMPLISHED PER DL ERA 302541-14AD. 2L73 4F A3WE 19951013004151995101300415NM 1995 10 13 DL72S953953 119951010A531165C362793 FRAME BOEING727 727232 1384082NM BS 761 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11516DA 21432 DURING ACCOMPLISHMENT OF THE MODIFICATION TO THE OVER-WING EXIT FRAME AT STA 761 ON THE LEFT SIDE, THE ADDED FASTENER HOLES THROUGH THE REPAIR ANGLE WEB AND FRAME WERE OVERSIZED TO .25 INCH. 2L73 4F A3WE 19951013004161995101300416NM 1995 10 13 DL72S953956 119951004A57546516224101 SKIN BOEING727 727232 1384082NM NR 1 LE SLAT GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11518DA 21469 DURING SHOP INSPECTION, NR 1 L/E SLAT WAS FOUND WITH LOWER SKIN GOUGED AT ACTUATOR ATTACH RIBS. REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19951013004171995101300417NM 1995 10 13 DL72S953957 119951010A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 FOUND ON CV2 CHECK, CORROSION ON FLOOR BEAM CORRODED AT STA 400 BETWEEN BL ZERO AND RBL 44. REPAIR: REPAIRED PER MM 53-20-11, FIG 804 A. 2L73 4F A3WE 19951013004181995101300418NM 1995 10 13 DL72S953958 119950921A3211 TRUNNION FTG BOEING727 727232 1384082NM LT MLG TRUNNION CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 UPON HMV, FOUND LT MLG FWD TRUNNION FITTING INNER FACES CORRODED. REMOVED BUSHINGS...BLENDED SURFACES WITHIN LIMITS PER M/M 57-43-0. 2L73 4F A3WE 19951013004191995101300419NM 1995 10 13 DL72W953950 119950929A531165C362803 FRAME BOEING727 727247 138408FNM BS 783.95 MISDRILLED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112821W 21059 EO144 DURING ACCOMPLISHMENT OF E.O. 4-61904-3AD FOR THE LT STA 783.95 FRAME, MTC FOUND THAT ONE OF THE FASTENERS INSTALLED THROUGH FRAME AND RING DOUBLER (65-16236-35) FELL OUT IN THE RADIUS OF THE 65C36280-3 REPAIR ANGLE. REPAIRS ACCOMPLISHED PER DL ERA 302567-14AD. 2L73 4F A3WE 19951013004201995101300420NM 1995 10 13 DL733953944 119951009A2510416000121 COFFEEMAKER BOEING737 737347 1384647NM LT COCKPIT SMOKED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11313WA 2031 23599 LOUD POP HEARD FROM AFT COFFEEMAKER FOLLOWED BY ELECTRIC SMOKE. REPLACED COFFEEMAKER CAPT SIDE AFT. 2L72 4F RTA16WE 19951013004211995101300421 1995 10 13 DL757953948 419951010A2210 AUTO PILOT 6224717003 BOEING757 757232 1384965NM FLIGHT DECK FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11603DL 1141 22810 EO144 FLT DIVERTED TO LAS WITH IN-FLIGHT EMERGENCY-SMOKE IN COCKPIT. FOUND RT A/P INOP ON ARRIVAL AND HEAVY BURNED SMELL EMANATING FROM RT SIDE OF A/P MODE CONTROL PANEL. INSTALLED NEW A/P. MCP AND PERFORMED TEST 01/04 AND 01/30 WITH MCDP. ALL NORMAL. 2L72 4F RTA2NM 19951013004221995101300422NM 1995 10 13 DL76S953955 119951010A2121 FAN 6066223 BOEING767 767332 1382001NM FLIGHT DECK FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11132DN 401334 24981 ELECTRICAL OVERHEATING ODOR IN COCKPIT AT FL370 FOR APPROX 30 SECS. LATER, RT RECIRC FAN EICAS MSG ILLUMINATED. RT RECIRC FAN TO OFF POS. RT RECIRC FAN FAILED. REPLACED FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19951013004231995101300423NE 1995 10 13 DLL13953981 219951006A7261727706605 OIL PUMP LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11787DL 193A1126 ON CLIMB-OUT, HAD STRONG BURNING ODOR IN AFT CABIN, RETURNED ATL. DETERMINED ODOR SOURCE NR 2 ENGINE. REPLACED ENGINE OIL PUMP AND PERFORMED DUCT BURN-OUT AND REPLACED WATER SEPARATOR BAGS, OPERATION NORMAL. 2L73 4F4 F A23WE A12EU 19951013004241995101300424WP 1995 10 13 DLL16953954 119951010A3350 EEL CHARGER 5165741 LKHEED1011 10113853 5265020WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11760DH 56672 193Y1194 AFT CABIN EMERG LIGHT INOP, FOUND DURING MTC. REPLACED AFT RT EMERG LIGHT CHARGER ASSY, CKS OK. 2L73 4F A23WE 19951013004251995101300425NM 1995 10 13 DLM88953980 119951009A2910 HYD LINE DOUG MD88 MD88 3023688NM AFT FUSELAGE LEAKING A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11930DL 49717 ON CLIMB-OUT, HAD HOT OR BURNING ODOR IN CABIN AND FLIGHT DECK, RETURNED ATL. FOUND HYDRAULIC LINE LEAKING AND FLUID DRAINING INTO APU INLET. SECURED LINE, OPERATION NORMAL. 2L72 4F RTA6WE 19951013004261995101300426NM 1995 10 13 UPS204752 119951010A5315 FLOOR BEAM BOEING727 727108 NM BS 328 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON FL BEAM STA 328, LBL 33 WL 208, ALSO, HAS MECH. DAMAGE LBL 54 WL 208. REPAIRED FL BEAM PER 727 SRM 53-10-08, FIG 7. 2L73 4F RTA3WE 19951013004271995101300427NM 1995 10 13 UPS204753 119951010A3230652448295 UPLOCK HOOK BOEING727 727108 NM LT MLG CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND LT UPLOCK HOOK HAS EXCESSIVE PLAY. FOUND UPLOCK CORRODED. REMOVED UPLOCK ASSY AND REPLACED WITH NEW PART PER MM 32-32-51, 32-32-61, 32-32-0. 2L73 4F RTA3WE 19951013004281995101300428NM 1995 10 13 UPS204754 119951010A5330 SKIN BOEING727 727108 NM BS 272-275 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (53-221-01.00-01) ON SKIN AT BS 272-275, LBL 56, WL 209-213. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, TRIMMED OUT DAMAGED AREA, FABED REPAIR DOUBLER, FINAL REPAIR PER SRM 53-30-1, 53-30-2, 51-10-2, 51-30-2. 2L73 4F RTA3WE 19951013004291995101300429NM 1995 10 13 UPS204755 119951010A5320 WEB BOEING727 727108 NM BS 600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND SUPPORT WEB TO BE CRACKED AT BS 600, LBL 7, WL 300. REPAIRED AREA PER E.O. B727-53-1683. 2L73 4F RTA3WE 19951013004301995101300430NM 1995 10 13 UPS204756 119951010A5315BAC1505100617 FLOOR BEAM BOEING727 727108 NM BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON BEAM STA 420 LBL 0 TO LBL 24 AND LBL 45 - LBL 65 WL 208 LWR SIDE OF UPPER CHORD. REMOVED CORROSION ON UPPER CHORD OF FLOOR BEAM. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED UPPER CHORD OF FLOOR BEAM PER UPS EO B727-5310-7455A. 2L73 4F RTA3WE 19951013004311995101300431NM 1995 10 13 UPS204757 119951010A5315BAC1505100617 FLOOR BEAM BOEING727 727108 NM BS 420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-01) ON FLOOR BEAM STA 420 RBL 45-65 WL 208 LWR SIDE OF UPPER CHORD. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED IAW UPS E.O. B727-5310-7455A. 2L73 4F RTA3WE 19951013004321995101300432NM 1995 10 13 UPS204758 119951010A5511 RIB BOEING727 727108 NM HORIZ STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION IN BORE FOR BOTTOM BUSHING AND OUTBOARD FACE ON UPPER THRUST RIB LUG FOR LWR SPLICE BEAM AT APPROX. RUDDER STA 128.765 LT. REMOVED CORROSION AND OVERSIZE BORE, INSTALL OVERSIZED BUSHING IAW TRAMCO EWO 95-3072. 2L73 4F RTA3WE 19951013004331995101300433NM 1995 10 13 UPS204783 119951010A5755 SKIN BOEING727 72727C 138400JNM NR 8 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR D-CHECK, MAINTENANCE FOUND NR 8 SPOILER HAS AN AREA OF 7 INCHES BY 7 INCHES DELAMINATED ON INBOARD FWD CORNER AND AREA 8 INCHES BY 8 INCHES DELAMINATED ON FWD OUTBOARD CORNER, BOTH ON UPPER SURFACE. REMOVED DAMAGED SKIN, VERIFIED DAMAGE REMOVAL, FABRICATED REPAIR AND INSTALLED IAW SRM 51-40-6. 2L73 4F A3WE 19951013004341995101300434NM 1995 10 13 UPS204784 119951010A2750652661418 BALL NUT BOEING727 72727C 138400JNM LT TE FLAP WORN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT INBOARD TRAILING EDGE FLAP INBOARD JACKSCREW BALL NUT WORN. REMOVED AND REPLACED JACKSCREW ASSY PER OHM 27-54-04. 2L73 4F A3WE 19951013004351995101300435NM 1995 10 13 UPS204785 119951010A5315BAC150529222 FLOOR BEAM BOEING727 72727C 138400JNM BS 344 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CENTER OF STA 344 FLOOR BEAM CORRODED AROUND FASTENER HOLES WHILE WORKING CARD 376276. REMOVED CORRODED PORTION OF FLOOR BEAM THAT WAS PREVIOUSLY REPLACED. FABRICATED REPLACEMENT BEAM PER SRM 53-10-2 AND 53-10-1. INSTALLED REPAIR PARTS PER SRM 51-10-2. 2L73 4F A3WE 19951013004361995101300436NM 1995 10 13 UPS204789 119951010A553169133001 SPAR BOEING727 727108C 1384039NM VERT STAB CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01936UP 19503 WHILE IN FOR SI CHECK, MAINTENANCE FOUND CORROSION ON VERTICAL FIN REAR SPAR CHORD, RUDDER STA 223-STA 238 WHERE PANEL 9515 MATES LT SIDE. REMOVED AND INSTALLED FABRICATED PARTS. WORK DONE IAW E.O. B727-5530-7482A. 2L73 4F A3WE 19951013004371995101300437NM 1995 10 13 UPS204793 119951007A5311 FRAME BOEING727 72727C 138400JNM BS 805 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND, WHILE WORKING NRC 376230, CRACK ON FRAME AT STA 805 RBL 66-70, WL 210. REPLACED FRAME SEGMENT PER SRM 51-30-2, 51-10-2, 51-20-1. 2L73 4F A3WE 19951013004381995101300438NM 1995 10 13 UPS204794 119951007A5754 ANGLE BOEING727 72727C 138400JNM NR 2 LE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP ACT. ATTACH FITTING ON ACFT SIDE CRACKED AT INBD UPPER ANGLE. REMOVED AND REPLACED UPPER LT ANGLE ON NR 2 K-FLAP SUPPORT PER SRM 57-40-00 AND 51-30-2. 2L73 4F A3WE 19951013004391995101300439NM 1995 10 13 UPS204797 119951007A52306518625108 ANGLE BOEING727 72727C 138400JNM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FWD ANGLE CRACKED FOR AFT HINGE INTERCOSTAL ON AFT CARGO DOOR. REMOVED DAMAGED ANGLE, INSTALLED NEW WEB AND ANGLE PER SRM 51-30-2, DWG 65-18625, SRM 51-40-01. 2L73 4F A3WE 19951013004401995101300440NM 1995 10 13 UPS204798 119951007A575465817879 ATTACH LUG BOEING727 72727C 138400JNM NR 4 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 K-FLAP HAS PITTING CORROSION ON INBOARD ATTACH LUG OF BULLNOSE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY PER SRM 27-81-01, 27-81-00. 2L73 4F A3WE 19951013004411995101300441NM 1995 10 13 UPS204799 119951007A575465162268A ATTACH LUG BOEING727 72727C 138400JNM NR 5 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 5 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE IS CORRODED AT BOTH FASTENER HOLES. REMOVED AND REPLACED K-FLAP ASSY PER MM 27-81-01, 27-81-00, E.O. B727-5750-5542. 2L73 4F A3WE 19951013004421995101300442NM 1995 10 13 UPS204800 119951007A5754 ATTACH LUG BOEING727 72727C 138400JNM NR 6 LE FLAP CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 K-FLAP OUTBOARD ATTACH LUG OUTBOARD SIDE HAS CORROSION AROUND LWR FASTENER HOLE. REMOVED AND REPLACED COMPLETE K-FLAP ASSY. ARM ADDENDUM 727-5750-5542, 51-30-2, MM 27-81-01, 27-81-00. 2L73 4F A3WE 19951013004431995101300443NM 1995 10 13 UPS204801 119951007A5720 BRACKET BOEING727 72727C 138400JNM WS 198 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED BRACKET AT WS 198.0 ON THE UPPER REAR SPAR CHORD LT SIDE. REMOVED DAMAGED BRACKET, FABED NEW ANGLE AND INSTALLED ALL PER SRM 51-20-1, MM 27-51-00. 2L73 4F A3WE 19951013004441995101300444NM 1995 10 13 UPS204802 119951007A5720 ANGLE BOEING727 72727C 138400JNM WS 198 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED ATTACH ANGLE AT WS 198.0 ON THE UPPER REAR SPAR CHORD, RT SIDE. REMOVED DAMAGE ANGLE, FABED NEW PART AND INSTALLED. ALL WORK PER SRM 51-20-1, MM 27-51-00. 2L73 4F A3WE 19951013004451995101300445WP 1995 10 13 UPS804745 119951003A2560 SLIDE DOUG DC8 DC871F 302199DWP EMER EXIT DOOR UNSECURED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01703UP 45939 WHILE ON GROUND, MAINTENANCE FOUND ENTRY DOOR EVACUATION SLIDE GIRTH BAR FAILED TO LATCH. REPACKED EVACUATION SLIDE. 2L74 4F RT4A25 19951013004461995101300446WP 1995 10 13 UPS804747 119951003A3260 CONNECTOR DOUG DC8 DC871F 302199DWP NLG LOOSE A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01755UP 46055 WHILE ON DEPARTURE FOR CLEVELAND, PILOT REPORTS ON UPLATCH CHECK, NOSE EXTENDED WITH GEAR NOT LATCHED LIGHT ILLUMINATED. UPLATCH CHECK PASSED ON 3RD ATTEMPT. PLUG NOT LATCHED ON SW. RESECURED, LUBED NOSE GEAR AS A PRECAUTION. CHKED PER MM 32-60-00, PG 201. 2L74 4F RT4A25 19951013004471995101300447WP 1995 10 13 UPS804790 119951010A53203755843501 FITTING DOUG DC8 DC871F 302199DWP FS 1220 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01798UP 45898 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD LOWER FLANGE OF FITTING CRACKED FS 1220 BETWEEN LONGERON 34R AND 35R. REMOVED DAMAGED FITTING ON FS 1220 LONGERON 34R - 35R AND REPLACED NEW FITTING PER SRM 53-2-0. 2L74 4F RT4A25 19951013004481995101300448WP 1995 10 13 UPS804791 119951009A3231 RELEASE PIN DOUG DC8 DC873F 302199FWP LT MLG DOOR DIRTY A IPXAK NONE O OTHER CLCLIMB 1 SO01814UP 46090 CREW REPORTED LOUD NOISE IN NOSE HEARD UPON GEAR RETRACTION. NOISE STOPPED WHEN GEAR EXTENDED. AIR TURN BACK. FOUND FWD LT DOOR LINK-RELEASED PIN DIRTY AND HALF HUNG UP. CLEANED AND LUBED LT DOOR LINK, OPS CK OK. 2L74 4F RT4A25 19951013004491995101300449WP 1995 10 13 UPS804792 119951010A3260 SWITCH DOUG DC8 DC871F 302199DWP LT MLG DOOR MALFUNCTION A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01715UP 45915 CREW REPORTED ON DEPARTURE, ROD GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. CYCLED GEAR AND PERFORMED UPLATCH CHECK. LIGHT WENT OUT. HOWEVER, LT MAIN AMBER ALTERNATE GEAR DOOR LIGHT REMAINED OUT, UNTIL APPROACH IN TURBULANCE, THEN AMBER LIGHT WENT OUT. REMOVED AND REPLACED LT GEAR ALTERERNATE SWITCH. C/W ADJ AND TEST PROCEDURES OF POS. AND WARNING SYS. PER DCE MM 32-60-00, PG 203, SYS OPS NORMAL. 2L74 4F RT4A25 19951013004501995101300450WP 1995 10 13 UPS804795 119951011A33506012233 EEL BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01748UP 45948 CREW REPORTED EMERGENCY LIGHTS CAME ON IN-FLIGHT AND WOULD NOT GO OUT. REPLACED EMERGENCY BATTERY PACK. 2L74 4F RT4A25 19951013004511995101300451WP 1995 10 13 UPS804796 119951011A2910 O-RING DOUG DC8 DC871F 302199DWP SLOT CNTRL VALVEFAILED A IPXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01700UP 45900 CREW REPORTED HYDRAULIC SYSTEM LOST FLUID RAPIDLY IN CRUISE EMERGENCY SHUT-DOWN. HYD FLUID FELL TO STANDPIPE. FOUND O-RING BLOWN ON SLPT INLET CHECK VALVE ON SLOT CONTROL VALVE. REPLACED O-RINGS ON CHECK VALVE. LEAK CHK NORMAL PER DC8 MM 27-80-04, PG.201. CHANGED NR 3 ENG HYD PUMP AND FILTERS IAW MM 29-10-12. SERVICED HYD RESERVOIR IAW 12-30-01. 2L74 4F RT4A25 19951013004701995101300470NM 1995 10 13 95ZZZX5735 119950610A2150 INLET VALVES BOEING727 727290 138408WNM AIR COND BAY OUT OF POSITION A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11774AT 21510 BFM - ON CLIMB-OUT, PACKS OVERHEAT WITH FLAPS UP. RETURNED TO BFM. REPOSITIONED RAM AIR INLET VALVES. 2L73 4F A3WE 19951013004711995101300471NM 1995 10 13 95ZZZX5736 119950720A33503300015 EEL CHARGER BOEING727 727290 138408WNM CABIN FAILED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11774AT 002025 21510 MDW - AT DEPARTURE, AFT SECTION OF EGRESS FLOOR LIGHTS WOULD NOT TEST. REMOVED AND REPLACED AFT EGRESS BATTERY PACK CHARGER. 2L73 4F A3WE 19951013004721995101300472SO 1995 10 13 95ZZZX5737 119950726A52105382700 LATCH SPRING PIPER PA31 PA31350 7103110SO CABIN DOOR STRETCHED A ECAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA1178GH 317852121 ON GROUND, CABIN DOOR WAS PROPERLY CLOSED AND LATCHED. DOOR LIGHT OUT. AFTER TAKEOFF AND DURING CLIMB, HEARD A RUSH OF AIR. DOOR LIGHT WAS ON. DOOR SEEMED TO BE LATCHED. RETURNED TO AIRPORT FOR VISUAL INSPECTION. INITIALLY NO DEFECTS NOTED. IN-DEPTH INSPECTION FOUND LATCH SPRING ON LOWER DOOR REAR LATCH PIN STRETCHED. REPLACED THE STRETCHED SPRING, PN 53827-00. OPS CHECK GOOD. 1L72 3O A20SO 19951013004731995101300473SO 1995 10 13 95ZZZX5738 119950815A24342317 ALTERNATOR PIPER PA32 PA32300 7103212SO ENGINE FAILED A ECAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA11250WA 327840102 PILOT REPORTED COMPLETE COMM FAILURE AS WELL AS TRANSPONDER REPORTED INOP BY ATC. PILOT RETURNED TO FRG WITHOUT INCIDENT. INSPECTED AND FOUND BATTERY VOLTAGE BELOW 10 VOLTS. STARTED AIRCRAFT WITH GPU. ALTERNATOR LIGHT WAS ILLUMINATED. ALTERNATOR WAS REMOVED AND REPLACED. AIRCRAFT BATTERY WAS REMOVED AND SERVICED. AIRCRAFT WAS GROUND RUN. OPS CHECKED OK. 1L71 3O A3SO 19951013004741995101300474WP 1995 10 13 CAL950770 119950820A5320 ANGLE DOUG DC9 DC982 3022082WP FWD BAGGAGE BIN CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND THRESHOLD Z-ANGLE CORRODED IN FORWARD BAGGAGE BIN. THE AREA WAS REPAIRED IAW SRM 53-01 AND SRM 51-10-1. (X) 2L72 4F A6WE 19951013004751995101300475WP 1995 10 13 CAL950771 119950821A5311 BELT FRAME DOUG DC9 DC982 3022082WP BS 1309 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND BELT FRAME CORRODED AT STA 1309, LONGERON 27L TO LONGERON 27R. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED AND PRIMED IAW SRM 53-01. (X) 2L72 4F A6WE 19951013004761995101300476WP 1995 10 13 CAL950772 119950821A5712 RIB DOUG DC9 DC982 3022082WP RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND A 3 INCH CRACK IN RT WING RIB. A DOUBLER WAS INSTALLED IAW SRM 57-06, FIGURE 5. (X) 2L72 4F A6WE 19951013004771995101300477WP 1995 10 13 CAL950773 119950821A5330 SKIN DOUG DC9 DC982 3022082WP BS 1193 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND A 1 INCH LONG DENT IN SKIN AT STA 1193, LONGERON 19L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 21. (X) 2L72 4F A6WE 19951013004781995101300478WP 1995 10 13 CAL950774 119950821A5712 RIB DOUG DC9 DC982 3022082WP NR 9 FLAP TRACK CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND A 1 INCH CRACK AT LOWER FLANGE OF FOURTH RIB OUTBOARD OF NR 9 FLAP TRACK. A NEW RIB WAS INSTALLED IAW SRM 51-30-2 AND SRM 51-30-5. (X) 2L72 4F A6WE 19951013004791995101300479NM 1995 10 13 CAL950786 119950902A3350 EEL FUSE BOEING737 737524 1384721NM CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914604 27317 IAH - FLT 1510 - INSPECTION FOUND MIDDLE ZONE OF AISLE PATH LIGHTING INOPERATIVE. A BLOWN FUSE WAS FOUND IN THE AFT EMERGENCY PATH LIGHTING BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE AISLE PATH LIGHTING WAS RESTORED. (X) 2L72 4F RTA16WE 19951013004811995101300481 1995 10 13 JBXA089501 419950725A2565D30664105 EVAC SLIDE AIRBUS320 A320231 3930325EU L-1 DOOR DEPLOYED A JBXAO OTHER O OTHER TXTAXI/GRND HDL 1 GL31301ML A5791 315 RDU/FLL - FLT 33 - UPON ARRIVAL AT GATE, FLIGHT ATTENDANT LIFTED DOOR OPEN HANDLE WITHOUT DISARMING SLIDE. DOOR CONTACTED JETWAY, AND DID NOT FULLY OPEN. SLIDE UNRAVELED, BUT DID NOT DEPLOY DUE TO DOOR STRIKING JETWAY. AIRCRAFT FERRIED TO RDU WHERE SLIDE WAS REPLACED AND DOOR RESERVICED. NO DAMAGE TO DOOR. (X) 2L72 4F RTA28NM 19951013004821995101300482EU 1995 10 13 JBXA089502 119950725A3230 RELAY FOKKERF28 F28MK0100 4990807EU LANDING GEAR MALFUNCTIONED A JBXAA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL31109ML 11485 RDU/PBI - FLT 304 - AIR RETURNED TO RDU DUE TO LANDING GEAR HANDLE WOULD NOT LIFT. MAINTENANCE FOUND ANTI-RETRACTION SOLENOID DID NOT RETRACT. ENTERED A DEFERRED MAINTENANCE ITEM. SYSTEM OPERATED NORMALLY FROM TIME OF FIRST FAILURE. SUSPECT RELAY STICKING. CLEANED DMI UPON RETURN TO RDU. (X) 2L72 4F RT 19951013004831995101300483CE 1995 10 13 MASA9516 119950830A3260H111541 SWITCH BEECH 1900 1900D 1154162CE NLG OUT OF ADJUST A MASAK NONE P NO WARNING INDICATION APAPPROACH 1 SW01162ZV UE162 DURING APPROACH INTO DUBOIS, PA, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWN AND LOCK INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED NOSE DRAG BRACE DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19951013004841995101300484NM 1995 10 13 MRKA9566 119950829A3350873100212 EEL BOEING737 7372X6C 1384552NM CABIN INOPERATIVE A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 EEL STROBE LIGHT INOPERATIVE. REMOVED AND REPLACED EEL STROBE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X) 2L72 4F RTA16WE 19951013004851995101300485NM 1995 10 13 P2EA95007 119950813A5101 STRUCTURE BOEING737 737205 NM AIRFRAME BIRD STRIKE A P2EAA UNSCHED LANDING C F.O.D. CLCLIMB 1 CE05412CE 20412 MCI - FLT 112 - CREW REPORTED SEVERAL BIRD STRIKES ON ROTATION. AIRCRAFT MADE AIR RETURN TO MCI. MAINTENANCE INSPECTED AIRFRAME AND ENGINES PER MM. NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A16WE 19951013004861995101300486EU 1995 10 13 RAIA950903 119950905A7921L86023281 COOLER JETAIRJETSTMJETSTM4101 1500501EU LT ENGINE LEAKING A RAIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 CE03550HK1716 41039 SUX - FLT NR 7216 - LOST OIL PRESSURE ON NR 1 ENGINE IN FLIGHT, PERFORMED PRECAUTIONARY SHUTDOWN. MAINTENANCE REPLACED LEFT ENGINE OIL COOLER. GROUND RUNS REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA41NM 19951013004871995101300487NE 1995 10 13 UIEA9504 219950827A73107321686003 SHUT-OFF VALVE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE LT ENGINE FAILED A UIEAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 EA15507MC 21380 517269 ON LEVEL OFF FROM A CLIMB TO F350, THE NR 4 ENGINE FLAMED OUT FOR NO APPARENT REASON. AIRCRAFT DIVERTED INTO JFK. FOUND NR 4 ENGINE FUEL SHUT OFF VALVE FAILED. REPLACED FUEL SHUT OFF VALVE ACTUATOR PER MM 76-11-04. OPS AND RUN-UP OK. ENGINE INLET, TAIL PIPE, INSPECTED OK. ACCOMPLISHED 'NO OIL PRESSURE' INSPECTION, MM 72-00-00. (X) 2L74 4F4 F A20WE E23EA 19951013004881995101300488EU 1995 10 13 VTZA95285 119950910A711014171020405 COWLING JETAIRJETSTMJETSTM4101 1500501EU RT NACELLE DAMAGED A VTZAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA27320UE 401 41043 IAD/JFK - FLT 6437 DURING CRUISE AT 1530 HOURS ON 9-10-95, A PORTION OF THE UPPER RT COWLING ASSEMBLY DETACHED FROM THE AIRCRAFT IN-FLIGHT. AIRCRAFT LANDED AT JFK WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED DAMAGE TO COWLING. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951013004891995101300489WP 1995 10 13 95ZZZM525 119950822A3231S2210370P9157 BUSHING DOUG DC9 DC982 3022082WP LT MLG DOOR MISSING A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE05920TW 49369 MCI - DURING CLIMB, LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AND LEFT MAIN LANDING GEAR UNSAFE RED LIGHT ILLUMINATED. VERIFIED LANDING GEAR WAS DOWN, AND DOOR REMAINED OPEN. FOUND LEFT MAIN LANDING GEAR DOOR ACTUATOR BUSHING, MFG P/N S2210370P9-157, MISSING. INSTALLED BUSHING AND LANDING GEAR AND LANDING GEAR DOOR OPERATION CHECKED NORMAL. 2L72 4F A6WE 19951013004901995101300490NM 1995 10 13 95ZZZM526 119950714A5320 DECK BOEING727 727231 1384079NM BS 950 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE055433162690 20309 MCI - DURING C-CHECK, FOUND TWO CRACKS EACH WERE APPROXIMATELY ONE INCH LONG, IN LEFT MLG WHEELWELL CEILING PRESSURE DECK AFT OUTBOARD CORNER, FORWARD OF 590 BULKHEAD, LBL 56 AND 58. REPAIRED BY INSTALLING DOUBLER PER ARA 9372. TOTAL CYCLES 42,177. 2L73 4F A3WE 19951013004911995101300491NM 1995 10 13 95ZZZM527 119950822A2530B006781 CONTROLLER BOEING747 747131 1384881NM SERVING CART FAILED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE SMOKE AND ELECTRICAL ODOR EMITTED FROM AFT GALLEY E-1 SERVING CART CONTROLLER, MFG P/N B00678-1. TURNED OFF CONTROLLER AND OPENED CIRCUIT BREAKERS. REPLACED THE E-1 CART CONTROLLER AND OPERATION CHECKED NORMAL. 2L74 4F A20WE 19951013004921995101300492NM 1995 10 13 95ZZZM528 119950822A2530888011 SERVING CART BOEING767 767231 1385131NM NR 4 FAILED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05605TW 22568 JFK - DURING CRUISE AFT GALLEY SERVING CART NR 4, EMITTED SMOKE AND ELECTRICAL ODOR. TURNED OFF AND DISCONNECTED CART, MFG P/N 88801-1. FOUND MALFUNCTIONING HEATING PLATES. REPLACED SERVING CART AND OPERATION CHECKED NORMAL. 2L72 4F RTA1NM 19951013004931995101300493NM 1995 10 13 95ZZZM529 119950714A5330 SKIN BOEING727 727231 1384079NM BS 720 WORN A TWAAK NONE O OTHER ININSP/MAINT 1 CE055434938173 21968 MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .030 TO .015, STRINGER 17R TO 19R, AND STRINGER 17L TO 19L, FS 720E TO 720F, ALSO WORN APPROXIMATELY .040, STRINGER 19L. REPAIRED PER ARA 9354. TOTAL CYCLES 24,723. 2L73 4F A3WE 19951013004941995101300494NM 1995 10 13 95ZZZM530 119950714A5532 SKIN BOEING727 727231 1384079NM FS 1330 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554349 21968 MCI - DURING OP-17, FOUND A ONE INCH CRACK IN SKIN ON VERTICAL STABILIZER LEFT SIDE AT BASE, FS 1330. STOP DRILLED CRACK PER SRM 51-10-1, AND REPAIRED PER ARA9370A. TOTAL CYCLES 24,723. 2L73 4F A3WE 19951013004951995101300495WP 1995 10 13 95ZZZM531 119950802A5347 SEAT TRACK DOUG DC9 DC931 3022065WP BS 200 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 47134 STL - DURING OP-15, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK, STATION 200 TO 266. SPLICED IN NEW SEAT TRACK PER SRM 53-05, FIGURE 4. TOTAL CYCLES 73,957. 2L72 4F A6WE 19951013004961995101300496WP 1995 10 13 95ZZZM532 119950802A5313 LONGERON DOUG DC9 DC931 3022065WP BS 945-996 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05988Z 47134 STL - DURING OP-15, FOUND CORROSION ON LONGERON 29L, STATION 945 TO 996. REMOVED AND REPLACED LONGERON SECTION PER SRM 51-30-5, 51-30-2, AND TWA STANDARD PRACTICES. TOTAL CYCLES 73,957. 2L72 4F A6WE 19951013004971995101300497WP 1995 10 13 95ZZZM533 119950804A5744 FITTING DOUG DC9 DC932 3022066WP RT WING CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05997Z 47029 MCI - DURING OP-15, FOUND RIGHT WING RS AFT FLAP CENTER HINGE FITTING MOUNT AREA REAR SPAR WEB, CRACKED .75 INCH IN EYEBROW AT UPPER OUTBOARD HOLE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SERVICE BULLETIN 57-179 AND DRAWING J060272-502. TOTAL CYCLES 78,686. 2L72 4F A6WE 19951013004981995101300498WP 1995 10 13 95ZZZM534 119950816A2110 COUPLING DOUG DC8 DC862 3021970WP HEAT EXCH DUCT DISCONNECTED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19802BN 45909 WHILE CLIMBING THROUGH 26,000 FEET WITH 3 TURBO COMPRESSORS OPERATING, LOST CABIN PRESSURIZATION WITH ASSOCIATED LOUD NOISE. DESCENDED TO 10,000 FEET AND RETURNED TO MIAMI WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT AND RIGHT T/C HEAT EXCHANGER DUCT COUPLINGS DISCONNECTED. RECONNECTED DUCTS AND SYSTEM OPERATIONAL CHECKED NORMAL. PRESSURIZATION OK ON THE GROUND. 2L74 4F 4A25 19951013005001995101300500NM 1995 10 13 95ZZZM536 119950710A5315CAB1518347 FLOOR BEAM BOEING727 727227 1384078NM BS 1130 CORRODED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15924TS 21041 DURING C-CHECK INSPECTION, DISCOVERED THE STATION 1130 FLOOR BEAM AT RBL 24.75 TO RBL 45.5 TO BE CORRODED. REMAINING THICKNESS AFTER BLENDOUT WAS BEYOND SRM LIMITS. FABRICATED AND INSTALLED A REPAIR ANGLE UNDER THE BLENDED AREA WET WITH SEALANT. ACCOMPLISHED IAW EVERGREEN AIR CENTER - ENGINEERING CHANGE/REPAIR AUTHORIZATION NR NN924TS-53-001-EAC. 2L73 4F A3WE 19951013005011995101300501WP 1995 10 13 95ZZZM537 119950901A53132777922512000 LONGERON DOUG DC9 DC932 3022066WP FS 965 CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11901VJ 47275 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND CORROSION ON LONGERON 23L FS 965 WHICH IS BEYOND THE SRM LIMITS 53-01. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR MEMBER AND SPLICES IAW DC9-SRM 53-02 FIG 5. (M) 2L72 4F A6WE 19951013005021995101300502WP 1995 10 13 95ZZZM538 119950830A5320 FRAME DOUG DC9 DC932 3022066WP AFT CARGO DOOR CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11901VJ 47275 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND SEVERAL CORRODED SPOTS AROUND THE AFT CARGO DOOR LOWER FRAME. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED A NEW SECTION AND SPLICES IAW DC-9 SRM 53-30-2. NR 027N1-0064. 2L72 4F A6WE 19951013005031995101300503NM 1995 10 13 AWXA9500592 119950828A335020121 EEL BATT CHARGER BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, AFT SECTION OF EMERGENCY EXIT LIGHTS STAYED ON. REPLACED BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951013005041995101300504NM 1995 10 13 AWXA9500593 119950829A335058731 EEL LEAD STRIP BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 16 BACK. REMOVED AND REPLACED EMERGENCY LEAD STRIP AT ROW 16. OPS CHECK GOOD. (M) 2L72 4F A16WE 19951013005051995101300505NM 1995 10 13 AWXA9500595 119950831A3350 EEL STRIP BOEING737 737275 1384485NM CABIN WET A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT R2 DOOR AND IN THE AFT SECTION OF AIRCRAFT. FLOOR TRACK FOUND TO BE WET. DRIED TRACK AND REINSTALLED LIGHT STRIPS. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F A16WE 19951013005061995101300506NM 1995 10 13 AWXA9500596 119950831A33506104781 EEL POWER SUPPLY BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND THE FIRST SIX ROWS OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F A16WE 19951013005071995101300507NM 1995 10 13 AWXA9500597 119950904A3350 EEL ASSY BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28172AW 23631 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND SEVERAL FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE IN MID CABIN. RECONNECTED LIGHT ASSEMBLIES, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951013005081995101300508NM 1995 10 13 AWXA9500598 119950904A5330 SKIN BOEING737 7373S3 1384711NM BS 364 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28313AW 23712 PHX - DURING SCHEDULED C9 INSPECTION, FOUND LIGHTNING STRIKE DAMAGE TO SKIN THAT EXCEEDED SRM LIMITS AT STATION 364 STRINGER 6L. CLEANED AREA AND REPAIRED PER SRM 53-00-01, FIGURE 201. (M) 2L72 4F RTA16WE 19951013005091995101300509NM 1995 10 13 AWXA9500603 119950909A2612 FIRE LOOP BOEING757 757225 1384959NM NR 1 ENGINE MALFUNCTIONED A AWXAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 WP28913AW 22207 PHX - FLT NR 294 - ON CLIMB-OUT OF PHX, THE NR 1 ENGINE NR 2 LOOP OVERHEAT STATUS MESSAGE ILLUMINATED ON EICAS. PILOT SHUT DOWN ENGINE AND RETURNED TO PHX LANDING OVER WEIGHT BUT UNEVENTFUL. MAINTENANCE REPLACED TWO OVERHEAT LOGIC CIRCUIT CARDS. QC COMPLIED WITH OVERWEIGHT LANDING INSPECTION. AOG FOR NR 2 OVERHEAT DETECTION LOOP. NR 1 ENGINE OVERHEAT PLACED ON MEL 26-11-03. AIRCRAFT RETURNED TO SERVICE. NO FAULTS WERE FOUND ON FURTHER TROUBLE SHOOTING OF FIRE LOOP SYSTEM. MEL REMOVED. AIRCRAFT REMAINED IN SERVICE. (M) 2L72 4F RTA2NM 19951013005101995101300510NM 1995 10 13 AWXA9500618 119950911A5315 FLOOR BEAM BOEING737 7373S3 1384711NM BS 986 GOUGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - DURING SCHEDULED C9 INSPECTION, FOUND UPPER SURFACE OF CABIN FLOOR BEAM AT STATION 986 LBL 16 TO RBL 4 GOUGED OUT OF LIMITS. INSTALLED T-CAP REPAIR PER AWA ER 3-53-16-28. (M) 2L72 4F RTA16WE 19951013005111995101300511NM 1995 10 13 AWXA9500620 119950911A532065C807351 CHORD BOEING737 7373S3 1384711NM BS 947-996 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - DURING SCHEDULED C9 INSPECTION, FOUND R2 DOOR CHORD AT STATION 947 TO STATION 996 CORRODED BEYOND LIMITS IN SEVERAL AREAS. REPLACED CHORD PER SRM 51-40-02. (M) 2L72 4F RTA16WE 19951013005121995101300512NM 1995 10 13 AWXA9500621 119950911A5315 FLOOR BEAM BOEING737 7373S3 1384711NM BS 967 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - DURING SCHEDULED C9 INSPECTION, FOUND FLOOR BEAM UPPER SURFACE CORRODED BEYOND LIMITS AT FASTENER HOLES, STATION 957 LBL 29. INSTALLED ANGLE REPAIR PER SRM 53-30-51. (M) 2L72 4F RTA16WE 19951013005131995101300513 1995 10 13 AWXA9500623 419950823A22104030952906 YAW DAMPENER BOEING737 7373G7 1384595NM AUTO PILOT MALFUNCTIONED A AWXAO OTHER O OTHER APAPPROACH 1 WP28303AW 87072625 24010 PHX - FLT 864 - UNCOMMANDED RUDDER MOVEMENT, ON APPROACH 10 TO 15 DEGREES OF BANK WITH FLAPS AT 15, AIRCRAFT EXPERIENCED A HARD RIGHT YAW LASTING LESS THAN ONE SECOND. AIRCRAFT DID NOT ROLL. MAINTENANCE PERFORMED FLIGHT CONTROL CHECK, NO DEFECTS OR BINDING NOTED. SUBSEQUENT MAINTENANCE ACTIONS TAKEN, YAW DAMPENER COUPLER WAS REMOVED AND REPLACED AS A PRECAUTION. RUDDER PCU HILT CHECK PERFORMED WITH NO DEFECTS NOTED. (M) 2L72 4F RTA16WE 19951013005141995101300514NM 1995 10 13 AWXA9500624 119950911A272065C370527 RUDDER PCU BOEING737 7373G7 1384595NM RUDDER MALFUNCTIONED A AWXAO OTHER O OTHER TOTAKEOFF 1 WP28303AW 926A 24010 PHX - FLT 440 - UNCOMMANDED RUDDER MOVEMENT (SECOND OCCURRENCE), DURING TAKEOFF ROLL JUST PRIOR TO V1 (139 KTS), A SHARP MOMENTARY YAW LEFT OCCURRED. YAW DAMPENER WAS NOT TURNED ON. TAKEOFF CONTINUED, FLIGHT AND LANDING WERE UNEVENTFUL. AS A PRECAUTION, MAINTENANCE REPLACED RUDDER PCU. OPS CHECK PERFORMED PER AWA TASK CARD F6B27003. AUTOPILOT AND YAW DAMPENER SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951013005151995101300515NM 1995 10 13 AWXA9500625 119950911A3350900835A EEL BATT PACK BOEING737 7372A6 138448BNM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28145AW 20194 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F A16WE 19951013005161995101300516NM 1995 10 13 AWXA9500626 119950911A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 THROUGH ROW 19. REPAIRED WIRE CONNECTION AT ROW 14, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951013005171995101300517NM 1995 10 13 AWXA9500633 119950915A3350900835A EEL BATT PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SECTION EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IN AFT SECTION, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951013005181995101300518SW 1995 10 13 MALA954612 119950829A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 438.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 438.060 TO BE CRACKED AT THE MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW FAC ARP 53-20-9503. (M) 1L72 4T A8SW 19951013005191995101300519EU 1995 10 13 MALA954617 119950904A33501072621 EEL FOKKERF27 F27MK200 4990620EU CABIN INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15278MA 10280 DURING A WALKAROUND INSPECTION, MAINTENANCE PERSONNEL NOTED AN EMERGENCY EXIT LIGHT SIGN INOP. THE MECHANICS REPLACED THE EXIT IDENTIFIER LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T A817 19951013005201995101300520NM 1995 10 13 MALA954618 119950904A7931APT761000100DW OIL PRESS TRANSD DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE INTERNAL FAULT A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15848MA 346 FLT 3458 - DURING DEPARTURE IN DTW, THE CREW NOTED THE NR 1 OIL PRESSURE WAS AT 70 PSI. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 OIL PRESSURE TRANSDUCER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951013005211995101300521SW 1995 10 13 MALA954620 119950906A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 491 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, THE AFT CARGO FUSELAGE FRAME AT FS 491 WAS FOUND TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW FAIRCHILD ARP 53-20-9503. (M) 1L72 4T A8SW 19951013005221995101300522SW 1995 10 13 MALA954621 119950907A53112722086 FRAME SWRNGNSA227 SA227AC 8780603SW FS 159 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, THE LEFT LOWER BELT FRAME AT FS 159 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC LAR 95-MALA-237 AND SRM 51-00-00. (M) 1L72 4T A8SW 19951013005231995101300523NE 1995 10 13 RAIA950823 219950817A7261 ENGINE OIL AEROSPATR72 ATR72202 8680940EU PWA PW120 PW124B NE RIGHT LOW A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03722TE4131 220 124410R STL FLT NR 7019 - RIGHT ENGINE OIL PRESSURE INTERMITTENT. MAINTENANCE SERVICED RIGHT ENGINE WITH OIL. NO LEAKS NOTED. RIGHT ENGINE PLACED ON OIL CONSUMPTION WATCH. (M) 2H72 4T4 TRTA53EU E2ONE 19951013005241995101300524NM 1995 10 13 W8PA9501 119950815A7830106122628 TR PROX SWITCH BOEING737 737301 1384611NM NR 2 ENGINE OUT OF ADJUST A W8PAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM03301AU 23229 FLT 115 - COS-LAS - NR 2 THRUST REVERSER LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND S832 STOW PROXIMITY SWITCH OUT OF ADJUSTMENT. ADJUSTED PROXIMITY SWITCH PER MM 78-34-03. (M) 2L72 4F RTA16WE 19951013005251995101300525SO 1995 10 13 WTAA950252 119950825A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP17285UE 120153 ACV - LEFT LANDING GEAR INTRANSIT REMAINS ILLUMINATED AND GEAR DOORS REMAINED OPEN FOLLOWING GEAR RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LEFT LANDING GEAR ACTUATOR ROD END LOCK TAB BROKEN. ADJUSTED ACTUATOR AND INSTALLED NEW LOCK WASHER. LANDING GEAR RETRACTION CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951013005261995101300526EU 1995 10 13 VTZA95301 119950921A56101379377C405 WINDSHIELD BAG JETSTMJETSTM3201 1500217EU LEFT CRACKED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27495UE 818 FLT NR 6583 - SWF-BOS - DURING CRUISE DECLARED AN EMERGENCY AND RETURNED TO SWF, DUE TO THE CAPTAINS WINDSCREEN OUTER PANE CRACKING AT 9000 FEET. AIRCRAFT LANDED AT SWF WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE CAPTAINS WINDSCREEN. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951013005271995101300527CE 1995 10 13 95ZZZM540 119950712A78001299500003 EXHAUST STACK BEECH 1900 1900D 1154162CE LT ENG CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW01124YV1198 UE124 LEFT ENGINE INBOARD EXHAUST STACK CRACKED AT BLAST TUBE ATTACH WELD JOINT, PROGRESSING CIRCUMFERENTIALLY AROUND ATTACH WELD. 2L72 4T RTA24CE 19951013005281995101300528WP 1995 10 13 95ZZZM541 119950908A32302680262M6 4 WAY/3 POS VLV LKHEED1011 10113851 5265010WP LANDING GEAR INOP A RIAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19762BE 193P1070 DURING CLIMB, RIA FLT NR 1111 OUT OF SFO, MAIN GEAR DOORS WOULD NOT CLOSE WITH GEAR HANDLE IN UP POSITION, NOSE GEAR OPERATED NORMALLY. AIRCRAFT DUMPED FUEL AND RETURNED TO SFO. AT SFO, REPLACED 4 WAY 3 POSITION VALVE, PERFORMED OPERATIONAL TEST (DOOR SWING), OPS CHECK OK. 2L73 4F A23WE 19951013005291995101300529WP 1995 10 13 95ZZZM542 119950913A323139265281 CONTROL CABLE DOUG DC9 DC951 3022051WP NLG DOOR FAILED A TWAAO OTHER E VIBRATION/BUFFET CLCLIMB 1 CE05418EA 47676 STL - DURING CLIMB AFTER LANDING GEAR RETRACTION, HAD SEVERE VIBRATION FROM NOSE GEAR AREA. CYCLED LANDING GEAR AND VIBRATION CONTINUED. FOUND LEFT NOSE LANDING GEAR DOOR STOP CABLE, MFG P/N 3926528-1, TENSION LOW. RIGGED CABLE TENSION AND NOSE LANDING GEAR AND DOORS CHECKED NORMAL. 2L72 4F RTA6WE 19951013005301995101300530NM 1995 10 13 95ZZZM543 119950913A80127265747 START VALVE BOEING747 747131 1384881NM NR 1 ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE0593104 19670 STL - DURING CRUISE SHUT DOWN NR 1 ENGINE, S/N 4165, DUE TO START VALVE LIGHT ILLUMINATED. FOUND START VALVE PRESSURE SWITCH, MFG P/N 21SN41-1B, WITH INTERNAL MALFUNCTION. REPLACED START VALVE PRESSURE SWITCH AND START VALVE, MFG P/N 726574-7. ENGINE OPERATION AND LEAK CHECK NORMAL. 2L74 4F A20WE 19951013005311995101300531NE 1995 10 13 C2XA95CL113 219950828A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE LEFT FAILED A C2XAAE UNSCHED LANDING ENGINE SHUTDOWN BJMSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION OVER TEMP CLCLIMB 1 SW0934817136909104 152 120413 FLT 3808 - EWR-HYA - ON CLIMB-OUT, LEFT ENGINE MADE LOUD POP, TORQUE SURGED AND ITT ROSE OVER 800 DEGREE'S. POWER LOSS OCCURED AND SMOKE WARNINGS WERE GENERATED. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE IAW MM 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19951013005321995101300532SO 1995 10 13 C2XA95CL114 119950917A79211602824 OIL COOLER EMB 120 EMB120RT SO LT ENGINE CRACKED A C2XAA UNSCHED LANDING JKYWARNING INDICATION FLUID LOSS ENGINE STOPPAGE CLCLIMB 1 SW0915721 79310 120160 FLT NR 3285 - CLE-CLE - AFTER TAKEOFF NR 1 ENGINE OIL PRESSURE WENT OT 0 PSI. CONTINUED CLIMB-OUT BEFORE CREW COULD SHUT ENGINE DOWN, THE ENGINE SHUT ITSELF DOWN. RETURNED TO CLE. MAINTENANCE INSPECTED AND FOUND OIL COOLER TO BE CRACKED. REPLACED OIL COOLER AND LEFT ENGINE IAW EMB MM 79-21-01 AND MAINTENANCE DIRECTIVE NR 7 AND NR 8. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951013005331995101300533SO 1995 10 13 C2XA95IA240 119950920A532012015374002 ANGLE EMB 120 EMB120RT SO FIN TO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FIN TO FUSELAGE ATTACH ANGLE CRACKED 16 INCHES FROM FORWARD END. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005341995101300534SO 1995 10 13 C2XA95IA241 119950920A572012017057007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL CYCLES 16,023. (M) 2L72 4T RTA31SO 19951013005351995101300535SO 1995 10 13 C2XA95IA242 119950920A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005361995101300536SO 1995 10 13 C2XA95IA243 119950920A572012017056021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005371995101300537SO 1995 10 13 C2XA95IA244 119950920A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005381995101300538SO 1995 10 13 C2XA95IA245 119950920A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005391995101300539SO 1995 10 13 C2XA95IA246 119950920A572012017057006 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005401995101300540SO 1995 10 13 C2XA95IA247 119950920A572012017056005 SUPPORT EMB 120 EMB120RT SO LEFT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005411995101300541SO 1995 10 13 C2XA95IA248 119950920A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2, AND NR 3 SKIN SUPPORTS WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005421995101300542SO 1995 10 13 C2XA95IA249 119950920A572012017057005 SUPPORT EMB 120 EMB120RT SO LEFT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0951726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005431995101300543SO 1995 10 13 C2XA95IA250 119950920A572012017056015 SUPPORT EMB 120 EMB120RT SO RIGHT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005441995101300544SO 1995 10 13 C2XA95IA251 119950920A572012017060007 SUPPORT EMB 120 EMB120RT SO RIGHT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951013005451995101300545WP 1995 10 13 HALA95122 119950914A3350 EEL BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13669HA 47654 HNL - FLT 551 - AFTER INTERIOR OVERWING EXIT EMERGENCY LIGHTS ARE INOP, BOTH SIDES. REPLACED BATTERIES FOR AFT EMERGENCY LIGHTS. OPERATIONS CHECK GOOD. (M) 2L72 4F A6WE 19951013005461995101300546WP 1995 10 13 HALA95123 119950915A2780 BOLT DOUG DC9 DC951 3022051WP LT LE SLAT SHEARED A HALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP13699HA 47763 HNL - FLT 138 - SLATS DO NOT EXTEND EVENLY. AIRCRAFT ROLLED RIGHT (CONTROLLABLE) ON INITIAL SLAT EXTENTION. ON THE GROUND LEFT SLAT REMAINED EXTENDED ON SHUT DOWN. FOUND SHEARED BOLT ON INBOARD SLAT ACTUATOR ROD END BOLT (LEFT WING SLATS). REMOVED AND REPLACED ROD END BOLT. SLAT OPERATIONAL CHECK GOOD PER MM 27-80-5. (M) 2L72 4F A6WE 19951013005471995101300547NM 1995 10 13 IXKA9500027 119950824A3610655880914 DUCT BOEING727 727225 1384077NM NR 3 ENG BLEED CRACKED A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25354PA 20624 ATL-TPA - FLT 25 - AFTER TAKEOFF NR 3 ENGINE STRUT OVERHEAT LIGHT ON, LIGHT GOES OFF AT IDLE, COMES BACK AFTER POWER RESTORED, ATB TO ATL. FOUND DUCT FLANGE ON DUCT ASSY FROM NR 3 ENGINE BLEED S/O VALVE CRACKED. REMOVED AND REPLACED DUCT ASSY AS PER MM 36-00-1. OPS AND LEAK CHECK OK ON ENG RUNUP. (M) 2L73 4F A3WE 19951013005481995101300548EU 1995 10 13 SIMA952581 119950915A33506013211 EEL BATT PACK SAAB SF340 SF340A 7850100EU RT FORWARD DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW2195MQ 4643 1202 19105 340A095 SGF - FLT 3512 - RIGHT FORWARD EMERGENCY LIGHTS FOUND TO BE INOPERATIVE ON PRE-FLIGHT INSPECTION. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4T RTA52EU 19951013005491995101300549EU 1995 10 13 SIMA952591 119950916A2710S2711201200300 IDLER ARM AEROSPATR72 ATR72212 EU LT AILERON LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21407AT 407 DFW - DURING COMPLIANCE OF EO E9-2700-001 (REPETITIVE INSPECTION AILERON CONTROL SYSTEM) AD 93-22-10, MAINTENANCE FOUND THE NR 2 IDLER ARM IN THE LEFT WING WITH A LOOSE BEARING. IDLER ARM WAS REMOVED AND REPAIRED IAW SRM 51-25-20. IDLER ARM WAS REINSTALLED AND OPS CHECK SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951013005501995101300550WP 1995 10 13 USAA950864 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 221 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND DENT IN SKIN 1.25 INCH BY 1.25 INCH BY .108 DEEP AT STATION 221 BETWEEN LONGERON 15L AND 16L. CUT OUT DAMAGE AND INSTALLED CLASS 1 REPAIR DOUBLER PER SRM 53-04 FIG 38 SHEET NR 21 VIEW 1. (M) 2L72 4F A6WE 19951013005511995101300551WP 1995 10 13 USAA950865 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK .125 INCH LONG IN SKIN AT STATION 1437 LONGERON 2L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER US AIR EA NR 30625. (M) 2L72 4F A6WE 19951013005521995101300552WP 1995 10 13 USAA950866 119950707A5320 CLIP DOUG DC9 DC981 3022081WP BS 1307 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH LONG CRACK STATION 1307 SKIN CLIP LONGERON 16L. SPLICED IN NEW SECTION OF SKIN CLIP PER SRM 53-03. (M) 2L72 4F A6WE 19951013005531995101300553WP 1995 10 13 USAA950867 119950707A5320 CLIP DOUG DC9 DC981 3022081WP BS 1307 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND ONE .5 INCH LONG CRACK IN SKIN CLIP STATION 1307 LONGERON 16R. SPLICED IN NEW SKIN CLIP PER SRM 53-03. (M) 2L72 4F A6WE 19951013005541995101300554WP 1995 10 13 USAA950871 119950707A5320 FITTING DOUG DC9 DC981 3022081WP BS 940 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH AND 1.5 INCH CRACK IN LEFT AND RIGHT SADDLE SUPPORT FITTING FORWARD END OF KEEL STRUCTURE, STATION 940. FABRICATED AND INSTALLED KEEL SADDLE SUPPORT FITTING PER SRM 53-05 FIG 81. (M) 2L72 4F A6WE 19951013005551995101300555WP 1995 10 13 USAA950872 119950707A5312 BULKHEAD DOUG DC9 DC981 3022081WP BS 1380 HOLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND .5 INCH DIAMETER HOLE AT STATION 1380 LONGERON 6L IN TAIL INTERIOR BULKHEAD. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 3. (M) 2L72 4F A6WE 19951013005561995101300556WP 1995 10 13 USAA950873 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 1309-1322 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE .014 INCH DEEP AT STATION 1309-1322 ABOVE LONGERON 20R. BLENDED GOUGE TO .016 INCH AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 VIEW G. (M) 2L72 4F A6WE 19951013005571995101300557 1995 10 13 USAA950929 419950908A34546223255009 NAV RECEIVER DOUG DC9 DC931 3022065WP NR 2 INOP A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19972VJ 47052 IND - FLT NR 673 - DIVERTED TO IND DUE TO LOSS OF THE NR 2 VOR. MAINTENANCE REPLACED THE NR 2 NAV RECEIVER. VOR GROUND CHECKED GOOD. (M) 2L72 4F A6WE 19951013005581995101300558EU 1995 10 13 VTZA95293 119950915A2721MS141024K BEARING JETAIRJETSTMJETSTM4101 1500501EU RUDDER TRIM TAB WORN A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA27312UE 41025 FLT NR 6170 - IAD-EWR - DURING CRUISE, RETURNED TO IAD DUE TO VIBRATION BEING EXPERIENCED FROM THE RUDDER. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RUDDER TRIM TAB BEARINGS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951013005591995101300559 1995 10 13 VTZA95294 419950915A3418C771075 TRANSDUCER BAG JETSTMJETSTM3201 1500217EU WING FAILURE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27475UE 850 FLT NR 6363 - LYH-IAD - ABORTED THE TAKEOFF DUE TO THE STALL WARNING ACTIVATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE STALL VANE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951013005601995101300560 1995 10 13 VTZA95295 419950917A23507207SH32QE PTT SWITCH BAG JETSTMJETSTM3201 1500217EU COCKPIT BROKEN A VTZAA UNSCHED LANDING O OTHER TOTAKEOFF 1 EA27474UE 849 FLT NR 6241 - IAD-PHF - DURING TAKEOFF, RETURNED TO IAD DUE TO THE COMM NR 2 RADIO WOULD NOT STOP TRANSMITTING FROM THE FIRST OFFICERS SWITCH. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED BOTH PUSH TO TALK SWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951013005611995101300561EU 1995 10 13 VTZA95296 119950917A2431 CONNECTOR BAG JETSTMJETSTM3201 1500217EU BATT TEMP LOOSE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27370MT 800 FLT NR 6284 - IAD-HPN - ABORTED TAKEOFF DUE TO BOTH BATTERY OVERTEMP LIGHTS ILLUMINATING DURING THE TAKEOFF ROLL, WITH BOTH TEMPS READING NORMAL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE RESECURED THE CONNECTOR ON THE BATT TEMP MONITOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951013005621995101300562EU 1995 10 13 VTZA95297 119950915A2910S1226142 PRESS SWITCH BAG JETSTMJETSTM3201 1500217EU LT HYD SYSTEM FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27483UE 898 FLT NR 6388 - IAD-PIT - DURING CRUISE, RETURNED TO IAD DUE TO THE LEFT HYDRAULIC PUMP FAILING. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951013005631995101300563EU 1995 10 13 VTZA95298 119950913A2611721112111000 SMOKE DET JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE POD DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27325UE 41063 FLT NR 6417 - CHS-IAD - ABORTED TAKEOFF DUE TO THE VENTRAL BAGGAGE BAY SMOKE DETECTOR WARNING DURING THE TAKEOFF ROLL. AN EMERGENCY WAS DECLARED AND THE FIRE DEPARTMENT DID INSPECT THE BAGGAGE BAY. NO DEFECTS WERE NOTED. AIRCRAFT THEN RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17732 IAW MEL 26-3. MAINTENANCE LATER CLEARED DMI NR 17732 ON 009-17-95, BY CLEANING THE SMOKE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951013005641995101300564WP 1995 10 13 VTZA95299 219950919A7314897780 PUMP ASSY BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILED A VTZAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27479UE 893 P66004 FLT NR 6286 - IAD-CMH - DURING TAXI FOR TAKEOFF, RETURNED TO GATE DUE TO THE LEFT ENGINE FLAMING OUT DURING TAXI WITH NO POWER OR CONDITION LEVER MOVEMENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE INVESTIGATED AND FOUND THE FUEL PUMP DRIVE GEAR SHEARED. MAINTENANCE CHANGED THE ENGINE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19951013005651995101300565EU 1995 10 13 VTZA95300 119950919A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27308UE 41023 FLT NR 6202 - MHT-IAD - ABORTED THE TAKEOFF DUE TO THE MAIN BAGGAGE BAY DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 02555 IAW MEL 52-3. MAINTENANCE LATER CLEARED DMI NR 02555 ON 09-19-95 BY ADJUSTING THE BAGGAGE DOOR MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951013005661995101300566EU 1995 10 13 USAA950806 119950626A5541 RIB FOKKERF28 F28MK4000 4990810EU RUDDER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND A 3.5 INCH CRACK IN THE RUDDER RIB NR 4 VERTICAL CHANNEL. INSTALLED DOUBLER REPAIR PER SRM 55-02-07 FIG 3. (M) 2L72 4F RTA20EU 19951013005671995101300567EU 1995 10 13 USAA950807 119950626A5320 FRAME FOKKERF28 F28MK4000 4990810EU PAX DOOR GOUGE A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND A .034 INCH DEEP BY 1.5 INCH LONG GOUGE IN MAIN ENTRANCE DOOR APERTURE FRAME JUST FORWARD OF INTERMEDIATE LEVER. INSTALLED DOUBLER REPAIR PER SRM 53-02-16 FIG 1. (M) 2L72 4F RTA20EU 19951013005681995101300568EU 1995 10 13 USAA950808 119950626A5330 SKIN FOKKERF28 F28MK4000 4990810EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND SKIN BUCKLED AND CRACKED JUST FORWARD OF APU EXHAUST. INSTALLED DOUBLER REPAIR PER SRM 53-02-04 FIG 1. (M) 2L72 4F RTA20EU 19951013005691995101300569EU 1995 10 13 USAA950809 119950628A5320 FRAME FOKKERF28 F28MK4000 4990810EU CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN FORWARD CARGO AFT FRAME AT DOOR HOLD OPEN ROD SUPPORT. INSTALLED DOUBLER REPAIR PER SRM 53-02-16. (M) 2L72 4F RTA20EU 19951013005701995101300570WP 1995 10 13 USAA950813 119950630A5311 FRAME DOUG DC9 DC981 3022081WP BS 1463 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS ONE .0625 INCH AND ONE .1875 INCH IN FRAME STATION 1463 LEFT SIDE DORSAL FIN ATTACH ANGLE. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 23B. (M) 2L72 4F A6WE 19951013005711995101300571WP 1995 10 13 USAA950814 119950706A5320 JAMB DOUG DC9 DC981 3022081WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CORROSION IN MED STATION 200 BOTTOM LEFT AFT DOOR JAMB. CUT OUT CORRODED SECTION OF JAMB AND INSTALLED DOUBLER REPAIR PER USAIR EA 308 AND SRM 53-05 FIG 55. (M) 2L72 4F A6WE 19951013005721995101300572WP 1995 10 13 USAA950815 119950706A5320993058211 ANGLE DOUG DC9 DC981 3022081WP BS 985 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A 1 INCH CRACK IN TOP KEEL BEAM 'T' ANGLE ON HORIZONTAL LEG AT STATION 985. SPLICED IN NEW SECTION OF ANGLE AND DOUBLER PER USAIR EA 30834. (M) 2L72 4F A6WE 19951013005731995101300573WP 1995 10 13 USAA950816 119950706A5330 SKIN DOUG DC9 DC981 3022081WP BS 636 DAMAGED A USAAK NONE C F.O.D. ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A LIGHTNING STRIKE LEAVING A .020 INCH PIT AT FUSELAGE SKIN STATION 636 BETWEEN LONGERON 9R AND 10R. REMOVED DAMAGE AND INSTALLED FILLER AND INTERNAL DOUBLER REPAIR PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19951013005741995101300574WP 1995 10 13 USAA950817 119950706A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .125 INCH CRACK IN LONGERON 3L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951013005751995101300575WP 1995 10 13 USAA950818 119950706A5320 CUSP WEB DOUG DC9 DC981 3022081WP BS 825-845 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK IN STATION 825 TO 845 LONGERON 18R CUSP WEB. REPLACED SECTION OF CUSP WEB PER SRM 53-05 FIG 27. (M) 2L72 4F A6WE 19951013005761995101300576WP 1995 10 13 USAA950819 119950711A5320 CLIP DOUG DC9 DC981 3022081WP BS 1459 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SKIN CLIP STATION 1459 BETWEEN LONGERON 2R AND 3R. MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28. (M) 2L72 4F A6WE 19951013005771995101300577WP 1995 10 13 USAA950820 119950711A5320 CLIP DOUG DC9 DC981 3022081WP BS 1459 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK AT SKIN CLIP .375 INCH LONG AT STATION 1459 BETWEEN LONGERON 2L AND 3L. MFG NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 28. (M) 2L72 4F A6WE 19951013005781995101300578WP 1995 10 13 USAA950821 119950710A5347 SEAT TRACK DOUG DC9 DC981 3022081WP FS 205 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT RIGHT INBOARD SEAT TRACK AT BOTTOM INBOARD FLOOR ATTACH ANGLE AT STATION FS-205 (PREVIOUSLY REWORKED) CORROSION TASK REF C46-53305. REMOVED CORROSION AND SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (M) 2L72 4F A6WE 19951013005791995101300579WP 1995 10 13 USAA950822 119950706A5730 SKIN DOUG DC9 DC981 3022081WP WING LE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK IN TEMPORARY REPAIR ON WING LE AT INBOARD AND OUTBOARD EDGE OF FUEL SERVICE PANEL IN SKIN. REMOVED TEMP REPAIR AND STOP DRILLED CRACKS. INSTALLED DOUBLER REPAIR PER SRM 57-06B. (M) 2L72 4F A6WE 19951013005801995101300580WP 1995 10 13 USAA950823 119950706A5320 ANGLE DOUG DC9 DC981 3022081WP BS 37 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SUPPORT ANGLE LEFT OF CENTER UNDER RADAR SUPPORT SHELF STATION 37 BULKHEAD HORIZONTAL ANGLE. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M) 2L72 4F A6WE 19951013005811995101300581WP 1995 10 13 USAA950824 119950706A53201097172 FITTING DOUG DC9 DC981 3022081WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 3 INCH BY 4 INCH AREA OF CORROSION (LEVEL 1) AT FITTING AT AFT LOWER CORNER OF AIR STAIR DOOR STATION 200 LONGERON 21L (PREVIOUSLY REWORKED). CORROSION TASK NR REF C45-53301. INSTALLED NEW FITTING P/N 109-7172. (M) 2L72 4F A6WE 19951013005821995101300582WP 1995 10 13 USAA950825 119950711A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 1287 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED IN 2 PLACES BOTH 1 INCH LONG AT STATION 1287 LEFT. MFG NEW CUSP MEMBRANE PER SRM 53-05 FIG 79. (M) 2L72 4F A6WE 19951013005831995101300583WP 1995 10 13 USAA950826 119950711A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 1250 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CUSP MEMBRANE CRACKED 1 INCH LONG STATION 1250 RIGHT SIDE. MFG CUSP MEMBRANE PER SRM 53-05 FIG 79. (M) 2L72 4F A6WE 19951013005841995101300584WP 1995 10 13 USAA950827 119950711A5320993636811 INTERCOSTAL DOUG DC9 DC981 3022081WP BS 988 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .375 INCH CRACK IN FITTING AT STATION 988 INSIDE HEEL ABOVE AFT END OF DOOR HINGE. INSTALLED DOUBLER REPAIR PER SRM 53-01. (M) 2L72 4F A6WE 19951013005851995101300585WP 1995 10 13 USAA950828 119950711A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND CRACK .25 INCH LONG AT BOTH ATTACH POINTS STATION 160 LONG 4L. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951013005861995101300586WP 1995 10 13 USAA950829 119950711A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK AT LONGERON ATTACH POINTS TO FRAME STATION 160 LONG 3L. ACCOMPLISHED SPLICE TYPE REPAIR PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951013005871995101300587WP 1995 10 13 USAA950830 119950712A5311 BELT FRAME DOUG DC9 DC981 3022081WP BS 1322 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND 2 CRACKS .25 INCH LONG IN BELTFRAME AT STATION 1322 AT LONGERON 17R. REPLACED SECTION OF FRAME AND INSTALLED DOUBLERS PER SRM 53-03 FIG 31. (M) 2L72 4F A6WE 19951013005881995101300588WP 1995 10 13 USAA950831 119950630A5510 LE WEB DOUG DC9 DC981 3022081WP HORIZ STAB CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND A .25 INCH CRACK RIGHT INBOARD WEB LEADING EDGE TO HORIZONTAL STABILIZER FROM SPAR. INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 5. (M) 2L72 4F A6WE 19951013005891995101300589WP 1995 10 13 USAA950832 119950630A5320 WINDOW PAN DOUG DC9 DC981 3022081WP BS 948 LT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 948 LEFT SIDE WINDOW PAN. INSTALLED DOUBLER TYPE REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M) 2L72 4F A6WE 19951013005901995101300590WP 1995 10 13 USAA950833 119950630A5320 WINDOW PAN DOUG DC9 DC981 3022081WP BS 929 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 929 LEFT SIDE WINDOW PAN. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M) 2L72 4F A6WE 19951013005911995101300591WP 1995 10 13 USAA950834 119950630A5320 WINDOW PAN DOUG DC9 DC981 3022081WP BS 8888 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 888 LEFT WINDOW PAN. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-50-06. (M) 2L72 4F A6WE 19951013005921995101300592WP 1995 10 13 USAA950835 119950711A5311 FRAME DOUG DC9 DC981 3022081WP BS 1287 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19808US37813 48040 PIT - DURING Q-4/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON BELTFRAME 1287 BETWEEN LONGERON 22L AND 23L (CORROSION TASK RED C57-53301). ACCOMPLISHED REPAIR TO BELTFRAME PER SRM 53-03 FIG 30. (M) 2L72 4F A6WE 19951013005931995101300593WP 1995 10 13 USAA950836 119950707A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 1322 RIGHT LAV FLOOR BEAM. CORROSION TASK NR C58-53308. CUT OUT CORRODED AREA AND INSTALLED FILLER, ANGLE AND DOUBLERS PER USAIR TYPICAL REPAIR 53-10-19. (M) 2L72 4F A6WE 19951013005941995101300594WP 1995 10 13 USAA950837 119950707A5315991556171 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 1338 RIGHT LAV FLOOR BEAM CORROSION TASK NR C58-53300. SPLICED IN NEW SECTION OF FLOOR BEAM PER USAIR TYPICAL REPAIR 53-10-14. (M) 2L72 4F A6WE 19951013005951995101300595WP 1995 10 13 USAA950855 119950707A5320 ANGLE DOUG DC9 DC981 3022081WP BS 180 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 4 INCH BY 2 INCH AREA OF CORROSION PREVIOUSLY REWORKED UPPER CUSP ANGLE AT APPROX STATION 180. REMOVED DAMAGED AREA FABRICATED NEW CUSP, INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 55 AND USAIR EA 30801. (M) 2L72 4F A6WE 19951013005961995101300596WP 1995 10 13 USAA950856 119950707A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1495 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 2 INCH CRACK RIGHT SIDE OF VERTICAL FIN DRAG ANGLE AT STATION 1495. CUT OUT DAMAGED AREAS AND INSTALLED A SPLICE REPAIR PER SRM 53-05 FIG 23A. (M) 2L72 4F A6WE 19951013005971995101300597WP 1995 10 13 USAA950857 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 522 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND CRACK .75 INCHES LONG AND CREASE .055 DEEP AT STATION 522 BETWEEN LONGERON 21R AND 22R FUSELAGE SKIN. CUT OUT DAMAGED AREA AND INSTALLED EXTERIOR DOUBLER AND INTERIOR FINGER DOUBLER PER SRM 53-04 FIG 12B. (M) 2L72 4F A6WE 19951013005981995101300598WP 1995 10 13 USAA950858 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 755 GOUGE A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CD-6 CHECK INSPECTION, FOUND GOUGE .015 BY 1.75 INCHES LONG AT STATION 755 LONGERON 15R. BLENDED GOUGE, DYE CHECKED AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW E. (M) 2L72 4F A6WE 19951013005991995101300599WP 1995 10 13 USAA950859 119950707A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1282-1300 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1282 TO 1300 LONGERON 30. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14. (M) 2L72 4F A6WE 19951013006001995101300600WP 1995 10 13 USAA950860 119950707A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1300-1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1300 TO 1338 LONGERON 29L. INSTALLED LONGERON SPLICE REPAIR PER SRM 53-02 FIG 14. (M) 2L72 4F A6WE 19951013006011995101300601WP 1995 10 13 USAA950861 119950707A53305910369 SKIN DOUG DC9 DC981 3022081WP APU SHROUD PUNCTURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND PUNCTURE IN APU SHROUD ENCLOSURE SKIN. MFG AND INSTALLED REPAIR DOUBLER PER SRM 53-01 PG 2. (M) 2L72 4F A6WE 19951013006021995101300602WP 1995 10 13 USAA950862 119950707A5313 LONGERON DOUG DC9 DC981 3022081WP BS 237/256 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND TWO .75 INCH LONGERON CRACKS AT STATION 237 AND 256 LONGERON 17L. INSTALLED SPLICE REPAIR PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951013006031995101300603WP 1995 10 13 USAA950863 119950707A5320 CLIP DOUG DC9 DC981 3022081WP BS 1307 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT -DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1.5 INCH CRACK IN SKIN CLIP STATION 1307 LONGERON 16R. MANUFACTURED SKIN SLIP AND INSTALLED PER SRM 51-01. (M) 2L72 4F A6WE 19951013006041995101300604EU 1995 10 13 USAA950942 119950901A5320 WEB FOKKERF28 F28MK4000 4990810EU BS 2220-3040 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19486US19907 11237 PIT - DURING SCHEDULED STRUCTURAL VISIT (SIP), FOUND A 1.5 INCH CRACK IN WEB BETWEEN STATION 2220 AND 3050 AT BEND LINE ABOVE CONNECTION ANGLES. (VISUAL INSPECTION VERIFIED BY HFEC) SIP REF 53-10-19. INSTALLED DOUBLER REPAIR PER SRM 53-02-18 PG 29. (M) 2L72 4F RTA20EU 19951013006051995101300605NM 1995 10 13 USAA950977 119950911A5330 SKIN BOEING737 737301 1384611NM BS 1040-1064 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19578US32305 23257 ROA - DURING 'FULL C' CHECK VISUAL INSPECTION, FOUND 6 INCH BY 3 INCH DENT BETWEEN STATION 1040 AND STATION 1064 LOWER RIGHT AFT FUSELAGE. INSTALLED DOUBLER, REPAIR DOCUMENT SRM 53-00-01 PAGE 204. (M) 2L72 4F RTA16WE 19951019000011995101900001 1995 10 19 TWRA9515 419950308A2564 LOWER TUBE BOEING747 747259B NM LIFE RAFT FAILED A TWRAK NONE O OTHER ININSP/MAINT 1 EA152FOR 21730 DURING A DITCHING DRILL EXERCISE, AT THE LONG BEACH RECREATION CENTER, THE 25 MAN LIFE RAFT (P/N 14D23041) USED DURING THE DRILL, FAILED TO DEPLOY PROPERLY. THE LOWER BUOYANCY TUBE FAILED TO INFLATE FULLY. THIS TYPE LIFE RAFT IS NOT INSTALLED ON ANY TOWER AIRCRAFT. (W) 2L74 4F RTA20WE 19951019000021995101900002NM 1995 10 19 TWRA9519 119950308A3350 EEL CONNECTOR BOEING747 747259B NM CABIN LOOSE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND MAIN CABIN INTERVAL LIGHT EXIT LIGHT AT L-5 DOOR INOPERATIVE. FOUND CONNECTOR LOOSE IN LIGHT ASSEMBLY. SECURED CONNECTOR, OPS CHECK OK. (W) 2L74 4F RTA20WE 19951019000031995101900003NM 1995 10 19 TWRA9520 119950308A335086210144 EEL BATTERY PACK BOEING747 747259B NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND MAIN CABIN INTERVAL EMERGENCY EXIT LIGHT AT L-1 MAIN ENTRY DOOR (SYSTEM INDICATOR LED) INOPERATIVE. DURING TROUBLESHOOTING, FOUND THE BATTERY PACK AT FAULT. REMOVED AND REPLACED THE BATTERY PACK, OPS CHECK OK. (W) 2L74 4F RTA20WE 19951019000041995101900004NM 1995 10 19 TWRA9521 119950308A335086210144 EEL BATTERY PACK BOEING747 747259B NM CABIN DISCHARGED A TWRAK NONE L NO TEST ININSP/MAINT 1 EA152FOR 21730 DURING DAILY SERVICE, FOUND MAIN CABIN INTERVAL EMERGENCY EXIT LIGHT AT L-3 MAIN ENTRY DOOR INOPERATIVE. DURING TROUBLESHOOTING, FOUND THE BATTERY PACK AT FAULT. REMOVED AND REPLACED THE BATTERY PACK, OPS CHECK OK. (W) 2L74 4F RTA20WE 19951019000061995101900006WP 1995 10 19 DLL10952643 119950602A5744 SWING LINK LKHEED1011 10113851 5265010WP NR 1 LE FLAP LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11721DA 193C1139 RT WING NR 1 FLAP I/B SWING LINK ATTACH POINT LOOSE. DISASSEMBLED AND FOUND FLAP FITTING BUSHING OUT OF LIMITS, BORED FITTING TO 1.319, MANUFACTURED BUSHING PER SRM 57-54-00. 2L73 4F A23WE 19951019000071995101900007NM 1995 10 19 95UAL900010 119950619A2760KBNE183 ROD END WESTON 346204 BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 6 SPOILER FAILED A UALAK NONE F FLT CONT AFFECTED LDLANDING 1 WP29153UA 463783 20102 THE NR 6 GROUND SPOILER POWER CONTROL PACKAGE ACTUATOR ROD END, SEPARATED FROM THE ACTUATOR UPON LANDING. DAMAGED SPOILER PANEL, SPOILER ACTUATOR SUPPORT FITTING, AND SURROUNDING STRUCTURE. THE ROD END/PISTON ROD THREADS FAILED AS A RESULT OF CORROSION. 2L74 4F4 F A20WE E20EA 19951019000081995101900008NM 1995 10 19 UPS203659 119950621A571265C215248 RIB BOEING727 72751C 1384015NM WS 70.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01902UP 18898 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT 70.5 RIB CHORD HAS CRACK. REPAIRED IAW B727-5710-7142-A. 2L73 4F A3WE 19951020000011995102000001WP 1995 10 20 9515299940 119951010A3260 WARNING LIGHT DOUG DC9 DC932 3022066WP LANDING GEAR ILLUMINATED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01322L 47031 ON APPROACH, THE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. A GO-AROUND WAS ACCOMPLISHED, RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED GEAR DOOR SWITCHES FOR SECURITY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020000021995102000002WP 1995 10 20 9515309607 119951010A3260 CONNECTOR DOUG DC9 DC932 3022066WP GEAR DOOR SWITCHLOOSE A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01607NW 47232 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. RESECURED CANNON PLUG ON LANDING GEAR DOOR INDICATOR SWITCH AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020000031995102000003WP 1995 10 20 9515319607 119951011A3260 SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01607NW 47232 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR DOOR SWITCH AND OPERATIONAL TEST GOOD. 2L72 4F A6WE 19951020000041995102000004WP 1995 10 20 9515329995 119951012A3231 BYPASS VALVE DOUG DC9 DC931 3022065WP LDG GEAR DOOR EXTENDED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018933E 47327 DURING CLIMB, LANDING GEAR DID NOT INDICATE UP AND LOCKED. RETURNED TO PHL AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND MAINTENANCE BYPASS VALVE DOOR EXTENDED. RESECURED DOOR AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020000051995102000005WP 1995 10 20 9515339156 119951011A213092274473 RELAY DOUG DC9 DC914 3022034WP OUTFLOW VALVE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018915E 45832 AFTER TAKEOFF, AUTO PRESSURIZATION SYSTEM FAILED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RELAY R2-55 AND OUTFLOW VALVE LINKAGE. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951020000061995102000006WP 1995 10 20 9515349101 119951012A2120 AIR DISTR DOUG DC9 DC915 3022036WP CABIN SMOKING A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL0191S 47063 GROUND BLOWER ON RIGHT PACK FAILED AFTER STARTING BOTH ENGINES. ELECTRICAL SMOKE AND ODOR IMMEDIATELY BEGAN FILLING COCKPIT AND CABIN. SHUTDOWN ENGINES AND PASSENGERS WERE PROMPTLY DEPLANED. CHECKED PACK FAN ROTORS AND WIRING, OPERATED BOTH PACKS WITH APU AIR AND ENGINE BLEEDS. ALL SYSTEMS CHECKED NORMAL, DISCREPANCY COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951020000071995102000007WP 1995 10 20 9515359758 119951011A2780 T-DUCTS DOUG DC9 DC941 302207NWP LE SLATS LACK OF LUBE A NWAAO OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 GL01758NW 47286 MEM - DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED ON SLAT EXTENSION. A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. LUBED SLAT T-DUCTS, CYCLED SLATS SEVERAL TIMES. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951020000081995102000008NM 1995 10 20 9515362275 119951010A3241423071 ANTI-SKID CNTRL BOEING727 727251 138408HNM E/E COMPT FAILED A NWAAO OTHER O OTHER LDLANDING 1 GL01275US4832 3696 21154 AFTER LANDING ROLLOUT, ANTI-SKID WAS PULSING CAUSING BRAKES TO RELEASE DURING RUNWAY TURN OFF. CREW ABORTED TURN OFF. MAINTENANCE REPLACED ANTI-SKID CONTROL BOX AND OPERATIONAL CHECK NORMAL. 2L73 4F A3WE 19951020000091995102000009NE 1995 10 20 95UAL900195 219951012A7230 COMPRESSOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE STALLED A UALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29576UA 26690 726693 ON CLIMBOUT, LEFT ENGINE HAD COMPRESSOR STALL WITH RISING EGT, MAX REACHED 657C. POWER REDUCED TO IDLE EGT STABLIZED AT 550C, LANDED OVERWEIGHT. 2L72 4F4 FRTA2NM E17NE 19951020000101995102000010NM 1995 10 20 95UAL900196 119951012A3350 EEL STRIP BOEING737 737291 138448WNM PWA JT8 JT8D9A 52048NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29979UA 21544 EEL LIGHT INOPERATIVE AT ROW 12 LT. REPLACED EEL STRIP. 2L72 4F4 F A16WE E2EA 19951020000111995102000011NM 1995 10 20 95UAL900197 119951012A3350 EEL SWITCH BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE COCKPIT FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29930UA 26655 EEL LIGHT SWITCH ON OVERHEAD PANEL IN FLIGHT DECK WILL NOT LIGHT EEL LIGHT, WHEN TURNED ON. REPLACED SWITCH IN FLIGHT DECK. 2L72 4F4 FRTA16WE E2GL 19951020000121995102000012NM 1995 10 20 95UAL900198 119951012A5610 WINDOW BOEING737 737291 138448WNM COCKPIT SHATTERED A UALAK NONE O OTHER ININSP/MAINT 1 WP29982UA 21640 WINDOW 2R SHATTERED WHEN WINDOW HEAT TURNED ON. REPLACED WINDOW, WINDOW WIRING AND WINDOW HEAT CONTROL UNIT AS PRECAUTIONARY. SYSTEM CHECKED OK. 2L72 4F A16WE 19951020000131995102000013NM 1995 10 20 95UAL900199 119951012A7603448774 THROTTLE CRANK BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE NR 2 ENGINE LOOSE A UALAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 WP29990UA 21980 702602 CREW REPORTS NR 2 ENGINE WILL NOT REDUCE FROM CRUISE POWER SETTING WITH THROTTLE AT IDLE. ENGINE SHUTDOWN FOR LANDING AT SLC DUE TO NO RESPONSE FROM THROTTLE. FOUND THROTTLE CRANK ARM NUT AT CROSS SHAFT BACKED OFF. REINSTALLED THROTTLE CRANK ARM TO CROSS SHAFT, TORQUED AND SAFETIED. JOB CARDS ARE BEING REVISED TO CHECK THIS NUT. 2L72 4F4 F A16WE E2EA 19951020000141995102000014NM 1995 10 20 DL72E953975 119951002A5530 STRINGER BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 STRINGER CRACKED VERT STAB INTERIOR STR 8R CRACKED, LOCATED IN 3RD BAY UP FROM ACCESS HOLE. WORKED AT HMV, REPAIRED PER M/M 55-30-00. 2L73 4F A3WE 19951020000151995102000015NM 1995 10 20 DL72E953976 119951005A5754 ANGLE BOEING727 727247 138408FNM NR 1 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 NR 1 L/E FLAP ACTUATOR ATTACH ANGLE CRACKED I/B SIDE. WORKED AT HMV, REPAIRED ANGLE PER M/M 57-20-21. 2L73 4F A3WE 19951020000161995102000016NM 1995 10 20 DL72E953977 119951010A5754 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, NR 4 SLAT RIB NR 18 CRACKED. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19951020000171995102000017NM 1995 10 20 DL72S953978 119951011A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 FOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 7 SLAT. FASTENERS LOOSE OUTBD SLAT TRACK FAIRING NR 7 SLAT. REPAIRED PER M/M 57-54-0 2. REPLACED FASTENER. 2L73 4F A3WE 19951020000181995102000018NM 1995 10 20 DL72S953979 119951011A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 FOUND ON CV2 CHECK, COVE SKIN SUPPORT ANGLE CRACKED AT INBD STOP PAD NR 6 SLAT. REPAIRED PER M/M 57-54-0 FIG 816. 2L73 4F A3WE 19951020000191995102000019WP 1995 10 20 DLL10953966 119951011A71101646118103 COWL LKHEED1011 10113851 5265010WP NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11720DA 193C1136 NR 2 ENGINE LOWER LT HINGED COWL, 6 INCH CRACK IN LOWER EDGE OF COWL, AFT OF 2ND LATCH FROM FORWARD EDGE. REPAIRED PER SRM 51-50-02 PAGE 3. 2L73 4F A23WE 19951020000201995102000020WP 1995 10 20 DLL13953963 119951011A3350RPS1 EEL POWER SUPPLY LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11790DL 193A1143 EMERGENCY LIGHT FLOOR TRACK IN D-ZONE IS INOP. REPLACED POWER SUPPLY, CKS GOOD. 2L73 4F A23WE 19951020000211995102000021WP 1995 10 20 DLL13953964 119951011A33500L3071BPEGPL EEL LAMP LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11790DL 193A1143 EMERGENCY FLOOR TRACK LIGHT AT SEAT 5D IS INOP. RELAMPED LIGHT. 2L73 4F A23WE 19951020000221995102000022NM 1995 10 20 DLM88953962 119951011A5320 ANGLE DOUG MD88 MD88 3023688NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11978DL 53259 FOUND DURING E-1 LETTER CHECK, 1.5 INCH CRACK IN STRIKER ANGLE AFT O/B SIDE OF RT WHEEL WELL. REPAIRED PER SRM 53-05. 2L72 4F RTA6WE 19951020000231995102000023EU 1995 10 20 WWMA9500065 119950927A215012502704041 BLOWER ASSY BAG JETSTMJETSTM3201 1500217EU FREON AC SYST FAILED A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15949AE 949 FLT 3313 - PILOT REPORTED, THE FREON AIR CONDITIONER FAN EMANATED A BURNING ODOR. COOL AIR CAME OUT, BUT THE FAN SEEMED TO BE BROKEN. MAINTENANCE DEFERRED THE FREON AIR CONDITIONING SYSTEM. UPON INVESTIGATION MAINTENANCE REPLACED BOTH EVAPORATOR MODULE BLOWER ASSEMBLIES, NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19951020000241995102000024WP 1995 10 20 9515379967 119951009A5220591015931 RELEASE MECH DOUG DC9 DC931 3022065WP RT EMER EXIT WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO RELEASE THE AFT RIGHT EMERGENCY OVERING EXIT. REPLACED THE DOOR AND RIGGED PER MM 52-21-501. 2L72 4F A6WE 19951020000251995102000025WP 1995 10 20 9515389102 119951005A5350 RELEASE MECH DOUG DC9 DC915 3022036WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL0192S 47064 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ADJUSTED AND LUBRICATED THE RELEASE MECHANISM, CHECKED OK. 2L72 4F A6WE 19951020000261995102000026WP 1995 10 20 9515399967 119951012A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVED THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. 2L72 4F A6WE 19951020000271995102000027WP 1995 10 20 9515409609 119950614A5713 LONGERON DOUG DC9 DC932 3022066WP WS 100 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STR 11 AT XORS 100. REPAIRED STRINGER (P/N DWG 5910465), PER EA 99-97588. 2L72 4F A6WE 19951020000281995102000028WP 1995 10 20 9515419609 119950619A5713 LONGERON DOUG DC9 DC932 3022066WP WS 69-91 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LEFT WING STR 20 AND RIGHT WING STR 13, XRS 69-91. REPAIRED BOTH PER EA 99-97591. 2L72 4F A6WE 19951020000291995102000029WP 1995 10 20 9515429609 119950628A5713 LONGERON DOUG DC9 DC932 3022066WP WS 110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 18 AT XRS 110. REPAIRED STRINGER (DWG 5910465), PER EA 99-97607. 2L72 4F A6WE 19951020000301995102000030WP 1995 10 20 9515439609 119950707A5754 RIB DOUG DC9 DC932 3022066WP NR 3 LE SLAT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT WING NR 1 AND NR 3 SLAT CENTER RIBS MOUNT HOLES. REPAIRED PER EA 99-97723. 2L72 4F A6WE 19951020000311995102000031WP 1995 10 20 9515449609 119950710A5320 DOUBLER DOUG DC9 DC932 3022066WP CARGO DOOR JAMB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE INTERNAL SKIN DOUBLER AT THE FORWARD CARGO DOOR LOWER JAMB. REPAIRED DOUBLER (P/N 5911412), PER EA 99-100402. 2L72 4F A6WE 19951020000321995102000032WP 1995 10 20 9515459607 119950711A5330 SKIN DOUG DC9 DC932 3022066WP FS 598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 598 SKIN DOUBLER AT LONGERON 21R TO 22R. REPAIRED DOUBLER (P/N 5910772-9), PER EA 96-98112. 2L72 4F A6WE 19951020000331995102000033WP 1995 10 20 9515469607 119950713A5313 LONGERON DOUG DC9 DC932 3022066WP FS 794 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30 AT FS 794. REPAIRED LONGERON (P/N 5920303-1), PER EA 96-98105. 2L72 4F A6WE 19951020000341995102000034WP 1995 10 20 9515479609 119950815A575459225332 RIB DOUG DC9 DC932 3022066WP NR 3 LE SLAT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING NR 3 SLAT CENTER RIB MOUNT HOLES. REPAIRED RIB (P/N 5922533-2), PER EA 99-97598. 2L72 4F A6WE 19951020000351995102000035WP 1995 10 20 9515489607 119950816A5512 SKIN DOUG DC9 DC932 3022066WP HORIZ STAB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT HORIZONTAL UPPER AFT SKIN. REPAIRED SKIN (P/N 5922578-502), PER EA 96-98094. 2L72 4F A6WE 19951020000361995102000036WP 1995 10 20 9515499953 119950905A5330 SKIN DOUG DC9 DC931 3022065WP FS 639 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01918RW 47158 DURING H-CHECK, FOUND CORROSION IN THE INNER SKIN AT FS 639, LONGERON 18L. REPAIRED PER EA 99-10973. 2L72 4F A6WE 19951020000371995102000037WP 1995 10 20 9515509609 119950907A5330 SKIN DOUG DC9 DC932 3022066WP FS 997 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01609NW 47234 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FUSELAGE SKIN FS 997 AT LONGERON 23R. REPAIRED SKIN (P/N 5911428-42), PER EA 99-97722. 2L72 4F A6WE 19951020000381995102000038WP 1995 10 20 9515519607 119950916A5730 SKIN DOUG DC9 DC932 3022066WP WS 90-383 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01607NW 47232 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE UPPER LEFT SKIN PANELS FROM XRS 90 TO 383. REPAIRED PER EA 96-100273. 2L72 4F A6WE 19951020000391995102000039WP 1995 10 20 9515529853 119950918A5347 SEAT TRACK DOUG DC9 DC951 3022051WP FS 230 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND CORROSION IN THE RIGHT INBOARD SEAT TRACK AT FS 230. REPAIRED TRACK (P/N 5910754-11), PER EA 98-101978. 2L72 4F A6WE 19951020000401995102000040WP 1995 10 20 9515539853 119950921A5320 SUPPORT DOUG DC9 DC951 3022051WP FS 237-264 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING H-CHECK, FOUND CORROSION ON THE CENTER LINE FLOOR SUPPORT FROM FS 237 TO 264. REPAIRED SUPPORT (P/N5910760-11), PER EA 98-103279. 2L72 4F A6WE 19951020000411995102000041WP 1995 10 20 9515549967 119951005A5312 BLKHD FITTING DOUG DC9 DC931 3022065WP FS 756 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND CRACKS IN THE FS 756 FORWARD BULKHEAD FITTINGS, SECOND FROM THE TOP AND SECOND FROM THE BOTTOM. REPLACED BOTH FITTINGS PER SRM 51-30-02 AND 51-30-05. 2L72 4F A6WE 19951020000421995102000042WP 1995 10 20 9515559601 119951006A5753 FITTING DOUG DC9 DC932 3022066WP LT TE FLAP VANE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT FLAP INBOARD FIXED VANE TIE FITTING. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951020000431995102000043WP 1995 10 20 9515569613 119951008A5312 BLKHD FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613NW 47438 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 996 AFT PRESSURE BULKHEAD LOWER FRAME FITTING. REPLACED FITTING PER SRM 51-10-03, 51-30. 2L72 4F A6WE 19951020000441995102000044WP 1995 10 20 9515579946 119951010A5313 LONGERON DOUG DC9 DC931 3022065WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 29L TO 30 FITTINGS AT FS 756. REPLACED FITTINGS PER SRM 51-05. 2L72 4F A6WE 19951020000451995102000045WP 1995 10 20 9515589601 119951011A5320 FITTING DOUG DC9 DC932 3022066WP FS 795 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 795 FRAME TO FLOOR MOUNT FITTING AT LONGERON 18L. REPLACED FITTING PER SRM 51-30-3. 2L72 4F A6WE 19951020000461995102000046WP 1995 10 20 9515599601 119951011A5320 FITTINGS DOUG DC9 DC932 3022066WP FS 200/208 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LBL 50 TO 55 FRAME TO FLOOR FITTINGS, FS 200 AND FS 208. REPLACED FITTINGS PER SRM 51-30-2. 2L72 4F A6WE 19951020000471995102000047WP 1995 10 20 9515609601 119951011A5320 FITTING DOUG DC9 DC932 3022066WP FS 160 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 160 FRAME TO FLOOR FITTING AT LONGERON 17R TO 18R. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951020000481995102000048WP 1995 10 20 9515619601 119951011A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 17L LONGERON TENSION TIE FITTING AT THE FS 996 FRAME. REPLACED FITTING PER SRM 51-30-05. 2L72 4F A6WE 19951020000491995102000049WP 1995 10 20 9515629601 119951011A5320 FITTING DOUG DC9 DC932 3022066WP FS 980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 18L TIE FITTING AT THE FS 980 FRAME. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951020000501995102000050WP 1995 10 20 9515639601 119951011A5754 FITTING DOUG DC9 DC932 3022066WP NR 5 SLAT TRACK CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO CRACKS IN THE LEFT WING NR 5 SLAT INBOARD IDLER TRACK ATTACH FITTING. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951020000511995102000051WP 1995 10 20 9515649613 119951012A5511 FITTING DOUG DC9 DC932 3022066WP HORIZ STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613NW 47438 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 1.2 INCH CRACK IN THE HORIZONTAL STABILIZER CENTER BOX T-FITTING AT THE FORWARD UPPER SPAR. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19951020000521995102000052 1995 10 20 9515652294 419951014A344220704100101 RADAR TRANS BOEING727 727251 138408HNM FWD FUS FAILED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01294US41071814 21505 DURING CRUISE, WEATHER RADAR INDICATION PRODUCED INTERMITTENT PATTERNS. FLIGHT DIVERTED TO ATL DUE TO WEATHER EN ROUTE. MAINTENANCE REPLACED THE RADAR TRANSCEIVER. OPERATIONAL CHECK NORMAL AND FLIGHT RESUMED SEGMENT TO MIA. 2L73 4F A3WE 19951020000531995102000053WP 1995 10 20 9515661160 119951012A2820ANL70311 TEE DOUG DC10 DC1040 3023508WP CTR FUEL TANK CRACKED A NWAAAJ UNSCHED LANDING DUMP FUEL O OTHER CRCRUISE 1 GL01160US 46769 DURING CRUISE, UNABLE TO TRANSFER FUEL FROM THE AUXILIARY TANK, DUMPED 35,000 LBS OF FUEL AND RETURNED TO BOS. REPLACED THE CENTER TANK FILL LINE TEE ASSEMBLY. 2L73 4F A22WE 19951020000541995102000054NM 1995 10 20 95FDEA01539 119951013A5330 SKIN BOEING727 727227 1384078NM BS 235 CREASED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CREASE IN SKIN BS 235 AT STR 20R. CUT OUT DAMAGE AT BS 235 STR 14R, FABRICATED NEW REPAIR DOUBLER AND INSTALLED AT BS 235 STR 20R PER FEDEX SRM 53-3-3 FIG 1. 2L73 4F A3WE 19951020000551995102000055NE 1995 10 20 95FDEA01540 219951013A7250 TURBINE BOEING727 7272S2F 1384O81NM PWA JT8 JT8D17A 52049NE NR 2 ENGINE FAILED A FDEACED ABORTED TAKEOFF ENGINE SHUTDOWN RETURN TO BLOCK AR FLAME/FIRE PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO25216FE 22937 ABORT ON RUNWAY FOR ENGINE FAILURE ABOUT 80K, #2 ENG MAXIMUM POWER T/O. FOUND NR 2 ENG TURBINE FAILURE. REMOVED NR 2 ENG AS PER WORKCARD 70T0002, INSTALLED NR 2 ENG PER WORKCARD 70T0002. COMPLIED WITH HOOKUPS OPERATIONAL AND LEAK CHECKS PER WORKCARD 70T0002 AND 70T0301, OPS CK GOOD. REQUIRED ITEMS INSPECTION COMPLIED WITH. 2L73 4F4 F A3WE E2EA 19951020000561995102000056WP 1995 10 20 ABXA9500822 119951012A323057146745503 CONTROL VALVE DOUG DC8 DC863 302198AWP LT MLG LEAKING A ABXAO OTHER K FLUID LOSS DEDESCENT 1 GL23825AX 46115 LEFT MAIN LANDING GEAR HAD TO BE CYCLED TO GET DOWNLOCK INDICATION. NO GREEN DOWNLOCK INDICATION OR SPOILER PRESSURE INDICATION OCCURRED ON THE FIRST ATTEMPT. DURING THE SECOND ATTEMPT, THE LEFT MAIN LANDING GEAR LOCKED DOWN, BUT AT A SLOWER RATE THAN THE OTHER GEARS. RIGGED LEFT MAIN LANDING GEAR DOORS, CHECKED MAIN GEAR UPLOCK ROLLER CLEARANCE AND REPLACED LANDING GEAR CONTROL VALVE IAW DC8 MM, CHAPTER 32. EXTENSION, RETRACTION, UPLATCH AND FREE-FALL CHECKS WERE GOOD IAW DC8 MM, CHAPTER 32. 2L74 4F 4A25 19951020000571995102000057WP 1995 10 20 ABXA9500823 119951013A3230 RETRACT MECH DOUG DC8 DC863 302198AWP NLG LACK OF LUBE A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23820AX 46155 AFTER TAKEOFF, THE LANDING GEAR RETRACTED NORMALLY, BUT THE UPLATCH CHECK WAS UNSATISFACTORY. THE LANDING GEAR WAS EXTENDED AND RETRACTED AGAIN AND A SQUEALING NOISE WAS HEARD FROM THE NOSE GEAR AREA. THE LANDING GEAR RETRACTED NORMALLY AND THE SECOND UPLATCH CHECK WAS GOOD. LUBRICATED THE NOSE LANDING GEAR AND PERFORMED SEVERAL RETRACTION CHECKS. NO NOISES WERE HEARD DURING THE RETRACTION CHECK AND THE UPLATCH CHECK WAS GOOD. THE LANDING GEAR RETRACTION CHECK WAS COMPLETED IAW DC8 MM, CHAPTER 32. 2L74 4F 4A25 19951020000581995102000058SO 1995 10 20 COMA9511982 119951007A27503471001001 ANNUNCIATIOR EMB 120 EMB120RT SO COCKPIT DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01266CA10383621 120258 FLAP DISPLAY CONTROL FAULT, NO FLAP MOVEMENT. REPLACED THE FLAP ANNUNCIATOR UNIT. 2L72 4T RTA31SO 19951020000591995102000059EA 1995 10 20 COMA9560567 119951006A5210 DOOR CNDAIRCL600 CL6002B19 EA CABIN NOT LATCHED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01912CA 7011 AIRCRAFT WILL NOT PRESSURIZE. STATUS MESSAGE, INBD COOL FAIL AND CAUTION MESSAGE, OVERBD COOL FAIL. OPENED AND CLOSED CABIN DOOR, PROBLEM DID NOT DUPLICATE AND AIRCRAFT PRESSURIZED NORMAL. 2L72 4F RTA21EA 19951020000601995102000060WP 1995 10 20 DHL80504 119950909A324426014112 TIRES DOUG DC8 DC873F 302199FWP NR 1/2 BLOWN A TDHLAO OTHER O OTHER LDLANDING 1 SO01805DH 46125 THE NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES WERE BLOWN ON LANDING. REMOVED AND REPLACED NR 1, 2, 5 AND 6 MAIN WHEEL ASSEMBLIES PER DC8 MM 32-40-0. REMOVED AND REPLACED ANTI-SKID CONTROL BOX AS PRECAUTIONARY, DEFERRED ARM-DISARM CHECK PER DC8 MM 32-43-0. 2L74 4F RT4A25 19951020000611995102000061NM 1995 10 20 DHL9572405 119950906A5230 MECHANISM BOEING727 727228 NM CARGO DOOR LACK OF LUBE A TDHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01724DH 19862 MAIN CARGO DOOR LIGHT ON DOOR ANNUNCIATOR PANEL ILLUMINATED AT FL 290. CARGO UNLOCK LIGHT ILLUMINATED ACCOMPANIED BY LOUD THUNK THAT WAS HEARD AND FELT. FOUND FASTENERS LOOSE AT TORQUE TUBE/ACTUATOR BRACKET ON LATCHES 6 AND 7, RESECURED, ADJUSTED AND LUBED. ADJUSTED LOCKING ROD MECHANISM, PRESS A/C TO 8.5 PSI, NO LEAKS OR WARNING INDICATIONS IAW 52-30-00. 2L73 4F A3WE 19951020000621995102000062NM 1995 10 20 DHL9572408 119950910A2751 INDICATION BOEING727 727228 NM TE FLAPS MALFUNCTIONED A TDHLAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 SO01724DH 19862 DURING EXTENSION FLAPS 2 BOTH INBOARD AND LEFT OUTBOARD WERE OUT OF INDICES ON FLAP GAUGE. SWAPPED FLAP INDICATORS FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN UNABLE TO FIND ANY TROUBLE, IAW MM 27-52-0A. 2L73 4F A3WE 19951020000631995102000063NE 1995 10 20 P5CA9500806 219951015A7260 CHIP DETECTOR BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A P5CAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS DEDESCENT 1 WP23859FT 20326 662376 NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY A PRESSURE FLUCTUATION. PRECAUTIONARY ENGINE SHUTDOWN COMPLIED WITH, 35 PSI AFTER SHUTDOWN. PERFORMED WINDMILLING INSP PER MM 72-00-00, PERFORMED LEAK CHECK PER MM 71-00-44. FOUND CHIP DETECTOR CRACKED, REPLACED SAME. CHECKED PER 72-61-00, INSPECTED CHIP DETECTORS PER MM 72-61-00, VISUAL INSPECTION FOUND ACCEPTABLE. 2L74 4F4 F A20WE E20EA 19951020000641995102000064NE 1995 10 20 P5CA9500807 219951015A7261 OIL SYST BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE ENGINE FAILED A P5CAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 WP23859FT 20326 662376 AT TOP OF CLIMB, OIL QTY INDICATION WAS 3.9 GALS, TIME 2359Z AND AT 0025Z QTY WAS 3.5 GALS. RAN THE ENGINE OIL QTY LOW CHECKLIST, AT 0100 OIL QTY WAS 2.8 GALS. RETURNED TO ANC, LANDED WITH .2 GAL INDICATING, HAD GOOD TEMP AND PRESSURE AT ALL TIMES. REPLACED ENGINE. 2L74 4F4 F A20WE E20EA 19951020000651995102000065NM 1995 10 20 SCNA95235 119951009A3350S106 EEL BATTERIES BOEING727 727227 1384078NM L 1 DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE PORTABLE EMERGENCY LIGHT AT THE L-1 DOOR WAS FOUND TO TEST DIM. REMOVED AND REPLACED BATTERIES IN L-1 DOOR EMERGENCY LIGHT IAW MM 33-50-101 AND LIGHT TESTED NORMAL. 2L73 4F A3WE 19951020000661995102000066NM 1995 10 20 SCNA95236 119951010A3350S106 EEL BATTERIES BOEING727 727282 2F0R NM COCKPIT DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 21949 THE COCKPIT PORTABLE EMERGENCY LIGHT TESTED DIM. REMOVED AND REPLACED BATTERIES IAW MM 33-50-101 AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951020000671995102000067NM 1995 10 20 SCNA95237 119951010A3350900835A EEL BATTERY PACK BOEING727 727282 2F0R NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 21949 THE RIGHT CENTER OVERWING EMERGENCY LIGHT TESTED DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-22 AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951020000681995102000068NM 1995 10 20 SCNA95238 119951011A3350582214 EEL BATTERY PACK BOEING727 727259 138408JNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE AFT THIRD OF EMERGENCY TRACK LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND REPLACED 2 STRIPS OF FLOOR LIGHTS. 2L73 4F A3WE 19951020000691995102000069WP 1995 10 20 SCNA95239 119951010A2611DDK1060 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP AFT LAVS INTERMITTENT A SCNAK NONE O OTHER UKUNKNOWN 1 GL15907WA 46946 THE AFT LAV SMOKE DETECTORS WERE INOPERATIVE. ACCOMPLISHED CHECK OF ALL SMOKE DETECTORS AND COULD NOT DUPLICATE PROBLEM. 2L73 4F A22WE 19951020000701995102000070NE 1995 10 20 SWAA0657 219951007A7200 ENGINE BOEING737 7372T4 1384492NM PWA JT8 JT8D9A 52048NE NR 2 FAILED A ASWAAEA ENGINE SHUTDOWN UNSCHED LANDING RY PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CLCLIMB 1 SW07129SW 22340 707329 SHORTLY AFTER TAKEOFF, NUMBER 2 ENGINE FAILED WITH ACCOMPANYING LOUD BANG AND SEVERE VIBRATION. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 2 ENGINE ASSEMBLY. 2L72 4F4 F A16WE E2EA 19951020000711995102000071NM 1995 10 20 SWAA0658 119951010A278265446519 ACTUATOR BOEING737 7372H4 138448CNM NR 4 LE FLAP MALFUNCTIONED A ASWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW0761SW 21970 IN FLIGHT, EXPERIENCED NUMBER 4 L/E SLAT UNCOMMANDED DEPLOYMENT. AIRCRAFT DIVERTED TO LAS AND MADE AN UNEVENTFUL LANDING. REPLACED NUMBER 4 L/E SLAT ACTUATOR. 2L72 4F A16WE 19951020000721995102000072NM 1995 10 20 SWAA0659 119951002A5320 POST BOEING737 7373H4 1384600NM LT COCKPIT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07686SW 23175 DURING SCHEDULED B/C CHECK, FOUND CAPTAIN'S NUMBER 1 WINDOW POST CRACKED .156 INCH. REPAIRED PER RA 1-A53-1156. 2L72 4F RTA16WE 19951020000821995102000082EA 1995 10 20 95ZZZX5748 219950724A7414 DISTRIBUTOR GEAR 103493051 PIPER PA28 PA28R200 7102811SO LYC O360 IO360C1C 41514EA MAGNETO TEETH STRIPPED A RGLAO OTHER O OTHER CRCRUISE 1 NM012742R183 F219401FR 28R35281 MAGNETO BECAME INOPERATIVE DURING FLIGHT. TROUBLESHOT TO DISTRIBUTOR GEAR TEETH STRIPPED. SUBMITTER STATED THIS IS THE THIRD OCCURRENCE OF THIS MALFUNCTION IN LAST 3 YEARS. 1L71 3O3 O 2A13 1E10 19951020001581995102000158CE 1995 10 20 95ZZZX5795 119950727A3260 LAMP BEECH 58 58 1152740CE NLG DOWNLOCK FAILED A BSYAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL07400RP TH319 NO GEAR DOWN AND LOCK INDICATION, FOUND BULB DEFECTIVE. REMOVED AND REPLACED BULB, CHECKS GOOD. 1L72 3O 3A16 19951020001591995102000159SO 1995 10 20 95ZZZX5796 219950801A8520 CONNECT ROD BEECH 58 58 1152740CE CONT O520 IO520C 17032SO NR 6 FAILED A BSYAO OTHER ERKVIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS NRNOT REPORTED 1 GL0795BB TH333 243682H RIGHT ENGINE, NR 6, CONNECTING ROD WENT THROUGH ENGINE CASE. REMOVED AND REPLACED ENGINE. CAUSE UNKNOWN AT THIS TIME. 1L72 3O3 O 3A16 E5CE 19951020002001995102000200 1995 10 20 DJSA950002 419950918A3451200021700 POWER SUPPLY KING KN65 DOUG DC3 DC3C 3021457WP DME SHORTED A DJSAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23105CA 9436 25720 DME POWER SUPPLY DIODE PN CR-127 SHORTED OUT CAUSING RESISTORS R-166 AND R-168 TO OVERHEAT RESULTING IN SMOKE IN THE COCKPIT. (X) 2L72 4R A669 19951020002011995102000201WP 1995 10 20 9515679994 119950707A5330 SKIN DOUG DC9 DC931 3022065WP AFT FUSELAGE CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018978E 47327 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FUSELAGE SKIN 9 INCHES ABOVE THE RIGHT PYLON REAR SPAR. REPAIRED PER EA 99-94727. 2L72 4F A6WE 19951020002021995102000202WP 1995 10 20 9515689994 119950730A5330 SKIN DOUG DC9 DC931 3022065WP FS 427 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018978E 47327 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 427 BETWEEN LONGERONS 22R TO 23R. REPAIRED PER EA 99-94741. 2L72 4F A6WE 19951020002031995102000203NM 1995 10 20 9515692204 119950901A5313 LONGERON BOEING727 727251 138408HNM FS 620 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 22544 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 27R AT FS 620. REPAIRED PER EA 22-99243. 2L73 4F A3WE 19951020002041995102000204WP 1995 10 20 9515709994 119950904A5330 SKIN DOUG DC9 DC931 3022065WP FS 800 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018978E 47327 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FUSELAGE SKIN FS 800 AT LONGERON 26R. REPAIRED PER EA 99-94747. 2L72 4F A6WE 19951020002051995102000205WP 1995 10 20 9515719994 119950904A5313 LONGERON DOUG DC9 DC931 3022065WP FS 408-427 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018978E 47327 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION ON LONGERON 29L BETWEEN FS 408 TO 427. REPAIRED PER EA 99-94755 REV A. 2L72 4F A6WE 19951020002061995102000206NM 1995 10 20 9515722204 119950905A5330 FLANGES BOEING727 727251 138408HNM NR 1140 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01204US 22544 DURING PERIODIC CHECK, FOUND CORROSION ON PANEL NR 1104 CUTOUT FLANGES, LBL 5 RBL 9. REPAIRED PER EA 22-99245. 2L73 4F A3WE 19951020002071995102000207WP 1995 10 20 9515731147 119950919A5347 SEAT TRACK DOUG DC10 DC1040 3023508WP FS 1530 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND CORROSION IN THE SEAT TRACK AT FS 1530, LBL 107. REPAIRED TRACK PER EA 11-99277. 2L73 4F A22WE 19951020002081995102000208 1995 10 20 9515741147 419950920A3416 MOUNTING RINGS DOUG DC10 DC1040 3023508WP RADIO ALTIMETER CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND CORROSION ON THREE RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS, AYB 7022 AND AYB 7053 PER EA 11-99260. 2L73 4F A22WE 19951020002091995102000209EU 1995 10 20 9515753209 119950921A5320 SILL AIRBUS320 A320211 3930320EU DOOR 4L CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON THE LEFT AFT DOOR SILL. REPAIRED SILL PER EA 32-99200. 2L72 4F RTA28NM 19951020002101995102000210WP 1995 10 20 9515761147 119950921A5312 BLKHD SKIN DOUG DC10 DC1040 3023508WP FS 1156 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND CORROSION ON THE CENTER WING FRONT SPAR PRESSURE BULKHEAD FS 1156 AT THE SKIN BETWEEN LONGERONS 47R TO 48R. REPAIRED BULKHEAD PER EA 11-98963. 2L73 4F A22WE 19951020002111995102000211WP 1995 10 20 9515771147 119950921A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME FS 879 AT LBL 33. REPAIRED FRAME (P/N ADA 7034), PER EA 11-99255. 2L73 4F A22WE 19951020002121995102000212WP 1995 10 20 9515789855 119950922A5312 BLKHD WEB DOUG DC9 DC951 3022051WP APB DOOR JAMB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND A CRACK IN THE AFT BULKHEAD DOOR JAMB WEB AT THE UPPER HINGE FITTING. REPAIRED WEB (P/N 5917463), PER EA 98-101981. 2L72 4F A6WE 19951020002131995102000213WP 1995 10 20 9515799855 119950922A5412 BLKHD WEB DOUG DC9 DC951 3022051WP FS 1136 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND OIL CANNING IN THE RIGHT PYLON BULKHEAD WEB AT FS 1136. REPAIRED WEB (P/N 9912243), PER EA 99-102576. 2L72 4F A6WE 19951020002141995102000214WP 1995 10 20 9515809855 119950922A5320 CUSP DOUG DC9 DC951 3022051WP DOOR 1 R CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND CORROSION ON THE RIGHT CUSP AT THE FORWARD AND AFT CORNERS OF DOOR 1R. REPAIRED CUSP (P/N 9910078-13), PER EA 98-102579. 2L72 4F A6WE 19951020002151995102000215NM 1995 10 20 9515815501 119950922A5320 DOOR SILL BOEING757 757251 1384970NM FS 1380 1440 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01501US 23190 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD FS 1380 TO 1440. REPAIRED CHORD (P/N 146N8522-51), PER EA 55-99002. 2L72 4F RTA2NM 19951020002161995102000216EU 1995 10 20 9515823209 119950922A5320 SUPPORTS AIRBUS320 A320211 3930320EU FS 31577-32571 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON THE RIGHT AND LEFT OUTBOARD FLOOR SUPPORTS BS 1292. REPAIRED SUPPORTS (P/N 534-72172-203, -204) PER EA 32-99197. 2L72 4F RTA28NM 19951020002171995102000217WP 1995 10 20 9515831147 119950923A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME FS 879 AT RBL 38. REPAIRED FRAME (P/N ADA 7034), PER EA 11-99259. 2L73 4F A22WE 19951020002181995102000218WP 1995 10 20 9515849752 119950925A5312 BLKHD FRAME DOUG DC9 DC941 302207NWP FS 1072 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND CORROSION IN THE AFT PRESSURE BULKHEAD FRAME FS 1072 FROM LONGERON 17L TO THE CUSP. REPAIRED FRAME (P/N 5910163-73), PER EA 97-101982. 2L72 4F A6WE 19951020002191995102000219NM 1995 10 20 9515852290 119950925A5313 LONGERON BOEING727 727251 138408HNM FS 950-1000 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01290US 21378 DURING PERIODIC CHECK, FOUND CORROSION ON STR 29L BETWEEN BS 950A TO 1000. REPAIRED STRINGER (P/N 65-56441-3), PER EA 22-99254. 2L73 4F A3WE 19951020002201995102000220WP 1995 10 20 9515861147 119950926A5330 SKIN DOUG DC10 DC1040 3023508WP FS 1661-1681 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND CORROSION IN THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L TO 51R BENEATH THE ANTI-COLLISION LIGHT. REPAIRED SKIN (P/N NFA 6214-1), PER EA 11-99325. 2L73 4F A22WE 19951020002211995102000221WP 1995 10 20 9515871147 119950926A5320 ANGLE DOUG DC10 DC1040 3023508WP FS 1159 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01147US 46756 DURING T-CHECK, FOUND A 4.3 CRACK IN THE RIGHT WING FRONT SPAR TO FUSELAGE ATTACH ANGLE FS 1159 AT LONGERON 28R. REPAIRED ANGLE (P/N ANB 7353-1), PER EA 11-99276. 2L73 4F A22WE 19951020002221995102000222WP 1995 10 20 9515889855 119950927A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FS 1136 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND CORROSION ON THE FLOORBEAM CHORD FS 1136 AT LBL 19. REPAIRED CHORD (P/N 2912578), PER EA 98-102585. 2L72 4F A6WE 19951020002231995102000223EU 1995 10 20 9515893209 119950927A5313 LONGERON AIRBUS320 A320211 3930320EU FS 12700-13233 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 30 TO 31. REPAIRED STRINGER (P/N D532-31542-200, D532-31543-200), PER EA 32-99208. 2L72 4F RTA28NM 19951020002241995102000224EU 1995 10 20 9515903209 119950927A5313 LONGERON AIRBUS320 A320211 3930320EU FS 14300-14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31523-200), PER EA 32-99207. 2L72 4F RTA28NM 19951020002251995102000225EU 1995 10 20 9515913209 119950927A5313 LONGERON AIRBUS320 A320211 3930320EU FS 13767-15367 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-200), PER EA 32-99209. 2L72 4F RTA28NM 19951020002261995102000226 1995 10 20 9515929927 419951014A344220671570153 RT UNIT DOUG DC9 DC931 3022065WP E/E COMPARTMENT MALFUNCTIONED A ANWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018920E1411 1402 45835 DURING CRUISE, RADAR WOULD NOT PAINT GROUND AND INDICATOR, ONLY SHOWED SOLID RED ARC OF 20 MILE RADIUS. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR RECEIVER TRANSMITTER AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020002271995102000227GL 1995 10 20 9515931221 219951014A7310 FUEL FILTER DOUG DC10 DC1030 3023501WP GE CF6 CF650C 30018GL NR 3 ENGINE DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01221NW 46579 455114 DURING TAKEOFF ROLL AT 80 KTS, THE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED FOR THE NR 3 ENGINE AND THE TAKEOFF WAS ABORTED. THE LIGHT CAME ON AGAIN FOR ONE MINUTE DURING CLIMB WHILE PASSING THROUGH 1,000 FT AND THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. THE WIRING WAS INSPECTED, THE FUEL FILTER WAS REPLACED, AND THE SYSTEM CHECKED OK. 2L73 4F4 F A22WE A23EA 19951020002281995102000228NE 1995 10 20 9515949912 219951013A7321 FUEL CONTROL DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01862N 47406 678061 NR 2 ENGINE INSTRUMENTS BEGAN TO FLUCTUATE AFTER DEPARTING MSP. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. THE FCU ASSEMBLY WAS REPLACED AND SUBSEQUENT OPERATIONAL TEST WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951020002291995102000229WP 1995 10 20 9516129994 119951014A3231 CONTROL VALVE DOUG DC9 DC931 3022065WP LT MLG DOOR FAILED A NWAAO OTHER J WARNING INDICATION DEDESCENT 1 GL018979E 47328 DURING DESCENT, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER EXTENDING LANDING GEAR. RECYCLED LANDING GEAR AND LEFT MAIN LANDING GEAR DOOR REMAINED EXTENDED. AIRCRAFT LANDED WITH LEFT MAIN LANDING GEAR DOOR EXTENDED. REPLACED LEFT MAIN LANDING GEAR DOOR, GEAR CONTROL VALVE, AND FOLLOW-UP CABLE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020002301995102000230EU 1995 10 20 9516133226 119951015A3350321454 EEL POWER SUPPLY AIRBUS320 A320211 3930320EU CABIN INOPERATIVE A NWAAO OTHER L NO TEST CRCRUISE 1 GL01326US161155213 282 DURING CRUISE, THE AFT CABIN EMERGENCY PATH LIGHTS REMAINED ILLUMINATED, RESETTING THE SYSTEM DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT, 11WL AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951020002311995102000231WP 1995 10 20 9516149967 119951014A7603 PWR LEVER BOLT DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE BROKEN A ANWAAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 GL019331 47263 657496 NR 1 ENGINE STOPPED RESPONDING TO POWER LEVER INPUTS, THEN ACCELERATED TO FULL THRUST. THE ENGINE WAS SHUTDOWN AND THE FLIGHT WAS CONCLUDED WITHOUT INCIDENT. MAINTENANCE REPLACED A BROKEN BOLT IN THE POWER LEVER LINKAGE AT THE FCU. SUBSEQUENT GROUND RUN WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951020002321995102000232NM 1995 10 20 95FDEA01541 119951016A5314 KEEL BEAM BOEING727 72722 1384002NM BS 1126-1129 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0079, DISCOVERED CORROSION ON RT KEEL BEAM BS 1126 TO 1129, STR 29R TO BE OUT OF LIMITS. 2L73 4F A3WE 19951020002331995102000233NM 1995 10 20 95FDEA01542 119951016A5320BAC15123387 STRAP BOEING727 72722 1384002NM BS 1110 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0562, FOUND REINFORCING STRAP CRACKED BS 1110 RBL 32 WL 132. REPAIRED REINFORCING STRAP AT BS 1110 RBL 32 WL 153 IAW FEDEX SRM 51-40-4. 2L73 4F A3WE 19951020002341995102000234NM 1995 10 20 95FDEA01543 119951016A5313 STRINGER BOEING727 72722 1384002NM BS 440-455 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0081, DISCOVERED CRACKED STR AT BS 440 PLUS 15 STR 23R. ACCESSED AND REPAIRED STR AT BS 440 PLUS 15 STR 23R PER FEDEX SRM 53-10-3. INSTALLED AND LEAK CHECKED OXYGEN CYLINDERS. 2L73 4F A3WE 19951020002351995102000235NM 1995 10 20 95FDEA01544 119951016A5320651986219 CHORD BOEING727 72722 1384002NM BS 312-350 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 SEVERAL AREAS OF CORROSION ON UPPER LT NOSE CHORD BS 312 TO 350, LBL 13 WL 169. WILL REQUIRE REMOVAL OF DOGHOUSE FLOOR, STIFFENER BRACKETS AND COOLING DUCT FOR ACCESS. REMOVED AND REPLACED LT NOSE CHORD BS 312 TO 350, LBL 13 WL 169, INSTALLED FASTENERS PER BAC DRAWING NR 65-18415. 2L73 4F A3WE 19951020002361995102000236NM 1995 10 20 95FDEA01545 119951016A5311 FRAME BOEING727 727227 1384078NM BS 950 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 DENT IN FRAME AT BS 950F LT BETWEEN STR 23 TO 26, AFT CARGO BIN. CUT OUT DAMAGED SECTION OF FRAME, FABRICATED REPAIR FRAME AND INSTALLED IAW SRM 51-40-5. 2L73 4F A3WE 19951020002371995102000237NM 1995 10 20 95FDEA01546 119951016A5315651627910 FLOORBEAM BOEING727 727233 138408ANM BS 766-852 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25265FE 21671 CORROSION ON LONGITUDINAL FLOORBEAM AT BS 766 TO 852 LBL 24 WL 208. FOUND CORROSION BEYOND LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED BEAM FABRICATED AND INSTALLED NEW BEAM PER FEDEX SRM 53-10-2 AND FEDEX MM 28-11-0. 2L73 4F RTA3WE 19951020002381995102000238NM 1995 10 20 95FDEA01547 119951016A5320 SILL BOEING727 72725C 138400HNM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 MCD THRESHOLE SILL PLATE CORRODED AT STA 560. REMOVED CORROSION PER 51-10-6 PG 4 TO 5, INSTALLED DOUBLER AT STA 560 PER SRM 53-10-9 PG 11, REF NR 0098. 2L73 4F A3WE 19951020002391995102000239NM 1995 10 20 95FDEA01548 119951015A5341 FITTING BOEING727 72725C 138400HNM BS 740 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 LT WING FRONT SPAR FWD TERMINAL PIN JOINT HOLE CRACKED AFT END. LEVELED AND SHORED A/C IAW SRM 51-50-1, CUT LOWER CHORD ANGLE AND WEB IAW BOEING DRWG NR 65C29064, REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGLE IAW BOEING DRWG NR 65C29064. 2L73 4F A3WE 19951020002401995102000240 1995 10 20 COMA9511983 419951016A34526221270001 TRANSPONDER EMB 120 EMB120RT SO NR 2 DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01130G 15451 120130 NR 2 TRANSPONDER INOPERATIVE. REPLACED THE NR 2 TRANSPONDER. 2L72 4T RTA31SO 19951020002411995102000241SO 1995 10 20 COMA9511984 119951011A76030881824 SOLENOID EMB 120 EMB120RT SO RT ENGINE FAILED A COMAK NONE O OTHER ININSP/MAINT 1 SO011110J 120110 THE RIGHT POWER LEVER FLIGHT IDLE STOP SOLENOID IS INOPERATIVE. REPLACED THE FLIGHT IDLE STOP SOLENOID. 2L72 4T RTA31SO 19951020002421995102000242SO 1995 10 20 COMA9511985 119951009A2432501122804 BATTERY EMB 120 EMB120RT SO AVIONIC BAY DISCHARGED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01159A 13548686 120159 BACKUP BATTERY DOES NOT TEST. REPLACED THE EMERGENCY POWER SUPPLY BATTERY. 2L72 4T RTA31SO 19951020002431995102000243NE 1995 10 20 COMA9511986 219951012A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01161CA 120143 115298 THE LEFT ENGINE NH AND OIL PRESSURE DROPPED TO ZERO DURING FLIGHT. INFLIGHT SHUTDOWN PERFORMED AND DIVERTED TO MCO. REPLACED THE LEFT ENGINE ASSEMBLY. 2L72 4T4 TRTA31SO E20NE 19951020002441995102000244SO 1995 10 20 COMA9511987 119951007A323112012347001 LATCH EMB 120 EMB120RT SO RT MLG DOOR BROKEN A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01259CA 120252 THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. REPLACED BROKEN MAIN LANDING GEAR DOOR LATCH. 2L72 4T RTA31SO 19951020002451995102000245EU 1995 10 20 COMA9531170 119951009A2730531137 SWITCH SAAB SF340 SF340A 7850100EU PILOTS YOKE DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01344CA 340A025 THE MAIN PITCH TRIM IS INTERMITTENT ON PILOTS YOKE. REPLACED THE PILOTS PITCH TRIM SWITCH. 2L72 4T RTA52EU 19951020002461995102000246EU 1995 10 20 COMA9531171 119951009A27508519M3 CONTROLLER SAAB SF340 SF340A 7850100EU TE FLAPS DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01320CA15606979 340A064 FLAP DISAGREEMENT INDICATOR FLASHES WITH EACH FLAP POSITION SELECTION. REPLACED THE FLAP CONTROL UNIT. 2L72 4T RTA52EU 19951020002471995102000247EA 1995 10 20 COMA9560568 119951015A2750855D1003 BPSU CNDAIRCL600 CL6002B19 EA RT TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01927CA 7031 FLAPS FAIL MESSAGE ON EICAS, FLAPS DID NOT EXTEND. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT. 2L72 4F RTA21EA 19951020002481995102000248EA 1995 10 20 COMA9560569 119951014A2410755469C IDG CNDAIRCL600 CL6002B19 EA RIGHT FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01936CA 7043 NR 2 GENERATOR FAILED INFLIGHT, FOLLOWED BY NR 1 GENERATOR FAILURE, RAT DEPLOYED. REPLACED THE NR 2 INTEGRATED DRIVE GENERATOR, NO DEFECTS NOTED ON NR 1 IDG. 2L72 4F RTA21EA 19951020002491995102000249EA 1995 10 20 COMA9560570 119951011A80128989308 AIR START VALVE CNDAIRCL600 CL6002B19 EA RT ENGINE FAILED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01946CA 7072 RIGHT ENGINE START MESSAGE ON EICAS. REPLACED THE RIGHT ENGINE START VALVE. 2L72 4F RTA21EA 19951020002501995102000250EA 1995 10 20 COMA9560571 119951011A274283963 TRIM ACTUATOR CNDAIRCL600 CL6002B19 EA VERT STAB FAILED A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01943CA 7062 HORIZONTAL STABILIZER TRIM CHANNEL NR 1 INOPERATIVE MESSAGE ON EICAS. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2L72 4F RTA21EA 19951020002511995102000251EA 1995 10 20 COMA9560572 119951011A2752853D100MD61 ACTUATOR CNDAIRCL600 CL6002B19 EA RT TE FLAP DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01917CA4759 1325 7017 FLAP FAIL WARNING AT 38 DEGREES. REPLACED THE RIGHT OUTBOARD FLAP ACTUATOR. 2L72 4F RTA21EA 19951020002521995102000252 1995 10 20 COMA9560573 419951010A22106229968001 YAW DAMPER CNDAIRCL600 CL6002B19 EA NR 2 DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01924CA5295 7026 YAW DAMPER NR 2 WILL NOT STAY ON LINE. REPLACED THE NR 2 YAW DAMPER SUL4000. 2L72 4F RTA21EA 19951020002531995102000253EA 1995 10 20 COMA9560574 119951009A2750 ECU CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01931CA 7037 FLAPS FAIL CAUTION MESSAGE WHEN FLAPS ARE SELECTED TO 45 DEGREES. RESET THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19951020002541995102000254EA 1995 10 20 COMA9560575 119951009A2621892480 EXTINGUISHER CNDAIRCL600 CL6002B19 EA CABIN NOT SEALED A COMAK NONE O OTHER ININSP/MAINT 1 SO01912CA6090 7011 SEAL BROKEN ON CABIN FIRE EXTINGUISHER. REPLACED THE CABIN FIRE EXTINGUISHER. 2L72 4F RTA21EA 19951020002551995102000255 1995 10 20 DHL95707002 419951014A3442MI585161 RADAR RT UNIT BOEING727 72722 1384002NM RADAR SYST MALFUNCTIONED A TDHLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01707DH 18321 WEATHER RADAR SPIKES WHEN AIRCRAFT IS IN TURBULENCE OF LIGHT AND GREATER INTENSITY. DIVERTED TO SAT AND LANDED WITHOUT INCIDENT. FOUND LOOSE WIRES IN RADAR JUNCTION BOX TERMINAL 56. TIGHTENED LOOSE WIRES PER MM 20-11, REMOVED AND REPLACED RADAR RECEIVER TRANSMITTER (RT) PER MM 34-41-0. RADAR OPS CHECKS GOOD PER MM 34-41. 2L73 4F A3WE 19951020002561995102000256NM 1995 10 20 P5CA9500808 119951009A5350 FAIRING BOEING747 747132 1384882NM FS 1000 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 FOUND CRACK IN FUSELAGE FAIRING PANEL BETWEEN A/C BAYS AT FORWARD ADF PANEL, APPROX STA 1000. STOP DRILLED CRACK IAW SRM 51-10-01. HFEC INSPECTED AND DETERMINED CRACK ENDS AT STOP DRILL IAW MM 51-00-00. 2L74 4F A20WE 19951020002571995102000257NM 1995 10 20 P5CA9500809 119951009A5400 SKIRT FAIRING BOEING747 747132 1384882NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE SKIRT FAIRING AT DRAIN TUBE CUTOUT HOLE AREA CRACKED. BLENDED DAMAGE IAW SRM 51-10-01. 2L74 4F A20WE 19951020002581995102000258NM 1995 10 20 P5CA9500810 119951009A5400 SKIRT FAIRING BOEING747 747132 1384882NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE OUTBOARD SKIRT FAIRING FORWARD PANEL CRACKED WITH 2 EACH FASTENERS MISSING. REMOVED DAMAGED PANEL IAW SRM 51-10-01, FABRICATED AND INSTALLED NEW PANEL IAW 51-10-01. 2L74 4F A20WE 19951020002591995102000259NM 1995 10 20 P5CA9500811 119951009A5400 SKIRT FAIRING BOEING747 747132 1384882NM NR 2 PYLON CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 2 ENG OUTBOARD SKIRT FAIRING AFT PANEL CRACKED. REMOVED DAMAGED PANEL AND ADJACENT SPLICE IAW SRM 51-10-01. FABRICATED AND INSTALLED NEW PARTS IAW SRM 51-10-01 2L74 4F A20WE 19951020002601995102000260NM 1995 10 20 P5CA9500812 119951009A7800 EXHAUST FUNNEL BOEING747 747132 1384882NM NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 2 ENGINE OUTBOARD CORE COWL INNER EXHAUST FUNNEL CRACKED. REPAIRED IAW BAC59-75 PER STEP 4 AND 5. 2L74 4F A20WE 19951020002611995102000261NM 1995 10 20 P5CA9500813 119951009A5280 DOOR BOEING747 747132 1384882NM NLG CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NOSE LANDING GEAR SERVICE PANEL DOOR CRACKED. REPAIRED DAMAGE AND REINSTALLED IAW 52-40-00. 2L74 4F A20WE 19951020002621995102000262NM 1995 10 20 P5CA9500814 119951009A7830 R RAIL BOEING747 747132 1384882NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 662566 NR 4 ENGINE R-RAIL IS CRACKED AT FIVE THIRTY POSITION. REPAIRED RAIL IAW MM 72-53-01. 2L74 4F4 F A20WE E20EA 19951020002631995102000263NM 1995 10 20 P5CA9500815 119951009A5400 ANGLE BOEING747 747132 1384882NM NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 2 ENGINE INBOARD CORE COWL FORWARD LOCK LATCH CUTOUT ANGLE CRACKED. INSTALLED NEW DOUBLER AND ANGLE IAW SRM 51-30-02. 2L74 4F A20WE 19951020002641995102000264NM 1995 10 20 P5CA9500816 119951009A5414 FIRESHIELD BOEING747 747132 1384882NM NR 1 ENGINE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE RT CORE COWL UPPER FAIRING LOWER SKIN DELAMINATED. REMOVED DAMAGED FIRESHIELD, FABRICATED NEW COUPLER AND INSTALLED IAW SRM 54-30-03. 2L74 4F A20WE 19951020002651995102000265NM 1995 10 20 P5CA9500817 119951009A5411 FRAME BOEING747 747132 1384882NM NR 1 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE LT CORE COWL HAS CRACKED FRAME LOWER SURFACE. REMOVED DAMAGED AREA, REPAIRED IAW SRM 54-14-03. REINSTALLED REPAIRED AREA IAW SRM 54-14-03. 2L74 4F A20WE 19951020002661995102000266NM 1995 10 20 P5CA9500818 119951009A5400 CLIP BOEING747 747132 1384882NM NR 1 ENGINE BROKEN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE LEFT HAND CORE COWL HAS BROKEN FRAME SUPPORT CLIP AT PRE-COOLER EXHAUST CUTOUT. FABRICATED NEW SUPPORT CLIP AND INSTALLED IAW SRM 51-10-01. 2L74 4F A20WE 19951020002671995102000267NM 1995 10 20 P5CA9500819 119951009A5400 LATCH BOEING747 747132 1384882NM NR 1 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 1 ENGINE LEFT HAND CORE COWL THIRD LATCH FROM LEADING EDGE HAS CRACKED REPAIR. FABRICATED AND INSTALLED DOUBLER IAW SRM 54-30-01. 2L74 4F A20WE 19951020002681995102000268NM 1995 10 20 P5CA9500820 119951009A5400 CORNER BOEING747 747132 1384882NM NR 1 ENGINE TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 NR 3 ENGINE INBOARD COWL OUTBOARD FORWARD TOP CORNER ON REPAIR TORN. REMOVED DAMAGED REPAIR, REPAIRED TORN DOUBLER IAW SRM 54-30-02. INSTALLED DOUBLER IAW SRM 51-10-01 AND 54-30-02. 2L74 4F A20WE 19951020002691995102000269EU 1995 10 20 WWMA9500066 119951016A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU LT MLG FAILED A WWMAO OTHER N FALSE WARNING DEDESCENT 1 WP15957AE 957 DURING DESCENT, THE LEFT MAIN LANDING GEAR INTRANSIT LIGHT ILLUMINATED AND REMAINED ON UNTIL THE LANDING GEAR WAS EXTENDED. THE LEFT MAIN LANDING GEAR UPLOCK SWITCH WAS REPLACED IAW J32 AMM 32-60, NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19951020002701995102000270WP 1995 10 20 95ZZZM544 119950921A3231510361C LINK DOUG DC8 DC862 3021970WP NLG DOOR DEFECTIVE A RRXAO OTHER E VIBRATION/BUFFET CLCLIMB 1 WP15993CF 46028 FLT NR 107 - KAUS-KPIA - ON GEAR RETRACTION SEVERE SHIMMY AND LOUD NOISE WAS EXPERIENCED. AS AIRSPEED INCREASED PROBLEM INCREASED IN NOSE WHEEL WELL AREA. RETURNED TO KAUS. FOUND LEFT FORWARD NLG DOOR IN DOWN POSITION, WOULD NOT LOCK UP. REMOVED AND REPLACED NLG DOOR LOCK LINK. OPS CHECKS GOOD. 2L74 4F 4A25 19951020002711995102000271NM 1995 10 20 AWXA9500627 119950912A3350 EEL WIRE BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 19 AND ROW 20. RESECURED WIRES AS REQUIRED, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020002721995102000272NM 1995 10 20 AWXA9500628 119950912A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304AW 24011 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH ROW 19. REPINNED WIRE AT ROW 19, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020002731995102000273NM 1995 10 20 AWXA9500629 119950913A335020131A EEL BATT PACK BOEING757 757225 1384959NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28913AW 22207 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND THE R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951020002741995102000274NM 1995 10 20 AWXA9500630 119950914A3350 EEL STRIP BOEING737 737275 1384485NM CABIN WET A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN FRONT SECTION. CLEANED UP A WATER SPILL ON TRACK AT ROWS 1 AND 2, OPS CHECK GOOD. (M) 2L72 4F A16WE 19951020002751995102000275NM 1995 10 20 AWXA9500631 119950914A3350 EEL WIRE BOEING737 7373G7 1384595NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 14 TO ROW 18 AND ROW 21 TO ROW 23. RECONNECTED WIRES AND TRIMMED FLOOR TRACK FILLER TO FIT. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020002761995102000276NM 1995 10 20 AWXA9500632 119950915A3350 EEL BOEING737 7373G7 1384595NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 20 THROUGH ROW 23. RECONNECTED LIGHT AT ROW 23, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020002771995102000277NM 1995 10 20 AWXA9500634 119950916A3350 EEL BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28322AW 25400 PHX- DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 8 THROUGH ROW 14. REPAIRED EMERGENCY LIGHT SYSTEM, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020002791995102000279NE 1995 10 20 CAL950591 219950712A7530 STATOR SUPPORT DOUG DC9 DC981 3022081WP PWA JT8 JT8D217A 52053NE NR 2 ENGINE FAILED A ACALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW09138811962716874 48045 717369 FLT NR 0554 - MCO - THE NR 2 ENGNIE FAILED WITH A LOUD POP AND FLAME SEEN IN THE EXHAUST DURING TAKEOFF ROLL AT 60 KNOTS. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. TEARDOWN REVEALED A CRACKED/BROKEN 8TH STAGE STATOR SUPPORT SHELF. (M) 2L72 4F4 F A6WE E9NE 19951020002801995102000280WP 1995 10 20 CAL950816 119950914A335041B004AD073 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914840 49580 FLT NR 0340 - EWR - THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-15 WERE FOUND INOPERATIVE. THE BATTERIES FOR THE OVERHEAD EMERGENCY LIGHTS AT ROWS 11-15 WERE REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19951020002811995102000281WP 1995 10 20 CAL950817 119950821A5720 DOUBLER DOUG DC9 DC982 3022082WP WS 194.843 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096982623020 49486 HOU - INSPECTION FOUND A 2 INCH CRACK IN SPLICE DOUBLER AT LEADING EDGE STATION 194.843. THE SPLICE DOUBLER WAS REPAIRED IAW ECRA 5710-01645. (M) 2L72 4F A6WE 19951020002821995102000282WP 1995 10 20 CAL950819 119950811A5320 FLOOR SUPP0RT DOUG DC9 DC982 3022082WP BS 1155 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091481030710 49264 HOU - INSPECTION FOUND FLOOR SUPPORT CORRODED AT STATION 1155. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-60-0. (M) 2L72 4F A6WE 19951020002831995102000283WP 1995 10 20 CAL950820 119950828A5530 ANGLE DOUG DC9 DC982 3022082WP VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091680237071 49222 HOU - INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STABILIZER LEFT ANGLE AT STATION 1388. THE AREA WAS REPAIRED BY INSTALLING A DOUBLER ANGLE CAP AND SPLICE PER SRM 55-02, FIGURE 2G. (M) 2L72 4F A6WE 19951020002841995102000284WP 1995 10 20 CAL950823 119950917A7603 LIMIT SWITCH DOUG DC9 DC982 3022082WP LT/RT THROTTLE LOOSE A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW09478AC 48063 FLT NR 0392 - PBI - ALL THREE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE GEAR WAS CYCLED WITH NO CHANGE, BUT THE RED GEAR LIGHTS EXTINGUISHED WITH THROTTLE MOVEMENT. MAINTENANCE TIGHTENED BOTH THE LEFT AND RIGHT AUTO THROTTLE LIMIT SWITCH SCREWS. THE SYSTEM CHECKED NORMAL PER MM 32-60-01, PAGE 203. (M) 2L72 4F A6WE 19951020002851995102000285WP 1995 10 20 CAL950831 119950910A5350 LOCK PINS DOUG DC9 DC982 3022082WP TAILCONE WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW0916802 49222 HOU - THE TAILCONE HUNG UP ON UPPER LATCHES AND FAILED TO DROP DURING TEST WHILE AIRCRAFT WAS IN D-CHECK, A NEW UPPER LEFT TAILCONE RETAINING LOCK PIN AND A NEW TAILCONE TO EMPENNAGE ALIGNMENT PIN WERE INSTALLED. THE TAILCONE WAS RIGGED AND THE RELEASE SYSTEM TESTED GOOD PER MM 53-53-00. (M) 2L72 4F A6WE 19951020002861995102000286WP 1995 10 20 CAL950832 119950906A5320 JAMB DOUG DC9 DC932 3022066WP BAGG DOOR CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND CORROSION ON FORWARD BAGGAGE BIN DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44, PAGE 105. (M) 2L72 4F A6WE 19951020002871995102000287WP 1995 10 20 CAL950833 119950908A5320 ANGLE DOUG DC9 DC932 3022066WP LT MLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT WHEEL WELL ATTACH ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30. (M) 2L72 4F A6WE 19951020002881995102000288WP 1995 10 20 CAL950834 119950907A5753 BRACKET DOUG DC9 DC932 3022066WP RT TE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A .5 INCH CRACK IN THE RIGHT FLAP NR 4 FLAP HINGE INBOARD AND OUTBOARD BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-5. (M) 2L72 4F A6WE 19951020002891995102000289NM 1995 10 20 CAL950836 119950914A5320 SHEAR BEAM BOEING737 737291 138448WNM BS 706 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091525553690 21069 GSO - INSPECTION FOUND A .5 INCH CRACK IN SHEAR BEAM WEB ON LEFT SIDE OF STATION 706 AT STRINGER 18A. THE SHEAR BEAM WEB WAS REPAIRED IAW ECRA 5310-0316 5310-03161 AND BAC DRAWING 65C29228. (M) 2L72 4F A16WE 19951020002901995102000290WP 1995 10 20 CAL950838 119950907A5320 CUSP DOUG DC9 DC932 3022066WP BS 200 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 200 JUST AFT OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M) 2L72 4F A6WE 19951020002911995102000291WP 1995 10 20 CAL950839 119950907A5320 CUSP DOUG DC9 DC932 3022066WP BS 165 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 165 JUST FORWARD OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M) 2L72 4F A6WE 19951020002921995102000292NM 1995 10 20 CAL950841 119950918A5330 SKIN BOEING727 727232 1384082NM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092778365768 20638 IAH - INSPECTION FOUND CORROSION ON FUSELAGE SKIN LAP JOINT AT STATION 500, STRINGER 26R. THE AREA WAS REPAIRED IAW SRM 53-30-3, FIGURE 5. (M) 2L73 4F A3WE 19951020002931995102000293WP 1995 10 20 CAL950842 119950917A5330 SKIN DOUG DC9 DC932 3022066WP BS 1038 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038 BETWEEN LONGERON 10R AND 11R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 8. (M) 2L72 4F A6WE 19951020002941995102000294WP 1995 10 20 CAL950843 119950907A5753 BRACKET DOUG DC9 DC932 3022066WP LT TE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A .75 INCH CRACK IN NR 4 LEFT FLAP HINGE OUTBOARD BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M) 2L72 4F A6WE 19951020002951995102000295WP 1995 10 20 CAL950844 119950920A5340 JAMB DOOR DOUG DC9 DC932 3022066WP FWD SERV DOOR DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M) 2L72 4F A6WE 19951020002961995102000296WP 1995 10 20 CAL950845 119950916A5313 LONGERON DOUG DC9 DC932 3022066WP BS 935-990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-02, FIG 16. (M) 2L72 4F A6WE 19951020002971995102000297WP 1995 10 20 CAL950846 119950920A3230NAS110811D BOLTS DOUG DC9 DC982 3022082WP NLG DEFLECTOR MISSING A ACALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0983870 48056 FLT NR 0715 - CLE - THE NLG WOULD NOT RETRACT AND WAS ACCOMPANIED BY ILLUMINATION OF THE RED NOSE GEAR LIGHT AFTER TAKEOFF FROM CLE. THE MAIN GEAR RETRACTED NORMALLY. THE GEAR WAS CYCLED FOUR TIMES, BUT WITH NO CHANGE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOLTS MISSING FROM THE NLG DEFLECTOR. THE MISSING BOLTS WERE INSTALLED. A NLG SWING WAS PERFORMED AND OPERATION CHECKED GOOD. (M) 2L72 4F A6WE 19951020002981995102000298NM 1995 10 20 CAL950849 119950921A29136507506 HYD PUMP BOEING737 7372C0 1384488NM NR 2 ENGINE INOPERATIVE A CALAO OTHER J WARNING INDICATION APAPPROACH 1 SW09732436648 211 20072 FLT NR 1746 - GSO - THE HYDRAULIC QUANTITY INDICATOR GAUGE DECREASED SLOWLY TO ZERO WITH NO OTHER INDICATIONS WHILE ON APPROACH TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND THE ENGINE WAS RUN WITH NO LEAKS NOTED. (M) 2L72 4F A16WE 19951020002991995102000299NM 1995 10 20 CAL950850 119950915A5315 FLOOR BEAM BOEING737 7373T0 1384582NM BS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096933328487 23571 HOU - INSPECTION FOUND A 2 INCH CRACK IN FLOOR BEAM UPPER FLANGE AT STATION 520, RBL 24.75. THE FLOOR BEAM UPPER FLANGE WAS REPAIRED IAW SRM 5320-01208. (M) 2L72 4F RTA16WE 19951020003001995102000300NM 1995 10 20 CAL950851 119950919A532065496169013 ANGLE BOEING737 7373T0 1384582NM BS 947.5 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096933328487 23571 HOU - INSPECTION FOUND CORROSION ON AFT BAGGAGE BIN AFT BULKHEAD LOWER ATTACH ANGLE AT VERTICAL SUPPORTS, STATION 947.5, LBL 12 AND RBL 12. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-60-53 AND SRM 51-10-2. (M) 2L72 4F RTA16WE 19951020003011995102000301WP 1995 10 20 CAL950852 119950915A5312 BLKHD WEB DOUG DC9 DC932 3022066WP AFT ENTRY DR JMBCRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091552562151 47531 HOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M) 2L72 4F A6WE 19951020003021995102000302EU 1995 10 20 USAA950804 119950622A5330 SKIN FOKKERF28 F28MK4000 4990810EU FUSELAGE DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND 2 DENTS .125 INCH DEEP IN FUSELAGE SKIN ABOVE LAV SERVICE DOOR RIGHT SIDE. INSTALLED DOUBLER REPAIR PER SRM 53-02-02. (M) 2L72 4F RTA20EU 19951020003031995102000303EU 1995 10 20 USAA950805 119950627A5541 RIB FOKKERF28 F28MK4000 4990810EU RUDDER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19490US30126 11152 PIT - DURING FC-6 CHECK INSPECTION, FOUND .125 INCH CRACK IN RUDDER RIB NR 5 BOTTOM ANGLE BOTH SIDES. INSTALLED DOUBLER REPAIR PER SRM 55-02-07. (M) 2L72 4F RTA20EU 19951020003041995102000304EU 1995 10 20 USAA950810 119950713A5330 SKIN FOKKERF28 F28MK0100 4990807EU BS 24001-24611 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19854US13365 11282 PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 LEFT FUSELAGE SKIN. INSTALLED TITANIUM DOUBLER REPAIR PER USAIR EA 30650. (M) 2L72 4F RT 19951020003051995102000305EU 1995 10 20 USAA950811 119950713A5330 SKIN FOKKERF28 F28MK0100 4990807EU BS 24011-24611 DELAMINATION A USAAK NONE O OTHER ININSP/MAINT 1 EA19854US13365 11282 PIT - DURING Q-1 CHECK INSPECTION, FOUND 14 INCH BY 24 INCH AREA OF DELAMINATION AT STATION 24011 AND 24611 RIGHT SIDE FUSELAGE SKIN. INSTALLED TITANIUM DOUBLER REPAIR PER USAIR EA 30650. (M) 2L72 4F RT 19951020003061995102000306EU 1995 10 20 USAA950812 119950629A5330 SKIN FOKKERF28 F28MK0100 4990807EU BS 5805 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19854US13365 11282 PIT - DURING Q-1 CHECK INSPECTION, FOUND A DENT .085 INCH DEEP LEFT SIDE FUSELAGE STATION 5805. INSTALLED EXTERNAL DOUBLER PER SRM 53-00-02 PG 201 AND 51-70-06 PG 201. (M) 2L72 4F RT 19951020003071995102000307SO 1995 10 20 WTAA950264 119950913A7712311197801 TQ MONITOR SEN EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17286UE 120175 SFO - LEFT ENGINE TORQUE INDICATION REPORTED ERRATIC DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE TORQUE SIGNAL CONDITION. PROBLEM REOCCURED ON SUBSEQUENT TAKEOFF ROLL. MAINTENANCE REPLACED TORQUE MONITOR SENSOR FOLLOWING SECOND ABORTED TAKEOFF. TORQUE INDICATION SYSTEM OPERATIONAL CHECK NORMAL DURING ENGINE GROUND RUN AND TEST FLIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951020003081995102000308NM 1995 10 20 95ZZZM545 119950823A323065163424 RETRACT MECH BOEING727 727259 138408JNM NLG LACK OF LUBE A UHVAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO17203AV 22474 FLT NR FKYC9318 - KMIA - AFTER TAKEOFF, THE NOSE LANDING GEAR, P/N 65163424, WOULD NOT RETRACT. CYCLED GEAR SEVERAL TIMES, NO HELP. AIRCRAFT RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. LUBRICATED NOSE GEAR. JACKED AIRCRAFT AND CYCLED GEAR NUMEROUS TIMES PER MM 32-33-0. OPERATIONALLY CHECKS OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L73 4F A3WE 19951020003091995102000309NM 1995 10 20 95ZZZM546 119950516A5711 SPAR CHORD BOEING707 707330C 138367GNM WS 188 CRACKED A CLCAK NONE K FLUID LOSS ININSP/MAINT 1 SO19707HE 20124 ON WALKAROUND INSPECTION IN MIAMI, NOTICED FUEL RUNNING FROM UNDERWING PANEL FORWARD OF LEFT MAIN LANDING GEAR. VISUAL AND EDDY CURRENT INSPECTION INSIDE CENTER FUEL TANK REVEALED CRACKED CHORD ON REAR SPAR AT WS 188. REPAIRS WERE ACCOMPLISHED PER BOEING ENGINEERING DRAWING NR 65C36277. AIRCRAFT WAS RELEASED FOR SERVICE ON AUGUST 22, 1995. 2L74 4F 4A26 19951020003101995102000310NM 1995 10 20 95ZZZM547 119950921A3610652663929 BLEED DUCT BOEING727 72722C 138400FNM NR 3 ENGINE LEAKING A RYNAF ACTIVATE FIRE EXT. J WARNING INDICATION CRCRUISE 1 CE07421EX 19099 NR 3 ENGINE FIRE WARNING SOUNDED IN FLIGHT. DISCHARGED LEFT FIRE BOTTLE. INSPECTED NR 3 ENGINE FOR FIRE DAMAGE, NONE FOUND. REPLACED NR 3 ANTI-ICE VALVE, 13TH STAGE BLEED DUCT AND ASSOCIATED CLAMPS AND SEALS. REPLACED LEFT FIRE BOTTLE. (M) 2L73 4F A3WE 19951020003111995102000311 1995 10 20 95ZZZM548 419950927A256245230500 ELT TRAY ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE BROKEN A AJJBAK NONE O OTHER ININSP/MAINT 1 EA01839CA2445 52436 UE36 DURING SCHEDULED MAINTENANCE, THE ELT WAS DISCOVERED UNSECURED. MOUNTING TRAY FOUND BROKEN IN HALF. ELT WAS HANGING FROM REMOTE SWITCH WIRING AND ANTENNA CABLE. RUDDER CONTROL CABLE PULLEY AT FS 570- 107 CHIPPED, CAUSED BY A PIECE OF MOUNTING TRAY JAMMED IN PULLEY. OPERATOR BELIEVES BROKEN TRAY CAUSED BY ACCUMULATION OF MOISTURE (WATER) AND SUBSEQUENT FREEZING. ALL DAMAGE COMPONENTS HAVE BEEN REPLACED WITH NEW. 2L72 4T RTA24CE 19951020003121995102000312SO 1995 10 20 ASOA95022 119950913A2120 AIR DISTR EMB 120 EMB120RT SO CABIN ODOR A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11285AS 120265 OUTBOUND FAY-ATL, RETURNED TO FAY AFTER TAKEOFF DUE TO A FUEL SMELL IN THE CABIN AND COCKPIT WITH THE APU BLEED OPEN. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FAY WHERE LANDING WAS MADE SAFELY AND WITHOUT INCIDENT. LOCAL MECHANIC COULD NOT LOCATE ANYTHING VISUALLY AND HAD THE CREW TO GROUND RUN THE AIRCRAFT WITH EACH BLEED OPEN ONE AT A TIME. NO DEFECTS WERE FOUND. THE FLIGHT CONTINUED WITH THE APU DEFERRED. UPON ARRIVAL IN ATL, AND ASA MECHANIC INSPECTED APU FOR LEAKAGE. FOUND NONE, AND OPERATED THE PACKS FOR 20 MINUTES WITH NO FUMES OR FUEL ODOR NOTED. (M) 2L72 4T RTA31SO 19951020003131995102000313WP 1995 10 20 GRAA9542 119950915A2170 CLAMP DOUG DC9 DC915 3022036WP WATER SEPARATOR LOOSE A GRAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP111068T 45782 ON CLIMB-OUT FROM ENV, AIRCRAFT WOULD NOT HOLD PRESSURIZATION IN AUTO OR MANUAL. AIRCRAFT RETURNED TO ENV WITHOUT FURTHER INCIDENT. MAINTENANCE DISCOVERED A CLAMP HAD COME LOOSE ON THE WATER SEPARATOR CANNISTOR. MAINTENANCE RESECURED THE CLAMP AND PERFORMED AN OPERATIONAL AND LEAK CHECK. AIR CONDITIONING SYSTEM OPERATIONAL CHECK NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951020003141995102000314WP 1995 10 20 GRAA9544 119950911A2420 CURRENT LIMITER DOUG DC9 DC915 3022036WP NR 1 ENGINE FAILED A GRAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 WP111070T 45784 AFTER TAKEOFF, MADE A CLIMBING RIGHT TURN THROUGH 2000 FEET MSC. THE AIRCRAFTS LEFT GENERATOR FAILED. MAINTENANCE REMOVED AND REPLACED THE LEFT GENERATOR POWER RELAY, PERFORMED OPERATIONAL CHECK ON THE AC CROSS-TIE SYSTEM, OPERATIONALLY CLEARED NORMAL. MAINTENANCE DEFERRED THE LEFT GENERATOR IAW MEL 24-1. AIRCRAFT WAS RELOCATED TO SANTA BARBARA, CA. FOR FURTHER TROUBLESHOOTING. MAINTENANCE FOUND A CURRENT LIMITER BROKEN ON NR 1 ENGINE. MAINTENANCE REMOVED AND REPLACED THE CURRENT LIMITER. OPERATIONAL CLEARED NORMAL, NO DEFECTS NOTED, DMI NR 87 CLEARED, PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951020003151995102000315NM 1995 10 20 MALA954631 119950912A3350 EEL SIGN DHAV DHC8 DHC8102 2809003NM CABIN BROKEN A MALAK NONE O OTHER ININSP/MAINT 1 GL15817MA 249 FLT NR 3099 - DURING THE POST FLIGHT INSPECTION IN DTW, THE EMERGENCY EXIT SIGN AT SEAT 1DE WAS FOUND TO BE BROKEN. MAINTENANCE REPLACED THE EMEREGENCY EXIT SIGN. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951020003161995102000316NE 1995 10 20 MALA954632 219950913A72613022375 SEAL DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RT HYD PUMP FAILED A MALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15848MA 346 FLT NR 3085 - IN CRUISE FLIGHT TO CMH, THE NR 2 OIL PRESSURE LIGHT ILLUMINATED AND THE OIL PRESSURE WAS DECREASING. THE CREW SHUT DOWN THE RIGHT ENGINE AND CONTINUED TO CMH. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC PUMP DRIVE SEAL. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T4 TRTA13NM E20NE 19951020003171995102000317 1995 10 20 MALA954633 419950913A3425 AHARS DHAV DHC8 DHC8102 2809003NM NR 2 MALFUNCTIONED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15846MA 344 FLT NR 3320 - IN CRUISE FLIGHT FROM DTW, THE NR 2 ADI AND NR 2 HSI OFF FLAGS APPEARED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE RE-INITIALIZED THE NR 2 AHRS SYSTEM. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951020003181995102000318SW 1995 10 20 MALA954634 119950914A3213 STRUT SWRNGNSA227 SA227AC 8780603SW RT MLG REQ'D SERVICE A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15424MA AC639 FLT NR 3385 - ON CLIMB-OUT FROM YXU, THE GEAR DOOR POSITION WARNING LIGHT ILLUMINATED WHEN RETRACTING THE GEAR. THE LIGHT ALSO ILLUMINATED WHEN THE GEAR WAS EXTENDED ON APPROACH TO DTW. MAINTENANCE SERVICED THE RIGHT MAIN LANDING GEAR STRUT. ALL CHECKS WERE SATISFACTORY. (M) 1L72 4T A8SW 19951020003191995102000319SW 1995 10 20 MALA954638 119950915A57202735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT WING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING SKIN TO NACELLE ATTACH ANGLE, 5TH RIVET FROM THE FORWARD END, IS CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101B. (M) 1L72 4T A8SW 19951020003201995102000320SW 1995 10 20 MALA954639 119950915A57202735112 ANGLE SWRNGNSA227 SA227AC 8780603SW WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD WING TO NACELLE SKIN ATTACH ANGLE CRACKED AT THE 5TH AND 8TH RIVETS. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-28-9101. (M) 1L72 4T A8SW 19951020003211995102000321NM 1995 10 20 MALA954640 119950915A3350 EEL DHAV DHC8 DHC8102 2809003NM FLIGHT DECK INTERMITTENT A MALAK NONE L NO TEST ININSP/MAINT 1 GL15865MA 364 FLT NR 3343 - DURING THE POST FLIGHT INSPECTION IN CWA, THE EMERGENCY LIGHT IN THE FLIGHT DECK WAS FOUND TO BE INTERMITTENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. (M) 2H72 4T RTA13NM 19951020003221995102000322SW 1995 10 20 MALA9546636 119950915A57202735112 ANGLE SWRNGNSA227 SA227AC 8780603SW WING/NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE 10TH RIVET FROM THE FORWARD END. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REVISION 10. (M) 1L72 4T A8SW 19951020003231995102000323WP 1995 10 20 ORJA9575 119950910A801239279623 START VALVE DOUG DC9 DC987 3022087WP NR 2 ENGINE FAILED A ORJAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP11751RA301 49779 RIGHT START VALVE OPEN LIGHT ON IN FLIGHT. RETURNED TO SJC. REMOVED AND REPLACED NR 2 ENGINE START VALVE. OPS AND LEAK CHECK GOOD PER MM 80-10-01. (M) 2L72 4F RTA6WE 19951020003241995102000324WP 1995 10 20 ORJA9582 119950910A5350 FRAME DOUG DC9 DC982 3022082WP BODY FAIRING CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11842RA 49604 FRAME FOR RIGHT BODY FAIRING AFT OF WHEEL WELL HAS MILD CORROSION. CLEANED CORROSION, ALODINED AND PRIMED REF SRM 51-10-3. (M) 2L72 4F A6WE 19951020003251995102000325WP 1995 10 20 ORJA9583 119950910A5350 FRAME DOUG DC9 DC982 3022082WP BODY FAIRING CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11842RA 49604 RIGHT BODY FAIRING FRAME JUST FORWARD OF WHEEL WELL HAS MILD CORROSION. BLENDED MILD CORROSION, FABRICATED DOUBLERS AND INSTALLED WITH REF TO DOUGLAS DC-9 SRM 53-01 PAGE 2, FIG 1 51-10-9 PAGE 1, 51-30-2 PAGE 12. (M) 2L72 4F A6WE 19951020003261995102000326WP 1995 10 20 ORJA9584 119950910A5350 FRAME DOUG DC9 DC982 3022082WP BODY FAIRING CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11842RA 49604 LEFT BODY FAIRING FRAME HAS MILD CORROSION FORWARD LEFT WHEEL WELL. BLENDED MILD CORROSION, FABRICATED DOUBLERS AND INSTALL WITH REF TO DOUGLAS DC-9 SRM 53-01 PAGE 2 FIG 1, 51-10-0 PAGE 1, 51-30-2 PAGE 12. (M) 2L72 4F A6WE 19951020003271995102000327WP 1995 10 20 ORJA9587 119950920A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP COCKPIT DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11823RA 49889 RNO - COCKPIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. OPS CHECK NORMAL. (M) 2L72 4F A6WE 19951020003281995102000328EA 1995 10 20 PLGA91095J 219950911A7230310920901 BEARING BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 1 SPALLED A PLGAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 NE056929M6200 1798 UB27 32165 BOS/BTV - FLT 4330 - DURING CRUISE FLIGHT, CREW EXPERIENCED SEVERAL LOUD BANGS FROM LT ENGINE AS ENG LOST POWER. ITT INCREASED TO 975 DEGREES CELSIUS PLUS & RISING AS OTHER PARAMETERS DECREASED. ENG SHUT DOWN & ACFT DIVERTED TO MHT WHERE UNEVENTFUL SINGLE ENG LANDING MADE. TECHNICIANS DISPATCHED & CONFIRMED GAS GENERATOR SEIZED. ENGINE WILL BE REMOVED & REPLACED FOR FURTHER INVESTIGATION. THIS REPORT CLOSES OUT INITIAL EVENT REPORTED 9-11-95. ENG REMOVED FOR IN-FLIGHT FAILURE & DIRECTED TO REPAIR FACILITY TO DETERMINE CAUSE OF SEIZED GAS GENERATOR. DISASSY REVEALED FAILED NR 1 BEARING. BEARING DIRECTED TO ENG MFG'S LAB & FOUND FAILED DUE ROLLING CONTACT FATIGUE ON BALLS & THRUST RING RACEWAY. (X) 2L72 4T4 TRTA24CE E4EA 19951020003291995102000329NE 1995 10 20 PLGA91195J2 219950910A7250 CARBON SEAL SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE NR 5 FAILED A PLGAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NE05346BE12704 340A150 367384 FLT NR 4899 - YYZ-BDL - THE LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 40 PSI. FLIGHT CREW SHUTDOWN THE ENGINE AND DIVERTED INTO ROC. MAINTENANCE INSPECTED ENGINE AND DETERMINED NR 5 CARBON SEAL FAULTY, WHERE UPON THE POWER TURBINE MODULE WAS REPLACED, REPLENISHED ENGINE OIL AND RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE6 19951020003301995102000330NE 1995 10 20 PLGA91495DM 319950914A6114660710377 CROSSHEAD SAAB SF340 340B 7860101EU ROTOL R354 R3544123F13 NE PROPELLER ASSY WORN A PLGAK NONE K FLUID LOSS ININSP/MAINT 1 NE05351BE 340B237 DRG612287 DURING A ROUTINE INSPECTION, EXCESSIVE BLADE ROTATIONAL PLAY WAS NOTED AND PROPELLER ASSY REMOVED FROM SERVICE FOR REPAIR. AFTER DISASSEMBLY, OIL WAS DISCOVERED IN THE HUB AREA. ALSO, BLADES NR 1, NR 2, AND NR 3 SHOWED EVIDENCE OF GREASE AND OIL EXITING FROM THE SEAM OUTBOARD OF THE OUTER SLEEVE. PROP ASSY WAS SHIPPED TO DOWTY AEROSPACE STERLING FOR OVERHAUL. OPEN PENDING INVESTIGATION FINDINGS. THIS SDR INITIALLY REPORTED EXCESSIVE BLADE ROTATIONAL PLAY FOUND ON THE PROP REFERENCED ABOVE. O/H FACILITY CONFIRMED REPORTED DISCREPANCY. INSP OF ASSY REVEALED 3 OPERATING PINS (PN 660710608), 3 PIN ROLLERS (PN 660712600), AND CROSSHEAD (PN 660710377) WORN BEYOND LIMITS. CONSIDER THIS SDR REPORT CLOSED. (X) 2L72 4T RTA52EU 6 CP61GL 19951020003311995102000331WP 1995 10 20 SRAA99506 119950914A326042028B RELAY DOUG DC8 DC873F 302199FWP LANDING GEAR DEFECTIVE A SRAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19873SJ 46091 FLIGHT 173 - MIAMI - AFTER TAKING OFF, WHEN LANDING GEAR CAME UP AND LOCKED TAKEOFF WARNING HORN CAME ON, AND AIRCRAFT WOULD NOT PRESSURIZE. DUMPED FUEL AND COMPLETED AIR TURN BACK TO MIAMI. TROUBLESHOT SYSTEM AND FOUND GROUND CONTROL RELAY DEFECTIVE. REPLACED RELAY, OPS CHECKED GOOD PER MAINTENANCE MANUAL. (M) 2L74 4F RT4A25 19951020003321995102000332WP 1995 10 20 SRAA99507 119950912A32305714676 LANDING GEAR DOUG DC8 DC873F 302199FWP NLG CORRODED A SRAAK NONE O OTHER UKUNKNOWN 1 SO19873SJ 46091 DURING M-CHECK, FOUND CORROSION AT TOP OF NOSE LANDING GEAR CROSS BRACE SUPPORT, BOLT WAS RUSTED INTO BUSHING. REPLACED NOSE LANDING GEAR ASSEMBLY PERFORMED GEAR RETRACTION, OPS CHECKED GOOD PER MAINTENANCE MANUAL CHAPTER 32. (M) 2L74 4F RT4A25 19951020003331995102000333SO 1995 10 20 SRAA99508 119950921A6120 PROP CONTROL LKHEED382 382G 526414USO NR 1 ENGINE MALFUNCTIONED A SRAAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 SO19920SJ 4561 DURING CLIMB-OUT FOR FLIGHT ADT3 FROM MHZ, NR 1 PROPELLER LOST TORQUE AND TIT WENT TO 1100 DEGREES, NR 1 ENGINE WAS SHUT DOWN AND WHILE FEATHERING PROP, CREW FELT JOLT TO AIRCRAFT, ACCOMPLISHED AIR TURN BACK TO MHZ. THREE ENGINE FERRY AIRCRAFT TO CAMBRIDGE, INSPECTED CAUSE, INGESTION STILL UNDER INVESTIGATION. NR 1 ENGINE, PROPELLER, AND CONTROL ASSEMBLY REPLACED. PERFORMED ENGINE RUN, OPS CHECKED GOOD. (M) 2H74 4T A1SO 19951020003341995102000334WP 1995 10 20 USAA950868 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 1380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND .5 INCH CRACK IN SKIN AT STATION 1380 RIGHT SIDE BETWEEN LONGERON 13R AND 14R. CUT OUT CRACK AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-04 FIG 18. (M) 2L72 4F A6WE 19951020003351995102000335WP 1995 10 20 USAA950869 119950707A5330 SKIN DOUG DC9 DC981 3022081WP BS 1309 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US37810 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND GOUGE .065 BY 1 INCH LONG STATION 1309 LONGERON 29L. NDT CHECK FOR CRACKS AND INSTALLED REPAIR DOUBLER PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19951020003361995102000336WP 1995 10 20 USAA950870 119950707A5320 SUPPORT DOUG DC9 DC981 3022081WP BS 937 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19810US 48042 PIT - DURING Q-1/CX-6 CHECK INSPECTION, FOUND 1 INCH CRACK STATION 937 LEFT AT KEEL TO SADDLE SUPPORT. FABRICATED SUPPORT CHANNEL AND INSTALLED PER SRM 53-05 FIG 81. (M) 2L72 4F A6WE 19951020003371995102000337WP 1995 10 20 USAA950920 119950823A3610 CLAMP DOUG DC9 DC982 3022082WP BLEED AIR DUCT LOOSE A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19818US 48098 CLT - FLT NR 944 - DIVERTED TO CLT DUE TO 2 INCH SPREAD IN THE THROTTLE POSITION. FOUND 8TH AND 13TH STAGE DUCTS CLAMP LEAKING. RETORQUED THE SAME. RAN ENGINE. LEAK CHECKED CLAMPS. CHECKED GOOD. (M) 2L72 4F A6WE 19951020003381995102000338NM 1995 10 20 USAA950971 119950823A5313 STRINGER BOEING737 7373B7 1384580NM BS 352-357 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19385US30420 22958 CLT - DURING DROP-IN CHECK INSPECTION, VISUALLY FOUND A 5 INCH BY 2 INCH CORRODED AREA LOCATED AT S-25RT FROM STATION 352 TO STATION 357. DROP IN AIRCRAFT. CORROSION LEVEL 2. INSTALLED REPAIR ANGLES. (M) 2L72 4F RTA16WE 19951020003391995102000339NM 1995 10 20 USAA950973 119950726A5330 SKIN BOEING737 737301 1384611NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19341US26195 23510 CLT - FOUND TWO CRACKS APPROXIMATELY 4 INCHES LONG LOWER FUSELAGE SKIN, 1 INCH LEFT AND 1 INCH RIGHT OF BL-0, STATION 727 D DIRECTLY BELOW VHF ANTENNA. VISUALLY INSPECTED. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951020003401995102000340WP 1995 10 20 VTZA95307 219950926A732089778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT/RT ENGINE OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27484UE 899 P66204 FLT NR 6352 - IAD-SWF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT ENGINE ONLY MAKING 99 PERCENT RPM AND THE RIGHT ENGINE WOULD ONLY MAKE 99.5 PERCENT RPM ON. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED FUEL CONTROL SCREW 'X' ON BOTH ENGINES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19951020003411995102000341WP 1995 10 20 VTZA95308 219950926A732089778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27484UE 899 P66204 FLT NR 6247 - IAD-BGM - ABORTED TAKEOFF DUE TO THE RIGHT ENGINE NOT MAKING TAKEOFF TORQUE. TARGET TORQUE WAS 100 PERCENT, ACTUAL WAS 96 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED FUEL CONTROL SCREW 'X'. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19951020003421995102000342NM 1995 10 20 WRLA95041 119950925A29136506606 HYD PUMP DOUG MD11 MD11 3023602NM NR 3 ENGINE INOPERATIVE A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27280WA 48458 AS AIRCRAFT TAXIED TO THE RUNWAY AT LAX, THE FLIGHT CREW EXPERIENCED A FAILURE OF THE NR 3 HYDRAULIC SYSTEM. THE CAPTAIN ELECTED TO RETURN TO THE GATE. MAINTENANCE PERSONNEL FOUND THE NR 3 ENGINE DRIVEN LEFT HYDRAULIC PUMP INOP. THE PUMP WAS REMOVED AND REPLACED. AN OPS AND LEAK CHECK WERE PERFORMED SUCCESSFULLY ON THE PUMP IAW MM 29-11-20. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2L73 4F RTA22WE 19951020003431995102000343EU 1995 10 20 WTAA950261 119950908A32307445B RELEASE VALVE BAG JETSTMJETSTM3101 1500215EU LANDING GEAR TRIPPED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17413UE 797 IPL - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR RELEASE VALVE RESET BUTTON POPPED. RESET LANDING GEAR RELEASE VALVE RESET BUTTON. GEAR SWING OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951020003441995102000344EU 1995 10 20 WTAA950262 119950910A32307445B RELEASE VALVE BAG JETSTMJETSTM3101 1500215EU LANDING GEAR TRIPPED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17413UE 797 LAX - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR RELEASE VALVE RESET BUTTON POPPED. RESET LANDING GEAR RELEASE VALVE RESET BUTTON. GEAR SWING OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951020003451995102000345SO 1995 10 20 WTAA950263 119950910A3241 ANTI-SKID EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17216YV 120216 PSP - LEFT ANTI-SKID INOP LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABORTED TAKEOFF WITHOUT INCIDENT. MAINTENANCE DEFERRED ANTI-SKID SYSTEM PER MEL 32-42-2. AIRCRAFT RETURNED TO SERVICE. SUBSEQUENTLY MAINTENANCE CLEARED THE DEFERRAL AFTER ACCOMPLISHING AN INSPECTION OF THE ANTI-SKID SYSTEM WITH NO DEFECTS NOTED AND A SUCCESSFUL COMPLETION OF ANTI-SKID OPERATIONAL CHECK DURING TAXI CHECK. MAINTENANCE WAS UNABLE TO DUPLICATE ORIGINAL DISCREPANCY. (M) 2L72 4T RTA31SO 19951020003461995102000346EU 1995 10 20 WTAA950265 119950914A32609005EN38 SWITCH WIRE BAG JETSTMJETSTM3101 1500215EU RT MLG BROKEN A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17430UE 784 SFO - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT FAILS TO ILLUMINATE DURING GEAR RETRACTION. MAINTENANCE REPAIRED BROKEN WIRE AT RIGHT MAIN LANDING GEAR UPLOCK SWITCH MICROSWITCH, P/N 9005EN38. LANDING GEAR POSITION INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951020003471995102000347NE 1995 10 20 YIEA00395 219950920A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE LEFT FLAMED OUT A YIEAB EMER. DESCENT X ENGINE FLAMEOUT CRCRUISE 1 GL23814AA12615 31 245U139 A/C WAS LVL AT CRUISE OF 35,000 FT, AIRSPEED WAS 200 KTS, OPERATING IN VICINITY OF LIGHT TO MODERATE PRECIP WITH THE ENG ANTI-ICE ON. A/C WAS DIRECTED TO CHANGE HEADING FROM 180 TO 240 DEGREES, WHEN LIGHT TO MODERATE TURBULENCE WAS ENCOUNTERED, AIRSPEED DECREASED TO 180 KTS, WHILE TURNING, LT ENG FLAMED OUT. ADVISED CENTER OF FLAMEOUT AND DESCENDED TO FL 190 WHERE ENG WAS RESTARTED. ENGINE PARAMETERS NORM AND A/C CLIMBED BACK TO FL 310. THE ENG AND NACELLE WAS INSPECTED FOR SIGNS OF DAMAGE, NONE FOUND. THE ENG WAS GROUND RUN AND CHCKD IAW GE MM. ALL PARAMETERS WERE MET, THE A/C RETURNED TO SERV. S/S TURBULENCE WHILE TURNING RT, AND DECREASE IN AIRSPEED 180 KTS, CAUSED ENG FLAMEOUT. (M) 2L72 4F4 F A7EU E7EA 19951020003481995102000348NE 1995 10 20 95ZZZM549 219950926A7200 ENGINE DOUG DC8 DC871 302199AWP GE CFM56 CFM56* 13802NE NR 1 MALFUNCTIONED A RRXAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP158091U 45995 FLT NR 137 - CYYZ-KDAY - NR 1 ENGINE UNSPOOLED IN FLIGHT. MAINTENANCE THOROUGHLY INSPECTED THE NR 1 ENGINE INLET AND EXHAUST AND FOUND NO DAMAGE. FUEL QUANTITY INDICATIONS MATCHED BETWEEN THE INDICATOR AND DRIPSTICKS. MAINTENANCE PERFORMED A POWER ASSURANCE RUN IAW THE EWA RUN UP HANDBOOK. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F4 F 4A25 E2GL 19951020003491995102000349WP 1995 10 20 95ZZZM550 119950921A3231510361C LINK DOUG DC8 DC862 3021970WP NLG DOOR DEFECTIVE A RRXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP15993CF 46028 FLT NR 107 - KAUS-KPIA - ON GEAR RETRACTION SEVERE SHIMMY AND LOUD NOISE WAS EXPERIENCED. AS AIRSPEED INCREASED PROBLEM INCREASED IN NOSE WHEEL WELL AREA. RETURNED TO KAUS. FOUND LEFT FORWARD NLG DOOR IN DOWN POSITION. WOULD NOT LOCK UP. REMOVED AND REPLACED NLG DOOR LOCK LINK. OPS CHECKS GOOD. (M) 2L74 4F 4A25 19951020003501995102000350NM 1995 10 20 AWXA9500645 119950913A5347 SEAT TRACK BOEING737 737277 1384570NM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD GALLEY SEAT TRACK AT STATION 294 RBL 25 CORRODED. INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-10-1, PAGE 5. (M) 2L72 4F RTA16WE 19951020003511995102000351NM 1995 10 20 AWXA9500646 119950913A5314 KEEL BEAM BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C4 INSPECTION, FOUND KEEL BEAM PANEL BETWEEN WHEEL WELL CRACKED IN TWO AREAS. CRACKS APPROXIMATELY ONE INCH IN LENGTH CONFIRMED WITH EDDY CURRENT. REPAIRED IAW ER 2-53-15-28. (M) 2L72 4F RTA16WE 19951020003521995102000352NM 1995 10 20 AWXA9500650 119950921A335020131A EEL BATT PACK BOEING737 7373G7 1384595NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 16 THROUGH ROW 19. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951020003531995102000353NM 1995 10 20 AWXA9500660 119950921A5320 SHEAR TIE BOEING737 737297 1384480NM BS 930 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON SHEAR TIE AT STATION 930, OUTBOARD OF STRINGER 28L IN AFT CARGO PIT. FABRICATED AND INSTALLED SHEAR TIE PER SRM 53-10-4, FIGURE 8. (M) 2L72 4F A16WE 19951020003541995102000354NE 1995 10 20 BUFA9521 219950921A7261 OIL LINE DOUG DC8 DC861 3021952WP PWA JT3D JT3D* 52039NE NR 1 ENGINE LOOSE A BUFAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE05915BV 45981 MROC-MIA - NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON 15 MILES TO MIA. AT FLIGHT IDLE, OIL PRESSURE INDICATOR READ LOW RED LINE. PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE COMPLETED BEFORE LANDING MIAMI. NO EMERGENCY DECLARED, LANDING UNEVENTFUL. FOUND LOOSE MAIN SUPPLY LINE AT MAIN FILTER ASSEMBLY. PROPERLY SECURED AND SAFETIED LINE, SERVICED OIL AND PERFORMED LEAK CHECK ON ENGINE RUN IAW PWA MM 72-00. (M) 2L74 4F4 F 4A25 1E8 19951020003551995102000355NM 1995 10 20 EIAA9541 119950907A291060B0025435 HOSE BOEING747 747121 1384871NM NR 4 HYD SYSTEM RUPTURED A EIAAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09473EV 19657 JFK - AFTER TAKEOFF, NR 4 HYDRAULIC QUANTITY LIGHT ILLUMINATED WITH LOSS OF HYDRAULIC QUANTITY ON GAUGE. FLUID LOSS CONTINUED WITH ADP OPS EDP PLACED IN DEPRESS. FLUID LEVEL STOPPED DECREASE AT 2.9 GALLONS WITH GEAR UP. RETURNED TO JFK, NO FUEL DUMP REQUIRED. WING GEAR EXTENDED BY USE OF ALTERNATE PROCEDURE. FOUND PRESS LINE ADP TO PRESS MODULE BLOWN OUT. REMOVED AND REPLACED LINE, REPLACED FILTERS IN PRESS MODULE AS PRECAUTION, NO EVIDENCE OF CONTAMINATION, PRESS CHECKED OK MM 29-11-00. TEST WING GEAR ALTERNATE EXTENTION ELECTRIC ACTUATOR MM 32-35-01, AIRCRAFT RETURNED TO NORMAL CONFIGURATION. (M) 2L74 4F A20WE 19951020003561995102000356NE 1995 10 20 EIAA9542 219950918A7320786824 PS4 LINE BOEING747 747273C 1384896NM PWA JT9 JT9D7F 52054NE NR 3 ENGINE CRACKED A AEIAAO OTHER J WARNING INDICATION CRCRUISE 1 NM09471EV 20651 686017 HNL - AT CURISE 31.0, EPR DROPPED FROM 1.37 TO 1.16, N1 DECREASED APPROXIMATELY 7 PERCENT, F/F DROPPED FROM 7000 LBS TO 4800 LBS N2, OIL PRESSURE, TEMPERATURE ALL NORMAL. EGT ROSE APPROXIMATELY 60 DEGREES. RETURNED TO HNL. FOUND CRACKED PS4 LINE AT BLEED CONTROL. INSTALLED FLEXIBLE LINE AND FITTINGS TO PS4 LINE WHERE CUT PER ECRA 686017-75-001-3. INSTALLED LINE AND RAN ENGINE. ALL OK. (M) 2L74 4F4 F A20WE E20EA 19951020003571995102000357NM 1995 10 20 EISA95277 119950914A5720 ANGLE BOEING727 727277 138408SNM WS 320 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 LEFT WING LEADING EDGE ANGLE FORWARD OF FRONT SPAR HAS HEAVY CORROSION AT WING STATION 320. SPLICE ANGLE PER SRM 51-40-4. (M) 2L73 4F RTA3WE 19951020003581995102000358NM 1995 10 20 EISA95278 119950914A53156520837 BEAM BOEING727 727277 138408SNM FS 1140 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FLOOR BEAM HAS HEAVY CORROSION FORWARD SIDE FS 1140, RBL 60. REPAIRED BEAM PER SRM 53-10-8, FIG 8. (M) 2L73 4F RTA3WE 19951020003591995102000359NM 1995 10 20 EISA95279 119950914A5320 STIFFENER BOEING727 727277 138408SNM WS 93 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FOUND RIGHT WING LEADING EDGE RIB INBOARD STIFFENER LOWER END CRACKED AT WS 93. REPAIRED STIFFENER PER SRM 51-40-3. (M) 2L73 4F RTA3WE 19951020003601995102000360NM 1995 10 20 EISA95280 119950914A5720 ANGLE BOEING727 727277 138408SNM WS 350 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FOUND RIGHT WING LEADING EDGE UPPER REPAIR ANGLE CRACKED, AFT SIDE OF WING STATION 350. REPLACED ANGLE PER SRM 51-30-2. (M) 2L73 4F RTA3WE 19951020003611995102000361NM 1995 10 20 EISA95281 119950914A5330 SKIN BOEING727 727277 138408SNM FWD ENTRY DOOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FUSELAGE SKIN HAS AN 1.25 INCH LONG CRACK AT TOP HINGE CUTOUT FOR FORWARD ENTRY DOOR. REPAIRED SKIN PER SERVICE BULLETIN 727-53-0198, FIG 3 AND 4. (M) 2L73 4F RTA3WE 19951020003621995102000362NM 1995 10 20 EISA95282 119950914A5720 ANGLE BOEING727 727277 138408SNM WS 130.7 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FOUND 5 CRACKS AT FASTENER HOLES INBOARD END OF LEFT WING LEADING EDGE STATION 130.7 LOWER WEB ANGLE. REPLACED ANGLE PER SRM 51-30-2. (M) 2L73 4F RTA3WE 19951020003631995102000363NM 1995 10 20 EISA95283 119950914A5330 SKIN BOEING727 727277 138408SNM FS 700 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 FOUND 2 CRACKS .5 INCH LONG, FS 700, LBL3, AT RBL 3 EXTERNAL SKIN. REPAIRED SKIN PER SRM 53-30-3. (M) 2L73 4F RTA3WE 19951020003641995102000364NM 1995 10 20 EISA95284 119950914A531565C3355711 FLOOR BEAM BOEING727 727277 138408SNM FS 1176-1179 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION ON CHORD, FLOOR BEAM STATION 1176-1179, LBL 65 (UPPER SIDE). REPAIRED CHORD PER BOEING DRAWING 6563357. (M) 2L73 4F RTA3WE 19951020003651995102000365NM 1995 10 20 EISA95285 119950914A53156520838 FLOOR BEAM BOEING727 727277 138408SNM FS 1130 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION ON FLOOR BEAM FS 1130, LBL 36, LOWER SIDE. REPAIRED BEAM PER DALFORT AVIATION XEA 1-53-688, REVISION 1. (M) 2L73 4F RTA3WE 19951020003661995102000366NM 1995 10 20 EISA95286 119950914A53116520840 FRAME BOEING727 727277 138408SNM FS 1166 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION ON BOLT FRAME, FS 1166, RIGHT AT FLOOR LINE. REPAIRED FRAME PER SRM 51-40-3. (M) 2L73 4F RTA3WE 19951020003671995102000367NM 1995 10 20 EISA95287 119950914A57556517347 SKIN BOEING727 727277 138408SNM RT SPOILER DELAMINATION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 RIGHT WING NR 12 SPOILER SKIN DELAMINATED. REPAIRED SPOILER PANEL PER SRM 57-50-6. (M) 2L73 4F RTA3WE 19951020003681995102000368NM 1995 10 20 EISA95288 119950914A57536521630 SKIN BOEING727 727277 138408SNM LT TE FORE FLAP DELAMINATION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 LEFT INBOARD FORE FLAP LEADING EDGE SKIN DELAMINATED. REPAIRED FLAP PER SRM 57-50-4 AND SRM 51-60-6. (M) 2L73 4F RTA3WE 19951020003691995102000369NM 1995 10 20 EISA95289 119950918A3234 CONNECTOR BOEING727 727277 138408SNM LANDING GEAR DAMAGED A EISAO OTHER J WARNING INDICATION CLCLIMB 1 SW07275WC 20549 GEAR HANDLE WOULD NOT RETRACT PAST 'OFF' POSITION ON DEPARTURE. STRAIGHTENED PIN NR 24 ON D4654P PLUG. OPS CHECKS GOOD IAW MM 32-09-121. (M) 2L73 4F RTA3WE 19951020003701995102000370NM 1995 10 20 IXKA9500028 119950923A27511812993 FLAP POS IND BOEING727 727225 1384077NM TE FLAPS STUCK A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA25353PA 0448AN 20622 FLT NR 80 - ATL - DURING FLAP RETRACTION, OUTBOARD FLAPS STAYED AT 2 DEGREES WHEN FLAPS WERE POSITIONED TO UP. CYCLED FLAPS AND OUTBOARDS STAYED AT 2 DEGREES. RETURNED TO ATL. INSPECTED FLAPS, NO ABNORMALITIES FOUND. REMOVED AND REPLACED OUTBOARD FLAP INDICATOR AND TESTED AS PER MM 27-52-13. CHECKED OK, RESET AND SAFETIED FLAP OVERRIDE SWITCH. (M) 2L73 4F A3WE 19951020003711995102000371WP 1995 10 20 ORJA9580 119950913A3350 EEL DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11843RA 49615 ON PREFLIGHT, EMERGENCY EXIT LIGHTS ON FLOOR ON FIRST CLASS DID NOT ILLUMINATE. INSPECTED EMERGENCY LIGHTS. FOUND MOISTURE IN TRACK. CLEANED AND DRIED ALL CONTACTS IN FIRST CLASS. LIGHT OPS CHECKED GOOD. (M) 2L72 4F A6WE 19951020003721995102000372WP 1995 10 20 ORJA9581 119950912A5350 TAILCONE DOUG DC9 DC982 3022082WP BS 10003 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11842RA 49604 SURFACE CORROSION AFT OF FAIRING UNDER NUT PLATES APPROXIMATELY STATION 10003, RT SIDE. REMOVED LIGHT SURFACE CORROSION AND NUT PLATES FOR INSPECTION. REINSTALLED NUT PLATES TREATED AREA WITH REF TO DOUGLAS DC-9 SRM 51-10-3 PG 12, 13-14-14A. FASTENERS INSTALLATION 51-30-7, PAGE 3-4. (M) 2L72 4F A6WE 19951020003731995102000373WP 1995 10 20 ORJA9585 119950915A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11876RA 53183 RNO - NOTED 4 LIGHTS BURNED OUT, CABIN EMERGENCY LT FLOOR TRACKS ON PREFLIGHT. FOUND BROKEN WIRE BETWEEN FIRST CLASS AND COACH. REPAIRED BROKEN WIRE. SYSTEM OPS CHECKS NORMAL. (M) 2L72 4F RTA6WE 19951020003741995102000374NM 1995 10 20 TA0A099511 119950924A33500L3071BPEGPL EEL LAMP GRIMES BOEING727 727225 1384077NM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 20441 AISLE PATH LIGHTING HAS BULB BURNED OUT AT ROW 17. RELAMPED ROW 17 AISLE PATH LIGHT BULB. OPS CHECKS OK. (M) 2L73 4F A3WE 19951020003751995102000375NM 1995 10 20 TAOA099508 119950919A3350900835A EEL BATT PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 15091 20445 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951020003761995102000376NM 1995 10 20 TAOA099509 119950922A2612106109605 FIRE SENSOR BOEING727 727294 1384088NM NR 1 ENG SHORTED A TAOAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 EA15921TS 3527 22043 FLT NR 6410 - EXPERIENCED A FIRE WARNING INBOUND LGA. THE NR 1 ENGINE WAS SHUT DOWN. FIRE WARNING PERSISTED. DISCHARGED FIRE BOTTLES INTO THE ENGINE, FIRE WARNING STAYED ON. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE. AFTER SHUT DOWN FIRE WARNING STAYED ON. INSPECTION OF THE NR 1 ENGINE REVEALED NO FIRE DAMAGE OR EVIDENCE OF FIRE. THIS SITUATION WAS DETERMINED TO BE A FALSE FIRE WARNING DUE TO A DEFECTIVE FIRE WARNING LOOP. REPLACED THE NR 1 ENGINE FIRE WARNING SENSOR ELEMENT PER MM 26-11-12, SQUIB PER MM 26-21-71, DISCHARGE DISK PER MM 71-00-30, FIRE EXTINGUISHERS AND THE FIRE WARNING CONTROL UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. (M) 0 4 A3WE 19951020003771995102000377NM 1995 10 20 TAOA099510 119950923A32603186301001036 GEAR LIGHT KORRY BOEING727 727225 1384077NM RT MLG FAILED A TAOAK NONE P NO WARNING INDICATION CRCRUISE 1 EA15919TS 20447 DURING GEAR EXTENSION, RIGHT MAIN GEAR GREEN LIGHT WOULD NOT ILLUMINATE UNTIL PRESSED TO TEST. REPLACED RIGHT GEAR GREEN LIGHT ASSEMBLY, OPS CHECKED OK. (M) 2L73 4F A3WE 19951020003781995102000378NM 1995 10 20 TAOA099512 119950926A3350OL3071BPE EEL ASSY GRIMES BOEING727 727227 1384078NM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15924TS 21041 ESCAPE PATH EMERGENCY LIGHT AT ROW 7 INOP. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951020003791995102000379NM 1995 10 20 TWRA9554 119950919A5210 PIN MECHANISM BOEING747 747136 1384883NM R4 DOOR LACK OF LUBE A TWRAK NONE O OTHER TXTAXI/GRND HDL 1 EA15606FF 20273 R4 DOOR WOULD NOT GO INTO AUTO. LUBRICATED TRIGGER PIN MECHANISM AND PIN R4 DOOR OPERATES NORMAL IN ALL FUNCTIONS. (M) 2L74 4F A20WE 19951020003801995102000380GL 1995 10 20 UIEA9505 219950921A73149039M45P07 FUEL PUMP BOEING747 747230B 1384889NM GE CF6 CF650E 30018GL NR 2 ENGINE MALFUNCTIONED A AUIEAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 EA15508MC 21644 517351 AIRCRAFT EXPERIENCED FLAME OUT NR 2 ENGINE TWO HOURS OUT OF ANCHORAGE. PER CREW ALL PARAMETERS DROPPED OFF AND ENGINE SHUT DOWN. ATTEMPTED RESTART UNSUCESSFUL. RETURNED TO ANCHORAGE WITH UNEVENTFUL LANDING. ACCOMPLISH AIRCRAFT HARD LANDING INSPECTION MM 5-51-05 AND ENGINE TROUBLESHOOTING MM 71-00-42. REPLACED MAIN ENGINE CONTROL AND FUEL PUMP. PERFORM GROUND MAX POWER ASSURANCE RUN ENGINE OPERATIONS NORMAL. (M) 2L74 4F4 F A20WE E23EA 19951020003811995102000381EU 1995 10 20 VTZA95303 119950924A277091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GUST LOCK HANDLEOUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27318UE 41041 FLT NR 6577 - IAD-JFK - ABORTED TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING ACTIVATING DURING THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE GUSTLOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951020003821995102000382EU 1995 10 20 VTZA95305 119950922A2450A2105E PDU JETAIRJETSTMJETSTM4101 1500501EU E/E BAY FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27326UE 41064 FLT NR 6416 - IAD-CHS - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE NON ESSENTIAL BUSS FAILING IN FLIGHT. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT POWER DISTRIBUTION UNIT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951020003831995102000383EU 1995 10 20 VTZA95306 119950922A2750TY17604A POTENTIOMETER JETAIRJETSTMJETSTM4101 1500501EU RT TE FLAP OUT OF ADJUST A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27312UE 41025 FLT NR 6306 - IAD-JFK - DURING CRUISE, RETURNED TO IAD DUE TO THE FLAP ASYMMETRY FAULT ACTIVATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE RT FLAP POSITION TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951020003841995102000384EU 1995 10 20 AWXA9500622 119950911A2910NSA5516A6NJ CLAMP AIRBUS320 A320231 3930325EU PTU MANIFOLD BROKEN A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28625AW 064 PHX-MSP - DURING CRUISE AT FL 39,000 FEET, CREW SHUT DOWN GREEN SYSTEM HYDRAULIC PUMP DUE TO GREEN HYDRAULIC RESERVOIR LOW QUANTITY MESSAGE. CREW DECLARED AN EMERGENCY LANDING AND MANUALLY EXTENDED GEAR. LANDING WAS UNEVENTFUL. AIRCRAFT WAS TOWED TO GATE WHERE CONTRACT MAINTENANCE ALSO FOUND TWO CLAMPS BROKEN ON THE SAME LINE. MAINTENANCE TIGHTENED FITTING, REPLACED TWO CLAMPS, AND SERVICED GREEN HYDRAULIC SYSTEM. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19951020003851995102000385NE 1995 10 20 AWXA9500640 219950918A7510567620 ANTI-ICE DUCT BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENGINE BROKEN A AWXAK NONE O OTHER ININSP/MAINT 1 WP28181AW 22648 708365 PHX - DURING ROUTINE MAINTENANCE CHECK FOLLOWING A HIGH EGT EXCURSION, FOUND NR 2 ENGINE 8TH STAGE ANTI-ICE DUCT RUPTURED 1 INCH FORWARD OF AFT MOUNT POINT. ENGINE REMOVED AND REPLACED WITH SERVICEABLE UNIT. (M) 2L72 4F4 FRTA16WE E2EA 19951020003861995102000386SO 1995 10 20 C2XA95IA252 119950922A572012017059009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, UPPER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951020003871995102000387SO 1995 10 20 C2XA95IA253 119950922A572012017059015 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951020003881995102000388SO 1995 10 20 C2XA95IA254 119950922A572012017059017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A RAIAK NONE O OTHER ININSP/MAINT 1 CE0315713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951020003891995102000389SO 1995 10 20 C2XA95IA255 119950922A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 20, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951020003901995102000390EU 1995 10 20 RAIA950906 119950906A3240 BRAKE FLUID BAG JETSTMJETSTM3201 1500217EU LT BRAKE LOW A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03339TE7122 935 STL - FLT NR 7077 - LEFT TOE BRAKE WORKS INTERMITTENTLY. MAINTENANCE SERVICED LEFT PEDAL MASTER CYCLINDER, P/N ACM26810, TAXI CHECK NORMAL. (M) 2L72 4T RTA56EU 19951020003911995102000391EU 1995 10 20 RAIA950907 119950906A3242AC63742 MAXERAT BAG JETSTMJETSTM3201 1500217EU LT MLG FAILED A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03339TE4809 935 STL - FLT NR 7333 - LEFT BRAKE NOT ACTUATING. MAINTENANCE REPLACED LEFT BRAKE MAXERAT. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19951020003921995102000392EU 1995 10 20 RAIA950908 119950905A33503012001 EEL BATTERY AEROSPATR72 ATR72202 8680940EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03721TE9211 1497 217 STL - EMERGENCY LIGHT BATTERY LOW VOLTS. MAINTENANCE REPLACED BATTERY AT ROW 1A/B. (M) 2H72 4T RTA53EU 19951020003931995102000393SO 1995 10 20 RAIA950909 119950909A3240 BOLT EMB 120 EMB120RT SO LT BRAKE LOOSE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03124AM19706305 120016 STL - FLT NR 7016 - BRAKES WILL SOMETIMES JUST RELEASE WHILE TAXIING AND THEN GRAB AGAIN. MAINTENANCE TORQUED AND SAFTIED LEFT BRAKE ASSEMBLY, P/N 214791, MOUNT ATTACH BOLT AS PER EMB MM 32-40-00. TAXI CHECK GOOD. (M) 2L72 4T RTA31SO 19951020003941995102000394EU 1995 10 20 RAIA950910 119950908A52702T2D126 INDICATION RELAY BAG JETSTMJETSTM3201 1500217EU BAGG DOOR FAILED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03871JX4729 871 MRY - FLT NR 4762 - POD DOOR LIGHT ILLUMINATED. MAINTENANCE DEFERRED POD DOOR LIGHT AS PER MEL 52-1, CAT C. SUBMITTER STATES, SUSPECT INDICATION RELAY. (M) 2L72 4T RTA56EU 19951020003951995102000395EU 1995 10 20 RAIA950911 119950909A33503012001 EEL BATT PACK AEROSPATR72 ATR72202 8680940EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE7247 283 STL - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY PACK. (M) 2H72 4T RTA53EU 19951020003961995102000396EU 1995 10 20 RAIA950912 119950909A33500L60424P EEL BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE7247 283 STL - FLT NR 7110 - AFT REAR EMERGENCY LIGHT OUT. MAINTENANCE REPLACED AFT EMERGENCY LIGHT BULB. (M) 2H72 4T RTA53EU 19951020003971995102000397EU 1995 10 20 RAIA950913 119950909A33507012210 EEL BULB AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE K FLUID LOSS TXTAXI/GRND HDL 1 CE032FOR 12645 199 STL - FLT NR 7531 - RIGHT FORWARD TOP EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (M) 2H72 4T RTA53EU 19951020003981995102000398EU 1995 10 20 RAIA950914 119950910A3240215221 BRAKE BAG JETSTMJETSTM3201 1500217EU LEFT REQ'D SERVICE A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03429AM9205 382 879 STL - CAPTAINS AND FLIGHT OFFICERS LEFT BRAKE WEAK. MAINTENANCE BLED LEFT BRAKE ASSY AND PERFORMED OPERATIONAL CHECK TO BE OK. (M) 2L72 4T RTA56EU 19951020003991995102000399EU 1995 10 20 RAIA950915 119950910A3242AC63742 MAXERAT BAG JETSTMJETSTM3201 1500217EU LT MLG FAILED A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03429AM2229 879 STL - FLT NR 7301 - WHILE TAXIING IN, LEFT BRAKE FAILED. MAINTENANCE REPLACED LEFT BRAKE MAXERAT UNTI AS PER J32 M/M 324000. BLEED AND SERVICE LEFT TOE BRAKE. (M) 2L72 4T RTA56EU 19951020004001995102000400EU 1995 10 20 RAIA950916 119950911A3242AC63742 MAXERAT BAG JETSTMJETSTM3201 1500217EU RT MLG WORN A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03423AM9825 858 STL - FLT NR 7475 - RIGHT BRAKE SEEMS SOFT AIRCRAFT PULLS TO THE LEFT WHILE BRAKING. MAINTENANCE CLEANED AND RESEALED MAXERAT ON RIGHT BRAKE. ALL INDICATIONS NORMAL. (M) 2L72 4T RTA56EU 19951020004011995102000401EU 1995 10 20 RAIA950918 119950913A771231024762 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03972JX4550 4550 972 ONT - FLT NR 4769 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19951020004021995102000402EU 1995 10 20 RAIA950920 119950914A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST TXTAXI/GRND HDL 1 CE03426TE 228 STL - FLT NR 7398 - EMERGENCY LIGHTS IN FRONT OF CABIN DO NOT COME ON. MAINTENANCE REPLACED FRONT LIGHT BATTERY (M) 2H72 4T RTA53EU 19951020004031995102000403EU 1995 10 20 RAIA950921 119950915A3222106A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NLG REQ'D SERVICE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03423AM141455645 858 STL - NR 7290 - NOSE GEAR UPLOCK LIGHT ILLUMINATED WOULD NOT EXTINGUISH. MAINTENANCE SERVICED NOSE GEAR STRUT WITH AIR AND FLUID. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19951020004041995102000404EU 1995 10 20 RAIA950922 119950917A77128961153 GASKETS BAG JETSTMJETSTM3201 1500217EU RT ENGINE LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03871JX8253 2153 871 ONT - FLT NR 4769 - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED RIGHT ENGINE BLEED AIR GASKETS. GROUND RUNS CHECK GOOD. (M) 2L72 4T RTA56EU 19951020004051995102000405EU 1995 10 20 RAIA950923 119950916A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE O OTHER ININSP/MAINT 1 CE03422TE4523 106 STL - EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT ROW 8CD. (M) 2H72 4T RTA53EU 19951020004061995102000406EU 1995 10 20 RAIA950924 119950916A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE4523 106 STL - EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT ROW 5CD. (M) 2H72 4T RTA53EU 19951020004071995102000407EU 1995 10 20 RAIA950925 119950916A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE4523 106 STL - EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT ROW 2AB. (M) 2H72 4T RTA53EU 19951020004081995102000408EU 1995 10 20 RAIA950926 119950916A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03422TE4523 620 106 STL - EMERGENCY LIGHTS ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT GALLEY AREA. (M) 2H72 4T RTA53EU 19951020004091995102000409EU 1995 10 20 RAIA950927 119950915A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03426TE9834 228 STL - EMERGENCY LIGHTS IN FRONT OF THE CABIN DO NOT COME ON. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT FRONT CABIN. (M) 2H72 4T RTA53EU 19951020004101995102000410EU 1995 10 20 RAIA950928 119950919A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03424AM1041610416 865 DEC - FLT NR 7285 - RIGHT ENGINE DID NTO MAKE TARGET TORQUE. MAINTENANCE ADJUSTED RIGGING AND RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUNS GOOD. (M) 2L72 4T RTA56EU 19951020004111995102000411EU 1995 10 20 RAIA950929 119950919A215032149602 PACK VALVE AEROSPATR72 ATR72202 8680940EU NR 2 PACK STICKING A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03722TE9108 220 SGF - FLT NR 7019 - DURING PARKING, CABIN FILLED WITH SMOKE. REPLACED RIGHT PACK VALVE. (M) 2H72 4T RTA53EU 19951020004121995102000412EU 1995 10 20 SIMA952621 119950919A261172111211001 SMOKE DETECTOR SAAB SF340 340B 7860101EU AFT CARGO MALFUNCTIONED A SIMAAF UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SW21329AE6152 A4012 340B329 FSM - FLT NR 3690 - AFT CARGO SMOKE WARNING ILLUMINATED IN FLIGHT, BLEW FIRE BOTTLE AND DIVERTED TO FSM. RAI'D SMOKE DETECTOR (GROUND OPS CHECK GOOD) AND REPLACED FIRE BOTTLE. FALSE SMOKE WARNING, NO FIRE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19951020004131995102000413EU 1995 10 20 SIMA952651 119950922A77143039242 PROBE AEROSPATR72 ATR72212 EU NR 1 ENGINE BROKEN A SIMAO OTHER O OTHER CLCLIMB 1 SW21270AT496 CH11949 270 ORD - FLT NR 4043 - NR 1 ENGINE TQ SURGED FROM APPROXIMATELY 40-110 PERCENT, SURGE STOPPED WHEN NP WAS SET TO 100 PERCENT. REPLACED NR 1 ENGINE NH SENSOR, IAW PWA MM, CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M0 2H72 4T RTA53EU 19951020004141995102000414NE 1995 10 20 SIMA952661 219950923A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE NR 2 SEIZED A SIMACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SW21301AE8028 3413 340B301 GEE785328 DFW - FLT NR 3503 - DURING TAKEOFF ENGINE NR 2 LOST POWER, TAKEOFF ABORTED. MAINTENANCE FOUND FIRST STAGE ROTOR DAMAGED. MAINTENANCE REPLACED NR 2 ENGINE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 19951020004151995102000415EU 1995 10 20 SIMA952662 119950923A2910MS219026D FITTING AEROSPATR42 ATR42300 8680920EU PWR BRAKE VLV CRACKED A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21273AT 273 ORD - FLT NR 4246 - LOW LEVEL HYDRAULIC GREEN SIDE IN FLIGHT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND FITTING GOING TO THE INLET PORT OF DUAL POWER BRAKE VALVE CRACKED. REMOVED AND REPLACED NR 6 FITTING AT VALVE. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951020004161995102000416EU 1995 10 20 SIMA952671 119950924A33503011210 EEL AEROSPATR42 ATR42300 8680920EU AIRSTAIR INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21209AT 251 0209 ORD - FLT NR 4265 - PASSENGER AIRSTAIR EMERGENCY LIGHT INOP. RAI'D LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951020004171995102000417EU 1995 10 20 SIMA952672 119950924A33503012001 EEL BATTERY AEROSPATR72 ATR72212 EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21426AT 426 DFW - FLT NR 3829 - EMERGENCY EXIT LIGHT 'DISARM' LIGHT WILL NOT ILLUMINATE ALWAYS WITH SWITCH IN DISARM POSITION. RAI'D BATTERY PACK 43WL, 61WL, 62WL, 73WL. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951020004181995102000418EU 1995 10 20 SIMA952681 119950925A33503011210 EEL ASSY AEROSPATR72 ATR72212 EU AIRSTAIRS CORRODED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21399AT 479 399 ORD - FLT NR 4235 - EMERGENCY LIGHT AT AIRSTAIRS INOP. RAI LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951020004191995102000419NM 1995 10 20 TWAA9571 119950919A3230 RETRACT MECH BOEING727 727231 1384079NM NLG MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION APAPPROACH 1 CE0564346 21633 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, NOSE LANDING GEAR DID NOT EXTEND. CYCLED LANDING GEAR AND NOSE LANDING GEAR EXTENDED NORMAL. JACKED AIRCRAFT AND OPERATED NOSE LANDING GEAR SEVERAL TIMES. NOSE LANDING GEAR OPERATION CHECKED NORMAL, NO MALFUNCTION FOUND. (M) 2L73 4F A3WE 19951020004201995102000420NM 1995 10 20 TWAA9572 119950920A3610600231 GASKETS BOEING727 727231 1384079NM NR 1 ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0554332 20310 STL - DURING CLIMB SHUT DOWN NR 1 ENGINE, S/N 1537, DUE TO STRUT OVERHEAT. FOUND 13TH STAGE AIR LEAK AT WING ANTI-ICE VALVE. REPLACED GASKETS, MFG P/N 60023-1, AT 13TH STAGE VALVE. PERFORMED HIGH POWER RUNUP LEAK CHECK AND OPERATION WAS NORMAL. (M) 2L73 4F A3WE 19951020004211995102000421NM 1995 10 20 TWAA9573 119950923A326069482722 TEST CARD BOEING727 727231 1384079NM LANDING GEAR FAILED A TWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 CE0564315 20048 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, THE GREEN DOWN AND LOCKED INDICATION DID NOT ILLUMINATE. VISUALLY CHECKED, LANDING GEAR WAS DOWN AND LOCKED. FOUND MASTER TEST DIM CAUTION LIGHT CARD MALFUNCTIONING, MFG P/N 69-48272-2. REPLACED MASTER TEST DIM CAUTION CARD AND LANDING GEAR INDICATION SYSTEM CHECKED NORMAL. (M) 2L73 4F A3WE 19951020004221995102000422NE 1995 10 20 TWAA9574 219950925A73213782017 FUEL CONTROL BOEING727 727231 1384079NM PWA JT8 JT8D9 52048NE NR 3 ENGINE FAILED A ATWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE0552310 19829 STL - DURING CLIMB, SHUT DOWN NR 3 ENGINE, S/N 1502, DUE TO ALL PARAMETERS WENT HIGH. FOUND ENGINE FUEL CONTROL SHAFT SHEARED. REPLACED FUEL CONTROL, MFG P/N 378201-7. GROUND RUNUP AND OPERATION CHECKED NORMAL. (M) 2L73 4F4 F A3WE E2EA 19951020004371995102000437CE 1995 10 20 95ZZZX5851 119950921A27529910055 FLAP MOTOR CESSNA500 500CESSNA 2076602CE FLAP FAILED A MDGAK NONE O OTHER ININSP/MAINT 1 SO0910UH 107 5000304 FLAP MOTOR BURNS OUT WHEN GEARBOX FAILS AND TRIPS CIRCUIT BREAKER. THERE ARE TWO MOTORS AND TWO GEARBOX UNITS. WHEN GEARBOX FAILS, THE OPPOSITE MOTOR BURNS OUT TRYING TO CARRY LOAD. 1L72 4F A22CE 19951020004381995102000438NE 1995 10 20 95ZZZX5852 219950830A7200 ENGINE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE RT ENGINE FLAME OUT A BSYAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 GL07121EL 010 251382 RIGHT ENGINE FLAMED OUT AT FL 41,000 FEET. CHECKED ENGINE FOR FOD DAMAGE, TIGHTENED P-3 LINE, RE-ROUTED FUEL CONTROL SENSE LINE. OPS CHECKED GOOD. 2L72 4J4 J A10CE 1E16 19951020004391995102000439CE 1995 10 20 95ZZZX5853 119950727A3260MS6838 LAMP LEAR 35 35A 5170602CE MLG DOWNLOCK INOP A BSYAK NONE O OTHER ININSP/MAINT 1 GL07700SJ 082 NOSE GEAR AND LEFT MAIN GEAR DOWN AND LOCK BULBS INOP. REMOVED AND REPLACED BOTH BULBS. OPS CHECKED GOOD. 2L72 4F A10CE 19951020004571995102000457CE 1995 10 20 95ZZZX5871 119950921A2750556517531 GEARBOX CESSNA500 500CESSNA 2076602CE FLAP STRIPPED A MDGAK NONE O OTHER ININSP/MAINT 1 SO0910UH 107 5000304 FLAP GEARBOX INTERNAL GEAR STRIPPED OUT. SUBMITTER STATED THIS IS AN ONGOING PROBLEM. ALSO, WRITTEN UP IN CESSNA SERVICE MANUAL. 1L72 4F A22CE 19951020004671995102000467CE 1995 10 20 95ZZZX5881 119950727A243430B10719A GENERATOR BENDIX LEAR 35 35A 5170602CE RT ENG STATOR FAILED ALABKAAE ENGINE SHUTDOWN EJHVIBRATION/BUFFET WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 SO1386BE 1543 2171 194 RT ENGINE STARTED A SEVERE VIBRATION AND DC GENERATOR FAIL LIGHT CAME ON. TEMP RISING (OIL). SHUT DOWN ENGINE. TEAR DOWN REPORT FOUND EXPLODED STATOR WINDING. SWELLING OF THE WINDING MADE THE ROTOR BIND AND RUB AND CAUSED THE HOUSING TO BREAK. BOTH BEARINGS ARE IN GOOD CONDITION. 2L72 4F A10CE 19951020004711995102000471EA 1995 10 20 95ZZZX5885 219950815A8530 RING PIPER PA28 PA28236 7102815SO LYC O540 O540J3A5 41532EA NR 4 CYL BROKEN AL DAMAK NONE O OTHER ININSP/MAINT 1 EA178107B 288011013 L2194140A DURING ANNUAL INSPECTION, FOUND NR 4 CYLINDER LOW COMP. (170 HR SMOH). INVESTIGATION FOUND TOP COMP RING BROKEN AND UNUSUAL WEAR ON RINGS. RINGS WORN TO A BEVEL EDGE DOWN OVER RING LANDS. CHECKED ALL CYLS AND FOUND SAME WEAR AND SOME BROKEN RINGS. ENG HAD BEEN OVERHAULED WITH CERMA CHROME CYLINDERS. 1L71 3O3 O 2A13 E295 19951020004751995102000475WP 1995 10 20 9515959752 119950927A5320 SUPPORT DOUG DC9 DC941 302207NWP FS 229-250 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND CORROSION IN THE CENTER LINE FLOOR SUPPORT CAP FS 229 TO 250. REPAIRED CAP (P/N 5910137-9), PER EA 97-103281. 2L72 4F A6WE 19951020004761995102000476NM 1995 10 20 9515962290 119950928A5312 BLKHD DR FRAME BOEING727 727251 138408HNM FS 1183 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01290US 21378 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD DOOR FRAME WEB AT THE FLOOR LEVEL FS 1183, LBL 18. REPAIRED FRAME (P/N 65-16350-299) PER EA 22-99355. 2L73 4F A3WE 19951020004771995102000477WP 1995 10 20 9515979855 119950929A5313 LONGERON DOUG DC9 DC951 3022051WP FS 873 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND CORROSION ON LONGERON 30 AT FS 873. REPAIRED LONGERON (P/N 5924878-503), PER EA 98-102581. 2L72 4F A6WE 19951020004781995102000478NM 1995 10 20 9515985501 119950929A5315 FLOORBEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01501US 23190 DURING T-CHECK, FOUND CORROSION ON THE FS 365 FLOORBEAM UPPER CHORD FROM RBL 1 TO 62. REPAIRED BEAM (P/N 141N5112), PER EA 55-99005. 2L72 4F RTA2NM 19951020004791995102000479EU 1995 10 20 9515993209 119950929A5320 SUPPORT AIRBUS320 A320211 3930320EU FS 31577-32571 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309US 118 DURING IL CHECK, FOUND CORROSION ON THE FLOOR SUPPORTS AT Y=+- 1929 FRAME 66 TO 68. REPAIRED SUPPORTS PER EA 32-99197. 2L72 4F RTA28NM 19951020004801995102000480WP 1995 10 20 95160098 119950930A5311 FRAME DOUG DC9 DC951 3022051WP FS 1209 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND TWO CRACKS IN THE FS 1209 FRAME SHEAR WEB BETWEEN LONGERONS 11R TO 12R. REPAIRED WEB (P/N 9912246-17), PER EA 98-102588. 2L72 4F A6WE 19951020004811995102000481WP 1995 10 20 9516019752 119951002A5320 INTERCOSTAL DOUG DC9 DC941 302207NWP FS 148 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND A CRACK IN THE SERVICE DOOR JAMB TO COCKPIT LOWER SILL INTERCOSTAL FS 148. REPAIRED INTERCOSTAL (P/N 911557-3), PER EA 97-101985. 2L72 4F A6WE 19951020004821995102000482WP 1995 10 20 9516029153 119951003A5720 FITTING DOUG DC9 DC914 3022034WP FS 69 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING MAINTENANCE INSPECTION, FOUND A CRACK IN THE LOWER FOOT FITTING FS 69 BETWEEN CENTER WING STRINGERS 11 AND 12. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19951020004831995102000483WP 1995 10 20 9516039752 119951003A5220 DOOR PAN DOUG DC9 DC941 302207NWP EMERG EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND A CRACK IN THE FORWARD RIGHT EMERGENCY EXIT DOOR PAN AT THE UPPER EDGE. REPAIRED PAN (P/N 5913195-1), PER EA 99-103287. 2L72 4F A6WE 19951020004841995102000484WP 1995 10 20 9516049752 119951003A5220 DOOR PAN DOUG DC9 DC941 302207NWP EMERG EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND A CRACK IN THE FORWARD LEFT EMERGENCY EXIT DOOR PAN UPPER EDGE. REPAIRED PAN (P/N 5913195-1), PER EA 97-102583. 2L72 4F A6WE 19951020004851995102000485WP 1995 10 20 9516059949 119951006A5320 FITTING DOUG DC9 DC931 3022065WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT AND RIGHT KEEL FITTINGS LONGERON 30 AT FS 604. REPLACED FITTINGS (P/N 3924029-1, -2), PER SRM 51-01. 2L72 4F A6WE 19951020004861995102000486WP 1995 10 20 9516069949 119951006A5320 FITTING DOUG DC9 DC931 3022065WP FS 579-598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 30 END FITTING AT FS 579 TO 598. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19951020004871995102000487WP 1995 10 20 9516079907 119951007A5320 FITTING DOUG DC9 DC931 3022065WP CARGO DOOR STOP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01957N 47253 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO UPPER AFT DOOR STOP FITTING. REPLACED FITTING PER MM 52-31-0. 2L72 4F A6WE 19951020004881995102000488WP 1995 10 20 9516089938 119951007A5330 SKIN DOUG DC9 DC931 3022065WP FS 1121 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011798U 47369 DURING L-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1121 ABOVE THE RIGHT PYLON TRAILING EDGE. REPAIRED SKIN (P/N 5912870-501), PER EA 99-102592. 2L72 4F A6WE 19951020004891995102000489NM 1995 10 20 9516096638 119951009A5280 DOOR FITTING BOEING747 747251B 1384892NM LT MLG DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01638US 23549 DURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT BODY MAIN LANDING GEAR OUTBOARD DOOR TO THE ACTUATING LINK FITTING. REPLACED FITTING. 2L74 4F A20WE 19951020004901995102000490WP 1995 10 20 9516109949 119951010A5320 FITTINGS DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT FS 996 UPPER TO LOWER FRAME ATTACH FITTINGS. REPLACED FITTINGS PER SRM 51-01 AND DWG 5913700. 2L72 4F A6WE 19951020004911995102000491EU 1995 10 20 9516113210 119951012A5320 FITTING AIRBUS320 A320211 3930320EU 4L DOOR FRAME CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01310NW 121 DURING IL CHECK, FOUND CORROSION ON THE 4L DOOR FRAME CORNER FITTING. REPLACED FITTING. 2L72 4F RTA28NM 19951020004921995102000492WP 1995 10 20 9516159882 119951016A32600080004003 PROX CONTROL BOX DOUG DC9 DC951 3022051WP LANDING GEAR MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01670MC2662524941 47659 DURING CLIMBOUT, ALL THREE LANDING GEAR RED UNSAFE LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED, RECYCLED GEAR WITH NO HELP. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY CONTROL BOX. OPERATIONAL CHECK OK ON GEAR SWING AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951020004931995102000493WP 1995 10 20 9516169921 119951016A3260 UP LIMIT SWITCH DOUG DC9 DC932 3022066WP LT MLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01943N 47647 DURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR UP LIMIT SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951020004941995102000494EU 1995 10 20 9516173202 119951015A2150 PACK AIRBUS320 A320211 3930320EU RIGHT OVERHEATED A NWAAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01302US 32 DURING CRUISE, THE RIGHT PACK OVERHEATED FOLLOWED BY SMOKE AFT CARGO SMOKE WARNING, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. THE WARNING INDICATION EXTINGUISHED APPROXIMATELY FIVE MINUTES AFTER THE FIRE BOTTLE WAS DISCHARGED. AIRCRAFT DIVERTED TO RNO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO EVIDENCE OF FIRE IN THE AFT CARGO COMPARTMENT. THE RIGHT PACK AND AFT CARGO FIRE EXTINGUISHER WERE PLACED ON MEL. 2L72 4F RTA28NM 19951020004951995102000495WP 1995 10 20 9516189921 119951016A3230 UP LATCH ASSY DOUG DC9 DC932 3022066WP LT MLG MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01943N 46747 DURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR UPLATCH ASSEMBLY. OPERATIONAL CHECK GOOD ON GROUND AND ON TEST FLIGHT. 2L72 4F A6WE 19951020004961995102000496EU 1995 10 20 95FDEA01549 119951006A5400 HEAT SHIELD AIRBUS310 A310203 EU NR 1 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25401FE 1941 NR 1 PYLON HEAT SHIELD IS CRACKED FWD OF PRECOOLER AIR DUCT, GI 44B0517 NR NR0009. 2L72 4F RTA35EU 19951020004971995102000497NM 1995 10 20 95FDEA01550 119951017A5320 ANGLE BOEING727 72725C 138400HNM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 FWD 2 HOLES IN LT CHORD ANGLE AT STA 760 SHOW CRACKS. REPAIR COMPLETED PER EA 7-5710-25838. 2L73 4F A3WE 19951020004981995102000498NM 1995 10 20 95FDEA01551 119951017A5712 RIB BOEING727 72725C 138400HNM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25135FE 19853 FWD UPPER HOLE AT 12 O'CLOCK ON THE RT RIB CHORD AT STA 760 IS CRACKED. REPAIRED PER EA 7-5710-25838 DATED 10-11-95. 2L73 4F A3WE 19951020004991995102000499NM 1995 10 20 95UAL900200 119951016A493038834123 SEAL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE APU FUEL CONTL STICKING A UALAK NONE L NO TEST ININSP/MAINT 1 WP29656UA 25394 61779 FOUND FUEL IN APU OIL SYSTEM AND REPLACED APU PRECAUTIONARY. FUEL CONTROL WAS DISASSEMBLED AND CARBON SEAL ON THE SIDE OF THE FUEL CONTROL SHAFT SEAL WAS FOUND STICKING. SEAL WAS REPLACED. 2L72 4F4 FRTA1NM E24NE 19951020005001995102000500NE 1995 10 20 95UAL900201 219951016A72501B4921 TURBINE BLADE BOEING757 757222 1384956NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 WP29576UA 26690 726693 DURING CLIMBOUT, LEFT ENGINE HAD A COMPRESSOR STALL WITH RISING EGT, MAXIMUM 657C. POWER WAS REDUCED TO IDLE AND EGT STABLIZED AT 550C, RETURNED TO DEN. INSPECTED ON GROUND, FOUND METAL IN THE TAILPIPE. ENGINE DISASSEMBLY FOUND A FAILED T-1 HIGH PRESSURE TURBINE BLADE. 2L72 4F4 FRTA2NM E17NE 19951020005011995102000501NM 1995 10 20 95UAL900202 119951016A5330 SKIN BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP297285U 21563 AFT LEFT SIDE OF FUSELAGE, NEXT TO VHF ANTENNA IS CRACKED AND SHOWS EVIDENCE OF CORROSION. REPAIRED CORROSION DAMAGE PER SRM 53-10-03 FIG 1 AND 3. 2L73 4F4 F A3WE E2EA 19951020005021995102000502NM 1995 10 20 95UAL900203 119951016A3350 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29577UA 26693 SLIDE EMERGENCY LIGHT INOP AT DOOR ONE LEFT. RELAMPED, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951020005031995102000503NE 1995 10 20 95UAL900204 219951016A723053A301 FAN BLADE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE LT ENGINE BENT A UALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP29653UA 2770 25391 717542 POSSIBLE BIRD STRIKE/INGESTION IN LEFT ENGINE, HAD UNUSUAL NOISE AND VIBRATION DURING CLIMB, RETURNED TO LHR. FOUND TWO FAN BLADES WITH BENT LEADING EDGES AT BLADE MID SPAN. REPLACED BENT BLADES AND THEIR MATCHING PAIRS. 2L72 4F4 FRTA1NM E24NE 19951020005041995102000504GL 1995 10 20 95UAL900205 219951016A7321 FUEL CONTROL WOODWARD GOV180327 DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 ENGINE FAILED A UALAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 WP291838U 46632 IAD - ON DESCENT, THE NR 2 ENG FAILED. PER CREW, ACCOMPLISHED ENG SHUTDOWN PROCEDURE AND NO ABNORMAL INDICATIONS OCCURRED. NR 2 ENG DID NOT RESPOND TO THROTTLE, SHUTDOWN NR 2 ENG PER FLAME-OUT PROCEDURES. DISASSEMBLEY OF THE MAIN FUEL CONTROL REVEALED THE DIFFERENTIAL PRESSURE PLUNGER BEARING FAILED ALLOWING TWO OF THE BALLS TO FALL DOWN AND JAM THE PLUNGER. THIS TYPE FAILURE HAS NOT HAPPENED BEFORE ON UNITED AIRCRAFT, ORIGINAL EQUIPMENT MANUFACTURER WILL BE CONTACTED. 2L73 4F4 F A22WE E23EA 19951020005051995102000505NM 1995 10 20 95UAL900206 119951016A2120 AIR DISTR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN ODOR A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 WP297289U 21567 ON TAKEOFF, CABIN SMOKE HEAVY WITH ODOR LIKE FLUID SMOKING. SMOKE DISSIPATED IN FLIGHT AFTER 10 MINUTES. ON LANDING AT HIGH THRUST, ODOR CAME BACK. 2L73 4F4 F A3WE E2EA 19951020005061995102000506NM 1995 10 20 95UAL900207 119951016A33506013211LB BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297263U 21410 FWD GALLEY DOOR EVACUATION SLIDE EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19951020005071995102000507WP 1995 10 20 95UAL900208 119951016A2150AR20497011 ACM AIRESRCH DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 MALFUNCTIONED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291833U 47965 HOT BURNING AIR SMELL IN CABIN WITH PACKS ON. UNABLE TO ISOLATE SOURCE. PASSENGERS REPORTING BURNING EYES, NAUSEA, ETC. REPLACED NR 1 AIR CYCLE MACHINE AND ALL 3 COALESER BAGS. NO DEFECTS NOTED IN SHOP. 2L73 4F4 F A22WE E23EA 19951020005081995102000508NE 1995 10 20 95UAL900209 219951017A753232144464 VALVE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE NR 2 ENGINE STICKING A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29352UA 24320 ABORTED TAKEOFF AT LGA AT 75 KNOTS DUE TO NR 2 ENGINE BLEED PROBLEM. REPLACED NR TWO ENGINE HIGH-STAGE VALVE. ALSO, REPLACED NR ONE ENGINE HIGH-STAGE VALVE AND REGULATOR. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951020005091995102000509NM 1995 10 20 95UAL900210 119951017A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29385UA 24660 EMERGENCY EGRESS LIGHTING AT SEAT ROW 3 INOPERATIVE. INSTALLED LIGHT STRIP, TESTS OK. 2L72 4F4 FRTA16WE E2GL 19951020005101995102000510NM 1995 10 20 95UAL900211 119951017A3320BV03031D078 SOCKET BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE GALLEY BURNED A UALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP299071U 19952 BURNING ELECTRICAL SMELL FROM AFT GALLEY AREA. SMELL DISSIPATED WHEN FLUORESCENT OVERHEAD LIGHTS AT GALLEY TURNED OFF. REPLACED LAMP HOLDER SOCKET, WIRES AND LAMPS. CHECKS O.K. 2L72 4F4 F A16WE E2EA 19951020005111995102000511NM 1995 10 20 95UAL900212 119951017A2560 SLIDE PRESS BOEING737 737291 138448WNM PWA JT8 JT8D9A 52048NE DOOR 1L LOW A UALAK NONE O OTHER ININSP/MAINT 1 WP29981UA 21546 DOOR 1 LEFT EVACUATION SLIDE PRESSURE INDICATING IN RED, APPROX 2,800 PSI. SERVICED PER MAINTENANCE MANUAL. 2L72 4F4 F A16WE E2EA 19951020005121995102000512NM 1995 10 20 95UAL900213 119951017A2781655280739 POS IND UNIT BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE LE FLAP INTERMITTENT A UALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP29382UA 24657 ABORTED TAKEOFF AT ORD AT 90 KNOTS DUE TO TAKEOFF WARNING HORN. REPLACED THE LEADING EDGE FLAP/SLAT POSITION INDICATING UNIT. TAKEOFF WARNING SYSTEM CHECKED O.K. NO FAULTS WERE FOUND WITH THE INDICATOR DURING OVERHAUL. 2L72 4F4 FRTA16WE E2GL 19951020005131995102000513NM 1995 10 20 95UAL900214 119951017A2760658420921 MODULE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE SPEED BRAKE MALFUNCTIONED A UALAO OTHER J WARNING INDICATION LDLANDING 1 WP29388UA 24663 SPEED BRAKE DID NOT DEPLOY ON LANDING WITH SPEED BRAKE ARMED LIGHT ON. MANUALLY WOULD ONLY DEPLOY TO FLIGHT POSITION. REPLACED THE AUTO SPEED BRAKE ACCESSORY MODULE PER MM 27-62-35. CHECKS O.K. THE MODULE WAS ROUTED TO THE SHOP WHERE NO FAULTS WERE FOUND. 2L72 4F4 FRTA16WE E2GL 19951020005141995102000514WP 1995 10 20 ABXA9500824 119951013A78304310001 TR UNIT DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE DEFECTIVE A ABXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 GL23945AX 47551 674385 JOLT FELT IN FLIGHT AT 13,000 FEET, ENGINE INSTRUMENTS NORMAL, NO COCKPIT INDICATION OF MALFUNCTION. CARGO INSPECTED IN FLIGHT BY FIRST OFFICER. EMERGENCY DECLARED FOR LANDING. LANDING NORMAL, EXCEPT LEFT ENGINE THRUST REVERSER DID NOT GET BLUE LIGHT. INSPECTION IN BLOCKS SHOWED LEFT THRUST REVERSER DAMAGE. INSPECTED NR 1 ENGINE, FOUND NR 1 THRUST REVERSER UPPER DOOR DEPLOYED. BOTH UPPER AND LOWER DOORS DAMAGED. ALSO, DAMAGE TO THE NR 1 PYLON AT THE AFT LOWER ENGINE MOUNT AREA. REMOVED NR 1 ENGINE TO FACILITATE PYLON REPAIR, THEN REINSTALLED ENGINE AFTER REPAIR, REF M17 WORKPACK. REPLACED NR 1 THRUST REVERSER ASSEMBLY AND OPS CHECKED GOOD ON GROUND RUN. 2L72 4F4 F A6WE E2EA 19951020005151995102000515NM 1995 10 20 DL72E953991 119951011A5744 FITTING BOEING727 727247 138408FNM NR 4 FLAP TRACK CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 FOUND AT HMV, FRETTING CORROSION ON I/B FACE OF LT MLG PORK CHOP FITTING AT FLAP TRACK ATTACH HOLE. REPAIRED PER MM 57-42-0 PG 814. 2L73 4F A3WE 19951020005161995102000516NM 1995 10 20 DL72E954015 119951002A5320 WEB BOEING727 727247 138408FNM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 LT ABOVE S-DUCT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19951020005171995102000517NM 1995 10 20 DL72E954016 119951002A5320 WEB BOEING727 727247 138408FNM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND .5 INCH CRACK IN WEB AT STA 1303 RT SIDE ABOVE S-DUCT. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19951020005181995102000518NM 1995 10 20 DL72E954017 119951002A5320 WEB BOEING727 727247 138408FNM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND .5 INCH CRACK IN LT TORQUE BOX WEB IN 48 SECT STA 1223 AT UPPER RIVET ROW. FABRICATED AND INSTALLED REPAIR PER MM 53-11-0 PG 833. 2L73 4F A3WE 19951020005191995102000519NM 1995 10 20 DL72E954022 119951003A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19951020005201995102000520NM 1995 10 20 DL72E954023 119951003A5530 WEB BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND WEB CRACKED VERT STAB INT STA 1303. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 53-10-4 FIG 17. 2L73 4F A3WE 19951020005211995102000521NM 1995 10 20 DL72E954024 119951002A7110 SKIN BOEING727 727247 138408FNM NR 2 ENG INLET CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND SKIN CRACKED NR 2 ENG INLET AT 3 O'CLOCK POS, 10 INCHES AFT OF LIP. FABRICATED AND INSTALLED NEW REPAIR PER MM 54-30-0 PG 801. 2L73 4F A3WE 19951020005221995102000522NM 1995 10 20 DL72E954027 119951011A5743 BUSHING BOEING727 727247 138408FNM NR 4 FLAP TRACK LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND BUSHING LOOSE IN LT MLG PORK CHOP FTG IN AFT HOLE FOR NR 4 FLAP TRACK. REPAIRED AND INSTALLED NEW BUSHING PER MM 57-42-0. 2L73 4F A3WE 19951020005231995102000523NM 1995 10 20 DL72L954033 119950922A5330 SKIN 6554577 BOEING727 727232 1384082NM FS 720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11507DA 21309 FUSELAGE SKIN, FS 720 TO 720B S-26R BL 0, CORROSION REPAIR. CORROSION ON THE LOWER SKIN PANEL REQUIRED CUT OUTS IN FOUR AREAS LOCATED FROM FS 720 + 10 TO 720B BETWEEN STRINGERS 26R AND BL 0. TWO OF THE CUT OUTS ARE UNDER THE LAPPED SKIN AT STRINGER 26R. THE FORWARD CUTOUT IS 2.25 BY 1 AND THE AFT IS 2.25 BY 2. THE THIRD IS 16 BY 5.375 LOCATED JUST FORWARD OF STA 720A BETWEEN STRINGERS 28R AND BL 0, THE FOURTH CUTOUT IS 2.75 BY 1.125 AND IS AFT OF STA 720A BETWEEN STRINGER 28R AND BL 0. THIS REPAIR REMOVED THE EXISTING EXTERNAL RING DOUBLER AND ADDED A DOUBLER AND A TRIPLER. 2L73 4F A3WE 19951020005241995102000524NM 1995 10 20 DL72S953982 119951012A52406556150137 DOOR BOEING727 727232 1384082NM R 1 DOOR CRACKED A DALAK NONE O OTHER CRCRUISE 1 SO11496DA 21076 A FIVE INCH CRACK WAS FOUND IN THE R-1 DOOR. THE CRACK EXTENDED FROM THE UPPER AFT CORNER DOWN THE AFT FRAME. REPAIR INCLUDED DOOR REPLACEMENT. 2L73 4F A3WE 19951020005251995102000525NM 1995 10 20 DL72S953989 119951012A3350 EEL BATTERY PACK 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11404DA 21148 LEFT CENTER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AT M954, OPERATION NORMAL. 2L73 4F A3WE 19951020005261995102000526NM 1995 10 20 DL72S953990 119951012A5320 ANGLE BOEING727 727232 1384082NM RT WHEEL WELL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11498DA 21142 FOUND DURING F-1 LETTER CHECK, .25 INCH CRACK IN RADIUS FROM UNDER BLOCK STA 910 RT MLG UPLOCK H-BRACKET FWD SUPPORT ANGLE. REPAIRED PER M/M 53-11-0 PG 834 AND 835. 2L73 4F A3WE 19951020005271995102000527NM 1995 10 20 DL72S953996 119951013A2130 FLOW CNTL VLV 39854021 BOEING727 727232 1384082NM CABIN FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11523DA P1139 21583 RIGHT PACK FAILED IN FLIGHT AT FL 250. AIRCRAFT LOST PRESSURIZATION, LT PACK ON MCO. REPLACED AFT FLOW CONTROL VALVE, OPERATION NORMAL. 2L73 4F A3WE 19951020005281995102000528NM 1995 10 20 DL72S954009 119950921A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ATL - HMV, ANGLE CRACKED NR 2 K-FLAP ACT MOUNT, INBD LOWER ANGLE IS CRACKED. REMOVED ANGLE, STOP DRILLED CRACK, DRILLED REPAIR DOUBLER PER MM 57-20-21 PG 811 AND INSTALLED REPAIR DOUBLER PER MM 57-20-21. 2L73 4F A3WE 19951020005291995102000529NM 1995 10 20 DL72S954010 119950922A5754 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ATL - HMV, RIB CRACKED NR 7 LE SLAT NR 10 RIB CRACKED ON TOP FLANGE. ROUTED OUT DAMAGE AND FABRICATED DOUBLER PER MM 57-54-0 PG 819. FABRICATED FILLER, INSTALLED DOUBLER AND FILLER PER M/M 57-54-0 PG 819. 2L73 4F A3WE 19951020005301995102000530NM 1995 10 20 DL72S954035 119950928A5730 SKIN 651855210 BOEING727 727232 1384082NM FS 761 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 WING SKIN, CENTER TANK UPPER SKIN STA 761 LBL 65, TWO EXISTING FASTENER HOLES IN THE WING CENTER SECTION UPPER PANEL WERE DAMAGED ON THE UNDERSIDE REQUIRING OVERSIZING. THE TWO HOLES ARE LOCATED AT FS 761 AT APPROX LBL 65. THE REPAIR OVERSIZES BOTH HOLES IN THE WING SKIN ONLY AND INSTALLS INTERFERENCE FIT BUSHINGS. 2L73 4F A3WE 19951020005311995102000531NM 1995 10 20 DL72S954036 119950920A5330 SKIN BOEING727 727232 1384082NM FS 700-720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 BELLY SKIN, CORROSION AT STA 700 TO 720, O/B OF S-28L AD 91-09-09, 94-05-04. SKIN CORROSION AT STA 700 TO 720, O/B OF S-28L HAS PROMPTED REQUEST FOR AN EXTENSION OF AN EXISTING DOUBLER IN THAT AREA TO COVER THE ADDED DAMAGE REMOVAL, APPROXIMATLY 2 BY 2 INCHES. THE ERA WILL INCORPORATE THE ADDED CUT OUT INTO THE PREVIOUS REPAIR. 2L73 4F A3WE 19951020005321995102000532NM 1995 10 20 DL72W954002 119951014A3350 EEL BATTERY PACK 900835A BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112814W WA6707 20870 717138 LT AFT OVER WING EMERGENCY LIGHT INOP. REPLACED LEFT OVER WING BATTERY PACK, OPS CHECK NORMAL. 2L73 4F4 F A3WE E2EA 19951020005331995102000533NE 1995 10 20 DL72W954005 219951015A7310 FUEL HEAT VLV 320115 BOEING727 727247 138408FNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SO11293WA 21480 22111 700534 NR 1 FUEL HEAT VALVE FAILED OPEN AFTER TAKEOFF, OIL TEMP HIT 120 DEGREES CENT, PULLED FUEL DE-ICE C/B. REPLACED FUEL HEAT VALVE, OPS CKS OK. 2L73 4F4 F A3WE E2EA 19951020005341995102000534NM 1995 10 20 DL72W954040 119951015A3350 BATTERY PACK 1000677 BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112807W 3868 20579 FWD RT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED RACK AND BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19951020005351995102000535NM 1995 10 20 DL72W954041 119951016A335037067001 BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112807W 20579 AFT RIGHT SERVICE DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, CHECKS NORMAL. 2L73 4F A3WE 19951020005361995102000536 1995 10 20 DL733954001 419951014A22102589124902 RATE GYRO 4030952906 BOEING737 737347 1384647NM YAW DAMPER FAILED BEARINGS A DALAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SO11303WA 88032775 23183 AT FLT LEVEL 230 WITH 'B' A/P ENGAGED AN UNCOMMANDED RUDDER INPUT OCCURED, JUST PRIOR THE MASTER CAUTION LIGHT WAS ILLUMINATED BY THE MACH TRIM FAIL LIGHT. YAW DAMPER INDICATOR ON FWD PANEL SHOWED FULL RT DEFLECTION. YAW DAMPER WAS TURNED OFF, MACH TRIM FAIL LIGHT EXTINGUISHED, THEN CAME BACK ON MOMENTARLY THEN REMAINED EXTINGUISHED. RECOVERY FROM UNCOMMANDED RUDDER INPUT REQUIRED ABOUT .5 TO .75 LT RUDDER DEFLECTION. RETURNED TO DFW WITH NO FUTHER UNCOMMANED RUDDER INPUT. INVESTIGATION FOUND MECHANICAL FAILURE OF RATE GYRO IN THE YAW DAMPER COUPLER. 2L72 4F RTA16WE 19951020005371995102000537NM 1995 10 20 DL73S953992 119950916A53156545410223 FLOORBEAM BOEING737 737232 1384475NM FS 662 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11303DL 23075 DURING CORROSION VISIT, FOUND THE BL 0 FLOORBEAM OF THE WING CENTER SECTION CRACKED AT FS 662. THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED THROUGH, INCLUDING TWO FASTENER HOLES. ACCOMPLISHED REPAIRS PER SB 737-57-1210. 2L72 4F RTA16WE 19951020005381995102000538NM 1995 10 20 DL73S954032 119950914A5315 FLOORBEAM 6545410515 BOEING737 737232 1384475NM FS 661 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11331DL 23103 THE BL 0.07 FLOORBEAM OF THE WING CENTER SECTION IS CRACKED AT STA 661 AND THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED THROUGH, INCLUDING TWO FASTENER HOLES. THIS AREA WILL BE TRIMMED OUT. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210, ER/A 302502-14 INSTALLED THE SERVICE BULLETIN REPAIR FOR THE CONDITION. 2L72 4F RTA16WE 19951020005391995102000539NM 1995 10 20 DL757954013 119950830A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11633DL 23614 RADOME WAS REMOVED FOR MOISTURE. SHOP INSPECTION FOUND OLD REPAIRS TO BE OF WET-LAY REPAIRS. CUT OLD SHELL OFF FROM BASE RING AND REBUILD RADOME COMPLETE PER SRM 53-10-72 USING 757 RADOME MOLD AND BOEING SPEC MATERIAL. 2L72 4F RTA2NM 19951020005401995102000540NM 1995 10 20 DL757954014 119950611A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11609DL 22816 RADOME CAVED IN DURING DESCENT. SHOP INSPECTION FOUND WHITE AND YELLOW MARKS OF PAINT IN CAVED AREA. THIS AREA SEEMED TO BE HIT. REBUILD RADOME COMPLETE USING 757 MOLD AND BOEING SPEC MATERIAL. 2L72 4F RTA2NM 19951020005411995102000541NM 1995 10 20 DL757954018 119950905A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11638DL 23761 HOLE AT 9 O'CLOCK POSITION. SHOP INSPECTION FOUND MOISTURE AND OLD WET-LAY REPAIRS. REBUILD RADOME COMPLETE USING 757 MOLD AND BOEING SPEC MATERIALS. 2L72 4F RTA2NM 19951020005421995102000542NE 1995 10 20 DL76L953988 219951012A7321 EEC 7911004089 BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11185DN DZL15 27961 RT ENGINE COMPUTED THRUST LIMIT INDICATOR IN EPR GAUGE INDICATES APPROXIMATELY .10 LOW IN CRUISE, LT ENGINE 1.69 RT ENGINE 1.57. REPLACED RT ENG EEC, R/U OK AT HIGH POWER. R/U REP TEST 15 PFHB. 2L72 4F4 FRTA1NM E24NE 19951020005431995102000543NM 1995 10 20 DL76S954006 119951015A3350 BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11118DL 23277 EMERGENCY LIGHT AT SEAT 13B IS INOP. REPLACED BULB, CKS GOOD. 2L72 4F RTA1NM 19951020005441995102000544WP 1995 10 20 DLL10953993 119951013A3610LS14468800 CLAMP LS24468800 LKHEED1011 10113851 5265010WP HYD SV CTR WORN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11714DA 193C1090 PIREP, ABOUT 30 MINUTES AFTER T/O PRIOR TO TOP OF CLIMB, GOT A VALID J-AREA OVERHEAT. FOUND CLAMP LEAKING AT FUSELAGE ISOLATION VALVE IN HYD SV CTR. REPLACED CLAMP DAL (P/N 297201028) REF IPC 36-14-06 FIG 1 SHEET 2 ITEM 80. LEAK CHECK OK. 2L73 4F A23WE 19951020005451995102000545WP 1995 10 20 DLL13953983 119951011A3350 EEL POWER SUPPLY RPS1 LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11790DL 0363 193A1143 THE D-ZONE EMERGENCY FLOOR TRACK LIGHTING INOP. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19951020005461995102000546WP 1995 10 20 DLL13953999 119951013A3350672320101 EEL PWR SPPLY LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11783DL 193A1009 FIRST CLASS EMERGENCY LIGHTS ONLY STAY ON FOR A FEW SECONDS. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A23WE 19951020005471995102000547WP 1995 10 20 DLL17954037 119950912A53131554989101 LONGERON LKHEED1011 10113853 5265020WP FS 1860 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 FUSELAGE, AFTERBODY, LLT LONGERON ASSY FS 1860 WL 328.942, REPAIR OF CRACKED LONGERON. THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTERBODY AT APPROX FS 1860 AND WL 328, WAS FOUND CRACKED IN THE RADIUS. THE CRACK EXTENDS FROM THE AFT END OF THE PART FWD APPROX 6 INCHES ALONG THE RADIUS OF THE PART. INSTALLED REPAIR DOUBLER PER DL ERA 271830-14. 2L73 4F A23WE 19951020005481995102000548WP 1995 10 20 DLL17954038 119950914A53201512169101 FITTINGS LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 THE LOWER DOOR SILL I/B CAP FITTINGS AT FS 901 RT AND LT SIDES, WERE FOUND CORRODED AND REQUIRED REPLACEMENT. ACCOMPLISHED REPAIRS PER DL ERA 271846-14. 2L73 4F A23WE 19951020005491995102000549NM 1995 10 20 DLM88953998 119951005A71105930645509 NOSE COWL DOUG MD88 MD88 3023688NM NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11907DE 53416 DURING SHOP INSPECTION, A DENT WAS FOUND IN THE LEADING EDGE LIP OF THE NOSE COWL. THE DAMAGE WAS REPAIRED PER SRM 54-04A. 2L72 4F RTA6WE 19951020005501995102000550NM 1995 10 20 P5CA9500821 119951018A2550 NET BOEING747 747122 1384872NM CARGO COMPT NOT SECURED A P5CAA UNSCHED LANDING O OTHER CLCLIMB 1 WP23850FT 19755 FELT YAW ON CLIMBOUT AT 5,500 FEET, ALL ENGINE INDICATIONS NORMAL AND NO FLUID LOSS OBSERVED. FLIGHT ENGINEER WAS SENT BACK TO CARGO DECK AFTER LEVEL OFF, OBSERVED BANGING SOUNDS OUTSIDE CARGO DOOR. RETURNED TO ORD, FOUND SECTION OF CARGO NET HANGING OUTSIDE MAIN CARGO DOOR FLAPPING IN THE WIND. 2L74 4F A20WE 19951020005511995102000551NM 1995 10 20 SWAA950660 119951012A5320 WEB BOEING737 7375H4 138449DNM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07510SW 24187 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT BS 344, BL 0 AT UPPER FWD CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951020005521995102000552NM 1995 10 20 SWAA950661 119951012A5320 DOOR FRAME BOEING737 7375H4 138449DNM BS 294 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07510SW 24187 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER CORNER, BS 294. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951020005531995102000553NM 1995 10 20 SWAA950662 119951015A80122730426 START VALVE BOEING737 7372H4 138448CNM GE CFM56 CFM563B1 13802NE NR 1 ENGINE FAILED A SWAADE RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW07102SW 23108 707433 DURING CLIMBOUT, NUMBER 1 ENGINE WAS SHUTDOWN DUE TO START VALVE OPEN LIGHT ILLUMINATING. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. REPLACED START VALVE AND START VALVE PRESSURE SWITCH PER BOEING MAINTENANCE MANUAL. 2L72 4F4 F A16WE E2GL 19951020005541995102000554NM 1995 10 20 SWAA950663 119951014A5313 STRINGER BOEING737 7375H4 138449DNM BS 303.9 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07510SW 24187 DURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 STRINGER WEB CRACKED AT BS 303.9 LEFT SIDE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951020005551995102000555NM 1995 10 20 SWAA950664 119951013A2910 LINE BOEING737 7372H4 138448CNM NR 2 ENGINE RUPTURED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0752SW 21533 DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PRESSURE LOSS. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AND REPLACED NUMBER 2 ENGINE REVERSER PRESSURE LINE AND HYDRAULIC CASE DRAIN FILTERS PER BOEING MAINTENANCE MANUAL. 2L72 4F A16WE 19951026000011995102600001NM 1995 10 26 95FDEA01423 119950925A5753652163491 SKIN BOEING727 72722 1384002NM LT TE AFT FLAP DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 THE L/W I/B AFT FLAP HAS AREA OF DELAMINATION ON LOWER SURFACE, APPROX 70 INCHES FROM I/B END ON FRONT SPAR. REPAIRED L/W I/B AFT FLAP LOWER SURFACE IAW FEDEX SRM 51-40-6. 2L73 4F A3WE 19951026000021995102600002NM 1995 10 26 95FDEA01507 119951005A2750 DRIVE MOTOR BOEING727 727233 138408ANM RT TE FLAPS LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25280FE 22347 DURING CLIMB, ENGINEER NOTICED A-SYS HYD DECREASING, PERFORMED IMMEDIATE ACTION, A-SYS KEPT DECREASING. PERFORMED HYD LEAK CKLIST AND RETURNED TO MEM. RAN WITH FLUID SHUT-OFF VALVES CLOSED FOR 15 MINS. FOUND RIGHT O/B MOTOR SEAL BLOWN, REPLACED MOTOR AND A-SYS PRESS FILTERS, NO CONTAMINATION FOUND. A/C WILL REQ ALL HYD SYS TO BE BLEED, RESVC, AND LEAK CK A-SYS FILTERS AND O/B FLAP DRIVE MOTOR. RAN ENG, LEAK CK'D, OPS CK'D A-SYS AND FLAP DRIVE SYS. SVC A-SYS TO 5 GALLONS, OK FOR SERVICE. 2L73 4F RTA3WE 19951026000031995102600003NM 1995 10 26 DL73S953952 119951009A53156545410223 FLOOR BEAM BOEING737 737232 1384475NM BS 661 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11327DL 23099 THE LB 0.07 FLOOR BEAM OF THE WING CENTER SECTION IS CRACKED AT STA 661. THE UPPER CAP OF THE BEAM IS COMPLETELY CRACKED, AND THE WEB AND WEB DOUBLER ARE CRACKED APPROXIMATELY 2.0 INCHES AT THE SAME LOCATION. THE CRACKS ARE TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210. THE 65C34537-11 REINFORCING ANGLE CANNOT BE INSTALLED PER THE SERVICE BULLETIN BECAUSE THE FWD FIVE FASTENERS FALL INTO THE RADIUS OF THE ANGLE. ELIMINATING THESE FIVE FASTENER ROWS MAKE THE 65C34537-11 EQUIVALENT TO THE ORIGINAL 65-45410-104 REINFORCEMENT ANGLE. THUS, THE ORIGINAL ANGLE WILL BE REINSTALLED. 2L72 4F RTA16WE 19951027000011995102700001SO 1995 10 27 95ZZZX5889 119950720A7712 TQ GAUGE EMB 120 EMB120ER 3260203SO LT ENGINE MALFUNCTIONED A GLBAA UNSCHED LANDING O OTHER TOTAKEOFF 1 CE01293UX 120293 IMT - THE CREW ELECTED AN AIR TURN BACK AFTER THE LT ENGINE TORQUE GAUGE WENT TO ZERO ON BOTH ANALOG AND DIGITAL. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AFTER WHICH MAINTENANCE SWAPPED TORQUE PROBES LT TO RT. ON A TEST RUN-UP, THE SYSTEM FUNCTIONED NORMALLY. 2L72 4T RTA31SO 19951027000021995102700002SO 1995 10 27 95ZZZX5890 119950808A771230005000053 TQ SIG COND EMB 120 EMB120ER 3260203SO RT ENGINE FAILED A GLBACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE01295UX1381 44115 120295 OSH - CREW ABORTED TAKEOFF WHEN RT ENGINE TORQUE GAUGE WENT INOP AND THE ENGINE AUTOFEATHERED. MAINTENANCE REPLACED THE TORQUE GAUGE (TORQUE SIGNAL CONDITIONER) AND PERFORMED SATISFACTORY ENGINE RUNS. 2L72 4T RTA31SO 19951027000031995102700003SO 1995 10 27 95ZZZX5891 119950722A2750 RETRACT MECH EMB 120 EMB120ER 3260203SO TE FLAPS MALFUNCTIONED A GLBAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 CE01295UX1229 120295 ORD - THE CREW ELECTED AN AIR TURN BACK AFTER THE FLAPS STUCK IN THE 15 DEGREE POSITION. AFTER AN UNEVENTFUL LANDING, MAINTENANCE CHECKED THE FAULT SYSTEM IN THE MX MODE OF THE FLAP COMPUTER AND CLEARED FAULTS PER BRASKA MM CH27-50-00. OPS CHECK OF FLAPS COULD NOT DUPLICATE PROBLEM. 2L72 4T RTA31SO 19951027000041995102700004CE 1995 10 27 95ZZZX5892 119950825A2910 PACKING BEECH 1900 1900 1154160CE HYD RESERVOIR CUT A GUUAO OTHER K FLUID LOSS APAPPROACH 1 SO198ZR UB8 MIA/EYW - FLT 103 - LANDING GEAR CIRCUIT BREAKER TRIPPED ON EXTENSION. RESET AND GEAR CAME DOWN. DETERMINED HYDRAULIC RESERVOIR CAP PREFORMED PACKING TO BE CUT, REMOVED AND REPLACED PACKING AND SERVICED SYSTEM. OPS CHECK/LEAK CHECKS GOOD ON JACKS. 2L72 4T RTA24CE 19951027000051995102700005EU 1995 10 27 95ZZZX5893 119950827A3260801801 PROX SWITCH ELDEC BAC 146 146200A 1500266EU NLG OUT OF ADJUST A TIXAO OTHER N FALSE WARNING CLCLIMB 1 WP19156TR E2156 AIRCRAFT'S 'MANUAL SPOILER FAULT' LIGHT ILLUMINATED AFTER TAKEOFF FROM LAS. THE AIRCRAFT RETURNED TO THE LAS STATION. AIRCRAFT N138TR WAS USED TO AVOID A CANCELLATION OF FLT 203/204. A LATER CANCELLATION OF FLT 104/303 WAS CAUSED DUE TO THE DELAY IN REPAIR OF THIS PROBLEM. THE NLG ELECTRONIC POSITION SENSOR WAS FOUND TO BE OUT OF ADJUSTMENT DUE TO NORMAL WEAR. THE SWITCH WAS ADJUSTED IAW THE AIRCRAFT MM. A TEST FLIGHT WAS CONDUCTED TO ENSURE NO FURTHER DIFFICULTIES WITH THE MANUAL SPOILER FAULT INDICATOR, THEN THE AIRCRAFT WAS RETURNED TO SERVICE. 2H74 4F A49EU 19951027000061995102700006NM 1995 10 27 95ZZZX5894 119950908A2611302842 SMOKE DETECTOR BOEING727 727222 1384073NM NR 3 POSITION FAILED A RYNAK NONE N FALSE WARNING APAPPROACH 1 CE077645U 20039 ON APPROACH INTO DAYTON, THE MAIN CARGO COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 POSITION SMOKE DETECTOR, OPS CHECKED NORMAL. 2L73 4F A3WE 19951027000071995102700007NE 1995 10 27 95ZZZX5895 219950901A7230 COMPRESSOR SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE STALLED A NVEAEA ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO03353SB7583 2894 340B353 785393 JAN - FLT 4596 - RIGHT ENGINE COMPRESSOR STALLED JUST AFTER TAKEOFF. AUTOCOARSEN SYSTEM ACTIVATED, AND CREW SHUT DOWN RT ENGINE. FLT 4596 RETURNED TO JAN SAFELY. REPLACED RIGHT ENGINE. 2L72 4T4 TRTA52EU E8NE 19951027000081995102700008EU 1995 10 27 95ZZZX5896 119950912A3230 BYPASS PIN BAG JETSTMJETSTM3101 1500215EU LANDING GEAR POPPED A SABAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05169PC 695 CLT/HTS - FLT 5100 - FLIGHT HAD JUST TAKEN OFF, FLIGHT CREW SELECTED GEAR UP, BUT, THE GEAR DID NOT RETRACT. THE CREW SELECTED GEAR DOWN AND RETURNED TO CLT FOR AN UNEVENTFUL LANDING. MAINTENANCE PERSONNEL WERE DISPATCHED TO TROUBLESHOOT THE PROBLEM. THE EMERGENCY LANDING GEAR BYPASS PIN WAS FOUND POPPED. THE PIN WAS RESET AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA21EU 19951027000091995102700009WP 1995 10 27 95ZZZX5897 119950815A4900GTCP85980 APU DOUG DC9 DC932 3022066WP CABIN SMOKING A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11901VJ 47275 FLL/ATL - FLT 134 - AFTER STARTING APU, SMOKE/FUMES STARTED TO ENTER THE AFT END OF THE CABIN, SHUT DOWN APU. PLACED ON MEL LOG PAGE NR 3586, ATA 49-01. 2L72 4F A6WE 19951027000101995102700010SO 1995 10 27 95ZZZX5898 119950731A32409121 BRAKES PIPER PA32 PA32R300 7103213SO RT MLG LEAKING A JIKAO OTHER K FLUID LOSS NRNOT REPORTED 1 WP018456F 32R7780100 AIRCRAFT EXPERIENCED LOSS OF BRAKING EFFECTIVENESS ON THE RIGHT SIDE. MAINTENANCE FOUND THE BRAKE CALIPER LEAKING FROM THE CYLINDER CONTAINING THE BRAKE PISTON ('PUCK'). LEAKING HYDRAULIC FLUID SOAKED THE BRAKE LININGS (P/N 66-30), REDUCING BRAKING EFFECTIVENESS. 1L71 3O A3SO 19951027000271995102700027EU 1995 10 27 95ZZZX5915 119950920A3210200952003 PINTEL PIN ROTOL STBROSSD3 SD360 8100606EU RT MLG CRACKED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03163DD12951 SH3733 DURING INSPECTION, A CRACK WAS FOUND IN THE RT GEAR FWD PINTLE PIN. THE CRACK ORIGINATED IN THE HOLE FOR THE RETAINING PIN. THE EXTENT OF THE CRACK WAS APPROXIMATELY ONE INCH LONG AND WAS CONFINED TO THE OUTER SLEEVE. REPLACED THE PINTLE PIN AND RETURNED THE ACFT TO SERVICE. 2H72 4T A41EU 19951027000281995102700028NM 1995 10 27 95ZZZX5916 119951004A3260327 IND LAMP BOEING727 72751C 1384015NM NOSE GEAR FAILED A RYNAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 CE07435EX 19288 PHX - ON APPROACH, THE NOSE GEAR GREEN DOWN AND LOCKED INDICATOR FAILED TO ILLUMINATE ON GEAR EXTENSION. TOWER VISUALLY VERIFIED GEAR DOWN. ON GO-AROUND, FLIGHT CREW RE-LAMPED INDICATOR AT WHICH TIME IT ILLUMINATED. CYCLED GEAR, INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. RE-LAMPED INDICATOR AND VERIFIED OLD LAMPS BURNED. 2L73 4F A3WE 19951027000291995102700029NM 1995 10 27 95ZZZX5917 119950924A2613356644400 OVERHEAT LOOP BOEING727 727225 1384077NM NR 3 ENG STRUT OUT OF POSITION A MYWACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO19887MA 21857 LOG REPORT: F-GL534 AT CHS, ON TAKEOFF ROLL, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT ON POWER REDUCTION. INSPECTION OF NR 3 ENGINE STRUT FOUND OVERHEAT LOOP TOUCHING DUCT ASSY. REPOSITIONED OVERHEAT LOOP. PEFORMED LEAK CHECK PER MM 36-10, AND ENGINE RUN IAW MM 72-10. NO LEAKS FOUND AND NO OVERHEAT LIGHT ILLUMINATED. ALL SYSTEMS OPERATE NORMAL. NOTE: THE DELAY OF 60 MINUTES WAS INCURRED. THIS WAS A POSITIONING FLIGHT. 2L73 4F A3WE 19951027000301995102700030 1995 10 27 95ZZZX5918 419950930A34212588423901 NR 1 INSTR RACK DOUG DC8 DC863F 302198FWP RADIO RACK INOP A ARWAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 SO19441J 8100046 45988 MIA/SJU - FLT 501 - AFTER DEPARTING MIA EN ROUTE TO SJU, CAPTAIN'S ADI ROLLED OVER. AIRCRAFT RETURNED TO MIA. FOUND NR 1 ADI AND INSTRUMENT RACK AT FAULT. REMOVED AND REPLACED NR 1 ADI AND NR 1 INSTRUMENT AMP RACK. OPS NORMAL IAW 34-23-0. REFERENCE: OPERATOR CONTROL NR ARWA0930501. 2L74 4F 4A25 19951027000311995102700031EU 1995 10 27 AALA951445 119950813A3241 ANTI-SKID CONTLR FOKKERF28 F28MK0100 4990807EU LANDING GEAR MALFUNCTIONED A AALAK NONE O OTHER LDLANDING 1 SW071430D 11415 IAH - FLT 2063 - DURING LANDING ROLL-OUT, NR 1 AND NR 2 MLG TIRES EXPERIENCED BLOW OUTS WHEN BRAKES WERE APPLIED. AIRCRAFT STOPPED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 MLG WHEELS AND BRAKES AND PLACARDED ANTI-SKID SYSTEM. AIRCRAFT MAINTENANCE FERRY IAH/DFW. ACCOMPLISHED BITE CHECK OF BRAKE ANTI-SKID CONTROLLER WITH NO DEFECTS FOUND. PRECAUTIONARY REPLACED BRAKE ANTI-SKID CONTROLLER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19951027000321995102700032EU 1995 10 27 AALA951561 119950817A323071539 VALVE FOKKERF28 F28MK0100 4990807EU NLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071471G 11507 DFW - FLT 0544 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, THE NLG ALERT ON THE MFDU WAS ACTIVATED. RECYCLED GEAR WITH SAME RESULT. AIRCAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED SEQUENCING VALVE AND RESTRICTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19951027000331995102700033WP 1995 10 27 AR022851 119950228A575357695832 SLOT DOOR DOUG DC8 DC862F 3021972WP RT TE FLAP CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD SLOT DOOR WITH LEVEL 2 CORROSION AT L/E, REF CPCP 031 116R0551. FABRICATED DOUBLER USING STAINLESS STEEL .040 301 1/2 HARD IAW EO NR 9503061 AND SRM 51-1-8. (X) 2L74 4F 4A25 19951027000341995102700034WP 1995 10 27 AR022853 119950228A5753 PANEL DOUG DC8 DC862F 3021972WP RT SLOT CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 RIGHT WING OUTBOARD SLOT MIDDLE PANEL HAS LEVEL 2 CORROSION, REF CPCP 027 115R 0551. FOUND AREA BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER IAW EO 9503061. (X) 2L74 4F 4A25 19951027000351995102700035WP 1995 10 27 AR031451 119950314A5730 SKIN DOUG DC8 DC862F 3021972WP WS 240 LE CRACK A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND LT LOWER WING L/E LOOSE, FASTENERS AT APPROXIMATELY XFS 240.000; FOUND SMALL CRACK AT FASTENER HOLE. THE DAMAGED AREA WAS CUT OUT AND DOUBLER AND FILLER WERE INSTALLED TO RESTORE THE LOST STRENGTH PER E.O. NR 9502274 AND SRM 51-1-8. (X) 2L74 4F 4A25 19951027000361995102700036WP 1995 10 27 AR082251 119950822A5512 SKIN DOUG DC8 DC862F 3021972WP RT HORIZ STAB CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND RT HORIZONTAL STABILIZER UPPER TIP WITH EXFOLIATION (LEVEL 2) CORROSION. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-2-1. SEALED REPAIR IAW SRM 51-20-0. (X) 2L74 4F 4A25 19951027000371995102700037WP 1995 10 27 AR091051 119950910A32313648616 LATCH HOOK DOUG DC8 DC863F 302198FWP LT MLG WW FROZEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19661AV 45969 MIAMI - AFTER TAKEOFF, DOOR NOT LATCHED LIGHT ON. RECYCLED GEAR AND ACCOMPLISHED APPROPRIATE CHECK LIST, LIGHT REMAINED ON. RETURN TO MIAMI. TROUBLESHOOTING FOUND LEFT DOOR UPLATCH HOOK AND ATTACH FITTING HARDWARE FROZEN. DISASSEMBLED, CLEANED, RE-LUBED, RE-ASSEMBLED. ACCOMPLISHED MAIN GEAR DOOR MECHANISM, ADJUSTMENT, AND TEST PER DACO MM 32-31-4. OPS NORMAL. (X) 2L74 4F 4A25 19951027000381995102700038WP 1995 10 27 AR091351 119950913A53305750901517 SKIN DOUG DC8 DC862 3021970WP DOOR CUTOUT CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 45896 FUSELAGE OUTER SKIN CRACKED 1.50 INCHES IN UPPER AFT CORNER OF FWD ENTRY DOOR CUT-OUT. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC-8 SB 53-075, AND DAC DWG SR 0850021. BLIND FASTENERS TO BE REPLACED AT NEXT C-CHECK PER DACO FAX DATED 9-15-95. (X) 2L74 4F 4A25 19951027000391995102700039NE 1995 10 27 ARWA0927951 219950922A7510361615 CLAMP DOUG DC8 DC863F 302198FWP PWA JT3D JT3D7 52039NE NR 3 ENGINE BROKEN A ARWAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 SO19661AV 45969 671222 BOGOTA - FLT 240 - AFTER DEPARTURE, CREW EXPERIENCED ABNORMAL INDICATIONS ON NR 3 ENGINE AND RETURNED TO POINT OF DEPARTURE. UPON ARRIVAL, MAINTENANCE FOUND A CLAMP ON THE ANTI-ICE MANIFOLD HAD FAILED WITH ASSOCIATED HEAT DAMAGE AND BURNED WIRING. REPLACED CLAMP AND BOLT. LEAK CHECK OK IAW MM 36-10-00. REPLACED DAMAGED WIRES WITH NEW IAW AC 43-13-1A AND MM 20-50-1. ENGINE OPS NORMAL IAW J/C 6528. (X) 2L74 4F4 F 4A25 1E8 19951027000401995102700040WP 1995 10 27 ARWA0927952 119950212A5712 RIB DOUG DC8 DC862F 3021972WP WS 761.695 BENT A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING INCIDENT INSPECTION, FOUND RIGHT WING RIB SUPPORT FOR WING TIP AT STA XW 761.695 DAMAGED AT LEADING EDGE AREA. FABRICATED NOSE SECTION OF BULKHEAD FROM .071 INCH 7075-0, AND NOSE DOUBLER AND SPLICE DOUBLER FROM .080 INCH 7075-0. HEAT TREATED, PRIMED, AND INSTALLED ON WING IAW DER EO ARW.950031-0036. 2L74 4F 4A25 19951027000411995102700041WP 1995 10 27 ARWA0927956 119950315A3210 BUSHING DOUG DC8 DC862F 3021972WP LT MLG PITTED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT HAD INTERNAL PITTING. REMOVED SIDE BRACE AND ROUTED TO SHOP FOR OVERHAUL. RE-BRUSHED STRUT PER MM 32-1-8, PAGE 402E. REINSTALLED SERVICEABLE SIDE BRACE PER MM 32-11-3. OPS NORMAL IAW MM 32-00-00. (X) 2L74 4F 4A25 19951027000421995102700042WP 1995 10 27 ARWA0927957 119950217A5522 SKIN DOUG DC8 DC862F 3021972WP ELEVATOR CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION BEYOND LIMITS ON ELEVATOR STA XE 176.156. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DER DRAWING ARW.950007-0169. REBALANCED ELEVATOR IAW SRM 51-4-0. (X) 2L74 4F 4A25 19951027000431995102700043WP 1995 10 27 ARWA0927958 119950212A5730 SKIN DOUG DC8 DC862F 3021972WP WS 763-636 DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND RT WING OUTBOARD TRAILING EDGE UPPER SURFACE PANEL DAMAGED FROM STA XW 763.0 TO XW 636.0. REPAIRED PANEL IAW SRM 51-1-9 AND DER EO 950031-0024. (X) 2L74 4F 4A25 19951027000441995102700044 1995 10 27 ARWA0930501 419950930A34212588369901 NR 1 ADI DOUG DC8 DC863F 302198FWP RADIO RACK INOP A ARWAA UNSCHED LANDING I FLT. ATTITUDE INST. CRCRUISE 1 SO19441J 78041006 45988 MIA/SJU - FLT 501 - AFTER DEPARTING MIA EN ROUTE TO SJU, CAPTAIN'S ADI ROLLED OVER. AIRCRAFT RETURNED TO MIA. FOUND NR 1 ADI AND INSTRUMENT RACK AT FAULT. REMOVED AND REPLACED NR 1 ADI AND NR 1 INSTRUMENT AMP RACK. OPS NORMAL IAW 34-23-0. REFERENCE: OPERATOR CONTROL NR 95ZZZX5918. (X) 2L74 4F 4A25 19951027000451995102700045WP 1995 10 27 ASAA9580192 119950827A3350014597101 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01976AS 53452 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT SIGN LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19951027000461995102700046WP 1995 10 27 CAL50885 119950925A5330 SKIN DOUG DC9 DC932 3022066WP BS 579 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND SKIN AND DOUBLER CRACKED AND BULGED AT STA 579, LONGERONS 29L-29R. THREE CRACKS WERE FOUND AND MEASURED .25 INCH, .50 INCH, AND .75 INCH LONG. THE SKIN AND DOUBLER WERE REPAIRED IAW SRM 53-04, FIGURE 43. (X) 2L72 4F A6WE 19951027000471995102700047NM 1995 10 27 CAL950610 119950720A490038042861 APU BOEING737 7373T0 1384582NM A/C TAIL MALFUNCTIONED A CALAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0917344294625606 23582 IAH - FLT 0426 - WHILE OPERATING THE APU WITH THE NR 1 GENERATOR PLACARDED INOPERATIVE, THE APU GENERATOR CONTROL CIRCUIT BREAKER POPPED ON CLIMB-OUT OF IAH. THE CIRCUIT BREAKER WAS RESET AND THE APU VOLTAGE FLUCTUATED FROM 110V TO 115V. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE APU WAS RUN AT FULL LOAD FOR SEVERAL HOURS WITHOUT FAULT. THE FAILURE COULD NOT BE DUPLICATED. (X) 2L72 4F RTA16WE 19951027000481995102700048NM 1995 10 27 CAL950630 119950801A3260 CIRCUIT BREAKER BOEING737 737130 1384435NM P6-3 PANEL POPPED A CALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW0959207 19024 EWR - FLT 1482 - WHEN LANDING GEAR WAS EXTENDED ON FINAL APPROACH TO EWR, THE GEAR 'DOWN AND LOCKED' LIGHTS DID NOT ILLUMINATE. A 'GO AROUND' WAS INITIATED AND THE CREW OBSERVED THE CIRCUIT BREAKER ON P6-3 PANEL LABELED 'SECT 5' POPPED. THE CIRCUIT BREAKER WAS RESET AND ALL GEAR INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE CIRCUIT BREAKER AND FOUND NO ABNORMALITIES. (X) 2L72 4F A16WE 19951027000491995102700049NM 1995 10 27 CAL950860 119950922A5320 CHORD BOEING737 737217 1384464NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091623274075 19886 GSO - INSPECTION FOUND A 2 INCH CRACK FROM FORWARD HOLE TO AFT HOLE OF RT CHORD AT STA 727, STR 18A. A REPAIR WAS ACCOMPLISHED IAW ECRA 5310-03165 AND EA 5310-02918. (X) 2L72 4F A16WE 19951027000501995102700050NM 1995 10 27 CAL950861 119950922A5210 HINGE CUT OUT BOEING737 7373T0 1384582NM ENTRY DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091434726205 23585 IAH - INSPECTION FOUND A .25 INCH CRACK IN LOWER CORNER OF FORWARD ENTRY DOOR HINGE LOWER CUT OUT. THE CUT OUT WAS REPAIRED IAW EA 5210-01055. (X) 2L72 4F RTA16WE 19951027000511995102700051NM 1995 10 27 CAL950862 119950922A5241 HINGE CUT OUT BOEING737 7373T0 1384582NM GALLEY DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091434726205 23585 IAH - INSPECTION FOUND A .1250 INCH CRACK IN UPPER CORNER OF FORWARD GALLEY DOOR HINGE LOWER CUT OUT. THE CUT OUT WAS REPAIRED IAW EA 5210-01055. (X) 2L72 4F RTA16WE 19951027000521995102700052NM 1995 10 27 CAL950864 119950927A21502040751 ACM BOEING727 727224 1384076NM RIGHT MALFUNCTIONED A CALAAG UNSCHED LANDING O2 MASK DEPLOYED H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW09797463971515822 22449 MIA - FLT 0702 - THE LT PACK TRIP-OFF LIGHT ILLUMINATED FOLLOWED BY LOSS OF CABIN PRESSURE WHILE EN ROUTE FROM SDQ TO EWR. THE CREW WAS UNABLE TO REGAIN CONTROL OF CABIN PRESSURE. ACFT DESCENDED TO FL 190 AND OXYGEN MASKS DROPPED. ACFT WAS DIVERTED TO MIA WHERE IT LANDED WITHOUT INCIDENT. RT ACM WAS REMOVED AND REPLACED. IN ADDITION, LT TURBO INLET OVHT SWITCH, LT COMPRESSOR DISCHARGE OVHT SWITCH, LT CONTROL CABIN DUCT OVHT SWITCH, AND LT PACK TRIP RELAY WERE ALL REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. LEAK AND OPERATIONAL CHECKS WERE NORMAL. MAINTENANCE FOUND ALL OXYGEN MASKS IN CABIN AND LAVATORIES HAD DEPLOYED. ALL OXYGEN BOTTLES CHECKED GOOD. (X) 2L73 4F A3WE 19951027000531995102700053WP 1995 10 27 CAL950865 119950927A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW09477AC 48062 MIA - FLT 0378 - INSPECTION FOUND THE EMERGENCY AISLE PATH LIGHTING AT ROWS 2-6 OFF THE TRACK AND INOPERATIVE. MAINTENANCE FOUND BROKEN WIRES AT TWO SECTIONS. THE WIRING WAS REPAIRED AND OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. (X) 2L72 4F A6WE 19951027000541995102700054WP 1995 10 27 CAL950866 119950928A25304110001131 COFFEEMAKER DOUG DC9 DC981 3022081WP AFT GALLEY LEAKING A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SW091688347 48073 EWR - FLT 0341 - CREW REPORTED SMOKE COMING FROM THE AFT GALLEY WHILE ON APPROACH TO EWR. THE GALLEY CIRCUIT BREAKERS WERE PULLED AND THE SMOKE DISAPPEARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFT GALLEY AND FOUND THE UPPER AFT COFFEEMAKER LEAKING. THERE WAS NO EVIDENCE OF FIRE. THE COFFEEMAKER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. NO OTHER DISCREPANCIES WERE NOTED. (X) 2L72 4F A6WE 19951027000551995102700055NM 1995 10 27 CAL950868 119950930A29136507506 HYD PUMP BOEING737 7373T0 1384582NM NR 2 ENGINE INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09713142225821435 23365 IAH - FLT 1769 - THE B-SYSTEM HYDRAULIC QUANTITY DECREASED TO JUST ABOVE ZERO AND WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 ENGINE B-HYDRAULIC PUMP LOW PRESSURE LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE DRIVEN B-SYSTEM HYDRAULIC PUMP WAS FOUND AT FAULT. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED, AND, LEAK AND OPERATIONAL CHECKS WERE GOOD. (X) 2L72 4F RTA16WE 19951027000561995102700056NM 1995 10 27 CAL950869 119950930A3260 CIRCUIT BREAKER BOEING737 7373T0 1384582NM AIR/GROUND SENSEPOPPED A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0917356 23942 EWR - FLT 0220 - THE GEAR INDICATOR WOULD NOT GO GREEN WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THE GEAR WAS VISUALLY CONFIRMED DOWN. IN ADDITION, THE STALL WARNING ACTIVATED AND THE GEAR WARNING HORN SOUNDED WITH FLAPS AT 15 ON FINAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR/GROUND SENSE CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. A BITE TEST OF THE LANDING GEAR LOGIC SHELF WAS PERFORMED IAW MM 32-09-10. THE LANDING GEAR WAS PINNED AND THE GEAR HANDLE WAS CYCLED SEVERAL TIMES. NO DEFECTS WERE NOTED. (X) 2L72 4F RTA16WE 19951027000571995102700057WP 1995 10 27 CAL950870 119951001A2160 TEMP SENSORS DOUG DC9 DC982 3022082WP CABIN PLUGGED A CALAAGB UNSCHED LANDING O2 MASK DEPLOYED EMER. DESCENT O OTHER CRCRUISE 1 SW0914839 49635 GSO - FLT 0562 - BOTH THE RIGHT AND LEFT AIR CONDITIONING PACKS TRIPPED OFF WHILE AT FL 330. AN EMERGENCY DESCENT WAS PERFORMED AND OXYGEN MASKS DEPLOYED. ACFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CABIN TEMPERATURE SENSORS PLUGGED. SENSORS WERE CLEANED AND REINSTALLED. AIR CONDITIONING SYSTEMS TESTED AND PERFORMED PER MM 21-00-00, PAGES 503-506, AND RT SIDE WAS FOUND INOPERATIVE IN AUTO. CABIN TEMP WAS PLACARDED INOP IN AUTO PER MEL 21-29. IN ADDITION, MX FOUND ALL OXYGEN MASKS DEPLOYED. PASSENGER OXYGEN SYSTEM WAS PLACARDED INOPERATIVE PER MEL 35-02. CREW OXYGEN WAS VERIFIED FULL. (X) 2L72 4F A6WE 19951027000581995102700058WP 1995 10 27 CAL950871 119951001A5330 SKIN DOUG DC9 DC982 3022082WP BS 207 PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578372545512433 49582 CLE - FLT 0286 - THE JETWAY PUNCTURED FUSELAGE SKIN AFT OF FORWARD ENTRY DOOR ATER ARRIVAL AT CLE. THE PUNCTURE WAS LOCATED AT STA 207, LONGERON 17L, AND WAS APPROXIMATELY 4 INCHES BY 1 INCH IN AREA. THE PUNCTURED AREA WAS TRIMMED OUT AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 12B, CLASS III REPAIR. A DIP WAS ISSUED TO REINSPECT THE AREA EVERY 3,000 FLIGHTS AND TO MAKE A CLASS I OR CLASS II REPAIR PRIOR TO 8,000 FLIGHTS. (X) 2L72 4F A6WE 19951027000591995102700059WP 1995 10 27 CAL950872 119950925A5330 SKIN DOUG DC9 DC982 3022082WP BS 427-507 TORN A CALAK NONE O OTHER ININSP/MAINT 1 SW097282129572 49481 TUS - FLT 0425 - INSPECTION FOUND A 1.5 INCH TEAR IN FUSELAGE SKIN AND DAMAGE TO TWO SKIN CLIPS DUE TO GROUND DAMAGE. THE DAMAGE WAS LOCATED AT STA 427-STA 507 AND LONGERONS 19L AND 20L. THE SKIN TEAR WAS REPAIRED IAW ECRA 5330-02317 AND SRM 53-04, FIGURE 12B. THE SKIN CLIPS WERE REPAIRED PER SRM 53-03, FIGURE 3. (X) 2L72 4F A6WE 19951027000601995102700060NM 1995 10 27 CAL950873 119950918A575365464273 TRACK BOEING737 737130 1384435NM LT TE FLAP CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097720466773 19021 EWR - INSPECTION FOUND A .25 INCH CRACK IN LT OUTBOARD TRAILING EDGE FLAP TRACK. THE CRACKED AREA WAS REPAIRED IAW ECRA 5750-02364. (X) 2L72 4F A16WE 19951027000611995102700061NM 1995 10 27 CAL950874 119950929A5414 SKIN BOEING737 7373T0 1384582NM NR 1 ENG PYLON CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091433528619 23573 HOU - INSPECTION FOUND A 1 INCH CRACK IN OUTER SKIN AT INBOARD SIDE OF PYLON OF NR 1 ENGINE PYLON ACCESS CUT OUT. A REPAIR WAS INSTALLED IAW ECRA 5430-01204. (X) 2L72 4F RTA16WE 19951027000621995102700062NM 1995 10 27 CAL950875 119950925A5730 SKIN BOEING737 7373T0 1384582NM RT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09143352861928619 23573 HOU - INSPECTION FOUND A .5625 INCH CRACK IN RT WING LOWER LEADING EDGE SKIN AT PYLON OUTBOARD MID-SPAR FITTING. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-70-13. (X) 2L72 4F RTA16WE 19951027000631995102700063NM 1995 10 27 CAL950876 119950926A5320 SHEAR TIE BOEING737 7373T0 1384582NM BS 460 BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW091433528619 23573 HOU - THE SKIN SHEAR TIE AT STA 460 BETWEEN S27R AND S28R WAS FOUND BROKEN DUE TO GROUND DAMAGE. A REPAIR WAS ACCOMPLISHED PER SRM 53-00-07, FIGURE 205, SHEET 2. (X) 2L72 4F RTA16WE 19951027000641995102700064 1995 10 27 CAL950877 419951002A22104030952906 COUPLER BOEING737 7373T0 1384582NM YAW DAMPER FAILED A ACALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW093934325005 23581 CLE - FLT 0288 - THE YAW DAMPER STARTED KICKING RUDDER BACK AND FORTH AT FL330. THE KICKING STOPPED WHEN YAW DAMPER WAS TURNED OFF. SHORTLY AFTER TURNING OFF YAW DAMPER, ACFT MADE 2 UNCOMMANDED ROLLS TO THE RIGHT WITH 'B' AUTOPILOT ENGAGED IN 'L-NAV, V-NAV' MODE. ACFT STABILIZED AFTER DESCENDING TO FL250. YAW DAMPER COUPLER REMOVED AND REPLACED. YAW DAMPER SYS TEST PERFORMED IAW MM 22-12-00 AND SYS CHECKED NORMAL. DFCS BITE TESTS PERFORMED AND ALL PASSED. A DFCS RIG CHK OF FLT CONTROLS PERFORMED AND ALL WERE WITHIN LIMITS. ALL SENSOR VALUES CHECKED AND FOUND WITHIN LIMITS. FLT CONTROL SURFACES ALL CHKD GOOD; INDICATIONS NORMAL WITH RESPECT TO CONTROL INPUT IN COCKPIT. (X) 2L72 4F RTA16WE 19951027000651995102700065WP 1995 10 27 CAL950878 119951003A3350EMBS1392 EEL BATT CHARGER DOUG DC10 DC1030 3023501WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW098307116826 48293 EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED. (X) 2L73 4F A22WE 19951027000661995102700066WP 1995 10 27 CAL950879 119951003A3350EMBS1392 EEL BATT CHRGER DOUG DC10 DC1030 3023501WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW098307134999 48293 EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED. (X) 2L73 4F A22WE 19951027000671995102700067WP 1995 10 27 CAL950882 119950928A5711 SPAR WEB DOUG DC9 DC932 3022066WP WS 58.1 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A 1.25 INCH CRACK IN RT WING SPAR WEB AT STA XCW 58.1. THE CRACK WAS ROUTED OUT IAW EA 5761-01003. (X) 2L72 4F A6WE 19951027000681995102700068WP 1995 10 27 CAL950883 119950927A5312991558241N BLKHD ANGLE DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A 1 INCH CRACK IN ANGLE CLIP ON AFT PRESSURE BULKHEAD AT OUTBOARD NR 1L HORIZONTAL BEAM. THE CLIP WAS REMOVED AND A NEW CLIP INSTALLED PER DOUGLAS DRAWING 991558. (X) 2L72 4F A6WE 19951027000691995102700069WP 1995 10 27 CAL950884 119950925A5720991982318 ANGLE DOUG DC9 DC932 3022066WP LT WING LE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A 1 INCH CRACK IN LT WING L/E SPLICE ANGLE BETWEEN NR 3 AND NR 4 SLAT TRACKS. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-0. (X) 2L72 4F A6WE 19951027000701995102700070NE 1995 10 27 CAL950886 219951005A7230790762 SUPPORT SHELF DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE BROKEN A CALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW0971828 49488 708471 FLT NR 723 - OMA - THE NR 2 ENGINE EXPERIENCED A LOSS OF POWER WHILE EN ROUTE FROM CLE TO LAS. THE ENGINE THROTTLE WAS REDUCED TO IDLE AND THE AIRCRAFT WAS DIVERTED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 2 ENGINE TAILPIPE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED AN 8TH STAGE STATOR SUPPORT SHELF HAD BROKEN OUT AND WAS THE PRIMARY CAUSE OF ENGINE FAILURE. (M) 2L72 4F4 F A6WE E9NE 19951027000711995102700071NM 1995 10 27 CAL950887 119951003A3350 EEL BATTERY BOEING737 7372C0 1384488NM R2 DOOR DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910242 20071 GSO - INSPECTION FOUND THE R-2 DOOR SLIDE LIGHT VOLTAGE READING ZERO. THE R-2 DOOR ESCAPE SLIDE LIGHT ASSY AND BATTERY WERE REMOVED AND REPLACED IAW MM 33-51-63. (X) 2L72 4F A16WE 19951027000721995102700072NM 1995 10 27 CAL950893 119950930A53206545801512 FRAME BOEING737 7372C0 1384488NM BS 227 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091024269260 20071 GSO - INSPECTION FOUND CORROSION ON CHORD AT STA 227.8, BL ZERO. THE CORRODED SECTION OF CHORD WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 51-40-4. (X) 2L72 4F A16WE 19951027000731995102700073NM 1995 10 27 CAL950894 119950911A5320 SUPPORT BOEING727 727232 1384082NM BS 345 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND FLOOR SUPPORT CORRODED ON THE FLANGE IN THE FORWARD GALLEY AREA AT BS 345, RBL 18. THE CORRODED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (X) 2L73 4F A3WE 19951027000741995102700074NM 1995 10 27 CAL950895 119950912A5311 FRAME BOEING727 727232 1384082NM BS 540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND CORROSION ON FRAME AT BS 540, STR 26R. THE CORRODED SECTION OF FRAME WAS REMOVED. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (X) 2L73 4F A3WE 19951027000751995102700075NM 1995 10 27 CAL950896 119950908A5330 SKIN BOEING727 727232 1384082NM BS 296 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND SKIN BULGED DUE TO CORROSION AT BS 296L. THE CORRODED AREA OF SKIN WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L73 4F A3WE 19951027000761995102700076NM 1995 10 27 CAL950897 119950911A5313 STRINGER BOEING727 727232 1384082NM BS 442 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND CORROSION ON STR 24R AND STR 28R AT BS 442. THE CORRODED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-3. (X) 2L73 4F A3WE 19951027000771995102700077WP 1995 10 27 CAL950898 119951005A2923414470 HYD PUMP DOUG DC9 DC983 3022083WP RIGHT INOPERATIVE A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09938MC16822 49525 BOS - FLT 0200 - THE RT HYD SYSTEM WAS LOST WHILE EN ROUTE FROM IAH TO BOS. A MANUAL GEAR EXTENSION WAS PERFORMED. LT MLG DOOR DAMAGED DURING LANDING AT BOS. FLIGHT CONTROLS WERE CYCLED SEVERAL TIMES AND NO LEAKS FOUND. SEVERAL GEAR SWINGS PERFORMED AND NO LEAKS NOTED. AN ENGINE HIGH POWER RUN WAS PERFORMED AND NO LEAKS NOTED. THE FLUID LEVEL DID NOT GO DOWN AFTER SERVICE. MAINTENANCE FOUND AUX HYD PUMP PUTTING OUT LOW PRESSURE. THE AUX HYD PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. LT MLG DOOR WAS REPAIRED IAW SRM 52-05, FIG 52. A GEAR SWING PERFORMED AND OPERATION CHECKED GOOD. (X) 2L72 4F RTA6WE 19951027000781995102700078NM 1995 10 27 CAL950900 119951008A2782269002911 ACTUATOR BOEING727 727227 1384078NM NR 2 LE SLAT BROKEN A CALAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW097075515559 21366 IAH - FLT 0525 - THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO UPON FLAP RETRACTION AFTER TAKEOFF FROM IAH. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FRONT END OF NR 2 LEADING EDGE SLAT ACTUATOR BROKEN. THE NR 2 SLAT ACTUATOR WAS REMOVED AND REPLACED PER MM 27-81-32. THE HYDRAULIC SYSTEM WAS SERVICED AND THE ENGINE PUMPS WERE RUN. OPERATION OF THE PUMPS AND SLAT ACTUATOR CHECKED GOOD. (X) 2L73 4F A3WE 19951027000791995102700079NM 1995 10 27 CAL950902 119950912A5313 STRINGER BOEING727 727232 1384082NM LAV SERVICE DOORCORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND CORROSION ON STRINGER AT LOWER FORWARD AND AFT CORNERS OF AFT LAV SERVICE DOOR. THE CORRODED SECTION OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X) 2L73 4F A3WE 19951027000801995102700080NM 1995 10 27 CAL950903 119950913A5320 SUPPORT BOEING727 727232 1384082NM BS 1072-1092 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND CORROSION ON THE OUTBOARD FLOOR SUPPORT AT BS 1072-BS 1092, RBL 60. THE CORRODED SECTION WAS REMOVED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X) 2L73 4F A3WE 19951027000811995102700081WP 1995 10 27 IXXA199578 119950922A3240 BRAKES DOUG DC8 DC862F 3021972WP NLG OUT OF ADJUST A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL2341CX 46129 CUF/WRI - DURING FLIGHT BETWEEN CUF AND WRI, CREW REPORTED BURNING RUBBER ODOR IN AIRCRAFT. MAINTENANCE ADJUSTED THE NOSE WHEEL BRAKE PADS, WHICH CAUSED THE RUBBER ODOR, AND CLIMINATED A PNEUMATIC LEAK AT NR 2 CABIN COMPRESSOR DUCT. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F 4A25 19951027000821995102700082EU 1995 10 27 SIMA952381 119950826A2612004W500 W.E.U. SAAB SF340 SF340A 7850100EU NR 1 ENGINE MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21115SB6462 96 1180 340A115 OKC - FLT 3554 - DURING TAKEOFF, NR 1 ENGINE FIRE WARNING CAP ILLUMINATED. NO FIRE HANDLE LIGHT, NO ENGINE FIRE DETECTED. RETURNED TO OKC. MAINTENANCE REPLACED THE W.E.U. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 5,981.0. (X) 2L72 4T RTA52EU 19951027000831995102700083EU 1995 10 27 SIMA952551 119950912A33506104781 EEL BATTERY PACK SAAB SF340 340B 7860101EU CABIN DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21346SB 340B346 DFW - FLT 3531 - AIRSTAIR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19951027000841995102700084 1995 10 27 USVA8954 419950824A25651161110DG EVAC SLIDE BFGOODRICH BOEING737 737247 138448DNM L-1 DOOR LOW PRESSURE A USVAK NONE O OTHER ININSP/MAINT 1 SO19308VA 11518 19613 L-1 DOOR SLIDE READS ZERO PRESSURE. REMOVED AND REPLACED DOOR SLIDE IAW BMM 25-61-311. (X) 2L72 4F A16WE 19951027000851995102700085NM 1995 10 27 USVA8955 119950821A57306546419504 SKIN BOEING737 737247 138448DNM RT WING LE CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19308VA 19613 RIGHT WING LEADING EDGE SKIN TORN AND CRACKED AT BULLNOSE INBOARD OF NR 5 SLAT ACTUATOR. REPAIRED SKIN. (X) 2L72 4F A16WE 19951027000861995102700086NM 1995 10 27 USVA8956 119950821A53136559664 STRINGER BOEING737 737247 138448DNM FS 323.7 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19308VA 19613 (N/R CARD 101N) GENERATED BY CPCP C53-202-02, FS 323.7 HEAVY CORROSION ON STR 27L. REPLACED STRINGER SECTION PER SRM 51-30-2. (X) 2L72 4F A16WE 19951027000871995102700087NM 1995 10 27 USVA8957 119950821A5751 SKIN BOEING737 737247 138448DNM LT AILERON DELAMINATION A USVAK NONE O OTHER ININSP/MAINT 1 SO19308VA 19613 LEFT AILIERON (PN 6573734) INBOARD UPPER AFT EDGE DELAMINATED. REBONDED AILERON EDGE PER SRM 51-40-6. (X) 2L72 4F A16WE 19951027000881995102700088NM 1995 10 27 USVA8958 119950821A532065458351 STRAP BOEING737 737247 138448DNM FS 351 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19308VA 19613 GENERATED BY CPCP C53-202-02. CORROSION BULGE AT SKIN LAP STRAP, FS 351, BETWEEN STR 28L-STR 28R. REPAIRED. (X) 2L72 4F A16WE 19951027000891995102700089EU 1995 10 27 VTZA95274 119950904A243523095002 STARTER/GEN JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILED A VTZAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 EA27326UE401 41064 JFK/IAD - FLT 6235 - DURING CRUISE AT 1100 HRS ON 9-4-95, DIVERTED TO PHL DUE TO THE RT GENERATOR FAILING IN-FLIGHT AND THEN A SUBSEQUENT ENGINE VIBRATION, ENGINE WAS ALSO SHUT DOWN IN-FLIGHT. AIRCRAFT LANDED AT PHL WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT STARTER/GENERATOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951027000901995102700090 1995 10 27 VTZA96006 419951007A23127510700901 COMM 1 JETAIRJETSTMJETSTM4101 1500501EU AVIONICS BAY BAD CONNECTION A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27317UE 41031 IAD/EWR - FLT 6150 - DURING CLIMB-OUT AT 0710 HRS ON 10-07-95, RETURNED TO IAD DUE TO THE NR 1 RMU HAS DASHES IN THE DISPLAY AND NO FREQUENCY. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RE-RACKED THE NR 1 COMM UNIT, OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951027000911995102700091EU 1995 10 27 VTZA96008 119951004A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGG DOOR MALFUNCTIONED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27302UE 41013 IAD/MHT - FLT 6205 - DURING TAKEOFF AT 1715 HRS ON 10-04-95, ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DOOR AND CYCLED THE DOOR WARNING MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951027000921995102700092WP 1995 10 27 9516009855 119950930A5311 FRAME DOUG DC9 DC951 3022051WP FS 1209 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01764NC 47717 DURING H-CHECK, FOUND TWO CRACK IN THE FS 1209 FRAME SHEAR WEB BETWEEN LONGERONS 11R TO 12R. REPAIRED WEB (P/N 9912246-17), PER EA 98-102588. OPERATOR CONTROL NR 9516098 CHANGED TO 9516009855. 2L72 4F A6WE 19951027000931995102700093WP 1995 10 27 9516199763 119951017A3260 DOOR SWITCH DOUG DC9 DC941 302207NWP LT MLG FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01763NW 47396 DURING CLIMB, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR DOOR WARNING SWITCH AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027000941995102700094WP 1995 10 27 9516209884 119951017A3260 DN LOCK SENSOR DOUG DC9 DC951 3022051WP NLG FAILED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01677MC 47756 DURING CLIMB, NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED, CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDING GEAR DOWNLOCK SENSOR, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027000951995102700095WP 1995 10 27 9516219921 119951017A3260 STRIKER DOUG DC9 DC932 3022066WP LT MLG WORN A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01943N 47647 DURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR STRIKER AND ADJUSTED THE LEFT MAIN LANDING GEAR UPLIMIT SWITCH. OPERATIONAL CHECK GOOD ON GROUND AND ON TEST FLIGHT. 2L72 4F A6WE 19951027000961995102700096WP 1995 10 27 9516229968 119951012A5320 FITTING DOUG DC9 DC931 3022065WP JACK SUPPORT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019332 47264 DURING D-CHECK, FOUND CORROSION ON THE JACK SUPPORT FITTING. REPLACED FITTING PER SRM 51-01 AND DWG 59-17491. 2L72 4F A6WE 19951027000971995102700097WP 1995 10 27 9516239601 119951013A5320 FITTING DOUG DC9 DC932 3022066WP KEEL BEAM CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT MAIN LANDING GEAR WHEEL WELL AFT KEEL BEAM FITTING. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951027000981995102700098WP 1995 10 27 9516249601 119951013A7120 MOUNT ASSY DOUG DC9 DC932 3022066WP LT/RT ENGINES CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT PYLON FORWARD ENGINE MOUNT ISOLATOR HOUSINGS. REPLACED BOTH YOKE ASSEMBLIES PER MM 71-20-3. 2L72 4F A6WE 19951027000991995102700099WP 1995 10 27 9516259920 119951013A5320 FITTING DOUG DC9 DC932 3022066WP FS 896 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01942N 47459 DURING H-CHECK, FOUND CORROSION AND A CRACK IN THE FLOOR SUPPORT STRAP FITTINGS FS 896 AND 965 ABOVE LONGERON 28L. REPLACED FITTINGS PER SRM 53-11-3 FIG 3A. 2L72 4F A6WE 19951027001001995102700100NM 1995 10 27 9516262715 119951015A5343 FITTING BOEING727 7272S7 138407ZNM NLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01719RC 22490 DURING SVI CHECK, FOUND CORROSION ON THE NOSE LANDING GEAR DRAG BRACE SUPPORT FITTING. REPLACED THE FITTING PER EO 5340-01033 AND CITEXT JA5340-01033007. 2L73 4F A3WE 19951027001011995102700101WP 1995 10 27 9516279603 119951016A5320 FITTING DOUG DC9 DC932 3022066WP FS 465 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH FITTING AT FS 465, LBL 54. REPLACED FITTING (P/N 4911383-1), PER SRM 51-10-3. 2L72 4F A6WE 19951027001021995102700102WP 1995 10 27 9516289603 119951016A5320 FITTING DOUG DC9 DC932 3022066WP FS 980 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FLOOR ATTACH FITTING AT FS 980, LONGERON 8L. REPLACED FITTING. 2L72 4F A6WE 19951027001031995102700103WP 1995 10 27 9516299926 119951016A5312 BLKHD FITTING DOUG DC9 DC932 3022066WP FS 521 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND A CRACK IN THE LOWER RIGHT HORIZONTAL STIFFENER END FITTING AT THE FS 521 BULKHEAD. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951027001041995102700104WP 1995 10 27 9516309864 119951017A5320 FITTINGS DOUG DC9 DC951 3022051WP FS 1167 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 19R TO 20R END FITTINGS AT FS 1167. REPLACED FITTINGS PER SRM 51-10-3. 2L72 4F A6WE 19951027001051995102700105WP 1995 10 27 9516319603 119951019A5320 FITTING DOUG DC9 DC932 3022066WP FS 237 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH FITTING AT FS 237, LBL 54. REPLACED FITTING PER SRM 51-10-3, 51-30 AND 53-01. 2L72 4F A6WE 19951027001061995102700106WP 1995 10 27 9516329885 119951014A5350 LATCHES DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01401EA 47682 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE LATCHES AND CHECKED OK. 2L72 4F A6WE 19951027001071995102700107WP 1995 10 27 9516339962 119951015A5350 SEAL DOUG DC9 DC931 3022065WP TAILCONE CONTAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01914RW 47362 DURING LINE CHECK, FOUND THAT THE TAILCONE DID NOT DROP FROM THE AIRCRAFT. CLEANED TAILCONE SEAL AND CHECKED OK. 2L72 4F A6WE 19951027001081995102700108WP 1995 10 27 9516349882 119951018A3260 SWITCH DOUG DC9 DC951 3022051WP THROTTLE LACK OF LUBE A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01670MC 47659 DURING CLIMB, ALL THREE LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHTS REMAINED ILLUMINATED. AIRCRAFT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. CLEANED AND LUBRICATED THROTTLE SWITCH WHICH WAS FOUND TO BE STICKY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027001091995102700109WP 1995 10 27 95FDEA01552 119951017A2720 SPRING DOUG DC10 DC1010F 3022111WP RUDDER CONTROLS MISSING A FDEAK NONE F FLT CONT AFFECTED NRNOT REPORTED 1 SO2568058 46705 PRESSURE REQUIRED TO MOVE RUDDER PEDALS IS CONSIDERABLY LESS THAN ON OTHER DC-10-A/C. FOUND UPPER RUDDER LOAD FEEL MECHANISM SECOND STAGE SPRING PRELOAD MISSING. INSTALLED SAME, OPS CKS GOOD IAW MM 27-20-00 ON (P/N AMH7002-1). 2L73 4F A22WE 19951027001101995102700110NM 1995 10 27 95FDEA01553 119951017A5320 STUB BEAM BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CRACK IN WEB OF 760 STUB BEAM, WL 206 RBL 65 BS 760. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS PER FEDEX EO NR 7-5310-25928. 2L73 4F A3WE 19951027001111995102700111NM 1995 10 27 95FDEA01554 119951018A5313 STRINGER BOEING727 72725 1384006NM BS 447 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25152FE 18285 CRACKED STR 26L BS 447. REMOVED CRACKED STR SECTIONS AT BS 447 STR 26L AND REPAIRED PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951027001121995102700112NM 1995 10 27 95FDEA01555 119951018A5313 STRINGER BOEING727 72725 1384006NM BS 427 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25152FE 18285 CRACK ON STR 27L STA 427. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951027001131995102700113NM 1995 10 27 95FDEA01556 119951016A5315 FLOORBEAM BOEING727 727227 1384078NM BS 344 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 CRACK IN FLOORBEAM AT STA 344 AT LBL 29.5 FROM CENTER AFT FLANGE. REPAIRED PER SRM 53-10-8. 2L73 4F A3WE 19951027001141995102700114NM 1995 10 27 95FDEA01557 119951017A5315 FLOORBEAM BOEING727 727227 1384078NM BS 540 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25476FE 21461 CORROSION AT STA 540 FLOORBEAM RBL 1. CUT OUT CORRODED AREA AND INSTALLED FILLER AND ANGLES PER SRM 53-10-08 FIG 8. 2L73 4F A3WE 19951027001151995102700115NM 1995 10 27 95FDEA01558 119951017A5315 FLOORBEAM BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 HEAVY CORROSION ON FLOORBEAM AT STA 480, JUST I/B OF SEAT T-RACK RBL 25. REMOVED CORRODED AREA AND INSTALLED FILLER AND ANGLES PER SRM 53-10-8 FIG 8. 2L73 4F A3WE 19951027001161995102700116NM 1995 10 27 95FDEA01559 119951017A5320 FLOOR WEB BOEING727 72725C 138400HNM BS 540 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 UPPER LOBE FLOOR WEB CORRODED AT STA 540 LBL 44 TO 65. REMOVED CORROSION PER SRM 51-10-6 PG 4 AND INSTALLED DOUBLER PER SRM CHAPTER 53-10-9. 2L73 4F A3WE 19951027001171995102700117NM 1995 10 27 95FDEA01560 119951017A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 CORROSION ON LWR SIDE OF UPPER LOBE FLOORBEAM STA 480 LBL 24 TO 44. INSTALLED REPAIR IAW 53-10-8 FIG 5 OF SRM AND IAW ATTACHED JOB PROGRESS FORM. 2L73 4F A3WE 19951027001181995102700118NM 1995 10 27 95FDEA01561 119951012A5311 FRAME BOEING727 727227 1384078NM BS 540 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 CRACK IN UPPER RADIUS OF FWD CARGO FLOOR FRAME STA 540 RBL 3. STOP DRILLED CRACK, INSTALLED DOUBLER AT FLOOR FRAME STA 540 RBL 3 PER SRM 51-40-3. 2L73 4F A3WE 19951027001191995102700119EU 1995 10 27 95FDEA01562 119951018A2820 AUTO FEED SYST AIRBUS310 A310203 EU INNER TANK INOPERATIVE A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO25404FE 233 AT FL 370 CREW NOTICED LEFT FUEL FEED MSG ON ECAM. FUEL PAGE SHOWED NO FUEL WAS BURNING FROM THE INNER TANKS, X-FEED WAS OPENED. O/B FUEL WAS 3.2 + 3.0, LEFT INNER PUMPS WERE TURNED OFF, THEN BACK ON AFTER SEEING NO FUEL BURN. NO ECAM WARNINGS OCCURRED, INNER TANKS STARTED BURN ON GND. REMOVED AND REPLACED RELAY 133QA PER 28-21-00 PRECAUTIONARY, SYS OPS CK NORMAL IN MANUAL MODE PER MM 28-21-00. PRECAUTIONARY INOP AUTO FEED SYS. TRANSFERRED TO DDL PER MEL 28-11 CAT B, EXP 10-20-95 CTL NR 1018068. 2L72 4F RTA35EU 19951027001201995102700120NM 1995 10 27 95FDEA01563 119951019A2611774001 SMOKE DETECTOR BOEING727 727225 1384077NM NR 2 CARGO MALFUNCTIONED A FDEAK NONE N FALSE WARNING APAPPROACH 1 SO25461FE 22548 NR 2 CARGO SMOKE LIGHT AND BELL CAME ON FOR 5 SECONDS, THEN OFF. AFTER 2 MINUTES BOTH CAME ON AGAIN FOR 5 SECONDS, THEN OFF AGAIN ON FINAL APPROACH. REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR AND OPS CK NORMAL. 2L73 4F A3WE 19951027001211995102700121NM 1995 10 27 95FDEA01572 119951020A5330 SKIN BOEING727 72722 1384002NM BS 950-1183 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (71C905-00), BS 950 TO 1183, STR 26L AND 26R ON EXTERIOR SKIN. COMPLIED WITH EA 7-5310-25938 (FEDEX EA), AT BS 950 TO 958, STR 28 TO 30L. REMOVED CORROSION ON REMAINDER OF SKIN FROM BS 950 TO 1183, STR 26 LT AND RT FOUND TO BE WITHIN LIMITS AS PER FEDEX SRM 53-30-1. 2L73 4F A3WE 19951027001221995102700122NM 1995 10 27 95FDEA01573 119951020A5711BAC15061577 SPAR BOEING727 72722 1384002NM BS 920 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (C53-132-02-1/2), WING CENTER SECTION BS 920 LOWER SPAR CHORD RBL 34 TO 44. REMOVED CORROSION ON STA 870 LOWER SPAR CHORD. FOUND CHORD IS OUT OF LIMITS PER FEDEX 727 SRM 75-10-1. REMOVED AND REPLACED STA 870 LOWER CHORD PER EWO NR 95-3133 (EA NR 7-5710-25916). 2L73 4F A3WE 19951027001231995102700123NM 1995 10 27 95FDEA01574 119951020A571165185385 SPAR BOEING727 72722 1384002NM BS 870 UPPER CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 CORROSION (C53-132-02-1/2), DETERIORATED FINISH, WING CENTER SECTION BS 870 UPPER SPAR CHORD, ENTIRE LENGTH. REMOVED CORROSION ON STA 870 UPPER SPAR CHORD, FOUND CHORD TO BE OUT OF LIMITS PER FEDEX 727 SRM (57-10-1). REMOVED AND REPLACED STA 870 UPPER CHORD PER EWO 95-3134 AND EA 7-5710-25916. 2L73 4F A3WE 19951027001241995102700124NM 1995 10 27 95FDEA01575 119951020A532065163387 CHORD BOEING727 72722 1384002NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0562, FOUND CORROSION AT BS 950 CHORD AT STR 26R. REMOVED AND REPLACED LOWER SKIN FORWARD CHORD AT BS 950 STR 26R AS PER DRAWING 65-16336. 2L73 4F A3WE 19951027001251995102700125NM 1995 10 27 95FDEA01576 119951020A5330 SKIN BOEING727 72722 1384002NM BS 320-360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0559, FOUND SIDE SKIN CORROSION AT BS 320 TO 360 WL 160, BS 328 TO 332 RBL 17 FROM WL 145 TO 160, BS 280 RBL 17 FROM WL 145 AND CRACKED SHEAR TIE AT BS 325 RBL 17 TO 22. COMPLIED WITH EA 7-5310-25937. 2L73 4F A3WE 19951027001261995102700126NM 1995 10 27 95FDEA01577 119951020A53206516338174 STRAP BOEING727 72722 1384002NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0562, FOUND CORROSION ON STRAP ON BS 950 MAIN FRAME RBL 19 TO 55 WL 144 TO 146. REMOVED AND REPLACED STRAP BS 950 RBL 19 TO 55 WL 144 TO 164 IAW FEDEX ES 7-5310-25935. 2L73 4F A3WE 19951027001271995102700127NM 1995 10 27 95FDEA01578 119951020A531165163387 FRAME BOEING727 72722 1384002NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0562, FOUND CORROSION ON BS 950 MAIN FRAME AT RBL 30 WL 144. REMOVED CORROSION ON BS 950 MAIN FRAME AT RBL 30 WL 144 AND REPAIRED PER FEDEX EA 7-5310-25935. 2L73 4F A3WE 19951027001281995102700128NM 1995 10 27 95FDEA01579 119951020A531465C80006104 KEEL BEAM BOEING727 72722 1384002NM BS 1126-1129 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25188FE 19081 WHILE WORKING NR 0079, DISCOVERED CORROSION ON RT KEEL BEAM BS 1126 TO 1129 STR 29R TO BE OUT OF LIMITS, REQUIRES REPLACEMENT FROM BS 950 TO 1060. REMOVED CORRODED KEEL BEAM AND INSTALLED NEW KEEL BEAM FROM BS 950 TO 1086 STR 29R IAW FEDEX EA 7-5310-25936. 2L73 4F A3WE 19951027001291995102700129NM 1995 10 27 95FDEA01580 119951019A531465C317681 KEEL BEAM BOEING727 727227 1384078NM BS 1000 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CORROSION IN AFT CARGO BAY, CORROSION FOUND ON SIDE OF STR 29, KEEL BEAM STA 1000 LBL 9. REMOVED AND REPLACED KEEL BEAM PER FEDEX EO NR 7-5310-7-2356 REV C PART 5. 2L73 4F A3WE 19951027001301995102700130NM 1995 10 27 95FDEA01581 119951022A78305T40013J55200 CLAMP BOEING747 7472R7F NM NR 1 ENG TR DUCTFAILED A FDEACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO25639FE 21650 DURING T/O ROLL, THE FIRE DETECTION LIGHT AND FIRE WARNING LIGHT ILLUMINATED ON NR 1 ENG. THE NR 1 ENG NACELLE OVERHEAT TEMP REACHED 9, THEN QUICKLY DROPPED TO ZERO. ABORTED T/O AT 60 KNOTS AND RETURNED TO RAMP. FOUND REVERSER DUCT CLAMP BLOWN. REMOVED AND REPLACED CLAMP, INSPECTED ENG AND PERFORMED GND ENG RUN. LK AND OPS CK GOOD. 2L74 4F RTA20WE 19951027001311995102700131NM 1995 10 27 95FDEA1564 119951018A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 488 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 CORROSION ON BOTTOM AND TOP OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE (NR 0757). FILE OPEN 2L73 4F A3WE 19951027001321995102700132NM 1995 10 27 95FDEA1565 119951018A5320 PRESS DECK BOEING727 72725C 138400HNM RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 HEAVY CORROSION IN RT WHEEL WELL PRESSURE DECK LOCATED JUST O/B AND AFT OF VIEW WINDOW (NR 1036). FILE OPEN 2L73 4F A3WE 19951027001331995102700133NM 1995 10 27 95FDEA1566 119951018A5320 CLIP BOEING727 72725C 138400HNM BS 970 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 STR 4L GOUGED UNDER STR CLIP STATION 970, (NR 0707). INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3 FIG 3 PG 5 TO 8. 2L73 4F A3WE 19951027001341995102700134NM 1995 10 27 95FDEA1567 119951018A5320 DOUBLER BOEING727 72725C 138400HNM BS 178 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 TOP FUSELAGE SKIN AT RADOME BULKHEAD STATION 178 CENTER, DOUBLER TOP OF SKIN IS CUT HAS SEVERAL CRACKS AT EDGE (NR 0704). REMOVED OLD DOUBLER, FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-3 PG 47. 2L73 4F A3WE 19951027001351995102700135NM 1995 10 27 95FDEA1568 119951018A5321 CARGO FLOOR BOEING727 72725C 138400HNM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 AFT CARGO FLOOR CRACK IN FRAME AROUND TOOLING HOLE STA 1090, JUST ABOUT STR 27 LT (NR 1020). FABRICATED FRAME REPAIR PER SRM 51-40-3, DOUBLER INSTALLED. 2L73 4F A3WE 19951027001361995102700136NM 1995 10 27 95FDEA1569 119951019A5313 STRINGER BOEING727 72725C 138400HNM BS 380 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 MAIN CARGO UPPER LOBE, STR 16R CRACKED AT STA 380 ATTACHMENT TO FRAME (NR 1020). CUT OUT DAMAGED AREA, REPAIRED PER SRM 53-10-3 PG 3. 2L73 4F A3WE 19951027001371995102700137NM 1995 10 27 95FDEA1570 119951019A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 920 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 STA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28 (NR 0753). REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DATED 10-13-95. 2L73 4F A3WE 19951027001381995102700138NM 1995 10 27 95FDEA1571 119951020A3411 PITOT TUBE BOEING727 7272S2F 1384O81NM LEFT BLOCKED A FDEAA UNSCHED LANDING I FLT. ATTITUDE INST. TOTAKEOFF 1 SO25207FE 22929 FIRST OFFICER'S AIR SPEED FAILED. FOUND PILOT TUBE BLOCKED. REMOVED BLOCKAGE, CHECKED INDICATION WITH BARFIELD TESTER AND OK FOR SERVICE. 2L73 4F A3WE 19951027001391995102700139NM 1995 10 27 95UAL900215 119951018A275065503276 TRANSMISSION BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 7 TE FLAP INOP A UALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 WP299069U 19950 EXECUTED MISSED APPROACH AT ORD, TRAILING EDGE FLAPS DID NOT EXTEND BEYOND 5 DEGREES. REPLACED NR 7 TRAILING EDGE FLAP TRANSMISSION, CHECKS OK. 2L72 4F4 F A16WE E2EA 19951027001401995102700140NM 1995 10 27 95UAL900216 119951019A2530 OVEN BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE GALLEY OVERTEMP A UALAFHJAACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITSDUMP FUEL UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 WP294717U 19878 FORWARD LOWER LOBE GALLEY FIRE WARNING AFTER TAKEOFF. SUSPECTED CAUSE IS EXCESSIVE TEMPERATURE SETTING FOR THE FOOD STUFFS/PACKAGING PLACED IN THE OVEN. CORRECTIVE ACTION HAS BEEN TO ISSUE AN ALERT BULLETIN FOR ALL MAINTENANCE PERSONNEL TO FOLLOW REVISED PROCEDURE FOR THE SELF CLEANING MAINTENANCE TASK. 2L74 4F4 F A20WE E20EA 19951027001411995102700141NM 1995 10 27 95UAL900217 119951019A3350 EEL CONNECTOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297458U 21912 EMERGENCY ESCAPE LIGHTING STRIP BETWEEN ROW 17 AND ROW 19 INOP. SECURED STRIP CONNECTOR. 2L73 4F4 F A3WE E2EA 19951027001421995102700142NM 1995 10 27 95UAL900218 119951019A3350 EEL BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29657UA 27112 EMERGENCY ESCAPE PATH LIGHTING INOP AT GALLEY. REPLACED LIGHT, CHECKS OK. 2L72 4F4 FRTA1NM E24NE 19951027001431995102700143NM 1995 10 27 95UAL900219 119951019A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOP A UALAK NONE L NO TEST ININSP/MAINT 1 WP29520UA 24890 EMERGENCY EXIT LIGHT AT ROW TWO INOP. REPLACED LIGHT, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951027001441995102700144NM 1995 10 27 95UAL900220 119951020A3350 EEL CONNECTOR BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29160UA 21237 EMERGENCY EXIT LIGHTS IN UPPER DECK ARE INOP. RECONNECTED LOOSE CONNECTOR. 2L74 4F4 F A20WE E20EA 19951027001451995102700145NM 1995 10 27 95UAL900221 119951020A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29541UA 25253 EMERGENCY EXIT LIGHTS, LEFT HAND OVERHEAD BINS AT ROW 15 AND 16 INOP. REPLACED LAMPS. 2L72 4F4 FRTA2NM E17NE 19951027001461995102700146NM 1995 10 27 95UAL900222 119951020A2120 AIR DISTRIBUTION BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN SMOKE A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP297453U 21907 AIRCRAFT RETURNED TO GATE ON ACCOUNT OF CABIN FILLED WITH SMOKE FROM AIR CONDITIONING SYSTEM. APU REMOVED AND OPERATED IN TEST CELL, NO EVIDENCE OF OIL LOSS OR PROBABILITY OF DUCT CONTAMINATION. OIL LOSS COULD HAVE BEEN OVERSERVICING. APU RECEIVED C-CHECK AND WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19951027001471995102700147NM 1995 10 27 95UAL900223 119951020A3150 AURAL WARN MOD BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE COCKPIT MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297451U 21905 DURING ENGINE FIRE WARNING TEST, FOUND WARNING BELL TO BE INTERMITTENT. REPLACED AURAL WARNING MODULE M6. OPERATIONAL CHECKED NORMAL WITH NO FURTHER PROBLEMS REPORTED. 2L73 4F4 F A3WE E2EA 19951027001481995102700148NM 1995 10 27 95UAL900224 119951023A324065461166 BRAKE FLANGE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE MLG CRACKED A UALAK NONE D INFLIGHT SEPARATION LDLANDING 1 WP299010U 19048 NR 4 WHEEL, BRAKE AND PART OF AXLE, DEPARTED FROM AIRCRAFT. REPLACED GEAR. CRACK WAS FOUND EMANATING FROM BRAKE ATTACH FLANGE, PER BOEING SERVICE BULLETIN 737-32-1068. 2L72 4F4 F A16WE E2EA 19951027001491995102700149WP 1995 10 27 ABXA9500885 119951019A2510092543172 SEAT DOUG DC9 DC932 3022066WP RT COCKPIT DEFECTIVE A ABXAK NONE O OTHER CRCRUISE 1 GL23983AX 47257 FIRST OFFICER'S SEAT LOOSE AND ROCKS ON SEAT RAILS. ALSO, SEAT BACK ROCKS AND SEAT CUSHION WORN OUT. REPLACED FIRST OFFICER'S SEAT ASSEMBLY IAW DC-9 MM. 2L72 4F A6WE 19951027001501995102700150WP 1995 10 27 ABXA9500886 119951020A2612D5020 FIRE LOOP DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 3 ENGINE DEFECTIVE A ABXAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 GL23801AX 46077 669292 FIRE WARNING INDICATION OCCURRED ON NR 3 ENGINE DURING CLIMB AND BOTH FIRE EXTINGUISHERS WERE DISCHARGED. FIRE WARNING INDICATION PERSISTED FOR SEVERAL MINUTES AND ENGINE WAS SHUTDOWN. ENGINE WINDMILLED FOR APPROXIMATELY 25 TO 30 MINUTES WITH 10 TO 15 PSI OF OIL PRESSURE. FLIGHT CONTINUED WITHOUT FURTHER PROBLEM. INSPECTED NR 3 ENGINE AND FOUND NO EVIDENCE OF FIRE. FOUND CANNON PLUG ON NR 3 ENGINE INBOARD LOWER FIRE LOOP SATURATED. CLEANED CANNON PLUG AND REPLACED THE LOWER SECTION OF FIRE LOOP. REPLACED NR 3 AND NR 4 FIRE EXTINGUISHER BOTTLES AND SQUIBS. TESTED FIRE WARNING SYSTEM AND OPS CHECK WAS GOOD. 2L74 4F4 F 4A25 1E8 19951027001511995102700151WP 1995 10 27 ABXA9500887 119951020A323045973405505J UPLATCH CYLINDER DOUG DC8 DC863 302198AWP LT MLG DEFECTIVE A ABXAO OTHER L NO TEST DEDESCENT 1 GL23825AX 46115 LEFT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED DURING INITIAL EXTENSION. LANDING GEAR WAS RECYCLED AND LANDING GEAR INDICATED DOWN AND LOCKED. REPLACED LEFT MAIN LANDING GEAR UPLATCH CYLINDER IAW DC8 MM CHAPTER 32. PERFORMED SEVERAL RETRACTION AND EXTENSION CHECKS AND ALL INDICATIONS WERE GOOD IAW DC8 MM CHAPTER 32. 2L74 4F 4A25 19951027001521995102700152WP 1995 10 27 ABXA9500888 119951019A2120 AIR DISTR DOUG DC9 DC941 302207NWP COCKPIT ODOR A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23975AX 47512 ORD - AFTER TAKEOFF, CREW REPORTED A STRONG RUBBER ODOR. INSPECTED TIRES, NOSE BRAKES AND ENGINE INLETS, FOUND NO DEFECTS. 2L72 4F A6WE 19951027001531995102700153SW 1995 10 27 COMA9520392 119951018A274027821687 TRIM BOX SWRNGNSA227 SA227AC 8780603SW COCKPIT DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01704C 13293192 AC704 PITCH TRIM INDICATOR IS INOPERATIVE. REPLACED PITCH TRIM CONTROL BOX. 1L72 4T A8SW 19951027001541995102700154EU 1995 10 27 COMA9531172 119951009A2711DL3827M131 TRIM ACTUATOR SAAB SF340 SF340A 7850100EU LT AILERON FAILED A COMAK NONE FJ FLT CONT AFFECTED WARNING INDICATION UKUNKNOWN 1 SO01344CA11157 340A025 LEFT AILERON TRIM DOES NOT WORK. REPLACED THE LEFT AILERON TRIM ACTUATOR. 2L72 4T RTA52EU 19951027001551995102700155EA 1995 10 27 COMA9560576 119951017A2610356124310 ELEMENT CNDAIRCL600 CL6002B19 EA AFT EQUIP DEFECTIVE A COMAK NONE L NO TEST UKUNKNOWN 1 SO01947CA 7077 LEFT 14TH STAGE BLEED AIR LEAK DETECTION CIRCUIT DOES NOT TEST. REPLACED THE LT 14TH STAGE BLEED LEAK DETECTION LOOP. 2L72 4F RTA21EA 19951027001561995102700156NM 1995 10 27 DL72E954067 119951002A5530 STRINGER BOEING727 727247 138408FNM VERTICAL STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND STRINGER CRACKED VERTICAL STAB INTERIOR STR 8R LOC IN 5TH BAY UP FROM ACCESS HOLE. REPAIRED PER M/M 55-30-00 FIG 803. 2L73 4F A3WE 19951027001571995102700157NM 1995 10 27 DL72E954069 119951003A5311 FRAME BOEING727 727247 138408FNM FS 930 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND FUSELAGE FRAME CRACKED AT REPAIR DOUBLER, UPPER FASTENER HOLE FS 930 RT SIDE. REPAIRED PER SRM 53-10-04 FIG 25 TYP B. 2L73 4F A3WE 19951027001581995102700158NM 1995 10 27 DL72L954059 119951019A2913 PUMP AS19570C BOEING727 727232 1384082NM B-HYD SYS LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11505DA MX321679 21307 THE B-SYS HYDRAULIC IND SHOWED ZERO IN FLT, SYS-A SHOWS 2.1 GAL AND IS STEADY. LOSS OF INDICATION IN B-SYS WENT FROM FULL TO ZERO IN ABOUT 1 HOUR. FOUND NR 2 B-PUMP LEAKING, REPLACED AND LEAK CHECK OK. REPLACED BOTH B-SYS CASE DRAIN AND PRESS FILTER, RAN ALL SYS AND ENG PUMPS AND ALL LEAK CHECKS OK. 2L73 4F A3WE 19951027001591995102700159NM 1995 10 27 DL72L954075 119951020A3350 BATTERY PACK 334101877 BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11502DA 21304 10140 ON LAYOVER, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19951027001601995102700160NM 1995 10 27 DL72S954045 119951017A5320 WEB BOEING727 727232 1384082NM BS 1243 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11522DA 21582 A .5 INCH CRACK AT LT TORQUE BOX WEB LIGHTENING HOLE STA 1243. FOUND DURING E-2 LTR CK TPAMM. REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19951027001611995102700161NM 1995 10 27 DL72S954060 119951019A5754 ANGLE BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11406DA 21150 NR 6 L/E SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT O/B END. REPAIRED PER SRM 57-54-0. FOUND AT LETTER CHECK. 2L73 4F A3WE 19951027001621995102700162NM 1995 10 27 DL72S954062 119951019A3350900542 BATTERY CHARGER BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11531DA 21814 FOUND AFT BULLNOSE EXIT LIGHT ABOVE AFT FLIGHT ATTENDANT SEAT INOP. REPLACED AFT BULLNOSE EXIT LIGHT BATTERY CHARGER, CKS NORMAL. 2L73 4F A3WE 19951027001631995102700163NM 1995 10 27 DL72S954063 119951019A3350BR9279109 EEL BOEING727 727232 1384082NM R1 DOOR BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11531DA 21814 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REPLACED R1 DOOR LOWER EMERGENCY EXIT LIGHT, CKS NORMAL. 2L73 4F A3WE 19951027001641995102700164NM 1995 10 27 DL72S954065 119951018A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11408DA 21152 EMERGENCY LIGHTS INOP AT REAR ENTRY EXIT SIGN. REPLACED BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19951027001651995102700165NM 1995 10 27 DL72S954066 119951019A3350900835A BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11408DA 21152 MID CABIN OVERHEAD AISLE EMERGENCY LT INOP. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19951027001661995102700166NM 1995 10 27 DL72S954074 119951020A5320 WEB BOEING727 727232 1384082NM BS 1303 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11537DA 22073 10140 A 1 INCH CRACK IN RT LWR TORGUE BOX WEB AT LIGHTENING HOLE STA 1303. FOUND AT B-1 LTR CK. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951027001671995102700167NM 1995 10 27 DL757954061 119951019A3350767 BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11630DL 22920 R2 EMERGENCY ESCAPE LIGHT IS INOP. RELAMPED, OPS CKS GOOD. 2L72 4F RTA2NM 19951027001681995102700168NM 1995 10 27 DL76L954049 119951018A2530811150417 COFFEE MAKER BOEING767 767332 1382001NM AFT GALLEY FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO11176DN 25061 APPROX ONE HOUR BEFORE DESCENT, F/A IN AFT GALLEY REPORTED SEEING SMOKE AND SMELLING ELECTRICAL WIRE BURNING. UTILITY BUSSES SWITCHES OFF. REPLACED NR 2 COFFEE MAKER DUE TO C/B POPPED. INSPECTED OVENS AND GALLEY WIRING OPERATION NORMAL. 2L72 4F RTA1NM 19951027001691995102700169NE 1995 10 27 DL76L954081 219951020A7230 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A DALAA UNSCHED LANDING CR F.O.D. PARTIAL RPM/PWR LOSS CLCLIMB 1 SO11178DN20767 25143 724169 AT 1,100 FT AFTER T/O, THE LT ENG COMP STALLED AND EGT WENT TO 652 DEGREES. PWR WAS REDUCED TO IDLE AND ENG OPS NOR TO LANDING. REVERSERS NOT USED, OVERWT LANDING ACCOMP VSI 300 FPM SPEED AT 170, LANDING SMOOTH. EVIDENCE OF BIRD STRIKE ON NOSE COWL, PERFORMED BORE OF ENG, FOUND OK, PERFORMED HIGH POWER RUNUP AND ALL OK. 2L72 4F4 FRTA1NM E24NE 19951027001701995102700170WP 1995 10 27 DLL14954080 119951022A3350 EEL WIRES LKHEED1011 1011385115 5265015WP CABIN CHAFED A DALAK NONE O OTHER ININSP/MAINT 1 SO11737D 193C1228 EMERGENCY PATH LIGHT WIRES CHAFED AT 21HJ REF R/C 476. C/A REPAIRED WIRES. 2L73 4F A23WE 19951027001711995102700171NM 1995 10 27 DLM11954073 119951021A3350CM77839 EEL LAMP DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11801DE 48472 EMERGENCY PATH LIGHT SYSTEM LIGHT BULBS DAL (P/N 349201652), AT LOCATIONS 1E, 35G, 36G, 39C, LAV-E AND LAV-F INOP. REPLACED BULBS, OPERATION NORMAL. 2L73 4F RTA22WE 19951027001721995102700172NM 1995 10 27 DLM11954076 119951021A3350 EEL LAMP 0105606203 DOUG MD11 MD11 3023602NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11803DE 48474 DURING MAINT TESTING OF EMERGENCY FLOOR TRACK LIGHTING, FOUND LAMP MODULE AT 2L DOOR DEFECTIVE. REPLACED FLOOR TRACK LAMP MODULE DAL (P/N 330201571), OPERATIONAL TEST NOW OK. 2L73 4F RTA22WE 19951027001731995102700173WP 1995 10 27 MEJA9509002 219950926A7200 ENGINE SWRNGNSA227 SA227AT 8780610SW GARRTTTPE331TPE33111U 01514WP RIGHT BIRD STRIKE E AMEJAK NONE C F.O.D. DEDESCENT 1 SW17564UP9353 3264 AT564 P44251 HRL-SAT - FLT 1853 - WHILE ON DESCENT, RIGHT ENGINE INJESTED A BIRD AND LANDED AT SAT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ENGINE, PERFORMED GROUND RUN AND LEAK CHECK. NO DEFECTS NOTED AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A5SW E4WE 19951027001741995102700174WP 1995 10 27 MWEA95358 119951019A3350 EEL SOCKET DOUG DC9 DC932 3022066WP CABIN INOP A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31602ME 48133 DURING INSPECTION, FOUND ONE EMERGENCY LIGHT ON FLOOR TRACK INOP. MAINTENANCE REPLACED LIGHT SOCKET AT ROW 17, OPS CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951027001751995102700175WP 1995 10 27 MWEA95359 119951021A33501001191 EEL DOUG DC9 DC932 3022066WP CABIN INOP A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31203ME 4511 47673 MAINT REPORTED, THE FWD EMERGENCY ENTRANCE LIGHT WILL NOT ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951027001761995102700176NM 1995 10 27 P5CA9500823 119951019A5522 TE PANEL BOEING747 747122 1384872NM RT ELEV CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 RIGHT INBOARD ELEVATOR PANEL, INBOARD TRAILING EDGE CRACKED AND DELAMINATED. SANDED AND CLEANED DAMAGED AREA, APPLIED FIBERGLASS OVERLAYS AS REQUIRED PER SRM 51-40-15. 2L74 4F A20WE 19951027001771995102700177NM 1995 10 27 P5CA9500824 119951019A7830 TR RAIL BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662628 NR 3 ENGINE R-RAIL CRACKED IN TWO PLACES, APPROXIMATELY 5 O'CLOCK POSITION. WELDED CRACK IAW P AND W MANUAL 72-53-01. 2L74 4F4 F A20WE E20EA 19951027001781995102700178NM 1995 10 27 P5CA9500825 119951019A7830 TR RAIL BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662575 NR 2 ENGINE R-RAIL CRACKED AT THE FOUR-THIRTY POSITION. WELDED CRACK IAW P AND W MM 72-53-01. 2L74 4F4 F A20WE E20EA 19951027001791995102700179NE 1995 10 27 P5CA9500826 219951019A7200 S-RAIL BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR2 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662575 NR 2 ENGINE S-RAIL CRACKED AT 6 O'CLOCK POSITION. WELDED CRACK IAW P AND W MM 72-53-01. 2L74 4F4 F A20WE E20EA 19951027001801995102700180NM 1995 10 27 P5CA9500827 119951019A7110 COWLING BOEING747 747122 1384872NM NR 3 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 NR 3 ENGINE INBOARD COWLING, 4TH FRAME FROM FRONT CRACKED INBOARD SIDE. REMOVED DAMAGE, ROUTED ANGLES TO SHOP FOR FABRICATION, INSTALLED NEW ANGLES PER SRM 54-10-03. 2L74 4F A20WE 19951027001811995102700181NM 1995 10 27 P5CA9500828 119951019A5320 FITTING BOEING747 747122 1384872NM DOOR SILL CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 FORWARD CARGO DOOR SILL NR 8 TRUSS FITTING CRACKED IN LOWER RADIUS. REMOVED AND REPLACED TRUSS FITTING IAW SRM 51-10-01. 2L74 4F A20WE 19951027001821995102700182NM 1995 10 27 P5CA9500829 119951019A5330 PANEL BOEING747 747122 1384872NM PACK ACCESS DOORDELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 FAIRING PANEL 191ML HAS DELAMINATED SPOT AT FORWARD END. SANDED AND CLEANED AREA, HOT BONDED FIBERGLASS OVERLAYS IAW SRM 51-40-12. 2L74 4F A20WE 19951027001831995102700183NM 1995 10 27 P5CA9500830 119951019A5330 PANEL BOEING747 747122 1384872NM PACK ACCESS DOORCRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 PACK ACCESS DOOR FAIRING PANEL 191ML CRACKED AT FORWARD OUTBOARD CORNER. SANDED AND CLEANED AREA, HOT BONDED FIBERGLASS OVERLAYS IAW SRM 51-40-12. 2L74 4F A20WE 19951027001841995102700184NM 1995 10 27 P5CA9500831 119951019A7800 EXHAUST SHROUD BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 662276 NR 4 EXHAUST SHROUD WORN AND CRACKED AT FORWARD FLANGE, 7 O'CLOCK POSITION. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED INTERNAL DOUBLER AND EXTERNAL WEAR PLATE IAW SRM 54-30-03. 2L74 4F4 F A20WE E20EA 19951027001851995102700185NM 1995 10 27 P5CA9500832 119951020A5244 DOOR HINGE BOEING747 747122 1384872NM NR 3 ACM CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 NR 3 ACM FAIRING DOOR FORWARD HINGE HAS EXFOLIATED CORROSION. REMOVED AND REPLACED HINGE IAW SRM 51-10-01. 2L74 4F A20WE 19951027001861995102700186NM 1995 10 27 SCNA95240 119951017A33501000677 EEL ASSY BOEING727 727259 138408JNM AFT ENTRY DOOR INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE AFT ENTRY EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED AFT ENTRY EMERGENCY EXIT LIGHT ASSEMBLY PER MM 33-50-101 AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951027001871995102700187NM 1995 10 27 SCNA95241 119951018A33501102832 BATTERY BOEING727 727227 1384078NM AFT ENTRY DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY EXIT BATTERY PACK PER MM 33-50-61. 2L73 4F A3WE 19951027001881995102700188NM 1995 10 27 SWAA950665 119951018A5312 BLKHD WEB BOEING737 7372H4 138448CNM BS 727 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND PRESSURE BULKHEAD WEB CHAFE DAMAGE AT BS 727 BL 0 WL 185. REPAIRED PER EWO 95-0595 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001891995102700189NM 1995 10 27 SWAA950666 119951018A5313 STRINGERS BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND STRINGER 3L CORRODED UNDER FASTENER BETWEEN BS 380 AND 400. ALSO, FOUND S11R CORRODED BETWEEN BS 478 AND 484. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001901995102700190NM 1995 10 27 SWAA950667 119951018A5313 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND CORROSION BETWEEN S4 AND 6R ON AFT FACE AND O/B FLANGE O/B SURFACE OF FRAME INCLUDING STRINGER CLIP. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001911995102700191NM 1995 10 27 SWAA950668 119951018A5330 SKIN BOEING737 7372H4 138448CNM BS 183 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND FUSELAGE SKIN SCRATCHED AND DENTED AT BS 183 LBL 2 TO RBL 9, FWD OF NOSE BAY ACCESS DOOR. ALSO, SKIN DENTED AT BS 904, ABOVE S25R. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001921995102700192NM 1995 10 27 SWAA950669 119951018A5313 STRINGER BOEING737 7372H4 138448CNM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND STRINGER 4R AND 4L SPLICE JOINT CRACKED AT BS 907. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001931995102700193NM 1995 10 27 SWAA950670 119951018A5320 CHORD BOEING737 7372H4 138448CNM BS 178-180 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND T-CHORD CRACKED BETWEEN BS 178 TO 180, WL 197 LBL 24. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001941995102700194NM 1995 10 27 SWAA950671 119951018A5313 STRINGER BOEING737 7372H4 138448CNM BS 787 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND STRINGER S15L CRACKED AT BS 787. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001951995102700195NM 1995 10 27 SWAA950672 119951018A5311 FRAME BOEING737 7372H4 138448CNM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND FUSELAGE FRAME AND SHEAR TIE CORRODED AT BS 747, RBL 6 TO 9 WL 148. ALSO, SHEAR TIE AT BS 727A BETWEEN 21 AND 22L. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001961995102700196NM 1995 10 27 SWAA950673 119951018A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 7 TO RBL 36 WL 208. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001971995102700197NM 1995 10 27 SWAA950674 119951018A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND THREE HOLES IN KEEL BEAM LOWER FLANGE AND RADIUS AT BS 727+16, RBL 7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001981995102700198NM 1995 10 27 SWAA950675 119951018A5311 FRAME BOEING737 7372H4 138448CNM BS 597 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND FUSE FRAME CRACKED AT BS 597, BL 71 WL 202 ON BOTH RT AND LT SIDES. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027001991995102700199NM 1995 10 27 SWAA950676 119951018A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 710-727 CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0753SW 21534 DURING D-CHECK, FOUND CHAFING DAMAGE ON LOWER O/B FLANGE OF KEEL BEAM BS 710 TO 727, LBL 7 WL 149. REPAIRED PER EWO 95-0596 AND BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951027002001995102700200SO 1995 10 27 SWIA95631 119951006A3231 UP LOCK HOOK EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG DOOR OUT OF ADJUST A SWIAA UNSCHED LANDING O OTHER CLCLIMB 1 NM07205SW 120260 RT A AND B LIGHTS ON RT MAIN GEAR WOULD NOT GO OUT ON RETRACTION, RECYCLED 2 TIMES. SOUNDS LIKE A GEAR DOOR WAS ANGLE DOWN, HEAVY WIND NOISE. ADJUSTED THE RT MLG UPLOCK HOOK/ACUATOR ROD END IAW MM 32-32-09. CYCLED GEAR SEVERAL TIMES, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951027002011995102700201WP 1995 10 27 SWIA95632 219951009A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RIGHT BIRD STRIKE A SWIAO OTHER C F.O.D. APAPPROACH 1 NM0727297 AC735 BIRD STRIKE ON APPROACH TO IPL, INGESTED INTO RT ENGINE. REPLACED RT ENGINE, LK CK GOOD AND NO DISCREPANCIES NOTED. 1L72 4T4 T A8SW E4WE 19951027002021995102700202SW 1995 10 27 SWIA95633 119951014A3260 POS SWITCH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP NLG FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM072699Y AC666 NOSE GEAR LIGHT WOULD NOT COME ON, CYCLED GEAR 3 TIMES THEN NOSE LIGHT CAME ON. REMOVED AND REPLACED RT DOWN POSITION SWITCH, CYCLED GEAR SEVERAL TIMES AND OPS CKS GOOD. 1L72 4T4 T A8SW E4WE 19951027002031995102700203SO 1995 10 27 SWIA95634 119951011A3610 PRESS VALVE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE ENGINE FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07204SW 120243 SHORTLY AFTER TAKEOFF, WE EXPERIENCED A DUCT LEAK WARNING. WE IMMEDIATELY LANDED AND SHUT THE ENGINE DOWN ON THE GROUND. REMOVED AND REPLACED PRESSURE VALUE, OPS RUN AND CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951027002041995102700204EA 1995 10 27 SWIA95635 119951011A3230 RETRACT MECH CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE NLG MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07403SW 7028 NOSE GEAR FAILED TO RETRACT. REMOVED AND REPLACED TOW BRACKET AND REINSTALLED PROX SENSOR. ADJUSTED SWITCH TO 0.045 TO 0.055 BRACKET IAW MM 32-61-05-400-805. 2L72 4F4 FRTA21EA E15NE 19951027002051995102700205SO 1995 10 27 SWIA95636 119950922A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 LT WING RIB 16 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SIDE. REPLACED THREE WING SUPPORT CLIPS ON LT WING RIB 16 IAW SB 120-57-0031, CLIPS INSTALLED. 2L72 4T4 TRTA31SO E20NE 19951027002061995102700206SO 1995 10 27 SWIA95637 119950922A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 LT WING RIB 15 HAS THREE CRACKED WING SUPPORT CLIPS. REPLACED 3 WING SUPPORT CLIPS ON LT WING RIB 15, IAW SB 120-57-0031. 2L72 4T4 TRTA31SO E20NE 19951027002071995102700207SO 1995 10 27 SWIA95638 119950922A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RT WING RIB 15 HAS 3 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 3 WING SUPPORT CLIPS ON RT WING RIB 15. 2L72 4T4 TRTA31SO E20NE 19951027002081995102700208SO 1995 10 27 SWIA95639 119950922A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RT WING RIB 16 HAS 2 CRACKED WING SUPPORT CLIPS ON BOTTOM. REPLACED 2 WING SUPPORT CLIPS ON RT WING RIB 16 IAW SB 120-57-0031. 2L72 4T4 TRTA31SO E20NE 19951027002091995102700209SO 1995 10 27 SWIA95640 119950922A2700 TIP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING DAMAGED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RT WING TIP DAMAGED AND DELAMINATING, NEEDS TO BE REPLACED. FITTED NEW WING TIP FOR RT WING. 2L72 4T4 TRTA31SO E20NE 19951027002101995102700210SO 1995 10 27 SWIA95641 119950923A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RT RUDDER AFT OUTBD CABLE WORN. REPLACED RT RUDDER OUTBD AFT CABLE PER MM 27-00-01. 2L72 4T4 TRTA31SO E20NE 19951027002111995102700211SO 1995 10 27 SWIA95642 119950923A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07212SW 120276 RT RUDDER INBD AFT CABLE WORN. REPLACED RT RUDDER INBD AFT CABLE PER MM 27-00-01. 2L72 4T4 TRTA31SO E20NE 19951027002121995102700212SO 1995 10 27 SWIA95643 119950929A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07205SW 120260 RT RUDDER OUTBD AFT CABLE WORN. REPLACED CABLE IAW MM 27-00-00, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951027002131995102700213SO 1995 10 27 SWIA95644 119950929A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07205SW 120260 RT RUDDER INBD AFT CABLE WORN. REPLACED CABLE IAW MM 27-00-00, OPS CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951027002141995102700214NM 1995 10 27 UPS204809 119951016A33501000679 EEL BOEING727 72725C 138400HNM CABIN MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01933UP 19857 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT ASSY AS YOU ENTER CABIN, WOULD NOT WORK WHEN LIGHTS ARMED AND POWER SHUTDOWN. ASSY WOULD ONLY WORK WITH SWITCH ON, ON THE ASSY ITSELF. REMOVED AND REPLACED ASSY USING ORIGINAL BATTERIES, OPS CHECKED NORMAL. 2L73 4F A3WE 19951027002151995102700215NM 1995 10 27 UPS204810 119951017A2150 ACM BOEING727 72730C 1384009NM LEFT MALFUNCTIONED A IPXAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01906UP 19314 CREW REPORTED, BTB DUE TO SMOKE IN FLIGHT DECK. RAN ENG 1 AT A TIME, ISOLATED PROBLEM TO LT PACK AND DEFERRED PACK PER MEL. REMOVED AND REPLACED LT AIR CYCLE MACHINE PER MM 21-51-12 PG 401. OPS CHECK OFF APU AND ALL ENGS DURING TAXI, NO DEFECTS NOTED. 2L73 4F A3WE 19951027002161995102700216NM 1995 10 27 UPS204811 119951017A5542 SKIN BOEING727 72727C 138400JNM RUDDER CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LOWER RUDDER SKIN ACCESS PANEL 9510. REMOVED CORROSION BY REMOVING BONDED SKIN, FABRICATED REPAIR PARTS AND FINAL INSTALLATION PER SRM 55-20-3. 2L73 4F A3WE 19951027002171995102700217NM 1995 10 27 UPS204812 119951017A5320155PH DOUBLED BOEING727 72727C 138400JNM BS 639 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MID GALLEY DOOR CUTOUT DOUBLER IS CRACKED AT BS 639.0 WL 274.25. STOP DRILLED CRACK, INSTALLED DOUBLER IAW EO B727-5330-2685. 2L73 4F A3WE 19951027002181995102700218NM 1995 10 27 UPS204813 119951017A5330 SKIN BOEING727 72727C 138400JNM BS 265 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HFEC INSPECTION REVEALED CRACK INDICATIONS AT FASTNERS BS 264 AND 265, STRINGER 9 RT ON EXTERIOR SKIN. ACCESS THE DAMAGED AREA, CUTOUT AREA OF SKIN AND FABRICATED REPAIR PARTS. INSTALLED REPAIR PART AND REINSTALLED ITEMS REMOVED FOR ACCESS IAW SRM 53-30-3. 2L73 4F A3WE 19951027002191995102700219NM 1995 10 27 UPS204814 119951017A5313652162910 STRINGER BOEING727 72727C 138400JNM BS 760 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DURING PRESSURE LEAK OF FUEL VENT FOUND FORWARD VENT STRINGER WEB CRACKED AT LBL 26, STA 760 1 INCH LONG. REPAIRED PER UPS EO 727-57-1658. 2L73 4F A3WE 19951027002201995102700220NM 1995 10 27 UPS204815 119951017A5311 FRAME BOEING727 72727C 138400JNM BS 760 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND DISCOVERED CORROSION ON BS 760 FRAME WEB FWD SIDE LBL 70 WL 203. REMOVED CORROSION AND REPAIRED AREA PER EO B727-53-1691. 2L73 4F A3WE 19951027002211995102700221NM 1995 10 27 UPS204816 119951017A5330 SKIN BOEING727 72727C 138400JNM BS 865-870 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND UPON REMOVAL OF RBL 45 LONGITUDINAL BEAM, FUEL CELL UPPER SKIN TO BE CORRODED AT BS 865 TO 870, RBL 45 WL 178. BLENDED OUT CORROSION AND REPAIRED DOUBLER PER EO B727-5730-7514-A. 2L73 4F A3WE 19951027002221995102700222NM 1995 10 27 UPS204817 119951017A5730 SKIN BOEING727 72727C 138400JNM BS 770-800 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 770 TO 800, LBL 64. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. CUT OUT CORRODED SKIN AND REPAIRED PER EO B727-5730-7506-A. 2L73 4F A3WE 19951027002231995102700223NM 1995 10 27 UPS204818 119951017A5730 SKIN BOEING727 72727C 138400JNM BS 775-785 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01909UP 19115 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FUEL CELL UPPER SKIN BS 775 TO 785 RBL 64. CUT OUT CORRODED SECTION OF FUEL CELL SKIN AND REPAIRED PER EO B727-5730-7507-A. 2L73 4F A3WE 19951027002241995102700224NM 1995 10 27 UPS404803 119951013A2612 FIRE WARNING BOEING747 747123F NM FLIGHT DECK ACTIVATED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01674UP 20100 PILOT REPORTED, SHORTLY AFTER T/O FIRE WARNING BELL AND LIGHT ACTIVATED FOR APPROX .5 SECOND. DUE TO THE SHORT DURATION OF WARNING, COULD NOT PINPOINT WHICH ENGINE BUT JUMPSEAT MECHANIC SAID DEFINITELY NR 3 OR NR 4 FIRE WARNINGS TESTED AND ALL CK OK. NR 4 ENG COMPARISON RUNS PERFORMED UP TO TAKEOFF POWER, COULD NOT DUPLICATE FIRE WARNING DISCREPANCIES. REPLACED A7 AND A11 FIRE WARNING CARDS, SYSTEMS OPS CHECKED GOOD IAW MM 26-11-00. 2L74 4F A20WE 19951027002251995102700225NM 1995 10 27 UPS404804 119951014A335051356B37 EEL BOEING747 747123F NM UPPER DECK INOP A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01675UP 20390 MAINTENANCE REPORTED, UD RT EMERGENCY LT OUT. INSTALLED SERVICABLE EMERGENCY LIGHT ASSEMBLY IN UPPER DECK MM 33-50, (P/N 51356B37), OFF (S/N 291-1571), ON (S/N 104-029). 2L74 4F A20WE 19951027002261995102700226NM 1995 10 27 UPS404805 119951013A5753 SKIN BOEING747 747121 1384871NM RT TE FOREFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01690UP 20348 WHILE ON GROUND, MAINTENANCE FOUND RT INBD FOREFLAP INBD EDGE HAS A CRACK APPROX 2.5 INCHES LENGTH, BEYOND SRM 51-40-09 LIMITS. REPAIRED IAW SRM 51-40-09. 2L74 4F A20WE 19951027002271995102700227NM 1995 10 27 UPS404806 119951013A5753 LE SKIN BOEING747 747121 1384871NM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01690UP 20348 WHILE ON GROUND, MAINTENANCE FOUND RT INBD MIDFLAP LEADING EDGE HAS MULTIPLE CRACKS ON INBD SIDE APPROX 14 INCHES LENGTH, BEYOND SRM 51-40-09 LIMITS. VACUUMED TO CORE TO REMOVE WATER, INSTALLED HOT BONDED REPAIR PER SRM 51-40-12, PRIMED AND PAINTED LEADING EDGE. 2L74 4F A20WE 19951027002281995102700228NM 1995 10 27 UPS404808 119951016A3350 BATTERY BOEING747 747SR46 NM UPPER DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01691UP 20784 WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK DOOR EMERGENCY LIGHT INOP. DURING TEST, ALL EXIT LIGHT CAME ON WITH EXCEPTION OF TWO WHITE LIGHTS AT UPPER DECK DOOR SILL WHICH CAME ON, THEN WENT OUT. UPPER DOOR RENDERED INOP, DEFERRED PER MEL 33-13. WHILE ON GROUND, MAINTENANCE FOUND WITH CHARGED BATTERIES OPS CK GOOD. THIS CLEARS DMI NR M99481 PLACARD REMOVED. 2L74 4F A20WE 19951027002291995102700229NM 1995 10 27 UPS404821 119951017A3350135610A BATTERY PACK BOEING747 747123 1384873NM UPPER DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 WHILE ON GROUND, MAINTENANCE FOUND UPPER DECK EMERGENCY LIGHT ASSEMBLY INOPERATIVE. INSTALLED SERVICABLE BATTERY PACK ON UPPER DECK EMERGENCY LIGHT ASSEMBLY PER MM 33-50. 2L74 4F A20WE 19951027002301995102700230NM 1995 10 27 UPS504822 119951018A3350S231T3002113 EEL INDICATOR BOEING757 75724APF 1384969NM FLIGHT DECK INOPERATIVE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01431UP 25462 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT UNARMED INDICATOR WOULD NOT RELAMP, A/C 431. REMOVED AND REPLACED UNARMED INDICATOR LIGHT ASSY, (P/N S231T300-2113) ALT (P/N BCREF 8550) PER IPC 33-51-08-02-15. 2L72 4F RTA2NM 19951027002311995102700231WP 1995 10 27 UPS804807 119951015A3232 RETRACT MECH DOUG DC8 DC871F 302199DWP LT MLG DOOR MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01715UP 45915 CREW REPORTED, AFTER T/O AND GEAR RAISED, DOORS NOT LATCHED LIGHT STAYED ON. RECYCLED GEAR AND COMPLIED WITH CHECK LIST, LIGHT REMAINED ON, CONTINUED TO SDF AT M 0.6. INSTALLED NEW CABLE PULLEY IN LT MLG DOOR FOLLOW-UP SYSTEM. LT MLG DOOR FOLLOW-UP SYS REQUIRES ADJ TEST. ADJUSTED LT MLG DOOR FOLLOW-UP MECHANISM IAW UPLATCH MECHANISM IAW DC8 MM 32-31-04. TEST GOOD, NO GEAR DOOR LIGHT DISCREPANCIES NOTED. 2L74 4F RT4A25 19951027002321995102700232WP 1995 10 27 UPS804819 119951016A33505708458503 EMERG BATT PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01880UP 46080 WHILE ON GROUND, MAINTENANCE FOUND ON PREFLIGHT BOTH EMERG LIGHTING BATTERY PACK AND MAIN SHIPS BATTERY LOW. REMOVED AND REPLACED BOTH EMERG LIGHTING BATTERY PACK AND MAIN SHIPS BATTERY, OPS CKS GOOD. 2L74 4F RT4A25 19951027002331995102700233WP 1995 10 27 UPS804823 119951018A8011 STARTER DOUG DC8 DC873F 302199FWP NR 1 ENGINE FAILED A IPXAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01805UP 46117 CREW REPORTED, ON CLIMBOUT NR 1 OIL QUANTITY DROPPED TO 2 QTS, THEN PROGRESSIVELY DROPPED TO 0. OIL PRESSURE STARTED TO FLUCTUATE NR 1 ENGINE SHUTDOWN, OCCURRED AT FL 310. WINDMILLING DATA N1 28.9, N2 14.9, 0 PSI OIL PRESSURE, 0 OIL QUANTITY. ENG OIL LOSS GAUGED BY STARTER INTERNAL FAILURE. REMOVED AND REPLACED STARTER ASSY AS PER MM 80-10-01, SERVICED STARTER OIL AND ENG OIL QTY TO PROPER LEVEL. RAN OPS, CK'D STARTER AND ENG FOR LEAKS, NO LEAKS FOUND. 2L74 4F RT4A25 19951027002341995102700234EU 1995 10 27 WWMA9500067 119951018A61201680640 MONOPOLE WOODWARD 8210263 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT PROP GOV INTERMITTENT A WWMAA UNSCHED LANDING O OTHER CRCRUISE 1 WP15965AE 2481609 965 DURING EN ROUTE PORTION OF FLIGHT, THE LEFT ENGINE TORQUE AND EGT DROPPED RADICALLY WITH THE POWER LEVERS MATCHED. CREW PERFORMED A PRECAUTIONARY LANDING IN SBP WITHOUT INCIDENT. DURING DEBRIEF THE CREW REPORTED THAT THE LEFT TORQUE HAD DROPPED 20 PERCENT. UPON APPROACH INTO SBP BOTH POWER LEVERS WERE PULLED TO FLIGHT IDLE TO DECREASE AIRCRAFT SPEED, THEN ADVANCED TO APPROX 45 TO 50 PERCENT TORQUE AND BOTH MOTORS RESPONDED NORMALLY. MAINTENANCE FOUND THE LEFT ENGINE PROPELLER GOVERNOR MONOPOLE INTERMITTENT. THE MONOPOLE WAS REPLACED, AIRCRAFT WAS TEST FLOWN AND ALL OPERATIONS WERE NORMAL. THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T4 TRTA56EU E4WE 19951027002351995102700235EU 1995 10 27 WWMA9500068 119951018A2120 AIR DISTR BAG JETSTMJETSTM3201 1500217EU CABIN SMOKE A WWMAAG UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15949AE 949 THE FLIGHT CREW OBSERVED SMOKE IN THE REAR PORTION OF THE PASSENGER CABIN, REPORTED IT APPEARED TO ORIGINATE FROM THE AIR CONDITIONER. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR CONDITIONING BLOWER AND FAN FOR ANY EVIDENCE OF BURNING OR SMOKE. ALSO, THE FREON AIR CONDITIONING SYSTEM WAS INSPECTED, NO EVIDENCE OF SMOKE OR BURNING WAS FOUND. THE AIRCRAFT WAS GROUND RUN FOR 45 MINUTES WITH ALL THE AIR CONDITIONING SYSTEMS RUNNING, NO DEFECTS NOTED. THE AIR CRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA56EU 19951027002361995102700236EU 1995 10 27 WWMA9500069 119951018A32407224105661 ACCUMULATOR SAAB SF340 340B 7860101EU LT INBD BRAKES FAILED A WWMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP15313AE 340B313 ON TAXI, THE CAPTAIN REPORTED THE BRAKES FAILED ON THE LEFT SIDE, BOTH PEDALS. RETURNING TO THE GATE, BRAKE EFFECTIVENESS WAS RETURNED APPROXIMATELY 25 TO 50 PERCENT. MAINTENANCE REPLACED THE INBOARD BRAKE ACCUMULATOR AND BLED BRAKES. THE AIRCRAFT WAS TAXI CHECKED AND RELEASED TO SERVICE. 2L72 4T RTA52EU 19951027002371995102700237EU 1995 10 27 WWMA950070 119951018A324114004120 CAP SAAB SF340 340B 7860101EU NR 4 A/S XDUCER DEFECTIVE A WWMAO OTHER O OTHER TXTAXI/GRND HDL 1 WP15313AE 340B313 PILOT REPORTED, THE BRAKES FAILED ON THE CAPTAIN'S SIDE, BOTH PEDALS. CYCLED THE BRAKE ANTI-SKID SWITCH WITHOUT RESTORING THE BRAKE EFFECTIVENESS. THIS WAS THE SECOND OCCURANCE OF THE SAME PROBLEM ON THE SAME DAY. MAINTENANCE FOUND THE NR 4 MAIN LANDING GEAR TIRE CAP TO BE LOOSELY FITTED TO THE ANTI-SKID TRANSDUCER. REPLACED THE TIRE CAP, ALL OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RELEASED WITH NO FURTHER PROBLEMS. 2L72 4T RTA52EU 19951027002391995102700239WP 1995 10 27 9516369882 119951021A3010 DE-ICE SYST DOUG DC9 DC951 3022051WP EMPENAGE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01670MC 47659 DURING CRUISE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED INTERMITTENTLY WITH TAIL DE-ICE ACTIVATED. AIRCRAFT DIVERTED TO FSD AND LANDED WITHOUT INCIDENT. REPLACED TAIL SHUTOFF VALVE, PRESSURE SWITCH, AND AIRFOIL PRESSURE DELAY RELAY AND OPERATIONAL TEST GOOD. 2L72 4F A6WE 19951027002401995102700240NM 1995 10 27 95FDEA01582 119951023A5330 SKIN BOEING727 72725C 138400HNM BS 441 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 LFEC INSP INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23 TO 24 RT FWD LAP. REMOVED CORROSION AND INSTALLED 6.5 INCH BY 14 INCH DOUBLER PER SRM 53-30-4. 2L73 4F A3WE 19951027002411995102700241NM 1995 10 27 95FDEA01583 119951023A5313 STRINGER BOEING727 727225 1384077NM BS 1613 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION IN STRINGER AT BS 1613 LBL 15 WL 150. REPAIRED STR PER SRM 53-40-3. 2L73 4F A3WE 19951027002421995102700242NM 1995 10 27 95FDEA01585 119951023A5311 FRAME BOEING727 727225 1384077NM BS 320 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21272 CRACK IN FRAME AT BS 320, JUST ABOVE STR 22L APPROX WL 175 LBL 49. REPAIRED CRACK IN FRAME AT BS 320, JUST ABOVE STR 21L APPROX WL 175 LBL 49 PER FEDEX SRM 51-40-02. 2L73 4F A3WE 19951027002431995102700243NM 1995 10 27 95FDEA01586 119951023A5313 STRINGER BOEING727 72725 1384006NM BS 556 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25152FE 18285 STR 28L CORRODED OUT OF LIMITS AT BS 556. REMOVED AND REPLACED FABRICATED STR SPLICE FROM BS 556 TO 607 IAW SRM 53-10-3. 2L73 4F A3WE 19951027002441995102700244NM 1995 10 27 95FDEA01587 119951023A531465564418 KEEL BEAM BOEING727 727227 1384078NM BS 950-1000 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CORROSION (71C712-00), AFT CARGO BAY NUMEROUS CORROSION FOUND ON KEEL BEAM FLANGE BS 950 TO 1000 STR 29R. REMOVED RT KEEL BEAM STR 29 RECEIVED NEW KEEL BEAM, DRILLED AND INSTALLED PER EO 7-5310-7-2356C PART 1 AND 7, FEDEX EA 7-5310-25739. 2L73 4F A3WE 19951027002451995102700245WP 1995 10 27 95UAL900116 119950906A5753ARC14555014G FLAP VANE DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE TE FLAP DEPARTED A UALAK NONE D INFLIGHT SEPARATION APAPPROACH 1 WP291857U 46986 DURING APPROACH TO HNL, A FIVE FOOT SECTION OF FLAP VANE SEPARATED FROM AIRCRAFT. REPLACED VANE, AREA INSPECTED FOR ADDITIONAL DAMAGE, NONE FOUND. 2L73 4F4 F A22WE E23EA 19951027002461995102700246NM 1995 10 27 95UAL900225 119951024A5210411N201611 DOOR HANDLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE PAX DOOR BROKEN A UALAK NONE O OTHER NRNOT REPORTED 1 WP29322UA 23954 PER CREW, THE FORWARD ENTRY DOOR HANDLE HUB BROKE AND HANDLE FELL OFF DOOR. UNABLE TO OPEN FORWARD ENTRY DOOR FROM THE INSIDE. REPLACED HUB ASSEMBLY. 2L72 4F4 FRTA16WE E2GL 19951027002471995102700247 1995 10 27 95UAL900226 419951024A22101FA061014 SOLENOID VALVE BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE AILERON INOPERATIVE A UALAH DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CRCRUISE 1 WP29974UA 21597 AUTOPILOT AILERON CHANNEL INITIATES UNCOMMANDED BANKS IN HEADING HOLD MODE - POPS C.B.D.C. ALSO, CAUSES A 1000 FOOT CLIMB OR DESCENT. REPLACED B-SYSTEM AILERON SOLENOID VALVE AND PERFORMED LEAK CHECK. ALSO, PERFORMED AUTOPILOT FUNCTION TEST, ROLL CHANNEL CAT II TEST, AND PITCH AND CONTROLLER CAT II TEST. CHECKED O.K. 2L72 4F4 F A16WE E2EA 19951027002481995102700248NM 1995 10 27 95UAL900227 119951024A4990 OIL SYST ALLIED SIGNA98CK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE APU MALFUNCTIONED A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP297453U 6391 21907 RETURNED T0 GATE. CABIN FILLED WITH SMOKE FROM AIR CONDITIONING SYSTEM. FOUND THAT APU HAD LOST ALL OIL IN TANK AND OIL IS VISIBLE IN APU EXHAUST. DIAGNOSTIC WAS PERFORMED TO CONFIRM REPORTED OIL LOSS. APU S/N 6391 TESTED OK. UNABLE TO ATTRIBUTE REPORTED OIL LOSS TO APU DEFECT. ACCOMPLISHED C-CHECK AND RETURNED APU TO SERVICE. 2L73 4F4 F A3WE E2EA 19951027002491995102700249NM 1995 10 27 95UAL900228 119951024A5610 WINDOW BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT COCKPIT CRACKED A UALAK NONE O OTHER NRNOT REPORTED 1 WP297291U 21569 FIRST OFFICER'S NR 1R WINDOW ARCED, POPPED AND OUTER PANE CRACKED. 2L73 4F4 F A3WE E2EA 19951027002501995102700250WP 1995 10 27 ABXA9500825 119950616A55303912060501 FITTING DOUG DC9 DC941 302207NWP VERT STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 WHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL STABILIZER, LEFT INBOARD HINGE ATTACH LUG ON THE VERTICAL STABILIZER CORRODED IN THE BEARING BORE. REPAIRED IAW ABX REA D955-11-55-MR. 2L72 4F A6WE 19951027002511995102700251WP 1995 10 27 ABXA9500826 119950621A533099581561 SKIN DOUG DC9 DC941 302207NWP FS 541-643 NO EDGE DISTANT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47492 DURING D-CHECK ACCEPTANCE INSPECTION WHILE REPLACING THE RIGHT WINDOW BELT PANEL, FROM FS 541 TO 643, FOUND THE PANEL HAD NO EDGE DISTANCE ON ONE FASTENER IN THE LOWER AFT CORNER. REPAIRED IAW ABX REA D953-11945-MR. 2L72 4F A6WE 19951027002521995102700252WP 1995 10 27 ABXA9500827 119950729A5755369232511 FITTING DOUG DC9 DC941 302207NWP RT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23968AX 47499 DURING COMPLIANCE OF AD 85-01-03, ASB 27-228, 27-229 AND EAAD 27-3209D, FOUND CRACK INDICATION ON THE RIGHT WING OUTBOARD SPOILER AFT FITTING. REPLACED SPOILER AFT DRIVE LINK IAW DC-9 MM 27-61-1, OPS CHECKED GOOD. 2L72 4F A6WE 19951027002531995102700253WP 1995 10 27 ABXA9500828 119951014A3231NAS110420D BOLT DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND DRIVER ROD AND SECONDARY ROD ATTACH POINT HAD PLAY ON THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002541995102700254WP 1995 10 27 ABXA9500829 119951014A3231S221037614101 BUSHING DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47494 DURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVER ROD AND SECONDARY ROD ATTACH POINT HAD EXCESSIVE PLAY. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002551995102700255WP 1995 10 27 ABXA9500830 119951014A3231AN960D716L SHIM DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23970AX 47491 WHILE COMPLYING WITH SD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR LINK HAD EXCESSIVE PLAY. REPAIRED ARTICULATING DOOR LINK IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002561995102700256WP 1995 10 27 ABXA9500831 119950824A552059104122 SPAR DOUG DC9 DC915 3022036WP RT ELEVATOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 79-19-02, X-RAY INSPECTION INDICATED A CRACK IN THE RIGHT ELEVATOR SPAR. REPLACED ELEVATOR IAW DC-9 MM 27-30-2. 2L72 4F A6WE 19951027002571995102700257WP 1995 10 27 ABXA9500832 119950824A55105912481517 FITTING DOUG DC9 DC933F 302207AWP HORIZ STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23932AX 47465 DURING COMPLIANCE OF AD 82-06-02, SB 55-32, FOUND A CRACK AT FORWARD UPPER RIGHT HAND HI-LOCK IN THE REAR SPAR FITTING. REPLACED CONSTANT SECTION IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19951027002581995102700258WP 1995 10 27 ABXA9500833 119950707A533059114065 SKIN DOUG DC9 DC931 3022065WP FWD ENTRY DOOR DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C-CHECK INSPECTION, A PREVIOUS REPAIR WAS FOUND TO BE DAMAGED AT THE FORWARD ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-12135-MR. 2L72 4F A6WE 19951027002591995102700259WP 1995 10 27 ABXA9500834 119950707A5330591140659 SKIN DOUG DC9 DC931 3022065WP FWD ENTRY DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23906AX 47072 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, A PREVIOUS REPAIR WAS FOUND CRACKED. REPAIRED IAW ABX REA D953-12134-MR. 2L72 4F A6WE 19951027002601995102700260WP 1995 10 27 ABXA9500835 119950816A3231NA1105 BOLT DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HAD EXCESSIVE PLAY. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002611995102700261WP 1995 10 27 ABXA9500836 119950816A3231NAS1304 BOLT DOUG DC9 DC932 3022066WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD ARTICULATING DOOR HAD EXCESSIVE PLAY. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002621995102700262WP 1995 10 27 ABXA9500837 119950816A3231NAS1104 BOLT DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR HAD EXCESSIVE PLAY. REPAIRED IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002631995102700263WP 1995 10 27 ABXA9500838 119950814A552339181501 SHIELD DOUG DC9 DC932 3022066WP ELEV TAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23985AX 47522 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 92-22-08, FOUND LEFT ELEVATOR GEARED TAB LINK WELL CRACKED. REPAIRED IAW ABX REA D955-12526. 2L72 4F A6WE 19951027002641995102700264WP 1995 10 27 ABXA9500839 119950816A5730 SKIN DOUG DC8 DC863 302198AWP WS 69.5 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23821AX 46113 DURING C-CHECK INSPECTION, FOUND CRACK INDICATIONS AT LEFT LOWER WING STATION XCW 69.5, HOLES 1, 2.A AND C. REPAIRED IAW ABX REA D857-12279-MR. 2L74 4F 4A25 19951027002651995102700265WP 1995 10 27 ABXA9500840 119950808A3231177323 ROD END DOUG DC9 DC914 3022034WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT OUTBOARD GEAR DOOR FORWARD LONG ROD ASSEMBLY HAD A WORN EYEBOLT. REPLACED ROD END IAW DC-9 OHM 32-10-6. 2L72 4F A6WE 19951027002661995102700266WP 1995 10 27 ABXA9500841 119950803A554049138631 TE WEDGE DOUG DC9 DC914 3022034WP RUDDER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 87-08-02, SB 55-23 REV 5, FOUND DEFECT IN RUDDER TRAILING EDGE PHENOLIC WEDGE DURING X-RAY INSPECTION. REPLACED PHENOLIC WEDGE IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19951027002671995102700267WP 1995 10 27 ABXA9500842 119950801A5280591055725N GEAR DOOR DOUG DC9 DC914 3022034WP LT MLG BENT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND TRAILING EDGE OF LEFT OUTBOARD GEAR DOOR BENT. REPLACED SEAL IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19951027002681995102700268WP 1995 10 27 ABXA9500843 119950808A3231S2210370P4101 BUSHING DOUG DC9 DC914 3022034WP LT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 91-22-07, ASB 32-244, FOUND LEFT OUTBOARD GEAR DOOR BEARING ON FORK ASSEMBLY WORN. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19951027002691995102700269WP 1995 10 27 ABXA9500844 119950824A53203616987501 BRACKET DOUG DC9 DC915 3022036WP FS 110 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING C-CHECK INSPECTION, FOUND A PULLEY BRACKET JUST FORWARD OF STA 110 CUT. REPAIRED IAW ABX REA D953-12626-MR. 2L72 4F A6WE 19951027002701995102700270WP 1995 10 27 ABXA9500845 119950820A5330591141623 SKIN DOUG DC9 DC915 3022036WP BS 585/604 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING C-CHECK INSPECTION, FOUND EXTERNAL DOUBLER DAMAGED AT STA 604 AND 585, LONGERON 17L. REPAIRED IAW ABX REA D953-12553-MR. 2L72 4F A6WE 19951027002711995102700271WP 1995 10 27 ABXA9500846 119950808A571159113012 SPAR CAP DOUG DC9 DC914 3022034WP WS 524 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND RIGHT WING AFT SPAR LOWER CAP CORRODED AROUND NUTPLATES OUTBOARD OF AILERON. REPAIRED IAW ABX REA D957-12414-MR. 2L72 4F A6WE 19951027002721995102700272WP 1995 10 27 ABXA9500847 119950802A54005913262 ANGLE DOUG DC9 DC914 3022034WP LT PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-8, FOUND LEFT UPPER PYLON ANGLE CRACKED ATSTA 860. REPAIRED IAW DC-9 SRM 54-04 FIG 10. 2L72 4F A6WE 19951027002731995102700273WP 1995 10 27 ABXA9500848 119950807A53125910163182 BLKHD WEB DOUG DC9 DC914 3022034WP BS 817 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND A GOUGE AND LEVEL I CORROSION IN TWO PLACES ON AFT PRESSURE BULKHEAD WEB FORWARD SIDE, BETWEEN FIVE-THIRTY AND SIX-THIRTY POSITIONS. REPAIRED IAW ABX REA D 953-12405-MR. 2L72 4F A6WE 19951027002741995102700274WP 1995 10 27 ABXA9500849 119950806A535059114233 FAIRING DOUG DC9 DC914 3022034WP FS 699-718 CORROSION A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION ALONG THE PARAMETER OF THE LEFT AFT WING TO BODY FAIRING. REPAIRED IAW ABX REA D953-12379-MR. 2L72 4F A6WE 19951027002751995102700275WP 1995 10 27 ABXA9500850 119950807A533059114243 SKIN DOUG DC9 DC914 3022034WP BS 718 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN FORWARD OF AFT BAG BIN. REPAIRED IAW ABX REA D953-12392-MR. 2L72 4F A6WE 19951027002761995102700276WP 1995 10 27 ABXA9500851 119950808A53205912528501 JAMB DOUG DC9 DC914 3022034WP BS 718-758 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND LOWER AFT CARGO DOOR JAMB CORRODED AT STA 718 TO 758. REPAIRED IAW ABX REA D953-12365-MR. 2L72 4F A6WE 19951027002771995102700277WP 1995 10 27 ABXA9500852 119950808A5320995791739 DOOR FRAME DOUG DC9 DC914 3022034WP BS 758 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR. 2L72 4F A6WE 19951027002781995102700278WP 1995 10 27 ABXA9500853 119950808A53205912528501 DOOR JAMB DOUG DC9 DC914 3022034WP BS 758 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR. 2L72 4F A6WE 19951027002791995102700279WP 1995 10 27 ABXA9500854 119950808A5320591015849 DOOR JAMB DOUG DC9 DC914 3022034WP BS 758 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN DOOR JAMB AREA OF AFT LOWER CARGO COMPARTMENT. REPAIRED IAW ABX REA D953-12393-MR. 2L72 4F A6WE 19951027002801995102700280WP 1995 10 27 ABXA9500855 119950810A53209910164103 ANGLE DOUG DC9 DC914 3022034WP BS 20 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23925AX 45728 DURING C-CHECK INSPECTION, FOUND LEFT UPPER KEEL WEB ANGLE AT STRINGER 17 HAD A HI-LOCK THAT HAD DENTED THE ANGLE. REPAIRED IAW ABX REA D953-12409-MR. 2L72 4F A6WE 19951027002811995102700281WP 1995 10 27 ABXA9500856 119950808A531327779225 LONGERON DOUG DC9 DC932F 3022067WP BS 1089 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 DURING C-CHECK INSPECTION, FOUND A LONGERON SPLICE AT STA 1089, LONGERON 12R MISSING A FASTENER. REPAIRED IAW ABX REA D953-12433-MR. 2L72 4F A6WE 19951027002821995102700282WP 1995 10 27 ABXA9500857 119950811A5330591140659 SKIN DOUG DC9 DC932F 3022067WP FS 205 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 DURING C-CHECK INSPECTION, THREE DENTS WITH GOUGES WERE FOUND JUST AFT OF THE FORWARD ENTRY DOOR BETWEEN LONGERONS 14 AND 15L. REPAIRED IAW ABX REA D953-12498-MR. 2L72 4F A6WE 19951027002831995102700283WP 1995 10 27 ABXA9500858 119950810A56105644324 RETAINER DOUG DC9 DC932F 3022067WP FWD FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, FOUND THE RIGHT OVERHEAD WINDOW OUTER RETAINER CRACKED. REPAIRED IAW ABX EA NR AD-56-03239-MA. 2L72 4F A6WE 19951027002841995102700284WP 1995 10 27 ABXA9500859 119950807A5330591442663 SKIN DOUG DC9 DC932F 3022067WP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 81-26-03, SB A53-147, FOUND A CRACK IN THE FUSELAGE SKIN AT STA 996, LONGERON 7 AND 8L. REPAIRED IAW ABX REA D953-12407-MR. 2L72 4F A6WE 19951027002851995102700285WP 1995 10 27 ABXA9500860 119950809A533039148701 SKIN DOUG DC9 DC932F 3022067WP FWD FUSELAGE DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23909AX 47148 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 94-03-01, A PREVIOUS REPAIR AND INTERNAL DOUBLER WAS FOUND DAMAGED AT THE UPPER FORWARD CORNER OF THE FORWARD ENTRY DOOR JAMB. REPAIRED IAW ABX REA D953-12388-MR. 2L72 4F A6WE 19951027002861995102700286WP 1995 10 27 ABXA9500861 119950906A5320575468827 RETAINER DOUG DC9 DC932 3022066WP BS 128 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03 AND SB 56-11 REV 3, FOUND EVIDENCE OF CRACKS ON TWO FASTENER HOLES ON THE LEFT EYEBROW WINDOW RETAINER, DURING X-RAY INSPECTION. REPLACED RETAINER IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19951027002871995102700287WP 1995 10 27 ABXA9500862 119950826A5320575468828 RETAINER DOUG DC9 DC932 3022066WP BS 128 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03, SB 56-11 REV 3, FOUND CRACKS ON THE EYEBROW WINDOW RETAINER AT FASTENER HOLE ON THE RIGHT SIDE OF AIRCRAFT. REPLACED RETAINER IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19951027002881995102700288WP 1995 10 27 ABXA9500863 119950828A5312591142342 BLKHD WEB DOUG DC9 DC932 3022066WP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 81-26-03, 90-18-03 AND SB 53-147 REV 7, ASB 53-147 REV 4, FOUND CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT SPLICE ABOVE LONGERON 13R AND 11R. REPAIRED IAW ABX REA D953-12628-SB. 2L72 4F A6WE 19951027002891995102700289WP 1995 10 27 ABXA9500864 119950829A53125910163184 BLKHD WEB DOUG DC9 DC932 3022066WP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03, AND SB 53-174 REV 3, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT FOUR HOLES AT THE TEE SPLICE PLATE ABOVE FRP, RIGHT SIDE. REPAIRED IAW DC-9 SB 53-174. 2L72 4F A6WE 19951027002901995102700290WP 1995 10 27 ABXA9500865 119950823A5312591016391 BLKHD T-CAP DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD T-CAP AFT SIDE GOUGED. BLENDED IAW DC-9 SRM 51-01 FIG 1. 2L72 4F A6WE 19951027002911995102700291WP 1995 10 27 ABXA9500866 119950824A5312J06023429 BLKHD PLATE DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5. 2L72 4F A6WE 19951027002921995102700292WP 1995 10 27 ABXA9500867 119950824A5312J06023427 BLKHD PLATE DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND LEFT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5. 2L72 4F A6WE 19951027002931995102700293WP 1995 10 27 ABXA9500868 119950824A5312J06023429 BLKHD PLATE DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5. 2L72 4F A6WE 19951027002941995102700294WP 1995 10 27 ABXA9500869 119950824A5312J06023427 BLKHD PLATE DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03 AND SB 53-174 REV 3, FOUND RIGHT AFT PRESSURE BULKHEAD SPLICE PLATE GOUGED. REPLACED SPLICE PLATE IAW DC-9 SRM 53-11-3 AND 51-30-5. 2L72 4F A6WE 19951027002951995102700295WP 1995 10 27 ABXA9500870 119950829A55305912175514 FAIRING DOUG DC9 DC932 3022066WP VERT STAB CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING CRACKED AT FORWARD END. REPAIRED FAIRING IAW DC-9 SRM 55-03 FIG 17. 2L72 4F A6WE 19951027002961995102700296WP 1995 10 27 ABXA9500871 119950826A55435910257501 TAB DOUG DC9 DC932 3022066WP RUDDER DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SEVERAL SMALL DENTS AND SCRATCHES ON LEFT SIDE OF RUDDER TAB. REPLACED RUDDER TAB IAW DC-9 MM 27-20-2. 2L72 4F A6WE 19951027002971995102700297WP 1995 10 27 ABXA9500872 119950822A57205919573501 DOOR DOUG DC9 DC932 3022066WP WS 324 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING OUTBOARD BUTE DOOR HAD TWO AREAS OF DELAMINATION. REPLACED BUTE DOOR IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 19951027002981995102700298WP 1995 10 27 ABXA9500873 119950831A57535910134147 SKIN DOUG DC9 DC932 3022066WP LT TE FLAP WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION, FOUND LEFT FLAP TOP SIDE SKIN HAD A WORN SPOT AFT OF THE INBOARD END OF THE NR 3 FIXED VANE. REPAIRED IAW ABX REA D957-12653-MR. 2L72 4F A6WE 19951027002991995102700299WP 1995 10 27 ABXA9500874 119950830A534059113661 FITTING DOUG DC9 DC932 3022066WP BS 737 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23905AX 47147 DURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR. 2L72 4F A6WE 19951027003001995102700300WP 1995 10 27 ABXA9500875 119950901A5320591016398 SHEAR TIE DOUG DC9 DC933F 302207AWP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18R. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951027003011995102700301WP 1995 10 27 ABXA9500876 119950901A5320591016397 SHEAR TIE DOUG DC9 DC933F 302207AWP BS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951027003021995102700302WP 1995 10 27 ABXA9500877 119950831A532099577397 SHEAR TIE DOUG DC9 DC933F 302207AWP FS 950 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 950, LONGERON 15R. REPLACED SHEAR TIE IAW DC-9SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951027003031995102700303WP 1995 10 27 ABXA9500878 119950828A5280S22103664C011 BUSHING DOUG DC9 DC933F 302207AWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN OUTBOARD LANDING GEAR DOOR HINGE WORN. HINGE BUSHINGS REPLACED IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19951027003041995102700304WP 1995 10 27 ABXA9500879 119950907A532049162221 FITTING DOUG DC9 DC933F 302207AWP BS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A FITTING CRACKED ON THE AFT SIDE OF A FLOORBEAM AT STA 965, RBL 49. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19951027003051995102700305WP 1995 10 27 ABXA9500880 119950908A532059114065 DOUBLER DOUG DC9 DC933F 302207AWP PAX DOOR AREA DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION AN EXISTING REPAIR WAS FOUND DAMAGED ON THE FORWARD UPPER CORNER OF THE FORWARD ENTRY DOOR. REPAIRED IAW ABX REA D953-12658-MR. 2L72 4F A6WE 19951027003061995102700306WP 1995 10 27 ABXA9500881 119950805A5330592176445 SKIN DOUG DC9 DC933F 302207AWP BS 440 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION, THE FUSELAGE SKIN AT STA 440 AND LONGERON 16L WAS FOUND GOUGED. REPAIRED IAW ABX REA D953-12668-MR. 2L72 4F A6WE 19951027003071995102700307WP 1995 10 27 ABXA9500882 119950907A53159922393501 FLOORBEAM DOUG DC9 DC933F 302207AWP BS 294 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOORBEAM AT STA 294, LBL 1. REPAIRED IAW ABX REA D953-12742-MR. 2L72 4F A6WE 19951027003081995102700308WP 1995 10 27 ABXA9500883 119950909A5311995821429 FRAME DOUG DC9 DC933F 302207AWP BS 897 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION, AN ELONGATED BARREL NUT HOLE WAS DISCOVERED BETWEEN LONGERONS 27R AND 28R AT STA 897. REPAIRED IAW ABX REA D953-12783-MR. 2L72 4F A6WE 19951027003091995102700309WP 1995 10 27 ABXA9500884 119950908A57205912168505 VANE DOUG DC9 DC933F 302207AWP LT WING DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23935AX 47413 DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, THE LEFT WING UPPER MOVEABLE VANE WAS FOUND DENTED. REPLACED VANE IAW DC-9 MM 27-51-2. 2L72 4F A6WE 19951027003101995102700310WP 1995 10 27 ABXA9500889 119950824A53203640085501 BRACKET DOUG DC9 DC915 3022036WP BS 110 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23927AX 45717 DURING C-CHECK INSPECTION, FOUND A PULLEY BRACKET JUST FORWARD OF STA 110 CUT. REPAIRED IAW ABX REA D953-12626-MR. 2L72 4F A6WE 19951027003111995102700311WP 1995 10 27 ABXA9500890 119951023A3350 EEL SOCKET DOUG DC8 DC862 3021970WP COCKPIT STUCK A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23801AX 46077 DURING PREFLIGHT INSPECTION, FOUND DISARM LIGHT INOPERATIVE FOR THE EMERGENCY EXIT LIGHTS. FOUND PRESS-TO-TEST SOCKET FOR THE EMERGENCY EXIT LIGHTING DISARM SWITCH STUCK. FREED SOCKET AND OPERATIONAL CHECK OF DISARM LIGHT WAS GOOD. 2L74 4F 4A25 19951027003121995102700312SO 1995 10 27 COMA9511988 119951023A323112012347001 LATCH ASSY EMB 120 EMB120RT SO LT MLG DOOR BROKEN A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01130G 120130 THE LEFT MAIN LANDING GEAR DID NOT RETRACT. REPLACED A BROKEN LANDING GEAR DOOR LATCH ASSEMBLY. 2L72 4T RTA31SO 19951027003131995102700313 1995 10 27 COMA9511989 419951019A34426222504001 ANTENNA EMB 120 EMB120RT SO RADAR BAY DEFECTIVE A COMAO OTHER O OTHER CLCLIMB 1 SO01130G 8863 277 120130 RADAR CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPLACED THE RADAR ANTENNA. 2L72 4T RTA31SO 19951027003141995102700314SO 1995 10 27 COMA9511990 119951020A5270 WARNING LIGHT EMB 120 EMB120RT SO CARGO DOOR ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01200CD 120200 CARGO DOOR WARNING ILLUMINATED DURING FLIGHT. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST. 2L72 4T RTA31SO 19951027003151995102700315SW 1995 10 27 COMA9520393 119951023A5512 SKIN SWRNGNSA227 SA227AC 8780603SW LT HORIZ STAB LEDENTED A COMAK NONE C F.O.D. UKUNKNOWN 1 SO01703CA AC703 THE LEFT HORIZONTAL STABILIZER LEADING EDGE WAS DENTED BY A BIRD STRIKE. THE DENT WAS FIVE INCHES LONG AT BL 73.43. A FLUSH DOUBLER REPAIR WAS FABRICATED AND INSTALLED PER FAIRCHILD SRM 55-90-10, ARP 55-10-8817. 2L72 4T RTA8SW 19951027003161995102700316EU 1995 10 27 COMA9531173 119951020A6120 CONNECTORS SAAB SF340 SF340A 7850100EU AUTO COARSEN DIRTY A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01380C 340A012 AUTO COARSEN FAILED DURING TAKEOFF. CLEANED CONNECTIONS AT THE P3 ARMING SWITCHES. 2L72 4T RTA52EU 19951027003171995102700317EA 1995 10 27 COMA9560577 119951023A3620356024310 DETECTION LOOP CNDAIRCL600 CL6002B19 EA RT BLEED AIR DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01917CA 7017 RT 14TH STAGE BLEED DUCT WARNING MESSAGE ON EICAS. REPLACED THE PYLON SECTION OF THE RT 14TH STAGE BLEED AIR LEAK DETECTION LOOP. 2L72 4F RTA21EA 19951027003181995102700318EA 1995 10 27 COMA9560578 119951019A323016600101 UPLOCK CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE NLG DEFECTIVE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01914CA4506 7012 THE NOSE LANDING GEAR DID NOT EXTEND, MLG INDICATED DOWN AND LOCKED. REPLACED THE NLG UPLOCK ASSEMBLY. 2L72 4F4 FRTA21EA E15NE 19951027003191995102700319NM 1995 10 27 DHL95742001 119951021A27511812993 INDICATOR BOEING727 727225 1384077NM TE FLAPS FAILED A TDHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01742DH 21290 DURING FLAP RETRACTION 5 DEG TO 2 DEG, BOTH INBD AND OTBD INDICATION DID NOT RETRACT INTO WHITE BAND, REMAINED TWO NEEDLE WIDTHS FROM WHITE BAND. REMOVED AND REPLACED INBD FLAP POSITION INDICATION AND ADJUSTED INBD AND OTBD FLAP POSITION TRANSMITTERS PER MM 27-52-0. NEEDLES NOW IN ALL BANDS GOING UP AND DOWN. 2L73 4F A3WE 19951027003201995102700320 1995 10 27 MWEA95360 419951021A256519D223682 SLIDE DOUG DC9 DC932 3022066WP GALLEY DOOR FAILED TEST A MWEAK NONE O OTHER ININSP/MAINT 1 GL31302ME 47102 DURING ROUTINE TIME CHANGE OF FWD GALLEY SERVICE DOOR EVACUATION SLIDE, THE DEPLOYMENT TEST FAILED. MAINTENANCE FOUND RELEASE LANYARD ROUTED INCORRECTLY INSIDE SLIDE AT BOTTLE REGULATOR. MAINTENANCE REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951027003211995102700321SO 1995 10 27 SWIA95645 119951017A3230 ROD END EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE NLG FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07190SW 120050 AFTER TAKEOFF, COULD NOT RETRACT NOSE GEAR. NOSE GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH A STRONG VIBRATION. REMOVED AND REPLACED UP ACTUATOR ROD END AT GEAR NOSE, SWUNG GEAR AND OPS CKS GOOD IAW MM 32-32-11. 2L72 4T4 TRTA31SO E20NE 19951027003221995102700322SO 1995 10 27 SWIA95646 119951019A3233 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT MLG OUT OF ADJUST A SWIAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 NM07203SW 120240 AFTER TAKEOFF, LT MAIN GEAR REMAINED IN TRANSIT, PULLING THE UP DOWN CONTROL C/B CORRECTED THE RESISTANCE. RETURN TO SLC FOR LANDING. MADE ADJUSTMENTS ON THE LT MLG ACTUATOR IAW MM 33-32-10, CKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951027003231995102700323EA 1995 10 27 SWIA95647 119951022A2751 FAIL MESSAGE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE TE FLAPS ACTIVATED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM07410SW 7066 FLAP FAIL MESSAGE AFTER TAKEOFF. ALSO, FLAP OVERSPEED AURAL WARNING AT 230 KTS. REVIEWED FLAP FAULTS AT FECU AND RESET FECU. OP CK FLAPS, OP CK GOOD. 2L72 4F4 FRTA21EA E15NE 19951027003241995102700324NM 1995 10 27 UPS204853 119951023A2150 PACK BOEING727 72730C 1384009NM LT PACK FAILED A IPXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01906UP 19314 CREW REPORTED, DURING TAKEOFF THRUST AND CLIMBOUT INCREASINGLY BAD FUMES AND SMELL. TURNED OFF NR 1 BLEED AND NR 1 PACK, SMELL WENT AWAY. LATER USED NR 2 BLEED TO SUPPLY NR 1 PACK AND SMELL AND FUMES WERE NOT EXISTANT. DEFERRED MAINTENANCE ITEM ASSIGNED PER MEL 21-1-2, LEFT PACK INOP DUE TO SIGNIFICANT OIL RESIDUE IN COLD AIR DUCTING DOWNSTREAM OF AIR CYCLE MACHINE UP TO AND THROUGH THE WATER SEPARATOR. ALSO, OIL RESIDUE IN 35 DEGREE VALVE DUCTING. 2L73 4F A3WE 19951027003251995102700325NM 1995 10 27 UPS204854 119951023A5753652162479 SKIN BOEING727 727173C 1384059NM LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01938UP 19506 WHILE ON GROUND, MAINTENANCE FOUND LEFT WING INBOARD FLAP TE 3 INCHES FROM OUTBOARD EDGE DELAMINATED 17 INCHES BY 4 INCHES, T/E IS SPLIT 3 INCHES. MAINTENANCE REMOVED AND REPLACED AFT FLAP ASSY IAW MM 27-51, OPS CK NORMAL. 2L73 4F A3WE 19951027003261995102700326NM 1995 10 27 UPS204855 119951023A3350 EEL BOEING727 727247 138408FNM COCKPIT MISINSTALLED A IPXAO OTHER O OTHER CLCLIMB 1 SO01209UP 21698 CREW REPORTED, EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED AFTER DEPARTURE, FOR REMAINDER OF FLIGHT. MAINTENANCE USED THE WRONG TYPE OF LIGHT ASSY FOR THE COCKPIT POSITION, TESTED OK. 2L73 4F A3WE 19951027003271995102700327NM 1995 10 27 UPS204856 119951023A5755 PANELS BOEING727 72725C 138400HNM SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINTENANCE FOUND 34 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS. 2L73 4F A3WE 19951027003281995102700328NM 1995 10 27 UPS204857 119951023A5755 PANEL BOEING727 72725C 138400HNM NR 4 SPOILER CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINTENANCE FOUND NR 4 SPOILER PANEL CRACKED AT ACTUATOR ATTACH POINTS. 2L73 4F A3WE 19951027003291995102700329WP 1995 10 27 UPS204858 119951024A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1766 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND SKIN BULGED ON FS 1766, LONGERON 32R. MAINTENANCE REPAIRED SKIN IAW UPS EO DC8-5330-7522A. 2L74 4F RT4A25 19951027003301995102700330WP 1995 10 27 UPS204859 119951024A5753 SPAR DOUG DC8 DC873F 302199FWP LT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING INBOARD FLAP REAR SPAR CRACKED FROM STA XW 59.5 TO XW 63.6. MAINTENANCE REPAIRED IAW UPS EO DC8-5710-7526A. 2L74 4F RT4A25 19951027003311995102700331WP 1995 10 27 UPS204860 119951024A5543 TAB DOUG DC8 DC873F 302199FWP RUDDER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RUDDER TAB DELAMINATED ON UPPER FORWARD SECTION. MAINTENANCE REPLACED TAB PER MM 27-21-02. 2L74 4F RT4A25 19951027003321995102700332WP 1995 10 27 UPS204861 119951024A5320 FITTING DOUG DC8 DC873F 302199FWP BAG SLIDING DOORCRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BANANA FITTING CRACKED ON FWD SIDE OF B/B X-SLIDING DOOR, LONGERON 33R. MAINTENANCE REPLACED FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003331995102700333WP 1995 10 27 UPS204862 119951024A5320 SHEAR TIES DOUG DC8 DC873F 302199FWP BS 1420 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME SHEAR TIE CRACKED AT FS 1420, LONGERON 3XR. MAINTENANCE REPLACED TIE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003341995102700334NM 1995 10 27 UPS204863 119951024A5744 FITTING BOEING747 747123 1384873NM NR 1 FLAP TRACK CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND FLAP TRACK NR 1 FORWARD SUPPORT FITTING AT WBL 743 INNER BORE CORRODED. MAINTENANCE REPLACED THE FITTING ASSY IAW IPC 57-12-11 ITEM 370. 2L74 4F A20WE 19951027003351995102700335NM 1995 10 27 UPS204866 119951024A5230 CORNER BOEING747 747123 1384873NM L4 DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN AFT LOWER CORNER OF DOOR 4 LT, DURING INTERNAL INSPECTION. MAINTENANCE REPAIRED THE CRACK IAW SRM 52-10-02 FIGURE 10. 2L74 4F A20WE 19951027003361995102700336WP 1995 10 27 UPS804824 119951020A53135264571612000 LONGERON DOUG DC8 DC873F 302199FWP FS 1540/1580 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 33L CRACKED AT FS 1540 AND FS 1580, LONGERON 33R. REPAIRED LONGERONS PER SRM 53-2-2. 2L74 4F RT4A25 19951027003371995102700337WP 1995 10 27 UPS804825 119951020A53135264571612000 LONGERON DOUG DC8 DC873F 302199FWP FS 1656 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 29R, 324 AND 33R CRACKED AT FS 1656. REPAIRED LONGERONS PER SRM 53-2-2 FIGURES 2 TO 6. 2L74 4F RT4A25 19951027003381995102700338WP 1995 10 27 UPS804826 119951020A53204653726501 SPLICE DOUG DC8 DC873F 302199FWP FS 210 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON SPLICE AT FS 210, LONGERON 30R CRACKED. REPLACED SPLICE PER SRM 51-1-20D. 2L74 4F RT4A25 19951027003391995102700339WP 1995 10 27 UPS804827 119951020A53204641324N FITTING DOUG DC8 DC873F 302199FWP FS 1680 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 28L FITTING CRACKED AT FS 1680, FWD SIDE. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951027003401995102700340WP 1995 10 27 UPS804828 119951020A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1346 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN CRACKED FWD UPPER RADIUS RT FWD SERVICE DOOR. REPAIRED PER UPS EO DC8-5310-7471-A. 2L74 4F RT4A25 19951027003411995102700341WP 1995 10 27 UPS804829 119951020A5330 SKIN DOUG DC8 DC873F 302199FWP FS 1340 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN CRACKED AFT UPPER RADIUS LT AFT ENTRY DOOR. REPAIRED PER UPS EO DC8-5310-7470-A. 2L74 4F RT4A25 19951027003421995102700342WP 1995 10 27 UPS804830 119951020A57535701473501 VANE DOUG DC8 DC873F 302199FWP LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 5 FLAP VANE DELAMINATED AT LOWER OUTBOARD END. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19951027003431995102700343WP 1995 10 27 UPS804831 119951020A57535652288505 VANE DOUG DC8 DC873F 302199FWP LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT NR 2 FLAP VANE DELAMINATED AT UPPER OUTBOARD END. REPLACED FLAP VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19951027003441995102700344WP 1995 10 27 UPS804832 119951020A575556551651 PANEL DOUG DC8 DC873F 302199FWP NR 1 SPOILER DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 1 SPOILER PANEL DELAMINATED AT INBOARD END. REPLACED SPOILER ASSY PER MM 27-61-01. 2L74 4F RT4A25 19951027003451995102700345WP 1995 10 27 UPS804833 119951023A5312 BLKHD CHANNEL DOUG DC8 DC873F 302199FWP BS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A 1 INCH CRACK ON CHANNEL BS 683, BULKHEAD, LONGERON 28R. MAINTENANCE REPAIRED CHANNEL IAW SRM 53-2-0. 2L74 4F RT4A25 19951027003461995102700346WP 1995 10 27 UPS804834 119951023A5320 FITTING DOUG DC8 DC873F 302199FWP BS 683 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FITTING HAS HEAVY CORROSION BETWEEN LONGERONS 36 TO 35R, BS 683. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20. 2L74 4F RT4A25 19951027003471995102700347WP 1995 10 27 UPS804835 119951023A5320 DOUBLER DOUG DC8 DC873F 302199FWP X-SLIDE DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND C X-SLIDE DOOR, LOWER FORWARD EXTERNAL CUTOUT DOUBLER CRACKED AND BENT. MAINTENANCE REPLACED THE DOUBLER IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951027003481995102700348WP 1995 10 27 UPS804836 119951023A5312 BULKHEAD DOUG DC8 DC873F 302199FWP BS 683 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 6 INCH CRACK AT PRESSURE BULKHEAD, BS 683 LONGERON 31R. ALSO, A 1.5 INCH CRACK RUNNING AT LONGERON 29R. MAINTENANCE REPLACED THE BULKHEAD ASSY IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003491995102700349WP 1995 10 27 UPS804837 119951023A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 879-884 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L HAS A 5 INCH LONG CRACK AT FS 879 TO 884 LOWER FLANGE RADIUS. MAINTENANCE REPAIRED THE LONGERON IAW SRM 53-2-2. 2L74 4F RT4A25 19951027003501995102700350WP 1995 10 27 UPS804838 119951023A5330 SKIN DOUG DC8 DC873F 302199FWP BS 165 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01819UP 46019 WHILE IN FOR C-CHECK, MAINTENANCE FOUND EXTERIOR SKIN CRACKED 1 INCH LONG AT FS 165. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-2-0. 2L74 4F RT4A25 19951027003511995102700351WP 1995 10 27 UPS804839 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1490-1660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND EXFOLIATION CORROSION AND CRACK, LONGERON 33R BETWEEN FS 1490 TO 1660. MAINTENANCE REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19951027003521995102700352WP 1995 10 27 UPS804840 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERONS 28L AND 28R HAVE HEAVY CORROSION AT FS 1690. MAINTENANCE REPAIRED IAW SRM 53-2-2. 2L74 4F RT4A25 19951027003531995102700353WP 1995 10 27 UPS804841 119951020A5320 DOUBLERS DOUG DC8 DC873F 302199FWP BS 1620-1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 INTERNAL DOUBLERS CORRODED AT FS 1620 TO 1690, LONGERONS 21L TO 21FL. MAINTENANCE REPLACED THE DOUBLERS IAW SRM 51-1-21. 2L74 4F RT4A25 19951027003541995102700354WP 1995 10 27 UPS804842 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1650 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 36 AND END FITTING, FS 1615. MAINTENANCE REPLACED THE FITTING AND REPAIRED LONGERON IAW SRM 53-2-2 AND 51-1-20. 2L74 4F RT4A25 19951027003551995102700355WP 1995 10 27 UPS804843 119951020A5320 FITTING DOUG DC8 DC873F 302199FWP FS 1685 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 26R AT FS 1685. MAINTENANCE REPAIRED IAW SRM 53-2-2 AND 51-1-22. 2L74 4F RT4A25 19951027003561995102700356WP 1995 10 27 UPS804844 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1490-1620 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE ON LONGERON 36, 34 LT AND RT, 35 LT AND RT, AT FS 1490 TO 1620. MAINTENANCE REPLACED ALL 5 LONGERON SECTIONS IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003571995102700357WP 1995 10 27 UPS804845 119951020A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1650-1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION IN FUSELAGE EXTERNAL SKIN AND INNER DOUBLER AT FS 1650 TO 1690, LONGERON 29R TO 32R. MAINTENANCE REPLACED THE SKI AND INNER DOUBLER PER SRM 51-1-21. 2L74 4F RT4A25 19951027003581995102700358WP 1995 10 27 UPS804846 119951020A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1580 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BOLT FRAME CRACKED AT FS 1580, 3 INCHES ABOVE LONGERON 21R. MAINTENANCE REPAIRED THE FRAME IAW SRM 53-2-0. 2L74 4F RT4A25 19951027003591995102700359WP 1995 10 27 UPS804847 119951020A5320 FITTING DOUG DC8 DC873F 302199FWP BS 700 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND END FITTING CRACKED AT FS 700, LONGERON 21L. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20B. 2L74 4F RT4A25 19951027003601995102700360WP 1995 10 27 UPS804848 119951020A5330 SKIN DOUG DC8 DC873F 302199FWP BS 273 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FORWARD BELLY SKIN HAS A 2 INCH CRACK AT FS 273, LONGERON 33R. MAINTENANCE REPLACED BELLY SKIN IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003611995102700361WP 1995 10 27 UPS804849 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 280 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 34L CRACKED ON THE OUTBOARD SIDE, FS 280. MAINTENANCE REPLACED THE LONGERON SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003621995102700362WP 1995 10 27 UPS804850 119951020A5320 FITTING DOUG DC8 DC873F 302199FWP BS 55 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 36 END FITTING CRACKED AT FS 55. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027003631995102700363WP 1995 10 27 UPS804851 119951020A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 879 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L CRACKED AT LOWER SURFACE, FS 879. MAINTENANCE REPAIRED THE LONGERON IAW SRM 53-2-2 FIGURE 9. 2L74 4F RT4A25 19951027003641995102700364WP 1995 10 27 UPS804864 119951024A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01801UP 46101 CREW REPORTED, EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. 2L74 4F RT4A25 19951027003651995102700365NM 1995 10 27 UPS804865 119951024A3350 BATTERY BOEING727 72722C 138400FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01940UP 19101 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS OVER THE FORWARD ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHTING BATTERIES, OPS CK GOOD. 2L73 4F A3WE 19951027003661995102700366EU 1995 10 27 WWMA9500071 119951023A5610 WINDOW SEALER BAG JETSTMJETSTM3201 1500217EU COCKPIT ODOR A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15966AE 966 THE CAPTAIN AND THE FIRST OFFICER REPORTED, SMELLING A SLIGHT ODOR OF ELECTRICAL SMOKE IN THE COCKPIT. THEY STATED THAT THEY COULD NOT DETERMINE THE SOURCE AND IT WAS NOT A STRONG ODOR, BUT THE ODOR DID COME AND GO. MAINTENANCE INSPECTED THE COCKPIT AND NOSE BAY AREA AND COULD NOT FIND ANY PROBLEMS OR SMELL. UPON FURTHER INVESTIGATION IT WAS DETERMINED WITH THE FLIGHT CREWS CONCURRENCE THAT THE SMELL WAS PRC SEALANT, THAT WAS USED TO RESENTLY INSTALL A NEW COCKPIT SIDE WINDOW. THE AIRCRAFT WAS RELEASED WITH NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19951027003671995102700367WP 1995 10 27 9516379967 119951001A5312 BLKHD WEB DOUG DC9 DC931 3022065WP FS 965 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND OIL CANNING IN THE FS 965 PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED WEB (P/N 9912243-3), PER EA 99-103284. 2L72 4F A6WE 19951027003681995102700368WP 1995 10 27 9516389967 119951004A5347 SEAT TRACK DOUG DC9 DC931 3022065WP FS 240 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019331 47263 DURING H-CHECK, FOUND CORROSION ON THE RIGHT INBOARD SEAT TRACK AT FS 240. REPAIRED TRACK (P/N 5910820-5), PER EA 99-103299. 2L72 4F A6WE 19951027003691995102700369NM 1995 10 27 9516396611 119951005A5315 FLOORBEAM BOEING747 747251B 1384892NM FS 460 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611US 20356 DURING PERIODIC CHECK, FOUND A ONE INCH CRACK IN THE UPPER DECK FLOORBEAM WEB, FS 460 RBL 88. REPAIRED WEB (P/N 65B10933-502), PER EA 66-99126. 2L74 4F A20WE 19951027003701995102700370NM 1995 10 27 9516406611 119951006A5313 LONGERON BOEING747 747251B 1384892NM FS 1466 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611US 20356 DURING PERIODIC CHECK, FOUND A CRACK IN STR 8R, BS 1466. REPAIRED STRINGER (P/N 65B07229-34), PER EA 66-99123. 2L74 4F A20WE 19951027003711995102700371NM 1995 10 27 9516416611 119951006A5313 LONGERON BOEING747 747251B 1384892NM FS 1307-1331 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611US 20356 DURING PERIODIC CHECK, FOUND TWO CRACKS, 0.75 AND 0.90 INCH STR 8R BS 1307, 1331 RESPECTIVELY. REPAIRED STRINGER (P/N 65B07229-34), PER EA 66-99128. 2L74 4F A20WE 19951027003721995102700372NM 1995 10 27 9516426611 119951006A5313 LONGERON BOEING747 747251B 1384892NM FS 1430-1458 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01611US 20356 DURING PERIODIC CHECK, FOUND TWO CRACKS, 1.1 AND 0.5 INCH IN STR 9R BS 1430, 1458 RESPECTIVELY. REPAIRED STRINGER (P/N 65B07229-8), PER EA 66-99128, -99157. 2L74 4F A20WE 19951027003731995102700373NM 1995 10 27 9516432289 119951007A5315 FLOORBEAM BOEING727 727251 138408HNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01289US 21377 DURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD BS 1130, LBL 15 TO 21. REPAIRED BEAM (P/N 65-86168) PER EA 22-99216. 2L73 4F A3WE 19951027003741995102700374NM 1995 10 27 9516442289 119951010A5315 FLOORBEAM BOEING727 727251 138408HNM FS 344 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01289US 21377 DURING PERIODIC CHECK, FOUND CORROSION ON THE FLOORBEAM UPPER CHORD BS 344, LBL 50 RBL 18. REPAIRED BEAM PER EA 22-99337. 2L73 4F A3WE 19951027003751995102700375WP 1995 10 27 9516459873 119951011A5312 BLKHD WEB DOUG DC9 DC951 3022051WP FS 1167 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01782NC 48107 DURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB FS 1167, LEFT AND RIGHT SIDES. REPAIRED WEB (P/N 9912243-81, -83, -84) PER EA 98-102596. 2L72 4F A6WE 19951027003761995102700376EU 1995 10 27 9516463210 119951012A5313 LONGERON AIRBUS320 A320211 3930320EU FS 13767-15367 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01310NW 121 DURING IL CHECK, FOUND CORROSION IN STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-201), PER EA 32-104278, -104279. 2L72 4F RTA28NM 19951027003771995102700377EU 1995 10 27 9516473210 119951012A5313 LONGERON AIRBUS320 A320211 3930320EU FS 14300-14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01310NW 121 DURING IL CHECK, FOUND CORROSION ON STR 44 BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31521-200), PER EA 32-104280. 2L72 4F RTA28NM 19951027003781995102700378WP 1995 10 27 9516489873 119951012A5220 DOOR PAN DOUG DC9 DC951 3022051WP OVERWING EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01782NC 48107 DURING H-CHECK, FOUND A CRACK IN THE RIGHT AFT EMERGENCY OVERWING EXIT DOOR PAN AT THE UPPER AFT DOOR STOP. REPAIRED PAN (P/N 5913195-1), PER EA 98-103292. 2L72 4F A6WE 19951027003791995102700379NM 1995 10 27 9516492289 119951013A5320 BEAM BOEING727 727251 138408HNM TAILSKID CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01289US 21377 DURING PERIODIC CHECK, FOUND CORROSION ON THE TAILSKID ACTUATOR BEAM LOWER CHORD LBL 12 TO 18. REPAIRED CHORD (P/N 65-26307-8), PER EA 22-99219. 2L73 4F A3WE 19951027003801995102700380WP 1995 10 27 9516509311 119951017A5241 SKIN DOUG DC9 DC982 3022082WP GALLEY DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01314RC 49110 DURING LINE CHECK, FOUND A CRACK IN THE SKIN OF DOOR 4L AT THE DOOR HANDLE CUTOUT. REPLACED CRACKED CASTING AND REPAIRED SKIN PER SRM 52-05 FIG 20A. 2L72 4F A6WE 19951027003811995102700381NM 1995 10 27 9516515502 119951017A5320 SILL BOEING757 757251 1384970NM NR 3 EMER EXIT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01502US 23191 DURING T-CHECK, FOUND CORROSION ON THE NR 3 EMERGENCY EXIT DOOR LOWER SILL INNER CHORD. REPAIRED CHORD (P/N 146N8326-2), PER EA 55-104324. 2L72 4F RTA2NM 19951027003821995102700382WP 1995 10 27 9516529979 119951018A5313 LONGERON DOUG DC9 DC931 3022065WP FS 605 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 28R AND 29R END FITTINGS AT FS 605. REPLACED FITTINGS PER SRM 51-30-5. 2L72 4F A6WE 19951027003831995102700383NM 1995 10 27 9516532289 119951022A3230 RETRACT MECH BOEING727 727251 138408HNM NLG LACK OF LUBE A NWAAK NONE O OTHER APAPPROACH 1 GL01289US 21377 UPON GEAR EXTENSION, NOSE GEAR HUNG UP FOR ABOUT 30 SECONDS AND EXTENDED NORMALLY, BUT WITH A LOUD THUMPING NOISE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE VISUALLY CHECKED NOSE LANDING GEAR FOR CRACKS, NONE FOUND. NOSE GEAR WAS GREASED AND AN OPERATIONAL CHECK AND INSPECTION WAS PERFORMED. 2L73 4F A3WE 19951027003841995102700384 1995 10 27 9516543230 419951023A3441 IRU AIRBUS320 A320211 3930320EU NR 1 FAILED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 GL01330NW 307 SHORTLY AFTER LEVEL OFF AT FL 310, AIRCRAFT WENT INTO ALTERNATE YAW. AIRCRAFT RETURNED TO MSP WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA IRU AND NR 2 SPOILER ELEVATOR COMPUTER, OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951027003851995102700385WP 1995 10 27 9516559958 119951024A3222 STRUT DOUG DC9 DC931 3022065WP NLG REQD SERVICE A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01917RW 47145 DURING CLIMB, LANDING GEAR WOULD NOT RETRACT. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND LANDING GEAR RETRACTED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND NOSE LANDING GEAR STRUT LOW. SERVICED NOSE LANDING GEAR STRUT, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027003861995102700386NM 1995 10 27 9516562295 119951024A2780 SAFETY LOCK BOEING727 727251 138408HNM NR 4 LE FLAP MISSING A NWAAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CLCLIMB 1 GL01295US 21506 NR 4 LEADING EDGE FLAP WOULD NOT RETRACT ON FLAP RETRACTION, AFTER TAKEOFF. FLAP POSITION AMBER LIGHT REMAINS ILLUMINATED WHEN FLAPS AT ZERO. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SAFETY LOCK MISSING ON SWITCH. ADJUSTED BOLT AND INSTALLED NEW LOCK, GROUND TEST NORMAL. 2L73 4F A3WE 19951027003871995102700387NM 1995 10 27 9516576310 119951024A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01670US 24225 DURING LINE CHECK, THE EMERGENCY PATH LIGHTS BETWEEN ROWS 26 TO 35 RIGHT WERE FOUND INOPERATIVE. RECONNECTED EMERGENCY PATH LIGHTS AT ROW 26, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951027003881995102700388WP 1995 10 27 9516589926 119951020A5350 RELEASE CABLE DOUG DC9 DC932 3022066WP TAILCONE FRAYED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR HANDLE FROM THE CLIPS AND TO DROP THE TAILCONE. ALSO, FOUND A FRAYED RELEASE CABLE AND A WORN UPPER LEFT SLIDER BLOCK. REPLACED THE CABLE AND SLIDER BLOCK AND RERIGGED THE RELEASE SYSTEM, CHECKED OK. 2L72 4F A6WE 19951027003891995102700389NM 1995 10 27 95FDEA01588 119951024A5330 SKIN BOEING727 72722 1384002NM BS 1120 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DENT IN SKIN AT STA 1120, BETWEEN STR 17 TO 18 R. REPAIRED DENT AT BS 1120 WL 204 BETWEEN STR 17 TO 18R. ALL WORK DONE IAW FEDEX SRM 53-30-3 FIG 1. 2L73 4F A3WE 19951027003901995102700390NM 1995 10 27 95FDEA01589 119951024A532065207264 STRAP BOEING727 72722 1384002NM BS 524-576 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION UNDER NUTPLATES ON THRESHOLD STRAP, STA 524 TO 576 RBL 24 WL 156, FWD BAY. 2L73 4F A3WE 19951027003911995102700391NM 1995 10 27 95FDEA01590 119951024A5530 STRINGER BOEING727 727225 1384077NM VERT FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 NR 7 STR IS CRACKED AT VERTICAL FIN STA 133.80 LT SIDE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX 55-30-4. 2L73 4F A3WE 19951027003921995102700392NM 1995 10 27 95FDEA01591 119951024A5330 STRINGER BOEING727 727225 1384077NM VERT FIN CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 NR 8 STRINGER IS CRACKED AT VERTICAL FIN STA 133.80 RT SIDE. REMOVED DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX 55-30-4. 2L73 4F A3WE 19951027003931995102700393NM 1995 10 27 95FDEA01592 119951024A5313 STRINGER BOEING727 727225 1384077NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON STRINGER AT BS 720F PLUS 16 LBL 23 WL 152. REPAIRED STR PER FEDEX SRM 53-10-5. 2L73 4F A3WE 19951027003941995102700394NM 1995 10 27 95FDEA01593 119951024A5320 CHORD BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 ON BL 70.5 LT RIB UPPER CHORD NOTED CRACKS IN THE FOLLOWING HOLES, FWD UPPER AND LOWER CRACKS APPROX 0.040 INCH LENGTH. NOTED DAMAGE AND/OR CRACK IN AFT LOWER HOLE. ALL NOTED IND MARKED ON A/C, CRACKS IN T-CHORD BS 760, LBL 70.5 WL 204. REPAIRED DISCREPENT HOLE PER FEDEX EO NR 7-5310-25982. 2L73 4F A3WE 19951027003951995102700395NM 1995 10 27 95FDEA01594 119951025A4900 APU BOEING727 727233 138408ANM AFT FUS FIRE A FDEAF ACTIVATE FIRE EXT. A FLAME/FIRE UKUNKNOWN 1 SO25272FE 22037 GROUND CREW REPORTED, APU W/N LIGHT OFF OR SHUTDOWN, RESIDUAL FUEL IGNITED CAUSING FIRE AND FIRE BOTTLE DISCHARGED. STARTED APU 3 TIMES, OPS CK GOOD. APU SHUTDOWN NORMALLY WITH MASTER SW OR FIRE HANDLE. SUSPECT NO LIGHT ON APU WAS CAUSED BY COLD SOAKED APU. FOUND CANNON PLUG FOR APU FIRE BOTTLE SQUIB DISCONNECTED, BOTTLE DID NOT DISCHARGE. CONNECTED SQUIB CANNON PLUG AND PERFORMED FIRING CIRCUIT PER CREW DEBRIEF, APU FUEL S/O VALVE STILL IND OPEN, NO TIME TO WORK. INSP A/C AND FOUND NO DAMAGE. RELEASE A/C PER MEL 49-1, CAT C, CONT 1024046, EXP 11-3-95. SUSPECT FIRE WAS CAUSED FROM RESIDUAL FUEL LIGHTING OFF. APU CONT C/B PULLED CONTINUITY CK IAW MM. 26-23-0 OPS CK GD. REMOVED FROM DDL. 2L73 4F RTA3WE 19951027003961995102700396NM 1995 10 27 95FDEA01595 119951023A5315 FLOORBEAM BOEING727 727227 1384078NM BS 400 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 FLOORBEAM HEAVY CORROSION ON STA 400 RBL 35 BOTTOM SIDE NR 0360. INSTALLED DOUBLER PER SRM 53-10-8, SEE NR 1032. 2L73 4F A3WE 19951027003971995102700397NM 1995 10 27 95FDEA01596 119951011A5312 BLKHD ANGLE BOEING727 727227 1384078NM BS 1183 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 AFT CARGO RT 1183 BULKHEAD CRACKED HORIZONTAL ANGLE JUST BELOW FLOOR LINE RBL 50. REMOVED DAMAGED PART AND INSTALLED NEW ANGLE PER SRM 51-10-1. 2L73 4F A3WE 19951027003981995102700398NM 1995 10 27 95FDEA01597 119951024A5320 INTERCOSTAL BOEING727 72725C 138400HNM BS 1110 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 AFT CARGO CEILING CORROSION AROUND NUTPLATES STA 1110 AT BL 0. REMOVED CORROSION AND REPAIRED BOTTOM CAP OF BL 0 INTERCOSTAL STA 1110 PER ESO 11782 WITH FEDEX EA 7-5310-25785. 2L73 4F A3WE 19951027003991995102700399NM 1995 10 27 95UAL900229 119951025A2120 AIR DISTRIBUTION BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN ODOR A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP297451U 21905 FUMES IN CABIN, SUSPECT APU. ACCOMPLISHED TROUBLE SHOOTING PER MM 49-00-08 H8. CLEANED ACCESSORY CASE AT PUMP AREA, CHECKED VENT, RAN APU AND BOTH PACKS HOT AND COLD FOR 1 HOUR AND NO OIL OR SMOKE SMELL. 2L73 4F4 F A3WE E2EA 19951027004001995102700400CE 1995 10 27 BIER950023 119951024A2750S19061 LIMIT SWITCH CESSNA172 172C 2072408CE FLAP LEVER MALFUNCTIONED B BIEAA UNSCHED LANDING J WARNING INDICATION LDLANDING 1 EA21622587169 17275236 FLAPS FAILED TO EXTEND FOR LANDING, FOUND LOWER LIMIT SWITCH ON FLAP LEVER/SWITCH NOT ACTUATING. 1H71 3O NT3A12 19951027004011995102700401SO 1995 10 27 BIER950024 119951024A28212523903 FITTING PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA FUEL SERVO CORRODED A BIEAK NONE O OTHER ININSP/MAINT 1 EA213521S 317952107 L79768A FOUND FITTING THAT HOLDS FUEL STRAINER IN SERVO CORRODED AWAY (AT LOWEST POINT OF FITTING WHEN INSTALLED IN SERVO). SUBMITTER STATES: SUSPECT WATER IN SERVO CORRODED STEEL FITTING. 1L72 3O3 O A20SO E14EA 19951027004021995102700402NM 1995 10 27 DL72L954084 119951023A5320 WEB BOEING727 727232 1384082NM BS 1243 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11513DA 21315 FOUND .125 INCH CRACK AT RT TORQUE BOX VERT WEB UPPER LIGHTENING HOLE, STA 1243. FOUND AT A-2 LTR CK, REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951027004031995102700403NM 1995 10 27 DL72S953913 119950910A5751657273411W SKIN BOEING727 727232 1384082NM LT AILERON WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11533DA 22046 DURING SHOP INSPECTION, L/W AILERON WAS FOUND WITH AREAS OF WEAR DAMAGE TO SKIN. ACCOMPLISHED REPAIRS PER SRM 51-50-5 AND SRM 51-40-3. 2L73 4F A3WE 19951027004041995102700404NM 1995 10 27 DL72S953984 119951012A5754651622296 RIB BOEING727 727225 1384077NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 UPON INSPECTION, A CRACK WAS FOUND RIB 16. REPAIRED RIB PER MM 57-54-0 FIG 4, FOR NR 6 L/E SLAT PANEL. 2L73 4F A3WE 19951027004051995102700405NM 1995 10 27 DL72S953985 119951012A5754651622296 RIB BOEING727 727225 1384077NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO118875Z 21293 UPON INSPECTION, FOUND A CRACK IN RIB 17. REPAIRED SRM 57-50-3, FOR NR 6 L/E SLAT PANEL. 2L73 4F A3WE 19951027004061995102700406NM 1995 10 27 DL72S954011 119950929A3231 BUSHINGS BOEING727 727232 1384082NM MLG STRUT DOOR LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ATL - HMV, NR 4 FLAP TRACK FWD HINGE FITTING FOR MLG STRUT DOOR HAS LOOSE BUSHINGS. REMOVED BUSHINGS, REAMED BORE TO .750, ACCOMPLISHED BUSHING REPLACEMENT PER MM 57-43-0. 2L73 4F A3WE 19951027004071995102700407NM 1995 10 27 DL72S954012 119950929A3231 BUSHINGS BOEING727 727232 1384082NM MLG STRUT DOOR LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ATL - HMV, NR 5 FLAP TRACK, FWD HINGE FITTING FOR MLG STRUT DOOR HAS LOOSE BUSHINGS. REMOVED BUSHINGS, REAMED BORE TO .750, ACCOMPLISHED BUSHING REPLACEMENT PER MM 57-43-0. 2L73 4F A3WE 19951027004081995102700408NM 1995 10 27 DL72S954034 119950925A5330 SKIN 65545831 BOEING727 727232 1384082NM FS 1158-1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 FUSELAGE SKIN REPAIR AT AFT LAVATORY SERVICE PANEL CUTOUT, FS 1158 TO FS 1183, BETWEEN STRINGERS 20L AND 24L. DURING THE ACCOMPLISHMENT OF EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND CRACKED AND CORRODED IN THE UPPER FWD CORNER OF THE AFT LAVATORY SERVICE PANEL. THE REPAIR CUTS OUT THE DAMAGE FROM THE STRINGER 20L SKIN LAP TO STR 23L FROM THE BS 1183 BUTT SPLICE TO APPROX FS 1158. THE REPAIR THEN INSERTS A SKIN REPLACEMENT SECTION AND A DOUBLER, SO THAT MTC CAN CONTINUE WITH EO 4-69078-3AD. REPAIRS ACCOMPLISHED PER DL ERA 302536-14. 2L73 4F A3WE 19951027004091995102700409NM 1995 10 27 DL72S954039 119951016A5522 SKIN BOEING727 727232 1384082NM RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11482DA 20862 FOUND ON B1 LETTER CK, RT ELEVATOR LWR SKIN CRACKED TWO PLACES, ONE INCH EACH, 12 INCHES FWD OF TAB OUTBD END. REPAIRED PER SRM 55-20-3 FIG 4. 2L73 4F A3WE 19951027004101995102700410NM 1995 10 27 DL72S954042 119951005A5754 RIB BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 ATL - HMV, NR 6 SLAT I/B RIB AT INBOARD SLAT TRACK CRACKED IN LWR RADIUS. REMOVED FASTENERS FROM REPAIR AREA, FABRICATED REPAIR PER 57-54-0 FIG 805. 2L73 4F A3WE 19951027004111995102700411NM 1995 10 27 DL72S954052 119951018A5530 ANGLE BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11477DA 20754 BULKHEAD ATTACH ANGLE CRACKED AT STR 10 LT SIDE FIN STA 180.600, INSIDE VERT STAB CRAWLWAY. FOUND AT D-2 LTR CK AND REPAIRED PER MM 55-30-0. 2L73 4F A3WE 19951027004121995102700412NM 1995 10 27 DL72S954053 119951011A5320 ANGLE BOEING727 727232 1384082NM BS 740 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 FOUND ON CV2 CHECK, CORROSION ON SKIN SUPPORT ANGLE STA 740 AND RBL 10. REPAIRED PER M/M 53-11-0 PG 858, REPLACED SKIN SUPPORT ANGLE. 2L73 4F A3WE 19951027004131995102700413NM 1995 10 27 DL72S954085 119951023A3350 BATTERY PACK 1102837 BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11477DA 2627 20754 CENTER AISLE OVERHEAD EMERGENCY LIGHT INOP AT ROW 26. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19951027004141995102700414NM 1995 10 27 DL72W954031 119950926A5753652163229 SPAR BOEING727 727247 138408FNM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112812W 20868 DURING HMV SHOP INSP, FOUND THE AFT LOWER SPAR CHORD CRACKED 56 INCHES FROM I/B END. REPAIRED PER M/M 57-52-0, FOR NR 2 MIDFLAP. 2L73 4F A3WE 19951027004151995102700415NM 1995 10 27 DL72W954071 119951018A2820 LINES 651671052 BOEING727 727247 138408FNM NR 3 FUEL TANK CRACKED A DALAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 SO112821W 21059 FUEL VENTED OUT OF RT VENT BOX ON ACTIVE RUNWAY, FUEL MIGRATING FROM OTHER TANK CAUSING THE NR 3 TANK TO OVERFILL. FOUND CRACK LINES MFG (P/N 65-22731-2 AND 65-16710-52) REF IPC 28-30-0-16 ITEMS 120 AND 140. BOTH LINES SENT TO SHOP FOR REPAIRS. 2L73 4F A3WE 19951027004161995102700416NM 1995 10 27 DL73E952016 119950510A5532657378715 LE SKIN BOEING737 737247 138448DNM VERT STAB DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11373DL 23520 DURING SHOP INSPECTION, VERTICAL STABILIZER L/E WAS FOUND DENTED BEYOND LIMITS. REPAIRS ACCOMPLISHED PER SRM 55-30-6. 2L72 4F A16WE 19951027004171995102700417NE 1995 10 27 DL73E954054 219951019A7310 VALVE 320115 BOEING737 737247 138448DNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE WORN A DALAA UNSCHED LANDING M OVER TEMP CLCLIMB 1 SO11374DL 10450 23521 709166 ON DESCENT, NR 1 ENG OIL TEMP RUNNING AT 140 DEG FOR A STEADY 15 MIN, TEMP LEVELED AT 130 DEG. DID NOT SHUT ENG DOWN, FUEL HEAT RECYCLED OK AND DIVERTED DFW. FOUND FUEL HEAT VALVE LEAKING. REPLACED VALVE, RAN ENG LEAK AND OPERATION OK. 2L72 4F4 F A16WE E2EA 19951027004181995102700418NE 1995 10 27 DL73S954000 219951013A7260780650 GEARBOX BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE STUDS STRIPPED A DALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO11324DL 23096 717138 AFTER START, OIL QTY WENT TO ZERO, PRESS WENT TO ZERO, THEN SHUTDOWN ENGINE. 2L72 4F4 FRTA16WE E2EA 19951027004191995102700419WP 1995 10 27 DLL10953994 119950929A57541565598102 RIB LKHEED1011 10113851 5265010WP NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 NR 6 L/E SLAT RIB CRACKED. REPAIRED PER SRM 57-51-00 FIG 812, FOUND AT LETTER CHECK. 2L73 4F A23WE 19951027004201995102700420WP 1995 10 27 DLL16954007 119951007A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 THE FS 901 BEAM WAS CORRODED AT LBL 45. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-21-00 PAGES 849 TO 852. 2L73 4F A23WE 19951027004211995102700421WP 1995 10 27 DLL16954008 119951007A5315 FLOORBEAM LKHEED1011 10113853 5265020WP FS 886 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 THE FS 886 FLOORBEAM WAS CORRODED ON THE UPPER CAP AT APPROX RBL 30. THE DAMAGE WAS OUT OF LIMITS SO THE REPAIR WAS ACCOMPLISHED PER SRM 53-21-00 PAGES 823 TO 824. 2L73 4F A23WE 19951027004221995102700422NM 1995 10 27 DLM88953987 119950815A7110 COWL 5930645509 DOUG MD88 MD88 3023688NM LT ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11953DL 49984 49884 L/E RING HAS DENT AT 9 O'CLOCK POS. REPAIRED PER SRM 54-04. FOUND DURING SHOP INSPECTION FOR NR 1 INTAKE COWL. 2L72 4F RTA6WE 19951027004231995102700423NE 1995 10 27 DLM88954087 219951023A751013277503 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE CRACKED A DALAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11978DL 53259 725911 ABE - AFTER T/O, THE NR 2 FIRE WARNING SOUNDED, WOULD STOP WITH THROTTLES PLACED AT IDLE. MTC FOUND THE 13TH STAGE COWL ANTI-ICE VALVE DUCT BLOWN ON THE ENG SIDE OF THE VALVE. REPLACED DUCT, OPERATION NORMAL. 2L72 4F4 FRTA6WE E9NE 19951027004241995102700424NE 1995 10 27 P5CA9500833 219951025A7230 COMPRESSOR BOEING747 747132 1384882NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE STALLED A P5CAECD ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TOTAKEOFF 1 WP23857FT 20246 685970 HKG - UPON APPLYING MAX TAKEOFF POWER, NR 3 ENGINE COMPRESSOR STALLED AT 1.40 EPR. HEARD A LOUD BANG, EGT PEGGED MAX TEMP INDICATOR POINTER AT BOTTOM OF GAUGE 1,100 DEGREES. ABORTED TAKEOFF AT APPROXIMATELY 5 KNOTS, RETARDED ENGINE TO IDLE, SHUTDOWN ENGINE IAW ENGINE STALL CHECKLIST. EGT EXCEEDED 915 DEGREES FOR APPROX 3 SECONDS. BORESCOPED ENGINE, NO DAMAGE FOUND. PRECAUTIONARY REPLACED TT2 SENSOR, PERFORMED FULL POWER RUNUP, ALL INDICATIONS NORMAL. ENGINE NOW 80 HOUR LIMITED. 2L74 4F4 F A20WE E20EA 19951027004251995102700425NM 1995 10 27 SCNA95242 119951021A33501315 EEL LAMP BOEING727 727227 1384078NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE VERTICAL EMERGENCY EXIT LIGHT AT THE R-1 DOOR WAS FOUND INOPERATIVE. RELAMPED LIGHT AND LIGHT TESTED GOOD PER MM 33-50-01. 2L73 4F A3WE 19951027004261995102700426NM 1995 10 27 SCNA95243 119951021A33505878 EEL BOEING727 727282 2F0R NM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE BETWEEN ROW 16 TO ROW 19. ALL CONNECTIONS WERE CHECKED, REMOVED DEBRIS AND WIPED UP MOISTURE FROM EMERGENCY FLOOR TRACK AND LIGHTS TESTED NORMAL. 2L73 4F RTA3WE 19951027004271995102700427NM 1995 10 27 SCNA95244 119951023A3350S106 BATTERY BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 THE AFT OVERHEAD SELF CONTAINED EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951027004281995102700428NM 1995 10 27 UPS404880 119951025A3350 EEL WIRE BOEING747 747123 1384873NM FLIGHT DECK FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND, MAINTENANCE FOUND FORWARD EMERGENCY LIGHT OVER THE MAIN ENTRANCE WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED FUSE IN AFT BATTERY PACK AND REPAIRED WIRE TO FRONT DOOR EMERGENCY LIGHT. OPS CK NORMAL, WORK PERFORMED IAW MM 33-51-00. 2L74 4F A20WE 19951027004291995102700429WP 1995 10 27 UPS804867 119951025A3260 GEAR HANDLE DOUG DC8 DC873F 302199FWP LANDING GEAR LACK OF LUBE A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01807UP 46007 CREW REPORTED, DOORS NOT LATCHED LIGHT CAME ON DURING UPLATCH CHECK, LIGHT WENT OUT AFTER GEAR RECYCLED. MAINTENANCE PERFORMED UPLATCH CHECK IAW MM 32-31-04, OPS CK NORMAL. FOUND GEAR HANDLE STICKY AND CLEANED AND LUBED GEAR HANDLE. 2L74 4F RT4A25 19951027004301995102700430WP 1995 10 27 UPS804868 119951025A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON I/B LOWER ANGLE INNER WEB FS 320, LONGERON 28L. MAINTENANCE REPAIRED ANGLE IAW SRM 52-2-2 AND 51-1-20D. 2L74 4F RT4A25 19951027004311995102700431WP 1995 10 27 UPS804869 119951025A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1360-1480 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 32L BETWEEN FS 1360 TO 1480. MAINTENANCE REPAIRED LONGERON IAW SRM 53-2-2 AND 51-1-20D. 2L74 4F RT4A25 19951027004321995102700432WP 1995 10 27 UPS804870 119951025A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 284-300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON INBOARD END OF LONGERON 34R AT FS 300 TO 284. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004331995102700433WP 1995 10 27 UPS804871 119951025A5320 FITTING DOUG DC8 DC873F 302199FWP FS 28 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT B/T FITTING LONGERON 34R TO 35R, FS 28. MAINTENANCE REPLACED THE FITTING IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004341995102700434WP 1995 10 27 UPS804872 119951025A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 200-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON FINGER DOUBLER AT FS 200 TO 450, LONGERON 31L. MAINTENANCE RPELACED DOUBLER IAW SRM 51-1-21 AND 51-4-20D. 2L74 4F RT4A25 19951027004351995102700435WP 1995 10 27 UPS804873 119951025A5330 SKIN DOUG DC8 DC873F 302199FWP BS 190-450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGES AT BELLY SKIN FS 190 TO 450. MAINTENANCE REPLACED THE SKIN IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004361995102700436WP 1995 10 27 UPS804874 119951025A5320 DOUBLER DOUG DC8 DC873F 302199FWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A X-SLIDE DOOR CUTOUT CENTER DOUBLER HAS HEAVY CORROSION BULGES. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951027004371995102700437WP 1995 10 27 UPS804875 119951025A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1350-1450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 34R, FS 1350 TO 1450. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004381995102700438WP 1995 10 27 UPS804876 119951025A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FUSE EXT BELLY SKIN, FS 1420. MAINTENANCE REPLACED SKIN SECTION IAW SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951027004391995102700439WP 1995 10 27 UPS804877 119951025A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 885-902 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION OUT OF LIMITS ON L-ANGLE, LONGERON 24 STA 885 TO 902. MAINTENANCE REPLACED ANGLE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004401995102700440WP 1995 10 27 UPS804878 119951025A5320 ANGLE DOUG DC8 DC873F 302199FWP FS-895 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION OUT OF LIMITS ON L-ANGLES, FS 895 LONGERON 24L. MAINTENANCE REPLACED THE ANGLE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004411995102700441WP 1995 10 27 UPS804879 119951025A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1420-1490 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 36 CRACKED AND HEAVILY CORRODED AT STA 1420 TO 1490. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027004421995102700442EU 1995 10 27 WWMA9500072 119951023A261172111211000 SMOKE DETECTOR SAAB SF340 340B 7860101EU CARGO BAY INOPERATIVE A WWMAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP15345SB 340B345 CARGO SMOKE ALARM ACTIVATED IN FLIGHT, THE NR 1 CARGO FIRE EXTINGUISHER WAS ACTUATED, THE LIGHT STAYED ON. THE AIRCRAFT RETURNED TO BTR WITHOUT INCIDENT. UPON INVESTIGATION, MAINTENANCE FOUND THE FORWARD CARGO SMOKE DETECTOR TO BE INOPERATIVE. REPLACED FORWARD SMOKE DETECTOR AND THE NR 1 CARGO FIRE BOTTLE, NO FURTHER PROBLEMS. 2L72 4T RTA52EU 19951027004711995102700471WP 1995 10 27 95ZZZM551 119950727A33506012231 EEL BATT PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A VJ6AK NONE L NO TEST ININSP/MAINT 1 SO11529MD 47262 THE GALLEY SLIDE SPOT LIGHT WOULD NOT COME ON. REMOVED AND REPLACED EXIT CHUTE LIGHT BATTERY PACK LEFT AND RT DOORS. (M) 2L72 4F A6WE 19951027004721995102700472WP 1995 10 27 95ZZZM552 119950728A3260 CONNECTOR DOUG DC9 DC932 3022066WP NLG DIRTY A VJ6AO OTHER N FALSE WARNING LDLANDING 1 SO11909VJ 47322 FLT NR 572 - ATL-MCI - RECEIVED AN UNSAFE NOSE GEAR INDICATION AFTER HANDLE WAS LOWERED FOR LANDING. WHEN AIRSPEED REDUCED BELOW 160 KTS FOR APPROACH, NOSE GEAR SAFE INDICATION WAS OBTAINED. FLIGHT OFFICER VISUALLY CONFIRMED DOWN. CLEANED CONNECTOR ON DOWNLOCK SWITCH, JACKED AIRCRAFT, PINNED GEAR SWING NOSE GEAR SEVERAL TIMES, COULD NOT DUPLICATE. OK TO CONTINUE SERVICE, REMOVED GEAR PINS. (M) 2L72 4F A6WE 19951027004731995102700473NM 1995 10 27 AALA951595 119950905A326043467410332205 LIGHT KORRY BOEING757 757223 1384957NM NLG DEFECTIVE A AALAA UNSCHED LANDING P NO WARNING INDICATION APAPPROACH 1 SW07629AA 24587 LAX - FLT NR 201 - DURING APPROACH TO SNA WIHT LANDING GEAR HANDLE IN DOWN POSITION, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR DOORS AND GEAR AMBER LIGHTS REMAINED OUT. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR GREEN LIGHT ASSEMBLY. ACCOMPLISHED BITE CHECK AT GROUND PROXIMITY UNIT WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951027004741995102700474NM 1995 10 27 AALA951599 119950905A26112156604 DETECTOR AUTRONICS BOEING757 757223 1384957NM FWD COMPT DEFECTIVE A AALAO OTHER N FALSE WARNING CRCRUISE 1 SW07614AA 24490 JFK - FLT NR 1759 - EN ROUTE BOS-JFK - DURING CRUISE, FORWARD EQUIPMENT SMOKE WARNING FOLLOWED BY FORWARD EQUIPMENT OVERHEAT INDICATIONS. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT PROCEEDED JFK, LANDING WITHOUT INCIDENT. REPLACED BOTH FORWARD FAN SUPPLY SMOKE DETECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951027004751995102700475NM 1995 10 27 AALA951658 119950915A5730111T3013 SKIN BOEING767 767223 1385123NM CTR WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 AFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN. AFTER BLENDING, FOUND BEYOND LIMITS. REMOVED FASTENERS IN CORRODED AREAS. EDDY CHECKED FASTENER HOLES AND SPOTFACED. SHOT PEENED AND ALODINED AREAS. APPLIED BMS 10-11 SEALANT AND APPLIED FUEL BARRIER TOP COAT. APPROVED BY ENGINEERING PER MRB 767-1012. (M) 2L72 4F RTA1NM 19951027004761995102700476NM 1995 10 27 AALA951660 119950915A5311146T1201 FRAME BOEING767 767223 1385123NM BS 1087 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 AFW - FOUND CRACK IN THE 146T1501-3 FRAME AND THE 146T1352-14 ANGLE ON THE FRAME. THE CRACK RUNS FROM THE CUTOUT IN THE FRAME AND ANGLE TO A FASTENER HOLE ABOVE THE CUTOUT. REMOVED CRACKED AREA. REMOVED FASTENERS AS REQUIRED. TREATED AND PRIMED AREA OVERSIZED HOLES AND INSTALLED CRES TENSION HEAD HI-LOKS, APPROVED BY ENGINEERING PER MRB 767-1015. (M) 2L72 4F RTA1NM 19951027004771995102700477NM 1995 10 27 AALA951665 119950915A5320143T15902 FAIL SAFE STRAP BOEING767 767223 1385123NM BS 5395 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 AFW - FOUND AND BLENDED OUT CORROSION IN FWD LOCATIONS ON THE UPPER SURFACE OF THE FAIL SAFE CHORD. REFINISHED AND INSTALLED SHIMS AS REQUIRED UNDER STRINGER APPROVED BY ENGINEERING PER MRB 767-1014. (M) 2L72 4F RTA1NM 19951027004781995102700478NM 1995 10 27 AALA951669 119950915A5320 SPLICE BOEING767 767223 1385123NM BS 1307 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 AFW - FOUND CORROSION ON STRINGER SPLICE, STRINGER 35L WAS TRIMMED BACK 1.5 INCHES TO REMOVE THE CORRODED AREA. FABRICATED AND INSTALLED A NEW SPLICE PIECE IDENTICAL TO OLD USING THE SAME MATERIAL TYPE AND SHAPE EXCEPT THAT NEW PIECE IS LONGER BY THE AMOUNT REMOVED FROM THE STRINGER END. APPROVED BY ENGINEERING PER MRB 767-1013. (M) 2L72 4F RTA1NM 19951027004791995102700479NM 1995 10 27 AALA951673 119950915A5330 SKIN BOEING767 767223 1385123NM BS 439 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 AFW - FOUND AND BLENDED OUT DAMAGE ON THE INNER SURFACE OF FUSELAGE SKIN. THE BLEND OUT IS APPROXIMATELY 1 INCH BY 2 INCHES WITH APPROX .050 MATERIAL REMAINING. THE DAMAGE IS UNDERNEATH STRINGER 38L. REFINISHED AND INSTALLED A FILLER. APPROVED BY ENGINEERING PER MRB767-1016. (M) 2L72 4F RTA1NM 19951027004801995102700480NM 1995 10 27 AALA951675 119950915A5315141T5113 FLOOR BEAM BOEING767 767223 1385123NM BS 325 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07305AA 22311 CORROSION FOUND ON FLOOR BEAM. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB767-1009. (M) 2L72 4F RTA1NM 19951027004811995102700481NM 1995 10 27 AALA951720 119950924A2710CTY1648501 CONTROL CABLE DOUG MD11 MD11 3023602NM LT AILERON BROKEN A AAALAK NONE O OTHER ININSP/MAINT 1 SW071759 48481 DFW - DURING B-CHECK, LEFT AILERON TRIM LEFT WING DOWN CABLE FOUND BROKEN AND LEFT AILERON TRIM RIGHT WING DOWN CABLE WAS FOUND BIRD CAGED. REPLACED LEFT AILERON TRIM LEFT WING DOWN AND LEFT AILERON TRIM RIGHT WING DOWN CABLES. ACCOMPLISHED RIGGING AND SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19951027004821995102700482SO 1995 10 27 C2XA95CL115 119950921A326019554 TARGET EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0927707 120095 GRR-CLE - LEFT MAIN GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO GRR. FERRIED AIRCRAFT TO CLE. MAINTENANCE ADJUSTED LEFT MAIN GEAR UPLOCK PROX SENSOR TARGET IAW EMB M/M 32-61-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027004831995102700483NE 1995 10 27 C2XA95CL116 219950923A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A C2XAK NONE E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SW0947722142477675 120166 115208 FLT NR 3230 - DAY - CLE - RIGHT POWER LEVER HAD VERY NOTICEABLE VIBRATION WITH PROPELLER IN FEATHER AND MINIMUM RPM. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW MAINTENANCE DIRECTIVE NR 7 AND NR 8. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19951027004841995102700484EU 1995 10 27 C2XA95CL117 119950925A2530VL700 HOT JUG AEROSPATR42 ATR42320 8680930EU GALLEY SHORTED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW0914829 181 FLT NR 3400 - EWR - FLIGHT CREW REPORTED BURNING ELECTRICAL SMELL IN GALLEY AREA. AIRCRAFT RETURNED TO EWR. MAINTENANCE INSPECTED AND REMOVED FAULTY HOT JUG FROM AIRCRAFT. PLACED SYSTEM ON MEL. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951027004851995102700485SO 1995 10 27 C2XA95IA256 119950922A572012017062013 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027004861995102700486SO 1995 10 27 C2XA95IA257 119950922A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027004871995102700487NM 1995 10 27 EISA95273 119950914A5320696203 DOUBLER BOEING727 727277 138408SNM CENTER WING BOX CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION AT CENTER WING BOX UPPER SKIN OUTBOARD OF FUEL CONNECTION, STATION 770, RT. REPLACED DOUBLER PER SRM 51-30-2. (M) 2L73 4F RTA3WE 19951027004881995102700488NM 1995 10 27 EISA95274 119950914A57126919277 RIB BOEING727 727277 138408SNM WS 738 CRACK A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 LEFT WING STATION 738 RIB TO STRINGER ATTACH HOLE CRACKED 1 INCH LONG AT FORWARD LOWER HOLE, REPAIRED. REPAIRED RIB PER SRM 57-10-5, FIG 2. (M) 2L73 4F RTA3WE 19951027004891995102700489NM 1995 10 27 EISA95275 119950914A5313 STRINGER BOEING727 727277 138408SNM FS 1166-1183 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION ON STRINGER 23L, FS 1166-1183. REPAIRED STRINGER SECTION PER SRM 53-10-3. (M) 2L73 4F RTA3WE 19951027004901995102700490NM 1995 10 27 EISA95276 119950914A5320 FITTING BOEING727 727277 138408SNM FS 1185 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07275WC 20549 HEAVY CORROSION ON FITTING, FS 1183 END OF STRINGER 23L. REPLACED FITTING PER SRM 51-30-2. (M) 2L73 4F RTA3WE 19951027004911995102700491NM 1995 10 27 TAOA099506 119950912A3260656021132 ACCY UNIT BOEING727 727225 1384077NM LANDING GEAR FAILED A TAOAO OTHER P NO WARNING INDICATION APAPPROACH 1 EA15919TS M00126 20447 AFTER GEAR EXTENSION, RIGHT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. LIGHT DID PRESS TO TEST OK. COMPLIED WITH AOM PROCEDURES, RECYCLED GEAR AND GREEN LIGHT ILLUMINATED. CHECKED RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR, LINKAGE AND SENSOR COILS FOR PROPER RESISTANCE. ALL CHECKED OK. REPLACED LANDING GEAR ACCESSORY UNIT. ALL DOWN LOCK INDICATIONS CHECKED OK. (M) 2L73 4F A3WE 19951027004921995102700492WP 1995 10 27 USAA950915 119950808A5320 BEAM DOUG DC9 DC981 3022081WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AROUND SEVERAL SCREW HOLES RIGHT LAV FLOOR REAR STATION 1322. CORROSION TASK NR C58-53300. REMOVED CORROSION AND INSTALLED DOUBLER AND STRAP PER USAIR TYPICAL REPAIR 53-10-19. (M) 2L72 4F A6WE 19951027004931995102700493WP 1995 10 27 USAA950916 119950810A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION STATION 1338 FLOOR BEAM NR 18, 24 INCHES FROM RIGHT SIDE WALL AT SCREW HOLES. CORROSION TASK NR C58-53300. REPLACED ANGLE FROM RBL 12 INCHES TO OUTBOARD SIDE PER USAIR TYPICAL REPAIR 53-10-14.` 2L72 4F A6WE 19951027004941995102700494EU 1995 10 27 USAA950928 119950901A3260 IND BULB FOKKERF28 F28MK4000 4990810EU NLG FAILED A USAAO OTHER P NO WARNING INDICATION DEDESCENT 1 EA19476US 11224 PHF - FLT NR 0121 - WHEN THE GEAR WAS EXTENDED THE NOSE GEAR FAILED TO GIVE A GREEN LIGHT. THE CAPTAIN PULLED OFF THE PATTERN AND RECYCLED THE GEAR. AGAIN NO NOSE GEAR GREEN LIGHT. AT THAT TIME THE CREW CHECKED THE VISUAL INDICATORS AND DETERMINED THE GEAR WAS DOWN AND LOCKED. THE EMERGENCY EQUIPMENT WAS CALLED OUT. THE FLIGHT LANDED WITH NO FURTHER INCIDENT AND TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE CHECKED THE NOSE GEAR DOWNLOCK POSITION SWITCH AND RELAMPED THE NOSE GEAR DOWNLOCK INDICATOR. OPERATIONS CHECKED NORMAL. (M) 2L72 4F RTA20EU 19951027004951995102700495WP 1995 10 27 USAA950930 119950808A5311 FRAME DOUG DC9 DC981 3022081WP BS 886 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND .75 INCH CRACK FORWARD UPPER CORNER OF WINDOW FRAME AT STATION 886 LONG 12R. STOP DRILLED CRACK AND REPAIRED PER USAIR TYPICAL REPAIR 53-30-06. (M) 2L72 4F A6WE 19951027004961995102700496WP 1995 10 27 USAA950931 119950808A5330 SKIN DOUG DC9 DC981 3022081WP BS 846 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND .5 INCH CRACK IN LOWER FORWARD CORNER OF WINDOW DOUBLER AFT OF STATION 846 LEFT SIDE. STOP DRILLED CRACK AND REPAIRED PER USAIR TYPICAL REPAIR 53-30-06. (M) 2L72 4F A6WE 19951027004971995102700497WP 1995 10 27 USAA950932 119950808A5280 STRINGER DOUG DC9 DC981 3022081WP LT MLG DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND 1.25 INCH CRACK IN STRINGER OF FWD INBOARD LEADING EDGE IN RADIUS JUST FWD OF LEFT MLG ATTACH FITTING. STOP DRILLED CRACK AND INSTALLED STAINLESS STEEL DOUBLERS PER SRM 52-05. (M) 2L72 4F A6WE 19951027004981995102700498WP 1995 10 27 USAA950933 119950810A53131195573 LONGERON DOUG DC9 DC981 3022081WP BS 237 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL 2 CORROSION AT STATION 237 LONGERON 29R. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951027004991995102700499WP 1995 10 27 USAA950934 119950810A5330 SKIN DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND .375 INCH CRACK AT STATION 160 UPPER FORWARD CORNER OF FORWARD AIRSTAIR DOOR. INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-05 FIG 57A SHT 6 VIEW G. (M) 2L72 4F A6WE 19951027005001995102700500WP 1995 10 27 USAA950935 119950808A5530 ANGLE DOUG DC9 DC981 3022081WP BS 1474 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND 1 INCH CRACK LEFT DRAG ANGLE STATION 1474 (CANTED FRAME). STOP DRILLED CRACK AND INSTALLED SKIN AND DOUBLER REPAIR PER SRM 53-05 FIG 23B CONF 7007. (M) 2L72 4F A6WE 19951027005011995102700501EU 1995 10 27 USAA950936 119950802A5313 STRINGER FOKKERF28 F28MK0100 4990807EU FRAME 3870 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19857US13576 11289 PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK IN STRINGER NR 68 RIGHT SIDE 4 INCHES AFT OF FRAME 3870. INSTALLED DOUBLER REPAIR PER SRM 51-70-06 FIG 202. (M) 2L72 4F RT 19951027005021995102700502EU 1995 10 27 USAA950939 119950816A5330 SKIN FOKKERF28 F28MK0100 4990807EU BS 24011-24611 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19857US13576 11289 PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED BETWEEN LEFT STUBWING UPPER AND LOWER CONNECTION ANGLES. AREA APPROXIMATELY 10 INCHES BY 24 INCHES AT STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA INSTALLED DOUBLER REPAIR PER USAIR EA NR 30990A. (M) 2L72 4F RT 19951027005031995102700503EU 1995 10 27 USAA950940 119950816A5330 SKIN FOKKERF28 F28MK0100 4990807EU BS 24011-24611 DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19857US13576 11289 PIT - DURING Q-1 INSPECTION, FOUND FUSELAGE SKIN DELAMINATED APPROXIMATELY 10 INCH BY 24 INCH AREA BETWEEN RIGHT STUB WING UPPER AND LOWER CONNECTION ANGLE FROM STATION 24011 TO STATION 24611. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER USAIR EA NR 30990A. (M) 2L72 4F RT 19951027005041995102700504EU 1995 10 27 USAA950941 119950731A5320 FITTING FOKKERF28 F28MK0100 4990807EU BS 8305-8805 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19857US13576 11289 PIT - DURING Q-1 INSPECTION, FOUND .5 INCH CRACK BETWEEN STATION 8305 AND STATION 8805 AT STRINGER NR 2 FITTING. INSTALLED DOUBLER ANGLE PER SRM 53-00-02. (M) 2L72 4F RT 19951027005051995102700505NM 1995 10 27 USAA950974 119950829A5330 SKIN BOEING757 757225 1384959NM BS 278-297 PUNCTURED A USAAK NONE O OTHER ININSP/MAINT 1 EA19606AU34578 22202 CLT - DURING AN UNSCHEDULED MAINTENANCE INSPECTION, FOUND A PUNCTURE, TEAR AND A DENT 7.3125 INCH BY 19.75 INCH BETWEEN S18L AND S16L FROM FRAME BS 278 TO 297. INSTALLED INTERIM DOUBLER. (M) 2L72 4F RTA2NM 19951027005061995102700506NM 1995 10 27 USAA950976 119950728A5414 NACELLE BOEING757 757225 1384959NM NR 2 STRUT DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU34462 22193 CLT - DURING A CMV-1 INSPECTION, FOUND A 2 INCH BY 3.5 INCH TEAR AND DENT AT NR 2 NACELLE STRUT RIGHT SIDE PP STATION 134.5. INSTALLED DOUBLER, FILLERS, SKIN. (M) 2L72 4F RTA2NM 19951027005071995102700507EU 1995 10 27 USAA9509937 119950811A5320 ANGLE FOKKERF28 F28MK0100 4990807EU NR 2 RADIO RACK CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19857US13576 11289 PIT - DURING Q-1 INSPECTION, FOUND CORROSION AT ATTACH ANGLE NR 2 RADIO RACK FLOOR PANEL. FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 53-12-10. (M) 2L72 4F RT 19951027005081995102700508EU 1995 10 27 USAA951005 119950923A3350 EEL WIRING FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19883US 11337 PHL - FLT NR 823 - FOUND FIRST CLASS EMERGENCY LIGHT WIRING INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE IN THE FIRST CLASS CLOSET. (M) 2L72 4F RT 19951027005091995102700509EU 1995 10 27 USAA951006 119950921A2120 AIR DISTR FOKKERF28 F28MK0100 4990807EU CABIN ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19850US 11276 CLT - FL 1112 - DURING TAKEOFF GROUND ROLL, CREW NOTED SMELL OF BURNING RUBBER. CREW LEFT GEAR DOWN, SMELL DID NOT DISSIPATE. CREW DECLARED AN EMERGENCY, DUMPED CABIN AIR, AND RETURNED TO CLT. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE RAN BOTH ENGINES AND BOTH PACKS. CABIN WAS PRESSURIZED TO APPROXIMATELY FOUR PSI. SMELL COULD NOT BE DUPLICATED. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RT 19951027005101995102700510NM 1995 10 27 95ZZZM553 119950926A213039606411 PACK CONTROL VLV BOEING737 737277 1384570NM RIGHT DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28186AW 2054 22653 PHX - FLT NR 580 - AIR TURN BACK, CREW UNABLE TO PRESSURIZE AIRCRAFT DURING CLIMB-OUT. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT PACK VALVES. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. REF NR AWXA9500664. (M) 2L72 4F RTA16WE 19951027005111995102700511EU 1995 10 27 95ZZZM554 119950924A2720810A000003 SERVO AIRBUS320 A320231 3930325EU RUDDER MALFUNCTIONED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28632AW 00384 81 AIR TURN BACK - CREW REPORTED AIRFRAME VIBRATION ON DEPARTURE FROM PHX AT APPROXIMATELY 290 KNOTS. VIBRATION STOPPED AT FL 31.7. AIRCRAFT RETURNED TO PHX DUE TO PAST HISTORY, LANDING UNEVENTFUL. MAINTENANCE INSPECTED ALL SYSTEMS AND AIRFRAME COMPONENTS WITH NO FAULTS FOUND. TEST FLIGHT RESULTS INDICATED RUDDER POSITION ELIMINATED VIBRATION. MAINTENANCE REPLACED RUDDER GREEN, YELLOW AND BLUE SYSTEMS SERVOS PER MM 27-24-51. ALSO, REPLACED SPRING ROD PER MM 27-21-40. OPS CHECK OK PER MM 27-24-00 710-001 AND 002. NO VIBRATION NOTED ON TEST FLIGHT. REF NR AWXA9500665. 2L72 4F RTA28NM 19951027005121995102700512EU 1995 10 27 95ZZZM555 119950924A2720810A000003 SERVO AIRBUS320 A320231 3930325EU RUDDER MALFUNCTIONED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28632AW 00385 81 AIR TURN BACK - CREW REPORTED AIRFRAME VIBRATION ON DEPARTURE FROM PHX AT APPROXIMATELY 290 KNOTS. VIBRATION STOPPED AT FL 31.7. AIRCRAFT RETURNED TO PHX DUE TO PAST HISTORY, LANDING UNEVENTFUL. MAINTENANCE INSPECTED ALL SYSTEMS AND AIRFRAME COMPONENTS WITH NO FAULTS FOUND. TEST FLIGHT RESULTS INDICATED RUDDER POSITION ELIMINATED VIBRATION. MAINTENANCE REPLACED RUDDER GREEN, YELLOW AND BLUE SYSTEMS SERVOS PER MM 27-24-51. ALSO, REPLACED SPRING ROD PER MM 27-21-40. OPS CHECK OK PER MM 27-24-00 710-001 AND 002. NO VIBRATION NOTED ON TEST FLIGHT. REF NR AWXA9500665. 2L72 4F RTA28NM 19951027005131995102700513EU 1995 10 27 95ZZZM556 119950924A2720D2727025000400 CONTROL SPRING AIRBUS320 A320231 3930325EU RUDDER MALFUNCTIONED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28632AW 81 AIR TURN BACK - CREW REPORTED AIRFRAME VIBRATION ON DEPARTURE FROM PHX AT APPROXIMATELY 290 KNOTS. VIBRATION STOPPED AT FL 31.7. AIRCRAFT RETURNED TO PHX DUE TO PAST HISTORY, LANDING UNEVENTFUL. MAINTENANCE INSPECTED ALL SYSTEMS AND AIRFRAME COMPONENTS WITH NO FAULTS FOUND. TEST FLIGHT RESULTS INDICATED RUDDER POSITION ELIMINATED VIBRATION. MAINTENANCE REPLACED RUDDER GREEN, YELLOW AND BLUE SYSTEMS SERVOS PER MM 27-24-51. ALSO, REPLACED SPRING ROD PER MM 27-21-40. OPS CHECK OK PER MM 27-24-00 710-001 AND 002. NO VIBRATION NOTED ON TEST FLIGHT. REF NR AWXA9500665. 2L72 4F RTA28NM 19951027005141995102700514WP 1995 10 27 95ZZZM557 119950923A2150 TEMP CONTROL VLV DOUG DC9 DC932 3022066WP RT PACK FAILED A VJ6AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11934VV 47488 FLT NR 238 - DFW-ATL - FLIGHT ATTENDANTS ON CLIMB-OUT REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO DFW. MAINTENANCE CHECKED SYSTEMS AND FOUND RIGHT PACK TEMPERATURE CONTROL VALVE AT FAULT, PLACED ON MEL LOG, PAGE 4928. 2L72 4F A6WE 19951027005151995102700515NE 1995 10 27 95ZZZM558 219951001A7310708241 JFC LINES DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 FUEL CONTRLCHAFFED A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 GL23788AL 45999 671271 TJSJ - ON DEPARTURE, THE NR 4 ENGINE FLAMED OUT AT FL 310. THE FLIGHT CREW CONTINUED THE SHUT DOWN PROCEDURES. NO ABNORMALITIES COULD BE IDENTIFIED. THE ENGINE WAS RE-STARTED, AND OPERATED NORMALLY, WITH THE EXCEPTION OF HIGH FUEL CONSUMPTION. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO TJSJ FOR MAINTENANCE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE JFC SUPPLY AND LOW PRESSURE OUTPUT LINES CHAFFED AND LEAKING. THE LINES WERE REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. REF NR IXXA199584. 2L74 4F4 F 4A25 1E8 19951027005161995102700516NM 1995 10 27 AWXA9500619 119950911A532065C807351 CHORD BOEING737 7373S3 1384711NM BS 947-996 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28314AW 23733 PHX - DURING SCHEDULED C9 INSPECTION, FOUND L2 DOOR CHORD AT STATION 947 TO STATION 996 CORRODED BEYOND LIMITS IN SEVERAL AREAS. REPLACED CHORD PER SRM 51-40-02. (M) 2L72 4F RTA16WE 19951027005171995102700517NM 1995 10 27 AWXA9500635 119950918A335020131A BATTERY PACK BOEING757 7572S7 1384962NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28905AW 23567 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND BATTERY PACK AT R2 DOOR INOPERATIVE. REMOVED AND REPLACED PACK, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951027005181995102700518NM 1995 10 27 AWXA9500636 119950913A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FORWARD GALLEY FLOOR BEAM AT STATION 328 LBL 45 TO BL0 CORRODED AT NUT PLATED HOLES. REPLACED T-CAP FROM BL 0 TO L1 DOOR PER SRM 51-30-2 AND SRM 51-10-1. (M) 2L72 4F RTA16WE 19951027005191995102700519NM 1995 10 27 AWXA9500637 119950913A5210 CHORD BOEING737 737277 1384570NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C8 INSPECTION, FOUND L1 DOOR INNER CHORD CORRODED AT NUT PLATE HOLES. REMOVED AND REPLACED L1 DOOR CHORD PER SRM 51-10-1, PAGE 5. (M) 2L72 4F RTA16WE 19951027005201995102700520NM 1995 10 27 AWXA9500638 119950913A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 294 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FORWARD GALLEY FLOOR BEAM AT STATION 294 BL ZERO NUT PLATE HOLES CORRODED. REPAIRED FLOOR BEAM PER SRM 53-10-9, FIGURE 5. (M) 2L72 4F RTA16WE 19951027005211995102700521NM 1995 10 27 AWXA9500639 119950913A5313 STRINGER BOEING737 737277 1384570NM BS 360 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C8 INSPECTION, FOUND STRINGER CORRODED ON ITS SIDES AT STATION 360 STRINGER 27L. REMOVED AND REPLACED STRINGER PER SRM 53-10-2. (M) 2L72 4F RTA16WE 19951027005221995102700522NM 1995 10 27 AWXA9500641 119950918A5320 DOOR FRAME BOEING737 737222 1384473NM BS 951 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28144AW 19074 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR FRAME CRACKED IN TWO AREAS, UPPER FORWARD CORNER OF FRAME AT BS 951, AND FORWARD NR 2 DOOR STOP CASTING, P/N 65558741, AT STOP BASE, FORWARD SIDE INNER SKIN WEB. REPAIRS COMPLIED WITH PER ER 2-53-16-41. (M) 2L72 4F A16WE 19951027005231995102700523NM 1995 10 27 AWXA9500642 119950913A5330 SKIN BOEING737 737277 1384570NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FUSELAGE SKIN CRACKED BELOW APU THERMAL DISCHARGE DISK. ONE INCH CRACK WAS CONFIRMED WITH EDDY CURRENT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M) 2L72 4F RTA16WE 19951027005241995102700524NM 1995 10 27 AWXA9500643 119950913A5330 SKIN BOEING737 737277 1384570NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C4 INSPECTION, FOUND L2 DOOR FUSELAGE MOUNTED TORQUE TUBE FORWARD LOWER CORNER SKIN CRACKED. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR PER SRM 53-30-3. (M) 2L72 4F RTA16WE 19951027005251995102700525NM 1995 10 27 AWXA9500644 119950913A5315 EXTRUSION BOEING737 737277 1384570NM BS 312 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD GALLEY FLOOR BEAM AT STATION 312 BL ZERO NUT PLATE HOLES CORRODED. REMOVED AND REPLACED SECTION OF T-CHORD IAW SRM 53-10-9 AND SRM 51-30-2. (M) 2L72 4F RTA16WE 19951027005261995102700526EU 1995 10 27 AWXA9500651 119950920A2710D5754038520000 BUSHING AIRBUS320 A320231 3930325EU RT AILERON WORN A AWXAO OTHER E VIBRATION/BUFFET CRCRUISE 1 WP28632AW 81 CMH/PHX - FLT NR 651 - CREW NOTED MID CABIN VIBRATION DURING CRUISE AT OR ABOVE 290 KNOTS. AIRCRAFT CONTINUED TO PHX LANDING WITHOUT INCIDENT. MAINTENANCE FOUND RT AILERON HINGE BUSHINGS AT POSITIONS 1,3, 4 AND 5 WORN BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED BUSHINGS PER CMM 57-61-21. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19951027005271995102700527NM 1995 10 27 AWXA9500652 119950921A5315 FLOOR BEAM BOEING737 737297 1384480NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT GALLEY FLOOR BEAM TOP CAP AT STATION 986.5 RBL 17 CORRODED BEYOND LIMITS. REMOVED AND REPLACED T-CAP PER SRM 53-10-09. (M) 2L72 4F A16WE 19951027005281995102700528NM 1995 10 27 AWXA9500653 119950921A5313 STRINGER BOEING737 737297 1384480NM BS 360 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53-11-04. (M) 2L72 4F A16WE 19951027005291995102700529NM 1995 10 27 AWXA9500654 119950921A5313 STRINGER BOEING737 737297 1384480NM BS 910 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND STRINGER 28L AT BS 910 CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED STRINGER PER SRM 53-10-3. (M) 2L72 4F A16WE 19951027005301995102700530NM 1995 10 27 AWXA9500655 119950921A5330 SKIN BOEING737 737297 1384480NM BS 685 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND TWO CRACKS IN RT SIDE OF KEEL BEAM SKIN. A 2 INCH CRACK FOUND AT STATION 685 BL ZERO AND A 1.5 INCH CRACK FOUND AT STAITON 706 BL ZERO. FABRICATED PANEL 7075 T6 .080 INCH AND INSTALLED PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2L72 4F A16WE 19951027005311995102700531NM 1995 10 27 AWXA9500656 119950921A5210 HINGE CUTOUT BOEING737 737297 1384480NM L1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND A CRACK IN L1 DOOR SKIN AT UPPER HINGE CUTOUT UPPER CORNER. ROUTED OUT CRACK PER SRM 52-00-2, PAGE 34. (M) 2L72 4F A16WE 19951027005321995102700532NM 1995 10 27 AWXA9500657 119950921A532065528941 ANGLE BOEING737 737297 1384480NM BS 540 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN LT SIDE OF ZERO FLOOR SUPPORT ANGLE AT STATION 540 BL 0. INSTALLED NEW SUPPORT ANGLE PER SRM 51-10-1 AND SRM 51-30-2. (M) 2L72 4F A16WE 19951027005331995102700533NM 1995 10 27 AWXA9500658 119950921A5315 FLOOR BEAM BOEING737 737297 1384480NM BS 947 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND AFT CABIN FLOOR BEAM AT STATION 947 RBL 5 TO RBL 6 CORRODED BEYOND LIMITS. REPAIRED BEAM PER SRM 53-10-9. (M) 2L72 4F A16WE 19951027005341995102700534NM 1995 10 27 AWXA9500659 119950921A5313 STRINGER BOEING737 737297 1384480NM BS 910 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND CORROSION BEYOND LIMITS ON STRINGER 28L BS 910 IN AFT CARGO PIT. FABRICATED AND INSTALLED NEW STRINGER PER SRM 53-10-3 FIGURE 1. (M) 2L72 4F A16WE 19951027005351995102700535NM 1995 10 27 AWXA9500661 119950921A5330 PANEL BOEING737 737297 1384480NM BS 685 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND A .75 INCH CRACK IN LEFT SIDE OF KEEL BEAM SKIN AT STATION 685 BL 0. FABRICATED AND INSTALLED REPLACEMENT PANEL PER SRM 51-10-1 AND SRM 51-30-02. (M) 2L72 4F A16WE 19951027005361995102700536NM 1995 10 27 AWXA9500663 119950921A5330 SKIN BOEING737 737297 1384480NM FUSELAGE CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28147AW 22630 PHX - DURING SCHEDULED C13 INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT L2 DOOR LOWER HINGE CUTOUT LOWER FORWARD CORNER. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 53-30-03, FIGURE 34. (M) 2L72 4F A16WE 19951027005371995102700537NM 1995 10 27 AWXA9500664 119950926A213039606411 PACK CONTROL VLV BOEING737 737277 1384570NM LEFT DEFECTIVE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28186AW 1891 22653 PHX - FLT NR 580 - AIR TURN BACK, CREW UNABLE TO PRESSURIZE AIRCRAFT DURING CLIMB-OUT. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT PACK VALVES. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951027005381995102700538EU 1995 10 27 AWXA9500665 119950924A2720810A000003 SERVO AIRBUS320 A320231 3930325EU RUDDER MALFUNCTIONED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28632AW 00383 81 AIR TURN BACK - CREW REPORTED AIRFRAME VIBRATION ON DEPARTURE FROM PHX AT APPROXIMATELY 290 KNOTS. VIBRATION STOPPED AT FL 31.7. AIRCRAFT RETURNED TO PHX DUE TO PAST HISTORY, LANDING UNEVENTFUL. MAINTENANCE INSPECTED ALL SYSTEMS AND AIRFRAME COMPONENTS WITH NO FAULTS FOUND. TEST FLIGHT RESULTS INDICATED RUDDER POSITION ELIMINATED VIBRATION. MAINTENANCE REPLACED RUDDER GREEN, YELLOW AND BLUE SYSTEMS SERVOS PER MM 27-24-51. ALSO, REPLACED SPRING ROD PER MM 27-21-40. OPS CHECK OK PER MM 27-24-00 710-001 AND 002. NO VIBRATION NOTED ON TEST FLIGHT. (M) 2L72 4F RTA28NM 19951027005391995102700539NE 1995 10 27 C2XA95IA270 319951003A6111SFA13M10A PROPELLER BLADE AEROSPATR42 ATR42320 8680930EU HAMSTD14SF 14SF6 NE LEFT NR 4 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW09148329460 2884 187 890434 IAH - DURING AN A-CHECK INSPECTION, THE NR 1 PROPELLER, NR 4 BLADE WAS REMOVED AND REPLACED TO CORRECT A PROP DE-ICE DISCREPANCY. UPON REMOVAL OF THE HEATER SHEATH, A CRACK IN THE LEADING EDGE OF THE PROPELLER BLADE WAS DISCOVERED. THE BLADE WAS THEN ROUTED TO A REPAIR FACILITY TO CORRECT THE DISCREPANCY. (M) 2H72 4T RTA53EU 6 CP7NE 19951027005401995102700540WP 1995 10 27 IXXA199581 119950911A5330 SKIN DOUG DC8 DC863 302198AWP FS 1916 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23788AL72167 45999 DURING C-CHECK, THREE RIVET HEADS WERE FOUND POPPED ON THE LOWER SIDE OF THE TAIL CONE JUST AFT OF PANEL NR 62 ACCESS DOOR. THE INTERNAL CORROSION WAS REMOVED, AND A NEW SKIN PANEL AND DOUBLERS INSTALLED IAW COTNEY/ENGINEERING DRAWING SKA95164-3, DATED 9/1/95. (M) 2L74 4F 4A25 19951027005411995102700541WP 1995 10 27 IXXA199582 119950911A53122610391 BLKHD STIFFENER DOUG DC8 DC863 302198AWP AFT PRESS BLKHD CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23788AL721678911 45999 DURING C-CHECK, AN AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER (THIRD FROM THE BOTTOM AT APPROXIMATELY STATION PLUS X3 TO MINUS X3) WAS FOUND TO BE CRACKED IN THE RADIUS. A DOUBLER REPAIR WAS INSTALLED IAW COTNEY ENGINEERING DRAWING SKA95164-2, DATED 8/23/95. (M) 2L74 4F 4A25 19951027005421995102700542WP 1995 10 27 IXXA199583 119950911A5532 SKIN DOUG DC8 DC863 302198AWP VERT STAB CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23788AL72167 45999 DURING C-CHECK, CORROSION WAS FOUND UNDER THE VERTICAL STABILIZER AFT SPAR CLOSE-OUT PANEL JUST FORWARD OF THE UPPER RUDDER DAMPER. THE CORRODED PARTS WERE REMOVED, AND A NEW SKIN AND FITTING WERE INSTALLED IAW COTNEY ENGINEERING DRAWING SKA95164-1, DATED 8/24/95. (M) 2L74 4F 4A25 19951027005431995102700543NE 1995 10 27 IXXA199584 219951001A7310591058 JFC LINES DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 FUEL CONTRLCHAFFED A IXXAEA ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 GL23788AL 45999 671271 TJSJ - ON DEPARTURE, THE NR 4 ENGINE FLAMED OUT AT FL 310. THE FLIGHT CREW CONTINUED THE SHUT DOWN PROCEDURES. NO ABNORMALITIES COULD BE IDENTIFIED. THE ENGINE WAS RE-STARTED, AND OPERATED NORMALLY, WITH THE EXCEPTION OF HIGH FUEL CONSUMPTION. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT RETURNED TO TJSJ FOR MAINTENANCE. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE JFC SUPPLY AND LOW PRESSURE OUTPUT LINES CHAFFED AND LEAKING. THE LINES WERE REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F4 F 4A25 1E8 19951027005441995102700544NE 1995 10 27 SRAA99518 319950928A6110 PROPELLER LKHEED382 382G 526414USO HAMSTD54H 54H60117 NE NR 1 LEAKING A SRAAE ENGINE SHUTDOWN BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CRCRUISE 1 SO19920SJ 4561 FLT ADT4 - MHZ - NR 1 PROP LOW OIL LIGHT CAME ON, PRECAUTIONARY SHUT DOWN NR 1 ENGINE DUE TO EXCESSIVE LEAK IN INTAKE AND FUMES IN COCKPIT. REPLACED NR 1 PROPELLER AND VALVE HOUSING ASSEMBLY, PERFORMED ENGINE RUN UP SYSTEM OPS CHECKED GOOD. (M) 2H74 4T A1SO 6 CP906 19951027005451995102700545NE 1995 10 27 SRAA99519 219950928A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 2 FAILED A SRAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SO19745SJ 20888 MIA - ON DESCENT, NR 2 ENGINE STALLED, AT IDLE THRUST EGT INCREASED TO 715, SHUT DOWN ENGINE AND RE-LIGHT NORMALLY INTO MIA. UNABLE TO DETERMINE CAUSE, REPLACED NR 2 ENGINE AND PERFORMED ENGINE RUN UP, OPS CHECKED AND LEAK CHECKED GOOD. (M) 2L74 4F4 F A20WE E20EA 19951027005461995102700546WP 1995 10 27 SRAA99520 119950930A5242 DOOR DOUG DC8 DC873F 302199FWP E/E COMP LACK OF LUBE A SRAAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19873SJ 46091 FLT NR 173 - MIA - ON CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE, BELLY DOOR E/E COMPARTMENT LIGHT CAME ON, DUMPED FUEL AND ACCOMPLISHED AIR TURN BACK. FOUND E/E DOOR DID NOT SHUT PROPERLY AND WARNING SWITCH BINDING, ADJUSTED SWITCH AND LUBED, CLOSED DOOR AND VERIFIED INDICATION. OPS CHECKED GOOD PER MM CH 52. (M) 2L74 4F RT4A25 19951027005471995102700547WP 1995 10 27 USAA950917 119950807A5312 BLKHD ANGLE DOUG DC9 DC981 3022081WP AFT PRESS BLKHD CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND LOWER AFT ANGLE AT PRESSURE BULKHEAD CORROSION APPROXIMATELY 6 INCHES BY 36 INCHES LOWER AFT FACE FROM LONGERON 25L-25R. CORROSION TASK NR C57-53300. SPLICED IN NEW ANGLE PER USAIR TYPICAL REPAIR 53-30-10. (M) 2L72 4F A6WE 19951027005481995102700548WP 1995 10 27 USAA950918 119950807A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 1220-1309 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19812US37779 48092 PIT - DURING Q-4 CHECK INSPECTION, FOUND LEFT INBOARD SEAT TRACK LEVEL 1 CORROSION 80 INCHES LONG, STATION 1220 TO STATION 1309. CORROSION TASK NR C58-53302 PREVIOUS REWORKED. REPLACED SECTION OF SEAT TRACK PER SRM 53-05 PG 8L FIG 4F. (M) 2L72 4F A6WE 19951027005491995102700549EU 1995 10 27 95ZZZM559 119950906A3350C77265 EEL LAMP AIRBUS A92393902064AIRBUS300 A300B4203 3930306EU CABIN FAILED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314976 271 DURING MAINTENANCE CHECK, FOUND EXIT SIGN INOPERATIVE, INBOARD OF 3L PASSENGER DOOR. FOUND LAMP BURNED OUT. REMOVED AND REPLACED LAMP UNIT. OPERATIONAL CHECK NORMAL. (M) 2L72 4F A35EU 19951027005501995102700550EU 1995 10 27 95ZZZM560 119950929A3350311701 EEL BATTERY BRUCE 10051911 AIRBUS300 A300B4203 3930306EU L-1 DOOR DISCHARGED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314976 271 DURING MAINTENANCE CHECK, FOUND L-1 DOOR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED L-1 DOOR OVERHEAD EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK NORMAL. (M) 2L72 4F A35EU 19951027005511995102700551 1995 10 27 C2XA95CL118 419951001A34177000700959 AIR DATA COMP AEROSPATR42 ATR42320 8680930EU NR 2 FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0914830106029129 84030492 184 FLT NR 3595 - EWR-EWR - NR 2 AIR DATA COMPUTER FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 AIR DATA COMPUTER IAW ATR JIC 34-11-81. OPERATIONAL AND LEAK CHECKS GOOD. (M) 2H72 4T RTA53EU 19951027005521995102700552NE 1995 10 27 C2XA95CL119 219951002A73103035681 FUEL FILTER AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 ENG CLOGGED A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0934820 159 FLT NR 3548 - EWR-EWR - AFTER TAKEOFF THE NR 1 ENGINE FUEL CLOG LIGHT CAME ON. AIRCRAFT RETURNED TO EWR. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL OUTLET FILTER IAW 72-01-40. OPERATIONAL CHECKED GOOD IAW 72-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19951027005531995102700553EU 1995 10 27 C2XA95CL120 119951002A2710S2738115700400 CONTROL CABLE AEROSPATR42 ATR42320 8680930EU CAPT COLUMN OUT OF ADJ A C2XAA UNSCHED LANDING O OTHER CLCLIMB 1 SW0915827 175 FLT NR 3747 - PWM-EWR - AILERON CABLE BANGING ON SIDE OF CONTROL COLUMN COVER, CAPTAIN'S SIDE. AIRCRAFT RETURNED TO PWM. MAINTENANCE ADJUSTED CAPTAIN'S AILERON CONTROL CABLE, NON-REGULATED LOOP IAW ATR JIC 27-11-14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951027005541995102700554EU 1995 10 27 C2XA95CL121 119951004A6120FE1595006 PROP BRAKE AEROSPATR42 ATR42320 8680930EU NR 2 ENGINE FAILED A C2XAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 SW09348201147 159 EWR - FLT NR 3614 - PRIOR TO AIRCRAFT TAXI, PROP BRAKE FAILED CAUSING ENGINE NR 2 TO CATCH ON FIRE. THE NR 1 AND NR 2 FIRE BOTTLES WERE DISCHARGE. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE PROP BRAKE TO HAVE OVERHEATED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE AND PROP BRAKE IAW ATR MAINTENANCE MANUAL 72-00-00, ALL OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. THE NR 2 ENGINE WAS CHANGED DUE TO DRY CHEMICAL FIRE AGENT BEING SPRAYED INTO THE ENGINE INLET. (M) 2H72 4T RTA53EU 19951027005551995102700555SO 1995 10 27 C2XA95IA258 119951003A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005561995102700556SO 1995 10 27 C2XA95IA259 119951003A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005571995102700557SO 1995 10 27 C2XA95IA260 119951003A572012017057015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005581995102700558SO 1995 10 27 C2XA95IA261 119951003A572012017057021 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005591995102700559SO 1995 10 27 C2XA95IA262 119951003A572012017056013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005601995102700560SO 1995 10 27 C2XA95IA263 119951003A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005611995102700561SO 1995 10 27 C2XA95IA264 119951003A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005621995102700562SO 1995 10 27 C2XA95IA265 119951003A572012017056019 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 5 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005631995102700563SO 1995 10 27 C2XA95IA266 119951003A572012017057015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005641995102700564SO 1995 10 27 C2XA95IA267 119950103A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005651995102700565SO 1995 10 27 C2XA95IA268 119951003A572012017059006 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, LOWER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005661995102700566SO 1995 10 27 C2XA95IA269 119951003A573012042999005 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER SKIN CRACKED AT AFT OUTBOARD CORNER OF FUELING ACCESS DOOR CUT OUT. MAINTENANCE STOP DRILLED, AND INSTALLED REPAIR DOUBLER PER CONTINENTAL EXPRESS ENGINEERING CHANGE, REPAIR AUTHORIZATION EC5730-01031. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951027005671995102700567WP 1995 10 27 GRAA9545 119950928A213121171802 CONTROLLER DOUG DC9 DC987 3022087WP E/E COMPT MALFUNCTIONED A GRAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP111075T 49724 IFP - DURING CLIMB-OUT, THE AIRCRAFT FAILED TO PRESSURIZE. THE AIRCRAFT RETURNED TO IFP, WITHOUT FURTHER INCIDENT. MAINTENANCE RERACKED THE STANDBY PRESSURE CONTROLLER, AND RESEATED THE STATIC LINES. MAINTENANCE PERFORMED A GROUND MAINTENANCE TEST IAW MD-80 MM 21-32. OPERATIONAL CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951027005681995102700568EU 1995 10 27 RAIA950930 119950920A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE10823823 102 STL - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT ROW 2AB. (M) 2H72 4T RTA53EU 19951027005691995102700569EU 1995 10 27 RAIA950931 119950920A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE10823823 102 STL - EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY AT GALLEY. (M) 2H72 4T RTA53EU 19951027005701995102700570EU 1995 10 27 RAIA950932 119950922A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE14239 119 STL - EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED MIDDLE EMERGENCY LIGHT BATTERY. (M) 2H72 4T RTA53EU 19951027005711995102700571EU 1995 10 27 RAIA950933 119950920A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 12723728 176 STL - EMERGENCY TRACK LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES AT ROW 2AB. (M) 2H72 4T RTA53EU 19951027005721995102700572EU 1995 10 27 RAIA950934 119950920A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 12723728 176 STL - EMERGENCY TRACK LIGHTS INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES AT ROW 5CD. (M) 2H72 4T RTA53EU 19951027005731995102700573EU 1995 10 27 RAIA950935 119950922A57301379352B LE SKIN BAG JETSTMJETSTM3201 1500217EU LT WING DENT A RAIAK NONE C F.O.D. LDLANDING 1 CE03872AE9808 872 SMF - FLT NR 4717 - BIRD STRIKE ON LEFT WING ON NORMAL LANDING. A/C FERRIED TO FAT MAINTENANCE FOR REPAIRS. MAINTENANCE REPAIRED LEFT WING DE-ICE LEADING EDGE AS PER J3201 SRM AND REPLACED LEFT LEADING EDGE DE-ICE BOOT. NO FURTHER DAMAGE WAS NOTICED. (M) 2L72 4T RTA56EU 19951027005741995102700574WP 1995 10 27 RAIA950936 219950922A732189737527A FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03871JX9086 3525 871 66324 MRY - FLT NR 4790 - LEFT ENGINE LOW TORQUE. MAINTENANCE REPLACED LEFT ENGINE FUEL CONTROL UNIT. GROUND RUNS REVEALED NORMAL TORQUE INDICATION. (M) 2L72 4T4 TRTA56EU E4WE 19951027005751995102700575EU 1995 10 27 RAIA950938 119950919A3242AC63742 BRAKE MAXARET BAG JETSTMJETSTM3201 1500217EU RT MLG FAULTY A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03434AM9621 887 STL - FLT NR 7089 - RIGHT BRAKE IS NOT OPERATING. MAINTENANCE REPLACED RIGHT BRAKE MAXARET. TAXI CHECK AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19951027005761995102700576EU 1995 10 27 VTZA95309 119950927A3260ATG135022 SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT MLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27315UE 41033 IAD-PHL - FLT NR 6237 - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE RED GEAR SELECTOR HANDLE REMAINED ILLUMINATED AFTER GEAR WAS UP AND LOCKED AFTER TAKEOFF. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT STANDBY UPLOCK MICRO-SWITCH. (M) 2L72 4T RTA41NM 19951027005771995102700577EU 1995 10 27 VTZA96001 119950929A2910HTE400005 NON RETURN VLV BAG JETSTMJETSTM3201 1500217EU FUS CTR BAY LEAKING A VTZAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27490UE 909 FLT NR 6412 - ROC-IAD - DURING CRUISE, AN EMERGENCY WAS DECLARED DUE TO THERE BEING A COMPLETE LOSS OF HYDRAULIC PRESSURE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND ONE NON RETURN VALVE LEAKING AND REPLACED BOTH OF THEM. MAINTENANCE ALSO REPLACED BOTH HYDRAULIC PUMPS DUE TO CAVITATION FROM FLUID LOSS. PERFORMED INSPECTION '05' FOR TOTAL LOSS OF HYDRAULIC FLUID. ALL OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951027005781995102700578EU 1995 10 27 VTZA96003 119950929A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27307UE 41021 FLT NR 36506 - LYH-CHO - ABORTED TAKEOFF DUE TO THE BAGGAGE DOOR WARNING ILLUMINATING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 09225 IAW MEL 52-3 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 09225 BY CLEANING THE FORWARD MICRO-SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETRUN TO SERVICE. (M) 2L72 4T RTA41NM 19951027005791995102700579EU 1995 10 27 VTZA96004 119951003A3150 TAKEOFF WARNING JETAIRJETSTMJETSTM4101 1500501EU COCKPIT ACTIVATED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27317UE 41031 FLT NR 6438 - IAD-CHS - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CYCLED POWER AND PERFORMED TAKEOFF CONFIGURATION WARNING TEST, SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951027005801995102700580EU 1995 10 27 VTZA96005 119951002A52101371020C DRAW BOLT BAG JETSTMJETSTM3201 1500217EU PAX DIRTY A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27489UE 908 FLT NR 6579 - EWR-IAD - DURING APPROACH, DECLARED AN EMERGENCY DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING IN FLIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE DOOR DRAW BOLTS AND THE MICRO-SWITCHES, P/N 91SE16. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951027005811995102700581SO 1995 10 27 WTAA950272 119950924A5610 WINDSHIELD EMB 120 EMB120RT SO COCKPIT BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17276UE 120067 SMF - BIRD STRIKE REPORTED AT LEFT WINDSHIELD. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027005821995102700582EU 1995 10 27 WTAA950273 119950926A3297 WIRE BAG JETSTMJETSTM3101 1500215EU LT MLG BROKEN A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17428UE 806 SFO - LEFT MAIN LANDING GEAR RED INTRANSIT LIGHT REPORTED INOPERATIVE DURING GEAR EXTENSION. MAINTENANCE REPAIRED BROKEN WIRE AT LEFT MAIN LANDING GEAR MICRO-SWITCH, P/N 9005EN38, GEAR INDICATION SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005831995102700583EU 1995 10 27 WTAA950274 119950926A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU LT MLG OUT OF ADJUST A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17428UE 806 SFO - LEFT MAIN LANDING GEAR RED INTRANSIT LIGHT REMAINS ILLUMINATED FOLLOWING GEAR RETRACTION. MAINTENANCE ADJUSTED AND RESECURED LEFT MAIN LANDING GEAR MICRO-SWITCH. GEAR INDICATION SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005841995102700584EU 1995 10 27 WTAA950275A 119950929A32301862F RADIUS ROD BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17425UE 798 SFO - MAIN LANDING GEAR INTRANSIT LIGHTS REMAIN ILLUMINATED FOLLOWING GEAR RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE CONFIRMED LANDING GEAR SLOW TO RETRACT. REPLACED RIGHT MAIN GEAR RADIUS ROD AND MAIN HYDRAULIC SYSTEM BYPASS VALVE. LANDING GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005851995102700585EU 1995 10 27 WTAA950275B 119950929A2910247439A BYPASS VALVE BAG JETSTMJETSTM3101 1500215EU CTR FUSELAGE FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17425UE 798 SFO - MAIN LANDING GEAR INTRANSIT LIGHTS REMAIN ILLUMINATED FOLLOWING GEAR RETRACTION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE CONFIRMED LANDING GEAR SLOW TO RETRACT. REPLACED RIGHT MAIN GEAR RADIUS ROD AND MAIN HYDRAULIC SYSTEM BYPASS VALVE. LANDING GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005861995102700586 1995 10 27 WTAA950276 419950930A341439948E2803 ASI EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17122AM 120013 FAT - HIGH SPEED WARNING INDICATION REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 AIRSPEED INDICATOR. SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027005871995102700587EU 1995 10 27 WTAA950277 119951001A3350311701 EEL BATTERY PACK BAG JETSTMJETSTM3101 1500215EU CABIN DISCHARGED A WTAAK NONE L NO TEST TXTAXI/GRND HDL 1 WP17107XV 723 SMF - CABIN EMERGENCY LIGHT SYSTEM REPORTED INOPERATIVE WITH CIRCUIT BREAKER REPORTED TRIPPED. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE DISCOVERED EMERGENCY LIGHTING SYSTEM BATTERY PACKS TO HAVE LOW VOLTAGE. REPLACED BATTERY PACKS. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005881995102700588SO 1995 10 27 WTAA950278 119951003A7714SEDL0C29J NH/N1 IND EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17286UE 120175 SFO - TAKEOFF ABORTED WITHOUT INCIDENT. NR 1 NH ANALOG AND DIGITAL INDICATION DISAGREEMENT REPORTED. MAINTENANCE REPLACED NR 1 NH/N1 INDICATOR. ALL INDICATIONS NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027005891995102700589NM 1995 10 27 95UAL900017 119950626A3350S52121 SWITCH BOEING777 777222 1385219NM CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29766UA 26917 ORD - FLT NR 940-22 - EXTERIOR EMERGENCY LIGHT AT MED L1 FAILED FUNCTIONAL CHECK. REPLACED SWITCH. (M) 2L72 4F RTT0001SE 19951027005901995102700590WP 1995 10 27 95ZZZM561 119950819A323057740355508 ACTUATOR DOUG DC8 DC863 302198AWP RT MLG OUT OF ADJUST A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15950R 45903 FLT 212 - KDAY-KMCI - DURING CLIMB, GEAR NOT LATCHED AND DOOR NOT LATCHED LIGHTS AND RIGHT ALT LIGHT ON AFTER RETACTION AND UPLATCH CHECK. EXTENDED GEAR, GOT 3 GREEN, NO ABNORMALITIES. CYCLED GEAR SEVERAL TIMES AND GOT ORIGINAL INDICATIONS. FOLLOWED ABNORMAL CHECK LIST AND LANDED NORMALLY. FERRIED AIRCRAFT TO KMCN FOR MAINTENANCE. ADJUSTED RT MLG ACTUATOR IAW MM 32-32-2. ADJUSTED RT MLG LOWER SIDE BRACE IAW MM 32-11-3. OPS CHECKED GOOD IAW MM 32-10-0. (M) 2L74 4F 4A25 19951027005911995102700591WP 1995 10 27 95ZZZM562 119950925A3310BA170 BALLAST DOUG DC8 DC861 3021952WP GLARE SHIELD SHORTED A FXLAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SO1927UA 45942 ON DESCENT INTO MIAMI, EXPERIENCED BURNING ODOR IN COCKPIT. ON GROUND INSPECTION FOUND GLARE SHIELD LIGHT BALLAST OVERHEATED. REPLACED BALLAST, SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951027005921995102700592WP 1995 10 27 95ZZZM564 119950909A2740MS3911305431 MOTOR DOUG DC8 DC862 3021970WP HORIZ STAB DEFECTIVE A RIAAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO191805 MX39928 45899 RIA - FLT NR 1805 - DURING CRUISE, RUDDER VIBRATION WAS ENCOUNTERED, CREW WENT TO MANUAL REVERSION AND VIBRATION CEASED. AIRCRAFT RETURNED TO MIA FOR MAINTENANCE. REPLACED HORIZONTAL STABILIZER HYDRAULIC MOTOR, LEAK AND OPS CHECKED OK. 2L74 4F 4A25 19951027005951995102700595EU 1995 10 27 95ZZZM567 119950724A527091SE13 SWITCH BAG JETSTMJETSTM3101 1500215EU ENTRY DOOR OUT OF ADJUST A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07837JS 736 FLT NR 4020 - ABORTED FIRST TAKEOFF FOR DOOR CAP, PERFORMED CHECKLIST. ABORTED SECOND FOR CAP, RETURNED TO GATE. DEFERRED ENTRY DOOR CAPTION. FOUND DOOR MICROSWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH IAW BAE MM 52-70-00. 2L72 4T RTA21EU 19951027005961995102700596EU 1995 10 27 95ZZZM568 119950801A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A VNAAO OTHER C F.O.D. TOTAKEOFF 1 GL07833JS 725 FLT NR 4135 - DURING TAKEOFF ROLL, CREW HEARD AN AUDIBLE THUMP ON THE RIGHT SIDE OF AIRCRAFT. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AS A RESULT OF A BIRD OR SMALL ANIMAL STRIKE. NO DAMAGE WAS FOUND, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951027005971995102700597WP 1995 10 27 95ZZZM569 219950904A732189737519 FUEL CONTROL WOODWARD BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP ENGINE DEFECTIVE A VNAAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 GL07834JS 2123480 726 FLT NR 4127 - SHORTLY AFTER TAKEOFF, WHILE SETTING CRUISE POWER (97 PERCENT RPM) THE LEFT ENGINE FLAMED OUT. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REMOVED AND REPLACED LEFT FUEL CONTROL IAW MM 73-00-00. GROUND CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19951027005981995102700598EU 1995 10 27 95ZZZM570 119950809A7920L8523427 THERMOSTAT BAG JETSTMJETSTM3101 1500215EU LT OIL COOLER DEFECTIVE A VNAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 GL07852JS 724 FLT NR 4040 - AIRCRAFT RETURNED TO GATE AFTER CREW NOTICED LEFT ENGINE OIL TEMP/PRESSURE FLUCTUATION DURING TAXI. OUT STATION MAINTENANCE REPLACED LEFT ENGINE OIL COOLER VERTATHERM IAW MM 79-20-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027005991995102700599 1995 10 27 95ZZZM571 419950805A3425 HSI WIRE BAG JETSTMJETSTM3101 1500215EU COCKPIT DAMAGED A VNAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL07853JS 730 FLT NR 4035 - AIRCRAFT RETURNED TO GATE AFTER CREW REPORTED SMOKE AND ELECTRICAL BURNING SMELL IN COCKPIT. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED CHAFFED WIRES FLIGHT OFFICER HSI. REPAIRED DAMAGED WIRES IAW STANDARD MAINTENANCE PRACTICES. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951027006001995102700600WP 1995 10 27 95ZZZM572 219950817A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RIGHT POWER LOSS A VNAACD ABORTED TAKEOFF RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 GL07853JS 730 FLT NR 4144 - CREW ELECTED TO ABORT TAKEOFF AFTER NOTICING AN RPM DROP TO 99 PERCENT RIGHT ENGINE, RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CONDUCTED ENGINE GROUND RUNS IAW MM 71-00-00. WERE NOT ABLE TO DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA21EU E4WE 19951027006011995102700601WP 1995 10 27 95ZZZM573 219950821A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RIGHT DAMAGED A VNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL07839JS 748 FLT NR 4097 - DURING CLIMB-OUT, CREW NOTICED AN UNUSUAL ODOR FROM BLEED AIR SYSTEM ASSOCIATED WITH A SLIGHT RISE IN EGT RIGHT ENGINE. POST FLIGHT CHECK, CREW FOUND BLOOD ON RIGHT NACELLE AND FUSELAGE RIGHT ENGINE. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE IAW MM 71-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19951027006021995102700602WP 1995 10 27 AALA951656 119950916A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07436AA 49454 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951027006031995102700603WP 1995 10 27 HALA95124 119950920A5320 FORMER DOUG DC9 DC951 3022051WP BS 541 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13672MC 47661 HNL - IN C-CHECK, FOUND FORMER CRACKED, 2 PLACES BETWEEN LONGERONS 29R AND 30 AT STATION 541. INSTALLED NESTED DOUBLER PER SRM 53-01. (M) 2L72 4F A6WE 19951027006041995102700604WP 1995 10 27 HALA95125 119950921A5315 FLOOR BEAM DOUG DC9 DC951 3022051WP E/E COMPT CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP13672MC 47661 HNL - IN C-CHECK, FOUND HEAVY CORROSION ON MID SECTION OF E/E COMPARTMENT AFT FLOOR BEAM, L-1 HEAVY LOCAL. REMOVED DAMAGED SECTION. INSTALLED FILLER AND REPAIR ANGLES PER SRM 53-01. (M) 2L72 4F A6WE 19951027006051995102700605WP 1995 10 27 HALA95126 119950920A5320 FORMER DOUG DC9 DC951 3022051WP BS 579 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13672MC 47661 HNL - IN C-CHECK, FOUND FORMER CRACKED, 2 PLACES BETWEEN LONGERONS 29L AND 30 AT STATION 579. INSTALLED NESTED DOUBLER PER SRM 53-01. (M) 2L72 4F A6WE 19951027006061995102700606WP 1995 10 27 HALA95127 119950926A2780 EYE BOLT DOUG DC9 DC951 3022051WP LT LE SLAT SHEARED A HALAO OTHER O OTHER APAPPROACH 1 WP13709HA 47764 HNL - FLT NR 501 - ON SLAT EXTENTION, AIRCRAFT ROLLED HARD RIGHT. NO SLAT EXTENTION LIGHT, ALL PUMPS ON HIGH. FOUND SLAT DRIVE ASSEMBLY DAMAGED AT ACTUATOR EYE BOLT MOUNT. REPLACED SLAT DRIVE ASSEMBLY PER MM 27-80-04 PARA B STEP 3 AND RIGGED SLAT CABLES PER 27-80-2. OPERATIONAL CHECK OF SLAT SYSTEM OK. (M) 2L72 4F A6WE 19951027006071995102700607NM 1995 10 27 IXKA9500029 119950925A7930 OIL BYPASS IND BOEING727 727225 1384077NM NR 3 ENGINE ILLUMINATED A IXKAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA25356PA 20626 FLT NR 40 - TPA-EWR - DIVERTED TO ATL, NR 3 ENGINE LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON IN FLIGHT. BURNED OUT TWO BULBS, ALL OTHER ENGINE INDICATIONS NORMAL. PERFORMED PRECAUTIONARY SHUTDOWN. FORTY MINUTES OF WINDMILL AT 30 PSI. CLEANED OIL IN CANNON PLUG OF DIFFERENTIAL PRESSURE SWITCH. REMOVED AND REPLACED MAIN OIL FILTER, NO DEBRIS OR CONTAMINATION FOUND, OIL LIGHT OPS OK PER MM 79-00. RAN ENGINE, OPS AND LEAK CHECK OK. (M) 2L73 4F A3WE 19951027006081995102700608WP 1995 10 27 IXXA199580 119950911A5730 SKIN DOUG DC8 DC863 302198AWP WS 885 LE CRACKED A IXXAK NONE O OTHER ININSP/MAINT 1 GL23788AL721678911 45999 DURING C-CHECK, THE RIGHT LEADING EDGE SKIN WAS FOUND TO BE CRACKED AT STATION XFS 885. A DOUBLER REPAIR WAS INSTALLED IAW COTNEY ENGINEERING DRAWING SKA95164-4, DATED 8/23/95. (M) 2L74 4F 4A25 19951027006091995102700609EU 1995 10 27 M3HA95018 119950927A3230D22719000 SAFETY PIN AEROSPATR42 ATR42320 8680930EU LT MLG NOT REMOVED A M3HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13988MA 380 HNL - FLT NR 702 - LANDING GEAR DOWN AND LOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION WAS SELECTED. FLIGHT CREW UNABLE TO RESET. AIRCRAFT RETURNED TO HNL. MECHANIC FOUND SHELL OF LANDING GEAR PIN STILL INSTALLED IN LEFT LANDING GEAR. REMOVED SHELL, INSPECTED FOR COLLATERAL DAMAGE, NONE FOUND. AIRCRAFT RETURNED FOR SERVICE. (M) 2H72 4T RTA53EU 19951027006101995102700610NM 1995 10 27 MRKA9568 119950926A3350BP573 EEL BATT CHARGER BOEING737 7373M8 1384615NM CABIN FAILED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03681MA 24376 LEFT FORWARD EMERGENCY BATTERY CHARGER INOP. SUSPECT BAD INTERNAL FUSE. REMOVED AD REPLACED FORWARD LEFT EMERGENCY CHARGER. OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 19951027006111995102700611CE 1995 10 27 PLGA92095E1 119950920A32341013841377 SELECTOR BEECH 1900 1900C 1154161CE LANDING GEAR MALFUNCTIONED A PLGAO OTHER J WARNING INDICATION APAPPROACH 1 NE053069K 262 UB71 BOS-YSJ - FLT NR 4945 - DURING APPROACH, THE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS ACTIVATED. CREW PERFORMED EMERGENCY PROCEDURE FOR A GEAR EXTENSION. GEAR EXTENDED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED GEAR WAS DOWN AND LOCKED, AND NO DAMAGE TO GEAR WAS APPARENT. AIRCRAFT WAS FERRIED TO PSM FOR REPAIRS. MAINTENANCE INSPECTED SYSTEM, AND PERFORMED OPERATIONAL CHECK OF GEAR. NO FAULT WAS FOUND. GEAR HANDLE WAS REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES. AIRCRAFT WAS RELEASED BACK INTO SERVICE. (M) 2L72 4T RTA24CE 19951027006121995102700612EU 1995 10 27 RAIA950937 119950922A33503011151 EEL BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE14583 119 STL - MAINTENANCE EMERGENCY LIGHTS WILL NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY LIGHTING BATTERY. (M) 2H72 4T RTA53EU 19951027006131995102700613EU 1995 10 27 RAIA950939 119950926A2910AN8344D TEE FITTING BAG JETSTMJETSTM3201 1500217EU RT HYD SYSTEM LEAKING A RAIAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 CE03872AE9824 872 LAX - FLT 4749 - LOSE OF BOTH HYDRAULIC PUMPS ON DESCENT. CREW PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT HYDRAULIC TEE AT RIGHT HYDRAULIC PRESSURE FILTER. GEAR SWINGS REVEALED NORMAL OPERATION AND LEAK OK. (M) 2L72 4T RTA56EU 19951027006141995102700614EU 1995 10 27 RAIA950940 119950928A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03424AM1022771 865 STL - FLT 7512 - RIGHT ENGINE LOW TORQUE. ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND RUNS CHECK NORMAL. (M) 2L72 4T RTA56EU 19951027006151995102700615EU 1995 10 27 RAIA950941 119950929A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03426AM9992 6546 874 BMI - FLT NR 7331 - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTINGS. GROUND RUNS CHECK GOOD. (M) 2L72 4T RTA56EU 19951027006161995102700616EU 1995 10 27 RAIA950942 119950928A215032149602 PACK VALVE AEROSPATR72 ATR72202 8680940EU LT PACK FAILED A RAIAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03723TE 283 STL - FLT NR 7144 - SMOKE IN THE CABIN DURING TAXI. MAINTENANCE INSPECTED LEFT PACK. DISCOVERED LEFT PACK VALVE TO BE INOPERATIVE. DEFERRED AS PER MEL 21501 CATEGORY C. (M) 2H72 4T RTA53EU 19951027006171995102700617EU 1995 10 27 RAIA951001 119951001A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03972JX4640 4640 972 SAN - FLT 4707 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND RUNS GOOD. (M) 2L72 4T RTA56EU 19951027006181995102700618EU 1995 10 27 RAIA951002 119951002A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03866AE9578 9578 866 LAX - FLT 4760 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED LEFT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTING. GROUND RUNS GOOD. (M) 2L72 4T RTA56EU 19951027006191995102700619NE 1995 10 27 SIMA952771 319951004A61117900961 PROP BLDE SHEATH SAAB SF340 340B 7860101EU HAMSTD14RF 14RF19 NE RT NR 3 MISSING A ASIMAA UNSCHED LANDING DE INFLIGHT SEPARATION VIBRATION/BUFFET CLCLIMB 1 SW21329AE8218 1068 340B329 1478 DURING CLIMB-OUT AT 4,000, PILOT NOTICED AND ENGINE SURGE AND ASSOCIATED PROP VIBRATION FROM NR 2 ENGINE. UPON RETURNING TO DFW, MAINTENANCE FOUND THE RIGHT PROP NR 3 BLADE MISSING APPROXIMATELY 10 INCH SECTION OF THE EDGE SHEATH AND FOUND A .25 INCH DENT ON THE NR 1 ENGINE NACELLE. RAI RIGHT PROP BLADE AND FERRIED AIRCRAFT TO LAW FOR NACELLE REPAIR. (M) 2L72 4T RTA52EU 6 CP11NE 19951027006201995102700620SO 1995 10 27 WTAA950266 119950916A5610 WINDSHIELD EMB 120 EMB120RT SO RIGHT BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17282UE 120124 SBA - EVIDENCE OF BIRD STRIKE REPORTED AT TOP OF RIGHT WINDSCREEN. PERFORMED BIRD STRIKE INSPECTION OF AIRCRAFT. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027006211995102700621SO 1995 10 27 WTAA950267 119950917A3350D36604001 EEL POWER SUPPLY EMB 120 EMB120RT SO CABIN LOW VOLTAGE A WTAAK NONE L NO TEST ININSP/MAINT 1 WP17274UE 120054 FAT - CABIN EMERGENCY LIGHTS REPORTED PARTIALLY INOPERATIVE DURING RON MAINTENANCE. REPLACED FORWARD CABIN EMERGENCY LIGHTING POWER SUPPLY. EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027006221995102700622EU 1995 10 27 WTAA950268 119950918A261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU BAGG COMPT DIRTY A WTAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP17107XV 723 PDX - SMOKE DETECTOR LIGHT ILLUMINATED ON TAXI OUT. AIRCRAFT RETURNED TO GATE. NO EVIDENCE OF SMOKE OR FIRE NOTED. MAINTENANCE CLEANED SMOKE DETECTOR. SMOKE DETECTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027006231995102700623SO 1995 10 27 WTAA950269 119950901A532012014968001 WINDSHIELD POST EMB 120 EMB120RT SO LEFT CRACKED A WTAAK NONE O OTHER ININSP/MAINT 1 WP17120AM 120012 FAT - LATERAL WINDSHIELD POST AND SKIN DOUBLER REPORTED CRACKED AT LOWER CORNER OF CAPTAINS WINDSHIELD. MAINTENANCE REPLACED LATERAL POST AND FABRICATED AND INSTALLED REPLACEMENT SKIN DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951027006241995102700624EU 1995 10 27 WTAA950270 119950921A2130 CONNECTOR BAG JETSTMJETSTM3101 1500215EU LEFT LOOSE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17107XV 723 SFO - LEFT AIR OFF LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. DEFERRED LT FLOW CONTROL VALVE PER MEL 21-2. AIRCRAFT RETURNED TO SERVICE. FAT MAINTENANCE SUBSEQUENTLY CLEARED DEFERRED ITEM WITH THE REPLACEMENT OF THE CANNON PLUG ON THE LEFT ENGINE 4 PSI SWITCH, P/N 1103P0648. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2L72 4T RTA21EU 19951027006251995102700625EU 1995 10 27 WTAA950271 119950921A32609959118 LAMPS BAG JETSTMJETSTM3101 1500215EU LANDING GEAR FAILED A WTAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 WP17419UE 779 FAT - LANDING GEAR POSITION INDICATION LIGHTS REPORTED PARTIALLY INOPERATIVE DURING GEAR EXTENSION FOR LANDING. CREW INITIATED A GO AROUND DUE TO GEAR POSITION INDICATION PROBLEM. AIRCRAFT LANDED WITHOUT INCIDENT ON SECOND APPROACH. MAINTENANCE REPLACED THREE GEAR DOWN INDICATION LAMPS IN LANDING GEAR POSITION INDICATOR. GEAR POSITION INDICATION LIGHTS GROUND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951027006261995102700626WP 1995 10 27 Y2PA950013 119950915A27503922841561 CONTROL CABLE DOUG DC9 DC915F 3022037WP RT TE FLAP VANE BROKEN A Y2PAO OTHER O OTHER CRCRUISE 1 GL23197US 47154 YIP - AIRPLANE HAS A RYTHMATIC VIBRATION AT ALL SPEEDS, BUT MORE PRONOUNCED AT LOW ALTITUDES. INSPECTED AND FOUND RIGHT MOVEABLE VANE CABLE FOUND TO BE BROKEN (CABLE RUN NR 169A, P/N 3922841-561). REMOVED AND REPLACED BROKEN CABLE. INSPECTED ASSOCIATED EQUIPMENT FOR DAMAGE AND CONDITION, RERIGGED CABLE SYSTEM. (M) 2L72 4F A6WE 19951027006271995102700627WP 1995 10 27 9516599952 119951024A2751 FOLLOW-UP SYST DOUG DC9 DC931 3022065WP TE FLAPS OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01916RW 47144 DURING TAKEOFF, TAKEOFF WARNING HORN SOUNDED AFTER THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. RIGGED FLAP FOLLOW-UP SYSTEM, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027006281995102700628WP 1995 10 27 9516609952 119951024A2751 CONNECTOR DOUG DC9 DC931 3022065WP TE FLAPS DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01916RW 47144 DURING TAKEOFF, TAKEOFF WARNING HORN SOUNDED AFTER THROTTLES WERE ADVANCED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. FOUND RIGHT FLAP TRANSMITTER CANNON PLUG DIRTY. CLEANED CANNON PLUG, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027006291995102700629WP 1995 10 27 9516619952 119951025A3230 UPLATCH MECH DOUG DC9 DC931 3022065WP LT MLG BINDING A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01916RW 47144 DURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. UPON INSPECTION, FOUND THE LEFT MAIN LANDING GEAR UPLATCH MECHANISM BINDING. FREED MECHANISM, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951027006301995102700630WP 1995 10 27 95FDEA01598 119951025A3234 GEAR LEVER DOUG DC10 DC1010CF 3023502WP LANDING GEAR DIRTY A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO2568049 47803 AFTER LANDING GEAR EXTENSION, BOTH LANDING GEAR ANNUNCIATOR PANELS REMAINED ALL RED, RECYCLED GEAR ANNUNCIATORS REMAINED ALL RED. AFTER PUSHING HARD AND DOWN ON LANDING GEAR HANDLE ALL INDICATIONS BECAME GREEN, NORMAL LANDING ACCOMPLISHED. PINNED LANDING GEAR, OPERATED LANDING GEAR LEVER. WHEN HANDLE IS PULLED OUT OF DETENT IT W/N ALWAYS RETURN INTO MAKE SWITCH. OPENED PANEL DEGREASED, CLEANED LEVER, SLIDE, ROLLER AND RELUBED. LANDING GEAR LEVER AND INDICATOR CHECKS OK, PANEL CLOSED AND PINS REMOVED. 2L73 4F RTA22WE 19951027006311995102700631NM 1995 10 27 95FDEA01599 119951026A2910 HYD SYST BOEING727 727225 1384077NM A-HYD SYST REQD SERVICE A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25467FE 21449 UPON GEAR RETRACTION, HYD A-SYS QTY, FELL FROM 3.5 TO 1.625 GALLONS. UPON BLOCK, FOUND 3 GALLONS IN SYS, BELIEVE AIR IN SYS FROM PREVIOUS MX REF WRI 29-10/378. SERVICED HYD AS REQ, CYCLED FLT CONTROLS SEVERAL TIMES AND NO LEAKS OR QTY DROP NOTED. OK FOR SERVICE. 2L73 4F A3WE 19951027006321995102700632WP 1995 10 27 95UAL900230 119951026A3350 EEL CABLE DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291831U 46630 EEL STRIP INOPERATIVE SEATS 23B TO 30B. REPLACED FEEDER CABLE FROM WALL CONNECTION. 2L73 4F4 F A22WE E23EA 19951027006331995102700633WP 1995 10 27 ABXA9500891 119951025A323027735101 BOLT DOUG DC8 DC863 302198AWP LT MLG MISSING A ABXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23814AX 46041 DURING CLIMB, RETRACTED LANDING GEAR HANDLE AND GEAR UNSAFE LIGHT REMAINED ON. CHECKED LANDING GEAR AND DOOR LATCH POSITION, LEFT GEAR DOOR HAD AN UNLATCHED INDICATION. RECYCLED LANDING GEAR AND THE UNSAFE LIGHT REMAINED ON, LANDING GEAR WAS EXTENDED AND INDICATED DOWN AND LOCKED. INSPECTED LEFT MAIN GEAR AND FOUND THE FORWARD ATTACH BOLT AND NUT FOR THE BOGIE TRIM CYLINDER MISSING. INSTALLED FORWARD ATTACH BOLT AND NUT FOR THE BOGIE TRIM CYLINDER I/A/W DC8 MM CHAPTER 32. COMPLETED LANDING GEAR RETRACTION CHECK AND OPS CHECK WAS GOOD. 2L74 4F 4A25 19951027006341995102700634SO 1995 10 27 COMA9511991 119951021A77123036928 TQ SIGNAL COND EMB 120 EMB120RT SO LT ENG DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01264CA9581 4521 120256 THE LEFT ENGINE TORQUE INDICATION FLUCTUATES. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER. 2L72 4T RTA31SO 19951027006351995102700635SW 1995 10 27 COMA9520394 119951024A1420 CONNECTOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE LOOSE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01457AM AC694 THE RIGHT ENGINE WILL NOT ROTATE DURING START CYCLE. REPAIRED LOOSE WIRE ON THE RIGHT ENGINE STOP BUTTON. 2L72 4T RTA8SW 19951027006361995102700636EU 1995 10 27 COMA9531174 119951024A243651539007A GCU SAAB SF340 SF340A 7850100EU LT DC GEN DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01320CA17437338 340064 THE LEFT ENGINE WILL NOT ROTATE DURING START CYCLE. REPLACED THE LEFT DC GENERATOR CONTROL UNIT. 2L72 4T RTA52EU 19951027006371995102700637EA 1995 10 27 COMA9560579 119951024A2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMAK NONE N FALSE WARNING TXTAXI/GRND HDL 1 SO01920CA 7022 CARGO SMOKE WARNING MESSAGE DURING GROUND OPERTION. DEFERRED ONE CARGO SMOKE DETECTOR, DEACTIVATED. 2L72 4F RTA21EA 19951027006381995102700638EA 1995 10 27 COMA9560580 119951025A3230864806 PSEU CNDAIRCL600 CL6002B19 EA NLG FAILED A COMAO OTHER J WARNING INDICATION CLCLIMB 1 SO01938CA1745 1024 7046 THE NOSE LANDING GEAR DOES NOT RETRACT WHEN LANDING GEAR IS SELECTED UP. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19951027006391995102700639EA 1995 10 27 COMA9560581 119951024A274070604 HSTCU CNDAIRCL600 CL6002B19 EA HORIZ STAB DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01920CA2875 249 7022 STABILIZER TRIM CHANNEL NR 1 FAILS DURING FLIGHT. REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT. 2L72 4F RTA21EA 19951027006401995102700640EA 1995 10 27 COMA9560582 119951024A2760 ECU CNDAIRCL600 CL6002B19 EA NR 1/2 SPOILERONREQD RESET A COMAK NONE N FALSE WARNING UKUNKNOWN 1 SO01940CA 7048 SPOILERS FAULT MESSAGE ON EICAS. RESET THE NR 1 AND NR 2 SPOILERON ELECTRONIC CONTROL UNITS. 2L72 4F RTA21EA 19951027006411995102700641EA 1995 10 27 COMA9560583 119951025A3350363782 EEL PATH LIGHTS CNDAIRCL600 CL6002B19 EA CABIN FAILED A COMAK NONE L NO TEST ININSP/MAINT 1 SO01915CA 7013 FLOOR PATH EMERGENCY LIGHTING AT ROW 1 IS INOPERATIVE. REPLACED DEFECTIVE SECTION OF FLOOR PATH LIGHTING. 2L72 4F RTA21EA 19951027006421995102700642EA 1995 10 27 COMA9560584 119951025A276054C54677E01 MANIFOLD CNDAIRCL600 CL6002B19 EA SPOILERS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01916CA 7014 OUTBOARD GROUND SPOILERS CAUTION MESSAGE ON EICAS. REPLACED THE GROUND SPOILERS MANIFOLD ASSEMBLY. 2L72 4F RTA21EA 19951027006431995102700643NM 1995 10 27 DL72W954092 119951024A5754 ANGLE BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 FOUND ON A1 LETTER CK, .5 INCH CRACK AT INBD STOP PAD NUMBER 7 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951027006441995102700644NM 1995 10 27 DL72W954093 119951024A5754 ANGLE BOEING727 727247 138408FNM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112813W 20869 FOUND ON A1 LETTER CK, NR 2 SLAT COVE SKIN ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951027006451995102700645NM 1995 10 27 DL757954088 119951024A3520 PBE 4566M37B BOEING757 757232 1384965NM CABIN DEFECTIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO11663DN 24992 DURING PREFLIGHT, PBE CONDITION INDICATOR BUTTON WAS FOUND PUSHED UP. REPLACED PBE ASSEMBLY. 2L72 4F RTA2NM 19951027006461995102700646WP 1995 10 27 DLL10954050 119951018A55111524064106 RIBS LKHEED1011 10113851 5265010WP HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 HORIZONTAL STAB RT NR 3 L/E PANEL HAS 4 RIBS CRACKED. REPAIRED PER SRM 55-12-00 FIG 802. 2L73 4F A23WE 19951027006471995102700647WP 1995 10 27 DLL10954051 119951017A55111524199106 RIBS LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING A ROUTINE INSPECTION, NR 6 RT HORIZONTAL LEADING EDGE WAS FOUND TO HAVE ALL OF THE RIBS CRACKED AT THE T/E. DOUBLERS WERE INSTALLED PER SRM 55-12-00 FIG 802. 2L73 4F A23WE 19951027006481995102700648NM 1995 10 27 DLM88954089 119951024A3350339101087 EEL LENSE COVER DOUG MD88 MD88 3023688NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11969DL 53172 EMERGENCY LIGHT COVER MISSING, ROW 1, 12 AND 26. REPLACED LENS COVERS. 2L72 4F RTA6WE 19951027006491995102700649WP 1995 10 27 MWEA95361 119951026A5220 DOOR LATCH DOUG DC9 DC914 3022034WP EMER EXIT DOOR OUT OF ADJUST A MWEAK NONE O OTHER ININSP/MAINT 1 GL31400ME 45727 DURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT DOOR HANDLE WAS DIFFICULT TO OPERATE. MAINTENANCE ADJUSTED DOOR LATCH IAW DAC MM 52-21-0. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951027006501995102700650NM 1995 10 27 SCNA95245 119951023A2750M8911302E DRIVE MOTOR BOEING727 7272A1 138407FNM TE FLAPS LEAKING A SCNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15286SC 21601 DURING CLIMBOUT AT 13,000 FEET, THE NUMBER 1 A-SYSTEM HYDRAULIC PUMP \LO PRESS\ LIGHT ILLUMINATED AND THE A-SYSTEM QUANTITY DROPPED RAPIDLY. THE OUTBOARD FLAP DRIVE MOTOR SEAL WAS FOUND BLOWN OUT. REMOVED AND REPLACED THE MOTOR PER MM 27-57-62. 2L73 4F A3WE 19951027006511995102700651NE 1995 10 27 UPS504881 219951026A7310UL16589 MANIFOLD TUBE BOEING757 75724APF 1384969NM RROYCERB211 RB211535E4 54555NE ENGINE COMP CHAFED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01437UP 25468 WHILE ON GROUND, MAINTENANCE FOUND THRUST REVERSER INTERIM REPAIR - ALTERNATE FASTENER TO ELIMINATE FUEL SPRAY NOZZLE MANIFOLD TUBE WEAR. MAINTENANCE REPAIRED IAW UPS E.O. B757-7830-7539A. 2L72 4F4 FRTA2NM E12EU 19951027006521995102700652NM 1995 10 27 UPS504882 119951026A7720 OVERHEAT LIGHT BOEING727 72731C 1384011NM NR 2 ENGINE ILLUMINATED A IPXAE ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CRCRUISE 1 SO01924UP 19234 CREW REPORTED AT TOP OF CLIMB AS THRUST WAS REDUCED, THE NR 2 ENGINE OVERHEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR FIVE SECONDS THEN WENT OUT. ALL ENGINE INDICATIONS NORMAL EXCEPT ON EVM, THE NR 2 ENG N1 WAS AT .5, WHILE NR 1 AND NR 3 WERE .24. AT THE TOP OF DESCENT DURING THRUST REDUCTION, THE NR 2 ENGINE OVERHEAT LIGHT CAME ON STEADY ILLUMINATING THE MASTER ENGINE OVHT LIGHT ON THE FWD PANEL. PER CHECK LIST, THE NR 2 ENGINE THROTTLE WAS CLOSED AND THE LIGHT WENT OUT. AFTER 3 MINUTES AT IDLE, ENGINE SHUT-DOWN CHECK LIST WAS PERFORMED. EMERGENCY WAS DECLARED, MAINTENANCE NOTIFIED, MRR FILED OPEN. 2L73 4F A3WE 19951027006531995102700653WP 1995 10 27 UPS504883 119951026A2910 FLUID DOUG DC8 DC871F 302199DWP HYD SYST LOST A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01700UP 45900 CREW REPORTED EXPERIENCE LOSS OF HYDRAULIC PRESSURE AND FLUID. PERFORMED LOSS OF HYDRAULIC CHECK LIST, CONTINUED TO MCO. NOTIFIED MIA CENTER TO INCOMING MCO APPROACH CONTROL OUR EMERGENCY AND ASKED FOR EMERGENCY EQUIPMENT TO STAND-BY. LANDING UNEVENTFUL, TAXIED CLEAR ON RUNWAY AND STOPPED. MCO MX TOWED A/C TO RAMP. MRR FILED OPEN. 2L74 4F RT4A25 19951027006541995102700654NM 1995 10 27 UPS504884 119951026A3260H1010154 POS SWITCH BOEING727 72730C 1384009NM NLG FAILED A IPXAO OTHER N FALSE WARNING APAPPROACH 1 SO01918UP 19008 CREW REPORTED ON FINAL, THE GREEN NOSE GEAR LIGHT SUDDENLY WENT OUT AND THE GEAR HORN CAME ON. GEAR WAS CYCLED AND ALL THREE GEAR LIGHTS ILLUMINATED AGAIN. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR POSITION SWITCH AND THE NOSE GEAR LOCK SWITCH IAW MM 32-61-21. 2L73 4F A3WE 19951027006551995102700655NM 1995 10 27 UPS504885 119951026A3350 BATTERY BOEING727 72730C 1384009NM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01212UP 21392 WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-101. OPS CHECKED GOOD PER MM 33-50-101. 2L73 4F A3WE 19951027006561995102700656WP 1995 10 27 UPS504886 119951026A5320 FITTING DOUG DC8 DC873F 302199FWP BS 280/300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION IN 3 EACH B/T FITTINGS, FS 300, LONGERON 34R-33R AND LONGERON 34L-35L, AND FS 280, LONGERON 32L-33L. MAINTENANCE REPLACED THE FITTINGS PER SRM 53-2-0, FIGURE D. 2L74 4F RT4A25 19951027006571995102700657WP 1995 10 27 UPS504887 119951026A5320 FITTING DOUG DC8 DC873F 302199FWP BS 280/300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING SPLICES FS 280, LONGERON 34L-35L, FS 300, LONGERON 354-34R. MAINTENANCE REPLACED THE FITTINGS IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027006581995102700658WP 1995 10 27 UPS504888 119951026A5311 FRAME DOUG DC8 DC873F 302199FWP BS 1420 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FRAME FS 1420 BETWEEN LONGERONS 33R-34R. MAINTENANCE REPLACED A SECTION OF FRAME IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027006591995102700659WP 1995 10 27 UPS504890 119951026A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 450 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FINGER DOUBLER HEAVY CORROSION AT FS 450 BETWEEN LONGERONS 32L-32R. MAINTENANCE REPLACED DOUBLER IAW SRM 51-1-21. 2L74 4F RT4A25 19951027006601995102700660WP 1995 10 27 UPS504891 119951026A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS 1535-1545 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION FINGER DOUBLER LONGERON 31R, FS 1535-1545. MAINTENANCE REPLACED THE DOUBLER IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027006611995102700661WP 1995 10 27 UPS504892 119951026A5320 DOUBLER DOUG DC8 DC873F 302199FWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FINGER DOUBLER, LONGERON 31R, FS 70-8. MAINTENANCE REPLACED DOUBLER PER SRM 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951027006621995102700662WP 1995 10 27 UPS504893 119951026A5311 BELT FRAME DOUG DC8 DC873F 302199FWP BS 1400 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON BELT FRAME FS 1400 BETWEEN LONGERONS 36-32R. MAINTENANCE REPAIRED IAW UPS EO DC8-5310-7537A. 2L74 4F RT4A25 19951027006631995102700663WP 1995 10 27 UPS504894 119951026A5320 FITTING DOUG DC8 DC873F 302199FWP BS 1140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME AND FITTING HAS HEAVY CORROSION ON FS 1140, LONGERON 21R. MAINTENANCE REPLACED THE FITTING IAW SRM 51-3-0. 2L74 4F RT4A25 19951027006641995102700664WP 1995 10 27 UPS504895 119951026A5320 ANGLE DOUG DC8 DC873F 302199FWP BS 395 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON FRAME ATTACH ANGLE AT FS 395, LONGERON 21L. MAINTENANCE REPLACED THE ANGLE IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027006651995102700665WP 1995 10 27 UPS504896 119951026A5320 SPLICE DOUG DC8 DC873F 302199FWP BS 1340-1360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT 2 EACH LONGERON SPLICE FITTINGS FS 1340-1360, LONGERON 29L AND, FS 1400, LONGERON 35L-34R. MAINTENANCE REPLACED THE FITTINGS IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951027006661995102700666WP 1995 10 27 UPS504897 119951026A5320 WEBBING DOUG DC8 DC873F 302199FWP BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE WEBBING CORRODED AT FS 1580-LBL 50. MAINTENANCE REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19951027006671995102700667WP 1995 10 27 UPS504898 119951026A5320 SHEAR TIE DOUG DC8 DC873F 302199FWP BS 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND SHEAR TIE HAS HEAVY CORROSION AT FS 1000, LONGERON 30R-31R. MAINTENANCE REPLACED THE SHEAR TIE PER SRM 51-1-20D. 2L74 4F RT4A25 19951027006681995102700668WP 1995 10 27 UPS504899 119951026A5313 LONGERON DOUG DC8 DC873F 302199FWP FS 1355 LON 35R CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AND CRACKS LONGERON 35R, FS 1355-1420. MAINTENANCE REPLACED LONGERON SECTION FS 1360-1460 IAW SRM 51-1-20D. 2L74 4F RT4A25 19951027006691995102700669WP 1995 10 27 UPS504900 119951026A5320 FITTING DOUG DC8 DC873F 302199FWP BS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME END FITTING HAS HEAVY CORROSION AT FS 80, LONGERON 21R. MAINTENANCE REPLACED THE FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951027006701995102700670EU 1995 10 27 WWMA9500073 119951024A3244 TIRES SAAB SF340 340B 7860101EU LT MLG FAILED A WWMAO OTHER O OTHER LDLANDING 1 WP15261AE 340B261 BOTH LEFT INBOARD AND OUTBOARD MAIN LANDING GEAR TIRES BLEW DURING LANDING. MAINTENANCE FOUND THE THERMAL PLUGS BLOWN ON ONE OF THE WHEELS, BUT NOT THE OTHER. REPLACED LEFT MAIN LANDING GEAR INBOARD AND OUTBOARD BRAKES, TIRE AND WHEEL ASSEMBLIES. ALSO, REPLACED THE LEFT OUTBOARD WEIGHT ON WHEELS SWITCH AND THE NR 1 AND NR 2 BRAKE HYDRAULIC LINES. THE AIRCRAFT WAS FERRIED TO ABI FOR REPAIRS TO THE LEFT FLAP DUE TO TIRE DAMAGE TO THE LOWER SKIN. FLAP REPAIRS WERE MADE AND THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T RTA52EU 19951102000011995110200001EU 1995 11 2 SIMA950491 119950218A2121011232500 RECIRC FAN AEROSPATR72 ATR72212 EU RIGHT FAILED A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21377AT2125 AFT138 377 ACT - FLT 3833 - DURING CRUISE FLIGHT, CREW SMELLED ODOR OF SMOKE. AIRCRAFT DIVERTED TO ACT AND CFR DECLARED. AIRCRAFT LANDING MADE WITHOUT INCIDENT. EMERGENCY EVACUATION WAS CONDUCTED. MTX INSPECTED, FOUND SMELL TO COME FROM NR 2 RECIRC FAN. MEL'D FAN AND CONTINUED FLIGHT TO DFW. DFW MTX REPLACED FAN. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2578. (X) 2H72 4T RTA53EU 19951102000021995110200002NE 1995 11 2 DL312951605 219950416A7230JT9D7R4E1H HPC BLADE AIRBUS310 A310222 3930315EU PWA JT9 JT9D7R4E 52054NE NR 2 ENGINE DAMAGED A DALAO OTHER C F.O.D. ININSP/MAINT 1 SO11807PA20623 346 716121 DURING BORESCOPE INSPECTION, NR 1 ENGINE WAS FOUND WITH ONE 5TH STAGE HPC BLADE WITH FOD DAMAGE 0.080 INCH TO 0.090 INCH DEEP APPROXIMATELY .25 INCH FROM TIP. THIS WAS OUT OF LIMITS, ENGINE WAS REMOVED AND ROUTED TO SHOP. 2L72 4F4 FRTA35EU E3NE 19951102000031995110200003NE 1995 11 2 DLL17951604 219950413A7530RB211524B4D SENSE LINE LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 2 ENGINE BROKEN A DALAAE UNSCHED LANDING ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO11767DA44423 193H1209 014738 ON CLIMBOUT, GOT NR 2 ENG REVERSER LIGHT ON S/O PANEL, ACCOMPANIED BY A VIBRATION LIGHT AND NOTICABLE VIBRATION. SHUT NR 2 DOWN, RETURNED FRA. FOUND TWO SENSE LINES TO PRSOV BROKEN. ALSO, ACOUSTIC PANELS AT TOP HALF COLLAPSED. REPLACED PANELS AND SENSE LINES OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19951102000041995110200004EU 1995 11 2 AALA950537 119950323A323471539 SELECTOR VALVE FOKKERF28 F28MK0100 4990807EU NLG DEFECTIVE A AALAO OTHER J WARNING INDICATION CLCLIMB 1 SW071473K 678G 11515 DFW - FLT 1658 - DURING TAKEOFF CRP, NOSE LANDING GEAR ALERT ON MFDU, GEAR HANDLE LIGHT ILLUMINATED WITH CORRESPONDING VIBRATION. GEAR CYCLED WITH NO IMPROVEMENT. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR SELECTOR VALVE AND RESTRICTOR. CYCLED GEAR, SYSTEM GROUND CHECKS NORMAL OPERATION. (X) 2L72 4F RT 19951102000051995110200005NM 1995 11 2 95ZZZW593 119950412A5400311N52111 FUSE PIN 311N50671 BOEING757 75723APF 1384966NM LT STRUT CRACKED A CLCAK NONE O OTHER ININSP/MAINT 1 SO19573CA 24971 ON C-CHECK INSPECTION IAW SB 757-54-0020 EDDY CURRENT INSPECTION REVEALED CRACKED MIDSPAR STRAIGHT FUSE PIN ON LEFT STRUT. REMOVED AND REPLACED CRACKED FUSE PIN. 2L72 4F RTA2NM 19951102000061995110200006EU 1995 11 2 SIMA950781 119950319A77123039242 TQ PROBE AEROSPATR72 ATR72212 EU NR 1 ENGINE DEFECTIVE A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW21377AT2217 CH10162 377 AFTER TAKEOFF FROM DFW, AIRCRAFT EXPERIENCED A NR 1 ENGINE TORQUE FLUX WITH YAW. CREW SHUT DOWN ENGINE AS A PRECAUTIONARY. REPLACED NH PROBE ON NR 1 ENGINE, PERFORMED GROUND MAINTENANCE RUNS AND PERFORMED SATISFACOTRY TEST FLIGHT. AIRCRAFT RELEASED FOR SERVICE. (W) 2H72 4T RTA53EU 19951102000071995110200007NM 1995 11 2 95ZZZW656 119950425A2910 HYDRAULIC LINE BOEING757 75723APF 1384966NM LT MLG BROKEN A CLCAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19573CA 24971 FLT 056 - AFTER TAKEOFF FROM BOG, LOST LEFT HYDRAULIC SYSTEM QTY LEFT HYDRAULIC PRESSURE LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECK LIST AND TURNED BACK. FOUND BROKEN UP LINE ON LEFT LANDING GEAR SEQUENCE VALVE CAUSED BY BLOWN NR 6 TIRE. REPLACED BROKEN LINE AND CHANGED TIRES WITH BLOWN FUSE. PRESSURE CHECK HYDRAULIC SYSTEM OK OVERWEIGHT LANDING INSPECTION PERFORMED. NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA2NM 19951102000091995110200009NE 1995 11 2 DLL16951932 219950505A7314 FUEL PUMP PAC102MK4 LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 1 ENGINE FAILED A DALAA UNSCHED LANDING JX WARNING INDICATION ENGINE FLAMEOUT CRCRUISE 1 SO11759DA B1426 193Y1176 014876 DURING CRUISE, HAD NR 1 ENGINE FUEL PRESSURE LIGHT ILLUMINATED, THEN ENGINE FLAMED-OUT, ALL AIR STARTS WERE UNSUCCESSFUL, DIVERTED TO KEF. REPLACED HP FUEL PUMP, OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19951102000101995110200010NE 1995 11 2 DLL14952011 219950508A7260M06592AA ACCESS GEARBOX LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B40254555NE NR 3 ENGINE FAILED A DALAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 SO111739D 193C1237 014701 DURING CRUISE, NR 3 ENGINE FLAMED-OUT, UNABLE TO RESTART, LANDED ATL. FOUND ACCESSORY GEARBOX WITH INTERNAL FAILURE. REPLACED GEARBOX, OPERATION NORMAL. 2L73 4F4 F A23WE E12EU 19951102000111995110200011WP 1995 11 2 BUFA9510 119950413A3230 UPLATCH DOUG DC8 DC8F54 3021926WP MAIN GEAR LACK OF LUBE A BUFAO OTHER J WARNING INDICATION CLCLIMB 1 CE05925BV 45885 GEAR UPLATCH CHECK WARNING LIGHT ON. CYCLE GEAR LIGHT OUT. CLEANED AND LUBED MLG UP-LATCH MECHANISM IAW MM 32-6-2, CYCLED GEAR 6 TIMES AND OPS CHECKED IAW MM 32-3-0. RII INSPECTED. OPS CHECK OKAY. (X) 2L74 4F 4A25 19951102000121995110200012NE 1995 11 2 DLL16952120 219950512A7261FC3520100 OIL CAP LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B40254555NE NR 2 ENGINE LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11762DA 193Y1210 014717 DURING CRUISE HAD EXCESSIVE OIL LOSS ON NR 2 ENGINE, 6 QTS IN IN ABOUT 3 HOURS, LANDED LGW. FOUND OIL TANK OIL CAP LEAKING THROUGH LOCK ASSEMBLY. REPLACED OIL CAP RETURNED TO SERVICE. 2L73 4F4 F A23WE E12EU 19951102000141995110200014EU 1995 11 2 AALA950837 119950507A3350 EEL WIRE FOKKERF28 F28MK0100 4990807EU CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW071454D 11466 DFW - DURING OVERNIGHT CHECK, 2 OVERHEAD AISLE AND EXTERIOR RIGHT OVERWING EMERGENCY EXITS FOUND INOPERATIVE. REPAIRED WIRE AND REPLACED BATTERY PACK. SYSTEM GROUND CHECKS, NORMAL OPERATION. (X) 2L72 4F RT 19951102000151995110200015NM 1995 11 2 95UAL900052 119950721A5210 ASSIST BOTTLE BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE CABIN DOOR EMPTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29160UA 21237 DOOR 3R ASSIST BOTTLE SHOWS EMPTY. REPLACED DOOR ASSIST BOTTLE AT 3R PER MM 52-11-06. 2L74 4F4 F A20WE E20EA 19951102000161995110200016NM 1995 11 2 95UAL900161 119950929A5400 SPAR BOEING747 747SP21 1384802NM PWA JT9 JT9D7A 52054NE NAC STA 210-216 CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29148UA 21648 DURING NR 2 ENGINE CHANGE, FOUND NR 2 LOWER HORIZONTAL SPAR WITH 6 INCH CRACK. CRACK WAS LOCATED BETWEEN NAC STA 210 AND 216, ADJACENT TO INBOARD CHORD. REPAIRED PER ADAPTION OF SRM 54-10-03. 2L74 4F4 F A20WE E20EA 19951106000011995110600001WP 1995 11 6 9516229608 119951017A5310 FITTING DOUG DC9 DC932 3022066WP JACK SUPPORT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING D-CHECK, FOUND CORROSION ON THE JACK SUPPORT FITTING. REPLACED FITTING PER SRM 51-01 AND DWG 59-17491. DUE TO INCORRECT AIRCRAFT NUMBER, ALL OTHER REFERENCES; MODEL NUMBER, SERIAL NUMBER, ETC HAVE BEEN CHANGED RESPECTIVELY. 2L72 4F A6WE 19951106000021995110600002NE 1995 11 6 9516626740 219951024A7230 FAN EXIT LINER BOEING747 747251F 1384898NM PWA JT9 JT9D7Q 52054NE NR 1 ENGINE DETACHED A NWAAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01640US 23888 702170 DURING CLIMB, THE NR 1 ENGINE EXPERIENCED A VIBRATION WHICH CONTINUED DOWN TO IDLE AND THE ENGINE WAS SHUTDOWN. DUMPED 60,000 LBS OF FUEL AND THE AIRCRAFT RETURNED TO ANC WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS MADE. INSPECTION FOUND A PORTION OF THE FAN EXIT LINER HAD DETACHED AND WAS AGAINST THE EXIT GUIDES. THE ACOUSTICAL PANEL WAS REPLACED AND GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19951106000031995110600003WP 1995 11 6 9516639854 119951025A3260 PROX CONTL BOX DOUG DC9 DC951 3022051WP RT MLG FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01763NC 47716 DURING CLIMB, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AT 25,000 FEET. CREW RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSPECTED RIGHT MAIN LANDING GEAR AND REPLACED THE LANDING GEAR PROXIMITY SWITCH CONTROL UNIT. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951106000041995110600004NM 1995 11 6 9516646302 119951026A2560 CONNECTOR BOEING747 747451 1384940NM L5 DOOR SLIDE LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01662US 23720 TPE - DURING LINE CHECK, THE DOOR 5L EMERGENCY SLIDE LIGHT WOULD NOT EXTINGUISH. CHECKED WIRING AND RESEATED CANNON PLUG, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951106000051995110600005WP 1995 11 6 9516659992 119951025A3260 DOOR SWITCH DOUG DC9 DC931 3022065WP LT/RT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL018960E 45869 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW RECYCLED THE LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT MAIN LANDING GEAR DOOR SWITCHES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106000061995110600006NM 1995 11 6 95FDEA01602 119951026A5712 RIB BOEING727 727227 1384078NM WS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 STA 760 R/RIB CHORD HFEC CRACK INDICATION FROM FWD HOLES. INSTALLED REPAIR DOUBLER PER BOEING DRAWING 63-68490. 2L73 4F A3WE 19951106000071995110600007NE 1995 11 6 95UAL900231 219951027A7260M83248II79 O-RING BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE ACCESSORY DRIVE LEAKING A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 WP297449U 21903 696516 MODERATE VERY NOTICEABLE SMELL OF OIL PRIOR TO AND DURING TAKEOFF ROLL, AT POWER CHANGES IN CRUISE AND DESCENT, MOST CERTAINLY ENGINE OIL, EITHER NR 1 OR NR 3 DUE TO BLEED CONFIGURATION. SUPPLEMENTAL DATA UPDATE: FOUND N-1 ACCESSORY DRIVE CASE COVER LEAKING. REMOVED COVER, REPLACED O-RING, AND REASSEMBLED. 2L73 4F4 F A3WE E2EA 19951106000081995110600008NM 1995 11 6 95UAL900232 119951027A3350 EEL BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP299007U 19045 EMERGENCY ESCAPE PATH LIGHTING INOP IN AFT CABIN. REPAIRED LIGHT, CHECKS OK. 2L72 4F4 F A16WE E2EA 19951106000091995110600009NM 1995 11 6 95UAL900233 119951027A3350 BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29512UA 24809 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS 16 AND 17. EMERGENCY EXIT LIGHT INOP AT ROW 13. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951106000101995110600010WP 1995 11 6 ABXA9500892 119951026A2120 AIR DISTR NIHON YS11 YS11A500 6310416WP COCKPIT SMOKE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23910AX 2050 SMOKE IN CABIN AND COCKPIT FROM BLEED HEAT SYSTEM. SMOKE WAS BAD ENOUGH TO CAUSE MINOR THROAT IRRITATION, BUT NOT ENOUGH TO USE SMOKE EQUIPMENT. TRIED TWICE, TOOK 3 TO 5 MINUTES FOR SMOKE TO START. VISUALLY INSPECTED BLEED AIR DUCTING TO COCKPIT, RAN ENGINES, PERFORMED BLEED HEAT CHECK, OPS CHECKED NORMAL IAW YS11 MM 71-60. 2L72 4T A1PC 19951106000111995110600011WP 1995 11 6 ABXA9500893 119951026A3260MS250081 SWITCH DOUG DC8 DC862 3021970WP LANDING GEAR DEFECTIVE A ABXAO OTHER N FALSE WARNING DEDESCENT 1 GL23803AX 45917 DURING DESCENT, UNABLE TO GET DOWN AND LOCKED INDICATION ON ANY LANDING GEAR DURING INITIAL EXTENSION. RECYCLED LANDING GEAR THREE MORE TIMES WITH NO DOWN AND LOCKED INDICATION. ABNORMAL PROCEDURES WERE INITIATED AND WHEN HYDRAULIC SYSTEM WAS DEPRESSURIZED WITH THE LANDING GEAR HANDLE DOWN, THE LANDING GEAR INDICATED DOWN AND LOCKED. HYDRAULICS WERE RESTORED AND A NORMAL LANDING WAS ACCOMPLISHED. REPLACED LANDING GEAR CONTROL LEVER SWITCH AND CLEANED CORROSION ON WIRE TERMINALS I/A/W DC8 MM CHAPTER 32. 2L74 4F 4A25 19951106000121995110600012NM 1995 11 6 SCNA95247 119951024A3350S106 BATTERY BOEING727 727259 138408JNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE FORWARD CEILING MOUNTED EMERGENCY AREA LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERIES IAW 33-50-81 AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951106000131995110600013NM 1995 11 6 SCNA95248 119951024A33501000677 EEL ASSY BOEING727 727259 138408JNM COCKPIT FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE COCKPIT PORTABLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY AND LIGHT TESTED GOOD. 2L73 4F A3WE 19951106000141995110600014EU 1995 11 6 WWMA9500074 119951027A29109302631001 HYD LINE SAAB SF340 340B 7860101EU FUSELAGE CRACKED A WWMAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP15231LN 340B231 PILOT REPORTED, ON TAXI THE HYDRAULIC LIGHT CAME ON, LOST ALL HYDRAULIC FLUID AND LOST BRAKING EFFECTIVENESS. AIRCRAFT WAS TOWED BACK TO THE GATE. UPON INVESTIGATION REPLACED THE HYDRAULIC LINE BETWEEN THE PUMP AND FILTER UNIT, SERVICED THE HYDRAULIC SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE. 2L72 4T RTA52EU 19951106000291995110600029SO 1995 11 6 95ZZZX5933 119950906A3230 ACTUATOR PIPER PA31 PA31350 7103110SO LT MLG REQ ADJUSTMENT A BSYAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL0735871 31852123 LEFT GEAR NO DOWN AND LOCK LIGHT (SOF). ADJUSTED ACTUATOR, OPS CHECKED GOOD. 1L72 3O A20SO 19951106000441995110600044EA 1995 11 6 BTHA95002 219951006A8520 CRANKCASE PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1G5 41532EA NR 2 CYL CRACKED A BTHAK NONE O OTHER ININSP/MAINT 1 AL014352F3013 1529 32R7680441 L1500148A DURING ANNUAL INSPECTION, FOUND CRANKCASE CRACKED FROM EDGE OF NR 2 CYLINDER FLANGE TO FORWARD CORNER AT CYLINDER BASE STUD. EDDY CURRENT INSPECTION VERIFIED CRACK TO BE SUBSURFACE. VISUAL INSPECTION SHOWED NO CRACKING ON INSIDE OF CASE. THE CRACK WAS APPROXIMATELY 1.50 INCHES LONG. ENGINE REPLACED. (X) 1L71 3O3 O A3SO 1E4 19951106000751995110600075NE 1995 11 6 95ZZZX5967 219950913A8530114652 CYLINDER DOUG DC3 DC3 3021401WP PWA R1830 R183092 52020NE NR 14 FAILED A ACHRAA UNSCHED LANDING BR SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS NRNOT REPORTED 1 GL0312BA 1040 10035 248514 PILOT NOTICED SPARKS COMING FROM THE LEFT ENGINE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION SHOWED THAT NR 14 CYLINDER HEAD SEPARATED FROM ITS BARREL. REPLACED CYLINDER WITH O/H UNIT AND RETURNED ACFT TO SERVICE. 2L72 4R4 R A669 5E4 19951106000901995110600090EA 1995 11 6 YADA95001 219950919A741410682016 GEAR ASSY ELECTROSYS PIPER PA32 PA32R300 7103213SO LYC O540 IO540K1A5 41532EA MAG TEETH FAILED AP YADACD ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TOTAKEOFF 1 AL011063H 335 32R7780129 C2189448A BOTH GEAR ASSYS (LEFT AND RIGHT) HAVE BROKEN TEETH AND CRACKS. THIS SITUATION CAUSED ENGINE TO QUIT OPERATING. THE ENGINE WITH THE MAG WAS INSTALLED ON 6-7-95 AND THE ENGINE QUIT OPERATING ON 9-16-95 WITH 334.8 HOURS SINCE OVERHAUL. ENGINE FAILURE OCCURRED ON ROLL-OUT FOR TAKEOFF. PRE-FLIGHT RUN-UP WAS SATISFACTORY WITH A 50 RPM DROP ON BOTH RIGHT AND LEFT MAGS. COWL DAMAGED BY ENGINE BACKFIRE. (X) 1L71 3O3 O A3SO 1E4 19951106000911995110600091WP 1995 11 6 9516669752 119951003A5220 DOOR PAN DOUG DC9 DC941 302207NWP EMERG EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01752NW 47116 DURING H-CHECK, FOUND A TWO INCH CRACK IN THE FORWARD LEFT EMERGENCY OVERWING EXIT DOOR PAN. REPAIRED PAN (P/N 5913195-1) PER EA 97-102583. 2L72 4F A6WE 19951106000921995110600092WP 1995 11 6 9516679873 119951012A5220 DOOR PAN DOUG DC9 DC951 3022051WP EMERG EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01782NC 48107 DURING H-CHECK, FOUND A 1.9 INCH CRACK IN THE FORWARD LEFT EMERGENCY OVERWING EXIT DOOR PAN. REPAIRED PAN (P/N 5913195-1) PER EA 98-103293. 2L72 4F A6WE 19951106000931995110600093NM 1995 11 6 9516685502 119951019A5320 FITTING BOEING757 757251 1384970NM BS 1383 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01502US 23191 DURING T-CHECK, FOUND CORROSION ON THE BS 1383 TIE DOWN FITTING. REPLACED FITTING. 2L72 4F RTA2NM 19951106000941995110600094WP 1995 11 6 9516699979 119951023A5320 FITTING DOUG DC9 DC931 3022065WP FS 586 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING H-CHECK, FOUND CORROSION ON LONGERON 29R END FITTING AT FS 586. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951106000951995110600095NM 1995 11 6 9516702288 119951024A5320 FITTING BOEING727 727251 138408HNM FS 1183 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US 21376 DURING T-CHECK, FOUND CORROSION ON THE STR 17R TIE FITTING AT BS 1183. REPLACED FITTING PER SRM 51-10-1, PARA 4. 2L73 4F A3WE 19951106000961995110600096NM 1995 11 6 9516716613 119951019A575465B3920037 FLAP BOEING747 747251B 1384892NM NR 11 LE FLAP DAMAGED A NWAAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 GL01613US2121 2121 20358 AFTER FLIGHT ARRIVAL, MAINTENANCE DISCOVERED THAT A LARGE SECTION OF THE NR 11 LEADING EDGE FLAP WAS MISSING. NO OTHER DAMAGE WAS FOUND. REPLACED FLAP PER MM 27-81-01, PG 401. CHECKED OK. (STA AMS). 2L74 4F A20WE 19951106000971995110600097WP 1995 11 6 9516729150 119951017A5720 FENCE DOUG DC9 DC914 3022034WP LT WING LE SEPARATED A NWAAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 GL018908E 45749 AFTER FLIGHT ARRIVAL, MAINTENANCE DISCOVERED THAT THE LEFT WING LEADING EDGE FENCE WAS MISSING. REPLACED THE FENCE. 2L72 4F A6WE 19951106000981995110600098WP 1995 11 6 9516739758 119951025A2780 BOLT DOUG DC9 DC941 302207NWP LT LE FLAP DRIVEBROKEN A NWAAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL01758NW 47286 ON APPROACH DURING SLAT EXTENSION, A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN BOLT AND ROD END BEARING ON THE LEFT WING SLAT DRIVE CYLINDER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106000991995110600099 1995 11 6 9516749102 419951026A3421258733511 VERTICAL GYRO DOUG DC9 DC915 3022036WP NR 2 FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL0192S 4315935 47064 DURING CLIMB, THE FIRST OFFICER'S PITCH AND ROLL INDICATOR WAS INOPERATIVE. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 VERTICAL GYRO. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106001001995110600100WP 1995 11 6 9516759886 119951026A213094840213 AMPLIFIER DOUG DC9 DC951 3022051WP CABIN FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01600TR302 302 47783 DURING CLIMB, THE AIRCRAFT DID NOT PRESSURIZE IN AUTO MODE. AIRCRAFT DID PRESSURIZE IN MANUAL MODE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE CABIN PRESSURE AMPLIFIER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106001011995110600101NM 1995 11 6 9516762285 119951029A2910 LINE BOEING727 727251 138408HNM A HYD SYST FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01285US 21324 ON DESCENT TO MSP, THE AIRCRAFT HAD LOSS OF A HYDRAULIC SYSTEM. FOLLOWED COM PROCEDURE. ISOLATION WAS USED WITH RESTORING OF 'A' HYDRAULICS WENT TO ZERO ON LANDING. REPLACED NR 2 ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE AND CHECK CASE DRAIN FILTERS. CHECKED OK. 2L73 4F A3WE 19951106001021995110600102NM 1995 11 6 95FDEA01603 119951027A552165174373 ELEV SUPT RIB BOEING727 727225 1384077NM ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 LT ELEVATOR SUPPORT RIB AT ELEVATOR STA 99.79 IS CRACKED AT I/B LOWER CORNER. REMOVED AND REPLACED LT ELEVATOR SUPPORT RIB AT ELEVATOR STA 99.79. 2L73 4F A3WE 19951106001031995110600103NM 1995 11 6 95FDEA01604 119951027A5330 SKIN BOEING727 727225 1384077NM BS 620 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON BILGE SKIN ALONG STR AT BS 620 - 640, RBL 8 WL 150. REMOVED CORROSION ON BILGE SKIN ALONG STR AT BS 620 - 640 RBL 8 WL 150, BS 620 - 628 AND BS 631 - 640 FOUND TO BE WITHIN LIMITS. BS 629 - 630 FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1 FABRICATED AND INSTALLED REPAIR DOUBLER AT BS 629 - 630 PER FEDEX SRM 53-30-3, FIG 3. 2L73 4F A3WE 19951106001041995110600104NM 1995 11 6 95FDEA01605 119951026A5330 SKIN BOEING727 727227 1384078NM BS 328 CREASED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CREASE IN SKIN AT BS 328 BETWEEN STR 17-18L. CUT OUT DAMAGED SKIN AND REPAIRED PER FEDEX EO NR 7-5330-25992. DUE TO PROXIMITY OF DAMAGE, THIS REPAIR INCORPORATED DAMAGE DOCUMENTED ON FEDEX NR 0167. 2L73 4F A3WE 19951106001051995110600105NM 1995 11 6 95FDEA01606 119951026A5330 SKIN BOEING727 727227 1384078NM BS 312 CREASED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 CREASE IN SKIN AT BS 312 BETWEEN STR 17-18L. CUT OUT DAMAGED SKIN. DUE TO PROXIMITY OF DAMAGE, INCORPORATED THIS REPAIR WITH REPAIR DOCUMENTED ON FEDEX NR 0168. REPAIR WAS ACCOMPLISHED PER FEDEX EO NR 7-5330-25992. 2L73 4F A3WE 19951106001061995110600106NM 1995 11 6 95FDEA01607 119951024A5313BAC1498137 STRINGER BOEING727 727227 1384078NM BS 278 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 MECHANICAL DAMAGE TO STR 16L, BS 278. CUT 3 SECTIONS FROM FRAME AT BS 277 ABOVE STR 16L FOR ACCESS. REMOVED STR FROM BS 259 - 294. FABRICATED NEW SECTION OF STR AND SPLICED NEW STR AT BS 264. (NEW STR INSTALLED FROM BS 264 - 294). INSTALLED REPAIRED STR FROM BS 259 - 294. REPAIRED FRAME AND FRAME CHORDS PER FEDEX SRM 51-40-4, 51-40-3, 51-40-2. STR REPAIRED PER FEDEX EO NR 7-5310-26104. 2L73 4F A3WE 19951106001071995110600107NM 1995 11 6 95FDEA01608 119951027A53206520726 THRESHOLD STRAP BOEING727 72722 1384002NM BS 524-576 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION UNDER NUTPLATES ON THRESHOLD STRAP, STA 524 - 576, RBL 24, WL 156 (FWD BAY). 2L73 4F A3WE 19951106001081995110600108NM 1995 11 6 95FDEA01609 119951103A5320 BEAM BOEING727 72722 1384002NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON BS 344 BEAM FROM LBL 37 - RBL 15, WL 208.1 AND DOUBLE HOLE THROUGH PREVIOUS REPAIR AT LBL 19. 2L73 4F A3WE 19951106001091995110600109NM 1995 11 6 95FDEA01610 119951103A5720 CHORD BOEING727 72722 1384002NM WS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON WING 870 LOWER CHORD STA 870, LBL 38 AND RBL 45, WL 140. 2L73 4F A3WE 19951106001101995110600110NM 1995 11 6 95FDEA01611 119951103A5720 UPPER CHORD BOEING727 72722 1384002NM WS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION AND PAINT FINISH IS PEELING ON 870, WING UPPER CHORD STA 870, RBL 70 - LBL 70, WL 178. 2L73 4F A3WE 19951106001111995110600111NM 1995 11 6 95FDEA01612 119951027A5311 FRAME BOEING727 72722 1384002NM BS 1070 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FRAME STA 1070, 1 INCH ABOVE STR 27L. REPAIRED FRAME IAW FEDEX SRM 51-40-3 AND SRM 53-10-2. 2L73 4F A3WE 19951106001121995110600112NM 1995 11 6 95FDEA01613 119951027A5330 SKIN BOEING727 72722 1384002NM BS 1240 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 OUTWARD DENTS IN SKIN BS 1240 BETWEEN STR 20 - 21L. 2L73 4F A3WE 19951106001131995110600113NM 1995 11 6 95FDEA01614 119951027A5330489506 SKIN BOEING727 727233 138408ANM BS 703 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON INTERIOR SKIN SURFACE AT BS 703, BL ZERO AROUND NUTPLATES. CUT OUT CORRODED SKIN THAT WAS BEYOND LIMITS PER FEDEX SRM 53-30-4. INSTALLED DOUBLER PER FEDEX SRM 53-30-3. CLEANED AND TREATED ALL AREAS. 2L73 4F RTA3WE 19951106001141995110600114WP 1995 11 6 95FDEA01615 119951028A5743 BUSHING DOUG DC10 DC1010 3022110WP RT MLG TRUNNION MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RIGHT MLG WING TRUNNION FWD FITTING FWD LUG BUSHING MIGRATED FWD/OUT OF LUG. 2L73 4F A22WE 19951106001151995110600115WP 1995 11 6 95FDEA01617 119951028A5743 BUSHING DOUG DC10 DC1010 3022110WP RT MLG TRUNNION MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RIGHT MLG STRUT AFT TRUNNION FITTING BUSHING MIGRATED FWD/OUT OF FITTING. 2L73 4F A22WE 19951106001161995110600116WP 1995 11 6 ABXA9500894 119951029A793141800141 TRANSMITTER DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 2 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL23824AX 46141 671015 DURING DESCENT, AFTER APPROACH CHECKLIST, NR 2 ENGINE OIL PRESSURE INDICATION WENT OFF SCALE (HIGH). CHECKED, PULLED, AND RESET CIRCUIT BREAKERS FOR NR 2 ENGINE OIL PRESSURE INDICATION WITH NO CHANGE. SHUTDOWN NR 2 ENGINE FOR APPROXIMATELY FIVE MINUTES PRIOR TO LANDING. REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER. 2L74 4F4 F 4A25 1E8 19951106001171995110600117SW 1995 11 6 COMA9520395 119951025A29102781032081 HYD LINE SWRNGNSA227 SA227AC 8780603SW NLG LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01459AM AC700 HYDRAULIC FLUID IS LEAKING FROM THE WING CENTER SECTION. REPLACED THE NLG RETRACT HYDRAULIC LINE ASSEMBLY. 1L72 4T A8SW 19951106001181995110600118EU 1995 11 6 COMA9531175 119951027A242131342001 GENERATOR SAAB SF340 SF340A 7850100EU RIGHT FAILED A COMAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO01146CA130771330 340A146 THE RIGHT AC GENERATOR FAILED DURING FLIGHT. REPLACED THE RT AC GENERATOR. 2L72 4T RTA52EU 19951106001191995110600119EU 1995 11 6 COMA9531176 119951027A21607769022 CONTL VALVE SAAB SF340 SF340A 7850100EU LT DUCT DEFECTIVE A COMAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01158CA15519 340A158 LEFT DUCT OVERHEAT WARNING DURING FLIGHT. REPLACED THE DUAL TEMPERATURE CONTROL VAVLE. 2L72 4T RTA52EU 19951106001201995110600120 1995 11 6 COMA9531177 419951027A34256226190113 COMPUTER SAAB SF340 SF340A 7850100EU NR 1 AHRS DEFECTIVE A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01158CA1451416 340A158 LEFT AND RIGHT HEADING COMPARATOR YELLOW FLAG DURING FLIGHT. REPLACED THE NR 1 AHRS COMPUTER. 2L72 4T RTA52EU 19951106001211995110600121 1995 11 6 COMA9560585 419951026A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 EA NR 2 YAW DAMPER DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 SO01932CA3870 7038 YAW DAMPER NR 2 WILL NOT STAY ON LINE. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR. 2L72 4F RTA21EA 19951106001221995110600122EA 1995 11 6 COMA9560586 119951026A323017300201 HARNESS CNDAIRCL600 CL6002B19 EA NLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01938CA 7046 THE NOSE LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED THE LT NLG WEIGHT-ON-WHEEL PROXIMITY SENSOR AND HARNESS ASSEBMLY. 2L72 4F RTA21EA 19951106001231995110600123NE 1995 11 6 COMA9560587 219951027A72505121T35G01 BORESCOPE PLUG CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT ENGINE BROKEN A COMAK NONE EC VIBRATION/BUFFET F.O.D. UKUNKNOWN 1 SO01946CA785 7072 LEFT ENGINE N2 VIBRATION WARNING ON EICAS. REMOVED AND REPLACED THE LT ENGINE DUE TO FOD CAUSED BY A DEFECTIVE BORESCOPE PLUG, WHICH SEPERATED AND ENTERED THE ENGINE. 2L72 4F4 FRTA21EA E15NE 19951106001241995110600124EA 1995 11 6 COMA9560588 119951027A28202421143 VALVE CNDAIRCL600 CL6002B19 EA LT FUEL SYST FAILED A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01943CA1485 7062 LEFT FUEL TRANSFER SHUT OFF VALVE CAUTION MESSAGE ON EICAS. REPLACED THE FUEL TRANSFER VALVE. 2L72 4F RTA21EA 19951106001251995110600125NE 1995 11 6 DL31L954119 219951026A7200 ENGINE AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE NR 1 ENGINE BIRD STRIKE A DALAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SO11837AB10269 674 724909 AIR-TURN-BACK, BIRD STRIKE ON CLIMB, NR 1 ENGINE APPROX 3000 FEET. ENGINE CONTINUED RUNNING, VIB 4.8. LANDED JFK WITHOUT INCIDENT. ENGINE WAS SHUT DOWN AFTER LANDING. FOUND NUMEROUS FIRST STAGE FAN BLADES DAMAGED AND DAMAGE TO INLET COWL INNER LINER. REPLACED ENGINE AND NOSE COWL. 2L72 4F RTA35EU E24NE 19951106001261995110600126NM 1995 11 6 DL72E954113 119951026A5320 HINGE COVER BOEING727 727247 138408FNM RT NLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11282WA 21484 FOUND ON D1 LETTER CK - RT NLG WW DOOR HINGE COVER CRACKED IN UPPER RADIUS. REPAIRED PER SRM 51-40-2. 2L73 4F A3WE 19951106001271995110600127NM 1995 11 6 DL72E954115 119951024A5315 FLOOR BEAM BOEING727 727247 138408FNM BS 400 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV 2 CHECK, CORROSION AT FLOOR BEAM STA 400, BETWEEN RBL 33 AND 57. REPAIRED PER M/M 53-20-11. 2L73 4F A3WE 19951106001281995110600128NM 1995 11 6 DL72E954116 119951008A533065C139131 SKIN BOEING727 727247 138408FNM BS 950 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV IN ATLANTA, MTC FOUND CORROSION IN FUSELAGE SKIN AT STA 950 PLUS 10 INCHES JUST OUTBOARD OF STR 30. FINAL CUT-OUT DIMENSIONS ARE 2.75 INCHES BY 3.75 INCHES. THE SKIN IS FABRICATED FROM 2024-T3 CLAD AND HAS A NOMINAL THICKNESS OF 0.183 INCH AT THE FWD LOCATION OF THE CUT-OUT AND 0.145 INCH ALONG THE AFT EDGE OF THE CUTOUT. ER/A REPAIRED DAMAGED AREA BY INSTALLING A DOUBLER, TRIPLER, AND QUADRUPLER AND CHEM TREATING THE AREA. 2L73 4F A3WE 19951106001291995110600129NM 1995 11 6 DL72E954117 119951006A5720 VENT ACCESS HOLE BOEING727 727247 138408FNM WS 656.5 MISLOCATED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO112824W 21329 DURING ACCOMPLISHMENT OF THE LT WING UPPER STRINGER 13/14 TAB ONLY REPAIR AT WS 656.5 RIB, THE VENTB OX ACCESS HOLE WAS INADVERTENTLY CUT INBD OF THE RIB INSTEAD OF OTBD. THIS REPAIR WAS BEING ACCOMPLISHED PER B727 M/M 57-13-0 FIG. 804, REPAIR FOR TAB CRACKS ONLY. THIS ER/A AUTHORIZES MIRRORING THE REPAIR TO ACCOMMODATE THE ACCESS HOLE ON THE INBD SIDE OF WS 656.5 RIB. AD 88-17-06. 2L73 4F A3WE 19951106001301995110600130NM 1995 11 6 DL72E954133 119951024A5315 FLOOR BEAM BOEING727 727247 138408FNM BS 344 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11830WA 21482 FOUND ON CV 2 CHECK, CORROSION AT NUT CLIP HOLES TOP AND UNDERSIDES OF FLOOR BEAM STA 344 BETWEEN LBL 10 AND 60. REPAIRED PER SRM 53-10-8, FIG 10. INSTALL DOUBLER AND TRIPLER ON CRACKED LEG ONLY PER ENGINEER D.S.W. 2L73 4F A3WE 19951106001311995110600131NM 1995 11 6 DL72L954126 119950621A5751652176634 SKIN BOEING727 727232 1384082NM RT AILERON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11513DA 21315 DURING SHOP INSPECTION, RIGHT WING OUTBOARD AILERON WAS FOUND WITH DENTED UPPER SKIN AT 37 INCHES FROM I/B END AND OVERSIDE HOLE SKIN TO RIB FASTENER HOLE AT 2ND FROM I/B RIB. REPAIRED PER SRM 57-50-5, FIG 2. 2L73 4F A3WE 19951106001321995110600132NM 1995 11 6 DL72S954104 119951025A3350 BATTERY 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11476DA 20753 L-2 PORTABLE EMERGENCY LIGHT INOP, REPLACED BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19951106001331995110600133NM 1995 11 6 DL72S954122 119951027A5754 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11540DA 22386 .25 INCH CRACK, NR 5 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW O/B STOP PAD. FOUND AT A-2 LTR, CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951106001341995110600134NM 1995 11 6 DL72S954123 119951027A5754 ANGLE BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11540DA 22386 .25 INCH CRACK, NR 8 SLAT, LWR COVE SKIN ATTACH ANGLE BELOW TAIL DUCT AT PREVIOUS DOUBLER. FOUND AT A-2 LTR CK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951106001351995110600135NM 1995 11 6 DL72S954137 119951024A33501102833 EEL BOEING727 727232 1384082NM AFT STAIRWELL INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11519DA 21470 DURING INSPECTION, FOUND AFT STAIRWELL EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY OPERATION NORMAL. 2L73 4F A3WE 19951106001361995110600136NM 1995 11 6 DL72S954138 119951013A3350900542 EEL BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11411DA 21223 DURING INSPECTION, RT AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19951106001371995110600137NM 1995 11 6 DL72S954139 119951015A2560 GIRT BAR HOOK BOEING727 727232 1384082NM FWD ENTRY DOOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11403DA 21147 ON DEPARTURE, FWD ENTRY DOOR SLIDE GIRT BAR HOOK BROKEN, REPLACED HOOK, OPERATION NORMAL. 2L73 4F A3WE 19951106001381995110600138NM 1995 11 6 DL72W954095 119951025A335081 BULB BOEING727 727247 138408FNM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112817W 20873 RT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED, OPERATION NORMAL. 2L73 4F A3WE 19951106001391995110600139NM 1995 11 6 DL72W954096 119951025A3350900542 BATTERY PACK BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112817W 9600 20873 LT AFT OVERWING EMERGENCY LIGHT INOP. FOUND DEFECTIVE BATTERY PACK, REPLACED PACK, OPERATION NORMAL. 2L73 4F A3WE 19951106001401995110600140NM 1995 11 6 DL72W954140 119951028A35304566M37B PBE BOEING727 727247 138408FNM CABIN POPPED INDICATORA DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO112822W 21327 DURING PRE-FLIGHT, FOUND FWD CABIN PBE INDICATOR POPPED. REPLACED PBE. 2L73 4F A3WE 19951106001411995110600141NM 1995 11 6 DL733954127 119951028A56105893543110 WINDOW BOEING737 737347 1384647NM RT COCKPIT CRACKED A DALAK NONE O OTHER CRCRUISE 1 SO11313WA 23599 FIRST OFFICER'S FORWARD WINDOW R1 OUTER PANE CRACKED IN-FLIGHT. LANDED SLC. REPLACED WINDOW PER MM. 2L72 4F RTA16WE 19951106001421995110600142NM 1995 11 6 DL73E954094 119951024A3350 EEL WIRE BOEING737 737247 138448DNM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11242WA 23516 FOUND EMERGENCY FLOOR TRACK LIGHT MISSING AT ROW 10, AND TRACK WIRING IN POOR CONDITION. REPLACED LIGHT AND REPAIRED WIRING AS NECESSARY, OPERATION NORMAL. 2L72 4F A16WE 19951106001431995110600143NM 1995 11 6 DL73S954118 119951022A57146545410223 FLOOR BEAM BOEING737 737232 1384475NM BS 662 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11308DL 23080 DURING LAYOVER AT ATLANTA, THE BL ZERO FLOOR BEAM OF THE WING CENTER SECTION WAS FOUND CRACKED AT STA 662. NO CRACKS WERE FOUND IN THE WEB. THE CRACK IS TYPICAL PER BOEING SERVICE BULLETIN 737-57-1210. REPAIRED DAMAGE PER S/B. 2L72 4F RTA16WE 19951106001441995110600144NM 1995 11 6 DL73S954135 119951026A3350 BATTERY BOEING737 737232 1384475NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11311DL 23083 ON PRE-FLIGHT CHECK, FWD CABIN FLOOR TRACK LIGHTS FOUND INOP. REPLACED BATTERY PACKS, OPERATION NORMAL. 2L72 4F RTA16WE 19951106001451995110600145NM 1995 11 6 DL757954141 119951015A3350 EEL TRACK BOEING757 757232 1384965NM CABIN LOOSE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11634DL 23615 DURING INSPECTION, SEVERAL EMERGENCY TRACK LIGHT MODULES FOUND LOOSE AND OUT OF TRACK IN FWD CABIN. SECURED TRACK MODULES RETURNED TO SERVICE. 2L72 4F RTA2NM 19951106001461995110600146NM 1995 11 6 DL767954120 119951027A3350 EEL POWER SUPPLY BPS73 BOEING767 767232 1385132NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11108DL 15859 22220 ON LAYOVER, FOUND 3 EXIT SIGNS EMERG LIGHTS INOP, MID-CABIN, RT SIDE. REPLACED POWER SUPPLY. OPERATION NORMAL. 2L72 4F RTA1NM 19951106001471995110600147NE 1995 11 6 DL76L954107 219951025A7230 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE STALLED A DALAEJA ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING JR WARNING INDICATION PARTIAL RPM/PWR LOSS CLCLIMB 1 SO11178DN20795 25143 724169 AT APPROX 1,000 FEET AFTER TAKEOFF IN FRA, THE LT ENGINE HAD A SERIES OF COMPRESSOR STALLS, OVERTEMP WARNING CAME ON, TEMP WENT TO 737 DEGREES, POWER DROPPED BACK TO NEAR IDLE. WITNESSES REPORTED FLAMES FROM LEFT ENGINE AND BAD VIBRATIONS. THE ENGINE WAS SHUT-DOWN AND A/C RETURNED TO FRA. FUEL DUMP WAS USED. REPLACED NR 1 ENGINE PER CARD DECK 1T148. PRE-FLIGHT CHECK AND OVERWEIGHT LANDING INSPECTION PERFORMED. 2L72 4F4 FRTA1NM E24NE 19951106001481995110600148NM 1995 11 6 DL76S954097 119951024A3411 PITOT TUBE 856LU1 BOEING767 767332 1382001NM LEFT CONTAMINATED A DALACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 SO11116DL 156681 23275 ABORTED TAKEOFF DUE TO NO AIRSPEED IND ON CAPTS A/S INDICATOR. AIRSPEED 105 KTS, GROSS WT 285, TEMP 60 DEGREES. BLEW DEBRIS OUT OF CAPTS PITOT TUBE. REPLACED PITOT TUBE, PRECAUTION BLEW PITOT AND STATIC LINE FROM ADC TO PITOT TUBE CONNECTORS. PUMPED A/C TO MAX AIRSPEED AND ALT - ALL CKS NORMAL. 2L72 4F RTA1NM 19951106001491995110600149WP 1995 11 6 DLL10954124 119951027A3350081691 BULB LKHEED1011 10113851 5265010WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11720DA 193C1136 EMERGENCY PATH LIGHT AT SEAT 23HJ IS BROKEN. REPLACED LAMP HOLDER AND BULB, CKS GOOD. 2L73 4F A23WE 19951106001501995110600150WP 1995 11 6 DLL17954100 119951025A3350 EEL POWER SUPPLY 5165741 LKHEED1011 10113853 5265020WP PWA JT8 JT8D15A 52051NE CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11769DL 37720 193H1218 687675 EMERGENCY LIGHTS AT L-2 DOOR INOP. REPLACED EMERGERGENCY LIGHT, POWER SUPPLY CKS OK. 2L73 4F4 F A23WE E2EA 19951106001511995110600151NM 1995 11 6 DLM88954114 119951026A5610 WINDSHIELD 5912290502 DOUG MD88 MD88 3023688NM RT COCKPIT SHATTERED A DALAO OTHER O OTHER CRCRUISE 1 SO11907DE UNKNOWN 53416 EN ROUTE DFW/OAK, F/O R1 WINDSHIELD SHATTERED. REPLACED R1 WINDOW AND CONTROLLER. 2L72 4F RTA6WE 19951106001521995110600152NM 1995 11 6 DLM88954136 119951024A3350 EEL WIRE DOUG MD88 MD88 3023688NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11910DL 49541 ON PRE-FLIGHT, FOUND EMERGENCY FLOOR LIGHTING INOP AFT OF ROW 24. REPAIRED BROKEN WIRE IN TRACK, OPERATION NORMAL. 2L72 4F RTA6WE 19951106001531995110600153SO 1995 11 6 SWIA95648 119951015A27225298 LINEAR ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER TRIM MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RUDDER CABLE OUTBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS AND ALL WORKS NORMAL. 2L72 4T4 TRTA31SO E20NE 19951106001541995110600154SO 1995 11 6 SWIA95649 119951015A27225298 LINEAR ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER TRIM MALFUNCTIONED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RUDDER TRIM CABLE INBOARD AFT SECTION WORN. INSTALLED RUDDER TRIM ACTUATOR AND ATTACHING CABLES. ADJUSTED CABLE TENSIONS TO 40 POUNDS. 2L72 4T4 TRTA31SO E20NE 19951106001551995110600155SO 1995 11 6 SWIA95650 119951015A2730 CABLES EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ELEVATOR WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RT ELEVATOR OUTBOARD AFT SECTION WORN. REMOVED AND REPLACED RT ELEVATOR OUTBOARD AFT CABLE. TIGHTENED CABLES. 2L72 4T4 TRTA31SO E20NE 19951106001561995110600156SO 1995 11 6 SWIA95651 119951015A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RT WING RIB NR 15 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 15. 2L72 4T4 TRTA31SO E20NE 19951106001571995110600157SO 1995 11 6 SWIA95652 119951015A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 RT WING RIB NR 16 HAS BROKEN CLIPS. REPLACED ALL BROKEN CLIPS ON RT WING RIB 16. 2L72 4T4 TRTA31SO E20NE 19951106001581995110600158SO 1995 11 6 SWIA95653 119951015A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 LT WING'S RIB NR 15 HAS BROKEN CLIPS. REMOVED AND REPLACED THREE WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 15. 2L72 4T4 TRTA31SO E20NE 19951106001591995110600159SO 1995 11 6 SWIA95654 119951015A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING BROKEN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07197SW 120186 LT WING RIB NR 16 HAS BROKEN CLIPS. REMOVED AND REPLACED SIX WING SKIN SUPPORT BRACKET CLIPS ON RIB NR 16, LT WING. 2L72 4T4 TRTA31SO E20NE 19951106001601995110600160NM 1995 11 6 UPS504901 119951026A5230 SEAL BOEING767 76734AF 1385212NM CARGO DOOR BLOWN A IPXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01302UP 27240 SIMULATED ETOPS WHILE AT YQX, A/C SUSTAINED RAPID DECOMPRESSION IN-FLIGHT AND DIVERTED TO YQX. MAINTENANCE FOUND MAIN CARGO DOOR SEAL BLOWN. REPLACED DOOR SEAL AND OPERATIONAL CHECK OF PRESSURIZATION SYSTEM NORMAL FOR BOTH SYS 1 AND SYS 2. 2L72 4F RTA1NM 19951106001611995110600161WP 1995 11 6 UPS504902 119951027A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1120.7 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE ON GROUND, MAINTENANCE FOUND CORROSION ON REPAIR DOUBLER AT FUSELAGE STA 1120.7. MRR FILED OPEN. 2L74 4F RT4A25 19951106001621995110600162WP 1995 11 6 UPS504903 119951027A5330 SKIN DOUG DC8 DC871F 302199DWP AFT FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 WHILE ON GROUND, MAINTENANCE FOUND SKIN CORROSION AFT OF AIR COND BAY DOOR. MRR FILED OPEN. 2L74 4F RT4A25 19951106001631995110600163WP 1995 11 6 UPS504904 119951027A2560 BATTERY WIRE DOUG DC8 DC873F 302199FWP ESCAPE SLIDE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 46080 WHILE ON GROUND IN EAST MIDLANDS, MAINTENANCE FOUND PIREP-EMERGENCY ESCAPE SLIDE BATTERY PACK WIRING BROKEN. MAINTENANCE REMOVED THE SLIDE AND DEFERRED PER E.O. MRR FILED OPEN. 2L74 4F RT4A25 19951106001641995110600164WP 1995 11 6 UPS504905 119951027A3260 UP LOCK LIGHT DOUG DC8 DC873F 302199FWP LDG GEAR HANDLE ILLUMINATED A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01807UP 46007 CREW REPORTED WITH LANDING GEAR HANDLE IN UP POSITION, DOOR NOT LATCHED LIGHT STAYED ON. LIGHT ON F.E. PANEL WAS NOT ON. CYCLED GEAR TWICE-NO HELP. PLACED GEAR IN UPLATCH POSITION AND LIGHT WENT OUT GIVING A GOOD UPLATCH CHECK. MAINTENANCE DEFERRED PER MEL 32-8 (M-99951). 2L74 4F RT4A25 19951106001651995110600165WP 1995 11 6 UPS504906 119951027A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1540 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION ON LONGERON 31R, FS 1540. MAINTENANCE REPAIRED PER UPS E.O. DC8-5310-7527A. 2L74 4F RT4A25 19951106001661995110600166WP 1995 11 6 UPS504907 119951027A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 1340-1460 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY INTERGRANULAR CORROSION ON LONGERON 31R, FS 1340 TO FS 1360. MAINTENANCE REPAIRED PER UPS E.O. DC8-5310-7520-D. 2L74 4F RT4A25 19951106001671995110600167WP 1995 11 6 UPS504908 119951027A5313 LONGERON DOUG DC8 DC873F 302199FWP BS 280-300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 35L, FS 280-300 AND ON LONGERON 33L, FS 320. MAINTENANCE REPLACED LONGERON SECTION FS 190-390 PER SRM 51-1-20D. 2L74 4F RT4A25 19951106001681995110600168WP 1995 11 6 UPS504909 119951027A5315 FLOOR BEAM DOUG DC8 DC873F 302199FWP BS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FLOOR BEAM HEAVY CORROSION AT FS 1580, LBL 50. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7529A. 2L74 4F RT4A25 19951106001691995110600169WP 1995 11 6 UPS504910 119951027A5330 SKIN DOUG DC8 DC873F 302199FWP BS 55 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FLOOR BEAM HEAVY CORROSION AT FS 1580, LBL 50. MAINTENANCE REPAIRED PER UPS EO DC8-5310-7529A. 2L74 4F RT4A25 19951106001701995110600170WP 1995 11 6 UPS504911 119951027A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1140-1150 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN HAS HEAVY CORROSION ON FS 1140-1150, LONGERON 33R. MAINTENANCE REPAIRED IAW UPS E.O. DC8-5330-7525A. 2L74 4F RT4A25 19951106001711995110600171WP 1995 11 6 UPS504912 119951027A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1350-1450 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FUSELAGE SKIN HAS CRACK DAMAGE AT FS 1350-1450, LONGERON 31R. MAINTENANCE REPAIRED IAW UPS E.O. DC8-5330-7546A. 2L74 4F RT4A25 19951106001721995110600172WP 1995 11 6 UPS504913 119951027A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE LOWER SIDE OF THE FRAME AT THE STRINGER CUT-OUT. MAINTENANCE REPAIRED THE FRAME IAW SRM 54-10-03. 2L74 4F RT4A25 19951106001731995110600173WP 1995 11 6 UPS504914 119951027A5320 SHEAR TIE DOUG DC8 DC873F 302199FWP BS 1640 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SHEAR TIE AT 2 PLACES AT STATION 1640L BETWEEN STRINGERS 50 AND 51L. MAINTENANCE REMOVED THE DAMAGED PART FROM SHEAR TIE AND REPAIRED SHEAR TIE ACCORDING TO SRM 53-10-04. 2L74 4F RT4A25 19951106001741995110600174WP 1995 11 6 UPS504915 119951027A5312 BLKHD WEB DOUG DC8 DC873F 302199FWP BS 2160 DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HOLE DAMAGE IN THE AFT BULKHEAD AT STATION 2160 AND LBL 45. MAINTENANCE REMOVED THE DAMAGED PART FROM THE WEB AND REPAIRED THE WEB ACCORDING TO SRM 51-40-02. 2L74 4F RT4A25 19951106001751995110600175WP 1995 11 6 UPS504916 119951027A5311 FRAME DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE RADIUS OF THE LOWER SIDE OF THE FRAME. MAINTENANCE REPAIRED THE FRAME IAW SRM 51-30-02/05. 2L74 4F RT4A25 19951106001761995110600176WP 1995 11 6 9516779989 119950729A5330 SKIN DOUG DC9 DC931 3022065WP FS 57 69 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018945E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT SIDE NOSE LANDING GEAR WHEELWELL SKIN FS 57 - 69. REPAIRED SKIN (P/N 5911400) PER EA 99-94862. 2L72 4F A6WE 19951106001771995110600177WP 1995 11 6 9516789989 119950729A5312 BLKHD WEB DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018945E 47181 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND THE AFT PRESSURE BULKHEAD WEB FS 996 TO HAVE LOOSE RIVETS (LONGERON 26R - 27R), CRACKS (AT LONGERON 28R, 29R), AND CORROSION (BL 0). REPAIRED WEB (P/N 5910130-65) PER EA 99-94812. 2L72 4F A6WE 19951106001781995110600178WP 1995 11 6 9516791159 119951012A5315 FLOOR BEAM DOUG DC10 DC1040 3023508WP FS 791 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND 0.5 INCH CRACKS IN THE FS 791 FLOOR BEAM UPPER CAP, LBL 20 - RBL 20. REPAIRED CAP (P/N ADA 7226-13) PER EA 11-99329. 2L73 4F A22WE 19951106001791995110600179WP 1995 11 6 9516801159 119951017A5320 WEB DOUG DC10 DC1040 3023508WP FS 1900-1928 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND CORROSION IN THE LEFT OUTBOARD FLOOR WEB AND DOUBLER AT FS 1900 - 1928, LBL 90. 2L73 4F A22WE 19951106001801995110600180NM 1995 11 6 9516812288 119951019A5313 LONGERON BOEING727 727251 138408HNM FS 480-520 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US 21376 DURING T-CHECK, FOUND CORROSION ON STR 26R AT BS 480 - 520. REPAIRED STRINGER (P/N 65-56236-52) PER EA 22-99221. 2L73 4F A3WE 19951106001811995110600181WP 1995 11 6 9516821159 119951019A5311 FRAME DOUG DC10 DC1040 3023508WP FS 879 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 33. REPAIRED FRAME (P/N ADA 7034) PER EA 11-99361. 2L73 4F A22WE 19951106001821995110600182WP 1995 11 6 9516831159 119951019A5320 MOUNTING PLATES DOUG DC10 DC1040 3023508WP RADIO ALTIMETER CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND CORROSION ON BOTH FORWARD RADIO ALTIMETER MOUNTING PLATES. REPAIRED RINGS (P/N AYB 7022, 7053) PER EA 11-103171. 2L73 4F A22WE 19951106001831995110600183NM 1995 11 6 9516842288 119951020A5313 LONGERON BOEING727 727251 138408HNM FS 414 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01288US 21376 DURING T-CHECK, FOUND A CRACK IN THE STR 26R AT BS 414. REPAIRED STRINGER (P/N 65-18220-83) PER EA 22-99222. 2L73 4F A3WE 19951106001841995110600184WP 1995 11 6 9516851159 119951024A5311 FRAME DOUG DC10 DC1040 3023508WP FS 895-1002 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAMES AT LONGERON 41R, FS 895 AND 1002. REPAIRED FRAMES (P/N ADA 0233-3, -4) PER EA 11-99323. 2L73 4F A22WE 19951106001851995110600185WP 1995 11 6 9516861159 119951024A5320 DOOR JAMB DOUG DC10 DC1040 3023508WP FS 892 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB INNER BEAM FS 882 AT LONGERON 43L. REPAIRED BEAM (P/N ADA 0251-1) PER EA 11-99322. 2L73 4F A22WE 19951106001861995110600186WP 1995 11 6 9516879979 119951025A5320 FITTING DOUG DC9 DC931 3022065WP FS 597 CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING H-CHECK, FOUND CORROSION ON THE CARGO TRACK SUPPORT FITTING AT FS 597 BETWEEN LONGERONS 27R - 28R. REPLACED FITTING PER SRM 51-30-8. 2L72 4F A6WE 19951106001871995110600187WP 1995 11 6 9516881159 119951025A5313 LONGERON DOUG DC10 DC1040 3023508WP FS 2160 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01159US 46768 DURING T-CHECK, FOUND A THREE INCH CRACK IN LONGERON 45L AT FS 2160. REPAIRED LONGERON (P/N AJC 7208-1) PER EA 11-103208. 2L73 4F A22WE 19951106001881995110600188WP 1995 11 6 9516899965 119951023A7711 EPR INDICATOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01911RW 47149 656091 NR 1 ENGINE EPR INDICATOR FROZE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE INDICATOR. SYSTEM OPERATION RETURNED TO NORMAL. 2L72 4F4 F A6WE E2EA 19951106001891995110600189WP 1995 11 6 9516909853 119951023A7830 TR UNLOCK SW DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01762NC 47710 696702 NR 1 THRUST REVERSER UNLOCK WARNING ILLUMINATED SHORTLY AFTER TAKEOFF. STAYED ON APPROXIMATELY 15 MINUTES THEN EXTINGUISHED. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE REVERSER UNLOCK SWITCH. SUBSEQUENT FUNCTIONAL TEST WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951106001901995110600190WP 1995 11 6 9516921161 119951028A2781802527 SLAT SENSOR DOUG DC10 DC1040 3023508WP LE FLAPS MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01161US3065319194 46770 DURING TAKEOFF, THE SLAT DISAGREE LIGHT AND THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED SLAT SENSORS AND REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX. 2L73 4F A22WE 19951106001911995110600191NM 1995 11 6 9516936306 119951024A521080330034 RESERVOIR BOEING747 747451 1384940NM R1 DOOR LOW PRESSURE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01666US 23821 DURING LINE CHECK (SEL), THE DOOR R1 EMERGENCY POWER RESERVOIR PRESSURE WAS FOUND BELOW LIMITS. REPLACED THE EMERGENCY POWER RESERVOIR. INSPECTED AND CHECKED OK. 2L74 4F RTA20WE 19951106001921995110600192NM 1995 11 6 9516942201 119951030A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01201US 22154 OVERNIGHT PRE-FLIGHT FOUND FIRST SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND BATTERY PACK. SYSTEM CHECK OK. 2L73 4F A3WE 19951106001931995110600193WP 1995 11 6 9516959920 119951027A5270 DOOR WARNING DOUG DC9 DC932 3022066WP AFT CABIN DOOR ACTIVATED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01942N 47459 DURING TAKEOFF ROLL IND-MEM AT APPROXIMATELY 20 KNOTS, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF WITHOUT FURTHER INCIDENT AND RETURNED TO THE GATE. DEFERRED REPAIR PER MEL 33-17A. 2L72 4F A6WE 19951106001941995110600194 1995 11 6 9516969869 419951028A2210 ACTUATOR DOUG DC9 DC951 3022051WP YAW DAMPER MALFUNCTIONED A NWAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL01778NC 48100 DURING CLIMB, OSCILLATIONS WERE EXPERIENCED IN THE YAW AXIS OF THE AIRCRAFT. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE YAW DAMPER ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106001951995110600195NM 1995 11 6 9516972294 119951030A2750 RETRACT MECH BOEING727 727251 138408HNM TE FLAPS LACK OF LUBE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01294US 21505 DURING INITIAL APPROACH WHEN LOWERING FLAPS, THE OUTBOARD FLAPS ASYMMETRIC TRIPPED AT APPROXIMATELY 5 DEGREES. CHECKED FLAP TRACK ROLLERS, TORQUE TUBES, AND TRANSMITTERS. CHECKED FOR BINDING AND SMOOTHNESS OF OPERATION. LUBED TRACKS AND JACKSCREWS. OPERATIONAL CHECK OK. 2L73 4F A3WE 19951106001961995110600196NM 1995 11 6 95UAL900234 119951030A2721 CONTROL SYST BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RUDDER TRIM BINDING A UALAO OTHER F FLT CONT AFFECTED TOTAKEOFF 1 WP29369UA 24538 ON TAKEOFF, RUDDER TRIM WAS ADDED WITH NO RESPONSE ON CONTROLS. SEVERAL MINUTES LATER, RUDDER PEDALS KICKED BACK TO RIGHT AND TRIM WAS ADDED INSTANTLY. SYSTEM SEEMS TO BIND. ALSO, BINDS WHEN PUTTING IN LEFT TRIM. 2L72 4F4 FRTA16WE E2GL 19951106001971995110600197NM 1995 11 6 95UAL900235 119951030A3350 BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29339UA 24243 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW FOUR. REPLACED BATTERY PACK. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951106001981995110600198 1995 11 6 95UAL900236 419951030A2211 ROLL COMPUTER HONEYWELL 4030951901 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE AUTO PILOT FAILED A UALAK NONE O OTHER NRNOT REPORTED 1 WP297290U 21568 BOTH CHANNELS 'A' AND 'B' UNCOMMANDED ROLL TO RIGHT. CHANNEL 'B' HAD TO MANUALLY OVERRIDE ROLL. ON GROUND ENGAGED AILERON GOES INTO RIGHT TURN, KNOB MUST BE TURNED FULL LEFT TO LEVEL AILERON. REPLACED AUTOPILOT ROLL COMPUTER, PASSED SELF TEST. 2L73 4F4 F A3WE E2EA 19951106001991995110600199NM 1995 11 6 95UAL900237 119951030A2550 CLIPS BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CARGO DOOR OUT OF POSITION A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP297255U 21402 FLIGHT DIVERTED TO ORD DUE TO UNABLE TO MAINTAIN CABIN PRESSURE. AT FLIGHT LEVEL, CABIN REACHED 11,000 FEET. UNABLE TO MAINTAIN CABIN ALTITUDE LOWER. FOUND DOOR NET CLIPS STUCK BETWEEN DOOR JAMB AND SEAL. INSTALLED NET CORRECTLY. 2L73 4F4 F A3WE E2EA 19951106002001995110600200NM 1995 11 6 95UAL900238 119951030A27819752844 SWITCH ASSY BOEING747 747422 1384935NM PWA 4056 PW4056 NE LE FLAPS MALFUNCTIONED A UALAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP29174UA 24381 AIRCRAFT EXPERIENCED INTERMITTENT -FLAPS PRIMARY+ AND -FLAPS DRIVE+ MESSAGES IN-FLIGHT SOON AFTER TAKE-OFF. FLIGHT CREW ELECTED TO DUMP FUEL AND RETURN TO FIELD. THE L1 LEADING EDGE FLAP DRIVE UNIT POSITION SWITCH ASSEMBLY WAS REPLACED WITH AN IMPROVED P/N SWITCH. THE OLD SWITCH HAS BEEN KNOWN TO CAUSE NUISANCE EICAS MESSAGES. 2L74 4F4 FRTA20WE E24NE 19951106002011995110600201WP 1995 11 6 ABX9500905 119951024A5311013500501 FRAME NIHON YS11 YS11A500 6310416WP BS 8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FUSELAGE FRAME AT STA 8080 BETWEEN LONGERONS 30LT TO 28RT. REPAIRED I/A/W YS-11 SRM 53-3-2. 2L72 4T A1PC 19951106002021995110600202WP 1995 11 6 ABXA9500895 119951027A2120 AIR DISTR NIHON YS11 YS11A500 6310416WP CABIN SMOKING A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23910AX 2050 SMOKE IN COCKPIT FROM BLEED HEAT, DRY TAKEOFF. DEFERRED NR 2 ENGINE BLEED HEAT I/A/W YS-11 M.E.L. 21-13. MAINTENANCE PROCEDURES COMPLIED WITH, PLACARD INSTALLED. D.I. NR 910-076. 2L72 4T A1PC 19951106002031995110600203WP 1995 11 6 ABXA9500896 119951026A5320013438001 INTERCOSTAL NIHON YS11 YS11A500 6310416WP BS 6120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A LONGITUDINAL FLOOR BEAM AT STA 6120. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002041995110600204WP 1995 11 6 ABXA9500897 119951027A5315013438001 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 7580 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A LONGITUDINAL FLOOR BEAM AT STA 7580. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002051995110600205WP 1995 11 6 ABXA9500898 119951024A5315013438001 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A LONGITUDINAL FLOOR BEAM AT STA 4200. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002061995110600206WP 1995 11 6 ABXA9500899 119951025A5315013438001 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4680 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A LONGITUDINAL FLOOR BEAM AT STA 4680. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002071995110600207WP 1995 11 6 ABXA9500900 119951024A531501353591 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 4200. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002081995110600208WP 1995 11 6 ABXA9500901 119951025A531501343331 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 6120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 6120. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002091995110600209WP 1995 11 6 ABXA9500902 119951026A531501343341 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 6600 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 6600. REPAIRED I/A/W ABX REA Y153 13209-MR. 2L72 4T A1PC 19951106002101995110600210WP 1995 11 6 ABXA9500903 119951025A531503343341 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 6600 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 6600. REPAIRED I/A/W ABX REA Y153 13193-MR. 2L72 4T A1PC 19951106002111995110600211WP 1995 11 6 ABXA9500904 119951025A5315013536721 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 8080. REPAIRED I/A/W ABX REA Y153 13193-MR. 2L72 4T A1PC 19951106002121995110600212WP 1995 11 6 ABXA9500906 119951022A531501353611 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 5160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 5160. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002131995110600213WP 1995 11 6 ABXA9500907 119951023A531501353571 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 3240 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 3240. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002141995110600214WP 1995 11 6 ABXA9500908 119951023A531501353591 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 4200. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002151995110600215WP 1995 11 6 ABXA9500909 119951023A531501353571 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 3240 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 3240. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002161995110600216WP 1995 11 6 ABXA9500910 119951025A531501353601 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4680 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 4680. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002171995110600217WP 1995 11 6 ABXA9500911 119951026A531503343361 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 7580 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 7580. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002181995110600218WP 1995 11 6 ABXA9500912 119951025A531501353601 FLOOR BEAM NIHON YS11 YS11A500 6310416WP BS 4680 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23922AX37750 2120 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOOR BEAM AT STA 4680. REPAIRED I/A/W ABX REA Y153 13211-MR. 2L72 4T A1PC 19951106002191995110600219WP 1995 11 6 ABXA9500913 119951026A3350 BULB DOUG DC8 DC862 3021970WP COCKPIT FAILED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23801AX 46077 DURING PRE-FLIGHT INSPECTION, FOUND EMERGENCY LIGHTS DISARM LIGHT INOP. RELAMPED EMERGENCY LIGHTS DISARM LIGHT. OPS CHECK WAS GOOD. 2L74 4F 4A25 19951106002201995110600220WP 1995 11 6 ABXA9500914 119950911A78306AL6V2SN TRANSLATING RING DOUG DC8 DC863 302198AWP NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING 825AX MOD, FOUND NR 2 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 2 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11887. 2L74 4F 4A25 19951106002211995110600221WP 1995 11 6 ABXA9500915 119950911A78306AL6V2SN TRANSLATING RING DOUG DC8 DC863 302198AWP NR 4 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING 825AX MOD, FOUND NR 4 ENGINE THRUST REVERSER TRANSLATING RING CRACKED. REPAIRED NR 4 ENGINE THRUST REVERSER TRANSLATING RING IAW ABX REA D878-11909. 2L74 4F 4A25 19951106002221995110600222WP 1995 11 6 ABXA9500916 119950911A57535653509501 SPAR CAP DOUG DC8 DC863 302198AWP LT TE FLAP SPLIT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING 825AX MOD, FOUND LEFT HAND OUTBOARD FLAP CENTER SLIDING PANEL STAINLESS STEEL DOUBLER HAS CORROSION AND AFT SPAR TOP CAP IS SPLIT. REPAIRED LEFT HAND OUTBOARD FLAP CENTER SLIDING PANEL STAINLESS STEEL DOUBLER ABD AFT SPAR TOP CAP IAW ABX REA D857-12444. 2L74 4F 4A25 19951106002231995110600223WP 1995 11 6 ABXA9500917 119950911A57535653509501 SPAR CAP DOUG DC8 DC863 302198AWP LT TE FLAP DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING 825AX MOD, FOUND LEFT HAND OUTBOARD FLAP UPPER SPAR CAP IS CUT OUT. REPAIRED LEFT HAND OUTBOARD FLAP UPPER SPAR CAP IAW ABX REA D857-12466. 2L74 4F 4A25 19951106002241995110600224WP 1995 11 6 ABXA9500918 119950911A3110 INSTRUMENT PANEL DOUG DC8 DC863 302198AWP COCKPIT MISLOCATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23825AX 46115 DURING 825AX MOD, FOUND INSTRUMENT PANEL ON MAIN FRAME NEEDS TO BE MODIFIED TO ABX STANDARDS. REPAIRED INSTRUMENT PANEL MAIN FRAME IAW ABX REA D825-11935. 2L74 4F 4A25 19951106002251995110600225WP 1995 11 6 ABXA9500919 119950911A53145614943101 KEEL BEAM DOUG DC8 DC863 302198AWP BS 920 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23813AX 46136 DURING 813AX C-CHECK INSPECTION, FOUND CRACK IN RIGHT HAND KEEL WEB AT STATION 920.00. REPAIRED RIGHT HAND KEEL WEB AT STATION 920.00 IAW ABX REA D853-12602. 2L74 4F 4A25 19951106002261995110600226WP 1995 11 6 ABXA9500920 119950911A5711 SPAR DOUG DC8 DC863 302198AWP WS 69.5 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23813AX 46136 DURING 813AX C-CHECK INSPECTION, FOUND LEFT HAND WING STATION XCW 69.5 CRACK INDICATIONS AT HOLES A AND C. REPAIRED LEFT HAND WING AT STATION XCW 69.5 LOWER REAR SPAR CAP AND WING SKIN IAW ABX REA D857-12573MR. 2L74 4F 4A25 19951106002271995110600227WP 1995 11 6 ABXA9500921 119950911A5711 SPAR DOUG DC8 DC863 302198AWP WS 69.5 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23813AX 46136 DURING 813AX C-CHECK INSPECTION, FOUND LEFT HAND WING AT STATION XCW 69.5 HAS 3 EACH DAMAGED HOLES IN FORWARD LEG OF FORWARD LOWER SPAR CAP IN CENTER TANK. REPAIRED DAMAGED HOLES AT LEFT WING STATION XCW 69.5 IAW ABX REA D857-12575MR. 2L74 4F 4A25 19951106002281995110600228WP 1995 11 6 ABXA9500922 119950911A3610 ANGLE DOUG DC8 DC863 302198AWP NR 3 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23813AX 46136 DURING 813AX C-CHECK INSPECTION, FOUND AFT BAND CLAMP ON NR 3 ENGINE TRANSITION DUCT CRACKED. REPAIRED ATTACH ANGLE CHANNEL ON NR 3 ENGINE TRANSITION DUCT IAW ABX REA D878-12566MR. 2L74 4F 4A25 19951106002291995110600229WP 1995 11 6 ABXA9500923 119950922A5315 FLOOR BEAM DOUG DC8 DC863 302198AWP FS 180 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND FLOOR BEAM SUPPORT LEG AT FS 180 CORRODED. REPAIRED FLOOR BEAM SUPPORT AT FS 180 IAW ABX REA D853-12608MR. 2L74 4F 4A25 19951106002301995110600230WP 1995 11 6 ABXA9500924 119950922A5311 FRAME DOUG DC8 DC863 302198AWP BS 702 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND NUMEROUS DRILLED HOLES AND CORROSION IN STATION 702 L1-L21R FRAME. REPAIRED STATION 702 L1-21R FRAME IAW ABX REA D853-12703MR. 2L74 4F 4A25 19951106002311995110600231WP 1995 11 6 ABXA9500925 119950922A5313 LONGERON DOUG DC8 DC863 302198AWP FS 1080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND LONGERON L27L CORRODED AT FS 1080 IN THE AFT CARGO PIT. REPAIRED LONGERON L27L AT FS 1080 IAW ABX REA D853-12471MR. 2L74 4F 4A25 19951106002321995110600232WP 1995 11 6 ABXA9500926 119950922A53205772787 DOOR JAMB DOUG DC8 DC863 302198AWP CARGO DOOR MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND NUMEROUS DRILL MARKS AND MISDRILLED HOLES ON MAIN CARGO DOOR AFT SIDE TORQUE BOX WEB STA 280. REPAIRED MAIN CARGO DOOR AFT JAMB STRUCTURE AND WEB IAW ABX REA D853-12582MR. 2L74 4F 4A25 19951106002331995110600233WP 1995 11 6 ABXA9500927 119950922A552056550153 TIP CAP DOUG DC8 DC863 302198AWP LT ELEVATOR DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND DENT IN LEFT HAND ELEVATOR OUTBOARD TIP CAP. REPAIRED LEFT HAND ELEVATOR OUTBOARD TIP CAP IAW ABX REA D855-12346MR. 2L74 4F 4A25 19951106002341995110600234WP 1995 11 6 ABXA9500928 119951006A53204645516501AX ANGLE DOUG DC8 DC863 302198AWP FS 958 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23824AX 46141 DURING 824AX C-CHECK INSPECTION, FOUND CRACK IN T-ANGLE UNDER KEEL BEAM AT FS 958 SEEN FROM LEFT HAND MAIN LANDING GEAR WHEELWELL. FABRICATED NEW T-ANGLE IAW ABX PFE D853-10446 AND INSTALLED IAW DC8 SRM, CHAPTER 51-1-20D. 2L74 4F 4A25 19951106002351995110600235NM 1995 11 6 DHL95741007 119951028A2611 SMOKE LIGHT BOEING727 7272Q9 138448MNM CARGO COMPT ILLUMINATED A TDHLAO OTHER N FALSE WARNING CRCRUISE 1 SO01741DH 21931 MAIN CARGO SMOKE DETECTOR INDICATOR LIGHT ILLUMINATED IN-FLIGHT. EXTINGUISHED ON FINAL APPROACH. INSPECTED MAIN CARGO DECK SMOKE DETECTOR SYSTEM. NO DEFECTS NOTED. SYSTEM OPS CHECKS NORMAL PER B727 M/M 26-10-7. 2L73 4F RTA3WE 19951106002361995110600236NM 1995 11 6 DHL95741008 119951031A2781H1010262 SWITCH BOEING727 7272Q9 138448MNM NR 5 LE FLAPS FAILED A TDHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01741DH 21931 NR 5 KRUGER FLAP LIGHTS REMAIN ON AT FORWARD AND S/O PANEL. REMOVED AND REPLACED NR 5 LEADING EDGE FLAP SWITCH PER M/M 27-81-0. OPS CHECK GOOD. 2L73 4F RTA3WE 19951106002371995110600237WP 1995 11 6 MWEA95362 119951029A5730 SKIN DOUG DC9 DC914 3022034WP LT WING LE DENTED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31500ME 45711 CREW REPORTS BIRD STRIKE ON LEFT WING AT DCA. DURING BIRD STRIKE INSPECTION AT DCA, FOUND LEFT WING LEADING EDGE DENTED BEYOND LIMITS STA XRS 80. AIRCRAFT FERRIED TO MKE. MAINTENANCE IN MKE INSTALLED DOUBLER REPAIR IAW SRM 57-06, FIG 2 AS A TEMPORARY REPAIR. WILL INSTALL PERMANENT REPAIR AT D-CHECK. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951106002381995110600238NM 1995 11 6 SCNA95211 119950912A5320608265 SUPPORT BOEING727 727259 138408JNM BS 380-400 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE FLOOR SUPPORT AT BS 380-400 RBL-WL 208 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW REPAIR MEMBERS IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002391995110600239NM 1995 11 6 SCNA95212 119950912A5320AND101331401 SUPPORT BOEING727 727259 138408JNM BS 344-360 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR SUPPORT AT BS 344-360, RBL 12 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED NEW REPAIR MEMBERS IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002401995110600240NM 1995 11 6 SCNA95213 119950912A5315608265 FLOOR BEAM BOEING727 727259 138408JNM BS 440 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR BEAM AT BS 440 RBL 4 TO RBL 12 WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED THE FLOOR BEAM IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002411995110600241NM 1995 11 6 SCNA95214 119950911A5347606549 SEAT TRACK BOEING727 727259 138408JNM BS 640 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE CENTER FLOOR MOUNT RAIL AFT OF BS 640, NEAR STRINGER 27R, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIRS IAW B727 51-40-03. 2L73 4F A3WE 19951106002421995110600242NM 1995 11 6 SCNA95215 119950911A5347606549 SEAT TRACK BOEING727 727259 138408JNM BS 640 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE CENTER FLOOR MOUNT RAIL AFT OF BS 640, INBOARD OF STRINGER 28L, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIRS IAW B727 SRM 53-40-03. 2L73 4F A3WE 19951106002431995110600243NM 1995 11 6 SCNA95216 119950912A5347606549 SEAT TRACK BOEING727 727259 138408JNM BS 360-440 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE OUTBOARD SEAT TRACK AT BS 360-440, NEAR STRINGER 17, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-05. 2L73 4F A3WE 19951106002441995110600244NM 1995 11 6 SCNA95217 119950912A5320 DOOR JAMB BOEING727 727259 138408JNM R1 DOOR CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), A CRACK WAS FOUND IN THE R1 DOOR JAMB LOWER FORWARD CORNER. THE DOOR JAMB WAS REMOVED, CRACK STOP DRILLED, REPAIRS FABRICATED AND INSTALLED IAW B727 SRM 51-40-03. 2L73 4F A3WE 19951106002451995110600245NM 1995 11 6 SCNA95218 119950908A53136516338352 STRINGER BOEING727 727259 138408JNM BS 720C-720D CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), STRINGER 27R WAS FOUND TO HAVE LEVEL 2 CORROSION BETWEEN STATION 720C THROUGH 720D. REMOVED CORRODED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR MEMBERS IAW B727, SRM 53-10-01 AND SRM 51-40-04. 2L73 4F A3WE 19951106002461995110600246NM 1995 11 6 SCNA95219 119950913A5320608265 SUPPORT BOEING727 727259 138408JNM BS 284.5 CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), A CRACK AND LEVEL 1 CORROSION WAS FOUND ON THE FLOOR SUPPORT AT BS 284.5, RBL 0 TO RBL 6. REMOVED CRACK AND CORROSION, FABRICATED L-ANGLE REPAIR AND FILLER AND INSTALLED IAW B727 SRM 51-40-04 AND SRM 53-10-08. 2L73 4F A3WE 19951106002471995110600247NM 1995 11 6 SCNA95220 119950925A5320 WEB BOEING727 727259 138408JNM BS 950 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE WEB AT BS 950B, LBL 10 WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIRS IAW B727 SRM 51-40-03 AND SRM 53-10-01. 2L73 4F A3WE 19951106002481995110600248NM 1995 11 6 SCNA95221 119950918A5320608265 SUPPORT BOEING727 727259 138408JNM BS 360-380 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE CABIN FLOOR SUPPORT AT BS 360-380, RBL 12 (NEAR STRINGER 17R) WAS FOUND TO HAVE LEVEL 1 CORROSION. REMOVED CORRODED FLOOR SUPPORT, FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002491995110600249NM 1995 11 6 SCNA95222 119950911A531514902831 FLOOR BEAM BOEING727 727259 138408JNM BS 1110 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE FLOOR BEAM AT BS 1110 WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED CORRODED UPPER CHORD, FABRICATED AND INSTALLED NEW UPPER CHORD, ANGLES, AND ANGLE STRAPS IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002501995110600250NM 1995 11 6 SCNA95223 119950912A5347AND101331401 SEAT TRACK BOEING727 727259 138408JNM BS 340-460 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), THE SEAT TRACK LOCATED AT BS 344-460, ON THE INBOARD SIDE OF STRINGER 17L, WAS FOUND TO HAVE LEVEL 2 CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW B727 SRM 53-10-05. 2L73 4F A3WE 19951106002511995110600251NM 1995 11 6 SCNA95224 119950912A5315606479 FLOOR BEAM BOEING727 727259 138408JNM BS 344 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE MAIN CABIN FLOOR BEAM UNDER TAPE AND CLIP NUTS AT BS 344, RBL 14 TO THE L-1 DOOR. REMOVED CORRODED SECTION OF BEAM, FABRICATED AND INSTALLED REPAIR MEMBERS IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002521995110600252NM 1995 11 6 SCNA95225 119950912A5315606479 FLOOR BEAM BOEING727 727259 138408JNM BS 400 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE MAIN CABIN FLOOR BEAM AT BS 400 STRINGER 17-LBL 24 THRU RBL 12. REMOVED AND REPLACED THE FLOOR BEAM IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002531995110600253NM 1995 11 6 SCNA95226 119950918A5320608265 SUPPORT BOEING727 727259 138408JNM BS 380 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), LEVEL 2 CORROSION WAS FOUND ON THE CABIN FLOOR SUPPORT AT BS 380 STRINGER 17R-RBL 64. REMOVED CORRODED SECTION OF BEAM, FABRICATED, AND INSTALLED REPAIR MEMBERS IAW B727 SRM 53-10-08. 2L73 4F A3WE 19951106002541995110600254NM 1995 11 6 SCNA95227 119950922A531265564418 BLKHD CHORD BOEING727 727259 138408JNM BS 950 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), BS 950 BULKHEAD LOWER T-CHORD HAS LEVEL 2 INTERGRANULAR CORROSION AT STRINGER 29R. REMOVED AND REPLACED THE LOWER CHORD IAW B727 SRM 51-40-04 AND SRM 51-10-06. 2L73 4F A3WE 19951106002551995110600255NM 1995 11 6 SCNA95228 119950911A532065255777 SUPPORT BOEING727 727259 138408JNM BS 750-740 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15289SC 22475 DURING HEAVY MAINTENANCE VISIT (HMV), LEFT LOWER SUPPORT FRAME AT BS 750E TO 740 FOR BODY FAIRINGS WAS FOUND TO HAVE LEVEL 2 CORROSION BEYOND SRM LIMITS. REMOVED AND REPLACED SUPPORT FRAME IAW B727 51-40-03. 2L73 4F A3WE 19951106002561995110600256NM 1995 11 6 SCNA95249 119951025A3350900835A BATTERY PACK BOEING727 727282 138408TNM CABIN DISCHARGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15281SC 21949 THE R-2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT THE TOP OF THE R-2 DOOR AND LIGHT TESTED GOOD IAW MM 33-50-01. 2L73 4F RTA3WE 19951106002571995110600257NM 1995 11 6 SWAA950677 119951022A7933162BLB02 OIL TEMP IND BOEING737 7372H4 138448CNM PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A SWAAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0724SW 20925 707324 EXPERIENCED NR 1 ENGINE OIL HIGH OIL TEMP. CREW PERFORMED ENGINE SHUT-DOWN CHECK LIST. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE. REPLACED OIL TEMP INDICATOR, OIL TEMP BULB, OIL, AND MAIN OIL FILTER. 2L72 4F4 F A16WE E2EA 19951106002581995110600258NM 1995 11 6 SWAA950678 119951022A323069355006 UPLOCK ACTUATOR BOEING737 7373H4 1384600NM LT MLG MALFUNCTIONED A SWAAK NONE J WARNING INDICATION APAPPROACH 1 SW07367SW 26578 ON APPROACH, AFTER GEAR EXTENSION, LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, WITH NO HELP. MANUALLY EXTENDED GEAR AND GREEN OK LIGHT ILLUMINATED. LANDED AT DAL WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR AND PERFORMED RETRACTION, OK PER BOEING M/M. 2L72 4F RTA16WE 19951106002591995110600259NM 1995 11 6 SWAA950679 119951022A2612896768 FIRE LOOP BOEING737 7372H4 138448CNM APU MALFUNCTIONED A SWAAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 SW0752SW 21533 APU FIRE DETECTION WARNING LIGHT ILLUMINATED. CREW EXPENDED FIRE BOTTLE. LANDED AT HOU WITHOUT INCIDENT. INSPECTED AREA AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REPLACED FIRE BOTTLE AND CONTINUED PER MEL 26-7. DURING RON, REPLACED APU TAILPIPE FIRE LOOP PER BOEING M/M. 2L72 4F A16WE 19951106002601995110600260NM 1995 11 6 SWAA950680 119951020A2781 SENSOR BOEING737 7375H4 138449DNM NR 2 LE FLAP MALFUNCTION A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW07502SW 24179 AFTER TAKEOFF, NR 2 KRUGER FLAP INDICATED NO RETRACTION. AIRCRAFT RETURNED TO HOU AND MADE AN UNEVENTFUL LANDING. INSPECTED AREA. REPLACED FLAP FULL UP PROXIMITY SENSOR PER BOEING M/M. 2L72 4F RTA16WE 19951106002611995110600261SO 1995 11 6 SWIA95655 119951021A5720 SUPPORT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 RT WING RIB NR 15 HAS 4 CRACKED WING SKIN SUPPORT BRACKETS. REMOVED AND REPLACED 4 CRACKED WING SKIN SUPPORT BRACKETS ON RIB NR 15 RT WING. 2L72 4T4 TRTA31SO E20NE 19951106002621995110600262SO 1995 11 6 SWIA95656 119951021A5720 SUPPORT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 RT WING RIB NR 16 HAS 2 CRACKED WING SKIN SUPPORT BRACKETS. REMOVED AND REPLACED 2 CRACKED WING SKIN SUPPORT BRACKETS WITH NEW ONES ON RT WING RIB NR 16. 2L72 4T4 TRTA31SO E20NE 19951106002631995110600263SO 1995 11 6 SWIA95657 119951022A5720 SUPPORT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 LT WING RIB NR 16 HAS 2 EACH CRACKED SKIN SUPPORT BRACKETS. REMOVED AND REPLACED 3 CRACKED SKIN SUPPORT BRACKETS ON RIB NR 16 IN THE LT WING. 2L72 4T4 TRTA31SO E20NE 19951106002641995110600264SO 1995 11 6 SWIA95658 119951022A5720 SUPPORT EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 LT WING RIB NR 16 HAS ONE SKIN SUPPORT BRACKET CRACKED. REMOVED AND REPLACED ONE CRACKED SKIN SUPPORT BRACKET ON THE LT WING. 2L72 4T4 TRTA31SO E20NE 19951106002651995110600265SO 1995 11 6 SWIA95659 119951021A2721 TRIM ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 RUDDER TRIM CABLE AT AFT BULKHEAD WORN. REPLACED RUDDER TRIM ACTUATOR AND CABLES WITH SERVICEABLE ASSEMBLY. OP CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19951106002661995110600266SO 1995 11 6 SWIA95660 119951021A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07203SW 120240 RT RUDDER OUTBOARD CABLE WORN AFT SECTION. REPLACED RT RUDDER OUTBOARD AFT SECTION CABLE WITH SERVICEABLE CABLE. 2L72 4T4 TRTA31SO E20NE 19951106002671995110600267NM 1995 11 6 UPS204917 119951028A2911 ACCUMULATOR BOEING727 72722C 138400FNM A HYD SYST LEAKING A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 SO01942UP 19101 ON DESCENT OUT OF 24,000 FEET 85 MILES NORTHWEST OF JAX, THE A-HYDRAULIC QTY GAUGE WENT TO ZERO. THE LEFT A-HYD LOW PRESSURE LIGHT CAME ON FOLLOWED BY THE RIGHT ONE. PILOT CALLED FOR THE A-HYDRAULIC LEAK OR LOSS CHECK LIST. MANUAL GEAR EXTENSION WAS INITIATED. NORMAL LANDING WAS MADE. NOSE PIN WAS INSTALLED, AND THE AIRCRAFT WAS TOWED INTO PARKING. MAINTENANCE REPAIRED THE LEAK AT A-SYS. ACCUMULATOR, SERVICED RESERVOIR. LUBRICATED NOSE GEAR. OPERATED ALL 3 LANDING GEARS MANUALLY AND HYDRAUCIALLY OPERATED NORMALLY IAW MM 32-34-00. 2L73 4F A3WE 19951106002981995110600298NM 1995 11 6 95FDEA01618 119951028A5311 FRAME BOEING727 72722 1384002NM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FRAME STA 1070, 1 INCH ABOVE STR 27L. INSTALLED FRAME REPAIR AT BS 1070 BETWEEN STR 26-27L IAW FEDEX SRM 51-40-3 AND SRM 53-10-2. 2L73 4F A3WE 19951106002991995110600299NM 1995 11 6 95FDEA01619 119951030A5330 SKIN BOEING727 72722 1384002NM BS 1240 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 OUTWARD DENTS IN SKIN BS 1240 BETWEEN STR 20-21L. REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951106003001995110600300NM 1995 11 6 95FDEA01620 119951030A5315652082725 FLOORBEAM BOEING727 72722 1384002NM BS 540 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FLOORBEAM LOWER CHORD BS 540 WL 200 LBL 22 TO RBL 22 WILL REQUIRE REMOVAL OF DOOR LATCH WEB. MECHANICAL REMOVED CORROSION FROM LOWER CHORD OF FLOORBEAM BS 540 RBL 22 TO LBL 22 WL 200, MATERIAL LOSS IS BEYOND LIMITS IAW FEDEX SRM 53-10-1 AT RBL 9 TO 19.5. CUT OUT EFFECTED AREAS 1 INCH BY 2 INCH AND REPAIRED IAW FEDEX SRM 53-10-8 FIG 8. 2L73 4F A3WE 19951106003011995110600301NM 1995 11 6 95FDEA01621 119951030A5311 FRAME BOEING727 72722 1384002NM BS 420 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 GOUGE ON FRAME AT BS 420 BETWEEN STR 14-15L. BLENDED GOUGE AND REPAIRED FRAME AT BS 420 BETWEEN STR 14-15L PER FEDEX SRM 53-10-4 FIG 11. ALODINED AND PRIMED AFFECTED AREA AND PARTS. 2L73 4F A3WE 19951106003021995110600302NM 1995 11 6 95FDEA01622 119951030A5330 SKIN BOEING727 72722 1384002NM BS 821-826 LIGHTNING STRIKEA FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 THREE EACH LIGHTNING STRIKES AT BS 821 - 826, LBL 68, WL 270. REPAIRED 3 EACH LIGHTNING AT BS 821 - 826, LBL 68, WL 270 PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951106003031995110600303NM 1995 11 6 95FDEA01623 119951103A5711 SPAR BOEING727 72722 1384002NM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-132-02-1) WING CENTER SECTION FRONT SPAR LOWER SPAR, BS 740, RBL 35. 2L73 4F A3WE 19951106003041995110600304NM 1995 11 6 95FDEA01624 119951030A5330 SKIN BOEING727 72722 1384002NM BS 1238 GOUGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 GOUGE IN SKIN BS 1238 BETWEEN STR 17 - 19R. REPAIRED GOUGE PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951106003051995110600305NM 1995 11 6 95FDEA01626 119951030A5315 FLOOR BEAM BOEING727 727225 1384077NM BS 920 DAMAGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 WHILE ACCESSING FOR EO 7-5300-7-2304M PART 3, DISCOVERED TOOLING DAMAGE ON TOP OF THE BS 920 FLOOR BEAM FROM LBL 15.5 TO LBL 19, WL 208. REPAIRED TOOLING DAMAGE PER FEDEX 7-5310-7-22611 AND EWO 95-3210. 2L73 4F A3WE 19951106003061995110600306NM 1995 11 6 95FDEA01627 119951030A5320694368310 SHEAR TIE BOEING727 727225 1384077NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION (C53-113-01-1) ON FRAME AND SHEAR TIE AT BS 680 LBL 17 - 20, WL 150. CORROSION REMOVAL ON FRAME FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1, CORROSION ON SHEAR TIE FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1, TREATED, ALODINED, PRIMED CORRODED AREA ON FRAME AND INSTALLED NEW SHEAR TIE BS 680, LBL 17 - 20, WL 150. 2L73 4F A3WE 19951106003071995110600307NM 1995 11 6 95FDEA01628 119951028A5720 ANGLE BOEING727 727227 1384078NM BS 760 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 FOUND MECHANICAL DAMAGE IN FWD UPPER HOLE IN ANGLE AT RBL 70.5, WL 210, BS 760. REPAIRED DAMAGED HOLE PER FEDEX EO 7-5710-25977. 2L73 4F A3WE 19951106003081995110600308NM 1995 11 6 95FDEA01629 119951028A5330 SKIN BOEING727 727227 1384078NM BS 360 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 DENT IN SKIN, BS 360, STR 17L. CUT OUT SKIN AND INSTALLED EXTERNAL DOUBLER PER FEDEX EA 7-5330-25929. 2L73 4F A3WE 19951106003091995110600309NM 1995 11 6 95FDEA01630 119951028A5320 T CHORD BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25484FE 21466 ON BL 70.5 RT RIB UPPER CHORD, NOTED CORROSION AND/OR CRACK IN FWD UPPER HOLE AND NOTED DAMAGE AND/OR CRACK IN AFT UPPER HOLE. ALL NOTED INDICATIONS MARKED ON A/C. (CORROSION IN ENTIRE HOLE, DAMAGE IN T-CHORD) BS 760. 2L73 4F A3WE 19951106003101995110600310NM 1995 11 6 95FDEA01631 119951023A5330 SKIN BOEING727 72725C 138400HNM BS 441 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 LFEC INSPECTION INDICATES CORROSION EXCEEDING 10 PERCENT AT BS 441 BETWEEN STR 23-24R FWD LAP. REMOVED CORROSION AND INSTALLED 6.50 INCH BY 14 INCH DOUBLER PER SRM 53-30-4. 2L73 4F A3WE 19951106003111995110600311NM 1995 11 6 95FDEA01632 119951018A5313 STRINGER BOEING727 72725C 138400HNM BS 970 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 14851 STR 41 GOUGED UNDER STR CLIP STA 970. INSTALLED STR SPLICE AND FILLER PER SRM 53-10-3, FIG 3, PG 5-8. 2L73 4F A3WE 19951106003121995110600312NM 1995 11 6 95FDEA01633 119951020A5313 STRINGER BOEING727 72725C 138400HNM BS 500 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 MAIN CARGO STR 16R CRACK AT FRAME STA 500. REMOVED INTERCOSTAL, CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED REPAIR PER SRM 53-10-3. 2L73 4F A3WE 19951106003131995110600313NM 1995 11 6 95FDEA01634 119951023A5711 SPAR WEB BOEING727 72725C 138400HNM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 WING CENTER SECTION, RT SPAR LOWER PORTION OF WEB, SHOWS EVIDENCE OF BULGING AND CORROSION AT LBL 20, BS 870, WEB AND LOWER SPAR CHORD. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS, TRIPLERS AND REPAIR ANGLES PER ESO 11782 AND EA 7-5710-25952 AND 51-10-1. 2L73 4F A3WE 19951106003141995110600314NM 1995 11 6 95FDEA01635 119951020A5330 SKIN BOEING727 72725C 138400HNM FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 SKIN CRACKED JUST BELOW STR 6 AT FWD ENTRY CUT-OUT (MARKED). INSTALLED FWD ENTRY DOUBLER PER SB 727-53-18621 AND AGING AIRCRAFT AD 94-05-04. 2L73 4F A3WE 19951106003151995110600315NM 1995 11 6 95FDEA01636 119951030A5320 DOOR FRAME BOEING727 72725C 138400HNM BS 572 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 FORWARD CARGO AFT CARGO DOOR FRAME STA 572 CRACKED FROM AROUND RIVET ON FRAME AFT DOOR STOP AREA. REMOVED RIVET AND STOP DRILLED. INSTALLED DOUBLER PER 51-10-4, PG 41. 2L73 4F A3WE 19951106003161995110600316NM 1995 11 6 95FDEA01637 119951030A5315 FLOOR BEAM BOEING727 72725C 138400HNM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 MAIN CARGO - CORROSION ON BOTTOM OF UPPER FLANGE OF FLOOR BEAM AT STA 640 BETWEEN NR 5 AND NR 6 SEAT TRACK. REMOVED CORROSION PER SRM 51-10-06. REPAIRED FLOOR BEAM PER ESO 11782 AND FEDEX EA 7-5310-25944. 2L73 4F A3WE 19951106003171995110600317NM 1995 11 6 95FDEA01638 119951029A5711 SPAR CHORD BOEING727 72725C 138400HNM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 BS 740, LBL 40 - 46: WING CENTER SECTION FRONT SPAR LOWER CHORD TO LOWER TANK SKIN HAS HEAVY CORROSION. RIVET HEADS SHEARED AND SKIN BULGING. REPAIR PER EA NR 7-5710-26102 DATED 10-24-95. 2L73 4F A3WE 19951106003181995110600318NM 1995 11 6 95FDEA01639 119951030A5320 RIB CHORD BOEING727 72725 1384006NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25152FE 18285 NOTED CRACK INDICATION IN FORWARD UPPER AND LOWER FASTENER HOLES AT BS 760, LBL 70.5 RIB UPPER CHORD, CRACKED IN 6 AND 12 O'CLOCK POSITIONS IN CHORD, BOTH HOLES. REPAIRED DAMAGED AREA AT BS 760, LBL 70.5, RIB UPPER CHORD IAW SB 727-57-0112, FEDEX EO 7-5710-7-2308H PART 2 AND FEDEX EA 7-5710-26120. 2L73 4F A3WE 19951106003191995110600319NM 1995 11 6 95FDEA01640 119951020A5313 STRINGER BOEING727 72725C 138400HNM BS 460 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 STR 8L IS CRACKED AT LOWER FLANGE ATTACH POINT TO FRAME AT STA 460 IN UPPER LOBE. REMOVED DAMAGED SECTION OF STR 8L STR 460 IN UPPER LOBE. REPAIRED PER SRM 53-10-3 PG 5 - 8. 2L73 4F A3WE 19951106003201995110600320NM 1995 11 6 95FDEA01641 119951024A5720 BOLTS BOEING727 727227 1384078NM RT RIB MISINSTALLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25479FE 21461 THREE EACH BOLTS WERE INSTALLED THROUGH HORIZONTAL FRAME BL 70.5, RT RIB CHORD REPAIR FOR EO 7-5710-7-2308 PART 3, BUT NOT PER EO (EO CALLS FOR 3 EACH HI-LOKS INSTEAD). ACQUIRED ESO 11782 DATED 10/24/95 TO ALLOW STO/S BOLTS TO BE INSTALLED, AWAITING EA NR. 2L73 4F A3WE 19951106003211995110600321NM 1995 11 6 95FDEA01642 119951031A5320 STRAP BOEING727 727227 1384078NM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT LOWER CARGO FLOOR BEAM STABILIZER STRAP CORRODED BEYOND SKIN LIMITS STA 1070, RBL 24. DOUBLER INSTALLED PER SRM 51-40-3. 2L73 4F A3WE 19951106003221995110600322NM 1995 11 6 95FDEA01643 119951031A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 AFT LOWER CARGO FLOOR BEAM LOWER FWD FLANGE CORRODED BEYOND SRM LIMITS STA 1070, RBL 12. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-6. 2L73 4F A3WE 19951106003231995110600323NM 1995 11 6 95FDEA01644 119951031A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 380 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FLOOR BEAM AT STA 380, RBL 47, WL 208.1, HAS CORROSION. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS .086 INCH. SHOULD BE .100 INCH. 2L73 4F A3WE 19951106003241995110600324WP 1995 11 6 95UAL900241 119951101A5330 SKIN DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP291859U 47819 SHEET METAL CRACKED AROUND RIVET, LEFT SIDE OF FUSELAGE, FORWARD OF OUTFLOW VALVE ALONG CIRCULAR FRAME LINE. THE SKIN CRACKING WAS ACTUALLY SKIN CORROSION DAMAGE COMMON TO FRAME LOCATIONS AND WAS REPAIRED PER SRM 53-20-00 FIGURE 6 SHEET 13 CLASS III REPAIR. EVA ORD-4022 WAS ISSUED TO COMBINE THESE REPAIRS WITH AN EXISTING SKIN REPAIR AND AUTHORIZE BLIND HUCK FASTENERS. 2L73 4F4 F A22WE E23EA 19951106003251995110600325WP 1995 11 6 ABXA9500929 119951031A3260H1410051 DNLOCK SWITCH DOUG DC9 DC933F 302207AWP RT MLG INTERMITTENT A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23935AX 47413 RIGHT MAIN GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED MAIN GEAR DOWNLOCK SWITCH IAW DC-9 SUPP. M.M. OPS CHECKED GOOD. 2L72 4F A6WE 19951106003261995110600326WP 1995 11 6 ABXA9500930 119951031A7931377649 RELIEF VALVE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 4 ENGINE DEFECTIVE A ABXAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL23825AX 46141 671316 DURING DESCENT, LOW OIL PRESSURE WARNING LIGHT ILLUMINATED FOR THE NR 4 ENGINE WITH AN OIL PRESSURE INDICATION OF 33 PSI WITH ENGINE POWER AT IDLE. PERFORMED PRECAUTIONARY SHUT-DOWN OF THE NR 4 ENGINE. REPLACED MAIN OIL FILTER FOR THE NR 4 ENGINE IAW DC8 MM, CHAPTER 79. REPLACED OIL PRESSURE RELIEF VALVE FOR THE NR 4 ENGINE IAW PWA JT3D MM, CHAPTER 72. CHECKED OIL PRESSURE INDICATION IAW DC8 MM, CHAPTER 79 AND OPS CHECK WAS GOOD. 2L74 4F4 F 4A25 1E8 19951106003271995110600327 1995 11 6 COMA9511992 419951027A34256226190204 AHRS COMPUTER EMB 120 EMB120RT SO AVIONICS BAY FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01268CA108201 120262 NR 2 AHRS FAILED DURING FLIGHT. REPLACED THE NR 2 AHRS COMPUTER. 2L72 4T RTA31SO 19951106003281995110600328SO 1995 11 6 COMA9511993 119951028A3241M610627023 RELAY EMB 120 EMB120RT SO ANTI SKID FAILED A COMAO OTHER J WARNING INDICATION UKUNKNOWN 1 SO01249CA 120230 WHEN THE LANDING GEAR WAS SELECTED UP, THE RIGHT INBOARD ANTI-SKID FAILED. REPLACED RELAY K0021. 2L72 4T RTA31SO 19951106003291995110600329SO 1995 11 6 COMA9511994 119951029A2820 CROSS FEED LIGHT EMB 120 EMB120RT SO FUEL SYST ILLUMINATED A COMAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01267CA 120259 BOTH FUEL CROSS-FEED LIGHTS ILLUMINATED WITH CROSS-FEED SWITCH IN THE OFF POSITION. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE, AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA31SO 19951106003301995110600330SW 1995 11 6 COMA9520396 119951027A2432235761 BATTERY SWRNGNSA227 SA227AC 8780603SW LEFT OVERHEATED A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO0127119103231 AC701 LEFT BATTERY OVERHEAT WARNING, BATTERY TEMPERATURE INDICATES ABOVE 180. REPLACED THE LEFT BATTERY. 1L72 4T A8SW 19951106003311995110600331EU 1995 11 6 COMA9531179 119951030A3150004WS00 WEU SAAB SF340 SF340A 7850100EU AVIONICS BAY DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01146CA16994335 340A146 THE RIGHT WINDSHIELD HEAT DOES NOT WORK. REPLACED THE WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19951106003321995110600332EU 1995 11 6 COMA9531180 119951029A27518565M1 POS TRANSMITTER SAAB SF340 SF340A 7850100EU FLAPS DEFECTIVE A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01320CA1699515451 340A064 UNCOMMANDED MOVEMENT OF FLAPS DURING FLIGHT. REPLACED THE LT AND RT FLAP POSITION TRANSMITTER. 2L72 4T RTA52EU 19951106003331995110600333EU 1995 11 6 COMA9531181 119951028A243523080031 STARTER GEN SAAB SF340 SF340A 7850100EU LT ENGINE FAILED A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01340SF18002876 340A014 THE LEFT ENGINE WOULD NOT ROTATE DURING START CYCLE. REPLACED THE LEFT ENGINE STARTER/GENERATOR. 2L72 4T RTA52EU 19951106003341995110600334 1995 11 6 COMA9531182 419951028A34206226342012 EFD 86 SAAB SF340 SF340A 7850100EU COCKPIT FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01342CA2293425 340A023 THE PILOT'S LEFT EADI TOP TUBE IS INOPERATIVE. REPLACED THE PILOT'S EFD-86. 2L72 4T RTA52EU 19951106003351995110600335EA 1995 11 6 COMA9560589 119951024A2760270003 PCU CNDAIRCL600 CL6002B19 EA RT SPOILER DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01914CA 7012 THE RIGHT FLIGHT SPOILER DEPLOYS UNCOMMANDED. REPLACED THE RIGHT FLIGHT SPOILER POWER CONTROL UNIT. 2L72 4F RTA21EA 19951106003361995110600336EA 1995 11 6 COMA9560590 119951027A323017300221 HARNESS CNDAIRCL600 CL6002B19 EA NLG DEFECTIVE A COMAK NONE J WARNING INDICATION CLCLIMB 1 SO01938CA2845 7046 THE NOSE LANDING GEAR FAILED TO RETRACT. REPLACED THE NLG RIGHT WEIGHT-ON-WHEELS PROXIMITY SWITCH AND HARNESS ASSEMBLY. 2L72 4F RTA21EA 19951106003371995110600337NM 1995 11 6 SCNA95250 119951027A3350900835A BATTERY PACK BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 THE EMERGENCY EXIT LIGHT ABOVE THE L-2 DOOR TESTED DIMLY. REMOVED AND REPLACED BATTERY PACK FOR THE L-2 DOOR EMERGENCY EXIT LIGHT IAW MM 33-50-71 AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951106003381995110600338NM 1995 11 6 SCNA95251 119951029A335057761 BATTERY PACK BOEING727 727282 138408TNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE MID-CABIN FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED MID-CABIN FLOOR TRACK LIGHTING BATTERY PACK AND SYSTEM CHECKED NORMAL. 2L73 4F RTA3WE 19951106003391995110600339NM 1995 11 6 SCNA95252 119951031A335090052 EEL POWER SUPPLY BOEING727 7272J4 1384006NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 THE FORWARD OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED FORWARD OVERHEAD EMERGENCY EXIT LIGHT POWER SUPPLY AND LIGHT TESTED GOOD. 2L73 4F RTA3WE 19951106003401995110600340NM 1995 11 6 SCNA95253 119951025A2611PC1604 SMOKE DET BATT BOEING727 7272J4 1384006NM RIGHT AFT LAV DISCHARGED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15288SC 20765 THE RIGHT AFT LAV SMOKE DETECTOR WAS FOUND BEEPING CONSTANTLY. THE BATTERY VOLTAGE WAS FOUND LOW, REPLACED BATTERY AND DETECTOR TESTED GOOD. 2L73 4F RTA3WE 19951106003411995110600341NM 1995 11 6 SWAA950681 119951023A56105717623122 WINDOW BOEING737 7373H4 1384600NM RT COCKPIT CRACKED A SWAAA UNSCHED LANDING O OTHER CLCLIMB 1 SW07313SW 23335 DURING CLIMBOUT AT 31,000 FEET, NOTED FIRST OFFICER'S SLIDING WINDOW CRACKED. AIRCRAFT RETURNED TO BOI AND MADE AN UNEVENTFUL LANDING. INSPECTED WINDOW AND CONFIRMED TO BE OUTER PANE. REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M.M. 2L72 4F RTA16WE 19951106003421995110600342NE 1995 11 6 SWAA950682 219951023A7200 ENGINE BOEING737 7375H4 138449DNM GE CFM56 CFM563B1 13802NE NR 1 BIRD STRIKE A SWAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW07519SW 25318 856218 DURING CLIMBOUT, EXPERIENCED BIRDSTRIKE TO NR 1 ENGINE. AIRCRAFT RETURNED TO BWI AND MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED BIRDSTRIKE INSPECTION, CONFIRMED BIRD ENTRY INTO ENGINE CORE. ENGINE PLACED ON 10-CYCLE FLYBACK. HOU RON BORESCOPED, NO DEFECTS NOTED. 2L72 4F4 FRTA16WE E2GL 19951106003431995110600343NM 1995 11 6 SWAA950683 119951028A5320 BEAM BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21262 DURING SCHEDULED A2 CHECK, FOUND LEFT W/W TRANSVERSE I BEAM FLOOR SUPPORT CRACKED APPROX 2 INCHES FWD OF BS 727 BULKHEAD AT CEILING FWD OF BULKHEAD. REPAIRED PER SWA RA 1-253-1398. 2L72 4F A16WE 19951106003441995110600344NM 1995 11 6 SWAA950684 119951028A5313 STRINGER BOEING737 7372H4 138448CNM BS 450-470 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0727SW 21262 DURING SCHEDULED A2 CHECK, FOUND FWD CARGO DOOR FRAME STRINGER CRACKED IN RADIUS S26R, AT BS 450 AND 470. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951106003451995110600345NM 1995 11 6 SWAA950685 119951020A5330 SKIN BOEING737 7372H4 138448CNM BS 381/766 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN LAP CRACK INDICATIONS AT THE FOLLOWING LOCATIONS: BS 766, S10L, AT BS 776, S10L, AND AT BS 381, S14R, AT LOWER ROW OF FASTENERS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951106003461995110600346NM 1995 11 6 SWAA950686 119951020A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0759SW 21811 DURING SCHEDULED SERVICE CHECK, FOUND SEVERAL CRACK INDICATIONS UNDER BULKHEAD STRAP, RBL 5.5, WL 188 TO 202.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F A16WE 19951106003471995110600347NM 1995 11 6 SWAA950687 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 947.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 10.5 TO LBL 21.0. REPAIRED PER SWA RA 1-353-1391. 2L72 4F RTA16WE 19951106003481995110600348NM 1995 11 6 SWAA950688 119951023A5330 SKIN BOEING737 7373H4 1384600NM CARGO DR CUTOUT DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOOR FRAME CUT-OUT CHIPPED AND BENT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951106003491995110600349NM 1995 11 6 SWAA950689 119951023A5320 ANGLE BOEING737 7373H4 1384600NM BS 747 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FLOOR ANGLE CRACKED AT BS 747. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL. 2L72 4F RTA16WE 19951106003501995110600350NM 1995 11 6 SWAA950690 119951023A5313 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGERS CRACKED AT LEFT AND RIGHT ICE LIGHTS LOCATIONS. REPAIRED PER SWA ACO 6405-53. 2L72 4F RTA16WE 19951106003511995110600351NM 1995 11 6 SWAA950691 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, RBL 7 TO LBL 7. REPAIRED PER SWA RA 1-353-1392. 2L72 4F RTA16WE 19951106003521995110600352NM 1995 11 6 SWAA950692 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 947.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 947.5, RBL 5. REPAIRED PER SWA RA 1-353-1390. 2L72 4F RTA16WE 19951106003531995110600353NM 1995 11 6 SWAA950693 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 344, BBL 0. REPAIRED PER SWA RA 1-353-1393. 2L72 4F RTA16WE 19951106003541995110600354NM 1995 11 6 SWAA950694 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 31.5. REPAIRED PER SWA RA 1-353-1395. 2L72 4F RTA16WE 19951106003551995110600355NM 1995 11 6 SWAA950695 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 328, RBL 41. REPAIRED PER SWA RA 1-353-1394. 2L72 4F RTA16WE 19951106003561995110600356NM 1995 11 6 SWAA950696 119951023A5315 FLOOR BEAM BOEING737 7373H4 1384600NM BS 294.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07353SW 24889 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM SCREW HOLE CORROSION AT BS 294.5, RBL 37.5 TO RBL 41.5, LONG STRAP, AFT FLANGE. REPAIRED PER SWA RA 1-353-1396. 2L72 4F RTA16WE 19951106003571995110600357NM 1995 11 6 UPS204882 119951025A7797 WIRE BOEING727 72731C 1384011NM NR 2 ENGINE DAMAGED A IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01924UP 19234 SUPPLEMENTAL MRR: CREW REPORTED AT TOC AS THRUST WAS REDUCED, NR 2 ENG O/HEAT LIGHT ON OVERHEAD PANEL FLICKERED FOR 5 SECONDS AND WENT OUT. AT THE TOD DESCENT DURING THRUST REDUCTION, NR 2 ENG O/HEAT LIGHT CAME ON STEADY ILLUMINATING THE MASTER ENGINE O/HEAT LIGHT ON THE FWD PANEL. PER CHECK LIST, NR 2 ENGINE THROTTLE WAS CLOSED AND LIGHT WENT OUT. AFTER 3 MINUTES AT IDLE, ENG SHUT-DOWN CHECK LIST PERFORMED. EMERGENCY DECLARED. MAINTENANCE NOTIFIED. MAINTENANCE T/S SYS IAW MM 71-00-00 AND FOUND WIRE NR 9281-E9202-20 SHORTED TO GROUND ABOVE ENGINE MOUNT. REPAIRED WIRE INSULATION AND ISOLATED TO PREVENT FURTHER ABRASION. MX PERFORMED ENG O/HEAT SYS FUNCTIONAL TEST IAW AMM 75-41-00, NO DEFECTS NOTED. 2L73 4F A3WE 19951106003581995110600358NM 1995 11 6 UPS204919 119951030A3350 BATTERY BOEING727 727247 138408FNM COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01210UP 21697 WHILE ON THE GROUND, MAINTENANCE FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES ON THE COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-101. PERFORMED ADJ/TEST IAW MM 33-50-01 GRD, OPS CK'D GOOD. 2L73 4F A3WE 19951106003591995110600359NM 1995 11 6 UPS504926 119951030A3260 IND LIGHT BOEING757 75724APF 1384969NM LT MLG FAILED A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01425UP 25370 CREW REPORTED LEFT GEAR INDICATION INOP - 60 AROUND PERFORMED - MAINTENANCE CONTACTED. EQUIPMENT CALLED FOR - COORDINATED APPROACH END OBSERVER WHICH CONFIRMED GEAR APPEARED DOWN - LANDING MADE WITHOUT INCIDENT. MAINTENANCE RE-LAMPED LEFT MAIN GEAR DOWN LIGHTS. OPS NORMAL. PERFORMED PRESS-TO-TEST FOR WARNING LIGHTS, FOUND BOTH LAMPS BURNED OUT IN LEFT GEAR GREEN DOWN LIGHTS. 2L72 4F RTA2NM 19951106003601995110600360WP 1995 11 6 UPS804902 119951026A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 SUPPLEMENTAL MRR: WHILE ON THE GROUND, MAINTENANCE FOUND CORROSION ON REPAIR DOUBLER AT FUSELAGE STATION 1120. REMOVED PREVIOUS DOUBLER REPAIR, BEGAN TO REMOVE DAMAGE IN REFERENCE TO SRM 53-02-01, FIGURE 7. REMOVED REMAINDER OF VISIBLE CORROSION. DOUBLER INSTALLED PER EO DC8-5330-7556A. 2L74 4F RT4A25 19951106003611995110600361WP 1995 11 6 UPS804903 119951026A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 SUPPLEMENTAL MRR: WHILE ON THE GROUND, MAINTENANCE FOUND CORROSION ON THE SKIN AFT OF THE AIR CONDITIONING BAY DOOR. MAINTENANCE REMOVED THE AREA OF CORROSION AS PER SRM 53-2-1. REPAIR DOUBLER WITH BLIND FASTENERS AS PER SRM 53-2-1. 2L74 4F RT4A25 19951106003621995110600362WP 1995 11 6 UPS804904 119951026A2560 BATTERY WIRE DOUG DC8 DC871F 302199DWP ESCAPE SLIDE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01880UP 45900 SUPPLEMENTAL MRR: WHILE ON THE GROUND IN EAST MIDLANDS, MAINTENANCE FOUND THE EMERGENCY ESCAPE SLIDE BATTERY PACK WIRING BROKEN. MAINTENANCE REMOVED THE SLIDE AND DEFERRED EPR EO. MAINTENANCE ALSO SECURED SLIDE PACK AS REQUIRED. 2L74 4F RT4A25 19951106003631995110600363 1995 11 6 UPS804920 419951031A2565 SLIDE DOUG DC8 DC873F 302199FWP EMER ESCAPE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01803UP 46073 WHILE ON THE GROUND, MAINTENANCE FOUND THE EMERGENCY ESCAPE SLIDE PRESSURE INDICATION WITH OPEN COVER. REPOSITIONED INDICATOR, SLIDE INFLATED, NEEDS REPLACED. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE PER MM 25-60-01. 2L74 4F RT4A25 19951106003641995110600364WP 1995 11 6 WWMA9500075 219951027A732189778025 FCU BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP RT ENGINE DEFECTIVE A WWMAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 WP15958AE5201 958 PILOT REPORTED IN CRUISE, THE RIGHT ENGINE HAD AN INTERMITTENT TORQUE FLUX OF 10 PERCENT AT 60 PERCENT TORQUE WITH A YAW AND CHANGES IN FUEL FLOW. ALL OTHER INDICATIONS WERE NORMAL. WHILE DESCENDING INTO LAX, TORQUE WAS BROUGHT BACK TO 20 PERCENT. THE RIGHT ENGINE WENT UNCOMMANDED TO 40 PERCENT. ENGINE SHUT-DOWN WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INVESTIGATION, MAINTENANCE REPLACED THE RIGHT ENGINE FUEL CONTROL UNIT IAW GARRETT MM 73-10. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2L72 4T4 TRTA56EU E4WE 19951106003651995110600365EU 1995 11 6 WWMA9500076 119951028A2530 CONNECTOR SAAB SF340 340B 7860101EU NR 2 HOT JUG CONTAMINATED A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15338SB 340B338 THE FLIGHT ATTENDANT REPORTED SMELLING AN ELECTRICAL BURNING SMELL AT THE NR 2 HOT JUG. UPON INVESTIGATION, MAINTENANCE FOUND THE EXTERIOR OF THE WATER JUG SOAKED WITH WATER AND WATER IN THE ELECTRICAL CONNECTION. THE JUG AND THE ELECTRICAL CONNECTION WERE DRIED WITH NO FURTHER PROBLEMS NOTED. 2L72 4T RTA52EU 19951106003661995110600366EU 1995 11 6 WWMA9500077 119951101A261172111211002 SMOKE DETECTOR BAG JETSTMJETSTM3201 1500217EU REAR CARGO BAY DEFECTIVE A WWMAO OTHER N FALSE WARNING TXTAXI/GRND HDL 1 WP15952AE 952 DURING PRE-FLIGHT, CREW REPORTED THAT THE CARGO SMOKE LIGHT WAS ON. MAINTENANCE REPLACED THE BAGGAGE SMOKE DETECTOR, THE AIRCRAFT WAS RELEASED WITH NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19951106003671995110600367WP 1995 11 6 95ZZZM574 119950910A2450H738D8A WIRE DOUG DC9 DC982 3022082WP AFT FUSELAGE OUT OF POSITION A AAALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW07575AM 53152 OMA - FLT 1501 - EN ROUTE ORD-DEN - DURING CRUISE, RIGHT AC GENERATOR TRIPPED WITH CROSSTIE LOCKOUT AND MULTIPLE ELECTRICAL ANNUNCIATOR LIGHTS. VOLTAGE AND FREQUENCIES CHECKED GOOD. RESET AC GENERATOR AND TRIPPED AGAIN. STARTED APU AND PLACED APU GENERATOR ON-LINE AND APU GENERATOR TRIPPED. AIRCRAFT DIVERTED TO OMA AND LANDED WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRY OMA/TUL, CORRECTED WIRES H736D8B AND H738D8A FOUND CONNECTED TO INCORRECT TRANSFORMERS. ACCOMPLISHED GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. REFERENCE NR AALA951638. 2L72 4F A6WE 19951106003681995110600368NM 1995 11 6 95ZZZM575 119950929A2611302842 SMOKE DETECTOR BOEING727 727222 1384073NM NR 2 POSITION FAILED A RYNAO OTHER N FALSE WARNING CRCRUISE 1 CE077645U 20039 DURING CRUISE THE MAIN CABIN SMOKE DETECTOR LIGHT ILLUMINATED. COMPLIED WITH EMERGENCY CHECK LIST. LANDED WITHOUT INCIDENT. LIGHT EXTINGUISHED ON TAXI IN. INSPECTED AND TESTED SMOKE DETECTOR SYSTEM. REPLACED THE NR 2 DETECTOR DUE TO INTERMITTENT TEST. SYSTEM OPS CHECK NORMAL. (M) 2L73 4F A3WE 19951106003691995110600369WP 1995 11 6 AALA951554 119950828A3350A3060698101 CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07167AA 46930 MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT SEAT 38H. SECURED WIRE PIN AT SEAT LIGHT CONNECTOR. GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19951106003701995110600370EU 1995 11 6 AALA951555 119950827A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0714056 463 JFK - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT SEATS 12B TO 15B. REPLACED CROSSOVER WIRE AT SEAT 15B. GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951106003711995110600371WP 1995 11 6 AALA951638 119950910A2450H736D8B WIRE DOUG DC9 DC982 3022082WP AFT FUSELAGE OUT OF POSITION A AAALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 SW07575AM 53152 OMA - FLT 1501 - EN ROUTE ORD-DEN - DURING CRUISE, RIGHT AC GENERATOR TRIPPED WITH CROSSTIE LOCKOUT AND MULTIPLE ELECTRICAL ANNUNCIATOR LIGHTS. VOLTAGE AND FREQUENCIES CHECKED GOOD. RESET AC GENERATOR AND TRIPPED AGAIN. STARTED APU AND PLACED APU GENERATOR ON-LINE AND APU GENERATOR TRIPPED. AIRCRAFT DIVERTED TO OMA AND LANDED WITHOUT INCIDENT. AIRCRAFT MAINTENANCE FERRY OMA/TUL, CORRECTED WIRES H736D8B AND H738D8A FOUND CONNECTED TO INCORRECT TRANSFORMERS. ACCOMPLISHED GROUND CHECKS WITH NO DEFECTS FOUND. SYSTEMS GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951106003721995110600372NM 1995 11 6 AALA951646 119950912A33501703643 EEL CONTACT PIN BOEING767 767323 1385205NM CABIN OUT OF POSITION A AALAK NONE L NO TEST ININSP/MAINT 1 SW07385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 25B INOPERATIVE. REPOSITIONED CONTACT PIN FOR PASSENGER SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951106003731995110600373EU 1995 11 6 AALA951647 119950912A3350 EEL WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770073 516 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROWS 24-25AB, 34AB AND AT L2 AND R2 DOORS INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRES BY PASSENGER SEAT ROW 24AB, 34AB AND AT L2 AND R2 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951106003741995110600374EU 1995 11 6 AALA951648 119950914A3350A3030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW077083A 645 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 10 AND 15 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951106003751995110600375NM 1995 11 6 AALA951649 119950914A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07613AA 24489 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 10 AND 16 INOPERATIAVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951106003761995110600376EU 1995 11 6 AALA951657 119950917A3350A3030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077082A 643 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE BY AFT LAVATORY INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE BY AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951106003771995110600377NM 1995 11 6 AALA951679 119950918A3350A3060720101 EEL CONDUCTOR DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071755 48490 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT RIGHT AISLE BUSINESS CLASS CABIN FORWARD OF CLOSET INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE AT RIGHT AISLE BUSINESS CLASS CABIN FORWARD OF CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19951106003781995110600378WP 1995 11 6 ARWA021751 119950217A5320 INTERCOSTAL DOUG DC8 DC862F 3021972WP FS 1600 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND MAIN CARGO COMPARTMENT AFT BULKHEAD FS 1600 AT L28L HAD CRACKED INTERCOSTAL. REMOVED CRACKED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-1-8, 51-1-20 AND 53-1-0. ARROW AIR WORK ORDER NR 950007-5110 (0249). (M) 2L74 4F 4A25 19951106003791995110600379WP 1995 11 6 ARWA022051 119950220A5320 SUPPORT DOUG DC8 DC862F 3021972WP FS 600 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND FLOOR SUPPORT CRACKED AT FS 600 BETWEEN L35L AND L36L. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-20-0. ARROW AIR WORK ORDER NR 950007-5164 (0411). (M) 2L74 4F 4A25 19951106003801995110600380WP 1995 11 6 ARWA022851 119950228A53202704089501 FITTING DOUG DC8 DC862F 3021972WP DOOR FRAME BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND 'B' BELLY LOWER DOOR FRAME SECOND FROM ATT 'T' BOLT BRACKET BROKEN IN HALF. REMOVED FITTINGS, FOUND AREA CORRODED REMOVED CORROSION AND TREATED AND PRIMED IAW SRM 51-1-8. REINSTALLED FITTING IAW SRM 51-3-0. RESEALED AREA WITH PRC 1422 B1/2 IAW SRM 51-1-16. (M) 2L74 4F 4A25 19951106003811995110600381WP 1995 11 6 ARWA022852 119950228A5320 WEB DOUG DC8 DC862F 3021972WP FS 35 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND FORWARD FUSELAGE STRUCTURE JUST BELOW RADOME SUPPORT RODS, CRACKED LEFT AND RIGHT SIDE. ROUTED OUT CRACKED MATERIAL BLENDED, TREATED AND PRIMED IAW SRM 51-1-8 AND 53-2-0. (M) 2L74 4F 4A25 19951106003821995110600382WP 1995 11 6 ARWA022854 119950228A5320 INTERCOSTAL DOUG DC8 DC862F 3021972WP FS 220 CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND FORWARD ACCESS COMP VERT STIFFENER AT L-28L AND FS 208.00 HAS LEVEL 2 CORROSION. CUT OFF CORROSION SECTION OF STIFFENER, FABRICATED NEW SECTION OF STIFFENER FROM .071 7075-T6 AS PER SRM 53-1-0 AND SRM 52-2-0. (M) 2L74 4F 4A25 19951106003831995110600383WP 1995 11 6 ARWA031351 119950313A5730 L/E SKIN DOUG DC8 DC862F 3021972WP RT WING CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND RIGHT WING LEADING EDGE BETWEEN NR 3 AND NR 4 ENGINES AT APPROXIMATE MID SECTION LOWER RIB SUPPORT PLATE WITH 2 CRACKS EMINATING FROM FASTENER HOLES. REMOVED AND FABRICATED REPLACEMENT PANEL PREPPED AND INSTALLED IAW SRM 57-2-1 PG 155/156 AND 51-1-8. (M) 2L74 4F 4A25 19951106003841995110600384WP 1995 11 6 ARWA031352 119950313A5320 SUPPORT DOUG DC8 DC862F 3021972WP FS 1120 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1120 L35-32L FRAME ATTACH FLOOR SUPPORT CRACKED AT TWO PLACES. REMOVED FLOOR SUPPORT, WELDED CRACKS PER DPS 102.25 AND REINSTALLED FLOOR SUPPORT IAW SRM 51-1-20D AND 51-1-21. ARROW AIR WORK ORDER NR 950007-5162 (0409). (M) 2L74 4F 4A25 19951106003851995110600385WP 1995 11 6 ARWA031355 119950313A5230 ANGLE DOUG DC8 DC862F 3021972WP MAIN CARGO DOOR CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND MAIN CARGO DOOR LATCH SUPPORT ANGLE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE IAW SRM 51-1-21, 51-3-0 AND 53-2-0. (M) 2L74 4F 4A25 19951106003861995110600386WP 1995 11 6 ARWA031356 119950313A5400 BRACKET DOUG DC8 DC862F 3021972WP NR 1 PYLON CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND NR 1 PYLON LEFT SIDE CENTER COWL SUPPORT FITTING SUPPORT BRACKETS ARE CRACKED. REMOVED AND REPLACED SUPPORT BRACKETS AS PER SRM 54-2-1. (M) 2L74 4F 4A25 19951106003871995110600387WP 1995 11 6 ARWA031357 119950313A5532 PANEL DOUG DC8 DC862F 3021972WP VERT STAB CORROSION A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND VERTICAL STABILIZER TOP LEADING EDGE LEFT SIDE LEVEL 2 CORROSION. REMOVED CORROSION, FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW SRM 55-2-1 FIG 4. (M) 2L74 4F 4A25 19951106003881995110600388WP 1995 11 6 ARWA031551 119950315A5753 SKIN DOUG DC8 DC862F 3021972WP RT TE FLAP CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP INBOARD LEADING END HAS (CORNER) PANEL CHAFFING AND CRACKED. REMOVED PANEL AND FABRICATED REPLACEMENT IAW SRM 53-1-0. INSTALLED PANEL SRM 53-1-0 AND 51-1-20. (M) 2L74 4F 4A25 19951106003891995110600389WP 1995 11 6 ARWA061752 119950617A5312 BLKHD BEAM DOUG DC8 DC862F 3021972WP FS 1606 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD AFT SIDE THIRD HORIZONTAL BEAM FROM BOTTOM CRACKED AT BL ZERO. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D AND 53-20-0. ARROW AIR WORK ORDER NR 950007-6006 (0106). (M) 2L74 4F 4A25 19951106003901995110600390WP 1995 11 6 ARWA061753 119950617A5311 CIRCUMFERENTIAL DOUG DC8 DC862F 3021972WP FS 410 CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DUIRNG C-CHECK, FOUND MAIN CABIN CIRCUMFERENTIAL CRACKED AT FS 410 BETWEEN L7R AND L8R. CUT OUT DAMAGED AREA, AND FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-2-0. ARROW AIR WORK ORDER NR 950007-5146 (0378). (M) 2L74 4F 4A25 19951106003911995110600391WP 1995 11 6 ARWA061754 119950617A5321 FLOOR WEB DOUG DC8 DC862F 3021972WP CARGO COMPT CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND 'A' PIT FLOOR WEB CRACKED. STOP DRILLED SMALL CRACK IAW WITH SRM 53-2-0. ARROW AIR WORKORDER NR 950007-5153 (0396). (M) 2L74 4F 4A25 19951106003921995110600392WP 1995 11 6 ARWA090651 119950906A5330 SKIN DOUG DC8 DC862F 3021972WP WS 315 LE CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK, FOUND R/W UPPER SURFACE LEADING EDGE CRACKED AT XFS 315. CUT OUT DAMAGED AREA FABRICATED 7075-T6 .063 FILLER AND 7075T6-071 DOUBLER AND INSTALLED IAW SRM 57-2-1. (M) 2L74 4F 4A25 19951106003931995110600393WP 1995 11 6 ARWA0927954 119950212A54005753010IN STRESS PLANK DOUG DC8 DC862F 3021972WP NR 4 PYLON DAMAGED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING INCIDENT, INSPECTION FOUND NR 4 PYLON INBAORD STRESS PANEL (STATIONARY PLANK) BENT. REMOVED AND REPLACED NR 4 PYLON INBOARD STATIONARY STRESS PLANK PER DAC DRAWINGS NR 5753010 AND 5753000. (M) 2L74 4F 4A25 19951106003941995110600394WP 1995 11 6 ARWA0927955 119950315A27204701024 CRANK DOUG DC8 DC862F 3021972WP RUDDER CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND RUDDER TAB CONTROL CRANK WITH LEVEL 2 CORROSION. CORROSION REMOVED. REPLACED RUDDER CONTROL CRANK IAW MM 27-21-2. RIGGED TAB PER MM 27-13-3. OPS CHECK NORMAL. (M) 2L74 4F 4A25 19951106003951995110600395WP 1995 11 6 AWRA0927953 119950315A3210 SIDE BRACE DOUG DC8 DC862F 3021972WP LT MLG CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19791AL 46150 DURING C-CHECK INSPECTION, FOUND LEFT MLG SIDE BRACE LUGS ON STRUT WITH INTERNAL PITTING. CLEANED LUGS, FABRICATED BUSHINGS IAW OHM 32-1-1B. INSTALLED SIDE BRACE BUSINGS IAW OHM 13-1-6. REINSTALLED SIDE BRACE ASSEMBLY IAW MM 32-11-5. (M) 2L74 4F 4A25 19951106003961995110600396NM 1995 11 6 CAL950837 119950902A5414 SKIN BOEING737 7373T0 1384582NM NR 1 STRUT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091732829566 23458 HOU - INSPECTION FOUND A .25 INCH CRACK IN NACELLE STRUT SKIN OF NR 1 ENGINE AT PANEL 5754 CUTOUT AND PANEL 5725 CUTOUT. A DOUBLER WAS INSTALLED IAW ECRA 5430-01024. (M) 2L72 4F RTA16WE 19951106003971995110600397NM 1995 11 6 CAL950840 119950919A5241 SKIN BOEING737 737130 1384435NM FWD GALLEY DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620365350 19020 GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FORWARD GALLEY DOOR UPPER HINGE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02315. (M) 2L72 4F A16WE 19951106003981995110600398WP 1995 11 6 CAL950848 119950920A2740 O-RING DOUG DC10 DC1010 3022110WP STAB CONTL VLV BLOWN A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0968044 46903 FLT NR 0961 - GUM - THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED AND THE HYDRAULIC QUANTITY DROPPED TO 5.9 GALLONS IN FLIGHT. THE RIGHT HYDRAULIC PUMP WAS TURNED OFF AND THE FLUID LOSS STOPPED AT 4.9 GALLONS. THE AIRCRAFT WAS RETURNED TO GUM AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE PRESSURE SIDE O-RING AT UPPER STABILIZER CONTROL VALVE BLOWN. THE SEAL AND BACKUP RING WERE REPLACED IAW MM 27-40. THE HYDRAULIC SYSTEM WAS SERVICED, LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L73 4F A22WE 19951106003991995110600399NE 1995 11 6 CAL950853 219950923A7200 ENGINE BOEING747 747230B 1384889NM PWA JT9 JT9D7A 52054NE NR 4 ENG FAILED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW097801939075 20527 662382 FLT NR 0006 - HNL - THE NR 4 ENGINE FAILED AT TOP OF CLIMB WITH EGT AT 968 DEGREES. THE CREW SHUT THE ENGINE DOWN AND RETURNED TO HNL WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL IN THE NR 4 ENGINE TAILPIPE. THE NR 4 ENGINE WAS REMOVED AND REPLACED. (M) 2L74 4F4 F A20WE E20EA 19951106004001995110600400NM 1995 11 6 CAL950854 119950923A5753 TOGGLES BOEING737 7373T0 1384582NM RT TE FOREFLAP WORN A CALAK NONE O OTHER ININSP/MAINT 1 SW0970330 23460 CLE - INSPECTION FOUND THE RIGHT INBOARD FOREFLAP GOUGED CAUSED BY THE FOREFLAP TOGGLE WHICH HAD WORN BEARINGS AND BUSHINGS. THE RIGHT INBOARD TRAILING EDGE FOREFLAP AND TOGGLE WERE REMOVED AND REPLACED IAW MM 27-51-07. (M) 2L72 4F RTA16WE 19951106004011995110600401NM 1995 11 6 CAL950855 119950924A2782651781823 ACTUATOR BOEING727 727232 1384082NM NR 6 TE SLAT LEAKING A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW092778317967 20638 FLT NR 0209 - CUN - THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE FROM IAH TO SAL. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO CUN. WHILE ON APPROACH TO CUN, THE NR 6 SLAT WOULD NOT COME DOWN AND LOCK USING THE ALTERNATE FLAP SYSTEM. THE SLAT WAS VISUALLY CONFIRMED TO BE IN THE 'UP' POSITION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NR 6 LE SLAT ACTUATOR WAS FOUND LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L73 4F A3WE 19951106004021995110600402WP 1995 11 6 CAL950856 119950919A5330 SKIN DOUG DC9 DC932 3022066WP BS 996 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW095854566871 47094 IAH - INSPECTION FOUND A .1250 INCH CRACK IN SKIN AT STATION 996 BETWEEN LONGERONS 9 AND 10R. A REPAIR WAS FABRICATED AND INSTALLED IN REFERENCE TO DAC DRAWING J060138 AND EA 5361-01001. (M) 2L72 4F A6WE 19951106004031995110600403NM 1995 11 6 CAL950857 119950911A5330 SKIN BOEING737 737130 1384435NM BS 400 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW092421364506 19030 IAH - INSPECTION FOUND A POPPED FASTENER WITH CORROSION IN SKIN AT LAP JOINT FORWARD OF C-1 DOOR THRESHOLD STATION 400. THE CORRODED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 16. (M) 2L72 4F A16WE 19951106004041995110600404NM 1995 11 6 CAL950858 119950814A5754 SKIN BOEING737 7373T0 1384582NM NR 6 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432528791 23455 HOU - INSPECTION FOUND A .25 INCH CRACK IN LOWER SKIN OF NR 6 SLAT AT SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159 AND BOEING DRAWING 65C30133. (M) 2L72 4F RTA16WE 19951106004051995110600405NM 1995 11 6 CAL950859 119950814A5754 SKIN BOEING737 7373T0 1384582NM NR 5 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091432528791 23455 HOU - INSPECTION FOUND A .25 INCH CRACK IN LOWER SKIN OF NR 5 SLAT AT SLAT ACTUATOR. THE SKIN WAS REPAIRED IAW ECRA 5750-01159 AND BOEING DRAWING 65C30133. (M) 2L72 4F RTA16WE 19951106004061995110600406WP 1995 11 6 CAL950863 119950922A5210 SKIN DOUG DC9 DC932 3022066WP CABIN DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092752266349 47524 IAH - INSPECTION FOUND A .75 INCH CRACK IN FORWARD CABIN DOOR SKIN AT HOLD OPEN HOOK CUTOUT. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5210-01235. (M) 2L72 4F A6WE 19951106004071995110600407NE 1995 11 6 EIAA9543 219950920A7250 ENGINE BOEING747 747273C 1384896NM PWA JT9 JT9D7F 52054NE NR 3 ENG LPT DAMAGED A EIAAE ENGINE SHUTDOWN C F.O.D. ININSP/MAINT 1 NM09471EV443679367 20651 685017 KHV - NR 3 ENGINE HAS EXCESSIVE NOISE AND VIBRATION AFTER ENGINE START. ON VISUAL INSPECTION FOUND FOD DAMAGE TO LP ROTOR AND STATOR VANES. FERRIED AIRCRAFT TO HKG. REMOVED AND REPLACED NR 3 ENGINE. (M) 2L74 4F4 F A20WE E20EA 19951106004081995110600408WP 1995 11 6 EIAA9544 119950916A3297 WIRE DOUG DC9 DC933F 302207AWP NLG BROKEN A EIAAO OTHER P NO WARNING INDICATION APAPPROACH 1 NM09933F 47191 DEN - ON DESCENT THROTTLES IDLE, NOSE GEAR UNSAFE LIGHT NOT ILLUMINATED. GEAR DOWN, 'NOSE LANDING GEAR' GREEN LIGHT NOT ILLUMINATED. GEAR HORN FUNCTIONS NORMALLY. VISUALLY CHECKED GEAR DOWN AND LOCKED. FOUND BROKEN WIRE AFT OF NOSE GEAR, WIRE G-2116-B24. REPAIRED WIRE GROUND CHECKED OK PER DC9 MM 32-60-00. (M) 2L72 4F A6WE 19951106004091995110600409WP 1995 11 6 HALA95128 119950929A3350 EEL BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - FLT NR 102 - FORWARD CABIN FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED FORWARD CABIN FLOOR EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106004101995110600410WP 1995 11 6 HALA95129 119951001A2780 EYEBOLT DOUG DC9 DC951 3022051WP RT LE SLAT ACT BROKEN A HALAO OTHER J WARNING INDICATION APAPPROACH 1 WP13420EA 47689 FLT NR 561 - ON INITIAL SLAT EXTENSION IN FLIGHT AIRCRAFT ROLLED TO THE LEFT. NO SLAT EXTENDED LIGHT ON. RETRACTED SLATS AND AIRCRAFT RETURNED TO NORMAL TRIM. ALL SUBSEQUENT SLAT EXTENSIONS CAUSED THE AIRCRAFT TO ROLL LEFT, THEN SLAT EXTEND LIGHT COMES ON. CONDITION SAME WITH EITHER SLATS ONLY OR SLATS AND FLAPS EXTENDED. FOUND SLAT ACTUATOR EYEBOLT BROKEN ON RIGHT SIDE. REPLACED EYEBOLT IAW MM27-80-5. GROUND CHECK GOOD. (M) 2L72 4F A6WE 19951106004111995110600411 1995 11 6 HALA95130 419951002A2220 CONTROL CABLE DOUG DC9 DC951 3022051WP MACH TRIM BROKEN A HALAO OTHER O OTHER CRCRUISE 1 WP132FOR 47742 FLT NR 530 - HNL - MACH TRIM INDICATOR WENT FULL FORWARD ON ITS OWN FOLLOWED BY A BANG. REPLACED CABLE RUN NR 129E. RIGGED CABLE PER MM 27-40-0. ADJUSTEMENT AND TEST GOOD, CLOSE UP COMPLETE PER MM 27-40-0. (M) 2L72 4F RTA6WE 19951106004121995110600412WP 1995 11 6 HALA95131 119951002A3350P4010049 EEL BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 4360 47764 FLT NR 1133 - HNL - FORWARD HALF OF EMERGENCY FLOOR LIGHTS DO NOT WORK. REPLACED EMERGENCY FLOOR LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106004131995110600413WP 1995 11 6 HALA95132 119951002A5400 ANGLE DOUG DC9 DC951 3022051WP RT PYLON CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13672MC 47661 HNL - IN C-CHECK, RIGHT PYLON TO FUSELAGE TOP ATTACH ANGLE HAS A CRACK APPROX 1.5 INCHES LONG BELOW AFT PRESSURE BULKHEAD TEE CAP. REPLACED PYLON ANGLE. REPLACED FASTENERS IN VERTICAL LEG THROUGH FUSELAGE PER SRM 54-04. INSTALLED HORIZONTAL LEG FASTENERS PER SRM 54-04 PAINTED. LEAK CHECK OK. (M) 2L72 4F A6WE 19951106004141995110600414WP 1995 11 6 HALA95133 119951004A335060030431 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13674MC 12585 47735 HNL - BOTH FORWARD OVERWING EMERGENCY LIGHTS DON'T COME ON DURING TEST. REPLACED BATTERY PACK OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106004151995110600415WP 1995 11 6 HALA95134 119951005A3350P4010049 EEL BATT PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 9014 47764 HNL - EMERGENCY FLOOR LIGHTS FROM OVERWING EXIT TO ROW 1 INOPERATIVE. REPLACED FLOOR LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106004161995110600416SW 1995 11 6 SWHA95005 119950828A2150 ACM SWRNGNSA227 SA227AC 8780603SW RIGHT FAILED A SWHAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW17368AE AC696 PILOT REPORTED THAT ON SCHEDULED FLIGHT FROM ABI TO AUS, AFTER TAKEOFF, THE AIR OUTLETS BECAME HOT AND THE AIRCRAFT FILLED WITH SMOKE. SMOKE EVACUATION PROCEDURES WERE CARRIED OUT AND THE AIRCRAFT RETURNED TO ABI AND LANDED WITHOUT INCIDENT. THE AIRCRAFT ENGINES WERE INSPECTED FOR COMPRESSOR SEAL FAILURE, NONE FOUND. THE AIRCRAFT WAS GROUND OPERATED AND THE RIGHT AIR CYCLE MACHINE WAS FOUND FAULTY AND PLACED ON MEL DEFERRAL, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19951106004171995110600417NM 1995 11 6 TAOA099513 119950929A335007912 EEL BOEING727 727225 1384077NM CABIN MISSING A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 20441 TWO 'E' PATH LIGHT ASSEMBLIES MISSING AT ROW 10. REPLACED LIGHT ASSEMBLIES. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951106004181995110600418NM 1995 11 6 USAA950990 119950915A5313 STRINGER BOEING737 737201 1384454NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19260AU33045 22866 ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND 8 INCH BY 3 INCH CORRODED AREA ON BOTTOM AND SIDES OF STRINGER. STRINGER 27L BENEATH FRAME AT BS 967. REMOVED CORRODED STRINGER AREA AND INSTALLED SPLICED STRINGER PER SRM. REPAIR PER SRM 53-10-3 FIG 1. (M) 2L72 4F A16WE 19951106004191995110600419NE 1995 11 6 USAA951000 219950907A7230 COMPRESSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE LT ENGINE FAILED A USAAK NONE R PARTIAL RPM/PWR LOSS DEDESCENT 1 EA19966VJ 47420 BNA - COMPRESSOR STALL ON LEFT ENGINE. CAPTAIN SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE PER JOB CARD. OPS AND LEAK CHECKED NORMAL. (M) 2L72 4F4 F A6WE E2EA 19951106004201995110600420NM 1995 11 6 USAA951001 119950916A5330 SKIN BOEING737 7372B7 1384560NM BS 747 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19283AU33022 23116 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 6.5 INCH BY 8 INCH CORRODED SKIN, BS 747 S-27R. REMOVED CORROSION AND INSTALLED DOUBLER, REPAIRED PER SRM 53-10-4. (M) 2L72 4F A16WE 19951106004211995110600421NM 1995 11 6 USAA951002 119950920A5313 STRINGER BOEING737 7372B7 1384560NM BS 986-1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19283AU33022 23116 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1 INCH CORRODED AREA STRINGER 27L BETWEEN STATION 986-1016. SPLICED NEW STRINGER, REPAIRED PER SRM 53-10-3. (M) 2L72 4F A16WE 19951106004221995110600422NM 1995 11 6 USAA951003 119950923A7931ST104Z OIL PRESS XMITTR BOEING737 737201 1384454NM NR 2 ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA19265AU45104 22962 BUF - FLT NR 1063 - ON CLIMB-OUT FROM BUF, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO 15 PSI. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO BUF WHERE LANDING WAS WITHOUT INCIDENT. SET WAS 11 MINUTES. MAINTENANCE REPLACED THE NR 2 ENGINE OIL PRESSURE TRANSMITTER. OPS CHECKED GOOD. (M) 2L72 4F A16WE 19951106004231995110600423 1995 11 6 95ZZZM576 419950918A2565300117265 CYLINDER 415670014 CVAC 440 440 2422902WP REAR SERV DOOR LOW PRESSURE A SPAAK NONE O OTHER ININSP/MAINT 1 WP0773157 FL015 312 DURING PREFLIGHT, THE EVACUATION SLIDE CYLINDER PRESSURE WAS FOUND TO BE BELOW LIMITS. THE EVACUATION SLIDE/CYLINDER ASSEMBLY WAS REPLACED. 2L72 4R 6A6 19951106004241995110600424WP 1995 11 6 95ZZZM577 119950801A5311ACA3750 FRAME DOUG DC10 DC1010 3022110WP BS 808 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07124AA68635 46524 DURING C-CHECK, FOUND EXISTING DAMAGED REPAIRS NOTED AFT OF CENTER LOWER CARGO DOOR, WITH ADDITIONAL DAMAGE SURROUNDING THE REPAIR DOUBLERS. REWORKED ALL SCRATCHES AND GOUGES PER DC-10 SRM 53-00-01 FIG 1, 'VISUALLY INSPECTED FUSELAGE SKIN FROM STATION 1781 TO STATION 1821, BETWEEN L-36R AND L-42R EVERY C-CHECK FOR ADDITIONAL DAMAGE' IAW LACI EO 3138. (M) 2L73 4F A22WE 19951106004251995110600425WP 1995 11 6 95ZZZM578 119950801A5311ADA0031 FRAME DOUG DC10 DC1010 3022110WP BS 808 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07124AA68635 46524 DURING C-CHECK, FOUND EXISTING DAMAGED REPAIRS NOTED AFT OF CENTER LOWER CARGO DOOR, WITH ADDITIONAL DAMAGE SURROUNDING THE REPAIR DOUBLERS. REWORKED ALL SCRATCHES AND GOUGES PER DC-10 SRM 53-00-01 FIG 1, 'VISUALLY INSPECTED FUSELAGE SKIN FROM STATION 1781 TO STATION 1821, BETWEEN L-36R AND L-42R EVERY C-CHECK FOR ADDITIONAL DAMAGE' IAW LACI EO 3138. (M) 2L73 4F A22WE 19951106004261995110600426WP 1995 11 6 95ZZZM579 119950728A5311ACA3750 FRAME DOUG DC10 DC1010 3022110WP BS 808 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07124AA6863525281 46524 DURING C-CHECK, FOUND FORWARD CARGO PIT FRAMES CRACKED, AT BS 808 AND 1099. THE FRAME AT 808 IS CRACKED 2 INCHES AT LBL 60, AND THE FRAME AT 1099 IS CRACKED 2 INCHES AT BOTH LBL 60 AND THE FRAME AT 1099 IS CRACKED 2.5 INCHES AT RBL 60. FABRICATED AND INSTALLED REPAIR ANGLES, IAW LACI EO 3112. (M) 2L73 4F A22WE 19951106004271995110600427WP 1995 11 6 95ZZZM580 119950728A5311ADA0031 FRAME DOUG DC10 DC1010 3022110WP BS 808 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07124AA6863525281 46524 DURING C-CHECK, FOUND FORWARD CARGO PIT FRAMES CRACKED, AT BS 808 AND 1099. THE FRAME AT 808 IS CRACKED 2 INCHES AT LBL 60, AND THE FRAME AT 1099 IS CRACKED 2 INCHES AT BOTH LBL 60 AND THE FRAME AT 1099 IS CRACKED 2.5 INCHES AT RBL 60. FABRICATED AND INSTALLED REPAIR ANGLES, IAW LACI EO 3112. (M) 2L73 4F A22WE 19951106004281995110600428NM 1995 11 6 95ZZZM581 119950811A3350 EEL WIRE BOEING767 767201 1385125NM CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 LAX - FLT NR 0816 - THE FLOOR TRACK LIGHTING IN THE FORWARD CABIN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE FLOOR TRACK LIGHTING WIRE ON THE FORWARD LEFT SECTION AND REPLACED THE BATTERY CHARGER ASSEMBLY. REFERENCE USAA950903. 2L72 4F RTA1NM 19951106004291995110600429NM 1995 11 6 95ZZZM582 119950911A5720 COMPRESSOR BOEING727 727290 138408WNM NR 2 ENGINE STALLED A UHVACD ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TOTAKEOFF 1 SO17295AS 22147 FLT NR KYC133 - KBOS-KPHL - ON TAKEOFF NR 2 ENGINE COMPRESSOR STALLED AT APPROXIMATELY 2.00 EPR. TAKEOFF ABORTED BELOW 60 KTS. VISUALLY INSPECTED C1 AND TURBINE. CHECKED BLEED VALVES AND SCHEDULING. ADJUSTED P AND D VALVE HALF TURN. ENGINE RUNUP CHECKED GOOD, NO STALLING. FERRIED AIRCRAFT TO KFLL NR 2 ENGINE AT REDUCED POWER. BORESCOPED ENGINE, NO DAMAGE. REPLACED P AND D VALVE. WATER WASHED ENGINE. RUNUP CHECKED OK. RETURNED TO SERVICE. 2L73 4F A3WE 19951106004301995110600430NM 1995 11 6 AALA99515 119950928A3244 TIRE BOEING747 747212B 1384886NM NR 7 FAILED A SRAAK NONE O OTHER LDLANDING 1 SO19745SJ 20888 ON LANDING AT BOGATA, NR 7 TIRE BLEW, NR 8 TIRE WENT FLAT AND NR 11 TIRE HAD A FLAT SPOT. AIRCRAFT SUFFERED BODY GEAR DOOR, AND BODY GEAR STEERING HARNESS DAMAGE. INSPECTED AIRCRAFT FOUND NO FURTHER DAMAGE. REPLACED DOOR AND NR 7, 8, AND 11 MAIN WHEEL, REPAIRED BODY GEAR STEERING HARNESS, SYSTEM OPS CHECKED GOOD. (M) 2L74 4F A20WE 19951106004311995110600431SW 1995 11 6 BDHA9500019 119950914A7931M401144 OIL PRESS SW SWRNGNSA226 SA226TC 8780404SW LT ENGINE FAILED A BDHAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15328BA TC253 MSP - FLT NR 421 - AFTER TAKEOFF, THE LEFT OIL PRESSURE WARNING LIGHT ILLUMINATED WITH ALL OTHER INDICATIONS NORMAL. THE AIRCRAFT RETURNED TO MSP FOR MAINTENANCE TO INSPECT. INSPECTION OF THE SYSTEM FOUND THE OIL PRESSURE WARNING LIGHT SWITCH STUCK CLOSED. THE SWITCH WAS REPLACED AND ALL INDICATION WERE NORMAL. THE AIRCRAFT WAS RELEASED. (M) 1L72 4T A8SW 19951106004321995110600432SW 1995 11 6 BDHA9500020 119950920A32440283353 TIRE SWRNGNSA226 SA226TC 8780404SW LT MLG FLAT SPOT A BDHAK NONE O OTHER LDLANDING 1 GL15328BA TC253 BIS - FLT NR 421 - ON LANDING, THE LEFT OUTBOARD TIRE WAS FLAT SPOTTED. THE BRAKE SYSTEM WAS INSPECTED AND THE TIRE WAS CHANGED. THE PARKING BRAKE WAS SET AT THE PREVIOUS STOP AND MAY NOT HAVE BEEN FULLY RELEASED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19951106004331995110600433SO 1995 11 6 SRAA99511 119950925A2612700120 FIRE LOOP LKHEED382 382G 526414USO NR 3 NACELLE FAULTY A SRAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO19912SJ 4388 FLT NR 1018 - MIA-STX - DURING FLIGHT NR 3 ENGINE FIRE INDICATION CAME ON, SHUTDOWN NR 3 ENGINE AND LIGHT WENT OUT, DIVERTED TO SJU AIRCRAFT LANDED SAFELY WITHOUT INCIDENT. FOUND FAULTY FIRE WARNING LOOP, REPLACED LOOP SYSTEM OPS CHECKED GOOD. (M) 2H74 4T A1SO 19951106004341995110600434NE 1995 11 6 SRAA99512 219950925A7530 FILTERS BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 2 EBC CLOGGED A SRAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SO19745SJ 20888 AT TOP OF DESCENT INTO MIA AT 43,000 FEET, NR 2 ENGINE STALLED AS THRUST BEING REDUCED, SHUT DOWN ENGINE, EGT AT 950 DEGREES, ENGINE RESTARTED NORMALLY AT 16,000 FEET. TROUBLESHOT ENGINE FOUND ENGINE BLEED CONTROL FILTER CLOGGED. REPLACED FILTER, PERFORMED ENGINE RUN UP, OPS CHECKED GOOD PER MM CH 71. (M) 2L74 4F4 F A20WE E20EA 19951106004351995110600435SO 1995 11 6 SRAA99514 119950925A2612 WIRE LKHEED382 382G 526414USO NR 2 ENGINE CHAFED A SRAAK NONE L NO TEST ININSP/MAINT 1 SO19918SJ 4208 ON PRE-FLIGHT, FOUND NR 2 ENGINE FIRE WARNING WILL NOT TEST. INSPECTED FIRE LOOP ALL SECURED, TROUBLESHOT SYSTEM AND FOUND CHAFED WIRE AT FIRE WARNING CONTROL UNIT. REPAIRED WIRE AT CONNECTOR, SYSTEM OPS CHECKED GOOD. (M) 2H74 4T A1SO 19951106004361995110600436 1995 11 6 SRAA99517 319950927A6140 PROPELLER LKHEED382 382G 526414USO NR 1 LOW OIL LIGHT A SRAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19920SJ 4561 DURING FLIGHT ADT4, NR 1 PROP LOW OIL LIGHT CAME ON, NR 1 PROP PITCH LOCK CHECKED IN FLIGHT, FOUND OK. SHUT DOWN ENGINE AS PRECAUTIONARY AND DIVERTED AIRCRAFT TO AVB. INSPECTED NR 1 PROPELLER SYSTEM FOUND OK. SERVICED PROP OIL AND CYCLED PROP, SYSTEM OPERATED NORMAL. (M) 2H74 4T A1SO 19951106004371995110600437NM 1995 11 6 USAA950840 119950808A5230 DOOR BOEING737 737301 1384611NM CARGO COMPT AJAR A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19334US 23231 PHL - FLT NR 1487 - RETURN TO FIELD DUE TO THE AFT CARGO DOOR LIGHT ILLUMINATING. MAINTENANCE FOUND THE REAR CARGO DOOR AJAR. VISUAL AND MECHANICAL INSPECTION CHECKS GOOD. NO DEFECTS OR LIGHT MALFUNCTION NOTED. (M) 2L72 4F RTA16WE 19951106004381995110600438NM 1995 11 6 USAA950903 119950811A335020121 EEL BATT CHARGER BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19650US 23902 LAX - FLT NR 0816 - THE FLOOR TRACK LIGHTING IN THE FORWARD CABIN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE FLOOR TRACK LIGHTING WIRE ON THE FORWARD LEFT SECTION AND REPLACED THE BATTERY CHARGER ASSEMBLY. (M) 2L72 4F RTA1NM 19951106004391995110600439EU 1995 11 6 USAA950989 119950915A3260 UPLOCK SWITCH FOKKERF28 F28MK4000 4990810EU LT MLG DOORS MISALIGNED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19490US 11152 PIT - FL 1749 - LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED WHEN GEAR SELECTED UP. CYCLED GEAR AND BOTH MAIN GEAR RED LIGHTS ILLUMINATED ALONG WITH BOTH MAIN GEAR DOOR YELLOW LIGHTS. FLIGHT RETURNED TO PIT WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE LANDING GEAR DOOR UPLOCK SWITCHES. (M) 2L72 4F RTA20EU 19951106004401995110600440NM 1995 11 6 USAA950991 119950824A5313 STRINGER BOEING737 7373B7 1384580NM BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 500 PLUS 4 STRINGER 16L. INSTALLED DOUBLER, REPAIRED PER EO 5393X228. (M) 2L72 4F RTA16WE 19951106004411995110600441NM 1995 11 6 USAA950992 119950824A5313 STRINGER BOEING737 7373B7 1384580NM BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL, FOUND .5 INCH CRACK BS 500 C PLUS 4 STRINGER 16R. INSTALLED DOUBLER, REPAIRED PER EO 539X228. (M) 2L72 4F RTA16WE 19951106004421995110600442NM 1995 11 6 USAA950993 119950824A5313 STRINGER BOEING737 7373B7 1384580NM BS 500 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 500 C PLUS 16, STRINGER 16R. INSTALLED DOUBLER, REPAIRED PER EO 5393X228. (M) 2L72 4F RTA16WE 19951106004431995110600443NM 1995 11 6 USAA950994 119950823A5330 SKIN BOEING737 7373B7 1384580NM BS 925 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK IN FUSELAGE SKIN BS 925. INSTALLED EXT FUSELAGE SKIN REPAIR. REPAIRED PER SRM 53-00-01 FIG 202. (M) 2L72 4F RTA16WE 19951106004441995110600444NM 1995 11 6 USAA950995 119950825A5330 SKIN BOEING737 7373B7 1384580NM BS 887-867 CHAFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CROWN SKIN CHAFED UNDER DORSAL FIN CONTACT AREA, S-1 BS 887 TO BS 867. INSTALLED EXT SKIN DOUBLER. REPAIRED PER TR 53-30-03, SRM 53-00-01. (M) 2L72 4F RTA16WE 19951106004451995110600445NM 1995 11 6 USAA950996 119950829A5320 ANGLE BOEING737 7373B7 1384580NM CARGO BIN CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AT CLIP NUT HOLES, AFT CARGO BIN AFT CENTER BULKHEAD LOWER ATTACH ANGLE. REPLACED ATTACH ANGLE, REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-202-01, CORR5OSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004461995110600446NM 1995 11 6 USAA950997 119950829A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 947.5-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION BS 947.5 TO BS 967 RBL 45 ON FLOOR BEAM T-CAP. FABRICATED NEW T-CAP 18 INCHES LONG, REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004471995110600447NM 1995 11 6 USAA950998 119950828A5313 STRINGER BOEING737 7373B7 1384580NM BS 870 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION BS 870 S-21L. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-70-11 FIG 1. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004481995110600448NM 1995 11 6 USAA950999 119950824A5320 DUMP SHOOT BASE BOEING737 7373B7 1384580NM BS 986.5-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19510AU27584 23385 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 6 INCH CORRODED AREA AFT CARGO BS 986.50- BS 1006 DUMP SHOOT BASE. INSTALLED NEW BASE PER DRAWING 65-45781, REPAIRED PER BOEING DRAWING 65-45781. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004491995110600449NM 1995 11 6 USAA951004 119950924A24209125ZC7C4001S RELAY BOEING737 7373B7 1384580NM NR 1 X-FER BUS FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19376US 22955 IND - FLT NR 1157 - EN ROUTE LGA TO MCI, NR 1 NORMAL TRANSFER BUS CIRCUIT BREAKER POPPED. CREW RESET BREAKER AND IT POPPED AGAIN. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TRANSFER RELAY. RAN ENGINES AND APU. OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19951106004501995110600450NM 1995 11 6 USAA951007 119950908A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 18 INCHES STATION 986.5 BL ZERO TO LBL 24 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004511995110600451NM 1995 11 6 USAA951008 119950906A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 36 INCHES STATION 344 LBL 24 INCHES TO RBL 12 INCHES. REPLACED UPPER T-CAP OF BEAM. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004521995110600452NM 1995 11 6 USAA951009 119950913A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 294.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES AT STATION 294.5 LBL 20 INCHES. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER. REPAIRED PER SRM 53-10-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004531995110600453NM 1995 11 6 USAA951010 119950921A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 958 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION EXCEEDING LIMITS AROUND HOLE, BS 958 RBL 7.5. FABRICATED NEW INTERCOSTAL FROM BAC1506-437075-T6 AND INSTALLED. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004541995110600454NM 1995 11 6 USAA951011 119950913A5320 ANGLE BOEING737 737301 1384611NM BS 370 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 5 INCHES AT STATION 370 AT FORWARD ENTRY THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING 65C80735. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004551995110600455NM 1995 11 6 USAA951012 119950912A5320 ANGLE BOEING737 737301 1384611NM SERVICE DOOR CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCHES AT FORWARD SERVICE DOOR THRESHOLD. REPLACED Z-ANGLE. REPAIRED PER BOEING DRAWING NR 6545875. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004561995110600456NM 1995 11 6 USAA951013 119950919A53201100377 ANGLE BOEING737 737301 1384611NM BS 947.5-992.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19339US27606 23236 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES AT BS 947.5 TO BS 992.5 LBL 53 AFT ENTRY DOOR. REPAIRED PER BOEING DRAWING 65-52878. CORROSION LEVEL 2. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19951106004571995110600457WP 1995 11 6 USAA951043 119950919A5320 T-CAP DOUG DC9 DC981 3022081WP BS 1338 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19801US39711 48037 PIT - DURING C-4 CHECK INSPECTION, FOUND A 3 INCH, 2 INCH AND A 1.1875 INCH CRACK AT STATION 1338 AT LONGERON 14L, 12L AND BETWEEN 14L AND 15L (EDDY CURRENT). REMOVED AND REPLACED UPPER LEFT T-CAP SEGMENT PER USAIR EO NR 5389X252 PART 2. (M) 2L72 4F A6WE 19951106004581995110600458 1995 11 6 USAA951045 419950926A3417HG480B42 AIR DATA COMP BOEING737 737401 1384701NM E/E BAY FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19407US48750 23877 PIT - FLT NR 0497 - AFTER TAKEOFF FROM PIT, FLIGHT OFFICERS AIRSPEED, ALTIMETER, AND RATE OF CLIMB INDICATORS FAILED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ADC. OPERATIONS CHECKED OK. (M) 2L72 4F RTA16WE 19951106004591995110600459NM 1995 11 6 USAA951048 119950929A2720308504 TRIM SWITCH 69737038 BOEING737 737301 1384611NM RUDDER TRIM FAILED A AUSAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19563AU D00029 23551 DAY - FLT 0223 - EN ROUTE IND TO BWI, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT FULL RUDDER TRIM. CREW DISCONNECTED THE AUTOPILOT AND YAW DAMPER WITH NO EFFECT. FLIGHT DIVERTED TO DAY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RUDDER TRIM INDICATOR, CONTROL MODULE, AND ACTUATOR. PROBLEM WAS CONFIRMED AS A BAD RUDDER TRIM SWITCH. (M) 2L72 4F RTA16WE 19951106004601995110600460NM 1995 11 6 USAA951051 119950907A5320 DOOR FRAME BOEING737 7374B7 1384702NM BS 296 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK, BS 296 AT WL 208 (RIGHT DOOR CUTOUT FRAME). CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-70-11. (M) 2L72 4F RTA16WE 19951106004611995110600461NM 1995 11 6 USAA951052 119950911A5315 FLOOR BEAM BOEING737 7374B7 1384702NM BS 986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION BS 986 RBL 31. CUT OUT CORROSION, INSTALLED FILLERS AND REPAIR ANGLES, REPAIRED PER SRM 53-60-51, FIG 203. (M) 2L72 4F RTA16WE 19951106004621995110600462NM 1995 11 6 USAA951053 119950915A5754 SKIN BOEING737 7374B7 1384702NM NR 1 SLAT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND THREE .375 INCH CRACKS AT NR 1 SLAT BS 299.32 ON BOTTOM SKIN. CUT OUT SECTION OF SKIN AND INSTALLED DOUBLER, REPAIRED PER EA 39909. (M) 2L72 4F RTA16WE 19951106004631995110600463NM 1995 11 6 USAA951054 119950926A53206545834256 INTERCOSTAL BOEING737 7374B7 1384702NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 8 INCH CORRODED AREA BETWEEN BS 312 THROUGH BS 328 AT RBL 12 INCHES. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004641995110600464NM 1995 11 6 USAA951055 119950926A53206545834259 INTERCOSTAL BOEING737 7374B7 1384702NM BS 328.344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 5 INCH AND .25 INCH BY 6 INCH CORRODED AREA BETWEEN BS 328 AND BS 344 AT LBL 12 INCHES. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004651995110600465NM 1995 11 6 USAA9510558 119950912A532065C333701 INTERCOSTAL BOEING737 7374B7 1384702NM BS 950 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOT OF CORROSION RBL 24 BS 950. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004661995110600466NM 1995 11 6 USAA951056 119950912A532065C333701 INTERCOSTAL BOEING737 7374B7 1384702NM BS 950 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION LBL 24 BS 950. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004671995110600467NM 1995 11 6 USAA951057 119950912A532065C3184779 INTERCOSTAL BOEING737 7374B7 1384702NM BS 968 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLE RBL 17 BS 968. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004681995110600468NM 1995 11 6 USAA951059 119950912A532069773083 LAV MOUNT PAD BOEING737 7374B7 1384702NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION AT BS 947 LBL 47. REPLACED MOUNT PAD, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004691995110600469NM 1995 11 6 USAA951060 119950912A5315 FLOOR BEAM BOEING737 7374B7 1384702NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION AT LBL 9 BS 947. CUT OUT DAMAGE, INSTALLED FILLER AND REPAIR ANGLES, REPAIRED PER SRM 53-60-51, FIG 203. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004701995110600470NM 1995 11 6 USAA951061 119950908A5315 FLOOR BEAM BOEING737 7374B7 1384702NM BS 987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH BY 2 INCH AREAS OF CORROSION BS 987 LBL 32 AND LBL 45. CUT OUT CORROSION AND INSTALLED REPAIR ANGLES AND STRAPS. REPAIRED PER TR 53-10-01A, SRM 53-60-51 FIG 203. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004711995110600471NM 1995 11 6 USAA951062 119950907A53206549631 ANGLE BOEING737 7374B7 1384702NM BS 500 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND SEVERAL .75 INCH BY .5 INCH SPOTS OF CORROSION BS 500G STRINGER 15R TO STRINGER 25L. REPLACED ATTACHED ANGLE, REPAIRED PER DRAWING 65-49631 AND SRM 51-10-2. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004721995110600472NM 1995 11 6 USAA951063 119950907A532065C8073518 ANGLE BOEING737 7374B7 1384702NM BS 303-360 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND ABOUT AN 1 INCH BY 57 INCH CORRODED AREA BS 303-360, S-17L, FORWARD ENTRY DOOR Z-ANGLE. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE FROM STOCK P/N 65C80735-18. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004731995110600473NM 1995 11 6 USAA951064 119950914A5320 BEAM BOEING737 7374B7 1384702NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 28 INCHES BY .5 INCH CORROSION AT STATION 344 LBL 28, LLB ZERO. FABRICATED T-CAP AND REPAIRED ANGLES. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004741995110600474NM 1995 11 6 USAA951065 119950914A53206545834611 INTERCOSTAL BOEING737 7374B7 1384702NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 16 INCH CORROSION RBL 12 STATION 328 TO STATION 344. FABRICATED INTERCOSTAL. REPAIRED PER BOEING DRAWING 65-45234. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004751995110600475NM 1995 11 6 USAA951066 119950913A5320 BEAM BOEING737 7374B7 1384702NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT -DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREA AT BS 328 LBL 35 INCHES TO RBL 65 INCHES. REMOVED DAMAGE, INSTALLED REPAIR PARTS COMPLETE REPAIR. REPAIRED PER SRM 53-10-51 T/R 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004761995110600476NM 1995 11 6 USAA951067 119950914A5315 FLOOR BEAM BOEING737 7374B7 1384702NM BS 294.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER AREA OF CORROSION STATION 294.5 FLOOR BEAM UPPER CHORD AT RBL 4. INSTALLED REPAIR ANGLES PER SRM 53-10-51 FIG 206. REPAIRED PER SRM 53-10-51, FIG 206. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004771995110600477NM 1995 11 6 USAA951068 119950913A5320 INTERCOSTAL BOEING737 7374B7 1384702NM BS 294.5-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 18 INCH CORRODED AREA BS 294.5 TO BS 312 AT RBL 12. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004781995110600478NM 1995 11 6 USAA951069 119950912A53201124784 ANGLE BOEING737 7374B7 1384702NM BS 947-997 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1 INCH BY 48 INCH AREA CORRODED AFT ENTRY DOOR Z-ANGLE BS 947 THROUGH BS 997. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE EPR SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004791995110600479NM 1995 11 6 USAA951070 119950911A5320654587545 ANGLE BOEING737 7374B7 1384702NM BS 280-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19430US17472 24552 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 60 INCH CORRODED AREA BS 280-BS 344, STRINGER 17R (FORWARD SERVICE DOOR Z-ANGLE). REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE FROM STOCK P/N 654587545. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C52-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951106004801995110600480NM 1995 11 6 95ZZZM583 119950816A3244 TIRE BOEING727 727259 138408JNM NR 2 WHEEL SEPARATED A UHVACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO17203AV 22474 XKYC - FLT NR 204 - ON TAKEOFF ROLL, REACHING 110 KNOTS, NR 2 MAIN TIRE SEPARATED, ABORTED TAKEOFF. FOUND DAMAGED FLAP COVE PANEL ABOVE NR 2 TIRE. ACCOMPLISHED TEMPORARY REPAIR PER AVITAS REPAIR ORDER 95AVAT.003R001 TO PANEL P/N 65-21656-621. REPLACED NR 1 AND NR 2 WHEEL ASSEMBLIES. REMOVED AND REPLACED LEFT WING INBOARD TRAILING EDGE FLAP COVE PANEL PER MM 57-20-31, REFERENCED IN AVITAS REPAIR ORDER 95AVAT.003R0-1. TEMPORARY REPAIR INSPECTIONS TERMINATED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 19951106004811995110600481NM 1995 11 6 95ZZZM584 119950816A5720 COVE PANEL BOEING727 727259 138408JNM LT WING DAMAGED A UHVACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO17203AV 22474 XKYC - FLT NR 204 - ON TAKEOFF ROLL, REACHING 110 KNOTS, NR 2 MAIN TIRE SEPARATED, ABORTED TAKEOFF. FOUND DAMAGED FLAP COVE PANEL ABOVE NR 2 TIRE. ACCOMPLISHED TEMPORARY REPAIR PER AVITAS REPAIR ORDER 95AVAT.003R001 TO PANEL P/N 65-21656-621. REPLACED NR 1 AND NR 2 WHEEL ASSEMBLIES. REMOVED AND REPLACED LEFT WING INBOARD TRAILING EDGE FLAP COVE PANEL PER MM 57-20-31, REFERENCED IN AVITAS REPAIR ORDER 95AVAT.003R0-1. TEMPORARY REPAIR INSPECTIONS TERMINATED. AIRCRAFT RETURNED TO SERVICE. 2L73 4F A3WE 19951106004821995110600482CE 1995 11 6 95ZZZM585 119951004A324611480017 WHEEL BFGOODRICH 3B1426 BEECH 1900 1900D 1154162CE NLG CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01848CA2639 0814 UE53 DURING DETAILED INSPECTION, NOSE WHEEL WAS DISCOVERED CRACKED AROUND VALVE STEM HOLE. REMOVED AND REPLACED COMPLETE WHEEL ASSEMBLE P/N 114-8001-3. 2L72 4T RTA24CE 19951106004831995110600483CE 1995 11 6 95ZZZM586 119951002A324611480017 WHEEL BFGOODRICH 3B1426 BEECH 1900 1900D 1154162CE NLG CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01857CA3394 0731 UE71 DURING ROUTINE INSPECTION, NOSE WHEEL WAS DISCOVERED CRACK AROUND VALVE STEM HOLE. REMOVED AND REPLACED COMPLETE WHEEL ASSEMBLY P/N 114-8001-3. 2L72 4T RTA24CE 19951106004841995110600484CE 1995 11 6 95ZZZM587 119951004A3230 CLEVIS 2570022 BEECH 1900 1900D 1154162CE NLG SEIZED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01836CA5541 288 UE32 DURING NOSE LANDING GEAR MAINTENANCE, THE EXTEND RETRACT ACTUATOR YOKE CLEVIS WAS DISCOVERED SEIZED IN PISTON END. THIS CONDITION PRECLUDED ACTUATOR RIGGING AND RESULTED IN A ACTUATOR CHANGE. S/S RECOMMEND CLEVIS BE INSTALLED WITH ANTI-SEIZE COMPOUND DURING MANUFACTURE. 2L72 4T RTA24CE 19951106004851995110600485WP 1995 11 6 95ZZZM588 119951009A57309919459509 COVER DOUG DC9 DC932 3022066WP RT WING NOT SEALED A VJ6AA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11915VV 47443 FLT NR 572 - ATL-MCI - CREW NOTICED FUEL LEAKING FROM RIGHT WING FUEL TANK ACCESS PLATE. FLIGHT RETURNED TO ATL FOR REPAIRS. ATL MAINTENANCE RESEALED RIGHT WING UPPER TANK PLATE BL 1426. 2L72 4F A6WE 19951106004861995110600486CE 1995 11 6 95ZZZM589 119950819A7120 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV12088 UC137 DURING A INSPECTION OF AREA 'A' ON THE RIGHT ENGINE TRUSS A .5 INCH CRACK. REPAIRED BY WELDING CRACK. (M) 2L72 4T RTA24CE 19951106004871995110600487CE 1995 11 6 95ZZZM590 119950920A575310116000144 RIB BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV 3351 853 UC134 DURING ROUTINE MAINTENANCE, RIGHT INBOARD FLAP WAS FOUND TO HAVE CRACKED AT TRAILING EDGE APPROXIMATELY 1 INCH LONG, AND ONE WAS .5 INCH LONG ON SECOND RIB FROM OUTBOARD END. REPAIRED WITH DOUBLER. (M) 2L72 4T RTA24CE 19951106004881995110600488CE 1995 11 6 95ZZZM591 119950920A575335165005259 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07134YV 712 UC134 DURING ROUTINE MAINTENANCE, A CRACK APPROXIMATELY 1 INCH WAS FOUND 34 INCHES FROM OUTBOARD END. REPAIRED WITH A DOUBLER. (M) 2L72 4T RTA24CE 19951106004891995110600489CE 1995 11 6 95ZZZM592 119951002A575335165050259 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07137YV 2625 745 UC137 RIGHT OUTBOARD FLAP CRACKED .75 INCH ON TRAILING EDGE, 35 INCHES FROM OUTBOARD END OF FLAP. STOPPED DRILLED AND INSTALLED DOUBLER. (M) 2L72 4T RTA24CE 19951106004901995110600490CE 1995 11 6 95ZZZM593 119950813A575335165050259 RIB BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07158YV 1819 UC158 DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND FOURTH RIB INBOARD 1.5 INCHES UP FROM TRAILING EDGE. REPAIRED WITH PATCH. 2L72 4T RTA24CE 19951106004911995110600491NM 1995 11 6 95ZZZM594 119951012A261269B475193 FIRE WARN CARD BOEING747 747132 1384882NM APU SHORTED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74607 20247 KLAX - APU 'A' LOOP FIRE DETECTOR FLICKERS IN FLIGHT. REMOVED AND REPLACED FIRE WARNING CONTROL CARD AND FIRE DETECTOR CONTROL CARD FOR APU 'A' LOOP SYSTEM. OPS CHECK GOOD IAW B747 MM 26-10-00 AND 26-15-00. DMI NR 248 CLEARED/PLACARD REMOVED. REFERENCE NR CKSA95106. 2L74 4F A20WE 19951106004921995110600492WP 1995 11 6 AALA951680 119950920A3350A3030398101 EEL CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07291AA 49303 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951106004931995110600493NM 1995 11 6 AALA951701 119950919A33508100022002 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07369AA 25196 SFO - DURING OVERNIGHT CHECK, ONE SEGMENT OF EMERGENCY LIGHTS AT MID-GALLEY CROSS AISLE INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT MID-GALLEY CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951106004941995110600494 1995 11 6 AALA951702 419950920A2564101651303 SLIDE RAFT BFGOODRICH BOEING767 767223 1385123NM FWD ENTRY DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A5938 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE RAFT UPPER AND LOWER TUBES FOUND TORN. EMERGENCY EVACUATION SLIDE RAFT ROUTED TO VENDOR FOR REPAIR. (M) 2L72 4F RTA1NM 19951106004951995110600495 1995 11 6 AALA951703 419950920A2564101651303 SLIDE RAFT BFGOODRICH BOEING767 767223 1385123NM FWD ENTRY DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW07 4313 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE RAFT SEPARATED AT LEFT ASPIRATOR TUBE. EMERGENCY EVACUATION SLIDE RAFT ROUTED TO VENDOR FOR REPAIR. (M) 2L72 4F RTA1NM 19951106004961995110600496NM 1995 11 6 AALA951704 119950920A3350A3060719102 EEL STRIP DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071759 48481 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 2D INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY PASSENGER SEAT 2D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19951106004971995110600497NM 1995 11 6 AALA951721 119950926A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07351AA 24032 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT FORWARD LEFT FIRST CLASS SEAT INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR FOR FORWARD LEFT FIRST CLASS SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951106004981995110600498NM 1995 11 6 AALA951732 119950927A3350 EEL WIRE BOEING767 767323 1385205NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07366AA 25193 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RIGHT AISLE BETWEEN PASSENGER SEAT ROWS 7 AND 12 INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19951106004991995110600499NM 1995 11 6 AALA951738 119950927A3350P2010031303 EEL ASSY DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071753 48487 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT EXIT LAMP AT L4 DOOR INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT EXIT LAMP AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19951106005001995110600500EU 1995 11 6 AALA951739 119950930A3350A1030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0733069 512 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 21GH INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 21GH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951106005011995110600501NM 1995 11 6 AALA951740 119951001A3350A3030398101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071755 48490 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE OF FIRST CLASS CABIN INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FIRST ROW OF PASSENGER SEATS AT LEFT AISLE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19951106005021995110600502NM 1995 11 6 AALA951742 119951002A3350A3030398101 EEL CONNECTOR BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07636AM 24594 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 9 AND 17 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19951106005031995110600503NM 1995 11 6 AALA951774 119951010A32306517840309 LINE BOEING727 727223 1384074NM RT MLG RUPTURED A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW07843AA 20984 MAI - FLT NR 0827 - EN ROUTE FLL-DFW - AFTER TAKEOFF, WHILE TRYING TO RETRACT LANDING GEAR, HYDRAULIC SYSTEM 'A' QUANTITY AND PRESSURE WENT TO ZERO. BOTH MAIN GEARS STAYED DOWN, NOSE GEAR RETRACTED. MANUALLY EXTENDED NOSE GEAR AND AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT GEAR ACTUATOR UP LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951106005041995110600504NM 1995 11 6 AWXA9500666 119950928A3350 EEL ASSY BOEING737 73733A 1384673NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28166AW 23627 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 13 AND ROW 14. RECONNECTED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951106005051995110600505NM 1995 11 6 AWXA9500667 119950929A335010006779 EEL ASSY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28187AW 22654 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951106005061995110600506NM 1995 11 6 AWXA9500668 119950930A3350900835A EEL BATTERY PACK BOEING737 737297 1384480NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28147AW 22630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT EMERGENCY EXIT LIGHT IDENTIFIER INOPERATIVE. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK, SYSTEM OPS CHECK GOOD. (M) 2L72 4F A16WE 19951106005071995110600507NM 1995 11 6 AWXA9500675 119951002A3230273N10694 CRANK ASSY BOEING757 7572G7 1384963NM NLG BROKEN A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28909AW 24522 EWR-PHX - FLT NR 16 - DURING CLIMB, GEAR DOOR MESSAGE APPEARED ON EICAS. CREW CYCLED GEAR AND RESET CIRCUIT BREAKERS WITH NO HELP. AIRCRAFT RETURNED TO EWR LANDING UNEVENTFULLY. CMH MAINTENANCE TECHS FOUND NLG SEQUENCING VALVE LOWER CRANK ASSEMBLY BROKEN. MAINTENANCE REPLACED VALVE ASSEMBLY PER MM 32-34-06. OPS CHECK OK PER MM 32-34-00. OVERWEIGHT INSPECTION C/W PER AWM386. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19951106005081995110600508NM 1995 11 6 AWXA9500682 119951003A3350 EEL WIRING BOEING737 737275 1384485NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR, R1 DOOR AND FIRST FOUR ROWS OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BASE WIRING OF FIRST FOUR ROWS. OPS CHECK GOOD. (M) 2L72 4F A16WE 19951106005091995110600509NM 1995 11 6 AWXA9500684 119951004A3350 EEL WIRE BOEING737 7373S3 1384711NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28316AW 23713 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 17 THROUGH ROW 21. REPAIRED BROKEN WIRE, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951106005101995110600510NM 1995 11 6 AWXA9500689 119951009A5312 BULKHEAD BOEING737 7372A6 138448BNM BS 227.8 CRACKED A AWXAO OTHER O OTHER CLCLIMB 1 WP28145AW 20194 TUS-PHX - CABIN WOULD NOT HOLD ALTITUDE WITH LT PACK OFF AND THRUST AT IDLE. DUCT PRESSURE 14 PSI AT 12,000 FEET CABINS CLIMBS AT 1500 FPM. AIRCRAFT CONTINUED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 10 INCH CRACK IN BULKHEAD AT STATION 227.8. MAINTENANCE INSTALLED FORWARD BULKHEAD REINFORCEMENT KIT PER EO 53-11-05. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19951106005111995110600511NM 1995 11 6 AWXA9500690 119951005A5720 ANGLE BOEING737 73733A 1384673NM LT RAM AIR DUCT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28167AW 23628 PHX - DURING SCHEDULED C10 INSPECTION, FOUND SHEARED RIVETS AND A CRACK IN ANGLE ALONG OUTER EDGE AT WING LOWER SKIN OF LT RAM AIR DUCT. INSTALLED NEW ANGLE PER SRM 57-40-02, AND RESHOT RIVETS. (M) 2L72 4F RTA16WE 19951106005121995110600512NM 1995 11 6 AWXA9500691 119951005A5220 SKIN BOEING737 73733A 1384673NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28167AW 23628 PHX - DURING SCHEDULED C10 INSPECTION, FOUND L2 DOOR UPPER HINGE CUTOUT ON DOOR CRACKED AT LOWER CORNER. INSTALLED REPAIR DOUBLER PER ER 3-52-11-08. (M) 2L72 4F RTA16WE 19951106005131995110600513NM 1995 11 6 AWXA9500692 119951004A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 294.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FLOOR BEAM UPPER T-CAP CORRODED AT BS 294.5 FROM LBL 10 TO RBL 42. REMOVED AND REPLACED T-CAP PER SRM 53-10-9, FIGURE 5. (M) 2L72 4F RTA16WE 19951106005141995110600514NM 1995 11 6 AWXA9500693 119951004A5313 STRINGER BOEING737 737277 1384570NM BS727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND STRINGER 2L AT BS 727B CRACKED. REPAIRED PER SRM 53-10-3, FIGURE 4. (M) 2L72 4F RTA16WE 19951106005151995110600515NM 1995 11 6 AWXA9500694 119951004A5753 FLAP TRACK BOEING737 737277 1384570NM TE FLAPS CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND NR 2 MAIN FLAP TRACK CORRODED AT PARTING SURFACE OF MOUNT BOLTS. MACHINED MOUNT SURFACE PER ER 2-57-20-12A. (M) 2L72 4F RTA16WE 19951106005161995110600516NM 1995 11 6 AWXA9500695 119951004A5320 FITTING BOEING737 737277 1384570NM R1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND R1 DOOR FORWARD GIRT BAR ATTACH FITTING CORRODED BEYOND LIMITS. FABRICATED REPLACEMENT FITTING AND INSTALLED PER SRM 51-30-2. (M) 2L72 4F RTA16WE 19951106005171995110600517NM 1995 11 6 AWXA9500696 119951004A5330 SKIN BOEING737 737277 1384570NM DOOR CUTOUT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND AFT GALLEY FUSELAGE DOOR CUTOUT LOWER FORWARD RADIUS AREA SKIN CRACKED AT RIVETS FORWARD OF THRESHOLD PLATE. INSTALLED REPAIR PER SRM 53-30-3, FIGURE 24. (M) 2L72 4F RTA16WE 19951106005181995110600518NM 1995 11 6 AWXA9500697 119951004A57536546428 FLAP TRACK BOEING737 737277 1384570NM LT TE FLAP CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 3733 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND NR 2 FLAP TRACK UPPER AFT MOUNT CORRODED. REPAIRED PER ER 2-57-40-13. (M) 2L72 4F RTA16WE 19951106005191995110600519NM 1995 11 6 AWXA9500698 119951004A5314 KEEL BEAM BOEING737 737277 1384570NM BS 663-727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND FUSELAGE LOWER LOBE BL 0 SKIN PANEL AT KEEL BEAM BETWEEN WHEEL WELLS STATION 663 TO STATION 727 CRACKED IN SEVERAL AREAS. FABRICATED KEEL BEAM PANEL AND INSTALLED PER SRM 51-30-2. (M) 2L72 4F RTA16WE 19951106005201995110600520NM 1995 11 6 AWXA9500699 119951004A5313 STRINGER BOEING737 737277 1384570NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28188AW 22655 PHX - DURING SCHEDULED C8 INSPECTION, FOUND CRACK IN LEFT STRINGER 18A SHEAR BEAM AT BS 727. REPAIRED PER EO 53-14-09. (M) 2L72 4F RTA16WE 19951106005211995110600521NM 1995 11 6 AWXA9500700 119951012A523010608214 SEAL BOEING737 73733A 1384673NM AFT CARGO DOOR TORN A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28169AW 23630 PHX-OAK - FLT NR 577 - CABIN WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AFT CARGO DOOR SEAL TORN AT LOWER FORWARD CORNER. MAINTENANCE REMOVED AND REPLACES SEAL PER BMM 52-31-12. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951106005221995110600522NM 1995 11 6 AWXA9500701 119951013A3350900835A EEL BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 9 THROUGH ROW 13. REMOVED AND REPLACED BATTERY PACK AT ROW 11, OPS CHECK GOOD. (M) 2L72 4F A16WE 19951106005231995110600523NM 1995 11 6 AWXA9500702 119951014A3350 EEL WIRE BOEING757 757225 1384959NM L1 DOOR BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28915AW 22209 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE IN FIRST CLASS SECTION. REPAIRED BROKEN WIRE AT L1 DOOR, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951106005241995110600524SW 1995 11 6 BDHA9500021 119950921A7331 FUEL LINE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE LOOSE A BDHAK NONE K FLUID LOSS ININSP/MAINT 1 GL15329BA TC238 P54118 BIS - FLT NR 421 - CREW REPORTED, THE LEFT ENGINE WAS DRIPPING FUEL OUT OF COWLING. MAINTENANCE PERSONNEL INSPECTED THE ENGINE AND FOUND THE LINE TO THE FUEL FLOW TRANSMITTER WET WITH FUEL. THE LINE WAS TIGHTENED AND ENGINE RUN AND LEAK CHECK PERFORMED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T4 T A8SW E4WE 19951106005251995110600525SW 1995 11 6 BDHA9500022 119950927A3230NAS110424 BOLT SWRNGNSA226 SA226TC 8780404SW RT MLG BROKEN A BDHAO OTHER J WARNING INDICATION CRCRUISE 1 GL15329BA TC238 BIS - FLT NR 421 - CREW REPORTED, THE RIGHT MAIN LANDING GEAR INDICATED DOWN IN FLIGHT AND THE AIRCRAFT HAD A YAW TO THE RIGHT. THE AIRCRAFT LANDED AND INSPECTION REVEALED THAT THE RIGHT UPLOCK ROLLER AND ATTACHMENT BOLT WERE MISSING, CAUSING THE RIGHT GEAR TO NOT LOCK UP. ALSO, THE UPLOCK SWITCHES WERE DAMAGED CAUSING THE HYDRAULIC POWER TO BE CUT OFF FROM THE LANDING GEAR SYSTEM, LETTING THE RIGHT GEAR FALL TO THE DOWN AND LOCK POSITION. BOTH RIGHT UPLOCK SWITCHES AND THE UPLOCK ROLLER WERE REPLACED. A GEAR RETRACTION TEST WAS COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 1L72 4T A8SW 19951106005261995110600526NM 1995 11 6 CKSA95106 119951012A2612897080 FIRE WARN CARD BOEING747 747132 1384882NM APU SHORTED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74607 20247 KLAX - APU 'A' LOOP FIRE DETECTOR FLICKERS IN FLIGHT. REMOVED AND REPLACED FIRE WARNING CONTROL CARD AND FIRE DETECTOR CONTROL CARD FOR APU 'A' LOOP SYSTEM. OPS CHECK GOOD IAW B747 MM 26-10-00 AND 26-15-00. DMI NR 248 CLEARED/PLACARD REMOVED. (M) 2L74 4F A20WE 19951106005271995110600527WP 1995 11 6 HALA95135 119951008A3350P4010049 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 9171 47764 HNL - FORWARD HALF OF EMERGENCY FLOOR LIGHTS DO NOT WORK. REPLACED FLOOR LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106005281995110600528WP 1995 11 6 HALA95136 119951007A335060030431 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 12060 48122 CEILING EMERGENCY LIGHTS FROM ROW 7-11 ARE INOPERATIVE. REPLACED EMERGENCY CEILING LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951106005291995110600529WP 1995 11 6 ORJA88 119950929A332041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC987 3022087WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11751RA 49779 EMERGENCY LIGHTS, ON THE FORWARD OVER THE WING EXIT LIGHTS, DO NOT ILLUMINATE WITH EMERGENCY POWER ON. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK GOOD. (M) 2L72 4F RTA6WE 19951106005301995110600530NE 1995 11 6 SIMA952912 319951018A61116607132886 PROP BLADE SAAB SF340 SF340A 7850100EU ROTOL R389 R3894123F25 NE NR 2 RT ENG CRACKED ASASIMAK NONE O OTHER ININSP/MAINT 1 SW21109AE 340A109 CW1157 LAW - PROP DOWTY MODEL R3894-123-F25, S/N CW1157, WAS REMOVED FROM AIRCRAFT FOR SLINGING GREASE. DURING SHOP TEARDOWN, NR 2 BLADE P/N 6607132886/ S/N SF340-132-1530, WAS FOUND TO HAVE A CRACK OF APPROX 5.5 INCHES LONG IN THE AREA BETWEEN THE COUNTER WEIGHT MOUNTING PAD AND THE ROLLER BEARING AREA ON THE BLADE SHANK. BLADED WAS REMOVED FROM SERVICE AND SENT TO DOWTY FACILITIES FOR EVALUATION. (M) 2L72 4T RTA52EU 6 CP30NE 19951106005311995110600531SO 1995 11 6 SRAA109507 119951009A7312UA5242401 FUEL HEATER LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 3 ENG DEFECTIVE A SRAAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO19906SJ 4477 ON CLIMB-OUT FOR FLIGHT ADN5 OUT OF MIA, NOTICED OIL QUANTITY STARTED TO DROP AFTER LEVELING OFF, OIL COULD BE SEEN COMING OUT OF DRAIN MAST. SHUT DOWN NR 3 ENGINE AND COMPLETED AIR TURN BACK TO MIA. FOUND FUEL HEATER STRAINER DEFECTIVE, REPLACED UNIT, PERFORMED OPS CHECK AND LEAK CHECK, OPERATED NORMAL PER MM CH 73. (M) 2H74 4T4 T A1SO E282 19951106005321995110600532EU 1995 11 6 USAA951049 119951006A3230H0643 CONNECTOR FOKKERF28 F28MK4000 4990810EU LT MLG WW BENT PIN A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19482US 11231 CLT - FLT NR 0578 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. USED OVERIDE BUTTON TO RETRACT LANDING GEAR. FOUND PIN IN CONNECTOR CM62 BENT. STRAIGHTENED PIN AND RECONNECTED CONNECTOR, SYSTEM TEST NORMAL PER CHAP 32 AND CHAP 27 IN MM. (M) 2L72 4F RTA20EU 19951106005331995110600533NM 1995 11 6 USAA951050 119950929A5313 STRINGER BOEING737 737201 1384454NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19263AU32606 22869 ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 12 INCHES, STRINGER 27L AT BSL 967. INSTALLED STRINGER SPLICE PER SRM 53-10-3. REPAIRED PER SRM 53-10-3, FIG 1. (M) 2L72 4F A16WE 19951106005341995110600534NM 1995 11 6 USAA951089 119950918A5313 STRINGER BOEING737 737201 1384454NM BS 350-360 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19240AU 22355 CLT - DURING A PCI INSPECTION, FOUND CORROSION 10 INCHES BY 1 INCH ON STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. CORROSION TASK NR C53-202-02/PCI 1227, CORROSION LEVEL 2. REPLACED END STRINGER 28R, RBL 6. (M) 2L72 4F A16WE 19951106005351995110600535EU 1995 11 6 USAA951096 119951012A3350363674 EEL STRIP FOKKERF28 F28MK0100 4990807EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19865US 11308 IND - FLT NR 301 - EMERGENCY FLOOR LIGHTING IN FIRST CLASS WAS REPORTED AS INOP. REPLACED EMERGENCY FLOOR LIGHTING LAMP STRIP. (M) 2L72 4F RT 19951106005361995110600536EU 1995 11 6 VTZA96009 119951016A7933MS280343 OIL TEMP BULB BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27493UE 805 FLT NR 6352 - IAD-SWF - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL TEMP RUNNING HIGH. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED OIL TEMP BULB. ALL OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951106005371995110600537WP 1995 11 6 WTAA950283 219951018A75308961153 GASKET BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RT ENGINE BLOWN A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17430UE 784 FAT - RIGHT ENGINE TORQUE AND EGT FLUCTUATION REPORTED DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE P3 BLANKING CAP GASKET. ENGINE PERFORMANCE REPORTED NORMAL DURING GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19951106005381995110600538EU 1995 11 6 WTAA950284 119951018A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG BROKEN WIRE A WTAAO OTHER P NO WARNING INDICATION APAPPROACH 1 WP17413UE 797 LAX - RIGHT MAIN LANDING GEAR INTRANSIT LIGHTS FAILED TO ILLUMINATE ON GEAR EXTENSION. MAINTENANCE REPAIRED BROKEN WIRE AT RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951106005391995110600539NM 1995 11 6 95ZZZM595 119950909A3350 CONNECTORS BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 12 THROUGH 16 AND ROW 27 AFT. SPLICED BROKEN WIRES AT ROWS 14-15, AND RECONNECTED LOOSE CONNECTORS AT ROWS 13, 27 AND AT THE AFT LAVATORY DOOR. REFERENCE ASAA9540050. 2L72 4F RTA16WE 19951106005401995110600540NM 1995 11 6 95ZZZM596 119950903A3350S417N5048 EEL ASSY BOEING737 737490 1384715NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - ON ARRIVAL OF FLT NR 103, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 10 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND REPLACED LIGHT ASSEMBLY AT ROW 11 AND LIGHTS OPERATED NORMALLY. REFERENCE ASAA9540049. 2L72 4F RTA16WE 19951106005411995110600541NM 1995 11 6 95ZZZM597 119950911A215039613211 PACK SHUTOFF VLV BOEING737 737210C 1384459NM RT PACK LEAKING A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01744AS11159 21822 OME - AIR TURN BACK OF FLT NR 58, CREW REPORTED SMOKEY ODOR IN CABIN DURING CLIMB-OUT. REPLACED RIGHT AIR CONDITIONING PACK SHUTOFF VALVE AND MIX CHAMBER AND OPERATED NORMALLY. REFERENCE NR ASAA9510085. 2L72 4F A16WE 19951106005421995110600542NM 1995 11 6 95ZZZM598 119950916A3350 EEL WIRING BOEING737 7374Q8 NM MAIN CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 19-22 WERE FOUND INOPERATIVE. RELAMPED DEFECTIVE LIGHT AND RECONNECTED WIRING. LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9540054. 2L72 4F RTA16WE 19951106005431995110600543NM 1995 11 6 ASAA9510082 119950901A3350900835A EEL BATT PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 20. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005441995110600544NM 1995 11 6 ASAA9510083 119950907A335020131A EEL BATTERY BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 17 AND 18 WERE FOUND INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19951106005451995110600545NM 1995 11 6 ASAA9510084 119950911A5210 MECHANISM BOEING737 737298C 1384490NM L-1 DOOR OUT OF ADJUST A ASAAO OTHER O OTHER TXTAXI/GRND HDL 1 NM01745AS 20794 ANC - FLT NR 59 - CREW REPORTED L-1 DOOR REQUIRES EXCESSIVE FORCE TO OPEN TO CLOSE. ADJUSTED L-1 DOOR AND LUBED MECHANISM AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005461995110600546NM 1995 11 6 ASAA9510085 119950911A2150657894710 MIX CHAMBER BOEING737 737210C 1384459NM RT PACK LEAKING A ASAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM01744AS 21822 OME - AIR TURN BACK OF FLT NR 58, CREW REPORTED SMOKEY ODOR IN CABIN DURING CLIMB-OUT. REPLACED RIGHT AIR CONDITIONING PACK SHUTOFF VALVE AND MIX CHAMBER AND OPERATED NORMALLY. (M) 2L72 4F A16WE 19951106005471995110600547NM 1995 11 6 ASAA9510086 119950914A253062000121 OVEN BOEING737 737290C 138448VNM NR 1 GALLEY DEFECTIVE A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM01730AS20341 22577 ANC - ON ARRIVAL OF FLIGHT 58, CREW REPORTED A STRONG ELECTRICAL ODOR EMINATED FROM OVEN IN FORWARD GALLEY WHILE IN USE. ODOR DISSIPATED WHEN GALLEY POWER TURNED OFF. REMOVED AND REPLACED DOUBLE OVEN IN NR 1 GALLEY AND OPERATED NORMALLY WITH NO ODORS NOTED. (M) 2L72 4F A16WE 19951106005481995110600548NM 1995 11 6 ASAA9510087 119950918A3350900835A EEL BATT PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01742AS 23136 ANC - DURING MAINTENANCE CHECK, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS FLASHED ON AND OFF WHEN ACTIVATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19951106005491995110600549NM 1995 11 6 ASAA9510088 119950918A3350900835A EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - PRIOR TO DEPARTURE OF FLIGHT NR 7831, CREW REPORTED ONE SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS IN MAIN CABIN WERE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005501995110600550NM 1995 11 6 ASAA9540049 119950903A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - ON ARRIVAL OF FLT NR 103, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 10 TO 13 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND REPLACED LIGHT ASSEMBLY AT ROW 11 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005511995110600551NM 1995 11 6 ASAA9540050 119950909A3350 EEL WIRING BOEING737 7374Q8 NM CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 12 THROUGH 16 AND ROW 27 AFT. SPLICED BROKEN WIRES AT ROWS 14-15, AND RECONNECTED LOOSE CONNECTORS AT ROWS 13, 27 AND AT THE AFT LAVATORY DOOR. (M) 2L72 4F RTA16WE 19951106005521995110600552NM 1995 11 6 ASAA9540051 119950909A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AFT OF ROW 27. RECONNECTED WIRE HARNESS IN TWO PLACES AFT OF ROW 27 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005531995110600553NM 1995 11 6 ASAA9540054 119950916A3350303 EEL LAMP BOEING737 7374Q8 NM MAIN CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 19-22 WERE FOUND INOPERATIVE. RELAMPED DEFECTIVE LIGHT AND RECONNECTED WIRING. LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005541995110600554NM 1995 11 6 ASAA9540055 119950916A3350 EEL CONNECTION BOEING737 7374Q8 NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 SEA - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTION AT FOURTH LIGHT AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005551995110600555NM 1995 11 6 ASAA9540056 119950916A3350 EEL CONNECTOR BOEING737 737490 1384715NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RECONNECTED LOOSE CONNECTOR AT SECOND FROM LAST RED LIGHT AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005561995110600556NM 1995 11 6 ASAA9540057 119950917A3350 EEL CONNECTOR BOEING737 737490 1384715NM CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN THE AFT CABIN. RECONNECTED LOOSE CONNECTOR AT SECOND FROM LAST RED LIGHT AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951106005571995110600557NM 1995 11 6 ASAA9540058 119950920A3241 ANTI-SKID LIGHT BOEING737 7374Q8 NM LANDING GEAR OUT OF ADJUST A ASAAO OTHER N FALSE WARNING CLCLIMB 1 NM01783AS 25114 SEA - FLT NR 479 - CREW REPORTED, ANTI-SKID INOP LIGHT ILLUMINATED AFTER GEAR RETRACTION WITH GEAR HANDLE IN UP OR OFF POSITIONS. CYCLED GEAR AND LIGHT EXTINGUISHED WITH GEAR DOWN. ILLUMINATED WITH GEAR UP. LIGHT FINALLY EXTINGUISHED PASSING 20,000 FEET. LANDED WITHOUT INCIDENT. INSPECTED SYSTEM AND PERFORMED ADJUSTMENT/TEST PER THE MAINTENANCE MANUAL. SYSTEM CHECKED NORMAL. (M) 2L72 4F RTA16WE 19951106005581995110600558 1995 11 6 ASAA9580188 419950821A2565D29982107 EVAC SLIDE DOUG DC9 DC983 3022083WP R1 DOOR FAILED TEST A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01939AS 49657 OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE EMERGENCY LIGHTS FAILED TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2L72 4F RTA6WE 19951106005591995110600559WP 1995 11 6 ASAA9580194 119950829A3230KP3AL BEARING DOUG DC9 DC982 3022082WP LANDING GEAR WORN A ASAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01951AS 49111 SEA - AIR TURN BACK OF FLT NR 540, CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDED WITHOUT INCIDENT. REPLACED WORN BEARING IN PEDAL STEERING OVERRIDE CAM FOLLOWER. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951106005601995110600560WP 1995 11 6 ASAA9580195 119950902A33500105610001 EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA - ON ARRIVAL OF FLT 467 - CREW REPORTED NUMEROUS EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE IN FORWARD CABIN. REPLACED LIGHT ASSEMBLY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951106005611995110600561WP 1995 11 6 ASAA9580196 119950904A3350S103 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01953AS 49386 SEA - DURING MAINTENANCE CHECK, ONE TAILCONE EMERGENCY LIGHT AND TWO AFT CABIN OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951106005621995110600562WP 1995 11 6 ASAA9580197 119950915A5210 HOLD OPEN LATCH DOUG DC9 DC983 3022083WP L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01965AS 53079 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE. ADJUSTED HOLD OPEN LATCH AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951106005631995110600563WP 1995 11 6 ASAA9580198 119950916A33501001191 PORTABLE EEL DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01958AS23217 53024 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951106005641995110600564WP 1995 11 6 ASAA9580200 119950919A5320 SPLICE STRAP DOUG DC9 DC983 3022083WP Y1174 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS14825 53018 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME SPLICE STRAP AT Y1174, X PLUS 24, Z-44. REMOVED CORRODED STRAP AND INSTALLED NEW SPLICE STRAP IAW DC-9 SRM 51-01, 51-10-03 AND 51-30-05. (M) 2L72 4F RTA6WE 19951106005651995110600565WP 1995 11 6 ASAA9580207 119950927A5210 LOCKING MECH DOUG DC9 DC983 3022083WP L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01943AS 53018 SEA - ON ARRIVAL OF FLT 595, CREW REPORTED THE L1 DOOR DIFFICULT TO LOCK CLOSED FROM INSIDE. LUBED LOCKING MECHANISM AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951106005661995110600566WP 1995 11 6 ASAA9580211 119951004A5311 FRAME DOUG DC9 DC983 3022083WP Y1271 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, X PLUS 19 TO X-19. CORROSION REMOVAL FROM X PLUS 19 TO X-14 WAS WITHIN LIMITS, X-14 TO X-19 WAS OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-20-00, 51-30-02 AND 53-03. (M) 2L72 4F RTA6WE 19951106005671995110600567WP 1995 11 6 ASAA9580212 119951004A5320 SHEAR TIE DOUG DC9 DC983 3022083WP Y1079 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE FASTENERS AT Y1079, Z-69 LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05, 53-01 AND 53-03. (M) 2L72 4F RTA6WE 19951106005681995110600568WP 1995 11 6 ASAA9580213 119951004A5320 SHEAR TIE DOUG DC9 DC983 3022083WP Y1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AND SHEAR TIE FASTENERS AT Y1231, X PLUS 12 TO X-7, Z-50. CORROSION REMOVAL ON FRAME FROM X PLUS 12 TO X-7 WAS WITHIN LIMITS, X-7 WAS OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-10-04 AND 53-01. (M) 2L72 4F RTA6WE 19951106005691995110600569WP 1995 11 6 ASAA9580214 119951004A5320 CHANNEL DOUG DC9 DC983 3022083WP Y1211-Y1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL CHANNEL AT Y1211 TO Y1212, X-3, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-04. (M) 2L72 4F RTA6WE 19951106005701995110600570WP 1995 11 6 ASAA9580215 119951004A5320 SUPPORT DOUG DC9 DC983 3022083WP Y769-Y788 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK SUPPORT NUTPLATE AT Y769 TO Y788, X-16, Z-46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-60-00 AND 53-01. (M) 2L72 4F RTA6WE 19951106005711995110600571WP 1995 11 6 ASAA9580219 119951006A5320 SHEAR TIE DOUG DC9 DC982 3022082WP Y1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AND SHEAR TIE AT Y1212, X-1, Z-50. CORROSION REMOVAL ON SHEAR TIE WAS OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-05, 53-14-03 AND 53-01. (M) 2L72 4F A6WE 19951106005721995110600572NM 1995 11 6 AWXA9500676 119950928A5320 CLIP BOEING737 737277 1384570NM L1 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND L1 DOOR AFT GIRT BAR ATTACH CLIP CORRODED. REMOVED AND REPLACED CLIP PER SRM 51-10-1 AND SRM 51-30-2. (M) 2L72 4F RTA16WE 19951106005731995110600573NM 1995 11 6 AWXA9500677 119950928A53156030577075T73 FLOOR BEAM BOEING737 737277 1384570NM BS 344 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND CABIN FLOOR BEAM TOP CHORD CORRODED AT FASTENER HOLE, STATION 344 LBL 50. INSTALLED REPAIR AND NEW T-CAP PER SRM 51-40-4 AND SRM 51-30-2 FIGURE 10. (M) 2L72 4F RTA16WE 19951106005741995110600574NM 1995 11 6 AWXA9500678 119950928A5210 DKIN BOEING737 737277 1384570NM L2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND CRACK IN L2 DOOR SKIN UPPER HINGE CUTOUT LOWER AFT CORNER. FABRICATED AND INSTALLED DOUBLER REPAIR PER ER 2-52-11-09. (M) 2L72 4F RTA16WE 19951106005751995110600575NM 1995 11 6 AWXA9500679 119950928A53206720381 GUSSETT BOEING737 737277 1384570NM BS 178 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND 2.5 INCH CRACK IN GUSSET AT STATION 178 STRINGER 18L. CRACK CONFIRMED WITH EDDY CURRENT. REMOVED AND REPLACED GUSSET PER SRM 51-30-2 AND SRM 51-10-11. (M) 2L72 4F RTA16WE 19951106005761995110600576NM 1995 11 6 AWXA9500680 119950928A5330 SKIN BOEING737 737277 1384570NM BS 188 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND EXTERNAL SKIN CRACKED AT STATION 188, ABOVE RADOME AFT EDGE. ROUTED OUT CRACK PER SRM 51-30-6. (M) 2L72 4F RTA16WE 19951106005771995110600577NM 1995 11 6 AWXA9500681 119950928A5314 KEEL PANEL BOEING737 737277 1384570NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28180AW 22647 PHX - DURING SCHEDULED C14 INSPECTION, FOUND KEEL BEAM PANEL CRACKED ON RT SIDE AT STATION 727. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR PER ER 2-53-15-29. (M) 2L72 4F RTA16WE 19951106005781995110600578EU 1995 11 6 AWXA9500683 119951003A3350321452 EEL BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28622AW 054 PHX - DURING ROUTINE MAINTENANCE CHECK, L1 DOOR AND LEFT BATTERY PACK FAILED TEST. REMOVED AND REPLACED LEFT BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19951106005791995110600579NE 1995 11 6 AWXA9500686 219951102A7250761392 NR 6 HEAT SHIELD BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A AWXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28183AW 22650 P7029793 ABQ- FLT 343 - EN ROUTE IAH-LAS, THE NR 2 ENGINE OIL QUANTITY BEGAN DECREASING RAPIDLY. CREW ELECTED TO DIVERT AIRCRAFT TO ABQ. AIRCRAFT ARRIVED AT GATE WITHOUT FURTHER INCIDENT. MAINTENANCE NOTED LESS THAN 1 QT OIL ON QUANTITY GAUGE, AND ALSO FOUND A PUDDLE OF OIL IN EXHAUST DUCT. MAINTENANCE ELECTED TO CHANGE ENGINE. TEARDOWN OF ENGINE FOUND FOD IMPACTED THE NR 6 BEARING HEAT SHIELD CAUSING IT TO CRACK AND COME INTO CONTACT/CHAF THE NR 6 BEARING PERSSURE TUBE. (M) 2L72 4F4 FRTA16WE E2EA 19951106005801995110600580EU 1995 11 6 AWXA9500687 119951008A3350321452 EEL BATT PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28625AW 064 PHX - DURING ROUTINE MAINTENANCE CHECK, RT CABIN EEL BATTERY FAULTED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19951106005811995110600581NE 1995 11 6 EISA95290 219951007A73217436024 FUEL CONTROL BOEING727 727221 1384071NM PWA JT8 JT8D17R 52049NE NR 3 ENGINE FAILED A AEISAEA ENGINE SHUTDOWN UNSCHED LANDING EPKVIBRATION/BUFFET NO WARNING INDICATION FLUID LOSS CLCLIMB 1 SW07368PA 66499 22540 NR 3 ENGINE QUIT AT 800 FEET AFTER TAKEOFF, NO WARNING, SHUTTERED AND QUIT. REMOVED AND REPLACED NR 3 ENGINE FUEL CONTROL IAW 73-21-1. OPS AND LEAK CHECK GOOD IAW 72-00. TRIMMED NR 3 ENGINE IAW 71-00-97. (M) 2L73 4F4 F A3WE E2EA 19951106005821995110600582EU 1995 11 6 RAIA951003 119951001A3350W220103924 EEL WIRE AEROSPATR42 ATR42300 8680920EU CABIN BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03425TE14624 125 STL - FLT NR 7118 - EMERGENCY ESCAPE LIGHT BY AFT CARGO DOOR INOP. MAINTENANCE REPAIRED BROKEN WIRE, LIGHT CHECK GOOD. (M) 2H72 4T RTA53EU 19951106005831995110600583EU 1995 11 6 RAIA951004 119950930A3240215492 BRAKE AEROSPATR42 ATR42300 8680920EU RT MLG REQ'D SERVICE A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE032FOR 4500 904 199 STL - FLT NR 7231 - RIGHT BRAKE LIGHT EXCESSIVELY SENSITIVE AND GRABS RESULTING IN ERRATIC BRAKING. MAINTENANCE BLED BRAKES. TAXI CHECK GOOD. (M) 2H72 4T RTA53EU 19951106005841995110600584EU 1995 11 6 RAIA951006 119951002A77128974764 EGT COMPENSATOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE MALFUNCTIONED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03425AM134127412 870 STL - FLT NR 7309 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT EGT COMPENSATOR AND ADJUSTED TO GARRETT DSC SETTINGS. GROUND RUNS CHECK OK. (M) 2L72 4T RTA56EU 19951106005851995110600585EU 1995 11 6 RAIA951007 119951004A33503011151 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03425TE7629 1598 125 STL - AFT FLOOR EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED AFT EMERGENCY LIGHT POWER SUPPLY. (M) 2H72 4T RTA53EU 19951106005861995110600586EU 1995 11 6 RAIA951008 119951004A3240S2728117820000 FEED BACK SPRING AEROSPATR42 ATR42300 8680920EU RT BRAKE FAULTY A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE032FOR 11711 199 STL - FLT NR 7487 - RIGHT BRAKE IS SOFT EXCESSIVE TRAVEL THEN BITES HARD. MAINTENANCE REPLACED RIGHT BRAKE FEED BACK SPRING. TAXI CHECK GOOD. (M) 2H72 4T RTA53EU 19951106005871995110600587EU 1995 11 6 RAIA951010 119951006A733441SG107100GH TRANSDUCER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03426AM10206 874 66297 STL - FLT NR 7464 - FUEL PRESSURE AND FUEL FLOW FLUCTUATES. MAINTENANCE REPLACED LEFT FUEL PRESSURE TRANSMITTER AND LEFT FUEL FLOW TRANSDUCER. GROUND RUN CHECK GOOD. TRANSMITTER P/N TNAS1024L1182, TOTAL TIME 2823, TIME SINCE OVERHAUL 449. (M) 2L72 4T4 TRTA56EU E4WE 19951106005881995110600588EU 1995 11 6 RAIA951011 119951006A3350W220103924 EEL WIRE AEROSPATR42 ATR42300 8680920EU CABIN BROKEN A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 11753 199 MX - LIGHT OUT AT MID CABIN ON CABIN EMERGENCY ESCAPE PATH LIGHTING. MAINTENANCE REPAIRED BROKEN WIRE ON EMERGENCY LIGHTS AT LEFT MID CABIN ROW 8AB. (M) 2H72 4T RTA53EU 19951106005891995110600589EU 1995 11 6 RAIA951012 119951009A7921L8602328 OIL COOLER JETAIRJETSTMJETSTM4101 1500501EU RT ENG FAILED A RAIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE03550HK2012 41039 STL - FLT NR 7534 - RIGHT ENGINE LOST OIL PRESSURE, CREW SHUT ENGINE AND LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE OIL COOLER ASSEMBLY. GROUND RUNS LEAK CHECK GOOD. (M) 2L72 4T RTA41NM 19951106005901995110600590EU 1995 11 6 RAIA951013 119951009A75008961153 GASKETS BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENG LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03434AM8503 2403 887 66139 STL - FLT NR 7304 - LEFT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE BLEED AIR GASKETS. GROUND PERFORMANCE RUNS REVEALED NORMAL ENGINE PARAMETERS. (M) 2L72 4T4 TRTA56EU E4WE 19951106005911995110600591GL 1995 11 6 SRAA109506 219951007A7250 BEARING LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL NR 3 ENGINE FAILED A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19909SJ 4763 42689 DURING FLIGHT AD73, NR 3 ENGINE LOST OIL PRESSURE, SHUT DOWN ENGINE AND LANDED AT CHS SAFELY. FOUND NR 3 ENGINE HAD TURBINE BEARING FAILURE, REPLACED NR 3 ENGINE AND PERFORMED ENGINE RUN UP, OPS CHECKED GOOD PER J/C 6101, 6104, 7103 AND 7001, 7002. (M) 2H74 4T4 T A1SO E282 19951106005921995110600592 1995 11 6 WTAA950279 419951005A3420 COMPASS SYSTEM BAG JETSTMJETSTM3101 1500215EU COCKPIT MALFUNCTIONED A WTAAA UNSCHED LANDING O OTHER CRCRUISE 1 WP17418UE 780 FAT - AIRCRAFT DIRECTIONAL HEADING REPORTED OFF DURING CRUISE FLIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AVIONICS INSPECTED AND TESTED COMPASS SYSTEM AND NAVIGATION SYSTEM. NO DEFECTS NOTED. UNABLE TO DUPLICATE REPORTED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951106005931995110600593EU 1995 11 6 WTAA950280 119951004A73128070306 FUEL CONTL UNIT BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17420UE 788 SMF - RIGHT ENGINE TORQUE LIMITED AT 65 PERCENT TO 70 PERCENT DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL UNIT. RIGHT ENGINE OPERATIONAL CHECK NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19951106005941995110600594SO 1995 11 6 WTAA950281 119951009A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17120AM 120012 SFO - TAKEOFF TRIM WARNING INDICATION ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951106005951995110600595SO 1995 11 6 WTAA950282 119951010A3230922FS2A6NZ735 PROXIMITY SENSOR EMB 120 EMB120RT SO LT MLG SHORTED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17276UE 120067 SFO - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR SHOCK ABSORBER PROXIMITY SENSOR. GEAR RETRACTON SYSTEM OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951106006361995110600636WP 1995 11 6 9516989935 119951030A2810 FUEL CAP DOUG DC9 DC931 3022065WP LT WING MISSING A NWAAA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 GL011332U 47404 DURING CLIMB, FUEL WAS LEAKING FROM THE TOP OF THE LEFT WING. THE AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. FOUND LEFT OVERWING CAP MISSING. INSTALLED CAP. LEAK CHECK GOOD. 2L72 4F A6WE 19951106006371995110600637WP 1995 11 6 9516999903 119951029A2720 THROW LIMITER DOUG DC9 DC931 3022065WP RUDDER OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01953N 47083 DURING TAKEOFF, FLAP/RUDDER STOP LIGHT ILLUMINATED. CREW ABORTED TAKEOFF. ADJUSTED AUXILIARY RUDDER THROW LIMITER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106006381995110600638WP 1995 11 6 9517009918 119951027A2780 RETRACT MECH DOUG DC9 DC932 3022066WP LE FLAPS LACK OF LUBE A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01940N 47572 ON APPROACH DURING SLAT EXTENSION, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED SLATS AND LUBRICATED SLAT ROLLERS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106006391995110600639 1995 11 6 9517019755 419951027A344220671570153 TRANSCEIVER DOUG DC9 DC941 302207NWP RADAR SYST FAILED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01755NW7510 151 47179 DURING CRUISE, THE WEATHER RADAR WOULD NOT PAINT LEVEL FIVE WEATHER BEYOND THIRTY MILES AND INSIDE THIRTY MILES. THE WEATHER RADAR WOULD PAINT A DIFFERENT PICTURE EVERY SWEEP. AIRCRAFT DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. REPLACED THE RADAR TRANSCEIVER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106006401995110600640 1995 11 6 9517029869 419951021A2211 ROLL AXIS COMP DOUG DC9 DC951 3022051WP AUTO PILOT MALFUNCTIONED A NWAAO OTHER F FLT CONT AFFECTED CRCRUISE 1 GL01778NC 48100 DURING CRUISE, THE RUDDER DEFLECTED TO THE RIGHT CAUSING THE AIRCRAFT TO ROLL. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE AUTOPILOT ROLL AXIS COMPUTER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106006411995110600641WP 1995 11 6 9517039935 119951028A3350 BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL011332U 47404 DURING LINE CHECK, FOUND EMERGENCY EXIT SIGNS OVER FORWARD EMERGENCY EXITS INOPERATIVE. REPLACED THE BATTERIES AND POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951106006421995110600642NE 1995 11 6 9517049987 219951030A7230 COMPRESSOR DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01987US 47458 FLIGHT EXPERIENCED A COMPRESSOR STALL ON TAKEOFF ROLL (ENGINE POSITION UNDETERMINED). THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES AND FOUND NO DISCREPANCIES. SUSPECT THIS EVENT WAS DUE TO SNOW AND SLUSH INGESTION. 2L72 4F4 F A6WE E2EA 19951106006431995110600643NM 1995 11 6 9517056622 119951031A2612 FIRE WARNING BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 3 ENGINE ACTIVATED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 GL01622US 21704 702240 DURING CLIMB, THE NR 3 ENGINE EXPERIENCED HIGH NACELLE TEMPERATURES FOLLOWED BY A FIRE WARNING. POWER WAS REDUCED TO IDLE AND THE NACELLE TEMPERATURES RETURNED TO NORMAL. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO NRT WHERE AN UNEVENTFUL THREE-ENGINE LANDING WAS ACCOMPLISHED. THE FIRE BOTTLES WERE NOT DISCHARGED, NO FUEL WAS DUMPED, AND NO EVIDENCE OF FIRE WAS FOUND. THE HIGH-STAGE BLEED VALVE WAS LOCKED OUT AND A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19951106006441995110600644NM 1995 11 6 9517062283 119951101A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01283US 21322 DURING LINE CHECK, FOUND RIGHT WING EMERGENCY LIGHT OUT, AFT GALLEY EMERGENCY LIGHT OUT, EMERGENCY LIGHT ROW 3 OUT, AND VENTRAL STAIRWAY EMERGENCY LIGHT OUT. RELAMPED RIGHT WING LIGHT AND REPLACED BATTERY PACKS FOR GALLEY ROW 3 AND VENTRAL STAIRWAY. 2L73 4F A3WE 19951106006451995110600645NM 1995 11 6 9517076303 119951101A3350900835A BATTERY PACK BOEING747 747451 1384940NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK, THE UPPER DECK DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951106006461995110600646NM 1995 11 6 95FDEA01645 119951101A5313BAC149139 STRINGER BOEING727 72722 1384002NM BS 419 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 14084 GOUGE AND DENT ON STR 15L AT BS 419. 2L73 4F A3WE 19951106006471995110600647NM 1995 11 6 95FDEA01646 119951106A5313 STRINGER BOEING727 72722 1384002NM BS 560-570 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND STR 21L HAS MECHANICAL DAMAGE AT STA 560 TO 570 L/LT, FWD BAY. REPAIRED STR 21L AT BS 560 TO 570 PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951106006481995110600648NM 1995 11 6 95FDEA01647 119951101A5315BAC1505100146 FLOOR BEAM BOEING727 72722 1384002NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-224-02) AROUND NUTPLATE HOLES AT BS 312, LBL 29 - 18, WL 208.1. 2L73 4F A3WE 19951106006491995110600649NM 1995 11 6 95FDEA01648 119951101A5315BAC1518338 FLOOR BEAM BOEING727 72722 1384002NM BS 1050 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01 (3)) BETWEEN LOWER FLANGE OF FLOOR BEAM AND STRAP BS 1050, RBL 45 - LBL 30, WL 200. REPAIRED FLOOR BEAM BS 1050, LBL 17.5, WL 200, AS PER FEDEX SRM 53-10-08, FIG 8. 2L73 4F A3WE 19951106006501995110600650NM 1995 11 6 95FDEA01649 119951103A5320 DOUBLER BOEING727 72722 1384002NM BS 178 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR0046 RADOME INSTALLATION, FOUND UPPER SKIN PANEL DOUBLER, STA 178, CRACKED. 2L73 4F A3WE 19951106006511995110600651NM 1995 11 6 95FDEA01650 119951031A5314 KEEL BEAM BOEING727 727225 1384077NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION ON FWD BAY KEEL BEAM BS 720B +1 AND +9, RBL 7, WL 150. REMOVED CORROSION ON KEEL BEAM FLANGES AND REPAIRED PER FEDEX EA NR 7-5310-26107. ADDITIONAL CORROSION WAS DISCOVERED BENEATH A PREVIOUS REPAIR ON SKIN AROUND RAM AIR INLET ACTUATOR ACCESS DOOR. REMOVED PREVIOUS REPAIR AND REPAIRED DAMAGE PER FEDEX EA NR 7-5330-26134. 2L73 4F A3WE 19951106006521995110600652NM 1995 11 6 95FDEA01651 119951101A5313 STRINGER BOEING727 727225 1384077NM FUSELAGE CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 CORROSION IN SEVERAL PLACES IN STR AND TWO STR CLIPS AT BS 560, 568, AND 574, RBL 15, WL 150. REMOVED CORROSION, FABRICATED REPLACEMENT PARTS, AND INSTALLED PER FEDEX SRM 53-10-3 AND SRM 53-10-2. 2L73 4F A3WE 19951106006531995110600653NM 1995 11 6 95FDEA01652 119951101A5753 TRACK BOEING727 727225 1384077NM NR 5 TE FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 RT WING NR 5 FLAP TRACK AUXILIARY SPAR HAS A 1 INCH CRACK JUST ABOVE INBOARD AUXILIARY SPAR FLAP TRACK BOLT. REPAIRED PER FEDEX EA 7-5710-26103. 2L73 4F A3WE 19951106006541995110600654NM 1995 11 6 95FDEA01653 119951101A2841 FUEL QTY IND BOEING727 7272D4 138407UNM NR 1 TANK FAILED A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 SO25287FE 21849 UNRELIABLE FUEL QTY IND ON FUEL GAUGES AFTER TAKEOFF. FOUND NR 2 FUEL GAUGE IN NR 3 POSITION AND NR 3 FUEL GAUGE IN NR 2 POSITION. SWAPPED FUEL GAUGES TO NORMAL POSITION, A/C REQUIRED DEFUELING. DEFUELED AND SUMPED NR 1, NR 2 AND NR 3 FUEL TANKS. CALIBRATED NR 2 AND NR 3 FUEL TANKS PER MM 28-41-02. SYSTEM OK FOR SERVICE. FOUND NR 1 TANK TO BE BAD, NO TIME TO WORK. DEF NR 1 FUEL QTY SYSTEM ON A/C MX LOG 440478. 2L73 4F A3WE 19951106006551995110600655NM 1995 11 6 95FDEA01655 119951102A5330 SKIN BOEING727 72722 1384002NM BS 1324 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DENT IN SKIN BS 1324 BETWEEN STR 21 - 22L. REPAIRED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951106006561995110600656NM 1995 11 6 95FDEA01656 119951102A5330 SKIN BOEING727 72722 1384002NM BS 1238 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 GOUGE IN SKIN BS 1238 BETWEEN STR 17-18R. 2L73 4F A3WE 19951106006571995110600657NM 1995 11 6 95FDEA01657 119951102A5320 RT FORGING BOEING727 72722 1384002NM BS 740 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CRACK ON 740 FORGING RT BETWEEN STR 18-19R. REPAIRED CRACK ON 740 FORGING RT, BETWEEN STR 18-19R PER FEDEX EA 7-5310-26123. 2L73 4F A3WE 19951106006581995110600658NM 1995 11 6 95FDEA01658 119951102A5320 LT FORGING BOEING727 72722 1384002NM BS 740 CRACKS A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CRACKS ON STA 740 FORGING LT, THREE LOCATIONS BETWEEN STR 23-24L, BETWEEN STR 18-19L, AND BETWEEN STR 19-20L (FWD BAY). 2L73 4F A3WE 19951106006591995110600659NM 1995 11 6 95FDEA01660 119951102A5315 FLOORBEAM BOEING727 72722 1384002NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01-3), ON LOWER FLANGE OF FLOORBEAM BS 1110 FROM RBL 28 TO 31 WL 200. REMOVED AND REPLACED ENTIRE LOWER CHORD OF THE BS 1110 FLOORBEAM PER FEDEX EA 7-5310-28196. 2L73 4F A3WE 19951106006601995110600660NM 1995 11 6 95FDEA01661 119951102A5311 FRAME BOEING727 72722 1384002NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FRAME BS 720, WL 155, LBL 10 - RBL 10. REPAIRED PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951106006611995110600661NM 1995 11 6 95FDEA01662 119951102A5320 ANGLES BOEING727 72722 1384002NM BS 1030 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01-3), IN THE NUTPLATE HOLES, AFT BAY AT BS 1030 WL 200 FROM LBL 20 TO RBL 14. REMOVED CORROSION, FABRICATED NEW REPAIR ANGLE AND INSTALLED FASTENERS. ALL WORK DONE IAW FEDEX EA 7-5310-26152. 2L73 4F A3WE 19951106006621995110600662NM 1995 11 6 95FDEA01663 119951102A5313 STRINGER BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 IN THE AFT GLY AT BS 1050 LBL 60 WL 176, THERE IS A CRACK IN THE LOWER FLANGE OF STR 21 UNDER THE FAIL-SAFE CHORD. REPAIRED CRACKED STR AT BS 1050 LBL 60 WL 176 ON LOWER FLANGE OF STR 21L PER FEDEX SRM 53-10-3 FIG 1. THE FAIL-SAFE CHORD PER FEDEX SRM 51-40-4 FIG 2, WHICH WAS REMOVED TO GAIN ACCESS TO DAMAGED AREA ON STR 21L. 2L73 4F A3WE 19951106006631995110600663NM 1995 11 6 95FDEA01664 119951101A5311 FRAME BOEING727 727227 1384078NM BS 640 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FORWARD LOWER CARGO FUSE FRAME STA 640 CRACKED AT RBL 8 FLOOR STR ATTACH. STOP DRILLED ENDS OF CRACK, CONFIRMED CRACK ENDS AT STOP DRILL WITH DYE PENETRANT. INSTALLED REPAIR DOUBLER PER SRM 51-40-3. 2L73 4F A3WE 19951106006641995110600664NM 1995 11 6 95FDEA01665 119951029A5311 FRAME BOEING727 727227 1384078NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STA 680 ABOVE STR 6R FRAME CRACKED AT RIVET. 2L73 4F A3WE 19951106006651995110600665NM 1995 11 6 95UAL900244 119951102A2450941D335 CIRCUIT BREAKER BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE COCKPIT BURNED A UALAK NONE O OTHER ININSP/MAINT 1 WP29984UA3492 21642 FOUND BURNED AND MELTED WIRE INSULATION STARTING AT APU GENERATOR CIRCUIT BREAKER (C803) AND RUNNING APPROXIMATELY 18 INCHES INTO WIRE BUNDLE (BLUE AND YELLOW PHASES). REPLACED APU GENERATOR CIRCUIT BREAKER AND REPAIRED WIRING TO THE CIRCUIT BREAKER. RAN APU AND CHECKED BREAKER WITH HEAVY ELECTRICAL LOAD. CHECKS O.K. 2L72 4F4 F A16WE E2EA 19951106006661995110600666EU 1995 11 6 COMA9531183 119951031A3150004WS00 WEU SAAB SF340 SF340A 7850100EU AVIONICS COMPT DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01361CA115453 340A056 THE LEFT ENGINE AIR VALVE LIGHT ILLUMINATED DURING FLIGHT. REPLACED THE WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19951106006671995110600667EU 1995 11 6 COMA9531184 119951030A76035308211 POWER CONTL QUAD SAAB SF340 SF340A 7850100EU COCKPIT DEFECTIVE A COMAK NONE O OTHER LDLANDING 1 SO01380CA211543368 340A012 DURING LANDING AND ROLLOUT, THE RIGHT PROPELLER R.P.M. DETERIORATES TO 1100 R.P.M. REPLACED THE POWER CONTROL QUADRANT. 2L72 4T RTA52EU 19951106006681995110600668 1995 11 6 COMA9531185 419951030A34176224401001 ADC SAAB SF340 SF340A 7850100EU AVIONICS COMPT DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01356CA170342983 340A034 THE LEFT AIRSPEED INDICATOR FAILED. REPLACED THE AIR DATA COMPUTER. 2L72 4T RTA52EU 19951106006691995110600669EA 1995 11 6 COMA9560591 119951030A323017300221 WOW HARNESS CNDAIRCL600 CL6002B19 EA NLG DEFECTIVE A COMAK NONE O OTHER CLCLIMB 1 SO01938CA2871 7046 THE NOSE GEAR WAS VERY SLOW TO RETRACT. REPLACED THE N.L.G. RIGHT WEIGHT-ON-WHEELS HARNESS. 2L72 4F RTA21EA 19951106006701995110600670EA 1995 11 6 COMA9560592 119951030A76032100140003 GEARBOX CNDAIRCL600 CL6002B19 EA LT ENG BINDING A COMAK NONE O OTHER UKUNKNOWN 1 SO01946CA2650 2650 7072 THE LEFT ENGINE POWER LEVER IS BINDING AND CANNOT BE MOVED TO REVERSE THRUST POSITION. REPLACED THE THROTTLE CONTROL GEARBOX. 2L72 4F RTA21EA 19951106006711995110600671NM 1995 11 6 DL72K954150 119951030A3350 BATTERY PACK 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11474DA 00 20751 LEFT LOWER AFT BODY FAIRING E-PATH LIGHT INOP. REPLACED BATTERY PACK AT APPROX ROW 23ABC. E-PATH LIGHT CKS NORMAL. 2L73 4F A3WE 19951106006721995110600672NM 1995 11 6 DL72K954156 119951031A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11481DA 20861 R1 DR OVERHEAD E-PATH LIGHT INOP. REPLACED BATTERIES. CKS NORMAL. 2L73 4F A3WE 19951106006731995110600673NM 1995 11 6 DL72L954131 119951029A3350S106 BATTERY BOEING727 727232 1384082NM AFT AIRSTAIR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11502DA 21304 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERIES. CKS NORMAL. 2L73 4F A3WE 19951106006741995110600674NM 1995 11 6 DL72S954129 119951029A5751652176633 SKIN BOEING727 727232 1384082NM LT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING INSPECTION, FOUND LEFT OUTBOARD AILERON WITH DENTS IN UPPER SKIN. ACCOMPLISHED REPAIRS PER SRM 57-50 -5. 2L73 4F A3WE 19951106006751995110600675NM 1995 11 6 DL72S954134 119951030A523065569271 SKIN BOEING727 727232 1384082NM CARGO DOOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING INSPECTION, C-3 CARGO DOOR WAS FOUND WITH INNER SKIN PUNCTURED, REPAIRED PER SRM 52-00-3. 2L73 4F A3WE 19951106006761995110600676NM 1995 11 6 DL72S954143 119951030A5712 RIB BOEING727 727232 1384082NM RT WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND ON HMV, RIGHT WING STRINGER TO RIB FASTENER HOLE HAS CRACK INDICATION AT STA. 629, 3RD STRINGER FWD FROM AFT SPAR. STOP DRILLED CRACK PER M/M 57-13-0. 2L73 4F A3WE 19951106006771995110600677NM 1995 11 6 DL72S954144 119951024A5280 BUSHING BOEING727 727232 1384082NM STRUT DOOR MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND DURING HMV, NR 5 FLAP TRACK FWD STRUT DOOR HINGE BUSHING MISSING. REMOVED FWD FITTING AND MACHINE BORED PER M/M 57-43-0 AND INSTALLED BUSHING PER M/M 57-43-0. 2L73 4F A3WE 19951106006781995110600678NM 1995 11 6 DL72S954145 119951030A5713 STRINGER BOEING727 727232 1384082NM WS 656.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND DURING HMV, RT OUTER WING UPPER STRINGER TO RIB SHOWS CRACK INDICATION ON FASTENER HOLE AT W.S. 656.5, STRINGER 10. MANUFACTURED REPAIR DOUBLER PER M/M 57-13-0 AND INSTALLED DOUBLER PER M/M 57-13-0, PG. 801. 2L73 4F A3WE 19951106006791995110600679NM 1995 11 6 DL72S954146 119951014A53306554590 SKIN BOEING727 727232 1384082NM BS 720 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11529DA 21703 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUT-OUT AT THE FWD LT CORNER AND LT SIDE OF THE AFT EDGE. THE SKIN IS 0.168 INCH (MEASURED) CLAD 2024-T3 AND IS CHEM MILLED AROUND THE DOOR TO 0.085 INCH (MEASURED). ACCOMPLISHED REPAIRS PER DL ERA 302626-14. 2L73 4F A3WE 19951106006801995110600680NM 1995 11 6 DL72W954132 119951019A5330 SKIN BOEING727 727247 138408FNM AIR STAIR CUTOUTCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV ATL, TEMP REPAIR INSTALLED. RT FWD CORNER OF AFT AIR STAIR CUT-OUT. REPAIR NOT MARKED PERMANENT. CORRECTION: REMOVED OLD REPAIR AND STARTED MAKING NEW REPAIR IAW M/M 53-30-0. OK TO INSTALL. VERIFIED TERMINATION OF CRACK PER P.S. 900-6-3 NR 1. INSTALLED PERMANENT REPAIR PER M/M 53-30-0 PP 803-804. 2L73 4F A3WE 19951106006811995110600681NM 1995 11 6 DL72W954148 119951022A5753652163234 SPAR BOEING727 727247 138408FNM NR 3 TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING SHOP INSPECTION, NR 3 MID-FLAP, LOWER AFT SPAR RAIL FOUND CRACKED 19 INCHES FROM INBOARD END OF FLAP. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951106006821995110600682NM 1995 11 6 DL72W954158 119951031A3350 EEL POWER SUPPLY WA332500129 BOEING727 727247 138408FNM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112821W L1675 21059 IRREG - CABIN EMERG EXIT LIGHT AT AIRSTAIR DOOR INOP. CORRECTIVE ACTION - REPLACED PWR SUPPLY AND BATTERY. 2L73 4F A3WE 19951106006831995110600683NM 1995 11 6 DL73S954105 119951025A2740 SCREWJACK BOEING737 737232 1384475NM STAB TRIM LACK OF LUBE A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO11306DL 23078 WITH AP ENGAGED, AP TRIM MOTOR RAN APPROX 9 AND ONE-HALF ROTATIONS FWD AND THEN 9 AND ONE-HALF ROTATIONS AFT. DOES THIS CONTINIOUSLY. WITH STAB TRIM SWITCHES OFF AND MANUALLY TRIMMING, IT FELT AS IF STABILIZER WAS BINDING. FOUND MOISTURE ON JACKSCREW. CLEANED AND LUBED SAME. RAN PDC BITE TEST AND SURFACE TEST FOR STAB TRIM. OPS CKS NORMAL. 2L72 4F RTA16WE 19951106006841995110600684NM 1995 11 6 DL757954147 119951025A5754114N300263 SKIN BOEING757 757232 1384965NM NR 5 LE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11652DL 24392 A PREVIOUS REPAIR TO THE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 5 LEADING EDGE SLAT IS DELAMINATED. THE DELAMINATION MEASURES 4 INCHES BY 3.5 INCHES AND IS CENTERED 10 INCHES FROM THE OTBD END AND 6 INCHES FWD OF THE T/E. THE SLAT IS IDENTIFIED AS AN ALUMINUM HONEYCOMB ASSEMBLY CONSISTING OF 0.016 INCH 2024-T3 FACESHEETS WITH BMS 4-4 TYPE 3-10N FLEX CORE AND MIL-C-7438 DENSE CORE HONEYCOMBS PER B757 57-43-02, FIG. 1, DETAIL XIII. REPAIRED PER DL ERA 302663-14AD. 2L72 4F RTA2NM 19951106006851995110600685NM 1995 11 6 DL757954153 119951030A33501317 BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11640DL 23994 DURING INSPECTION FOUND EMERGENCY FLOOR TRACK LIGHT AT ROW 34DEF INOP, RELAMPED, OPERATION NORMAL. 2L72 4F RTA2NM 19951106006861995110600686NM 1995 11 6 DL757954154 119951030A3350767 BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11640DL 23994 LT AFT OVERWING EMERG LIGHT INOP. RELAMPED. OPERATION NORMAL. 2L72 4F RTA2NM 19951106006871995110600687NM 1995 11 6 DL757954155 119951030A33501317 BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11640DL 23994 EMERG LIGHT SEAT 32ABC INOP, RELAMPED, OPERATION NORMAL. 2L72 4F RTA2NM 19951106006881995110600688NM 1995 11 6 DL767954159 119951017A5754114T410422A TE WEDGE BOEING767 767232 1385132NM NR 9/11 LE SLATSDELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11110DL 22222 RT WING NR 9 AND NR 11 SLAT TRAILING EDGE WEDGES HAVE AREAS OF DELAMINATION. ACCOMPLISHED REPAIRS PER DL ERA 272145-14AD. 2L72 4F RTA1NM 19951106006891995110600689NM 1995 11 6 DL76S954090 119951024A3411 PITOT PROBE BOEING767 767332 1382001NM FWD FUSELAGE CLOGGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11139DL 25984 AT V1 PLUS 3 KNOTS, LOST CAPTS A/S, ALTITUDE, AND HAD L AND REEC WARNING. RETURNED TO ATL. FOUND CAPTAIN'S PITOT PROBE PARTIALLY PLUGGED, REPLACED PROBE, OPERATION NORMAL. 2L72 4F RTA1NM 19951106006901995110600690WP 1995 11 6 DLL10954161 119951027A5743 ATTACH FITTING LKHEED1011 10113851 5265010WP RT MLG CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 RIGHT MLG ATTACH RIB FITTING WAS CORRODED AT THE MLG RETRACT ACTUATOR ATTACH FITTING LOCATION. ATTACH RIB UPPER AND LOWER ACTUATOR ATTACH PAD FASTENER HOLES WERE OVERSIZED. VERTICAL WEB AND FLANGES HAVE BEEN MACHINED/LOCALLY BLENDED PER DL ERA 272017-14. 2L73 4F A23WE 19951106006911995110600691WP 1995 11 6 DLL10954162 119951018A5312 BLKHD STRAPS LKHEED1011 10113851 5265010WP BS 1363 CUT A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 DURING ACCOMPLISHMENT OF S.I. 7-69959-12AD, THE AFT WEB SPLICE STRAPS AT RBL 42.5 AND LBL 42.5 WERE CUT AT LOWER END TO FACILITATE INSTALLATION OF THE LOWER CAP. THEY WILL BE REPAIRED PER THE L-1011 SRM AND DL ERA 272060-14AD. 2L73 4F A23WE 19951106006921995110600692WP 1995 11 6 DLL10954163 119951001A5312 BLKHD WEB LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11712DA 193C1088 DURING INSPECTION PER DAL S.I. 7-69959-12AD PART 1, THE SUBJECT AIRCRAFT WAS FOUND WITH A CRACK IN THE FUSELAGE FS 1363 BULKHEAD WEB. FURTHER INSPECTION REVEALED A SMALL CRACK AT A FASTENER HOLE LOCATED APPROXIMATELY .4 INCH ABOVE THE WEB CRACK. ACCOMPLISHED REPAIRS PER DL ERA 271982-14. 2L73 4F A23WE 19951106006931995110600693WP 1995 11 6 DLL10954164 119950713A53121505220 BLKHD WEB LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING INSPECTION, THE SUBJECT AIRCRAFT WAS FOUND WITH A CRACK IN THE FUSELAGE 1363 BULKHEAD WEB. THE CRACK IS LOCATED AT LBL 85 EXTENDING DIAGONALLY UPWARD. ACCOMPLISHED REPAIRS PER DL ERA 371384-14. 2L73 4F A23WE 19951106006941995110600694WP 1995 11 6 DLL10954169 119950925A5330 SKIN LKHEED1011 10113851 5265010WP BS 1363 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING REPAIR OF 1363 BULKHEAD, FOUND SEVERAL FASTENER HOLES BETWEEN STR'S 21 AND 23 AND STR'S 43-45 WERE OVERSIZED TO A .3885 INCH DIAMETER AND .344 INCH DIAMETER, RESPECTIVELY, DURING FASTENER REMOVAL. ACCOMPLISHED REPAIRS PER DL ERA 271890-14AD. 2L73 4F A23WE 19951106006951995110600695WP 1995 11 6 DLL10954171 119950926A53121554952102 BLKHD SPLICE LKHEED1011 10113851 5265010WP AFT PRESS DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11729DA 193C1180 DURING INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS, THE STR 10 FITTING WAS FOUND TO BE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 271943-14AD. 2L73 4F A23WE 19951106006961995110600696WP 1995 11 6 DLL10954172 119951006A5712 RIB LKHEED1011 10113851 5265010WP WS 555 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 THE LT WING IWS 555 RIB UPPER AND LOWER CAP WERE FOUND WITH CRACKS IN THE ATTACH TABS AT TYPICAL LOCATIONS. ACCOMPLISHED REPAIRS PER DL ERA 272011-14AD. 2L73 4F A23WE 19951106006971995110600697WP 1995 11 6 DLL10954174 119951006A5712 RIB LKHEED1011 10113851 5265010WP WS 503 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 THE RT WING IWS 503 RIB UPPER CAP ATTACH TAB IS CRACKED IN THE TYPICAL LOCATION BETWEEN STR 18 AND 19. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD. 2L73 4F A23WE 19951106006981995110600698WP 1995 11 6 DLL10954177 119951005A5320150617 DECK LKHEED1011 10113851 5265010WP FS 409 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11718DA 193C1097 THE PRESSURE DECK WAS FOUND DAMAGED AT FS 409 AND RBL 80 ON BOTH THE HORIZONTAL LEG AND THE LOWER SURFACE. THE DAMAGE WAS BLENDED OUT PER DL ERA 268387-14. 2L73 4F A23WE 19951106006991995110600699WP 1995 11 6 DLL10954183 119950822A5312 BLKHD SKIN LKHEED1011 10113851 5265010WP BS 1363 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11713DA 193C1089 WHILE ACCOMPLISHING RE-WORK OF 1363 BLKHD, SEVERAL HOLES THROUGH THE FUSELAGE SKIN AND THE MOD DOUBLERS UNDER THE CAP WERE FOUND WITH OVERSIZED FASTENER HOLES ON THE LT SIDE, REPAIRED IAW DL ERA 271609-14AD. 2L73 4F A23WE 19951106007001995110600700WP 1995 11 6 DLL13954165 119950929A5330 SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 A VISUAL INSPECTION REVEALED THAT THE FUSELAGE SKIN AT F.S. 1363 HAS A 2 INCH LONG CRACK RUNNING AFT FROM THE FORWARD EDGE OF THE PANEL JUST ABOVE STR 45. ACCOMPLISHED REPAIRS PER DL ERA 271883-14AD. 2L73 4F A23WE 19951106007011995110600701WP 1995 11 6 DLL13954167 119950922A5311 FRAME LKHEED1011 10113851 5265010WP FS 1343 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 DURING ACOMPLISHMENT OF S.I. 7-69903-12, FOUND TWO EXISTING FASTENER HOLES IN THE FRAME WEB AT FS 1343 WERE DAMAGED. THE TWO HOLES WERE O.S. TO .437 INCH PER DL ERA 271920-14AD. 2L73 4F A23WE 19951106007021995110600702WP 1995 11 6 DLL13954168 119950927A57111527095 REAR SPAR LKHEED1011 10113851 5265010WP WS 116-151 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11782DL 193A1006 THE RT WING REAR SPAR WAS FOUND WITH A CRACK LOCATED AT OWS 126 (2.75 INCHES LONG). THE CRACK EXTENDS ABOVE AND BELOW A FASTENER HOLE. DURING REMOVAL OF THE ATTACHING STRUCTURE, ANOTHER 1 INCH CRACK WAS FOUND AT OWS 147. ACCOMPLISHED REPAIRS PER DL ERA 271930-14. 2L73 4F A23WE 19951106007031995110600703WP 1995 11 6 DLL13954176 119951006A57201537600101 FASTENERS LKHEED1011 10113851 5265010WP WS 346.109 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 THE LT MLG SUPPORT RAIL WAS FOUND WITH A DAMAGED FASTENER JUST FORWARD OF THE REAR SPAR PLANE AND REQUIRES A SUBSTITUTE FASTENER TO BE INSTALLED. SUBSITUTION APPROVAL PER DL ERA 272006-14. 2L73 4F A23WE 19951106007041995110600704WP 1995 11 6 DLL13954178 119950918A5311 FRAME LKHEED1011 10113851 5265010WP FS 983 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 DURING INTERNAL INSPECTION OF THE FS 983 FRAME, A 1.25 INCH CRACK WAS FOUND ON THE RHS. THE CRACK IS COMPLETELY CONTAINED IN THE MAIN FRAME WEB AREA ADJACENT TO AN INTEGRAL HORIZONTAL STIFFENER. ACCOMPLISHED REPAIRS PER DL ERA 269695-14AD. 2L73 4F A23WE 19951106007051995110600705WP 1995 11 6 DLL13954185 119951004A53201504420101102 FITTING LKHEED1011 10113851 5265010WP FS 1212 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 THE LT AND RT KEELS ON BEAM OUTER SPLICE FITTINGS AND THE INNER SPLICE FITTINGS WERE FOUND CRACKED. THE CRACKS ARE CONFINED TO THE LOWER MOST ATTACHING ANGLE OF THE SUBJECT FITTINGS. 2L73 4F A23WE 19951106007061995110600706WP 1995 11 6 DLL15954160 119951027A53401582145101102 LATCH FITTINGS LKHEED1011 10113853 5265020WP CARGO DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11753DA 193W1189 DURING ACCOMPLISHMENT OF S.I. 7-58181-12AD, THE NR 7 C-1A CARGO DOOR LATCH FITTING HAD SURFACE CORROSION IN THE UPPER WELL. DRAIN HOLES HAVE BEEN ADDED IN THE CENTER OF THE LOWER WEB FOR FITTINGS NR 1, NR 2, NR 5, NR 6, NR 7, NR 8. THE SURFACE CORROSION ON THE NR 7 FITTING HAS BEEN BLENDED OUT PER DL ERA 272152-14AD. 2L73 4F A23WE 19951106007071995110600707WP 1995 11 6 DLL16954151 119951007A5347 SEAT TRACK LKHEED1011 10113853 5265020WP BS 1665-1725 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 AT HMV, FOUND LBL 30 SEAT TRACK CORRODED AT FS 1665 TO FS 1725. REPAIRED PER SRM 53-21-00 PG 836-840. 2L73 4F A23WE 19951106007081995110600708WP 1995 11 6 DLL16954152 119951007A5315 FLOOR BEAM LKHEED1011 10113853 5265020WP FS 1763 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 AT HMV, FOUND CABIN FLOOR BEAM CORRODED AT FS 1763 AT RBL 442, 76, 81, 86 AND 91. REPLACED FLOOR BEAM CAP PER SRM 53-21-00, PG 849-852. 2L73 4F A23WE 19951106007091995110600709WP 1995 11 6 DLL17954181 119951004A57431591922 FITTING LKHEED1011 10113853 5265020WP LT MLG CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 THE LT MLG ATTACH FITTING WAS FOUND CORRODED ON THE UPPER FLANGE. DURING REMOVAL, FASTENER HOLES WERE FOUND OVERSIZED AND SPOT FACED IN ACCORDANCE WITH THE SRM. SOME REQUIRED SPOT FACING DEEPER THAN THE LIMIT ALLOWED IN THE SRM. REPAIR APPROVAL PER DL ERA 271876-14. 2L73 4F A23WE 19951106007101995110600710WP 1995 11 6 DLL17954182 119951003A53301505639 SKIN LKHEED1011 10113853 5265020WP BS 1363 SHORT EDGE DIST A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 WHEN PICKING UP FASTENER LOCATIONS IN THE SKIN ATTACH FLANGE OF THE 1363 BULKHEAD CAP, NINE .25 INCH FASTENER HOLES ON BOTH THE LT AND RT SIDES WERE FOUND WITH SHORT EDGE DISTANCE ON THE FUSELAGE SKIN. REPAIRED IAW DL ERA 271825-14AD. 2L73 4F A23WE 19951106007111995110600711WP 1995 11 6 DLL17954184 119951003A57431604672102 ATTACH FITTING LKHEED1011 10113853 5265020WP RT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 TOOLING DAMAGE WAS INCURRED DURING RE-WORK TO AN INBOARD .6250 INCH FASTENER HOLE THROUGH THE RT MAIN LDG ATTACH FITTING. REPAIRED IAW DL ERA 271908-14 AD. 2L73 4F A23WE 19951106007121995110600712NM 1995 11 6 DLM88954166 119951002A533059304543565 SKIN DOUG MD88 MD88 3023688NM FS 229-294 PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO11911DL 49542 THE LT LOWER FORWARD FUSELAGE WAS PUNCTURED BY GROUND EQUIPMENT RESULTING IN DAMAGE TO THE SKIN, FRAMES, AND STRINGERS AT FS 229-294. ACCOMPLISHED REPAIRS PER DL ERA 271965-14. 2L72 4F RTA6WE 19951106007131995110600713NE 1995 11 6 P5CA9500834 219951102A7320 FUEL CONTROL BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 3 ENGINE OUT OF ADJUST A P5CACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP23851FT4897726677 19756 685904 DURING TAKEOFF ROLL AT 40-60 KTS, A/C VEERED TO LEFT OF CENTERLINE. BROUGHT POWER BACK ON ALL ENG'S AND ABORTED TAKEOFF. ADVANCING POWER ON ALL ENGINES EVENLY UP TO 1.30 EPR. AT THAT TIME, NR 3 ENG EPR JUMPED TO 1.53, CAUSING A/C TO VEER. A/C WAS VERY LIGHT AND INCREASED EPR AT LOW GROUND SPEED PRODUCED ASYM THRUST. RE-CHECKED RIG AND FOUND TO BE WITHIN LIMITS. FOUND NR 3 FCU OUT OF RIG, RIGGED SAME AND C/W POWER RUN. OPS CHECKS GOOD PER MM 71-00-00. 2L74 4F4 F A20WE E20EA 19951106007141995110600714NM 1995 11 6 UPS204927 119951101A3350 BATTERY BOEING727 7272A1 138407FNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01214UP 21342 WHILE ON THE GROUND, MAINTENANCE FOUND FLIGHT DECK DOOR AND MAIN ENTRY DOOR EMERGENCY EXIT LIGHTS INOP DURING DAILY CHECK. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DECK DOOR AND MAIN ENTRY DOOR EMERGENCY EXIT LIGHT BATTERIES PER MM 30-50-101. OPS CHECKED GOOD PER MM 33-50-01. 2L73 4F A3WE 19951106007151995110600715NM 1995 11 6 UPS204928 119951101A3350 BATTERY BOEING727 72722C 138400FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01941UP 19196 WHILE ON THE GROUND IN CGN, MAINTENANCE FOUND EMERGENCY LIGHT DOES NOT COME ON WHEN SWITCHED TO ON. MAINTENANCE REPLACED THE BATTERIES, FUNCTIONAL CHECKS GOOD. 2L73 4F A3WE 19951106007161995110600716WP 1995 11 6 UPS804929 119951101A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01752UP 45952 WHILE ON THE GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN DISARM AND OFF DISARM/CHECK POSITION LIGHT WAS OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK ASSEMBLY AND LIGHT DIMING RELAY. 2L74 4F RT4A25 19951106007171995110600717EU 1995 11 6 WWMA9500078 119951031A261272111211000 FIRE DETECTOR SAAB SF340 340B 7860101EU REAR CARGO BAY DEFECTIVE A WWMAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP15326AE6168 340B326 CARGO SMOKE WARNING LIGHT CAME ON IN-FLIGHT, CARGO FIRE BOTTLE NR 1 WAS FIRED. UPON INVESTIGATION, MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE, BOTH CARGO FIRE DETECTORS AND THE NR 1 FIRE BOTTLE WERE REPLACED, THE AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER PROBLEMS. 2L72 4T RTA52EU 19951108000011995110800001WP 1995 11 8 MEJA9509001 219950907A73228950935 DIAPHRAM SWRNGNSA227 SA227AT 8780610SW GARRTTTPE331TPE33111U 01514WP RT ENG FCU DEFECTIVE E AMEJAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS APAPPROACH 1 SW17563UP AT563 P44253 AMA-DFW - FLT 1911 - WHILE ON APPROACH, THE RIGHT ENGINE TORQUE STARTED TO SURGE, TORQUE COULD ONLY BE DECREASED TO 31 PERCENT. RIGHT ENGINE WAS SHUTDOWN AND SECURED, LANDED AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE P3 DIAPHRAM IN THE RIGHT ENGINE FUEL CONTROL WAS DEFECTIVE. REPLACED THE P3 DIAPHRAM IN ACCORDANCE WITH WOODWARD SB 64043. PERFORMED GROUND RUN, NO DEFECTS NOTED. FUNCTIONAL CHECK FLIGHT WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A5SW E4WE 19951109000011995110900001EU 1995 11 9 COMA9531178 119951027A32465009237 INNER RACE SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 1323738 340A140 MECHANIC REMOVED WHEEL ASSY FROM AIRCRAFT DUE TO TIRE WORN TO LIMITS. DURING INSPECTION, FOUND THAT THE INNER RACE HAD SPUN. SUBASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19951109000021995110900002WP 1995 11 9 95FDEA01616 119951028A5743 BUSHING DOUG DC10 DC1010 3022110WP RT MLG TRUNNION MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RIGHT MLG WING TRUNNION FWD FITTING AFT LUG BUSHING MIGRATED FWD/OUT OF LUG. 2L73 4F A22WE 19951109000031995110900003NE 1995 11 9 9516916613 219951026A7532 PRBCV BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 2 ENGINE MALFUNCTIONED A NWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DEDESCENT 1 GL01613US 20358 662633 DURING TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. A RE-LIGHT WAS ACCOMPLISHED, BUT THE POWER LEVER COULD NOT BE ADVANCED WITHOUT THE COMPRESSOR STALLING. THE ENGINE WAS SHUT DOWN AGAIN DURING APPROACH AND AN UNEVENTFUL THREE-ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. THE ENGINE WAS INSPECTED AND A BORESCOPE WAS ACCOMPLISHED. THE PRESSURE RATIO BLEED CONTROL AND BLEED CONVERTER VALVE WERE REPLACED AND PROPER ENGINE OPERATION WAS CONFIRMED DURING AN ENGINE RUN-UP. 2L74 4F4 F A20WE E20EA 19951113000381995111300038SW 1995 11 13 95ZZZX6087 119950321A2910MS21902W4 FITTING BELL 214 214ST 1182106SW HYD SYSTEM LEAKING A HEEAK NONE KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SW035748M 28102 OIL COOLER CAUTION LIGHT ILLUMINATED. FOUND FITTING LEAKING ON UTILITY MOTOR CASE. REMOVED AND RESEATED FITTING. SERVICED HYDRAULIC SYSTEM. IPC 29-12-00, PAGE 42, FIGURE 4, ITEM 55. 2G72 4U H10SW 19951113000401995111300040WP 1995 11 13 9417109935 119951031A3350 BATTERY PACK DOUG DC9 DC931 3022065WP COCKPIT DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL011332U 47404 DURING LINE CHECK, COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000411995111300041 1995 11 13 9517082202 419951102A344220704100101 TRANSCEIVER BOEING727 727251 138408HNM RADAR FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01202US160631106 22155 DURING DEPARTURE 40 MILES NW OF MSY, RADAR UNIT FAILED, NO RETURNS. WEATHER IN THE AREA OF DESTINATION, FLIGHT RETURNED TO MSY WITHOUT INCIDENT. REPLACED THE RADAR TRANSCEIVER UNIT, OPERATIONAL CHECK OK. 2L73 4F A3WE 19951113000421995111300042WP 1995 11 13 9517099604 119951101A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01604NW 47222 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 TO 9. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000431995111300043WP 1995 11 13 9517119868 119951030A3350 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01777NC 47787 DURING LINE CHECK, STATION 700 CABIN OVERHEAD EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000441995111300044WP 1995 11 13 9517129872 119951030A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01781NC 48121 DURING LINE CHECK, FOUND CEILING LIGHTS INOPERATIVE AT ROWS 16 TO 20. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000451995111300045WP 1995 11 13 9517139991 119951101A3260 RELAY DOUG DC9 DC932 3022066WP LANDING GEAR MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018957E 47215 DURING CLIMB, THE GREEN NOSE GEAR LIGHT ILLUMINATED. CREW RECYCLED LANDING GEAR AND THE LIGHT REMAINED ILLUMINATED. ALSO, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR SWITCH S1-11 TIE-WRAPPED TO THE ENERGIZED POSITION. ALSO, FOUND CONDUIT FOR RIGHT MAIN LANDING GEAR DOOR INTERFERING WITH UPLATCH HOOK. REMOVED TIE-WRAP, REROUTED CONDUIT, ADJUSTED ROLLERS, AND REPLACED THE R2-28 LANDING GEAR RELAY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000461995111300046WP 1995 11 13 9517149924 119951031A3230 DOOR DOUG DC9 DC932 3022066WP CARGO COMPT NOT CLOSED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01926RC 47473 DURING CLIMB, THE AIRCRAFT DID NOT PRESSURIZE. THE AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. FOUND AFT CARGO DOOR OPEN, INSPECTED AND CLOSED DOOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000471995111300047WP 1995 11 13 9517159753 119951101A3260 STRICKER BOLT DOUG DC9 DC941 302207NWP RT MLG DOOR OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01753NW 47117 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. CREW RECYCLED THE LANDING GEAR AND THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. FOUND THE RIGHT MAIN LANDING GEAR DOOR STRIKER BOLT NOT MAKING CONTACT WITH THE DOOR SWITCH. REPLACED AND ADJUSTED BOLT, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951113000481995111300048WP 1995 11 13 9517169753 119951031A3260 BRACKET DOUG DC9 DC941 302207NWP GEAR DOOR OUT OF ADJUST A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01753NW 47117 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. CREW RECYCLED THE LANDING GEAR AND THE LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND BRACKET OUT OF ADJUSTMENT. READJUSTED BRACKET, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113000491995111300049EU 1995 11 13 9517173239 119951101A3260848401 PROX SENSOR AIRBUS320 A320211 3930320EU LT MLG MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01339NW 367 DURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE LOCKED AFTER LANDING GEAR EXTENSION. PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND CYCLED LANDING GEAR. ALL INDICATIONS NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN LANDING GEAR DOOR PROXIMITY SENSORS, 27GA AND 29GA. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951113000501995111300050EU 1995 11 13 9517183239 119951101A3260 DOOR INDICATION AIRBUS320 A320211 3930320EU LT MLG MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01339NW 367 DURING APPROACH INTO BWI, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE LOCKED AFTER GEAR EXTENSION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, CYCLED LANDING GEAR AND ACCOMPLISHED A GO-AROUND. ALL INDICATIONS WERE NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2L72 4F RTA28NM 19951113000511995111300051NM 1995 11 13 9517196304 119951030A2612 FIRE DETECTOR BOEING747 747451 1384940NM APU MALFUNCTIONED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 GL01664US 23819 DURING APPROACH, APU FIRE BELL SOUNDED, THE FIRE LIGHT ILLUMINATED AND APU FIRE BOTTLE DISCHARGED. AIRCRAFT LANDED IN DTW WITHOUT FURTHER INCIDENT. REPLACED APU FIRE DETECTOR AND BOTTLE. OPERATIONAL CHECK GOOD. 2L74 4F RTA20WE 19951113000521995111300052EU 1995 11 13 9517203234 219951101A73211459M55P17 ECU AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 2 ENGINE MALFUNCTIONED A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 GL01334NW9961 9961 339 731743 DURING DESCENT AT 33,000 FEET, NR 2 ENGINE OVERSPEED OCCURRED. AUTO THROTTLE WAS DISENGAGED, POWER LEVER WAS PULLED BACK, AND ENGINE RPM CONTINUED TO ACCELERATE. ENGINE WAS MANUALLY SHUTDOWN. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BORESCOPE AND ENGINE OVERSPEED INSPECTION REVEALED NO DISCREPANCIES. REPLACED THE NR 2 ENGINE CONTROL UNIT, OPERATIONAL CHECK OK. 2L72 4F4 FRTA28NM 19951113000531995111300053NM 1995 11 13 95FDEA01666 119951102A5313BAC149134 STRINGER BOEING727 72722 1384002NM BS 419 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 GOUGE AND DENT ON STR AT BS 419 STR 15L. REPAIRED DENT ON STR AT BS 419 STR 15L. REPAIRED FROM BS 416 TO 439 PER FEDEX SRM 53-10-03. 2L73 4F A3WE 19951113000541995111300054NM 1995 11 13 95FDEA01667 119951102A5315BAC1505100246 FLOORBEAM BOEING727 72722 1384002NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-224-02), AROUND NUTPLATE HOLES AT BS 312 LBL 29 TO 18 WL 208.1. REPAIRED CORROSION REMOVAL AREA AT LBL 18 BS 312 WL 208 PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19951113000551995111300055NM 1995 11 13 95FDEA01668 119951102A5330 SKIN BOEING727 727225 1384077NM BS 1342 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25466FE 21292 MISC WORKING FASTENERS IN SKIN AT BS 1342 LBL 45 WL 260 TO 270. ACCESSED AREA, CUT OUT DAMAGED SKIN AND U-CHANNEL, REPAIRED PER SRM 54-30-3 FIG 7, INSTALLED ALL ITEMS REMOVED FOR ACCESS. 2L73 4F A3WE 19951113000561995111300056NM 1995 11 13 95FDEA01669 119951102A3260694710566 MODULE BOEING727 727227 1384078NM LT MLG LIGHT INOP A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25479FE 21461 WHEN GEAR LEVER DOWN, LEFT MAIN GREEN DOWN AND LOCK LIGHT DID NOT ILLUMINATE AND OTHER LIGHTS OK. RECYCLED GEAR, THREE GREEN DOWN AND LOCKED LIGHTS OK. FOUND LEFT GEAR LIGHT INOPERATIVE. REPLACED LANDING GEAR MODULE, OPERATIONAL CHECK GOOD. 2L73 4F A3WE 19951113000571995111300057WP 1995 11 13 95FDEA01670 119951102A5311AKC7003 FRAME DOUG DC10 DC1010F 3022111WP TAIL CONE CRACK A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 TAIL CONE FWD FRAME CRACKED LT SIDE AT TOP GUIDE PIN HOLE. STOP DRILLED CRACK IN FRAME, INSTALLED FRAME DOUBLER PER TAIL CONE FRAME CRACK REPAIR SRM 53-30-00 FIG 3 PAGE 2. VERIFIED FOR CRACK INDICATION BEYOND STOP DRILL HOLES WITH H/FEC, NO INDICATION, REF SRM NR 3096. 2L73 4F A22WE 19951113000581995111300058WP 1995 11 13 95FDEA01671 119951102A5311 BELLFRAME DOUG DC10 DC1010F 3022111WP BS 1841 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 CENTER CARGO COMPARTMENT CORROSION ON BELLFRAME, STA 1841 STRINGER 50R THROUGH 506 AFT SIDE OF BELLFRAME. CUT AND REMOVED DAMAGED SECTION OF BELLFRAME, REMOVED LIGHT REMAINING CORROSION. ALODINED AND PRIMED AREA, FABRICATED, SPLICE AND DOUBLER INSTALLED SPLICE AND DOUBLER PER SRM NR 53-00-01. 2L73 4F A22WE 19951113000591995111300059NM 1995 11 13 95UAL900245 119951103A5330 SKIN BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE FUSELAGE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP299025U 19063 FOUND TWO-INCH CRACK IN FUSELAGE ON AFT SIDE OF E AND E COOLING FAN EXHAUST PORT. ACCOMPLISHED PERMANENT SKIN REPAIR PER STRUCTURAL REPAIR MANUAL 53-30-3 USING .10 INCH THICK 2024-T3 CIRCULAR EXTERNAL REPAIR DOUBLER WITH THREE FASTENER ROWS. 2L72 4F4 F A16WE E2EA 19951113000601995111300060NM 1995 11 13 95UAL900246 119951103A5270 SENSOR BOEING737 737222 1384473NM CARGO DOOR INTERMITTENT A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP299063U 19944 CREW REPORTS, AFT CARGO DOOR LIGHT FLICKERED AND THEN REMAINED ON. REPLACED PROXIMITY SENSOR AND ADJUSTED GAP PER MM CHECKS OK. 2L72 4F A16WE 19951113000611995111300061NM 1995 11 13 95UAL900247 119951103A261218252 DETECTOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 2 ENGINE SHORTED A UALAK NONE N FALSE WARNING ININSP/MAINT 1 WP297461U 21915 NR 2 ENGINE FIRE WARNING GROUND FAULT DETECTOR LIGHT ON. DETECTOR ELEMENT WAS REPOSITIONED TO PREVENT CONTACT WITH STRUCTURE. NO FURTHER PROBLEMS REPORTED. 2L73 4F4 F A3WE E2EA 19951113000621995111300062NM 1995 11 13 P5CA9500835 119951103A2781 POSITION IND BOEING747 747122 1384872NM OUTBD FLAP INOPERATIVE A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23851FT 19756 DURING TAXI OUT, LOWERING FLAPS, OUTBOARD FLAP POSITION INDICATIONS SPLIT LT/RT. SPLIT CAUSED ASYMMETRY LOCKOUT. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR IAW MM 27-58-00, PERFORMED SEVERAL OP CHECKS AND ALL FOUND NORMAL. 2L74 4F A20WE 19951113000631995111300063WP 1995 11 13 SCNA95254 119951031A5730ARB09402 SKIN DOUG DC10 DC1015 3022118WP RT WING CRACK A SCNAK NONE O OTHER ININSP/MAINT 1 GL15152SY 48289 DURING A SCHEDULED MAINTENANCE CHECK, THE LOWER RIGHT WING SKIN AT XORS 981, STRINGER 32 WAS FOUND WITH IMPACT DAMAGE CONSISTING OF A 0.375 CRACK AND A SMOOTH DENT. THE CRACK AND DENT WERE REPAIRED IAW WITH SUN COUNTRY EO 57-5164-1. 2L73 4F A22WE 19951113000651995111300065EU 1995 11 13 95ZZZX6090 119950911A2612 DETECTOR AEROSPAS355 AS355F1 8680810EU NR 1 ENG FWD BROKEN A ALGAO OTHER N FALSE WARNING APAPPROACH 1 SW03376E 5213 DURING APPROACH TO LAND, NR 1 ENGINE FIRE LIGHT ILLUMINATED. DURING TROUBLESHOOTING, THE WIRE AT NR 1 ENGINE FORWARD INBOARD FIRE DETECTOR WAS FOUND BROKEN. REPAIRED WIRE. 1G72 3U H11EU 19951113000701995111300070SW 1995 11 13 95ZZZX6095 119950831A6410206016201127 BLADE BELL 206 206L1 1182107SW T/R BEARING CRACKED B ZV1RK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW0340LP 1401 CS5458 45233 DURING MAINTENANCE ON T/R HUB AND BLADE (HIGH FREQ VIB), FOUND INBOARD BEARINGS CRACKED, TOTAL TIME OF BEARINGS, 921.7 HOURS. 1G71 3U H2SW 19951113000711995111300071SW 1995 11 13 95ZZZX6096 119950831A6410206016201127 BLADE BELL 206 206L1 1182107SW T/R BEARING CRACKED B ZV1RK NONE E VIBRATION/BUFFET ININSP/MAINT 1 SW0340LP 1401 CS5456 45233 DURING MAINTENANCE ON T/R HUB AND BLADE (HIGH FREQ VIB), FOUND INBOARD BEARINGS CRACKED, TOTAL TIME OF BEARINGS, 921.7 HOURS. 1G71 3U H2SW 19951113000741995111300074WP 1995 11 13 95ZZZX6099 119950910A2420914F5673 POWER RELAY DOUG DC9 DC915 3022036WP E/E BAY MALFUNCTIONED A GRAAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP111070T 45784 STS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GENERATOR POWER RELAY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ELECTRICAL SYSTEM. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. REF CONTROL GRAA9543, AND CONTROL NR 95ZZZX6100. 2L72 4F A6WE 19951113000751995111300075WP 1995 11 13 95ZZZX6100 119950910A24201914F5653 BUSS PROT PNL DOUG DC9 DC915 3022036WP E/E BAY MALFUNCTIONED A GRAAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP111070T 45784 STS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GENERATOR POWER RELAY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ELECTRICAL SYSTEM. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. REF CONTROL GRAA9543, AND CONTROL NR 95ZZZX6099. 2L72 4F A6WE 19951113000771995111300077SO 1995 11 13 95ZZZX6102 119950811A321314470 TORQUE LINK ERAM EMB 110 EMB110P1 3260122SO RT MLG BROKEN AS BQTAK NONE O OTHER TXTAXI/GRND HDL 1 NE05621KC13739 110335 RT MLG UPPER TORQUE LINK FAILED AT CENTER PIVOT POINT. THIS WAS CAUSED BY A LOCKING PIN FAILURE (ITEM 66A) AND (ITEM 67A). 1L72 4T A21SO 19951113000781995111300078CE 1995 11 13 95ZZZX6103 119950912A21507756355 ACM BEECH 1900 1900D 1154162CE LT INBD WING SEIZED A MASAK NONE O OTHER ININSP/MAINT 1 SW01133YV948 UE133 ACM WILL NOT BLOW COOL AIR. FOUND ACM TURBINE SEIZED. REMOVED AND REPLACED ACM WITH OVERHAULED SERVICEABLE ACM. OPERATIONAL CHECK GOOD. ORIGINAL ACM HAD FULL OIL AND PROPERLY SERVICED. S/N OFF, 940911. 2L72 4T RTA24CE 19951113000791995111300079WP 1995 11 13 95ZZZX6104 119950923A2910 LINE DOUG DC8 DC871F 302199DWP HYD SYSTEM FAILED A RRXAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 WP15500MH 45812 LIPA/EBBR - FLT 882 - HYDRAULIC QUANTITY DROPPED TO STANDPIPE AND PRESSURE BEGAN TO FLUCTUATE. CREW ACCOMPLISHED HYDRAULIC EMERGENCY CHECK LIST. MAINTENANCE REMOVED AND REPLACED THE FLEX LINE FROM THE RUDDER PUMP TO THE ACCUMULATOR. AN OPERATIONAL CHECK OF THE HYDRAULIC SYSTEM WAS GOOD. 2L74 4F RT4A25 19951113000801995111300080EU 1995 11 13 95ZZZX6105 119950920A3246AH52997 WHEEL STBROSSD3 SD360 8100606EU NLG CRACKED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03165DD 209 SH3740 JFK - FLT 4922 - UPON POST-FLIGHT INSPECTION, FOUND LT NOSE WHEEL HALF BEAD AREA CRACKED OFF APPROXIMATELY ONE-THIRD AROUND WHEEL. REMOVED AND REPLACED WHEEL AND TIRE ASSYS. 2H72 4T A41EU 19951113000811995111300081EU 1995 11 13 95ZZZX6106 119951017A3260622800200 UPLOCK SWITCH 1849E BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A SABAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO05159PC LK8709073 768 CLT/HTS - FLT 5100 - ON 10-17-95, USAIR EXPRESS FLIGHT HAD JUST DEPARTED CLT WHEN THE RT LANDING GEAR INTRANSIT LIGHT ILLUMINATED. THE CAPTAIN DID NOT DECLARE AN EMERGENCY, BUT HE DID REQUEST THAT EMERGENCY EQUIPMENT BE STANDING BY. THE AIRCRAFT MADE A SAFE LANDING IN CLT. MAINTENANCE PERSONNEL INSPECTED THE RT LANDING GEAR POSITION AND WARNING SYSTEM AND DETERMINED THE UPLOCK MICROSCITCH WAS FAULTY. THE MICROSWITCH WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951113000821995111300082EU 1995 11 13 95ZZZX6107 119951017A3260622800200 DOWNLOCK SWITCH B00A702852A BAG JETSTMJETSTM3101 1500215EU NLG FAILED A SABAO OTHER N FALSE WARNING APAPPROACH 1 SO05161PC BADL182 675 RDU/GSP - FLT 5010 - ON 10-17-95 USAIR EXPRESS FLT WAS APPROX 20 MILES FROM DEST IN GSP WHEN NOSE GEAR GREEN DOWN & LOCKED LIGHT ILLUMINATED. CREW VISUALLY VERIFIED NOSE GEAR STILL IN UP POSITION BY LOOKING AT PROP SPINNER. LDNG GEAR SELECTED DOWN & NOSE GEAR SHOWED GREEN & RED INDICATIONS, BOTH MAIN GEAR INDICATIONS NORMAL. LDNG GEAR VISUALLY VERIFIED IN DOWN POSITION. CAPT DECLARED CONDITIONAL EMERG & HAD EMERG EQUIP STANDING BY. ACFT MADE SAFE LDNG IN GSP. AFTER SAFELY REACHING GATE & DEPLANING PASSENGERS, CAPT VISUALLY VERIFIED GEAR HAD BEEN DOWN & LOCKED. ACFT FERRIED TO CLT. MX INSP NLG POS & WARNING SYS, FND DNLK MICROSWITCH FAILED & REPLACED W/DIFFERENT P/N IAW JTSTRM SB 32JA891142, PART NR 1. 2L72 4T RTA21EU 19951113000831995111300083WP 1995 11 13 95ZZZX6108 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 SKIN CRACK 10 INCHES FORWARD AND 12 INCHES ABOVE UPPER HINGE OF CREW DOOR. REPAIR IAW SRM 12-19. 2L74 4R 6A3 19951113000841995111300084WP 1995 11 13 95ZZZX6109 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 SKIN CRACK AFT OF ENTRY DOOR BELOW HANDLE. REPAIR IAW SRM 12-19. 2L74 4R 6A3 19951113000851995111300085WP 1995 11 13 95ZZZX6110 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP FUSELAGE CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 SKIN CRACK AT BUTT SEAM BETWEEN ENTRY DOOR AND FIRST OFFICER'S WINDOWS. REPAIR IAW SRM 12-56. 2L74 4R 6A3 19951113000861995111300086WP 1995 11 13 95ZZZX6111 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 938 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 SKIN CRACK FS 938, RT AT 'N' NR. REPAIR IAW SRM 12-56. 2L74 4R 6A3 19951113000871995111300087WP 1995 11 13 95ZZZX6112 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 100 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 SKIN CRACK FS 100, CENTER. REPAIR IAW SRM 12-21. 2L74 4R 6A3 19951113000881995111300088WP 1995 11 13 95ZZZX6113 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 217 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 CORROSION AND SKIN CRACK FS 217 FROM STR 4R TO STR 4L. REPAIR IAW SRM 12-55. 2L74 4R 6A3 19951113000891995111300089WP 1995 11 13 95ZZZX6114 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 340 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 CORROSION AND SKIN CRACK FS 340 FROM STR 4L TO STR 4R. REPAIR IAW SRM 12-55. 2L74 4R 6A3 19951113000901995111300090WP 1995 11 13 95ZZZX6115 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 520 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 CORROSION AND SKIN CRACKED FS 520 FROM STR 4L TO STR 4R. REPAIR IAW SRM 12-55. 2L74 4R 6A3 19951113000911995111300091WP 1995 11 13 95ZZZX6116 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 640 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 CORROSION AND SKIN CRACKS FS 640 FROM STR 4L TO STR 5L. REPAIR IAW SRM 12-56. 2L74 4R 6A3 19951113000921995111300092WP 1995 11 13 95ZZZX6117 119951011A5330 SKIN DOUG DC6 DC6A 3021706WP BS 820 CRACKED A TALAK NONE O OTHER ININSP/MAINT 1 SO19874TA35235 44641 CORROSION AND SKIN CRACKS FS 820 FROM STR 4L TO STR 4R. REPAIR IAW SRM 12-56. 2L74 4R 6A3 19951113000931995111300093CE 1995 11 13 95ZZZX6118 119950914A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01105GL6636 1040 UC105 SPW - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND RT TRUSS INBOARD UPPER TUBE CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1. 2L72 4T RTA24CE 19951113000941995111300094CE 1995 11 13 95ZZZX6119 119950920A21501143800025 PRECOOLER BEECH 1900 1900C 1154161CE RT ENGINE LEAKING A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE01126UE 649 UC126 HON - DURING CLIMB-OUT AFTER DEPARTURE, THE CREW ELECTED AN AIR TURN-BACK DUE TO SMOKE IN THE CABIN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE FOUND OIL IN THE RT PRECOOLER. THE INSTALLATION TESTED SATISFACTORILY. 2L72 4T RTA24CE 19951113000951995111300095CE 1995 11 13 95ZZZX6120 119950907A712012991003279 TRUSS BEECH 1900 1900D 1154162CE RT ENGINE CHAFED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0194UX 4026 UE94 SPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE RT ENGINE TRUSS TOP INBOARD TUBE IN AREA 'A' CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1. 2L72 4T RTA24CE 19951113000961995111300096CE 1995 11 13 95ZZZX6121 119950918A712012991003279 TRUSS BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01125GL 1057 1025 UC125 SPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE LT TRUSS CRACKED ALONG THE TOP COWLING ATTACH BRACKETS BOTH INBOARD AND OUTBOARD. THE TRUSS WAS REPLACED. 2L72 4T RTA24CE 19951113000971995111300097CE 1995 11 13 95ZZZX6122 119950922A5610114504315 WINDSHIELD BEECH 1900 1900C 1154161CE LT COCKPIT CRACKED A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01557823059 446 UC168 MBL - AFTER DEPARTURE AND DURING CLIMB-OUT, THE NR 1 WINDSHIELD CRACKED. THE CREW ELECTED AN AIR TURN-BACK AND COMPLETED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4T RTA24CE 19951113000981995111300098CE 1995 11 13 95ZZZX6123 119951004A57301181100471 LE SKIN BEECH 1900 1900C 1154161CE LT WING CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0187GL 15791 UC87 SPW - DURING ROUTINE INSPECTION, A 4 INCH CRACK WAS FOUND ON THE LT WING 4 FEET INBOARD OF THE TIP AND 3 INCHES AFT OF THE TOP AFT EDGE OF THE WING BOOT. A FLUSH PATCH WAS INSTALLED IAW BEECH SRM 51-70-00, PAGES 26-27 AND LEAK CHECKED OK. 2L72 4T RTA24CE 19951113000991995111300099SO 1995 11 13 95ZZZX6124 119951015A2720MS202J74 HINGE EMB 110 EMB110P1 3260122SO RUDDER LOOSE A BQTAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 NE05621KC13842 110335 DURING FLIGHT, PILOT REPORTED SEVERE VIBRATION FROM RUDDER. UPON INSPECTION, FOUND UPPER RUDDER HINGE CRACKED WHERE BOLT PASSES THROUGH TOP AND BOTTOM. RUDDER TRIM TAB HINGE WHERE ACTUATOR ARM ATTACHES WAS FOUND LOOSE (WORKING CHERRYMAX RIVETS). THIS DAMAGE APPEARS TO HAVE HAPPENED DURING A WINDSTORM AND ACFT TAILED INTO WIND. (ALL CONTROL LOCKS WERE INSTALLED.) 1L72 4T A21SO 19951113001001995111300100SO 1995 11 13 95ZZZX6125 119951005A3246GYS187C35 BOLT GOODYEARAERO95610619 GULSTMG1159 G1159 3953505SO NR 2 MLG WHEEL BROKEN A AKKYAK NONE O OTHER ININSP/MAINT 1 NE03220FL APRFF154 50 DURING A POST-FLIGHT INSPECTION, MAINTENANCE FOUND A BROKEN BOLT ON THE NR 4 WHEEL. FLIGHT CREW INDICATED ALL OPS WERE NORMAL. BOLTS HAD 174 LANDINGS SINCE NDT. WHEEL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. CYCLES, 174. 2L72 4F RTA12EA 19951113001011995111300101NE 1995 11 13 95ZZZX6126 219951016A7320101MK14 FFR LUCAS LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 2 ENGINE FAILED A RAIAAJ UNSCHED LANDING DUMP FUEL RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CE03313EA B1464 193A1020 10218 NR 2 ENGINE LOST POWER AFTER TAKEOFF, POWER RETARDED ITSELF TO 80 PERCENT N1. AIRCRAFT DUMPED FUEL AND RETURNED TO GATE. CHANGED FFR TO CORRECT PROBLEM AND CHANGED FUEL PUMP AS A PRECAUTIONARY MEASURE. ACCOMPLISHED NORMAL ENGINE RUN AND RETURNED AIRCRAFT TO SERVICE. 2L73 4F4 F A23WE E12EU 19951113001021995111300102EU 1995 11 13 95ZZZX6127 119950827A3260801801 PROXIMITY SWITCHELDEC BAC 146 146200A 1500266EU NLG WORN A TIXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP19156TR E2156 LAS - MANUAL SPOILER FAULT LIGHT ILLUMINATED AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE LAS STATION. TNE NLG ELECTRONIC POSITION SENSOR WAS FOUND TO BE OUT OF ADJUSTMENT DUE TO NORMAL WEAR. THE SWITCH WAS ADJUSTED IAW THE AIRCRAFT MM. A TEST FLIGHT WAS CONDUCTED TO ENSURE NO FURTHER DIFFICULTIES WITH THE MANUAL SPOILER FAULT INDICATOR, THE AIRCRAFT WAS RETURNED TO SERVICE. 2H74 4F A49EU 19951113001031995111300103NM 1995 11 13 95ZZZX6128 119950925A612030005100044 TQ CONTROL UNIT DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A HNAAK NONE N FALSE WARNING CLCLIMB 1 EA07925HA11643 786 111 TPA/JAX - FLT 3166 - AFTER TAKEOFF DURING CLIMB, THE AUTOFEATHER ARM LIGHT ILLUMINATED INTERMITTENTLY. THE AIRCRAFT CONTINUED ON TO JAX AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 TORQUE SENSOR CONTROL UNIT. 2H72 4T RTA13NM 19951113001041995111300104EA 1995 11 13 95ZZZX6129 119950920A3350 EEL DHAV DHC7 DHC7102 2802708EA CABIN INOPERATIVE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07901HA 042 ORF/DCA - FLT 3003 - AFTER FCD7-33-95-022 COMPLIANCE, THE EMERGENCY LIGHTS OPERATIONAL CHECK FAILED. RETURNED EMERGENCY LIGHTS WIRING TO ORIGINAL CONFIGURATION AND ENTERED ON DML. 2H74 4T A20EA 19951113001051995111300105NM 1995 11 13 95ZZZX6130 119951005A3260864202 SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAK NONE N FALSE WARNING CRCRUISE 1 EA07924HA19999 105 CLT/CHA - FLT 3204 - THE NOSE GEAR CYCLED SEVERAL TIMES IN GEAR WELL IN CRUISE. THE INTRANSIT AND HANDLE LIGHTS CYCLED ON AND OFF. THE AIRCRAFT CONTINUED ON TO CHA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG STRUT SENSOR. 2H72 4T RTA13NM 19951113001061995111300106NM 1995 11 13 95ZZZX6131 119951005A5210 BOLT DHAV DHC8 DHC8102 2809003NM AIRSTAIR DOOR LOOSE A HNAAO OTHER O OTHER TXTAXI/GRND HDL 1 EA07921HA 089 LYN/PIT - FLT 3401 - AFTER LANDING IN PIT, THE AIRSTAIR DOOR WOULD NOT OPEN. FOUND UNSECURED BOLT ON FORWARD LOWER HANDRAIL ASSEMBLY. SECURED THE BOLT AS REQUIRED. 2H72 4T RTA13NM 19951113001071995111300107EA 1995 11 13 95ZZZX6132 119951002A3230805310 PROX SWITCH DHAV DHC7 DHC7102 2802708EA RT MLG FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07902HA12347 372 52 ORF/DCA - FLT 3130 - AFTER DEPARTURE, THE RT MAIN GEAR WOULD NOT RETRACT. THE AIRCRAFT TURNED BACK AND LANDED IN ORF WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT GEAR PROXIMITY SWITCH. 2H74 4T A20EA 19951113001081995111300108NE 1995 11 13 95ZZZX6133 219950929A732082455011S011 ENGINE HARNESS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE FAILED A HNAAK NONE N FALSE WARNING TOTAKEOFF 1 EA07925HA19511 111 TPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROPELLER AUTOFEATHER SWITCH AND THE NR 1 BRAIDED ENGINE HARNESS FROM FIREWALL TO EEC DISCONNECT PLUG. REFERENCE CONTROL NR 95ZZZX6134. 2H72 4T4 TRTA13NM E20NE 19951113001091995111300109NM 1995 11 13 95ZZZX6134 119950929A6123954215B653323 AUTOFEATHER SW DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE COCKPIT FAILED A HNAAK NONE N FALSE WARNING TOTAKEOFF 1 EA07925HA19511 111 TPA/MIA - FLT 3005 - THE AUTOFEATHER ARM LIGHT FLICKERED AND WENT OUT DURING TAKEOFF. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE PROPELLER AUTOFEATHER SWITCH AND THE NR 1 BRAIDED ENGINE HARNESS FROM FIREWALL TO EEC DISCONNECT PLUG. REFERENCE CONTROL NR 95ZZZX6133. 2H72 4T4 TRTA13NM E20NE 19951113001101995111300110NM 1995 11 13 95ZZZX6135 119951013A3244 TIRES BOEING747 747131 1384881NM NR 7 OVERLOAD A EIAAJA DUMP FUEL UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM09472EV 9 20320 HNL - LOG PAGE F03682 - AFTER V1 ANTI-SKID LIGHT ILLUMINATED, 10 SECONDS AFTER ROTATION LOSS OF HYD SYS 1, 15 SECONDS LATER LOSS OF HYD SYS 4. DURING ALTERNATE FLAP EXTENSION, INBOARD FLAPS WOULD NOT EXTEND BEYOND 18 DEGREES. RECYCLED ALT INBD T/E FLAP C/B SEVERAL TIMES. TOOK 10 MINUTES TO GET FLAPS FROM 18 DEGREES TO 25 DEGREES. FUEL DUMP OF 108,000 POUNDS FOR A LANDING WEIGHT OF 570,000 POUNDS. REPLACED BLOWN TIRES NR 8 AND NR 7 DUE OVERLOAD PER MM 32-45-01. BLOWN TIRE CAUSED EXCESSIVE DAMAGE. REFERENCE CONTROL EIAA9545. (X) 2L74 4F A20WE 19951113001111995111300111NM 1995 11 13 95ZZZX6136 119951017A3244 TIRE BOEING747 747131 1384881NM NR 7 OVERLOAD A EIAAO OTHER O OTHER TOTAKEOFF 1 NM09472EV 5 20320 STU - LOGPAGE F03686 - NR 8 TIRE SHREDDED ON DEPARTURE HNL, NR 6 TIRE DEFLATED AFTER BLOCK IN STU. TIRE DID NOT ROTATE AFTER DEFLATION. NR 7 TIRE OVERLAODED DUE TO FAILURE OF NR 8. REPLACED BLOWN TIRE, TIRES NR 8 AND NR 7 DUE OVERLOAD, AND TIRE NR 6 FOR DEFLATION PER MM 32-45-01. REFERENCE CONTROL NR EIAA9546, AND NR 95ZZZX6137. (X) 2L74 4F A20WE 19951113001121995111300112NM 1995 11 13 95ZZZX6137 119951017A3244 TIRE BOEING747 747131 1384881NM NR 6 DEFLATED A EIAAO OTHER O OTHER TOTAKEOFF 1 NM09472EV 20320 STU - LOG PAGE F03686 - NR 8 TIRE SHREDDED ON DEPARTURE HNL, NR 6 TIRE DEFLATED AFTER BLOCK IN STU. TIRE DID NOT ROTATE AFTER DEFLATION. NR 7 TIRE OVERLAODED DUE TO FAILURE OF NR 8. REPLACED BLOWN TIRE, TIRES NR 8 AND NR 7 DUE OVERLOAD, AND TIRE NR 6 FOR DEFLATION PER MM 32-45-01. REFERENCE CONTROL NR EIAA9546, AND NR 95ZZZX6136. (X) 2L74 4F A20WE 19951113001131995111300113NM 1995 11 13 95ZZZX6138 119951022A28222580005 BOOST PUMP BOEING737 7372E3 NM TANK 1 FWD FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28138AW 1000367 22792 ABQ - FLT 0592 - MCI/PHX; CREW OBSERVED CENTER TANK FUEL QUANTITY INCREASING, AND RT CENTER BOOST PUMP CIRCUIT BREAKER TRIPPED. ACFT DIVERTED TO ABQ AND LANDED WITHOUT FURTHER INCIDENT. UMSR 28-01 WAS ISSUED. ACFT RETURNED TO PHX. MX REMOVED AND REPLACED TANK 1 AFT BOOST PUMP, TANK 1 FWD BOOST PUMP, CENTER TANK RIGHT BOOST PUMP CHECK VALVE, AND TANK 1 FORWARD BOOST PUMP CHECK VALVE. OPS CHECK OK. ACFT RETURNED TO SERVICE. REFERENCE CONTROL NR AWXA 9500719, NR 95ZZZX6139 AND NR 95ZZZX6140. (X) 2L72 4F RTA16WE 19951113001141995111300114NM 1995 11 13 95ZZZX6139 119951022A282020C1444 CHECK VALVE BOEING737 7372E3 NM CENTER RIGHT FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28138AW 3116 22792 ABQ - FLT 0592 - MCI/PHX; CREW OBSERVED CENTER TANK FUEL QUANTITY INCREASING, AND RT CENTER BOOST PUMP CIRCUIT BREAKER TRIPPED. ACFT DIVERTED TO ABQ AND LANDED WITHOUT FURTHER INCIDENT. UMSR 28-01 WAS ISSUED. ACFT RETURNED TO PHX. MX REMOVED AND REPLACED TANK 1 AFT BOOST PUMP, TANK 1 FWD BOOST PUMP, CENTER TANK RIGHT BOOST PUMP CHECK VALVE, AND TANK 1 FORWARD BOOST PUMP CHECK VALVE. OPS CHECK OK. ACFT RETURNED TO SERVICE. REFERENCE CONTROL NR AWXA 9500719, NR 95ZZZX6138, AND NR 95ZZZX6140. (X) 2L72 4F RTA16WE 19951113001151995111300115NM 1995 11 13 95ZZZX6140 119951022A282020C1444 CHECK VALVE BOEING737 7372E3 NM TANK 1 FWD FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28138AW 3116 22792 ABQ - FLT 0592 - MCI/PHX; CREW OBSERVED CENTER TANK FUEL QUANTITY INCREASING, AND RT CENTER BOOST PUMP CIRCUIT BREAKER TRIPPED. ACFT DIVERTED TO ABQ AND LANDED WITHOUT FURTHER INCIDENT. UMSR 28-01 WAS ISSUED. ACFT RETURNED TO PHX. MX REMOVED AND REPLACED TANK 1 AFT BOOST PUMP, TANK 1 FWD BOOST PUMP, CENTER TANK RIGHT BOOST PUMP CHECK VALVE, AND TANK 1 FORWARD BOOST PUMP CHECK VALVE. OPS CHECK OK. ACFT RETURNED TO SERVICE. REFERENCE CONTROL NR AWXA 9500719, NR 95ZZZX6138, AND NR 95ZZZX6139. (X) 2L72 4F RTA16WE 19951113001161995111300116NM 1995 11 13 AWXA9500719 119951022A28222580005 BOOST PUMP BOEING737 7372E3 NM TANK 1 AFT FAILED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28138AW 10130221B 22792 ABQ - FLT 0592 - MCI/PHX; CREW OBSERVED CENTER TANK FUEL QUANTITY INCREASING, AND RT CENTER BOOST PUMP CIRCUIT BREAKER TRIPPED. ACFT DIVERTED TO ABQ AND LANDED WITHOUT FURTHER INCIDENT. UMSR 28-01 WAS ISSUED. ACFT RETURNED TO PHX. MX REMOVED AND REPLACED TANK 1 AFT BOOST PUMP, TANK 1 FWD BOOST PUMP, CENTER TANK RIGHT BOOST PUMP CHECK VALVE, AND TANK 1 FORWARD BOOST PUMP CHECK VALVE. OPS CHECK OK. ACFT RETURNED TO SERVICE. REFERENCE CONTROL NR 95ZZZX6138, NR 95ZZZX6139, AND NR 95ZZZX6140. (X) 2L72 4F RTA16WE 19951113001171995111300117NE 1995 11 13 AWXA9500720 219951023A7320 ENGINE BOEING737 7373G7 1384595NM GE CFM56 CFM563B1 13802NE POWER CONTROL REQ RERIG A AWXAA UNSCHED LANDING MR OVER TEMP PARTIAL RPM/PWR LOSS CLCLIMB 1 WP28155AW 23777 PHX - FLT 226 - AIR TURN-BACK. CREW REPORTED NR 2 ENGINE OVERTEMP ON TAKEOFF, AND UNABLE TO MAINTAIN CLIMB POWER. HAD 4 KNOB THROTTLE SPLIT. ACFT RETURNED TO PHX FOR MX TROUBLESHOOTING. MX PERFORMED PART POWER RIG AND POWER ASSURANCE TEST ON BOTH ENGINES. BOTH ENGINE PARAMETERS WITHIN MM LIMITS. ACFT RELEASED FOR SERVICE. (X) 2L72 4F4 FRTA16WE E2GL 19951113001181995111300118NM 1995 11 13 CAL950847 119950921A2530416100129 COFFEEMAKER BOEING737 737524 1384721NM NR 2 INOPERATIVE A CALAHF DEACTIVATE SYST/CIRCUITSACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW09326261279 27530 ORD - FLT 1616 - THE AFT NR 2 COFFEEMAKER BEGAN TO SMOKE IN-FLIGHT. THE SMOKE CEASED AFTER PULLING THE CIRCUIT BREAKER AND USING THE FIRE EXTINGUISHER. THE NR 2 AFT COFFEEMAKER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. THERE WERE NO OTHER DISCREPANIES NOTED. IN ADDITION, THE AFT FIRE EXTINGUISHER WAS REPLACED. (X) 2L72 4F RTA16WE 19951113001191995111300119NM 1995 11 13 CAL950881 119950930A55106547985504 HORIZ STAB BOEING737 737524 1384721NM RIGHT DENTED A CALAK NONE C F.O.D. ININSP/MAINT 1 SW09166173177 27330 IAH - INSPECTION FOUND THE HORIZONTAL STABILIZER RIB CORD AND SKIN DENTED ON INBOARD RT SIDE CAUSED BY A BIRD STRIKE. (X) 2L72 4F RTA16WE 19951113001201995111300120NM 1995 11 13 CAL950901 119950913A5311 FRAME BOEING727 727232 1384082NM BS 560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW093378565448 20640 INSPECTION FOUND CORROSION ON THE FORWARD FRAME AT BS 560 IN THE FORWARD BILGE INTERIOR. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (X) 2L73 4F A3WE 19951113001211995111300121NM 1995 11 13 EIAA9545 119951013A3244 TIRES BOEING747 747131 1384881NM NR 8 BLOWN A EIAAJA DUMP FUEL UNSCHED LANDING KJFFLUID LOSS WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NM09472EV 9 20320 HNL - LOG PAGE F03682 - AFTER V1 ANTI-SKID LIGHT ILLUMINATED, 10 SECONDS AFTER ROTATION LOSS OF HYD SYS 1, 15 SECONDS LATER LOSS OF HYD SYS 4. DURING ALTERNATE FLAP EXTENSION, INBOARD FLAPS WOULD NOT EXTEND BEYOND 18 DEGREES. RECYCLED ALT INBD T/E FLAP C/B SEVERAL TIMES. TOOK 10 MINUTES TO GET FLAPS FROM 18 DEGREES TO 25 DEGREES. FUEL DUMP OF 108,000 POUNDS FOR A LANDING WEIGHT OF 570,000 POUNDS. REPLACED BLOWN TIRES NR 8 AND NR 7 DUE OVERLOAD PER MM 32-45-01. BLOWN TIRE CAUSED EXCESSIVE DAMAGE. REFERENCE CONTROL NR 95ZZZX6135. (X) 2L74 4F A20WE 19951113001221995111300122NM 1995 11 13 EIAA9546 119951017A3244 TIRE BOEING747 747131 1384881NM NR 8 BLOWN A EIAAO OTHER O OTHER TOTAKEOFF 1 NM09472EV 5 20320 STU - LOG PAGE F03686 - NR 8 TIRE SHREDDED ON DEPARTURE HNL, NR 6 TIRE DEFLATED AFTER BLOCK IN STU. TIRE DID NOT ROTATE AFTER DEFLATION. NR 7 TIRE OVERLAODED DUE TO FAILURE OF NR 8. REPLACED BLOWN TIRE, TIRES NR 8 AND NR 7 DUE OVERLOAD, AND TIRE NR 6 FOR DEFLATION PER MM 32-45-01. REFERENCE CONTROL NR 95ZZZX6136. AND NR 95ZZZX6137. (X) 2L74 4F A20WE 19951113001231995111300123NE 1995 11 13 EIAA9547 219951021A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 BIRD STRIKE A EIAAAJ UNSCHED LANDING DUMP FUEL C F.O.D. CLCLIMB 1 NM09479EV479498482 19898 685936 JFK - LOG PAGE F03795 - AT ROTATION, LOUD BANG, NR 2 ENGINE STALLED, EGT 1,000, SUSPECTED BIRD STRIKE. DUMPED 37,000 POUNDS FUEL. RETURNED TO JFK. PERFORMED BIRD STRIKE AND OVERTEMP INSPECTIONS ON COMPRESSOR STAGE 1,2,3,4,5,7,9,15, AND TURBINE STAGE 1,2,3 PER MM 72-00-00. NIL DEFECTS, ITEM TRANSFERRED TO COI 003 FOR 80-HOUR FLT LIMIT PER MM 71-00-00, PAGE 220, FIG 205. (X) 2L74 4F4 F A20WE E20EA 19951113001241995111300124NE 1995 11 13 EIAA9548 219951021A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 DAMAGED A EIAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 NM09479EV479498482 19898 685936 JFK - LOG PAGE F03797 - OUT OF 19,000 FEET, NR 2 ENGINE STALLED, EGT CLIMBED TO 920 DEGREES, RETARDED THROTTLE TO IDLE, EGT DECREASED TO 640 DEGREES, N1 29 PERCENT, N2 70 PERCENT. AFTER 2 MINUTES, EGT DECREASED TO 340 DEGREES, ENGINE OPERATION AT IDLE NORMAL. RETURNED TO JFK, WHEN EGT WAS HIGH, VIBRATION WAS FELT FROM NR 2 ENGINE. CHANGED ENGINE NR 2 PER WORKCARD F7201/F7202/F7203/F7204, AND PERFORMED OPERATION CHECK PER WORKCARD F7207. (X) 2L74 4F4 F A20WE E20EA 19951113001251995111300125NM 1995 11 13 EIAA9549 119951020A2410 CSD O-RING BOEING747 747212B 1384886NM NR 1 LEAKING A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09485EV368078212 20712 JED - LOG PAGE 90728 - AFTER TAKEOFF AND CLIMB, NR 1 ENGINE OIL QUANTITY DECREASED TO ZERO AND OIL PRESSURE DROPPED TO 30 PSI, SHUT DOWN ENGINE. CHECKED ENGINE NR 1 MCD, NORMAL. REPLACED MAIN OIL FILTER, REPLACED CSD O-RINGS PER MM 24-11-01, REPLACED GENERATOR GARLOCK SEAL PER MM 72-61-08. OPS AND LEAK CHECKS PERFORMED PER MM 71-00-00. (X) 2L74 4F A20WE 19951113001261995111300126WP 1995 11 13 EIAA9550 119951020A3230 RETRACT MECH DOUG DC9 DC932F 3022067WP NLG OUT OF ADJUST A EIAAO OTHER J WARNING INDICATION APAPPROACH 1 NM09932F 45491 47355 SEA - LOG PAGE F05757 - AFTER TAKEOFF, NOSE GEAR UNSAFE LIGHT CAME ON. RECYCLED GEAR, NO HELP. COULD SEE DAYLIGHT AND NOSE GEAR WAS PRESENT THROUGH PEEPHOLE. INSPECTION REVEALED NOSE GEAR RETRACTED ACTUATING CYCLINDER OUT OF RIG. ADJUSTED PER MM 32-32-06, SWUNG GEAR, OPS CHECK GOOD, NIL DEFECTS NOTED. INSPECT NOSE GEAR DOOR AND LINKAGE PER MM 32-22-01, NIL DEFECTS. (X) 2L72 4F A6WE 19951113001271995111300127WP 1995 11 13 GRAA9543 119950910A2420976J3646 GEN CONTL UNIT DOUG DC9 DC915 3022036WP E/E BAY MALFUNCTIONED A GRAAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 WP111070T 45784 STS - UPON DESCENT, LT GENERATOR FEEDER FAULT, LT GENERATOR OFF, AND AC CROSS-TIE LOCKOUT ANNUNCIATOR LIGHTS ILLUMINATED. LOST LT SIDE ELECTRONICS. AIRCRAFT DIVERTED TO RNO. MAINTENANCE REPLACED LT GENERATOR CONTROL PANEL, LT BUSS PROTECTION PANEL, AND LT GENERATOR POWER RELAY. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE ELECTRICAL SYSTEM. OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. REF CONTROL NR 95ZZZX6099, AND CONTROL NR 95ZZZX6100. (X) 2L72 4F A6WE 19951113001281995111300128WP 1995 11 13 HAL95137 119951017A3350 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13420EA 47689 HNL - INFORMATION FROM LOG PAGE 143713-2. BOTH AFT OVERWING EMERGENCY LIGHTS VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2L72 4F A6WE 19951113001291995111300129WP 1995 11 13 IXXA199579 119950922A3260 UPLOCK SWITCH DOUG DC8 DC871 302199AWP LT MLG BENT PIN A IXXAO OTHER N FALSE WARNING CLCLIMB 1 GL23824BX 45946 ORD/PDX - ON TAKEOFF, CREW REPORTED WITH LANDING GEAR HANDLE UP, LANDING GEAR UNSAFE LIGHT REMAINED ON. CREW RECYCLED GEAR HANDLE AND IT OPERATED NORMALLY. ON APPROACH TO PDX, GEAR EXTENDED NORMALLY. CREW DID OPS CK AND RETRACTED GEAR. WITH GEAR HANDLE UP, THE DOORS LIGHT AND LT GEAR UNSAFE LIGHTS REMAINED ON. LANDING GEAR EXTENDED NORMALLY. MAINTENANCE REPAIRED A BENT PIN ON THE LT GEAR UPLOCK SWITCH AND CLEANED WATER FROM GEAR DOOR SWITCH. OPERATIONAL CHECK NORMAL PER DACO MM. AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19951113001301995111300130EU 1995 11 13 JBXA9500001 119950921A261251218701 FIRE LOOP FOKKERF28 F28MK0100 4990807EU APU COMPARTMENT OUT OF POSITION A JBXAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 GL31103ML 11444 DCA/RDU - FLT 802 - APU FIRE WARNING ON DESCENT INTO RDU. AGENT LOW LIGHT ILLUMINATED. MANUALLY DISCHARGED AGENT TO ENSURE PROCEDURE COMPLETED. INSPECTION REVEALED NO FIRE HAD OCCURRED. REPOSTIONED APU FIRE LOOP AND REPLACED FIRE EXTINGUISHER BOTTLE. (X) 2L72 4F RT 19951113001311995111300131WP 1995 11 13 ORJA9586 119950918A32462601483 BOLT BENDIX 2688911 DOUG DC9 DC982 3022082WP NR 2 MAIN WHEEL BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11824RA 4809 53017 NR 2 MAIN WHEEL ASSY, BROKEN WHEEL BOLT. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSY DUE TO BROKEN WHEEL BOLT. IAW MM 32. (X) 2L72 4F A6WE 19951113001321995111300132EU 1995 11 13 P2RA950016 119951018A2611605122 SMOKE DET AIRBUS300 A300B4203 3930306EU LAV 'F' WIRED WRONG A P2RAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 WP2314976 271 LIGHT OUTSIDE LAV 'F' AND F/A O/H DO NOT LIGHT WITH SMOKE DETECTOR TEST. FOUND PLUG BAD AND WIRED WRONG. REPLACED PLUG, LAV 'F' SMOKE DETECTOR SYSTEM, OPS CHK GOOD. (X) 2L72 4F A35EU 19951113001331995111300133CE 1995 11 13 PLGA108951 119951008A2750101521057T ASYMMETRY CAM BEECH 1900 1900C 1154161CE LT TE FLAPS WORN A PLGAA UNSCHED LANDING JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 NE05818BE UB61 BOS/LEB - FLT 4616 - EN ROUTE WHEN IT WAS NOTED THE FLAPS WOULD NOT RETRACT, AIRCRAFT DIVERTED INTO PSM. MAINTENANCE REMOVED AND REPLACED THE FLAP ASYMMETRY CAM AND FLAP SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE. (X) 2L72 4T RTA24CE 19951113001341995111300134CE 1995 11 13 PLGA10995E1 119951009A3260 EI BEECH 1900 1900C 1154161CE LANDING GEAR TRIPPED A PLGAO OTHER P NO WARNING INDICATION APAPPROACH 1 NE05808BE UB45 BOS/BDR - FLT 4343, BDR FROM BOS DID NOT GET 3 GREEN DOWN AND LOCKED LIGHTS WHEN GEAR WAS EXTENDED. CREW PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. THE LANDING GEAR E.I. WAS RESET AND ALL 3 GREEN LIGHTS, OPS CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE (X) 2L72 4T RTA24CE 19951113001351995111300135EU 1995 11 13 RAIA50919 119950914A5270 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR MALFUNCTIONED A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03555HK 41072 STL - FLT 7502 - CARGO DOOR LIGHT CAME ON. MAINTENANCE DEFERRED CARGO DOOR INDICATION PER MEL 52-3 CAT 3. (X) 2L72 4T RTA41NM 19951113001361995111300136EU 1995 11 13 RAIA950917 119950913A5270SP4594 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR DIRTY A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03555HK7 41072 STL - FLT 7017 - BAGGAGE LIGHT CAME ON AFTER DEPARTURE. MAINTENANCE CLEANED BAGGAGE DOOR MICROSWITCH. (X) 2L72 4T RTA41NM 19951113001371995111300137NM 1995 11 13 TSAA9525180 119951009A2530 COFFEE JUG BOEING737 7372Q9 138448MNM NR 6 SHORTED A TSAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP13809AL 21720 FLT 30 - PIREP 1 - SMOKE IN GALLEY COMING FROM COFFEE/HOT JUG AT L1H. ISOLATED TROUBLE TO NR 6 COFFEE JUG, JUG REMOVED. CIRCUIT BREAKER PULLED AND SWITCHED TO OFF FOR NR 6 COFFEE JUG RECEPTACLE. AIRCRAFT AND LOG BOOK PLACARDED PER MEL 25-10. HNL - REPLACED POWER RECEPTACLE, AND OPS CHK ACCOMPLISHED. PLACARDS REMOVED AND AIRCRAFT RETURNED TO SERVICE. TAT: 41,488.23 HRS. TAC: 48,948. (X) 2L72 4F A16WE 19951113001381995111300138NM 1995 11 13 TSAA9532181 119951009A3260 MODULAR UNIT BOEING737 7372S5C 1384499NM MLG DEFECTIVE A TSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13802AL 22148 FLT 216, PIREP NR 1 - AFTER TAKEOFF WITH LANDING GEAR HANDLE PLACED 'UP' THEN 'OFF', NOSE GEAR INDICATED UP AND LEFT AND RIGHT MAIN GEAR INDICATED DOWN (GREEN LIGHT ILLUMINATED) WITH BOTH GEAR UNSAFE (RED LIGHT ILLUMINATED). GEAR HANDLE PLACED DOWN AND RED LIGHTS WENT OUT. OVERHEAD GEAR LIGHTS REMAINED ON (GREEN) BEFORE AND AFTER GEAR HANDLE PLACED DOWN. UNEVENTFUL LANDING-HNL. MX ACTION: RETRACTION CHK NORMAL. REPLACED 'A' SYS MODULAR PACKAGE, GEAR RETRACTION CHECK OK. AIRCRAFT RETURNED TO SERVICE. TAT: 27,302.37 HRS. TAC: 49,187. (X) 2L72 4F RTA16WE 19951113001391995111300139NM 1995 11 13 TSAA9553175 119950920A5311 FRAME BOEING737 737297 1384480NM BS 400 LT CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP1370723 21739 DURING HEAVY MAINTENANCE VISIT, FOUND FWD CARGO COMPARTMENT LEFT SIDE FRAME AT BS 400 ABOVE S24L CRACKED. REPAIRED PER SRM 53-10-4. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19951113001401995111300140NM 1995 11 13 TSAA955317U 119950920A5320 T-BRACKET BOEING737 737297 1384480NM BS 178 LT CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP1370723 21739 DURING HEAVY MAINTENANCE VISIT, FOUND BS 178 LOWER T-BRACKET CRACKED, LEFT SIDE. REPAIRED PER ECO 2518R1. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19951113001411995111300141NE 1995 11 13 UIEA9502 219951110A72509299M30G09R BLADE BOEING747 747230B 1384889NM GE CF6 CF650E2 30018NE HPT FRACTURE A UIEAEAJFENGINE SHUTDOWN UNSCHED LANDING DUMP FUEL ACTIVATE FIRE EXT. AEKFLAME/FIRE VIBRATION/BUFFET FLUID LOSS CLCLIMB 1 EA15509MC24031112 21221 455833 ENGINE, SN 455833, TEAR DOWN REVEALED CONSIDERABLE TURBINE DAMAGE. HPT STAGE 1 BLADES METALLURGICAL ANALYSIS FOR PRIMARY FAILURE MODE. ONE BLADE FOUND WITH FAILURE PATTERNS IN THE TRAILING EDGE AREA. BLADE, PN 9299M30G09R, SN KTWD2263, REPAIR HISTORY M1K-M2K-M3K-M4H, TSN/CSN, 24,031 HOURS/5,199 CYCLES. BLADES EXHIBITED 2 FAILURE MODES - 1 TRAILING EDGE CRACKING AND SEPARATION, 2 INTERGRANULAR OXIDATION (IGO) ON INNER PASSAGE WALLS. BLADE ANALYSIS REVEALED PRESENCE OF MISLOCATED COOLING HOLE ON BLADE CONVEX SIDE WITHOUT INTERSECTING BLADE INNER OR OUTER WALLS. THE PRIMARY BLADE FAILURE ATTRIBUTED MORE TO INTERGRANULAR OXIDATION DUE TO LACK OF INTERNAL COATING. (X) 2L74 4F4 F A20WE E23EA 19951113001421995111300142EU 1995 11 13 VTZA96010 119951019A7714AG34 TACH GENERATOR BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27480UE 894 IAD/RON - FLT 6459 - DURING CLIMB-OUT AT 1510 HRS ON 10-19-95, RETURNED TO IAD DUE TO THE RT ENGINE RPM FLUCTUATION. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE TACH GENERATOR. ALL OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19951113001431995111300143NE 1995 11 13 VTZA96011 219951020A732031058691 PRESS TRANSDUCER JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE FAILED A AVTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27311UE 291 41029 P76080 IAD/DAY - FLT 6250 - DURING CLIMB-OUT AT 1750 HRS ON 10-20-95, AIRCRAFT RETURNED TO IAD DUE TO RT IEC CAP LIGHT ILLUMINATING. ENGINE WAS ALSO SLOW TO MAKE TAKEOFF TORQUE. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE DELTA P OVER P TRANSDUCER. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. TSI - 143.8 HOURS. (X) 2L72 4T4 TRTA41NM E18NE 19951113001441995111300144NE 1995 11 13 VTZA96012 219951020A73203105900S FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE OUT OF ADJUST A AVTZAD RETURN TO BLOCK X ENGINE FLAMEOUT TXTAXI/GRND HDL 1 EA27310UE 41028 P75049 IAD/EWR - FLT 6150 - DURING TAXI AT 0718 HRS ON 10-20-95, RETURNED TO GATE DUE TO LT ENGINE FLAMING OUT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED DECELERATION SCHEDULE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19951113001451995111300145EU 1995 11 13 VTZA96014 119951020A2422PC125123B INVERTER JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27319UE 41042 IA/RDU - FLT 6323 - DURING CRUISE AT 1913 HRS ON 10-20-95, RETURNED TO IAD DUE TO THE LT INVERTER FAILING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED INVERTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951113001461995111300146WP 1995 11 13 9517219949 119951012A5330 SKIN DOUG DC9 DC931 3022065WP FS 980 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .5 INCH LONG CRACKS IN THE FUSELAGE SKIN AND A PYLON ATTACH ANGLE AT A COMMON FASTENER HOLE. REPAIRED BOTH PER EA 99-102923. 2L72 4F A6WE 19951113001471995111300147WP 1995 11 13 9517229949 119951012A5320 CORNER DOUG DC9 DC931 3022065WP DOOR JAMB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 2.6 INCH CRACK IN THE FORWARD SERVICE DOOR JAMB UPPER FORWARD CORNER. REPAIRED THE JAMB PER EA 99-102680. 2L72 4F A6WE 19951113001481995111300148WP 1995 11 13 9517239949 119951013A5312 BLKHD WEB DOUG DC9 DC931 3022065WP FS 1038 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018928E 45865 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 1038 BULKHEAD WEB, BETWEEN LONGERONS 7L TO 12L. REPAIRED WEB (P/N 9912246-17), PER EA 99-102958. 2L72 4F A6WE 19951113001491995111300149WP 1995 11 13 9517249603 119951027A5320 FITTING DOUG DC9 DC932 3022066WP FS 1104-1121 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 12L END FITTING AT FS 1104 TO 1121. REPLACED THE END FITTING PER SRM 53-02 AND 51-30. 2L72 4F A6WE 19951113001501995111300150WP 1995 11 13 9517259864 119951027A5320 FITTING DOUG DC9 DC951 3022051WP FS 1167 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 22R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951113001511995111300151WP 1995 11 13 9517269972 119951029A5312 BLKHD PANEL DOUG DC9 DC931 3022065WP FS 83 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019336 47338 DURING L-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 83 PRESSURE PANEL, LEFT SIDE. REPAIRED PER EO 5310-01134. 2L72 4F A6WE 19951113001521995111300152WP 1995 11 13 9517279864 119951007A5350 CABLE DOUG DC9 DC951 3022051WP TAIL CONE FRAYED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAIL CONE. ALSO, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS AND THAT CABLE RUN 301A WAS FRAYED. ADJUSTED THE CLIPS/RELEASE SYSTEM AND REPLACED THE CABLE, CHECKED OK. 2L72 4F RTA6WE 19951113001531995111300153WP 1995 11 13 9517289866 119951102A2760 MECHANISM DOUG DC9 DC951 3022051WP SPOILER LACK OF LUBE A NWAAO OTHER F FLT CONT AFFECTED DEDESCENT 1 GL01775NC 47785 DURING DESCENT WITH SPEED BRAKE FULLY EXTENDED, THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. CREW DISCONNECTED AUTOPILOT AND RETRACTED SPEED BRAKES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND ACCUMULATION OF ICE IN THE RIGHT SPOILER CONTROL. REMOVED THE ICE AND LUBRICATED THE SYSTEM, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113001541995111300154WP 1995 11 13 9517299966 119951102A3260 DNLOCK SW DOUG DC9 DC931 3022065WP RT MLG MALFUNCTIONED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL019330 47138 DURING APPROACH, THE RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. CREW RECYCLED THE LANDING GEAR AND THE LIGHT STILL DID NOT ILLUMINATE. CREW USED PERISCOPE TO VERIFY THE RIGHT MAIN LANDING GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113001551995111300155WP 1995 11 13 9517309604 119951101A3350 BATTERY PACK DOUG DC9 DC932 3022066WP NACELLE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01604NW 47222 DURING LINE CHECK, THE TAIL CONE FLOODLIGHTING FAILED TEST. REPLACED THE NACELLE LIGHT BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113001561995111300156WP 1995 11 13 9517319604 119951101A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01604NW 47222 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS AT ROWS 9 TO 12 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113001571995111300157WP 1995 11 13 9517329751 119951102A3350 BATTERY PACK DOUG DC9 DC941 302207NWP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01751NW 47115 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT SEVERAL ROWS INOPERATIVE. REPLACED THREE SETS OF BATTERY PACKS, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113001581995111300158NM 1995 11 13 9517336305 119951102A3234 CONTL HANDLE BOEING747 747451 1384940NM LANDING GEAR MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01665US 23820 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR HANDLE, SELECTED OVERRIDE AND GEAR RETRACTED NORMALLY. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL HANDLE MODULE, RELAY R127, SWITCH S1340, AND THE LANDING GEAR CONTROL MODULE. OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951113001591995111300159NM 1995 11 13 9517342289 119951105A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01289US 21377 DURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHT IN AFT VENTRAL STAIRS INOPERATIVE. REPLACED BATTERY PACK, CHECKED NORMAL. 2L73 4F A3WE 19951113001601995111300160NM 1995 11 13 95FDEA01654 119951102A5320 DOOR SILL WEB BOEING727 72722 1384002NM BS 1070 BUCKLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR 0654, FOUND DOOR SILL WEB BUCKLED AT BS 1070 RBL 22 WL 152.5. 2L73 4F A3WE 19951113001611995111300161NM 1995 11 13 95FDEA01659 119951102A53156517543 FLOORBEAM BOEING727 72722 1384002NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-224-02), AROUND NUTPLATE HOLES AT BS 312 LBL 2 TO 18 WL 208.1. 2L73 4F A3WE 19951113001621995111300162NM 1995 11 13 95FDEA01672 119951103A5330MA489506 SKIN BOEING727 727233 138408ANM BS 703 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25267FE 21673 CORROSION ON INTERIOR SHIP SURFACE AT BS 703, BL O AROUND NUTPLATES. CUT OUT CORRODED SKIN THAT WAS BEYOND LIMITS PER FEDEX SRM 53-30-4, INSTALLED DOUBLER PER FEDEX SRM 53-30-8, CLEANED AND TREATED AREA. 2L73 4F RTA3WE 19951113001631995111300163 1995 11 13 95FDEA01673 219951101A7200 TURBINE BOEING727 7272S2F 1384O81NM NR 2 ENGINE FAILED A AFDEACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 SO25209FE 22931 DURING LOW SPEED TAKEOFF ROLL, ALOUD POP/SHUDDER OF THE AIRCRAFT WAS FELT WITH A SIMULTANEOUS ENGINE FAIL LIGHT ILLUMINATION. A REJECTED TAKEOFF WAS ACCOMPLISHED. AIRCRAFT WAS TAXIED BACK TO RAMP, WITH MAINTENANCE PERSONNEL IN COCKPIT. THE NR 2 ENGINE WAS ADVANCED TO FULL THROTTLE, BUT EPR DID NOT GO PAST 1.9, A COMPRESSOR STALL WAS FELT AGAIN AND NR 2 ENGINE WAS SHUTDOWN. INSPECTION NR 2 ENGINE TAIL PIPE FOUND LOW PRESSURE TURBINE FAILURE. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD NR 70T0002. 2L73 4F A3WE 19951113001641995111300164WP 1995 11 13 95FDEA01674 119951102A3260 SWITCH ACTUATOR DOUG DC10 DC1010F 3022111WP LANDING GEAR DAMAGED A FDEAO OTHER N FALSE WARNING CLCLIMB 1 SO2510060 46970 AFTER TAKEOFF WITH GEAR HANDLE UP, GOT THREE RED GEAR INDICATORS WITH GEAR HORN. CYCLED GEAR 2 TIMES, NO CHANGE. COMPLIED WITH EMERGENCY PROCEDURES. FOUND LANDING GEAR SWITCH 5341 ACTUATOR DAMAGED. REMOVED AND REPLACED SWITCH ACTUATOR 5341 PER M/M 76-11-04. OPS CHECKED NORMAL. 2L73 4F A22WE 19951113001651995111300165NM 1995 11 13 95FDEA01675 119951102A2750MS939110ZE4C DRIVE MOTOR BOEING727 727233 138408ANM FLAP SYST LEAKING A FDEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO25219FE 21102 LOSS OF SYSTEM-A OCCURRED 30 MINUTE AFTER TAKEOFF. RAN CHECK LIST VERIFIED SYSTEM-A LEAK. SHUT-OFF BOTH SYSTEM-A FLUID SHUT-OFF SWITCHES. LEAK/FLUID LOSS STOPPED WITH LESS THAN 1 GALLON. REMOVED 40 DEGREE FLAP STOP, REMOVED AND REPLACED HYDRAULIC FLAP DRIVE MOTOR AND SERVICED A-SYSTEM HYDRAULIC. REMOVED AND REPLACED A-SYSTEM CASE DRAIN FILTERS ON NR 1 AND NR 2 MOTORS. REMOVED AND REPLACED A-SYSTEM PRESSURE FILTER ON A-SYSTEM MODULAR UNIT PER MM 29-11-62 PG 301. NO METAL FOUND, CHECKS GOOD, INTALLED FLAP STOP. 2L73 4F RTA3WE 19951113001661995111300166WP 1995 11 13 95FDEA01676 119951102A5743 BUSHING DOUG DC10 DC1010F 3022111WP RT MLG TRUNNION MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RT MAIN LANDING GEAR WING TRUNNION AFT FITTING, AFT LUG BUSHING MIGRATED FWD OUT OF LUG. FOUND THAT AFT LUG BUSHING WAS A SPACER AND NOT A TRUNNION BUSHING MIGRATING OUT, REF DAC B/P 3800, DC10 MM 32-11-01 FIG 106, OK'ED FOR SERVICE. RESEALED SPACER PER DAC B/P ARB 3800. 2L73 4F A22WE 19951113001671995111300167WP 1995 11 13 95FDEA01677 119951102A5743 BUSHING DOUG DC10 DC1010F 3022111WP RT MLG TRUNNION MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RT MAIN LANDING GEAR WING TRUNNION AFT FITTING, AFT LUG BUSHING MIGRATED FWD OUT OF LUG. FOUND THAT AFT LUG BUSHING WAS A SPACER AND NOT A TRUNNION BUSHING MIGRATING OUT, REF DAC B/P 3800, DC10 MM 32-11-01 FIG 406, OK'ED FOR SERVICE. RESEALED SPACER PER DAC B/P ARB 3800. 2L73 4F A22WE 19951113001681995111300168WP 1995 11 13 95FDEA01678 119951102A5743 BUSHING DOUG DC10 DC1010F 3022111WP RT MLG MIGRATED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568057 48264 RT MAIN LANDING GEAR WING TRUNNION AFT FITTING, AFT LUG BUSHING MIGRATED FWD OUT OF LUG. FOUND THAT AFT LUG BUSHING WAS A SPACER AND NOT A TRUNNION BUSHING MIGRATING OUT, REF DAC B/P 3800, DC10 MM 32-11-01 FIG 409, OK'ED FOR SERVICE. RESEALED SPACER PER DAC B/P ARB 3800. 2L73 4F A22WE 19951113001691995111300169NM 1995 11 13 95UAL900248 119951106A2750 HYD MOTOR MS939113ZE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE TE FLAPS FAILED A UALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP297256U MX94951A 21403 HYDRAULIC SYSTEM 'A' DROPPED TO ZERO QUANTITY AND ZERO PRESSURE SHORTLY AFTER TAKEOFF. REPLACED TRAILING EDGE FLAP HYDRAULIC MOTOR DUE TO SHAFT SEAL LEAKAGE. 2L73 4F4 F A3WE E2EA 19951113001701995111300170NM 1995 11 13 95UAL900249 119951106A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297292U 21570 EMERGENCY ESCAPE LIGHTING EXIT LIGHT INOP, DOOR 1 LEFT. 2L73 4F4 F A3WE E2EA 19951113001711995111300171NM 1995 11 13 DHL95742002 119951102A7722 CONNECTOR BOEING727 7272Q9 138448MNM NR 2 EGT LOOSE A TDHLAAJ UNSCHED LANDING DUMP FUEL O OTHER CLCLIMB 1 SO01742DH 21290 THE NR 2 EGT INOP, DUMPED FUEL, PERFORMED AIR TURNBACK. REPLACED K AND L SOCKETS IN CONNECTOR D376J. ALL OTHER CONNECTORS CLEANED AND RESECURED, PERFORMED EGT CHECK PER JRH 06-01 AND NR 2 EGT CHECKS NORMAL. 2L73 4F RTA3WE 19951113001721995111300172NM 1995 11 13 SCNA95255 119951102A32325144 HARNESS BOEING727 727259 138408JNM NLG INDICATION CHAFED A SCNAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15289SC 22475 NOSE GEAR INDICATION PROBLEM WAS NOTED DURING GEAR RETRACTION, AIRCRAFT RETURNED TO STATION. WHEN THE GEAR WAS LOWERED ALL INDICATIONS WERE NORMAL. DURING POST FLIGHT INSPECTION THE LOWER LINK ATTACH BOLT (NAS-104-47W), WAS FOUND CRACKED. THE BOLT WAS REPLACED. ALSO, WIRE BUNDLE 5144 WAS FOUND CHAFED AGAINST THE NUMBER 1 HIGH FREQUENCY TRANSCEIVER AND WORN THROUGH CAUSING THE NOSE GEAR INDICATION PROBLEM. REPAIRED AND REROUTED THE HARNESS, SYSTEM TESTED GOOD DURING THE NOSE GEAR SWING. 2L73 4F A3WE 19951113001731995111300173NM 1995 11 13 SCNA95256 119951102A2612106109624 FIRE LOOP BOEING727 7272A1 138407FNM NR 1 ENGINE OIL CAKED A SCNAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 GL15286SC 21601 THE NUMBER 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL RANG DURING GROUND OPERATIONS. ALL ENGINE INDICATIONS WERE NORMAL. THE ENGINE WAS SHUTDOWN. DURING INSPECTION TWO CONNECTORS FOR FIRE LOOP IN STUB WING WERE FOUND OIL CAKED CAUSING FALSE FIRE INDICATION. CLEANED CONNECTORS AND SYSTEM CHECKED GOOD IAW MM 26-11-01, RAN ENGINE AT TAKEOFF POWER AND SYSTEM TESTED GOOD. 2L73 4F A3WE 19951113001741995111300174NM 1995 11 13 SCNA95257 119951101A33506104781 EEL POWER SUPPLY BOEING727 7272A1 138407FNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE EMERGENCY EXIT ESCAPE SLIDE LIGHTS AT THE L2 AND R2 DOOR WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED AFT EMERGENCY EXIT SLIDE LIGHTS POWER SUPPLY PER MM 33-50-51, OPS CHECK GOOD. 2L73 4F A3WE 19951113001751995111300175NM 1995 11 13 SCNA95258 119951102A33506013211 BATTERY PACK BOEING727 7272A1 138407FNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE EMERGENCY EXIT ESCAPE SLIDE LIGHTS AT THE L2 AND R2 DOOR WERE FOUND TO BE DIM. REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT EMERGENCY EXIT SLIDE LIGHTS, OPS CHECKED GOOD. 2L73 4F A3WE 19951113001761995111300176NM 1995 11 13 UPS204931 119951101A261365249203 OVERHEAT MODULE BOEING727 72762C 138402CNM NR 1 ENGINE MALFUNCTION A IPXAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 SO01912UP 19244 CREW REPORTED NR 1 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. APPROPRIATE CHECKLIST WAS PERFORMED AND ENGINE WAS SHUTDOWN. ACT NOTIFIED, EMERGENCY DECLARED AND FLIGHT PROCEEDED WITHOUT FURTHER EVENT TO DFW. REMOVED AND REPLACED OVERHEAT DETECTION MODULE PER MM 26-14-00, OPS TEST GOOD. REPAIRED CHAFED WIRE AT FWD PYLON LOOP FWD CONNECTOR IN STAIRWELL AREA, OPS CK NORMAL. 2L73 4F A3WE 19951113001771995111300177NM 1995 11 13 UPS204934 119951104A33501000679 EEL ASSY BOEING727 727247 138408FNM CABIN MALFUNCTIONED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01210UP 21697 CREW REPORTED, EMERGENCY EXIT LIGHTS VERY DIM. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. 2L73 4F A3WE 19951113001781995111300178NM 1995 11 13 UPS204935 119951102A33501000679 EEL ASSY BOEING727 72725C 138400HNM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01932UP 19856 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT WOULD NOT TEST DURING PREFLIGHT. REMOVED AND REPLACED EXIT LIGHT ASSEMBLY. 2L73 4F A3WE 19951113001791995111300179WP 1995 11 13 UPS804932 119951102A3231 RETRACT MECH DOUG DC8 DC873F 302199FWP RT MLG DOOR OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01807UP 46007 CREW REPORTED, AFTER TAKEOFF FROM HONOLULU ON GEAR RETRACTION, GEAR DOOR LIGHT ON FWD PANEL REMAINED ON, ALT LIGHTS OUT. RECYCLE GEAR, SAME RESULTS, UPLATCH CHECK LIGHT WENT OUT AND REMAINED OUT. REPLACED RT AND LT GEAR DOOR PROX SWITCHES AND WIRING. PERFORMED GEAR RETRACTION TEST AND UPLATCH TEST IAW M/M 32-31-04, ALL OPS CHECKS OK. 2L74 4F RT4A25 19951113001801995111300180WP 1995 11 13 UPS804933 119951103A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01866UP 45966 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN FLIGHT DECK INOP. REPLACED BATTERY PACK. 2L74 4F RT4A25 19951113001811995111300181WP 1995 11 13 UPS804936 119951106A57535701446 VANE DOUG DC8 DC871F 302199DWP RT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 3 FLAP VANE DELAMINATED ON TOP SIDE AT I/B END. REPLACED VANE IAW M/M 27-51-14. 2L74 4F RT4A25 19951113001821995111300182WP 1995 11 13 UPS804937 119951106A57535652288505 VANE DOUG DC8 DC871F 302199DWP LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 2 FLAP VANE DELAMINATED ON TOP SIDE AT I/B END. REPLACED VANE IAW M/M 27-51-14. 2L74 4F RT4A25 19951113001831995111300183WP 1995 11 13 UPS804938 119951106A57535701152501 VANE DOUG DC8 DC871F 302199DWP LT TE FLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 4 FLAP VANE DELAMINATED ON TOP CENTER SIDE. REPLACED VANE IAW M/M 27-51-14. 2L74 4F RT4A25 19951113001841995111300184WP 1995 11 13 UPS804939 119951106A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT AND RT FORWARD NOSE GEAR DOOR HINGE CUTOUTS HAVE .5 INCH CRACKS. REPAIRED SKIN IAW SRM 53-2-0, DC8-5330-4154B. 2L74 4F RT4A25 19951113001851995111300185WP 1995 11 13 UPS804940 119951106A5230 FRAME DOUG DC8 DC871F 302199DWP BAGGAGE DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND D-BAG/BIN DOOR LOWER AFT CORNER FRAME HAS 2 INCH CRACK. REPAIRED IAW UPS DC8-5230-6603A. 2L74 4F RT4A25 19951113001911995111300191SO 1995 11 13 95ZZZX6146 219951003A8540643259A17 ADAPTER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO LT ENG STARTER WORN A ABQTAK NONE O OTHER ININSP/MAINT 1 NE05404BA300 4040237 276151R INSPECTED BOTH STARTER ADAPTERS AND FOUND THEM WORN BEYOND LIMITS PER SB MEB 94-4. THIS PART IS THE NEW IMPROVED STYLE ADAPTER AND DOES NOT REQUIRE ANY FURTHER INSPECTIONS. 1L72 3O3 O A25CE E7CE 19951113001921995111300192SO 1995 11 13 95ZZZX6147 219951003A8540643259A17 ADAPTER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO RT ENG STARTER WORN A ABQTAK NONE O OTHER ININSP/MAINT 1 NE05404BA420 4040237 276457R INSPECTED BOTH STARTER ADAPTERS AND FOUND THEM WORN BEYOND LIMITS PER SB MEB 94-4. THIS PART IS THE NEW IMPROVED STYLE ADAPTER AND DOES NOT REQUIRE ANY FURTHER INSPECTIONS. 1L72 3O3 O A25CE E7CE 19951113001931995111300193EA 1995 11 13 95ZZZX6148 219951016A8540 BEARING BNORM BN2 BN2A26 1520226EU LYC O540 O540E4C5 41532EA MAG DRIVE FAILED A DCRAK NONE O OTHER ININSP/MAINT 1 WP1326MR 882 1243340A DURING ROUTINE OIL CHANGE, FND METAL PIECES OF BALL BEARING CAGE IN SUCTION SCREEN. REMOVAL OF LT MAG REVEALED ALMOST TOTAL FAILURE OF LT MAG DRIVE BRG & ITS SLEEVE IN CRANKCASE. SLEEVE HAD BEEN INSTALLED IAW LYC SI NR 1140 DURING ENG O\H. THIS IS 5TH FINDING OF THIS NATURE IN FLEET OF 6 AIRPLANES IN 12 MONTHS. PREV FINDINGS COINCIDED WITH C/W AD 78-09-7R3, BENDIX MAG IMPULSE COUPLING INSP. THIS LAST ENG DID NOT REQUIRE AD INSP DUE TO SLICK MAG INSTALL. SUBMITTER STATED FAILURE LEFT UNDETECTED COULD CAUSE TOTAL ENG FAILURE. UNNECESSARY C/W SI NR 1140, WHEN NOT NEEDED, IMPROPER FAB & FITTING OF SLEEVE IN CRANKCASE BY O/H MIGHT CAUSE FAILURES. ENG RETURNED TO O/H FOR REPAIRS. ENG TSOH 462.0 HRS. 1H72 3O3 O A17EU E295 19951113001961995111300196NM 1995 11 13 95ZZZX6151 119951001A5754 SLAT BOEING767 7673T7 1385201NM NR 5-8 DISBONDED B AQOCYK NONE O OTHER ININSP/MAINT 1 WP03602EV 25117 THE NR 5 AND NR 8 SLAT WEDGES DISBONDED. THE DAMAGE WAS SUSPECTED TO BE CAUSED BY MOISTURE IN THE SLAT CORE AND SUBSEQUENT CORE CORROSION AND WHEN SLAT IS IN STOW POSITION, IT PUSHES TOO HARD ON LEADING EDGE FIXED PANEL AND GENERATES EXTRA BENDING FORCE TO TRAILING EDGE WEDGE. FAA AD 93-14-19 WAS ISSUED AND METHOD FOR CORRECTION IS PROVIDED IN THE AD IAW BOEING SB 767-57A0039, REV 1. A CORROSION RESISTING BONDING MATERIAL SHOULD BE USED. 2L72 4F RTA1NM 19951113002201995111300220SO 1995 11 13 95ZZZX6175 219951013A8530653142 CYLINDER CESSNA207 T207 2073612CE CONT O520 TSIO520M 17040SO NR 4 HEAD CRACKED A GSUAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 WP193156X 1246 T20700376 522456 ROUGHLY 15 MINUTES INTO FLIGHT, THE ENGINE LOST MANIFOLD PRESSURE. MAXIMUM M/P WAS 25 INCHES. INSPECTION FOUND THE NR 4 CYLINDER CRACKED AND STARTING TO MELT THE NR 6 CYLINDER. 1H71 3O3 O A16CE E8CE 19951113002211995111300221EU 1995 11 13 9517353239 119951101A3260 TARGET AIRBUS320 A320211 3930320EU LT MLG DOOR LOOSE A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01339NW 367 DEN - DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR DOOR INDICATED IN TRANSIT AFTER LANDING GEAR WAS RETRACTED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO DTW WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR (27GA), TARGET LOOSE. TIGHTENED SAME AND ALL INDICATIONS WERE NORMAL. 2L72 4F RTA28NM 19951113002221995111300222NM 1995 11 13 9517362296 119951105A2131 CONTROLLER BOEING727 727251 138408HNM CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01296US 21788 DURING CLIMB, COULD NOT CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL. AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT. REPLACED THE MANUAL PRESSURE CONTROLLER, LEFT OUTFLOW VALVE AND AUTO PRESSURE CONTROLLER. PRESSURIZATION CHECK OK. 2L73 4F A3WE 19951113002231995111300223NM 1995 11 13 9517376613 119951103A335039B4601036 BATTERY PACK BOEING747 747251B 1384892NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01613US 20358 DURING CHECK, FOUND THE EMERGENCY LIGHT AT DOOR 5R INOPERATIVE. REPLACED THE BATTERY PACK, PERFORMED FUNCTIONAL CHECK AND UNIT CHECKED NORMAL. 2L74 4F A20WE 19951113002241995111300224WP 1995 11 13 9517389950 119951103A2750 RETRACT MECH DOUG DC9 DC932 3022066WP TE FLAPS LACK OF LUBE A NWAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 GL019346 47376 DURING CLIMB, AIRCRAFT EXPERIENCED A SLIGHT ROLL WHEN THE FLAPS WERE RETRACTED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. LUBRICATED FLAP SYSTEM AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113002251995111300225WP 1995 11 13 9517399912 119951105A2720 SWITCHES DOUG DC9 DC931 3022065WP RUDDER CONTROL DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01962N 47406 DURING TAKEOFF, THE FLAP/RUDDER STOP INOPERATIVE LIGHT ILLUMINATED AND CREW ABORTED TAKEOFF. INSPECTED AND CLEANED SYSTEM SWITCHES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113002261995111300226WP 1995 11 13 9517409970 119951104A3260 AIR GROUND RELAY DOUG DC9 DC931 3022065WP LANDING GEAR MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL019334 47247 DURING CRUISE, THE AIRCRAFT LOST PRESSURIZATION AT 23,000 FEET. CREW EMERGENCY DESCENDED TO 12,000 FEET AND CONTINUED TO DTW. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE AIR/GROUND RELAY (R2-4), OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113002271995111300227NM 1995 11 13 95FDEA01679 119951102A5320NAS6404U74 BOLTS DOUG MD11 MD11 3023602NM FWD FUSELAGE LOOSE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25609FE 48549 INTERCONNECT TORQUE TUBE BETWEEN PILOT'S AND COPILOT'S CONTROL COLUMNS WERE FOUND LOOSE. INSPECTED BOLTS AND HOLES, FOUND NO DISCREPANCIES. TORQUED BOLTS, PER CMM 27-31-02 PAGE 502 AND RETURNED TO SERVICE. 2L73 4F RTA22WE 19951113002281995111300228NM 1995 11 13 95FDEA01680 119951106A5313 STRINGER BOEING727 72722 1384002NM BS 433-460 GOUGES A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 NUMEROUS GOUGES IN STR AT BS 433 TO 460 STR 16L AND MISSING FASTENER AT BS 450 STR 16L. REPAIRED NUMEROUS GOUGES IN STR 16L AT BS 433 TO 460 AND MISSING FASTENER AT BS 450 STR 16L PER FEDEX SRM 53-10-1 AND 53-10-3. 2L73 4F A3WE 19951113002291995111300229NM 1995 11 13 95FDEA01681 119951106A5311 FRAME BOEING727 72722 1384002NM BS 520 DAMAGED HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND DAMAGED FASTENER HOLE ON FRAME STA 520 STR 22L, FWD BAY. REPAIRED DAMAGED HOLE ON FRAME STA 520 STR 22L IAW FEDEX SRM 51-40-3. 2L73 4F A3WE 19951113002301995111300230NM 1995 11 13 95FDEA01682 119951106A5315 FLOORBEAM BOEING727 72722 1384002NM BS 680 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 MECHANICAL DAMAGE ON FLOORBEAM LOWER CHORD BS 680 RBL 15 TO LBL 19 WL 200 WILL REQUIRE REMOVAL OF BULKHEAD UPPER SUPPORT ANGLE FOR ACCESS. BLENDED AND REMOVED DAMAGE ON FLOORBEAM STA 680 LBL 125 RBL 15. FOUND FLOORBEAM OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED DAMAGED ON FLOORBEAM, REPAIRED FLOORBEAM PER FEDEX SRM 53-10-18. 2L73 4F A3WE 19951113002311995111300231NM 1995 11 13 95FDEA01683 119951106A5313BAC1493513 STRINGER BOEING727 72722 1384002NM BS 400 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON STR 25R BS 400 PLUS 8 WL 155. 2L73 4F A3WE 19951113002321995111300232NM 1995 11 13 95FDEA01684 119951106A532069144925 SPLICE BOEING727 72722 1384002NM BS 436 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 STR SPLICE STA 436 STR 20R HAS CORROSION. REMOVED AND REPLACED STR SPLICE AT STA 436 STR 20R WHICH WAS OUT OF LIMITS PER FEDEX STR 53-10-1. 2L73 4F A3WE 19951113002331995111300233NM 1995 11 13 95FDEA01685 119951106A5320 FAIL-SAFE CHORD BOEING727 72722 1384002NM BS 440 CUT A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR 0210, FAIL-SAFE CHORD GOT CUT IN RADIUS AT STA 440 BETWEEN STR 15 TO 16 LBL 68. REPAIRED FAIL-SAFE CHORD AT BS 440 LBL 68 WL 216 TO 232 PER FEDEX SRM 51-40-03. 2L73 4F A3WE 19951113002341995111300234NM 1995 11 13 95FDEA01686 119951106A5313 STRINGER BOEING727 72722 1384002NM BS 1105 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR 0049, FOUND CORROSION IN CHANNEL OF STR 28R RBL 14.5 WL 155 BS 1105 REPAIR PER SRM. 2L73 4F A3WE 19951113002351995111300235NM 1995 11 13 95FDEA01687 119951106A5313BAC1493513 STRINGER BOEING727 72722 1384002NM BS 400 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON STR 25R BS 400 PLUS 8 WL 155. REMOVED CORROSION ON STR 25R BS 400 PLUS 8 WL 155, OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED STR REPAIR AND INSTALLED PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951113002361995111300236NM 1995 11 13 95FDEA01688 119951106A5320 SHEAR TIE BOEING727 72722 1384002NM BS 460 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR 0210, DISCOVERED CRACK IN SHEAR TIE AT BS 460 BETWEEN STR 15L AND 14L AFTER REMOVING FASTENERS FOR STR REMOVAL. REPAIRED SHEAR TIE AT BS 460 BETWEEN STRINGER 14L TO 15L PER FEDEX SRM 53-10-04. 2L73 4F A3WE 19951113002371995111300237NM 1995 11 13 95FDEA01689 119951106A5311 FRAME BOEING727 72722 1384002NM BS 520 DOUBLE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DOUBLE HOLE IN FRAME BS 520 STR 25L. REPAIRED DOUBLE HOLE IN FRAME AT BS 520 STR 25L PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951113002381995111300238NM 1995 11 13 95FDEA01690 119951107A5720 CLIP BOEING727 72722C 138400FNM BS 760 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 WING TOE CLIP STA 760 LBL 65 HAS CORROSION. 2L73 4F A3WE 19951113002391995111300239NM 1995 11 13 95FDEA01691 119951107A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55. 2L73 4F A3WE 19951113002401995111300240NM 1995 11 13 95FDEA01692 119951107A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 CORROSION ON FLOORBEAM STA 640 RBL 21 TO 58. 2L73 4F A3WE 19951113002411995111300241NM 1995 11 13 95FDEA01693 119951107A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 640 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 FLOORBEAM STA 640 LBL 53 HAS CORROSION. 2L73 4F A3WE 19951113002421995111300242SO 1995 11 13 COMA9511196 119951106A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO011105G 120105 FLAP CONTROL FAULT WARNING. REPLACED THE LEFT INBOARD FLAP ACTUATOR. 2L72 4T RTA31SO 19951113002431995111300243SO 1995 11 13 COMA9511995 119951104A324112038594001 CONTROL BOX EMB 120 EMB120RT SO ANTI SKID DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01249CA9458 4742 120230 RIGHT ANTI-SKID INOPERATIVE WARNING AFTER LANDING GEAR WAS RETRACTED. REPLACED THE ANTI-SKID CONTROL BOX. 2L72 4T RTA31SO 19951113002441995111300244EU 1995 11 13 COMA9531187 119951104A2731DL3827M157 TRIM ACTUATOR SAAB SF340 SF340A 7850100EU LT ELEVATOR FAILED A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01361CA128791755 340A056 THE MAIN ELEVATOR PITCH TRIM IS INOPERATIVE. REPLACED THE MAIN ELEVATOR PITCH TRIM ACTUATOR. 2L72 4T RTA52EU 19951113002451995111300245EU 1995 11 13 COMA9531188 119951106A2197 WIRE SAAB SF340 SF340A 7850100EU CABIN PRESS SYSTSHORTED A COMAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO01343CA 340A024 THE CABIN PRESSURIZATION AND AUTO DUMP CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPAIRED SHORTED WIRING IN THE RIGHT WHEEL WELL. 2L72 4T RTA52EU 19951113002461995111300246GL 1995 11 13 ERA00017 219951024A7320 TD SYST CVAC 440 440 2422902WP ALLSN 501D 501D13H 03004GL NR 1 ENGINE MALFUNCTIONED A ERAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 AL03566EA 381 ON TAKEOFF, NR 1 ENGINE WOULD NOT MAKE POWER. CREW ABORTED TAKEOFF AND RETURNED TO GATE. TD SYSTEM HAD BEEN PREVIOUSLY DEFERRED, HOWEVER SYSTEM WAS TURNED ON. DEACTIVATED TD SYSTEM, GROUND CHECKED GOOD. 2L72 4R4 T 6A6 E282 19951113002471995111300247NE 1995 11 13 ERA00018 219951024A8530401093 NR 3 CYLINDER DOUG DC3 DC3C 3021457WP PWA R1830 R183075 52020NE LT ENGINE LOST VALVE A ERAAAE UNSCHED LANDING ENGINE SHUTDOWN KE FLUID LOSS VIBRATION/BUFFET CRCRUISE 1 AL031944H 434 34278 LT ENGINE VIBRATION AND LEAKING OIL, SHUTDOWN ENGINE AND MADE UNEVENTFUL LANDING. REPLACED NR 3 CYLINDER. 2L72 4R4 R A669 5E4 19951113002481995111300248WP 1995 11 13 MWEA95363 119951105A4930360231021 FUEL CONTROL DOUG DC9 DC914 3022034WP APU LEAKING A MWEAK NONE BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TXTAXI/GRND HDL 1 GL3180ME 45795 CREW REPORTS, WHILE TAXIING TO GATE, STRONG FUEL ODOR PERMEATED THE CABIN AFTER STARTING APU. MAINTENANCE FOUND FUEL LEAKING FROM APU FUEL CONTROL DRAIN. REPLACED APU FUEL CONTROL, OPS AND LEAK CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951113002491995111300249WP 1995 11 13 MWEA95364 119951108A335060030431 EEL POWER SUPPLY DOUG DC9 DC914 3022034WP CABIN MALFUNCTIONED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31500ME 45711 MAINTENANCE REPORTS, DURING SERVICE CHECK THE RT OVERHEAD EMERGENCY ESCAPE LIGHT WOULD NOT EXTINGUISH. MAINTENANCE REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951113002501995111300250WP 1995 11 13 MWEA95365 119951111A2560113313 EVAC SLIDE DOUG DC9 DC932 3022066WP FWD GALLEY DOOR LOOSE A MWEAK NONE O OTHER LDLANDING 1 GL31203ME 47673 CREW REPORTS, UPON LANDING THE GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE BECAME LOOSE. MAINTENANCE RESECURED ESCAPE SLIDE, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951113002511995111300251WP 1995 11 13 MWEA95366 119951106A335060030431 BATTERY PACK DOUG DC9 DC914 3022034WP COCKPIT LOW CHARGE A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31700ME 45696 DURING SERVICE CHECK, FOUND FWD GALLEY AND COCKPIT OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951113002521995111300252NM 1995 11 13 P5CA9500836 119951106A27811815866 TRANSMITTER BOEING747 747121 1384871NM RT LE FLAP FAILED A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23830FT 19642 DURING TAXI OUT, FLAPS SELECTED 10 DEGREES, THE OUTBOARD STOP AT 5 DEGREES, RECYCLED NO HELP. FOUND RIGHT OUTBOARD FLAP TRANSMITTER AT FAULT REPLACED TRANSMITTER AND CANNON PLUG PER MAINTENANCE MANUAL 27-58-01. 2L74 4F A20WE 19951113002531995111300253NM 1995 11 13 SCNA95259 119951103A33501000677 EEL SIGN BOEING727 727259 138408JNM L 1 DOOR INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE EMERGENCY EXIT SIGN AT THE L1 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED EXIT SIGN AT THE L1 DOOR, LIGHT TESTED GOOD. 2L73 4F A3WE 19951113002541995111300254SO 1995 11 13 SWIA95661 119951029A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 LT WING RIB 15 AND 16 HAVE SEVERAL CLIPS CRACKED. REMOVED AND REPLACED 5 WING SKIN SUPPORT CLIPS ON LT WING RIB 15 AND 16 IAW SB 120-57-0031 AND RII-33. 2L72 4T4 TRTA31SO E20NE 19951113002551995111300255SO 1995 11 13 SWIA95662 119951029A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 RT WING RIB 15 HAS CRACKED CLIPS. REMOVED AND REPLACED THREE SKIN WING SUPPORT CLIPS ON RT WING RIB 15 IAW SB 120-57-0031 AND RII-33. 2L72 4T4 TRTA31SO E20NE 19951113002561995111300256SO 1995 11 13 SWIA95663 119951030A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 RT RUDDER O/B CABLE WORN, AFT SECTION. REMOVED AND REPLACED RT O/B RUDDER CABLE IAW EMB MM 27-00-01, OPS CHECK OK. 2L72 4T4 TRTA31SO E20NE 19951113002571995111300257SO 1995 11 13 SWIA95664 119951030A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 RT RUDDER I/B CABLE WORN, AFT SECTION. REMOVED AND REPLACED RT I/B RUDDER CABLE IAW EMB MM 27-00-01, OP CHECK OK. 2L72 4T4 TRTA31SO E20NE 19951113002581995111300258SO 1995 11 13 SWIA95665 119951030A2731 CABLES EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE ELEVATOR TRIM WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 ELEVATOR TRIM CABLES WORN. REMOVED AND REPLACED ELEVATOR TRIM CABLES IAW EMB MM 27-00-01, OPS CHECK OK. 2L72 4T4 TRTA31SO E20NE 19951113002591995111300259SO 1995 11 13 SWIA95666 119951030A27215298 CABLES EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER TRIM WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07194SW 120120 RUDDER TRIM CABLES WORN. REMOVED AND REPLACED RUDDER TRIM CABLES IAW EMB MM 2-00-01, OPS CHECK OK. 2L72 4T4 TRTA31SO E20NE 19951113002601995111300260WP 1995 11 13 WWMA9500080 219951103A7310 FUEL SYST BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP RT ENGINE MALFUNCTIONED A WWMAE ENGINE SHUTDOWN X ENGINE FLAMEOUT LDLANDING 1 WP15966AE 966 DURING LANDING ROLLOUT, WHEN POWER LEVERS WERE PLACED IN REVERSE THE RIGHT ENGINE SHUT ITSELF DOWN. MAINTENANCE PERFORMED GROUND RUNS AND WAS UNABLE TO DUPLICATE THE PROBLEM . REPLACED THE RIGHT ENGINE FUEL FLOW DIVIDER AND FUEL SHUTOFF VALVE, AS A PRECAUTIONARY MEASURE. ALSO, REPLACED THE RIGHT ENGINE FUEL PRESSURE REGULATOR, DUE TO SLOW ACCELERATION DURING ENGINE STARTS, THAT WERE NOTED DURING THE MAINTENANCE GROUND RUNS. THE AIRCRAFT WAS TEST FLOWN AND RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2L72 4T4 TRTA56EU E4WE 19951113002611995111300261NM 1995 11 13 95ZZZM599 119950726A33403014013 ROTATING BEACON BOEING737 7372H4 138448CNM FS 570 DEFECTIVE A AA6XAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO132FOR 21612 WHILE PUSING BACK FROM GATE AT JAX, FLIGHT ATTENDANT REPORTED SMOKE FROM OVERHEAD BIN AROUND ROW NR 9. AIRCRAFT WAS TOWED BACK TO THE GATE AND PASSENGER DEPLANNED. ALL POWER WAS REMOVED, UPPER BEACON CIRCUIT BREAKER WAS FOUND POPPED. MAINTENANCE IN JAX FOUND UPPER ANTI-COLLISION BEACON DEFECTIVE. ITEM WAS DEFERRED PER MEL 33-6. REMOVED AND REPLACED UPPER ANTI-COLLISION LIGHT, OPS CHECK OK. (M) 2L72 4F A16WE 19951113002621995111300262WP 1995 11 13 95ZZZM600 119950831A5311 FRAME DOUG DC9 DC932 3022066WP FS 218 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11901VJ 47275 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FUOND IN THE FORWARD PIT CRACKS, AT FS 218, ON THE LOWER FRAME. REMOVED DAMAGED SECTION. FABRICATED REPAIR MEMBER AND INSTALLED IAW DC-9 SRM 51-10-3, 51-10-1 AND 51-10-2A. (M) 2L72 4F A6WE 19951113002631995111300263WP 1995 11 13 95ZZZM601 119950901A5320 DOUBLERS DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11901VJ 47275 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, EVIDENCE OF CORROSION WAS FOUND ON THE TCAS ANTENNA AFT SIDE. REMOVED MOUNTING PLATE AND FINGER DOUBLERS. FABRICATED A NEW PLATE AND FINGER DOUBLERS AND INSTALLED ALL PARTS IAW DC9 SRM 53-04 FIG 12B. (M) 2L72 4F A6WE 19951113002641995111300264WP 1995 11 13 95ZZZM602 119951013A53205645827 PRESS DECK DOUG DC8 DC8F54 3021926WP BS 159.5-248 CORRODED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23802CK6640710480 45679 OSC - SEVERAL AREAS OF CORROSION STATION 159.5 TO STATION 2480 COCKPIT PRESSURE DECK JUST BELOW LONG 21R. INSTALLED REPAIR AS IT REQUIRED ACCORDING TO COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2109 AND IAW DC-8 SRM 53-2-0, 51-1-2, 51-1-11. (ALSO BMS FORM 6008 NR 03548, 03550, 03551, 02479). 2L74 4F 4A25 19951113002651995111300265WP 1995 11 13 95ZZZM603 119951015A53472772659 SEAT TRACK DOUG DC8 DC8F54 3021926WP BS 1269.5-1380 CORRODED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23802CK6640710480 45679 OSC - NR 5 SEAT TRACK CORRODED AT STATION 1269.5 TO STATION 1380. REPLACED NR 5 SEAT TRACK FROM STATION 1269.5 TO STATION 1380 IAW DC-8 SRM 53-2-3 AND FUSELAGE CENTER SECTION FLOOR PLANK. REPAIR IAW COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2112. (M) 2L74 4F 4A25 19951113002661995111300266WP 1995 11 13 95ZZZM604 119951013A5730 SKIN DOUG DC8 DC8F54 3021926WP WS 23 CORRODED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23802CK6640710480 45679 OSC - LEFT TOP SURFACE OF CENTER WING TANK CORROSION AT PANEL NR 516. INSTALLED REPAIR ACCORDING TO COTNEY DESIGNATION NR SO-782, SKETCH AIA/E/2107 AS IT REQUIRED AND IAW DC-8 SRM 51-1-20B AND 51-1-12. (M) 2L74 4F 4A25 19951113002671995111300267WP 1995 11 13 95ZZZM605 119951011A571256110401 RIB DOUG DC8 DC8F54 3021926WP WS 219 CRACKED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23802CK6640710480 45679 OSC - FLAP WELL SUPPORT RIB CRACKED JUST OUTBOARD OF STATION 219 FLAP ACTUATOR. INSTALLED REPAIR ACCORDING TO SKETCH AIA/E/2108 AS IT REQUIRED. 2L74 4F 4A25 19951113002681995111300268WP 1995 11 13 95ZZZM606 119951001A3246 BEARINGS DOUG DC8 DC862 3021970WP NR 2 WHEEL FAILED A TC8AA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL23803MG 45910 SCEL - ON TAKEOFF, TOWER REPORTED THAT PIECES OF TIRE AND SCRAPS OF METAL WERE FOUND. NR 2 WHEEL BEARINGS CAME APART DURING TAKEOFF CAUSING NR 6 TIRE TO BLOW. REMOVED AND REPLACED NR 1, NR 2, NR 5 AND NR 6 TIRE ASSEMBLYS PER MM CHAP 32-40-1. ALL TIRES SERVICED AS REQUIRED. SPIN CHECKED GOOD. 2L74 4F 4A25 19951113002691995111300269WP 1995 11 13 95ZZZM607 119951010A53121642725 BLKHD ANGLE DOUG DC8 DC8F54 3021926WP BS 980 CORRODED A TC8AK NONE O OTHER ININSP/MAINT 1 GL23802CK6640710480 45679 OSC - FOUND CORROSION C-PIT STATION 980 TO 36R AND 34R, BODY TO BULKHEAD ANGLE. CUT OUT DAMAGED AREA, INSTALLED REPAIR AS IT REQUIRED ACCORDING TO SKETCH AIA/E/2104 AND DOUGLAS SRMS 51-1-8 AND 51-1-20D. ENGINEERING DESIGNATION NR SO-782, SKETCH AIA/E/2104. 2L74 4F 4A25 19951113002701995111300270WP 1995 11 13 CKSA95098 119950923A24204TL1150K SWITCH DOUG DC8 DC8F55 3021928WP FE PANEL FAILED A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL236161C56094 45856 KMIA - SMOKE COMING FROM F/E ELECTRICAL PANEL. AFTER REMOVING THE PANEL, TROUBLESHOT AND FOUND SWITCH BURNED. REINSTALLED THE PANEL, DISCONNECTED THE NR 2 AND DMI'D IT IAW 24-1-1 AS ITEM NR 274. (M) 2L74 4F 4A25 19951113002711995111300271NM 1995 11 13 CKSA95100 119950910A2612897080 A-5 CARD BOEING747 747132 1384882NM APU DIRTY A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74308 20247 APU FIRE WARNING IS INTERMITTENT ON 'A' LOOP. 'B' LOOP OK. CLEANED CONTACTS ON APU FIRE WARNING 'A' LOOP CIRCUIT CARD. OP'S CHECK GOOD ON GROUND. (M) 2L74 4F A20WE 19951113002721995111300272NM 1995 11 13 CKSA95101 119950914A2612D5922 CONNECTORS BOEING747 747132 1384882NM APU CONTAMINATED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74308 20247 KLAX - APU 'A' FIRE DETECTOR FLICKERED ON AND OFF IN FLIGHT. AURAL WARNING ACCOMPANIED BY FLICKERING LIGHT, SWITCH WAS IN BOTH, SWITCHED TO 'B' PROBLEM WENT AWAY. CLEANED CONTAMINATED CONNECTORS AND RESECURED. OPS CHECK GOOD 26-10-00. (M) 2L74 4F A20WE 19951113002731995111300273NM 1995 11 13 CKSA95102 119950919A2612 FIRE WARNING BOEING747 747132 1384882NM APU MALFUNCTIONED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74308 20247 PHNL - APU 'A' FIRE WARNING GIVES INTERMITTENT FIRE WARNING IN FLIGHT WITH APU SHUTDOWN. NORMAL OPS ON GROUND. TROUBLESHOT WIRING, COULD NOT DUPLICATE ON GROUND. OPS CHECKED GOOD. (M) 2L74 4F A20WE 19951113002741995111300274NM 1995 11 13 CKSA95103 119950922A2612897080 A5 CARD BOEING747 747132 1384882NM APU SHORTED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74308 20247 KLAX - APU FIRE WARNING 'A' LOOP GIVES INTERMITTENT WARNING DURING FLIGHT WITH APU SHUTDOWN. 'B' CIRCUIT OK. REMOVED AND REPLACED A5 CARD PER MM 26-10-00. OPS CHECK FOUND SATISFACTORY. (M) 2L74 4F A20WE 19951113002751995111300275NM 1995 11 13 CKSA95104 119950927A2612 CONNECTOR BOEING747 747132 1384882NM APU LOOSE A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74466 20247 KLAX - APU FIRE WARNING 'A' DETECTOR LIGHT FLASHED IN FLIGHT BUT NO FIRE WARNING WAS GIVEN. 'B' LOOP FUNCTIONS NORMALLY. LOOSE CONNECTOR ON UPPER FORWARD SENSOR. TIGHTENED AND GROUND CHECKS GOOD IAW MM 26-10-00. (M) 2L74 4F A20WE 19951113002761995111300276WP 1995 11 13 CKSA95105 119951011A2612CA00KE16S8S CONNECTOR DOUG DC8 DC861 3021952WP NR 2 ENGINE SHORTED A CKSAFA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23817CK49835 45887 KMIA - ON CLIMB-OUT, HAD ENGINE FIRE INDICATION ON NR 2 ENGINE. FIRED ONE BOTTLE, FIRE INDICATION PERSISTED. FIRED SECOND BOTTLE, FIRE INDICATION PERSISTED. REPLACED DAMAGED AND SHORTED CANNON PLUG. CONNECTOR AT LOWER FORWARD FIRE LOOP CONNECTION RAN ENGINE AT VARIOUS POWER SETTINGS. OPS CHECK NORMAL IAW 26-2-0. ALSO, REMOVED AND REPLACED BOTH LEFT HALF INBOARD AND OUTBOARD FIRE BOTTLES IAW MM 26-3-0. (M) 2L74 4F 4A25 19951113002771995111300277SW 1995 11 13 MALA954635 119950913A54142735002 SKIN SWRNGNSA227 SA227AC 8780603SW NS 141-143 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, A CRACK WAS NOTED ON THE RIGHT NACELLES INBOARD KEELSON WEB BETWEEN THE MAIN SPAR AND THE MAIN LANDING GEAR DRAG BRACE. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER AS PER LIMITED AUTHORIZED REPAIR 95-MALA-214. (M) 1L72 4T A8SW 19951113002781995111300278NE 1995 11 13 SRAA109509 219951012A7200 ENGINE BOEING747 747246F NM PWA JT9 JT9D7Q 52054NE NR 4 BIRD STRIKE A SRAACD ABORTED TAKEOFF RETURN TO BLOCK XC ENGINE FLAMEOUT F.O.D. TOTAKEOFF 1 SO19740SJ 22477 ON TAKEOFF ROLL FOR FLIGHT DLH8622 OUT OF FRANKFURT, NR 4 ENGINE HAD BIRD STRIKE SUBSEQUENTLY CAUSING IT TO STALL. REJECTED TAKEOFF AT 100KTS WHICH CAUSED 8 TIRES TO THERMAL. PERFORMED BIRD STRIKE INSPECTION AND HIGH ENERGY STOP INSPECTION PER BOEING CHAP 5-51-14 AND 5-51-10. FOUND 6 FAN BLADES DAMAGED, REPLACED 6 FAN BLADES, BOROSCOPED NR 4 ENGINE. FOUND ALL WITHIN OPERATIONAL LIMITS. REPLACED ALL 8 TIRES ON RHS. PERFORMED ENGINE RUN UP, OPS CHECKED GOOD PER MM CH 71. (M) 2L74 4F4 F A20WE E3NE 19951113002791995111300279WP 1995 11 13 USAA950803 119950629A5330 SKIN DOUG DC9 DC982 3022082WP BS 560 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US36793 48098 IND - DURING CX-6 CHECK INSPECTION, FOUND A .125 INCH CRACK IN THE FUSELAGE SKIN AT STATION 560 LONGERON 22R. INSTALLED CLASS 2 REPAIR PER SRM 53-04. (M) 2L72 4F A6WE 19951113002801995111300280NM 1995 11 13 USAA950943 119950829A5313 STRINGER BOEING737 7372B7 1384560NM BS 767 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19275AU33742 22887 ROA - DURING CD-3 CHECK VISUAL INSPECTION, FOUND STRINGER CORRODED AT BS 767, STRINGER 276 BS 767. REMOVED DAMAGED STRINGER AND SPLICED NEW STRINGER PER SRM 53-10-3. (M) 2L72 4F A16WE 19951113002811995111300281NM 1995 11 13 USAA950972 119950720A5315TR531006 FLOOR BEAM BOEING737 737301 1384611NM BS 772 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19341US26488 23510 CLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED CARGO FLOOR BEAM. CORROSION FOUND AT STATION 772 AT CARGO FLOOR SUPPORT CHANNEL. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. INSTALLED REPAIR ANGLES. (M) 2L72 4F RTA16WE 19951113002821995111300282NM 1995 11 13 USAA951014 119950814A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK INSPECTION, VISUALLY INSPECTED A 2 INCH CORRODED AREA LOCATED AT THE FLOOR BEAM STATION 312 RBL 6. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP. (M) 2L72 4F RTA16WE 19951113002831995111300283NM 1995 11 13 USAA951015 119950808A5320 DOOR FRAME BOEING737 737401 1384701NM AFT CARGO BIN CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A 1 INCH BY 4 INCH CORRODED AREA AFT CARGO BIN DOOR FRAME AT LOWER FORWARD CORNER. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. DOUBLER INSTALLED ON FRAME. (M) 2L72 4F RTA16WE 19951113002841995111300284NM 1995 11 13 USAA951016 119950807A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US18448 23985 CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES (40 INCHES) AT STATION 344 RBL 8 TO LBL 45.5, ON FLOOR BEAM. CORROSION TASK NR C53-127-02, CORROSION LEVEL 2. REMOVED AND REPLACED T-CAP. (M) 2L72 4F RTA16WE 19951113002851995111300285NM 1995 11 13 USAA951017 119950807A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US18448 23985 CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORRODED AREAS AROUND FLOOR BOARD ATTACH HOLES 30 INCHES AT STATION 328 FROM LBL TO RBL 55, ON FLOOR BEAM. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP (UPPER) PER TYPICAL REPAIR 53-10-03. (M) 2L72 4F RTA16WE 19951113002861995111300286NM 1995 11 13 USAA951018 119950808A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A MQ6-CHECK INSPECTION, VISUALLY FOUND CORROSION AT FLOOR BOARD ATTACH HOLES AND AT TOP HORIZONTAL EDGE 10 INCHES LOCATED ON FLOOR BEAM AT STATION 986.5 ATTACH HOLES ALONG SPAN OF BEAM AND LEADING EDGE BL 33R TO BL 44R. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. INSTALLED T-CAP. (M) 2L72 4F RTA16WE 19951113002871995111300287NM 1995 11 13 USAA951019 119950831A5330 SKIN BOEING737 737401 1384701NM BS 288 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A SKIN DENT 3.5 INCHES BY 3.5 INCHES BY .180 INCH DEEP IN THE LAV SERVICE DOOR STATION 288 AT STRINGER 20R AND 21R. INSTALLED SKIN. (M) 2L72 4F RTA16WE 19951113002881995111300288NM 1995 11 13 USAA951020 119950804A5347 SEAT TRACK BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK, INSPECTION FOUND BY EDDY CURRENT A 2.2 INCH CRACKED TRACK LOCATED AT STATION 520 A CENTERED RBL 45.5. INSTALLED DOUBLERS, TRIMMED FITTINGS, TRACKS AS REQUIRED. (M) 2L72 4F RTA16WE 19951113002891995111300289NM 1995 11 13 USAA951021 119950804A5347 TRACK BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q-6 CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.9 INCH CRACKED TRACK LOCATED AT STATION 520 EXTENDING 1.1 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75. INSTALLED DOUBLERS AND TUB FITTINGS. (M) 2L72 4F RTA16WE 19951113002901995111300290NM 1995 11 13 USAA951022 119950831A5330 SKIN BOEING737 737401 1384701NM BS 921 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK INSPECTION, VISUALLY FOUND A DENT 2.5 INCHES BY 5 INCHES BY .060 DEEP AT STATION 921 BETWEEN STRINGER 17R AND 18R. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113002911995111300291NM 1995 11 13 USAA951023 119950804A5347 TRACK ASSY BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19418US19449 23985 CLT - DURING A Q6-CHECK INSPECTION, FOUND BY EDDY CURRENT A 1.8 INCH CRACK LOCATED AT STATION 520, CENTERED AT LBL 45.5. INSTALLED TUB FITTING AND TRACK ASSY KIT 65C3468827. (M) 2L72 4F RTA16WE 19951113002921995111300292NM 1995 11 13 USAA951024 119950822A5315 FLOOR BEAM BOEING737 737301 1384611NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.4 INCH CRACK LOCATED AT STATION 520 EXTENDING .6 INCH OUTBOARD AND .8 INCH INBOARD OF LBL 45.5. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113002931995111300293NM 1995 11 13 USAA951025 119950816A5330 SKIN BOEING737 737301 1384611NM BS 492.4 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY INSPECTED AND FOUND A 1 INCH SKIN BULGE AND CHUNK MISSING BETWEEN STRINGER 21-20 RIGHT STATION 492.4. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113002941995111300294NM 1995 11 13 USAA951026 119950822A5330 SKIN BOEING737 737301 1384611NM FS 935 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH ROUND HOLE IN SKIN (PRIOR REPAIR CLEANUP) LOCATED FS 935, STRINGER 18 RT. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113002951995111300295NM 1995 11 13 USAA951030 119950919A5320 DOUBLER BOEING737 737301 1384611NM BS 144 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19349US24504 23552 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1 INCH HOLE REPAIR LOCATED AT STATION 344, STRINGER 18L. EXISTING REPAIR, DOUBLER INSTALLED. (M) 2L72 4F RTA16WE 19951113002961995111300296NM 1995 11 13 USAA951031 119950919A5320 DOUBLER BOEING737 737301 1384611NM BS 365 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19349US24504 23552 CLT - DURING A Q3-CHECK INSPECTION, A 16 INCH BY 10 INCH REPAIR INSTALLED LOCATED AT STATION 365, STRINGER 11L WAS VISUALLY FOUND. EXISTING REPAIR DOUBLER INSTALLED. (M) 2L72 4F RTA16WE 19951113002971995111300297NM 1995 11 13 USAA951032 119950919A5320 DOUBLER BOEING737 737301 1384611NM BS 430 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19349US24504 23552 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 8 INCH BY 8 INCH REPAIR INSTALLED LOCATED AT STATION 430 STRINGER 10L. PREVIOUS REPAIR DOUBLER INSTALLED. (M) 2L72 4F RTA16WE 19951113002981995111300298NM 1995 11 13 USAA951033 119950919A5330 DOUBLER BOEING737 737301 1384611NM BS 867 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19349US24504 23552 CLT - PREVIOUS 14 INCH BY 10 INCH REPAIR (EXT DOUBLER) INSTALLED LOCATED STATION 867 BETWEEN STRINGER 21R AND STRINGER 22R. VISUALLY INSPECTED. PREVIOUS REPAIR DOUBLER INSTALLED. (M) 2L72 4F RTA16WE 19951113002991995111300299NM 1995 11 13 USAA951034 119950919A5330 SKIN BOEING737 737301 1384611NM BS 390 MIS MFG A USAAK NONE W INADEQUATE Q C ININSP/MAINT 1 EA19349US24504 23552 CLT - VISUALLY INSPECTED EXISTING REPAIR, LARGE RIVET IN SKIN BAY LOCATED AT STATION 390 ABOVE STRINGER 11L. INSTALLED PROTRUDING HEAD RIVET 211TT3. (M) 2L72 4F RTA16WE 19951113003001995111300300GL 1995 11 13 VTZA95282 319950904A6110A163364 O-RING JETAIRJETSTMJETSTM4101 1500501EU MCAULY5JFR C5JFR36C1102GL RT PROP FAILED A VTZAA UNSCHED LANDING O OTHER CRCRUISE 1 EA27316UE930 41055 942069 FLT NR 6537 - LGA-IAD - DURING CRUISE, EMERGENCY WAS DECLARED AND FLIGHT DIVERTED TO EWR DUE TO THE RIGHT ENGINE EGT AND TORQUE FLUCTUATIONS. AIRCRAFT LANDED AT EWR WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE BETA TUBE O-RINGS AND ADJUSTED THE PROP BLADE ANGLES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 5 CP15WE 19951113003011995111300301NM 1995 11 13 95ZZZM608 119950925A2910AS115060220 HOSE ASSY BOEING757 7572B7 1384964NM CTR HYD SYSTEM LEAKING A USAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 EA19621AU 27200 PIT - FL 0576, AFTER TAKEOFF, CREW RECEIVED THE NR 1 CENTER HYDRAULIC PUMP PRESS LIGHT. CREW NOTED LOSS OF HYDRAULIC QUANTITY FROM CENTER SYSTEM. FLIGHT RETURNED TO PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED TWO HYDRAULIC LINES (PUMP TO FILTER MODULE LINES). (M) 2L72 4F RTA2NM 19951113003021995111300302EU 1995 11 13 95ZZZM609 119951006A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R-2 DOOR MISALIGNED A P2RAK NONE O OTHER LDLANDING 1 WP2314975 261 R-2 DOOR WOULD NOT DISARM ON GROUND. PLACARDED PER MEL 25-61-01. REINSTALLED FORWARD END OF GIRT BAR. OPS CHECKED OK PER MM 25-60-00. PLACARD REMOVED. (M) 2L72 4F A35EU 19951113003031995111300303EU 1995 11 13 95ZZZM610 119951006A3350P4010021 EEL BATTERY AIRBUS300 A300B4203 3930306EU CABIN DISCHARGED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314975 261 EMERGENCY FLASH LIGHT AT DOOR R-4 DOES NOT FLASH. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASH LIGHT BATTERY. OPS CHECKED GOOD. (M) 2L72 4F A35EU 19951113003041995111300304SO 1995 11 13 C2XA95IA281 119951007A551012015374002 DRAG ANGLE EMB 120 EMB120RT SO RT VERT STAB CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003051995111300305SO 1995 11 13 C2XA95IA282 119951007A572012017056019 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 5 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003061995111300306SO 1995 11 13 C2XA95IA283 119951007A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003071995111300307SO 1995 11 13 C2XA95IA284 119951007A572012017057006 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003081995111300308WP 1995 11 13 IXXA199585 119951010A3260H146 UPLATCH SWITCH DOUG DC8 DC871 302199AWP LT MLG FAILED A IXXAO OTHER N FALSE WARNING CLCLIMB 1 GL23824BX 45946 ON DEPARTURE OUT OF BOS, THE LANDING GEAR FAILED THE UPLATCH CHECK. THE LANDING GEAR WAS CYCLED THREE TIMES WITH THE SAME RESULT, WITH THE LANDING GEAR LEVER IN THE UPLATCH CHECK POSITION, THE UNSAFE LIGHT WAS ILLUMINATED WITH NO APPARENT GEAR EXTENSION. INSPECTION ON THE GROUND IN TOL REVEALED A MALFUNCTIONING LEFT MLG UPLATCH SWITCH. THE SWITCH WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951113003091995111300309EU 1995 11 13 P2RA950014 119951007A3350 CONNECTOR GRIMES AIRBUS300 A300B4203 3930306EU CABIN LOOSE A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314975 261 DURING OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS, LIGHTS AT 1K AND 1L LOCATIONS WOULD NOT TEST. MAINTENANCE REPOSTIONED LOOSE CONNECTIONS AT SEATS INSTALLATION 1K AND 1L. OPERATIONAL CHECK NORMAL. (M) 2L72 4F A35EU 19951113003101995111300310EU 1995 11 13 P2RA950015 119951009A3350P4010021 EEL BATTERY AIRBUS300 A300B4203 3930306EU CABIN DISCHARGED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314975 261 EMERGENCY FLASHLIGHT AT DOOR L-3 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECKED GOOD. (M) 2L72 4F A35EU 19951113003111995111300311WP 1995 11 13 USAA950966 119950818A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1287 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 28R AT STATION 1287. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) 2L72 4F A6WE 19951113003121995111300312WP 1995 11 13 USAA950967 119950818A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1297 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION LONGERON 29R AT STATION 1297 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) 2L72 4F A6WE 19951113003131995111300313WP 1995 11 13 USAA950968 119950824A5320 FITTING DOUG DC9 DC981 3022081WP BS 200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 INCH BY 6 INCH AREA OF CORROSION LEVEL 2 IN CUSP ANGLE AT MED FRAME LOWER ATTACH FITTING STATION 200. CORROSION TASK NR C46-53303. REMOVED CORRODED SECTION AND SPLICED NEW SECTION IN PER USAIR EA 31153. (M) 2L72 4F A6WE 19951113003141995111300314WP 1995 11 13 USAA950969 119950823A5311 FRAME DOUG DC9 DC981 3022081WP BS 1250 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 3 AREAS 2 INCHES BY 3 INCHES OF LEVEL 2 CORROSION AFT SIDE OF FRAME AT STATION 1250 FROM LONGERON 28L TO 28R. CORROSION TASK NR C57-53300. CLEANED CORRODED SECTION AND INSTALLED DOUBLERS PER SRM 53-03 FIG 2A. (M) 2L72 4F A6WE 19951113003151995111300315WP 1995 11 13 USAA950970 119950811A53201198595 DOUBLER DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 2 CORROSION 2 INCHES BY 35 INCHES STATION 1338, JACK PAD DOUBLER AFT CARGO AREA. CORROSION TASK NR C57-53300. REPLACED DOUBLER, CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-30-10. (M) 2L72 4F A6WE 19951113003161995111300316WP 1995 11 13 USAA950978 119950810A5320 JAMB DOUG DC9 DC981 3022081WP CABIN DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK UPPER FORWARD CORNER OF MED JAMB. INSTALLED INTERNAL AND EXTERNAL DOUBLER PER SRM 53-05 FIG 2B. (M) 2L72 4F A6WE 19951113003171995111300317WP 1995 11 13 USAA950979 119950810A5313 LONGERON DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND .75 INCH CRACK LONGERON 4L AT STATION 160. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951113003181995111300318WP 1995 11 13 USAA950980 119950810A5313 LONGERON DOUG DC9 DC981 3022081WP BS 237-508 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 6 CRACKS APPROXIMATELY .125 INCH TO .25 INCH IN LONGERON 17L AT BELTFRAME 237, 275, 295, 332, 370 AND 389. SPLICED IN NEW SECTION OF LONGERON BETWEEN STATION 237 TO 408 PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951113003191995111300319WP 1995 11 13 USAA950981 119950816A5313 LONGERON DOUG DC9 DC981 3022081WP BS 256-408 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 5 CRACKS .125 INCH TO .375 INCH LONG, BELTFRAME 256 TO 408 IN LONGERON 17R. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19951113003201995111300320WP 1995 11 13 USAA950982 119950816A5320 CUSP MEMBRANE DOUG DC9 DC981 3022081WP BS 1231 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 12 INCH CRACK IN CUSP MEMBRANE STATION 1231, LONGERON 18L. INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 96. (M) 2L72 4F A6WE 19951113003211995111300321WP 1995 11 13 USAA950983 119950816A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1463 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND .25 INCH CRACK LEFT SIDE STATION 1463, DRAG ANGLE. INSTALLED FILLER AND DOUBLER PER SRM 53-05 FIG 23. (M) 2L72 4F A6WE 19951113003221995111300322WP 1995 11 13 USAA950984 119950818A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1211-1231 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1 INCH BY 20 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED AT LONGERON 28L, STATION 1211 TO 1231 CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) 2L72 4F A6WE 19951113003231995111300323WP 1995 11 13 USAA950985 119950812A5320 ANGLE DOUG DC9 DC981 3022081WP BS 1309-1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND 2 INCH BY 29 INCH AREA OF LEVEL 1 CORROSION PREVIOUSLY REWORKED RIGHT LAV T-CUSP ANGLE FROM STATION 1309 TO 1338 LONGERON 18R. CORROSION TASK NR C58-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05 FIG 25. (M) 2L72 4F A6WE 19951113003241995111300324WP 1995 11 13 USAA950986 119950816A5311 BELTFRAME DOUG DC9 DC981 3022081WP BS 180 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN BELTFRAME BETWEEN LONGERON 28R AND 28L BELTFRAME 180. CORROSION TASK NR C45-53300. REMOVED SECTION OF BELTFRAME AND SPLICED IN NEW SECTION PER SRM 53-03 FIG 2A. (M) 2L72 4F A6WE 19951113003251995111300325WP 1995 11 13 USAA950987 119950814A5347 TRACK DOUG DC9 DC981 3022081WP BS 1205 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES LEFT INBOARD SEAT TRACK MOUNT HOLES AT STATION 1205. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2L72 4F A6WE 19951113003261995111300326WP 1995 11 13 USAA950988 119950823A5320 JAMB DOUG DC9 DC981 3022081WP CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19827US37695 48049 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FORWARD CARGO DOOR JAMB PAN ALONG BOTTOM EDGE BETWEEN PAN AND FUSELAGE SKIN CORROSION REF C51-53300. REMOVED LOWER SECTION OF DOOR JAMB AND SPLICED IN NEW SECTION PER SRM 53-05 FIG 44. (M) 2L72 4F A6WE 19951113003271995111300327NM 1995 11 13 USAA951027 119950818A5330 SKIN BOEING737 737301 1384611NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A 1.8 INCH CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH INBOARD AND .8 INCH OUTBOARD OF RBL 24.75. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113003281995111300328NM 1995 11 13 USAA951028 119950818A5330 SKIN BOEING737 737301 1384611NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q-3 CHECK INSPECTION, VISUALLY FOUND A 1.9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING .9 INCH OUTBOARD AND 1 INCH INBOARD OF LBL 24.75. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113003291995111300329NM 1995 11 13 USAA951029 119950818A5330 SKIN BOEING737 737301 1384611NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19340US27587 23237 CLT - DURING A Q3-CHECK INSPECTION, VISUALLY FOUND A .9 INCH SKIN CRACK LOCATED AT STATION 520 EXTENDING 1.0 INCH OF RBL 45.5. INSTALLED DOUBLER. (M) 2L72 4F RTA16WE 19951113003301995111300330NM 1995 11 13 USAA951035 119950925A2910AS115080200 HOSE ASSY BOEING757 7572B7 1384964NM CTR HYD SYSTEM LEAKING A USAAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CLCLIMB 1 EA19621AU 27200 PIT - FL 0576, AFTER TAKEOFF, CREW RECEIVED THE NR 1 CENTER HYDRAULIC PUMP PRESS LIGHT. CREW NOTED LOSS OF HYDRAULIC QUANTITY FROM CENTER SYSTEM. FLIGHT RETURNED TO PIT WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED TWO HYDRAULIC LINES (PUMP TO FILTER MODULE LINES). (M) 2L72 4F RTA2NM 19951113003311995111300331EU 1995 11 13 USAA951036 119950926A32321252515 ACTUATOR FOKKERF28 F28MK4000 4990810EU LT MLG DOOR INOPERATIVE A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19481US 11230 CMH - FL 1101, AFTER TAKEOFF FROM FWA AND GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. ABNORMAL PROCEDURES COMPLIED WITH, INDICATIONS SHOWED AND UNLOCKED DOOR. GEAR WAS SELECTED DOWN AND FLIGHT DIVERTED TO CMH. AFTER LANDING AND ENGINE SHUTDOWN, LEFT MAIN GEAR DOOR OPENED AND RESTED ON THE GROUND. MAINTENANCE REPLACED THE LEFT MAIN GEAR DOOR ACTUATOR. (M) 2L72 4F RTA20EU 19951113003321995111300332EU 1995 11 13 USAA951037 119950927A3230 UPLOCK ROLLER FOKKERF28 F28MK4000 4990810EU LT MLG MISALIGNED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19490US 11152 CLT - FL 799 - AFTER TAKEOFF FROM CLT, CREW RECEIVED RED WARNING LIGHT ON LEFT MAIN GEAR UPON GEAR RETRACTION. CREW EXTENDED GEAR AND THE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE POSITION OF THE LEFT UPLOCK ROLLER ASSEMBLY AND FLYING DOOR. AIRCRAFT WAS JACKED AND A GEAR SWING PERFORMED. (M) 2L72 4F RTA20EU 19951113003331995111300333EU 1995 11 13 USAA951038 119950927A2612 FIRE WARNING FOKKERF28 F28MK0100 4990807EU APU ACTIVATED A USAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 EA19859US 11293 CLT - FL 1229, ON APPROACH, CREW RECEIVED APU FIRE WARNING LIGHT AND APU AUTO SHUTDOWN. THE APU FIRE BOTTLE DISCHARGED AUTOMATICALLY. THE APPROACH CONTINUED AND THE FLIGHT LANDED WITH NO FURTHER INCIDENT. NO INDICATION OF FIRE WAS FOUND. MAINTENANCE CHECKED FOR HOT AIR LEAKS AND FOUND NONE. ALL OTHER SYSTEMS CHECKED NORMAL. FIRE BOTTLE REPLACED AND AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RT 19951113003341995111300334EU 1995 11 13 USAA951039 119950917A335014597101 EEL BATTERY FOKKERF28 F28MK4000 4990810EU CABIN DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19475AU 11222 CLE - RIGHT INTERIOR OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK, CHECKS SATISFACTORY. (M) 2L72 4F RTA20EU 19951113003351995111300335EU 1995 11 13 USAA951040 119950929A3260201251225 PROX SENSOR FOKKERF28 F28MK0100 4990807EU LT MLG MISALIGNED A USAAA UNSCHED LANDING ON OTHER FALSE WARNING CLCLIMB 1 EA19894US 11379 GSO - FLIGHT NR 1794 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GROUND FLIGHT FAULT ON MULTI FUNCTION DISPLAY UNIT. RETURNED TO GSO FOR LANDING. FOUND PROXIMITY SENSORS ON LEFT GEAR FOR FLT GROUND OUT OF ADJUSTMENT. ADJUSTED BOTH FLT GROUND PROXIMITY SENSOR IAW 32-63-03. (M) 2L72 4F RT 19951113003361995111300336EU 1995 11 13 USAA951041 219950928A7310 O-RING FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515P 54521EU NR 1 ENGINE CUT A USAAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 EA19494US 11167 9771 GSO - FLT NR 735 - NR 1 ENGINE SHUT DOWN ON SHORT FINAL DUE TO CSD LIGHT, LOW OIL PRESSURE AND DECAYING RPM TO 38 PERCENT HP RPM. FOUND O-RING CUT AND LEAKING FROM HP FUEL SHUTOFF VALVE AT THE PRESSURE INLET TO THE FUEL FLOW REGULATOR. OIL LEVEL GOOD, CSD LEVEL GOOD. GROUND RAN ENGINE, OPS CHECK GOOD. (M) 2L72 4F4 FRTA20EU E2EU 19951113003371995111300337EU 1995 11 13 USAA951042 119950930A3260201251225 SENSOR FOKKERF28 F28MK1000 4990808EU RT MLG FAILED A USAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 EA19868US 11313 PIT - FLT NR 1025 - AFTER TAKEOFF WE RECEIVED A GND/FLT CONTROL MSG ON MFDU. ALL INDICATIONS INDICATED AIRCRAFT WAS STILL ON GND. RETURNED TO PIT AFTER CONSULTING WITH MAINTENANCE CONTROL. REPLACED NR 3 RT PROXIMITY SENSOR PER MM 32-63-03. ADJUSTED AND OPS CHECKS GOOD PER SAME. (M) 2L72 4F RTA20EU 19951113003381995111300338 1995 11 13 USAA951046 419950927A22104038890951 MODE CNTL PNL BOEING737 7372B7 1384560NM AUTOPILOT FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19286AU26613 23133 PHL - FLT NR 0117 - CLIMBING OUT FROM LGA EN ROUTE TO MCO WITH ALT ALERTING AND 'A' CHANNEL AUTOPILOT ON MEL, AIRCRAFT WOULD NOT HOLD ALTITUDE OR RESPOND TO CHANGES WITHOUT USING ALT SEL. MAINTENANCE REPLACED THE AUTOPILOT MODE CONTROL PANEL. BITE CHECKED AND FUNCTIONAL CHECKED GOOD. (M) 2L72 4F A16WE 19951113003391995111300339EU 1995 11 13 95ZZZM611 119950930A275091SE16 SWITCH HONEYWELL BAG JETSTMJETSTM3101 1500215EU TE FLAP TQ TUBE DEFECTIVE A AVNAAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL07834JS 726 FLT NR 4097 - CREW EXPERIENCED AN UNCOMMANDED FLAP POSITION WHEN SELECTING FLAPS 10 DEGREE. FLAPS CONTINUED TO 25 DEGREE SETTINGS. PIT MAINTENANCE REPLACED FLAP POSITION MICRO-SWITCH IAW MM 27-50-00. GROUND CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951113003401995111300340NE 1995 11 13 95ZZZM612 219950927A7200 ENGINE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LEFT OVER TORQUE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07426JS 3038 FLT NR 4241 - CREW EXPERIENCED AN OVER TORQUE SITUATION LEFT ENGINE DURING TAKEOFF ROLL, ABORTED TAKEOFF RETURNED TO GATE WITHOUT FURTHER INCIDENT. COMPLIED WITH ENGINE OVER TORQUE INSPECTION IAW D0328 MM 05-57-01. NO DEFECTS NOTED, REPLACED RGB SCAVANGE FILTER PER MM. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA45NM E20NE 19951113003411995111300341NM 1995 11 13 95ZZZM613 119950928A32606839 INDICATOR BULB DORNERDO32 DO328100 2996000NM LANDING GEAR FAILED A VNAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 GL07430JS 3044 FLT NR 4151 - WHEN SELECTING GEAR DOWN, CREW DID NOT RECEIVE A SAFE GEAR INDICATION. CONDUCTED A FLY BY TOWER TO ENSURE GEAR WAS DOWN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BULBS IN LANDING GEAR POSITION INDICATOR. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 19951113003421995111300342NM 1995 11 13 95ZZZM614 119950924A7603 POWER LEVER DORNERDO32 DO328100 2996000NM LEFT LACK OF LUBE A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07426JS 3038 FLT NR 4247 - CREW RETURNED TO GATE, WERE UNABLE TO ADVANCE LEFT POWER LEVER BEYOND FI POSITION. MAINTENANCE LUBRICATED LEFT POWER LEVER PRIMARY LOW PITCH MECHANISM IAW STD MAINTENANCE PRACTICES. GROUND CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 19951113003431995111300343NM 1995 11 13 95ZZZM615 119950801A3230651781914 DN LOCK ACT BOEING737 7372P6 NM NLG BROKEN A A6XAO OTHER J WARNING INDICATION APAPPROACH 1 SO132FOR 21733 NOSE GEAR WOULD NOT EXTEND NORMALLY, MANUALLY EXTENDED OK. GOOD DOWN AND LOCKED INDICATION. DOWN LOCK ACTIVATOR WAS BROKEN. (M) 2L72 4F RTA16WE 19951113003441995111300344NM 1995 11 13 95ZZZM616 119950801A2612894093 FIRE LOOP BOEING737 7372P6 NM LOWER BROKEN A A6XAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 SO132FOR 21677 NR 2 ENGINE FIRE WARNING STARTED FLICKERING AND EVENTUALLY CAME ON STEADY. CAPTAIN PULLED BACK THROTTLE, NO HELP. SHUT DOWN ENGINE, NO HELP. FIRED ONE FIRE BOTTLE, NO HELP. DURING DESCENT, LIGHT FLICKERED AGAIN AND WENT OUT. FOUND BOTTOM FIRE LOOP FORWARD LOWER CONNECTOR BROKEN LOOSE FROM MOUNTING AND LOOP WAS TOUCHING CASE, CAUSING FALSE WARNING. REPLACED LOWER FIRE LOOP ASSY AND FIRE BOTTLE ASSY. (M) 2L72 4F RTA16WE 19951113003451995111300345NM 1995 11 13 95ZZZM617 119950623A2613894093 OVERHEAT BOEING737 7372P6 NM NR 2 ENGINE DEFECTIVE A A6XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO132FOR 21677 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED EN ROUTE TO PIE FROM MIA. FOUND DEFECTIVE OVERHEAT LOOP NR 2 ENGINE. REMOVED AND REPLACED OVERHEAT LOOP NR 2 ENGINE, OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 19951113003461995111300346NM 1995 11 13 95ZZZM618 119950719A25601181200 LATCH CABLE BOEING737 7372P6 NM ESCAPE SLIDES MISROUTED A A6XAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO132FOR 21677 ALL EMERGENCY ESCAPE SLIDES LATCH CABLE NOT PROPERLY ROUTED. REMOVED AND REPOSITIONED CABLE. 2L72 4F RTA16WE 19951113003471995111300347NM 1995 11 13 95ZZZM619 119950719A353080230014 PBE BOEING737 7372P6 NM FWD/AFT GALLEY TORN A A6XAK NONE O OTHER ININSP/MAINT 1 SO132FOR 21677 FORWARD AND AFT GALLEYS HAVE ONE EACH PBE'S UNSERVICEABLE DUE TO HOLE TORN IN CASE ONE AND LATCH BROKEN ON OTHER. REMOVED AND REPLACED PBE'S AND SECURED WELL WITH VELCRO STRAP. 2L72 4F RTA16WE 19951113003481995111300348 1995 11 13 95ZZZM620 419950719A256522D22900139 ESCAPE SLIDE BOEING737 7372P6 NM L1 DOOR TORN A A6XAK NONE O OTHER ININSP/MAINT 1 SO132FOR 21677 ESCAPE SLIDE AT POSITION L1 FRAYED AND TORN AT THE GIRT AREA. REMOVED AND REPLACED SLIDE, NOT RUBBING NOTED ON SCUFF PLATE. 2L72 4F RTA16WE 19951113003491995111300349NM 1995 11 13 ASAA9510091 119950922A335020131A EEL BATTERY BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 ANC - FLT NR 39 - DURING RECON, FOUND NR 5 PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19951113003501995111300350NM 1995 11 13 ASAA9540059 119950925A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 ANC - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED AFT FLOOR TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951113003511995111300351NM 1995 11 13 ASAA9540060 119950925A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 ANC - DURING MAINTENANCE CHECK, THE AFT TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED AFT FLOOR TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951113003521995111300352WP 1995 11 13 ASAA9580199 119950919A53305936667501 SKIN DOUG DC9 DC983 3022083WP Y1287 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS14825 53018 PAE - DURING 15K CHECK, FOUND CORROSION ON SKIN AT Y1287, X MINUS 1 TO X MINUS 6, Z MINUS 47. REMOVED CORRODED AREA OF SKIN AND REPAIRED IAW DC-9 SRM 53-04. (M) 2L72 4F RTA6WE 19951113003531995111300353WP 1995 11 13 ASAA9580201 119950919A5320 SHEAR TIE DOUG DC9 DC983 3022083WP Y1060 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS14825 53018 PAE - DURING 15K CHECK, FOUND CORROSION ON SHEAR TIE AT Y1060, X PLUS 4, Z MINUS 47. REMOVED CORROSION AND INSTALLED NEW SHEAR TIE IAW DC-9 SRM 51-10-01, 51-10-03, 51-30-01 AND 53-03. (M) 2L72 4F RTA6WE 19951113003541995111300354WP 1995 11 13 ASAA9580202 119950920A3350014597101 EEL BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01946AS 49658 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT SIGN LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951113003551995111300355WP 1995 11 13 ASAA9580203 119950922A53203920342504N ANGLE DOUG DC9 DC982 3022082WP FS 826 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01934AS28435 49235 OAK - DURING 30K CHECK, ATTACH ANGLE WAS FOUND CRACKED AT FS 826 ON CENTER WING TO FUSELAGE ATTACH POINT ON RIGHT FORWARD CORNER UNDER CABIN FLOOR PANEL E9. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-05. (M) 2L72 4F A6WE 19951113003561995111300356WP 1995 11 13 ASAA9580204 119950922A3350014597101 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951113003571995111300357WP 1995 11 13 ASAA9580205 119950923A52104928806501 HOOK ASSY DOUG DC9 DC982 3022082WP L1 DOOR WON'T ENGAGE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE. REPLACED THE HOOK ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951113003581995111300358WP 1995 11 13 ASAA9580206 119950925A5311 FRAME DOUG DC9 DC983 3022083WP Y1287 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01943AS148258868 53018 PAE - DURING 15K CHECK, FOUND CORROSION ON FRAME AT Y1287, X MINUS 6 TO X MINUS 8, Z-48. REMOVED CORROSION AND INSTALLED NEW PIECES IAW DC-9 SRM 51-20-00, 51-30-02, 53-01 AND 53-03. (M) 2L72 4F RTA6WE 19951113003591995111300359WP 1995 11 13 ASAA9580216 119951004A5347TMS6019943 SEAT TRACK DOUG DC9 DC983 3022083WP Y1003-Y1322 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1003 TO Y1322, X PLUS 45, Z MINUS 43. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M) 2L72 4F RTA6WE 19951113003601995111300360WP 1995 11 13 ASAA9580217 119951004A5330 SKIN DOUG DC9 DC983 3022083WP Y788 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON EXTERNAL SKIN AT Y788, LONGERON 28R TO 29R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-04. (M) 2L72 4F RTA6WE 19951113003611995111300361WP 1995 11 13 ASAA9580218 119951004A5330 SKIN DOUBLER DOUG DC9 DC983 3022083WP Y1168 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01947AS14710 53020 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON EXTERNAL SKIN AT Y1168, LONGERON 29L TO 30L. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5330-01208. (M) 2L72 4F RTA6WE 19951113003621995111300362SO 1995 11 13 C2XA95CL122 119951010A326019554 SENSOR TARGET EMB 120 EMB120RT SO RT MLG LOOSE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0917728 120182 CLE - FLT NR 3235 - AFTER TAKEOFF AND GEAR RETRACTION, ONE RED A-SYSTEM AND ONE RED B-SYSTEM LIGHTS REMAINED ON. THE LANDING GEAR WAS CYCLED WITH THE SAME RESULTS. MAINTENANCE INSPECTED LANDING GEAR AND FOUND THE RIGHT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR TARGET LOOSE, MAINTENANCE RESECURED TARGET. OPERATIONAL CHECK OF LANDING GEAR SYSTEM GOOD IAW EMB-120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4T RTA31SO 19951113003631995111300363SO 1995 11 13 C2XA95CL123 119951011A3230SV14H11004 SOLENOID VALVE EMB 120 EMB120RT SO NOSE HYD BAY FAILED A C2XAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW091772810135 120182 DTW - FLT NR 3152 - AFTER TAKEOFF AND GEAR RETRACTION THE CREW REPORTED A VIBRATION, ALSO THE LEFT MAIN GEAR FORWARD INBOARD DOOR DID NOT CLOSE. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE LANDING GEAR SOLENOID VALVE. OPERATIONAL AND LEAK CHECKS GOOD IAW EMB-120 MAINTENANCE MANUAL 32-32-00, 32-33-01 AND 32-32-14. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951113003641995111300364SO 1995 11 13 C2XA95IA271 119951007A534712015997002 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003651995111300365SO 1995 11 13 C2XA95IA272 119951007A534712015997002 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003661995111300366SO 1995 11 13 C2XA95IA273 119951007A523012020235005 MOUNT EMB 120 EMB120RT SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR FORWARD TORSION BAR MOUNT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003671995111300367SO 1995 11 13 C2XA95IA274 119951007A540012030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003681995111300368SO 1995 11 13 C2XA95IA275 119951007A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003691995111300369SO 1995 11 13 C2XA95IA276 119951007A572012017063011 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 22, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003701995111300370SO 1995 11 13 C2XA95IA277 119951007A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003711995111300371SO 1995 11 13 C2XA95IA278 119951007A532012004149001 T-CAP EMB 120 EMB120RT SO AFT CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-CAP, AT FRAME 36, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-CAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003721995111300372SO 1995 11 13 C2XA95IA279 119951007A571212017058001 NOSE RIB EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 17 WAS FOUND TO BE CRACKED ALONG THE UPPER EDGE. MAINTENANCE REPAIRED THE RIB BY REMOVING THE CRACKED PORTION AND INSERTING A SPLICE ANGLE. ALL WORK WAS ACCOMPLISHED IN REFERENCE TO EMBRAER DER FAX EST431/95. (M) 2L72 4T RTA31SO 19951113003731995111300373SO 1995 11 13 C2XA95IA280 119951007A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951113003741995111300374EU 1995 11 13 SIMA952721 119950929A33503012000 EEL CONTROLLER AEROSPATR72 ATR72212 EU CABIN FAILED A SIMAK NONE O OTHER LDLANDING 1 SW21288AM7039 234 288 DFW - FLT NR 3722 - UPON LANDING AT DFW THE REAR HALF OF THE INTERIOR EMERGENCY LIGHTS ILLUMINATED. BATTERY PACK CONTROLLER ASSY AND BATTERY WERE REPLACED. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951113003751995111300375NE 1995 11 13 SIMA952731 219950930A732032448713 HMU AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENGINE MALFUNCTIONED A SIMAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW21425MJ2019 C38002N 425 127114 ORD - FLT NR 4058 - NR 2 TQ DROPPED TO 50 PERCENT WITH POWER LEVERS IN NOTCH. ATTEMPTED EEC RESET, CAUSING ENGINE FAILURE. WHEN TQ DROPPED TO 50 PERCENT ALL OTHER PARAMETERS FOLLOWED. REPLACED RT ENGINE FUEL SYSTEM COMPONENTS INCLUDING FLOW DIVIDER, FUEL PUMP, HMU, MFC AND FUEL NOZZLES. PERFORMED ENGINE GROUND CHECKS. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19951113003761995111300376EU 1995 11 13 SIMA952761 119951003A793181071100010A OIL PSI TRANSM AEROSPATR72 ATR72212 EU NR 2 ENG INTERMITTENT A SIMAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW21451AT 1470 451 LBB - FLT NR 3826 - DURING TAKEOFF FROM LBB, NR 2 ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO, NO LOW OIL PRESSURE WARNINGS GIVEN. CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO LBB. DFW - MAINTENANCE SENT TO LBB WHERE THEY GROUND RAN AIRCRAFT SATISFACTORY, BUT REPLACED THE OIL PRESSURE TRANSMITTER AS PRECAUTION. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951113003771995111300377NM 1995 11 13 TAOA109506 119951011A335090052 EEL BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 6570 22043 RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19951113003781995111300378NM 1995 11 13 TAOA109507 119951011A3350900835A EEL BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS B3246 22043 RIGHT FORWARD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19951113003791995111300379WP 1995 11 13 95ZZZM621 119951006A3231AN843A BOLT DOUG DC8 DC862 3021970WP LT MLG DOOR BROKEN A ARWAK NONE O OTHER ININSP/MAINT 1 SO191803 45895 DURING PREFLIGHT INSPECTION, THE F/E FOUND LEFT MLG UPPER STRUT DOOR SUPPORT LINK BROKEN. DOOR WAS REMOVED AND AIRCRAFT MOVED TO DAYTON, IAW DOUGLAS FAX MISC-5725/JCT DATED 10/6/95. AT DAYTON, MAINTENANCE REPLACED LINK BOLT AND PERFORMED OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM. GEAR CHECKED OK. (M) 2L74 4F 4A25 19951113003801995111300380WP 1995 11 13 95ZZZM622 119950925A3244 TIRES DOUG DC9 DC951 3022051WP RT MLG FAILED A A4JACD ABORTED TAKEOFF RETURN TO BLOCK EM VIBRATION/BUFFET OVER TEMP TOTAKEOFF 1 SO15919PJ 47663 BOTH RIGHT MAIN TIRES BLEW ON TAKEOFF ROLL. TAKEOFF ABORTED. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES (P/N 95608591). NR 4 WHEEL RIM BROKEN. BOTH TIRES AND WHEELS ARE BEING SENT OUT FOR ANALYSIS. WILL ADVISE FAA AS SOON AS ANALYSIS IS COMPLETE. (M) 2L72 4F A6WE 19951113003811995111300381WP 1995 11 13 95ZZZM623 119950117A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1190-1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, FOUND CORROSION AT STRINGER 34R BETWEEN STATION 1190 AND 1200 INSIDE OF C-3 CARGO. REMOVED CORROSION TREATED AND PRIMED AREA, AND INSTALLED NEW FITTING PER SRM 53-2-0. (M) 2L74 4F 4A25 19951113003821995111300382NM 1995 11 13 AALA950050H 119951012A5315141T5113 FLOOR BEAM BOEING767 767223 1385123NM BS 325 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FLOOR BEAM HAS CORROSION BEYOND LIMITS. FABRICATED REPAIR DOUBLER FROM 0.050 CRES STEEL AND INSTALL WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1030. (M) 2L72 4F RTA1NM 19951113003831995111300383NM 1995 11 13 AALA950051H 119951012A5313146T3002 STRINGER BOEING767 767223 1385123NM BS 1472 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - REMOVED STRINGER SECTION, CORRODED BEYOND SRM LIMITS. FABRICATE LONGER SPLICE FROM SAME MATERIAL TYPE AND SHAPE PER ENGINEERING MRB 767-1032. (M) 2L72 4F RTA1NM 19951113003841995111300384NM 1995 11 13 AALA950052H 119951012A5230143T51902 FAIL/SAFE STRAP BOEING767 767223 1385123NM BS 747 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FORWARD CARGO DOOR FAIL/SAFE STRAP HAD CORROSION BEYOND SRM LIMITS. REMOVED CORROSION AND REPLACED FASTENERS PER ENGINEERING MRB 767-1023. (M) 2L72 4F RTA1NM 19951113003851995111300385NM 1995 11 13 AALA951693 119950818A5315141N2930 FLOOR BEAM BOEING757 757223 1384957NM BS 324 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07630AA 24588 AFW - CORROSION BLENDED ON FLOOR BEAM AT STATION 324, RBL 61 IS BEYOND SRM LIMITS, REPAIRED PER MRB. (M) 2L72 4F RTA2NM 19951113003861995111300386NM 1995 11 13 AALA951694 119950818A5315141N5111 FLOOR BEAM BOEING757 757223 1384957NM BS 345 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07630AA 24588 AFW - CORROSION BLENDED ON FLOOR BEAM AT STATION 345, LBL 12, IS BEYOND SRM LIMITS, PER MRB 757-589. (M) 2L72 4F RTA2NM 19951113003871995111300387NM 1995 11 13 AALA951695 119950816A5315146N5089 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07630AA 24588 AFW - FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED BEYOND SRM LIMITS, PER MRB 757-586. (M) 2L72 4F RTA2NM 19951113003881995111300388NM 1995 11 13 AALA951696 119950816A5320146N5300 DECK BOEING757 757223 1384957NM BS 1681/1716 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07630AA 24588 AFW - PRESSURE DECK HAS CORROSION REMOVAL AT STATION 1716 AND STATION 1681 AT VARIOUS BL LOCATIONS, MATERIAL REMAINING IS BEYOND SRM LIMITS, PER MRB 757-587. (M) 2L72 4F RTA2NM 19951113003891995111300389NM 1995 11 13 AALA951697 119950816A5320141N8315 DOOR FRAME BOEING757 757223 1384957NM BS 338 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07630AA 24588 AFW - FRAME AT STATION 338, WL 263 AND LBL IS CRACKED, PER MRB 757-585. (M) 2L72 4F RTA2NM 19951113003901995111300390NM 1995 11 13 AALA951707 119950925A5315141N5112 FLOOR BEAM BOEING757 757223 1384957NM BS 365 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07633AA 24591 AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS AT STATION 365, LBL 10, RBL 14 AND RBL 61, PER MRB 757-610. (M) 2L72 4F RTA2NM 19951113003911995111300391NM 1995 11 13 AALA951708 119950925A5320146N5300 PLATE BOEING757 757223 1384957NM DECK CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07633AA 24591 AFW - CORROSION BLENDED BEYOND SRM LIMITS IN SEVERAL AREAS OF THE DECK PLATE, PER MRB 757-611. (M) 2L72 4F RTA2NM 19951113003921995111300392NM 1995 11 13 AALA951710 119950925A5315141N2932 FLOOR BEAM BOEING757 757223 1384957NM BS 324 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07633AA 24591 AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS AT STATION 324 RBL 60, PER MRB 757-608. (M) 2L72 4F RTA2NM 19951113003931995111300393NM 1995 11 13 AALA951712 119950925A5315146N5090 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07633AA 24591 AFW - FLOOR BEAM HAD CORROSION BLENDED BEYOND SRM LIMITS, STATION 1640 RBL 54, LBL 54, PER MRB 757-607. (M) 2L72 4F RTA2NM 19951113003941995111300394NM 1995 11 13 AALA951713 119950925A5512185N4002 SKIN BOEING757 757223 1384957NM HORIZ STAB DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW07633AA 24591 AFW - RIGHT HORIZ SKIN PANEL HAS DENT ON LOWER SURFACE (HONEYCOMB PANEL), PER MRB 757-616. (M) 2L72 4F RTA2NM 19951113003951995111300395NM 1995 11 13 ASAA9510089 119950922A3350MS250851 EEL SWITCH BOEING737 737290C 138448VNM CABIN FAILED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING MAINTENANCE CHECK, THE AFT FLIGHT ATTENDANT EMERGENCY EXIT LIGHT SWITCH FAILED. REPLACED SWITCH AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19951113003961995111300396NM 1995 11 13 ASAA9510090 119950923A3350900835A EEL BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - FLT NR 340 - CREW REPORTED THE WHITE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 REMAINED ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19951113003971995111300397NM 1995 11 13 ASAA9540052 119950911A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01778AS 25110 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951113003981995111300398NM 1995 11 13 ASAA9540053 119950913A3350273005 EEL PICO FUSE BOEING737 7374Q8 NM CABIN BLOWN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 JNU - DURING MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN MAIN CABIN. REPLACED PICO FUSE IN BATTERY POWER SUPPLY AND ALL LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951113003991995111300399WP 1995 11 13 ASAA9580185 119950814A78307936907603 HYD LINE DOUG DC9 DC982 3022082WP LT ENGINE TR BROKEN A ASAAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 NM01932AS 49233 PDX - JUST PRIOR TO PARKING AT GATE OF FLIGHT NR 475, CREW REPORTED SMOKE/FUMES IN CABIN AND LEFT HYDRAULIC QUANTITY DECREASED TO ZERO. SHUTDOWN ENGINES, APU, ELECTRICAL POWER AND OPENED ALL DOORS. PASSENGERS DEPLANED WITHOUT INCIDENT. FOUND HYDRAULIC LINE TO LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE SWITCH BROKEN. REPLACED HYDRAULIC LINE AND SERVICED LEFT HYDRAULIC SYSTEM. (M) 2L72 4F A6WE 19951113004001995111300400 1995 11 13 ASAA9580189 419950821A2565D37013109 SLIDE BOTTLE DOUG DC9 DC983 3022083WP L1 DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01949AS 53022 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE. (M) 2L72 4F RTA6WE 19951113004011995111300401NE 1995 11 13 MRKA9570 219951004A7230817401E C-1 FAN BOEING737 7372X6C 1384552NM PWA JT8 JT8D17A 52049NE NR 1 ENGINE BENT A MRKAO OTHER C F.O.D. APAPPROACH 1 AL03673MA 23124 ON APPROACH TO MDW, AIRCRAFT SUSTAINED DAMAGE TO THE NR 1 ENGINE FAN BY A BIRD STRIKE. THE LANDING OCCURED WITHOUT FURTHER INCIDENT. INSPECTED NR 1 ENGINE PER MAINTENANCE MANUAL 72-00. FOUND TWO BLADES BENT BEYOND LIMITS PER 72-33-21, PAGE 801-808, FIGURE 802-803, AND THREE BLADES SHINGLED AT MIDSPAN. REMOVED AND REPLACED C-1 FAN PER WORK CARD 7205 AND ACCOMPLISHED BIRD STRIKE INSPECTION PER JOB CARD 0511. NO FURTHER DAMAGE NOTED. (M) 2L72 4F4 FRTA16WE E2EA 19951113004021995111300402WP 1995 11 13 ORJA9589 119951003A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 OVERHEAD EMERGENCY LIGHTS INOP, ROW 20-26. INSTALLED NEW BATTERIES. OPS TEST NORMAL. (M) 2L72 4F RTA6WE 19951113004031995111300403WP 1995 11 13 ORJA9590 119951002A33500105606003 EEL WIRE DOUG DC9 DC982 3022082WP CABIN FAILED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11843RA 49615 FIRST CLASS FLOOR TRACK LIGHTING INOP. FIRST CLASS FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED FIRST CLASS FLOOR TRACK SOCKET STRIP, OPS NORMAL. (M) 2L72 4F A6WE 19951113004041995111300404WP 1995 11 13 ORJA9591 119951007A335060330431 EEL BATTERY PACKGRIMES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11836RA 53046 OVERHEAD 'CEILING' EMERGENCY LIGHT INOP, SEAT 6 THROUGH 10. REMOVED AND REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS SEAT 6 THROUGH 10. (M) 2L72 4F RTA6WE 19951113004051995111300405WP 1995 11 13 ORJA9592 119951007A335041B004AD073 EEL BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11821RA 49931 OVERHEAD EXIT LIGHT OUT AT ROW 21 RIGHT SIDE. REPLACED BATTERIES. EXIT LIGHT ILLUMINATES WITH EMERGENCY POWER ON. (M) 2L72 4F A6WE 19951113004061995111300406WP 1995 11 13 ORJA9593 119950929A5320 STRAKE DOUG DC9 DC983 3022083WP RIGHT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11872RA 49793 RIGHT STRAKE HAS CORROSION ON BOTTOM SIDE. REMOVED CORROSION ON RT STRAKE BOTTOM SIDE IAW SRM 51-10-03 AND 53-05-00 WITHIN LIMITS. (M) 2L72 4F RTA6WE 19951113004071995111300407 1995 11 13 ORJA9594 419950929A3442 ANTENNA DOUG DC9 DC983 3022083WP RADAR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11872RA 49793 RADAR ANTENNA RADIATOR HAS PITS AND SLIGHT SURFACE CORROSION IN ONE SPOT ON THE BACK. REMOVED SLIGHT SURFACE CORROSION REF SRM 51-10-3 AND TREATED SURFACE REF SRM 51-10-3. (M) 2L72 4F RTA6WE 19951113004081995111300408WP 1995 11 13 ORJA9595 119950930A2910 HYD LINES DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11872RA 49793 LEFT TUNNEL, HYDRAULIC LINES 1PBD OF OUT FLOW VALVES, CORROSION ON LINES. CLEANED CORROSION IAW SRM 51-10-3 AND CHEMICALLY TREATED AND PAINTED. (M) 2L72 4F RTA6WE 19951113004091995111300409WP 1995 11 13 ORJA9596 119951009A5320 WINDOW FRAME DOUG DC9 DC983 3022083WP LT COCKPIT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11873RA 53093 MINOR SURFACE CORROSION ON EXTERNAL WINDOW FRAME AROUND CAPTAIN SLIDING WINDOW, 3 PLACES. CLEANED AND TREATED CORROSION IAW MD80, 51-10-3. (M) 2L72 4F RTA6WE 19951113004101995111300410WP 1995 11 13 ORJA9597 119951009A5320 WINDOW FRAME DOUG DC9 DC983 3022083WP RT COCKPIT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11873RA 53093 MINOR SURFACE CORROSION ON EXTERNAL WINDOW FRAME BETWEEN CO-PILOTS SLIDING WINDOW AND AFT WINDOW, 2 PLACES. CLEANED AND TREATED CORROSION IAW MD80, 51-10-3. (M) 2L72 4F RTA6WE 19951113004111995111300411 1995 11 13 ORJA9598 419951009A3442 ANTENNA DOUG DC9 DC983 3022083WP RADAR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11873RA 53093 CORROSION ON BACK SIDE RADAR ANTENNA. CLEANED AND TREATED CORROSION, IAW MD80 SRM 51-10-3. (M) 2L72 4F RTA6WE 19951113004121995111300412WP 1995 11 13 ORJA9599 119951001A33501001191 EEL DOUG DC9 DC983 3022083WP CABIN INOP A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11836RA 808 53046 EMERGENCY PORTABLE FLASH LIGHT AT FWD CABIN DOOR NOT PROPERLY WORKING. REMOVED AND REPLACED UNIT SYSTEM ARMS AND OPS NORMAL. (M) 2L72 4F RTA6WE 19951113004131995111300413NM 1995 11 13 P91A008 119951016A3230 CABLES BOEING727 727231 1384079NM RT MLG LACK OF LUBE A P9IAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 SO037431861915 20051 RIGHT MAIN MANUAL GEAR EXTENSION CABLES ARE BINDING. REPORTED DURING MANUAL EXTENSION AFTER 'A' SYSTEM FAILURE. LUBED CABLES AND ACCOMPLISHED GEAR SWING AND MANUAL EXTENSION PER M/M 32-30-6. (M) 2L73 4F A3WE 19951113004141995111300414NM 1995 11 13 P9IA007 119951016A2910651784417 HYD TUBE BOEING727 727231 1384079NM NR 2 ENGINE CHAFED A P9IAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 SO037431861915 20051 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO IN ABOUT 20 MINUTE TIME SPAN. FOLLOWED 'A' SYSTEM FAILURE CHECK LIST, MANUALLY LOWERED LANDING GEAR AND FLAPS. REPLACED NR 2 ENGINE 'A' SYSTEM PRESSURE LINE, SERVICED HYDRAULIC SYSTEM. RUN UP AND LEAKED CHECKED GOOD PER MM 71-00 AND 29-10-0. (M) 2L73 4F A3WE 19951113004151995111300415WP 1995 11 13 TWAA9575 119950822A5320 T-CAP DOUG DC9 DC932 3022066WP FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05997Z 47029 MCI - DURING OP-15, FOUND CORROSION IN HORIZONTAL LEG AT T-CAP BETWEEN STRINGERS 12 AND 13. REMOVED CORROSION AND INSTALLED CLIPS PER SERVICE BULLETIN 57-98. (M) 2L72 4F A6WE 19951113004161995111300416NM 1995 11 13 TWAA9578 119951008A497038760245 OIL PRESS SW BOEING767 767231 1385131NM APU MALFUNCTIONED A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE05603TW 22566 JFK - DURING CLIMB, APU HAD AN AUTO SHUT DOWN. BITE CHECK SHOWED LOW OIL PRESSURE. REPLACED LOW OIL PRESSURE SWITCH, MFG P/N 3876024-5. APU OPERATION THEN CHECKED NORMAL. (M) 2L72 4F RTA1NM 19951113004171995111300417NE 1995 11 13 TWAA9579 219951010A7261RD21891 OIL TUBE BOEING727 727231 1384079NM PWA JT8 JT8D9A 52048NE NR 1 ENGINE CRACKED A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0554342 21629 STL - DURING CRUISE, NR 1 ENGINE WAS SHUT DOWN DUE TO OIL QUANTITY DECREASING TO ONE GALLON. FOUND NR 6 SCAVANGE PUMP OIL TUBE, MFG P/N RD2189-1, TO BE CRACKED. REMOVED AND REPLACED CRACKED SCAVANGE OIL TUBE, RAN ENGINE PERFORMANCE LEAK CHECK, FOUND NORMAL. (M) 2L73 4F4 F A3WE E2EA 19951113004331995111300433CE 1995 11 13 95ZZZX6191 119950824A27305052443934 CONTROL CABLE BEECH 90 E90 1152914CE ELEV CONTROL SEVERED ALABBCAK NONE F FLT CONT AFFECTED ININSP/MAINT 1 EA03214K 9284 LW34 PILOT REPORTED PARTIAL LOSS OF ELEVATOR CONTROL. UPON TROUBLESHOOTING THE SYSTEM, FOUND THE DOWN CONTROL CABLE SEVERED BELOW PILOT'S FLOORBOARDS AT A POINT WHERE A WIRING BUNDLE CROSSES THIS CABLE. IN THIS WIRE BUNDLE, WIRE NR H16A10 WHICH IS FOR THE COPILOT'S WINDSHIELD HEAT, HAD CHAFED ON THE CONTROL CABLE, AND, AS A RESULT, AN ARCING HAD OCCURRED. THERE WAS NO INDICATION THIS WIRE BUNDLE HAD EVER BEEN WORKED ON IN THIS AREA. SUBMITTER SUSPECTS SAGGING OF THIS BUNDLE OVER THE LIFE OF THE AIRCRAFT MAY HAVE CONTRIBUTED TO THIS PROBLEM. 1L72 3T 3A20 19951113004421995111300442EA 1995 11 13 95ZZZX6200 219950208A7261 OIL SCREEN BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA NR 1 BRG OIL JETFAILED A ALCFAE ENGINE SHUTDOWN O OTHER NRNOT REPORTED 1 NM0981FL 30753 PS60382 OPERATOR ADVISED OF IN-FLIGHT SHUT DOWN AND SAFE LANDING. INCIDENT TRACED TO LAST SHOP VISIT WHERE NON-EMBODIMENT OF SB 5241R2 AND SIL 5051. 1G71 4U4 U H4SW E22EA 19951113004431995111300443WP 1995 11 13 9517419930 119951106A3350 BATTERIES DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL0189S 47042 DURING LINE CHECK, FOUND CENTER SECTION UPPER EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004441995111300444WP 1995 11 13 9517429991 119951106A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN FAILED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018957E 47215 DURING LINE CHECK, FOUND THREE AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004451995111300445WP 1995 11 13 9517439106 119951106A3350 BATTERY PACK DOUG DC9 DC915 3022036WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL0196S 47206 DURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004461995111300446WP 1995 11 13 9517449301 119951105A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01301RC 48054 DURING LINE CHECK, FOUND FORWARD SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951113004471995111300447WP 1995 11 13 9517459305 119951105A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01307RC 48086 DURING LINE CHECK, FOUND FORWARD SECTION OF FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004481995111300448WP 1995 11 13 9517469958 119951103A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01917RW 47145 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004491995111300449WP 1995 11 13 9517479971 119951103A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019335 47337 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 5-10. REPLACED BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951113004501995111300450NE 1995 11 13 9517489976 219951103A7200 ENGINE PWA JT8D7B DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE LEFT BIRD STRIKE A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN CY F.O.D. ENGINE STOPPAGE CLCLIMB 1 GL019340 657271 47389 657271 DURING CLIMB, THE LEFT ENGINE INGESTED A LARGE BIRD. CREW SHUT DOWN THE ENGINE AND RETURNED TO DTW. THE AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED BIRD STRIKE INSPECTION AND REPLACED THE LEFT ENGINE. OPERATIONAL CHECK GOOD. 2L72 4F4 F A6WE E2EA 19951113004511995111300451NM 1995 11 13 9517492283 119951105A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01283US 21322 DURING SERVICE CHECK, FOUND OVERHEAD EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2L73 4F A3WE 19951113004521995111300452EU 1995 11 13 9517503225 119951106A3350321454 BATTERY PACK AIRBUS320 A320211 3930320EU CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01325US 281 DURING LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS TEST FAULTED LEFT. REPLACED THE BATTERY PACK (13WL). OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951113004531995111300453NM 1995 11 13 9517512294 119951107A2761 ACTUATOR BOEING727 727251 138408HNM SPOILER FAILED A NWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 GL01294US 21505 DURING TAKEOFF, TAKEOFF WARNING HORN SOUNDED AT V1, HORN STOPPED WHEN AIRBORNE WITH FLAPS AND SLATS RETRACTED. AIRCRAFT ALSO HAD HEAVY VIBRATION DURING TAKEOFF, CONDITION STOPPED WITH FLAPS RETRACTED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. PERFORMED TAKEOFF WARNING CHECK AND FOUND SPOILER ACTUATOR BYPASSING FLUID. REPLACED SPOILER ACTUATOR. RE-PERFORMED TAKEOFF WARNING CHECK. CHECKED OK. 2L73 4F A3WE 19951113004541995111300454NM 1995 11 13 9517522294 119951106A2751 POSITION IND BOEING727 727251 138408HNM RT TE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 GL01294US 21505 DURING DESCENT ON FLAP EXTENSION TO 5 DEGREES, OUTBOARD FLAPS HAD ASYMMETRIC TRIP AT 3 DEGREES. AIRCRAFT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. CHECKED OUTBOARD FLAP TRANSMISSIONS, TORQUE TUBES, AND CABLES. ALL CHECKED NORMAL. FOUND RIGHT OUTBOARD FLAP INDICATOR NEEDLE ERRATIC. REPLACED FLAP POSITION INDICATOR. OPERATIONAL CHECK OK. 2L73 4F A3WE 19951113004551995111300455WP 1995 11 13 9517531160 119951104A3231 LINK DOUG DC10 DC1040 3023508WP CTR MLG DOOR FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL E VIBRATION/BUFFET CLCLIMB 1 GL01160US 46769 DURING CLIMB, THE AIRCRAFT EXPERIENCED EXCESSIVE VIBRATION. AIRCRAFT DUMPED 120,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED LEFT FORWARD CENTER GEAR DOOR DRIVE LINK AND OPERATIONAL CHECK OK. 2L73 4F A22WE 19951113004561995111300456WP 1995 11 13 9517549903 119951103A5350 CLIPS DOUG DC9 DC931 3022065WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01953N 47083 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS. REPLACED THE AFT CLIP, CLEANED THE FORWARD CLIP, AND ADJUSTED BOTH. CHECKED OK. 2L72 4F A6WE 19951113004571995111300457 1995 11 13 9517559925 419951107A344220671570153 TRANSCEIVER DOUG DC9 DC932 3022066WP RADAR FAILED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01925US177871044 47472 DURING CRUISE, WEATHER RADAR RETURNS WERE INTERMITTENT. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED RADAR TRANSCEIVER. OPERATIONAL TEST GOOD. 2L72 4F A6WE 19951113004581995111300458NM 1995 11 13 9517565531 119951107A2751215016001 INDICATOR BOEING757 757251 1384970NM TE FLAPS MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01531US9518 9518 23846 DURING APPROACH INTO MSP, THE TRAILING EDGE FLAPS WERE ASYMMETRIC BETWEEN FLAPS POSITION 15 AND 20 DEGREES. AN EMERGENCY WAS DECLARED WITH EQUIPMENT STANDING BY. THE AIRCRAFT LANDED WITHOUT INCIDENT WITH FLAPS IN THE 15 DEGREE POSITION. MAINTENANCE REPLACED THE FLAP POSITION INDICATOR. OPERATIONAL CHECK OK. 2L72 4F RTA2NM 19951113004591995111300459NM 1995 11 13 95FDEA01695 119951107A5210 CLOSING MECH BOEING727 727277 138408SNM PAX DOOR OUT OF ADJUST A FDEAAI UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CRCRUISE 1 SO25243FE 21480 FORWARD ENTRY DOOR LIGHT ILLUMINATED IN-FLIGHT, DEPRESSURIZED AND DESCENT TO 5000 FEET MSL. A/C WAS DEPRESSURIZED FOR REMAINDER OF FLIGHT (15 MINUTES) AT 5000 FEET. REMOVED DOOR LINER AND ADJUSTED UPPER AND LOWER LATCH TORQUE TUBE CONTROL RODS. OPS CHECK NORMAL. REINSTALLED LINER. MM REF 52-11-01 PAGES 514 - 516 AND 52-11-61. 2L73 4F RTA3WE 19951113004601995111300460NM 1995 11 13 95FDEA01696 119951102A24007161M661G03 HARNESS DOUG MD11 MD11 3023602NM NR 1 ENGINE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 NR 1 ENG ELECTRICAL HARNESS, BROWN AT THE SIX O'CLOCK POSITION IS CHAFING HARD AGAINST DRAW LINES THROUGH COATING AND WIRE MESH. REMOVED AND REPLACED ELECTRICAL HARNESS (P/N 7161M661G03), COMPLIED WITH EO 1-7520-7-3304 ON NEW HARNESS (P/N 1821M62G03). PERFORMED POWER ASSURANCE ENG RUN PER MM 71-50-04-4-1, ELECTRICAL HARNESS REPLACEMENT PER MM 71-50-04-1-1 AND MM 70-10-00-2-1. 2L73 4F RTA22WE 19951113004611995111300461NM 1995 11 13 95FDEA01697 119951106A24007161M661G04 HARNESS DOUG MD11 MD11 3023602NM NR 1 ENGINE CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25606FE 48602 NR 1 ENG ELECTRICAL HARNESS, BLACK AT THE SIX O'CLOCK POSITION IS CHAFING HARD AGAINST TRAIN LINES THROUGH THE COATING AND WIRE MESH. REMOVED AND REPLACED CABLE (P/N 7161M60G04) INSTALLED PER MM 71-50-04-4-1. PERFORMED POWER ASSURANCE RUN REQUIRED PER MM 71-50-04-4-1 AND INSTALLED PER MM 70-10-00-2-1. 2L73 4F RTA22WE 19951113004621995111300462NM 1995 11 13 95UAL900250 119951107A321365461166 STRUT BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 3 MLG CRACKED A UALAK NONE L NO TEST ININSP/MAINT 1 WP299053U1910019100 19934 NR THREE MAIN LANDING GEAR INNER CYLINDER BRAKE FLANGE HAS TWO CRACKS. CRACKS START FROM THE INSIDE OF THE MOUNT BOLT HOLES AT THE 2 O'CLOCK AND 10 O'CLOCK POSITIONS AND EXTEND INWARD TOWARD FLANGE RADIUS. CRACKS CONFIRMED BY EDDY CURRENT INSPECTION. REPLACED LOWER STRUT PER MM 32-11-11. 2L72 4F4 F A16WE E2EA 19951113004631995111300463NM 1995 11 13 95UAL900251 119951108A3233119851 ACTUATOR BOEING747 747122 1384872NM NLG FAILED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP294732U 19927 NLG DOOR LIGHTS STAYED ON AFTER GEAR RETRACTION. ALSO, HAD AIR NOISE WHEN HANDLE WAS IN OFF POSITION. CYCLED GEAR AND LIGHTS WENT OUT. HOWEVER, NOISE RETURNED AND LIGHTS CAME ON WITH HANDLE IN OFF POSITION. NOSE GEAR ACTUATOR PISTON FAILED. REPLACED NOSE GEAR ACTUATOR. 2L74 4F A20WE 19951113004641995111300464NM 1995 11 13 95UAL900252 119951108A3350 BATTERY PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29182UA 25279 EMERGENCY ESCAPE LIGHTS INOP AT G4 CEILING, DOOR 4L OVERDOOR EXIT SIGN AND DOOR 4L THRESHOLD LIGHTS. REPLACED CHARGER AND BATTERY PACK. 2L74 4F4 FRTA20WE E24NE 19951113004651995111300465SW 1995 11 13 MEJA951001 119951011A53302621000031 SKIN SWRNGNSA227 SA227AC 8780603SW FWD FUSELACE CRACKED E AMEJAK NONE C F.O.D. DEDESCENT 1 SW172691W AC655 FLIGHT 361, RDU TO CVG, 35 NAUTICAL MILES SOUTHWEST OF CVG WHILE DESCENDING OUT OF 8,000 FEET FOR 4,000 FEET, A LARGE BIRD STRUCK THE AIRCRAFT ABOVE THE CENTER WINDSHIELD. AIRCRAFT LANDED AT CVG WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED TO RDU FOR REPAIR. MAINTENANCE REPAIRED CRACKED SKIN ABOVE WINDSHIELD IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT STRUCTURAL REPAIR MANUAL 51-90-04. PRESSURIZATION CHECK WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951113004661995111300466SW 1995 11 13 MEJA951002 119951014A573027310008003 SKIN SWRNGNSA226 SA226TC 8780404SW LT WING LE CRACKED E AMEJAK NONE C F.O.D. CRCRUISE 1 SW17162MA TC234 FLIGHT 9821, CRP TO SAT, WHILE IN CRUISE AT 6,000 FEET, THE FLIGHT CREW HEARD A LOUD THUMP. CONTINUED FLIGHT TO SAT AND LANDED WITHOUT INCIDENT. AFTER LANDING, THE AIRCRAFT WAS INSPECTED AND IT WAS FOUND THAT A LARGE BIRD HAD STRUCK THE LEFT INBOARD LEADING EDGE OF THE WING, JUST INBOARD OF THE ENGINE NACELLE. MAINTENANCE REMOVED AND REPLACED THE LEADING EDGE SKIN IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT STRUCTURAL REPAIR MANUAL 51-00-00. FUNCTIONAL CHECK FLIGHT WAS PERFORMED AFTER REPLACEMENT AND NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA8SW 19951113004671995111300467SW 1995 11 13 MEJA951003 119951021A77228974697 EGT HARNESS SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE BROKEN E AMEJACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SW17163MA TC236 P54032 FLIGHT 9936, FAR TO BIS, THE LEFT ENGINE EGT FLUCTUATED AND THEN WENT TO ZERO DURING THE TAKEOFF ROLL. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE RAMP. MAINTENANCE FOUND BROKEN EGT HARNESS. REMOVED AND REPLACED HARNESS IN ACCORDANCE WITH GARRETT MAINTENANCE MANUAL. FUNCTIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19951113004681995111300468SW 1995 11 13 MEJA951004 119951024A771231024761E TQ SIGNAL COND SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE FAILED E AMEJAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SW172671V AC437 P44090 FLIGHT 8043, TJSJ TO TTPP, THE LEFT TORQUE WOULD NOT INCREASE ABOVE 77 PERCENT. THE AIRCRAFT RETURNED TO TJSJ AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BAD TORQUE SIGNAL CONDITIONER. REMOVED AND REPLACED TORQUE SIGNAL CONDITIONER IN ACCORDANCE WITH THE GARRETT MAINTENANCE MANUAL. PERFORMED FUNCTIONAL CHECK. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T4 TRTA8SW E4WE 19951113004691995111300469SW 1995 11 13 MEJA951005 119951027A7603111B0100 CONTL MECH SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT POWER LEVER WORN E AMEJAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 SW17163MA TC236 P54032 FLIGHT 9935, BIS TO FAR, WHILE ON DESCENT TO FAR THE LEFT ENGINE POWER WOULD NOT REDUCE BELOW 47 PERCENT TORQUE. THE FLIGHT CREW SHUT DOWN THE ENGINE FOR POSITIVE CONTROL AND LANDED AT FAR WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE POWER LEVER BALL JOINT AND ROD END DEFECTIVE. REMOVED AND REPLACED THE BALL JOINT AND ROD END IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT INCORPORATED MAINTENANCE MANUAL 76-10-10. FUNCTIONAL GROUND CHECK WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19951113004701995111300470SW 1995 11 13 MEJA951006 119951019A33102719115023 PANEL LIGHT SWRNGNSA227 SA227AT 8780610SW LT COCKPIT SHORTED E AMEJAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW17573G AT446 FLIGHT 7074, MKJP TO MIA, DURING CLIMB OUT, SMOKE APPEARED IN THE COCKPIT. THE AIRCRAFT RETURNED TO MKJP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THAT THE LEFT CONSOLE PANEL LIGHT WAS SHORTED. MAINTENANCE CUT, CAPPED AND STOWED THE WIRES FOR THE LEFT HAND CONSOLE PANEL LIGHTS AND THE ITEM WAS MEL'D IN ACCORDANCE WITH 33-1. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19951113004711995111300471SW 1995 11 13 MEJA951007 119951103A612031030952 NTS ORIFICE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE CRACKED E AMEJAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW17682AV AC682 P44200 FLIGHT FAE 131, DTW TO SAT, WHILE IN CRUISE, THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE PRESSURE INDICATOR DECREASED BELOW 40 PSI. THE FLIGHT CREW SHUT DOWN THE ENGINE AND LANDED AT CMI WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A DEFECTIVE NEGATIVE TORQUE SENSOR (NTS) ORIFICE HOUSING. REMOVED ORIFICE AND CONNECTING TUBE ASSEMBLY IN ACCORDANCE WITH THE GARRETT MAINTENANCE MANUAL. FUNCTIONAL CHECK WAS PERFORMED AND NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A8SW E4WE 19951113004721995111300472EU 1995 11 13 WWMA9500081 119951107A3150 WEU SAAB SF340 340B 7860101EU COCKPIT MALFUNCTIONED A WWMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP15313AE 340B313 AIRCRAFT ABORTED TAKEOFF DUE TO THE AUTOCOARSEN LIGHT ILLUMINATING AT 40 KNOTS. MAINTENANCE RERACKED THE WEU AND RELEASED THE AIRCRAFT. 2L72 4T RTA52EU 19951117000011995111700001WP 1995 11 17 9517579991 119950911A5412 BLKHD WEB DOUG DC9 DC931 3022065WP FS 965 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND OIL CANNING IN THE FS 965 PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED WEB (P/N 9912243-81), PER EA 99-102744. 2L72 4F A6WE 19951117000021995111700002WP 1995 11 17 9517589751 119951002A5522 SKIN DOUG DC9 DC941 302207NWP RT ELEVATOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01751NW 47115 DURING B-CHECK, FOUND TWO, 2 INCH CRACKS IN THE RIGHT ELEVATOR LOWER SKIN AT STA 658. REPAIRED PER EA 97-102591. 2L72 4F A6WE 19951117000031995111700003WP 1995 11 17 9517599991 119951007A5311 FRAME DOUG DC9 DC931 3022065WP FS 908 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 908 FRAME BETWEEN LONGERONS 13L TO 17L. REPAIRED FRAME PER EA 99-102887. 2L72 4F A6WE 19951117000041995111700004WP 1995 11 17 9517609979 119951019A5412 BLKHD WEB DOUG DC9 DC931 3022065WP FS 965 OIL CANNING A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB FS 965, LEFT SIDE. REPAIRED WEB (P/N 9912243-3), PER EA 99-103304. 2L72 4F A6WE 19951117000051995111700005WP 1995 11 17 9517619864 119951019A5320 INTERCOSTAL DOUG DC9 DC951 3022051WP FS 140 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK, FOUND A CRACK IN THE INTERCOSTAL BETWEEN THE SERVICE DOOR JAMB AND COCKPIT LOWER SILL FS 140. REPAIRED INTERCOSTAL (P/N 9911557-3), PER EA 98-101990. 2L72 4F A6WE 19951117000061995111700006WP 1995 11 17 9517629864 119951019A5412 BLKHD WEB DOUG DC9 DC951 3022051WP FS 1136 OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01773NC 47775 DURING H-CHECK, FOUND OIL CANNING IN THE FS 1136 PYLON BULKHEAD WEB, LEFT AND RIGHT SIDES. REPAIRED WEBS (P/N 9912243-81, -4, -3) PER EA 98-103301. 2L72 4F A6WE 19951117000071995111700007WP 1995 11 17 9517639878 119951025A5412 BLKHD WEB DOUG DC9 DC951 3022051WP LT/RT PYLON OIL CANNED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01787NC 48149 DURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB, LEFT AND RIGHT SIDES. REPAIRED WEB (P/N 9912243), PER EA 98-102600. 2L72 4F A6WE 19951117000081995111700008WP 1995 11 17 9517649979 119951026A5311 FRAME DOUG DC9 DC931 3022065WP FS 408 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING H-CHECK, FOUND A .375 INCH CRACK IN THE FS 408 FRAME AT LONGERON 17R. REPAIRED FRAME (P/N 5911447-1), PER EA 99-103307. 2L72 4F A6WE 19951117000091995111700009WP 1995 11 17 9517659878 119951026A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FS 1136 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01787NC 48149 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOORBEAM CHORD AT RBL 25. REPAIRED FLOORBEAM (P/N 9912243-55), PER EA 98-103308. 2L72 4F A6WE 19951117000101995111700010WP 1995 11 17 9517669991 119951026A5712 RIB DOUG DC9 DC931 3022065WP WS 69 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT WING RIB LOWER SUPPORT TEE, STA 69. REPAIRED TEE (P/N 9919349-7), PER EA 99-102885. 2L72 4F A6WE 19951117000111995111700011WP 1995 11 17 9517679991 119951026A5311 FRAME DOUG DC9 DC931 3022065WP FS 945 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018957E 47215 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 945 FRAME BETWEEN LONGERONS 29L TO 30. REPAIRED FRAME (P/N 9957739-45), PER EA 99-102722. 2L72 4F A6WE 19951117000121995111700012WP 1995 11 17 9517689972 119951029A5330 SKIN DOUG DC9 DC931 3022065WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019336 47338 DURING L-CHECK, FOUND CORROSION IN THE FUSELAGE SKIN AT FS 604, LONGERON 30. REPAIRED SKIN (P/N 5911418-503), PER EA 99-103309. 2L72 4F A6WE 19951117000131995111700013NM 1995 11 17 9517696635 119951102A5415 FITTING BOEING747 747227B 1384888NM NR 3 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01635US 21682 DURING PERIODIC CHECK, FOUND A .375 INCH CRACK IN THE NR 3 PYLON STRUT TO DIAGONAL BRACE ATTACH FITTING. REPLACED FITTING PER EA 5440-01025. 2L74 4F A20WE 19951117000141995111700014WP 1995 11 17 9517709610 119951102A5320 FITTING DOUG DC9 DC932 3022066WP FS 37 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL LEFT TIE FITTING FS 37. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951117000151995111700015NM 1995 11 17 9517716635 119951104A5744 FITTINGS BOEING747 747227B 1384888NM FLAP TRACK CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01635US 21682 DURING PERIODIC CHECK, FOUND CORROSION IN THE RIGHT WING OUTBOARD FLAP SIDE LOAD FITTINGS, NR 7 FLAP TRACK, INBOARD AND OUTBOARD. ALSO, NR 8 FLAP TRACK, INBOARD. REPLACED FITTINGS PER CITEXT 04139. 2L74 4F A20WE 19951117000161995111700016WP 1995 11 17 9517729877 119951105A5320 FITTING DOUG DC9 DC951 3022051WP FS 1167 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01786NC 48148 DURING H-CHECK, FOUND A CRACK IN THE FS 1167 FLOORBEAM END FITTING, RIGHT SIDE. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19951117000171995111700017NM 1995 11 17 9517736739 119951107A324626070812 WHEEL BOEING747 747251F 1384898NM WHEEL WELL DAMAGED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK CE F.O.D. VIBRATION/BUFFET TOTAKEOFF 1 GL01639US 23887 DURING TAKEOFF, THE AIRCRAFT HIT A LARGE BRAKE DRUM ON THE RUNWAY AND ABORTED TAKEOFF AT 1340 KNOTS. BOTH THE FIRST OFFICER'S AND SECOND OFFICER'S INSTRUMENT PANELS WERE FOUND LOOSE. ALSO, SEVERAL INSTRUMENT GAUGES CAME LOOSE DUE TO SEVERE VIBRATION FROM THE INCIDENT. REPLACED THE RIGHT AND LEFT NOSE WHEELS AND NOSE TIRES. RESECURED ALL INSTRUMENTS AND PANELS. ALSO, DAMAGED INSTRUMENTS WERE REPLACED. PERFORMED CHECK AND TEST WAS NORMAL. 2L74 4F A20WE 19951117000181995111700018NM 1995 11 17 9517742708 119951108A3350 EEL POWER SUPPLY BOEING727 727225 1384077NM CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01817EA 22554 DURING PREFLIGHT, FOUND THE LEFT SIDE OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. 2L73 4F A3WE 19951117000191995111700019NM 1995 11 17 9517755503 119951109A3350 EEL WIRE BOEING757 757251 1384970NM CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01503US 23192 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS AT ROWS 23 THROUGH 32 INOPERATIVE. REPAIRED BROKEN WIRE. 2L72 4F RTA2NM 19951117000201995111700020NM 1995 11 17 9517765502 119951107A3350 EEL WIRE BOEING757 757251 1384970NM COCKPIT BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01502US 23191 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE, OPERATIONAL CHECK NORMAL. 2L72 4F RTA2NM 19951117000211995111700021NM 1995 11 17 9517776308 119951108A3350 BATTERY CHARGER BOEING747 747451 1384940NM EXTERIOR INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01668US 24223 DURING LINE CHECK, TWO EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED AFT EXTERIOR EMERGENCY LIGHT ASSEMBLY AND BATTERY PACK CHARGER, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951117000221995111700022NM 1995 11 17 9517786622 119951108A7830 TR LIGHT BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 1 ENGINE ILLUMINATED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01622US 21704 702039 DURING CLIMB, THE NR 1 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. ACFT DUMPED 90,000 LBS OF FUEL AND FLIGHT DIVERTED TO MSP WHERE THE REVERSER WAS LOCKED OUT AND PLACED ON MEL. 2L74 4F4 F A20WE E3NE 19951117000231995111700023WP 1995 11 17 9517799103 119951108A2133 OUT FLOW VALVE DOUG DC9 DC915 3022036WP CABIN OBSTRUCTED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL0193S 47078 DURING CLIMB, CABIN OVERPRESSURIZED AND CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN BOTH AUTO AND MANUAL MODE. DEACTIVATED BOTH PACKS TO DEPRESSURIZE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. FOUND INSULATION BLANKET OBSTRUCTING THE TRAVEL OF THE OUTFLOW VALVE. REMOVED BLANKET AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117000241995111700024NM 1995 11 17 95FDEA01698 119951107A2750 MECHANISM BOEING727 72725 1384006NM TE AFT FLAPS WORN A FDEAAB UNSCHED LANDING EMER. DESCENT E VIBRATION/BUFFET CRCRUISE 1 SO25507FE 18278 FL 31.0, MACH .84 NOTICED 10 TO 12 DEG R/YOKE DISPLACEMENT. ATTEMPTED TO TRIM RUDDER AND GOT A MOD-SEVERE BUFFET, CONTINUED AFTER SLOWING TO .80 MACH. BUFFET STOPPED WHEN EXTENDING SPEED BRAKES SLIGHTLY 1 TO 2 DEGREES. BUFFET WOULD BEGIN AGAIN AFTER RETRACTING SPEEDBRAKE. DECLARED AN EMERGENCY LANDING INTO ICT. VISUALLY INSP/OPS FLT CONT, T/E AFT FLAPS LOOSE. REPLACED CARRIAGE PLATES AND ECCENTRIC BUSHING ON RT I/B AFT FLAP AND ADJ MM 27-51-2. ADJ ECCENTRIC BUSHING ON LT I/B AND RE-ADJ DROOP ON BOTH I/B FLAPS MM 27-51-2. REPLACED 2 CARRIAGE PLATE ASSYS ON RT O/B AFT FLAP ADJ ECCENTRIC BUSHINGS AND RE-ADJ DROOP O/B FLAPS AND INSP AFT FLAP T/E FLAP RIG MM 27-51-12. 2L73 4F A3WE 19951117000251995111700025NM 1995 11 17 95FDEA01699 119951108A5320 FITTINGS BOEING727 72722C 138400FNM BS 740-870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 SEVERAL STRINGER END FITTINGS AT STA 870 TO 740 CRACKED ON INNER LANDING STR 8 RT AND LT MPN'S 69-16380-3 AND 69-34593-1. 2L73 4F A3WE 19951117000261995111700026NM 1995 11 17 95FDEA01700 119951114A532065184175 STIFFENER BOEING727 727223 1384074NM BS 308 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-014), ON HORIZONTAL STIFFENER AT BS 308 WL 170 LBL 13 RBL 13 (P/N 65-18417-5). REMOVED HORIZONTAL STIFFENER AT BS 309 WL 170 LBL RBL 13 AND INSTALLED NEXT STIFFENER. 2L73 4F A3WE 19951117000271995111700027NM 1995 11 17 95FDEA01701 119951108A5320652073215 CHANNEL BOEING727 72722 1384002NM BS 1058 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-1111-01, 3), ON SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5. REMOVED AND REPLACED SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01. 2L73 4F A3WE 19951117000281995111700028NM 1995 11 17 95FDEA01702 119951108A5320 DOORWAY FRAME BOEING727 72722 1384002NM BS 1056 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DOUBLE HOLE IN FRAME STA 1056 FWD SIDE OF CARGO DOORWAY UNDER WEB STR 27R. REPAIRED DOUBLE HOLE IN FRAME AT STA 1056 FWD SIDE OF CARGO DOORWAY UNDER WEB STR 27R AS PER FEDEX SRM 51-40-3 AND 53-10-4. 2L73 4F A3WE 19951117000291995111700029NM 1995 11 17 95FDEA01703 119951108A5320 DOORWAY FRAME BOEING727 72722 1384002NM BS 1110 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DOUBLE HOLE IN FRAME STA 1110, AFT SIDE OF DOORWAY UNDER WEB STR 27R. REPAIRED DOUBLE HOLE IN FRAME AT STA 1110, AFT SIDE OF CARGO DOORWAY UNDER WEB STR 27R AS PER FEDEX SRM 51-40-3 FIG 1. 2L73 4F A3WE 19951117000301995111700030NM 1995 11 17 95FDEA01704 119951108A5311 FRAME BOEING727 72722 1384002NM BS 580 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND 2 DAMAGED FASTENER HOLES ON FRAME, STA 580 STR 22 TO 24 AND 25L, FWD BAY. REPAIRED BY CUTTING OUT DAMAGED AREAS ON 550 BS FRAME ABOVE STR 22, 24, AND 25L, FABRICATED, ALODINED, PRIMED AND INSTALLED THREE REPAIR DOUBLERS PER FEDEX SRM 51-40-3 AND 53-10-2. 2L73 4F A3WE 19951117000311995111700031NM 1995 11 17 95UAL900253 119951109A3350 BATTERY PACK BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP294728U 19925 EMERGENCY EXIT LIGHTS STAY ON E-ZONE AT DOOR 5 CROSS AISLE. REPLACED EEL BATTERY PACK. 2L74 4F4 F A20WE E20EA 19951117000321995111700032NM 1995 11 17 95UAL900254 119951109A5320 RIVET BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT WINDOW POST SHEARED A UALAK NONE C F.O.D. NRNOT REPORTED 1 WP297251U 21398 RETURNED TO ORD DUE TO BIRD STRIKE. ACCOMPLISHED BIRD STRIKE INSPECTION. ALL THREE ENGINE INLETS CHECKED AND NO DAMAGE FOUND. REPLACED SHEARED RIVET AT CO-PILOT'S WINDOW POST. 2L73 4F4 F A3WE E2EA 19951117000331995111700033NM 1995 11 17 95UAL900255 119951109A3350 BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297293U 21571 EMERGENCY LIGHT IN AISLE BETWEEN 16C AND 16D IS INOPERATIVE. REPLACED BATTERY AT M1094. 2L73 4F4 F A3WE E2EA 19951117000341995111700034WP 1995 11 17 ABXA9500931 119951107A56105912290501 WINDSHIELD DOUG DC9 DC932 3022066WP LT COCKPIT BROKEN A ABXAA UNSCHED LANDING O OTHER CLCLIMB 1 GL23901AX 47381 OUTER PANE OF CAPTAIN'S WINDSHIELD SHATTERED AT FL 330, DURING CLIMB TO FL350. CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT FURTHER INCIDENT. REPLACED WINDSHIELD IAW DC-9 MM 56-10-2. 2L72 4F A6WE 19951117000351995111700035WP 1995 11 17 ABXA9500932 119951109A3350305 EEL LAMP DOUG DC8 DC861 3021952WP CABIN FAILED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23848AX 46032 DURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTING INOP. RELAMPED POSITIONS AND EMERGENCY LIGHTING OPS CHECKED GOOD IAW ABX WORK CARD DC-8-1 ITEM NR 8. 2L74 4F 4A25 19951117000361995111700036SW 1995 11 17 COMA9520397 119951106A3260 DOOR LIGHT SWRNGNSA227 SA227AC 8780603SW LT MLG ILLUMINATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01703CA AC703 AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR DOOR OPEN INDICATOR REMAINED ON. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE. CLEANED GEAR DOOR MICROSWITCHES AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951117000371995111700037 1995 11 17 COMA9531189 419951107A3418861CAR AOA VANE SAAB SF340 SF340A 7850100EU LEFT DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO01358CA1959814852 340A047 THE LEFT ALPHA LIGHT ILLUMINATED DURING FLIGHT. REPLACED THE LEFT AOA VANE. 2L72 4T RTA52EU 19951117000381995111700038EA 1995 11 17 COMA9560593 119951108A5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA RT COCKPIT CRACKED A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01924CA 7026 THE COPILOTS WINDSHIELD CRACKED DURING DE-ICING OPERATIONS, WINDSHIELD ANTI-ICE WAS ON. 2L72 4F RTA21EA 19951117000391995111700039EA 1995 11 17 COMA9560594 119951108A5240 DOOR CNDAIRCL600 CL6002B19 EA OXYGEN SERVICE OPEN A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01938CA 7046 THE PILOTS AIRSPEED INDICATOR BECAME ERRATIC AND LOUD WHINE FROM RT SIDE OF NOSE. ALSO, STALL FAIL MESSAGE ON EICAS AND PILOTS AIRSPEED ERRATIC. MAINTENANCE FOUND OXYGEN SERVICE DOOR OPEN, DOOR IN OPEN POSITION OBSTRUCTS AIR FLOW AT PITOT HEAD, SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951117000401995111700040EU 1995 11 17 DL31L954279 119951108A7110221405057 NOSE COWL AIRBUS310 A310324 3930206EU NR 1 ENGINE DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11837AB 674 DURING INSPECTION, NR 1 ENGINE INLET COWL L/E LIP WAS FOUND DENTED BEYOND LIMITS, AT THE 11 O'CLOCK POSITION. REPAIRED PER SRM 54-10-00. 2L72 4F RTA35EU 19951117000411995111700041NM 1995 11 17 DL72E954266 119951011A5320 DOUBLER BOEING727 727247 138408FNM BS 938 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 THE LT MAIN LANDING GEAR WHEEL WELL PRESSURE DECK WAS FOUND WITH A PREVIOUS MODIFICATION DOUBLER INSTALLED FOR A CRACK AT LBL 55 AND STA 938. THE PREVIOUS DOUBLER WILL BE REMOVED AND A NEW DOUBLER INSTALLED PER REVISION 4 OF THE SERVICE BULLETIN E0 4.61537-3AD, S/B 727-53-0149. THE NEW DOUBLER WILL BE EXTENDED TO PICK UP ANY FASTENER LOCATIONS INSTALLED BY THE ORIGINAL REPAIR. ACCOMPLISHED REPAIRS PER DL ERA 302615-14AD. 2L73 4F A3WE 19951117000421995111700042 1995 11 17 DL72E954307 419951108A3442 ANTENNA 10608972 BOEING727 727247 138408FNM RADAR FAILED A DALAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO112823W 344201919 21328 WX RADAR SPOKES AND DISPLAYS TEST PATTERN WHILE IN NORM AND CONTOUR. REPLACED RADAR ANTENNA AND WAVE GUIDE, OPERATION NORMAL. 2L73 4F A3WE 19951117000431995111700043NM 1995 11 17 DL72K954262 119950822A53306554566 SKIN BOEING727 727232 1384082NM BS 540 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11466DA 20743 AT CV2 IN TPA, THE FUSELAGE SKIN AT STA 540 BETWEEN S-26R AND S-27R, JUST BELOW THE LAP SPLICE HAS BEEN TRIMMED TO REMOVE CORROSION. THE CUT OUT MEASURES 5 INCH BY 11 INCH. THIS ER/A REPAIRS THE AREA BY ADDING A .090 2024-T3 CLAD FILLER, .050 2024-T3 CLAD DOUBLER AND A .063 2024-T3 CLAD TRIPLER. ACCOMPLISHED REPAIRS PER DL ERA 302359-14. 2L73 4F A3WE 19951117000441995111700044NM 1995 11 17 DL72K954264 119951102A5320 SIDE WALL BOEING727 727232 1384082NM BS 277 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 DURING LETTER CHECK AT TPA, TWO .25 CRACKS WERE DISCOVERED IN THE .040 2024-T3 CLAD RIGHT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL APPROX STA 277.0. THIS ER/A PROVIDES REPAIR OF CRACK DAMAGE AND INSTALLATION OF A MOD STRAP AT DAMAGE LOCATION, AD 90-06-09 PER DL ERA 302710-14AD. 2L73 4F A3WE 19951117000451995111700045NM 1995 11 17 DL72K954265 119951102A5330 SKIN BOEING727 727232 1384082NM BS 294-312 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 AT LETTER CHECK IN TPA, CORROSION WAS DISCOVERED ON THE UPPER SKIN AT THE S-24R LAP JOINT THAT WARRANTED A 12.5 INCH BY 3 INCH CUT OUT, BETWEEN STA 294.5 AND STA 312 BY MTC. THIS ER/A WILL REPAIR THE DAMAGED AREA PER SRM 53-30-3 FIG 14 DETAIL 4 WITH THE VARIATION OF BLIND FASTENERS, PER DL ERA 302714-14. 2L73 4F A3WE 19951117000461995111700046NM 1995 11 17 DL72K954283 119951108A2782 ACTUATOR 269002914 BOEING727 727232 1384082NM NR 7 LE SLAT FAILED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11414DA 21256 LOST A-SYST HYD, ON CLIMBOUT. PERFORMED ABNORMAL PROCEED CK LIST, ELECT EXT FLAPS, MANUALLY EXT GEAR, FOUND NR 7 L/E SLAT ACTUATOR CASE SPLIT. REPLACED ACTUATOR, OPERATION NORMAL. 2L73 4F A3WE 19951117000471995111700047NM 1995 11 17 DL72L954246 119951106A335081 BULB BOEING727 727232 1384082NM LT OVERWING FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11508DA 21310 ON LAYOVER, LEFT AFT OVERWING EMERGENCY LIGHT INOP. RELAMPED AND CKS NORMAL. 2L73 4F A3WE 19951117000481995111700048NM 1995 11 17 DL72L954305 119951108A3350 BATTERY PACK 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11508DA 7309 21310 FOUND LT CENTER OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2L73 4F A3WE 19951117000491995111700049NM 1995 11 17 DL72L954319 119951029A3350 EEL CHARGER BOEING727 727232 1384082NM CABIN MALFUNCTIONED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11505DA 21307 ON PREFLIGHT, EMERGENCY EXIT LIGHTING BATTERY CHARGER POPS CIRCUIT BREAKER. T/S SYS REPLACED BATT CHARGER C/B AND SPLICE SM17 WDM 33-51-02 PG 5, OPERATION NORMAL. 2L73 4F A3WE 19951117000501995111700050NM 1995 11 17 DL72S954252 119951106A3233731414 ACTUATOR BOEING727 727232 1384082NM LT MLG DOOR CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11400DA 21144 A-SYS HYD FAILURE AFTER GEAR SELECTED UP. A-SYS QTY WAS FLUX AT THE ZERO MARK. FOUND LT MLG DOOR ACTUATOR CRACKED. REPLACED SAME, OPERATION NORMAL. 2L73 4F A3WE 19951117000511995111700051NM 1995 11 17 DL72S954255 119951106A3350 BATTERY RPS1B BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11489DA 0368 21019 CENTER SECTION OF FLOOR EMERGENCY EXIT LIGHTS INOP. REPLACED RACK M9026 AND BATTERIES, ALL CKS NORMAL. 2L73 4F A3WE 19951117000521995111700052NM 1995 11 17 DL72S954257 119951106A3350 BATTERY 90052 BOEING727 727232 1384082NM FWD BULLNOSE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11489DA 21019 FWD BULLNOSE EMERGENCY LIGHT INOP. REPLACED RACK M1088 AND BATTERIES, ALL CKS NORMAL. 2L73 4F A3WE 19951117000531995111700053NM 1995 11 17 DL72S954258 119951106A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11489DA 21019 FWD OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS NORMAL. 2L73 4F A3WE 19951117000541995111700054NM 1995 11 17 DL72S954259 119951106A5754 ANGLE BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING F-1 LETTER CHECK, FOUND .375 INCH CRACK AND 1 INCH CRACK, NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951117000551995111700055NM 1995 11 17 DL72S954267 119950214A5743651927015 FLAP TRACK BOEING727 727232 1384082NM INBD TE FLAP CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11543DA 22392 THE LEFT SIDE INBOARD TRACK FOR THE INBOARD FLAP WAS FOUND WITH CORROSION IN THE RADIUS BLOCK FASTENER HOLE, FORWARD OF THE AFT TRACK TO MAIN LANDING GEAR BEAM ATTACH HOLE, ON BOTH THE INBOARD AND OUTBOARD SIDES OF THE TRACK. THE HOLES WERE BOTH OVERSIZED TO .560 DIAMETER TO REMOVE CORROSION AND ALLOW FOR REPAIR BUSHING INSTALLATION. A STEEL REPAIR BUSHING WILL BE INSTALLED, PER DL ERA 301187-14AD. 2L73 4F A3WE 19951117000561995111700056NM 1995 11 17 DL72S954268 119951029A5330651842012 SKIN BOEING727 727232 1384082NM BS 259.5-312 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11484DA 20864 CORROSION AT AN EXISTING EXTERNAL REPAIR DOUBLER ON THE LOWER FUSELAGE SKIN PANEL, BETWEEN BS 259.5 AND BS312, AT STRINGER 20R. REMOVAL OF THE DOUBLER REVEALED EXTENSIVE CORROSION DAMAGE. THE SKIN WAS TRIMMED TO REMOVE CORROSION DAMAGE BELOW THE FORWARD LAVATORY SERVICE DOOR. A NEW EXTERNAL REPAIR DOUBLER WILL BE INSTALLED PER DL ERA 302687-14. 2L73 4F A3WE 19951117000571995111700057NM 1995 11 17 DL72S954273 119951107A3350 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11419DA 21272 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL. 2L73 4F A3WE 19951117000581995111700058NM 1995 11 17 DL72S954282 119951108A524065569923 SKIN BOEING727 727232 1384082NM SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11520DA 21471 DURING SHOP INSP, A CRACK WAS FOUND AT THE LOWER HINGE CUTOUT. THE CRACK WAS ROUTED OUT AND A STEEL DOUBLER WAS INSTALLED AS PER SRM 52-40-2 FIG 4, FOR LT AFT SERVICE DOOR. 2L73 4F A3WE 19951117000591995111700059NM 1995 11 17 DL72S954285 119951024A2750 BRACKET BOEING727 727232 1384082NM NR 2 FLAP ACT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 FLAP ACTUATOR SUPPORT BRACKET CRACKED AT UPPER AND LOWER CORNERS OF I/B SIDE. REMOVED FLAP ACTUATOR, REMOVED SUPPORT BRACKET AND INSTALLED DOUBLER PER M/M 57-20-1 PG 811. REINSTALLED ACTUATOR. 2L73 4F A3WE 19951117000601995111700060NM 1995 11 17 DL72S954286 119951024A2750 BRACKET BOEING727 727232 1384082NM NR 2 FLAP ACT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 FLAP ACTUATOR SUPPORT BRACKET CRACKED AT UPPER O/B CORNER. REMOVED SUPPORT BRACKET AND INSTALLED DOUBLER PER M/M 57-20-1. REINSTALLED SUPPORT BRACKET. 2L73 4F A3WE 19951117000611995111700061NM 1995 11 17 DL72S954287 119951024A5260 WEB BOEING727 727232 1384082NM VENTRAL STAIRS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND STATION 1240, LEFT SIDE LOWER WEB IN VENTRAL STAIRS HAS TEMPORARY REPAIRS. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER M/M 53-11-0 PG 832 AND ID TAGGED PER PS 900-5-1. 2L73 4F A3WE 19951117000621995111700062NM 1995 11 17 DL72S954288 119951024A5260 WEB BOEING727 727232 1384082NM VENTRAL STAIRS DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND STATION 1240 RIGHT SIDE LOWER WEB IN VENTRAL STAIRS HAS TEMPORARY REPAIRS. REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PER M/M 53-11-0 PG 832 AND ID TAGGED PER PS 900-5-1. 2L73 4F A3WE 19951117000631995111700063NM 1995 11 17 DL72S954289 119951025A5311 FRAME BOEING727 727232 1384082NM BS 930 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND STATION 930 FRAME ABOVE PREVIOUS REPAIR CRACKED BETWEEN BOTTOM OF WINDOW AND STRINGER 14L. REPAIR DOUBLER WAS MADE AND INSTALLED PER M/M 53-10-4 FIG 25. 2L73 4F A3WE 19951117000641995111700064NM 1995 11 17 DL72S954290 119951025A5754 RIB BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 3 SLAT, NR 12 RIB WAS CRACKED. FABRICATED REPAIR DOUBLER AND INSTALLED PER 57-54-0. 2L73 4F A3WE 19951117000651995111700065NM 1995 11 17 DL72S954291 119951024A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 FLAT, RIB NR 18 CRACKED AT UPPER SKIN AREA. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER M/M 57-54-00 FIG 809. INSTALLED DOUBLER. 2L73 4F A3WE 19951117000661995111700066NM 1995 11 17 DL72S954292 119951025A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 SLAT, RIB NR 8 IS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 819. 2L73 4F A3WE 19951117000671995111700067NM 1995 11 17 DL72S954293 119951025A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 SLAT, RIB NR 7 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-0 PG 818. 2L73 4F A3WE 19951117000681995111700068NM 1995 11 17 DL72S954294 119951025A5754 RIB BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 2 SLAT, RIB NR 6 WAS CRACKED. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER M/M 57-54-1 PG 818. 2L73 4F A3WE 19951117000691995111700069NM 1995 11 17 DL72S954295 119951025A5754 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 4 SLAT, NR 2 RIB WAS CRACKED. FABRICATED REPAIR AND INSTALLED PER M/M 57-54-0 PG 818. 2L73 4F A3WE 19951117000701995111700070NM 1995 11 17 DL72S954296 119951025A5754 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 4 SLAT, NR 3 RIB WAS CRACKED. MANUFACTURED AND INSTALLED REPAIR PER M/M 57-54-0 PG 818. 2L73 4F A3WE 19951117000711995111700071NM 1995 11 17 DL72S954297 119951025A5754 RIB BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 5 SLAT, NR 1 RIB WAS CRACKED. REPAIRED CRACKED RIB PER M/M 57-54-0. 2L73 4F A3WE 19951117000721995111700072NM 1995 11 17 DL72S954298 119951025A5754 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 6 SLAT, NR 12 RIB WAS CRACKED. STOP DRILLED NR 12 RIB AND REPAIRED CRACK PER M/M 57-54-0 FIG 814. 2L73 4F A3WE 19951117000731995111700073NM 1995 11 17 DL72S954299 119951025A5754 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 6 SLAT, NR 7 RIB WAS CRACKED. STOP DRILLED CRACK AND REPAIRED RIB PER M/M 57-54-0 FIG 814. 2L73 4F A3WE 19951117000741995111700074NM 1995 11 17 DL72S954300 119951025A5754 RIB BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 DURING HMV, FOUND NR 7 SLAT, NR 8 RIB CRACKED AND NR 10 RIB MISSING FASTENER AND ONE IS LOOSE. REPAIRED NR 8 PER M/M 57-54-0 PGS 818 AND 819. REPLACED LOOSE AND MISSING FASTENER ON NR 10 RIB. 2L73 4F A3WE 19951117000751995111700075NM 1995 11 17 DL72S954301 119951108A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11484DA 20864 CENTER AISLE OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, CKS NORMAL. 2L73 4F A3WE 19951117000761995111700076NM 1995 11 17 DL72W954245 119951102A5713 STRINGER BOEING727 727247 138408FNM WS 686.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 ATL - HMV, HFEC INSP OF WS 686.50 STR 9 HAS A CRACK EXITING FASTENER HOLE AWAY FROM RADIUS. REPAIRED PER MM 57-13-0. 2L73 4F A3WE 19951117000771995111700077NM 1995 11 17 DL72W954261 119951026A5320 VERTICAL BEAM BOEING727 727247 138408FNM BS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 ATL - HMV, A CRACK WAS FOUND ON THE VERTICAL BEAM ON THE OUTBOARD SIDE STATION 1183 RBL 8 AND AN EXISTING REPAIR FOR SIMILAR DAMAGE FOR LBL 8. ALSO, ON THE VERTICAL BEAM ON THE OUTBOARD SIDE STATION 1183, THAT WAS NOT INSTALLED PER EO 4-59275-3AD FIG 3. THIS ER/A WILL REMOVE THE EXISTING REPAIR AND REPAIR THE DAMAGE PER THIS EO FOR AD 90-06-09, PER DL ERA 302677-14AD. 2L73 4F A3WE 19951117000781995111700078NM 1995 11 17 DL72W954263 119951030A53306554583188119 SKIN BOEING727 727247 138408FNM BS 1010-1030 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 AT CV2 IN TPA, CORROSION WAS DISCOVERED ON THE FUSELAGE SKIN BETWEEN STA 1010 AND 1030 STR 23R AND 24R. A SECTION OF THE BONDED DOUBLER AT STR 24R AND TWO AREAS OF THE FUSELAGE SKIN, 4 INCH BY 1.25 INCH AND 2.75 INCH BY 2.5 INCH WERE CUT OUT TO REMOVE CORROSION. ALSO, STR 23R WAS CUT AT APPROX STA 1040 AND REMOVED UP TO STA 1010. A FILLER AND DOUBLER WAS INSTALLED, ACCOMPLISHED REPAIRS PER DL ERA 302689-14. 2L73 4F A3WE 19951117000791995111700079NM 1995 11 17 DL72W954269 119951030A533065545901 SKIN BOEING727 727247 138408FNM FS 720 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO112807W 20579 ADDITIONAL CORROSION WAS CUT OUT JUST AFT OF FS 720A. THE NEW CUT OUT AND THE PREVIOUS CUT OUT ARE SEPARATED BY APPROXIMATELY 5.5 INCHES. THE ORIGINAL DOUBLER WAS REMOVED AND A NEW DOUBLER FOR BOTH CUT OUTS WAS INSTALLED. THE DOUBLER DOES AND WILL CONTINUE TO BUTT UP AGAINST THE SPLICE DOUBLER INSTALLED AT FS 720 PER ER/A 210265-14. 2L73 4F A3WE 19951117000801995111700080NM 1995 11 17 DL72W954275 119951031A5754 RIB BOEING727 727247 138408FNM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING HMV, FOUND NR 8 SLAT, NR 3 L/E REINFORCING RIB CRACKED. REMOVED O/B TRACK FOR ACCESS AND REPAIRED RIB PER M/M 57-54-0 PG 806 AND 807. 2L73 4F A3WE 19951117000811995111700081NM 1995 11 17 DL72W954277 119951019A5400 DUCT HOUSING BOEING727 727247 138408FNM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING HMV, FOUND TEMP REPAIR ON RT SIDE OF NR 2 ENGINE INLET DUCT HOUSING. REPAIRED PER SRM 54-10-3 FIG 4. 2L73 4F A3WE 19951117000821995111700082NM 1995 11 17 DL72W954303 119951020A5713 STRINGER BOEING727 727247 138408FNM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 FOUND AT HMV REF OPN 8502AD LT WING STRINGER TO RIB HFEC INSP, SHOWS FWD TAB OF FWD VENT BOX, STRINGER S-14 CRACKED AT STRINGER TO RIB ATTACH POINT AT WS 629. REPAIRED VENT BOX STRINGER PER MM 57-13-0. 2L73 4F A3WE 19951117000831995111700083NE 1995 11 17 DL72W954316 219951107A7250 BLADE BOEING727 7272Q8 138407WNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE FAILED A DALAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TOTAKEOFF 1 SO11831L 21826 700235 ON TAKEOFF, NR 3 ENGINE FLAMED-OUT, RETURNED PVR. INITIAL INSPECTION FOUND NR 3 TURNBINE BLADES DISINTEGRATED. REPLACED NR 3 ENGINE FOR RETURN TO SERVICE. 2L73 4F4 F A3WE E2EA 19951117000841995111700084NM 1995 11 17 DL73S954260 119951106A3350OL3071BPEGPL BULB BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11311DL 23083 EMERGENCY FLOOR TRACK LIGHT INOP AT SEAT 23D. REPLACED LAMP, CKS NORMAL. 2L72 4F RTA16WE 19951117000851995111700085NE 1995 11 17 DL757954270 219951107A7230 COMPRESSOR BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO11629DL 22919 716434 DURING CLIMBOUT THROUGH 27,000 FEET, RT ENGINE HAD A SERIES OF RAPID COMPRESSOR STALLS WITH MASSIVE N1/EPR FLUX. REPLACED ENGINE AND ROUTED TO SHOP. 2L72 4F4 FRTA2NM E17NE 19951117000861995111700086NM 1995 11 17 DL757954276 119950919A5350141N782013 RADOME BOEING757 757232 1384965NM FWD FUSELAGE IMPLODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11667DN 25035 RADOME IMPLODED IN NOSE AREA. INSPECTION OF RADOME WAS ACCOMPLISHED, NO CAUSE FOR DAMAGE WAS FOUND. REBUILDED RADOME COMPLETE PER SRM 53-10-72. 2L72 4F RTA2NM 19951117000871995111700087NM 1995 11 17 DL757954278 119951108A5754 TE WEDGE 114N300251 BOEING757 757232 1384965NM NR 5 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11615DL 22822 DURING SHOP INSPECTION, NR 5 L/E SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED T/E WEDGE PER SRM. 2L72 4F RTA2NM 19951117000881995111700088NM 1995 11 17 DL757954281 119951108A335008163069401 EEL TRACK BOEING757 757232 1384965NM CABIN DAMAGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11623DL 22913 ON LAYOVER, F/C EMERGENCY FLOOR TRACK DAMAGED. C/A REPLACED FIRST SECTION ON FIRST CLASS FLOOR TRACK, CKS OK. 2L72 4F RTA2NM 19951117000891995111700089NM 1995 11 17 DL76S954306 119951108A3350 BULB BOEING767 767332 1382001NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11119DL 23278 DURING L/O, FOUND AFT RT DOOR EMERGENCY LIGHT INOP AND LT WING SLIDE LIGHT INOP. RELAMPED BOTH, CKS GOOD. 2L72 4F RTA1NM 19951117000901995111700090WP 1995 11 17 DLL10954256 119951106A2913 PUMP 3508807 LKHEED1011 10113851 5265010WP C-HYD SYST LEAKING A DALAO OTHER K FLUID LOSS APAPPROACH 1 SO11728DA MX306549 193C1173 DURING GEAR EXT ON APPROACH, C-SYS HYD QTY LO QTY LIGHT ON AND C-SYS PRESSURE DROPPED TO ZERO. HOWEVER, GEAR HAD FULLY EXTENDED, 3 GREEN QTY IN C-SYS DROPPED TO AND REMAINED AT .125 FULL. FOUND C-SYS ATM HYD PUMP LEAKING AT SPLIT LINE. REMOVED PUMP AND REPLACED SAME. 2L73 4F A23WE 19951117000911995111700091WP 1995 11 17 DLL10954271 119951107A2150 CONTROL VALVE FS21415 LKHEED1011 10113851 5265010WP NR 2 PAC FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11725DA 193C1162 LAX - ON CLIMBOUT, REPORT SMOKE OILY/CHEM SMELL AFT CABIN. VENTED A/C PER POM, NR 2 PACK HOT AIR MAN SHOWED 145, NO LIGHT. CA CREW VERBAL NR 2 PACK OFF, NO MORE SMOKE. FWD NR 2 PACK TO MCO AND PLAC PER 21-51-07A, PACK VALVE LOCKED CLOSED. REPLACED TRIM VALVE SEAL UNLOCKED PACK FLOW CONTROL VALVE, OPERATION NORMAL. 2L73 4F A23WE 19951117000921995111700092WP 1995 11 17 DLL10954309 119951024A5312 BULKHEAD LKHEED1011 10113851 5265010WP BS 1363 OVERSIZED HOLE A DALAK NONE O OTHER ININSP/MAINT 1 SO11735D 193C1226 DURING ACCOMPLISHMENT OF THE FS 1363 BULKHEAD REPAIR PER SI 7-69959-12, TWO FASTENER HOLES WERE OVERSIZED DUE TO FASTENER REMOVAL. THE SUBJECT FASTENERS ARE LOCATED 2 ROWS BELOW S-23. THE FWD HOLE IS .328 MAX DIAMETER AND THE AFT HOLE IS .4364 MAX DIAMETER. REPAIR APPROVAL PER DL ERA 272198-14AD. 2L73 4F A23WE 19951117000931995111700093WP 1995 11 17 DLL13954274 119951107A33502233 BULB LKHEED1011 10113851 5265010WP L3 DOOR BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11785DL 193A1121 ON LAYOVER, FOUND EXTERIOR LIGHT ON L-3 DOOR EMERGENCY LIGHTING SYSTEM INOP. RELAMPED LIGHT, OPERATION NORMAL. 2L73 4F A23WE 19951117000941995111700094WP 1995 11 17 DLL16954310 119951030A57301605416 SKIN LKHEED1011 10113853 5265020WP WS 425-451 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 WHILE ACCOMPLISHING OPN104 OF EO 7-57989-3, FASTENER HOLES 1 A AND B THROUGH 8 A AND B, 16 HOLES IN BAY 12 WERE FOUND TO HAVE OVERSIZED FASTENERS. ALREADY INSTALLED THROUGH THE REAR SPAR LOWER CAP AND LOWER WING SKIN. REPAIR APPROVAL PER DL ERA 272150-14. 2L73 4F A23WE 19951117000951995111700095WP 1995 11 17 DLL16954311 119951030A53121505312101 BLKHD FRAME LKHEED1011 10113853 5265020WP AFT P-DOME CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 THE AFT P-DOME FRAME SEGMENTS BETWEEN S-22 AND S-44 WERE FOUND WITH CRACKS IN THE LOWER FLANGE RADIUS. THE FRAME SEGMENTS ARE MADE FROM .050 THICK 7178-T6 AL SHEET. ALSO, THE FRAME WEB BETWEEN S-44 AND S-33 WAS FOUND BADLY CORRODED. THE WEB IS FABRICATED FROM .090 7075-T6, ACCOMPLISHED REPAIRS PER DL ERA 272168-14. 2L73 4F A23WE 19951117000961995111700096WP 1995 11 17 DLL16954312 119951013A53301618861101 SKIN LKHEED1011 10113853 5265020WP BS 1625 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 DURING CORROSION REMOVAL, AN AREA OF SKIN AND TWO LAYERS OF BONDED SKIN WERE TRIMMED OUT IN A 9.5 INCH BY 8.75 INCH CUT OUT AT STA 1625 STRINGER 30. ALSO, THE AFT EDGE OF THE DOOR TRIPLER WAS NOTCHED APPROXIMATELY 6 INCHES IN LENGTH AND .75 INCH INTO THE STRAP. THE SKIN IS A BONDED ASSEMBLY OF .075 2024-T3 DOUBLE AND .020 2024-T3 TRIPLER. ACCOMPLISHED REPAIRS PER DL ERA 272040-14. 2L73 4F A23WE 19951117000971995111700097WP 1995 11 17 DLL16954313 119951102A52301582145102 LATCH FITTINGS LKHEED1011 10113853 5265020WP C-1A CARGO DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 DURING THE ACCOMPLISHMENT OF SI 7-58181-12AD, THE NR 1, 2, 3 AND 8 C-1A CARGO DOOR LATCH FITTINGS WERE FOUND WITH SURFACE CORROSION IN THE UPPER WELL. ALSO, DRAIN HOLES IN THE CENTER OF THE LOWER WEB WERE ADDED FOR ALL 8 OF THE SUBJECT FITTINGS. THE SURFACE CORROSION WILL BE BLENDED OUT ON FITTINGS NR 1, 2, 3 AND 8. FITTINGS NR 4, 5, 6, 7 WILL HAVE DRAIN HOLES MACHINED. THE SUBJECT FITTINGS ARE MACHINED FROM 4330M STEEL HEAT TREATED TO THE 220-240 KSI CONDITION. REPAIR APPROVAL PER DL ERA 272151-14AD. 2L73 4F A23WE 19951117000981995111700098WP 1995 11 17 DLL16954314 119951102A5711 REAR SPAR LKHEED1011 10113853 5265020WP WS 293-346 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11762DA 193Y1210 DURING THE ACCOMPLISHMENT OF EO 7-59089-3 FOR THE RIGHT WING, CRACKS WERE FOUND EMANATING FROM EXISTING FASTENERS HOLES BETWEEN IWS 293.58 AND IWS 346.109. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP AT LOCATION 12A AND IN THE REAR SPAR WEB AT LOCATION 16B. THE SUBJECT FASTENER HOLES WERE OVERSIZED TO REMOVE CRACKS IN THE DAMAGED MEMBERS ONLY. ACCOMPLISHED REPAIRS PER DL ERA 272179-14AD. 2L73 4F A23WE 19951117000991995111700099NM 1995 11 17 DLM11954251 119951106A2120ABO467286 FILTER DOUG MD11 MD11 3023602NM CABIN DIRTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11803DE 48474 DURING CRUISE HAS STRONG ELECTRICAL BURNING SMELL THROUGHOUT CABIN. DEACTIVATED RECIRC FAN, SMELL DISSIPATED. FOUND NR 1 RECIRC FAN MOTOR HOT TO TOUCH AND ADJACENT RECIRC FILTER VERY DIRTY. REPLACED FILTER, FAN OPERATION NORMAL. 2L73 4F RTA22WE 19951117001001995111700100NM 1995 11 17 DLM88954284 119951108A2910AS153080254 HOSE DOUG MD88 MD88 3023688NM RT HYD SYST BROKEN A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11918DL 49583 AFTER TAKEOFF ON CLIMBOUT, RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO 0 QUANTITY 3 QTS. FOUND FLEX LINE 153-08-0254, FROM FILTER MODULE BROKEN. REPLACED LINE, OPERATION NORMAL. 2L72 4F RTA6WE 19951117001011995111700101NM 1995 11 17 DLM88954320 119951104A2560 LANYARD DOUG MD88 MD88 3023688NM L2 DOOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11917DL 49573 ON PREFLIGHT, L-2 DOOR SLIDE LANYARD WIRE FOUND BROKEN. REPLACED LANYARD. 2L72 4F RTA6WE 19951117001021995111700102NM 1995 11 17 SCNA95260 119951107A33506104781 BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE AFT OVERWING LOWER EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR FAULTY EXIT SIGNS AND SYSTEM TESTED GOOD PER 33-50-01. 2L73 4F A3WE 19951117001031995111700103NM 1995 11 17 SWAA950704 119951108A2913887477 PUMP BOEING737 7373H4 1384600NM W/W OVERHEATED A SWAAD RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SW07318SW6686 6102 23339 DURING CLIMBOUT, EXPERIENCED A-SYSTEM HYDRAULIC PUMP OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED PUMP, FILTERS AND FLUSHED SYSTEM PER BOEING M/M. 2L72 4F RTA16WE 19951117001041995111700104NM 1995 11 17 SWAA950705 119951107A5315 FLOORBEAM BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07312SW 23334 DURING SCHEDULED C1 CHECK, FOUND FLOORBEAM STRAPS CRACKED AT RBL 32 AND AT LBL 12 BS 312 IN E AND E COMPARTMENT. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951117001051995111700105SO 1995 11 17 SWIA95669 119951105A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT WING RIB 20 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SURFACE. REMOVED AND REPLACED THREE WING SUPPORT CLIPS ON UPPER SURFACE OF RIB 20 ON RT WING, IAW EMB SRM 51-30-00 AND EMB SB 120-57-0031 PART 1. 2L72 4T4 TRTA31SO E20NE 19951117001061995111700106SO 1995 11 17 SWIA95670 119951105A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT WING RIB 16 HAS TWO CRACKED WING SUPPORT CLIPS ON UPPER SURFACE AND CRACKED WING SUPPORT CLIPS ON LOWER SURFACE. REMOVED AND REPLACED FIVE WING SUPPORT CLIPS, TWO ON UPPER SURFACE AND THREE ON LOWER SURFACE, RIB 16 RT WING IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1. 2L72 4T4 TRTA31SO E20NE 19951117001071995111700107SO 1995 11 17 SWIA95671 119951105A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT WING RIB 15 HAS THREE CRACKED WING SUPPORT CLIPS ON UPPER SURFACE AND FOUR CRACKED WING SUPPORT CLIPS ON LOWER SURFACE. REMOVED AND REPLACED SEVEN WING SUPPORT CLIPS, THREE ON UPPER AND FOUR ON LOWER SURFACE ON RIB 15 RT WING, IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1. 2L72 4T4 TRTA31SO E20NE 19951117001081995111700108SO 1995 11 17 SWIA95672 119951105A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT WING RIB 22 HAS THREE CRACKED CLIPS ON UPPER SURFACE. REMOVED AND REPLACED THREE WING SUPPORT CLIPS ON UPPER SURFACE RIB 22 OF RT WING IAW EMB SRM 51-30-00 AND 51-40-00 AND EMB SB 120-57-0031 PART 1. 2L72 4T4 TRTA31SO E20NE 19951117001091995111700109SO 1995 11 17 SWIA95673 119951105A5720 CLIPS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT WING CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07187SW 120037 RT WING RIB 21 HAS FOUR CRACKED SUPPORT CLIPS ON UPPER SURFACE. REMOVED AND REPLACED FOUR WING SUPPORT CLIPS ON UPPER SURFACE OF RIB 21 ON RT WING, IAW EMB SRM 51-30-00, 51-40-00 AND EMB SB 120-57-0031 PART 1. 2L72 4T4 TRTA31SO E20NE 19951117001101995111700110NM 1995 11 17 UPS204948 119951107A335037067001 BATTERY BOEING727 72725C 138400HNM COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED N1-CAD BATTERIES, OPS CHECK GOOD. 2L73 4F A3WE 19951117001111995111700111NM 1995 11 17 UPS204949 119951107A5720 WING TIP BOEING727 72725C 138400HNM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01915UP 19533 WHILE ON GROUND, MAINTENANCE FOUND RT WING TIP LWR SURFACE HAS TWO, 6 INCH CRACKS. C/W TEMPORARY REPAIR OF RT WING TIP LOWER SURFACE PER EO B727-5730-7604-A. 2L73 4F A3WE 19951117001121995111700112WP 1995 11 17 UPS804941 119951109A575556551672 SKIN DOUG DC8 DC871F 302199DWP NR 3 SPOILER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 3 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER MM 27-61-01. 2L74 4F RT4A25 19951117001131995111700113WP 1995 11 17 UPS804942 119951109A5414 SKIN DOUG DC8 DC871F 302199DWP NR 2 PYLON TE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 PYLON TRAILING EDGE SKIN CRACKED 1 INCH LONG ABOVE FWD DRAIN TUBE RT SIDE. REPAIRED PER UPS EO DC8-5420-4308-A. 2L74 4F RT4A25 19951117001141995111700114WP 1995 11 17 UPS804943 119951109A53135750198 LONGERON DOUG DC8 DC871F 302199DWP FS 857-920 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LONGERON 24L HAS 2 CRACKS AT FS 857 AND AT FS 902 TO 920. REPAIRED LONGERON PER SRM 53-2-2 FIG 5. 2L74 4F RT4A25 19951117001151995111700115WP 1995 11 17 UPS804944 119951109A5530565192744 ANGLE DOUG DC8 DC871F 302199DWP VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS 1 INCH LONG CRACK. REPAIRED PER UPS EO DC8-5310-7585-A. 2L74 4F RT4A25 19951117001161995111700116WP 1995 11 17 UPS804945 119951101A3350 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS IN DISARM AND OFF DISARM, CHECK POSITION LIGHT WAS OFF, IT SHOULD BE ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY AND LIGHT DIMING RELAY RS-60. 2L74 4F RT4A25 19951117001171995111700117WP 1995 11 17 UPS804951 119951109A532036410042N FITTING DOUG DC8 DC871F 302199DWP FS 879 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING ABOVE LONG 24R HEAVY CORROSION AT FS 879. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117001181995111700118WP 1995 11 17 UPS804952 119951109A53203755842509N FITTING DOUG DC8 DC871F 302199DWP FS 1200 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING LONGERON 29L FS 1200. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117001191995111700119WP 1995 11 17 UPS804953 119951109A53203755843502N FITTING DOUG DC8 DC871F 302199DWP FS 1160 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1160, LONGERON 35R. REPLACED FITTING PER SRM 51-1-20D AND SRM 53-2-0. 2L74 4F RT4A25 19951117001201995111700120WP 1995 11 17 UPS804954 119951109A53203755841501 FITTING DOUG DC8 DC871F 302199DWP FS 1180 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1180, LONG 33R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117001211995111700121WP 1995 11 17 UPS804955 119951109A532037558241 FITTING DOUG DC8 DC871F 302199DWP FS 340 CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 340, BETWEEN LONGERONS 33L TO 34R. REPLACED FITTING PER SRM 53-2-0 FIG 20. 2L74 4F RT4A25 19951117001231995111700123NE 1995 11 17 95ZZZX6202 119951012A6510S163561202002 COUPLING SKRSKYS58T S58ET 8141803NE T/R DRIVESHAFT DEBONDED A NYBAK NONE O OTHER ININSP/MAINT 1 EA1147781 1708 CHP002 58855 DURING A 1,750 HOUR INSPECTION, THE MECHANIC NOTED THAT EVERY DOUBLE SEGMENT, THE RUBBER WAS DEBONDED BEYOND LIMITS IAW S-58T MMS. THIS COUPLING WAS IN THE NR 5 POSITION. SUBMITTER STATED INADEQUATE RUBBER BONDING ON THIS NEW FAA-PMA. REPLACED FLEX COUPLING IAW S-58T MM. 2G72 4U 1H11 19951117001321995111700132NM 1995 11 17 95ZZZX6212 119951001A3260BACR15AZ631 RIVET BOEING727 72722C 138400FNM NOSE GEAR MISSING A RYNAO OTHER P NO WARNING INDICATION LDLANDING 1 CE07421EX 19099 NO DOWN AND LOCKED INDICATION OF NOSE GEAR UPON DESCENT INTO SEA. CYCLED GEAR ONCE AND GREEN LIGHT ILLUMINATED AFTER APPROXIMATELY 4 MINUTES. FOUND 2 OF 3 RIVETS RETAINING NOSE GEAR LOCK SWITCH MOUNT BRACKETS TO NOSE GEAR BRACES MISSING ALLOWING SWITCH TO ROTATE. REPLACED MISSING HARDWARE. 2L73 4F A3WE 19951117001331995111700133NM 1995 11 17 95ZZZX6213 119951024A2163 CONNECTOR DORNERDO32 DO328100 2996000NM TEMP SENSOR DIRTY A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07328JS 3030 DAY/PHL - FLT 4149 - EN ROUTE, CREW WAS UNABLE TO COOL CABIN. ELECTED TO RETURN TO DAY. MAINTENANCE CLEANED CONNECTOR ON BOTH LT AND RT PACK DUCT TEMP SENSOR IAW STANDARD MAINTENANCE PRACTICES. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951117001341995111700134EU 1995 11 17 95ZZZX6214 119951023A3150JS5 SW ACTUATOR HONEYWELL BAG JETSTMJETSTM3101 1500215EU COCKPIT DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07833JS 725 FLT 4089 - AFTER TAKEOFF, 'BETA' HORN SOUNDED, CREW UNABLE TO CANCEL HORN, ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. DAY MAINTENANCE INSPECTED AIRCRAFT, DISCOVERED A DEFECTIVE MICROSWITCH ACTUATOR. MAINTENANCE REPLACED ACTUATOR IAW MM 27-00-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951117001351995111700135NM 1995 11 17 95ZZZX6215 119951021A3230001U102A06000 SAFETY PIN DORNERDO32 DO328100 2996000NM NLG INSTALLED A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07328JS 3030 FLT 4002 - CREW REPORTED GEAR UNSAFE LIGHT (NLG) AFTER TAKEOFF. RETURNED TO FIELD WITHOUT FURTHER INCIDENT. CAK MAINTENANCE REMOVED NLG SAFETY PIN. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951117001361995111700136EA 1995 11 17 95ZZZX6216 119951022A3234574205 SELECTOR VALVE DHAV DHC7 DHC7102 2802708EA LANDING GEAR FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA07900HA152162884 308 025 ORF/DCA - FLT 3144 - THE LEFT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. INSPECTED THE LEFT MAIN GEAR AND FOUND NO DISCREPANCIES. THE EVALUATION FLIGHT WAS SATISFACTORY. PHL/DCA - FLT 3121 - LATER, AFTER TAKEOFF OUT OF PHL, THE LEFT MAIN GEAR WOULD NOT FULLY RETRACT. CYCLED GEAR AND GEAR RETRACTED NORMALLY. CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE EMERGENCY RELEASE MAIN LANDING GEAR VALVE. REF OPERATOR CONTROL NR 95ZZZX6217. 2H74 4T A20EA 19951117001371995111700137EA 1995 11 17 95ZZZX6217 119951022A32301498451 EMER RELSE VALVEWHITTAKER DHAV DHC7 DHC7102 2802708EA LANDING GEAR FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA07900HA38584 294 025 ORF/DCA - FLT 3144 - THE LEFT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. INSPECTED THE LEFT MAIN GEAR AND FOUND NO DISCREPANCIES. THE EVALUATION FLIGHT WAS SATISFACTORY. PHL/DCA - FLT 3121 - LATER, AFTER TAKEOFF OUT OF PHL, THE LEFT MAIN GEAR WOULD NOT FULLY RETRACT. CYCLED GEAR AND GEAR RETRACTED NORMALLY. CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE AND THE EMERGENCY RELEASE MAIN LANDING GEAR VALVE. REF OPERATOR CONTROL NR 95ZZZX6216. 2H74 4T A20EA 19951117001381995111700138WP 1995 11 17 95ZZZX6218 119951005A3350 EEL BATTERY PACK LKHEED1011 10113851 5265010WP CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11192AT 053994 193C1057 MCO - EMERGENCY EXIT SIGN AND OVERHAUL EXIT LIGHT WILL NOT COME ON AT THE 3R PASSENGER EXIT DOOR. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT THE R3 DOOR. OPS CHECK GOOD. 2L73 4F A23WE 19951117001391995111700139WP 1995 11 17 95ZZZX6219 119950802A32313250006 CONTROL MODULE LKHEED1011 10113851 5265010WP GEAR DOOR FAILED A AMTAK NONE O OTHER TOTAKEOFF 1 GL11197AT 000227 193P1082 SFO - WITH GEAR LEVER UP, THE GEAR REMAINED DOWN AND LOCKED (3 GREENS), DOOR INTRANSIT LIGHT ON AND AUTO GROUND SPOILER LIGHT ON. (NO GEAR/DOOR LIGHT ON AT FE ANNUNCIATOR.) RECYCLED LEVER GEAR UP - NORMAL. REMOVED AND REPLACED MODULE PER MM 32-31-01. OPS AND LEAK CHECK OK. 2L73 4F A23WE 19951117001401995111700140NM 1995 11 17 95ZZZX6220 119951010A33503322037 EEL BATTERY BOEING727 727227 1384078NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11767AT 24027 22001 IND - FORWARD SECTION EGRESS LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY, OPS CHECKS NORMAL. 2L73 4F A3WE 19951117001411995111700141CE 1995 11 17 95ZZZX6221 119951016A2841509215821 GASKET 999200653 BEECH 99 C99 1154006CE FUEL PROBE DEFORMED A GUUAO OTHER BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS NRNOT REPORTED 1 SO19216EE U206 MIA/HAV - FLT DS101 - PILOT REPORT: FUEL LEAK ON RIGHT NACELLE, FUMES IN CABIN. MAINTENANCE: RETORQUED FUEL PROBE HARDWARE FOR NACELLE TANK. 1L72 3T A14CE 19951117001421995111700142CE 1995 11 17 95ZZZX6222 119951019A3260 ANNUNCIATOR LITE BEECH 99 C99 1154006CE LANDING GEAR MALFUNCTIONED A GUUAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO19987RA U205 FLL/GNV - FLT 381 - PILOT REPORT: MAIN GEAR ANNUNCIATOR LIGHTS WOULD NOT ILLUMINATE, ON GEAR EXTENSION, POPPED. MAINTENANCE: INSPECTED ALL UPLOCK AND DOWNLOCK SWITCHES AND COMPONENTS AND INSPECTED GEAR SELECTOR HANDLE AND WIRING, NO DEFECTS NOTED. SWUNG GEAR SEVERAL TIMES, COULD NOT DUPLICATE. AIRCRAFT RELEASED. 1L72 3T A14CE 19951117001461995111700146EU 1995 11 17 95ZZZX6226 119951020A5755 BOLT BAG BAE146BAE146200A 1500266EU RT SPOILER LOOSE A A6WAK NONE E VIBRATION/BUFFET CLCLIMB 1 GL31606AW E2033 ATW - FLT 309 - DURING EN ROUTE CLIMB WITH TMS TGT SYNC SELECTED, THE CPT AND FO FELT A PRONOUNCED AIRFRAME VIBRATION ON COCKPIT FLOOR AND COCKPIT SEATS. NO VIBRATION WAS FELT IN CONTROL YOKE. REMOVED AND REPLACED LOCKING PLATE ON RT WING MIDDLE SPOILER HINGE BOLT. (LOOSE BOLT CAUSED PLAY IN SPOILER HINGE.) OPS CHECK SATISFACTORY. 2H74 4F RTA49EU 19951117001471995111700147 1995 11 17 95ZZZX6227 419951019A2312101182 ANTENNA BAG BAE146BAE146300A 1500267EU NR 1 VHF FAILED A A6WAA UNSCHED LANDING O OTHER CLCLIMB 1 GL31614AW14547 1170 E3132 DEN - FLT 354 - NR 1 COMM RADIO BECOMES TOTALLY UNUSEABLE AS DISTANCE INCREASES TO STATION. COMPLETELY DEAD ON 1ST CENTER FREQUENCY. REMOVED AND REPLACED NR 1 VHF COMM ANTENNA PER MM. OPS CHECK GOOD. 2H74 4F RTA49EU 19951117001481995111700148EU 1995 11 17 95ZZZX6228 119951019A5320 FAIRING BAG BAE146BAE146200A 1500266EU LT MLG BIRD STRIKE A A6WAK NONE C F.O.D. LDLANDING 1 GL31293UE E2097 SGF - FLT 379 - BIRD STRIKE FORWARD OF LEFT LANDING GEAR ON FAIRING. C/W BIRD STRIKE INSPECTION PER AMM 05-50-21. 2H74 4F RTA49EU 19951117001491995111700149WP 1995 11 17 BUFA9523 119951012A2910 LINES DOUG DC8 DC861 3021952WP HYD SYSTEM LEAKING A BUFAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 CE05915BV 45981 GGT/MIA - FLT CWC148 - LOSS OF HYDRAULIC FLUID TO STAND PIPE. COMPLETED EMERGENCY PROGRESS CHECK LIST. FOUND LEAK AT SEVERAL HYDRAULIC LINES. REMOVED AND REPLACED BAD HYDRAULIC LINES IAW MM 29-10. (X) 2L74 4F 4A25 19951117001501995111700150NE 1995 11 17 BUFA9524 219951014A7261 OIL LINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 4 ENGINE LOOSE A BUFAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE05924BV 45920 671024 BBR/BOS - FLT AI197 - AFTER TAKEOFF, NR 4 ENGINE OIL PRESSURE LIGHT FLICKERED. CHECKED OIL PRESSURE GAUGE, FLUCTUATING RAPIDLY AND QUANTITY NEAR ZERO. SHUT DOWN ENGINE IAW BUFFALO PROCEDURES. FOUND OIL SUPPLY LINE TO GEARBOX UNSECURED, SECURED LINE AND INSPECTED ENGINE IAW JT3D MM 72-00. SYS OPS CHECK GOOD AND NO LEAKS IAW 7200 AND 79-20-00. (X) 2L74 4F4 F 4A25 1E8 19951117001511995111700151WP 1995 11 17 GRAA9546 119951005A7711AE7013105E0196 LINE DOUG DC9 DC987 3022087WP NR 1 ENGINE DEFECTIVE A GRAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP111074T 49727 ON OCTOBER 5, 1995, AIRCRAFT DEPARTED BELLINGHAM, WASHINGTON, EN ROUTE TO LAS VEGAS, NEVADA. AT CRUISE, THE PILOT REPORTED THE NR 2 ENGINE SEEMED TO BE PRODUCING PARTIAL POWER. THE AIRCRAFT DIVERTED INTO RENO, NEVADA, WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND DISCOVERED THE NR 2 ENGINE WAS PERFORMING NORMALLY, NR 1 ENGINE EPR WAS READING INCORRECTLY. MAINTENANCE DETERMINED THE NR 1 ENGINE, PT7, EPR LINE WAS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE LINE. AN OPERATIONAL CHECK OF THE SYSTEM WAS PERFORMED, NO DEFECTS NOTED, THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F RTA6WE 19951117001521995111700152 1995 11 17 IXXA199592 419951027A34202589201913 INSTRUMENT AMP DOUG DC8 DC863F 302198FWP RADIO RACK ERRATIC A IXXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23784AL 1534 46135 FLL/TOL - AFTER TAKEOFF, CREW NOTED THE NR 2 COMPASS SYSTEM INDICATORS WERE ERRATIC AND THE CAPTAIN'S ATTITUDE INDICATOR FLAG WAS IN VIEW WITH NO PITCH INDICATION. THE CREW RETURNED TO FLL FOR MAINTENANCE. MAINTENANCE REPLACED THE NR 1 INSTRUMENT AMP AND ALL SYSTEM OPS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L74 4F 4A25 19951117001531995111700153WP 1995 11 17 ORJA95100 119951014A3350 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11842RA 49604 EMERGENCY FLOOR TRACT LIGHTING, ROW 21 TO ROW 25, INOPERATIVE. REMOVED AND REPLACED BATTERIES AT ASSOCIATED BATTERY PACK. OPS NORMAL. (X) 2L72 4F A6WE 19951117001541995111700154WP 1995 11 17 ORJA95101 119951012A3244 TIRE DOUG DC9 DC983 3022083WP NR 4 WHEEL ASSY FAILED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11875RA 5403 53182 NR 4 TIRE BLOWN DUE TO TREAD SEPARATION. REMOVED AND REPLACED NR 4 TIRE DUE TO TREAD SEPARATION DURING TAKEOFF. (X) 2L72 4F RTA6WE 19951117001551995111700155WP 1995 11 17 ORJA95102 119951015A5330 SKIN DOUG DC9 DC983 3022083WP FUSELAGE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11879RA 53185 SURFACE CORROSION ON PRODUCTION SKIN SPLICE 3 FRAMES AFT OF L-1 DOOR CUT OUT BETWEEN 4TH AND 5TH STRINGERS BELOW CUSP. CLEANED AND TREATED AREA. IAW MD-80 SRM 51-10-3. (X) 2L72 4F RTA6WE 19951117001561995111700156 1995 11 17 ORJA95103 419951015A3442 DISH DOUG DC9 DC983 3022083WP RADAR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11879RA 53185 MINOR SURFACE CORROSION ON AFT FACE OF RADAR DISH. REMOVED MINOR CORROSION AND TREATED WITH ALODINE. REF SRM 51-10-3. (X) 2L72 4F RTA6WE 19951117001571995111700157WP 1995 11 17 ORJA95104 119951013A3350 MODULE DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11833RA 53045 EMERGENCY LIGHT AT ROW 18 FLOOR FAILS TO ILLUMINATE. REMOVED AND REPLACED LAMP MODULE TO EMERGENCY LIGHT AT ROW 18. (X) 2L72 4F RTA6WE 19951117001581995111700158WP 1995 11 17 ORJA95105 119951018A3350 EEL TRACK DOUG DC9 DC983 3022083WP CABIN INOPERATIVE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11878RA 53184 E-PATH TRACK OFF AT ROW 2. REINSTALLED E-PATH TRACK. (X) 2L72 4F RTA6WE 19951117001591995111700159EU 1995 11 17 P2RA950019 119951031A3350311701 BATTERY PACK AIRBUS300 A300B4203 3930306EU CABIN DISCHARGED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314976 3175 271 EMERGENCY EXIT LIGHT AT R-3 DOOR INOPERATIVE. RE N/R NR 749. REMOVED AND REPLACED BATTERY PACK EMERGENCY LIGHT AT R-3 DOOR. OPS CHECK GOOD. REF MM 33-51-14. (X) 2L72 4F A35EU 19951117001601995111700160SO 1995 11 17 SRAA109502 119951003A2460 FREQ RELAY LKHEED382 382E 526413USO COCKPIT SHORTED A SRAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO19901SJ 4299 MHZ - AFTER TAKEOFF, AIRCRAFT LOST ELECTRICAL POWER TO ESSENTIAL NAVIGATION SYSTEMS FOR THE NR 1 RADAR, OMEGA AND VOR/ILS SYSTEMS. ACCOMPLISHED AIR TURN-BACK TO MHZ AND LANDED SAFELY. INSPECTED WIRING, FOUND NR 2 FREQUENCY RELAY SHORTED AND NR 1 FREQUENCY RELAY CONNECTOR HAD CRIMPED WIRES, REPLACED NR 2 FREQUENCY RELAY AND REPAIRED CRIMPED WIRE ON NR 1 SYSTEM. OPS CHECKED GOOD PER CHAPTER 24. (X) 2H74 4T A1SO 19951117001611995111700161 1995 11 17 SRAA109504 419951003A3454 WIRE LKHEED382 382E 526413USO BS 245 SHORTED A SRAAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19901SJ 4299 FLT ADT3 - DURING FLIGHT, BOTH NR 1 AND NR 2 VOR'S WENT INOP. ACCOMPLISHED AIR TURN-BACK TO MHZ FOR REPAIR. FOUND SHORTED COAX CABLE AT BODY STA 245 AND TAIL. REPLACED COAX CABLE AND OPS CHECK SYSTEM, BOTH VOR'S OPERATED NORMAL PER MM CHAPTER 34. (X) 2H74 4T A1SO 19951117001621995111700162SO 1995 11 17 SRAA109505 119951005A291366039 HYD PUMP LKHEED382 382B 5264104SO NR 3/4 FAILURE A SRAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO19907SJ 4248 CHS - FLT ADN5 - DURING FLIGHT FROM CHS, SUCTION BOOST PUMP LIGHT CAME ON, FOUND RESERVOIR EMPTY, SERVICED SYSTEM, BOTH SYSTEMS' PRESSURE WENT BACK UP, THEN NR 3 DROPPED DOWN FROM 1800 TO 1600 PSI. NR 4 SYSTEM DROPPED TO 1200 PSI. SHUT OFF BOTH SYSTEMS AND DIVERTED TO MIA. REPLACED BOTH NR 3 AND NR 4 ENGINE DRIVEN HYD PUMPS, BOOST SYSTEM FILTERS, AND ENGINE PRESSURE FILTERS, FLUSHED. SYSTEM OPS CHECKED GOOD PER MM CH 29 AND CH 71. (X) 2H74 4T A1SO 19951117001631995111700163SO 1995 11 17 SRAA99513 119950925A61207143253 VALVE HOUSING LKHEED382 382E 526413USO NR 3 PROP MALFUNCTIONED A SRAAE ENGINE SHUTDOWN O OTHER TOTAKEOFF 1 SO19923SJ 4301 LAE - FLT 1093 - DURING TAKEOFF ROLL, NR 3 PROP FLUXED 1 TO 2 PERCENT, TORQUE WAS HIGHER THAN OTHER ENGINES, SHUT DOWN ENGINE AS PRECAUTIONARY. FOUND VALVE HOUSING NOT FUNCTIONING PROPERLY. REPLACED NR 3 PROP VALVE HOUSING ASSY. PERFORMED ENGINE RUN-UP, OPS CHECKED GOOD PER J/C 7101 AND 7101-2. (X) 2H74 4T A1SO 19951117001641995111700164GL 1995 11 17 SRAA99516 219950926A72106850209 RED GEARBOX LKHEED382 382B 5264104SO ALLSN 501D 501D22A 03006GL NR 1 FAILED A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19916SJ 4134 550226 RMS - FLT ADT4 - DURING FLIGHT, NR 1 ENGINE REDUCTION GEARBOX FAILED. SHUT DOWN NR 1 ENGINE AND LANDED SAFELY. FOUND METAL IN MAG PLUGS AT REDUCTION GEARBOX. REPLACED NR 1 ENGINE AND PROPELLER PER J/C 7103, 6101. PERFORMED ENGINE RUN-UP, SYSTEM OPS CHECKED GOOD. (X) 2H74 4T4 T A1SO E282 19951117001651995111700165NM 1995 11 17 TAOA109520 119951029A3350900835A BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS UA5221 22043 FORWARD OVERHEAD EMERGENCY LIGHT WILL NOT TEST. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 0 4 A3WE 19951117001661995111700166NM 1995 11 17 USAA950975 119950714A5315 FLOOR BEAM BOEING757 757225 1384959NM BS 1640 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19601AU34462 22193 CLT - DURING A CMV 1 INSPECTION, VISUALLY FOUND 6 INCH BY 5 INCH AREAS PITTED CORROSION AFT FLANGE OF FLOOR BEAM 1640. REPLACED T-CAP. (M) 2L72 4F RTA2NM 19951117001671995111700167NE 1995 11 17 VTZA96020 219951103A726131041793 OIL SUPPLY TUBE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE FAILED A VTZAA UNSCHED LANDING JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA27306UE3976 497 41020 P75009 IAD/ROC - FLT 6296 - DURING CRUISE AT 0830 HRS ON 11-03-95, DECLARED AN EMERGENCY AND DIVERTED TO MDT DUE TO THE LEFT ENGINE OIL PRESSURE DROPPED AND THE CAP LIGHT ILLUMINATED. FLIGHT CREW SHUT DOWN ENGINE AND LANDED AT MDT WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE TURBINE BEARING OIL SUPPLY TUBE. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19951117001681995111700168EU 1995 11 17 VTZA96022 119951030A3240JE5 ACTUATOR ARM JETAIRJETSTMJETSTM4101 1500501EU EMERGENCY BRAKE BROKEN A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27308UE 41023 IAD/CLE - FLT 6551 - DURING TAKEOFF AT 1951 HRS ON 10-30-95, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE EMERGENCY BRAKE MICROSWITCH ACTUATOR ARM. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951117001691995111700169NE 1995 11 17 WRLA95043 219951022A73208010002 FMU DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 1 ENGINE FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27271WA 48518 DURING INITIAL CRUISE, FLIGHT CREW NOTED NR 1 ENGINE EPR INDICATED 10 PERCENT LESS THAN NR 2 AND NR 3 ENGINE WITH ALL N2 MATCHED. FLIGHT CREW CONTACTED MAINTENANCE CONTROL VIA HF RADIO TO DISCUSS THE SITUATION. MAINTENANCE CONTROL REQUESTED THE AIRCRAFT RETURN TO DEPARTURE POINT FOR TROUBLESHOOTING. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE STATION WITHOUT FURTHER INCIDENT. AFTER MAINTENANCE TROUBLESHOOTING, DETERMINED NR 1 ENGINE'S FMU WAS FAULTY. MAINTENANCE REPLACED THE FMU, BORESCOPED THE ENGINE AS A PRECAUTION (NO FAULTS FOUND). PERFORMED ENGINE GROUND RUN - ALL PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F4 FRTA22WE E24NE 19951117001701995111700170NM 1995 11 17 WRLA95044 119951023A7830TY162910 TR DOUG MD11 MD11 3023602NM NR 2 ENGINE FAILED A WRLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27271WA 48518 DURING INITIAL TAKEOFF ROLL, FLIGHT CREW NOTED NR 1 ENGINE NOT REACHING TARGETED EPR. TAKEOFF TERMINATED. ACFT RETURNED TO GATE. DURING MAINTENANCE T/S, MAINTENANCE CONFIRMED NR 1 ENGINE WOULD NOT ACCELERATE PAST GROUND IDLE POWER. CFDS FAULT REVIEW INDICATED NR 1 THRUST REVERSER NOT STOWED. PHYSICAL EXAM OF THRUST REVERSER VERIFIED THRUST REVERSER IN STOWED POSITION. FURTHER TROUBLESHOOTING IDENTIFIED ERRONEOUS SIGNAL FROM THRUST REVERSER LVDT ACTUATOR TO EEC LIMITING ENGINE TO GROUND IDLE. INOPED THRUST REVERSER LVDT ACTUATOR AND LOCKED THRUST REVERSER IN CLOSED POSITION PER MM. THRUST REVERSER DEFERRED PER MEL 78-30-01. ENG GROUND RUN PERFORMED. ALL PARAMETERS NORMAL. ACFT RETURNED TO SERVICE.(X) 2L73 4F RTA22WE 19951117001921995111700192WP 1995 11 17 9517809987 119951109A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP LT NACELLE MALFUNCTIONED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01987US 47458 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117001931995111700193WP 1995 11 17 9517829997 119951109A3260 CONNECTOR DOUG DC9 DC931 3022065WP NLG LOOSE A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL018933E 47142 DURING APPROACH, THE GREEN LIGHT FOR THE NOSE LANDING GEAR DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. RECYCLED THE LANDING GEAR AND THE LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LOOSE CANNON PLUG FOR THE NOSE LANDING GEAR DOWNLOCK SWITCH. TIGHTENED THE CANNON PLUG, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117001941995111700194WP 1995 11 17 9517839880 119951107A2421 GENERATOR DOUG DC9 DC951 3022051WP RIGHT FAILED A NWAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL01675MC 47651 DURING CRUISE, THE RIGHT GENERATOR FAILED FOLLOWED BY AN AIRCRAFT CROSSTIE LOCKOUT. FOLLOWED COCKPIT OPERATIONAL MANUAL PROCEDURES FOR BOTH FAULTS. THE AIRCRAFT DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117001951995111700195NM 1995 11 17 95FDEA01705 119951111A215032167441 PACK VALVE BOEING727 727227 1384078NM LEFT PACK MALFUNCTIONED A FDEAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO25484FE 21466 ON CLIMBOUT OF DSM PASSING 3,000 FT, THE NR 5 MAIN CARGO SMOKE DETECTOR ILLUMINATED. DETECTOR REMAINED ON APPROXIMATELY 2 MINUTES, THEN EXTINGUISHED. APPROXIMATELY 4 MINUTES LATER THE NR 5 LIGHT ILLUMINATED AGAIN. FOUND PACK C/B TRIPPED. REMOVED AND REPLACED L/PACK VALVE. REPAIRED BLEED AIR LEAK AT CHECK VALVE. RAN PACKS, OPS NORMAL AFTER DUCTS PURGED. 2L73 4F A3WE 19951117001961995111700196NM 1995 11 17 95FDEA01706 119951111A5350 FAIRING BOEING747 7472R7F NM LT WING TE DAMAGED A FDEAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO25639FE 21650 SYD - A/C HAS AN AERODYNAMIC VIBRATION STARTING AT APPROXIMATELY 220 KIAS AND CONTINUING ALL THE WAY TO NORMAL CRUISE. FOUND I/B T/E L/UPPER FAIRING DAMAGED BEYOND REPAIR. NEW FAIRING INSTALLED PER SRM 51-30-02 7, ADJ PER MM 57-22-01. ALSO, FOUND O/B DIAGONAL TIE ROD LWR CLEVIS BROKEN. NEW TIE ROD FITTED AND ADJ PER MM 57-22-01. FOUND FOREFLAP (L/I/B) UPPER AND LOWER SURFACES DAMAGED AND DELAMINATED ADJACENT TO FIXED PANEL DAMAGE. FOREFLAP ASSEMBLY REMOVED AND REPLACED PER MM 27-51-02. FOUND L/I/B ACCESS PANELS DAMAGED BEYOND REPAIR. PANELS REMOVED AND REPLACED PER MM 12-09-00, I/B T/E FLAPS OPS CHECKED SERVICEABLE. 2L74 4F RTA20WE 19951117001971995111700197NM 1995 11 17 95FDEA01707 119951113A5315 FLOORBEAM BOEING727 727227 1384078NM BS 380 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION. CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8. 2L73 4F A3WE 19951117001981995111700198NM 1995 11 17 95FDEA01708 119951031A5330 SKIN BOEING727 727227 1384078NM BS 965 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STA 965 STR 30L FASTENER HEAD PULLED AND SKIN BULGING SUSPECT CORROSION. CUT OUT CORROSION STA 965 STR 30L AND INSTALLED FILLER AND DOUBLER PER SRM 53-30-3 PG 11. 2L73 4F A3WE 19951117001991995111700199NM 1995 11 17 95FDEA01709 119951029A5311 FRAME BOEING727 727227 1384078NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STA 680 ABOVE STR 6R FRAME CRACKED AT RIVET. ROUTED OUT CRACK, INSTALLED REPAIR DOUBLER PER SRM 51-40-3. 2L73 4F A3WE 19951117002001995111700200NM 1995 11 17 95FDEA01710 119951113A5712 RIB BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 STA 760 RT RIB CHORD, HFEC INDICATES CRACKS TOP AND BOTTOM FWD HOLE. INSTALLED REPAIR PER BOEING DRAWING 65-68492-18. 2L73 4F A3WE 19951117002011995111700201NM 1995 11 17 95FDEA01711 119951113A5320 SUPPORT BOEING727 727227 1384078NM BS 1035 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 MAIN CARGO, FLOOR BOARD SUPPORT CORRODED AT STA 1035 AT 12 RBL. INSTALLED NEW PART PER SRM 51-10-1. 2L73 4F A3WE 19951117002021995111700202NM 1995 11 17 95FDEA01712 119951110A5320 ANGLE BOEING727 727227 1384078NM BS 750-760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 LT FLOOR BOARD CHORD ANGLE AT 750 TO 760 LBL 62 IS CRACKED. REMOVED CRACKED CHORD ANGLE, REPLACED LT 760 CHORD ANGLE PER SRM 51-10-1. 2L73 4F A3WE 19951117002031995111700203NM 1995 11 17 95FDEA01713 119951110A5315 FLOORBEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CORROSION ON FLOORBEAM STA 344 BL O LBL 22.5. CORROSION BEYOND LIMITS, REMOVED T-CHORD FROM LBL 2 TO 32 SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007. 2L73 4F A3WE 19951117002041995111700204NM 1995 11 17 95FDEA01714 119951110A5315 FLOORBEAM BOEING727 727227 1384078NM BS 344 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CABIN FLOORBEAM UPPER AFT CHORD CRACKED AT SCREW HOLE STA 344 LBL 25. REMOVED CRACKED SECTION OF CHORD. SPLICED IN NEW SECTION OF CHORD PER FEDEX DRAWING NR SRM 27-53-007. 2L73 4F A3WE 19951117002051995111700205NM 1995 11 17 95FDEA01715 119951110A5315 FLOORBEAM BOEING727 727227 1384078NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 CABIN FLOORBEAM UPPER CHORD LWR SURFACE CORRODED AROUND SCREW HOLE STA 344 LBL 25.5 RBL 20. SPLICED IN NEW SECTION PER FEDEX DRAWING SR 27-53-007. REMOVED CORROSION OUTSIDE OF SPLICE SECTION PER SRM 51-10-6. 2L73 4F A3WE 19951117002061995111700206NM 1995 11 17 95FDEA01716 119951113A5315 FLOORBEAM BOEING727 727227 1384078NM BS 380 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25485FE 21488 FLOORBEAM AT STA 380 RBL 47 WL 208.1 HAS CORROSION, CORROSION REMOVED FOUND OUT OF LIMITS. CUT OUT CORRODED SECTION OF FLOORBEAM AND INSTALLED FLOORBEAM PER SRM 53-10-8. 2L73 4F A3WE 19951117002071995111700207WP 1995 11 17 9817819872 119951108A3350 EEL POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN MALFUNCTIONED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01781NC 48121 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE IN MID CABIN. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117002081995111700208SO 1995 11 17 COMA9511997 119951108A2450 CURRENT RELAYS EMB 120 EMB120RT SO NR 2 BUS FAILED A COMAK NONE H ELECT. POWER LOSS-50 PC UKUNKNOWN 1 SO01257CA 120248 NR 2 ELECTRICAL BUS FAILED. RESET THE NR 2 AND NR 4 OVER CURRENT RELAYS. SYSTEM CHECKS NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951117002091995111700209NE 1995 11 17 COMA9511998 219951109A73217863904 FCU EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01130G 7390 50 120130 LEFT ENGINE WILL NOT START. REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. 2L72 4T4 TRTA31SO E20NE 19951117002101995111700210SO 1995 11 17 COMA9511999 119951110A2916 HYD RESERVOIR EMB 120 EMB120RT SO LH WHEEL WELL OVER FULL A COMAK NONE K FLUID LOSS ININSP/MAINT 1 SO01164D 120164 HYDRAULIC LEAK, LT WHEEL WELL AREA. CLEANED AREA AND CHECKED ALL SYSTEMS, NO LEAKS FOUND. SUSPECT OVERSERVICED RESERVOIR. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951117002111995111700211NE 1995 11 17 COMA9531190 219951111A7230 COMPRESSOR SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LT ENGINE DAMAGED A COMAO OTHER C F.O.D. TOTAKEOFF 1 SO01358CA 2906 340A047 367470 LEFT ENGINE IS MAKING A HIGH PITCHED WHINE DURING TAKEOFF. FOUND COMPRESSOR TO HAVE FOD DAMAGE, REPLACED ENGINE. 2L72 4T4 TRTA52EU E8NE6 19951117002121995111700212EU 1995 11 17 COMA9531191 119951112A61208210151 PCU SAAB SF340 SF340A 7850100EU RT ENGINE DEFECTIVE A COMAO OTHER O OTHER CLCLIMB 1 SO01380CA1713371 340A012 RT PROPELLER WILL NOT MAINTAIN 100 PERCENT RPM DURING TAKEOFF AND APPROACH. REPLACED THE PROPELLER PITCH CONTROL UNIT. 2L72 4T RTA52EU 19951117002131995111700213EA 1995 11 17 COMA9560595 119951110A2760270003 PCU CNDAIRCL600 CL6002B19 EA LT SPOILERS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01920CA5880 2934 7022 FLIGHT SPOILERS STATUS MESSAGE ON EICAS. REPLACED THE LT FLIGHT SPOILER POWER CONTROL UNIT. 2L72 4F RTA21EA 19951117002141995111700214EA 1995 11 17 COMA9560597 119951107A3260864806 PSEU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01931CA3941 272 7037 NOSE WHEEL STEERING FAILED AND ANTI-SKID FAIL MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19951117002151995111700215EA 1995 11 17 COMA956096 119951109A274283963 HSTA CNDAIRCL600 CL6002B19 EA VERT STAB FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01929CA4029 1239 7035 HORIZONTAL STABILIZER TRIM CHANNEL NR 2 INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2L72 4F RTA21EA 19951117002161995111700216EU 1995 11 17 DL31L954333 119951111A3350321440 EEL POWER SUPPLY AIRBUS310 A310324 3930206EU CABIN INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO11835AB 650 EMERGENCY LIGHTS TEST FAIL, THIS WAS DISCOVERED ON A ROUTINE TEST. REPLACED TWO POWER SUPPLIES, OPERATION NORMAL. 2L72 4F RTA35EU 19951117002171995111700217NM 1995 11 17 DL72E954020 119951002A5330 SKIN BOEING727 727247 138408FNM ACC DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND .375 CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUOUT. REPAIRED PER MM 53-30-0 PG 803. 2L73 4F A3WE 19951117002181995111700218NM 1995 11 17 DL72E954025 119951005A5532 SKIN BOEING727 727247 138408FNM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112824W 21329 AT HMV, FOUND VERT STABILIZER SKIN STOPPED DRILLED 3 TIMES AT RT FS 1333 AT BOTTOM OF VERT FIN. REPAIRED PER MM 55-30-0 PG 801. 2L73 4F A3WE 19951117002191995111700219NM 1995 11 17 DL72L954329 119951026A5754 ANGLE 651622296 BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11513DA BN129 21315 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH THE LOWER ANGLE CRACKED AT THE I/B SIDE BEHIND UPSTOP. REPAIRED PER MM 57-54-0 FIG 812. 2L73 4F A3WE 19951117002201995111700220NM 1995 11 17 DL72L954359 119951107A5754 SKIN BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 FOUND ON CV2 CHECK, .25 INCH CRACK IN NR 5 SLAT COVE SKIN AT CUTOUT FOR I/B STOP PAD. REPAIRED PER SRM 57-50-3 FIG 23. 2L73 4F A3WE 19951117002211995111700221NM 1995 11 17 DL72S953666 119950822A5210 ATTACH LUG BOEING727 727232 1384082NM PAX DOOR BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO11499DA 21143 AT HMV, FWD ENTRY DOOR UPPER GATE STOP ROD ATTACH LUG FOUND BROKEN. REPAIRED PER 52-10-2 FIG 10. 2L73 4F A3WE 19951117002221995111700222NM 1995 11 17 DL72S953764 119950908A5531 RIB BOEING727 727232 1384082NM VERTICAL STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 FOUND ON HMV, 4TH RIB DOWN FROM HOLE STA 6 STR 8L CRACKED. FABRICATED REPAIR PER M/M 55-33-0 PG 803. 2L73 4F A3WE 19951117002231995111700223NM 1995 11 17 DL72S954043 119951002A5210 GATE BEAM BOEING727 727232 1384082NM PAX DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 AT HMV, FWD ENTRY DOOR UPPER GATE BEAM CRACKED AT AFT CORNER STOP LUG. REPLACED UPPER GATE BEAM AND INSTALLED REPAIR PER MM 52-11-01. 2L73 4F A3WE 19951117002241995111700224NM 1995 11 17 DL72S954304 119951109A3350900835A BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11408DA 21152 LT FWD OVERWING EMERGENCY LIGHT INOP IN TEST. REPLACED BATTERY PACK, CHECKS GOOD. 2L73 4F A3WE 19951117002251995111700225NM 1995 11 17 DL72S954308 119951109A52306557140514 SKIN BOEING727 727232 1384082NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11516DA 21432 INNER DOOR SKIN CRACKED AT LIGHTNING HOLE. REPAIRED CRACK PER SRM 52-00-3 FIG 3. FOUND DURING SHOP INSPECTION NR 1 CARGO DOOR. 2L73 4F A3WE 19951117002261995111700226NM 1995 11 17 DL72S954315 119951109A2913 HYD PUMP BOEING727 727232 1384082NM NR 2 LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO11522DA 21582 HYD PRESSURE LOSS IN FLT FOUND NR 2 B-HYD PUMP LEAKING. REPLACED NR 2 B-HYD PUMP, OPS NORMAL. 2L73 4F A3WE 19951117002271995111700227NM 1995 11 17 DL72S954331 119951110A3350S106 BATTERIES BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11524DA 21584 AFT AISLE EMERGENCY FLOOD LIGHT INOP. REPLACED BATTERIES IN AFT AISLE EMERGENCY FLOOD LIGHT, CHECKS NORMAL. 2L73 4F A3WE 19951117002281995111700228NM 1995 11 17 DL72S954332 119951111A5347 SEAT TRACK BOEING727 727232 1384082NM BS 1110 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11408DA 21152 THE INBOARD LT SEAT TRACK IS CRACKED AT FLANGE STA 1110, JUST FWD OF FLOORBEAM. REPAIRED TRACK BY SPLICING IN NEW SECTION OF SEAT TRACK PER 727 M/M 53-20-11 FIG 802. 2L73 4F A3WE 19951117002291995111700229NE 1995 11 17 DL72S954340 219951111A731437820113 FUEL PUMP BOEING727 727232 1384082NM PWA JT8 JT8D15 52051NE NR 2 ENGINE FAILED A DALACD ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TOTAKEOFF 1 SO11478DA 5201 20755 696641 ON TAKEOFF ROLL WITH ALT POWER SET, NR 2 ENG ROLLED BACK AND SHUTDOWN ACCOMPANIED BY AUTO PACK TRIP. TAKEOFF ABORTED AND RETURNED TO GATE. INSPECTED NR 2 ENG INLET AND EXH FOR VISIBLE DAMAGE, NONE FOUND. REPLACED ENG DRIVEN FUEL PUMP, LEAK CKS GOOD. PERFORMED TAKEOFF PWR AND ENG RUN UP PER PFHB, ALL CKS GOOD. 2L73 4F4 F A3WE E2EA 19951117002301995111700230NM 1995 11 17 DL72S954343 119951111A2780NAS6604H8 BOLT BOEING727 727232 1384082NM NR 2 SLAT MISSING A DALAO OTHER J WARNING INDICATION TOTAKEOFF 1 SO11536DA 22049 14865 ON DEPARTURE, NR 2 SLAT FAILED TO RETRACT, AIL WAS DISPLACED 30 UNITS, NR 2 SLAT SHOWED GREEN ON S/O PANEL, NR 2 SLAT FINALLY STOWED WITH SPEED REDUCTION. FOUND NR 2 SLAT LWR INBRD BOLT MISSING FROM TRUNNION BRACKET, INTERMITTENTLY BINDING SLAT RETRACTION REPLACED SAME. 2L73 4F A3WE 19951117002311995111700231NM 1995 11 17 DL72W954101 119951025A524265216357 SKIN BOEING727 727247 138408FNM E/E DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112820W 21058 DURING SHOP INSPECTION, THE FWD E/E ACCESS DOOR WAS FOUND WITH INNER SKIN CRACKED .5 INCH ON THE LEFT EDGE. THE DAMAGE WAS REPAIRED PER DL ERA 271810-14AD. 2L73 4F A3WE 19951117002321995111700232NM 1995 11 17 DL72W954103 119951022A5315 FLOORBEAM BOEING727 727247 138408FNM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV, FS 344 FLOORBEAM UPPER CAP CORRODED AT BL 0 TO LBL 60. REPAIRED UPPER CAP PER SRM 53-10-8 FIG 10. 2L73 4F A3WE 19951117002331995111700233NM 1995 11 17 DL72W954244 119951022A5713 STRINGR BOEING727 727247 138408FNM WS 656.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 ATL - HMV, RT WING TANK AFT VENT BOX STRINGER EAR AT RIB 656.5 CRACKED. REPAIRED PER MM 57-13-0. 2L73 4F A3WE 19951117002341995111700234NM 1995 11 17 DL72W954326 119951021A5330 SKIN BOEING727 727247 138408FNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV, FOUND .25 INCH CRACK AT AFT INBD CORNER OF PNEU AIR CONNECTION ACCESS DOOR CUTOUT. STOP DRILLED CRACK IAW M/M 53-30-0 PG 803, LOCATED AND DRILLED REPAIR DOUBLER IAW M/M 53-30-0 PG 803, INSTALLED REPAIR. 2L73 4F A3WE 19951117002351995111700235NM 1995 11 17 DL72W954337 119951021A5520 ANGLE BOEING727 727247 138408FNM ELEVATOR WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV, FOUND ACCESS PANELS 9601 AND 9602 MOUNTING SCREW WORN THROUGH SUPPORT ANGLE. INSTALLED DOUBLER PER SRM 51-40-4 PG 14. 2L73 4F A3WE 19951117002361995111700236NM 1995 11 17 DL757954334 119951110A5350141N782013 RADOME BOEING757 757232 1384965NM NOSE BIRD STRIKE A DALAO OTHER C F.O.D. DEDESCENT 1 SO11655DL 24395 SHORTLY AFTER T/O, HAD BIRD STRIKE, ALL INDICATIONS NORMAL UNTIL DESCENT. DESCENDING THROUGH FL 320, A/C EXPERIENCED LOUD BANG FOLLOWED BY AIR RUSHING NOISE, NO OTHER ABNORMAL INDICATIONS. FOUND RADOME AND RADAR ANTENNA DAMAGED. REPLACED RADOME AND ANTENNA, OPERATIONAL CHECK GOOD. COMPLETED BIRD STRIKE INSPETION PER M/M, NO ADDITIONAL DAMAGE FOUND. 2L72 4F RTA2NM 19951117002371995111700237NM 1995 11 17 DL757954344 119951111A33501317 BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11631DL 23612 14865 EMERGENCY LIGHT IN OVERHEAD BIN AT SEAT GROUP 30 D, E, F IS OUT. RELAMPED ASSY, SYSTEM CKS GOOD. 2L72 4F RTA2NM 19951117002381995111700238NM 1995 11 17 DL757954345 119951111A33500L3071BPEGPL BULB BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11631DL 23612 14865 EMERGENCY ESCAPE FLOOR PATH LIGHT OUT AT SEAT 6. RELAMPED ASSY, CKS GOOD. 2L72 4F RTA2NM 19951117002391995111700239NM 1995 11 17 DL757954351 119951101A5315 FLOORBEAM BOEING757 757232 1384965NM FS 680 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 CORROSION VISIT NR 241, FLOORBEAM CORRODED FS 680 LBL 12 RBL 24, UPPER SURFACE OF BEAM. CLEANED CORROSION PER SRM 51-10-00, CHECKED LIMITS PER SRM 53-00-51. MEASURED WITHIN LIMITS LBL 12 TO LBL 2 AND MEASURED OUT OF LIMITS LBL 2 TO RBL 20. REPAIRED PER SRM 53-30-51. 2L72 4F RTA2NM 19951117002401995111700240NM 1995 11 17 DL757954352 119951101A5315 FLOORBEAM BOEING757 757232 1384965NM BS 760 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING CORROSION VISIT IN ATL, INSP FOUND MAIN CABIN FLOORBEAM BS 760 CORROSION ON FLOORBEAM TOP FROM RBL 20 TO LBL 3. CLEANED CORROSION SRM 51-00-00, CORROSION NO GREATER THAN .020, BLENDED OUT CORROSION PER SRM 53-30-51 AND FABRICATED REPAIR ANGLE. FILLED BLENDED AREAS WITH EPOCAST 15-11 A/B PER PS 900-11-1 NR 11, INSTALLED REPAIR PER SRM 53-30-51. 2L72 4F RTA2NM 19951117002411995111700241NM 1995 11 17 DL757954353 119951031A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1640 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING CORR VISIT IN ATL, INSP FOUND FLOORBEAM STA 1640 BL 0 TO R4 DOOR CORROSION ON TOP OF BEAM AND ON BOTTOM SIDE AT NUT CLIP HOLES. REPAIRED PER SRM 53-30-51 FIG 204. 2L72 4F RTA2NM 19951117002421995111700242NM 1995 11 17 DL757954354 119951031A5315 FLOORBEAM BOEING757 757232 1384965NM FS 1640 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11656DL 24396 DURING CORR VISIT IN ATL, INSP FOUND FLOORBEAM CORROSION AT STA 1640 BL 0 TO L4 DOOR ON TOP OF BEAM AND ON BOTTOM AT NUT CLIP HOLES. REPAIRED PER SRM 53-31-51 FIG 204. 2L72 4F RTA2NM 19951117002431995111700243NM 1995 11 17 DL76L954197 119950930A5414311T3450 SKIN BOEING767 767332 1382001NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11176DN 25061 AT LETTER CHECK, FOUND 2 CRACKS IN NR 2 ENGINE PYLON O/B STRUT SKIN. REPAIRED PER DL ERA 2 71983-14. 2L72 4F RTA1NM 19951117002441995111700244NM 1995 11 17 DL76L954198 119950926A5414311T3450 SKIN BOEING767 767332 1382001NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11175DN 24803 TWO CRACKS HAVE BEEN REPORTED IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THEY BOTH GO THROUGH BOTH SHEETS OF THE BONDED SKIN ASSEMBLY. REPAIRED PER DL ERA 271951-14. 2L72 4F RTA1NM 19951117002451995111700245WP 1995 11 17 DLL10954203 119950907A53301641603 SKIN LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11715DA 193C1092 DURING COMPLETION OF SI 7-69959-12, SEVERAL FASTENER HOLES WERE OVERSIZED AND A 1.75 CRACK WAS FOUND BETWEEN STR 44 AND 45, AT FS 1363. REPAIRED PER DL ERA 271816-14AD. 2L73 4F A23WE 19951117002461995111700246WP 1995 11 17 DLL10954204 119950908A5312 BLKHD CAP LKHEED1011 10113851 5265010WP FS 328 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11715DA 193C1092 CORROSION WAS FOUND IN THE FUSELAGE SKIN AROUND LBL 22 AND ON THE LOWER SURFACE OF THE BULKHEAD CAP AT LBL 18. A CRACK WAS DISCOVERED UNDER THE BLKHD CAP AT LBL 22, FS 328. REPAIRED PER DL ERA 271812-14AD. 2L73 4F A23WE 19951117002471995111700247WP 1995 11 17 DLL10954206 119950906A5712 RIB CAP LKHEED1011 10113851 5265010WP WS 555 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11714DA 193C1090 DURING THE ACCOMPLISHMENT OF SI 7-59208-12AD ON THE RT WING, 2 CRACKS WERE FOUND ON CASTELLATIONS OF THE IWS 555 UPPER RIB CAP. REPAIRED PER DL ERA 271818-14AD. 2L73 4F A23WE 19951117002481995111700248WP 1995 11 17 DLL10954225 119951017A5511 RIBS 1524065106 LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11723DA 193C1150 DURING INSPECTION, FOUND RT STABILZER L/E PANEL WITH 8 CRACKED RIB ASSEMBLIES. REPAIRED PER SRM 55-12-00. 2L73 4F A23WE 19951117002491995111700249WP 1995 11 17 DLL10954347 119951111A3350 EEL POWER SUPPLY 5165741 LKHEED1011 10113851 5265010WP DOOR 2L INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11714DA 193C1090 EMERGENCY EXIT SIGN AND OUTSIDE LIGHT AT 2L DOOR ARE INOP. REPLACED POWER SUPPLY AT 2L DOOR, OPS CKS NORMAL. 2L73 4F A23WE 19951117002501995111700250WP 1995 11 17 DLL12953862 119950926A5347 SEAT TRACK LKHEED1011 1011385115 5265015WP FS 923 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11724DA 193C1151 SEAT TRACK CORRODED FS 923 LBL 94.5. REPAIRED PER SRM 53-21-00. 2L73 4F A23WE 19951117002511995111700251WP 1995 11 17 DLL12953863 119950924A5280 DOOR LKHEED1011 1011385115 5265015WP NLG DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11724DA 193C1151 RT AFT NLG W/W DOOR DENTED AT OUTBD END. REPAIRED PER SRM 52-81-00. 2L73 4F A23WE 19951117002521995111700252WP 1995 11 17 DLL13954213 119950831A5312 BLKHD CAP LKHEED1011 10113851 5265010WP FS 449 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11790DL 193A1143 PREVIOUSLY STOP DRILLED CRACKS IN NLG W/W AFT BULKHEAD ARE EXTENDED BEYOND THOSE STOP DRILLS. ACCOMPLISHED REPAIRS PER DL ERA 271754-1AD. 2L73 4F A23WE 19951117002531995111700253WP 1995 11 17 DLL17954189 119951003A5711 REAR SPAR LKHEED1011 10113853 5265020WP WS 319-346 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 DURING THE ACCOMPLISHMENT OF EO 7-59089-3, CRACK INDICATIONS WERE FOUND EMANATING FROM TWO FASTENER HOLES COMMON TO THE UPPER WING SKIN AND THE UPPER SPAR CAP. ACCOMPLISHED REPAIRS PER DL ERA 271961-14AD. 2L73 4F A23WE 19951117002541995111700254WP 1995 11 17 DLL17954190 119951003A5320 ANGLE LKHEED1011 10113853 5265020WP WING/FUS OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 SEVERAL FASTENERS IN THE BASE HOR FLANGE OF THE FAIL-SAFE ANGLE WERE FOUND TO BE OVERSIZED, WING TO FUSELAGE. REPAIRED PER DL ERA 271865-14 AD. 2L73 4F A23WE 19951117002551995111700255WP 1995 11 17 DLL17954191 119951003A53131554989105 LONGERON LKHEED1011 10113853 5265020WP FS 1860 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 THE OUTER CAP ANGLE OF THE LT UPPER LONGERON IN THE FUSELAGE AFTER BODY AT STA 1860 WAS FOUND CRACKED IN THE RADIUS. REPAIRED PER DL ERA 271830-14. 2L73 4F A23WE 19951117002561995111700256WP 1995 11 17 DLL17954192 119951003A53201512169101 DOOR SILL LKHEED1011 10113853 5265020WP FS 901 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 THE LOWER DOOR SILL INBOARD CAP FITTINGS WERE FOUND CORRODED AND REQUIRED REPLACEMENT. REPAIRED PER DL ERA 271846-14. 2L73 4F A23WE 19951117002571995111700257WP 1995 11 17 DLL17954193 119951003A53121641603101 BULKHEAD LKHEED1011 10113853 5265020WP BS 1363 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 SEVERAL FASTENER HOLES BETWEEN STR 21 AND 22 WERE OVERSIZED TO A .25 DIAMETER. FASTENER REMOVAL ACCOMPLISHMENT OF EO 7-69959-12AD, REPAIRED PER DL ERA 271854-14AD. 2L73 4F A23WE 19951117002581995111700258WP 1995 11 17 DLL17954194 119951003A52301582145102 LATCH FITTINGS LKHEED1011 10113853 5265020WP CARGO DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 THE NR 1 THROUGH NR 8 C-1A CARGO DOOR LATCH FITTINGS WERE FOUND WITH PITTING IN THE UPPER WELLS. DRAIN HOLES WILL BE DRILLED IN ALL EIGHT FITTINGS PER DL ERA 271881-14AD. 2L73 4F A23WE 19951117002591995111700259NE 1995 11 17 DLM11954335 219951110A7261 OIL SEAL DOUG MD11 MD11 3023602NM PWA 4460 PW4460 NE NR 3 ENGINE FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO11807DE14020 48478 723929 AIR TURNBACK, OIL SMELL IN CABIN CAUSED BY NR 3 ENG. LOCKED OUT PRESSURE REGULATOR VALVE FWD TO MC OPER MEL 36-12-01. REPLACED COALESCER BAG, REPLACED NR 3 ENG PER ROUTINE CARD DECK, OPERATION NORMAL. 2L73 4F4 FRTA22WE E24NE 19951117002601995111700260NM 1995 11 17 DLM88954205 119950908A533059304831 SKIN DOUG MD88 MD88 3023688NM C3 DOOR CUTOUT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO11964DL 49983 THE FUSELAGE SKIN AND DOOR DOUBLER ALONG THE AFT EDGE OF THE C-3 DOOR CUTOUT HAVE SUSTAINED GROUND DAMAGE, JUST BELOW THE NR 3 DOOR STOP. REPAIRED PER DL ERA 271824-14. 2L72 4F RTA6WE 19951117002611995111700261 1995 11 17 DLM88954324 419951110A2230 CONTROL PANEL 4034242906 DOUG MD88 MD88 3023688NM PWA JT8 JT8D15A 52051NE AUTO THROTTLE MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11928DL 87040759 49715 700235 DURING CLIMB PASSING APPROX 1,000 FT, AUTO THROTTLES WOULD NOT WORK, MODE CONTROL PANEL FROZE AND A/C HAD UNCOMMANDED ROLL/YAW. REPLACED DFGC CONTROL PANEL, RAN RTS ON DFGC 1 AND 2, BOTH SYSTEMS GO. CREW HAD RESET DFG SW-B CKT BRKR SYSTEM HAD RETURNED TO NORMAL. 2L72 4F4 FRTA6WE E2EA 19951117002621995111700262NM 1995 11 17 DLM88954330 119951110A32305952247503 SPRAY DEFLECTOR DOUG MD88 MD88 3023688NM NLG BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11922DL 49646 ON T/O, COULD NOT RAISE THE NOSE GEAR HAD A RED LIGHT UNSAFE ON NOSE GEAR ONLY. FOUND LEFT HAND NOSE SPRAY DEFLECTOR BROKEN. REPLACED SAME, RAN NOSE GEAR, CHECKS GOOD. 2L72 4F RTA6WE 19951117002631995111700263NM 1995 11 17 P5CA9500837 119951110A5320654U6039111 FITTING BOEING747 747123 1384873NM STRINGER 11 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23858FT 20109 FOUND CRACK ON SPLICE FITTING AT STRINGER 11 FWD AREA, NO OTHER DEFECTS. REPLACED FITTING WITH (P/N 654U6039-112) IAW SB 53-A2280. 2L74 4F A20WE 19951117002641995111700264NM 1995 11 17 P5CA9500838 119951111A29309750018007 OVERHEAT SWITCH BOEING747 747121 1384871NM NR 4 HYD SYSTEM DEFECTIVE A P5CAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP23832FT 20347 DURING TAXI, NR 4 HYDRAULIC OVERHEAT LIGHT ILLUMINATED NR 4 SYSTEM. REMOVED AND REPLACED NR 4 HYDRAULIC OVERHEAT SWITCH IAW MM 29-41-00. 2L74 4F A20WE 19951117002651995111700265WP 1995 11 17 SCNA95262 119951108A261172130000011 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 8 LAV FAILED A SCNAK NONE N FALSE WARNING UKUNKNOWN 1 GL15573SC 46905 THE NUMBER 8 LAVATORY SMOKE DETECTOR WAS FOUND TO SOUND FOR NO APPARENT REASON. REMOVED AND REPLACED NUMBER 8 LAV SMOKE DETECTOR, NEW DETECTOR OPS CHECKED GOOD. 2L73 4F A22WE 19951117002661995111700266WP 1995 11 17 UPS804956 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 691.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 691.25 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951117002671995111700267WP 1995 11 17 UPS804957 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 741.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 741.25 IS CRACKED AT THE AFT LOWER END. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21. 2L74 4F RT4A25 19951117002681995111700268WP 1995 11 17 UPS804958 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 691.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 766.25 CRACKED AT THE AFT UPPER END. INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D, SRM 51-1-21 AND 57-2-0. 2L74 4F RT4A25 19951117002691995111700269WP 1995 11 17 UPS804959 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 227.335 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD L/E RIB AT STA XS 227.335 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-2-0, 51-1-20D, AND SRM 51-1-21. 2L74 4F RT4A25 19951117002701995111700270WP 1995 11 17 UPS804960 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 811 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED UPPER AFT END STA XFS 811. INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21. 2L74 4F RT4A25 19951117002711995111700271WP 1995 11 17 UPS804961 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 484.895 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XS 484.895 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR IAW SRM 51-1-21, 51-1-20D AND SRM 57-2-0. 2L74 4F RT4A25 19951117002721995111700272WP 1995 11 17 UPS804962 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 70.95 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD L/E RIB AT STA XILD 70.95 IS CRACKED AT THE AFT UPPER END. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 57-2-0. 2L74 4F RT4A25 19951117002731995111700273WP 1995 11 17 UPS804963 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 722.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING AT BD L/E RIB AT STA XFS 72.25 CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW SRM 57-2-0 AT STA XFS 72.25. 2L74 4F RT4A25 19951117002741995111700274WP 1995 11 17 UPS804964 119951110A5531 RIB DOUG DC8 DC871F 302199DWP VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB SECTION INTERIOR HAS TWO RIB ENDS CRACKED AT STA ZFS 279 AND ZFS 273. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 55-2-0 AND 51-1-20D. 2L74 4F RT4A25 19951117002751995111700275WP 1995 11 17 UPS804965 119951110A5531 RIB DOUG DC8 DC871F 302199DWP VERT STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND VERTICAL STAB LE LOWER INTERIOR SECTION HAS THE ENDS OF FRAME RIBS CRACKED AT XFS 104.75 LT AND RT, XFS 111.15 AND LT XFS 122.75. STOP DRILLED CRACKS, FABRICATED REPAIR ANGLE AND INSTALLED REPAIR PER SRM 55-2-0 AND 51-1-20D. 2L74 4F RT4A25 19951117002761995111700276WP 1995 11 17 UPS804966 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 628.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING O/B LE RIB STA 628.75 CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE DOUBLER IAW SRM 57-2-0. 2L74 4F RT4A25 19951117002771995111700277WP 1995 11 17 UPS804967 119951110A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FS 281 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN SEAT TRACK RBL 24 POSITION 3 APPROX STA 28 HAS MODERATE CORROSION. REMOVED DAMAGED AREA IAW SRM 53-2-3 FIG 6D AND TR 53-89. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED PLUG IAW SRM 51-1-7 AND SRM 53-2-3 FIG 6D. 2L74 4F RT4A25 19951117002781995111700278WP 1995 11 17 UPS804968 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 365 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE CRACKED UNDER GUSSET, WS 365 PANEL 522B ACCESS. FABRICATED PARTS AND INSTALLED REPAIR IAW SRM 57-2-0 AND 51-1-2D. 2L74 4F RT4A25 19951117002791995111700279WP 1995 11 17 UPS804969 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 597.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED AFT LOWER END XFS 597.5. FABRICATED AND INSTALLED REPAIR ANGLES PER SRM 57-2-0, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951117002801995111700280WP 1995 11 17 UPS804970 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 610 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING O/B LE RIB AT STA XFS 610.0 IS CRACKED AT AFT UPPER END. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 SRM 51-1-20D. 2L74 4F RT4A25 19951117002811995111700281WP 1995 11 17 UPS804971 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 616.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LEADING EDGE RIB CRACKED AT XFS 616.25 AT AFT LWR END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0. 2L74 4F RT4A25 19951117002821995111700282WP 1995 11 17 UPS804972 119951110A5521 RIB DOUG DC8 DC871F 302199DWP ELEVATOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT ELEV WEB CRACKED AT HOLE CUTOUT STA XE 26. REMOVED AND REPLACED WEB AT STA XE 26 IAW SRM 51-1-21 AND 51-1-21A. 2L74 4F RT4A25 19951117002831995111700283WP 1995 11 17 UPS804973 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 70-190 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 34R HAS HEAVY CORROSION THROUGH AT FS 70 TO 190 AND OVER SIZE HOLES BEYOND LIMITS. REMOVED AND REPLACED LONG 34R AT FS 70 TO FS 190 IAW SRM 53-2-2, SRM 53-4-1, FIS 29 AND SRM 51-1-20D. FABRICATED REPLACEMENT LONG PER SRM 53-4-1 FIG 29. 2L74 4F RT4A25 19951117002841995111700284WP 1995 11 17 UPS804974 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 467.323 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE RIB AT XFS 467.323 CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0. 2L74 4F RT4A25 19951117002851995111700285WP 1995 11 17 UPS804975 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 70-190 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 34 LEFT HAS CORROSION THROUGHOUT ENTIRE LENGTH AT FS 70 TO FS 190. FABRICATED AND INSTALLED LONGERON AT FS 70 TO FS 190, LONGERON 34L IAW SRM 53-22 AND SRM 53-4-1 FIG 29. 2L74 4F RT4A25 19951117002861995111700286WP 1995 11 17 UPS804976 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BATHTUB FITTING CRACKED AT STATION 1690 LONG 16L. REPLACED FITTING PER SRM 51-1-21 AND 51-3-0. 2L74 4F RT4A25 19951117002871995111700287WP 1995 11 17 UPS804977 119951110A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP FS 1702 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHEAR TIE CORRODED STA 1702 BETWEEN LONG 35 AND 34L. REMOVED SHEAR TIE, FABRICATED SHEAR TIE PER SRM 53-5-1 AND INSTALLED IAW SRM 51-1-21. 2L74 4F RT4A25 19951117002881995111700288WP 1995 11 17 UPS804978 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 11.25 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LEFT WING LE UPPER RIB STA XFS 1125 IS CORRODED BEYOND LIMITS. REMOVED RIB, FABED AND INSTALLED RIB IAW SRM 57-2-0 AND SRM 51-1-21. 2L74 4F RT4A25 19951117002891995111700289WP 1995 11 17 UPS804979 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 448.581 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE RIB AT STA XFS 5448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-21. 2L74 4F RT4A25 19951117002901995111700290WP 1995 11 17 UPS804980 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 610 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LE RIB CRACKED AFT LOWER END XFS 610. STOP DRILLED CRACK, FAB DOUBLER AND INSTALLED PER SRM 57-20 AND 51-1-20D. 2L74 4F RT4A25 19951117002911995111700291WP 1995 11 17 UPS804981 119951110A5730 SKIN DOUG DC8 DC871F 302199DWP RT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT OUTBD LEADING EDGE LOWER SKIN ABOVE NR 4 PYLON IS CRACKED AT PYLON CUTOUT, APPROX 3.4 INCHES LONG. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 57-2-1A AND SRM 51-1-20D. 2L74 4F RT4A25 19951117002921995111700292WP 1995 11 17 UPS804982 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 100-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 36 CORRODED THROUGH AFT AT FS 100 TO FS 190. REMOVED AND FABRICATED LONGERON 36 FROM FS 100 TO FS 190 AND INSTALLED IAW SRM 53-4-12 AND SRM 51-1-20D. 2L74 4F RT4A25 19951117002931995111700293WP 1995 11 17 UPS804983 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 442.185 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING LE RIB AT STA XFS 442.105 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER SRM 57-20 AND 51-1-21. 2L74 4F RT4A25 19951117002941995111700294WP 1995 11 17 UPS804984 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 741.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0. 2L74 4F RT4A25 19951117002951995111700295WP 1995 11 17 UPS804985 119951110A5320 INTERCOASTAL DOUG DC8 DC871F 302199DWP BS 1240 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERCOASTAL CRACKED AT STA 1240 LONG 10L. REPAIR ANGLE FABRICATED AND INSTALLED SRM 53-2-0. 2L74 4F RT4A25 19951117002961995111700296WP 1995 11 17 UPS804986 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 212.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED UPPER AFT END XFS 212.75. STOP DRILLED CRACK, FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 57-3-0 AND 51-30-2. 2L74 4F RT4A25 19951117002971995111700297WP 1995 11 17 UPS804987 119951110A5712 RIB DOUG DC8 DC871F 302199DWP WS 26.25 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING LE TANK RIB AT STA XFS 26.25 IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, FAB AND INSTALLED ANGLE REPAIR IAW SRM 57-3-0, TREATED AND PRIMED IAW SRM 51-1-8. 2L74 4F RT4A25 19951117002981995111700298WP 1995 11 17 UPS804988 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP FS 70 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35R END FITTING CORRODED BEYOND LIMITS AT FS 70. REMOVED AND REPLACED END FITTING AT STA 70, LONGERON 35R PER SRM 53-1-0 AND SRM 51-1-21. 2L74 4F RT4A25 19951117002991995111700299WP 1995 11 17 UPS804989 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35R CORRODED BEYOND LIMITS FROM STA 70 TO 190. REMOVED, FABRICATED AND REPLACED LONGERON 35R FROM STA 70 TO STA 190 IAW SRM 51-1-4 AND SRM 51-1-20D. 2L74 4F RT4A25 19951117003001995111700300WP 1995 11 17 UPS804990 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP FS 852 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERMINAL FITTING CRACKED STA 852 LONGERON 9R. REMOVED FITTING, DRILLED AND INSTALLED NEW FITTING IAW SRM 51-1-0, 51-1-20D AND 51-3-1. 2L74 4F RT4A25 19951117003011995111700301WP 1995 11 17 UPS804991 119951110A5711 SPAR CAP DOUG DC8 DC871F 302199DWP RT AUX SPAR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING I/B LOWER AUX SPAR CORRODED BEYOND LIMITS. REMOVED AND REPLACED ANX SPAR RT WING LOWER I/B IAW DWG 5615058 AND SRM 51-1-20. 2L74 4F RT4A25 19951117003021995111700302WP 1995 11 17 UPS804992 119951110A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 80-140 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER HAS CORROSION AND GROUND OUT THROUGHOUT AND BULGE AT LONG 31L AT FS 80 TO FS 140. REMOVED FINGER DOUBLER FROM FS 70 TO FS 210, FABRICATED REPLACEMENT DOUBLER IAW SRM 53-4-1, 53-1-0 AND INSTALLED IAW SRM 51-1-21. 2L74 4F RT4A25 19951117003031995111700303WP 1995 11 17 UPS804993 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 35L STA 70 TO 190 HAS CORROSION THROUGHOUT AND OVERSIZED HOLES. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-3-2 AND 53-4-1 FIG L9. 2L74 4F RT4A25 19951117003041995111700304WP 1995 11 17 UPS804994 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP BS 674. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERM FITTING CRACKED STA 674 LONG 4L. REMOVED FITTING AND INSTALLED REPLACEMENT FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117003051995111700305WP 1995 11 17 UPS804995 119951110A5720 SPLICE DOUG DC8 DC871F 302199DWP WS 67.5 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE RT WING FRONT SPAR UPPER CAP SPLICE ANGLE AT STA XWS 67.5 IS CRACKED. FABRICATED CAP SPLICE ANGLES AND INSTALLED AT STA XWS 67.5 RT WING IAW SRM 57-6-1 AND 51-1-20D. 2L74 4F RT4A25 19951117003061995111700306WP 1995 11 17 UPS804996 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32L, STA 70 TO 190 CORRODED THROUGHOUT ENTIRE LENGTH BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-2-2 AND 53-4-1. 2L74 4F RT4A25 19951117003071995111700307WP 1995 11 17 UPS804997 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP BS 852. CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN LONGERON TERM FITTING CRACKED STA 852, LONG 5R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20. 2L74 4F RT4A25 19951117003081995111700308WP 1995 11 17 UPS804998 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 33L HAS CORROSION THROUGHOUT ENTIRE LENGHT FROM STA 70 TO 190. REMOVED LONG 33L FROM FS 70 TO 190 PER SRM 53-2-2, 53-4-1 AND 51-1-20D. 2L74 4F RT4A25 19951117003091995111700309WP 1995 11 17 UPS804999 119951110A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 70-190 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32 CORRODED FROM STA 70 TO 190. REMOVED AND FABRICATED REPLACEMENT LONGERON IAW SRM 52-4-1 FIG 29, INSTALLED REPLACEMENT LONGERON 32L STA 190 IAW SRM 51-1-20D. 2L74 4F RT4A25 19951117003101995111700310WP 1995 11 17 UPS805000 119951110A5330 SKIN DOUG DC8 DC871F 302199DWP BS 680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON SKIN FS 680 FRAME AND LONG 34R. REMOVED FASTENERS AND CORROSION PER SRM 51-1-21, 51-1-20D AND 51-1-8, REPLACED FASTENERS AND REPAIRED PER. 2L74 4F RT4A25 19951117003111995111700311WP 1995 11 17 UPS805001 119951110A5330 SKIN DOUG DC8 DC871F 302199DWP BS 660-680 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON SKIN, LONGERON AND TIE CLIP AT FS 660 TO 680 LONG 34L TO 33L. REMOVED FASTENERS SEALANT AND CORROSION PER SRM 51-1-21, 51-1-20D AND 51-1-8. TREATED, PRIMED AND REINSTALLED FASTENERS AND SEALANT PER SRM 51-1-21, 51-1-20D AND 51-1-8. 2L74 4F RT4A25 19951117003121995111700312WP 1995 11 17 UPS805002 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP FS 670 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CABIN LONGERON TERMINAL FITTING CRACKED STA 670 LONG 11R. FABRICATED FITTING PER DWG 5750540 AND REPLACED FITTING PER SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19951117003131995111700313WP 1995 11 17 UPS805003 119951110A5711 SPAR CAP DOUG DC8 DC871F 302199DWP LT AUX SPAR CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING I/B LOWER ANX SPAR CORRODED BEYOND LIMITS. REPLACED LT ANX SPAR PER DOUGLAS BWG 561508 AND SRM 57-1-0. 2L74 4F RT4A25 19951117003141995111700314WP 1995 11 17 UPS805004 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP FS 670 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 11L TO FRAME ATTACH FITTING CRACKED BS 670. REMOVED CRACKED FITTING IAW SMR 51-1-20, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 5750540 SRM 51-1-20D AND 51-3-0. 2L74 4F RT4A25 19951117003151995111700315WP 1995 11 17 UPS805005 119951110A5320 FITTING DOUG DC8 DC871F 302199DWP BS 796 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 796 RBL 02 KEEL BEAM SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND INSTSALLED NEW FITTING IAW DAC DWG 3750727 AND SRM 51-1-20D. 2L74 4F RT4A25 19951117003161995111700316WP 1995 11 17 UPS805006 119951110A5712 TIE RIB DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING INBD TIE RIB, 1ST RIB OTBD OF THE WHEEL WELL IS CRACKED. REPAIRED CRACK IAW SRM 51-1-2. 2L74 4F RT4A25 19951117003171995111700317WP 1995 11 17 UPS805007 119951110A5313 STRINGER DOUG DC8 DC871F 302199DWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CRACK INDICATION NOTED ON STRINGER 63, AFT FLANGE AT 4TH FASTENER OUTBOARD OF RT PYLON WING INTERSECTION OUTBOARD BRACKET. CRACK EXTENDS FROM FASTENER HOLE EDGE TO THE EDGE OF STRINGER. CUT OUT DAMAGED AREA PER SRM 57-2-2 FIG 3E, FABRICATED AND INSTALLED SECTION STRINGER 63 FROM XRS 378 TO XRS 420 AND TWO SPLICES PER SRM 57-2-2. 2L74 4F RT4A25 19951117003181995111700318EU 1995 11 17 WWMA9500082 119951110A2530180140R HOT CONTAINER SAAB SF340 340B 7860101EU GALLEY DEFECTIVE A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15320AE 340B320 THE FLIGHT CREW REPORTED, THAT THE NR 2 HOT WATER CONTAINER SMELLS LIKE BURNING PLASTIC WHEN HEATED. ALSO, THAT THE ODOR ORIGINATED FROM THE PLUG IN CONNECTION ON THE BACK OF THE CONTAINER. MAINTENANCE INSPECTED THE AIRFRAME HOT WATER CONTAINER SOCKET, NO DISCREPANCIES FOUND. THE CONTAINER WAS REMOVED FROM THE AIRCRAFT WITH NO FURTHER PROBLEMS NOTED. 2L72 4T RTA52EU 19951117003581995111700358WP 1995 11 17 9517849155 119951112A3350 BATTERY PACK DOUG DC9 DC914 3022034WP RT OVERWING DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018914E 45831 DURING LINE CHECK, THE RIGHT OVERWING EXIT AND RIGHT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003591995111700359WP 1995 11 17 9517859301 119951112A3350 BATTERY PACK DOUG DC9 DC982 3022082WP TAIL COMPT DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01301RC 48054 DURING LINE CHECK, FOUND EMERGENCY LIGHTS OVER CATWALK IN TAIL COMPARTMENT INOPERATIVE. REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003601995111700360WP 1995 11 17 9517869301 119951112A3350 BATTERY PACK DOUG DC9 DC982 3022082WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01301RC 48054 DURING LINE CHECK, FOUND EMERGENCY SLIDE LIGHT IN TAILCONE INOPERATIVE. REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003611995111700361WP 1995 11 17 9517879851 119951111A3350 BATTERY PACK DOUG DC9 DC951 3022051WP AFT OVERWING DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01760NC 47708 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003621995111700362 1995 11 17 9517889938 419951112A3417 ADC DOUG DC9 DC931 3022065WP E/E COMPT FAILED A ANWAAA UNSCHED LANDING JG WARNING INDICATION MULTIPLE FAILURE CLCLIMB 1 GL011798U 47369 DURING CLIMB, THE ALTIMETER AND BOTH THE NR 1 AND NR 2 ATC TRANSPONDERS FAILED AND THE AUTOPILOT WOULD NOT ENGAGE. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE AIR DATA COMPUTER AND THE NR 2 ATC TRANSPONDER, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003631995111700363WP 1995 11 17 9517899178 119951111A3231 DOOR LATCH DOUG DC9 DC914 3022034WP LT MLG DOOR OUT OF ADJUST A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL013310N 45705 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED THE LANDING GEAR AND LIGHT EXTINGUISHED. THE AIRCRAFT CONTINUED TO CMH AND LANDED WITHOUT INCIDENT. ADJUSTED THE SPRING TENSION ON THE LEFT MAIN LANDING GEAR DOOR LATCH ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003641995111700364WP 1995 11 17 9517909906 119951108A5350 GUIDE PINS DOUG DC9 DC931 3022065WP TAILCONE WORN A NWAAK NONE O OTHER ININSP/MAINT 1 GL01956N 47252 DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE. ALSO, FOUND 5 WORN GUIDE PINS. REPLACED THE PINS AND ADJUSTED THE PULL FORCE. 2L72 4F A6WE 19951117003651995111700365EU 1995 11 17 9517913222 119951109A3350321430 BATTERY PACK AIRBUS320 A320211 3930320EU CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01322US 263 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS BATTERY TEST FAILED EMER L AND EMER R POSITIONS. REPLACED THE BATTERY PACKS AT FORWARD LEFT AND MIDDLE LEFT POSITIONS. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951117003661995111700366EU 1995 11 17 9517923215 119951112A2410740119D IDG AIRBUS320 A320211 3930320EU NR 2 ENGINE FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01315US9507 171 DURING CLIMBOUT, RECEIVED NR 2 ENGINE IDG FAULT ACCOMPANIED WITH THE GENERATOR DROPPING OFF LINE. CREW DISCONNECTED NR 2 IDG PER COCKPIT OPERATING MANUAL PROCEDURE. DUE TO THE APU PREVIOUSLY ON MEL, RETURNED TO SEA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG, OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951117003671995111700367NM 1995 11 17 9517932287 119951112A3350 BULB BOEING727 727251 138408HNM RT HORIZ FAILED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01287US 21375 DURING LINE CHECK, FOUND THE RIGHT FORWARD HORIZONTAL OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULB, CHECKED OK. 2L73 4F A3WE 19951117003681995111700368WP 1995 11 17 9517949942 119951113A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL013991C 47175 DURING LINE CHECK, FOUND THE FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED FOUR BATTERY PACKS, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117003691995111700369NM 1995 11 17 95FDEA01600 119951018A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 CORROSION ON TOP AND BOTTOM OF UPPER FLANGE OF FLOORBEAM STA 480 LBL 24 RBL 24 IN UPPER LOBE. REMOVED CORROSION AND INSTALLED REPAIR IAW 53-10-8 AND EA 7-5310-2595. 2L73 4F A3WE 19951117003701995111700370NM 1995 11 17 95FDEA01717 119951018A5341 PIN BOEING727 72725C 138400HNM LT SPAR/BODY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 LT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN. 2L73 4F A3WE 19951117003711995111700371NM 1995 11 17 95FDEA01718 119951018A5341 PIN BOEING727 72725C 138400HNM LT SPAR/BODY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 LT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN. 2L73 4F A3WE 19951117003721995111700372NM 1995 11 17 95FDEA01719 119951018A2810 TANK BOEING727 72725C 138400HNM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 CTR FUEL TANK NR 3 BAY RIVET HEAD POPPED AND WEB BULGING AT STA 870, APPROX RBL 12 AT UPPER REAR CHORD ANGLE. INSTALLED REPAIR PER ESO 11782 DATED 10-12-95 AND INSPECTED RBL 12 STA 870 REPAIR IAW ESO 11782 AND REPAIRED PER EA 7-5710-25953. 2L73 4F A3WE 19951117003731995111700373NM 1995 11 17 95FDEA01720 119951017A5741 PIN BOEING727 72725C 138400HNM RT SPAR/BODY CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 R/W REAR SPAR TO BODY FITTING PIN CORRODED. REMOVED RUSTED CORRODED BODY FITTING PIN. INSTALLED NEW R/W REAR TO BODY FITTING PIN MM 57-41-1. 2L73 4F A3WE 19951117003741995111700374NM 1995 11 17 95FDEA01721 119951019A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 920 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 STA 920 FLOORBEAM IN UPPER LOBE, LOWER FLANGE CHIPPED OUT AT FASTENER HOLE RBL 28. REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER ESO 11782 DATED 10-13-95 AND EA 7-5310-25946. 2L73 4F A3WE 19951117003751995111700375NM 1995 11 17 95FDEA01722 119951113A5315 FLOORBEAM BOEING727 72725C 138400HNM BS 380 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 STA 380 FLOORBEAM FOUND TO BE TOO THIN AFTER CORROSION REWORK AT APPROX LBL 54 UPPER AFT FLANGE. REPAIRED FLOORBEAM PER EA 7-5310-25983 DATED 10-26-95. 2L73 4F A3WE 19951117003761995111700376NM 1995 11 17 95FDEA01723 119951109A5743651621813 TRUNNION BOEING727 72725C 138400HNM FS 740 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 L/W FRONT SPAR BOTTLE BOLT TRUNNION FS 740 CRACKED INSIDE PIN HOLE, 3 PLACES. REMOVED AND REPLACED TRUNNION IAW BOEING DRAWING NR 65C29064. 2L73 4F A3WE 19951117003771995111700377NM 1995 11 17 95FDEA01724 119951114A5312655860863 BLKHD ANGLE BOEING727 727227 1384078NM BS 400 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39 WL 155. CORROSION OUT OF LIMIT ON BULKHEAD SUPPORT ANGLE AT BS 480 RBL 24 TO 39. ROBBED SERVICEABLE BULKHEAD SUPPORT FROM N489FE AND REMOVED AND REPLACED SERVICEABLE BULKHEAD SUPPORT. 2L73 4F A3WE 19951117003781995111700378NM 1995 11 17 95FDEA01725 119951114A53126557172113 BLKHD ANGLE BOEING727 727227 1384078NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-2), ON BULKHEAD SUPPORT ANGLE AROUND NUTPLATE HOLES BS 720D LBL 28 WL 156. CORROSION WAS FOUND TO BE OUT LIMITS. REMOVED BULKHEAD SUPPORT AND INSTALLED NEW BULKHEAD SUPPORT ANGLE AT BS 720D LBL 28 WL 156. 2L73 4F A3WE 19951117003791995111700379NM 1995 11 17 95FDEA01726 119951113A5311 FRAME BOEING727 727227 1384078NM BS 1039 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 IN THE AFT CARGO BAY THE FRAME IS DENTED AT STA 1039 BETWEEN STR 25 TO 26L. REPAIRED FRAME AT BS 1030 BETWEEN STR 25 TO 26L PER FEDEX SRM STR 40-3. ALODINED, PRIMED AND PAINTED, REPAIR DOUBLER FRAME WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. 2L73 4F A3WE 19951117003801995111700380NM 1995 11 17 95FDEA01727 119951114A5311 FRAME BOEING727 727227 1384078NM BS 1090 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 PUNCTURED FRAME BS 1090 STR 7L WL 281. REPAIRED DAMAGED FRAME AT BS 1090 STR 7L WL 281 PER FEDEX SRM 53-10-4 FIG 2. 2L73 4F A3WE 19951117003811995111700381NM 1995 11 17 95FDEA01728 119951114A5320BACN103R3F SUPPORT BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1) ON UNDERSIDE OF FLOOR TO SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. CORROSION REMOVED AROUND NUTPLATES ON SIDEWALL SUPPORT PLATE BS 720D TO BS 720C, LBL 25, WL 155. IN FOUR PLACES, 1.50 INCH BY 1.50 INCH BY .004 INCH FROM ORGINAL THICKNESS OF .063 INCH, FOUND TO BE WITHIN LIMITS. CLEANED AND TREATED PER SRM 51-10. 2L73 4F A3WE 19951117003821995111700382NM 1995 11 17 95FDEA01729 119951114A5314125A16661560242 KEEL BEAM BOEING727 727227 1384078NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 POSSIBLE CRACK FOUND ON SIDE OF RT KEEL BEAM APPROX 2 INCHES LONG AT BS 950E PLUS 3 STR 29R WL 145. REPAIRED CRACKED KEEL BEAM AFT CARGO BAY BS 950E PLUS 3 STR 29R WL 145 PER PER EA 7-5310-26741. 2L73 4F A3WE 19951117003831995111700383NM 1995 11 17 95FDEA01730 119951114A5313 STRINGER BOEING727 727227 1384078NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-3), ON STR AT BS 950F PLUS 10, STR 28L, WHILE WORKING ON NR 0208. 2L73 4F A3WE 19951117003841995111700384NM 1995 11 17 95FDEA01731 119951114A5751 SKIN BOEING727 727227 1384078NM LT AILERON DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 DENT ON I/B UPPER SURFACE OF LEFT WING I/B AILERON. REMOVED, REPAIRED AND REINSTALLED SERVICEABLE LEFT WING I/B AILERON IAW FEDEX MM 27-10-1, FUNCTIONAL TESTED IAW FEDEX MM 27-10-00. 2L73 4F A3WE 19951117003851995111700385NM 1995 11 17 95FDEA01732 119951114A5330 SKIN BOEING727 727227 1384078NM BS 700 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-2), ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R FOUND ON INNER SURFACE WHILE WORKING NR0235. CORROSION ON SKIN AT BS 700 WL 145 RBL 8 O/B OF STR 28R WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED DAMAGED AREA, FABRICATED DOUBLER, CLEANED, TREATED AND INSTALLED PER FEDEX 53-30-3. 2L73 4F A3WE 19951117003861995111700386NM 1995 11 17 95FDEA01733 119951114A5320NAS1329A3130 FLOOR SUPPORT BOEING727 727227 1384078NM BS 480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED CORROSION ON UNDERSIDE OF FLOOR SUPPORT AROUND RIVNUT BS 480 WL 155 LBL 13.5. REMOVED .003 INCH BY 1 INCH BY 1.125 INCH FROM ORIGINAL THICKNESS OF .071. FOUND TO BE WITHIN LIMIT PER FEDEX SRM 53-10-1, ALODINED AND PRIMED. 2L73 4F A3WE 19951117003871995111700387NM 1995 11 17 95FDEA01734 119951113A5313 STRINGER BOEING727 727225 1384077NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON STR AT BS 720 PLUS 10 STR 27R, INSIDE BAY. 2L73 4F A3WE 19951117003881995111700388NM 1995 11 17 95FDEA01735 119951114A5313 STRINGER BOEING727 727227 1384078NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (53-111-01-1), ON STR AT BS 720 A PLUS 10 STR 27R, INSIDE BAY. REMOVED CORROSION 1.5 INCH BY 1.5 INCH BY .011 INCH DEEP AT BS 720A PLUS 2 TO 720A PLUS 17 STR 27R, ORIGINAL THICKNESS .084. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANED AND TREATED. 2L73 4F A3WE 19951117003891995111700389NM 1995 11 17 95FDEA01736 119951113A2810 FUEL CELL SKIN BOEING727 72722 1384002NM BS 870 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR O494, FOUND CORROSION ON TOP SIDE OF LOWER FUEL CELL SKIN RBL 41 WL 162.5 BS 870. REMOVED CORROSION FROM TOP SIDE OF LOWER FUEL CELL SKIN RBL 41 WL 162.5 BS 870. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 51-30-1 AND REPAIRED PER EA 7-5730-26153. 2L73 4F A3WE 19951117003901995111700390NM 1995 11 17 95FDEA01737 119951113A5320 SHEAR TIE BOEING727 72722 1384002NM BS 1130 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE WORKING NR 0349, FOUND SHEAR TIE AT BS 1130 RBL 2 WL 148.5 TO BE CRACKED AND CORRODED. REMOVED CRACKED AND CORRODED SHEAR TIE FLANGE ANGLE AT BS 1130 RBL 2 WL 148.5, FABRICATED AND INSTALLED TWO REPAIR ANGLES AND ONE SUPPORT CLIP. ALL WORK ACCOMPLISHED PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19951117003911995111700391NM 1995 11 17 95FDEA01738 119951113A5315652082726 FLOORBEAM BOEING727 72722 1384002NM BS 540 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION ON FLOORBEAM LOWER CHORD BS 540 WL 200 LBL 22 TO RBL 22 WILL REQUIRE REMOVAL OF DOOR LATCH WEB. MECH REMOVED CORROSION FROM LOWER CHORD OF FLOORBEAM BS 540 RBL 22 TO LBL 22 WL 200 MATERIAL LOSS IS BEYOND LIMITS IAW FEDEX SRM 53-10-1 AT RBL 9 AND RBL 19.5. CUT OUT EFFECTED AREAS 1 INCH BY 2 INCH AND REPAIRED IAW FEDEX SRM 53-10-8 FIG 8. 2L73 4F A3WE 19951117003921995111700392NM 1995 11 17 95FDEA01739 119951113A5313 STRINGER BOEING727 72722 1384002NM BS 1050 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 IN THE AFT GALLEY AT BS 1050 LBL 60 WL 176, THERE IS A CRACK IN THE LOWER FLANGE OF STR 21 UNDER THE FAIL-SAFE CHORD. REPAIRED CRACKED STR AT BS 1050 LBL 60 WL 176 ON LOWER FLANGE OF STR 21L PER FEDEX SRM 53-10-3 FIG 1 AND FAIL-SAFE CHORD PER FEDEX SRM 51-40-4 FIG 2, WHICH WAS REMOVED TO GAIN ACCESS TO DAMAGED AREA ON STR 21L. 2L73 4F A3WE 19951117003931995111700393NM 1995 11 17 95FDEA01740 119951111A5320 LWR CHORD BOEING727 72722 1384002NM BS 1030 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01-3), IN THE AFT BAY AT BS 1030 WL 200 FROM LBL 20 TO RBL 14, THERE IS CORROSION IN THE NUTPLATE HOLES. REMOVED CORROSION, FABRICATED NEW REPAIR ANGLE AND INSTALLED FASTENERS. ALL WORK DONE IAW FEDEX EA 7-5310-26152. 2L73 4F A3WE 19951117003941995111700394NM 1995 11 17 95FDEA01741 119951113A5315 FLOORBEAM BOEING727 72722 1384002NM BS 1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01-3), ON LOWER FLANGE OF FLOORBEAM BS 1110 RBL 28 TO LBL 31 WL 200. REMOVED AND REPLACED ENTIRE LWR CHORD OF THE BS 1110 FLOORBEAM PER FEDEX EA 7-5310-20796. 2L73 4F A3WE 19951117003951995111700395NM 1995 11 17 95FDEA01742 119951113A5320652073215 CHANNEL BOEING727 72722 1384002NM BS 1058-1110 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-111-01, 3) ON SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5. REMOVED AND REPLACED SUB-THRESHOLD SUPPORT CHANNEL FROM BS 1058 TO 1110 RBL 27.5 WL 150.5, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01. 2L73 4F A3WE 19951117003961995111700396NM 1995 11 17 95FDEA01743 119951111A5313 STRINGER BOEING727 72722 1384002NM BS 1140 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE INSTALLING FASTENERS IN BELLY SKIN DISCOVERED CHIPPED OUT AREA ON STR 27R BS 1140 RBL 21 WL 153. REPAIRED DAMAGED AREA ON STR 27R AT BS 1140 RBL 21 WL 153 PER FEDEX EA 7-5310-28199. 2L73 4F A3WE 19951117003971995111700397NM 1995 11 17 95FDEA01744 119951114A5320 WEB BOEING727 72722 1384002NM BS 870 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE REMOVING BS 870 LOWER WING CHORD, FOUND BS 870 WEB TO BE SEVERELY CORRODED. 2L73 4F A3WE 19951117003981995111700398NM 1995 11 17 95FDEA01745 119951113A5313 STRINGER BOEING727 72722 1384002NM BS 1140 CHIPPED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 WHILE INSTALLING FASTENERS IN BELLY SKIN DISCOVERED CHIPPED OUT AREA ON STR 27R AT BS 1140 RBL 21 WL 153. 2L73 4F A3WE 19951117003991995111700399NM 1995 11 17 95FDEA01746 119951114A5313 STRINGER BOEING727 727227 1384078NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON STR 27R AT BS 720B PLUS 10, INSIDE BAY. REMOVED CORROSION 1 INCH BY 2 INCH BY .005 INCH DEEP AT BS 720 PLUS 10 STR 27R, ORIGINAL THICKNESS 0.89. FOUND WITHIN ALLOWABLE LIMITS PER FEDEX SRM 53-10-1, CLEANED AND TREATED. 2L73 4F A3WE 19951117004001995111700400NM 1995 11 17 95FDEA01747 119951108A2432AAN7214501 SHUNT MOUNT DOUG MD11 MD11F 3023600NM LT EMER DC BUS MELTED A FDEAO OTHER L NO TEST ININSP/MAINT 1 SO25609FE 48549 EMERGENCY POWER TEST WOULD NOT PASS. FOUND BATTERY AMMETER SHUNT S4-1, MOUNT HAD MELTED WHERE SHUNT IS ATTACHED TO THE L EMERGENCY DC BUS FEED RCCB, B1-189. R EPLACED BATTERY EQUIPMENT PANEL AND F/C OK PER MM 21-34-00. ALSO, EPCU R-T-S TEST PASSED PER MM 24-08-01. 2L73 4F RTA22WE 19951117004011995111700401WP 1995 11 17 ABXA9500933 119951110A3260 UPLOCK SWITCH DOUG DC9 DC932 3022066WP NLG ICED UP A ABXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23903AX 47427 NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER RAISING GEAR ON TAKEOFF. RECYCLED GEAR, LIGHT REMAINED ON. LIGHT DID GO OUT ONCE WE SLOWED TO 170 KIAS. FOUND ICE AROUND UPLOCK SWITCH. REMOVED ICE AND ALL ICE IN NOSE WHEEL WELL AREA. LUBED NOSE GEAR, GEAR DOOR ACTUATORS AND CYCLED SEVERAL TIMES, OPS CHECKED NORMAL. CLEANED NOSE GEAR UPLATCH CONNECTOR, SWITCH OPS CHECKED NORMAL. 2L72 4F A6WE 19951117004021995111700402NM 1995 11 17 DL72E954224 119951102A5754 ANGLE BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112826W 21331 FOUND DURING A-2 LETTER CHECK, .25 INCH CRACK IN NR 7 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER MM 57-54-0 PAR 5A. 2L73 4F A3WE 19951117004031995111700403NM 1995 11 17 DL72K954217 119951101A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 FOUND ON A2 LETTER CK, .25 INCH CRACK NR 2 SLAT TAI DUCT CUTOUT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951117004041995111700404NM 1995 11 17 DL72K954218 119951101A5320 WEB BOEING727 727232 1384082NM LT TORQUE BOX CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 FOUND ON A2 LETTER CK, 1 INCH CRACK IN TORQUE BOX WEB LT SIDE FWD END ALONG UPPER ROW OF RIVETS. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951117004051995111700405NM 1995 11 17 DL72K954219 119951101A5414 SKIN BOEING727 727232 1384082NM LT ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11474DA 20751 FOUND ON A2 LETTER CK, 1 INCH CRACK AT FASTENER NUMBER 2 ENGINE INLET OUTER SKIN LT SIDE FWD OF SADDLE PANEL. REPAIRED PER MM 54-30-0. 2L73 4F A3WE 19951117004061995111700406NM 1995 11 17 DL72L954215 119951101A3350S106900835A BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11506DA 21308 MID CABIN CENTER AISLE AND RT OVERWING EMERGENCY EXIT, EMERGENCY LIGHTS INOP. REPLACED BATTERIES, OPERATION NORMAL. 2L73 4F A3WE 19951117004071995111700407NM 1995 11 17 DL72L954230 119951026A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11513DA 21315 DURING THE SHOP INITIAL INSPECTION, THE INBOARD ACTUATOR RIB WAS FOUND TO HAVE CRACKED AT THE FORWARD LOWER CORNER WHERE THE RIB ATTACHES TO THE SLAT SPAR. THE RIB WAS REPAIRED PER SRM 57-54-0 FIG 804. 2L73 4F A3WE 19951117004081995111700408NM 1995 11 17 DL72S954216 119951101A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11418DA 21271 AFT AIRSTAIR EMER LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL. 2L73 4F A3WE 19951117004091995111700409NM 1995 11 17 DL72S954220 119951102A335007912 EEL MODULE BOEING727 727232 1384082NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11520DA 21471 EMERGENCY FLOOR TRACK MISSING IN FLOOR TRACK AT SEAT 10 C. REPLACED EMERGENCY PATH LIGHT HOLDER MODULE AND BULB, OPERATION NORMAL. 2L73 4F A3WE 19951117004101995111700410NM 1995 11 17 DL72S954226 119951024A5312 BULKHEAD BOEING727 727232 1384082NM FS 870 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND AT HMV, FS 870 BULKHEAD CRACKED AT APU BLEED AIR DUCT CUTOUT AT LWR O/B CORNER. REPAIRED PER SRM 53-10-9. 2L73 4F A3WE 19951117004111995111700411NM 1995 11 17 DL72S954227 119951023A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND AT HMV, STRINGER 11L CRACKED AT STA 1342 INSIDE VERT STAB. REPAIRED PER MM 53-30-0 PG 803. 2L73 4F A3WE 19951117004121995111700412NM 1995 11 17 DL72S954228 119951023A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND AT HMV, STRINGER 8R CRACKED IN VERTICAL STAB INTERIOR IN 2ND BAY DOWN. REPAIRED PER MM 55-30-0 PG 803. 2L73 4F A3WE 19951117004131995111700413NM 1995 11 17 DL72S954232 119950906A5754651622373 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING A ROUTINE SHOP INSPECTION, NR CARD 8598 WAS WRITTEN FOR A CRACK IN THE 15TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19951117004141995111700414NM 1995 11 17 DL72S954233 119950906A5754651622373 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING A ROUTING SHOP INSPECTION, NR 8598 WAS WRITTEN FOR A CRACK IN THE 17TH RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819. 2L73 4F A3WE 19951117004151995111700415NM 1995 11 17 DL72S954234 119950906A5754651622373 RIB BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11401DA 21145 DURING A ROUTINE SHOP INSPECTION, NR 8596 WAS WRITTEN FOR A CRACK IN THE 3RD RIB FROM I/B EDGE OF THE NR 2 SLAT. THE CRACK WAS REPAIRED PER M/M 57-54-0 FIG 819. 2L73 4F A3WE 19951117004161995111700416NM 1995 11 17 DL72S954253 119951027A5753652163261 CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING SHOP VISIT, A CRACK AND TEMPORARY REPAIR DOUBLER WAS FOUND ON AFT CHORD OF NR 2 MIDFLAP. INSTALLED PERMANENT REPAIR PER MM 57-53-0. 2L73 4F A3WE 19951117004171995111700417NM 1995 11 17 DL72S954254 119951019A5753652163261 CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11544DA 22493 DURING SHOP VISIT, A CRACK WAS DISCOVERED ON AFT CHORD AT I/B DRIVE ROD CUTOUT, OF NR 2 MIDFLAP. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19951117004181995111700418NM 1995 11 17 DL72W954221 119951102A5755651734874 SKIN BOEING727 727247 138408FNM RT SPOILER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 SPOILER WAS DENTED ON UPPER SKIN SURFACE APPROX 8 INCHES FROM L/E AND 6 INCHES FROM I/B EDGE. REPAIRED PER MM 57-50-6. 2L73 4F A3WE 19951117004191995111700419NM 1995 11 17 DL72W954236 119951103A3350BR9279108 EEL SIGN BOEING727 727247 138408FNM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO112825W 21330 ON S/C, FOUND L-1 EMERGENCY LIGHT BASE CRACKED. REPLACED L-1 EMERGENCY LIGHT ASSEMBLY, CHECKS GOOD. 2L73 4F A3WE 19951117004201995111700420NM 1995 11 17 DL72W954239 119951020A5320 DOUBLER BOEING727 727247 138408FNM R1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING HMV, INSP FOUND FUS EXT SKIN DOUBLER CRACKED AT FWD UPPER CUTOUT RADIUS FOR R-1 DOOR UPPER HINGE. HFEC VERIFIED AND MARKED END OF CRACK, REMOVED DOUBLER. HFEC HOLES CRACK END AT FASTENER HOLE, LOC A PER 53-30-0. MANUFACTURED DOUBLER PER M/M 53-30-0, INSTALLED REAIRS. 2L73 4F A3WE 19951117004211995111700421NM 1995 11 17 DL72W954240 119951102A5713 STRINGER BOEING727 727247 138408FNM WS 629 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV INSPECTION, HFEC INSP OF WS 629.00 STR NR 9 HAS A CRACK EXITING FASTENER HOLE AWAY FROM RADIUS. DRILLED REPAIR ANGLE PER M/M 57-13-0, INSTALLED REPAIR. 2L73 4F A3WE 19951117004221995111700422NM 1995 11 17 DL72W954241 119951104A2750 VALVE 65404494 BOEING727 727247 138408FNM FLAP CONTROL LEAKING A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 SO11291WA DBP36079 22109 ON TAKEOFF, A-SYSTEM HYD QTY AND PRESS WENT TO ZERO. FOUND OUTBD FLAP CONTROL VALVE LEAKING. REPLACED SAME, NOW CKS OK. CHECKED FILTERS FOR METAL, NONE FOUND AND AC OK FOR SERVICE. 2L73 4F A3WE 19951117004231995111700423NM 1995 11 17 DL72W954371 119951109A3350 BATTERY BOEING727 727247 138408FNM AFT FUSELAGE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11293WA 22111 FOUND EXTERIOR OVERWING EMERGENCY LIGHTS, AFT CARGO DOOR AND LEFT FUSELAGE INOP. RELAMPED AND REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19951117004241995111700424NM 1995 11 17 DL73E954357 119951112A3350BPS73 EEL POWER SUPPLY BOEING737 737247 138448DNM L1 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11245WA 23519 L1 DOOR EMERGENCY SLIDE LIGHT IS DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK, CHECKS OK. 2L72 4F A16WE 19951117004251995111700425NM 1995 11 17 DL73E954358 119951112A3350BPS73 EEL POWER SUPPLY BOEING737 737247 138448DNM R1 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11245WA 23519 R1 DOOR EMERGENCY SLIDE LIGHT IS OUT. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2L72 4F A16WE 19951117004261995111700426NM 1995 11 17 DL73S954360 119951112A2560 MEGAPHONE BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE O OTHER ININSP/MAINT 1 SO11326DL 23098 ON 7802L, FOUND F/C GALLEY MEGAPHONE WOULD NOT PROJECT VOICE WHEN THE BUTTON ON THE HANDLE WAS PUSHED. TRIED CHANGING THE BATTERIES, NO HELP. REPLACED MEGAPHONE. 2L72 4F RTA16WE 19951117004271995111700427NM 1995 11 17 DL757954157 119951101A3350 EEL WIRE BOEING757 757232 1384965NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO11669DN 25142 EMERGENCY TRACK LIGHT AT 3A AND 44C HAS A BROKEN WIRE. REPAIRED WIRES, OPERATION NORMAL. 2L72 4F RTA2NM 19951117004281995111700428NM 1995 11 17 DL757954223 119951102A3350 EEL TRACK 0816302750 BOEING757 757232 1384965NM CABIN CRACKED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11606DL 22813 DURING INSPECTION, FOUND EMERGENCY PATH LIGHT TRACK CRACKED JUST INBOARD OF AFT LAVATORY. REPLACED SECTION OF TRACK LIGHT, OPERATION NORMAL. 2L72 4F RTA2NM 19951117004291995111700429NM 1995 11 17 DL757954372 119951110A3350 EEL POWER SUPPLY BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11607DL 22814 DURING INSPECTION, FOUND FWD CABIN EMERGENCY TRACK LIGHT INOP. REPLACED F/C EMERGENCY LIGHT POWER PACK. FOUND BROKEN GROUND STUD IN OVERHEAD INSTALLATION. REPLACED GROUND STUD, OPS NORMAL. 2L72 4F RTA2NM 19951117004301995111700430NM 1995 11 17 DL76E954321 119950522A7830315T472571 THRUST REVERSER BOEING767 767232 1385132NM NR 1 ENGINE DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO11111DN 22223 NUMBER ONE ENGINE LEFT THRUST REVERSER ASSEMBLY INNER WALL HAD EXISTING SRM REPAIRS AND ADDITIONAL DELAMINATION. ALSO, UPPER BEAM HAD EXISTING SRM REPAIR AND ADDITIONAL DELAMINATION. COMPONENT WAS REPAIRED PER ER/A 276777-14. REPAIR CONSISTED OF REPLACING FACE SHEETS AND REBONDING. RETURNED TO SERVICE 11-10-95. 2L72 4F RTA1NM 19951117004311995111700431NM 1995 11 17 DL76L954186 119951101A2797 WIRE BOEING767 767332 1382001NM AIL LOCK ACT BROKEN A DALAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO11183DN 27110 AILERON LOCKOUT MSG ON EICAS, DIVERTED CVG. FOUND BROKEN WIRE ON CANNON PLUG FOR RT AILERON LOCK ACTUATOR. REPAIRED WIRE, OPERATION NORMAL. 2L72 4F RTA1NM 19951117004321995111700432NE 1995 11 17 DL76L954369 219951110A7530 VSV GUIDE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENGINE MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11176DN15241 25061 724158 DURING INSPECTION, FOUND NR 1 ENGINE VARIABLE STATOR VANES RING GUIDE BLOCKS MISSING IN SEVERAL LOCATION AND LOOSE IN OTHERS. REPLACED NR 1 ENG AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19951117004331995111700433NM 1995 11 17 DL76P954222 119951102A2121 COOLING FAN 732591D BOEING767 767332 1382001NM E/E BAY FAILED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11140LL 3094 25988 ON CLIMBOUT, HAD ELECTRICAL BURNING SMELL IN COCKPIT AND FWD EQUIPMENT COOLING FAN C/B TRIPPED, RETURNED JAX. REPLACED COOLING FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19951117004341995111700434NM 1995 11 17 DL76S954237 119951103A3350 EEL BOEING767 767332 1382001NM LEFT WING INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11120DL11051 23279 LEFT WING LWR AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK. 2L72 4F RTA1NM 19951117004351995111700435WP 1995 11 17 DLL10954187 119951003A53121554952102 BLKHD FITTING LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11725DA 193C1162 DURING THE INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS, STR 10 WAS FOUND TO BE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 271858-14AD. 2L73 4F A23WE 19951117004361995111700436WP 1995 11 17 DLL10954199 119951030A57201503213 STIFFENER LKHEED1011 10113851 5265010WP RBL 22.5 LBL 10 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11714DA 193C1090 THE INSPECTION BY EO 7-39578-3, FOUND CRACKS IN THE VERTICAL STIFFENERS AT RBL 22.5 AND LBL 10. THE RBL 22.5 STIFFENER HAD ITS UPPER LIGHTENING HOLE DAMAGED AND THE REPAIR STRAP ON THE FWD SIDE OF THE LBL 10 STIFFENER WAS FOUND CRACKED. REPAIRED PER DL ERA 236746-14AD. 2L73 4F A23WE 19951117004371995111700437WP 1995 11 17 DLL10954202 119950905A5712 RIB LKHEED1011 10113851 5265010WP WS 503 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11714DA 193C1090 DURING THE COMPLETION OF SI 7-59208-2AD ON THE LT WING, A CRACK WAS FOUND ON A CASTELLATION OF THE IWS 503 UPPER RIB CAP. THE CRACK IS BETWEEN STR 18 AND 19 AND IS 1.0625 INCH LONG. ACCOMPLISHED REPAIRS PER DL ERA 271804-14AD. 2L73 4F A23WE 19951117004381995111700438WP 1995 11 17 DLL10954209 119951030A53301503542107 SKIN LKHEED1011 10113851 5265010WP BS 1575 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11727DA 193C1167 THE FUSELAGE SKIN AT STA 1575 AND STR 38 WAS FOUND TO HAVE CORROSION DAMAGE UNDER THE FAIL-SAFE STRAP. ACCOMPLISHED REPAIRS PER DL ERA 265143-14. 2L73 4F A23WE 19951117004391995111700439NE 1995 11 17 DLL10954341 219951111A7261 ENGINE LKHEED1011 10113851 5265010WP RROYCERB211 RB21122B02 54555NE NR 3 OIL LEAK A ADALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 SO11717DA52011 193C1096 010382 SMOKE IN CABIN, ALL SMOKE ALARMS WENT OFF. THE NR 3 ISOL VLV UNLATCHED SEEMED TO HELP SOME, BUT NOT COMPLETELY. FWD TO MCO PER MEL 36-11-18. SUBSEQUENTLY NR 3 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR OIL LEAK IN COMPRESSOR. 2L73 4F4 F A23WE E12EU 19951117004401995111700440WP 1995 11 17 DLL13954200 119950830A53121554947102 BLKHD FITTINGS LKHEED1011 10113851 5265010WP AFT PRESS BLKHD CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 DURING THE ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STRINGER SPLICE FITTINGS PER SI 7-66332-12, THE STR 11 FITTING WAS FOUND TO HAVE CRACKS, IT IS 7075-T6 FORGED AL. ACCOMPLISHED REPAIRS PER DL ERA 271759-14AD. 2L73 4F A23WE 19951117004411995111700441WP 1995 11 17 DLL13954210 119950526A5712 RIB LKHEED1011 10113851 5265010WP WS 346 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11784DA 193A1038 DURING THE COMPLETION OF EO 7-56199-3AD, THE RT IWS 346 MLG ATTACH RIB UPPER I/B 1.125 HOLE WAS FOUND WITH CORROSION IN THE HOLE BORE. REPAIRED PER DL ERA 270991-14AD. 2L73 4F A23WE 19951117004421995111700442WP 1995 11 17 DLL13954242 119951103A32401535930109 BRAKES LKHEED1011 10113851 5265010WP RT MLG SEIZED A ADALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO11784DA 193A1038 AFTER START BRAKES REMAINED LOCKED, ALTHOUGH HANDLE RELEASED AND LIGHT WENT OUT. FOUND NR 3 FRONT BRAKE ASSY FROZEN ON AXLE. REPLACED RT FWD MAIN GEAR AXLE, BRAKE AND WHEEL ASSY. WHEEL BEARING FAILED, DAMAGED AND CUT INTO AXLE. 2L73 4F A23WE 19951117004431995111700443 1995 11 17 DLL14954317 419951110A2220 MACH FEEL LKHEED1011 1011385115 5265015WP NR 1/2 MOTORS FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO111739D 193C1237 CLIMBING THROUGH 14,000 FT, PITCH TRIM NR 2 FAIL LIGHT ILLUMINATED. SHORTLY THEREAFTER MACH FEEL NR 1 AND 2 ILLUMINATED. PITCH TRIM RESET OK, UNABLE TO RESET MACH FEEL, RETURNED JFK. REPLACED NR 1 AND NR 2 MACH FEEL SCHEDULE MOTORS, PERFORMED MACH FEEL SCHEDULE MOTORS ADJ AND TEST PER MM 22-21-20 PG 501-504, OPERATION NORMAL. 2L73 4F A23WE 19951117004441995111700444WP 1995 11 17 DLL15954342 119951111A2420 HARNESS LKHEED1011 10113853 5265020WP NR 2 GCU SHORTED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11753DA 193W1189 14865 NR 2 GEN DISCONNECTED FROM BUS WOULD NOT RESET, VOLTS AND FREQS NORMAL, DIVERTED JFK. FOUND PIN 55 ON B1A GCU RACK CONNECTOR PUSHED BACK AND FOUND PIN 43 ON J1B SHORTED TO GROUND. REPLACED NR 2 GCU RACK HARNESS, RAN ENGINES AND ALL CHECKS GOOD. 2L73 4F A23WE 19951117004451995111700445WP 1995 11 17 DLL16954356 119951112A2130 CONTROLLER ED7244366 LKHEED1011 10113853 5265020WP CABIN FAILED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO11763DL AA1788 193Y1197 PASSING 17,000 FT, UNABLE TO MAINTAIN CABIN PRESSURE. WENT TO MANUAL WITH AFT OUTFLOW VALVE TO REGAIN CONTROL. REPLACED CABIN PRESSURE CONTROLLER, BITE CK OK. 2L73 4F A23WE 19951117004461995111700446WP 1995 11 17 DLL17954188 119951003A53201503812 ANGLE LKHEED1011 10113853 5265020WP FS 1203 OVERSIZED HOLE A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO11765DA 193H1206 DURING REMOVAL OF EXISTING FASTENERS AT RT 1203, THE UPPER FWD HOLE COMMON TO THE VERTICAL LEG OF THE FAIL-SAFE ANGLE, SKIN PANEL, FRAME FITTING, AND OVERWING TITANIUM TEE WAS OPENED TO .438. REPAIR APPROVAL PER DL ERA 271858-14AD. 2L73 4F A23WE 19951117004471995111700447NM 1995 11 17 DLM11954170 119951101A3350 EEL MODULE 250205239 DOUG MD11 MD11 3023602NM 1L CABIN DOOR INOP A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO11805DE 48476 2R DOOR SLIDE LIGHT INOP. REPLACED LIGHT MODULE, OPERATION NORMAL. 2L73 4F RTA22WE 19951117004481995111700448NM 1995 11 17 DLM11954175 119951101A3350 BATTERY DOUG MD11 MD11 3023602NM 2R CABIN DOOR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11805DE 48476 2R DOOR SLIDE LIGHT INOP. INSTALLED BATTERIES IN CORRECT POSITION, OPERATION NORMAL. 2L73 4F RTA22WE 19951117004491995111700449NM 1995 11 17 DLM88954207 119950906A5330 SKIN DOUG MD88 MD88 3023688NM FS 237 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11913DE 49956 THE FUSELAGE SKIN NEAR FS 237, BELOW THE CUSP AT S-18L WAS BADLY DENTED BETWEEN S-18L AND 20L. ACCOMPLISHED REPAIRS PER DL ERA 271814-14. 2L72 4F RTA6WE 19951117004501995111700450NM 1995 11 17 DLM88954212 119950906A533059360043 SKIN DOUG MD88 MD88 3023688NM BS 598 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11975DL 53243 THE INNER SURFACE OF THE FUSELAGE SKIN AT STA 598 AND STR 29R WAS FOUND CORRODED BETWEEN THE UNDERLYING C2 DOOR CUTOUT DOUBLER. ACCOMPLISHED REPAIRS PER DL 271817-14. 2L72 4F RTA6WE 19951117004511995111700451NM 1995 11 17 DLM88954366 119951112A3350 EEL FUSE 276005 DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11903DL 49534 NO FLOOR PROXIMITY EMERGENCY ESCAPE MARKING LIGHTS ILLUMINATED FROM ROW 29 TO REAR OF AIRCRAFT. REPLACED FUSES IN BATT RACK B5-212, OPS CHECK GOOD. 2L72 4F RTA6WE 19951117004521995111700452NM 1995 11 17 P5CA9500839 119951114A3246260356115 WHEEL BOEING747 747122 1384872NM NR 11 WHEEL FAILED A P5CAK NONE O OTHER LDLANDING 1 WP23852FT 959 19757 THE NR 11 WHEEL AND TIRE DAMAGED ON LANDING DUE TO FAILURE OF WHEEL RIM. REPLACED TRUCK BEAM ASSY DUE TO OVERHEAT OF AXLE. WHEEL AND TRUCK BEAM REPLACED IAW MM 32-13-11. TOTAL LANDINGS SINCE SHOP VISIT 211. 2L74 4F A20WE 19951117004531995111700453NE 1995 11 17 P5CA9500840 219951114A7250 T2 TURBINE BLADE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE FAILED A P5CAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 WP23831FT737792248 19648 662378 NR 1 ENGINE FL 19,000 COMPRESSOR STALL WITH EGT RISE, PRECAUTIONARY ENGINE SHUTDOWN. FOUND TWO FAILED T2 TURBINE BLADES. ENGINE TO BE REPLACED PER POLAR WORK CARDS. 2L74 4F4 F A20WE E20EA 19951117004541995111700454EU 1995 11 17 QXEA9500374 119951108A3350683 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09464US 11063 GEG - FORWARD EXIT SIGN ON FORWARD CABIN BULKHEAD INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004551995111700455SW 1995 11 17 QXEA9500375 119951109A32601EN516 DNLOCK SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A QXEAK NONE N FALSE WARNING APAPPROACH 1 NM0926877 AC652 PDX - NOSE GEAR INTRANSIT LIGHT STAYS ON TOO LONG. NOSE GEAR LEFT DOWNLOCK SWITCH REPLACED AND RIGGED I/A/W/ MAINT. MANUAL. NOSE GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951117004561995111700456EU 1995 11 17 QXEA9500376 119951109A3350MGG1280 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 SEA - EXIT SIGN IN MIDDLE OF AISLE IS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004571995111700457EU 1995 11 17 QXEA9500377 119951108A3231A11340415 BRACKET A11320440 FOKKERF28 F28MK1000 4990808EU LT MLG DOOR OUT OF ADJUST A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09466US 11075 PDX - LEFT MAIN GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION, LEFT GEAR DOOR UPLOCK BRACKET FORWARD ROLLER WAS TOO TIGHT AT FORWARD HOOK. SHIMS WERE ADDED AT FORWARD POINT ON BRACKET AND GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004581995111700458NM 1995 11 17 QXEA9500378 119951109A3350MS3474L2241P EEL CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09102AU 91 SEA - AFT OVERHEAD EMERGENCY LIGHT INOP. CANNON PLUG WAS RESEATED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951117004591995111700459NM 1995 11 17 QXEA9500379 119951110A3260 CONNECTOR DORNERDO32 DO328100 2996000NM RT MLG LOOSE A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM09332PH 3010 PDX - RIGHT MAIN GEAR INDICATION LIGHT FLICKERS AND PROXIMITY HYD CAS MESSAGE ON GEAR EXTENSION, ONLY RIGHT MAIN GEAR LIGHT FLICKERS. S12 DOWNLOCK SWITCH CANNON PLUG CLEANED AND RESEATED. GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951117004601995111700460EU 1995 11 17 QXEA9500380 119951110A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 BOI - EMERGENCY LIGHT AT ROW 8E IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004611995111700461EU 1995 11 17 QXEA9500381 119951110A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 BOI - EMERGENCY EXIT LIGHT ON FORWARD FLIGHT ATTENDANT PANEL IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004621995111700462EU 1995 11 17 QXEA9500382 119951110A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 PDX - ONE EMERGENCY LIGHT AT ROW 3 INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004631995111700463 1995 11 17 QXEA9500383 419951111A2565S130508 SLIDE FOKKERF28 F28MK1000 4990808EU GALLEY LOW PRESSURE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09801PH 11097 GEG - DURING PRE-FLIGHT, FOUND THE BOTTLE PRESSURE FOR EMERGENCY ESCAPE SLIDE WAS LOW. SLIDE ASSY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004641995111700464EU 1995 11 17 QXEA9500384 119951111A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 BOI - BOTH EMERGENCY LIGHTS FOR SLIDE ILLUMINATION ARE INOP. BULBS WERE REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004651995111700465EU 1995 11 17 QXEA9500385 119951111A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 BOI - EMERGENCY LIGHT IS INOP ON THE FORWARD FLIGHT ATTENDANT PANEL. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004661995111700466EU 1995 11 17 QXEA9500386 119951111A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 BOI - EXIT LIGHT AT ROW 8 BURNED OUT. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951117004671995111700467NM 1995 11 17 QXEA9500387 119951112A33506104781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09102AV 91 PDX - EMERGENCY LIGHTS ARE INOP. ALL BATTERY PACKS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951117004681995111700468WP 1995 11 17 SCNA95263 119951105A3233ARG70255523 RETRACT ACT DOUG DC10 DC1010 3022110WP LT MLG FAILED A ASCNAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL15907WA 46946 DURING LANDING GEAR EXTENSION A LOUD BANG WAS HEARD AND THE NUMBER 3 HYDRAULIC QUANTITY DECREASE TO ZERO. INSPECTION OF THE LEFT MAIN LANDING GEAR REVEALED THE FAILURE OF THE TWO UPPER BOLTS ATTACHING THE RETRACT CYLINDER A BRACKET TO THE AIRFRAME, ALLOWING THE GEAR TO FREE FALL INTO THE LOCKED POSITION, WHICH SEVERED THE HYDRAULIC LINES LEADING TO THE RETRACT CYLINDER CAUSING THE LOSS OF THE NUMBER 3 HYDRAULICS. REMOVED AND REPLACED THE LEFT MLG RETRACT CYLINDER AND BRACKET. MAJOR REPAIR TO FITTINGS (P/N ARB06420 AND ARG0272-1), ACCOMPLISHED PER DOUGLAS INSTRUCTIONS. 2L73 4F A22WE 19951117004691995111700469NM 1995 11 17 SCNA95264 119951112A3260656021123 ACCESSORY UNIT BOEING727 727259 138408JNM LANDING GEAR FAILED A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15289SC 22475 DURING CLIMB AFTER GEAR RETRACTION, RED AND GREEN NOSE GEAR LIGHTS ILLUMINATED. ALL INDICATIONS WERE NORMAL DURING RETRACTION AND EXTENSION. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER MM 32-09-12, OPS CHECKED GOOD PER MM 32-09-121. 2L73 4F A3WE 19951117004701995111700470NM 1995 11 17 SCNA95265 119951109A2612106087713 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A SCNAK NONE N FALSE WARNING CRCRUISE 1 GL15275AF 22092 THE NUMBER 3 ENGINE FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. THE A-CIRCUIT BREAKER WAS PULLED AND THE LIGHT EXTINGUISHED. REPOSITIONED NUMBER 3 ENGINE FIRE WARNING ELEMENT AND THE SYSTEM TESTED GOOD. 2L73 4F A3WE 19951117004711995111700471NM 1995 11 17 SCNA95266 119951109A2612876633 FIRE WIRE BOEING727 7272A1 138407FNM NR 1 ENGINE OUT OF POSITION A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15286SC 21601 DURING EN ROUTE CLIMB, THE NUMBER 1 ENGINE FIRE DETECTION LIGHT FLICKERED ON AND OFF, LASTED A FEW SECONDS THEN WENT OFF AND STAYED OFF. ALL ENGINE INDICATIONS READ NORMAL. FOUND FORWARD PLUG CONNECTOR STRAIN RELIEF RUBBING WIRE. REROUTED WIRING FOR BETTER RELIEF AND RAN ENGINE AT FULL POWER AND HALF POWER WITH NO DEFECTS NOTED. 2L73 4F A3WE 19951117004721995111700472SO 1995 11 17 SWIA95674 119951106A3610 REGULATOR VLV EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE NR 2 ENGINE MALFUNCTIONED A SWIAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 NM07220SW 120288 DUCT LEAKAGE LIGHT ILLUMINATED IN FLIGHT, PROCEEDED WITH ENGINE SHUTDOWN. FOUND GASKET NR 2 ENGINE BLOWN ON RT SIDE OF 18 PSI REGULATOR FOR DE-ICE SYSTEM. REPLACED 18 PSI REGULATOR VALVE. RAN RT ENGINE TO TAKEOFF POWER AND OPS CK GOOD. 2L72 4T4 TRTA31SO E20NE 19951117004731995111700473SW 1995 11 17 SWIA95675 119951108A2740 TRIM SWITCH SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP CONTROL WHEEL FAILED A SWIAO OTHER O OTHER DEDESCENT 1 NM072685L AC648 WITHIN 500 FT OF GROUND, FO'S TRIM FAILED. FLIPPED SWITCH BACK AND FORTH, PULLED AND RESET CB, NO GOOD. RETURNED TO SBA. CLEANED SWITCH AND OP CK GOOD. 1L72 4T4 T A8SW E4WE 19951117004741995111700474SO 1995 11 17 SWIA95676 119951109A27215298 LINEAR ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER TRIM WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07199SW 120237 RUDDER TRIM ACTUATOR CABLE WORN. REMOVED AND REPLACED RUDDER TRIM LINEAR ACTUATOR IAW EMB120 MAINTENANCE MANUAL 27-00-01 AND R2 9 REV 19 DATED 7-1-91. 2L72 4T4 TRTA31SO E20NE 19951117004751995111700475SW 1995 11 17 SWIA95677 119951110A6120 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE RPM WANDER A SWIAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM072720B AC715 LT RPM IS WANDERING UP AND DOWN 2 PERCENT MOSTLY IN DESCENT ANYTIME THERE IS A PITCH CHANGE, RPM CHANGES, OCCASIONAL VIBRATION FROM LT PROP. INSPECTED LT ENGINE RIGGING AND PERFORMED OPERATIONAL CHECK OF ENGINE ON GROUND, OPS CKS GOOD. ENGINE PERFORMING WITHIN NORMAL PARAMETERS. 1L72 4T4 T A8SW E4WE 19951117004761995111700476SW 1995 11 17 SWIA95678 119951110A5210 PRESS LINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP PAX DR SEAL LOOSE A SWIAO OTHER O OTHER CLCLIMB 1 NM0727297 AC735 AIRCRAFT WOULD NOT PRESSURIZE. FOUND MAIN CABIN DOOR SEAL LINE OFF INSIDE DOOR. REATTACHED DOOR SEAL PRESSURE LINE AT UNION. PRESSURIZED AIRCRAFT AND OPS CKS GOOD. 1L72 4T4 T A8SW E4WE 19951117004771995111700477NM 1995 11 17 UPS205011 119951111A3260 CONNECTOR BOEING727 72727C 138400JNM NLG SHORTED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01908UP 19114 CREW REPORTED ON TAKEOFF, WHEN LDG GEAR WAS RETRACTED, RED WARNING LIGHTS ILLUMINATED. RECYCLED AND DOOR WARNING LIGHT WORKED NORMAL. AMBER F/E LIGHTS OPS NORMAL. RED WARNING LIGHTS REMAINED ILLUMINATED UNTIL LANDING, WHEN GEAR WAS SELECTED DOWN, THEN THEY EXTINGUISHED UNTIL ROLL OUT, WHEN THE RUB NOSE GEAR WARNING LIGHT ILLUMINATED AND REMAINED ON. T/S WITH REF TO WDM 32-64-01 AND -02. FOUND C/P D298 PIN-C SHORTED TO GROUND. REPLACED D298, JACKED A/C AND PERFORMED EXTENSION AND RETRACTION SEVERAL TIMES. ALL GEAR POSITION INDICATING GROUND CKS GOOD AND ALL WITH REF TO M/M 07-11-00 AND 32-31-00. 2L73 4F A3WE 19951117004781995111700478NM 1995 11 17 UPS205015 119951111A3350 BATTERY BOEING727 72722C 138400FNM FLIGHT DECK MISSING A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01212UP 19092 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT IN FLIGHT DECK INOP. BATTERIES ROBBED FOR A/C 212 FROM 929. REMOVED AND REPLACED 2 BATTERIES, OPS GOOD. 2L73 4F A3WE 19951117004791995111700479NM 1995 11 17 UPS205016 119951111A7160 AIR INTAKE BOEING727 7272A1 138407FNM BS 1200 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND PULLED FASTENER IN NR 2 ENG DUCT, BL O APPROX BS 1200. FOUND CORROSION IN THE LOCATION OF PULLED FASTENER. REMOVED DAMAGED SECTION AND REPAIRED 1AW 727 SRM 54-10-3. 2L73 4F A3WE 19951117004801995111700480NM 1995 11 17 UPS205017 119951111A575165217387 HINGE PIN BOEING727 7272A1 138407FNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING I/B AILERON FWD, LOWER BALANCE PANEL HINGE PIN IS CORRODED. REMOVED CORRODED HINGE PIN, INSTALLED NEW HINGE PIN IAW 27-10-21. 2L73 4F A3WE 19951117004811995111700481NM 1995 11 17 UPS205018 119951111A5752BACB10C237 HINGE TAB BOEING727 7272A1 138407FNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W I/B AILERON TAB FITTINGS ARE CORRODED. REMOVED CORRODED TAB FITTINGS, INSTALLED NEW TAB FITTINGS IAW SRM 51-30-2 MM 27-10-11. 2L73 4F A3WE 19951117004821995111700482NM 1995 11 17 UPS205018A 119951111A575265217387 HINGE TAB BOEING727 7272A1 138407FNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING I/B AILERON FWD, LOWER BALANCE PANEL HINGE PIN IS CORRODED. REMOVED CORRODED HINGE PIN, INSTALLED NEW HINGE PIN IAW 27-10-21. 2L73 4F A3WE 19951117004831995111700483NM 1995 11 17 UPS205019 119951111A57526521773501 HINGE TAB BOEING727 7272A1 138407FNM LT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND L/W I/B AILERON TAB FITTINGS ARE CORRODED. REMOVED CORRODED FITTINGS, REPLACED WITH NEW FITTINGS IAW SRM 51-30-2 MM 27-10-11. 2L73 4F A3WE 19951117004841995111700484NM 1995 11 17 UPS205020 119951111A57536521630187A SKIN BOEING727 7272A1 138407FNM LT TE FOREFLAP DISBONDED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING I/B FOREFLAP HAS DISBOND 12 INCHES FROM I/B END UPPER SURFACE. REPAIRED PER SRM 51-40-6 AND MM 51-20-02. 2L73 4F A3WE 19951117004851995111700485NM 1995 11 17 UPS205021 119951111A57536521630187A SKIN BOEING727 7272A1 138407FNM LT TE FOREFLAP DISBONDED A AIPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING I/B FOREFLAP HAS LARGE DISBONDS IN CENTER OF FLAP ON THE UPPER SURFACE. REPAIRED PER SRM 51-40-6 AND MM 51-20-02. 2L73 4F A3WE 19951117004861995111700486NM 1995 11 17 UPS205022 119951113A572065247516A BULLNOSE BOEING727 7272A1 138407FNM NR 4 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 4 BULLNOSE F/B ATTACH POINT IS CRACKED AT BOTH I/B ATTACH POINTS. REMOVED CRACKED BULLNOSE, INSTALLED SERVICEABLE BULLNOSE IAW SRM 51-30-2 MM 27-81-01. 2L73 4F A3WE 19951117004871995111700487NM 1995 11 17 UPS205023 119951114A5751 RIBS BOEING727 7272A1 138407FNM RT AILERON CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01213UP 21341 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 2ND, 4TH, 5TH AND 6TH RIBS FROM I/B END CORRODED ON RT I/B AILERON. REMOVED CORRODED RIBS AND INSTALLED NEW RIBS PER SRM 51-00, 51-30-2, 51-10-1. 2L73 4F A3WE 19951117004881995111700488NM 1995 11 17 UPS205024 119951114A5753 BRACKET BOEING757 75724APF 1384969NM LT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01425UP 25370 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING OUTBOARD MAIN FLAP BRACKET ON OUTBOARD EDGE IS CRACKED. REMOVED CRACKED BRACKET FROM O/B EDGE OF L/W O/B MAIN FLAP, FABRICATED NEW BRACKET AND INSTALLED. ALL WORK DONE PER SRM 51-30-01, 51-40-02, 51-20-01, AND MM 51-20-10. 2L72 4F RTA2NM 19951117004891995111700489NM 1995 11 17 UPS205025 119951114A5753113N26052 TEE ANGLE BOEING757 75724APF 1384969NM RT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01425UP 25370 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBD MAIN FLAP AFT COVE OUTBOARD END HAS CRACKED TEE ANGLE ON THE LOWER SURFACE OF THE UPPER SKIN, AS MARKED. REPLACED TEE ANGLE PER SRM 51-40-02. 2L72 4F RTA2NM 19951117004901995111700490NM 1995 11 17 UPS205026 119951114A575329510892 RIB BOEING757 75724APF 1384969NM LT TE FLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01425UP 25370 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LEFT WING INBD MAIN FLAP HAS CRACKED RIB IN AFT COVER OF THE MAIN OUTBOARD END UPPER SKIN LOWER SURFACE. REMOVED CRACKED RIB FROM L/W INBD FLAP, FABRICATED NEW RIB FROM STOCK EXTRUSION, INSTALLED ON L/W INBD FLAP. ALL WORK DONE IAW SRM 51-70-12. 2L72 4F RTA2NM 19951117004911995111700491 1995 11 17 UPS805008 419951107A2565 LATCH DOUG DC8 DC871F 302199DWP ESCAPE SLIDE BROKEN A IPXAK NONE O OTHER ININSP/MAINT 1 SO01752UP 45952 WHILE ON GROUND, MAINTENANCE FOUND LATCH FOR ESCAPE SLIDE BROKEN. REMOVED AND REPLACED ESCAPE SLIDE CONTAINER AND SECURED. 2L74 4F RT4A25 19951117004921995111700492WP 1995 11 17 UPS805009 119951108A5730 FLANGE DOUG DC8 DC873F 302199FWP RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01816UP 45990 WHILE ON GROUND, MAINTENANCE FOUND RT WING PANEL 505F FLANGE CRACKED .5 INCH FROM SCREW INWARD AND .25 INCH OUTWARD ON FLANGE AT SCREW NUTPLATE ON RIGHT SIDE OF PANEL FLANGE. REMOVED DAMAGED AREA PER SRM 57-2-1, REPAIRED PER DC8-57-0617, SRM 57-2-1 AND LEAK CHECKED PER MM 28-10-01. 2L74 4F RT4A25 19951117004931995111700493WP 1995 11 17 UPS805010 119951109A2120 AIR DISRT DOUG DC8 DC873F 302199FWP COCKPIT ODOR A IPXAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO01811UP 46089 WHILE ON GROUND, CREW REPORTED STRONG SMOKE SMELL IN COCKPIT AFTER SELECTING GROUND POWER. FOUND PACK SWITCH IN THE ON POS W/O AIR FLOW. CYCLED POWER NUMEROUS TIMES, NO UNUSUAL ODORS IN FLIGHT DECK. 2L74 4F RT4A25 19951117004941995111700494WP 1995 11 17 UPS805012 119951111A3350 BATTREY PACK DOUG DC8 DC873F 302199FWP CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01810UP 46001 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2L74 4F RT4A25 19951117004951995111700495WP 1995 11 17 UPS805013 119951111A3260 SENSOR DOUG DC8 DC873F 302199FWP LANDING GEAR DR DIRTY A IPXAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01812UP 46059 CREW FOUND ON TAKEOFF WHEN GEAR RAISED, GOT DOOR NOT LATCHED LIGHT. DID UPLATCH CHECK THEN GEAR HANDLE BACK UP, LIGHT WENT OUT. INSPECTED, CLEAN AND LUBED DOOR LATCH AND DOOR SENSOR. 2L74 4F RT4A25 19951117004961995111700496NE 1995 11 17 95ZZZX6229 219951004A732177390010 FUEL CONTROL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE BROKEN ADAPTER A A6WAO OTHER X ENGINE FLAMEOUT ININSP/MAINT 1 GL31294UE F8324 E2107 PIA - FLT 370 - NR 1 ENGINE FLAMED OUT AT GATE AT GROUND IDLE. INSPECTED NR 1 ENGINE, FOUND T2 AND P2 MOUNTING ADAPTERS BROKEN ON FCU. REMOVED AND REPLACED NR 1 ENGINE FCU. OPS CHECK AND LEAK CHECKS OK IAW MM. 2H74 4F4 FRTA49EU E6NE 19951117004971995111700497EU 1995 11 17 95ZZZX6230 119950924A5610 WINDOW SEAL BAG BAE146BAE146200A 1500266EU LT COCKPIT TORN A A6WAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL31607AW E2052 ATW - FLT 300 - LOUD AIRSPEED RELATED NOISE IN COCKPIT COMING FROM CAPTAIN'S SIDE WINDOW. AIRCRAFT RETURNED TO ATW. REMOVED AND REPLACED CAPTAIN'S DV WINDOW SEAL. SEAL WAS TORN. 2H74 4F RTA49EU 19951117004981995111700498NE 1995 11 17 95ZZZX6231 219950904A7261 ENGINE OIL BAG BAE146BAE146300A 1500267EU LYC ALF502ALF502R5 41580NE NR 1 REQD SERVICE A A6WAK NONE O OTHER NRNOT REPORTED 1 GL31615AW E3141 MLI - FLT 365 - NR 1 ENGINE OIL LEVEL LOW. FOUND NO EXTERNAL LEAKS, SERVICED WITH 4 QUARTS OF OIL. REFERENCE OPERATOR CONTROL NR 95ZZZX6232, AND 95ZZZX6233. 2H74 4F4 FRTA49EU E6NE 19951117004991995111700499EU 1995 11 17 95ZZZX6232 119950904A3610 PERI SEALS BAG BAE146BAE146300A 1500267EU APU FAILED A A6WAK NONE MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 GL31615AW E3141 MLI - FLT 365 - RIGHT ZONE HIGH TEMP OCCURRED WHEN THE APU WAS SUPPLYING THE NR 2 PACK. REPLACED PERI SEALS. REFERENCE OPERATOR CONTROL NR 95ZZZX6231, AND 95ZZZX6233. 2H74 4F RTA49EU 19951117005001995111700500EU 1995 11 17 95ZZZX6233 119950904A3010 ANTI ICE VALVE BAG BAE146BAE146300A 1500267EU EMPENNAGE INOPERATIVE A A6WAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31615AW E3141 MLI - FLT 365 - TAIL ANTI-ICE VALVE INOP OPEN. REPLACED THE ANTI-ICE VALVE ACTUATOR. REFERENCE OPERATOR CONTROL NR 95ZZZX6231, AND 95ZZZX6232. 2H74 4F RTA49EU 19951117005011995111700501EU 1995 11 17 95ZZZX6234 119951013A3297 WIRE BAG BAE146BAE146200A 1500266EU LANDING GEAR LOOSE A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31607AW E2052 ATW - FLT 322 - GEAR WOULD NOT RETRACT. GEAR HANDLE COULD NOT BE RAISED NORMALLY OR IN OVERRIDE. MANUAL SPOILER FAULT LIGHT ILLUMINATED, WENT OUT WHEN AIRCRAFT LANDED. RESOLDERED 2 WIRES IN RAYCHEM CONNECTOR 131-13-00 DL PINS A1 AND A5. REMOVED AND REPLACED GEAR SELECTOR HANDLE AND CHECKED GEAR FOR PROPER OPERATION. 2H74 4F RTA49EU 19951117005021995111700502EU 1995 11 17 95ZZZX6235 119950811A3350 EEL CONNECTOR BAG BAE146BAE146300A 1500267EU CABIN DIRTY A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31612AW E3122 DEN - FLT 364 - LEFT AND CENTER EXIT SIGNS IN FORWARD VESTIBULE INOPERATIVE. 2H74 4F RTA49EU 19951117005031995111700503EU 1995 11 17 95ZZZX6236 119951005A2760 CONTROL MECH BAG BAE146BAE146100A 1500260EU SPEED BRAKES MALFUNCTIONED A A6WAO OTHER F FLT CONT AFFECTED APAPPROACH 1 GL31463AP E1063 ATW - FLT 265 - UNCOMMANDED OPENING OF AIR BRAKE ON APPROACH INTO ATW. ADJUSTED AND TESTED COMMAND AND FEED BACK POTENTIOMETER IAW 27-63-00, PAGE 501, PARAGRAPH 1C. CLEANED AND ADJUSTED LEVER FRICTION DAMPENERS AND TESTED IAW 27-63-00, PAGE 509. TESTED SENSOR IAW PAGE 504P.2ABCD. OK FOR SERVICE. 2H74 4F RTA49EU 19951117005041995111700504NE 1995 11 17 95ZZZX6237 219951015A7200 ENGINE DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE NR 1 MALFUNCTIONED A VJ6AA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SO11914VV 47486 657563 ATL/MDW - FLT 248 - THE CAPTAIN CALLED BACK WITH ENGINE VIBRATION. THE AIRCRAFT RETURNED TO ATL. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECKED OK. 2L72 4F4 F A6WE E2EA 19951117005051995111700505EU 1995 11 17 UF6A950704 119950720A7603JD574J0110000 CONTROL CABLE BAG ATP ATP EU POWER LEVER FAILED A UF6AO OTHER O OTHER TXTAXI/GRND HDL 1 CE03854AW2176 2028 CAK - FLT 5016 - NR 1 POWER LEVER CABLE FRAYED. MAINTENANCE REPLACED THE POWER LEVER CABLE. ACFT TT, 8,357 HRS. (X) 2L72 4T RTA27NM 19951117005061995111700506NE 1995 11 17 UF6A950705 219950726A7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE RIGHT FAILED A UF6AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL31860AW6856 2037 124400 ORD - FLT NR 5089 - SMOKE APPEARED IN THE CABIN AFTER TAKEOFF. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) 2L72 4T4 TRTA27NM E2ONE 19951117005071995111700507EU 1995 11 17 UF6A950904 119950920A6120M832481157 PCU O-RING HAMSTD 7863364 BAG ATP ATP EU LT ENGINE FAILED A UF6ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL31857AW7615 ATPC0140 2034 GRB - FLT 5060 - PROPELLER'S NR 1 OIL PRESSURE LIGHT ON CENTRAL WARNING PANEL, ILLUMINATED DURING TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED PROPELLER CONTROL UNIT O-RING. A/C TT: 7,615 HRS. (X) 2L72 4T RTA27NM 19951117005081995111700508NE 1995 11 17 UF6A950905 219951002A73223244841121418 FUEL CONTROL BAG ATP ATP EU PWA PW120 PW126A NE LT ENGINE FAILED A UF6AE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE03852AW5257 2977 2021 124224 SBN - FLT 5116 - LOSS OF POWER ON NR 1 ENGINE, ON CLIMB-OUT. MAINTENANCE REMOVED AND REPLACED MECHANICAL FUEL CONTROL. ACFT TT, 9,411 HRS. ENGINE TT, 7,169 HRS. (X) 2L72 4T4 TRTA27NM E2ONE 19951117005091995111700509EU 1995 11 17 UF6A950906 119950929A6120ABA5100002A PCU BAG ATP ATP EU RT ENGINE MALFUNCTIONED A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 GL31860AW4176 2037 ORD - FLT 5009 - RIGHT PROPELLER WOULD NOT FEATHER ON SHUT-DOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK, OPS CHECK GOOD. (X) 2L72 4T RTA27NM 19951117005101995111700510EU 1995 11 17 UF6A951001 119951004A7603JD760J0620020 THROTTLE CABLE BAG ATP ATP EU LT ENGINE FAILED A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 GL31852AW9416 2021 CAK - FLT NR 5018 - AFTER LANDING THE POWER LEVER WOULD NOT RETARD BELOW 20 PERCENT TORQUE. MAINTENANCE REMOVED AND REPLACED THE THROTTLE CABLE. (M) 2L72 4T RTA27NM 19951117005111995111700511EU 1995 11 17 UF6A951003 119951013A61208022631 O-RING BAG ATP ATP EU RT ENGINE FAILED A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 GL31860AW6474 2037 ORD - FLT 5092 - RIGHT PROPELLER WOULD NOT FEATHER ON SHUT-DOWN. MAINTENANCE REMOVED AND REPLACED TRANSFER TUBE O-RING. (X) 2L72 4T RTA27NM 19951117005121995111700512EU 1995 11 17 UF6A951004 119951013A6120ABA5100002A PCU BAG ATP ATP EU RT ENG FAILED A UF6AK NONE O OTHER TXTAXI/GRND HDL 1 GL31860AW4253 2037 ORD - RIGHT PROPELLER WILL NOT FEATHER ON SHUTDOWN. MAINTENANCE REMOVED AND REPLACED PCU. (M) 2L72 4T RTA27NM 19951117005131995111700513EU 1995 11 17 UF6A951005 119951016A28205905587 FUEL FILTER BAG ATP ATP EU LT ENGINE DIRTY A UF6ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL31851AW834 2020 AZO - FLT 5002 - NR 1 FUEL FILTER CWP ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LOW PRESSURE FUEL FILTER. ACFT TT: 9,720 HRS. ENGINE TT: 5,945 HRS. (X) 2L72 4T RTA27NM 19951117005141995111700514NE 1995 11 17 UF6A951007 219951019A73203034989 PY LINE BAG ATP ATP EU PWA PW120 PW126A NE RT ENGINE LOOSE A UF6AK NONE O OTHER DEDESCENT 1 GL31851AW7586 2020 124241 CWA - FLT 5031 - DURING DESCENT, OBSERVED A 15 PERCENT DROP IN TORQUE AND A 20 PERCENT - 25 PERCENT DROP IN THE NH. MAINTENANCE TIGHTENED THE 'PY' LINE ON OVERSPEED GOVERNOR. ACFT TT: 9,747 HRS. ENGINE TT: 7,586 HRS. (X) 2L72 4T4 TRTA27NM E2ONE 19951117005151995111700515NM 1995 11 17 USAA951114 119951018A53206545834257 INTERCOSTAL BOEING737 7373B7 1384580NM BS 328-344.17 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND .50 INCH BY 1 INCH CORRODED AREA 3 PLACES ON INTERCOSTAL, BS 328 - BS 344.17, RBL 11. REPLACED INTERCOSTAL WITH NEW ONE. REPAIRED PER SRM 53-10-51. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005161995111700516NM 1995 11 17 USAA951115 119951018A53201123845 ANGLE BOEING737 7373B7 1384580NM BS 294.5-344.17 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 28 INCH AREA CORRODED AT BS 294.5 - BS 344.17. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-2. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005171995111700517NM 1995 11 17 USAA951116 119951018A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURNG 'Q-3' CHECK, VISUAL INSPECTION FOUND 4 INCH BY 2 INCH CORRODED AREA BS 312, RBL ZERO - 11, ON FLOOR BEAM. INSTALLED NEW T-CAP SECTION. REPAIRED PER TR 53-10-03. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005181995111700518NM 1995 11 17 USAA951117 119951018A5330 SKIN BOEING737 7373B7 1384580NM BS 336-348 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURNG 'Q-3' CHECK, VISUAL INSPECTION FOUND 12 INCH BY 5.75 INCH PREVIOUSLY INSTALLED SKIN DOUBLER (NO SDA) STA 336 TO STA 348 BETWEEN STR 19R PLUS STR 20R, CRACKED. DOUBLER INSTALLED. REPAIRED PER SRM 53-00-01, FIGURE 202. (X) 2L72 4F RTA16WE 19951117005191995111700519NM 1995 11 17 USAA951118 119951018A5320 SUPPORT CHANNEL BOEING737 7373B7 1384580NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK, SEAT TRACK SUPPORT CHANNEL STA 520, LBL 24.75 AFT SIDE WL 207.5. REPAIRED PREVIOUSLY. REPAIRED PER EA 34112. (X) 2L72 4F RTA16WE 19951117005201995111700520NM 1995 11 17 USAA951119 119951018A5230 SKIN BOEING737 7373B7 1384580NM AFT CARGO DOOR DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 11 INCH BY 12 INCH DENT, AFT CARGO DOOR. DOUBLER INSTALLED. REPAIRED PER SRM 52-00-01, FIGURE 202. (X) 2L72 4F RTA16WE 19951117005211995111700521NM 1995 11 17 USAA951122 119951018A532065C807396 ANGLE BOEING737 7373B7 1384580NM BS 953-996 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 2 INCH BY 42 INCH CORRODED AREA, STA 953 - STA 996, LBL 54 (LEFT AFT CABIN DOOR) ON Z-ANGLE. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-02. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005221995111700522NM 1995 11 17 USAA951123 119951018A5320 BEAM BOEING737 7373B7 1384580NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION AT FLOORBOARD HOLES ON BEAM T-CAP, BS 328, LBL 10 TO RBL 45. INSTALLED NEW SECTION OF T-CAP. REPAIRED PER SRM 53-0-51. THIS IS LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005231995111700523NM 1995 11 17 USAA951124 119951018A532065C105925 INTERCOSTAL BOEING737 7373B7 1384580NM BS 957 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL BS 957, RBL 18 TO RBL 45. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-2. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005241995111700524NM 1995 11 17 USAA951125 119951018A53206946812170 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL, BS 947 TO BS 967, RLB 25. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-2. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005251995111700525NM 1995 11 17 USAA951126 119951018A5315 FLOORBEAM BOEING737 7373B7 1384580NM BS 986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION AT FLOORBOARD ATTACH HOLES ON FLOOR BEAM. INSTALLED UPPER T-CAP SECTION ON FLOOR BEAM. REPAIRED PER TR 53-10-05. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005261995111700526NM 1995 11 17 USAA951127 119951018A532065C10592905 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION ON INTERCOSTAL, BS 947 TO BS 967, RBL 45. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-2. LEVEL 1 CORROSION. CORROSION TASK NR C53-107-02. (X) 2L72 4F RTA16WE 19951117005271995111700527NM 1995 11 17 USAA951128 119951018A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 328-312 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 3 INCH CRACK BETWEEN BS 328 AND BS 312 AT RBL 32 INCH, ON INTERCOSTAL WEB. FABRICATED NEW WEB. REPAIRED PER DRAWING 65-45834. (X) 2L72 4F RTA16WE 19951117005281995111700528NM 1995 11 17 USAA951129 119951018A5347 SEAT TRACK BOEING737 7373B7 1384580NM BS 328-373 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 6 INCH CORROSION BS 328 - BS 331, AND BS 370 - BS 373, SEAT TRACK. REPLACED SEAT TRACK. REPAIRED PER SRM 53-00-52, FIGURE 202, REPAIR 1. (X) 2L72 4F RTA16WE 19951117005291995111700529NM 1995 11 17 USAA951130 119951017A5330 SKIN BOEING737 737301 1384611NM BS 927 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19579US33535 23258 ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR FUSELAGE SKIN BS 927, STR 18L - STR 19L, DAMAGED. ONE DOUBLER INSTALLED 12 INCH BY 10.50 INCH. REPAIRED PER SRM 53-00-01. (X) 2L72 4F RTA16WE 19951117005301995111700530NM 1995 11 17 USAA951131 119951017A5230 SKIN BOEING737 737301 1384611NM AFT CARGO DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19579US33535 23258 ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, AFT CARGO DOOR. TWO DOUBLERS INSTALLED ONE ABOVE HANDLE, 7 INCHES BY 12.50 INCHES BY 7.50 INCHES BY 21 INCHES. ONE BELOW HANDLE, 8.25 INCHES BY 7.25 INCHES. REPAIRED PER SRM 52-30-01. (X) 2L72 4F RTA16WE 19951117005311995111700531NM 1995 11 17 USAA951132 119951017A5240 SKIN BOEING737 737301 1384611NM FWD SERVICE DOORDAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19579US33535 23258 ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, FORWARD SERVICE DOOR, TOP AND LOWER HINGE, DAMAGED. TWO DOUBLERS INSTALLED, ONE TOP HINGE, AND ONE BOTTOM HINGE, TOP 7 INCHES BY 8 INCHES, BOTTOM 5 INCHES BY 5 INCHES. REPAIRED PER SRM 52-00-01. (X) 2L72 4F RTA16WE 19951117005321995111700532NM 1995 11 17 USAA951135 119951011A5230 SKIN BOEING737 7373B7 1384580NM AFT CARGO DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19502AU30313 23377 ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, AFT CARGO DOOR SKIN, DAMAGED. ONE DOUBLER PREVIOSULY INSTALLED 8 INCHES BY 16 INCHES. REPAIRED PER SRM 52-30-01. (X) 2L72 4F RTA16WE 19951117005331995111700533NM 1995 11 17 USAA951136 119951011A5230 SKIN BOEING737 7373B7 1384580NM FWD CARGO DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19502AU30313 23377 ROA - DURING 'FULL C' CHECK, VISUAL INSPECTION FOUND PREVIOUSLY INSTALLED REPAIR, FORWARD CARGO DOOR SKIN, DAMAGED. ONE DOUBLER PREVIOSULY INSTALLED, 8 INCHES BY 11 INCHES. REPAIRED PER SRM 52-30-01. (X) 2L72 4F RTA16WE 19951117005341995111700534NM 1995 11 17 USAA951138 119951019A532065C10592155 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947.5-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 14 INCH BY 2 INCH CORROSION, BS 947.5 - BS 967, RLB 8, ON INTERCOSTAL. REPLACED WITH NEW INTERCOSTAL. REPAIRED PER 737-300, SRM 51-10-02, PAGE 16. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005351995111700535NM 1995 11 17 USAA951139 119951019A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 55 INCHES, STA 967, RBL 27, LBL 45, ON FLOOR BEAM. REPLACED T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005361995111700536NM 1995 11 17 USAA951140 119951019A5320 INTERCOSTAL BOEING737 7373B7 1384580NM BS 967-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND CORROSION 1 INCH BY 3 INCH, STA 967 TO STA 986, RBL 18 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005371995111700537NM 1995 11 17 USAA951141 119951019A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 100 INCH BY 3 INCH CORROSION AROUND SCREW HOLES, BS 986.5, ON FLOOR BEAM. REPLACED T-CAP ON TOP OF CABIN FLOOR BEAM. REPAIRED PER TR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005381995111700538NM 1995 11 17 USAA951142 119951019A53206546812170 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947.5-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING 'Q-4' CHECK, VISUAL INSPECTION FOUND 14 INCH BY 2 INCH CORROSION, BS 947.5 - BS 967, RLB 18, ON INTERCOSTAL. REPLACED INTERCOSTAL. REPAIRED PER BOEING 737-300, SRM 51-1-02, PAGE 16. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005391995111700539NM 1995 11 17 USAA951146 119951018A53206546812169 INTERCOSTAL BOEING737 7373B7 1384580NM BS 967-986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION AROUND NUTPLATE HOLES (2 PLACES) INTERCOSTAL RBL 18 BETWEEN BS 967 - BS 986.5. REPLACED INTERCOSTAL. REPAIRED PER BOEING DRAWING 65-46812, SRM 53-60-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005401995111700540NM 1995 11 17 USAA951147 119951018A5321 FLOOR PAN BOEING737 7373B7 1384580NM BS 1038 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 1 INCH CORROSION ON FLOOR PAN, SEVERAL SPOTS, STA 1038, LBL 8. FABRICATED AND INSTALLED NEW FLOOR PAN. REPAIRED PER DRAWING 65C33419, SRM 53-60-51. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005411995111700541NM 1995 11 17 USAA951148 119951018A5320654585541 ANGLE BOEING737 7373B7 1384580NM BS 940-993 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 10 INCH BY 2 INCH CORRODED AREA, RBL 53, BS 940 TO BS 993, RIGHT AFT DOOR. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005421995111700542NM 1995 11 17 USAA951149 119951018A5315 FLOOR BEAM BOEING737 7373B7 1384580NM BS 1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 1 INCH BY 2 INCH CORROSION (2 PLACES), BS 1016, FLOOR BEAM LBL 4 AND LBL 27. REPLACED ENTIRE T-CAP PER SRM 51-10-2, BOEING DRAWING 65C32677 AND DRAWING 65C33419. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19951117005431995111700543NM 1995 11 17 USAABB95002 119951022A3350 EEL WIRING BOEING767 767201 1385125NM CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19647US 23899 FRA - FLT 893 - DURING TEST, FOUND LEFT AISLE FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING AND RELAMPED SOME SOCKETS. (X) 2L72 4F RTA1NM 19951117005441995111700544NM 1995 11 17 USAABB95003 119951022A3350873100251REV9 EEL IDENTIFIER BOEING757 7572B7 1384964NM 4 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19624AU 27245 LGA - FLT 0089 - THE AFT ENTRY DOOR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. (X) 2L72 4F RTA2NM 19951117005451995111700545NM 1995 11 17 USAABB95004 119951021A3350 EEL BOEING767 767201 1385125NM CABIN MALFUNCTIONED A USAAD RETURN TO BLOCK L NO TEST TXTAXI/GRND HDL 1 EA19648US 23900 BOS - FLT 816 - AIRCRAFT RETURNED TO THE GATE BECAUSE THE FLOOR LEVEL EMERGENCY LIGHTS ILLUMINATED AND WOULD NOT SHUT OFF. MAINTENANCE CYCLED THE APPROPRIATE CIRCUIT BREAKERS AND THE SYSTEM RESPONDED CORRECTLY. (X) 2L72 4F RTA1NM 19951117005461995111700546NE 1995 11 17 9517956633 219951111A7200 ENGINE 386900 BOEING747 747227B 1384888NM PWA JT9 JT9D7Q 52054NE NR 3 FAILED A NWAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 GL01633US 105 21991 702166 AT TOP OF DESCENT WHEN THE THROTTLES WERE RETARDED, THE NR 3 ENGINE EXPERIENCED A FLAME-OUT. A RELIGHT ATTEMPT WAS UNSUCCESSFUL. THE AIRCRAFT CONTINUED TO AN UNEVENTFUL THREE ENGINE LANDING AT NRT, NO FUEL WAS DUMPED. METAL PARTICLES FROM THE FUEL PUMP WERE FOUND AT THE FUEL NOZZLES AND THE ENGINE WAS REPLACED. 2L74 4F4 F A20WE E3NE 19951117005471995111700547NE 1995 11 17 9517961159 219951110A7321 FUEL CONTROL DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 2 ENGINE FAILED A NWAADE RETURN TO BLOCK ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION TXTAXI/GRND HDL 1 GL01159US 46768 686175 DURING TAXI OUT, THE NR 2 ENGINE EGT WENT TO 1,000 DEGREES FOR 30 SECONDS AND THE ENGINE WAS SHUTDOWN. THE ENGINE WAS INSPECTED AND THE EPR INDICATOR WAS REPLACED. DURING THE SECOND TAXI OUT THE FUEL FLOW PEGGED AND THE EGT AGAIN ROSE. THE FUEL CONTROL AND EVC WERE REPLACED AND A GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L73 4F4 F A22WE E20EA 19951117005481995111700548NM 1995 11 17 9517972289 119951114A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01298US 22152 DURING PREFLIGHT, FOUND RIGHT AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE BATTERY PACK, CHECKED OK. 2L73 4F A3WE 19951117005491995111700549NM 1995 11 17 9517985507 119951115A3350 BATTERY PACK BOEING757 757251 1384970NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01507US 21396 DURING PREFLIGHT, CABIN EMERGENCY LIGHTS IN FORWARD SECTION OF MAIN CABIN WOULD ONLY STAY ON FOR A SHORT TIME. REPLACED THE BATTERY PACK AT DOOR 2L, EMERGENCY LIGHTS CHECKED OK. 2L72 4F RTA2NM 19951117005501995111700550NM 1995 11 17 9517996310 119951114A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01670US 24225 TPE - DURING LINE CHECK, THE FLOOR EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 21R TO 24R AND 27R TO 31R WERE FOUND INOPERATIVE. RECONNECTED LOOSE PINS TO LIGHT ASSEMBLIES, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951117005511995111700551NM 1995 11 17 9518006633 119951114A33506106765 BATTERY PACK BOEING747 747227B 1384888NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01633US 21991 DURING LINE CHECK, FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY PACK, PERFORMED FUNCTIONAL CHECK AND TEST WAS NORMAL. 2L74 4F A20WE 19951117005521995111700552NM 1995 11 17 9518016638 119951114A33506106765 BATTERY PACK BOEING747 747251B 1384892NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01638US 23549 DURING LINE CHECK, FOUND THE EMERGENCY FLOOR LIGHTS IN ZONE-A INOPERATIVE. REPLACED ZONE-A BATTERY PACK AND POWER SUPPLY, PERFORMED FUNCTIONAL CHECK AND TEST WAS NORMAL. 2L74 4F A20WE 19951117005531995111700553WP 1995 11 17 9518029984 119951114A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01984US 47383 DURING LINE CHECK, FOUND RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE POWER SUPPLY, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117005541995111700554WP 1995 11 17 9518039852 119951114A3350 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01761NC 47709 DURING LINE CHECK, THE RIGHT EMERGENCY LIGHT WAS VERY DIM AND WOULD NOT EXTINGUISH. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951117005551995111700555NM 1995 11 17 95FDEA01748 119951114A5311 FRAME BOEING727 727227 1384078NM BS 700 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENT ON FRAME. 2L73 4F A3WE 19951117005561995111700556NM 1995 11 17 95FDEA01749 119951114A5311 FRAME BOEING727 727227 1384078NM BS 680 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD BAY FRAME DENTED AT BS 680 AT STR 24 L. 2L73 4F A3WE 19951117005571995111700557NM 1995 11 17 95FDEA01750 119951116A5311 FRAME BOEING727 727227 1384078NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FRAME DENTED AT BS 500 BETWEEN STR 24 TO 25R AND DENT WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA FROM FRAME, FABRICATED, TREATED AND INSTALLED DOUBLER PER FEDEX SRM 53-10-1 AND 51-40-3. 2L73 4F A3WE 19951117005581995111700558NM 1995 11 17 95FDEA01751 119951114A5320 CHANNEL BOEING727 727227 1384078NM BS 328 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-224-01), ON HAT CHANNEL BS 328 WL 208 RBL 13. REMOVED CORRODED HAT CHANNEL, FABRICATED AND INSTALLED HAT CHANNEL AT BS 303 TO 344 RBL 10 TO 15 WL 208. 2L73 4F A3WE 19951117005591995111700559NM 1995 11 17 95FDEA01752 119951114A5330 SKIN BOEING727 727227 1384078NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON EXTERIOR SKIN SURFACE AT BS 720A PLUS 10 TO 720C, BL 0 WL 145. CORROSION FOUND WHILE ACCESSING NR0481 BENEATH RAM AIR DOOR'S SPLITTER VALVE. BLENDED CORROSION ON EXTERIOR SKIN BS 720A TO 720C BL 0 WL 145 BENEATH RAM AIR SPLITTER VANE. CORROSION FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-30-1, CLEANED AND TREATED SKIN. 2L73 4F A3WE 19951117005601995111700560NM 1995 11 17 95FDEA01753 119951114A5720 FITTING BOEING727 72725C 138400HNM BS 740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25133FE 19851 LT STA 740 WING TERMINAL FITTING ON FUSELAGE, BORE IS CORRODED. REMOVED CORROSION BY BORING HOLE TO 3500 PER SRM 57-10-7 PAGE 3, MADE SLEEVE PER SRM 57-10-7 PART 9 AND 10. INSTALLED TERMINAL SLEEVE PER SRM 51-10-1. 2L73 4F A3WE 19951117005611995111700561NM 1995 11 17 95UAL900256 119951114A335058781 EEL CABLE BOEING737 737291 138448WNM PWA JT8 JT8D17 52049NE CABIN DAMAGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29976UA 21598 AFT SECTION OF EMERGENCY ESCAPE PATH LIGHTING DAMAGED. THREE LIGHT SEGMENTS ARE INOP. REPLACED CABLE, CHECKS OK. 2L72 4F4 F A16WE E2EA 19951117005621995111700562NM 1995 11 17 95UAL900257 119951114A3350 EEL HARNESS BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29952UA 26699 AFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED BATTERY AND INVERTERS, NO HELP. REPLACED HARNESS, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951117005631995111700563NM 1995 11 17 95UAL900258 119951114A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29392UA 24667 ONE LIGHT STRIP OF EMERGENCY ESCAPE PATH LIGHTING ROW NR 21 INOP. REPLACED LIGHT, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951117005641995111700564NM 1995 11 17 95UAL900259 119951114A2150655281059 AC MODULE BOEING737 737322 1384676NM GE CFM56 CFM563B1 13802NE E/E COMPT INOP A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29374UA 24639 AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE AFTER TAKEOFF. AIR CONDITIONING RELAY MODULE OPERATIONALLY CHECKS PACKS OK. AFTER ARRIVING AT GATE, FOUND NO PACK OPERATION. REPLACED THE AIR CONDITIONING ACCESSORY MODULE, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951117005651995111700565NM 1995 11 17 95UAL900260 119951114A27813F15825501 INDICATOR WIRE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 3 LE SLAT FAILED A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP299054U 19935 NR THREE LEADING EDGE DEVICE FAILED TO RETRACT AFTER TAKEOFF. THIS WAS FOUND TO BE AN INDICATION PROBLEM. THE NR THREE LEADING EDGE SLAT ACTUATOR ROD END WIRE ASSEMBLY WAS REPLACED. CHECKS O.K. 2L72 4F4 F A16WE E2EA 19951117005661995111700566NM 1995 11 17 95UAL900261 119951115A3350 EEL LAMP BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29508UA 24744 LEFT HAND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED LAMP, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951117005671995111700567WP 1995 11 17 95UAL900262 119951115A49003600760 GEARBOX DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL APU CRACKED A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP291843U 4555 46636 PUNGENT ODOR/SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. FOUND APU GEARBOX CRACKED AT STARTER PAD STUDS AT ONE AND THREE O'CLOCK POSITIONS (LOOKING AFT). SMOKE ATTRIBUTED TO OIL BEING INTRODUCED INTO PNEUMATIC DUCTING. REMOVED AND REPLACED GEARBOX. 2L73 4F4 F A22WE E23EA 19951117005681995111700568NM 1995 11 17 DL72L954349 119951112A3350244202815 EEL HARNESS BOEING727 727232 1384082NM CENTER CARGO DR DAMAGE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11511DA 21313 CENTER CARGO EMERGENCY LIGHT INOP. REPLACED RACK AND REPAIRED DAMAGED WIRE HARNESS, OPERATION NORMAL. 2L73 4F A3WE 19951117005691995111700569NM 1995 11 17 DL72S954363 119951113A5320 WEB BOEING727 727232 1384082NM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11541DA 22387 FOUND ON A2 LETTER CK, TORQUE BOX WEB CRACKED .5 INCH AT FASTENER UPPER ROW OF RIVETS LT SIDE STA 1223. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951117005701995111700570NM 1995 11 17 DL72S954364 119951113A5754 ANGLE BOEING727 727232 1384082NM NR 5 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11541DA 22387 FOUND ON A2 LETTER CK, .5 INCH VISIBLE CRACK ON COVE SKIN ATTACH ANGLE BELOW THE OUTBOARD STOP PAD NUMBER 5 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951117005711995111700571NM 1995 11 17 DL72S954384 119951110A2750693017311 ROD BOEING727 727232 1384082NM RT TE AFT FLAP SHEARED RIVET A DALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO11420DA 21273 AIRFRAME VIBRATION AT 300 KNOTS. FOUND RIVET SHEARED AT RT OUTBOARD AFT FLAP OUTBOARD DRIVE ROD. REPLACED ROD, OPERATION NORMAL. 2L73 4F A3WE 19951117005721995111700572NM 1995 11 17 DL72W954367 119951113A3350 BATTERY 20131A BOEING727 727247 138408FNM CABIN OUT OF POSITION A DALAK NONE L NO TEST ININSP/MAINT 1 SO112817W 19491 20873 OVERHEAD EMERGENCY LIGHT AT ROW 29 INOP. FOUND BATTERY CASE OUT OF POSITION. REPLACED BATTERY AS PRECATIONARY, OPN NORMAL. 2L73 4F A3WE 19951117005731995111700573WP 1995 11 17 DLL13954196 119950924A5312 BLKHD STRAP LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11783DL 193A1009 THE BULKHEAD STRAP AT FS 1363 RBL 42.5 WAS FOUND CRACKED. THE SUBJECT STRAP IS M/F .100 7075-T6 CLAD. REPAIRED PER DL ERA 271928-14AD. 2L73 4F A23WE 19951117005741995111700574WP 1995 11 17 DLL15954361 119951113A2130 DUCT LKHEED1011 10113853 5265020WP NR 3 OUT FLOW VLDETACHED A DALAA UNSCHED LANDING O OTHER CRCRUISE 1 SO11753DA 193W1189 EXPERIENCED LOUD THUMP, UNKNOWN PROBLEM, OUTFLOW VALVE FULL CLOSED. FOUND COMPRESSOR OUTLET DUCT DETACHED. INSP AND REINSTALLED DUCT, LEAK CK OK NR 3 A/C PACK. 2L73 4F A23WE 19951117005751995111700575WP 1995 11 17 DLL17954195 119950912A53121646545155189 BLKHD SKIN LKHEED1011 10113853 5265020WP FS 328 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11765DA 193H1206 ON 8-9-91 CRACKS WERE DISCOVERED IN THE FS 328 CANTED BULKHEAD STRUCTURE DURING HMV. THIS DAMAGE WAS REPAIRED BY LAC DWG 1646545 PER ER/A 226719-14. AFTER THAT, EO 7-53207-3AD WAS ISSUED TO REINFORCE THE FS 328 CANTED BULKHEAD STRUCTURE FOR ALL DAL L1011'S, PART 2 CALLED FOR INSPECTION OF PERMANENT REPAIRS FOR UNITY WITH THE EO. THE DOUBLERS OF THE BULKHEAD MOD WERE MISSING FASTENERS IN SEVERAL LOCATIONS. ACCOMPLISHED REPAIRS PER DL ERA 271850-14AD. 2L73 4F A23WE 19951117005761995111700576WP 1995 11 17 DLL17954362 119951113A2910 HYD LINE LKHEED1011 10113853 5265020WP BS 1975 CHAFED A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11766DA 193H1207 SHORTLY AFTER LEVEL OFF AT FL 330, B-HYD QTY DROPPED TO BELOW .25 AND LOW QTY LIGHT ILLUMINATED. FOLLOWED PROCEDURES, DIVERTED ATL. FOUND CHAFED B-SYS PRESS LINE AT FS 1975, ABOVE STABILIZER. REPAIRED LINE, OPERATION NORMAL. 2L73 4F A23WE 19951117005771995111700577WP 1995 11 17 MWEA95381 119951115A5320 SPLICE DOUG DC9 DC932 3022066WP BS 1076 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND CRACKS IN LONGERON SPLICE AT LONGERON 2L AND 2R AT STA 1076. REMOVED AND INSTALLED SPLICE (P/N 3924814-501) PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005781995111700578WP 1995 11 17 MWEA95382 119951115A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 218-237 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL BETWEEN STA 218 AND 237 BETWEEN LONGERON 27L AND 28L CORRODED BEYOND LIMITS. MAINTENANCE FABRICATED AN INTERCOSTAL FROM .050 INCH 2024-T3 ALUMINUM AND INSTALLED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005791995111700579WP 1995 11 17 MWEA95383 119951115A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 218-237 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL BETWEEN STA 218 AND 237, BETWEEN LONGERON 27R AND 28R CORRODED BEYOND LIMITS. MAINTENANCE FABRICATED AN INTERCOSTAL FROM .050 INCH 2024-T3 ALUMINUM AND INSTALLED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005801995111700580WP 1995 11 17 MWEA95384 119951115A5313 LONGERON DOUG DC9 DC932 3022066WP BS 136 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 25R AT STA 136 HAS AN AREA OF CORROSION BEYOND LIMITS. MAINTENANCE FABRICATED A DOUBLER SPLICE FROM 7637813-3 EXTRUSION AND INSTALLED PER SRM 53-01 PG 1. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005811995111700581WP 1995 11 17 MWEA95385 119951115A53159911544501 FLOORBEAM DOUG DC9 DC932 3022066WP BS 237 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE FLOORBEAM AT STA 237 HAS A 4 INCH CRACK IN THE UPPER WEB 5 INCHES LEFT OF CENTERLINE. INSTALLED DOUBLER ON BEAM IAW SRM 53-05 FIG 73 PER DAC TELEX ORD-SVC-0218/PDG. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005821995111700582WP 1995 11 17 MWEA95386 119951115A53152912758 FLOORBEAM DOUG DC9 DC932 3022066WP BS 996 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE FLOORBEAM TOP ANGLE IN AFT LAVATORY AREA AT STA 996 IS CORRODED. REPLACED TOP ANGLE PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005831995111700583WP 1995 11 17 MWEA95387 119951115A5312 BLKHD CLIP DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-14 CRACKED. FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005841995111700584WP 1995 11 17 MWEA95388 119951115A5312 BLKHD CLIP DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-24 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005851995111700585WP 1995 11 17 MWEA95389 119951115A5312 BLKHD CLIP DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z34 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005861995111700586WP 1995 11 17 MWEA95390 119951115A5320 CLIPS DOUG DC9 DC932 3022066WP BS 980 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE RT LAVATORY STA 980 ATTACH CLIPS ON FUSELAGE SKIN AT LONGERONS 14, 15 AND 16 HAVE .125 INCH CRACKS. MAINTENANCE FABRICATED AND INSTALLED CLIPS OF 0.050 INCH 2024-T3 ALUMINUM PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005871995111700587WP 1995 11 17 MWEA95391 119951115A5320 CLIPS DOUG DC9 DC932 3022066WP BS 980 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY STA 980 ATTACH CLIPS ON FUSELAGE SKIN AT LONGERONS 14, 15 AND 16 HAVE .125 INCH CRACKS. MAINTENANCE FABRICATED AND INSTALLED CLIPS OF 0.050 INCH 2024-T3 ALUMINUM PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117005881995111700588NM 1995 11 17 SWAA950706 119951112A5320 INTERCOSTAL BOEING737 7372H4 138448CNM BS 469 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0786SW 22827 DURING SCHEDULED SERVICE CHECK, FOUND INTERCOSTAL CRACKED AT FWD CARGO THRESHOLD AT BS 469. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117005891995111700589NM 1995 11 17 SWAA950707 119951110A5210 ANGLE BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4 D-CHECK, FOUND FWD ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN AFT NR 3 AND 4 STOP FITTINGS. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951117005901995111700590NM 1995 11 17 SWAA950708 119951110A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT THE FOLLOWING AREAS, BETWEEN BS 363 TO 420, S21 TO 22R, BS 919, S18R, BETWEEN BS 911 TO 920, S23 TO 25R, BS 944, S23 TO 24R, BS 925, S25 TO 26R, BS 369 TO 379, S4L, BS 373, S4 TO 5L, BETWEEN BS 321 TO 334, S22 TO 24R, BS 1040, RBL 3, WL 148, BS 960, S21 TO 22R, BS 342, BETWEEN 23 TO 24R, BS 929, BETWEEN 24 TO 25L AND BS 911, S21 TO 22R. REPAIRED ALL PER BOEING SRM. 2L72 4F A16WE 19951117005911995111700591NM 1995 11 17 SWAA950709 119951110A5210 SKIN BOEING737 7372H4 138448CNM PAX DOOR DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR SKIN DENTED 4 PLACES BETWEEN HINGE AND ARM CUTOUTS. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117005921995111700592NM 1995 11 17 SWAA950710 119951110A5247 SKIN BOEING737 7372H4 138448CNM APU DOOR DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND APU DOOR SKIN DENTED BETWEEN S5 TO 6L AND RT AFT CORNER BENT. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117005931995111700593NM 1995 11 17 SWAA950711 119951110A53206941460 SPLICE BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM I/B T-SPLICE CRACKED AT BS 727 RBL WL 154. REPLACED PER BOEING SRM. 2L72 4F A16WE 19951117005941995111700594NM 1995 11 17 SWAA950712 119951110A5320 CHORD BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND LEFT OUTER CHORD AT BS 178 CRACKED IN RADIUS FROM WL 194.25 TO 196.5. REPAIRED PER TRAMCO EWO 95-0659. 2L72 4F A16WE 19951117005951995111700595NM 1995 11 17 SWAA950713 119951110A5320 MOPSILL BOEING737 7372H4 138448CNM BS 940-990 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND MOPSILL CORROSION AT BS 940 TO 990, RBL 45 TO RBL 57, WL 208, AND AT BS 940 TO 990, RBL 57 TO 45, WL 208. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117005961995111700596NM 1995 11 17 SWAA950714 119951110A5311 FRAME BOEING737 7372H4 138448CNM BS 639 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME I/B CHORDS CRACKED AT BS 639, LBL 66, WL 215 AND AT S16R. REPLACED PER BOEING SRM. 2L72 4F A16WE 19951117005971995111700597NM 1995 11 17 SWAA950715 119951110A5312 BULKHEAD BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE PRESSURE BULKHEAD GOUGED AT FLAP DRIVE UNIT ATTACH POINT. REPAIRED PER TRAMCO EWO 95-0658. 2L72 4F A16WE 19951117005981995111700598NM 1995 11 17 SWAA950716 119951110A5311 FRAMES BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 597 LBL 70 WL 202, BS 727A WL 209 LBL 64, BS 663 S1 TO S2R, BS 360 BETWEEN S20 TO 21R, BS 727A WL 209 BL LBL 64, BS 663, S1 TO 2R, BS 440 S2 TO 4R, BS 1086, RBL 30. REPAIRED PER BOEING SRM AND TRAMCO EWO 95-0648. 2L72 4F A16WE 19951117005991995111700599NM 1995 11 17 SWAA950717 119951110A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 715-721 CHAFED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND LEFT KEEL BEAM CHAFED AT THREE SCREW ATTACH POINTS IN LOWER CHORD AT BS 715 TO 721, LBL WL 148. REPAIRED PER TRAMCO EWO 95-0655. 2L72 4F A16WE 19951117006001995111700600NM 1995 11 17 SWAA950718 119951110A5330 SKIN BOEING737 7372H4 138448CNM BS 1156 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, SKIN DAMAGED AT BS 1156 RBL 16, ABOVE APU DOOR AT RIGHT AFT CORNER. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006011995111700601NM 1995 11 17 SWAA950719 119951110A5330 SKIN BOEING737 7372H4 138448CNM BS 1136 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FUSELAGE SKIN CRACKED AT BS 1136, LBL 26 WL 181. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006021995111700602NM 1995 11 17 SWAA950720 119951110A5330 SKIN BOEING737 7372H4 138448CNM BS 492 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FUSELAGE SKIN CRACKED AT BS 492, RBL 35 WL 157. REPAIRED PER TRAMCO EWO 95-0639. 2L72 4F A16WE 19951117006031995111700603NM 1995 11 17 SWAA950721 119951110A5330 SKIN BOEING737 7372H4 138448CNM FUSELAGE GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FUSELAGE SKIN GOUGED AT BS 939 S19L, BS 1132 LBL 26, BS 1073 BETWEEN S16 AND 17L, BS 467 RBL 5 WL 149. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006041995111700604NM 1995 11 17 SWAA950722 119951110A5330 SKIN BOEING737 7372H4 138448CNM BS 633 LIGHTNING STRIKEA SWAAK NONE C F.O.D. ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT BS 633 S6L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006051995111700605NM 1995 11 17 SWAA950723 119951110A5330 SKIN BOEING737 7372H4 138448CNM BS 847 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND SKIN AND SHEAR TIE CORRODED AT BS 847 BBL 0 TO LBL 4 S27L TO 27R. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006061995111700606NM 1995 11 17 SWAA950724 119951110A5240 FRAME BOEING737 7372H4 138448CNM BS 494 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND RIGHT AFT SERVICE DOOR FRAME CRACKED AT BS 494 RBL 36 S24R. REPAIRED PER TRAMCO EWO 95-0644. 2L72 4F A16WE 19951117006071995111700607NM 1995 11 17 SWAA950725 119951110A5311 FRAME BOEING737 7372H4 138448CNM BS 480 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES DENTED AT BS 480 LBL 33 WL 160, LBL 40 WL 163, LBL 50 WL 173. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006081995111700608NM 1995 11 17 SWAA950726 119951110A5313 STRINGER BOEING737 7372H4 138448CNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 480 S24L AND 25L, BS 727 PLUS 8, S9L, BS 727 PLUS 8, S9L, AND BS 296 S10L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006091995111700609NM 1995 11 17 SWAA950727 119951110A5320 SPLICE BOEING737 7372H4 138448CNM BS 663 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663 S1 AND S3R. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006101995111700610NM 1995 11 17 SWAA950728 119951110A5313 STRINGER BOEING737 7372H4 138448CNM BS 727 MISDRILLED A SWAAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND STRINGER MISDRILLED AT BS 727A S8L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006111995111700611NM 1995 11 17 SWAA950729 119951110A5320 SHEAR TIE BOEING737 7372H4 138448CNM BS 927 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CORRODED AT BS 927 LBL 6 WL 168 BETWEEN S26 TO 27L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006121995111700612NM 1995 11 17 SWAA950730 119951110A5320 BEAM BOEING737 7372H4 138448CNM BS 685 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM, VERTICAL FLANGE CRACKED AT BS 685 WL 207 RBL 25. REPAIRED PER TRAMCO EWO 95-0663. 2L72 4F A16WE 19951117006131995111700613NM 1995 11 17 SWAA950731 119951110A5210 BEAM BOEING737 7372H4 138448CNM FWD PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER GATE BEAM CRACKED. REPLACED PER BOEING SRM. 2L72 4F A16WE 19951117006141995111700614NM 1995 11 17 SWAA950732 119951110A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 344 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 344 BL 0 LBL 8, 15, 22, 30, RBL 9, 12, WL 208. REPLACED PER BOEING SRM. 2L72 4F A16WE 19951117006151995111700615NM 1995 11 17 SWAA950733 119951110A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 978.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM FASTENER HOLE CORROSION AT BS 987.5 LBL 13 WL 208 RBL 7, 10, 21, 23.5 AND RBL 31 WL 208. REPAIRED PER TRMCO EWO 95-0656. 2L72 4F A16WE 19951117006161995111700616NM 1995 11 17 SWAA950734 119951110A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 328 LBL 12 RBL 10, 24, 27, WL 208. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006171995111700617NM 1995 11 17 SWAA950735 119951110A5315 FLOORBEAM BOEING737 7372H4 138448CNM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0756SW 21721 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORROSION AT BS 312 LBL 12 RBL 14 WL 208. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951117006181995111700618NM 1995 11 17 SWAA950736 119951015A80122730426 START VALVE BOEING737 7372H4 138448CNM NR 1 MALFUNCTIONED A SWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW07102SW 23108 BHM - DURING CLIMBOUT PASSING 13,000 FT, NUMBER 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. ALSO, ENGINE OIL TEMP BEGAN INCREASING. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT RETURNED TO BHM AND MADE AN UNEVENTFUL LANDING. INSPECTED, MEL'D NUMBER 1 ENGINE START VALVE PER 80-2 AND CONTINUED. 2L72 4F A16WE 19951117006971995111700697NM 1995 11 17 9518046601 119951114A323069B803587 ACTUATOR BOEING747 747151 1384891NM RT BODY GEAR LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL01601US 19778 DURING DESCENT, THE NR 1 HYDRAULIC SYSTEM FAILED. ALSO, ALTERNATE ELECTRICAL SYSTEM FAILED TO OPERATE FLAPS. CREW LANDED AIRCRAFT WITH OUTBOARD FLAPS AT 25 DEGREES AND INBOARD AT 10 DEGREES. FLIGHT LANDED WITHOUT INCIDENT AND WAS TOWED TO GATE. FOUND LEAKING DOWNLOCK ACTUATOR ON RIGHT BODY GEAR. REPLACED UNIT AND CHECK WAS NORMAL. 2L74 4F A20WE 19951117006981995111700698NM 1995 11 17 9518052295 119951115A2913 HYD PUMP BOEING727 727251 138408HNM NR 2 FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 GL01295US 21506 DURING CLIMB AFTER GEAR RETRACTION, 'A' SYSTEM HYDRAULICS DROPPED BELOW TWO GALLONS WITH 'B' SYSTEM HYDRAULIC QUANTITY DROPPING TO ZERO. AIRCRAFT RETURNED TO MSP, DUMPED 10,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT. FOUND QUICK DISCONNECT IN HYDRAULIC SYSTEM BAY LEAKING AT ADAPTER ON PRESSURE SIDE OF NR 2 HYDRAULIC PUMP. REPLACED NR 2 HYDRAULIC PUMP, LEAK CHECK OK. 2L73 4F A3WE 19951117006991995111700699NM 1995 11 17 9518062293 119951116A3350 EEL BOEING727 727251 138408HNM AFT AIRSTAIR INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01293US 21504 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, FUNCTIONAL CHECK OK. 2L73 4F A3WE 19951117007001995111700700NM 1995 11 17 95FDEA01754 119951114A5754 FLAP BOEING727 727232 1384082NM NR 5 LE FLAP CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DUE TO EXCESSIVE CORROSION (C57-562-01-2) NR 5 K-FLAP REQUIRES REPLACEMENT. REMOVED AND REPLACED NR 5 K-FLAP IAW FEDEX MM 27-81-1. C/A ADDITION. 2L73 4F A3WE 19951117007011995111700701NM 1995 11 17 95FDEA01755 119951115A5311 FRAME BOEING727 727227 1384078NM BS 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 AND 25L. 2L73 4F A3WE 19951117007021995111700702NM 1995 11 17 95FDEA01756 119951115A5313BAC1493508 SRTINGER BOEING727 727227 1384078NM BS 765 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-224-01, 2), ON STR 4L AT BS 765. ACCOMPLISHED STR REPAIR AT BS 765 STR 4L IAW FEDEX SRM 53-10-3. 2L73 4F A3WE 19951117007031995111700703NM 1995 11 17 95FDEA01757 119951114A5330 SKIN BOEING727 727227 1384078NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (53-111-01-3), ON SKIN AT BS 950F PLUS 10 STR 28L WHILE WORKING ON CARD NR0208, CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER, INSTALLED PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951117007041995111700704NM 1995 11 17 95FDEA01758 119951114A5320 NUTPLATE STRIP BOEING727 727227 1384078NM BS 720 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON PRESSURIZATION NUTPLATE DOMES AT BS 720B LBL 5 TO RBL 5 IN BILGE. REMOVED NUTPLATE STRIP AT BS 720B LBL 5. REMOVED .5 INCH BY 1 INCH BY .026 INCH. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-6. FABRICATED NEW STRIP, CLEANED AND TREATED MNR4489073. INSTALLED NUTPLATES AND NEW NUTPLATE STRIP. 2L73 4F A3WE 19951117007051995111700705NM 1995 11 17 95FDEA01759 119951112A5313 STRINGER BOEING727 727225 1384077NM BS 720 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-1), ON STRINGER AT BS 720 PLUS 10 STR 27R, INSIDE BAY. REMOVED CORROSION AT BS 720 PLUS 10 STR 27R, REPAIRED DAMAGE PER FEDEX SRM 53-10-3 DETAIL 1. CUT OUT CORROSION AREA OUT OF LIMITS PER FEDEX 53-10-1. 2L73 4F A3WE 19951117007061995111700706NM 1995 11 17 95FDEA01760 119951115A5311 FRAME BOEING727 727227 1384078NM BS 700 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD CARGO BAY BS 700 BETWEEN STR 22 TO 25R DENTED ON FRAME. REMOVED DAMAGED AREA OF FRAME AT BS 700 BETWEEN STR 22 TO 25R, FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951117007071995111700707NM 1995 11 17 95FDEA01761 119951115A532065453132 CLIP BOEING727 727227 1384078NM BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 660 STR 8L. REMOVED CRACKED STR CLIP AND REPLACED WITH NEW STR CLIP AT BS 660 STR 8L. 2L73 4F A3WE 19951117007081995111700708NM 1995 11 17 95FDEA01762 119951115A532065453132 CLIP BOEING727 727227 1384078NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 680 STR 2L. REMOVED STR CLIP AT BS 680 STR 2L AND REPLACEMENT WITH NEW STR CLIP AT ABOVE AREA. 2L73 4F A3WE 19951117007091995111700709NM 1995 11 17 95FDEA01763 119951115A532065453132 CLIP BOEING727 727227 1384078NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 680 STR 3L. REMOVED STR CLIP AT BS 680 STR 3L AND REPLACED WITH NEW STR CLIP AT ABOVE AREA. 2L73 4F A3WE 19951117007101995111700710WP 1995 11 17 ABXA9500934 119951114A21105614845517 CTC DOUG DC8 DC863 302198AWP NR 4 DEFECTIVE A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23824AX2142 46141 DURING CRUISE, NR 4 CTC EMITTED BURNING OIL ODOR AND LIGHT SMOKE THROUGHOUT AIRCRAFT. A HOWLING NOISE COULD BE HEARD FROM THE NR 4 CTC. DEFERRED THE NR 4 CTC PER DC8 MEL 21-1-13. 2L74 4F 4A25 19951117007111995111700711SO 1995 11 17 COMA9512002 119951112A301044E202A SEPARATOR EMB 120 EMB120RT SO RT AIR FOIL LEAKING A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01200CD5606 120200 RT DUCT LEAK WARNING ACTIVATED. REPLACED LEAKING AIR FOIL DE-ICE WATER SEPARATOR. 2L72 4T RTA31SO 19951117007121995111700712SW 1995 11 17 COMA9520399 119951113A3230AN1745A BOLT OZONE 54510431 SWRNGNSA227 SA227AC 8780603SW NLG MISSING A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO0127119 AC701 NLG INTRANSIT LIGHT REMAINED ON AFTER LANDING GEAR RETRACTED. FOUND TWO OF THE THREE BOLTS THAT ATTACH THE NLG UP LOCK CAM, MISSING. REPLACED BOLTS AND ACFT RETURNED TO SERVICE. 1L72 4T A8SW 19951117007131995111700713SW 1995 11 17 COMA9520400 119951115A57302731322008 SKIN SWRNGNSA227 SA227AC 8780603SW WS 217.5 CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO01459AM AC700 INSPECTION REVEALED CORROSION WITH A SMALL CRACK APPROXIMATELY 1.25 INCH LONG ON THE RIGHT WING LOWER SKIN, LOCATED 2 INCHES OUTBOARD OF WS 217.500 AND 5 INCHES FORWARD OF THE WING TRAILING EDGE. THE DAMAGED AREA WAS REMOVED AND A REPAIR INSTALLED PER AERODESIGN REPORT NR 1689-1 REV IR, DATED 11-15-95. 1L72 4T A8SW 19951117007141995111700714 1995 11 17 COMA9531192 419951115A34256226190113 COMPUTER SAAB SF340 SF340A 7850100EU AVIONICS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01380CA201141630 340A012 HEADING COMPARATOR WARNING. REPLACED THE NR 1 AHC. 2L72 4T RTA52EU 19951117007151995111700715 1995 11 17 COMA9560600 419951112A22116229945001 POWER SUPPLY CNDAIRCL600 CL6002B19 EA AUTOPILOT DEFECTIVE A COMAK NONE O OTHER APAPPROACH 1 SO01937CA 7044 IAPS OVERTEMP MESSAGE, AUTOPILOT DISENGAGED. REPLACED THE PWR-4000 POWER SUPPLY. 2L72 4F RTA21EA 19951117007161995111700716EA 1995 11 17 COMA9560601 119951112A3411 PITOT TUBE CNDAIRCL600 CL6002B19 EA FWD FUS CONTAMINATED A COMAK NONE O OTHER UKUNKNOWN 1 SO01936CA 7043 THERE IS A 55 KNOT DIFFERENCE BETWEEN THE NR 1 AND STANDBY AIR SPEED INDICATORS. CLEARED WATER FROM PITOT SYSTEM LINES AND SYSTEM TEST NORMAL. 2L72 4F RTA21EA 19951117007171995111700717EA 1995 11 17 COMA9560602 119951115A2750855D1005 BPSU 855D1005 CNDAIRCL600 CL6002B19 EA LT/RT FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01937CA3901 786 229 7044 FLAPS FAILED AT 30 DEGREES. REPLACED HE LT AND RT FLAP BRAKE AND POSITION SENSOR. 2L72 4F RTA21EA 19951117007181995111700718EA 1995 11 17 COMA9560603 119951115A5210 DOOR LATCH CNDAIRCL600 CL6002B19 EA PAX DOOR LACK OF LUBE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01943CA 7062 CABIN DOOR HANDLE CAME UNLATCHED DURING TAKEOFF. LUBRICATED ROLLERS ON DOOR FRAME AND ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951117007191995111700719EA 1995 11 17 COMA9560604 119951115A7332 WIRE CNDAIRCL600 CL6002B19 1900309EA FUEL PRESSURE CHAFED A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01945CA 7069 LEFT ENGINE LOW FUEL PRESSURE MESSAGE ON EICAS. REPAIRED CHAFED WIRING IN AFT EQUIPMENT BAY AND ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951117007201995111700720EA 1995 11 17 COMA9560605 119951115A34119035025 DRAIN ASSY CNDAIRCL600 CL6002B19 EA PITOT SYST CRACKED A COMAO OTHER J WARNING INDICATION CRCRUISE 1 SO01915CA 7013 EFIS COMPARATOR MESSAGE ON EICAS. REPLACED PITOT SYSTEM DRAINS WHICH HAD BEEN CRACKED BY FREEZING WATER. 2L72 4F RTA21EA 19951117007211995111700721NM 1995 11 17 DL72S954368 119951113A2810 FUEL TANK BOEING727 727232 1384082NM RT WING FUEL LEAK A DALAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11545DA 22494 IN FLIGHT RT WING WAS LEAKING FUEL 3 TO 6 FT INBD FROM WINGTIP. FOUND SEVERAL SCREWS MISSING FROM TANK ACCESS PANEL NR 5. REMOVED PANELS 3, 4 AND 5, CLEANED SEALS, INSTALLED NEW SCREWS, LEAK CHECK NORMAL. 2L73 4F A3WE 19951117007221995111700722NM 1995 11 17 DL72S954377 119951114A5530 ANGLE BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11523DA 21583 FOUND DURING E-2 LETTER CHECK, VERTICAL STAB FORMER ATTACH ANGLE CRACKED AT FIN STA 157.2 AND STR8 LEFT. REPAIRED PER M/M 55-30-0 PAR 2. 2L73 4F A3WE 19951117007231995111700723NM 1995 11 17 DL72S954378 119951114A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11523DA 21583 FOUND DURING E-2 LETTER CHECK, VERT STAB STRINGER CRACKED AT FIN STA 110.4 AND STR 10 LEFT. REPAIRED PER M/M 55-30-0 PAR 3. 2L73 4F A3WE 19951117007241995111700724NM 1995 11 17 DL72S954383 119951114A56105893543109RPR WINSHIELD BOEING727 727232 1384082NM LT COCKPIT DELAMINATED A DALAO OTHER O OTHER CRCRUISE 1 SO11416DA 21258 CAPT WINDSCREEN DELAMINATED, RETARDS VISION. REPLACED WINDSCREEN. 2L73 4F A3WE 19951117007251995111700725NM 1995 11 17 DL72S954396 119951024A5312 BLKHD SUPPORTS BOEING727 727232 1384082NM BS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND AT HMV, RT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAM STRINGER 26R AND 22R, C-1 BIN FS 720D. REPAIRED PER SRM 53-10-9 FIG 9. 2L73 4F A3WE 19951117007261995111700726NM 1995 11 17 DL72S954397 119951024A5312 BLKHD SUPPORTS BOEING727 727232 1384082NM BS 720 WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO11490DA 21020 FOUND AT HMV, LT VERTICAL BULKHEAD SUPPORTS WORN AT FLOATING MOUNT BOLTS TO CABIN FLOORBEAMS ABOVE STRINGER 26L AND 22L, FS 720D C1 BAG BIN. REPAIRED PER SRM 53-10-9 FIG 9. 2L73 4F A3WE 19951117007271995111700727NM 1995 11 17 DL72S954399 119951114A5330655838515 SKIN BOEING727 727232 1384082NM BS 870 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11408DA 21152 THE FUSELAGE SKIN WAS FOUND CORRODED AND CRACKED AT STA 870 STRINGER 10R. ONE CRACK WAS .25 INCH LENGTH AND THE OTHER 1.50 INCH LENGTH. DAMAGE WAS LOCATED IN OVERLAPPED SKIN PANELS FORWARD AND AFT OF THE BUTT SPLICE AND DAMAGE REMOVAL RESULTED IN TWO 2.75 BY 4.75 CUTOUTS. THE SKIN IS MILLED FROM 2024-T351 CLAD PLATE. MAINTENANCE REPORTS THAT THE MAXIMUM THICKNESS AT EITHER CUTOUT LOCATION IS .225. ACCOMPLISHED REPAIRS PER DL ERA 302753-14. 2L73 4F A3WE 19951117007281995111700728NM 1995 11 17 DL72W954393 119951022A5320 ANGLE BOEING727 727247 138408FNM BS 1342 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV-1, INSPECTION FOUND THE CHORD ANGLE CRACKED AT STA 134248 SECTION HORIZONTAL CHORD ANGLE LOC ABOVE S-DUCT. IT IS CRACKED JUST I/B OF RT FIN TERMINAL FITTING. CHORD HAS BEEN PREVIOUSLY STOP DRILLED, CRACK APPEARS TO HAVE CONTINUED PAST STOP DRILL HOLES. REPAIRED CRACK PER M/M 53-11-0 PG 808. 2L73 4F A3WE 19951117007291995111700729NM 1995 11 17 DL72W954394 119951022A5320 ANGLE BOEING727 727247 138408FNM BS 1342 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 AT HMV-1, INSP FOUND CHORD ANGLE CRACKED AT 48 SECTION LT SIDE STA 1342. THE HORIZONTAL CHORD ANGLE IS CRACKED JUST I/B OF FIN TERMINAL FITTING. FITTING IS PREVIOUSLY STOP DRILLED. REPAIRED CRACK PER M/M 53-11-0 PG 808. 2L73 4F A3WE 19951117007301995111700730NM 1995 11 17 DL733954375 119951114A3350 EEL POWER SUPPLY 20131A BOEING737 737347 1384647NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11304WA 23345 BOTH OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L72 4F RTA16WE 19951117007311995111700731NM 1995 11 17 DL733954382 119951111A532065479592 DOOR FRAME BOEING737 737347 1384647NM BS 794.3 CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO11302WA 23182 THE AFT CARGO DOOR OPENING FORWARD FRAME WAS FOUND WITH A .5 INCH CRACK AT THE NR 5 STOP FITTING. THE FRAME IS MADE FROM A 0.071 7075-T6 CLAD MATERIAL. THIS ER/A WILL ALLOW THE USE OF THE SRM TYPICAL FORMED SECTION REPAIR. 2L72 4F RTA16WE 19951117007321995111700732NM 1995 11 17 DL767954374 119951114A2710698812842 SPRING 253T11423 BOEING767 767232 1385132NM AILERON DRUM BROKEN A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO11103DA 22215 ON TAXI OUT, CHECKING CONTROLS F/O SIDE AILERONS EXTREMELY STIFF, VERY DIFFICULT TO MOVE. AFTER INSPECTION FOUND SPRING (P/N 69881284-2), BROKEN ON F/O AILERON DRUM ASSY (P/N 253T1142-3). 2L72 4F RTA1NM 19951117007331995111700733NM 1995 11 17 DL76S954373 119951114A3320 LIGHT SOCKET BOEING767 767332 1382001NM MID GALLEY DIRTY A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO11134DL 25123 MID GALLEY WORK LIGHT SMOKING IN FLT, TURNED OFF LIGHT SMOKE STOPPED. MTC FOUNG COFFEE SPLASHED ON LIGHT SOCKETS. FWD TO MCO DUE TO TIME. SOCKETS NEED CLEANED AND RELAMPED. 2L72 4F RTA1NM 19951117007341995111700734WP 1995 11 17 DLL14954381 119951114A2530 OVEN LKHEED1011 1011385115 5265015WP LWR GALLEY DIRTY A DALAF ACTIVATE FIRE EXT. A FLAME/FIRE CRCRUISE 1 SO111739D 193C1237 NR 6 OVEN LOWER GALLEY GREASE FIRE. C/B PULLED, HALON DISCHARGED. VENT APPEARS CLOGGED WITH FOIL. CLEANED NR 6 OVEN, OK FOR SERVICE. 2L73 4F A23WE 19951117007351995111700735WP 1995 11 17 DLL15954392 119951031A57531529112110AD VANE LKHEED1011 10113853 5265020WP RT TE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11755DL 193Y1184 DURING SHOP INSPECTION, NR 1 RT FLAP VANE WAS FOUND WITH WEAR DAMAGE AT OUTBOARD RUB STRIP 8 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 57-53-00. 2L73 4F A23WE 19951117007361995111700736WP 1995 11 17 MWEA95421 119951116A5320 ANGLE DOUG DC9 DC932 3022066WP BS 980 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND TIP ANGLE OF LAVATORY FLOORBEAM AT STA 980 HAS A SMALL AREA OF CORROSION. MAINTENANCE INSTALLED REPAIR IAW SRM 53-05, FIG 2A. 2L72 4F A6WE 19951117007371995111700737WP 1995 11 17 MWEA95422 119951116A53203924809503 FITTING DOUG DC9 DC932 3022066WP BS 571 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND END FITTING AT LONGERON 30 HAS A CRACK AT STA 571. MAINTENANCE REMOVED AND REPLACED FITTING FROM STA 571 TO 598 PER SRM 51-30. 2L72 4F A6WE 19951117007381995111700738WP 1995 11 17 MWEA95423 119951116A531359203191 LONGERON DOUG DC9 DC932 3022066WP BS 229-415 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 29L IS CORRODED IN NUMEROUS AREAS FROM STA 229 TO 415. MAINTENANCE REMOVED AND REPLACED LONGERON PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117007391995111700739WP 1995 11 17 MWEA95424 119951116A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 332-351 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND INTERCOSTAL AT LONGERON 29R BETWEEN STA 332 TO 351 HAS AREAS OF CORROSION. MAINTENANCE FABRICATED AND INSTALLED AN INTERCOSTAL OF 0.050 INCH 7075-T6 ALUMINUM PER SRM 51-30. 2L72 4F A6WE 19951117007401995111700740WP 1995 11 17 MWEA95425 119951116A53135920319508 LONGERON DOUG DC9 DC932 3022066WP BS 415-572 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 30 IS CORRODED IN SEVERAL AREAS FROM STA 415 TO 572. MAINTENANCE REMOVED AND REPLACED LONGERON PER SRM 51-30. 2L72 4F A6WE 19951117007411995111700741WP 1995 11 17 MWEA95426 119951116A5330 SKIN DOUG DC9 DC932 3022066WP BS 300-337 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE REMOVED A TEMPORARY EXTERNAL SKIN REPAIR AT STA 300 TO 337 FROM LONGERON 24L TO 25L. INSTALLED A PERMANENT REPAIR FROM STA 287 TO 358 FROM LONGERON 24L TO 26L IAW ME53-149 SKETCH PER DAC TELEX ORD-SVC-0300/JSS. 2L72 4F A6WE 19951117007421995111700742WP 1995 11 17 MWEA95427 119951116A531359203192 LONGERON DOUG DC9 DC932 3022066WP BS 229-415 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 30 IS CRACKED IN 3 PLACES. MAINTENANCE REMOVED AND REPLACED LONGERON FROM STA 229 TO 415 PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117007431995111700743WP 1995 11 17 MWEA95428 119951116A5313 LONGERON DOUG DC9 DC932 3022066WP BS 415 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 29L IS CRACKED AT STA 415. MAINTENANCE REMOVED LONGERON FROM SPLICE AT STA 415 TO STA 579. FABRICATED SPLICE FROM 7074-T7351 AND LONGERON FROM 7075-T611. INSTALLED SPLICE AND LONGERON PER SRM 53-01 PG 1 AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117007441995111700744WP 1995 11 17 MWEA95429 119951116A53203924050501 FITTING DOUG DC9 DC932 3022066WP BS 554 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 57133 DURING D-CHECK, MAINTENANCE FOUND LONGERON 28L HAS A CRACKED SPLICE FITTING AT STA 554. MAINTENANCE REMOVED AND REPLACED FITTING FROM STA 554 TO 579 PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951117007451995111700745WP 1995 11 17 MWEA95430 119951116A531159114481 FRAME DOUG DC9 DC932 3022066WP BS 446 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, MAINTENANCE FOUND THE FRAME AT STA 446 FROM LONGERON 26R TO 26L HAS SEVERAL AREAS OF CORROSION. MAINTENANCE REPAIRED FRAME IAW SPLICE REPAIR PER SRM 53-03 FIG 2A. 2L72 4F A6WE 19951117007461995111700746NM 1995 11 17 P5CA9500841 119951115A2761298402 ACTUATOR BOEING747 747122 1384872NM NR 6 SPOILER CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 DURING WALKAROUND, FOUND SEPARATION OF AFT END OF NR 7 GROUND SPOILER ACTUATOR. REPLACED CRACKED ACTUATOR IAW MM 27-11-15. 2L74 4F A20WE 19951117007471995111700747NM 1995 11 17 SCNA95261 119951106A2612106087713 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A SCNAK NONE N FALSE WARNING UKUNKNOWN 1 GL15275AF 22092 THE NUMBER 3 ENGINE FIRE DETECTOR LIGHT ILLUMINATED. REPOSITIONED THE NUMBER 3 FIRE WARNING ELEMENT AND SYSTEM TESTED GOOD IAW MM 26-11-00. 2L73 4F A3WE 19951117007481995111700748NM 1995 11 17 SCNA95267 119951110A2612876633 FIRE CONNECTOR BOEING727 7272A1 138407FNM NR 1 ENGINE LOOSE A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15286SC 21601 DURING EN ROUTE CLIMB, THE NUMBER 1 ENGINE FIRE DETECTION LIGHT FLICKERED ON AND OFF. FOUND FIRE LOOP CONNECTOR D1926 CERAMIC INSULATION DAMAGED, REPLACED CONNECTOR. INSPECTED LOOPS AND ATTACHING WIRING AND FOUND NO OTHER DISCREPANCIES. PERFORMED SYSTEM TEST IAW MM 26-11-01 PAGE 501-502, OPS CHECKED GOOD. 2L73 4F A3WE 19951117007491995111700749NM 1995 11 17 SCNA95268 119951113A3350S106 BATTERY BOEING727 7272J4 1384006NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15285SC 21676 THE FORWARD CEILING MOUNTED EMERGENCY AREA LIGHT TESTED DIM. REMOVED AND REPLACED BATTERIES IN AREA LIGHT, TESTED NORMAL IAW MM 33-50-81. 2L73 4F RTA3WE 19951117007501995111700750NM 1995 11 17 SCNA95269 119951113A3350582214 BATTERY PACK BOEING727 727282 138408TNM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 THE CENTER SECTION OF EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, LIGHTING TESTED GOOD IAW MM 33-50-00. 2L73 4T RTA3WE 19951117007511995111700751NM 1995 11 17 SCNA95270 119951113A2612106087713 FIRE LOOP BOEING727 727227 1384078NM NR 3 ENGINE OUT OF POSITION A SCNAK NONE N FALSE WARNING UKUNKNOWN 1 GL15275AF 22092 THE NUMBER 3 ENGINE FIRE DETECTION LIGHT ILLUMINATED DURING FLIGHT. REPOSITIONED NUMBER 3 ENGINE DETECTOR, SYSTEM CHECKED GOOD IAW MM 26-11-00 PAGE 501. 2L73 4F A3WE 19951117007521995111700752WP 1995 11 17 SCNA95271 119951109A261172130000002 SMOKE DETECTOR DOUG DC10 DC1010 3022110WP NR 3 LAV DIRTY A SCNAK NONE N FALSE WARNING LDLANDING 1 GL15573SC 46905 THE SMOKE DETECTOR IN THE NUMBER 3 LAV SOUNDED DURING LANDING, NO APPARENT REASON. CLEANED SMOKE DETECTOR AND UNIT PASSED SELF TEST. 2L73 4F A22WE 19951117007531995111700753NM 1995 11 17 SCNA95272 119951114A33501619 EEL LAMP BOEING727 727259 138408JNM R 1 DOOR FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE R-1 DOOR SLIDE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. RELAMPED LIGHT AND UNIT TESTED GOOD. 2L73 4F A3WE 19951117007541995111700754NM 1995 11 17 UPS205078 119951115A33505106 BATTERY BOEING727 72731C 1384011NM CABN LOOSE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01926UP 19233 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. FOUND BATTERIES LOOSE. TIGHTENED BATTERIES AND REINSTALLED EMERGENCY EXIT LIGHTS, OPS CK GOOD. 2L73 4F A3WE 19951117007551995111700755NM 1995 11 17 UPS505075 119951113A3350BPS73 BATTERY PACK BOEING757 75724APF 1384969NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01412UP 2385 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK, OPS OK. 2L72 4F RTA2NM 19951117007561995111700756WP 1995 11 17 UPS805027 119951115A5320 TRAP FITTING DOUG DC8 DC871F 302199DWP FS 879-940 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT MAIN LANDING GEAR WHEEL WELL TRAPEZOIDAL FITTING CRACKED. REPAIRED FITTING PER UPS EO DC8-5340-0748A. 2L74 4F RT4A25 19951117007571995111700757WP 1995 11 17 UPS805028 119951115A5730 SKIN DOUG DC8 DC871F 302199DWP WS 304 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01744UP 45944 WHILE IN FOR C-CHECK, MAINTENANCE LT WING LEADING EDGE LOWER SKIN CRACKED 1 INCH AT STA XFS 304. REPAIRED PER UPS EO DC8-5720-7598-A. 2L74 4F RT4A25 19951117007581995111700758WP 1995 11 17 UPS805029 119951115A5712 RIB DOUG DC8 DC871F 302199DWP WS 653.75 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB CRACKED LOWER AFT END XFS 653.75. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-20. 2L74 4F RT4A25 19951117007591995111700759WP 1995 11 17 UPS805030 119951115A5311 FRAME DOUG DC8 DC871F 302199DWP FS 1320 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FRAME CORRODED BEYOND LIMITS FS 1320 LONG 35L-35R. REPAIRED FRAME PER SRM 51-1-0, 51-1-8, 51-1-11, 51-1-20D AND EO DC8-5310-7547A. 2L74 4F RT4A25 19951117007601995111700760WP 1995 11 17 UPS805031 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE LONGERON 36 CORRODED BEYOND LIMITS FS1690. REMOVED DAMAGED SECTION OF LONGERON FS 1690 TO 1717, FABRICATED AND INSTALLED SPLICE SECTION IAW SRM 53-1-0 AND 53-2-2 FIG 10. 2L74 4F RT4A25 19951117007611995111700761WP 1995 11 17 UPS805032 119951115A5320 JAMB FITTING DOUG DC8 DC871F 302199DWP LT FWD EXIT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE LT FWD TYPE 1 DOOR JAMB, UPPER FWD CORNER FITTING IS CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH SRM 51-1-40. 2L74 4F RT4A25 19951117007621995111700762WP 1995 11 17 UPS805033 119951115A5730 SKIN DOUG DC8 DC871F 302199DWP WS 711 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING, LE SKIN CRACKED AT SCREW HOLE XFS 711 ON L E LOWER SIDE. CUT OUT DAMAGED AREA PER SRM 57-2-0, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 57-3-0 AND SRM 57-2-0 AT LT WING LOWER SKIN XFS 711. 2L74 4F RT4A25 19951117007631995111700763WP 1995 11 17 UPS805034 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 32R CORRODED BEYOND LIMITS AND CRACKED STA 1690. REMOVED DAMAGED SECTION, REPLACED WITH LIKE SECTION PER UPS SRM 53-2-2 AND 53-5-1. 2L74 4F RT4A25 19951117007641995111700764WP 1995 11 17 UPS805035 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP BS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 34R CRACKED ON END STA 1690. REMOVED AND REPLACED DAMAGED SECTION PER UPS SRM 53-2-2 AND 5351. 2L74 4F RT4A25 19951117007651995111700765WP 1995 11 17 UPS805036 119951115A5320 SHEAR TIE DOUG DC8 DC871F 302199DWP BS 1700 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHEAR TIE CORRODED BEYOND LIMITS LONG 35R STA 1700. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 53-5-1 AND 51-1-21. 2L74 4F RT4A25 19951117007661995111700766WP 1995 11 17 UPS805037 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 90 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 31L HAS CORRISION AND PREVIOUS REPAIR AT FLIGHT STA 90. REPLACED LONG PER SRM 53-2-2 AND 53-4-1 FIG FROM FS 70 TO FS 210. 2L74 4F RT4A25 19951117007671995111700767WP 1995 11 17 UPS805038 119951115A5712 RIB DOUG DC8 DC871F 302199DWP WS 6.225 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED ABOVE PNUEMATIC DUCT. STOP DRILLED CRACK, FABRICATED ANGLE DOUBLER, FILLED AND INSTALLED IAW SRM 57-20 AND 51-1-20D. 2L74 4F RT4A25 19951117007681995111700768WP 1995 11 17 UPS805039 119951115A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 70-210 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER CORRODED BEYOND LIMITS, STA 210 TO STA 70 AT LONG 31R. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 51-1-21 AND 53-4-1. 2L74 4F RT4A25 19951117007691995111700769WP 1995 11 17 UPS805040 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP BS 270 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG FITTING CRACKED AT STA 270 LONG 31R. REMOVED, FABRICATED AND INSTALLED PER UPS SRM 51-1-0, 51-1-21 AND 51-1-20D. 2L74 4F RT4A25 19951117007701995111700770WP 1995 11 17 UPS805041 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP BS 440-460 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG SPLICE FITTING CRACKED STA 440 TO 460 LONG 17R. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 51-1-20, DOUG DWG 3887799. 2L74 4F RT4A25 19951117007711995111700771WP 1995 11 17 UPS805042 119951115A5320 SUPPORT DOUG DC8 DC871F 302199DWP BS 1520 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CRACKED FRAME TO FLOORBEAM SUPPORT FS 1520 LONG 26L. REPAIRED IAW SRM 53-2-0. 2L74 4F RT4A25 19951117007721995111700772WP 1995 11 17 UPS805043 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP BS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING FS 80 LONG 36 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED END FITTING FROM STATION 70 TO STA 80 AT LONG 36 PER SRM 53-1-0 AND SRM 51-1-21. 2L74 4F RT4A25 19951117007731995111700773WP 1995 11 17 UPS805044 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP BS 70 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND I/B END FITTING CRACKED AT STA 70 LONG 31R. REMOVED AND REPLACED I/B END FITTING AT STA 70 LONG 31R PER SRM 51-1-0 AND SRM 51-1-20D. 2L74 4F RT4A25 19951117007741995111700774WP 1995 11 17 UPS805045 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP BS 100 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED BEYOND LIMITS FS 100 LONG 36. REMOVED AND REPLACED LONG END FITTING PER SRM 53-1-0 AND 51-1-21. 2L74 4F RT4A25 19951117007751995111700775WP 1995 11 17 UPS805046 119951115A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 70-90 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND ANTENNA DOUBLER CORRODED BEYOND LIMITS BS 70 TO BS 90 LONG 35L TO 35R. REMOVED, FABRICATED, AND INSTALLED REPLACMENT ANTENNA DOUBLERS PER SDAC DWS 3649127 SRM 51-1-21, 53-1-0. 2L74 4F RT4A25 19951117007761995111700776WP 1995 11 17 UPS805047 119951115A5320 SPLICE DOUG DC8 DC871F 302199DWP FS 1696 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND BUTT SPLICE CRACKED AND CORRODED AT LONG 28L AT FS 1696. REMOVED AND REPLACED IAW SRM 51-1-21. 2L74 4F RT4A25 19951117007771995111700777WP 1995 11 17 UPS805048 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1540 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 35L CORRODED BEYOND LIMITS STA 1540. FABRICATED LONG SECTION, REMOVED DAMAGE AND INSTALLED FABRICATED SECTION PER SRM 51-1-20D, 53-2-2. 2L74 4F RT4A25 19951117007781995111700778WP 1995 11 17 UPS805049 119951115A5330 SKIN DOUG DC8 DC871F 302199DWP BS 80 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE SKIN BS 80 AT LONGERON 36 CORRODED BEYOND LIMITS FWD OF ANTENNA. REMOVED CORRODED SKIN PANEL FS 70 TO 190 LONG 31L TO 31R PER SRM 51-1-21. FABRICATED REPLACEMENT SKIN PANEL PER DWG 5779925 AND SRM 53-4-1 AND INSTALLED PER SRM 51-1-21 AND SEALED PER SRM 51-1-17. 2L74 4F RT4A25 19951117007791995111700779WP 1995 11 17 UPS805050 119951115A5320 TIE CLIP DOUG DC8 DC871F 302199DWP FS 1120 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1120 BETWEEN LONG 36 AND 35R, TIE CLIP IS OUT OF LIMITS. REPAIRED TIE CLIP IAW SRM 53-2-0. 2L74 4F RT4A25 19951117007801995111700780WP 1995 11 17 UPS805051 119951115A5320 FITTINGS DOUG DC8 DC871F 302199DWP FS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1690 AT LONG 34L AND 35L BATHTUB FITTINGS ARE CORRODED. REMOVED AND REPLACED 2 BATHTUB FITTINGS IAW SRM 53-1-01. 2L74 4F RT4A25 19951117007811995111700781WP 1995 11 17 UPS805052 119951115A5313 LONGERON DOUG DC8 DC871F 302199DWP FS 1340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND STA 1340 LONG 36 LOWER CHORD RADIUS IS OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED FRAME REPAIR IAW SRM 53-2-0. 2L74 4F RT4A25 19951117007821995111700782WP 1995 11 17 UPS805053 119951115A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CRACKED AND CORRODED BEYOND LIMITS, LONG 36 FS 1690. REMOVED AND REPLACED FITTING IAW SRM 53-1-01. 2L74 4F RT4A25 19951117007831995111700783WP 1995 11 17 UPS805054 119951115A53204641324N FITTING DOUG DC8 DC871F 302199DWP FS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION INSIDE BOTH TUB FITTING AT STA 169 LONG 31R. 2L74 4F RT4A25 19951117007841995111700784WP 1995 11 17 UPS805055 119951116A53204641324N FITTING DOUG DC8 DC871F 302199DWP FS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CORRODED AND CRACKED AT FS 1690 LONG 3LR. REMOVED AND REPLACED FITTING IAW SRM 53-1-01. 2L74 4F RT4A25 19951117007851995111700785WP 1995 11 17 UPS805056 119951116A53204641324N FITTING DOUG DC8 DC871F 302199DWP FS 1690 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD END FITTING CRACKED AT FS 1690 LONG 34R. REMOVED AND REPLACED FITTING IAW SRM 53-1-01. 2L74 4F RT4A25 19951117007861995111700786WP 1995 11 17 UPS805057 119951116A5330 SKIN DOUG DC8 DC871F 302199DWP FS 1690-1720 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE AFT SKIN BUCKLED AND CORRODED BEYOND LIMITS AT FS 1690 TO FS 1720, LONG 33L TO LONG 33R. CUT OUT DAMAGED AREA AND SPLICED IN NEW SKIN PANEL PER SRM 53-2-1, FIG 8. 2L74 4F RT4A25 19951117007871995111700787WP 1995 11 17 UPS805058 119951116A532037540231 FITTING DOUG DC8 DC871F 302199DWP BS 300 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED STA 300 LONG 33R. REMOVED AND REPLACED FITTING AT LONG 33R STA 300 IAW SRM 52-2-0 FIG 2D. 2L74 4F RT4A25 19951117007881995111700788WP 1995 11 17 UPS805059 119951116A532037540231 FITTING DOUG DC8 DC871F 302199DWP BS 305 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING CORRODED STA 305 LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 19951117007891995111700789WP 1995 11 17 UPS805060 119951116A532037558251 FITTING DOUG DC8 DC871F 302199DWP BS 340 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING AT STA 340 LONG 33R IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG D. 2L74 4F RT4A25 19951117007901995111700790WP 1995 11 17 UPS805061 119951116A5320 ANGLE DOUG DC8 DC871F 302199DWP FS 1690 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RING SUPPPORT ANGLE FS 1690 CORRODED BEYOND LIMITS, RB 3434 LONG 35L TO 33R. CUT OUT DAMAGED AREA PER SRM 53-2-5 FIG 8C. FABRICATED AND INSTALLED DOUBLER ANGLES AND FILLER PER SRM 53-2-5 FIG 8C. 2L74 4F RT4A25 19951117007911995111700791WP 1995 11 17 UPS805062 119951116A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1340-1360 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FINGER DOUBLER FLS 1340 TO 1360 LONG 30L TO 31L. REMOVED DAMAGED FINGER DOUBLER 31L STA 1350 T0 1430, FABRICATED FINGER DOUBLER AND INSTALLED PER SRM 53-4-1 AND 51-1-21. 2L74 4F RT4A25 19951117007921995111700792WP 1995 11 17 UPS805063 119951116A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1350 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FINGER DOUBLER, ONE EAR BROKEN OFF, STA 1350 LONG 29R TO 30R. REMOVED CORROSION, FOUND SKIN TO BE WITHIN LIMITS AND FINGER DOUBLER TO BE OUT OF LIMITS. FABRICATED FINGER DOUBLER AND INSTALLED ALL PARTS PER UPS SRM 51-1-8, 53-4-1, 51-1-20D AND 51-1-21. 2L74 4F RT4A25 19951117007931995111700793WP 1995 11 17 UPS805064 119951116A5415 FITTING DOUG DC8 DC871F 302199DWP LE NR 3 PLYON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLANGE ON FITTING CRACKED L/E AT PYLON NR 3. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 51-1-20D, 51-1-20, 51-1-21 AND DOUG DWG 5754705. 2L74 4F RT4A25 19951117007941995111700794WP 1995 11 17 UPS805065 119951116A2750 ANGLE DOUG DC8 DC871F 302199DWP WS 98 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SUPPORT ANGLE CRACKED LWR TWO BOLT HOLES VERTICAL ANGLE O/B FLAP ACT BKT WS 98R. REMOVED, FABRICATED AND INSTALLED ANGLE PER DOUG DWG 3643320 AND SRM 51-1-20, 51-1-20D. 2L74 4F RT4A25 19951117007951995111700795WP 1995 11 17 UPS805066 119951116A5311 FRAME DOUG DC8 DC871F 302199DWP BS 180 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED BEYOND LIMITS STA 180 LONG 36. REMOVED, FABRICATED AND INSTALLED FRAME SECTION PER UPS SRM 53-2-0 FIG 2 AND 51-1-21. 2L74 4F RT4A25 19951117007961995111700796WP 1995 11 17 UPS805067 119951116A5712 RIB DOUG DC8 DC871F 302199DWP WS 226 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING RIB CRACKED UPPER AFT END XFS226. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIRS AND DICTS PER M/M 20-16-00 AND UPS SRM 51-3-0, 57-2-0, 51-1-21, 51-1-20D AND M/M 36-11-00 AND 36-11-01. 2L74 4F RT4A25 19951117007971995111700797WP 1995 11 17 UPS805068 119951116A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 240-260 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERNAL ANTENNA DOUBLER CORRODED BEYOND LIMITS STA 240 TO 260 LONG 34L TO 35L. REMOVED, FABRICATED AND INSTALLED ANTENNA DOUBLER PER UPS SRM 51-9-0, 51-1-21. 2L74 4F RT4A25 19951117007981995111700798WP 1995 11 17 UPS805069 119951116A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1540 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND AFT ACC COMPT STA 1540 LONG 33R END FITTING CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED FITTING PER UPS SRM 53-4-1, 51-1-21, 51-1-21, SEALED PER 51-1-11. 2L74 4F RT4A25 19951117007991995111700799WP 1995 11 17 UPS805070 119951116A5320 FITTING DOUG DC8 DC871F 302199DWP BS 1350 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CRACKER AT FWD I/B WALL STA 1350 LONG 36. REMOVED AND REPLACED SPLICE FITTING PER UPS SRM 51-1-20. 2L74 4F RT4A25 19951117008001995111700800WP 1995 11 17 UPS805071 119951116A5320 WEB DOUG DC8 DC871F 302199DWP BS 340 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND C-1 PIT BASKET WEB SEVERELY CORRODED FWD OF STA 340 AT LONG 33R. REMOVED DAMAGED PART OF WEB AND REPAIRED PER DHC SK 729-179. 2L74 4F RT4A25 19951117008011995111700801WP 1995 11 17 UPS805072 119951116A5713 STRINGER DOUG DC8 DC871F 302199DWP WS 484 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND NR 4 ALT TANK STRINGER 54 AT APPROX STA XW484 IS CRACKED ALMOST IN TWO. FABRICATED STRINGER, STRINGER SPLICES AND INSTALLED PER SRM 57-2-2, FIG 3D AND DC8-5710-7559-A. 2L74 4F RT4A25 19951117008021995111700802WP 1995 11 17 UPS805073 119951116A5754 CHORD DOUG DC8 DC871F 302199DWP RT WING L/E CRACKED A IPXAO OTHER O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E AT THE OTBD END OF THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. THE CRACK IS APPROX 1.8 INCH. STOP DRILLED CRACK IAW SRM 57-2-0. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-2-0 FIG D. 2L74 4F RT4A25 19951117008031995111700803WP 1995 11 17 UPS805074 119951116A5320 ANGLE DOUG DC8 DC871F 302199DWP BS 280 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01729UP 46029 WHILE IN FOR D-CHECK, MAINTENANCE FOUND ANGLE CRACKED AT STA 280 ABOVE LONG 36 FWD END OF PIT DOOR. REMOVED AND REPLACED ANGLE PER UPS SRM 53-1-0. 2L74 4F RT4A25 19951117008041995111700804WP 1995 11 17 UPS805079 119951116A5320 ANGLE DOUG DC8 DC871F 302199DWP BS 1610 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE BETWEEN FLOOR WEB AND STIFFENER IN AFT ACCY COMPT FS 1610, ABOVE LONG 23R. REPLACED STIFFENER PER SRM 51-1-20D. 2L74 4F RT4A25 19951117008051995111700805WP 1995 11 17 UPS805080 119951116A53203755822502N FITTING DOUG DC8 DC871F 302199DWP BS 350 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 350, BETWEEN LONG 35L TO 36. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117008061995111700806WP 1995 11 17 UPS805081 119951116A57535652288506 VANE DOUG DC8 DC871F 302199DWP RT WING DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 2 VANE DELAMINATED. REPLACED VANE ASSY PER MM 27-51-14. 2L74 4F RT4A25 19951117008071995111700807WP 1995 11 17 UPS805082 119951116A575556551681 SKIN DOUG DC8 DC871F 302199DWP NR 4 SPOILER DELAMINATION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 4 SPOILER LOWER SURFACE DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01. 2L74 4F RT4A25 19951117008081995111700808WP 1995 11 17 UPS805083 119951116A5320 DOUBLER DOUG DC8 DC871F 302199DWP BS 1583 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND FINGER DOUBLER CRACKED AT FS 1583 LONGERON 31R. REPLACED DOUBLER SECTION PER SRM 51-1-21. 2L74 4F RT4A25 19951117008091995111700809WP 1995 11 17 UPS805084 119951116A53203755822 FITTING DOUG DC8 DC871F 302199DWP BS 270 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 270 LONGERONS 35R TO 36. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117008101995111700810WP 1995 11 17 UPS805085 119951116A53203751062501 FITTING DOUG DC8 DC871F 302199DWP BS 1600 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME TO FLOORBEAM ATTACH FITTING BRACKET CRACKED AT FS 1600 LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117008111995111700811WP 1995 11 17 UPS805086 119951116A5342565172743 ANGLE DOUG DC8 DC871F 302199DWP VERT STAB/FUS CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT REAR SPAR, LOWER FWD SCREW HOLE. REPAIRED PER UPS EO DC8-5310-7584-A. 2L74 4F RT4A25 19951117008121995111700812WP 1995 11 17 UPS805087 119951116A5230 FRAME DOUG DC8 DC871F 302199DWP BAGGAGE DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND D-BAG BIN DOOR HAS A 2 INCH LONG CRACK ON LOWER FRAME TOWARDS AFT CORNER. REPAIRED PER UPS EO AND DC8-5230-6643-A. 2L74 4F RT4A25 19951117008131995111700813WP 1995 11 17 UPS805088 119951116A53203755843501N FITTING DOUG DC8 DC871F 302199DWP BS 1180 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1180 LONGERON 35R. REPLACED FITTING PER SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 19951117008141995111700814WP 1995 11 17 UPS805089 119951116A532037558412 FITTING DOUG DC8 DC871F 302199DWP BS 1250 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED BETWEEN LONGERONS 33R TO 34 FS 1250. REPLACED FITTING PER SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 19951117008151995111700815WP 1995 11 17 UPS805090 119951116A57545769581 SKIN DOUG DC8 DC871F 302199DWP RT LE FLAP CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBD SLOT PANEL HAS 1 INCH LONG CRACK ON TOP SIDE. REPLACED SLOT PANEL PER MM 27-80-01. 2L74 4F RT4A25 19951117008161995111700816WP 1995 11 17 UPS805091 119951116A5312577263837 BLKHD J-BEAM DOUG DC8 DC871F 302199DWP BS 1766 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND 5TH J-BEAM ON AFT SIDE OF PRESSURE BULKHEAD FS 1766 CRACKED AT RADIUS RT CORNER. REPAIRED PER UPS EO DC8-5310-7630-A. 2L74 4F RT4A25 19951117008171995111700817WP 1995 11 17 UPS805092 119951116A531397585023 LONGERON DOUG DC8 DC871F 302199DWP BS 1220-1240 CORROSION A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 30L ANGLE FS 1200 TO 1240. REPAIRED PER UPS EO DC8-5310-7645-A. 2L74 4F RT4A25 19951117008181995111700818WP 1995 11 17 UPS805093 119951116A532037558541 FITTING DOUG DC8 DC871F 302199DWP BS 1200 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK AT STOP FITTING FWD AND AFT SIDES, LONGERON 27L FS 1200. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19951117008191995111700819WP 1995 11 17 UPS805094 119951116A53203755842505N FITTING DOUG DC8 DC871F 302199DWP BS 2100 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01779UP 45479 WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 2100, ABOVE LONERON 28L. REPLACED FITTING PER SRM 53-2-0 FIG 2D. 2L74 4F RT4A25 19951117008201995111700820NM 1995 11 17 95ZZZM624 119951017A3350900835A BATTERY PACK GRIMES BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS T3921 22043 FORWARD RIGHT EXTERIOR OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19951117008211995111700821NM 1995 11 17 AALA950045H 119951012A5315141T5110 FLOOR BEAM BOEING767 767223 1385123NM BS 266 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FOUND FLOOR BEAM HAS CORROSION BEYOND LIMITS. ALODINED, FILLED WITH BMS 5-92 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5095 SEALANT, PRIMED AND PAINTED PER ENGINEERING MRB 767-1025. (M) 2L72 4F RTA1NM 19951117008221995111700822NM 1995 11 17 AALA950046H 119951012A5315141T5112 FLOOR BEAM BOEING767 767223 1385123NM BS 303 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS. FABRICATED REPAIR DOUBLER FROM .050 STAINLESS STEEL INSTALLED WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1026. (M) 2L72 4F RTA1NM 19951117008231995111700823NM 1995 11 17 AALA950047H 119951012A5315141T5111 FLOOR BEAM BOEING767 767223 1385123NM BS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMTS. FABRICATE REPAIR STRAP FROM 0.050 THK CRES AND INSTALL WET PER ENGINEERING MRB 767-1027. (M) 2L72 4F RTA1NM 19951117008241995111700824NM 1995 11 17 AALA950048H 119951012A5315141T5112 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS. FABRICATE REPAIR DOUBLER FROM 0.050 CRES AND INSTALLED WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1028. (M) 2L72 4F RTA1NM 19951117008251995111700825NM 1995 11 17 AALA950049H 119951012A573011T3013 SKIN BOEING767 767223 1385123NM WS 995 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - WING BOX SKIN HAS CORROSION BEYOND SRM LIMITS. BLENDED AND APPROVED FOR CONTINUED SERVICE PER ENGINEERING MRB 767-1029. (M) 2L72 4F RTA1NM 19951117008261995111700826NM 1995 11 17 AALA950053H 119951012A5315111T65007 FLOOR BEAM BOEING767 767223 1385123NM BS 852 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - FOUND CORRODED BEYOND LIMITS. CUT OUT DAMAGED FLOOR BEAM AND INSTALLED REPAIR SPLICE PER ENGINEERING MRB 767-1031. (M) 2L72 4F RTA1NM 19951117008271995111700827NM 1995 11 17 AALA951716 119950924A3350 EEL WIRE BOEING727 727227 1384078NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07730AA 20737 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN AND FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRE FOR EXIT LIGHT AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008281995111700828EU 1995 11 17 AALA951722 119950926A3350A3060720101 EEL CONDUCTOR AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0711060 470 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 12H TO 15H INOPERATIVE. REPLACED FLAT CONDUCTOR WIRE BY PASSENGER SEAT ROW 12H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19951117008291995111700829WP 1995 11 17 AALA951741 119951002A3350A3060720204 EEL CONDUCTOR DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07563AA 49345 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 19951117008301995111700830NM 1995 11 17 AALA951743 119951002A3222 STRUT BOEING727 727223 1384074NM NLG NEEDED REPACK A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07889AA 21527 DFW - FLRN NR 1310 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, THE DOORS LIGHT ABOVE THE LANDING GEAR HANDLE REMAINED ILLUMINATED WITH CORRESPONDING NOSE LANDING GEAR DOOR LIGHT ILLUMINATED ON F/E PANEL. EXTENDED LANDING GEAR AND AIRCRAFT RETURNED TO DFW, LANDING WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND REPLACED UPPER GLAND NUT. SERVICED NOSE LANDING GEAR STRUT WITH OIL AND NITROGEN. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008311995111700831NM 1995 11 17 AALA951756 119951004A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07898AA 22014 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD END OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT AFT END OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008321995111700832NM 1995 11 17 AALA951761 119951008A3233651781915 LOCK ACTUATOR BOEING727 727223 1384074NM LT MLG DOOR DEFECTIVE A AALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW07701AA 22459 RDU - FLT NR 1040 - DURING APPROACH WHEN LOWERING GEAR THE LEFT GEAR DOOR, LIGHT AND RED GEAR LIGHT ILLUMINATED. CYCLED GEAR WITH SAME RESULTS. DID FLY BY AND CONFIRM LEFT MLG DID NOT EXTEND. MANUALLY LOWERED GEAR AND RECEIVED THREE GREEN DOWN AND LOCKED LIGHTS. GEAR WAS HEARD FALLING DOWN. LANDED RDU WITHOUT INCIDENT. REPLACE SEQUENCE DOOR LOCK ACUTATOR AND ACCOMPLISH RETRACTION AND EXTENSION OF LEFT MLG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008331995111700833NE 1995 11 17 AALA951762 219951009A7510577957 HEAT VALVE BOEING727 727223 1384074NM PWA JT8 JT8D9 52048NE NR 3 ENGINE DEFECTIVE A AALAE ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SW07849AA 20990 ALT - FLT NR 1142 - WHILE EN ROUTE DFW-ATL, THE NR 3 ENGINE FUEL HEAT VALVE BECAME STUCK IN THE OPEN POSITION, RESULTING IN ABNORMALLY HIGH OIL TEMPERATURE. SHUT DOWN NR 3 ENGINE. LANDED ATL WITHOUT INCIDENT. REPLACED NR 3 FUEL HEAT VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F4 F A3WE E2EA 19951117008341995111700834 1995 11 17 AALA951770 419951010A2565101623303 SLIDE BFGOODRICH BOEING767 767223 1385123NM FWD ENTRY DOOR DEFECTIVE A AALAK NONE O OTHER ININSP/MAINT 1 SW072FOR A3023 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE HAD SEAM DEFECTS AND POROSITY LEAKS. EMERGENCY EVACUATION SLIDE SCRAPPED. (M) 2L72 4F RTA1NM 19951117008351995111700835NM 1995 11 17 AALA951773 119951010A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW076818 19493 DFW - DURING OVERNIGHT CHECK, FOUND THE MID CABIN EMERGENCY LIGHT SIGN INOPERATIVE. REPAIRED CONNECTOR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008361995111700836NM 1995 11 17 AALA951786 119951013A33505013CW EEL BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07865AA 21370 DFW - DURING OVERNIGHT CHECK, FOUND OVERHEAD EMERGENCY LIGHT AT SEAT ROW 25 INOPERATIVE. REPLACED OVERHEAD EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951117008371995111700837NM 1995 11 17 AWXA9500703 119951010A5314 KEEL BEAM BOEING737 73733A 1384673NM FWD FUS CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND TWO CRACKS IN KEEL BEAM SKIN BETWEEN WHEEL WELL. REPAIRED CRACKS PER SRM 53-60-12, FIGURE 202. (M) 2L72 4F RTA16WE 19951117008381995111700838NM 1995 11 17 AWXA9500704 119951010A5315 FLOOR BEAM BOEING737 73733A 1384673NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FLOOR BEAM CORRODED AT NUT PLATE HOLES, STATION 986.5 RBL 23.5 TO RBL 40. (M) 2L72 4F RTA16WE 19951117008391995111700839NM 1995 11 17 AWXA9500705 119951010A5230 SKIN BOEING737 73733A 1384673NM FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DUIRNG SCHEDULED C11 INSPECTION, FOUND FORWARD CARGO DOOR OUTER SKIN CRACKED AT DOOR HANDLE FLAPPER DOOR CUTOUT. REPAIRED PER ER 1-52-30-01B. (M) 2L72 4F RTA16WE 19951117008401995111700840NM 1995 11 17 AWXA9500706 119951010A5230 SKIN BOEING737 73733A 1384673NM FWD GALLEY DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND FORWARD GALLEY DOOR OUTER SKIN CUTOUT FOR UPPER HINGE CRACKED IN LOWER AFT RADIUS CORNER. FABRICATED AND INSTALLED DOUBLER REPAIR PER ER 3-52-48-04A. (M) 2L72 4F RTA16WE 19951117008411995111700841NM 1995 11 17 AWXA9500707 119951010A5320 THRESHOLD BOEING737 73733A 1384673NM L2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND L2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-11. (M) 2L72 4F RTA16WE 19951117008421995111700842NM 1995 11 17 AWXA9500708 119951010A5320 THRESHOLD BOEING737 73733A 1384673NM R2 DOOR CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND R2 DOOR THRESHOLD CHORD NUT PLATE HOLE CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-70-11. (M) 2L72 4F RTA16WE 19951117008431995111700843NM 1995 11 17 AWXA9500709 119951010A5320 BRACKET BOEING737 73733A 1384673NM COCKPIT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX - DURING SCHEDULED C11 INSPECTION, FOUND SUPPORT BRACKET CRACKED UNDER NOSE GEAR VIEWING WINDOW PANEL. FABRICATED AND INSTALLED NEW ANGLE BRACKET AND DOUBLER PER SRM 51-10-25. (M) 2L72 4F RTA16WE 19951117008441995111700844NM 1995 11 17 AWXA9500710 119951014A5753 FLAP TRACK BOEING737 737112 1384412NM LT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28708AW 19771 PHX - DURING SCHEDULED C21 INSPECTION, FOUND LT WING NR 2 FLAP TRACK AFT OUTBOARD MOUNT HOLE CORRODED AT BUSHING. COMPLIED WITH OVERSIZING OF MOUNT HOLE PER ER 2-57-44-19A. (M) 2L72 4F A16WE 19951117008451995111700845NM 1995 11 17 AWXA9500711 119951014A575365671581 FLAP TRACK BOEING737 737112 1384412NM RT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28708AW 2350 19771 PHX - DURING SCHEDULED C21 INSPECTION, FOUND CORROSION BETWEEN WING SHIM AND NR 8 FLAP TRACK AFT MOUNTING. REPAIRED PER ER 2-57-40-15A. (M) 2L72 4F A16WE 19951117008461995111700846NM 1995 11 17 AWXA9500712 119951014A575365671582 FLAP TRACK BOEING737 737112 1384412NM RT WING CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28708AW 0430 19771 PHX - DURING SCHEDULED C21 INSPECTION, FOUND NR 7 FLAP TRACK CORRODED ON UPPER SURFACE WHERE TRACK MOUNTS TO WING. ALSO, FOUND SMALL NICK ON ONE BOLT HOLE. REPAIRED PER ER 2-57-40 15A. (M) 2L72 4F A16WE 19951117008471995111700847NM 1995 11 17 AWXA9500713 119951018A2910AS116080264 HOSE BOEING737 7373S3 1384711NM B-HYD SYSTEM FAILED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 WP28313AW 23712 PHX - FLT 460 - DURING FINAL APPROACH TO PHX, THE B-SYSTEM HYDRAULIC QUANTITY STARTED DECREASING. B-SYSTEM WAS SHUT DOWN AND AIRCRAFT CONTINUED TO PHX, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC PRESSURE LINE FROM PUMP TO HYDRALIC PRESSURE MODULE. LEAK CHECK COMPLIED WITH. NO LEAKS NOTED. (M) 2L72 4F RTA16WE 19951117008481995111700848EU 1995 11 17 AWXA9500714 119951018A3350321430 BATTERY PACK AIRBUS320 A320231 3930325EU CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28634AW 091 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM SEATS 4ABC TO 10ABC. REMOVED AND REPLACED BATTERY PACK AT 2L, OPS CHECK GOOD. (M) 2L72 4F RTA28NM 19951117008491995111700849NM 1995 11 17 AWXA9500715 119951020A335020211 EEL LOGIC UNIT BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28302AW 24009 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 7 THROUGH 9 OVERHEAD BULLNOSE. REPLACED OVERHEAD RT CENTER CHARGER LOGIC UNIT, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008501995111700850NM 1995 11 17 AWXA9500716 119951022A3350276005 EEL FUSE BOEING737 7373G7 1384595NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28303AW 24010 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED FUSE IN BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008511995111700851NM 1995 11 17 AWXA9500718 119951022A5220 MECHANISM BOEING757 7572G7 1384963NM L2 DOOR LACK OF LUBE A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28910AW 24523 PHX/SAN - FLT NR 19 - AIR TURNBACK, L2 DOOR WARNING LIGHT ILLUMINATED DURING CLIMB-OUT OF PHX. FLIGHT CREW VERIFIED HANDLE WAS ROTATED TOWARD OPEN, AND MANUALLY HELD HANDLE DOWN. AIRCRAFT RETURNED TO PHX, LANDING WITH FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED MICRO-SWITCH PLUNGER, AND CHECKED DOOR RIB IAW BMM 52-11-01 AND 52-11-00. CYCLED DOOR TEN TIMES, ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19951117008521995111700852WP 1995 11 17 IXXA199587 119951013A57535751182 FLAP FITTING DOUG DC8 DC871 302199AWP WS 98 BROKEN A IXXAK NONE O OTHER ININSP/MAINT 1 GL23824BX15249 45946 AT MSP, IT WAS DISCOVERED THAT THE STATION 98 OUTBOARD FLAP BASE FITTING ON LEFT INBOARD FLAP SECTION HAD EXPERIENCED A TYPICAL FAILURE DUE TO A CRACK THAT ORIGINATED IN THE UPPER FLAP VANE ATTACH BOLT HOLE. THE OPPOSING BASE FITTING AT THAT STATION HAD RECIEVED SUBSEQUENT DAMAGE. THE LEFT INBOARD FLAP SECTION WAS REMOVED AND REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951117008531995111700853NM 1995 11 17 MRKA9571 119951006A3350862100601 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 AISLE EMERGENCY EXIT LIGHTS INOP. BATTERY PACK DEAD. REMOVED AND REPLACED FLOOR PROXIMITY BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008541995111700854NM 1995 11 17 MRKA9572 119951006A335086101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 LEFT EMERGENCY LIGHTS INOP. BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008551995111700855NM 1995 11 17 MRKA9573 119951010A3350862100601 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 FLOOR PROXIMITY BATTERY PACK LOW. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008561995111700856NM 1995 11 17 MRKA9574 119951010A3350862101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE O OTHER ININSP/MAINT 1 AL03673MA 23124 RIGHT OVERWING EMERGENCY BATTERY PACK HAS A LOW CHARGE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. (M) 2L72 4F RTA16WE 19951117008571995111700857NM 1995 11 17 MRKA9575 119951010A3350862101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 LEFT OVERWING EMERGENCY BATTERY PACK HAS A LOW CHARGE. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008581995111700858NM 1995 11 17 MRKA9576 119951010A3350862101401 EEL BATTERY PACK BOEING737 7372X6C 1384552NM CABIN CORRODED A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03673MA 23124 BATTERY PACK AT R-2 WAS FOUND CORRODED. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951117008591995111700859EU 1995 11 17 USAA951095 119950929A5532 SKIN FOKKERF28 F28MK1000 4990808EU VERT STAB GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19868US12408 11313 PIT - C-1 CHECK INSPECTION, FOUND GOUGE 5 INCH LENGTH AND .047 DEEP, MAXIMUM AT THE TOP IN VERTICAL STAB RIGHT SIDE NEAR RIB NR 5, UNDER ICE SCRAPPER. INSTALLED EXTERNAL DOUBLER REPAIR PER USAIR EA NR 31389. (M) 2L72 4F RTA20EU 19951117008601995111700860WP 1995 11 17 95ZZZM625 119951016A7331101MK14 FFR LUCAS LKHEED1011 10113851 5265010WP RROYCERB211 RB21122* 54555NE NR 2 ENGINE FAILED A RIAAAJ UNSCHED LANDING DUMP FUEL R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO19313EA B1464 193A1020 10218 NR 2 ENGINE LOST POWER AFTER TAKEOFF POWER RETARDED ITSELF TO 80 PERCENT N1. AIRCRAFT DUMPED FUEL AND RETURNED TO GATE. CHANGED FFR TO CORRECT PROBLEM AND CHANGED FUEL PUMP AS A PRECAUTIONARY MEASURE. ACCOMPLISHED NORMAL ENGINE RUN AND RETURNED AIRCRAFT TO SERVICE. (M) 2L73 4F4 F A23WE A12EU 19951117008611995111700861NM 1995 11 17 95ZZZM626 119950822A5330 SKIN BOEING727 727231 1384079NM FS 720 WORN A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554348 21967 MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN APPROXIMATELY .035 INCH AT STRINGER 19L, STATION 720E. REPAIRED PER ARA 9388. (M) 2L73 4F A3WE 19951117008621995111700862WP 1995 11 17 95ZZZM627 119950928A253061171034351 SERVING CART LKHEED1011 10113851 5265010WP GALLEY FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531014 193B1036 SFO - DURING CRUISE SERVING CART EMITTED SMOKE AND ELECTRICAL ODOR. DISCONNECTED SERVING CART. FOUND DEFECTIVE POWER CORD ON SERVING CART. REPLACED SERVING CART, MFG P/N 611-710345-1. OPERATION CHECKED NORMAL. (M) 2L73 4F A23WE 19951117008631995111700863NM 1995 11 17 95ZZZM628 119950929A3230651781915 UPLOCK ACT BOEING727 727231 1384079NM RT MLG FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0554329 20307 STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED. EXTENDING LANDING GEAR WAS NORMAL. FOUND RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR, MFG P/N 65-17819-15, ROD END FRACTURED. REPLACED UPLOCK ACTUATOR AND RIGHT MAIN LANDING GEAR UPLOCK OPERATION CHECKED NORMAL. (M) 2L73 4F A3WE 19951117008641995111700864NM 1995 11 17 95ZZZM629 119950811A5313 STRINGER BOEING727 727231 1384079NM FS 990 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554348 21967 MCI - DURING OP-17, FOUND CORROSION ON RIGHT OUTBOARD FLANGE, STRINGER 29R, FS 990. REMOVED CORROSION PER SSRM 51-10-6 AND REPLACED STRINGER 29R PER SSRM 53-10-213. (M) 2L73 4F A3WE 19951117008651995111700865WP 1995 11 17 95ZZZM630 119951014A2120 AIR DISTR LKHEED1011 10113851 5265010WP CABIN ODOR A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE0511004 193B1016 JFK - DURING DESCENT, BURNING ODOR DETECTED IN CABIN NEAR R3 DOOR. IN DEPTH VISUAL INSPECTION OF CEILING WIRING AND ELECTRICAL COMPONENTS AND AN OPERATION CHECK OF ALL CABIN LIGHTS AND MUX SYSTEM, INCLUDING OPERATION CHECK OF R-3 DOOR, WAS PERFORMED. (M) 2L73 4F A23WE 19951117008661995111700866NM 1995 11 17 95ZZZM631 119951015A7930MEGA008032 BYPASS SW BOEING727 727231 1384079NM NR 3 ENGINE FAILED A TWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0554327 20234 STL - DURING CLIMB NR 3 ENGINE, S/N 3901, OIL BYPASS LIGHT CAME ON. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED FROM FLIGHT. REPLACED NR 3 ENGINE BYPASS SWITCH, MFG P/N MEGA00803-2, REPLACED FILTER, DRAINED AND RESERVICED OIL. PERFORMED HI-POWER RUNUP, REMOVED AND REPLACED FILTER. ENGINE OPERATION AND FILTER CHECKS NORMAL. (M) 2L73 4F A3WE 19951117008671995111700867NM 1995 11 17 95ZZZM632 119950919A5320 CASTING BOEING727 727231 1384079NM FS 940 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0594314 20047 MCI - DURING C-CHECK, FOUND AFT END OF FLOOR BEAM CASTING CRACKED, FS 940. REPAIRED PER ARA 9659. (M) 2L73 4F A3WE 19951117008681995111700868WP 1995 11 17 95ZZZM633 119950911A5347 SEAT TRACK DOUG DC9 DC915 3022036WP FS 237 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05971Z 45773 STL - DURING OP-9, FOUND CORROSION IN NR 2 GALLEY RIGHT CABIN OUTBOARD SEAT TRACK MOUNT AREA, STATION 237. INSTALLED NEW SEAT TRACK PER SRM 53-05, FIGURE 4. (M) 2L72 4F A6WE 19951117008691995111700869NM 1995 11 17 95ZZZM634 119950913A5315 FLOOR BEAM BOEING727 727231 1384079NM FS 740 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554326 20233 MCI - DURING C-CHECK, FOUND 2 INCH CRACK IN CABIN FLOOR BEAM RADIUS AT NR 4 CHAIR TRACK, RBL 48, STATION 740. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLES PER SSRM 53-40-03. (M) 2L73 4F A3WE 19951117008701995111700870WP 1995 11 17 95ZZZM635 119950925A5312 BLKHD PANEL LKHEED1011 10113851 5265010WP PRESS BLKHD CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531014 193B1036 JFK - DURING C-CHECK, FOUND A 3.5 INCH CRACK IN AFT PRESSURE BULKHEAD TOP LEFT GORE PANEL. REPAIRED PER LOCKHEED SERVICE BULLETIN 93-53-258, PAGES 15 AND 16, FIGURE 4. 2L73 4F A23WE 19951117008711995111700871NE 1995 11 17 95ZZZM636 219950929A73143782017 FUEL PUMP BOEING727 727231 1384079NM PWA JT8 JT8D7B 52053NE NR 3 ENGINE DEFECTIVE A TWAAE ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 CE0554335 20462 STL - DURING TAKEOFF NR 3 ENGINE, S/N 4018, SPUN DOWN. SHUT DOWN ENGINE PER FLIGHT HANDBOOK PROCEDURES. FOUND DEFECTIVE FUEL PUMP, MFG P/N 378201-7. REPLACED ENGINE DRIVEN FUEL PUMP. ENGINE OPERATION THEN CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 19951117008721995111700872WP 1995 11 17 95ZZZM637 119950822A5730 SKIN DOUG DC9 DC932 3022066WP RT WING TANK CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05997Z 47029 MCI - DURING OP-15, FOUND CORROSION IN RIGHT WING TANK AROUND FASTENER IN STRINGER 11, BETWEEN STRINGERS 69 AND 91.0. REMOVED CORROSION PER SRM 51-10-3, REPAIRED PER ATA 9183 AND STANDARD PRACTICES. 2L72 4F A6WE 19951117008731995111700873NM 1995 11 17 95ZZZM638 119950822A5330 SKIN BOEING727 727231 1384079NM FUSELAGE WORN A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554348 21967 MCI - DURING OP-17, FOUND FUSELAGE SKIN WORN .015 INCH, STRINGER 17L. REPAIRED PER ARA 9388. 2L73 4F A3WE 19951117008741995111700874WP 1995 11 17 95ZZZM639 119950822A5711 SPAR DOUG DC9 DC932 3022066WP RT WING CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05997Z 47029 MCI - DURING OP-15, FOUND CRACK IN LOWER REAR SPAR HORIZONTAL LEG OF RIGHT WING TANK, FROM HOLE IN AFT ROW TO RADIUS. REMOVED CRACK PER STANDARD PRACTICES AND SRM 51-10-1, REPAIRED PER ARA 9184. (M) 2L72 4F A6WE 19951117008751995111700875NE 1995 11 17 95ZZZM640 219951003A73217911004087 EEC BOEING767 7673Y0 NM PWA JT9 JT9D* NE RT ENGINE MALFUNCTIONED A TWAAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 CE052FOR 24953 BGR - DURING CRUISE SHUT DOWN RIGHT ENGINE, S/N 4704, DUE TO SURGING WITH ACCOMPANYING VIBRATION. FOUND ENGINE ELECTRONIC CONTROL COMPUTER, MFG P/N 791100-4-087, AND FUEL METERING UNIT, MFG P/N 801000-3, MALFUNCTIONING. REPLACED ENGINE ELECTRONIC CONTROL COMPUTER AND FUEL METERING UNIT, AND ENGINE OPERATION CHECKED NORMAL. 2L72 4F4 FRTA1NM E20EA 19951117008761995111700876WP 1995 11 17 BUFA9522 119951003A79211544051 OIL COOLER PWA 154405 DOUG DC8 DC861 3021952WP NR 1 ENGINE MALFUNCTIONED A BUFAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 CE05915BV 371919 45981 MIA-MCI - SHUT DOWN NR 1 ENGINE, OIL TEMPERATURE 143 DEGREES AND RISING, CSD RISE TEMPERATURE PLUS 15 DEGREES, RETURNED TO MIA. REMOVED AND REPLACED NR 1 ENGINE OIL COOLER. OP CHECK GOOD IAW 79-00. (M) 2L74 4F 4A25 19951117008771995111700877SO 1995 11 17 C2XA95IA290 119951019A572012017057007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 AND NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117008781995111700878SO 1995 11 17 C2XA95IA291 119951019A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 AND NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117008791995111700879SO 1995 11 17 C2XA95IA292 119951019A572012017057005 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 AND NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117008801995111700880SO 1995 11 17 C2XA95IA293 119951019A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15 AND NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M0 2L72 4T RTA31SO 19951117008811995111700881SO 1995 11 17 C2XA95IA294 119951019A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15 AND NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117008821995111700882SO 1995 11 17 C2XA95IA295 119951019A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15 AND NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117008831995111700883WP 1995 11 17 CAL950906 119950929A5311 FRAME DOUG DC9 DC932 3022066WP BS 37 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT OVERHEAD FRAME IN FORWARD ACCESSORY COMPARTMENT AT STATION 37. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-05. (M) 2L72 4F A6WE 19951117008841995111700884WP 1995 11 17 CAL950907 119950927A5320 WINDOW FRAME DOUG DC9 DC932 3022066WP LT NR 23 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A .25 INCH CRACK IN LEFT WINDOW NR 23 FRAME. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 2. (M) 2L72 4F A6WE 19951117008851995111700885WP 1995 11 17 CAL950908 119950927A5311 FRAME DOUG DC9 DC932 3022066WP BS 870 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND CORROSION ON BELT FRAME IN AFT BAGGAGE BIN AT STATION 870. THE CORROSION WAS REMOVED AFTER REMOVING THE FASTENERS. THE AREA WAS ALODINED AND PRIMED AND THE FASTENERS WERE REINSTALLED. THE REPAIR WAS PERFORMED IAW SRM 51-10-3 AND 51-30-0. (M) 2L72 4F A6WE 19951117008861995111700886WP 1995 11 17 CAL950909 119950927A5330 SKIN DOUG DC9 DC932 3022066WP BS 990 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND A 1 INCH CRACK AT RIVET OF FUSELAGE SKIN STATION 990, LONGERON 14L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 41. (M) 2L72 4F A6WE 19951117008871995111700887NE 1995 11 17 CAL950912 219951012A7230790762 SUPPORT SHELF DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE BROKEN A CALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW099387522409 49125 717400 FLT NR 477 - RDU - THE NR 1 ENGINE COMPRESSOR BEGAN TO STALL AT FL 310 WHILE EN ROUTE FROM EWR TO TPA. THE STALL WAS ACCOMPANIED BY A LOUD BANGING IN REAR OF AIRCRAFT. THE NR 1 ENGINE WAS BROUGHT TO IDLE AND THE STALLING CEASED. THE AIRCRAFT WAS DIVERTED TO RDU WHERE IT LANDED WITHOUT INCIDENT. A BOROSCOPE OF THE NR 1 ENGINE FOUND THE 6TH AND 7TH STAGE COMPRESSOR DAMAGED. THE NR 1 ENGINE WAS REMOVED AND REPLACED. A POWER ASSURANCE/TRIM RUN WAS PERFORMED IAW MM 71-00-00 AND ALL PARAMETERS WERE NORMAL. INVESTIGATION REVEALED AN 8TH STAGE STATOR SUPPORT SHELF HAD BROKEN OUT AND WAS THE PRIMARY CAUSE OF ENGINE FAILURE. (M) 2L72 4F4 F A6WE E9NE 19951117008881995111700888WP 1995 11 17 CAL950913 119951112A3350 EEL WIRES DOUG DC9 DC932 3022066WP CABIN BROKEN A CALAK NONE L NO TEST ININSP/MAINT 1 SW0927509 47798 FLT NR 1080 - IAH - AN EMERGENCY FLOOR TRACK LIGHT IN FORWARD COACH SECTION WAS FOUND PULLED LOOSE AND THE LIGHT WAS INOPERATIVE. MAINTENANCE FOUND THE TRACK LIGHT HAD BROKEN WIRES. THE WIRING WAS REPAIRED AND THE TRACK WAS REINSTALLED. (M) 2L72 4F A6WE 19951117008891995111700889WP 1995 11 17 CAL950918 119951014A2421 GENERATOR GARRTT 3812761 DOUG DC9 DC982 3022082WP NR 1 ENGINE FAILED A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0916807 P231 49261 FLT 0462 - LAX - THE NR 1 ENGINE GENERATOR FAILED IN FLIGHT AND WOULD NOT RESET. THE APU WAS STARTED TO COVER BUS. THE APU GENERATOR SUBSEQUENTLY FAILED AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE APU INLET SCREEN DIRTY. THE INLET SCREEN WAS CLEANED. THE APU WAS RUN FOR 30 MINUTES AND APU GENERATOR FREQUENCY AND VOLTAGE WAS NORMAL. IN ADDITION, THE NR 1 ENGINE GENERATOR, CSD, AND CSD OIL COOLER WERE REMOVED AND REPLACED. LEAK AND OP CHECKS WERE GOOD. (M) 2L72 4F A6WE 19951117008901995111700890WP 1995 11 17 CAL950930 119950926A5311 BELT FRAME DOUG DC9 DC932 3022066WP BS 64398 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW0912539 45792 HOU - INSPECTION FOUND CORROSION ON BELTFRAME FROM LONGERON 25L TO 24R AT STATION 832. THE CORROSION WAS REMOVED. A DOUBLER AND REPAIR ANGLE WERE INSTALLED IAW SRM 53-03, FIGURE 5. (M) 2L72 4F A6WE 19951117008911995111700891WP 1995 11 17 CAL950931 119951004A5320 ANGLE DOUG DC9 DC932 3022066WP FS 990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091253964398 45792 HOU - INSPECTION FOUND CUSP ANGLE CORRODED ON LOWER FRAME AT FS 990, LEFT SIDE. THE CORRODED SECTION OF CUSP ANGLE WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 25. (M) 2L72 4F A6WE 19951117008921995111700892WP 1995 11 17 CAL950932 119951007A5320101372007 ANGLE DOUG DC9 DC931 3022065WP FS 926 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091456466007 47490 STA 31J - INSPECTION FOUND CORROSION ON L-ANGLE ATTACHED TO FLOOR BEAM AT FS 926, LBL 25. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-05-0 AND SRM 51-40-2. (M) 2L72 4F A6WE 19951117008931995111700893NE 1995 11 17 IXXA199588 219951014A7510B650510 AI DUCT SEAL DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 1 NOSE COWL BLOWN ALAIXXAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 GL23788AL 45999 EN ROUTE FROM BDL TO SJU - THE UPPER HALF OF THE NR 1 ENGINE OUTBOARD COWL DOOR PEELED OFF, LEAVING ITS LOWER HALF FIRMLY LATCHED IN PLACE ON THE NR 1 ENGINE. INSPECTION ON THE GROUND IN SJU, REVEALED BLOWN NOSE COWL ANTI-ICE DUCT SEALS, A 3 INCH BY 6 INCH OVAL ACCESS PLATE BLOWN FROM THE AFT BULKHEAD OF THE NOSE COWL, AND PYLON APRON DAMAGE. SUBMITTER STATES, THE PROBABLE CAUSE OCCURED WHEN THE ENGINE ANTI-ICE WAS APPLIED. THE NOSE COWL ANTI-ICE DUCT SEALS THEN BLEW. THIS PRESS BLEW THE OUTBOARD COWL DOOR. THE BLOWN ANTI-ICE DUCT SEALS WERE REPLACED, THE PYLON APRON WAS REPAIRED, AND THE COWLING DOOR WAS REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F4 F 4A25 1E8 19951117008941995111700894EU 1995 11 17 PAYA95A4038 119951010A3230E0242AZ28A0 RELAY AEROSPATR42 ATR42300 8680920EU NLG FAILED A PAYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA174208G 086 FLT 7727 - JFK-BWI - NOSE GEAR SLOW TO RETRACT. THUMPING NOISE HEARD IN GEAR WELL. REMOVED AND REPLACED RELAY. OPS CHECKED SYSTEM IAW JIC. OPS CHECKS NORMAL. (M) 2H72 4T RTA53EU 19951117008951995111700895EU 1995 11 17 PAYA95A4039 119951012A32341005383Y00REVC CONTROL VLV AEROSPATR42 ATR42300 8680920EU LANDING GEAR INTERMITTENT A PAYAO OTHER J WARNING INDICATION LDLANDING 1 EA174208G 086 FLT NR 7736 - JFK-DCA - LANDING GEAR EXTENSION INTERMITTENT. REPLACED LANDING GEAR CONTROL VALVE. A/C OPERATED ON LEG IAW THE MEL TO RETURN TO PNE FOR REPAIR. (M) 2H72 4T RTA53EU 19951117008961995111700896CE 1995 11 17 S2YA950024 119951018A2120 AIR DISTR BEECH 1900 1900D 1154162CE COCKPIT ODOR A S2YAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL13145SK UE145 AS FLT 1093 - MKE-LSE - PROGRESSING IN THE AREA NORTH OF MSN, THE CREW NOTICED THE SMELL OF SMOKE IN THE CABIN, THOUGHT TO BE ENVIRONMENTAL. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO MSN. A MECHANIC WAS FLOWN THERE, HE GROUND RAN THE AIRCRAFT WITH ALL ELECTRICAL AND ENVIRONMENTAL SYSTEMS ON AND OPERATIONAL CHECKED GOOD. (M) 2L72 4T RTA24CE 19951117008971995111700897EU 1995 11 17 SIMA952811 119951008A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21235RM9047 290 235 RFD - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE PASSENGER ENTRANCE STAIR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY, IAW ATR 42 JIC 33-51-24. OPS CHECK IAW ATR 42 JIC 33-50-00. OPS CHECK WAS GOOD. AIRCRAFT WAS OK FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19951117008981995111700898EU 1995 11 17 SIMA952891 119951016A2710ASNA240305 BEARING AEROSP S27112012002AEROSPATR72 ATR72212 EU LT AILERON LOOSE A SIMAK NONE O OTHER ININSP/MAINT 1 SW21248AT 248 DFW - DURING COMPLIANCE OF ENGINEERING ORDER E9-2700-001 REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM (AD 93-22-10). MAINTENANCE FOUND THE NR 4 IDLER ARM IN THE LEFT WING WITH A LOOSE BEARING. IDLER ARM WAS REMOVED AND REPAIRED BY INSTALLING A NEW BEARING IAW SRM 51-25-21. MAINTENANCE REINSTALLED IDLER ARM ON AIRCRAFT. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951117008991995111700899SW 1995 11 17 95ZZZM641 119951009A32302752000191 TQ TUBE ARM SWRNGNSA227 SA227AC 8780603SW NLG CORRODED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15438MA AC721B FLT NR 3192 - ON CLIMB-OUT FROM DTW, THE CREW NOTED A STEADY THUMPING FROM THE NOSE GEAR AREA AFTER TAKEOFF. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT AND RIGHT NOSE LANDING GEAR UPLOCK HOOK TORQUE TUBE ARM ASSEMBLIES. SYSTEM OPERATED SATISFACTORILY. REFERENCE MALA954660. 1L72 4T A8SW 19951117009001995111700900SO 1995 11 17 C2XA95IA285 119951011A540012030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT NACELLE FRAME NR 2, MID SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009011995111700901SO 1995 11 17 C2XA95IA286 119951011A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE FRAME NR 2, MID SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009021995111700902SO 1995 11 17 C2XA95IA287 119951011A532012015374002 ATTACH ANGLE EMB 120 EMB120RT SO VERT STAB/FUS CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FIN TO FUSELAGE ATTACH ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009031995111700903SO 1995 11 17 C2XA95IA288 119951011A572012017052017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB NR 6 UPPER AND NR 1 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009041995111700904SO 1995 11 17 C2XA95IA289 119951011A572012017054007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB NR 8 UPPER NR 5, AND NR 6 SKIN SUPPORTS CRACKED. MAINTENACNE REMOVED AND REPLACED THE SUPPORTS, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009051995111700905SO 1995 11 17 C2XA95IA296 119951019A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 5 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009061995111700906SO 1995 11 17 C2XA95IA297 119951019A572012017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21 AND NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009071995111700907SO 1995 11 17 C2XA95IA298 119951019A572012017060011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 19 AND NR 1 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009081995111700908SO 1995 11 17 C2XA95IA299 119951019A572012017060013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 19 AND NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009091995111700909SO 1995 11 17 C2XA95IA300 119951019A572012017059015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18 AND NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009101995111700910SO 1995 11 17 C2XA95IA301 119951019A572012017057015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 AND NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009111995111700911SO 1995 11 17 C2XA95IA302 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009121995111700912SO 1995 11 17 C2XA95IA303 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009131995111700913SO 1995 11 17 C2XA95IA304 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009141995111700914SO 1995 11 17 C2XA95IA305 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009151995111700915SO 1995 11 17 C2XA95IA306 119951019A572012017057009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16 NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009161995111700916SO 1995 11 17 C2XA95IA307 119951019A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16 NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009171995111700917SO 1995 11 17 C2XA95IA308 119951019A572012017057006 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16 NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009181995111700918SO 1995 11 17 C2XA95IA309 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15 NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009191995111700919SO 1995 11 17 C2XA95IA310 119951019A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009201995111700920SO 1995 11 17 C2XA95IA311 119951019A572012017056013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15 NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009211995111700921SO 1995 11 17 C2XA95IA312 119951019A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DUIRNG C-CHECK INSPECTION, THE RIGHT WING RIB NR 15 NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009221995111700922SO 1995 11 17 C2XA95IA313 119951019A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15 NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951117009231995111700923SW 1995 11 17 MALA954637 119950915A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15426MA AC645 DURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ELEVENTH RIVET. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101, REVISION B. (M) 1L72 4T A8SW 19951117009241995111700924NM 1995 11 17 MALA954643 119950920A7600839101105017 ENG TRIM PNL DHAV DHC8 DHC8102 2809003NM COCKPIT CONTAMINATED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15816MA 231 FLT NR 3106 - AT TAKEOFF SETTINGS, THE CREW NOTED A POWER LEVER SPLIT WITH NORMAL POWER INDICATIONS. WHEN THE CREW SELECTED BLEED AIR, THE NR 1 TORQUE DROPPED 2-3 PERCENT WITH NO CHANGE TO THE NR 2 TORQUE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE ENGINE TRIM PANEL ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951117009251995111700925SW 1995 11 17 MALA954654 119951002A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 174 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER LEFT BELT FRAME RELIEF RADIUS CRACKED AT FS 174.00. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 53-20-9148 REV A. (M) 1L72 4T A8SW 19951117009261995111700926SW 1995 11 17 MALA954655 119951002A5320 WEB SWRNGNSA227 SA227AC 8780603SW FS 197 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CENTER AISLE FLOOR BOARD LEFT WEB CRACKED AT FS 197. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1L72 4T A8SW 19951117009271995111700927SW 1995 11 17 MALA954660 119951009A32302752000192 TQ TUBE ARM SWRNGNSA227 SA227AC 8780603SW NLG CORRODED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15438MA AC721B FLT NR 3192 - ON CLIMB-OUT FROM DTW, THE CREW NOTED A STEADY THUMPING FROM THE NOSE GEAR AREA AFTER TAKEOFF. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT AND RIGHT NOSE LANDING GEAR UPLOCK HOOK TORQUE TUBE ARM ASSEMBLIES. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951117009281995111700928NM 1995 11 17 MALA954661 119951009A3244314353A TIRE DHAV DHC8 DHC8102 2809003NM RT MLG OUT OF ROUND A MALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL15831MA 339 FLT NR 3127 - ON CLIMB-OUT FROM DTW, THE CREW NOTED A VIBRATION FROM THE RIGHT WHEEL WELL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR WHEEL ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951117009291995111700929NM 1995 11 17 MALA954662 119951010A335082410162007 EEL CONTL BOX DHAV DHC8 DHC8102 2809003NM CABIN FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15826MA 330 DURING MAINTENANCE IN MSP, THE EMERGENCY LIGHTING DID NOT EXTINGUISH WITH THE COCKPIT OR FLIGHT ATTENDANT SWITCH UNLESS IN ARMED POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHTING CONTROL BOX, P/N 82410162-007. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951117009301995111700930EU 1995 11 17 REXA95045 119950711A2720KAF1407P BUSHING BAG JETSTMJETSTM3101 1500215EU RT RUDDER PEDAL WORN A REXAO OTHER O OTHER CLCLIMB 1 SO25300PX 652 AFTER TAKEOFF LEFT RUDDER PEDAL WOULD NOT MAKE MORE THAN ABOUT ONE THIRD OF TRAVEL REQ'D CAPTAIN AND FORWARD OFFICERS SIDES. RIGHT RUDDER PEDAL APPEARS TO HAVE FULL TRAVEL ON BOTH SIDES. FULL LEFT AND RIGHT RUDDER TRAVEL WAS AVAILABLE BEFORE TAKEOFF. FOUND WORN BUSHING ON RUDDER PEDAL CONN ROD CAUSING BOLT TO RUB ON YOKE LEVEL ASSEMBLY. INSTALLED SERVICEABLE BUSHING, RUDDER PEDAL OPERATES NORMALLY WITH NO INTERFERENCE. (M) 2L72 4T RTA21EU 19951117009311995111700931EU 1995 11 17 REXA95052 119950814A3241426832FT COMPUTER SAAB SF340 SF340A 7850100EU ANTI-SKID FAILED A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25329PX 340A076 NO BRAKES WHILE TAXIING. REMOVED AND REPLACED ANTI-SKID COMPUTER IAW SAAB AMM. (M) 2L72 4T RTA52EU 19951117009321995111700932EU 1995 11 17 REXA95058 119950911A332066453202S WINDOW LIGHT SAAB SF340 SF340A 7850100EU RT FWD EXIT TERMINAL BORKEN A REXAO OTHER O OTHER TXTAXI/GRND HDL 1 SO25346AM 340A032 BRAKES FAIL TO STOP AIRCRAFT ON SEVERAL OCCASSIONS, TURNING OFF ANTI-SKID FIXES PROBLEM. OHMED WHEEL SPEED TRANSDUCERS, OHMED GOOD. OHMED LEFT AND RIGHT ANTI-SKID CONTROL VALVES, ALSO OHMED GOOD. SECURED WIRING FROM ANTI-SKID COMPUTER AWAY FROM WINDOW LIGHT INVERTERS. REPLACED WINDOW LIGHT AT RIGHT FWD EXIT AND REPAIRED TERMINAL, COMPLIED WITH AD 90-14-06 A2 AT SAID POSITION TAXI CHECK BRAKES GOOD. OK FOR CONTINUED SERVICE. (M) 2L72 4T RTA52EU 19951117009331995111700933 1995 11 17 REXA95060 419950918A3455071128417 ADF CONTROL HEAD SAAB SF340 SF340A 7850100EU COCKPIT SMOKED A REXAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25403BH 340A060 SMOKE IN COCKPIT FROM CENTER PANEL. FOUND SMOKE TO BE COMING FROM ADF CONTROL HEAD. ADF SYSTEM ALREADY DEFERRED. PULLED AND COLLARED ADF C/B. (M) 2L72 4T RTA52EU 19951117009341995111700934NE 1995 11 17 REXA95062 219950925A72106044T35P10 GEARBOX HAMSTD GC491 SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE FAILED A REXAE ENGINE SHUTDOWN T ENGINE CASE PENETRATION CLCLIMB 1 SO25365PX7551 UDAG0542 340B265 SHUT DOWN LEFT ENGINE IN FLIGHT, DUE TO PROP GEARBOX FAILURE. INSTALLED SERVICEABLE PGB IAW GE MM. (M) 2L72 4T4 TRTA52EU E8NE 19951117009351995111700935EU 1995 11 17 REXA95063 119950929A3350 CONNECTOR BAG JETSTMJETSTM3101 1500215EU CABIN DIRTY A REXAK NONE L NO TEST ININSP/MAINT 1 SO25301PX 654 TWO AFT EMERGENCY LIGHTS IN ROOF WILL NOT ILLUMINATE WHEN TURNED ON BY COCKPIT SWITCH. CLEANED CANNON PLUG TO EMERGENCY LIGHTING AFT POWER UNIT (P/N 312111). OPS CHECK GOOD. (M) 2L72 4T RTA21EU 19951117009361995111700936EU 1995 11 17 REXA95064 119951012A26117211121100 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU CARGO COMPT MALFUNCTIONED A REXAF ACTIVATE FIRE EXT. N FALSE WARNING NRNOT REPORTED 1 SO25327PX 340A059 CARGO SMOKE CAUTION IN FLIGHT, FOLLOWED CHECK LIST, FIRED CARGO EXTINGUISHER. RETURNED TO MEM. REPLACED CARGO DETECTOR. (M) 2L72 4T RTA52EU 19951120000011995112000001EU 1995 11 20 COMA9531186 119951105A2750 RETRACT MECH SAAB SF340 SF340A 7850100EU TE FLAPS OUT OF ADJUST A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01357CA 340A044 FLAP FAULT ON CAUTION WARNING PANEL. PERFORMED FLAP CONTROL SYSTEM RIGGING AND ADJUSTMENT. 2L72 4T RTA52EU 19951121000011995112100001EU 1995 11 21 DL31L954318 119951110A33501317 BULB AIRBUS310 A310324 3930206EU CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11837AB 674 PATH MARKING ON LT SIDE LAST AFT RED LAMP DOES NOT OPERATE. RELAMPED, CKS GOOD. 2L72 4F RTA35EU 19951121000021995112100002NM 1995 11 21 DL72S954355 119951112A217017805021 DUCT BOEING727 727232 1384082NM WATER SEPERATOR CRACKED A DALAO OTHER O OTHER CRCRUISE 1 SO11533DA 22046 UNABLE TO MAINTAIN PRESSURIZATION DURING CRUISE. FOUND LEFT WATER SEPARATOR FWD CLAMP SEPARATED AND WATER SEPARATOR TO MIZ VALVE DUCT CRACKED IN SEVERAL PLACES. REPLACED DUCT AND SEPARATOR, OPERATION NORMAL. 2L73 4F A3WE 19951124000011995112400001WP 1995 11 24 9518079929 119951114A56105912290506 WINDSHIELD DOUG DC9 DC931 3022065WP COCKPIT CRACKED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018923E498 45838 MSP-YQR - DURING CRUISE AT FL350, THE FIRST OFFICER'S OUTER WINDSHIELD CRACKED. ACFT RETURNED TO MSP WITHOUT FURTHER INCIDENT. REPLACED THE WINDSHIELD AND WINDOW HEAT CONTROLLER, CHECKED OK. 2L72 4F A6WE 19951124000021995112400002WP 1995 11 24 9518089987 119951115A3350 EEL WIRE DOUG DC9 DC932 3022066WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01987US 47458 DURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPAIRED WIRE AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124000031995112400003WP 1995 11 24 9518099978 119951115A3350 BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019342 47391 DURING LINE CHECK, FOUND FORWARD ENTRY AND COCKPIT DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124000041995112400004WP 1995 11 24 9518109613 119951115A3350 BULB DOUG DC9 DC932 3022066WP CABIN MISSING A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01613NW 47438 DURING ROUTINE CHECK, FOUND TOP AND BOTTOM BULBS MISSING IN THE EMERGENCY EXIT LIGHT AT THE FORWARD ENTRANCE DOOR. INSTALLED BULBS AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124000051995112400005WP 1995 11 24 9518119750 119951115A3350 EEL DOUG DC9 DC941 302207NWP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01750NW 47114 DURING LINE CHECK, FOUND EMERGENCY LIGHT AT FORWARD LEFT DOOR INOPERATIVE. REPLACED LIGHT UNIT AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124000061995112400006NM 1995 11 24 9518126309 119951115A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 TPE - DURING LINE CHECK, THE FLOOR EMERGENCY OATH LIGHTS BETWEEN ROWS 36L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE LIGHT ASSEMBLY PIN AND OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951124000071995112400007NM 1995 11 24 9518246305 119951116A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01665US 23820 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHTS BETWEEN SEAT ROWS 36L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTOR PINS AT ROW 36L AND OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951124000081995112400008WP 1995 11 24 9518259929 119951109A2822 BOOST PUMP DOUG DC9 DC931 3022065WP FUEL SYST MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018923E 45838 DURING CLIMB, FUEL WAS PUMPING INTO RIGHT FUEL TANK AND WAS UNABLE TO CROSSFEED FUEL WITH FUEL IN CENTER TANK. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSTALLED NEW BOOST PUMP VOLUTE AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124000091995112400009NM 1995 11 24 95FDEA01764 119951116A532066118099 CLIP BOEING727 727227 1384078NM BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 660 STR 15L. REPLACED OLD STR CLIP AT BS 660 STR 15L WITH NEW STR CLIP. 2L73 4F A3WE 19951124000101995112400010NM 1995 11 24 95FDEA01765 119951116A5311 FRAME BOEING727 727227 1384078NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD BAY FRAME DENTED AT BS 500 BETWEEN STR 23 TO 22L AND DENT FOUND TO BE OUT OF LIMITS. REPAIRED DENTED FRAME AT BS 500 BETWEEN STR 23 TO 22L PER FEDEX SRM 51-40-3 AND 53-10-1. 2L73 4F A3WE 19951124000111995112400011NM 1995 11 24 95FDEA01766 119951116A5315 FLOORBEAM BOEING727 727227 1384078NM BS 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 MECHANICAL DAMAGE TO FLOORBEAM LOWER SURFACE OF UPPER FLANGE BS 600 RBL 11 WL 207. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS. REPAIRED FLOORBEAM AT BS 600 RBL 11 WL 207 PER FEDEX SRM 53-10-1 AND 53-10-8. 2L73 4F A3WE 19951124000121995112400012NM 1995 11 24 95UAL900240 119951031A56105893543109 WINDOW BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 1L CRACKED A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP297460U 21914 RETURNED TO ORD, DUE TO CAPTAIN'S WINDSHIELD CRACKED. REPLACED CAPTAIN'S NR 1L WINDOW. 2L73 4F4 F A3WE E2EA 19951124000131995112400013NM 1995 11 24 95UAL900263 119951116A5753113N280096R SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT TE FLAP CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29544UA 13363 25322 RIGHT INBOARD MAIN FLAP, TRAILING EDGE FLAP, HAS A CRACK IN THE SKIN AND SPAR. RIGHT AFT FLAP TRAILING EDGE REMOVED AND REPLACED. ASSEMBLY SENT TO SHOP FOR ANALYSIS AND REPAIR. 2L72 4F4 FRTA2NM E17NE 19951124000141995112400014NM 1995 11 24 DHLA9574200 119951115A275110619261 FLAP INDICATOR BOEING727 727225 1384077NM COCKPIT STICKS A DHLAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01742DH 21290 DURING FLAP RETRACTION I/B HUNG UP BETWEEN 2O AND 5O, WENT TO ALT. PROCEDURES RETURNING TO MSP. REMOVED AND REPLACED I/B FLAP INDICATOR AND ADJUSTED TRANSMITTER PER MM 27-52-2. 2L73 4F A3WE 19951124000151995112400015EU 1995 11 24 DL31L954391 119951115A33500L3071BPEGPL BULB AIRBUS310 A310324 3930206EU CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11835AB 650 FLOOR LIGHT BULB OUT AT 14B. RELAMPED, OPERATION NORMAL. 2L72 4F RTA35EU 19951124000161995112400016NM 1995 11 24 DL72L954400 119951108A2780 MOUNT BOEING727 727232 1384082NM NR 2 SLAT ACT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 FOUND ON CV-2 CHECK, NR 2 SLAT ACTUATOR MOUNT CRACKED AT UPPER O/B LOBE. REPAIRED PER M/M 57-42-0 PG 812. 2L73 4F A3WE 19951124000171995112400017NM 1995 11 24 DL72L954401 119951108A5240 FRAME BOEING727 727232 1384082NM LT AFT SERV DOORCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 FOUND ON CV-2 CK, LT AFT SERVICE DOOR (S/N 593) HAS A .5 INCH CRACK IN THE UPPER HINGE CUTOUT OF THE FWD FRAME. REPAIRED PER SRM 52-40-2 FIG 4. 2L73 4F A3WE 19951124000181995112400018NM 1995 11 24 DL72L954402 119951109A5320 STIFFENER BOEING727 727232 1384082NM BS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11509DA 21311 FOUND ON CV-2 CK, .125 INCH VISABLE CRACK EXTENDING FROM LOWER O/B RADIUS BLOCK AT VERTICAL STIFFENER STA 1183 LBL 8. REPAIRED PER M/M 53-11-0 PAR 9. 2L73 4F A3WE 19951124000191995112400019NM 1995 11 24 DL72P954409 119951106A573065877421 SKIN BOEING727 727225 1384077NM LOWER WING CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO118890Z 21859 DURING INSPECTION OF THE LOWER SKIN PER EO 4-37113-3, CORROSION WAS DISCOVERED ON THE AFT SKIN BETWEEN S-4C AND S-3C AT APPROX RBL 30. MTC REPORTS A MIN REMAINING THICKNESS OF .063 AT THE DAMAGE AREA. ERA WILL PROVIDE TEMP AND PERM REPAIR INSTRUCTIONS. TEMP INSTR WILL REMOVE ALL EVIDENCE OF CORROSION AND TREAT THE SURFACE. PERM INSTR WILL INSTALL A DOUBLER AND TRIPLER AND FILLER IN DAMAGE AREA, PER DL ERA 302731-14AD. 2L73 4F A3WE 19951124000201995112400020NM 1995 11 24 DL72S954406 119951115A53306554590 SKIN BOEING727 727232 1384082NM BS 720 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO11523DA 21583 CORROSION WAS FOUND ON THE RAM AIR ACTUATOR ACCESS DOOR CUTOUT AT THE FWD LT CORNER. THE CORROSION WAS CUT OUT. REPAIARED PER DL ERA 302764-14. 2L73 4F A3WE 19951124000211995112400021NM 1995 11 24 DL72S954408 119951019A5720 STIFFENER BOEING727 727232 1384082NM ATTACH RIB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11520DA 21471 WHILE WORKING ON A HYDRAULIC LEAK ON THE NR 7 SLAT ACTUATOR ATTACH RIB STIFFENER WAS FOUND CRACKED. THE DAL MFG (P/N 57-0367-001) ON THE STIFFENER. THIS ER/A WILL REPLACE THE OUTBD ATTACH RIB STIFFENER PER EO 4-59271-3AD. 2L73 4F A3WE 19951124000221995112400022NM 1995 11 24 DL72W954395 119951115A5320 WEB BOEING727 727247 138408FNM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 FOUND DURING A-1 LETTER CHECK, .125 INCH CRACK IN LWR TORQUE BOX VERT WEB LIGHTENING HOLE FS 1223 LEFT SIDE. REPAIRED PER M/M 53-11-0 PAR 15. 2L73 4F A3WE 19951124000231995112400023NM 1995 11 24 DL72W954398 119951115A2780 ACTUATOR BRACKET BOEING727 727247 138408FNM NR 2 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 FOUND ON A-1 LETTER CK, NR 2 LE FLAP O/B ACTUATOR BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2L73 4F A3WE 19951124000241995112400024NM 1995 11 24 DL72W954403 119951115A5330 SKIN BOEING727 727247 138408FNM FS 344-360 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING HMV, AN TIME LIMITED REPAIR WAS FOUND LOCATED APPROXIMATELY 6 INCHES ABOVE AND AFT OF THE RAIN GUTTER AT THE L-1 DOOR, AT APPROXIMATELY FS 344 TO 360. THE EXISTING REPAIR WAS REMOVED AND ADDITIONAL DAMAGE CUT OUT. TOTAL DAMAGE REMOVAL RESULTED IN A 6 INCH BY 5.5 CUT OUT. THIS ER/A INSTALLED A NEW DOUBLER. 2L73 4F A3WE 19951124000251995112400025NM 1995 11 24 DL72W954405 119951115A5330 SKIN BOEING727 727247 138408FNM FS 300 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 DURING LOWERING OF THE NOSE JACK STAND, A STAND SUPPORT PIN SHEARED CAUSING EQUIPMENT ON THE STAND TO STRIKE THE AIRCRAFT. A 2 INCH BY 2 INCH HOLE WAS TORN INTO THE FUSELAGE AT FS 300 BETWEEN STR 9R AND STR 10R. THAT WAS CLEANED UP AND THE FINAL DIMENSIONS OF 4 INCH BY 2.5 INCH. ACCOMPLISHED REPAIRS PER DL ERA 302767-14. 2L73 4F A3WE 19951124000261995112400026NM 1995 11 24 DL733954404 119951115A5230 FRAME BOEING737 737347 1384647NM CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11304WA 23345 THE C-1 DOOR, LWR AFT FRAME HAS A 2.5 INCH LONG CRACK IN THE OUTBOARD RADIUS BELOW STOP NUMBER 4 AND OUTBOARD OF THE LOWER TORQUE TUBE. THE LOWER FWD FRAME HAS A 0.75 INCH CRACK ON THE INBOARD RADIUS JUST ABOVE STOP NUMBER 5. THIS ER/A INSTALLS A STEEL REPAIR ANGLE FOR THE AFT FRAME AND REPAIRS PER SRM 51-70-11 FIGURE 1 FOR THE FWD FRAME, PER DL ERA 302763-14. 2L72 4F RTA16WE 19951124000271995112400027NM 1995 11 24 DL76E954385 119951115A3350BPS73 EEL POWER SUPPLY BOEING767 767232 1385132NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11111DN 22223 BATTERY PACK DOES NOT HOLD CHARGE FOR EMERGENCY LIGHTS. REPLACED POWER SUPPLY BATTERY, SYSTEM OPS CHECKS NORMAL. POWER SUPPLY (P/N BPS7-3)(S/N 5449), BATTERY (P/N 2013-1A) (S/N 1851). 2L72 4F RTA1NM 19951124000281995112400028WP 1995 11 24 DLL10954379 119951115A3350 EEL POWER SUPPLY 5165741 LKHEED1011 10113851 5265010WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO11717DA 61468 193C1096 L2 EMERGENCY EXTERIOR LIGHT INOP. T/S SYSTEM FOUND PWR SUPPLY BAD. REPLACED SAME OPS, CHECK SYSTEM CHECKS GOOD. 2L73 4F A23WE 19951124000291995112400029WP 1995 11 24 DLL16954380 119951115A55401525200105 WEB LKHEED1011 10113853 5265020WP RUDDER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11760DH 193Y1194 HMV, RUDDER SUPPORT STRUCTURE IS CRACKED, SEEN THROUGH THE LOWER LIGHTENING HOLE. REPLACED WEB PER LAC DWG 1525200-105. 2L73 4F A23WE 19951124000301995112400030NM 1995 11 24 DLM11954387 119951115A3350 EEL 0105606205 DOUG MD11 MD11 3023602NM CABIN SHORTED A DALAK NONE L NO TEST CRCRUISE 1 SO11810DE 48565 EMERGENCY TRACK LIGHT SHORTED AND NR 5 EMERGENCY TRACK BATTERY LOW MSG. REPLACED SHORTED LIGHT MODULE, OPERATION NORMAL. 2L73 4F RTA22WE 19951124000311995112400031NM 1995 11 24 DLM88954388 119951115A3300 BULB OL3071BEPGPLDOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11939DL 49812 FOUND ONE EEPL BULB INOP ON SYS TEST. RELAMPED, NOW CKS NORMAL. 2L72 4F RTA6WE 19951124000341995112400034NM 1995 11 24 95ZZZX6272 119950920A5330 SKIN BOEING737 7372H5 138448ENM FS 727 CRACKED A E9WAK NONE O OTHER ININSP/MAINT 1 SO05221US57633 20454 GSO - DURING SCHEDULED MAINTENANCE CHECK, NDT INSPECTION FOUND FUSELAGE SKIN LAP, TWO .25 INCH CRACKS WERE DETECTED AT ONE RIVET AND ONE .3125 INCH CRACK WAS DETECTED AT ONE RIVET STA 727 A, STR 14 L. REPAIRED CRACKED AREA BY INSTALLING EXTERNAL DOUBLER IAW SRM 53-30-3. (X) 2L72 4F A16WE 19951124000351995112400035EU 1995 11 24 95ZZZX6273 119950922A61208930823 LINKAGE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110U 01514WP RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27490UE 909 P66096 ABE/IAD - FLT 6154 - DURING TAKEOFF AT 2222 HRS ON 9-22-95, ABORTED TAKEOFF DUE TO RT ENGINE BETA LIGHT NOT EXTINGUISHING UNTIL THE ENGINE RPM REACHED 104 PERCENT. ALSO, THE TORQUE HUNG AT 23 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT PROP GOVERNOR AND RIGGED THE RIGHT SPEED LEVER LINKAGE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE OPERATOR CONTROL NR VTZA95304. 2L72 4T4 TRTA56EU E4WE 19951124000361995112400036NM 1995 11 24 95ZZZX6274 119950922A5101 STRUCTURE DORNERDO32 DO328100 2996000NM AIR FRAME BIRD STRIKE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 GL07425JS 3037 FLT 4175 - CREW ABORTED TAKEOFF AFTER ENCOUNTERING A BIRD STRIKE DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT IAW MM 05-00-00. NO DAMAGE DETECTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951124000371995112400037NE 1995 11 24 95ZZZX6275 219950913A7261 ENGINE OIL DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LT/RT REQ'D SERVICE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07425JS 3037 FLT 4236 - DURING CLIMB-OUT, CREW NOTICED BOTH RT AND LT ENGINE OIL PRESSURE INDICATOR IN 'YELLOW' ARC. CREW ELECTED TO RETURN TO FIELD, AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE SERVICED BOTH LT AND RT ENGINES WITH OIL IAW MM 12-00-00. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 19951124000381995112400038NE 1995 11 24 95ZZZX6276 219950824A7530MS920823 BOLT DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE ENGINE LOOSE A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07427JS 3039 FLT 4228 - CREW ELECTED TO RETURN TO FIELD AFTER EXPERIENCING A P/L SPLIT IN CRUISE CONFIGURATION. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED BLEED AIR ADAPTER ATTACH BOLTS WERE LOOSE, TIGHTENED BOLTS IAW MM 75-00-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 19951124000391995112400039NM 1995 11 24 95ZZZX6277 119950731A36100132ADK TEMP SWITCH DORNERDO32 DO328100 2996000NM ENGINE DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL07427JS 74869 3039 FLT 4240 - DURING TAKEOFF ROLL, CREW ADVISORY MESSAGE - BLEED AIR FAIL, CREW ELECTED TO ABORT TAKEOFF AND RETURN TO GATE. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED A FAULTY BLEED AIR SHUT-OFF VALVE TEMP SWITCH. REMOVED AND REPLACED FAULTY SWITCH IAW MM 36-1-04. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951124000401995112400040NM 1995 11 24 95ZZZX6278 119950830A7603 POWER LEVER DORNERDO32 DO328100 2996000NM COCKPIT LACK OF LUBE A VNAAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL07427JS 3039 FLT 4138 - CREW ELECTED TO RETURN TO GATE WHEN CAPTAIN WAS UNABLE TO ADVANCE RT POWER LEVEL BEYOND THE F.I. GATE. MAINTENANCE LUBRICATED PRIMARY LOW PITCH LOCK-OUT DEVICE IAW STD MAINTENANCE PRACTICES. GROUND CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951124000411995112400041NM 1995 11 24 95ZZZX6279 119950912A5610001A561A0000201 WINDSHIELD DORNERDO32 DO328100 2996000NM RT COCKPIT CRACKED A VNAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL07427JS 130 3039 FLT 7187 - DURING CRUISE AT FLT LEVEL 240, CREW REPORTED A CRACK IN THE FIRST OFFICER'S WINDSHIELD. AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT FERRIED TO CAK WHERE MAINTENANCE REPLACED FIRST OFFICER'S WINDSHIELD. WORK ACCOMPLISHED IAW MM 56-11-00. 2H72 4T RTA45NM 19951124000421995112400042NM 1995 11 24 95ZZZX6280 119950720A7712311649201 TQ SENSOR DORNERDO32 DO328100 2996000NM RT ENGINE DEFECTIVE A VNAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL07429JS 3043 FLT 4228 - FLIGHT CREW REJECTED TAKEOFF AFTER NOTICING A TORQUE FLUX RT ENGINE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. AIRCRAFT LATER FERRIED TO PIT WHERE MAINTENANCE REMOVED AND REPLACED RT ENGINE TORQUE SENSOR IAW MM 77-11-00. OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951124000431995112400043NM 1995 11 24 95ZZZX6281 119951002A5101 STRUCTURE DORNERDO32 DO328100 2996000NM AIRFRAME BIRD STRIKE A VNAAO OTHER C F.O.D. CLCLIMB 1 GL07432JS 3045 FLT 4248 - CREW REPORTED STRIKING A BIRD AT 1,000 FEET AGL. ARCRAFT CONTINUED IN-FLIGHT AND LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT IAW MM 5-50-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951124000441995112400044CE 1995 11 24 95ZZZX6282 119950805A323212805132 ACTUATOR CESSNA210 T210F 2073422CE LT MLG DOOR LEAKING A HSYAO OTHER JK WARNING INDICATION FLUID LOSS CLCLIMB 1 NM056193R 1924 T2100093 BIL - AFTER TAKEOFF, GEAR WOULD NOT FULLY RETRACT WHEN SELECTED UP. GEAR WAS SELECTED DOWN, AND DOWN AND LOCKED WAS INDICATED. GEAR WAS CYCLED 4 TIMES TO THE DOWN POSITION WITH NO POSITIVE INDICATION. GEAR WAS HAND-PUMPED DOWN, AND AIRCRAFT LANDED WITHOUT INCIDENT. LEFT REAR MLG DOOR ACTUATOR SHAFT O-RING LEAKED. REPLACED O-RINGS ON THE ACTUATOR. LEAK CHECK AND OPS CHECK OKAY. 1H71 3O 3A21 19951124000451995112400045NE 1995 11 24 95ZZZX6283 219950929A7260 CHIP LIGHT BEECH 99 C99 1154006CE PWA PT6 PT6A36 52043NE NR 2 ENGINE ILLUMINATED A HSYAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 NM05167EE U167 PCE38077 DEN - FLT 7625 - NR 2 ENGINE CHIP DETECTOR LIGHT ILLUMINATED 35 MILES OUT ON INBOARD LEG. PILOT SECURED NR 2 ENGINE AND CONTINUED TO LAND WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. METAL FUZZ FOUND ON RGB CHIP DETECTOR AND IN OIL FILTER. INSPECTED CHIP DETECTOR IAW PWC 72-13-01. FOUND CONTAMINATION WITHIN ALLOWABLE LIMITS. SUBMITTED SOAP SAMPLE. CLEANED AFFECTED PARTS AND PLACED ON 10-HOUR RE-INSPECT INTERVAL IAW PWC 79-23-04. AIRCRAFT RETURNED TO SERVICE. ENGINE TSO, 2,325.6 HRS. 1L72 3T4 T A14CE E4EA 19951124000461995112400046NE 1995 11 24 95ZZZX6284 219950920A7310320115 FUEL HEAT VALVE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO11906VJ 47379 666862 NR 1 ENGINE OIL TEMP EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMP 139 DEGREES. REPLACED FUEL HEAT VALVE. DRAINED AND REPLACED ENGINE OIL. REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C CKS OK. NO LEAKS ON RUN-UP. 2L72 4F4 F A6WE E2EA 19951124000471995112400047CE 1995 11 24 95ZZZX6285 119950928A532058130412 WEB CESSNA404 404CESSNA 2075901CE LT/RT NLG WW CRACKED AS BQTAK NONE O OTHER ININSP/MAINT 1 NE05404BA9241 4040237 FOUND BOTH NOSE GEAR DRAG BRACE ATTACH POINTS (WHEELWELL SKINS) CRACKED IN SEVERAL PLACES. 1L72 3O A25CE 19951124000481995112400048CE 1995 11 24 95ZZZX6286 119950927A32601003810061 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG/RT MLG MALFUNCTIONED A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19196GA UB31 MCO/MIA - FLT 428 - PILOT REPORT: GEAR UNSAFE LIGHT ON IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR DOWNLOCK AND RIGHT MAIN UPLOCK SWITCHES. 2L72 4T RTA24CE 19951124000491995112400049WP 1995 11 24 95ZZZX6287 119950928A3350 EEL BATTERY CVAC 340 34031 2422704WP CABIN DIRTY A SPAAK NONE L NO TEST ININSP/MAINT 1 WP0773153 179 DURING SCHEDULED CHECK, THE MOST FORWARD INTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED OXIDATION FROM BATTERY CONTACTS. SUBSEQUENT OPERATIONAL CHECKS WERE SATISFACTORY. 2L72 4R 6A6 19951124000501995112400050SW 1995 11 24 95ZZZX6288 119950921A3230 CIRCUIT BREAKER SWRNGNSA226 SA226TC 8780404SW LANDING GEAR FAILED A BSAAO OTHER J WARNING INDICATION CLCLIMB 1 NM05116BS TC311 BIL - LANDING GEAR WOULD NOT RETRACT DURING TRAINING FLIGHT. REPLACED LANDING GEAR CONTROL CIRCUIT BREAKER WITH NEW. CYCLED GEAR SEVERAL TIMES. NO PROBLEMS NOTED. AIRCRAFT TEST FLOWN AND GEAR CYCLED SEVERAL TIMES. NORMAL OPERATION. 1L72 4T A8SW 19951124000511995112400051NE 1995 11 24 95ZZZX6289 219950926A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 FAILED A HNAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA07984HA11910 377 120911 BWI/HNP - FLT 3072 - ON FLIGHT 3072 BWI TO HPN, THE CABIN FILLED WITH SMOKE DURING DESCENT. THE AIRCRAFT LANDED IN HPN WITHOUT INCIDENT. FOUND THAT WITH THE BLEEDS OFF, SMOKE BEGAN TO DISSIPATE. REMOVED AND REPLACED THE NR 1 ENGINE. 2H72 4T4 TRTA13NM E20NE 19951124000521995112400052WP 1995 11 24 95ZZZX6290 119951011A3350 EEL BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05408EA 47693 STL - FLT 290 - DURING PRE-FLIGHT, ESCAPE PATH LIGHTING STRIP FROM SEAT ROW 6 TO ROW 23, REMAINED ILLUMINATED WITH LIGHT SWITCH IN THE ARMED POSITION. REPLACED BATTERY PACK, MFG PN 5822-2. ESCAPE PATH LIGHTING SYSTEM THEN CHECKED NORMAL. CHECK C-7-8-95 - STL. 2L72 4F A6WE 19951124000531995112400053NM 1995 11 24 AALA951681 119950920A3350 EEL WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07660AM 25294 DFW - EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 17D TO 26D INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT ROW 17D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19951124000541995112400054NM 1995 11 24 AALA951685 119950913A5330141N3231 SKIN BOEING757 757223 1384957NM BS 416 DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - FUSELAGE SKIN HAS TEMPORARY REPAIR INSTALLED WITH BLIND FASTENERS BETWEEN S21 AND S22L. REPAIRED PER MRB 757-604. TST, 15,867.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000551995112400055NM 1995 11 24 AALA951686 119950913A5330146N3511 SKIN BOEING757 757223 1384957NM BS 1400-1420 DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - FUSELAGE SKIN HAS SEVERAL DENTS BEYOND SRM LIMITS AT STA 1400 AND STA 1420 FROM S28L TO S27R. REPAIRED PER MRB 757-603. TST, 15,867.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000561995112400056NM 1995 11 24 AALA951687 119950913A5310146N5300 DECK PLATE BOEING757 757223 1384957NM BS 1680/1720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - DECK PLATE AT STA 1680 AND STA 1720 HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS BL LOCATIONS. MATERIAL REMAINING IS BEYOND SRM ALLOWABLE LIMITS. REPAIRED PER MRB 757-602. TST, 15,867.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000571995112400057NM 1995 11 24 AALA951688 119950913A5315141N5112 FLOOR BEAM BOEING757 757223 1384957NM BS 365 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - CORROSION BLEND OUT AT STA 365, RBL 10 AND RBL 59, BEYOND SRM LIMITS. REPAIRED PER MRB 757-597. TST, 15,687.21 HRS, CYCLES 5,989. (X) 2L72 4F RTA2NM 19951124000581995112400058NM 1995 11 24 AALA951689 119950913A5315141N5113 FLOOR BEAM BOEING757 757223 1384957NM BS 377 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 377, LBL 42 AND LBL 48, ALSO, LBL 31 AND LBL 22, BEYOND SRM LIMITS. REPAIRED PER MRB 757-596. TST, 15,687.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000591995112400059NM 1995 11 24 AALA951690 119950913A5315141N2932 FLOOR BEAM BOEING757 757223 1384957NM BS 324 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 324, RLB 60, BEYOND SRM LIMITS. REPAIRED PER MRB 757-595. TST, 15,687.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000601995112400060NM 1995 11 24 AALA951691 119950913A5315146N5090 FLOOR BEAM BOEING757 757223 1384957NM BS 1661 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - CORROSION BLENDED OUT ON FLOOR BEAM AT STA 1661, LBL 9.5, BEYOND SRM LIMITS. REPAIRED PR MRB 757-594. TST 15,867.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000611995112400061NM 1995 11 24 AALA951692 119950913A5315146N5136 FLOOR BEAM BOEING757 757223 1384957NM BS 1630 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07632AA 24590 AFW - CORROSION BLENDED OUT ON FLOORBOARD AT STA 1640, RBL 57 AND RBL ZERO, BEYOND SRM LIMITS. REPAIRED PER MRB 757-593. TST, 15,867.21 HRS. CYCLES, 5,989. (X) 2L72 4F RTA2NM 19951124000621995112400062NM 1995 11 24 AWXA9500688 119951009A2133322684 OUTFLOW VALVE BOEING737 737301 1384611NM CABIN FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28324AW 2800159 23261 LAS/LAX - FLT 707 - DURING TAKEOFF/CLIMB, AIRCRAFT WAS UNABLE TO BE PRESSURIZED. CREW RETURNED AIRCRAFT TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FORWARD OUTFLOW VALVE INOPERATIVE. REMOVED AND REPLACED FORWARD OUTFLOW VALVE. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F RTA16WE 19951124000631995112400063NE 1995 11 24 CAL950835 219950919A7250 BEARING BOEING737 737524 1384721NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE FAILED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SW09186113847 27324 857886 FLT NR 397 - DEN - THE NR 2 ENGINE SUDDENLY SPOOLED DOWN WITH VIBRATION, IN FLIGHT AT 31,000 FEET. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. DISASSEMBLY OF THE ENGINE REVEALED NR 4 BEARING FAILURE AS THE PRIMARY CAUSE OF THE ENGINE IN FLIGHT SPOOL DOWN. (M) 2L72 4F4 FRTA16WE E2GL 19951124000641995112400064 1995 11 24 CAL950867 419950923A2565D31393110 SLIDE BOEING757 757224 1384958NM RT OVERWING DEPLOYED A ACALAO OTHER J WARNING INDICATION CLCLIMB 1 SW09331034386 27293 FLT NR 711 - IAH - THE EICAS MESSAGE RIGHT OVERWING SLIDE DISPLAYED STEADY AND THE EMERGENCY DOORS OVERHEAD LIGHT ILLUMINATED STEADY AFTER TAKEOFF FROM EWR. CABIN PRESSURE WAS GOOD AND A VISUAL INSPECTION OF BOTH EXITS APPEARED NORMAL. THE FLIGHT WAS CONTINUED TO IAH. UPON LANDING AT IAH THE TOWER REPORTED THAT THE SLIDE APPEARED TO BE DRAPED OVER THE RT WING. MX FOUND THE RT OVERWING EMERGENCY EXIT DOOR PROPERLY INSTALLED, BUT THE EXTERIOR SLIDE COMPART DOOR WAS OPEN. THE RT INBOARD T/E FLAP WAS FOUND DAMAGED DUE TO SLIDE DEPLOYMENT. THE SLIDE WAS REMOVED AND REPLACED. THE FLAP WAS REPAIRED IAW SRM 57-53-01. CAUSE OF FAILURE COULD NOT BE DETERMINED. A BULLETIN ON SLIDE INSTALLATION WAS ISSUED. (M) 2L72 4F RTA2NM 19951124000651995112400065WP 1995 11 24 IXXA199586 119951010A2611302313 SMOKE DETECTOR DOUG DC8 DC861 3021952WP NR 2 POSITION MALFUNCTIONED A IXXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL23861PL 45964 FLL/BNA - EN ROUTE, MAIN CARGO COMPARTMENT SMOKE DETECTORS 2, 4, 6, 8, AND 10 ILLUMINATED. THE LIGHTS WOULD EXTINGUISH FOR SHORT PERIODS OF TIME, AND ILLUMINATE AGAIN. THERE WAS NO EVIDENCE OF FIRE, BUT THE AIRCRAFT PRECAUTIONARILY DIVERTD TO ATL TO MAKE A CONFIRMATION ON THE GROUND. INSPECTION ON THE GROUND IN ATL REVEALED THE NR 2 SMOKE DETECTOR UNIT WAS CAUSING THE FALSE FIRE WARNING. THE UNIT WAS REPLACED, AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2L74 4F 4A25 19951124000661995112400066NM 1995 11 24 KPVA099A 119950917A3230DSC2541 MODULE DIODE DHAV DHC8 DHC8103 1386005NM MLG SHORTED WIRE A KPVAA UNSCHED LANDING O OTHER CLCLIMB 1 WP13801WP 086 LANDING GEAR STUCK IN DOWN POSITION. RECYCLED GEAR, HYDRAULIC AND FUEL CIRCUIT BREAKERS TRIPPED. REPAIRED SHORTED WIRE, TEST FLIGHT C/W, CYCLED GEARS 2 TIMES, OPS CHECK GOOD. (X) 2H72 4T RTA13NM 19951124000671995112400067EU 1995 11 24 RAIA951005 119951001A3350DM21 EEL CONNECTOR JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03553HK1863 41066 STL - FT 7492 - FLOOR EMERGENCY LIGHTS AFT SECTION INOP. MAINTENANCE SECURED LOOSE CONNECTION. OPS CHECK GOOD. AIRCRAFT TT 1863.0 HRS. (X) 2L72 4T RTA41NM 19951124000681995112400068EU 1995 11 24 RAIA951009 119951008A7920PE20243J10 B-NUT JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE LOOSE A RAIAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE03550HK 41039 STL - FLT 7492 - RT ENGINE OIL PRESSURE DROPPED TO ZERO. CREW SHUT ENGINE DOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED B-NUT ON INLET LINE GOING TO OIL COOLER. GROUND RUN, LEAK CHECK GOOD. AIRCRAFT TT, 2,000.0 HRS. (X) 2L72 4T RTA41NM 19951124000701995112400070NM 1995 11 24 SRAA99509 119950924A2760 SWITCH BOEING747 747249F 1384849NM SPOILER OUT OF ADJUST A SRAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO19742SJ 21827 MIA - FLT 101 - ON TAKEOFF, SPOILER WARNING HORN CAME ON. ABORTED TAKEOFF AND RETURNED TO BLOCK. ADJUSTED SPOILER ARMED SWITCH, SYSTEM OPS CHECKED GOOD PER MM CHT 27. (X) 2L74 4F A20WE 19951124000711995112400071NM 1995 11 24 SRAA99510 119950923A2612 FIRE LOOP BOEING747 747246F NM APU LOOSE A SRAAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SO19741SJ 22063 DURING APPROACH TO KUWAIT, APU FIRE HANDLE ILLUMINATED WITH FIRE BELL, EMERGENCY PROCEDURE USED, APU FIRE EXTINGUISHER BOTTLE USED. ON GROUND, INSPECTED APU AND FOUND NO EVIDENCE OF FIRE. DEFERRED APU FIRE EXTINGUISHER PER MEL CH 26-8. REPLACED APU FIRE BOTTLE AND SECURED LOOSE CONNECTOR ON 'A' LOOP WHICH CAUSED FALSE WARNING. SYSTEM OPS CHECKED GOOD PER MM CH 26. (X) 2L74 4F A20WE 19951124000721995112400072NM 1995 11 24 TAOA109502 119951005A21503216741 PACK VALVE GARRTT BOEING727 727227 1384078NM RIGHT FAILED A TAOAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15925TS 983839 21244 SMOKE IN CABIN. FOUND RIGHT PACK VALVE STUCK OPEN. NUMEROUS LEAKS FOUND IN VICINITY OF VALVE. REPLACED PACK VALVE. REPLACED COUPLING SEALS. OPERATIONAL CHECK AND LEAK CHECK OK. (X) 2L73 4F A3WE 19951124000731995112400073NM 1995 11 24 TAOA109505 119951010A33501315 EEL LAMP GE BOEING727 727227 1384078NM CABIN FAILED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15925TS 21244 AFT STAIR EMERGENCY EXIT LIGHT INOP. RELAMPED. OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19951124000741995112400074WP 1995 11 24 VTZA95302 219950921A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RIGHT MALFUNCTIONED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27473UE 9499 828 P66050 IAD/SCE - FLT 6475 - DURING TAKEOFF AT 1715 HRS ON 9-21-95, ABORTED TAKEOFF DUE TO RT ENGINE DID NOT MAKE TARGET TAKEOFF TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO LYH FOR AN ENGINE CHANGE. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE COMPLETED ENGINE CHANGE ON 9-23-95. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA21EU E4WE 19951124000751995112400075 1995 11 24 VTZA95304 419950922A612289741016 PROP GOVERNOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110U 01514WP RT ENGINE OVERSPEED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27490UE 909 P66096 ABE/IAD - FLT 6154 - DURING TAKEOFF AT 2222 HRS ON 9-22-95, ABORTED TAKEOFF DUE TO RT ENGINE BETA LIGHT NOT EXTINGUISHING UNTIL THE ENGINE RPM REACHED 104 PERCENT. ALSO, THE TORQUE HUNG AT 23 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT PROP GOVERNOR AND RIGGED THE RIGHT SPEED LEVER LINKAGE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REFERENCE OPERATOR CONTROL NR 95ZZZX6273. (X) 2L72 4T4 TRTA56EU E4WE 19951124000761995112400076EU 1995 11 24 VTZA96002 119950930A32307445B SHUTTLE VALVE BAG JETSTMJETSTM3201 1500217EU LANDING GEAR ACTIVATED A VTZAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA27490UE 909 IAD/EWR - FLT 6263 - DURING TAKEOFF AT 1,115 HRS ON 9-30-95, RETURNED TO IAD DUE TO THE LANDING GEAR WILL NOT RETRACT WHEN SELECTED UP AFTER TAKEOFF. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE RESET THE SHUTTLE RELEASE VALVE AND THEN PERFORMED GEAR SWINGS. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19951124000771995112400077NM 1995 11 24 WRLA95042 119951008A32402609913 TEMP SENSOR DOUG MD11 MD11 3023602NM NR 7 BRAKE FAILED A WRLAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA27276WA 48632 OMDB - ON TAXI TO RUNWAY, AIRCRAFT EXPERIENCED A FAILIURE OF THE NR 7 BRAKE TEMPERATURE SENSOR. THE CAPTAIN ELECTED TO RETURN TO THE GATE FOR MAINTENANCE REVIEW OF THE MALFUNCTION. MAINTENANCE REPS INSPECTED THE NR 7 BRAKE TEMP INDICATOR CANNON PLUGS, SECURED WIRING AND INSTALLED DUST CAPS ON PLUGS. SENSOR STILL INOP. SENSOR DISCONNECTED AND DMI'D PER MEL 32-46-1 M320C08-12. TWO FLIGHTS LATER, IN KUL, BRAKE TEMP SENSOR REMOVED AND REPLACED (PN 2609913, SN OFF D6900, SN ON D7816). REACTIVATED THE NR 7 BRAKE TEMPERATURE SENSORS PER MEL. OPS CHECK NORMAL. DMI CLEARED. AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19951124000911995112400091WP 1995 11 24 9518139946 119950914A5330 SKIN DOUG DC9 DC931 3022065WP FS 746 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 746 BETWEEN LONGERON 20R TO 21R. REPAIRED SKIN (P/N 5911420-3), PER EA 99-102910. 2L72 4F A6WE 19951124000921995112400092NM 1995 11 24 9518142767 119951024A5315 FLOORBEAM BOEING727 7272M7 138407SNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01727RW 21656 DURING T-CHECK, FOUND CORROSION ON THE BS 1130 FLOORBEAM LOWER FORWARD CHORD LBL 30 TO RBL 60. REPAIRED CHORD (P/N 65-20822-3), PER EA 27-99369. 2L73 4F A3WE 19951124000931995112400093NM 1995 11 24 9518156635 119951028A5320 WEB BOEING747 747227B 1384888NM FS 2020 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01635US 21682 DURING PERIODIC CHECK, FOUND CORROSION ON THE BULK CARGO DOOR UPPER SILL WEB BS 2020. REPAIRED WEB (P/N 65B04262-3), PER EA 66-99161. 2L74 4F A20WE 19951124000941995112400094NM 1995 11 24 9518162767 119951101A5320 BEAM BOEING727 7272M7 138407SNM TAILSKID CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01727RW 21656 DURING T-CHECK, FOUND CORROSION ON THE TAIL SKID ACTUATOR BEAM LOWER CHORD, HORIZONTAL FLANGE. REPAIRED THE CHORD (P/N 65-26307-8), PER EA 22-99223. 2L73 4F A3WE 19951124000951995112400095WP 1995 11 24 9518179608 119951106A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 996 FITTING BETWEEN LONGERONS 27L TO 28L. REPLACED FITTING PER SRM 51-01. 2L72 4F A6WE 19951124000961995112400096NM 1995 11 24 9518186635 119951107A5320 FITTINGS BOEING747 747227B 1384888NM PORTAL LATCH CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01635US 21682 DURING PERIODIC CHECK, FOUND CORROSION ON THE NR 9 AND NR 13 PORTAL LATCH FITTINGS AND SERRATED PLATES. REPLACED FITTINGS, NR 9 PLATE AND REPAIRED THE WEB BENEATH NR 13 PER SRM 51-40-02. 2L74 4F A20WE 19951124000971995112400097WP 1995 11 24 9518199603 119951108A5320 FITTING DOUG DC9 DC932 3022066WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 29R END FITTING AT FS 756. REPLACED FITTING PER SRM 51-00 AND 51-30. 2L72 4F A6WE 19951124000981995112400098WP 1995 11 24 9518209966 119951108A5753 HINGE DOUG DC9 DC931 3022065WP LT TE CTR FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019330 30941 47138 DURING L-CHECK, FOUND CORROSION IN THE LEFT WING TRAILING EDGE CENTER FLAP HINGE UPPER INBOARD BOLT HOLE. REPLACED NR 3 FLAP HINGE (P/N 5919217-501). 2L72 4F A6WE 19951124000991995112400099WP 1995 11 24 9518219613 119951112A5320 FITTING DOUG DC9 DC932 3022066WP FS 1038 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01613NW 47438 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 1.5 INCH CRACK IN SUPPORT MOUNT FITTING FS 1038 AT LONGERON 14R. REPLACED FITTING PER SRM 51-00. 2L72 4F A6WE 19951124001001995112400100WP 1995 11 24 9518229978 119951113A5320 FITTING DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019342 47391 DURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L END FITTING AT FS 996. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951124001011995112400101WP 1995 11 24 9518239608 119951114A5312 BLKHD FITTING DOUG DC9 DC932 3022066WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD T-CAP TO FLOORBEAM TIE FITTING FS 996, RIGHT SIDE. REPLACED CASTING PER SRM 51-30-5 AND DWG 5911546. 2L72 4F A6WE 19951124001021995112400102NM 1995 11 24 9518266628 119951116A3610 DUCT BOEING747 747251B 1384892NM PWA JT9 JT9D7Q 52054NE NR 2 ENGINE FAILED A ANWAAAEFJUNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01628US 22389 702102 DURING ROTATION, THE NR 2 ENGINE FIRE WARNING ILLUMINATED, NACELLE TEMPERATURES PEGGED AND THE THRUST LEVER WOULD NOT REDUCE POWER. A FIRE BOTTLE WAS DISCHARGED, THE ENGINE WAS SHUTDOWN, AND ALL TEMPERATURES RETURNED TO NORMAL, 100,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO SFO WHERE AN UNEVENTFUL THREE ENGINE LANDING WAS ACCOMPLISHED. A 15TH STAGE DUCT HAD SEPARATED AT THE TOP OF THE ENGINE, SEVERAL WIRES WERE HEAT DAMAGED AND THE THRUST LEVER WAS STILL BOUND. THE AIRCRAFT WAS FERRIED TO ORD WHERE THE ENGINE WAS REPLACED AND ALL DISCREPANCIES WERE CORRECTED. 2L74 4F4 F A20WE E3NE 19951124001031995112400103WP 1995 11 24 9518271149 119951116A7830 TR UNIT DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 3 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01149US 46758 686146 THE NR 3 ENGINE REVERSER LIGHT ILLUMINATED AT 80 KNOTS AND THE TAKEOFF WAS ABORTED. THE REVERSER WAS LOCKED OUT AND PLACED ON MEL. 2L73 4F4 F A22WE E20EA 19951124001041995112400104WP 1995 11 24 9518289601 119951116A3350 EEL CONNECTOR DOUG DC9 DC932 3022066WP CABIN LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ROUTINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE IN THE AFT FOUR ROWS OF THE AIRCRAFT. RECONNECTED CONNECTOR, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124001051995112400105WP 1995 11 24 9518299866 119951106A7711 EPR IND/TRANS DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018913E 47785 68811 NR 1 ENGINE EPR DECREASED BY 0.10 ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND TRANSMITTER. SUBSEQUENT RUNUP WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951124001061995112400106NE 1995 11 24 9518309950 219951109A7321 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL019346 47376 655056 NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL ASSEMBLY, PRBC AND PERFORMED A FULL ENGINE TRIM. SUBSEQUENT RUNUP WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951124001071995112400107NE 1995 11 24 9518319154 219951110A7532 PRBC DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL018913E 45830 656991 NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC AND INSPECTED THE ENGINE, NO DAMAGE NOTED. SUBSEQUENT RUNUP WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951124001081995112400108NM 1995 11 24 9518326306 119951118A3350 EEL WIRE BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01666US 23821 TPE - DURING LINE CHECK, THE EMERGENCY PATH FLOOR LIGHTS BETWEEN SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRE PIN AT SEAT 42, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951124001091995112400109NM 1995 11 24 95FDE01755 119951117A5311 FRAME BOEING727 727227 1384078NM BS 600 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD BAY, FRAME DENTED AT BS 600 BETWEEN STR 22 TO 25L. REPAIRED DENTED FRAME IN FWD BAY AT BS 600 BETWEEN STR 22 TO 25L IAW FEDEX SRM 51-40-3. 2L73 4F A3WE 19951124001101995112400110NM 1995 11 24 95FDEA01768 119951121A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1148 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01, 2), ON BOTTOM CHORD OF FLOORBEAM BS 1148 LBL 21 RBL 12 WL 200 AT NUTPLATE HOLES. REPAIRED BOTTOM CHORD OF FLOORBEAM BS 1148 LBL 21 RBL 12 WL 200 AT NUTPLATE HOLES PER FEDEX SRM 53-10-1 AND 53-10-8 THAT WAS OUT OF LIMITS. 2L73 4F A3WE 19951124001111995112400111NM 1995 11 24 95FDEA01769 119951121A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 1130 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01(3)) ON BOTTOM CHORD OF FLOOR BEAM BS 1130, LBL 43-RBL 51, WL 200 AT NUTPLATE HOLES. REMOVED CORROSION ON BOTTOM CHORD OF FLOOR BEAM BS 1130, LBL 43-RBL 51. CORROSION FOUND TO BE OUT OF LIMITS AS PER FEDEX SRM 53-10-1. REPAIRED BOTTOM CHORD OF FLOOR BEAM BS 1130, LBL 43-RBL 51 AS PER FEDEX SRM 53-10-8 FIG 2. 2L73 4F A3WE 19951124001121995112400112NM 1995 11 24 95FDEA01770 119951121A5313 STRINGER BOEING727 727232 1384082NM BS 1126 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-04), ON STR 7R BS 1126. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED STRINGER IAW FEDEX SRM 53-10-3 AND EA 7-5310-26724. 2L73 4F A3WE 19951124001131995112400113NM 1995 11 24 95FDEA01771 119951121A5313 STRINGER BOEING727 727227 1384078NM BS 753-756 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 MECHANICAL DAMAGE ON STR 7L AT BS 753 TO 756. REPAIRED STR 7L AT 753 TO 756 PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951124001141995112400114NM 1995 11 24 95FDEA01772 119951116A5720 WEB BOEING727 727227 1384078NM WS 70.5-80.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5 IN L/W PIE SECTION. 2L73 4F A3WE 19951124001151995112400115NM 1995 11 24 95FDEA01773 119951117A5313 STRINGER BOEING727 727227 1384078NM BS 600 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 WHILE WORKING NR 0137, FOUND DAMAGED STRINGER 24L AT BS 600. 2L73 4F A3WE 19951124001161995112400116NM 1995 11 24 95FDEA01774 119951121A5315 FLOORBEAM BOEING727 727227 1384078NM BS 480 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 WHILE WORKING NR0651, FOUND CORROSION (C53-224-01) UNDER C-TRACK BS 480 WL 208 RBL 45. REMOVED CORROSION ON FLOORBEAM BS 480 WL 208 RBL 45. CORROSION WAS FOUND TO BE OUT LIMITS PER SRM 53-10-1, AREA 1 INCH BY 1 INCH BY .004 INCH, ORIGINAL THICKNESS .180. REPAIRED FLOORBEAM PER FEDEX SA 7-5310-26726. 2L73 4F A3WE 19951124001171995112400117NM 1995 11 24 95FDEA01775 119951121A572064834219 WEB BOEING727 727227 1384078NM WS 70.5-80.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5 IN LEFT WING PIE SECTION. REMOVED LEFT WING PIE SECTION, CRACKED WEB AND SUPPORT ANGLES BETWEEN WING STA 70.5 AND 80.5. FABRICATED NEW WEB, INSTALLED NEW WEB AND ANGLES AND REINSTALLED LEFT WING PER PIE SECTION. 2L73 4F A3WE 19951124001181995112400118NM 1995 11 24 95FDEA01776 119951117A2612 FIRE WIRE BOEING727 7272S2F 1384O81NM LT/RT MLG WW LOOSE A FDEAO OTHER N FALSE WARNING UKUNKNOWN 1 SO25206FE 22928 FIRE WARNING BELL SOUNDED INTERMITTENTLY AND FIRE WARNING LIGHTS ON THE DASH AND WHEEL WELL LIGHT FLICKERED. NO LIGHTS IN THE HANDLES ON THE OVERHEAD PANEL. BELL SILENCED ITSELF AND LIGHTS WENT OUT. RESECURED L AND R LOOP CONNECTIONS IN WHEEL WELLS AND OPS CHECK GOOD. 2L73 4F A3WE 19951124001191995112400119NM 1995 11 24 95FDEA01778 119951118A2612 FIRE WIRE CONN BOEING727 7272S2F 1384O81NM NR 3 ENGINE DIRTY A FDEAO OTHER N FALSE WARNING UKUNKNOWN 1 SO25206FE 22928 IMMEDIATELY AFTER DISCONNECTING NR 3 CSD, FIRE BELL AND WARNING LIGHTS ON PILOTS PANEL AND NR 3 FIRE HANDLE ILLUMINATED MOMENTARILY BOTH SYS-A AND LOOPS WERE TESTED, TEST WAS GOOD. FIRE BELL WOULD INTERMITTENLY COME ON. FOUND LOOSE CLAMP ON LOWER PART OF NR 3 ENG, CLEANED OILY CONNECTORS AND TIGHTENED CLAMP, OPS CK GOOD. 2L73 4F A3WE 19951124001201995112400120WP 1995 11 24 95FDEA01779 119951119A551272071 SKIN DOUG DC10 DC1010CF 3023502WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 HORIZONTAL STAB HAS ONE CRACK .948 INCH LONG IN THE AFT UPPER CONSTANT SECTION PANEL. CRACK STARTS AT AFT BOLT HOLE GOING FWD AND CRACK IS WITHIN FLYABLE LIMITS. REPETITIVE INSP PART 1 AT 24 MONTHS INTERVALS AND SPECIAL INSP TO START PART 2 AT 3 MONTHS INTERVALS PER WORK CARD WO 8-5510-7-2307H3, PT 1 AND 2 REF AD 88-03-08. 2L73 4F RTA22WE 19951124001211995112400121WP 1995 11 24 9DEA01780 119951119A2760APH72794 MIXER BRACKET DOUG DC10 DC1010CF 3023502WP SPOILER CONTROL CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 LT LATERAL CONTROL MIXER BRACKET ASSY WAS FOUND CRACKED ON HFEC INSP, PART 1 OF EO 8-2760-7-3310 C1. CRACK IS .25 INCH LONG ON RT LEG OF BRACKET AT RADIUS. 2L73 4F RTA22WE 19951124001221995112400122WP 1995 11 24 ABXA9500935 119951117A3260 DOOR LIGHT DOUG DC8 DC863 302198AWP RT MLG DOOR ILLUMINATED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23825AX 46115 DURING GEAR RETRACTION AFTER TAKEOFF, RIGHT MAIN LANDING GEAR DOOR LATCH LIGHT ILLUMINATED. RECYCLED LANDING GEAR AND LIGHTS EXTINGUISHED. INSPECTED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH AND WIRING, NO DEFECTS WERE FOUND. COMPLETED RIGHT MAIN LANDING GEAR DOOR PROXIMITY SWITCH TEST, THE DOOR LATCHED NORMALLY AND ALL INDICATIONS WERE GOOD. 2L74 4F 4A25 19951124001231995112400123NM 1995 11 24 DL72E951068 119950301A5347 SEAT TRACK BOEING727 727247 138408FNM BS 420-380 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO112823W 21328 SEAT TRACK CORRODED STA 420 TO 380. REPLACED SECTION OF TRACK PER MM 53-20-11. 2L73 4F A3WE 19951124001241995112400124NM 1995 11 24 DL72K954415 119951117A5320 ANGLE BOEING727 727232 1384082NM BS 913 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11414DA 21256 RT W/W STA 913 SHELF ANGLE CRACKED. REPAIRED PER MM 53-11-0, FOUND DURING A-2 LTR CK TPAMM. 2L73 4F A3WE 19951124001251995112400125NM 1995 11 24 DL72K954417 119951117A5414 SKIN BOEING727 727232 1384082NM NR 2 DUCT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11414DA 21256 ITEM FOUND DURING A-2 LTR CHK, 1.25 INCH CRACK AT FASTENERS AFT LWR CORNER PANEL 9516 RT SIDE NR 2 ENG DUCT HOUSING. REPAIRED PER B727 MM 54-30-0 PAR 1. 2L73 4F A3WE 19951124001261995112400126NM 1995 11 24 DL72K954418 119951117A5414 SKIN BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11414DA 21256 FOUND DURING A-2 LTR CHK, NR 2 ENG NOSECOWL SKIN CRACKED .75 INCH AT 1ST RIB AFT OF LIP. REPAIRED PER MM 54-30-0 PAR 1. 2L73 4F A3WE 19951124001271995112400127NM 1995 11 24 DL72K954419 119951117A5320 WEB BOEING727 727232 1384082NM BS 1183 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11414DA 21256 FOUND DURING A-2 LETTER CHECK, .25 INCH CRACK AT LIGHTENING HOLE AT TORQUE BOX VERTICAL WEB STA 1183. REPAIRED PER MM 53-11-0 PAGE 15. 2L73 4F A3WE 19951124001281995112400128NM 1995 11 24 DL72S954410 119951116A5754 ANGLE BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11494DA 21074 FOUND DURING A-1 LETTER CHECK, 4 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951124001291995112400129NM 1995 11 24 DL72S954416 119951117A2130 FLOW CONTL VLV 39608831 BOEING727 727232 1384082NM LEFT FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11523DA 495 21583 UNABLE TO MAINTAIN CABIN ALTITUDE IN CLIMB, REGAINED PRESSURIZATION BY CHECK LIST, FL 180 CABIN ALT CLIMBING OFF, LANDING PIT. REPLACED LEFT FLOW CONTROL VALVE AND RETURNED TO SERVICE. 2L73 4F A3WE 19951124001301995112400130NM 1995 11 24 DL72S954434 119951116A3350RPS1 EEL PWR SUPPLY BOEING727 727232 1384082NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11408DA 21152 DURING POWER TRANSFER FWD CABIN EMERGENCY FLOOR TRACK LIGHTS FAILED TO LIGHT. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L73 4F A3WE 19951124001311995112400131NM 1995 11 24 DL72W951524 119950331A5313 STRINGER BOEING727 727247 138408FNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11294WA 22112 REMOVED FASTENERS AND STOP DRILLED CRACK IN STRINGER 15L. INSTALLED REPAIR PER SRM 53-10-3 NR 2. 2L73 4F A3WE 19951124001321995112400132NM 1995 11 24 DL72W954421 119951117A2913MS219028 HYD PUMP BOEING727 727247 138408FNM B-HYD SYST FAILED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO112820W 21058 BIL - EN ROUTE, B-HYD PUMP NR 2 LOW PRESS LIGHT ILLUM, B-QTY WENT TO 0. B-SYS LOSS OCCURED FOLLOWED BY UNEVENTFUL LANDING. REPLACED NR 2 B-HYD PUMP AND B-SYS CASE DRAIN FILTERS, HYD MODULE B-NUT FITTING AND LEAK CHECK OK. 2L73 4F A3WE 19951124001331995112400133NM 1995 11 24 DL72W954426 119951117A5542 SKIN BOEING727 727247 138408FNM RUDDER DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO112814W 20870 RT SIDE OF LOWER RUDDER HAS A SMALL 1 INCH CREASE, APPROX 8 INCHES ABOVE PANEL 9901 MIDDLE OF RUDDER. STOP DRILLED DAMAGE AS PER B-727 SRM 55-40-2 FIG 1 AND B727 SRM 55-20-3 FIG 4. FABRICATED REPAIR PART AS PER B727 SRM 55-40-2 FIG 1 AND B727 SRM 55-20-3 FIG 4. 2L73 4F A3WE 19951124001341995112400134NM 1995 11 24 DL72W954431 119951118A3350900851A BATTERY PACK BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO112822W 21327 CENTER AISLE EMERGENCY EXIT SIGN FLASHES. REPLACED BATTERY PACK, CHECKS GOOD. 2L73 4F A3WE 19951124001351995112400135NM 1995 11 24 DL73S954423 119951118A3350 EEL PIGTAIL 081691 BOEING737 737232 1384475NM CABIN MISSING A DALAK NONE L NO TEST ININSP/MAINT 1 SO11305DL 23077 PIGTAIL FOR A WHITE EMERGENCY FLOOR TRACK LIGHT WAS TORN OUT. REPLACED PIGTAIL ASSY LIGHT BULB AND LENS ASSY AT SEAT 1-C. LIGHT OPS CHECK OK. 2L72 4F RTA16WE 19951124001361995112400136NM 1995 11 24 DL757954411 119951116A2560D30655123 SLIDE BOTTLE BOEING757 757232 1384965NM R 2 DOOR LOW PRESSURE A DALAK NONE O OTHER ININSP/MAINT 1 SO11640DL 23994 DURING SERVICE CHECK, FOUND R-2 SLIDE BOTTLE PRESSURE BELOW LIMITS. REPLACED SAME. 2L72 4F RTA2NM 19951124001371995112400137NM 1995 11 24 DL767954412 119951105A5712113T15671 RIB BOEING767 767232 1385132NM WS 716 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11106DA 22218 NR 2 SPOILER ACTUATOR OUTBOARD SUPPORT RIB AT WS 716 CRACKED IN HALF, IPC 57-11-53-03, ITEM 715. REPLACED RIB. 2L72 4F RTA1NM 19951124001381995112400138NM 1995 11 24 DL767954424 119951118A2910AE70577778 HYD LINE AE70577778 BOEING767 767232 1385132NM NR 1 ENGINE CHAFED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO11101DA 22213 LT HYD SYS PRES MESSAGE, HYD QTY APPEARED TO STOP DECREASING AFTER TURNING OFF LEFT HYD SYSTEM. FOUND LEFT ENG HYD LINE FROM ENG PUMP CHAFING. REPLACED HYD LINE PER M/M CHAPTER 29. RAN ENG AND OPERATED ALL FLT CONTROLS, NO FURTHER LEAKS FOUND. A/C OK FOR SERVICE. 2L72 4F RTA1NM 19951124001391995112400139NE 1995 11 24 DL76L954435 219951118A7314825500 FUEL PUMP BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 ENG CRACKED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO11175DN 24803 DIFFERENCE BETWEEN CALCULATED AND TOTALIZER FUEL GREW TO 4,000 LBS. CALCULATED WAS GREATER, NO FUEL LEAK OBSERVED DURING FLT. FOUND NR 1 ENGINE FUEL PUMP HOUSING CRACKED. REPLACED PUMP, OPERATION NORMAL. 2L72 4F4 FRTA1NM E24NE 19951124001401995112400140NM 1995 11 24 DL76S951861 119950503A5754114T410338A TE WEDGE BOEING767 767332 1382001NM RT LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11135DL 25145 DURING SHOP INSPECTION, RT WING L/E SLAT PANEL WAS FOUND WITH HAIL DAMAGE TO T/E WEDGE. REPLACED WEDGE PER MM 57-43-55. 2L72 4F RTA1NM 19951124001411995112400141WP 1995 11 24 DLL10951922 119950502A5755 BEAM LKHEED1011 10113851 5265010WP NR 2 SPOILER CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO11717DA 193C1096 DURING INSPECTION, FOUND LT NR 2 SPOILER BAT WING HINGE ATTACH STRUCTURE CRACKED. INSTALLED REPAIR PER SRM 57-22-00 PG 807 AND 808. 2L73 4F A23WE 19951124001421995112400142WP 1995 11 24 DLL10954420 119951116A2150 DUCT 1505475163D LKHEED1011 10113851 5265010WP NR 3 ACM RUPTURED A DALAO OTHER O OTHER CRCRUISE 1 SO11721DA 193C1139 AT FL 370 HEARD LOUD BANG, POSSIBLY PNEU IN NATURE. CABIN PRESSURE NORMAL, ENGINE BLD CONT PANEL PSIG NORMAL. SUBSEQUENTLY C/D ZONES TURNED ICE COLD, WAS ABLE TO SUPPLY MAX HOT TEMP IN DUCT SUPPLY, BUT ZONE NEVER WARMED UP. SUSPECT POSSIBLE DUCT FAILURE. FOUND RT O/B DUCT RUPTURED ON NR 3 ACM. REPLACED SAME, OPERATION NORMAL. 2L73 4F A23WE 19951124001431995112400143WP 1995 11 24 DLL13952196 119950510A57551529104190 PANEL LKHEED1011 10113851 5265010WP NR 4 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO11785DL 193A1121 DURING SHOP INSPECTION, NR 4 SPOILER PANEL WAS FOUND WITH DELAMINATION. REPAIRED PANEL PER LAC DWG 1529104190. 2L73 4F A23WE 19951124001441995112400144WP 1995 11 24 DLL14954407 119951116A3350 EEL LENS LKHEED1011 1011385115 5265015WP CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO11741DA 193C1245 EXIT LIGHT LENS ON FWD SIDE OF FIRST CLASS GALLEY RIGHT SIDE MISSING. REPLACED LENS, LIGHT OP CHECKS NORMAL. 2L73 4F A23WE 19951124001451995112400145WP 1995 11 24 DLL16950922 119950212A5330 SKIN LKHEED1011 10113853 5265020WP FS 323 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO11759DA 193Y1176 DURING INSPECTION, FOUND LT FUSELAGE SKIN AT FS 323 DENTED BEYOND LIMITS. CUT OUT DAMAGE AND DYE CHECKED, FOUND NO CRACKS. C/W STEPS 3 AND 4 OF ERA 270330-14. 2L73 4F A23WE 19951124001461995112400146NM 1995 11 24 DLM88954414 119951117A2910 HYD FITTING DOUG MD88 MD88 3023688NM TAIL COMP LOOSE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11918DL 49583 SMOKE IN CABIN JUST AFTER T/O. REPLACED COALESCER BAGS, INSP BOTH MAIN WHEEL WELLS. HYDRAULIC FLUID OVERFLOW BOTTLES EMPTY AND FOUND RT HYD SYSTEM FILTER LEAKING. SECURED FITTING, LEAK CHECK GOOD. CLEANED LOWER FUSELAGE, RAN ENGINES AND PACKS, NO SMOKE NOTED, RETURNED TO SERVICE. 2L72 4F RTA6WE 19951124001471995112400147NM 1995 11 24 DLM88954433 119951117A3350 EEL FUSE DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO11911DE 49967 DURING PREFLIGHT, FWD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED FUSE IN BATTERY PACK, OPERATION NORMAL. 2L72 4F RTA6WE 19951124001481995112400148 1995 11 24 MWEA95431 419951117A2565113317 EVAC SLIDE DOUG DC9 DC914 3022034WP FWD GALLEY DOOR LOW PRESSURE A MWEAK NONE O OTHER ININSP/MAINT 1 GL3180ME 1526 45795 DURING INSPECTION, FOUND GALLEY SERVICE DOOR EVACUATION SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951124001491995112400149WP 1995 11 24 MWEA95432 119951117A2560 SLIDE PIN DOUG DC9 DC932 3022066WP SERVICE DOOR FELL OUT A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31204ME 47680 CREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER RETAINING PIN FELL OUT. MAINTENANCE REPLACED EVACUATION SLIDE DOOR AND PIN, RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951124001501995112400150WP 1995 11 24 MWEA95433 119951119A25603952273501 GIRT BAR LATCHES DOUG DC9 DC915 3022036WP FWD PAX DOOR DIRTY A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31300ME 45718 CREW REPORTS, GIRT BAR ON FWD PAX DOOR IS DIFFICULT TO ARM AND DISARM. MAINTENANCE CLEANED AND LUBRICATED GIRT BAR LATCHES. OPS CHECK GOOD AND A/C RETURNED TO SERVICE. 2L72 4F A6WE 19951124001511995112400151NM 1995 11 24 P5CA9500842 119951117A5347 SEAT TRACK BOEING747 747121 1384871NM F/O'S SEAT BROKEN A P5CAK NONE O OTHER TOTAKEOFF 1 WP23832FT 20347 ON TAKEOFF FROM CHICAGO, F/O'S LEFT AFT SEAT TRACK BROKE. ALSO, UPON ARRIVAL AT ANCHORAGE, MAINTENANCE DISCOVERED RIGHT FWD TRACK CRACKED. REPLACED BOTH SEAT TRACK ASSEMBLIES, PART NR 812168-8 AND 811371-412, IAW MM 25-11-01. 2L74 4F A20WE 19951124001521995112400152SO 1995 11 24 SWIA95679 119951111A2912 HYD FILTER EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT HYD SYST DIRTY A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07209SW 120269 AFTER TAKEOFF, RT HYDRAULIC FILTER LIGHT ILLUMINATED. FOUND RETURN HYDRAULIC FILTER BYPASS BUTTOM POPPED. REPLACED RETURN HYD FILTER, RESET BYPASS BUTTON, RAN RT HYD SYSTEM AND INSPECTED FOR LEAKS. NO LEAKS NOTED AND OPS CK GOOD. 2L72 4T4 TRTA31SO E20NE 19951124001531995112400153SO 1995 11 24 SWIA95680 119951113A3230 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG FAILED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07203SW 120240 LANDING GEAR HANDLE WILL NOT COME UP WITHOUT DOWN LOCK RELEASE BUTTON PRESSED MEL 32-31-1. ELIMINATED LANDING GEAR SHOCK ABSORBER PROXIMITY SENSORS, ALL THREE LT LANDING DOWN LOCK PROXIMITY SENSORS BY SLAVING IN GOOD SENSORS. REMOVED AND REPLACED RT MAIN LANDING SHOCK ABSORBER PROXIMITY SENSOR, ALL SYSTEMS OPERATE NORMAL. GEAR HANDLE RELEASES AS REQUIRED, ALL OTHER RELATED SYSTEMS MM 32-01-01, ALL CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951124001541995112400154SW 1995 11 24 SWIA95681 119951113A2710 ROD END SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT AILERON FAILED A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM0726895 AC656 WHILE ON APPROACH, HEARD A POP AND LOST HALF OF AILERON CONTROLS. ON POST FLIGHT INSPECTION, FOUND TOWARD ROD END ON LT AILERON BELL CRANK TO BE BROKEN. REMOVED AND REPLACED BOTH FORWARD AND AFT ROD END ON LT AILERON BELL CRANK, TRAVEL CHECK GOOD. 1L72 4T4 T A8SW E4WE 19951124001551995112400155SO 1995 11 24 SWIA95682 119951119A3232WTC22461 ACTUATOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT MLG DOOR FAILED A SWIAO OTHER J WARNING INDICATION CLCLIMB 1 NM07205SW 120260 LT MAIN GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LT MAIN GEAR DOOR ACTUATOR I/B. OPERATED GEAR SEVERAL TIMES, OPS CHECK AND LEAK CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19951124001561995112400156EA 1995 11 24 SWIA95683 119951119A5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT COCKPIT CRACKED A SWIAA UNSCHED LANDING O OTHER CRCRUISE 1 NM07403SW 7028 WHILE LEVEL AT FL 350, CAPTAIN'S WINDSHIELD CRACKED, DIVERTED TO RKS. DESCENT AND LANDING WERE UNEVENTFULL. CONTACTED SGU MX CONTROL REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-00 PAGES 401 TO 410. TORQUED ALL BOLTS AND REINSTALLED NEW SEAL. 2L72 4F4 FRTA21EA E15NE 19951124001571995112400157WP 1995 11 24 UPS205096 119951115A33506012335 BATTERY PACK DOUG DC8 DC871F 302199DWP CABIN DISCHARGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01797UP 45897 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS DO NOT DISARM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2L74 4F RT4A25 19951124001581995112400158WP 1995 11 24 UPS205098 119951117A3231 RETRACT MECH DOUG DC8 DC873F 302199FWP RT MLG DOOR OUT OF ADJUST A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01816UP 45990 CREW REPORTED AFTER GEAR RETRACTION, DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED. RECYCLED GEAR AND LIGHT WENT OUT, UPLATCH CHECK NORMAL. MAINTENANCE REPORTED RIGHT MLG DOOR RUBBING AGAINST FUSELAGE WHEN IN THE UP POSITION. REPAIRED IAW EO DC8-5720-3729-A. 2L74 4F RT4A25 19951124001591995112400159NM 1995 11 24 UPS205101 119951117A3230 RETRACT MECH BOEING727 72727C 138400JNM NLG LACK OF LUBE A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01909UP 19115 SDF - CREW REPORTED ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. MAINTENANCE CHECKED OVER CENTER LINK AND LUBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECKED TIME PER MM 32-32-00, WITHIN TIME LIMIT. 2L73 4F A3WE 19951124001601995112400160WP 1995 11 24 UPS805100 119951116A3350 EEL WIRE DOUG DC8 DC873F 302199FWP CABIN FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01805UP 46117 CREW REPORTED, F/O'S OTB BACKGROUND LIGHT INOP IN NORMAL AND EMERGENCY. MAINTENANCE REPAIRED WIRE AT RECEPTACLE. 2L74 4F RT4A25 19951124001611995112400161EA 1995 11 24 95ZZZX6291 119951016A29136305405 HYDRAULIC PUMP DHAV DHC7 DHC7102 2802708EA NR 3 ENGINE FAILED A HNAAK NONE J WARNING INDICATION CRCRUISE 1 EA07900HA19758 168392 025 BWI/DCA - FLT 3281 - THE LEFT MAIN GEAR DROPPED SLIGHTLY IN-FLIGHT AND THE GEAR DOOR OPENED. THE AIRCRAFT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. FOUND NR 2 HYDRAULIC SYSTEM CASE DRAIN FILTER CONTAMINATED. REMOVED AND REPLACED NR 3 AND NR 4 HYDRAULIC PUMPS. REFERENCE OPERATOR CONTROL NR 95ZZZX6292. 2H74 4T A20EA 19951124001621995112400162EA 1995 11 24 95ZZZX6292 119951016A29136305405 HYDRAULIC PUMP DHAV DHC7 DHC7102 2802708EA NR 4 ENGINE FAILED A HNAAK NONE J WARNING INDICATION CRCRUISE 1 EA07900HA7976 168554 025 BWI/DCA - FLT 3281 - THE LEFT MAIN GEAR DROPPED SLIGHTLY IN-FLIGHT AND THE GEAR DOOR OPENED. THE AIRCRAFT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. FOUND NR 2 HYDRAULIC SYSTEM CASE DRAIN FILTER CONTAMINATED. REMOVED AND REPLACED NR 3 AND NR 4 HYDRAULIC PUMPS. REFERENCE OPERATOR CONTROL NR 95ZZZX6291. 2H74 4T A20EA 19951124001631995112400163NM 1995 11 24 95ZZZX6293 119951007A3260 GEAR LIGHT DHAV DHC8 DHC8102 2809003NM NLG ILLUMINATED A HNAAO OTHER N FALSE WARNING CRCRUISE 1 EA07910HA 022 EYW/MIA - FLT 3298 - THE NOSE GEAR UNSAFE LIGHT CAME ON IN-FLIGHT. THE NOSE GEAR CYCLED SEVERAL TIMES. THE AIRCRAFT CONTINUED ON TO MIA AND LANDED WITHOUT INCIDENT. CLEANED AND INSPECTED NOSE GEAR DOWNLOCK/UPLOCK SENSOR AND WIRING. CHECKED GAP ON SENSOR, NO DEFECTS NOTED. 2H72 4T RTA13NM 19951124001641995112400164EA 1995 11 24 95ZZZX6294 119951029A323072970021001 SURGE DAMPER DHAV DHC7 DHC7102 2802708EA LT MLG FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07900HA38625 025 ORF/DCA - FLT 3004 - THE LEFT MAIN GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. THE AIRCRAFT TURNED BACK TO ORF AND LANDED WITHOUT INCIDENT. INSPECTED THE GEAR AND RELEASED FOR AN EVALUATION FLIGHT. EVALUATION FLIGHT WAS SATISFACTORY, NO DISCREPANCY NOTED AT THIS TIME. DCA/HPN - FLT 3093 - LATER IN THE DAY, THE LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT TURNED BACK TO DCA AND LANDED WITHOUT INCIDENT. AFTER FERRYING TO ORF, FOUND THE LEFT SURGE DAMPER BAD. REMOVED AND REPLACED THE LEFT SURGE DAMPER. 2H74 4T A20EA 19951124001651995112400165NM 1995 11 24 95ZZZX6295 119951025A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07906HA20656 313 009 TPA/TLH - FLT 3040 - THE LANDING GEAR WOULD NOT EXTEND AFTER SELECTED DOWN UPON APPROACH. THREE RED UNSAFE LIGHTS ILLUMINATED. THE CREW PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. 2H72 4T RTA13NM 19951124001661995112400166EA 1995 11 24 95ZZZX6296 119951029A5220 PRESSURE LINE DHAV DHC7 DHC7102 2802708EA EMER EXIT DOOR FAILED A HNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA07905HA31636 070 ORF/DCA - FLT 3144 - THE AIRCRAFT RETURNED TO THE GATE PRIOR TO TAKEOFF BECAUSE THE AIRSTAIR DOOR SEAL AND EMERGENCY DOOR SEAL, PN 75210458109, WOULD NOT INFLATE. REPAIRED THE BROKEN PRESSURE LINE INSIDE THE RIGHT REAR EMERGENCY EXIT DOOR. LATER IN THE DAY, REMOVED AND REPLACED THE UPPER AIRSTAIR DOOR END PLATE SEALS. 2H74 4T A20EA 19951124001671995112400167CE 1995 11 24 95ZZZX6297 119951020A56101143840201 WINDSHIELD BEECH 1900 1900D 1154162CE LT SHORTED OUT A UUAAO OTHER O OTHER CLCLIMB 1 SO1745AR 1374 UE12 UPON CLIMB-OUT, PILOTS WINDSHIELD SHORTED, BURNING OFF THE CONNECTION AT THE BOTTOM RT ELECTRICAL CONNECTION. 2L72 4T RTA24CE 19951124001681995112400168NM 1995 11 24 95ZZZX6298 119951103A33506005401 BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSEMBLY AND BATTERY; LIGHT OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR ASAA9510101. (X) 2L72 4F RTA16WE 19951124001691995112400169NM 1995 11 24 ASAA510099 119951102A33508731002142 EEL ASSY BOEING737 7372X6C 1384552NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001701995112400170NM 1995 11 24 ASAA9510092 119951008A33501060091101 EEL ASSY BOEING737 7372X6C 1384552NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001711995112400171NM 1995 11 24 ASAA9510093 119951009A3350900835A EEL BATTERY PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS IN THE FORWARD SEAT PALLET WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A16WE 19951124001721995112400172NM 1995 11 24 ASAA9510096 119951024A3350900835A BATTERY PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST NRNOT REPORTED 1 NM01741AS 21959 ANC - ON ARRIVAL OF FLT 87, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 6 AND 7 COME ON INADVERTENTLY. UNABLE TO DUPLICATE PROBLEM. REPLACED BATTERY PACK AS PRECAUTIONARY MEASURE AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A16WE 19951124001731995112400173NM 1995 11 24 ASAA9510097 119951031A3350900835A BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 14 AND 15 REMAINED ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A16WE 19951124001741995112400174NM 1995 11 24 ASAA9510098 119951031A335086210144 BATTERY PACK BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHT OPERATED NORMALLY. (X) 2L72 4F A16WE 19951124001751995112400175NM 1995 11 24 ASAA9510100 119951103A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE AT ROW 20. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001761995112400176NM 1995 11 24 ASAA9510101 119951103A33501060091102 EEL ASSY BOEING737 7372X6C 1384552NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND DIM. REPLACED LIGHT ASSEMBLY AND BATTERY; LIGHT OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR 95ZZZX6298. (X) 2L72 4F RTA16WE 19951124001771995112400177NM 1995 11 24 ASAA9510102 119951103A3350MISC0639 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE R-1 OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. CHARGED BATTERY PACK AND LIGHT OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001781995112400178NM 1995 11 24 ASAA9540061 119950930A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 SEA - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT THIRD LIGHT AND ALL LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001791995112400179NM 1995 11 24 ASAA9540062 119951002A33508100022607 EEL ASSY BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001801995112400180NM 1995 11 24 ASAA9540063 119951014A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK LIGHT WIRING AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001811995112400181NM 1995 11 24 ASAA9540064 119951015A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK LIGHT WIRING, REPLACED LENS AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001821995112400182NM 1995 11 24 ASAA9540065 119951015A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK LIGHT WIRING, REPLACED LENS AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001831995112400183NM 1995 11 24 ASAA9540066 119951016A3350900835A BATTERY PACK BOEING737 7374Q8 NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01779AS 25111 JNU - DURING MAINTENANCE CHECK, THE LEFT AFT EMERGENCY LIGHTS BATTERY PACK WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001841995112400184NM 1995 11 24 ASAA9540067 119951017A3350276005 EEL FUSE BOEING737 7374Q8 NM CABIN BLOWN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 SEA - DURING MAINTENANCE CHECK, THE AFT SIX EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED FUSE IN BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001851995112400185NM 1995 11 24 ASAA9540072 119951025A3230189915 SENSOR BOEING737 7374Q8 NM NLG OUT OF ADJUST A ASAAO OTHER J WARNING INDICATION CLCLIMB 1 NM01754AS 25095 SFO - FLT 110 - GEAR HANDLE WOULD NOT GO BEYOND THE 'OFF' POSITION AFTER TAKEOFF SEA. RETRACTED THE FLAPS AND NO HORN SOUNDED. USED OVERRIDE AND GEAR RETRACTED NORMALLY. RECYCLED GEAR AGAIN WITH NORMAL RETRACTION AND INDICATIONS. CONTINUED TO SFO AND LANDED WITHOUT INCIDENT. FOUND AIR SAFETY SENSOR AIR GAP EXCESSIVE. ADJUSTED SENSOR, PERFORMED GEAR RETRACTION, AND SYSTEM OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951124001861995112400186NM 1995 11 24 CAL950916 119951014A276165449617 ACTUATOR BOEING737 7372C0 1384488NM NR 1 GRD SPOILERLEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW091024215524 20071 EWR - FLT 0244 - THE A-HYDRAULIC SYSTEM WAS LOST AFTER LANDING AT EWR. THE PUMPS WERE FEATHERED WITHIN ONE MINUTE OF LOW PRESSURE LIGHT ILLUMINATION. MAINTENANCE FOUND THE NR 1 GROUND SPOILER ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-62-101, PAGE 401. LEAK AND OPERATIONAL CHECKS WERE GOOD. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. (X) 2L72 4F A16WE 19951124001871995112400187NM 1995 11 24 CAL950917 119951015A3260 DNLOCK SENSOR BOEING737 7373T0 1384582NM NLG INOPERATIVE A CALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW0914308 23359 IAH - FLT 0692 - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED ON APPROACH TO IAH. THE TOWER REPORTED THE NLG WAS NOT DOWN. DURING A FLY-BY, A VISUAL INSPECTION ALSO CONFIRMED NLG WAS NOT DOWN. CYCLING GEAR TWICE AND USING MANUAL EXTENSION PROCEDURES RESULTED IN NO CHANGE. AN EMERGENCY WAS DECLARED, GEAR WAS RETRACTED AGAIN, AND ANOTHER APPROACH WAS ATTEMPTED. WHEN GEAR WAS EXTENDED, MLG LIGHTS WERE NORMAL, BUT NO NLG GREEN LIGHT, NLG LIGHT WAS SWITCHED WITH LT MLG GREEN LIGHT AND NLG SHOWED DOWN AND GREEN. ACFT LANDED WITHOUT INCIDENT. MX FOUND NLG DOWNLOCK SENSOR AT FAULT. SENSOR REMOVED AND REPLACED PER MM 32-61-41. OPER CHKS GOOD DURING GEAR SWING. (X) 2L72 4F RTA16WE 19951124001881995112400188NM 1995 11 24 CAL950924 119951011A5320 ANGLE BOEING737 737130 1384435NM BS 664 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092421364630 19030 GSO - INSPECTION FOUND A 2.5 INCH CRACK IN RADIUS OF RT LOWER FORWARD SHEAR BEAM ATTACH ANGLE AT STA 664. THE CRACKED ANGLE WAS REMOVED AND SHEAR BEAM MODIFICATION KIT PART NR 5310-02450-10 WAS INSTALLED IAW EA 5310-02450. (X) 2L72 4F A16WE 19951124001891995112400189NM 1995 11 24 CAL950925 119951004A5315 FLOOR BEAM BOEING737 737130 1384435NM BS 700-717 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW092421364630 19030 GSO - INSPECTION FOUND FLOOR BEAM WEB CRACKED AT FIVE EACH LOWER FASTENER HOLES BETWEEN BS 700-BS 717, BBL 0.07. THE COMBINED CRACK LENGTH WAS APPROXIMATELY 5 INCHES. THE CRACKED SECTION OF WEB WAS REMOVED AND A NEW WEB AND DOUBLER WERE FABRICATED AND INSTALLED IAW EA 5710-01322. (X) 2L72 4F A16WE 19951124001901995112400190NM 1995 11 24 CAL950926 119951004A5754 SKIN BOEING737 7373T0 1384582NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW095933827928 23576 HOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF THREE RIVETS ON NR 6 SLAT LOWER SKIN AT INBOARD AUXILIARY TRACK. TOTAL LENGTH OF CRACKS WAS 2.5 INCHES. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-01159. (X) 2L72 4F RTA16WE 19951124001911995112400191NM 1995 11 24 CAL950927 119951004A5754 SKIN BOEING737 7373T0 1384582NM NR 6 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW095933827928 23576 HOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF TWO RIVETS ON NR 6 SLAT LOWER SKIN BETWEEN TAIL DUCT AND ACTUATOR. TOTAL LENGTH OF CRACKS WAS 1.125 INCHES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5750-01159. (X) 2L72 4F RTA16WE 19951124001921995112400192NM 1995 11 24 CAL950928 119951004A5754 SKIN BOEING737 7373T0 1384582NM NR 1 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW095933827928 23576 HOU - INSPECTION FOUND CRACKS COMING FROM A LINE OF SIX RIVETS ON NR 1 SLAT LOWER SKIN JUST OUTBOARD OF ACTUATOR ATTACH FITTING. TOTAL LENGTH OF CRACKS WAS 5.5 INCHES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C30133 AND ECRA 5750-01159. (X) 2L72 4F RTA16WE 19951124001931995112400193NM 1995 11 24 CAL950929 119951004A5542 SKIN BOEING737 7373T0 1384582NM RUDDER GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW095933827928 23576 HOU - INSPECTION FOUND A 0.2 INCH WIDE BY 6 INCH LONG GOUGE IN RUDDER RIGHT SKIN PANEL. THE AREA WAS REPAIRED IAW ECRA 5540-01061 AND SRM 51-70-17, FIGURE 19. (X) 2L72 4F RTA16WE 19951124001941995112400194NE 1995 11 24 CAL950948 219951023A7260 O-RINGS BOEING737 7373T0 1384582NM GE CFM56 CFM563B1 13802NE NR 2 GEARBOX CUT A CALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0912349 23587 721227 GSO - FLT 0171 - THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO GSO. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE CREW REPORTED LOSING LESS THAN 8.5 PSI OIL PRESSURE. MAINTENANCE FOUND THE NR 2 ENGINE ANGLE GEARBOX LEAKING AT O-RINGS. THE O-RINGS WERE REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. THE NR 2 ENGINE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE DUE TO THE OIL LOSS. (X) 2L72 4F4 FRTA16WE E2GL 19951124001951995112400195NM 1995 11 24 CAL950956 119951024A5230 SKIN BOEING737 737222 1384473NM CARGO DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - INSPECTION FOUND A .50 INCH CRACK AT FORWARD LOWER CORNER OF AFT CARGO DOOR CUT-OUT, EXTERNAL SKIN. THE CRACKED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW TIMCO ENGINEERING ORDER RFO-01655. (X) 2L72 4F A16WE 19951124001961995112400196NM 1995 11 24 CAL950958 119951024A531165C2511345 FRAME BOEING737 737222 1384473NM BS 420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - INSPECTION FOUND A CRACK IN FRAME AT BS 420 BETWEEN S22R AND S21R AND BETWEEN S21R AND S20R. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X) 2L72 4F A16WE 19951124001971995112400197NM 1995 11 24 CAL950959 119951024A531165C2511310 FRAME BOEING737 737222 1384473NM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500 BETWEEN STR 21L AND STR 22L AND STR 22L AND STR 23L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .75 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X) 2L72 4F A16WE 19951124001981995112400198NM 1995 11 24 CAL950960 119951024A531165C2511315 FRAME BOEING737 737222 1384473NM BS 500B CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - INSPECTION FOUND CRACKS IN FRAME AT BS 500B BETWEEN STR 19L AND STR 20L, AND BETWEEN STR 25L AND STR 27L. THE CRACK AT EACH LOCATION WAS APPROXIMATELY .33 INCH LONG. THE CRACKED SEGMENT OF FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113. (X) 2L72 4F A16WE 19951124001991995112400199NM 1995 11 24 CAL950962 119951024A531165C251137 FRAME BOEING737 737222 1384473NM BS 460 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023663432 19937 GSO - AIRCRAFT IN 1/2 D-CHECK DURING INSPECTION, FOUND CRACK IN FRAME SEGMENT AT BS 460 APPROXIMATELY .75 INCH, BETWEEN S20L AND S21L. REMOVED AND REPAIRED. (X) 2L72 4F A16WE 19951124002001995112400200NM 1995 11 24 CAL950963 119951024A531165C251139 FRAME BOEING737 737222 1384473NM BS 480 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0910236 19937 GSO - AIRCRAFT IN ONE-HALF D-CHECK DURING INSPECTION, FOUND CRACK FRAME SEGMENT APPROXIMATELY .05 INCH AT BS 480 BETWEEN S20L AND S21L. REMOVED AND REPLACED. (X) 2L72 4F A16WE 19951124002011995112400201NM 1995 11 24 CAL950997 119951013A5754 SKIN BOEING737 7373T0 1384582NM NR 2 SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091333128453 23569 HOU - INSPECTION FOUND CRACKS EXTENDING FROM RIVET HOLES OF NR 2 SLAT LOWER SKIN. THE CRACKS RAN FROM RIVET TO RIVET. ONE CRACK TOTALED 6 INCHES IN LENGTH AND THE OTHER TOTALED 5 INCHES IN LENGTH. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-01159 AND BOEING DRAWING NR 65C30133. (X) 2L72 4F RTA16WE 19951124002021995112400202NM 1995 11 24 CAL950998 119951013A5330 SKIN BOEING737 7373T0 1384582NM BS 294.5-344 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091333128453 23569 HOU - INSPECTION FOUND A .25 INCH DENT IN FUSELAGE SKIN BELOW R-2 DOOR BETWEEN STA 294.5 AND STA 344. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210. (X) 2L72 4F RTA16WE 19951124002031995112400203WP 1995 11 24 CKSA95052 119950615A5320 STIFFENER DOUG DC8 DC855 3021927WP BS 1340 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING B-CHECK INSPECTION, FOUND FS 1340 - FS 1360 AT LONGERON 26 LEFT STIFFENER, CORRODED. REPLACED DAMAGED STIFFENER IAW SRM 51-1-0. FASTENERS INSTALLED IAW SRM 51-3-0. (X) 2L74 4F 4A25 19951124002041995112400204WP 1995 11 24 CKSA95053 119950615A5320 FITTING DOUG DC8 DC855 3021927WP BS 1490 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING C-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 34 LEFT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) 2L74 4F 4A25 19951124002051995112400205WP 1995 11 24 CKSA95054 119950615A5320 FITTING DOUG DC8 DC855 3021927WP BS 1490 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 30 LEFT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) 2L74 4F 4A25 19951124002061995112400206WP 1995 11 24 CKSA95055 119950615A5320 FITTING DOUG DC8 DC855 3021927WP BS 1490 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 34 RIGHT END, FITTING CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) 2L74 4F 4A25 19951124002071995112400207WP 1995 11 24 CKSA95056 119950615A5320 FITTING DOUG DC8 DC855 3021927WP BS 1490 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 32 RIGHT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) 2L74 4F 4A25 19951124002081995112400208WP 1995 11 24 CKSA95057 119950615A5320 FITTING DOUG DC8 DC855 3021927WP BS 1490 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK58768 45816 KMIA - DURING B-CHECK INSPECTION, FOUND FS 1490 EMPENNAGE, LONGERON 28 RIGHT END FITTING, CRACKED. REMOVED CRACKED FITTING, CLEANED AREA, AND INSTALLED NEW FITTING IAW SRM 53-1-0, AND NEW FASTENERS IAW SRM 51-1-20. (X) 2L74 4F 4A25 19951124002091995112400209WP 1995 11 24 CKSA95058 119950620A5321 PANEL DOUG DC8 DC861F 3021953WP GALLEY FLOOR CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23813CK49741 45893 KYIP - DURING 'C-3' CHECK INSPECTION, FOUND GALLEY FLOOR CORRODED. REMOVED AND CUT OUT CORRODED PORTION OF GALLEY FLOOR AND REPAIRED PER EA NR 95-168.C. (X) 2L74 4F 4A25 19951124002101995112400210WP 1995 11 24 CKSA95059 119950620A5320 ANGLE DOUG DC8 DC861F 3021953WP BS 280.0 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23813CK49741 45893 KYIP - DURING 'C-3' CHECK INSPECTION, FOUND CORROSION AT STA 280.0 BETWEEN LONGERONS 32L AND 33L. REMOVED AND REPLACED CORRODED ANGLE IAW EA NR 95-168. (X) 2L74 4F 4A25 19951124002111995112400211WP 1995 11 24 CKSA95060 119950620A5315 FLOOR BEAM DOUG DC8 DC861F 3021953WP BS 798 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23813CK49741 45893 KYIP - DURING 'C-3' CHECK INSPECTION, FOUND FLOOR BEAM AT STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 WITH END CLIPS CRACKED. REMOVED AND REPLACED END CLIP STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 PER SKA95110-3. INSTALLED PANELS AS REQUIRED. REPAIRED END CLIP STA 798.00 IAW EA NR 95-167.C. (X) 2L74 4F 4A25 19951124002121995112400212WP 1995 11 24 CKSA95062 119950628A5320 FITTING DOUG DC8 DC863F 302198FWP BS 1660 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23867BX74760 46049 KYIP - DURING B-CHECK INSPECTION, FOUND LONGERON 30L AT FS 1660, CORRODED. REPAIRED PER DC-8 SRM 53-2-2. REPLACED LONGERON END FITTING, STA 1660 LONGERON 30L. (X) 2L74 4F 4A25 19951124002131995112400213WP 1995 11 24 CKSA95063 119950711A5320 ANGLE DOUG DC8 DC8F54 3021926WP BS 857 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23806CK60926 45932 KOSC - DURING C-CHECK INSPECTION, FOUND INBOARD LOWER AFT ANGLE IN WHEELWELL DOGHOUSE AREA SURFACE CORRODED. REMOVED ANGLE, REMOVED CORROSION IN CENTER WING UPPER SKIN PANEL. CORROSION REMOVAL OUT OF SRM LIMITS. REPAIRED SKIN PER ENGINEERING SKETCH SKA95118-2. SPLICED IN NEW SECTION OF REAR SPAR TO FUSELAGE ANGLE IAW DC-8 SRM 53-2-5, FIGURE 12. C/W AIA EA95-177. (X) 2L74 4F 4A25 19951124002141995112400214WP 1995 11 24 CKSA95129 119951017A261205020 FIRE LOOP DOUG DC8 DC863 302198AWP NR 4 ENGINE SHORTED A CKSAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 GL23868BX56154 46034 KLAX - NR 4 ENGINE FIRE WARNING INDICATION CAME ON APPROXIMATELY ONE MINUTE FOLLOWING ENGINE SHUT-DOWN DURING TAXI. ENGINE FIRE HANDLE PULLED. ENGINE VISUALLY SCANNED OKAY. REPLACED LOWER FIRE LOOP IAW MM CHAPTER 26. GROUND OPS CHECKS GOOD. (X) 2L74 4F 4A25 19951124002151995112400215WP 1995 11 24 CKSA95131 119951101A322257671525001 STRUT DOUG DC8 DC861F 3021953WP NLG BROKEN A CKSAK NONE O OTHER ININSP/MAINT 1 GL23813CK4906111264 149 45893 MIA - FLT 61556 - REFERENCE MRR NR 95-002, DATED 1-15-95. IN THE PROCESS OF TOWING AIRCRAFT, THE NOSE GEAR LOWER STRUT BROKE OFF APPROXIMATELY 12 INCHES FROM THE BOTTOM OF THE STRUT. UPON DISASSEMBLY AND INVESTIGATION, FOUND CRACK INITIATION WAS ATTRIBUTED TO AN ABUSIVE GRINDING OPERATION OF THE CHROMIUM PLATING WHICH GENERATED EXTENSIVE CIRCUMFERENTIAL INTERGRANULAR CRACKS OF SHALLOW DEPTH AND VARIABLE LENGTH ON THE BASE METAL. (X) 2L74 4F 4A25 19951124002161995112400216WP 1995 11 24 CKSA95132 119951019A3260DS073S CONNECTOR DOUG DC8 DC863 302198AWP LT MLG DOOR BAD A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23869BX54908 46035 KIND/KTOL - FLT 68093 - ON TAKEOFF FROM IND, UPLATCH CHECK FAILED. (DOORS NOT LATCHED AND LEFT DOOR UNSAFE LIGHT ON.) FOUND BAD PIN AT DOOR SWITCH. SECURED NEW PIN. DOOR LIGHTS OPS CHECK GOOD IAW DACO MM 32-12-1. (X) 2L74 4F 4A25 19951124002171995112400217WP 1995 11 24 CKSA95133 119951101A29107614033704 HYD LINE DOUG DC8 DC863F 302198FWP NR 2 PYLON CHAFED A CKSAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL23811CK38367 46147 KMIA - FLT 68424 - AILERON AND RUDDER CONTROL MANUAL LIGHTS ILLUMINATED IN-FLIGHT, LOSS OF QUANTITY. HYDRAULICS DOWN TO AUXILIARY POSITION. FOUND HYDRAULIC PRESSURE LINE IN AFT SECTION OF NR 2 PYLON CHAFED THROUGH. REPLACED WITH FLEX LINE IAW EA 94-192. NO LEAKS NOTED. PLACED FLEX LINE ON CARRY OVER NR 072. (X) 2L74 4F 4A25 19951124002181995112400218NM 1995 11 24 PCAA9500242 119951013A2910 O-RINGS DHAV DHC8 DHC8102 2809003NM NR 2 HYD SYS LEAKING A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA13825EX 388 LOST NR 2 HYDRAULIC QUANTITY AND PRESSURE, AFTER 20 MINUTES HYDRAULIC PUMP CAUTION LIGHT ILLUMINATED. INSPECTED, FOUND O-RING ON UNION OF GROUND HYDRAULIC LINE LEAKING. REPLACED O-RING, REMOVED AND REPLACED HYDRAULIC PUMP. OPERATIONAL CHECKED SYSTEM IAW MM. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19951124002191995112400219NM 1995 11 24 PCAA9500243 119951025A2611473054 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM COCKPIT FALSE WARNING A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA13827EX2466 390 INTERMITTENT SMOKE WARNING OCCURRED 5 TIMES IN 5 MINUTES. CLEANED CANNON PLUGS ON BOTH SMOKE DETECTORS, PRESSURIZED A/C, AND TURNED ON HEAT. COULD NOT DUPLICATE PROBLEM ON GROUND. ELECTRICALLY DISABLED FORWARD SMOKE DETECTOR AS PRECAUTIONARY. SYSTEM MEL'D. SMOKE DETECTOR REMOVED AND REPLACED LATER IN LGA. A/C RETURNED TO SERVICE. ACTC: 2,877. (X) 2H72 4T RTA13NM 19951124002201995112400220WP 1995 11 24 9518339911 119951118A216160714621 TEMP CONTROL DOUG DC9 DC931 3022065WP LT PACK MALFUNCTIONED A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01961N 1567215669 47405 YXE - DURING CLIMB, SMOKE ACCUMULATED IN THE CABIN, CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. AIRCRAFT RETURNED TO YXE AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AIR CONDITIONING PACK CONTROLLER AND COALESCER BAG, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951124002211995112400221WP 1995 11 24 9518341145 119951117A3350 EEL POWER SUPPLY DOUG DC10 DC1040 3023508WP CABIN FAILED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01145US 46754 DURING LINE CHECK, MID CABIN EMERGENCY FLOOR LIGHTS FAILED TEST. REPLACED THE POWER SUPPLY AND BATTERY. 2L73 4F A22WE 19951124002221995112400222NE 1995 11 24 9518356608 219951117A73217480005 FUEL CONTROL BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01608US9419 19785 62402 DURING TAKEOFF, THE NR 1 ENGINE SLOW TO RESPOND AS THROTTLE WAS ADVANCED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE FUEL PUMP, FUEL CONTROL, PERFORMED ENGINE RUNUP AND TEST WAS NORMAL. 2L74 4F4 F A20WE E20EA 19951124002231995112400223NM 1995 11 24 9518366601 119951117A24101574609 CSD OIL COOLER BOEING747 747151 1384891NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE LEAKING A NWAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01601US412357727 19778 85642 AT FL 350, THE NR 2 ENGINE FIRE WARNING LIGHT ACTIVATED. BOTH A AND B NACELLE TEMPERATURES AT 9 DEGREES AND RISING, NR 2 GENERATOR FIELD AND PRESSURE LIGHTS INCLUDING GROUND BRAKER LIGHT CAME ON. CREW ACCOMPLISHED ENGINE SHUTDOWN, FIRED BOTTLE, AND RETURNED TO HNL. FOUND NR 2 CSD OIL COOLER LEAKING. REPLACED THE OIL COOLER AND VISUALLY CHECKED FOR LEAKS, NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE. 2L74 4F4 F A20WE E20EA 19951124002241995112400224NM 1995 11 24 9518376636 119951119A33506106765 BATTERY PACK BOEING747 747251B 1384892NM CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01636US 23548 DURING LINE CHECK, FOUND THE EMERGENCY LIGHTS AT DOOR 1L AND 1R INOPERATIVE. REPLACED THE BATTERY PACK AND PERFORMED FUNCTIONAL CHECK, TEST WAS NORMAL. 2L74 4F A20WE 19951124002251995112400225WP 1995 11 24 9518389759 119951118A2120 AIR DUCTS DOUG DC9 DC941 302207NWP CABIN DIRTY A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01759NW 47287 CABIN FILLED WITH SMOKE ACCOMPANIED BY STRONG OIL SMELL AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND OIL RESIDUE IN PACK DUCTING FROM PREVIOUS APU PROBLEM. CLEANED DUCTING, REPLACED WATER SEPARATOR BAGS AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951124002261995112400226WP 1995 11 24 9518399138 119951116A3320 LIGHT WIRES DOUG DC9 DC915 3022036WP CABIN DAMAGED A NWAAF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL019348 45787 ELECTRICAL SMELL WAS NOTICED COMING FROM FORWARD AREA OF CABIN OR GALLEY AFTER PARKING AT GATE. FOUND FORWARD FLIGHT ATTENDANT SIDEWALL LIGHT SWITCH SMOKING AND FLIGHT CREW UTILIZED PORTABLE FIRE EXTINGUISHER. MAINTENANCE REPAIRED TWO DAMAGED WIRES, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951124002271995112400227WP 1995 11 24 9518409152 119951019A2750 CONNECTOR DOUG DC9 DC914 3022034WP LT FLAP TRANS CORRODED A NWAAL ABORTED APPROACH O OTHER APAPPROACH 1 GL018911E 45825 DURING APPROACH AT 5,000 FEET, 160 KNOTS, AND FLAPS AT 20 DEGREES, STALL WARNING STICK SHAKER ACTIVATED. EXECUTED GO-AROUND PROCEDURES AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. FOUND CORROSION AT THE LEFT FLAP TRANSMITTER CANNON PLUG. CLEANED PLUG AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951124002281995112400228WP 1995 11 24 9518419878 119951118A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT VENTRAL STAIR DOOR INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK B5-27, NO HELP. FOUND WIRE L800A18N LOOSE AT GROUND STUD 415, SECURED WIRE AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951124002291995112400229WP 1995 11 24 9518429878 119951118A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT STA 828 INOPERATIVE. FOUND WIRE L1233K18N DISCONNECTED AT GROUND STUD, RECONNECTED WIRE AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951124002301995112400230NM 1995 11 24 9518432767 119951120A3350 EEL WIRING BOEING727 7272M7 138407SNM CABIN DAMAGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01727RW 21656 DURING PREFLIGHT, FOUND AFT TWO LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING ON CENTER LIGHT AND RECONNECTED AFT LIGHT ASSEMBLY, CHECKED OK. 2L73 4F A3WE 19951124002311995112400231NM 1995 11 24 9518442287 119951120A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01287US 21375 DURING PREFLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK, CHECKED OK. 2L73 4F A3WE 19951124002321995112400232WP 1995 11 24 95UAL900264 119951120A217021D10011 COALESCER BAGS DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL A/C COMPT DIRTY A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP291811U 46610 PUNGENT ODOR/SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER AFTER TAKEOFF. ACCOMPLISHED AIR CONDITIONING PACK BURN OUT AND REPLACED COALESCER BAGS. 2L73 4F4 F A22WE E23EA 19951124002331995112400233NM 1995 11 24 95UAL900265 119951120A271069710028 LEVER ASSY BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE AILERONS WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29311UA 23672 AILERON AUTOPILOT ACTUATOR LEVER ASSEMBLY WAS FOUND WITH SHEAR FASTENERS SHEARED. ONE FASTENER MAINTAINED CONNECTION BETWEEN THE POWER CONTROL UNIT AND THE LEVER ASSEMBLY. THE PLAY IN THE ASSEMBLY ELONGATED THE HOLES OF THE LEVER ATTACH HOLES AND CAUSED DRIFTING IN THE 'A' AUTOPILOT SYSTEM. AILERON LEVER ASSEMBLY WAS REPAIRED PER BOEING OVERHAUL MANUAL 27-09-05 AND RETURNED TO SERVICE. 2L72 4F4 FRTA16WE E2GL 19951124002341995112400234NM 1995 11 24 95UAL900266 119951120A3350M732 BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29514UA 24839 FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS INOP. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951124002351995112400235NM 1995 11 24 95UAL900267 119951120A261320035008300 OVERHEAT CONTROL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE RT WING INOPERATIVE A UALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP29360UA 24453 CREW REPORTS RIGHT WING BODY OVERHEAT LIGHT FLICKERED DURING FLIGHT. TURNED OFF BLEED AND CLOSED ISOLATION VALVE, NO HELP. DIVERTED TO IAD. REPLACED THE OVERHEAT CONTROL UNIT. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951124002361995112400236NM 1995 11 24 P5CA9500843 119951120A3246 TIRE BOEING747 747122 1384872NM MLG FAILED A P5CAK NONE O OTHER LDLANDING 1 WP23854FT 19754 DURING LANDING ROLLOUT, TIRES 10 AND 12 FAILED, DUE TO SUSPECTED LOCKED WHEEL CONDITION. CAUSED MATERIAL LOSS WHICH PENETRATED THE INBOARD RIGHT MIDFLAP, CAUSING A HOLE APPROXIMATELY 2.5 INCHES BY 2.5 INCHES. REPLACED FAILED AND ADJACENT TIRES AND WHEEL ASSEMBLIES. LOCKED OUT NUMBERS 10 AND 12 BRAKES PER MEL 32-05. REPAIR MIDFLAP PER SRM 51-40-09. 2L74 4F A20WE 19951124002371995112400237NE 1995 11 24 SCNA95273 219951116A7200 ENGINE BOEING727 7272J4 1384006NM PWA JT8 JT8D17A 52049NE NR 2 FAILED A SCNACD ABORTED TAKEOFF RETURN TO BLOCK YT ENGINE STOPPAGE ENGINE CASE PENETRATION TOTAKEOFF 1 GL15288SC 20765 DURING TAKEOFF ROLL, THE NUMBER TWO ENGINE EXPERIENCED A CONTAINED FAILURE AND ENGINE PARTS WERE REPORTED DEPARTING THE AIRCRAFT. THE ENGINE WAS REPLACED. THE FAILED ENGINE IS CURRENTLY UNDER EVALUATION AND SUN COUNTRY IS AWAITING THE RESULTS. 2L73 4F4 FRTA3WE E2EA 19951124002381995112400238WP 1995 11 24 SCNA95274 119951114A335014111101 BATTERIES DOUG DC10 DC1010 3022110WP L3 DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15573SC 46905 THE L-3 DOOR SLIDE WOULD NOT TEST. REMOVED AND REPLACED BATTERIES FOR L-3 DOOR SLIDE LIGHT AND SLIDE TESTED GOOD. 2L73 4F A22WE 19951124002391995112400239NM 1995 11 24 UPS205102 119951117A3230 RETRACT MECH BOEING727 72727C 138400JNM NLG LACK OF LUBE A IPXAO OTHER J WARNING INDICATION APAPPROACH 1 SO01909UP 19115 SDF - ON APPROACH, NOSE GEAR DID NOT ILLUMINATE DOWN AND LOCKED. RECYCLED GEAR AND NOSE GEAR DID INDICATE DOWN AND LOCKED ON SECOND ATTEMPT. HANDLE HARDER TO MOVE THAN NORMAL. CHECKED OVER CENTER LINK AND LIBED LINKAGES, OPERATED GEAR SEVERAL TIMES AND CHECK TIME PER MM 32-32-00, WITHIN TIME LIMIT. 2L73 4F A3WE 19951124002401995112400240NM 1995 11 24 UPS205103 119951120A33501000679 EEL ASSY BOEING727 72731C 1384011NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01926UP 19233 M/X DISCOVERED FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY, OPS CK GOOD. ON (P/N 10-0067-9) (S/N 9493), OFF (P/N 10-0067-9) (S/N 17745). 2L73 4F A3WE 19951124002411995112400241NM 1995 11 24 UPS205105 119951120A3350 BATTERY BOEING727 72725C 138400HNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINT FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BOTH EMERGENCY LIGHT BATTERIES, OPS CHECK OK. 2L73 4F A3WE 19951124002421995112400242NM 1995 11 24 UPS205106 119951120A3260 UPLOCK SW BOEING727 72731C 1384011NM NLG OUT OF POSITION A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01925UP 19230 CREW REPORTED AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT IN ACC WITH ADM PROCEDURES. THE GEAR WAS CYCLED AND IT STILL WOULD NOT RETRACT, BTB ACCOMPLISHED. RESEATED UPLOCK CHECK SWITCH ON CANNON PLUG PIN. 2L73 4F A3WE 19951124002731995112400273NM 1995 11 24 PCAA9500244 119951027A3260864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A PCAAO OTHER N FALSE WARNING CLCLIMB 1 EA132FOR 258 UPON RETRACTION, NOSE GEAR (RED) INDICATION LIGHT WOULD FLICKER OFF AND ON, THEN FINALLY EXTINGUISHED. GEAR EXTENDED NORMALLY. AIRCRAFT RETURNED TO FIELD. AIRCRAFT FERRIED TO BGM FOR REPAIR. REMOVED AND REPLACED NOSE GEAR DRAG STAY PROXIMITY SENSOR. RETRACTION TEST PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ACTT: 11,502:24 HRS. ACTC: 11,818. (X) 2H72 4T RTA13NM 19951124002901995112400290NE 1995 11 24 95ZZZX6328 219951103A723052H19101 STATOR SET BOEING767 767 1385102NM PWA 4060 PW4060 52119NE 11TH STAGE LIBERATED SEAL BL WA2DE ENGINE SHUTDOWN O OTHER NRNOT REPORTED 1 NE032FOR 7427 P724203CN CAUSE OF IN-FLIGHT SHUTDOWN FOUND TO BE LIBERATED BRAZED HONEYCOMB SEGMENT FROM THE 11TH STAGE STATOR INNER SHROUD. 2L72 4F4 F EXPA2L72E24NE 19951124003081995112400308WP 1995 11 24 95ZZZM642 119950930A3350014597101 EEL BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS 49364 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND BATTERIES AND LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9580208. 2L72 4F A6WE 19951124003091995112400309WP 1995 11 24 95ZZZM643 119951024A3350L201913 EEL DOUG DC9 DC982 3022082WP CATWALK DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND AFT OVERHEAD LIGHT ASSEMBLY AND OPERATED NORMALLY. REFERENCE NR ASAA9580246. 2L72 4F A6WE 19951124003101995112400310WP 1995 11 24 95ZZZM644 119951024A3350RPS1B EEL POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, THE FORWARD ONE-THIRD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, LIGHTS OPERATED NORMALLY. REFERENCE NR ASAA9580247. 2L72 4F A6WE 19951124003111995112400311NM 1995 11 24 ASAA9540068 119951018A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT FORWARD AND AFT TRACKS AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003121995112400312NM 1995 11 24 ASAA9540069 119951021A33503114981 EEL REFLECTOR BOEING737 737490 1384715NM L-2 DOOR WORN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - DURING MAINTENANCE CHECK, THE L-2 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED REFLECTOR/SOCKET ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003131995112400313NM 1995 11 24 ASAA9540070 119951024A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 JNU - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003141995112400314NM 1995 11 24 ASAA9540071 119951024A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003151995112400315NM 1995 11 24 ASAA9540073 119951027A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - FLT NR 191 - CREW REPORTED AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE. REPAIRED WIRING CONNECTION ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003161995112400316NM 1995 11 24 ASAA9540074 119951030A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON THE AFT TRACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003171995112400317NM 1995 11 24 ASAA9540075 119951101A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01762AS 25099 JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003181995112400318NM 1995 11 24 ASAA9540076 119951102A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROWS 14 TO 15 WERE FOUND INOPERATIVE. RECONNECTED WIRING TO LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003191995112400319NM 1995 11 24 ASAA9540077 119951102A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01764AS 25101 SEA - DURING MAINTENANCE CHECK, THE THREE FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003201995112400320NM 1995 11 24 ASAA9540078 119951103A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS BETWEEN ROWS 14 AND 17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AT ROW 14 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19951124003211995112400321WP 1995 11 24 ASAA9580208 119950930A3350RPS1B EEL BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS 49364 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003221995112400322WP 1995 11 24 ASAA9580209 119950930A3350 EEL CONNECTOR DOUG DC9 DC982 3022082WP TAIL COMPARTMENTDEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01956AS 48079 SEA - DURING MAINTENANCE CHECK, THE MIDDLE OVERHEAD EMERGENCY LIGHT ABOVE THE CATWALK WAS FOUND INOPERATIVE. REPAIRED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003231995112400323WP 1995 11 24 ASAA9580210 119951003A33500105606003 EEL WIRE DOUG DC9 DC983 3022083WP CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01968AS 53016 SEA - DURING MAINTENANCE CHECK, THE FORWARD FOUR EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED WIRE HARNESS BETWEEN 4TH AND 5TH TRACK LIGHTS AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951124003241995112400324WP 1995 11 24 ASAA9580231 119951015A3350014597101 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01933AS 49234 SEA - DURING MAINTENACNE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 22 AND BETWEEN AFT LAVS WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003251995112400325WP 1995 11 24 ASAA9580232 119951016A33501001191 EEL PORTABLE DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS3948 49364 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003261995112400326WP 1995 11 24 ASAA9580233 119951016A335020131A BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN AFT CABIN AND TAILCONE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003271995112400327WP 1995 11 24 ASAA9580234 119951018A3350014597101 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003281995112400328WP 1995 11 24 ASAA9580242 119951019A335041B004AD07G3 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 13 TO 18 WERE FOUND DIM. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003291995112400329WP 1995 11 24 ASAA9580246 119951024A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND AFT OVERHEAD LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003301995112400330WP 1995 11 24 ASAA9580247 119951024A335020131A BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01931AS 49232 SEA - DURING MAINTENANCE CHECK, THE FORWARD ONE-THIRD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19951124003311995112400331WP 1995 11 24 ASAA9580259 119951102A3350S103 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01944AS 53019 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE BATTERY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19951124003321995112400332NM 1995 11 24 AWXA9500724 119951025A5241 SKIN BOEING737 7373S3 1384711NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 DURING SCHEDULED C11 INSPECTION, FOUND FORWARD GALLEY DOOR LOWER HINGE CUTOUT CRACKED. FABRICATED DOUBLER AND REPAIRED PER EO 52-00-02, FIGURE 6. (M) 2L72 4F RTA16WE 19951124003331995112400333NM 1995 11 24 AWXA9500725 119951025A5241 SKIN BOEING737 7373S3 1384711NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 DURING SCHEDULED C11 INSPECTION, FOUND FORWARD GALLEY DOOR UPPER HINGE CUTOUT CRACKED. FABRICATED REPAIR PER EO 52-00-02, FIGURE 6. (M) 2L72 4F RTA16WE 19951124003341995112400334NM 1995 11 24 AWXA9500726 119951103A3260106122619 SENSOR BOEING737 737301 1384611NM NOSE GEAR BAD A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28325AW 23260 LAS/DEN - FLT NR 749 - WHEN GEAR HANDLE WAS RAISED ON TAKEOFF, THE RED LIGHT ILLUMINATED AND REMAINED ON. GEAR WAS RECYCLED WITH NO HELP. AIRCRAFT RETURNED TO LAS LANDING UNEVENTFULLY. MAINTENANCE FOUND S846 NOSE LOCK SENSOR BAD. REMOVED ADN REPLACED SENSOR PER BMM 32-60-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951124003351995112400335NM 1995 11 24 AWXA9500727 119951021A5315 FLOOR BEAM BOEING737 7373G7 1384595NM BS 344 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 PHX - DURING SCHEDULED C10 INSPECTION, FOUND FLOOR BEAM T-CAP CORRODED AT STATION 344 BETWEEN BL 0 AND LBL 44. REPAIRED FLOOR BEAM PER SRM 53-10-51, FIG 205. (M) 2L72 4F RTA16WE 19951124003361995112400336NM 1995 11 24 AWXA9500728 119951021A5330 SKIN BOEING737 7373G7 1384595NM KEEL BEAM CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28157AW 23779 PHX - DURING SCHEDULED C10 INSPECTION, FOUND A 1.5 INCH CRACK IN KEEL BEAM SKIN PANEL BETWEEN WHEEL WELL AFT END. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-60-12, FIGURE 202. (M) 2L72 4F RTA16WE 19951124003371995112400337NM 1995 11 24 AWXA9500730 119951101A3030 PITOT TUBE BOEING737 737297 1384480NM VERT STAB HEAT INOP A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28147AW 22630 PHX/DEN - FLT NR 499 - AIR TURNBACK DUE TO LEFT ELEVATOR PITOT HEAT LIGHT ILLUMINATED DURING CRUISE. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ELEVATOR PITOT TUBE. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19951124003381995112400338NM 1995 11 24 AWXA9500740 119951105A291069547678 LINE BOEING737 737277 1384570NM 'A' HYD SYSTEM RUPTURED A AWXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28181AW 22648 LAS/PDX - FLT NR 671 - TWENTY MILES FROM PDX, CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC FLUID. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AFTER DECLARING AN EMERGENCY LANDING. MAINTENANCE FOUND RUPTURED LINE AT THE 'A' SYSTEM HYDRAULIC MODULE. REPLACED LINE, INSPECTED PRESSURE AND CASE DRAIN FILTERS, NO CONTAMINATION NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951124003391995112400339NM 1995 11 24 AWXA9500741 119951106A5240 DOOR BOEING737 7372A6 138448BNM GROUND ELECT NOT SECURED A AWXAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP28145AW 20194 LAS/PHX - FLT NR 312 - CREW REPORTED AIRFRAME VIBRATION AT TAKEOFF AND ELECTED TO RETURN TO LAS. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND GROUND ELECTRICAL SERVICE DOOR OPEN. NO DAMAGE TO AIRFRAME NOTED. MAINTENANCE SECURED DOOR. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F A16WE 19951124003401995112400340WP 1995 11 24 USAA951081 119950918A5320 JAMB DOUG DC9 DC981 3022081WP CARGO DOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND PREVIOUS TEMPORARY REPAIRS TO BOTTOM SECTION OF DOOR JAMB IN FORWARD CARGO, 2 EACH. REPLACED BOTTOM SECTION OF DOOR JAMB PER SRM 53-05 FIG 44. (M) 2L72 4F A6WE 19951124003411995112400341WP 1995 11 24 USAA951082 119950918A5311 FRAME DOUG DC9 DC981 3022081WP BS 1463 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND 5 CRACKS .5 INCH TO 1 INCH LONG IN CANTED FRAME STATION 1463, BELOW LONGERON NR 5L AND 5R. CUT OUT SECTION OF DAMAGED AREA AND INSTALLED NEW SECTION PER USAIR EA NR 28127A. (M) 2L72 4F A6WE 19951124003421995112400342WP 1995 11 24 USAA951083 119950918A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1401 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN END OF LONGERON 2L STATION 1401. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 5 AND USAIR EA NR 28221. (M) 2L72 4F A6WE 19951124003431995112400343WP 1995 11 24 USAA951084 119950918A5347 TRACK DOUG DC9 DC981 3022081WP BS 1287-1309 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STATION 1287 LEFT INBOARD SEAT TRACK CORROSION. REF C58-53302. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M) 2L72 4F A6WE 19951124003441995112400344WP 1995 11 24 USAA951085 119950918A5347 TRACK DOUG DC9 DC981 3022081WP BS 1287-1300 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1287 TO 1300 RIGHT INBOARD SEAT TRACK. CORROSION REF C58-53302. SPLICED IN NEW SECTION OF SEAT TRACK FROM STATION 1260 TO 1309 PER SRM 53-05 FIG 4F. (M) 2L72 4F A6WE 19951124003451995112400345WP 1995 11 24 USAA951086 119950918A573059374683 SKIN DOUG DC9 DC981 3022081WP WS 65 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK LEFT WING LEADING EDGE STATION XFS 45. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 57-06B FIG 8 AND USAIR EA NR 31310. (M) 2L72 4F A6WE 19951124003461995112400346WP 1995 11 24 USAA951087 119950918A5347 TIE DN RAIL DOUG DC9 DC981 3022081WP BS 636-731 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 636 TO 731 LONGERON 28L TIE DOWN RAIL. MANUFACTURED NEW RAIL SECTION AND SPLICED PER SRM 53-05 4E AND DAC DWG SR09530082. (M) 2L72 4F A6WE 19951124003471995112400347WP 1995 11 24 USAA951099 119950919A5320 T-CAP DOUG DC9 DC981 3022081WP BS 1338 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19801US39711 48037 PIT - DURING C-4 CHECK INSPECTION, FOUND 3 INCH, 2 INCH AND A 1.1875 INCH CRACK IN STATION 1338 T-CAP AT LONGERON 14L, 12L AND BETWEEN 14L AND 15L. REMOVED AND REPLACED UPPER LEFT TEE CAP SEGMENT PER USAIR EO 5389X252 PART 2. (M) 2L72 4F A6WE 19951124003481995112400348NM 1995 11 24 AALA950054H 119951012A5720112T7004 FITTING BOEING767 767223 1385123NM WING DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07312AA 22315 AFW - EDGE DAMAGE BEYOND SRM 57-20-90-1 FIG 101 DETAIL V LIMITS. BLENDED DAMAGED AREA, NDT INSPECT, FLAP PEEN AND RESTORE FINISH PER ENGINEERING MRB 767-1034. (M) 2L72 4F RTA1NM 19951124003491995112400349NM 1995 11 24 AALA950056H 119951012A5315111T5007 FLOOR BEAM BOEING767 767323 1385205NM BS 834 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0739356 24037 AFW - TOP SIDE OF FLOOR BEAM CORRODED BEYOND SRM LIMITS. SPLICED IN NEW SECTION OF FLOOR BEAM PER MRB 767-1017. (M) 2L72 4F RTA1NM 19951124003501995112400350NM 1995 11 24 AALA951758 119951006A3260106122629 DNLOCK SENSOR BOEING727 727223 1384074NM LT MLG DEFECTIVE A AALAO OTHER N FALSE WARNING APAPPROACH 1 SW07874AA 21386 DFW - FLT NR 1612 - DURING APPROACH DFW AFTER GEAR WAS CYCLED DOWN, THE LEFT MAIN GEAR DID NOT SHOW GREEN DOWN AND LOCKED. CYCLING GEAR HANDLE, STILL DID NOT SHOW DOWN AND LOCKED. ACCOMPLISH CRANK DOWN PROCEDURE AND STILL DID NOT RECEIVE GREEN LIGHT INDICATION DOWN AND LOCKED. GEAR ALIGNMENT INDICATOR DID SHOW DOWN AND LOCKED. THE RED GEAR LIGHT STAYED ILLUMINATED ALL THE TIME. LEFT DOOR LIGHT REMAINED ILLUMINATED. HYDRAULIC PRESSURE READING NORMAL THROUGH OUT ALL CYCLES. LANDED DFW WITHOUT INCIDENT. REPLACED LEFT HAND MLG DOWN LOCK SENSOR AND ADJUSTED TARGET. SWUNG GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951124003511995112400351WP 1995 11 24 AALA951779 119951011A3350 EEL CRT BREAKER DOUG DC9 DC983 3022083WP COCKPIT TRIPPED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07562AA 49344 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. RESET EMERGENCY EXIT FLOOR PATH LIGHT CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA6WE 19951124003521995112400352WP 1995 11 24 AALA951783 119951012A3350A3060719102 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07481AA 49656 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AFT OF ROW 22 INOPERATIVE. REPLACED AFT EMERGENCY EXIT FLOOR PATH LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951124003531995112400353WP 1995 11 24 AALA951806 119951016A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07498AA 49736 DFW - DURING OVERNIGHT CHECK, FORWARD RIGHT DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY EXIT SIGN WIRE AT FORWARD RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951124003541995112400354NM 1995 11 24 AALA951828 119951019A3350A3060698101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07701AA 22459 RDU - FLT NR 0627 - DURING MAINTENANCE CHECK, EMERGENCY FLOOR LIGHTS IN AFT CABIN INOPERATIVE. AIRCRAFT MAINTENANCE FERRY RDU/MIA. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951124003551995112400355NM 1995 11 24 AALA951838 119951021A361032146451 VALVE GARRTT BOEING727 727227 1384078NM NR 3 STRUT DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07725AA P4420 20732 MIA - FLT NR 0695, AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND AIRCRAFT RETURNED TO MIA, LANDING WITHOUT INCIDENT. REPLACED LEFT PNEUMATIC SHUTOFF VALVE. ALSO, REPLACED NR 3 STRUT OVERHEAT CONTROL AND REPOSITIONED OVERHEAT DETECTOR LOOP. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19951124003561995112400356NM 1995 11 24 AALA951847 119951010A5315141N5113 FLOOR BEAM BOEING757 757223 1384957NM BS 377 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07634AA 24592 AFW - FLOOR BEAM AT STATION 377 HAS CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-625. (M) 2L72 4F RTA2NM 19951124003571995112400357NM 1995 11 24 AALA951848 119951010A5315141N2932 FLOOR BEAM BOEING757 757223 1384957NM BS 324 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07634AA 24592 AFW - FLOOR BEAM AT STATION 324, HAS CORROSION REMOVED ON UPPER SURFACE, MATERIAL REMAINING IS BEYOND SRM LIMITS. PER MRB 757-623. (M) 2L72 4F RTA2NM 19951124003581995112400358NM 1995 11 24 AALA951849 119951010A5320141N8322 ANGLE BOEING757 757223 1384957NM CABIN CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07634AA 24592 AFW - CORROSION REMOVED FROM ANGLE AT L-1 DOOR FLOOR BEYOND LIMITS. PER MRB 757-622. (M) 2L72 4F RTA2NM 19951124003591995112400359NM 1995 11 24 AALA951850 119951010A5315146N5090 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07634AA 24592 AFW - FLOOR BEAM AT STATION 1640 HAS 3 AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-620. (M) 2L72 4F RTA2NM 19951124003601995112400360NM 1995 11 24 AALA951851 119951010A5321146N5300 DECK PLATE BOEING757 757223 1384957NM BS 1681 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07634AA 24592 AFW - SEVERAL AREAS OF DECK PLATE HAS CORROSION BEYOND SRM LIMITS. PER MRB 757-619. (M) 2L72 4F RTA2NM 19951124003611995112400361NM 1995 11 24 AALA951853 119951022A5315146N5090 FLOOR BEAM BOEING757 757223 1384957NM BS 1661 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07635AA 24593 AFW - FLOOR BEAM AT STATION 1661 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-635. (M) 2L72 4F RTA2NM 19951124003621995112400362NM 1995 11 24 AALA951855 119951022A5321 DECK PLATE BOEING757 757223 1384957NM BS 1681/1720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07635AA 24593 AFW - DECK PLATE, AT STATION 1681 AND 1720, HAS CORROSION REMOVED AT VARIOUS BL LOCATIONS BEYOND SRM LIMITS. PER MRB 757-637. (M) 2L72 4F RTA2NM 19951124003631995112400363NM 1995 11 24 AWXA9500721 119951025A5241 SKIN BOEING737 7373S3 1384711NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 PHX - DURING SCHEDULED C11 INSPECTION, FOUND CRACK IN FORWARD GALLEY DOOR LOWER HINGE CUT OUT. FABRICATED DOUBLER REPAIR PER EO 52-00-02, FIGURE 6 PART 2. (M) 2L72 4F RTA16WE 19951124003641995112400364NM 1995 11 24 AWXA9500722 119951025A5241 SKIN BOEING737 7373S3 1384711NM R1 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28316AW 23713 PHX - DURING SCHEDULED C11 INSPECTION, FOUND CRACK IN FORWARD GALLEY DOOR UPPER HINGE CUT OUT. FABRICATED REPAIR PER EO 52-00-02, FIGURE 6. (M) 2L72 4F RTA16WE 19951124003651995112400365NM 1995 11 24 AWXA9500723 119951023A335020131A BATTERY PACK BOEING737 7373S3 1384711NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28314AW 23733 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR AND CENTER GALLEY EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19951124003661995112400366NM 1995 11 24 USAA951044 119951001A213121173886 CONTROLLER BOEING767 7672B7 1385107NM CABIN FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19656US9829 26847 FRA - FL 817, IMMEDIATELY AFTER TAKEOFF FROM FRA, THE AUTO INOP LIGHT ILLUMINATED AND THE EICAS MESSAGES 'CABIN ALT AUTO 1/2' AND 'CABIN AUTO INOP' ILLUMINATED. FLIGHT RETURNED TO FRA AND LANDED WITH NO FURTHER INCIDENT. THE NR 1 PRESSURE CONTROL UNIT FAULTED ON BITE AND WAS REPLACED. ALSO, AS A PRECAUTION, THE OUTFLOW VALVE ASSEMBLY WAS REPLACED. (M) 2L72 4F RTA1NM 19951124003671995112400367WP 1995 11 24 USAA951071 119950922A5320 ANGLE DOUG DC9 DC931 3022065WP BS 1059 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK RIGHT FORWARD DORSAL FIN DRAG ANGLE AT APPROXIMATELY STATION 1059. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19951124003681995112400368WP 1995 11 24 USAA951072 119950913A5720 WEB DOUG DC9 DC931 3022065WP WS 58.5 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND .875 INCH CRACK IN WEB WING STATION XCW 58.5 RIGHT SIDE. ROUTED OUT AREA AND REPAIRED PER USAIR EO 5790D573. (M) 2L72 4F A6WE 19951124003691995112400369WP 1995 11 24 USAA951073 119950919A5720 DOUBLER DOUG DC9 DC931 3022065WP WS 58.5 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND 2 INCH CRACK IN LEFT WEB AND 2 INCH CRACK IN DOUBLER WING STATION XCW 58.5 LEFT. REMOVED AND REPLACED DOUBLER AND WEB PLATES PER USAIR EO NR 5790D573. (M) 2L72 4F A6WE 19951124003701995112400370WP 1995 11 24 USAA951074 119950913A5720 DOUBLER DOUG DC9 DC931 3022065WP WS 58.5 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND .625 INCH CRACK RIGHT SIDE WING DOUBLER STATION XCN 58.5. ROUTED OUT CRACKED AREA AND REPAIRED PER USAIR EO NR 5790D573. (M) 2L72 4F A6WE 19951124003711995112400371WP 1995 11 24 USAA951075 119950922A5313 LONGERON DOUG DC9 DC931 3022065WP BS 680 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 680, LONGERON 6L. REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN A NEW SECTION PER SRM 53-02. (M) 2L72 4F A6WE 19951124003721995112400372WP 1995 11 24 USAA951076 119950922A5311 BELTFRAME DOUG DC9 DC931 3022065WP BS 1076 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19931VJ71931 47188 PIT - DURING C-1 CHECK INSPECTION, FOUND TWO .5 INCH BY .5 INCH CRACKS, FRAME STATION 1076 AT BOTH LONGERON NR 12 ATTACH FITTINGS. REMOVED DAMAGED SECTION OF BELTFRAME AND INSTALLED FILLER AND DOUBLERS PER SRM 53-03 FIG 34 SHEET 4. (M) 2L72 4F A6WE 19951124003731995112400373WP 1995 11 24 USAA951077 119950918A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1330 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 28L, AT STATION 1330, CORROSION REF C57-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (M) 2L72 4F A6WE 19951124003741995112400374WP 1995 11 24 USAA951078 119950918A5311 BELTFRAME DOUG DC9 DC981 3022081WP BS 1416 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND SEVEN CRACKS RANGING FROM .25 INCH TO .5 INCH, AT BELTFRAME 1416 AT FASTENERS TO LONGERON 3L, 4L, 5L, 6L, 4R, AND 5R. REPAIRED BELTFRAME PER SRM 53-04. (M) 2L72 4F A6WE 19951124003751995112400375WP 1995 11 24 USAA951079 119950918A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1418 HOLE A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH BY 1 INCH HOLE TAIL COMPARTMENT STATION 1418, LONGERON 8R. SPLICED IN NEW SECTION OF LONGERON. (M) 2L72 4F A6WE 19951124003761995112400376WP 1995 11 24 USAA951080 119950918A5320 FRAME DOUG DC9 DC981 3022081WP BS 845 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US38593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN FORWARD UPPER WINDOW FRAME STATION 845. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-30-06. (M) 2L72 4F A6WE 19951124003771995112400377WP 1995 11 24 USAA951088 119950918A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1307 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19813US37593 48093 PIT - DURING Q-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED STATION 1307 FLOOR BEAM, RIGHT SIDE. MANUFACTURED NEW FLOOR SUPPORT, L ANGLES AND SUPPORTS. SPLICED IN NEW SECTION PER USAIR TYPICAL REPAIR 53-10-14 AND USAIR EA NR 31216. (M) 2L72 4F A6WE 19951124003781995112400378NM 1995 11 24 USAA951090 119951007A7722TC17400 EGT HARNESS BOEING737 7373B7 1384580NM LT ENGINE DEFECTIVE A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA19533AU 24515 CLT - FL 2761, EN ROUTE TO MIA, LEFT ENGINE OVERHEAT LIGHT CAME ON AND EGT PEGGED AT 1250 DEGREES. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO CLT SET WAS 20 MINUTES. MAINTENANCE REPLACED NR 1 ENGINE EGT SOFT CORE HARNESS AND 6 O'CLOCK THERMOCOUPLE HARNESS. NR 1 EGT SYSTEM OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19951124003791995112400379WP 1995 11 24 USAA951091 119950920A5330 SKIN DOUG DC9 DC982 3022082WP BS 807 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 2 SKIN CORROSION .063 DEEP AROUND FILLET SCREW HOLE STATION 807, LONGERON 29R AREA. CORROSION TASK NR C22-57301. REMOVED CORROSION AND ACCOMPLISHED DOUBLER REPAIR PER SRM 53-14 FIG 53. (M) 2L72 4F A6WE 19951124003801995112400380WP 1995 11 24 USAA951092 119950918A5311 FRAME DOUG DC9 DC931 3022065WP BS 1104 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19985VJ70880 47208 PIT - DURING C-1 CHECK INSPECTION, FOUND CANTED FRAME 1104 AT UPPER ATTACH FASTENER CRACK .5 INCH LONGERON 4L. SPLICED IN NEW SECTION OF FRAME PER SRM 53-03 FIG 30. (M) 2L72 4F A6WE 19951124003811995112400381WP 1995 11 24 USAA951093 119951004A5320 APERTURE DOUG DC9 DC931 3022065WP VENT DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19985VJ70880 47208 PIT - DURING C-1 CHECK INSPECTION, FOUND 3 INCH CRACK AND A .75 INCH IN VENTRAL DOOR APERTURE TO LEFT CORNER. ROUTED OUT CRACKED AREAS AND INSTALLED FILLER AND DOUBLERS PER DRW NR J060088 AND USAIR EA NR 31358. (M) 2L72 4F A6WE 19951124003821995112400382WP 1995 11 24 USAA951094 119950926A5320591013037 ANGLE DOUG DC9 DC931 3022065WP PAX DOOR SILL CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19966VJ67843 47420 PIT - DURING RON CHECK, 1.25 INCH RUNNING FORE AND AFT AT AFT PASSENGER DOOR FLOOR SILL PLATE SUPPORT ANGLE. INSTALLED DOUBLER REPAIR PER USAIR EA NR 28484A AND SRM 53-05 FIG 40. (M) 2L72 4F A6WE 19951124003831995112400383WP 1995 11 24 USAA951097 119951005A5320 JAMB DOUG DC9 DC931 3022065WP LT EMERG EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19987VJ71421 47210 PIT - DURING C-3 INSPECTION, FOUND 2 INCH CRACK LEFT FORWARD EMERGENCY EXIT WINDOW JAMB PAN FORWARD OF LATCH PIN AND A .5 INCH CRACK AFT OF LATCH PIN. STOP DRILLED CRACKS AND INSTALLED DOUBLER REPAIR PER SRM 53-05 FIG 32. (M) 2L72 4F A6WE 19951124003841995112400384WP 1995 11 24 USAA951098 119951002A5312 BLKHD SKIN DOUG DC9 DC931 3022065WP AFT PRESS BLKHD CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19942VJ69633 47057 PIT - DURING B-CHECK INSPECTION, FOUND .25 INCH BY .5 INCH BY .022 DEEP CHAF MARK, AFT PRESSURE BULKHEAD AFT SIDE LEFT BULKHEAD SKIN. INSTALLED .063 DOUBLER AND .025 FINGER DOUBLER PER USAIR EA NR 31415. 2L72 4F A6WE 19951124003851995112400385EU 1995 11 24 USAA951100 119951016A78306258889 SWITCH FOKKERF28 F28MK0100 4990807EU NR 1 THRUST REV OUT OF ADJUST A USAAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 EA19853US 11281 PIT - FLT NR 591 - AFTER TAKEOFF AT APPROXIMATELY 2000, NR 1 THRUST REVERSER LIGHT FLICKERED ON AND OFF. AT 3000, THE PROCEDURE LIGHT CAME ON STEADY. CREW ELECTED TO RETURN TO FIELD. NO EMERGENCY DECLARED. MEL WAS ADDED AND FLIGHT DEPARTED TO SDF WITH DELAY. ADJUSTED THE LOWER AND UPPER DOOR SWITCH AND ACTUATOR SWITCH. (M) 2L72 4F RT 19951124003861995112400386EU 1995 11 24 USAA951101 119951019A33505515800104 EEL LEGEND PLATE FOKKERF28 F28MK4000 4990810EU CABIN FAILED A USAAK NONE L NO TEST NRNOT REPORTED 1 EA19481US 11230 PIT - FLIGHT 464 - PIREP READS, CHECK BULBS IN CABIN OVERHEAD EMERGENCY EXIT LIGHTS. REPLACED LIGHT PLATE ASSEMBLYS IN FORWARD CABIN AND MID CABIN EMERGENCY EXIT SIGNS. OPS CHECKED. (M) 2L72 4F RTA20EU 19951124003871995112400387WP 1995 11 24 USAA951102 119950918A53205912494501 JAMB DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND .025 INCH CRACK ROUTED OUT TO A . 375 INCH HOLE IN AFT DOOR JAMB, FORWARD CARGO BETWEEN 2ND AND 3RD STOP. INSTALLED DOUBLER REPAIR PER USAIR EA NR 27454 REV A. (M) 2L72 4F A6WE 19951124003881995112400388WP 1995 11 24 USAA951103 119951004A53111090345 FRAME DOUG DC9 DC982 3022082WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK STATION 1437, LONGERON 12L IN FRAME WEB. REPLACED CRACKED FRAME AND INSTALLED DOUBLER 7075 T-6 .050 PER SRM 53-01 FIG 2. (M) 2L72 4F A6WE 19951124003891995112400389WP 1995 11 24 USAA951104 119951002A5220 PAN DOUG DC9 DC982 3022082WP EMERG EXIT DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK LEFT FORWARD EMERGENCY EXIT DOOR (OVER WING EXIT). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03 FIG 1. (M) 2L72 4F A6WE 19951124003901995112400390WP 1995 11 24 USAA951105 119951004A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP BS 1510 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 1510 LONGERON 20 LEFT. INSTALLED DOUBLER REPAIR PER SRM 51-01. (M) 2L72 4F A6WE 19951124003911995112400391WP 1995 11 24 USAA951106 119950911A5330 SKIN DOUG DC9 DC982 3022082WP BS 1211 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND SKIN DAMAGE 2 INCH BY .5 INCH ON DOOR FRAME AREA STATION 1211, AFT CARGO DOOR. INSTALLED FILLER AND DOUBLER REPAIR (EXTERNAL) PER SRM 53-05 FIG 80. (M) 2L72 4F A6WE 19951124003921995112400392WP 1995 11 24 USAA951107 119951004A5320 DOUBLER DOUG DC9 DC982 3022082WP BS 484-503 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND 2 INCH CRACK LONGERON 30 SPLICE DOUBLER BETWEEN STATION 484 AND 503. REPLACED SPLICE DOUBLER PER SRM 53-02. (M) 2L72 4F A6WE 19951124003931995112400393WP 1995 11 24 USAA951108 119951004A5210 SKIN DOUG DC9 DC982 3022082WP PAX DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND PREVIOUS REPAIR CLASS 3, UPPER AFT AREA OF MED SKIN. REMOVED PREVIOUS REPAIR AND INSTALLED CLASS 1 REPAIR PER SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19951124003941995112400394WP 1995 11 24 USAA951109 119951004A5347 SEAT TRACK DOUG DC9 DC982 3022082WP BS 256 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 256 LEFT INBOARD SEAT TRACK. CORROSION TASK NR C58-53302. REPLACED SEAT TRACK SECTION PER SRM 53-05 FIG 4. (M) 2L72 4F A6WE 19951124003951995112400395WP 1995 11 24 USAA951110 119951004A5320 JAMB DOUG DC9 DC982 3022082WP CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AFT JAMB BETWEEN 2ND AND 3RD STOPS FOR BOTTOM (FORWARD CARGO). INSTALLED PERMANENT REPAIR PER 53-05 FIG 4 AND USAIR EA NR 27454. (M) 2L72 4F A6WE 19951124003961995112400396WP 1995 11 24 USAA951111 119951004A5220 PAN DOUG DC9 DC982 3022082WP EMER EXIT DR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK, LEFT AFT EMERGENCY EXIT DOOR TOP PAN LEFT STOP. SID REF 52-21-003. REMOVED AND REPLACED EXIT DOOR. (M) 2L72 4F A6WE 19951124003971995112400397WP 1995 11 24 USAA951112 119951004A5347 SEAT TRACK DOUG DC9 DC982 3022082WP BS 1297 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19815US37697 48095 PIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1297, LEFT INBOARD SEAT TRACK. REPLACED SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (M) 2L72 4F A6WE 19951124003981995112400398NM 1995 11 24 USAA951113 119951113A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION, FOUND BY EDDY CURRENT 1 INCH CRACK AT FLOOR BEAM AT STATION 520 EXTENDING .5 INCH OUTBOARD AND .5 INCH INBOARD OF LBL 45.5. REPAIR DOUBLER INSTALLED AS PER USAIR EA NR 40294. (M) 2L72 4F RTA16WE 19951124003991995112400399NM 1995 11 24 USAA951120 119951018A5320654587512 ANGLE BOEING737 7373B7 1384580NM FWD SERVICE DOORCORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2.1 INCH BY 24 INCH CORRODED AREAS, FORWARD SERVICE DOOR Z-ANGLE. CLEANED AND TREATED Z-ANGLE. REPLACED ASSOCIATED STRAP ANGLE. REPAIRED PER SRM 51-10-2, SRM 53-10-51, BOEING DRAWING 65-45875. LEVEL 1 CORROSION, CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19951124004001995112400400NM 1995 11 24 USAA951121 119951018A53201136992 INTERCOSTAL BOEING737 7373B7 1384580NM BS 328-344.17 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA IN 4 PLACES ON INTERCOSTAL BETWEEN BS 328 TO BS 344.17 AT LBL 10. REPLACED INTERCOSTAL WITH NEW PART. REPAIRED PER SRM 53-10-51. LEVEL 1 CORROSION, CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19951124004011995112400401NM 1995 11 24 USAA951133 119951011A5730 SKIN BOEING737 737201 1384454NM LT WING LE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19262AU 22868 CLT - DURING A UNSCHEDULED MAINTENANCE INSPECTION, VISUALLY FOUND A 6 INCH BY 4 INCH .5 INCH BY .150 INCH DENT WITH 9.5 INCH CRACK, LOCATED LEFT WBL 86 AT THE WING LEADING EDGE. INSTALLED INTERIM REPAIR PER EA 40063. (M) 2L72 4F A16WE 19951124004021995112400402NM 1995 11 24 USAA951134 119950918A5313 STRINGER BOEING737 737201 1384454NM BS 350/360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19240AU38335 22355 CLT - DURING A PCI INSPECTION, A 10 INCH BY 1 INCH CORROSION WAS FOUND AT STRINGER 28R, RBL 6 BETWEEN BS 350 AND 360. REPLACED END STRINGER 28R, RBL 6. (M) 2L72 4F A16WE 19951124004031995112400403NM 1995 11 24 USAA951144 119951018A532065C105922 INTERCOSTAL BOEING737 7373B7 1384580NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA, BS 947 TO 967, ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951124004041995112400404NM 1995 11 24 USAA951145 119951018A5313 STRINGER BOEING737 7373B7 1384580NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19508AU27759 23383 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 16 INCHES BY 1 INCH CORROSION BS 312 TO BS 328, ON STRINGER. REMOVED CORROSION, FABRICATED REPAIR AND SHIMS. REPAIRED SRM 53-00-03 FIG 201, PG 207. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951124004051995112400405NM 1995 11 24 USAA951150 119951018A5210 SKIN BOEING737 7373B7 1384580NM AFT ENTRY DOOR DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH BY .15625 DENT, AFT ENTRY DOOR AFT REAR UPPER CORNER. INSTALLED DOUBLER, REPAIRED PER SRM 52-00-01, FIG 206. (M) 2L72 4F RTA16WE 19951124004061995112400406NM 1995 11 24 USAA951151 119951018A5230 SKIN BOEING737 7373B7 1384580NM CENTER OF DOOR DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19509AU27987 23384 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH DENT CENTER OF CARGO DOOR, 3 INCHES FORWARD OF AFT EDGE. FABRICATED REPAIR DOUBLER FROM2024-T3, .063 AND INSTALLED 6 INCH BY 7 INCH DOUBLER. REPAIRED PER SRM 52-00-01 PAGE 203. (M) 2L72 4F RTA16WE 19951124004071995112400407WP 1995 11 24 USAA951152 119951102A5330 SKIN DOUG DC9 DC931 3022065WP BS 639 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19974VJ86102 47130 PIT - DURING C-1 CHECK CARD NR J9-50-0949, .1250 INCH CRACK FROM RIVET STATION 639 JUST BELOW LONGERON 1. INSTALLED CLASS 2 TEMPORARY REPAIR DOUBLER PER SRM 53-04 PAGE 55, FIG 12B. (M) 2L72 4F A6WE 19951124004081995112400408WP 1995 11 24 USAA951153 119950111A5330 SKIN DOUG DC9 DC931 3022065WP BS 200 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19916VJ68208 47023 PIT - DURING C-3 CHECK CARD 9-46-80-146, FOUND .3750 INCH CRACK BOTH SIDES OF 4TH DOOR STOP HOLE FROM BOTTOM, STATION 200 LEFT. INSTALLED DOUBLER PER EA NR 311550. (M) 2L72 4F A6WE 19951124004091995112400409EU 1995 11 24 USAA951154 119951101A5720 WEB FOKKERF28 F28MK4000 4990810EU WING DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU20822 11229 CLT - CLT INSPECTION VISUALLY FOUND WEB NR 3 CRUSHED 10 INCH ALONG ITS LENGTH BETWEEN RIB NR 2 AND NR 4 OF LOWER FLANGE ON TAIL BOX STRUCTURE. REPLACED WEB NR 3 AS PER SRM 57-22-03. (M) 2L72 4F RTA20EU 19951124004101995112400410EU 1995 11 24 USAA951155 119951101A5720 WEB FOKKERF28 F28MK4000 4990810EU WING DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU20822 11229 CLT - CLT INSPECTION VISUALLY FOUND WEB NR 4 CRUSHED 4 INCH BETWEEN RIB NR 2 AND NR 4 LOWER FLANGE ON TAILBOX STRUCTURE. FABRICATED NEW WEB. REPAIRED WEB NR IV AS PER SRM 57-22-03. (M) 2L72 4F RTA20EU 19951124004111995112400411EU 1995 11 24 USAA951156 119951101A5730 SKIN FOKKERF28 F28MK4000 4990810EU WINGS DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU20822 11229 CLT - CLT INSPECTION VISUALLY FOUND 4 INCH BY 6 INCH TEARS THROUGH SKIN AT WEBS 3 AND 4 BETWEEN RIBS 2 AND 4 OF LOWER SKIN TAIL BOX STRUCTURE. FABRICATED NEW SKIN. REPLACED LOWER SKIN ON TAIL BOX STRUCTURE PER SRM 51-11-42 AND 57-01-00. (M) 2L72 4F RTA20EU 19951124004121995112400412EU 1995 11 24 USAA951157 119951101A5712 RIB FOKKERF28 F28MK4000 4990810EU NR 4 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19480AU20822 11229 CLT - .5 INCH CRACK AT NR 4 FORWARD CAP RIB AT LOWER FLANGE RADIUS AND TORQUE ROD CUT OUT. CRACK WAS VISUALLY FOUND BY CLT INSPECTION. REPAIRED NR 4 CAP RIB. FABRICATED NEW RIB, PER SRM 57-02-03 AND SRM 20-30-06. (M) 2L72 4F RTA20EU 19951124004131995112400413NM 1995 11 24 USAABB95001 119951021A29133508806 HYDRAULIC PUMP BOEING757 7572B7 1384964NM RT ENGINE FAILED A USAAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 EA19621AU 27200 SFO - FL0066, AFTER TAKEOFF FROM SFO, CREW RECEIVED THE RIGHT ENGINE HYDRAULIC PUMP OVERHEAT LIGHT, RIGHT ELECTRIC PUMP OVERHEAT LIGHT, AND THE ASSOCIATED EICAS MESSAGES. FLIGHT RETURNED TO SFO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP. (M) 2L72 4F RTA2NM 19951124004141995112400414NE 1995 11 24 USAABB95005 219951024A7230ULC35853 ANNULUS FILLERS BOEING757 757225 1384959NM RROYCERB211 RB211535E4 54555NE LT ENG FAN JAMMED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 EA19600AU 22192 030510 PIT - FLT 115, ENROUTE PIT-SEA, NR 1 ENGINE BEGAN TO VIBRATE. REDUCTION IN POWER DID NOT ELIMINATE THE VIBRATION. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE INSPECTED THE ENGINE INLET AND EXHAUST SECTIONS, AND FOUND THE RUBBER SEALS ON THE ANNULUS FILLERS TO BE OUT OF POSITION. THE STRIPS WERE REPOSITIONED. (M) 2L72 4F4 FRTA2NM E12EU 19951124004151995112400415NE 1995 11 24 USAABB95006 219951031A7320556115488000 TUBE BOEING757 7572B7 1384964NM RROYCERB211 RB211535E4 54555NE RT ENGINE CRACKED A USAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 EA19613AU 27144 030896 STL - FL 63, EN ROUTE PHL-SFO, RIGHT ENGINE BEGAN LOSING POWER. CREW COULD NOT GET MORE THAN 3000 LB/HR AT FORWARD THROTTLE STOP, OR LESS THAT 1500 LB/HR AT IDLE. FLIGHT DIVERTED TO STL AND LANDED WITH NO FURTHER INCIDENT. ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE FOUND A PIN HOLE IN THE LINE FROM P1 ACCUMULATOR, AND REPLACED THE LINE. (M) 2L72 4F4 FRTA2NM E12EU 19951124004161995112400416WP 1995 11 24 USAAD95001 119951019A3222 O-RING DOUG DC9 DC981 3022081WP NOSE GEAR LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19805US 48053 EWR - FLT NR 497 - AFTER TAKEOFF, THE CREW WAS UNABLE TO RETRACT THE NOSE GEAR. THE CAPTAIN CYCLED THE GEAR, BUT FAILED TO GET THE GREEN LIGHT. THE FLT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE GEAR SHRADER VALVE O-RING. PERFORMED FULL NOSE STRUT SERVICING. (M) 2L72 4F A6WE 19951124004171995112400417WP 1995 11 24 USAAD95002 119951019A3222 O-RING DOUG DC9 DC981 3022081WP NOSE GEAR LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19805US 48053 MCI - FLT 987 - AFTER TAKEOFF, THE CREW COULD NOT RETRACT THE NOSE GEAR. THE FLT RETURNED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED NOSE GEAR SHRADER VALVE O-RING. SERVICED STRUT WITH NITROGEN. LEAK CHECK OK. (M) 2L72 4F A6WE 19951124004181995112400418WP 1995 11 24 USAAD95003 119951019A56105912290501 WINDSHIELD DOUG DC9 DC981 3022081WP COCKPIT CRACKED A USAAA UNSCHED LANDING O OTHER TOTAKEOFF 1 EA19812US 48092 PHL - FLT NR 1926 - DURING TAKEOFF, CAPTAINS WINDSHIELD CRACKED AND THEN SHATTERED. THE FLT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD. (M) 2L72 4F A6WE 19951124004191995112400419WP 1995 11 24 USAAD95005 119951021A3230 RETRACT MECH DOUG DC9 DC931 3022065WP LT MLG MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19919VJ 48139 CLT - FLT 880 - AFTER RETRACTING GEAR, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. THE CAPTAIN DECIDED TO RETURN TO CLT. THE FLT LANDED WITHOUT FURTHER INCIDENT. RECYCLED LEFT MAIN GEAR THROUGH 5 CYCLES ON GROUND. GEAR INDICATION NORMAL. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F A6WE 19951124004201995112400420NE 1995 11 24 USAAD955004 219951021A73217696067 FUEL CONTROL DOUG DC9 DC981 3022081WP PWA JT8 JT8D217 52053NE NR 2 ENGINE FAILED A AUSAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 EA19810US 48042 IND - FLT NR 987 - AT CRUISE, NR 2 ENGINE ADVANCED TO FULL THROTTLE AND WOULD NOT RESPOND TO CONTROLS. THE CAPTAIN SHUT DOWN NR 2 ENGINE DIVERTED TO IND. THE FLT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED RIGHT FUEL CONTROL. RAN ENGINE. OPS CHECK OK. (M) 2L72 4F4 F A6WE E9NE 19951124004211995112400421EU 1995 11 24 USAAF95004 119951024A335059256 EEL INVERTER FOKKERF28 F28MK0100 4990807EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19892US 11372 ORF - MTC DISCREPANCY, EMERGENCY FLOOR LIGHTING INOP ROW 16. REPLACED INVERTER. (M) 2L72 4F RT 19951124004221995112400422EU 1995 11 24 USAAF95005 119951027A3244 TIRE FOKKERF28 F28MK4000 4990810EU LT MLG FAILED A USAAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 EA19480AU 11229 CAPTAIN ADVISED THAT ON TAKEOFF ROLL AND AND JUST AFTER REACHING V2, A STRONG VIBRATION WAS NOTICED. A PRECAUTIONARY FLY-BY WAS MADE BY CLT TOWER AND THE LEFT INBOARD TIRE WAS APPARENTLY BLOWN. NO EMERGENCY WAS DECLARED, HOWEVER, CFR WAS CALLED OUT BY ATC. THE FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT INCIDENT. (M) 2L72 4F RTA20EU 19951124004231995112400423NM 1995 11 24 USAASB95001 119951021A2421106122412 GENERATOR BOEING737 737301 1384611NM LT ENGINE FAILED A USAAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 EA19354US 23557 CLT - FL 2040 - EN ROUTE TO LGA, CREW NOTED PERIODIC SPIKING FROM THE NR 1 GENERATOR, WHICH CAUSED TR NR 1 CIRCUIT BREAKER TO TRIP. CREW DISCONNECTED THE GENERATOR, AND COULD NOT GET THE APU TO START. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER PROBLEMS. THE GENERATOR WAS PLACED ON MEL AND SUBSEQUENTLY REPLACED DUE TO A BURNED 'B' PHASE TERMINAL. THE APU WAS INSPECTED AND STARTED SEVERAL TIMES WITH NO PROBLEMS NOTED. (M) 2L72 4F RTA16WE 19951124004241995112400424NM 1995 11 24 USAASB95004 119951027A2150 PRESSURIZATION BOEING737 7373B7 1384580NM RT PACK MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19508AU 23383 PIT - FLT NR 1567 - AIRCRAFT DISPATCHED WITH MEL 21-1A ON RIGHT PACK. COULD NOT PRESSURIZE AFTER TAKEOFF. RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE PRESSURIZED AIRCRAFT TO 6 PSID. NO DEFECTS NOTED. RELEASED AIRCRAFT FOR SERVICE. (M) 2L72 4F RTA16WE 19951124004251995112400425NE 1995 11 24 USAASB95006 219951028A7261 OIL LINE BOEING737 7372B7 1384560NM PWA JT8 JT8D15A 52051NE RT ENGINE LOOSE A USAAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA19268AU29107 22880 709096 MSP - FLT NR 1090 - ON CLIMB-OUT, PASSING THROUGH 10,000 FEET, NR 2 ENGINE LOP LIGHT ILLUMINATED ALONG WITH OIL QUANTITY AND OIL PRESSURE DECREASE TO ZERO. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO MSP WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 4 BEARING PRESSURE LINE LOOSE, TIGHTENED SAME. ALSO, FOUND NR 4 BEARING CHIP DETECTOR MISSING AND REPLACED CHIP DETECTOR. SERVICED OIL AND RAN ENGINE. OPS NORMAL. REPLACED ENGINE DUE TO LOW OIL PRESSURE OPERATION AND RETURNED AIRCRAFT TO SERVICE. (M) 2L72 4F4 F A16WE E2EA 19951124004261995112400426NM 1995 11 24 USAASB95007 119951031A79331122514 OIL TEMP BULB BOEING737 737301 1384611NM NR 1 ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CRCRUISE 1 EA19300AU 23228 MCO - FLT NR 0417 - EN ROUTE FLL TO PIT, NR 1 ENGINE OIL TEMP CLIMBED ABOVE RED RADIAL. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER PILOTS HANDBOOK. FLIGHT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED ALL CHIP DETECTORS, NO PROBLEMS FOUND. REPLACED OIL TEMP BULB AND RAN ENGINE AT CRUISE POWER. OIL TEMP INDICATION CHECKED GOOD. (M) 2L72 4F RTA16WE 19951129000011995112900001WP 1995 11 29 UPS804883 119951011A2910 O RING DOUG DC8 DC871F 302199DWP SLOT CHECK VALVEFAILED A IPXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO01700UP 45900 SUPPLEMENTAL MRR: CREW REPORTED LOSS OF HYDRAULIC PRESSURE AND FLUID. PERFORMED LOSS OF HYDRAULIC CHECK LIST, CONTINUED TO MCO. NOTIFIED MIA CENTER TO INCOMING MCO APPROACH CONTROL OUR EMERGENCY AND ASKED FOR EMERGENCY EQUIPMENT TO STAND BY. LANDING UNEVENTFUL, TAXIED CLEAR ON RUNWAY AND STOPPED. MCO MX TOWED A/C TO RAMP. MAINTENANCE FOUND O-RING BLOWN ON SLOT INLET CHECK VALVE ON SLOT CONTROL VALVE. REPLACED O-RINGS ON CHECK VALVE. OPS AND LEAK CHECK NORMAL PER DCI MM 27-80-04, PAGE 201. 2L74 4F RT4A25 19951201000011995120100001WP 1995 12 1 9518459954 119951115A5350 RELEASE MECH DOUG DC9 DC931 3022065WP TAILCONE MALFUNCTIONED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01921RW 47164 DURING H-CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP FROM THE AIRCRAFT. CLEANED THE TAILCONE SEAL, REPLACED 6 GUIDE PINS, AND POLISHED 6 OTHER GUIDE PINS. CHECKED OK. 2L72 4F A6WE 19951201000021995120100002WP 1995 12 1 9518469984 119951118A5350 CLIPS DOUG DC9 DC932 3022066WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND THAT THE TAILCONE DID NOT DROP. ALSO, FOUND A FRAYED RELEASE CABLE AND TWO WORN GUIDE PINS. REPLACED THE CABLE AND PINS, REMOVED THE SEALANT FROM THE RAIN GUTTERS (BOTH SIDES), CLEANED THE TAILCONE SEAL, AND ADJUSTED THE CLIPS. CHECKED OK. 2L72 4F A6WE 19951201000031995120100003NE 1995 12 1 9518479885 219951114A7230 COMPRESSOR DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01401EA 47682 688816 NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE ENGINE WAS INSPECTED, NO DISCREPANCIES NOTED. SUSPECT STALL WAS THE RESULT OF SNOW AND SLUSH INGESTION. ENGINE PERFORMANCE CHECKED OK. 2L72 4F4 F A6WE E2EA 19951201000041995120100004NE 1995 12 1 9518489995 219951114A7230 COMPRESSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL018978E 47327 656955 NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ENGINE WAS INSPECTED, NO DISCREPANCIES NOTED. SUSPECT STALL WAS THE RESULT OF SNOW AND SLUSH INGESTION. ENGINE PERFORMANCE CHECKED OK. 2L72 4F4 F A6WE E2EA 19951201000051995120100005 1995 12 1 9518499946 419951117A3418 TRANSDUCER DOUG DC9 DC931 3022065WP STALL WARNING FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018926E 45863 DURING CLIMB, THE STALL WARNING SYSTEM ACTIVATED AND THE RED STALL LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND SYSTEM MALFUNCTION CONTINUED. PULLED CIRCUIT BREAKER TO DEACTIVATE SYSTEM. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE ANGLE OF ATTACK TRANSDUCER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201000061995120100006WP 1995 12 1 9518509964 119951118A2410 CSD DOUG DC9 DC931 3022065WP RT ENGINE FAILED A NWAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CRCRUISE 1 GL01912RW 47150 DURING CRUISE, THE RIGHT ENGINE CONSTANT SPEED DRIVE HAD A HIGH TEMPERATURE INDICATION AND THE RIGHT GENERATOR TRIPPED OFF LINE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. FLIGHT DIVERTED TO YYZ AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE CONSTANT SPEED DRIVE AND GENERATOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201000071995120100007NM 1995 12 1 9518516308 119951121A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01668US 24223 DURING LINE CHECK (TPE), THE FLOOR EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 51R TO 64R WERE FOUND INOPERATIVE. RECONNECTED LOOSE LIGHT ASSEMBLY PIN AT SEAT ROW 64R. OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951201000081995120100008WP 1995 12 1 9518529945 119951119A2160 THERMAL SWITCH DOUG DC9 DC931 3022065WP LT PACK FAILED A NWAAA UNSCHED LANDING BM SMOKE/FUMES/ODORS/SPARKS OVER TEMP CLCLIMB 1 GL018925E 45840 DURING CLIMB, THE LEFT PACK OVERHEATED AND SMOKE ACCUMULATED IN THE FLIGHT DECK AND CABIN. DEACTIVATED THE LEFT PACK. FLIGHT RETURNED TO ROC AND LANDED WITHOUT INCIDENT. REPLACED THE THERMAL SHUTOFF SWITCH. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201000091995120100009WP 1995 12 1 9518539926 119951119A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01926NW 47425 DURING TAKEOFF, THE AIRCRAFT STARTED TO PRESSURIZE NEGATIVELY. PROBLEM CONTINUED DURING CLIMB AND COULD NOT CONTROL CABIN MANUALLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE DIFFERENTIAL PRESSURE SENSOR, OUTFLOW VALVE ACTUATOR, AND PRESSURE CONTROLLER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201000101995120100010NE 1995 12 1 9518542705 219951120A7230 COMPRESSOR BOEING727 727225 1384077NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE STALLED A NWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01802EA 22433 700572 THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS DURING CLIMB-OUT FROM MSP. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2L73 4F4 F A3WE E2EA 19951201000111995120100011NM 1995 12 1 95FDE01788 119951121A5311 FRAME BOEING727 727227 1384078NM BS 580 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FORWARD BAY FRAME DENTED AT BS 580, BETWEEN STR 25 - STR 22 LT. DENT FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER FEDEX SRM 53-10-1 AND SRM 53-10-4. 2L73 4F A3WE 19951201000121995120100012NM 1995 12 1 95FDEA01781 119951121A57126587019 RIB CHORD BOEING727 7272S2F 1384O81NM BS 760.75 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 REPAIR WING RIB UPPER CHORDS BS 760.75, RBL AND LBL 70.5, IAW FEDEX EA 7-5710-26265 AND 7-5710-26266. REPAIRED LT RIB UPPER CHORD, BS 760.95 IAW FEDEX EA 7-5710-26266. ALSO, REPAIRED RT RIB UPPER CHORD BS 760.95 IAW FEDEX EA 7-5710-26265. 2L73 4F A3WE 19951201000131995120100013NM 1995 12 1 95FDEA01782 119951120A5311 FRAME BOEING727 727227 1384078NM BS 1090 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FRAME CRACKED TOP FLANGE FOUND IN AFT CARGO BAY AT BS 1090, STR 27L. REPAIRED CRACK IN FRAME BS 1090, STR 27L PER FRI 111595TC1 AND FEDEX SRM 53-10-1 FIG 1 DETAIL IV. 2L73 4F A3WE 19951201000141995120100014NM 1995 12 1 95FDEA01783 119951120A5311 FRAME BOEING727 727227 1384078NM BS 970 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FRAME DENTED IN AFT CARGO BAY AT STA 970, STR 23L. REPAIRED DENTED FRAME IN AFT CARGO BAY AT STA 970, STR 23L. ALL WORK DONE PER FEDEX SRM 51040-3. 2L73 4F A3WE 19951201000151995120100015NM 1995 12 1 95FDEA01784 119951120A5311 FRAME BOEING727 727227 1384078NM BS 980 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 IN AFT CARGO BAY, FRAME IS DENTED AT STA 980, STR 23L. DENTED FRAME WAS OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED PER FEDEX SRM 51-40-3, FRAME WAS OUT OF LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19951201000161995120100016NM 1995 12 1 95FDEA01785 119951120A5320 CLIP BOEING727 727227 1384078NM BS 950 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CRACKED STR CLIP BS 950C, STR 7R. REPLACED STR CLIP AT BS 950C, STR 7R. 2L73 4F A3WE 19951201000171995120100017NM 1995 12 1 95FDEA01786 119951118A5320 DOUBLER BOEING727 727227 1384078NM BS 985 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 DENT ON WEB BS 985, BL ZERO, WL 205. ACCOMPLISHED REPAIR ON WEB BS 985, BL ZERO, WL 205, IAW FEDEX SRM 51-40-2. 2L73 4F A3WE 19951201000181995120100018NM 1995 12 1 95FDEA01787 119951121A5720 WEB BOEING727 72722 1384002NM BS 740 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CRACK ON STA 740 WEB AT RBL 42, WL 185 (CENTER TANK). REPAIRED CRACK ON STA 740 WEB AT RBL 42, WL 185 (CENTER TANK) IAW EA 7-5710-26212. 2L73 4F A3WE 19951201000191995120100019NM 1995 12 1 95FDEA01789 119951121A532065453132 CLIP BOEING727 727227 1384078NM BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 660, STR 4L. REMOVED CRACKED STR CLIP, BACK DRILLED NEW STR CLIP, AND INSTALLED FASTENER AT BS 660, STA 4L. 2L73 4F A3WE 19951201000201995120100020NM 1995 12 1 95FDEA01790 119951120A5753BAC1503100046 CHORD BOEING727 7272S2F 1384O81NM TE MID FLAP CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25216FE 22937 RIGHT INBOARD MID-FLAP AFT LOWER CHORD CRACKED AT INBOARD AFT FLAP ACTUATOR RUDDER CUT-OUT. REMOVED NR 5 FLAP TRACK AFT FAIRING. REMOVED DAMAGED PORTION OF AFT LOWER CHORD ON RT INBD MID-FLAP AND REPAIRED IAW FEDEX SRM 51-40-4, FIG 1. REINSTALLED NR 5 FLAP TRACK AFT FAIRING PER FEDEX MM 27-51-31. 2L73 4F A3WE 19951201000211995120100021NM 1995 12 1 95FDEA01791 119951127A5320 INTERCOSTAL BOEING727 727227 1384078NM BS 950-970 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-3), IN AFT CARGO BAY ON INTERCOSTAL BETWEEN BS 950F AND 970 LBL 16 WL 140. FABRICATED AND INSTALLED INTERCOSTAL BETWEEN BS 950F TO 970 LBL 16 WL 140 IAW FEDEX SRM 51-20-1, 51-30-2 AND 53-10-2. 2L73 4F A3WE 19951201000221995120100022NM 1995 12 1 95FDEA01792 119951120A5320 SHEAR TIE BOEING727 727227 1384078NM BS 700 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FWD BAY, CORROSION (C53-111-01-2) ON SHEAR TIE AT BS 700 BETWEEN STR 28 AND 27R, AFT OF FRAME FOUND WHILE WORKING NR0413. CORROSION ON SHEAR TIE AT BS 700 BETWEEN STR 28 AND 27R WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED AND REPLACED SHEAR TIE ON AFT SIDE OF FRAME. 2L73 4F A3WE 19951201000231995120100023NM 1995 12 1 95FDEA01793 119951117A29102249409503 DRAIN LINE DOUG MD11 MD11F 3023600NM NR 3 HYD SYST BROKEN A FDEAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO25605FE 48514 HYD NR 3 FAIL ALERT ILLUMINATED AND NR 3 HYD WENT TO ZERO. FOUND CASE DRAIN LINE BROKEN ON NR 3 ENGINE. MADE INTERIM REPAIR BY REMOVING PUMP AND CASE DRAIN LINE, FOLLOWED MEL 29-3 PROCEDURE. INSTALLED CASE DRAIN LINE AND HYD PUMP, HYD FLUID LEAK TEST COMPLIED PER MM 29-11-20. NO HYD FLUID LEAK WAS FOUND. 2L73 4F RTA22WE 19951201000241995120100024NM 1995 12 1 95FDEA01794 119951118A2613 OVERHEAT WIRE BOEING727 7272S2F 1384O81NM NR 2 ENGINE BARE A FDEAO OTHER N FALSE WARNING APAPPROACH 1 SO25206FE 22928 DIA - NR 2 FIRE WARNING IND ON MOMENTARILY ON APPROACH INTO DEN, LESS THAN 2 SECOND BELL AND LIGHT. SYS CHECKS OK. OPENED COWL AND INSPECTED ALL DUCTS AND ENGINE. FOR LOOSE CONNECTIONS OR BREAKS, CHECKED OK. FOUND EXPOSED WIRE ON OVER HEAT WIRE ADJACENT TO GENERATOR FEEDER CABLES. INSTALLED HEAT SHRINK AND CLEANED CONNECTOR. FOUND AFT CONNECTORS OILY, CLEANED, CHECKED PER JET RUN HANDBOOK 5-17, OK FOR SERVICE. 2L73 4F A3WE 19951201000251995120100025NM 1995 12 1 95FDEA01795 119951109A2612 FIRE CONTL UNIT BOEING727 7272S2F 1384O81NM NR 2 ENGINE MALFUNCTIONED A FDEAO OTHER N FALSE WARNING CRCRUISE 1 SO25206FE 22928 NR 2 ENG FIRE WARNING WOULD INTERMITTENTLY COME ON IN FLT AND DURING TAXI IN. FIRE TEST SYSTEMS CHECKED AND TESTED GOOD. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT PER MM 26-11-01 AND OPS CHECK NORMAL. REMOVED AND REPLACED FIRE AND OVERHEAT DETECTOR, PRECAUTIONARY DUE TO HISTROY. 2L73 4F A3WE 19951201000261995120100026NE 1995 12 1 95UAL900268 219951121A7200 TAILPIPE BOEING747 747238B 1384828NM PWA JT9 JT9D7J 52054NE NR 1 ENGINE FIRE A UALAF ACTIVATE FIRE EXT. L NO TEST TXTAXI/GRND HDL 1 WP29165UA 21658 686035 DURING LANDING ROLLOUT, CREW FIRED BOTH FIRE EXTINGUISHER BOTTLES DUE TO NR 1 ENGINE TAILPIPE FIRE. FLIGHT DATA RECORDER ANALYZED AND IT WAS DETERMINED THAT THE EGT WAS EXCEEDED BY 3 DEGREES FOR ONE SECOND. INSPECTION OF AREA NOTED NO DAMAGE FROM FIRE. POSSIBLE CAUSE OF FIRE: FLIGHT CREW LEFT THE ENGINE IN REVERSE WHILE AT LOW N1 SPEED. 2L74 4F4 F A20WE E20EA 19951201000271995120100027NM 1995 12 1 95UAL900269 119951121A3350 BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297278U 21425 BOTH FORWARD AND AFT LEFT OVERWING EMERGENCY EXIT LIGHTS ARE OUT. REPLACED BATTERIES. 2L73 4F4 F A3WE E2EA 19951201000281995120100028NM 1995 12 1 95UAL900270 119951122A2612162502 CONNECTOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 ENGINE GROUNDED A UALAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP297255U 21402 NR 3 ENGINE FIRE WARNING SYSTEM SHOWS GROUND FAULT AND NR 3 FIRE DETECTOR CIRCUIT GROUND LIGHT ILLUMINATED IN FLIGHT. CLEANED CONNECTOR D1504 ON NR 3 ENGINE AND GROUND CHECKS OKAY. 2L73 4F4 F A3WE E2EA 19951201000291995120100029EU 1995 12 1 95UAL900271 119951122A326085GA2 LGCIU AIRBUS320 A320232 3930326EU NR 2 FAILED A UALAO OTHER N FALSE WARNING APAPPROACH 1 WP29406UA 454 RECEIVED AN ECAM FLIGHT CONTROL FLAPS LOCKED FAULT MESSAGE. FOLLOWED APPROPRIATE PROCEDURES AND LANDED WITH SLATS, BUT NO FLAPS. LANDING WAS UNEVENTFUL. FOUND SENSOR NR 1 (P/N ABS0121-30) MISADJUSTED AND LGCIU NR 2 HAD A HARD FAULT. SFCC INTERPRETED SIGNAL AS A RUNAWAY FLAP AND WING TIP BRAKES WERE DEPLOYED. REPLACED LGCIU NR 2 AND READJUSTED SENSOR NR 1, OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA28NM 19951201000301995120100030SO 1995 12 1 COMA9512008 119951119A325012037995001 TILLER EMB 120 EMB120RT SO NLG STEERING OUT OF ADJUST A COMAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 SO01246CA 120223 NOSE WHEEL STEERING PULLS TO LEFT AND WILL NOT CENTER. PEDAL STEER INOP LIGHT IS ON. ADJUSTED THE STEERING TILLER LOAD POT. SYSTEM TEST SATISFACTORY. 2L72 4T RTA31SO 19951201000311995120100031 1995 12 1 COMA9531194 419951118A34256226190113 AHRS COMPUTER SAAB SF340 SF340A 7850100EU NR 1 DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01359CA17283224 340A053 LEFT H.S.I. HEADING IS SLEWING OUT OF TOLERANCE. REPLACED THE NR 1 AHRS COMPUTER. 2L72 4T RTA52EU 19951201000321995120100032EU 1995 12 1 COMA9531195 119951117A2700 FLIGHT CONTROLS SAAB SF340 SF340A 7850100EU CONTROL YOKES VIBRATION A COMAO OTHER E VIBRATION/BUFFET CLCLIMB 1 SO01158CA 340A158 DURING TAKEOFF, A FORE AND AFT VIBRATION WAS NOTED IN CONTROL YOKES. FLIGHT CONTROL SYSTEM WAS INSPECTED AND NO DEFECTS NOTED. ACFT RELEASED FOR FLIGHT CHECK WHICH WAS SATISFACTORY. 2L72 4T RTA52EU 19951201000331995120100033NM 1995 12 1 DHL95724010 119951121A3240SRL07CA PRESS INDICATOR 1356603399 BOEING727 727228 NM BRAKE SYST FAILED A TDHLAA UNSCHED LANDING N FALSE WARNING DEDESCENT 1 SO01724DH 662 19862 ON DESCENT, HYDRAULIC BRAKE PRESSURE INDICATED 2000 PSI. REMOVED AND REPLACED HYDRAULIC BRAKE ACCESSORY, BRAKE ACCUMULATOR PRESSURE TRANSMITTER AND HYDRAULIC BRAKE PRESSURE GAGE. MM 32-40. 2L73 4F A3WE 19951201000341995120100034NE 1995 12 1 SCNA95275 219951120A7230 N2 ROTOR BOEING727 727225 1384077NM PWA JT8 JT8D17R 52049NE NR 1 ENGINE LOCKED A SCNAE ENGINE SHUTDOWN Y ENGINE STOPPAGE UKUNKNOWN 1 GL15283SC 22559 707176 THE NR 1 ENGINE WAS SHUTDOWN IN-FLIGHT DUE TO A LOCKED N2 ROTOR. REMOVED AND REPLACED THE NR 1 ENGINE. 2L73 4F4 F A3WE E2EA 19951201000351995120100035EU 1995 12 1 WWMA9500083 119951120A3230 FUELING CLIP BAG JETSTMJETSTM3201 1500217EU NLG NOT REMOVED A WWMAO OTHER J WARNING INDICATION CLCLIMB 1 WP15965AE 965 THE NOSE LANDING GEAR INTRANSIT LIGHT CAME IN-FLIGHT, CYCLED GEAR AND HAD NORMAL GEAR DOWN INDICATIONS. AFTER RETRACTION, THE NOSE GEAR INTRANSIT LIGHT STAYED ILLUMINATED. UPON INVESTIGATION, MAINTENANCE FOUND A 5 INCH FUELING GROUND CLIP ATTACHED TO THE NOSE GEAR UPLOCK ROLLER. REMOVED CLIP, INSPECTED FOR DAMAGE AND PERFORMED GEAR SWINGS WITH NO PROBLEMS FOUND. AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T RTA56EU 19951201000361995120100036NM 1995 12 1 95FDEA1796 119951121A5320 GUSSET BOEING727 727232 1384082NM BS 825.95 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 GUSSET AT FRAME BS 825.95 IS CRACKED RBL 65, WL 198. 2L73 4F A3WE 19951201000371995120100037NM 1995 12 1 95FDEA1797 119951121A5315 FLOORBEAM BOEING727 727232 1384082NM BS 1070 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01-3), ON BOTTOM CHORD OF FLOORBEAM AT BS 1070 WL 200 RBL 51 LBL 42 AT NUTPLATE HOLES. 2L73 4F A3WE 19951201000381995120100038NM 1995 12 1 95FDEA1798 119951121A5313 STRINGER BOEING727 727232 1384082NM BS 1133/1139 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-04), ON STRINGER AT BS 1133 AND 1139 STR 6 RT. 2L73 4F A3WE 19951201000391995120100039NM 1995 12 1 95FDEA1799 119951121A5313 STRINGER BOEING727 727232 1384082NM BS 1042-1048 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01-3), ON STRINGER AT BS 1042 TO 1048. 2L73 4F A3WE 19951201000401995120100040NM 1995 12 1 95FDEA1800 119951121A5313 STRINGER BOEING727 727232 1384082NM BS 600-740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01), ON STRINGER NR 5 RT AT BS 600 TO 740. 2L73 4F A3WE 19951201000411995120100041NM 1995 12 1 95FDEA1801 119951121A5320 CHORD BOEING727 727232 1384082NM BS 430 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AT BS 430 BEAM LOWER CHORD LBL 46 LBL 52 WL 801. 2L73 4F A3WE 19951201000421995120100042NM 1995 12 1 DHL95712002 119951119A53203126 ACCESS PANELS BOEING727 72729 1384007NM NLG W/W NOT SECURED A TDHLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01712DH 19401 AFTER TAKEOFF AT 230 KTS, NOSE GEAR DOOR LIGHT ILLUMINATED ON S/O PANEL AND RED NOSE GEAR DOOR LIGHT ILLUMINATED ON FWD PANEL. AIRCRAFT FAILED TO PRESSURIZE IN AUTO, PERFORMED ALTERNATE PROCEDURES AND COULD NOT PRESSURIZE IN MANUAL. SECURED NOSE GEAR ACCESS PLATES, ACCOMPLISHED NOSE GEAR SWING, INDICATIONS OK. PRESSURIZED AIRCRAFT AND CHECKED NORMAL IN AUTO AND MANUAL. 2L73 4F A3WE 19951201000431995120100043NE 1995 12 1 P5CA950844 219951123A7250 TURBINE BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 1 ENGINE FAILED A AP5CAE ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 WP23850FT 19755 685616 WITH POWER STABLE AT 1.36 EPR AND NO THROTTLE MOVEMENT AT 26,000 FT CLIMBING TO 29,000 FT, NR 1 ENGINE APPEARED TO SURGE AND COMPRESSOR STALLED WITH A RAPID RISE IN EGT, 975 FOR 5 TO 6 SECONDS UNTIL THROTTLE WAS RETARDED. ENGINE WAS COOLED FOR 5 MINUTES AND SHUTDOWN. ENGINE WAS RESTARTED, WOULD NOT PRODUCE FULL POWER WITHOUT GOING INTO CAUTION RANGE. PROCEEDED WITH REDUCED POWER TO JNB. FOUND METAL IN TAIL PIPE, ENGINE TO BE REPLACED. 2L74 4F4 F A20WE E20EA 19951201000441995120100044 1995 12 1 SCNA95276 419951121A25655WD230600203 SLIDE DOUG DC10 DC1010 3022110WP R-3 DOOR FAILED A SCNAK NONE O OTHER NRNOT REPORTED 1 GL15573SC 46905 WHEN OPENING THE R-3 DOOR THE SLIDE WAS DEPLOYED INADVERTENTLY AND THE UPPER PORTION OF THE SLIDE FAILED TO INFLATE. REMOVED AND REPLACED THE R-3 DOOR SLIDE. 2L73 4F A22WE 19951201000451995120100045NM 1995 12 1 SWAA950737 119951114A2170 CLAMP BOEING737 7372H4 138448CNM RT PACK BROKEN A SWAAAB UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW0771SW 22358 AT 33,000 FL, EXPERIENCED CABIN PRESSURE DROP. INITIATED EMERGENCY DESCENT, O2 MASKS WERE NOT DEPLOYED. AIRCRAFT DIVERTED TO AUS AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND RIGHT A/C PACK WATER SEPARATOR FWD CLAMP BROKEN. REPLACED CLAMP PER BOEING M/M. 2L72 4F A16WE 19951201000501995120100050EU 1995 12 1 95ZZZX6350 119951101A2750FE204000 RESTRICTORS AEROSPATR72 ATR72212 EU TE FLAPS CLOGGED A SIMAK NONE O OTHER APAPPROACH 1 SW21263AT21246 53 263 MKE - FLT 4234 - DURING APPROACH, FLAP EXTENSION LIGHT ILLUMINATED. FLAPS VERY SLOW TO RETRACT, AFTER EXTENSION, FLAPS RETRACTED. FLAPS EXTENSION AND RETRACTION INTERMITTENT. REMOVED AND INSPECTED FLAP VALVE BLOCK RESTRICTORS IAW JIC 27-54-21, OPS CHECK AND LCK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 26297.0. REFERENCE, OPERATOR CONTROL NR SIMA953052. 2H72 4T RTA53EU 19951201000511995120100051NE 1995 12 1 95ZZZX6351 219951030A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 4 FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION DEDESCENT 1 SO191803 51981 45895 669587 AIR TURN-BACK - PRECAUTIONARY SHUT DOWN OF NR 4 ENGINE. OIL PRESSURE LIGHT ON WITH THROTTLE AT IDLE. DURING TROUBLESHOOTING, PIECES OF METAL WERE FOUND IN THE SCAVENGE PUMP CHIP DETECTOR. ENGINE WAS REMOVED AND REPLACED. 2L74 4F4 F 4A25 1E8 19951201000521995120100052WP 1995 12 1 95ZZZX6352 119951101A323048023301 RETRACT PIN 5753118N DOUG DC8 DC862 3021970WP LT MLG SHEARED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO191803 19730 7593 45895 AFTER GEAR RETRACTION, 'GEAR NOT LATCHED' LIGHT ILLUMINATED. AIRCRAFT MADE AIR TURN-BACK AND RETURNED TO MIAMI WITHOUT INCIDENT. UPON LANDING, FOUND LT MLG RETRACT PIN SHEARED. REMOVED REMAINING PART OF PIN AND INSTALLED NEW PIN AND NUT IAW SB 32-102. OPS CHECKED IAW MM 32-32-2 AND FOUND NORMAL AT THIS TIME. 2L74 4F 4A25 19951201000531995120100053NE 1995 12 1 95ZZZX6353 219951016A7250 CAP LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122* 54555NE NR 3 ENGINE LOOSE A AMTAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL N FALSE WARNING CLCLIMB 1 GL11194AT 193B1230 ON TAKEOFF, NR 3 ENGINE FIRE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN. AIRCRAFT PERFORMED AIR TURN-BACK. INSPECTION REVEALED 6 O'CLOCK BORESCOPE BLANKING PLUG CAP LOOSE. INSTALLED NEW HELICOIL FOR BLANKING CAP RETAINING BOLTS AND REPLACED CROSS-THREADED BLANKING PLUG. 2L73 4F4 F A23WE A12EU 19951201000541995120100054 1995 12 1 95ZZZX6354 419951027A344220871810501 ANTENNA DOUG DC8 DC862 3021970WP RADOME MALFUNCTIONED A ARWAA UNSCHED LANDING O OTHER CRCRUISE 1 SO191804 3577 45896 AIR TURN-BACK, RADAR UNRELIABLE AND PAINTING ERRATICALLY. REPLACED RADAR ANTENNA; OPS CHECK NORMAL. 2L74 4F 4A25 19951201000551995120100055WP 1995 12 1 95ZZZX6355 119951029A2120 CLAMP DOUG DC8 DC862 3021970WP RT NLG WW LOOSE A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19802BN 45909 AIR TURN-BACK. WHILE CLIMBING TO 20,000 FEET OUT OF BOGOTA, LOST CABIN PRESSURE AND WAS UNABLE TO CONTROL CABIN CLIMB. RETURNED TO BOGOTA. REINSTALLED AND SAFETIED CLAMP TO AIR DISTRIBUTION DUCT IN RIGHT NOSE WHEELWELL TUNNEL. SYSTEM OPS CHECKED NORMAL. 2L74 4F 4A25 19951201000561995120100056WP 1995 12 1 95ZZZX6356 119951027A5330 SKIN DOUG DC8 DC862 3021970WP FS 225 DENTED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 DURING PRE-FLIGHT, FOUND DENT ON FUSELAGE AT FS 225.00 BETWEEN L27L AND L25L. DENT WAS BEYOND LIMITS. PERFORMED REPAIR PER SRM 53-2-1, FIGURE 5, PAGE 5. DETAILS OF REPAIR FILED UNDER WO 950102-0015. THIS REPAIR MUST BE REPLACED BY A CLASS 1 OR CLASS 2 REPAIR WITHIN 6,000 LANDINGS AFTER ACCOMPLISHMENT. 2L74 4F 4A25 19951201000571995120100057WP 1995 12 1 95ZZZX6357 119951027A5753 SKIN DOUG DC8 DC862 3021970WP TE FLAP CRACKED A ARWAK NONE O OTHER ININSP/MAINT 1 SO19802BN 45909 ON PRE-FLIGHT INSPECTION, FOUND TWO CRACKS ON OUTBOARD FLAP, INBOARD SECTION, JUST AFT OF FUEL DUMP. PERFORMED REPAIR PER SRM 52-2-0, FIGURE 2, PAGE 9. 2L74 4F 4A25 19951201000581995120100058EA 1995 12 1 95ZZZX6358 119950824A3231MS1699847 BOLT DHAV DHC8 DHC8311 1386006EA LT MLG DOOR FAILED A MASAA UNSCHED LANDING DJ INFLIGHT SEPARATION WARNING INDICATION CLCLIMB 1 SW01432AW 286 GJT - ATER DEPARTURE, PILOTS NOTICED LDG GEAR DOORS CYCLING OPEN AND CLOSED. AIRCRAFT RETURNED TO GJT. UPON INSPECTION, MECHANICS FOUND BOLT ATTACHING THE REAR OF THE AFT OUTBOARD LDG GEAR DOOR ON THE LT MAIN GEAR HAD BACKED OUT AND DEPARTED THE AIRCRAFT. THIS RESULTED IN THE DOOR PIVOTING ON THE REMAINING ATTACH POINT WHICH THEN PULLED TWO INSERTS OUT OF THE COMPOSITE DOOR. A REPAIR WAS DONE TO THE DOOR IAW DHC-8 SRM 51-20-71. A NEW BOLT INSTALLED AS WELL AS A NEW LDG GEAR UPLOCK HOOK. RETRACTIONS WERE PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201000591995120100059WP 1995 12 1 95ZZZX6359 119951027A3241 ANTI SKID SYS DOUG DC8 DC873F 302199FWP MLG MALFUNCTIONED A RRXAO OTHER O OTHER TXTAXI/GRND HDL 1 WP15870TV 46086 KTUS/KDAY - FLT 011 - ON LANDING ROLL-OUT, BRAKES FADE WITH ANTI-SKID ON, HYDRAULIC PRESSURE DROPPED TO 2,000 PSI. MAINTENANCE PERFORMED AN OPERATION CHECK OF THE ANTI-SKID SYSTEM IAW MM CHAPTER 32. NO DEFECTS WERE NOTED. BRAKE SERVICE LIMITS WERE CHECKED BY MAINTENANCE AND FOUND TO BE GOOD. (X) 2L74 4F RT4A25 19951201000601995120100060WP 1995 12 1 95ZZZX6360 119951021A2612D0520 FIRE LOOP DOUG DC8 DC863F 302198FWP NR 2 ENGINE FAILED A RRXAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 WP15865F 46088 KSEA/KDAY - FLT 025 - DURING CRUISE, NR 2 ENGINE FIRE WARNING SOUNDED. THE AIR CREW DISCHARGED THE O/B FIRE AGENT AND FOLLOWED ENGINE SHUT-DOWN PROCEDURES. MAINTENANCE REMOVED AND REPLACED THE LOWER FIRE LOOP AND THE UPPER REAR FIRE LOOP ELECTRICAL CONNECTOR. MAINTENANCE REMOVED AND REPLACED THE O/B FIRE BOTTLE. AN OPERATIONAL CHECK OF THE FIRE WARNING SYSTEM WAS GOOD ON GROUND RUN. (X) 2L74 4F 4A25 19951201000621995120100062 1995 12 1 95ZZZX6362 319951008A61128022521 DEICE BOOT DHAV DHC8 DHC8311 1386006EA PROPELLER BLADE FAILED A MASAO OTHER M OVER TEMP ININSP/MAINT 1 SW01434AW8374 311 INTERNAL SHORT OF ELECTRIC DEICE BOOT CAUSED AN OVERHEAT CONDITION, MELTING COMPOSITE AND FOAM FILLER OF PROPELLER BLADE. (APPROXIMATELY 1 INCH SQUARE BY 1 INCH DEEP AREA AT MID-POINT OF BLADE.) FOUND DURING PRE-FLIGHT INSPECTION ON THE LEFT PROPELLER, NR 4 BLADE. 2H72 4T RTA13NM 19951201000631995120100063EA 1995 12 1 95ZZZX6363 119951029A271082700568S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON DAMAGED A AMASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9136 286 INSPECTION OF AILERON CABLE REVEALED NUMEROUS BROKEN STRANDS ON RIGHT LOWER AILERON CABLE AT STA YW177, RENDERING CABLE UNSERVICEABLE. THE CABLE WAS REPLACED AND RIGGED, A TEST FLIGHT WAS PERFORMED, AND THEN THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201000641995120100064CE 1995 12 1 95ZZZX6364 119951020A56101143840201 WINDSHIELD BEECH 1900 1900D 1154162CE LT COCKPIT FAILED A UUAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO1745AR 1374 UE12 UPON CLIMB-OUT, PILOTS WINDSHIELD SHORTED, BURNING OFF THE CONNECTION AT THE BOTTOM RT ELECTRICAL CONNECTION. (X) 2L72 4T RTA24CE 19951201000651995120100065 1995 12 1 95ZZZX6365 419951006A25624523050 ELT TRAY ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01836CA987 UE32 DURING SCHEDULED INSPECTION, THE ELT MOUNTING TRAY WAS DISCOVERED AS HAVING CRACKED EXTENDING FROM MOUNTING TRAY MOUNT SCREW HOLES. TRAY REPLACED WITH NEW. 2L72 4T RTA24CE 19951201000661995120100066 1995 12 1 95ZZZX6366 419951012A25624530150 ELT CASE ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01848CA3177 52388 UE53 DURING MAINTENANCE IN AFT FUSELAGE, THE ELT WAS DISCOVERED AS HAVING CASE CRACKS, ADDITIONALLY, ELT MOUNTING TRAY HAD CRACKS EXTENDING FROM ALL FOUR MOUNTING SCREW HOLES. UNIT WAS REMOVED AND REPLACED WITH NEW. 2L72 4T RTA24CE 19951201000671995120100067 1995 12 1 95ZZZX6367 419951017A25624253050 ELT TRAY ARTEX 1104 BEECH 1900 1900D 1154162CE AFT FUSELAGE CRACKED A JJBAK NONE O OTHER ININSP/MAINT 1 EA01837CA1133 54121 UE16 DURING SCHEDULED INSPECTION OF AFT FUSELAGE, THE ELT MOUNTING TRAY WAS FOUND CRACKED AROUND 2 MOUNT HOLES. ADDITIONALLY, A 3 INCH CRACK ON AFT END OF TRAY WAS NOTED. COMPLETE ELT ASSEMBLY WAS REPLACED WTIH NEW UNIT. 2L72 4T RTA24CE 19951201000681995120100068WP 1995 12 1 95ZZZX6368 119951009A324095607887 BRAKE ASSY DOUG DC9 DC932 3022066WP NR 1 LEAKING A VJ6AA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11905VJ 47378 ATL - FLT 522 - FLT RETURNED TO ATL DUE TO HYDRAULIC LEAK. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY PER MM 32-40. 2L72 4F A6WE 19951201000691995120100069WP 1995 12 1 95ZZZX6369 119950928A4990GTCP8598D OIL SYSTEM DOUG DC9 DC932 3022066WP APU LEAKING A VJ6AO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO11902VJ 47177 PHL/ATL - FLT 219 - AT THE GATE IN PHL, THE FLIGHT CREW FOUND SMOKE IN THE CABIN. FOUND APU (PN GTCP8598D) LEAKING OIL CAUSING SMOKE IN THE CABIN; THE APU WAS PLACED ON MEL. 2L72 4F A6WE 19951201000701995120100070WP 1995 12 1 95ZZZX6370 119951008A2820 MANIFOLD VALVE DOUG DC9 DC932 3022066WP RT WING OUT OF POSITION A VJ6AA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 SO11915VV 47443 ATL - FLT 505 - FUEL STREAMING OUT OF RIGHT WING TIP, NOTED ON TAKEOFF AND CLIMB-OUT. AIRCRAFT RETURNED TO ATL. FOUND MANIFOLD DRAIN VALVE STUCK OPEN, REPOSITIONED VALVE. VALVE WAS CLEANED AND OPERATION WAS CHECKED FOR FREEDOM OF MOVEMENT PER MM 28-12. 2L72 4F A6WE 19951201000711995120100071WP 1995 12 1 95ZZZX6371 119951025A56105912290502 WINDSHIELD DOUG DC9 DC932 3022066WP RT COCKPIT FAILED A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11919VV 47260 ATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB-OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED. REFERENCE, OPERATOR CONTROL NR 95ZZZX6372. 2L72 4F A6WE 19951201000721995120100072WP 1995 12 1 95ZZZX6372 119951025A30409615059002 WINDOW HEAT CNTL DOUG DC9 DC932 3022066WP RT COCKPIT MALFUNCTIONED A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11919VV 47260 ATL - FLT 919 - AIRCRAFT RETURN, ON THE CLIMB, OUT OF ATL AT 17,000 FEET, 300 KNOTS, THE FIRST OFFICER DISCOVERED FORWARD OUTER PANE WINDOW SPIDER-WEBBED. REFERENCE, OPERATOR CONTROL NR 95ZZZX6371. 2L72 4F A6WE 19951201000731995120100073WP 1995 12 1 95ZZZX6373 119951028A217021D101 COALESCER BAG DOUG DC9 DC932 3022066WP LT/RT DIRTY A VJ6AO OTHER J WARNING INDICATION DEDESCENT 1 SO11918VV 47320 DFW/ATL - FLT 224 - ON DESCENT INTO ATL, LOST PRESSURIZATION. OXYGEN MASKS DID NOT DROP DUE TO FLIGHT LEVEL. INSTALLED BOTH RIGHT AND LEFT AIR CYCLE MACHINE SUPPLY DUCTS, AND RIGHT AND LEFT COALESCER BAGS. 2L72 4F A6WE 19951201000741995120100074WP 1995 12 1 95ZZZX6374 119951102A2130 PRESSURIZATION DOUG DC9 DC932 3022066WP CABIN MALFUNCTIONED A VJ6ABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 SO11901VJ 47275 ATL/MEM - FLT 512 - CABIN PRESSURE LOST AT FL 240. CABIN ALTITUDE INCREASED TO OVER 15,000 FEET DURING EMERGENCY DESCENT. MASKS DEPLOYED, UNABLE TO CONTROL CABIN WITH MANUAL CONTROLLER. INSPECTED TAIL SECTION FOR BLOWN DUCTS, CHECKED OUTFLOW VALVE, PERFORMED DECAY RATE CHECK AND STOWED ALL OXYGEN MASKS AND PERFORMED DROP CHECK PER MM 35-20. NO DEFECTS NOTED. 2L72 4F A6WE 19951201000751995120100075WP 1995 12 1 95ZZZX6375 119951007A28107912854537 SUPPLY LINE DOUG DC9 DC932 3022066WP LT WING FAILED A VJ6AA UNSCHED LANDING K FLUID LOSS TOTAKEOFF 1 SO11938VV 47442 FLT 520 - CENTER TANK VENTED 3,000 POUNDS OF FUEL THROUGH FUEL VENT. REPLACED LEFT WING FUEL SUPPLY PIPE ASSEMBLY. 2L72 4F A6WE 19951201000761995120100076NE 1995 12 1 95ZZZX6376 219950920A7310320115 FUEL HEAT VALVE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A VJ6AAE UNSCHED LANDING ENGINE SHUTDOWN MJ OVER TEMP WARNING INDICATION CRCRUISE 1 SO11906VJ 47379 666862 NR 1 ENGINE OIL TEMPERATURE EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMPERATURE, 139 DEGREES. REPLACED FUEL HEAT VALVE. DRAINED AND REPLACED ENGINE OIL. REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C. CHECKS OK. NO LEAKS ON RUN-UP. 2L72 4F4 F A6WE E2EA 19951201000771995120100077WP 1995 12 1 95ZZZX6377 119950928A2810 FUEL TANK DOUG DC9 DC932 3022066WP LT WING OVERFILLED A VJ6AA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SO11915VV 47443 ATL - FLT 276 - AFTER TAKEOFF, AIRCRAFT EXPERIENCED FUEL VENTING OVERBOARD. AIRCRAFT RETURNED TO ATL. FOUND LT WING INDICATION READING LOW. WING OVER-SERVICED, BACK FLUSHED FUEL, NO TRANSFER OCCURRED. 2L72 4F A6WE 19951201000781995120100078WP 1995 12 1 CKSA95039 119951128A532037558261 FITTING DOUG DC8 DC862F 3021972WP BS 492 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL233931A58215 45961 KOSC - FLT 72016 - DURING 'C-1' CHECK INSPECTION FOUND, CARD NR 5570-0551 AREA, FORWARD LOWER CARGO BILGE, FORWARD PIT STA 492-STA 500 AT 32L-31L, CORROSION ON SKIN AND ANGLE. LEVEL 2 TASK NR 74816. CLEANED AND REMOVED CORROSION AS REQUIRED IAW SRM 51-1-8. REPLACED FITTING IAW DC8 SRM 51-1-20D. (X) 2L74 4F 4A25 19951201000791995120100079NM 1995 12 1 CKSA95127 119951007A2612897080 A5 CIRCUIT CARD BOEING747 747132 1384882NM APU SHORTED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23625PL74582 20247 NSTU/YMML - FLT 67785 - APU FIRE DETECTOR BLINKS IN-FLIGHT WHEN SELECTED TO BOTH. RESECURED A-5 CIRCUIT CARD FOR APU 'A' FIRE LOOP, OPS CHECK GOOD ON GROUND IAW B747 MM 26-10-00. (X) 2L74 4F A20WE 19951201000801995120100080WP 1995 12 1 CKSA95128 119951013A261237715523 FIRE AMP DOUG DC8 DC851 3021920WP NR 4 ENGINE NO POWER A CKSAK NONE N FALSE WARNING ININSP/MAINT 1 GL23804CK56154 45689 KPHX - FLT 67919 - ON ENGINE START, NR 4 ENGINE INDICATED FIRE WARNING MOMENTARILY. WHEN TESTED, THE WARNING LIGHT WAS INOPERATIVE. REMOVED AND REPLACED NR 4 ENGINE FIRE AMP. OPS CHECKS GOOD. (X) 2L74 4F 4A25 19951201000811995120100081WP 1995 12 1 CKSA95130 119951021A261224490222 FIRE DETECTOR DOUG DC8 DC8F55 3021928WP NR 4 ENGINE GROUNDED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL236161C56275 45856 KMIA - FLT 68166 - AT 30,000 FEET, FIRE WARNING ON NR 4 ENGINE, WITH LIGHT IN HANDLE AND BELL, AFTER PULLING NR 4 POWER LEVER TO IDLE. FIRE WARNING WENT OUT. FOUND FIRE WARNING DETECTOR LOOP GROUNDED TO AFT INBOARD COWL. REPAIRED AS NECESSARY. OPS CHECK NORMAL ON RUN-UP IAW MM 26-2-3. (X) 2L74 4F 4A25 19951201000821995120100082NM 1995 12 1 EISA95417 119950926A2611 SENSING TUBE BOEING727 72725 1384006NM SMOKE DETECTOR BENT A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 SMOKE DETECTOR SENSING TUBE BENT LT SIDE COMP 1. REMOVED DAMAGE PER MM 20-10-5. FABRICATED NEW TUBE PER MM 26-17-0 AND BPS 5001. INSTALLED AND SECURED PER MM 26-17-0 AND SRM 51-30-2. (X) 2L73 4F A3WE 19951201000831995120100083WP 1995 12 1 HAL95140 119951028A33506011775 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13679HA 143 47662 HNL - INFORMATION FROM LOG PAGE 144164-3. EXTERIOR EMERGENCY LIGHTING INOP ON BOTH SIDES. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT TT, 35,898 HOURS. AIRCRAFT TOTAL CYCLES, 58,671. (X) 2L72 4F A6WE 19951201000841995120100084WP 1995 12 1 HAL95141 119951029A33506003043 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 10559 47764 HNL - INFORMATION FROM LOG PAGE 143949. FORWARD HALF OF FLOOR EMERGENCY LIGHTNG INOP. REPLACED EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT TT, 27,451 HOURS. AIRCRAFT TOTAL CYCLES, 68,526. (X) 2L72 4F A6WE 19951201000851995120100085CE 1995 12 1 HERA9514 119950715A3297 WIRE BEECH 1900 1900C 1154161CE LANDING GEAR BROKEN A HERAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL031553C UC24 ANC - FLT 1421 - AIR RETURN DUE TO LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT LANDED ANC WITHOUT INCIDENCE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LANDING GEAR RELAY CIRCUIT BREAKER. THREE LANDING GEAR RETRACTIONS SHOWED THE SYSTEM TO BE WORKING NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4T RTA24CE 19951201000861995120100086EU 1995 12 1 P2RA950020 119951101A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU L2 DOOR INOPERATIVE A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314975 261 ATL - FLT CREW FOUND L2 DOOR GIRT BAR WILL NOT ENGAGE. ITEM WAS DEFERRED PER MEL 15-61-01. MAINTENANCE REINSTALLED GIRT BAR ON L-2 DOOR. PERFORMED OPERATIONAL CHECKS PER AMM 52-22-22. RESULTS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2L72 4F A35EU 19951201000871995120100087CE 1995 12 1 S2YA950027 119951010A32311148100451 CAM BEECH 1900 1900D 1154162CE LT OTBD MLG DOORBROKE A S2YAK NONE O OTHER ININSP/MAINT 1 GL1391SK 3320 526 UE91 DURING A POST-FLIGHT INSPECTION, FLIGHT CREW NOTICED THE OUTBOARD GEAR DOOR ACTUATING CAM HAD THE UPPER TANG BROKEN OFF. MAINTENANCE REPLACED THE CAM ASSY AND OPERATIONAL CHECKED GOOD. THE TANG THAT BROKE HAD SIGNS OF A PREVIOUS BREAK. (X) 2L72 4T RTA24CE 19951201000881995120100088EU 1995 12 1 SIMA953041 119951031A33506013211 EEL POWER SUPPLY SAAB SF340 340B 7860101EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21346SB1233 19881 340B346 DFW - FLT 3527 - EMERGENCY LIGHTS BY ROW 6 AND ROW 7 INOPERABLE. REMOVED AND INSPECTED POWER SUPPLY 27 LN. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 1384.0. (X) 2L72 4T RTA52EU 19951201000891995120100089NE 1995 12 1 SIMA953051 219951101A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 1 FAILED A ASIMAAF UNSCHED LANDING ACTIVATE FIRE EXT. AP FLAME/FIRE NO WARNING INDICATION CLCLIMB 1 SW21426MQ157535738 037 120214 ORD - FLT 4076 - DURING TAKEOFF, NR 1 ENGINE LOST POWER, LOUD NOISE HEARD FROM ENGINE. F/O REPORTED FIRE FROM ENGINE, NO FIRE WARNINGS GIVEN ON ALERTS. FIRE BOTTLE BLOWN. AIRCRAFT LANDED IN ORD. MAINTENANCE REPLACED THE ENGINE DUE TO INTERNAL ENGINE DAMAGE. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 20131.0. (X) 2H72 4T4 TRTA53EU E20NE 19951201000901995120100090EU 1995 12 1 SIMA953052 119951101A2750025AB1115 RESTRICTORS AEROSPATR72 ATR72212 EU TE FLAPS CLOGGED A SIMAK NONE O OTHER APAPPROACH 1 SW21263AT21246 158 263 MKE - FLT 4234 - DURING APPROACH, FLAP EXTENSION LIGHT ILLUMINATED. FLAPS VERY SLOW TO RETRACT, AFTER EXTENSION, FLAPS RETRACTED. FLAPS EXTENSION AND RETRACTION INTERMITTENT. REMOVED AND INSPECTED FLAP VALVE BLOCK RESTRICTORS IAW JIC 27-54-21, OPS CHECK AND LCK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. PART TOTAL CYCLES, 26297.0. REFERENCE, OPERATOR CONTROL NR 95ZZZX6350. (X) 2H72 4T RTA53EU 19951201000911995120100091NE 1995 12 1 SIMA953053 219951101A7261ST3086013 VENT TUBE O-RING AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE NR 1 ENGINE WORN A SIMAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SW21242AT 242 120261 SBN - FLT 4023 - NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED WITH OIL PRESSURE FLUCTUATING AT 40-45. CAPTAIN DIVERTED TO SBN AFTER SHUTTING DOWN ENGINE DURING FLIGHT. FOUND OIL LEVEL LOW. REMOVED AND INSPECTED O-RING ON OIL VENT TRANSFER TUBE AND TIGHTENED B-NUT ON SCAVENGE TUBE. PERFORMED LOW OIL PRESSURE CHECK IAW P/W MM. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T4 TRTA53EU E20NE 19951201000921995120100092EU 1995 12 1 SIMA953061 119951102A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU CABIN SHORTED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21423MQ3452 812 547 030 RFD - DURING PHASE 1 INSPECTION, MAINTENANCE DISCOVERED THE PASSENGER ENTRANCE STAIR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY IAW ATR 42 JIC 33-51-24. OPS CHECK IAW ATR 42 JIC 33-50-00. OPS CHECK WAS GOOD. AIRCRAFT WAS OK FOR RETURN TO SERVICE. PART TOTAL CYCLES, 4435.0. (X) 2H72 4T RTA53EU 19951201000931995120100093EU 1995 12 1 SIMA953062 119951102A3010B03AA1031 DEICE CONTROLLER AEROSPATR42 ATR42300 8680920EU AIRFRAME MALFUNCTIONED A SIMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21422MQ8123 817 T1753 0028 ORD - FLT 4340 - AIRFRAME DE-ICE FAULTY IN-FLIGHT. AIRCRAFT RETURNED TO ORD. LANDING UNEVENTFUL IN ORD. REMOVED AND INSPECTED AIRFRAME DE-ICE CONTROLLER 'B'. GROUND RUN CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 10799.0. (X) 2H72 4T RTA53EU 19951201000941995120100094EU 1995 12 1 SIMA953121 119951108A3320BR6303121 LIGHT SAAB SF340 SF340A 7850100EU CABIN FAILED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SW21119AE 340A119 LAW - FLT 3798 - DURING THE PROCESS OF PREPARING AIRCRAFT FOR DEPARTURE FROM GATE AREA, SMOKE WAS DETECTED COMING FROM VICINITY OF WINDOW LIGHT AT SEAT 11A. MAINTENANCE INSPECTED AND FOUND THE WINDOW LIGHT FIXTURE HAD FAILED. THE LIGHT FIXTURE AND FLUORESCENT BULB WERE REPLACED AND GROUND CHECK GOOD. ALL WORK IAW PER SAAB AMM. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19951201000951995120100095NE 1995 12 1 TWRA9557 219951029A75307479555 ENG VANE CONTROL BOEING747 747121 1384871NM PWA JT9 JT9D7AH 52054NE NR 1 ENGINE FAILED A TWRAK NONE X ENGINE FLAMEOUT DEDESCENT 1 EA15604FF 19659 685714 NR 1 ENGINE STALLED AT TOP OF DESCENT. EGT MAX 778 DEGREES, ENGINE SHUT-DOWN. RE-LIT NORMAL IN DESCENT AT FLIGHT LEVEL 280. ENGINE OPS NORMAL REMAINDER OF FLIGHT. REMOVED AND REPLACED EVC. OPS CHECK OK. (X) 2L74 4F4 F A20WE E20EA 19951201000961995120100096NM 1995 12 1 TWRA9558 119951030A275065B156948 SUPPORT LINK BOEING747 747121 1384871NM RT TE FLAP CRACKED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15604FF 19659 NR 7 CANOE AFT SUPPORT LINK CRACKED. REMOVED AND REPLACED NR 7 FLAP TRACK LINK. OPS CHECK OK. (X) 2L74 4F A20WE 19951201000971995120100097NM 1995 12 1 TWRA9559 119951106A261130326E8 SMOKE DET AMP BOEING747 747121 1384871NM AFT CARGO INTERMITTENT A TWRAF ACTIVATE FIRE EXT. N FALSE WARNING DEDESCENT 1 EA15613FF 19647 MIA - AIRCRAFT EXPERIENCED AN INTERMITTENT AFT CARGO FIRE WARNING ON DESCENT INTO MIA. THE NR 1 BOTTLE WAS FIRED. THE SECOND BOTTLE WAS DISCHARGED ON APPROACH PER FM 2-12-3. UPON ARRIVAL, MAINTENANCE INSPECTED SYSTEM AND REPLACED 3 SMOKE DETECTORS AND 1 AMPLIFIER. SYSTEM TEST OK. (X) 2L74 4F A20WE 19951201000981995120100098EU 1995 12 1 VTZA96021 119951108A315091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU COCKPIT CONSOLE DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27306UE 41020 IAD/RIC - FLT 6444 - DURING TAKEOFF AT 1949 HRS ON 11-08-95, ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE GUST LOCK AND PARKING BRAKE MICROSWITCHES. OPS CHECKED GOOD SEVERAL TIMES. ARCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951201000991995120100099NM 1995 12 1 W8PA9502 119951030A7830315A18004 ACTUATOR BOEING737 737301 1384611NM NR 2 TR UNIT BYPASSING A W8PAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 NM03301AU29882 0650 23229 COS - RIGHT ENGINE THRUST REVERSER OVERHEAD LIGHT ILLUMINATED JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO COS. FOUND NR 2 THRUST REVERSER OUTBOARD CENTER ACTUATOR BYPASSING. REPLACED ACTUATOR. ALSO, ADJUSTED THRUST REVERSER TARGETS ON SWITCHES S-831 AND S-832. (X) 2L72 4F RTA16WE 19951201001001995120100100EU 1995 12 1 WTAA950292 119951028A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG BROKEN WIRE A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17401UE 729 RIGHT MAIN GEAR 'RED' INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE AT RIGHT MAIN GEAR UPLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA21EU 19951201001011995120100101SO 1995 12 1 WTAA950294 119951027A325019582 CYLINDER EMB 120 EMB120RT SO NLG STEERING CRACKED A WTAAD RETURN TO BLOCK JK WARNING INDICATION FLUID LOSS TXTAXI/GRND HDL 1 WP17251YV 120251 SFO - NOSE WHEEL STEERING REPORTED INOPERATIVE DURING TAXI OUT. CREW RECEIVED GREEN HYDRAULIC LOW PRESSURE, LOW LEVEL AND MAIN HYDRAULIC PUMP LOW PRESSURE WARNINGS. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND CRACK AT NOSE GEAR RIGHT SIDE STEERING RACK CYLINDER HOUSING TO BE CAUSE OF STEERING SYSTEM FAILURE AND HYDRAULIC FLUID LEAK. MAINTENANCE REPLACED CYLINDER HOUSING AND REPLENISHED HYDRAULIC FLUID SUPPLY. NOSE STEERING OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA31SO 19951201001021995120100102WP 1995 12 1 9518719927 119951115A2780 RETRACT CABLES DOUG DC9 DC931 3022065WP RT LE FLAPS MISROUTED A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL018920E 45835 DURING APPROACH, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND AIRCRAFT CONTINUED TO GRR LANDING WITHOUT INCIDENT. FOUND RIGHT WING RETRACT CABLES MISROUTED AND WEARING INTO PULLEY SUPPORT BRACKET AT DRIVE TRACK. REPLACED SUPPORT BRACKET, PULLEYS, AND RETRACT CABLES. RIGGED SLAT SYSTEM, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001031995120100103WP 1995 12 1 9518729942 119951121A3350 EEL DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL013991C 47175 DURING LINE CHECK, FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. REPLACED DEFECTIVE EMERGENCY LIGHT ASSEMBLY AT FORWARD LEFT DOOR, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001041995120100104WP 1995 12 1 9518739942 119951120A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL013991C 47175 DURING LINE CHECK, FOUND ALL FLOOR EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED FORWARD POWER SUPPLY, ALL FOUR BATTERY PACKS AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001051995120100105WP 1995 12 1 9518749996 119951119A3350 EEL SOCKET DOUG DC9 DC931 3022065WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018932E 47141 DURING LINE CHECK, FOUND FORWARD AISLE EMERGENCY LIGHT AT STATION 232 INOPERATIVE. REPLACED BROKEN BULB SOCKETS AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001061995120100106WP 1995 12 1 9518759996 119951119A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018932E 47141 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS FROM ROWS 6 THROUGH 12 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001071995120100107WP 1995 12 1 9518769922 119951119A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01945N 47664 DURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001081995120100108WP 1995 12 1 9518779963 119951118A3350 BATTERY DOUG DC9 DC931 3022065WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01913RW 47171 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHT DEFECTIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001091995120100109WP 1995 12 1 9518789978 119951117A3350 EEL WIRE DOUG DC9 DC931 3022065WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019342 47391 DURING LINE CHECK, FOUND EMERGENCY LIGHT ABOVE AFT FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPAIRED BROKEN WIRE, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001101995120100110WP 1995 12 1 9518799978 119951117A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019342 47391 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT ROWS 12 AND 13 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001111995120100111WP 1995 12 1 9518809911 119951119A3231 RETRACT MECH DOUG DC9 DC931 3022065WP NLG DOOR LACK OF LUBE A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL01961N 47405 DURING CLIMB, A VIBRATION WAS FELT FROM THE NOSE LANDING GEAR, AFTER LANDING GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND RIGHT NOSE LANDING GEAR DOOR OPEN. INSPECTED ALL HINGE POINTS AND DOOR RELEASE MECHANISM, LUBRICATED ALL HINGE POINTS AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201001121995120100112WP 1995 12 1 9518819884 119951121A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01677MC 47756 DURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS BETWEEN ROWS 6 AND 11 INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201001131995120100113WP 1995 12 1 9518829152 119951117A3350 EEL TRACK DOUG DC9 DC914 3022034WP CABIN OUT OF ADJUST A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018911E 45825 DURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT FORWARD CABIN GALLEY INOPERATIVE. FOUND FLOOR LIGHTING TRACK OUT OF ALIGNMENT, ADJUSTED TRACK AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201001141995120100114NM 1995 12 1 9518832711 119951121A2751 INDICATOR BOEING727 7272S7 138407ZNM TE FLAPS MALFUNCTIONED A NWAAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 GL01715RC 22019 DURING CLIMB WITH RETRACTION OF FLAPS, AN ASYMMETRIC TRIP OF THE INBOARD FLAPS OCCURRED AT TWO DEGREES. AIRCRAFT DUMPED FUEL, RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED INBOARD TRAILING EDGE FLAP INDICATOR, CHECKED TRANSMITTERS AND CABLES, SYSTEM CHECKED OK. 2L73 4F A3WE 19951201001151995120100115NE 1995 12 1 9518849907 219951123A7200 ENGINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 2 BIRD STRIKE A NWAAA UNSCHED LANDING C F.O.D. TOTAKEOFF 1 GL01957N 47253 653680 GCM - NR 2 ENGINE INGESTED A BIRD AT ROTATION ON TAKEOFF. THE AIRCRAFT RETURNED TO GCM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE WITH A SERVICEABLE UNIT. 2L72 4F4 F A6WE E2EA 19951201001161995120100116NM 1995 12 1 9518852702 119951123A3150 T/O WARNING BOEING727 727225 1384077NM COCKPIT SOUNDED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL018877Z 21450 DURING TAKEOFF ROLL, SPEED BRAKE FLAP WARNING SOUNDED. ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED TAKEOFF WARNING TEST, COULD NOT DUPLICATE. ALL CHECKS NORMAL. 2L73 4F A3WE 19951201001171995120100117EU 1995 12 1 9518863247 119951123A3260 PROXIMITY SW AIRBUS320 A320211 3930320EU LT MLG DOOR DIRTY A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01347NW 408 BOS - DURING APPROACH, AFTER THE LANDING GEAR WAS EXTENDED RECEIVED L/G DOORS NOT CLOSED MESSAGE. THE LEFT MAIN LANDING GEAR DOOR INDICATED PARTIALLY OPEN ON ECAM. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CYCLED LANDING GEAR HANDLE. ALL INDICATIONS NORMAL AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED THE CANNON PLUGS ON BOTH MAIN LANDING GEAR DOOR PROXIMITY SWITCHES AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951201001181995120100118EU 1995 12 1 9518873247 119951123A3260848401 PROXIMITY SENSOR AIRBUS320 A320211 3930320EU LT MLG FAILED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01347NW 408 DURING LANDING GEAR RETRACTION AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE CLOSED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR (27GA), OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951201001191995120100119WP 1995 12 1 95FDEA01802 119951124A5511 SPAR DOUG DC10 DC1010CF 3023502WP HORIZ STAB CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO2568053 47807 REF EO 8-5510-7-3312 PT 4, RT HORIZ STAB, FWD SPAR, UPPER CHORD, FWD TANG CRACKED AT 2ND HOLE I/B OF CLOSING RIB PLANE. CRACK MOVES AFT FROM HOLE .375 INCH. TRIMMED OUT CRACKED AREA PER SRM 55-20-00, FABRICATED DOUBLER, FILLER, SHIM PER SRM 55-20-00. INSTALLED DOUBLER PER SRM 55-20-00. 2L73 4F RTA22WE 19951201001201995120100120SO 1995 12 1 COMA9512009 119951121A323012038594001 CONTROL MODULE EMB 120 EMB120RT SO LANDING GEAR MALFUNCTIONED A COMAO OTHER O OTHER APAPPROACH 1 SO01403CA1586887 120267 LANDING GEAR HESITATED ABOUT 5 SECONDS BEFORE EXTENDING WHEN SELECTED DOWN DURING APPROACH. COULD NOT DUPLICATE FAULT. REPLACED THE LANDING GEAR CONTROL MODULE FOR TROUBLE SHOOTING. 2L72 4T RTA31SO 19951201001211995120100121 1995 12 1 COMA9512010 419951120A34256226342022 EFIS TUBE EMB 120 EMB120RT SO RT COCKPIT FAILED A COMAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO01189CA 120189 COPILOTS TOP EFIS TUBE SMELLED OF ELECTRICAL BURNING AND TUBE FAILED SHORTLY THEREAFTER. REPLACED THE COPILOTS EADI-EFD-86. 2L72 4T RTA31SO 19951201001221995120100122SO 1995 12 1 COMA9512011 119951118A612078249024 PCU EMB 120 EMB120RT SO LT PROP DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01161CA7928 242 120143 LEFT PROPELLER BETA INDICATOR IS FLASHING ON AND OFF AND PROP IS LURCHING. REPLACED THE PROPELLER PITCH CONTROL UNIT. 2L72 4T RTA31SO 19951201001231995120100123EU 1995 12 1 COMA9531196 119951119A2730531137 SWITCH SAAB SF340 SF340A 7850100EU RT PITCH TRIM DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01341CA 340A021 PITCH TRIM FUNCTION FROM COPILOTS POSITION IS INTERMITTENT. REPLACED THE COPILOTS PITCH TRIM SWITCH. 2L72 4T RTA52EU 19951201001241995120100124EU 1995 12 1 COMA9531197 119951119A3150004WS00 WEU SAAB SF340 SF340A 7850100EU AVIONICS DEFECTIVE A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01357CA19746100 340A044 CON FIG WARNING, DURING TAKEOFF ROLL. REPLACED THE WARNING ELECTRONIC UNIT AND ACFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19951201001251995120100125EA 1995 12 1 COMA9560607 119951121A2750 RETRACT MECH CNDAIRCL600 CL6002B19 EA TE FLAPS OUT OF ADJUST A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01932CA 7038 FLAPS FAILED AT ZERO DEGREES, FAULT COULD NOT BE DUPLICATED. CHECKED FLAP RIGGING AND ADJUSTED TO MAINTENANCE MANUAL SPECIFICATIONS. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951201001261995120100126EU 1995 12 1 DL31L954429 119951119A3350 EEL WIRE 081691 AIRBUS310 A310324 3930206EU CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27835AB 650 EMERGENCY LIGHT AT SEAT 2C HAS A BROKEN WIRE. REPLACED EMERGENCY FLOOR LIGHT AT 2C AND TESTS OK. 2L72 4F RTA35EU 19951201001271995120100127NM 1995 12 1 DL72E954430 119951119A2160 TEMP CONTROLLER 5483803 BOEING727 727247 138408FNM LT PACK SHORTED A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27830WA 17C822 21482 ONCE AIRBORNE, THE LEFT PACK CONTROLLER WOULD NOT RESPOND TO MANUAL INPUTS. EVENTUALLY THE CONTROLLER GAVE OFF SOME SMOKE AND POPPED THE MAIN CONTROL CIRCUIT BREAKER. SELECTOR SHORTED INTERNALLY, REPLACED PANEL AND OPERATION NORMAL. 2L73 4F A3WE 19951201001281995120100128NM 1995 12 1 DL72E954446 119951120A5320 WEB BOEING727 727247 138408FNM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272829W 21481 A .375 INCH CRACK IN LT LWR TORQUE BOX VERTICAL WEB AT UPPER FWD LIGHTENING HOLE ADJACENT TO DOUBLER. FOUND DURING F-2 LETTER CHECK TPAMM, REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19951201001291995120100129NM 1995 12 1 DL72E954454 119950620A5330 SKIN BOEING727 727247 138408FNM BS 1010 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27831WA 21483 THE SKIN AT THE BUTT SPLICE AT STA 1010 WAS FOUND TO BE CORRODED AT SEVERAL PLACES. THREE AREAS WERE CUT OUT ALONG THE SPLICE TO REMOVE DAMAGE AT S-29L, 29R AND 27R. AN EXISTING BUTT SPLICE REPAIR EXISTED AT STR 30 AND WAS REMOVED. THE CUT AT STR 29L MEASURES 2.25 INCH BY 1.75 INCH, THE CUT AT S-30 MEASURES 3 INCH BY 4 INCH, THE CUT AT S-29R MEASURES 2.5 INCH BY 1.75 INCH, AND THE CUT AT S-27R MEASURES 6 INCH BY 2 INCH. THE ORIGINAL SKIN IS MANUFACTURED FROM 2024-T3 CLAD MILLED TO 0.071 LOCALLY. ERA301979-14 AUTHORIZES A DOUBLER REPAIR TO COVER THE THREE AREAS AT S-29L, 30 AND 29R. S-27R WILL BE REPAIRED PER SRM. 2L73 4F A3WE 19951201001301995120100130NM 1995 12 1 DL72E954489 119951125A2150 PACK VALVE 39854021 BOEING727 727247 138408FNM LT MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO272829W P3606 21481 ON CLIMBOUT, A/C WOULD NOT HOLD PRESSURIZATION. DESCENDED AND CABIN STILL CLIMBED, LT DUCT PRESS 20 LBS HIGHER THAN RT. CA REPLACED LT PAC VALVE, CLEANED TRASH FROM LWR AFT CORNER OF C2 BIN DOOR AND A/C PRESSURE CHECK OK. 2L73 4F A3WE 19951201001311995120100131NM 1995 12 1 DL72L954439 119951119A5755651734781A PANEL 651734781A BOEING727 727232 1384082NM NR 2 SPOILER DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27514DA 2393 21430 FOUND NR 2 SPOILER PANEL DELAMINATED. REPLACED PANEL, ROUTED TO SHOP FOR REPAIRS. 2L73 4F A3WE 19951201001321995120100132NM 1995 12 1 DL72L954440 119951119A3350900835A BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27510DA 21312 EMERGENCY LIGHTS INOP 2R AND AFT AISLE. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F A3WE 19951201001331995120100133NM 1995 12 1 DL72S954436 119951020A5754 RIB 651622373 BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27522DA BN504 21582 DURING INSPECTION, NR 2 L/E SLAT WAS FOUND WITH L/E SUPPORT RIB NR 3 CRACKED. REPAIRED PER SRM 57-50-3. 2L73 4F A3WE 19951201001341995120100134NM 1995 12 1 DL72S954444 119951120A57546516224101 SKIN BOEING727 727232 1384082NM NR 8 LE SLAT DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27401DA 21145 DURING ROUTINE SHOP INSPECTION, AN AREA ON THE OUTER SKIN 11 INCHES FROM THE I/B END WAS FOUND TO BE DENTED AND OIL CANNED. THE DAMAGED AREA WAS CUT OUT AND REPAIRED PER SRM 57-50-3 FIG 1 FOR NR 8 L/E SLAT PANEL. 2L73 4F A3WE 19951201001351995120100135NM 1995 12 1 DL72S954450 119951120A3350 BATTERY S106 BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27545DA 22494 AFT BULLNOSE EMERGENCY LIGHT DIM. C/A REPLACED BATTERIES, OPS CHECK GOOD. 2L73 4F A3WE 19951201001361995120100136NM 1995 12 1 DL72S954453 119951106A57126518522 RIB BOEING727 727232 1384082NM BS 760 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 DURING ACCOMPLISHMENT OF EO 4-58560-3AD, A CRACK WAS DISCOVERED IN THE VERTICAL FLANGE OF THE LBL 70.5 WING RIB CHORD. THE CRACK RAN FROM ONE OF THE UPPER FASTENERS IN THE VERTICAL FLANGE AT STA 760.95 DOWN TO THE HORIZONTAL FLANGE. THIS CRACK REQUIRES AN ALTERNATE METHOD OF REMOVAL TO THE ONE IN THE REFERENCED EO. THE RIB CHORD IS MANUFACTURED FROM 7075-T6 EXTRUSION. REPAIRED PER DL ERA 302686-14AD. 2L73 4F A3WE 19951201001371995120100137NM 1995 12 1 DL72S954462 119950727A57546516221100 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27517DA 21433 COVE PANEL ATTACHING ANGLE CRACKED UNDER UPSTOPS. REPAIRED AS PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2L73 4F A3WE 19951201001381995120100138NM 1995 12 1 DL72S954463 119950727A5754651622100 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27517DA 21433 SKIN ATTACHING ANGLE CRACKED 31 INCHES FROM OUTBOARD END. REPAIRED AS PER M/M 57-54-0. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2L73 4F A3WE 19951201001391995120100139NM 1995 12 1 DL72S954465 119951121A2780 ACT FITTING BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27525DA 21585 NR 2 SLAT ACTUATOR O/B ATTACH FITTING BROKEN AT UPPER ATTACH BOLT AREA. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER 57-42-0 AND ERA 302790-14. 2L73 4F A3WE 19951201001401995120100140NM 1995 12 1 DL72S954466 119951121A5320 WEB BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27525DA 21585 LWR LT TORQUE BOX VERT WEB CRACKED .375 INCH AT LWR FWD LIGHTENING HOLE NEXT TO EXISTING DOUBLER. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER M/M 53-11-0. 2L73 4F A3WE 19951201001411995120100141NM 1995 12 1 DL72S954467 119951121A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27525DA 21585 A .25 INCH CRACK AT COVE SKIN ANGLE FOR NR 2 SLAT AT ANTI-ICE DUCT. FOUND DURING E-1 LTR CK TPAMM AND REPAIRED PER 57-54-0. 2L73 4F A3WE 19951201001421995120100142NM 1995 12 1 DL72S954469 119951121A2780 ACT FITTING BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27525DA 21585 FOUND DURING E-1 LETTER CHECK, NR 2 SLAT ACTUATOR O/B ATTACH FITTING BROKEN AT I/B ATTACH BOLT AREA. REPAIRED PER ERA 302790-14 CODE 4-57-45. 2L73 4F A3WE 19951201001431995120100143NM 1995 12 1 DL72S954473 119951122A5720 SPAR STIFFENER BOEING727 727232 1384082NM AFT OF NR 3 SLATCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27536DA 22049 FOUND ON B1 LETTER CK, LE SPAR STIFFENER CRACKED OUTBD TRACK NUMBER 3 SLAT INBD ANGLE. REPAIRED PER MM 57-20-21. 2L73 4F A3WE 19951201001441995120100144NM 1995 12 1 DL72S954475 119951122A2780 ACTUATOR MOUNT BOEING727 727232 1384082NM NR 7 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27536DA 22049 FOUND DURING B-1 LETTER CHECK, NR 7 L/E SLAT ACTUATOR MOUNT FITTING CRACKED 1 INCH AT LWR I/B MOUNT BOLT. REPAIRED PER M/M 57-42-0 PAR 5. 2L73 4F A3WE 19951201001451995120100145NM 1995 12 1 DL72S954476 119951122A5754 ANGLE BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27536DA 22049 FOUND DURING B-1 LETTER CHECK, NR 5 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED .25 INCH AT O/B END. REPAIRED PER M/M 57-54-0 PAR 5A. 2L73 4F A3WE 19951201001461995120100146NM 1995 12 1 DL72S954482 119951123A332010617823 BALLAST BOEING727 727232 1384082NM BS 910 FAILED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27533DA 22046 LOG ITEM 2, ELECTRICAL SMELL IN MID CABIN POPPED LT AFT CABIN CEILNG LIGHT C/B. FOUND BALLAST AT STA 910 INTERNALLY SHORTED CAUSING BURNT ELECTRICAL SMELL IN CABIN. REPLACED BALLAST, OPERATION NORMAL. 2L73 4F A3WE 19951201001471995120100147NM 1995 12 1 DL72S954483 119951123A2120656024013 DUCT BOEING727 727232 1384082NM LT PACK RUPTURED A DALAB EMER. DESCENT E VIBRATION/BUFFET CRCRUISE 1 SO27421DA 21274 FLT DIVERTED INTO DCA AT FL 350, CABIN ALT 5,600 FT, AFTER ABOUT 10 MIN OF LITE VIBRATION OF UNKNOWN ORIGIN, CABIN CLIMBED AT 500 FT/MIN AND UNABLE TO CONTROL IN ANY MODE OF PRESS. ACCOMPLISHED LOSS OF PRESS AND EMERGENCY DESCENT CK LIST AT 10,000 FT, CABIN CONTROL WAS REGAINED IN ALL MODES AS LONG AS PWR WAS KEPT ABOVE 1.2 EPR. ON INTIATION OF EMERGENCY DESCENT A LOUD ROAR BEGAN AT FWD ENTRY DOOR AFT SIDE. FOUND DUCT JUST FORWARD OF LEFT WATER SEPARATOR HAD RUPTURED. REPLACED DUCT, OPERATION NORMAL. 2L73 4F A3WE 19951201001481995120100148NM 1995 12 1 DL72S954493 119951101A5753 DOUBLER BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 NR 2 MIDFLAP WAS FOUND TO HAVE CRACKED DOUBLER AT AFT LOWER SPAR ANGLE REPAIR AT I/B QUADRANT CUTOUT. REPAIR WAS PERFORMED PER M/M 57-52-0 FIG 802. FOUND DURING SHOP MTC VISIT. 2L73 4F A3WE 19951201001491995120100149NM 1995 12 1 DL72S954494 119951114A5753652163362 DOUBLER BOEING727 727232 1384082NM NR 4 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 DURING SHOP INSPECTION, NR 4 MIDFLAP WAS FOUND WITH CRACKED DOUBLER AT AFT CLOSE OUT RIB LOWER AFT CORNER. REPAIRED PER MM 57-52-0. 2L73 4F A3WE 19951201001501995120100150NM 1995 12 1 DL72S954495 119951028A53206554583156 DOUBLER BOEING727 727232 1384082NM FS 1158-1183 DISBONDED A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 FUSELAGE SKIN REPAIR AT AFT LAVATORY SERVICE PANEL CUTOUT, FS 1158 TO FS 1183, BETWEEN S-20L AND S-24L. DURING ACCOMPLISHMENT OF EO 4-69078-3AD, THE INTERNAL BONDED DOUBLER WAS FOUND DISBONDED IN SEVERAL LOCATIONS AROUND THE AFT LAVATORY SERVICE PANEL. AFFECTED UNITS S-14L AND S-20L SKIN ASSY: 65-54583-156, S-20L/S-26L SKIN ASSY: 65-54583-142; -125 SKIN; -126 DOUBLER; 65-25607-2 TRIPLER. FAA/DER APPROVAL FORM 8110-3, DTD 11-16-95. 2L73 4F A3WE 19951201001511995120100151NM 1995 12 1 DL72W954438 119951119A5754 RIBS BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272814W 20870 RIBS ON I/B AND O/B SIDES OF ACT ATTACH POINT NR 4 SLAT ARE CRACKED FWD OF PREVIOUS REPAIRS. REMOVED OLD DOUBLERS AND DAMAGED AREAS, FABRICATED DOUBLERS PER M/M 57-54-0 FIG 804 AND INSTALLED DOUBLERS PER M/M 57-54-0. 2L73 4F A3WE 19951201001521995120100152NM 1995 12 1 DL72W954457 119951120A5522657278420 SKIN BOEING727 727247 138408FNM RT ELEVATOR DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO272814W 20870 DURING SHOP INSPECTION, RT ELEVATOR WAS REPAIRED FOR DAMAGE TO LOWER SKIN AT ACCESS ANGLE 9, PER SRM 55-20-3. 2L73 4F A3WE 19951201001531995120100153NM 1995 12 1 DL73E954496 119950922A5230 FRAME 65C25180 BOEING737 7372S3 NM AFT CARGO DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27367DL 360 21774 AIRWORTHINESS DIRECTIVE 90-06-02, DOOR AFT CARGO, LOWER AFT CORNER, FRAME AND BEAM REPAIR. DURING ROUTINE OVERHAUL, THE LOWER AFT CORNER OF THE AFT CARGO DOOR WAS FOUND DAMAGED. THE FRAME WAS CRACKED AXIALLY ALONG THE RADIUS APPROX 20 INCHES. THE LOWER BEAM WEB WAS SEVERED AND THE O/B ATTACHMENT ANGLE WAS CRACKED IN THE UPPER FLANGE INTO THE RADIUS. REPAIRED PER DL ERA 271679-14AD. 2L72 4F RTA16WE 19951201001541995120100154NM 1995 12 1 DL73S954428 119951119A575465162221 RIB BOEING737 737232 1384475NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27322DL BN1181 23094 NR 3 L/E SLAT SUPPORT RIB IS CRACKED 8 INCHES FROM I/B END. REPAIRED PER SRM 57-54-0. 2L72 4F RTA16WE 19951201001551995120100155NM 1995 12 1 DL73S954455 119951117A53156545808535 FLOORBEAM BOEING737 737232 1384475NM BS 294.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27322DL 23094 THE STA 294.5 FLOORBEAM UPPER T-CAP WAS FOUND CRACKED AT RBL 52, UPON INSPECTION PER SI 3-61663-12AD. THE UPPER CAP IS MANUFACTURED FROM 10136-2401 (0.094 7075-T6511 EXTRUSION). ACCOMPLISHED REPAIRS PER DL ERA 302777-14AD. 2L72 4F RTA16WE 19951201001561995120100156NM 1995 12 1 DL73S954478 119951122A79311163P181 DIFF PRESS SW BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27311DL 23083 717140 ON CLIMBOUT, NR 2 ENG OIL PRESS BYPASS LIGHT ON. ALL OTHER IND NORMAL, DIVERTED TO MEM, LIGHT STAYED ON. NORTHWEST MTC CHECKED AND REPLACED OIL FILTER AND NO CONTAMINATION WAS FOUND. PUT THE NR 2 ENG BYPASS LIGHT ON MCO MEL 79-00-02. WHEN A/C ARRIVED ATL, MTC REPLACED DIFF PRESS SW 793701055 AND REMOVED MCO. 2L72 4F4 FRTA16WE E2EA 19951201001571995120100157NM 1995 12 1 DL767954432 119951119A3350BPS73 EEL POWER SUPPLY BOEING767 767232 1385132NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27113DA 22225 POWER SUPPLY FOR ESCAPE PATH LIGHTING FAILED TEST DURING LAYOVER AT TOC. REPLACED POWER SUPPLY UNIT (P/N 333780100), CLEARED BY LOG BOOK ITEM. 2L72 4F RTA1NM 19951201001581995120100158NM 1995 12 1 DL76L954470 119951122A3350 BATTERY PACK 20131A BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27179DN 22333 25144 ON SERVICE CHECK, FOUND AFT RT EMERGENCY LIGHT IN CEILING INOP. REPLACED AFT RT BATTERY PACK EMERGENCY LIGHTS, CHECKED NORMAL (P/N 337101963), (S/N 22333). 2L72 4F RTA1NM 19951201001591995120100159NE 1995 12 1 DL76L954480 219951123A7230 COMPRESSOR BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE STALLED A DALACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 SO27178DN 25143 724149 NR 2 ENGINE COMPRESSOR STALLED ON T/O. THROTTLED BACK, ENGINE OPERATED NORMAL AT LOW POWER SETTINGS. ENGINE WAS NOT SHUTDOWN, OVERTEMP 684 DEGREES. REPLACED NR 2 ENGINE AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19951201001601995120100160NE 1995 12 1 DL76L954481 219951123A723056A521 FAN BLADES BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 ENGINE BENT A DALAA UNSCHED LANDING CJEF.O.D. WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 SO27180DN 25985 724418 JFK - AIR TURNBACK DUE TO SUSPECTED BIRD STRIKE. THE RT ENGINE HAD LOUD VIBRATIONS AND ENGINE VIB READING 3.5 ON CLIMBOUT. NORMAL LANDING COMPLETED. PERFORMED BIRD STRIKE INSPECTION AND FOUND FAN BLADES NR 36, 35 AND 34 BENT. REPLACED BLADE SETS. ALSO, FOUND FAN EXIT GUIDE VANE DAMAGED AT 4 O'CLOCK POSITION. REPAIRED VANE PER MM 72-33-02. 2L72 4F4 FRTA1NM E24NE 19951201001611995120100161NM 1995 12 1 DL76P954477 119951122A335008163000510 EEL ASSY BOEING767 767332 1382001NM CABIN MISSING A DALAK NONE O OTHER ININSP/MAINT 1 SO27140LL 25988 EMERGENCY PATH LIGHTS MISSING SEATS 25B AND 25G. REPLACED MISSING LIGHT ASSY, OPN OK. 2L72 4F RTA1NM 19951201001621995120100162WP 1995 12 1 DLL10954456 119951121A2750 ROLLER/BRACKET LKHEED1011 10113851 5265010WP NR 3 TE FLAP MISSING A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27721DA 193C1139 ON TAKEOFF, FLAPS DID NOT COME UP BEYOND 8 DEGREES, RETURNED ATL. FOUND NR 3 RT FLAP IB ACTUATING ROLLER AND BRACKET MISSING. REPLACED ROLLER AND BRACKET INSTALLED PER ERA 272472-14. RIGGED VANE ROLLER REF MM 27-51-00. 2L73 4F A23WE 19951201001631995120100163WP 1995 12 1 DLL10954486 119951124A7932 OIL PRESS TRANS 797001019 LKHEED1011 10113851 5265010WP NR 3 ENGINE FAILED A DALACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO27728DA TA3490 193C1173 ON TAKEOFF, NR 3 ENG OIL PRESS INDICATED HIGH, 100 PSI PLUS. ABORTED TAKEOFF UNDER 60 KTS, RETURNED TO GATE AT LOW POWER, EQUAL N2 ON NR 1 AND NR 3 ENG AT 85 PERCENT, NR 2 ENG OIL PRESS READ 58 PSI, NR 3 ENG OIL PRESS INDICATING 82 PSI. REPLACED OIL PRESS TRANSMITTER, BLEW OUT TRANSMITTER AND PRESS SW LINE AND CHECKED CHIP DETS. RAN ENG LEAK AND OPS CK NORMAL. 2L73 4F A23WE 19951201001641995120100164WP 1995 12 1 DLL13954464 119951121A53501547690109 FILLET PANEL LKHEED1011 10113851 5265010WP LT FUS/WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27786DL 193A1123 A/C ARRIVED AT GATE WITH LEFT SIDE AFT FUSELAGE TO WING FILLET PANEL DAMAGED, 3 FT BY 5 FT SECTION WAS MISSING. REPLACED PANEL, RETURNED TO SERVICE. 2L73 4F A23WE 19951201001651995120100165WP 1995 12 1 DLL17954459 119951119A57541592943140 TE SKIN LKHEED1011 10113853 5265020WP NR 6 LE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27768DL 193H1216 DURING SHOP INSPECTION, NR 6 RT L/E SLAT PANEL WAS FOUND WITH DAMAGE TO TRAILING EDGE SKIN. REPAIRED PER SRM 57-51-00 FIG 805. 2L73 4F A23WE 19951201001661995120100166WP 1995 12 1 DLL17954460 119951119A57541592943140 RIB LKHEED1011 10113853 5265020WP NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27768DL 193H1216 DURING SHOP INSPECTION, RT NR 6 L/E SLAT WAS FOUND WITH CRACKED INTERNAL RIB AT 55 INCHES FROM I/B END. REPAIRED PER SRM 57-51-0. 2L73 4F A23WE 19951201001671995120100167WP 1995 12 1 DLL17954461 119951121A57541592941118 RIB LKHEED1011 10113853 5265020WP NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27768DL 193H1216 DURING SHOP INSPECTION, A CRACK WAS FOUND IN A RIB AT 7 INCHES FROM THE O/B END OF THE NR 4 SLAT. THE DAMAGE WAS REPAIRED PER SRM 57-51-00. 2L73 4F A23WE 19951201001681995120100168NM 1995 12 1 DLM11954447 119951121A33507839 BULB DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27807DE 48478 FLOOR TRACK EELS INOP, SEAT 35 AND 42 LEFT, 45 AND 39 RT. RELAMPED, OPN CKS OK. 2L73 4F RTA22WE 19951201001691995120100169NM 1995 12 1 DLM11954452 119951121A33507839 BULB DOUG MD11 MD11 3023602NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27807DE 48478 FLT ATTENDANT CREW REST AND L2 RED EMERGENCY LT INOP. REPLACED BULB, OPN OK. 2L73 4F RTA22WE 19951201001701995120100170NM 1995 12 1 DLM88954427 119951119A3350RPS1 EEL PWR SUPPLY RPS1 DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27904DE 8569 53409 EMERGENCY EXIT TRACK LIGHTING INOP BETWEEN ROWS 24 TO 38. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L72 4F RTA6WE 19951201001711995120100171NE 1995 12 1 DLM88954468 219951120A7261 ENGINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 LEAKING OIL A DALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO27918DL 49583 718145 ON TAKEOFF BETWEEN 2,000 AND 14,000 FT, MILD SMOKE ODOR IN CABIN. ALL FDW AND AFT LAV SMOKE DETECTOR ACTIVATED. FOUND OIL IN 8TH STAGE SADDLE DUCT. FERRY A/C TO ATL AND REPLACED ENG. 2L72 4F4 FRTA6WE E9NE 19951201001721995120100172NM 1995 12 1 DLM88954474 119951122A3350 BULB DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27944DL 49817 EMERGENCY ESCAPE TRACK LIGHT PULLED OUT AT SEAT 3C. REBULBED AND REINSTALLED LENS. 2L72 4F RTA6WE 19951201001731995120100173NM 1995 12 1 DLM88954485 119951124A3350 EEL POWER SUPPLY 110049 DOUG MD88 MD88 3023688NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27995DL 7908 53362 FOUND 2 E-PATH LIGHTING STRIPS NOT WORKING. REPLACED BATTERY PWR SUPPLY, OPN NOW CKS GOOD. 2L72 4F RTA6WE 19951201001741995120100174NM 1995 12 1 P5CA9500845 119951125A2612 FIRE LIGHT BOEING747 747121 1384871NM APU ILLUMINATED A P5CAF ACTIVATE FIRE EXT. N FALSE WARNING ININSP/MAINT 1 WP23831FT 19648 DURING PREFLIGHT CHECK, FOUND APU FIRE HANDLE HAD LIGHTS ON WITH NO BELL. FEO PULLED THE FIRE HANDLE, LIGHT REMAINED ON, FEO FIRED THE FIRE BOTTLE AND LIGHT WENT OUT. APU PLACED ON DMI NOT TO BE USED. REPLACED BOTTLE AND SQUIB PER MM 26-22-01. APU OPS DURING RUN OK, UNABLE TO DUPLICATE ON GROUND. RETURNED TO SERVICE. 2L74 4F A20WE 19951201001751995120100175NM 1995 12 1 P5CA9500846 119951126A323065B825582 DNLOCK ACTUATOR BOEING747 747122 1384872NM RT MLG FAILED A P5CAO OTHER JK WARNING INDICATION FLUID LOSS APAPPROACH 1 WP23851FT 19756 NR 1 HYDRAULIC SYSTEM FAILED WHEN LANDING GEAR WAS EXTENDED, DURING FINAL APPROACH. DUE TO UNSAFE, UNCOMPLETED GEAR EXTENSION, ALT EXTENSION WAS COMPLETED WITH NO EFFECT. ACCOMPLISHED BODY GEAR NOT EXTENDED CHECKLIST AND LANDED WITHOUT FURTHER INCIDENT. RIGHT BODY GEAR DOWNLOCK ACTUATOR REMOVED AND REPLACED IAW MM 32-33-15 PG 401. 2L74 4F A20WE 19951201001761995120100176NM 1995 12 1 P5CA9500847 119951125A5270 SWITCH BOEING747 747122 1384872NM CARGO DOOR OUT OF ADJUST A P5CAK NONE N FALSE WARNING ININSP/MAINT 1 WP23851FT 19756 DURING PREFLIGHT INSPECTION, PILOT'S POSITION INDICATION SHOWED CARGO DOOR OPEN, FEO'S ANNUNCIATOR INDICATED AFT CARGO DOOR OPEN. ADJUSTED DOOR LATCH SWITCH IAW MM 52-34-09 AND OPS CHECK OK. 2L74 4F A20WE 19951201001771995120100177WP 1995 12 1 UPS805109 119951121A3350 BATTERY PACK DOUG DC8 DC873F 302199FWP CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01806UP 46006 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS INOP. REPAIRED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, SYSTEM CHECKS GOOD PER MM 33-50-01. 2L74 4F RT4A25 19951201001781995120100178WP 1995 12 1 UPS805110 119951123A32305708458503 RETRACT MECH DOUG DC8 DC871F 302199DWP MAIN GEAR LACK OF LUBE A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01701UP 45938 CREW REPORTED ON UPLATCH CHECK, GEAR NOT LATCHED LIGHT ON. RECYCLED, NO HELP, DOORS DID HOLD GEAR UP. CHECKED OPERATION OF ALL MLG AND MLG DOOR SWITCHES, ALL CHECKED GOOD. LUBED MAIN GEAR AND DOOR MECHANISMS, CHECKED UPLATCHES, ALL CHECKED OK. NO DEFECTS NOTED, OK FOR SERVICE. 2L74 4F RT4A25 19951201001791995120100179WP 1995 12 1 UPS805111 119951126A33505708458503 BATTERY PACK DOUG DC8 DC873F 302199FWP FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01813UP 46059 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHTS INOP IN FLIGHT DECK. ACCOMP, REMOVED AND REPLACED BATTERY PACK. 2L74 4F RT4A25 19951201001801995120100180NM 1995 12 1 95ZZZX6378 119950723A2612894093 FIRE LOOP BOEING737 7372P6 NM NR 2 ENGINE MALFUNCTIONED A A6XAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SO132FOR 21677 MIA/PIE - ON CLIMB-OUT OF MIA TO PIE, CREW GOT A NR 2 ENGINE FIRE INDICATION. C/W SPECIAL PROCEDURE, SHUT DOWN ENGINE, AND FIRED BOTTLE. LANDED IN PIE. INSPECTED, FOUND LOWER LOOP DETECTOR BAD. REPLACED LOOP, FIRE BOTTLE, AND SQUIBS. 2L72 4F RTA16WE 19951201001841995120100184GL 1995 12 1 95ZZZX6382 319951106A6111 SNAP RING CESSNA207 207A 2073604CE MCAULYD3A34 D3A34C404 GL BLADE BASE DEPARTED A OEZAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 WP1973426 1 20700588 796960 DURING FLIGHT, SNAP RING DEPARTED PROPELLER BLADE BASE CAUSING DAMAGE TO BLADE. UNKNOWN CAUSE. 1.1 HOURS SINCE OVERHAUL. 1H71 3O A16CE 5 CP47GL 19951201001951995120100195EA 1995 12 1 95ZZZX6393 219951026A852075060 CONNECT ROD PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA ENGINE FAILED A LFQAO OTHER ERKVIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS CRCRUISE 1 SW1543519940 347450192 L102967 DURING LEVEL FLIGHT WITHOUT INDICATION OF POSSIBLE PROBLEM, THE ENGINE FAILED. PROBLEM WAS DETERMINED TO BE A BROKEN CONNECTING ROD BOLT. ENGINE CASE WAS DESTROYED. AIRCRAFT WAS NOT DAMAGED. 1L72 3O3 O A7SO 1E10 19951201002001995120100200SO 1995 12 1 ZWZA0012 219951030A7414101630203 MAGNETO CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO LT ENG LT MAG FAILED A ZWZAK NONE O OTHER ININSP/MAINT 1 GL2380Q 214 4102690 402B1384 DURING REPOSITIONING OF AIRCRAFT, NOTICED DEAD LT MAG ON LT ENGINE. CHANGED MAG WITH SERVICEABLE UNIT, BUT NOTICED DEFECTIVE MAG WAS RECENTLY OVERHAULED AND HAD ONLY 213.8 HOURS SINCE OVERHAUL. (X) 1L72 3O3 O A7CE E8CE 19951201002011995120100201WP 1995 12 1 9518559926 119951014A5220 FRAME DOUG DC9 DC932 3022066WP OVERWING EXITS CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND CRACKS IN ALL FOUR OVERWING EMERGENCY EXIT DOOR PANS, BENEATH NR 14 SUPPORT. REPAIRED PANS (P/N 5913195-1) PER EA 99-103294, -103295, -103296 AND -103297. 2L72 4F A6WE 19951201002021995120100202WP 1995 12 1 9518569763 119951014A5753 SKIN DOUG DC9 DC941 302207NWP LT/RT TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01763NW 47396 DURING LINE CHECK, FOUND CRACKS IN THE LEFT AND RIGHT FLAP TRAILING EDGES. REPAIRED FLAPS PER EA 98-104972, -104973 RESPECTIVELY. 2L72 4F A6WE 19951201002031995120100203WP 1995 12 1 9518579926 119951016A5315 FLOORBEAM DOUG DC9 DC932 3022066WP FS 689-699 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND CORROSION IN THE BL 0 FLOOR CAP BETWEEN FS 689 TO 699. REPAIRED CAP (P/N 5910347-25), PER EA 99-103291. 2L72 4F A6WE 19951201002041995120100204WP 1995 12 1 9518589926 119951016A5320 WEB DOUG DC9 DC932 3022066WP FS 699 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND CORROSION IN THE LEFT MAIN LANDING GEAR WHEEL WELL FORWARD SLANT PRESSURE PANEL WEB. REPAIRED WEB (P/N 5956065-41), PER EA 99-102597. 2L72 4F A6WE 19951201002051995120100205WP 1995 12 1 9518599926 119951018A5320 ANGLE DOUG DC9 DC932 3022066WP FS 198-203 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01926NW 47425 DURING H-CHECK, FOUND CORROSION IN THE UPPER CUSP ANGLE AT THE MAIN CABIN DOOR FS 198 TO 203. REPAIRED ANGLE (P/N 9910078-9), PER EA99-103303. 2L72 4F A6WE 19951201002061995120100206WP 1995 12 1 9518609877 119951103A5220 DOOR PAN DOUG DC9 DC951 3022051WP EMERGENCY EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01786NC 48148 DURING H-CHECK, FOUND A CRACK IN BOTH THE RIGHT FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR PANS, BENEATH NR 14 SUPPORT. REPAIRED PANS (P/N 5913195-1), PER EA 98-101997 AND 98-101998. 2L72 4F A6WE 19951201002071995120100207NM 1995 12 1 9518612291 119951108A5315 FLOORBEAM BOEING727 727251 138408HNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01291US 21379 DURING T-CHECK, FOUND CORROSION ON THE BS 1130 FLOORBEAM UPPER CHORD LBL 38 TO LBL 43 AND LOWER CHORD LBL 57 TO RBL 50. REPAIRED CHORDS (P/N 65-20838-34), PER EA 22-105020, -105021 RESPECTIVELY. 2L73 4F A3WE 19951201002081995120100208EU 1995 12 1 9518623211 119951109A5320 SILL AIRBUS320 A320211 3930320EU LT/RT SERV DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01311US 125 DURING IL CHECK, FOUND CORROSION IN BOTH THE LEFT AND RIGHT AFT SERVICE DOOR LOWER SILLS. REPAIRED SILLS (P/N D534-80043-204, -205), PER EA 32-104298, -104291 RESPECTIVELY. 2L72 4F RTA28NM 19951201002091995120100209WP 1995 12 1 9518631223 119951110A5320 SUPPORT DOUG DC10 DC1030 3023501WP FS 495 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01223NW 46580 DURING T-CHECK, FOUND CORROSION ON THE FS 495 FLOOR SUPPORT BETWEEN RBL 25 TO 50. REPAIRED SUPPORT PER EA 12-104181. 2L73 4F A22WE 19951201002101995120100210WP 1995 12 1 9518641223 119951110A5330 SKIN DOUG DC10 DC1030 3023501WP FS 1524 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01223NW 46580 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN INNER SURFACE FS 1524 BETWEEN LONGERON 50R TO 51R. REPAIRED SKIN (P/N AYB7065-2). 2L73 4F A22WE 19951201002111995120100211WP 1995 12 1 9518651223 119951113A5330 SKIN DOUG DC10 DC1030 3023501WP FS 1197-2005 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01223NW 46580 DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN BS 1197 TO 2005, LONGERONS 45L TO 46L AND 45R TO 46R. REPAIRED SKIN (P/N AJC 7164), PER EA 12-103213 AND -103214. 2L73 4F A22WE 19951201002121995120100212WP 1995 12 1 9518669940 119951115A5720 FITTING DOUG DC9 DC932 3022066WP WS 164 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013322L 47031 DURING MAINTENANCE CHECK, FOUND A CRACK IN THE LEFT WING FITTING STA 164 AT STR 20, OUTBOARD SIDE. REPLACED FITTING PER EA 99-10239. 2L72 4F A6WE 19951201002131995120100213WP 1995 12 1 9518679603 119951117A5320 FITTING DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 25L AND 18R END FITTINGS AT THE FS 996 PRESSURE BULKHEAD. REPLACED FITTINGS PER SRM 51-30, 51-10-3, AND 53-02. 2L72 4F A6WE 19951201002141995120100214WP 1995 12 1 9518689603 119951117A5320 FITTING DOUG DC9 DC932 3022066WP FS 603 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 603 FRAME TO TANK ATTACH FITTING, BETWEEN LONGERONS 19L TO 22L. REPLACED FITTING. 2L72 4F A6WE 19951201002151995120100215WP 1995 12 1 9518699603 119951117A5320 FITTING DOUG DC9 DC932 3022066WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 756. REPLACED FITTING PER SRM 53-02, 51-30. 2L72 4F A6WE 19951201002161995120100216WP 1995 12 1 9518709603 119951118A5320 FITTING DOUG DC9 DC932 3022066WP FS 200 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE BS 200 FLOORBEAM ATTACH FITTING AT LONGERON 18R. REPLACED FITTING PER SRM 51-30-0. 2L72 4F A6WE 19951201002171995120100217WP 1995 12 1 9518889308 119951124A32225910448537 STRUT DOUG DC9 DC982 3022082WP NLG REQD SERVICE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01311RC 48089 DURING CLIMBOUT, NOSE LANDING GEAR RED UNSAFE REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND AIRCRAFT LANDED WITHOUT INCIDENT. DRAINED FLUID FROM STRUT AND RESERVICED TO PROPER LEVELS. RETRACTED GEAR SEVERAL TIMES, OPERATIONAL CHECK OK. MOISTURE WAS FOUND IN FLUID. 2L72 4F A6WE 19951201002181995120100218WP 1995 12 1 9518899875 119951125A3350 EEL POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01784NC 48109 DURING LINE MAINTENANCE INSPECTION, FOUND ONE SECTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERY, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201002191995120100219WP 1995 12 1 9518909853 119951123A5270 SWITCH BRACKET DOUG DC9 DC951 3022051WP CABIN DOOR LOOSE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01762NC 47110 DTW-RDU - DURING TAKEOFF AT APPROXIMATELY 80 KNOTS, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. FOUND AND TIGHTENED A LOOSE WARNING SWITCH BRACKET, CHECKED OK. 2L72 4F A6WE 19951201002201995120100220NM 1995 12 1 9518916739 119951123A2930 HYD PRESS SW BOEING747 747251F 1384898NM NR 3 ENGINE FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01639US 23887 ANC-LCK - EN ROUTE, THE NR 3 ENGINE EDP/ADP PRESSURE LIGHT ILLUMINATED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND FLIGHT DIVERTED TO ORD. REPLACED THE NR 3 ENGINE DRIVEN PUMP LOW PRESSURE SWITCH AND CHECK WAS NORMAL. 2L74 4F A20WE 19951201002211995120100221WP 1995 12 1 9518929940 119951127A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL013322L 47031 DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FORWARD OF ROW 6 AND THE TWO EMERGENCY EXIT SIGNS BY THE MAIN CABIN DOOR AND SERVICE DOOR INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201002221995120100222WP 1995 12 1 9518939926 119951126A3350 BATTERY PACK DOUG DC9 DC932 3022066WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01926NW 47425 DURING LINE CHECK, FOUND CATWALK AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201002231995120100223WP 1995 12 1 9518949935 119951122A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL011331U 47404 DURING LINE CHECK, FOUND LEFT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201002241995120100224NM 1995 12 1 9518956309 119951123A3350 EEL PIN BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 TPE - DURING LINE CHECK, THE EMERGENCY PATH LIGHTS BETWEEN SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE PIN, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951201002251995120100225WP 1995 12 1 9518969968 119951121A801138334221 STARTER DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE LT ENGINE FAILED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019332 326032196 47138 666089 ON START, THE NR 1 ENGINE STARTER EXPERIENCED AN UNCONTAINED FAILURE. THE STARTER AND ADJACENT LINES AND DUCTS DAMAGED BY THE FAILURE WERE REPLACED WITH SERVICEABLE PARTS. 2L72 4F4 F A6WE E2EA 19951201002261995120100226WP 1995 12 1 9518979860 119951124A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN NOT SEATED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01769NC 47757 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. RESEATED BATTERIES AT AFT CABIN EMERGENCY LIGHTS, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201002271995120100227WP 1995 12 1 9518989152 119951123A3350 EEL WIRE DOUG DC9 DC914 3022034WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018911E 45825 THE EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE IN FORWARD CABIN AREA. REPAIRED SPLICE AT ROW 1, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951201002281995120100228NM 1995 12 1 9518992289 119951122A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE J WARNING INDICATION ININSP/MAINT 1 GL01289US 21377 DURING PREFLIGHT, FOUND THE RIGHT MIDDLE OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY, SYSTEM CHECKED OK. 2L73 4F A3WE 19951201002291995120100229NM 1995 12 1 9519002202 119951123A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01202US 22155 DURING PREFLIGHT, FOUND FORWARD EMERGENCY CABIN LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKED OK. 2L73 4F A3WE 19951201002301995120100230NE 1995 12 1 9519011146 219951123A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 2 ENGINE STALLED A NWAAAE UNSCHED LANDING ENGINE SHUTDOWN RM PARTIAL RPM/PWR LOSS OVER TEMP CRCRUISE 1 GL01146US 46755 686172 DURING CRUISE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL WITH THE EGT GOING TO MAX FOR 30 SECONDS. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED. NO FUEL WAS DUMPED. THE AIRCRAFT WAS FERRIED TO MSP WHERE THE ENGINE WAS REPLACED. 2L73 4F4 F A22WE E20EA 19951201002311995120100231WP 1995 12 1 9519029310 119951126A7331 FF TRANSMITTER DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01313RC 48091 708443 NR 2 ENGINE FUEL FLOW WAS 3,000 PPH GREATER IN CLIMB AND 1,000 PPH GREATER IN CRUISE THAN NR 1 ENIGNE. NR 2 ENGINE FUEL USEAGE WAS 1,000 LBS MORE ON LEVEL OFF WHEN CHECKED WITH THE FUEL QUANTITY SYSTEM. THE FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL FLOW TRANSMITTER, RUNUP AND LEAK CHECK WAS SATISFACTORY. 2L72 4F4 F A6WE E9NE 19951201002331995120100233NM 1995 12 1 9519042298 119951124A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01298US 22152 DURING PREFLIGHT, FOUND EMERGENCY EXIT SIGN OVER DOOR R2 INOPERATIVE. REPLACED THE BATTERY PACK, CHECKED OK. 2L73 4F A3WE 19951201002341995120100234NM 1995 12 1 95FDEA01803 119951127A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55. CUT AWAY CORRODED AREA FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8. 2L73 4F A3WE 19951201002351995120100235NM 1995 12 1 95FDEA01804 119951127A572069184741 CLIP BOEING727 72722C 138400FNM WS 760 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 WING TEE CLIP STA 760 RBL 665 HAS CORROSION. REMOVED CORRODED TEE CLIP, COLD WORKED HOLES PER EO 7-5710-7-2308 AND INSTALLED TEE CLIP. 2L73 4F A3WE 19951201002361995120100236NM 1995 12 1 95FDEA01805 119951127A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 600 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 STA 600 RBL 60 TO 41 WL 208.1 FLOORBEAM HAS CORROSION ON UPPER AND LWR LANDING. REMOVED TOP FLANGE OF FLOORBEAM RBL 44 TO 56 PER SRM 53-10-8 FIG 5 AND FABRICATED REPAIR AND INSTALLED PER SRM 53-10-8 FIG 5, 51-10-6 AND 51-10-1. 2L73 4F A3WE 19951201002371995120100237NM 1995 12 1 95FDEA01806 119951127A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 569 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 HEAVY CORROSION ON FLOORBEAM STA 560 LBL 0 TO 22. REMOVED CORROSION, FABRICATED REPAIR PIECES IAW 53-10-8, INSTALLED REPAIR PIECES, DOUBLER AND FASTENERS PER 53-10-8. 2L73 4F A3WE 19951201002381995120100238NM 1995 12 1 95FDEA01807 119951127A5320 FITTING BOEING727 72722C 138400FNM BS 870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 BS 870 LT TERMINAL FITTING LOWER HOLE NR 4 SHOWS CRACK WITH A HFEC AT STR 9 TO 10. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND DOUBLER IAW 727-53-0194 BOEING SB AND INSTALLED ON A/C PER BOEING SB 727-53-0194. 2L73 4F A3WE 19951201002391995120100239NM 1995 12 1 95FDEA01808 119951126A5311 FRAME BOEING727 72722C 138400FNM BS 804.5 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 BS 804.5 LT SIDE 23 ABOVE WL 208.1 STR 14 FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 51-40-3. 2L73 4F A3WE 19951201002401995120100240NM 1995 12 1 95FDEA01809 119951126A5320 FITTING BOEING727 72722C 138400FNM BS 740/870 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25112FE 19890 SEVERAL STR END FITTINGS AT STA 870 AND 740 CRACKED ON INNER LANDING STR 8R AND L MPN'S 69-16380-3 AND 69-34593-1. REMOVED AND REPLACED END FITTINGS PER STANDARD PRACTICE. 2L73 4F A3WE 19951201002411995120100241NM 1995 12 1 95FDEA01810 119951127A532065207264 THRESHOLD BOEING727 72722 1384002NM BS 524-576 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION UNDER NUTPLATES ON THRESHOLD STRAP, STA 524 TO 576 RBL 24 WL 156, FWD BAY. REPLACED STRAP FROM BS 520 TO 600 RBL 24 WL 156. 2L73 4F A3WE 19951201002421995120100242NM 1995 12 1 95FDEA01811 119951127A53156517593 FLOORBEAM BOEING727 72722 1384002NM BS 312 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 CORROSION (C53-224-02), AROUND NUTPLATE HOLES AT BS 312 LBL 2 TO 18 WL 208.1. REPAIRED CORRODED AREA AT BS 312 LBL 2 TO 18 WL 208.1 IAW FEDEX SRM 53-10-8. 2L73 4F A3WE 19951201002431995120100243NM 1995 12 1 95FDEA01812 119951123A5320 FORGING BOEING727 72722 1384002NM BS 740 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CRACKS ON STA 740 FORGING LT. THREE LOCATIONS BETWEEN STR 23 TO 24L, BETWEEN STR 18 TO 19L AND BETWEEN STR 19 TO 20L. REPAIRED DAMAGED AREAS PER FEDEX EA 7-5310-26123. 2L73 4F A3WE 19951201002441995120100244NM 1995 12 1 95FDEA01813 119951123A5320 SILL WEB BOEING727 72722 1384002NM BS 1070 BUCKLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND DOOR SILL WEB BUCKLED AT BS 1070 RBL 22 WL 152.5. UPON FURTHER INVESTIGATION OF DAMAGE DETERMINED THAT THIS REPAIR IS NOT ODR REPORTABLE PER FEDEX GMM SECTION. 2L73 4F A3WE 19951201002451995120100245NM 1995 12 1 95FDEA01814 119951123A5313 STRINGER BOEING727 72722 1384002NM BS 1105 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 FOUND CORROSION IN CHANNEL OF STR 28R RBL 14.5 WL 155 BS 1105. CUT OUT DAMAGE AND REPAIRED PER FEDEX SRM 53-10-03 FIG 1. 2L73 4F A3WE 19951201002461995120100246NM 1995 12 1 95FDEA01815 119951123A5311 FRAME BOEING727 72722 1384002NM BS 825.95 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25191FE 19084 DURING INSPECTION PER EO 7-5310-7-3367, A FREEZE PLUG WAS FOUND PREVIOUSLY INSTALLED IN A FASTENER HOLE AT WL 208.10, IN THE LT 825.95 FRAME WEB FLANGE AND REINFORCING CHORD. OLD FREEZE PLUG WAS FOUND DAMAGED. REMOVED OLD FREEZE PLUG, OVERSIZED HOLE AND INSTALLED NEW FREEZE PLUG AND NEW REINFORCING CHORD. CONTINUED ACCOMPLISHMENT OF FEDEX EO 7-5310-7-3367A PT 5. 2L73 4F A3WE 19951201002471995120100247WP 1995 12 1 95UAL900272 119951127A21213600760 COOLING FAN DOUG DC10 DC1010 3022110WP APU GEARBOX LEAKING A UALAO OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 WP291823U 46622 PUNGENT ODOR/SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. FOUND APU OIL CONTAMINATING SYSTEM. APU OIL QUANTITY DROPPED FROM 3 QTS TO 1.5 QTS. APU GEARBOX LEAKING OIL FROM COOLING FAN ASSEMBLY. REPLACED COOLING FAN. 2L73 4F A22WE 19951201002481995120100248NM 1995 12 1 95UAL900273 119951128A3350 BULB BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29184UA 25380 FLOOR EEL LIGHT SEGMENT INOP AT ROW 56C. REPLACED LAMP SEGMENT. 2L74 4F4 FRTA20WE E24NE 19951201002491995120100249WP 1995 12 1 ABXA9500936 119951121A2923AA19020 HYD PUMP NIHON YS11 YS11A500 6310416WP AUX HYD SYST FAILED A ABXAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL23913AX 844 2053 CREW REPORT, HEATER 'ON', NO HEAT. WENT OUTSIDE TO CHECK PLUG AND SAW SMOKE, CALLED MAINTENANCE. REMOVED PANEL AND SAW FIRE, AUXILIARY HYDRAULIC PUMP FOUND OVERHEATED AND WIRING ABOVE AUXILIARY PUMP BURNED. AUXILIARY HYDRAULIC PUMP REPLACED, OPS CHECKED GOOD, LEAK CHECKED GOOD. WIRING REPAIRED IAW YS-11 WDM, ALL SYSTEMS OPS CHECKED GOOD IAW YS-11 MM CHAPTER 27, 29.76 AND 80. 2L72 4T A1PC 19951201002501995120100250 1995 12 1 COMA9512012 419951124A34256226190204 AHRS COMPUTER EMB 120 EMB120RT SO NR 1 FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01162CA8466 4049 120150 NR 1 AHRS IS INOP. REPLACED THE NR 1 AHRS COMPUTER. 2L72 4T RTA31SO 19951201002511995120100251SO 1995 12 1 COMA9512013 119951127A5753PE610261 ROLLER EMB 120 EMB120RT SO LT TE FLAP WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01241CA 120211 FLAP DISAGREEMENT WARNING CLIMB. OUTBOARD FLAPS DID NOT RETRACT FULLY. REPLACED THE LT OUTBOARD FLAP ASSY ROLLERS. 2L72 4T RTA31SO 19951201002521995120100252SO 1995 12 1 COMA9512014 119951127A31508005579 AURAL WARN UNIT EMB 120 EMB120RT SO AVIONICS DEFECTIVE A COMAO OTHER N FALSE WARNING TOTAKEOFF 1 SO01152CA15814 120152 AURAL WARNING DURING TAKEOFF - TRIM FAIL AFTER TAKEOFF. REPLACED THE AURAL WARNING UNIT. 2L72 4T RTA31SO 19951201002531995120100253 1995 12 1 COMA9560608 419951126A22106229968001 ACTUATOR CNDAIRCL600 CL6002B19 EA NR 1 YAW DAMPER DEFECTIVE A COMAD RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 SO01938CA1414 819 7046 VIBRATION FELT IN LEFT RUDDER PEDAL WHEN NR 1 YAW DAMPER ENGAGED. REPLACED THE YAW DAMPER ACTUATOR. 2L72 4F RTA21EA 19951201002541995120100254EA 1995 12 1 COMA9560609 119951126A3260864806 PSEU CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAO OTHER N FALSE WARNING CRCRUISE 1 SO01931CA2879 31 7037 W.O.W. OUTPUT, W.O.W. INPUT, AND STALL FAIL MESSAGE CAME ON IN-FLIGHT. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT. 2L72 4F RTA21EA 19951201002551995120100255EA 1995 12 1 COMA9560610 119951123A2450V210D090BC RELAY CNDAIRCL600 CL6002B19 EA ESSENTIAL BUSS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01948CA499 7079 ESSENTIAL BUS CAUTION MESSAGE IS ON AND THE BUS IS FULLY POWERED. REPLACED THE BUS SENSE RELAY. 2L72 4F RTA21EA 19951201002561995120100256WP 1995 12 1 DHL9805005 119951123A324426014112 TIRES 26014112 DOUG DC8 DC873F 302199FWP NR 1/2 WHEELS FAILED A DHLAK NONE O OTHER LDLANDING 1 SO01805DH H1049 46125 SNN - NR 1 AND NR 2 MAIN TIRES BLEW ON LANDING. REMOVED AND REPLACED NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES IAW 32-40-0. 2L74 4F RT4A25 19951201002571995120100257NM 1995 12 1 DL72S954497 119951102A5753652163262 SPAR BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 DURING HMV INSP, NR 3 MIDFLAP WAS FOUND WITH AFT SPAR CHORD CRACKED AT I/B QUADRANT CUTOUT. REPAIRD PER MM 57-52-0 PAGE 807. 2L73 4F A3WE 19951201002581995120100258NM 1995 12 1 DL72S954498 119951102A5753652163262 DOUBLER BOEING727 727232 1384082NM NR 3 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 DURING HMV SHOP INSP, NR 3 MIDFLAP AFT SPAR CHORD DOUBLER CRACKED AT I/B AFT FLAP TRACK. REPAIRED PER MM 57-52-0 PAGE 807. 2L73 4F A3WE 19951201002591995120100259NM 1995 12 1 DL72W954490 119951126A56105717623134 WINDOW BOEING727 727247 138408FNM COCKPIT CRACKED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO272817W 20873 R2 WINDOW OUTER PANE CRACKED PASSING THROUGH 23,000 ON CLIMBOUT. REPLACED R2 WINDOW AND HEAT CONTROLLER. 2L73 4F A3WE 19951201002601995120100260NM 1995 12 1 DL757954538 119951113A5754114N3002120A TE WEDGE BOEING757 757232 1384965NM NR 6 LE FLAP BROKEN A DALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SO27619DL 22909 DURING CRUISE, HAD VIBRATION IN CABIN AT ROWS 23 TO 28. FOUND NR 6 L/E SLAT PANEL TRAILING EDGE WEDGE BROKEN OUT AND VIBRATING. ALSO, A SECTION APPROX 10 BY 20 WITH SURROUNDING HONEY COMB DAMAGED. REPLACED SLAT ASSEMBLY FOR RETURN TO SERVICE. 2L72 4F RTA2NM 19951201002611995120100261NM 1995 12 1 DL767954527 119951118A5754114T410518A SKIN BOEING767 767232 1385132NM NR 8 LE SLAT DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27113DA 22225 THE NR 8 L/E SLAT T/E WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. REPAIRED PER DL ERA 272443-14AD. 2L72 4F RTA1NM 19951201002621995120100262NM 1995 12 1 DL767954539 119951119A21216066223 FAN BOEING767 767232 1385132NM AC COMP FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27110DL 22222 DURING CRUISE, HAD ELECTRICAL BURNING ODOR IN CABIN. DEACTIVATED RECIRC FAN AND ODOR DISSIPATED. REPLACED RECIRC FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19951201002631995120100263NM 1995 12 1 DL76L954511 119951013A5415112T7041 FITTING BOEING767 767332 1382001NM RT PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT PYLON STRUT SUPPORT CENTER FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTING WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS. DAMAGE FROM LANDING GEAR COLLAPSE REPAIRED PER DL ERA 272109-14. 2L72 4F RTA1NM 19951201002641995120100264NM 1995 12 1 DL76L954515 119951013A5743 FITTING BOEING767 767332 1382001NM MLG DAMAGE A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 AFTER FAILURE OF THE MLG UPPER STRUT AT THE AFT TRUNNION, BAC RECOMMENDED INSPECTION AND REWORK OF THE MLG BEAM AND THE FORWARD AND AFT PLATES ARE BEING REPLACED. DL ERA 272107 DOCUMENTS THE REWORK OF THE MLG O/B SUPPORT FITTING LOWER HOLE. 2L72 4F RTA1NM 19951201002651995120100265NM 1995 12 1 DL76L954516 119951013A5415112T7006112T7007FITTINGS BOEING767 767332 1382001NM RT PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT PYLON STRUT SUPPORT UPPER LINK FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTINGS WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS, PER DL ERA 272106-14. 2L72 4F RTA1NM 19951201002661995120100266NM 1995 12 1 DL76L954517 119951013A5415112T7003112T7004FITTINGS BOEING767 767332 1382001NM RT PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT PYLON MID SPAR SUPPORT FITTING BUSHINGS WERE FOUND DAMAGED, REQUIRING REPLACEMENT. THE FITTINGS WILL BE REWORKED TO ACCEPT OVERSIZE BUSHINGS, PER DL ERA 272105-14. 2L72 4F RTA1NM 19951201002671995120100267NM 1995 12 1 DL76L954518 119951013A5415112T7004 FITTING BOEING767 767332 1382001NM RT PYLON GOUGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 RT WING I/B MID SPAR STRUT SUPPORT FITTING WAS GOUGED IN THREE PLACES. THE LEADING EDGE OF THE LUG IN THE TRANSITION AREA TO THE WING SKIN ATTACH FLANGE WAS GOUGED APPROX 18 INCHES DEEP ACROSS THE LUG THICKNESS. ALSO, TWO SMALL GOUGES APPROX .15 INCH IN DIAMETER WERE FOUND ON THE I/B WING SKIN ATTACH FLANGE AND ARE APPROX 0.030 DEEP. REPAIRED PER DL ERA 272103-14. 2L72 4F RTA1NM 19951201002681995120100268NM 1995 12 1 DL76L954519 119951028A5730 SKIN BOEING767 767332 1382001NM WS 306 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT UPPER WING SKIN WAS DENTED DOWN AND GOUGED JUST AFT OF THE REAR SPAR AT WING STA 306. REPAIRED PER DL ERA 272100-14. 2L72 4F RTA1NM 19951201002691995120100269NM 1995 12 1 DL76L954520 119951028A5730 SKIN BOEING767 767332 1382001NM RT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 DURING INSTALLATION OF THE NEW DIAGONAL BRACE ATTACH FITTING, MOST HOLES IN THE FITTING WERE DRILLED TO WING HOLE SIZE, COLD WORKED AND THEN THE WING SKIN AND FITTING TOGETHER WERE OVERSIZED BY .0156 INCH AS AN INSURANCE CUT. FIVE HOLES WERE OVERSIZED TO ELIMINATE DAMAGE DURING DRILLING OPERATIONS, PER DL ERA 272114-14. 2L72 4F RTA1NM 19951201002701995120100270NM 1995 12 1 DL76L954521 119951028A5730 SKIN BOEING767 767332 1382001NM WS 377 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT LOWER WING SKIN LIP WAS DENTED UP AND GOUGED AT LE STA 377. THE COLLINEAR GOUGES ARE IMMEDIATELY AFT OF THE DEEPEST DENTED REGION. REPAIRED PER DL ERA 272102-14. 2L72 4F RTA1NM 19951201002711995120100271NM 1995 12 1 DL76L954522 119951028A5743 TRUNNION BOEING767 767332 1382001NM RT WING OVERSIZE HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 DURING INSTALLATION OF NEW I/B FWD TRUNNION ATTACH FITTING, SOME FASTENERS REQUIRED OVERSIZING TO ALIGN THE EXISTING HOLES IN THE REAR SPAR WITH THE NEW HOLES IN THE FITTING, PER DL ERA 272115-14. 2L72 4F RTA1NM 19951201002721995120100272NM 1995 12 1 DL76L954523 119951028A5743 TRUNNION BOEING767 767332 1382001NM RT WING OVERSIZE HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 DURING INSTALLATION OF NEW O/B FWD TRUNNION ATTACH FITTING, SOME FASTENERS REQUIRED OVERSIZING TO ALIGN THE EXISTING HOLES IN THE REAR SPAR WITH THE NEW HOLES IN THE FITTING, PER DL ERA 272119-14. 2L72 4F RTA1NM 19951201002731995120100273NM 1995 12 1 DL76L954524 119951028A5720 LE SKIN BOEING767 767332 1382001NM WS 416.20 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE RT WING L/E ASSY AT THE NACELLE STRUT AND AT LE STA 416.20 REQUIRES REPLACEMENT. THIS ER/A PROVIDES THE PART NUMBERS FOR INSTALLATION ON THIS A/C, DL ERA 272108-14. 2L72 4F RTA1NM 19951201002741995120100274NM 1995 12 1 DL76L954525 119951028A5720 STRUCTURE BOEING767 767332 1382001NM WS 372 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE WING TRAILING EDGE UPPER AND LOWER PANELS AND SUPPORT STRUCTURE REQUIRE REPLACEMENT FROM APPROX WBL 98 TO WS 372. REPAIRED PER DL ERA 272104-14. 2L72 4F RTA1NM 19951201002751995120100275NM 1995 12 1 DL76L954526 119951026A5400 FAIRING BOEING767 767332 1382001NM RT PYLON DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27172DN 24775 THE NR 2 PYLON SAILBOAT FAIRING IS DAMAGED REQUIRING REPLACEMENT. DL ERA 272101-14 DOCUMENTS PARTS REPLACEMENT INFORMATION. 2L72 4F RTA1NM 19951201002761995120100276WP 1995 12 1 DLL10954500 119951026A5712 RIB TABS LKHEED1011 10113851 5265010WP WS 503/529 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27718DA 193C1097 THE RT/LT WINGS IWS 503 AND IWS 529 RIB UPPER/LWR CAP ATTACH TABS ARE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD. 2L73 4F A23WE 19951201002771995120100277WP 1995 12 1 DLL10954501 119951031A53201517032101 DOOR FRAME LKHEED1011 10113851 5265010WP FS 829 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27728DA 193C1173 THE FS 829 DOOR FRAME HAD CORROSION DAMAGE AT THE FWD FLANGE JUST O/B OF THE SILL. ALSO, THE FS 829 FRAME SUSTAINED CORROSION DAMAGE TO THE WEB JUST O/B OF THE SILL TENSION FITTING. ACCOMPLISHED REPAIRS PER DL ERA 272242-14. 2L73 4F A23WE 19951201002781995120100278WP 1995 12 1 DLL10954503 119950714A53121505220 BLKHD WEB LKHEED1011 10113851 5265010WP BS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO271732D 193C1213 A CRACK WAS FOUND IN THE FS 1363 BULKHEAD WEB AND LOWER CAP, LOCATED BETWEEN STR 18 AND 19, EXTENDS DIAGONALLY I/B. REPAIRED PER DL ERA 271398-14. 2L73 4F A23WE 19951201002791995120100279WP 1995 12 1 DLL10954504 119950714A53121505220 BLKHD WEB LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO271731D 193C1200 A CRACK WAS FOUND IN THE FS 1363 BULKHEAD WEB AND LOWER CAP, LOCATED BETWEEN STR 47 AND 48. REPAIRED PER DL ERA 271397-14. 2L73 4F A23WE 19951201002801995120100280WP 1995 12 1 DLL10954506 119951023A5510 STRUCTURE LKHEED1011 10113851 5265010WP HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA-H LE 332.7 TO 455.2. THE DAMAGE CONSISTS OF CRACKED SKIN PANELS, CRACKED UPPER AND LWR AUXILIARY SPARS AND CRACKED RIBS ALONG WITH ATTACHED BRACES. ERA 272205 WILL AUTHORIZE INSTALLATION OF THE ALTERNATE CONFIGURATION AND PROVIDE OVERALL INSTRUCTION FOR THE MODIFICATIONS REQUIRED, REPAIRED PER. 2L73 4F A23WE 19951201002811995120100281WP 1995 12 1 DLL10954507 119951102A55111532177 AUX SPARS LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZONTAL STABILIZER L/E AUXILIARY SPARS WERE FOUND WITH NUMEROUS CRACKS. THE CRACKS ARE LOCATED ON BOTH THE UPPER AND LOWER CAPS. SPLICED IN NEW SECTION OF CAP ON BOTH SPARS PER DL ERA 272186-14. 2L73 4F A23WE 19951201002821995120100282WP 1995 12 1 DLL10954508 119951102A55111524299 RIB LKHEED1011 10113851 5265010WP RT HORIZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZ STAB L/E INTERMEDIATE RIB LOCATED AT 'H' LE 414.405 WAS FOUND CRACKED. THE CRACK WAS LOCATED IN THE UPPER FLANGE RADUIS OF THE UPPER CAP ON THE AFT END OF THE RIB WHERE IT ATTACHES TO THE FRONT SPAR FORWARD FLANGE. REPAIRED PER DL ERA 272209-14. 2L73 4F A23WE 19951201002831995120100283WP 1995 12 1 DLL10954509 119951025A55121524245143146 SKIN LKHEED1011 10113851 5265010WP RT HORIZ STAB LECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. REPAIRED PER DL ERA 272226-14. 2L73 4F A23WE 19951201002841995120100284WP 1995 12 1 DLL10954510 119951102A5512 SKIN LKHEED1011 10113851 5265010WP RT HORIZ STAB LECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BET STA-H LE 332.7 TO 455.2. A REPLACEMENT FROM A/C 781 IS BEING SPLICED IN. AS A RESULT OF THE DIFFERENT CONFIGURATION RIBS AT 'H' LE 332.7 AND 455.2 AND REPLACEMENT AUX SPAR CAP SECTIONS BEING INSTALLED ON THIS A/C, TWO ATTACHMENT HOLE PATTERNS DO NOT MATCH. AN EXTERNAL SPLICE REPAIR WAS INSTALLED PER DL ERA 272236-14. 2L73 4F A23WE 19951201002851995120100285WP 1995 12 1 DLL10954514 119951102A551215240421532181 SKIN LKHEED1011 10113851 5265010WP RT HORIZ STAB LECRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 THE RT HORIZ STAB L/E WAS FOUND WITH EXTENSIVE DAMAGE FWD OF THE FRONT SPAR BETWEEN STA 'H' LE 332.7 TO 455.2. ACCOMPLISHED REPAIRS PER DL ERA 272204-14. 2L73 4F A23WE 19951201002861995120100286WP 1995 12 1 DLL10954528 119950903A53121554947102 BLKHD FITTING LKHEED1011 10113851 5265010WP AFT PRESS DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27713DA 193C1089 DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STR SPLICE FITTINGS PER SI 7-66332-12, THE STR 4 AND 8 FITTING WERE FOUND TO BE CRACKED. REPAIRED PER DL ERA 271738-14AD. 2L73 4F A23WE 19951201002871995120100287WP 1995 12 1 DLL10954530 119950901A53121554950102101 BLKHD FITTING LKHEED1011 10113851 5265010WP AFT PRESS DOME CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27723DA 193C1150 DURING ACCOMPLISHMENT OF AN INSPECTION OF THE AFT PRESSURE BULKHEAD STR SPLICE FITTINGS PER SI 7-66332-12, THE STR 8 AND 58 FITTINGS WERE FOUND TO BE CRACKED AND COMPLETELY SEVERED. REPAIRED PER DL ERA 272751-14AD. 2L73 4F A23WE 19951201002881995120100288WP 1995 12 1 DLL16954502 119951104A5312 BLKHD CAP LKHEED1011 10113853 5265020WP FS 449 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27762DA 193Y1210 THE STA 449 BULKHEAD CAP WAS FOUND WITH A 7 INCH LONG CRACK IN ITS BEND RADIUS AT RBL 90.70. REPAIRED PER DL ERA 272084-14. 2L73 4F A23WE 19951201002891995120100289WP 1995 12 1 DLL16954505 119951019A5330 SKIN LKHEED1011 10113853 5265020WP FS 1545/1565 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27762DA 193Y1210 THE FUSELAGE SKIN BET FS 1545, FS 1565 AND AT STR 36 WAS CORRODED AND GROUND BEYOND LIMITS. REPAIRED PER DL ERA 272061-14. 2L73 4F A23WE 19951201002901995120100290WP 1995 12 1 DLL16954533 119951019A53301608988101 SKIN LKHEED1011 10113853 5265020WP BS 1423-1453 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27762DA 193Y1210 THE FUSELAGE SKIN PANEL WAS CUT TO REMOVE CORROSION FROM STA 1423 TO 1453 AT STR 35. REPAIRED PER DL ERA 272098-14. 2L73 4F A23WE 19951201002911995120100291NM 1995 12 1 DLM88954532 119951122A5330 SKIN DOUG MD88 MD88 3023688NM FS 484 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27976DL 53257 THE FUSELAGE SKIN AT FS 484 BETWEEN STR 27 AND 28R WAS DAMAGED REQUIRING A CUTOUT MEASURING APPROX 3 INCH BY 4.5 INCH. ACCOMPLISHED REPAIRS PER DL ERA 27245-14. 2L72 4F RTA6WE 19951201002921995120100292WP 1995 12 1 MWEA95434 119951122A2520502745E1023 SEAT BELT DOUG DC9 DC932 3022066WP PAX COMPT BROKEN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31204ME 47680 DURING AN INTERIOR EQUIPMENT CHECK, A SEAT BELT BUCKLE ON A PASSENGER SEAT FELL OFF OF THE STRAP. MAINTENANCE REPLACED THE SEAT BELT ASSY AND OPERATIONALLY CHECKED IT OK FOR SERVICE. 2L72 4F A6WE 19951201002931995120100293WP 1995 12 1 MWEA95435 119951128A24222655000601 AC INVERTER DOUG DC9 DC932 3022066WP FWD ACCESS COMPTINOPERATIVE A MWEAO OTHER J WARNING INDICATION NRNOT REPORTED 1 GL31202ME 47672 WHEN EMERGENCY POWER IS TURNED ON, AC EMERGENCY BUS OFF LIGHT ILLUMINATED AND AC EMERGENCY BUS IS NOT POWERED. REMOVED AND REPLACED EMERGENCY POWER. 2L72 4F A6WE 19951201002941995120100294NM 1995 12 1 P5CA9500848 119951127A326069B475307 A-12 CARD BOEING747 747124 1384874NM LOGIC MODULE INOPERATIVE A P5CAO OTHER N FALSE WARNING DEDESCENT 1 WP23855FT 19733 DURING LANDING APPROACH WITH FLAPS AT 25 DEGREES AND GEAR DOWN, WARNING HORN SOUNDED AND COULD NOT SILENCE WARNING HORN. FOUND A-12 CARD IN PRIMARY LANDING GEAR LOGIC MODULE INOP. REPLACED A-12 CARD IAW MM 32-61-14, OPS CHECKS GOOD. 2L74 4F A20WE 19951201002951995120100295NM 1995 12 1 SCNA95277 119951126A278010608197 SWITCH BOEING727 7272J4 1384006NM NR 1 LE FLAP DIRTY A SCNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15288SC 20765 THE NUMBER ONE LEADING EDGE FLAP FAILED TO RETRACT AFTER TAKEOFF, AIRCRAFT RETURNED TO BASE. THE NUMBER ONE LEADING EDGE FLAP POSITION SWITCH AND ACTUATOR CANNON PLUG WERE CLEANED. PERFORMED ADJUSTMENT\TEST PER BOEING MAINTENANCE MANUAL AND FLAP TESTED GOOD. 2L73 4F RTA3WE 19951201002961995120100296SO 1995 12 1 SWIA95684 119951117A2720 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RUDDER CONTL WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07224SW 120294 RT RUDDER OUTBOARD AFT SECTION OF CABLE WORN. REPLACED RT RUDDER OUTBOARD AFT CABLE PER MM 27-00-01. 2L72 4T4 TRTA31SO E20NE 19951201002971995120100297SO 1995 12 1 SWIA95685 119951117A2710 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT AILERON WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07224SW 120294 LT AILERON CABLE OUTBOARD OF NACELLE IS WORN. REPLACED BOTH AILERON CABLES FOR LT AILERON. 2L72 4T4 TRTA31SO E20NE 19951201003241995120100324SO 1995 12 1 FFSA95001 119951031A8120557369 CLAMP GARRTT LW1246375 PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA TURBO V-BAND MISSING A AFFSAE ENGINE SHUTDOWN A FLAME/FIRE CLCLIMB 1 AL017164D1547 XG019091 318052013 L184768A AIRCRAFT WAS CLIMBING THROUGH APPROXIMATELY 7,000 FEET, PILOT HEARD A MUFFLED SOUND FROM RIGHT ENGINE AND NOTICED FLAMES BURNING THROUGH THE TOP OF ENGINE COWLING. PILOT SHUT DOWN ENGINE. V-BAND CLAMP FROM TURBOCHARGER MALFUNCTIONED AND EXHAUST MANIFOLD BECAME DETACHED FROM TURBOCHARGER. (CLAMP MISSING.) (X) 1L72 3O3 O A20SO E14EA 19951201003251995120100325WP 1995 12 1 95ZZZX6425A 119951113A324226088921 BRAKE ASSY DOUG DC9 DC982 3022082WP NR 3 MLG WHEEL WORN A ASAAK NONE O OTHER LDLANDING 1 NM01935AS 49236 LAX - FLT 256 - AFTER ARRIVAL, CREW REPORTED THE BRAKES FADED DURING LANDING ROLL-OUT AND TAXI. REPLACED NR 1 AND NR 3 BRAKE ASSEMBLIES AND BLED NR 2 AND NR 4 BRAKE HYDRAULIC SYSTEMS. TAC: 02066. REFERENCE, OPERATOR CONTROL NR ASAA9580270. (X) 2L72 4F A6WE 19951201003271995120100327WP 1995 12 1 AASA9580241 119951018A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP BS 1309-1322 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS14681 53021 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL AT Y1309 TO Y1322, X17, Z42. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, SRM 51-20-00, SRM 51-30-02, SRM 53-24-00, AND SRM 53-01. TAC: 8795. (X) 2L72 4F RTA6WE 19951201003281995120100328NM 1995 12 1 ASAA9510103 119951106A33506013211 BATTERY BOEING737 737210C 1384459NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 ANC - DURING MAINTENANCE CHECK, THE FORWARD RIGHT EMERGENCY EXIT SLIDE LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (X) 2L72 4F A16WE 19951201003291995120100329NM 1995 12 1 ASAA9510104 119951107A33508821004 BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT THE LAST ROW IN CABIN. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003301995120100330NM 1995 12 1 ASAA9510105 119951111A3350883200312 BATTERY BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 SEA - DURING MAINTENANCE CHECK, THE AFT SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WAS FOUND INOPERATIVE. REPLACED REMOTE FLOOR PROXIMITY LIGHT ASSEMBLY AND BATTERY; LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003311995120100331NM 1995 12 1 ASAA9510106 119951112A33501060091102 EEL ASSY BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 SEA - DURING MAINTENANCE CHECK, THE AFT AIRSTAIR DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2L72 4F A16WE 19951201003321995120100332NM 1995 12 1 ASAA9510107 119951114A33501060091102 EEL ASSY BOEING737 7372X6C 1384552NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003331995120100333NM 1995 12 1 ASAA9540079 119951104A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 SEA - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003341995120100334NM 1995 12 1 ASAA9540080 119951106A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 JNU - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003351995120100335NM 1995 12 1 ASAA9540081 119951106A3230BACC18Z3R CIRCUIT BREAKER BOEING737 7374Q8 NM LANDING GEAR TRIPPED A ASAAO OTHER O OTHER TOTAKEOFF 1 NM01754AS 25095 SFO - FLT 88 - ON ARRIVAL, CREW REPORTED UNABLE TO MOVE GEAR HANDLE TO THE 'UP' POSITION AFTER TAKEOFF SEA. USED OVERRIDE TO RAISE THE HANDLE. NOTED LANDING GEAR 'LATCH AND PRESS WARN' CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER, CYCLED GEAR AND ALL SYSTEMS OPERATED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER AS PRECAUTIONARY. PERFORMED LANDING GEAR EXTENSION AND RETRACTION SEVERAL TIMES AND OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003361995120100336NM 1995 12 1 ASAA9540082 119951107A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003371995120100337NM 1995 12 1 ASAA9540083 119951107A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01780AS 25112 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 20-25 WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003381995120100338NM 1995 12 1 ASAA9540084 119951108A335010617838 EEL ASSY BOEING737 737490 1384715NM CABIN BROKEN A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01768AS 27082 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT THE L-2 DOOR WAS FOUND BROKEN. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003391995120100339NM 1995 12 1 ASAA9540085 119951109A3350 EEL WIRING BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE FORWARD 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON FORWARD TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003401995120100340NM 1995 12 1 ASAA9540086 119951108A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING ON AFT TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003411995120100341NM 1995 12 1 ASAA9540087 119951111A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 25 AFT. RECONNECTED WIRING AT ROW 25 AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003421995120100342NM 1995 12 1 ASAA9540088 119951111A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01773AS 25106 JNU - DURING MAINTENANCE CHECK, 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROW 16. RECONNECTED WIRING AT ROW 16 AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003431995120100343NM 1995 12 1 ASAA9540089 119951112A3350 EEL WIRING BOEING737 7374Q8 NM AFT GALLEY DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - FLT 625 - THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AT AFT GALLEY NR 3 AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003441995120100344NM 1995 12 1 ASAA9540090 119951114A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 26 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003451995120100345NM 1995 12 1 ASAA9540091 119951114A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 JNU - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003461995120100346NM 1995 12 1 ASAA9540092 119951115A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15 THROUGH 17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003471995120100347NM 1995 12 1 ASAA9540093 119951115A3350 EEL WIRING BOEING737 7374Q8 NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19951201003481995120100348WP 1995 12 1 ASAA9580236 119951018A5320 SHEAR TIE DOUG DC9 DC982 3022082WP BS 1287 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1287, LONGERON 28R TO LONGERON 29L. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-30-02, SRM 51-30-03, AND ARM 53-03. TAC: 23488. (X) 2L72 4F A6WE 19951201003491995120100349WP 1995 12 1 ASAA9580237 119951018A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP BS 1290-1310 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CRACK WAS FOUND ON INTERCOSTAL AT Y1290 TO Y1310, X0, Z0 TO Z6. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, SRM 51-30-01, SRM 51-30-02, AND SRM 53-14-03. TAC: 23488. (X) 2L72 4F A6WE 19951201003501995120100350WP 1995 12 1 ASAA9580238 119951018A575339542731 BOLT DOUG DC9 DC982 3022082WP LT TE FLAP CRACKED A AASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, MOUNTING BOLT WAS FOUND CRACKED IN THE LT INBOARD FLAP OUTBOARD HINGE, BOLT HEAD BROKE OFF WHEN TORQUE APPLIED. REPLACED BOLT IAW DC-9, MM 27-51-01. TAC: 23488. (X) 2L72 4F A6WE 19951201003511995120100351WP 1995 12 1 ASAA9580239 119951018A575342121811 MOUNTING LUG DOUG DC9 DC982 3022082WP RT TE FLAP VANE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CRACK WAS FOUND ON THE OUTBOARD MOUNTING LUG ON THE RT INBOARD FLAP VANE. REPLACED MOUNTING LUG IAW DC-9, MM 27-50-01. TAC: 23488. (X) 2L72 4F A6WE 19951201003521995120100352WP 1995 12 1 ASAA9580240 119951018A5320 SHEAR TIE DOUG DC9 DC983 3022083WP BS 1021 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS4681 53021 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1021, X6, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-01 AND SRM 53-03. (X) 2L72 4F RTA6WE 19951201003531995120100353WP 1995 12 1 ASAA9580243 119951020A5320 SHEAR TIE DOUG DC9 DC983 3022083WP BS 1212 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS14681 53021 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1212, X2 TO X7, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-02, SRM 51-10-03, SRM 51-10-04, SRM 51-30-02, AND SRM 53-14-03. TAC: 8795. (X) 2L72 4F RTA6WE 19951201003541995120100354WP 1995 12 1 ASAA9580244 119951020A524049376951 BOLT DOUG DC9 DC983 3022083WP L2 DOOR BROKEN A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01943AS 53018 PHX - FLT 94 - ON ARRIVAL, CREW REPORTED THE L2 DOOR HANDLE RETAINER BOLT BROKEN. REPLACED BOLT AND OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19951201003551995120100355WP 1995 12 1 ASAA9580245 119951023A5210 DOOR SEAL DOUG DC9 DC982 3022082WP L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. LUBED DOOR SEAL AND OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003561995120100356WP 1995 12 1 ASAA9580248 119951027A5330 SKIN DOUG DC9 DC983 3022083WP BS 1164 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS14681 53021 PAE - DURING A 15K CHECK, CORROSION WAS FOUND ON SKIN AT Y1164, X3, Z50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA E.A. 5330-01212. TAC: 8795. (X) 2L72 4F RTA6WE 19951201003571995120100357WP 1995 12 1 ASAA9580249 119951027A5320 INTERCOSTAL DOUG DC9 DC983 3022083WP BS 769-786.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01948AS 53021 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL AT Y769 TO Y786.5, X16, Z46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-02, SRM 53-10-03, AND SRM 53-01. (X) 2L72 4F RTA6WE 19951201003581995120100358WP 1995 12 1 ASAA9580250 119951030A57549955845503 FITTING DOUG DC9 DC982 3022082WP NR 4 LE SLAT CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01955AS46963 48080 OAK - DURING C-CHECK, CRACK WAS FOUND ON NR 2 L/E SLAT LT OUTBOARD FITTING. REPLACED FITTING IAW DOUGLAS DRAWING 5922534. TAC: 24866.(X) 2L72 4F A6WE 19951201003591995120100359WP 1995 12 1 ASAA9580251 119951031A5210 DOOR LINK DOUG DC9 DC982 3022082WP L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01956AS 48079 SAN - FLT 9000 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE AND LATCH. RESET L1 DOOR LINK AND CYCLED DOOR AND OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003601995120100360WP 1995 12 1 ASAA9580252 119951101A575339542731 BOLT DOUG DC9 DC982 3022082WP RT TE FLAPS BROKEN A AASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, MOUNTING BOLT HEAD WAS FOUND BROKEN OFF IN THE RT INBOARD FLAP OUTBOARD HINGE. REPLACED BOLT IAW DC-9, SRM 51-30-01. TAC: 22728. (X) 2L72 4F A6WE 19951201003611995120100361WP 1995 12 1 ASAA9580253 119951101A5320 WEB DOUG DC9 DC982 3022082WP BS 1176 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON L2 WEB AT Y1176, X49 TO X54. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA E.A. 5320-01203. TAC: 22728. (X) 2L72 4F A6WE 19951201003621995120100362WP 1995 12 1 ASAA9580254 119951101A5320S3932140 SUPPORT DOUG DC9 DC982 3022082WP BS 200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CHANNEL SUPPORTS AT Y200, X6, AND X8, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-30-01, AND SRM 51-01. TAC: 22728. (X) 2L72 4F A6WE 19951201003631995120100363WP 1995 12 1 ASAA9580255 119951101A53209936535507 FLOOR SUPPORT DOUG DC9 DC982 3022082WP BS 206.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y206.5, X14, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03 AND SRM 51-30-02. TAC: 22728 (X) 2L72 4F A6WE 19951201003641995120100364WP 1995 12 1 ASAA9580256 119951101A53205936797535 SUPPORT DOUG DC9 DC982 3022082WP BS 1117 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y1117, X20, Z47. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, SRM 51-20-00, SRM 51-30-02, AND SRM 53-14-03. TAC: 22728. (X) 2L72 4F A6WE 19951201003651995120100365WP 1995 12 1 ASAA9580257 119951101A5320S2929169 SUPPORT DOUG DC9 DC982 3022082WP BS 1155 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y1155, X27 TO X41, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, SRM 51-30-02, SRM 51-30-05, AND SRM 53-14-03. TAC: 22728. (X) 2L72 4F A6WE 19951201003661995120100366WP 1995 12 1 ASAA9580258 119951101A53206015609 GALLEY MOUNT DOUG DC9 DC982 3022082WP BS 1148 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON GALLEY MOUNT AT Y1148, X0, Z0.5. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, AND SRM 53-14-03. TAC: 22728. (X) 2L72 4F A6WE 19951201003671995120100367WP 1995 12 1 ASAA9580260 119951103A5315 FLOOR BEAM DOUG DC9 DC982 3022082WP BS 1338 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR BEAM AT Y1338, X25 TO X32, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 53-05. TAC: 22728. (X) 2L72 4F A6WE 19951201003681995120100368WP 1995 12 1 ASAA9580261 119951103A5320 ANGLES DOUG DC9 DC982 3022082WP BS 1143-1167 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON DRAIN PAN ATTACH ANGLES AT Y1143 TO Y1167, X59, Z1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03, AND SRM 51-30-02. TAC: 22728. (X) 2L72 4F A6WE 19951201003691995120100369WP 1995 12 1 ASAA9580262 119951103A5320 STRAP DOUG DC9 DC982 3022082WP BS 1218 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON STRAP AT Y1218, X2 TO X21, Z45. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03 AND SRM 51-30-05, SRM 53-14-03, AND SRM 53-01. TAC: 22728. (X) 2L72 4F A6WE 19951201003701995120100370WP 1995 12 1 ASAA9580263 119951104A5347TMS6019609 CARGO TRACK DOUG DC9 DC982 3022082WP BS 480-636 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS39018 49111 PAE - DURNG 15K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y480 TO Y636, X15, Z46. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-04, SRM 51-30-00, SRM 51-30-01, AND SRM 51-30-02. TAC: 22728. (X) 2L72 4F A6WE 19951201003711995120100371WP 1995 12 1 ASAA9580264 119951106A3350S103 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01967AS 49103 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003721995120100372WP 1995 12 1 ASAA9580265 119951107A3350S103 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01933AS 49234 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003731995120100373WP 1995 12 1 ASAA9580266 119951108A3350S103 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003741995120100374WP 1995 12 1 ASAA9580267 119951109A3350 EEL WIRING DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01930AS 49231 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS ABOVE THE L1 DOOR AND COCKPIT DOOR WOULD NOT TURN OFF. REPAIRED WIRING AT FORWARD FLIGHT ATTENDANT PANEL AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003751995120100375WP 1995 12 1 ASAA9580268 119951110A3350S103 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01945AS 49643 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19951201003761995120100376WP 1995 12 1 ASAA9580269 119951111A3350 EEL WIRING DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 29 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN TRACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19951201003771995120100377WP 1995 12 1 ASAA9580270 119951113A324226088921 BRAKE ASSY DOUG DC9 DC982 3022082WP NR 1 MLG WHEEL WORN A ASAAK NONE O OTHER LDLANDING 1 NM01935AS 49236 LAX - FLT 256 - AFTER ARRIVAL, CREW REPORTED THE BRAKES FADED DURING LANDING ROLL-OUT AND TAXI. REPLACED NR 1 AND NR 3 BRAKE ASSEMBLIES AND BLED NR 2 AND NR 4 BRAKE HYDRAULIC SYSTEMS. TAC: 06465. REFERENCE, OPERATOR CONTROL NR 95ZZZX6425A. (X) 2L72 4F A6WE 19951201003781995120100378WP 1995 12 1 ASAA9580271 119951116A3350S103 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01935AS 49236 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F A6WE 19951201003791995120100379WP 1995 12 1 ASAA9580272 119951116A3350 EEL WIRING DOUG DC9 DC983 3022083WP CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01943AS 53018 SEA - DURING MAINTENANCE CHECK, THE EMRGENCY FLOOR TRACK LIGHTS FROM ROWS 25 TO 29 WERE FOUND INOPERATIVE. RECONNECTED WIRING IN TRACK AT ROW 25 AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19951201003801995120100380EU 1995 12 1 SIMA953111 119951107A33506013211 EEL POWER SUPPLY SAAB SF340 340B 7860101EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21586MA15898 2001 340B165 DFW - FLT 3899 - EMERGENCY LIGHTS FOUND INOPERATIVE DURING PRE-FLIGHT INSPECTION. REMOVED AND INSPECTED SUPPLIES 20 LN, 21 LN, AND 22 LN. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 17442. (X) 2L72 4T RTA52EU 19951201003811995120100381WP 1995 12 1 VRZA96023 219951102A7320 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE3311 01514WP LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27472UE 823 IAD/RDG - FLT 6346 - DURING TAKEOFF AT 0905 HRS ON 11-9-95, ABORTED TAKEOFF DUE TO LT PROP RPM ONLY REACHED 99 PERCENT. AIRCRAFT RETURNED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED 'X' SCREW. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E3WE 19951201003821995120100382EU 1995 12 1 VTZA96024 119951109A243029529 SENSOR UNIT BAG JETSTMJETSTM3201 1500217EU LT GENERATOR FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27494UE 810 IAD/SWF - FLT 6351 - DURING CLIMB-OUT AT 1300 HRS ON 11-9-95, RETURNED TO IAD DUE TO AMP SPLIT, LT 50 AMPS, RT 100 AMPS; 40 AMPS ALLOWABLE IN ARM. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED BROKEN SENSING UNIT ON LT GENERATOR. (X) 2L72 4T RTA56EU 19951201003831995120100383EU 1995 12 1 VTZA96025 119951110A2910137311D1443 HYDRAULIC LINE BAG JETSTMJETSTM3201 1500217EU FUSELAGE BROKEN A VTZAAB UNSCHED LANDING EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27496UE 900 ROC/IAD - FLT 6412 - DURING CRUISE AT 1730 HRS ON 11-10-95, DECLARED AN EMERGENCY AND RETURNED TO IAD DUE TO A DUAL HYDRAULIC SYSTEM FAILURE. FLIGHT CREW HAD TO USE EMERGENCY HAND PUMP TO EXTEND LANDING GEAR. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND A HYDRAULIC LINE BROKEN ABOVE THE BAGGAGE POD. REPLACED LINE AND OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19951201003841995120100384NE 1995 12 1 VTZA96026 219951110A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT FAILED A VTZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA27306UE 4001 41020 P75009 IAD/RDU - FLT 6590 - DURING CRUISE, DECLARED AN EMERGENCY AND DIVERTED TO LYH DUE TO THE LT ENGINE OIL PRESSURE LOSS. FLIGHT CREW SHUT DOWN THE LT ENGINE AND LANDED AT LYH WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED AN ENGINE CHANGE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. PART TSI: 521.3. (X) 2L72 4T4 TRTA41NM E18NE 19951201003851995120100385WP 1995 12 1 9519059946 119950713A5312 BLKHD WEB DOUG DC9 DC931 3022065WP FS 604 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 604 BULKHEAD WEB LOWER AFT EDGE. REPAIRED WEB (P/N 5914865-23), PER EA 99-92255. 2L72 4F A6WE 19951201003861995120100386WP 1995 12 1 9519069925 119950811A5400 ANGLE DOUG DC9 DC932 3022066WP FS 1019 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01925US 47472 DURING LINE CHECK, FOUND A CRACK IN THE RIGHT PYLON LOWER ATTACH ANGLE AT FS 1019. REPAIRED PER EA 99-98960. 2L72 4F A6WE 19951201003871995120100387WP 1995 12 1 9519079946 119950905A5511 SPAR WEB DOUG DC9 DC931 3022065WP HORIZ STAB CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE HORIZONTAL STABILIZER REAR SPAR WEB AT STA 104. REPAIRED WEB (P/N 9918401-103), PER EA 99-102688. 2L72 4F A6WE 19951201003881995120100388WP 1995 12 1 9519089946 119950930A5320 ANGLE DOUG DC9 DC931 3022065WP FS 43 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE NOSE GEAR FORWARD LEFT DOOR JAMB INNER ANGLE FS 43. REPAIRED ANGLE PER EA 99-102962. 2L72 4F A6WE 19951201003891995120100389WP 1995 12 1 9519099946 119951003A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP FS 190 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 190 INTERCOSTAL ABOVE THE FORWARD STAIR CUTOUT. REPAIRED INTERCOSTAL (P/N 9957838-3), PER EA 99-102920. 2L72 4F A6WE 19951201003901995120100390WP 1995 12 1 9519109946 119951011A5311 FRAME DOUG DC9 DC931 3022065WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 996 FRAME ANGLE AT THE T-CAP BETWEEN LONGERONS 26R TO 27R. REPAIRED PER EA 99-102943. 2L72 4F A6WE 19951201003911995120100391WP 1995 12 1 9519119946 119951030A5312 BULKHEAD TEE DOUG DC9 DC931 3022065WP FS 996 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 AFT PRESSURE BULKHEAD FLOOR TEE AT RBL 34. REPAIRED TEE (P/N 5910163-139), PER EA 99-102944. 2L72 4F A6WE 19951201003921995120100392WP 1995 12 1 9519129946 119951102A5320 WEB DOUG DC9 DC931 3022065WP FS 83 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 83 FLIGHT COMPARTMENT PRESSURE PANEL WEB, RIGHT SIDE. REPAIRED WEB (P/N 9910073), PER EA 99-103091. 2L72 4F A6WE 19951201003931995120100393WP 1995 12 1 9519139946 119951103A5312 BULKHEAD TEE DOUG DC9 DC931 3022065WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 T-CAP AT LONGERON 30. REPAIRED T-CAP (P/N 3915182-502), PER EA 99-103092. 2L72 4F A6WE 19951201003941995120100394WP 1995 12 1 9519149946 119951106A5313 LONGERON DOUG DC9 DC931 3022065WP FS 541-579 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 19L BETWEEN FS 541 TO 579. REPAIRED LONGERON (P/N 5920354-1), PER EA 99-103115. 2L72 4F A6WE 19951201003951995120100395WP 1995 12 1 9519159946 119951106A5330 SKIN DOUG DC9 DC931 3022065WP FS 94-110 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 94 TO 110 AT LONGERON 24L AND ON THE T-CAP, FS 110 BETWEEN LONGERONS 24L TO 27R. REPAIRED SKIN (P/N 991911509-85) AND T-CAP (P/N 5911400) PER EA 99-102691. 2L72 4F A6WE 19951201003961995120100396WP 1995 12 1 9519169931 119951107A5753 TRACK DOUG DC9 DC931 3022065WP TE FLAP CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0190S 47244 DURING LINE CHECK, FOUND A CRACK IN THE LEFT TRAILING EDGE FLAP TRACK WEB AFT INBOARD END. REPAIRED PER EA 98-105026. 2L72 4F A6WE 19951201003971995120100397WP 1995 12 1 9519179877 119951109A5315 FLOORBEAM DOUG DC9 DC951 3022051WP FS 1136 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01786NC 48148 DURING H-CHECK, FOUND CORROSION ON THE FS 1136 FLOORBEAM CAP 3 INCHES INBOARD OF THE RIGHT INBOARD SEAT TRACK. REPAIRED TRACK (P/N 9912243-55), PER EA 98-102610. 2L72 4F A6WE 19951201003981995120100398WP 1995 12 1 9519189966 119951109A5210 DOOR FRAME DOUG DC9 DC931 3022065WP AFT CABIN CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019330 47138 DURING L-CHECK, FOUND A .375 INCH CRACK IN THE AFT CABIN DOOR FRAME AT THE UPPER HINGE. REPAIRED FRAME (P/N 9915565-25) PER EA 99-103317. 2L72 4F A6WE 19951201003991995120100399WP 1995 12 1 9519199946 119951109A5347 SEAT TRACK DOUG DC9 DC931 3022065WP FS 284 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018926E 45863 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RBL 44 SEAT TRACK AT FS 284. REPAIRED TRACK (P/N 2772660), PER EA 99-103090. 2L72 4F A6WE 19951201004001995120100400WP 1995 12 1 9519209162 119951110A5330 SKIN DOUG DC9 DC914 3022034WP FS 332-351 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018907E 45748 DURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 332 TO 351, LONGERONS 28L TO 29R. REPAIRED SKIN (P/N5911412-3), PER EA 91-103318. 2L72 4F A6WE 19951201004011995120100401WP 1995 12 1 9519219311 119951116A5320 WEB DOUG DC9 DC982 3022082WP FS 1155 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01314RC 49110 DURING PERIODIC CHECK, FOUND CORROSION ON THE FLOOR CUSP WEB AT FS 1155 LBL 54. REPAIRED WEB (P/N 9930612-13), PER EA 93-105053. 2L72 4F A6WE 19951201004021995120100402WP 1995 12 1 9519229311 119951116A5315 FLOORBEAM DOUG DC9 DC982 3022082WP FS 1338 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01314RC 49110 DURING PERIODIC CHECK, FOUND CORROSION ON THE FS 1338 FLOORBEAM UPPER CHORD AT LBL 20 TO 44 AND RBL 29. REPAIRED CHORD (P/N S2912758), PER EA 93-105042. 2L72 4F A6WE 19951201004031995120100403WP 1995 12 1 9519239880 119951117A5312 BULKHEAD ANGLE DOUG DC9 DC951 3022051WP FS 37 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01675MC 47651 DURING L-CHECK, FOUND A CRACK IN THE FS 37 BULKHEAD SUPPORT ANGLE. REPAIRED ANGLE (P/N 9911500-509), PER EA 99-102613. 2L72 4F A6WE 19951201004041995120100404WP 1995 12 1 9519249603 119951120A5720 FITTING DOUG DC9 DC932 3022066WP WS 69 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603NW 47101 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING TANK FITTING, WS 69 AT STR 22. REPLACED FITTING PER SRM 51-00. 2L72 4F A6WE 19951201004051995120100405WP 1995 12 1 9519259947 119951127A2420 ELECT TERMINAL DOUG DC9 DC931 3022065WP RT GENERATOR BROKEN A NWAAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 GL018938E 47161 DURING CLIMB, THE RIGHT GENERATOR TRIPPED OFF LINE. RESET RIGHT GENERATOR AND RIGHT BUSS CAME BACK ON LINE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPAIRED BROKEN ELECTRICAL TERMINAL, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201004061995120100406EU 1995 12 1 9519263247 119951126A3260 TARGET BOLT AIRBUS320 A320211 3930320EU LT MLG DOOR FAILED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01347NW 408 DURING CLIMBOUT, RECEIVED L/G DOORS NOT CLOSED MESSAGE ON ECAM. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR DOOR UPLOCK TARGET BOLT. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951201004071995120100407NM 1995 12 1 9519272713 119951121A3350 BATTERY BOEING727 7272S7 138407ZNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01716RC 22021 PILOT REPORTED EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR WAS LOOSE AND WOULD ILLUMINATE WHEN JARRED. REPLACED BATTERIES AND SECURED, CHECKED OK. 2L73 4F A3WE 19951201004081995120100408NM 1995 12 1 9519282297 119951127A3350 BATTERY PACK BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01297US 21789 DURING PREFLIGHT, FOUND AFT EMERGENCY DOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, CHECKED OK. 2L73 4F A3WE 19951201004091995120100409NE 1995 12 1 9519296740 219951125A7200 ENGINE BOEING747 747251F 1384898NM PWA JT9 JT9D7Q 52054NE NR 1 FLAMED-OUT A NWAAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CLCLIMB 1 GL01640US 23888 702170 NR 1 ENGINE FLAMED-OUT AT TOP OF CLIMB WHEN POWER WAS REDUCED. A RELIGHT WAS SUCCESSFUL AND THE FLIGHT CONTINUED ON TO AN UNEVENTFUL LANDING AT TPE. NO FUEL WAS DUMPED. THE ENGINE WAS INSPECTED, BORESCOPED AND A GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19951201004101995120100410NE 1995 12 1 9519306632 219951128A7200 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 3 FLAMED-OUT A NWAAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 GL01632US 23112 715186 DURING CRUISE FL 390, THE NR 3 ENGINE FLAMED-OUT. THE RELIGHT WAS SUCCESSFUL AND THE ENGINE OPERATIONAL WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED, THE FUEL FILTER WAS REPLACED AND A GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E3NE 19951201004111995120100411WP 1995 12 1 9519319913 119951128A2780 RETRACT MECH DOUG DC9 DC931 3022065WP LE FLAPS MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION APAPPROACH 1 GL01963N 47415 DURING APPROACH, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AFTER EXTENDING SLATS AND THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. RECYCLED SLATS AND THE LIGHT ILLUMINATED AGAIN, BUT EXTINGUISHED SHORTLY AFTER SLATS WERE EXTENDED. INSPECTED, OPERATIONALLY CHECKED SLAT SYSTEM AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201004121995120100412NM 1995 12 1 95FDEA01799 119951128A5313 STRINGER BOEING727 727232 1384082NM BS 1042-1048 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01-, 3), ON STR 20L AT BS 1042 TO 1048. REMOVED CORROSION ON STR 20L AT BS 1042 TO 1048. FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REPAIRED STR 20L PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951201004131995120100413NM 1995 12 1 95FDEA01816 119951129A5311 FRAME BOEING727 727232 1384082NM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME AT BS 520, RBL 38-50, WL 172-164. REMOVED DAMAGES AT BS 520, RBL 38-50, WL 172-164. FABRICATED PART, ALODINED, AND PRIMED, AND INSTALLED ON ABOVE AREA, AS PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951201004141995120100414NM 1995 12 1 95FDEA01817 119951128A5311 FRAME BOEING727 727232 1384082NM BS 1010 DOUBLE DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25498FE 20867 DOUBLE HOLE IN FRAME WEB BS 1010, WL 295, LBL 33. REMOVED DAMAGED AREA, INSTALLED REPAIR IAW FEDEX SRM 53-10-4. C/A ADDITION. 2L73 4F A3WE 19951201004151995120100415NM 1995 12 1 95FDEA01818 119951127A5320 FAILSAFE BOEING727 727232 1384082NM BS 1030 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION ON FAILSAFE AT BS 1030, LBL 65, WL 189. REPAIRED FAILSAFE AT BS 1030, LBL 65, WL 189 IAW FEDEX SRM 51-40-4. 2L73 4F A3WE 19951201004161995120100416NM 1995 12 1 95FDEA01819 119951127A5320 BEAM BOEING727 727232 1384082NM BS 750 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AT BS 750 BEAM UPPER CHORD FROM LBL 27 RBL 27 WL 208.1. 2L73 4F A3WE 19951201004171995120100417NM 1995 12 1 95FDEA01820 119951127A5315 FLOORBEAM BOEING727 727232 1384082NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01), ON FLOORBEAM UPPER CHORD AT BS 950D LBL 20 RBL 20 WL 208.1. REPLACED UPPER CHORD FROM BS 950D FLOORBEAM RBL 20 LBL 15 WL 208.1, WORK DONE IAW FEDEX SRM 53-10-8 FIG 3. 2L73 4F A3WE 19951201004181995120100418NM 1995 12 1 95FDEA01821 119951128A5315BAC14902888 FLOORBEAM BOEING727 727232 1384082NM BS 540 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AROUND FASTENER HOLE ON TOP CHORD OF FLOORBEAM AT BS 540 LBL 10.5 WL 208. REMOVED CORROSION AROUND FASTENER HOLE ON TOP CHORD OF FLOORBEAM AT BS 540 LBL 10.5 WL 208. DAMAGE WAS FOUND TO BE BEYOND LIMITS PER FEDEX SRM 53-10-1. REPAIRED DAMAGED AREA PER FEDEX SRM 53-10-8. 2L73 4F A3WE 19951201004191995120100419NM 1995 12 1 95FDEA01822 119951128A532065453132 STR CLIP BOEING727 727232 1384082NM BS 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CRACKED STR CLIP AT BS 600 STR 4R. REMOVED AND REPLACED CRACKED STR CLIP AT BS 600 4R IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19951201004201995120100420NM 1995 12 1 95FDEA01823 119951129A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 328 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01(1) FLOOR BEAM STA 328, WL 208.1, LBL 20-LBL 3. 2L73 4F A3WE 19951201004211995120100421NM 1995 12 1 95FDEA01824 119951125A5320 SHEAR TIE BOEING727 727232 1384082NM BS 1010 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-04) ON SHEAR TIE BS 1010, STR 7L. REMOVED CORROSION FROM SHEAR TIE FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1010, STR 7L. 2L73 4F A3WE 19951201004221995120100422NM 1995 12 1 95FDEA01825 119951128A5315 FLOORBEAM BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AROUND FASTENER HOLES ON TOP CHORD OF FLOORBEAM AT BS 720A RBL 21 LBL 10, 16 AND 21 WL 208. 2L73 4F A3WE 19951201004231995120100423NM 1995 12 1 95FDEA01826 119951128A5320 WEB BOEING727 727232 1384082NM BS 219.8 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING NR0676, FOUND CORROSION ON AFT SIDE OF WEB STA 219.8 WL 214 TO 222 LBL 44. 2L73 4F A3WE 19951201004241995120100424NM 1995 12 1 95FDEA01827 119951128A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 950 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AROUND FASTENER HOLES ON BS 950F, FLOOR UPPER CHORD, RBL 10-RBL 21, WL 208. REPAIRED BS 950F FLOOR BEAM AT RBL 10, WL 208 IAW FEDEX EA 7-5310-26291. C/A ADDITION. 2L73 4F A3WE 19951201004251995120100425NM 1995 12 1 95UAL900274 119951128A3350M10699 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29515UA 24840 EMERGENCY LIGHT INOP AT ROW 26. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951201004261995120100426NM 1995 12 1 95UAL900275 119951128A5210 SEAL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN DOOR LEAKING A UALAA UNSCHED LANDING O OTHER CLCLIMB 1 WP29350UA 24301 PRESSURE LEAK AT DOOR ONE LEFT AT LOWER FORWARD CORNER. REPAIRED LOWER FORWARD DOOR HINGE SEAL, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951201004271995120100427NM 1995 12 1 95UAL900276 119951128A213010607263 CABIN PRESS IND BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE COCKPIT LEAKING A UALAAG UNSCHED LANDING O2 MASK DEPLOYED O OTHER CLCLIMB 1 WP299065U 19946 PASSING THROUGH 25,000 FEET, CABIN ALTITUDE WAS 6,500 FEET AND CLIMBING AT 700 FEET. THE DIFFERENTIAL PRESSURE WAS 2.1 AT 29,000 FEET, CABIN WAS AT 6,500 FEET AND DIFFERENTIAL PRESSURE WAS 2.8, STANDBY NO HELP. CAPTAIN WENT ON OXYGEN BECAUSE NOT FEELING WELL AND FLIGHT RETURNED TO ORD. REPLACED CABIN PRESSURE INDICATOR. TESTED PRESSURIZATION SYSTEM AND CHECKED OK. TESTED ENGINE BLEED SYSTEM AND NO LEAKS WERE FOUND. 2L72 4F4 F A16WE E2EA 19951201004281995120100428NM 1995 12 1 95UAL900277 119951128A3350 EEL STRIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29947UA 26688 EMERGENCY ESCAPE PATH LIGHTING INOP IN AFT CABIN SECTION. REPLACED LIGHT STRIP, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951201004291995120100429NM 1995 12 1 95UAL900278 119951128A3350 EEL POWER CABLE BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29380UA 24655 EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 12 TO 15. REPLACED POWER CABLE, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951201004301995120100430NM 1995 12 1 95UAL900279 119951128A2751SCR72243 POSITION IND BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE TE FLAPS MALFUNCTIONED A UALAA UNSCHED LANDING N FALSE WARNING APAPPROACH 1 WP29354UA 2108 24360 ON APPROACH AT ORD, FLAPS DID NOT INDICATE PAST 10 DEGREES WHEN 25 DEGREES SELECTED. INITIATED GO AROUND, SELECTED FLAPS 15 DEGREES. AFTER A FEW SECONDS, FLAPS INDICATED 15 DEGREES. DIVERTED TO IND. FLAPS OPERATED NORMALLY INTO IND. LIGHT RIME ICE ENCOUNTERED ON APPROACH TO ORD. FLAPS WERE CHECKED PER MM. NO BINDING OR OTHER DISCREPANCIES FOUND. FLAP POSITION INDICATOR CHANGED, PRECAUTIONARY. 2L72 4F4 FRTA16WE E2GL 19951201004311995120100431NM 1995 12 1 95UAL900280 119951128A2910 FLEX LINE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE ENGINE CLOGGED A UALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP299007U 19045 BOTH LOW PRESSURE LIGHTS FOR 'A' SYSTEM HYDRAULIC PUMPS CAME ON FOLLOWED BY LOW PRESSURE LIGHT FOR NUMBER ONE 'B' PUMP AND FEEL DIFFERENTIAL PRESSURE LIGHT. FOUND OBSTRUCTION IN ENGINE FLEX LINE CAUSING LOW PRESSURE INDICATION. REPLACED RESERVOIR AIR PRESSURE REGULATOR AND CHECK VALVE AS PRECAUTIONARY. 2L72 4F4 F A16WE E2EA 19951201004321995120100432NM 1995 12 1 95UAL900281 119951128A3350 BATTERY BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29564UA 26666 EMERGENCY EXIT GREEN LIGHTS INOP AT LEFT AND RIGHT REAR SERVICE DOORS. WHITE EMERGENCY EXIT LIGHT INOP AT LEFT REAR SERVICE DOOR. REPLACED BATTERY, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951201004331995120100433NM 1995 12 1 95UAL900282 119951128A3350 EEL CABLE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29611UA 21872 EEL INOP ROW 9 TO 11. REPLACED FEEDER CABLE, OPS CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951201004341995120100434WP 1995 12 1 ERA00019 119951122A780090632323 TAILPIPE JOINT CVAC 440 440 2422902WP NR 1 ENG SEPARATED A ERAAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03566EA 381 ENGINE FIRE WARNING ON ENGINE NR 1, ZONE NR 1. SHUTDOWN NR 1 ENGINE AND MADE UNEVENTFUL LANDING AT ADQ. FIRE WARNING OUT ON ENGINE SHUTDOWN, RESET AND TESTED GOOD. FOUND UNIVERSAL JOINT ON NR 1 ENGINE TAILPIPE SEPARATED. REMOVED AND REPLACED UNIVERSAL JOINT AND RECONNECTED TAILPIPE IAW CV580 MM 78-10-00. GROUND RUNS CHECKED GOOD. 2L72 4R 6A6 19951201004351995120100435CE 1995 12 1 ERA00020 119951126A5210101430142601 AIRSTAIR DOOR BEECH 200 B200C 1152924CE PAX DOOR OUT OF ADJUST A AERAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 AL03143LG BL5 MRI - AIRSTAIR DOOR OPENED AT ROTATION. RETURNED TO MRI AND MADE UNEVENTFUL LANDING. INSPECTED AIRSTAIR DOOR RIGGING AND STRUCTURE, NO DEFECTS NOTED. TESTED DOOR WARNING SYSTEM FOR PROPER OPERATION IAW MM 52-71-00. ADJUSTED AIRSTAIR DOOR HANDLE SWITCH SLIGHTLY TO PRECLUDE FALSE LOCKED SIGNAL. FOUND SWITCH ACTIVATION WAS OCCURRING 0.030 BEFORE PRESSURE LOCK FULLY ENGAGED. 1L72 4T A24CE 19951201004361995120100436WP 1995 12 1 MWEA95436 119951128A2560A12SA MEGAPHONE DOUG DC9 DC915 3022036WP AFT CABIN INOP A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31900ME 45841 CREW REPORTS, A/C MEGAPHONE INOP. MAINTENANCE REMOVED AND REPLACED MEGAPHONE AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951201004371995120100437NM 1995 12 1 P5CA9500849 119951129A5330 SKIN BOEING747 747121 1384871NM BS 2710 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND 4 INCH CRACK IN FUSELAGE SKIN AT STA 2710, ABOVE LEFT ELEVATOR. REPAIRED PER SRM 53-30-03. 2L74 4F A20WE 19951201004381995120100438NM 1995 12 1 P5CA9500850 119951129A5753 PANEL BOEING747 747121 1384871NM TE MIDFLAP TORN A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND PANEL TORN AT LEFT WING INBOARD MIDFLAP BETWEEN NR 3 AND NR 4 FLAP TRACK FAIRINGS. REPAIRED PANEL PER SRM 51-40-04. 2L74 4F A20WE 19951201004391995120100439NM 1995 12 1 P5CA9500851 119951129A5230 BOLT BOEING747 747121 1384871NM CARGO DOOR CORRODED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND RUST ON BOLT AND HOLE AT NR 3 LATCH LOWER ATTACH POINT FOR AFT CARGO DOOR. REMOVED CORROSION PER SRM 51-10-01, TREATED AND PRIMED PER SRM 51-10-02. 2L74 4F A20WE 19951201004401995120100440NM 1995 12 1 P5CA9500852 119951129A5330 SKIN BOEING747 747121 1384871NM BS 2650 CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 2650 ABOVE LEFT ELEVATOR. REPAIRED PER SRM 53-30-03. 2L74 4F A20WE 19951201004411995120100441NM 1995 12 1 P5CA9500853 119951129A5520 SKIN BOEING747 747121 1384871NM LT ELEVATOR DAMAGED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND HOLE IN LEFT INBOARD ELEVATOR UPPER SURFACE WITH HONEYCOMB EXPOSED. REPAIRED PER SRM 51-40-15. 2L74 4F A20WE 19951201004421995120100442NM 1995 12 1 SWAA950738 119951118A242091252FC7C4001 RELAY BOEING737 7373H4 1384600NM NR 1 BUSS MALFUNCTIONED A SWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW07305SW 22945 EN ROUTE, NUMBER 1 TRANSFER BUSS CIRCUIT BREAKER TRIPPED. RESET BREAKER, BUT TRIPPED AGAIN. CABIN PRESSURE BEGAN TO CLIMB IN AUTO. AIRCRAFT DESCENDED TO 10,000, DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDING. INSPECTED, REPLACED R3 RELAY AND PERFORMED BUSS TRANSFER CHECK. 2L72 4F RTA16WE 19951201004431995120100443NM 1995 12 1 SWAA950739 119951118A3350 EEL WIRING BOEING737 7373H4 1384600NM CABIN DISCONNECTED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07610SW 27696 FOUND SECTION OF EMERGENCY ESCAPE PATH LIGHTING INOP. SECURED LIGHTING AND RECONNECTED WIRING. 2L72 4F RTA16WE 19951201004441995120100444NM 1995 12 1 SWAA950740 119951119A3260 UPLOCK SWITCH BOEING737 7373H4 1384600NM LT MLG FAILED A SWAAD RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SW07337SW 23959 LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR, NO HELP. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED LEFT GEAR UPLOCK SWITCH PER BOEING M/M. 2L72 4F RTA16WE 19951201004451995120100445NM 1995 12 1 SWAA950741 119951119A5311 FRAME BOEING737 7372H4 138448CNM BS 727 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0757SW 21722 DURING SCHEDULED MAINTENANCE, FOUND RT BS 727 O/B CHORD FRAME AT STRINGER 18A CRACKED FROM FWD EDGE OF FLANGE TO SECOND FASTENER. REPAIRED PER SWA ACO 651-53 REV 2. 2L72 4F A16WE 19951201004461995120100446NM 1995 12 1 SWAA950742 119951119A5315 FLOORBEAM STRAP BOEING737 7373H4 1384600NM BS 314 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAPS CRACKED IN E AND E COMPT BS 314 RBL 30 ON BOTTOM OF FLOORBEAM AND AT LBL 12. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951201004471995120100447NM 1995 12 1 SWAA950743 119951119A5315 FLOORBEAM STRAP BOEING737 7373H4 1384600NM BS 344 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4 D-CHECK, FOUND STABILIZER STRAP CRACKED AT LEFT BS 344. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951201004481995120100448NM 1995 12 1 SWAA950744 119951119A5210 ANGLE BOEING737 7373H4 1384600NM PAX DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4 D-CHECK, FOUND MAIN ENTRY DOOR AFT INNER PANEL SUPPORT ATTACH ANGLE CRACKED BETWEEN NUMBER 3 AND 4 STOP FITTINGS. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951201004491995120100449NM 1995 12 1 SWAA950745 119951119A5511 SPAR WEB BOEING737 7373H4 1384600NM LT HORIZ STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07336SW 23940 DURING SCHEDULED 1/4 D-CHECK, FOUND HORIZONTAL STAB IN SPAR SKIN CRACKED. REPAIRED PER SWA RA 1-355-201. 2L72 4F RTA16WE 19951201004501995120100450NM 1995 12 1 SWAA950746 119951119A5315 FLOORBEAM STRAP BOEING737 7373H4 1384600NM E/E COMP CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07685SW 23401 DURING SCHEDULED C1 CHECK, FOUND RIGHT I/B FLOORBEAM STRAP CRACKED IN E AND E COMPT. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951201004511995120100451NM 1995 12 1 SWAA950747 119951120A5313 STRINGER BOEING737 7372T4 1384492NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 16R CRACKED AT FASTENER HOLES AFT OF WING ICE LIGHT FRAME RIGHT SIDE. REPAIRED PER SWA ACO 6405-53. 2L72 4F A16WE 19951201004521995120100452NM 1995 12 1 SWAA950748 119951120A5315 FLOORBEAM BOEING737 7372T4 1384492NM BS 312 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 312 RBL 7. REPAIRED PER SWA RA 1-253-1402. 2L72 4F A16WE 19951201004531995120100453NM 1995 12 1 SWAA950749 119951120A5230 DOOR BOEING737 7375H4 138449DNM FWD CARGO COMPT UNLOCKED A SWAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW07506SW 24183 DURING CLIMBOUT EXPERIENCED BUFFETING, THEN FWD CARGO COMPT DOOR OPEN LIGHT ILLUMINATED AND PRESSURIZATION REMAINED NORMAL. AIRCRAFT DESCENDED TO 6,000 AND RETURNED TO BOI. INSPECTED AND LOCKED DOOR NORMALLY. 2L72 4F RTA16WE 19951201004541995120100454NM 1995 12 1 SWAA950750 119951121A5610 WINDSHIELD BOEING737 7375H4 138449DNM LT COCKPIT CRACKED A SWAAA UNSCHED LANDING O OTHER CRCRUISE 1 SW07503SW 24180 CAPTAIN'S WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO OAK AND MADE AN UNEVENTFUL LANDING. REPLACED PER BOEING M/M. 2L72 4F RTA16WE 19951201004551995120100455 1995 12 1 WWMA9500084 419951126A34256227713004 DPU SAAB SF340 340B 7860101EU LT AVIONICS FAILED A WWMAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP15312AE6180 340B312 AFTER TAKEOFF, THE CREW SMELLED ELECTRICAL SMOKE. THE CAPTAINS EADI SCREEN WENT BLANK AND THE SMOKE STOPPED WHEN THE LEFT AVIONICS WAS SWITCHED OFF. THE AVIONICS SMOKE LIGHT ON THE ANNUNCIATOR PANEL DID NOT ILLUMINATE. THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. UPON INVESTIGATION MAINTENANCE FOUND THE LEFT DIGITAL PROCESSING UNIT, DPU FAILED. REPLACED LEFT DPU, EFIS SCREEN AND THE AVIONICS RACK FILTER. AIRCRAFT RELEASED FOR SERVICE. 2L72 4T RTA52EU 19951201004561995120100456NE 1995 12 1 9519322715 219951129A7532 PRBC VLV BOEING727 7272S7 138407ZNM PWA JT8 JT8D17R 52049NE NR 2 ENGINE MALFUNCTION A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01719RC 22490 689868 NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC VALVE AND INSPECTED THE ENGINE. NO DAMAGE NOTED. 2L73 4F4 F A3WE E2EA 19951201004571995120100457NM 1995 12 1 9519332281 119951128A3350 BATTERY BOEING727 727251 138408HNM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01281US 21160 DURING SERVICE CHECK, FOUND FORWARD GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES. CHECKED OK. 2L73 4F A3WE 19951201004581995120100458WP 1995 12 1 9519349907 119951129A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01957N 47253 DURING LINE CHECK, FOUND AFT OVERWING EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201004591995120100459WP 1995 12 1 9519359156 119951130A3231 RETRACT MECH DOUG DC9 DC914 3022034WP LT NLG DOOR MALFUNCTIONED A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL018915E 45832 DURING CLIMB, A VIBRATION WAS FELT IN THE NOSE LANDING GEAR AREA. AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. FOUND THE LEFT FORWARD NOSE LANDING GEAR DOOR OPEN. REPLACED GEAR DOOR, FORWARD LINK, AND DOOR STOP CABLES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201004601995120100460WP 1995 12 1 9519369949 119951125A2120 AIR DISTR DOUG DC9 DC931 3022065WP CABIN SMOKING A NWAAD RETURN TO BLOCK BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 GL018928E 45865 DURING POWERBACK, SMOKE ACCUMULATED IN THE CABIN AND THE FORWARD LAVATORY SMOKE DETECTOR ACTIVATED. AIRCRAFT RETURNED TO THE GATE AND THE PASSENGERS WERE UNLOADED. INSPECTED AND OPERATIONALLY CHECKED THE AIRCRAFT SYSTEMS. COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951201004611995120100461NM 1995 12 1 95FDEA01828 119951129A5522 SKIN BOEING727 727232 1384082NM LT ELEVATOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 THE LOWER SURFACE OF THE LT ELEVATOR AT ELEVATOR STA 138, 24 INCHES FORWARD OF T/E HAS A PUNCTURE HOLE THAT IS CRACKED. FABRICATED REPAIR PART AND INSTALLED IT ON THE LOWER SURFACE OF THE LT ELEVATOR AT ELEVATOR STA 138, 24 INCHES FORWARD OF THE T/E IAW FEDEX SRM 53-10-3. 2L73 4F A3WE 19951201004621995120100462NM 1995 12 1 95FDEA01829 119951129A5311 FRAME BOEING727 727232 1384082NM BS 720 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME BS 720, LBL 31-37, WL 160. REPAIRED FRAME AT BS 720, LBL 31-37, WL 160 IAW FEDEX SRM 51-40-3. 2L73 4F A3WE 19951201004631995120100463NM 1995 12 1 95FDEA01830 119951129A5311 FRAME BOEING727 727232 1384082NM BS 420 DOUBLE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DOUBLE HOLE IN FRAME AT BS 420, STR 4R. REPAIRED DOUBLE HOLE IN FRAME AT BS 420, STR 4R IAW FEDEX SRM 53-10-4. 2L73 4F A3WE 19951201004641995120100464NM 1995 12 1 95FDEA01831 119951129A5311 FRAME BOEING727 727232 1384082NM BS 520 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME AT BS 520, LBL 32, RBL 46, WL 159 AND 168. REPAIRED DENT IN FRAME AT BS 520, LBL 32, LBL 46, WL 159-168 PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951201004651995120100465NM 1995 12 1 95FDEA01832 119951127A5311 FRAME BOEING727 727232 1384082NM BS 500 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN TOP OF FRAME AT BS 500, LBL 32, WL 158. REPAIRED FRAME AS PER FEDEX SRM 51-40-3 AND 53-10-2 AT BS 500, LBL 32, WL 158. 2L73 4F A3WE 19951201004661995120100466NM 1995 12 1 95FDEA01833 119951127A5330 SKIN BOEING727 727232 1384082NM BS 230 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN SKIN AT BS 230 BETWEEN STR 24-25L. MEASURED DEPTH OF DENT AT .7 INCH BY .035 INCH FOUND TO BE OUT OF LIMITS. REPAIRED DENT PER FEDEX SRM 53-30-3, FIG 13, PG 74-74D. DENT FOUND OUT OF LIMITS PER FEDEX SRM 53-30-1. 2L73 4F A3WE 19951201004671995120100467NM 1995 12 1 95FDEA01834 119951127A5311 FRAME BOEING727 7272S2F 1384O81NM BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 CRACK IN LOWER LOBE FRAME BS 660, RBL 2, WL 154. CUT OUT DAMAGED AREA AT BS 660, BL ZERO - RBL 5, WL 154. FABRICATED REPAIR PARTS OUT OF 7075T6.050 MATERIAL, AND INSTALLED WET WITH SEAL AS PER FEDEX SRM 53-10-2 AND 51-40-3. 2L73 4F A3WE 19951201004681995120100468NM 1995 12 1 95FDEA01835 119951127A5241 DOOR SKIN BOEING727 727227 1384078NM GALLEY DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 FORWARD GALLEY DOOR OUTER SKIN HAS CRACK ON THE UPPER HINGE CUT-OUT. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER ON FORWARD GALLEY DOOR OUTER SKIN UPPER CUT-OUT PER FEDEX SRM 52-00-3. 2L73 4F A3WE 19951201004691995120100469NM 1995 12 1 95FDEA01836 119951127A5320654531313 CLIP BOEING727 727227 1384078NM BS 660 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 660, STR 9L. REMOVED CRACKED CLIP, BACK DRILLED NEW CLIP AND INSTALLED FASTENERS AT BS 660, STR 9L. CORRECTION ON A/C NR. 2L73 4F A3WE 19951201004701995120100470NM 1995 12 1 95FDEA01837 119951125A5320651758866 G BEAM BOEING727 727227 1384078NM BS 264-269 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 WHILE WORKING NR0623, FOUND CORROSION ON G-BEAM BS 264-269, WL 208, BL 0 - LBL 8. FOUND CORROSION OUT OF LIMITS PER SRM 53-10-01, REMOVED AND REPLACED G-BEAM, REF FEDEX DWG 65-17588. 2L73 4F A3WE 19951201004711995120100471NM 1995 12 1 DL72K954537 119951127A2910651782119 HYD MODULE BOEING727 727232 1384082NM A HYD SYSTEM CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27480DA 20860 FOUND DURING A-2 LETTER CHECK - CHECK VALVE BROKEN/BLOWN AT BASE OF A-SYSTEM PRESSURE MODULE. REPLACED A-SYSTEM MODULE, P/N 294001002. 2L73 4F A3WE 19951201004721995120100472NM 1995 12 1 DL72L954540 119951117A533065C139131 SKIN BOEING727 727232 1384082NM BS 950 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27509DA 21311 CORROSION WAS FOUND IN THE FUSELAGE SKIN APPROXIMATELY 2 INCHES AFT OF STA 950F, AT S-28R. DAMAGE REMOVAL RESULTED IN A 4.125 INCH INBD/OUTBD BY 6.0 INCH FWD/AFT CUT-OUT. THE SKIN IS FABRICATED FROM CLAD 2024-T3 AND WAS MEASURED AT 0.150 INCH THICK. REPAIRED PER DL ERA 302750-14. 2L73 4F A3WE 19951201004731995120100473NM 1995 12 1 DL72S954536 119951127A3350334701748 EEL BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27468DA 20745 AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L73 4F A3WE 19951201004741995120100474NM 1995 12 1 DL72S954547 119951128A291065178234 HYD MODULE BOEING727 727232 1384082NM ELEVATOR LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27528DA 9245 21702 ON CLIMB-OUT, ELEV FEEL DIFFERENTIAL PRESS LIGHT BEGAN TO FLICKER, HYDRAULIC PRESSURE AND QUANTITY GOOD ON ALL SYSTEMS, ABOUT 5 MINUTES LATER, THE HYDRAULIC SYSTEM-A OVERHEAT LIGHT ILLUMINATED. TURNED NR 1 PUMP BACK ON, WAS GOOD FOR ABOUT 2 MINUTES, AND LIGHT RE-ILLUMINATED WITH LOSS OF PRESSURE AND QUANTITY ALMOST INSTANTANONEOUSLY. HAD UNEVENTFUL LANDING, FOUND ELEVATOR HYDRAULIC MODULE LEAKING FROM PLUG AT COMPENSATOR. REPLACED ELEVATOR HYDRAULIC MODULE. 2L73 4F A3WE 19951201004751995120100475NM 1995 12 1 DL72S954549 119951128A575465162222 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27408DA 21152 DURING SHOP INSPECTION, NR 6 L/E RIB WAS FOUND WITH L/E SUPPORT RIBS NRS 3, 4, 7, 8, 10 AND 12 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951201004761995120100476NM 1995 12 1 DL72S954558 119951128A5754651622199 SKIN BOEING727 727232 1384082NM NR 4 LE FLAP BENT A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 LOWER SKIN BENT AND A PIECE MISSING AT THE ACTUATOR RIBS LOCATION. INSTALLED DOUBLER PER M/M 57-54-0, FIG. 815, DURING SHOP VISIT, FOR NR 4 L/E SLAT. 2L73 4F A3WE 19951201004771995120100477NM 1995 12 1 DL72S954562 119951116A5754651622172 RIB BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 DURING SHOP INSPECTION, RIB NR 17 WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER B-727 M/M 57-54-0 FOR NR 5 L/E SLAT. 2L73 4F A3WE 19951201004781995120100478NM 1995 12 1 DL72S954563 119951116A5754651622172 SKIN BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 DURING SHOP INSPECTION, A CRACK WAS FOUND IN THE EXTERIOR SKIN 37.5 INCHES FROM THE OUTBOARD END AT THE FENCE ATTACH POINT. THE DAMAGE WAS REPAIRED PER THE B-727 M/M 57-54-0, PG 817 FOR NR 5 L/E SLAT. 2L73 4F A3WE 19951201004791995120100479NM 1995 12 1 DL72S954564 119951116A5754651622172 ANGLE BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 DURING SHOP INSPECTION, THE LOWER ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ACTUATOR RIB. THE CRACK WAS REPAIRED PER THE B-727 M/M 57-54-0 FOR NR 5 L/E SLAT. 2L73 4F A3WE 19951201004801995120100480NM 1995 12 1 DL72W954541 119951117A5712652163832 RIB BOEING727 727247 138408FNM BS 850 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272814W 20870 THE RBL 70.65 WING RIB HAS A CRACK EMANATING FROM THE LOWER OF TWO FASTENER HOLES USED FOR A FUEL CROSSOVER LINE ATTACH CLIP, AND TERMINATING IN THE LOWER FUEL CROSSOVER CUT-OUT LOCATED AT APPROXIMATELY BS 835. THE CRACK MEASURES 0.5 INCH IN LENGTH. THE WEB IS MADE FROM MACHINED 7178-T651 PLATE WITH A WEB THICKNESS OF 0.21 INCH. THE PADDED REGION ADJACENT TO FUEL CROSSOVER CUT-OUT (CRACKED AREA) IS 0.58 INCH THICK. REPAIRED PER DL ERA 302716-14. 2L73 4F A3WE 19951201004811995120100481NM 1995 12 1 DL72W954555 119951128A5320 ANGLE BOEING727 727247 138408FNM BS 870 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272810W 20648 FOUND ON C-1 LETTER CHECK, 1.250 INCH CRACK IN THE RT W/W VERTICAL KEEL BEAM ANGLE AT STA 870. REPAIRED PER SRM 53-10-9 TIME LIMITED INSTRUCTIONS. 2L73 4F A3WE 19951201004821995120100482NM 1995 12 1 DL72W954556 119951128A5754 ANGLE BOEING727 727247 138408FNM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272810W 20648 FOUND ON C-1 LETTER CHECK, .25 INCH CRACK IN SLAT COVE SKIN ATTACH ANGLE BELOW THE ANTI-ICE DUCT, NR 2 SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951201004831995120100483NM 1995 12 1 DL733954545 119951128A2721308504 SWITCH BOEING737 737347 1384647NM RUDDER TRIM FAILED A ADALAO OTHER F FLT CONT AFFECTED APAPPROACH 1 SO27311WA 23597 ON SHORT FINAL, RUDDER TRIM RAN AWAY TO 7 DEGREES ON LEFT TRIM. PER TROUBLESHOOTING CHART CHECK RUDDER CENTERING PER M/M, RUDDER CENTERING CHECKS NORMAL, REPLACED RUDDER TRIM SWITCH. SWITCH CHECKS GOOD PER M/M. 2L72 4F RTA16WE 19951201004841995120100484NM 1995 12 1 DL757954535 119951127A3350BP573 EEL POWER SUPPLY BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27684DA 27104 IRR - ON LAYOVER, FOUND R1 EXTERIOR DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY M730. OPS GOOD. 2L72 4F RTA2NM 19951201004851995120100485WP 1995 12 1 DLL10954542 119950825A53121505220103 BLKHD WEB LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27717DA 193C1096 THE FUSELAGE STATION 1363 BULKHEAD CAP AND WEB ARE CRACKED BETWEEN STRINGERS 47 AND 48 AT APPROX WL 160. REPAIRED PER DL ERA 271718-14. 2L73 4F A23WE 19951201004861995120100486WP 1995 12 1 DLL10954569 119951123A29112730522 ACCUMULATOR LKHEED1011 10113851 5265010WP C HYD SYSTEM CRACKED A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27714DA 193C1090 NOTICED C-SYSTEM HYDRAULIC QUANTITY BELOW ONE-FOURTH AND DECREASING. TURNED OFF C-SYSTEM PUMP S/O SWITCHED TO ATM. QUANTITY CEASED DECREASING, LOWERED LANDING GEAR MANUALLY, DOWN AND LOCKED. FOUND C-SYSTEM ACCUMULATOR CRACKED AND LEAKING. REPLACED ACCUMULATOR, OPERATION NORMAL. 2L73 4F A23WE 19951201004871995120100487WP 1995 12 1 DLL14954534 119951127A3350 EEL POWER SUPPLY 5165741 LKHEED1011 1011385115 5265015WP R1 DOOR INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO271739D 37245 193C1237 1R EMERERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY. CHECKS GOOD. 2L73 4F A23WE 19951201004881995120100488NM 1995 12 1 DLM11954544 119951128A33506044113 EEL PWR PACK DOUG MD11 MD11 3023602NM NR 5 FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27803DE 48474 EEL BATTERY NR 5, LOW MSG ON EEL TEST. REPLACED NR 5 BATTERY POWER PACK. 2L73 4F RTA22WE 19951201004891995120100489NM 1995 12 1 DLM88954512 119951127A2910 HYD LINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE SPLIT A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO27954DL 49885 725419 ON DEPARTURE (ABOUT 12,000 FEET), RT HYDRAULIC PRESSURE LOW MESSSAGE AND INDICATOR LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. BOTH RT HYDRAULIC PRESSURE AND QUANTITY READ ZERO. RETURNED TO ATLANTA. FOUND RT ENGINE HYDRAULIC RETURN FLEX LINE LEAKING AT FILTER MODULE. REPLACED LINE, BLED HYDRAULIC SYSTEM AND SERVICED. LEAK CHECK OK. 2L72 4F4 FRTA6WE E9NE 19951201004901995120100490NM 1995 12 1 P5CA9500854 119951130A5310 STRUCTURE BOEING747 747121 1384871NM NLG WW CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND NOSE LANDING GEAR ACTUATOR UPPER SUPPORT STRUCTURE CRACKED AT LOWER INBOARD FLANGE AREA JUST AFT OF WEB. BLENDED OUT CRACKED AREA PER EA PAO-LAX-95-0041RE. 2L74 4F A20WE 19951201004911995120100491NM 1995 12 1 UPS205112 119951129A33501000679 EEL ASSY BOEING727 72731C 1384011NM FLIGHT DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01922UP 19231 WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. 2L73 4F A3WE 19951201004921995120100492NM 1995 12 1 UPS205116 119951130A3350S106 BATTERY BOEING727 72725C 138400HNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPAIRED BATTERY (BOTH) EMERGENCY LIGHTS. OPS CHECK O.K. 2L73 4F A3WE 19951201004931995120100493NM 1995 12 1 UPS205118 119951129A3350 BATTERY BOEING727 72725C 138400HNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 WHILE ON GROUND, MAINTENANCE FOUND FLIGHT DECK EMERGENCY EXIT LIGHTS WILL NOT ILLUMIATE. REPLACED BATTERY. OP CHECK GOOD. 2L73 4F A3WE 19951201004941995120100494NM 1995 12 1 UPS505120 119951128A32604648876 IND BULB BOEING757 75724APF 1384969NM LT MLG FAILED A IPXAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO01440UP 25471 CREW REPORTED ON GEAR EXTENSION AT PBI, LEFT MAIN GEAR LIGHT DID NOT ILLUMINATE. GEAR DISAGREE EICAS MSG ILLUMINATED. RAN APPROPRIATE CHECK LISTS AND PERFORMED NORMAL LANDING. PBI CFR PINNED LEFT MAIN GEAR AFTER LANDING. RELAMPED LT GEAR LIGHT PER MM 33-16-02, FIG 103. PERFORMED PSCU BITE TEST. NO DEFECTS FOUND. 2L72 4F RTA2NM 19951201004951995120100495WP 1995 12 1 UPS805113 119951129A5730 PANEL DOUG DC8 DC873F 302199FWP RT WING CRACK A IPXAK NONE O OTHER ININSP/MAINT 1 SO01816UP 45990 WHILE IN FOR SERVICE VISIT, RIGHT WING FUEL TANK PANEL LANDING 505F CRACKED 1 INCH AT SCREW HOLE. REPAIRED PER DC8 SRM 57-2-1, FIGURE 36. 2L74 4F RT4A25 19951201004961995120100496WP 1995 12 1 UPS805114 119951129A573057695893 SKIN DOUG DC8 DC871F 302199DWP LT WING LE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01797UP 45897 WHILE ON GROUND, MAINTENANCE FOUND CRACK ABOUT 1.25 INCHES LONG ON WING L/E LOWER OUTBOUND OF NR 2 ENGINE, 8 INCHES AFT OF FIRE BOTTLE INSP PLATE INBOUND. REPAIRED PER UPS ENGINEERING FILE NR DC8-57-0615. 2L74 4F RT4A25 19951201004971995120100497WP 1995 12 1 UPS805115 119951129A3231 LATCH MECH DOUG DC8 DC873F 302199FWP LDG GEAR DOORS LACK OF LUBE A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01866UP 45966 CREW REPORTED DOOR NOT LATCHED LIGHT ON AFTER GEAR RETRACTED - CHECK LIST ACCOMPLISHED: LIGHT EXTINGUISHED AFTER 4 CYCLES. INSPECTED DOOR LATCH MECHANISMS AND SWITCHES. LUBED BOTH GEAR DOOR LATCH MECHANISMS, TESTED O.K. I.A.W. DC-8-M/M 32-31-04. 2L74 4F RT4A25 19951201004981995120100498WP 1995 12 1 UPS805119 119951129A32324648876 DOOR ACTUATOR DOUG DC8 DC873F 302199FWP RT MLG DOOR FAILED A IPXAO OTHER O OTHER CLCLIMB 1 SO01802UP 46100 CGN - ON CLIMBOUT, RT MAIN LANDING GEAR DOOR ACTUATOR SWIVEL GLAND SHAFT WAS FOUND TO HAVE SHEARED AND MIGRATED OUT, JAMMING THE DOOR SEQUENCING MECHANISM DURING GEAR RETRACTION, CAUSING THE RT MAIN LANDING GEAR DOOR FILLET TO CONTACT NR 3 FWD AND AFT TIRES. RT MAIN LANDING GEAR DOOR REPAIRED AND INSTALLED IAW MM 32-12-01. NEW MAIN LANDING GEAR DOOR ACTUATOR, CONTROL VALVE, SWIVEL GLAND SHAFT AND ADJUSTABLE LINK ASSY INSTALLED IAW MM 32-32-01 (02). OPERATION AND INDICATION NORMAL ON GEAR SWING. 2L74 4F RT4A25 19951201004991995120100499NM 1995 12 1 QXEA9400403 119951122A3260864202 SENSOR DHAV DHC8 DHC8102 2809003NM RT MLG DOOR OUT OF ADJUST A QXEAK NONE N FALSE WARNING CLCLIMB 1 NM09840PH 074 PDX - RIGHT MAIN DOOR ADVISORY LIGHT STAYS ON AFTER GEAR RETRACTION. ABOVE 215 KNOTS, LIGHT GOES OUT. PSEU INDICATES FORWARD RIGHT GEAR DOOR SENSOR FAILED WITH GEAR UP. FORWARD GEAR ACTUATOR ADJUSTED AND FORWARD GEAR DOOR GAP ADJUSTED. GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201005001995120100500NM 1995 12 1 QXEA9500356 119951027A3350MS25231316 BULB DHAV DHC8 DHC8102 2809003NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09816PH 54 SEA - OVERHEAD EMERGENCY LIGHT INOP. BULB REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201005011995120100501EU 1995 12 1 QXEA9500357 119951028A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09801PH 11097 PDX - SEVERAL EMERGENCY LIGHTS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005021995120100502EU 1995 12 1 QXEA9500358 119951028A5220A20446005 SPRINGS FOKKERF28 F28MK1000 4990808EU LT EMER EXIT WEAK A QXEAK NONE O OTHER LDLANDING 1 NM09801PH 11097 PDX - LEFT OVERWING EXIT HANDLE MOVED AND EXIT OPENED PART WAY ON LANDING IN PDX. OVER-CENTER SPRINGS WERE REPLACED AND DOOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005031995120100503EU 1995 12 1 QXEA9500359 119951028A3350608905 BATTERY PACK FOKKERF28 F28MK1000 4990808EU CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 483 11107 PDX - EMERGENCY LIGHTS OVER ROWS 4 AND 6 ARE INOP. BATTERY PACK REPLACED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005041995120100504NM 1995 12 1 QXEA9500360 119951028A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09815PH 50 PSC - LANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE SELECTED DOWN. ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. AIRCRAFT LANDED IN PSC WITHOUT INCIDENT. AIRCRAFT FERRIED TO PDX FOR REPAIR. GEAR SELECTOR VALVE REPLACED I/A/W MAINT. MANUAL. GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201005051995120100505EU 1995 12 1 QXEA9500361 119951029A33506008905 BATTERY PACK FOKKERF28 F28MK1000 4990808EU CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 135 11107 PDX - EMERGENCY LIGHT AT ROW 8 INOP. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005061995120100506EU 1995 12 1 QXEA9500362 119951029A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09802PH 11017 GEG - ONE OVERHEAD EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005071995120100507EU 1995 12 1 QXEA9500363 119951030A3350683 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - FORWARD EXIT SIGN HAS SEVERAL 28V LAMPS INOP. BULBS WERE REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005081995120100508EU 1995 12 1 QXEA9500364 119951030A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 BOI - RIGHT SIDE EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005091995120100509EU 1995 12 1 QXEA9500365 119951031A3350A89315401 EEL CIRCUIT BD FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 PDX - EXIT LIGHT AT ROW 8 NOT ILLUMINATING. EXIT LIGHT CIRCUIT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005101995120100510NM 1995 12 1 QXEA9500366 119951031A2121011291500 FAN DORNERDO32 DO328100 2996000NM AVIONIC RACK FAILED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09332PH3335 3010 SEA - SMELL OF SMOKE IN AIRCRAFT FOLLOWED BY AVIONIC FAN FAIL CAS MESSAGE. AFT AVIONIC FAN REPLACED I/A/W MAINT. MANUAL. FAN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951201005111995120100511SW 1995 12 1 QXEA9500367 119951101A26203219027001 CONNECTOR SWRNGNSA227 SA227AC 8780603SW COCKPIT DISCONNECTED A QXEAK NONE N FALSE WARNING ININSP/MAINT 1 NM092727B14547 AC730 NR 2 FIRE EXTINGUISHER E-LIGHT ILLUMINATED, BOTTLE PRESSURE NORMAL. FOUND LOGIC MODULE CONNECTOR UNLATCHED AND LOOSE. RESECURED CONNECTOR AND TESTED SYSTEM. AIRCRAFT RELEASED FOR SERVICE. 1L72 4T A8SW 19951201005121995120100512NM 1995 12 1 QXEA9500368 119951101A2611MS1557081 SMOKE DET LAMP KIDDE 302313 DHAV DHC8 DHC8102 2809003NM CARGO BAY FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09812PH 31914 26 NR 2 SMOKE DETECTOR IN BAGGAGE COMPARTMENT WOULD NOT TEST. REPLACED BURNED OUT TEST BULB, PERFORMED OPS TEST. AIRCRAFT RELEASED FOR SERVICE. 2H72 4T RTA13NM 19951201005131995120100513NM 1995 12 1 QXEA9500388 119951112A7714M8372382K2041N CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NL PROBE CORROSION A QXEAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 NM09826PH 214 PSC - NR 1 ENGINE ECU MANUAL LIGHT ILLUMINATED ON TAKEOFF ROLL, CONTINUED TAKEOFF. ENGINE AUTO FEATHERED ON CLIMB, BUT CONTINUED TO RUN. FLIGHT CREW PERFORMED AN IN-FLIGHT SHUTDOWN AND RETURNED TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. ECU WAS NOT FLAGGED ON ENG CONDITION PANEL. NL, NP, NH, ECU, TSC AND INLET TEMP PROBES CANNON PLUGS INSPECTED FOR CORROSION. NL CANNON PLUG WAS CORRODED. PLUG WAS CLEANED AND REINSTALLED. ENGINE OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 19951201005141995120100514EU 1995 12 1 QXEA9500389 119951114A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 PDX - LEFT OVERWING EXIT EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005151995120100515NM 1995 12 1 QXEA9500390 119951115A21210113899500 FAN DORNERDO32 DO328100 2996000NM COCKPIT SMOKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 NM09336PH2820 3014 PDX - SMOKE IN COCKPIT ON LANDING ROLLOUT. A FAN FAIL CAS MESSAGE DID APPEAR ON CAS SCREEN. NR 2 HX FAN REPLACED I/A/W MAINT. MANUAL. FAN OPS CHECKED GOOD ON GROUND RUN. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951201005161995120100516EU 1995 12 1 QXEA9500391 119951115A33505515800106 EEL SIGN FOKKERF28 F28MK1000 4990808EU CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 PDX - EXIT SIGN ABOVE COCKPIT DOOR INOP. EXIT SIGN REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005171995120100517NM 1995 12 1 QXEA9500392 119951115A3260864202 SENSOR DHAV DHC8 DHC8102 2809003NM NLG OUT OF ADJUST A QXEAK NONE N FALSE WARNING CRCRUISE 1 NM09825PH 213 BOI - NOSE GEAR INTRANSIT LIGHT ILLUMINATES IN-FLIGHT. AIRCRAFT LANDED IN BOI WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. NOSE GEAR DRAG LINK PROXIMITY SENSOR ADJUSTED I/A/W MAINT MANUAL. PSEU TARGET/SENSOR TEST PERFORMED, CHECK GOOD. SENSOR CANNON PLUG CLEANED. NOSE GEAR INIDICATION OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201005181995120100518NM 1995 12 1 QXEA9500394 119951117A33508GH00567806 BULB DORNERDO32 DO328100 2996000NM LAVATORY FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09335PH 3013 SEA - LAV LIGHT IS DIM WHEN EMERGENCY LIGHTS ARE ON. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951201005191995120100519NM 1995 12 1 QXEA9500395 119951118A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR MALFUNCTIONED A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM09102AV 13608 91 SEA - GEAR INTRANSIT LIGHTS CAME ON, BUT GEAR DID NOT EXTEND AFTER SELECTING GEAR DOWN. GEAR HANDLE CYCLED UP AND RED LIGHTS WENT OUT. ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. AIRCRAFT FERRIED TO PDX FOR REPAIR. LANDING GEAR SELECTOR VALVE REPLACED I/A/W MAINT. MANUAL. VALVE OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951201005201995120100520EU 1995 12 1 QXEA9500396 119951119A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 PDX - RIGHT OVERWING EXIT LAMP IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005211995120100521EU 1995 12 1 QXEA9500397 119951119A3310561408BVL2 BALLAST FOKKERF28 F28MK1000 4990808EU COCKPIT SHORTED A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09454US 11107 OAK - FIRST OFFICERS EYEBROW LIGHTS ARE INOP. BURNT BALLAST SMELL IN COCKPIT AND MAIN INST PANEL LIGHTS CIRCUIT BREAKER 8M RT TRIPPED. BALLAST FOR FIRST OFFICER'S RED FLOOD LIGHT REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005221995120100522EU 1995 12 1 QXEA9500398 119951119A33506008903 BATTERY FOKKERF28 F28MK1000 4990808EU CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 PDX - FLOOR PROXIMITY LIGHTS AFT OF ROW 8 ARE INOP. BATTERY PACK REPLACED AT ROW 12 AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005231995120100523EU 1995 12 1 QXEA9500399 119951119A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09803PH 11031 BOI - BOTH EMERGENCY LIGHTS ABOVE FORWARD FLIGHT ATTENDANT PANEL ARE INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005241995120100524EU 1995 12 1 QXEA9500400 119951119A32341N40051 DIODE FOKKERF28 F28MK1000 4990808EU GEAR HANDLE SHORTED A QXEAK NONE J WARNING INDICATION CLCLIMB 1 NM09803PH 11031 PDX - LANDING GEAR HANDLE COULD NOT BE MOVED FROM THE DOWN POSITION AFTER TAKEOFF. CHECKLIST PERFORMED AND GEAR WAS RAISED USING OVERRIDE. DIODE REPLACED FOR GEAR SOLINOID AND SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005251995120100525EU 1995 12 1 QXEA9500401 119951120A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 SEA - SEAT 8A EXIT LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005261995120100526EU 1995 12 1 QXEA9500402 119951121A33501315 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 GEG - ONE OVERHEAD EMERGENCY LIGHT IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005271995120100527NM 1995 12 1 QXEA9500404 119951122A2121011291500 FAN DORNERDO32 DO328100 2996000NM AVIONICS SMOKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09329PH1728 3007 PDX - AVIONICS FAN EMITTED SMOKE. AFT AVIONICS FAN REPLACED IAW MAINT MANUAL AND FAN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SRVICE. 2H72 4T RTA45NM 19951201005281995120100528EU 1995 12 1 QXEA9500405 119951123A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452US 11105 PDX - EGRESS ARM LIGHT ON OVERHEAD AT ROW 1 INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005291995120100529EU 1995 12 1 QXEA9500406 119951124A499036068121 OIL TANK GARRTT FOKKERF28 F28MK1000 4990808EU APU LEAKING A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 NM09466US 11075 SEA - SMOKE COMMING FROM APU EXHAUST AND ALSO BEING CIRCULATED THROUGH AIR CONDITIONING PACK NR 2. FUEL FOUND IN APU OIL SYSTEM. APU OIL TANK REPLACED AND APU RESERVICED WITH OIL. APU OPS CHECKED AND NO SMOKE OR SMELL NOTED FROM NR 2 PACK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005301995120100530EU 1995 12 1 QXEA9500407 119951126A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09466US 11075 PDX - PULL HANDLE SIGN AT LEFT OVERWING EXIT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005311995120100531EU 1995 12 1 QXEA9500408 219951127A73227863916 HMU DHAV DHC8 DHC8102 2809003NM RROYCESPEY SPEY55515 54521EU NR 1 ENGINE MALFUNCTIONED A AQXEAK NONE O OTHER TXTAXI/GRND HDL 1 NM09802PH118935751 63 PDX - STRONG FUEL SMELL IN COCKPIT AND CABIN AFTER STARTING NR 1 ENGINE. NR 1 HMU REPLACED I/A/W MAINT. MANUAL. HMU OPS CHECKED GOOD ON GROUND RUN. NO FUEL SMELL NOTED IN COCKPIT OR CABIN. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 FRTA13NM E2EU 19951201005321995120100532SW 1995 12 1 QXEA9500409 119951128A3610 NR 2 BLEED AIR SWRNGNSA227 SA227AC 8780603SW CABIN SMOKING A QXEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM0926861 AC649 GEG - NR 2 BLEED AIR GENERATING SMOKE IN CABIN. NR 2 BLEED AIR PLACED ON MEL 21-4. 1L72 4T A8SW 19951201005331995120100533SW 1995 12 1 QXEA9500410 119951128A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A QXEAO OTHER N FALSE WARNING APAPPROACH 1 NM0931168 AC599 PDX - GEAR WARNING HORN SOUNDED WHEN FLAPS WERE SELECTED TO FULL FROM HALF. GEAR WAS DOWN AND LOCKED. GEAR WARNING CIRCUIT BREAKER PULLED. AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. CIRCUIT BREAKER WAS RESET AFTER THE AIRCRAFT WAS PARKED AND HORN DID NOT SOUND. RIGHT MAIN GEAR DOWN POSITION SWITCH WAS REPLACED AND ADJUSTED I/A/W MAINT. MANUAL. GEAR OPS CHECKED GOOD ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951201005341995120100534EU 1995 12 1 QXEA9500411 119951129A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 PDX - EMERGENCY EXIT LIGHT BURNED OUT ON THE RIGHT SIDE. BULB WAS REPLACED AND LIGHT OPS CHECKED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951201005351995120100535WP 1995 12 1 95ZZZM645 119951018A5210 DOOR DOUG DC9 DC932 3022066WP AFT AIRSTAIR NOT LATCHED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11904VJ 47377 FLT NR 547 - PHL - AIR RETURN, AFT AIRSTAIR DOOR LIGHT ILLUMINATED. RECYCLED AFT STAIRS, SYSTEM CHECK NORMAL. (M) 2L72 4F A6WE 19951201005361995120100536WP 1995 12 1 95ZZZM646 119951014A2150 PACK DOUG DC9 DC932 3022066WP RIGHT INOP A VJ6AA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 SO11934VV 47488 ON FLT 440 - ATL - AIR RETURN, THE RIGH PACK OVERHEATED IN FLIGHT. THE TEMP CONTROL KNOB HAD NO EFFECT ON VALVE POSITION WHICH WAS IN FULL HOT. ASSIGNED MEL NR DM5116, SEQ 21-01 RIGHT PACK INOP. 2L72 4F A6WE 19951201005371995120100537EU 1995 12 1 95ZZZM647 119951016A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A VNAAO OTHER C F.O.D. NRNOT REPORTED 1 GL07855JS 739 FLT NR 4195 - CREW REPORTED STRIKING A BIRD EN ROUTE TO DAY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT IAW MM 05-00-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951201005381995120100538EU 1995 12 1 95ZZZM648 119951010A3246 WHEEL ASSY BAG JETSTMJETSTM3101 1500215EU NLG MISSING A VNAAO OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 GL07844JS 418 760 FLT NR 4119 - CREW NOTICED LEFT NOSE WHEEL ASSEMBLY MISSING FROM AIRCRAFT AFTER LANDING IN PIT. MAINTENANCE REPLACED LEFT NOSE WHEEL ASSY IAW MM 32-40-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951201005391995120100539EU 1995 12 1 95ZZZM649 119951010A243523079005 STARTER GEN BAG JETSTMJETSTM3101 1500215EU LT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 GL07841JS 4963 751 FLT NR 4032 - CREW ELECTED TO RETURN TO FIELD, NOT ABLE TO GET LEFT GENERATOR ON LINE. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED LEFT S/G, GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951201005401995120100540EU 1995 12 1 95ZZZM650 119951010A772221180422 SRL COMPUTER GARRTT BAG JETSTMJETSTM3101 1500215EU RT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL07856JS 47702 744 FLT NR 4165 - CREW ELECTED TO RETURN TO FIELD AFTER RIGHT ENGINE EGT WENT TO 100 DEGREES. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SRL COMPUTER IAW MM 71-00-00. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951201005411995120100541EU 1995 12 1 95ZZZM651 119951008A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIR FRAME BIRD STRIKE A VNAAO OTHER C F.O.D. APAPPROACH 1 GL07839JS 748 FLT NR 4182 - CREW REPORTED, STRIKING A BIRD, RIGHT SIDE OF AIRCRAFT WHILE ON APPROACH TO RIC. AIRCRAFT LANDED WITHOUT INCIDENT. OUT STATION MAINTENANCE INSPECTED AIRCRAFT IAW MM 05-00-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951201005421995120100542CE 1995 12 1 95ZZZM652 119951002A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE LANDING GEAR FAILED A GPPAO OTHER O OTHER APAPPROACH 1 CE0919016 UC22 EN ROUTE, LANDING GEAR WOULD NOT EXTEND, AFTER SEVERAL TRIES GEAR CAME DOWN ON ITS OWN WITH HANDLE IN DOWN POSITION. AIRCRAFT FERRIED TO GSO. REMOVED AND REPLACED LANDING GEAR RELAY. (M) 2L72 4T RTA24CE 19951201005431995120100543CE 1995 12 1 95ZZZM653 119950928A32341013841375 GEAR HANDLE BEECH 1900 1900C 1154161CE LANDING GEAR MALFUNCTIONED A GPPAO OTHER J WARNING INDICATION APAPPROACH 1 CE0919016 UC22 LANDING GEAR WON'T EXTEND. AFTER A FEW MINUTES GEAR WENT DOWN. LANDING WAS ACOMPLISHED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED HANDLE ASSEMBLY. (M) 2L72 4T RTA24CE 19951201005441995120100544EA 1995 12 1 95ZZZM654 219951002A75301149700201 EVA TUBE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT BLEED AIR LEAKING A GPPAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE0939019 UC39 LEFT BLEED AIR FAIL ILLUMINATED IN FLIGHT, RETURNED TO IAD. REPAIRED HOLE IN EVA TUBE DUE TO CHAFING. 2L72 4T4 TRTA24CE E4EA 19951201005451995120100545EU 1995 12 1 95ZZZM655 119951028A33503011151 BATTERY PACK AEROSPATR42 ATR42300 8680920EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21223AT AEB023 223 RFD - THREE FLOOR PROXIMITY LIGHTS INOP IN FORWARD CABIN, MEL 33-22. MAINTENANCE REMOVED AND INSTALLED EMERGENCY POWER SUPPLY AND BATTERY PACK IAW ATR 42 JIC MM CH 33-51-21. OPS CHECK GOOD ON ALL TRACK LIGHTING. AIRCRAFT WAS RETURNED TO SERVICE. REFERENCE SIMA953011. 2H72 4T RTA53EU 19951201005461995120100546WP 1995 12 1 95ZZZM656 119951013A323048008731 UPLATCH PIN DOUG DC8 DC863 302198AWP NLG SHEARED A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15950R 45903 FLT NR 021 - KDFW-KDAY - AFTER TAKEOFF UPLATCH CHECK WAS NOT GOOD. GEAR UNSAFE LIGHT ON. EXTENDED GEAR AND RETRACTED GEAR. WHEN UPLATCH CHECK WAS ATTEMPTED AGAIN, THE GEAR HANDLE WOULD NOT MOVE. UNABLE TO MOVE LONG HANDLE, SHORT HANDLE WAS PUT DOWN AND GEAR EXTENDED NORMALLY. RETURNED TO KDFW. MAINTENANCE FOUND SHEER PIN ON NOSE GEAR UPLATCH BROKEN LETTING UPLATCH ASSEMBLY DANGLE. S/D - MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLATCH SHEER PIN PER MM 32-31-6. AN OPERATIONAL CHECK OF THE LANDING GEAR RETRACTION SYSTEM WAS NORMAL. (M) 2L74 4F 4A25 19951201005471995120100547WP 1995 12 1 95ZZZM657 119951013A323057698712 ARM ASSY DOUG DC8 DC8F54 3021926WP RT MLG SHEARED A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15992CF 45884 FLT NR 517 - KPDX-KPIA - ON GEAR RETRACTION OUT OF KPDX, GEAR UNSAFE LIGHT AND RT ALTERNATE GEAR WARNING LIGHT CAME ON. ACCOMPLISHED QRH AND RETURNED TO KPDX. FOUND BOGIE UNLOCK SWIVEL ARM SHEARED. S/D - MAINTENANCE REMOVED AND REPLACED THE BOGIE PIVOT ARM IAW MM 32-11-61. AN OPERATIONAL CHECK WAS GOOD. 2L74 4F 4A25 19951201005481995120100548WP 1995 12 1 95ZZZM658 119951023A5245 DOOR DOUG DC8 DC863F 302198FWP A/C COMPT OUT OF ADJUST A RRXAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 WP15959R 46143 FLT MAC 111 - OMFJ-LICZ - AIRCRAFT EXPERIENCED RAPID DE-PRESSURIZATION AT FL 390. CABIN ALTITUDE STABILIZED AT 13,500 FEET. MAX CABIN DIFFERENTIAL AT 6.6 PSI. PERFORMED CHECKLIST IAW QRH. MAINTENANCE FOUND THE FORWARD AIR CONDITIONING ACCESS DOOR OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE ACCESS DOOR IAW EWA MM. GROUND PRESSURIZATION WAS GOOD. NO PRESSURIZATION DISCREPANCIES WERE REPORTED ON SUBSEQUENT FLIGHTS AS OF 10/24. 2L74 4F 4A25 19951201005491995120100549NM 1995 12 1 95ZZZM659 119950929A326087003 PSEU ELDEC DORNERDO32 DO328100 2996000NM RT AVIONICS RACKFAILED A EQGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW19328LS1879 23 3025 WHILE EN ROUTE TO CUU FROM DFW, THE AIRCRAFT HAD A PROXIMITY SYSTEM FAILURE. THE CREW RETURNED TO DFW AND MADE AN EMERGENCY LANDING DUE TO ALL THE FAILED SYSTEM INDICATIONS. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED FOR FERRY FLIGHT AND FERRIED TO HOT-MAINTENANCE. THE PSEU WAS REPLACED AND RETRACTION CHECKS PERFORMED. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 19951201005501995120100550NM 1995 12 1 95ZZZM660 119951022A27606517840118 RETURN LINE BOEING727 72722C 138400FNM NR 2 SPOILER CRACKED A RYNAO OTHER K FLUID LOSS CRCRUISE 1 CE07429EX 19100 EN ROUTE FROM IND TO DEN, THE AIRCRAFT STARTED LOOSING 'A' SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 2 SPOILER ACTUATOR RETURN LINE CRACKED AT T-FITTING B-NUT. REPLACED LINE, BOTH 'A' SYSTEM HYDRAULIC PUMPS AND 'A' SYSTEM RETURN FILTERS. 2L73 4F A3WE 19951201005511995120100551EU 1995 12 1 95ZZZM661 119951025A3610 POPPET VALVE BAG BAE146BAE146100A 1500260EU NR 1 ENGINE DIRTY A A6WAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL31463AP E1063 ENGINE 1 DOES NOT MAKE TAKEOFF POWER. CLEANED NR 1 ENGINE POPPET VALVES SUCCESSFULLY GROUND RAN NR 1 ENGINE TO ACTIVE TAKEOFF POWER. 2H74 4F RTA49EU 19951201005521995120100552EU 1995 12 1 95ZZZM662 119951011A2400 ELECT SYSTEM STBROSSD3 SD360 8100606EU LT/RT MALFUNCTIONED A ASABAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO05121PC SH3721 FLT NR 5087 - HAD JUST DEPARTED CLT WHEN THE AIRCRAFT EXPERIENCED A PARTIAL ELECTRICAL FAILURE. THE GROUND SERVICES BUS DROPPED OFF LINE, THE LT AND RT SHEDDING BUSSES DROPPED OFF LINE, PANEL 9P WENT BLANK. THE EMERGENCY LIGHTS C/B TRIPPED AND THE EMERGENCY LIGHTS CAME ON, AND THE CAPTAINS EHSI INDICATED FAIL. AFTER THE CAPTAIN HAD TALKED TO MAINTENANCE CONTROL ON THE RADIO AND TRIED TO RESET THE ESSENTIAL SERVICES TRANSFER RELAYS, RETURNED TO CLT AND MADE A SAFE UNEVENTFUL LANDING. UPON LANDING ALL EFFECTED SYSTEMS RETURNED TO NORMAL. MX PERSONNEL WAS DISPATCHED TO T\S THE PROBLEMS. A COMPLETE TEST OF THE ELECTRICAL SYSTEMS INVOLVED FOUND NO PROBLEMS. THE A/C WAS THEN RETURNED TO SERVICE. 2H72 4T A41EU 19951201005531995120100553NM 1995 12 1 95ZZZM663 119951008A3260MS253831 SWITCH BOEING727 72751C 1384015NM NR 3 THROTTLE INOP A RYNAO OTHER N FALSE WARNING CLCLIMB 1 CE07436EX 19289 ON GEAR RETRACTION ALL THREE GEAR UNSAFE LIGHTS REMAINED ON. GEAR DOOR LIGHTS OUT. REPLACED HORN AND WARNING CUT OUT SWITCH ON NR 3 ENGINE THROTTLE PER MM 31-26-13 AND 32-61-01. GEAR INDICATIONS AND HORN OPS CHECK NORMAL. (M) 2L73 4F A3WE 19951201005541995120100554NE 1995 12 1 95ZZZM664 219951010A73217436023 FUEL CONTROL BOEING727 72782C 1384026NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE FAILED A ARYNAE ENGINE SHUTDOWN O OTHER CLCLIMB 1 CE07528PC 19597 ON TAKEOFF AT 300 FT AGL, THE NR 1 ENGINE SHUT DOWN. FUEL FLOW WENT TO ZERO. ACCOMPLISHED APPROPRIATE CHECK LISTS AND LANDED WITHOUT INCIDENT. REPLACED FUEL CONTROL UNIT PER MM 73-21-1. REPLACED ENGINE DRIVEN FUEL PUMP PER 73-11-1 AS PRECAUTION. TRIMMED ENGINE PER MM 71-00-30. ENGINE OPS CHECK OK. 2L73 4F4 F A3WE E2EA 19951201005551995120100555CE 1995 12 1 95ZZZM665 119950915A575310116000144 SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07121ZR 2667 502 UC121 DURING ROUTINE MAINTENANCE, A CRACK AT THE OUTBOARD BUMPER STOP AND ON BOTTOM OF FLAP, AFT OF SPAR APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED WITH DOUBLERS. 2L72 4T RTA24CE 19951201005561995120100556WP 1995 12 1 95ZZZM666 119951010A32304783031A ACTUATOR PIN DOUG 5753118N DOUG DC8 DC862 3021970WP RT MLG BROKEN A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO191803 10007 DL210 45895 AFTER 13 MINUTES FLIGHT TIME, AIRCRAFT RETURNED TO BRO BECAUSE 'GEAR UNSAFE' LIGHT ILLUMINATED. FOUND RIGHT MLG RETRACT ACTUATOR PIN BROKEN. INSPECTED AIRCRAFT RIGHT MLG AND FOUND TO BE SAFE FOR GEAR DOWN AND PINNED FERRY TO MIAMI. REMOVED AND REPLACED PIN. LUBRICATED LANDING GEAR. OPS CHECK OK ON RETRACTION. 2L74 4F 4A25 19951201005571995120100557NE 1995 12 1 95ZZZM667 219951009A7261387188F RELIEF VALVE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 3 ENGINE STUCK OPEN A ARWAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO191804 523061447 45896 AFTER 27 MINUTES FLIGHT TIME, NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. ENGINE WAS SHUT DOWN AT 13:45Z. UPON INSPECTION AT BRO, FOUND OIL PRESSURE RELIEF VALVE NOT REGULATING. REPLACED RELIEF VALVE. ENGINE OPS CHECK NORMAL IAW MM 79-32-0. 2L74 4F4 F 4A25 1E8 19951201005581995120100558WP 1995 12 1 95ZZZM668 119951016A5730 SKIN DOUG DC8 DC862 3021970WP LT WING CORRODED A ARWAK NONE O OTHER ININSP/MAINT 1 SO191804 64515 45896 DURING B-3 INSPECTION, FOUND LEVEL 2 CORROSION AT LEFT WING LEADING EDGE ATTACH POINT STATION X 526. CORROSION REMOVED AND FOUND BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER OF .63 INCH 7075T6 AND .071 INCH 7075T6. PRIMED WITH ALODINE AND INSTALLED IAW SRM 51-1-8 AND JOSSAIR, INC EO ARW 950092-0011. 2L74 4F 4A25 19951201005591995120100559NM 1995 12 1 95ZZZM669 119950928A2750793T1005 MOTOR BOEING737 737214 138446RNM FLAPS INOP A ZZDAO OTHER J WARNING INDICATION LDLANDING 1 SO15460AT 20158 ON APPROACH WHEN FLAP HANDLE WAS SELECTED TO 15, THE FLAPS REMAINED AT 5. THE POSITION OF THE FLAP HANDLE HAD NO EFFECT ON THE FLAP POSITION BEYOND 5 DEGREES. INSPECTED FLAP SYSTEM AND FOUND ALTERNATE SYSTEM ALSO INOP. REPLACED ALTERNATE FLAP DRIVE MOTOR. FLAP DRIVE SYSTEMS NORMAL AND ALTERNATE CHECK SATISFACTORY. 2L72 4F A16WE 19951201005601995120100560NM 1995 12 1 95ZZZM670 119951102A2611302842 SMOKE DETECTOR BOEING727 72731 1384010NM NR 2 POSITION FAILED A RYNAO OTHER N FALSE WARNING CRCRUISE 1 CE07210NE 18903 CABIN SMOKE DETECTOR LIGHT ILLUMINATED IN FLIGHT AT FL 28,000 FT AND REMAINED ILLUMINATED UNTIL APPROX FL 3000 FT AT WHICH TIME IT EXTINGUISHED AND SYSTEM TESTED NORMAL. VISUALLY CONFIRMED NO SMOKE PRESENT AND LANDED AT DAYTON WITHOUT INCIDENT. REPLACED NR 2 SMOKE DETECTOR PER MM 26-17-0. OPS CHECKS NORMAL. (M) 2L73 4F A3WE 19951201005611995120100561NM 1995 12 1 95ZZZM671 119951103A27606517840409 RETURN LINE BOEING727 72776 1384016NM NR 2 SPOILER BROKEN A RYNAO OTHER JK WARNING INDICATION FLUID LOSS CRCRUISE 1 CE07721JE 18843 EN ROUTE FROM RIC TO IND, THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC PRESSURE AND QUANTITY. ACCOMPLISHED EMERGENCY CHECKLIST PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND 'A' SYSTEM RETURN LINE FROM NR 2 SPOILER ACTUATOR BROKEN. TRAILING EDGE COVE SUPPORT CHANNELS AND ROD ALSO, BROKEN UNDER NR 2 SPOILER. ALL DAMAGED PARTS REPLACED. 2L73 4F A3WE 19951201005621995120100562NM 1995 12 1 95ZZZM672 119951101A3260H1010153 LOCK SWITCH BOEING727 727231 1384079NM NLG MALFUNCTIONED A TWAAO OTHER P NO WARNING INDICATION CLCLIMB 1 CE0564322 20055 STL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE RED NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE. FOUND NOSE LANDING GEAR LOCK SWITCH, MFG P/N H10-1015-3, MALFUNCTIONING. REPLACED NOSE LANDING GEAR LOCK SWITCH AND NOSE LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL. 2L73 4F A3WE 19951201005631995120100563NE 1995 12 1 95ZZZM673 219951030A7261 ENGINE BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 4 OIL LEAK A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0553110 19676 JFK - DURING CRUISE SHUT DOWN NR 4 ENGINE, S/N 4199, DUE TO DECREASING OIL QUANTITY. FOUND OIL LEAKING IN ENGINE CORE. REPLACED NR 4 ENGINE AND ENGINE OPERATION CHECKED NORMAL. 2L74 4F4 F A20WE E20EA 19951201005641995120100564WP 1995 12 1 95ZZZM674 119951030A3222 SEALS DOUG DC9 DC983 3022083WP NLG STRUT FAILED A TWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE059307R 49663 STL - AFTER TAKEOFF NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE LANDING GEAR STRUT SEALS PREVENTING FULL EXTENSION OF NOSE LANDING GEAR STRUT. REPLACED NOSE LANDING GEAR STRUT SEALS AND NOSE LANDING GEAR OPERATION CHECKED NORMAL. 2L72 4F RTA6WE 19951201005651995120100565NM 1995 12 1 95ZZZM675 119951026A2530 OVEN BOEING747 747131 1384881NM GALLEY DIRTY A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0553116 20321 JFK - DURING CRUISE A STRONG NON-ELECTRICAL BURNING ODOR WAS DETECTED IN GALLEY 'A'. REMOVED AND REPLACED DIRTY OVEN, OPERATIONAL CHECK NORMAL. 2L74 4F A20WE 19951201005661995120100566WP 1995 12 1 95ZZZM676 119951029A33201125563 BALLAST LKHEED1011 10113851 5265010WP SERVICE CTR FAILED A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE0531019 193B1066 JFK - DURING CRUISE, DETECTED BURNING SMELL IN NR 1 SERVICE CENTER. REMOVED AND REPLACED BALLAST, MFG P/N 11-2556-3. OPERATIONAL CHECK OF BALLAST AND WIRING OK. 2L73 4F A23WE 19951201005671995120100567NM 1995 12 1 95ZZZM677 119951021A7930A008032 OIL BYPASS SW BOEING727 727231 1384079NM NR 3 ENGINE MALFUNCTIONED A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE0554327 20234 STL - DURING CLIMB, SHUT DOWN NR 3 ENGINE, S/N 3901, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND FILTER BYPASS PRESSURE SWITCH, MFG P/N A00803-2, MALFUNCTIONING. REPLACED OIL FILTER BYPASS SWITCH. ENGINE OPERATION AND OIL BYPASS LIGHT SYSTEM CHECKED NORMAL. (M) 2L73 4F A3WE 19951201005681995120100568NE 1995 12 1 95ZZZM678 219951022A731470530132 FUEL PUMP BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 2 ENGINE MALFUNCTIONED A TWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 CE0553116 20321 CDG - DURING CLIMB NR 2 ENGINE, S/N 4159, SPOOLED DOWN. SHUTDOWN ENGINE PER STANDARD PROCEDURES. FOUND ENGINE FUEL PUMP, MFG P/N 705301-32, MALFUNCTIONING. REPLACED ENGINE FUEL PUMP. ENGINE OPERATION CHECK NORMAL. 2L74 4F4 F A20WE E20EA 19951201005691995120100569NE 1995 12 1 95ZZZM679 219951019A7230 BEARING DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE NR 1 ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CE05931L 47173 2130 STL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION. FOUND METAL PARTICLES IN OIL FILTER. REPLACED ENGINE. GROUND OPERATION CHECKED NORMAL. INVESTIGATION OF OIL FILTER BYPASS LIGHT ILLUMINATION AND METAL PARTICLES FOUND IN OIL FILTER OF NR 1 ENGINE REVEALED NR 3 BEARING FAILED. REMOVED AND REPLACED NR 3 BEARING, AND ENGINE RETURNED TO SERVICE. (M) 2L72 4F4 F A6WE E2EA 19951201005701995120100570WP 1995 12 1 95ZZZM680 119951018A2810 FUEL TANK DOUG DC9 DC931 3022065WP CTR TANK LEAKING A TWAAO OTHER BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CRCRUISE 1 CE05988Z 47134 ATL - DURING CRUISE, FUEL SMELL DETECTED IN CABIN. FOUND FUEL LEAK FROM CENTER TANK IN RIGHT WHEEL WELL. 2L72 4F A6WE 19951201005711995120100571NE 1995 12 1 95ZZZM681 219951019A73143782017 FUEL PUMP BOEING727 727231 1384079NM PWA JT8 JT8D9 52048NE NR 3 ENGINE MALFUNCTIONED A TWAAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION CLCLIMB 1 CE0552312 19831 OKC - DURING CLIMB NR 3 ENGINE, S/N 1910, SPOOLED DOWN. SHUT DOWN ENGINE FUEL PUMP, MFG P/N 378201-7, MALFUNCTIONING. REPLACED ENGINE FUEL PUMP AND ENGINE PERFORMANCE CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 19951201005721995120100572WP 1995 12 1 95ZZZM682 119951016A5200 DOOR BEAM DOUG DC9 DC932 3022066WP NR 2 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05922L 47108 STL - DURING C-CHECK, FOUND TWO INCH CRACK IN NR 2 DOOR BEAM FORWARD END. REPAIRED PER SRM 51-30 AND STANDARD PRACTICES. 2L72 4F A6WE 19951201005731995120100573NM 1995 12 1 95ZZZM683 119951006A5320 WEB BOEING727 727231 1384079NM BS 948 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554327 20234 MCI - DURING C-CHECK, FOUND A TWO INCH CRACK BETWEEN BEADED EXTRUSION IN HORIZONTAL PRESSURE DECK WEB OF LEFT MLG WHEEL WELL, AFT OUTBOARD CORNER OF WHEEL WELL CEILING, BS 948, LBL 59. INSTALLED DOUBLER REPAIR PER SERVICE BULLETIN 727-53-0149, DRAWING 65-8960 AND TWA STANDARD PRACTICES. 2L73 4F A3WE 19951201005741995120100574WP 1995 12 1 95ZZZM684 119951006A5315 FLOOR BEAM DOUG DC9 DC951 3022051WP BS 239 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05418EA 47676 STL - DURING C-CHECK, FOUND A TWO INCH CRACK IN FLOOR BEAM AT CENTER AISLE AREA, STATION 239. REPAIRED PER ARA 8749. 2L72 4F A6WE 19951201005751995120100575NM 1995 12 1 95ZZZM685 119951006A5311 FRAME BOEING727 727231 1384079NM FS 783.85 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554327 20234 MCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN LEFT SIDE FRAME WEB, FS 783.85. STOP DRILLED CRACK AND REPAIRED PER SRM 51-10-1, PAGE 6A. 2L73 4F A3WE 19951201005761995120100576NM 1995 12 1 95ZZZM686 119951025A3260 DOOR SW BOEING727 727231 1384079NM RT MLG DOOR DIRTY A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE0554348 21967 IND - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN GEAR DOOR WARNING LIGHT REMAINED ON. GEAR CYCLED, LIGHT WENT OUT. INSPECTED AND CLEANED GEAR DOOR SWITCH. OPERATIONAL CHECK GOOD. 2L73 4F A3WE 19951201005771995120100577WP 1995 12 1 95ZZZM687 119951011A5330 SKIN LKHEED1011 1011385115 5265015WP FS 529-549 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531029 193B1109 MCI - DURING OP-16, FOUND CORROSION ON SKIN DOUBLER BETWEEN STRINGER 32 AND 33, FS 529 TO FS 549. REPAIRED PER SRM 53-31-00, FIGURE 826. 2L73 4F A23WE 19951201005781995120100578NM 1995 12 1 95ZZZM688 119951006A5713 STRINGER BOEING727 727231 1384079NM WS 656.56 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554327 20234 MCI - DURING C-CHECK, FOUND CRACK IN STRINGER FORWARD SIDE OF STRINGER TO RIB, INSIDE FUEL TANK, LEFT WING STATION 656.56. REPAIRED PER SRM 57-10-4, FIGURE 8 AND SERVICE BULLETIN 727-57A-159, FIGURE 4. 2L73 4F A3WE 19951201005791995120100579NM 1995 12 1 95ZZZM689 119951105A5753652678976A BRACKET BOEING727 72751C 1384015NM RT TE FLAP BROKEN A RYNAO OTHER O OTHER APAPPROACH 1 CE07435EX 19288 AS FLAPS WERE LOWERED TO 2 DEGREES FOR LANDING AT PHX ONLY INBOARD FLAPS EXTENDED, OUTBOARD FLAPS STAYED AT 0 DEGREES. ACCOMPLISHED SPLIT FLAPS CHECKLIST, HOWEVER, OUTBOARD FLAPS REMAINED AT 0 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT OUTBOARD FLAP JACKSCREW FAIRING BRACKET HAD BROKEN, CAUSING OUTBOARD FLAPS TO JAMB. REPLACED FAIRING AND RETURNED FLAP SYSTEM TO NORMAL OPS. 2L73 4F A3WE 19951201005801995120100580EU 1995 12 1 95ZZZM690 119951030A3320AL5113 CONNECTOR A212451220 BRAERODH125 HS125700A 4230170EU CABIN LIGHTS OVERHEATED AS KKYAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NE03270KA222 NA0307 EN ROUTE FROM BOS TO TEB, A PASSENGER REPORTED A BURNED PLASTIC SMELL IN THE CABIN, IT WAS TRACED TO A CABIN LIGHT BULB CONNECTION. THE LIGHT WAS DISCONNECTED AND THE SMELL WENT AWAY. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. AN INSPECTION OF THE AREA REVEALED THAT THE PLASTIC CONNECTOR ON A LIGHT BULB AND MATING CONNECTOR SHOWED SIGNS OF OVERHEATING. THE BULB AND CONNECTOR WERE REPLACED. THE APPARENT CAUSE OF THE OVERHEATING IS THE PIN IN CONNECTOR, PART NR AL5113, NOT BEING FULLY ENGAGED. 2L72 4F A3EU 19951201005811995120100581NE 1995 12 1 95ZZZM691 219951029A7200 ENGINE AMD FALC20FALCON 2720302EU GE CF700 CF7002D2 30010NE NR 1 FLAMED OUT A AFUBAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 NE0320AE 258 304443 WHILE LEVEL AT FL410 IN CRUISE, A MINOR THROTTLE ADJUSTMENT WAS MADE AND THE NR 1 ENGINE FLAMED OUT. THE CREW DESCENDED TO FL 270 AND PERFORMED A NORMAL AIRSTART. ENGINE PARAMETERS AFTER AIRSTART WERE NORMAL. A PRECAUTIONARY LANDING WAS MADE AT SPI. MAINTENANCE PERSONNEL PERFORMED FOD INSPECTION AND BOROSCOPED PER GE MAINTENANCE MANUAL. NO DEFECTS WERE NOTED. ENGINE WILL BE CHANGED AS PRECAUTIONARY MEASURE. 2L72 4F4 F A7EU E7EA 19951201005821995120100582NE 1995 12 1 95ZZZM692 219951004A726031010351 TQ SENSOR BRG GARRTT 8968268 MTSBSIMU2 MU2B36 5780412CE GARRTTTPE331TPE3316252M 01514NE NR 2 ENGINE FAILED A MUAAEA ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 GL23305CW5347 014565054 667 P20020C AT FL 150 IN LEVEL CRUISE CONDITIONS, THE NR 2 ENGINE FLAMED OUT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT IPT . TROUBLESHOOTING OF THE ENGINE REVEALED THE MAIN OIL AND SCAVENGE PUMPS NOT ROTATING, THESE PUMPS ARE DRIVEN BY THE TORQUE SENSOR, THE MAIN FUEL PUMP AND FUEL CONTROL ARE DRIVEN BY THE OIL PUMPS. ENGINE TEAR DOWN REVEALED THAT THE TORQUE SENSOR BEARINGS P/N 3103035-1 FAILED ALLOWING SPUR GEAR, P/N 896805-1, TO COCK AND SHATTER, THERE BY UNCOUPLING THE DRIVE TO THE PUMPS. THIS ENGINE HAD A LIMITED GEAR BOX REPAIR ACCOMPLISHED 47 HOURS PRIOR. SUBMITTER STATES, SUGGEST REPLACEMENT OF THE 3103035-1 BEARINGS ANYTIME THE TORQUE SENSOR IS DISTURBED. 1H72 3T RTA10SW E2WE 19951201005831995120100583WP 1995 12 1 95ZZZM693 119951108A3310 BALLAST DOUG DC8 DC873F 302199FWP COCKPIT FAILED A RRXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP15795FT 46103 FLT NR 026 - KDAY-KSEA - THE CENTER GLARESHEILD LIGHTS WENT BRIGHT THEN OUT. THIS WAS FOLLOWED BY SMOKE FROM THE FIRST OFFICERS RIGHT CONSOLE. MAINTENANCE FOUND THE GLARESHEILD FLOOD LIGHT BALLAST SHORTED. MAINTENANCE TRANSFERRED THE GLARESHEILD LIGHTING TO THE DMI LIST IAW MEL 33-1. 2L74 4F RT4A25 19951201005841995120100584WP 1995 12 1 95ZZZM694 119951014A3230 RETRACT MECH DOUG DC9 DC981 3022081WP RT MLG MALFUNCTIONED A A4JAO OTHER J WARNING INDICATION CLCLIMB 1 SO15817SJ 48051 HAD TO CYCLE LANDING GEAR AFTER TAKEOFF DUE TO RIGHT MAIN (P/N 59305935508) LANDING GEAR UNSAFE INDICATION (RED LIGHT). LIGHT WENT OUT AFTER RECYCLE. JACKED AIRCRAFT AND PERFORMED RETRACTION TEST. ALL GEAR INDICATIONS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951201005851995120100585WP 1995 12 1 AALA951804 119951013A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07481AA 49656 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 22E INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PASSENGER SEAT ROW 22E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19951201005861995120100586WP 1995 12 1 ASAA9580220 119951011A5320 SHEAR TIE DOUG DC9 DC982 3022082WP BS 750 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE FASTENERS AT Y750, LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-01. (M) 2L72 4F A6WE 19951201005871995120100587WP 1995 12 1 ASAA9580221 119951011A5320 WEB DOUG DC9 DC982 3022082WP BS 1302 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, WEB WAS FOUND CRACKED AT Y1302, X PLUS 50, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-01. (M) 2L72 4F A6WE 19951201005881995120100588WP 1995 12 1 ASAA9580222 119951011A5320 SHEAR TIE DOUG DC9 DC982 3022082WP BS 1041 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1041, X-1 TO X PLUS 15, Z-45. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 51-30-05 AND 53-03. (M) 2L72 4F A6WE 19951201005891995120100589WP 1995 12 1 ASAA9580223 119951011A53135911401103 LONGERON DOUG DC9 DC982 3022082WP BS 229 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SPLICE ON LONGERON 30L AT Y229, X-0, Z-51. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02 AND 53-02. (M) 2L72 4F A6WE 19951201005901995120100590WP 1995 12 1 ASAA9580224 119951011A5313277792232500 LONGERON DOUG DC9 DC982 3022082WP BS 229 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SPLICE ON LONGERON 29L AT Y229, X PLUS 7, Z-51. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-02. (M) 2L72 4F A6WE 19951201005911995120100591WP 1995 12 1 ASAA9580225 119951011A5347TMS6022044 SEAT TRACK DOUG DC9 DC982 3022082WP BS 237 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y237, X-25, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03 AND 53-05. (M) 2L72 4F A6WE 19951201005921995120100592WP 1995 12 1 ASAA9580226 119951011A5347TSM6019943 SEAT TRACK DOUG DC9 DC982 3022082WP BS 237 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y237, X-45, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M) 2L72 4F A6WE 19951201005931995120100593WP 1995 12 1 ASAA9580227 119951011A53203932140 CHANNEL SUPPORT DOUG DC9 DC982 3022082WP BS 165.5 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON CHANNEL SUPPORT AT Y165.5, X PLUS 7, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-14-01 AND 53-01. (M) 2L72 4F A6WE 19951201005941995120100594WP 1995 12 1 ASAA9580228 119951013A5320 CHANNEL DOUG DC9 DC982 3022082WP BS 1322 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON INTERCOSTAL CHANNEL AT Y1322, X-16, Z-38. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-02, 51-10-03, 51-30-05 AND 53-01. (M) 2L72 4F A6WE 19951201005951995120100595WP 1995 12 1 ASAA9580229 119951013A5311 FRAME DOUG DC9 DC982 3022082WP BS 1309 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON FRAME AT Y1309, X PLUS 16, Z-40. CORROSION REMOVAL WAS WITHIN LIMITS. DURING REMOVAL OF FASTENERS FOUND CRACK IN FRAME AT Y1309, X PLUS 2, Z-43. STOP DRILLED CRACK, NDI VERIFIED CONTAINMENT. FABRICATED PARTS AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-70-02 AND 53-01. (M) 2L72 4F A6WE 19951201005961995120100596WP 1995 12 1 ASAA9580230 119951013A5347TMS6019609 SEAT TRACK DOUG DC9 DC982 3022082WP BS 636-788 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS38207 49104 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y636 TO Y788, X PLUS 17. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M) 2L72 4F A6WE 19951201005971995120100597WP 1995 12 1 ASAA9580235 119951019A5210 LATCH MECHANISM DOUG DC9 DC982 3022082WP L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01933AS 49234 ANC - ON ARRIVAL OF FLIGHT 112, CREW REPORTED THE L1 DOOR LEVER LATCH DIFFICULT TO OPEN. LUBED LATCH MECHANISM AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19951201005981995120100598SO 1995 12 1 C2XA95IA314 119951020A523012020235005 BRACKET EMB 120 EMB120RT SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR COUNTER BALANCE MECHANISM FORWARD TORSION BAR MOUNT ATTACH BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201005991995120100599SO 1995 12 1 C2XA95IA315 119951020A534712016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. THE AFFECTED PORTIONS OF SEAT TRACK WERE REMOVED AND REPLACED BY MAINTENANCE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006001995120100600SO 1995 12 1 C2XA95IA316 119951020A534712015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0922727 120177 IAH - DURING C-CHECK INSPECTION, THE LEFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTIONS OF SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006011995120100601EU 1995 12 1 C2XA95IA317 119951023A5320S53372411200 SUPPORT AEROSPATR42 ATR42320 8680930EU CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914825 170 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 39 FLOOR SUPPORT BEAM CORRODED, AT FASTENER HOLES. MAINTENANCE REPAIRED THE SUPPORT BEAM USING ANGLE DOUBLER, AIRCRAFT APPROVED FOR RETURN TO SERVICE, REF EC 5310-01037. (M) 2H72 4T RTA53EU 19951201006021995120100602SO 1995 12 1 C2XA95IA318 119951101A3350F02A250V1A EEL FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0912703 120084 IAH - DURING PREFLIGHT, PILOT REPORTED SEVERAL AFT INTERNAL AND EXTERNAL EMERGENCY LIGHTS NOT ILLUMINATED. MAINTENANCE REPLACED THE FUSELAGE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006031995120100603SO 1995 12 1 C2XA95IA319 119951101A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 5 LOWER WING SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006041995120100604SO 1995 12 1 C2XA95IA320 119951101A572012017057005 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 4 LOWER WING SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006051995120100605SO 1995 12 1 C2XA95IA321 119951101A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16 NR 3 LOWER WING SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006061995120100606SO 1995 12 1 C2XA95IA322 119951101A532012004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, FOUND T-PROFILE CORRODED AT FRAME 16 LEFT. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AIRCRAFT APROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006071995120100607SO 1995 12 1 C2XA95IA323 119951101A532012004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, FOUND T-PROFILE CORRODED, LEFT CENTER AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006081995120100608SO 1995 12 1 C2XA95IA324 119951101A572012004345009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB NR 8 SUPPORT CRACKED AT STRINGER NR 10. MAINTENANCE STOP DRILLED, AND INSTALLED A REPAIR DOUBLER. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006091995120100609SO 1995 12 1 C2XA95IA325 119951101A532012020235001 BRACKET EMB 120 EMB120RT SO CARGO CEILING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, FOUND CARGO DOOR TORSION BAR FORWARD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED BRACKET WITH A MODIFIED ONE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951201006101995120100610NM 1995 12 1 CAL950888 119951003A3350 EEL EXIT SIGN BOEING737 7372C0 1384488NM R1 DOOR INOPERATIVE A CALAK NONE O OTHER ININSP/MAINT 1 SW0910242 20071 GSO - INSPECTION FOUND THE R-1 DOOR EMERGENCY EXIT LIGHT DIM. THE EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-101. (M) 2L72 4F A16WE 19951201006111995120100611WP 1995 12 1 CAL950919 119951013A5520 TRAILING EDGE DOUG DC10 DC1030 3023501WP RT ELEVATOR MISSING A CALAK NONE O OTHER ININSP/MAINT 1 SW091406285049 47863 FLT NR 0011 - ORY - A WALK AROUND INSPECTION, FOUND RIGHT INBOARD ELEVATOR TRAILING EDGE STRIP MISSING (APPROXIMATELY 24 INCHES). A PERMANENT REPAIR WAS PERFORMED PER SRM 55-30-00, FIGURE 2. (M) 2L73 4F A22WE 19951201006121995120100612WP 1995 12 1 CAL950920 119951016A275231758871 ACTUATOR DOUG DC10 DC1010 3022110WP LT TE FLAP INOPERATIVE A ACALAAJ UNSCHED LANDING DUMP FUEL JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SW096804724784 47801 FLT NR 0973 - GUM - THE FLAPS WOULD NOT FULLY RETRACT AFTER TAKEOFF FROM GUM. THE RIGHT SIDE WAS DRAGGING 3-4 DEGREES AND 3 DEGREES OF RIGHT RUDDER WAS REQUIRED FOR LEVEL FLIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GUM. THE FLAPS WOULD NOT EXTEND FOR LANDING AND A ZERO FLAP LANDING WAS PERFORMED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE INBOARD FLAP SELECTOR VALVE AND THE RESTRICTOR VALVES FOR ALL THREE FLAP SELECTOR VALVES, BUT THIS DID NOT CORRECT THE PROBLEM. THE LEFT OUTBOARD TRAILING EDGE FLAP INBOARD ACTUATOR AND THE LEFT INBOARD TRAILING EDGE FLAP OUTBOARD ACTUATOR WERE BOTH REMOVED AND REPLACED. THE FLAPS WERE OPERATED SEVERAL TIMES AND CHECKED GOOD. (M) 2L73 4F A22WE 19951201006131995120100613WP 1995 12 1 CAL950921 119951016A27523187007 ACTUATOR DOUG DC10 DC1010 3022110WP LT TE FLAP INOPERATIVE A ACALAAJ UNSCHED LANDING DUMP FUEL JF WARNING INDICATION FLT CONT AFFECTED CLCLIMB 1 SW096804723805 47801 FLT NR 0973 - GUM - THE FLAPS WOULD NOT FULLY RETRACT AFTER TAKEOFF FROM GUM. THE RIGHT SIDE WAS DRAGGING 3-4 DEGREES AND 3 DEGREES OF RIGHT RUDDER WAS REQUIRED FOR LEVEL FLIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GUM. THE FLAPS WOULD NOT EXTEND FOR LANDING AND A ZERO FLAP LANDING WAS PERFORMED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE INBOARD FLAP SELECTOR VALVE AND THE RESTRICTOR VALVES FOR ALL THREE FLAP SELECTOR VALVES, BUT THIS DID NOT CORRECT THE PROBLEM. THE LEFT OUTBOARD TRAILING EDGE FLAP INBOARD ACTUATOR AND THE LEFT INBOARD TRAILING EDGE FLAP OUTBOARD ACTUATOR WERE BOTH REMOVED AND REPLACED. THE FLAPS WERE OPERATED SEVERAL TIMES AND CHECKED GOOD. (M) 2L73 4F A22WE 19951201006141995120100614WP 1995 12 1 CAL950922 119950922A5320ADA02331 DOOR FRAME DOUG DC10 DC1030 3023501WP BS 895.7 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096806071601 47850 KUL - INSPECTION FOUND THE FORWARD CARGO LOWER DOOR FRAME CORRODED AT STATION 895.7. THE CORRODED AREA WAS REPAIRED IAW ECRA 5330-02320 AND SRM 53-13-01. (M) 2L73 4F A22WE 19951201006151995120100615WP 1995 12 1 CAL950923 119950921A5532 SKIN DOUG DC10 DC1030 3023501WP VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096806071601 47850 KUL - INSPECTION FOUND A 1.5 INCH CRACK IN SKIN UPPER SURFACE FORWARD OF VERTICAL STABILIZER REAR SPAR ON RIGHT SIDE. THE SKIN WAS REPAIRED IAW ECRA 5530-01159. (M) 2L73 4F A22WE 19951201006161995120100616NM 1995 12 1 CAL950933 119951018A2750 BEARING BOEING727 727224 1384076NM TE FLAP RUSTED A ACALAAJ UNSCHED LANDING DUMP FUEL F FLT CONT AFFECTED CLCLIMB 1 SW0979748 22450 FLT NR 0267 - EWR - THE TRAILING EDGE FLAPS WOULD NOT RETRACT BEYOND 3.5 DEGREES AFTER TAKEOFF FROM EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE FLAP HANDLE BINDING. THE INPUT CRANK IN RIGHT WHEEL WELL WAS DISCONNECTED AND THE FLAP HANDLE OPERATED FREELY. THE PULLEY WAS LUBRICATED AND CABLE RUNS AND CONTROL VALVES WERE INSPECTED. THE LOWER BEARING ON CONTROL DRUM WAS FOUND RUSTED. THE BEARING WAS REPLACED AND THE FLAPS WERE CYCLED SEVERAL TIMES WITH NO BINDING. (M) 2L73 4F A3WE 19951201006171995120100617NM 1995 12 1 CAL950934 119951018A27821U1110 ACTUATOR FTG BOEING727 727232 1384082NM NR 2 LE FLAP CRACKED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW091079117880 20645 FLT NR 0219 - EWR - THE 'A' SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW PRESSURE LIGHTS DURING CLIMB-OUT OF EWR. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH, FUEL WAS DUMPED, AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACUTATOR WAS REPLACED. ALL FLIGHT CONTROLS WERE CYCLED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L73 4F A3WE 19951201006181995120100618 1995 12 1 CAL950935 419951018A2300G5919 AUDIO SELECT PNL DOUG DC9 DC982 3022082WP NR 3 FAILED A CALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW091883324958 49493 FLT NR 0730 - DCA - THE NR 3 AUDIO SELECT PANEL BEGAN TO SMOKE IN FLIGHT. THE SMOKE CEASED AFTER THE CIRCUIT BREAKERS WERE PULLED AND THE UNIT WAS REMOVED FROM OVERHEAD PANEL. THE NR 3 AUDIO SELECT PANEL WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE GOOD. AN INSPECTION OF THE INSIDE OF THE REMOVED UNIT FOUND A BURNED CIRCUIT BOARD. (M) 2L72 4F A6WE 19951201006191995120100619WP 1995 12 1 CAL950936 119951018A4900 ACTUATOR GARRTT 3812761 DOUG DC9 DC982 3022082WP APU INOPERATIVE A CALAO OTHER O OTHER CRCRUISE 1 SW0969803 P500 49229 FLT NR 0594 - EWR - THE APU AUTO SHUT DOWN IN FLIGHT AND CONTINUED TO WINDMILL 8-10 PERCENT AFTER MASTER SWITCH WAS TURNED OFF. MAINTENANCE REMOVED AND REPLACED BENT NON-RAM DOOR ACTUATOR PER MM 49-10-00. AN OPERATIONAL CHECK WAS PERFORMED AND NO DEFECTS WERE NOTED. (M) 2L72 4F A6WE 19951201006201995120100620WP 1995 12 1 CAL950937 119951018A29107936907665 HYD LINE DOUG DC9 DC981 3022081WP RUDDER LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0913881 48045 FLT NR 0378 - BOS - THE RIGHT HYDRAULIC QUANTITY BEGAN TO DROP RAPAIDLY WHILE CLIMBING THROUGH 1700 FEET LEAVING EWR, BOUND FOR BOS. THE FLIGHT MANUAL PROCEDURES WERE FOLLOWED AND THE LANDING GEAR WAS EXTENDED MANUALLY FOR AN UNEVENTFUL LANDING AT BOS. MAINTENANCE FOUND THE RUDDER POWER HYDRAULIC SUPPLY LINE LEAKING AT B-NUT. THE LINE WAS REMOVED AND A HYDRAULIC FLEX LINE WAS INSTALLED. A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 500 FLIGHTS OR 1200 FLIGHT HOURS, WHICHEVER OCCURS FIRST. LEAK CHECKS WERE GOOD. (M) 2L72 4F A6WE 19951201006211995120100621WP 1995 12 1 CAL950938 119951018A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW099287442231 49122 HOU - INSPECTION FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT LOWER NR 1 VHF FORWARD ANTENNA. THE SKIN WAS REPAIRED IAW EA 5330-01823. (M) 2L72 4F A6WE 19951201006221995120100622WP 1995 12 1 CAL950939 119951018A325049206301 ACTUATOR PIN DOUG DC9 DC932 3022066WP NLG STEERING SHEARED A CALAK NONE O OTHER ININSP/MAINT 1 SW0943537 47112 DHN - INSPECTION FOUND THE NLG RIGHT NOSE STEERING ACTUATOR PIN SHEARED. THE STEERING CONTROL LEVER ASSEMBLY AND RIGHT NOSE STEERING CYLINDER ASSEMBLY WERE REMOVED AND REPLACED. (M) 2L72 4F A6WE 19951201006231995120100623NM 1995 12 1 CAL950940 119951019A3234 GEAR HANDLE BOEING727 727227 1384078NM COCKPIT LACK OF LUBE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0979754 21363 FLT NR 0299 - MIA - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO MIA, ALL THREE GREEN GEAR LIGHTS AND ALL THREE RED GEAR UNSAFE LIGHTS ILLUMINATED. THE GEAR WAS CYCLED AND CREW RECEIVED THREE GREEN GEAR INDICATION LIGHTS WITH NO RED LIGHTS. THE GEAR HANDLE HAD BEEN STICKY AND DID NOT GO INTO DETENT ON FIRST ATTEMPT. MAINTENANCE LUBRICATED THE GEAR HANDLE. A LANDING GEAR OPERATIONAL CHECK WAS PERFORMED IAW MM 32-30-00 AND OPERATION WAS GOOD. (M) 2L73 4F A3WE 19951201006241995120100624WP 1995 12 1 CAL950941 119951019A3350 EEL PIN DOUG DC10 DC1030 3023501WP CABIN LOOSE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914062 47863 LAX - FLT NR 0063 - ROWS 19-33, INCLUDING OVERWING EMERGENCY LIGHTS COME ON WHEN POWER IS SHUTOFF. FOUND PIN 'V' DISARMED, PUSHED PIN BACK IN AT CONNECTOR. (M) 2L73 4F A22WE 19951201006251995120100625NM 1995 12 1 CAL950944 119951021A2613894261001 OVERHEAT LIGHT BOEING737 737217 1384464NM NR 1 ENGINE ILLUMINATED A CALAO OTHER N FALSE WARNING CLCLIMB 1 SW0912230 19884 FLT NR 1444 - EWR - AIRCRAFT INBOUND, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATES WITH THROTTLE ADVANCE. RETURNED TO BASE. MAINTENANCE REPLACED CONNECTOR AND ELEMENTS. (M) 2L72 4F A16WE 19951201006261995120100626NM 1995 12 1 CAL950945 119951021A5330 SKIN BOEING737 7373T0 1384582NM BS 500 DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0969351 23589 FLT NR 1627 - EWR - FUSELAGE SKIN DAMAGED AT FS 500. REPAIRED AREA PER SRM 53-00-01 PG 204/206 SRM 53-00-07 PG 212/214 AND 51-70-11 PG 116. (M) 2L72 4F RTA16WE 19951201006271995120100627NM 1995 12 1 CAL950946 119951021A5320 SILL PLATE BOEING737 7373T0 1384582NM AFT CARGO PIT DAMAGED A CALAK NONE O OTHER ININSP/MAINT 1 SW0960312 23363 FLT NR 0653 - CLE - REPAIRED AFT CARGO PIT SILL PLATE HAD .75 INCH HOLE PER ECRA 5310-01126 STOPPED DRILLED AND SEALED TO BE WELDED WITHIN 100 FLT HOURS. (M) 2L72 4F RTA16WE 19951201006281995120100628NM 1995 12 1 CAL950947 119951022A2750 RETRACT MECH BOEING727 727224 1384076NM TE FLAPS JAMMED A ACALAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 SW0979746 22449 FLT NR 0294 - EWR - DURING LANDING, FLAPS JAMMED AT 5 DEGREES, HANDLE SET AT 25 DEGREES HAD SPLIT INDICATION. PERFORMED ONE GO AROUND 'NO EMERGENCY DECLARED'. (M) 2L73 4F A3WE 19951201006291995120100629NM 1995 12 1 CAL950965 119951024A531165C2511312 FRAME BOEING737 737222 1384473NM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATELY .75 INCH AT BS 500A BETWEEN S20R AND S21R, REMOVED AND REPLACED. (M) 2L72 4F A16WE 19951201006301995120100630NM 1995 12 1 CAL950966 119951024A531154C251132 FRAME BOEING737 737222 1384473NM BS 400 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023662342 19937 GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND CRACK APPROXIMATELY .75 INCH IN FRAME SEGMENT AT BS 400 BETWEEN S21L AND S22L, REMOVED AND REPLACED. (M) 2L72 4F A16WE 19951201006311995120100631NM 1995 12 1 CAL950967 119951024A531165C2511311 FRAME BOEING737 737222 1384473NM BS 500 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091023663432 19937 GSO - AIRCRAFT IN D-CHECK, FOUND CRACK IN FRAME SEGMENT APPROXIMATLY .75 INCH AT BS 500A BETWEEN S20L, S21L, AND ABOVE S23L, REMOVED AND REPLACED. (M0 2L72 4F A16WE 19951201006321995120100632NM 1995 12 1 CAL950968 119951024A3350 BATTERY PACK BOEING737 737222 1384473NM L-1 SLIDE LIGHT DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09102366234262342 19937 GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND BATTERY PACK INOP. REPLACED BATTERY PACK FOR L-1 SLIDE. (M) 2L72 4F A16WE 19951201006331995120100633NM 1995 12 1 CAL950969 119951024A3350 BATTERY PACK BOEING737 737222 1384473NM LT EMER EXIT DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09102366343263432 19937 GSO - AIRCRAFT IN 1/2 D-CHECK, FOUND LEFT EXTERNAL EMERGENCY LIGHT INOP. REPLACED LEFT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M) 2L72 4F A16WE 19951201006341995120100634NM 1995 12 1 CAL950970 119951024A3350 BATTERY PACK BOEING737 737222 1384473NM RT EMER EXIT DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09102366334263342 19937 GSO - EXIT LIGHT INOP. REPLACED RIGHT EXTERNAL EMERGENCY EXIT LIGHT BATTERY PACK AND BATTERY. (M) 2L72 4F A16WE 19951201006351995120100635NM 1995 12 1 CAL950976 119951020A5330 SKIN BOEING727 727227 1384078NM BS 590/617 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW099976357423 20772 IAH - INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 590, S26L AND BS 617 S26L. THE CORODED AREA AT EACH STATION WAS APPROXIMATELY 2 INCHES SQUARE. THE SKIN WAS REPAIRED IAW SRM 53-30-3, PAGE 76-80A, DETAIL IV, FIGURE 14. (M) 2L73 4F A3WE 19951201006361995120100636NM 1995 12 1 CAL950980 119951027A278265446518 ACTUATOR BOEING737 737130 1384435NM NR 4 SLAT INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW097720415570 19021 FLT NR 1598 - GSO - THE NR 4 SLAT WOULD NOT RETRACT DURING CLIMB-OUT OF GSO, THE AIRCRAFT WAS RETURNED TO GSO. MAINTENANCE FOUND THE NR 4 LEADING EDGE SLAT ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L72 4F A16WE 19951201006371995120100637NM 1995 12 1 CAL950986 119951030A3260 M982 CARD BOEING737 7373T0 1384582NM RT MLG IND INOPERATIVE A CALAO OTHER P NO WARNING INDICATION APAPPROACH 1 SW0917345 23583 FLT NR 0309 - PHX - THE RIGHT MLG RED LIGHT DID NOT ILLUMINATE DURING GEAR TRANSIT TO EXTENDED POSITION. THE GEAR WAS RAISED AND THE RED LIGHT REMAINED OFF. THE GEAR WAS EXTENDED AGAIN AND ALL INDICATIONS WERE NORMAL. MAINTENANCE RESEATED THE M982 LOGIC CARD ON THE E11 LG LOGIC SHELF PER MM 32-61-00. THE SYSTEM TESTED NORMAL. (M) 2L72 4F RTA16WE 19951201006381995120100638WP 1995 12 1 CAL950999 119951017A5320 SUPPORT BEAM DOUG DC10 DC1030 3023501WP UNDER GALLEY NR2CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096806574346 46590 KUL - INSPECTION FOUND CABIN FLOOR BOARD SUPPORT BEAM CORRODED UNDER GALLEY NR 2. A REPAIR WAS PERFORMED IAW SRM 53-22. (M) 2L73 4F A22WE 19951201006391995120100639WP 1995 12 1 CAL951000 119951019A5320 SUPPORT BEAM DOUG DC10 DC1030 3023501WP UNDER LAV 'B' CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW096806574346 46590 KUL - INSPECTION FOUND CABIN FLOOR BOARD SUPPORT BEAM CORRODED UNDER LAV 'B'. THE SUPPORT BEAM WAS REPLACED IAW SRM 53-22. (M) 2L73 4F A22WE 19951201006401995120100640WP 1995 12 1 CKSA95061 119950628A5330 SKIN DOUG DC8 DC863F 302198FWP BS 1660 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23867BX74760 46049 KYIP - DURING B-CHECK INSPECTION, FOUND FUSELAGE SKIN BULGING FROM CORROSION AT STATION 1660, LONGERON 30L. REPAIRED FUSELAGE SKIN AT STATION 1660, LONGERON 30L IAW EA NR 95-178. (M) 2L74 4F 4A25 19951201006411995120100641WP 1995 12 1 CKSA95064 119950711A5315 FLOOR BEAM DOUG DC8 DC8F54 3021926WP FS 440 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23806CK60926 45932 KOSC - DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOOR BEAM WEB AT LIGHTING HOLE AT RIGHT END STATION 440 'A' PIT. REMOVED CORROSION IAW SRM 51-1-6 FABRICATED AND INSTALLED PART IAW ENGINEERING SKA95118-1. COMPLIED WITH AIA EA95-176. (M) 2L74 4F 4A25 19951201006421995120100642WP 1995 12 1 HALA95138 119951021A3020 GASKET DOUG DC9 DC951 3022051WP NR 1 ENGINE BLOWN A HALAK NONE J WARNING INDICATION CLCLIMB 1 WP13674MC 47735 HNL - FLT NR 167 - ON CLIMB-OUT, AFTER POWER WAS SET 'FIRE DETECTION LOOP' ANNUNCIATED AND RIGHT ENGINE LOOP 'A' ILLUMINATED. SELECTED LOOP 'B' PER CHECK LIST AND LIGHTS WENT OUT. DURING CLIMB-OUT RIGHT ENGINE OIL PRESSURE WAS 54 PSI, CRUISE 52 PSI WITH NEEDLE BOUNCING 2 PSI. FOUND 13TH STAGE NOSE COWL DE-ICE VALVE GASKET BLOWN AND OIL PRESSURE LOW LIGHT SWITCH SEPARATED AT SOLDER JOINT. REPLACED GASKET ON 13TH STAGE NOSE COWL DE-ICE VALVE AND OIL LOW PRESSURE SWITCH. LEAK CHECK GOOD. OPERATIONAL CHECK OF 'A' LOOP GOOD. (M) 2L72 4F A6WE 19951201006431995120100643WP 1995 12 1 HALA95139 119951022A3350P4010049 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13603DC 4006 47784 IN C-CHECK, EMERGENCY FLOOR LIGHTS VERY DIM. REPLACED EMERGENCY FLOOR LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951201006441995120100644NM 1995 12 1 IXKA9500030 119951023A326022BBRC10147S CONNECTOR BOEING727 727225 1384077NM RT MLG DOOR DEFECTIVE A IXKAO OTHER P NO WARNING INDICATION DEDESCENT 1 EA258882Z 21579 INBOUND TO ATL, FLT NR 47, RIGHT GEAR DOOR WARNING LIGHT DID NOT COME ON WHEN GEAR WAS PUT UP OR DOWN AT FE PANEL. REMOVED AND REPLACED DEFECTIVE CANNON PLUG ON RIGHT DOOR WARNING SWITCH, PER MM 32-62-0, OPS CHECKED OK. (M) 2L73 4F A3WE 19951201006451995120100645WP 1995 12 1 IXXA199589 119951021A3260DS073S411 CONNECTOR DOUG DC8 DC871 302199AWP RT MLG DOOR DETERIORATED A IXXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL23824BX 45946 WHEN THE LANDING GEAR UPLATCH CHECK WAS PERFORMED ON DEPARTURE OUT OF TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON. THE AIRCRAFT ELECTED TO RETURN TO TOL FOR MAINTENANCE. TOL MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE ELECTRICAL CONNECTOR FOR THE RIGHT MLG DOOR UPLOCK SWITCH WAS IN POOR CONDITION DUE TO DETERIORATION OF THE INSULATOR. THE CONNECTOR WAS REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951201006461995120100646WP 1995 12 1 IXXA199590 119951021A2910AN624610 SEAL DOUG DC8 DC863 302198AWP RT HYD MANIFOLD LEAKING A IXXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL23788AL 45999 ON TAKEOFF OUT OF SJU, LOSS OF HYDRAULIC QUANTITY WAS NOTED BY THE FLIGHT CREW. THE AIRCRAFT RETURNED TO SJU FOR MAINTENANCE. UPON ARRIVAL AT SJU, ALL HYDRAULIC QUANTITY HAD BEEN LOST. SJU MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A HYDRAULIC LEAK ON THE RIGHT HYDRAULIC MANIFOLD AT THE SLOT CONTROL VALVE. THE VALVE WAS RESEALED AND LEAK CHECKED. THE HYDRAULIC SYSTEM WAS OPS CHECKED, AND A FINAL RESERVICING WAS ACOMPLISHED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951201006471995120100647WP 1995 12 1 IXXA199591 119951021A2910436392212 SEAL DOUG DC8 DC863 302198AWP RT HYD MANIFOLD LEAKING A IXXAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 GL23788AL 45999 EN ROUTE FROM SJU TO BDL, ALL HYDRAULIC QUANTITY WAS LOST. THE AIRCRAFT DIVERTED TO ATL FOR MAINTENANCE. MAINTENANCE INSPECTED THE AIRCRAFT ON THE GROUND IN ATL AND FOUND A HYDRAULIC LEAK AT THE FLAP CONTROL VALVE ON THE RIGHT HYDRAULIC MANIFOLD. THE SEALS WERE REPLACED UNDER THE FLAP CONTROL VALVE AND THE SYSTEM LEAK CHECKED. THE HYDRAULIC SYSTEM WAS OPS CHECKED, AND RECEIVED A FINAL SERVICING. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L74 4F 4A25 19951201006481995120100648SW 1995 12 1 MALA954587 119950820A52102724180117 BUSHING SWRNGNSA227 SA227AC 8780603SW CABIN DOOR WORN A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL15159MC AC728B FLT 3220 - ON CLIMB-OUT FROM MSP, THE CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP. REPAIRS WERE COMPLETED BY REPLACING THE BUSHING FOR THE UPPERMOST BAYONET. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951201006491995120100649SW 1995 12 1 MALA954641 119950920A5712 RIB SWRNGNSA227 SA227AC 8780603SW WS 100.6 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15436MA AC719 DURING A SCHEDULED INSPECTION IN DTW, THE LEFT AFT FLAP ACTUATOR RIB CONTOUR FLANGE AT WS 100.6 WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW FAC ARP 57-20-9007. (M) 1L72 4T A8SW 19951201006501995120100650SW 1995 12 1 MALA954642 119950921A2435230790001 STARTER GEN SWRNGNSA227 SA227AC 8780603SW RT ENGINE FAILED A MALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 GL15436MA AC719 FLT NR 3084 - AFTER TAKEOFF IN MSP, THE BATTERY FAULT, BOTH BATTERY DISCONNECT, AND THE RIGHT GENERATOR FAIL LIGHT ILLUMINATED. THE CREW PERFORMED TH QUICK REFERENCE CHECKLIST AND RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT STARTER/GENERATOR. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951201006511995120100651NM 1995 12 1 MALA954644 119950923A335010005511 EEL DHAV DHC8 DHC8102 2809003NM COCKPIT FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15849MA 347 FLIGHT 3426 - DURING THE PREFLIGHT IN DTW, THE COCKPIT OVERHEAD EMERGENCY LIGHT ILLUMINATED WHEN THE SYSTEM IS ARMED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951201006521995120100652NM 1995 12 1 MALA954645 119950922A33506104781 EEL BATT PACK DHAV DHC8 DHC8102 2809003NM CABIN FAILED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15817MA 249 DURING MAINTENANCE IN DTW, THE LEFT FORWARD EMERGENCY EXIT LIGHT WAS INOP. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19951201006531995120100653SW 1995 12 1 MALA954647 119950926A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M) 1L72 4T A8SW 19951201006541995120100654SW 1995 12 1 MALA954648 119950926A5400 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED A DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M) 1L72 4T A8SW 19951201006551995120100655SW 1995 12 1 MALA954649 119950926A5522 SKIN SWRNGNSA227 SA227AC 8780603SW RT ELEV CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT ELEVATOR SKIN UNDER A STATIC WICK BASE. THEY REMOVED AND DAMAGED AREA AND INSTALLED AN EXTERNAL DOUBLER AND FILLER IAW FAIRCHILD SRM 51-90-04. (M) 1L72 4T A8SW 19951201006561995120100656SW 1995 12 1 MALA954650 119950926A5320 SKIN SWRNGNSA227 SA227AC 8780603SW BATT BOX CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL152693C AC659B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK AT THE RIGHT WING AFT OUTBOARD BATTERY BOX CORNER. THEY REPAIRED THE CRACK BY REMOVING THE SKIN SEGMENT AND INSTALLING A STAINLESS FILLER AND SPLICE PLATE. (M) 1L72 4T A8SW 19951201006571995120100657SW 1995 12 1 MALA954651 119950926A61208975428 SWITCH SWRNGNSA227 SA227AC 8780603SW RT PROP STICKING A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1526906 AC654B FLT 3242 - AFTER TAKEOFF FROM MSP, THE RIGHT BETA LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE RIGHT BETA SWITCH TO BE STICKING AND REPLACED THE SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19951201006581995120100658SW 1995 12 1 MALA954652 119950927A5400 FORMERS SWRNGNSA227 SA227AC 8780603SW LT/RT NACELLES CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT INBOARD AND RIGHT INBOARD NACELLE FORMERS CRACKED. THEY REPAIRED THE CRACKS BY STOP DRILLING AND INSTALLING A DOUBLER IAW FAIRCHILD SRM 54-90-10. (M) 1L72 4T A8SW 19951201006591995120100659NM 1995 12 1 MALA954653 119950927A534785320490 SEAT TRACK DHAV DHC8 DHC8102 2809003NM BS 231 CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15829MA 335 DURING A SCHEDULED INSPECTION IN BNA, MAINTENANCE FOUND THE LEFT INBOARD SEAT TRACK AT STATION X231.0 TO BE HEAVILY CORRODED. REPAIRS WERE COMPLETED BY REPLACING THE SECTION IAW DEHAVILLAND RD8-53-1491. (M) 2H72 4T RTA13NM 19951201006601995120100660NM 1995 12 1 MRKA9577 119951011A3350BPS73 EEL BATT CHARGER BOEING737 73725A 1384481NM CABIN INOP A MRKAK NONE L NO TEST ININSP/MAINT 1 AL03685MA 23791 RIGHT AFT EMERGENCY LIGHTS INOP. WILL NOT TEST. REMOVED AND REPLACED RIGHT AFT EMERGENCY BATTERY CHARGER. LIGHT OPS NOW NORMAL. (M) 2L72 4F RTA16WE 19951201006611995120100661EU 1995 12 1 P2RA950017 119951026A2611 SMOKE DETECTOR AIRBUS300 A300B4203 3930306EU CARGO COMPT MALFUNCTIONED A P2RAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP2314976 271 FORWARD CARGO COMPARTMENT SMOKE DETECTOR LIGHT AND MASTER WARNING PANEL LIGHT CAME ON DURING TAXI. INSPECTED FORWARD CARGO COMPARTMENT SMOKE DETECTOR AND FOUND CARGO COMPARTMENT LIGHT EXTINGUISHED. OPS CHECKED SYSTEM AND CHECKED GOOD. (M) 2L72 4F A35EU 19951201006621995120100662EU 1995 12 1 P2RA950018 119951027A335010051911 EEL GRIMES 33000469 AIRBUS300 A300B4203 3930306EU CABIN INOPERATIVE A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314975 1311 261 OVERHEAD EMERGENCY LIGHT AT B-ZONE RIGHT NR 2 IS INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT AT B-ZONE RIGHT NR 2. OPS CHECKED GOOD. (M) 2L72 4F A35EU 19951201006631995120100663CE 1995 12 1 PLGA101995E 119951019A27205052432626 PEDAL BEECH 1900 1900C 1154161CE CAPT RT RUDDER BROKEN A APLGAO OTHER O OTHER TXTAXI/GRND HDL 1 NE05810BE UB48 DURING TAXI IN FROM FLT NR 4453 - THE CAPTAINS RIGHT RUDDER PEDDLE ARM BROKE OFF. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT, AND FOUND ARM HAD FAILED AT PEDAL PIVOT POINT. THE ARM WAS REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 2L72 4T RTA24CE 19951201006641995120100664EU 1995 12 1 PLGA92795E1 119950927A5270 SWITCH SAAB SF340 SF340A 7850100EU CABIN DOOR OUT OF ADJUST A PLGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE05340BE 340A062 FLT NR 4561 - BOS-ACK - DURING CLIMB-OUT, THE MAIN CABIN DOOR HANDLE WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE DOOR WAS CONFIRMED LATCHED AND THE DOOR WARNING HANDLE LIGHT WAS DEFERRED PER MEL 57-70-1. AIRCRAFT WAS RETURNED TO SERVICE. ON SEPT 28, THE SWITCH FOR THE HANDLE LIGHT WAS ADJUSTED AND THE SYSTEM OPS CHECKED GOOD. MEL SIGNED OFF AND AIRCRAFT RELEASED TO SERVICE. (M) 2L72 4T RTA52EU 19951201006651995120100665CE 1995 12 1 PLGA92895G1 119950928A57301141100403 SKIN BEECH 1900 1900C 1154161CE WS 151 CRACKED A PLGAK NONE O OTHER ININSP/MAINT 1 NE05815BE UB54 DURING PILOT PREFLIGHT, A 3.5 INCH SPANWISE UPPER WING SKIN CRACK WAS NOTED ON THE LEFT WING. THE CRACK WAS CENTERED AT APPROXIMATELY LWS 151.0, 22.5 INCH AFT OF WING SPAR CENTER LINE. CRACK WAS REPAIRED IAW BEECH DWG FR-60-00001 AND BEECH SRM. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19951201006661995120100666EU 1995 12 1 RAIA951014 119951008A3350311701 EEL BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03431AM9839 881 EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED ALL EMERGENCY LIGHTING BATTERIES. (M) 2L72 4T RTA56EU 19951201006671995120100667EU 1995 12 1 RAIA951015 119951008A33503012001 EEL POWER SUPPLY AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03722TE9435 1563 220 EMERGENCY TRACK LIGHTING INOP FROM ROW 8 AFT. MAINTENANCE REPLACED EMERGENCY LIGHTING POWER SUPPLY. (M) 2H72 4T RTA53EU 19951201006681995120100668EU 1995 12 1 RAIA951016 119951012A3230PVX62461PWR CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT MLG DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03339TE7325 935 STL - FLT 7416 - GEAR WOULD NOT RETRACT WHEN SELECTED UP. MAINTENANCE CLEANED CONNECTOR ON GEAR SELECTOR VALVE. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19951201006691995120100669EU 1995 12 1 RAIA951017 119951012A2913PV304426 HYD PUMP BAG JETSTMJETSTM3201 1500217EU RT ENG LOW PRESS A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03432AM5619 883 MWA - FLT NR 7350 - HYDRAULIC OVER PRESSURE CAPTION CAME ON. MAINTENANCE ADJUSTED RIGHT PRESSURE ON HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006701995120100670EU 1995 12 1 RAIA951018 119951009A21501531D000 ACM BAG JETSTMJETSTM3201 1500217EU LT/RT REQ'D SERVICE A RAIAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03339TE7325 935 STL - FLT NR 7493 - STRONG 'OIL' SMELL COMING FROM LEFT AND RIGHT FLOW WHEN TEMP CONTROL IS SELECTED. MAINTENANCE SERVICED LEFT AND RIGHT ACM RAN AIRCRAFT SYSTEM CHECKS GOOD. (M) 2L72 4T RTA56EU 19951201006711995120100671EU 1995 12 1 RAIA951019 119951014A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03428AM 877 STL - FLT NR 7341 - RIGHT ENGINE ACHIEVED 90 PERCENT TORQUE. MAINTENANCE RECALIBRATED RIGHT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SHEETS. CHECKED FOR BLEED LEAKS. GROUND RUN ENGINE PERFORMANCE CHECK GOOD. NO BLEED LEAKS FOUND. (M) 2L72 4T RTA56EU 19951201006721995120100672 1995 12 1 RAIA951021 419951015A34227000622901 VERT GYRO BAG JETSTMJETSTM3201 1500217EU NR 1 FAILED A RAIAO OTHER I FLT. ATTITUDE INST. CRCRUISE 1 CE03339TE7278 935 STL - FLT 7370 - LEFT ATTITUDE INDICATOR DISPLAYS A 20 DEGREE LEFT BANK IN STRAIGHT AND LEVEL FLIGHT. MAINTENANCE REPLACED NR 1 VERTICAL GYRO. SYSTEM CHECKS GOOD. (M) 2L72 4T RTA56EU 19951201006731995120100673WP 1995 12 1 RAIA951022 219951017A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03431AM 881 66192 JLN - FLT NR 7060 - LEFT ENGINE DID NOT MAKE TORQUE. MAINTENANCE REPLACED LEFT ENGINE BLEED AIR GASKETS. GROUND PERFORMANCE RUNS OK. (M) 2L72 4T4 TRTA56EU E4WE 19951201006741995120100674EU 1995 12 1 RAIA951023 119951016A7921HTE860028 OIL COOLER BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03343TE2292 955 DEC - FLT 7291 - LEFT OIL COOLER FLAP STUCK OPEN. MAINTENANCE REPLACED LEFT OIL COOLER ACTUATOR. SYSTEM CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006751995120100675EU 1995 12 1 RAIA951024 119951017A3350311701 BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03867AE9652 9652 867 MX - STATION 130 EMERGENCY LIGHT BATTERY INOP. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERIES. (M) 2L72 4T RTA56EU 19951201006761995120100676EU 1995 12 1 RAIA951025 119951018A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03434AM9044 5461 887 STL - FLT 7448 - LEFT ENGINE 5 PERCENT SHY TARGET TORQUE. MAINTENANCE RECALIBRATED LEFT TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SHEETS. GROUND RUNS CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006771995120100677EU 1995 12 1 RAIA951026 119951018A527091SE13 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03341TE6921 950 STL - FLT NR 7312 - PASSENGER DOOR LIGHT ILLUMINATED. MAINTENANCE ADJUSTED CENTER FLOOR MICRO-SWITCH, OPERATIONAL DOOR CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006781995120100678 1995 12 1 RAIA951027 319951020A6112 DE-ICE SYSTEM BAG JETSTMJETSTM3201 1500217EU NR 2 PROP INOP A RAIAO OTHER O OTHER CRCRUISE 1 CE03422AM 856 STL - FLT NR 7532 - RIGHT PROP DE-ICE FAILED. MAINTENANCE REMOVED AND REPLACED RIGHT PROPELLER ASSEMBLY, GROUND RUNS OPS CHECKED GOOD. (M) 2L72 4T RTA56EU 19951201006791995120100679EU 1995 12 1 RAIA951028 119951022A2910137311D1619 LINE BAG JETSTMJETSTM3201 1500217EU LOWER FUSE CRACKED A RAIAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 CE03862JX9033 862 PSP - FLT NR 4705 - TOTAL HYDRAULIC FAILURE. MAINTENANCE REMOVED AND REPLACED HYDRAULIC LINE FOR HYDRAULIC PRESSURE FILTER, HYDRAULIC SYSTEM FUNCTION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006801995120100680WP 1995 12 1 RAIA951029 219951022A7200310338026 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 1 LOW POWER A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03341TE8532 2492 950 66139 JLN - FLT NR 7068 - LEFT ENGINE DID NOT MAKE PROJECTED TARGET TORQUE OF 94 PERCENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE, GROUND RUNS CHECKED GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19951201006811995120100681EU 1995 12 1 RAIA951031 119951023A36101158200 PRESSURE SWITCH AEROSPATR42 ATR42300 8680920EU CENTER WING FAILED A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03421TE5472 102 STL - FLT 7180 - AIRFRAME AIRBLEED FAULT LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH, PERFORMED GROUND RUNS OPS CHECK GOOD. (M) 2H72 4T RTA53EU 19951201006821995120100682EU 1995 12 1 RAIA951032 119951023A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03429AM9875 5305 879 RIGHT ENGINE DID NOT ACHIEVE TARGET TORQUE. MAINTENANCE ADJUSTED TORQUE SIGNAL CONDITIONER, GROUND RUNS OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951201006831995120100683EU 1995 12 1 RAIA951033 119951025A5270SP4594 SWITCH JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR OUT OF ADJUST A RAIAO OTHER N FALSE WARNING TOTAKEOFF 1 CE03554HK851 41067 GRR - FLT NR 7517 - AFT CARGO DOOR LIGHT CAME ON DURING TAKEOFF. MAINTENANCE ADJUSTED CARGO DOOR MICROSWITCH 1WN6, OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA41NM 19951201006841995120100684EU 1995 12 1 RAIA951034 119951025A73341103P0645 FUEL PRESS SW BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03430AM10354 880 SPI - FLT NR 7095 - LEFT ENGINE FUEL PRESSURE CAP ILLUMINATED ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED FUEL PRESSURE SWITCH, GROUND RAN OPS CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19951201006851995120100685EU 1995 12 1 RAIA951035 119951025A29101379305A155 HYD LINE BAG JETSTMJETSTM3201 1500217EU RT MLG LEAKING A RAIAAB UNSCHED LANDING EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03430AM9947 9947 880 SPI - FLT 7548 - LOST HYDRAULIC PRESSURE IN FLIGHT. MAINTENANCE REMOVED AND REPLACED RIGHT LANDING GEAR RADIUS ROD FLEXIBLE HYDRAULIC LINE, GEAR SWING PERFORMED LEAK CHECKS GOOD. (M) 2L72 4T RTA56EU 19951201006861995120100686EU 1995 12 1 REXA95061 119950918A3241140041 TRANSDUCER ASSY SAAB SF340 SF340A 7850100EU LT/RT MLG MALFUNCTIONED A REXAH DEACTIVATE SYST/CIRCUITS O OTHER TXTAXI/GRND HDL 1 SO25346AM 340A032 BRAKES OCCASIONALLY FAIL TO STOP AIRCRAFT UNLESS ANTI-SKID SYSTEM IS TURNED OFF. SEPT 11, 1995 TO SEPT 18, 1995, THREE WRITE-UPS. SEPT 11, OHMED ALL WHEEL SPEED TRANSDUCERS AND NO DEFECTS NOTED. SEPT 14, REPLACED LEFT AND RIGHT INBOARD WHEEL SPEED TRANSDUCERS, S/N LT 222, RT 1090. SEPT 18, REPLACED LEFT AND RIGHT OUTBOARD WHEEL SPEED TRANSDUCERS. (M) 2L72 4T RTA52EU 19951201006881995120100688EU 1995 12 1 SIMA952892 119951016A33503012000 BALLAST AEROSPATR72 ATR72212 EU CABIN MALFUNCTIONED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21410AT 300 410 ORD - FLT NR 4119 - AFT ROW OF EMERGENCY LIGHTS STAY ON. RAI BALLAST. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951201006891995120100689NE 1995 12 1 SIMA952911 219951018A7313ST3367009 O-RING AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 5 FUEL NOZZLEFAILED A ASIMAEA ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CRCRUISE 1 SW21410AT 410 127079 FWA - FLT NR 4003 - EN ROUTE TO CMH, LEFT ENGINE TORQUE DROPPED 30 PERCENT THEN BEGAN TO DECLINE STEADILY. CREW ELECTED TO DIVERT TO FWA AND PROCEEDED WITH IN FLIGHT SHUTDOWN PROCEDURES WHEN TORQUE REACHED 30 PERCENT. UNEVENTFUL LANDING WAS MADE IN FWA. MAINTENANCE INSPECTED AND FOUND FUEL LEAK AT NR 5 NOZZLE ON THE LEFT ENGINE. NOZZLE TRANSFER TUBE O-RINGS WERE REPLACED AND SATISFACTORY LEAK CHECK ACCOMPLISHED. AIRCRAFT WAS THEN FERRIED TO ORD WHERE ALL LEFT ENGINE FUEL NOZZLES WERE REMOVED AND RI-INSTALLED WITH NEW O-RINGS AS A PRECAUTIONARY PROCEDURE. LEAK CHECKS PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19951201006901995120100690EU 1995 12 1 SIMA952922 119951019A33503011151 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN DEFECTIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21421MQ 014 CVG - FLT 4020 - EMERGENCY BATTERY SUPPLY WILL NOT POWER EMERGENCY EXIT LIGHTS OVER EXITS AND FLOOR LIGHTING. RAI BATTERY PACKS AT 3WL AND 18WL, S/N 2456 AND 2981. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951201006911995120100691EU 1995 12 1 SIMA952961 119951023A261172111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU AVIONICS RACK FAILED A SIMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2191MQ A2813 340A091 DFW - FLT NR 3515 - AVIONICS SMOKE WARNING AFTER TAKEOFF. REMOVED AND INSTALLED AVIONICS SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19951201006921995120100692NE 1995 12 1 SIMA952971 219951024A7313AS3209009 O-RING AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 12 FUEL NOZZ FAILED A ASIMAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21263AT 263 127113 DFW - 3588 - DURING CRUISE FLT NR 1 ENGINE TQ DROPPED TO 67 PERCENT, CONTINUED ON, LATER DURING DESCENT NR 1 FIRE WARNING ILLUMINATED. PILOT SHUT DOWN ENGINE AND DISCHARGED FIRE BOTTLE. MAINTENANCE ON SIGHT FOUND FUEL LEAKING FROM THE FUEL NOZZLE AREA. REMOVED AND INSPECTED FUEL NOZZLE O-RINGS. AIRCRAFT RETURNED TO SERVICE. AFTER COWLING WAS REMOVED, INSPECTION VERIFIED ENGINE FIRE IN ENGINE COMPARTMENT. 2H72 4T4 TRTA53EU E20NE 19951201006931995120100693EU 1995 12 1 SIMA952981 119951025A29109302631001 HYD LINE SAAB SF340 340B 7860101EU FUSELAGE BROKEN A SIMAO OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SW21593MA 340B206 DFW - FLT NR 3586 - DFW - PILOT REPORTED LOSS OF ALL HYDRAULICS ON TAXI IN. MAINTENANCE REMOVED AND REPLACED RUPTURED HYDRAULIC LINE. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19951201006941995120100694EU 1995 12 1 SIMA952991 119951026A53207253722001 ANGLE SAAB SF340 340B 7860101EU BS 258 CORROSION A SIMAK NONE O OTHER ININSP/MAINT 1 SW21297AE 340B297 LAW - DURING MBV/HMBV INSPECTION, FOUND ANGLE WHICH ATTACHES TO FLOOR FRAME AT STATION 258 HAD CORROSION ALONG ITS FULL LENGTH. REMOVED AND REPLACED ANGLE P/N 7253722-001 ATTACHED TO FRAME AT STATION 258 IAW SAB SRM 51-20. (M) 2L72 4T RTA52EU 19951201006951995120100695EU 1995 12 1 SIMA952992 119951026A53207253720320 INTERCOSTAL SAAB SF340 340B 7860101EU STA 272/288 CRACKED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21297AE 340B297 LAW - DURING MBV/HMBV INSPECTION, FOUND LEFT INTERCOSTAL BETWEEN STATION 272 AND 288 HAD A 1.5 INCH CRACK IN UPPER FLANGE AT NUT PLATE. REMOVED AND REPLACED INTERCOSTAL P/N 7253720-325, IAW SAAB SRM 51-20. (M) 2L72 4T RTA52EU 19951201006961995120100696EU 1995 12 1 SIMA952993 119951026A53477253721459 SEAT TRACK SAAB SF340 340B 7860101EU BS 231-270 CORROSION A SIMAK NONE O OTHER ININSP/MAINT 1 SW21297AE 340B297 LAW - DURING MBV/HMBV INSPECTION, FOUND CORROSION ON INBOARD SEAT TRACK BELOW THE GALLEY (STATION 231-270). REMOVED AND REPLACED SEAT TRACK ASSEMBLY (P/N 7253721-459, IAW SAAB SRM 53-70. (M) 2L72 4T RTA52EU 19951201006971995120100697EU 1995 12 1 SIMA953011 119951028A33503011180 EEL POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21223AT 978 223 RFD - THREE FLOOR PROXIMITY LIGHTS INOP IN FORWARD CABIN, MEL 33-22. MAINTENANCE REMOVED AND INSTALLED EMERGENCY POWER SUPPLY AND BATTERY PACK IAW ATR 42 JIC MM CH 33-51-21. OPS CHECK GOOD ON ALL TRACK LIGHTING. AIRCRFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951201006981995120100698SO 1995 12 1 SRAA109508 119951012A291366039 HYD PUMP LKHEED382 382E 526413USO NR 2 ENG INOP A SRAAK NONE J WARNING INDICATION ININSP/MAINT 1 SO19901SJ 4299 ON TAXI IN FOR FLIGHT 1003 NR 2 ENGINE HYDRAULIC PUMP FAILED, CAUSING LOSS OF UTILITY HYDRAULIC PRESSURE. FOUND NR 2 ENGINE DRIVEN HYDRAULIC PUMP INOP. REPLACED HYDRAULIC PUMP. OPS CHECKED AND LEAK CHECKED PER MM CH29-8. (M) 2H74 4T A1SO 19951201006991995120100699WP 1995 12 1 SRAA109510 119951027A323045973405505 UPLOCK ACTUATOR DOUG DC8 DC873F 302199FWP LT MLG FAILED A SRAAO OTHER J WARNING INDICATION CLCLIMB 1 SO19873SJ 46091 FLT 174 - LIM-MIA, DURING FLIGHT, LANDING GEAR UNSAFE LIGHT CAME ON AT UPLATCH CHECK, CYCLED GEAR SEVERAL TIMES NO HELP, CONTINUED FLIGHT WITH GEAR NOT LATCH LIGHT EXTINGUISHED. SUPPORTED AIRCRAFT ON JACKS, FOUND LEFT MLG WOULD NOT STAY IN THE UPLATCH POSITION. REPLACED UPLATCH ACTUATOR AND PERFORMED GEAR RETRACTION, FOUND OPERATION NORMAL PER MM CH 32-32-5. (M) 2L74 4F RT4A25 19951201007001995120100700SO 1995 12 1 SRAA109511 119951029A61207143253 VALVE HOUSING LKHEED382 382G 526414USO NR 2 PROP FAILED A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19912SJ 4388 FLT AU80 - DNA - DURING FLIGHT NR 2 PROPELLER RPM DROPS TO 97 PERCENT IN BOTH NORMAL OR MECHANICAL GOVERNING. SHUT DOWN NR 2 ENGINE RUN UP, OPS CHECKED GOOD PER JC 7101, AND 7101-2. (M) 2H74 4T A1SO 19951201007011995120100701NM 1995 12 1 TAOA109510 119951014A3350900835A BATTERY PACK BELL BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15924TS 10044 21041 RIGHT EXTERIOR OVERWING EXIT LIGHT INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951201007021995120100702NM 1995 12 1 TAOA109511 119951016A532065C34406XX VERTICAL BEAM BOEING727 727254 138408LNM BS 1183 CRACKED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15916TS4248552867 20437 ROUTINE VISUAL AND EDDY CURRENT INSPECTIONS PERFORMED DURING C-CHECK, REVEALED A 3 INCH CRACK AT WL 237 ON BS 1183 RBL 36.9 VERTICAL BEAM, AND A 1.5 INCH CRACK AT WL 238 ON THE LEFT 36.9 VERTICAL BEAM. INSTALLED REPAIR DOUBLERS PER SB 727-53-0192 RI (EA S1435). (M) 2L73 4F A3WE 19951201007031995120100703NM 1995 12 1 TAOA109512 119951016A532065198622 CHORD ANGLE BOEING727 727254 138408LNM BS 314-321 CORRODED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15916TS 20437 VISUAL INSPECTION PERFORMED DURING C-CHECK, REVEALED A 7 INCH LONG CORRODED AREA FROM BS 314 TO BS 321 ON THE NOSE WHEEL WELL RIGHT CHORD ANGLE. REPLACED CHORD ANGLE, P/N 65-19862-2, PER SRM STANDARD PRACTICE. (M) 2L73 4F A3WE 19951201007041995120100704NM 1995 12 1 TAOA109517 119951020A335090052 BATTERY CHARGER BELL BOEING727 727225 1384077NM CABIN MALFUNCTIONED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS VA5502 20441 EMERGENCY LIGHT AT ROW 3 STAYS ON AFTER TEST. REPLACED BATTERY PACK CHARGER. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951201007051995120100705NM 1995 12 1 TWRA9555 119951025A3350 EEL BOEING747 747121 1384871NM CABIN INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15604FF 19659 FORTY FOUR G/H LIGHT OVERHEAD EVAC LIGHTS INOP. REPLACED LIGHT ASSEMBLY. OPS CHECKS OK, MM33-50-00. SEAT MOUNTED EVAC LIGHT 14H INOP. REPAIRED WIRING. OPS CHECK OK 33-51-00. EVAC LENS MISSING SEAT 4H. REPLACED MISSING LENS. EVAC LENS PUSHED IN AT 5H. SECURED LENS. OPS CHECK OK 33-51-00. (M) 2L74 4F A20WE 19951201007061995120100706WP 1995 12 1 USAA950899 119950811A335014597101 EEL BATTERIES DOUG DC9 DC981 3022081WP CABIN INOP A USAAK NONE L NO TEST ININSP/MAINT 1 EA19812US 48092 PIT - THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERTIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19951201007071995120100707EU 1995 12 1 USAAF95001 119951021A5210 MECHANISM FOKKERF28 F28MK4000 4990810EU MAIN PAX DOOR OUT OF ADJUST A USAAK NONE O OTHER NRNOT REPORTED 1 EA19490US 11152 PIT - FLT NR 473 - CREW MOVED EMERGENCY DOOR HANDLE FOR MAIN ENTRY DOOR. THEREFORE MAIN ENTRY DOOR WOULD NOT OPERATE AT DEPARTURE TIME. RESET DOOR. OPS CHECKED NORMAL. (M) 2L72 4F RTA20EU 19951201007081995120100708EU 1995 12 1 USAAF95002 119951022A32321252515 ACTUATOR FOKKERF28 F28MK4000 4990810EU RT MLG DOOR OUT OF ADJUST A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19482US 11231 SDF - FLT NR 846 - AFTER TAKEOFF, RIGHT MAIN RED GEAR LIGHT REMAINED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE 1-312-5 OF PHB AND RECYCLED GEAR. AFTER RECYCLE ALL RED AND AMBER LIGHTS STAYED ON ALONG WITH GREEN LIGHTS. THEN FOLLOWED ABNORMAL PROCEDURE 1-312-4 AF PHB AND CYCLED GEAR DOWN AND UP. RED RIGHT GEAR STAYED ON. FOLLOWED PROCEDURE 1-312-5 AGAIN, NO HELP. RETURNED TO SDF, LANDING NORM. FOUND RIGHT MLG DOOR NOT CLOSING PROPERLY. ADJUSTED DOOR ACTUATOR. AFT AND LANDING GEAR OPERATED NORMAL. ALL INDICATIONS NORMAL PER M/M. AIRCRAFT OK FOR SERVICE. (M) 2L72 4F RTA20EU 19951201007091995120100709EU 1995 12 1 USAAF95003 119951022A7331CASC211 FUEL FLOW REG FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515P 54521EU LT ENGINE FAILED A USAAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 EA19476US 11224 CLT - FLT NR 379 - AFTER TAKEOFF, CLIMBING THROUGH FL 100, THE CREW FELT AND ENGINE VIBRATION. THERE WAS A DROP IN EGT, DROP IN FUEL FLOW AND A DROP IN LP RPM. THE CREW DID NOT DECLARE AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT. THE ATC TOWER DID CALL OUT THE CFR EQUIPMENT. THE FLIGHT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE FUEL FLOW GOVERNOR PER MM 73-20-11. LEAK AND RUN CHECK NORM. NO VIBRATION FELT AT 96 PERCENT HP. (M) 2L72 4F4 FRTA20EU E2EU 19951201007101995120100710NM 1995 12 1 USAASB95002 119951022A4990 OIL COOLER BOEING737 737301 1384611NM APU BLOCKED A USAAA UNSCHED LANDING HIMELECT. POWER LOSS-50 PC FLT. ATTITUDE INST. OVER TEMP CRCRUISE 1 EA19354US 23557 EWR - FL 1468 - EN ROUTE DCA-BOS, WITH THE NR 1 GENERATOR ON MEL AND THE APU RUNNING, THE APU SHUT DOWN DUE TO HIGH OIL TEMPERATURE. FLIGHT DIVERTED TO EWR AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND COULD NOT FIND A PROBLEM WITH THE APU. THE APU OIL AND OIL FILTER WERE CHANGED. SUBSEQUENTLY, MAINTENANCE FOUND THAT THE APU OIL INLET COOLER WAS BLOCKED, CAUSING THE HIGH TEMPERATURES. (M) 2L72 4F RTA16WE 19951201007111995120100711NE 1995 12 1 USAASB95003 219951023A7314378200 FUEL PUMP BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE LT ENGINE FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19225US28242 21667 656103 PHL - FL 330, CLIMBING OUT OF LGA, AT FL 280, THE LEFT ENGINE SHUT DOWN AND COULD NOT BE RESTARTED. FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN FUEL PUMP FAILED AND REPLACED IT. (M) 2L72 4F4 F A16WE E2EA 19951201007121995120100712NM 1995 12 1 USAASB95005 119951028A793041820044 OIL QTY XMITTER BOEING737 737301 1384611NM NR 2 ENGINE FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA19592US27442 23937 STL - FLT NR 0091 - EN ROUTE FROM PIT TO SAN, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE WAS FLUCTUATING BETWEEN 35 AND 40 PSI. FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED TO STL WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE MEL'D THE NR 2 ENGINE OIL QUANTITY INDICATION. THE OIL QUANTITY TRANSMITTER WAS REPLACED ON THE RON. MAINTENANCE ALSO CLEANED THE CONNECTOR ON THE OIL PRESSURE TRANSMITTER. RAN ENGINE AND OPS WAS NORMAL. (M) 2L72 4F RTA16WE 19951201007131995120100713NE 1995 12 1 VTZA96013 219951020A73201003573 FETM JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE INOPERATIVE A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27306UE3905 41020 P75009 FLT NR 6536 - IAD-ORF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE LEFT ENGINE IEC CAP LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE FUEL ENRICHMENT TORQUE MOTOR. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA41NM E18NE 19951201007141995120100714WP 1995 12 1 VTZA96015 219951024A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RIGHT MALFUNCTIONED A AVTZAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 EA27484UE 899 P66204 FLIGHT NR 6340 - PWM-BOS - DURING CLIMB-OUT THE FLIGHT CREW EXPERIENCED ROUGHNESS WITH THE RIGHT ENGINE WITH A SUBSEQUENT DROP IN TORQUE AND RISE IN EGT. CREW SHUT ENGINE DOWN AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT PWM WITH NO FURTHER INCIDENTS. MAINTENANCE IS CHANGING THE ENGINE IN PWM. MAINTENANCE COMPLETED ENGINE CHANGE ON 10-26-95. (M) 2L72 4T4 TRTA56EU E4WE 19951201007151995120100715 1995 12 1 VTZA96018 419951027A3197 WIRE JETAIRJETSTMJETSTM4101 1500501EU COCKPIT CHAFED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27306UE 41020 FLT NR 6305 - IAD-JFK - DURING TAKEOFF, RETURNED TO IAD DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM COMING ON AFTER TAKEOFF. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED CHAFED WIRE WC-11 WITH AWG 22 GAUGE WIRE OF THE SAME LENGTH AND REPOSITIONED IT. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951201007161995120100716EU 1995 12 1 VTZA96019 119951027A326091SE16 DOWNLOCK SWITCH JETAIRJETSTMJETSTM4101 1500501EU NLG FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27306UE 41020 FLT NR 6214 - IAD-ORF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE TAKEOFF CONFIGURATION WARNING ON THE CAP PANEL FLICKERING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE NOSE DOWNLOCK STANDBY MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951201007171995120100717NE 1995 12 1 WTAA950285 219951020A7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT BIRD STRIKE A WTAAK NONE C F.O.D. CLCLIMB 1 WP17454UE 120155 MRY - BIRD STRIKE REPORTED AT LEFT ENGINE ON CLIMB-OUT FROM SFO. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION OF AIRCRAFT . NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19951201007181995120100718NE 1995 12 1 WTAA950286 219951022A7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT REQ'D OIL SERV A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17284UE 120145 SMF - RIGHT ENGINE OIL PRESSURE REPORTED LOW WITH ASSOCIATED AURAL WARNING INDICATION ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED RIGHT ENGINE NO EVIDENCE OF OIL LEAKAGE NOTED. SERVICED ENGINE WITH 3 QUARTS OF OIL. OIL PRESSURE INDICATIONS NORMAL ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19951201007191995120100719SO 1995 12 1 WTAA950287 119951022A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO AURAL WARNING TRIPPED A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17122AM 120013 LAX - AURAL 'TRIM' WARNING INDICATION REPORTED DURING TAKEOFF ROLL, TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND AURAL WARNING SYSTEM CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER. AURAL WARNING SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951201007201995120100720SO 1995 12 1 WTAA950288 119951017A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17120AM 120012 SFO - TAKEOFF TRIM WARNING INDICATION ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND AURAL WARNING CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AURAL WARNING SYSTEM OPERATONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951201007211995120100721SO 1995 12 1 WTAA950289 119951025A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG GEAR FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17216YV 120216 RNO - LEFT MAIN LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR ACTUATOR. LANDING GEAR RETRACTION SYSTEM OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951201007221995120100722NE 1995 12 1 WTAA950290 219951024A7321 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17454UE 120155 FAT - RIGHT ENGINE ELECTRONIC ENGINE CONTROLS (EEC) FAILED ON TAKEOFF ROLL. AIRCRAFT ABORTED TAKEOFF WITHOUT INCIDENT. MAINTENANCE DEFERRED THE RIGHT ENGINE EEC SYSTEM PER MEL 73-21-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL WITH THE REPLACEMENT OF THE RIGHT ENGINE EEC AND TORQUE SIGNAL CONDITION UNIT. (M) 2L72 4T4 TRTA31SO E20NE 19951201007231995120100723SO 1995 12 1 WTAA950291 119951025A7712 TQ SIG COND EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A AWTAAO OTHER O OTHER NRNOT REPORTED 1 WP17454UE 120155 FAT - DURING SIMULATED RIGHT ENGINE FAILURE ON TRAINING FLIGHT, WITH RIGHT ENGINE AT APPROXIMATELY 25 PERCENT TORQUE, RIGHT PROPELLER AUTO FEATHERED. CREW SELECTED AUTO FEATHER SYSTEM OFF AND RIGHT ENGINE NP RETURNED TO NORMAL. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITION UNIT. PROPELLER AUTO FEATHER SYSTEM OPERATIONAL CHECKED NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951201007241995120100724 1995 12 1 WTAA950293 419951026A34181R1606 SWITCH GUARD EMB 120 EMB120RT SO COCKPIT OUT OF POSITION A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17276UE 120067 LAX - STALL WARNING SYSTEM ACTIVATED (SHAKER AND PUSHER) ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT STALL WARNING TEST SWITCH ON STALL WARNING PANEL STUCK IN THE DOWN (TEST) POSITION. REMOVED SWITCH GUARD AND DEBURED. REINSTALLED COVER. SWITCH OPERATION NORMAL. STALL WARNING SYSTEM OPERATIONAL CHECK NORMAL DURING AIRCRAFT GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951207000011995120700001NM 1995 12 7 P5CA9500822 119951020A2710 AILERON BOEING747 747121 1384871NM RIGHT LOCKED OUT A P5CAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 WP23830FT 19642 RETURNED TO BLOCKS DUE TO RIGHT HAND OUTBOARD AILERON LOCKED OUT WITH FLAPS AT 20 UNITS. INSPECTED RIGHT HAND OUTBOARD AILERON LOCKOUT ACTUATOR INSTRUMENTS AND WIRING. REMOVED, CLEANED, INSPECTED ELECTRICAL CONNECTIONS AND FOUND NO OBVIOUS DEFECTS, SYSTEM CHECKS SATISFACTORY. 2L74 4F A20WE 19951207000021995120700002NM 1995 12 7 95ZZZM563 119950920A3244AHA1648 TIRE BOEING757 75723APF 1384966NM NR 5 MAIN BLOWN A CLCAO OTHER O OTHER LDLANDING 1 SO19573CA 24971 FLT NR 096 - ON LANDING IN MIA, NR 5 MAIN TIRE LOST RECAP AND BLEW. ON INSPECTION NOTICED A HALF INCH PUNCTURE ON LOWER SURFACE OF LEFT HAND INBOARD FLAP. INTERIM REPAIR PERFORMED ON FLAP AS PER SRM 57-53-01. REPLACED NR 5 MAIN WHEEL/TIRE ASSEMBLY. NR 6 MAIN WHEEL/TIRE REPLACED AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURN TO SERVICE. (M) 2L72 4F RTA2NM 19951207000031995120700003NM 1995 12 7 UPS404918 119951030A2610 FIRE DET BOEING747 747123 1384873NM MAIN CARGO DECK MALFUNCTIONED A IPXAAB UNSCHED LANDING EMER. DESCENT N FALSE WARNING CRCRUISE 1 SO01675UP 20390 CREW REPORTED WHILE CRUISING AT 35,000 FEET BETWEEN EWR AND SDF, HAD A MAIN CARGO DECK FIRE WARNING. COULD NOT DETECT ANY FIRE OR SMOKE VISUALLY, UPS EMERGENCY PROCEDURES WERE USED. MADE EMERGENCY DESCENT INTO PIT. FIRE TRUCKS MET THE AIRCRAFT. FIRE TEAM CAME ON BOARD, NO FIRE WAS FOUND. DEFERRED DETECTOR, RETURNED TO SDF. 2L74 4F A20WE 19951207000041995120700004NM 1995 12 7 UPS404921 119951101A5313 STRINGER BOEING747 747123 1384873NM BS 1000 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE STRINGERS UNDER END STOP FITTINGS AT STATION 1000, STRINGER 47R AND STRINGER 45L IN FORWARD CARGO COMPARTMENT. MAINTENANCE REPAIRED THE STRINGERS IAW SRM 53-10-03. 2L74 4F A20WE 19951207000051995120700005NM 1995 12 7 UPS404922 119951101A5311 FRAME BOEING747 747123 1384873NM BS 194 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TOP SIDE OF FRAME. MAINTENANCE REPLACED THE FRAME IAW SRM 51-30-02/05. 2L74 4F A20WE 19951207000061995120700006NM 1995 12 7 UPS404923 119951101A5320 CHORD BOEING747 747123 1384873NM BS 1000 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CRACKS IN THE LOWER CHORD AT STATION 1000, BETWEEN STRINGERS 46 AND 47R AND STRINGERS 46 AND 47L. MAINTENANCE REPLACED THE LOWER CHORD PARTLY WITH REPAIR KIT PER SRM 51-30-02. 2L74 4F A20WE 19951207000071995120700007NM 1995 12 7 UPS404924 119951101A5320 SHEAR TIE BOEING747 747123 1384873NM BS 1660 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE SHEAR TIE AT STATION 1660, BETWEEN STRINGERS 46 AND 47L IN THE AFT CARGO COMPARTMENT. MAINTENANCE REMOVED THE DAMAGED SHEAR TIE AND REPAIRED SHEAR TIE IAW SRM 53-10-04. 2L74 4F A20WE 19951207000081995120700008NM 1995 12 7 UPS404925 119951101A5320 WEB BOEING747 747123 1384873NM BS 260 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE NOSE LANDING GEAR WHEELWELL CRAWL-WAY AT STATION 260, WL 160 IN OUTBOARD CORNER OF CUT-OUT, LEFT HAND AND RIGHT HAND SIDE. MAINTENANCE REPAIRED IAW SRM 53-10-04. 2L74 4F A20WE 19951207000091995120700009NM 1995 12 7 UPS404950 119951109A5320 PRESSURE DECK BOEING747 747123 1384873NM BS 1290 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01671UP 20323 WHILE IN AMS FOR C-CHECK, MAINTENANCE FOUND CORROSION AT PRESSURE DECK BS 1290 TO 1300 LBL 75. REMOVED CORROSION AT PRESS DECK BS 1290 TO 1300 ACC SRM 51-10-01, CORR NOT IN LIMITS ACC SRM 53-10-01. REPAIRED PRESS DECK FROM BS 1290 TO 1300 LBL 75, SRM 53-10-07 FIG 2. 2L74 4F A20WE 19951207000101995120700010WP 1995 12 7 COMA9520398 219951109A732089778014 FCU SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE DEFECTIVE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01458AM3066 1715 AC699 RT ENGINE WILL NOT ACHIEVE TAKEOFF TORQUE. REPLACED THE FUEL CONTROL UNIT. 1L72 4T4 T A8SW E4WE 19951207000111995120700011NM 1995 12 7 DL757954247 119951105A4940A703CD K117 RELAY BOEING757 757232 1384965NM APU FAILED A ADALAK NONE O OTHER ININSP/MAINT 1 SO11618DL18421 22908 WORKING INOP APU, FOUND STARTER BURNED UP AND APU BATTERY DEAD. RELAY K-117 CONTACTS WELDED CLOSED CAUSING STARTER TO RUN CONTINUOUS UNTIL APU BATTERY WENT DEAD. 2L72 4F RTA2NM 19951207000121995120700012NM 1995 12 7 UPS405014 119951111A3350 EEL WIRE BOEING747 747123 1384873NM CARGO DECK BROKEN A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 WHILE IN 'A' CHECK, MAINTENANCE FOUND MAIN CARGO DECK RT OVERHEAD FWD EMERGENCY LIGHT INOP. FOUND BROKEN WIRE, REPAIRED SAME, CHECKS OK. 2L74 4F A20WE 19951207000131995120700013NM 1995 12 7 UPS405076 119951114A3350 BULB BOEING747 747123 1384873NM CREW SVC DOOR FAILED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT BY CREW SERVICE DOOR, X325 INOP. RELAMPED, OPS CK OK. 2L74 4F A20WE 19951207000141995120700014NM 1995 12 7 UPS405077 119951113A3350 EEL CONNECTOR BOEING747 747121 1384871NM L1 ENTRY DOOR LOOSE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01683UP 20353 WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LT TEST FOUND INOP, EMERGENCY LT ON L-1 ENTRY DOOR INOP, FWD LIGHT AND ONE UPPER CARGO DECK CEILING LIGHT INTERMITTENT. RESECURED CONNECTOR AT M415 EMER LIGHT ASSY, OPS CHECKS GOOD. 2L74 4F A20WE 19951207000151995120700015NM 1995 12 7 UPS205097 119951115A5330 SKIN BOEING747 747123 1384873NM APU INSP PORT WRINKLED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE ON GROUND DURING PREFLIGHT, MAINTENANCE FOUND WRINKLED SKIN IN VICINITY OF APU FIRE EXT INSPECTION PORT. INSPECTED DENTED AREAS IAW SRM 53-30-01 PAGE 2A, NO CRACKS FOUND, DENTS ARE SMOOTH. REINSPECT EVERY 250 CYCLES WITH PERMANENT REPAIR NEXT HEAVY CHECK. ISSUED DEFERRED MAINTENANCE ITEM. 2L74 4F A20WE 19951207000161995120700016NM 1995 12 7 UPS405099 119951117A5220 ESCAPE HATCH BOEING747 747123 1384873NM FLIGHT DECK NOT SECURE A IPXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO01673UP 20325 CREW REPORTED ON TAKEOFF ROLL, TOP ESCAPE HATCH OPENED, TAKEOFF ABORTED. SECURED TOP ESCAPE HATCH. 2L74 4F A20WE 19951207000171995120700017NM 1995 12 7 UPS405104 119951120A3350 BATTERY PACK BOEING747 747123 1384873NM ESCAPE SLIDE DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 19641 WHILE ON GROUND, MAINT FOUND EMERGENCY LIGHTS AT ESCAPE SLIDE INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD (P/N 9008-4) ON, (S/N 5342) OFF. 2L74 4F A20WE 19951208000011995120800001NE 1995 12 8 9519379880 219951130A7261 OIL FILTER DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 2 ENGINE DIRTY A NWAAED ENGINE SHUTDOWN RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL01675MC 47651 696730 AFTER 15 MINUTES OF TAXI TIME, THE NR 2 ENGINE OIL FILTER CLOG WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE OIL FILTER FOR ABNORMALITIES, NONE NOTED. A NEW OIL FILTER WAS INSTALLED AND NO DISCREPANCIES NOTED ON RUNUP. 2L72 4F4 F A6WE E2EA 19951208000021995120800002WP 1995 12 8 ABXA9500937 119951106A5744995760016 FITTING DOUG DC9 DC941 302207NWP RT FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951208000031995120800003WP 1995 12 8 ABXA9500938 119951106A5744995760020 FITTING DOUG DC9 DC941 302207NWP RT FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH FITTING CRACKED. REPLACED ATTACH FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951208000041995120800004WP 1995 12 8 ABXA9500939 119951112A57535912168503 VANE DOUG DC9 DC941 302207NWP LT FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT FLAP FORWARD MOVEABLE VANE DELAMINATED. REPLACED VANE IAW DC-9 SUPP MM 27-51-2. 2L72 4F A6WE 19951208000051995120800005WP 1995 12 8 ABXA9500940 119951108A57535910134146 SKIN DOUG DC9 DC941 302207NWP RT FLAP CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE RIGHT FLAP UPPER SKIN. REPAIRED IAW ABX REA D957-13446-MR. 2L72 4F A6WE 19951208000061995120800006WP 1995 12 8 ABXA9500941 119951108A53305920323129 SKIN DOUG DC9 DC941 302207NWP BS 540 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION, FOUND OIL CANNING ON EXTERIOR SKIN AT STA 540, BETWEEN LONGERONS 21R AND 22R. REPAIRED IAW ABX REA D953-13477-MR. 2L72 4F A6WE 19951208000071995120800007WP 1995 12 8 ABXA9500942 119951108A57115911300502 SPAR CAP DOUG DC9 DC941 302207NWP WS 566 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23951AX 47616 DURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR UPPER CAP CORRODED AT XRS 566 TO 568. REPAIRED IAW ABX REA D957-13436-MR. 2L72 4F A6WE 19951208000081995120800008WP 1995 12 8 ABXA9500945 119951025A55115918000508 SPAR CAP DOUG DC9 DC933F 302207AWP HORIZ STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23930AX 47363 DURING C-CHECK INSPECTION, FOUND CORROSION ON LOWER SURFACE OF AFT UPPER SPAR CAP, FORWARD FLANGE ON RIGHT HORIZONTAL STABILIZER. REPAIRED IAW ABX REA D955-13276-MR. 2L72 4F A6WE 19951208000091995120800009WP 1995 12 8 ABXA9500946 119951002A5720591000643 ANGLE DOUG DC9 DC932 3022066WP WS 48 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103. 2L72 4F A6WE 19951208000101995120800010WP 1995 12 8 ABXA9500947 119950928A532049157601 PAN DOUG DC9 DC932 3022066WP BS 148 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND UPPER FORWARD END OF SERVICE DOOR HOLD OPEN LATCH PAN CRACKED AT WELD. REPLACED LATCH PAN IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19951208000111995120800011WP 1995 12 8 ABXA9500948 119950930A533059114013 SKIN DOUG DC9 DC932 3022066WP BS 115 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DENT IN THE FUSELAGE SKIN AT STA 115, LONGERON 21L. REPAIRED IAW DC-9 SRM 53-04 FIG 38 VIEW 1. 2L72 4F A6WE 19951208000121995120800012WP 1995 12 8 ABXA9500949 119950930A5280591498525 ANGLE DOUG DC9 DC932 3022066WP NLG DOOR MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SERVICE BULLETIN FITTINGS MISSING FROM NOSE LANDING GEAR DOORS. REPAIRED FITTINGS IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-4 AND INSTALLED DOUBLERS IAW EA NR FS-53-03529-MA. 2L72 4F A6WE 19951208000131995120800013WP 1995 12 8 ABXA9500950 119950930A53305911401 SKIN DOUG DC9 DC932 3022066WP BS 110-218 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTNING STRIKES FROM STA 110 TO 218, LONGERON 26R. REPAIRED IAW DC-9 SRM 53-04 FIG 38. 2L72 4F A6WE 19951208000141995120800014WP 1995 12 8 ABXA9500951 119950929A573059127352 TE PANEL DOUG DC9 DC932 3022066WP WS 445-509 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND WING TRAILING EDGE PANEL FORWARD OF RIGHT AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 19951208000151995120800015WP 1995 12 8 ABXA9500952 119950928A5320991560013AX ANGLE DOUG DC9 DC932 3022066WP BS 110 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND PANEL 110 SUPPORT ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW PFEA NR PFE-D953-10918 AND DC-9 SRM 51-30-5. 2L72 4F A6WE 19951208000161995120800016WP 1995 12 8 ABXA9500953 119950927A573059127371 PANEL DOUG DC9 DC932 3022066WP WS 363-414 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING UPPER BONDED PANEL FORWARD OF AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19951208000171995120800017WP 1995 12 8 ABXA9500954 119951008A5330591970731 SKIN DOUG DC9 DC932 3022066WP BS 917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND PSE INSPECTION 53.09.035A, AD 94-03-01, FOUND EXCESSIVE CORROSION ON THE FUSELAGE SKIN. REPAIRED SKIN IAW ABX REA D953-12953-MR. 2L72 4F A6WE 19951208000181995120800018WP 1995 12 8 ABXA9500955 119951008A5230591015825 DOUBLER DOUG DC9 DC932 3022066WP BS 917 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND EXCESSIVE CORROSION ON AFT LOWER CARGO DOOR DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-12953-MR. 2L72 4F A6WE 19951208000191995120800019WP 1995 12 8 ABXA9500956 119951006A5320991015128 WEB DOUG DC9 DC932 3022066WP BS 699-737 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR. 2L72 4F A6WE 19951208000201995120800020WP 1995 12 8 ABXA9500957 119951006A5320991015127 WEB DOUG DC9 DC932 3022066WP BS 699-737 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR. 2L72 4F A6WE 19951208000211995120800021WP 1995 12 8 ABXA9500958 119951006A5320991015117 WEB DOUG DC9 DC932 3022066WP BS 699-737 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR. 2L72 4F A6WE 19951208000221995120800022WP 1995 12 8 ABXA9500959 119951006A532099101514 WEB DOUG DC9 DC932 3022066WP BS 699-737 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR. 2L72 4F A6WE 19951208000231995120800023WP 1995 12 8 ABXA9500960 119951006A532099101513 WEB DOUG DC9 DC932 3022066WP BS 699-737 CUT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR. 2L72 4F A6WE 19951208000241995120800024WP 1995 12 8 ABXA9500961 119951002A5720591000644 ANGLE DOUG DC9 DC932 3022066WP WS 48 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103. 2L72 4F A6WE 19951208000251995120800025WP 1995 12 8 ABXA9500962 119951012A532059124921 JAMB DOUG DC9 DC932 3022066WP BS 200 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND SERVICE DOOR JAMB DENTED. REPAIRED IAW ABX REA D953-12952-MR. 2L72 4F A6WE 19951208000261995120800026WP 1995 12 8 ABXA9500963 119951003A53125910130 BLKHD SKIN DOUG DC9 DC932 3022066WP BS 996 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND DAMAGE AT FORWARD SIDE OF AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-13005-MR. 2L72 4F A6WE 19951208000271995120800027WP 1995 12 8 ABXA9500964 119951004A5330591142485 SKIN DOUG DC9 DC932 3022066WP BS 897 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DAMAGED AT THE FORWARD EDGE OF THE ALC DOOR CUTOUT. REPAIRED IAW ABX REA D953-13004-MR. 2L72 4F A6WE 19951208000281995120800028WP 1995 12 8 ABXA9500965 119951004A53159911544507 FLOORBEAM DOUG DC9 DC932 3022066WP BS 389 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FLOORBEAM STA 389, GOUGED. REPAIRED IAW ABX REA D953-13009-MR. 2L72 4F A6WE 19951208000291995120800029WP 1995 12 8 ABXA9500966 119951005A53305911401 SKIN DOUG DC9 DC932 3022066WP BS 206 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 206, LONGERON 19R. REPAIRED IAW ABX REA D953-12989-MR. 2L72 4F A6WE 19951208000301995120800030WP 1995 12 8 ABXA9500967 119951005A53305911408125 SKIN DOUG DC9 DC932 3022066WP BS 298.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN IN AREA OF NR 2 ADF LOOP ANTENNA, STA 298.5, BETWEEN LONGERON 1 AND 2L. REPAIRED IAW ABX REA D953-12973-MR. 2L72 4F A6WE 19951208000311995120800031WP 1995 12 8 ABXA9500968 119951003A5330591142485 SKIN DOUG DC9 DC932 3022066WP BS 937 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 937, LONGERON 23. REPAIRED IAW ABX REA D953-12993-MR. 2L72 4F A6WE 19951208000321995120800032WP 1995 12 8 ABXA9500969 119951005A53305911401 SKIN DOUG DC9 DC932 3022066WP BS 168 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND A DENT WITH A GOUGE IN FUSELAGE SKIN STA 168, LONGERON 19R. REPAIRED IAW ABX REA D953-12980-MR. 2L72 4F A6WE 19951208000331995120800033WP 1995 12 8 ABXA9500970 119951005A53159911544507 FLOORBEAM DOUG DC9 DC932 3022066WP BS 389 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOORBEAM AT STA 389 AT RBL 44. REPAIRED IAW ABX REA D953-13029-MR. 2L72 4F A6WE 19951208000341995120800034WP 1995 12 8 ABXA9500971 119951006A5330591140027 SKIN DOUG DC9 DC932 3022066WP BS 105 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 94-03-01, FOUND FUSELAGE SKIN DENTED AND CRACKED AT STA 105, LONGERON 18L. REPAIRED IAW ABX REA D953-13037-MR. 2L72 4F A6WE 19951208000351995120800035WP 1995 12 8 ABXA9500972 119951003A53305911401 SKIN DOUG DC9 DC932 3022066WP BS 189 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 189, LONGERON 19R. REPAIRED IAW ABX REA D953-12988-MR. 2L72 4F A6WE 19951208000361995120800036WP 1995 12 8 ABXA9500973 119950929A533059114065 SKIN DOUG DC9 DC932 3022066WP BS 160 REQ'D REPAIR A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK AND PSE INSPECTIONS, FOUND PREVIOUS REPAIR AT FORWARD UPPER CORNER OF ENTRY DOOR CUTOUT. REPAIRED IAW ABX REA D953-12981-MR. 2L72 4F A6WE 19951208000371995120800037WP 1995 12 8 ABXA9500974 119950929A531199196181 FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON LEFT SIDE. REPAIRED IAW ABX REA D953-12966-SB. 2L72 4F A6WE 19951208000381995120800038WP 1995 12 8 ABXA9500975 119950930A531199196182 FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON RIGHT SIDE. REPAIRED IAW ABX REA D953-12966-SB. 2L72 4F A6WE 19951208000391995120800039WP 1995 12 8 ABXA9500976 119950930A5312991183879 BLKHD SKIN DOUG DC9 DC932 3022066WP BS 1046 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND THE INLET DUCT GOUGED THE BULKHEAD SKIN AT STA 1046. REPAIRED IAW ABX REA D953-12991-MR. 2L72 4F A6WE 19951208000401995120800040WP 1995 12 8 ABXA9500977 119951002A53125910130279 BLKHD SKIN DOUG DC9 DC932 3022066WP BS 996 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND A GOUGE IN THE AFT SIDE OF THE AFT PRESSURE BULKHEAD. REPAIRED IAW ABX REA D953-12990-MR. 2L72 4F A6WE 19951208000411995120800041WP 1995 12 8 ABXA9500978 119951004A533059114023 SKIN DOUG DC9 DC932 3022066WP BS 80 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 80, LONGERON 18. REPAIRED IAW ABX REA D953-12995-MR. 2L72 4F A6WE 19951208000421995120800042WP 1995 12 8 ABXA9500979 119951011A5320991245321 FORMER DOUG DC9 DC932 3022066WP BS 370 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE FORMER AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR. 2L72 4F A6WE 19951208000431995120800043WP 1995 12 8 ABXA9500980 119951011A532099196503 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 370 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23982AX 47317 DURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE INTERCOSTAL AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR. 2L72 4F A6WE 19951208000441995120800044WP 1995 12 8 ABXA9500981 119950629A32105925306501 BUSHINGS DOUG DC9 DC931 3022065WP RT MLG WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 2341 47551 DURING OFF WING OVERHAUL PROCEDURES, FOUND BUSHINGS WORN. REPAIRED IAW ABX REA D932-12004-MR. 2L72 4F A6WE 19951208000451995120800045WP 1995 12 8 ABXA9500982 119950714A323039140165503D CYL ATTACH DOUG DC9 DC932 3022066WP LT MLG CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23902AX 3890 47426 DURING OFF WING OVERHAUL PROCEDURES, FOUND CORROSION IN THE ATTACHMENT HOLES. REPAIRED IAW ABX REA D932-12028-MR. 2L72 4F A6WE 19951208000461995120800046WP 1995 12 8 ABXA9500983 119951016A5730 TE SKIN DOUG 5910411515 DOUG DC9 DC932 3022066WP WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX ABXH315 47314 DURING CARGO MOD OFF WING INSPECTION, FOUND LEVEL 2 CORROSION IN TWO AREAS ON THE LOWER SKIN DOUBLER ALONG THE TRAILING EDGE. REPLACED CENTER SKIN IAW DC-9 DRAWING 5910411. 2L72 4F A6WE 19951208000471995120800047WP 1995 12 8 ABXA9500984 119951020A575149147943 FITTING DOUG 5910051501 DOUG DC9 DC941 302207NWP LT AILERON CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23965AX ABXE720 47498 DURING DC-9 AILERON OFF WING INSPECTION, FOUND LEVEL 2 CORROSION ON THE FITTING ASSEMBLY AROUND BUSHING HOLE. REPLACED FITTING ASSEMBLY IAW DC-9 OVERHAUL MANUAL 27-10-2. 2L72 4F A6WE 19951208000481995120800048WP 1995 12 8 ABXA9500985 119950304A78305958782503 TR LINK PWA 591029415 DOUG DC9 DC931 3022065WP NR 1 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23948AX R0515 47065 DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-40 AND 78-66, FOUND THE NR 1 LOWER RIGHT DRIVER LINK SHOWED A CRACK INDICATION DURING EDDY CURRENT INSPECTION. REPLACED DRIVER LINK IAW DC-9 MM. SHOP FINDING, LINK CRACKED AND SCRAPPED LINK. 2L72 4F A6WE 19951208000491995120800049WP 1995 12 8 ABXA9500986 119950615A5522 SKIN DOUG 3910411515 DOUG DC9 DC941 302207NWP ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47777 47492 DURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE LOWER OUTBOARD SKIN AROUND DOUBLERS. REPLACED SKIN IAW DC-9 SRM 55-21-0. 2L72 4F A6WE 19951208000501995120800050WP 1995 12 8 ABXA9500987 119950615A5522 SKIN DOUG 3910411515 DOUG DC9 DC941 302207NWP LT ELEVATOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23979AX 47777 47492 DURING CARGO MOD, DC-9 ELEVATOR OFF WING PROCEDURES, FOUND LEVEL 2 CORROSION ON THE CENTER SKIN. REPLACED CENTER SKIN IAW DC-9 SRM 55-21-0. 2L72 4F A6WE 19951208000511995120800051WP 1995 12 8 ABXA9500988 119951020A57535912125 SPAR DOUG 5910039560 DOUG DC9 DC932 3022066WP RT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX IBF020 47314 DURING CARGO MOD, OFF WING FLAP INSPECTION, FOUND LEVEL 2 CORROSION ON THE AFT LOWER SPAR. REPLACED LOWER AFT SPAR IAW DC-9 DRAWING 5910039 AND SRM 57-50-1. 2L72 4F A6WE 19951208000521995120800052WP 1995 12 8 ABXA9500989 119951020A5753 SKIN DOUG 5910039560 DOUG DC9 DC932 3022066WP RT TE FLAP CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX IBF020 47314 DURING CARGO MOD, OFF WING INSPECTION, FOUND LEVEL 2 CORROSION ON THE INBOARD LOWER SKIN. REPLACED SKIN IAW DC-9 DRAWING 5910039 AND SRM 51-10-3. 2L72 4F A6WE 19951208000531995120800053WP 1995 12 8 ABXA9500990 119951129A3231 CABLES DOUG DC8 DC863 302198AWP RT MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23825AX 46115 DURING LANDING GEAR RETRACTION, AFTER TAKEOFF, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. UPLATCH CHECK INDICATED RIGHT MAIN GEAR DOOR UNLOCKED. RECYCLED GEAR AND UNSAFE LIGHT EXTINGUISHED AFTER TEN MINUTES. UPLATCH CHECK WAS SATISFACTORY. CLEANED AND LUBRICATED RIGHT MAIN GEAR DOOR PROXIMITY SWITCH. AFTER SUBSEQUENT FLIGHT, FOUND RIGHT GEAR DOOR SEQUENCE CABLES OUT OF RIG. ADJUSTED CABLES IAW DC-8 MM, SYSTEM OPS CHECKED GOOD DURING GEAR SWING. 2L74 4F 4A25 19951208000541995120800054WP 1995 12 8 ABXA9500991 119951130A3310BA170MODB BALLAST DOUG DC8 DC863 302198AWP RT GLARESHIELD DEFECTIVE A ABXAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23822AX 46079 DURING FLIGHT TRAINING, GLARESHIELD FLUORESCENT LIGHT BLINKED, THEN EMITTED LIGHT SMOKE. REPLACED FLUORESCENT BALLAST ASSEMBLY, OPS CHECKED GOOD IAW DC-8 MM 33-0. 2L74 4F 4A25 19951208000551995120800055NM 1995 12 8 DL72S954565 119951129A5320 ANGLE BOEING727 727232 1384082NM RT MLG WW CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27545DA 22494 FWD KEEL BEAM ANGLE CRACKED 1 INCH BELOW APU RT SIDE, FOUND DURING A-1 LTR CK TPAMM. TIME LIMITED REPAIR ACCOMPLISHED PER SRM 53-10-9 FIG 13. DAILY INSP REQUIRED AND PERM REPAIR TO BE ACCOMPLISHED WITHIN 100 FLT HOURS. 2L73 4F A3WE 19951208000561995120800056NM 1995 12 8 DL72S954566 119951129A5754 ANGLE BOEING727 727232 1384082NM NR 3 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27545DA 22494 FOUND .5 INCH CRACK BELOW NR 3 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER SRM 57-54-0. 2L73 4F A3WE 19951208000571995120800057NM 1995 12 8 DL72S954567 119951129A5754 ANGLE BOEING727 727232 1384082NM NR 2 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27545DA 22494 FOUND .5 INCH CRACK BELOW NR 2 SLAT TAI DUCT, FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208000581995120800058NM 1995 12 8 DL72W954568 119951129A3350 BATTERY S106 BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO272807W 20579 DURING LAYOVER, MTC FOUND EMERGENCY LIGHT ABOVE AFT RIGHT SERVICE DOOR WOULD NOT TEST. REPLACED BATTERIES, NOW OPERATION IS NORMAL. 2L73 4F A3WE 19951208000591995120800059NM 1995 12 8 DL72W954576 119951129A5754651622296 SKIN BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272815W 20871 BN1054 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH FLOATING SKIN CRACKED AT FASTENERS BETWEEN RIBS NR 8 AND 9, 13 AND 14. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208000601995120800060NM 1995 12 8 DL72W954577 119951120A5754651622296 RIB BOEING727 727247 138408FNM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272815W 20871 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH RIB NR 13 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208000611995120800061NM 1995 12 8 DL72W954580 119951120A57546516224101 RIB BOEING727 727247 138408FNM NR 1 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272815W 20871 BN1054 NR 1 SLAT RIB MARKED 15 CRACKED. REPAIRED PER MM 57-54-0 PG 819. 2L73 4F A3WE 19951208000621995120800062NM 1995 12 8 DL733954571 119951129A5210 CORNER BOEING737 737347 1384647NM R-1 DOOR CRACK A DALAK NONE O OTHER ININSP/MAINT 1 SO27305WA 23346 FOUND DURING LETTER CHECK, R-1 DOOR LOWER HINGE CUTOUT UPPER CORNER CRACKED. MFG DOUBLER AND INSTALLED TEMP REPAIR PER SRM 52-OO-01. 2L72 4F RTA16WE 19951208000631995120800063NM 1995 12 8 DL73E954574 119951129A5753656826911 FAIRING BOEING737 737247 138448DNM LT TE MIDFLAP CAME LOOSE A DALAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO27236WA 23184 LEFT INBD FLAP FAIRING CANOE BROKE LOOSE IN FLT AND WAS FOUND PARTLY DETACHED FROM WING DURING POST FLT. REMOVED LEFT WING MIDFLAP CANOE, REPLACED BELL CRANK ASSY, INBD AND OTBD STRUTS AND REINSTALLED FAIRING PER MM 27-51-21. 2L72 4F A16WE 19951208000641995120800064NM 1995 12 8 DL757954559 119951129A2913 NR 1 EDP 3508807 BOEING757 757232 1384965NM LT MLG WW FAILED A DALAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27601DL 22808 DURING CRUISE, LT HYD QTY EICAS MSG AND RSVR LIGHT. QTY .16, AFTER 5 MINS LT SYSTEM PRESSURE MSG, FLAPS 20, LANDING MADE AND NO NOSE WHEEL STEERING. FOUND PRESSURE LINE FROM PTU CONTROL MODULE LEAKING. SECURED SAME, CKS OK. FOUND NR 1 EDP NOT PRODUCING PRESS AND METAL IN FILTER. REMOVED AND REPLACED NR 1 EDP, FLUSHED LINES, REPLACED FILTERS AND OPS CKS GOOD. 2L72 4F RTA2NM 19951208000651995120800065NM 1995 12 8 DL76S954557 119951129A3350 BATTERY 1000677 BOEING767 767332 1382001NM COCKPIT DISCHARGED A DALAK NONE L NO TEST CRCRUISE 1 SO27131DN 27883 24852 EMERGENCY EXIT LIGHT OVER FLIGHT DECK DOOR CAME ON EN ROUTE DFW AND DEPLETED BATTERY. REPLACED EMERGENCY LIGHT ASSY AND NEW BATTERYS OPN NML. 2L72 4F RTA1NM 19951208000661995120800066NM 1995 12 8 P5CA9500855 119951201A5730 PANEL BOEING747 747121 1384871NM RT WING LE DELAMINATED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23831FT 19648 FOUND RIGHT HAND WING UPPER LEADING EDGE PANEL DELAMINATED WITH SECTION MISSING JUST OUTBOARD OF NR 3 ENGINE PYLON. REPAIRED PANEL PER SRM 51-40-14. 2L74 4F A20WE 19951208000671995120800067NM 1995 12 8 SCNA95278 119951129A3270655792614 SHOCK ABSORBER BOEING727 7272J4 1384006NM TAIL SKID DAMAGED A SCNAO OTHER J WARNING INDICATION CLCLIMB 1 GL15285SC 21676 AFTER GEAR RETRACTION, TAIL SKID LIGHT ILLUMINATED. INSTALLED NEW SHOCK ABSORBER ASSEMBLY IAW MM 32-71-81 AND OPS TESTED GOOD IAW 32-71-01. 2L73 4F RTA3WE 19951208000681995120800068NM 1995 12 8 SCNA95279 119951130A291065178494061 HYD LINE BOEING727 7272J4 1384006NM NR 2 HYD PUMP LEAKING A SCNAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15284SC 21438 THE B-SYSTEM HYDRAULIC PUMP LIGHTS AND PRESSURE BEGAN TO FLUCTUATE WHILE LEVEL AT FL 310. LIGHT ILLUMINATED STEADILY WHEN B-SYSTEM HYDRAULIC QUANTITY REACHED 0. FOUND FITTING ON HYDRAULIC RETURN LINE ON NR 2 B-PUMP LEAKING. REPLACED RETURNED LINE, SERVICED HYDRAULIC SYSTEM AND THE LINE LEAK CHECKED GOOD. 2L73 4F RTA3WE 19951208000691995120800069NM 1995 12 8 SCNA95280 119951129A33501619 EEL LAMP BOEING727 727225 1384077NM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15283SC 22559 THE AFT EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. RELAMPED LIGHT AND UNIT OPS CHECKED GOOD. 2L73 4F A3WE 19951208000701995120800070NM 1995 12 8 SCNA95281 119951126A29102145014 RETURN LINE BOEING727 7272J4 1384006NM NR 13 SPOILER LEAKING A SCNAK NONE KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL15284SC 21438 AFTER DEPARTURE, THE A-SYSTEM HYDRAULIC QUANTITY DECREASED TO .25 GALLONS AND STABILIZED. FOUND RETURN LINE FOR THE NR 13 SPOILER ACTUATOR LEAKING AT THE B-NUT, TIGHTENED B-NUT AT ACTUATOR. RAN HYDRAULIC PUMPS AND NO LEAKS WERE NOTED. 2L73 4F RTA3WE 19951208000711995120800071NM 1995 12 8 SWAA950751 119951128A5531 RIB BOEING737 7372T4 1384492NM VERT STAB CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07129SW 22340 DURING SCHEDULED 1/2 D-CHECK, FOUND VERT STAB 5TH RIB ASSEMBLY CRACKED AT FASTENER HOLE ON LEFT SIDE. REPAIRED PER BOEING M/M. 2L72 4F A16WE 19951208000721995120800072NM 1995 12 8 SWAA950752 119951128A5712 RIB BOEING737 7373H4 1384600NM LT WING CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07677AA 23289 DURING SCHEDULED CHECK, FOUND LT WING I/B UPPER AFT WING PANEL RIB CRACKED. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000731995120800073NM 1995 12 8 SWAA950753 119951128A5320 CLIPS BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND THE FOLLOWING STRINGER CLIPS CRACKED: S10 AND 11R AT BS 277, S8L AT BS 685, S10L AT BS 663, S5L AND S8R AT BS 616, S8L AT BS 639, S19R AT BS 500D, S22L AT BS 380, S19 TO 20L AT BS 938, S8L AT BS 616. REPLACED PER BOEING SRM. 2L72 4F RTA16WE 19951208000741995120800074NM 1995 12 8 SWAA950754 119951128A5313 STRINGER BOEING737 7373H4 1384600NM BS 333 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND WEB AND STRINGER CRACKED AT BS 333, S8R. REPAIRED STRINGER AND REPLACED WEB PER BOEING SRM. 2L72 4F RTA16WE 19951208000751995120800075NM 1995 12 8 SWAA950755 119951128A5313 STRINGER BOEING737 7373H4 1384600NM BS 475 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND STRINGER FLANGE CRACKED AT BS 475, S22R. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000761995120800076NM 1995 12 8 SWAA950756 119951128A5320 SPLICE BOEING737 7373H4 1384600NM BS 907 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, S4R. REPLACED PER BOEING SRM. 2L72 4F RTA16WE 19951208000771995120800077NM 1995 12 8 SWAA950757 119951128A5320 SHEAR TIE BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND SHEAR TIES CRACKED AT BS 616 BETWEEN S7 AND 8L, BETWEEN S15 AND 14L, BS 360, WL 228. REPLACED PER BOEING SRM. 2L72 4F RTA16WE 19951208000781995120800078NM 1995 12 8 SWAA950758 119951128A5311 FRAME BOEING737 7373H4 1384600NM BS 616 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME I/B CHORD CRACKED AT LOWER FASTENER HOLE, BS 616 WL 200. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000791995120800079NM 1995 12 8 SWAA950759 119951128A5311 FRAME BOEING737 7373H4 1384600NM BS 294.5 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE LEFT FRAME CRACKED AT BS 294.5 WL 208 RBL 54. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000801995120800080NM 1995 12 8 SWAA950760 119951128A5311 FRAME BOEING737 7373H4 1384600NM BS 294.5 GOUGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME GOUGED AT BS 294.5, RIGHT SIDE AT S4R. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000811995120800081NM 1995 12 8 SWAA950761 119951128A5311 FRAMES BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 294 S7R, BS 616 S9L, BS 787 S9L, BS 907 S9L, BS 827 S9L, BS 867 S9L, BS 847 S9L, AND BS 887 S9L. REPAIRED ALL PER BOEING SRM. 2L72 4F RTA16WE 19951208000821995120800082NM 1995 12 8 SWAA950762 119951128A5320 ANGLE BOEING737 7373H4 1384600NM BS 570 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 570 LBL 46 TO 51, WL 170. REPLACED PER BOEING SRM. 2L72 4F RTA16WE 19951208000831995120800083NM 1995 12 8 SWAA950763 119951128A5330 SKIN BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 200 TO 201 RBL 5. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000841995120800084NM 1995 12 8 SWAA950764 119951128A5330 SKIN BOEING737 7373H4 1384600NM BS 360-971 DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AND DENTED FROM BS 360 TO 375 BETWEEN S4 AND 6L AND AT BS 962 TO 971 BETWEEN S19 TO 20L. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000851995120800085NM 1995 12 8 SWAA950765 119951128A5330 SKIN BOEING737 7373H4 1384600NM FUSELAGE DAMAGED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 318 BETWEEN 18 AND 19, BS 356 BETWEEN S23 TO 24R, BS 818 LBL 7 RBL 12 WL 151, BS 767 BETWEEN S19 AND 20L AND AT BS 203.8 LBL 21 WL 172. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000861995120800086NM 1995 12 8 SWAA950766 119951128A5330 SKIN BOEING737 7373H4 1384600NM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178 WL 218 RBL 10 TO 12 AND AT WL 217 LBL 11 TO 12, BS 178 WL 212 TO 213 RBL 5. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000871995120800087NM 1995 12 8 SWAA950767 119951128A5315 FLOORBEAM BOEING737 7373H4 1384600NM BS 986.5 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5 LBL 5 TO RBL 32 WL 208 AND 207. REPAIRED PER TRAMCO EWO 95-0727. 2L72 4F RTA16WE 19951208000881995120800088NM 1995 12 8 SWAA950768 119951128A5315 FLOORBEAM BOEING737 7373H4 1384600NM BS 328 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 328 RBL 10 WL 208. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000891995120800089NM 1995 12 8 SWAA950769 119951128A5330 SKIN BOEING737 7373H4 1384600NM BS 328 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND FWD SERVICE DOORWAY LOWER AFT CORNER SKIN CRACKED AT BS 328 RBL 64 WL 210. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000901995120800090NM 1995 12 8 SWAA950770 119951128A5330 SKIN BOEING737 7373H4 1384600NM BS 380 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07316SW 23338 DURING SCHEDULED D-CHECK, FOUND CRACK IN SKIN AT AFT EDGE OF EQUIPMENT COOLING EXHAUST, BS 380 LBL 5 WL 148. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951208000911995120800091NM 1995 12 8 UPS505121 119951125A7120 FUSE PIN BOEING757 75724APF 1384969NM RT ENGINE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01404UP 23726 WHILE ON GROUND, MAINT FOUND RT ENGINE O/B FUSE PIN CRACKED. REMOVED AND REPLACED BOTH FUSE PINS ON RT ENG IAW EO B757-440-0431. ENG OPS AND LEAK CKS GOOD. 2L72 4F RTA2NM 19951208000921995120800092CE 1995 12 8 1069583CK 119951005A291023170882 LINE LEAR 25 25B 5170511CE RT ENG PYLON FAILED A KKFAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL2383CK 183 HYDRAULIC PRESSURE WENT TO ZERO. LANDING GEAR EXTENDED USING EMERGENCY SYSTEM. UNEVENTFUL LANDING ACCOMPLISHED. REPLACED RT PYLON HYDRAULIC PRESSURE LINE, SERVICED SYSTEM WITH 5606 AND NITROGEN. PERFORMED GEAR RETRACTION AND EXTENSION, BLED BRAKES AND RELEASED FOR SERVICE. (X) 2L72 4J A10CE 19951208000931995120800093NE 1995 12 8 10995789AA 219951010A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ6106 30006NE LT ENGINE BIRD STRIKE A KKFACD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 GL23789AA8396 4590 309 211ZA032A LEFT ENGINE INGESTED BIRD ON TAKEOFF. TAKEOFF ABORTED, AIRCRAFT RETURNED TO RAMP. ENGINE WAS CLEANED, INSPECTED, AND GROUND RUN SATISFACTORY. AIRCRAFT TEST FLOWN AND RETURNED TO SERVICE. (X) 2L72 4J4 J A10CE 1E16 19951208001241995120800124CE 1995 12 8 95ZZZX6457 119950925A321123411101 TRUNNION PIN LEAR 25 25B 5170511CE LT MLG DETACHED A AGQLAO OTHER J WARNING INDICATION CLCLIMB 1 SW0598RS 148 AIRCRAFT DEPARTED AND NOTICED GEAR UNSAFE LIGHT, FLEW BY THE TOWER SEVERAL TIMES AND NOTICED THE LT GEAR WOULD NOT RETRACT, OR EXTEND COMPLETELY. FLEW THE PLANE TO ALLIANCE AIRPORT AND BELLIED IN WITH MINIMAL DAMAGE TO THE AIRFRAME. FOUND THAT LT AFT TRUNNION PIN CAME OUT AND LET THE LT GEAR COME LOOSE. SUBMITTER RECOMMENDATION - INSTALL AFT TRUNNION PIN AND BOLT THROUGH GEAR. INSPECT WITH MIRROR, THEN PHYSICALLY PLACE FINGER ON PIN BOSS AND MAKE SURE IT IS TIGHT AGAINST SPAR. 2L72 4J A10CE 19951208001281995120800128CE 1995 12 8 95ZZZX6461 119951108A2910239720435 LINE LEAR 25 25 5170506CE HYD SYS FILTER CRACKED A VLLAO OTHER K FLUID LOSS APAPPROACH 1 GL05294NW787 25031 AIRCRAFT LOST SYSTEM HYDRAULIC PRESSURE DUE TO FLUID LOSS. AFTER LANDING, GEAR WAS DOWN AND LOCKED. FOUND SMALL HAIRLINE FATIGUE CRACK IN BEND OF HYDRAULIC PRESSURE LINE. THE LINE CONNECTS HYDRAULIC SYSTEM FILTER TO SYSTEM REGULATOR. 2L72 4J A10CE 19951208001331995120800133CE 1995 12 8 95ZZZX6466 119951019A24257007453903 RATE GYRO CESSNA525 525 2076601CE COCKPIT FAILED A IMJAO OTHER I FLT. ATTITUDE INST. CRCRUISE 1 EA25800HS 95063845 5250051 RATE GYRO FAILED CAUSING THE YAW DAMPER TO DISENGAGE. TEN MINUTES LATER, THE EFIS A.C. CIRCUIT BREAKER TRIPPED (1 AMP) WHICH RESULTED IN THE LOSS OF THE EADI AND EHSI. FLIGHT WAS UNDER VFR CONDITIONS. THIS PROBLEM LED TO THE LOSS OF THE PILOT'S FLIGHT INSTRUMENTS. COPILOT'S INSTRUMENTS ARE NOT AFFECTED. SUBMITTER SUGGESTS A SEPARATE BREAKER FOR THE RATE GYRO TO PREVENT ITS FAILURE FROM CAUSING A LOSS OF ALL EFIS TUBES. 1L72 4F RTA1WI 19951208001611995120800161 1995 12 8 95ZZZX6495 419950830A3160066040211110 SYMBOL GENERATOR BELL 230 230 1182149SW COCKPIT INOPERATIVE B TI1RK NONE O OTHER ININSP/MAINT 1 SW05230JP139 1998 23019 INOPERATIVE SYMBOL GENERATOR. REMOVED AND REPLACED. 1G72 3U NCH9SW 19951208001841995120800184NM 1995 12 8 95ZZZX6518 119951028A77123039242 SENSOR DORNERDO32 DO328100 2996000NM LT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07430JS CH11036 3044 FLT 4086 - SHORTLY AFTER TAKEOFF, CREW NOTICED A LARGE TORQUE FLUX LT ENGINE. LT ENGINE SHUT DOWN, EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SENSOR IAW MM 77-12-00. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951208001851995120800185NM 1995 12 8 95ZZZX6519 119951030A3060 DEICE WIRE DORNERDO32 DO328100 2996000NM RT PROPELLER BROKEN A VNAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL07426JS 3038 FLT 4154 - CREW ELECTED TO RETURN TO FIELD AFTER RT PROPELLER HEAT FAILED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE PROPELLER DE-ICE SYSTEM IAW MM 61-00-60. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951208001861995120800186NM 1995 12 8 95ZZZX6520 119951028A77123039242 SENSOR DORNERDO32 DO328100 2996000NM LT ENGINE DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL07430JS CH11048 3044 FLT 4148 - CREW NOTICED 50 PERCENT TORQUE FLUX LT ENGINE, ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LT ENGINE NP SENSOR IAW MM 77-12-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951208001871995120800187NM 1995 12 8 95ZZZX6521 119951102A712065B903555 AFT MOUNT BOEING747 747212B 1384886NM NR 3 ENGINE DAMAGED A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV601005622 20712 JFK - LOG PAGE: E 07985 - NR 3 ENGINE AFT MOUNT THRUST LINK BOLT MISSING. REPLACED AFT ENGINE MOUNT IAW MM 71-23-03, PAGE 401, RII. BORESCOPED ENGINE AND PERFORMED ECRA 485-54-088-1 AND ECRA 485-54-089-1. REFERENCE OPERATOR CONTROL NR EIAA9556. 2L74 4F A20WE 19951208001881995120800188NM 1995 12 8 CAL950889 119951003A3350 EEL BOEING737 7372C0 1384488NM E/E HATCH INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910242 20071 GSO - THE LT E AND E HATCH PORTABLE EXIT LIGHT WAS FOUND DIM. THE E AND E HATCH PORTABLE EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-01. (X) 2L72 4F A16WE 19951208001891995120800189NM 1995 12 8 CAL950890 119951003A3350 EEL BOEING737 7372C0 1384488NM AFT BULLNOSE INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910242 20071 GSO - THE AFT BULLNOSE PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-31. (X) 2L72 4F A16WE 19951208001901995120800190NM 1995 12 8 CAL950891 119951003A3350 EEL BOEING737 7372C0 1384488NM R-2 DOOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910242 20071 GSO - THE R-2 DOOR PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EXIT LIGHT BATTERIES WERE RECHARGED IAW MM 33-51-101. (X) 2L72 4F A16WE 19951208001911995120800191NM 1995 12 8 CAL950892 119951003A3350 EEL BOEING737 7372C0 1384488NM FWD BULLNOSE INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0910242 20071 GSO - THE FORWARD BULLNOSE PORTABLE EXIT LIGHT WAS FOUND INOPERATIVE. THE PORTABLE EXIT LIGHT WAS REMOVED AND REPLACED IAW MM 33-51-31. (X) 2L72 4F A16WE 19951208001921995120800192NM 1995 12 8 CAL951035 119951106A3350 BATTERY PACK BOEING737 737130 1384435NM LT/RT OVERWING DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959207 19024 GSO - INSPECTION FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACKS FOR THE LT AND RT OVERWING EMERGENCY LIGHTS WERE REMOVED AND REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X) 2L72 4F A16WE 19951208001931995120800193NM 1995 12 8 CAL951036 119951106A3350 EEL BOEING737 737130 1384435NM AFT EXTERIOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0959207 19024 GSO - INSPECTION FOUND THE RT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE RT AFT EXTERIOR LIGHT ASSY WAS REMOVED AND REPLACED IAW MM 33-51-01. (X) 2L72 4F A16WE 19951208001941995120800194WP 1995 12 8 CAL951042 119951114A3260 DOWNLOCK SWITCH DOUG DC9 DC932 3022066WP RT MLG INOPERATIVE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0914534 47110 AWS - FLT 0575 - WHEN THE GEAR WAS EXTENDED ON APPROACH TO AUS, THE RT REAR GREEN LIGHT AND RED UNSAFE LIGHT WERE BOTH ILLUMINATED. CYCLING THE GEAR WAS NO HELP. A TOWER FLY-BY WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN FOR A NORMAL LANDING. MAINTENANCE CLEANED THE CANNON PLUG FOR THE RIGHT MLG DOWNLOCK SWITCH AND GEAR INDICATIONS CHECKED GOOD. THE SAME PROBLEM WAS REPEATED ON SUBSEQUENT FLIGHTS. AT THAT TIME, MAINTENANCE FOUND A BAD SET OF CONTACTS ON THE RT DOWNLOCK SWITCH. THE SWITCH WAS REPLACED AND THE PROBLEM WAS CORRECTED. (X) 2L72 4F A6WE 19951208001951995120800195 1995 12 8 EIAA9551 419951020A341737571832 CADC BOEING747 747121 1384871NM NR 1 SYSTEM FAILED A EIAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09473EV 19657 JFK - LOG PAGE: F 02023 - NR 1 CADC FAILED, ALL ASSOCIATED FLAGS IN VIEW, RETURNED TO JFK. REPLACED NR 1 CADC PER MM 34-12-01 AND ACCOMPLISHED PITOT/STATIC CHECK OF SYSTEM PER MM 34-11-00. OPER TEST OK. (X) 2L74 4F A20WE 19951208001961995120800196NM 1995 12 8 EIAA9552 119951029A3244 TIRE BOEING747 747212B 1384886NM NR 11 MLG TIRE FAILED A EIAAO OTHER O OTHER CLCLIMB 1 NM09485EV 199 20712 AFTER DEPARTURE, TOWER INFORMED THAT RUBBER WAS FOUND ON RUNWAY. FOUND WING-TO-BODY FAIRING PANEL, 194C, DAMAGED. PERFORMED INTERIM REPAIR PER EC/RA 485-53-002-3. REQUIRES INSPECTION EVERY 20 FLIGHT HOURS, SSR OR PERM REPAIR ON OR BEFORE 'A' CHECK AND REPLACED NR 11 MAIN WHEEL TIRE. (X) 2L74 4F A20WE 19951208001971995120800197NM 1995 12 8 EIAA9553 119951030A21507644762 FLOW CONTROL BOEING747 747212B 1384886NM NR 3 PACK FAILED A EIAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 NM09485EV 20712 JED - LOG PAGE: E 07977 - AFTER TAKEOFF, PACK NR 3 WOULD NOT OPERATE. AIRCRAFT WOULD NOT HOLD PRESSURIZATION. MADE OVERWEIGHT LANDING ON RETURN TO OEJN. INSPECTION REQUIRED. GW = 706.5. REPLACED NR 3 FLOW CONTROL AND SHUT-OFF VALVE PER MM 21-51-01, PAGE 401. OPS AND LEAK CHECK CHECKED. PERFORMED OVERWEIGHT LANDING INSPECTION PER MM 5-51-39, PAGE 201, PHASE 1 EXAMINATION, NO DAMAGE NOTED. (X) 2L74 4F A20WE 19951208001981995120800198NE 1995 12 8 EIAA9555 219951105A7200 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 OIL LOSS A EIAAE ENGINE SHUTDOWN J WARNING INDICATION NRNOT REPORTED 1 NM09479EV755943910 19898 662747 LAX - LOG PAGE: F 00729 - NR 2 ENGINE OIL QUANTITY DECREASED FROM .75 INCH TO .1850 INCH IN 2.50 HOURS, AT ONE-EIGHTH QUANTITY, REDUCED POWER TO IDLE. QUANTITY DECREASED TO ZERO AND ENGINE WAS SHUT DOWN. INSPECTED NR 2 ENGINE OIL FILTER AND CHIP DETECTORS PER MM 72-00-00, NO CONTAMINATION FOUND, CLEANED ENGINE, RAN ENGINE FOR 30 MINUTES, NO EVIDENCE OF OIL LEAK FOUND. (X) 2L74 4F4 F A20WE E20EA 19951208001991995120800199NM 1995 12 8 EIAA9556 119951102A712065B159501 ROD ASSY BOEING747 747212B 1384886NM NR 3 ENGINE BOLT MISSING A EIAAK NONE O OTHER ININSP/MAINT 1 NM09485EV601005622 20712 JFK - LOG PAGE: E 07985 - NR 3 ENGINE AFT MOUNT THRUST LINK BOLT MISSING. REPLACED AFT ENGINE MOUNT IAW MM 71-23-03, PAGE 401, RII. BORESCOPED ENGINE AND PERFORMED ECRA 485-54-088-1 AND ECRA 485-54-089-1. REFERENCE OPERATOR CONTROL NR 95ZZZX6521. (X) 2L74 4F A20WE 19951208002001995120800200NM 1995 12 8 EIAA9557 119951109A2710 CONTROL CABLE BOEING747 747212B 1384886NM AILERONS OUT OF ADJ A EIAAK NONE O OTHER ININSP/MAINT 1 NM09482EV 20713 JFK - LOG PAGE: F 03234 - AILERON CONTROL TO RIGHT BINDING, NO DIFFERENCE FLAPS RETRACTED/EXTENDED. RIGGED LOAD LIMIT INPUT CABLE REF M6670, RIGGED BACK DRIVE LOAD LIMIT ROD REF M6671, ADJUSTED RT AILERON INBD INPUT ROD REF 6672, OPS CHECK PER 27-11-00. (X) 2L74 4F A20WE 19951208002011995120800201WP 1995 12 8 VTZA96027 219951114A732189778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33110U 01514WP LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK OR OTHER PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27482UE 6037 897 P66196 IAD/BDL - FLT 6198 - DURING TAKEOFF AT 0810 HRS ON 11-14-95, ABORTED TAKEOFF DUE TO THE LT ENGINE ONLY MAKING 96 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED SCREW 'X' AND PERFORMED OPS CHECKS. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. PART TSN 11,445.0 HRS. (X) 2L72 4T4 TRTA56EU E4WE 19951208002021995120800202EU 1995 12 8 VTZA96028 119951117A32336158E ACTUATOR BAG JETSTMJETSTM3201 1500217EU NLG FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27479UE 893 FLT NR 6365 - IAD-ROC - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE NOSE GEAR UPLOCK INTRANSIT LIGHT STAYING ON AFTER GEAR INDICATED UP AND LOCKED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED NOSE GEAR RETRACTION JACK. PERFORMED OPS CHECKS, OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951208002031995120800203NE 1995 12 8 VTZA96029 219951116A7200 ENGINE JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LEFT BIRD STRIKE A VTZAK NONE C F.O.D. LDLANDING 1 EA27305UE 41019 P75036 IAD/PVD - FLT 6211 - AT 0845 HRS ON 11-16-95, ENCOUNTERED A BIRD STRIKE INTO THE LT ENGINE INTAKE. AIRCRAFT COMPLETED LANDING WITH NO FURTHER INCIDENTS. A BIRD STRIKE INSPECTION WAS PERFORMED AND AIRCRAFT WAS FERRIED TO LYH FOR AN ENGINE CHANGE. AIRCRAFT LANDED AT LYH WITH NO FURTHER INCIDENTS. AIRCRAFT IS CURRENTLY UNDERGOING AN ENGINE CHANGE IN LYH. (X) 2L72 4T4 TRTA41NM E18NE 19951208002041995120800204WP 1995 12 8 VTZA96030 219951122A732089778025 FUEL CONTROL BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE OUT OF ADJUST A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27472UE 823 P66030C FLT NR 6564- GSO-IAD - DURING CLIMB-OUT, RETURNED TO GSO DUE TO THE LEFT ENGINE RPM ROLLED BACK TO 90 PERCENT DURING CLIMB TO 1500 FT. AIRCRAFT LANDED AT GSO WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED SCREW 'X' ON THE FUEL CONTROL. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19951208002051995120800205 1995 12 8 VTZA96032 319951129A614031656294 SWITCH JETAIRJETSTMJETSTM4101 1500501EU RT ENGINE FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27315UE 41033 FLIGHT NR 6266 - IAD-BTV - ABORTED THE TAKEOFF, DUE TO THE RIGHT BETA CAP LIGHT ILLUMINATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE BETA SWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951208002061995120800206NM 1995 12 8 9519032710 119951201A3350 BATTERY BOEING727 727225 1384077NM LT OVERWING DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01820EA 22557 DURING PREFLIGHT, FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT L895 INOPERATIVE. REPLACED BATTERY M955, LIGHT CHECKED OK. 2L73 4F A3WE 19951208002071995120800207EU 1995 12 8 9519383211 119951110A5320 SILL AIRBUS320 A320211 3930320EU DOOR 2R CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01311US 125 DURING IL CHECK, FOUND CORROSION ON THE DOOR 2R LOWER SILL. REPAIRED SILL (P/N D534-80043-205), PER EA 32-104299. 2L72 4F RTA28NM 19951208002081995120800208WP 1995 12 8 9519399311 119951121A5347 CARGO TRACK DOUG DC9 DC982 3022082WP FS 579-598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01314RC 49110 DURING PERIODIC CHECK, FOUND CORROSION ON THE MID CARGO LEFT TIE-DOWN TRACK BETWEEN FS 579 TO 598. REPAIRED TRACK (P/N 5936594-501), PER EA 93-105055. 2L72 4F A6WE 19951208002091995120800209NM 1995 12 8 9519405503 119951128A5320 SILL FITTING BOEING757 757251 1384970NM CARGO DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01503US 23192 DURING T-CHECK, FOUND CORROSION IN THE AFT CARGO FORWARD DOOR SILL FITTING. REPLACED FITTING. 2L72 4F RTA2NM 19951208002101995120800210WP 1995 12 8 9519419925 119951128A5313 LONGERON DOUG DC9 DC932 3022066WP FS 996 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01925US 47472 DURING L-CHECK, FOUND CORROSION IN THE LONGERON 23L END FITTING AT FS 996. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19951208002111995120800211WP 1995 12 8 9519429153 119951130A5320 FITTING DOUG DC9 DC914 3022034WP FS 566 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND .25 INCH AND 1 INCH CRACKS IN THE VERTICAL SEAT TRACK SUPPORT FITTING FS 566. REPLACED FITTING (P/N 3916209-502), PER SRM 51-30-5. 2L72 4F A6WE 19951208002121995120800212NM 1995 12 8 9519432707 119951130A2750 RETRACT MECH BOEING727 727225 1384077NM TE FLAPS MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01816EA 22553 DURING CLIMB FLAPS SELECTED TO 2 DEGREES, INBOARD FLAPS WOULD NOT RETRACT AND ALTERNATE FLAPS WERE USED. AIRCRAFT RETURNED TO FAR AND LANDED WITHOUT INCIDENT. FLAPS WERE CHECKED ELECTRICALLY AND HYDRAULICALLY PER MAINTENANCE MANUAL. GROUND OPERATIONAL CHECK OK. 2L73 4F A3WE 19951208002131995120800213NM 1995 12 8 95FDEA01838 119951130A2710 ACTUATOR DOUG MD11 MD11F 3023600NM RT AILERON MALFUNCTIONED A FDEAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 SO25601FE 48401 UPON FLAP/SLAT RETRACTION FOLLOWING T/O, AILERON DEFLECT DISAGREE LEVEL 2 LIGHT ILLUMINATED. PERFORMED ABNORMAL CHECKLIST IN RED BOOK PAGE 2-5-13 AND IAW CHECKLIST DUMPED FUEL AND RETURNED FOR LANDING. FOUND RT O/B AILERON FULLY DEFLECTED AND LT O/B AILERON IN DROOP NEUTRAL POSITION. C/W MXP 27-2 AND DEFERRED AILERON DEFLECTION SYSTEM. DEFERRED PER MEL 27-2 AND FINAL FIX TO BE DONE IN TPE 12-3-95. REPLACED RT O/B AILERON CONTROL LINEAR ACT, OPS CK'D GOOD PER MM 27-16-02 AND FCC-1 AND FCC-2 RTS. ALL PASSED DMI CLEARED. 2L73 4F RTA22WE 19951208002141995120800214NM 1995 12 8 95FDEA01840 119951201A532069144693 CHORD BOEING727 7272S2F 1384O81NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 NOTED CRACK INDICATIONS LT 70.5 BS 760 WHILE PERFORMING INSPECTION CARD NR 7-5710-7-2308H PT1, CRACK LOCATIONS ARE THE FWD UPPER HOLE AT 11 AND 5 O'CLOCK POSITION L/B LOOKING I/B. CRACK INDICATION ARE IN THE T-CHORD, PLUS CHORD. ACCOMPLISHED CRACK CONTAINMENT BY REAMING HOLES UP TO .278 AND ACCOMPLIHSED INSTALLATION OF SMALL REPAIR PER SB 727-57-0112 AT BS 760 LBL 70.5 WL 204. 2L73 4F A3WE 19951208002151995120800215NM 1995 12 8 95FDEA01841 119951202A5330 SKIN BOEING727 727233 138408ANM FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25258FE 20940 A/C STRIKE IN FRONT OF CARGO DOOR, APPROX 12 INCHES LONG ON FUSELAGE. REMOVED GILLINER TO ACCESS BACKSIDE OF DAMAGE. REPAIRED PER EA NR 7-5330-26264 WITH FILLER, DOUBLER AND HI-LOKS. 2L73 4F RTA3WE 19951208002161995120800216NM 1995 12 8 95FDEA01842 119951201A2612 FIRE WARNING BOEING727 727232 1384082NM NR 2 ENGINE ACTIVATED A FDEAO OTHER N FALSE WARNING DEDESCENT 1 SO25206FE 22928 NR 2 ENGINE HAD FIRE WARNING IN FLT. LIGHT WENT OUT WHEN THRUST LEVER RETARDED TO IDLE. LIGHT CAME ON AT TOP OF DESCENT AT 35,000 FT. SUSPECT BLEED AIR LEAK, FIRE LOOPS CHECKED GOOD. RAN NR 2 ENGINE, CHECKED FOR AIR LEAKS, CHECKED FIRE WARNING SYSTEM. FOUND NO AIR LEAKS AND SYSTEM CHECKS OK PER MM 26-11-00. 2L73 4F A3WE 19951208002171995120800217NM 1995 12 8 95UAL900283 119951201A3350 EEL LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29175UA 24382 FLOOR EEL INOP FROM ROW 24L FWD TO LAV 104 AND DOOR 2 GALLEY CROSS AISLE. REPLACED SHORTED TWO LAMP SEGMENT NEXT TO DOOR 2L. 2L74 4F4 FRTA20WE E24NE 19951208002181995120800218NM 1995 12 8 DL72E954603 119951201A3350 BATTERY PACK 900835A BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO272824W 14152 21329 ON LAYOVER, FOUND EMERGENCY LIGHTS INOP ABOVE FWD AND AFT OVERWING EMERGENCY EXITS LT SIDE. REPLACED M1090 BATTERY PACK, EMERGENCY LIGHTS OPS NORMAL. 2L73 4F A3WE 19951208002191995120800219NM 1995 12 8 DL72K954602 119951201A5754 COVE SKIN BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27471DA 20748 FOUND DURING A-2 LETTER CHECK, NR 7 SLAT COVE SKIN ANGLE CRACKED I/B OF TAI DUCT AND UNDER STOP PAD. ALSO, NR 8 COVE SKIN ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER 57-54-0 PG 807 AND 816. 2L73 4F A3WE 19951208002201995120800220NM 1995 12 8 DL72L954595 119951130A53306554596953 SKIN BOEING727 727232 1384082NM FS 440 PUNCTURED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27512DA 21314 DURING GROUND HANDLING, A HOLE WAS PUNCTURED IN THE FUSELAGE SKIN 14 INCHES BY 18 INCHES, BETWEEN FS 420 TO 440 AND S-23R TO S-26R. A PIN IN THE TOWBAR BROKE DURING TOWING AND THE AIRCRAFT STRUCK THE TUG. A TEMPORARY REPAIR WAS INSTALLED AND THE AIRCRAFT WAS FERRIED TO ATL FROM BOS. DAMAGED AREA WAS TRIMMED OUT FROM FS 440 BUTT JOINT FORWARD FOR 25.375 INCHES AND FROM THE SKIN LAP JOINT AT S-26R TO 3.5 INCHES ABOVE S-23R. ALSO, THE STRINGER AT S-23R WAS BROKEN. STRINGER WAS REPAIRED PER BOEING 727 SRM. THE REFERENCE ER/A REPLACED THE SKIN AND INSTALLED AN EXTERNAL SPLICE DOUBLER, ERA 302820-14. 2L73 4F A3WE 19951208002211995120800221NM 1995 12 8 DL72S954573 119951130A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 DURING SHOP INSPECTION, NR 6 L/E SLAT INTERNAL RIB NR 17 WAS FOUND ROUTED BEYOND LIMITS. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208002221995120800222NM 1995 12 8 DL72S954582 119951130A5530 TIE ANGLE BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27404DA 21148 FOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGER TIE ANGLES CRACKED AT STA 157.200 2ND BAY FROM TOP LT SIDE. TWO ANGLES CRACKED AT 4TH BAY FROM TOP STA 133.800. REPAIRED PER M/M 53-30-0 PAR 3. 2L73 4F A3WE 19951208002231995120800223NM 1995 12 8 DL72S954583 119951130A575465162222 SKIN BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27408DA 21152 DURING SHOP INSPECTION, NR 6 L/E SLAT WAS FOUND WITH L/E SKIN CRACKED AT OUTBOARD END. REPAIRED PER SRM 57-30. 2L73 4F A3WE 19951208002241995120800224NM 1995 12 8 DL72S954585 119951130A5313 STRINGER BOEING727 727232 1384082NM FS 1176 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27519DA 21470 DURING INSPECTION, FOUND MISSING AND SHEARED RIVETS AT STRINGER NR 29R AT FS 1176. ALSO, FOUND STRINGER CORRODED. REPAIRED BY REPLACING SECTION OF STRINGER PER SRM 53-10-03 PG 3. 2L73 4F A3WE 19951208002251995120800225NM 1995 12 8 DL72S954588 119951201A575465162296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, A CRACK WAS FOUND IN RIB NR 18 ON NR 6 L/E SLAT. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208002261995120800226NM 1995 12 8 DL72S954589 119951201A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, RIB NR 9 ON NR 6 L/E SLAT WAS FOUND CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208002271995120800227NM 1995 12 8 DL72S954590 119951201A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, A CRACK WAS FOUND IN A PREVIOUS REPAIR IN RIB NR 10. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT. 2L73 4F A3WE 19951208002281995120800228NM 1995 12 8 DL72S954591 119951201A5754651622296 HOOK BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, A CRACK WAS FOUND IN O/B HOOK. REPAIRED PER SRM 57-50-3 FOR NR 6 L/E SLAT. 2L73 4F A3WE 19951208002291995120800229NM 1995 12 8 DL72S954592 119951201A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, RIB NR 16 WAS FOUND CRACKED. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT. 2L73 4F A3WE 19951208002301995120800230NM 1995 12 8 DL72S954593 119951201A5754651622296 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 UPON INSPECTION, A CRACK WAS FOUND IN RIB NR 9. REPAIRED PER MM 57-54-0 FOR NR 6 L/E SLAT. 2L73 4F A3WE 19951208002311995120800231NM 1995 12 8 DL72S954596 119951128A5754651622199 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT I/B SIDE OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 FIG 805. 2L73 4F A3WE 19951208002321995120800232NM 1995 12 8 DL72S954597 119951129A5754651622199 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB ON O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0 PG 805. 2L73 4F A3WE 19951208002331995120800233NM 1995 12 8 DL72S954598 119951129A5754651622199 RIB BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECITON, NR 4 L/E SLAT WAS FOUND WITH CRACKED RIB AT O/B SIDE OF THE O/B SLAT TRACK. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208002341995120800234NM 1995 12 8 DL72S954599 119951130A5754651622199 ANGLE BOEING727 727232 1384082NM NR 4 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECTION, FOUND NR 4 L/E SLAT WITH LOWER COVE PANEL SUPPORT ANGLE CRACKED AT RIB NR 9. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19951208002351995120800235NM 1995 12 8 DL72W954611 119951121A575465162241 RIB BOEING727 727247 138408FNM NR 1 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272815W 20871 DURING ROUTINE SHOP INSPECTION, RIB NR 13 FROM THE O/B END WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER THE B-727 MM 57-54-0 PG 806 AND 807, FOR NR 1 L/E SLAT. 2L73 4F A3WE 19951208002361995120800236NM 1995 12 8 DL72W954614 119951129A3350 BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO27296WA 22533 UPON TRANSFER TO GROUND, EXTERNAL POWER FLIGHT ATTENDANTS FOUND EMERGENCY EXIT LIGHTS WERE INTERMITTENTLY, AT ROW 20 TO 22 ABC. REPLACED BATTERY PACK, OPS CKS GOOD. 2L73 4F A3WE 19951208002371995120800237NM 1995 12 8 DL733954594 119951129A2530 OVEN 8606010000 BOEING737 737347 1384647NM FWD GALLEY SMOKING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27313WA 85110015 23599 SMOKE OBSERVED COMING FROM FWD GALLEY INBD OVEN. TURNED OFF AND SMOKE CLEARED. PUT ON MCO C/N 549351002 BY SLC. ITEM CLEARED BY REPLACEMENT OF OVEN. 2L72 4F RTA16WE 19951208002381995120800238NM 1995 12 8 DL757954579 119951130A3350201212 EEL PWR SUPPLY 333780100 BOEING757 757232 1384965NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27679DA 9518 26955 AFT FLOOR TRACK LIGHTING INOP. REPLACED EMERGENCY BATTERY PACK AND PWR SUPPLY. 2L72 4F RTA2NM 19951208002391995120800239NM 1995 12 8 DL767954607 119951202A2530 OVEN 828450405 BOEING767 767232 1385132NM AFT GALLEY OVERHEATED A DALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27111DN 22223 UPPER RT SIDE AFT GALLEY OVEN OVERHEATED AND BEGAN TO SMOKE. FOUND THERMOSTAT FAULTY. SET UP FOR OVEN REPLACEDMENT AND FWD TO MCO. 2L72 4F RTA1NM 19951208002401995120800240NE 1995 12 8 DL76L954613 219951130A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 MALFUNCTIONED A DALAO OTHER K FLUID LOSS CRCRUISE 1 SO27178DN 25143 724158 OIL QTY DROPPED TO 5 QTS ON RT ENG FOR MOST OF FLT. ON DESCENT INTO ATL, DROPPED TO 2 QTS AND RETURNED TO 5 AFTER LEVEL OFF. DUE TO HISTORY, ENGINE WAS REPLACED AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19951208002411995120800241 1995 12 8 DL76P954584 419951130A2330 PROJECTOR 257012489 BOEING767 767332 1382001NM CABIN FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO271402A 1105 25989 DURING CRUISE, AFTER MOVIE WAS SHOWN AND DURING HBO VIDEO BEGAN TO SMELL LIKE OVERHEATED ELECTRICS. TRACED TO C-ZONE PROJECTOR. DEACT PROJECTOR, REPLACED MID PROJECTOR AND OPS NML. MCO AND PLACARD REMOVED. 2L72 4F RTA1NM 19951208002421995120800242WP 1995 12 8 DLL15954581 119951130A3350 EEL WIRE LKHEED1011 10113853 5265020WP CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27756DR 193Y1185 ON LAYOVER, FOUND EMERGENCY AISLE LIGHTS INOP RT AISLE IN COACH. FOUND BROKEN WIRE AT 26J. REPAIRED WIRE, OPS CHECKS GOOD. 2L73 4F A23WE 19951208002431995120800243WP 1995 12 8 DLL17954575 119951130A3231 ROD ATTACH PIN LKHEED1011 10113853 5265020WP NLG DOOR NOT ATTACHED A DALAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 SO27767DA 193H1209 WHILE RAISING GEAR AT T/O, RED DOOR LIGHT AND RED INTRANSIT LIGHT REMAINED ILLUM AS WELL AS VIBS COMING FROM NOSE GEAR AREA. AFTER LOWERING GEAR VIBS WENT AWAY, BUT RED DOOR AND INTRANSIT LIGHT REMAINED ON, WITH YELLOW NOSE GEAR AND DOOR LIGHT ON S/O PANEL. INSPECTED AND FOUND RIGHT FWD NOSE GEAR DOOR FOLLOW UP ROD ATTACHING PIT PIN OUT. INSTALLED PIN, OPS NORMAL. 2L73 4F A23WE 19951208002441995120800244NM 1995 12 8 DLM88954570 119951130A2120 AIR DISTR DOUG MD88 MD88 3023688NM CABIN SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27912DL 49543 AFTER T/O, SMOKE APPEARED IN CABIN. SMOKE DETECTORS LT AND RT WENT OFF. ACCOMPLISHED CHECKLIST AND SMOKE DISAPPEARED WITH REDUCED POWER. COULD NOT ISOLATE PROBLEM PACK AND SMOKE REAPPEARED ON FINAL. PERFORMED SMOKE BURNOUT, REPLACED BOTH PACK COALESCER BAGS, RAN BOTH ENGINES TO T/O POWER WITH PACKS AND NO SMOKE WAS NOTED. 2L72 4F RTA6WE 19951208002451995120800245NM 1995 12 8 DLM88954601 119951201A2120 AIR DISTR DOUG MD88 MD88 3023688NM CABIN SMOKE A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27925DL 49712 IMMEDIATELY AFTER T/O, THE ENTIRE CABIN FILLED WITH SMOKE. RETURNED AND LANDED ASAP. NO ANTI-ICE OR APU IN USE. REPLACED APU DUE TO OIL LEAK. PERFORMED DUCT BURNOUT, REPLACED COALESCER BAGS AND RETURNED A/C TO SERVICE. 2L72 4F RTA6WE 19951208002461995120800246 1995 12 8 DLM88954615 419951201A34605D00015 DFGS SWITCH DOUG MD88 MD88 3023688NM FTL DECK FAILED A DALAA UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO27968DL 53161 DURING CRUISE AT FL 330, AIRCRAFT ROLLED HARD TO THE RIGHT, YAW DAMP AND MACH TRIM AUTOMATICALLY DISCONNECTED AND THE DFGS SWITCH C/B POPPED. A/C RETURNED TO ATL. REPLACED DFGS SWITCH A C/B RTS ON BOTH DFGS, CHECKS OK. 2L72 4F RTA6WE 19951208002471995120800247NM 1995 12 8 P5CA9500856 119951203A3231 RETRACT MECH BOEING747 747123 1384873NM RT NLG DOOR MALFUNCTIONED A P5CAAJ UNSCHED LANDING DUMP FUEL JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 WP23859FT 20326 ON DEPARTURE FROM ANC AFTER GEAR RETRACTION, RIGHT WING GEAR DOOR REMAINED OPEN AND GEAR REMAINED EXTENDED AS CONFIRMED BY BOTH PRIMARY/ALTERNATE INDICATION SYSTEMS. DUMPED FUEL TO MAX LANDING WEIGHT, RETURNED TO DEPARTURE AIRPORT. CHECKED RIG OF DOOR SEQUENCE VALVE, OPS CHECK GOOD. LUBED GEAR AND C/W GEAR SWING, ALL CHECKED NORMAL. COULD NOT DUPLICATE ON GROUND. 2L74 4F A20WE 19951208002481995120800248NE 1995 12 8 P5CA9500857 219951204A7200 ENGINE BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 1 FAILED A P5CAO OTHER Y ENGINE STOPPAGE CLCLIMB 1 WP23832FT 20347 662295 NR 1 ENGINE STALL WHILE CLIMBING FROM 34.0 TO 35.0. ALL PARAMETERS SLOW AFTER STALL, EGT DID NOT EXCEED 760 DEGREES. ON LANDING IN KHV, FOUND METAL IN TAILPIPE. ENGINE TO BE CHANGED IAW POLAR WORK CARDS M7100-002 AND M7100-002A. 2L74 4F4 F A20WE E20EA 19951208002491995120800249WP 1995 12 8 UPS804905 119951026A3260 PROX SWITCHES DOUG DC8 DC873F 302199FWP LT/RT MLG DOOR MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CLCLIMB 1 SO01807UP 46007 CREW REPORTED, WITH LANDING GEAR HANDLE IN THE UP POSITION, THE DOOR NOT LATCH LIGHT STAYED ON AND AFT LIGHT ON FE PANEL WERE NOT ON. CYCLED GEAR TWICE, NO HELP. PLACED GEAR IN UP LATCH POSITION AND LIGHT WENT OUT GIVING A GOOD UP LATCH CHECK. REPLACED LEFT AND RIGHT GEAR DOOR PROX SWITCHES AND FOUND BROKEN SPLICE ON LT PROX SWITCH. SYSTEM OPS CHECKS GOOD PER DC8 MM 32-31-04 PAGE 503 B. 2L74 4F RT4A25 19951208003331995120800333WP 1995 12 8 9519449916 119951204A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP LT NACELLE INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01949N 47566 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003341995120800334WP 1995 12 8 9519459609 119951203A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP LT NACELLE INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01609NW 47234 DURING LINE CHECK, FOUND LEFT ENGINE NACELLE LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003351995120800335WP 1995 12 8 9519469990 119951130A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018950E 47186 DURING LINE CHECK, FOUND FORWARD EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003361995120800336WP 1995 12 8 9519479909 119951202A3350 BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01959N 47255 DURING LINE CHECK, FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003371995120800337WP 1995 12 8 9519489973 119951201A3350 BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019337 47346 DURING LINE CHECK, FOUND AISLE EMERGENCY LIGHTS ROWS 5 TO 10 INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003381995120800338WP 1995 12 8 9519499609 119951201A3350 BATTERY DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01609NW 47234 DURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003391995120800339WP 1995 12 8 9519509973 119951201A3350 EEL CONTACTS DOUG DC9 DC931 3022065WP CABIN DIRTY A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019337 47346 DURING LINE CHECK, FOUND FORWARD OVERHEAD EMERGENCY LIGHT INOPERATIVE. CLEANED BULB CONTACTS. 2L72 4F A6WE 19951208003401995120800340WP 1995 12 8 9519519975 119951204A3350 BATTERY DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019339 47382 DURING LINE CHECK, FOUND BOTH FORWARD OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208003411995120800341NM 1995 12 8 9519525504 119951204A3350 BATTERY BOEING757 757251 1384970NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01504US 23193 DURING LINE CHECK, FOUND EMERGENCY LIGHTS L25, L31, L42, L33, AND L589 INOPERATIVE. REPLACED BATTERY IN M731 POWER SUPPLY AND OPERATIONAL CHECK NORMAL. 2L72 4F RTA2NM 19951208003421995120800342WP 1995 12 8 9519539861 119951202A2913AS66411LS666 HYD PUMP DOUG DC9 DC951 3022051WP LT ENGINE LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01770NC243293825 47758 DTW - ON APPROACH, LOSS OF LEFT HYDRAULIC FLUID AND PRESSURE OCCURRED AFTER AUXILIARY AND ALTERNATE PUMPS WERE ACTIVATED. FOLLOWED COCKPIT OPERATING PROCEDURES AND LANDED WITHOUT INCIDENT. FOUND LEFT ENGINE HYDRAULIC PUMP LEAKING FROM SCREW HOLE AT BOTTOM OF PUMP. HOLE THREADS WERE STRIPPED WITH SCREW HANGING FROM SAFETY WIRE. REPLACED THE LEFT ENGINE HYDRAULIC PUMP AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951208003431995120800343WP 1995 12 8 9519549876 119951203A33506014113 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01785NC 48110 DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION ESCAPE PATH LIGHTING INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY. 2L72 4F A6WE 19951208003441995120800344EU 1995 12 8 9519553238 119951130A2822 BOOST PUMPS AIRBUS320 A320211 3930320EU RT TANK FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01338NW 360 DURING TAKEOFF ROLL AS N1 REACHED 40 PERCENT, BOTH FUEL PUMPS IN THE RIGHT TANK INDICATED LOW PRESSURE, ACCOMPANIED BY BOTH PUMP FAULT LIGHTS ILLUMINATING AND A MASTER CAUTION. THE TAKEOFF WAS ABORTED. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. 2L72 4F RTA28NM 19951208003451995120800345NE 1995 12 8 9519569983 219951202A7320 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D15 52051NE NR 1 ENGINE MOISTURE CONTAM A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01983US 47282 656984 NR 1 ENGINE EPR AND N1 WERE FLUCTUATING ON POWER LEVER CHANGES AFTER DEPARTURE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED THE FCU MOISTURE TRAP. SUBSEQUENT RUNUP WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951208003461995120800346NM 1995 12 8 95FDEA01843 119951204A5311 FRAME BOEING727 727232 1384082NM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME BS 660 RBL 31 TO 36 WL 157. REPAIRED DENT IN FRAME BS 660 RBL 30 TO 43 WL 157 PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951208003471995120800347NM 1995 12 8 95FDEA01844 119951204A5311 FRAME BOEING727 727232 1384082NM BS 680 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01), ON LOWER SIDE OF FLANGE ON BS 680 FRAME BETWEEN STR 23 TO 25L. REPAIRED LOWER SIDE OF FLANGE ON BS 680 FRAME BETWEEN STR 23 TO 25L, DUE TO CORROSION BEING OUT OF LIMITS PER FEDEX SRM 53-10-01. 2L73 4F A3WE 19951208003481995120800348NM 1995 12 8 95FDEA01845 119951204A5330 SKIN BOEING727 727232 1384082NM BS 1304 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING NR0774, FOUND DENT IN THE FUSELAGE SKIN BS 1304 UNDER STR 17R. REMOVED DAMAGE, FABRICATED DOUBLER, SEALED AND INSTALLED DOUBLER PER FEDEX SRM 53-30-3 FIG 1. 2L73 4F A3WE 19951208003491995120800349NM 1995 12 8 95FDEA01846 119951204A5315 FLOORBEAM BOEING727 727232 1384082NM BS 580 DOUBLE DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25498FE 20867 UPON REMOVAL OF SEAT TRACK NR0788, FOUND DOUBLE HOLES IN FLOORBEAM BS 580 BL 0 WL 208.5. REPAIRED DOUBLE HOLES IN FLOORBEAM BS 580 BL 0 WL 208.5 IAW FEDEX SRM 53-10-8 FIG 3. 2L73 4F A3WE 19951208003501995120800350NM 1995 12 8 95FDEA01847 119951204A5330 SKIN BOEING727 727232 1384082NM BS 713 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01), ON INTERIOR OF SKIN AT BS 713 BETWEEN STR 22 TO 23L. REMOVED CORROSION FROM INTERIOR OF SKIN AT BS 713 BETWEEN STR 22 TO 23L. REMOVED .014 FROM ORIGINAL MATERIAL THICKNESS, IN AN AREA OF 1.5 INCH BY 2.5 INCH BY .050 INCH. CORROSION WAS FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-30-1. REPAIRED SKIN PER FEDEX 727 SRM 53-30-3. 2L73 4F A3WE 19951208003511995120800351NM 1995 12 8 95FDEA01848 119951204A5311 FRAME BOEING727 727232 1384082NM BS 680 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 MECHANICAL DAMAGE ON FRAME BS 680 RBL 38 WL 162. REPAIRED FRAME AT BS 680 RBL 38 WL 162 IAW FEDEX SRM 51-40-3, DUE TO MECHANICAL DAMAGE PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19951208003521995120800352NM 1995 12 8 95FDEA01849 119951204A5320 BEAM BOEING727 727232 1384082NM BS 950 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01), AT BS 950 BEAM TOP CHORD LBL TO RBL 27 WL 208.1. REMOVED CORROSION AND REPAIRED OUT OF LIMIT AREAS PER EA 7-5310-26740 AND FEDEX SRM 53-10-01. 2L73 4F A3WE 19951208003531995120800353NM 1995 12 8 95FDEA01850 119951204A532065453132 CLIP BOEING727 727227 1384078NM BS 680 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 STR CLIP IS CRACKED BS 680 STR 5L. REPLACED STR CLIP AND ACCOMPLISHED STR REPAIR, BS 680 STR 6L IAW FEDEX EA NR 7-5310-26289. 2L73 4F A3WE 19951208003541995120800354NM 1995 12 8 95FDEA01851 119951204A5330 SKIN BOEING727 727232 1384082NM BS 680 LIGHTNING STRIKEA FDEAK NONE C F.O.D. ININSP/MAINT 1 SO25498FE 20867 LIGHTNING STRIKE AT BS 680 RBL 5 WL 148. DUE TO BULGE IN SKIN PATCH AT STA 683 RBL 20 WL 150, THE ORIGINAL SKIN PATCH WAS REPLACED AND ALL WORK WAS DONE IAW FEDEX 727 SRM 53-30-3. 2L73 4F A3WE 19951208003551995120800355NM 1995 12 8 95FDEA01852 119951204A5313 STRINGER BOEING727 727232 1384082NM BS 965 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 GOUGE IN STR 7 LT, BS 965 WL 285 LBL 58. REMOVED DAMAGED STR AND REPAIRED PER SRM 53-10-3. 2L73 4F A3WE 19951208003561995120800356NM 1995 12 8 95FDEA01853 119951204A5315BAC14902864 FLOORBEAM BOEING727 727232 1384082NM BS 400 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01, 1) FLOORBEAM STA 400 WL 208.1 LBL 8. FLOORBEAM WAS REPAIRED PER FEDEX B727 SRM 53-10-8 FIG 8 AT STA 400 WL 208.1 LBL 16 TO RBL 9. 2L73 4F A3WE 19951208003571995120800357NM 1995 12 8 95FDEA01854 119951204A5311 FRAME BOEING727 727232 1384082NM BS 660 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME BS 660 LBL 34 WL 160. REPAIRED DAMAGED FRAME AT BS 660 LBL 34 WL 160 IAW FEDEX B727 SRM 51-40-3. 2L73 4F A3WE 19951208003581995120800358NM 1995 12 8 95FDEA01855 119951204A5320 SPLICE BOEING727 727232 1384082NM BS 1130 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DRILL START ON FRAME SPLICE BS 1130 BETWEEN STR 6 TO 7R. REMOVED FRAME SPLICE AT BS 1130 BETWEEN STR 6 TO 7R AND INSTALLED NEW FRAME SPLICE. 2L73 4F A3WE 19951208003591995120800359NM 1995 12 8 95FDEA01856 119951204A5311 FRAME BOEING727 727232 1384082NM BS 480 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 GOUGE AT FRAME BS 480 BETWEEN STR 14 TO 13R. REPAIRED FRAME AT BS 480 BETWEEN STR 14 TO 13R PER FEDEX 727 SRM 53-10-4. 2L73 4F A3WE 19951208003601995120800360NM 1995 12 8 95FDEA01857 119951127A5311 FRAME BOEING727 727223 1384074NM BS 640 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25274FE 22039 LOWER FWD CARGO FLOOR FRAME CRACKED STA 640 LBL 10. STOP DRILLED CRACK, INSTALLED REPAIRED PER SRM 51-40-3. 2L73 4F A3WE 19951208003611995120800361NM 1995 12 8 95FDEA01858 119951204A5311 FRAME BOEING727 727232 1384082NM BS 1030 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME AT BS 1030 BETWEEN STR 25 AND 26 LBL 30 WL 150. REPAIRED DENT IN FRAME AT BS 1030 BETWEEN STR 25 AND 26 LBL 30 WL 150 PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951208003621995120800362NM 1995 12 8 95FDEA01859 119951204A5330 SKIN BOEING727 727227 1384078NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 HFEC INSPECTION OF 6 HOLES COMMON TO BS 760 RBL 70.5 WL 208, SHOWS CRACK INDICATION IN THE UPPER FWD HOLE AND THE UPPER OUTER HOLE. THE REMAINING HOLES SHOW TINY CORROSION INDICATIONS. REPAIRED DRILL START PER EA 7-5710-26288 AND REPAIR CARD EA 7-5710-26747. 2L73 4F A3WE 19951208003631995120800363NM 1995 12 8 95FDEA01860 119951204A5313655623622 STRINGER BOEING727 727225 1384077NM BS 690-701 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25490FE 21493 CORROSION (C53-111-01-2), ON STRINGER 28R FROM BS 690 TO 701 ON O/B SIDE OF U-CHANNEL. THE CORROSION WAS FOUND WHILE WORKING CUSTOMER CARD NRO0235. CORROSION WAS FOUND OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED STR 28R BS 680 TO 720, BACK DRILLED NEW STR, TREATED METAL AND INSTALLED. 2L73 4F A3WE 19951208003641995120800364NM 1995 12 8 95FDEA01861 119951204A5347BAC15201873 SEAT TRACK BOEING747 7472R7F NM BS 1140-1260 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25639FE 21650 MAIN CARGO COMPT SEAT TRACK CORRODED BEYOND MANUFACTURER'S LIMITS AT LBL 75 STA 1140 TO 1260. REPLACED MAIN CARGO COMPT SEAT TRACK AT LBL 75 STA 1140 TO 1265 IAW SRM 51-10-01. 2L74 4F RTA20WE 19951208003651995120800365NM 1995 12 8 95FDEA01862 119951204A5347T3AC15201873 SEAT TRACK BOEING747 7472R7F NM BS 1140-1260 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25639FE 21650 MAIN CARGO COMPT SEAT TRACK CORRODED BEYOND MANUFACTURER'S LIMITS AT LBL 33 STA 1140 TO 1260. REPLACED MAIN CARGO COMPT SEAT TRACK AT LBL 33 STA 1000 TO 1265 IAW SRM 51-10-01. 2L74 4F RTA20WE 19951208003661995120800366SO 1995 12 8 COMA9512017 119951202A3240 ACCUMULATOR EMB 120 EMB120RT SO CENTER WING REQUIRED SERVICEA COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01196CA 120196 DURING TAKEOFF, RECEIVED EMERGENCY PARKING BRAKE LOW PRESSURE WARNING. SERVICED THE EMERGENCY PARKING BRAKE ACCUMULATOR TO CORRECT NITROGEN CHARGE. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951208003671995120800367SO 1995 12 8 COMA9512018 119951203A3230MS3470L106S WOW SENSOR EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01164D 120164 LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. REPLACED WEIGHT ON WHEELS SENSOR, WIRING CONNECTOR 2J0318 AT RT MLG. 2L72 4T RTA31SO 19951208003681995120800368 1995 12 8 COMA9531198 419951204A34256226342012 EFIS TUBE SAAB SF340 SF340A 7850100EU INST PANEL SMOKING A COMAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO01340SF129624339 340A014 DURING ENGINE START PILOT'S EFIS TUBES WENT BLANK AND SMOKE WAS NOTICED FROM GLARESHIELD AREA. REPLACED THE PILOT'S EAD2-EFD-86. 2L72 4T RTA52EU 19951208003691995120800369NE 1995 12 8 COMA9531199 219951130A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT HIGH OIL CONSUMPA COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01347CA 1627 340A028 367166 LEFT ENGINE OIL CONSUMPTION IS VERY HIGH. REPLACED THE LT ENGINE. 2L72 4T4 TRTA52EU E8NE6 19951208003701995120800370EA 1995 12 8 COMA9560612 119951201A5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA RT COCKPIT SHATTERED A COMAH DEACTIVATE SYST/CIRCUITS O OTHER CLCLIMB 1 SO01949CA 7080 DURING FLIGHT, RT SIDE WINDSHIELD SHATTERED. REPLACED THE COPILOT'S SIDE WINDSHIELD ASSY. 2L72 4F RTA21EA 19951208003711995120800371NE 1995 12 8 COMA9560613 219951201A73216078T55PO5 FUEL CONTROL CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LT ENGINE DEFECTIVE A COMAK NONE O OTHER CRCRUISE 1 SO01936CA 7043 THERE IS A POWER LEVER WIDTH STAGGER BETWEEN THE LT AND RT POWER LEVERS. REPLACED THE LT ENGINE FUEL CONTROL UNIT. 2L72 4F4 FRTA21EA E15NE 19951208003721995120800372EA 1995 12 8 COMA9560614 119951129A274283962 TRIM ACT CNDAIRCL600 CL6002B19 EA VERT STAB DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01927CA 7031 HORIZONTAL STABILIZER CHANNEL 2 IS INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. 2L72 4F RTA21EA 19951208003731995120800373EA 1995 12 8 COMA9560615 119951201A3250601R751461 SELECTOR VALVE CNDAIRCL600 CL6002B19 EA NLG STEERING DEFECTIVE A COMAK NONE O OTHER CLCLIMB 1 SO01938CA 7046 NOSE LANDING GEAR HESITATES BEFORE RETRACTING. REPLACED THE NLG SELECTOR VALVE. 2L72 4F RTA21EA 19951208003741995120800374 1995 12 8 COMA9560616 419951201A34183995100207A STALL COMPUTER CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 SO01914CA707 7012 STALL FAIL CAUTION MESSAGE ON EICAS. REPLACED THE STALL PROTECTION COMPUTER. 2L72 4F RTA21EA 19951208003751995120800375EA 1995 12 8 COMA9560617 119951129A5610NP1393221 WINDSHIELD CNDAIRCL600 CL6002B19 EA LT COCKPIT DEFECTIVE A COMAK NONE O OTHER UKUNKNOWN 1 SO01925CA 7027 LEFT WINDSHIELD HEAT MESSAGE ON EICAS. REPLACED THE PILOT'S SIDE WINDSHIELD ASSY. 2L72 4F RTA21EA 19951208003761995120800376WP 1995 12 8 MWEA95437 119951201A29107912697538 HYD LINE DOUG DC9 DC914 3022034WP AFT ACCESSORY LEAKING A MWEAK NONE KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 GL31400ME 45727 MKE - DURING DESCENT, PILOTS REPORT, A LOSS OF HYDRAULIC FLUID AND PRESSURE ON RIGHT SIDE SYSTEM. MAINTENANCE FOUND BROKEN HYDRAULIC LINK FROM THE RUDDER MANUAL CONTROL VALVE. INSTALLED NEW LINE, LEAK CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951208003771995120800377 1995 12 8 MWEA95438 419951203A3421258733511 VERT GYRO DOUG DC9 DC932 3022066WP FWD ACCESSORY INOP A MWEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31302ME 3562 47102 MKE - DURING CLIMBOUT, VERTICAL GYRO FLAG INTERMITTENTLY COMING INTO VIEW ON FIRST OFFICER'S ADI. FLIGHT RETURNED TO MKE. MAINTENANCE VERIFIED, REMOVED AND REPLACED NR 2 VERTICAL GYRO. OPS CHECK GOOD AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951208003781995120800378WP 1995 12 8 MWEA95439 119951204A5347 SEAT TRACK DOUG DC9 DC915 3022036WP FLIGHT COMPT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 DURING C-CHECK, FOUND CAPTAIN'S FWD OUTBOARD SEAT TRACK WORN ON TOP. MAINTENANCE REPAIRED SEAT TRACK WITH STAINLESS STEEL IAW DAC DRAWING 9957855-501. RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951208003791995120800379WP 1995 12 8 MWEA95440 119951204A5311 FRAME DOUG DC9 DC915 3022036WP BS 897 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31300ME 45718 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STA 897 IN 2 PLACES, LONGERONS 2R AND 2L. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 53-01 FIG 2 SHEET 4 AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951208003801995120800380NM 1995 12 8 SWAA950771 119951130A323069355006 UPLOCK ACTUATOR BOEING737 7373Y0 1384671NM RT MLG FAILED A SWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07664WN 23495 DURING CLIMBOUT, RIGHT MAIN GEAR EXTENDED TO FULL DOWN POSITION. CREW RECYCLED GEAR TO UP POSITION AND GEAR OPERATED NORMALLY FOR REMAINDER OF FLIGHT. AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR UPLOCK ACTUATOR, INSPECTED WALKING BEAM BOLT AND PERFORMED GEAR RETRACTION TEST PER BOEING M/M. 2L72 4F RTA16WE 19951208003811995120800381NM 1995 12 8 SWAA950772 119951130A2910 BRAKE LINE BOEING737 7375H4 138449DNM LT MLG RUPTURED A SWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW07505SW 24182 EN ROUTE, NOTED HYDRAULIC QUANTITY DROP. DIVERTED TO ELP AND MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND LEFT MAIN GEAR BRAKE LINE LEAKING. REMOVED, REPLACED LINE AND LEAKED CHECKED PER BOEING M/M. 2L72 4F RTA16WE 19951208003821995120800382EA 1995 12 8 95ZZZX6522 219951010A8520LW12186 NUT PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA NR 6 CYL CON RODDETACHED A GAJAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 NM113528Y1598 317952149 RL22168A AIRCRAFT WAS IN-FLIGHT, RT ENGINE WAS ROUGH. AFTER LANDING, FOUND NR 6 CYLINDER CONNECTING ROD END CAP HAD COME OFF DUE TO ROD BOLT NUT BECAME LOOSE THEN SHEARED BOLT. 1L72 3O3 O A20SO E14EA 19951208004431995120800443SW 1995 12 8 95ZZZX6584 119951121A5320206033110241 STIFFENER BELL 206 206L 1181522SW CENTER POST CRACKED A NYBAK NONE O OTHER ININSP/MAINT 1 EA11121NH20873 46610 WHILE PERFORMING AN INSPECTION OF THE CENTER POST AREA, MECHANIC NOTED A CRACK IN THE LT VERTICAL STIFFENER, P/N 206-033-110-241. THE CRACK WAS APPARENTLY THROUGH THE WHOLE STIFFENER. REPLACED LT VERTICAL STIFFENER, P/N 206-033-110-241, IAW AC43.13-A, CHAPTER 2, SECTION 3, AND 206 SRM-1, REPAIR 5-1-1. 1G71 3U H2SW 19951208004561995120800456WP 1995 12 8 CAL950082 119950201A7920 OIL TUBE DOUG DC10 DC1030 3023501WP NR 2 ENGINE LEAKING A CALAAE UNSCHED LANDING ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW09870703462712716 48292 EWR - FLT 0004 - THE NR 2 ENGINE LOST OIL QUANTITY WHILE IN-FLIGHT. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OUT OF SERVICE AND AN ENGINE CHANGE IS PLANNED. THE SDR WILL REMAIN OPEN FOR FURTHER DETAILS AND PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THE OIL SUPPLY TUBE HAD RUBBED AGAINST INSULATION BLANKET RESULTING IN TWO SMALL PIN HOLES. (X) 2L73 4F A22WE 19951208004571995120800457WP 1995 12 8 CAL950220 119950317A3210 TORQUE LINK DOUG DC9 DC982 3022082WP LT MLG FAILED A CALAO OTHER O OTHER LDLANDING 1 SW09168043452015645 49246 EWR - FLT 0364 - THE LT MLG SHUDDERED UPON TOUCH DOWN AT IAH. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE LT MLG UPPER TORQUE LINK HAD BROKEN AND RESULTED IN ADDITIONAL DAMAGE TO THE LT MLG, P/N 59305935511. THE LT MLG WAS REMOVED AND REPLACED IAW MM 32-11-01, PAGES 405-407, AND OPERATION CHECKED GOOD. THE SDR WILL REMAIN OPEN PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED VIBRATION AS THE CAUSE OF FAILURE. AN E.A. HAS BEEN ISSUED TO MODIFY THE HYDRAULIC SHIMMY DAMPER TO CONTROL VIBRATION. AN ADDITIONAL MODIFICATION WILL BE DONE TO INSTALL RESTRICTORS ON HYDRAULIC BRAKE LINES TO CONTROL FLOW TO BRAKES AND ANTI-SKID TO PREVENT VIBRATION. (X) 2L72 4F A6WE 19951208004581995120800458GL 1995 12 8 CAL950231 219950324A72509079M51P01 DISK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 2 ENGINE DECOUPLED A ACALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SW0968046491844461 47800 451464 FLT NR 960 - NRT - THE NR 2 ENGINE FIRE WARNING ACTIVATED ACCOMPANIED BY ENGINE POWER LOSS DURING TAKEOFF AT 40 KNOTS. THE TAKEOFF WAS ABORTED AND THE ENGINE FIRE/FAILURE CHECKLIST WAS COMPLETED. THE A/C WAS RETURNED TO THE GATE. MX FOUND THE NR 2 ENGINE TURBINE HAD FAILED WITH RESULTANT DAMAGE TO BOTH THE LEFT AND RIGHT CORE COWLS. THE LEFT AND RIGHT CORE COWLS WERE REPLACED. THE NR 2 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED LPT ROTOR DISK DECOUPLING AS THE PRIMARY CAUSE OF FAILURE. ANALYSIS WAS UNABLE TO CONFIRM REASON FOR DECOUPLING. SUBMITTER STATES, THE PREVIOUS SUPPLEMENT STATED, THERE WAS 'DISK SEPARATION', RATHER THAN 'DISK DECOUPLING'. (M) 2L73 4F4 F A22WE E23EA 19951208004591995120800459NM 1995 12 8 CAL950794 119950907A3213 BEARING BOEING737 7373T0 1384582NM RT MLG FAILED A CALAO OTHER O OTHER TXTAXI/GRND HDL 1 SW0961304 23355 RDU - FLT 0238 - THE RT MLG BRAKE APPEARED TO BE DRAGGING AFTER LANDING AT RDU. MAINTENANCE FOUND THE NR 4 WHEEL BEARING ON THE RT MLG FAILED WITH RESULTANT DAMAGE TO THE AXLE. THE LOWER STRUT ASSY WAS REPLACED. BOTH THE NR 3 AND NR 4 BRAKE, TIRE AND WHEEL ASSYS ON THE RT GEAR WERE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN PENDING INVESTIGATION OF THE BEARING FAILURE. SUPPLEMENT - ENGINEERING CONFIRMED NR 4 BEARING FAILURE AS CAUSE. (X) 2L72 4F RTA16WE 19951208004601995120800460NM 1995 12 8 CAL950942 119951020A3241 TRANSDUCER BOEING727 727224 1384076NM ANTI-SKID SYSTEMINOPERATIVE A CALACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SW0979746 22449 EWR - FLT 0293 - LOW SPEED TAKEOFF ABORT. SUPPLEMENT - TAKEOFF WAS ABORTED DUE TO A LOUD POPPING NOISE FOLLOWED BY A JOLT. THE ANTI-SKID SYSTEM WAS TROUBLESHOT AND ALL ANTI-SKID VALVES CHECKED GOOD. MAINTENANCE FOUND THE RT ANTI-SKID TRANSDUCER CONNECTOR PINS PULLED. THE CONNECTOR WAS RE-PINNED. THE LT INBD ANTI-SKID TRANSDUCER HAD PIN NR 4 PUSHED BACK. THE PIN WAS RE-SECURED. THE ANTI-SKID SYSTEM FUNCTIONED NORMALLY. (X) 2L73 4F A3WE 19951208004611995120800461NM 1995 12 8 CAL950964 119951024A531165C251134 FRAME BOEING737 737222 1384473NM BS 420 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW0910236 19937 GSO - AIRCRAFT IN ONE-HALF D-CHECK. DURING INSPECTION, FOUND CRACK APPROXIMATELY .75 INCH AT BS 420 BETWEEN S21L, S22L, S23L. STOP DRILLED CRACK AND INSTALLED DOUBLER. (X) 2L72 4F A16WE 19951208004621995120800462NM 1995 12 8 CAL951006 119951015A5311 FRAME BOEING727 727232 1384082NM BS 970 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 2 INCH CRACK IN CIRCUMFERENTIAL BY INNER FLANGE ABOVE S25L AT BS 970. AN L-ANGLE AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (X) 2L73 4F A3WE 19951208004631995120800463NM 1995 12 8 CAL951007 119951007A5320 WEB BOEING727 727232 1384082NM BS 1144-1148 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND CORROSION IN WEB, AFT FRAME OF AFT CARGO DOOR ABOVE S27R, BS 1114-BS 1148. THE CORROSION WAS REMOVED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (X) 2L73 4F A3WE 19951208004641995120800464NM 1995 12 8 CAL951017 119951103A32606552811120 ACCESSORY UNIT BOEING737 7372C0 1384488NM NLG INOPERATIVE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW09142411528 1265 20070 ORF - FLT 1215 - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO ORF, THE NOSE GEAR INITIALLY INDICATED GREEN, THEN THE RED LIGHT ILLUMINATED AND THE GREEN LIGHT WENT OUT. THE CREW PERFORMED A MANUAL GEAR EXTENSION, BUT THE LIGHT REMAINED RED. THE GEAR WAS CONFIRMED DOWN AND LOCKED BY A VISUAL CHECK THROUGH THE VIEWPORT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR ACCESSORY UNIT AT FAULT. THE LANDING GEAR ACCESSORY UNIT WAS REMOVED AND REPLACED. ALL OPERATION AND INDICATIONS CHECKED GOOD. (X) 2L72 4F A16WE 19951208004651995120800465NM 1995 12 8 CAL951018 119951103A5320 FASTENERS BOEING727 727224 1384076NM RT FUEL PANEL LOOSE A ACALAAJ UNSCHED LANDING DUMP FUEL K FLUID LOSS CRCRUISE 1 SW0966734 20663 IAH - FLT 0495 - A LIQUID VAPOR TRAIL WAS REPORTED COMING FROM BETWEEN RT OUTBOARD AILERON AND NR 7 JACKSCREW FAIRING WHILE IN-FLIGHT. FUEL WAS DUMPED TO 21,000 POUNDS AND THE TRAIL OF VAPOR CEASED. THE AIRCRAFT WAS RETURNED TO IAH. MAINTENANCE FOUND SEVERAL LOOSE FASTENERS IN RT WING LOWER SIDE FUEL ACCESS PANEL NR 15. THE FASTENERS WERE TORQUED PER MM 28-11-21, PAGE 407. THE PANEL WAS LEAK CHECKED AND NO LEAKS WERE NOTED. (X) 2L73 4F A3WE 19951208004661995120800466NM 1995 12 8 CAL951019 119951103A3350 EEL WIRE BOEING727 727227 1384078NM AFT AIRSTAIRS FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0976752 21248 EWR - FLT 0539 - A PRE-FLIGHT INSPECTION FOUND THE AFT AIRSTAIR EMERGENCY OVERHEAD LIGHTS INOPERATIVE. MAINTENANCE FOUND A BAD SPLICE ON POWER WIRE IN BUNDLE. THE WIRE WAS RE-SPLICED AND OPERATION OF THE AFT AIRSTAIR EMERGENCY OVERHEAD LIGHTS WAS RESTORED. (X) 2L73 4F A3WE 19951208004671995120800467WP 1995 12 8 CAL951020 119951024A5330 SKIN DOUG DC9 DC932 3022066WP BS 250 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND CORROSION ON SKIN AT STA 250 BELT FRAME, LONGERON 25L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38. (X) 2L72 4F A6WE 19951208004681995120800468WP 1995 12 8 CAL951021 119951019A5311 BELT FRAME DOUG DC9 DC932 3022066WP BS 980 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A .25 INCH CRACK COMING FROM HI-LOCK HOLE ON BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED SECTION OF BELT FRAME WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-03, FIGURE 32. (X) 2L72 4F A6WE 19951208004691995120800469WP 1995 12 8 CAL951022 119951019A5320 BRACKET DOUG DC9 DC932 3022066WP BS 160 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND CABIN FLOOR SUPPORT BRACKET AT STA 160, AND 8 INCHES - 10 INCHES, LEFT OF CENTERLINE CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-0. (X) 2L72 4F A6WE 19951208004701995120800470WP 1995 12 8 CAL951023 119951019A5320 DOUBLER DOUG DC9 DC932 3022066WP BS 218 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 218, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2L72 4F A6WE 19951208004711995120800471WP 1995 12 8 CAL951024 119951018A5313 LONGERON DOUG DC9 DC932 3022066WP BS 218 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND LONGERON 30 AT STA 218 CORRODED IN TWO. A LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02. (X) 2L72 4F A6WE 19951208004721995120800472NM 1995 12 8 CAL951026 119951107A2910840002074 FILTER BOEING737 7373T0 1384582NM A-HYD SYS LEAKING A CALAOH OTHER DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0963305 23356 MCO - FLT 0259 - THE A-SYSTEM HYRAULIC QUANTITY WENT TO ONE-HALF FULL INDICATION DURING CLIMB-OUT. THE INDICATION SLOWLY DECREASED TO LESS AND ONE-QUARTER FULL DURING THE FLIGHT. THE A-SYSTEM HYDRAULIC ENGINE PUMP LOW PRESSURE LIGHT ILLUMINATED DURING DESCENT INTO MCO. THE PUMP WAS TURNED OFF PER THE 'ABNORMAL' CHECK LIST. MAINTENANCE FOUND THE A-SYSTEM ELECTRIC PUMP ACOUSTICAL FILTER LEAKING FROM UPPER FITTING. THE ACOUSTICAL FILTER ASSEMBLY WAS REMOVED AND REPLACED. THE A-HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECK WAS GOOD. (X) 2L72 4F RTA16WE 19951208004731995120800473WP 1995 12 8 CAL951027 119951022A5230 PAN DOUG DC9 DC982 3022082WP BAGG DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096980337413 49229 HOU - INSPECTION FOUND A 2.5 INCH CRACK IN PAN OF FORWARD BAGGAGE BIN DOOR ON AFT SIDE AT LATCH. THE PAN WAS REPAIRED PER ECRA 5261-01000. (X) 2L72 4F A6WE 19951208004741995120800474WP 1995 12 8 CAL951028 119951026A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP BS 1271-1287 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096980337413 49229 HOU - INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL AT NUTPLATE IN AFT BAGGAGE BIN CEILING, STA 1271 TO STA 1287. A REPAIR WAS INSTALLED PER SRM 53-01. (X) 2L72 4F A6WE 19951208004751995120800475WP 1995 12 8 CAL951029 119951030A5230 PAN DOUG DC9 DC982 3022082WP BAGG DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096980337413 49229 HOU - INSPECTION FOUND A 1.75 INCH CRACK IN UPPER PAN OF MAIN BAGGAGE BIN DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-03, FIGURE 1, AND ECRA 5230-01291. (X) 2L72 4F A6WE 19951208004761995120800476WP 1995 12 8 CAL951030 119951023A5720 SUPPORT DOUG DC9 DC982 3022082WP WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096980337413 49229 HOU - INSPECTION FOUND UPPER WING PANEL T-SUPPORT CRACKED IN HALF. THE T-SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (X) 2L72 4F A6WE 19951208004771995120800477WP 1995 12 8 CAL951031 119951022A5240 ANGLE DOUG DC9 DC982 3022082WP FWD SERVICE DR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW096980337413 49229 HOU - INSPECTION FOUND THE FORWARD SERVICE DOOR UPPER FORWARD CORNER INTERNALLY CRACKED THROUGH ACROSS RADIUS OF ANGLE. THE CRACK WAS 1.5 INCHES LONG. A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. (X) 2L72 4F A6WE 19951208004781995120800478WP 1995 12 8 CAL951033 119951112A3234 GEAR HANDLE DOUG DC9 DC982 3022082WP COCKPIT BINDING A CALAO OTHER N FALSE WARNING TOTAKEOFF 1 SW0914890 49114 EWR - FLT 0609 - ALL THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHTS EXTINGUISHED. MAINTENANCE CLEANED AND LUBRICATED THE LANDING GEAR HANDLE AND SWITCH. GEAR OPERATION AND INDICATIONS TESTED GOOD. (X) 2L72 4F A6WE 19951208004791995120800479WP 1995 12 8 CAL951034 119951105A5330 SKIN DOUG DC9 DC932 3022066WP AFT FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094353767314 47112 IAH - INSPECTION FOUND A 1.5 INCH CRACK ON FUSELAGE SKIN ADJACENT TO THE LEFT AFT ATTACH ANGLE AT DORSAL FIN AREA. THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-04, FIGURE 27. (X) 2L72 4F A6WE 19951208004801995120800480WP 1995 12 8 CAL951037 119951112A3230 RETRACT MECH DOUG DC9 DC982 3022082WP LANDING GEAR MALFUNCTIONED A CALAA UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CLCLIMB 1 SW0976823 49483 ANC - FLT 0662 - THE LANDING GEAR RED UNSAFE LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED WITH LANDING GEAR NOISE AND VIBRATION AFTER THE GEAR HANDLE WAS RAISED DEPARTING ANC. CYCLING THE GEAR TWICE DID NOT HELP. THE AIRCRAFT WAS RETURNED TO ANC HERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A LANDING GEAR EXTENSION AND RETRACTION TEST PER MM 32-30-00 AND MM 07-11-00, WITH NO DEFECTS NOTED. THE FAILURE COULD NOT BE DUPLICATED. (X) 2L72 4F A6WE 19951208004811995120800481NM 1995 12 8 CAL951039 119951102A5330 SKIN BOEING727 727232 1384082NM BS 540 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091079165593 20645 INSPECTION FOUND CORROSION ON SKIN AT LAP SEAM FORWARD OF CARGO DOOR, STA 540. THE CORRODED SECTION WAS CUT OUT. A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L73 4F A3WE 19951208004821995120800482NM 1995 12 8 CAL951040 119951102A5330 LAP SEAM BOEING727 727232 1384082NM BS 660 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091079165593 20645 INSPECTION FOUND CORROSION ON SKIN AT LAP SEAM AT BS 660 AND STR 30. THE CORROSION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X) 2L73 4F A3WE 19951208004831995120800483NM 1995 12 8 CAL951041 119951102A5320 SPLICE BOEING727 727232 1384082NM BS 965 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091079165593 20645 INSPECTION FOUND STRINGER SPLICE CORRODED AT BS 965 IN AFT BAGGAGE BIN. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X) 2L73 4F A3WE 19951208004841995120800484NM 1995 12 8 CAL951043 119951114A33501000677 EEL BOEING727 727227 1384078NM COCKPIT INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW09997632487213714 20772 IAH - FLT 0384 - INSPECTION FOUND THE COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. THE COCKPIT EMERGENCY EXIT LIGHT WAS REMOVED AND REPLACED. (X) 2L73 4F A3WE 19951208004851995120800485EU 1995 12 8 VTZA96036 119951115A277091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU GUST LOCK OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA27309UE 41022 IAD/JFK - FLT 6193 - DURING TAKEOFF AT 0825 HRS ON 11-15-95, ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATON WARNING ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED GUST LOCK MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951208004861995120800486 1995 12 8 VTZA96037 419951116A34257003360948 AHRS JETAIRJETSTMJETSTM4101 1500501EU AVIONICS BAY FAILURE A VTZAO OTHER O OTHER CRCRUISE 1 EA27311UE 41029 IAD/JFK - FLT 6529 - DURING CRUISE AT 0930 HRS ON 11-16-95, THE LT ADC SOURCE AND LT AHRS SOURCE FAILED IN-FLIGHT. FLIGHT CREW SWITCHED BOTH TO RT SOURCE TO REGAIN ADC AND AHRS. AIRCRAFT WAS FERRIED TO IAD AND LT AHRS WAS REPLACED. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19951208004871995120800487EU 1995 12 8 9519573223 119951128A4900GTCP36300 APU AIRBUS320 A320211 3930320EU AFT FUSELAGE FIRE A NWAAF ACTIVATE FIRE EXT. AP FLAME/FIRE NO WARNING INDICATION ININSP/MAINT 1 GL01323US8046 184 272 AT THE GATE PRIOR TO PUSHBACK, AIRCRAFT CABIN FILLED WITH SMOKE AND FLAMES WERE REPORTED COMING FROM APU EXHAUST DUCT BY GROUND PERSONNEL. NO FIRE INDICATION IN COCKPIT. APU WAS SHUTDOWN AND APU FIRE BOTTLE DISCHARGED. AIRCRAFT PASSENGERS WERE EVACUATED THROUGH FORWARD ENTRY DOOR VIA THE JETWAY AND AT DOOR 2L IN REAR CABIN AREA VIA EMERGENCY SLIDE. NO INJURIES WERE REPORTED. THE EMERGENCY SLIDE WAS REPLACED AND THE APU PLACED ON MEL. 2L72 4F RTA28NM 19951208004881995120800488WP 1995 12 8 9519589917 119951205A3350 EEL DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01967N 47573 DURING LINE CHECK, FOUND RIGHT FORWARD DOOR AND CENTER AISLE LIGHTS MALFUNCTIONING. REPLACED LIGHT AT RIGHT FORWARD DOOR AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951208004891995120800489NM 1995 12 8 9519596302 119951205A3350 EEL CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01662US 23720 TPE - DURING LINE CHECK, THE EMERGENCY PATH FLOOR LIGHTS BETWEEN SEAT ROWS 20L TO 14L WERE FOUND INOPERATIVE. RECONNECTED PIN IN FLOOR TRACK AT LIGHT ASSEMBLY AND OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951208004901995120800490EU 1995 12 8 9519603244 119951202A3150 WARNING SYST AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 EU NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01344NW 388 731741 DURING TAKEOFF ROLL, ECAM MESSAGE FOR ENGINE NR 2 COMPRESSOR VANE ILLUMINATED. ABORTED TAKEOFF AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PERFORMED NR 2 ENGINE FADEC 'A' AND 'B' TEST. ALL INDICATIONS WERE NORMAL, NO FAULT MESSAGES. 2L72 4F4 FRTA28NM 19951208004911995120800491NM 1995 12 8 95FDEA01863 119951205A5315 FLOORBEAM BOEING727 727232 1384082NM BS 720 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AROUND FASTENER HOLES ON TOP CHORD OF FLOORBEAM AT BS 720A RBL 21 LBL 10, 16 AND 21 WL 208. TOP CHORD OF FLOORBEAM AT BS 720A LBL RBL 21 WL 208, FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED FLOORBEAM AT BS 720A LBL 32 RBL 34 WL 208 IAW FEDEX SRM 53-10-8. 2L73 4F A3WE 19951208004921995120800492NM 1995 12 8 95FDEA01864 119951205A5311 FRAME BOEING727 727232 1384082NM BS 1050 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME AT BS 1050 BETWEEN STR 25 AND 26 LBL 30 WL 150. REPAIRED DENT IN FRAME AT BS 1050 BETWEEN STR 25 TO 26 LBL 30 WL 150. ALL WORK DONE PER FEDEX SRM 51-40-03 FIG 1. 2L73 4F A3WE 19951208004931995120800493NM 1995 12 8 95FDEA01865 119951206A571265C3320292 RIB BOEING727 7272S2F 1384O81NM BS 760 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25211FE 22933 WHILE WORKING INSP CARD 7-5710-7-2308H PT 1 NOTED CRACK INDICATIONS IN THE FWD UPPER AND LOWER HOLES OF THE 70.5 CHORD BS 760 RT. CRACK INDICATIONS IN THE FWD UPPER ARE IN THE 1 AND 6 O'CLOCK POSITION, LWR FWD HOLE IN 2 O'CLOCK POSITION. TRIMMED OUT CRACKED FWD UPPER AND LOWER HOLES IN THE RIB CHORD ONLY 760 RBL 70.5 WL 206 IAW EWO 95-3292. ACCOMPLISHED ALL WORK DONE ON 70.5 IAW FEDEX PREVENTIVE MOD EA 7-5710-26723. 2L73 4F A3WE 19951208004941995120800494NM 1995 12 8 95FDEA01866 119951202A26121061096125 FIRE DETECTORS BOEING727 7272S2F 1384O81NM NR 2 ENGINE MALFUNCTIONED A FDEAO OTHER N FALSE WARNING UKUNKNOWN 1 SO25206FE 22928 ENG FIRE WARNING LIGHT ILLUMINATES WHEN POWER WAS REDUCED ON ENG NR 2. OPS AT IDLE AND LIGHT REMAINS OUT. LEAK CHECKED ENG AND FOUND NO BLEED AIR LEAKS. REMOVED AND REPLACED ENG AND FIREWALL FIRE DETECTION ELEMENTS. RAN ENG FOR 5 MINUTES AT POWER, PLUS TAXI TO AND FROM RUNUP AREA. NR 2 FIRE WARNING OPS CHECK GOOD. 2L73 4F A3WE 19951208004951995120800495NM 1995 12 8 95UAL900284 119951205A24217P2094 PMA SHAFT BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 2 ALTERNATOR FAILED A UALAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 WP29565UA16265 26669 717965 NR TWO ENGINE SHUT DOWN IN FLIGHT WITH NO INDICATION OF IMPENDING FAILURE. SUPPLEMENTAL DATA UPDATE. THE IN-FLIGHT SHUT DOWN DUE TO THE FAILURE OF THE PERMANENT MAGNET ALTERNATOR DRIVESHAFT. PRELIMINARY INVESTIGATION OF THE SHAFT FAILURE INDICATED THE SHAFT FRACTURED TRANSVERSELY THROUGH THE .031 INCH DIAMETER STUD SECTION. FURTHER INVESTIGATION BY PRATT & WHITNEY AND FIAT INDICATE THE FRACTURE WAS THE RESULT OF HIGH CYCLE FATIGUE (HCF). THE EXACT CAUSE OF THE ORGIN OF HCF IS STILL UNDER INVESTIGATION. PART TOTAL CYCLES, 6,178. 2L72 4F4 FRTA2NM E17NE 19951208004961995120800496NM 1995 12 8 95UAL900285 119951205A3350 BATTERY BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29612UA 21873 RIGHT HAND EMERGENCY ESCAPE PATH LIGHTING INOP FROM ROW 7 TO ROW 15. REPLACED BATTERY PACK, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951208004971995120800497NM 1995 12 8 95UAL900286 119951205A3350 BATTERY BOEING737 737522 138449FNM CFMINTCFM56 CFM563C1 13802EU CABIN DISCHARGED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29909UA 25009 EMERGENCY EXIT LIGHT INOP, DOOR TWO LEFT. REPLACED BATTERY, CHECKS OK. 2L72 4F4 FRTA16WE E21EU 19951208004981995120800498EU 1995 12 8 95UAL900287 119951205A3350 BATTERY PACK AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29416UA 479 RIGHT HAND OVERWING EMERGENCY EXIT LIGHT INOPERABLE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATED NORMAL. 2L72 4F RTA28NM E40NE 19951208004991995120800499NM 1995 12 8 95UAL900288 119951205A5230 SEAL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CARGO DOOR OUT OF POSITION A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP297443U 21897 AIRCRAFT WOULD NOT PRESSURE AFTER TAKEOFF WITH LEFT PACK ONLY ON. OUTFLOW VALVE FULLY CLOSED WITH MANUAL AC, NO HELP. REINSTALLED REAR CARGO DOOR SEAL, PRESSURE CHECKED NORMAL. 2L73 4F4 F A3WE E2EA 19951208005001995120800500NM 1995 12 8 95UAL900289 119951205A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM563B1 13802NE CABIN LOOSE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29386UA 24661 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW TWO. SECURED LOOSE LIGHT STRIP, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951208005011995120800501NM 1995 12 8 95UAL900290 119951205A2750 DRIVE MOTOR AVIALL 793T1001 BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE TE FLAPS MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 WP297286U 21564 RETURNED TO SAN, DUE TO FLAP CONTROL PROBLEM AND TRIP CANCELED. REPLACED OTBD FLAP ALT DRIVE MOTOR DUE TO MOTOR FAILURE, OTBD FLAP ALT UP DRIVE RELAY R71 (P/N 9274-6686) DUE TO PHASE A OPEN AND OTBD FLAP INDICATOR (P/N 2061-12-1). 2L73 4F4 F A3WE E2EA 19951208005021995120800502NM 1995 12 8 95UAL900291 119951205A3350 EEL BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29572UA 26682 EMERGENCY LIGHT INOP AT DOOR ONE RIGHT HAND. REPLACED LIGHT, CHECKS OK. 2L72 4F4 FRTA2NM E17NE 19951208005031995120800503NM 1995 12 8 95UAL900292 119951205A2820312T30004 FUEL LINE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE LT/RT ENGINE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29610UA 21871 FOUND FUEL LINE END FITTING WORN ON BOTH ENGINE FUEL LINES. WEAR IS ATTRIBUTED TO CHAFING OF THE BACKUP RING IN ASSOCIATION WITH THE O-RING, DUE TO ENGINE VIBRATION. REPLACED FUEL LINE, CHECKS OK. 2L72 4F4 FRTA1NM E3NE 19951208005041995120800504WP 1995 12 8 95UAL900293 119951205A3620 PNEU MANIFOLD DOUG DC10 DC1030F 3023504WP GE CF6 CF650C2 30018NE NR 2 FAIL INDICATION A UALAK NONE O OTHER NRNOT REPORTED 1 WP291859U 47819 NR 2 MANIFOLD INDICATION FAILURE. THE TRIP WAS CANCELED. 2L73 4F4 FRTA22WE E23EA 19951208005051995120800505NM 1995 12 8 DHL95708002 119951130A3040 TERMINAL END BOEING727 72725 1384006NM R-1 WINDOW BURNED A DHLAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01708DH 18275 DURING CLIMBOUT, R-1 TOP CENTER AND TOP RIGHT CORNER OF WINDOW BEGAN TO SPARK AND SMOKE. FLIGHT RETURNED TO AIRPORT. CLEANED CONTACT BASE, REMOVED AND REPLACED TERMINAL END ON UPPER RT CORNER OF R-1 WINDOW IAW MM30-40. 2L73 4F A3WE 19951208005061995120800506WP 1995 12 8 MWEA95441 119951201A7712JG298H1 EPR INDICATOR DOUG DC9 DC915 3022036WP COCKPIT MALFUNCTIONED A MWEACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL31300ME 45718 MKE - PILOT REPORTS, WHEN ADDING POWER FOR TAKEOFF THE RIGHT ENGINE EPR DID NOT RESPOND AND ONLY OBTAINED 1.6 EPR. ABORTED TAKEOFF AT APPROX 40 KNOTS. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE EPR INDICATOR, PERFORMED 5 TAKEOFF POWER CHECKS. ALL PARAMETERS NORMAL AND RETURNED A/C TO SERVICE. 2L72 4F A6WE 19951208005071995120800507NM 1995 12 8 P5CA9500858 119951205A5347811371411 SEAT TRACK BOEING747 747122 1384872NM LT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND CAPTAIN'S FORWARD OUTBOARD SEAT TRACK CRACKED. REPLACED SAME, OPS CHECK OK IAW MM 25-11-01. 2L74 4F A20WE 19951208005081995120800508NM 1995 12 8 P5CA9500859 119951205A53478121688 SEAT TRACK BOEING747 747122 1384872NM RT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED AND GOUGED. REPLACED SAME IAW MM 25-11-01, OPS CHECK OK. 2L74 4F A20WE 19951208005091995120800509NM 1995 12 8 P5CA9500860 119951205A534781217012 SEAT TRACK BOEING747 747122 1384872NM RT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23851FT 19756 FOUND FIRST OFFICER'S FORWARD INBOARD SEAT TRACK CRACKED. REPLACED SAME IAW MM 25-11-01, OPS CHECK OK. 2L74 4F A20WE 19951208005101995120800510NM 1995 12 8 P5CA9500861 119951203A53478121687 SEAT TRACK BOEING747 747122 1384872NM LT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23853FT 19753 FOUND PILOT'S AFT INBOARD SEAT TRACK CRACKED, CRACK CONTAINED BY STOP HOLES ON BOTH SIDES. REPLACED SEAT TRACK IAW MM 25-11-01, OPS CHECK OK. 2L74 4F A20WE 19951208005111995120800511EU 1995 12 8 QXEA9500413 119951201A3350MGG1280 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09450US 11101 SEA - EXIT LIGHT ON THE CEILING AT ROW 8 IS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951208005121995120800512NM 1995 12 8 QXEA9500414 119951202A3350 EEL CONNECTOR DORNER DORNERDO32 DO328100 2996000NM CABIN LOOSE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09328PH 3006 PDX - FLOOR PROXIMITY LIGHTING IS INOP FROM ROW 1 TO ROW 3. THE CONNECTOR WAS FOUND LOOSE. CONNECTOR WAS RECONNECTED AND LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951208005131995120800513NM 1995 12 8 QXEA9500415 119951202A33506038443 EEL POWER SUPPLYDHAV DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09828PH 287 SEA - AFT CEILING EGRESS LIGHT INOP. POWER SUPPLY AND BATTERY WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951208005141995120800514SW 1995 12 8 QXEA9500416 119951203A32302719248003 DNLOCK SPRING SWRNGN SWRNGNSA227 SA227AC 8780603SW NLG WEAK A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM0926877 AC652 BOI - NOSE GEAR IS SLOW TO INDICATE DOWN. AIRCRAFT LANDED IN BOI WITHOUT FURTHER PROBLEM. NOSE GEAR RIGHT HAND DOWNLOCK SPRING REPLACED IAW MAINT MANUAL. NLG INDICATION OPS CHECKED GOOD ON GEAR SWING. 1L72 4T A8SW 19951208005151995120800515NM 1995 12 8 QXEA9500417 119951204A3350321430 BATTERY DORNER DORNERDO32 DO328100 2996000NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09330PH 3008 PDX - GALLEY DOOR EXTERIOR EMERGENCY LIGHT IS INOP. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19951208005161995120800516SW 1995 12 8 QXEA9500418 119951204A32332752010003 ACTUATOR SWRNGN SWRNGNSA227 SA227AC 8780603SW NLG WEAK A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM093116Z AC598 PDX - NOSE GEAR IS SLOW TO EXTEND. NOSE GEAR TAKE 15 TO 20 SEC LONGER THAN MAIN GEAR. NOSE GEAR LEFT HAND ACTUATOR REPLACED AND RIGGED IAW MAINT MANUAL. NOSE GEAR OPS CHECKED GOOD ON GEAR SWING AND AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T A8SW 19951208005171995120800517EU 1995 12 8 QXEA9500419 119951204A3350 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 GEG - OVERHEAD EMERGENCY LIGHTING IS INOP AT THE AFT 4 SEAT ROWS. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951208005181995120800518NM 1995 12 8 UPS205127 119951202A5320 DOOR FRAME BOEING727 72727C 138400JNM CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01908UP 19114 WHILE ON GROUND, MAINTENANCE FOUND FWD CARGO DOOR FUSELAGE FRAME, FWD SIDE, 4TH STOP UP, DOUBLER CRACKED BEYOND STOP DRILL LIMITS. 2L73 4F A3WE 19951208005191995120800519NM 1995 12 8 UPS505126 119951202A5754 SKIN BOEING757 75724APF 1384969NM NR 5/8 LE SLATS DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01415UP 23855 WHILE ON GROUND, MAINTENANCE FOUND NUMBERS 5 AND 8 SLATS WERE DELAMINATED. 2L72 4F RTA2NM 19951208005201995120800520EU 1995 12 8 9519613220 119951121A5313 LONGERON AIRBUS320 A320211 3930320EU FS 2700-14834 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01320US 213 DURING C-CHECK, FOUND CORROSION ON STR 39R-41R AND STR 40L-41L, FRAMES 30-34. REPAIRED STRINGER (P/N 0532-31508-200) PER EA 32-104303 AND 32-104304. 2L72 4F RTA28NM 19951208005211995120800521WP 1995 12 8 9519629917 119951130A5210 DOOR DOUG DC9 DC932 3022066WP AFT CABIN CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01967N 47573 DURING M-CHECK, FOUND A CRACK IN THE AFT CABIN DOOR, LOWER LEFT SIDE. REPAIRED DOOR PER EA 99-102790. 2L72 4F A6WE 19951208005221995120800522NM 1995 12 8 9519636603 119951130A5230 WEB BOEING747 747151 1384891NM FS 1850-1900 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603US 19780 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER BEAM WEB BS 1850 AND BS 1900. REPAIRED WEB (P/N 65B04721-1) PER EA 66-104402, EA 66-104387. 2L74 4F A20WE 19951208005231995120800523WP 1995 12 8 9519649153 119951201A5320 FITTING DOUG DC9 DC914 3022034WP FS 237 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND A CRACK IN THE FS 237 RIGHT CUSP SPLICE FITTING. REPLACED FITTING PER SRM 51-30-1. 2L72 4F A6WE 19951208005241995120800524NM 1995 12 8 9519652761 119951203A5320 FITTING BOEING727 7272M7 138407SNM FS 1183 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RW 21200 DURING H-CHECK, FOUND CORROSION ON THE BS 1183 FLOOR BEAM END FITTING AT LBL 67. REPLACED FITTING PER SRM 51-10-01. 2L73 4F A3WE 19951208005251995120800525NM 1995 12 8 9519662294 119951206A2910 HYD HOSE BOEING727 727251 138408HNM LT MLG ACT FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01294US 21505 DURING APPROACH ON EXTENSION OF LANDING GEAR, AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND ALL FLUID. THE LEFT GEAR AND NOSE GEAR WERE MANUALLY CRANKED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT GEAR ACTUATOR HOSE WITH EMERGENCY HYDRAULIC HOSE. LEAK CHECKED OK. 2L73 4F A3WE 19951208005261995120800526NM 1995 12 8 9519672717 119951207A3350 BATTERY BOEING727 7272S7 138407ZNM VENTRAL STAIRS DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01721RC 22492 DURING PRE-FLIGHT, FOUND EMERGENCY LIGHTS IN VENTRAL STAIRWAY INOPERATIVE. REPLACED VENTRAL STAIRS EMERGENCY LIGHT BATTERIES. CHECKED OK. 2L73 4F A3WE 19951208005271995120800527NM 1995 12 8 95FDEA01867 119951205A5311 FRAME BOEING727 727232 1384082NM BS 950 MIS DRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25498FE 20867 INSTALLATION OF FASTENERS IN FRAME WEB BS 950F, WL 295, LBL 35 WITH IMPROPER SPACING AND FASTENERS DAMAGED. REPAIRED FRAME AT BS 950F, WL 295, LBL 35 PER FEDEX SRM 5-10-4. C/A ADDITION. 2L73 4F A3WE 19951208005281995120800528NM 1995 12 8 95FDEA01868 119951206A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 1070 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-111-01(3)) ON BOTTOM CHORD OF FLOOR BEAM AT BS 1070, WL 200, RBL 51-LBL 42 AT NUTPLATE HOLES. REPAIRED OUT OF LIMITS FLOOR BEAM AT BS 1070, WL 200 FROM SKIN-TO-SKIN. REPAIRED AS PER FEDEX EA 7-5310-26725. 2L73 4F A3WE 19951208005291995120800529NM 1995 12 8 95FDEA01869 119951206A5320 STR SPLICE BOEING727 727232 1384082NM BS 1015 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-04) ON STR 7 SPLICE LT, BS 1015. REMOVED OLD STR SPLICE, STR 7L BS 1015 AND INSTALLED NEW STR SPLICE. 2L73 4F A3WE 19951208005301995120800530NM 1995 12 8 95FDEA01870 119951206A5330 SKIN BOEING727 727232 1384082NM BS 343-374 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION ON SKIN AT BS 343-374, STR 27L-R. REMOVED CORROSION AT BS 352-360. FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-30-1. FABRICATED AND INSTALLED NEW SKIN PANEL AT BS 352-360, STR 27L-R PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951208005311995120800531NM 1995 12 8 95FDEA01871 119951206A5311 FRAME BOEING727 727232 1384082NM BS 460 DOUBLE HOLE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DOUBLE HOLE IN FRAME AT BS 460, STR 7R. REPAIRED DOUBLE HOLE IN FRAME AT BS 460, STR 7R PER FEDEX SRM 53-10-4, FIG 2. 2L73 4F A3WE 19951208005321995120800532NM 1995 12 8 95FDEA01872 119951206A5320651627910 BEAM BOEING727 727232 1384082NM BS 760-848 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01) FOUND ON TOP CHORD OF LONGITUDINAL BEAM AT BS 760-848, LBL 25, WL 208.1 (OUT OF LIMITS PER FEDEX SRM 53-10-01). REMOVED AND REPLACED TOP CHORD OF LONGITUDINAL BEAM AT BS 760-848, LBL 25, WL 208.1 IAW FEDEX 53-10-01 DUE TO CORROSION OUT OF LIMTS. 2L73 4F A3WE 19951208005331995120800533NM 1995 12 8 95FDEA01873 119951206A5330 SKIN BOEING727 727232 1384082NM BS 750-950 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING CARD NR 0812, DISCOVERED CORROSION ON SKIN ALONG FAIRING SEAM, BS 950F-1010, STR 21L-20L. REPAIRED DAMAGED SKIN ALONG FAIRING SEAM AT BS 750D-950F PER FEDEX SRM 53-30-3, FIG 14, ALSO REMOVED CORROSION FROM BS 950F-BS 1010 AND FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-30-1. 2L73 4F A3WE 19951208005341995120800534NM 1995 12 8 95FDEA01874 119951207A3234 SOLENOID BOEING727 727232 1384082NM LDG GEAR HANDLE FAILED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25499FE 21018 AFTER TAKEOFF FROM PHL, LANDING GEAR LEVER FAILED TO RAISE PASS THE OFF POSITION. THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. CHECKLIST WAS ACCOMPLISHED. LANDING GEAR WAS SUBSEQUENTLY RETRACTED USING THE LANDING GEAR LEVER LATCH TRIGGER. SWAPPED LANDING GEAR ACCESSORY MODULE, NO HELP. REINSTALLED ORIGINAL BOX. REPLACED R92 LANDING GEAR SAFETY RELAY (OVERHEAT), NO HELP. FOUND NO POWER GOING TO LEVER LATCH SOLENOID (LANDING GEAR HANDLE), WITH LEVER LATCH CIRCUIT BREAKER PULLED. CHANGED LEVER LATCH SOLENOID. GEAR HANDLE CHECKED BY DISCONNECTING WALKING BEAM. OK FOR SERVICE. 2L73 4F A3WE 19951208005351995120800535SO 1995 12 8 COMA9512019 119951206A2797 WIRE EMB 120 EMB120RT SO LT TE FLAP CHAFED A COMAO OTHER N FALSE WARNING UKUNKNOWN 1 SO01264CA9955 120256 FLAP CONTROL FAULT WARNING, LT OUTBOARD FLAPS WILL NOT MOVE. REPAIRED CHAFED WIRE AT LT OUTBOARD FLAP ACTUATOR. 2L72 4T RTA31SO 19951208005361995120800536NE 1995 12 8 COMA9520401 319951206A6114 PROP HUB SWRNGNSA227 SA227AC 8780603SW MCAULY4HFR344HFR34C652 NE LEFT LEAKING A COMAK NONE K FLUID LOSS UKUNKNOWN 1 SO01703CA 117 AC703 881168 FLUID LEAKING FROM LEFT PROPELLER HUB. REPLACED THE LT PROPELLER ASSY. 1L72 4T A8SW 6 C3PNE 19951208005371995120800537EU 1995 12 8 COMA9531200 119951205A2750HP14161005 CONTROL VALVE SAAB SF340 SF340A 7850100EU TE FLAPS MALFUNCTIONED A COMAO OTHER JF WARNING INDICATION FLT CONT AFFECTED CRCRUISE 1 SO01344CA214847989 340A25 UNCOMMANDED FLAP EXTENSION AND RETRACTION DURING FLIGHT. FLAPS WOULD OSCILLATE 3 DEGREES EVERY TEN MINUTES. REPLACED THE FLAP HYDRAULIC CONTROL VALVE. 2L72 4T RTA52EU 19951208005381995120800538NE 1995 12 8 COMA9531201 319951206A6114660714258 PROP HUB SAAB SF340 SF340A 7850100EU ROTOL R354 R3544123F13 NE PROPELLER BOLT HOLE DMG A COMAK NONE O OTHER ININSP/MAINT 1 SO01361CA7426 1427 340A056 DRG421283 FOUND MULTIPLE FLAW INDICATIONS DURING ULTRASONIC INSPECTION IN COMPLIANCE WITH AD93.19.01. PROPELLER WAS DISASSEMBLED AND HUB, S/N CW1042, REMOVED FROM SERVICE. 2L72 4T RTA52EU 6 CP61GL 19951208005391995120800539EU 1995 12 8 COMA9531202 119951205A32465006488 WHEEL SAAB SF340 SF340A 7850100EU NLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01146CA14074 NOV84139 340A146 MECHANIC REMOVED NOSE WHEEL TIRE DUE TO TIRE ROTATING ON RIM. WHEEL WAS TAKEN TO THE TIRE SHOP FOR INSPECTION. WHEEL WAS DISASSEMBLED, CLEANED AND INSPECTED. THE MECHANIC FOUND A 3.50 INCH CRACK IN THE BEAD AREA ON THE OUTBOARD SUBASSEMBLY BY USING EDDY CURRENT. WHEEL HAS BEEN REMOVED FROM SERVICE. 2L72 4T RTA52EU 19951208005401995120800540EU 1995 12 8 COMA9531203 119951205A32465006227 WHEEL 5006227 SAAB SF340 SF340A 7850100EU NLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01146CA14689 JUL84101 340A146 MECHANIC REMOVED NOSE WHEEL TIRE DUE TO TIRE ROTATING ON RIM. WHEEL WAS TAKEN TO THE TIRE SHOP FOR INSPECTION. WHEEL WAS DISASSEMBLED, CLEANED AND INSPECTED. THE MECHANIC FOUND THE CRACK BY USING EDDY CURRENT. CRACK .50 INCH LONG. WHEEL HAS BEEN REMOVED FROM SERVICE. 2L72 4T RTA52EU 19951208005411995120800541NM 1995 12 8 DL72L954625 119951204A5610 WINDOW 5893543109 BOEING727 727232 1384082NM LT COCKPIT ARCING A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27504DA 91252H7390 21306 TOP LEFT CORNER OF L1 WINDOW AROUND SCREWS THERE WAS SPARKS AND SMOKE. WITH L1 WINDOW HEAT TURNED OFF THERE WAS NO SMOKE OR SPARKS. REPLACED WINDOW AND CONTROLLER. 2L73 4F A3WE 19951208005421995120800542NM 1995 12 8 DL72S954621 119951204A3350S106 BATTERY S106 BOEING727 727232 1384082NM AFT AIRSTAIR DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27523DA 21583 DURING LAYOVER, FOUND AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19951208005431995120800543NM 1995 12 8 DL72S954622 119951127A5313 STRINGER BOEING727 727232 1384082NM BS 1000 DAMAGED A DALAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO27496DA 21076 FROM ATL/HMV - STR 29L HAS TOOLING DAMAGE AT STA 1000. CORRECTION: FORMED REPAIR DOUBLER AND BEGAN DRILLING DOUBLER. ROUTED OUT DAMAGE, FABRICATED FILLER PER M/M 53-12-0, FIG. 806. OK TO INSTALL REPAIR. INSTALLED DOUBLER PER M/M 53-12-0. 2L73 4F A3WE 19951208005441995120800544NM 1995 12 8 DL72S954623 119951120A5754 SKIN BOEING727 727232 1384082NM NR 5 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 FOUND ON CV2 CHECK, 1 CRACK IN SKIN OF NR 5 L/E FLAP AT OUTBOARD LOWER LIP HINGE CUTOUT. REPAIR: REPAIRED PER M/M 57-53-0. 2L73 4F A3WE 19951208005451995120800545NM 1995 12 8 DL72S954624 119951120A5330 SKIN BOEING727 727232 1384082NM FUSELAGE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 FOUND ON CV2 CHECK, PREVIOUSLY STOP-DRILLED CRACK IN SKIN, LT FORWARD AIRSTAIR CUT-OUT. REPAIR: REPAIRED PER M/M 53-30-0. 2L73 4F A3WE 19951208005461995120800546NM 1995 12 8 DL72W954619 119951104A2620A21885895302 SHUT DN SWITCH BOEING727 727247 138408FNM APU FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO272822W 21327 APU FIRE TEST INCOMPLETE, RED WARNING LIGHT IN FIRE HANDLE DOES NOT ILLUMINATE DURING TEST (HORN SOUNDS GOOD). APU STARTS NORMALLY AFTER RESET. REPLACED THE APU FIRE SHUT-DOWN SWITCH. SYSTEM TEST NORMAL. 2L73 4F A3WE 19951208005471995120800547NM 1995 12 8 DL72W954620 119951204A5754 DOUBLER BOEING727 727247 138408FNM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272825W 21330 FOUND ON F-1 LTR CHECK - DOUBLER CRACKED AT NR 7 SLAT INBOARD DOWNSTOP. REPLACED DOUBLER PER M/M 57-54-0. 2L73 4F A3WE 19951208005481995120800548NM 1995 12 8 DL73S954627 119951125A271069394293 SPRING BOEING737 737232 1384475NM AILERON CONTROL BROKEN A DALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SO27301DL 23073 WHEN MAKING TURNS, CONTROL YOKE DOES NOT RETURN TO CENTER. IT MUST BE MANUALLY CENTERED. ROUND AILERON RETURN SPRINGS FOR MANUAL YOKE CENTERING BROKEN. REPLACED SPRINGS. OPERATION NORMAL. 2L72 4F RTA16WE 19951208005491995120800549NM 1995 12 8 DL757954608 119951203A2560 SLIDE BULB 387 BOEING757 757232 1384965NM R1 SVC DOOR FAILED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27673DL 25978 FORWARD R1 SIDE DOOR SLIDE LIGHT BURNED OUT IN-FLIGHT. RELAMPED BULBS, OPERATION NORMAL. 2L72 4F RTA2NM 19951208005501995120800550NE 1995 12 8 DL76L954612 219951203A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 HIGH OIL CONSUMPA DALAK NONE O OTHER ININSP/MAINT 1 SO27182DN16170 25987 724416 DUE TO HIGH OIL CONSUMPTION HISTORY, NR 2 ENGINE WAS REMOVED AND ROUTED TO SHOP. 2L72 4F4 FRTA1NM E24NE 19951208005511995120800551WP 1995 12 8 DLL10954628 119951129A57111528389108 SPAR CAP LKHEED1011 10113851 5265010WP WS 332 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27733DS 193C1224 DURING ACCOMPLISHMENT OF SI 7-63370-12AD, A CRACK WAS NOTED AT HOLE NR 10A BETWEEN IWS 319.83 AND IWS 346.109 IN THE RT WING REAR SPAR UPPER CAP. THE WING SKIN IS NOT DAMAGED IN THIS LOCATION. ERA272791 AUTHORIZES INSTALLATION OF A BUSHING IN THE DISCREPANT HOLE, AND PERIODIC INSPECTIONS UNTIL THE NEXT HMV. 2L73 4F A23WE 19951208005521995120800552WP 1995 12 8 DLL15954617 119951204A33505165741 EEL POWER SUPPLY LKHEED1011 10113853 5265020WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27751DA 193W1166 ON MTC PRE-FLIGHT, FOUND EMERGENCY LIGHTS IN L-1 DOOR AREA AND FLIGHT DECK ARE INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY. EMERGENCY LIGHTS CHECK GOOD. 2L73 4F A23WE 19951208005531995120800553NM 1995 12 8 DLM11954618 119951204A33500105606203 EEL POWER SUPPLY DOUG MD11 MD11 3023602NM CABIN SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27801DE 48472 B/C EMERGENCY LIGHTS ILLUMINATE VERY DIM. REPLACED B/C POWER SUPPLY AND SHORTED TRACK LIGHT, RT AISLE FORWARD POSITION. LIGHTS CHECK GOOD. 2L73 4F RTA22WE 19951208005541995120800554NM 1995 12 8 DLM88954610 119951203A2421 GENERATOR 976J2526 DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 1 ENGINE MALFUNCTIONED A DALAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 SO27920DE UN7964 53423 726980 WHEN STARTING RT ENGINE, LT GENERATOR CYCLED ON AND OFF. FREQS WERE 380 CPS THEN CAME BACK TO 400. AFTER TAKEOFF, LT GENERATOR CYCLED ON AND OFF AT 380 CPS. RETURNED TO ATL DUE TO APU INOP. FOUND NR 1 ENG CSD FILTER INDICATOR PIN POPPED. REMOVED CSD, GENERATOR, AND COOLER. INSTALLED SERVICEABLE CSD, GENERAT0R, AND COOLER. LEAK AND OPERATION CHECK OK. 2L72 4F4 FRTA6WE E9NE 19951208005551995120800555NM 1995 12 8 P5CA9500862 119951203A53478121688 SEAT TRACK BOEING747 747124 1384874NM FO SEAT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED AT FORWARD END. REPLACED SEAT TRACK IAW MM 25-11-01, OPS CHECK OK. 2L74 4F A20WE 19951208005561995120800556NM 1995 12 8 P5CA9500863 119951203A5347 SEAT TRACK BOEING747 747132 1384882NM COPILOT SEAT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 FOUND CO-PILOT'S AFT OUTBOARD SEAT TRACK CRACKED AT AFT END. MAINTENANCE CARRYOVER ITEM 857016, TRACK TO BE REPLACED IAW MM 25-11-01. 2L74 4F A20WE 19951208005571995120800557EA 1995 12 8 SWIA95686 119951128A5210 SEAL CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE CABIN DOOR FAILED A SWIAK NONE O OTHER CLCLIMB 1 NM07408SW 7055 MAIN CABIN DOOR SEAL LEAKS. VERY LOUD SQUEAL AND LOSS OF CABIN PRESSURE. REPLACED CABIN DOOR SEAL WITH A NEW UNIT. OPERATION AND LEAK CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 19951208005581995120800558EA 1995 12 8 SWIA95687 119951129A3610 CLAMP CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE BLEED SO VALVE FAILED A SWIAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 NM07406SW 7030 LT 14TH STAGE DUCT WARNING, FOLLOWED BY LT JET PIPE OVERHEAT MESSAGE. REPLACED AFT CLAMP ON LT 14TH STAGE BLEED AIR SHUT-OFF VALVE. RAN LT 14TH STAGE BLEED AIR AND LEAK CHECK GOOD. 2L72 4F4 FRTA21EA E15NE 19951208005591995120800559SO 1995 12 8 SWIA95688 119951203A7712 GROUND BLOCK EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT TQ IND NOT GROUNDED A SWIAD RETURN TO BLOCK O OTHER CLCLIMB 1 NM07226SW 120296 AFTER DEPARTURE, ON CLIMB OUT, AFTER SETTING CLIMB DOWN, AIRCRAFT SURGED AND RT ENGINE TORQUE SETTING WENT TO 127 PERCENT. WHILE REDUCING POWER, PROP WAS AT 127 PERCENT, TORQUE MOMENTARILY 1 SEC OR LESS. AFTER INSPECTION, FOUND CASE GROUND BLOCK NOT GROUNDED FOR TORQUE INDICATOR. CLEANED AND RE-GROUND BLOCK IAW MM 77-13-00. BONDING CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951208005601995120800560NE 1995 12 8 SWIA95689 219951205A73213037139 EEC EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07226SW 120296 AFTER TAKEOFF, WITH CLIMB POWER SET, RT ENGINE TORQUE CLIMBS TO 109 PERCENT. UNABLE TO CONTROL WITH POWER LEVER. RETURNED TO YUM. SWAPPED EEC FROM SIDE TO SIDE. PROBLEM STAYED WITH RT SIDE. RAN ENGINE AT TAKEOFF POWER FOR 20 MINUTES WITH EEC OFF, NO PROBLEMS OCCURRED. EEC DEFERRED PER THE MEL 73-21-1, LT EEC'S SWAPPED FOR FURTHER CONFIRMATION. COULD NOT PRODUCE. RAN ENGINES ON GROUND, COULD NOT DUPLICATE PROBLEM. ALL SYSTEMS CHECK GOOD. NO TORQUE FLUCTUATIONS OR FUEL FLOW. 2L72 4T4 TRTA31SO E20NE 19951208005611995120800561WP 1995 12 8 UPS805128 119951129A3260 GEAR LIGHT DOUG DC8 DC871F 302199DWP LT MLG MALFUNCTIONED A IPXAO OTHER P NO WARNING INDICATION DEDESCENT 1 SO01701UP 45938 CREW REPORTED UPON SELECTING LANDING GEAR TO DOWN, NO GREEN LIGHT SHOWED ON LEFT GEAR. RECYCLED LDG GEAR WHEN GEAR HANDLE WAS SELECTED DOWN. LT MLG GREEN LIGHT ILLUMINATED BRIEFLY THEN REMAINED OUT. FLY-BY TOWER CONFIRMED ALL GEAR DOWN. APPROPRIATE EMERGENCY CHECKLISTS WERE COMPLETED. NORMAL LANDING WAS MADE, ACFT WAS STOPPED ON RUNWAY TO ALLOW MX TO INSTALL GEAR PINS PRIOR TO TAXI TO RAMP. MRR FILED OPEN. 2L74 4F RT4A25 19951208005621995120800562NM 1995 12 8 UPS805130 119951206A33501000677 EEL BOEING727 727247 138408FNM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01210UP 21697 WHILE ON GROUND IN YHM, MAINTENANCE FOUND EMERGENCY EXIT LIGHT AT L1 CABIN ENTRY DOOR DOES NOT TEST. EMERGENCY EXIT LIGHT ASSY REMOVED AND REPLACED AS PER M/M 33-50-01, OPS CHK GOOD. 2L73 4F A3WE 19951208005631995120800563NM 1995 12 8 UPS805131 119951205A5730 PANEL BOEING747 747121 1384871NM LT WING DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01690UP 20348 WHILE ON GROUND, MAINTENANCE FOUND LEFT WING LOWER TRAILING EDGE PANEL DELAMINATED. REPAIRED IAW EO B747-5730-7572A, FIXED COMPOSITE PANEL A-BEAM OF WING GEAR IAW SRM 51-10-01, SRM 51-40-09. 2L74 4F A20WE 19951208005671995120800567 1995 12 8 95ZZZX6599 419951105A34257000469901 INDICATOR HONEYWELL LEAR 55 55LEAR 5170702CE COCKPIT HSI FAILED A IMKAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 EA25733EY 80050209 057 AFTER CONFIRMING EXISITNG H.S.I. IN AIRCRAFT HAD A MALFUNCTION, A LOANER H.S.I. WAS INSTALLED AND PROPERLY TESTED. THE LOANER UNIT WAS PROVIDED BY HONEYWELL. APPROXIMATELY 20 MINUTES AFTER TAKEOFF, AIRCRAFT RETURNED TO HOME BASE TO REPORT 'PRI DIR' CIRCUIT BREAKER HAD POPPED. EXTENSIVE TROUBLESHOOTING OF SYSTEM CONCLUDED IN A DEFECTIVE LOANER H.S.I. SUBMITTER RECOMMENDATIONS - INCREASE QUALITY CONTROL ON LOANER COMPONENTS FROM HONEYWELL. 2L72 4F A10CE 19951208005921995120800592NE 1995 12 8 DJSA950003 219951110A853084086 CYLINDER DOUG DC3 DC3C 3021457WP PWA R1830 R183094 52020NE NR 11 CRACKED A DJSAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 GL239382 233 12331 P144634 AIRCRAFT EN ROUTE FRM RWI TO PTK. RT ENGINE BACKFIRED AND RAN ROUGH. PRECAUTIONARY LANDING AT HLG WITHOUT INCIDENT. UPON INSPECTION, NR 11 CYLINDER ON NR 2 ENGINE WAS FOUND TO BE CRACKED. CHANGED CYLINDER. (X) 2L72 4R4 R A669 5E4 19951208005931995120800593CE 1995 12 8 95ZZZM695 119950910A6120 BETA LINKAGE BEECH 1900 1900C 1154161CE NR 2 PROP OUT OF ADJUST A AHERAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL0380532 UC95 IMMEDIATELY AFTER LIFT OFF FROM ANC, NR 2 ENGINE AUTO FEATHERED. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BETA LINKAGE OUT OF ADJUSTMENT RIGGED BETA, TORQUE AND PROPELLER LINKAGES. ENGINE RUN AND AUTO FEATHER SYSTEM CHECK NORMAL. AIRCRAFT RETURNED TO GATE DUE TO NR 2 ENGINE AUTO FEATHER WOULD NOT ARM. MAINTENANCE REPLACED THE HIGH PRESSURE AUTO FEATHER SWITCH. OPS CHECKED OK. (M) 2L72 4T RTA24CE 19951208005941995120800594NM 1995 12 8 95ZZZM696 119951114A21503964421 FLOW CONTROL VLV BOEING737 7373G7 1384595NM NR 1 PACK FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28306AW 1044 24633 CMH - FLT 250 - CMH/PHL - AIRCRAFT WOULD NOT PRESSURIZE, AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CLOSE OUTFLOW VALVE IN ANY MODE. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR MIX VALVE, NR 1 PACK SENSE LINE, NR 2 AIR CYCLE MACHINE, AND THE NR 2 PACK AIR MIX VALVE DUCT. AIRCRAFT PRESSURIZED ON GROUND PER BMM 05-51-91, PAGE 202. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500762. 2L72 4F RTA16WE 19951208005951995120800595NM 1995 12 8 95ZZZM697 119951114A2150 AIR MIX VLV DUCT BOEING737 7373G7 1384595NM NR 2 PACK CRACKED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28306AW 24633 CMH - FLT 250 - CMH/PHL - AIRCRAFT WOULD NOT PRESSURIZE, AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CLOSE OUTFLOW VALVE IN ANY MODE. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR MIX VALVE, NR 1 PACK SENSE LINE, NR 2 AIR CYCLE MACHINE, AND THE NR 2 PACK AIR MIX VALVE DUCT. AIRCRAFT PRESSURIZED ON GROUND PER BMM 05-51-91, PAGE 202. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500762. 2L72 4F RTA16WE 19951208005961995120800596NM 1995 12 8 95ZZZM698 119951114A2150 SENSE LINE BOEING737 7373G7 1384595NM NR 1 PACK CRACKED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28306AW 24633 CMH - FLT 250 - CMH/PHL - AIRCRAFT WOULD NOT PRESSURIZE, AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CLOSE OUTFLOW VALVE IN ANY MODE. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR MIX VALVE, NR 1 PACK SENSE LINE, NR 2 AIR CYCLE MACHINE, AND THE NR 2 PACK AIR MIX VALVE DUCT. AIRCRAFT PRESSURIZED ON GROUND PER BMM 05-51-91, PAGE 202. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500762. 2L72 4F RTA16WE 19951208005971995120800597EU 1995 12 8 AWXA9500647 119950918A5230 FITTING AIRBUS320 A320231 3930325EU FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW 81 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CRACK IN AFT LOWER CORNER FITTING OF FORWARD CARGO DOOR. REMOVED AND REPLACED FITTING PER SRM 51-42-11. (M) 2L72 4F RTA28NM 19951208005981995120800598EU 1995 12 8 AWXA9500648 119950918A5280D52880008001G2 DOOR AIRBUS320 A320231 3930325EU RT MLG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW CG1052 81 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RT MLG DOOR ACTUATOR ATTACH FITTING CRACKED IN TWO PLACES. REMOVED AND REPLACED DOOR PER AIRBUS MAINTENANCE MANUAL. (M) 2L72 4F RTA28NM 19951208005991995120800599EU 1995 12 8 AWXA9500649 119950918A5280D52880008000051 DOOR AIRBUS320 A320231 3930325EU LT MLG CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28632AW CG1047 81 PHX - DURING SCHEDULED C4 INSPECTION, FOUND LOOSE MOUNT BOLTS ON LEFT MLG DOOR FORWARD HINGE MOUNT LUG ASSEMBLY. REMOVED AND REPLACED DOOR PER AIRBUS MAINTENANCE MANUAL. (M) 2L72 4F RTA28NM 19951208006001995120800600EU 1995 12 8 AWXA9500669 119950921A5553 ARM FITTING AIRBUS320 A320231 3930325EU VERTICAL STAB DELAMINATED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND VERTICAL STABILIZER UPPER RUDDER HINGE ARM FITTING SUPPORT WEB DELAMINATED AT HINGE ATTACH POINT UPPER SURFACE. REMOVED AND REPLACED ARM FITTING PER SRM 55-36-42. (M) 2L72 4F RTA28NM 19951208006011995120800601EU 1995 12 8 AWXA9500670 119950921A5320 SPLICE WEB AIRBUS320 A320231 3930325EU BS 1292 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL, AT FS 14 TO FS 17 Y 1292, CORRODED BEYOND LIMITS. REMOVED AND REPLACED RAIL SECTION PER SRM 53-00-14. (M) 2L72 4F RTA28NM 19951208006021995120800602EU 1995 12 8 AWXA9500671 119950921A5230 HANDLE AIRBUS320 A320231 3930325EU FWD CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO DOOR HANDLE MOUNT BASE CRACKED. DRILLED NEW CASTING, INSTALLED AND ADJUSTED PER SRM 52-31-11. (M) 2L72 4F RTA28NM 19951208006031995120800603EU 1995 12 8 AWXA9500672 119950921A5280 DOOR AIRBUS320 A320231 3930325EU RT MLG NICKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RT MLG DOOR T/E NICKED APPROXIMATELY 6 INCHES FROM INBOARD EDGE. ROUTED OUT DAMAGE AND APPLIED FILLER PER SRM 51-81-14. (M) 2L72 4F RTA28NM 19951208006041995120800604EU 1995 12 8 AWXA9500673 119950921A5230 HANDLE AIRBUS320 A320231 3930325EU AFT CARGO DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT CARGO DOOR HANDLE MOUNT BASE CRACKED. INSTALLED HANDLE AND LOCKING MECHANISM, AND ADJUSTED PER SRM 52-31-11. (M) 2L72 4F RTA28NM 19951208006051995120800605EU 1995 12 8 AWXA9500674 119950921A5320 RAIL AIRBUS320 A320231 3930325EU BS 254 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28633AW 082 PHX - DURING SCHEDULED C4 INSPECTION, FOUND RAIL CORRODED BEYOND LIMITS, FS 12 TO FS14, MINUS Y 254. INSTALLED REPAIR PARTS PER SRM 53-00-14. (M) 2L72 4F RTA28NM 19951208006061995120800606EU 1995 12 8 AWXA9500685 119951005A3240A25315 VALVE AIRBUS320 A320231 3930325EU PARKING BRAKE LEAKING A AWXAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 WP28624AW U596 55 EN ROUTE FROM DFW TO PHX, ECAM INDICATED YELLOW SYSTEM HYDRAULIC QUANTITY LOW. CREW SHUT YELLOW SYSTEM DOWN AND CONTINUED TO PHX, LANDING UNEVENTFULLY. MAINTENANCE FOUND PARKING BRAKE VALVE LEAKING. MAINTENANCE REMOVED AND REPLACED VALVE. OPS CHECKED PER AMM 32-43-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19951208006071995120800607EU 1995 12 8 AWXA9500717 119951023A5230 LATCH MECH AIRBUS320 A320231 3930325EU CARGO DOOR OUT OF ADJUST A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28625AW 064 CMH - FLT 990 - CMH-LAS - ON CLIMB-OUT, THE DOOR ANNUNCIATOR ECAM MESSAGE APPEARED AT 6000 FEET. AIRCRAFT RETURNED TO CMH LANDING OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AFT CARGO DOOR HANDLE UNLATCHED. MAINTENANCE ADJUSTED HANDLE LINKAGE PER AMM 52-31-11. OPS CHECK GOOD. VERTICAL SPEED WITHIN LIMITS PER AMM 05-51-11. OVERWEIGHT INSPECTION NOT REQUIRED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19951208006081995120800608EU 1995 12 8 AWXA9500729 119951030A383014403003 WASTE LVL TRANS AIRBUS320 A320231 3930325EU LAV SYSTEM MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CRCRUISE 1 WP28622AW 054 MCI - FLT 264 - CMH-PHX - AIRCRAFT DIVERTED TO MCI DUE TO FAILURE OF ALL LAVS TO FLUSH. MCI RAMP PERSONNEL SERVICED LAVS. AIRCRAFT DEPARTED MCI AND SYSTEM FAILED AGAIN. PHX MAINTENANCE DISCONNECTED WASTE LEVEL TRANSMITTER. SYSTEM OPS CHECK OK. TRANSMITTER PLACED ON ORDER. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA28NM 19951208006091995120800609EU 1995 12 8 AWXA9500731 119951101A3412102EH2BH TTL TEMP SENSOR AIRBUS320 A320231 3930325EU NR 1 FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28635AW 16055E 092 LAS - FLT NR 495 - PHX-DEN - DURING CRUISE, NAV ADRI CLASS 1 MESSAGE ILLUMINATED FOLLOWED BY NUMEROUS ADDITIONAL CLASS 1 AND 2 MESSAGES. AIRCRAFT DIVERTED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TAT 1 PROBE FAILED. REMOVED AND REPLACED PROBE. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F RTA28NM 19951208006101995120800610NM 1995 12 8 AWXA9500738 119951103A2780251N51443 TORQUE TUBE BOEING757 757225 1384959NM LE SLATS SHEARED A AWXAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP28907AW 22691 PHX-SAN - FLT NR 5 - LEADING EDGE SLAT ASYMMETRY MESSAGE APPEARED AFTER FLAPS FIVE SELECTED FOR TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND SLAT DRIVE TORQUE TUBE SHEARED UNDER SINGLE POINT REFUELING PANEL CAUSED BY BENT LIGHT BRACKET. MAINTENANCE REPLACED TORQUE TUBE ASSEMBLY UNDER SINGLE POINT REFUELING PANEL PER BMM 27-81-20. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA2NM 19951208006111995120800611NM 1995 12 8 AWXA9500744 119951108A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 377 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON FORWARD GALLEY FLOOR BEAM UPPER CAP, AT STATION 377 LBL 24. REMOVED AND REPLACED CAP PER SRM 53-00-51, FIGURE 203. (M) 2L72 4F RTA2NM 19951208006121995120800612NM 1995 12 8 AWXA9500745 119951108A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 324 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION BEYOND CLEAN UP LIMITS ON FLOOR BEAM TO CAP, AT STATION 324 RBL 45 TO RBL 60. REPAIRED PER SRM 51-70-12. (M) 2L72 4F RTA2NM 19951208006131995120800613NM 1995 12 8 AWXA9500746 119951108A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 397 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR STABILIZER CORRODED AT STATION 397 RBL 45. FABRICATED AND INSTALLED NEW STABILIZER PER SRM 51-10-00. (M) 2L72 4F RTA2NM 19951208006141995120800614NM 1995 12 8 AWXA9500747 119951108A5313 STRINGER BOEING757 7572S7 1384962NM BS 1720 LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEVERAL STRINGERS AT AFT PRESSURE BULKHEAD SHOWING SIGNS OF MOVEMENT. RETORQUED ALL BOLTS PER REQUIREMENTS OF BOEING SERVICE BULLETIN 757-53-00-17 AND ER 5-53-16-10A. (M) 2L72 4F RTA2NM 19951208006151995120800615NM 1995 12 8 AWXA9500748 119951009A5315 FLOOR BEAM BOEING737 73733A 1384673NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28169AW 23630 PHX - DURING SCHEDULED C11 INSPECTION, FOUND CORROSION AROUND FASTENER HOLES OF FLOOR BEAM UPPER 'T' CAP, BS 986.5 RBL 18. REMOVED AND REPLACED 'T' CAP PER SRM 53-70-12, FIGURE 1. (M) 2L72 4F RTA16WE 19951208006161995120800616EU 1995 12 8 AWXA9500752 119951110A3260E0245115B0 RELAY AIRBUS320 A320231 3930325EU COCKPIT FAILED A AWXAO OTHER N FALSE WARNING APAPPROACH 1 WP28626AW 65 FLT NR 1284 - SEA/PHX - CREW REPORTED, ON FINAL APPROACH EXTENDED GEAR HANDLE WITH NO INDICATION OF DOWN AND LOCKED ON FORWARD PANEL. NO ECAM WARNING OR MESSAGES PRESENT. CREW MANUALLY EXTENDED GEAR. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RELAY 40 LP. GEAR SWING COMPLIED WITH, OPERATION AND INDICATION NORMAL. AIRCRAFT RELEASED FOR FURTHER SERVICE. (M) 2L72 4F RTA28NM 19951208006171995120800617NM 1995 12 8 AWXA9500753 119951113A5240 DOOR BOEING737 7372A6 138448BNM ELECT SERVICE NOT LATCHED A AWXAO OTHER O OTHER CLCLIMB 1 WP28145AW 20194 PHX - FLT NR 573 - PHX-OAK - CREW REPORTED, ON DEPARTURE A LOUD NOISE ON THE RT SIDE OF AIRCRAFT. AIRCRAFT RETURNED TO PHX, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND ELECTRIC SERVICE DOOR OPEN. MAINTENANCE STRAIGHTENED DOOR. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19951208006181995120800618NM 1995 12 8 AWXA9500754 119951101A5320 STRIP BOEING757 7572S7 1384962NM FWD BAG PIT CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD BAG COMPARTMENT FLOOR PANEL 5B RT ATTACH STRIP CORRODED. REMOVED, FABRICATED AND INSTALLED ATTACH STRIP PER SRM 51-10-00, PARA 8. (M) 2L72 4F RTA2NM 19951208006191995120800619NM 1995 12 8 AWXA9500755 119951101A5320 CHANNEL BOEING757 7572S7 1384962NM BS 342-366 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND R1 DOOR HAT CHANNEL CORRODED BEYOND LIMITS FROM STATION 342 TO STATION 366. INSTALLED NEW FLOOR SUPPORT PER SRM 53-10-51, FIGURE 1. (M) 2L72 4F RTA2NM 19951208006201995120800620NM 1995 12 8 AWXA9500756 119951101A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 324 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR BEAM CORRODED BEYOND LIMITS AT STATION 324 RBL 45 TO RBL 60. REMOVED, FABRICATED AND INSTALLED NEW FLOOR BEAM PER SRM 51-70-12. (M) 2L72 4F RTA2NM 19951208006211995120800621NM 1995 12 8 AWXA9500757 119951101A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 377 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD GALLEY FLOOR BEAM UPPER CAP CORRODED BEYOND LIMITS, BS 377 LBL 24 TO RBL 6. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PER SRM 53-00-51, FIGURE 203. (M) 2L72 4F RTA2NM 19951208006221995120800622NM 1995 12 8 AWXA9500758 119951101A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 394 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CRACK IN FLOOR BEAM WEB FROM STATION 394 TO STATION 418 RBL 45. REPAIRED WEB PER SRM 51-70-13. (M) 2L72 4F RTA2NM 19951208006231995120800623NM 1995 12 8 AWXA9500759 119951101A5315BAC05038237 FLOOR BEAM BOEING757 7572S7 1384962NM BS 397 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR BEAM STABILIZER CORRODED AT STATION 397 RBL 24. REPAIRED PER SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19951208006241995120800624NM 1995 12 8 AWXA9500760 119951101A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 397 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR BEAM STABILIZER CORRODED AT STATION 397 RBL 45. REPAIRED PER SRN 51-10-00. (M) 2L72 4F RTA2NM 19951208006251995120800625NM 1995 12 8 AWXA9500761 119951101A5312 BLKHD BOLT BOEING757 7572S7 1384962NM BS 1720 LOOSE A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEVERAL AFT PRESSURE BULKHEAD TO STRINGER BOLTS SHOWING EVIDENCE OF MOVEMENT. RETORQUED PER ER 5-53-16-10A. (M) 2L72 4F RTA2NM 19951208006261995120800626NM 1995 12 8 AWXA9500762 119951114A215020405010 ACM BOEING737 7373G7 1384595NM NR 2 PACK FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP28306AW 03996537 24633 CMH - FLT 250 - CMH/PHL - AIRCRAFT WOULD NOT PRESSURIZE, AUTO FAIL LIGHT ILLUMINATED. CREW COULD NOT CLOSE OUTFLOW VALVE IN ANY MODE. AIRCRAFT RETURNED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 PACK AIR MIX VALVE, NR 1 PACK SENSE LINE, NR 2 AIR CYCLE MACHINE, AND THE NR 2 PACK AIR MIX VALVE DUCT. AIRCRAFT PRESSURIZED ON GROUND PER BMM 05-51-91, PAGE 202. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19951208006271995120800627NM 1995 12 8 BJNA951101 119951111A33500816901 BULB BOEING737 7372H4 138448CNM CABIN FAILED A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11456TM 20336 EMERGENCY EXIT TRACK HAS LIGHT OUT AT ROW 6. REMOVED AND REPLACED PIT TAIL AS REQUIRED, OPS GOOD AT THIS TIME. (M) 2L72 4F A16WE 19951208006281995120800628 1995 12 8 BJNA951102 419951111A256515611124DME EVAC SLIDE AIRCRUISERS 22D22901151 BOEING737 7372H4 138448CNM R-2 DOOR BOTTLE LEAKING A BJNAK NONE O OTHER ININSP/MAINT 1 WP11456TM 189231179 20336 R-2 SLIDE LEAKING PRESSURE FROM BOTTLE. REMOVED AND REPLACED THE R-2 SLIDE PER BMM 25-61-311. (M) 2L72 4F A16WE 19951208006291995120800629SO 1995 12 8 C2XA95IA332 119951115A572012017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 20, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006301995120800630SO 1995 12 8 C2XA95IA336 119951115A572012017056013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006311995120800631SO 1995 12 8 C2XA95IA337 119951115A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006321995120800632SO 1995 12 8 C2XA95IA338 119951115A572012017056017 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006331995120800633SO 1995 12 8 C2XA95IA339 119951115A572012017056019 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 5 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006341995120800634SO 1995 12 8 C2XA95IA340 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006351995120800635SO 1995 12 8 C2XA95IA341 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 15, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006361995120800636SO 1995 12 8 C2XA95IA342 119951115A572012017057015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006371995120800637SO 1995 12 8 C2XA95IA343 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006381995120800638SO 1995 12 8 C2XA95IA344 119951115A572012017057006 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 4 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006391995120800639SO 1995 12 8 C2XA95IA345 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006401995120800640SO 1995 12 8 C2XA95IA346 119951115A572012017062013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 21, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006411995120800641SO 1995 12 8 C2XA95IA347 119951115A572012017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 21, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006421995120800642SO 1995 12 8 C2XA95IA348 119951115A572012017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 21, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006431995120800643SO 1995 12 8 C2XA95IA349 119951115A572012017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 20, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006441995120800644SO 1995 12 8 C2XA95IA350 119951115A572012017062013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, NR 1 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006451995120800645SO 1995 12 8 C2XA95IA351 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006461995120800646SO 1995 12 8 C2XA95IA352 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006471995120800647SO 1995 12 8 C2XA95IA353 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 2 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006481995120800648SO 1995 12 8 C2XA95IA354 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006491995120800649SO 1995 12 8 C2XA95IA355 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951208006501995120800650NE 1995 12 8 CAL950950 219951022A7230500002102 BLADE DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE BROKEN A ACALAEA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 SW0992874231152622 49122 717425 FLT NR 423 - ELP - THE NR 1 ENG FAILED WITH AN ENGINE FIRE WARNING INDICATION WHILE EN ROUTE FROM IAH TO LAX. THE FAILURE WAS ACCOMPANIED BY VIBRATION AND LOSS OF THE LEFT HYDRAULIC SYSTEM. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO ELP WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. INVESTIGATION REVEALED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO THE LIBERATION OF A STAGE 1 BLADE WHICH BROKE ONE INCH BELOW MID-SPAN. THE BLADE FAILURE WAS CAUSED BY FOD. SUBMITTER STATES 'BLUE ICE WAS SUSPECTED'. 2L72 4F4 F A6WE E9NE 19951208006511995120800651WP 1995 12 8 CAL950983 119951028A3222 STRUT DOUG DC9 DC982 3022082WP NLG FLAT A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09937MC 49450 FLT NR 305 - EWR - THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED UNTIL THE GEAR HANDLE WAS SELECTED DOWN FOR RETURN TO EWR. THE NOSE GEAR LIGHT INDICATED GREEN FOR LANDING AT EWR. MAINTENANCE FOUND THE NLG SHOCK STRUT BOTTOMED OUT. A FULL NOSE STRUT SERVICING WAS PERFORMED IAW MM 32-21-02. THE NOSE STRUT SCHRADER VALVE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE NOSE GEAR GEAR WAS CYCLED SEVERAL TIMES AND LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L72 4F A6WE 19951208006521995120800652WP 1995 12 8 CAL950988 119951019A5311 FRAME DOUG DC9 DC932 3022066WP BS 794 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A 3 INCH CRACK EXTENDING FROM FASTENER IN FRAME AT STATION 794, STRINGER 18L. THE FRAME WAS REPAIRED IAW SRM 53-11-3, FIGURE 1. (M) 2L72 4F A6WE 19951208006531995120800653WP 1995 12 8 CAL950989 119951017A57115912125 SPAR CAP DOUG DC9 DC932 3022066WP WS 325 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND INTERGRANULAR CORROSION ON LOWER SPAR CAP AT FXLS 325. THE SPAR CAP WAS REPAIRED IAW SRM 57-01, FIGURE 2. (M) 2L72 4F A6WE 19951208006541995120800654WP 1995 12 8 CAL950990 119951017A5720 LE SPLICE DOUG DC9 DC932 3022066WP WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A 1 INCH CRACK IN LEADING EDGE SPLICE BETWEEN THE NR 3 AND NR 4 SLAT TRACK. A DOUBLER WAS INSTALLED IAW ECRA 5710-01697. (M) 2L72 4F A6WE 19951208006551995120800655WP 1995 12 8 CAL950991 119951024A53204911383502 FITTING DOUG DC9 DC932 3022066WP BS 832 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND INTERGRANULAR CORROSION AT BELTFRAME STATION 832, FITTING TO RIGHT CUSP. THE FITTING WAS REPLACED IAW SRM 51-30-0. (M) 2L72 4F A6WE 19951208006561995120800656WP 1995 12 8 CAL950992 119951019A5320 FLOOR SUPPORTS DOUG DC9 DC932 3022066WP BS 200 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STATION 200. THE CORROSION EXTENDED THE FULL LENGTH FROM LEFT TO RIGHT SIDE OF FUSELAGE. FOUR FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-2. (M) 2L72 4F A6WE 19951208006571995120800657WP 1995 12 8 CAL950993 119951019A5311 FRAME DOUG DC9 DC932 3022066WP BS 813 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM FASTENER HOLE ABOVE FLOOR ON FRAME AT STATION 813. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-03. (M) 2L72 4F A6WE 19951208006581995120800658WP 1995 12 8 CAL950995 119951018A5313 LONGERON DOUG DC9 DC932 3022066WP BS 446 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 8L AT STATION 446. THE LONGERON WAS REPAIRED IAW SRM 53-02. (M) 2L72 4F A6WE 19951208006591995120800659NM 1995 12 8 CAL951001 119951020A5730 SKIN BOEING727 727232 1384082NM LT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 1 INCH CRACK AND LOOSE FASTENERS IN LEFT WING TIP UPPER SKIN BY FLUX VALVE ACCESS AND TRAILING EDGE NAV LIGHT. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01422, REV IR. (M) 2L73 4F A3WE 19951208006601995120800660NM 1995 12 8 CAL951002 119951018A5320 FLANGE BOEING727 727232 1384082NM BS 529-740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND CORROSION AT LOWER FLANGE OF FORWARD CARGO COMPARTMENT, BS 529-740R. THE CORROSION WAS REMOVED, AN L-ANGLE WAS FABRICATED AND INSTALLED IAW AERO CORP ENGINEERING ORDER 95-208, REV IR. (M) 2L73 4F A3WE 19951208006611995120800661NM 1995 12 8 CAL951003 119951005A5311 FRAME BOEING727 727232 1384082NM BS 520 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT BS 520 ABOVE STRINGER 24L. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. (M) 2L73 4F A3WE 19951208006621995120800662NM 1995 12 8 CAL951004 119951014A5330 SKIN BOEING727 727232 1384082NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND SKIN CORRODED IN FORWARD CARGO PIT BILGE AT BS 720C TO BS 720D, LBL 20. THE CORROSION WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3. (M) 2L73 4F A3WE 19951208006631995120800663NM 1995 12 8 CAL951005 119951013A5712 RIB BOEING727 727232 1384082NM WS 686.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 2.8 INCH CRACK IN OUTBOARD SIDE OF RIB AT RIGHT WING STATION 686.5. A U-CHANNEL REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-5. (M) 2L73 4F A3WE 19951208006641995120800664NM 1995 12 8 CAL951008 119951018A5320 ANGLE BOEING727 727232 1384082NM BS 320 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND ANGLE CORRODED AT BS 320, LBL 15, WL 179, INSIDE E/E COMPARTMENT AT NOSE WHEEL, LEFT SIDE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2L73 4F A3WE 19951208006651995120800665NM 1995 12 8 CAL951009 119951014A5320 FORMER BOEING727 727232 1384082NM BS 1345 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 6 INCH CRACK IN FORMER AT STATION 1345 ABOVE NR 2 ENGINE FIREWALL. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19951208006661995120800666NM 1995 12 8 CAL951010 119951016A532069144582 SUPPORT BOEING727 727232 1384082NM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND FORWARD CARGO COMPARTMENT LOWER CIRCUMFERENTIAL SUPPORT CORRODED AT BS 740, RBL 5, S28R TIE IN. THE CIRCUMFERENTIAL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-1 AND 51-30-2. (M) 2L73 4F A3WE 19951208006671995120800667NM 1995 12 8 CAL951011 119951012A5311 FRAME BOEING727 727232 1384082NM BS 970 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND A 1.5 INCH CRACK IN FRAME AROUND RADIUS TO TOOL HOLE AT BS 970 BETWEEN S26L AND S27L. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 53-30-3 AND 51-40-2. (M) 2L73 4F A3WE 19951208006681995120800668NM 1995 12 8 CAL951012 119951015A5313 STRINGER BOEING727 727232 1384082NM BS 738 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND STRINGER 24R CORRODED AT ATTACH POINT IN FORWARD CARGO COMPARTMENT, BS 738, RBL 40. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW SECTION AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-5. (M) 2L73 4F A3WE 19951208006691995120800669NM 1995 12 8 CAL951013 119951016A5330 SKIN BOEING727 727232 1384082NM BS 737 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND LOWER SKIN AND STRINGER CORRODED AFT OF DUCT ATTACH POINT IN FORWARD CARGO COMPARTMENT AT STATION 737, RBL 25. THE CORRODED AREA WAS CUT OUT AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (M) 2L73 4F A3WE 19951208006701995120800670NM 1995 12 8 CAL951014 119951016A5313BAC1498132 STRINGER BOEING727 727232 1384082NM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND FORWARD CARGO COMPARTMENT STRINGER 27R CORRODED AT BS 740. THE CORROSION WAS REMOVED FROM STRINGER AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19951208006711995120800671NM 1995 12 8 CAL951015 119951006A5320 ATTACH FITTING BOEING727 727232 1384082NM BS 560-566 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091777965778 20634 INSPECTION FOUND CORROSION ON AND UNDER FORWARD CARGO DOOR THRESHOLD FORWARD ATTACH FITTING AT BS 560-566. THE FITTING AND CLIP ASSEMBLY UNDER FORWARD CARGO DOOR THRESHOLD WERE REMOVED AND REPLACED IAW SRM 52-10-1 AND 53-10-1. (M) 2L73 4F A3WE 19951208006721995120800672NM 1995 12 8 EISA95393 119951003A27306572799K BOB WEIGHTS BOEING727 72725 1384006NM LT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07300NE 84 18974 LEFT ELEVATOR BOB WEIGHTS FOUND CRACKED. REMOVED AND REPLACED ELEVATOR BOB WEIGHTS IAW B727 MM 27-30-0. (M) 2L73 4F A3WE 19951208006731995120800673NM 1995 12 8 EISA95394 119950913A5523 TE SKIN BOEING727 72725 1384006NM LT ELEVATOR TAB DISBONDED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 LEFT ELEVATOR TAB TRAILING EDGE HAS DISBONDED AT THE INBOARD END. REPAIRED AND REBALANCED IAW SRM 51-40-10 FIG 2 DETAIL 2 AND INSTALLED IAW 27-30-11. (M) 2L73 4F A3WE 19951208006741995120800674NM 1995 12 8 EISA95395 119950914A5330 SKIN BOEING727 72725 1384006NM CARGO DR AREA TORN A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 UPON SCHEDULED INSPECTION, FOUND HOLE AND TEAR IN SKIN UNDER THRESHOLD OF THE AFT CARGO BIN CUTOUT. REPAIRED DISCREPANCY IAW EO 1280-003. (M) 2L73 4F A3WE 19951208006751995120800675NM 1995 12 8 EISA95396 119950911A574169139004 BOTTLE PIN BOEING727 72725 1384006NM RT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 RIGHT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT FORWARD BOTTLE PIN WITH SERVICEABLE UNIT IAW BOEING MM CH 57-00-00. (M) 2L73 4F A3WE 19951208006761995120800676NM 1995 12 8 EISA95397 119950911A574169139015 BOTTLE PIN BOEING727 72725 1384006NM RT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 RIGHT AFT WING FITTING TERMINAL BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED RIGHT AFT WING BOTTLE PIN, P/N 69-13901-5, IAW MM 57-00-00. (M) 2L73 4F A3WE 19951208006771995120800677NM 1995 12 8 EISA95398 119950911A574169139015 BOTTLE PIN BOEING727 72725 1384006NM LT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 LEFT AFT WING TERMINAL FITTING IS PITTED AND CHROME IS FLAKING. REMOVED AND REPLACED WITH SERVICEABLE UNIT, P/N 69-13901-5, IAW BOEING MM 57-00-00. (M) 2L73 4F A3WE 19951208006781995120800678NM 1995 12 8 EISA95399 119950912A574169139004 BOTTLE PIN BOEING727 72725 1384006NM LT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 LEFT FORWARD WING TERMINAL FITTING BOTTLE PIN IS PITTED AND CHROME IS FLAKING OFF. REMOVED AND REPLACED BOTTLE PIN WITH SEREVICEABLE UNIT IAW BOEING MAINTENANCE MANUAL CHAPTER 57. (M) 2L73 4F A3WE 19951208006791995120800679NM 1995 12 8 EISA95400 119950913A273165C337351 BOB WEIGHTS BOEING727 72725 1384006NM RT ELEVATOR TAB CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 RIGHT ELEVATOR TAB HAS 3 BOB WEIGHTS CRACKED. REPLACED 3 BOB WEIGHTS AND BALANCED TAB IAW SRM 51-00-09. INSTALLED RIGHT ELEVATOR TAB IAW MM 27-30-11, RIG AND OPS CHECK IAW MM 27-30-0. (M) 2L73 4F A3WE 19951208006801995120800680NM 1995 12 8 EISA95401 119951010A5330 SKIN BOEING727 72725 1384006NM BS 1157-1183 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 CORROSION FOUND LAP STATION 1157 TO 1183 STRINGER 20L. REMOVED CORROSION AND REPAIRED PER AAL EO 1280-011 REV A. (M) 2L73 4F A3WE 19951208006811995120800681NM 1995 12 8 EISA95402 119950913A273065C337351 BOB WEIGHTS BOEING727 72725 1384006NM LT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 LEFT ELEVATOR TAB HAS 3 BOB WEIGHTS CRACKED. REMOVED AND REPLACED BOB WEIGHTS AND BALANCED TAB IAW SRM 51-80-9 INSTALLED LEFT ELEVATOR TAB IAW MM 27-30-11, RIG AND OPS CHECK IAW 27-30-0. (M) 2L73 4F A3WE 19951208006821995120800682NM 1995 12 8 EISA95403 119951006A532065956002595 FITTING BOEING727 72725 1384006NM BS 1183 MISDRILLED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 FUSELAGE BS 1183, STRINGER 201 LOWER BATHTUB FITTING HAS DRILL STARTS. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-10-1 TORQUED BOLTS IAW 51-30-4. (M) 2L73 4F A3WE 19951208006831995120800683NM 1995 12 8 EISA95404 119950929A5330 SKIN BOEING727 72725 1384006NM BS 441 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 CORROSION FOUND STRINGER 19L EXCEEDING 10 PERCENT AT BS 441. REMOVED CORROSION REPAIRED PER AAC EO 1280-0009. (M) 2L73 4F A3WE 19951208006841995120800684NM 1995 12 8 EISA95405 119950913A5330 SKIN BOEING727 72725 1384006NM BS 482-740 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 FUSELAGE LAP JOINT AT STRINGER 4R HAS MATERIAL LOSS IN EXCESS OF 10 PERCENT FROM BS 482-740 IN AREAS THAT WERE NOT PREVIOUSLY TERMINATED WITH REPAIRS. REPAIRED AND INSTALLED DOUBLER IAW SRM 53-30-3. (M) 2L73 4F A3WE 19951208006851995120800685NM 1995 12 8 EISA95406 119951004A5280 SKIN BOEING727 72725 1384006NM RT MLG DOOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 RIGHT MLG STRUT DOOR AFT HINGE SKIN MISSING SEVERAL FASTENERS AND THE SKIN IS CRACKED. REMOVED DAMAGE AND REPAIRED PER SRM 52-80-2. (M) 2L73 4F A3WE 19951208006861995120800686NM 1995 12 8 EISA95407 119951002A5330 SKIN BOEING727 72725 1384006NM BS 1080 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 AN .75 INCH CRACK INDICATION, STRINGER 3L BS 1080. HFEL CONFIRMED CRACK LOCATED STRINGER 4L STATION 1072. REPAIRED PER SRM 53-30-3 AND SB 727-53-0072 AND AD 91-06-06. (M) 2L73 4F A3WE 19951208006871995120800687NM 1995 12 8 EISA95408 119950914A5730 PANEL BOEING727 72725 1384006NM RT WING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 RIGHT WING LOWER ACCESS PANEL JUST FORWARD AND INBOARD OF VENT SCOOP HAS A 4 INCH CRACK. FABRICATED NEW PANEL IAW SRM 51-30-8 AND 51-10-1 INSTALLED PANEL IAW SRM 51-30-2. (M) 2L73 4F A3WE 19951208006881995120800688NM 1995 12 8 EISA95409 119950918A5330 SKIN BOEING727 72725 1384006NM BS 360-380 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 FUSE EXT BS 360-380 STRINGERS 17L-19L SKIN HAS PILLOWING. REMOVED CORROSION IAW 51-10-6. INSTALLED DOUBLER IAW SRM 51-30-2. (M) 2L73 4F A3WE 19951208006891995120800689NM 1995 12 8 EISA95410 119950928A5330 SKIN BOEING727 72725 1384006NM BS 640 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 BS 640 STRINGER 22L UPPER FLANGE, HAS AN OPEN HOLE ADJACENT FASTENER HOLE. REPAIRED PER SRM 53-10-3 FIG 2. (M) 2L73 4F A3WE 19951208006901995120800690NM 1995 12 8 EISA95411 119950930A5330 SKIN BOEING727 72725 1384006NM BS 660 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 BS 660 STRINGER 22L UPPER FLANGE HAS A HOLE. REPAIRED PER SRM 53-10-3 FIG 2. (M) 2L73 4F A3WE 19951208006911995120800691NM 1995 12 8 EISA95412 119950929A5230AE727104313 SKIN BOEING727 72725 1384006NM CARGO DOOR DEFECTIVE A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 REPLACED INNER STRUCTURE,16 FEET LONG (P/N AE 727-1-043-13). REMOVED AND REPLACED STRUCTURE PER SRM 51-10-1 AND SRM 51-30-2. (M) 2L73 4F A3WE 19951208006921995120800692NM 1995 12 8 EISA95413 119950929A2611 SENSING TUBE BOEING727 72725 1384006NM SMOKE DETECTOR BENT A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 CABIN SMOKE DETECTION SENSING TUBE IS BENT AT STATION 680 RIGHT. REMOVED DAMAGED REPOSITION TUBING PER MM 20-10-5 AND MM26-17-0 FIG 1. (M) 2L73 4F A3WE 19951208006931995120800693NM 1995 12 8 EISA95414 119950926A5330 SKIN BOEING727 72725 1384006NM BS 560 OPEN HOLES A EISAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07290NE 18972 BS 560 STRINGER 21L UPPER AND LOWER FLANGES, HAVE OPEN HOLES ADJACENT TO FASTENER HOLES. REPAIRED IAW SRM 53-10-3 FIG 2. (M) 2L73 4F A3WE 19951208006941995120800694NM 1995 12 8 EISA95415 119950926A2611 SENSING TUBE BOEING727 72725 1384006NM SMOKE DETECTOR BENT A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 SMOKE DETECTION SENSING TUBE BEN RIGHT SIDE COMP 2. REMOVED DAMAGES SECTION OF TUBING PER MM 20-10-5 REPOSITIONED PER ANI CARGO DOOR MANUAL PG 17 FIG 6. (M) 2L73 4F A3WE 19951208006951995120800695NM 1995 12 8 EISA95416 119950908A5330 SKIN BOEING727 72725 1384006NM BS 380 DENTED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 FUSELAGE SKIN, AT STATION 380 STRINGER 18LT, HAS DENTS OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLERS IAW SRM 53-30-3 FIG 3. (M) 2L73 4F A3WE 19951208006961995120800696NM 1995 12 8 EISA95418 119951003A5330 SKIN BOEING727 72725 1384006NM BS 530 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 TWO CRACKS UPPER SKIN LAP AT STATION 520 CENTER ROW AND STATION 530 BOTTOM ROW OF STRINGER 19L. FAB DOUBLER PER EO 1280-008. (M) 2L73 4F A3WE 19951208006971995120800697NM 1995 12 8 EISA95419 119951008A5330 SKIN BOEING727 72725 1384006NM BS 1183 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 BS 1183 STRINGER 19L END FITTING HAS SEVERAL DRILL STARTS AND BROKEN SCREWS. REMOVED FITTING AND INSTALLED NEW PER SRM 51-10-2 AND SRM 51-30-4 AND SRM 51-10-1. (M) 2L73 4F A3WE 19951208006981995120800698NM 1995 12 8 EISA95420 119950908A5312 BLKHD SKIN BOEING727 72725 1384006NM BS 1183 CRACK A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 LOWER LOBE INTERIOR 1.5 INCH CRACK IN VERTICAL STRAP AT RBL 46, BULKHEAD 1183 OUTBOARD SIDE. FABRICATED ANGLE AND FILLER IAW SRM 51-40-4 FIG 1 AND SRM 51-30-2. (M) 2L73 4F A3WE 19951208006991995120800699NM 1995 12 8 EISA95421 119951005A5330 SKIN BOEING727 72725 1384006NM BS 259-360 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07290NE 18972 SKIN LAP JOINT, AT STRINGER BS 259-360, HAS 9 SINK HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE PER SRM 53-30-3 FIG 5. COMPLETED REPAIR PER SB 53-0072 REV 5 AND SRM 53-30-3. (M) 2L73 4F A3WE 19951208007001995120800700NM 1995 12 8 EISA95422 119951102A3260 DOOR LIGHT BOEING727 72731 1384010NM RT MLG ILLUMINATED A EISAO OTHER N FALSE WARNING TOTAKEOFF 1 SW07240NE 18906 DURING TAKEOFF AT DAL, RIGHT MAIN GEAR DOOR UNSAFE INDICATION AFTER GEAR RETRACTED. REMOVED APU SLING BRACKETS FROM RIGHT WHEEL WELL. INSPECTED AREA FOR DAMAGE. PERFORMED GEAR RETRACTION AND EXTENSION CHECK PER MM 32-40-00. OPS CHECK GOOD. (M) 2L73 4F A3WE 19951208007011995120800701EA 1995 12 8 HERA9516 219950715A7200 ENGINE DHAV DHC6 DHC6300 EA PWA PT6 PT6A34 52043EA NR 2 FAILED A HERAEA ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 AL03442CA16117 290 PCE56816 FLT NR 1107 - EN ROUTE TO ENA, NR 2 ENGINE SEIZED DUE INTERNAL FAILURE. THE FLIGHT CREW SECURED THE ENGINE AND MADE AN UNEVENTFUL LANDING AT ENA. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND PROPELLER DUE METAL CONTAMINATION THROUGHOUT THE OIL SYSTEM. THE AIRCRAFT WAS THEN RELEASED FOR FLIGHT. (M) 1H72 3T4 T A9EA E4EA 19951208007021995120800702CE 1995 12 8 HERA9519 119950912A3230MS24171D1 RELAY BEECH 1900 1900C 1154161CE LANDING GEAR ERRODED A HERAO OTHER J WARNING INDICATION DEDESCENT 1 AL0355635 UC161 FLT NR 1481 - ON APPROACH TO LANDING AT ANC, THE LANDING GEAR HANDLE WAS SELECTED TO THE DOWN POSITION BUT DID NOT GET ANY LIGHTS INDICATING THE GEAR WAS DOWN AND LOCKED. THE EMERGENCY EXTENSION HAND PUMP WAS PUMPED BUT THERE WAS NO INDICATION OF PRESSURE, BUT AFTER ABOUT 10 SECONDS THE THREE GREEN DOWN LIGHTS ILLUMINATED. THE AIRCRFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR MOTOR RELAY CONTACTS AND FOUND THEM TO BE ERRODED. THE RELAY WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19951208007031995120800703CE 1995 12 8 HERA9520 119950913A32601148200773 BRACKET BEECH 1900 1900C 1154161CE NLG BENT A HERAO OTHER N FALSE WARNING DEDESCENT 1 AL0380598 UC99 FLT NR 1122 - ON LANDING AT ANC, WHEN THE LANDING GEAR WAS EXTENDED, THE NOSE GEAR FAILED TO GET A SAFE INDICATION (GREEN LIGHT). THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED AND THE WARNING HORN REMAINED SOUNDING UNTIL THE NOSEWHEEL TOUCHED DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SWITCH ADJUSTABLE STOP SUPPORT BRACKET BENT. THE BRACKET WAS STRAIGHTENED AND THE DOWN LOCK SWITCH ADJUSTED IAW THE BEECHCRAFT MAINTENANCE MANUAL. RETRACTION AND EXTENSION TESTS WERE ACCOMPLISHED SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19951208007041995120800704CE 1995 12 8 HERA9521 119950917A3260R100381001 DOWNLOCK SWITCH BEECH 1900 1900C 1154161CE NLG OUT OF ADJUST A HERAO OTHER N FALSE WARNING DEDESCENT 1 AL0380346 UC94 FLT NR 1125 - ON LANDING GEAR EXTENSION COULD NOT GET A SAFE NOSE GEAR INDICATION, (GREEN LIGHT). AIRCRAFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR DOWNLOCK SWITCH AND AFTER NUMEROUS TESTS RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA24CE 19951208007051995120800705CE 1995 12 8 HERA9522 119950925A3230 CIRCUIT CARD BEECH 1900 1900C 1154161CE LANDING GEAR DIRTY A HERAL ABORTED APPROACH J WARNING INDICATION DEDESCENT 1 AL0355635 UC161 FLT NR 1426 - LANDING GEAR WOULD NOT COME DOWN WHEN SELECTED. THE GEAR WAS RECYCLED BUT HAD NO EFFECT. AFTER GOING AROUND AND RIGHT BEFORE STARTING THE MANUAL GEAR EXTENSION CHECKLIST THE LANDING GEAR CAME DOWN. THE GEAR WAS CHECKED VISUALLY AND THE LANDING WAS NORMAL AND WITHOUT INCIDENT. MAINTENANCE CLEANED THE LANDING GEAR TIME DELAY RELAY CIRCUIT CARD. GEAR RETRACTION AND EXTENSION WAS NORMAL AND THE AIRCRAFT RELEASED TO SERVICE. (M) 2L72 4T RTA24CE 19951208007061995120800706CE 1995 12 8 HERA9523 119951009A2140 HEATER SHROUD CESSNA207 207A 2073604CE MUFFLER OILY A HERAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 AL0373733 20700618 FLT NR 1527 -ORV-OTZ - PILOT DETECTED SMOKE COMING FROM UNDER INSTRUMENT PANEL AND THOUGHT IT SMELLED LIKE AND ELECTRICAL SHORT. A LANDING WAS MADE AT OTZ WITHOUT INCIDENT. MX INSPECTED THE ELECTRICAL SYSTEM FOR SHORTS OR BURNED WIRING, BUT NO DEFECTS WERE NOTED. THE SMOKE WAS DETERMINED COMING INTO THE COCKPIT, DUE TO OIL SPILLED ON THE MUFFLER HEAT SHROUD AND ENTERING VIA THE RAM AIR INLET. THE OIL WAS CLEANED FROM THE HEAT SHROUD AND A RUNUP WAS PERFORMED WITH NO SMOKE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR FLIGHT. (M) 1H71 3O A16CE 19951208007071995120800707EA 1995 12 8 HERA9524 219951016A73103040637 FUEL LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA NR 1 ENGINE LEAKING A HERACD ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TOTAKEOFF 1 AL0380598 UC99 PCE32498 FLT NR 1451 - ANC - ON TAKEOFF, THE NR 1 ENGINE INDICATED 1000 LBS OF TORQUE AT 84 PERCENT NI. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND FUEL LINE, P/N 3040637, LEAKING DUE TO THE GENERATOR BLAST TUBE HAD CHAFFED A HOLE IN IT. THE FUEL LINE WAS REPLACED AND AFTER LEAK CHECK RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T4 TRTA24CE E4EA 19951208007081995120800708EU 1995 12 8 RAIA951036 119951025A3222109A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NLG REQ'D SERVICE A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03972JX 972 SMF - FLT 4717 - NOSE GEAR SQUAT SWITCH FAILED TO ENGAGE. MAINTENANCE SERVICED NOSE STRUT, GEAR SWING AND OPERATIONAL CHECKS GOOD. (M) 2L72 4T RTA56EU 19951208007091995120800709WP 1995 12 8 RAIA951037 219951026A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE LEAKING A RAIAA UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CLCLIMB 1 CE03433AM8976 885 66146 FLT NR 7431 - CMI - RIGHT ENGINE BETA LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED ENGINE BLEED AIR GASKETS. INSPECTED BETA SWITCH AND GROUND RAN AIRCRAFT, CHECKS GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19951208007101995120800710NE 1995 12 8 RAIA951038 219951027A732131059005 FUEL CONTROL JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03553HK894 41066 76083 STL - FLT 7472 - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE ADJUSTED MAX FUEL FLOW, GROUND RUNS CHECK GOOD. (M) 2L72 4T4 TRTA41NM E18NE 19951208007111995120800711 1995 12 8 RAIA951039 319951030A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAULTY A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03343TE10402 955 STL - FLT 7494 - RIGHT BETA WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED RIGHT BETA SWITCH PERFORMED GROUND RUNS, OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007121995120800712EU 1995 12 8 RAIA951040 119951030A5270 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR ILLUMINATED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03554HK 41067 GRR - FLT 7519 - CARGO DOOR LIGHT ILLUMINATED. MAINTENANCE DEFFERED CARGO DOOR WARNING SYSTEM PER MEL 52-3. (M) 2L72 4T RTA41NM 19951208007131995120800713EU 1995 12 8 RAIA951041 119951031A77128972605 PRESS TRANSDUCER BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER O OTHER TOTAKEOFF 1 CE03341TE9341 6301 950 STL - FLT NR 7444 - LEFT EGT FLUX ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED DELTA P/P PRESSURE TRANSDUCER. PERFORMED GROUND RUNS, OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007141995120800714 1995 12 8 RAIA951043 419951101A34546226137001 NAV RECIEVER BAG JETSTMJETSTM3201 1500217EU AVIONICS BAY FAILED A RAIAD RETURN TO BLOCK O OTHER CLCLIMB 1 CE03343TE 955 STL - FLT NR 7316 - UNABLE TO RECEIVE COURSE INDICATION ON NR 1 AND NR 2 NAVS AFTER TAKEOFF. NR 2 EVENTUALLY RECEIVED HEADING INFORMATION. MAINTENANCE RERACKED NR 1 AND NR 2 NAV RECEIVERS. OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007151995120800715EU 1995 12 8 RAIA951044 119951103A3222B00A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NLG REQ'D SERVICE A RAIAA UNSCHED LANDING O OTHER CLCLIMB 1 CE03431AM9899 881 STL - FLT 7438 - AFTER TAKEOFF, UNABLE TO RAISE GEAR, HYDRAULIC PRESSURE NORMAL. GEAR HANDLE WOULD NOT MOVE. MAINTENANCE SERVICED NOSE STRUT, PERFORMED GEAR SWING. OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007161995120800716EU 1995 12 8 RAIA951045 119951104A2420SM400D30 CONTACTOR AEROSPATR42 ATR42300 8680920EU NR 2 BUS FAILED A RAIAD RETURN TO BLOCK H ELECT. POWER LOSS-50 PC CLCLIMB 1 CE03421TE16251 102 STL - FLT 7176 - DC BUS NR 2 FAULTED. MAINTENANCE REMOVED AND REPLACED CONTACTOR 12PU. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007171995120800717 1995 12 8 RAIA951046 319951106A61408659566 SWITCH BAG JETSTMJETSTM3201 1500217EU LT ENG FAILED A RAIAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 CE03340TE6267 939 STL - FLT 7094 - LEFT BETA LIGHT CAME ON. MAINTENANCE REMOVED AND REPLACED LEFT BETA SWITCH. GROUND RUNS, OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007181995120800718EU 1995 12 8 RAIA951101 119951105A21302758A000 PRESSURE SWITCH BAG JETSTMJETSTM3201 1500217EU LT CABIN DUCT FAILED A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03871JX9321 871 LAX - FLT NR 4761 - LEFT AIR OFF CAPTION ILLUMINATED IN FLIGHT, UNABLE TO RESET. MAINTENANCE REMOVED AND REPLACED LEFT OVER PRESSURE SWITCH. OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007191995120800719EU 1995 12 8 RAIA951102 119951105A33506047051 EEL POWER SUPPLY JETAIRJETSTMJETSTM4101 1500501EU CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03554HK1053 41067 STL - FLT 7326 - APPROXIMATELY 6 EMERGENCY LIGHTS IN CABIN INOP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA41NM 19951208007201995120800720EU 1995 12 8 RAIA951103 119951107A5311S53674406200 FRAME AEROSPATR42 ATR42300 8680920EU FRAME 39 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE10625 228 STL - DURING CYCLE 6 PHASE 6 INSPECTION, FOUND RIGHT SIDE OF FRAME 39 CORRODED NEAR FLOOR BEAM BETWEEN STRINGERS 14 AND 16. MAINTENANCE TREATED CORRODED AREA PER ATR SRM 51-21-42. (M) 2H72 4T RTA53EU 19951208007211995120800721EU 1995 12 8 RAIA951104 119951107A5315S53189533202 FLOOR BEAM AEROSPATR42 ATR42300 8680920EU FUSELAGE CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE10627 228 STL - FLOOR BEAMS AT FRAMES 36, 37, 38, 39 AND 40 HAVE SURFACE CORROSION AT THE NUTPLATE HOLES. MAINTENANCE TREATED CORROSION ON FLOOR BEAMS 36, 37, 39 AND 40 PER ATR SRM 51-21-42, AND REPAIRED FLOOR BEAM AT FRAME 38 PER ATR SRM 53-61-0. (M) 2H72 4T RTA53EU 19951208007221995120800722EU 1995 12 8 RAIA951105 119951107A5347S53678001236 SEAT TRACK AEROSPATR42 ATR42300 8680920EU FUSELAGE CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE10627 228 STL - BOTH SEAT TRACKS BETWEEN FRAMES 36 AND 39 ARE CORRODED AND NEED REPLACED. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS BETWEEN FRAMES 36 AND 39 PER ATR SRM 53-00-00. (M) 2H72 4T RTA53EU 19951208007231995120800723EU 1995 12 8 RAIA951106 119951107A5311S53672406200 FRAME AEROSPATR42 ATR42300 8680920EU FRAME 36 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE10627 228 STL - FRAME 36 RIGHT SIDE BETWEEN STRINGERS 14 AND 16 HAS SURFACE CORROSION. MAINTENANCE TREATED AREA PER ATR SRM 51-21-42. (M) 2H72 4T RTA53EU 19951208007241995120800724EU 1995 12 8 RAIA951107 119951107A5311S53672406200 FRAME AEROSPATR42 ATR42300 8680920EU FRAME 37 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE 228 STL - FRAME 37 RIGHT SIDE BETWEEN STRINGERS 14 AND 16 HAS CORROSION. MAINTENANCE REPAIRED FRAME 37 PER ATR SRM 53-67-70 AND REPAIR DRAWING N16S536R0054. (M) 2H72 4T RTA53EU 19951208007251995120800725EU 1995 12 8 RAIA951108 119951107A5311S536724082 FRAME AEROSPATR42 ATR42300 8680920EU FRAME 39 CORROSION A RAIAK NONE O OTHER ININSP/MAINT 1 CE03426TE10627 228 STL - FRAME 39 CORRODED BETWEEN STRINGERS 21L AND 21R. MAINTENANCE REPAIRED FRAME 39 PER ATR SRM CHAPTER 51. (M) 2H72 4T RTA53EU 19951208007261995120800726EU 1995 12 8 RAIA951109 119951110A302031P172321 DE-ICE BOOT AEROSPATR72 ATR72202 8680940EU NR 2 ENG INLET LOOSE A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03722TE9363 220 STL - FLT 7130 - NR 2 ENGINE DE-ICE FAULT. MAINTENANCE REPAIRED HOSE ON THROAT DE-ICE BOOT, OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007271995120800727EU 1995 12 8 RAIA951110 119951110A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE ERRATIC A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03436AM1047810478 891 FLT 7060 - JLN - RIGHT ENGINE WENT DOWN TO 50 PERCENT TORQUE ON TAKEOFF ROLL. MAINTENANCE DETERMINED IT TO BE AN INDICATION PROBLEM. AIRCRAFT FERRIED BACK TO STL TTL OFF WITHOUT INCIDENT. MAINTENANCE THEN REMOVED AND REPLACED NR 2 SIGNAL CONDITIONER. OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007281995120800728EU 1995 12 8 RAIA951111 119951110A772221186009 SRL COMPUTER BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER O OTHER CLCLIMB 1 CE03436AM9433 891 FLT 7482 - STL - AT 1000 FEET AGL, BOTH ENGINES TQ 98 PERCENT, EGT 630, RIGHT ENGINE WENT ABOVE REDLINE AND STARTED BYPASSING. PULLED BOTH P/L TO 90 PERCENT. LEFT ENGINE STARTED TO BYPASS, TURNED SRL'S OFF. LT STABILIZED, RT ENG TQ FLUCTUATES PLUS OR MINUS 8 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 SRL COMP. OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007291995120800729EU 1995 12 8 RAIA951112 119951110A772221186009 SRL COMPUTER BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIAO OTHER O OTHER CLCLIMB 1 CE03436AM9805 891 FLT 7482 - STL - AT 1000 FEET AGL, BOTH ENGINES TQ 98 PERCENT, EGT 630, RIGHT ENGINE WENT ABOVE REDLINE AND STARTED BYPASSING. PULLED BOTH P/L TO 90 PERCENT. LEFT ENGINE STARTED TO BYPASS, TURNED SRL'S OFF. LT STABILIZED, RT ENG TQ FLUCTUATES PLUS OR MINUS 8 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 SRL COMP. OPS CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007301995120800730 1995 12 8 RAIA951113 419951110A3442MI5853505 TRANSCEIVER AEROSPATR72 ATR72202 8680940EU RADAR FAILED A RAIAO OTHER O OTHER CLCLIMB 1 CE03723TE10875 283 FLT 7164 - STL - RADAR SPOKING AND UNUSABLE. MAINTENANCE REMOVED AND REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007311995120800731EU 1995 12 8 RAIA951114 119951112A5610NA1588012 WINDSCREEN AEROSPATR42 ATR42300 8680920EU LT COCKPIT SHATTERED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03425TE14917 125 FLT 7405 - FYV - FIRST OFFICERS WINDSCREEN OUTER PANE SHATTERED. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDSCREEN. (M) 2H72 4T RTA53EU 19951208007321995120800732EU 1995 12 8 RAIA951115 119951112A5210S5367129039002 SEAL AEROSPATR42 ATR42300 8680920EU PAX DOOR DIRTY A RAIAO OTHER O OTHER CLCLIMB 1 CE03426TE10634 228 FLT NR 7389 - STL - MAIN CABIN DOOR MAKING LOUD WHISTLING NOISE DURING FLIGHT. MAINTENANCE CLEANED DOOR SEAL. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007331995120800733EU 1995 12 8 RAIA951116 119951113A3230DHE1148 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG DIRTY A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03428AM10154 877 FLT NR 7364 - STL - DURING TAKEOFF, SQUAT SWITCH STUCK AND COULD NOT GET THE GEAR TO RETRACT AND OIL COOLER DOOR DOES NOT CLOSE. MAINTENANCE CLEANED NOSE GEAR SQUAT SWITCH, OPERATIONAL CHECK GOOD. (M) 2L72 4T RTA56EU 19951208007341995120800734EU 1995 12 8 RAIA951117 119951112A215032149602 PACK VALVE AEROSPATR72 ATR72202 8680940EU RIGHT FAILED A RAIAO OTHER JB WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03721TE9136 217 FLT NR 7003 - STL - SMOKE IN COCKPIT 'ELECTRICAL' ACTIVATED ON CCAS. MAINTENANCE DEFERRED RIGHT PACK VALVE. MAINTENANCE CLEARED DMI, REMOVED AND REPLACED RIGHT PACK VALVE. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007351995120800735EU 1995 12 8 RAIA951118 119951112A2121E0039R10T5SNE CONNECTOR AEROSPATR72 ATR72202 8680940EU LT TURBO FAN LOOSE A RAIAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CE03721TE9633 217 FLT NR 7166 - STL - DURING TAXI, CABIN FILLED UP WITH SMOKE, RETURNED TO THE GATE. MAINTENANCE RESECURED PIN ON CANNON PLUG OF THE LEFT TURBO FAN PRESSURE SWITCH AND REROUTED WATER EXTRACTOR DRAIN HOSE. OPERATIONAL CHECK GOOD. (M) 2H72 4T RTA53EU 19951208007361995120800736WP 1995 12 8 RAIA951119 219951114A7530137115436401 BLEED LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE CRACKED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03428AM10161 877 66178 FLT NR 7409 - EVV - LEFT ENGINE TEMP SPIKED TO 700. MAINTENANCE REMOVED AND REPLACED P3 BLEED LINE, OPERATIONAL CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19951208007371995120800737WP 1995 12 8 RAIA951120 219951115A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE LEAKING A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03428AM8318 877 66188 FLT NR 7310 - STL - RIGHT ENGINE ONLY MADE 90 PERCENT TORQUE, TARGET TORQUE 100 PERCENT. MAINTENANCE REMOVED AND REPLACED P3 BLEED GASKETS. OPERATIONAL CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19951208007381995120800738 1995 12 8 RAIA951121 419951115A34207003110901 CRT JETAIRJETSTMJETSTM4101 1500501EU COCKPIT FAILED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03555HK508 41072 JFK - FLT 7759 - IN FLIGHT RADIO MANAGEMENT UNIT FAULTED. REPLACED CRT UNIT. (M) 2L72 4T RTA41NM 19951208007391995120800739WP 1995 12 8 USAA951159 119951106A5220 PAN DOUG DC9 DC982 3022082WP RT EMER EXIT CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND 1 INCH CRACK IN FORWARD RIGHT OVERWING EXIT DOOR PAN UPPER AFT DOOR STOP. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 52-20-03. (M) 2L72 4F A6WE 19951208007401995120800740WP 1995 12 8 USAA951160 119951106A53209915561533 WEB DOUG DC9 DC982 3022082WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION ON WEB OF AFT CARGO WALL AT STATION 1338 PREVIOUSLY REWORKED CORROSION REF NR C57-53300. MANUFACTURED AND SPLICED IN NEW WEB SECTION AND ANGLES PER USAIR TYPICAL REPAIR 53-30-10. (M) 2L72 4F A6WE 19951208007411995120800741NM 1995 12 8 USAA951190 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 TO 2 INCH DIAMETER SPOTS OF CORROSION ON THE FLOOR BEAM AT SCREW HOLES, BS 986 LBL 45 TO RBL 45. CUT OFF 'T' CAP AND INSTALLED NEW 'T' CAP AND REPAIR ANGLE. REPAIRED PER EA 40072A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951208007421995120800742NM 1995 12 8 USAA951191 119951103A5320654795711 STRAP BOEING737 737401 1384701NM BS 800-840 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 40 INCH CORROSION ON STRAP, STATION 800 TO 840. INSTALLED NEW PART, REPAIRED PER SRM 51-10-02, DRAWING 65-47957. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951208007431995120800743NM 1995 12 8 USAA951192 119951103A5240 HINGE BOEING737 737401 1384701NM BS 328 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCH CRACK AT HINGE LUGS, BS 328 FORWARD SERVICE DOOR LOWER GATE. REPLACED HINGE ASSEMBLY. REPAIRED PER SRM 51-10-2 AND MM 52-41-00. (M) 2L72 4F RTA16WE 19951208007441995120800744NM 1995 12 8 USAA951194 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 1.50 INCH CORRODED AREA, BS 967, RBL 45 ON FLOOR BEAM. INSTALLED NEW T-CAP AND REPAIR ANGLES, REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19951208007451995120800745NM 1995 12 8 USAA951195 119951023A5414 SKIN BOEING757 757225 1384959NM NR 2 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU34453 22204 CLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO 5492R274 PART IV STEPS 2 AND 3, ON NR 2 PYLON. REPAIRED SKIN PER DRAWING 013N8774. (M) 2L72 4F RTA2NM 19951208007461995120800746NM 1995 12 8 USAASB95009 119951104A32302670064409 CHECK VALVE BOEING737 7373B7 1384580NM LT MLG CLOGGED A USAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA19532AU22500 24479 CLT - FLT 2722 - ON APPROACH TO CLT, LEFT MAIN GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. DURING GO-AROUND, TOWER OBSERVED LEFT MAIN GEAR EXTEND ALONG WITH FLIGHT CREW GETTING GREEN INDICATION. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RESTRICTOR CHECK VALVE TO DOWN SIDE OF UPLOCK PLUGGED. REPLACED RESTRICTOR CHECK VALVE. GEAR OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19951208007471995120800747NM 1995 12 8 USAASB95012 119951108A2820 FUEL BOEING737 7373B7 1384580NM AFT GALLEY ODOR A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19505AU29259 23380 CLT - FLT 1276 - EN ROUTE MIA TO PHL, FLIGHT CREW NOTED A FAINT ODOR, POSSIBLY FUEL IN THE AFT GALLEY. FLIGHT MADE A PRECAUTIONARY LANDING IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT FUEL SYSTEM. PRESSURIZED AIRCRAFT, COULD NOT DUPLICATE. (M) 2L72 4F RTA16WE 19951215000011995121500001WP 1995 12 15 9519689613 119951124A56105912290505 WINDSHIELD DOUG DC9 DC932 3022066WP LT COCKPIT CRACKED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01613NW38 38 47438 DURING CLIMB, GDC-MSP AT 3000 FEET, THE LEFT WINDSHIELD HEAT SYSTEM BEGAN ARCING. THE SYSTEM WAS SHUT OFF AT WHICH TIME THE WINDSHIELD CRACKED. THE AIRCRAFT RETURNED TO GDC WITHOUT FURTHER INCIDENT. REPLACED THE WINDSHIELD AND HEAT CONTROLLER. 2L72 4F A6WE 19951215000021995121500002WP 1995 12 15 9519699970 119951206A3350 BATTERY PACK DOUG DC9 DC931 3022065WP AFT AIRSTAIR DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019334 47247 DURING LINE CHECK, FOUND TAIL AIRSTAIR EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215000031995121500003WP 1995 12 15 9519709970 119951206A3350 BATTERY PACK DOUG DC9 DC931 3022065WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019334 47247 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215000041995121500004WP 1995 12 15 9519719920 119951206A3350 EEL CONNECTOR DOUG DC9 DC932 3022066WP CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01942N 47459 DURING LINE CHECK, FOUND LEFT EMERGENCY FLOOR LIGHTS, ROWS 1-4, INOPERATIVE. REPAIRED ELECTRICAL CONNECTOR ON SERVICE DOOR EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215000051995121500005WP 1995 12 15 9519729903 119951206A3231 LATCH MECH DOUG DC9 DC932 3022066WP MLG DOORS OUT OF ADJUST A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01603NW 47101 DURING CLIMB OF TEST FLIGHT (GDC), THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND THE LEFT AND RIGHT UNSAFE LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUSTED BOTH THE LEFT AND RIGHT MAIN LANDING GEAR DOOR LATCH MECHANISMS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215000061995121500006WP 1995 12 15 9519739861 119951205A3230 SPRING ROD DOUG DC9 DC951 3022051WP NLG FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01770NC 47758 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE NOSE WHEEL STEERING WAS OPERATIONAL AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND SPRING ROD TO GROUND SHIFT MECHANISM HAD FAILED. REPLACED THE SPRING ROD. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951215000071995121500007WP 1995 12 15 9519749867 119951206A3230 RETRACT MECH DOUG DC9 DC951 3022051WP LANDING GEAR MALFUNCTIONED A NWAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 GL01776NC 47786 LANDING GEAR WOULD NOT EXTEND ON APPROACH INTO DTW. LOWERED GEAR BY UTILIZING EMERGENCY EXTENSION PROCEDURES. EXECUTED GO-AROUND AND ACCOMPLISHED SUCCESSFUL LANDING ON SECOND ATTEMPT. FOUND DAMAGE TO THE LEFT MAIN GEAR DOOR LEADING EDGE AND DOOR SKID PLATES. REPAIRED DAMAGE PER SRM 52-01 AND 51-50, REPLACED DOOR SKID PLATES. INSPECTED GEAR HANDLE AND CLEANED. CHECKED NOSE GEAR GROUND SHIFT MECHANISM AND LUBED. INSPECTED LANDING GEAR CONTROL VALVE, PULLEYS, AND CABLES. ALL SYSTEMS CHECKED NORMAL AFTER NUMEROUS GEAR CYCLES. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951215000081995121500008WP 1995 12 15 9519759101 119951205A3350 BATTERY PACK DOUG DC9 DC915 3022036WP LT/RT NACELLES DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL0191S 47063 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH EMERGENCY NACELLE LIGHTS INOPERATIVE. REPLACED BOTH BATTERY PACKS. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951215000091995121500009NE 1995 12 15 9519761158 219951202A7320 PT2 PROBE DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 2 ENGINE CRACKED A NWAAE ENGINE SHUTDOWN M OVER TEMP DEDESCENT 1 GL01158US 46767 686131 DURING START OF DESCENT, THE NR 2 ENGINE EGT WENT TO 1010 DEGREES FOR 90 SECONDS. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO AN UNEVENTFUL TWO-ENGINE LANDING AT MSP. THE PRBC AND EVC WERE REPLACED AND A PT2 PROBE WAS FOUND CRACKED AND REPLACED. A GROUND RUN-UP AND TRIM WAS ACCOMPLISHED AND CONFIRMED PROPER ENGINE OPERATION. 2L73 4F4 F A22WE E20EA 19951215000101995121500010NE 1995 12 15 9519771150 219951204A7261 OIL FILTER DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20 52054NE NR 1 ENGINE DIRTY A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01150US 46759 686178 DURING APPLICATION OF TAKEOFF POWER, THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. THE OIL FILTER AND PRESSURE SWITCH WERE REPLACED. THE SYSTEM CHECKED OK DURING A GROUND RUN-UP. 2L73 4F4 F A22WE E20EA 19951215000111995121500011NE 1995 12 15 9519786638 219951205A7230 FAN BOEING747 747251B 1384892NM PWA JT9 JT9D7R4G2 52054NE NR 4 ENGINE SEIZED A NWAAAEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL EBYVIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS ENGINE STOPPAGE CRCRUISE 1 GL01638US 23549 715183 DURING CRUISE (TPE), THE NR 4 ENGINE EXPERIENCED COMPRESSOR STALLS FOLLOWED BY SMOKE IN THE CABIN AND THE ENTIRE AIRCRAFT SHAKING. THE NR 4 BLEED VALVE WAS CLOSED AND THE SMOKE STOPPED. THE NR 4 ENGINE WAS SHUT DOWN BUT THE AIRCRAFT CONTINUED TO VIBRATE AND THE NR 3 ENGINE INDICATIONS WERE FLUCTUATING. 127,000 POUNDS OF FUEL WAS DUMPED AND THE AIRCRAFT DIVERTED TO TPE WHERE AN UNEVENTFUL THREE-ENGINE LANDING WAS ACCOMPLISHED. THE NR 4 ENGINE FAN WAS FOUND TO BE SEIZED AND THE ENGINE WAS REPLACED. AN INSPECTION OF THE AIRFRAME, PYLONS, AND NR 3 ENGINE WAS ACCOMPLISHED AND CHECKED OK. A GROUND RUN-UP CONFIRMED PROPER OPERATION OF THE ENGINES. 2L74 4F4 F A20WE E3NE 19951215000121995121500012NM 1995 12 15 9519792296 119951207A3350 EEL POWER SUPPLY BOEING727 727251 138408HNM CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01296US 21788 DURING PRE-FLIGHT, FOUND EMERGENCY LIGHT ABOVE DOOR 1R INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES. CHECKED OK. 2L73 4F A3WE 19951215000131995121500013WP 1995 12 15 95FDEA01875 119951207A3234 GEAR HANDLE DOUG DC10 DC1010F 3022111WP LANDING GEAR LACK OF LUBE A FDEAO OTHER J WARNING INDICATION APAPPROACH 1 SO2568059 46907 RED GEAR LIGHTS REMAINED ILLUMINATED AFTER SELECTING GEAR DOWN AND GEAR SHOULD HAVE BEEN DOWN. RECYCLED, AND SAME THING HAPPENED, THEN GREEN LIGHTS SUDDENLY CAME ON. A/C LANDED MEM WITHOUT INCIDENT. MAINTENANCE FOUND GEAR HANDLE GUMMED UP. CLEANED GEAR HANDLE AND RELUBED, OPS CHECKED GOOD. OK FOR SERVICE. 2L73 4F A22WE 19951215000141995121500014NM 1995 12 15 95FDEA01876 119951207A3270 ACTUATOR BOEING727 7272D4 138407UNM TAIL SKID MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25287FE 21849 TAIL SKID EXTENDED LIGHT ILLUMINATED AFTER TAKEOFF, WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION. RECYCLED GEAR TO UP AND LIGHT EXTINGUISHED. RECYCLED TO OFF. HANDLE AND LIGHT ILLUMINATED AGAIN. CONTACTED GOCC AND GOT NEW FUEL NUMBERS. TAKEOFF PLUS 10 MINUTES. LIGHT OUT WHEN LANDING GEAR DOWN. TESTED TAIL SKID AS PER MM 32-71-01, PAGE 503. SKID LIGHT DOES COME ON WITH GEAR HANDLE IN OFF POSITION. REPLACED TAIL SIDE ACTUATOR PER MM 32-71-12. GROUND OPS CHECK GOOD. 2L73 4F A3WE 19951215000151995121500015NM 1995 12 15 95FDEA01877 119951207A5313 STRINGER BOEING727 727232 1384082NM BS 541 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION ON STR 27R AT BS 541. REPAIRED STR PER FEDEX SRM 53-10-3. 2L73 4F A3WE 19951215000161995121500016NM 1995 12 15 95FDEA01878 119951207A5311 FRAME BOEING727 727232 1384082NM BS 500 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 GOUGE ON FRAME BS 500 BETWEEN STR 13-14R. REPAIRED DAMAGED FRAME AT BS 500, STR 13-14R PER FEDEX SRM 53-10-4. 2L73 4F A3WE 19951215000171995121500017NM 1995 12 15 95UAL900294 119951206A25302TC1415 CIRCUIT BREAKER BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE GALLEY FAILED A UALAHF DEACTIVATE SYST/CIRCUITSACTIVATE FIRE EXT. A FLAME/FIRE UKUNKNOWN 1 WP294729U 19926 SMOKE, SPARKS AND FLAMES SEEN FROM COFFEE MAKER AT GALLEY 411. EXTINGUISHER USED AND CIRCUIT BREAKERS WERE PULLED. REPLACED FAILED CIRCUIT BREAKER AND ENTREE CART POWER CORD. CAUSE OF FAILURE NOT DETERMINED. POSSIBLE CAUSE: OVERCYCLING OF CIRCUIT BREAKER WHILE OPERATING IT AS ON-OFF SWITCH. 2L74 4F4 F A20WE E20EA 19951215000181995121500018EU 1995 12 15 95UAL900295 119951206A49904950242 OIL COOLER AIRBUS320 A320232 3930326EU APU LEAKING A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29410UA 463 EXPERIENCED STRONG ODOR AFTER TAKEOFF. ODOR WAS EVIDENT THROUGHOUT CABIN AND FLIGHT RETURNED TO BOSTON. THE SOURCE OF THE ODOR WAS AN OIL LEAK FROM THE APU OIL COOLER ASSEMBLY AT THE IN OIL LINE UNION. OIL COOLER WAS REPLACED AND OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA28NM 19951215000191995121500019NM 1995 12 15 95UAL900296 119951206A3350 EEL STRIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29301UA 23642 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROWS 19 AND 20. RERPLACED LIGHT STRIP. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951215000201995121500020NM 1995 12 15 95UAL900297 119951206A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297449U 21903 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE ROW 8. REPLACED EMERGENCY LIGHT ASSEMBLY. 2L73 4F4 F A3WE E2EA 19951215000211995121500021NM 1995 12 15 95UAL900298 119951206A3350 BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297461U 21915 EMERGENCY EXIT LIGHTING INOPERATIVE AT AFT FACE OF FORWARD DROP CEILING. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19951215000221995121500022NM 1995 12 15 95UAL900299 119951206A3350 BATTERY PACK BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29346UA 24250 EMERGENCY EXIT LIGHTS INOP IN AFT GALLEY AND DOOR TWO RIGHT. REPLACED BATTERY PACK. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951215000231995121500023NM 1995 12 15 95UAL900300 119951207A3350 BATTERY PACK BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297442U 21896 EMERGENCY LIGHT ON AISLE CEILING AT ROW 3C INOPERATIVE. REPLACED BATTERY PACK. 2L73 4F4 F A3WE E2EA 19951215000241995121500024EU 1995 12 15 95UAL900301 119951208A3350 EEL POWER SUPPLY AIRBUS320 A320232 3930326EU IAE V2500 V2527A5 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29412UA 465 AFT EMERGENCY LIGHTS OVER AFT DOORS ARE INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA28NM E40NE 19951215000251995121500025EU 1995 12 15 95UAL900302 119951208A5270E36000770 PROXIMITY SWITCH AIRBUS320 A320232 3930326EU CARGO DOOR DIRTY A UALAK NONE N FALSE WARNING CRCRUISE 1 WP29404UA 450 CREW REPORTED, THAT THE FORWARD CARGO DOOR LIGHT CAME ON INTERMITTENTLY IN CRUISE AND THEN WENT OUT. FOUND DOOR PROXIMITY SWITCH DIRTY, CLEANED AND OPERATIONALLY CHECKED NORMAL. 2L72 4F RTA28NM 19951215000261995121500026EU 1995 12 15 95UAL900303 119951208A24214004C66D14 IDG AIRBUS320 A320232 3930326EU NR 1 FAILED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29417UA 483 ABORTED TAKEOFF AT ORD BETWEEN 80 AND 100 KNOTS, DUE TO NR 1 IDG LOW OIL PRESSURE WARNING LIGHT. REPLACED NR 1 IDG. IDG WAS FOUND TO HAVE A FAILED LEFT HAND FIXED UNIT BEARING SET RUBBING AGAINST THE HOUSING. THE RUBBING GENERATED SUFFICIENT METAL TO PLUG THE FILTER AND CAUSE THE WARNING LIGHT TO COME ON. 2L72 4F RTA28NM 19951215000271995121500027NM 1995 12 15 95UAL900304 119951208A573065B0806012 SKIN BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE RT WING LE CRACKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29155UA 20104 ON ARRIVAL, FOUND RIGHT HAND WING LEADING EDGE CRACKED, LENGTH 11 INCHES. LOCATION IS APPROXIMATELY 19 INCHES OUTBOARD FROM FUSELAGE. CRACK WAS DETERMINED TO BE FATIGUE INDUCED. CRACK WAS REPAIRED PER 747SRM 57-30-04 AND S/B 57-2090. 2L74 4F4 F A20WE E20EA 19951215000281995121500028NM 1995 12 15 95UAL900305 119951208A3350 BULB BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29176UA 24383 FLOOR EMERGENCY ESCAPE LIGHTING INOP AT ROW 54 ON RIGHT AISLE. LAMP BURNED OUT. REPLACED BULB. 2L74 4F4 FRTA20WE E24NE 19951215000291995121500029NM 1995 12 15 95UAL900306 119951208A3350 POWER SUPPLY BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29180UA 25224 EMERGENCY EXIT SIGNS INOP OVEHEAD AT DOOR 1 RIGHT. ALSO, DOOR SILL LIGHT INOP. FOUND FAULTY POWER SUPPLY AND REPLACED POWER SUPPLY. 2L74 4F4 FRTA20WE E24NE 19951215000301995121500030NE 1995 12 15 95UAL900307 219951208A7321 EEC BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE ENGINE MALFUNCTIONED A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP29617UA 21877 707502 JFK - ABORTED TAKEOFF AT 100 KNOTS, DUE TO EEC PROBLEM. 2L72 4F4 FRTA1NM E3NE 19951215000311995121500031NM 1995 12 15 95UAL900308 119951208A261218252 FIRE SENSOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 ENGINE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297260U 21407 NR 3 ENGINE FIRE TEST INOPERATIVE IN ENGINE POSITION. FIRE WALL ON NR 3 TESTS NORMALLY. ENGINE FIRE SENSOR REPLACED. 2L73 4F4 F A3WE E2EA 19951215000321995121500032NM 1995 12 15 DL72E954633 119951206A5522 SKIN BOEING727 727247 138408FNM RT ELEVATOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27831WA 21483 RIGHT ELEVATOR LOWER INBOARD SKIN IS CRACKED 2.50 INCHES AFT OF PREVIOUS REPAIR. FOUND DURING D-1 LTR CK TPA MM. REPAIRED PER SRM 55-20-3. 2L73 4F A3WE 19951215000331995121500033NM 1995 12 15 DL72E954634 119951206A2780 ACT BRACKET BOEING727 727247 138408FNM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27831WA 21483 NR 6 L/E FLAP ACTUATOR BRACKET CRACKED OUTBOARD END. FOUND ON D-1 LTR CK TPA MM. REPAIRED PER 57-20-21. 2L73 4F A3WE 19951215000341995121500034NM 1995 12 15 DL72S954499 119951127A5754651622296 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27408DA 21152 DURING ROUTINE SHOP INSPECTION A CRACK WAS FOUND IN THE 16TH RIB AND A DOUBLER WAS INSTALLED USING MM 57-54-0 FOR NR 6 L/E SLAT. 2L73 4F A3WE 19951215000351995121500035NM 1995 12 15 DL72S954629 119951205A3350 BATTERY PACK 900835A BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27420DA 21273 BOTH AFT SERVICE DOOR EMERGENCY LIGHTS INOP C/A REPLACED BATTERY PACK M983. OPS CHKS GOOD. 2L73 4F A3WE 19951215000361995121500036NM 1995 12 15 DL72S954630 119951205A3350 BATTERY PACK 6104789 BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27420DA 21273 AFT EXIT EMERGENCY LIGHT INOP C/A REPLACED BATTERY PACK M1089. OPS CHKS GOOD. 2L73 4F A3WE 19951215000371995121500037NM 1995 12 15 DL72S954637 119951120A5720 STIFFENER BOEING727 727232 1384082NM RT WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 FOUND ON CV2 CHECK, 1 INCH CRACK IN LOWER END OF SPAR STIFFENER ON INBOARD SIDE NR 6 SLAT OUTBOARD TRACK. REPAIR: REPAIRED PER M/M 57-20-21, PG 813. 2L73 4F A3WE 19951215000381995121500038NM 1995 12 15 DL72W954635 119951205A5330 SKIN BOEING727 727247 138408FNM BS 580 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272822W 21327 LEFT FUSELAGE SKIN CRACKED TWO STRINGERS ABOVE THE 'E' IN 'DELTA', JUST FORWARD OF STA 580 AND UNDER STR 4. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLERS PER ERA 302855-14 ON NR 011. 2L73 4F A3WE 19951215000391995121500039NE 1995 12 15 DL73S954638 219951206A7260 GEARBOX STUDS 780650 BOEING737 737232 1384475NM PWA JT8 JT8D15A 52051NE NR 1 ENGINE PULLED LOOSE A DALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27322DL 23094 709226 LOW OIL QTY LIGHT ON - THEN LOW OIL PRESS LIGHT. ENGINE SHUT-DOWN. MTC SENT FROM ATL - REPLACED 2 STUDS FOUND PULLED LOOSE ON THE GEARBOX. HAD TO INSTALL HELICOIL. 2L72 4F4 FRTA16WE E2EA 19951215000401995121500040WP 1995 12 15 DLL10954631 119951206A3350 EEL POWER SUPPLY 5165741 LKHEED1011 10113851 5265010WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27718DA 54039 193C1097 L-2 DOOR EMERGENCY EXIT LIGHT POWER SUPPLY INOP. REPLACED SAME, OPERATION NORMAL. 2L73 4F A23WE 19951215000411995121500041WP 1995 12 15 DLL10954648 119951201A3230 RETRACT MECH LKHEED1011 10113851 5265010WP NLG MALFUNCTIONED A DALAA UNSCHED LANDING O OTHER CLCLIMB 1 SO27713DA 193C1089 AFTER TAKOFF WHEN GEAR HANDLE WAS PLACED TO NEUTRAL, NOSE GEAR STARTED TO EXTEND. RAISED GEAR HANDLE TO UP, GEAR RETRACTED. RETURNED BOS. FERRIED TO ATL. INSPECTED AND SWUNG GEAR. NO PROBLEMS NOTED, RETURNED TO SERVICE. 2L73 4F A23WE 19951215000421995121500042NM 1995 12 15 DLM88954632 119951205A3350 BATTERY PACK DOUG MD88 MD88 3023688NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27957DL 49976 ON THRU SVC CK, FOUND AFT SECTION ROW 29 AND AFT EMERGENCY PATH LIGHTS INOP. C/A REPLACED BATTERY PACK, NO HELP. REPLACED FUSES. OPS NORMAL. 2L72 4F RTA6WE 19951215000431995121500043NM 1995 12 15 DLM88954647 119951205A3350 EEL WIRE DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27937DL 49810 DURING PRE-FLIGHT, 3 ESCAPE PATH OVERWING EXIT IDENTIFIER LIGHTS FOUND INOP. REPAIRED WIRING TO LIGHTS, OPS NORMAL. 2L72 4F RTA6WE 19951215000441995121500044NM 1995 12 15 P5CA9500866 119951207A2710DL1326M1192 ACTUATOR BOEING747 747122 1384872NM RT AILERON FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23850FT 476 19755 DURING FLIGHT CONTROL CHECK, RT OUTBOARD AILERON DID NOT MOVE. GATE TURN BACK. AIRCRAFT DISPATCHED TO SJU FOR LOCKOUT ACTUATOR CHANGE DUE TO STRIKE AT CAY. AILERON LOCKOUT ACTUATOR REPLACED IAW MM 27-11-16. 2L74 4F A20WE 19951215000451995121500045NM 1995 12 15 UPS405132 119951204A5414 SKIN BOEING747 747123F NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 MAINTENANCE REPORTED NR 3 ENGINE PYLON INBOARD SIDE SKIN DOUBLER AFT OF SLOT SEAL FAIRING HAS CRACK AT INNER RADIUS OF DOUBLER EXTENDING INTO BASE METAL. REPAIRED IAW EO B747-5430-7704B. 2L74 4F A20WE 19951215000461995121500046NM 1995 12 15 95FDEA01879 119951212A5530 STRINGER BOEING727 727232 1384082NM VERT STAB WORN A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 VERTICAL FIN, BAY NR 9 FIN STA 180.6, STR 7R, WORN FASTENER HOLE AT THE RIB CHORD AND STR. REPAIRED WORN RIB CHORD AND STR PER FEDEX SRM 55-30-4, FIG 1 AND FEDEX EA 7-5510-26736. C/A ADDITION. 2L73 4F A3WE 19951215000471995121500047NM 1995 12 15 95FDEA01880 119951208A5330 SKIN BOEING727 727232 1384082NM BS 312 GOUGE A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 AT BS 312, STR 24, WL 158, THERE IS ONE SHEARED FASTENER AND A GOUGE THROUGH SKIN AND FASTENER. BLENDED GOUGE AT BS 312, STR 24, WL 158, OUT OF LIMITS PER FEDEX SRM 53-30-1. REMOVED DAMAGED AREA, INSTALLED EXTERNAL REPAIR PATCH PER FEDEX SRM 53-30-3. 2L73 4F A3WE 19951215000481995121500048NM 1995 12 15 95FDEA01881 119951208A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 344 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-229-01(1) FLOOR BEAM STA 344, LBL 3-58, WL 208.1, UPPER SURFACE OF TOP CHORD, RBL 0-42, WL 208, LOWER SURFACE OF TOP CHORD. TOP CHORD OF THE FLOOR BEAM AT BS 344 WAS FOUND TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REPAIRED FLOOR BEAM AT BS 344 IAW FEEX DRAWING SR 27-53-007. 2L73 4F A3WE 19951215000491995121500049NM 1995 12 15 95FDEA01882 119951208A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 360 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION STA 360, FLOOR BEAM WL 208.1, LBL 3-8. REMOVED CORROSION FROM FLOOR BEAM STA 360, WL 208.1, LBL 3.5. AREA WAS 2.5 INCHES BY .25 INCH. ORIGINAL THICKNESS .125 INCH. REMOVED .022 INCH, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED FILLER WASHER AND REPAIRED PER FEDEX EA 7-5310-26785. 2L73 4F A3WE 19951215000501995121500050NM 1995 12 15 95FDEA01883 119951208A5311 FRAME BOEING727 727232 1384082NM BS 720 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME BS 720A, LBL 31-LBL 37, WL 160. REPAIRED DENT IN FRAME PER FEDEX SRM 51-40-3. 2L73 4F A3WE 19951215000511995121500051NM 1995 12 15 95FDEA01884 119951208A5320 BEAM BOEING727 727232 1384082NM BS 178 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION WAS FOUND WHILE WORKING NR 0685 ON FLANGE OF BEAM AT BS 178, WL 184-189, LBL 16. 2L73 4F A3WE 19951215000521995121500052NM 1995 12 15 95FDEA01885 119951207A2433241804 TRANS/RECTIFIER BOEING747 747245F 1384897NM NR 2 FAILED A FDEAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO25641FE 20827 REFER PG 4427 (REMOVED AND REPLACED GCU). AFTER DEPART HNL, CLIMB TO FL 270, A FLASH CAME WITH LOUD BANG AND ELECTRICAL BURN SMELL (SMOKE) FROM UNDER S/O PANEL, NR 2 FIELD LIGHT ON, GEN OPEN LIGHT ON, NR 2 TRANSFORMER RECTIFIER READ ZERO VOLTS AND ZERO AMP, TR NR 2 CIRCUIT BREAKER POPPED, AND NR 2 GCU ANNUNCIATOR LIGHT ON, ON S/O PANEL. RETURNED TO HNL. REMOVED AND REPLACED NR 2 TRANSFORMER RECTIFIER, BORROWED FROM CAL AT HNL. TR OPS CHECKS OK IAW MM 24-30-00. RAN NR 2 ENG FOR OPS CHECK OF AC ENG GEN AND NR 2 ELECTRICAL SYS. OPS OK IAW MM 22-20-00. 2L74 4F A20WE 19951215000531995121500053NM 1995 12 15 95FDEA01886 119951209A2820 MANIFOLD VLV BOEING727 727233 138408ANM NR 2 TANK WIRED CLOSED A FDEAA UNSCHED LANDING O OTHER UKUNKNOWN 1 SO25262FE 21624 DIVERTED TO MCI DUE TO NR 2 FUEL TANK WITH NO CROSSFEED. ENG BURN ONLY. FOUND NR 2 MANIFOLD VALVE DEFERRED ON LOG PAGE 345931. ALSO, FOUND WIRED IN CLOSED POSITION. REPOSITIONED VALVE TO OPEN POSITION AND SECURED MANUAL HANDLE WITH SAFETY WIRE. OKAY TO CONTINUE. REMAINS DEFERRED OPEN. 2L73 4F RTA3WE 19951215000541995121500054NM 1995 12 15 95FDEA01887 119951209A2782651781823 ACTUATOR BOEING727 727225 1384077NM NR 1 LE SLAT MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25467FE 21449 NR 1 LT WING SLAT DID NOT RETRACT ON SCHEDULE. NR 1 SLAT OPS CHECK NORMAL ON EXTEND AND RETRACT. INSTALLED SLAT SWITCH JUMPER CABLE. LIGHT INDICATIONS NORMAL. RETURN JUMPER CABLE TO SECOND OFFICER'S DESK WHEN SWITCH REPLACED. REPLACED L/E SLAT ACTUATOR PER 27-80-01 COMPLIED WITH REQ ITEMS INSPECTION. OPS CHECKED, LEAK CHECKED OK. CLOSED ALL PANELS. 2L73 4F A3WE 19951215000551995121500055NE 1995 12 15 95FDEA01888 219951210A73207551501 TT2 SENSOR BOEING747 747245F 1384897NM PWA JT9 JT9D70A 52054NE NR 2 ENGINE FAILED A FDEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT CRCRUISE 1 SO25636FE 21764 IN-FLIGHT SHUTDOWN NR 2 ENGINE, ENGINE NOT RESPONDING TO THROTTLE MOVEMENT AT FL 370 IAS 250 (ATC REQ) NO TURB, ENG WAS RESTARTED AT FL 290, DESCENT AND APPROACH NORMAL. REMOVED AND REPLACED TT2 SENSOR AS PER MM 73-21-04, PG 401, RAN ENG, OPS CHECKS GOOD. ENG RESPONDED TO THROTTLE MOVEMENTS SMOOTHLY. 2L74 4F4 F A20WE E3NE 19951215000561995121500056EU 1995 12 15 COMA9531204 119951208A3150004WS00 WEU SAAB SF340 SF340A 7850100EU LT ENGINE DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01356CA14134521 340A034 LEFT ENGINE INTAKE HEAT FAILED INDICATION. REPLACED THE WARNING ELECTRONIC UNIT. 2L72 4T RTA52EU 19951215000571995121500057EU 1995 12 15 COMA9531205 119951206A2710 CONTROLS SAAB SF340 SF340A 7850100EU AILERONS LACK OF LUBE A COMAK NONE F FLT CONT AFFECTED CRCRUISE 1 SO01341CA 340A021 AILERONS ARE BINDING. INSPECTED AILERON SYSTEM AND NO FAULTS FOUND. LUBRICATED AILERON CENTERING CAMS AND ACFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19951215000581995121500058EA 1995 12 15 COMA9560618 119951206A2760 SPOILER MESSAGE CNDAIRCL600 CL6002B19 EA COCKPIT ACTIVATED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01948CA 7079 INBOARD AND OUTBOARD GROUND LIFT DUMP SPOILERS FAULT MESSAGE ON EICAS. ACFT RETURNED TO FIELD. COULD NOT DUPLICATE, NO FAULT CODES LOGGED IN SPOILER ELECTRONIC CONTROL UNIT. ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951215000591995121500059EA 1995 12 15 COMA9560619 119951207A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 EA LT COCKPIT SHATTERED A COMAK NONE O OTHER CRCRUISE 1 SO01924CA1953 7026 PILOT'S WINDSHIELD SHATTERED AT 35,000 FEET. REPLACED CAPTAIN'S WINDSHIELD. 2L72 4F RTA21EA 19951215000821995121500082WP 1995 12 15 MWEA 95444 119951208A53203915134515N FITTING DOUG DC9 DC932 3022066WP BS 756 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT AFT KEEL AT STA 756, LONGERON 30L HAS A CORRODED END FITTING. 2L72 4F A6WE 19951215000831995121500083WP 1995 12 15 MWEA 95473 119951208A531359248752N LONGERON DOUG DC9 DC932 3022066WP BS 718 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND CORROSION IN LONGERON 20 IN RT MLG WHEELWELL WHERE FS FRAME 718 MEETS LONGERON 20. REPLACED LONGERON 20 AS PER THE SRM 51-30. 2L72 4F A6WE 19951215000841995121500084WP 1995 12 15 MWEA95442 119951208A53203915135506N FITTING DOUG DC9 DC932 3022066WP BS 756 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND RIGHT AFT KEEL AT STA 756, LONGERON 29R HAD A CRACKED END FITTING. MAINTENANCE INSTALLED A NEW END FITTING IAW SRM 51-30-1, SRM 51-30-5. 2L72 4F A6WE 19951215000851995121500085WP 1995 12 15 MWEA95443 119951208A53203915134517N FITTING DOUG DC9 DC932 3022066WP BS 756 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND RT AFT KEEL AT STA 756, LONGERON 30R, HAS A CORRODED END FITTING. DRILLED UP AND INSTALLED NEW FITTING PER SRM 51-30-1. 2L72 4F A6WE 19951215000861995121500086WP 1995 12 15 MWEA95445 119951208A5314 KEEL WEB DOUG DC9 DC932 3022066WP BS 604-639 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A 1 INCH DIAMETER CORROSION HOLE IN THE FORWARD KEEL AREA SECONDARY WEB AT LONGERON 30 FROM STA 604 TO STA 639. REPLACED THE FORWARD KEEL WEB PLATING IAW SRM 51-30. 2L72 4F A6WE 19951215000871995121500087WP 1995 12 15 MWEA95446 119951208A32319915512501 FITTING DOUG DC9 DC932 3022066WP BS 699 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A CRACK IN RT GEAR DOOR ACTUATOR ATTACH FITTING AT BOTTOM OF KEEL AREA COMING OUT OF THE AFT OUTBOARD FASTENER HOLE AT STA 699. REPAIRED THE CRACK AS PER DAC TELEX ORD-SVC-0311/JSS, 27 OCT 95. 2L72 4F A6WE 19951215000881995121500088WP 1995 12 15 MWEA95447 119951208A521059347961 BEAM DOUG DC9 DC932 3022066WP PAX DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND FORWARD PASSENGER DOOR HAS A 2 INCH CRACK IN A REPAIR ON THE TOP DOOR BEAM ON THE AFT BOTTOM SIDE. REPAIRED CRACKED BEAM IAW SRM 52-05, FIGURE 31. 2L72 4F A6WE 19951215000891995121500089WP 1995 12 15 MWEA95448 119951208A5320 DOUBLER DOUG DC9 DC932 3022066WP COCKPIT WORN A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND BOTH CAPTAIN'S AFT SEAT RAILS REMOVED TO FACILITATE STRAP REPAIR. INSTALLED DOUBLER ON SEAT TRACKS AND MACHINED LOCKPIN HOLES PER SRM 53-05, FIGURE 28. INSTALLED SEAT TRACKS IAW MM 53-40. 2L72 4F A6WE 19951215000901995121500090WP 1995 12 15 MWEA95449 119951208A53209959073 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 408 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE INTERCOSTAL BELOW THE CUSP ANGLE AT STA 408 CRACKED. INSTALLED A FABRICATED INTERCOSTAL IAW SRM 53-01, PG 1. 2L72 4F A6WE 19951215000911995121500091WP 1995 12 15 MWEA95450 119951208A53132777948 LONGERON DOUG DC9 DC932 3022066WP BS 570 OVERSIZE HOLE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND ONE LONGERON WITH OVERSIZED HOLES IN SEVERAL PLACES AT STA 570, LONGERON 26L. REPLACED THE LONGERON AND SPLICE IAW SRM 53-04, FIG 2, FROM STA 551 TO STA 579. 2L72 4F A6WE 19951215000921995121500092WP 1995 12 15 MWEA95451 119951208A5330 SKIN DOUG DC9 DC932 3022066WP BS 917 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND FUSELAGE SKIN AT STA 917 AT CARGO DOOR CUT-OUT AT LONGERON 27R HAS A 2.50 INCH CRACK. FABRICATED A DOUBLER AND INSTALLED IT IAW ROD SKETCH 95-11-06-007. 2L72 4F A6WE 19951215000931995121500093WP 1995 12 15 MWEA95452 119951208A5314 KEEL WEB DOUG DC9 DC932 3022066WP BS 744-756 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT GEAR KEEL WEB HAD A SMALL AREA OF CORROSION THAT WAS BEYOND LIMITS AT STA 744 TO STA 756. FABRICATED A REPAIR WEB AND INSTALLED IAW SRM 53-01, FIG 2, SHEET 3. 2L72 4F A6WE 19951215000941995121500094WP 1995 12 15 MWEA95453 119951208A532039132081 SPLICE DOUG DC9 DC932 3022066WP BS 794-813 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 27R SPLICE WAS CRACKED AT STA 794-STA 813. FABRICATED A NEW SPLICE FITTING AND INSTALLED IAW SRM 51-30-5. 2L72 4F A6WE 19951215000951995121500095WP 1995 12 15 MWEA95454 119951208A5320 DOUBLER DOUG DC9 DC932 3022066WP BS 699 CORROSION A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT WHEELWELL KEEL WEB DOUBLER AT STA 699 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-01, FIG 2, SHEET 3. 2L72 4F A6WE 19951215000961995121500096WP 1995 12 15 MWEA95455 119951208A532049567711 ANGLE DOUG DC9 DC932 3022066WP BS 604 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND IN THE LT KEEL A CANTED ANGLE SUPPORT CRACKED IN THE RADIUS AS STA 604, LONGERON 24L. FABRICATED A NEW FITTING IAW DAC DWG 4956771 AND INSTALLED THAT ANGLE IAW THE SRM 51-30. 2L72 4F A6WE 19951215000971995121500097WP 1995 12 15 MWEA95456 119951208A53205911418514 ANGLE DOUG DC9 DC932 3022066WP RT MLG WW CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND IN THE RT WHEELWELL THE ATTACH Z-ANGLE FOR INBOARD DOOR HINGE CORRODED BEYOND LIMITS. INSTALLED A NEW Z-ANGLE IAW SRM 51-30. 2L72 4F A6WE 19951215000981995121500098WP 1995 12 15 MWEA95457 119951208A53205911418121 ANGLE DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE LT CANTED KEEL BOTTOM ANGLE HAS A CRACK IN THE RADIUS. INSTALLED A NEW ANGLE IAW THE SRM 51-30. 2L72 4F A6WE 19951215000991995121500099WP 1995 12 15 MWEA95458 119951208A5330 SKIN DOUG DC9 DC932 3022066WP BS 588-667 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE BELLY SKIN AT FORWARD KEEL STA 588 TO STA 667 HAS SEVERAL AREAS OF CORROSION UNDER LONGERONS. CORRODED SKIN REPLACED IAW SRM 51.30. 2L72 4F A6WE 19951215001001995121500100WP 1995 12 15 MWEA95459 119951208A532099115937 SUPPORT DOUG DC9 DC932 3022066WP BS 160 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE UPPER CAP AT FLOOR SUPPORT STRUCTURE AT STA 160 AT X 44.5 IS EXFOLIATED. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT SECTION IAW DOUGLAS TELEX SVC-ORD-0240/AJC. 2L72 4F A6WE 19951215001011995121500101WP 1995 12 15 MWEA95460 119951208A53305911410 SKIN DOUG DC9 DC932 3022066WP BS 570 OVERSIZE HOLES A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND 6 OVERSIZE HOLES IN SKIN AT STA 570, LONGERON 26L. REPAIRED THE OVERSIZE HOLES IAW SRM 53-04, FIG 37 PER DAC TELEX SVC-ORD-0230/DME. 2L72 4F A6WE 19951215001021995121500102WP 1995 12 15 MWEA95461 119951208A53205911366501 FITTING DOUG DC9 DC932 3022066WP BS 718 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND RT FITTING WITH CORROSION OUT OF LIMITS IN A BARREL NUT HOLE AT STA 718 JUST BELOW LONGERON 18. REMOVED AND REPLACED THE FITTING IAW SRM 51-30-1. 2L72 4F A6WE 19951215001031995121500103WP 1995 12 15 MWEA95462 119951208A53205911366501 FITTING DOUG DC9 DC932 3022066WP BS 718 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT FITTING WITH CORROSION OUT OF LIMITS IN A BARREL NUT HOLE AT STA 718 JUST BELOW LONGERON 18. REPLACED THE FITTING IAW SRM 51-30-1. 2L72 4F A6WE 19951215001041995121500104WP 1995 12 15 MWEA95463 119951208A574339150181 SPAR SPLICE DOUG DC9 DC932 3022066WP LT TE FLAP CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT FLAP FORWARD SPAR SPLICE PLATE WAS CORRODED TO EXCESS AT STA XFLS 154.5. FABRICATED A NEW SPLICE PLATE AND INSTALLED IAW SRM 57-09, PARA 14. 2L72 4F A6WE 19951215001051995121500105WP 1995 12 15 MWEA95464 119951208A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 313-332 OVERSIZED HOLES A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 21R. REPLACED THE LONGERON SECTION IAW SRM 51-30. 2L72 4F A6WE 19951215001061995121500106WP 1995 12 15 MWEA95465 119951208A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 313-332 OVERSIZED HOLES A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 22R. REPLACED THE LONGERON SECTION IAW SRM 51-30 FROM FS 229 TO 370. 2L72 4F A6WE 19951215001071995121500107WP 1995 12 15 MWEA95466 119951208A531327779225 LONGERON DOUG DC9 DC932 3022066WP BS 455 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 25R CRACKED AT FS 455. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-5 IAW SRM 51-10-4. 2L72 4F A6WE 19951215001081995121500108WP 1995 12 15 MWEA95467 119951208A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 313 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 25R DAMAGED AT STA 313. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-3 IAW SRM 51-30. 2L72 4F A6WE 19951215001091995121500109WP 1995 12 15 MWEA95468 119951208A531327779225 LONGERON DOUG DC9 DC932 3022066WP BS 455 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 24R CRACKED AT STA 455. REPLACED THE LONGERON WITH EXTRUSION P/N 27779225 IAW SRM 51-30. 2L72 4F A6WE 19951215001101995121500110WP 1995 12 15 MWEA95469 119951208A53203925966503 FITTING DOUG DC9 DC932 3022066WP BS 579 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 25R END FITTING CRACKED AT STA 579. INSTALLED A NEW END FITTING IAW SRM 51-30. 2L72 4F A6WE 19951215001111995121500111WP 1995 12 15 MWEA95470 119951208A53203915784503N FITTING DOUG DC9 DC932 3022066WP BS 699 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AN ATTACH FITTING AT THE BOTTOM LEFT OF THE KEEL BEAM CRACKED AT STA 699. FABRICATED A FITTING AND INSTALLED PER SRM 51-30. 2L72 4F A6WE 19951215001121995121500112WP 1995 12 15 MWEA95471 119951208A540049198641 BRACKET DOUG DC9 DC932 3022066WP LT PYLON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE LT PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30. 2L72 4F A6WE 19951215001131995121500113WP 1995 12 15 MWEA95472 119951208A540049198642 BRACKET DOUG DC9 DC932 3022066WP RT PYLON CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30. 2L72 4F A6WE 19951215001141995121500114WP 1995 12 15 MWEA95474 119951208A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 84 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AN INTERCOSTAL CRACKED AT STA 84 AS VIEWED THROUGH THE CAPTAIN'S AND F/O'S WINDSHIELD WIPER MOTOR COVERS. FABRICATED A REPAIR IAW THE SRM 53-03, FIG 34 AND INSTALLED IAW SRM 51-30-5. 2L72 4F A6WE 19951215001151995121500115WP 1995 12 15 MWEA95475 119951208A5330 SKIN DOUG DC9 DC932 3022066WP BS 285-323 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 TEMPORARY EXTERNAL SKIN REPAIR LOCATED AT STA 285 THROUGH 323, LONGERONS 20 THROUGH 23 RT. INSTALLED A NEW SKIN PANEL IAW THE SRM 51-30. 2L72 4F A6WE 19951215001161995121500116NM 1995 12 15 UPS205136 119951208A3260 WARNING LIGHT BOEING727 72762C 138402CNM LDG GEAR DOOR ILLUMINATED A IPXAO OTHER N FALSE WARNING ININSP/MAINT 1 SO01913UP 19245 CREW REPORTED LANDING GEAR DOOR WARNING LIGHT ILLUMINATED ON CLIMB-OUT WHEN HANDLE WAS PLACED IN OFF POSITION. CYCLED 3 TIMES, LIGHT WENT OUT. INDICATIONS ON ENGINEER PANEL WERE NORMAL. MRR FILED OPEN PENDING MX ACTION. 2L73 4F A3WE 19951215001171995121500117NM 1995 12 15 UPS405133 119951204A5414 SKIN BOEING747 747123F NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 MAINTENANCE REPORTED NR 3 ENGINE PYLON INBOARD SIDE SKIN DOUBLER AFT OF SLOT SEAL FAIRING HAS CRACK AT INNER RADIUS OF DOUBLER EXTENDING INTO BASE METAL. REPAIRED IAW EO B747-5430-7704B. 2L74 4F A20WE 19951215001181995121500118WP 1995 12 15 UPS805138 119951210A2560 BOTTLE DOUG DC8 DC873F 302199FWP EVAC SLIDE OUT OF LIMITS A IPXAK NONE O OTHER ININSP/MAINT 1 SO01816UP 45990 MAINTENANCE REPORTED BOTTLE PRESSURE OF 2500 PSI AT 25 DEGREES FAHRENHEIT, INBOARD EVACUATION SLIDE. INSTALLED SLIDE ROBBED FROM N755UP. 2L74 4F RT4A25 19951215001191995121500119NE 1995 12 15 WWMA9500086 219951209A7260J221P14 O-RING SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LT ENGINE DAMAGED A WWMAA UNSCHED LANDING K FLUID LOSS CRCRUISE 1 WP15245AE 340B245 LAS/SAN - FLT 7794 - THE AIRCRAFT DIVERTED TO LAX DUE TO A LARGE AMOUNT OF ENGINE OIL VISIBLE ON THE LEFT NACELLE AND WING. AIRCRAFT LANDED WITHOUT INCIDENT AND UPON INVESTIGATION, MAINTENANCE FOUND A CUT ON THE AC GENERATOR STATOR O-RING. THE O-RING WAS REPLACED AND THE AIRCRAFT RELEASED TO SERVICE. 2L72 4T4 TRTA52EU E8NE 19951215001201995121500120EU 1995 12 15 95ZZZX6623 119951123A2710S001003400000 ROD ASSY AEROSPATR42 ATR42300 8680920EU LT/RT AILERONS BENT A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 ORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENT. SPOILER CONTROL RODS AT BOTH LT AND RT RIB STA NR 16 BENT. REMOVED & REPLACED LT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NRS 16, 14, 13, & 8 AND RT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NR 21. REMOVED & REPLACED LT AND RT SPOILER CONTROL RODS AT RIB STA NR 16. REMOVED & REPLACED RT AILERON BELL CRANK AT RIB STA NR 27. PERFORMED ATR MM CHECKS. ACFT RETURNED TO SERVICE. REF CNTRL NRS SIMA953271, 95ZZZX6624, & 95ZZZX6625. 2H72 4T RTA53EU 19951215001211995121500121EU 1995 12 15 95ZZZX6624 119951123A2710S2711006400200 CRANK ASSY AEROSPATR42 ATR42300 8680920EU LT/RT AILERONS WORN BEARING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 ORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENT. SPOILER CONTROL RODS AT BOTH LT AND RT RIB STA NR 16 BENT. REMOVED & REPLACED LT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NRS 16, 14, 13, & 8 AND RT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NR 21. REMOVED & REPLACED LT AND RT SPOILER CONTROL RODS AT RIB STA NR 16. REMOVED & REPLACED RT AILERON BELL CRANK AT RIB STA NR 27. PERFORMED ATR MM CHECKS. ACFT RETURNED TO SERVICE. REF CNTRL NRS SIMA953271, 95ZZZX6623, & 95ZZZX6625. 2H72 4T RTA53EU 19951215001221995121500122EU 1995 12 15 95ZZZX6625 119951123A2710S2711001400100 CRANK ASSY AEROSPATR42 ATR42300 8680920EU LT/RT AILERONS WORN BEARING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 ORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENT. SPOILER CONTROL RODS AT BOTH LT AND RT RIB STA NR 16 BENT. REMOVED & REPLACED LT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NRS 16, 14, 13, & 8 AND RT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NR 21. REMOVED & REPLACED LT AND RT SPOILER CONTROL RODS AT RIB STA NR 16. REMOVED & REPLACED RT AILERON BELL CRANK AT RIB STA NR 27. PERFORMED ATR MM CHECKS. ACFT RETURNED TO SERVICE. REF CNTRL NRS SIMA953271, 95ZZZX6623, & 95ZZZX6624. 2H72 4T RTA53EU 19951215001231995121500123WP 1995 12 15 95ZZZX6626 119951114A3310BA170M0DB BALLAST DOUG DC8 DC873F 302199FWP GLARESHIELD SHORTED A RRXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP15795FT 661219002 46103 KDAY/KSEA - FLT 026 - THE CENTER GLARESHIELD LIGHTS WENT BRIGHT THEN OUT. THIS WAS FOLLOWED BY SMOKE FROM THE FIRST OFFICER'S RT CONSOLE. MAINTENANCE FOUND THE GLARESHIELD FLOOD LIGHT BALLAST SHORTED. MAINTENANCE TRANSFERRED THE GLARESHIELD LIGHTING TO THE DMI LIST IAW MEL 33-1. SD MAINTENANCE REMOVED AND REPLACED THE GLARESHIELD LIGHTS BALLAST TRANSFORMER. AN OPERATIONAL CHECK OF THE GLARESHIELD LIGHT WAS GOOD. DMI CLEARED. 2L74 4F RT4A25 19951215001241995121500124WP 1995 12 15 95ZZZX6627 119951114A27505751152503 LINK ASSEMBLY DOUG DC8 DC863 302198AWP RT TE FLAP BROKEN A RRXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP15929R 45901 KDAY/MMEX - FLT 152 - ON TAKEOFF FROM DAY, RT FLAPS EXTENDED TO 35 DEGREE FLAP INDICATION WITH SELECTOR IN 18 DEGREE POSITION. RETRACTED FLAPS TO 12 DEGREE FLAP INDICATION LT 12 DEGREES AND RT 18 DEGREES. WHEN FLAPS RE-EXTENDED TO 18 DEGREES, RT FLAP INDICATED 35 DEGREES WITH AN ASSOCIATED ROLL TO THE LEFT. AIRCRAFT RETURNED TO KDAY. SD MAINTENANCE REMOVED AND REPLACED THE RT INBOARD FLAP LINK IAW MM 27-52-02. MAINTENANCE REMOVED AND REPLACED THE INBOARD FLAP ACTUATOR AS A PRECAUTION. AN OPERATIONAL AND LEAK CHECK OF THE FLAP CONTROL SYSTEM WAS GOOD. NO DEFECTS NOTED. 2L74 4F 4A25 19951215001251995121500125WP 1995 12 15 95ZZZX6628 119951113A2150 PACK DOUG DC8 DC873F 302199FWP RIGHT OVERHEATED A RRXAA UNSCHED LANDING JMBWARNING INDICATION OVER TEMP SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP15961R 46133 KSLC/KDAY - FLT 211 - AFTER TAKEOFF FROM KSLC, CARGO COMPARTMENT FILLED WITH SMOKE. AIRCRAFT RETURNED TO KSLC. MAINTENANCE FOUND THE RT PACK OVERHEATED. MAINTENANCE TRANSFERRED THE RT PACK TO THE DMI LIST IAW MEL 21-38. SUPPLEMENTAL DATA TO FOLLOW. 2L74 4F RT4A25 19951215001261995121500126WP 1995 12 15 95ZZZX6629 119951115A2910 CONNECTOR DOUG DC8 DC873F 302199FWP SPOILER HYD PUMPDIRTY A RRXAB EMER. DESCENT J WARNING INDICATION NRNOT REPORTED 1 WP15792FT 46046 KSAN/KDAY - FLT 011 - DURING FLIGHT, THE SPOILER HYDRAULIC PUMP CIRCUIT BREAKERS TRIPPED AND WOULD NOT RESET. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED IN KDAY. MAINTENANCE CLEANED THE ELECTRICAL CONNECTOR ON THE SPOILER PUMP. AN OPERATIONAL CHECK OF THE SPOILER SYSTEM WAS GOOD ON THE GROUND. 2L74 4F RT4A25 19951215001271995121500127WP 1995 12 15 95ZZZX6630 119951116A3230 UPLATCH MECH DOUG DC8 DC862 3021970WP NLG LACK OF LUBE A RRXAO OTHER J WARNING INDICATION CLCLIMB 1 WP15990CF 46048 KDAY/KCLT - FLT 004 - AFTER TAKEOFF DURING THE UPLATCH CHECK, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED AND THE NOSE GEAR APPEARED TO FALL OUT OF THE NOSE WELL. THIS OCCURRED AFTER SEVERAL CYCLES OF THE LANDING GEAR. MAINTENANCE LUBED THE NOSE GEAR UPLATCH MECHANISM. AN OPERATIONAL CHECK OF THE NOSE GEAR UPLATCH WAS GOOD IAW MM 32-22-1. 2L74 4F 4A25 19951215001281995121500128WP 1995 12 15 95ZZZX6631 119951116A3230 UPLOCK MECH DOUG DC8 DC862 3021970WP MLG DOOR LACK OF LUBE A RRXAO OTHER J WARNING INDICATION CLCLIMB 1 WP15994CF 45956 KDAY/KAUS - FLT 108 - ON GEAR RETRACTION, THE GEAR DOOR LIGHT REMAINED ON. THE FLIGHT CREW CYCLED THE LANDING GEAR PER THE ABNORMAL OPERATIONS PROCEDURES AND CONTINUED AT REDUCED AIRSPEED (230 KNOTS). THE MLG DOOR UPLATCH MECHANISM WAS LUBRICATED, AND AN OPERATIONAL CHECK WAS PERFORMED IAW 32-00. NO DEFECTS NOTED. 2L74 4F 4A25 19951215001291995121500129EA 1995 12 15 95ZZZX6632 119951122A273082710093103 ELEV OUTPUT LVR DHAV DHC8 DHC8311 1386006EA CONTROL COLUMN LOOSE BOLTS A MASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9238 286 DURING MAINTENANCE, THE LT YOKE WAS FOUND TO HAVE PLAY IN THE PITCH CONTROL. AFTER INSPECTION, FOUND THE 6 BOLTS ON THE ELEVATOR OUTPUT LEVER WERE ALL LOOSE, NO APPARENT VISUAL DAMAGE FOUND TO THE OUTPUT LEVER ASSY. THE BOLTS REQUIRED RE-TORQUING ON THE LT AND RT OUTPUT LEVER. THESE BOLTS WERE RE-TORQUED IAW DASH 8-300 MM 27-32-41, PAGE 201. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19951215001301995121500130NE 1995 12 15 95ZZZX6633 219951125A7261 DRAIN ELBOW BOEING747 747212B 1384886NM PWA JT9 JT9D7F 52054NE NR 3 BEARING LEAKING A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM09482EV 20713 662333 JFK - LOG PAGE F00707 - NR 4 ENGINE OIL QUANTITY INDICATOR STEADILY DROPPED TO APPROXIMATELY 1 GALLON, THEN PEGGED OFF. SHUT DOWN ENGINE DUE TO FLUX OIL PRESSURE AND UNKNOWN QUANTITY, MAXIMUM TEMPERATURE 110 DEGREES FOR 1 MINUTE, WINDMILLING PRESSURE, 14 PSI. OPS CHECK OF ENG, SYSTEM WORKS NORMALLY. PERFORMED ENG WINDMILLING INSP PER 72-00-00, GEARBOX STATIC LEAK CHECK CARRIED OUT, FOUND HYD PUMP SEAL DRAIN LEAKING, CHANGED CARBON SEAL. AFTER POWER RUN, FOUND NR 3 BEARING DRAIN ELBOW LEAKING. REPLACED ELBOW, FOUND COVER ON GEARBOX LEAKING, RETORQUED BOLTS. REFERENCE OPERATOR CONTROL NR EIAA9562. (X) 2L74 4F4 F A20WE E20EA 19951215001311995121500131CE 1995 12 15 95ZZZX6634 119951027A57301181100476 LE SKIN BEECH 1900 1900C 1154161CE RT WING CRACKED A GLBAO OTHER C F.O.D. CRCRUISE 1 CE01555229880 UC171 MSP - CREW REPORTED A BIRDSTRIKE ON THE RT WING LEADING EDGE 4 FEET OUTBOARD OF NACELLE. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A SEALED FLUSH PATCH REPAIR IAW BEECH SRM 57-90-00, PAGES 14-16. 2L72 4T RTA24CE 19951215001321995121500132CE 1995 12 15 95ZZZX6635 119951102A3230571302 POWER PACK MOTOR BEECH 1900 1900C 1154161CE LANDING GEAR INOPERATIVE A GLBAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 CE01123UE2901 181A UC123 YKN - CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. THEY ELECTED TO DIVERT TO GRI, MANUALLY LOWERED THE GEAR, AND ACCOMPLISHED A SUCCESSFUL LANDING. MAINTENANCE CHANGED THE POWER PACK MOTOR, THE RT SQUAT SWITCH, AND THE POSITION INDICATOR DIODE. A SUCCESSFUL GEAR SWING AND TEST WERE ACCOMPLISHED. 2L72 4T RTA24CE 19951215001331995121500133CE 1995 12 15 95ZZZX6636 119951102A532050420076 BEAM BEECH 1900 1900C 1154161CE COCKPIT BENT A GLBAO OTHER C F.O.D. APAPPROACH 1 CE0160UE 17288 UC60 SPW - DURING APPROACH, A MALLARD CONTACTED THE LT WINDSHIELD. THE WINDSHIELD COBWEBBED AND HAD A SMALL AMOUNT OF SHATTER. THE UPPER WINDSHIELD BEAM AND LT WINDSHIELD WERE REPLACED. REFERENCE OPERATOR CONTROL NR 95ZZZX6637. 2L72 4T RTA24CE 19951215001341995121500134CE 1995 12 15 95ZZZX6637 119951102A56101143840201 WINDSHIELD BEECH 1900 1900C 1154161CE WINDSHIELD BROKEN A GLBAO OTHER C F.O.D. APAPPROACH 1 CE0160UE 17288 UC60 SPW - DURING APPROACH, A MALLARD CONTACTED THE LT WINDSHIELD. THE WINDSHIELD COBWEBBED AND HAD A SMALL AMOUNT OF SHATTER. THE UPPER WINDSHIELD BEAM AND LT WINDSHIELD WERE REPLACED. REFERENCE OPERATOR CONTROL NR 95ZZZX6636. 2L72 4T RTA24CE 19951215001351995121500135CE 1995 12 15 95ZZZX6638 119951102A3230 SWITCHES BEECH 1900 1900C 1154161CE LANDING GEAR FROZEN A GLBAA UNSCHED LANDING O OTHER CLCLIMB 1 CE01101UE UC101 DVL - AFTER DEPARTURE, THE CREW ELECTED AN AIR TURN BACK DUE TO INABILITY TO RETRACT LANDING GEAR. MAINTENANCE PLACED THE AIRPLANE IN A HEATED HANGAR, THAWED OUT THE SWITCHES, AND ACCOMPLISHED SATISFACTORY GEAR SWINGS. 2L72 4T RTA24CE 19951215001361995121500136CE 1995 12 15 95ZZZX6639 119951102A32341013841377 CONTROL HANDLE BEECH 1900 1900C 1154161CE LANDING GEAR OPEN A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01101UE 180 UC101 JMS - ON DEPARTURE FROM JMS, THE CREW DETERMINED THE LANDING GEAR WOULD NOT RETRACT. THEY ELECTED AN AIR TURN BACK AND ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR CONTROL HANDLE. THE GEAR SWING AND OPS CHECK WERE SATISFACTORY. 2L72 4T RTA24CE 19951215001371995121500137SO 1995 12 15 95ZZZX6640 119951021A30402SC1601 CURRENT SENSOR EMB 120 EMB120RT SO RT WINDSHIELD SHORTED A GLBAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE01281UE 120092 ORD - CREW REPORTED AN ELECTRICAL SMELL IN THE COCKPIT. MAINTENANCE FOUND THE LEADS FOR THE WINDSHIELD HEAT CURRENT SENSOR HAD ARCED. THE CURRENT SENSOR WAS REPLACED. THE SYSTEM TESTED SATISFACTORILY. 2L72 4T RTA31SO 19951215001381995121500138CE 1995 12 15 95ZZZX6641 119951024A712012991003279 TRUSS BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0198GL 5078 425 UC98 SPW - DURING THE SCHEDULED VISUAL INSPECTION OF AREA 'A' OF THE LT ENGINE TRUSS AS REQUIRED BY AD 95-02-18, A SMALL CRACK WAS FOUND ON THE UPPER RT BRACKET THAT HOLDS THE COWL. THE CRACK WAS REPAIRED IAW BEECH KIT NR 129-9006. 2L72 4T RTA24CE 19951215001391995121500139CE 1995 12 15 95ZZZX6642 119951024A712012991003279 TRUSS BEECH 1900 1900C 1154161CE LT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE0160UE 7784 324 UC60 SPW - DURING VISUAL INSPECTION OF AREA 'A' REQUIRED BY AD 95-02-18, THE TRUSS WAS FOUND CRACKED AT THE LT OUTBOARD SIDE AT THE WELD FOR THE COWL MOUNT. THE LT TRUSS WAS REPAIRED IAW BEECH KIT NR 129-9006. 2L72 4T RTA24CE 19951215001401995121500140CE 1995 12 15 95ZZZX6643 119951012A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01557823652 497 UC168 ESC - DURING SCHEDULED VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE ENGINE TRUSS WAS FOUND CRACKED AT THE INBOARD TOP STRUT AT THE OIL PLUG. THE CRACK WAS REPAIRED IAW BEECH REPAIR KIT 129-9006. 2L72 4T RTA24CE 19951215001411995121500141CE 1995 12 15 95ZZZX6644 119951101A3260444EH496 SQUAT SWITCH BEECH 1900 1900C 1154161CE MLG OUT OF ADJUST A GPPAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE09120GP UC59 GSP/DAY - FLT 2300 - DURING CLIMB, GEAR WOULD NOT RETRACT. AIR RETURNED TO CMH GATE AND RETURNED TO MAINTENANCE. UPON INSPECTION, MAINTENANCE ADJUSTED SQUAT SWITCH. PERFORMED SEVERAL GEAR SWINGS ON GROUND. AIRCRAFT RELEASED FOR FLIGHT. 2L72 4T RTA24CE 19951215001431995121500143CE 1995 12 15 95ZZZX6646 119951006A29101013880083 SERVICE VALVE BEECH 1900 1900C 1154161CE HYD SYSTEM STICKING A GPPAO OTHER O OTHER APAPPROACH 1 CE0919016 UC22 GREENSBORO - FLT 2304 - UPON ARRIVAL INTO GREENSBORO 18:00 EASTERN TIME, GEAR WOULD NOT EXTEND, PILOTS MANUALLY EXTENDED GEAR. REMOVED AND REPLACED HYDRAULIC SERVICE VALVE. 2L72 4T RTA24CE 19951215001441995121500144CE 1995 12 15 95ZZZX6647 119951101A26127C14 FIRE LOOP CLAMP BEECH 1900 1900C 1154161CE NR 2 ENGINE BROKEN A GPPAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE09125GP UB6 MCI - FLT 2111 - DURING TAKEOFF AND CLIMB APPROXIMATELY 6:00 A.M., RT T-HANDLE ILLUMINATED FOR ABOUT 10 SECONDS AND EXTINGUISHED. PLANE RETURNED TO GRI FOR MAINTENANCE. AIRCRAFT WAS HEADING TO MCI, FLT 2111. REMOVED AND REPLACED BROKEN FIRE LOOP CLAMP, PN 7C1-4, NEAR OUTBOARD EXHAUST STACK. 2L72 4T RTA24CE 19951215001451995121500145NE 1995 12 15 EIAA9562 219951125A7260 CARBON SEAL BOEING747 747212B 1384886NM PWA JT9 JT9D7F 52054NE HYD PUMP LEAKING A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM09482EV 20713 662333 JFK - LOG PAGE F00707 - NR 4 ENGINE OIL QUANTITY INDICATOR STEADILY DROPPED TO APPROXIMATELY 1 GALLON, THEN PEGGED OUT. SHUT DOWN ENGINE DUE TO FLUX OIL PRESSURE AND UNKNOWN QUANTITY, MAXIMUM TEMPERATURE 110 DEGREES FOR 1 MINUTE, WINDMILLING PRESSURE, 14 PSI. OPS CHECK OF ENG, SYSTEM WORKS NORMALLY. PERFORMED ENG WINDMILLING INSP PER 72-00-00, GEARBOX STATIC LEAK CHECK CARRIED OUT, FOUND HYD PUMP SEAL DRAIN LEAKING, CHANGED CARBON SEAL. AFTER POWER RUN, FOUND NR 3 BEARING DRAIN ELBOW LEAKING. REPLACED ELBOW, FOUND COVER ON GEARBOX LEAKING, RETORQUED BOLTS. REFERENCE OPERATOR CONTROL NR 95ZZZX6633. (X) 2L74 4F4 F A20WE E20EA 19951215001461995121500146WP 1995 12 15 GRAA9550 119951111A3350502B EEL SOCKET DOUG DC9 DC982 3022082WP TAIL SECTION FAILED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP11500TR 49144 WHILE PERFORMING A TURNAROUND/OVERNIGHT INSPECTION, MAINTENANCE DISOVERED THAT THE LEFT EMERGENCY STAIRWAY LIGHT IN THE TAIL SECTION TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT SOCKET ASSEMBLY. OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951215001471995121500147WP 1995 12 15 GRAA9551 119951119A3222MS288892 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG FAILED A GRAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP11500TR 49144 MYR - AIRCRAFT DEPARTED AND THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED WITH NO AIR SHIFT. AIRCRAFT RETURNED TO MYR; MADE AN OVERWEIGHT LANDING. MAINTENANCE DISCOVERED THE SCHRADER VALVE FOR THE NOSE STRUT LEAKING. MAINTENANCE REPLACED THE SCHRADER VALVE AND SERVICED THE STRUT TO THE PROPER LIMIT WITH FLUID AND AIR. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PROXIMITY SWITCH. NO DEFECTS NOTED. MAINTENANCE PERFORMED AN OVERWEIGHT INSPECTION, 'PART A'. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2L72 4F A6WE 19951215001481995121500148WP 1995 12 15 HAL95145 119951108A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13420EA 47689 HNL - INFORMATION FROM LOG PAGE 146503 - OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 2-7 INOPERATIVE AND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 17-21 ARE DIM. (X) 2L72 4F A6WE 19951215001491995121500149WP 1995 12 15 HAL95147 119951112A33501001191 EEL DOUG DC9 DC951 3022051WP FWD ENTRANCE INOPERATIVE A HALAK NONE L NO TEST ININSP/MAINT 1 WP13603DC 771 47784 HNL - INFORMATION FROM LOG PAGE 146538-3 - EMERGENCY EXIT LIGHT OUT AT FRONT ENTRANCE. (PORTABLE EMERGENCY LIGHT.) REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPERATIONAL CHECK OK. (X) 2L72 4F A6WE 19951215001501995121500150 1995 12 15 HAL95148 419951112A3442 RADAR DOUG DC9 DC951 3022051WP FORWARD FUSELAGEFAILED A HALAK NONE O OTHER ININSP/MAINT 1 WP13679HA 47662 HNL - INFORMATION FROM LOG PAGE 146631-1 - DURING RADAR CHECK, RADAR SCREEN WENT BLANK AND LOUD BANG HEARD FROM FRONT OF AIRCRAFT. SMELL OF BURNING ELECTRICAL COMPONENTS IN COCKPIT. DEFERRED PER MEL 34-19. RADAR PLACARDED INOP. TRANSCRIBED TO HAL 1414, DMI NR 97173. TROUBLESHOOTING IN PROGRESS. (X) 2L72 4F A6WE 19951215001511995121500151WP 1995 12 15 HAL95149 119951110A3350 BATTERY PACK DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13148AA 46703 HNL - INFORMATION FROM LOG PAGE 3590898 - ON PRE-FLIGHT, FOUND FORWARD POWER SUPPLY OF EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY SUPPLY PACK, OPERATIONAL CHECK OK. (X) 2L73 4F A22WE 19951215001521995121500152WP 1995 12 15 HAL95150 119951112A3820159445 HOSE DOUG DC10 DC1010 3022110WP AFT LAVATORY PUNCTURED A HALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP13171AA 46906 HNL - FLT 22 - INFORMATION TAKEN FROM LOG PAGE 3657248 - REAR LAVATORIES, DENSE SMOKE, STEAM, AND ODOR. FOUND HOSE, PN 159445, PUNCTURED IN NR 3 AFT LAVATORY, REMOVED AND REPLACED HOSE. OPS CHECK, LEAK CHECK OK. (X) 2L73 4F A22WE 19951215001531995121500153EU 1995 12 15 P2RA950027 119951113A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R2 DOOR MALFUNCTIONED A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 R-2 DOOR WILL NOT DISARM. CHECKED GIRT BAR AND SLIDE BAR FOR BEING IN PLACE, CHECKED OK, CYCLED ARM/DISARM HANDLE, OPERATES NORMALLY PER MM 52-22-22. (X) 2L72 4F A35EU 19951215001541995121500154EU 1995 12 15 P2RA950028 119951114A2611 SMOKE DET SW AIRBUS300 A300B4203 3930306EU F LAVATORY OUT OF POSITION A P2RAO OTHER N FALSE WARNING CLCLIMB 1 WP2314975 261 LAV 'F' SMOKE DETECTOR ALARM ACTIVATED DURING CLIMB. FOUND LAV 'F' SMOKE DETECTOR TEST SWITCH NOT ALL THE WAY IN OFF POSITION. ROTATED TO OFF, OPERATIONAL CHECK GOOD. (X) 2L72 4F A35EU 19951215001551995121500155EU 1995 12 15 P2RA950029 119951114A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R2 DOOR INOPERATIVE A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 R-2 DOOR WILL NOT DISARM. OPERATED DISARM HANDLE SEVERAL CYCLES, DOOR DISARM OK PER MM 52-22-22. (X) 2L72 4F A35EU 19951215001561995121500156EU 1995 12 15 SIMA953221 119951118A77128108001002 T1.8 SENSOR AEROSPATR72 ATR72212 EU NR 1 ENGINE SHORTED A SIMAA UNSCHED LANDING O OTHER TOTAKEOFF 1 SW21440AM425 4 C94040006 440 DFW - FLT 3599 - DURING TAKEOFF, NR 1 ENGINE TORQUE INDICATION SURGED. AIRCRAFT RETURNED TO DFW. REMOVED AND INSPECTED T1.8 SENSOR. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 391.0. (X) 2H72 4T RTA53EU 19951215001571995121500157EU 1995 12 15 SIMA953271 119951123A2710S2711009200000 BELL CRANK ASSY AEROSPATR42 ATR42300 8680920EU LT/RT AILERONS WORN BEARING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21421MQ 014 ORD - DURING ACCOMPLISHMENT OF EO E9-2700-001 INSP OF AILERON CONTROL SYS, FOUND PENDULAR LEVER ASSY AT LT WING RIB STA NRS 16, 14, 13, AND 8, RT WING RIB STA NR 21 FAILED TOLERANCE REQUIREMENTS. RT WING BELL CRANK ASSY AT RIB STA NR 27 HAS EXCESSIVE MOVEMENT. SPOILER CONTROL RODS AT BOTH LT AND RT RIB STA NR 16 BENT. REMOVED & REPLACED LT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NRS 16, 14, 13, & 8 AND RT WING AILERON PENDULAR LEVER CRANK ASSY AT RIB STA NR 21. REMOVED & REPLACED LT AND RT SPOILER CONTROL RODS AT RIB STA NR 16. REMOVED & REPLACED RT AILERON BELL CRANK AT RIB STA NR 27. PERFORMED ATR MM CHECKS. ACFT RETURNED TO SERVICE. REF CNTRL NRS 95ZZZX6623, 95ZZZX6624, & 95ZZZX6625. (X) 2H72 4T RTA53EU 19951215001581995121500158EU 1995 12 15 SIMA953301 119951126A33503011210 EEL ASSY AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21249AT2041 550 0249 ORD - FLT 4061 - EMERGENCY LIGHT ON PASSENGER DOOR INOP. REMOVED AND INSPECTED LIGHT ASSY, SYSTEM OPS CHECKED GOOD. ACFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2,582. (X) 2H72 4T RTA53EU 19951215001591995121500159EU 1995 12 15 SIMA953321 119951128A2910L387105A SWIVEL FITTING SAAB SF340 SF340A 7850100EU RT MLG BROKEN A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21107AE 340A107 DFW - FLT 3537 - SHORTLY AFTER TAKEOFF, AIRCRAFT HAD A COMPLETE HYDRAULIC SYSTEM FAILURE. CREW PUMPED GEAR DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE SWIVEL FITTING ON THE RT MAIN GEAR FAILED. REPLACED FITTING, OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T RTA52EU 19951215001601995121500160EU 1995 12 15 SIMA953332 119951129A7931311489201 SWITCHING VALVE AEROSPATR72 ATR72212 EU NR 2 ENGINE MALFUNCTIONED A SIMAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW21274AT 274 ORD - FLT 4256 - PIREP SMOKE/OIL SMELL IN CABIN. REMOVED AND INSPECTED NR 2 ENGINE P3/25 SWITCHING VALVE. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19951215001611995121500161SO 1995 12 15 SRAA119501 119951109A291366039 HYD PUMP LKHEED382 382E 526413USO NR 1 ENGINE FAILED A SRAAO OTHER J WARNING INDICATION DEDESCENT 1 SO19522SJ 4362 NBO - FLT R515 - DURING DESCENT INTO NBO, NR 1 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IMMEDIATELY AFTER LANDING GEAR INDICATED DOWN AND LOCKED. UNABLE TO RESTORE PRESSURE, ISOLATED UTILITY SYSTEM PER AOM. REPLACED ENGINE DRIVEN HYDRAULIC PUMP, DRAINED UTILITY SYSTEM, AND REPLACED ALL UTILITY SYSTEM FILTERS, PERFORMED ENGINE RUN-UP AND DRAINED, RE-SERVICED SYSTEM, OPS CHECKED PR MM, CHAPTER 29. (X) 2H74 4T A1SO 19951215001621995121500162SO 1995 12 15 SRAA119502 119951109A6120582855 VALVE HOUSING LKHEED382 382E 526413USO NR 4 PROP FAILED A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19923SJ 4301 RMS - FLT ADT4 - DURING FLIGHT INTO RMS, NR 4 PROPELLER FLUCTUATED OUT OF LIMITS, FEATHERED PROP AND SHUT DOWN NR 4 ENGINE. REPLACED NR 4 PROPELLER VALVE HOUSING AND RIGGED PROP PER JOB CARDS 6103 AND 6101-1, PERFORMED ENGINE RUN-UP. OPS CHECKED GOOD IAW MM CHAPTER 61 AND CHAPTER 71. (X) 2H74 4T A1SO 19951215001631995121500163NM 1995 12 15 SRAA119503 119951113A5413 SKIN BOEING747 747246F NM NR 3 PYLON CRACKED A SRAAK NONE O OTHER NRNOT REPORTED 1 SO19740SJ 22477 ON WALK-AROUND INSPECTION, FOUND NR 3 PYLON INBOARD SKIN AT STA 180 BULKHEAD AND FORWARD LOWER SPAR HAS CRACK FROM LOWER EDGE OF SKIN THROUGH 2 FASTENER HOLES, TOTAL LENGTH OF 1.5 INCHES. STOP DRILLED CRACK AND INSTALLED INTERIM REPAIR PER BOEING INSTRUCTION REF STTE951113,/2, STT-SDF-95-003RE, STTE951114, AND STT-SDF-95-0005RE. PERMANENT REPAIR TO BE CARRIED OUT AT NEXT B-CHECK. (X) 2L74 4F A20WE 19951215001641995121500164NM 1995 12 15 SRAA119504 119951113A5413 SKIN BOEING747 747246F NM NR 4 PYLON CRACKED A ASRAAK NONE O OTHER NRNOT REPORTED 1 SO19740SJ 22477 ON WALK-AROUND INSPECTION, FOUND NR 4 PYLON INBOARD SKIN AT STA 180 BULKHEAD AND FORWARD LOWER SPAR HAS CRACK FROM LOWER EDGE OF SKIN THROUGH 2 FASTENER HOLES, TOTAL LENGTH OF CRACK IS 2.25 INCHES. STOP DRILLED CRACK AND INSTALLED INTERIM REPAIR PER BOEING INSTRUCTION REF STTE951113,/2, STT-SDF-95-003RE, STTE951114, AND STT-SDF-9-0005RE. PERMANENT REPAIR TO BE CARRIED OUT AT NEXT B-CHECK. (X) 2L74 4F A20WE 19951215001651995121500165WP 1995 12 15 9519809106 119951204A5320 FITTING DOUG DC9 DC915 3022036WP FS 503 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0196S 47206 DURING H-CHECK, FOUND A CRACK IN THE LONGERON 29A RIGHT FITTING AT FS 503. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19951215001661995121500166WP 1995 12 15 9519819153 119951204A5320 FITTING DOUG DC9 DC914 3022034WP FS 468 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND A THREE INCH CRACK IN THE LONGERON 30 END FITTING AT FS 468. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19951215001671995121500167WP 1995 12 15 9519829307 119951205A5320 FITTING DOUG DC9 DC982 3022082WP FS 1338 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING H-CHECK, FOUND CORROSION IN THE RIGHT FS 1338 FRAME TO LAVATORY WEB FITTING. REPLACED FITTING (P/N 5913700-2) PER ARM 51-01. 2L72 4F A6WE 19951215001681995121500168NM 1995 12 15 9519832285 119951205A5230 FITTING BOEING727 727251 138408HNM CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01285US 21324 DURING LINE CHECK, FOUND A CRACK IN THE AFT CARGO DOOR LOWER FORWARD ROLLER GUIDE FITTING. REPLACED FITTING. 2L73 4F A3WE 19951215001691995121500169WP 1995 12 15 9519849857 119951205A5320 FITTING DOUG DC9 DC951 3022051WP FS 1167 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01766NC 47739 DURING H-CHECK, FOUND CORROSION IN THE LONGERON 22R END FITTING AT FS 1167. REPLACED FITTING PER SRM 51-30. 2L72 4F A6WE 19951215001701995121500170WP 1995 12 15 9519859922 119951206A5744 FITTING DOUG DC9 DC932 3022066WP SPOILER CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01945N 47664 DURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD FLIGHT SPOILER SUPPORT FITTING. REPLACED FITTING. 2L72 4F A6WE 19951215001711995121500171WP 1995 12 15 9519869153 119951207A5320 FITTING DOUG DC9 DC914 3022034WP FS 786 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND A CRACK IN THE FS 786 FITTING AT THE INBOARD CORNER OF THE LEFT LAVATORY FORWARD BULKHEAD JUST BELOW THE FLOOR LINE. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19951215001721995121500172WP 1995 12 15 9519879153 119951207A5220 UNLOCK MECH DOUG DC9 DC914 3022034WP EMER EXIT DOOR OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND THAT INADQUATE FORCE WAS REQUIRED TO OPERATE THE RIGHT OVERWING EMERGENCY EXIT USING THE EXTERIOR HANDLE. RE-RIGGED THE DOOR PER MM 52-21-0-501. 2L72 4F A6WE 19951215001731995121500173WP 1995 12 15 9519889916 119951207A3350 BATTERY PACK DOUG DC9 DC932 3022066WP NACELLE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01949N 47566 DURING LINE CHECK, FOUND NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001741995121500174WP 1995 12 15 9519899952 119951207A3350 EEL DOUG DC9 DC931 3022065WP CABIN DEFECTIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01916RW 47144 DURING LINE CHECK, FOUND AFT CABIN FLOOR EMERGENCY LIGHTS DEFECTIVE. REPLACED THE TAIL COMPARTMENT EXIT SIGN. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001751995121500175WP 1995 12 15 9519909311 119951207A3350 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01314RC 49110 DURING LINE CHECK, FOUND EMERGENCY CEILING LIGHTS ROWS 24-30 INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001761995121500176WP 1995 12 15 9519919852 119951207A3350 BATTERY PACK DOUG DC9 DC951 3022051WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01761NC 47709 DURING LINE CHECK, FOUND TAILCONE OVERHEAD EMERGENCY LIGHT INOPERATIVE. ALSO, FOUND OVERHEAD AISLE LIGHTS ROWS 16-19 AND 23 INOPERATIVE. REPLACED BATTERIES FOR TAILCONE EMERGENCY LIGHTS. RESECURED BATTERIES AND REPLACED BULB FOR AISLE LIGHTS. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001771995121500177WP 1995 12 15 9519929138 119951207A3350 BATTERY PACK DOUG DC9 DC915 3022036WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019348 45787 DURING LINE CHECK, FOUND TAIL ESCAPE PATH LIGHTS, AFT EMERGENCY EXIT DOOR LIGHT, RIGHT EMERGENCY FLOOR LIHGTS, AND LAV AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED NR 6, 7, AND 8 BATTERY PACKS AND REPAIRED WIRE IN LAV AISLE EMERGENCY LIGHT FIXTURE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001781995121500178NM 1995 12 15 9519932255 119951208A3260 IND SWITCH BOEING727 727251 138408HNM LANDING GEAR MALFUNCTIONED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL01255US 19974 DURING APPROACH ON LANDING GEAR EXTENSION, NO GREEN LIGHTS ILLUMINATED, JUST ONE RED GEAR LIGHT. RECYCLED GEAR, TWO GREEN MAIN ON AND THIRTY SECONDS LATER NOSE GREEN LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED SWITCHES AT S93 AND S96 AND LOCK SWITCH LINKAGE. SWUNG GEAR. CHECKED OK. 2L73 4F A3WE 19951215001791995121500179NM 1995 12 15 9519945518 119951209A3350 BATTERY PACK BOEING757 757251 1384970NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01518US 23206 DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING INOPERATIVE FROM DOOR 1 TO DOOR 2. REPLACED LEFT FLOOR BATTERY. 2L72 4F RTA2NM 19951215001801995121500180EU 1995 12 15 9519953204 119951208A3350321454 EEL POWER SUPPLY AIRBUS320 A320211 3930320EU CABIN INOPERATIVE A NWAAK NONE L NO TEST UKUNKNOWN 1 GL01304US139826009 040 CABIN EMERGENCY LIGHT CIRCUIT BREAKER POPPED ON THE OVERHEAD PANEL. MAINTENANCE REPLACED THE FORWARD EPSU AND BATTERIES. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951215001811995121500181EU 1995 12 15 9519963204 119951208A2611 SMOKE LIGHT AIRBUS320 A320211 3930320EU AVIONICS COMPT ILLUMINATED A NWAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL01304US 040 DURING CRUISE, THE SMOKE LIGHT ON THE GEN 1 LINE PUSH BUTTON SWITCH ON THE FLIGHT DECK OVERHEAD PANEL ILLUMINATED ACCOMPANIED BY AN INTERMITTENT VENT EXTRACT FAULT. AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO SIGN OF SMOKE OR FIRE. AIRCRAFT WAS MAINTENANCE FERRIED TO DCA WHERE DEICING FLUID WAS FOUND ON AND IN THE 70VU CARD FILE. GLYCOL WAS ALSO FOUND CONTAMINATING THE AVIONICS EQUIPMENT VENTILATION FILTERS. REPLACED THE FILTERS AND CLEANED AREA. AIRCRAFT WAS OK FOR SERVICE. 2L72 4F RTA28NM 19951215001821995121500182WP 1995 12 15 9519979986 119951209A3260 UPLOCK SWITCH DOUG DC9 DC932 3022066WP LANDING GEAR DR MALFUNCTIONED A NWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 GL01986US 47480 DURING APPROACH, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER THE LANDING GEAR WAS EXTENDED. APPROACH WAS ABORTED AND A GO-AROUND PERFORMED. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED UPLOCK SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001831995121500183NM 1995 12 15 9519982285 119951208A3610 FLEX LINE BOEING727 727251 138408HNM NR 3 STRUT BBOKEN A NWAAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL01285US 21324 DURING CLIMB PASSING THROUGH 2000 MSL ON TAKEOFF, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED BROKEN FLEX LINE. OPERATIONAL CHECK OK. 2L73 4F A3WE 19951215001841995121500184EU 1995 12 15 9519993211 119951208A2810568127202002 FUEL TANK AIRBUS320 A320211 3930320EU NR 1 MAIN CONTAMINATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01311US 125 DURING CLIMBOUT, BOTH LEFT MAIN FUEL PUMPS WENT TO LOW PRESSURE WHEN CLIMB POWER WAS CALLED FOR. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ICE AND WATER FROM THE NR 1 FUEL TANK. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951215001851995121500185 1995 12 15 9520003232 419951130A3417HG1150AC05 AIR DATA COMP AIRBUS320 A320211 3930320EU AVIONICS BAY MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01332NW1171811718 319 WHILE CLIMBING THROUGH 15,000 FEET MSL, RECEIVED F/CTL ADR DISAGREE AND F/CTL ALTN LAW (PROT LOST) MESSAGES. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CONTINUED ON TO ORIGINAL DESTINATION WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA COMPUTER. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951215001861995121500186WP 1995 12 15 9520019995 119951206A3213 STRUT DOUG DC9 DC931 3022065WP LT MLG WORN A NWAAK NONE O OTHER LDLANDING 1 GL018978E 47327 WHILE AIRCRAFT WAS IN DTW, MAINTENANCE NOTICED THE LEFT MAIN LANDING GEAR WHEEL ASSEMBLY MISSING. MAINTENANCE ALSO FOUND DAMAGE ON THE LEFT INBOARD TRAILING EDGE FLAP. INSPECTED AND FOUND LEFT MAIN LANDING GEAR STRUT WORN BEYOND LIMITS. REPLACED LEFT MAIN LANDING GEAR SHOCK STRUT PISTON ASSEMBLY AND LEFT INBOARD TRAILING EDGE FLAP PANEL. REPLACED BOTH LEFT MAIN LANDING GEAR WHEEL AND BRAKE ASSSEMBLIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001871995121500187 1995 12 15 9520029928 419951209A3416 ALTIMETER DOUG DC9 DC931 3022065WP LEFT FAILED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018921E 45836 DURING CRUISE, THE CAPTAIN'S ALTIMETER FAILED. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE CAPTAIN'S ALTIMETER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001881995121500188WP 1995 12 15 9520039996 119951209A351015830AB OXYGEN REG DOUG DC9 DC931 3022065WP LT COCKPIT LEAKING A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018932E4571621754 47141 DURING CRUISE, CREW OXYGEN DEPLETED. THE AIRCRAFT DIVERTED TO STL AND LANDED WITHOUT INCIDENT. FOUND CAPTAIN'S OXYGEN REGULATOR LEAKING. REPLACED REGULATOR AND OXYGEN BOTTLE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001891995121500189WP 1995 12 15 9520049935 119951208A2120 AIR DISTR DOUG DC9 DC931 3022065WP CABIN ODOR A NWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL011332U 47404 DURING CLIMB, AN UNIDENTIFIED SMELL WAS REPORTED BY THE FLIGHT ATTENDANTS. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT SYSTEMS AND COMPONENTS AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951215001901995121500190WP 1995 12 15 9520059919 119951209A3230 RETRACT MECH DOUG DC9 DC932 3022066WP LANDING GEAR OUT OF ADJUST A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01941N 47450 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRACTION BY USING LANDING GEAR HANDLE RELEASE BUTTON. RECYCLED LANDING GEAR AND LANDING GEAR OPERATED NORMALLY. AIRCRAFT CONTINUED TO SLC AND LANDED WITHOUT INCIDENT. RIGGED GROUND SHIFT CABLES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001911995121500191WP 1995 12 15 9520069919 119951207A3230 RETRACT MECH DOUG DC9 DC932 3022066WP NLG LACK OF LUBE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01941N 47450 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BIL AND LANDED WITHOUT INCIDENT. REMOVED AND LUBRICATED APEX BOLT ON NOSE LANDING GEAR TRUNNION LINK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001921995121500192WP 1995 12 15 9520079957 119951210A2824 CIRCUIT BREAKER DOUG DC9 DC931 3022065WP AUX FUEL PUMP TRIPPED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL01915RW 47139 DURING CRUISE, THE FUEL IN THE AUXILIARY FUEL TANK WOULD NOT TRANSFER. AIRCRAFT DIVERTED TO MOT TO REFUEL. RESET CIRCUIT BREAKER FOR AUXILIARY FUEL PUMP. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001931995121500193WP 1995 12 15 9520089996 119951209A5244 DOOR DOUG DC9 DC931 3022065WP ACCESSORY COMPT NOT LATCHED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL018932E 47141 DURING CLIMB, THE FORWARD ACCESSORY COMPARTMENT DOOR LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND FORWARD ACCESSORY COMPARTMENT DOOR OPEN. SECURED DOOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001941995121500194WP 1995 12 15 9520099911 119951211A3350 EEL POWER SUPPLY DOUG DC9 DC931 3022065WP LT/RT NACELLES INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01961N 47405 DURING LINE CHECK, FOUND BOTH NACELLE EMERGENCY LIGHTS AND BOTH TAIL SLIDE LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001951995121500195WP 1995 12 15 9520109960 119951208A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01920RW 47163 DURING LINE CHECK, FOUND FORWARD ENTRY EMERGENCY AISLE LIGHTS VERY WEAK. REPLACED BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001961995121500196WP 1995 12 15 9520119977 119951208A3350 EEL POWER SUPPLY DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019341 47390 DURING LINE CHECK, FOUND AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001971995121500197WP 1995 12 15 9520129974 119951210A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019338 47347 DURING LINE CHECK, FOUND FIRST CLASS FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001981995121500198WP 1995 12 15 9520139875 119951210A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN SHORTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01784NC 48109 DURING LINE CHECK, FOUND THIRD SECTION OF EMERGENCY PROXIMITY LIGHTS INOPERATIVE. FOUND POWER SUPPLY BURNED DUE TO A SHORTED WIRE. INSULATED WIRE AND REPLACED POWER SUPPLY AND BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215001991995121500199WP 1995 12 15 9520149973 119951209A27225914387509 ACTUATOR DOUG DC9 DC931 3022065WP FUSELAGE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019337 3519835198 47346 DURING CLIMB, THE RUDDER UNRESTRICTED LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RUDDER LIMITER ACTUATOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215002001995121500200EU 1995 12 15 95UAL900309 119951211A2611 SMOKE WARNING AIRBUS320 A320232 3930326EU CARGO COMPT ACTIVATED A UALAFD ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 WP29424UA 506 GOT AN AFT CARGO SMOKE ANNUNCIATION WARNING. DISCHARGED AGENT AND RETURNED TO GATE. FIRE BOTTLE WAS REPLACED. UPON FURTHER INVESTIGATION NO SPECIFIC CAUSE COULD BE IDENTIFIED. SYSTEM OPERATIONALLY CHECKED NORMAL WITH NO FURTHER OCCURRENCES. 2L72 4F RTA28NM 19951215002011995121500201NM 1995 12 15 95UAL900310 119951212A79307584655 OIL FILTER BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE NR 2 ENGINE DIRTY A UALAD RETURN TO BLOCK J WARNING INDICATION NRNOT REPORTED 1 WP29619UA 21879 707516 RECEIVED EICAS MESSAGE NR 2 ENGINE OIL FILTER PER AMIS WRITE UP NR 2926001. THIS CONDITION OCCURRED AFTER ROLLBACK. THIS IS AFTER ENGINE START WHEN EGT ROLLS BACK. THIS COULD HAVE BEEN AFTER OR BEFORE OR DURING PUSH BACK FROM THE GATE. THE OIL FILTER WAS REPLACED ON 12/8/95. THERE HAVE NOT BEEN ANY FURTHER PROBLEMS IN THIS REGARD SINCE THAT TIME. 2L72 4F4 FRTA1NM E3NE 19951215002021995121500202NM 1995 12 15 95UAL900311 119951212A3350 EEL POWER CABLE BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE CABIN DAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29603UA 21864 EMERGENCY ESCAPE PATH LIGHTS INOP FROM ROW 10 TO COACH SECTION. REPAIRED EMERGENCY ESCAPE POWER CABLE. CHECKS O.K. 2L72 4F4 FRTA1NM E3NE 19951215002031995121500203NM 1995 12 15 95UAL900312 119951212A261218252 FIRE SENSOR BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 ENGINE INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297275U 21422 NR 3 ENGINE WOULD NOT FIRE TEST. FIREWALL TEST OKAY. ENGINE'S FIRE SENSOR REPLACED. 2L73 4F4 F A3WE E2EA 19951215002041995121500204NM 1995 12 15 95UAL900313 119951212A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297257U 21404 EMERGENCY LIGHT INOPERATIVE IN FIRST CLASS OVERHEAD. REPLACED LIGHT ASSY. 2L73 4F4 F A3WE E2EA 19951215002051995121500205SO 1995 12 15 COMA9512020 119951209A3260 UPLOCK EMB 120 EMB120RT SO LT MLG DIRTY A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01200CD 120200 WHEN LANDING GEAR SELECTED UP, LT MLG INTRANSIT LIGHTS REMAINED ON. CLEANED LT MLG UPLOCK, RETRACTION CHECK NORMAL AND ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951215002061995121500206EU 1995 12 15 COMA9531206 119951211A1420 CONNECTOR SAAB SF340 SF340A 7850100EU AUTO COARSEN LOOSE A COMACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01356CA 340A034 AUTO COARSEN SYSTEM DID NOT ARM DURING TAKE OFF. TIGHTENED WIRING CONNECTORS AT THE P3 ARMING SWITCHES. SYSTEM TEST NORMAL. 2L72 4T RTA52EU 19951215002071995121500207EU 1995 12 15 COMA9531207 119951208A3234D49408001 CONTROL ASSY SAAB SF340 SF340A 7850100EU INST PANEL MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01361CA8577 944 340A056 LANDING GEAR INTRANSIT LIGHT REMAINED ON WHEN GEAR SELECTED UP. COULD NOT DUPLICATE, REPLACED THE LANDING GEAR CONTROL ASSY FOR TROUBLESHOOTING. 2L72 4T RTA52EU 19951215002081995121500208NM 1995 12 15 P5CA9500867 119951211A2751 TRANSMITTER MNT BOEING747 747121 1384871NM LT TE FLAPS OUT OF RIG A P5CAJA DUMP FUEL UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP23830FT 19642 DURING CLIMBOUT, OUTBOARD FLAPS WOULD NOT RETRACT HYDRAULICALLY PAST APPROX 7 DEGREES. FOUND LEFT OUTBOARD TRANSMITTER MOUNT ASSY OUT OF RIG. RE-RIGGED AND REPLACED TRANSMITTER ASSY PER BOEING MAINTENANCE MANUAL 27-58-01, OPERATIONAL CHECK OK. REPLACED FLAP INDICATOR FOR OUTBOARD FLAPS PRECAUTIONARY PER M/M 27-51-00 AND 27-58-01. 2L74 4F A20WE 19951215002091995121500209NM 1995 12 15 P5CA9500868 119951210A27501176T1003 MOTOR CLUTCH BOEING747 747121 1384871NM TE FLAPS SLIPS A P5CAJA DUMP FUEL UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP23830FT 19642 DURING AIR TURN BACK FOR SPLIT FLAP, INBOARD FLAPS DID NOT WORK IN ALTERNATE WORK, OK IN NORMAL. FOUND THAT THE INBOARD FLAP ELECTRIC MOTOR CLUTCH SLIPPING REPLACED ALTERNATE FLAP MOTOR ASSY PER BOEING M/M 27-51-17. OPERATIONAL CHECK OK PER M/M 27-51-00. 2L74 4F A20WE 19951215002101995121500210NM 1995 12 15 P5CA9500869 119951210A32402660472101 ACCUMULATOR BOEING747 747121 1384871NM BRAKE FAILED A P5CAD RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 WP23831FT 19648 NR 1 AND NR 4 HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO DURING PUSHBACK. FOUND BRAKE SURGE ACCUMULATOR FAILED, REPLACED SAME IAW MM 32-41-22. SERVICED SYSTEM IAW MM 12-15-11, REPLENISHED HYDRAULIC FLUID, LEAK CHECK GOOD 2L74 4F A20WE 19951215002431995121500243SO 1995 12 15 95ZZZX6680 119951017A52804752932 HINGE 4752930 PIPER PA31 PA31350 7103110SO LT MLG DOOR BROKEN A JIKAK NONE O OTHER ININSP/MAINT 1 WP0127579 317852063 THE INBOARD MLG DOOR WAS FOUND TO HAVE A BROKEN FORWARD HINGE DURING PRE-FLIGHT. SUBMITTER STATED THIS IS THE THIRD REPORT ON THIS SAME TYPE OF FAILURE WHICH AMERIFLIGHT (JIKA) HAS SUBMITTED THIS YEAR. AIRCRAFT TOTAL TIME: 11,116 HOURS. 1L72 3O A20SO 19951215003101995121500310NE 1995 12 15 95ZZZX6696 219951117A7200 ENGINE LEAR 25 25 5170506CE GE CJ610 CJ6106 30006NE RT ENGINE FLAME OUT A BYSAB EMER. DESCENT X ENGINE FLAMEOUT CRCRUISE 1 EA09121EL142554760 010 251307 RIGHT ENGINE FLAMED OUT AT FL 370 WHEN ANTI-ICE WAS SWITCHED ON. DESCENDED TO FL 290 AND ENGINE RE-STARTED. FLIGHT CONTINUED WITH NO PROBLEMS. AFTER RETURNING TO HOME BASE, COULD NOT DUPLICATE PROBLEM. INSTALLED A LOANER ENGINE AND SENT DEFECTIVE ENGINE FOR TEST AND REPAIR AS NEEDED. 2L72 4J4 J A10CE 1E16 19951215003471995121500347EA 1995 12 15 PLG102195G2 219951021A73203033266 PY LINE BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT ENGINE CRACKED A PLGAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE05806BE UB41 32383 LGA - FLT 4727 - EN ROUTE, THE LEFT ENGINE SPOOLED TO 40 PERCENT N1. THE FLIGHT CREW SECURED THE ENGINE AND DIVERTED TO SWF LANDING WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE FOUND THE PY LINE BETWEEN THE FCU AND P3 FILTER HAD CRACKED. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4T4 TRTA24CE E4EA 19951215003481995121500348WP 1995 12 15 9520159968 119951212A3245 TIRE DOUG DC9 DC931 3022065WP NLG FLAT SPOT A NWAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL019332 47264 DURING CLIMB, AIRCRAFT FAILED TO GROUND SHIFT AND A VIBRATION WAS FELT FROM THE NOSE WHEEL. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. INSPECTED NOSE GEAR GROUND SHIFT MECHANISM. UNABLE TO FIND ANY MALFUNCTIONS IN GROUND SHIFT MECHANISM. FOUND A FLAT SPOT ON THE RIGHT NOSE TIRE WHICH CAUSED THE NOSE WHEEL VIBRATION. REPLACED THE RIGHT NOSE TIRE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215003491995121500349NM 1995 12 15 9520165513 119951211A80127755386 START VALVE BOEING757 757251 1384970NM PWA 2037 PW2037 NE LT ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01513US 157 23201 16445 DURING TAKEOFF ROLL, EICAS MESSAGE FOR L-STARTER CUTOUT ILLUMINATED. TAKEOFF WAS ABORTED AT 50 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED LEFT ENGINE STARTER VALVE. OPERATIONAL CHECK OK. 2L72 4F4 FRTA2NM E17NE 19951215003501995121500350NM 1995 12 15 9520176614 119951209A33506012111 EEL POWER SUPPLY BOEING747 747251B 1384892NM CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01614US 20359 DURING LINE CHECK, FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE AT STA 1395 AND STA 1530. REPLACED POWER SUPPLY AND BATTERY PACK. FUNCTIONAL CHECK WAS NORMAL. 2L74 4F A20WE 19951215003511995121500351WP 1995 12 15 9520189969 119951212A3350 BATTERY PACK DOUG DC9 DC931 3022065WP TAILCONE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019333 47246 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215003521995121500352WP 1995 12 15 9520199923 119951212A3350 BATTERY PACK DOUG DC9 DC932 3022066WP LT NACELLE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01927RC 47469 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215003531995121500353NM 1995 12 15 95FDEA01889 119951211A5311 FRAME BOEING727 727232 1384082NM BS 219.8 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-100-01) ON FRAME WEB BS 219.8, LBL 19-32, RBL 16-24, WL 165. CORROSION FOUND TO BE OUT OF LIMITS PER FEDEX 53-10-1. REMOVED WEB AT BS 219.8, TRIM LBL - RBL 25, FABRICATED AND INSTALLED NEW WEB IAW FEDEX SRM 51-40-2. 2L73 4F A3WE 19951215003541995121500354NM 1995 12 15 95FDEA01890 119951211A5312 BLKHD SKIN BOEING727 727232 1384082NM BS 1342 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING 7-5310-7-2301G1, FOUND DENT IN 1342 BULKHEAD SKIN APPROX WL 258 LT. REPAIRED DENT AT BS 1342 BULKHEAD, WL 258 LT. ALL WORK DONE PER FEDEX SRM 54-30-03 AND FEDEX EA 7-5310-26290. 2L73 4F A3WE 19951215003551995121500355NM 1995 12 15 95FDEA01891 119951212A5311 FRAME BOEING727 727232 1384082NM BS 560 DENTED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 DENT IN FRAME AT BS 560, LBL 38, WL 162. REPAIRED DENT IN FRAME IAW FEDEX SRM 51-40-3. C/A ADDITION. 2L73 4F A3WE 19951215003561995121500356NM 1995 12 15 95FDEA01892 119951212A5320 GUSSET BOEING727 727232 1384082NM BS 825.95 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 GUSSET AT FRAME BS 825.95 IS CRACKED, RBL 65, WL 198. REPAIR ACCOMPLISHED IAW FEDEX EO 7-5310-7-3367A1, PART 6. 2L73 4F A3WE 19951215003571995121500357NM 1995 12 15 95FDEA01893 119951211A7110 INTAKE COWL DOUG MD11 MD11F 3023600NM NR 2 ENGINE SEPARATED A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25617FE 48748 EN ROUTE FROM VANCOUVER TO MEM, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARATED FROM THE A/C RESULTING IN DAMAGE TO THE NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER. 2L73 4F RTA22WE 19951215003581995121500358NM 1995 12 15 95FDEA01894 119951213A3230 DNLOCK BUSHING BOEING727 727233 138408ANM NLG WORN A FDEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO25222FE 20933 LANDING AT MEM, PUT DOWN GEAR; MAINS GOOD BUT NOSE GEAR KEPT RED LIGHT AND NO GREEN LIGHT. RECYCLED GEAR, GOT GREEN MAINS AGAIN, AND RED NOSE GEAR LIGHT. ON GO AROUND, NOSE GEAR AND LIGHTS WENT GREEN APPROX 1 MINUTE AFTER RECYCLED GEAR. REPLACED BUSHING ON NOSE LANDING GEAR DOWNLOCK SWITCH. LUBED NOSE LANDING GEAR DOWNLOCK. CYCLED NOSE LANDING GEAR SEVERAL TIMES, OPS CHECK GOOD IAW MM 32-61-01. 2L73 4F RTA3WE 19951215003591995121500359NM 1995 12 15 95FDEA01895 119951213A5730 ACCESS PANEL BOEING727 7272S2F 1384O81NM LT NAV LIGHT MISSING A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25201FE 22924 UPPER ACCESS PANEL MISSING ON LT NAVIGATION LIGHT. INSTALLED PANEL. 2L73 4F A3WE 19951215003601995121500360NM 1995 12 15 DL72E954676 119951211A5343 TRUNNION BOEING727 727247 138408FNM NLG W/W CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27283WA 21485 CORROSION ON ATTACH POINTS FOR NLG TRUNNION AT MATING SURFACE FOR CAPS AND SURFACE WHERE BEARINGS SET. REPAIRED PER MM 53-40-0. 2L73 4F A3WE 19951215003611995121500361NM 1995 12 15 DL72S954665 119951210A3350 BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27489DA 21019 LT FORWARD EXT OVERWING EMERGENCY LIGHT OUT. REPLACED RACK OPS CHECK GOOD. 2L73 4F A3WE 19951215003621995121500362NM 1995 12 15 DL72S954666 119951129A2780 BRACKET BOEING727 727232 1384082NM NR 1 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 BRACKET CRACKED: NR 1 LE FLAP ACTUATOR INBOARD BRACKET ON FRONT SPAR IS CRACKED IN LOWER FORWARD RADIUS. REMOVED BRACKET. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER MM 57-20-21, PG 811. 2L73 4F A3WE 19951215003631995121500363NM 1995 12 15 DL72S954685 119951118A5753652163261 SPAR CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 DURING SHOP VISIT, NR 2 MIDFLAP AFT LOWER CHORD WAS FOUND TO BE CRACKED 55 INCHES FROM INBOARD END. THE CHORD WAS REPAIRED PER MM 57520. 2L73 4F A3WE 19951215003641995121500364NM 1995 12 15 DL72S954686 119951118A5753652163261 SPAR CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 DURING SHOP VISIT, THE NR 2 MIDFLAP AFT LOWER CHORD WAS FOUND CRACKED AT INBOARD AFT FLAP TRACK. THE CHORD WAS REPAIRED PER MM 57520. 2L73 4F A3WE 19951215003651995121500365NM 1995 12 15 DL72S954687 119951118A5753652163261 SPAR CHORD BOEING727 727232 1384082NM NR 2 TE MIDFLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27516DA 21432 DURING SHOP VISIT, THE NR 2 MIDFLAP AFT CHORD WAS FOUND CRACKED AT CUTOUT FOR INBOARD AFT FLAP DRIVE ROD. THE CHORD WAS REPAIRED PER MM 57520. 2L73 4F A3WE 19951215003661995121500366NM 1995 12 15 DL72W954680 119951120A5754 SKIN 656221100 BOEING727 727247 138408FNM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272815W BN1053 20871 UPON INITIAL INSPECTION, CRACK FOUND IN NR 5 SLAT SKIN UNDER AIR FENCE. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951215003671995121500367NM 1995 12 15 DL73E954677 119951203A5321 FLOOR PANEL BOEING737 737247 138448DNM BS 500-520 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27242WA 23516 AT HMV INSPECTION, FOUND THE FORWARD B/B LT FIXED FLOOR PANEL CORRODED AT STA 500-520. CORRECTION: REMOVED FIXED FLOOR. REPLACED FIXED FLOOR. INSTALLED FIXED FLOOR PANEL. 2L72 4F A16WE 19951215003681995121500368NM 1995 12 15 DL757954679 119951211A3350 BATTERY PACK BPS73 BOEING757 757232 1384965NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27608DA 5485 22815 FOUND ON T/S CK - FIRST CLASS EMERGENCY TRACK LIGHTING INOP. CORRECTIVE ACTION - REPLACED M731 POWER SUPPLY AND BATTERY PACK. 2L72 4F RTA2NM 19951215003691995121500369NE 1995 12 15 DL76L954663 219951210A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 2 MALFUNCTIONED A DALAK NONE O OTHER ININSP/MAINT 1 SO27175DN21168 24803 724165 PERFORMED ENGINE STABILITY RUN, FOUND LOW STALL MARGIN. ENGINE WAS REMOVED AND ROUTED TO SHOP FOR COMPLETION OF EO SI-690053. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS 2L72 4F4 FRTA1NM E24NE 19951215003701995121500370WP 1995 12 15 DLL17954678 119951211A33500L3071BPEGPL EEL LENS LKHEED1011 10113853 5265020WP CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27767DA 193H1209 EMERGENCY TRACK LIGHT BROKEN AT SEAT 23C. 2L73 4F A23WE 19951215003711995121500371NM 1995 12 15 DLM11954664 119951211A3350 MODULE 0105606203 DOUG MD11 MD11 3023602NM PWA 4060 PW4060 52119NE EMERGENCY LIGHTSSHORTED A DALAK NONE L NO TEST TXTAXI/GRND HDL 1 SO27801DE 48472 724165 LEFT EMERGENCY TRACK LIGHTS F/C CABIN INOP. REPLACED SHORTED LT MODULE ASSY OPS CK NORMAL. 2L73 4F4 FRTA22WE E24NE 19951215003721995121500372NM 1995 12 15 DLM88954681 119951211A335061020 BATTERY DOUG MD88 MD88 3023688NM AFT GALLEY DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27959DL 49978 EMERGENCY FLASHLIGHT AT AFT GALLEY INOP. NO MRR. REJECTED 12-12-95, GT 595. 2L72 4F RTA6WE 19951215003731995121500373NM 1995 12 15 DLM90954689 119951211A2910 HYD TUBE DOUG MD90 MD9030 3023690NM FS 1322 LEAKING A DALAO OTHER K FLUID LOSS ININSP/MAINT 1 SO27904DA 53384 IR - L-SYSTEM HYD QTY READS 8 QTS. ON WALK-AROUND, SAW FLUID LEAKING FROM 2 DRAIN HOLES AFT OF MAIN GEAR. FOUND FWD PRESS LINE TO EMPENNAGE RUBBED THROUGH ON OUTFLOW VALVE ACTUATOR AT LT FS 1322. REVERSED BOLTS TO GAIN CLEARANCE AND MADE PERMANENT REPAIR TO LINE WITH RING LOCK. 2L72 4F RTA6WE 19951215003741995121500374WP 1995 12 15 MWEA95476 119951211A53305911410175 SKIN DOUG DC9 DC932 3022066WP BS 300-337 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A TEMPORARY EXTERNAL SKIN REPAIR AT STA 300 THRU 337, LONGERONS 24L-25L. INSTALLED A REPAIR PER ME DRAWING NR 53-149 AND DAC TELEX ORD-SVC-03001/JSS. 2L72 4F A6WE 19951215003751995121500375WP 1995 12 15 MWEA95477 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 167-193 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A TEMPORARY CLASS 3 REPAIR INSTALLED TO FUSELAGE SKIN CRACKED AT STA 167 AND 193 AT LONGERON 22L. FABRICATED A REPAIR AND INSTALLED PER SRO 9530219. 2L72 4F A6WE 19951215003761995121500376WP 1995 12 15 MWEA95478 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 190-229 CREASED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THAT THE FUSELAGE SKIN HAS A 40 INCH CREASE AT STA 190 - 229 NEAR LONGERON 24R. COLD FORMED THE DENT PER SRM 53-04, FIG 38, AND INSTALLED A DOUBLER IAW DAC TELEX. 2L72 4F A6WE 19951215003771995121500377WP 1995 12 15 MWEA95479 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 996 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE AFT FUSELAGE SKIN AT STA 996 AND LONGERON 23L CRACKED .3750 INCH FROM EDGE OF SKIN TO FASTENER HOLE. FABRICATED INTERNAL AND EXTERNAL DOUBLERS, A FILLER, CLEANED CORROSION AND INSTALLED IAW SRM 53-04 AND 53-01, PG 8. 2L72 4F A6WE 19951215003781995121500378WP 1995 12 15 MWEA95480 119951211A532099115151339 ANGLE DOUG DC9 DC932 3022066WP BS 160 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND TWO CRACKED ANGLES AT STA 160, LONGERON 28L AND 28R VISIBLE THROUGH INSP LIGHTENING HOLES IN E/E DOOR JAMB AFT CORNERS. INSTALLED TWO NEW SHEAR TIES IAW SRM 51-30. 2L72 4F A6WE 19951215003791995121500379WP 1995 12 15 MWEA95481 119951211A57535914872503J FITTING DOUG DC9 DC932 3022066WP LT FLAP CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT FLAP INBOARD FLAP HINGE FITTING INTERNAL FITTING FOR ATTACHMENT OF THE HINGE CRACKED. INSTALLED A NEW FITTING IAW SRM 57-09, PAR 14. 2L72 4F A6WE 19951215003801995121500380WP 1995 12 15 MWEA95482 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 229-589 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THAT THE FUSELAGE FORWARD LOWER SKIN HAS MULTIPLE DENTS AND PULLED RIVETS FROM STA 229 TO 589 FROM LONGERON 26L TO 26R. REPLACED THE FORWARD LOWER SKIN IAW SRM 51-30. 2L72 4F A6WE 19951215003811995121500381WP 1995 12 15 MWEA95483 119951211A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE FUSELAGE SKIN IN FRONT OF THE FORWARD CARGO DOOR AND AROUND THE STATIC PORT AREA HAS MULTIPLE DENTS THAT ARE OUT OF SRM LIMITS. INSTALLED A NEW SKIN PANEL IAW SRM 51-30 FROM STA 229-589, LONGERON 18R-26R. 2L72 4F A6WE 19951215003821995121500382WP 1995 12 15 MWEA95484 119951211A5230 DOUBLER DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE AFT CARGO DOOR REPAIR WAS CRACKED ON THE FORWARD SIDE AT THE BAYONET. FABRICATED A DOUBLER PER SRM 51-10 AND INSTALLED IAW SRM 51-30. 2L72 4F A6WE 19951215003831995121500383WP 1995 12 15 MWEA95485 119951211A532059101577 PAN DOUG DC9 DC932 3022066WP AFT CARGO DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO DOOR BOTTOM PAN CRACKED IN TWO AREAS. REPAIRED PAN PER SERVICE RE-WORK DRAWING NR 5934142. 2L72 4F A6WE 19951215003841995121500384WP 1995 12 15 MWEA95486 119951211A5320J0602283 PAN DOUG DC9 DC932 3022066WP FWD CARGO DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND FORWARD CARGO DOOR SILL PAN CORRODED. SPLICED IN A NEW SECTION OF FORWARD CARGO DOOR PAN IAW SRM 53-05, FIG 44. 2L72 4F A6WE 19951215003851995121500385WP 1995 12 15 MWEA95487 119951211A5312 BLKHD CLIP DOUG DC9 DC932 3022066WP BS 996 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A CLIP CRACKED IN THE RT LAV PRESSURE BULKHEAD AT Z34, STA 996. FABRICATED A NEW CLIP IAW THE SRM 53-01 AND INSTALLED IAW SRM 51-30. 2L72 4F A6WE 19951215003861995121500386WP 1995 12 15 MWEA95488 119951211A27204912110501 BRACKET DOUG DC9 DC932 3022066WP RUDDER DAMPER CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LOWER RUDDER DAMPER IDLER ARM MOUNT BRACKET HAD HEAVY CORROSION. REPLACED BRACKET IAW MM 20-16-0. 2L72 4F A6WE 19951215003871995121500387WP 1995 12 15 MWEA95489 119951211A57533914981503 FITTING DOUG DC9 DC932 3022066WP LT TE FLAP CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT FLAP TRACK LOWER ATTACH FITTING IS CRACKED. DRILLED UP AND INSTALLED NEW FITTING IAW SRM 51-30. 2L72 4F A6WE 19951215003881995121500388WP 1995 12 15 MWEA95490 119951211A5313591141899 LONGERON DOUG DC9 DC932 3022066WP BS 658-676 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LIGHT CORROSION AND BARE METAL ALONG LONGERON 29L IN KEEL AREA AT STA 658-676. A NEW LONGERON WAS INSTALLED IAW SRM 51-10-3. 2L72 4F A6WE 19951215003891995121500389WP 1995 12 15 MWEA95491 119951211A53135911418101 LONGERON DOUG DC9 DC932 3022066WP KEEL AREA CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LIGHT CORROSION ON LONGERON 29R IN KEEL AREA UNDER THE AUXILIARY HYD RESERVOIR AND ON KEEL WEB. NEW LONGERON WAS INSTALLED IAW SRM 51-10-3. 2L72 4F A6WE 19951215003901995121500390WP 1995 12 15 MWEA95492 119951211A5230 PAN DOUG DC9 DC932 3022066WP CARGO DOOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO DOOR PAN LOWER SECTION CORRODED. REPAIRED THE LOWER DOOR PAN SECTION IAW SRM 53-05, FIG 44. 2L72 4F A6WE 19951215003911995121500391WP 1995 12 15 MWEA95493 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 917 CORROSION A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO OPENING UNDER EXTERNAL SCUFF PLATE AT STA 917 SKIN AND INTERNAL DOUBLER HAVE CORROSION BULGE BETWEEN LAYERS. FABRICATED DOUBLER AND INSTALLED IAW ROD SKETCH 95-11-06-007. 2L72 4F A6WE 19951215003921995121500392WP 1995 12 15 MWEA95494 119951211A5320 DOUBLER DOUG DC9 DC932 3022066WP BS 325 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND ANTENNA SUPPORT DOUBLER AT STA 325 BETWEEN LONGERON 30L AND 29L CORRODED BEYOND LIMITS. FABRICATED A NEW DOUBLER PER SRM 53-01, PG 1 AND INSTALLED PER SRM 51-30. 2L72 4F A6WE 19951215003931995121500393WP 1995 12 15 MWEA95495 119951211A53205911412115 DOUBLER DOUG DC9 DC932 3022066WP BS 341 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE RT ALTERNATE STATIC PORT SUPPORT DOUBLER AT STA 341 BETWEEN LONGERONS 26R AND 27R WAS CORRODED BEYOND LIMITS. INSTALLED A NEW STATIC PORT DOUBLER IAW SRM 51-30. 2L72 4F A6WE 19951215003941995121500394WP 1995 12 15 MWEA95496 119951211A53209919402506N TRAPEZOID PANEL DOUG DC9 DC932 3022066WP BS 718 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND SEVERE CORROSION IN THE RT TRAPEZOIDAL PANEL AT STA 718 AROUND THE TWO OUTBOARD TOP AFT BOLT HOLES. REPLACED THE TRAPEZOIDAL PANEL IAW SRM 51-30 AND 57-04, FIG 34. 2L72 4F A6WE 19951215003951995121500395WP 1995 12 15 MWEA95497 119951211A532059114237N INTERCOSTAL DOUG DC9 DC932 3022066WP BS 465-484 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND VHF COMM ANTENNA INTERCOSTAL SUPPORT FROM STA 465 TO 484 BETWEEN LONGERON 29L AND 30L WITH VARIOUS AREAS OF VISIBLE MILD CORROSION. INSTALLED A NEW INTERCOSTAL IAW SRM 51-30. 2L72 4F A6WE 19951215003961995121500396WP 1995 12 15 MWEA95498 119951211A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 427-446 DENTED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND INTERCOSTAL BETWEEN STA 427 AND 446 AT LONGERON 29L HAS VARIOUS AREAS OF MILD CORROSION BEYOND LIMITS. FABRICATED A NEW INTERCOSTAL IAW 53-11-2 AND INSTALLED PER SRM 53-01. 2L72 4F A6WE 19951215003971995121500397WP 1995 12 15 MWEA95499 119951211A5320591014221 DOOR JAMB DOUG DC9 DC932 3022066WP BS 370/427 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND FORWARD CARGO DOOR OPENING JAMB AT STA 370 AND 427 CRACKED AT AFT STOP. REPLACED DOOR JAMB IAW SRM 51-30. 2L72 4F A6WE 19951215003981995121500398WP 1995 12 15 MWEA95500 119951211A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 218 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 21R HAS CORROSION JUST AFT OF STA 218 FRAME. REPLACED LONGERON SECTION IAW SRM 51-30. 2L72 4F A6WE 19951215003991995121500399WP 1995 12 15 MWEA95501 119951211A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 237-256 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 21R HAS LIGHT CORROSION LOCATED BETWEEN STA 237 AND 256. REPLACED THE LONGERON SECTION IAW SRM 51-30. 2L72 4F A6WE 19951215004001995121500400WP 1995 12 15 MWEA95502 119951211A5311 FRAME DOUG DC9 DC932 3022066WP AFT ACCESS COMPTCORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND CORROSION ON CANTED FRAME RT SIDE AFT ACCESSORY COMPARTMENT BEHIND FDR. FABRICATED REPAIR PARTS AND INSTALLED PER 53-01, FIG 2, SHEET 4. 2L72 4F A6WE 19951215004011995121500401WP 1995 12 15 MWEA95503 119951211A524839251342 FITTING DOUG DC9 DC932 3022066WP VENTRAL DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE VENTRAL DOOR TOP RIGHT STOP FITTING WAS CRACKED. INSTALLED A NEW FITTING IAW SRM 50-2-0, PAGE 1. 2L72 4F A6WE 19951215004021995121500402WP 1995 12 15 MWEA95504 119951211A52489915565 ANGLES DOUG DC9 DC932 3022066WP VENTRAL DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE VENTRAL DOOR ANGLES UPPER AND LOWER AT THE TOP FIXED BAYONET ARE CRACKED. INSTALLED NEW ANGLES IAW SRM 51-30-2. 2L72 4F A6WE 19951215004031995121500403WP 1995 12 15 MWEA95505 119951211A52489915565 ANGLES DOUG DC9 DC932 3022066WP VENTRAL DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE VENTRAL DOOR ANGLES UPPER AND LOWER AT MIDPOINT BETWEEN THE FIXED BAYONETS ARE CRACKED. INSTALLED NEW ANGLES IAW SRM 51-30-2. 2L72 4F A6WE 19951215004041995121500404WP 1995 12 15 MWEA95506 119951211A52489915565137 ANGLE DOUG DC9 DC932 3022066WP VENTRAL DOOR CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE VENTRAL DOOR PAN AT MIDPOINT BETWEEN THE FIXED BAYONETS IS CRACKED COMING FROM UNDER THE ANGLE INSIDE. REPAIRED THE CRACKED PAN IAW SRM 52-01 AND 51-30-2. 2L72 4F A6WE 19951215004051995121500405WP 1995 12 15 MWEA95507 119951211A53209919402503N FITTING DOUG DC9 DC932 3022066WP LT MLG WW CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE LEFT TRAPEZOIDAL PANEL LOWER SUPPORT FITTING CRACKED. REPLACED THE SUPPORT FITTING PER SRM 51-30. 2L72 4F A6WE 19951215004061995121500406WP 1995 12 15 MWEA95508 119951211A53205920302509 FITTING DOUG DC9 DC932 3022066WP BS 756 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29R END FITTING AT STA 756 HAS EXFOLIATION CORROSION. DRILLED UP AND INSTALLED LONGERON IAW SRM 51-30 AND SRM 51-10-4. 2L72 4F A6WE 19951215004071995121500407WP 1995 12 15 MWEA95509 119951211A532039146751 FITTING DOUG DC9 DC932 3022066WP BS 897-917 EXFOLIATED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE AFT CARGO COMPARTMENT LONGERON 22L SPLICE FITTING HAS SEVERE EXFOLIATION CORROSION AT STA 897-STA 917. INSTALLED A NEW FABRICATED PART PER SRM 53-01. 2L72 4F A6WE 19951215004081995121500408WP 1995 12 15 MWEA95510 119951211A532099155617 SUPPORT DOUG DC9 DC932 3022066WP BS 996 CORROSION A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND CENTER VERTICAL SUPPORT LOWER END EXTENSIVELY CORRODED ABOVE AFT FUSELAGE JACK SUPPORT AT STA 996. REPLACED THE HAT SECTION IAW SRM 51-10-4. 2L72 4F A6WE 19951215004091995121500409WP 1995 12 15 MWEA95511 119951211A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 389 DAMAGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE FLOOR BEAM AT STA 389 HAS A DIME-SIZED HOLE IN THE LOWER FLANGE AND RADIUS LOCATED NEAR THE CENTER OF THE BEAM. FABRICATED AND INSTALLED THE REPAIR IAW SRM 53-05, FIG 86. 2L72 4F A6WE 19951215004101995121500410WP 1995 12 15 MWEA95512 119951211A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BA 408 GOUGE A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THAT THE FLOOR BEAM AT STA 408 HAS STRUCTURAL DAMAGE IN THE FORM OF A GOUGE IN THE LOWER FLANGE AND RADIUS LOCATED NEAR CENTER OF BEAM. FABRICATED AND INSTALLED REPAIR IAW SRM 53-05, FIG 86. 2L72 4F A6WE 19951215004111995121500411WP 1995 12 15 MWEA95513 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 370-389 GOUGED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A GOUGE APPROX .031 INCH ON THE INNER SKIN LOCATED BETWEEN STA 370 AND STA 389 JUST UNDER LONGERON 18R. INSTALLED A NEW SKIN PANEL IAW SRM 51-30. 2L72 4F A6WE 19951215004121995121500412WP 1995 12 15 MWEA95514 119951211A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 889-897 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO COMPARTMENT STRUCTURE DOOR JAMB INTERCOSTAL GUSSET PLATE HAS EXTENSIVE CORROSION AT STA 889-STA 897, LONGERON 29R. FABRICATED A NEW INTERCOSTAL IAW SRM 51-10-4. INSTALLED ATTACH CLIP AND INTERCOSTAL PER SRM 51-30. 2L72 4F A6WE 19951215004131995121500413WP 1995 12 15 MWEA95515 119951211A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 889-897 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND AFT CARGO DOOR JAMB INTERCOSTAL AT LONGERON 28R HAS MODERATE CORROSION AT LOWER FLANGE STA 889-STA 897. FABRICATED NEW INTERCOSTAL PER SRM 51-10-4 AND INSTALLED PER SRM 53-01. 2L72 4F A6WE 19951215004141995121500414WP 1995 12 15 MWEA95516 119951211A5330 SKIN DOUG DC9 DC932 3022066WP BS 683-686 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A 1.1250 INCH CRACK IN SKIN RADIUS ON FORWARD END OF KEEL SKIN ATTACH ANGLE AT STA 683-STA 686 AT XCW10. FABRICATED AND INSTALLED A NEW SKIN IAW SRM 51-30. 2L72 4F A6WE 19951215004151995121500415WP 1995 12 15 MWEA95517 119951211A55204918019501 BRACKET DOUG DC9 DC932 3022066WP RT ELEVATOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THAT THE RIGHT ELEVATOR NR 4 HINGE BRACKET AT STA XE225 HAS SPOTS OF CORROSION OUT OF LIMITS. INSTALLED NEW BRACKET IAW SB 55-31, FIG 3 AND MM 20-16-0. 2L72 4F A6WE 19951215004161995121500416WP 1995 12 15 MWEA95518 119951211A55204918019 BRACKET DOUG DC9 DC932 3022066WP LT ELEVATOR CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THE LEFT ELEVATOR NR 4 HINGE BRACKET AT STA XE225 HAS SPOTS OF MODERATE CORROSION OUT OF LIMITS. INSTALLED A NEW BRACKET IAW MM 20-16-0. 2L72 4F A6WE 19951215004171995121500417WP 1995 12 15 MWEA95519 119951211A5320 DOUBLER DOUG DC9 DC932 3022066WP BS 908 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND A CRACK IN THE AFT CARGO DOOR FLOOR PAN AT STA 908. INSTALLED A REPAIR IAW SRM 53-01, FIG 2, SHEET 4. 2L72 4F A6WE 19951215004181995121500418WP 1995 12 15 MWEA95520 119951211A5320S2912282 CHANNEL DOUG DC9 DC932 3022066WP BS 129-160 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND FLOOR PANEL CORRODED RT SIDE STA 120-STA 160. REPLACED MOST OUTBOARD HAT CHANNEL IAW SRM 53-01. 2L72 4F A6WE 19951215004191995121500419WP 1995 12 15 MWEA95521 119951211A53135914258502 LONGERON DOUG DC9 DC932 3022066WP BS 730 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND RT LONGERON 20 OUTBOARD MEMBER TO BE CORRODED TO EXCESS IN ONE BOLT HOLE AND ALONG THE RADIUS OF THE ANGLE AT STA 730. REPLACED THE OUTBOARD LONGERON MEMBER IAW SRM 51-30. 2L72 4F A6WE 19951215004201995121500420WP 1995 12 15 MWEA95522 119951211A5320591141853 ANGLE DOUG DC9 DC932 3022066WP BS 699-750 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND MODERATE CORROSION EVIDENT ALONG INBD EDGE OF LT WHEELWELL CUTOUT BEHIND INBD DOOR HINGE ON STRUCTURE FROM STA 699-STA 750. INSTALLED NEW ANGLE IAW SRM 51-30. 2L72 4F A6WE 19951215004211995121500421WP 1995 12 15 MWEA95523 119951211A5330 WEB DOUG DC9 DC932 3022066WP LT MLG WW CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND MODERATE CORROSION AT VARIOUS LOCATIONS ALONG AFT WALL OF LT WHEELWELL WEB SKIN. REPLACED THE WEB SKIN AND T-FITTING IAW SRM 53-03, FIG 17. 2L72 4F A6WE 19951215004221995121500422WP 1995 12 15 MWEA95524 119951211A53209919402505 FITTING DOUG DC9 DC932 3022066WP LT MLG WW CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LIGHT CORROSION IN SEVERAL PLACES ON INBD SURFACE OF TRAPEZOIDAL FITTING BEHIND THE REMOVED SKI FITTING IN THE LT WHEELWELL. FOUND THE TRAPEZOIDAL FITTING TO BE CRACKED AND REPLACED IT IAW SRM 57-09, FIG 34 AND 51-30. 2L72 4F A6WE 19951215004231995121500423WP 1995 12 15 MWEA95525 119951211A53203920595501 FITTING DOUG DC9 DC932 3022066WP BS 570 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 28R END FITTING AT STA 570 IS CRACKED. INSTALLED A NEW END FITTING IAW SRM 51-30. 2L72 4F A6WE 19951215004241995121500424WP 1995 12 15 MWEA95526 119951211A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 200-218 CORROSION A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND INTERCOSTAL AT LONGERON 26R HAS CORROSION FROM STA 200-STA 218 ON BOTH SURFACES IN E/E COMPARTMENT. FABRICATED A NEW INTERCOSTAL IAW SRM 53-01, PAGES 1 AND 51-60. INSTALLED INTERCOSTAL IAW SRM 53-03, PAGE 1. 2L72 4F A6WE 19951215004251995121500425WP 1995 12 15 MWEA95527 119951211A53203924810501 FITTING DOUG DC9 DC932 3022066WP BS 573-604 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LONGERON 26L END FITTING FROM STA 573 TO STA 604 HAD EXCESSIVE CORROSION AROUND NUTPLATE HOLE AT AFT END. INSTALLED A NEW FITTING IAW SRM 53-01, PG 1. 2L72 4F A6WE 19951215004261995121500426WP 1995 12 15 MWEA95528 119951211A53203920595501 FITTING DOUG DC9 DC932 3022066WP BS 565-586 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND THAT LONGERON 27R END FITTING AT STA 565 AND STA 586 IS CRACKED. INSTALLED A NEW END FITTING IAW SRM 51-30. 2L72 4F A6WE 19951215004271995121500427WP 1995 12 15 MWEA95529 119951211A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP BS 180 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND IN E/E COMPARTMENT INTERCOSTAL AT STA 180 AND LONGERON 22L HAS CORROSION. FABRICATED INTERCOSTAL AND INSTALLED IAW SRM 53-01, PG 1. 2L72 4F A6WE 19951215004281995121500428WP 1995 12 15 MWEA95530 119951211A2560 GIRT BAR LATCH DOUG DC9 DC932 3022066WP FWD ENTRY FOULED A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31302ME 47102 CREW REPORTS FORWARD ENTRANCE DOOR EVACUATION SLIDE IS DIFFICULT TO DISARM. TRIMMED CARPET AROUND FORWARD GIRT BAR LATCH. 2L72 4F A6WE 19951215004291995121500429NE 1995 12 15 P5CA9500870 219951210A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE NR 3 BIRD STRIKE A P5CAK NONE C F.O.D. APAPPROACH 1 WP23859FT66665760 20326 695755 AT 7500 FEET WHILE BEING VECTORED FOR APPROACH AT NIGHT ENCOUNTERED BIRD FLOCK, HAD MULTIPLE BIRD STRIKES. WEATHER CONDITIONS, SCATTERED BROKEN LAYERS. NO ABNORMAL ENGINE OR FLIGHT INSTRUMENT INDICATIONS NOTED, NORMAL APPROACH AND LANDING FOLLOWING BIRD STRIKE. ON INSPECTION, FOUND NR 3 ENGINE DAMAGED BEYOND LIMITS, REPLACED SAME IAW PAC WORKCARDS M7100-002, M7100-002A. FOUND NR 4 NOSE COWL DAMAGED, REPLACED IAW 71-11-01. REPAIRED DAMAGE TO SECTION 41 RIBS IAW 53-12, REPAIRED DAMAGE TO WING L/E IAW 57-31. 2L74 4F4 F A20WE E20EA 19951215004301995121500430NM 1995 12 15 P5CA9500871 119951212A2820 CIRCUIT BREAKER BOEING747 747122 1384872NM NR 1 BOOST PUMP FAILED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23852FT 19757 ON TAXI OUT, NR 1 MAIN FORWARD BOOST PUMP LOW PRESSURE LIGHT AND NR 4 MAIN AFT BOOST PUMP LOW PRESSURE LIGHT CAME ON. FOUND CIRCUIT BREAKERS AT FAULT, REPLACED SAME IAW MM 28-22-01. BOOST PUMPS OPS CHECKS NORMAL. 2L74 4F A20WE 19951215004311995121500431NM 1995 12 15 SCNA95282 119951207A5320 ANGLE BOEING727 7272A1 138407FNM BS 1010 CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15286SC 21601 DURING HEAVY MAINTENANCE VISIT, FOUND AFT CARGO SUPPORT ANGLE CRACKED AT STATION 1010, STRINGERS 26L TO 28L. FABRICATED AND INSTALLED REPAIR ANGLE IAW B727 SRM 53-10-04. 2L73 4F A3WE 19951215004321995121500432WP 1995 12 15 SCNA95283 119951206A5330 SKIN DOUG DC10 DC1015 3022118WP BS 1902 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15151SY 48295 DURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN WAS FOUND BULGING WITH A PULLED FASTENER AT FRAME STATION 1902 BETWEEN LONGERONS 45R AND 48R. THE CAUSE OF THE BULGING SKIN WAS ATTRIBUTED TO CORROSION BETWEEN THE FUSELAGE SKIN AND THE UNDERLYING TITANIUM TEARSTRAP. THE DAMAGED SKIN WAS CUTOUT, A FILLER AND DOUBLER INSTALLED PER DC-10 SRM, VOL 1, CH 53-20-00, FIG 6. 2L73 4F A22WE 19951215004331995121500433WP 1995 12 15 SCNA95284 119951204A5230 PAN DOUG DC10 DC1015 3022118WP AFT CARGO DOOR CRACKED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15151SY 48295 DURING A SCHEDULED INSPECTION, THE AFT CARGO DOOR WAS FOUND WITH A .75 INCH CRACK IN THE AFT DOOR PAN. THE CRACK EXTENDED FROM AN EXISTING FASTENER HOLE TO THE AFT EDGE OF THE PAN. THE DAMAGE WAS CUTOUT, A FILLER AND DOUBLER INSTALLED PER DC-10 SRM, VOL 1 CH 52-10-00, FIGURE 7. 2L73 4F A22WE 19951215004341995121500434NE 1995 12 15 SCNA95285 219951204A7261699151 OIL SCREEN BOEING727 7272J4 1384006NM PWA JT8 JT8D217C 52053NE NR 1 ENGINE FAULTY A SCNACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL15284SC 21438 THE NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKEOFF, ABORTED TAKEOFF. REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL SCREEN. 2L73 4F4 FRTA3WE E9NE 19951215004351995121500435NM 1995 12 15 SCNA95286 119951211A335058731 EEL TRACK BOEING727 727259 138408JNM CABIN FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOPERATIVE IN THE AFT CABIN. REMOVED AND REPLACED SHORTED LUMINESCENT FLOOR TRACK LIGHTING STRIP, OPS CHECKED NORMAL. 2L73 4F A3WE 19951215004361995121500436NM 1995 12 15 SWAA950776 119951212A5314 KEEL BEAM BOEING737 7372H4 138448CNM BS 947 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND TOP OF FLOOR BEAM CHORD CORRODED AT BS 947, WL 208, RBL 55 TO LBL 55. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951215004371995121500437NM 1995 12 15 SWAA950777 119951212A5330 SKIN BOEING737 7372H4 138448CNM BS 907 DENTED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN DENTED AT BS 907, BETWEEN STRINGERS 22 AND 23L AND AT BS 940 AT S18 AND 19L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951215004381995121500438NM 1995 12 15 SWAA950778 119951212A5330 SKIN BOEING737 7372H4 138448CNM BS 713 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AT BS 713, LBL 24.5, WL 204. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951215004391995121500439NM 1995 12 15 SWAA950779 119951212A5320 WEB BOEING737 7372H4 138448CNM BS 178 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND PRESSURE WEB CRACKED AT BS 178, WL 217, RBL 9.5 TO 13. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951215004401995121500440NM 1995 12 15 SWAA950780 119951212A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 928 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 928, RBL 14-55, WL 208. REPAIRED PER SWA RA 1-253-423. 2L72 4F A16WE 19951215004411995121500441NM 1995 12 15 SWAA950781 119951212A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 294 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 294, RBL 14 TO LBL 14, WL 208. REPAIRED PER SWA TR 1-353-009. 2L72 4F A16WE 19951215004421995121500442NM 1995 12 15 SWAA950782 119951212A5313 STRINGER BOEING737 7372H4 138448CNM BS 1006 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0780SW 22675 DURING SCHEDULED MAINTENANCE, FOUND STRINGER 27L CORRODED AT BS 1006. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951215004451995121500445EU 1995 12 15 95ZZZX6736 119950925A3211 FLANGE RIVETS BNORM BN2 BN2A26 1520226EU MLG ATTACH SHEARED A ADCRAK NONE O OTHER TXTAXI/GRND HDL 1 WP1329MR 6988 885 DURING TAXI, THE MLG ATTACHMENT FLANGE RIVETS SHEARED ALLOWING THE MLG ASSY TO ROTATE IN THE UNDERCARRIAGE LEG TUBE. FURTHER INSPECTION ON RT MLG REVEALED LOOSE RIVETS. BRITTEN NORMAN SB 191 TALKS OF PRODUCT IMPROVEMENT BY ADDING 6 ADDITIONAL RIVETS IN THE FLANGE AND TUBE ASSY. FURTHER INSPECTION OF ALL COMPANY AIRCRAFT REVEALED NO DEFECTS. 1H72 3O A17EU 19951215004471995121500447SO 1995 12 15 95ZZZX6738 119951107A5740 ATTACH FITTING PIPER PA32 PA32300 7103212SO WING AFT CORRODED A AETVAK NONE O OTHER ININSP/MAINT 1 SW21419PH4085 327940039 CHECKED SB 977 (PIPER DATED 12-12-94). REAR STEEL WING ATTACH FITTING CORROSION INSPECTION, FOUND ON THIS ACFT THERE WAS SEVERE CORROSION. REQUIRED THE REPLACEMENT OF THE STEEL ATTACHING PARTS. 1L71 3O A3SO 19951215004521995121500452SO 1995 12 15 95ZZZX6743 219950901A8530649317RB CYLINDER CESSNA207 T207 2073612CE CONT O520 TSIO520M 17040SO HEAD CRACKED A GBWAK NONE O OTHER ININSP/MAINT 1 NM111599U 1339 20700199 511722 INSPECTION FOUND CYLINDER HEAD WAS SUBSTANTIALLY CRACKED FROM BOTTOM SPARK PLUG HOLE TO TOP SPARK PLUG HOLE THROUGH THE EXHAUST PORT. SUBMITTER STATED THIS IS THE FIFTH (OUT OF SIX) THAT HAVE HAD TO BE REPLACED SINCE ENGINE OVERHAUL (1,339 HOURS AGO) DUE TO HEAD CRACKS AND CYLINDERS WERE EC1 CERMISTEEL WITH IFR HEAD TREATMENT. 1H71 3O3 O A16CE E8CE 19951215004841995121500484EA 1995 12 15 95ZZZX6775 219951114A7414D6LN3000 MAGNETO PIPER PA32 PA32RT300 7103215SO LYC O540 IO540K1G5 41532EA FLANGE WORN A ALHOAK NONE O OTHER ININSP/MAINT 1 EA053421W400 32R7885276 MAGNETO FLANGE WEAR. A D6LN-3000 (DUAL MAGNETO) WAS FOUND TO HAVE ITS BASE CLAMPS SECURED. HOWEVER, THE MAGNETO WAS ABLE TO CHAFE BETWEEN THE FLANGE AND THE HOLD-DOWN CLAMP. THIS CAUSED A WEAR PATTERN THE SHAPE OF THE 'MOUSE EAR CLAMP', PN 66M19385, INTO THE FLANGE OF THE MAG. A SECOND MAG (ANOTHER ACFT) WAS CHECKED, IT, TOO, HAD FLANGE WEAR. FLANGES WERE MEASURED, FOUND TO BE .300 INCH-.318 INCH. THE GRIP OF PN 66M19385 IS .365 INCH AS SAMPLED. EVEN WITH A .015 INCH GASKET, IT STILL DOES NOT PROVIDE MAG FLANGE WEAR. ADEQUATE PRESSURE. REPLACEMENT MAG FLANGE MEASURED .365 INCH. SUBMITTER SUGGESTS ONLY EARLIER 'STAMPED' MAG CLAMPS BE USED WITH THINNER FLANGE MAGNETOS. 1L71 3O3 O A3SO 1E4 19951215004891995121500489NM 1995 12 15 9520206303 119951212A3350 BATTERY PACK BOEING747 747451 1384940NM UPPER DECK DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01663US 23818 DURING LINE CHECK, THE UPPER DECK FORWARD FLOOR EMERGENCY LIGHTS AND LEFT DOOR LIGHTS WERE FOUND INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACKS FOR FLOOR TRACK LIGHTING AND UPPER DECK DOOR. OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951215004901995121500490 1995 12 15 9520219603 419951213A2312 VHF TRANSCEIVED DOUG DC9 DC932 3022066WP NR 1 SYST FAILED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01603NW 47101 DURING CLIMB, THE NR 1 VHF COMM FAILED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 NAV COMM CONTROL PANEL AND VHF TRANSCEIVER. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951215004911995121500491EU 1995 12 15 9520223239 119951213A2810568127202002 FUEL TANK AIRBUS320 A320211 3930320EU LEFT CONTAMINATED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01339NW 367 DURING TAKEOFF ROLL, THE LEFT WING FUEL BOOST PUMPS LOW PRESSURE WARNING LIGHTS ILLUMINATED. TAKEOFF WAS ABORTED AT APPROXIMATELY 60 KNOTS. MAINTENANCE REMOVED ICE AND WATER IN LEFT FUEL TANK. ALSO, SUMPED THE CENTER AND RIGHT TANKS AS WELL. 2L72 4F RTA28NM 19951215004921995121500492EU 1995 12 15 9520233240 119951213A2810568127202002 FUEL TANK AIRBUS320 A320211 3930320EU LEFT COMTAMINATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01340NW 372 DURING CLIMBOUT, BOTH LEFT WING FUEL BOOST PUMPS LOW PRESSURE WARNING LIGHTS ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED ICE AND WATER FROM THE LEFT WING FUEL TANK. 2L72 4F RTA28NM 19951215004931995121500493NM 1995 12 15 9520245524 119951213A3350 BATTERY PACK BOEING757 757251 1384970NM CABIN DISCHARGED A NWAAK NONE L NO TEST UKUNKNOWN 1 GL01524US 23618 DOOR 4L AND 4R EMERGENCY LIGHTS CYCLE ON AND OFF DURING DIFFERENT PERIODS OF FLIGHT. REPLACED BATTERY. 2L72 4F RTA2NM 19951215004941995121500494NM 1995 12 15 95FDEA01896 119951213A5311 FRAME BOEING727 727232 1384082NM BS 783 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING EO 7-5310-7-3367A1 PT9, FOUND FIVE EXISTING HOLES IN 783 FRAME WHEN DRILLED IN NEW REPAIR WOULD FALL OUT IN RADIUS OF REPAIR ON 783 FRAME RT WL 200 TO 201, 207 AND 214 TO 216. INSTALLED FASTENERS IAW FEDEX EA 7-5310-26784. 2L73 4F A3WE 19951215004951995121500495NM 1995 12 15 95FDEA01897 119951213A5311 FRAME BOEING727 727232 1384082NM BS 760 MISDRILLED A FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25498FE 20867 WHEN WORKING 7-5310-7-3367 REV A1 PART 1, FOUND PILOT HOLES ON EDGE OF 3RD AND 4TH EXISTING FASTENER HOLES ABOVE THE FLOOR AT BS 760 LT WL 208. PILOT HOLES ARE IN FRAME ONLY. REPAIRED DAMAGED FRAME IAW FEDEX 7-5310-26784. 2L73 4F A3WE 19951215004961995121500496NM 1995 12 15 95FDEA01898 119951213A5311 FRAME BOEING727 727232 1384082NM BS 783.95 MISDRILLED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHEN WORKING 7-5310-7-3367A1 PT 4, FOUND PILOT HOLE ON EDGE OF 3RD ABOVE THE FLOOR BS 783.95 RT WL 208. PILOT HOLES ARE IN FRAME ONLY. REPAIRED DAMAGED FRAME IAW FEDEX EA 7-5310-26784. 2L73 4F A3WE 19951215004971995121500497WP 1995 12 15 ABXA9500992 119951102A531501353591 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 4200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 4200. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215004981995121500498WP 1995 12 15 ABXA9500993 119951103A531501353581 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 3720 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 3720. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215004991995121500499WP 1995 12 15 ABXA9500994 119951103A531501353391 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 6390 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 6390. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005001995121500500WP 1995 12 15 ABXA9500995 119951105A5315013534211 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 4470 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 4470. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005011995121500501WP 1995 12 15 ABXA9500996 119951105A531501353491 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 1535 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 1535. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005021995121500502WP 1995 12 15 ABXA9500997 119951105A531501353611 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 5160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 5160. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005031995121500503WP 1995 12 15 ABXA9500998 119951105A531501353481 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 2095 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 2095. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005041995121500504WP 1995 12 15 ABXA9500999 119951106A531501353561 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 2280 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 2280. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005051995121500505WP 1995 12 15 ABXA9501000 119951107A5315013533311 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 9180 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 9180. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005061995121500506WP 1995 12 15 ABXA9501001 119951106A531501353411 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 5430 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 5430. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005071995121500507WP 1995 12 15 ABXA9501002 119951106A531501353461 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 3030 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 3030. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005081995121500508WP 1995 12 15 ABXA9501003 119951106A531501353411 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 5430 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 5430. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005091995121500509WP 1995 12 15 ABXA9501004 119951106A5315013534711 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 2550 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 2550. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005101995121500510WP 1995 12 15 ABXA9501005 119951107A531501353541 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 840 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 840. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005111995121500511WP 1995 12 15 ABXA9501006 119951107A531501353501 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 1080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 1080. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005121995121500512WP 1995 12 15 ABXA9501007 119951107A531501353551 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 1800 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 1800. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005131995121500513WP 1995 12 15 ABXA9501008 119951110A5315013536721 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 8080. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005141995121500514WP 1995 12 15 ABXA9501009 119951106A531501353631 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 6120 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 6120. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005151995121500515WP 1995 12 15 ABXA9501010 119951108A531501353571 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 3240. CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 3240. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005161995121500516WP 1995 12 15 ABXA9501011 119951102A5315013535611 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 2760 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 2760. REPAIRED IAW REA Y153-13321-MR. 2L72 4T A1PC 19951215005171995121500517WP 1995 12 15 ABXA9501012 119951108A531501353651 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 7580 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 7580. REPAIRED IAW REA Y153-13322-MR. 2L72 4T A1PC 19951215005181995121500518WP 1995 12 15 ABXA9501013 119951110A5315013536721 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 8080. REPAIRED IAW REA Y153-13322-MR. 2L72 4T A1PC 19951215005191995121500519WP 1995 12 15 ABXA9501014 119951108A531501353651 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 7580 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, CORROSION WAS FOUND ON A FLOORBEAM AT STA 7580. REPAIRED IAW REA Y153-13322-MR. 2L72 4T A1PC 19951215005201995121500520WP 1995 12 15 ABXA9501015 119951103A532001343611 SUPPORT NIHON YS11 YS11A500 6310416WP BS 2280-2760 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 2280 AND 2760 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005211995121500521WP 1995 12 15 ABXA9501016 119951103A532001354212 SUPPORT NIHON YS11 YS11A500 6310416WP BS 7580-8080 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 7580 AND 8080 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005221995121500522WP 1995 12 15 ABXA9501017 119951103A531501353741 SUPPORT NIHON YS11 YS11A500 6310416WP BS 3720-4200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 3720 AND 4200 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005231995121500523WP 1995 12 15 ABXA9501018 119951103A532001353731 SUPPORT NIHON YS11 YS11A500 6310416WP BS 2760-3240 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 2760 AND 3240 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005241995121500524WP 1995 12 15 ABXA9501019 119951103A532001343741 SUPPORT NIHON YS11 YS11A500 6310416WP BS 5160-5640 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 5160 AND 5640 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005251995121500525WP 1995 12 15 ABXA9501020 119951103A532001353721 SUPPORT NIHON YS11 YS11A500 6310416WP BS 4680-4200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 4680 AND 4200 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005261995121500526WP 1995 12 15 ABXA9501021 119951103A532001343751 SUPPORT NIHON YS11 YS11A500 6310416WP BS 6600-7080 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 6600 AND 7080 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005271995121500527WP 1995 12 15 ABXA9501022 119951103A532001343731 SUPPORT NIHON YS11 YS11A500 6310416WP BS 5160-5640 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 5160 AND 5640 LBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005281995121500528WP 1995 12 15 ABXA9501023 119951103A532001343692 SUPPORT NIHON YS11 YS11A500 6310416WP BS 4680-5160 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 4680 AND 5160 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005291995121500529WP 1995 12 15 ABXA9501024 119951103A532001343792 SUPPORT NIHON YS11 YS11A500 6310416WP BS 7080-7580 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 7080 AND 7580 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005301995121500530WP 1995 12 15 ABXA9501025 119951103A53200134791 SUPPORT NIHON YS11 YS11A500 6310416WP BS 7580-8080 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 7580 AND 8080 LBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005311995121500531WP 1995 12 15 ABXA9501026 119951103A532001343792 SUPPORT NIHON YS11 YS11A500 6310416WP BS 7580-8080 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 7580 AND 8080 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005321995121500532WP 1995 12 15 ABXA9501027 119951103A532001353741 SUPPORT NIHON YS11 YS11A500 6310416WP BS 3720-4200 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 3720 AND 4200 LBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005331995121500533WP 1995 12 15 ABXA9501028 119951103A532001343791 SUPPORT NIHON YS11 YS11A500 6310416WP BS 7080-7580 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 7080 AND 7580 LBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005341995121500534WP 1995 12 15 ABXA9501029 119951103A532001343772 SUPPORT NIHON YS11 YS11A500 6310416WP BS 6120-6600 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 6120 AND 6600 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005351995121500535WP 1995 12 15 ABXA9501030 119951111A532001343752 SUPPORT NIHON YS11 YS11A500 6310416WP BS 5640-6120 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 5640 AND 6120 RBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005361995121500536WP 1995 12 15 ABXA9501031 119951106A532001343791 SUPPORT NIHON YS11 YS11A500 6310416WP BS 840-8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 840 AND 8080 LBL 300 WAS FOUND CORRODED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005371995121500537WP 1995 12 15 ABXA9501032 119951110A532001343792 SUPPORT NIHON YS11 YS11A500 6310416WP BS 840-8080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 840 AND 8080 RBL 300 WAS FOUND CORRODED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005381995121500538WP 1995 12 15 ABXA9501033 119951110A532003343211 SUPPORT NIHON YS11 YS11A500 6310416WP BS 1320-5160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 1320 AND 5160 RBL 1180 WAS FOUND CORRODED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005391995121500539WP 1995 12 15 ABXA9501034 119951106A531501353641 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 6600 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE FLOORBEAM AT STA 6600 WAS FOUND CORRODED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005401995121500540WP 1995 12 15 ABXA9501035 119951109A531501353651 FLOORBEAM NIHON YS11 YS11A500 6310416WP BS 7080 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE FLOORBEAM AT STA 7080 WAS FOUND CORRODED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005411995121500541WP 1995 12 15 ABXA9501036 119951103A532001343691 SUPPORT NIHON YS11 YS11A500 6310416WP BS 4680-5160 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23919AX 2113 DURING C-CHECK, THE LONGITUDINAL FLOOR SUPPORT BETWEEN STA 4680 AND 5160 LBL 300 WAS FOUND DAMAGED. REPAIRED IAW REA Y153-13320-MR. 2L72 4T A1PC 19951215005421995121500542WP 1995 12 15 ABXA9501037 119951211A323129162283 DOOR ROLLER DOUG DC9 DC932 3022066WP LT MLG OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23989AX 47314 BWI - DURING INITIAL GEAR RETRACTION AFTER TAKEOFF, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME INDICATION. UPLATCH CHECK YIELDED GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT. ADJUSTED LEFT MAIN LANDING GEAR DOOR ROLLER IAW DC-9 MM 32-51-4. TEST OF MAIN GEAR LATCH MECHANISM WAS GOOD AT THIS TIME. 2L72 4F A6WE 19951215005431995121500543WP 1995 12 15 ABXA9501038 119951213A3231 RETRACT MECH DOUG DC8 DC862 3021970WP RT MLG DOOR MALFUNCTIONED A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23804AX 45987 AFTER TAKEOFF DURING GEAR RETRACTION, GEAR NOT LATCHED LIGHT ILLUMINATED. CONFIRMED RIGHT GEAR DOOR NOT LATCHED, RECYCLED GEAR AND LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR RETRACTION CHECK AND COULD NOT DUPLICATE DISCREPANCY. OPS CHECK WAS GOOD. 2L74 4F 4A25 19951215005441995121500544WP 1995 12 15 ABXA9501039 119951210A5610 SLIDING WINDOW DOUG DC8 DC862 3021970WP LT COCKPIT OUT OF ADJUST A ABXAK NONE O OTHER ININSP/MAINT 1 GL23805AX 45906 CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. RIGGED AND PRESSURE CHECKED CAPTAIN'S SLIDING WINDOW I/A/W DC8 MM 56-10-3. 2L74 4F 4A25 19951215005451995121500545WP 1995 12 15 ABXA9501040 119951213A3260H141003 SWITCH DOUG DC8 DC862 3021970WP RT MLG DEFECTIVE A ABXAO OTHER N FALSE WARNING APAPPROACH 1 GL23816AX 46093 DURING APPROACH, LANDING GEAR WAS EXTENDED AND RIGHT MAIN LANDING GEAR DID NOT INDICATE A GREEN DOWNLOCK LIGHT. LANDING GEAR WAS RECYCLED TWICE WITH NO CHANGE. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH IAW DC8 MM 32-60-0. OPS CHECK WAS GOOD. 2L74 4F 4A25 19951215005461995121500546WP 1995 12 15 ABXA9501041 119951212A3231NAS120538D BOLT DOUG DC9 DC932 3022066WP LT MLG OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION CLCLIMB 1 GL23989AX 47314 AFTER TAKEOFF ON INITIAL GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, GOT THE SAME INDICATION. AFTER GEAR UPLATCH CHECK, GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT INDICATION. PERFORMED GEAR SWING, FOUND THROUGH BOLT IN PIVOT POINT OF MAIN LANDING GEAR TORQUED TOO TIGHT AND WOULD NOT LET SPRING ENGAGE HOOK ON ROLLERS. RETORQUED CASTELLATED NUT AND INSTALLED COTTER PIN IAW DC-9 SUPP MM 32-31-4. GEAR SWING OPS CHECKED GOOD AND ALL INDICATIONS NORMAL. 2L72 4F A6WE 19951215005471995121500547WP 1995 12 15 ABXA9501042 119951212A335041B004AD07G3 BATTERY PACK DOUG DC9 DC941 302207NWP CABIN DISCHARGED A ABXAK NONE L NO TEST ININSP/MAINT 1 GL23979AX 47492 UPON COCKPIT INSPECTION, FOUND EMERGENCY LIGHT SWITCH IN THE ON POSITION. EMERGENCY BATTERIES VOLTS AT ZERO. REPLACED TWO EACH NICAD BATTERIES FOR EMERGENCY LIGHTING SYSTEM IAW DC-9 SUPP MM 33-53-0 AND OPS CHECKED GOOD. 2L72 4F A6WE 19951215005481995121500548SO 1995 12 15 COMA9512021 119951208A7330725825 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01179CA 120179 LT ENGINE FUEL FILTER BYPASS WARNING CAME ON. REPLACED FUEL FILTER. 2L72 4T4 TRTA31SO E20NE 19951215005491995121500549SO 1995 12 15 COMA9512022 119951212A215022045402 ACM EMB 120 EMB120RT SO RIGHT FAILED A COMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO01164D 1291 120164 DURING FLIGHT, OIL SMELL FROM BOTH COOLING PACKS. REPLACED THE RT AIR CYCLE MACHINE. 2L72 4T RTA31SO 19951215005501995121500550SO 1995 12 15 COMA9512023 119951212A32503085501003 MANIFOLD ASSY EMB 120 EMB120RT SO NLG STEERING DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01137H 164285722 120137 NOSE WHEEL STEERING IS JERKY, DRIFTS TO ONE SIDE AND THEN JERKS BACK. ABNORMAL AMOUNT OF LEFT RUDDER REQUIRED FOR TAKEOFF. REPLACED THE NEW MANIFOLD ASSY. 2L72 4T RTA31SO 19951215005511995121500551SO 1995 12 15 COMA9512024 119951213A2731 CONNECTORS EMB 120 EMB120RT SO ELEV TAB WRONG TYPE A ACOMACD ABORTED TAKEOFF RETURN TO BLOCK NW FALSE WARNING INADEQUATE Q C TOTAKEOFF 1 SO01243CA 1212 DURING TAKEOFF ROLL, TAKEOFF TRIM WARNING SOUNDED. REPLACED HANDSHAKE TYPE WIRING CONNECTORS AT THE ELEVATOR TAB PROXIMITY SENSORS WITH THE CORRECT ENVIRONMENTAL TYPE SPLICES. 2L72 4T RTA31SO 19951215005521995121500552SO 1995 12 15 COMA9512025 119951213A3060 CIRCUIT BREAKER EMB 120 EMB120RT SO LT PROP DE-ICE TRIPPED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01246CA 120223 LEFT PROPELLER DE-ICE FAILED. RESET TRIPPED CIRCUIT BREAKER. SYSTEM CHECK NORMAL AND ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951215005531995121500553EU 1995 12 15 COMA9531208 119951212A2910L387105A SWIVEL SAAB SF340 SF340A 7850100EU RT MLG BROKEN A COMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO01342CA 340A023 EVV - DURING DEPARTURE, LOST ALL HYDRAULIC PRESSURE AND QUANTITY. ACFT RETURNED TO FIELD. REPLACED BROKEN DOWNLOCK HYDRAULIC LINE SWIVEL FITTING AND ACFT RETURNED TO SERVICE. 2L72 4T RTA52EU 19951215005541995121500554EU 1995 12 15 COMA9531209 119951212A32509302533001 SWIVEL JOINT SAAB SF340 SF340A 7850100EU NLG STEERING BROKEN A COMAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO01146CA 340A146 DURING TAXI, NOSE WHEEL STEERING FAILED. REPLACED A BROKEN STEERING TILLER SWIVEL JOINT. 2L72 4T RTA52EU 19951215005551995121500555EA 1995 12 15 COMA9560620 119951212A2510601R412153 ACCESS PANEL CNDAIRCL600 CL6002B19 EA COCKPIT NOT SECURED A COMAD RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 SO01949CA 7080 ACCESS PANEL ON LT SIDE OF CENTER INSTRUMENT PEDESTAL CAME LOOSE AND JAMMED RUDDER PEDALS. SECURED THE THREE FASTENERS ON ACCESS PANEL AND ACFT RETURNED TO SERVICE. 2L72 4F RTA21EA 19951215005561995121500556WP 1995 12 15 MWEA95531 119951213A3010B714032 TEMP SWITCH DOUG DC9 DC914 3022034WP AIRFOIL DE-ICE INOPERATIVE A MWEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL31700ME 1755 45696 DURING FLIGHT, RIGHT ICE PROTECTION TEMP HI LIGHT ILLUMINATED. FLIGHT RETURNED TO MKE. REPLACED RT ICE TEMP HIGH SWITCH AND THERMOSTAT. 2L72 4F A6WE 19951215005571995121500557NM 1995 12 15 UPS205140 119951212A3350 BATTERY PACK BOEING727 727247 138408FNM FLIGHT DECK DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01207UP 21699 MAINT REPORTED, FLIGHT DECK EMERGENCY EXIT LIGHT DIM DUE TEST. FOUND COCKPIT DOOR EMERGENCY LIGHT ASSY BAD. REMOVED AND REPLACED LIGHT ASSY AND BATTERIES IAW MM 33-50-101 PAR 1 TO 3 PAGE 202 TO 203, GND OPS GOOD. 2L73 4F A3WE 19951215005581995121500558WP 1995 12 15 UPS805141 119951212A3230 DNLOCK CYLINDER DOUG DC8 DC871F 302199DWP LT MLG MALFUNCTIONED A IPXAO OTHER J WARNING INDICATION DEDESCENT 1 SO01701UP 45938 CREW REPORTED, LT LANDING GEAR DID NOT INDICATE DOWN AND LOCKED UPON INITIAL GEAR EXTENSION AND 2ND GEAR CYCLE OK. REPLACED DOWNLOCK BUNGEE CYLINDER. 2L74 4F RT4A25 19951215005591995121500559 1995 12 15 UPS805142 419951211A2565 SLIDE DOUG DC8 DC873F 302199FWP ESCAPE SLIDE LOW PRESSURE A IPXAK NONE O OTHER ININSP/MAINT 1 SO01811UP 46089 MAINT REPORTED, ESCAPE SLIDE PRESSURE BELOW LIMITS AND DUE 12/95. REMOVED AND REPLACED SLIDE PER M/M 25-60-01, CHECKS OK. 2L74 4F RT4A25 19951215005601995121500560WP 1995 12 15 UPS805143 119951211A5714 SKIN DOUG DC8 DC873F 302199FWP LEFT CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01809UP 46109 MAINT REPORTED, CRACK AT BOX ROOT AREA LT WING. STOP PER EO DC8-5750-7635C. 2L74 4F RT4A25 19951215005611995121500561EU 1995 12 15 WWMA9500087 119951211A242131342001 AC GENERATOR SAAB SF340 340B 7860101EU LT ENGINE DEFECTIVE A WWMAO OTHER AJ FLAME/FIRE WARNING INDICATION TXTAXI/GRND HDL 1 WP15343SB6094 1765 340B343 LCH - FLT 5045 - DURING GROUND STARTING PROCEDURES THE CREW NOTED THAT THE LEFT AC GENERATOR LIGHT ILLUMINATED AND FLAMES WERE NOTED FROM THE GENERATOR VENT. MAINTENANCE REPLACED THE LEFT AC GENERATOR AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T RTA52EU 19951215005621995121500562CE 1995 12 15 95ZZZM699 119951030A3230 RETRACT MECH BEECH 1900 1900C 1154161CE LANDING GEAR FAILED A GUUAO OTHER J WARNING INDICATION APAPPROACH 1 SO19199GA UB13 FLT NR 479 - TPA-MIA - LANDING GEAR FAILED TO EXTEND, BREAKER POPPED. INSPECTED HYDRAULIC SYSTEM, ACCUMULATION SYSTEM AND ELECTRICAL SYSTEM NO DEFECTS NOTED. SWUNG GEAR ON JACKS NO DEFECTS NOTED. 2L72 4T RTA24CE 19951215005631995121500563NM 1995 12 15 95ZZZM700 119951102A3260MS250081 SQUAT SWITCH BOEING727 727225 1384077NM NLG MALFUNCTIONED A UHVAO OTHER O OTHER LDLANDING 1 SO17805EA 22436 FLT KIC019 - AKL-SYD - ON LANDING, BOTH RIGHT MAIN TIRES BLEW CAUSING GEAR DOOR AND FLAP TRACK DAMAGE. FOUND NOSE GEAR SQUAT SWITCH (S480) OUT OF RIG. RIGGED SWITCH PER MM 32. REPLACED NR 4 BRAKE ANTI-SKID VALVE (LOOSE SOLENOID). REPLACED RIGHT BRAKE CONTROL VALVE AS A PRECAUTIONARY MEASURE. BRAKE CONTROL AND ANTI-SKID SYSTEMS TESTED OK PER MM 32. REPLACED DAMAGED DOOR AND FAIRINGS. ACCOMPLISHED B-CHECK AND RETURNED AIRCRAFT BACK TO SERVICE. 2L73 4F A3WE 19951215005641995121500564WP 1995 12 15 95ZZZM701 119951102A3260DT2RA7 SWITCH DOUG DC9 DC981 3022081WP GEAR HANDLE DIRTY A A4JAO OTHER N FALSE WARNING CLCLIMB 1 SO15818SJ 48058 AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR UNSAFE LIGHTS REMAINED ON. GEAR DOWN LIMITATIONS OBSERVED FOR THE REMAINDER OF FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED CONTACTS OF LANDING GEAR HANDLE SWITCH. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951215005651995121500565CE 1995 12 15 95ZZZM702 119951111A3244 TIRE CLEVELAND 4087 MTSBSIMU2 MU2B36 5780412CE NLG FAILED A MUAAO OTHER O OTHER LDLANDING 1 GL23305CW305 667 ON LANDING AT DET, BOTH NOSE TIRES FAILED (BLEW OUT). THIS FAILURE CAUSED BOTH NOSE WHEEL RIMS TO CONTACT THE RUNWAY SURFACE AT HIGH SPEED DESTROYING BOTH NOSE WHEEL ASSEMBLIES. AT THIS TIME WE ARE NOT ABLE TO ESTABLISH THE CAUSE OF THE TIRE FAILURE. WE HAVE HAD NO PREVIOUS NOSE TIRE FAILURES IN NINE YEARS OF MU-2 AIRCRAFT OPERATION. 1H72 3T RTA10SW 19951215005661995121500566CE 1995 12 15 95ZZZM703 119951115A575335165050259 TE SKIN BEECH 1900 1900C 1154161CE RT TE FLAP CRACKED A AMWAK NONE O OTHER ININSP/MAINT 1 CE07160AM 2095 525 UC160 RIGHT OUTBOARD FLAP, P/N 35165050259, HAS A CRACK APPROXIMATELY .75 INCH LONG ON THE TRAILING EDGE, ON THE UNDERSIDE, 12 INCHES FROM INBOARD END. REPAIRED WITH A DOUBLER. (M) 2L72 4T RTA24CE 19951215005671995121500567WP 1995 12 15 95ZZZM704 119950909A3610 CLAMP LKHEED1011 10113851 5265010WP NR 2 ENG DETERIORATED A AMTAA UNSCHED LANDING JM WARNING INDICATION OVER TEMP CLCLIMB 1 GL11191AT 193C1084 DURING CLIMB, NR 2 NACELLE PYLON OVERHEAT LIGHT CAME ON, BOTH A AND B HIGH PRESSURE VALVES UNLATCHED, WHEN THROTTLE WAS REDUCED THE LIGHT WENT 'OUT', WHEN THROTTLE WAS ADVANCED LIGHT CAME BACK 'ON'. LOWER HIGH PRESSURE VALVE CLAMP AND GASKET WERE REPLACED. 2L73 4F A23WE 19951215005691995121500569EA 1995 12 15 95ZZZM706 119951122A2730NAS110416 BOLTS DHAV DHC8 DHC8311 1386006EA ELEVATOR CONTL LOOSE A AMASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9238 286 DURING MAINTENANCE, THE LEFT YOKE WAS FOUND TO HAVE PLAY IN THE PITCH CONTROL. AFTER INSPECTION, IT WAS FOUND THAT THE SIX BOLTS ON THE ELEVATOR OUTPUT LEVER WERE ALL LOOSE, NO APPARENT VISUAL DAMAGE WAS FOUND TO THE OUTPUT LEVER ASSY. THE BOLTS REQUIRED RETORQUING ON THE LEFT AND THE RIGHT OUTPUT LEVER, P/N 82710093103. THESE BOLTS WERE RETORQUED IAW DASH 8-300 MAINTENANCE MANUAL 27-32-41 PAGE 201. A TEST FLIGHT WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19951215005701995121500570EA 1995 12 15 95ZZZM707 119951122A2730NAS110416 BOLTS DHAV DHC8 DHC8311 1386006EA ELEVATOR CONTL LOOSE A AMASAK NONE O OTHER ININSP/MAINT 1 SW01433AW8929 305 DURING COMPLIANCE WITH MESA FCD 95-32, TWO BOLTS ON THE PILOTS SIDE ELEVATOR OUTPUT LEVER AND FIVE BOLTS ON THE CO-PILOTS SIDE ELEVATOR OUTPUT LEVER, P/N 82710093103, WERE FOUND TO BE LOOSE. NO APPARENT DAMAGE WAS NOTICED ELSEWHERE. BOLTS WERE RETORQUED IAW DHC-8 MM 27-32-41, PAGE 201. (M) 2H72 4T RTA13NM 19951215005711995121500571EA 1995 12 15 95ZZZM708 119951123A2730NAS110416 BOLTS DHAV DHC8 DHC8311 1386006EA ELEVATOR CONTL LOOSE A AMASAK NONE O OTHER ININSP/MAINT 1 SW01435AW8399 315 DURING COMPLIANCE OF FCD 95-32, THE LEFT ELEVATOR OUTPUT LEVER BOLTS THAT ATTACH THE OUTPUT LEVER, P/N 82710093105, TO THE TORQUE TUBE WERE ALL LOOSE. TORQUED ALL LOOSE BOLTS IAW DASH 8 MM 27-32-41. NO DISCREPANCIES ON THE RIGHT SIDE. NO OTHER DAMAGE IS NOTED. (M) 2H72 4T RTA13NM 19951215005721995121500572EA 1995 12 15 95ZZZM709 119951122A2730NAS110416 BOLTS DHAV DHC8 DHC8311 1386006EA ELEVATOR CONTL LOOSE A AMASAK NONE O OTHER ININSP/MAINT 1 SW01430AW10133 279 DURING COMPLIANCE OF FCD 95-32, THREE BOLTS ON THE LEFT ELEVATOR OUTPUT LEVER WERE LOOSE. NO APPARENT VISUAL DAMAGE WAS FOUND TO THE OUPUT LEVER ASSY. THESE BOLTS WERE RETORQUED IAW DASH 8-300 MM 27-32-41, PAGE 201. (M) 2H72 4T RTA13NM 19951215005731995121500573WP 1995 12 15 95ZZZM710 119951111A242092274473 RELAY DOUG DC9 DC932 3022066WP EMER POWER MALFUNCTIONED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11915VV 47443 UPON ARRIVAL OF FLT 586, TPA TO ATL, EMERGENCY POWER WOULD NOT TURN OFF. MAINTENANCE REPLACED R2-7 TRANSFER BUS SENSE RELAY AND R2-7 GROUND REFUEL RELAY. (M) 2L72 4F A6WE 19951215005741995121500574NE 1995 12 15 95ZZZM711 219951113A726171700 GEARBOX DOUG DC9 DC915F 3022037WP PWA JT8 JT8D7B 52053NE LT ENGINE FAILED A Y2PAK NONE K FLUID LOSS ININSP/MAINT 1 GL23197US 47154 P657238 OIL LEAK DISCOVERED ON THE LEFT ENGINE (S/N 657238) AFTER LANDING IN YIP. FURTHER INVESTIGATION REVEALED FOUR BROKEN STUBS IN THE MAIN ENGINE GEARBOX HOUSING. THE GEAR BOX WAS REMOVED AND REPLACED. (M) 2L72 4F4 F A6WE E2EA 19951215005751995121500575NE 1995 12 15 95ZZZM712 219951112A7230 COMPRESSOR PWA 553846 DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 1 ENGINE STALLED A ARWAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 SO19802BN 6710 45909 669175 PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE AFTER 25 MINUTES INTO FLIGHT. ENGINE COMPRESSOR STALLED FOLLOWED BY OIL TEMPERATURE 140 DEGREES CELSIUS AND CLIMBING. RETURNED TO MIAMI WITHOUT INCIDENT. CHECKED GEARBOX OIL SCREEN, ALL PNEUMATIC DUCTS AND ANTI-ICE VALVES. ALL FOUND OK. TOOK OK SAMPLES, VISUAL CHECK OK. PULLED MAIN OIL SCREEN, FOUND OK. REMOVED AND REPLACED TEMP BULB AND CANNON PLUG. IDLE RUN OK. HIGH POWER RUN OK. COULD NOT DUPLICATE COMPRESSOR STALL. (M) 2L74 4F4 F 4A25 1E8 19951215005761995121500576NM 1995 12 15 95ZZZM713 119951114A3610MVB69282350 CLAMP BOEING727 72721 1384003NM NR 3 ENGINE DISTORTED A RYNAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE07359QS 19007 AT APPROX 6000 FEET, A LOW AIR PRESSURE WAS NOTED ON NR 3 BLEED SHORTLY THEREAFTER THE NR 3 FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY. THE NR 3 ENGINE WAS SHUT DOWN AND AIRCRAFT WAS LANDED AT CAE WITHOUT INCIDENT. FOUND 13TH STAGE BLEED DUCT SEPARATED FROM ENGINE AT V-BAND CLAMP CONNECTION. NO DAMAGE NOTED AT DUCT FLANGES AND CLAMP WAS IN A 'TIGHTENED' CONDITION. RECONNECTED DUCT AND REPLACED CLAMP. PERFORMED ENGINE RUN WITH NO LEAKS NOTED. (M) 2L73 4F A3WE 19951215005771995121500577NM 1995 12 15 95ZZZM714 119951112A323065404676 LOCK ACTUATOR BOEING727 727172C 1384058NM NLG FAILED A RYNAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE07527PC 19665 DURING CLIMB-OUT OF IND, THE NOSE GEAR WOULD NOT RETRACT. AN AIR TURN BACK WAS MADE. AIRCRAFT WAS LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK ACTUATOR PER BOEING MM 32-33-11. OPERATIONAL CHECKS GOOD. (M) 2L73 4F A3WE 19951215005781995121500578EU 1995 12 15 95ZZZM715 119951030A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A VNAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 GL07833JS 725 FLT NR 4122 - AIRCRAFT STRUCK A BIRD ON CLIMB-OUT. AIRCRAFT RETURNED TO FIELD LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT IAW MM 5-00-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951215005791995121500579EU 1995 12 15 95ZZZM716 119951121A33503351115001 EEL WIRE AEROSPATR72 ATR72212 EU PASSENGER DOOR BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21369AT 369 ORD - FLT 4187 - CREW REPORTED PASSENGER STAIRS EMERGENCY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRES UNDER TOP STEP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215005801995121500580EA 1995 12 15 95ZZZM717 119951031A3230157077 UPPER LOCK STRUTMENASCO DHAV DHC7 DHC7102 2802708EA LT MAIN GEAR FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07900HA30125 393 025 FLT NR 3170 - HPN - DCA - THE LEFT MAIN GEAR WOULD NOT COME UP WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED IN TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE UPPER AND LOWER LOCK STRUTS. (M) 2H74 4T A20EA 19951215005811995121500581EA 1995 12 15 95ZZZM718 119951031A3230157003 LOWER LOCK STRUTMENASCO DHAV DHC7 DHC7102 2802708EA LT MAIN GEAR FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07900HA32453 078 025 FLT NR 3170 - HPN - DCA - THE LEFT MAIN GEAR WOULD NOT COME UP WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED IN TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE UPPER AND LOWER LOCK STRUTS. 2H74 4T A20EA 19951215005821995121500582EA 1995 12 15 95ZZZM719 119951031A3230157207 LOCK STRUT ASSY MENASCO DHAV DHC7 DHC7102 2802708EA LT MAIN GEAR FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07900HA30125 212 025 FLT NR 3170 - HPN - DCA - THE LEFT MAIN GEAR WOULD NOT COME UP WHEN THE GEAR WAS RETRACTED. THE AIRCRAFT CONTINUED IN TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE UPPER AND LOWER LOCK STRUTS. 2H74 4T A20EA 19951215005831995121500583EA 1995 12 15 95ZZZM720 119951113A2912DSC161 FILTERS DHAV DHC7 DHC7102 2802708EA NR 2 HYD SYSTEM FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07900HA38652 025 FLT NR 3102 - HPN-DCA - THE LEFT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. CYCLED THE GEAR AND IT RETRACTED NORMALLY. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RETURN AND PRESSURE MANIFOLD FILTERS ON THE NR 2 HYDRAULIC SYSTEM. PERFORMED GEAR SWING SEVERAL TIMES AND NO DISCREPANCIES WERE NOTED. (M) 2H74 4T A20EA 19951215005841995121500584EA 1995 12 15 95ZZZM721 119951113A2912DSC160 FILTERS DHAV DHC7 DHC7102 2802708EA NR 2 HYD SYSTEM FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07900HA38652 025 FLT NR 3102 - HPN-DCA - THE LEFT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. CYCLED THE GEAR AND IT RETRACTED NORMALLY. THE FLIGHT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RETURN AND PRESSURE MANIFOLD FILTERS ON THE NR 2 HYDRAULIC SYSTEM. PERFORMED GEAR SWING SEVERAL TIMES AND NO DISCREPANCIES WERE NOTED. (M) 2H74 4T A20EA 19951215005851995121500585NM 1995 12 15 AWXA9500763 119951101A5315 FLOOR BEAM BOEING757 7572S7 1384962NM BS 690-700 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28903AW 23323 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FORWARD CARGO COMPARTMENT FLOOR BEAM CORRODED BEYOND LIMITS, STATION 690 TO STATION 700 LBL 18. REMOVED AND REPLACED FLOOR BEAM CAP PER SRM 53-30-53 AND SRM 51-10-00. (M) 2L72 4F RTA2NM 19951215005861995121500586NM 1995 12 15 AWXA9500769 119951117A3350 PIN BOEING757 7572G7 1384963NM CABIN PULLED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 24-26 FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE. REINSTALLED PIN IN CONNECTOR AT ROW 26, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19951215005871995121500587NM 1995 12 15 AWXA9500779 119951109A5315BAC1505100257 FLOOR BEAM BOEING757 757225 1384959NM BS 1640 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - DURING SCHEDULED C4 INSPECTION, FOUND ENTIRE LENGTH OF FLOOR BEAM, AT STATION 1640, CORRODED. INSTALLED NEW T-CAP IAW SRM 51-40-02. (M) 2L72 4F RTA2NM 19951215005881995121500588NM 1995 12 15 AWXA9500780 119951109A5315 FLOOR BEAM BOEING757 757225 1384959NM BS 365.25 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - DURING SCHEDULED C4 INSPECTION, FOUND TOP CAP FASTENER HOLES CORRODED ON FLOOR BEAM AT STATION 365.25 RBL 6 TO RBL 60. REPAIRED PER SRM 53-00-51, FIGURE 203. (M) 2L72 4F RTA2NM 19951215005891995121500589NM 1995 12 15 AWXA9500781 119951109A5347 SEAT TRACK BOEING757 757225 1384959NM BS 395 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON OUTER FLANGE OF SEAT TRACK AT STATION 395 RBL 24.75. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19951215005901995121500590NM 1995 12 15 AWXA9500782 119951109A5347 SEAT TRACK BOEING757 757225 1384959NM BS 405 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON INNER FLANGE OF SEAT TRACK AT STATION 405 RBL 45. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19951215005911995121500591NM 1995 12 15 AWXA9500783 119951109A5347 SEAT TRACK BOEING757 757225 1384959NM BS 377.7 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28914AW 22208 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON INNER FLANGE OF SEAT TRACK AT STATION 377.7 LBL 24. FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK PER SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19951215005921995121500592SO 1995 12 15 C2XA95IA326 119951102A571312016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915721 120160 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER NR 10 CRACKED JUST FORWARD OF PANEL NR 622DB. MAINTENANCE REMOVED DAMAGE, AND INSTALLED REPAIR SPLICE REF FAX NR EST-475/95. (M) 2L72 4T RTA31SO 19951215005931995121500593EU 1995 12 15 C2XA95IA327 119951112A5311S53671312200 FRAME AEROSPATR42 ATR42320 8680930EU CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915823 165 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 37 CORRODED AT FLOOR LEVEL, JUST ABOVE RIGHT THRESHOLD PLATE FORWARD OF SERVICE DOOR. MAINTENANCE REMOVED CORROSION, AND INSTALLED REPAIR DOUBLER REF EC5310-01013. (M) 2H72 4T RTA53EU 19951215005941995121500594SO 1995 12 15 C2XA95IA328 119951115A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF EMB FAX EST 435/95. (M) 2L72 4T RTA31SO 19951215005951995121500595SO 1995 12 15 C2XA95IA329 119951115A540012030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF EMB FAX EST435/95. (M) 2L72 4T RTA31SO 19951215005961995121500596SO 1995 12 15 C2XA95IA330 119951115A532012015374002 ANGLE EMB 120 EMB120RT SO RT DRAG ANGLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, FOUND A CRACK BETWEEN NR 2 FASTENER LOWR FLANGE AT RT DRAG ANGLE 14 INCHES FROM FORWARD EDGE. MAINTENANCE REMOVED AND REPLACED RT DRAG ANGLE. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951215005971995121500597EU 1995 12 15 C2XA95IA331 119951115A5320S53575102206 STRAP AEROSPATR42 ATR42320 8680930EU BS 11660 CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0914819 156 IAH - DURING C-CHECK INSPECTION, FOUND A CRACK AT THE RIGHT MLG WHEEL WELL STRAP FORWARD CORNER, AT STATION 11660 FS 25, BETWEEN STRINGER 15 AND 16. THE AFFECTED AREA WAS REPAIRED BY BLENDING THE CRACKED MATERIAL, AND INSTALLING A DOUBLER. ALL WORK WAS ACCOMPLISHED IAW ATR 42 DRAWING NR 15S535R0045. (M) 2H72 4T RTA53EU 19951215005981995121500598SO 1995 12 15 C2XA95IA360 119951115A572012017059009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 4 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951215005991995121500599SO 1995 12 15 C2XA95IA361 119951115A572012017059009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951215006001995121500600SO 1995 12 15 C2XA95IA362 119951115A572012017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 20, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19951215006011995121500601EU 1995 12 15 COEA9572901 219951028A7260E027271 VENT LINE FOKKERF27 F27MK600 4990706EU RROYCEDART DART5297E 54507EU NR 2 ENGINE CRACKED A COEAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM01729FE 10385 DURING CRUISE OF FLIGHT 729, NR 2 GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. CREW SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED GEARBOX AND FOUND LEAK AT VENT LINE. REPAIRED LINE IAW AC 43.13 STANDARD PRACTICES. SERVICED GEARBOX, LEAK AND OPERATIONAL CHECK GOOD. (M) 2H72 4T4 T A817 E297 19951215006021995121500602NM 1995 12 15 EISA95292 119950918A5220 RIVETS BOEING727 72782 1384029NM LT EMER EXIT MISSING A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT AFT EMERGENCY EXIT HATCH HAS TWO MISSING FASTENERS (RIVETS) AND TWO DRILL OFF FASTENERS ON UPPER LEFT AND RIGHT CORNERS BY UPPER LATCH ROLLERS (MARKED). REMOVED AND INSTALLED NEW FASTENERS IAW B727 SRM 51-30-2. (M) 2L73 4F A3WE 19951215006031995121500603NM 1995 12 15 EISA95293 119950901A5313BAC1498143 STRINGER BOEING727 72782 1384029NM BS 870 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, BS 870 MAIN CABIN INT, AT STRINGER 3L, WAS FOUND CRACKED IN THE CHANNEL AT TIE IN (X-RAY VERIFIED). REMOVED CRACKED STRINGER. FABRICATED NEW SECTION AND INSTALLED IAW B727 SRM 53-10-3. (M) 2L73 4F A3WE 19951215006041995121500604NM 1995 12 15 EISA95294 119950827A5330 SKIN BOEING727 72782 1384029NM BS 480 SHORTED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A RIVET WAS FOUND IMPROPERLY INSTALLED IN LEFT BS 480 STRINGER 18L. FABRICATED DOUBLER AND INSTALLED IAW B727 SRM 53-30-3 AND SEALED IAW 51-20-4. (M) 2L73 4F A3WE 19951215006051995121500605NM 1995 12 15 EISA95295 119950827A5320 WINDOW FRAME BOEING727 72782 1384029NM BS 255 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A CRACK AROUND THE RIVET ON THE RIGHT AFT COCKPIT WINDOW FRAME WAS FOUND. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR. REINSTALLED WINDOW IAW B727 SRM 53-30-3 AND MM 56-00-00. (M) 2L73 4F A3WE 19951215006061995121500606NM 1995 12 15 EISA95297 119950902A5712 RIB BOEING727 72782 1384029NM WS 629 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING RIB 629 LOWER CHORD HAS A CRACK AT THE THIRD STRINGER FROM THE END, CRACK LENGTH WAS 1 INCH. STOP DRILLED CRACK. FABRICATED DOUBLER AND INSTALLED IAW B727 SRM 57-10-2, 51-20-4. (M) 2L73 4F A3WE 19951215006071995121500607NM 1995 12 15 EISA95299 119950906A5320603630 SUPPORT BOEING727 72782 1384029NM BS 312 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AT BS 312 RBL 20 IN THE MAIN CABIN INTERIOR (1) T-SUPPORT FOR LAV FLOOR HAS CORROSION ON THE LOWER FLANGE AREA. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW B727 SRM 53-20-2. (M) 2L73 4F A3WE 19951215006081995121500608NM 1995 12 15 EISA95301 119950827A532065C352877 WINDOW POST BOEING727 72782 1384029NM FWD FUSELAGE CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FORWARD FUSELAGE EXT LEFT SIDE E/F WINDOW POST IS CRACKED. CRACK RUNS FORWARD AND AFT (X-RAY). STOP DRILLED CRACK. FABRICATED AND INSTALLED E/F WINDOW POST DOUBLER REPAIR IAW B727 SB 53-0086. (M) 2L73 4F A3WE 19951215006091995121500609NM 1995 12 15 EISA95304 119950929A5400 S-DUCT BOEING727 72782 1384029NM AFT FUSELAGE CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE S-DUCT AT RIB NR 1 STAINLESS STEEL REPAIR HAS WORKING FASTENERS, 45 EACH. DURING REMOVAL OF FASTENERS AND REPAIR FOUND CRACK HAD EXCEEDED LENGTH OF REPAIR. REMOVED SECTION WITH CRACK. FORMED AND FABRICATED THREE STRAPS AND WELDED INTO 'Z' CONFIGURATION IAW BAC-5975. FABRICATED SS REPAIR AND INSTALLED ALL PARTS IAW B727 SRM 54-10-3 FIG 4. (M) 2L73 4F A3WE 19951215006101995121500610NM 1995 12 15 EISA95306 119950825A5414 SKIN BOEING727 72782 1384029NM NR 2 PYLON CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE NR 2 ENGINE PYLON HAS CORROSION BULGES ON LEFT SIDE AT LOWER SIDE OF SKIN UPPER SURFACE. REMOVED, FABRICATED AND INSTALLED THREE SKIN PANELS, ONE RAIN GUTTER DUE TO OUT OF SRM LIMITS IAW B727 SRM 53-30-1 AND 54-30-2 FIG 4. (M) 2L73 4F A3WE 19951215006111995121500611NM 1995 12 15 EISA95308 119950829A5315 FLOOR BEAM BOEING727 72782 1384029NM BS 1166 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO IN LAKE CITY, FL, THE AFT CARGO PIT WAS FOUND WITH A CRACKED FLOOR SUPPORT BEAM IN THE CENTER SECTION AT BS 1166. REMOVED CRACKED FLOOR SUPPORT BEAM. FABRICATED NEW FLOOR SUPPORT BEAM, SPLICE, TWO L-ANGLES AND INSTALLED ALL PARTS IAW B727 SRM 53-10-5. (M) 2L73 4F A3WE 19951215006121995121500612NM 1995 12 15 EISA95309 119950828A5320 INTERCOSTAL BOEING727 72782 1384029NM BS 950 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE INTERCOSTAL AFT OF BULKHEAD 950 BELOW STRINGER 21R WAS FOUND CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED A DOUBLER REPAIR IAW B727 SRM 53-10-8. (M) 2L73 4F A3WE 19951215006131995121500613NM 1995 12 15 EISA95310 119950901A5312 BULKHEAD BOEING727 72782 1384029NM BS 740 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE AFT BULKHEAD CENTER PANEL, FORWARD CARGO PIT HAS CRACKED AND TORN FASTENER HOLES IN BOTTOM END OF PANEL. DRESSED OUT CRACKED AND TORN AREA. FABRICATED AND INSTALLED TWO DOUBLERS IAW B727 SRM 51-40-2. (M) 2L73 4F A3WE 19951215006141995121500614NM 1995 12 15 EISA95311 119950825A5330 SKIN BOEING727 72782 1384029NM BS 428 SHORT A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LAP JOINT SKIN AT BS 428 AND STRINGER 19L HAS 2 FASTENERS WITH NO EO. REMOVED SECTION OF LAP. FABRICATED AND INSTALLED REPAIRS IAW B727 SRM 53-30-3. (M) 2L73 4F A3WE 19951215006151995121500615NM 1995 12 15 EISA95312 119950823A5320608004 ATTACH ANGLE BOEING727 72782 1384029NM BS 780 CHAFFED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AT BS 780 RBL 10 THE FAIRING ATTACH ANGLE WAS FOUND CHAFFED MORE THAN 50 PERCENT. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW B727 SRM 51-40-4 AND MM 51-20-00. (M) 2L73 4F A3WE 19951215006161995121500616NM 1995 12 15 EISA95313 119950823A5320AND101342003 ANGLE BOEING727 72782 1384029NM BS 480 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE CENTER LINE FLOOR SUPPORT AT BS 480 WAS FOUND MISDRILLED AND CORRODED. REMOVED FLOOR SUPPORT ANGLE, FABRICATED AND INSTALLED A NEW ANGLE IAW B727 SRM 53-10-8. (M) 2L73 4F A3WE 19951215006171995121500617NM 1995 12 15 EISA95314 119950828A5311 FRAME BOEING727 72782 1384029NM BS 1166 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE CIRCUMFERENTIAL SKIN BUTT JOINT FRAME AT BS 1166 RIGHT AT WL 208 IS GOUGED AND CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIRS IAW B 727 SRM 51-40-3. (M) 2L73 4F A3WE 19951215006181995121500618NM 1995 12 15 EISA95315 119950828A5330 SKIN BOEING727 72782 1384029NM BS 1166 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE CIRCUMFERENTIAL SKIN BUTT JOINT AT BS 1166 LEFT SIDE AT WL 208 IS GOUGED AND CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLER IAW B727 SRM 51-40-2. (M) 2L73 4F A3WE 19951215006191995121500619NM 1995 12 15 EISA95317 119950824A531160445 FRAME BOEING727 72782 1384029NM BS 760 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE FORWARD LOWER INNER FLANGE OF FUSELAGE FROME BS 760 LT SIDE ABOVE THE CENTER TANK PLATE SKIN. REMOVED CORRODED STRAP AND ANGLE. FABRICATED AND INSTALLED NEW STRAPS AND ANGLES IAW B727 SRM 51-40-4, 51-40-2 AND MM 51-20-2. (M) 2L73 4F A3WE 19951215006201995121500620NM 1995 12 15 EISA95318 119950824A5320 GUSSET BOEING727 72782 1384029NM BS 760.95 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE GUSSET ON FORWARD SIDE OF FUSELAGE FRAME BS 760.95 RT, BY OUTER FLANGE BELOW CREASE AREA IN CABIN. REMOVED GUSSET, FABRICATED AND INSTALLED NEW GUSSET IN CONJUNCTION WITH NR 060N1-05051 IAW B727 SB 727-57-0112. (M) 2L73 4F A3WE 19951215006211995121500621NM 1995 12 15 EISA95319 119950824A5320 ANGLE BOEING727 72782 1384029NM BS 825 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON SCHEDULED INSPECTION AT AERO CORP ON LAKE CITY, FL, A CRACKED ANGLE AT THE LOWER END OF FUSELAGE FRAME AT BS 825 RT SIDE INNER FLOOR BEAM LOWER ANGLE WAS FOUND. REMOVED CRACKED L-ANGLE. FABRICATED AND INSTALLED NEW L-ANGLE IAW B727 SRM 51-20-1 AND 51-30-2. (M) 2L73 4F A3WE 19951215006221995121500622NM 1995 12 15 EISA95320 119950824A532069174966 GUSSET BOEING727 72782 1384029NM BS 825 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION ON AERO CORP IN LAKE CITY, FL, THE GUSSET AT BS 825 FORWARD SIDE INNER FLANGE TO LOWER ANGLE OF CABIN FLOOR BEAM WAS FOUND CRACKED. REMOVED CRACKED GUSSET. ORDERED NEW GUSSET AND INSTALLED NEW GUSSET IAW B727 SRM 51-30-2. (M) 2L73 4F A3WE 19951215006231995121500623NM 1995 12 15 EISA95322 119950906A5320 SHEAR WEB BOEING727 72782 1384029NM BS 1166 ELONGATED HOLES A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AT BS 1166 LEFT SIDE 1 FLOOR PAN SHEAR WEB HAS 15 ELONGATED HOLES AND LIGHT SURFACE CORROSION AT DOUBLER. REMOVED SHEAR WEB. FABRICATED AND INSTALLED NEW WEB IAW B727 SRM 53-20-2. (M) 2L73 4F A3WE 19951215006241995121500624NM 1995 12 15 EISA95323 119950906A5320 RETAINER BOEING727 72782 1384029NM BS 1166 ELONGATED HOLES A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE BS 1166 RIGHT SIDE 1 RETAINED STRIP FOR FLOOR PAN HAS 1 ELONGATED HOLE IN FLANGE. REMOVED THE FLOOR PAN. FABRICATED AND INSTALLED NEW PAN AND RETAINER IAW B727 SRM 51-40-2. (M) 2L73 4F A3WE 19951215006251995121500625 1995 12 15 EISA95324 419950912A3420 FLUX VLV HARNESS BOEING727 72782 1384029NM LT WING TOO SHORT A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING F.O.M., THE LENGTHENING OF FLUX VALVE HARNESS WAS REQUIRED TO RELOCATE A BRACKET IAW B727 MM 34-21-0. (M) 2L73 4F A3WE 19951215006261995121500626NM 1995 12 15 EISA95325 119950913A532069144621 SPLICE PLATE BOEING727 72782 1384029NM BS 870 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT BS 870 SPLICE PLATE BELOW 5-9 WAS FOUND CRACKED BETWEEN FASTENER HOLES. REMOVED CRACKED SPLICE PLATE. FABRICATED AND INSTALLED NEW PLATE IAW B727 SB 53-0194 AND AD 91-24-11. (M) 2L73 4F A3WE 19951215006271995121500627NM 1995 12 15 EISA95326 119950831A5320 RIB CHORD BOEING727 72782 1384029NM BS 760 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE BS 760R RIB CHORD UPPER VERTICAL FLANGE FORWARD OF FRAME IS CRACKED ACROSS HOLES AND FROM THE LOWER HOLE DIAGONALLY AFT .375 INCH. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED SHIM AND FREEZE PLUGS IAW B727 SB 727-57-0112. (M) 2L73 4F A3WE 19951215006281995121500628NM 1995 12 15 EISA95327 119950827A5522 SKIN BOEING727 72782 1384029NM RT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT ELEVATOR SKIN HAS ONE CRACK BEYOND PREVIOUS REPAIR AT HAT STIFFENER CENTER PORTION (X-RAY). REMOVED ELEVATOR. FABRICATED AND INSTALLED REPAIR IAW B727 MM 27-30-1 AND SRM 51-80-7. (M) 2L73 4F A3WE 19951215006291995121500629NM 1995 12 15 EISA95328 119950827A575465162272 FLAP BOEING727 72782 1384029NM NR 6 LE FLAP CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, UPON REMOVAL OF CORROSION IN NR 6 K-FLAP BEHIND INBOARD ADJUSTMENT BRACKET, AREA FOUND TO BE OUT OF LIMITS PER THE SRM 57-50-1. REMOVED AND REPLACED THE NR 6 KRUGER FLAP IAW B727 MM 27-81-1. OPS CHECKED GOOD. (M) 2L73 4F A3WE 19951215006301995121500630NM 1995 12 15 EISA95329 119950824A5320 ANGLE BOEING727 72782 1384029NM BS 825 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FORWARD ANGLE IS CRACKED ON LOWER END OF FUSELAGE FRAME BS 825L AT INNER FLANGE TO FLOOR BEAM. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW L-ANGLE IAW B727 SRM 51-40-3. (M) 2L73 4F A3WE 19951215006311995121500631NM 1995 12 15 EISA95330 119950826A534765196011 SEAT TRACK BOEING727 72782 1384029NM BS 820 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE MAIN CABIN BS 760 TO BS 820 RBL 40, ONE AREA OF SEAT TRACK HAS CORROSION IN UPPER CHANNEL. REMOVED AND REPLACED THE SEAT TRACK IAW B727 SRM 53-10-5. (M) 2L73 4F A3WE 19951215006321995121500632NM 1995 12 15 EISA95331 119951009A5320 STIFFENER BOEING727 72782 1384029NM BS 1335 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE HORIZONTAL ATTACH STIFFENER FOR AFT AIR STAIR OVERHEAD LIGHT AT BS 1335 IN AIR STAIR HAS CORROSION. CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B727 51-40-4. (M) 2L73 4F A3WE 19951215006331995121500633NM 1995 12 15 EISA95332 119951009A5330 SKIN BOEING727 72782 1384029NM BS 1183-1464 DELAMINATED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 REMOVE BAD FASTENERS UPPER RIGHT AFT FUSELAGE FROM BS 1183 TO BS 1464. REMOVED, FABRICATED AND INSTALLED TWO SKIN PANELS ONE WAS 19 INCHES BY 33 INCHES, AND THE SECOND ONE WAS 24 INCHES BY 30 INCHES IAW B727 SRM 53-30-2 AND 53-30-3. (M) 2L73 4F A3WE 19951215006341995121500634NM 1995 12 15 EISA95333 119950914A5531 FRAME BOEING727 72782 1384029NM VERT STAB BROKEN A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, TWO FRAME WEBS WERE FOUND TO BE CRACKED AND BROKEN VSS 1365.5R AND 1387.5R. REMOVED CRACKED AND BROKEN WEBS. FABRICATED AND INSTALLED TWO WEBS IAW B727 SRM 51-40-2. (M) 2L73 4F A3WE 19951215006351995121500635NM 1995 12 15 EISA95334 119950923A575465973471 HINGE FITTING BOEING727 72782 1384029NM NR LE FLAP CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING NR 3 KRUGER FLAP INBOARD HINGE FITTING WAS FOUND WITH CORROSION. REMOVED AND REPLACED THE NR 3 KRUGER FLAP INBOARD HINGE FITTING IAW B727 MM 27-81-0. (M) 2L73 4F A3WE 19951215006361995121500636NM 1995 12 15 EISA95335 119950917A5730 SKIN BOEING727 72782 1384029NM WS 171.5 LE CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT WING LEADING EDGE WAS FOUND CRACKED ON THE INNER SKIN APPROXIMATELY WS 171.5 IN AREA OF NR 3 D-FLAP. CUT OUT CRACKED SECTION. FABRICATED FILLERS, SPACERS, COVERS, L-ANGLE, AND SPLICE ANGLES AND INSTALLED ALL PARTS IAW B727 SRM 51-10-2, 51-40-1 AND MM 51-20-2. (M) 2L73 4F A3WE 19951215006371995121500637NM 1995 12 15 EISA95336 119950825A5414 SKIN BOEING727 72782 1384029NM NR 2 ENG PYLON CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING INSPECTION AT AERO CORP IN LAKE CITY, FL, NR 2 ENGINE PYLON HAS CORROSION BULGING ON RIGHT SIDE AT LOWER EDGE OF SKIN UPPER SURFACE. REMOVED FASTENERS IAW SRM 51-30-2. CLEANED CORROSION IAW SRM 51-10-6 (AT APPROXIMATELY STATION 1352 ONLY). OK TO ALODINE AND PRIME AND INSTALL FASTENERS. INSTALL FASTENERS AT STATION 1352 IAW SRM 51-30-2 SEALED AREA IAW 51-20-4 AND 8-29-95. REMOVED GUTTER TO F.O.M. IAW SRM 51-30-2. REINSTALLED GUTTER IAW SRM 51-30-2, FAB FILLER AND DOUBLER FROM 2024-T3. (M) 2L73 4F A3WE 19951215006381995121500638NM 1995 12 15 EISA95337 119950827A5220 WEB BOEING727 72782 1384029NM RT EMERG HATCH MISSING A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT FORWARD EMERGENCY EXIT HATCH IS MISSING UPPER LEFT AND RIGHT WEBS. FABRICATED TWO WEBS AND INSTALLED IAW B727 SRM 52-20-1 FIG 1 AND 51-20-1. (M) 2L73 4F A3WE 19951215006391995121500639NM 1995 12 15 EISA95338 119950829A5313 STRINGER BOEING727 72782 1384029NM BS 400 HOLES A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, STRINGER 4L AT STATION 400 UNDER CIRCUFERENTIAL HAS 2 HOLES. REMOVED SECTION WITH HOLES. FABRICATED REPAIR MEMBER AND SPLICES AND INSTALLED ALL PARTS IAW B727 SRM 53-10-3. (M) 2L73 4F A3WE 19951215006401995121500640NM 1995 12 15 EISA95341 119950825A5220 WEB BOEING727 72782 1384029NM RT HATCH CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL RIGHT AFT EMERGENCY EXIT HATCH CORRODED INTERNALLY. REMOVED LOWER INTERNAL WEB, REMOVED AND INSTALLED NUT CHANNELS. REMOVED LESS THAN .002 MATERIAL, TREATED AND PRIMED THEN REINSTALLED WEB IAW B727 SRM 51-30-2, 51-10-2, AND MM 51-20-2. (M) 2L73 4F A3WE 19951215006411995121500641NM 1995 12 15 EISA95346 119950824A5523 TRIM TAB BOEING727 72782 1384029NM RT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, RIGHT ELEVATOR TRIM TAB WAS FOUND TO HAVE TWO BOB WEIGHTS CRACKED AND SPLIT. REMOVED RIGHT ELEVATOR TRIM TAB, REPAIRED TWO WEIGHTS, BALANCED TRIM TAB, REINSTALLED TRIM TAB. MAINTENANCE PERFORMED IAW B 727 MM 27-30-1 SRM 51-10-1, 51-30-2, 51-80-9. OPS CHECK TO BE PERFORMED UNDER 060N1-1651. (M) 2L73 4F A3WE 19951215006421995121500642NM 1995 12 15 EISA95349 119950825A5753652163479 SKIN BOEING727 72782 1384029NM TE FLAP CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE BN295 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LEFT INBOARD AFT FLAP, ONE AREA OF SEVERE I/G CORROSION (100 PERCENT THROUGH MATERIAL) THROUGH UPPER SKIN SURFACE. REMOVED AND REPLACED THE LEFT INBOARD AFT FLAP IAW B727 MM 27-51-1. OPS CHECK GOOD. (M) 2L73 4F A3WE 19951215006431995121500643NM 1995 12 15 EISA95350 119950902A7100 HOIST MOUNT PAD BOEING727 72782 1384029NM NR 2 ENGINE CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE VERTICAL STAB RIGHT TRAILING EDGE PANEL AT NR 2 ENGINE HOIST MOUNT PAD HAS BULGING CORROSION. OPENED AREA, REMOVED CORROSION, FABRICATED AND INSTALLED THREE SKIN PANELS AND ONE RAIN GUTTER IAW B727 SRM 54-30-2. (M) 2L73 4F A3WE 19951215006441995121500644NM 1995 12 15 EISA95351 119950919A5753 L-ANGLE BOEING727 72782 1384029NM TE MID FLAP CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE RIGHT INBOARD FLAP TRAILING EDGE AFT LOWER SPAR (L-ANGLE EXTRUSION) IS CRACKED 1.5 INCHES LONG. STOP DRILLED CRACK. FABRICATED AN L-ANGLE REPAIR AND INSTALLED IAW B727 SRM 51-40-4. (M) 2L73 4F A3WE 19951215006451995121500645NM 1995 12 15 EISA95353 119950823A7110 INNER SKIN BOEING727 72782 1384029NM NR 3 COWLING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE NR 3 ENGINE UPPER COWLING TRAILING EDGE CORNER, INNER SKIN IS BENT AND CRACKED. CUT OUT CRACKED INNER SKIN, FABRICATED FILLER, DOUBLER AND INSTALLED IAW B727 SRM 54-10-3. (M) 2L73 4F A3WE 19951215006461995121500646NM 1995 12 15 EISA95356 119950905A5754 FITTING BOEING727 72782 1384029NM NR 2 LE FLAP CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE MOUNT FITTING AT INBOARD END OF NR 2 LEADING FLAP. REMOVED NR 2 KRUGER FLAP. REMOVED AND REPLACED MOUNT FITTING. REPLACED ATTACH ANGLE AND REINSTALLED NR 2 KRUGER FLAP IAW B727 MM 27-8-1 SRM 51-40-3 AND 51-30-2. (M) 2L73 4F A3WE 19951215006471995121500647NM 1995 12 15 EISA95357 119950905A5720651626415 BRACKET BOEING727 72782 1384029NM L/E FLAPWELL CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSEPCTION AT AERO CORP IN LAKE CITY, FL, A CORRODED BRACKET WAS FOUND IN THE LEADING EDGE FLAPWELL BETWEEN NR 2 AND NR 4 LEADING EDGE FLAPS. REMOVED AND REPLACED CORRODED BRACKET IAW B727 SRM 51-30-2 AND 57-10-0. (M) 2L73 4F A3WE 19951215006481995121500648NM 1995 12 15 EISA95358 119950901A5730 PANEL BOEING727 72782 1384029NM NR 3343 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, WING PANEL 3343 HAD DELAMINATION AND CRACK AT REPAIR DOUBLER. REBONDED STRIP IAW SRM 51-40-6. REMOVED OLD PATCH AND FABRICATED NEW REPAIR IAW 51-40-6, LOCATED AND DRILLED UP IAW 51-30-2, ALODINED AND PRIMED IAW SRM 51-10-6. INSTALLED IAW SRM 51-30-2. (M) 2L73 4F A3WE 19951215006491995121500649NM 1995 12 15 EISA95359 119950914A5754 SKIN BOEING727 72782 1384029NM NR 3 LE SLAT DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, HEADS GROUND OFF HI-LOCS AND EXCESSIVE MATERIAL WAS REMOVED FROM NR 3 SLAT SKIN. REMOVED FASTENERS AND CLOSED OUT PANELS TO F.O.M. REPAIR. FABRICATED REPAIR 5 INCHES BY 6.5 INCHES FROM 2024T3-.080 IAW 57-30-3, LOCATED AND DRILLED UP IAW 51-30-2, ALODINED AND PRIMED ONE SIDE ONLY IAW B727 SRM 51-10-6. INSTALLED REPAIR IAW SRM 51-50-3 AND 51-30-2, INSTALLED CLOSE OUT PANELS AND SEALS IAW 51-30-2. (M) 2L73 4F A3WE 19951215006501995121500650NM 1995 12 15 EISA95360 119950912A5320 ACCESS PANEL BOEING727 72782 1384029NM LT MLG CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT MAIN LANDING GEAR, FORWARD TRUNNION ACCESS PANEL AROUND MOUNTING HOLES. REMOVED DAMAGED AREA IAW B727 SRM 53-30-3. FAB NEW REPAIR IAW SRM B727 53-30-3. PRIMED AND ALODINED REPAIR IAW SRM B727 53-10-2. INSTALLED NEW REPAIR IAW SRM B727 53-30-3. (M) 2L73 4F A3WE 19951215006511995121500651NM 1995 12 15 EISA95361 119950905A5754 SKIN BOEING727 72782 1384029NM NR 3 LE SLAT CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION AROUND FASTENERS FORWARD OF REPAIR ON NR 3 SLAT SKIN AT ACTUATOR ATTACH POINT WAS FOUND. CORROSION WAS FOUND TO BE OUT OF LIMITS BY APPROXIMATELY 20 PERCENT. FABRICATED REPAIR IAW SRM 57-50-3. TREATED AND ALODINED IAW 51-10-2. INSTALLED NEW FASTENERS AND REPAIR IAW SRM 51-30-2. (M) 2L73 4F A3WE 19951215006521995121500652NM 1995 12 15 EISA95362 119950916A5754 SKIN BOEING727 72782 1384029NM NR 3 LE SLAT DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 SLAT HAS EXCESSIVE MATERIAL REMOVED FROM UPPER SKIN IN AREA OF INBOARD SLAT HOOK FORWARD MOUNTING SCREW. FABRICATED REPAIR WITH 2024T3 X.090 TRAV NR 1A-720 PO NR 605687 APPROX 4.5 INCHES BY 5 INCHES IAW B727 SRM CH 57-50-3. TREATED AND PRIMED MATING SURFACES IAW B727 SRM CH 51-10-2. INSTALLED REPAIR WASHERS IAW B727 SRM CH 51-30-8, INSTALLED REPAIR IAW B727 SRM CH 51-30-2. (M) 2L73 4F A3WE 19951215006531995121500653NM 1995 12 15 EISA95363 119950824A575541400106 BEAM BOEING727 72782 1384029NM SPOILER CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT MLG WHEEL WELL, RIGGING BEAM ASSY HAS DEEP PITTING CORROSION IN SEVERAL AREAS AT SPOILER MIXER AREA. MECHANICALLY REMOVED CORROSION, GROUND OUT .055 AND CORROSION STILL EXISTS. REMOVED AND REPLACED RIGGING BEAM IAW B727 MM 27-61-31. RIG CHECKED GOOD, OPS CHECK WILL BE COMPLIED ON NR 060N112241 (05402). (M) 2L73 4F A3WE 19951215006541995121500654NM 1995 12 15 EISA95364 119950826A5720 STIFFENER BOEING727 72782 1384029NM WING TE CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND TRAILING EDGE PANEL BELOW NR 13 SPOILER HAS CRACKED STIFFENER. REMOVED, FAB NEW PART AND INSTALLED PART IAW 51-40-4. (M) 2L73 4F A3WE 19951215006551995121500655NM 1995 12 15 EISA95365 119950829A5753 RIB BOEING727 72782 1384029NM LT TE MID FLAP CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT INBOARD MID FLAP, 11TH INTERNAL RIB FROM INBOARD UNDERSIDE OF FLANGE NEAR CENTER SPAR, CORROSION FOUND TO BE OUT OF LIMITS. MADE L-ANGLE AND INSTALLED IAW SRM 57-40-2 FIG 1. FABRICATED ONE ANGLE 1 INCH BY 2.25 INCH BY 2 INCH FROM 7075-T6 .O63 IAW SRM 57-40-2 FIG 1. (M) 2L73 4F A3WE 19951215006561995121500656NM 1995 12 15 EISA95367 119950830A5712 RIB BOEING727 72782 1384029NM LT WING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT WING RIB 738.5 LOWER CHORD IS CRACKED AT FORWARD STRINGER BOLT HOLE. STOP DRILLED ENDS OF CRACK. FABRICATED, LOCATED AND DRILLED DOUBLER AND FILLERS IAW B727 SRM 51-10-1 AND 57-10-5. ALODINED AND PRIMED PARTS IAW B727 SRM 51-10-2 AND INSTALLED DOUBLER AND FILLERS IAW B727 SRM 57-10-5 AND 51-30-2. FABRICATED 1 INCH BY 3 INCH BY 5 INCH DOUBLER OUT OF 7075-T6 X .063. (M) 2L73 4F A3WE 19951215006571995121500657NM 1995 12 15 EISA95368 119950902A5712 RIB BOEING727 72782 1384029NM LT WING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT WING RIB 546.5 LOWER CHORD HAS A CRACK AT THIRD STRINGER FROM FORWARD END. STOP DRILLED, FABRICATED DOUBLER REPAIR OUT OF 7075-0 .080 APPROX DIM2.5 INCH BY 7 INCH LONG. INSTALLED DOUBLER IAW B727 SB57-0127 AND SRM 57-10-5. ALL OTHER MAINTENANCE PERFORMED IAW SRM 51-10-1, 51-10-3, 51-30-2, 51-10-2 AND 57-10-3. (M) 2L73 4F A3WE 19951215006581995121500658NM 1995 12 15 EISA95369 119950916A5720 BRACKET BOEING727 72782 1384029NM WS 200 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, NR 2 KRUGER FLAP AREA OF WING LEADING EDGE HAS CORROSION ON RIB ATTACH FITTING APPROXIMATELY WS 200. REPAIRED WEB PER 51-40-2 B727 SRM, FASTENERS PER 51-30-2 B727 SRM, CORROSION INHIBITOR PER 51-10-2 B727 SRM. (M) 2L73 4F A3WE 19951215006591995121500659NM 1995 12 15 EISA95370 119950919A5754 RIBS BOEING727 72782 1384029NM NR 3 LE SLAT MISMANUFACTURED A EISAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 LEADING EDGE SLAT HAS THREE RIBS WITH LOWER SURFACE FLANGES PREVIOUSLY TRIMMED BEYOND .100 INCH LIMIT. FABRICATED THREE REPAIR ANGLES IAW B727 SRM CH 57-50-3 PO NR 60733 7075-0 X .040 HEAT TREAT TO T6 PER BAC 5606 HARDNESS TEST PER RWB SCALE (REF NR NR 11020) TREATED, PRIMED ANGLES IAW B727 SRM CH 51-10-2. INSTALLED IAW CH 51-30-6. (M) 2L73 4F A3WE 19951215006601995121500660NM 1995 12 15 EISA95371 119950911A5730 SKIN BOEING727 72782 1384029NM RT WING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND SEVERAL CRACKS ON INNER SKIN BEHIND NR 4 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. REMOVED TWO CLOSE OUT PANELS AND FOUR RIBS AND BLEED AIR DUCT TO F.O.M. ON CRACKED SKIN. CUT OUT INNER SKIN DAMAGE APPROXIMATELY 15 INCHES BY 4 INCHES AND FABRICATED REPAIR IAW B727 SRM 57-30-4. FABRICATED 3 SHIMS IAW SRM 57-30-4, LOCATED AND DRILLED UP IAW SRM 51-30-2. ALODINED AND PRIMED IAW 51-10-6. INSTALLED IAW SRM 57-30-4 AND 51-30-2. INSTALLED CLOSE OUT PANELS AND RIBS AND BLEED AIR DUCT IAW 51-30-2. (M) 2L73 4F A3WE 19951215006611995121500661NM 1995 12 15 EISA95372 119950905A5754 RIB BOEING727 72782 1384029NM NR 3 LE FLAP CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND NR 3 SLAT ACTUATOR RIB CRACKED INBOARD RIB. REMOVED INNER SKIN TO ACCESS AREA. FABRICATED ANGLE FROM 7075-0 X .040 IAW B727 SRM CH 57-50-3. HEAT TREATED TO T-6 IAW BAC 5606 AND RWB SCALE PN NR 60733 TRAV NR 1A-1181. TREATED AND PRIMED ANGLE IAW B727 SRM CH 51-10-2. INSTALLED ANGLE IAW B727 SRM CH 51-30-2. REINSTALLED INNER SKIN IAW B727 SRM CH 51-30-2. (M) 2L73 4F A3WE 19951215006621995121500662NM 1995 12 15 EISA95373 119950825A278066973473 MOUNT BOEING727 72782 1384029NM NR 6 LE ACTUATORCORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON MOUNT FOR NR 6 LEADING EDGE ACTUATOR. MECHANICALLY REMOVED CORROSION, MATERIAL LOSS AND CORROSION BEYOND LIMITS IAW B727 SRM 51-20-2. NEW MOUNT INSTALLED IAW 57-40-1. (M) 2L73 4F A3WE 19951215006631995121500663NM 1995 12 15 EISA95374 119950916A5720 FITTING BOEING727 72782 1384029NM RT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, WEB SUPPORT FITTING ON RIGHT WING LEADING EDGE CAVITY CORRODED APPROXIMATELY WS 173. REMOVED WEB SUPPORT FITTING IAW SRM B727 51-10-1. FAB NEW SUPPORT FITTING IAW SRM B727 51-10-1. ALODINED AND PRIMED WEB SUPPORT AREA AND FITTING IAW SRM B727 51-10-6. INSTALLED NEW WEB FITTING IAW SRM B727 51-10-1. (M) 2L73 4F A3WE 19951215006641995121500664NM 1995 12 15 EISA95375 119950905A5754 SKIN BOEING727 72782 1384029NM NR 4 LE FLAP DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, EXCESSIVE METAL REMOVED FROM NR 4 SLAT SKIN NEXT TO TELESCOPING DUCT PANEL SEAL. FABRICATED REPAIR IAW SRM 57-30-3, ALODINED IAW SRM 51-10-2, SEALED REPAIR IAW SRM 57-30-5. INSTALLED REPAIR IAW SRM 57-30-3. REPAIR DOUBLER FABRICATED FROM 2024-T3-0.080 APPROX 6 INCHES BY 3.5 INCHES. (M) 2L73 4F A3WE 19951215006651995121500665NM 1995 12 15 EISA95376 119950902A5712 RIB BOEING727 72782 1384029NM LT WING CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LEFT WING RIB 546.5 LOWER CHORD HAS A CRACK AT 4TH STRINGER FROM FORWARD END. STOP DRILLED CRACK. FABRICATED DOUBLER REPAIR OT OF 7075-0 BY .080 APPROXIMATE DIA 2.5 INCH BY 7.25 INCH LONG. INSTALLED DOUBLER IAW SB 57-0127 AND SRM 57-10-5. ALL OTHER MAINTENANCE PERFORMED IAW SRM 51-10-1, 51-10-3, 51-30-2, 51-20-2, AND 57-10-3. (M) 2L73 4F A3WE 19951215006661995121500666NM 1995 12 15 EISA95377 119950913A5754 ANGLE BOEING727 72782 1384029NM NR 2 LE FLAP CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION BEYOND LIMITS NR 2 SLAT ATTACH ANGLE IAW 51-10-6 100 PERCENT METAL REMOVAL WAS FOUND. FABRICATED NEW ATTACH ANGLE, ALODINED AND PRIMED AND INSTALLED NEW BRACKET IAW B727 SRM 51-10-1, 51-10-2, 51-40-3 L-ANGLE 7075T6 .063 5.2187 BY 1.5 BY .75 INCH. (M) 2L73 4F A3WE 19951215006671995121500667NM 1995 12 15 EISA95378 119950905A5754 SKIN BOEING727 72782 1384029NM NR 3 LE FLAP CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION AROUND FASTENER HOLES ON NR 3 SLAT SKIN OUTBOARD OF THE OUTBOARD TRACK, (SOME MATERIAL PREVIOUSLY REMOVED). REMOVED CORROSION IAW SRM 51-10-6, FOUND MATERIAL TO BE OUT OF LIMITS BY 20 PERCENT AT DEEPEST POINT. FABRICATED REPAIR IAW SRM 57-50-3. TREATED, ALODINED IAW SRM 51-10-2. INSTALLED FASTENERS IAW 51-30-2 FAX SEALED IAW SRM 57-30-5. REPAIR DOUBLER FABRICATED FROM 2024-T3-0.080 APPROX 4.5 ICH 4.5 INCH. (M) 2L73 4F A3WE 19951215006681995121500668NM 1995 12 15 EISA95379 119950825A5754 RIB BOEING727 72782 1384029NM NR 5 LE FLAP CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON RIB ABOVE INBOARD END OF NR 5 LEADING EDGE FLAP (CORROSION UNDER WIRE STAN OFF 3 ON TOP). REMOVED CORROSION IAW SRM 51-10-6. REMOVED T-ANGLE FROM RIB IAW SRM 51-40-3. FABRICATED NEW T-ANGLE FROM AND 10136-1303 (T-ANGLE). ALODINED AND PRIMED IAW SRM 51-10-2. REINSTALLED NEW T-ANGLE IAW SRM 51-30-2 AND 51-40-3. (M) 2L73 4F A3WE 19951215006691995121500669NM 1995 12 15 EISA95387 119950825A5730 SKIN BOEING727 72782 1384029NM WS 383 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A CRACK WAS FOUND IN THE TOP OF LEADING AT WS 383 RT WING. CUT OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR IAW B727 SRM 57-30-4. (M) 2L73 4F A3WE 19951215006701995121500670NM 1995 12 15 EISA95388 119951012A5312 BULKHEAD BOEING727 72782 1384029NM BS 251 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A 2 INCH CRACK WAS FOUND AT BS 242, 1 INCH CRACK AT BS 250, 1 INCH CRACK AT BS 251 ON N.W.W LEFT PRESS BULKHEAD. STOP DRILLED CRACKS. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B727 SRM 51-40-2 AND 53-10-9. (M) 2L73 4F A3WE 19951215006711995121500671NM 1995 12 15 EISA95389 119950831A5321 FLOORBOARD BOEING727 72782 1384029NM BS 360 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 UPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AT BS 360 THE 9G BULKHEAD LOWER PORTION HAS CORROSION AT FLOORBOARDS AND LOWER WEB SURFACES. REMOVED FLOORBOARDS. FABRICATED NEW FLOORBOARD USING GILL FLOOR AND .016 SM OUTER SKIN PER AERONAUTICAL ENGINEERS STC 179850 .071 SH WEB. INSTALLED 9G BULKHEAD AND WEB IAW STC SA 129850. (M) 2L73 4F A3WE 19951215006721995121500672WP 1995 12 15 HALA95143 119951104A3350P4010049 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - FLOOR LIGHTS FROM ROW 1 TO FORWARD EMERGENCY EXIT INOP. REPLACED FORWARD FLOOR LIGHTS BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2L72 4F A6WE 19951215006731995121500673WP 1995 12 15 HALA95144 119951106A3350 EEL CONNECTOR DOUG DC9 DC951 3022051WP CABIN SHORTED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - FORWARD FLOOR EMERGENCY LIGHTS INOP. CLEARED SHORT MAIN ENTRY DOOR WIRE CONNECTION. OPERATIONAL CHECK OK. (M) 2L72 4F A6WE 19951215006741995121500674 1995 12 15 HALA95154 419951115A344256TN3467 RT UNIT DOUG DC9 DC951 3022051WP FWD FUSELAGE INOP A HALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP13679HA 47662 HNL - RADAR SCREEN WENT BLANK, LOUD BANG FROM FRONT OF AIRCRAFT, SMELL OF BURNING ELECTRICAL COMPONENTS IN COCKPIT. REPLACED RADAR INDICATOR AND WEATHER RADAR REC/TRANS. GROUND CHECKED NORMAL. (M) 2L72 4F RTA6WE 19951215006751995121500675EA 1995 12 15 HNAA9590309 219951114A7200 ENGINE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA NR 2 ENGINE BIRD STRIKE A HNAAO OTHER CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA07903HA 061 FLT NR 3169 - DCA-PHL - ON DEPARTURE FROM DCA, A NOTICEABLE AMOUNT OF SMOKE FILLED THE COCKPIT. AIRCRAFT CONTINUED ON TO PHL AND LANDED WITHOUT INCIDENT. INSPECTED ENGINES NR 1 NR 4 BLEED VALVES AND DUCTING, FLOW CONTROL VALVES AND DUCTING. INSPECTED NR 2 ACM FOR CONDITION AND SECURITY. FOUND BIRD LODGED ON INTAKE SCREEN NR 2 ENGINE. REMOVED BIRD DEBRIS AND CLEANED INTAKE SCREEN. NO OTHER DISCREPANCIES NOTED. (M) 2H74 4T4 T A20EA E4EA 19951215006761995121500676EA 1995 12 15 HNAA9590310 219951115A7200 ENGINE DHAV DHC7 DHC7102 2802708EA PWA PT6 PT6A50 52043EA NR 3 FAILED A HNAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA07903HA18801 061 86246 FLT NR 3015 - CRW-DCA - SHORTLY AFTER DEPARTURE, THE CABIN AND COCKPIT FILLED WITH SMOKE. THE AIRCRAFT RETURNED TO CRW AND LANDED WITHOUT INCIDENT. PERFORMED GROUND RUN WITH LEFT PACK ONLY, COULD NOT DUPLICATE, MEL 21-1. AT RON, REMOVED AND REPLACED NR 3 ENGINE. (M) 2H74 4T4 T A20EA E4EA 19951215006771995121500677NM 1995 12 15 HNAA9590908 119951115A3231YCRS14 BEARING DHAV DHC8 DHC8102 2809003NM LT MLG DOOR FAILED A HNAAO OTHER J WARNING INDICATION CLCLIMB 1 EA07909HA27259 018 FLT NR 3126 - CLT-EWN - AFTER GEAR RETRACTION, THE LEFT GEAR DOOR INDICATION STAYS ON. THE FLIGHT CONTINUED ON TO EWN AND LANDED WITHOUT INCIDENT. FOUND FORWARD GEAR DOOR ACTUATING MECHANISM ROLLER BEARING LOCKED UP. REMOVED AND REPLACED THE ROLLER BEARING AND ADJUSTED THE FORWARD GEAR DOOR ACTUATOR ROD END LENGTH. (M) 2H72 4T RTA13NM 19951215006781995121500678NM 1995 12 15 HNAA9592503 119951103A3260MS3476L833SW CONNECTOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAO OTHER N FALSE WARNING APAPPROACH 1 EA07925HA19783 111 FLT NR 3066 - MCO-TLH - AFTER GEAR EXTENSION, THE NOSE GEAR SHOWED UNSAFE. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TLH WITHOUT INCIDENT. REMOVED AND REPLACED THE CANNON PLUG FOR THE DRAG STAY SENSOR. (M) 2H72 4T RTA13NM 19951215006791995121500679NM 1995 12 15 HNAA9593301 119951101A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07933HA1226612266 347 134 FLT NR 3166 - MCO-TCB - THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. PERFORMED ALTERNATE GEAR EXTENSION AND LANDED IN TCB WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2H72 4T RTA13NM 19951215006801995121500680NM 1995 12 15 HNAA9593402 119951102A521085210240005 UPPER STRUT DHAV DHC8 DHC8102 2809003NM PAX DOOR FAILED A HNAAK NONE O OTHER ININSP/MAINT 1 EA07934HA18600 139 FLT NR 3473 - RDU-BWI - UPON ARRIVAL IN BWI, THE PASSENGER DOOR WOULD NOT OPEN WITHOUT OUTSIDE ASSISTANCE. FOUND THE LEFT FORWARD UPPER STRUT CRACKED. REMOVED AND REPLACED THE LEFT FORWARD UPPER STRUT. (M) 2H72 4T RTA13NM 19951215006811995121500681NM 1995 12 15 HNAA9593711 119951116A6123M390166105L RELAY DHAV DHC8 DHC8102 2809003NM AUTOFEATHER SYS FAILED A HNAAO OTHER N FALSE WARNING CLCLIMB 1 EA07937HA18240 148 FLT NR 3096 - JAX-TPA - THE AUTOFEATHER ARM LIGHT IS INTERMITTENT ON CLIMB-OUT. THE FLIGHT CONTINUED ON TO TPA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RELAY 6121-K5 AND CHECKED WIRING AT BACK OF AUTOFEATHER SELECT SWITCH. (M) 2H72 4T RTA13NM 19951215006821995121500682NM 1995 12 15 HNAA9594213 119951118A3230864202 DN/UPLOCK SENSOR DHAV DHC8 DHC8102 2809003NM NLG FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07942HA17552 163 FLT 3465 - MIA-MCO - ON FINAL APPROACH WITH GEAR SELECTED DOWN AND THREE GREEN, THE NOSE GEAR DOORS BEGAN TO CYCLE OPEN AND CLOSED WITH ACCOMPANYING INDICATIONS ON FLIGHT DECK. AIRCRAFT LANDED IN MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR DRAG STRUT DOWN/UPLOCK SENSOR. (M) 2H72 4T RTA13NM 19951215006831995121500683NM 1995 12 15 HNAA9595504 119951104A33506013211X EEL POWER SUPPLYGRIMES DHAV DHC8 DHC8102 2809003NM CABIN INOP A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07925HA15587 ORF63 111 FLT NR 3040 - FLL TO TPA - DURING PREFLIGHT WALKAROUND, FOUND THE FIRST 2 RED FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE POWER SUPPLY AT 3352-PS2. (M) 2H72 4T RTA13NM 19951215006841995121500684NM 1995 12 15 HNAA9598005 119951105A5210MS24586C140 SPRING DHAV DHC8 DHC8102 2809003NM PAX DOOR MISSING A HNAAK NONE O OTHER ININSP/MAINT 1 EA07980HA4512 376 FLT NR 80 - ORF-PHF - DURING PREFLIGHT CHECK, UNABLE TO CLOSE MAIN CABIN DOOR. FOUND TOP STEP SPRING MISSING. DOOR OPERATES NORMALLY WITH STEP POSITIONED PROPERLY. REPLACED SPRING AND DOOR OPERATES NORMALLY. (M) 2H72 4T RTA13NM 19951215006851995121500685EU 1995 12 15 P2RA950021 119951031A3350311701 BATTERY PACK AIRBUS300 A300B4203 3930306EU L-4 DOOR DISCHARGED A P2RAK NONE L NO TEST ININSP/MAINT 1 WP2314977 0274 274 L-4 DOOR OVERHEAD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED 2 BATTERY PACKS PER MM 33-51-14. LIGHT OPS CHECK GOOD. (M) 2L72 4F A35EU 19951215006861995121500686EU 1995 12 15 P2RA950022 119951106A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R-2 DOOR INOP A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 R-2 DOOR WOULD NOT DISARM. MANUALLY DISARM GIRT BAR. REINSTALLED GIRT BAR AND CHECKED GOOD PER MM 52-22-22. (M) 2L72 4F A35EU 19951215006871995121500687EU 1995 12 15 P2RA950023 119951112A29136506606 HYD PUMP AIRBUS300 A300B4203 3930306EU YELLOW SYSTEM FAILED A P2RAH DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 WP2314975 261 YELLOW HYDRAULIC SYSTEM FAILED IN FLIGHT. HYDRAULIC PRESSURE ZERO. NO FLUID LOSS. FOUND ENGINE DRIVEN PUMP FAILED. REPLACED PUMP AND CASE FILTER. OPS AND LEAK CHECKS GOOD IAW 29-11-32. (M) 2L72 4F A35EU 19951215006881995121500688EU 1995 12 15 P2RA950024 119951109A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R-2 DOOR INOP A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 ON ARRIVAL, UNABLE TO DISARM R-2 DOOR. REINSTALLED GIRT BAR IN FORWARD END LATCH, OPS CHECKED GOOD PER MM 52-22-22. (M) 2L72 4F A35EU 19951215006891995121500689EU 1995 12 15 P2RA950025 119951109A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R-2 DOOR INOP A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 R-2 DOOR SOMETIMES DOES NO DISARM. INSPECTED, CLEANED AND LUBRICATED DOOR. NO PROBLEMS FOUND, OPS CHECKED GOOD. (M) 2L72 4F A35EU 19951215006901995121500690 1995 12 15 S2YA950028 419951107A22101303800031 RUDDER BOOST SYS BEECH 1900 1900D 1154162CE LT ENGINE INOPERATIVE A S2YACD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TOTAKEOFF 1 GL13118SK699 UE108 THE CREW OF FLIGHT NR 1902 AT MKE, ABORTED TAKEOFF ROLL AFTER THEY FELT RESISTANCE AT THEIR RUDDER PEDALS. THE PROBLEM WAS THOUGHT TO BE THE RUDDER BOOST SYSTEM. THEY RETURNED TO THE GATE AND MAINTENANCE MEL'D THE SYSTEM. (M) 2L72 4T RTA24CE 19951215006911995121500691EU 1995 12 15 SIMA953131 119951109A33503012000 EEL POWER SUPPLY AEROSPATR72 ATR72212 EU CABIN INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT3165 264 263 ORD - FLT 4233 - AFT EMERGENCY LIGHTS WILL NOT SHUT OFF, ILLUMINATED CONTINUOUSLY. MX REMOVED AND REPLACED POWER SUPPLY. SYSTEM OPS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215006921995121500692EU 1995 12 15 SIMA953141 119951110A33503011206 EEL AEROSPATR42 ATR42300 8680920EU RT FWD FUS INOPERATIVE A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21262AT3455 0262 RFD - DURING PS-2 CHECK, MAINTENANCE DISCOVERED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW JIC 33512-0. PERFORMED OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215006931995121500693EU 1995 12 15 SIMA953171 119951113A3350 EEL WIRE AEROSPATR72 ATR72212 EU CABIN BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT 263 ORD - FLT 4067 - AIRSTAIR EMERGENCY EXIT LIGHT INOP. REPAIRED BROKEN GROUND WIRE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215006941995121500694EU 1995 12 15 SIMA953191 119951115A3230C4589000 UPLOCK BOX AEROSPATR72 ATR72212 EU RT MLG MALFUNCTIONED A SIMAO OTHER J WARNING INDICATION CRCRUISE 1 SW21438AT1384 4615 438 DFW - FLT 3814 - RIGHT MAIN GEAR CAME DOWN IN FLIGHT, RED UNLOCK LIGHT CAME ON OVERHEAD GREEN SYSTEM CYCLES. TROUBLESHOT, FOUND UPLOCK BOX NOT FUNCTIONING PROPERLY. RAI RIGHT UPLOCK BOX, IAW 32-31-00 OF AMM. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215006951995121500695NE 1995 12 15 SIMA953212 219951117A73215071T20P16 DECU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ENGINE FAILED A ASIMAAE UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT DEDESCENT 1 SW21344SB5022 ECDT1752 340B344 785517 CRS - FLT 3570 - EN ROUTE FROM CRP TO DFW AT FL 120, LEFT ENGINE FAILED WITHOUT ANY INDICATION OF AUTO-RELIGHT. AFTER LEFT ENGINE WAS FEATHERED, THE RIGHT ENGINE DEVELOPED MOMENTARY SURGE RESEMBLING COMPRESSOR STALLS. THE AIRCRAFT HAD BEEN OPERATING IN LIGHT ICING CONDITIONS. PILOT REDUCED POWER SLIGHTLY ON RIGHT ENGINE AND TORQUE STABILIZED. PILOT DECLARED EMERGENCY AND DIVERTED TO CRS WHERE AN UNEVENTFUL LANDING WAS MADE. PEFORMED BOROSCOPE AND RAI'D DECU (DIGITAL ELECTRONIC CONTROL UNIT). OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 19951215006961995121500696EU 1995 12 15 SIMA953251 119951121A33503351115000 EEL WIRE AEROSPATR72 ATR72212 EU PASSENGER DOOR BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21369AT 369 ORD - FLT 4187 - CREW REPORTED PASSENGER STAIRS EMERGENCY LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRES UNDER TOP STEP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951215006971995121500697NM 1995 12 15 TA0A119502 119951105A3350 EEL WIRE GRIMES BOEING727 727254 138408LNM CABIN BROKEN A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15914TS 20251 EMERGENCY PATH LIGHTING AT MID CABIN INOP. REPAIRED BROKEN WIRE AT ROW 7. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951215006981995121500698NM 1995 12 15 TA0A119503 119951108A3350900835A BATTERY PACK GRIMES BOEING727 727225 1384077NM LT EXTERIOR DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 7710 20445 DURING L/S, FOUND LEFT EXTERIOR EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK FOR LEFT EXTERIOR EMERGENCY LIGHT. OPS CHECKED OK. (M) 2L73 4F A3WE 19951215006991995121500699NM 1995 12 15 TAOA119501 119951105A3350900835A BATTERY PACK GRIMES BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS 22415 20441 AISLE OVERHEAD EMERGENCY SIGN AT ROW 15 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19951215007001995121500700NM 1995 12 15 TAOA119504 119951107A2611824P4 SMOKE DETECTOR BOEING727 727254 138408LNM AFT LAVATORY DEFECTIVE A TAOAO OTHER N FALSE WARNING CRCRUISE 1 EA15916TS 2091 20437 AFT LAVATORY SMOKE DETECTOR INOPERABLE, GOES OFF IN FLIGHT. DISCONNECTED SMOKE DETECTOR. REPLACED SMOKE DETECTOR FOR AFT LAVATORY, CHECKS OK. (M) 2L73 4F A3WE 19951215007011995121500701NM 1995 12 15 TAOA119505 119951108A3350900835A BATTERY PACK BOEING727 727225 1384077NM LT EXTERIOR DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15918TS 7710 20445 LEFT FORWARD OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK FOR LEFT FORWARD OVERWING EMERGENCY LIGHT. OPS CHECKED OK. (M) 2L73 4F A3WE 19951215007021995121500702NM 1995 12 15 TAOA119506 119951115A2752MS93911302E DRIVE MOTOR BOEING727 727225 1384077NM LT TE FLAPS LEAKING A TAOAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 EA15918TS MX96131D 20445 ON CLIMB-OUT FROM LGA, PASSING THROUGH 1700 FEET, A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO. COMPLETED ABNORMAL PROCEDURE AND LANDED UNEVENTFULLY. FOUND FLAP DRIVE MOTOR LEAKING. REPLACED SAME, SERVICED HYDRAULIC RESERVOIRS. ALL CHECKED OK PER MM 27-51-62. REPLACED CASE DRAIN FILTERS NR 1 AND NR 2. LEAK CHECKED OK ON ENGINE RUN. (M) 2L73 4F A3WE 19951215007031995121500703NM 1995 12 15 TAOA119507 119951117A3240106128718 BRAKE BOEING727 727254 138408LNM NR 4 SMOKING A TAOAO OTHER B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 EA15913TS 9570 20250 NR 4 BRAKE SMOKING ON LANDING. CHECKED BRAKE PER MM 32-40, CHECKED GOOD. NR 4 BRAKE CHANGED ON OVERNIGHT. OK FOR SERVICE. (M) 2L73 4F A3WE 19951215007041995121500704NM 1995 12 15 TWRA9561 119951116A217025TD47 COALESCER BOEING747 747282B 1384860NM AC BAY DIRTY A TWRAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA15611FF 20502 DURING TAKEOFF WITH PACKS TURNED ON, CABIN FILLED WITH BLUE SMOKE FOR A SHORT PERIOD OF TIME. MAINTENANCE AT JFK CHECKED ALL FOUR ENGINES FUEL HEATERS AND BLEED SYSTEMS. ALL FOUND OK. COALESCER BAGS WERE REPLACED IAW 21-51-05. ALSO, CLEARED BLOCKAGE IN THE NR 1 PACK DRAIN LINE. (M) 2L74 4F A20WE 19951215007051995121500705WP 1995 12 15 USAA951158 119951106A5210 SKIN DOUG DC9 DC982 3022082WP PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND TWO .5 INCH CRACKS IN PAX DOOR RIVNUT BELOW BAYONET. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01. (M) 2L72 4F A6WE 19951215007061995121500706NM 1995 12 15 USAA951167 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 25, WL 207.75. DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 40020, REF SB 737-53-1120. (M) 2L72 4F RTA16WE 19951215007071995121500707NM 1995 12 15 USAA951168 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK NDT INSPECTION, FOUND 1.25 INCH CRACK FLOOR BEAM, .75 INCH CRACK SEAT TRACK SUPPORT CHANNEL DETECTED BY VISUAL INSPECTION, STATION 520 FLOOR BEAM LBL 25, WL 207.75. DOUBLERS INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 40020, REF SB 737-53-1120. (M) 2L72 4F RTA16WE 19951215007081995121500708NM 1995 12 15 USAA951169 119951103A5330 SKIN BOEING737 737401 1384701NM BS 265-277 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO SKIN DENTS, AT STATION 265 TO 277 ABOVE STRINGER 11 R AND 13 R. CUTOUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. REPAIRED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 19951215007091995121500709NM 1995 12 15 USAA951170 119951103A532065C333755 INTERCOSTAL BOEING737 737401 1384701NM BS 952 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, APPROXIMATELY 1 INCH BY 12 INCH AREA CORRODED STATION 952 BETWEEN LBL 25 AND LBL 51. REPAIRED AND REPLACED INTERCOSTAL. REPAIRED PER SRM DOCUMENT 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951215007101995121500710NM 1995 12 15 USAA951181 119951103A532065479573 SILL BOEING737 737401 1384701NM BS 794-847 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 IND - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL 4 INCH BY 4 INCH CORRODED AREAS BETWEEN BS 794 AND BS 847 (AFT CARGO DOORWAY SILL). INSTALLED NEW WEB. REPAIRED PER SRM 51-10-02, DRAWING 65-47957. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951215007111995121500711NM 1995 12 15 USAA951187 119951103A532065C333701 INTERCOSTAL BOEING737 737401 1384701NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORRODED AREA, ON INTERCOSTAL AT 25, BETWEEN BS 947 AND BS 967, WL 208. REMOVED CORRODED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL FROM STOCK P/N 65C333701. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951215007121995121500712NM 1995 12 15 USAA951188 119951103A5320 BEAM BOEING737 737401 1384701NM BS 942 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 20 INCH CORRODED AREA, ON BEAM AT STATION 947 LBL 5 - RBL 15. INSTALLED CAP AND REPAIRED ANGLE. REPAIRED PER EA 40080. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951215007131995121500713NM 1995 12 15 USAA951189 119951103A532065C80735116 ANGLE BOEING737 737401 1384701NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 59 INCHES CORRODED AREA, BS 947-1006, S-17 L (AFT ENTRY DOOR Z-ANGLE). REMOVED CORRODED CHORD Z-ANGLE. DRILLED UP AND INSTALLED NEW ANGLE FROM STOCK. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19951215007141995121500714WP 1995 12 15 USAA951196 119951107A5330 SKIN DOUG DC9 DC931 3022065WP FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19974VJ73000 47130 PIT - DURING C-1 CHECK INSPECTION ACCOMPLISHED SID PSE 53.09.031A AND FOUND A 1 INCH SKIN CRACK TOP AFT DOOR STOP ADJUST HOLE. VISUAL VERIFIED BY NDT. CUT OUT CRACKED AREA INSTALLED FILLER AND .071 INCH AND .100 INCH DOUBLER REPAIR PER USAIR EA 31604 AND SRM 53-05 FIG 26A. (M) 2L72 4F A6WE 19951215007151995121500715 1995 12 15 USAAD95006 419951112A3421258733511 VERTICAL GYRO DOUG DC9 DC931 3022065WP NR 1 FAILED A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19951VJ 47576 FLT NR 2058 - CAPTAINS VERTICAL GYRO FAILED ON CLIMB-OUT. FLIGHT RETURNED TO FIELD. REPLACED NR 1 VERTICAL GYRO. OPERATIONAL CHECK WAS NORMAL. (M) 2L72 4F A6WE 19951215007161995121500716SO 1995 12 15 WTAA950295 119951109A77120029R TQ IND EMB 120 EMB120RT SO COCKPIT FAILED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17250YV 120250 RNO - RIGHT ENGINE TORQUE INDICATOR FAILED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE TORQUE INDICATOR. TORQUE INDICATIONS OPERATIONAL CHECK NORMAL DURING ENGINE GROUND RUNS. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951215007171995121500717SO 1995 12 15 WTAA950296 119951109A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT GEAR FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 WP17122AM 120013 LAX - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED FOLLOWING GEAR RETRACTION AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR HYDRAULIC ACTUATOR. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951215007181995121500718SO 1995 12 15 WTAA950297 119951111A32301959500007 ACTUATOR LINKAGE EMB 120 EMB120RT SO LT GEAR OUT OF ADJUST A WTAAO OTHER J WARNING INDICATION APAPPROACH 1 WP17122AM 120013 RNO - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED FOLLOWING GEAR EXTENSION. CREW ACCOMPLISHED EMERGENCY GEAR EXTENSION PROCEDURES PER QRH MANUAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE REPORTED DISCREPANCY DURING GROUND RETRACTION CHECK. AIRCRAFT RETURNED TO SERVICE. NOTE, LEFT MAIN LANDING GEAR ACTUATOR LINKAGE ADJUSTED DURING RON MAINTENANCE. (M) 2L72 4T RTA31SO 19951218000021995121800002NM 1995 12 18 P5CA9500864 119951203A5347 SEAT TRACK BOEING747 747132 1384882NM COPILOT SEAT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23857FT 20246 FOUND CO-PILOT'S OUTBOARD FORWARD SEAT TRACK CRACKED AT AFT END. TRANSFERRED TO MAINTENANCE CARRYOVER ITEM 857016, TRACK TO BE REPLACED IAW MM 25-11-01. 2L74 4F A20WE 19951222000011995122200001NE 1995 12 22 9520251156 219951213A7230 COMPRESSOR DOUG DC10 DC1040 3023508WP PWA JT9 JT9D20J 52054NE NR 1/3 ENGINES STALLED A NWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LDLANDING 1 GL01156US 46765 686164 DURING LANDING WHILE IN REVERSE THRUST, THE NR 1 AND NR 3 ENGINES COMPRESSOR STALLED WITH THE EGTS GOING TO 980 DEGREES FOR 5 SECONDS BEFORE THE ENGINES WERE SHUTDOWN. THE ENGNE WAS INSPECTED, BORESCOPED AND A GROUND RUNUP CONFIRMED PROPER OPERATION OF THE ENGINES. 2L73 4F4 F A22WE E20EA 19951222000021995122200002NE 1995 12 22 9520269953 219951206A7230 COMPRESSOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 1 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01918RW 47158 657515 ONE OR BOTH ENGINES EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES. THE NR 1 ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. SNOW AND SLUSH INGESTION IS SUSPECTED AS THE PRIME CAUSE OF THE COMPRESSOR STALL. 2L72 4F4 F A6WE E2EA 19951222000031995122200003NE 1995 12 22 9520272703 219951205A7230 COMPRESSOR BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 2 ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL018878Z 21451 696466 NR 2 ENGINE STALLED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. NO DISCREPANCIES WERE NOTED ON INSPECTION OR DURING RUNUP. AIRCRAFT CONTINUES IN SERVICE. NOTE: STRONG CROSSWINDS NOTED AT TIME OF TAKEOFF ATTEMPT. 2L73 4F4 F A3WE E2EA 19951222000041995122200004NM 1995 12 22 9520282714 119951212A4900 APU BOEING727 7272S7 138407ZNM RT WW ON FIRE A NWAAO OTHER A FLAME/FIRE ININSP/MAINT 1 GL01718RC 22344 DURING WALK-AROUND, BLUE FLAMES AND SMOKE WERE NOTICED IN THE AREA OF THE APU EXHAUST DUCT. APU SHUTDOWN AND FLAMES SUBSEQUENTLY EXTINGUISHED. NO FIRE BOTTLES WERE USED. MAINTENANCE INSPECTED THE AREA AND FOUND NO DAMAGE. THE APU WAS PLACED ON MEL. 2L73 4F A3WE 19951222000051995122200005NM 1995 12 22 9520292707 119951209A4900 APU BOEING727 727225 1384077NM RT WW ON FIRE A NWAAF ACTIVATE FIRE EXT. A FLAME/FIRE ININSP/MAINT 1 GL01816EA 22553 PRIOR TO ENGINE START, GROUND PERSONNEL NOTICED A FLAME IN THE RIGHT WHEEL WELL AND APU EXHAUST DUCT AREA. THE APU WAS SHUTDOWN USING A FIRE SWITCH AND FLAMES EXTINGUISHED. MAINTENANCE REPLACED THE APU FIRE EXTINGUISHER BOTTLE, CLEANED THE WHEEL WELL AREA AND INSPECTED THE AREA FOR DAMAGE. NO DAMAGE NOTED THE APU WAS PLACED ON MEL. 2L73 4F A3WE 19951222000061995122200006WP 1995 12 22 9520309968 119951214A3222 SCHRADER VALVE DOUG DC9 DC931 3022065WP NLG STRUT LEAKING A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019332 47264 DURING CLIMB, THE AIRCRAFT FAILED TO SHIFT INTO FLIGHT MODE. PULLED GROUND SHIFT CIRCUIT BREAKERS TO GET AIRCRAFT TO SHIFT INTO FLIGHT MODE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT SCHRADER VALVE LEAKING. REPLACED VALVE AND SERVICED NOSE STRUT. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222000071995122200007NE 1995 12 22 9520312705 219951209A7320 FCU WATER TRAP BOEING727 727225 1384077NM PWA JT8 JT8D15 52051NE NR 3 ENGINE CONTAMINATED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01802EA 22433 696534 NR 3 ENGINE WAS SLOW TO ACCELERATE DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE FCU MOISTURE TRAP. SUBSEQUENT ENGINE RUN-UP WAS SATISFACTORY. 2L73 4F4 F A3WE E2EA 19951222000081995122200008WP 1995 12 22 9520329851 119951208A7722 EGT INDICATOR DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01760NC 47708 696686 NR 1 ENGINE EGT SYSTEM FAILED ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EGT INDICATOR WITH A SERVICEABLE UNIT. SYSTEM CHECKED OK ON RUNUP. 2L72 4F4 F A6WE E2EA 19951222000091995122200009NM 1995 12 22 9520332201 119951208A7711 EPR SYST BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 2 ENGINE MALFUNCTIONED A NWAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 GL01210US 22154 695264 NR 2 ENGINE EPR INDICATION ABNORMALLY HIGH ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND RUNUP. NORMAL INDICATIONS WERE OBSERVED. THE FLIGHT CONTINUED AS SCHEDULED WITH THE NR 2 EPR SYSTEM ON MEL. 2L73 4F4 F A3WE E2EA 19951222000101995122200010WP 1995 12 22 9520349953 119951208A7711 EPR INDICATOR DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01918RW 47158 666669 NR 1 EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR AND PERFORMED A TAKEOFF POWER ASSURANCE RUN. THE NR 1 EPR SYSTEM OPERATION WAS NORMAL ON RUNUP. 2L72 4F4 F A6WE E2EA 19951222000111995122200011NE 1995 12 22 9520359953 219951208A7320 PT2 PROBE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9A 52048NE NR 1 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01918RW 47158 666669 NR 1 ENGINE EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE PT2 LINE, LEAK CHECKED THE PT2 SYSTEM AND REPLACED THE NOSE DOME/PT2 PROBE ASSEMBLY. SUBSEQUENT RUNUP WAS SATISFACTORY. 2L72 4F4 F A6WE E2EA 19951222000121995122200012WP 1995 12 22 9520369910 119951214A2150 DUCT DOUG DC9 DC931 3022065WP COOLING TURBINE OUT OF POSITION A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01960N 47256 DURING CLIMB, THE AIRCRAFT WOULD NOT PRESSURIZE ADEQUATELY. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND DUCT POSITIONED INCORRECTLY ON COOLING TURBINE. REPOSITIONED AND SECURED DUCT. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222000131995122200013NM 1995 12 22 95FDEA01899 119951214A3230 RETRACT MECH BOEING727 727225 1384077NM LANDING GEAR MALFUNCTIONED A FDEAO OTHER J WARNING INDICATION CLCLIMB 1 SO25465FE 21289 ON CLIMBOUT WHEN RETURNING GEAR LEVER TO OFF POSITION, RED GEAR LIGHTS CAME ON AND GEAR BEGAN TO EXTEND. THE GEAR LEVER WAS QUICKLY RETURNED TO THE UP POSITION RESULTING IN A PARTIAL RETRACTION AT 240 KIAS. COULD NOT DUPLICATE. JACKED AIRCRAFT AND CYCLED GEAR SEVERAL TIMES, NO DEFECTS NOTED. INSPECTED LANDING GEAR DOORS AND WHEEL WELLS, NO DEFECTS NOTED. OK FOR SERVICE. 2L73 4F A3WE 19951222000141995122200014NM 1995 12 22 95UAL900314 119951213A3350 EEL BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297259U 21406 EMERGENCY LIGHT OVER AIRSTAIR ENTRANCE INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L73 4F4 F A3WE E2EA 19951222000151995122200015NM 1995 12 22 95UAL900315 119951213A3350 EEL LAMP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29944UA 26683 EXTERIOR EMERGENCY EXIT LIGHT AT DOOR ONE RIGHT INOP. REPLACED LAMP, CHECKS OK. 2L72 4F4 FRTA16WE E2GL 19951222000161995122200016WP 1995 12 22 95UAL900316 119951214A3350 EEL LAMP DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP291814U 46613 AISLE EEL LIGHT AT FORWARD DOOR 2L HAS ONE LAMP INOPERATIVE. REPLACED LAMP. 2L73 4F4 F A22WE E23EA 19951222000171995122200017NM 1995 12 22 DL72L954688 119951212A5320 WEB BOEING727 727232 1384082NM RT TORQUE BOX CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27504DA 21306 FOUND ON E2 LETTER CK, .2187 INCH CRACK IN 48 SECT TORQUE BOX WEB LIGHTENING HOLE RT FWD SIDE. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19951222000181995122200018NM 1995 12 22 DL72S954692 119951209A53126516350344 BLKHD WEB BOEING727 727232 1384082NM FS 1183 CRACKED A aDALAK NONE O OTHER ININSP/MAINT 1 SO27519DA 21470 THE BS 1183 BULKHEAD WEB WAS FOUND CRACKED IN TWO LOCATIONS AT RBL 18. THERE IS A 1 INCH CRACK AT WL 166.3 TO WL 167.5 AND A .1875 INCH CRACK AT WL 169. THE WEB IS A BONDED ASSEMBLY OF 2024-T3 CLAD WITH A LOCAL THICKNESS OF 0.050 INCH. THE CRACK LOCATIONS ARE OUTSIDE OF THE INSPECTION AREA SPECIFIED BY BOEING SERVICE BULLETIN 727-53-171. MTC REPORTS THAT THE VERTICAL STIFFENER AT RBL 18, THE TOPIC OF BOEING SB 727-53-0202, IS NOT DAMAGED. THE CRACKS WILL BE STOP DRILLED AND A REPAIR DOUBLER INSTALLED PER DL ERA 302880-14. 2L73 4F A3WE 19951222000191995122200019NM 1995 12 22 DL72S954698 119951123A5400 ANGLE BOEING727 727232 1384082NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 UPON HMV, FOUND NR 2 ENG PYLON CIRCUMFERENTIAL ANGLE FOR MOUNTING SURFACE OF FWD COWL HAS TEMPORARY REPAIR INSTALLED. FABRICATED AND INSTALLED NEW ANGLE PER MM 53-11-0. 2L73 4F A3WE 19951222000201995122200020NM 1995 12 22 DL72S954699 119951208A5522 TE SKIN BOEING727 727232 1384082NM ELEVATOR SEPARATING A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 AT HMV, TRAILING EDGE OF LEFT ELEVATOR SEPARATED IN SEVERAL PLACES. REPAIRED PER MM 55-20-0 PG 801. 2L73 4F A3WE 19951222000211995122200021NM 1995 12 22 DL72S954704 119951211A3350 EEL POWER PACK BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27526DA 21586 EMERGENCY LIGHT TRACKS BETWEEN SECTION 12A AND 19A. REPLACED EMERGENCY PACK POWER SUPPLY AND BATTERY PACK CHECKS OK. 2L73 4F A3WE 19951222000221995122200022NM 1995 12 22 DL72W954693 119951012A533065545839 SKIN BOEING727 727247 138408FNM FS 1070 GOUGES A DALAK NONE O OTHER ININSP/MAINT 1 SO272816W 20872 MTC REPORTS, 3 GOUGES IN THE FUSELAGE SKIN BELOW AND JUST AFT OF THE L2 DOOR LWR AFT CORNER. THE FIRST GOUGE IS LOCATED JUST AFT OF FS 1070, IT IS 7 INCHES LENGTH, HAS A MAX DEPTH OF 0.010, AND RUNS PERPENDICULAR TO S-18L. IT WILL BE BLENDED AND TREATED PER B727 SRM 53-30-1 FIG 1 DETAIL 1. THE OTHER TWO GOUGES ARE LOCATED AT FS 1070, BETWEEN S-17L AND S-18L. THE FWD GOUGE IS 4 INCHES IN LENGTH AND HAS A MAX DEPTH OF 0.014. THE AFT GOUGE HAS A MAX DEPTH OF 0.028 AND IS 5 INCHES IN LENGTH. REPAIRED PER DL ERA 302623-14. 2L73 4F A3WE 19951222000231995122200023NM 1995 12 22 DL73S954682 119951212A2910 HYD LINE BOEING737 737232 1384475NM LT MLG RUPTURED A DALAK NONE KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 SO27324DL 23096 A/C 324 FLT 1500, JUST PRIOR TO TOUCHDOWN MASTER CAUTION LIGHT CAME ON FOR A-SYS HYD LEAK. WHILE TURNING OFF RUNWAY A-SYS HYD QUANTITY WENT TO ZERO, FLAP LEVER WAS LEFT AT 30 DEGREES TO AGREE WITH FLAPS. FOUND HYD PRESSURE LINE LEAKING ON LEFT LANDING GEAR ACTUATOR. REPLACED LINE. 2L72 4F RTA16WE 19951222000241995122200024NM 1995 12 22 DL73S954683 119951212A2150 HEAT EXCHANGER BOEING737 737232 1384475NM RT PACK DIRTY A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27303DL 23075 IN FLT STRONG SMOKE SMELL IN CABIN, BOTH LAV SMOKE ALARMS WENT OFF RETURNED ATL. REMOVED DEBRIS FROM RIGHT PACK HEAT EXCHANGER, RAN ENGINES AND PACKS ALL NORMAL. 2L72 4F RTA16WE 19951222000251995122200025NE 1995 12 22 DL76L954695 219951213A7200 ENGINE BOEING767 767332 1382001NM PWA 4060 PW4060 52119NE NR 1 VIBRATION A DALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO27179DN 25144 724638 ABNORMAL VIB INDICATIONS ON LT ENG FLUX N1 .8 TO 3.8 ON PERFORMANCE PAGE, N1 AND N2 NORMAL, BB FLUX 1.0 TO 3.8. RETURNED ATL AND PERFORMED FAN TRIM BALANCE PER MM 72-00-00. RETURNED TO SERVICE. 2L72 4F4 FRTA1NM E24NE 19951222000261995122200026NM 1995 12 22 DLM88954674 119951210A3320 LIGHT SOCKET DOUG MD88 MD88 3023688NM CABIN SHORTED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27945DL 49818 CREW REPORTS, BURNED ODOR AT SEAT ROW 30 TO 31. FOUND SIDEWALL LIGHT SOCKET AND BULB BURNED. REMOVED AND DISCONNECTED BALLAST FWD TO MCO AND PLAC PER MEL 33-00-02. REPLACED LIGHT SOCKET AND OPERATION NORMAL. 2L72 4F RTA6WE 19951222000271995122200027 1995 12 22 DLM88954691 419951213A3425 AHRS UNIT 4608000307 DOUG MD88 MD88 3023688NM NR 2 FAILED A DALAO OTHER N FALSE WARNING TOTAKEOFF 1 SO27909DL 0958 49540 LOST HDG/ATT INDICATION ON LIFT OFF FROM BOS. ALSO, HAD IND OF NR 2 PLATFORM AHRS FAILED. INST LOST WERE ON FIRST OFFICER'S SIDE. WHEN EFIS WAS SELECTED TO BOTH ON ATT INFO WAS REGAINED ON FIRST OFFICER'S SIDE. REPLACED NR 2 AHRS UNIT AND NR 2 SYMBOL GEN, BOTH CK PER MM OPERATION NOW NORMAL IN ALL MODES. PERFORMED RETURN TO SERV TEST, ALL OK. 2L72 4F RTA6WE 19951222000281995122200028EU 1995 12 22 WWMA9500088 119951213A2932GPP125012 PRESS TRANS SAAB SF340 340B 7860101EU MAIN HYD SYST DEFECTIVE A WWMAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP15312AE 340B312 MAIN HYDRAULIC LIGHT ILLUMINATED AND THE PRESSURE INDICTIONS WERE AT THE RED LINE. THE CREW PERFORMED AN EMERGENCY LANDING GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED THE GEAR DOORS AND INSTALLED THE LANDING GEAR PINS. THE AIRCRAFT WAS FERRIED TO LAX WHERE THE HYDRAULIC PRESSURE TRANSMITTER WAS REPLACED. NO LEAKS OR OTHER PROBLEMS WERE FOUND. THE AIRCRAFT WAS RELEASED TO SERVICE. 2L72 4T RTA52EU 19951222000301995122200030SO 1995 12 22 95ZZZX6781 119951115A32304198301 DOWNLOCK PIPER PA31 PA31350 7103110SO RT MLG LACK OF LUBE A ECAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA1178GH 317852121 FRG - FLT 1 - AFTER TAKEOFF, GEAR UNSAFE LIGHT ILLUMINATED. UPON GEAR EXTENSION, RT MAIN GEAR LIGHT WAS NOT ILLUMINATED. THE AIRCRAFT RETURNED TO FRG. AFTER LANDING AT FRG, TOWER OBSERVED RT INBOARD GEAR DOOR RAISING, AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT WAS RETURNED TO MAINTENANCE HANGAR. MOISTURE AND ICE WERE OBSERVED ON LANDING GEAR. RT MLG DOWN AND LOCK HAD VISIBLE MOISTURE AND WAS STIFF TO OPERATE. AIRCRAFT WAS HANGARED. NEXT DAY, 11-16-96, LANDING GEAR WAS DRY. CLEANED AND LUBED, PERFORMED SEVERAL GEAR SWINGS, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 3O A20SO 19951222000311995122200031WP 1995 12 22 95ZZZX6782 119951027A2612 GROMMETS DOUG DC8 DC8F55 3021928WP NR 4 ENGINE MISSING A CKSAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL236161C56305 45856 KMIA - FLT 68305 - MASTER FIRE WARNING SHUT DOWN. IN MIA TERMINAL AREA, NR 4 ENGINE MASTER FIRE WARNING, SHUT DOWN NR 4 ENGINE. NORMAL LANDING. FOUND SEVERAL FIRE LOOP MOUNTING BRACKETS LOOSE AND GROMMETS MISSING. REPAIRED AND REPLACED MOUNTING BRACKETS. INSTALLED MISSING GROMMETS. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES WITH BLEED AIR ON. NO FIRE WARNING. FIRE WARNING SYSTEM OPS NORMAL IAW MM 26-2-0. REFERENCE, OPERATOR CONTROL NR CKSA95140. 2L74 4F 4A25 19951222000321995122200032NM 1995 12 22 AALA951757 119951005A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07334AA 22332 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 4B FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 4B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000331995122200033NM 1995 12 22 AALA951759 119951006A33508100022002 EEL ASSY BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, THE EMERGENCY FLOOR EXIT PATH LIGHTS AT ROW 24H AND AFT GALLEY CROSS AISLE LIGHTS WERE FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY AT ROW 24H AND AFT GALLEY CROSS AISLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000341995122200034NM 1995 12 22 AALA951760 119951006A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739365 24046 SFO - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT FLOOR PATH LIGHTS FOUND INOPERATIVE. SECURED LOOSE CONNECTION AT SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000351995122200035NM 1995 12 22 AALA951778 119951011A3350 EEL CONNECTOR BOEING767 767223 1385123NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07338AA 22335 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE BETWEEN ROWS 31 AND 37 ON THE RT SIDE. REPAIRED CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000361995122200036NM 1995 12 22 AALA951805 119951014A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739356 24037 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 9H FOUND INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR AS PASSENGER SEAT 9H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000371995122200037NM 1995 12 22 AALA951807 119951016A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07366AA 25193 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PASSENGER SEAT ROWS 7H AND 12H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 7H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000381995122200038NM 1995 12 22 AALA951826 119951017A3350A3060698101 EEL CONNECTOR DOUG MD11 MD11 3023602NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071751A 48420 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 7 AND 8 AT LT AISLE FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 7. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F RTA22WE 19951222000391995122200039WP 1995 12 22 AALA951827 119951019A3350A3060720101 EEL CONDUCTOR DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07491AA 49684 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19951222000401995122200040WP 1995 12 22 AALA951833 119951020A3350A3060819104 EEL STRIP DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07595AA 53285 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 21DEF AND 29DEF FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 21DEF AND 29DEF. SYSTEM GROUND CHECK NORMAL OPERATION. (X) 2L72 4F RTA6WE 19951222000411995122200041EU 1995 12 22 AALA951834 119951021A3350A3060819104 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077062A 474 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE BETWEEN PASSENGER SEAT ROWS 12 AND 20 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PASSENGER SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA35EU 19951222000421995122200042NM 1995 12 22 AALA951835 119951021A3350 EEL CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PASSENGER SEATS 8 THROUGH 12 AND 35 THROUGH 41 FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTORS AT PASSENGER SEATS 8 THROUGH 12 AND 35 THROUGH 41. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000431995122200043NM 1995 12 22 AALA951836 119951022A3350 EEL WIRE BOEING767 767223 1385123NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07339AA 22336 SFO - DURING OVERNIGHT CHECK, RT FORWARD GALLEY EMERGENCY FLOOR LIGHT FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY RT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19951222000441995122200044WP 1995 12 22 AALA951837 119951022A3350A3060819104 EEL CONNECTOR DOUG DC9 DC983 3022083WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07599AA 53289 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 30D AND 31D AND PASSENGER SEAT ROWS 22D AND 23D FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTORS BY PASSENGER SEATS 30D AND 22D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA6WE 19951222000451995122200045WP 1995 12 22 AALA951863 119951024A3350L204827 EEL SIGN DOUG DC10 DC1010 3022110WP 2L DOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07160AA 46710 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIGN AT DOOR 2L FOUND INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AT DOOR 2L. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A22WE 19951222000461995122200046NM 1995 12 22 AALA951866 119951027A3350A306081104 EEL STRIP DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071768D 48436 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD LT AISLE OF BUSINESS CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FORWARD LT AISLE OF BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F RTA22WE 19951222000471995122200047NM 1995 12 22 AALA951867 119951028A3350A3060720101 EEL CONDUCTOR DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071765B 48596 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LT AISLE OF FIRST CLASS CABIN FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR AT LT AISLE OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F RTA22WE 19951222000481995122200048NM 1995 12 22 AALA951868 119951028A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07709AA 22466 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 3EF TO 17DEF FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 17DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000491995122200049NM 1995 12 22 AALA951869 119951028A326063200036 SWITCH BOEING727 727223 1384074NM RT MLG DOOR DEFECTIVE A AALAK NONE N FALSE WARNING APAPPROACH 1 SW07709AA 22466 DFW - FLT 1039 - DURING APPROACH TO DFW WHEN LANDING GEAR EXTENDED, RT MLG DOOR LIGHT ON F/E PANEL DID NOT ILLUMINATE WHEN GEAR DOORS OPENED. ALL OTHER INDICATIONS NORMAL AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REPLACED RT MLG DOOR WARNING SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000501995122200050EU 1995 12 22 AALA951872 119951030A5320A34430199 ANGLE FOKKERF28 F28MK0100 4990807EU BS 25016 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071402K 11353 TUL - LEFT OUTBOARD PROFILE ANGLE CRACKED OUTBOARD SIDE. INSTALLED DOUBLER PER ESO 51000 DATED 10-27-95. TST 8,673. CYCLES, 7,365. (X) 2L72 4F RT 19951222000511995122200051NM 1995 12 22 AALA951885 119951102A3350A3030398101 EEL CONNECTOR BOEING727 727223 1384074NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07862AA 21089 BWI - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTORS BY OVERWING EXIT AND FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000521995122200052NM 1995 12 22 AALA951892 119951102A5730 SKIN BOEING767 767223 1385123NM WS 955 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07335AA 22333 AFW - WING BOX UPPER SKIN HAS CORROSION REMOVED. T-ANGLE AT RBL 74.81 WAS CUT TO PROVIDE AND FACILITATE CORROSION REMOVAL. FABRICATED AND INSTALLED REPAIR PER INSTRUCTIONS AT MRB 767-1054. TST, 33,946.03. CYCLES, 6,219. (X) 2L72 4F RTA1NM 19951222000531995122200053NM 1995 12 22 AALA951893 119951102A5315141T5114 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07335AA 22333 AFW - REMOVED CORROSION ON FLOOR BEAM. AFTER BLENDING, FOUND BEYOND SRM LIMITS. ALODINED AND BLENDED. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 1/2 HARD STAINLESS STEEL. INSTALLATION APPROVED BY ENGINEERING PER MRB 767-1050. (X) 2L72 4F RTA1NM 19951222000541995122200054NM 1995 12 22 AALA951894 119951102A5320143T80042 CHORD BOEING767 767223 1385123NM BS 615.5 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07335AA 22333 AFW - FOUND AND BLENDED CORROSION IN THE UPPER SURFACE OF THE CHORD IN TWO AREAS. THE FWD BLEND-OUT IS WITHIN LIMITS, HOWEVER, DURING ULTRASONIC THICKNESS CHECK, A THICKNESS OF APPROXIMATELY 0.140 INCH WAS INDICATED EVEN THOUGH MINIMAL MATERIAL WAS REMOVED. SUSPECT INTERNAL INCLUSION OR POCKET OF FILLIFORM CORROSION, RUNNING HORIZONTALLY. ALODINED AND PRIMED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1055. PART WILL BE REPLACED AT NEXT MRB NOT TO EXCEED 18 MONTHS FROM 11-3-95, OR 3,000 CYCLES FROM 5,657 CYCLES, WHICHEVER OCCURS FIRST. TST 33,946.03. CYCLES, 6,219. (X) 2L72 4F RTA1NM 19951222000551995122200055WP 1995 12 22 AALA951903 119951108A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07167AA 46930 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 10H FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 10H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A22WE 19951222000561995122200056EU 1995 12 22 AALA951904 119951108A3350A3030398101 EEL CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW073075A 606 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 1B FOUND INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 1B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA35EU 19951222000571995122200057WP 1995 12 22 AALA951907 119951108A3350A3030398101 EEL CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07135AA 47830 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT 1L DOOR FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT 1L DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A22WE 19951222000581995122200058NM 1995 12 22 AALA951914 119951109A5312 BLKHD SKIN DOUG MD11 MD11 3023602NM BS 464 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - RIGHT A/C COMP - SMALL CRACK ON AFT BULKHEAD SKIN INBOARD OF ADG ACTUATOR. INSTALLED 1032 TITANIUM REPAIR DOUBLER PER SRM 53-20-00-0, FIGURE 6, SHEET 14. TST 11,610. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000591995122200059EU 1995 12 22 AALA951921 119951110A3350A3060819104 EEL STRIP AIRBUS300 A300B4605R 3930308EU CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077083A 645 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 15B AND 17B FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 15B AND 17B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA35EU 19951222000601995122200060EU 1995 12 22 AALA951922 119951109A252010117861 PSU FOKKERF28 F28MK0100 4990807EU CABIN DEFECTIVE A AALAK NONE BM SMOKE/FUMES/ODORS/SPARKS OVER TEMP CRCRUISE 1 SW071427A 0105 11412 DFW - FLT 1738 - EN ROUTE DTW/DFW DURING CRUISE, ODOR SIMILAR TO HOT PLASTIC NOTED IN CABIN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED TO DFW LANDING WITHOUT INCIDENT. REPLACED PASSENGER SERVICE UNIT PANEL AT SEAT 5DE DUE TO RELAY FOUND HOT AND MELTING. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19951222000611995122200061WP 1995 12 22 AALA951924 119951109A3350P2010031302 EEL DOUG DC10 DC1010 3022110WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07147AA 46702 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT EXIT LIGHT AT 3R DOOR FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT EXIT LIGHT AT 3R DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A22WE 19951222000621995122200062NM 1995 12 22 AALA951933 119951113A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07701AA 22459 RDU - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH TRACK LIGHTING BRIGHT IN FIRST CLASS AND DIMMING TOWARDS THE AFT LAVATORIES. REPAIRED SPLICE IN THE EMERGENCY EXIT FLOOR PATH TRACK LIGHTING STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000631995122200063NM 1995 12 22 AALA951935 119951111A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW076811 19486 MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT TRACK LIGHTING IN FIRST CLASS ON THE RIGHT SIDE INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000641995122200064NM 1995 12 22 AALA951940 119951110A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 842-919 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - NR 5 SEAT TRACK - DEEP CORROSION. INSTALLED NEW SEAT TRACK SECTION PER SRM 53-70-00, PAGES 3 AND 4, FIGURE 1, FROM STA 824 TO STA 919. TST, 11,610. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000651995122200065NM 1995 12 22 AALA951941 119951110A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 840-879 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - NR 3 SEAT TRACK - CORRODED AFT GALLEY TIE-DOWN AND FORWARD LAV TIE-DOWN AREA. INSTALLED SEAT TRACK PLUG. REMOVED AND REPLACED PER SRM 53-70-00, FIGURE 4, PAGE 8 STA 840 TO STA 879. TST, 11,610. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000661995122200066NM 1995 12 22 AALA951942 119951110A5320 SUPPORT DOUG MD11 MD11 3023602NM BS 791-824 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - GALLEY SEAT SUPPORT CRACKED. INSTALLED NEW GALLEY SUPPORT SEAT TRACK PER SRM 53-70-00, PAGES 3 AND 4, FIGURE 1, FROM STA 791 TO STA 824. TST, 11,610. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000671995122200067NM 1995 12 22 AALA951943 119951110A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 840-879 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - NR 6 SEAT TRACK - CORRODED IN AFT LAV TIE-DOWN AREA. INSTALLED SEAT TRACK PLUG. REMOVED AND REPLACED PER SRM 53-70-00, FIGURE 4, PAGE 8, FROM STA 840 TO STA 879. TST, 11,610. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000681995122200068NM 1995 12 22 AALA951944 119951110A53474013697 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1962-1964 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071765B 48596 TUL - NR 9 SEAT TRACK HAS CORROSION, STA 1962 TO STA 1964. REMOVED 55 INCHES OF SEAT TRACK AND REPLACED WITH SPLICED IN NEW SECTION OF TRACK PER SRM 53-70-00. TST, 11,610.02. CYCLES, 1,576. (X) 2L73 4F RTA22WE 19951222000691995122200069WP 1995 12 22 AALA951945 119951113A3350 EEL WIRE DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07451AA 49477 DFW - DURING OVERNIGHT CHECK, FOUND THE FORWARD SECTION OF THE EMERGENCY EXIT FLOOR PATH LIGHT STRIPS HAS NO POWER FEED FROM BATTERY PACK. REPLACED WIRE LEAD FROM FORWARD BATTERY PACK MODULE TO FLOOR PROXIMITY MARKER LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19951222000701995122200070NM 1995 12 22 AALA951948 119951113A2560ADA33052 BRACKET DOUG MD11 MD11 3023602NM 4R DOOR BROKEN A AALAK NONE O OTHER TXTAXI/GRND HDL 1 SW071752K 48421 EZE - FLT 0900 - WHILE AT GATE, FOUND THE 4R DOOR FORWARD SLIDE BAR BRACKET BROKEN. PLACARDED 4R DOOR/SLIDE INOPERATIVE PER MEL. REPLACED FORWARD SLIDE BAR BRACKET AND REMOVED MEL IN MIA. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F RTA22WE 19951222000711995122200071NM 1995 12 22 AALA951955 119951113A33506013211 EEL CHARGER BOEING727 727223 1384074NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07845AA 20986 DFW - DURING OVERNIGHT CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY CHARGER FOR RIGHT OVERWING EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000721995122200072WP 1995 12 22 AALA951962 119951116A3350A3060719101 EEL STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077538A 49992 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 12D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19951222000731995122200073NM 1995 12 22 AALA951964 119951116A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07897AA 22013 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHT FROM FIRST CLASS TO MID-COACH DIM. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19951222000741995122200074SW 1995 12 22 BDHA9500023 119951023A2435230790001 STARTER/GEN LEARSIEGLER SWRNGNSA226 SA226TC 8780404SW RT ENGINE INOPERATIVE A BDHAO OTHER O OTHER UKUNKNOWN 1 GL15229AM393 1125 TC305 FAR - FLT 421 - RIGHT GENERATOR WOULD NOT COME ON LINE, THE VOLTMETER SHOWED NO RESET VOLTAGE. WHEN START ATTEMPT WAS MADE, THE STARTER FAILED TO ROTATE THE ENGINE. MAINTENANCE PERSONNEL REPLACED THE STARTER GENERATOR UNIT AND PERFORMED OPERATIONAL CHECKS. ALL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19951222000751995122200075SW 1995 12 22 BDHA9500024 119951009A7931 CONNECTOR SWRNGNSA226 SA226TC 8780404SW LT NACELLE WATER LOGGED A BDHACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL15229AM TC305 MSP - FLT 434 - ON TAKEOFF ROLL, THE LEFT OIL PRESSURE WARNING LIGHT ILLLUMINATED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE HANGAR. MAINTENANCE INSPECTED THE SWITCH ASSY AND FOUND WATER IN THE CANNON PLUG. THE PLUG WAS DRIED OUT AND THE SYSTEM OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19951222000761995122200076WP 1995 12 22 BDHA9500025 219951025A7320 LOCK OUT VL WIRE SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE BROKEN A BDHAO OTHER O OTHER NRNOT REPORTED 1 GL15328BA TC253 P54269 BIS - FLT 421 - THE LEFT ENGINE WOULD NOT LIGHT-OFF AFTER 10 PERCENT RPM. INSPECTION REVEALED A BROKEN WIRE AT THE FUEL ANTI-ICE LOCK OUT VALVE. REPAIRS WERE MADE AND THE ENGINE OPERATED NORMALLY. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T4 T A8SW E4WE 19951222000771995122200077WP 1995 12 22 BUFA9525 119951114A3411 PITOT TUBE DOUG DC8 DC861 3021952WP LEFT DIRTY A BUFACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE05915BV 45981 FLT EWW133 ELP-PIA ELP-ELP - CAPTAIN'S AIRSPEED INDICATOR INOP. DURING TAKEOFF ROLL, ZERO KNOTS, FIRST OFFICER 80 KNOTS. TAKEOFF ABORTED. FOUND OBSTRUCTION (SAND) IN CAPTAIN'S PITOT TUBE. CLEANED AND REMOVED SAND. OP CHECK OK PER MM 34-11. (X) 2L74 4F 4A25 19951222000781995122200078WP 1995 12 22 CKSA95134 119951024A5730 PANEL DOUG DC8 DC862 3021970WP WS 152 CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801MG44966 45986 KOSC - DURING C-CHECK INSPECTION FOUND UPPER SKIN PANEL JUST FORWARD OF CENTER SPAR AT APPROXIMATELY STA XRS 152 - CORROSION REMOVAL EXCEEDS 20 PERCENT OF PANEL THICKNESS. REPAIRED IAW SKETCH AIA/E/2102 AT RT WING CENTER SPAR AREA AT STA XRS 152. (X) 2L74 4F 4A25 19951222000791995122200079WP 1995 12 22 CKSA95135 119951024A53132753715 LONGERON DOUG DC8 DC862 3021970WP FS 1190 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801MG44966 45986 KOSC - DURING C-CHECK INSPECTION FOUND - LONGERON 36 CRACKED FORWARD OF SPLICE FS 1190. REPAIRED LONGERON CRACK IAW COTNEY ENGINEERING 8110-13, SKETCH NR SKA 95167-13, LONGERON 36. (X) 2L74 4F 4A25 19951222000801995122200080WP 1995 12 22 CKSA95136 119951024A53132753715 LONGERON DOUG DC8 DC862 3021970WP FS 1190 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801MG44966 45986 KOSC - DURING C-CHECK INSPECTION FOUND - LONGERON 33R CRACKED FORWARD OF SPLICE AT FS 1190. REPAIRED CRACK IAW COTNEY ENG 8110-3 AND SKETCH NR SKA 95167-13. (X) 2L74 4F 4A25 19951222000811995122200081WP 1995 12 22 CKSA95137 119951024A532037546251 FITTING DOUG DC8 DC862 3021970WP FS 1190 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801MG44966 45986 KOSC - DURING C-CHECK INSPECTION, FOUND LONGERON SPLICE FITTING CRACKED L35R AT FS 1190. REMOVED AND REPLACED LONGERON 35R 1190 FITTING IAW COTNEY ENG 8110-3 AND SKETCH NR SKA 95167-13. (X) 2L74 4F 4A25 19951222000821995122200082WP 1995 12 22 CKSA95138 119951024A532037546251 SPLICE DOUG DC8 DC862 3021970WP FS 1190 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23803MG44966 45910 KOSC - DURING C-CHECK INSPECTION, FOUND LONGERON 35L, FS 1190, SPLICE CRACKED. REMOVED AND REPLACED LONGERON 35L, FS 1190, SPLICE IAW COTNEY ENG 8110-3 AND SKETCH NR SKA95167-13. (X) 2L74 4F 4A25 19951222000831995122200083WP 1995 12 22 CKSA95139 119951026A3231510361 LINK ASSY DOUG DC8 DC8F54 3021926WP NLG DOOR FAILED A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL23806CK61261 45932 KCVG - FLT 68278 - UPON GEAR RETRACTION DURING CLIMB, NOSE GEAR DOOR DID NOT FULLY CLOSE. THIS CAUSED A VIBRATION IN NOSE GEAR DOOR WELL. FLEW ACFT AT 230KIAS/M.65. (UPLATCH FAIL CHECK SPEED). WITH GEAR DOWN, NO VIBRATION NOTED. ALL OTHER GEAR INDICATIONS NORMAL. INSPECTED NOSE GEAR DOORS, FOUND LT NOSE GEAR DOOR NOT LATCHED. REMOVED AND REPLACED LT NOSE GEAR DOOR FWD LINK ASSY IAW DC-8 MM CHAP 32-2-5. ADJUSTED NOSE GEAR DOORS IAW DC-8 MM CHAP 32-2-5 PAR 5. NOSE LANDING GEAR DOORS OPS CHECK NORMAL ON GEAR SWING IAW DC-8 MM CHAP 32-2-5 PAR 5. (X) 2L74 4F 4A25 19951222000841995122200084WP 1995 12 22 CKSA95140 119951027A2612 BRACKETS DOUG DC8 DC8F55 3021928WP NR 4 ENGINE LOOSE A CKSAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL236161C56305 45856 KMIA - FLT 68305 - MASTER FIRE WARNING SHUT DOWN. IN MIA TERMINAL AREA, NR 4 ENGINE MASTER FIRE WARNING, SHUT DOWN NR 4 ENGINE. NORMAL LANDING. FOUND SEVERAL FIRE LOOP MOUNTING BRACKETS LOOSE AND GROMMETS MISSING. REPAIRED AND REPLACED MOUNTING BRACKETS. INSTALLED MISSING GROMMETS. RAN ENGINE AT TAKEOFF POWER FOR 5 MINUTES WITH BLEED AIR ON. NO FIRE WARNING. FIRE WARNING SYSTEM OPS NORMAL IAW MM 26-2-0. REFERENCE, OPERATOR CONTROL NR 95ZZZX6782. (X) 2L74 4F 4A25 19951222000851995122200085WP 1995 12 22 CKSA95141 119951109A261257775621 FIRE LOOP DOUG DC8 DC852 3021922WP NR 2 ENGINE BROKEN A CKSAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 GL23810CK34936 45814 KCLE - FLT 68675 - ON SHORT APPROACH INTO CLE, HAD FIRE INDICATION ON NR 2 ENGINE. ACCOMPLISHED ALL APPROPRIATE CHECK LISTS. PULLED NR 2 FIRE HANDLES, DISCHARGED BOTTLE - LIGHT WAS STILL ON. ASKED FOR EMERGENCY EQUIPMENT. UPON INSPECTION, THERE WAS NO FIRE. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW DC-8 MM 26-4-1. WHEN TROUBLESHOOTING FIRE WARNING, FOUND BOTTOM ENGINE FIRE LOOP CANNON PLUG WIRE BROKEN AND GROUNDING ON COWLING. REMOVED AND REPLACED BOTTOM ENGINE FIRE LOOP IAW DC-8 MM 26-2-1. OPS CHECK NORMAL. (X) 2L74 4F 4A25 19951222000861995122200086EA 1995 12 22 COEA9522205 119951121A32609009Y78 STRIKER PLATE ROTOL 200085014 FRCHLDF27 F27F 3373008EA NLG LOOSE A COEAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 NM01222DG3337 CPACC159 31 MAF - ON APPROACH INTO MIDLAND, TX, CREW LOWERED LANDING GEAR BUT WAS UNABLE TO GET A POSITIVE DOWN & LOCKED INDICATION FOR NOSE LANDING GEAR. APPROACH ABORTED. GEAR CYCLED SEVERAL TIMES & FOLLOWING THE EMERGENCY PROCEDURES CHECKLIST, CREW WAS ABLE TO DETERMINE GEAR WAS DOWN. ACFT LANDED WITHOUT INCIDENT. ACFT STOPPED AT RUNWAY END. GEAR LOCKS INSTALLED & ACFT WAS THEN TAXIED TO MX. INVESTIGATION REVEALED NLG DOWNLOCK STRIKER PLATE LOOSE. STRIKER PLATE REMOVED, CLEANED & REINSTALLED. LANDING GEAR RETRACTION TESTS PERFORMED TO VERIFY PROPER OPERATION OF LANDING GEAR AND INDICATING SYS. ACFT TEST FLOWN TO ALSO VERIFY PROPER IN-FLT OPER OF LANDING GEAR SYS. NO ADDITIONAL GEAR SYS DISCREPANCIES NOTED. (X)2H72 4T 7A1 19951222000871995122200087NM 1995 12 22 9520372296 119951211A7711 EPR INDICATOR BOEING727 727251 138408HNM PWA JT8 JT8D15A 52051NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01296US 21788 700798 NR 1 ENGINE EPR INDICATION WAS LOW AND FLUCTUATING ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. 2L73 4F4 F A3WE E2EA 19951222000881995122200088WP 1995 12 22 9520389884 119951213A32225910448563 STRUT DOUG DC9 DC951 3022051WP NLG DEFLATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01677MC 47756 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RED NOSE UNSAFE LIGHT REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND ICE ACCUMULATION AROUND BASE OF NOSE GEAR GLAND NUT AND NOSE STRUT DEFLATED. CLEANED ICE FROM AROUND NOSE GEAR AND SERVICED NOSE STRUT TO PROPER LEVELS. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951222000891995122200089WP 1995 12 22 9520399140 119951212A5244 DOOR DOUG DC9 DC914 3022034WP FWD ACCESS OUT OF ADJUST A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01930RC 45729 FORWARD ACCESSORY COMPARTMENT DOOR WARNING LIGHT ILLUMINATED DURING INITIAL TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO THE GATE. ADJUSTED DOOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951222000901995122200090 1995 12 22 9520409105 419951213A3418 TRANSPONDER DOUG DC9 DC915 3022036WP STALL WARNING MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL0195S 47205 STALL WARNING AND STICK SHAKER ACTIVATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT STALL WARNING TRANSDUCER, FLAP POSITION TRANSMITTER, AND YAW DAMPER ACTUATOR. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951222000911995122200091WP 1995 12 22 9520419882 119951214A3350 EEL POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01670MC 47659 DURING PERIODIC CHECK, EMERGENCY LIGHTS IN TAIL AND AFT STAIRWELL AREA FAILED TEN MINUTE TEST. REPLACED BOTH BATTERY POWER SUPPLIES. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222000921995122200092WP 1995 12 22 9520429868 119951213A335060030451 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222000931995122200093WP 1995 12 22 9520439851 119951212A3350 BATTERY PACK DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01760NC 47708 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 7, 8, 9, AND ROWS 20 AND 21. REPLACED THE BATTERY PACK POWER SUPPLY. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222000941995122200094WP 1995 12 22 9520449163 119951213A33506014113 BATTERY PACK DOUG DC9 DC914 3022034WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018906E 45747 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED BATTERY PACK POWER SUPPLY. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222000951995122200095WP 1995 12 22 9520459153 119951213A3520 OXY MANIFOLDS DOUG DC9 DC914 3022034WP CABIN OXY SYS MALFUNCTIONED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING PERIODIC CHECK, MULTIPLE OXYGEN SYSTEM MANIFOLDS FAILED SYSTEM CHECK. REPLACED MANIFOLDS. OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222000961995122200096NM 1995 12 22 9520462709 119951213A3350 BATTERY PACK BOEING727 727225 1384077NM COCKPIT DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01818EA 22555 DURING PRE-FLIGHT, FOUND COCKPIT EMERGENCY EXIT SIGN INOPERATIVE. REPLACED LIGHT BATTERY PACK AND BATTERIES. CHECKED OK. 2L73 4F A3WE 19951222000971995122200097NM 1995 12 22 9520472715 119951214A2781 INDICATING SW BOEING727 7272S7 138407ZNM NR 3 LE FLAP MALFUNCTIONED A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01719RC 22490 DURING APPROACH, NR 3 LEADING EDGE DEVICE DID NOT INDICATE EXTENDED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT LEADING EDGE INBOARD INDICATING SWITCH. CHECKED OK. 2L73 4F A3WE 19951222000981995122200098NM 1995 12 22 9520482298 119951214A4900 APU BOEING727 727251 138408HNM RT MLG WW SMOKING A NWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL01298US 22152 AT GATE, SMOKE BEGAN TO FILL CABIN AND HEAVY SMOKE WAS ALSO OBSERVED COMING FROM RIGHT WHEELWELL AREA. APU SHUT DOWN AND SMOKE CEASED TO ACCUMULATE. PASSENGERS DEPLANED. MAINTENANCE FOUND GLYCOL IN AND AROUND APU EXHAUST DUCT. GLYCOL WAS REMOVED. APU OPERATED NORMALLY. 2L73 4F A3WE 19951222000991995122200099WP 1995 12 22 9520499604 119951212A7711 PT2 PROBES DOUG DC9 DC932 3022066WP PWA JT8 JT8D7B 52053NE LT/RT ENGINES ICED UP A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01604NW 47222 657167 EPR INDICATION WAS LOW ON BOTH ENGINES DURING TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ICE WAS FOUND IN BOTH PT2 PROBES. THE ICE WAS REMOVED AND THE ENGINES WERE RUN-UP. NO FURTHER DISCREPANCIES NOTED. 2L72 4F4 F A6WE E2EA 19951222001001995122200100NE 1995 12 22 9520509310 219951211A7260 ACCESSORY GB DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE FAILED A NWAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01313RC 48091 708443 NR 2 ENGINE LOST POWER ON TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. THE FRONT ACCESSORY COVER HAD LIBERATED FROM THE FRONT ACCESSORY SUPPORT AND FOUND LAYING IN THE ENGINE INLET. MAINTENANCE REPLACED THE NR 2 ENGINE WITH A SERVICEABLE UNIT. 2L72 4F4 F A6WE E9NE 19951222001011995122200101 1995 12 22 9520513230 419951120A2565D30665103 SLIDE AIRBUS320 A320211 3930320EU DOOR 4R MALFUNCTIONED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01330NW9202 7348 307 AFTER THE AIRCRAFT ARRIVED AT THE GATE, THE FLIGHT ATTENDANT INADVERTENTLY DEPLOYED THE SLIDE AT DOOR 4R. THE SLIDE DID NOT FULLY INFLATE. MAINTENANCE REMOVED SLIDE AND SENT TO THE SHOP WHERE THE SLIDE WAS REPACKED. THIS SLIDE WILL BE INSTALLED ON AN AIRCRAFT AND RE-DEPLOYED FOR TROUBLESHOOTING PURPOSES AT A LATER DATE. 2L72 4F RTA28NM 19951222001021995122200102WP 1995 12 22 9520529924 119951216A3222 STRUT DOUG DC9 DC932 3022066WP NLG REQD SERVICE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01926RC 47473 DURING CLIMB, CREW WAS UNABLE TO RAISE THE LANDING GEAR HANDLE. UTILIZED GROUND SHIFT OVERRIDE TO RAISE THE HANDLE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. DRAINED AND SERVICED NOSE STRUT. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001031995122200103NM 1995 12 22 95FDEAO1826 119951204A5320 WEB BOEING727 727232 1384082NM BS 219.8 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 WHILE WORKING NRO 676, FOUND CORROSION ON AFT SIDE OF WEB STATION 219.8 W/L 214 TO 222, LBL 44. UPON REMOVING CORROSION AFT SIDE OF WEB STATION 219.8 W/L 214 TO 222, LBL 44, FOUND CRACK. REPAIRED WEB IAW FEDEX SRM 51-40-2. CORROSION WAS FOUND TO BE WITHIN LIMITS PER FEDEX SRM 53-10-1. 2L73 4F A3WE 19951222001041995122200104NM 1995 12 22 95UAL900317 119951215A2710 CONTROLS BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE AILERON LOCKED OUT A UALAO OTHER FJ FLT CONT AFFECTED WARNING INDICATION NRNOT REPORTED 1 WP29642UA 25092 AN AILERON LOCKOUT OCCURRED IN FLIGHT. THE EICAS DISPLAY VERIFIED THIS CONDITION. THIS INDICATION WILL BE ADDRESSED BY THE ACCOMPLISHMENT OF BOEING SERVICE LETTER 767-27-081-A. 2L72 4F4 FRTA1NM E24NE 19951222001051995122200105WP 1995 12 22 95UAL900318 119951215A3350 BATTERY PACK DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291838U 46632 EMERGENCY LIGHTS FAILED NR 2 SVC TEST. REPLACED THE MID-BATTERY PACK AND THE OVERWING BATTERY PACK AND POWER SUPPLY. 2L73 4F4 F A22WE E23EA 19951222001061995122200106NM 1995 12 22 95UAL900319 119951215A2780 RETRACT MECH BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 5 LE FLAP MALFUNCTIONED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP297455U 21909 NR 5 L.E. FLAP WOULD NOT RETRACT WHEN FLAPS RETRACTED FROM 2 DEGREES TO ZERO DEGREES. RETURNED TO ORD. 2L73 4F4 F A3WE E2EA 19951222001071995122200107NM 1995 12 22 95UAL900320 119951215A3350 BULB BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN FAILED A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29357UA 24378 EMERGENCY OVERWING EXIT LIGHTS INOP ON BOTH THE LEFT AND RIGHT SIDES. REPLACED BULBS. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951222001081995122200108NM 1995 12 22 95UAL900321 119951215A2560 SLIDE AIRCRUISERS 62774402 BOEING777 777222 1385219NM DOOR 4R DEPLOYED A UALAK NONE O OTHER ININSP/MAINT 1 WP29768UA 0021 26919 DOOR 4 RIGHT ESCAPE SLIDE PARTIALLY INFLATED AFTER INADVERTENT DEPLOYMENT. SLIDE INADVERTENTLY DEPLOYED CONTACTING FOOD SERVICE TRUCK WHICH PRODUCED AN L-SHAPED TEAR ON THE AFT TOP INFLATION TUBE. REPAIRED TEAR AND MADE SLIDE SERVICEABLE. 2L72 4F RTT0001SE 19951222001091995122200109 1995 12 22 95UAL900322 419951218A2210 AUTOPILOT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE E/E COMPT MALFUNCTIONED A UALAO OTHER O OTHER DEDESCENT 1 WP297269U 21416 AUTOPILOT COUPLED APPROACH UNSATISFACTORY. PITCHES DOWN VIOLENTLY ON GLIDESLOPE CAPTURE AT 160 KIAS. 2L73 4F4 F A3WE E2EA 19951222001101995122200110WP 1995 12 22 95UAL900323 119951218A5210NBA62622 DOOR MECHANISM DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL DOOR 1R OUT OF ADJUST A UALAK NONE O OTHER ININSP/MAINT 1 WP291813U 46612 WHILE AIRCRAFT WAS IN FOR A C-CHECK, A ROUTINE OPERATIONAL CHECK OF DOOR 1R EMERGENCY PNEUMATIC ACTUATION SYS WAS PERFORMED. THE DOOR OPENED APPROXIMATELY 18 INCHES AND STOPPED, BECOMING JAMMED ON A PIECE OF ADJACENT STRUCTURE. THE DOOR RIG WAS ADJUSTED PER JIC 20002515 (MM 52-11-00) AND THE DOOR OPERATION WAS RE-TESTED IN BOTH PNEUMATIC AND ELECTRIC MODES. DOOR OPERATED SUCESSFULLY THREE TIMES. 2L73 4F4 F A22WE E23EA 19951222001111995122200111 1995 12 22 95UAL900324 419951218A3441 INS DELCO 7890860011 DOUG DC10 DC1010 3022110WP NR 1 FAILED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP291843U 01178 46636 NR 1 INS WARN LIGHT ON AT FL 370, AIRCRAFT OSCILLATES IN YAW AND CAPT'S ADI TUMBLED. DISCONNECTED AP, LOWER YAW DMPR INOP LIGHT ON. FLIGHT RETURNED TO ORD. WHEN PILOT SWITCHED TO CAPTAIN ON THE AUXILIARY VERTICAL GYRO/DIRECTIONAL GYRO, ALL SYSTEMS AFFECTED BY THE NR 1 INERTIAL NAV UNIT RETURNED TO NORMAL. REPLACED NR 1 INERTIAL NAV UNIT. 2L73 4F A22WE 19951222001121995122200112NM 1995 12 22 95UAL900325 119951218A2710 CONTROLS BOEING767 767222 1385122NM PWA JT9 JT9D7R4D 52054NE AILERONS LOCKED OUT A UALAO OTHER JF WARNING INDICATION FLT CONT AFFECTED DEDESCENT 1 WP29620UA 21880 AILERON LOCK OUT MESSAGE INDICATION OCCURRED AT 255 KNOTS AND 12,000 FEET DURING DESCENT. THE AILERONS EXTENDED AND LOCKED OUT. THIS INDICATION WILL BE ADDRESSED BY THE ACCOMPLISHMENT OF BOEING SERVICE LETTER 767-27-081-A. 2L72 4F4 FRTA1NM E3NE 19951222001131995122200113NM 1995 12 22 95UAL900326 119951218A3350 EEL BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29390UA 24665 FORWARD GALLEY EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED LIGHT ASSEMBLY. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951222001141995122200114SO 1995 12 22 COMA9512026 119951214A3260922AASYA6P2722 DNLOCK SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01241CA 120211 LANDING GEAR WOULD NOT EXTEND NORMALLY. EMERGENCY EXTENTION SYSTEM USED. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR. 2L72 4T RTA31SO 19951222001151995122200115EU 1995 12 22 COMA9531210 119951216A552312008898001 BEARINGS EMB 1201129500 SAAB SF340 SF340A 7850100EU LT ELEV TAB SEIZED A ACOMAO OTHER O OTHER APAPPROACH 1 SO01358CA 340A047 WITH FLAPS AT 35 DEGREES, THE ELEVATORS REQUIRE EXCESSIVE CONTROL TO FORCE BOTH NOSE DOWN AND NOSE UP DURING FLARE. REPLACED SEIZED BEARINGS ON LEFT ELEVATOR TRIM TAB. 2L72 4T RTA52EU 19951222001161995122200116EU 1995 12 22 COMA9531211 119951214A2613 OVERHEAT IND SAAB SF340 SF340A 7850100EU LT TAIL PIPE ACTIVATED A COMAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01358CA 340A047 LEFT TAIL PIPE HOT WARNING AFTER TAKEOFF. ENGINE SECURED AND ACFT RETURNED TO FIELD. COULD NOT DUPLICATE DISCREPANCY. GROUND RUN AT 100 PERCENT POWER FOR 10 MINUTES. NO FURTHER TAIL PIPE HOT WARNING. 2L72 4T RTA52EU 19951222001171995122200117EU 1995 12 22 COMA9531212 119951207A324650092371 BEARING RACE LORAL 5010488 SAAB SF340 SF340A 7850100EU MLG WHEEL SPUN A COMAK NONE O OTHER ININSP/MAINT 1 SO01146CA OCT920494 340A146 WHEEL ASSEMBLY WAS REMOVED FROM A/C FOR TIRE WORN TO LIMITS. UPON DISASSEMBLY AND INSPECTION OF WHEEL, FOUND BEARING RACE IN HUB ASSEMBLY TURNING. SUB-ASSEMBLY HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR REPAIR. 2L72 4T RTA52EU 19951222001181995122200118 1995 12 22 COMA9531213 419951216A2312 NR 1 COMM SAAB SF340 SF340A 7850100EU RADIO RACK MALFUNCTIONED A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01357CA 340A044 NR 1 COMM RADIO WILL RECEIVE, BUT WILL NOT TRANSMIT. COULD NOT DUPLICATE - NR 1 COMM RADIO SYSTEM TEST OK. 2L72 4T RTA52EU 19951222001191995122200119EA 1995 12 22 COMA9560621 119951214A5610NP1393211 WINDSHIELD CNDAIRCL600 CL6002B19 EA LT COCKPIT CRACKED A COMAA UNSCHED LANDING O OTHER CLCLIMB 1 SO01951CA88 7091 PILOT'S WINDSHIELD CRACKED DURING CLIMB. REPLACED WINDSHIELD. 2L72 4F RTA21EA 19951222001201995122200120NE 1995 12 22 DL72S954696 219951213A7260 GEARBOX BOEING727 727232 1384082NM PWA JT8 JT8D15A 52051NE NR 2 ENGINE FAILED A DALAA UNSCHED LANDING X ENGINE FLAMEOUT TOTAKEOFF 1 SO27532DA55677 22045 687654 NR 2 ENG FAILED ON TAKEOFF. AFTER RETURNING TO YVR, CNTR MAINT FOUND THE NR 2 ENGINE GEARBOX HAD COME APART. REPLACED ENGINE AND ROUTED TO SHOP. 2L73 4F4 F A3WE E2EA 19951222001211995122200121NM 1995 12 22 DL72S954705 119951212A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 FOUND ON CV2 CHECK 1.) 1.25 INCH CRACK AT NR 7 SLAT COVE PANEL ATTACH ANGLE JUST INBOARD OF INBOARD TRACK. 2.) SCREWS/BOLTS LOOSE AT NR 7 SLAT INBOARD TRACK FAIRING. REPAIR: 1.) REPAIRED PER M/M 57-54-0 PAR 2. 2.) REPAIRED AS SECURED FASTENERS. 2L73 4F A3WE 19951222001221995122200122NM 1995 12 22 DL72S954706 119951212A5754 ANGLE BOEING727 727232 1384082NM NR 7 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 FOUND ON CV2 CHECK, TWO CRACKS IN NR 7 SLAT COVE PANEL ATTACH ANGLE BELOW TAI DUCT. REPAIR: REPAIRED PER M/M 57-54-0, PAR 5A. 2L73 4F A3WE 19951222001231995122200123NM 1995 12 22 DL72S954709 119951215A2150 COOLING VALVE M9131 BOEING727 727232 1384082NM AIR CONNECTOR FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27407DA 21151 DURING CLIMB AND LEVEL AT FL 240, WERE UNABLE TO MAINTAIN, CABIN SLOWEST RATE OF ASSENT WAS 700 FPM. DESCENDED AND RETURNED TO JFK. FOUND EQUIPMENT COOLING VALVE STUCK OPEN. REPLACED VALVE. RETURNED TO SERVICE. 2L73 4F A3WE 19951222001241995122200124NM 1995 12 22 DL72S954711 119951211A5713 STRINGER BOEING727 727232 1384082NM WS 686.50 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 FROM ATL HMV: REF OPN 8602AD HFEC INSP. RT WING OUTER UPPER STRINGER TO RIB INSP. CRACK IND. W.S. 686.50 AFT VENT BOX FWD TAB. CORRECTION: STOP DRILLED CRACK AND INSTALLED REPAIR PER MM 57-13-0, FIG 804. 2L73 4F A3WE 19951222001251995122200125NM 1995 12 22 DL72S954715 119951216A3350 EEL POWER SUPPLY BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27477DA 20754 AFT SECTION OF EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED BATTERY POWER SUPPLY, OPS CHECKS NORMAL. S/N ON 0483. 2L73 4F A3WE 19951222001261995122200126NM 1995 12 22 DL72S954716 119951216A3350337202143 EEL BOEING727 727232 1384082NM LT GALLEY BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27477DA 20754 EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR IS BROKEN (LEFT). REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2L73 4F A3WE 19951222001271995122200127NM 1995 12 22 DL72W954720 119951216A5347 SEAT TRACK BOEING727 727247 138408FNM G-3 GALLEY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO272817W 20873 10533 SEAT TRACK AT G-3 GALLEY INBOARD AFT MOUNT IS CORRODED. REPAIR PER M/M 53-20-11, PAGE 805. 2L73 4F A3WE 19951222001281995122200128NM 1995 12 22 DL767954712 119951215A2121732591D FAN BOEING767 767232 1385132NM CARGO COMPT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27102DA 22214 ELECTRICAL SMELL IN COCKPIT AT CRUISE. FORWARD EQ EXHAUST FAN EICAS MSG. SMELL DISSIPATED IN COCKPIT. F/A REPORTED SMELL DIRECTED AFT THROUGH CABIN. FOUND FAN AT FAULT. DEFERRED PER MEL, THEN REPLACED FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19951222001291995122200129NM 1995 12 22 DL767954722 119951208A21216054577 FAN BOEING767 767232 1385132NM AC COMPT FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27104DA 22216 IR - GASPER FAN OFF LIGHT ILLUMINATED WITH SWITCH ON AND ACCOMPANIED BY ELECTRICAL SMELL REPORTED IN CABIN. FORWARD TO MCO AND PLACKARD PER MEL. REPLACED GASPER FAN, OPERATION NORMAL. 2L72 4F RTA1NM 19951222001301995122200130WP 1995 12 22 DLL14954714 119951216A33505165741 EEL POWER SUPPLY LKHEED1011 1011385115 5265015WP GALLEY INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27741DA 193C1245 ON LAYOVER, FOUND EMERGENCY LIGHTS IN LOWER GALLEY INOP. REPLACED EMERGENCY LIGHT POWER SUPPLY. CHECKS GOOD. 2L73 4F A23WE 19951222001311995122200131NM 1995 12 22 DLM88954708 119951206A5320 JAMB DOUG MD88 MD88 3023688NM C 1 DOOR CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27944DL 49817 DURING HMV, FOUND FORWARD CARGO DOOR JAMB CORRODED. REPAIRED PER SRM 53-05, FIG 44. 2L72 4F RTA6WE 19951222001331995122200133NM 1995 12 22 DLM88954723 119951210A3241406256 TRANSDUCER DOUG MD88 MD88 3023688NM LT MLG FAILED A DALAO OTHER O OTHER LDLANDING 1 SO27985DL 53312 ON LANDING ROLLOUT, BRAKING EFFECTIVENESS ON THE LEFT SIDE WAS ALMOST NON-EXISTENT, SOMEWHAT MORE EFFECTIVE AT TAXI SPEEDS. RESET LEFT GEAR IN LINE FUSE, VERIFIED BRAKES ARE OPERATING AT GATE, PERFORMED HIGH SPEED TAXI, FOUND ANTI-SKID INOP. OPERATES NORMAL WITH ANTI-SKID OFF. REPLACED BOTH WHEEL TRANSDUCERS, OPERATION NORMAL. 2L72 4F RTA6WE 19951222001341995122200134WP 1995 12 22 MWEA95533 119951216A33506011777 EEL POWER SUPPLY DOUG DC9 DC915 3022036WP CABIN INOPERATIVE A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31300ME 45718 DURING SERVICE CHECK, FOUND LT ENGINE NACELLE LIGHT WOULD NOT ILLUMINATE WITH EMERGENCY LIGHTS ON. REPLACED EMERGENCY LIGHT POWER SUPPLY. OPS CK GOOD. 2L72 4F A6WE 19951222001351995122200135WP 1995 12 22 MWEA95534 119951216A2560 SLIDE COVER DOUG DC9 DC932 3022066WP FWD PAX DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31602ME 48133 CREW REPORTS FORWARD ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. RESECURED SLIDE COVER. 2L72 4F A6WE 19951222001361995122200136WP 1995 12 22 MWEA95535 119951215A2560 SLIDE COVER DOUG DC9 DC915 3022036WP PAX DOOR FELL OFF A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31900ME 45841 CREW REPORTS FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. RESECURED DOOR SLIDE COVER. 2L72 4F A6WE 19951222001371995122200137NM 1995 12 22 P5CA9500872 119951213A3244 TIRES BOEING747 747121 1384871NM LT MLG FAILED A P5CACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP23830FT 19642 DURING TAKEOFF ROLL, AIRCRAFT SWUNG VIOLENTLY TO THE LEFT, CAUSING LEFT WING AND BODY GEAR TRUCKS TO DEPART LEFT SIDE OF RUNWAY. ABORTED TAKEOFF. INCIDENT CAUSED DAMAGE TO LT WING GEAR BRAKE EQUALIZATION RODS, BRAKE SYSTEM HYDRAULIC LINES, 2 DEFLATED TIRES. COMPONENTS TO BE REPLACED IAW MM 32. AIRCRAFT INSPECTED PER MM 05-51-37 AND MM 05-51-05; NO ADDITIONAL DISCREPANCIES FOUND. BASED ON PILOT REPORT, BELIEVE CAUSE TO BE FLAT TIRES ON LEFT WING GEAR DUE TO A LONG TAXI. 2L74 4F A20WE 19951222001381995122200138SO 1995 12 22 SWIA95690 119951208A3260 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG OUT OF ADJUST A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07188SW 120039 LANDING GEAR WOULD NOT EXTEND OR RETRACT WITHOUT USING ELECTRICAL OVERRIDE. RT GEAR UPLOCK PROXIMITY SENSOR NEEDED ADJUSTMENT. ADJUSTED AND OPS CHECK GOOD. CYCLED GEAR TWELVE TIMES. 2L72 4T4 TRTA31SO E20NE 19951222001391995122200139SW 1995 12 22 SWIA95691 119951208A77122719158007 TQ INDICATOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT ENGINE FAILED A SWIAO OTHER N FALSE WARNING CLCLIMB 1 NM072720B AC715 RT ENGINE LOST TORQUE APPROXIMATELY 20 PERCENT (WILL NOT MAKE TARGET TORQUE). CHECKED RT ENGINE TORQUE CALS, CHECKED GOOD. RAN RT ENGINE TO TAKEOFF TORQUE. ONLY MADE 82 PERCENT AT 650 DEGREES. REMOVED AND REPLACED RT TORQUE INDICATOR. RAN ENGINE TO TAKEOFF TORQUE, 84 PERCENT AT 610 DEGREES. OPS CHECK GOOD. ALSO, RAN ENGINE AT ALL POWER SETTINGS AND TORQUE STAYED STEADY. OPS CHECK. 1L72 4T4 T A8SW E4WE 19951222001401995122200140SW 1995 12 22 SWIA95692 119951212A2751 POTENTIOMETER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP TE FLAPS DIRTY A SWIAD RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 NM0726974 AC664 AFTER TAKEOFF, GEAR HORN SOUNDED UPON RETRACTION. AT THIS POINT, IT WAS NOTICED THAT THE FLAP INDICATOR SHOWED FULL DOWN DEFLECTION, HOWEVER, FLAPS WERE RETRACTED. FLAPS INOP AFTER THIS. SUSPECT LOGIC BOX FAILURE. CLEANED FLAP TRANSMITTER POTENTIOMETER SEAL POT AND TERMINAL STRIP. FLAPS SYSTEM OPS CHECK GOOD. 1L72 4T4 T A8SW E4WE 19951222001411995122200141SO 1995 12 22 SWIA95693 119951212A3260 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE NLG FAILED A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07212SW 120276 AFTER TAKEOFF AT LAX, NOSE GEAR WOULD NOT COME UP. CYCLED GEAR SEVERAL TIMES AND GEAR WOULD NOT CYCLE UP OR DOWN. ELECTRICALLY OVERRIDED GEAR SUCCESSFULLY AND RETURNED TO LAX WITHOUT INCIDENT. REPLACED A-SYSTEM DOWN INDICATION PROXIMITY SENSOR. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19951222001421995122200142SO 1995 12 22 SWIA95694 119951213A3297 HARNESS EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT MLG FAILED A SWIAO OTHER N FALSE WARNING CRCRUISE 1 NM07186SW 120034 LT 'A' GEAR LIGHT ILLUMINATED IN-FLIGHT. GEAR WOULD NOT EXTEND NORMALLY. USED ELECTRIC OVERRIDE. REMOVED AND REPLACED UP AND DOWNLOCK WIRING HARNESS. PROBLEM STILL EXISTS. REPAIRED WIRING HARNESS ON UP AND DOWNLOCK SWITCHES. CYCLED GEAR UP AND DOWN THREE TIMES. OPERATED NORMALLY. LT 'A' GEAR LIGHT NO LONGER ILLUMINATED. 2L72 4T4 TRTA31SO E20NE 19951222001431995122200143SO 1995 12 22 SWIA95695 119951215A3260 PROX SENSOR EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT MLG MALFUNCTIONED A SWIAO OTHER N FALSE WARNING DEDESCENT 1 NM07188SW 120039 GEAR FAILED TO EXTEND NORMALLY, USED ELECTRIC OVERRIDE FOR GEAR EXTENSION, ABNORMAL LIGHT INDICATIONS A-SYSTEM RT MAIN GEAR. REPLACED RT AIR/GROUND PROXIMITY SENSOR PER MM 32-01-01. LANDING GEAR FUNCTION CHECKS GOOD. 2L72 4T4 TRTA31SO E20NE 19951222001441995122200144NM 1995 12 22 UPS5O5147 119951215A3350 EEL DIODE CARD BOEING757 75724APF 1384969NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST UKUNKNOWN 1 SO01413UP 23853 EMERGENCY UNARMED LIGHT MODULE ONLY HAD ONE BULB ILLUMUMINATE. REMOVED AND REPLACED DIODE CARD AND LENS ASSEMBLY. OPS CHECK GOOD. 2L72 4F RTA2NM 19951222001451995122200145NM 1995 12 22 9520532276 119951215A3350 EEL WIRE BOEING727 727251 138408HNM PAX DOOR BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01276US 21155 DURING PREFLIGHT, FOUND MAIN CABIN FORWARD DOOR EMERGENCY SLIDE LIGHT SWITCH SAFETY WIRE BROKEN. REPLACED BATTERY AND SECURED SWITCH BALL, CHECKED OK. 2L73 4F A3WE 19951222001461995122200146NM 1995 12 22 9520542201 119951215A4900GTCP8598C APU WIRING BOEING727 727251 138408HNM RT MLG WW BURNED A NWAAF ACTIVATE FIRE EXT. BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION ININSP/MAINT 1 GL01201US380162416 22154 AT THE GATE WHILE APU WAS RUNNING, THE PILOT NOTICED THE SMELL OF BURNT ELECTRICAL WIRING FOLLOWED BY APU FIRE WARNING LIGHT. THE PILOT PULLED THE FIRE HANDLE AND DISCHARGED THE FIRE BOTTLE. MAINTENANCE CLEANED AND INSPECTED THE WHEEL WELL AREA FINDING BURNT WIRING IN THE APU SHROUD. APU WAS LISTED ON MEL. 2L73 4F A3WE 19951222001471995122200147NE 1995 12 22 9520552762 219951217A7230 COMPRESSOR BOEING727 7272M7 138407SNM PWA JT8 JT8D17 52049NE ENGINE STALLED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01722RW 21201 COMPRESSOR STALL ON TAKEOFF, ENGINE POSITION UNDETERMINED AND THE TAKEOFF WAS ABORTED. THE ENGINES WERE RUNUP AND CHECKED, NO DISCREPANCIES WERE NOTED. THE AIRCRAFT CONTINUED AS SCHEDULED. 2L73 4F4 F A3WE E2EA 19951222001481995122200148WP 1995 12 22 9520569912 119951214A7711 EPR TRANSMITTER DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01962N 47406 678061 NR 2 ENGINE EPR INDICATION LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT. 2L72 4F4 F A6WE E2EA 19951222001491995122200149WP 1995 12 22 9520579927 119951217A2910 HYD SHUTOFF VLV DOUG DC9 DC931 3022065WP RT HYD SYST FAILED A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL018920E 45835 DURING APPROACH, THE AIRCRAFT LOST HYDRAULIC QUANTITY AND PRESSURE. ALSO, THE LANDING GEAR WOULD NOT EXTEND USING ALTERNATE HYDRAULIC PUMP. EXTENDED LANDING GEAR USING EMERGENCY EXTENSION LEVER. FOUND HYDRAULIC SOLENOID SHUTOFF VALVE DAMAGED. REPLACED THE VALVE, ENGINE PUMP, AUXILIARY PUMP, ALTERNATE PUMP, RIGHT SIDE HYDRAULIC SYSTEM FILTERS AND SERVICED RESERVOIR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001501995122200150WP 1995 12 22 9520589984 119951217A3350 EEL SIGN DOUG DC9 DC932 3022066WP AFT DOOR MISSING A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING LINE CHECK, FOUND VERTICAL EMERGENCY EXIT FLOOR TRACK LIGHTING SIGN MISSING AT AFT DOOR. INSTALLED SIGN AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001511995122200151WP 1995 12 22 9520599942 119951217A3350 EEL SIGN DOUG DC9 DC932 3022066WP AFT DOOR BROKEN A NWAAK NONE O OTHER ININSP/MAINT 1 GL013991C 47175 DURING LINE CHECK, FOUND AFT DOOR ESCAPE PATH EXIT SIGN BROKEN. REPLACED SIGN AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001521995122200152WP 1995 12 22 9520609607 119951216A3350 EEL POWER SUPPLY DOUG DC9 DC932 3022066WP TAILCONE INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01607NW 47232 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHT INOPERATIVE. FOUND POWER SUPPLY SHORTED DUE TO DE-ICE FLUID. REPLACED THE POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001531995122200153WP 1995 12 22 9520619962 119951216A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01914RW 47362 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS AFT OF OVERWING EXITS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001541995122200154WP 1995 12 22 9520629993 119951215A3350 EEL SIGN DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A NWAAK NONE L NO TEST UKUNKNOWN 1 GL01913RW 47171 FLIGHT ATTENDANT FOUND LEFT AFT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SIGN AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222001551995122200155WP 1995 12 22 9520631158 119951218A3610 PNEU MANIFOLD DOUG DC10 DC1040 3023508WP NR 2 FAILED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01158US 46767 DURING CLIMB, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED INTERMITTENTLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. ITEM ENTERED IN MINIMUM EQUIPMENT LIST AND AIRCRAFT APPROVED FOR SERVICE. 2L73 4F A22WE 19951222001561995122200156WP 1995 12 22 9520649886 119951216A3350 EEL WIRE DOUG DC9 DC951 3022051WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01600TR 47783 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 16 WITH BROKEN WIRE. REPAIRED WIRE AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001571995122200157WP 1995 12 22 9520659886 119951216A3350 EEL SOCKET DOUG DC9 DC951 3022051WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01600TR 47783 DURING LINE MAINTENANCE INSPECTION, FOUND TWO CEILING EMERGENCY LIGHTS OVER AFT FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPAIRED SOCKET AND REPLACED BULB, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001581995122200158WP 1995 12 22 9520669886 119951216A3350 EEL SOCKETS DOUG DC9 DC951 3022051WP CABIN FAILED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01600TR 47783 DURING LINE MAINTENANCE INSPECTION, FOUND TWO OVERHEAD EMERGENCY LIGHTS WITH BAD SOCKETS. CLEANED AND REPAIRED AFT OVERHEAD SOCKET. REPAIRED CENTER PRONG ON FORWARD SOCKET AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001591995122200159WP 1995 12 22 9520679870 119951216A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01779NC 48101 DURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS AT ROWS 21 THROUGH 26 INOPERATIVE. REPLACED BATTERIES AT ROW 22R AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001601995122200160WP 1995 12 22 9520689857 119951216A3350 EEL WIRES DOUG DC9 DC951 3022051WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01766NC 47739 DURING PERIODIC CHECK, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SECTION ONE VERY DIM. REPAIRED BROKEN WIRES AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001611995122200161WP 1995 12 22 9520699857 119951217A3350 BATTERY DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01766NC 47739 DURING PERIODIC CHECK, LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS AND THIRD SECTION OF FLOOR PROXIMITY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY AND OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001621995122200162WP 1995 12 22 9520709138 119951217A3350 EEL POWER SUPPLY DOUG DC9 DC915 3022036WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019348 45787 DURING PERIODIC CHECK, FOUND MID CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK OK. 2L72 4F A6WE 19951222001631995122200163NM 1995 12 22 95DEA001893 119951220A7110 NOSE COWL DOUG MD11 MD11F 3023600NM NR 2 ENGINE SEPARATED A FDEAK NONE D INFLIGHT SEPARATION UKUNKNOWN 1 SO25617FE 48748 EN ROUTE FROM VANCOUVER TO MEMPHIS, THE TOP OF THE NR 2 ENGINE INTAKE COWLING SEPARTED FROM THE AIRCRAFT, RESULTING IN DAMAGE TO NOSE COWL AND THE LEADING EDGE OF THE VERTICAL STABILIZER. NOSE COWL REMOVED AND REPLACED. BULKHEAD BLANKETS REPLACED AND REPAIRED, RESEALED BY DOUGLAS SUPPORT TEAM PER FAA FORM 337 DATED 14 DEC 1995 DOCUMENTS ON FILE. SECONDARY DAMAGE TO VERTICAL STAB LEADING EDGE REPAIRED AND REPLACED PER DOCUMENTATION NOTED ABOVE. 2L73 4F RTA22WE 19951222001641995122200164CE 1995 12 22 BIER950028 119951219A32501698200385 STEERING ADAPTER BEECH 23 C24R 1151254CE NLG CRACKED B BIEAK NONE O OTHER ININSP/MAINT 1 EA216006L MC640 FOUND NOSE GEAR STEERING ADAPTER BENT AT CLEVIS ATTACH POINT AND ADAPTER ATTACH BOLT PULLED OUT OF ADAPTER. FURTHER INSPECTION REVEALED CRACKED ADAPTER AND PULLED THREADS. SUBMITTER STATES SUSPECTS IMPROPER TOWING TO BE THE CAUSE. 1L71 3O A1CE 19951222001651995122200165WP 1995 12 22 ERA00022 119951210A33506104781 BATTERY PACK GRIMES CVAC 340 34031 2422704WP CABIN DISCHARGED A ERAAK NONE L NO TEST ININSP/MAINT 1 AL03538JA 34 TWO INTERIOR EMERGENCY LIGHTS INOP, LT SIDE FACING FORWARD ROW 5 AND 8. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKS GOOD. 2L72 4R 6A6 19951222001661995122200166NM 1995 12 22 P5CA9500873 119951208A53478121688 SEAT TRACK BOEING747 747122 1384872NM RT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 FOUND FIRST OFFICER'S AFT INBOARD SEAT TRACK CRACKED. REMOVED AND REPLACED SAME IAW MM 25-11-01. 2L74 4F A20WE 19951222001671995122200167NM 1995 12 22 P5CA9500874 119951208A5347811371411 SEAT TRACK BOEING747 747122 1384872NM LT COCKPIT CRACKED A P5CAK NONE O OTHER ININSP/MAINT 1 WP23852FT 19757 FOUND CAPTAIN'S FORWARD OUTBOARD SEAT TRACK CRACKED. REMOVED AND REPLACED SAME IAW MM 25-11-01. 2L74 4F A20WE 19951222001681995122200168NM 1995 12 22 SCNA95287 119951211A5313 STRINGER BOEING727 7272A1 138407FNM BS 312-328 MISSING A SCNAK NONE O OTHER ININSP/MAINT 1 GL15287SC 21345 DURING HEAVY MAINTENANCE VISIT, A PIECE OF STRINGER 24R WAS FOUND MISSING IN THE NOSE GEAR TUNNEL AREA AT STATION 312 TO 328. APPROXIMATELY 1 INCH BY .3750 INCH OF MATERIAL WAS MISSING. FABRICATED AND INSTALLED STRINGER REPAIR IAW B727 SRM 51-30-1, 51-8-1, 53-10-3 AND 51-30-3. 2L73 4F A3WE 19951222001691995122200169NM 1995 12 22 SCNA95288 119951202A33506104781 BATTERY PACK BOEING727 727282 2F0R NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15281SC 21949 DURING LINE CHECK, THE EMERGENCY EXIT LIGHT AT THE LOWER AFT AIRSTAIR DOOR, L-2 LOWER EXIT LIGHT AND FLOOR TRACK LIGHTING FROM SEAT 30 TO 34 CAME ON MOMENTARILY AND THEN WENT OUT. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01 AND EMERGENCY LIGHTS CHECKED NORMAL. 2L73 4F RTA3WE 19951222001701995122200170NM 1995 12 22 SCNA95289 119951211A3350S106 BATTERY PACK BOEING727 7272A1 138407FNM AFT AIRSTAIR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15286SC 21601 THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERIES IN AFT AIRSTAIR EMERGENCY EXIT LIGHT AND LIGHT CHECKED GOOD. 2L73 4F A3WE 19951222001711995122200171WP 1995 12 22 SCNA95290 119951215A256014111101 SLIDE BATTERIES DOUG DC10 DC1015 3022118WP R-2 DOOR FAULTY A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15151SY 48295 THE R-2 DOOR EVACUATION SLIDE WOULD NOT TEST. REMOVED AND REPLACED BATTERIES FOR THE EVACUATION SLIDE AND SELF TESTED IAW MM 25-61-03, OPS CHECKED GOOD. 2L73 4F A22WE 19951222001721995122200172WP 1995 12 22 SCNA95291 119951215A261113131 SMOKE DET LAMP DOUG DC10 DC1015 3022118WP CARGO COMPT FAILED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15151SY 48295 THE NUMBER 3 CARGO SMOKE DETECTOR WOULD NOT TEST. RELAMPED DETECTOR AND UNIT OPS CHECKED GOOD. 2L73 4F A22WE 19951222001731995122200173NM 1995 12 22 SCNA95292 119951213A33501060091102 EEL BOEING727 7272A1 138407FNM CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15287SC 21345 THE FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. INSTALLED NEW EMERGENCY EXIT LIGHT IAW B727 MM 33-50-00. 2L73 4F A3WE 19951222001741995122200174NM 1995 12 22 UPS205148 119951216A335037067001 BATTERY BOEING727 72725C 138400HNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01937UP 19302 MAINTENANCE REPORTED, DURING WEEKEND CHECK EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND OPS CHECK GOOD. 2L73 4F A3WE 19951222001751995122200175NM 1995 12 22 UPS205152 119951216A323037067001 RETRACT MECH BOEING727 72722C 138400FNM NLG LACK OF LUBE A IPXAO OTHER J WARNING INDICATION LDLANDING 1 SO01928UP 19091 CREW REPORTED, NOSE GEAR DID NOT EXTEND ON FIRST ATTEMPT AND RED DOOR LIGHT ON FWD PANEL. MAIN GEAR EXTENDED NORMALLY AND ALL GEAR EXTENDED NORMALLY ON SECOND ATTEMPT. JACKED NOSE GEAR AND LUBED NOSE GEAR, RETRACTED AND EXTENDED GEAR SEVERAL TIMES AND OPS CHECK GOOD. 2L73 4F A3WE 19951222001761995122200176NM 1995 12 22 UPS405144 119951215A2612 FIRE LOOP BOEING747 747123 1384873NM APU MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01671UP 20323 WHILE IN FLIGHT AND WITH APU OFF, APU DET LOOP-A ILLUMINATES OCCASIONALLY, SETTING OFF APU FIRE SIGNAL. APU FIRE LOOP-A PLACARDED INOP PER MEL 26-7 ASSIGNED M-103273. 2L74 4F A20WE 19951222001771995122200177EU 1995 12 22 95ZZZX6783 119951117A21208810K12 VALVE SWITCH CUTLERHAM FOKKERF27 F27MK500 4990629EU COPILOT'S PANEL BURNED A MTNAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO05707FE 10371 GRR/IND - EN ROUTE, THE FLIGHT CREW DETECTED A BURNING SMELL IN THE COCKPIT. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO GRR. AFTER AN INSPECTION BY THE MECHANIC, IT WAS DETERMINED THE SPILL VALVE SWITCH WAS FAULTY. 2H72 4T A817 19951222001781995122200178CE 1995 12 22 95ZZZX6784 119950830A3240 BRAKE LINE BEECH 18 D18S 1151004CE RT MLG OUT OF POSITION A GGPAO OTHER O OTHER CLCLIMB 1 NM011827M9062 A394 LOP/ESO - AIRCRAFT GOING FROM LOP TO ESO, PILOT FELT A SMALL BUMP AFTER GEAR WAS RETRACTED. AIRCRAFT LANDED AT ESO AND PILOT NOTICED RT GEAR DOOR OUTBOARD SIDE WAS BENT. AIRCRAFT WAS FERRIED TO PAE FOR REPAIR. DOOR CAUGHT SHIFTED BRAKE LINE. NO DAMAGE TO LINE. ISOLATED INCIDENT. BRAKE LINE SECURED CLEAR OF DOOR ACTION. 1L72 3R A765 19951222001791995122200179CE 1995 12 22 95ZZZX6785 119950929A3230ANLM250 LIMITER BEECH 1900 1900D 1154162CE LANDING GEAR BLOWN A GPPAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 CE0938537 UE158 CLE - PLANE DEPARTED. UPON TRYING TO RETRACT GEAR, RECEIVED NO INTRANSIT LIGHTS INDICATION OF MOTOR OPERATION. PILOTS THEN TURNED BACK AND LANDED AT CLE. FLT 2403 DEPARTING CLE, REMOVED AND REPLACED BLOWN CURRENT LIMITER. 2L72 4T RTA24CE 19951222001801995122200180 1995 12 22 95ZZZX6786 319951101A61128022591 DEICE BOOT AEROSPATR42 ATR42300 8680920EU RT PROP BLADE SHORTED/BURNED A NVEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO03293AT 293 CREW REPORTS RIGHT PROPELLER BLADE DE-ICE BOOT SHORTED OUT CAUSING SPARKS AND A RED GLOW. DEACTIVATED THE SYSTEM AND LANDED WITHOUT INCIDENT. REPLACED PROPELLER BLADE. (X) 2H72 4T RTA53EU 19951222001811995122200181WP 1995 12 22 95ZZZX6787 119951031A2612D5020 FIRE LOOP DOUG DC8 DC862 3021970WP NR 2 ENGINE BROKEN A RIAAF ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 SO198974U 46110 LICZ/ETAR - FLT BEHF800 - FIRE INDICATION DURING FLIGHT AT CRUISE ON NR 2 ENGINE. SHUT DOWN ENGINE, AND FIRED BOTH FIRE BOTTLES. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND FIRE LOOP BROKEN AND SHORTED. REPLACED LOOP AND BOTH FIRE BOTTLES. SYSTEM OPERATED GOOD ON GROUND. NO CAUSE FOR ORIGINAL BREAK WAS FOUND. 2L74 4F 4A25 19951222001821995122200182NM 1995 12 22 95ZZZX6789 119951031A273065C370525 PCU BOEING737 7372L9 1384497NM RUDDER FAILED A AZZDAK NONE K FLUID LOSS ININSP/MAINT 1 SO15737Q 5734 21279 DURING MAINTENANCE, DISCOVERED THE RUDDER BEGAN TO FLUTTER WHEN THE SYSTEM WAS PRESSURIZED. VISUAL INSPECTION REVEALED THE RUDDER POWER CONTROL UNIT (PCU) WAS LEAKING AND VERY HOT. REPLACED THE RUDDER PCU. POWER CONTROL UNIT WAS OVERHAULED BY AERO CONTROLS, INC., 6-28-95. THIS IS THE SECOND FAILURE OF A PCU OVERHAULED BY AERO CONTROL, INC., WITHIN SIX MONTHS. 2L72 4F RTA16WE 19951222001831995122200183EU 1995 12 22 95ZZZX6790 119950801A3040111267 CONTROLLER BAG JETSTMJETSTM3101 1500215EU LT WINDSHIELD FAILED A CX7AA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL03827JS12632 697 GRR - AFTER TAKEOFF, PILOT NOTICED SMOKE IN COCKPIT. RETURNED TO GRR. INSPECTION FOUND WINDSHIELD HEAT CONTROLLER FAILED WHICH CAUSED SMOKE AROUND LOWER LEFT SIDEWALL NEXT TO RUDDER PEDALS. 2L72 4T RTA21EU 19951222001841995122200184EU 1995 12 22 95ZZZX6791 119951017A2910 HYDRAULIC LINE BAG JETSTMJETSTM3101 1500215EU LANDING GEAR LOOSE A CX7AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL03832JS 721 DSM - EN ROUTE, AIRCRAFT LOST HYDRAULIC PRESSURE. USED EMERGENCY LANDING GEAR PUMP TO LOWER GEAR. UNEVENTFUL LANDING. MECHANIC FOUND HYDRAULIC LINE TO THE PUMP CHECK VALVE LOOSE. REMOVED THE LINE, CLEANED FLARE AND SEAT THEN REINSTALLED. LEAK CHECK SATISFACTORY. 2L72 4T RTA21EU 19951222001851995122200185EU 1995 12 22 95ZZZX6792 119951026A29107445B HYD RELEASE VLV BAG JETSTMJETSTM3101 1500215EU WS 36 LEAKING A CX7AA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL03832JS 721 MIDWAY - FLT 168 - DEPARTED, MAIN HYDRAULIC SYSTEM PRESSURE FLUCTUATED AND THEN LOST PRESSURE. PILOT RETURNED TO MIDWAY. USED EMERGENCY LANDING GEAR HAND PUMP TO LOWER GEAR. LANDING WAS UNEVENTFUL. MECHANIC FOUND HYDRAULIC SYSTEM RELEASE VALVE LEAKING EXTERNALLY. REPLACED VALVE, LEAK CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19951222001861995122200186EU 1995 12 22 95ZZZX6793 119951017A2910 LINE BAG JETSTMJETSTM3101 1500215EU HYDAULIC SYSTEM LOOSE A CX7AO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 GL03832JS 721 DSM - EN ROUTE, AIRCRAFT LOST HYDRAULIC PRESSURE. USED EMERGENCY LANDING GEAR PUMP TO LOWER GEAR. UNEVENTFUL LANDING. MECHANIC FOUND HYDRAULIC LINE TO THE PUMP CHECK VALVE LOOSE. REMOVED THE LINE, CLEANED FLARE AND SEAT THEN REINSTALLED. LEAK CHECK SATISFACTORY. 2L72 4T RTA21EU 19951222001871995122200187CE 1995 12 22 95ZZZX6794 119951023A324621400100 CUP BEARING 40273A BEECH 1900 1900 1154160CE NR 1 MLG FAILED A AGUUAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO1917ZR 41 1300 UB17 MIA/MCO - FLT 395 - PILOT REPORT: HALF-WAY TO TAXIWAY FELT SHIMMY, RETURNED TO GATE. NOTICED NR 1 MAIN WHEEL ASSY WAS CANTERED. MAINENTANCE: INSPECTED FOR FURTHER DAMAGE. REPLACED LOWER SHOCK STRUT ASSY, LT MAIN WHEEL ASSY, AND LT BRAKE ASSY. MAIN WHEEL ASSY SENT TO MFG FOR ANALYSIS. 2L72 4T RTA24CE 19951222001881995122200188CE 1995 12 22 95ZZZX6795 119951006A3260C2006 SWITCH BEECH 1900 1900 1154160CE GEAR HORN FAILED A GUUAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 SO19194GA UB8 MCO/MIA - FLT 486 - PILOT REPORT: GEAR WARNING HORN DOES NOT SOUND WHEN RED GEAR HANDLE LIGHT COMES ON. MAINTENANCE: TROUBLESHOT AND REMOVED AND REPLACED GEAR HORN SILENCE SWITCH. OPS CHECK GOOD, AIRCRAFT RELEASED. 2L72 4T RTA24CE 19951222001891995122200189NM 1995 12 22 95ZZZX6798 119950919A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554337 20491 MCI - DURING CHECK-C, FOUND .25 INCH CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER CUT-OUT. REPAIRED PER SSRM 53-30-206. AIRCRAFT TOTAL TIME: 61,301 HOURS; 41,020 CYCLES. 2L73 4F A3WE 19951222001901995122200190WP 1995 12 22 95ZZZX6799 119950929A5101 STRUCTURE DOUG DC9 DC983 3022083WP AIRFRAME LIGHTNING STRIKEA TWAAO OTHER CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059409F 53121 STL - FLT 464 - DURING CRUISE, EXPERIENCED A POSSIBLE LIGHTNING STRIKE WITH ACCOMPANYING AIR NOISE AND SMOKE IN THE CABIN. ALL OPERATIONS AND INDICATIONS WERE NORMAL. PERFORMED LIGHTNING STRIKE/STATIC DISCHARGE CONDITION CHECK. CHECKED NR 1 ENGINE FOR POSSIBLE COMPRESSOR STALL, CHECKED TAIL COMPARTMENT AIR CONDITIONING SYSTEM. ALL CHECKS WERE FOUND TO BE NORMAL. CHECK C-1D - 5-18-95 - MCI. 2L72 4F RTA6WE 19951222001911995122200191WP 1995 12 22 95ZZZX6800 119951003A4990 OIL DOUG DC9 DC983 3022083WP APU OVERSERVICED A TWAAB EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059409F 53121 IND - FLT 444 - DURING CRUISE, SMOKE STARTED ENTERING CABIN. DESCENDED TO 8,000 FEET. FOUND APU OIL OVERSERVICED. SERVICED APU TO PROPER LEVEL AND REPLACED BOTH COALESCER BAGS, MFG P/N 22D10. AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. CHECK C-1A - 5-18-95 - MCI. 2L72 4F RTA6WE 19951222001921995122200192WP 1995 12 22 95ZZZX6801 119951028A25308203110000 OVEN DOUG DC9 DC983 3022083WP GALLEY SMOKING A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059413T 53188 PDX - FLT 173 - DURING CRUISE, 'D' GALLEY OVEN, MFG P/N 8203-11-0000, EMITTED SMOKE. OVEN WAS TURNED OFF AND CIRCUIT BREAKER PULLED. TROUBLESHOOTING UNDERWAY TO DETERMINE CAUSE. OP-16 - 8-25-95 - MCI. 2L72 4F RTA6WE 19951222001931995122200193WP 1995 12 22 95ZZZX6802 219951024A7260 GEAR BOX BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A SABAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05170PC 717 P63222 BWI/SHD - FLT 5116 - FLIGHT JUST DEPARTED, LT ENG OIL PRESS LIGHT ILLUMINATED. PRESS GAUGE DROPPED TO ZERO & ENG STARTED TO SHUT ITSELF DOWN. FLT CREW MANUALLY SHUT ENG DOWN. THEY DECLARED AN EMERGENCY & RETURNED TO BWI WHERE THEY MADE A SAFE LANDING. MX DISPATCHED FROM CLT. IN BWI, EXAMINED ENG & FND EVIDENCE OF OIL LEAK IN NOSE CASE AREA. SEVERAL BOLTS ON NOSE CASE FND LOOSE WERE RETORQUED. ENG SERVICED WITH OIL & A DRY MOTORING RUN PERFORMED. NO LEAKS FND. ENG OIL AGAIN RE-SERVICED & ENG START ATTEMPTED, ENG DID NOT START. GRBX DRAIN PLUG REMOVED & APPROX 5 GAL OF OIL DRAINED FROM GRBX. T/S REVEALED DRIVE GR FOR SCAV PUMP ONLY TURNING 1/3 THE TIME. ENG REMOVED & REPLACED & A/C RETURNED TO SERV. 2L72 4T4 TRTA21EU E4WE 19951222001941995122200194SO 1995 12 22 95ZZZX6803 219951013A8530653142 CYLINDER ASSY CESSNA207 T207A 2073614CE CONT O520 TSIO520M 17040SO NR 4/6 CRACKED A aGSUAO OTHER J WARNING INDICATION CRCRUISE 1 WP193156X 1246 T20700376 522456 ENGINE OPERATION NORMAL ON TAKEOFF, CLIMB, AND CRUISE SETTING. ROUGHLY 15 MINUTES INTO FLIGHT, THE ENGINE LOST MANIFOLD PRESSURE. FULL THROTTLE MANIFOLD PRESSURE WAS 25 INCHES. PILOT LANDED WITHOUT INCIDENT. INSPECTION FOUND THE NR 4 CYLINDER HAD CRACKED ON THE EXHAUST SIDE OF THE CYLINDER HEAD AND HAD STARTED MELTING THE NR 6 CYLINDER HEAD ASSY. THE TWO AFFECTED CYLINDER ASSEMBLIES WERE REPLACED. THE OIL FILTER INSPECTED AND REPLACED. NO OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 1H71 3O3 O A16CE E8CE 19951222001951995122200195WP 1995 12 22 AALA951777 119951012A3350 EEL WIRE DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07593AA 53256 DFW - DURING OVERNIGHT CHECK, FOUND THE FIRST CLASS FORWARD EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED WIRE ON FIRST CLASS FORWARD EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA6WE 19951222001961995122200196CE 1995 12 22 BUHA95002 119951101A326021EN96 DOWNLOCK SWITCH MTSBSIMU2 MU2B36 5780412CE LANDING GEAR FAILED AL BUHAO OTHER N FALSE WARNING TOTAKEOFF 1 GL23201UV 680 INTERNAL FAILURE OF NOSE GEAR DOWNLOCK SWITCH ALLOWED INDICATOR LIGHT VOLTAGE TO BLEED OVER TO THE LANDING GEAR CONTROL SECTION OF THE SWITCH. (X) 1H72 3T RTA10SW 19951222001971995122200197NE 1995 12 22 C1HA9502110 219951025A7532 PBRC VALVE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 4 ENGINE LACK OF LUBE A C1HACD ABORTED TAKEOFF RETURN TO BLOCK ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 WP23802MG 46098 669668 YYC - REJECTED TAKEOFF AT 103 KNOTS. RETURNED TO THE RAMP DUE TO COMPRESSOR STALL ON NR 4 ENGINE. ON POST-FLIGHT, FOUND NR 6 TIRE OVERHEATED AND BLOWN FUSE PLUG. REMOVED AND REPLACED NR 5 AND NR 6 MAIN WHEEL ASSEMBLIES IAW MM 32-40-2. PERFORMED INSPECTION OF FUSELAGE, ENGINE, AND BRAKES BECAUSE OF REJECTED TAKEOFF. NO DEFECTS NOTED. SUSPECT NR 4 ENGINE PBRC VALVE STICKING. LUBED SAME. RAN ENGINE FULL TAKEOFF POWER. RESULTS SATISFACTORY. AIRCRAFT RELEASED FOR FLIGHT. (X) 2L74 4F4 F 4A25 1E8 19951222001981995122200198NM 1995 12 22 C1HA9502210 119951030A33501104441 EEL MTG PLATE BOEING727 727223 1384074NM R-1 DOOR BROKEN A C1HAK NONE L NO TEST ININSP/MAINT 1 WP236804 19479 R-1 OVERHEAD EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. BATTERY PACK TESTS GOOD. SUSPECT MOUNTING PLATE ASSY. REMOVED AND REPLACED MOUNTING PLATE ASSY. OPS CHECK NORMAL DURING TEST PER MM 33-00-00. (X) 2L73 4F A3WE 19951222001991995122200199NM 1995 12 22 CA950197 119951003A3350 EEL WIRE BOEING727 727223 1384074NM CABIN BROKEN A C1HAK NONE L NO TEST ININSP/MAINT 1 WP236804 19479 AFT FLOOR LIGHTING FROM SEAT 14 TO THE REAR OF CABIN IS DIM. REPAIRED BROKEN WIRE AT AFT GALLEY. OPS CHECK OK. (X) 2L73 4F A3WE 19951222002001995122200200NE 1995 12 22 CA950208 219951013A7200 ENGINE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 1 MALFUNCTIONED A C1HACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP23802MG 46098 ABORTED TAKEOFF AT 105 KNOTS AND RETURNED TO RAMP. DUE TO SUSPECTED NR 1 ENGINE STALL, INSPECTED AIRFRAME, MLG, ENGINE. ALL GROUND CHECKS NORMAL. RAN ENGINE AT LOW POWER, ALL PARAMETERS NORMAL. PNEUMATIC DECAY CHECK. NO DEFECTS NOTED IAW DAC DC-8 MM. RELEASED FOR FLIGHT. (X) 2L74 4F4 F 4A25 1E8 19951222002011995122200201NM 1995 12 22 CA950217 119951013A3230 UPLATCH HOOK BOEING727 727223 1384074NM LT MLG OUT OF ADJUST A C1HAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP236821 19496 ON PRE-FLIGHT, FOUND LEFT GEAR RED UNSAFE LIGHT ON. ALL OTHER INDICATIONS NORMAL. AIRCRAFT ISSUED FERRY PERMIT TO FLY TO MAINTENANCE AT EWR. AFTER TAKEOFF, UNABLE TO RAISE LEFT MLG. DIVERTED TO DALFORT AVIATION IN DALLAS FOR REPAIR. DALFORT JACKED AIRCRAFT PER MM 32-32-0 AND FOUND GEAR UPLATCH HOOK OUT OF SEQUENCE. RETURNED UPLOCK HOOK TO UNLOCKED POSITION. PERFORMED GEAR SWING - GEAR POSITION INDICATION NORMAL. (X) 2L73 4F A3WE 19951222002021995122200202NM 1995 12 22 CAL950982 119951028A3260 BRACKET BOEING737 7373Q8 1384670NM LDG LEVER SW LOOSE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0919382 26311 BWI - FLT 1623 - WHEN GEAR WAS EXTENDED FOR LANDING AT BWI, THE CREW RECEIVED 3 GREEN AND 3 RED GEAR INDICATION LIGHTS WITH GROUND PROXIMITY WARNING. THE GEAR WAS CYCLED AND ON THE THIRD TRY, THE CREW RECEIVED 3 GREEN LIGHTS WITH NO RED LIGHTS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SUPPORT BRACKET FOR LANDING GEAR LEVER SWITCH LOOSE. THE SUPPORT BRACKET WAS ADJUSTED IAW MM 32-61-11 AND GEAR INDICATIONS AND OPERATION WERE GOOD. (X) 2L72 4F RTA16WE 19951222002031995122200203NM 1995 12 22 EISA95423 119951108A3260656021132 ACCESSORY UNIT BOEING727 727223 1384074NM LANDING GEAR MALFUNCTIONED A aEISAO OTHER N FALSE WARNING CLCLIMB 1 SW07313NE R00272 19702 CLIMBING THROUGH 13,000 FEET, RED GEAR UNSAFE LIGHT AND GREEN LIGHT CAME ON SIMULTANEOUSLY. MOVED GEAR HANDLE TO UP, LIGHTS REMAINED ON. PUT GEAR HANDLE DOWN, LEFT GEAR UNSAFE LIGHT CAME ON AND RIGHT GEAR UNSAFE LIGHT WENT OUT. GEAR CAME UP NORMALLY, RED UNSAFE LIGHT CAME BACK ON AND LEFT UNSAFE LIGHT WENT OUT. RIGHT GEAR UNSAFE LIGHT FLICKERED ON AND OFF REMAINDER OF FLIGHT. APPROACH TO IND GEAR DOWN, RED UNSAFE LIGHT ON, BOTH MAINS CAME ON. SECONDARY MAIN GEAR LIGHTS INDICATE GREEN. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT, PERFORMED ADJUSTMENT AND TEST IAW MM 32-09-121. OPS CHECK GOOD. (X) 2L73 4F A3WE 19951222002041995122200204NE 1995 12 22 JBXA950601 219950627A75301685MK6 VSV ACTUATOR AIRBUS320 A320231 3930325EU IAE V2500 V2500A1 NE NR 2 ENGINE INOPERATIVE A JBXAE ENGINE SHUTDOWN M OVER TEMP DEDESCENT 1 SO05300ML6179 317 V0107 BOS/RDU - FLT 16 - GOT ECAM MESSAGE, "NR 2 COMPRESSOR VANE MESSAGE". FOLLOWING MESSAGE, ENGINE SURGED. ENGINE WAS SHUT DOWN. LANDING WAS UNEVENTFUL. POST-FLIGHT REPORT REVEALED ENGINE HAD EXCEEDED ALLOWABLE EGT LIMITS. ENGINE WAS REMOVED AND REPLACED. (X) 2L72 4F4 FRTA28NM E311NE 19951222002051995122200205 1995 12 22 JBXA950701 419950703A2565D30664103 EVAC SLIDE AIRBUS320 A320231 3930325EU R-1 DOOR DEPLOYED A JBXAO OTHER O OTHER TXTAXI/GRND HDL 1 GL31303ML 304 FLT 167 - WHILE AT GATE ON 7-3-95, FLIGHT ATTENDANT LIFTED R-1 DOOR HANDLE TO 'CRACK' DOOR FOR CATERING. EVACUATION SLIDE WAS ARMED AND SLIDE DEPLOYED. NO INJURIES WERE REPORTED. AIRCRAFT WAS FERRIED BACK TO RDU WHERE SLIDE WAS REPLACED. (X) 2L72 4F RTA28NM 19951222002061995122200206EU 1995 12 22 RAIA951020 119951015A5270 WARNING LIGHT JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR ILLUMINATED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03553HK 41066 SBN - FLT 7495 - CARGO DOOR WARNING ILLUMINATED. MAINTENANCE DEFERRED CARGO LIGHT PR MEL 52-3, CAT C. ACFT TT, 777.3 HOURS. (X) 2L72 4T RTA41NM 19951222002071995122200207EU 1995 12 22 REXA95059 119950918A33506104781 EEL BATTERY GRIMES SAAB SF340 340B 7860101EU CABIN DISCHARGED A REXAK NONE L NO TEST ININSP/MAINT 1 SO25251PX 13245 340B251 FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHTS 1B AND 3B INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT BATTERY. CHECKS GOOD. (X) 2L72 4T RTA52EU 19951222002081995122200208CE 1995 12 22 S2YA950025 119951021A2731 TRIM BEECH 1900 1900D 1154162CE ELEVATOR LACK OF LUBE A S2YAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL1392SK UE92 AFTER THE FLIGHT CREW ASCENDED TO FLIGHT LEVEL 230, THEY NOTICED THE ELECTRIC ELEVATOR TRIM APPARENTLY FROZE AND WOULD NOT MOVE MANUALLY. THE CREW DECIDED TO TURN BACK TO MKE AND CALL MAINTENANCE. A MECHANIC INSPECTED THE ELEVATOR TRIM SYSTEM, REMOVED VISIBLE MOISTURE FROM THE ACTUATORS, AND RE-GREASED AS NEEDED. HE THEN OPERATIONALLY CHECKED THE SYSTEM ON THE GROUND AND FOUND OKAY. (X) 2L72 4T RTA24CE 19951222002091995122200209CE 1995 12 22 S2YA950026 119951022A2750100384040 FLAP MOTOR BEECH 1900 1900D 1154162CE TE FLAPS SHORTED A aS2YAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL1392SK 2792 526 UE92 THE FLIGHT CREW NOTICED AN UNKNOWN SOURCE OF SMOKE IN THE CABIN (ACRID SMELL) AND NOTICED THE FLAPS WOULD NOT SELECT 17 OR 35 DEGREES FROM THE FULL UP POSITION. OUTSIDE MAINTENANCE WAS CALLED AND THE MECHANIC C/W THE MAINTENANCE ACTION FOR FLAPS INOP BY PULLING BOTH CIRCUIT BREAKERS AS CALLED FOR. HE VERIFIED THE SMOKE/SMELL CAME FROM AN INTERNALLY SHORTED FLAP MOTOR. (X) 2L72 4T RTA24CE 19951222002101995122200210EU 1995 12 22 SIMA952921 119951019A77123037603 SENSOR AEROSPATR42 ATR42300 8680920EU NR 2 ENGINE DEFECTIVE A SIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21271AT 18518 273 ORD - FLT 4365 - AIR TURN-BACK. NR 2 ENGINE TORQUE SURGED PLUS AND MINUS 10 PERCENT. REMOVED AND INSPECTED T1.8 SENSOR. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19951222002111995122200211 1995 12 22 SRAA109503 419951003A22103001300017 CENT CONTL ACT BOEING747 747212B 1384886NM EMPENNAGE DEFECTIVE A ASRAAJA DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CRCRUISE 1 SO19745SJ 20888 MIA - FLT 203 - DURING FLIGHT, CREW ATTEMPTED TO ENGAGE AUTOPILOT ON CHANNEL 'A'. THIS CAUSED AIRCRAFT TO ROLL SEVERELY, SWITCHED OVER TO 'B' CHANNEL, CAUSED THE SAME RESULT. DUMPED FUEL TO MEET WEIGHT RESTRICTION AND AIR TURN BACK TO MIA. REPLACED MONITOR TEST BOX 'A' CHANNEL, ROLL COMPUTER, AND CENTRAL CONTROL ACTUATOR AT THE 'A' CHANNEL. SYSTEM OPERATED GOOD ON GROUND PER MM CHAPTERS 22, 27 AND 34. (X) 2L74 4F A20WE 19951222002121995122200212NM 1995 12 22 TAOA109519 119951028A3350900835A BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15925TS MJG14532 21244 EMERGENCY EXIT SIGN AT ROW 3 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19951222002131995122200213NM 1995 12 22 USAASB95010 119951107A77149974M82P03 CONTL ALTERNATOR BOEING737 737301 1384611NM RT ENGINE LEAKING A USAAAE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS CRCRUISE 1 EA19589US 23934 PIT - FLT 0223 - EN ROUTE IND TO BWI, NR 2 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED TO RED LINE. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND DIVERTED TO PIT. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED RT ENGINE N2 ALTERNATOR AND ROTOR DUE TO INTERNAL FAILURE. RAN ENGINE AND CHECKED CHIP DETECTORS AND OIL FILTERS. OPS CHECKED GOOD. (X) 2L72 4F RTA16WE 19951222002141995122200214EU 1995 12 22 95ZZZM722 119951015A56107256100502 WINDSHIELD SAAB SF340 340B 7860101EU COCKPIT BIRD STRIKE A NVEAO OTHER C F.O.D. CRCRUISE 1 SO03269AE 340B269 IN CRUISE, BIRD STRUCK FIRST OFFICERS FRONT CENTER WINDSHIELD. WINDOW SHATTERED BUT STAYED IN TACT NO EMERGENCY DEPRESSURIZATION OR OTHER INCIDENT. (M) 2L72 4T RTA52EU 19951222002151995122200215WP 1995 12 22 95ZZZM723 219951031A732189778025 FCU BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENGINE FAILED A NVEAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO03913AE7800 2505 913 P66221 ON APPROACH INTO CLT, THE LEFT ENGINE TORQUE, EGT, AND RPM DROPPED. CREW SHUT DOWN THE ENGINE WITH THE STOP AND FEATHER. AIRCRAFT LANDED WITHOUT INCIDENT. CHANGED LEFT FCU. THIS FCU HAS BEEN ON THIS ENGINE FOR 375.4 HOURS. (M) 2L72 4T4 TRTA56EU E4WE 19951222002161995122200216 1995 12 22 95ZZZM724 419951012A2320TP4429 ACARS PRINTER SAAB SF340 340B 7860101EU FLIGHT DECK SHORTED A NVEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO03268AE 340B268 FLT NR 4561 - CLE - CREW REPORTS SMOKE ON THE FLIGHT DECK IS COMING FROM THE ACARS PRINTER. CREW PULLED CB FOR THE PRINTER, PROBLEM WENT AWAY. CONTRACT MAINTENANCE IN CLE ISSUED MEL. PRINTER WILL BE CHANGED AT LATER DATE. (M) 2L72 4T RTA52EU 19951222002171995122200217EU 1995 12 22 95ZZZM725 119951106A77228974768 EGT CONNECTOR BAG JETSTMJETSTM3201 1500217EU LT ENGINE LOOSE GROUND A NVEAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 SO03913AE 913 FLT NR 4433 - HSV - ON APPROACH INTO HSV, THE LEFT ENGINE FLAMED OUT. AFTER ABOUT 5 SECONDS THE CREW SHUT THE SRL AND TTL SYSTEMS OFF AND THE ENGINE RELIT. AIRCRAFT CONTINUED INTO HSV WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AND CORRECTED A LOOSE GROUND WIRE ON THE LEFT ENGINE EGT COMPENSATOR CANNON PLUG. AIRCRAFT WAS TEST FLOWN ON THREE STEEP APPROACHES IN ADDITION TO GROUNDS RUNS. ALL SYSTEMS OPERATIONALLY TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA56EU 19951222002181995122200218WP 1995 12 22 95ZZZM726 119951202A7603 BEARING DOUG DC8 DC862 3021970WP POWER LEVER LACK OF LUBE A TC8AO OTHER O OTHER TOTAKEOFF 1 GL23803MG 45910 UNABLE TO SET TAKEOFF POWER NR 3 ENGINE. THROTTLE FULL FORWARD, EPR ORIGINALLY SET AT 1.6, THEN CREPT TO 1.7 N2 96 PERCENT, N1 100 PERCENT. CHECK TRAVEL THROTTLE AND FOUND CROSS SHAFT BEARING FROZEN. LUBE AND RUN-UP ENGINE. EPR READING LOW. TRANSFERRED EPR TO DMI NR 5206 AS PER MEL 77-1. (M) 2L74 4F 4A25 19951222002191995122200219 1995 12 22 95ZZZM727 419951203A3421 ADI DOUG DC8 DC862 3021970WP LT/RT FLAGGED A TC8AO OTHER J WARNING INDICATION CLCLIMB 1 GL23803MG 45910 BOTH ATTITUDE INDICATOR, BOTH COMPASS GSL/FLAG ON. RERACKED ALL ELECTRONIC EQUIPMENT FOR THIS SYSTEM. BOTH ATTITUDE INDICATORS, BOTH COMPASS NO FLAGS/GSL FLAG. (M) 2L74 4F 4A25 19951222002201995122200220EU 1995 12 22 95ZZZM728 119951120A3240AH52591 MAXARET BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A WTAAO OTHER O OTHER LDLANDING 1 WP17422UE 782 SFO - RIGHT BRAKE REPORTED INOPERATIVE DURING LANDING ROLL OUT. MAINTENANCE REPLACED RIGHT LANDING GEAR BRAKE MAXARET ASSEMBLY. RIGHT BRAKE REPORTED OPERATIONAL DURING GROUND TAXI CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222002211995122200221CE 1995 12 22 95ZZZM729 119951119A29101153800025 PWR PACK MOTOR BEECH 99 C99 1154006CE HYD SYSTEM FAILED A GUUAO OTHER J WARNING INDICATION APAPPROACH 1 SO19232BH U232 FLT NR 418 - LEFT MAIN LANDING GEAR WOULD NOT EXTEND. MANUALLY EXTENDED GEAR. REMOVED AND REPLACED HYDRAULIC POWER PACK MOTOR. OPS CHECKED NORMAL. (M) 1L72 3T A14CE 19951222002231995122200223NE 1995 12 22 95ZZZM731 219951129A7261 OIL LINE BOEING727 72731 1384010NM PWA JT8 JT8D7B 52053NE GEAR BOX LOOSE A RYNAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE07210NE 18903 657350 DURING CRUISE, THE NR 1 ENGINE OIL QUANTITY STARTED DEPLETING. THE AIRCRAFT MADE AN UNSCHEDULED LANDING AT SHV WITHOUT INCIDENT. OIL QUANTITY INDICATION WAS NEAR ZERO WITH OIL PRESS AND TEMP NORMAL. FOUND THE OIL FILTER BYPASS SWITCH RETURN LINE LEAKING AT ITS THREADED CONNECTION TO THE ACCESSORY GEAR BOX. REPAIRED THREADS WITH HELI-COIL INSERT, RECONNECTED OIL LINE, SERVICED ENGINE OIL AND LEAK CHECKED GOOD. (M) 2L73 4F4 F A3WE E2EA 19951222002241995122200224CE 1995 12 22 95ZZZM732 119951124A32331143800415 ACTUATOR BEECH 1900 1900C 1154161CE LT MLG FAILED A GUUAO OTHER P NO WARNING INDICATION APAPPROACH 1 SO19196GA 427 UB31 FLT NR 103 - MIA - LANDING GEAR APPEARED DOWN, BUT DID NOT GET GREEN UNTIL AFTER TOUCH AND GO. FOUND LEFT MAIN LANDING GEAR ACTUATOR BYPASSING INTERNALLY, ALLOWING ASSY TO CREEP OUT OF RIG. REPLACED ACTUATOR, RE-RIGGED ASSY. OPS CHECK GOOD. 2L72 4T RTA24CE 19951222002251995122200225WP 1995 12 22 95ZZZM733 119951001A2781 SENSOR LKHEED1011 10113851 5265010WP NR 2 LE SLAT OUT OF ADJUST A AMTACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL11185AT 193C1052 FLT NR 647 - IND - ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN, LEADING EDGE INTRANSIT LIGHT ON LEFT NR 2 SLAT LIGHT EXTINGUISHED. MAINTENANCE ADJUSTED NR 2 LEFT SLAT SENSOR IN ACCORDANCE WITH MM 27-82-03. OPS CHECKED NORMAL. (M) 2L73 4F A23WE 19951222002261995122200226NM 1995 12 22 95ZZZM734 119950907A5241 ROD BOEING727 727227 1384078NM LT GALLEY DOOR DISCONNECTED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11768AT 21996 IND - FLT NR 428 - THE L-2 (GALLEY DOOR) IS HARD TO OPEN AND CLOSE. IT WAS FOUND THAT THE L-2 DOOR WAS HARD TO OPEN DUE TO THE LOWER GATE ON L-2 NOT RAISING. REMOVED DOOR LINING AND FOUND THE ROD TO THE LOWER GATE DISCONNECTED. REATTACHED ROD, REINSTALLED DOOR LINING, OPS CHECK OK. (M) 2L73 4F A3WE 19951222002271995122200227WP 1995 12 22 95ZZZM735 119951001A3230 LINKAGE LKHEED1011 10113851 5265010WP LT MLG OUT OF RIG A AMTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11181AT 193L1125 IND- FLT NR 647 - ON TAKEOFF THE LEFT MAIN GEAR DID NOT RETRACT, AIRCRAFT DID TURNBACK. THE PHASE CONTROL VALVE LINKAGE WAS OUT OF RIG. RE-RIGGED LINKAGE PER MM CH 32-33-06. CYCLED LDG TEN TIMES, OPS CHECK, NORMAL PER MM CH 32-30-00. (M) 2L73 4F A23WE 19951222002281995122200228NE 1995 12 22 95ZZZM736 219950913A7240 OUTLET DUCT BOEING727 727227 1384078NM PWA JT8 JT8D17A 52049NE NR 1 ENGINE CRACKED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11772AT 22003 P696202B NR 1 ENGINE FAILED, NR 9 COMBUSTION CAN INSPECTED. INNER OUTLET DUCT AFT OF NR 9 COMBUSTION CAN CRACKED BEYOND LIMITS OF MM 72-44 PAGE 201 TO 206. REMOVED AND REPLACED NR 1 ENGINE IAW J771-00-01. LEAK AND OPS CHECKS GOOD. ENGINE LAST SHOP VISIT, 10875 HOURS AND 2468 CYCLES. 2L73 4F4 F A3WE E2EA 19951222002291995122200229 1995 12 22 95ZZZM737 419951111A2350B692229 STATION BOX BAG JETSTMJETSTM3101 1500215EU LT COCKPIT DEFECTIVE A VNAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 GL07834JS 726 FLT NR 4072 - CREW ELECTED TO RETURN TO FIELD AFTER EXPERIENCING VHF COMM AND INTERCOMM PROBLEMS. MAINTENANCE REPLACED CAPTIANS STATION BOX IAW MM 23-00-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222002301995122200230NE 1995 12 22 95ZZZM739 219951121A7261 OIL SYSTEM DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE RT ENGINE REQ'D SERVICE A VNAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL07424JS 3033 FLT NR 4010 - EN ROUTE FROM PHL TO CVG, CREW NOTICE A FLUCTUATION OF OIL PRESSURE RIGHT ENGINE. OIL PRESSURE WAS FLUCTUATING BETWEEN THE YELLOW AND GREEN ARC'S. CREW ELECTED TO DIVERT TO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE SERVICED THE RIGHT ENGINE WITH FOUR QUARTS OF EXXON 2380 TURBINE OIL. ENGINE GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 19951222002311995122200231EU 1995 12 22 95ZZZM740 119951114A2750 SWITCH BAG JETSTMJETSTM3101 1500215EU TE FLAPS OUT OF ADJUST A VNAAO OTHER J WARNING INDICATION APAPPROACH 1 GL07841JS 751 FLT NR 4134 - FLAP POSITION WARNING SOUNDED WHEN CREW WAS PREPARING FOR LANDING, ATTEMPTS TO POSITION FLAPS FOR LANDING WERE UNSUCCESSFUL. CREW PREPARED FOR NO FLAPS LANDING AND DECLARED AN EMERGENCY CRASH TRUCKS DISPATCHED. AIRCRAFT LANDED WITHOUT INCIDENT. DAY MAINTENANCE RIGGED FLAP POSITION MICRO-SWITCH IAW MM 27-50-00. GROUND CHECK GOOD, AIRCRAFT RELEASED FOR SERVICE. 2L72 4T RTA21EU 19951222002321995122200232NM 1995 12 22 95ZZZM741 119951113A5610601A561A0000200 WINDSHIELD DORNERDO32 DO328100 2996000NM LT COCKPIT FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07429JS 229 3043 FLT NR 4159 - CAPTAINS WINDSCREEN FRACTURED DURING CLIMB-OUT AT 15,000 AGL. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CAPTAINS WINDSCREEN IAW MM 56-10-00. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 19951222002331995122200233NE 1995 12 22 95ZZZM742 219951114A7200 ENGINE DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LEFT OVERTORQUED A aVNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07425JS 3037 FLT NR 4168 - CREW EXPERIENCED AN OVER TORQUE OF 126 PERCENT LEFT ENGINE DURING CLIMB-OUT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CONDUCTED AN OVER TORQUE INSPECTION IAW MM 05-00-00. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA45NM E20NE 19951222002341995122200234WP 1995 12 22 95ZZZM743 119951107A33506100928 EEL LAMP DOUG DC9 DC915 3022036WP CABIN MISSING A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111064T 45778 WHILE PERFORMING AN A-1 INSPECTION ON AIRCRAFT, MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT MISSING THE LENS AND LAMP AT ROW 4. MAINTENANCE REPLACED THE LENS AND LAMP. THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. REF NR GRAA9548. 2L72 4F A6WE 19951222002351995122200235WP 1995 12 22 95ZZZM744 119951107A33506100928 EEL LAMP DOUG DC9 DC915 3022036WP CABIN MISSING A GRAAK NONE O OTHER ININSP/MAINT 1 WP111064T 45778 WHILE PERFORMING AN A-1 INSPECTION ON AIRCRAFT, MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT MISSING THE LENS AND LAMP AT ROW 10. MAINTENANCE REPLACED THE LENS AND LAMP. THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. REF NR GRAA9549. 2L72 4F A6WE 19951222002361995122200236WP 1995 12 22 95ZZZM745 119951104A33506100928 EEL LAMP DOUG DC9 DC987 3022087WP CABIN FAILED A GRAAK NONE O OTHER ININSP/MAINT 1 WP111075T 49724 MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (REF NR GRAA9554) 2L72 4F RTA6WE 19951222002371995122200237NE 1995 12 22 95ZZZM746 219951102A7200 ENGINE AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE LEFT FAILED A NVEAAE UNSCHED LANDING ENGINE SHUTDOWN BEXSMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET ENGINE FLAMEOUT CRCRUISE 1 SO03282AT 282 121116 BGM - FLT NR 4863 - ELECTRICAL SMOKE WARNING EN ROUTE TO SYR, SMOKE ON THE FLIGHT DECK. CREW FOLLOWED EMERGENCY CHECKLIST. DURING EMERGENCY DESCENT, LEFT ENGINE FAILED. CREW ISOLATED LEFT ENGINE. FLIGHT SAFELY DIVERTED TO BGM. SMOKE WAS FROM LEFT ENGINE BLEED, PRIOR TO ENGINE FAILURE. REPLACED LEFT ENGINE. (M) 2H72 4T4 TRTA53EU E20NE 19951222002381995122200238WP 1995 12 22 95ZZZM747 119951112A3234H50002125218 BYPASS HANDLE DOUG DC9 DC983 3022083WP LANDING GEAR MALFUNCTIONED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE059307R 49663 STL - AFTER TAKEOFF WHEN LANDING GEAR SELECTOR WAS RAISED, LANDING GEAR DID NOT RETRACT. FOUND LANDING GEAR MAINTENANCE BYPASS HANDLE LATCH MALFUNCTION, MFG P/N H5000-2-125-218. REPAIRED LOCK AND LANDING GEAR BYPASS HANDLE OPERATION CHECKED NORMAL. 2L72 4F RTA6WE 19951222002391995122200239WP 1995 12 22 95ZZZM748 119951111A3260 SENSOR DOUG DC9 DC983 3022083WP RT MLG DIRTY A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE059307R 49663 STL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MAIN LANDING DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. VISUALLY CHECKED RIGHT MAIN LANDING GEAR, IT WAS DOWN AND LOCKED. FOUND DEBRIS ON RIGHT MAIN LANDING GEAR INDICATION SENSOR. REMOVED DEBRIS FROM SENSOR AND LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL. 2L72 4F RTA6WE 19951222002401995122200240NE 1995 12 22 95ZZZM749 219951110A7250 TURBINE BLADES BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 1 ENG DAMAGED A TWAAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 CE0593104 19670 HNL - DURING CLIMB, SHUT DOWN NR 1 ENGINE, S/N 4165, DUE TO COMPRESSOR STALL AND RISING EGT. FOUND METAL PARTICLES IN TAILPIPE AND TURBINE BLADE DAMAGE. REPLACED ENGINE AND ENGINE OPERATION CHECKED NORMAL. 2L74 4F4 F A20WE E20EA 19951222002411995122200241WP 1995 12 22 95ZZZM750 119951111A3297 WIRE DOUG DC9 DC932 3022066WP GEAR INDICATION BROKEN A TWAAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 CE05924L 47324 SHV - DURING LANDING, WHEN GEAR HANDLE WAS EXTENDED, RIGHT GEAR RED AND GREEN LIGHTS DID NOT ILLUMINATE. A FLY-BY WAS PERFORMED TO ENSURE GEAR WAS DOWN AND LOCKED. REPLACED BROKEN WIRE, REFERENCE WIRING DIAGRAM 32-61-00. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951222002421995122200242NE 1995 12 22 95ZZZM751 219951111A7260783310 BUSHING DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENG GEARBOXFAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE05911TW 49182 3210 ICT - DURING CRUISE, NR 1 ENGINE, S/N 3210, SPOOLED DOWN. SHUT DOWN ENGINE. FOUND INTERNAL MALFUNCTION IN N-2 ACCESSORY GEARBOX, MFG P/N 758300. CHANGED ENGINE AND ENGINE OPERATION CHECKED NORMAL. INVESTIGATION OF SPOOL DOWN OF NR 1 ENGINE, REVEALED A BUSHING, P/N 783310, ALLOWED THE INPUT GEAR TO SHIFT CAUSING RAPID TOOTH WEAR, RESULTING IN GEARBOX FAILURE. GEARBOX REPAIRED AND RETURNED TO SERVICE. (M) 2L72 4F4 F A6WE E9NE 19951222002431995122200243NM 1995 12 22 95ZZZM752 119951118A3230 PIVOT PIN BOEING747 747131 1384881NM RT MLG LACK OF LUBE A TWAAA UNSCHED LANDING O OTHER CLCLIMB 1 CE0593107 19673 HNL - AFTER TAKEOFF RIGHT WING LANDING GEAR WOULD NOT TILT FULL FORWARD. LUBED RIGHT WING LANDING GEAR TRUCK PIVOT PIN. JACKED AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF LANDING GEAR TILT SYSTEM. OPERATIONAL CHECK NORMAL. 2L74 4F A20WE 19951222002441995122200244NM 1995 12 22 95ZZZM753 119951120A2520 INSUL BLANKET BOEING727 727231 1384079NM CABIN OUT OF POSITION A aTWAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE0554342 21629 DURING CLIMB, LOST CABIN PRESSURE AT 17,000 FEET, FLIGHT RETURNED. FOUND INSULATION BLANKET UNDER LEFT OUTFLOW VALVE. REMOVED INSULATION BLANKET AND REMOVED AND REPLACED LEFT OUTFLOW VALVE, MFG P/N 103280-5-1. ALSO, REMOVED AND REPLACED RIGHT OUTFLOW VALVE, MFG P/N 103280-5-1, AUTOMATIC CABIN PRESSURE CONTROL, MFG P/N 102518-3-1 AND MANUAL PRESSURE CONTROLLER, MFG P/N 131046-1. PERFORMED CABIN PRESSURE LEAK CHECK, CHECKED NORMAL. 2L73 4F A3WE 19951222002451995122200245NM 1995 12 22 95ZZZM754 119951119A3350 EEL BOEING727 727231 1384079NM CABIN INOPERATIVE A TWAAK NONE L NO TEST ININSP/MAINT 1 CE0512308 19565 STL - DURING LANDING, EGRESS PATH LIGHTING AT R-2 DOOR CAME OUT OF TRACK. REINSTALLED LIGHT STRIP, CHECKED WIRING, AND LIGHT OPERATION CHECKED NORMAL. 2L73 4F A3WE 19951222002461995122200246NM 1995 12 22 95ZZZM755 119951118A323065B015397 ACTUATOR BOEING747 747131 1384881NM RT MLG FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE0593107 19823 HNL - AFTER TAKEOFF, RIGHT WING LANDING GEAR TRUCK TILT LIGHT ILLUMINATED ON BOTH PRIMARY AND ALTERNATE. REPLACED RIGHT WING GEAR TRUCK TILT ACTUATOR, MFG P/N 65B015397, AND CHECKED LANDING GEAR TRUCK TILT INDICATION. LANDING GEAR INDICATION SYSTEMS CHECKED NORMAL. 2L74 4F A20WE 19951222002471995122200247EU 1995 12 22 95ZZZM756 119951114A2730S2738196320000 FLANGE AEROSPATR72 ATR72201 EU ELEV TQ TUBE CRACKED ASTTRBAK NONE O OTHER ININSP/MAINT 1 SO212FOR 12527 147 ELEV TQ TUBE FLANGE FOUND CRACKED DURING INSPECTION AFTER PILOT REPORT. PART REPLACED WITH NEW ASSEMBLY. OPS CHECK GOOD. 2H72 4T RTA53EU 19951222002481995122200248EU 1995 12 22 95ZZZM757 119951029A261172111211000 SMOKE DET SAAB SF340 SF340A 7850100EU CARGO BAY FAILED A PLGAF ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 NE05344BE A347 340A104 FLT 4719 - ON APPROACH, CREW RECEIVED 2 INTERMIT CARGO SMOKE DETECT LIGHT WARN. APPROX 500 FEET, CARGO WARN LIGHT REMAINED ILLUMINATED. THE CARGO FIRE EXTINGUISHER SWITCH SELECTED. AFTER ACTUATING THE SWITCH, THE SMOKE DETECT WARNING LIGHT REMAINED ILLUMINATED AND THE CARGO FIRE EXTINGUISHER DISCHARGE LIGHT FAILED TO ILLUMINATE. AN EMERG DECLARED, THE A/C LANDED IN LGA W/O INCIDENT. LGA MX INSPECTED THE A/C AND REPAIR. PSM MX REPLACED ON FAULTY DETECT WHICH CAUSED THE WARN LIGHT TO ILLUMINATE. ELECT SQUIBB WAS REMOVED AND FOUND TO HAVE TIP OF CARTRIDGE MISSING, THE CARTRIDGE HAD NOT FIRED AND THE SEAL ON THE FIRE EXTINGUISHER HAD NOT BEEN PENETRATED. MX REPLACED CARTRIDGE AND RETURNED A/C TO SERVICE.(M)2L72 4T RTA52EU 19951222002491995122200249WP 1995 12 22 95ZZZM758 119951119A5310 STRUCTURE DOUG DC9 DC932 3022066WP TAIL SKID AREA DAMAGED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11918VV 47320 UPON ARRIVAL OF FLT 306, MIA-IAD, MX FOUND THE TAIL SKID AND SURROUNDING STRUCTURE DAMAGED APPARENTLY FROM GROUND CONTACT. INSPECTED AND FERRIED AIRCRAFT TO LACI, ID 7A1 FOR STRUCTURE REPAIR. PERFORMED NECESSARY REPAIRS TO STRUCTURE AND SKID IAW SRM 53-01, 53-04, 51-60, 51-30. 2L72 4F A6WE 19951222002501995122200250NM 1995 12 22 AWXA9500791 119951129A5320BAC1518338 THRESHOLD BOEING757 7572S7 1384962NM BS 1661 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - DURING SCHEDULED C4 INSPECTION, FOUND CORROSION ON FLOOR BEAM AT STATION 1661 LBL 45 TO L4 DOOR THRESHOLD. INSTALLED REPLACEMENT T-CAP AND REPAIR PARTS PER SRM 53-00-51, FIGURE 203. (M) 2L72 4F RTA2NM 19951222002511995122200251NM 1995 12 22 AWXA9500792 119951129A5347 SEAT TRACK BOEING757 7572S7 1384962NM BS 1640 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - DURING SCHEDULED C4 INSPECTION, FOUND SEAT TRACK CORRODED AT STATION 1640 LBL 45. FABRICATED AND INSTALLED SEAT TRACK IAW SRM 51-10-00 AND SRM 51-40-02. (M) 2L72 4F RTA2NM 19951222002521995122200252NM 1995 12 22 AWXA9500793 119951129A53212024T3080 FLOOR BOEING757 7572S7 1384962NM BS 1691 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - DURING SCHEDULED C4 INSPECTION, FOUND FLOOR PAN AT BS 1691 TO BS 1710 LBL 55 CORRODED. INSTALLED REPAIR IAW ER 5-53-16-11. (M) 2L72 4F RTA2NM 19951222002531995122200253NM 1995 12 22 AWXA9500794 119951129A5321 FLOOR BOEING757 7572S7 1384962NM FS 1681-1740 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28901AW 23321 PHX - DURING SCHEDULED C4 INSPECTION, FOUND AFT GALLEY FLOOR PAN CORRODED IN NUMEROUS AREAS FROM STATION 1681.8 THROUGH STATION 1740, RBL 2 THROUGH LBL 55. REPAIRED PER ER 5-53-16-11. (M) 2L72 4F RTA2NM 19951222002541995122200254 1995 12 22 EIAA9558 419951113A3454 RMI CONNECTOR DOUG DC9 DC932F 3022067WP LT COCKPIT DIRTY A EIAAO OTHER N FALSE WARNING NRNOT REPORTED 1 NM09932F 47355 SEA - HEADING COMPASS LIGHT CAME ON DURING TURN ON DEPARTURE. 30 DEGREES DIFFERENCE IN COMPASS HEADING. 30 DEGREES DIFFERENCE IN VOR NEEDLES ON BOTH RMI'S. CAPTAIN'S RMI COMPASS HEADING WITHIN 10 DEGREES OF STANDBY MAGNATIC COMPASS. CHECKED SECURITY OF COMPASS COMPONENTS, CLEANED CONNECTION AND RESECURED. CAPTAINS RMI WAS WITHIN 2 DEGREES OF STANDBY COMPASS. COULD NOT DUPLICATE ANY PROBLEM WITH VOR TESTER. ALL SYSTEMS CHECKED GOOD. (M) 2L72 4F A6WE 19951222002551995122200255WP 1995 12 22 EIAA9559 119951116A33501001191 EEL DOUG DC9 DC932F 3022067WP CABIN MALFUNCTIONED A EIAAK NONE L NO TEST ININSP/MAINT 1 NM09935F 47220 DEN - EMERGENCY EXIT LIGHT LOCATED AT MAIN ENTRANCE SWITCH IS BROKEN, STAYS ON ALL THE TIME. REPLACED LIGHT ASSY, EMERGENCY EXIT PANEL, SYSTEM OPS. CHECK GOOD IAW MM 33-50-00. (M) 2L72 4F A6WE 19951222002561995122200256NE 1995 12 22 EIAA9560 219951120A7200 ENGINE BOEING747 747212B 1384886NM PWA JT9 JT9D7J 52054NE NR 1 OVERTEMP A aEIAAO OTHER JM WARNING INDICATION OVER TEMP LDLANDING 1 NM09482EV68059 20713 662971 CYQX - OVERTEMP NR 1 ENGINE, APPROX 1150 CELSIUS FOR 5 TO 10 SECONDS, SHUTDOWN ENGINE DURING LANDING. ACCOMPLISHED OVERTEMP INSPECTION PER B747 MM 72-00-00 PAGE 601, BORESCOPED HPT, LPT, COMBUSTION CHAMBER, NGV NO DEFECTS NOTED, VISUALLY INSPECTED ENGINE EXTERNALLY, INTAKE AND EXHAUST, NO DEFECTS NOTED. PERFORMED FULL POWER RUN. ALL PARAMETERS WITHIN LIMITS. (M) 2L74 4F4 F A20WE E20EA 19951222002571995122200257NM 1995 12 22 EIAA9561 119951118A3230 PRESS RELIEF BOEING747 747121 1384871NM CARGO DOOR OPEN A EIAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 NM09474EV 19637 EHAM - AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. AFTER SECOND PACK WAS TURNED ON, UNABLE TO PRESSURIZE. DOOR ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT AND DEPRESSURIZATION PROCEDURES CHECK COMPLETED, FUEL JETTISONED AND RETURNED TO EHAM. FOUND AFT CARGO DOOR PRESSURE RELIEF DOORS OPEN, CLOSED RELIEF DOORS. GROUND PRESSURE CHECK OK. (M) 2L74 4F A20WE 19951222002581995122200258NM 1995 12 22 EIAA9563 119951124A2612 FIRE CARDS BOEING747 747132 1384882NM FIRE WARNING DIRTY A EIAAO OTHER N FALSE WARNING DEDESCENT 1 NM09481EV 19896 JFK - DURING DESCENT BOTH MASTER FIRE WARNING LIGHTS ILLUMINATED FOR ONE SECOND THEN WENT OUT. ALL FIRE WARNING SYSTEMS THEN TESTED OK. CLEANED AND RESEATED ALL FIRE WARNING CARDS, OPS CHECK OK PER MM 26-11-00. (M) 2L74 4F A20WE 19951222002591995122200259NM 1995 12 22 EISA95424 119951118A5730 PANEL BOEING727 727221 1384071NM LT WING CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 RT WING PANEL AT NR 7 SLAT ACTUATOR HAS EXFOLIATING CORROSION. REMOVED RIGHT WING PANEL, NR 7 SLAT FROM AIRCRAFT FABRICATED NEW HORSESHOE BRACKET AND FACE PANEL. TREATED, PRIMED AND INSTALLED NEW PANEL AND HORSESHOE BRACKET PER SRM 51-10-4. (M) 2L73 4F A3WE 19951222002601995122200260NM 1995 12 22 EISA95425 119951118A5330 SKIN BOEING727 727221 1384071NM BS 580 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 REPAIR BENT DAMAGED STATION 580 TOP OF FWD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER IAW 51-10-1. TREATED PRIMED AND INSTALLED DOUBLER PER SRM 51-10-1. (M) 2L73 4F A3WE 19951222002611995122200261NM 1995 12 22 EISA95426 119951118A5320 DOUBLER BOEING727 727221 1384071NM BS 600 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 REPAIR DAMAGED ELONGATED HOLE, STATION 600, TOP OF FORWARD CARGO DOOR CUT OUT. REMOVED DAMAGED DOUBLER IAW SRM 51-10-1, FABRICATED NEW DOUBLER 51-10-1, TREATED AND PRIMED AND INSTALLED DOUBLER PER 51-10-1 AND 51-30-1. (M) 2L73 4F A3WE 19951222002621995122200262NM 1995 12 22 EISA95427 119951118A5320 TIE CLIP BOEING727 727221 1384071NM BS 1183 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 DITCHING PAN TIE CLIP CRACKED AT STATION 1183, BL 27L. FABRICATED NEW TIE CLIP PER SRM 51-30-2. INSTALLED NEW TIE CLIP PER SRM 51-30-2. (M) 2L73 4F A3WE 19951222002631995122200263NM 1995 12 22 EISA95428 119951118A5320 TIE CLIP BOEING727 727221 1384071NM BS 1183 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 DITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 37. REMOVED CLIP, FABRICATED NEW CLIP PER SRM 51-30-2, INSTALLED CLIP PER SRM 51-10-1. (M) 2L73 4F A3WE 19951222002641995122200264NM 1995 12 22 EISA95429 119951118A5320 TIE CLIP BOEING727 727221 1384071NM BS 1183 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 DITCHING PAN TIE CLIP CRACKED STATION 1183, RBL 47. FABRICATED NEW TIE CLIP AND INSTALLED PER SRM 51-40. (M) 2L73 4F A3WE 19951222002651995122200265NM 1995 12 22 EISA95433 119951118A5532 SKIN BOEING727 727221 1384071NM VERT STAB CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 VERTICAL STABILIZER RIGHT SIDE, JUST BELOW NR 7 VORTEX GENERATOR FROM TOP, SKIN CRACKED AT RIVET HEAD. STOP DRILLED CRACK PER SRM 55-30-3. HFEC CONFIRMED CRACK CONTAINED BY STOP HOLE. EXTERNAL DOUBLER INSTALLED AND SEALED PER SRM 55-30-3. (M) 2L73 4F A3WE 19951222002661995122200266NM 1995 12 22 EISA95434 119951118A5320 CHANNEL BOEING727 727221 1384071NM BS 303-320 CRACK A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 CORROSION AT HAT CHANNEL UNDER RIGHT LAV DOOR WAY, APPROXIMATELY STATION 303-320. CORRODED HAT CHANNEL, FABRICATED NEW SECTION, INSTALLED PER SRM 51-30-2. (M) 2L73 4F A3WE 19951222002671995122200267NM 1995 12 22 EISA95435 119951118A5320 TIE CLIP BOEING727 727221 1384071NM BS 1183 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 DITCHING PAN CLIP CRACKED, STATION 1183, BL 37 LEFT. REMOVED TIE CLIP AND FABRICATED PER SRM 51-30-2. TREATED, PRIMED AND INSTALLED PER SRM 51-10-2 AND 51-10-5. (M) 2L73 4F A3WE 19951222002681995122200268NM 1995 12 22 EISA95436 119951118A5531 RIB BOEING727 727221 1384071NM VERT STAB CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 INSIDE VERTICAL STAB THROUGH ACCESS PANEL 9504, FOURTH COMPARTMENT UP FROM ENTRANCE, THE EIGHTH RIB FROM THE TOP IS CRACKED. REPAIRED CRACK IN RIB PER SRM 55-30-4. (M) 2L73 4F A3WE 19951222002691995122200269NM 1995 12 22 EISA95437 119951118A5313 STRINGER BOEING727 727221 1384071NM BS 990 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 STATION 990, STRINGER 29R HAS CORROSION ON OUTBOARD FLANGE. REMOVED CORROSION AND FOUND 2 INCH CRACK. STOP DRILLED CRACK PER SRM 51-10-1. HFEC CONFIRMS CRACK CONTAINED, FABRICATED REPAIR PARTS AND INSTALLED PER CA22026-5068. (M) 2L73 4F A3WE 19951222002701995122200270NM 1995 12 22 EISA95438 119951116A5712 RIB BOEING727 727221 1384071NM BS 760 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 CRACK INDICATION, FORWARD 2 FASTENER HOLES, BS 760 LBL 70.5 RIB CHORD VERTICAL FLANGE. REMOVED ANGLE AND SUPPORT. REMOVED FASTENERS FOR NDT, ACCOMPLISHED HFEC TO FASTENER HOLES. NO OTHER CRACKS NOTED. FABRICATED REPAIR ANGLE REF BAC DRAWING 65-68492, COMPLETED INSTALLATION PER BAC DRAWING 65-68492. (M) 2L73 4F A3WE 19951222002711995122200271NM 1995 12 22 EISA95439 119951116A5712 LE RIB BOEING727 727221 1384071NM LT WING CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 CORROSION AT RIB AND STIFFENER INSIDE LEFT WING LE AFT OF NR 2 LE FLAP AND 14 INCHES OUTBOARD OF ACTUATOR. FABRICATED REPAIR PARTS PER SRM 51-40-4. INSTALLED PER SRM 51-40-4. (M) 2L73 4F A3WE 19951222002721995122200272NM 1995 12 22 EISA95440 119951124A5320 WEB BOEING727 727251 138408HNM BS 340-360 TORN A EISAK NONE O OTHER ININSP/MAINT 1 SW07263US 19982 SHEAR WEB, AT STATION 340-360 LT, TORN AT STRINGER 7. FABRICATED SHEAR WEB IAW SRM 51-30-10, INSTALLED PER SRM 51-10-00. (M) 2L73 4F A3WE 19951222002731995122200273NM 1995 12 22 EISA95442 119951124A5311 FRAME BOEING727 727251 138408HNM BS 360 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07263US 19982 AT STATION 360 LT, AT STRINGER 7, CRACK EXISTS AT CIRCUMFERENCE. FABRICATED REPAIR PARTS PER 8110-3, INSTALLED PER SRM 51-10-00. (M) 2L73 4F A3WE 19951222002741995122200274NM 1995 12 22 F3LA95016 119951116A33506104781 BATTERY PACK BOEING737 737201 1384454NM CABIN DISCHARGED A F3LAK NONE L NO TEST ININSP/MAINT 1 NM03214AU 20214 FAR - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND SYSTEM CHECKED OK. (M) 2L72 4F A16WE 19951222002751995122200275NM 1995 12 22 F3LA95017 119951121A3260 TARGET BOEING737 737300 1384610NM RT MLG OUT OF ADJUST A F3LAO OTHER N FALSE WARNING APAPPROACH 1 NM032FOR FLT NR 441 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. MAINTENANCE ADJUSTED TARGET ON THE PROXIMITY SWITCH AND SYSTEM CHECKED OK. (M) 2L72 4F RTA16WE 19951222002761995122200276NM 1995 12 22 F3LA95018 119951128A21701808494 COALESOR BOEING737 737201 1384454NM LEFT DIRTY A F3LAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 NM03214AU 20214 SLC - AIR TURN BACK. UPON TAKEOFF, FLIGHT CREW REPORTED AN ODOR IN THE COCKPIT AFTER TURNING ON LEFT PACK. THE SMOKE DETECTOR IN THE FORWARD LAVATORY ACTIVATED AND THE AIRCRAFT WAS RETURNED TO SLT. MAINTENANCE INSPECTED THE AIRCRAFT INTERIOR AND THE AIR CONDITIONING BAY AREA AND CHECKED OK. PLACARDED LEFT PACK INOPERATIVE PER MEL 21-1 AND 21-2. UPON ARRIVAL IN DEN, MAINTENANCE REPLACED THE LEFT WATER SEPARATOR BAG AND SYSTEM CHECKED OK. (M) 2L72 4F A16WE 19951222002771995122200277WP 1995 12 22 GRAA9547 119951029A27817951209501 SWITCH DOUG DC9 DC987 3022087WP FLAP/SLAT DIRTY A GRAAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP111074T 49727 AIRCRAFT HAD A SLAT DISAGREEMENT LIGHT ILLUMINATE AT CRUISE WITH AN OVERSPEED WARNING. AIRCRAFT DIVERTED INTO RENO NEVADA WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE FLAP/SLAT SWITCH. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951222002781995122200278WP 1995 12 22 GRAA9548 119951107A3350079123 EEL LENS DOUG DC9 DC915 3022036WP CABIN MISSING A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111064T 45778 WHILE PERFORMING AN A-1 INSPECTION ON AIRCRAFT, MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT MISSING THE LENS AND LAMP AT ROW 4. MAINTENANCE REPLACED THE LENS AND LAMP. THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM OPERATIONAL CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951222002791995122200279WP 1995 12 22 GRAA9549 119951107A3350079123 EEL LENS DOUG DC9 DC915 3022036WP CABIN MISSING A GRAAK NONE O OTHER ININSP/MAINT 1 WP111064T 45778 WHILE PERFORMING AN A-1 INSPECTION ON AIRCRAFT, MAINTENANCE DISCOVERED THE EMERGENCY FLOOR TRACK LIGHT MISSING THE LENS AND LAMP AT ROW 10. MAINTENANCE REPLACED THE LENS AND LAMP. THE EMERGENCY FLOOR TRACK LIGHTING SYSTEM OPERATIONALLY CHECKED NORMAL, NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A6WE 19951222002801995122200280WP 1995 12 22 GRAA9552 119951025A335060030451 BATTERY PACK DOUG DC9 DC987 3022087WP CABIN DISCHARGED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111075T 49724 AT IFP, FORWARD EMERGENCY CABIN LIGHTS WERE DISCOVERED TO BE INOPERATIVE. MAINTENANCE DISCOVERED THAT THE FORWARD EMERGENCY BATTERY PACK HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY PACK. THE SYSTEM WAS OPERATIONALLY CHECKED, AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951222002811995122200281WP 1995 12 22 GRAA9553 119951104A335060030431 BATTERY PACK DOUG DC9 DC987 3022087WP CABIN DISCHARGED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111075T 49724 AT IFP, FORWARD EMERGENCY CABIN OVERHEAD LIGHTS ILLUMINATE WHEN ELECTRICAL POWER IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN OVERHEAD EMERGENCY LIGHTS BATTERY PACK. OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951222002821995122200282WP 1995 12 22 GRAA9554 119951104A3350079123 EEL LENS DOUG DC9 DC987 3022087WP CABIN MISSING A GRAAK NONE O OTHER ININSP/MAINT 1 WP111075T 49724 MAINTENANCE AT IFP, CLEARED A DMI THAT PERTAINED TO THE FORWARD EMERGENCY TRACK LIGHTING. MAINTENANCE REPLACED THE FLOOR TRACK LAMP PIGTAIL, AND LENS. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F RTA6WE 19951222002831995122200283WP 1995 12 22 HALA9515 119951116A5311 FRAME DOUG DC9 DC951 3022051WP BS 1326 CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 HNL - IN C-CHECK, FOUND CANTED STATION 1326 FRAME RIGHT SIDE BOTTOM END SEVERELY CORRODED, REPAIRED PER SRM 53-01. CUT OUT LOWER RHS END OF FRAME AND REMOVED DAMAGE. FABRICATED REPAIR FILLER (.050, 7075-T6 CLAD). FABRICATED REPAIR SPLICE DOUBLER (.063, 7075-T6). INSTALLED REPAIR SPLICE DOUBLER USING HL 328-5 HI-LOCKS IN ADDED HOLES. (M) 2L72 4F A6WE 19951222002841995122200284WP 1995 12 22 HALA95152 119951116A5320 DOUBLER DOUG DC9 DC951 3022051WP LT MLG CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 HNL - IN C-CHECK, FOUND LEFT WING LOWER MAIN LANDING GEAR DOUBLER HAS MODERATE CORROSION, REPAIRED PER SRM 57-03. CUT OUT BLENDED EDGE ON MLG DOUBLER. FABRICATED REPAIR FILLER (.125, 2024-T3). INSTALLED FILLER USING SAME SIZE AND TYPE AS THOSE REMOVED. (M) 2L72 4F A6WE 19951222002851995122200285WP 1995 12 22 HALA95153 119951114A2612 FIRE LOOP WIRE DOUG DC9 DC951 3022051WP NR 2 ENGINE BROKEN A HALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP13674MC 47735 HNL - FLT NR 8030 - FIRE DETECTION LOOP LIGHT CAME ON WITH CLIMB POWER ON RIGHT ENGINE. DID NOT GET FULL FIRE WARNING, JUST DETECTION LOOP LIGHT. REPAIRED WIRE AT APRON LOOP. OPERATIONAL CHECK OK. (M) 2L72 4F A6WE 19951222002861995122200286WP 1995 12 22 HALA95155 119951116A5330 SKIN DOUG DC9 DC951 3022051WP BS 927 CORRODED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 HNL - IN C-CHECK DURING FUSELAGE MAPPING, FOUND EXFOLIATION ON FUSELAGE SKIN AT STATION 927, 1.5 INCH ABOVE LEFT LONGERON 26L. REPAIRED PER SRM 53-01. REMOVED DAMAGED SECTION. FABRICATED REPAIR FILLER (7075-T6 CLAD). FABRICATED INTERNAL REPAIR FILLER DOUBLER (0.032 INCH, TI-6AL-4V). INSTALLED REPAIR DOUBLER USING MS20470AD5 AND NAS1097AD5/6 RIVETS IN EXISTING AND ADDED HOLES. (M) 2L72 4F A6WE 19951222002871995122200287WP 1995 12 22 HALA95157 119951120A3350 BATTERY DOUG DC9 DC951 3022051WP TAIL COMPT DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP132FOR 47742 HNL - IN C-CHECK, TAIL COMPARTMENT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES IN POWER SUPPLY B5-28. OPERATIONAL CHECK OK. (M) 2L72 4F A6WE 19951222002881995122200288NM 1995 12 22 HNAA9591715 119951120A3230104451 SPRING DHAV DHC8 DHC8102 2809003NM STAY STRUT ACT BROKEN A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07917HA23242 075 FLT NR 3162 - DCA-ISP - AFTER GEAR DOWN SELECTION, DURING APPROACH, THE LEFT GEAR UNSAFE LIGHT ILLUMINATED AND STAYED ON. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN ISP WITHOUT INCIDENT. REMOVED AND REPLACED THE STAY STRUT OUTBOARD SPRING. (M) 2H72 4T RTA13NM 19951222002891995122200289NE 1995 12 22 HNAA9593016 219951125A7200 ENGINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 FAILED A aHNAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA07930HA1752711419 126 120559 FLT NR 3249 - HPN-BWI - DURING FLIGHT, NR 2 ENGINE TORQUE BEGAN TO FLUCTUATE AND WAS FOLLOWED BY A LOUD BANG. THE CREW SHUT THE ENGINE DOWN IN FLIGHT AND LANDED IN BWI WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 ENGINE. (M) 2H72 4T4 TRTA13NM E20NE 19951222002901995122200290NM 1995 12 22 HNAA9594218 119951128A5280 GEAR DOOR DHAV DHC8 DHC8102 2809003NM RT MLG CRACKED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07942HA 163 FLT NR 3079 - MIA-JAX - ON APPROACH INTO TPA, THE RIGHT GEAR AFT DOORS WAS BINDING AND WILL NOT MANUALLY EXTEND. THE AIRCRAFT LANDED IN TPA WITHOUT INCIDENT. FOUND TO BE CRACKED IN TWO LOCATIONS. REPAIRED IAW RD8-54-068. (M) 2H72 4T RTA13NM 19951222002911995122200291NM 1995 12 22 IXKA9500031 119951219A79311163P182 LOW OIL PRESS SW BOEING727 727225 1384077NM NR 3 ENG FAILED A IXKAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA25356PA 20626 ATL - FLT 53 - NR 3 ENGINE LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON AND WOULD NOT GO OUT WITH IDLE POWER. ALL OTHER INDICATIONS NORMAL. ENGINE WAS SHUT DOWN. REMOVED AND REPLACED NR 3 ENGINE LOW OIL PRESSURE BYPASS SW AS PER MM 79-31-1. REMOVED AND REPLACED MOS FOUND LOOSE GROUND WIRE ON NR 3 ENGINE LOW PRESSURE LIGHT SOCKET ON FORWARD COCKPIT PANEL, RETIGHTENED. ENGINE RAN UP AND LEAK CHECK OK. (M) 2L73 4F A3WE 19951222002921995122200292NM 1995 12 22 IXKA9500032 119951124A5220 DOOR BOEING727 727225 1384077NM L2 NOT LATCHED A IXKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA258880Z 21453 EWR-ATL - FLT NR 9059 - UNABLE TO PRESSURIZE, AIR TURN BACK TO EWR. FOUND L2 DOOR COCKED, LIGHTS OPS CHECKED GOOD, RESET DOOR, PRESSURIZED OK. (M) 2L73 4F A3WE 19951222002931995122200293WP 1995 12 22 IXXA9597 119951120A3350 EEL WIRE DOUG DC8 DC862 3021970WP CABIN FAILED A IXXAK NONE L NO TEST ININSP/MAINT 1 GL2361CX 1364 46142 MAINTENANCE FOUND THE FOUR FORWARD FLOOR EMERGENCY TRACK LIGHTS TO BE INOPERATIVE. THE POWER SUPPLY PROVIDING POWER TO THESE LIGHTS WAS BLOWING PICOFUSES FOR THAT SET OF LIGHTS. TROUBLESHOOTING INDENTIFIED A SHORT IN THE POWER WIRE BETWEEN THE POWER SUPPLY AND THE LIGHT SET. THE SHORTED WIRE WAS REPAIRED, RETURNING THE SYSTEM TO NORMAL OPERATION. 2L74 4F 4A25 19951222002941995122200294WP 1995 12 22 NOCA0995 119951124A33507732 EEL LAMP DOUG DC9 DC983 3022083WP CABIN FAILED A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15183NA 49808 EMERGENCY EGRESS LIGHT INOP BY ROWS 29DEF AND 14DEF. REPLACED LAMPS, CHECKED OK. (M) 2L72 4F RTA6WE 19951222002951995122200295WP 1995 12 22 ORJA95106 119951025A5320 JAMB DOUG DC9 DC983 3022083WP AFT CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CORROSION ON AFT DOOR JAMB OUTBOARD OF DOOR LATCH FITTING AFT CARGO DOOR CUTOUT. REMOVED CORROSION MIN MATERIAL REMOVED. ALODINED AND PRIMED, REF SRM 51-10-3 AND 53-05. (M) 2L72 4F RTA6WE 19951222002961995122200296WP 1995 12 22 ORJA95107 119951025A5320 JAMB DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 HEAVY CORROSION AND PITTING ON LOWER DOOR JAMB, INNER FRAME FROM FORWARD TO AFT CORNERS OF AFT PIT DOOR CUTOUT. BLEND AND CHECK LIMITS. REPAIRED CORRODED AND PITTED LOWER DOOR JAMB, INNER FRAME, IAW SRM 53-05 FIG 63. INSTALLED THRESHOLD AND SCUFF PLATE, IAW SRM 51-30-1. (M) 2L72 4F RTA6WE 19951222002971995122200297WP 1995 12 22 ORJA95108 119951025A5320 JAMB DOUG DC9 DC983 3022083WP FWD CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 HEAVY CORROSION ON INNER LOWER DOOR JAMB FRAME FROM FWD TO AFT CORNER FWD CARGO DOOR CUTOUT. BLENDED OUT CORROSION LESS THAN 20 PERCENT. DOES NOT REQUIRE FURTHER RE WORK, IAW SRM 53-05 PG 173 SEC B-13. (M) 2L72 4F RTA6WE 19951222002981995122200298WP 1995 12 22 ORJA95109 119951025A5320 SILL DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CORROSION UPPER DOOR SILL INSIDE HOLE AT FASTENER AND WHERE REINFORCEMENT MEETS BODY, OVERHEAD, MID CARGO. CLEANED DIRT AND DEBRIS. FOUND NO CORROSION TO EXIST. (M) 2L72 4F RTA6WE 19951222002991995122200299WP 1995 12 22 ORJA95110 119951025A5320 SILL DOUG DC9 DC983 3022083WP CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CORROSION ON LOWER DOOR SILL, MID CARGO. REPAIRED CORRODED LOWER DOOR SILL, MID CARGO, IAW SRM 53-05 FIG 63. (M) 2L72 4F RTA6WE 19951222003001995122200300WP 1995 12 22 ORJA95111 119951025A5350 SEAL DOUG DC9 DC983 3022083WP RADOME CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LIGHT CORROSION AROUND AFT RADOME SEAL AREA INSIDE LIP OF RADOME. REMOVED CORROSION. MIN MATERIAL REMOVED. ALODINED AND PRIMED OK, REF SRM 51-10-3 A. (M) 2L72 4F RTA6WE 19951222003011995122200301NM 1995 12 22 ORJA95112 119951219A32303955923507 ROD ASSY DOUG MD90 MD9030 3023690NM NLG MALFUNCTIONED A ORJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP11902RA 53490 AFTER TAKEOFF FROM SAN JOSE, THE AIRCRAFT REMAINED IN GROUND MODE. RETURNED TO SAN JOSE. REMOVED AND REPLACED NOSE GEAR GROUND SENSING CONTROL ROD ASSEMBLY. OPS CHECK NORMAL PER MM 32-22-02. (X) 2L72 4F RTA6WE 19951222003021995122200302WP 1995 12 22 ORJA95113 119951026A5230 DOOR DOUG DC9 DC983 3022083WP CARGO COMPT CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CORRODED (RUST) FASTENER AFT UPPER MID CARGO INTERNAL CARGO DOOR. CLEANED UP CORROSION (RUST) REF SRM 51-10-3. (M) 2L72 4F RTA6WE 19951222003031995122200303WP 1995 12 22 ORJA95114 119951027A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP CARGO COMPT PUNCTURED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 METAL FLOOR PANEL PUNCTURED AND DEFORMED WITH CORROSION AFT PIT FLOOR PLATE. REPAIRED 2 PUNCTURED AND DEFORMED AREAS ON AFT PIT FLOOR PLATE. INSTALLATION OF DOUBLER AT EACH LOCATION USING MATERIAL OF SAME THICKNESS. INSTALLED PER REF DC9 SRM 53-01 PAGE 17 AND 53-04 FIG 1. (M) 2L72 4F RTA6WE 19951222003041995122200304WP 1995 12 22 ORJA95115 119951027A5347 SEAT TRACK DOUG DC9 DC983 3022083WP BS 1250 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 SMALL SPOT OF CORROSION IN BASE OF SEAT TRACK, APPROXIMATELY STATION 1250, OUTBOARD RIGHT. REMOVE CORROSION PER SRM 51-8-1. PROTECTIVE TREATMENT, SRM 51-8-0. WITHIN LIMITS PER SRM 53-05 PG 8P. (M) 2L72 4F RTA6WE 19951222003051995122200305WP 1995 12 22 ORJA95116 119951028A5320 THRESHOLD DOUG DC9 DC983 3022083WP L1 DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CORROSION ON INNER EDGE OF L-1 DOOR THRESHOLD AT MOON MAT EDGE. CORROSION REMOVED REF DOUGLAS SRM 51-22-1. NEW FILLER STRIP MADE AND INSTALLED. REF DOUGLAS SRM 51-10-2 AND 51-10-3. (M) 2L72 4F RTA6WE 19951222003061995122200306WP 1995 12 22 ORJA95117 119951026A5320 ANGLE DOUG DC9 DC983 3022083WP BS 1485 CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 CANT FRAME FORWARD LOWER ANGLE STATION 1485 CORROSION (MARKED). (M) 2L72 4F RTA6WE 19951222003071995122200307WP 1995 12 22 ORJA95118 119951026A5753 SUPPORT DOUG DC9 DC983 3022083WP NR 2 TE VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 RT WING INBOARD NR 2 FLAP VANE SUPPORT IS WORN ON LEADING EDGE AND HAS LIGHT CORROSION. REMOVED AND CLEANED CORROSION AND APPLIED CORROSION INHIBITING COMPOUND PER SRM CHAP 51-10-3. (M) 2L72 4F RTA6WE 19951222003081995122200308WP 1995 12 22 ORJA95119 119951026A5730 ACCESS PANEL DOUG DC9 DC983 3022083WP LT/RT WING TANKSCORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 MINOR SURFACE CORROSION ON WING TANK ACCESS PANEL 1335C ON LEFT WING AND 1436C RIGHT WING. CORROSION FOUND TO BE PREDOMINENTLY CONFINED TO SEAL CONTACT RING AND DOME NUTS. REMOVED AND REPLACED LEFT AND RIGHT SEAL CONTACT RINGS AND DOME NUTS. REMOVED OTHER LOCALIZED CORROSION, MIN MATERIAL REMOVED, ALODINED AND PRIMED OK. (M) 2L72 4F RTA6WE 19951222003091995122200309WP 1995 12 22 ORJA95120 119951026A5753 BRACKET DOUG DC9 DC983 3022083WP LT TE FLAP VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LEFT WING FLAP VANE HAS CORROSION, BOTTOM, AFT OF 3RD FROM THE END FLAP VANE BRACKET. CLEANED, TREATED AND PRIMED AREA, IAW MD80 SRM 51-10-03. (M) 2L72 4F RTA6WE 19951222003101995122200310WP 1995 12 22 ORJA95121 119951026A5753 SUPPORT DOUG DC9 DC983 3022083WP NR 3 TE VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LEFT WING INBOARD FLAP NR 3 FLAP VANE SUPPORT IS WORN ON LEADING EDGE AND HAS CORROSION ON UPPER SIDE. BLENDED VANE SUPPORT PER SRM 51-01, PG 3 AND REMOVED CORROSION PER SRM 51-10-03. (M) 2L72 4F RTA6WE 19951222003111995122200311WP 1995 12 22 ORJA95122 119951026A5753 SUPPORT DOUG DC9 DC983 3022083WP LT NR 3 VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LEFT WING INBOARD FLAP NR 3 VANE SUPPORT UPPER FITTINGS ARE CORRODED. REMOVED CORROSION AND COATED WITH PRIMER. (M) 2L72 4F RTA6WE 19951222003121995122200312WP 1995 12 22 ORJA95123 119951026A5753 SUPPORT DOUG DC9 DC983 3022083WP LT NR 2 VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LEFT WING FLAP NR 2 FLAP VANE SUPPORT IS GOUGED AT LOWER LEADING EDGE AND CORRODED AROUND UPPER ATTACHED FITTINGS. CLEANED CORROSION, IAW MD80, SRM DC9 51-10-3, AND BURNISHED VANE SUPPORT ASSY. (M) 2L72 4F RTA6WE 19951222003131995122200313WP 1995 12 22 ORJA95124 119951026A5753 SUPPORT DOUG DC9 DC983 3022083WP LT NR 1 VANE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11833RA 53045 LEFT WING INBOARD FLAP NR 1 FLAP VANE SUPPORT HAS CORROSION AROUND UPPER ATTACH FITTINGS. REMOVED CORROSION AT ATTACHED FITTINGS, ON LEFT WING FLAP NR 1 VANE SUPPORT IAW SRM 51-10-3. (M) 2L72 4F RTA6WE 19951222003141995122200314WP 1995 12 22 ORJA95125 119951113A5330 SKIN DOUG DC9 DC982 3022082WP FWD FUSELAGE CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 SURFACE CORROSION ON RIGHT FUSELAGE SKIN, FORWARD OF RAM AIR TEMP PROBE. SURFACE DAMAGE REQUIRED BLEND OUT, ITS ACCEPTABLE AS IS, REF DC9 SRM 53-04, TABLE A, COND 1. (M) 2L72 4F A6WE 19951222003151995122200315 1995 12 22 ORJA95126 419951113A3442 ANTENNA DOUG DC9 DC982 3022082WP RADAR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 MINOR SURFACE CORROSION ON FORWARD AND AFT FACE OF RADAR DISH. REMOVED SURFACE CORROSION AND TREATED, REF DC9 SRM 51-10-3. OK FOR CONTINUED SERVICE. (M) 2L72 4F A6WE 19951222003161995122200316WP 1995 12 22 ORJA95129 119951114A5320 THRESHOLD DOUG DC9 DC982 3022082WP CARGO DOOR CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 AFT CARGO DOOR THRESHOLD PLATE HAS CORROSION AROUND MOUNTING SCREWS, MARKED. REMOVED CORROSION FROM SCREW HOLES, REF SRM 51-10-3. (M) 2L72 4F A6WE 19951222003171995122200317EU 1995 12 22 P2RA950030 119951122A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R2 DOOR INOPERATIVE A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 FLT NR 603 - CREW REPORTED THAT R2 DOOR COULD NOT BE DISARMED AFTER LANDING. REINSTALLED GIRT SLIDE BAR ON DOOR. CHECKED NORMAL PER AMM 52-22-22. (M) 2L72 4F A35EU 19951222003181995122200318EU 1995 12 22 P2RA950031 119951123A2560 GIRT BAR AIRBUS300 A300B4203 3930306EU R2 DOOR LACK OF LUBE A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 FLT NR 300, LGB-ATL - R2 DOOR WILL NOT DISARM. MAINTENANCE UNABLE TO DUPLICATE, DOOR DISARMED ON ARRIVAL. LUBED ARM/DISARM HANDLE AND SLIDE BAR LINKAGE. OPERATIONAL CHECK NORMAL PER AMM 52-22-22. (M) 2L72 4F A35EU 19951222003191995122200319EU 1995 12 22 P2RA950032 119951127A2611 SMOKE DET WIRE AIRBUS300 A300B4203 3930306EU LAVATORY SHORTED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314975 261 LGB - LAV SMOKE DETECTORS NOT WORKING IN FLIGHT. TROUBLESHOT AND FOUND SHORTED WIRE IN ZONE 121, REPAIRED WIRING. SYSTEM OPS CHECK GOOD PER WIRING DIAGRAM 24-50-48. (M) 2L72 4F A35EU 19951222003201995122200320EU 1995 12 22 P2RA950033 119951126A2560 SILL AIRBUS300 A300B4203 3930306EU R2 DOOR OUT OF ADJUST A P2RAK NONE O OTHER TXTAXI/GRND HDL 1 WP2314975 261 PASSENGER DOOR R2 SLIDE WILL NOT DISARM AT TERMINATION OF FLIGHT. MAINTENANCE INSPECTED THE R2 DOOR SLIDE ARMING SYSTEM AND READJUSTED AFT SILL PLATE AS PER AMM 52-10-11. RESULTS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F A35EU 19951222003211995122200321EU 1995 12 22 P2RA950034 119951201A2913650660 HYD PUMP AIRBUS300 A300B4203 3930306EU NR 1 ENGINE FAILED A P2RAH DEACTIVATE SYST/CIRCUITS KJ FLUID LOSS WARNING INDICATION DEDESCENT 1 WP2314975 261 FLT NR 603 - ATL-LGB - CREW REPORTED, THAT NR 1 ENGINE GREEN HYD PUMP 'MI' WENT AMBER SHORTLY BEFORE TOP OF DESCENT. NR 1 PUMP WAS SET TO DUMP. PRESSURE AND QTY NORMAL. APPROX 5 MINUTES LATER, QTY WENT TO ZERO. LANDED LGB SAFELY. AIRCRAFT TOWED TO TERMINAL FROM RUNWAY. MAINTENANCE REPLACED NR 1 ENGINE HYD GREEN PUMP, CASE DRAIN FILTER AND FLUSHED OUT THE HYD SYSTEM. OPERATIONAL CHECK NORMAL. AIRCRAFT RELEASED FOR SERVICE. (M) 2L72 4F A35EU 19951222003221995122200322EU 1995 12 22 PLG103095G1 119951028A30205056T88P01 GARRETT VLV SAAB SF340 SF340A 7850100EU RT ENGINE MALFUNCTIONED A APLGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE05341BE AEX10420 340A063 FLT NR 4483 - EN ROUTE TO BOS, RECEIVED A RIGHT ENGINE ANTI-ICE VALVE LIGHT AND THE CAPTAINS AIRSPEED INDICATOR FAILED. THE AIRCRAFT RETURNED TO HPN, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE CLEANED THE CANNON PLUG AT THE CAPTAINS AIRSPEED INDICATOR AND DEFERRED THE AIR VALVE LIGHT IAW THE MEL, AND RETURNED THE AIRCRAFT TO SERVICE. UPON ARRIVAL IN BOS, MAINTENANCE REPLACED THE RIGHT ENGINE ANTI-ICE GARRETT VALVE TO CLEAR THE MEL. (M) 2L72 4T RTA52EU 19951222003231995122200323 1995 12 22 PLG103095G2 419951028A2350 CONTROL PNL BEECH 1900 1900C 1154161CE COCKPIT WET A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE05818BE UB61 FLT NR 3101 - ON CLIMB-OUT FROM LEB, A LOUD SQUEAL WAS HEARD OVER THE HEADSETS WHICH COULD NOT BE CLEARED. THE AIRCRAFT RETURNED TO LEB, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT WHERE THE AUDIO CONTROL PANEL AND CO-PILOT MIC JACK WERE FOUND TO BE VERY WET. ONCE DRIED, THE SYSTEM FUNCTIONED NORMALLY AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19951222003241995122200324EU 1995 12 22 PLG103095G3 119951029A26203090870 SQUIBB SAAB SF340 SF340A 7850100EU CARGO BAY FAILED A PLGAF ACTIVATE FIRE EXT. J WARNING INDICATION APAPPROACH 1 NE05344BE AEN11 340A104 FLT 4719 - ON APPROACH, CREW RECEIVED 2 INTERMIT CARGO SMOKE DETECT LIGHT WARN. APPROX 500 FEET, CARGO WARN LIGHT REMAINED ILLUMINATED. THE CARGO FIRE EXTINGUISHER SWITCH SELECTED. AFTER ACTUATING THE SWITCH, THE SMOKE DETECT WARNING LIGHT REMAINED ILLUMINATED AND THE CARGO FIRE EXTINGUISHER DISCHARGE LIGHT FAILED TO ILLUMINATE. AN EMERG DECLARED, THE A/C LANDED IN LGA W/O INCIDENT. LGA MX INSPECTED THE A/C AND REPAIR. PSM MX REPLACED FAULTY DETECT WHICH CAUSED THE WARN LIGHT TO ILLUMINATE. ELECT SQUIBB WAS REMOVED AND FOUND TO HAVE TIP OF CARTRIDGE MISSING, THE CARTRIDGE HAD NOT FIRED AND THE SEAL ON THE FIRE EXTINGUISHER HAD NOT BEEN PENETRATED. MX REPLACED CARTRIDGE AND RETURNED A/C TO SERVICE.(M) 2L72 4T RTA52EU 19951222003251995122200325EU 1995 12 22 SIMA953331 119951129A3350 EEL WIRE AEROSPATR72 ATR72212 EU AIRSTAIR BROKEN A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21263AT 263 ORD - FLT NR 4286 - EMERGENCY AIRSTAIR LIGHT INOP. REPAIRED BROKEN WIRE AT BOTTOM OF TOP STEP. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19951222003261995122200326EU 1995 12 22 SIMA953333 119951129A3231S5287910100000 LINK ASSY AEROSPATR72 ATR72212 EU MLG DOOR FAILED A SIMAK NONE O OTHER CRCRUISE 1 SW21425MJ 425 ORD - FLT NR 4373 - LEFT MAIN GEAR DOOR NOTED TO BE OUT OF NORMAL POSITION IN FLIGHT. MAINTENANCE FOUND DOOR SUPPORT LINK TO HAVE FAILED. REPLACED LINK ASSY, PERFORMED GEAR RETRACTION TEST AND RELEASED AIRCRAFT FOR SERVICE. (M) 2H72 4T RTA53EU 19951222003271995122200327EU 1995 12 22 SIMA953361 119951202A7931S7931000600200 OIL LINE AEROSPATR42 ATR42300 8680920EU NR 2 ENGINE CRACKED A SIMAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW21424MQ 045 ORD - FLT NR 4200 - NR 2 ENGINE LOW OIL PRESSURE WARNINGS IN FLIGHT, NR 2 ENGINE SHUT DOWN. INSPECTED ENGINE AND FOUND OIL PRESSURE LINE TO THE LOW PRESSURE SWITCH WAS CRACKED. RAI'D LINE OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE. (M) 2H72 4T RTA53EU 19951222003281995122200328NE 1995 12 22 SIMA953362 219951202A73203039242 NH SENSOR AEROSPATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 ENG FAILED A aSIMAA UNSCHED LANDING O OTHER CLCLIMB 1 SW21263AT CH10660 263 127094 TOL - FLT NR 4350 - JUST AFTER TAKEOFF, THE NR 2 ENGINE SURGED 35 PERCENT, CREW SELECTED BLEEDS AND SYCHOPHASER OFF, NO EFFECT. REDUCED POWER TO 60 PERCENT AND ENGINE STABILIZED, RETURNED TO TOL WITHOUT FURTHER INCIDENT. RAI'S NR 2 NH SENSOR CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19951222003291995122200329NM 1995 12 22 TAOA119508 119951119A2611824PY SMOKE DETECTOR BOEING727 727294 1384088NM FWD LAV BROKEN WIRE A TAOAO OTHER P NO WARNING INDICATION ININSP/MAINT 1 EA15921TS TS411 22043 FORWARD LAV SMOKE DETECTOR WAS FOUND TAMPERED WITH AND WAS DISMOUNTED. REPAIRED BROKEN WIRE, CHECKED SMOKE DETECTOR, OK IN TEST. (M) 0 4 A3WE 19951222003301995122200330NM 1995 12 22 TAOA119509 119951122A2611824PY SMOKE DETECTOR BOEING727 727227 1384078NM LT LAVATORY INOPERABLE A TAOAO OTHER P NO WARNING INDICATION ININSP/MAINT 1 EA15925TS 21244 LEFT AFT LAV SMOKE DETECTOR INOPERABLE. REPLACED SMOKE DETECTOR FOR LEFT AFT LAVATORY. OPS CHECKED OK AS PER MM 26-00. (M) 2L73 4F A3WE 19951222003311995122200331WP 1995 12 22 USAA951234 119951122A5320 MEMBRANE DOUG DC9 DC982 3022082WP BS 1032 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING A Q-1 CHECK INSPECTION, FOUND .5 INCH CRACK IN CUSP MEMBRANE WEB STATION 1032 OUTBOARD OF RT SEAT TRACK. ACCOMPLISHED SPLICE REPAIR PER USAIR EA NR 315530A. (M) 2L72 4F A6WE 19951222003321995122200332EU 1995 12 22 USAAF95007 119951121A3350500000043 EEL BATT CHARGER FOKKERF28 F28MK4000 4990810EU CABIN FAILED A USAAK NONE L NO TEST NRNOT REPORTED 1 EA19482US 11231 CLT - FLT NR 947 - EMERGENCY EXIT LIGHTS FORWARD CABIN STAY ON WITH SWITCH IN ARMED OR OFF POSITION. REPLACED BATTERY CHARGER. EMERGENCY LIGHTS CHECK OK. (M) 2L72 4F RTA20EU 19951222003331995122200333NM 1995 12 22 USAASB95015 119951117A2130 PRESSURIZATION BOEING737 7374B7 1384702NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19779AU 24996 PHL - FLT NR 1535 - CLIMBING THROUGH FL 310, CABIN ALTITUDE WAS CLIMBING AT 1000 FPM. FLIGHT CREW WAS UNABLE TO CONTROL CABIN PRESSURE IN AUTO OR STANDBY. RETURNED TO PHL AND LANDED WITHOUT INCIDENT. PERFORMED PRESSURIZATION CHECK. SYSTEM CHECKED NORMAL. UNABLE TO DUPLICATE ANY DEFECT. (M) 2L72 4F RTA16WE 19951222003341995122200334NE 1995 12 22 USAASB95016 219951119A75307064004 BLEED VLV BOEING737 7373B7 1384580NM GE CFM56 CFM563B1 13802NE NR 2 ENGINE FAILED A aUSAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19392US19590 23314 MCO - FLT NR 378 - NR 2 ENGINE OVERTEMPED ON TAKEOFF TO 944 DEGREES FOR 2 SECONDS. FLIGHT CREW REDUCED POWER AFTER TAKEOFF TO BELOW RED LINE. CREW COULD NOT SELECT NORMAL CLIMB N1 WITHOUT EGT EXCEEDANCE. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND VLV GEAR MOTOR FAILURE. REPLACED VLV MOTOR AND MASTER BALLSCREW ACTUATOR. ENGINE OPS CHECKED NORMAL. (M) 2L72 4F4 FRTA16WE E2GL 19951222003351995122200335NM 1995 12 22 USVA10951 119950929A57536573732 FLAP 6545412 BOEING737 737247 138448DNM LT TE AFT FLAP CRACK A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 LEFT INBOARD AFT FLAP LOWER SURFACE HAS A 2 INCH LONG CRACK. REPAIRED CRACK PER SRM 51-40-6. (M) 2L72 4F A16WE 19951222003361995122200336NM 1995 12 22 USVA109510 119951006A5313BAC149320 STRINGER BOEING737 737247 138448DNM FS 500 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 STRINGER 26R IS CRACKED ON FORWARD SIDE OF FS 500B. REPLACED STRINGER PER SRM 52-10-3, FIG 2. (M) 2L72 4F A16WE 19951222003371995122200337NM 1995 12 22 USVA109511 119951006A5730 SKIN BOEING737 737247 138448DNM LT WING CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 LEFT WING UPPER SURFACE LEADING EDGE SKIN AFT OF NR 1 SLAT GUIDE CUTOUT HAS A 1 INCH WING CRACK. REPLACED SKIN PER SRM 57-30-4. (M) 2L72 4F A16WE 19951222003381995122200338NM 1995 12 22 USVA109512 119951104A5313BAC1493574 STRINGER BOEING737 737247 138448DNM FS 500 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 MODERATE CORROSION AND CRACK AT STRINGER 26L, FS 500A. REPAIRED STRINGER PER SRM 53-10-3, FIG 1. (M) 2L72 4F A16WE 19951222003391995122200339NM 1995 12 22 USVA109513 119951006A3350D43637 EEL ASSY GRIMES BOEING737 737247 138448DNM FS 950 INOPERATIVE A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 AFT EMERGENCY EXIT LIGHTS AFT OF CABIN CEILING INOP. REPLACED LIGHT ASSY PER MM 33-20-00. (M) 2L72 4F A16WE 19951222003401995122200340NM 1995 12 22 USVA109514 119951004A5315BAC1505100246 FLOOR BEAM BOEING737 737247 138448DNM FS 1016 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 FLOOR BEAM HAS HEAVY CORROSION AND CRACK FS 1016, BETWEEN RBL 5 T0 20. REPAIRED BEAM PER SRM 53-10-9. (M) 2L72 4F A16WE 19951222003411995122200341NM 1995 12 22 USVA109515 119951004A5311 FRAME BOEING737 737247 138448DNM FS 460 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 BELT FRAME AT FS 460 IS CRACKED BETWEEN STRINGERS 20L-21L. REPAIRED FRAME PER SRM 51-40-3. (M) 2L72 4F A16WE 19951222003421995122200342NM 1995 12 22 USVA109516 119951004A575365478416 SPAR 65719712 BOEING737 737247 138448DNM RT TE MID FLAP CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 RIGHT WING MID INBOARD FLAP REAR SPAR UPPER ANGLE CRACKED 1 INCH LONG AT STATION WLB 73. REPAIRED PER DALFORT AVIATION XEA NR X8-57-82. (M) 2L72 4F A16WE 19951222003431995122200343NM 1995 12 22 USVA109517 119951004A532065498801 BEAM BOEING737 737247 138448DNM FS 887 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON TRANSVERSE BEAM FS 887 RBL 60.750. REPAIRED PER DALFORT AVIATION XEA NR X2-53-163. (M) 2L72 4F A16WE 19951222003441995122200344NM 1995 12 22 USVA109518 119951004A5313BAC1498156 STRINGER BOEING737 737247 138448DNM FS 925 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON STRINGER 22L, FS 925. REPAIRED STRINGER PER SRM 53-10-3, FIG 1. (M) 2L72 4F A16WE 19951222003451995122200345NM 1995 12 22 USVA109519 119951004A53156546809 FLOOR BEAM BOEING737 737247 138448DNM FS 947 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON FLOOR BEAM UPPER SURFACE FS 947 BETWEEN 2BL 0 TO RBL 60. REPAIRED PER DALFORT AVIATION XEA NR X2-53-161 REVISION 1. (M) 2L72 4F A16WE 19951222003461995122200346NM 1995 12 22 USVA10952 119950929A53156546817 FLOOR BEAM BOEING737 737247 138448DNM FS 369 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON UPPER SURFACE OF FLOOR BEAM, FS 360, JUST AFT OF GALLEY. REPAIRED BEAM PER SRM 53-10-9, FIGURE 9. (M) 2L72 4F A16WE 19951222003471995122200347NM 1995 12 22 USVA109520 119950929A57556573730 SPOILER 6545412 BOEING737 737247 138448DNM RT WING DELAMINATION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 NR 6 SPOILER DELAMINATED ON TOP OUTBOARD END. REPAIRED SPOILER PER SRM 57-50-5. (M) 2L72 4F A16WE 19951222003481995122200348NM 1995 12 22 USVA10953 119950929A5320 WEB BOEING737 737247 138448DNM FS 967-1006 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON RIGHT CUSP LINE WEB FS 967-1006. REPLACED WEB ASSEMBLY PER SRM 51-40-2. (M) 2L72 4F A16WE 19951222003491995122200349NM 1995 12 22 USVA10954 119950929A53116546533 FRAME BOEING737 737247 138448DNM FS 500 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 BELT FRAME UPPER SURFACE AT FS 500, STRINGER 26L HAS A .75 INCH CRACK. REPAIRED FRAME PER SRM 51-40-3. (M) 2L72 4F A16WE 19951222003501995122200350NM 1995 12 22 USVA10955 119950929A53156546811 FLOOR BEAM BOEING737 737247 138448DNM FS 987 CORROSION A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 HEAVY CORROSION ON ENTIRE LENGTH OF UPPER SURFACE OF FLOOR BEAM FS 987. REPAIRED FRAME PER SRM 53-10-9, FIGURE 1. (M) 2L72 4F A16WE 19951222003511995122200351NM 1995 12 22 USVA10956 119950929A5320651758347 CHORD BOEING737 737247 138448DNM FS 178 CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 VERTICAL CHORD ANGLE HAS A 1.75 INCH LONG CRACK AT FS 178, LBL 7, WL 184. REPAIRED PER DALFORT AVIATION XEA NR X2-53-162. (M) 2L72 4F A16WE 19951222003521995122200352NM 1995 12 22 USVA10957 119950929A57556573750 SPOILER 6545412 BOEING737 737247 138448DNM LT WING CRACKED A USVAK NONE O OTHER ININSP/MAINT 1 SO19305VA 19606 NR 2 SPOILER HAS A 2 INCH CRACK ON TOP OF TRAILING EDGE. REPAIRED SPOILER PER SRM 51-40-6. (M) 2L72 4F A16WE 19951222003531995122200353NM 1995 12 22 USVA10958 119951006A335008163000610 EEL TRACK BRUCE BOEING737 737247 138448DNM BS 950, 900 SPLIT A USVAK NONE L NO TEST ININSP/MAINT 1 SO19305VA 19606 AFT PIECE OF EMERGENCY PATH LIGHTING SYSTEM TRACK SPLIT. REPLACED AFT SECTION PER MM 33-20-00. (M) 2L72 4F A16WE 19951222003541995122200354WP 1995 12 22 VTZA96031 219951126A73201379287L405 P3 LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENGINE BROKEN A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27475UE 850 P66197 FLT NR 6284 - IAD-HPN - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE RIGHT SRL AND RT BETA LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE P3 LINE, WHICH WAS BROKEN. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA56EU E4WE 19951222003551995122200355EU 1995 12 22 VTZA96033 119951130A77228974696 EGT SOFT HARNESS BAG JETSTMJETSTM3201 1500217EU LEFT ENGINE FAILED A VTZAA UNSCHED LANDING O OTHER CLCLIMB 1 EA27489UE 908 FLT NR 6552 - IAD-SWF - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE RIGHT ENGINE EGT FLUCTUATING 30 TO 40 DEGREES. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RIGHT ENGINE EGT SOFT HARNESS. OPS CHECKS GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951222003561995122200356EU 1995 12 22 VTZA96034 119951201A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR FAILED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27488UE 907 FLT NR 6155 - IAD-ALB - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE PASSENGER DOOR WARNING CPA LIGHT COMING ON IN FLIGHT. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE PASSENGER DOOR HANDLE MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19951222003571995122200357 1995 12 22 VTZA96035 419951203A22127003897903 CONTROLLER JETAIRJETSTMJETSTM4101 1500501EU AUTOPILOT FAILED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27302UE 41013 IAD-TYS - FLT NR 6160 - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THERE BEING A BURNING SMELL IN THE CABIN. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE AUTO-PILOT CONTROLLER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19951222003581995122200358EU 1995 12 22 WTAA950298 119951106A5350 RADOME BAG JETSTMJETSTM3101 1500215EU FUS NOSE SECT BIRDSTRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17425UE 798 FAT - BIRD STRIKE REPORTED ON NOSE SECTION OF AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003591995122200359EU 1995 12 22 WTAA950299 119951107A5270 DOOR LIGHT BAG JETSTMJETSTM3101 1500215EU COCKPIT ILLUMINATED A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17103XV 747 LAX - DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. CREW COMPLIED WITH EMERGENCY PROCEDURES IN QRH. LIGHT REMAINED ON. AIRCRAFT CONTINUED TO STATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED DOOR MECHANISM, INCLUDING LOCK PINS AND MICROSWITCHES. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF DOOR AND WARNING SYSTEM. SYSTEM OPERATIONAL CHECK NORMAL. UNABLE TO DUPLICATE REPORTED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003601995122200360EU 1995 12 22 WTAA950300 119951108A3260622800200 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG DIRTY A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17423UE 799 LAX - RIGHT MAIN LANDING GEAR 'GREEN' POSITION INDICATION LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE CLEANED RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003611995122200361EU 1995 12 22 WTAA950301 119951108A3260 GEAR LIGHT BAG JETSTMJETSTM3101 1500215EU RT MLG ILLUMINATED A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17423UE 799 FAT - RT MAIN LANDING GEAR 'GREEN' POSITION INDICATION LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE INSPECTED AND TESTED RT MAIN LANDING GEAR DOWNLOCK MICROSWITCH, NO DEFECTS NOTED. GEAR INDICATIONS NORMAL DURING GROUND TEST. MAINTENANCE UNABLE TO DUPLICATE REPORTED DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003621995122200362EU 1995 12 22 WTAA950302 119951108A3260 CONNECTOR BAG JETSTMJETSTM3101 1500215EU RT MLG LOOSE A WTAAO OTHER N FALSE WARNING CLCLIMB 1 WP17423UE 799 FAT - RIGHT MAIN LANDING GEAR 'GREEN' POSITION INDICATION LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE REPLACED WORN ELECTRICAL CONNECTOR AT RIGHT MAIN GEAR UPLOCK MICROSWITCH P/N 622800200. GEAR INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003631995122200363EU 1995 12 22 WTAA950303 119951108A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG OUT OF ADJUST A WTAAK NONE N FALSE WARNING LDLANDING 1 WP17423UE 799 FAT - NOSE LANDING GEAR 'GREEN' POSITION INDICATION LIGHT REPORTED INTERMITTENT ON LANDING ROLL OUT. MAINTENANCE ADJUSTED NOSE GEAR DOWN LOCK MICROSWITCH. GEAR POSITION INDICATIONS NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003641995122200364EU 1995 12 22 WTAA950304 119951116A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU RT MLG BROKEN WIRE A WTAAK NONE N FALSE WARNING LDLANDING 1 WP17331CA 793 SEA - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT FAILS TO ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRE AT RIGHT MAIN LANDING GEAR UPLOCK MICROSWITCH. GEAR INDICATIONS NORMAL DURING GROUND TEST. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003651995122200365EU 1995 12 22 WTAA950307 119951119A6120897410 PROP GOVERNOR BAG JETSTMJETSTM3101 1500215EU RT ENGINE OUT OF ADJUST A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17418UE 780 RDM - RIGHT ENGINE OBTAINS ONLY 97 PERCENT RPM ON TAKEOFF ROLL WITH SPEEDS HIGH. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT ENGINE PROP GOVERNOR CONTROLS. ENGINE OPERATION NORMAL DURING GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19951222003661995122200366SO 1995 12 22 WTAA950310 119951126A5330 SKIN EMB 120 EMB120RT SO FUSELAGE BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17285UE 120153 SFO - BIRD STRIKE REPORTED ON RIGHT SIDE OF AIRCRAFT. ACCOMPLISHED INSPECTION OF AIRCRAFT. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19951222004211995122200421CE 1995 12 22 95ZZZX6823 119951113A7160 RAM AIR BEECH 80 65B80 1152812CE ENGINE INLET FOD A A7MAK NONE O OTHER NRNOT REPORTED 1 GL27768A 238 LD315 THE DAMAGE WAS CAUSED BY FOD THROUGH RAM AIR INLET WHICH CAUSED SUPERCHARGER IMBALANCE WHICH CAUSED LEANING OF NR 6 CYLINDER ALONG WITH SUPERCHARGE BEING THROWN OUT OF BALANCE CAUSED BEARING TO SPIN AND BREAK OFF. SUBMITTER STATED TO PREVENT THIS, PRE-FLIGHT INSPECTION OF RAM AIR INLET AT EACH FLIGHT. 1L72 3O 3A20 19951222004271995122200427GL 1995 12 22 95ZZZX6829 319951117A6110 PROPELLER CESSNA402 402C 207590RCE MCAULY3AF32C3AF32C93 GL DOME LEAKING A BAJAK NONE K FLUID LOSS ININSP/MAINT 1 AL013246M 1105 402C0294 795936 RED DYE LEAKING FROM DOME. SUSPECTED SEALS FAILED INTERNALLY. ONE BLADE LOOSE BEYOND MANUFACTURER'S LIMITS. 1L72 3O A7CE 5 CP22EA 19951222004331995122200433CE 1995 12 22 95ZZZX6835 119951003A5246555215017 ACCESS DOOR CESSNA500 550 2076604CE LT ENG COWL DEPARTED A AIMJAK NONE C F.O.D. CRCRUISE 1 EA25232DM5432 550079 LEFT ENGINE OIL ACCESS DOOR (APPROXMATELY 6 INCHES BY 8 INCHES) DEPARTED THE AIRCRAFT STRIKING THE LT HORIZONTAL STABILIZER, CUTTING A SMALL HOLE IN THE DEICE BOOT AND DENTING THE LEADING EDGE SKIN. INSPECTION OF THE HINGE REMAINING ON THE COWLING REVEALED THAT HINGE PIN WORKED ITS WAY FORWARD FROM THE HINGE DUE TO WEAR IN THE HINGE. AFTER THE HINGE PIN WORKED FORWARD, THE OIL DOOR FELL OFF. INSPECTION OF THE RT OIL ACCESS DOOR REVEALED A SIMILAR WORN HINGE. THE NEW DOOR ASSY (PN 5552150-37) HAS AN IMPROVED HINGE. RT DOOR HINGE WAS REPLACED. 1L72 4F A22CE 19951222004401995122200440WP 1995 12 22 9520719603 119951218A3231 DOOR CABLE DOUG DC9 DC932 3022066WP NLG OUT OF ADJUST A NWAAO OTHER P NO WARNING INDICATION CLCLIMB 1 GL01603NW 47101 DURING CLIMB, A NOISE WAS NOTICED COMING FROM THE NOSE LANDING GEAR AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND NOISE CONTINUED. AIRCRAFT CONTINUED TO DESTINATION BELOW 250 KIAS AND WITH LANDING GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT FORWARD LANDING GEAR DOOR OPEN. ADJUSTED NOSE LANDING GEAR DOOR CABLE TENSION AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222004411995122200441WP 1995 12 22 9520729996 119951218A2170 COALESCER BAG DOUG DC9 DC931 3022065WP CABIN DIRTY A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL018932E 47141 DURING CRUISE, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED AND CABIN PRESSURE BEGAN TO CLIMB. DESCENDED TO 10,000 FEET AND THE LIGHT EXTINGUISHED AND AIRCRAFT MAINTAINED NORMAL CABIN PRESSURE. AIRCRAFT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BOTH WATER SEPARATOR BAGS. OPERATIONAL CHECK OF BOTH AIR CONDITIONING SYSTEMS WAS GOOD. 2L72 4F A6WE 19951222004421995122200442WP 1995 12 22 9520739908 119951218A3350 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01958N 47254 DURING LINE CHECK, FOUND FORWARD ENTRY OVERHEAD AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222004431995122200443WP 1995 12 22 9520749908 119951218A2130 FLOW CONTL VLV DOUG DC9 DC931 3022065WP CABIN MALFUNCTIONED A NWAAAB UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01958N 47254 DURING CRUISE, THE AIRCRAFT LOST CABIN PRESSURIZATION AND THE OXYGEN MASKS DEPLOYED. EMERGENCY DESCENDED AND DIVERTED TO BHM AND LANDED WITHOUT FURTHER INCIDENT. REPLACED THE LEFT FLOW CONTROL VALVE AND LEFT UPPER AIR CONDITIONING PRESSURE REGULATOR VALVE, OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951222004441995122200444EU 1995 12 22 9520753208 119951218A2742 PACKING AIRBUS320 A320211 3930320EU LT HORIZ STAB LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION UKUNKNOWN 1 GL01308US 107 FLIGHT CREW SENT ACARS MESSAGE NOTIFYING OF GREEN HYDRAULIC SYSTEM LOW LEVEL. THE LANDING GEAR WAS MANUALLY EXTENDED, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT ELEVATOR GREEN SERVO CONTROL ACTUATOR FILTER ASSEMBLY PACKING LEAKING. REPLACED PACKING, LEAK AND OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951222004451995122200445WP 1995 12 22 95FDEA01900 119951219A3230 RETRACT MECH DOUG DC10 DC1030 3023501WP LANDING GEAR LACK OF LUBE A FDEAK NONE N FALSE WARNING LDLANDING 1 SO25302FE 46801 LANDING GEAR TOOK EXCESSIVE AMOUNT OF TIME TO EXTEND. JACKED A/C AS PER MM 7-10-00, LUBED LANDING GEAR, CLEANED LANDING GEAR SELECTOR LEVER IN COCKPIT AND CYCLED LANDING GEAR AS PER MM 32-30-00. CHECKED OK AND NO DEFECTS FOUND. 2L73 4F A22WE 19951222004461995122200446NM 1995 12 22 95FDEA01901 119951220A2612 FIRE LOOP BOEING727 7272S2F 1384O81NM NR 1 ENGINE MALFUNCTIONED A FDEAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO25213FE 22935 INTERMITTENT FIRE WARNING NR 1 ENG FOLLOWED BY CONTINUOUS INTERMITTENT WARNING ON SAME. COMPLIED WITH PROCEDURE AND SHUTDOWN NR 1 ENG WARNING, PERSISTED. FIRED NR 1 AND NR 2 BOTTLE INTO NR 1 ENG PER PROCEDURE. WARNING PERSISTED INTERMITTENTLY TILL TOUCHDOWN AND TAXI TO PARKING. REMOVED AND REPLACED NR 1 ENG FIRE DETECT ELEMENT AS PRECAUTION. ALSO, CK'D INLET AND EXT-RAN NR 1 PNU DUCTS. ALL OK AND PYLON AREA. REMOVED AND REPLACED 2 EA BOTTLE ASSY PER MM 26-21-1, DUE TO DISCHARGE. FOUND NR 1 ENG A-LOOP INOP. SUSPECT MOISTURE IN FIRE DETECT BOX. DEFERRED PER 26-6(A) CNT NR 1219105 EXP 12-29-95. 2L73 4F A3WE 19951222004471995122200447WP 1995 12 22 ABXA9501043 119951219A3260189915 UPLOCK SWITCH DOUG DC8 DC862 3021970WP RT MLG DOOR DEFECTIVE A ABXAK NONE N FALSE WARNING CLCLIMB 1 GL23804AX 45987 DURING DEPARTURE, UPLATCH CHECK FAILED FOR RIGHT MAIN LANDING GEAR DOOR AFTER GEAR RETRACTION. RECYCLED GEAR AND UNSAFE LIGHT REMAINED ILLUMINATED. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLATCH SWITCH AND OPS CHECK WAS GOOD. 2L74 4F 4A25 19951222004481995122200448SO 1995 12 22 COMA9512027 119951215A2450JLD4N103 RELAY EMB 120 EMB120RT SO NR 2 BUSS DEFECTIVE A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01257CA 120248 THE NR 2 ELECTRIC BUS OFF WARNING LIGHT ILLUMINATED. REPLACED THE CURRENT PROTECTION RELAY KO128. 2L72 4T RTA31SO 19951222004491995122200449SO 1995 12 22 COMA9512028 119951215A325020500 POTENTIOMETER EMB 120 EMB120RT SO NLG STEERING DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01137H 120137 NOSE WHEEL STEERING IS ERRATIC AND PULLS HARD TO THE RIGHT. REPLACED THE FEED BACK POTENTIOMETER BOX. 2L72 4T RTA31SO 19951222004501995122200450SO 1995 12 22 COMA9512029 119951218A2731ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB FAILED A COMACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 SO01243CA 120212 RECEIVED PITCH TRIM WARNING DURING TAKEOFF ROLL. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. 2L72 4T RTA31SO 19951222004511995122200451SO 1995 12 22 COMA9512030 119951218A532012031657002 ANGLE EMB 120 EMB120RT SO RT WING CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO011110J 120110 RT WING ROOT FAIRING UPPER ATTACH ANGLE HAS NUMEROUS BROKEN RIVET HEADS AND POSSIBLE CRACKS. REPAIRED FAIRING SUPPORT ANGLE. 2L72 4T RTA31SO 19951222004521995122200452SO 1995 12 22 COMA9512031 119951218A2750PE610261 ROLLER EMB 120 EMB120RT SO RT TE FLAP WORN A COMAK NONE J WARNING INDICATION UKUNKNOWN 1 SO01256CA 120245 RECEIVED FLAP DISAGREE WARNING, WHEN FLAPS SELECTED TO ZERO DEGREES. REPLACED THE ROLLERS ON THE RT OUTBD FLAP. 2L72 4T RTA31SO 19951222004531995122200453SW 1995 12 22 COMA9520402 119951216A3230 RETRACT MECH SWRNGNSA227 SA227AC 8780603SW LANDING GEAR MALFUNCTIONED A COMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01703CA 227703 LANDING GEAR HAD TO BE CYCLED 3 TIMES TO GET GREEN DOWN AND LOCK INDICATION ON LT MLG. INSPECTED LANDING GEAR AND NO DEFECTS NOTED. CLEANED AND LUBED LANDING GEAR, ACFT RETURNED TO SERVICE. 1L72 4T A8SW 19951222004541995122200454EU 1995 12 22 COMA9531214 119951218A77226058T28P01 ITT HARNESS ASSY SAAB SF340 SF340A 7850100EU RT ENGINE ERRATIC A COMAK NONE O OTHER CRCRUISE 1 SO01340SF2135 682 340A014 RT ENGINE ITT INDICATION IS ERRATIC. REPLACED THE ITT THERMOCOUPLE HARNESS ASSY. 2L72 4T RTA52EU 19951222004551995122200455 1995 12 22 COMA9531215 419951217A34146225353011 ASI SAAB SF340 SF340A 7850100EU LT COCKPIT DEFECTIVE A COMAK NONE O OTHER TXTAXI/GRND HDL 1 SO01361CA183557563 340A056 PILOTS AIR SPEED INDICATOR SHOWS RED FLAG. REPLACED AIR SPEED INDICATOR. 2L72 4T RTA52EU 19951222004561995122200456EU 1995 12 22 COMA9531216 119951218A302072PEF9109013 DUCT ASSY SAAB SF340 SF340A 7850100EU RT ENGINE FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01341CA 340A021 RT ENGINE INTAKE HEAT FAIL INDICATION AND A WHITE FLASHING GLOW VISIBLE INSIDE INTAKE. REPLACED UPPER INLET ASSY. 2L72 4T RTA52EU 19951222004571995122200457 1995 12 22 COMA9560622 419951217A34183995100207A STALL WARN UNIT CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAK NONE O OTHER CRCRUISE 1 SO01949CA 7080 AT 37,000 FEET THERE IS A 12 KNOT DIFFERENCE BETWEEN PILOTS AND COPILOTS STALL WARNING SYSTEM. REPLACED THE STALL PROTECTION UNIT. 2L72 4F RTA21EA 19951222004581995122200458EA 1995 12 22 COMA9560623 119951218A322016410101 DRAG BRACE CNDAIRCL600 CL6002B19 EA NLG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01929CA4882 7035 UNABLE TO RETRACT NOSE LANDING GEAR. REPLACED NLG DRAG BRACE ASSY. 2L72 4F RTA21EA 19951222004591995122200459 1995 12 22 DHL95802005 419951214A3425258733511 FLIGHT DIR IND 2587909 DOUG DC8 DC873F 302199FWP NR 1 MALFUNCTIONED A TDHLACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO01802DH 8123084 46076 EMA - DURING TAKEOFF, CAPT ATTITUDE GYRO FLAG AND INSTRUMENT COMPARATOR WARNING CAME ON WHEN THRUST LEVERS ADVANCED FOR TAKEOFF. THE TAKEOFF WAS REJECTED. REMOVED AND REPLACED VERTICAL GRYO IAW M/M 34-25-1. REMOVED AND REPLACED FLIGHT DIRECTOR INDICATOR IAW M/M 34-23-01, OPS CHECK NORMAL. 2L74 4F RT4A25 19951222004601995122200460NM 1995 12 22 DL72S954726 119951213A571165192923 WEB BOEING727 727232 1384082NM REAR SPAR FATIGUE A DALAK NONE O OTHER ININSP/MAINT 1 SO27403DA 21147 MTC REPORTS, DAMAGE TO THE REAR SPAR WEB OF THE CENTER SECTION FUEL TANK. THE DAMAGE IS LOCATED APPROXIMATELY BETWEEN LBL 17.2 AND LBL 25.5. DAMAGE REMOVAL RESULTED IN A 3 I/B - O/B BY 1 UP/DOWN CUTOUT. THE WEB IS MANUFACTURED FROM 0.375 2024-T351 MACHINED LOCALLY TO A MINIMUM THICKNESS OF 0.040. REPAIRED PER DL ERA 302906-14. 2L73 4F A3WE 19951222004611995122200461NM 1995 12 22 DL72S954727 119951218A5754 ANGLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27521DA 21472 FOUND DURING E-2 LETTER CHECK, NR 2 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED UNDER TAI DUCT. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19951222004621995122200462NM 1995 12 22 DL72S954728 119951218A5530 STRINGER BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27521DA 21472 FOUND DURING E-2 LETTER CHECK, VERTICAL STAB STRINGERS CRACKED, STR 8 RIGHT STA 133.8 AND STR 9 RIGHT STA 133.8. REPAIRED PER M/M 53-30-0 PAR 3. 2L73 4F A3WE 19951222004631995122200463NM 1995 12 22 DL72S954729 119951109A5753652163361 LE SKIN BOEING727 727232 1384082NM LT TE MID FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 L/E EDGE SKIN WORN AT I/B END OF NR 1 MIDFLAP. REPAIRED PER MM 57-53-00. 2L73 4F A3WE 19951222004641995122200464NM 1995 12 22 DL72S954730 119951211A5330 SKIN BOEING727 727232 1384082NM BS 1166 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 FOUND ON CV2 REWRITTEN FROM N/R 1, .25 INCH CRACK ON PNEUMATIC AIR ACCESS DOOR CUTOUT AFT I/B END. REPAIRED PER M/M 53-30-0. 2L73 4F A3WE 19951222004651995122200465NM 1995 12 22 DL72S954731 119951212A5754 RIB BOEING727 727232 1384082NM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 FOUND ON CV2 CHECK TRANSFERRRED FROM N/R 33 ITEM NR 2, .4375 INCH CRACK AT NR 6 SLAT NOSE RIB INBD SIDE OF ACTUATOR. REPAIRED PER M/M 57-54-0 AND ID PER PS 900-5-1 NR 4. 2L73 4F A3WE 19951222004661995122200466NM 1995 12 22 DL72S954740 119951211A5754 RIB BOEING727 727232 1384082NM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 FOUND ON CV2 CHECK, .75 INCH CRACK PAST PREVIOUS STOP DRILL I/B NOSE RIB AT ACTUATOR ROD END ATTACH NR 4 SLAT. REPAIRED RIB PER M/M 57-54-0 PAR 4, NR 4 SLAT. 2L73 4F A3WE 19951222004671995122200467NM 1995 12 22 DL72W954739 119951114A5753652163362 DOUBLER BOEING727 727247 138408FNM LT TE MID FLAP CARCKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272814W 20870 DURING HMV SHOP INSP, FOUND THAT THE NR 4 O/B MIDFLAP, I/B RIB AFT LOWER CORNER REPAIR DOULBER WAS NOT INSTALLED PER M/M. INSTALLED NEW DOULBER PER M/M 57-52-0. 2L73 4F A3WE 19951222004681995122200468NM 1995 12 22 DL73E954725 119951214A53306545768 SKIN BOEING737 7372J8 1384489NM FS 380-400 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27235WA 22859 THE FUSELAGE SKIN WAS GOUGED BETWEEN FS 380 AND FS 400. THE DAMAGE CUT OUT MEASURES APPROX 4.9 BY 23.1. THE NEWLY DAMAGED SECTION IS BETWEEN 2 PREVIOUSLY DAMAGED SKIN SECTIONS, REPAIRS ACCOMPLISHED PER ER/A'S 230787-14 AND 230789-14. IN ADDITION, AN EXISTING DENT HAS BEEN CUT OUT FWD OF FS 380, ABOVE STR 19R, 2.8 BY 5. THIS ER/A SUPERSEDES PREVIOUS SUBJECT ER/A'S. THE SKIN IS MANUFACTURED FROM 0.036 2024-T3 CLAD SHEET WITH A BONDED 0.036 2024-T3 CLAD WAFFLE DOUBLER. INSTALLED NEW REPAIR PER DL ERA 302905-14. 2L72 4F RTA16WE 19951222004691995122200469NM 1995 12 22 DL73S954724 119951216A5330 SKIN BOEING737 737232 1384475NM R-1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27316DL 23088 THE R-2 DOOR HAS A 1.3 INCH CRACK AT THE LOWER AFT CORNER. IT WILL BE REPAIRED PER THE SRM WITH THE EXCEPTION OF BLIND FASTENER SUBSTITUTION TO FACILITATE MAINTENANCE IN MEETING THE LETTER CHECK TIME LIMIT REQUIREMENTS PER DL ERA 302921-14. 2L72 4F RTA16WE 19951222004701995122200470 1995 12 22 DLL10954718 219951215A7530 BLEED AIR LKHEED1011 10113851 5265010WP NR 2 ENGINE OIL FUMES A DALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 SO27722DA30078 193C1147 SMOKE IN REAR CABIN AREA AND ALL 5 AFT LAV SMOKE DETECTORS WENT OFF. ISOLATED NR 2 ENG BLEED, SMOKE DISSIPATED. LOCKED OUT NR 2 EJECTOR AND FWD TO MCO PER MEL 36-11-08A. 2L73 4F A23WE 19951222004711995122200471WP 1995 12 22 DLL10954719 119951217A3244 TIRE LKHEED1011 10113851 5265010WP LT MLG FAILED A DALAC ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 SO27735D 193C1226 ON TAKEOFF, NR 2 TIRE RECAP CAME OFF AND WAS INGESTED INTO NR 1 ENGINE. REJECTED TAKEOFF AT 130 KNOTS, HAD REPORT OF SPARKS FROM NR 1 ENGINE. AT GATE FOUND FOD DAMAGE TO ENGINE. REPLACED ENGINE AND ROUTED TO SHOP. REPLACED NR 1 AND NR 2 WHEEL ASSEMBLIES. 2L73 4F A23WE 19951222004721995122200472NM 1995 12 22 DLM11954721 119951217A3350 BATTERY PACK 6044113 DOUG MD11 MD11 3023602NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27806DE 0782 48477 FAILED EMER LIGHT TEST MSC EMER LIGHT BAT 2 LOW. REPLACED EMER LIGHT BAT 2, OPS CKS OK. 2L73 4F RTA22WE 19951222004731995122200473NM 1995 12 22 DLM88954732 119951218A3350 BULB 07912 DOUG MD88 MD88 3023688NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27988DL 53339 3 WHITE EMERGENCY EXIT TRACK LIGHTS INOP AT ROWS 15, 23 AND 30. RELAMPED SAME, OPN NORMAL. 2L72 4F RTA6WE 19951222004741995122200474WP 1995 12 22 SCNA95293 119951216A256035124389001 SLIDE PRESS IND DOUG DC10 DC1010 3022110WP L 2 DOOR MALFUNCTIONED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15573SC 46645 THE L-2 DOOR SLIDE WOULD NOT TEST. REMOVED AND REPLACED SLIDE PACK PRESSURE INDICATOR IAW MM 25-61-03 AND SLIDE TESTED GOOD. 2L73 4F A22WE 19951222004751995122200475NM 1995 12 22 UPS405129 119951202A5412 FIREWALL BOEING747 747123 1384873NM NR 3 PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 MAINTENANCE FOUND NR 3 ENG PYLON CRACKED AT HORIZONTAL FIREWALL SPLICE INBD DOUBLE ROW OF RIVETS. REMOVED DAMAGED SECTION OF HORIZONTAL WEB AND REMOVED FWD STIFFENER. FABRICATED REPAIR DOUBLER PER EO NR B747-5410-7771, REPAIRED EO AS STATED. 2L74 4F A20WE 19951222004761995122200476NE 1995 12 22 UPS405139 219951211A7230JT9D7AH COMPRESSOR BOEING747 747121 1384871NM PWA JT9 JT9D7A 52054NE NR 2 STALLED A IPXAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO01681UP 19661 CREW REPORTED EN ROUTE TO HKG, NR 2 ENG SHUTDOWN DUE TO SEVERE COMPRESSOR STALL CLIMBING THROUGH 11,000 FEET. EGT RECORDED AT 1096 DEGREES, ENG SHUTDOWN IAW ENG SEVERE DAMAGE CHECK LIST. REMOVED AND REPLACED NR 2 ENG PER MM TC5000. OPS AND LEAK CHECK GOOD. OFF (P/N JT9D-7AH) (S/N 662911), ON (P/N JT9D-7AH) (S/N 663073). 2L74 4F4 F A20WE E20EA 19951222004771995122200477NM 1995 12 22 UPS405145 119951218A3350S135610A EEL BOEING747 747123 1384873NM CARGO DECK INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01673UP 20325 MAINTENANCE REPORTED, EMERGENCY LIGHT ON MAIN CARGO DECK INOP AT POS 3L WEAK. REMOVED AND REPLACED LIGHT MODULE AT MAIN DECK STATION 600 LT PER MM 33-51-00. 2L74 4F A20WE 19951222004781995122200478NM 1995 12 22 UPS405151 119951215A335090084 BATTERY PACK BOEING747 747123 1384873NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01672UP 20324 MAINTENANCE REPORTED, CREW SERVICE DOOR 2 EMERGENCY EXIT LIGHTS INOP AT TOP OF DOOR FRAME. REMOVED AND REPLACED BATTERY PACK. 2L74 4F A20WE 19951222004791995122200479WP 1995 12 22 UPS805146 119951217A2934 FLOAT SWITCH DOUG DC8 DC871F 302199DWP HYD SYST INOPERATIVE A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01744UP 45944 EMERGENCY HYD LEVEL LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED FLOAT SWITCH IAW MM 29-20-00. 2L74 4F RT4A25 19951222004801995122200480NM 1995 12 22 95FDEA01798 119951212A5313 STRINGER BOEING727 727232 1384082NM BS 1133-1139 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-04) ON STR 6R, BS 1133 AND BS 1139. REMOVED DAMAGED AREA AND REPAIRED STR IAW FEDEX EA 7-5310-26724. 2L73 4F A3WE 19951222004811995122200481NM 1995 12 22 95FDEA01800 119951212A5313 STRINGER BOEING727 727232 1384082NM BS 600-740 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION (C53-224-01) ON STR 5R, BS 600-740. REPAIRED OUT OF LIMITS AREA IAW FEDEX EA 7-5310-26724A. C/A ADDITION. 2L73 4F A3WE 19951222004821995122200482NM 1995 12 22 95FDEA01801 119951212A5320 BEAM BOEING727 727232 1384082NM BS 930 CORROSION A FDEAK NONE O OTHER ININSP/MAINT 1 SO25498FE 20867 CORROSION AT BS 930 BEAM LOWER CHORD LBL 46-LBL 52, WL 201. REMOVED CORROSION AT BS 930 LOWER CHORD, LBL 46-LBL 52, WL 201. AREA WITHIN LIMITS PER BAC DRAWING 65-19872-3. C/A ADDITION. 2L73 4F A3WE 19951222004831995122200483EU 1995 12 22 95FDEA01902 119951220A2612 NR 1 FIRE SQUIB AIRBUS300 A300F4605R 3930327EU NR 2 ENGINE MALFUNCTIONED A FDEAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING LDLANDING 1 SO25653FE 736 NR 2 ENGINE FIRE LIGHT, ECAM AND BELL ON LANDING AT EWR. AFTER PHASE I ITEMS COMPLETED, FIRE LIGHT CAME ON AGAIN IN HANDLE. DISCHARGED AGENT AND SECURED ENG. REMOVED AND REPLACED NR 2 ENGINE, NR 1 FIRE EXTINGUISHER BOTTLE PER MM 26-21-15, AFTER NR 1 FIRE BOTTLE REMOVED AND REPLACED, NR 1 AND NR 2 SQUIB W/N TEST. REMOVED AND REPLACED ENGINE S/O MODULE, NR 2 SQUIB TEST GOOD, NR 1 SQUIB DOES NOT TEST. REMOVED AND REPLACED NR 1 SQUIB, NR 2 FIRE DETECTION AND PROTECTION CHECKS GOOD AS PER MM. REF TO WRI 72-00/844 FOR ENGINE FIRE INSPECTION. 2L72 4F RTA35EU 19951222004841995122200484NM 1995 12 22 95FDEA01903 119951129A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 UPPER LOBE CORROSION ON FLOOR BEAM LBL 10, STA LT 480. CLEANED AND BLENDED CORROSION. CORROSION REMOVAL OUT OF LIMITS PER SRM 51-10-6. CUT OUT CORRODED AREA AND INSTALLED REPAIR ON FLOOR BEAM PER SRM 53-10-8. 2L73 4F A3WE 19951222004851995122200485NM 1995 12 22 95FDEA01904 119951205A5313 STRINGER BOEING727 727227 1384078NM BS 407 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 CRACK IN INNER FLANGE OF STR 3L, STA 407. STOP DRILLED CRACK TO .25 INCH AND INSTALLED REPAIR PART NR 1 53-10-3, PG 4D, FIG 2 (7075T6.040). 2L73 4F A3WE 19951222004861995122200486NM 1995 12 22 95FDEA01905 119951208A5313 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 UPPER LOBE STR 15L CRACKED STA 720B (AT ICE LIGHT). STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-3. 2L73 4F A3WE 19951222004871995122200487NM 1995 12 22 95FDEA01906 119951208A5313 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 UPPER LOBE STA 15L CRACKED STA 720B (AT ICE LIGHT). REPAIRED STR 15L CRACK IAW SRM 53-10-3 AND ATTACHED JOB PROGRESS FORM. 2L73 4F A3WE 19951222004881995122200488NM 1995 12 22 95FDEA01907 119951208A5313 STRINGER BOEING727 727227 1384078NM BS 720 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 MAIN CARGO STR 15R CRACKED STA 720B JUST FWD OF ICE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, PG 4D. 2L73 4F A3WE 19951222004891995122200489NM 1995 12 22 95FDEA01908 119951207A5320 BOX SUPPORT BOEING727 727227 1384078NM CARGO DOOR MISSING FASTENERA FDEAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO25486FE 21489 FORWARD CARGO DOOR HINGE BOX SUPPORT BOTH FWD AND AFT BOXES FASTENERS MISSING ON FWD AND AFT SIDE OF EACH BOX. INSTALLED FWD AND AFT WEBS AND DOUBLERS PER ESO 11782 DATED 12-07-95, EA 7-5310-26761 DATED 12-6-95. 2L73 4F A3WE 19951222004901995122200490NM 1995 12 22 95FDEA01909 119951208A5315 FLOOR BEAM BOEING727 727227 1384078NM BS 480 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 UPPER LOBE FLOOR - CORR AROUND NUTPLATE HOLE STA 480, RBL 10. REMOVED DAMAGED SECTION OF FLOOR BEAM PER SRM 51-10-6 AND INSTALLED DOUBLER REPAIR SECTIONS PER SRM 53-10-6. 2L73 4F A3WE 19951222004911995122200491NM 1995 12 22 95FDEA01910 119951208A5311 BELL FRAME BOEING727 727227 1384078NM BS 800 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 BELL FRAME IN MAIN CARGO STA 800 CRACKED AT STR 14R. STOP DRILLED CRACK, INSTALLED REPAIR PER SRM 51-40-1, PG 1. REJECTED AND BOUGHT ON NR 1207 PER 51-40-3. 2L73 4F A3WE 19951222004921995122200492NM 1995 12 22 95FDEA01911 119951208A5320 STR SPLICE BOEING727 727227 1384078NM BS 600 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25486FE 21489 FORWARD CARGO STA 680, STA 28L SPLICE END CRACKED. REMOVED STR SPLICE - FABRICATED NEW SPLICE FROM 7075T6.063. INSTALLED SPLICE PER SRM 51-10-1. 2L73 4F A3WE 19951222004931995122200493NM 1995 12 22 95UAL900327 119951219A3350 BATTERY BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE LT OVERWING DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297457U 21911 LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY. 2L73 4F4 F A3WE E2EA 19951222004941995122200494WP 1995 12 22 95UAL900328 119951219A2450 AC POWER SYST DOUG DC10 DC1030 3023501WP GE CF6 CF650C2 30018NE RIGHT MALFUNCTIONED A UALAK NONE L NO TEST CLCLIMB 1 WP291859U 47819 DURING INITIAL CLIMB AC BUS NR 3 AND ASSOCIATED LIGHTS RT EMERGENCY, AC AND RT EMERGENCY DC BUS LIGHTS CAME ON. COULD NOT RESTORE THE RT EMERGENCY BUS. FLIGHT RETURNED TO ORD. REPLACED THE GENERATOR CONTROL UNIT AND THE BUS POWER CONTROL AND RECONNECTED THE CSD. BOTH UNITS TESTED GOOD IN THE SHOP. CAUSE OF PROBLEM WAS NOT DETERMINED. 2L73 4F4 F A22WE E23EA 19951222004951995122200495WP 1995 12 22 95UAL900329 119951219A3350 STRIP DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN SAMAGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291812U 46611 EEL LIGHTS DAMAGED. REPLACED EEL LIGHT STRIP AT SEAT 5E. 2L73 4F4 F A22WE E23EA 19951222004961995122200496NE 1995 12 22 95UAL900330 219951220A7261 OIL LINE BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE NR 3 ENGINE LEAKING A UALAK NONE JK WARNING INDICATION FLUID LOSS NRNOT REPORTED 1 WP297464U 21918 696566 LANDED SJC UNDER AMBER ALERT WITH NR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE LIGHT. SUPPLEMENTAL DATA UPDATE S/D: REPLACED OIL LINE FROM OIL COOLER TO RELIEF VALVE DUE TO SMALL HOLE IN LINE. REPLACED OIL FILTER. NO METAL NOTED. 2L73 4F4 F A3WE E2EA 19951222004971995122200497NM 1995 12 22 95UAL900331 119951220A3350 STRIP BOEING737 737322 1384676NM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29368UA 24537 EMERGENCY ESCAPE PATH LIGHTING INOP AT ROW 13. REPLACED EMERGENCY ESCAPE PATH LIGHT STRIP. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951222004981995122200498NM 1995 12 22 95UAL900332 119951220A3350 STRIP BOEING737 737522 138449FNM GE CFM56 CFM56* 13802NE CABIN INOPERATIVE A UALAK NONE L NO TEST NRNOT REPORTED 1 WP29936UA 26667 AFT GALLEY EMERGENCY ESCAPE PATH LIGHT STRIP ASSEMBLY MISSING. REPLACED MISSING EMERGENCY LIGHT STRIP. CHECKS O.K. 2L72 4F4 FRTA16WE E2GL 19951222004991995122200499SO 1995 12 22 COMA9512032 119951220A27503075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAK NONE J WARNING INDICATION APAPPROACH 1 SO01164D 3006 22 120164 FLAP CONTROL FAULT, ASYMMETRY, AND DISAGREEMENT WARNINGS, ZERO FLAPS LANDING. REPLACED THE FLAP CONTROL UNIT AND ANNUNCIATOR PANEL. 2L72 4T RTA31SO 19951222005001995122200500SO 1995 12 22 COMA9512033 119951219A6123M610627023 RELAY EMB 120 EMB120RT SO AUTO FEATHER FAILED A COMAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO01179CA 120179 AUTO FEATHER AURAL WARNING DURING TAKEOFF. REPLACED THE AUTO FEATHER ARMING RELAY. 2L72 4T RTA31SO 19951222005011995122200501 1995 12 22 COMA9512034 419951219A3450DMN4171A ANTENNA EMB 120 EMB120RT SO VERT STAB DEFECTIVE A COMAO OTHER O OTHER APAPPROACH 1 SO01258CA 120247 DURING ILS APPROACH, BOTH LT AND RT CDI NEEDLES ARE DEFLECTING LEFT AND RIGHT OF CENTER. REPLACED THE TAIL NAV ANTENNAS. 2L72 4T RTA31SO 19951222005021995122200502 1995 12 22 COMA9512035 419951220A3413066500011801 IVA-81A AV EMB 120 EMB120RT SO LEFT DEFECTIVE A COMAK NONE O OTHER CRCRUISE 1 SO01205CA172 120205 THE PILOTS VSI IS COMPLETELY UNUSABLE IN ALL PHASES OF FLIGHT. REPLACED THE PILOTS TCASIVSI. 2L72 4T RTA31SO 19951222005031995122200503SO 1995 12 22 COMA9512036 119951219A27523203001005 ACTUATOR 3203001005 EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A aCOMAO OTHER J WARNING INDICATION APAPPROACH 1 SO01164D 1434612573 0733 120164 FLAP CONTROL FAULT, FLAP DISAGREEMENT, AND FLAP ASYMMETRY WARNINGS WHEN FLAPS SELECTED TO 15 DEGREES FOR LANDING APPROACH. REPLACED THE LT AND RT INBD FLAP ACTUATORS. 2L72 4T RTA31SO 19951222005041995122200504EU 1995 12 22 COMA9531217 119951219A3020ND00752200 CONTROLLER SAAB SF340 SF340A 7850100EU LT ENGINE DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01356CA2369 74 340A034 LEFT INTAKE HEAT IS INOP. REPLACED THE LT ENGINE INTAKE HEAT CONTROLLER. 2L72 4T RTA52EU 19951222005051995122200505EA 1995 12 22 COMA9560624 119951220A2750 RETRACT MECH CNDAIRCL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01932CA 7038 FLAPS FAILED AT ZERO DEGREES WHEN SELECTED FOR LANDING APPROACH. COULD NOT DUPLICATE - NO FAULTS FOUND IN FLAP COMPUTER. 2L72 4F RTA21EA 19951222005061995122200506EA 1995 12 22 COMA9560625 119951220A2750860D10018A ECU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION LDLANDING 1 SO01941CA782 1 7050 FLAP FAIL MESSAGE ON EICAS ZERO FLAPS LANDING. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19951222005071995122200507NM 1995 12 22 DL72L954738 119951219A215032167431 PACK VALVE BOEING727 727232 1384082NM RT PACK MALFUNCTIONED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27509DA 21311 A/C WOULD NOT MAINTAIN PRESSURIZATION WITH SINGLE PACK. OPS CARGO HEAT VALVE CLOSED. REPLACED RT FWD PACK VALVE. REPLACED EQUIPMENT COOLING. SHUT OFF VALVE. PRESSURIZED A/C. CKS NORMAL. 2L73 4F A3WE 19951222005081995122200508NM 1995 12 22 DL72S954733 119951219A3530 PBE 4566M37B BOEING727 727232 1384082NM CABIN DEFECTIVE A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO27541DA 22387 PBE, LOCATED IN FIRST CLASS COAT CLOSET, HAS UNSERVICEABLE INDICATOR PROTRUDING PAST CONTAINER. REPLACED PBE. 2L73 4F A3WE 19951222005091995122200509NM 1995 12 22 DL72W954736 119951219A5754 ANGLE BOEING727 727247 138408FNM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27297WA 22534 NR 2 SLAT COVE SKIN ATTACH ANGLE AT TAI DUCT. PREVIOUS REPAIR DOUBLER CRACKED .25 INCH. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER 57-54-0. 2L73 4F A3WE 19951222005101995122200510NM 1995 12 22 DL72W954737 119951219A2612 BULB 387 BOEING727 727247 138408FNM NR 1 ENGINE FAILED A DALAK NONE J WARNING INDICATION ININSP/MAINT 1 SO272815W 20871 ENGINE FIRE TEST CAUSES NR 1 ENG A/B FIRE DETECTION CIRCUIT BREAKER TO TRIP. REPLACED ENG FIRE TEST PANEL. REPLACED FIRE DET MOD. NO HELP. REPLACED FAULT BULB IN FIRE HANDLE. SYSTEM NOW CKS NORMAL. 2L73 4F A3WE 19951222005111995122200511NM 1995 12 22 DLM88954742 119951219A3222 STRUT DOUG MD88 MD88 3023688NM NLG UNDERSERVICED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27944DL 49817 ON TAKEOFF FROM LGA, UPON GEAR RETRACTION, RED NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR TO NO SATISFACTION. CONCURRENTLY LOST AUTO PRESSURIZATION, TRANSPONDER AND HAD STALL IND FAILURE AND AUTO SPOILER FAIL MSGS ON OAP. DIVERTED TO JFK. SERVICED NOSE GEAR STRUT PER 32-21-02. PERFORMED BITE OF PROX BOX, SHOWS NO FAULT. CABLE-TO-GROUND CONTROL RELAY OK. 2L72 4F RTA6WE 19951222005121995122200512NM 1995 12 22 SCNA95294 119951218A3350S106 BATTERIES BOEING727 727259 138408JNM L-1 DOOR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15289SC 22475 THE OVERHEAD L-1 DOOR PORTABLE EMERGENCY EXIT LIGHT ILLUMINATES MOMENTARILY THEN GOES OUT. REMOVED AND REPLACED BATTERIES IAW MM 33-50-101, LIGHT OPS CHECKED GOOD. 2L73 4F A3WE 19951222005131995122200513NM 1995 12 22 SCNA95295 119951213A5347BAC1520792 SEAT TRACK BOEING727 727227 1384078NM BS 1050-1070 CORRODED A SCNAK NONE O OTHER ININSP/MAINT 1 GL15275AF 22092 DURING SCHEDULED INSPECTION, CORROSION WAS FOUND ON SEAT TRACK AT STATION 1050-1070, RBL 20. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS. FABRICATED, INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-05, 51-10-12, 51-20-02, 51-10-05, 51-10-03. 2L73 4F A3WE 19951222005201995122200520SW 1995 12 22 95ZZZX6847 119951108A6230206101335001 LEVER ASSY 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032758L1347 45266 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 1346.5 HOURS. 1G71 3U H2SW 19951222005211995122200521SW 1995 12 22 95ZZZX6848 119951108A6230206010336005 LINK IDLER 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW032758L1347 45266 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 1346.5 HOURS. 1G71 3U H2SW 19951222005301995122200530SW 1995 12 22 95ZZZX6857 119951108A6230206010335001 LEVER ASSY 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW035756N645 45546 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 645.2 HOURS. 1G71 3U H2SW 19951222005311995122200531SW 1995 12 22 95ZZZX6858 119951108A6230206010336005 LINK IDLER 206010350021BELL 206 206L1 1182107SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW035756N645 45546 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 645.2 HOURS. 1G71 3U H2SW 19951222005321995122200532SW 1995 12 22 95ZZZX6859 119951108A6230206010335001 LEVER ASSY 206010350021BELL 206 206L3 1182108SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW03359AL478 51461 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 478.1 HOURS. 1G71 3U H2SW 19951222005331995122200533SW 1995 12 22 95ZZZX6860 119951108A6230206010336005 LINK IDLER 206010350021BELL 206 206L3 1182108SW PYLON WORN B ALGRK NONE O OTHER ININSP/MAINT 1 SW03359AL478 51461 DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 478.1 HOURS. 1G71 3U H2SW 19951226000011995122600001WP 1995 12 26 MWEA95444 119951208A53203915134515N FITTING DOUG DC9 DC932 3022066WP BS 756 CORRODED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING D-CHECK, FOUND LT AFT KEEL AT STA 756, LONGERON 30L HAS A CORRODED END FITTING. 2L72 4F A6WE 19951227000011995122700001NE 1995 12 27 P5CA9500865 219951206A75307479555 EVC BOEING747 747122 1384872NM PWA JT9 JT9D7A 52054NE NR 4 ENGINE FAILED A P5CAE ENGINE SHUTDOWN JY WARNING INDICATION ENGINE STOPPAGE CRCRUISE 1 WP23852FT 1388 19757 662276 NR 4 ENGINE SHUT DOWN IN-FLIGHT WITH LOW OIL QTY AND OIL PRESSURE LIGHT ON. OIL PRESSURE DROPPED TO 37 PSI WITH ALL OTHER INDICATIONS NORMAL. ENGINE WINDMILLED FOR 2 HOURS. REPLACED NR 4 EVC IAW MM 75-31-01. ALSO, REPLACED EVC ACTUATOR, P/N 719999-6, S/N 6050074, IAW 75-31-02. OPS AND LEAK CHECK GOOD. 2L74 4F4 F A20WE E20EA 19951228000011995122800001NE 1995 12 28 UPS604852 219951023A7314 FUEL PUMP BOEING767 76734AF 1385212NM GE CF6 CF680C2B2 30025NE RT ENGINE FAILED A IPXAO OTHER X ENGINE FLAMEOUT DEDESCENT 1 SO01302UP 27240 CREW REPORTED, RT ENGINE FLAMED-OUT AT TOP OF DESCENT. INFLIGHT START ATTEMPT UNSUCCESSFUL DUE TO NO FUEL FLOW. MAINTENANCE REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01. 2L72 4F4 FRTA1NM E13NE 19951228000021995122800002EU 1995 12 28 DLL14954110 219951026A7314PAC102MK4 FUEL PUMP LKHEED1011 1011385115 5265015WP RROYCERB211 RB211524B4D 54555EU NR 2 ENGINE FAILED A DALAA UNSCHED LANDING XJ ENGINE FLAMEOUT WARNING INDICATION CRCRUISE 1 SO11740DA 193C1244 014717 NR 2 ENGINE FLAMED OUT AT FL 370. LANDED ATL WITHOUT INCIDENT. REPLACED ENGINE DRIVEN FUEL PUMP AND FFR. OPERATION NORMAL. 2L73 4F4 F A23WE E21EU 19951228000031995122800003EU 1995 12 28 DLL16954272 219951107A732044A2562 SWITCH LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4D 54555EU NR 2 ENGINE INOP A DALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO11762DA 193Y1210 014764 ATL - ON CLIMBOUT, NR 2 ENG WOULD NOT DEVELOPE CLIMB POWER. REPLACED ALTITUDE PRESS SWITCH. 2L73 4F4 F A23WE E21EU 19951228000051995122800005EU 1995 12 28 DLL16954336 219951111A7220RB211524B4I SPINNER LKHEED1011 10113853 5265020WP RROYCERB211 RB211524B4D 54555EU NR1 ENGINE LOOSE A DALAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SO11763DL51520 193Y1197 014614 NR 1 ENG HIGH VIB STARTED AT 2.5, THEN UP TO 4.0, NORMAL AT IDLE. VIBS FELT IN FLT DECK, NR 1 ENG SHUTDOWN AT FL 310. LANDED WITHOUT FURTHER INCIDENT. FOUND FAIRING ATTACHMENT AT SPINNER BROKEN. REPLACED SPINNER AND FAIRING, CKD CHIP DETECTORS, BORESCOPED 7TH STAGE IPC, 1ST STAGE HPT. REPLACED OIL FILTER LUBED FAN, RAN PER PFHB TEST 11 AND CKS GOOD. 2L73 4F4 F A23WE E21EU 19951228000061995122800006NM 1995 12 28 TSAA9521177 119950921A5230 SEAL BOEING737 7372Y5 1384554NM AFT CARGO DOOR BLOWN A TSAABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP13810AL 24031 KOA/HNL - FLT 481 - PILOT REPORT: 4 LOUD THUMPS FOLLOWED BY LOSS OF PRESSURIZATION AT FL 220. BEGAN DESCENT AND DECLARED EMERGENCY. LANDING UNEVENTFUL. POST-FLIGHT INSPECTION SHOWS AFT CARGO DOOR SEAL BLOWN OUT. MAINTENANCE REPLACED AFT CARGO DOOR SEAL. LEAK AND PRESSURIZATION CHECK OK. (X) 2L72 4U RTA16WE 19951228000071995122800007NM 1995 12 28 UPS405107 119951120A5512 PANEL BOEING747 747123 1384873NM RT HORIZ STAB CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE ON GROUND, MAINTENANCE FOUND RT HORIZ STAB T/E CRACKED AT NAV LIGHT AREA. ACCOMP COMPOSITE REPAIR PER SRM 51-40-09. 2L74 4F A20WE 19951228000081995122800008NM 1995 12 28 UPS405108 119951120A5753 SKIN BOEING747 747123 1384873NM RT TE MIDFLAP CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01673UP 20325 WHILE ON GROUND, MAINTENANCE FOUND RIGHT WING I/B MIDFLAP, O/B EDGE APPEARS TO HAVE A 3 INCH CRACK. AREA MARKED WITH RED TAPE. ACCOMPLISHED COMPOSITE REPAIR PER SRM 51-40-09. 2L74 4F A20WE 19951228000091995122800009NM 1995 12 28 UPS405117 119951126A5753 TE SKIN BOEING747 747123 1384873NM TE MIDFLAP DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01676UP 20101 WHILE ON GROUND, MAINTENANCE FOUND RT WING INBOARD MID-FLAP TRAILING EDGE OUTBOARD SECTION DELAMINATED. PERFORMED INTERIM REPAIR PER SRM 51-05, PG 21. 2L74 4F A20WE 19951228000101995122800010NE 1995 12 28 SIMA952951 219951022A7313STE3367009 O-RING AEROSPATR72 ATR72212 EU PWA PW120 PW124B NE NR 12 FUEL NOZZ LEAKING A SIMAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 SW21349AT 349 DFW - FLT 3864 - IN CRUISE FLIGHT THE NR 2 ENGINE POWER DROPPED OFF TO 40 PERCENT AND STABILIZED. FEATHERED PROP AND CONTINUED TO DFW WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION REVEALED FUEL LEAK FROM NR 12 FUEL NOZZLE TRANSFER TUBE O-RING. REPLACED ALL FUEL NOZZLES AND O-RINGS WITH NEW. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E2ONE 19951228000111995122800011NM 1995 12 28 DL72S954604 119951202A49008598CK APU BOEING727 727232 1384082NM CABIN SMOKING A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27541DA 22387 DEPARTURE TIME WITH APU, EITHER PACK PUTS SMOKE IN CABIN. FOUND APU PUTTING SMOKE IN CABIN DEACTIVATED APU PER MEL. 2L73 4F A3WE 19951228000121995122800012WP 1995 12 28 DLL10954605 119951202A2910 HYD LINE 290023500 LKHEED1011 10113851 5265010WP C-HYD SYSTEM LEAKING A DALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27721DA 193C1139 C-SYSTEM HYD QUANTITY DECREASED TO BELOW HALF FULL. TURNED OFF C-SYS PUMPS. FOUND LINE ABOVE C-SYSTEM RETURN FILTER LEAKING. REPLACED LINE, OPERATION NORMAL. 2L73 4F A23WE 19951228000131995122800013NM 1995 12 28 UPS205123 119951130A3270 ACT CONNECTOR BOEING727 727185C 138406NNM TAIL SKID DIRTY A IPXAO OTHER J WARNING INDICATION CLCLIMB 1 SO01940UP 19826 CREW REPORTED, TAIL SKID WOULD NOT RETRACT. RECYCLED GEAR, TAIL SKIRT THEN CAME UP. CLEANED CONNECTION ON TAIL SKID ACTUATOR, CHECK OK IAW 32-71-01 PAGE 501. 2L73 4F A3WE 19951228000141995122800014NM 1995 12 28 UPS405125 119951203A5730 SKIN BOEING747 747123 1384873NM LT WING LE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01674UP 20100 WHILE ON GROUND, MAINTENANCE FOUND LEFT WING L/E INBOARD OF NR 2 PYLON HAS DELAMINATION. ACCOMPLISHED COMPOSITE REPAIR REF: SRM 51-40-09. 2L74 4F A20WE 19951228000151995122800015NE 1995 12 28 WWMA9500085 219951130A73108346 FUEL PRESS SW SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE RT ENGINE LEAKING A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP15247AE 340B247 CREW REPORTED, AFTER START FUEL WAS POURING OUT OF THE RIGHT ENGINE FORWARD DRAIN TUBE UNTIL THE ENGINE WAS SHUTDOWN. PASSENGERS WERE EVACUATED DUE TO FUEL SMELLS IN THE CABIN. UPON INVESTIGATION MAINTENANCE REPLACED THE RIGHT ENGINE HMU FUEL LINE AND THE RIGHT STANDBY FUEL PRESSURE SWITCH. NO LEAKS NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4T4 TRTA52EU E8NE 19951228000161995122800016NM 1995 12 28 UPS805129 119951202A5412 FIREWALL SPLICE BOEING747 747123 1384873NM PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01677UP 20391 WHILE ON GROUND, MAINTENANCE FOUND PYLON CRACKED HORIZONATAL FIREWALL SPLICE. MRR FILED OPEN. 2L74 4F A20WE 19951228000171995122800017NM 1995 12 28 UPS405134 119951203A5730 SKIN BOEING747 747123 1384873NM LT WING LE DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01674UP 20100 MAINTENANCE REPORTED LEFT WING L/E BEHIND LANDING LIGHT HAS DELAMINATION. REPAIRED IAW SRM 51-40-09. 2L74 4F A20WE 19951228000181995122800018NM 1995 12 28 UPS405135 119951203A5414 SKIN BOEING747 747123 1384873NM NR 2 PYLON DELAMINATED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01674UP 20100 MAINTENANCE REPORTED LEFT WING L/E INBOARD OF NR 2 PYLON HAS DELAMINATION. REPAIRED IAW SRM 51-40-09. 2L74 4F A20WE 19951228000191995122800019NM 1995 12 28 UPS405137 119951209A3350 EEL BOEING747 747123 1384873NM COCKPIT INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 MAINTENANCE REPORTED FORWARD LT SIDE EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. DEFERRED DOOR PER MEL 33-13, DEACTIVIATED PER 25-11. MRR FILED OPEN PENDING MX CORRECTIVE ACTION. 2L74 4F A20WE 19951229000011995122900001WP 1995 12 29 9520761211 119951123A5320 DOOR FRAME DOUG DC10 DC1030 3023501WP FS 1708 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01211NW 46868 DURING LINE CHECK, FOUND CORROSION ON THE CENTER CARGO DOOR JAMB LOWER FORWARD FRAME, FS 1708 AT LONGERON 41R. REPAIRED FRAME (P/N AFA 3873-3) PER EA 12-99308. 2L73 4F A22WE 19951229000021995122900002WP 1995 12 29 9520779106 119951125A5330 SKIN DOUG DC9 DC915 3022036WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0196S 47206 DURING H-CHECK FOUND (2) CRACKS, .1250 INCH AND .3125 INCH, IN THE FUSELAGE SKIN AFT OF THE MCD, FS 200. REPAIRED SKIN (P/N 5911406-5, -59) PER EA 91-103341. 2L72 4F A6WE 19951229000031995122900003NM 1995 12 29 9520785503 119951129A5320 CHORD BOEING757 757251 1384970NM FS 1380-1440 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01503US 23192 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO DOOR LOWER SILL INNER CHORD, BS 1380-1440. REPAIRED SILL (P/N 146N8522-51) PER EA 55-105061. 2L72 4F RTA2NM 19951229000041995122900004NM 1995 12 29 9520795503 119951129A5347 SEAT TRACK BOEING757 757251 1384970NM FS 898 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01503US 23192 DURING T-CHECK, FOUND A CRACK IN THE RBL 45 LONGITUDINAL FLOOR BEAM SEAT TRACK UPPER CHORD AT BS 898. REPAIRED CHORD (P/N 111N5207-5) PER EA 55-105062. 2L72 4F RTA2NM 19951229000051995122900005NM 1995 12 29 9520806633 119951130A5347 SEAT TRACK BOEING747 747227B 1384888NM FS 1265-1318 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01633US 21991 DURING PCK, FOUND CORROSION IN THE CROWNLESS SEAT TRACK, LBL 11.33, BS 1265-1318. REPAIRED TRACK (P/N 65B 23464-7) PER EA 66-104417. 2L74 4F A20WE 19951229000061995122900006WP 1995 12 29 9520819857 119951201A5220 DOOR PAN DOUG DC9 DC951 3022051WP EMER EXIT DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01766NC 47739 DURING H-CHECK, FOUND CRACKS IN (2) EMERGENCY EXIT DOOR PANS (RIGHT AFT, LEFT FORWARD), ONE EACH AT THE UPPER FORWARD AND AFT DOOR STOPS. REPAIRED THE PANS (P/N 5913195-1) PER EAS 98-103345 AND -103347. 2L72 4F A6WE 19951229000071995122900007NM 1995 12 29 9520825503 119951201A5542173N210233 SKIN BOEING757 757251 1384970NM RUDDER DELAMINATION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01503US 23192 DURING T-CHECK, FOUND DELAMINATION IN THE RUDDER TRAILING EDGE SKIN, LEFT SIDE STATION 153. REPAIRED SKIN (P/N 173N2102-33) PER EA 55-103371. 2L72 4F RTA2NM 19951229000081995122900008NM 1995 12 29 9520845503 119951202A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 1681 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01502US 23192 DURING T-CHECK, FOUND CORROSION ON THE AFT CARGO BS 1681 FLOOR BEAM FORWARD UPPER CHORD, LBL 52-RBL 14. REPAIRED CHORD (P/N 146N5091) PER EA 55-105068. 2L72 4F RTA2NM 19951229000091995122900009WP 1995 12 29 9520859139 119951202A5320 JAMB DOUG DC9 DC914 3022034WP SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01948L 470479 DURING LINE CHECK, FOUND APPROX 1.4375 INCH CRACK IN THE FORWARD SERVICE DOOR JAMB LOWER AFT CORNER. REPAIRED JAMB (P/N 5911407-33) PER EA 91-104980. 2L72 4F A6WE 19951229000101995122900010WP 1995 12 29 9520869972 119951205A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP DOOR JAMB CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019336 47338 DURING LINE CHECK, FOUND CORROSION ON THE FORWARD AIRSTAIR CUT OUT LOWER DOOR JAMB INTERCOSTAL. REPAIRED INTERCOSTAL (P/N 9957839-3) PER EA 99-103384. 2L72 4F A6WE 19951229000111995122900011EU 1995 12 29 9520873213 119951206A5313 LONGERON AIRBUS320 A320211 3930320EU FS 14300-14834 CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01313US 153 DURING 1C1 MAINTENANCE VISIT, FOUND CORROSION ON STRINGER 41R BETWEEN FRAMES 33-34. REPAIRED STRINGER PER EA 32-104389. 2L72 4F RTA28NM 19951229000121995122900012WP 1995 12 29 9520881220 119951206A5730 SKIN DOUG DC10 DC1030 3023501WP WING CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01220NW 46577 DURING M-CHECK, FOUND A CRACK IN THE RIGHT WING LEADING EDGE SKIN AFT OF NR 3 SLAT AT THE UPPER INBOARD CORNER OF THE ANTI-ICE DUCT CUT OUT. REPAIRED SKIN PER EA 12-103235. 2L73 4F A22WE 19951229000131995122900013WP 1995 12 29 9520891220 119951206A5753 SKIN DOUG DC10 DC1030 3023501WP LT TE FLAP DELAMINATED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01220NW 46577 DURING M-CHECK, FOUND DELAMINATION IN THE LEFT WING INBOARD FLAP UPPER SKIN. REPAIRED SKIN (P/N ARC2369-503) PER EA 12-103872. 2L73 4F A22WE 19951229000141995122900014WP 1995 12 29 9520909972 119951206A5320 JAMB DOUG DC9 DC931 3022065WP AIRSTAIR DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019336 47338 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD AIRSTAIR DOOR JAMB, AFT LOWER CORNER. REPAIRED JAMB PER EA 99-103377. 2L72 4F A6WE 19951229000151995122900015WP 1995 12 29 9520919106 119951208A5744 HINGE FITTING DOUG DC9 DC915 3022036WP LT TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0196S 47206 DURING H-CHECK, FOUND CORROSION IN THE LEFT FLAP, NR 2 AND NR 3 FORWARD HINGES. REPLACED BOTH HINGE FITTINGS (P/N 5912479-501) PER CITEXT 09-5740-9800. 2L72 4F A6WE 19951229000161995122900016NM 1995 12 29 9520926633 119951208A5400 SPAR WEB BOEING747 747227B 1384888NM NR 3 PYLON CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01633US 21991 DURING PCK, FOUND A CRACK IN THE NR 3 PYLON MID-SPAR WEB, STATION 301. REPAIRED WEB (P/N 65B90421) PER EA 66-104418. 2L74 4F A20WE 19951229000171995122900017WP 1995 12 29 9520939152 119951211A5720 CLIPS DOUG DC9 DC914 3022034WP WS 111 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018911E 45825 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STATION 69 RIB TO STRINGER LOWER ATTACH CLIPS BETWEEN STRINGERS 15-17 AND A CRACK IN THE LEFT WING STATION 111 LOWER ATTACH CLIP BETWEEN THE AFT SPAR AND STRINGER 11. REPLACED CLIPS PER EA 91-102349. 2L72 4F A6WE 19951229000181995122900018WP 1995 12 29 9520949160 119951211A5713 LONGERON DOUG DC9 DC914 3022034WP RT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON RIGHT WING STRINGERS 18 AND 20-21. REPAIRED STRINGERS PER EA 91-102348. 2L72 4F A6WE 19951229000191995122900019NM 1995 12 29 9520955512 119951212A5315 FLOOR BEAM BOEING757 757251 1384970NM FS 365 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01512US 23200 DURING PCK, FOUND CORROSION ON THE BS 365 FLOOR BEAM UPPER CHORD, LBL 60 - RBL 60. REPAIRED CHORD (P/N 141N5112) PER EA 55-104346. 2L72 4F RTA2NM 19951229000201995122900020WP 1995 12 29 9520969152 119951212A5713 LONGERON DOUG DC9 DC914 3022034WP WS 91-111 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018911E 45825 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON THE LEFT WING STRINGER 12 LOWER FLANGE BETWEEN WS 91-111. REPAIRED STRINGER PER EA 91-104032. 2L72 4F A6WE 19951229000211995122900021WP 1995 12 29 9520979160 119951212A5720 CLIP DOUG DC9 DC914 3022034WP WS 69 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION AND CRACKS IN THE WS 69 WING RIB TO STRINGER ATTACH CLIPS BETWEEN STRINGERS 14-17, AND BETWEEN STRINGER 11 AND THE RIGHT SPAR. REPLACED CLIPS PER EA 91-102344, -102346. 2L72 4F A6WE 19951229000221995122900022WP 1995 12 29 9520989857 119951213A5320 FLOOR SUPPORT DOUG DC9 DC951 3022051WP FS 636-737 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01766NC 47739 DURING H-CHECK, FOUND A CRACK ON THE FUSELAGE FLOOR SUPPORT VERTICAL WEB, FS 636-737. REPAIRED SUPPORT (P/N 5910740-13) PER EA 98-102007. 2L72 4F A6WE 19951229000231995122900023WP 1995 12 29 9520999152 119951213A5720 TRAPEZOIDAL FTG DOUG DC9 DC914 3022034WP RT REAR SPAR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018911E 45825 DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE RIGHT REAR SPAR TRAPEZOIDAL ATTACH FITTING. REPLACED FITTING (P/N 3912073-502) PER EM 5710-00028, SECTION 07-B. 2L72 4F A6WE 19951229000241995122900024WP 1995 12 29 9521009160 119951213A5713 LONGERON DOUG DC9 DC914 3022034WP LT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018903E 45744 DURING SPECIAL MAINTENANCE VISIT, FOUND CORROSION ON LEFT WING STRINGERS 19-20. REPAIRED STRINGERS PER EA 91-104027. 2L72 4F A6WE 19951229000251995122900025WP 1995 12 29 9521019969 119951214A5330 SKIN DOUG DC9 DC931 3022065WP FS 370 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR JAMB SKIN, UPPER FORWARD CORNER FS 370. REPAIRED DOOR JAMB SKIN PER EA 99-103407. 2L72 4F A6WE 19951229000261995122900026WP 1995 12 29 9521029104 119951216A5313 LONGERON DOUG DC9 DC915 3022036WP FS 477-480 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194US 47204 DURING H-CHECK, FOUND CRACKS IN BOTH LONGERON 27L AND 28R END FITTINGS AT FS 477-480. REPLACED BOTH END FITTINGS PER SRM 51-30-2. 2L72 4F A6WE 19951229000271995122900027WP 1995 12 29 9521039104 119951217A5312 BLKHD FTG DOUG DC9 DC915 3022036WP RT LAV CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194US 47204 DURING H-CHECK, FOUND A CRACK IN THE RIGHT LAV FORWARD BULKHEAD, LOWER AFT INBOARD FITTING. REPLACED FITTING PER SRM 51-30-5. 2L72 4F A6WE 19951229000281995122900028WP 1995 12 29 9521049104 119951219A5320 LONGERON DOUG DC9 DC915 3022036WP FS 761-801 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194US 47204 DURING H-CHECK, FOUND CORROSION ON LONGERON 22R FROM FS 761-801. REPLACED LONGERON AND END FITTING PER SRM 53-02 FIG 2A. 2L72 4F A6WE 19951229000291995122900029NM 1995 12 29 9521055524 119951219A3397 WIRE BOEING757 757251 1384970NM CABIN SHORTED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01524US 23618 EMERGENCY LIGHTS ILLUMINATE WITH SWITCH IN THE ARMED POSITION. MAINTENANCE RESET CANNON PLUG. THEN EMERGENCY LIGHTS AT DOOR 3L AND 3R ILLUMINATED WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACK. FINALLY, AFT CABIN EMERGENCY LIGHTS ILLUMINATED IN FLIGHT. MAINTENANCE FOUND WIRE NR W03050003-20 SHORTED TO GROUND AT P62 PANEL. REPAIRED WIRE. 2L72 4F RTA2NM 19951229000301995122900030NM 1995 12 29 9521065502 119951216A2410729825C IDG BOEING757 757251 1384970NM NR 1 FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TOTAKEOFF 1 GL01502US247865470 23191 DURING TAKE-OFF, NR 1 GENERATOR DROPPED OFF LINE. ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED THE NR 1 IDG AND CANNON PLUG D5132. OPERATIONAL AND LEAK CHECK NORMAL. 2L72 4F RTA2NM 19951229000311995122900031NM 1995 12 29 9521075635 119951221A2120 AIR DISTR BOEING757 757251 1384970NM FLIGHT DECK SMOKE A NWAAAB UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL01535US 26482 DURING CRUISE FLIGHT, VISUALLY NOTED AND SMELLED ELECTRICAL SMOKE IN FLIGHT DECK. INITIATED EMERGENCY DESCENT, DONNED OXYGEN MASKS, AND DECLARED AN EMERGENCY WITH ATC. UPON COMPLETION OF CHECK LIST PROCEDURE, SMOKE DISSIPATED. DIVERTED TO MLI AND LANDED WITHOUT FURTHER INCIDENT. FIRE RESCUE FOLLOWED AIRCRAFT TO THE GATE WHERE PASSENGERS DEPLANED NORMALLY. COMPLETED INSPECTION OF THE AIRCRAFT WITH NO ABNORMALITIES NOTED. MAINTENANCE PERFORMED MULTIPLE INSPECTIONS OF SUSPECT COMPONENTS, TO NO AVAIL. INVESTIGATION CONTINUES. 2L72 4F RTA2NM 19951229000321995122900032NM 1995 12 29 9521086307 119951219A3350 PINS BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01667US 24222 DURING LINE CHECK, THE FLOOR PATH EMERGENCY LIGHT BETWEEN SEAT ROWS 26L AND 31L AND 53L TO 58L WERE FOUND INOPERATIVE. RECONNECTED SEAT PINS IN FLOOR TRACK AT ROWS 26L AND 58L, OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19951229000331995122900033WP 1995 12 29 9521099857 119951127A5350 RELEASE MECH DOUG DC9 DC951 3022051WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01766NC 47739 DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LEFT LATCH DURING THE DROP CHECK. ADJUSTED THE CLIPS AND MODIFIED THE TAILCONE RELEASE CABLE LOCKING FITTING PER CITEXT 09-5353-1-0003. CHECKED OK. 2L72 4F A6WE 19951229000341995122900034WP 1995 12 29 9521109307 119951215A5350 LATCHES DOUG DC9 DC982 3022082WP TAILCONE OUT OF ADJUST A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING P-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE USING THE INTERIOR HANDLE. LUBRICATED THE LOCKING PINS AND ADJUSTED THE LATCHES. CHECKED OK. 2L72 4F A6WE 19951229000351995122900035WP 1995 12 29 9521119986 119951215A3260 TARGET DOUG DC9 DC932 3022066WP LT MLG DOOR OUT OF ADJUST A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01986US 47480 DURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. ADJUSTED LEFT MAIN LANDING GEAR DOOR TARGET FOR SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229000361995122900036WP 1995 12 29 9521129952 119951218A2421 GENERATOR DOUG DC9 DC932 3022066WP RT ENGINE FAILED A NWAAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 GL019347 45827 DURING CRUISE, THE RIGHT AC BUS, RIGHT GENERATOR, AND DC BUS OFF LIGHTS ILLUMINATED. THE RIGHT DC BUS WAS RESTORED BY DC BUS CROSSTIE. AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RIGHT CONSTANT SPEED DRIVE, GENERATOR CONTROL PANEL, AND ENGINE GENERATOR. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229000371995122900037NE 1995 12 29 9521139980 219951219A7510 FUEL HEAT VLV DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL019344 47440 649148 NR 1 ENGINE EXPERIENCED UNCOMMANDED OPERATION OF THE FUEL HEAT SYSTEM DURING CLIMB OUT. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL HEAT VALVE WITH A SERVICEABLE UNIT. 2L72 4F4 F A6WE E2EA 19951229000381995122900038WP 1995 12 29 9521149991 119951220A3260 DNLOCK SW DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018957E 47215 DURING CLIMB, THE NOSE LANDING GEAR GREEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR. LIGHT REMAINED ILLUMINATED AND THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ALSO ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWN AND LOCKED SWITCH. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229000391995122900039EU 1995 12 29 9521153204 119951220A2611 SMOKE DET AIRBUS320 A320211 3930320EU CARGO COMPT MALFUNCTIONED A NWAAF ACTIVATE FIRE EXT. N FALSE WARNING TXTAXI/GRND HDL 1 GL01304US 040 DURING ENGINE START, RECEIVED 'SMOKE AFT CARGO SMOKE' WARNING. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DISCHARGED FIRE BOTTLE, RETURNED TO GATE AND DEPLANED PASSENGERS. MAINTENANCE INSPECTION REVEALED NO EVIDENCE OF FIRE OR SMOKE. 2L72 4F RTA28NM 19951229000401995122900040NM 1995 12 29 95FDEA01912 119951221A2782 ACTUATOR BOEING727 72727C 138400JNM NR 5 LE FLAP MALFUNCTIONED A FDEAA UNSCHED LANDING J WARNING INDICATION TXTAXI/GRND HDL 1 SO25145FE 19109 WHEN RETRACTING FLAPS TO A 2 DEGREE POSITION AFTER TAKEOFF, NR 5 LED REMAINED EXTENDED, FLAPS POSITIONED TO 5 DEGREES NORMAL LED EXTENSION, FLAPS TO 2 DEGREE POSITION REMAINED EXTENDED. REMOVED AND REPLACED NR 5 L/E FLAP ACTUATOR. OPS AND LEAK CHECKS NORMAL PER MM 27-81-22. 2L73 4F A3WE 19951229000411995122900041WP 1995 12 29 95UAL900333 119951221A3350 BATTERY DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291824U 46623 EMERGENCY LIGHTS TEST FAILED ON AFT BATTERY PACK. REPLACED BATTERY. 2L73 4F4 F A22WE E23EA 19951229000421995122900042NM 1995 12 29 95UAL900334 119951221A3350 LIGHT BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP297450U 21904 EEL LIGHT ON FLOOR BY R0W 14C IS INOPERATIVE. SECURED LIGHT. 2L73 4F4 F A3WE E2EA 19951229000431995122900043NM 1995 12 29 95UAL900335 119951221A2782 ACTUATOR RONSON 10605582 BOEING727 727222 1384073NM NR 2 LE FLAP FAILED A UALAO OTHER J WARNING INDICATION CLCLIMB 1 WP297268U 8772DFGKL 21415 AFTER TAKEOFF THE NR 2 LEADING FLAP STUCK IN THE EXTENDED POSITION. CYCLED FLAPS, NO HELP AND RETURNED TO TPA. WORN INTERNAL ACTUATOR SEALS CAUSED THE NR 2 LEADING EDGE FLAP TO STICK. REPLACED ACTUATOR. 2L73 4F A3WE 19951229000441995122900044NM 1995 12 29 95UAL900336 119951221A2130 PRESSURIZATION BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE CABIN MALFUNCTIONED A UALAK NONE O OTHER CLCLIMB 1 WP297443U 21897 PRESSURIZATION PANEL PROPERLY CONFIGURED ON TAKEOFF. AFTER TAKEOFF, AUTO FAIL LIGHT ON. WENT TO STANDBY AND NOTHING HAPPENED. WENT TO MANUAL AC-DC AND NOTHING HAPPENED. DIVERTED TO IAD. 2L73 4F4 F A3WE E2EA 19951229000451995122900045WP 1995 12 29 95UAL900337 119951222A3350 POWER LEAD DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291831U 46630 LEFT SIDE C-ZONE EEL LIGHTS INOPERATIVE DURING POWER LOSS WITH LIGHTS ARMED. REPLACED LEFT AFT POWER LEAD. 2L73 4F4 F A22WE E23EA 19951229000461995122900046NM 1995 12 29 95UAL900338 119951222A3350 BATTERY PACK BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29503UA 24624 EMERGENCY LIGHTS IN BULLNOSE AT ROWS 30 AND 33 GO OUT AFTER 30 SECONDS. BATTERY PACK LOW. REPLACED BATTERY PACK. 2L72 4F4 FRTA2NM E17NE 19951229000471995122900047NM 1995 12 29 95UAL900339 119951222A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29183UA 25379 EMERGENCY LIGHT AT DOOR 5 CEILING INOP. LAMP BURNED OUT. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 19951229000481995122900048WP 1995 12 29 SCNA95296 119951214A2612ASL0387503 FIRE LOOP DOUG DC10 DC1010 3022110WP NR 2 ENGINE INTERMITTENT A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15572SC 46977 THE NR 2 ENGINE A-SYSTEM FIRE DETECTION LOOP FLICKERED DURING CLIMB. ALL OTHER ENGINE PARAMETERS WERE NORMAL. INSPECTED NR 2 A-SYSTEM LOOP AND NO DISCREPANCIES WERE NOTED. 2L73 4F A22WE 19951229000491995122900049NM 1995 12 29 UPS05154 119951221A2612 FIRE DET BOEING747 747121 1384871NM CARGO COMPT MALFUNCTIONED A IPXAO OTHER N FALSE WARNING CRCRUISE 1 SO01690UP 20348 LOWER CARGO AFT FIRE LIGHT FLICKERED MOMENTARILY. LOWER AFT CARGO FIRE DETECTOR TEST NORMAL. NO PROBLEM AFTER FLICKER. 2L74 4F A20WE 19951229000661995122900066NM 1995 12 29 95ZZZX6926 119951001A3230 ATTACH BOSS PIPER PA60 PA60600 7106001NM MLG TORQ LINK BROKE A DKBAK NONE O OTHER LDLANDING 1 SO097499S 600050111 ATTACH POINT FOR UPPER TORQUE LINK FOR MLG BAND, WHERE LINK ATTACHES TO STRUT CRACKED AND BROKE AT LANDING. TIRE TURNED SIDEWAYS, AND AIRCRAFT DEPARTED THE RUNWAY AND HIT VASI LIGHTS CAUSING BOTH GEARS TO COLLAPSE. TTAF, 7,928.7 HRS. 1M72 3O RTA17WE 19951229000691995122900069CE 1995 12 29 95ZZZX6929 119951013A5522 SKIN BEECH 58 58 1152740CE RT ELEV BOTTOM CRACKED A EAPAK NONE O OTHER ININSP/MAINT 1 GL0946US TH294 FOUND BOTTOM SKIN OF RT ELEVATOR CRACKED DURING PROGRESSIVE INSPECTION. UPON SKIN REMOVAL (FOR REPAIR), FOUND HINGE ATTACH BRACKET CRACKED AND END ATTACH TAB OF SPAR BROKEN OFF. SUGGEST WIDER RE-INFORCEMENT GUSSETS AT SPAR AND END CLOSURE RIB. 1L72 3O 3A16 19951229000701995122900070CE 1995 12 29 95ZZZX6930 119951013A55219661000613 SPAR BEECH 58 58 1152740CE RT ELEV CRACKED AS EAPAK NONE O OTHER ININSP/MAINT 1 GL0946US TH294 FOUND BOTTOM SKIN OF RT ELEVATOR CRACKED DURING PROGRESSIVE INSPECTION. UPON SKIN REMOVAL (FOR REPAIR), FOUND HINGE ATTACH BRACKET CRACKED AND END ATTACH TAB OF SPAR BROKEN OFF. SUGGEST WIDER RE-INFORCEMENT GUSSETS AT SPAR AND END CLOSURE RIB. 1L72 3O 3A16 19951229000781995122900078WP 1995 12 29 ABXA9501044 119951222A3260189915 CONNECTOR DOUG DC8 DC862 3021970WP RT MLG DIRTY A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23804AX 45987 AFTER TAKEOFF FROM ILN, GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED AND RIGHT MAIN GEAR DOOR NOT LATCHED WAS ILLUMINATED. RECYCLED GEAR AND PERFORMED ABNORMAL PROCEDURE IAW DC-8 OPS MANUAL. NO HELP. CLEANED CONNECTOR AT PROXIMITY SWITCH AFTER VERIFYING MALFUNCTION. SYSTEM OPS CHECKED GOOD IAW MAB DC8-32-6. 2L74 4F 4A25 19951229000791995122900079WP 1995 12 29 ABXA951045 119951222A32600080004002 PROX BOX DOUG DC8 DC862 3021970WP MLG MALFUNCTIONED A ABXAO OTHER N FALSE WARNING CLCLIMB 1 GL23804AX 45987 AFTER TAKEOFF FROM TPA, RED GEAR UNSAFE LIGHT REMAINED ON. NO LIGHT WAS ON IN ANY GEAR/DOOR POSITION. RECYCLED GEAR AND PERFORMED ABNORMALS IAW DC-8 OPS MANUAL. NO HELP. REPLACED MAIN LANDING GEAR DOOR PROXIMITY BOX AND CLEANED UPLATCH ASSEMBLIES ON BOTH GEAR DOORS. PERFORMED RETRACTION CHECK IAW MAB DC8-32-6. OPS CHECKED GOOD ON THE GROUND. 2L74 4F 4A25 19951229000801995122900080SW 1995 12 29 QXEA9500426 119951207A2742DL5040M5 ACTUATOR SWRNGN SWRNGNSA227 SA227AC 8780603SW HORIZ STAB MALFUNCTIONED A QXEAO OTHER O OTHER APAPPROACH 1 NM093116Z 1737 AC598 ALW - FIRST OFFICER NOTED TRIM-IN-MOTION BEEP, BUT HAD NO STABILIZER TRIM AFTER FLAPS WERE SELECTED TO FULL. TRIM SELECTED TO CAPTAIN'S SIDE AND STILL NO TRIM. AIRCRAFT LANDED IN ALW WITHOUT FURTHER INCIDENT. 1L72 4T A8SW 19951229000811995122900081EU 1995 12 29 QXEA9500427 119951208A33501315 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 BOI - EMERGENCY LIGHT ON FORWARD FLIGHT ATTENDANT'S PANEL IS INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000821995122900082SW 1995 12 29 QXEA9500428 119951208A29102781032501 HYD LINE SWRNGN SWRNGNSA227 SA227AC 8780603SW COCKPIT LEAKING A QXEAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09384PH AC592 BOI - HYDRAULIC PRESS DROPPED TO ZERO, LEFT AND RIGHT HYDRAULIC. WARNING LIGHTS ILLUMINATED. SYSTEM OPERATED AT ZERO PRESSURE FOR APPROXIMATELY 15-20 MINUTES. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. GEAR UP LINE AND FLAP UP LINE REPLACED I/A/W MAINT. MANUAL. COMPLIED WITH CAUTION PUMP PROCEDURES I/A/W MAINT. MANUAL. HYDRAULIC LINES LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951229000831995122900083NE 1995 12 29 QXEA9500429 219951208A7320323305 VALVE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 NM09814PH 043 PCE120215 PDX - DISTINCT OIL SMELL IN COCKPIT LOWER POWER SETTINGS FROM NR 1 ENGINE. NR 1 ENGINE P2.5/3 SWITCHING VALVE REPLACED I/A/W MAINT. MANUAL. ENGINE OPS CHECKED GOOD ON GROUND RUN, NO OIL SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 19951229000841995122900084EU 1995 12 29 QXEA9500430 119951209A3350MGG1280 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09452AU 11105 PDX - AFT SIDE OF EXIT SIGN AT ROW 8 HAS NUMEROUS 28V BULBS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000851995122900085NE 1995 12 29 QXEA9500431 219951210A7261 OIL SYST DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE OVER SERVICED A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM09814PH 043 PCE120215 SEA - STRONG OIL SMOKE SMELL IN COCKPIT. NR 1 ENGINE OIL PRESSURE FLUCUATED BETWEEN 55-60 PSI. SMELL WENT AWAY AFTER TURNING OFF NR 1 BLEED AIR. OIL LEVEL IN NR 1 ENGINE REDUCED TO BELOW MAX ON SIGHT GAUGE. NR 1 ENGINE GROUND RUN WITH BLEED AIR ON AND NO SMOKE OR SMELL NOTED. NR 1 ENGINE OIL PRESSURE WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 19951229000861995122900086EU 1995 12 29 QXEA9500432 119951211A33505515800104 BOARD FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 GEG - EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS INOP. LIGHT BOARD REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000871995122900087EU 1995 12 29 QXEA9500433 119951212A33501312 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 SEA - EMERGENCY EXIT LIGHT AT 8A INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000881995122900088NM 1995 12 29 QXEA9500434 119951212A33501013075 BULB DHAV DHAV DHC8 DHC8102 2809003NM CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09831PH 328 GEG - ONE RED FLOOR PROXIMITY LIGHT IS INOP. LAMP WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000891995122900089NM 1995 12 29 QXEA9500435 119951212A534785331040109 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - SEAT TRACK P/N 85331040-109 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000901995122900090NM 1995 12 29 QXEA9500436 119951212A534785320701125 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - SEAT TRACKS P/N 85320701-125 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000911995122900091NM 1995 12 29 QXEA9500437 119951212A534785330469001 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - SEAT TRACK P/N 85330469-001 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000921995122900092NM 1995 12 29 QXEA9500438 119951212A534785330217001 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - SEAT TRACK P/N 85330217-001 FOUND CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000931995122900093NM 1995 12 29 QXEA9500439 119951212A534785330507107 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - SEAT TRACK P/N 85330507-107 FOUND CORRODED BEYOND MANFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000941995122900094NM 1995 12 29 QXEA9500440 119951212A534785320701123 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A QXEAK NONE O OTHER ININSP/MAINT 1 NM09102AV13735 091 PDX - DURING C-CHECK, FOUND SEAT TRACK P/N 85320701-123 IS CORRODED BEYOND MANUFACTURER'S LIMITS. NEW TRACK WAS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229000951995122900095EU 1995 12 29 QXEA9500441 119951213A33501312 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - LEFT EMERGENCY LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000961995122900096EU 1995 12 29 QXEA9500442 119951213A3350MGG1280 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09457US 11036 PDX - FORWARD CABIN AISLE EXIT SIGN HAS SEVERAL EMERGENCY LIGHT BULBS (28V) INOP. ALL SEVEN 28V BULBS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000971995122900097EU 1995 12 29 QXEA9500443 119951214A3350MGG1280 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09450US 11101 SEA - CABIN EMERGENCY EXIT SIGN WILL NOT ILLUMINATE WITH EMERGENCY LIGHTS IN THE ARMED POSITION. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229000981995122900098SW 1995 12 29 QXEA9500444 119951216A3310LT52A POWER SUPPLY SWRNGNSA227 SA227AC 8780603SW COCKPIT INOP A QXEAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM093116888767 AC599 GEG - LOST LIGHTING ON FIRST OFFICER'S SIDE, FLIGHT INSTRUMENTS WITH STRONG ELECTRICAL BURNING SMELL OCCURRING DURING FAILURE. REPLACED POWER SUPPLY AND LIGHTING, OPS CHECKED GOOD. REMOVED POWER SUPPLY, HAD STRONG BURNED ODOR. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951229000991995122900099EU 1995 12 29 QXEA9500445 119951221A33501315 BULB FOKKER FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 GEG - SEVERAL OVERHEAD EMERGENCY LIGHTS INOP. BULBS WERE REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229001001995122900100WP 1995 12 29 9521169140 119951222A7931 OIL PRESS TRANS DOUG DC9 DC914 3022034WP PWA JT8 JT8D7A 52053NE NR 1 ENGINE FAILED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01930RC 45729 653779 NR 1 ENGINE OIL PRESSURE INDICATION FAILED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER WITH A SERVICEABLE UNIT. 2L72 4F4 F A6WE E2EA 19951229001011995122900101WP 1995 12 29 9521179909 119951224A7711 PT7 LINE DOUG DC9 DC931 3022065WP PWA JT8 JT8D9 52048NE NR 2 ENGINE BROKEN A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL01959N 47255 657497 NR 2 ENGINE EPR INDICATION WAS LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED A BROKEN PT7 LINE WITH A NEW PART. 2L72 4F4 F A6WE E2EA 19951229001021995122900102EU 1995 12 29 9521183221 119951222A490038002783 APU AIRBUS320 A320211 3930320EU TAIL FIRE A NWAAF ACTIVATE FIRE EXT. A FLAME/FIRE ININSP/MAINT 1 GL01321US124508703 262 AT THE GATE, SHORTLY AFTER APU SHUTDOWN, SMOKE AND FLAMES WERE NOTICED COMING OUT OF APU EXHAUST DUCT. APU FIRE BOTTLE WAS DISCHARGED AND FIRE EXTINGUISHED. MAINTENANCE INSPECTED THE APU AND SURROUNDING AREA. NO DAMAGE BEYOND APU NOTED. APU PLACED ON MEL. 2L72 4F RTA28NM 19951229001031995122900103NM 1995 12 29 9521196717 119951221A304065B4609930 CONTROL PANEL BOEING747 747251F 1384898NM WINDOW HEAT MALFUNCTION A NWAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL01617US229103077 21121 EN ROUTE ANC-JFK, THE R1-L1 WINDOW HEAT FAILED TO OPERATE. CREW FOLLOWED COCKPIT OPERATING MANUAL AND DIVERTED FLIGHT TO DTW. MAINTENANCE REPLACED WINDOW HEAT CONTROL PANEL AND CHECK WAS NORMAL. 2L74 4F A20WE 19951229001041995122900104WP 1995 12 29 9521201150 119951221A2170 COALESCER BAGS DOUG DC10 DC1040 3023508WP CABIN CONTAMINATED A NWAAAJ UNSCHED LANDING DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01150US 46759 AFTER TAKEOFF, CABIN BEGAN TO FILL WITH SMOKE, PILOT BEGAN DUMPING FUEL AND RETURNED TO DEPARTURE AIRPORT. AIRCRAFT LANDED, TAXIED TO GATE AND DEPLANED PASSENGERS THROUGH JETWAY WITHOUT FURTHER INCIDENT. MAINTENANCE INSTALLED NEW COALESCER BAGS AND RAN AIRCRAFT ENGINES, PACKS ON. NO SMOKE OR FUMES NOTED. 2L73 4F A22WE 19951229001051995122900105NE 1995 12 29 9521219311 219951219A7230 COMPRESSOR DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 2 ENGINE STALLED A NWAAO OTHER R PARTIAL RPM/PWR LOSS CLCLIMB 1 GL01314RC 49110 708432 NR 2 ENGINE LOST POWER ON TAKEOFF. THE CREW CONTINUED THE TAKEOFF DUE TO HIGH AIRSPEED AND POOR RUNWAY CONDITIONS. AFTER LIFT OFF A COMPRESSOR STALL OCCURRED AND THE ENGINE RESUMED NORMAL OPERATION. THE AIRCRAFT COMPLETED ITS SCHEDULED FLIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED BOTH ENGINES UPON ARRIVAL. NO DISCREPANCIES WERE NOTED. 2L72 4F4 F A6WE E9NE 19951229001061995122900106WP 1995 12 29 9521229947 119951221A3297 WIRE DOUG DC9 DC931 3022065WP NLG BROKEN A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL018938E 47161 DURING APPROACH, THE NOSE LANDING GEAR SAFE LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. A DOWNLOCK CHECK WAS PERFORMED WHICH VERIFIED THE NOSE LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN WIRE FROM DOWNLOCK SWITCH TO GROUND STUD. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229001071995122900107WP 1995 12 29 9521239920 119951220A3350 POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN FAILED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01940N 47459 DURING LINE CHECK, FOUND EMERGENCY ESCAPE LIGHTS FORWARD OF FIRST CLASS SEATS INOPERATIVE. RESECURED PIN ON LEFT FORWARD ENTRY DOOR CHARGER ASSEMBLY. REPLACED LIGHT ASSEMBLY AND POWER SUPPLY. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229001081995122900108WP 1995 12 29 9521249864 119951220A33506014113 POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01773NC 47775 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROW 23 INOPERATIVE. REPLACED POWER SUPPLY FOR AFT SECTION OF FLOOR EMERGENCY LIGHTS. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229001091995122900109WP 1995 12 29 9521259163 119951219A33506014113 BATTERY PACK DOUG DC9 DC914 3022034WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018906E 45747 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF FLOOR PROXIMITY EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229001101995122900110 1995 12 29 9521269972 419951220A2212 CONTROLLER DOUG DC9 DC931 3022065WP AUTOPILOT MALFUNCTIONED A NWAAO OTHER O OTHER UKUNKNOWN 1 GL019336 47338 ON THE FIRST TWO ATTEMPTS TO ENGAGE THE AUTOPILOT SYSTEM, THE AIRCRAFT EXPERIENCED A SLIGHT ROLL. AIRCRAFT OPERATED NORMALLY AFTER ENGAGING THE AUTOPILOT SYSTEM FOR THE THIRD TIME. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED AUTOPILOT CONTROLLER AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229001111995122900111WP 1995 12 29 9521279102 119951217A2760 CONTROL CABLE DOUG DC9 DC915 3022036WP RT SPOILER BINDING A NWAAO OTHER F FLT CONT AFFECTED UKUNKNOWN 1 GL0192S 47064 EN ROUTE GSO-MSP, AIRCRAFT WAS CONTINUOUSLY ROLLING 3 TO 4 DEGREES LEFT AND RIGHT. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING INBOARD SPOILER RETRACT CABLE DEFLECTED AND HUNG ON ADEL CLAMP. FREED CABLE AND RIGGED. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229001121995122900112WP 1995 12 29 9521289853 119951221A3350 BATTERIES DOUG DC9 DC951 3022051WP COCKPIT DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01762NC 47710 DURING PREFLIGHT CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19951229001131995122900113WP 1995 12 29 9521299864 119951219A3350 POWER SUPPLY DOUG DC9 DC951 3022051WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01773NC 47775 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY AND EMERGENCY EXIT SIGN LIGHTS INOPERATIVE, AFT OF ROW 22. REPLACED POWER SUPPLIES AND BATTERIES. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229001141995122900114WP 1995 12 29 9521309861 119951219A32225910448563 STRUT DOUG DC9 DC951 3022051WP NLG UNDERSERVICED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01770NC 47758 LANDING GEAR HANDLE WOULD NOT RAISE AND AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT RETURNED TO YWG AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT UNDERSERVICED. SERVICED STRUT TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229001151995122900115 1995 12 29 9521319305 419951219A34216224507001 ATTITUDE IND DOUG DC9 DC982 3022082WP COCKPIT RIGHT MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION UKUNKNOWN 1 GL01307RC276844488 48086 EN ROUTE MSP-MCO, FIRST OFFICER'S ATTITUDE INDICATOR FLAGGED WITH INTERMITTENT READINGS. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. REPLACED FIRST OFFICER'S ATTITUDE INDICATOR. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229001161995122900116WP 1995 12 29 9521329885 119951218A213110256852 CONTROLLER DOUG DC9 DC951 3022051WP COCKPIT PANEL MALFUNCTIONED A NWAAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 GL01401EA29441399 47682 LOSS OF CABIN PRESSURIZATION OCCURRED AT 33,000 FEET UPON SELECTION OF ENGINE AND AIRFOIL ANTI-ICE. CABIN ALTITUDE REACHED 10,000 FEET AND EMERGENCY DESCENT WAS MADE TO 18,000 FEET. CABIN PRESSURE WAS REGAINED AND FLIGHT CONTINUED TO MEM WITHOUT FURTHER INCIDENT. REPLACED CABIN PRESSURE CONTROLLER AND RETORQUED CLAMP ON CROSSOVER DUCTS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229001171995122900117WP 1995 12 29 9521331150 119951220A4900TSCP7004B APU DOUG DC10 DC1040 3023508WP TAIL FAILED A ANWAAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL01150US55547752 46759 PRIOR TO DEPARTURE, A LARGE CLOUD OF SMOKE DISCHARGED OUT OF APU EXHAUST DUCT. NO UNUSUAL COCKPIT INDICATIONS. APU WAS SHUTDOWN, AT WHICH TIME THE CABIN BEGAN TO FILL WITH SMOKE. PASSENGERS DEPLANED THROUGH MAIN CABIN DOOR WITHOUT INCIDENT. APU PLACED ON MEL. 2L73 4F A22WE 19951229001181995122900118EU 1995 12 29 9521343242 119951221A21319022157028 CONTROLLER AIRBUS320 A320211 3930320EU AVIONICS COMP MALFUNCTIONED A NWAAAG UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL01342NW191854547 381 DURING CRUISE WHILE AT FL 350, RECEIVED CAB PR SYS 1 AND 2 FAULT AND CABIN ALTITUDE CLIMBED TO 18.500 FEET. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND INITIATED EMERGENCY DESCENT. ALL OXYGEN MASKS AND OXYGEN GENERATORS DEPLOYED AND ACTIVATED PROPERLY. THE AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH SYSTEM 1 AND SYSTEM 2 CABIN PRESSURE CONTROLLERS AND OPERATIONAL CHECK OK. REPACKED ALL OXYGEN MASKS IN THE LAVATORIES AND RESTORED THE OXYGEN SYSTEM IN THE CABIN. OPERATIONAL CHECK OK. 2L72 4F RTA28NM 19951229001191995122900119EU 1995 12 29 9521353208 119951221A3350321430 BATTERY PACK AIRBUS320 A320211 3930320EU CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01308US 107 DURING LINE MAINTENANCE, FOUND DOORS 3 AND 4 EMERGENCY EXIT LIGHTS AND AFT CABIN EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR POWER SUPPLY 13WL, OPS CHECK OK. 2L72 4F RTA28NM 19951229001201995122900120NM 1995 12 29 95UAL900340 119951226A3350 FUSE BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29176UA 24383 LEFT EXTERIOR EMERGENCY LIGHTS INOP. BLOWN FUSE WAS FOUND. REPLACED FUSE IN POWERPACK ABOVE DOOR 3L. 2L74 4F4 FRTA20WE E24NE 19951229001211995122900121NM 1995 12 29 95UAL900341 119951226A3350 POWER PACK BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29176UA 24383 UPPER DECK LIGHT ABOVE LT DOOR GOES OUT AFTER 10 TO 20 SECONDS. FOUND LOW BATTERY. REPLACED POWER PACK AND BATTERY. 2L74 4F4 FRTA20WE E24NE 19951229001221995122900122NM 1995 12 29 95UAL900342 119951226A3350 LAMP BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29176UA 24383 FLOOR EMERGENCY EXIT LIGHT INOP AT ROW 58C. FOUND BURNED OUT LAMP. REPLACED LAMP. 2L74 4F4 FRTA20WE E24NE 19951229001231995122900123NE 1995 12 29 95UAL900343 219951226A7200 ENGINE BOEING747 747123 1384873NM PWA JT9 JT9D7A 52054NE WING FLAMED-OUT A UALAK NONE X ENGINE FLAMEOUT LDLANDING 1 WP29157UA 20106 695722 ENGINE FLAME-OUT ON LANDING. 2L74 4F4 F A20WE E20EA 19951229001241995122900124NM 1995 12 29 95UAL900344 119951226A2720251W315012 B-NUT BOEING777 777222 1385219NM PWA PW4077PW4077 NE RUDDER CONTROL LOOSE A UALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP29771UA 26932 SMOKE AND ODOR IN CABIN. SMOKE DUE TO INGESTION OF HYDRAULIC FLUID INTO APU AIR INLET. LOOSE B-NUT ON RETURN LINE FOR RUDDER LOWER POWER CONTROL UNIT DETERMINED TO BE SOURCE OF LEAK. B-NUT TIGHTENED, OIL RESIDUE CLEANED UP AND PNEUMATIC AND AIR CONDITIONING DUCTING PURGED USING HIGH TEMPERATURE AIR. 2L72 4F4 FRTT0001SE E46NE 19951229001251995122900125SO 1995 12 29 COMA9512037 119951221A2750KRP138112VT ROLLER EMB 120 EMB120RT SO FLAPS WORN A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254CA 120233 FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP. REPLACED THE LT AND RT OUTBD FLAP SECTIONS ROLLERS. 2L72 4T RTA31SO 19951229001261995122900126SO 1995 12 29 COMA9512038 119951221A2750 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01254CA 120233 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. CLEANED ICE AND SLUSH FROM OUTBD FLAP TRACKS. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951229001271995122900127SO 1995 12 29 COMA9512039 119951221A27523203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAK NONE J WARNING INDICATION TXTAXI/GRND HDL 1 SO01164D 120164 AFTER LANDING WHEN FLAPS SELECTED UP, CONTROL FAULT WARNING ACTIVATED. REPLACED THE RT INBD FLAP ACTUATOR. 2L72 4T RTA31SO 19951229001281995122900128SO 1995 12 29 COMA9512040 119951223A2750KRP138112VT ROLLERS EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01255CA 120238 FLAP DISAGREEMENT WARNING DURING TAKEOFF CLIMB. REPLACED THE OUTBD FLAP SECTION ROLLERS. 2L72 4T RTA31SO 19951229001291995122900129SO 1995 12 29 COMA9512041 119951222A5270 DOOR WARNING EMB 120 EMB120RT SO CARGO DOOR MALFUNCTIONED A COMAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO01265CA 120257 CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB. FOUND TO BE FALSE WARNING. PLACED DOOR WARNING SYSTEM ON DEFERRED MAINT LIST AND ACFT CONTINUED SERVICE. 2L72 4T RTA31SO 19951229001301995122900130NE 1995 12 29 COMA9531218 219951221A75307275031502 TUBE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE RT ENGINE CRACKED A COMAK NONE J WARNING INDICATION CRCRUISE 1 SO01356CA 340A034 RT ENGINE ITT IS HIGHER THAN NORMAL DURING CRUISE. REPLACED CRACKED HIGH PRESSURE BLEED AIR TUBING ON RT ENGINE. 2L72 4T4 TRTA52EU E8NE6 19951229001311995122900131EA 1995 12 29 COMA9560626 119951224A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO01941CA 7050 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE LT AND RT BRAKE AND POSITION SENSOR UNIT. 2L72 4F RTA21EA 19951229001321995122900132NM 1995 12 29 MWEA95537 119951224A25603952273501 GIRT BAR LATCH DOUG MD88 MD88 3023688NM CABIN DIRTY A MWEAK NONE O OTHER NRNOT REPORTED 1 GL31601ME 49762 CREW REPORTS, AFT LEFT SERVICE DOOR EVACUATION SLIDE GIRT BAR VERY DIFFICULT TO ENGAGE AND DISENGAGE. CLEANED AND LUBED GIRT BAR LATCHES, OPS CHECK GOOD. 2L72 4F RTA6WE 19951229001331995122900133WP 1995 12 29 MWEA95538 119951225A2150 CLAMP DOUG DC9 DC915 3022036WP LT PACK FAILED A MWEABG EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CRCRUISE 1 GL31300ME 45718 PILOT REPORTS, DURING CRUISE AT 33,000 FT CABIN PRESSURE LIGHT ILLUMINATED. CABIN ALTITUDE REACHED 10,500 FT, DESCENDED TO 19,500 FT, CABIN ALTITUDE DESCENDED TO 9,000 FT AND ALL OXYGEN MASKS DEPLOYED. FOUND LEFT PACK DUCT OFF DUE TO FAULTY CLAMP. REPLACED CLAMP AND STOWED O2 MASKS. 2L72 4F A6WE 19951229001341995122900134WP 1995 12 29 MWEA95539 119951225A2120 AIR DISTR DOUG DC9 DC932 3022066WP CABIN SMOKE A MWEAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL31204ME 47680 CREW REPORTS, RT LAV SMOKE DETECTOR SOUNDED WHILE TAXIING TO GATE AFTER LANDING. FLIGHT ATTENDANT REPORTED FOG IN CABIN AND NO FIRE DETECTED AT THAT TIME. RAN LT AND RT ENGINES WITH PACKS ON, RAN APU AND COULD NOT DUPLICATE PROBLEM. NO FOG OR SMOKE IN CABIN. LEAK CHECKED APU AND ENGINE, ALL OK. 2L72 4F A6WE 19951229001351995122900135NM 1995 12 29 P5CA9500876 119951223A2613 OVERHEAT WARNING BOEING747 747122 1384872NM RT WING ACTIVATED A P5CAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 WP23852FT 19757 RT WING LEADING EDGE OVERHEAT FAULT, ON TAXI OUT FOR TAKEOFF. RETURNED TO GATE, UNABLE TO DUPLICATE OVERHEAT CONDITION WITH EITHER APU OR ENGINE PNEUMATICS. DETERMINED TO BE FALSE WARNING. 2L74 4F A20WE 19951229001361995122900136NE 1995 12 29 P5CA9500877 219951225A7230 FAN BLADES BOEING747 747124 1384874NM PWA JT9 JT9D7A 52054NE NR 1/2/3 ENGINESFOD A P5CAK NONE O OTHER ININSP/MAINT 1 WP23855FT 19733 DISCOVERED FAN BLADE DAMAGE NUMBERS 1, 2 AND 3 ENGINES, DUE TO ICE INGESTION. BLENDED BLADES TO FLYBACK LIMITS AT EWE AND AT JFK REPLACED COMPLETE SET OF FAN BLADES ON NR 2 ENGINE. BLENDED AND REPLACED MATCHED SETS NR 1 AND NR 3 ENGINE IAW MM 72-31-02. 2L74 4F4 F A20WE E20EA 19951229001371995122900137WP 1995 12 29 SCNA95297 119951220A2612ASL0387503 FIRE LOOP DOUG DC10 DC1010 3022110WP NR 2 ENGINE INTERMITTENT A SCNAK NONE N FALSE WARNING CLCLIMB 1 GL15572SC 46977 THE NUMBER 2 ENGINE A-SYSTEM FIRE DETECTION LOOP FLICKERED DURING CLIMB AND DESCENT, BUT NOT IN CRUISE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. FOUND IMPROPERLY ROUTED WIRING, REROUTED WIRING AND SYSTEM TESTED GOOD IAW MM 26-00-00. 2L73 4F A22WE 19951229001381995122900138NM 1995 12 29 SWAA950783 119951214A5313 STRINGER BOEING737 7372H4 138448CNM APU COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT END OUTBOARD OF FWD BULKHEAD OF APU COMPARTMENT. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951229001391995122900139NM 1995 12 29 SWAA950784 119951214A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 1006 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY FLOOR BEAM CORRODED AT SCREW HOLES, UPPER AND LOWER SURFACES AT AFT FLANGE AT BS 1006, LBL 15, 19 AND 23. INSTALLED REPAIR STRAPS PER SWA RA 1-253-1411. 2L72 4F A16WE 19951229001401995122900140NM 1995 12 29 SWAA950785 119951217A26126937307112 CONTROL PANEL BOEING737 7372H4 138448CNM NR 2 ENGINE MALFUNCTIONED A SWAAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SW0729SW 21340 DURING DESCENT, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED ENGINE/APU FIRE CONTROL PANEL, CLEANED AND RESECURED ENGINE FIRE LOOP CONNECTORS PER BOEING M/M. 2L72 4F A16WE 19951229001411995122900141NM 1995 12 29 SWAA950786 119951214A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 1006 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 1006, LBL 15. REPAIRED PER SWA RA 1-253-1411. 2L72 4F A16WE 19951229001421995122900142NM 1995 12 29 SWAA950787 119951214A5315 FLOOR BEAM BOEING737 7372H4 138448CNM BS 1016 CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR BEAM CORRODED AT BS 1016, LBL 15 AND 10. REPAIRED PER SWA RA 1-253-1409. 2L72 4F A16WE 19951229001431995122900143NM 1995 12 29 SWAA950788 119951214A5347 SEAT TRACK BOEING737 7372H4 138448CNM BS 706-715 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND 7 CRACKS IN SEAT TRACK WEB EXTENDING FROM RIVET HEADS THAT SECURE WEB TO PRESS DECK ATTACHING ANGLES BETWEEN BS 706/715 AT RBL 24.75. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951229001441995122900144NM 1995 12 29 SWAA950789 119951214A5320 ANGLE BOEING737 7372H4 138448CNM BS 348 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME CHORD ANGLE CRACKED AT BELT FRAME AFT OF FWD ENTRY DOOR AT BS 348 FROM S14 TO 17L. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951229001451995122900145NM 1995 12 29 SWAA950790 119951214A5313 STRINGER BOEING737 7372H4 138448CNM APU COMPT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0781SW 22730 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 17L CRACKED AT END OUTBOARD OF FWD BULKHEAD OF APU COMPARTMENT. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951229001461995122900146NM 1995 12 29 SWAA950791 119951220A5315 STRAP BOEING737 7373H4 1384600NM BS 312 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07323SW 23344 DURING SCHEDULED BC1 CHECK, FOUND FLOOR BEAM SUPPORT STRAPS CRACKED AT BS 312, AT BL ZERO, RBL 46, AND RBL 28. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19951229001471995122900147NM 1995 12 29 SWAA950792 119951220A5244 PANEL BOEING737 7372H4 138448CNM NLG WW CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW0761SW 21970 DURING SCHEDULED B-CHECK, FOUND NOSE GEAR WHEELWELL ACCESS PANEL OPENING CRACKED. REPAIRED PER BOEING SRM. 2L72 4F A16WE 19951229001481995122900148NM 1995 12 29 SWAA950793 119951220A32606552811115 MODULE BOEING737 7372H4 138448CNM NLG FAILED A SWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0756SW 21721 NLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. REPLACED LANDING GEAR CONTROL MODULE PER BOEING M/M. 2L72 4F A16WE 19951229001491995122900149NM 1995 12 29 SWAA950794 119951222A5610 WINDOW BOEING737 7372H4 138448CNM RT COCKPIT CRACKED A SWAAA UNSCHED LANDING C F.O.D. CLCLIMB 1 SW0785SW 22826 EXPERIENCED BIRDSTRIKE TO FIRST OFFICER'S NR 1 WINDOW. AIRCRAFT RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. PERFORMED BIRDSTRIKE INSPECTION. ALSO, FOUND NR 4 WINDOW CHIPPED. REPLACED NRS 1 AND 4 WINDOW ASSEMBLIES PER BOEING M/M. 2L72 4F A16WE 19951229001501995122900150NM 1995 12 29 UPS405160 119951223A3350 LIGHT BOEING747 747121 1384871NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01683UP 20353 MAINTENANCE FOUND FWD L1 DOOR EMERGENCY LIGHT AND CEILING EMERGENCY LIGHT FWD OF CREW STAIRS ARE INOP. REPLACED CEILING AISLE LIGHT ASSY L1 AND AISLE EMERGENCY LIGHT OP NORMAL. 2L74 4F A20WE 19951229001511995122900151WP 1995 12 29 9521519106 119951202A5315 FLOOR BEAM DOUG DC9 DC915 3022036WP FS 503 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0196S 47206 DURING H-CHECK, FOUND A 1.50 INCH CRACK IN THE FS 503 FLOOR SUPPORT BEAM AT THE LEFT FRAME. REPAIRED BEAM. (P/N 9915527-1) PER EA 91-102005. 2L72 4F A6WE 19951229001521995122900152WP 1995 12 29 9521529153 119951204A5220 FRAME DOUG DC9 DC914 3022034WP OVERWING DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND A .50 INCH CRACK IN THE RIGHT OVERWING EMERGENCY EXIT DOOR PAN BY NR 14 SUPPORT. REPAIRED FRAME (P/N 5913195-1) PER EA 91-103342. 2L72 4F A6WE 19951229001531995122900153WP 1995 12 29 9521539969 119951206A5313 LONGERON DOUG DC9 DC931 3022065WP CTR FUEL TANK CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019333 47246 DURING A SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN LONGERON 16R IN THE CENTER FUEL TANK. REPAIRED PER EA 99-87836. 2L72 4F A6WE 19951229001541995122900154WP 1995 12 29 9521549307 119951209A5315 FLOOR BEAM DOUG DC9 DC982 3022082WP FS 1338 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING H-CHECK, FOUND CORROSION ON THE FS 1338 FLOOR BEAM UPPER CHORD BETWEEN RBL 8-RBL 60. REPAIRED CHORD (P/N S2912758) PER EA 93-104981. 2L72 4F A6WE 19951229001551995122900155NM 1995 12 29 9521552761 119951214A5320 DOOR SILL BOEING727 7272M7 138407SNM FS 950-990 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RW 21200 DURING H-CHECK, FOUND CORROSION ON NR 2 CARGO DOOR LOWER MAIN SILL OUTBOARD CHORD. REPAIRED CHORD (P/N 65-56129-10) PER EA 27-103392. 2L73 4F A3WE 19951229001561995122900156WP 1995 12 29 9521569307 119951214A5230 DOOR PAN DOUG DC9 DC982 3022082WP FS 357 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING H-CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR INNER AND OUTER PANS, LOWER EDGE, FS 357. REPAIRED BOTH PANS (P/N 5910141-9,-5) PER EA 93-103393. 2L72 4F A6WE 19951229001571995122900157WP 1995 12 29 9521579307 119951216A5347 CARGO TRACK DOUG DC9 DC982 3022082WP FS 598-693 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING H-CHECK, FOUND CORROSION ON THE LEFT CARGO TRACK SPLICE, FS 598-693. REPAIRED TRACK (P/N 5936594-501) PER EA 93-103380. 2L72 4F A6WE 19951229001581995122900158WP 1995 12 29 9521589979 119951216A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP FS 154 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL019343 47439 DURING M-CHECK, FOUND A CRACK IN THE SERVICE DOOR JAMB TO COCKPIT LOWER SILL INTERCOSTAL, LONGERON 12R AT APPROX FS 154. REPAIRED INTERCOSTAL (P/N 9911557-3) PER EA 99-102010. 2L72 4F A6WE 19951229001591995122900159NM 1995 12 29 9521592761 119951219A5315 FLOOR BEAM BOEING727 7272M7 138407SNM FS 1130 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RW 21200 DURING H-CHECK, FOUND CORROSION ON THE BS 1130 FLOORBEAM LOWER CHORD FROM LBL 44-RBL 50. REPAIRED CHORD (P/N 65-20838-17) PER EA 27-103386. 2L73 4F A3WE 19951229001601995122900160NM 1995 12 29 9521602761 119951219A5240 FRAME BOEING727 7272M7 138407SNM SERVICE DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RW 53829 21200 DURING H-CHECK, FOUND A CRACK IN THE AFT LEFT SERVICE DOOR FRAME, LOWER FORWARD CORNER. REPAIRED FRAME. (P/N 65-24571-1) PER EA 27-103412. 2L73 4F A3WE 19951229001611995122900161WP 1995 12 29 9521619610 119951221A5753 FITTING DOUG DC9 DC932 3022066WP FLAP HINGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND RUST ON THE CENTER FLAP HINGE FITTING UPPER BUSHINGS. REPLACED FITTING PER MM 57-40-1. 2L72 4F A6WE 19951229001621995122900162NM 1995 12 29 9521622761 119951222A5311 FRAME BOEING727 7272M7 138407SNM FS 760 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01721RW 21200 DURING H-CHECK, FOUND A 1.1250 INCH CRACK IN THE BS 760 FRAME RIGHT INBOARD FLANGE REINFORCEMENT CHORD. REPAIRED CHORD (P/N 65-16325-111) PER EA 27-103413. 2L73 4F A3WE 19951229001631995122900163WP 1995 12 29 9521639754 119951223A5320 FITTING DOUG DC9 DC941 302207NWP FS 160 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01754NW 47178 DURING H-CHECK, FOUND CORROSION ON THE FS 160 FRAME FITTING BENEATH THE FORWARD LOWER CORNER OF THE SERVICE DOOR SCUFF PLATE. REPLACED FITTING PER SRM 51-10. 2L72 4F A6WE 19951229001641995122900164WP 1995 12 29 9521649754 119951226A5240 FITTING DOUG DC9 DC941 302207NWP SERVICE DOOR CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01754NW 47178 DURING H-CHECK, FOUND CORROSION ON THE FORWARD SERVICE DOOR NB 4 BEAM FITTING AT THE FORWARD INTERCOSTAL. REPLACED FITTING PER SRM 51-30-2. 2L72 4F A6WE 19951229001651995122900165NE 1995 12 29 9521656613 219951227A7300 ENGINE BOEING747 747251B 1384892NM PWA JT9 JT9D7F 52054NE NR 3 MALFUNCTIONED A NWAAK NONE R PARTIAL RPM/PWR LOSS CRCRUISE 1 GL01613US 20358 662545 DURING CRUISE, THE NR 3 ENGINE ROLLED BACK TWICE WITH EGT, N1 AND FUEL FLOW GOING TO BOTTOM OF SCALE. WHEN THE THRUST LEVER WAS ADVANCED, ALL READINGS RETURNED TO NORMAL AND THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. FUEL PRESSURES WERE CHECKED, THE FUEL PUMP AND FUEL CONTROL WERE REPLACED. A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. 2L74 4F4 F A20WE E20EA 19951229001661995122900166NM 1995 12 29 9521662203 119951222A5230 DOOR BOEING727 727251 138408HNM CARGO COMPT NOT SEALED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01203US 22543 DURING TAKE-OFF CLIMB, AFT CARGO DOOR LIGHT ILLUMINATED, AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REMOVED DEBRIS FROM AFT CARGO DOOR SILL. CHECKED OK. 2L73 4F A3WE 19951229001671995122900167WP 1995 12 29 ABXA9501046 119951226A326092693759 BOX DOUG DC8 DC863F 302198FWP RT MLG DEFECTIVE A ABXAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL23816AX 46093 UPON GEAR EXTENSION, DID NOT GET A DOWN INDICATION ON THE RIGHT MAIN LANDING GEAR. GEAR WAS RECYCLED TWICE WITH THE SAME RESULTS. REPLACED BULB AND HAD SAME RESULT. RIGHT GEAR INDICATION CAME ON BY ITSELF AFTER ABOUT 15 MINUTES. DID A FLY-BY AT EWR FOR TOWER TO VERIFY THAT GEAR WAS DOWN. REPLACED WIRE SEGMENTS G352J20, 352AN20 AND G307N20 TO P1-398 PLUG. REPLACED DIMMER BOX B15-60 AND CONTACTS 4 AND 5 IN P1-1344 PLUG IAW DC-8 WDG 32-61-01. REPLACED DOWN LOCK SWITCH IAW DC-8 M.M. 32-60-0. OPS CHECKED GOOD AT THIS TIME. 2L74 4F 4A25 19951229001681995122900168WP 1995 12 29 ABXA9501047 119951228A3260 PROX SWITCH DOUG DC8 DC862 3021970WP RT MLG DOOR OUT OF ADJUST A ABXAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL23804AX 45987 UPON GEAR RETRACTION FROM ILN, GEAR NOT LATCHED LIGHT REMAINED ON. DISCRIMINATOR PANEL (F/E STATION) INDICATED RIGHT MAIN DOOR NOT LATCHED. CYCLED LANDING GEAR WITH NO DIFFERENCE. PROCEEDED TO DESTINATION AT FL 330 AND M.65. COMPLIED WITH MAB DC-8-32-6. MAIN GEAR DOOR CLOSED, PROX. SWITCH ADJUSTMENT AND TEST. OPS CHECKED GOOD. 2L74 4F 4A25 19951229001691995122900169SO 1995 12 29 COMA9512042 119951226A2750 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01267CA 120259 FLAPS DID NOT RETRACT AFTER TAKEOFF. FLAP DISAGREEMENT WARNING. CLEANED FLAP TRACKS AND SYSTEM CHECK NORMAL. ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951229001701995122900170SO 1995 12 29 COMA9512043 119951226A27523203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO011117H1504213888 120117 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. INBD FLAPS STUCK AT 15 DEGREES. REPLACED THE LT INBD FLAP ACTUATOR. 2L72 4T RTA31SO 19951229001711995122900171SO 1995 12 29 COMA9512044 119951227A2750 TRACKS EMB 120 EMB120RT SO TE FLAPS DIRTY A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01246CA 120223 FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY, CLEANED FLAP TRACKS AND ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19951229001721995122900172SO 1995 12 29 COMA9512045 119951226A27523430001003 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01267CA5142 971 120259 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. REPLACED THE RT OTBD FLAP ACTUATOR. 2L72 4T RTA31SO 19951229001731995122900173EU 1995 12 29 COMA9531219 119951219A32465006488 WHEEL HALF LORAL 5005267 SAAB SF340 SF340A 7850100EU NLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01140N 14716288 NOV84152 340A140 NOSE WHEEL ASSEMBLY S/N NOV84-152 WAS REMOVED FROM A/C FOR TIRE WORN TO LIMITS. UPON DISASSEMBLY AND EDDY CURRENT INSPECTION, FOUND OUTBOARD WHEEL HALF TO HAVE APPROXIMATELY .25 INCH CRACK. REMOVED WHEEL ASSEMBLY FROM SERVICE. 2L72 4T RTA52EU 19951229001741995122900174EU 1995 12 29 COMA9531220 119951219A32465009237 WHEEL ASSY LORAL 5010488 SAAB SF340 SF340A 7850100EU RT MLG CRACKED A COMAK NONE O OTHER ININSP/MAINT 1 SO01343CA1027313 FEB0248 340A024 UPON LANDING IN CVG, MAINTENANCE REPORTED RIGHT INBOARD MAIN WHEEL ASSEMBLY P/N 5010488 S/N FEB 97-0248 WAS FLAT AND PART OF INBOARD SUB-ASSEMBLY FLANGE HAD SEPARATED. WHEEL ASSEMBLY REMOVED FROM SERVICE. 2L72 4T RTA52EU 19951229001751995122900175EU 1995 12 29 COMA9531221 119951219A77224078T09P02 ITT TRIMMER SAAB SF340 SF340A 7850100EU LT ENG DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO01358CA 340A047 LEFT ENGINE ITT INDICATION FLUCTUATES, RETURNED TO CVG FOR REPAIR. REPLACED THE ITT TRIMMER. 2L72 4T RTA52EU 19951229001761995122900176 1995 12 29 COMA9560627 419951227A34183995100207A COMPUTER CNDAIRCL600 CL6002B19 EA AVIONICS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01940CA3738 1163 7048 STALL FAIL MESSAGE AFTER TAKEOFF. REPLACED THE STALL PROTECTION COMPUTER. 2L72 4F RTA21EA 19951229001771995122900177EA 1995 12 29 COMA9560628 119951227A2750860D10018 FECU CNDAIRCL600 CL6002B19 EA TE FLAPS DEFECTIVE A COMAO OTHER J WARNING INDICATION DEDESCENT 1 SO01952CA49 7092 FLAPS FAIL MESSAGE ON EICAS. ZERO FLAP LANDING AT MDT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2L72 4F RTA21EA 19951229001781995122900178NM 1995 12 29 DL72E954786 119951219A3350 BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27283WA 21485 DURING STANDBY POWER CHECK, FIRST CLASS EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK OPERATION NORMAL. 2L73 4F A3WE 19951229001791995122900179NM 1995 12 29 DL72E954787 119951221A324140533 TRANSDUCER BOEING727 727247 138408FNM NR 3 WHEEL FAULTY A DALAO OTHER O OTHER TXTAXI/GRND HDL 1 SO27282WA 21484 IR - RT BRAKE EXTREMELY WEAK. NR 3 BRAKE AT FAULT, TURNED OFF ANTI-SKID BRAKES, OPS NORMAL. REPLACED NR 3 TRANSDUCEDR ANTI-SKID, OPS NORMAL. 2L73 4F A3WE 19951229001801995122900180NM 1995 12 29 DL72L954775 119950829A7110 COWLING 6519685453 BOEING727 727232 1384082NM NR 3 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27508DA DL4 21310 DURING SHOP INSPECTION, NR 3 ENGINE NOSE COWL WAS FOUND WITH CRACKED WEB AT STA 69.00 AT 4'CLOCK POSITION, REPAIRED PER SRM 54-00. 2L73 4F A3WE 19951229001811995122900181NM 1995 12 29 DL72L954782 119950829A711065196854539 FRAME 6519685453 BOEING727 727232 1384082NM NR 3 ENG COWL CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27508DA DL4 21310 CAP FRAME CRACKED AT STATION 69.00, AT THE 7:00 POSITION. DURING SHOP INSPECTION OF NR 3 ENGINE NOSE COWL, REPAIRED CAP PER SRM 54-10-3. 2L73 4F A3WE 19951229001821995122900182NM 1995 12 29 DL72L954783 119950829A711065196854539 NOSE COWL 6519685453 BOEING727 727232 1384082NM NR 3 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27508DA DL4 21310 DL4 CAP-FRAME CRACKED INSIDE AT ACCESS HOLE NR 2. DURING SHOP INSPECTION OF NR 3 NOSE COWL, REPAIRED PER SRM 54-10-3, FIG NR 3. 2L73 4F A3WE 19951229001831995122900183NM 1995 12 29 DL72S954747 119951219A3350 BATTERY PACK BOEING727 727232 1384082NM RT OVERWING DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27407DA 21151 EMERGENCY LIGHT OUT LOWER RT OVERWING FAIRING. REPLACED EMERGENCY LIGHT BATTERY PACK. CKS NORMAL. 2L73 4F A3WE 19951229001841995122900184NM 1995 12 29 DL72S954750 119951221A3234 SOLENOID A420060283 BOEING727 727232 1384082NM GEAR SELECTOR FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27405DA UNK 21149 IRR - ON TAKEOFF, GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION. PUT GEAR HANDLE BACK DOWN. DIVERTED TO DEN DUE TO GEAR HANDLE. CORRECTIVE ACTION - REPLACED LANDING GEAR HANDLE LATCH LEVER SOLENOID PER DELTA M/M 32-31-16. CYCLED GEAR SEVERAL TIMES, ALL NORMAL. 2L73 4F A3WE 19951229001851995122900185NM 1995 12 29 DL72S954753 119951208A5522 SKIN 657278420 BOEING727 727232 1384082NM RT ELEVATOR PUNCTURED A DALAK NONE O OTHER ININSP/MAINT 1 SO27484DA DL90068RH 20864 DURING A SHOP INSPECTION FOUND PUNCTURE DAMAGE TO RT ELEVATOR SKIN AT AT THE OUTBOARD END. REPAIR WAS INSTALLED PER SRM 55-20-3. 2L73 4F A3WE 19951229001861995122900186NM 1995 12 29 DL72S954761 119951223A2910651784961DM TUBE BOEING727 727232 1384082NM B HYD SYS WORN A DALAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO27408DA 21152 PIREP LOSS OF ALL HYD B-QUANTITY IN-FLIGHT. FOUND HYD LINE IN LEFT BODY FAIRING AREA LEAKING. REF IPC 29-14-0-6, ITEM 155, AND ITEM 160. HOLE IN LINE DUE TO CHAFING. 2L73 4F A3WE 19951229001871995122900187NM 1995 12 29 DL72S954771 119951226A5210 SKIN BOEING727 727232 1384082NM L1 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27529DA 21703 FOUND ON C2 LETTER CHECK, MAIN ENTRY DOOR OUTER SKIN CRACKED .75 INCH LOWER AFT CORNER. REPAIRED PER MM 52-11-01. 2L73 4F A3WE 19951229001881995122900188NM 1995 12 29 DL72W954754 119951222A291065178494061 LINE BOEING727 727247 138408FNM B HYD SYST LEAKING A DALAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO272814W 20870 LOSS OF B-SYSTEM QUANITITY DOWN TO ZERO - ON FINAL AFTER GEAR DOWN BRAKE PRESSURE ABOVE 1500 PSI, NR 1 B-SYSTEM PUMP OFF. NR 2 SYSTEM TURNED OFF AND FLICKER OF LOW PRESSURE LIGHT. CORRECTIVE ACTION - FOUND B-HYDRAULIC LINE LEAKING. REPLACED SAME, LEAK CKS AND PUMP OPS CK GOOD. 2L73 4F A3WE 19951229001891995122900189NM 1995 12 29 DL72W954772 119951226A3350 BATTERY PACK 900835A BOEING727 727247 138408FNM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO272819W UA4710 21057 TWO AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. OPS CK GOOD. 2L73 4F A3WE 19951229001901995122900190NM 1995 12 29 DL73E954745 119951221A5230 RIB 6547952524 BOEING737 7372S3 NM C 2 DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27367DL 360 21774 DURING SHOP INSPECTION, C-2 CARGO DOOR WAS FOUND WITH CRACKS TO A RIB AND SUPPORT ANGLE AT ACCESS HOLE NR 23. ACCOMPLISHED REPAIRS PER ERA 271679-14AD AND SRM 52-30-2. 2L72 4F RTA16WE 19951229001911995122900191NM 1995 12 29 DL757954765 119951225A3510 PBE 4566M37B BOEING757 757232 1384965NM COCKPIT MALFUNCTIONED A DALAK NONE O OTHER ININSP/MAINT 1 SO27631DL E9235522 23612 PBE INDICATOR EXPOSED. REPLACED SAME. 2L72 4F RTA2NM 19951229001921995122900192NM 1995 12 29 DL757954769 119951226A3397 WIRE BOEING757 757232 1384965NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27616DL 22823 INTERIOR EMERGENCY TRACK LIGHTING ON FLOOR NEXT TO FIRST CLASS CLOSET INOP. FOUND BROKEN WIRE. SPLICED SAME, OPS CKS GOOD. 2L72 4F RTA2NM 19951229001931995122900193NM 1995 12 29 DL76E954788 119951222A3610 DUCTS BOEING767 767232 1385132NM LT WING BLOWN A DALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27112DL 22224 IR - ON DEPARTURE, LOUD BANG HEARD FOLLOWED BY BAD SMELL IN CABIN. PACK OFF LIGHT FOLLOWED BY NO AIR PRESSURE IN LT MANIFOLD. RETURNED FRA. FOUND ONE LT WING L/E SUPPLY DUCT AND ONE C/O SUPPLY DUCT. REPLACED BLOWN DUCTS, LEAK AND OPS CHECK NORMAL. 2L72 4F RTA1NM 19951229001941995122900194NM 1995 12 29 DL76S954749 119951221A335020131A BATTERY PACK BOEING767 767332 1382001NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27125DL 24075 NR 1 DOOR LEFT AND RIGHT EXIT EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK, CHECKS GOOD. 2L72 4F RTA1NM 19951229001951995122900195WP 1995 12 29 DLL10954767 119951225A2910 PRESS MODULE 1549211107 LKHEED1011 10113851 5265010WP C HYD SYST CRACKED A DALAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27727DA 2876 193C1167 UPON LOWERING LANDING GEAR, C-HYDRAULIC SYSTEM PRESSURE WENT TO ZERO AND QUANTITY WENT TO ONE-QUARTER. GEAR LOCKED DOWN OK. FOUND C-SYSTEM PRESSURE MODULE IN STABILIZER AREA CRACKED. REPLACED MODULE AND CHECKED CASE DRAIN FILTERS. LEAK CHECK AND OPS CHECKS OK. 2L73 4F A23WE 19951229001961995122900196WP 1995 12 29 DLL15954758 119951223A33505165741 POWER SUPPLY LKHEED1011 10113853 5265020WP CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27751DA 193W1166 DURING LAYOVER, FOUND AFT LEFT AND RIGHT EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY PACK. 2L73 4F A23WE 19951229001971995122900197NM 1995 12 29 DLM11954748 119951222A3350 BATTERY PACK 6044113 DOUG MD11 MD11 3023602NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27804DE 857 48475 DURING INSPECTION, CABIN EMERGENCY LIGHTS FAIL TO TEST. REPLACED BATTERY PACK, OPERATION NORMAL. 2L73 4F RTA22WE 19951229001981995122900198NE 1995 12 29 DLM88954746 219951221A7261 ENGINE 20495061 DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 OIL LEAK A DALAA UNSCHED LANDING BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CLCLIMB 1 SO27920DE5842 53423 726984 ATB/MCO - SMOKE IN CABIN OIL SMELL. UNABLE TO ISOLATE DUE TO TIME AVAILABLE BEFORE LANDING. FOUND RT AIR CYCLE MACHINE SYSTEM FILLED WITH OIL. FORWARD RT PACK TO MCO AND PLA. DISC SENSE LINE TO FLOW CONTROL VALVE. ALSO, FORWARD RT CROSS-FEED VALVE CLOSED TO MCO AND PLA. REPLACED NR 2 ENGINE DUE TO OIL LEAK IN COMPRESSOR SECTION. 2L72 4F4 FRTA6WE E9NE 19951229001991995122900199NM 1995 12 29 DLM88954760 119951223A3260SS092200017023 SWITCH DOUG MD88 MD88 3023688NM MLG FAILED A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27986DL IDL73ODL 53313 ON TAKEOFF, THE LANDING GEAR WARNING HORN CAME ON (UNTIL IT WAS RAISED). WHEN GEAR HANDLE WAS RAISED, THE RED LIGHT STAYED ON AND THE GEAR DOOR LIGHT WENT OUT. CYCLED THE LANDING GEAR AND GOT 3 DOWN AND LOCKED (NORMAL INDICATIONS). WHEN GEAR WAS RAISED AGAIN, THE RED WARNING LIGHT REMAINED LIT. REPLACED SWITCH S-320, SYSTEM CKS NORMAL PER M/M. 2L72 4F RTA6WE 19951229002001995122900200NM 1995 12 29 DLM88954768 119951226A2760 SPOILER LIGHT DOUG MD88 MD88 3023688NM COCKPIT ILLUMINATED A DALAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 SO27918DL 49583 SPOILER DEPLOYED, MESSAGE ILLUMINATED ON OAP. MSG ON WITH HANDLE ARMED. ALL SPOILERS DOWN FWD TO MCO AND PLAC PER MEL 27-00-32. NO MRR, REJECTED 12-28-95 GT 595. 2L72 4F RTA6WE 19951229002011995122900201NE 1995 12 29 DLM88954774 219951226A7250 TURBINE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED A DALAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 SO27928DL19416 49715 718134 CLIMBING THROUGH FL 240, FELT A STRONG JOLT AND LOUD BANG, THE RT ENGINE EPR AND N1 BEGAN TO DETERIORATE, BUT ALL ELSE WAS NORMAL. ENGINE SHUT-DOWN BEFORE LANDING. FOUND METAL IN T/P. CORRECTIVE-REPLACED NR 2 ENGINE AND T/R. REROUTED TO SHOP. SUPPLEMENT: (03-07-96). SHOP EXAMINATION SHOWED 3RD STAGE TURBINE INNER AIR-SEALING ANTI-ROTATION PIN (QTY-1) MISSING. PIN DAMAGED TURBINE BLADES, RESULTING IN TURBINE FAILURE. 2L72 4F4 FRTA6WE E9NE 19951229002021995122900202NM 1995 12 29 DLM88954785 119951219A3320R52102 BALLAST DOUG MD88 MD88 3023688NM CABIN FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27930DL 49717 F/A AND GROUND CREW SMELLED ELECTRICAL BURNING IN AFT CABIN. FOUND OVHD LIGHTS INOP. BALLAST 26BD INOP. REPLACED BALLAST, OPERATION NORMAL. 2L72 4F RTA6WE 19951229002031995122900203NM 1995 12 29 DLM90954773 119951226A5244 ACCESS PANEL 29000322C DOUG MD90 MD9030 3023690NM NR 2 ENGINE MISSING A DALAO OTHER D INFLIGHT SEPARATION ININSP/MAINT 1 SO27909DA NONE 53389 POST-FLIGHT, NR 2 ENGINE LATCH ACCESS PANEL FOUND MISSING. REPLACED NR 2 ENGINE ACCESS PANEL. FERRY FLT TO DFW FOR REPAIRS. 2L72 4F RTA6WE 19951229002041995122900204NE 1995 12 29 RRXA9500002 219951223A7200 ENGINE DOUG DC8 DC863 302198AWP PWA JT3D JT3D7 52039NE NR 1 BIRD STRIKE A RRXAE ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP15796AL 46054 40621 AT APPROX 500 FT AGL NR 1 ENGINE COMPRESSOR STALLED THREE TIMES. TOWER REPORT SPARKS AND FLAMES COMING FROM NR 1 ENGINE. NR 1 ENGINE EGT WAS AT 510 DEGREES CELSIUS ALL OTHER ENGINE INDICATIONS WERE NORMAL. NR 1 ENGINE SHUTDOWN AS A PRECAUTION AND CONTINUED FLIGHT TO KATL. MAINTENANCE FOUND NR 1 ENGINE COMPRESSOR AND TURBINE SECTIONS, NR 1 ENGINE NOSE COWL, AND BI-DUCTS DAMAGED AS A RESULT OF MULTIPLE BIRD INGESTION. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE, NR 1 ENGINE NOSE COWL, AND BI-DUCTS. NR 1 ENGINE OPERATED NORMALLY ON GROUND RUN. 2L74 4F4 F 4A25 1E8 19951229002051995122900205NM 1995 12 29 SCNA95301 119951223A3350S106 BATTERIES BOEING727 727225 1384077NM CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15282SC 22558 THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN THE ABOVE LIGHT. OPS CHECKED GOOD PER MM 33-50-101. 2L73 4F A3WE 19951229002061995122900206NM 1995 12 29 SCNA95302 119951224A3350S106 BATTERIES BOEING727 727227 1384078NM AFT AIRSTAIR DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15275AF 22092 THE AFT AIRSTAIR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN THE ABOVE LIGHT PER B727 MM 33-50-71. LIGHT OPS CHECKED GOOD. 2L73 4F A3WE 19951229002071995122900207SO 1995 12 29 SWIA95696 119951213A2710 CONTROL CABLE EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LT AILERONS WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07213SW 120277 LT AILERON CABLES WORN OUTBOARD OF NACELLE. REPLACED LT AILERON CABLES PER MM 27-00-01. 2L72 4T4 TRTA31SO E20NE 19951229002081995122900208SO 1995 12 29 SWIA95697 119951213A2710 CABLES EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE RT AILERON WORN A SWIAK NONE O OTHER ININSP/MAINT 1 NM07213SW 120277 RT AILERON CABLES WORN OUTBOARD OF NACELLE. REPLACED RT AILERON CABLES PER MM 27-00-01. 2L72 4T4 TRTA31SO E20NE 19951229002091995122900209NE 1995 12 29 SWIA95698 319951217A61117801009 BLADE TIP EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE RT PROP DAMAGED A SWIAO OTHER E VIBRATION/BUFFET CLCLIMB 1 NM07207SW 120266 VIBRATION ON CLIMB-OUT FROM SLC, FOUND RT PROPELLER DAMAGED, ALL ENGINE PARAMETERS WERE NORMAL FOR TAKEOFF AND CLIMB. FOUND DAMAGED TO NR TWO BLADE TIP. PROPELLER REMOVED FROM SERVICE. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 19951229002101995122900210SO 1995 12 29 SWIA95699 119951219A3260 PROX SWITCH EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE LANDING GEAR OUT OF ADJUST A SWIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NM07232SW 120306 AFTER TAKEOFF, RECEIVED RED LANDING GEAR LIGHTS. GREEN EXTINGUISHED. CYCLED GEAR 9-10 TIMES. RECEIVED COMBINATION OF A AND/OR B-SYSTEM RED LIGHTS ON ALL THREE GEARS. ADJUSTED PROXIMITY SWITCH TARGETS ON BOTH MAIN GEARS. OPERATIONAL CHECKS WERE GOOD. 2L72 4T4 TRTA31SO E20NE 19951229002111995122900211WP 1995 12 29 SWIA95700 219951223A7530 BLEED VALVE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RIGHT MALFUNCTIONED A SWIAA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 NM072720B AC715 RT INTAKE HEAT DOES NOT ILLUMINATE WHEN PROPELLER ENGINE HEAT SWITCH IN THE ON POSITION. REPLACED RT INLET BLEED VALUE. OPERATION CHECKS GOOD. 1L72 4T4 T A8SW E4WE 19951229002121995122900212SO 1995 12 29 SWIA95701 119951225A5230 SEAL EMB 120 EMB120ER 3260203SO PWA 118 PW118A NE CARGO DOOR LOOSE A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM07207SW 120266 CLIMBING THROUGH 24,000 FEET, CABIN ALTITUDE LIGHT CAME ON. TESTED ALTITUDE WARNING SWITCH SYSTEM IAW MM 21-30-08. SYSTEM OPERATION CHECKS GOOD. FOUND CARGO DOOR SEAL PULLED OUT. REINSTALLED SEAL AS NEEDED. PRESSURIZED AIRCRAFT. CARGO DOOR LEAK CHECK GOOD. 2L72 4T4 TRTA31SO E20NE 19951229002131995122900213SW 1995 12 29 SWIA95702 119951225A3230 GEAR HANDLE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LANDING GEAR MISINSTALLED A SWIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM0727278 AC732 LANDING GEAR WILL NOT RETRACT. CHECKED EMERGENCY VALVE PIP PIN. ALL CIRCUIT BREAKERS ARE IN. TRIED GEAR OVERRIDE, STILL COULD NOT GET GEAR TO RETRACT. HYDRAULIC PRESSURE CHECKS IN GREEN. FOUND LANDING GEAR OVERRIDE BUTTON IMMOBILE DUE TO INSTALLATION OF INCORRECT SCREW STYLE IN BOTTOM MOUNT HOLE FOR LANDING GEAR SELECTOR HANDLE ASSEMBLY. INSTALLED SHORTER SCREW IN BOTTOM MOUNT HOLE. ALL LANDING GEAR OPERATES NORMALLY NOW. 1L72 4T4 T A8SW E4WE 19951229002141995122900214NM 1995 12 29 UPS205161 119951226A3350 BATTERY BOEING727 727247 138408FNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01211UP 21700 MAINTENANCE FOUND CREW FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD. 2L73 4F A3WE 19951229002151995122900215EU 1995 12 29 9521363230 119951224A3350321430 BATTERY PACK AIRBUS320 A320211 3930320EU CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01330NW 307 DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED BATTERIES AT THE FORWARD LEFT CABIN, 10WL. REPLACED BATTERY PACKS, OPS CHECK OK. 2L72 4F RTA28NM 19951229002161995122900216 1995 12 29 9521379310 419951224A2350 MICROPHONES DOUG DC9 DC982 3022082WP LT/CTR COCKPIT INOPERATIVE A NWAAA UNSCHED LANDING O OTHER UKUNKNOWN 1 GL01313RC 48091 CAPTAIN'S AND JUMPSEAT VHF COMMUNICATIONS FAILED EN ROUTE ONT-MSP. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. FOUND MICROPHONES ON BOTH COMMS INOPERATIVE. REPLACED MICROPHONES AND OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002171995122900217 1995 12 29 9521389852 419951225A3197 WIRE DOUG DC9 DC951 3022051WP TAKEOFF WARNING CHAFED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01761NC 47709 TAKEOFF WARNING HORN SOUNDED AS POWER LEVERS WERE ADVANCED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPAIRED CHAFED WIRE TO WARNING SYSTEM. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA6WE 19951229002181995122900218WP 1995 12 29 9521399155 119951225A32225910096 STRUT DOUG DC9 DC914 3022034WP NLG DEFLATED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL018914E 45831 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. NOSE WHEEL WAS STEERABLE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED AND SERVICED NOSE LANDING GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002191995122900219WP 1995 12 29 9521409884 119951222A32225910448563 STRUT DOUG DC9 DC951 3022051WP NLG DEFLATED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01677MC 47756 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. SERVICED NOSE LANDING GEAR STRUT TO PROPER LEVELS OF FLUID AND NITROGEN. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002201995122900220WP 1995 12 29 9521419884 119951225A32225910448563 STRUT DOUG DC9 DC951 3022051WP NLG DEFLATED A NWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL01677MC 47756 LANDING GEAR WOULD NOT RETRACT DUE TO GROUND SHIFT FAILURE AFTER TAKEOFF. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR STRUT AND SERVICED TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002211995122900221WP 1995 12 29 9521429991 119951222A3260 UPLOCK SWITCH DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL018957E 47215 DURING CLIMBOUT, NOSE LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH NO CHANGE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UPLOCK SWITCH. ALSO, REPLACED NOSE GEAR GREEN SAFE AND RED UNSAFE LIGHT ASSEMBLIES. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002221995122900222 1995 12 29 9521439944 419951224A3400 NAV INSTRUMENTS DOUG DC9 DC931 3022065WP COCKPIT FAILED A NWAAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 GL011309T 47316 SEVERAL COCKPIT NAVIGATION INSTRUMENTS FAILED AFTER TAKEOFF FROM DTW. FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. PERFORMED TEST OF INDIVIDUAL COMPONENTS AND ALL SYSTEMS CHECKED NORMAL. PROBLEM COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19951229002231995122900223WP 1995 12 29 9521449862 119951222A3350 BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01771NC 47769 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 20 THROUGH 24 INOPERATIVE. REPLACED BATTERIES IN PACK AT AFT CABIN AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229002241995122900224WP 1995 12 29 9521459864 119951220A3397 WIRE DOUG DC9 DC951 3022051WP CABIN CHAFED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01773NC 47775 DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF FLOOR PROXIMITY EMERGENCY LIGHT WIRING CHAFER AT SIDEWALL. REPAIRED WIRING AND OPERATIONAL CHECK NORMAL. 2L72 4F RTA6WE 19951229002251995122900225WP 1995 12 29 9521469160 119951223A3350 BATTERIES DOUG DC9 DC914 3022034WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018903E 45744 DURING LINE MAINTENANCE INSPECTION, FOUND CENTER CABIN AND LEFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229002261995122900226WP 1995 12 29 9521479609 119951225A335060030451 BATTERY PACK DOUG DC9 DC932 3022066WP LT NACELLE DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229002271995122900227WP 1995 12 29 9521489956 119951223A335060030451 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01923RW 47183 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19951229002281995122900228NM 1995 12 29 9521496717 119951224A278060B8004225 PDU BOEING747 747251F 1384898NM NR 4 LE FLAP FAILED A NWAAAJ UNSCHED LANDING DUMP FUEL J WARNING INDICATION CLCLIMB 1 GL01617US 21121 HKG-NRT - AFTER TAKEOFF, THE NR 4 LEADING EDGE FLAP FAILED TO RETRACT IN NORMAL AND ALTERNATE. CREW FOLLOWED COCKPIT OPERATING MANUAL, DUMPED 50,000 LBS OF FUEL AND DIVERTED FLIGHT TO TPE. REPLACED NR 4 RT L/E PDU AND OPERATIONAL CHECK WAS NORMAL. 2L74 4F A20WE 19951229002291995122900229EU 1995 12 29 9521503215 119951226A3610 CLAMP AIRBUS320 A320211 3930320EU LT WING LOOSE A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01315US 171 DURING CLIMBOUT, RECEIVER 'AIR L WING LEAK' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND DIVERTED TO MEM DUE TO ICING CONDITIONS AT ORIGINAL DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REINSTALLED CLAMP ON EXTERNAL AIR DUCT. OPS AND LEAK CHECK OK. 2L72 4F RTA28NM 19951229002301995122900230NM 1995 12 29 DHL95742004 119951223A3830332000101 WASTE DRAIN BOEING727 7272Q9 138448MNM LAVATORY LEAKING A TDHLAH DEACTIVATE SYST/CIRCUITS K FLUID LOSS UKUNKNOWN 1 SO01742DH 21290 LAVATORY DUMP LEAKING AND FORMING BLUE ICE. DRAINED LAVATORY AND DEFERRED PER DHL GENERAL MAINTENANCE MANUAL. 2L73 4F RTA3WE 19951229002311995122900231WP 1995 12 29 MWEA95540 119951227A25605917689103 EVAC SLIDE COVER DOUG DC9 DC932 3022066WP FWD GALLEY FELL OFF A MWEAK NONE O OTHER ININSP/MAINT 1 GL31401ME 47133 DURING INSPECTION WHEN GALLEY SERVICE DOOR WAS OPENED THE EVACUATION SLIDE COVER FELL OFF. INSPECTED AND REINSTALLED SLIDE COVER. 2L72 4F A6WE 19951229002321995122900232SW 1995 12 29 QXEA9500446 119951214A32302751000062 CAM OZONE 2751046041 SWRNGNSA227 SA227AC 8780603SW LT MLG DAMAGED A QXEAK NONE J WARNING INDICATION APAPPROACH 1 NM09384PH 592 PDX - THE LT MLG WOULD NOT EXTEND, RECYCLED THE LANDING GEAR AND GOT A DOWN AND LOCKED INDICATION AFTER APPROX 15 TO 20 SECONDS. COMPLIED WITH GEAR SWINGS AND FOUND THE LT MLG I/B CAM NEEDED REWORK. REWORKED THE I/B CAM AND COMPLIED WITH GEAR SWINGS. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19951229002331995122900233 1995 12 29 QXEA9500447 419951216A2565S130508 SLIDE ASSY FOKKERF28 F28MK1000 4990808EU GALLEY LOW PRESSURE A QXEAK NONE O OTHER ININSP/MAINT 1 NM09801PH 1703 11097 SEA - THE EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE IS LOW. REMOVED AND REPLACED SLIDE ASSEMBLY AND AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA20EU 19951229002341995122900234NM 1995 12 29 QXEA9500448 119951218A3260864202 PROX SENSOR DHAV DHAV DHC8 DHC8102 2809003NM DRAG STRUT INOPERATIVE A QXEAO OTHER N FALSE WARNING CLCLIMB 1 NM09824PH 157 IDA - THE NOSE GEAR UNSAFE LIGHT DID NOT EXTINGUISH DURING RETRACTION OR FURTHER EXTENSION. ALTERNATE INDICATOR SHOWED DOWN AND LOCKED. AIRCRAFT WAS INSPECTED AND FERRIED TO PDX FOR REPAIR. REMOVED AND REPLACED THE DRAG STRUT PROX SENDOR IAW 32-20-16. ADJUSTED SENSOR IAW 32-20-11. GEAR SWINGS COMPLIED WITH, OPERATIONAL CHECKS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229002351995122900235SW 1995 12 29 QXEA9500449 119951216A32601ENS16 POS SWITCH SWRNGN SWRNGNSA227 SA227AC 8780603SW NLG BROKEN A QXEAO OTHER P NO WARNING INDICATION CLCLIMB 1 NM0926959 662 PDX - THE RED INTRANSIT LIGHT DOES NOT ILLUMINATE DURING RETRACTION OR EXTENSION ON NOSE WHEEL ONLY, BULB TESTS GOOD. REMOVED AND REPLACED UP POSITION SWITCH AND COMPLIED WITH GEAR SWINGS. OPERATIONAL CHECKED GOOD AND A/C WAS RETURNED TO SERVICE. 1L72 4T A8SW 19951229002361995122900236NM 1995 12 29 QXEA9500450 119951222A335010005511 LIGHT DHAV DHAV DHC8 DHC8102 2809003NM COCKPIT MALFUNCTIONING A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09822PH 106 BOI - COCKPIT EMERGENCY FLASHLIGHT ILLUMINATES ON ITS OWN. LIGHT ASSY WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229002371995122900237NM 1995 12 29 QXEA9500451 119951224A33506104781 BATTERY DHAV DHAV DHC8 DHC8102 2809003NM CABIN INOP A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09826PH 214 SEA - PS3 EMERGENCY LIGHT INOP. PS3 BATTERY REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229002381995122900238NM 1995 12 29 QXEA9500452 119951225A3350 CONNECTOR DHAV DHAV DHC8 DHC8102 2809003NM CABIN LOOSE PINS A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09841PH 82 BOI - EMERGENCY LIGHT BY FLIGHT ATTENDANT SEAT INOP. LIGHT CONNECTOR REPAIRED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19951229002391995122900239WP 1995 12 29 SCNA95298 119951218A335020131A BATTERY PACK DOUG DC10 DC1010 3022110WP CABIN DISCHARGED A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15571SC 46645 EMERGENCY FLOOR PATH LIGHTING WAS FOUND INOPERATIVE IN THE MID CABIN. REMOVED AND REPLACED MID CABIN BATTERY PACK IAW MM 33-51-01 AND LIGHTS OPS CHECKED NORMAL. 2L73 4F A22WE 19951229002401995122900240NM 1995 12 29 SCNA95299 119951224A3260656021123 ACCESSORY UNIT BOEING727 727259 138408JNM NLG FAILED A SCNAO OTHER N FALSE WARNING CLCLIMB 1 GL15289SC 22475 MCO - ON DEPARTURE AFTER GEAR RETRACTION, NOSE GEAR RED AND GREEN LIGHT REMAINED ON. RECYCLED GEAR WITH SAME RESULT. INSPECTED NOSE GEAR THROUGH VIEWER AND VISUALLY CONFIRMED NOSE GEAR UP AND DOORS CLOSED. CHECKED NOSE GEAR UPLOCK SWITCH, DOWN LOCK SWITCH AND WIRING, NO DEFECTS WERE NOTED. REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT PER B727 MM 32-61-01. JACKED AND SWUNG GEAR NUMEROUS TIMES AND ALL INDICATIONS WERE NORMAL. 2L73 4F A3WE 19951229002411995122900241NM 1995 12 29 SCNA95300 119951224A3230656021132 ACCESSORY UNIT BOEING727 727227 1384078NM LANDING GEAR FAILED A SCNAK NONE J WARNING INDICATION CLCLIMB 1 GL15275AF 22092 ON DEPARTURE TO MSP, LANDING GEAR DID NOT RETRACT NORMALLY ON FIRST ATTEMPT. LANDING GEAR RETRACTED FOLLOWING COM PROCEDURES. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND PERFORMED SUCCESSFUL GEAR SWING PER B727 MM 32-30-00, 32-32-00. 2L73 4F A3WE 19951229002421995122900242EU 1995 12 29 WWMA9500089 119951222A21505419C000 ACM BAG JETSTMJETSTM3201 1500217EU LEFT OVERSERVICED A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15967JS 967 THE FLIGHT CREW REPORTED A SOUR OILY SMELL COMES FROM THE AIR VENTS, WHEN THE LEFT FLOW WAS TURNED ON. UPON INVESTIGATION MAINTENANCE FOUND THE LEFT AIR CYCLE MACHINE TO BE OVERSERVICED. THE ACM WAS RESERVICED AND THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2L72 4T RTA56EU 19951229002661995122900266CE 1995 12 29 1179596CK 119951113A3610 HOSE LEAR 23 23LEAR 5170102CE UNDER BRKR PANELDETERIORATED A AKKFAO OTHER O OTHER CRCRUISE 1 GL2396CK 6695 23016 IN-FLIGHT MAIN DC CIRCUIT BREAKERS TRIPPED. CIRCUIT BREAKER PANEL WAS HOT TO TOUCH. BREAKERS WERE RESET AND A NORMAL LANDING MADE. INSPECTION OF ELECTRICAL SYSTEM AND CIRCUIT BREAKER PANEL REVEALED NO DEFECTS. A BLEED AIR HOSE UNDER THE PANEL WAS FOUND TO HAVE SEVERAL SMALL HOLES IN IT CAUSING THE PANEL TO OVERHEAT. HOSE WAS REPLACED. RECOMMEND INSTALLING INSULATION. (X) 1L72 4J A5CE 19951229002731995122900273NE 1995 12 29 95ZZZX7013 219951207A8530114651 CYLINDER DOUG DC3 DC3C 3021457WP PWA R1830 R183090D 52020NE LT ENG NR 11 HEAD SEPARATED A VLLAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS APAPPROACH 1 GL059923S 117 25964 CP351777 DURING APPROACH, LEFT ENGINE STARTED RUNNING ROUGH. INSPECTION FOUND NR 11 CYLINDER HEAD HAD SEPARATED FROM BARREL. 2L72 4R4 R A669 5E4 19951229002781995122900278CE 1995 12 29 95ZZZX7018 119951207A324301003600 MASTER CYLINDER CESSNA402 402C 207590RCE BRAKE CONTAMINATED A OEZAK NONE O OTHER ININSP/MAINT 1 WP1926150 402C0111 CONSTANT REPORTS OF POOR BRAKES PROMPTED A REMOVAL AND INSPECTION OF MASTER CYLINDER. FOUND SIGNS OF CONTAMINATION BY REMAINS OF DISSOLVED RUBBER. REPLACED MASTER CYLINDER AND HOSES. SUBMITTER BELIEVES BRAKES WERE SERVICED WITH SOMETHING OTHER THAN WHAT IS SPECIFIED IN THE SERVICE MANUAL. 1L72 3O A7CE 19951229002791995122900279CE 1995 12 29 95ZZZX7019 119951201A7810S19211 CLAMP CESSNA207 T207 2073612CE CONT O520 TSIO520G 17040SO TURBO TO PIPE BROKEN A OEZAK NONE O OTHER ININSP/MAINT 1 WP191562U 20700162 PRE-FLIGHT REVEALED LOOSE TAILPIPE. FOUND CLAMP BROKEN. CLAMP APPEARED TO BE HIGH-TIME, BUT ENGINE WAS INSTALLED LESS THAN 50 HOURS EARLIER. SUBMITTER RECOMMENDS CLAMP BE CHANGED EVERY ENGINE CHANGE AND BE TORQUED PROPERLY. 1H71 3O3 O A16CE E8CE 19951229002911995122900291SO 1995 12 29 95ZZZX7031 119951123A792253E19600 VALVE PIPER PA31 PA31350 7103110SO THERMO BYPASS LOOSE CRIMP NUT B APCRK NONE O OTHER ININSP/MAINT 1 NM0127343300 63126 317752163 DURING INSPECTION PER LYCOMING SB 518C, A NUT WAS FOUND LOOSE ON SHAFT. NOTE THAT SERIAL NUMBER OF THIS UNIT IS BEYOND RANGE OF SERVICE BULLETIN AND, THEORETICALLY, HAS BEEN REDESIGNED TO ELIMINATE THIS PROBLEM. (FIFTH VERNATHERM WITH PROBLEM FOUND IN LAST TWO WEEKS.) 1L72 3O A20SO 19951229002971995122900297WP 1995 12 29 HAL95146 119951108A5260 STAIRS DOUG DC9 DC951 3022051WP VENTRAL DOOR CORROSION A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 HNL - INFORMATION FROM C-CHECK NR 142905. SEVERE CORROSION ON VENTRAL STAIRS EXTERIOR SURFACE, RIGHT SIDE APPROXIMATELY MIDWAY, LEVEL 2. REPAIRED PASSENGER AFT ENTRY STAIRWAY DOOR SKIN CUTOUT PER SRM 52-01. (X) 2L72 4F A6WE 19951229002981995122900298WP 1995 12 29 95ZZZX6938 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE NOT TORQUED A R7MAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM11479MA 4 25991 1553SA P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. UNABLE TO TEST HIGH CROSS FLOW. HEAD NOT TORQUED PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229002991995122900299WP 1995 12 29 95ZZZX6939 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11479MA 4 13099 1553SA P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND TO BE SPLITTING PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229003001995122900300WP 1995 12 29 95ZZZX6940 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11479MA 4 24190 1553SA P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229003011995122900301WP 1995 12 29 95ZZZX6941 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11479MA 4 27134 1553SA P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. FOUND PRIMARY SIDE OF NOZZLE PLUGGED, EXCEPT FOR SOLID THIN STREAM AT 40 DEGREE PATTERN POSITION, PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229003021995122900302WP 1995 12 29 95ZZZX6942 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11479MA 4 38139 15535A P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE INSPECTED AND FOUND TO BE EJECTING A SOLID STREAM PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229003031995122900303WP 1995 12 29 95ZZZX6943 219950308A731331032358 NOZZLE ASSY MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP NR 1 ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11479MA 4 C10011 15535A P36379C ENGINE WILL NOT START. HIGH EGT AND HUNG AT 24 PERCENT RPM. NOZZLE FOUND LEAKING PER SPECS. 1H72 3T4 TRTA10SW E4WE 19951229003041995122900304EU 1995 12 29 95ZZZX6944 119951118A2610B332M FIRE DETECTOR BOLKMS105 BO105S 5626006EU NR 1 ENGINE FAULTY A ERAAO OTHER N FALSE WARNING CRCRUISE 1 AL03423EH 100 S543 NR 1 FIRE LIGHT BLINKED NUMEROUS TIMES AFTER FLYING THROUGH CONSIDERABLE RAIN. LIGHT WOULD STAY ON FOR 6 OR 7 SECONDS AT A TIME, THEN GO OUT. 1G72 3U H3EU 19951229003151995122900315EU 1995 12 29 95ZZZX6955 119951107A624010594575 TRANSMITTER BOLKMS117 BK117B1 5626012EU MAST MOMENT DEFECTIVE B TI1RK NONE O OTHER ININSP/MAINT 1 SW05215AE126 E080698 7216 TRANSMITTER UNRELIABLE AND INTERMITTENTLY WILL NOT CALIBRATE. UNIT WAS OVERHAULED IN JULY, 1995, STILL UNDER WARRANTY. 1G72 3U H13EU 19951229003301995122900330WP 1995 12 29 95ZZZX6970 119951113A217017946081 COALESCER BAGS DOUG DC9 DC983 3022083WP CABIN CONTAMINATED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059409F 53121 STL - FLT 176 - DURING CRUISE, EXPERIENCED SMOKE IN CABIN AND COCKPIT. TURNED OFF RIGHT SUPPLY HIGH PRESSURE BLEED AIR, SMOKE DISSIPATED. FOUND WATER SEPARATOR COALESCERS OIL CONTAMINATED, MFG PN 179460-8-1. REPLACED WATER SEPARATOR COALESCERS AND AIR CONDITIONING SYSTEM OPERATION CHECKED NORMAL. 2L72 4F RTA6WE 19951229003341995122900334EU 1995 12 29 95ZZZX6974 119950925A6322355A34107701 SHAFT NUT AEROSPAS355 AS355F 8680806EU BLOWER FAN LOOSE A NYBAK NONE O OTHER ININSP/MAINT 1 EA115776D 5030 DURING C/W AD 88-25-09, RECEIVED INDICATION OF 3.0 IPS. TORQUED FAN NUT BECAME UNTORQUED. UPON PERFORMING A TEAR DOWN AND VISUAL INSPECTION, FOUND FAN NUT LOOSE ON SHAFT CAUSING BEARING TO SPIN FREELY ON SHAFT CAUSING GROOVES ON SHAFT. REPLACED SHAFT AND BEARINGS AND ALL HARDWARE WITH NEW. TIGHTENED NUT TO PROPER TORQUE. NO OTHER DEFECTS NOTED AT THIS TIME. 1G72 3U H11EU 19951229003361995122900336EU 1995 12 29 95ZZZX6976 119951010A6320350A32313400 SWITCH SNIAS 350 AS350B 8680801EU GEARBOX PRESS INTERMITTENT A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 1168 SWITCH INTERMITTENT INOP, VARIABLE INDICATOR LIGHT STRENGTH. RMA NR R004206. 1G71 3U H9EU 19951229003371995122900337EU 1995 12 29 95ZZZX6977 119951006A7712305731366 INDICATOR SNIAS 350 AS350B 8680801EU ENGINE TORQUE FAILED A S9HAK NONE O OTHER ININSP/MAINT 1 WP19208755 253 1168 THIS INDICATOR WAS INSTALLED DURING TROUBLESHOOTING OF TORQUE SYSTEM. SHORTLY THEREAFTER, IT BEGAN SPINNING INTERMITTENTLY ON POWER UP AND WOULD NOT FIND ZERO. ORIGINAL INDICATOR WAS REINSTALLED. RMA NR R004242. 1G71 3U H9EU 19951229003381995122900338 1995 12 29 95ZZZX6978 419951106A34143839949002 INDICATOR SNIAS 350 AS350B 8680801EU COCKPIT AIRSPEEDREADS LOW A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 4924 1168 INDICATES 8 KNOTS LOW RMA NR R004613. 1G71 3U H9EU 19951229003391995122900339EU 1995 12 29 95ZZZX6979 119951102A6520350A33215001 BEARING SNIAS 350 AS350B 8680801EU T/R LOOSE A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 1168 BEARING UNSTAKED. RMA NR 4004596. 1G71 3U H9EU 19951229003401995122900340EU 1995 12 29 95ZZZX6980 119951103A3213350A75205006 SHOCK ABSORBER SNIAS 350 AS350B 8680801EU MLG LEAKS A S9HAK NONE K FLUID LOSS ININSP/MAINT 1 WP1920875 1168 SHOCK ABSORBER LEAKS. RMA NR 4004602. 1G71 3U H9EU 19951229003411995122900341EU 1995 12 29 95ZZZX6981 119951003A65207704411 SEAL SNIAS 350 AS350B 8680801EU T/R GEARBOX LEAKS A S9HAK NONE K FLUID LOSS ININSP/MAINT 1 WP1920875 1168 MAGNETIC SEAL LEAKS. 1G71 3U H9EU 19951229003421995122900342EU 1995 12 29 95ZZZX6982 119951030A6321350A32501020 LINING SUPPORT SNIAS 350 AS350B 8680801EU ROTOR BRAKE WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 1168 BRAKE LINING WORN TO MINIMUM. 1G71 3U H9EU 19951229003431995122900343NE 1995 12 29 95ZZZX6983 219951028A74219550168770 IGNITER SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE INOP A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 0260 1168 4162 IGNITER INOP. 1G71 3U3 U H9EU E19EU 19951229003441995122900344EU 1995 12 29 95ZZZX6984 119951031A7920350A54111001 HOSE SNIAS 350 AS350B 8680801EU OIL DIST BRACKET CRACKED A S9HAK NONE O OTHER ININSP/MAINT 1 WP1920875 1168 MOUNT BRACKET CRACKED. 1G71 3U H9EU 19951229003451995122900345NE 1995 12 29 95ZZZX6985 219951031A73210164448330 FUEL CONTROL SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE NR 1 ENGINE DEFECTIVE A S9HAK NONE O OTHER ININSP/MAINT 1 WP19208752624 A698B 1168 4162 SLOW/HUNG STARTS AT 1ST PEAK, THEN GOES HOT DURING 1ST START OF DAY ONLY. 1G71 3U3 U H9EU E19EU 19951229003461995122900346EU 1995 12 29 95ZZZX6986 119951018A6320RH2113 COOLER SNIAS 350 AS350B 8680801EU MGB OIL METAL CONTAM A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 319 1188 OIL COOLER REMOVED FOR METAL CONTAMINATION FROM FAILING EPICYCLIC GEAR. 1G71 3U H9EU 19951229003471995122900347EU 1995 12 29 95ZZZX6987 119951018A6320350A32040000 PUMP SNIAS 350 AS350B 8680801EU MGB OIL METAL CONTAM A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 2736 2345 M879 1188 OIL PUMP REMOVED WITH MGB, SN M839, FOR METAL CONTAMINATION FROM FAILING EPICYCLIC GEARS. 1G71 3U H9EU 19951229003481995122900348EU 1995 12 29 95ZZZX6988 119951018A6320350A32010004 REDUCTION GEAR SNIAS 350 AS350B 8680801EU EPICYCLIC ROLLERS FAILED A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 4322 1978 M1463 1188 EPICYCLIC REMOVED FOR 2,000 HR O/H. ON REMOVAL, FOUND SYSTEM CONTAMINATED WITH LARGE AMOUNTS OF METAL RESULTING IN COMPLETE MGB/OIL PUMP, COOLER REPLACEMENT. NO CHIP LIGHTS EVER ILLUMINATED EVEN THOUGH SYSTEM WAS FUNCTIONAL. METAL REACHING PLUG HAD BEEN GROUND TO FINE PASTE WITH LARGE PIECES RETAINED ABOVE MGB AND IN OIL FILTER. SUBMITTER SUGGESTS SHOULD CONSIDER ADDING CHIP PLUG TO MONITOR EPICYCLIC. RMA NR R004466. 1G71 3U H9EU 19951229003491995122900349EU 1995 12 29 95ZZZX6989 119951018A6320350A32030001 REDUCTION GEAR SNIAS 350 AS350B 8680801EU MGB METAL CONTAM A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 2736 2345 M839 1188 REMOVED GEAR FOR METAL CONTAMINATION FROM FAILING EPICYCLIC GEARS. 1G71 3U H9EU 19951229003501995122900350 1995 12 29 95ZZZX6990 419951025A3421AIM5101A GYRO SNIAS 350 AS350B 8680801EU COCKPIT FAILED A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 4314 1188 ATTITUDE GYRO TUMBLES. NEEDS OVERHAUL. 1G71 3U H9EU 19951229003511995122900351EU 1995 12 29 95ZZZX6991 119951018A2913704A34310006 PUMP SPLINES SNIAS 350 AS350B 8680801EU HYDRAULIC WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 495 40185291 1188 HYDRAULIC PUMP SPLINES WORN ON HYDRAULIC PUMP. 1G71 3U H9EU 19951229003521995122900352EU 1995 12 29 95ZZZX6992 119950720A6321350A33501000 SUPPORT ASSY SNIAS 350 AS350B 8680801EU ROTOR BRAKE LINING WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 1188 ROTOR BRAKE LINING WORN. NORMAL WEAR. 1G71 3U H9EU 19951229003531995122900353EU 1995 12 29 95ZZZX6995 119951024A6220126892P BALL JOINT SNIAS 350 AS350B 8680801EU M/R WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 1188 BALL JOINT BEARINGS WORN. NORMAL WEAR. REPLACED 3 EACH. 1G71 3U H9EU 19951229003541995122900354EU 1995 12 29 95ZZZX6996 119950720A6220704A34114008 BALL JOINT SNIAS 350 AS350B 8680801EU M/R WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 1188 BALL JOINT BEARINGS WORN. NORMAL WEAR. REPLACED 3 EACH. 1G71 3U H9EU 19951229003551995122900355EU 1995 12 29 95ZZZX6997 119951018A6230704A33652050 BEARING SNIAS 350 AS350B 8680801EU MAST MAKING METAL A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 1013 1188 MAST BEARING SUSPECTED MAKING METAL. NEEDS EVALUATION. 1G71 3U H9EU 19951229003561995122900356EU 1995 12 29 95ZZZX6998 119951018A622047896WVC47820X BEARING SNIAS 350 AS350B 8680801EU MAST MAKING METAL A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 1013 1188 MAST BEARING SUSPECTED MAKING METAL. NEEDS EVALUATION. 1G71 3U H9EU 19951229003571995122900357EU 1995 12 29 95ZZZX6999 119951018A6230350A37118101 GUIDE SNIAS 350 AS350B 8680801EU SWASHPLATE WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 2927 1188 SWASHPLATE WORN PAST LIMITS. 1G71 3U H9EU 19951229003581995122900358EU 1995 12 29 95ZZZX7000 119951018A6720350A33105803 BELLCRANK SNIAS 350 AS350B 8680801EU T/R CLEVIS WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA MA0385 1188 T/R BELLCRANK INPUT CLEVIS WORN PAST LIMITS. 1G71 3U H9EU 19951229003591995122900359EU 1995 12 29 95ZZZX7001 119951018A6300S40 SPLINES SNIAS 350 AS350B 8680801EU M/R COUPLING WORN A S9HAK NONE O OTHER ININSP/MAINT 1 WP1932GA 495 1188 SPLINES WORN ON COUPLING SLEEVE. 1G71 3U H9EU 19951229003641995122900364NM 1995 12 29 CIHA9502311 119951130A2612 FIRE WIRE BOEING727 727191 1384063NM NR 2 ENGINE SHORTED A C1HAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CLCLIMB 1 WP23504MG 19395 PHX - AFTER DEPARTING & DURING CLIMB AT 8,500 FEET, NR 2 ENGINE FIRE BELL & LIGHT CAME ON. ACCOMPLISHED ENG FIRE CHECK LIST. AFTER BOTH FREON BOTTLES DISCHARGED, LIGHT DID NOT GO OUT. DECLARED EMERG & RETURNED PHX PRIOR TO SHUT DOWN. ALL NR 2 ENGINE PARAMETERS NORMAL. INSPECTED DUCTING FOR BLEED AIR LEAKS. ENG DUCTING AIRWORTHY. T/S NR 2 FIRE SYS IAW MM 26-11-0, FOUND WIRES AT ELEC CONN ON LOWER LOOP SHORTED & OIL SOAKED. REPAIRED AS NECESSARY. REPLACED AURAL WARNING BOX DUE BELL DID NOT SOUND DURING T/S. AURAL WARNING NORMAL IAW MM26-11-0. REPLACED BOTH FIRE BOTTLES & SQUIBS. SYS CHKS SATIS. SEE N/R FOR RII. RAN ENG UP TO 90 PERCENT N2 WITH GEN ON.. FAULT DID NOT RECUR. TAT 53837, TAC 42098.(X)2L73 4F A3WE 19951229003651995122900365GL 1995 12 29 WTAA950305 319951116A61147503503AF PISTON SEAL BAG JETSTMJETSTM3101 1500215EU ROTOL R333 R333482F12 GL LT PROP ASSY TORN A WTAAE ENGINE SHUTDOWN BJKSMOKE/FUMES/ODORS/SPARKS WARNING INDICATION FLUID LOSS CRCRUISE 1 WP17429UE 807 SMF - EN ROUTE ACV TO SMF, SMOKE REPORTED IN CABIN WITH ASSOCIATED LOW OIL PRESSURE INDICATION OF LEFT ENGINE. CREW SECURED LEFT ENGINE IN-FLIGHT. SMOKE IN CABIN DISSIPATED FOLLOWING ENGINE SHUT DOWN. (X) 2L72 4T RTA21EU 6 CP61GL 19960105000011996010500001NM 1996 1 5 9520836603 119951201A5315 FLOOR BEAM BOEING747 747151 1384891NM FS 1050 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01603US 19780 DURING PERIODIC CHECK, FOUND CORROSION ON THE RBL 98.8 LONGITUDINAL FLOOR BEAM, LOWER CHORD AT BS 1050. REPAIRED CHORD (P/N 65B10823-4) PER EA 66-104409. 2L74 4F A20WE 19960105000031996010500003GL 1996 1 5 95ZZZX7038 219951113A723023038126 COMPRESSOR AGUSTAA109 A109C 0260118EU ALLSN 250C 250C20 03013GL NR 2 ENGINE FOD A SNCAOA OTHER UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO1794WH 403 15290 7618 CAEC295173 AIRCRAFT ON PART 91 FLIGHT RETURNING TO BASE, PILOT OBSERVED A TORQUE SPLIT OF APPROXIMATELY 12-15 PERCENT. PILOT MATCHED TORQUE WITH TRIM SWITCH, NOTICED NR 2 ENGINE RUNNING HOTTER AND FASTER THAN NR 1. PILOT REDUCED POWER TO KEEP ENGINES IN NORMAL OPERATING RANGE. FLEW 15 MINUTES TO RETURN TO BASE. AFTER SHUT DOWN, INSPECTION SHOWED F.O.D. DAMAGE TO NR 12 COMPRESSOR. A 'AN3' BOLT WAS FOUND IN THE AIR BOX, ORIGIN UNKNOWN. ALL HARDWARE IN AIR BOX ACCOUNTED FOR. 1G72 3U3 U H7EU E4CE 19960105000191996010500019EU 1996 1 5 95ZZZX7054 119951127A6330350A38101832 CROSSBEAM SNIAS 350 AS350B1 8680811EU MAIN GEARBOX CRACKED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03178EH3500 96 2264 DURING ROUTINE NDT INSPECTION OF MGB SUSPENSION CROSSBEAM, PN 350A38-1018-32, A SURFACE CRACK WAS FOUND APPROXIMATELY .8750 INCH LONG, IN THE RADIUS OF THE THIN ARM THAT ATTACHES TO THE MGB. THE CRACK DOES NOT GO ALL THE WAY THROUGH THE ARM, DEPTH IS UNKNOWN. THIS IS THE FIRST BEAM EVER FOUND CRACKED. NO PITTING OR CORROSION WAS EVIDENT IN THIS AREA, CAUSE OF CRACK CANNOT BE DETERMINED AT OUR LEVEL. 1G71 3U H9EU 19960105000211996010500021NE 1996 1 5 95ZZZX7056 119951203A6510S163564301 DRIVE ASSY SKRSKYS58T S58ET 8141803NE T/R NR 6 DEBONDED A NYBAK NONE O OTHER ININSP/MAINT 1 EA1126567 NYH65493 581514 DURING A DAILY INSPECTION, A MECHANIC NOTICED THE BEARING SLEEVE WAS SHOWING SIGNS OF DEBONDING FROM THE SHAFT. NO OTHER DEFECTS WERE NOTED WITH THE SHAFT. REMOVED AND REPLACED NR 6 TAIL ROTOR DRIVE SHAFT ASSY WITH A SERVICEABLE UNIT. PERFORMED FLIGHT OPS CHECK. NO DEFECTS NOTED. 2G72 4U 1H11 19960105000401996010500040WP 1996 1 5 9521679970 119951226A3222 STRUT DOUG DC9 DC931 3022065WP NLG REQD SERVICE A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 GL019334 47247 LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF DUE TO GROUND SHIFT FAILURE. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTIONARY MEASURE. CYCLED GEAR SEVERAL TIMES. ALL CHECKED NORMAL. WASHED GEAR DUE TO HEAVY GRIT AND SERVICE NOSE GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105000411996010500041WP 1996 1 5 9521689903 119951225A3260 GREEN LIGHT DOUG DC9 DC931 3022065WP NLG MALFUNCTIONED A NWAAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL01953N 47083 ON APPROACH INTO DTW, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. CYCLED GEAR SEVERAL TIMES. ALL CHECKED NORMAL. PROBLEM COULD NOT BE DUPLICATED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105000421996010500042WP 1996 1 5 9521699866 119951225A32600080004003 PROX CONTROL BOX DOUG DC9 DC951 3022051WP LANDING GEAR MALFUNCTIONED A NWAAO OTHER N FALSE WARNING CLCLIMB 1 GL01775NC3565835658 47785 DURING CLIMBOUT FROM BUF, NOSE LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND NORMAL INDICATIONS WERE ARCHIEVED. FLIGHT CONTINUED TO DESTINATION (DTW) AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY CONTROL BOX. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105000431996010500043 1996 1 5 9521709936 419951227A2565113317 SLIDE DOUG DC9 DC931 3022065WP MAIN CABIN DOOR LOW BATTERY A NWAAK NONE L NO TEST ININSP/MAINT 1 GL011799U168023733 47370 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY CHECK. REPLACED SLIDE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105000441996010500044WP 1996 1 5 9521719968 119951227A3350 BATTERIES DOUG DC9 DC931 3022065WP OVERWING EXITS DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019332 47264 DURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS VERY WEAK. REPLACED BATTERIES. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105000451996010500045WP 1996 1 5 9521729903 119951226A335060030451 BATTERY PACK DOUG DC9 DC931 3022065WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105000461996010500046NM 1996 1 5 9521732707 119951228A2130 PRESSURIZATION BOEING727 727225 1384077NM CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01816EA 22553 DURING CLIMB OUT, COULD NOT CONTROL CABIN PRESSURE IN STANDBY OR MANUAL. AIRCRAFT RETURNED DTW, LANDED WITHOUT INCIDENT. PRESSURIZED AIRCRAFT TO 6 PSI IN MANUAL AC/DC, NO EXTERIOR LEAKS NOTED. PRESSURE HELD WITH APU AIR ONLY AND PACKS RUNNING, CONTROLLED RATE AND DESCENT THROUGHOUT ALL MODES OF MANUAL CONTROL PRESSURIZATION. SYSTEM CHECKED OK. 2L73 4F A3WE 19960105000471996010500047WP 1996 1 5 ABXA9501048 119951228A3222 STRUT DOUG DC9 DC941 302207NWP NLG REQD SERVICE A ABXAK NONE J WARNING INDICATION CLCLIMB 1 GL23952AX 47615 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RAISE AND AIRCRAFT FAILED TO GO INTO FLIGHT MODE. PRIOR TO LANDING, LANDING GEAR RETRACTION WAS ATTEMPTED AND LANDING GEAR RETRACTED NORMALLY AND AIRCRAFT WENT INTO FLIGHT MODE. FOUND NOSE STRUT SLOW TO EXTEND DUE TO WATER IN THE STRUT FREEZING. FLUSHED AND SERVICED THE NOSE STRUT WITH HYDRAULIC FLUID PER DC9 MM, CHAPTER 32-21-2. GROUND SHIFT MECHANISM WAS OPS CHECKED IAW DC9 MM, CHAPTER 32-23-1. 2L72 4F A6WE 19960105000481996010500048NM 1996 1 5 DL72S954616 119951120A5512 SKIN BOEING727 727232 1384082NM LT HORIZ STAB WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 FOUND ON CV2 CHECK WEAR MARK FROM CONTACT ON UPPER SKIN OF LT HORIZONTAL STABILIZER INBOARD OF ELEVATOR ACTUATOR ACCESS PANEL AND ABOVE BALANCE BOARD BAY NR 1. 2L73 4F A3WE 19960105000491996010500049NM 1996 1 5 DL72S954778 119951227A5320 WEB BOEING727 727232 1384082NM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27483DA 20863 FOUND ON B1 LETTER CK, LOWER LT TORQUE BOX WEB CRACKED TWO PLACES, 1 INCH AT FORWARD CENTER LIGHTNING HOLE STA 1223 AND .25 INCH CRACK AT THE NEXT LIGHTNING HOLE AFT AND BELOW THE FORWARD CENTER LIGHTNING HOLE. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19960105000501996010500050NM 1996 1 5 DL72S954779 119951227A7110 INLET SKIN BOEING727 727232 1384082NM NR 2 ENGINE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27483DA 20863 FOUND ON B1 LETTER CK, 1 INCH CRACK IN THE NR 2 ENGINE INLET HOUSING AT LOWER AFT CORNER OF PANEL 9516. REPAIRED PER MM 54-30-0. 2L73 4F A3WE 19960105000511996010500051NM 1996 1 5 DL72S954780 119951227A5320 ANGLE BOEING727 727232 1384082NM BS 910 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27483DA 20863 FOUND ON B1 LETTER CK, ANGLE CRACKED STA 910 LT SIDE. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19960105000521996010500052NM 1996 1 5 DL72S954791 119951220A5313 STRINGER BOEING727 727232 1384082NM BS 480 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27407DA 21151 FORWARD LOWER FUSELAGE BS-480 STRINGER 28R SKIN BULGING AND CRACKED. REPAIRED PER DL ERA 302938-14. 2L73 4F A3WE 19960105000531996010500053NM 1996 1 5 DL72W954776 119951227A5510 BEADED DOUBLER BOEING727 727247 138408FNM RT HORZ STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272817W 20873 DURING C/V, FOUND RT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BEADED DOUBLER LOWER PANEL CRACKED. REPAIRED PER SRM 55-20-3 FIG 3. 2L73 4F A3WE 19960105000541996010500054NM 1996 1 5 DL73E954784 119951227A3350 SOCKET 081691 BOEING737 737247 138448DNM CABIN SHORTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27379DL 23606 DURING SVC CK, FOUND LAST SECTION OF CABIN EMERGENCY FLOOR TRACK ESCAPE LIGHTS INOP. PROBLEM CAUSED BY FARTHEST AFT LIGHT SOCKET WAS SHORTED AND FUSE BLOWN IN POWER SUPPLY. REPLACED SHORTED LIGHT SOCKET AND POWER SUPPLY. 2L72 4F A16WE 19960105000551996010500055NM 1996 1 5 DL73S954777 119951227A3350 LIGHT BOEING737 737232 1384475NM LT AFT DOOR INOP A DALAK NONE L NO TEST ININSP/MAINT 1 SO27332DL 23104 LEFT AFT DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. CHECKS NORMAL. 2L72 4F RTA16WE 19960105000561996010500056WP 1996 1 5 DLL10954781 119951227A2910 CAP 22969 LKHEED1011 10113851 5265010WP LT MLG WW BROKEN A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27719DA 193C1135 UPON LOWERING LT GEAR LOST C-SYSTEM FLUID TO ONE-QUARTER. FOUND LEFT LANDING GEAR PHASE CONTROL MODULE CAP BROKEN. REPLACED CAP, SERVICED SYSTEM OPERATION NORMAL. 2L73 4F A23WE 19960105000571996010500057WP 1996 1 5 RRXA9500003 119951227A3297DC26A1415S WIRE DOUG DC8 DC873F 302199FWP RT MLG BROKEN A RRXAO OTHER P NO WARNING INDICATION APAPPROACH 1 WP15870TV 46086 KDAY/KORD - FLT 036 - ON APPROACH, THE RT MLG DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. CYCLED GEAR, NO HELP. MAINTENANCE FOUND A BROKEN WIRE AND TWO PINS PUSHED BACK IN THE ELECTRICAL CONNECTOR. MAINTENANCE REMOVED AND REPLACED THE ELECTRICAL CONNECTOR AND REPAIRED THE BROKEN WIRE. AN OPERATIONAL CHECK OF THE LANDING GEAR, FOUND DOWN AND LOCKED SYSTEM WAS GOOD. 2L74 4F RT4A25 19960105000581996010500058EU 1996 1 5 WWMA9500090 119951228A33202LA00517125 SOCKET SAAB SF340 340B 7860101EU CABIN BURNED A WWMAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP15359SB 340B359 DFW/LRD - FLT 5049 - REPORTED A LIGHT ABOVE WINDOW 14C SEEMED TO HAVE SHORTED OUT. A PASSENGER SAID HE HEARD AN ARCING OR SIZZLING NOISE FOLLOWED BY AN EXTREMELY STRONG ODOR OF BURNED WIRING, THE FIRST OFFICER CONFIRMED THE STRONG ODOR. THE AIRCRAFT DIVERTED TO SAT AND LANDED WITHOUT INCIDENT. UPON INVESTIGATION, MAINTENANCE FOUND A READING LIGHT SOCKET IN THE PASSENGER SERVICE UNIT TO BE BURNED. THE BULB WAS REMOVED AND NO SMOKE OR SMELLS WERE FOUND WHEN THE LIGHTS WERE TURNED ON. THE LIGHT WAS DEFERRED IAW MEL 33-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE WITHOUT INCIDENT. THE LIGHT SOCKET WAS SUBSEQUENTLY REPLACED AND THE MEL WAS CLEARED. 2L72 4T RTA52EU 19960105000591996010500059 1996 1 5 AWXA9500739 419951103A3460 FMC BOEING737 7373G7 1384595NM COCKPIT MALFUNCTIONED A AWXAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 WP28302AW 24009 CORRECTION TO SDR, ORIGINAL SUBMITTED 951103. PHX/SNA - FLT 663 - CREW REPORTED FMC FAILED AT TAKEOFF. HEADING INFORMATION WOULD NOT DISPLAY ON EITHER SYSTEM, BOTH INDICATORS HAD HEADING FLAGS. CREW CONFIRMED THAT ALL CIRCUIT BREAKERS WERE IN. BOTH IRU'S WERE SET IN THE ATTITUDE MODE. UNABLE TO ENTER HEADING INFORMATION IN ISDU. NO FAULTS ON EITHER IRS. CREW RETURNED TO PHX LANDING WITHOUT FURTHER INCIDENT. UPON TOUCH DOWN, ALL FLAGS DISAPPEARED AND SYSTEM APPEARED TO RESET ITSELF. MAINTENANCE PERFORMED IRS OPERATION TEST. SYSTEM NORMAL. C/W IRS BITE CHECK, NO CURRENT OR IN-FLIGHT FAULTS WERE DISPLAYED. AIRCRAFT PUT IN AIR MODE, UNABLE TO DUPLICATE PROBLEM. AIRCRAFT RELEASED FOR SERVICE. (X) 2L72 4F RTA16WE 19960105000601996010500060NM 1996 1 5 AWXA9500751 119951111A3350900835A BATTERY BOEING737 7372M8 1384483NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28141AW 21955 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR AND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AT L1 DOOR, OPS CHECK GOOD. (X) 2L72 4F A16WE 19960105000611996010500061NM 1996 1 5 AWXA9500771 119951118A3350900835A BATTERY PACK BOEING737 7372U9 1384498NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28149AW 22575 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L1 DOOR AND R1 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19960105000621996010500062NM 1996 1 5 AWXA9500796 119951204A3340 TAXI LIGHT WIRE BOEING737 7372A6 138448BNM COCKPIT FAILED A AWXAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 WP28145AW 20194 LAS/ELP - FLT 976 - AIR TURNBACK; ON TAKEOFF ROLL, CREW NOTED A MINOR ODOR. AFTER TAKEOFF AND ON WHEELS UP, SMOKE FILLED THE COCKPIT, SUBSIDING ON FINAL APPROACH. MAINTENANCE FOUND A BURNED WIRE ON THE NOSE TAXI LIGHT SWITCH. REPLACED THE WIRE. FUNCTIONAL AND OPS CHECK ON LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960105000631996010500063NM 1996 1 5 USAA91299 119951206A5320 SUPPORT BOEING737 7372B7 1384560NM BS 520 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 25, WL 207.5. INSTALLED FLOOR BEAM REPAIR, WEIGHT .8 POUNDS, AT BS 520, REPAIRED PER SB 737-53-1120 EA 40385. (X) 2L72 4F A16WE 19960105000641996010500064WP 1996 1 5 USAA951236 119951122A53201795346 CLIP DOUG DC9 DC982 3022082WP BS 1060 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STA 1060 BETWEEN LONGERON 29R AND LONGERON 30R SKIN CLIP. CORROSION TASK NR C57-53300. SPLICED IN SECTION OF SKIN CLIP PER SRM 53-03, FIGURE 3. (X) 2L72 4F A6WE 19960105000651996010500065WP 1996 1 5 USAA951237 119951122A5330 SKIN DOUG DC9 DC982 3022082WP BS 380 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND .020 INCH CRACK IN LIGHTNING STRIKE AREA OF FUSELAGE EXTERIOR SKIN AT STA 380, LONGERON 6L AND LONGERON 7L. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR NR 53-30-11. (X) 2L72 4F A6WE 19960105000661996010500066WP 1996 1 5 USAA951238 119951122A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND CRACK APPROXIMATELY 1 INCH LONG IN SECOND LAYER OF SKIN IN UPPER FORWARD CORNER OF M.E.D. IN FUSELAGE SKIN (X-RAY INSPECTION) SSI 53-11-015. CUT OUT CRACK AND INSTALLED FILLER AND DOUBLERS PER SRM 53-05, FIGURE 25A. (X) 2L72 4F A6WE 19960105000671996010500067WP 1996 1 5 USAA951239 119951122A5313 LONGERON DOUG DC9 DC982 3022082WP BS 1315-1332 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US3741 48097 PIT - DURING Q1/C6 INSPECTION, FOUND .50 INCH BY 9 INCH AREA OF LEVEL 1 CORROSION RESULT FROM UNIQUE EVENT, BROKEN WATER LINE. CORROSION TASK NR C57-53300. LONGERON 28L FROM STA 1315 - STA 1332. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14 AND USAIR EA NR 31600. (X) 2L72 4F A6WE 19960105000681996010500068WP 1996 1 5 USAA951240 119951122A5730 SKIN DOUG DC9 DC982 3022082WP WING LE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND 4.75 INCH CRACK JUST OUTBOARD OF NR 7 SLAT TRACK CUT-OUT LEADING EDGE SKIN. INSTALLED INTERNAL AND EXTERNAL DOUBLERS PER SRM 57-06A, FIGURE 1, AND USAIR EA NR 31672. (X) 2L72 4F A6WE 19960105000691996010500069WP 1996 1 5 USAA951241 119951122A5320 SUPPORT RAIL DOUG DC9 DC982 3022082WP BS 218-541 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LT AND RT FLOOR SUPPORT RAILS, STA 218 - STA 541, FORWARD CARGO, CORROSION TASK NR C51-5330. INSTALLED SPLICE REPAIR PER USAIR TYPICAL REPAIR 53-20-09A. (X) 2L72 4F A6WE 19960105000701996010500070WP 1996 1 5 USAA951242 119951122A531348122611 LONGERON DOUG DC9 DC982 3022082WP BS 228 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, LONGERON 28L SPLICE AT STA 228. CORROSION TASK NR C51-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-02-14. (X) 2L72 4F A6WE 19960105000711996010500071WP 1996 1 5 USAA951243 119951122A5320 FITTING DOUG DC9 DC982 3022082WP BS 182-200 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURING Q1/C6 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED, STA 180 - STA 200, RT SIDE BELOW FORWARD SERVICE DOOR IN FITTINGS AND CUSP ANGLE. CORROSION TASK NR C46-53305. SPLICED IN NEW SECTION OF CUSP AND FITTINGS PER SRM 53-03-5, CONF. J060288-1. (X) 2L72 4F A6WE 19960105000721996010500072WP 1996 1 5 USAA951244 119951122A5311 FRAME DOUG DC9 DC982 3022082WP BS 1250 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37461 48097 PIT - DURNG Q1/C6 INSPECTION, FOUND 2 INCH BY 1 INCH CORRODED AREA PREVIOUSLY REWORKED BELT FRAME, STA 1250, BETWEEN LONGERON 28R AND LONGERON 29R. CORROSION TASK REF C57-53300, LEVEL 1. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-14, FIGURE 5. (X) 2L72 4F A6WE 19960105000731996010500073WP 1996 1 5 USAA951245 119951205A5320 MEMBRANE DOUG DC9 DC982 3022082WP BS 905-927 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN RT CUSP MEMBRANE BETWEEN STA 905 AND STA 927, RT SIDE. MFG NEW MEMBRANE AND SPLICED PER SRM 53-05, FIGURE 97. (X) 2L72 4F A6WE 19960105000741996010500074WP 1996 1 5 USAA951246 119951205A5313 LONGERON DOUG DC9 DC982 3022082WP BS 313 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND .50 INCH CRACK IN LONGERON AT STA 313, LONGERON 16L. REMOVED DAMAGED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-02, FIGURE 2. (X) 2L72 4F A6WE 19960105000751996010500075WP 1996 1 5 USAA951247 119951202A5311953005715 FRAME DOUG DC9 DC931 3022065WP BS 965 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19935VJ40754 48115 PIT - DURING C-3 INSPECTION, FOUND LEVEL 1 CORROSION ON BELT FRAME APPROXIMATELY 12 INCHES LONG AT STA 965 FROM LONGERON 29L TO LONGERON 29R (NOT A CORROSION TASK AREA). REMOVED CORRODED AREA AND INSTALLED ROLLER Z-FRAME SPLICE REPAIR PER SRM 53-03, FIGURE 2A. (X) 2L72 4F A6WE 19960105000761996010500076WP 1996 1 5 USAA951249 119951208A5330 PANEL DOUG DC9 DC931 3022065WP BS 110 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19973VJ73319 47099 PIT - DURING C-3 CHECK INSPECTION, FOUND 2 INCH AREA OF CORROSION ON PRESSURE PANEL AT STA 110 RT, 12 INCHES RT OF AIRCRAFT CENTERLINE. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIGURE 2. (X) 2L72 4F A6WE 19960105000771996010500077WP 1996 1 5 USAA951250 119951208A5400 ANGLE DOUG DC9 DC931 3022065WP BS 980 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19973VJ73319 47099 PIT - DURING C-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK TOP DRAG ANGLE OF PYLON AT STA 980. INSTALLED DOUBLER REPAIR PER SRM 53-04, FIGURE 10, AND USAIR EA NR 31737. (X) 2L72 4F A6WE 19960105000781996010500078NM 1996 1 5 USAA951251 119951207A5330 SKIN BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19285AU31298 23132 CLT - CLT INSPECTION VISUALLY FOUND A 2 INCH SKIN CRACK AT BS 727, STR 17L. INSTALLED DOUBLER PER SRM 53-30-3. (X) 2L72 4F A16WE 19960105000791996010500079EU 1996 1 5 USAA951262 119951211A5320A21156102 ANGLE FOKKERF28 F28MK4000 4990810EU NR 2 WINDOW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU23021 11222 ROA - DURING 'TRANSIT CHECK' VISUAL INSPECTION, FOUND .75 INCH CRACK, RT NR 2 WINDOW CONNECTION ANGLE. INSTALLED REPAIR PATCH, REPAIRED PER EA 31753. (X) 2L72 4F RTA20EU 19960105000801996010500080NM 1996 1 5 USAA951263 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 45 INCHES, STA 328, BL ZERO TO RBL 45 INCHES. CUT OFF T-CAP FROM LBL 28 TO RBL 45, FABRICATED NEW T-CAP AND SPLICES AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000811996010500081NM 1996 1 5 USAA951264 119951206A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 294-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 294 TO STA 312, RBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000821996010500082NM 1996 1 5 USAA951265 119951206A5320CCN1137215 INTERCOSTAL BOEING737 7372B7 1384560NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 312 TO STA 328, RBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000831996010500083NM 1996 1 5 USAA951266 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 947.6 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREAS AROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, LBL 24 TO RBL 6 (6 PLACES). INSTALLED NEW T-CAP SECTION, RBL 37 INCHES TO LBL 60 INCHES, REPAIRED PER TR 53-10-05C, WEIGHT ADDED 3.6 POUNDS AT BS 947.5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000841996010500084NM 1996 1 5 USAA951267 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 947.6 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORRODED AREA ROUND NUTPLATE HOLES, .50 INCH BY .50 INCH, FLOOR BEAM BS 947.6, RBL 34 TO RBL 52, AND LBL 35 TO LBL 41. INSTALLED T-CAP REPAIR ANGLES. REPAIRED PER TR 53-10-05. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000851996010500085NM 1996 1 5 USAA951268 119951206A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 927-947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 927 TO STA 947, RBL 7, ON INTERCOSTAL. REPLACED INTECOSTAL PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000861996010500086NM 1996 1 5 USAA951269 119951206A53201123575 INTERCOSTAL BOEING737 7372B7 1384560NM BS 957 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH, STA 957, RBL 18 - RBL 45, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000871996010500087NM 1996 1 5 USAA951270 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 1050 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH BY .25 INCH HOLE GOUGED IN OUTBOARD J-SECTION OF STRINGER, STA 1050, STR 27L. FORMED AND INSTALLED DOUBLER FOR J-LEG OF STRINGER, REPAIRED PER SRM 53-10-3, FIGURE 1. (X) 2L72 4F A16WE 19960105000881996010500088NM 1996 1 5 USAA951271 119951206A532065516983 SPLICE BOEING737 7372B7 1384560NM BS 907 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 1 INCH CORROSION, STA 907 - STR 26L, ON STRINGER SPLICE. REPLACED SPLICE, REPAIRED PER SRM 51-10-1. REPLACED SPLICE, REPAIRED PER SRM 51-10-1. (X) 2L72 4F A16WE 19960105000891996010500089NM 1996 1 5 USAA951272 119951206A5320 CHORD BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1.5 INCH LONG CRACK IN UPPER COMPRESSION CHORD, BS 727 - RLB 24. INSTALLED ANGLE REPAIR, REPAIRED PER EA NR 40453. (X) 2L72 4F A16WE 19960105000901996010500090NM 1996 1 5 USAA951273 119951206A53146562125502 KEEL BEAM BOEING737 7372B7 1384560NM BS 719-727 WORN A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND WORN AREAS AT SCREW HOLES, BS 719 TO BS 727, RIGHT WHEELWELL ON KEEL BEAM. INSTALLED STRAP, REPAIR PER EA 40457. (X) 2L72 4F A16WE 19960105000911996010500091NM 1996 1 5 USAA951274 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 707 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, RLB 25 LONGITUDINAL FLOOR BEAM LOWER WEB, STA 707, WL 203. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2 AND DWG 65C34537. (X) 2L72 4F A16WE 19960105000921996010500092NM 1996 1 5 USAA951277 119951206A53206546812170 INTERCOSTAL BOEING737 7372B7 1384560NM BS 967 BS 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORRODED AREA BETWEEN BS 967 AND BS 947 AT RBL 7 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000931996010500093NM 1996 1 5 USAA951278 119951206A53206546812198 INTERCOSTAL BOEING737 7372B7 1384560NM BS 984 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA, BS 984, LBL 19, ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000941996010500094NM 1996 1 5 USAA951279 119951206A5347 SEAT TRACK BOEING737 7372B7 1384560NM BS 943 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SPOT OF CORROSION ON SEAT TRACK, .75 INCH BY 6 INCHES, LBL 24, BS 943. INSTALLED NEW TRACK SECTION. REPAIRED PER SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000951996010500095NM 1996 1 5 USAA951280 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 2 INCHES BY 4 INCHES, STA 344, BL ZERO TO LBL 8 INCHES, ON FLOOR BEAM. CUT OUT FLOOR BEAM SECTION, FABRICATED NEW T-CAP, AND REPAIRED DOUBLERS AND INSTALLED PER TR 53-10-13. CORROSION TASK NR C53-107-01. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000961996010500096NM 1996 1 5 USAA951281 119951206A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION, 1 INCH BY 3 INCHES, STA 312 TO STA 328, LBL 12 INCHES, ON INTERCOSTAL. REPLACED INTERCOSTAL, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-01. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000971996010500097NM 1996 1 5 USAA951287 119951206A532065C10592906 INTERCOSTAL BOEING737 7372B7 1384560NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND CORROSION 1.50 INCHES BY 1 INCH, STA 947 TO STA 967, RBL 45 ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000981996010500098NM 1996 1 5 USAA951288 119951206A532065468912183 INTERCOSTAL BOEING737 7372B7 1384560NM BS 986.5-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 1 INCH, STA 986.5 TO 1006 BL ZERO ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105000991996010500099NM 1996 1 5 USAA951289 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH BY .50 INCH CORRODED AREA FLOOR BEAM BS 1016, LBL 15. REMOVED CORROSION AND INSTALLED REPAIR STRAP, REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105001001996010500100NM 1996 1 5 USAA951290 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCHES BY 2 INCHES, STA 312 RBL 35 INCHES ON FLOOR BEAM. REPLACED T-CAP FROM LBL 6 TO RBL 36, REPAIRED PER TR 53-10-13. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105001011996010500101NM 1996 1 5 USAA951292 119951206A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 328-340 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 2 INCHES, STA 328 TO 340, LBL 12 INCHES ON INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-10. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105001021996010500102NM 1996 1 5 USAA951293 119951206A5347654681530 SEAT TRACK BOEING737 7372B7 1384560NM BS 990-1015 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3.50 INCH BY 1 INCH AND 2 INCHES BY 1 INCH, BS 990 AND BS 1015 AT RBL 8 INCHES ON SEAT TRACK. REPLACED TRACK, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960105001031996010500103NM 1996 1 5 USAA951295 119951206A53206545775553 DOUBLER BOEING737 7372B7 1384560NM BS 794 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 5 INCH SLOT IN BEAR STRAP - DOUBLER PREVIOUSLY INSTALLED, BUT NOT PER SRM BS 794 AT S23R. REMOVED PREVIOUSLY INSTALLED DOUBLER AND INSTALLED REPAIR PER EA. (X) 2L72 4F A16WE 19960105001041996010500104NM 1996 1 5 USAA951296 119951206A5210 SKIN BOEING737 7372B7 1384560NM ENTRY DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK IN OUTER SKIN AT UPPER HINGE CUT-OUT AT ENTRY DOOR. INSTALLED EXTERIOR SKIN REPAIR. REPAIRED PER EA 40360. (X) 2L72 4F A16WE 19960105001051996010500105NM 1996 1 5 USAA951297 119951206A531565255896 FLOOR BEAM BOEING737 7372B7 1384560NM BS 675 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, LBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED BY FASTENER HOLE AND CUT-OUT INSTALL REPAIR CHANNEL, DOUBLERS, AND RADIUS FILLER AS REQUIRED BY EO 5791G632 AND EA 40396. (X) 2L72 4F A16WE 19960105001061996010500106NM 1996 1 5 USAA951298 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 675 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK, RBL 24.5, STA 675, IN FLOOR BEAM. CRACK CONTAINED AT AILERON QUADRANT CUT-OUT. INSTALLED REPAIR CHANNEL AMD DOUBLERS, AND RADIUS FILLERS AS REQUIRED PER CO 5791G632 AND EA 40396. (X) 2L72 4F A16WE 19960105001071996010500107NM 1996 1 5 USAA951300 119951206A5320 SUPPORT BOEING737 7372B7 1384560NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK, SEAT TRACK SUPPORT CHANNEL, STA 520, LBL 45, WL 207.5. INSTALLED FLOOR BEAM REPAIR, REPAIRED PER SB 737-53-1120, EA 40385, .8 POUNDS AT BS 520. (X) 2L72 4F A16WE 19960105001081996010500108NM 1996 1 5 USAA951301 119951206A5311 FRAME BOEING737 7372B7 1384560NM BS 616 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, LT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER AND ANGLE, WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EA 40391. (X) 2L72 4F A16WE 19960105001091996010500109NM 1996 1 5 USAA951302 119951206A5311 FRAME BOEING737 7372B7 1384560NM BS 616 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK, STA 616, RIGHT FRAME INBOARD CHORD, FIRST FASTENER ABOVE CENTER WING SKIN. INSTALLED FILLER ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER EA 40391. (X) 2L72 4F A16WE 19960105001101996010500110NM 1996 1 5 USAA951303 119951206A5320 ATTACH ANGLE BOEING737 7372B7 1384560NM BS 639 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, STA 639, STUB BEAM ATTACH ANGLE, RBL 45, WL 207. REPLACED ATTACH ANGLE, WEIGHT CHANGE LESS THAN 1 POUND, REPAIRED PER SRM 51-10-1. (X) 2L72 4F A16WE 19960105001111996010500111NM 1996 1 5 USAA951304 119951206A5320 ANGLE BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 1.50 INCH CRACK, BS 727, RBL 24.5 ON ANGLE. INSTALLED REPAIR ANGLE, REPAIRED PER EA 40453. (X) 2L72 4F A16WE 19960105001121996010500112NM 1996 1 5 USAA951305 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 1044 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND DEEP GOUGE .25 INCH BY 2 INCHES IN UPPER INBOARD LEG OF S26L, BS 1044. INSTALLED STR REPAIR, LESS THAN 1 POUND ADDED, REPAIRED PER SRM 53-10-3, FIGURE 1. (X) 2L72 4F A16WE 19960105001131996010500113NM 1996 1 5 USAA951306 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK IN UPPER RADIUS OF BEAM CAP, STA 520, FLOOR BEAM RBL 25. INSTALLED FLOOR BEAM REPAIR, .8 POUNDS AT BS 520, REPAIRED PER SB 737-53-1120, EA 40385. (X) 2L72 4F A16WE 19960105001141996010500114NM 1996 1 5 USAA951307 119951206A5330 SKIN BOEING737 7372B7 1384560NM BS 227-235 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING 'Q-3' CHECK VISUAL INSPECTION (PREVIOUS REPAIR NOT PER SRM), FOUND UNKNOWN DAMAGED DOUBLER, 8 INCHES BY 9.50 INCHES, BS 227 TO BS 235, S19R TO S20R. INSTALLED DOUBLER PER SRM, REPAIRED PER SRM 53-30-3. (X) 2L72 4F A16WE 19960105001151996010500115WP 1996 1 5 9521749101 119951227A5744 FITTING DOUG DC9 DC915 3022036WP FLAP HINGE CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0191S 31006 47063 DURING H-CHECK, FOUND CORROSION IN THE NR 2 FLAP FORWARD HINGE FITTING, LOWER OUTBOARD BOLT HOLE. REPLACED FITTING (P/N 5912479-502). 2L72 4F A6WE 19960105001161996010500116WP 1996 1 5 9521751154 119951228A5230 FITTING DOUG DC10 DC1040 3023508WP CARGO DOOR CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01154US 46763 DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR LIFT ACTUATOR FITTING, FORWARD LOWER LUG. REPLACED FITTING. 2L73 4F A22WE 19960105001171996010500117WP 1996 1 5 9521769610 119951228A5343 FITTING DOUG DC9 DC932 3022066WP RT MLG CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR RETRACT FITTING PIN. REPLACED FITTING PER OHM 57-40-1. 2L72 4F A6WE 19960105001181996010500118WP 1996 1 5 9521779604 119951228A3350 BATTERY PACK DOUG DC9 DC932 3022066WP AFT EXTERIOR DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01604NW 47222 DURING LINE CHECK, FOUND RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105001191996010500119NE 1996 1 5 9521789948 219951231A7321 FUEL CONTROL DOUG DC9 DC931 3022065WP PWA JT8 JT8D7B 52053NE NR 1 ENGINE MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CRCRUISE 1 GL018929E 45866 653630 NR 1 ENGINE POWER LEVER FROZE AT FL 330. FLIGHT DESCENDED TO FL 270 WHERE THE THROTTLE FREED UP. THE FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL ASSEMBLY WITH A SERVICEABLE UNIT. RUNUP AND LEAK CHECK WERE SATISFACTORY. 2L72 4F4 F A6WE E2EA 19960105001201996010500120WP 1996 1 5 95UAL900362 119951229A26117049 SMOKE DET BULB DOUG DC10 DC1010 3022110WP NR 4 CARGO COMPTFAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP291816U 46615 CARGO PIT NR 4 SMOKE DETECTOR WILL NOT TEST, LIGHT SOURCE FAILED. REPLACED BULB. 2L73 4F A22WE 19960105001211996010500121NM 1996 1 5 95UAL900363 119951229A2612 FIRE DETECTOR BOEING727 727222 1384073NM APU MALFUNCTIONED A UALAK NONE L NO TEST ININSP/MAINT 1 WP297261U 21408 APU WILL NOT FIRE TEST. 2L73 4F A3WE 19960105001221996010500122NM 1996 1 5 95UAL900364 119951229A3350 LAMP BOEING757 757222 1384956NM CABIN FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29535UA 25130 EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT ROW 33ABC IS INOP. LAMP BURNED OUT. REPLACED LAMP. 2L72 4F RTA2NM 19960105001241996010500124NM 1996 1 5 96FDEA00002 119951228A5330 SKIN BOEING727 7272S2F 1384O81NM BS 527 GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 SO25213FE 22935 THERE IS A GOUGE IN FUSELAGE SKIN EXTERIOR AT BS 527, WL 192 BETWEEN STR 18 - 19L. 2L73 4F A3WE 19960105001281996010500128WP 1996 1 5 ABXA9600001 119951228A213010315411 VALVE DOUG DC9 DC941 302207NWP CABIN DEFECTIVE A ABXABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23951AX 47616 AIRCRAFT LOST ALL CABIN PRESSURE FROM FL 350, COULD NOT CONTROL MANUALLY OR AUTOMATICALLY. FOUND FORWARD PRESSURIZATION VALVE OPENING AT 7.6 PSI. REPLACED FORWARD SAFETY VALVE IAW DC-9 MM AND OPS CHECKED GOOD. 2L72 4F A6WE 19960105001291996010500129SO 1996 1 5 COMA9610001 119951231A2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01189CA 120189 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. OUTBD FLAPS DID NOT RETRACT FULLY. COULD NOT DUPLICATE DISCREPANCY. INSPECTED FLAP SYSTEM, NO DEFECTS NOTED AND ACFT RETURNED TO SERVICE. 2L72 4T RTA31SO 19960105001311996010500131EA 1996 1 5 COMA9660001 119951227A2450V210D090BC RELAY CNDAIRCL600 CL6002B19 EA E/E COMPT FAILED A COMAK NONE O OTHER UKUNKNOWN 1 SO01917CA 7017 EMERGENCY LIGHT SYSTEM WILL NOT ARM. AC ESS BUS IS INOP. REPLACED AC SENSOR RELAY KIXD. 2L72 4F RTA21EA 19960105001321996010500132EA 1996 1 5 COMA9660002 119951228A2750855D1005 BPSU CNDAIRCL600 CL6002B19 EA LT/RT TE FLAPS DEFECTIVE A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO01952CA 7092 FLAPS FAILED DURING TAKEOFF ROTATION. REPLACED THE LT AND RT FLAP BRAKE AND POSITION UNITS. 2L72 4F RTA21EA 19960105001341996010500134NM 1996 1 5 QXEA9500453 119951226A33506104781 BATTERY DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09812PH 26 PDX - LEFT HAND FORWARD EMERGENCY LIGHT OUT. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19960105001351996010500135EU 1996 1 5 QXEA9500454 119951226A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 PDX - EMERGENCY EXIT LIGHT AT SEAT 8A IS INOP. BULBS WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105001361996010500136EU 1996 1 5 QXEA9500455 119951227A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 GEG - SEVERAL OVERHEAD CABIN (28V) EMERGENCY LIGHTS ARE INOP. BULBS WERE REPLACED AS REQUIRED. LIGHTS OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105001371996010500137NM 1996 1 5 QXEA9500456 119951227A33508GH00567806 BULBS DORNERDO32 DO328100 2996000NM CABIN BROKEN A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09336PH 3014 SEA - EMERGENCY EXIT LIGHT COVER ABOVE SEAT 11A CAME LOOSE AND SEVERAL BULBS INSIDE WERE BROKEN. BULBS WERE REPLACED AND COVER WAS SECURED. LIGHT OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960105001381996010500138EU 1996 1 5 QXEA9500458 119951228A33501312 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09464US 11063 PDX - EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105001391996010500139NM 1996 1 5 UPS405162 119951228A2613S1048 SENSOR BOEING747 747SR46 NM NR 4 PYLON SHORTED A IPXAO OTHER M OVER TEMP CRCRUISE 1 SO01680UP 20923 CREW REPORTED, RT WING LE OVERHEAT LIGHT ILLUMINATED. RAN ALL ABNORMAL CHECKLISTS AND OVERHEAT LIGHT FAILED TO EXTINGUISH. LIGHT REMAINED ILLUMINATED FOR OVER TWO HRS AFTER ENG SHUTDOWN. FOUND SENSOR S1048 IN PYLON NR 4 SHORTED TO GND. 2L74 4F A20WE 19960105001401996010500140NM 1996 1 5 95ZZZM759 119951109A2913 HYDRAULIC PUMP BOEING707 707330C 138367GNM NR 4 ENGINE LEAKING OIL A CLCAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19707HE 20124 FLT NR 87 - MIAMI - NR 4 ENGINE OIL LOSS TWO GALLONS IN CLIMB AND 2 GALLONS MORE AT REDUCED POWER, RETURNED TO MIAMI. INSTALLED HYDRAULIC PUMP CAVITY BOTTOM PLUG. ENGINE RUN-UP, NO LEAK NOTED. OVERWEIGHT LANDING INSPECTION PERFORMED PER CARD HVY PHASE 1. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2L74 4F 4A26 19960105001411996010500141NM 1996 1 5 95ZZZM760 119951026A33506013211 POWER SUPPLY GRIMES BOEING737 7372P6 NM CABIN INOPERATIVE A A6XAK NONE L NO TEST ININSP/MAINT 1 SO132FOR 6593 21733 FORWARD CABIN EEL POWER SUPPLY INOPERATIVE. CHANGED EEL POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105001421996010500142NM 1996 1 5 95ZZZM761 119951115A532065507429 GUSSET BOEING737 7373Q8 1384670NM BS 219.8 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH LONG SKIN CRACK ON VISUAL INSPECTION AND .625 INCH LONG GUSSET CRACK LEFT C-D WINDOW POST SKIN AND GUSSET BS APPROX 219.8 BY EDDY CURRENT. REMOVED DAMAGED AREA AND INSTALLED FILLERS AND DOUBLERS. REPAIRED PER EA 40239. REFERENCE USAA951217. 2L72 4F RTA16WE 19960105001431996010500143WP 1996 1 5 95ZZZM762 119951202A52303485173503 SEAL DOUG DC8 DC863F 302198FWP MAIN CARGO DOOR FAILED A ARWAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO19441J 2662 45988 AIR TURNBACK, LOUD BANG AND PRESSURE LEAK AT CARGO DOOR AT FL 270. UNABLE TO MAINTAIN PRESSURE WITH FOUR TURBO COMPRESSORS ON AND OUTFLOW VALVE FULL CLOSE. RETURNED TO MIAMI WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MAIN CARGO DOOR SEAL TORN AND DETERIORATED IN SEVERAL PLACES. REMOVED AND REPLACED CARGO DOOR SEAL. LEAK CHECK GOOD. PRESSURIZATION NORMAL ON GROUND CHECK. (M) 2L74 4F 4A25 19960105001441996010500144NE 1996 1 5 95ZZZM763 219951126A7261 OIL SYSTEM DOUG DC8 DC862F 3021972WP PWA JT3D JT3D7 52039NE NR 3 ENGINE FAILED A ARWAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19791AL52536 46150 671137 AIR TURNBACK AFTER APPROXIMATELY 15 MINUTES IN FLIGHT FROM JFK TO SDQ. SHUTDOWN NR 3 ENGINE DUE TO LOSS OF OIL QUANTITY. AIRCRAFT RETURNED TO JFK WHERE MAINTENANCE REPORTED INTERNAL FAILURE OF THE ENGINE OIL SYSTEM. THREE-ENGINE FERRIED AIRCRAFT TO MIAMI FOR ENGINE CHANGE. (M) 2L74 4F4 F 4A25 1E8 19960105001451996010500145EA 1996 1 5 95ZZZM764 119951111A271082700564S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9179 286 DURING INSPECTION, THE LEFT AND RIGHT WING AILERON CABLES WERE FOUND TO BE WORN 40 TO 50 PERCENT BY A PULLEY AT YW 404. THE CABLES WERE REPLACED ON FIELD AVIATION COMPANY WO NR 21978 AT C-CHECK. 2H72 4T RTA13NM 19960105001461996010500146EA 1996 1 5 95ZZZM765 119951030A271082700568S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01433AW8801 305 DURING INSPECTION OF AIRCRAFT IT WAS NOTED THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190RT. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK. (M) 2H72 4T RTA13NM 19960105001471996010500147EA 1996 1 5 95ZZZM766 119951111A271082700565S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA LT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9179 286 DURING INSPECTION, THE LEFT WING AILERON CABLE WAS FOUND TO BE WORN 50 PERCENT BY A FAIRLEAD AT YW 155 LEFT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. 2H72 4T RTA13NM 19960105001481996010500148EA 1996 1 5 95ZZZM767 119951111A271082700567S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9179 286 DURING INSPECTION, THE RIGHT WING AILERON CABLE WAS FOUND TO BE WORN BY A PULLEY AT YW 170 RT. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M) 2H72 4T RTA13NM 19960105001491996010500149EA 1996 1 5 95ZZZM768 119951112A276082700503003 SPOILER CABLE DHAV DHC8 DHC8311 1386006EA WS 90 WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01432AW9179 286 DURING INSPECTION, THE LEFT WING ROLL SPOILER CABLE WAS FOUND TO BE WORN 50 PERCENT AT YW 90 BY A FAIRLEAD. THE CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORKORDER NR 21978 AT C-CHECK. (M) 2H72 4T RTA13NM 19960105001501996010500150SO 1996 1 5 C2XA95IA333 119951115A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001511996010500151SO 1996 1 5 C2XA95IA334 119951115A572012017056019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, NR 5 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001521996010500152SO 1996 1 5 C2XA95IA335 119951115A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING NR 15, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001531996010500153SO 1996 1 5 C2XA95IA356 119951115A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, NR 3 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001541996010500154SO 1996 1 5 C2XA95IA357 119951115A572012023818009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 3 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001551996010500155SO 1996 1 5 C2XA95IA358 119951115A572012017059015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 2 LOWER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001561996010500156SO 1996 1 5 C2XA95IA359 119951115A572012017059011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0915730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 18, NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105001571996010500157WP 1996 1 5 CAL950973 119951025A335020131A BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09938754028040280 49125 FLT NR 0743 - IAH - PRIOR TO DEPARTURE, AISLE LIGHTING COMES ON WHEN SWT IN ARM POSITION. REMOVED BATTERY PACK AND REPLACED, OPS CHECKS NORMAL. (M) 2L72 4F A6WE 19960105001581996010500158WP 1996 1 5 CAL951048 119951117A3222 STRUT DOUG DC9 DC982 3022082WP NLG LOW PRESSURE A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09478AC 48063 FLT NR 0289 - CLE - THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING CLE. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE FOUND THE NOSE STRUT PRESSURE LOW. THE NOSE STRUT WAS SERVICED TO PROPER LIMITS. A GEAR SWING WAS PEFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD. IN ADDITION, THE NOSE GEAR AND DOORS WERE LUBRICATED AS A PRECAUTIONARY MEASURE. (M) 2L72 4F A6WE 19960105001591996010500159NM 1996 1 5 CAL951051 119951118A3350P4010020 BATTERY BOEING737 737291 138448WNM R-2 DOOR DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0917252 20362 FLT NR 1205 - EWR - INSPECTION FOUND THE AFT GALLEY R-2 DOOR SLIDE PACK DOOR LIGHT INOPERATIVE. THE BATTERY FOR THE LIGHT WAS REPLACED AND OPERATION CHECKED GOOD. (M) 2L72 4F A16WE 19960105001601996010500160WP 1996 1 5 CAL951052 119951110A52109955752501 BEAM DOUG DC9 DC981 3022081WP PAX DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091688433517 48074 HOU - INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL BEAM AT MAIN CABIN DOOR UPPER AFT CORNER. THE CRACK WAS STOP DRILLED IAW SRM 52-05, PAGE 189, FIGURE 31. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, PAGE 189, FIGURE 31, SRM 51-30-2, AND SRM 51-30-5. (M) 2L72 4F A6WE 19960105001611996010500161WP 1996 1 5 CAL951053 119951017A5720 SPLICE DOUG DC9 DC932 3022066WP LE WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A 4 INCH CRACK IN LEADING EDGE SPLICE BETWEEN NR 6 AND NR 7 SLAT TRACK. THE LEADING EDGE SPLICE WAS REPAIRED IAW ECRA 5710-01701. (M) 2L72 4F A6WE 19960105001621996010500162WP 1996 1 5 CAL951054 119951015A5312 DOOR JAMB DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND A 2 INCH CRACK AT LEFT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03176 AND EA 653A006. (M) 2L72 4F A6WE 19960105001631996010500163WP 1996 1 5 CAL951055 119951021A5312 BULKHEAD DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND CORROSION NEAR T-CAP ON RIGHT SIDE OF AFT PRESSURE BULKHEAD. THE CORRODED SECTION WAS CUTOUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 22. (M) 2L72 4F A6WE 19960105001641996010500164WP 1996 1 5 CAL951056 119951018A5330 SKIN DOUG DC9 DC932 3022066WP BS 1038 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOOU - INSPECTION FOUND A .75 INCH CRACK IN SKIN LAP AT STATION 1038 ABOVE LEFT PYLON. THE SKIN CRACK WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M) 2L72 4F A6WE 19960105001651996010500165WP 1996 1 5 CAL951057 119951018A5330 SKIN DOUG DC9 DC932 3022066WP BS 1038 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753568601 47111 HOU - INSPECTION FOUND TWO .75 INCH CRACKS AT RIVETS IN SKIN LAP AT STA 1038 ABOVE RIGHT PYLON. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 18. (M) 2L72 4F A6WE 19960105001661996010500166NM 1996 1 5 CAL951058 119951113A335020121 POWER SUPPLY BOEING737 7373T0 1384582NM ROW 11-12 INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914308 23359 HOU - THE EMERGENCY EXIT SIGN, BETWEEN ROW 11 AND ROW 12, FAILED THE 15 MINUTE DURATION TEST. THE POWER SUPPLY (CHARGER AND BATTERY) FOR THE EXIT SIGN WAS REMOVED AND REPLACED AND OPERATION WAS RESTORED. (M) 2L72 4F RTA16WE 19960105001671996010500167 1996 1 5 CAL951061 419951121A22104030952906 YAW DAMP COUPLER BOEING737 7373T0 1384582NM AUTOPILOT INOPERATIVE A ACALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW093934017383 23578 FLT NR 449 - EWR - THE AIRCRAFT EXPERIENCED DUTCH ROLL IN FLIGHT FROM DCA TO EWR. THE YAW DAMPER SYSTEM WAS PLACARDED INOPERATIVE AT THE TIME. THE AIRCRAFT LANDED SAFELY AT EWR. THE YAW DAMPER COUPLER WAS REMOVED AND REPLACED PER MM 22-12-31 AND OPERATION CHECKED GOOD. THE YAW DAMPER PLACARD WAS REMOVED. FAILURE HAS BEEN CONFIRMED. TEARDOWN FINDINGS REVEALED THAT THE RATE GYRO WAS AT FAULT. (M) 2L72 4F RTA16WE 19960105001681996010500168WP 1996 1 5 CAL951062 119951121A2913AS66411LS666 HYD PUMP DOUG DC9 DC982 3022082WP NR 2 ENGINE LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW091689218590 49391 FLT 0545 - IAH - THE RIGHT HYDRAULIC QUANTITY DROPPED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. (M) 2L72 4F A6WE 19960105001691996010500169WP 1996 1 5 CAL951063 119951121A33501001191 LIGHT DOUG DC9 DC982 3022082WP L-1 DOOR INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0935888 49117 FLT NR 0603 - EWR - WHEN EMERGENCY LIGHTS TEST WAS PERFORMED, THE EMERGENCY PORTABLE LIGHT AT THE L-1 DOOR WOULD NOT ILLUMINATE. THE L-1 DOOR EMERGENCY PORTABLE LIGHT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2L72 4F A6WE 19960105001701996010500170WP 1996 1 5 CAL951065 119951122A2410 CSD WASHER DOUG DC9 DC932 3022066WP NR 1 ENG BROKEN A ACALAK NONE O OTHER ININSP/MAINT 1 SW091950454472536 47638 FLT 1804 - CLE - THE NR 1 ENGINE EXPERIENCED AN UNCOMMANED SHUT DOWN ON FINAL APPROACH TO CLE. THE LANDING WAS UNEVENTFUL. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK CHECK AND POWER ASSURANCE RUN WERE GOOD. SHOP FINDINGS REVEALED CSD REAR BEARING SHAFT LOCKING WASHER HAD BROKEN TANGS. (M) 2L72 4F A6WE 19960105001711996010500171WP 1996 1 5 CAL951066 119951125A361022142231 RUBBER DUCT DOUG DC10 DC1030 3023501WP NR 2 PACK BLOWN A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0913067 47866 GUM - FLT 0900 - THE SYSTEM NR 1 AND NR 2 MANIFOLD FAIL LIGHTS ILLUMINATED IN FLIGHT WITH NR 2 DISPLAYING THE LOWEST PRESSURE. THE AIRCRAFT WAS RETURNED TO GUM WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BLOWN RUBBER DUCT ON NR 2 PACK HEAT EXCHANGER. THE DUCT WAS REPLACED AND LEAK CHECK WAS GOOD. THE AIRCRAFT WAS PRESSURIZED TO 4 PSI USING PACKS NR 2 AND NR 3, AND NO ABNORMAL INDICATIONS WERE NOTED. (M) 2L73 4F A22WE 19960105001721996010500172WP 1996 1 5 CAL951067 119951126A323129235941 LATCH SPRING DOUG DC9 DC932 3022066WP LT MLG DOOR LACK OF LUBE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW0917535 47111 FLT NR 1090 - ATL - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. THE RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT EXTINGUISHED AFTER UPLATCH CHECK. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH. THE A/C HAD A HISTORY OF THE LT MLG RED UNSAFE LIGHT REMAINING ILLUMINATED. MAINTENANCE FOUND THE LEFT MLG DOOR LATCH ROLLER SPRING TENSION OUT OF LIMITS. BOTH SPRINGS WERE R/R. TENSION CHK WAS PERFORMED AND BOTH SPRINGS WERE WITHIN LIMIT. THE PROB WAS REPEATED ON THE SUBSEQUENT FLT AND LUBRICATION OF THE UPLATCH ASSY FIXED THE PROB. THE A/C HAS FLOWN 7 FLTS W/O A REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. M2L72 4F A6WE 19960105001731996010500173WP 1996 1 5 CAL951068 119951127A29136506606 HYD PUMP DOUG DC10 DC1030 3023501WP NR 3 ENGINE CASE CRACKED A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW091406210965 47863 FLT NR 0005 - IAH - THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED AND THE NR 3 HYDRAULIC QUANTITY AND PRESSURE DECREASED TO ZERO IN FLIGHT. THE EMERGENCY CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE RIGHT HYDRAULIC PUMP CASE CRACKED. BOTH NR 3 ENGINE RIGHT AND LEFT HYDRAULIC PUMPS WERE REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. THE HYDRAULIC CONTROLS WERE OPERATED WHILE ENGINE WAS RUNNING WITH NO LEAKS OR OTHER DISCREPANCIES NOTED. (M) 2L73 4F A22WE 19960105001741996010500174NM 1996 1 5 CAL951069 119951120A3350 BATTERY PACK BOEING737 737217 1384464NM EMER EXITS INOP A CALAK NONE L NO TEST ININSP/MAINT 1 SW0912231 19885 GSO - INSPECTION FOUND THE L-1 AND R-1 EXTERIOR EMEREGNCY EXIT SLIDE LIGHTS INOPERATIVE. THE BATTERY PACK FOR THE L-1 AND R-1 EMERGENCY EXIT SLIDE LIGHTS WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. (M) 2L72 4F A16WE 19960105001751996010500175NM 1996 1 5 CAL951070 119951120A5315 FLOOR BEAM BOEING737 737217 1384464NM BS 660 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223173264 19885 GSO - INSPECTION FOUND A 1.5 INCH CRACK IN CENTER FLOOR BEAM OF MAIN CABIN AT STATION 660, BL 0. A REPAIR WAS FABRICATED AND INSTALLED IAW BAC DRAWING 65C34537 AND EA 5710-01322. (M) 2L72 4F A16WE 19960105001761996010500176NM 1996 1 5 CAL951071 119951120A5330 SKIN BOEING737 737217 1384464NM BS 350 CREASED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223173264 19885 GSO - INSPECTION FOUND A CREASE IN SKIN PANEL ON RIGHT SIDE OF FUSELAGE AT STATION 350 AFT OF R-1 DOOR BETWEEN S18R AND S20R. THE DAMAGED AREA WAS CUTOUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (M) 2L72 4F A16WE 19960105001771996010500177NM 1996 1 5 CAL951072 119951120A5312 BULKHEAD BOEING737 737217 1384464NM NLG WW CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09122317326473264 19885 GSO - INSPECTION FOUND A 4.05 INCH CRACK IN WEB ON LEFT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT LBL 6.12 AND A 3.25 INCH CRACK ON RIGHT SIDE OF NOSE WHEEL WELL AFT BULKHEAD AT RBL 7.50. THE CRACKS WERE LOCATED AT STATION 294.5. THE CRACKS WERE STOP DRILLED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW BAC DRAWING 65C35690, EA 5310-02452, AND ECRA 5310-03183. (M) 2L72 4F A16WE 19960105001781996010500178NM 1996 1 5 CAL951073 119951120A5320 SHEAR BEAM WEB BOEING737 737217 1384464NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223173264 19885 GSO - INSPECTION FOUND A 1.5 INCH CRACK IN LOWER INBOARD RADIUS OF SHEAR BEAM WEB JUST FORWARD OF STATION 727 AT S18A, LEFT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW BAC DRAWING 65C29228. (M) 2L72 4F A16WE 19960105001791996010500179NM 1996 1 5 CAL951074 119951101A5320 CHORD BOEING737 737217 1384464NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223173264 19885 GSO - INSPECTION FOUND A 1 INCH CRACK AT FASTENERS IN LEFT STATION 727 OUTBOARD CHORD, STRINGER 18A. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BAC DRAWING 65C33722. (M) 2L72 4F A16WE 19960105001801996010500180NM 1996 1 5 CAL951075 119951129A2910 HYD LINE BOEING737 737247 138448DNM A-HYD SYSTEM CHAFED A CALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0914246 20129 FLT 1616 - MCO - THE NR 1 ENGINE A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED WITH THE HYDRAULIC QUANTITY GAUGE READING NEAR ZERO WHILE EN ROUTE FROM MIA TO GSO. THE AIRCRAFT WAS DIVERTED TO MCO AND WHILE ON SHORT FINAL THE 'B LOW QUANTITY' LIGHT CAME ON. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM HYDRAULIC PRESSURE LINE ALONG KEEL BEAM IN RIGHT WHEEL WELL CHAFED THROUGH. THE LINE WAS REPLACED USING FLEX LINE AND A DIP WAS ISSUED TO REPLACE THE FLEX LINE WITHIN 500 FLIGHTS OR 1200 HOURS, WHICHEVER COMES FIRST. (M) 2L72 4F A16WE 19960105001811996010500181NM 1996 1 5 CAL951076 119951129A3260 SAFETY SENSOR BOEING737 7373T0 1384582NM RIGHT LOOSE A CALAO OTHER O OTHER TOTAKEOFF 1 SW0959302 23353 FLT NR 0320 - EWR - THE GEAR HANDLE WOULD NOT MOVE TO UP POSITION WHEN RAISING GEAR AFTER TAKEOFF. THE LANDING GEAR LATCH AND PRESS WARNING CIRCUIT BREAKER WAS RESET IN ACCORDANCE WITH QRH AND THE GEAR RAISED NORMALLY. MAINTENANCE FOUND THE RIGHT SAFETY SENSOR LOOSE IN ITS MOUNTING BRACKET AND CLEARANCE WAS EXCESSIVE. THE SAFETY SENSOR WAS ADJUSTED AD TIGHTENED PER MM 32-09-01, PAGES 501-507. OPERATION OF THE GEAR LEVER LATCH SYSTEM CHECKED GOOD. (M) 2L72 4F RTA16WE 19960105001821996010500182NM 1996 1 5 CAL951077 119951128A3350 GROUND WIRE BOEING757 757224 1384958NM SEAT 19 LOOSE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0918112 27302 LAX - INSPECTION FOUND THE RIGHT EMERGENCY AISLE LIGHT ON OVERHEAD BIN NEAR SEAT 19 INOPERATIVE. MAINTENANCE FOUND THE GROUND WIRE ON STUD ABOVE CEILING PANEL ON RIGHT SIDE LOOSE. THE GROUND WIRE WAS TIGHTENED TO THE STUD AND OPERATION OF THE LIGHT WAS RESTORED. (M) 2L72 4F RTA2NM 19960105001831996010500183WP 1996 1 5 HALA95156 119951116A5330 SKIN DOUG DC9 DC951 3022051WP AFT FUSELAGE GOUGED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 47742 HNL - DURING C-CHECK, GOUGE IN FUSELAGE APPROX 2.5 INCHES AFT OF FORWARD CARGO DOOR CUTOUT BELOW 2ND DOOR ADJUSTMENT SET SCREW. DEPTH CHECK SKIN REMAINING .023 INCH, 1 INCH BY 1 INCH. REPAIRED PER SRM 53-05, FIG 82. REMOVED DAMAGED SECTION. FABRICATED INTERNAL DOUBLER (.025 INCH TI-6AL-4V). FABRICATED EXTERNAL REPAIR DOUBLER (0.071 INCH 2024-T3 CLAD) INSTALLED REPAIR DOUBLER USING NAS1097AD5/6 RIVETS AND HLT435-6 HI-LOCKS IN EXISTING AND ADDED HOLES. (M) 2L72 4F A6WE 19960105001841996010500184SW 1996 1 5 MALA954723 119951124A52102724044 DOOR SWRNGNSA227 SA227AC 8780603SW CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER FORWARD PASSENGER DOOR CORNER, P/N 27-24044 AND WEAR IN THE LOWER FORWARD PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IN ACCORDANCE WITH SRM 51-00-00. (M) 1L72 4T A8SW 19960105001851996010500185SW 1996 1 5 MALA954724 119951124A52102724044 DOOR SWRNGNSA227 SA227AC 8780603SW CABIN CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER AFT PASSENGER DOOR CORNER P/N 27-24044 AND WEAR IN THE LOWER AFT PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IAW SRM 51-30-02, -04, AND 51-40-00. (M) 1L72 4T A8SW 19960105001861996010500186SW 1996 1 5 MALA954725 119951124A5311 FRAME SWRNGNSA227 SA227AC 8780603SW FS 242.27 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME RELIEF RADIUS AT FS 242.27 AND WL 81.07 BELOW STRINGER NR 11. THE CRACK WAS REPAIRED BY STOP DRILLING IT AND FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1L72 4T A8SW 19960105001871996010500187NM 1996 1 5 MALA954727 119951127A5400 BYPASS DOOR DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE WILL NOT OPEN A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15833MA 343 FLT NR 3094 - EN ROUTE FROM MSP-BMI - THE NR 1 ENGINE INTAKE BYPASS DOOR WOULD NOT OPEN. DUE TO EN ROUTE WEATHER, THE AIRCRAFT RETURNED TO MSP. MAINTENANCE PERSONNEL DEFERRED THE SYSTEM UNDER MEL 71-1 AND THE AIRCRAFT WAS RETURNED TO SERVICE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960105001881996010500188WP 1996 1 5 ORJA95130 119951114A5320 STIFFENER DOUG DC9 DC982 3022082WP RT MLG WW CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 RIGHT MLG W/W AFT WEB, THROUGH CUTOUT CORROSION ON STIFFENER, LOWER ANGLE, SIMILAR CORROSION FOUND ON LEFT SIDE. COMPLIED WITH REPAIR IAW EA 13-57-EA005, DATED 11-17-95. REINSTALLED ANGLE ON A/C REF TO SRM 51-30-2, FOR LEFT AND RIGHT SIDE. (M) 2L72 4F A6WE 19960105001891996010500189WP 1996 1 5 ORJA95131 119951125A3350 CONNECTOR DOUG DC9 DC983 3022083WP CABIN LOOSE A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 SECTION 1 THROUGH 3 RIGHT FLOOR EMERGENCY TRACK LIGHTING INOP. SECURED PLUG ON FLOOR TRACK EMERGENCY. OPS GOOD. (M) 2L72 4F RTA6WE 19960105001901996010500190NM 1996 1 5 TAOA119510 119951128A793142D107A2 SWITCH BOEING727 727225 1384077NM NR 1 ENGINE STUCK A TAOAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 EA15922TS 3676 20415 FLT NR 6450 - DCA-LGA - IN CRUISE, EXPERIENCED A NR 1 OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATE. RETARDED NR 1 THROTTLE, LIGHT STAYED ON. SHUTDOWN NR 1 ENGINE, OIL PRESSURE REMAINED IN THE GREEN BAND. NR 1 OIL PRESSURE SWITCH STUCK IN THE ON POSITION. REPLACED OIL PRESSURE SWITCH, RAN CHECKED, OPS OK PER MM 79-33-1. (M) 2L73 4F A3WE 19960105001911996010500191NM 1996 1 5 TWRA9565 119951126A535065B06723 FAIRING BOEING747 747124 1384874NM LT WING/FUS MISSING A ATWRAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA15602FF 19734 DURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON LEFT SIDE BELOW NR 3 MED. AIRCRAFT WAS INSPECTED AND FOUND OK FOR FERRY FLIGHT TO JFK. FUSELAGE FAIRING WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE NOV 31, 1995. (M) 2L74 4F A20WE 19960105001921996010500192NM 1996 1 5 TWRA9566 119951201A335030041801A LIGHT BOEING747 747136 1384883NM CABIN INOPERATIVE A TWRAK NONE L NO TEST ININSP/MAINT 1 EA15606FF 20273 BUSSLE EMERGENCY LIGHTS ARE INOP AT 1L, 4R, 5L, 5R. REPLACED LIGHT ASSYS. OPS CHECK OK. (M) 2L74 4F A20WE 19960105001931996010500193WP 1996 1 5 USAA9511206 119951018A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION IN SUPPORT BEAM WEB AT STATION 1338 OUTBOARD END OF FLOOR BEAM UNDER AFT RIGHT LAV, PREVIOUSLY REWORKED CORROSION TASK NR C58-5330. SPLICED IN DOUBLER FILLER AND WEB SECTION PER USAIR EA 31376A. (M) 2L72 4F A6WE 19960105001941996010500194WP 1996 1 5 USAA951161 119951106A5347 TRACK DOUG DC9 DC982 3022082WP BS 1174 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION LEFT OUTBOARD SEAT TRACK AT STATION 1174 PREVIOUSLY REWORKED CORROSION TASK NR 05853302. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG F. (M) 2L72 4F A6WE 19960105001951996010500195WP 1996 1 5 USAA951162 119951106A5315 FLOOR BEAM DOUG DC9 DC982 3022082WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND LEVEL 1 CORROSION AROUND FLOOR BEAM NUT PLATE HOLES TOP AND BOTTOM SURFACE AT STATION 1338 AFT RT LAV PREVIOUSLY REWORKED. CORROSION TASK REF C53-53300. REPLACED TOP CAP OF FLOOR BEAM PER USAIR TYPICAL REPAIR 53-10-14. (M) 2L72 4F A6WE 19960105001961996010500196WP 1996 1 5 USAA951163 119951106A5330 SKIN DOUG DC9 DC982 3022082WP BS 229-256 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19816US37510 48096 PIT - DURING Q-3/C-6 INSPECTION, FOUND CLASS 3 REPAIR INSTALLED PER OM-7 NR 69263 (DEFERRED MAINTENANCE). REPLACED REPAIR AT SKIN STATION 228 TO 256 BETWEEN LONGERON 14L AND 17L PER USAIR TYPICAL REPAIR NR 53-30-12 AND SRM 53-04 FIG 4. (M) 2L72 4F A6WE 19960105001971996010500197NM 1996 1 5 USAA951165 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK NDT INSPECTION, FOUND ONE .25 INCH CRACK, STATION 520, FLOOR BEAM UPPER RADIUS LBL 45, WL 207.75. DOUBLER INSTALLED PER EA 40020, REF SB 737-53-1120. REPAIRED PER EA 40020 REF SB 737-53-1120. (M) 2L72 4F RTA16WE 19960105001981996010500198NM 1996 1 5 USAA951166 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 520 FLOOR BEAM UPPER RADIUS RBL 45, WL 207.75. STOP DRILLED AND INSTALLED DOUBLER REPAIR/MODIFICATION. REPAIRED PER EA 40020. (M) 2L72 4F RTA16WE 19960105001991996010500199NM 1996 1 5 USAA951171 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED AREA ON FLOOR BEAM AT BS 328. REMOVED CORRODED AREA, INSTALLED REPAIR PARTS COMPLETED REPAIR. REPAIRED PER SRM 53-10-51, FIG 205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002001996010500200NM 1996 1 5 USAA951172 119951103A52101123845 ANGLE BOEING737 737401 1384701NM FWD ENTRY DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 36 INCH AREA CORRODED, FORWARD ENTRY DOOR Z-ANGLE. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002011996010500201NM 1996 1 5 USAA951173 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING A-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, STATION 328 FLOOR BEAM UPPER FLANGE AT NUT PLATE HOLES. SECTION CUT OUT AND REPLACED PER SRM 53-10-51 FIG 205. REPAIRED PER SRM 53-10-51, FIG 205. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002021996010500202NM 1996 1 5 USAA951174 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 68 INCH CORRODED AREA ON FLOOR BEAM BS 344 LBL 51 TO RBL 17. INSTALLED T-CAP AND REPAIRED ANGLE. REPAIRED PER SRM TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002031996010500203NM 1996 1 5 USAA951175 119951103A53206545834259 INTERCOSTAL BOEING737 737401 1384701NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH DIAMETER AREA, INTERCOSTAL UPPER FLANGE STATION 328 TO 344 LBL 12, WL 208. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002041996010500204NM 1996 1 5 USAA951176 119951103A5347 SEAT TRACK BOEING737 737401 1384701NM BS 344-360 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 16 INCH CORRODED AREA ON SEAT TRACK AT BS 344 TO BS 360 LBL 25 INCHES. REMOVED AND REINSTALLED REPAIR PART COMPLETED REPAIR. REPAIRED PER SRM 53-00-52, FIG 202. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002051996010500205NM 1996 1 5 USAA951177 119951103A53206545834260 INTERCOSTAL BOEING737 737401 1384701NM BS 328-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH AREA, BS 328 TO BS 312, RBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002061996010500206NM 1996 1 5 USAA951178 119951103A53206545834255 INTERCOSTAL BOEING737 737401 1384701NM BSS 294-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 2 INCH CORRODED AREA BS 294 TO BS 312, RBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002071996010500207NM 1996 1 5 USAA951179 119951103A53206545834260 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 312 TO BS 328, LBL 12 INCHES. REMOVED AND REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002081996010500208NM 1996 1 5 USAA951180 119951103A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 747 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA RBL 14 CARGO FLOOR SUPPORT STRINGER (BEAM) AT BS 747. CUT OUT CORRODED SECTION OF BEAM BS 733-778. FABRICATED AND INSTALLED NEW SECTION OF BEAM (TRACK) AND SPLICES. REPAIRED PER SRM 53-00-53 FIG 202 AND BOEING DRAWING 65-47957. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002091996010500209NM 1996 1 5 USAA951182 119951103A5320654587545 ANGLE BOEING737 737401 1384701NM BS 280-326 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 46 INCH CORRODED AREA BS 280-326, STRINGER 17 RT (RT SERVICE DOORWAY CHORD ANGLE). REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE WITH SAME P/N FROM STOCK. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002101996010500210NM 1996 1 5 USAA951183 119951103A532065C8073511 ANGLE BOEING737 737401 1384701NM BS 947-1006 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, ON Z ANGLE BS 947-BS 1006, RBL 53. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002111996010500211NM 1996 1 5 USAA951184 119951103A532065C333701 SUPPORT BOEING737 737401 1384701NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 10 INCH AREA CORRODED ON SUPPORT AT STATION 947 TO 967 AT LBL 25. REMOVED AND REPLACED CHANNEL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002121996010500212NM 1996 1 5 USAA951185 119951103A532065C33371 SUPPORT BOEING737 737401 1384701NM BS 947-967 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 7 INCH AREA CORRODED, ON SUPPORT AT 967 AT LBL 51. REMOVED AND REPLACED SUPPORT CHANNEL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002131996010500213NM 1996 1 5 USAA951186 119951103A532065C323672 SUPPORT BOEING737 737401 1384701NM BS 947 TO 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19417US19934 23984 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 8 INCH CORROSION ON SUPPORT AT STATION 947 TO 967 RBL 51. REPLACED SUPPORT CHANNEL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002141996010500214NM 1996 1 5 USAA951193 119951023A5414 SKIN BOEING757 757225 1384959NM NR 2 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19608AU34453 22204 CLT - CLT INSPECTION VISUALLY FOUND CORRODED SKIN PAST LIMITS OF EO NR 5492R274 PART IV STEPS 2 AND 3 LOCATED AT NR 2 ENGINE PYLON INBOARD. REPAIRED SKIN PER DRAWING 012N8774 AND EA 40036. (M0 2L72 4F RTA2NM 19960105002151996010500215WP 1996 1 5 USAA951197 119951018A5311 FRAME DOUG DC9 DC981 3022081WP BS 11322 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON BELTFRAME STATION 1322 LOWER FWD SURFACE LONGERON 30. CORROSION TASK NR C57-53300 PREVIOUSLY RE WORKED. SPLICED IN NEW SECTION BELTFRAME PER SRM 53-03 FIG 2A. (M) 2L72 4F A6WE 19960105002161996010500216WP 1996 1 5 USAA951198 119951018A5313 LONGERON DOUG DC9 DC981 3022081WP BS 446 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 446 NEAR ALT STATIC PORT. PREVIOUSLY RE WORKED FROM LAV SPILL. CORROSION TASK NR C51-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-2. (M) 2L72 4F A6WE 19960105002171996010500217WP 1996 1 5 USAA951199 119951018A5313 LONGERON DOUG DC9 DC981 3022081WP BS 227 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 227 LONGERON 29R AT RIVET HEADS PREVIOUSLY RE WORKED CORROSION TASK NR C51-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 2. (M) 2L72 4F A6WE 19960105002181996010500218WP 1996 1 5 USAA951200 119951018A5330 SKIN DOUG DC9 DC981 3022081WP BS 160 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND SKIN CRACK APPROXIMATELY 2 INCHES IN LENGTH IN MED UPPER FORWARD JAMB CORNER STATION 160 FUSELAGE EXTERIOR SKIN. INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-05 FIG 25A. (M) 2L72 4F A6WE 19960105002191996010500219WP 1996 1 5 USAA951201 119951018A5230 PAN DOUG DC9 DC981 3022081WP CARGO DOOR CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION LOWER FORWARD CARGO DOOR PAN ASSY PREVIOUSLY RE WORKED. CORROSION TASK NR C51-53300. INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 14. (M) 2L72 4F A6WE 19960105002201996010500220WP 1996 1 5 USAA951202 119951018A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 210 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION STATION 210 FORWARD END OF RIGHT SEAT TRACK. CORROSION TASK C46-53305 PREVIOUSLY REWORKED. SPLICED IN SEAT TRACK PER SRM 53-05 FIG 4. (M) 2L72 4F A6WE 19960105002211996010500221WP 1996 1 5 USAA951203 119951018A5315 FLOOR BEAM DOUG DC9 DC981 3022081WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1322 FLOOR BEAM RIGHT SIDE LAV AREA. CUT OUT DAMAGED AREAS INSTALLED FILLERS AND REPAIR ANGLES PER USAIR TYPICAL REPAIR 53-10-19. (M) 2L72 4F A6WE 19960105002221996010500222WP 1996 1 5 USAA951204 119951018A5347 SEAT TRACK DOUG DC9 DC981 3022081WP BS 1309 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT INBOARD SEAT TRACK LEFT STATION 1309 IN 2 POSITIONS. CORROSION TASK NR C58-53301 PREVIOUSLY RE WORKED. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (M) 2L72 4F A6WE 19960105002231996010500223WP 1996 1 5 USAA951205 119951018A5320 BEAM DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND CORROSION LEVEL 1 AT STATION 1338 UNDER RIGHT LAV AROUND FLOOR SUPPORT BEAM SCREW HOLES. PREVIOUSLY REWORKED CORROSION TASK NR C58-53309. SPLICED IN NEW SECTION OF FLOOR SUPPORT BEAM PER USAIR TYPICAL REPAIR 53-10-14. (M) 2L72 4F A6WE 19960105002241996010500224WP 1996 1 5 USAA951207 119951018A5320 BEAM DOUG DC9 DC981 3022081WP BS 1302 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1322 AROUND SCREW HOLES RIGHT OF CENTER LINE UNDER AFT LAV FLOOR SUPPORT BEAM. CORROSION TASK NR C58-53300. REMOVED CORROSION AND INSTALLED STRAP AND ANGLE INSTALLATION REPAIR PER USAIR TYPICAL REPAIR 53-10-19. (M) 2L72 4F A6WE 19960105002251996010500225WP 1996 1 5 USAA951208 119951018A5313 LONGERON DOUG DC9 DC981 3022081WP BS 456 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19814US37621 48094 PIT - DURING Q-3/C-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION AT LONGERON STATION 456. CORROSION TASK NR C51-53300. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-10-2A. (M) 2L72 4F A6WE 19960105002261996010500226WP 1996 1 5 USAA951209 119951114A5320 CUSP MEMBRANE DOUG DC9 DC982 3022082WP BS 984-1003 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37430 48097 PIT - DURING Q-1/C-6 INSPECTION, FOUND .25 INCH CRACK RIGHT SIDE CABIN STATION 984 AND 1003 AT LONGERON 18 CUSP LINE MEMBRANE. MANUFACTURED CUSP MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97. (M) 2L72 4F A6WE 19960105002271996010500227WP 1996 1 5 USAA951210 119951114A53201196506 CLIP DOUG DC9 DC982 3022082WP BS 1437 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37430 48097 PIT - DURING Q-1/C-6 INSPECTION, FOUND 1 INCH CRACK IN FRAME TO FUSELAGE CLIP AFT SIDE OF BS 1437 AT LONGERON 1. SPLICED IN NEW CLIP PER SRM 53-03 FIG 6. (M) 2L72 4F A6WE 19960105002281996010500228WP 1996 1 5 USAA951211 119951114A5330 SKIN DOUG DC9 DC982 3022082WP BS 821 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37430 48097 PIT - DURING Q-1/C-6 INSPECTION, FOUND 1.09375 INCH CRACK AT STATION 821 AND LONGERON 17R IN EXTERIOR SKIN. CUTOUT DAMAGED AREA AND INSTALLED FILLER AND 6.5 INCH BY 8.5 INCH INTERNAL DOUBLER PER SRM 53-04 FIG 38 VIEW H. (M) 2L72 4F A6WE 19960105002291996010500229WP 1996 1 5 USAA951212 119951114A53119911842103 FRAME DOUG DC9 DC982 3022082WP BS 1485 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19817US37430 48097 PIT - DURING Q-1/C-6 INSPECTION, FOUND .5 INCH CRACK AT CANTED FRAME 1485 AT LONGERON 7L. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-14-4 FIG 3. (M) 2L72 4F A6WE 19960105002301996010500230NM 1996 1 5 USAA951213 119951104A5313 STRINGER BOEING737 7372B7 1384560NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19266AU35797 22878 ROA - DURING 'BX' CHECK VISUAL INSPECTION, FOUND 18.5 INCHES BY 2 INCHES CORROSION (STRINGER IS CORRODED), BS 967 STRINGER 27 LEFT. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3, FIG 1. (M) 2L72 4F A16WE 19960105002311996010500231WP 1996 1 5 USAA951215 119951113A53132777922 LONGERON DOUG DC9 DC931 3022065WP BS 617 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19991VJ69520 47310 PIT - DURING C-2 CHECK INSPECTION, FOUND .5 INCH CRACK IN LONGERON 6R AT STATION 617 SID INSPECTION REF PSE 53.09.009 AND 010 LFEC INSPECTION. INSTALLED LONGERON SPLICE AND DOUBLERS PER SRM 53-10-17. (M) 2L72 4F A6WE 19960105002321996010500232WP 1996 1 5 USAA951216 119951113A53132777922 LONGERON DOUG DC9 DC931 3022065WP BS 756 LONG 4L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19991VJ69520 47310 PIT - DURING C-2 CHECK INSPECTION, FOUND .25 INCH CRACK STATION 756 AT LONGERON 4L. SID INSPECTION REF PSE 53.09.009 AND .010 LFEC INSPECTION. INSTALLED LONGERON SPLICE AND DOUBLERS PER USAIR SRM 53-10-17. (M) 2L72 4F A6WE 19960105002331996010500233NM 1996 1 5 USAA951217 119951115A533065184201139 SKIN BOEING737 7373Q8 1384670NM BS 219.8 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .25 INCH LONG SKIN CRACK ON VISUAL INSPECTION AND .625 INCH LONG GUSSET CRACK LEFT C-D WINDOW POST SKIN AND GUSSET BS APPROX 219.8 BY EDDY CURRENT. REMOVED DAMAGED AREA AND INSTALLED FILLERS AND DOUBLERS. REPAIRED PER EEA 40239. (M) 2L72 4F RTA16WE 19960105002341996010500234NM 1996 1 5 USAA951218 119951115A53206545834259 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DRUING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH DIAMETER .020 DEEP CORROSION INTERCOSTAL BETWEEN STATION 328 AND STA 344 LBL 8.5. REPLACED WITH INDENTICAL PART NR 65-45834-259. LEVEL 1 CORROSION, CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19960105002351996010500235NM 1996 1 5 USAA951219 119951115A53206546812170 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 967.5-947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORRODED AREA AROUND NUT PLATE HOLES ON INTERCOSTAL BETWEEN STATION 967.5 TO STATION 947 AT LBL 42. LEVEL 1 CORROSION. REPLACED WITH NEW INTERCOSTAL FROM STOCK. REPAIRED PER SRM 51-10-2 AND BAC DRAWING 65-46812-170. (M) 2L72 4F RTA16WE 19960105002361996010500236NM 1996 1 5 USAA951220 119951115A53206545834257 INTERCOSTALS BOEING737 7373Q8 1384670NM BS 328-360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORROSION 8 PLACES, STATION 328 TO 344 AND STATION 344 TO 360 RBL 12. REPLACED INTERCOSTALS. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002371996010500237NM 1996 1 5 USAA951221 119951115A5315 FLOOR BEAAM BOEING737 7373Q8 1384670NM BS 312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 45 INCHES STATION 312, LBL 16 TO RBL 36. REPLACED UPPER T-CAP. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002381996010500238NM 1996 1 5 USAA951222 119951115A5330 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CHAFFED A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 10 INCH AREA OF FUSELAGE SKIN CHAFFED, FORWARD END OF DORSAL FIN CONTACT AREA. INSTALLED EXT FUSELAGE SKIN DOUBLER. REPAIRED PER SRM 53-00-01, FIG 202. (M) 2L72 4F RTA16WE 19960105002391996010500239NM 1996 1 5 USAA951223 119951115A5330 SKIN BOEING737 7373Q8 1384670NM BS 344 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND DENT 3.5 INCHES BY 4.75 INCHES, STATION 344 AT STRINGER 19R. INSTALLED DOUBLER. REPAIRED PER SRM 53-00-01. (M) 2L72 4F RTA16WE 19960105002401996010500240NM 1996 1 5 USAA951224 119951115A53206545834256 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 328-312 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOOR INTERCOSTAL BS 328 TO 312 RBL 12. LEVEL 1 CORROSION. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. (M) 2L72 4F RTA16WE 19960105002411996010500241NM 1996 1 5 USAA951225 119951115A5315 FLOOR BEAM BOEING737 7373Q8 1384670NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 50 INCH CORROSION AREA AT NUT PLATE HOLES, BS 328 FLOOR BEAM CAP LBL 34 TO RBL 65. INSTALLED NEW T-CAP SECTION. (M) 2L72 4F RTA16WE 19960105002421996010500242NM 1996 1 5 USAA951226 119951115A5315 FLOOR BEAM BOEING737 7373Q8 1384670NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 28 INCH CORROSION AT STATION 967 LBL 28 INCHES TO LBL 50 INCHES. REPLACED T-CAP OF FLOOR BEAM. REPAIRED PER SRM 53-00-51. (M) 2L72 4F RTA16WE 19960105002431996010500243NM 1996 1 5 USAA951227 119951115A5347 SEAT TRACK BOEING737 7373Q8 1384670NM BS 335 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 5 INCHES OF CORROSION BS 335, RBBL 51. REPLACED SEAT TRACK. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002441996010500244NM 1996 1 5 USAA951228 119951115A5347 SEAT TRACK BOEING737 7373Q8 1384670NM BS 348-360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 6 INCHES OF CORROSION BS 348-360. REPLACED SEAT TRACK. REPAIRED PER SRM 53-00-52. (M) 2L72 4F RTA16WE 19960105002451996010500245NM 1996 1 5 USAA951229 119951115A5315 FLOOR BEAM BOEING737 7373Q8 1384670NM BS 986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-CHECK VISUAL INSPECTION, FOUND 1 INCH BY 48 INCH CORROSION STATION 986 RBL 4 INCHES TO LBL 52 INCHES. REPLACED UPPER T-CAP. REPAIRED PER SRM 53-00-51. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002461996010500246NM 1996 1 5 USAA951230 119951115A5320 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 967-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORROSION LBL 18 INCHES STATION 967 TO STATION 986. REPLACED INTERCOSTAL. REPAIRED PER SRM 51-10-4. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002471996010500247NM 1996 1 5 USAA951231 119951115A53206546812187 INTERCOSTAL BOEING737 7373Q8 1384670NM BS 1006-1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CORROSION STATION 1006 TO STATION 1016 LBL 16 INCHES. REPLACED WITH LIKE PART. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002481996010500248NM 1996 1 5 USAA951232 119951115A5315 FLOOR BEAM BOEING737 7373Q8 1384670NM BS 907 SHORTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 8 INCH SCREW HOLES TO CLOSE TO EDGE, STATION 907 RBL 24 TO LBL 45. INSTALLED NEW T-CAP SECTION. REPAIRED PER TR 53-10-05 AND SRM 53-60-51. (M) 2L72 4F RTA16WE 19960105002491996010500249NM 1996 1 5 USAA951233 119951115A5320 SUPPORT BOEING737 7373Q8 1384670NM BS 106 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19398US27808 23507 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORROSION STATION 1016 LBL 6 INCHES TO RBL 6 INCHES. INSTALLED REPAIR DOUBLER. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960105002501996010500250WP 1996 1 5 USAAD95007 119951115A3222MS288892 SCHRADER VALVE DOUG DC9 DC981 3022081WP NOSE GEAR LEAKING A USAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA19805US 48053 PHL - FLT 2184 - DURING RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. THE CAPTAIN CYCLED THE GEAR, BUT THE LIGHT DID NOT GO OUT. THE CAPTAIN DECIDED TO RETURN TO PHL. REMOVED AND REPLACED THE LEAKING SCHRADER VALVE. (M) 2L72 4F A6WE 19960105002511996010500251NM 1996 1 5 USAASB95011 119951107A28202820095101 VALVE BOEING737 7373B7 1384580NM LT FUEL TANK FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19384US30134 22957 PIT - FLT NR 1133 - EN ROUTE PIT TO IAH, LEFT FORWARD AND RIGHT AFT FUEL BOOST PUMP CIRCUIT BREAKERS TRIPPED AND WOULD NOT RESET. FLIGHT RETURNED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL SCAVENGE SOLENOID VALVE INOP. RELEASED WITH FUEL SCAVENGE SYSTEM ON MEL 28-17 FOR SOLENOID VALVE REPLACEMENT. (M0 2L72 4F RTA16WE 19960105002521996010500252NM 1996 1 5 USAASB95013 119951112A29136507506 HYD PUMP BOEING737 737301 1384611NM NR 2 ENGINE FAILED A USAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 EA19334US 15632 23231 IND - FLIGHT NR 0133 - RIGHT ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED AND B-SYSTEM HYDRAULIC QUANTITY DROPPED TO ONE QUARTER. FLIGHT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP AND SERVICED HYDRAULICS. OPS/LEAK CHECKED GOOD. (M) 2L72 4F RTA16WE 19960105002531996010500253NM 1996 1 5 USAASB95014 119951113A26126937307145 FIRE CONTL PNL BOEING737 7373B7 1384580NM FLIGHT DECK FAILED A USAAAE UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 EA19531AU18080 24478 PIT - FLIGHT NR 0009 - AIRCRAFT DISPATCHED WITH MEL 26-2A FOR NR 2 ENGINE B-LOOP. ON CLIMB-OUT FROM PIT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. FLIGHT CREW SHUT DOWN NR 2 ENGINE AND RETURNED TO PIT. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED THE P8-1 FIRE CONTROL PANEL AND PERFORMED ENGINE RUN UP. OPS CHECKED GOOD. (M) 2L72 4F RTA16WE 19960105002541996010500254NE 1996 1 5 VTZA96038 219951205A72605725109162 DETECTOR CHIP JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE ACTIVATED A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27312UE 41025 P76029C FLTNR 6510 - IAD-BOS - DURING CRUISE RETURNED TO IAD DUE TO THE RIGHT ENGINE OIL CONTAMINATION LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED AND FOUND AN ACCEPTABLE SLIVER ON THE DETECTOR. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA41NM E18NE 19960105002551996010500255CE 1996 1 5 1239563CK 119951206A3233MS287786 O-RING 23171003 LEAR 24 24 5170302CE MLG ACTUATOR LEAK A KKFAO OTHER JK WARNING INDICATION FLUID LOSS APAPPROACH 1 GL2363CK 6578 578 M6649 24119 ON APPROACH TO LANDING, HYDRAULIC PRESSURE WAS NOTED TO BE ZERO. LANDING GEAR WAS EXTENDED USING EMERGENCY AIR SYSTEM AND A NORMAL LANDING WAS MADE. EXAMINATION REVEALED A O-RING RETAINING JAMB NUT ON THE MAIN GEAR ACTUATOR HAD BACKED OFF CAUSING A HYDRAULIC LEAK. LEAK WAS REPAIRED, SYSTEM TESTED AND SERVICED. RECOMMEND THOROUGH INSPECTION OF LANDING GEAR ACTUATOR JAMB NUTS. (X) 2L72 4J A10CE 19960105002701996010500270SW 1996 1 5 96ZZZX20 119951101A5700 WING SWRNGNSA226 SA226TC 8780404SW LT OTBD LE FOD A BDHAO OTHER C F.O.D. NRNOT REPORTED 1 GL15327BA TC249 BIRD STRIKE TO LEFT OUTBOARD WING. OUTBOARD LEADING EDGE DAMAGE. 1L72 4T A8SW 19960105002811996010500281 1996 1 5 96ZZZX30 419951207A612231039391 ELBOW WOODWARD 89741016 SWRNGNSA227 SA227AC 8780603SW PROPELLER GOV CRACKED A PNSAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 AL03630PA 5501 1943243 AC463 RIGHT ENGINE SECURED AT CRUISE. FOUND 90 DEGREE ELBOW FITTING FOR PROPELLER RESET MOUNTED ON PROPELLER GOVERNOR CRACKED ON INSIDE RADIUS. SUBMITTER STATED THIS IS POST-SB 7700-90, WHICH IS SUPPOSED TO PREVENT THIS OCCURENCE. 1L72 4T A8SW 19960105002861996010500286NM 1996 1 5 96ZZZX8 119950207A3244 TIRE BOEING747 747312 1384932NM MLG NR 11 FAILED AL SBOFO OTHER E VIBRATION/BUFFET LDLANDING 1 WP33116KB 23207 ON LANDING ROLL, VIBRATION FELT SIMILAR TO NOSE WHEEL SHIMMY. AFTER ENGINE SHUT DOWN, GROUND ENGINEER REPORTED NR 11 TIRE BURST WITH DAMAGE TO ACFT BELLY AREA ABOVE TIRE. APPROACH AND LANDING WERE NORMAL APART FROM VIBRATION OF REVERSERS AND MINIMUM AUTO BRAKE USED. ATC KIX REPORTED NO DEBRIS FOUND ON RUNWAY AFTER LANDING. ON TAKEOFF, SIMILAR VIBRATION FELT. 1. NR 11 AND NR 12 MAIN WHEEL ASSYS WERE REPLACED. 2. ALL MAIN GEAR BRAKE OPERATIONS CHECK OK. 3. ANTI-SKID CONTROL UNIT FUNCTION CHECKED OK. 4. ACCOMPLISHED TIRE BURST INSP PER AMM 5-51-34, PG 201. 5. TEMPORARY REPAIR ON BODY FAIRING. PERMANENT REPAIR C/FWD TO BASE. 2L74 4F RTA20WE 19960105002881996010500288NM 1996 1 5 AWXA9500742 119951103A3350900835A BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20922 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 3 THROUGH ROW 8. REMOVED AND REPLACED BATTERY PACK AT STA 500BR, OPS CHECK GOOD. (X) 2L72 4F A16WE 19960105002891996010500289NM 1996 1 5 AWXA9500749 119951110A3350900835 BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20958 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND OVERHEAD MID-CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F A16WE 19960105002901996010500290NM 1996 1 5 AWXA9500789 119951127A3350900835A BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 20959 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 7 THROUGH ROW 13. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (X) 2L72 4F A16WE 19960105003331996010500333NM 1996 1 5 9521802293 119951230A3350 BATTERY PACK BOEING727 727251 138408HNM RT OVERWING DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01293US 21504 DURING PREFLIGHT, FOUND OVERWING EMERGENCY LIGHT RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK AND CHECKED OK. 2L73 4F A3WE 19960105003341996010500334NM 1996 1 5 9521812707 119951228A2131 CONTROLLER BOEING727 727225 1384077NM CABIN MALFUNCTIONED A NWAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL01816EA 22553 DURING CLIMBOUT, COULD NOT CONTROL CABIN PRESSURIZATION. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PERFORMED VESSEL LEAK CHECK. REPLACED THE LEFT PACK SHUTOFF VALVE, CABIN CONTROLLER, AND PANEL. ALSO, REPLACED EQUIPMENT COOLING PRESSURE SWITCH AND PERFORMED HIGH PRESSURE BLEED CHECK, CHECKED OK. 2L73 4F A3WE 19960105003351996010500335NM 1996 1 5 9521825521 119951229A3233162N000135 ACTUATOR BOEING757 757251 1384970NM NLG MALFUNCTIONED A NWAAO OTHER J WARNING INDICATION DEDESCENT 1 GL01521US 23209 UPON DESCENT INTO DTW DURING GEAR EXTENSION, NOSE GEAR DOOR INDICATION REMAINED ILLUMINATED AND NOSE GEAR INDICATED RETRACTED. DURING LANDING GEAR RECYCLE, GEAR SAFE INDICATION TOOK THREE MINUTES TO ILLUMINATE AND NOSE GEAR MADE A LOUD NOISE UPON EXTENSION. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR ACTUATOR. LEAK AND OPERATIONAL CHECK WAS NORMAL. 2L72 4F RTA2NM 19960105003361996010500336WP 1996 1 5 9521869178 119951231A3350 BATTERIES DOUG DC9 DC914 3022034WP CABIN DISCHARGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL013310L 45705 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19960105003371996010500337NM 1996 1 5 9521886305 119951231A3350 CONNECTOR BOEING747 747451 1384940NM CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01665US 23820 DURING LINE CHECK, THE EMERGENCY PATH LIGHTS AT SEAT ROWS 52R TO 56R WERE FOUND INOPERATIVE. RECONNECTED LIGHT ASSEMBLY PIN IN FLOOR TRACK AND OPERATIONAL CHECK OK. 2L74 4F RTA20WE 19960105003381996010500338WP 1996 1 5 9521899918 119951229A2751ST12AF TRANSMITTER DOUG DC9 DC932 3022066WP LT TE FLAP MALFUNCTIONED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01940N 518502772 47572 DURING CLIMB, THE STALL WARNING SYSTEM ACTIVATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THE STALL WARNING SYSTEM CONTINUED TO ACTIVATE. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED LEFT FLAP POSITION TRANSMITTER AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105003391996010500339WP 1996 1 5 9521929604 119951229A3260 DOWNLOCK WIRE DOUG DC9 DC932 3022066WP NLG BROKEN A NWAAO OTHER N FALSE WARNING APAPPROACH 1 GL01604NW 47222 DURING APPROACH, THE GREEN LIGHT FOR THE NOSE LANDING GEAR DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. EMERGENCY EXTENSION PROCEDURES WERE UTILIZED TO EXTEND THE GEAR. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REPAIRED BROKEN WIRE AT NOSE LANDING GEAR DOWNLOCK SWITCH AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105003401996010500340WP 1996 1 5 9521939919 119951229A32225910448511 SHOCK STRUT DOUG DC9 DC932 3022066WP NLG FAILED A NWAAO OTHER J WARNING INDICATION CLCLIMB 1 GL01941N 8649 8649 47450 DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. UTILIZED LANDING GEAR RELEASE BUTTON AND LANDING GEAR RETRACTED. AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE UNITL 15 MINUTES INTO FLIGHT. AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR SHOCK STRUT AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105003411996010500341WP 1996 1 5 9521949607 119951230A3260 SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR FAILED A NWAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL01607NW 47232 DURING CLIMB, THE LEFT MAIN LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR DOOR MICRO SWITCH AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105003421996010500342WP 1996 1 5 9521959751 119951230A3233 ACTUATOR DOUG DC9 DC941 302207NWP LT MLG LEAKING A NWAAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL01751NW 47115 LOSS OF RIGHT HYDRAULIC SYSTEM OCCURRED DURING APPROACH INTO MSP. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND RIGHT HYDRAULIC FILTER HOUSING AND LEFT MAIN GEAR ACTUATOR LEAKING. REPLACED FILTER HOUSING AND ACTUATOR. ALSO, REPLACED LEFT AND RIGHT MAIN GEAR DOOR SKID PLATES AND LEFT BUNGEE CYLINDER DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105003431996010500343WP 1996 1 5 9521969304 119951230A2530 COFFEE MAKER DOUG DC9 DC982 3022082WP GALLEY MALFUNCTIONED A NWAAO OTHER BH SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC CRCRUISE 1 GL01931MC 48057 EN ROUTE MSP-ATL, SMOKE BEGAN EMANATING FROM THE COFFEE MAKER AREA. GALLEY POWER WAS EXTINGUISHED AND SMOKE DISSIPATED SHORTLY THEREAFTER. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND RIGHT COFFEE MAKER WATER TANK HEATER MELTED. REPLACED COFFEE MAKER AND RESTORED GALLEY POWER. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105003441996010500344WP 1996 1 5 9521979751 119951229A32225910448563 STRUT DOUG DC9 DC941 302207NWP NLG DEFLATED A NWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL01751NW 47115 NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED NOSE GEAR STRUT AND SERVICED TO PROPER LEVELS. OPERATIONAL CHECK NORMAL AND AIRCRAFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105003451996010500345WP 1996 1 5 9521999874 119951229A335060030451 BATTERY PACK DOUG DC9 DC951 3022051WP AFT BAGG BIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01783NC 48108 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EVACUATION SIDE ILLUMINATION LIGHT INOPERATIVE. REPLACED BATTERY PACK IN AFT BAGGAGE BIN AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19960105003461996010500346WP 1996 1 5 9522009308 119951231A3350 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01311RC 48089 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AFT OF ROW 32 INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19960105003561996010500356NM 1996 1 5 DL72K954796 119951228A3350900835A BATTERY PACK BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27417DA 21259 EMERGENCY LIGHTING INOP OVER L-2 DOOR. ITEM FOUND DURING MTC LAYOVER. REPLACED BATT PACK AND ALL OPS NORMAL. 2L73 4F A3WE 19960105003581996010500358NM 1996 1 5 DL72S954792 119951228A5754 SKIN BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27497DA 21077 FOUND DURING A-1 LETTER CHECK, NR 7 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED O/B END. REPAIRED PER M/M 57-54-0 PAR 5A. 2L73 4F A3WE 19960105003591996010500359NM 1996 1 5 DL72S954793 119951228A5754 SKIN BOEING727 727232 1384082NM NR 8 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27497DA 21077 FOUND DURING A-1 LETTER CHECK, NR 8 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12. 2L73 4F A3WE 19960105003601996010500360NM 1996 1 5 DL72S954794 119951228A5720 ANGLE BOEING727 727232 1384082NM RT WING LE CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27497DA 21077 FOUND DURING A-1 LETTER CHECK, NR 6 L/E FLAP ACTUATOR I/B ATTACH ANGLE CRACKED. REPAIRED PER M/M 57-20-21 PAR 12. 2L73 4F A3WE 19960105003611996010500361NM 1996 1 5 DL72S954807 119951129A5315 FLOORBEAM BOEING727 727232 1384082NM FS 344 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 AT HMV, CORROSION ON FS 344 FLOORBEAM UPPER CAP LBL 35R BL 25 C53-224-01.05. REPAIRED PER SRM 53-10-8 FIG 10. 2L73 4F A3WE 19960105003621996010500362NM 1996 1 5 DL72S954811 119951231A3350 POWER SUPPLY BOEING727 727232 1384082NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27495DA 21075 RT AFT OVER DOOR EMERGENCY LIGHT OUT. REPLACED M1093 RACK AND OPERATIONAL CHECKS GOOD. 2L73 4F A3WE 19960105003651996010500365NM 1996 1 5 DL73S954800 119951229A2910 PRESS LINE BOEING737 737232 1384475NM LT MLG LEAKING A DALAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27310DA 23082 HYD SYS-A LOST QTY AND INDICATES ZERO. REPLACED LEFT MLG UPLOCK PRESS LINE. 2L72 4F RTA16WE 19960105003661996010500366NM 1996 1 5 DL73S954804 119951229A3397 WIRE BOEING737 737232 1384475NM CABIN BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 EMERGENCY PATH LIGHTS IN F/C CABIN DAMAGED. REPAIRED WIRE AND OPERATION NORMAL. 2L72 4F RTA16WE 19960105003671996010500367NM 1996 1 5 DL73S954805 119951229A33501619 BULB BOEING737 737232 1384475NM CABIN FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27311DL 23083 L-1 DOOR EMERGENCY SLIDE LIGHT INOP. RELAMPED. 2L72 4F RTA16WE 19960105003681996010500368NM 1996 1 5 DL757954797 119951210A5414 SKIN BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27653DL 24393 PYLON SKIN CRACKED NR 2 PYLON I/B SIDE AT FWD ACCESS HOLE, 2 PLACES. DRILLED OUT ALL FASTENERS, CUT OUT DAMAGED AREA, DRILLED AND INSTALLED REPAIR PER 54-50-01 PG 207. 2L72 4F RTA2NM 19960105003691996010500369NM 1996 1 5 DL757954798 119951210A5414 SKIN BOEING757 757232 1384965NM NR 2 PYLON CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27653DL 24393 PYLON SKIN CRACKED NR 2 PYLON O/B SIDE AT FWD ACCESS HOLE, 1 PLACE. REMOVED FASTENERS/CRACK PER SRM 54-51-01 AND INSTALLED DOUBLER PER SRM 54-51-01. 2L72 4F RTA2NM 19960105003701996010500370NE 1996 1 5 DL757954813 219951231A7261 SCAV VALVE BOEING757 757232 1384965NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALAK NONE J WARNING INDICATION CRCRUISE 1 SO27620DL 22910 716318 STATUS MSG CAME ON IN FLIGHT, L OIL SCAV CLOSE. REPLACED NR 4 BEARING SCAV VALVE PER MM 79-21-12, PERFORMED PFHB TEST 11. T/O PWR ACHIEVED, LEAK CK GOOD AND ALL CKS NORMAL. 2L72 4F4 FRTA2NM E17NE 19960105003721996010500372WP 1996 1 5 DLL10954795 119951228A3350 POWER SUPPLY LKHEED1011 10113851 5265010WP CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27729DA 193C1180 EMERGENCY LIGHTS TEST CAUSES CB2 ON LT FWD POWER PACK TO POP. REPLACED POWER SUPPLY AND OPERATION NORMAL. 2L73 4F A23WE 19960105003731996010500373WP 1996 1 5 DLL10954799 119951229A3244 TIRE LKHEED1011 10113851 5265010WP LEFT GEAR SEPERATION A DALAE ENGINE SHUTDOWN D INFLIGHT SEPARATION TOTAKEOFF 1 SO27729DA 193C1180 AT ROTATION ON TAKEOFF, EXPERIENCED THREE COMPRESSOR STALLS ON NR 1 ENGINE. ENGINE VIBRATION LIGHT ON AND NR 1 ENGINE WAS SHUTDOWN. ON ARRV AT GATE FOUND FOD DAMAGE TO ENG AND NOSE COWL. FOUND NR 2F TIRE RECAP SECTION TO BE CAUSE OF FOD. 2L73 4F A23WE 19960105003741996010500374WP 1996 1 5 DLL10954808 119951231A57431591922108 FITTING LKHEED1011 10113851 5265010WP RT MLG WW CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27716DA 193C1095 THE RT MLG RETRACT ACTUATOR ATTACH FITTING WAS FOUND WITH CORROSION IN INNER AND OUTER FACES OF LUGS NR 21 AND NR 22. REPAIRED PER DL ERA 273024-14. 2L73 4F A23WE 19960105003751996010500375WP 1996 1 5 DLL10954809 119951231A3340 LANDING LIGHT LKHEED1011 10113851 5265010WP RT WING FAILED A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SO27713DA 193C1089 ON SHORT FINAL F/A REPORTED, ELECTRICAL BURNING SMELL AT SEAT 32 AND 33 H/J. SMELL DID NOT INCREASE DURING TAXI TO GATE. ALSO, WINGLANDING LIGHT APPEARED TO BE INOP. INSPECTED CABIN AREA AT SEAT 32 AND 33. COULD NOT IDENTIFY SMOKE SMELL OR ANY EVIDENCE OF FIRE. ALSO, INSPECTED LWR GALLEY AREA, MESC, HYD CTR AND NO TROUBLE FOUND. RAN ENGINES, TURNED ON PACKS AND NO PROBLEMS FOUND. REMOVED RIGHT LANDING LIGHT PANEL AND FOUND GROUND STUD WIRING BURNT. REPAIRS IN PROGRESS. 2L73 4F A23WE 19960105003761996010500376WP 1996 1 5 DLL12954803 119951229A5230 SEAL LKHEED1011 1011385115 5265015WP FWD CARGO DOOR MISSING A DALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO27724DA 193C1151 APPROX 5 MIN AFTER T/O, THE FWD CARGO HOT LIGHT ILLUMINATED. SHORTLY AFTERWARD A POPPING NOISE BEGAN EMANATING FROM RT SIDE OF A/C JUST AFT OF F/C. AFTER LEVEL OFF AT FL 310 TROUBLESHOT BY TURNING ONE PACK OFF AT A TIME, UNABLE TO MAINTAIN PRESSURIZATION WITH 2 PACKS OPERATING AT FL 310. RETURNED TO SJU FOR MTC. FOUND C-1 DOOR FWD UPPER SEAL MISSING. INSTALLED NEW SEAL AND PRESSURIZED A/C PER MM 21-31-00 PG 508, CKD OK. 2L73 4F A23WE 19960105003771996010500377WP 1996 1 5 DLL13954801 119951229A57511529293101 FITTING LKHEED1011 10113851 5265010WP LT AILERON BROKEN A DALAK NONE O OTHER ININSP/MAINT 1 SO27784DA 193A1038 LEFT INBOARD AILERON POSITION INDICATOR ON SPI IS STUCK IN FULL DOWN POSITION. REPLACED LEFT INBD AILERON POSITION TRANSMITTER. ALSO, FOUND LEFT O/B ACTUATOR ATTACH FITTING HAD BROKEN LOOSE FROM AILERON. REPLACED AILERON AND ROUTED TO SHOP. 2L73 4F A23WE 19960105003781996010500378NM 1996 1 5 DLM88954789 119951228A2150 DUCT CLAMP DOUG MD88 MD88 3023688NM RT PACK WORN A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27907DL 49538 DURING CLIMB THROUGH FL 270, FLOW LIGHT ILLUMINATED AND CABIN BEGAN 1,000 FPM CLIMB, UNABLE TO CONTROL MIX VALVE POSITION AND CABIN PRESSURE. FOUND RT PACK DUCT BLOWN OFF. REINSTALLED DUCT, INSTALLED NEW NUT ON CLAMP AND LEAK CHECKED OK. ALSO, CHECKED ALL DOOR SEALS AND ALL CHECKS NORMAL. 2L72 4F RTA6WE 19960105003801996010500380WP 1996 1 5 MWEA95541 119951226A5320 INTERCOSTAL DOUG DC9 DC932 3022066WP FS 426-446 CRACKED A MWEAK NONE O OTHER ININSP/MAINT 1 GL31301ME 47190 DURING INSPECTION, FOUND INTERCOSTAL CRACKED BETWEEN STA 427 AND 446 AT LONGERON 29L. MAINTENANCE REPAIRED INTERCOSTAL IAW SRM 53-01 FIG 2 SHEET 3. 2L72 4F A6WE 19960105003811996010500381 1996 1 5 MWEA96001 219950101A7261 BREATHER O-RING DOUG DC9 DC932 3022066WP LT ENGINE CRACKED A MWEAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31301ME 47190 PILOT REPORTS UPON REACHING CRUISE ALTITUDE FROM DFW, OBSERVED ABNORMAL OIL CONSUMPTION ON LT ENGINE. LANDED IN MCI AS A PRECAUTIONARY MEASURE. MAINTENANCE IN MCI FOUND NR 4 BREATHER LINE O-RING BROKEN. REPLACED O-RING AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. 2L72 4F A6WE 19960105003821996010500382NM 1996 1 5 SCNA95303 119951223A291065178494061 LINE BOEING727 7272J4 1384006NM B-HYD SYS CHAFED A SCNAK NONE KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 GL15284SC 21438 DURING APPROACH, LOST B-SYSTEM HYDRAULIC QUANTITY. A CHAFED HYDRAULIC LINE WAS FOUND IN THE B-SYSTEM HYDRAULIC BAY. REPLACED CHAFED LINE. 2L73 4F RTA3WE 19960105003831996010500383NM 1996 1 5 SCNA95304 119951227A291065178494061 LINE BOEING727 7272J4 1384006NM B-HYD SYS BROKEN A SCNAK NONE KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL15284SC 21438 WHILE EN ROUTE, THE NUMBER 2 B-SYSTEM PUMP OVERHEAT LIGHT ILLUMINATED AND B-SYSTEM QUANTITY WAS NOTED TO BE LOW. PUMP NUMBER 2 WAS TURNED OFF AND THE OVERHEAT LIGHT EXTINGUISHED. FOUND A BROKEN HYDRAULIC LINE AT THE B-SYSTEM MODULAR UNIT. THE HYDRAULIC SYSTEM WAS SERVICED AND THE BROKEN LINE REPLACED. 2L73 4F RTA3WE 19960105003841996010500384NM 1996 1 5 SCNA95305 119951228A3260656021132 ACCESSORY BOX BOEING727 727227 1384078NM E/E BAY FAILED A SCNAK NONE N FALSE WARNING APAPPROACH 1 GL15275AF 22092 THE NOSE GEAR GREEN LIGHT FLICKERED AND THE WARNING HORN SOUNDED SIMULTANEOUSLY. THE LANDING GEAR ACCESSORY BOX WAS REPLACED, THE NOSE GEAR SWUNG FIVE TIMES AND NO DEFECTS WERE NOTED PER MM 32-21-00. 2L73 4F A3WE 19960105003851996010500385NM 1996 1 5 SCNA95306 119951231A2612894120 FIRE LOOP BOEING727 7272A1 138407FNM NR 1 ENGINE DAMAGED A SCNAEF ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CRCRUISE 1 GL15287SC 21345 THE NUMBER ONE ENGINE FIRE WARNING LIGHT ILLUMINATED AND THE BELL SOUNDED DURING FLIGHT. THE ENGINE WAS SHUTDOWN AND BOTH FIRE BOTTLES BLOWN. THE FIRE WARNING DID NOT EXTINGUISH. NO SIGNS OF FIRE WERE NOTED DURING POSTFLIGHT INSPECTION. THE NUMBER 1 ENGINE B-LOOP WAS FOUND CRIMPED IN A CLAMP ON THE ENGINE. REMOVED AND REPLACED LOOP AND FIRE DETECTION SYSTEM TESTED GOOD. 2L73 4F A3WE 19960105003861996010500386WP 1996 1 5 SCNA95307 119951229A3620NHM6031503 SENSE ELEMENT DOUG DC10 DC1010 3022110WP NR 2 PNUEMATICS FAULTY A SCNAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15572SC 46977 THE NUMBER 2 MANIFOLD FAIL LIGHT ILLUMINATED DURING FLIGHT. SHUTDOWN THE NUMBER 2 ENGINE AND FAIL LIGHT REMAINED ON. FLIGHT DIVERTED TO DFW. FOUND BAD SENSE ELEMENT D1-28. REMOVED AND REPLACED SENSE ELEMENT IAW MM 36-23-02. TESTED MANIFOLD SYSTEM PER MM 36-23-00, OPS CHECKED NORMAL. 2L73 4F A22WE 19960105003871996010500387WP 1996 1 5 SCNA95308 119951230A3350EMBS1392 POWER SUPPLY DOUG DC10 DC1010 3022110WP CABIN INOPERATIVE A SCNAK NONE L NO TEST ININSP/MAINT 1 GL15572SC 46977 THE FORWARD CABIN EMERGENCY LIGHTING FAILED SELF TEST. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHTING POWER SUPPLY FOR THE FORWARD CABIN IAW MM 33-50-01, OPS CHECKED NORMAL. 2L73 4F A22WE 19960105003881996010500388NM 1996 1 5 UPS205165 119951216A3350 BATTERY BOEING727 72727C 138400JNM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01907UP 19118 MAINTENANCE REPORTED, CREW ENTRY DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE DURING TEST. REMOVED AND REPLACED CREW ENTRY EMERGENCY EXIT LIGHT BATTERIES AND LIGHT OPERATES NORMALLY. 2L73 4F A3WE 19960105004171996010500417GL 1996 1 5 96ZZZX59 319951005A6111AS841 COUNTERWEIGHT BEECH 58 58 1152740CE MCAULY2AF34CD2AF34C* GL PROP NR 2 BLD CLAMP BROKE A FGHAO OTHER O OTHER TOTAKEOFF 1 AL05619BE 602 TH20 763284 AIRCRAFT WAS ON TAKEOFF ROLL, NO INDICATION OF PROBLEM DURING RUN-UP OR INITIAL POWER APPLICATION DURING TAKEOFF. ABOUT 750 FEET DOWN THE RUNWAY, THE RT ENGINE'S RPM SURGED. THE PILOT THOUGHT MAYBE A CABLE BROKE. AS ACFT SLOWED DOWN, PILOT NOTICED THE RT SPINNER WAS WOBBLING. ACFT EXITED THE RUNWAY, PARKED, AND SHUT BOTH ENGINES DOWN. UPON FURTHER INVESTIGATION, FOUND THE BROKEN COUNTERWEIGHT CLAMP. 1L72 3O 3A16 5 CP5EA 19960105004251996010500425SO 1996 1 5 ZWZA0013 219951118A7414101630203 MAGNETO CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO LT MAG LT ENG FAILED A ZWZAK NONE O OTHER ININSP/MAINT 1 GL2380Q 34 5070956 402B1384 LEFT MAG, LEFT ENGINE, HAS DEAD MAG ON GROUND RUN CHECK. THE FAILED MAGNETO HAD 33.6 HOURS SINCE BEING OVERHAULED. THIS WAS THE THIRD MAG FAILURE IN A ROW, SAME MAG, SAME PLANE, SAME OVERHAULER. (X) 1L72 3O3 O A7CE E8CE 19960105004271996010500427EA 1996 1 5 96ZZZM10 119951113A521085210181003 CABLE ASSY DHAV DHC8 DHC8311 1386006EA AIRSTAIR DOOR BROKEN A MASAK NONE O OTHER ININSP/MAINT 1 SW01431AW 284 AIRSTAIR DOOR CABLE HAD BROKEN AT TERMINAL END DURING NORMAL SERVICE. AFTER REMOVAL OF OLD TERMINAL END IT WAS NOTED THAT THE INNER BEARING WAS EXCESSSIVELY TIGHT AND WOULD NOT ALLOW ROTATION. CABLE WAS REPLACED. (M) 2H72 4T RTA13NM 19960105004281996010500428NM 1996 1 5 96ZZZM12 119951207A335020131A BATTERY PACK BOEING737 7374Q8 NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01779AS 25111 SFO - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9540105. 2L72 4F RTA16WE 19960105004291996010500429WP 1996 1 5 96ZZZM13 119951201A532039361902 ATTACH FITTINGS DOUG DC9 DC982 3022082WP BS 196 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON R1 DOOR GIRT MOUNT ATTACH FITTINGS AT Y174 AND Y196, X MINUS 53, Z PLUS 1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-01 AND 51-01. REFERENCE ASAA9580285. 2L72 4F A6WE 19960105004311996010500431EA 1996 1 5 96ZZZM4 119951030A323085411782001 BRACKET DHAV DHC8 DHC8311 1386006EA LT/RT MLG CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW01433AW8801 305 DURING INSPECTION OF AIRCRAFT IT WAS NOTED THAT THE LEFT AND RIGHT MLG RETRACTION SUPPORT BRACKETS APPEARED TO HAVE A FRETTING CONDITION. THE BRACKETS WERE REMOVED AND INSPECTED IAW AD CF 91-25R2. POSSIBLE CRACK INDICATIONS WERE VERIFIED BY MPI. IT SHOULD BE NOTED THAT THESE BRACKETS WERE PRE-MOD 8/2049 AND POST-MOD 8/1830 AND THAT MOD 8/1830 IS PART OF THE TERMINATING ACTION OF AD CF 91-25R2. BRACKETS WERE REPLACED PER MOD 8/2049 AND SB 8-54-34 ON FIELD AVIATION COMPANY WORK ORDER NR 21973. 2H72 4T RTA13NM 19960105004321996010500432EA 1996 1 5 96ZZZM5 119951031A245082450067001 BRACKET DHAV DHC8 DHC8311 1386006EA LT CONTACTOR BOXCRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW01433AW8801 305 DURING INSPECTION IT WAS NOTED THAT THE CIRCUIT BREAKER BRACKET HAD CRACKED ALLOWING THE CIRCUIT BREAKERS AND WIRING TO BECOME LOOSE IN THE AC CONTACTOR BOX. SUBMITTER STATES, THIS COULD CAUSE A SHORT CIRCUIT OF THE AFFECTED WIRING. A NEW BRACKET WAS FABRICATED AND INSTALLED ON FIELD AVIATION COMPANY WORK ORDER NR 21973. 2H72 4T RTA13NM 19960105004331996010500433EA 1996 1 5 96ZZZM6 119951030A271082700564S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA LT/RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01433AW8801 305 DURING INSPECTION OF AIRCRAFT, FOUND THAT THE LEFT AND RIGHT WING AILERON LOWER CABLES WERE WORN BY PULLEY AT YW 400. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK. 2H72 4T RTA13NM 19960105004341996010500434EA 1996 1 5 96ZZZM7 119951020A271082700568S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01430AW9888 279 DURING INSPECTION, FOUND THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL. THE CABLE WAS CHANGED ON FIELD AVIATION COMPANY WOR NR 21964 AT C-CHECK. (M) 2H72 4T RTA13NM 19960105004351996010500435EA 1996 1 5 96ZZZM8 119951020A271082700568S001 CONTROL CABLE DHAV DHC8 DHC8311 1386006EA RT AILERON WORN A MASAK NONE O OTHER ININSP/MAINT 1 SW01431AW 284 DURING INSPECTION, FOUND THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190. IT SHOULD BE NOTED THAT THIS CONDITION IS NOT VISIBLE WITH THE GUST LOCK ENGAGED AND THE AILERONS IN NEUTRAL POSITION. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21968 AT C-CHECK. 2H72 4T RTA13NM 19960105004361996010500436EA 1996 1 5 96ZZZM9 119951020A323085411782001 BRACKET DHAV DHC8 DHC8311 1386006EA RT MLG CRACKED A MASAK NONE O OTHER ININSP/MAINT 1 SW01431AW 704950G 284 DURING INSPECTION OF AIRCRAFT, FOUND A PROBABLE FRETTING CONDITION EXISTED AT THE RT MLG RETRACTION ACTUATOR SUPPORT BRACKET. THE BRACKET WAS REMOVED AND INSPECTED IAW AD CF91-25R2. A POSSIBLE CRACK INDICATION WAS VERIFIED BY MPI. IT SHOULD BE NOTED THAT THE BRACKET WAS POST MOD 8/1830 AND PRE MOD 8/2049 WHICH IS PART OF THE TERMINATING ACTION OF AD CF91-25R2. THE BRACKET WAS REPLACED PER MOD 8/2049 AND SB 8-54-27 ON FIELD AVIATION COMPANY WORK ORDER NR 21968. 2H72 4T RTA13NM 19960105004371996010500437NM 1996 1 5 ASAA9510110 119951211A33508821004 BATTERY PACK BOEING737 7372Q8C 138448SNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 8 AND 9. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19960105004381996010500438WP 1996 1 5 ASAA95170 119951207A3350 BULB DOUG DC9 DC951 3022051WP VENTRAL STAIRS FAILED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - VENTRAL STAIRS RIGHT SIDE EMERGENCY LIGHT OUT. REPLACED LAMP OPERATIONAL CHECK. (M) 2L72 4F A6WE 19960105004391996010500439NM 1996 1 5 ASAA9540104 119951207A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS, IN AREA OF ROW 15, WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960105004401996010500440NM 1996 1 5 ASAA9540105 119951207A3350PB273 BATTERY CHARGER BOEING737 7374Q8 NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01779AS 25111 SFO - DURING MAINTENANCE CHECK, THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960105004411996010500441NM 1996 1 5 ASAA9540106 119951210A3350S417N50914 TRACK LIGHT BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 2 LIGHT ASSEMBLY BASES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960105004421996010500442NM 1996 1 5 ASAA9540107 119951211A3397 WIRE BOEING737 737490 1384715NM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 21 THROUGH 24. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960105004431996010500443WP 1996 1 5 ASAA9580274 119951123A5210 MECHANISM DOUG DC9 DC982 3022082WP L1 DOOR OUT OF ADJUST A ASAAK NONE O OTHER ININSP/MAINT 1 NM01966AS 49104 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. FOUND DOOR VERTICAL ADJUSTMENT LOW. ADJUSTED VERTICAL RIG OF DOOR PER MM AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960105004441996010500444WP 1996 1 5 ASAA9580278 119951201A5210 MECHANISM DOUG DC9 DC982 3022082WP L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01951AS 49111 SEA - ON ARRIVAL OF FLIGHT 373 CREW REPORTED, THE L1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. LUBED L1 DOOR MECHANISM AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960105004451996010500445WP 1996 1 5 ASAA9580279 119951201A5320S3932140 FLOOR SUPPORT DOUG DC9 DC982 3022082WP BS 159-200 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y159 TO Y200, X PLUS 7, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-01 AND 53-14-01. (M) 2L72 4F A6WE 19960105004461996010500446WP 1996 1 5 ASAA9580280 119951201A5320 SHEAR TIE DOUG DC9 DC982 3022082WP BS 1079 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SHEAR TIE AT Y1079, X PLUS 12, Z MINUS 44. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-03. (M) 2L72 4F A6WE 19960105004471996010500447WP 1996 1 5 ASAA9580281 119951201A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP BS 1212-1231 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, FOUND CORROSION ON INTERCOSTAL AT Y1212 TO Y1231, X PLUS 7, Z MINUS 45. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-04, 53-10-02 AND 53-14-03. (M) 2L72 4F A6WE 19960105004481996010500448WP 1996 1 5 ASAA9580282 119951201A5320S4616493 SUPPORT DOUG DC9 DC982 3022082WP BS 179-216 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, FOUND CORROSION ON L1 DOOR THRESHOLD SUPPORT AT Y179 TO Y216, X PLUS 56, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-10-04, 51-30-05 AND 51-30-08. (M) 2L72 4F A6WE 19960105004491996010500449WP 1996 1 5 ASAA9580283 119951201A5320 MOPSILL DOUG DC9 DC982 3022082WP R1 DOOR CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, FOUND CORROSION ON R1 DOOR MOPSILL. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-02, 51-10-04, AND 53-01. (M) 2L72 4F A6WE 19960105004501996010500450WP 1996 1 5 ASAA9580284 119951201A5320993061269 WEB DOUG DC9 DC982 3022082WP BS 1098-1175 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, FOUND CORROSION ON L2 DOOR WEB AT Y1098 TO Y1175, X PLUS 49, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-01, 51-30-02, AND 51-30-05. (M) 2L72 4F A6WE 19960105004511996010500451WP 1996 1 5 ASAA9580285 119951201A532039361901 ATTACH FITTINGS DOUG DC9 DC982 3022082WP BS 174 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON R1 DOOR GIRT MOUNT ATTACH FITTINGS AT Y174 AND Y196, X MINUS 53, Z PLUS 1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-01 AND 51-01. (M) 2L72 4F A6WE 19960105004521996010500452WP 1996 1 5 ASAA9580287 119951204A5347TMS6013506 CARGO TRACK DOUG DC9 DC982 3022082WP BS 1212-1272 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CARGO TRACK AT Y1212 TO Y1272, X MINUS 16. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-04 AND 51-30-01. (M) 2L72 4F A6WE 19960105004531996010500453WP 1996 1 5 ASAA9580288 119951206A32225958412511 STRUT DOUG DC9 DC983 3022083WP NLG REQ'D SERVICE A ASAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM01968AS261953606 53016 ANC - AIR TURN BACK OF FLIGHT NR 82, CREW REPORTED, THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR STRUT LOW. SERVICED NOSE LANDING GEAR STRUT TO PROPER DIMENSION. ACCOMPLISHED GEAR SWING AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19960105004541996010500454WP 1996 1 5 ASAA9580289 119951207A78307936907603 HYD LINE DOUG DC9 DC982 3022082WP LT TR UNIT BROKEN A ASAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM01932AS 49233 PDX - AIR TURN BACK OF FLIGHT 524, CREW REPORTED, THE LEFT ENGINE THRUST REVERSER ACCUMULATOR LOW PRESSURE WARNING LIGHT ILLUMINATED AND LEFT HYDRAULIC QUANTITY DECREASED, SHUT OFF LEFT ENGINE DRIVEN HYDRAULIC PUMP AND HYDRAULIC QUANTITY STABILIZED. LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LINE FROM LEFT ENGINE THRUST REVERSER ACCUMULATOR TO ACCUMULATOR LOW PRESSURE WARNING SWITCH LEAKING. REPLACED HYDRAULIC LINE AND SERVICED HYDRAULIC SYSTEM. (M) 2L72 4F A6WE 19960105004551996010500455WP 1996 1 5 ASAA9580290 119951209A33501001191 LIGHT DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01966AS45056 49104 SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY LIGHT WOULD NOT TURN OFF. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960105004561996010500456NM 1996 1 5 AWXA9500732 119951028A3350 TRACK BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28305AW 24012 PHX - DURING ROUTINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 21 THROUGH ROW 23. REINSTALLED TRACKS, OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 19960105004571996010500457NM 1996 1 5 AWXA9500733 119951028A335020131A BATTERY PACK BOEING737 73733A 1384673NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28173AW 23632 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FORWARD CEILING EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004581996010500458NM 1996 1 5 AWXA9500734 119951030A3397 WIRE BOEING737 737112 1384412NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28708AW 19771 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND ROW 3 EMERGENCY EXIT LIGHTS INOPERATIVE. RECONNECTED POWER SUPPLY CABLE, OPS CHECK GOOD. (M) 2L72 4F A16WE 19960105004591996010500459NM 1996 1 5 AWXA9500735 119951030A3350900835A LIGHT BOEING737 737277 1384570NM RT EXTERIOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28188AW 22655 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERIOR RT AFT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004601996010500460NM 1996 1 5 AWXA9500736 119951030A335020131A BATTERY PACK BOEING737 73733A 1384673NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28169AW 23630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004611996010500461NM 1996 1 5 AWXA9500737 119951031A33501000679 LIGHT BOEING737 737277 1384570NM L2 DOOR INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR PORTABLE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE LIGHT ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004621996010500462NM 1996 1 5 AWXA9500743 119951105A3350 CONNECTOR BOEING737 7373Y0 1384671NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 23747 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RECONNECTED LIGHT ASSEMBLY CONNECTOR. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004631996010500463NM 1996 1 5 AWXA9500764 119951116A5330 SKIN BOEING737 737277 1384570NM BS 767-777 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28185AW 22652 PHX - FLT 450 - DURING WALK AROUND INSPECTION, A 4 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AT STRINGER 16L, STATION 767 TO STATION 777. REPAIRED CRACK PER SRM 53-30-03. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960105004641996010500464NM 1996 1 5 AWXA9500765 119951116A5330 SKIN BOEING737 737112 1384412NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28708AW 19771 PHX - FLT NR 425 - DURING WALK AROUND INSPECTION, 1.2 INCH CRACK WAS FOUND IN BELLY SKIN AT STATION 727. REPAIRED PER SRM 53-30-03, FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19960105004651996010500465NM 1996 1 5 AWXA9500766 119951116A5330 SKIN BOEING737 7372M8 1384483NM BS 947 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28141AW 21955 LAS - FLT NR 067 - ON WALK AROUND INSPECTION, FOUND A 2.375 INCH CRACK IN FUSELAGE SKIN, AT STATION 947 STRINGER 18L. REPAIRED IAW SRM 53-30-03, FIGURE 6. (M) 2L72 4F A16WE 19960105004661996010500466NM 1996 1 5 AWXA9500767 119951115A3350900835A POWER SUPPLY BOEING737 737277 1384570NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004671996010500467NM 1996 1 5 AWXA9500768 119951116A3350 CONNECTOR BOEING737 7373G7 1384595NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304AW 24011 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 6 THROUGH ROW 10. RECONNECTED LOOSE CONNECTOR AT ROW 10, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004681996010500468NM 1996 1 5 AWXA9500770 119951117A3350900835A BATTERY PACK BOEING737 737277 1384570NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28189AW 22656 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND AFT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT OVERHEAD BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004691996010500469NM 1996 1 5 AWXA9500772 119951119A3350 SPLICE BOEING737 737277 1384570NM CABIN BAD A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28179AW 22646 PHX - DURING ROUTINE MAINTENANCE CHECK, WHEN EMERGENCY EXIT LIGHT SWITCH IS ARMED, HALF OF THE LIGHTS REMAIN ON. REPLACED BAD SPLICE, SYSTEM OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004701996010500470NM 1996 1 5 AWXA9500773 119951119A3397 WIRE BOEING737 737297 1384480NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28147AW 22630 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT ROW 1L. REPAIRED WIRES, OPS CHECK GOOD. (M) 2L72 4F A16WE 19960105004711996010500471NM 1996 1 5 AWXA9500774 119951120A3350900835A POWER SUPPLY BOEING737 7372U9 1384498NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28149AW 22575 PHX - DURING ROUTINE MAINTENANCE CHECK, FORWARD EXIT EMERGENCY LIGHT REMAINED ON WHEN SWITCH IN ARMED POSITION. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004721996010500472NM 1996 1 5 AWXA9500775 119951118A5315 FLOOR BEAM BOEING737 737277 1384570NM BS 297 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - DURING SCHEDULED C14 INSPECTION, FOUND FLOOR BEAM T-CAP CORRODED BEYOND LIMITS AT STATION 297 LBL 11 TO RBL 47. REPAIRED PER SRM 53-10-9, FIGURE 5. (M) 2L72 4F RTA16WE 19960105004731996010500473NM 1996 1 5 AWXA9500776 119951118A5347 SEAT TRACK BOEING737 737277 1384570NM BS 328 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - DURING SCHEDULED C14 INSPECTION, FOUND SEAT TRACK FASTENER HOLES CORRODED BEYOND LIMITS, AT STATION 328 RBL 24.5. REPLACED SECTION OF SEAT TRACK PER SRM 53-10-5, FIGURE 2. (M) 2L72 4F RTA16WE 19960105004741996010500474NM 1996 1 5 AWXA9500777 119951118A5330 SKIN BOEING737 737277 1384570NM R2 DOOR CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28179AW 22646 PHX - DURING SCHEDULED C14 INSPECTION, FOUND ONE INCH CRACK IN FUSELAGE SKIN AT R2 DOOR HINGE CUTOUT. REPAIRED PER ER 2-53-36-17A. (M) 2L72 4F RTA16WE 19960105004751996010500475NM 1996 1 5 AWXA9500784 119951120A3350276005 FUSE BOEING737 73733A 1384673NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3 THROUGH ROW 6. REMOVED AND REPLACED FUSE AT FORWARD OVERHEAD BATTERY PACK, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004761996010500476NM 1996 1 5 AWXA9500785 119951122A3350276005 FUSE BOEING737 73733A 1384673NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE, FROM ROW 3ABC THROUGH ROW 6ABC. REMOVED AND REPLACED FUSE IN BATTERY CHARGER ASSEMBLY, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004771996010500477NM 1996 1 5 AWXA9500786 119951121A575465C26601170 SLAT BOEING737 7373G7 1384595NM NR 1 LE SLAT CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28154AW 316 23776 PHX - DURING SCHEDULED C9 INSPECTION, FOUND A 1.75 INCH CRACK IN NR 1 SLAT LOWER T/E SKIN, INBOARD OF SLAT ACTUATOR. REPAIRED PER BOEING REPAIR DRAWING 65C30133. (M) 2L72 4F RTA16WE 19960105004781996010500478NM 1996 1 5 AWXA9500798 119951208A3412102LA2AG TAT PROBE BOEING757 7572S7 1384962NM COCKPIT FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP28901AW 81601 23321 PHX - FLT NR 3808 - AIR-TURNBACK - EICAS MESSAGE FOR TAT. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED TAT PROBE. ALSO, REPLACED RELAYS K203 AND K410, PRECAUTIONARY. (M) 2L72 4F RTA2NM 19960105004791996010500479NM 1996 1 5 AWXA9500800 119951212A5315BAC14902720 FLOOR BEAM BOEING757 7572S7 1384962NM BS 1681 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PAE - FLT NR 1018 - DURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION OUT OF LIMITS UPPER CHORD OF FLOOR BEAM, BS 1681 RBL 15 - LBL 53. REPAIRED FLOOR BEAM IAW TRAMCO EWO 95-4073, MWO INTERIOR 151 AND 152. (M) 2L72 4F RTA2NM 19960105004801996010500480NM 1996 1 5 AWXA9500801 119951201A33506104781 BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 72914 20922 PHX - FLT NR 604 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ON LEFT SIDE AFT CARGO. OPS CHECKED NORMAL, OK FOR SERVICE. (M) 2L72 4F A16WE 19960105004811996010500481NM 1996 1 5 AWXA9500802 119951201A3350900835A BATTERY PACK BOEING737 737275 1384485NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP282FOR 05617 20922 PHX - FLT NR 604 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT SIGNS AT OVERWING WILL NOT LIGHT. REMOVED AND REPLACED BATTERY PACK. OPS GOOD ON GROUND. (M) 2L72 4F A16WE 19960105004821996010500482NM 1996 1 5 AWXA9500803 119951202A3350 CONNECTOR BOEING737 737277 1384570NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28178AW 22645 PHX - FLT NR 1267 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT ROW 19 INOP. RECONNECTED EMERGENCY LIGHT CONNECTOR AT SEAT 19 ABC. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004831996010500483NM 1996 1 5 AWXA9500804 119951205A3397 WIRE BOEING737 7373G7 1384595NM CABIN FAILED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28309AW 24711 PHX - FLT NR 0536 - DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT EMERGENCY LIGHTS INOP, AT ROWS 15-17. REPAIRED WIRING SYSTEM. OPS GOOD. (M) 2L72 4F RTA16WE 19960105004841996010500484NM 1996 1 5 AWXA9500805 119951206A335020121 BATTERY PACK BOEING757 75723A 1384967NM CABIN DISCHARGED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28916AW 60540 24291 PHX - FLT NR 0001 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT R2 DOOR INOP. REMOVED AND REPLACED CHARGER AND BATTERY PACK, OPS CHECK OK. (M) 2L72 4F RTA2NM 19960105004851996010500485NM 1996 1 5 AWXA9500806 119951208A335020131 BATTERY PACK BOEING737 7373G7 1384595NM CABIN INOPERATIVE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304AW 20131 24011 PHX - FLT NR 1258 - DURING ROUTINE MAINTENANCE CHECK, FOUND CENTER CABIN BULL NOSE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED RIGHT MID BATTERY PACK. OPS CHECKED GOOD ON GROUND. (M) 2L72 4F RTA16WE 19960105004861996010500486NM 1996 1 5 AWXA9500807 119951209A3397 WIRE BOEING757 7572S7 1384962NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28906AW 23568 PHX - FLT NR 0700 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT SEAT ROW 20 INOP. REPAIRED WIRING AS REQUIRED, OPS CHECK GOOD. (M) 2L72 4F RTA2NM 19960105004871996010500487NM 1996 1 5 AWXA9500808 119951210A3397 WIRE BOEING737 7373G7 1384595NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28155AW 23777 PHX - FLT NR 0480 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT ON SEAT 1L INOP. REPAIRED BROKEN WIRES ON CONN AT ROW 1. SYSTEM OPS CHECK NORMAL. (M) 2L72 4F RTA16WE 19960105004881996010500488NM 1996 1 5 AWXA9500809 119951210A3350 LIGHT BOEING737 737277 1384570NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28188AW 22655 PHX - FLT NR 0499 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT, AT ROW 17, HANGING FROM HOUSING. RESECURED LIGHT ASSEMBLY. SYSTEM OPS GOOD. (M) 2L72 4F RTA16WE 19960105004891996010500489NM 1996 1 5 AWXA9500810 119951212A5315BAC14902865 FLOOR BEAM BOEING757 7572S7 1384962NM BS 1661 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PAE - FOUND CORROSION OUT OF LIMITS, FLOOR BEAM UPPER CHORD BS 1661 LBL 56-RBL 56, WL 208. REPAIRED FLOOR BEAM IAW SRM 53-00-51 (MWO INTERIOR 122). (M) 2L72 4F RTA2NM 19960105004901996010500490NM 1996 1 5 AWXA9500811 119951212A5315BAC14902734 FLOOR BEAM BOEING757 7572S7 1384962NM BS 1640 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28902AW 23322 PAE - CORROSION OUT OF LIMITS ON FLOOR BEAM UPPER CHORD BS 1640, RBL 59-BLQ, WL 208 SEVERAL AREAS. REPAIRED FLOOR BEAM IAW 53-00-51 (MWO INTERIOR 134). (M) 2L72 4F RTA2NM 19960105004911996010500491NM 1996 1 5 AWXA9500812 119951213A3397 WIRE BOEING737 73733A 1384673NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28509DC 23636 PHX - FLT NR 0202 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OUT AT ROW 4. BROKEN WIRE, REPINNED, OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004921996010500492NM 1996 1 5 AWXA9500813 119951213A3350 LIGHT BOEING737 7373G7 1384595NM CABIN BARE WIRES A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28156AW 23778 PHX - FLT NR 0653 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT ROW 22 HAS BARE WIRES. REPLACED EMERGENCY LIGHT ASSEMBLY AT ROW 22. OPS CHECK GOOD. (M) 2L72 4F RTA16WE 19960105004931996010500493NM 1996 1 5 AWXA9500818 119951217A3350 CONNECTOR BOEING757 75723A 1384967NM CABIN LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28916AW 24291 PHX - FLT NR 0020 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERENCY LIGHTS INOP AT R2 OVERHEAD AND AFT LAV CENTER AND RIGHT OVERHEAD. FOUND LOOSE CONNECTION AT POWER SUPPLY AFT OF L2 DOOR, OVERHEAD BIN NR 10 LEFT SIDE. RECONNECTED SYSTEM, OPS CHECKED GOOD. (M) 2L72 4F RTA2NM 19960105004941996010500494SO 1996 1 5 C2XA95CL124 119951212A27503075001007 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09127152628 0066 120125 CLE - FLT NR 3285 - AFTER TAKEOFF, CREW REPORTED A FLAP DISAGREEMENT, AIR TURN BACK TO CLE. MAINTENANCE RESET THE FLAP CONTROL UNIT. THE SUBSEQUENT FLIGHT ALSO NR 3285, AIR RETURNED TO CLE DUE TO FLAP DISAGREEMENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB120 MM 27-50-06, ALL OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 27-50-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960105004951996010500495SO 1996 1 5 C2XA95CL125 119951212A27523203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTIONED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW091271512438 120125 CLE - FLIGHT NR 3347 - AFTER TAKEOFF, CREW REPORTED A FLAP DISAGREEMENT UPON FLAP RETRACTION. AIRCRAFT AIR RETURNED TO CLE. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ROLLERS AND THE RIGHT OUTBOARD FLAP ACTUATOR IAW EMB-120 MM 27-50-12, 27-50-04 AND 27-50-09. OPERATIONAL TEST WERE GOOD IAW EMB-120 MM 27-50-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960105004961996010500496SO 1996 1 5 C2XA95CL126 119951212A323020885 UPLOCK ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW093171113003 506 120107 GRR - FLT NR 3378 - AFTER TAKEOFF AND GEAR RETRACTION, THE LEFT MAIN LANDING GEAR DID NOT INDICATE AN UP AND LOCKED CONDITION. THE LANDING GEAR WAS RECYCLED WITH THE SAME RESULTS. THE AIRCRAFT AIR RETURNED TO GRR. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED THE LEFT MAIN LANDING GEAR UPLOCK ACTUATOR LINKAGE, IAW EMB-120 MM 32-32-09. ALL OPERATIONAL CHECKS WERE GOOD IAW EMB120 MM 32-32-00. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960105004971996010500497SO 1996 1 5 C2XA95IA384 119951210A573012033270001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING 1A, 3A CHECK INSPECTION, FOUND A CRACK IN THE LOWER INBOARD WING SKIN BETWEEN TWO FASTENERS, AT THE AFT OUTBOARD CORNER OF PANEL 522EB. MAINTENANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IN REFERENCE TO THE EMB 120 SRM 57-20-01. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105004981996010500498SO 1996 1 5 C2XA95IA385 119951210A571312016088001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0912709 120101 IAH - DURING 1A, 3A CHECK, FOUND LEFT WING LOWER SURFACE INTERNAL STRINGER NR 10 CRACKED, FORWARD OF FUEL PANEL NR 522EB. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR SPLICE IN REF TO EMB DER APPROVED FAX NR EST-501/95. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105004991996010500499SO 1996 1 5 C2XA95IA386 119951207A32331959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0915732 120195 JAN - FLT NR 2683 - PILOT REPORTED, THAT THE LEFT GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT, AND WAS THEN FERRIED TO IAH, WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT GEAR RETRACT ACTUATOR. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005001996010500500EU 1996 1 5 C2XA95IA387 119951210A33503011180 POWER SUPPLY AEROSPATR42 ATR42320 8680930EU CABIN FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0917810 093 IAH - DURING A 3A INSPECTION, THE FORWARD SET OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19960105005011996010500501SO 1996 1 5 C2XA95IA388 119951213A572012017096017 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15, LOWER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005021996010500502SO 1996 1 5 C2XA95IA389 119951213A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15, LOWER NR 3, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005031996010500503SO 1996 1 5 C2XA95IA390 119951213A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15 LOWER NR 4, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005041996010500504SO 1996 1 5 C2XA95IA391 119951213A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 16, UPPER NR 5, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005051996010500505SO 1996 1 5 C2XA95IA392 119951213A572012017057007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 16 LOWER NR 3, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005061996010500506SO 1996 1 5 C2XA95IA393 119951213A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 16 LOWER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005071996010500507SO 1996 1 5 C2XA95IA394 119951213A572012017056011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0926714 120118 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 16 LOWER NR 4, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005081996010500508SO 1996 1 5 C2XA95IA395 119951218A540012030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE NACELLE FRAME NR 2 UPPER ANGLE CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005091996010500509SO 1996 1 5 C2XA95IA396 119951218A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME, NR 2 UPPER ANGLE, CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005101996010500510SO 1996 1 5 C2XA95IA397 119951218A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME, NR 2 UPPER ANGLE, CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005111996010500511SO 1996 1 5 C2XA95IA398 119951218A572012017051014 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 5 LOWER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005121996010500512SO 1996 1 5 C2XA95IA399 119951218A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 16 UPPER NR 2 AND NR 3, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005131996010500513SO 1996 1 5 C2XA95IA400 119951218A572012017056013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15 LOWER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005141996010500514SO 1996 1 5 C2XA95IA401 119951218A572012017056015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15 LOWER NR 3, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005151996010500515SO 1996 1 5 C2XA95IA402 119951218A572012017056017 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 15 LOWER NR 4, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005161996010500516SO 1996 1 5 C2XA95IA403 119951218A572012017063009 SKIN SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT WING, RIB NR 21 UPPER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005171996010500517SO 1996 1 5 C2XA95IA404 119951219A572012017056013 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 15 LOWER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005181996010500518SO 1996 1 5 C2XA95IA405 119951219A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 15 LOWER NR 3, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005191996010500519SO 1996 1 5 C2XA95IA406 119951219A572012017056015 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 15 LOWER NR 4, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005201996010500520SO 1996 1 5 C2XA95IA407 119951219A572012017056019 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 15 LOWER NR 5, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005211996010500521SO 1996 1 5 C2XA95IA408 119951219A572012017056007 SKIN SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING, RIB NR 16 UPPER NR 2, SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005221996010500522SO 1996 1 5 C2XA95IA409 119951219A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005231996010500523SO 1996 1 5 C2XA95IA410 119951219A5347120159997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT SIDEWALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005241996010500524SO 1996 1 5 C2XA95IA411 119951219A534712015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD FLOOR SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005251996010500525SO 1996 1 5 C2XA95IA412 119951219A534712016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD FLOOR SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005261996010500526SO 1996 1 5 C2XA95IA413 119951219A532012034416001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE LEFT FUSELAGE SKIN SUPPORT, AT FRAME NR 9, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005271996010500527SO 1996 1 5 C2XA95IA414 119951219A532012034416001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916724 120171 IAH - DURING C-CHECK INSPECTION, THE RIGHT FUSELAGE SKIN SUPPORT, AT FRAME NR 9, WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960105005281996010500528NM 1996 1 5 CAL950984 119951030A271065447618 PCU BOEING737 737130 1384435NM AILERON LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW093320214401 19019 FLT NR 1790 - THE B-HYDRAULIC SYSTEM HAD A PARTIAL DROP IN QUANTITY WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE B-SYSTEM AILERON PCU LEAKING. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71 AND OPERATION CHECKED GOOD. (M) 2L72 4F A16WE 19960105005291996010500529NM 1996 1 5 CAL950985 119951030A2612472622 FIRE DET MODULE BOEING737 7373T0 1384582NM E/E COMPT INOPERATIVE A CALAF ACTIVATE FIRE EXT. N FALSE WARNING APAPPROACH 1 SW0914335640 23573 FLT NR 0118 - IAH - THE APU FIRE WARNING LIGHT ILLUMINATED WHILE CRANKING APU ON SHORT FINAL. THE APU FIRE WARNING HANDLE WAS PULLED, BUT THE LIGHT REMAINED ON. THE APU FIRE BOTTLE WAS DISCHARGED AND THE LIGHT EXTINGUISHED. THE APU AND REAR OF AIRCRAFT WERE INSPECTED WITH NO EVIDENCE OF FIRE FOUND. THE APU WAS RUN AND NO DISCREPANCIES WERE OBSERVED. THE FIRE DETECTION CONTROL MODULE FAILED SYSTEM TEST PER MM 26-15-00. THE FIRE DETECTION MODULE WAS REMOVED AND REPLACED. THE MODULE TESTED GOOD AND THE APU WAS RUN WITHOUT FAULT. IN ADDITION, THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. (M) 2L72 4F RTA16WE 19960105005301996010500530NM 1996 1 5 CAL950987 119951029A2612 FIRE LOOP GARRTT 38042861 BOEING737 7373T0 1384582NM APU SHORTED A CALAO OTHER N FALSE WARNING CRCRUISE 1 SW0976355 P60402 23593 FLT NR 1523 - IAH - TWENTY MINUTES INTO THE FLIGHT, AFTER THE APU HAD BEEN SHUT DOWN. THE APU FIRE LIGHT ILLUMINATED WITH FIRE BELL. THE FIRE HANDLE WAS PULLED AND THE WARNING CEASED WITHIN 3-4 MINUTES. MAINTENANCE FOUND THE APU FIRE DETECTION LOOP SHORTING AGINST LOWER SHROUD. THE LOOP WAS REPOSITIONED AND THE FALSE FIRE INDICATION WAS ELIMINATED. IN ADDITION, A HOLE WAS DISCOVERED IN THE APU MUFFLER. THE APU HAD BEEN PLACARDED INOPERATIVE, DUE TO THE FIRE DETECTION PROBLEM, AND THE PLACARD WILL REMAIN PENDING EXHAUST SHROUD REPLACEMENT. (M) 2L72 4F RTA16WE 19960105005311996010500531WP 1996 1 5 CAL951016 119951103A3260 DOWNLOCK SENSOR DOUG DC9 DC932 3022066WP NLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0969523 47520 FLT NR 1100 - LEAVING IAH, THE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED, AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE RED LIGHT REMAINED ON WITH GEAR RETRACTED. WHEN THE GEAR WAS EXTENDED FOR RETURN TO IAH, INDICATIONS WERE NORMAL. THE NOSE GEAR DOWNLOCK SENSOR WAS REMOVED AND REPLACED. THE NOSE GEAR WAS RETRACTED AND EXTENDED SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING NORMAL PER MM 32-60-1. (M) 2L72 4F A6WE 19960105005321996010500532NM 1996 1 5 CAL951049 119951118A3610652244143 DUCT BOEING727 727243 138408DNM NR 3 ENGINE RUPTURED A CALAAJ UNSCHED LANDING DUMP FUEL N FALSE WARNING CLCLIMB 1 SW0917407 21270 FLT NR 0382 - FLL - THE NR 3 ENGINE LIGHT ILLUMINATED AFTER TAKEOFF FROM FLL. ENGINE POWER WAS REDUCED AFTER LEVELING OFF AND THE ENGINE FIRE WARNING LIGHT EXTINGUISHED. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO FLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 13TH STAGE DUCT RUPTURED WITH RESULTING DAMAGE TO THE UPPER COWLING. THE 13TH STAGE DUCT AND UPPER COWLING WERE REMOVED AND REPLACED. THE NR 3 ENGINE WAS RUN AND OPERATION CHECKED GOOD WITH NO LEAKS NOTED. (M) 2L73 4F RTA3WE 19960105005331996010500533WP 1996 1 5 CAL951050 119951118A3260 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG WIRING PULLED A CALAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW0912539 45792 FLT NR 1401 - IAH - THE LEFT MLG HAD NO TRANSIT LIGHT OR GEAR DOWN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE CHECKLIST WAS COMPLIED WITH, A TOWER FLY-BY WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRING PULLED OUT OF CANNON PLUG FOR THE LEFT MLG DOWNLOCK SWITCH. THE CANNON PLUG WAS REMOVED AND REPLACED. GEAR OPERATION AND INDICATIONS CHECKED GOOD. (M) 2L72 4F A6WE 19960105005341996010500534NM 1996 1 5 EISA95430 119951118A5320 ANGLE BOEING727 727221 1384071NM BS 1183 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 PRESSURE BULKHEAD STATION 1183, FORWARD SIDE RBL HORIZONTAL ANGLE AND TIE CLIP CORRODED. INSTALLED ALL PARTS, REMOVED AND FABRICATED PER SRM 51-81-1. (M) 2L73 4F A3WE 19960105005351996010500535NM 1996 1 5 EISA95431 119951120A5320 CHANNEL BOEING727 727221 1384071NM BS 967 DENTED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 AFT CARGO LOWER BILGE HAT CHANNEL DENTED, AT STATION 967 ABOVE AND BETWEEN STRINGER 30 AND 29L. REMOVED HAT CHANNEL AND DENT, FABRICATED REPAIR PER SRM 51-40-1 TREATED AND PRIMED PER 51-10-2. INSTALLED HAT CHANNEL PER SRM 51-10-2. (M) 2L73 4F A3WE 19960105005361996010500536NM 1996 1 5 EISA95432 119951118A5320 FLANGE BOEING727 727221 1384071NM BS 950 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07368PA 22540 FOUND CORROSION, AT STRINGER 950D LOWER FLANGE. REMOVED FLANGE PER SRM 51-10-1, FABRICATED NEW FLANGE AND INSTALLED PER SRM 51-10-6 AND 51-10-2. (M) 2L73 4F A3WE 19960105005371996010500537NM 1996 1 5 EISA95441 119951124A5311 FRAME BOEING727 727251 138408HNM BS 340 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07263US 19982 AT STATION 340 LEFT, CRACK EXISTS ON FRAME AT THE QG BARRIER ATTACH FITTING. REMOVED AND REPLACED FITTING IAW SRM 51-10-00 AND 57-10-30. (M) 2L73 4F A3WE 19960105005381996010500538WP 1996 1 5 HALA95162 119951129A52805913433503N HINGE DOUG DC9 DC951 3022051WP LT MLG DOOR CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP132FOR 48122 IN S-CHECK, DURING ACCOMPLISHMENT OF AD 91-22-07, FOUND LEFT OUTBOARD GEAR DOOR HINGE HAD 3 CRACKED LOBES. REPLACED LEFT OUTBOARD GEAR DOOR HINGE. (M) 2L72 4F A6WE 19960105005391996010500539WP 1996 1 5 HALA95166 119951206A3222 STRUT DOUG DC9 DC951 3022051WP NLG REQ'D SERVICE A HALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP13699HA 47763 FLT NR 545 - HNL - NOSE GEAR WOULD NOT RETRACT ON GO-AROUND. SERVICED NOSE STRUT PER MM 32-71-2 PARA 3B. RETRACTION CHECK ACCOMPLISHED. OPERATIONS CHECK OK. (M) 2L72 4F A6WE 19960105005401996010500540WP 1996 1 5 HALA95168 119951207A3350 BATTERIES DOUG DC9 DC951 3022051WP CABIN DISCHARGED A HALAK NONE L NO TEST ININSP/MAINT 1 WP13709HA 47764 HNL - EMERGENCY LIGHT AISLE OVERHEAD IS DIM, FROM ROW 17 AFT. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONS CHECK OK. (M) 2L72 4F A6WE 19960105005411996010500541WP 1996 1 5 9521799989 119951231A3350 POWER SUPPLY DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018945E 47181 DURING LINE CHECK, FOUND TAILCONE EMERGENCY LIGHTS AND ENTRY DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY, BATTERIES AND REPLACED FUSE. OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105005421996010500542WP 1996 1 5 9521839104 119951228A5210 SKIN DOUG DC9 DC915 3022036WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194S 47204 DURING H-CHECK, FOUND A .25 INCH CRACK IN THE MAIN CABIN DOOR SKIN AT THE AFT SIDE FS 200, NR 4 STOP. REPAIRED SKIN (P/N 5911406-59) PER EA 91-102632. 2L72 4F A6WE 19960105005431996010500543WP 1996 1 5 9521849936 119951229A5320 DOOR JAMB DOUG DC9 DC931 3022065WP CARGO COMPT CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL011799U 47370 DURING L-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB PAN SPLICE JOINTS. REPAIRED PAN (P/N 5912494-501) PER EA 99-103354. 2L72 4F A6WE 19960105005441996010500544WP 1996 1 5 9521859610 119951230A5320 FITTINGS DOUG DC9 DC932 3022066WP FS 908 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 908 LOWER FRAME FITTINGS AT LONGERON 18R. REPLACED FITTINGS (P/N 49129-501, 4912817-501, 4912817-504) PER SRM 51-30-5. 2L72 4F A6WE 19960105005451996010500545WP 1996 1 5 9521879984 119951229A3350 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01984US 47383 DURING LINE CHECK, FOUND LEFT AND RIGHT EMERGENCY EXIT SIGNS AT ROW 13 INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105005461996010500546WP 1996 1 5 9521909997 119951229A3350 LIGHT DOUG DC9 DC931 3022065WP CABIN BROKEN A NWAAK NONE L NO TEST ININSP/MAINT 1 GL018933E 47142 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN ON THE LEFT SIDE OF THE AFT FLIGHT ATTENDANT SEAT. REPLACED LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD. 2L72 4F A6WE 19960105005591996010500559WP 1996 1 5 MWEA96002 119950103A335060030451 BATTERY PACK DOUG DC9 DC932 3022066WP CABIN DISCHARGED A MWEAK NONE L NO TEST ININSP/MAINT 1 GL31202ME 47672 DURING A CHECK FOUND FIRST FOUR ROWS OF OVERHEAD EMERGENCY LAMPS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. 2L72 4F A6WE 19960105005601996010500560EU 1996 1 5 QXEA9500459 119951230A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09454US 11107 GEG - EXIT ROW LIGHTING ROW 8, RIGHT SIDE IS INOP IN ARMED POSITION. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105005611996010500561EU 1996 1 5 QXEA9500460 119951231A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09468US 11095 PDX - LEFTHAND OVERWING EMERGENCY EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105005621996010500562EU 1996 1 5 QXEA9500461 119951231A3350608905 BATTERY FOKKERF28 F28MK1000 4990808EU CABIN DISCHARGED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09462AU 11054 PDX - ROW 8 EVAC LIGHT INOP. BATTERY PAC WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105005631996010500563NM 1996 1 5 QXEA9500462 119951231A33506104781 POWER SUPPLY DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09828PH 287 SEA - SEVERAL EMERGENCY LIGHTS ARE DIM. POWER SUPPLY PS 4 REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19960105005641996010500564NM 1996 1 5 QXEA9500463 119951231A3260870003 PSEU DORNERDO32 DO328100 2996000NM RADIO RACK MALFUNCTIONING A QXEAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NM09336PH868 3014 PDX - EN ROUTE TO RDM, RECEIVED NUMEROUS HYD PROXI FAIL CAS MESSAGES, GEAR WAS SELECTED DOWN ON APPROACH TO RDM, GEAR DIDN'T MOVE. CREW COULDN'T MOVE HANDLE TO UP POSITION. LANDING GEAR CYCLED SEVERAL TIMES WITH THE HANDLE STILL DOWN. CREW CYCLED GEAR AND RECEIVED THREE GREEN. AIRCRAFT RETURNED TO PDX AND LANDED WITHOUT FURTHER INCIDENT. 2H72 4T RTA45NM 19960105005661996010500566EU 1996 1 5 QXEA9600002 119950101A33501820 BULB FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 BOI - RIGHTHAND OVERWING EXIT LIGHT INOP. BULB WAS REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960105005681996010500568SW 1996 1 5 QXEA9600005 119950101A3230246006 VALVE SWRNGNSA227 SA227AC 8780603SW HYD POWER PACK INOPERATIVE A QXEAO OTHER J WARNING INDICATION APAPPROACH 1 NM0926959 AC662 PDX - LANDING GEAR WOULDN'T EXTEND USING NORMAL SYSTEM, ALTERNATE GEAR EXTENSION PERFORMED AND GEAR EXTENDED. LANDING GEAR VALVE ON HYDRAULIC POWER PACK REPLACED IAW MAINT MANUAL. GEAR OPS CHECKED GOOD ON GEAR SWING AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19960105005701996010500570EU 1996 1 5 WWMA9500091 119951230A5720137835C5152 CHANNELS BAG JETSTMJETSTM3201 1500217EU WS 257.8 CRACKED A WWMAK NONE O OTHER ININSP/MAINT 1 WP15949AE7092 949 WHILE PERFORMING AN 8,000 HOUR HEAVY INSPECTION, MAINTENANCE FOUND IDENTICAL 4 INCH CRACKS IN THE LEFT AND RIGHT SIDE STUB WING STIFFENER CHANNELS AT STATION 257.8 ALONG THE LOWER CHANNELS INBOARD OF THE JACKING POINTS. REPLACED CHANNELS IAW MM 20-10-00 AND SRM 51-30-91. 2L72 4T RTA56EU 19960105006021996010500602 1996 1 5 96ZZZX92 419950614A25620025004 BATTERY MARTECH EB2BCD PIPER PA12 PA12 7101202SO ELT CRACKED A RKWAK NONE O OTHER ININSP/MAINT 1 NM113168M 121847 ELT BATTERY ARTEX WAS FOUND CRACKED ON LOWER SIDE UPON DISASSEMBLY OF ELT. BATTERY EXPIRATION DATE IS JANUARY '96. ELT EXHIBITED CORROSION DAMAGE TO LOWER CIRCUIT BOARD AND WAS INOPERATIVE. 1H71 3O A780 19960105006031996010500603CE 1996 1 5 96ZZZX93 119951215A7810991029915 EXHAUST CESSNA340 340CESSNA 2076404CE AFT ELBOW HOLED A SQPAK NONE O OTHER ININSP/MAINT 1 NM11592GC2500 3400152 FOUND SMALL HOLE IN CENTER OF THE LT EXHAUST AFT ELBOW WHILE C/W AD 75-23-08R5, EFFECTIVE DATE 11-4-86. THIS PART HAS BEEN INSTALLED ON THIS C-340 L.A.W. RAM STC SA234SW. SAID PART IS LISTED IN TABLE III OF AD 75-23-08R5 AS AN EXEMPT COMPONENT PER PART I(A). SUBMITTER RECOMMENDATION WOULD BE TO EXCLUDE THIS PART FROM THE EXEMPT LIST. 1L72 3O 3A25 19960105006041996010500604CE 1996 1 5 96ZZZX94 119951201A2752C3010020108 MOTOR CESSNA207 207A 2073604CE FLAP ACTUATOR MALFUNCTION A BAJAO OTHER F FLT CONT AFFECTED APAPPROACH 1 AL016908M 2070672 WHEN THE PILOT SELECTS FLAPS DOWN FROM 20 DEGREES TO 30 DEGREES ABOVE 90 KNOTS I.A.S., THE FLAP CIRCUIT BREAKER WOULD OPEN. AT AIRSPEEDS BELOW 90 KNOTS WHEN FLAPS WERE AGAIN SELECTED DOWN FROM 20 DEGREES - 30 DEGREES, THE FLAPS WOULD FUNCTION NORMALLY. NO VISUAL DEFECTS WERE FOUND IN THE CIRCUIT WIRING OR COMPONENTS. THE FLAP ACTUATOR MOTOR WAS REPLACED WITH A NEW UNIT AND AIRCRAFT WAS TEST FLOWN SATISFACTORILY. 1H71 3O A16CE 19960105006151996010500615GL 1996 1 5 96ZZZX109 219951117A7323355A5747221 SPRING AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL NR 2 ENG GOV BROKEN A ALGAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW03372AL 5208 DURING CRUISE FLIGHT, NR 2 ENGINE DROPPED TO FLIGHT IDLE. GOVERNOR SPRING ON NR 2 ENGINE WAS FOUND BROKEN. 1G72 3U3 U H11EU E4CE 19960105006181996010500618WP 1996 1 5 96ZZZX112 119950930A2720 COMPUTER LKHEED1011 10113851 5265010WP RUDDER CONTROL MALFUNCTIONED A AMTAK NONE J WARNING INDICATION DEDESCENT 1 GL11183AT 193A1153 DURING DESCENT WITH FLAP EXTENSION, RUDDER HYDRAULIC PRESSURE LIGHT CAME 'ON' ALONG WITH RUDDER HYDRAULIC LIMITER LIGHT. AIRSPEED WAS APPROXIMATELY 165,000 TO 170,000, AND 290 KNOTS ON A PREVIOUS FLIGHT. LRS COMPUTER WAS RESET AND SYSTEM OPS CHECKED NORMAL. 2L73 4F A23WE 19960105006191996010500619NE 1996 1 5 96ZZZX113 219950914A7230 COMPRESSOR BOEING727 727290 138408WNM PWA JT8 JT8D17 52049NE NR 1 DAMAGED A AMTAO OTHER C F.O.D. LDLANDING 1 GL11775AT 21511 65A637 NR 1 ENGINE HAS C-1 AND C-2 DAMAGE. T7 LEADING EDGE DAMAGE. REMOVED AND REPLACED NR 1 ENGINE. LEAK AND OPS CHECKS GOOD. 2L73 4F4 F A3WE E2EA 19960105006201996010500620CE 1996 1 5 96ZZZX114 119951004A523010151418313 GAS SHOCK BEECH 1900 1900D 1154162CE CARGO DOOR BENT A AMWAK NONE O OTHER ININSP/MAINT 1 CE07171ZV15 UE171 WHEN CLOSING THE CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED GAS SHOCK. 2L72 4T RTA24CE 19960105006211996010500621CE 1996 1 5 96ZZZX115 119951002A523010151418313 GAS SHOCK BEECH 1900 1900D 1154162CE CARGO DOOR BENT A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV149 UE163 WHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK. 2L72 4T RTA24CE 19960105006221996010500622CE 1996 1 5 96ZZZX116 119950911A523010151418313 GAS SHOCK BEECH 1900 1900D 1154162CE CARGO DOOR BENT A AMWAK NONE O OTHER ININSP/MAINT 1 CE07163YV147 UE163 WHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK. 2L72 4T RTA24CE 19960105006231996010500623EA 1996 1 5 96ZZZX117 219951110A72303017701 COMPRESSOR BLADE STBROSSD3 SD330 8100602EU PWA PT6 PT6A45R 52043EA RT ENGINE BENT A DATAE ENGINE SHUTDOWN RC PARTIAL RPM/PWR LOSS F.O.D. APAPPROACH 1 GL13937MA SH3040 PCE84172 CWA/MKE - EN ROUTE, PILOTS HEARD A LOUD NOISE THEN A HIGH PITCH NOISE FROM RT ENGINE. PILOT REDUCED POWER SETTING AND NOISE WENT AWAY. ON APPROACH INTO MKE, PILOT CONFIGURED AIRCRAFT FOR LANDING. THE RT ENGINE BEGAN TO HAVE TORQUE FLUCTUATION, LOUD NOISE AND FLAMES COMING FROM RT ENGINE. ENGINE WAS SHUT DOWN, AND AIRCRAFT LANDED AT MKE WITOUT INCIDENT. MAINTENANCE INSPECTED ENGINE AND FOUND ONE 1ST STAGE COMPRESSOR BLADE BENT AT 90 DEGREES. ENGINE REMOVED FOR REPAIRS OF FOD. PART CYCLES, 6,929. 2H72 4T4 T A41EU E4EA 19960105006241996010500624WP 1996 1 5 96ZZZX118 119951107A335058531 CONTROL CABLE DOUG DC9 DC982 3022082WP ROW 15-19 FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05955U 49427 STL - FLT 202 - A CHECK OF THE EGRESS LIGHTS REVEALED ROW 15 TO ROW 19 INOPERATIVE. REMOVED AND REPLACED FEEDER LINE FLEX CABLE, MFG PN 5853-1. OPERATIONAL CHECK OF THE EGRESS LIGHT SYSTEM WAS NORMAL. CHECK C-2D - 10-17-95 - MCI. 2L72 4F A6WE 19960105006251996010500625SW 1996 1 5 96ZZZX119 119951001A792031039081 TUBE FRCHLDSA227 SA227DC 3377521SW RT ENGINE CRACKED A EQGAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW19847LS4093 DC847B DFW/ROW - WHILE EN ROUTE, RT ENGINE LOST ALL OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO ABI AND LANDED WITHOUT FURTHER INCIDENT. ON INSPECTION OF THE ENGINE, AN OIL PRESSURE LINE WAS FOUND CRACKED. THIS LINE WAS A POST-DATED SB 77-0050, WHICH WAS MADE TO STOP THIS SAME PROBLEM. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1L72 4T RTA18SW 19960105006261996010500626NM 1996 1 5 96ZZZX120 119950913A5610SPSDO328131 WINDSHIELD DORNERDO32 DO328100 2996000NM RT COCKPIT SHATTERED A EQGAA UNSCHED LANDING O OTHER CRCRUISE 1 SW19335LS757 142 3035 DFW/DRT - WHILE EN ROUTE, THE FIRST OFFICER'S WINDSHIELD OUTER LAYER FAILED. THE AIRCRAFT LANDED IN DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO HOT-MAINTENANCE FOR REPLACEMENT OF THE FIRST OFFICER'S WINDSHIELD. DORNIER WAS NOTIFIED THIS WAS THE SECOND WINDSHIELD REPLACEMENT IN A ONE-MONTH PERIOD. 2H72 4T RTA45NM 19960105006301996010500630NM 1996 1 5 AALA950319 119950223A76034111116 CONTROL BOX TELEFLEX BOEING757 757223 1384957NM LT THROTTLE DEFECTIVE A AALAE ENGINE SHUTDOWN O OTHER CRCRUISE 1 SW07661AA 0721 25295 RDU - FLT 0879 - EN ROUTE ORD/RDU DURING CRUISE, LT ENGINE POWER LEVER FROZE AND UNABLE TO REDUCE POWER FOR DESCENT/LANDING. ACCOMPLISHED LT ENGINE SHUT DOWN AND AIRCRAFT LANDED RDU WITHOUT INCIDENT. REPLACED LT ENGINE THROTTLE LOWER CONTROL BOX AND LOWER CABLE ASSSEMBLY. ACCOMPLISHED GROUND ENGINE RUN TO TAKEOFF POWER WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19960105006311996010500631NE 1996 1 5 AALA950971 219950527A7530N14FF104 TRANSDUCER BOEING757 757223 1384957NM RROYCERB211 RB211535E4 54555NE NR 1 ENGINE DEFECTIVE A AALAE ENGINE SHUTDOWN XB ENGINE FLAMEOUT SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW07633AA 1150 24591 DFW - FLT 1366 - DESCENT THROUGH 26,000 FEET, A FUEL SMELL WAS NOTICED IN COCKPIT AND CABIN. ON LEVEL OFF AT 24,000 FEET, NR 1 ENGINE APPEARED TO HAVE FLAMED OUT. DID ENGINE SHUT DOWN PROCEDURE FOLLOWED BY IN-FLIGHT RE-START PER QRH PROCEDURES. ENGINE OPERATED NORMALLY FOR REST OF FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED THROTTLE ANGLE TRANSDUCER. REMOVED AND REPLACED BLEED VALVE CONTROL UNIT. ALL TESTS COMPLETED SATISFACTORILY. ENGINE RUN ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F4 FRTA2NM E12EU 19960105006321996010500632NM 1996 1 5 NOCA0895 119951124A33507715AS15 FUSE BOEING757 75728A 1384976NM SEAT 34&47ABC FAILED A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15750NA 26277 EMERGENCY EGRESS LIGHTS INOP BY SEATS 34ABC AND 47ABC. REPLACED FUSE ON AFT RT EMERGENCY BATTERY PACK. OPS CHECK OK. (X) 2L72 4F RTA2NM 19960105006331996010500633NM 1996 1 5 USAABB95008 119951125A33508731002511 LIGHT BOEING757 7572B7 1384964NM L4 DOOR INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19632AU 27810 SFO - UPON TEST, THE L4 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (X) 2L72 4F RTA2NM 19960110000021996011000002NM 1996 1 10 UPS405150 119951209A33503004543 CONNECTOR BOEING747 747123 1384873NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 FORWARD (LEFT SIDE) EMERGENCY EXIT LIGHT ON CREW SERVICE DOOR INOP. REPLACED CANNON PLUG ON DX 327. REPLACED X325. LIGHTS OPERATE, BUT NOT NORMALLY. CONTINUE ON DMI. PN ON 30-0454-3, P/N OFF 30-0454-3. S/N ON UPS 0470, S/N OFF UP10954. 2L74 4F A20WE 19960110000031996011000003NM 1996 1 10 UPS405149 119951216A335037067001 BATTERY BOEING747 747123 1384873NM CABIN DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01671UP 20323 MAINTENANCE REPORTED, 3 EMERGENCY EXIT LIGHTS OUT IN MAIN DECK, 1 IN L1 ENTRY DOOR AND 2 ON CEILING. ITEM DEFFERED. 2L74 4F A20WE 19960110000041996011000004NM 1996 1 10 95ZZZX6788 119951022A2820 FUELING VALVE BOEING757 75723N 1384973NM LT FUEL TANK MALFUNCTIONED A AMTAK NONE O OTHER CRCRUISE 1 GL11515AT 27598 MDW - FUEL MIGRATION FROM LEFT TANK TO CENTER TANK IN-FLIGHT AND ON GROUND. APPROXIMATELY 2,500 POUNDS OVER 3 HOUR TIME PERIOD. SWAPPED CENTER TANK FUELING VALVE WITH LEFT TANK FUELING VALVE, NO FURTHER MIGRATION NOTED. S/N POSITIONS NOW, CENTER 1041---LH 1051. 2L72 4F RTA2NM 19960110000051996011000005NE 1996 1 10 95ZZZX6796 219951011A7310AC9227F1740 FUEL FILTER BOEING767 767216 1385124NM GE CF6 CF680A 30025NE ENGINE NR 1 CLOGGED A TACACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03762TA 23623 580300 SAL/LAX - FLT 510 - DURING TAKEOFF, ENGINE NR 1 DID NOT REACH N1 REQUIRED FOR TAKEOFF AT THE RUNWAY HEADING. DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO GATE. THE NR 1 ENGINE WAS INSPECTED, AND FOUND WITH A CLOGGED FUEL FILTER WHICH WAS REPLACED. AFTER TESTING, TAKEOFF POWER OK, THE AIRCRAFT RETURNED TO NORMAL OPERATION. 2L72 2F4 FRTA1NM E13NE 19960110000061996011000006NM 1996 1 10 95ZZZX6797 119951015A7830315T30562 TR ISOLATION VLV BOEING767 767216 1385124NM RT ENGINE DIRTY A TACAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03762TA 23623 SAL/LAX - FLT 510 - DURING CLIMB, THE ADVISORY MESSAGE R REV ISOLATION VALVE WAS SHOWN ON THE EICAS. DUE TO THIS SITUATION, THE AIRCRAFT RETURNED TO SAL. AFTER CHECKING RT ENGINE THRUST REVERSER VALVE AND CLEANING THE ISOLATION VALVE PRESSURE, AND CHECKING THE PROXIMITY SENSORS PER MM 78-34-00, PERFORMED AN OPERATIONAL CHECK TESTING, OK. AFTER THIS, THE AIRPLANE RETURNED TO NORMAL OPERATION. 2L72 2F RTA1NM 19960110000071996011000007EU 1996 1 10 JBXA9500002 119951103A291342046 HYDRAULIC PUMP FOKKERF28 F28MK0100 4990807EU NR 2 ENGINE LEAKING A JBXAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL31106ML 11477 ABE/RDU - FLT 670 - LOW HYDRAULIC QUANTITY SYSTEM 1 DURING FLIGHT. UPON INSPECTION IN RDU FOUND O-RING ON NR 1 SYSTEM RT ENGINE HYDRAULIC PUMP CUT. REPLACED O-RING AND GROUND RAN NR 2 ENGINE, NO LEAKS NOTED. ALL WORK ACCOMPLISHED IAW 29-11-01 FOKKER MM. (X) 2L72 4F RT 19960110000081996011000008NE 1996 1 10 95ZZZM738 319951122A6112 DE-ICE BOOTS DORNERDO32 DO328100 2996000NM HARTZLHDE6C HDE6C3B NE LT PROP DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07430JS 3044 HL125 FLT NR 4168 - AFTER TAKEOFF FLT CREW NOTICED LEFT PROPELLER HEAT HAD FAILED. CREW ELECTED TO RETURN TO FIELD. AIRCRFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT DISCOVERED DE-ICE BOOTS ON BLADES NR 2 AND NR 4 WERE DEFECTIVE. PIT MAINTENANCE REMOVED AND REPLACED LEFT PROPELLER IAW MM 61-00-00, GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA45NM 6 CP34NE 19960111000011996011100001EU 1996 1 11 96ZZZM3 119951014A75406411343 TEMP SWITCH AEROSPATR42 ATR42300 8680920EU PWA 120 PW120 NE RT WING FAILED A RAIAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE032FOR 9097 176 STL - FLT NR 7162 - THE RIGHT BLEED FAULTED. MAINTENANCE REMOVED AND REPLACED TEMP SWITCH, PERFORMED GROUND RUN, OPS CHECK GOOD. (M) 2H72 4T4 TRTA53EU E20NE 19960112000181996011200018SO 1996 1 12 COMA9610003 119950104A325012037995001 TILLER ASSY EMB 120 EMB120RT SO NLG STEERING DEFECTIVE A COMAO OTHER O OTHER TXTAXI/GRND HDL 1 SO01258CA 120247 NOSE WHEEL STEERING FAILS DURING LEFT TURNS. REPLACED THE STEERING TILLER ASSY. 2L72 4T RTA31SO 19960112000221996011200022NM 1996 1 12 SWAA950795 119951223A3520 OXYGEN MASKS BOEING737 7373H4 1384600NM CABIN DEPLOYED A SWAAGA O2 MASK DEPLOYED UNSCHED LANDING O OTHER CLCLIMB 1 SW07347SW 24374 CABIN O2 MASKS DEPLOYED DURING CLIMBOUT. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING. REPACKED MASKS, REPLACED O2 GENERATORS, AND PRESSURIZATION CHECKED AIRCRAFT PER BOEING M/M. 2L72 4F RTA16WE 19960112000231996011200023NM 1996 1 12 SWAA950796 119951228A5320 STRAP BOEING737 7373H4 1384600NM E/E BAY CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07304SW 22944 DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST O/B AND ABOVE BATTERY. REPAIRED PER BOEING SRM. 2L72 4F RTA16WE 19960112000241996011200024NM 1996 1 12 SWAA950797 119951219A7930 BYPASS SWITCH BOEING737 7372T4 1384492NM NR 1 ENGINE MALFUNCTIONED A SWAAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 SW07105SW 23249 DURING DESCENT, NUMBER 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECKLIST. AIRCRAFT MADE AN UNEVENTFUL LANDING AT DAL. INSPECTED, NO CONTAMINATION NOTED. REPLACED BYPASS SWITCH, LEAK CHECKED AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. 2L72 4F A16WE 19960112000281996011200028SW 1996 1 12 96ZZZX121 119951019A77122719158007 INDICATOR SWRNGNSA227 SA227AC 8780603SW COCKPIT TORQUE INOPERATIVE A PNSACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 AL03670PA 4974 AC613B TORQUE INDICATION WENT TO ZERO. ABORTED TAKEOFF. 1L72 4T A8SW 19960112000291996011200029CE 1996 1 12 96ZZZX122 119951018A3500IN4006 DIODE CESSNA441 441 2076020CE OXYGEN MASK DEFECTIVE A PNSAG O2 MASK DEPLOYED O OTHER ININSP/MAINT 1 AL03544AL 4410120 OXYGEN MASKS DEPLOYED DURING PRE-FLIGHT, REPLACED DIODE. 1L72 3T RTA28CE 19960112000301996011200030CE 1996 1 12 96ZZZX123 119950927A2150 SEAL CESSNA441 441 2076020CE ACM LEAKING A PNSAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 AL03544AL 5913 4410120 AIR CYCLE MACHINE'S (PN 73844315) OIL SEAL FAILED DURING TAKEOFF CAUSING SMOKE IN COCKPIT. 1L72 3T RTA28CE 19960112000311996011200031SO 1996 1 12 96ZZZX124 119951011A2435MHB4018R STARTER PIPER PA31 PA31350 7103110SO RT ENGINE INOPERATIVE A PNSAK NONE H ELECT. POWER LOSS-50 PC ININSP/MAINT 1 AL033588Z 318052130 RIGHT STARTER INOPERATIVE AT ENGINE START. NO ROTATION. 1L72 3O A20SO 19960112000321996011200032SW 1996 1 12 96ZZZX125 119950913A56102621126005 WINDSHIELD SWRNGNSA227 SA227AC 8780603SW LT COCKPIT SHATTERED A PNSAB EMER. DESCENT O OTHER CRCRUISE 1 AL03630PA 5756 AC463 CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. DEPRESSURIZED, DESCENDED TO LOWER ALTITUDE. 1L72 4T A8SW 19960112000331996011200033NM 1996 1 12 96ZZZX126 119951115A77123037603 SENSOR 3037743 DORNERDO32 DO328100 2996000NM LT ENGINE FAILED A EQGAO OTHER N FALSE WARNING DEDESCENT 1 SW19340LS251 NR00673 3040 DTW - AIRCRAFT WAS ON DESCENT TO LAND AT DTW WHEN ECU FAIL MESSAGE APPEARED. THE PILOT RESET THE ECU AND IT STAYED ON LINE FOR APPROXIMATELY 4 MINUTES, THEN FAILED AGAIN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED TO HOT FOR MAINTENANCE. INSPECTION REVEALED THE T18 SENSOR HAD CARBON TRACKING ALONG SENSOR WHICH SENT A BOGUS READING TO THE EEC CAUSING THE FAILURE. THE T18 SENSOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960112000341996011200034NM 1996 1 12 96ZZZX127 119951102A7712 TQ CONNECTORS DORNERDO32 DO328100 2996000NM LT ENGINE DIRTY A VNAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL07433JS 3047 FLT 1002 - CREW ELECTED TO RETURN TO FIELD AFTER EXPERIENCING TORQUE FLUX, LT ENGINE. SHUT DOWN LT ENGINE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED CONNECTORS ON NP AND TQ SENSORS IAW STANDARD MAINTENANCE PRACTICES. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960112000351996011200035CE 1996 1 12 96ZZZX128 119951114A561010138402515 WINDSHIELD BEECH 1900 1900D 1154162CE LT COCKPIT CRACKED A AMWAO OTHER O OTHER TXTAXI/GRND HDL 1 CE07178YV74 UE178 CAPTAIN'S WINDSHIELD CRACKED ALONG THE OUTBOARD EDGE OF WINDSHIELD APPROXIMATELY 14 INCHES LONG. REMOVED AND REPLACED WINDSHIELD. AIRCRAFT HAD 74 FLIGHT HOURS AND 119 CYCLES SINCE NEW FROM BEECHCRAFT. 2L72 4T RTA24CE 19960112000361996011200036WP 1996 1 12 96ZZZX129 119951030A792186745 OIL COOLER CVAC 240 240* 2422601WP NR 2 ENGINE LEAKING A TFAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SO1587949 491935 PSE/SJU - FLT 7026 - EN ROUTE, SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE AND QUANTITY. FOUND THE OIL COOLER LEAKING. REPLACED OIL COOLER. 2L72 4R A793 19960112000371996011200037CE 1996 1 12 96ZZZX130 119951031A32601EN516 GEAR SWITCH BEECH 1900 1900C 1154161CE NLG OUT OF ADJUST A GUUAO OTHER N FALSE WARNING APAPPROACH 1 SO19195GA UB65 MIA/MCO - FLT 427 - PILOT REPORT: NOSE GEAR UNSAFE INDICATION WHILE AIRBORNE, SAFE INDICATION ON GROUND. MAINTENANCE: HAD AIRCRAFT FERRIED TO MIA, GEAR DOWN AND LOCKED, TROUBLESHOT AND ADJUSTED NOSE GEAR DOWNLOCK SWITCH. AIRCRAFT RELEASED. 2L72 4T RTA24CE 19960112000401996011200040NE 1996 1 12 96ZZZX133 219951212A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE LEFT FAILED A GUUAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 SO19826BE8794 2318 SH3745 PCE10671 MIA/MIA - FLT 204 (TRAINING) - PILOT REPORT: ON SIMULATED MISSED APPROACH (TRAINING) HEARD A LOUD BANG FROM LEFT ENGINE. ENGINE SHUT DOWN BY ITSELF, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE: LEFT ENGINE CHANGE IN PROGRESS FOR EVALUATION BY MANUFACTURER. 2H72 4T4 T A41EU E26NE 19960112000411996011200041CE 1996 1 12 96ZZZX134 119951130A3260404EN16 DOWNLOCK SW BEECH 1900 1900C 1154161CE LT MLG FAILED A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19196GA UB31 NAS/MIA - FLT 488 - PILOT REPORT: LANDING GEAR DOWN, RED HANDLE LIGHTS, LT MAIN 'GREEN' NOT LIT. CYCLED GEAR AND GOT PROPER INDICATIONS UNTIL PUT FLAPS TO LANDING POSITION, THEN RED LIGHTS IN HANDLE ILLUMINATED AND LT MAIN GREEN LIGHT EXTINGUISHED AN AURAL WARNING. MAINTENANCE: REMOVED AND REPLACED LT MAIN GEAR DOWN POSITION SWITCH, SWUNG GEAR. OPS CHECKS ALL GOOD. 2L72 4T RTA24CE 19960112000421996011200042CE 1996 1 12 96ZZZX135 119951129A2612302158 FIRE DETECTOR BEECH 99 C99 1154006CE RT ENGINE DIRTY A GUUAO OTHER N FALSE WARNING NRNOT REPORTED 1 SO19216EE U206 NAS/FLL - FLT 424 - PILOT REPORT: RT FIRE WARNING LIGHT IN-FLIGHT. MAINTENANCE: CLEANED DETECTORS, SYSTEM OPS CHECK NORMAL AT THIS TIME. 1L72 3T A14CE 19960112000431996011200043WP 1996 1 12 96ZZZX136 119951121A33501102833 LIGHT CVAC 440 440 2422902WP FORWARD GALLEY INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP0773157 312 DURING SCHEDULED CHECK, THE FORWARD ENTRYWAY/GALLEY INTERNAL EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT BASE WAS REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY. 2L72 4R 6A6 19960112000441996011200044WP 1996 1 12 96ZZZX137 119951121A33501102833 LIGHT CVAC 440 440 2422902WP FORWARD GALLEY INOPERATIVE A SPAAK NONE L NO TEST ININSP/MAINT 1 WP0773157 312 DURING SCHEDULED CHECK, THE FORWARD ENTRYWAY/GALLEY INTERNAL EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT BASE WAS REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY. 2L72 4R 6A6 19960112000451996011200045NM 1996 1 12 96ZZZX138 119951120A3350900835A BATTERY PACK BOEING737 7372T4 1384492NM CABIN DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP07703S 22529 DURING SCHEDULED CHECK, THE FORWARD BULLNOSE INTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED SYSTEM BATTERY PACK WAS REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY. 2L72 4F A16WE 19960112000461996011200046NM 1996 1 12 AALA951864 119951026A3350A3060819104 EEL STRIP DOUG MD11 MD11 3023602NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071766A 48597 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS AT FORWARD LT AISLE OF BUSINESS CLASS CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP AT FORWARD LT AISLE OF BUSINESS CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F RTA22WE 19960112000471996011200047EU 1996 1 12 AALA951873 119951030A3260200392605 DOOR BUFFER ROTOL FOKKERF28 F28MK0100 4990807EU LT MLG DEFECTIVE A AALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW071428D 11413 DFW - FLT 1021 - AFTER TAKEOFF DFW WHEN LANDING GEAR RETRACTED, LT MLG UNSAFE MESSAGE ON MFDU. RECYCLED LANDING GEAR WITH SAME RESULTS. EXTENDED LANDING GEAR AND ALL INDICATIONS RETURNED TO NORMAL. AIRCRAFT RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED LT MLG DOOR UP-STOP BUFFER. ACCOMPLISHED LANDING GEAR REETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RT 19960112000481996011200048WP 1996 1 12 AALA951905 119951107A3350A3060719102 STRIP DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07417AA 49328 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BY FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F A6WE 19960112000491996011200049NM 1996 1 12 AALA951908 119951006A5315141N5112 FLOOR BEAM BOEING757 757223 1384957NM BS 365 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07637AM15651 24595 AFW - FLOOR BEAM AT STA 365 FROM RBL 6 TO RBL 18 HAS CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-646. CYCLES, 5,937. (X) 2L72 4F RTA2NM 19960112000501996011200050NM 1996 1 12 AALA951909 119951006A2750113N2363 SUPPORT BOEING757 757223 1384957NM T/E FLAPS GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07637AM15651 24595 AFW - BEAM-BELL CRANK SUPPORT-INBOARD MAIN FLAP RT WING HAS GOUGE BLENDED. PARENT MATERIAL 0.130 INCH, MINIMUM MATERIAL 0.117 INCH. PER MRB 757-647. CYCLES, 5,937. (X) 2L72 4F RTA2NM 19960112000511996011200051NM 1996 1 12 AALA951910 119951006A521014AN6302 HANDLE PAN BOEING757 757223 1384957NM L-1 DOOR GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07637AM15651 24595 AFW - L-2 DOOR HANDLE PAN HAS SMALL GOUGE. AFTER BLENDING, IS BEYOND LIMITS. PER MRB 757-648. CYCLES, 5,937. (X) 2L72 4F RTA2NM 19960112000521996011200052NM 1996 1 12 AALA951911 119951006A5321146N5300 DECK PLATE BOEING757 757223 1384957NM BS 1681/1720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07637AM15651 24595 AFW - DECK PLATE HAS CORROSION BLENDED BEYOND SRM LIMITS. CYCLES, 5,937. (X) 2L72 4F RTA2NM 19960112000531996011200053NM 1996 1 12 AALA951912 119951006A5315146N5090 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07637AM15651 24595 AFW - TWO AREAS OF CORROSION REMOVED ON FLOOR BEAM STA 1640, LBL 2 AND RBL 57 BEYOND SRM LIMITS. CYCLES, 5,937. (X) 2L72 4F RTA2NM 19960112000541996011200054WP 1996 1 12 AALA951937 119951111A3350P6010006 BATTERY CHGR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07557AN 53087 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT SIGN LIGHTS ON LT AND RT AFT OVERWING EXITS INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F A6WE 19960112000551996011200055SW 1996 1 12 BDHA9500027 119951121A324221203 BRAKE SWRNGNSA226 SA226TC 8780404SW LT MLG INBOARD LEAKING A BDHAK NONE K FLUID LOSS ININSP/MAINT 1 GL15327BA 476 3846 TC249 RAP - FLT 475 - UPON POST-FLIGHT INSPECTION OF AIRCRAFT, PILOT NOTICED FLUID LEAKING FROM THE LT BRAKE ASSEMBLIES AND THE LT INBOARD TIRE WAS FLAT. MAINTENANCE REPLACED BOTH BRAKE ASSEMBLIES AND THE INBOARD WHEEL ASSEMBLY AND THE AIRCRAFT BRAKING SYSTEM WAS OPS CHECKED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 1L72 4T A8SW 19960112000561996011200056NM 1996 1 12 CAL951032 119951111A2612106109648 FIRE LOOP BOEING737 7373T0 1384582NM NR 1 ENGINE INOPERATIVE A CALAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 SW0914346 23584 CUN - FLT 0642 - NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT OF CUN. THE NR 1 ENGINE WAS SHUT DOWN AND LT FIRE BOTTLE DISCHARGED, BUT LIGHT DID NOT EXTINGUISH. ACFT RETURNED TO CUN AND LIGHT EXTINGUISHED JUST BEFORE LANDING. MAINTENANCE FOUND NO EVIDENCE OF FIRE. NR 1 ENGINE 'B' LOOP FOUND AT FAULT. ENGINE CORE FIRE DETECTION LOOP REPLACED AND CONNECTOR FOR 'B' LOOP REPLACED. IN ADDITION, LOWER FAN 'A' LOOP CONNECTOR REPLACED. FIRE DETECTION SYSTEM CHECKED GOOD PER MM 26-21-31, PAGE 201. LT ENGINE FIRE BOTTLE REPLACED. (X) 2L72 4F RTA16WE 19960112000571996011200057NM 1996 1 12 CAL951045 119951113A5330 SKIN BOEING737 737291 138448WNM BS 440 DENTED A CALAK NONE O OTHER ININSP/MAINT 1 SW091525554098 21069 IND - INSPECTION FOUND A DENT IN FORWARD LOWER FUSELAGE SKIN AT STA 440, RBL 4. THE DENT MEASURED 0.325 INCH WIDE BY 2.5 INCHES LONG BY 0.102 INCH DEEP. THE SKIN WAS REPAIRED IAW SRM 53-30-3. (X) 2L72 4F A16WE 19960112000581996011200058WP 1996 1 12 CAL951060 119951118A5530 ANGLE DOUG DC9 DC932 3022066WP VERT STAB CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091652171502 47521 IAH - INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LT SIDE. A REPAIR WAS PERFORMED IAW SRM 53-05, FIGURE 23A. (X) 2L72 4F A6WE 19960112000591996011200059NM 1996 1 12 CAL951129 119951110A5311 FRAME BOEING737 737130 1384435NM BS 440 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093320266090 19019 GSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT STA 440. THE FRAME WAS REMOVED AND REPLACED IAW SRM 53-10-04 AND SRM 51-30-0. (X) 2L72 4F A16WE 19960112000601996011200060NM 1996 1 12 CAL951130 119951122A5713 STRINGER BOEING737 737130 1384435NM RT WING CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093320266090 19019 GSO - INSPECTION FOUND A 2 INCH CRACK IN RT WING STR 13 AT WBL 92.5 AND A 1.5 INCH CRACK IN SAME STRINGER AT WBL 114. THE STRINGER WAS REPAIRED IAW BOEING DWG 65C34533. (X) 2L72 4F A16WE 19960112000611996011200061NM 1996 1 12 CAL951131 119951117A5320 CHORD BOEING737 737130 1384435NM BS 727 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093320266090 19019 GSO - INSPECTION FOUND STA 727 RT CHORD CRACKED AT STR 18A. THE CRACK WAS LOCATED AT BOTH FORWARD AND AFT FASTENERS AND TOTALED 1 INCH IN LENGTH. THE CRACKED CHORD SEGMENT WAS REMOVED AND REPLACED IAW EA 5310-01638 AND BOEING DWG 65C33722. (X) 2L72 4F A16WE 19960112000621996011200062WP 1996 1 12 CAL951140 119951207A5320 FLOOR WEB DOUG DC9 DC932 3022066WP BS 83.55/89.05 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091452464475 47539 IAH - INSPECTION FOUND A 1 INCH CRACK IN COCKPIT FLOOR WEB AT BS 89.050 AND A 2 INCH CRACK FOUND AT BS 83.550. THE FLOOR WEB WAS REPAIRED IAW ECRA 5310-03193 AND ECRA 531003031. (X) 2L72 4F A6WE 19960112000631996011200063NM 1996 1 12 EISA95366 119950825A5753652466628 BRACKET BOEING727 72782 1384029NM NR 2 FOREFLAP CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07357NE 19405 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING INBOARD FLAP MID-FLAP NR 2 FOREFLAP TRACK BRACKET (OUTBOARD BRACKET) HAS 1.50 INCH CRACK IN TOP FLANGE. REMOVED OLD FITTING, DRILLED, DEBURRED AND TREATED NEW FITTING AND INSTALLED IAW B727 SRM 51-10-1 AND SRM 51-10-2 AND SRM 57-2-7. NR 060N1-1235. (X) 2L73 4F A3WE 19960112000641996011200064CE 1996 1 12 HERA9525 119951031A780012502505 MUFFLER CESSNA207 207A 2073604CE ENGINE BURNED OUT A HERAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 AL0373733 20700618 ABL - FLT 1521 - ON TAKEOFF, THE ENGINE BEGAN LOOSING POWER AND DEVELOPED A NOTICEABLE VIBRATION. THE CYLINDER HEAD TEMPERATURE AND EXHAUST GAS TEMPERATURE BEGAN TO CLIMB SO THE PILOT REDUCED POWER AND RETURNED TO THE AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND THE RT FLAME CONE IN THE EXHAUST MUFFLER HAD COME LOOSE AND WAS BLOCKING THE EXHAUST OUTLET. THE MUFFLER WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1H71 3O A16CE 19960112000651996011200065CE 1996 1 12 HERA9526 119951107A3397 WIRE CESSNA207 207A 2073604CE COCKPIT SHORTED A HERAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 AL031809Q 20700787 BET - FLT 1202 - INBOUND TO BET, SMELL OF SMOKE IN COCKPIT COMING FROM UNDER THE INSTRUMENT PANEL. THE AIRCRAFT LANDED AT BET WITHOUT INCIDENT. MAINTENANCE FOUND SHORTED AND BURNED STROBE LIGHT WIRES BETWEEN THE CIRCUIT BREAKER AND ON/OFF SWITCH. THE STROBE LIGHT SYSTEM WAS DEACTIVATED AND COMPONENTS REMOVED. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1H71 3O A16CE 19960112000661996011200066NM 1996 1 12 IXKA950035 119951216A2150 PACK BOEING727 727251 138408HNM LT/RT MALFUNCTIONED A IXKACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 EA25264US 19983 FLT 72 - AT 1.5 EPR, TAKEOFF ROLL AUTO PRESSURE GREEN LIGHT ILLUMINATED. APPROXIMATELY SEVERAL SECONDS LATER, BOTH PACKS TRIPPED OFF, TEMPS AND PRESSURE NORMAL. DID NOT RETARD THROTTLES UNTIL ABORT WAS INITATED. RAN AIRCRAFT AT HIGH POWER, SYSTEM CHECKS NORMAL IAW MM 21-11-00, PAGES 501-503. (X) 2L73 4F A3WE 19960112000671996011200067EU 1996 1 12 PLG121895E1 119951214A3020 CONNECTORS SAAB SF340 SF340A 7850100EU RT ENGINE DIRTY A PLGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE05741BA 340A090 BDL/YYZ - FLT 4881 - DURING THE FIRST PART OF FLIGHT, RT INTAKE FAIL LIGHT ILLUMINATED. DUE TO THE EXISTING WEATHER CONDITIONS, THE AIRCRAFT RETURNED TO BDL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OIL IN ONE OF THE CONNECTORS FOR THE LOWER DUCT DURING THE SYSTEM INSPECTION. THE OIL WAS CLEANED FROM THE CONNECTOR AND THE SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED BACK TO SERVICE. (X) 2L72 4T RTA52EU 19960112000681996011200068EU 1996 1 12 PLG121895E2 119951209A26131734362450 TEMP SENSOR SAAB SF340 SF340A 7850100EU RT TAILPIPE CONTAMINATED A PLGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE05741BA 340A090 PVD/LGA - FLT 4783 - AFTER TAKEOFF, THE RT TAIL PIPE HOT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT LOWER AFT SENSOR AND SYSTEM OPERATIONS CHECKED GOOD. AIRCRAFT WAS RELEASED BACK TO SERVICE. (X) 2L72 4T RTA52EU 19960112000691996011200069EU 1996 1 12 SIMA953521 119951214A2710S2711201200400 IDLER ARM AEROSPATR72 ATR72212 EU RT WING LOOSE BEARING A SIMAK NONE O OTHER ININSP/MAINT 1 SW21399AT 399 DFW - DURING SCHEDULED COMPLIANCE OF ENGINEERING ORDER E9-2700-001R2 (REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM, AD 93-22-10), THE NR 1 IDLER ARM IN THE RT WING WAS FOUND TO HAVE A LOOSE BEARING. IDLER ARM ASSY WAS REMOVED AND REPLACED. OPERATIONAL CHECK OF AILERON SYSTEM WAS SATISFACTORY AND AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19960112000701996011200070NM 1996 1 12 TAOA129506 119951217A3350900835A BATTERY PACK BOEING727 727225 1384077NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15923TS WA6740 20441 EMREGENCY EXIT SIGN AT ROW 16D INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 2L73 4F A3WE 19960112000711996011200071NM 1996 1 12 TAOA129507 119951217A3350900835A BATTERY PACK BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS VA5725 22043 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (X) 0 4 A3WE 19960112000721996011200072NM 1996 1 12 TWRA9562 119951018A2560 GIRT BAR BOEING747 747212B 1384886NM R4 MAIN ENTRY DRDIRTY A TWRAK NONE O OTHER ININSP/MAINT 1 EA15616FF 21939 R4 DOOR WOULD NOT GO INTO AUTO. CLEANED GIRT BAR FITTING, DOOR OPERATION NORMAL. (X) 2L74 4F A20WE 19960112000731996011200073EU 1996 1 12 VTZA96046 119951220A21501379211L401 PACK BAG JETSTMJETSTM3201 1500217EU LT WING OVERSERVICED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27495UE 818 IAD/ROC - FLT 6423 - DURING CLIMB-OUT AT 1940 HRS ON 12-20-95, AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO IAD DUE TO THERE BEING SMOKE IN THE CABIN. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE DRAINED A SMALL AMOUNT OF OIL FROM THE LT COLD AIR UNIT. PERFORMED MAINTENANCE RUNS, BUT COULD NOT DUPLICATE DISCREPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19960112000741996011200074EU 1996 1 12 VTZA96047 119951220A3260 INDICATOR LIGHT BAG JETSTMJETSTM3201 1500217EU RT MLG MALFUNCTIONED A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27492UE 790 IAD/BGM - FLT 6180 - DURING CLIMB-OUT AT 1100 HRS ON 12-20-95, RETURNED TO IAD DUE TO THE RT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATED WITH THE LANDING GEAR SELECTED UP. AIRCRAFT DID SHOW 3 GREEN LIGHTS FOR GEAR DOWN AND LOCKED WHEN GEAR WAS SELECTED DOWN. ACFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED RT MAIN GEAR UPLOCK AND DOWNLOCK MICROSWITCHES, NO DEFECTS NOTED. PERFORMED GEAR SWINGS, NO FAULT FOUND, UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19960112000751996011200075EU 1996 1 12 VTZA96048 119951226A243523079009 STARTER/GEN JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TOTAKEOFF 1 EA27325UE 41063 IAD/JFK - FLT 6171 - DURING TAKEOFF AT 1230 HRS ON 12-26-95, ABORTED TAKEOFF DUE TO LT GENERATOR FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED STARTER GENERATOR, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19960112000761996011200076 1996 1 12 VTZA96049 419951225A3417 DADC RELAY JETAIRJETSTMJETSTM4101 1500501EU LEFT FAILED A VTZACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 EA27323UE 41059 IAD/JFK - FLT 6485 - DURING CLIMB AT 1400 HOURS ON 12-25-95, LT ALTIMETER FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED DADC SWITCHING RELAY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19960112000771996011200077NM 1996 1 12 96ZZZX139 119951218A2420902F2425 CONTROL PANEL BOEING727 72776 1384016NM NR 1 GENERATOR SHORTED A RYNAO OTHER HJBELECT. POWER LOSS-50 PC WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE07721JE 18843 IN CRUISE, NR 1 GENERATOR LIGHT FLICKERED, ESSENTIAL SWITCHED TO NR 3, NR 3 GENERATOR FAILED. ALL LIGHTS FLICKERED, NR 1 GEN FAILED, AND NR 2 GEN DROPPED OFF LINE. STANDBY POWER SELECTED, NR 2 GEN PUT BACK ON LINE. ELECTRICAL SMELL NOTED IN COCKPIT. ONE GEN OPERATION WAS EXECUTED. AIRCRAFT LANDED AT DTW WITHOUT INCIDENT. FOUND EVIDENCE OF SHORTING IN NR 1 GENERATOR CONTROL PANEL. REPLACED PANEL, OPS CHECK NORMAL. 2L73 4F A3WE 19960112000781996011200078EU 1996 1 12 96ZZZX140 119951213A2841710920 FUEL QTY IND INTERTECHNIQ710920 STBROSSD3 SD330 8100602EU AFT FUEL TANK OUT OF CAL A DATAE ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL1355AN SH3025 CRW - AIRCRAFT FUELED TO 3,950 POUNDS FUEL. EN ROUTE FROM CRW TO MEM, CREW OBSERVED AN IMBALANCE OF FUEL. CROSSFEED PROCEDURES SELECTED UNTIL IMBALANCE CORRECTED. ON DESCENT INTO MEM (VFR MODERATE TURBULENCE), CROSSFEED LIGHT CAME ON, CROSSFEED WAS VERIFIED CLOSED. ON FINAL, RT ENGINE BEGAN TO SURGE, CREW ELECTED TO SHUT DOWN RT ENG AND NOTIFIED MEM THEY WERE SINGLE ENGINE AND THERE WAS NO EMERGENCY. ONCE ON THE GROUND, FUEL TANKS WERE DIP STICKED FINDING THE AFT TANKS NEAR EMPTY. RT ENG RESTARTED AND RAN NORMAL. FUEL GAUGE DEFERRED PER MEL. ACFT RETURNED TO SERVICE WITHOUT FURTHER PROBLEMS. MX CHECKED FUEL QTY INDICATING SYS CALIBRATION AND FUEL SYS AFT FUEL TANK INDICATING CORRECTED AND MEL CLEARED. 2H72 4T A41EU 19960112000791996011200079NM 1996 1 12 CAL951125 119951211A323069355005 UPLOCK ACTUATOR BOEING737 7373T0 1384582NM RT MLG INOPERATIVE A CALAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 SW097033030095 23460 FLT NR 1525 - CLE - THE RIGHT MLG RED LIGHT REMAINED ILLUMINATED AFTER TAKEOFF WITH THE GEAR HANDLE IN THE UP POSITION. WHEN HANDLE WAS SELECTED TO OFF THE RED LIGHT REMAINED ON AND THE RIGHT GEAR GREEN LIGHT CAME ON AFTER A FEW SECONDS. THE GEAR HANDLE WAS CYCLED UP AND THE GREEN LIGHT WENT OUT AND THE GEAR COULD BE FELT COMING UP. THE GEAR WAS CYCLED DOWN WITH SAFE INDICATIONS AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE RIGHT MLG UPLOCK ACTUATOR WAS REMOVED AND REPLACED. IN ADDITION, THE RIGHT MLG UPLOCK SENSOR WAS ALSO REPLACED. GEAR OPERATION AND INDICATIONS CHECKED GOOD. (M) 2L72 4F RTA16WE 19960112000801996011200080NM 1996 1 12 CAL951132 119951128A5320 PANEL BOEING737 7372C0 1384488NM STA 277 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097324370967 20072 GSO - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEELWELL CEILING PRESSURE PANEL AT STA 277, RT SIDE. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5310-03186. (X) 2L72 4F A16WE 19960112000811996011200081NM 1996 1 12 CAL951134 119951201A5330 SKIN BOEING737 7372C0 1384488NM BS 290 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097324370967 20072 GSO - INSPECTION FOUND RT FUSELAGE SKIN PANEL CORRODED AT STA 290. THE SKIN PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19960112000821996011200082NM 1996 1 12 CAL951135 119951201A5320 ANGLE BOEING737 7372C0 1384488NM BS 323-328 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097324370967 20072 GSO - INSPECTION FOUND T-ANGLE CORRODED AT STA 323 - STA 328, RT SIDE. A NEW T-ANGLE, SPLICES, AND DOUBLER WERE INSTALLED IAW ECRA 5330-02337. (X) 2L72 4F A16WE 19960112000831996011200083NM 1996 1 12 CAL951136 119951201A5320 ANGLE BOEING737 7372C0 1384488NM BS 323 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097324370967 20072 GSO - INSPECTION FOUND T-ANGLE CORRODED AT STA 323, S27L TO S27R. A NEW T-ANGLE WAS INSTALLED IAW SRM 51-30-2. (X) 2L72 4F A16WE 19960112000841996011200084NM 1996 1 12 CAL951137 119951201A5320 DOUBLER BOEING737 7372C0 1384488NM BS 323 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097324370967 20072 GSO - INSPECTION FOUND DOUBLER CORRODED AT STA 323, STR 27L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02337. (X) 2L72 4F A16WE 19960112000851996011200085WP 1996 1 12 CAL951139 119951206A55305939711502 ANGLE DOUG DC9 DC982 3022082WP RT VERTICAL FIN CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW093588838870 49117 IAH - INSPECTION FOUND A .25 INCH CRACK AT FASTENER HOLE OF RT VERTICAL FIN ATTACH ANGLE. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 19. (X) 2L72 4F A6WE 19960112000861996011200086WP 1996 1 12 CAL951141 119951214A2450FLLCG4 CURRENT LIMITER DOUG DC9 DC982 3022082WP AC CROSS-TIE RLYBLOWN A CALAA UNSCHED LANDING JH WARNING INDICATION ELECT. POWER LOSS-50 PC CRCRUISE 1 SW09937MC 49450 ORF - FLT 0443 - THE LEFT ENGINE GENERATOR WAS LOST ACCOMPANIED BY FEEDER FAULT LIGHT AND A CROSS-TIE LOCK OUT WHILE EN ROUTE FROM EWR TO FLL. THE AIRCRAFT WAS DIVERTED TO ORF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AC CROSS-TIE RELAY PHASE CURRENT LIMITER BLOWN. THE CURRENT LIMITER WAS REPLACED. THE GENERATORS WERE OPERATED WITH BOTH ENGINES RUNNING AND OPERATION CHECKED GOOD. THE AC CROSS-TIE SYSTEM TESTED NORMAL. (X) 2L72 4F A6WE 19960112000871996011200087NM 1996 1 12 CAL951148 119951215A3610652673831 DUCT BOEING727 727227 1384078NM NR 3 ENGINE FAILED A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW0988770 20839 ATL - FLT 1432 - THE NR 3 ENGINE FIRE LIGHT AND NR 3 START VALVE LIGHT BOTH ILLUMINATED INTERMITTENTLY IN-FLIGHT WITH A LOSS OF CABIN PRESSURE. ACFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 3 ENGINE'S 13TH STAGE PNEUMATIC DUCT BLOWN. NO OTHER DAMAGE WAS NOTED. THE 13TH STAGE DUCT REMOVED AND REPLACED. IN ADDITION, NR 1 ENGINE PRE-COOLER HEAT EXCHANGER FOUND INOPERATIVE. PRE-COOLER HEAT EXCHANGER REMOVED AND REPLACED. ACFT PRESSURIZED AND A DECAY CHECK PERFORMED WITH ALL SYSTEMS CHECKING NORMAL. (X) 2L73 4F A3WE 19960112000881996011200088WP 1996 1 12 CAL951149 119951216A27604936976501 BOLT DOUG DC9 DC982 3022082WP RT SPOILER ACT BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW0983870 48056 DEN - INSPECTION FOUND RT INBOARD GROUND SPOILER FORWARD ACTUATOR PIVOT BOLT BROKEN. THE FORWARD ACTUATOR PIVOT BOLT WAS REMOVED AND REPLACED. (X) 2L72 4F A6WE 19960112000891996011200089WP 1996 1 12 CAL951151 119951215A33506011777 POWER SUPPLY DOUG DC9 DC932 3022066WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0918513 48112 IAH - INSPECTION FOUND THE LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. (X) 2L72 4F A6WE 19960112000901996011200090WP 1996 1 12 CAL951153 119951128A5320 BRACKET DOUG DC9 DC982 3022082WP BS 946 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091689226763 49391 HOU - INSPECTION F0UND A .75 INCH CRACK IN LT KEEL BEAM BRACKET AT STA 946. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5. (X) 2L72 4F A6WE 19960112000911996011200091WP 1996 1 12 CAL951155 119951201A53203920341501 BRACKET DOUG DC9 DC982 3022082WP BS 845 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091689226763 49391 HOU - INSPECTION FOUND A 3 INCH CRACK IN BRACKET AT LT OUTBOARD END OF FLOOR BEAM, STA 845, LONGERON 18. THE BRACKET WAS REMOVED AND REPLACED. (X) 2L72 4F A6WE 19960112000921996011200092WP 1996 1 12 CAL951156 119951128A5280 DOOR JAMB DOUG DC9 DC982 3022082WP BS 946 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091689226763 49391 HOU - INSPECTION FOUND A .50 INCH CRACK AT INBOARD END OF LT WHEELWELL FORWARD DOOR JAMB, STA 946. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2. (X) 2L72 4F A6WE 19960112000931996011200093NM 1996 1 12 CAL951157 119951215A5720 TEE CHORD BOEING737 737130 1384435NM WS 685 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094421464706 19031 GSO - INSPECTION FOUND A 2 INCH CRACK IN TEE CHORD AT STA 685, BL ZERO. THE CRACK WAS STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5710-01705. (X) 2L72 4F A16WE 19960112000941996011200094WP 1996 1 12 CAL951158 119951206A53112777930 BELT FRAME DOUG DC9 DC932 3022066WP BS 980 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091755762473 47424 HOU - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. (X) 2L72 4F A6WE 19960112000951996011200095WP 1996 1 12 CAL951159 119951206A5320 FORMER DOUG DC9 DC932 3022066WP BS 980 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091755762473 47424 HOU - INSPECTION FOUND A 1.5 INCH CRACK IN SKIN CLIP (FORMER) AT STA 980 BELOW LONGERON 14R. THE CRACK WAS STOP DRILLED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 5301, FIGURE 2, SHEET 4. (X) 2L72 4F A6WE 19960112000961996011200096NM 1996 1 12 USAA951321 119951211A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 957 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 2.50 INCH DIAMETER SPOT OF CORROSION, BS 957, LBL 50, ON INTERCOSTAL. REPAIRED PER SRM 51-10-02. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19960112000971996011200097NM 1996 1 12 USAA951322 119951211A5320650103184779 INTERCOSTAL BOEING737 737401 1384701NM BS 967-987 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1.50 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES, RBL 16, BS 967 TO BS 987, ON INTERCOSTAL. REMOVED AND REPLACED WITH NEW PART. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19960112000981996011200098NM 1996 1 12 USAA951323 119951211A52406545871124 HINGE BOEING737 737401 1384701NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 6 INCH CRACK FORWARD SERVICE DOOR LOWER GATE. REPLACED HINGE ASSEMBLY. REPAIRED PER EA 40346. (X) 2L72 4F RTA16WE 19960112000991996011200099NM 1996 1 12 USAA951324 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND STA 520 FLOOR BEAM NEEDS TO BE MODIFIED AT BL ZERO PER SB 737-53-1120 DUE TO CRACKS AT LBL 45, RLB 25, RBL 45 AND LBL 25. MODIFIED CHANNEL PLUS LINK INSTALLED PER REF EA 40383 SB 737-53-1120. NOTE: NO REPAIR MADE. MODIFIED CHANNEL PLUS LINK INSTALLED ONLY. REPAIRED PER SB 737-53-1120, EA 40383. (X) 2L72 4F RTA16WE 19960112001001996011200100NM 1996 1 12 USAA951325 119951211A53206545855101 ANGLE BOEING737 737401 1384701NM BS 936-975 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 3 INCH DIAMETER SPOT OF CORROSION AND 3.50 INCH BY 18 INCH AREA OF CORROSION, BS 936 AND BS 957 ON DOOR Z-ANGLE. REMOVED CORRODED Z-ANGLE AND INSTALLED NEW Z-ANGLE FROM STOCK, PN 65-45855-101. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19960112001011996011200101NM 1996 1 12 USAA951326 119951211A5347 FLOOR TRACK BOEING737 737401 1384701NM BS 727-787 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US 23989 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND SEVERAL .50 INCH BY 1 INCH CORRODED AREAS, BS 727F TO BS 787, RBL 14, CARGO FLOOR TRACK. CUT OUT CORRODED TRACK (BEAM) FROM BS 727E PLUS 14 TO BS 807. FABRICATED AND INSTALLED NEW BEAM SECTION AND SPLICES. REPAIRED PER SRM 53-00-53, FIGURES 202 AND 203, TR 53-10-06. CORROSION TASK NR C53-208-01. CORROSION LEVEL 2. (X) 2L72 4F RTA16WE 19960112001021996011200102WP 1996 1 12 9521919601 119951002A5330 SKIN DOUG DC9 DC932 3022066WP FS 180 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT THE ATC TRANSPONDER ANTENNA FS 180. REPAIRED SKIN PER EA 12-5330-9-C0533. 2L72 4F A6WE 19960112001031996011200103WP 1996 1 12 9521989601 119951006A5730 SKIN DOUG DC9 DC932 3022066WP WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT AND RIGHT WING LOWER SKIN PANELS. REPAIRED SKIN (P/N 5910465), PER EA 12-5720-9-C0494. 2L72 4F A6WE 19960112001041996011200104WP 1996 1 12 9522019601 119951006A5311 FRAME DOUG DC9 DC932 3022066WP FS 1168 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE TAIL SECTION LEFT HAND FRAME FS 1168. REPAIRED FRAME (P/N 9911843-5), PER EA 12-5310-9-C0608. 2L72 4F A6WE 19960112001051996011200105WP 1996 1 12 9522029601 119951011A5330 SKIN DOUG DC9 DC932 3022066WP FS 770 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 770 BETWEEN LONGERONS 18L TO 19L. REPAIRED SKIN PER EA 12-5330-9-C0603. 2L72 4F A6WE 19960112001061996011200106WP 1996 1 12 9522039601 119951011A5713 LONGERON DOUG DC9 DC932 3022066WP WS 58 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STRINGERS 17L AND 19L OUTBOARD OF STA 58 WEB. REPAIRED STRINGER PER EA 12-5720-9-C0543. 2L72 4F A6WE 19960112001071996011200107WP 1996 1 12 9522049601 119951012A5711 SPAR CAP DOUG DC9 DC932 3022066WP WS 477-509 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER CAP XRS 477-509. REPAIRED CAP (P/N 5911301), PER EA 12-5720-9-C0486. 2L72 4F A6WE 19960112001081996011200108WP 1996 1 12 9522059601 119951019A5312 BLKHD WEB DOUG DC9 DC932 3022066WP FS 756 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE WHEEL WELL BULKHEAD KEEL WEB FS 756. REPAIRED WEB (P/N 9910164-3), PER EA 12-5310-9-C0614. 2L72 4F A6WE 19960112001091996011200109WP 1996 1 12 9522069608 119951024A5311 FRAME DOUG DC9 DC932 3022066WP FS 598 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 598 FRAME BETWEEN LONGERONS 19R TO 23R INBOARD FLANGE. REPAIRED FRAME (P/N 9919621-2), PER EA 99-102766. 2L72 4F A6WE 19960112001101996011200110WP 1996 1 12 9522079601 119951027A5313 LONGERON DOUG DC9 DC932 3022066WP FS 690 CORROSION A NWAAK NONE O OTHER ININSP/MAINT 1 GL01601NW 47038 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 30 AT FS 690. REPAIRED LONGERON (P/N 9915525-1), PER EA 12-5315-9-C0609. 2L72 4F A6WE 19960112001111996011200111WP 1996 1 12 9522089608 119951102A5711 SPAR CAP DOUG DC9 DC932 3022066WP WS 445-454 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING REAR SPAR UPPER 'T' CAP XRS 445 TO 454. REPAIRED 'T' CAP (P/N 5911300-1), PER EA 99-102931. 2L72 4F A6WE 19960112001121996011200112WP 1996 1 12 9522099608 119951106A5330 SKIN DOUG DC9 DC932 3022066WP FS 205-209 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE INNER SKIN AT LONGERON 18L BETWEEN FS 205 TO 209. REPAIRED SKIN (P/N 5956879-1), PER EA 99-103113. 2L72 4F A6WE 19960112001131996011200113WP 1996 1 12 9522109608 119951114A5311 FRAME DOUG DC9 DC932 3022066WP FS 1168 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1168 CANTED FRAME BETWEEN LONGERONS 21L TO 22L. REPAIRED FRAME (P/N 9911843-501), PER EA 99-103125. 2L72 4F A6WE 19960112001141996011200114WP 1996 1 12 9522119608 119951120A5330 SKIN DOUG DC9 DC932 3022066WP FS 813 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 813 AT LONGERON 26L. REPAIRED SKIN PER EA 99-103144. 2L72 4F A6WE 19960112001151996011200115WP 1996 1 12 9522129608 119951220A5753 SKIN DOUG DC9 DC932 3022066WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT FLAP LEADING EDGE SKIN AT XRS 148. REPAIRED SKIN (P/N 5913560-155), PER EA 99-102935. 2L72 4F A6WE 19960112001161996011200116WP 1996 1 12 9522139608 119951220A5753 SPAR CAP DOUG DC9 DC932 3022066WP RT TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01608NW 47233 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT FLAP REAR SPAR LOWER CAP, XFLS 334. REPAIRED CAP (P/N 9991234-501), PER EA 99-102936. 2L72 4F A6WE 19960112001171996011200117NE 1996 1 12 9522149150 219951211A7532 PRBC DOUG DC9 DC914 3022034WP PWA JT8 JT8D7B 52053NE NR 2 ENGINE MALFUNCTIONED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 GL018908E 45749 NR 2 ENGINE EPR WAS LOW AND UNSTABLE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC WITH A SERVICEABLE UNIT. ENGINE PERFORMANCE WAS STAISFACTORY ON SUBSEQUENT RUNUP. 2L72 4F4 F A6WE E2EA 19960112001481996011200148NM 1996 1 12 DL72S960019 119951129A5330 SKIN BOEING727 727232 1384082NM L 1 DOOR CUTOUT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 TPA MAINTENANCE REPORTED, TWO CRACKS IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE FIRST CRACK, APPROXIMATELY 5 INCHES LENGTH, HAS PROPAGATED THROUGH THE EXTERNAL SKIN AND THE BONDED DOUBLER. THE SECOND CRACK 6 INCHES LONG, WAS CONTAINED WITH THE BEAR STRAP. THE DAMAGE WAS CUT OUT AND AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLED PER FAA/DER FORM 8110-3 DATED 12-05-95. 2L73 4F A3WE 19960112001491996011200149NM 1996 1 12 DL72S960020 119951221A5311 FRAMES BOEING727 727232 1384082NM FS 784 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 THE LT FS 784 OVERWING EXIT FRAME WAS FOUND WITH A CRACK 1.1 INCH LONG. IT BEGAN AT A FASTENER HOLE ON THE INBD FLANGE AT WL 215 AND RAN HORIZONTALLY FWD AND THROUGH THE BEND RADIUS JUST INTO THE WEB. THIS CRACK IS OUTSIDE THE TYPICAL CRACK AREA AS DEFINED IN S/B 727-53-0197 REV 2. ALSO, A 1 INCH CRACK WAS FOUND ON THE LT FRAME OUTBD FLANGE RADIUS JUST ABOVE THE LOWER END OF THE PART. INSTALLED A MODIFIED REPAIR BASED ON THE 727-53-0197 REV 2 SERVICE BULLETIN PER FAA LETTER 95-120S-1456, DL ERA 302852-14AD. 2L73 4F A3WE 19960112001501996011200150NM 1996 1 12 DL72S960021 119951220A533065545662 SKIN BOEING727 727232 1384082NM FS 500 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27531DA 21814 THE FUSELAGE SKIN AT STA 500 STR 28R WAS DAMAGED BY CORROSION AND A 13.5 INCH BY 3.5 INCH SECTION WAS CUTOUT. A SKIN REPAIR WAS ACCOMPLISHED PER B727 SRM 53-30-3 FIG 3, EXCEPT THE DOUBLER WAS EXTENDED FORWARD TO STA 480 BUTT JOINT. REPAIRS ACCOMPLISHED PER DL ERA 302931-14. 2L73 4F A3WE 19960112001511996011200151NM 1996 1 12 DL72S960022 119951212A5311 FRAME BOEING727 727232 1384082NM FS 761 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 DURING ACCOMPLISHMENT OF EO4-61904-3AD, SEVERAL HOLES IN THE INB'D FRAME FLANGE AT FS 760.95 LT AND RT WERE OVERSIZED BEYOND LIMITS. THE OVERSIZED HOLES WERE REWORKED AND OVERSIZED FASTENERS WERE INSTALLED PER BACO TWX DAL-ATL-95-1340RR DTD 11 DEC 95, DL ERA 302845-14AD. 2L73 4F A3WE 19960112001521996011200152NM 1996 1 12 DL72S960024 119951228A533065545662 SKIN BOEING727 727232 1384082NM FS 480 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27407DA 21151 A SKIN CRACK, 1.75 INCH BY 2 INCH WAS DISCOVERED BETWEEN STRINGER 27R AND 28R, FS 481. THE PREVIOUS REPAIR ON THIS SECTION MEASURED 5.5 INCH BY 13 INCH. THE REPAIRS WERE INCORPORATED INTO ONE REPAIR AFTER REMOVAL OF PREVIOUS REPAIR. THIS ER/A SUPERCEDES ER/A 233402-14. DURING INSTALLATION OF REPAIR FURTHER CORROSION WAS DISCOVERED AT PREVIOUS CUT OUT. FINAL CUT OUT DIMENSIONS ARE 9 INCHES BY 15 INCHES. REVISION WILL REMOVE CORROSION AND INSTALL A LARGER DOUBLER PER B727 SRM 53-30-3 FIG 3A. 2L73 4F A3WE 19960112001531996011200153NM 1996 1 12 DL72S960025 119951222A5330655458310 SKIN BOEING727 727232 1384082NM SERV DOOR CUTOUTCRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 THE FUSELAGE SKIN AT THE RT AFT SERVICE DOOR CUTOUT, LOWER AFT CORNER WAS CUT OUT TO REMOVE DAMAGE AROUND EXISTING NUTPLATE HOLE. THE RESULTANT CUT OUT IS APPROX 2.3 UP/DOWN AND 2.1 FWD/AFT. THE CUT OUT IS THROUGH THE SKIN AND BONDED DOUBLER ONLY. INSTALLED A REPAIR DOUBLER AND TRIPLER TO RESTORE THE INTEGRITY OF THE LOWER AFT CORNER OF THE RT AFT SERVICE DOOR CUTOUT. THIS WAS REPAIRED PER FAA/DER FORM 8110-3, 12-22-95 DL ERA 302894-14. 2L73 4F A3WE 19960112001541996011200154NM 1996 1 12 DL72S960026 119951222A5713 STRINGER BOEING727 727232 1384082NM WS 656.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 THE VENT STRINGER 13 ON THE LT WING WAS FOUND WITH A CRACK IN THE STRINGER TO RIB ATTACH TAB AT WING STATION 656.5. DUE TO THE EXTENT OF THE CRACK, THE STOP DRILL REPAIR CALLED OUT IN EO 4-60350-3AD COULD NOT BE ACCOMPLISHED. THE DAMAGED TAB WAS REMOVED AND A FILLER INSTALLED PER FAA/DER FORM 8110-3, 12-21-95 DL ERA 302915-14AD. 2L73 4F A3WE 19960112001571996011200157NM 1996 1 12 DL72S960030 119950929A5754 RIBS BOEING727 727232 1384082NM LE FLAPS CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 DURING INITIAL SHOP INSPECTION, FOUND RIBS NR 16 AND 17 CRACKED AT UPPER FORWARD CORNER. REPAIRED CRACKED AS PER MM 57-54-0. 2L73 4F A3WE 19960112001581996011200158NM 1996 1 12 DL72S960035 119951002A5754 RIB BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 DURING A SHOP INSPECTION, A CRACK WAS FOUND ON THE NR 3 RIB AT THE I/B TRACK ATTACH. A REPAIR WAS INSTALLED PER THE M/M 57-54-0 PG 807, FOR NR 3 L/E SLAT. 2L73 4F A3WE 19960112001591996011200159NM 1996 1 12 DL72S960036 119951002A5754 COVE PANEL 651622295 BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA BN163 21469 DURING A SHOP INSPECTION, A CRACK WAS FOUND ON A COVE PANEL LOCATED AT THE I/B UP STOP ATTACH POINT. A REPAIR WAS INSTALLED PER THE M/M 57-54-0, FOR NR 3 L/E SLAT. 2L73 4F A3WE 19960112001601996011200160NM 1996 1 12 DL72S960037 119950105A5754651622295 ANGLE BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 COVE ANGLE CRACKED AT I/B UP STOP ATTACH POINT. REPAIRED PER M/M 57-54-0, FOR NR 3 L/E SLAT AT SHOP INSPECTION. 2L73 4F A3WE 19960112001611996011200161NM 1996 1 12 DL72S960038 119950105A5754651622295 RIB BOEING727 727232 1384082NM NR 3 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 NR 3 RIB CRACKED AT I/B TRACK ATTACH POINT. REPAIRED PER M/M 57-54-0 PG 807. FOUND DURING NR 3 L/E SLAT AT SHOP INSPECTION. 2L73 4F A3WE 19960112001641996011200164NM 1996 1 12 DL72W960023 119951228A533065545655 SKIN BOEING727 727247 138408FNM FS 660-680 DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO272817W 20873 THE FUSELAGE SKIN WAS OIL CANNED BETWEEN FS 660 TO 680 STR 23R AND STR 26R. THE DAMAGED AREA OF THE SKIN WAS TRIMMED OUT FROM FS 680 BUTT JOINT FORWARD FOR 19.75 AND FROM THE SKIN LAP JOINT AT STR 26R UP 25.75. A REPAIR DOUBLER WAS INSTALLED PER 8110-3 12-28-95, DL ERA 302929-14. 2L73 4F A3WE 19960112001671996011200167NM 1996 1 12 DL757960009 119950102A2530 COFFEE MAKER 811150417 BOEING757 757232 1384965NM AFT GALLEY ODOR A DALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 SO27681DA 26957 REPORTED BY FLIGHT ATTENDANT, AFT GALLEY NR 1 COFFEE MAKER HAS SLIGHT ELE SMELL. FWD TO MCO, THEN REPLACED COFFEE MAKER. 2L72 4F RTA2NM 19960112001691996011200169NM 1996 1 12 DL757960032 119951030A5754 TE WEDGE 114N4005178 BOEING757 757232 1384965NM NR 7 LE FLAP DELAMINATED A DALAK NONE O OTHER ININSP/MAINT 1 SO27604DL 000011 22811 T/E DELAMINATED, REPLACED WEDGE PER SRM 57-43-02. FOUND DURING SHOP INSPECTION FOR NR 7 SLAT. 2L72 4F RTA2NM 19960112001701996011200170NM 1996 1 12 DL757960041 119951112A5754 TE WEDGE 14N300220 BOEING757 757232 1384965NM RT LE FLAP DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27619DL 00036 22909 UPON ROUTINE INSPECTION, T/E WEDGE WAS FOUND DENTED. REPLACED WEDGE AS PER 57-43-02. ALSO, PERFORMED TERMINATING ACTION OF AD 90-23-06 BY INSTALLING T/E WEDGE 114N3003-34. 2L72 4F RTA2NM 19960112001731996011200173WP 1996 1 12 DLL15960050 119951211A52301582145 FITTING LKHEED1011 10113853 5265020WP C1 CARGO DOOR CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27754DL 193Y1181 DURING COMPLETION OF SI 7-58-181-12AD, SURFACE CORROSION WAS FOUND IN THE UPPER WELL LOWER WEBS ON EACH OF THE EIGHT FITTINGS. IN ADDITION THE NR 1 LATCH FITTING HAD A CORRODED ATTACH BOLT HOLE AND FITTINGS HAD CORROSION IN THE LOCKING PIN BORE. ALL SURFACE CORROSION WAS BLENDED AWAY AND THE BOLT HOLES WERE OVERSIZED TO REMOVE THE DAMAGE. 2L73 4F A23WE 19960112001771996011200177NM 1996 1 12 DLM88960051 119951108A53305953050 SKIN DOUG MD88 MD88 3023688NM BS 541-560 DAMAGED A DALAK NONE C F.O.D. TXTAXI/GRND HDL 1 SO27938DL 49811 DURING ROUGH WEATHER AT BDL, AN AIR STAIR CART COLLIDED WITH THE FUSELAGE AND LEFT A 4 INCH BY 9 INCH HOLE. ALSO, DAMAGING LONGERON 20L, BETWEEN FS 541 AND 560. 2L72 4F RTA6WE 19960112001791996011200179WP 1996 1 12 UPS805176 119951130A5742 FITTINGS DOUG DC8 DC873F 302199FWP PYLON CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 2 AND NR 3 WING FRONT SPAR PYLON SUPPORT FITTINGS CRACKED. REPLACED FITTINGS PER UPS EO. 2L74 4F RT4A25 19960112002161996011200216SO 1996 1 12 96ZZZX145 119951213A5230 DOOR EMB 110 EMB110P1 3260122SO AFT CARGO OPENED A APIVAA UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 WP13110EM14397 110426 AFTER TAKEOFF, THE AFT CARGO DOOR CAME OPEN CAUSING THE CARGO DOOR LINING TO COME OFF AND THE AIRCRAFT TO BUFFET. THE DOOR WAS CHECKED SECURE AT PRE-FLIGHT AND THE 'DOOR OPEN' CAUTION LIGHTS ON THE PILOT'S PANEL WERE CHECKED PRIOR TO TAKEOFF WITH NO INDICATIONS. AIRCRAFT WAS LANDED WITHOUT FURTHER INCIDENT. DOOR AND LATCHING MECHANISMS WERE CHECKED AND CYCLED SEVERAL TIMES. NO DAMAGE WAS FOUND. LATCHES WORKED PROPERLY, AIRCRAFT RETURNED TO SERVICE. 1L72 4T A21SO 19960112002251996011200225 1996 1 12 96ZZZX154 419951120A61228971609 GOVERNOR CESSNA441 441 2076020CE LT ENG PROP MALFUNCTION A R7MAO OTHER O OTHER CRCRUISE 1 NM118970N 1050 P1326 4410092 SURGING OF LEFT ENGINE DURING FLIGHT. PROP GOVERNOR, POSSIBLE FAILURE. REPLACED PROP GOVERNOR AND TESTED OVERSPEED SYSTEM, FOUND OVERSPEED FUNCTIONS PROPERLY AND LIMITS WERE NOT EXCEEDED DURING FLIGHT. 1L72 3T RTA28CE 19960112002271996011200227EU 1996 1 12 96ZZZX156 119950718A2150365A32285802 BRACKET AEROSPSA365 AS365N2 8680815EU AIR CONDITIONER CRACKED A ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365WM376 6429 AIR CONDITIONER BRACKET CRACKED. REMOVED AND REPLACED BRACKET. 1G72 3U RTH10EU 19960112002281996011200228EU 1996 1 12 96ZZZX157 119951016A793158004658014 DATA PACK AEROSPSA365 SA365N 8680669EU NR 2 OIL PRESS INDICATOR STICKSA ZYWAK NONE O OTHER ININSP/MAINT 1 GL09365SJ 435 6018 NR 2 OIL PRESSURE INDICATOR STICKS AT ZERO ON POWER-UP AND START. REMOVED AND REPLACED 14 DATA PACK. 1G72 3U H10EU 19960112002291996011200229EU 1996 1 12 96ZZZX158 119951109A321017835100 DRAG STRUT AEROSPSA365 SA365N 8680669EU MLG SEAL LEAKING A ZYWAK NONE K FLUID LOSS ININSP/MAINT 1 GL09365SJ2966 37 6018 SEALS LEAKING ON DRAG STRUT. REMOVED AND REPLACED DRAG STRUT. 1G72 3U H10EU 19960112002301996011200230EA 1996 1 12 96ZZZX159 219951206A852075060 BOLT ENSTRMF28 F28C 3300407GL LYC O360 HIO360E1AD 41514EA NR 3 CON ROD FAILED A H7LAK NONE O OTHER NRNOT REPORTED 1 NM115697B881 5052 RL207051A THE NR 3 ROD CAP SEPARATED FROM ROD. ROD BOLTS WERE DAMAGED TOO BADLY TO BE IDENTIFIED FOR SURE, BUT SHOULD BE PART NUMBER LISTED. THESE BOLTS HAVE STRETCH TORQUE. SUBMITTER SUSPECTS IMPROPER TORQUING (EITHER TOO MUCH OR NOT ENOUGH) CAUSING BOLT FAILURE. AD 95-07-1 DOES NOT APPLY. 1G71 3O3 O H1CE 1E10 19960112002561996011200256NE 1996 1 12 96ZZZX185 219951009A7230 BEARING FOKKERF27 F27MK600 4990706EU RROYCEDART DART5327R 54509NE LT ENGINE FAILED A OIZAO OTHER J WARNING INDICATION CLCLIMB 1 WP192FOR 10394 18049 CREW NOTED REDUCED TORQUE INDICATED ON TAKEOFF. CLIMB TORQUE INDICATED NORMAL. PCU AND FCU WERE CHANGED WITH NO EFFECT. WET TAKEOFF POWER NORMAL. ENGINE WAS REMOVED AND SENT TO ROLLS ROYCE CANADA. TEAR DOWN INDICATES FAILURE OF LAY SHAFT FRONT BEARING ROLLERS AND INNER TRACKS. ALL FILTERS IN OTHER ENGINES IN FLEET INSPECTED WITH NO EVIDENCE OF TROUBLE WITH OTHER ENGINES. 2H72 4T4 T A817 E297 19960112002601996011200260WP 1996 1 12 9522159310 119951229A5230 CARGO DOOR DOUG DC9 DC982 3022082WP FWD CARGO COMPT NOT CLOSED A NWAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL01313RC 48091 IND-MSP - AS POWER WAS APPLIED FOR TAKEOFF, THE FORWARD CARGO DOOR ANNUNCIATOR LIGHT ILLUMINATED. ABORTED TAKEOFF AND ANNUNCIATOR REMAINED ILLUMINATED. MAINTENANCE RECLOSED DOOR UPON RETURN TO GATE AREA. DEPARTED IND WITHOUT FURTHER INCIDENT. 2L72 4F A6WE 19960112002721996011200272EU 1996 1 12 QXEA9600010 119950104A33505515800104 CIRCUIT BOARD FOKKERF28 F28MK1000 4990808EU CABIN FAILED A QXEAK NONE L NO TEST ININSP/MAINT 1 NM09469US 11096 PDX - EXIT SIGN ON FORWARD CABIN BULKHEAD INOP. CIRCUIT BOARD WAS REPLACED AND SIGN OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA20EU 19960112002741996011200274NM 1996 1 12 QXEA9600012 119950105A335082410162007 CONTROL BOX DHAV DHAV DHC8 DHC8102 2809003NM CABIN MALFUNCTIONED A QXEAK NONE L NO TEST CLCLIMB 1 NM09813PH 32 PDX - ON CLIMBOUT, WHEN GEAR IS RAISED CABIN EMER LIGHTS FLICKER. CONTROL BOX AND BATTERY PACKS PS3 AND PS4 REPLACED. EMER LIGHTS OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA13NM 19960112002781996011200278SO 1996 1 12 SWIA95703 119951227A3260 IND BULBS EMB 120 EMB120ER 3260203SO NLG FAILED A SWIAO OTHER P NO WARNING INDICATION DEDESCENT 1 NM07214SW 120280 NO GREEN LIGHTS ON NOSE GEAR ILLUMINATED WITH GEAR HANDLE DOWN. REPLACED BULBS IN NOSE DOWN INDICATOR LIGHTS AND A AND B CHECKS GOOD. 2L72 4T RTA31SO 19960112002831996011200283WP 1996 1 12 96ZZZM14 119951216A3260 SW WIRE DOUG DC8 DC851 3021920WP LT MLG BROKEN A TC8AK NONE N FALSE WARNING LDLANDING 1 GL23805CK 45649 BYH - NO GREEN LIGHT FOR LEFT MAIN LANDING GEAR ON LANDING. FOUND BROKEN WIRE AT LEFT MAIN GEAR SWITCH. REPAIRED WIRE, OPS CHECKS GOOD ON GROUND. (M) 2L74 4F 4A25 19960112002841996011200284WP 1996 1 12 96ZZZM15 119951221A3230 RETRACT MECH DOUG DC8 DC862 3021970WP NLG MALFUNCTIONED A RRXAA UNSCHED LANDING JE WARNING INDICATION VIBRATION/BUFFET CLCLIMB 1 WP15995CF 46024 FLT - NR 651 - KPDX-KDAY - ON GEAR RETRACTION, A LOUD NOISE AND VIBRATION WAS NOTICED IN THE NOSE AREA. THE LANDING GEAR WAS RECYCLED WITH THE SAME RESULTS. RETURNED TO KPDX. MAINTENANCE INSPECTED THE UPLATCH FITTINGS, TRUNNION AND THE NOSE WHEEL WELL. NO DEFECTS WERE NOTED. (M) 2L74 4F 4A25 19960112002851996011200285SW 1996 1 12 96ZZZM16 119951108A32601EN516 DNLOCK SWITCH SWRNGNSA226 SA226TC 8780404SW RT MLG DEFECTIVE A BSAAO OTHER N FALSE WARNING DEDESCENT 1 NM05115BS TC324 NOSE LANDING GEAR WOULD NOT INDICATE 'GREEN' AFTER SELECTION TO DOWN ON DESCENT INTO LWT. DEFECTIVE DOWNLOCK SWITCH. REMOVED AND REPLACED DEFECTIVE DOWNLOCK SWITCH. GEAR RETRACT FUNCTION CHECK PERFORMED NORMAL. (M) 1L72 4T A8SW 19960112002861996011200286WP 1996 1 12 96ZZZM17 219951024A73218070225 FUEL CONTROL SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP NR 2 ENGINE LEAKING A BSAAO OTHER K FLUID LOSS CLCLIMB 1 NM05139PA TC296 RIGHT ENGINE TORQUE BEGAN FLUCTUATING 900 LBS. NR 2 ENGINE FUEL CONTROL HAS A LEAK IN THE P3 BELLOWPHRAM. REMOVED AND REPLACED P3 BELLOWPHRAM. GROUND POWER RUN OPS CHECKED NORMAL. 1L72 4T4 T A8SW E4WE 19960112002871996011200287EU 1996 1 12 96ZZZM18 119951128A2731SD3456031XA CABLE ASSY STBROSSD3 SD360 8100606EU ELEVATOR TRIM BROKEN AS PCAAO OTHER O OTHER APAPPROACH 1 EA13711PM SH3715 FLT NR 3809 - SAIPAN TO ROTA - WHILE ON SHORT FINAL TO RUNWAY 9 AT ROTA, THE ELEVATOR TRIM WHEEL WOULD NOT TRIM THE ELEVATOR PROPERLY. THE AIRCRAFT WAS LANDED SAFELY. MAINTENANCE WAS CALLED IN FROM SAIPAN. OPEN AIRCRAFT FOR INSPECTION, AT FR315 TAILPLANE. THE FOLLOWING CABLE WAS FOUND BROKEN (P/N SD3-45-6031XA), LOWER MID ELEVATOR TRIM CABLE. 2H72 4T A41EU 19960112002881996011200288NM 1996 1 12 96ZZZM19 119951011A2436B003063 VOLTAGE REG PIPER PA60 PA60600 7106001NM RT ALT FAILED A ECBAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL09300SK 600355127 AIRCRAFT EXPERIENCED ELECTRICAL SYSTEM FAILURE IN FLIGHT. INVESTIGATION REVEALED THAT THE RIGHT ALTERNATOR HAD BEEN PUTTING OUT FULL VOLTAGE, AND WAS PROBABLY FULL FIELDED. SUBMITTER STATES, SUSPECT DEFECTIVE VOLTAGE REGULATOR, COMPONENTS DAMAGED TOO BADLY TOO TELL. ADDITIONALLY, THE RIGHT OVER VOLTAGE RELAY FAILED, POSSIBLY A RESULT OF THE EXTREME OVERVOLTAGE CONDITION. THE FOLLOWING COMPONENTS WERE DAMAGED AND SUBSEQUENTLY REPAIRED OR REPLACED; BATTERY, COMM 1, COMM 2, AUDIO PANEL, MARKER BEACON, HSI, DME, ADF, FUEL CONDITIONER, DE-ICE BOOT CONTROLLER, MISC LIGHTS, LORAN, WX RADAR. 1M72 3O RTA17WE 19960112002891996011200289CE 1996 1 12 96ZZZM20 119951209A32422117411 BRAKE BFGOODRICH MTSBSIMU2 MU2B36 5780412CE RT MLG BURNED A MUAAO OTHER M OVER TEMP LDLANDING 1 GL23305CW 658 667 ON LANDING AT YIP, AIRCRAFTS RIGHT MAIN BRAKE WAS DRAGGING. RESUTLED IN FLAT SPOT ON TIRE AND OVERHEATED BRAKE ASSEMBLY. WHEEL AND BRAKE REPLACED WITH SERVICEABLE UNITS. BRAKE HYDRAULIC SYSTEM BLED TO REMOVE ANY CONTAMINATION. SYSTEM OPS CHECKED GOOD. SUBMITTER STATES, SUSPECT WATER IN BRAKE SYSTEM CAUSING BRAKE TO DRAG. 1H72 3T RTA10SW 19960112002901996011200290NM 1996 1 12 96ZZZM21 119951216A3260 SWITCH WIRE BOEING727 72751C 1384015NM NLG BROKEN A RYNAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 CE07436EX 19289 DURING LANDING AT MKE, GEAR EXTENSION FAILED TO GET A DOWN INDICATION ON THE NOSE GEAR. CYCLED GEAR ONCE WITH SAME RESULTS. COMPLIED WITH GEAR MANUAL EXTENSION. MADE FLYBY AND MAINTENANCE VERIFIED GEAR APPEARED DOWN. AIRCRAFT WAS LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE AT NOSE GEAR DOWN AND LOCKED SWITCH PIN 'C'. 2L73 4F A3WE 19960112002911996011200291NE 1996 1 12 96ZZZM22 219951216A7230 COMPRESSOR BLADE BOEING727 727151C 138404VNM PWA JT8 JT8D7B 52053NE NR 3 ENGINE DAMAGED A RYNACE ABORTED TAKEOFF ENGINE SHUTDOWN E VIBRATION/BUFFET TOTAKEOFF 1 CE07432EX 19867 649667 DURING TAKEOFF ROLL AT BUF, A VIBRATION WAS NOTED IN THE NR 3 ENGINE. THE TAKEOFF ROLL WAS REJECTED AT 60 KNOTS. THE ENGINE WAS SHUTDOWN AND AIRCRAFT TAXIED BACK TO RAMP WITHOUT INCIDENT. FOUND EXTENSIVE DAMAGE TO THE C-1 FAN BLADES. REPLACED ENGINE. 2L73 4F4 F A3WE E2EA 19960112002921996011200292WP 1996 1 12 96ZZZM23 119951211A53119923406502 FRAMES DOUG DC9 DC951 3022051WP LT/RT BS 734 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13669HA40457 47654 HNL - DURING D-CHECK AT SBA, FOUND FUSELAGE SIDEWALL STATION FRAME HAS 1.5 INCH CRACK AT FUSELAGE STATION 734 LEFT AND A 1 INCH CRACK AT FUSELAGE STATION 734 RT. THE CRACKS ARE IN THE RADIUS AT THE LOWER END OF THE FLOOR BEAM ATTACHMENTS. THESE ARE PSE 53.09.013 AND 014 AFFECTED BY AD 94-03-01 RELATIVE TO THE SID PROGRAM. FABRICATED AND INSTALLED STEEL ANGLES PER SRM 53-03 FIG 16 SECTION Q-Q. CRACKS WERE STOP DRILLED. REFER TO DACO FAX MIS 6754 DLP (SRM 53-03, FIG 16, 505). ALTERNATE METHOD OF COMPLIANCE WITH THE REPAIR REQUIREMENT OF AD 94-03-01 AFFECTING PSE, 53-09-013 AND 53-09-014. REFERENCE HALA95172. 2L72 4F A6WE 19960112002931996011200293NM 1996 1 12 96ZZZM24 119951205A2910112151072 VALVE BOEING727 72751C 1384015NM A-SYSTEM HYD LEAKING A RYNAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CE07435EX 19288 ON APPROACH INTO SAN, AS THE LANDING GEAR WAS EXTENDED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED LEFT HYDRAULIC FLOW REGULATOR VALVE. INSPECTED A-SYSTEM HYDRAULIC PUMPS AND FILTERS. SERVICED HYDRAULIC SYSTEM. OPS CHECK GOOD. (M) 2L73 4F A3WE 19960112002941996011200294NE 1996 1 12 96ZZZM25 219951207A7321 EEC CONNECTOR DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE LT ENGINE DIRTY A VNAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 GL07328JS 3030 FLT NR 4038 - CREW WAS ALERTED BY ELECTRONIC ENGINE CONTROL FAIL INDICATION LEFT SIDE. ELECTED TO RETURN TO GATE. OUT STATION MAINTENANCE CLEANED THE EEC CANNON PLUG CONNECTORS IAW MM 72-00-00. GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA45NM E20NE 19960112002951996011200295CE 1996 1 12 96ZZZM26 119951211A3222 STRUT LEAR 35 35A 5170602CE NLG LEAKING A AOQAO OTHER K FLUID LOSS APAPPROACH 1 EA11717JB 348 229 DURING APPROACH TO TOL, EXTENDED LANDING GEAR AND NOSE GEAR, UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR, NORMAL DOWN AND LOCKED INDICATION. CONTACTED TOL TOWER TO CONFIRM NOSE GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENT. NOSE GEAR STRUT DEFLATED AND LEAKING HYDRAULIC FLUID. REPLACED NOSE STRUT SEALS, SERVICED STRUT. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A10CE 19960112002961996011200296EU 1996 1 12 96ZZZM27 119951116A71107271110605 COWLING SAAB SF340 340B 7860101EU LT ENGINE DENTED A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE05363BE 340B293 FLT NR 4590 - JUST AFTER TAKEOFF, THE FLIGHT CREW NOTED THAT THE RIGHT OUTBOARD FORWARD COWLING WAS NOT SECURED. THE AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE INSPECTED THE COWLING STRUCTURE AND FOUND ONLY THE DOORS WERE DAMAGED. THE RIGHT INBOARD AND OUTBOARD FORWARD COWLING DOORS WERE REMOVED AND REPLACED. THE AIRCRAFT WAS FOUND SAFE FOR FERRY FLIGHT FROM PHL TO PSM FOR FINAL REPAIRS OF THE MINOR DENTS ON THE NACELLE AND WING AREA. FINAL REPAIRS WERE COMPLETED IN PSM AND AIRCRAFT WAS RELEASED TO SERVICE. REFERENCE PLG112095E1. 2L72 4T RTA52EU 19960112002971996011200297NE 1996 1 12 96ZZZM28 219951201A7510320115 FUEL HEAT VLV DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE LT ENGINE INOP A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11935VV 47534 676203 ON FLT NR 248 - ATL- AIRCRAFT RETURN, AFTER DEPARTURE THE LEFT FUEL HEAT CAME ON AND STAYED ON, DID NOT EXCEED OIL TEMP LIMITS. REMOVE AND REPLACE FUEL HEAT VALVE ON LEFT ENGINE PER MM 73-11-2, OPS CHECK NORMAL. (M) 2L72 4F4 F A6WE E2EA 19960112002981996011200298WP 1996 1 12 96ZZZM29 119951021A5244 DOOR DOUG DC9 DC932 3022066WP EXT POWER NOT CLOSED A VJ6AA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11910VJ 47277 ON FLT 530 - ATL - AIRCRAFT EXPERIENCED A VIBRATION ON THE LEFT SIDE OF THE AIRCRAFT BY THE COCKPIT. AIRCRAFT RETURNED. CHECKED AROUND THE NOSE GEAR AREA AND FOUND THE EXTERNAL POWER DOOR PANEL LEFT OPEN AND CLOSED DOOR. 2L72 4F A6WE 19960112002991996011200299EU 1996 1 12 96ZZZM30 119951126A3260622800200 UPLOCK SWITCH HONEYWELL BAG JETSTMJETSTM3101 1500215EU LT MLG DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07852JS 724 FLT NR 4039 - AFTER TAKEOFF LEFT MAIN LANDING GEAR FAILED TO SHOW TO BE UP AND LOCKED. CREW CYCLED THE ONCE, DID NOT SOLVE PROBLEM. CREW ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT-MX INSPECTED AIRCRAFT AND DISCOVERED THE LEFT MAIN LANDING GEAR UPLOCK MICROSWITCH TO BE DEFECTIVE. REPLACED MICROSWITCH IAW MM 32-10-00. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA21EU 19960112003001996011200300EU 1996 1 12 AALA951829 119951019A3230D226550002 DAMPER MESSIER AIRBUS300 A300B4605R 3930308EU LT MLG BENT ROD A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW077062A 474 MIA - FLT NR 1901 - AFTER TAKEOFF MIA, UNABLE TO RETRACT LANDING GEAR. AIRCRAFT RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS FOUND. SYSTEM OPERATIONAL CHECKED NORMAL. (M) 2L72 4F RTA35EU 19960112003011996011200301EU 1996 1 12 AALA951865 119951025A2916C19ES0020 HYD RESERVOIR LUCAS AIRBUS300 A300B4605R 3930308EU YELLOW SYS DEFECTIVE A AALAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SW0711060 470 SDQ - FLT 1266 - AFTER T/O SDQ, SMOKE NOTED IN CABIN AND COCKPIT AND YELLOW HYD SYSTEM QUANTITY NOTED TO HAVE DECREASED. A/C RETURNED TO SDQ AND LANDED WITHOUT INCIDENT, CHECKED WHEEL WELLS FOR HYDRAULIC LEAKS W/NO DEFECTS FOUND. SERVICED YELLOW HYD SYSTEM AND ACCOMPLISHED GROUND ENG RUN WITH NO DEFECTS FOUND. A/C REDEPARTED AND SMOKE AGAIN NOTED IN CABIN AND COCKPIT, BUT NO HYDRAULIC QUANTITY DECREASE. AIRCRAFT RETURNED SDQ AND LANDED WITHOUT INCIDENT. REPLACED YELLOW HYDRAULIC SYSTEM RESERVOIR, REPLACED SMOKE DETECTOR IN LOWER AVIONICS COMPARTMENT AND REPLACED COALESCER BAGS ON BOTH AIR CYCLE MACHINES. AIRCRAFT FUNCTIONAL CHECK FLT AND MX FERRY SDQ/MIA WITH NO DEFECTS FOUND. SYS OPS CHECKED NORMAL. (M)2L72 4F RTA35EU 19960112003021996011200302NM 1996 1 12 AALA951878 119951031A3350P2010031303 LIGHT BOEING767 767223 1385123NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07315AA 22317 SFO - DURING OVERNIGHT CHECK, RIGHT AFT DOOR EMERGENCY EXIT BULKHEAD LIGHT INOPERATIVE. REPLACED RIGHT AFT EMERGENCY EXIT BULKHEAD LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003031996011200303WP 1996 1 12 AALA951879 119951101A3350A3030398101 CONNECTOR DOUG DC10 DC1010 3022110WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07160AA 46710 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE AFT OF CENTER GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE BY CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19960112003041996011200304NM 1996 1 12 AALA951886 119951103A33508100022601 LIGHT BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SJC - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEAT 2H AND AT PAX SEATS 7H THROUGH 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 2H AND RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT ROW 20H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003051996011200305NM 1996 1 12 AALA951887 119951104A33508100022601 LIGHT BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07368AA 25195 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 37E THROUGH 41E INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLIES AT PAX SEATS 37E THROUGH 41E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003061996011200306NM 1996 1 12 AALA951888 119951105A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07358AA 24039 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 11B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT 11B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003071996011200307NM 1996 1 12 AALA951895 119951106A3350A3030398101 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07613AA 24489 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROW 1E AND 15D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTORS AT PAX SEAT ROWS 1E AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003081996011200308NM 1996 1 12 AALA951919 119951110A3397 WIRE BOEING767 767323 1385205NM CABIN CHAFED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07388AA 27448 JFK - DURING OVERNIGHT CHECK, CIRCUIT BREAKER FOR EMERGENCY LIGHTS STANDBY B1-905 POPPING. REPAIRED CHAFED WIRE (L2712L12) AT OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003091996011200309NM 1996 1 12 AALA951920 119951110A3350P12068 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07388AA 27448 JFK - DURING OVERNIGHT CHECK, EMERGENCY LIGHT SYSTEM FAILED TEST IN COCKPIT. RESECURED LOOSE CANNON PLUG P1-2068 AT MID CABIN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003101996011200310NM 1996 1 12 AALA951923 119951109A3350A30330398101 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07692AA 26972 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT EXIT LIGHT AT RIGHT MID DOOR INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT EXIT CONNECTOR AT RIGHT MID CABIN DOOR CROSS AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003111996011200311NM 1996 1 12 AALA951925 119951109A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RIGHT AISLE JUST FORWARD AND AFT OF MID GALLEY INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR BY PAX SEAT ROW 18H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003121996011200312NM 1996 1 12 AALA951934 119951111A3397 WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07691AA 25697 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING IN THE AFT CABIN DIM. REPAIRED BROKEN WIRE ON THE EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003131996011200313NM 1996 1 12 AALA951936 119951111A3397 WIRE BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE K FLUID LOSS ININSP/MAINT 1 SW07633AA 24591 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT STATION 880L INOPERATIVE. REPAIRED GROUND WIRE, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003141996011200314NM 1996 1 12 AALA951946 119951113A3350 CONNECTOR BOEING767 767323 1385205NM CABIN NEED SECURING A AALAK NONE L NO TEST ININSP/MAINT 1 SW07379AA 25448 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 20B INOPERATIVE. RECONNECTED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003151996011200315NM 1996 1 12 AALA951947 119951113A33508100022607 LIGHT ASSY BOEING767 767323 1385205NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07380AN 25449 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 17B INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003161996011200316NM 1996 1 12 AALA951960 119951115A3397 WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739365 24046 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS, BETWEEN SEATS 26H-34H, SEATS 42H-2R DOOR, AND BELOW AFT GALLEY FLIGHT ATTENDANTS SEAT, INOPERATIVE. REATTACHED WIRE BETWEEN SEATS 26H-34H. REPAIRED WIRE ON FLOOR TRACK LIGHTING BETWEEN 42H AND 2R DOOR, AND WIRE AFT OF FLIGHT ATTENDANTS SEATS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003171996011200317EU 1996 1 12 AALA951963 119951116A3397 WIRE AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770054 461 MIA - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 11B THROUGH 23B INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE AT SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960112003181996011200318EU 1996 1 12 AALA951977 119951118A213081050B020100 RELIEF VALVE AIRBUS300 A300B4605R 3930308EU ACM COMPT DEFECTIVE A AALAB EMER. DESCENT J WARNING INDICATION CRCRUISE 1 SW0780052 460 TUL - FLT 9186 - DURING FUNCTIONAL AT FL 370 - AMBER SAFETY VALVE INDICATED OPEN AND CABIN ALTITUDE BEGAN TO CLIMB. NR 1 PRESSURE REGULATOR FAULTED. MANUALLY SWITCHED TO NR 2 REGULATOR AND REGAINED CONTROL OF CABIN PRESSURIZATION. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT LANDED TUL WITHOUT INCIDENT. REPLACED NR 2 SAFETY RELIEF VALVE. REPLACED NR 1 AND NR 2 CABIN PRESSURIZATION CONTROLLERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960112003191996011200319WP 1996 1 12 AALA951978 119951117A3350A3060720101 CONDUCTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07210AA 49161 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT FLAT CONDUCTOR WIRE BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960112003201996011200320NM 1996 1 12 AALA951979 119951119A3350A3030398101 CONNECTOR BOEING727 727223 1384074NM ROW 17D LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07865AA 21370 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 17D INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960112003211996011200321EU 1996 1 12 AALA951981 119951120A3350A3030398101 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770072 515 JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 18HJ AND 22HJ INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 18HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960112003221996011200322NM 1996 1 12 AALA951983 119951121A3350 CONNECTOR BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739365 24046 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT LAST FOUR SEAT ROWS OF AFT CABIN RIGHT SIDE INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003231996011200323NM 1996 1 12 AALA951984 119951121A3350 CONNECTOR BOEING767 767323 1385205NM SEAT 4B-12B LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07373AA 25200 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 4B THROUGH 12B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003241996011200324NM 1996 1 12 AALA951985 119951122A3350 STRIP BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07632AA 24590 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS FROM OVERWING EXIT TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP BETWEEN OVERWING EXIT AND FORWARD GALLEY. ALSO, REPLACED FORWARD EPM BATTERY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003251996011200325NM 1996 1 12 AALA951986 119951126A33508100022601 LAMP BOEING767 767323 1385205NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 4H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT PAX SEAT 4H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003261996011200326NM 1996 1 12 AALA951987 119951127A3350A3060720101 CONDUCTOR BOEING757 757223 1384957NM CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07659AA 24617 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 9 THROUGH 17 AND SIDEWALL DIRECTIONAL ARROW LIGHTS AT L2 AND R2 DOORS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT FLAT CONDUCTOR WIRE BY CENTER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960112003271996011200327NM 1996 1 12 AALA951988 119951126A3350 CONNECTOR BOEING767 767323 1385205NM ROWS 36H-41H LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0739364 24045 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS BETWEEN PAX SEAT ROWS 36H THROUGH 41H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT SIDEWALL CONNECTOR AT PAX SEAT ROW 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003281996011200328NM 1996 1 12 AALA951990 119951129A3397 WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW077375A 25202 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS ON LEFT SIDE OF FIRST CLASS AND BUSINESS CLASS CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003291996011200329EU 1996 1 12 AALA951991 119951130A3350A3030398101 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0770073 516 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 16B TO 23B INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960112003301996011200330NM 1996 1 12 AALA952028 119951202A3397 WIRE BOEING767 767323 1385205NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07351AA 24032 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING LEFT SIDE IN FIRST CLASS INOPERATIVE. RECONNECTED WIRES ON EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003311996011200331NM 1996 1 12 AALA952029 119951202A3350 CONNECTOR BOEING767 767323 1385205NM SEAT ROW 3H DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07386AA 27060 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 3H INOPERATIVE. REPLACED CONNECTOR AT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003321996011200332EU 1996 1 12 AALA952030 119951202A3397 WIRE FOKKERF28 F28MK0100 4990807EU CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW071412A 11370 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED WIRES ON EMERGENCY EXIT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19960112003331996011200333NM 1996 1 12 AALA952031 119951203A3350 CONNECTOR BOEING767 767323 1385205NM ROWS 40-43AB LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07369AA 25196 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT ROWS 40 TO 43AB INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH TRACK CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960112003341996011200334NM 1996 1 12 AALA952032 119951204A33505013CW LIGHT BOEING727 727227 1384078NM GALLEY DOORS DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07719AA 20612 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS OVER FORWARD GALLEY AND AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER FORWARD AND AFT GALLEY DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960112003351996011200335NM 1996 1 12 ASAA9510108 119951123A3350900835A BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19960112003361996011200336NM 1996 1 12 ASAA9510109 119951126A335086210144 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19960112003371996011200337NM 1996 1 12 ASAA9510112 119951215A2782654465113 ACTUATOR BOEING737 737298C 1384490NM NR 6 SLAT MALFUNCTIONED A ASAAA UNSCHED LANDING F FLT CONT AFFECTED TOTAKEOFF 1 NM01745AS 20794 ANC - FLT NR 145 - AIR TURN BACK DUE TO NR 6 SLAT REMAINING IN EXTENDED POSITION AFTER FLAPS RAISED DURING TAKEOFF. CYCLED FLAPS AND USED WING ANTI-ICE. NO CHANGE AND SLIGHT ROLL WITH FLAPS RETRACTED. FLAPS AND LEADING EDGE DEVICES OPERATED NORMALLY IN THE EXTENDED POSITION. LANDED WITHOUT INCIDENT. REPLACED NR 6 SLAT ACTUATOR AND OPS LEAK CHECKED NORMAL. (M) 2L72 4F RTA16WE 19960112003381996011200338NM 1996 1 12 ASAA9510115 119951217A323069141067 CYLINDER BOEING737 737290C 138448VNM NLG FAILED A ASAAO OTHER J WARNING INDICATION APAPPROACH 1 NM01742AS 23136 ANC - FLIGHT 44 - DURING APPROACH, THE NOSE LANDING GEAR FAILED TO EXTEND. RECYCLED GEAR AND ALL LANDING GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. CLEANED AND LUBED NOSE LANDING GEAR ASSEMBLY. REPLACED NOSE LANDING GEAR TRANSFER CYLINDER, PERFORMED GEAR RETRACTION, SERVICED STRUT AND OPERATED NORMALLY. (M) 2L72 4F A16WE 19960112003391996011200339NM 1996 1 12 ASAA9540094 119951116A3350 END STOP BOEING737 7374Q8 NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED END STOP SECTION AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003401996011200340NM 1996 1 12 ASAA9540095 119951120A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01776AS 25109 JNU - DURING MAINTENANCE CHECK, THE AFT 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003411996011200341NM 1996 1 12 ASAA9540096 119951121A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01774AS 25107 SEA - DURING MAINTENANCE CHECK, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003421996011200342NM 1996 1 12 ASAA9540097 119951123A3350900835A BATTERY PACK BOEING737 7374Q8 NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01779AS 25111 SEA - DURING MAINTENANCE CHECK, ALL EMERGENCY LIGHTS AFT OF ROW 25 WERE FOUND INOPERATIVE. REPLACED AFT BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003431996011200343NM 1996 1 12 ASAA9540098 119951124A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - DURING MAINTENANCE CHECK, THE FORWARD 2 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003441996011200344NM 1996 1 12 ASAA9540099 119951126A3350S417N50914 LAMP BASE BOEING737 737490 1384715NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01767AS 27081 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS FROM ROW 22 AFT WERE FOUND INOPERATIVE. REPLACED LAMP BASE ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003451996011200345NM 1996 1 12 ASAA9540100 119951128A521090100721 SNUBBER BOEING737 737490 1384715NM L1 DOOR DEFECTIVE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01767AS 27081 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. REPLACED DOOR SNUBBER ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003461996011200346NM 1996 1 12 ASAA9540101 119951203A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - FLT NR 279 - CREW REPORTED, AFT MOST SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTING WAS INOPERATIVE. INSTALLED NEW LENS COVER AND SECURED TRACK AND WIRING, LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003471996011200347NM 1996 1 12 ASAA9540102 119951204A33505417N50914 LIGHT BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01755AS 25096 JNU - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED 4TH FROM LAST LAMP BASE AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003481996011200348NM 1996 1 12 ASAA9540103 119951205A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01760AS 25098 SEA - FLT NR 62 - CREW REPORTED AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960112003491996011200349WP 1996 1 12 ASAA9580273 119951117A3350S103 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19960112003501996011200350WP 1996 1 12 ASAA9580275 119951124A3350S103 BATTERIES DOUG DC9 DC982 3022082WP CABIN LOW CHARGE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01957AS 49126 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE TAILCONE AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19960112003511996011200351WP 1996 1 12 ASAA9580277 119951125A33501001191 LIGHT DOUG DC9 DC983 3022083WP CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01969AS22378 53063 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19960112003521996011200352NM 1996 1 12 BJNA951201 119951204A33506104781 BATTERY PACK BOEING737 737214 138446RNM CABIN INOPERATIVE A BJNAK NONE L NO TEST ININSP/MAINT 1 WP11457TM 20156 EMERGENCY EXIT LIGHTS FORWARD BATTERY PACK LOW. REMOVED AND REPLACED FORWARD EMERGENCY EXIT LIGHT BATTERY PACK PER BMM 33-51-51. OPS CHECK GOOD AT THIS STATION. (M) 2L72 4F A16WE 19960112003531996011200353NM 1996 1 12 CAL951078 119951201A3610652244131 DUCT BOEING737 737217 1384464NM NR 2 ENGINE RUPTURED A CALAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS CLCLIMB 1 SW0912231 19885 FLT NR 1495 - BOS - THE NR 2 ENGINE SURGED ON TAKEOFF ROLL AT V1. THE TAKEOFF WAS CONTINUED AND ENGINE POWER WAS REDUCED TO KEEP EGT BELOW REDLINE. THE NR 2 ENGINE WOULD ONLY DEVELOP ABOUT 50 PERCENT POWER. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE NR 2 ENGINE 13TH STAGE CROSSOVER DUCT RUPTURED. THE 13TH STAGE DUCT WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND ALL PARAMETERS WERE WITHTIN LIMITS WITH NO DUCT LEAKS NOTED. (M) 2L72 4F A16WE 19960112003541996011200354NM 1996 1 12 CAL951079 119951201A2170 CLAMP BOEING727 727227 1384078NM RT PACK BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW097975419274 21363 FLT NR 682 - ATL - THE AIRCRAFT WOULD NOT HOLD PRESSURE WITH RIGHT PACK BELOW 120 DEGREES WHILE ENROUTE FROM RSW TO EWR. PRESSURE COULD NOT BE CONTROLLED USING AUTO, STANDBY, OR MANUAL MODE. THE PRESSURE ABNORMAL CHECKLIST WAS FOLLOWED AND THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT WATER SEPARATOR CANISTER CLAMP BROKEN. THE CANISTER ASSEMBLY (P/N 17805021) WAS REPLACED. IN ADDITION, THE RIGHT 35 DEGREE VALVE WAS STICKING. THE VALVE CONNECTIONS WERE CLEANED. THE AIRCRAFT WAS PRESSURIZED AND DECAY CHECK WAS GOOD PER MM 21-31-0. (M) 2L73 4F A3WE 19960112003551996011200355NE 1996 1 12 CAL951080 219951201A7230 SUPPORT SHELF DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE NR 1 ENGINE BROKEN A CALACD ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW091681526642 49113 717372 EWR - FLT 0428 - TAKEOFF WAS ABORTED AT LESS THAN 60 KNOTS AFTER TOWER REPORTED SPARKS WERE COMING FROM THE LEFT ENGINE TAILPIPE. MAINTENANCE PERFORMED A BORESCOPE INSPECTION OF THE NR 1 ENGINE AND FOUND DAMAGE TO THE 6TH STAGE COMPRESSOR BLADES. THE NR 1 ENGINE WAS REMOVED AND REPLACED. SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT: TEAR DOWN FINDINGS REVEALED 8TH STAGE STATOR SUPPORT SHELF BROKE AND CAUSED COMPRESSOR DAMAGE. (X) 2L72 4F4 F A6WE E9NE 19960112003561996011200356NE 1996 1 12 CAL951081 219951203A72609699M16P03 BEARING DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE NR 2 ENGINE FAILED A CALAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW0983071492952421 48293 57696 FLT NR 28 - LGW - THE NR 2 ENGINE WAS SHUT DOWN FOR LOSS OF OIL WHILE EN ROUTE TO LGW. THE ENGINE WAS SHUT DOWN WITH POSITIVE OIL PRESSURE AND THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. PRELIMINARY FINDINGS REVEALED THE TRANSFER GEARBOX HAD SEPARATED FROM THE ENGINE. PRIMARY CAUSE OF FAILURE WAS DUE TO FAILURE OF LOWER RADIAL DRIVESHAFT BEARING. (M) 2L73 4F4 F A22WE E23EA 19960112003571996011200357NM 1996 1 12 CAL951082 119951120A5320 DOUBLER BOEING737 737217 1384464NM FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091223173264 19885 GSO - INSPECTION FOUND A 1.25 INCH CRACK IN THIRD LAYER OF FUSELAGE INTERNAL DOUBLER AT AFT GALLEY DOOR FORWARD LOWER CORNER. THE CRACKED AREA WAS CUTOUT. A DOUBLER AND TRIPLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2. (M) 2L72 4F A16WE 19960112003581996011200358NM 1996 1 12 CAL951083 119951028A5314 KEEL BEAM BOEING727 727232 1384082NM BS 740 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09777806579465794 20635 INSPECTION FOUND A 1 INCH CRACK IN KEEL BEAM, AT BS 740 AND STRINGER 28R, IN AIRCRAFT BAY. THE CRACK WAS TRIMMED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03180. (M) 2L73 4F A3WE 19960112003591996011200359NM 1996 1 12 CAL951084 119951109A5320 DOUBLER BOEING727 727232 1384082NM BS 714 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND SKIN DOUBLER CORRODED AT STRINGER 14R AND BS 714. THE CORRODED SECTION OF SKIN DOUBLER WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M) 2L73 4F A3WE 19960112003601996011200360NM 1996 1 12 CAL951085 119951108A5311 FRAME BOEING727 727232 1384082NM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND AIRCRAFT BAY AFT FRAME CORRODED AT PANEL NR 3458R, BS 740. THE CORRODED SECTION OF FRAME WAS REMOVED. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2L73 4F A3WE 19960112003611996011200361NM 1996 1 12 CAL951086 119951031A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 840 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A .5 INCH CRACK IN LATERAL FLOOR BEAM WEB AT CABLE PASS THROUGH, BS 840, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960112003621996011200362NM 1996 1 12 CAL951087 119951031A5320 L-ANGLE BOEING727 727232 1384082NM BS 804 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A .75 INCH CRACK IN ATTACH L-ANGLE AT LEFT BS 804 LATERAL FLOOR BEAM WEB TO LBL 46 LONGITUDINAL FLOOR BEAM WEB. THE CRACK WAS LOCATED AT THE LIGHTENING HOLE ON AFT SIDE. THE CRACK ANGLE WAS REMOVED. A NEW L-ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-2. (M) 2L73 4F A3WE 19960112003631996011200363NM 1996 1 12 CAL951088 119951101A5320 THRESHOLD BOEING727 727232 1384082NM BS 560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION AT FORWARD CARGO DOOR THRESHOLD, STATION 560. THE CORROSION WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960112003641996011200364NM 1996 1 12 CAL951089 119951029A5330 SKIN BOEING727 727232 1384082NM BS 430 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION ON LOWER FUSELAGE BELLY SKIN AT STATION 430, RBL 15. THE CORRODED SECTION WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 53-30-3. (M) 2L73 4F A3WE 19960112003651996011200365NM 1996 1 12 CAL951090 119951031A5320 DOUBLER BOEING727 727232 1384082NM BS 826 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A 1 INCH CRACK IN DOUBLER ON AFT SIDE OF BS 826 LATERAL FLOOR BEAM WEB, LBL 54. THE CRACK WAS STOP DRILLED. A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960112003661996011200366NM 1996 1 12 CAL951092 119951029A5311 FRAME BOEING727 727232 1384082NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND FRAMES CORRODED AT NUT PLATES FOR LOWER FUSELAGE PANEL IN AIRCRAFT BAY AT STA 720 C/D, LBL 10 TO RBL 10. THE CORROSION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960112003671996011200367NM 1996 1 12 CAL951093 119951031A5311 FRAME BOEING727 727232 1384082NM BS 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 CORROSION WAS FOUND AT STATION 1130 FRAME DURING INSPECTION ON RIGHT FUSELAGE WALL. THE CORROSION EXTENDED ABOVE AND BELOW FLOOR LEVEL. THE CORRODED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-2, AND 53-10-4. (M) 2L73 4F A3WE 19960112003681996011200368NM 1996 1 12 CAL951094 119951030A5713 STRINGER BOEING727 727232 1384082NM WS 656.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A .5 INCH CRACK IN LEFT WING STRINGER FLANGE AT WS 656.5. THE CRACK WAS STOP DRILLED. REPAIR CHANNELS WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M) 2L73 4F A3WE 19960112003691996011200369NM 1996 1 12 CAL951095 119951030A5313 STRINGER BOEING727 727232 1384082NM WS 629 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A 2 INCH IN THE STRINGER FLANGE AT LT WS 629. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, AND 51-20-4. (M) 2L73 4F A3WE 19960112003701996011200370NM 1996 1 12 CAL951096 119951108A5321 FLOOR PANEL BOEING727 727232 1384082NM BS 950 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 THE RIGHT FLOOR SUPPORT PANEL WAS FOUND CORRODED IN THE AFT CARGO COMPARTMENT AT BS 950-950F. THE FLOOR SUPPORT PANEL WAS REMOVED. A NEW FLOOR SUPPORT PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-6, AND 51-10-2. (M) 2L73 4F A3WE 19960112003711996011200371NM 1996 1 12 CAL951097 119951101A5320 INTERCOSTAL BOEING727 727232 1384082NM BS 680-700 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND THE INTERCOSTAL CORRODED AT BS 680-700 AND STRINGER 27R. THE INTERCOSTAL WAS REMOVED AND THE CORROSION WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2L73 4F A3WE 19960112003721996011200372NM 1996 1 12 CAL951098 119951028A5330 SKIN BOEING727 727232 1384082NM BS 1342.4 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND THE CENTER ENGINE SUPPORT STRUCTURE SKIN CORRODED AT STATION 1342.4, LEFT SIDE. THE CORRODED SECTION OF SKIN WAS REMOVED. A NEW SECTION OF SKIN AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 54-30-3 AND ECRA 5330-02330. (M) 2L73 4F A3WE 19960112003731996011200373NM 1996 1 12 CAL951099 119951031A5320 STRINGER BOEING727 727232 1384082NM BS 1030-1166 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION ON FLOOR SUPPORT STRINGER NR 9 AT BS 1030-1166. THE CORRODED SECTIONS WERE REMOVED. L-ANGLES AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2. (M) 2L73 4F A3WE 19960112003741996011200374NM 1996 1 12 CAL951100 119951104A5320 INTERCOSTAL BOEING727 727232 1384082NM BS 1130-1148 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION ON INTERCOSTAL AT BS 1130-1148, LT SIDE. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. (M) 2L73 4F A3WE 19960112003751996011200375NM 1996 1 12 CAL951101 119951110A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 460 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION ON FLOOR BEAM AT BS 460, RBL 45. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. (M) 2L73 4F A3WE 19960112003761996011200376NM 1996 1 12 CAL951102 119951029A5532 SKIN BOEING727 727232 1384082NM VERTICAL CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER, 24 INCHES FROM LEADING EDGE. THE CRACK WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-6. (M) 2L73 4F A3WE 19960112003771996011200377NM 1996 1 12 CAL951103 119951101A5330 SKIN BOEING727 727232 1384082NM BS 294 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND CORROSION ON SKIN AT BS 294, RBL 16, STRINGER 22R. THE SKIN WAS REPAIRED IAW SRM 51-10-6, 51-10-2, AND 51-30-2. (M) 2L73 4F A3WE 19960112003781996011200378NM 1996 1 12 CAL951104 119951031A5720 DOUBLER BOEING727 727232 1384082NM WS 656.5 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A 1.5 INCH CRACK IN RIB DOUBLER WS 656.50, NR 3 FUEL TANK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-5. (M) 2L73 4F A3WE 19960112003791996011200379NM 1996 1 12 CAL951105 119951030A5320 DOOR FRAME BOEING727 727232 1384082NM AFT ENTRY CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097778065794 20635 INSPECTION FOUND A 6 INCH CRACK IN AFT ENTRY DOOR FRAME ON LEFT SIDE BETWEEN THIRD AND FOURTH DOOR STOP FROM BOTTOM. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960112003801996011200380WP 1996 1 12 CAL951106 119951205A2910 B-NUT DOUG DC9 DC982 3022082WP RT HYD SYSTEM LOOSE A CALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SW0916815 49113 FLT NR 120 - LGA - THE RIGHT HYDRAULIC SYSTEM EXPERIENCED FLUID LOSS ON APPROACH TO LGA. POWER TO THE AUX AND RIGHT HYDRAULIC PUMPS WERE TURNED OFF. A RIGHT HYDRAULIC OFF APPROACH AND LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. THE RIGHT HYD SYSTEM RESERVOIR WAS SERVICED WITH FLUID. THE AIRCRAFT WAS JACKED AND THE LANDING GEAR, SPOILERS, FLAPS, AND SLATS WERE CYCLED. LEAKAGE WAS FOUND AT THE RIGHT LANDING GEAR CONTROL VALVE B-NUT. THE B-NUT WAS TIGHTENED. THE LANDING GEAR AND FLIGHT CONTROLS WERE CYCLED AGAIN SEVERAL TIMES WITH NO DEFECTS OR FLUID LOSS NOTED. (M) 2L72 4F A6WE 19960112003811996011200381WP 1996 1 12 CAL951107 119951206A335041B004AD073 BATTERIES DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914810 49264 FLT NR 0579 - EWR - INSPECTION FOUND THE FIRST CLASS CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES FOR THE FIRST CLASS OVERHEAD EMERGENCY LIGHT BATTERY PACK WERE REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2L72 4F A6WE 19960112003821996011200382NM 1996 1 12 CAL951108 119951026A5730 SKIN BOEING747 747230B 1384889NM WS 1330 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097801982102 20527 TLV - INSPECTION FOUND LOWER SKIN CORRODED ON LEFT WING AT WS 1330. A REPAIR ANGLE AND STRAP WERE INSTALLED IAW ENGINEERING ORDER MF MAN-B47-57-84000. (M) 2L74 4F A20WE 19960112003831996011200383NM 1996 1 12 CAL951109 119951112A575565B080995 FITTING BOEING747 747230B 1384889NM NR 5 SPOILER BROKEN A CALAK NONE O OTHER ININSP/MAINT 1 SW097801982102 20527 TLV - INSPECTION FOUND A LEFT WING NR 5 GROUND SPOILER ACTUATOR FITTING BROKEN. A REPAIR WAS INSTALLED IAW ECRA 5750-02392. (M) 2L74 4F A20WE 19960112003841996011200384NM 1996 1 12 CAL951110 119951113A5730 SKIN BOEING747 747230B 1384889NM WS 660 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097801982102 20527 TLV - INSPECTION FOUND CORROSION UNDER UPPER SKIN OF TOP FIXED FAIRING AT LEFT WING LEADING EDGE, WS 660. A TEE ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02. (M) 2L74 4F A20WE 19960112003851996011200385WP 1996 1 12 CAL951122 119951209A2120 AIR DISTR DOUG DC9 DC932 3022066WP CABIN SMOKE A CALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW09541NY 45793 FLT NR 1589 - CMH - SMOKE APPEARED IN CABIN ON ROTATION AND INITIAL CLIMB-OUT AND THEN WENT AWAY ON DEPARTURE FROM CMH. THE AIRCRAFT WAS RETURNED TO CMH. THE PASSENGERS WERE EVACUATED VIA THE JETWAY, AS A PRECAUTIONARY MEASURE. THE AIR CONDITIONING SYSTEM WAS TESTED AND NO DISCREPANCIES WERE NOTED. THE ACM OK LEVEL, APU, AND ENGINE BLEEDS WERE ALL CHECKED WITH NO TROUBLE FOUND. THE SMOKE COULD NOT BE DUPLICATED. THE AIRCRAFT HAD BEEN HEAVILY DE-ICED PRIOR TO TAKEOFF. SUBMITTER STATES, INGESTION OF DE-ICING FLUID WAS SUSPECT. (M) 2L72 4F A6WE 19960112003861996011200386WP 1996 1 12 CAL951126 119951211A3260 SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING TOTAKEOFF 1 SW0914534 47110 FLT NR 1512 - CLE - THE GEAR DOOR OPEN LIGHT REMAINED ON WITH GEAR UP AFTER TAKEOFF FROM CLE. CYCLING THE GEAR WAS OF NO HELP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO CLE THE DOOR OPEN LIGHT EXTINGUISHED. MAINTENANCE FOUND THE LEFT MAIN DOOR INBOARD SWITCH AT FAULT. THE LEFT DOOR SWITCH WAS REMOVED AND REPLACED IAW MM 32-60-3. OPERATION OF THE DOOR WARNING LIGHT SYSTEM CHECKED GOOD. (M) 2L72 4F A6WE 19960112003871996011200387WP 1996 1 12 CAL951127 119951211A3260 PROX SENSOR DOUG DC9 DC981 3022081WP RT MLG INOPERATIVE A CALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SW0937882 48027 FLT NR 0327 - EWR - THE RIGHT MLG RED LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH TO EWR. THE GEAR EMERGENCY EXTENSION LEVER WAS PULLED, BUT THE LIGHT REMAINED RED. A TOWER FLYBY WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. ALL CAWS UNSAFE WARNINGS ASSOCIATED WITH GEAR UP WERE RECEIVED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT GEAR DOWN AND LOCK PROXIMITY SENSOR PER MM 32-60-05. GEAR OPERATION AND INDICATION CHECKED GOOD. (M) 2L72 4F A6WE 19960112003881996011200388NM 1996 1 12 CAL951128 119951211A3350 FUSE BOEING727 727243 138408DNM CABIN BLOWN A CALAK NONE L NO TEST ININSP/MAINT 1 SW09571PE 21264 FLT NR 0631 - EWR - A PREFLIGHT INSPECTION, FOUND FORWARD SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE FROM ROW 1-7. MAINTENANCE FOUND A FUSE BLOWN ON FORWARD POWER SUPPLY. THE FUSE WAS REMOVED AND REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2L73 4F RTA3WE 19960112003891996011200389WP 1996 1 12 CKSA95146 119951212A32600080004005 PROX SWITCH BOX DOUG DC8 DC863F 302198FWP LANDING GEAR INOP A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23815CK33778 227 46151 KMSP - LANDING GEAR LATCHED LIGHT AND DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION. WHEN LANDING GEAR SELECTED DOWN, LEFT MAIN GREEN LIGHT ON INSTANTLY, RIGHT MAIN LANDING GEAR WOULD NOT EXTEND UNTIL IAS BELOW 160 KIAS. REMOVED AND REPLACED LANDING GEAR PROXIMITY SWITCH BOX SYSTEM. OPS CHECKED GOOD IAW DC-8 MM 32-10-0. INSPECTED AND TESTED RIGHT GEAR OPERATION IAW DC-8 MM 32-10-0. SYSTEM OPS CHECKED GOOD. (M) 2L74 4F 4A25 19960112003901996011200390WP 1996 1 12 CKSA95147 119951214A261257775621 FIRE LOOP DOUG DC8 DC852 3021922WP NR 2 ENGINE DIRTY A CKSAF ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 GL23810CK34797 45814 KBYH - AT APPROXIMATELY THREE MINUTES AFTER TAKEOFF WE HAD A FIRE WARNING AND BELL ON NR 2 ENGINE. WE PERFORMED EMERGENCY PROCEDURES FOR ENGINE FIRE. FIRE WARNING WENT OUT AFTER SECOND BOTTLE DISCHARGE. FOUND MOISTURE AND CORROSION AT SEVERAL FIRE LOOP CANNON PLUGS, CLEANED AND SECURED PLUGS, RAN ENGINE AND FOUND SEVERAL PNEUMATIC LEAKS. TIGHTENED CLAMPS TO FIX PNEUMATIC LEAKS, SWAPPED FIRE DETECTION AMPS FOR POSSIBLE FURTURE PROBLEMS. NR 2 FIRE WARNING OPS CHECKS GOOD IAW MM 26-4-1. (M) 2L74 4F 4A25 19960112003911996011200391 1996 1 12 CKSA95162 419951215A2210 AUTO PILOT DOUG DC8 DC8F55 3021928WP STAB TRIM MALFUNCTIONED A CKSAO OTHER J WARNING INDICATION CRCRUISE 1 GL236161M71170 45762 STABILIZER ELECTRIC TRIM (SLOW) RUNAWAY AFTER TAKEOFF (CIRCUIT BREAKERS PULLED) AUTO PILOT ENGAGED. SUBSEQUENT FLIGHT REVEAL NO FURTHER PROBLEMS. UNABLE TO DUPLICATE AUTO PILOT SYSTEM GROUND TESTS NORMAL IAW MM CHAPTER 22-1-0. (M) 2L74 4F 4A25 19960112003921996011200392WP 1996 1 12 CKSA95163 119951219A3260189915 PROX SW DOUG DC8 DC863F 302198FWP RT MLG SHORTED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23811CK38866 46147 KMIA - GEAR 'DOOR NOT LATCHED LIGHT' CAME ON IN FLIGHT. CAME ON DURING UPLATCH CHECK. CYCLED GEAR, LIGHT ON AGAIN. UPLATCH CHECKED AGAIN NO GOOD. REMOVED AND REPLACED RIGHT MAIN GEAR LANDING GEAR DOOR PROXIMITY SWITCH. PROXIMITY SWITCH TEST GOOD. FOUND RIGHT UPLATCH VERY STIFF LUBED UPLATCH AND PERFORMED GEAR RETRACTION. OPS CHECKED NORMAL IAW 32-30-0. (M) 2L74 4F 4A25 19960112003931996011200393WP 1996 1 12 EIAA9567 119951216A215068347811 SWITCH DOUG DC9 DC933F 302207AWP LT PACK FAILED A EIAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM09940F 47414 DEN - ON CLIMB-OUT AFTER PASSING 10,000 FEET, MASTER WARNING AND CABIN PRESS WARNING CAME ON. THE RIGHT PACK HAD TRIPPED AND THE LEFT PACK WAS NOT PUTTING OUT ENOUGH TO MAINTAIN CABIN PRESSURE, BEGAN TO GET SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND RETURNED TO DEN. REMOVED AND REPLACED LEFT A/C PACK 190 DEGREES TEMP SENSOR, SYSTEM FUNCTION CHECK ON LEFT AND RIGHT AIR CONDITIONS SYSTEMS NORMAL IAW DC9 MM 21-60-00. FAILURE OF THE 190 DEGREE LIMIT SWITCH CAUSED OVERHEATING OF LEFT SYSTEM WHICH EMITTED SMOKE IN THE COCKPIT. 2L72 4F A6WE 19960112003941996011200394NM 1996 1 12 EIAA9568 119951215A2612 FIRE LOOP BOEING747 747121 1384871NM NR 1 ENGINE MALFUNCTIONED A EIAAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 NM09474EV 19637 NR 1 ENGINE B-LOOP FAULT LIGHT ON IN FLIGHT, DID PRECAUTIONARY ENGINE SHUT DOWN BECAUSE NR 1 ENGINE A-LOOP SHOWS SPIKING INDICATION AND IS ENTERED ON DMI 792. AIRCRAFT RETURNED TO JFK. REPAIRED CONNECTOR AT LOWER FORWARD ELEMENT B-LOOP, OPS CHECK OK PER MM 26-11-02, A-LOOP DMI 792 IS CLEARED ON LOGPAGE F02736. (M) 2L74 4F A20WE 19960112003951996011200395NM 1996 1 12 EISA95443 119951203A5330 SKIN BOEING727 72731 1384010NM BS 259 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 HFEC INSPECTION REVEALS MATERIAL LOSS OF APPROXIMATELY 10-15 PERCENT AT BS 259, STRINGER 10R. REMOVED CORROSION, FABRICATED DOUBLER PER BAC DRAWING 69-62161. INSTALLED REPAIR PER BAC DRAWING 69-62161. (M) 2L73 4F A3WE 19960112003961996011200396NM 1996 1 12 EISA95445 119951203A5754 RIB BOEING727 72731 1384010NM NR 2 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 LEFT WING NR 2 SLAT HAS INBOARD RIB CRACKED WHERE ACTUATOR ROD END ATTACHES. INSTALLED DOUBLER PER SRM 57-50-03. (M) 2L73 4F A3WE 19960112003971996011200397NM 1996 1 12 EISA95451 119951201A5713 STRINGER BOEING727 72731 1384010NM WS 3835 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 LEFT WING 7TH STRINGER FROM AFT SPAR IS CRACKED IN TWO PLACES AT TOP OF RIB WS 383.5. FABRICATED REPAIR IAW SRM 57-10-4. (M) 2L73 4F A3WE 19960112003981996011200398NM 1996 1 12 EISA95453 119951201A5712 RIB BOEING727 72731 1384010NM WS 686.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 TWO CRACKS IN RT WING RIB NEAR LOWER FASTENER HOLES AT WS 686.5 AT 2ND STRINGER AFT OF FRONT SPAR. INSTALLED MANUFACTURED RIB PER SB 727-57-0127. (M) 2L73 4F A3WE 19960112003991996011200399NM 1996 1 12 EISA95456 119951201A5713 STRINGER BOEING727 72731 1384010NM WS 629.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 TWO CRACKS IN WING RIB AT WING STATION 629.5 LOWER FLANGE, 3RD STRINGER AFT OF FRONT SPAR. FABRICATED DOUBLER AND INSTALLED PER SRM 57-10-5. (M) 2L73 4F A3WE 19960112004001996011200400NM 1996 1 12 EISA95458 119951201A5713 STRINGER BOEING727 72731 1384010NM WS 519 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 RIGHT WING UPPER STRINGER 2ND AFT FROM FRONT SPAR IS CRACKED AT STATION 519. INSTALLED MANUFACTURED ANGLES AND FILLER PER SB 727-57A159. (M) 2L73 4F A3WE 19960112004011996011200401NM 1996 1 12 EISA95462 119951201A5712 RIB BOEING727 72731 1384010NM WS 738.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK IN LEFT WING RIB AT LOWER FASTENER HOLE WS 738.5 AND FIRST STRINGER AFT OF REAR SPAR. REPAIRED PER SRM 57-10-5. (M) 2L73 4F A3WE 19960112004021996011200402NM 1996 1 12 EISA95463 119951201A5712 RIB BOEING727 72731 1384010NM WS 686.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK IN LEFT WING RIB, LOWER FASTENER HOLE, WS 686.5 AND FIRST STRINGER AFT OF REAR SPAR. INSTALLED REPAIR PER SRM 57-10-5. (M) 2L73 4F A3WE 19960112004031996011200403NM 1996 1 12 EISA95464 119951201A5712 RIB BOEING727 72731 1384010NM WS 783.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK IN RT WING RIB NEAR LOWER FASTENER HOLE AT WS 783.50 RT AND FIRST STRINGER AFT OF FRONT SPAR. INSTALLED DOUBLER PER 57-10-5. (M) 2L73 4F A3WE 19960112004041996011200404NM 1996 1 12 EISA95469 119951201A5712 RIB BOEING727 72731 1384010NM WS 656.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 FOUR CRACKS IN RIGHT WING RIB WS 656.5. REPLACED RIB PER SB 727-57-0127. (M) 2L73 4F A3WE 19960112004051996011200405NM 1996 1 12 EISA95470 119951201A5712 RIB BOEING727 72731 1384010NM WS 546.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 THREE CRACKS IN LEFT WING INTERNAL RIB AT WS 546.5. STOP DRILLED CRACKS FABRICATED DOUBLER PER SRM 57-10-5 AND INSTALLED DOUBLER PER SRM 57-10-5. (M) 2L73 4F A3WE 19960112004061996011200406NM 1996 1 12 EISA95471 119951201A5712 RIB BOEING727 72731 1384010NM WS 546.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 TWO CRACKS RIGHT WING INTERNAL RIB AT WS 546.50 LOWER FLANGE. INSTALLED DOUBLER PER SRM 57-10-05. (M) 2L73 4F A3WE 19960112004071996011200407NM 1996 1 12 EISA95474 119951201A5220 DOOR BOEING727 72731 1384010NM EMER EXIT DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 TOP EXTERIOR SURFACE OF FWD RIGHT EMERGENCY EXIT DOOR DAMAGED. REPAIRED DAMAGED DOOR PER SRM 52-20-2. (M) 2L73 4F A3WE 19960112004081996011200408NM 1996 1 12 EISA95475 119951201A5311 FRAME BOEING727 72731 1384010NM BS 760 CRACK A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 HFEC INSPECTION INDICATES CRACKS IN FWD 2 FASTENER HOLES, FS 760 RIGHT FRAME CHORD UPPER VERTICAL FLANGE. FABRICATED REPAIR ANGLE REF, BAC DRAWING 65-68492. INSTALLED ALL REPAIR PARTS AND FASTENERS PER SB 727-57-0112. (M) 2L73 4F A3WE 19960112004091996011200409NM 1996 1 12 EISA95476 119951201A5311 FRAME BOEING727 72731 1384010NM BS 760 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 HFEC INSPECTION INDICATES CRACKS IN FORWARD 2 FASTENER HOLES FS 760 LT FRAME CHORD UPPER VERTICAL FLANGE. FABRICATED REPAIR ANGLE REF, BAC DRAWING 65-68492. INSTALLED ALL REPAIR PARTS AND FASTENERS PER SB 727-57-0112. (M) 2L73 4F A3WE 19960112004101996011200410NM 1996 1 12 EISA95478 119951204A5311 FRAME BOEING727 72731 1384010NM BS 940 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK EMANATING FROM FASTENER HOLE AT FWD SIDE OF LANDING GEAR SUPPORT BEAM STATION 940L CABIN INTERIOR BELOW FLOOR LEVEL. INSTALLED DOUBLER ANGLES AND STRAP PER SB 727-53-0118. (M) 2L73 4F A3WE 19960112004111996011200411NM 1996 1 12 EISA95479 119951204A5347 SEAT TRACK BOEING727 72731 1384010NM BS 680-700 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CABIN INTERIOR, CORROSION AT RIGHT INBOARD SEAT TRACK BETWEEN STATION 680-700 (23 INCHES RIGHT OF BL 0). INSTALLED NEW SECTION OF SEAT TRACK PER SRM 53-10-05. (M) 2L73 4F A3WE 19960112004121996011200412NM 1996 1 12 EISA95480 119951201A5713 STRINGER BOEING727 72731 1384010NM WS 383.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 LEFT WING 3RD STRINGER AFT OF FRONT SPAR CRACKED AT TOP OF RIB AT WS 383.5. FABRICATED STRINGER REPAIR PER SRM 57-10-04. (M) 2L73 4F A3WE 19960112004131996011200413NM 1996 1 12 EISA95481 119951201A5713 STRINGER BOEING727 72731 1384010NM WS 656 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 LEFT WING UPPER AFT STRINGER ATTACHED TO RIB AT STATION 656 IS CRACKED AT VERTICAL LEG JUST INBOARD OF RIB. STOP DRILLED CRACK HFEC VERIFIES CRACK CONTAINED DOUBLER INSTALLED PER SB 727-57-0127. (M) 2L73 4F A3WE 19960112004141996011200414NM 1996 1 12 EISA95483 119951108A5754 RIB BOEING727 72731 1384010NM NR 4 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 NR 4 SLAT INBOARD AND OUTBOARD NOSE RIB CRACKED AT PREVIOUSLY INSTALLED DOUBLERS WHERE ACTUATOR ROD END ATTACHES. FABRICATED DOUBLERS PER SRM 57-50-03. INSTALLED DOUBLERS PER SRM 57-50-3. (M) 2L73 4F A3WE 19960112004151996011200415NM 1996 1 12 EISA95488 119951201A5712 RIB BOEING727 72731 1384010NM WS 601.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 TWO CRACKS IN LEFT WING RIB WS 601.5. REPLACED RIB PER SB 727-57-0127. (M) 2L73 4F A3WE 19960112004161996011200416NM 1996 1 12 F3LA95019 119951214A272065C370528 PCU BOEING737 737201 1384454NM RUDDER MALFUNCTIONED A F3LAO OTHER O OTHER LDLANDING 1 NM03217US 20215 FLT NR 465 - DEN -UPON ARRIVAL, FLIGHT CREW REPORTED RUDDER TRIM REQUIRED ONE FULL UNIT OF RIGHT RUDDER ADJUSTMENT TO ESTABLISH ZERO DEGREE DRIFT. MAINTENANCE REPLACED THE RUDDER POWER CONTROL UNIT AND SYSTEM CHECKED OK. (M) 2L72 4F A16WE 19960112004171996011200417NM 1996 1 12 F3LA95020 119951215A2910BACH8C08NN025 LINE BOEING737 737201 1384454NM B-HYD SYSTEM FAILED A F3LAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 NM03207AU 19423 FLT NR 221 - DEN - AIR TURN BACK, DURING CLIMB-OUT OF DEN, FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. THE AIRCRAFT WAS RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC LINE FROM THE NR 2 B-SYSTEM MODULE. PERFORMED LEAK CHECK AND SYSTEM CHECKED OK. (M) 2L72 4F A16WE 19960112004181996011200418WP 1996 1 12 GRAA9555 119951123A335041B004AA15 BATTERIES DOUG DC9 DC915 3022036WP COCKPIT DISCHARGED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111068T 45782 AT RNO - LINE MAINTENANCE DISCOVERED THAT THE COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE COCKPIT EMERGENCY LIGHT BATTERIES. COCKPIT EMERGENCY LIGHTS OPERATIONALLY CHECKED NORMAL. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4F A6WE 19960112004191996011200419WP 1996 1 12 HALA95159 119951122A32600800004003 PROX CONTL BOX DOUG DC9 DC951 3022051WP NLG MALFUNCTIONED A HALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP132FOR 47796 HNL - FLT NR 351 - AFT GEAR RETRACTION 'RIGHT GEAR UNSAFE' LIGHT REMAINED ON AFTER APPROX 1 MINUTE. 'GEAR DOOR OPEN' LIGHT CAME ON. RETURNED TO HILO FOR PRECAUTIONARY LANDING. DURING DESCENT SPEED BRAKE HANDLE WOULD NOT LOCK IN DETENTS. DURING DESCENT BOTH 'GEAR' AND 'DOOR' LIGHTS WENT OUT, NORMAL INDICATIONS. THEREAFTER, GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR PROXIMITY CONTROL BOX. LUBRICATED UPLOCK SWITCH. CLEANED SENSORS. GEAR SWING OPERATIONAL CHECK GOOD. OPERATIONAL CHECK OF SPEED BRAKE CHECKED NORMAL. (M) 2L72 4F A6WE 19960112004201996011200420WP 1996 1 12 HALA95160 119951123A2530 CONNECTOR DOUG DC9 DC951 3022051WP GALLEY SHORTED A HALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP13709HA 47764 HNL - FLT NR 506 - FLIGHT ATTENDANT REPORTED SMOKE (ELECTRICAL SMELL) FROM COFFEE MAKER. FOUND NR 2 COFFEE MAKER CANNON PLUG FROM AIRCRAFT SOURCE SHORTED. REPLACED NR 2 COFFEE MAKER. REPAIRED CANNON PLUGS. OPERATIONAL AND LEAK CHECK GOOD. (M) 2L72 4F A6WE 19960112004211996011200421WP 1996 1 12 HALA95161 119951123A2612 CONNECTORS DOUG DC10 DC1010 3022110WP NR 1 ENGINE DIRTY A HALAE ENGINE SHUTDOWN N FALSE WARNING TXTAXI/GRND HDL 1 WP13119AA 46519 HNL - FLT NR 25 - NR 1 FUEL LEVER, FIRE HANDLE AND A-LOOP LIGHT FLICKERED INTERMITTENTLY ON DESCENT WITH ENGINES AT IDLE. NO AURAL WARNING. MOVED NR 1 THROTTLE SLIGHTLY FORWARD AND INDICATION WENT AWAY. OTHERWISE, FOLLOWED H.A. S.O.P. AFTER LANDING ON TAXI IN. NR 1 FIRE WARNING CAME ON WITH AURAL WARNING. SHUT DOWN NR 1 ENGINE AND FIRE WARNING LIGHT WENT OUT. ASKED TOWER IF THERE WAS ANY SMOKE FROM ENGINE, BUT, THEY SAID ALL LOOKED NORMAL. CLEANED NR 1 ENGINE FIRE DETECTOR CANNON PLUGS ON ELEMENTS. A-LOOP TESTED GOOD. (M) 2L73 4F A22WE 19960112004221996011200422WP 1996 1 12 HALA95164 119951127A553071658H11108 ATTACH BOLT DOUG DC10 DC1010 3022110WP VERT STAB CRACKED A AHALAK NONE O OTHER ININSP/MAINT 1 WP13153AA 46708 LAX - DURING ACCOMPLISHMENT OF SPECIAL CARD ITEM NR 3950-1F, FOUND RIGHT FORWARD VERTICAL STABILIZER ATTACH BOLT CRACKED, LOCATED UNDER LEADING EDGE WRAP AROUND PANEL. REPLACED RIGHT FRONT SPAR VERTICAL STABILIZER ATTACH BOLT WITH P/N 3D0031-20-86. (M) 2L73 4F A22WE 19960112004231996011200423WP 1996 1 12 HALA95165 119951201A3231 BRACKET DOUG DC9 DC951 3022051WP NLG DOOR BENT A HALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP13420EA 47689 HNL - FLT NR 128 - AFTER TAKEOFF WHEN NOSE WHEEL RETRACTION, LOUD BANG WAS HEARD IN NOSE WHEEL COMPARTMENT ALONG WITH EXCESS VIBRATION. RETURNED FOR LANDING. UPON INSPECTION OF NLG FOUND, HOLE IN NLG LEFT AFT FIXED DOOR INTERIOR FWD SIDE. LEFT AFT FIXED DOOR AFT HINGE HAS EXCESSIVE PLAY. ATTACH BRACKET BENT ON RIGHT FWD NLG DOOR (ACTUATOR BRACKET). INSPECTED NOSE GEAR AND WHEEL WELL AREA. REMOVED AND REPLACED RIGHT FWD NLG DOOR ACTUATOR FOR PRECAUTIONARY CHANGE. REPLACED ACTUATOR BRACKET. GEAR SWING CHECKS OK. (M) 2L72 4F A6WE 19960112004241996011200424WP 1996 1 12 HALA95171 119951210A3246DC9MAIN WHEEL DOUG DC9 DC951 3022051WP NR 3 MLG RIM CRACKED A AHALAK NONE D INFLIGHT SEPARATION LDLANDING 1 WP13673MC MAR841271 47726 HNL - AFTER LANDING, EXPERIENCED LOUD BANG. NR 3 TIRE LEFT AIRCRAFT. REPLACED NR 3 MAIN WHEEL ASSY SPIN CHECKED OK. FOUND RIM AND NUT/HUB CAP STILL SECURE. TIRE LEFT AIRCRAFT DUE TO RIM CRACK. SECURITY CHECKED OF RIGHT WING NO ADDITIONAL DAMAGED NOTED. (M) 2L72 4F A6WE 19960112004251996011200425WP 1996 1 12 HALA95172 119951211A53129923406501 FRAMES DOUG DC9 DC951 3022051WP LT/RT BS 734 CRACKED A AHALAK NONE O OTHER ININSP/MAINT 1 WP13669HA40457 47654 HNL - DURING D-CHECK AT SBA, FOUND FUSELAGE SIDEWALL STATION FRAME HAS 1.5 INCH CRACK AT FUSELAGE STATION 734 LEFT AND A 1 INCH CRACK AT FUSELAGE STATION 734 RT. THE CRACKS ARE IN THE RADIUS AT THE LOWER END OF THE FLOOR BEAM ATTACHMENTS. THESE ARE PSE 53.09.013 AND 014 AFFECTED BY AD 94-03-01 RELATIVE TO THE SID PROGRAM. FABRICATED AND INSTALLED STEEL ANGLES PER SRM 53-03 FIG 16 SECTION Q-Q. CRACKS WERE STOP DRILLED. REFER TO DACO FAX MIS 6754 DLP (SRM 53-03, FIG 16, 505). ALTERNATE METHOD OF COMPLIANCE WITH THE REPAIR REQUIREMENT OF AD 94-03-01 AFFECTING PSE, 53-09-013 AND 53-09-014. (M) 2L72 4F A6WE 19960112004261996011200426WP 1996 1 12 HALA95173 119951126A5320 BLKHD ANGLES DOUG DC9 DC951 3022051WP BS 1167 CRACKED A HALAK NONE O OTHER ININSP/MAINT 1 WP13673MC40457 47726 SBA - DURING D-CHECK AT SBA, FOUND AFT PRESSURE BULKHEAD, AT FUSELAGE STATION 1167 FWD SIDE RIGHT STIFFENERS 3 BETWEEN STRINGER LOCATIONS R14 TO 17 UPPER AND LOWER SUPPORT ANGLES SIX AT OUTBOARD PERIPHERY, HAVE .5 INCH CRACKS AT OUTBOARD RADIUS (REFER SDR 95-172). FABRICATED AND INSTALLED 3 UPPER ANGLES. STOP DRILLED LOWER ANGLES AND INSTALLED NESTED ANGLE REPAIRS PER SRM 51-10-2 ADN 51-3. (M) 2L72 4F A6WE 19960112004271996011200427EA 1996 1 12 HNAA9590524 119951211A3233165007 DNLOCK ACT DHAV DHC7 DHC7102 2802708EA NLG FAILED A HNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA07905HA18886 070 FLT NR 3028 - PHL-DCA - AFTER TAKEOFF, THE NOSE GEAR UNSAFE LIGHT CAME ON AFTER GEAR SELECTED UP. THE AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK ACTUATOR. (M) 2H74 4T A20EA 19960112004291996011200429NE 1996 1 12 M3HA95019 219951207A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 2 FAILED A M3HAE ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 WP13985MA 358 121273 HNL - DURING FINAL APPROACH CRC SOUNDED, CREW OBSERVED ZERO TORQUE AND OIL PRESSURE INDICATIONS ON NR 2 ENGINE. CREW SHUTDOWN ENGINE AND CONTINUED WITH LANDING. REMOVED AND REPLACED NR 2 ENGINE. (M) 2H72 4T4 TRTA53EU E20NE 19960112004301996011200430NM 1996 1 12 MZZA95046 119950907A3350900835A BATTERY PACK BOEING727 727224 1384076NM CABIN DISCHARGED A MZZAK NONE L NO TEST ININSP/MAINT 1 WP1379744 22253 GUM - DURING B-CHECK, FOUND CABIN FORWARD AXLE CEILING EMERGENCY EXIT SIGN INOP. MAINTENANCE REPLACED BATTERY PACK, SYSTEM OPERATION CHECK PER MM 33-50-71 AND FOUND SATISFACTORY. (M) 2L73 4F A3WE 19960112004311996011200431NM 1996 1 12 MZZA95047 119951016A2782651781820 ACTUATOR BOEING727 7272F9 138407DNM LT LE FLAP CRACK A MZZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP13299AS 21427 FLT NR 925 - GUM - AFTER TAKEOFF, LOSS A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. AIRCRAFT DIVERTED TO GUAM. MAINTENANCE DISCOVERED THAT HYDRAULIC FLUID LEAK FROM NR 3 LEADING EDGE FLAP ACTUATOR HOUSING. REPLACED NR 3 LEADING EDGE FLAP ACTUATOR PER MM 27-81-22. INSPECTED A-SYSTEM HYDRAULIC PUMPS AND PRECAUTION REPLACED ALL CASE DRAIN FILTERS. A-SYSTEM LEAK AND OPERATIONAL CHECK ALL GOOD. AIRCRAFT RETURN BACK IN SERVICE. (M) 2L73 4F RTA3WE 19960112004321996011200432NM 1996 1 12 MZZA95049 119951102A2782269002911 ACTUATOR BOEING727 727232 1384082NM NR 1 LE SLAT BROKEN A MZZAAJ UNSCHED LANDING DUMP FUEL KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP1315790 20644 FLT NR 917 - GUM - ON CLIMB-OUT, LOST A-SYSTEM HYDRAULICS, CREW SHUT DOWN SYSTEM A-PUMPS PRIOR TO COMPLETE HYDRAULIC FLUID LOSS. AIRCRAFT DIVERTED BACK TO GUAM. MAINTENANCE FOUND NR 1 LED SLAT ACTUATOR LEAKING FLUID AND REPLACED ACTUATOR PER MM 27-81-04. SYSTEM SERVICE BACK TO NORMAL AND OPERATION CHECK GOOD. AIRCRAFT RETURN BACK TO SERVICE. (M) 2L73 4F A3WE 19960112004331996011200433WP 1996 1 12 ORJA95132 119951205A335041B004AD073 BATTERY EA1D131D3 DOUG DC9 DC982 3022082WP FLIGHT DECK DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11843RA 49615 EMERGENCY LIGHTS IN FLIGHT DECK INOP AND FWD GALLEY. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FLIGHT DECK AND FWD GALLEY. (M) 2L72 4F A6WE 19960112004341996011200434WP 1996 1 12 ORJA95133 119951207A3350 SOCKET DOUG DC9 DC982 3022082WP CABIN BROKEN A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11821RA 49931 TWO FLOOR EMERGENCY LIGHTS ARE INOP, AT ROW 18-32. REPLACED BROKEN WIRE WIRE/SOCKET ASSY AND RELAMPED. ALL CHECK GOOD. (M) 2L72 4F A6WE 19960112004351996011200435WP 1996 1 12 ORJA95134 119951207A3350 LIGHT DOUG DC9 DC983 3022083WP EMPENNAGE BROKEN A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11832RA 53044 FORWARD E-PATH LIGHT ASSY IN EMPENNAGE PATH WAY SIDEWALL BROKEN. INSTALLED FORWARD E-PATH LIGHT ASSY, OPS CHECK GOOD. (M) 2L72 4F RTA6WE 19960112004361996011200436WP 1996 1 12 ORJA95135 119951208A335041B004AD073 BATTERY EA1D13D3 DOUG DC9 DC983 3022083WP EMPENNAGE DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11872RA 49793 EMERGENCY LIGHTS, AFT 2 FLOOD LIGHTS IN EMPENNAGE ARE OUT. REPLACED NICAD BATTERIES IN POWER PACK. OPS CHECKED GOOD. (M) 2L72 4F RTA6WE 19960112004371996011200437WP 1996 1 12 ORJA95136 119951208A335041B994AD073 BATTERY EA1D13D3 DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11840RA 49424 OVERHEAD EMERGENCY LIGHTING IS DIM, LOWER ROWS 1 AND 6. REPLACED BATTERY PACK AND OPS CHECKED GOOD. (M) 2L72 4F A6WE 19960112004381996011200438NM 1996 1 12 PCAA9500245 119951106A335010005511 BATTERY DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13419AW7178 297 COCKPIT EMERGENCY LIGHT BATTERY IS DEAD. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004391996011200439NM 1996 1 12 PCAA9500246 119951108A273182760174005 JACKSCREW DHAV DHC8 DHC8102 2809003NM ELEV TRIM FROZEN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13417AW9510 285 ELEVATOR TRIMS BINDS IN THE MIDDLE OF THE TAKEOFF RANGE, TO COMPLETELY NOSE UP RANGE IN FLIGHT. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR TRIM JACKSCREWS. SUBMITTER STATES, SUSPECT FREEZING OF JACKSCREWS IN FLIGHT, DUE TO WATER COMING OUT OF WEEP HOLES AFTER REMOVAL. SUBMITTER STATES, THESE ARE THE LATEST MOD FROM DHC. LEFT TRIM CABLE IN TAIL CONE FOUND CHAFED. ALSO, REMOVED AND REPLACED CABLE. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004401996011200440NM 1996 1 12 PCAA9500247 119951209A2913570347001 HYD PUMP DHAV DHC8 DHC8102 2809003NM RT ENGINE FAILED A PCAAO OTHER J WARNING INDICATION CLCLIMB 1 EA13817EX 191 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT WITH GEAR SELECTED UP, A LOUD CONTINUOUS RUMBLING NOISE HEARD IN NOSE WHEEL AREA. LEFT MAIN AND NOSE DOOR YELLOW LIGHTS STAYED ON AND RIGHT MAIN RED JACKED AIRCRAFT. PERFORMED SEVERAL GEAR RETRACTION TESTS. GEAR AND INDICATIONS OPERATED NORMALLY. TEST FLIGHT PERFORMED UNSATISFACTORY. AIRCRAFT RETURNED FOR FURTHER TROUBLESHOOTING AND REPAIRS. REMOVED AND REPLACED RIGHT ENGINE DRIVEN PUMP, BLED HYDRAULIC SYSTEM. SUBSEQUENT TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004411996011200441NM 1996 1 12 PCAA9500248 119951113A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT INTERMITTENT A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13821EX7831 173 THE PORTABLE OVERHEAD EMERGENCY LIGHT FLASHES INTERMITTENTLY, AND SHOWS LOW ILLUMINATION ON GROUND. REMOVED AND REPLACED C/P EMERGENCY LIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004421996011200442NM 1996 1 12 PCAA9500249 119951116A4920T62T40C7B APU DHAV DHC8 DHC8102 2809003NM RT WING FAILED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13816EX5900 925162 329 APU FAILED ON START UP. INSPECTED APU PER MEL PROCEDURES, FOUND APU DAMAGED. AIRCRAFT FERRIED TO MDT FOR REPAIRS. INSPECTED APU, FOUND UNCONTAINED CATASTROHIC FAILURE OF THE COMPRESSOR ROTOR. REMOVED AND REPLACED APU. PERFORMED STRUCTURAL REPAIR MANUAL AND REPAIR DRAWINGS. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004431996011200443NM 1996 1 12 PCAA9500250 119951121A5610NP1579016 WINDSHIELD DHAV DHC8 DHC8102 2809003NM RT COCKPIT CRACKED A PCAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA13818EX11052 DH014B 235 FIRST OFFICERS WINDSHIELD HAS LARGE CRACK IN IT. AIRCRAFT RETURNED TO FIELD IN BWI. FERRIED TO MDT FOR REPAIR. REMOVED AND REPLACED FLIGHT OFFICERS WINDSHIELD AND HEAT CONTROLLER AS A PRECAUTIONARY MEASURE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004441996011200444NM 1996 1 12 PCAA9500251 119951124A2913570347 HYD PUMP DHAV DHC8 DHC8102 2809003NM NR 2 FAILED A PCAAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 EA132FOR 12079 258 ON TAKEOFF FROM BGM, NR 2 HYDRAULIC FAIL LIGHT ILLUMINATED UPON LANDING GEAR RETRACTION. AIRCRAFT RETURNED TO FIELD. TROUBLESHOT AND FOUND NR 2 ENGINE DRIVEN HYDRAULIC PUMP AT FAULT. REMOVED AND REPLACED PUMP, BLED SYSTEM. SUBSEQUENT TEST FLIGHT PROVED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004451996011200445NM 1996 1 12 PCAA9500252 119951127A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13800MX8048 007 COCKPIT PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED COCKPIT OVERHEAD EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004461996011200446NM 1996 1 12 PCAA9500253 119951126A3260 UPLOCK SW DHAV DHC8 DHC8102 2809003NM RT MLG OUT OF ADJUST A PCAAO OTHER N FALSE WARNING NRNOT REPORTED 1 EA132FOR 215 LANDING GEAR TRANSIT LIGHT ILLUMINATED DURING FLIGHT. TROUBLESHOT AND ADJUSTED RIGHT UPLOCK PROX SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960112004471996011200447EA 1996 1 12 PLG102395J1 219951023A7210310076701 RED GEAR BOX BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA LT PROP FAILED A PLGAK NONE O OTHER TXTAXI/GRND HDL 1 NE05154868086 UC131 32326 DURING SHUTDOWN, THE LEFT PROPELLER STOPPED ROTATION IMMEDIATELY AFTER THE CONDITION LEVER WAS PLACED IN THE FUEL CUT OFF POSITION. TECHNICIANS ATTEMPTED TO ROTATE PROPELLER WITHOUT SUCCESS. FURTHER TROUBLESHOOTING REVEALED METAL PARTICLE CONTAMINATION IN THE GAS GENERATOR OIL FILTER. THE ENGINE WAS REMOVED AND SUBSEQUENTLY HAD THE POWER SECTION SEPARATED AND DIRECTED TO A REPAIR SHOP WHERE, UPON DISASSEMBLY, THE FAILED HARDWARE WAS REVEALED. (M) 2L72 4T4 TRTA24CE E4EA 19960112004481996011200448CE 1996 1 12 PLG103095G7 119951030A2730101524887605 TRIM ACTUATOR BEECH 1900 1900C 1154161CE ELEVATOR FAILED A APLGAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING O OTHER CLCLIMB 1 NE053069K574 333A86 UB71 FLT NR 4724 - BOS - ON CLIMB-OUT, ELEVATOR TRIM WAS SELECTED, WHICH CONTINUED TO TRAVEL BEYOND THE SELECTED COMMAND. THE CREW SELECTED THE TRIM TO OFF. MANUAL TRIM WAS SELECTED, WHEREUPON THE TRIM SYSTEM WAS FOUND FROZEN. THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. BOS MAINTENANCE FOUND THE ELEVATOR TRIM SERVO ACTUATOR HAD SHORTED INTERNALLY CAUSING THE SYSTEM TO LOCK. THE SYSTEM WAS DEFERRED PER THE MEL AND THE AIRCRAFT RETURNED TO SERVICE. A REPLACEMENT SERVO IS ON ORDER. (M) 2L72 4T RTA24CE 19960112004491996011200449EU 1996 1 12 PLG103095G8 119951030A2611 SMOKE DETECTOR SAAB SF340 340B 7860101EU AVIONICS RACK FAILED A PLGAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 NE05362BE 340B291 FLT NR 4312 - DCA-BOS - DIVERTED TO BWI DUE TO AN AVIONICS SMOKE DETECTOR LIGHT. NO EVIDENCE OF SMOKE WAS NOTED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. INSPECTION REVEALED NO EVIDENCE OF SMOKE OR FIRE. MAINTENANCE DEFERRED THE SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. UPON ARRIVAL IN BOS, MAINTENANCE REPLACED THE DEFECTIVE SMOKE DETECTOR AND RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA52EU 19960112004501996011200450EU 1996 1 12 PLG112095E1 119951116A71107271110804 COWLING SAAB SF340 340B 7860101EU RT ENGINE DENTED A PLGAA UNSCHED LANDING O OTHER CLCLIMB 1 NE05363BE 340B293 FLT NR 4590 - JUST AFTER TAKEOFF, THE FLIGHT CREW NOTED THAT THE RIGHT OUTBOARD FORWARD COWLING WAS NOT SECURED. THE AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE INSPECTED THE COWLING STRUCTURE AND FOUND ONLY THE DOORS WERE DAMAGED. THE RIGHT INBOARD AND OUTBOARD FORWARD COWLING DOORS WERE REMOVED AND REPLACED. THE AIRCRAFT WAS FOUND SAFE FOR FERRY FLIGHT FROM PHL TO PSM FOR FINAL REPAIRS OF THE MINOR DENTS ON THE NACELLE AND WING AREA. FINAL REPAIRS WERE COMPLETED IN PSM AND AIRCRAFT WAS RELEASED TO SERVICE. (M) 2L72 4T RTA52EU 19960112004511996011200451EU 1996 1 12 PLG120495E1 119951129A3010NH24668081 LOWER DUCT SAAB SF340 SF340A 7850100EU LT ENGINE DAMAGED A PLGAA UNSCHED LANDING O OTHER CRCRUISE 1 NE05751BA L180815 340A157 FLT NR 4401 - PQI-BOS - DURING FLIGHT, THE LEFT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT DIVERTED INTO PWM AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE REMOVED AND REPLACED THE LOWER DUCT DUE TO A BURN HOLE IN THE HEATING MAT OF THE DUCT. THE SYSTEM WAS OPERATIONS CHECKED AND NO FAULT WAS FOUND. AIRCRAFT WAS RELEASED TO SERVICE. (M) 2L72 4T RTA52EU 19960112004521996011200452CE 1996 1 12 PLG121195E1 119951209A3010 DE-ICE BOOTS BEECH 1900 1900C 1154161CE WINGS MALFUNCTIONED AP PLGAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 NE0515553 UC128 FLT NR 4948 - BOS-YQB - AFTER REACHING CRUISE ALTITUDE, THE CAPTAIN REPORTED THAT THE OUTER WING DE-ICE BOOTS WERE NOT INFLATING. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN INSPECTION OF THE DE-ICE BOOTS AND OPERATIONAL CHECKED THE SYSTEM. NO FAULTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA24CE 19960112004531996011200453EU 1996 1 12 RAIA951122 119951119A3231 RETRACT MECH BAG JETSTMJETSTM3201 1500217EU NLG DOOR OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03342TE7086 954 STL - FLT 7054 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTED. PERFORMED RIGGING CHECK OF NOSE GEAR DOORS (P/N 137581C425). (M) 2L72 4T RTA56EU 19960112004541996011200454EU 1996 1 12 RAIA951124 119951117A793141SG107150G14 TRANSMITTER BAG JETSTMJETSTM3201 1500217EU NR 2 ENGINE FAILED A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03424AM6242 865 STL - FLT 7073 - RIGHT OIL PRESSURE WENT TO 140. REPLACED OIL PRESSURE TRANSMITTER. (M) 2L72 4T RTA56EU 19960112004551996011200455WP 1996 1 12 RAIA951125 219951117A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 1 ENGINE LEAKING A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03428AM8582 877 66178 STL - FLT NR 7073 - LOW TORQUE ON TAKEOFF. REPLACED BLEED AIR GASKET. (M) 2L72 4T4 TRTA56EU E4WE 19960112004561996011200456WP 1996 1 12 RAIA951126 219951118A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 1 ENG LEAKING A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03875JX7784 875 66140 CMI - FLT 7439 - LEFT FUEL CAPTION AND LEFT BETA LIGHT ILLUMINATED ON TAKEOFF. REPLACED BLEED AIR PORT GASKET. (M) 2L72 4T4 TRTA56EU E4WE 19960112004571996011200457WP 1996 1 12 RAIA951127 219951119A73201379287L405 P3 LINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP NR 2 ENG LOOSE A RAIAA UNSCHED LANDING O OTHER TXTAXI/GRND HDL 1 CE03427AM10303 876 66163 STL - FLT 7878 - NR 2 ENGINE EGT SPIKED. RETORQUED P3 BLEED LINE. PERFORMED GROUND RUN AND FOUND SYSTEM TO OPERATE NORMAL. (M) 2L72 4T4 TRTA56EU E4WE 19960112004581996011200458EU 1996 1 12 RAIA951128 119951118A3350167006 LAMP AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03722TE 220 ONE LIGHT OUT ON ESCAPE PATH LIGHTING. REPLACED LAMP. (M) 2H72 4T RTA53EU 19960112004591996011200459EU 1996 1 12 RAIA951129 119951119A32609005EN38 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG DIRTY A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03342TE7086 954 STL - FLT 7440 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTED. CLEANED UPLOCK SWITCH. (M) 2L72 4T RTA56EU 19960112004601996011200460EU 1996 1 12 RAIA951130 119951118A33507012210 LAMP AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 176 STL - FLT NR 7210 - EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP. (M) 2H72 4T RTA53EU 19960112004611996011200461WP 1996 1 12 RAIA951133 219951124A73208974575 BYPASS VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP RT ENG FAILED A RAIAF ACTIVATE FIRE EXT. A FLAME/FIRE TXTAXI/GRND HDL 1 CE03866AE2917 2917 866 66119 LAX - FLT 4727 - RIGHT ENGINE HAD FLAMES COMING FROM EXHAUST ON TAXI. CREW SHUT DOWN ENGINE AND SHOT BOTH FIRE BOTTLES FOR PRECAUTION. MAINTENANCE REPLACED FIRE BOTTLES AND REPLACED RIGHT FAULTY FUEL BYPASS VALVE. GROUND CHECK GOOD. (M) 2L72 4T4 TRTA56EU E4WE 19960112004621996011200462EU 1996 1 12 RAIA951135 119951130A3260AIR135672 DNLOCK SW JETAIRJETSTMJETSTM4101 1500501EU NLG FAILED A RAIAO OTHER N FALSE WARNING LDLANDING 1 CE03550HK2390 41039 STL - FLT NR 7462 - SECONDARY NOSE GEAR DOWN LIGHT INOP. WARNING HORN WENT OFF WITH FLAPS AT 15 DEGREES AIRSPEED AT 140. MAINTENANCE REPLACED NOSE GEAR DOWN LOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA41NM 19960112004631996011200463EU 1996 1 12 RAIA951136 119951130A3233 O-RINGS BAG JETSTMJETSTM3201 1500217EU NLG ACT LEAKING A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03424AM14784 865 EVV - FLT NR 7423 - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR O-RINGS (P/N 173M165 AND 134M33206A). GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19960112004641996011200464EU 1996 1 12 RAIA951201 119951205A2913PV304426 HYD PUMP BAG JETSTMJETSTM3201 1500217EU LT ENG FAILED A RAIACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CE03422AM10489 856 ALT - FLT NR 7467 - LEFT HYD PUMP WENT TO ZERO ON TAKEOFF. MAINTENANCE REPLACED LEFT HYD PUMP. SYSTEM CHECK GOOD AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19960112004651996011200465EU 1996 1 12 RAIA951202 119951204A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03428AM6601 6601 877 STL - FLT NR 7059 - RIGHT ENGINE ONLY ACHIEVED 95 PERCENT TORQUE. MAINTENANCE ADJUSTED RIGHT ENG TORQUE SIGNAL CONDITIONER AS PER GARRETT DSC SETTINGS. GROUND PERFORMANCE RUNS CHECK GOOD. (M) 2L72 4T RTA56EU 19960112004661996011200466EU 1996 1 12 RAIA951203 119951204A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03428AM6601 6601 877 STL - FLT 7 - RIGHT ENGINE ONLY ACHIEVED 95 PERCENT TORQUE. MAINTENANCE SWAPPED TORQUE SIGNAL CONDITIONER BRIDGE. ADJUSTED SIGNAL CONDITIONER PER GARRETT DSC SETTINGS. GROUND PERFORMANCE RUN CHECK GOOD. (M) 2L72 4T RTA56EU 19960112004671996011200467EU 1996 1 12 RAIA951204 119951206A78001379048H401 TAIL PIPE BAG JETSTMJETSTM3201 1500217EU LT ENG SEPARATED A RAIAK NONE O OTHER LDLANDING 1 CE03427AM10399 876 STL - FLT 7309 - LEFT TAIL PIPE INNER EXHAUST SEPARATED FROM AIRCRAFT. CREW LANDED AIRCRAFT WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT EXHAUST TAIL PIPE. (M) 2L72 4T RTA56EU 19960112004681996011200468EU 1996 1 12 RAIA951205 119951206A30607826892 BRUSH BLOCK AEROSPATR42 ATR42300 8680920EU RT PROP FAILED A RAIAK NONE J WARNING INDICATION CRCRUISE 1 CE032FOR 132871734 176 STL - FLT NR 7417 - RIGHT PROP DE-ICE INOP. MAINTENANCE REPLACED RIGHT PROP DE-ICE BRUSH BLOCK. SYSTEM CHECK GOOD. (M) 2H72 4T RTA53EU 19960112004691996011200469EU 1996 1 12 RAIA9551123 119951117A2612D2370120 FIRE LOOP BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAE ENGINE SHUTDOWN N FALSE WARNING CLCLIMB 1 CE03342TE7084 954 FWA - FLT 7541 - AFTER TAKEOFF, LEFT ENGINE FIRE WARNING OCCURRED. MAINTENANCE REPLACED THE ENGINE FIRE LOOP. (M) 2L72 4T RTA56EU 19960112004701996011200470SO 1996 1 12 SRAA129503 119951214A6120582855 VALVE HOUSING HAMSTD 54H60117 LKHEED382 382E 526413USO NR 1 PROP DAMAGED A SRAAA UNSCHED LANDING O OTHER CRCRUISE 1 SO19910SJ 2988 234382 4383 FLT NR 9006 - SNN-YQX - NR 1 ENGINE RPM SLOWLY DECAYED TO 98 PERCENT WHILE SLAVING TO NR 2 ENGINE AS MASTER. WITH NO MASTER SELECTED, NR 1 PROP GOES TO 96.7 PERCENT. SHUT DOWN NR 1 ENGINE AND ACCOMPLISHED AIR TURN BACK TO SNN. FOUND NR 1 PROP VALVE HOUSING FAILED TO OPERATE NORMALLY. WITH EVIDENCE OF METAL SHAVING ON UNIT, PERFORMED THREE ENGINE FERRY FLIGHT TO CBG. REPLACED NR 1 PROP ASSEMBLY AND VALVE HOUSING, PERFORMED ENGINE RUN UP. OPS CHECKED GOOD PER MM CH 61. (M) 2H74 4T A1SO 19960112004711996011200471NM 1996 1 12 TAOA129501 119951205A335008527 BASE BRUCE BOEING727 727225 1384077NM AFT OVERWING CRACKED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15922TS 20415 AFT RIGHT OVERWING EMERGENCY EXIT LIGHT BASE CRACKED. REPLACED BASE ASSEMBLY FOR AFT RIGHT OVERWING EMERGENCY EXIT LIGHT. OPS CHECKED GOOD. (M) 2L73 4F A3WE 19960112004721996011200472NM 1996 1 12 TAOA129502 119951205A3350BL3071BPEGPL LAMP GRIMES BOEING727 727227 1384078NM CABIN BURNED OUT A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15925TS 21244 ESCAPE PATH LIGHTING AT ROW 6 HAS ONE LAMP INOP. RELAMPED ESCAPE PATH LIGHTING AT ROW 6, OPS CHECKED OK. (M) 2L73 4F A3WE 19960112004731996011200473NM 1996 1 12 TAOA129503 119951209A3350900835A BATTERY PACK BELL BOEING727 727294 1384088NM CABIN DISCHARGED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS UA5221 22043 EMERGENCY LIGHT AT ROW 4 INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19960112004741996011200474NM 1996 1 12 TAOA129504 119951208A3350900835A BATTERY PACK BOEING727 727294 1384088NM CABIN DEPLETED A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15921TS 9427 22043 EMERGENCY LIGHT AT LEFT AFT SERVICE DOOR INOP. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. (M) 0 4 A3WE 19960112004751996011200475NM 1996 1 12 TAOA129508 119951212A57136972877 STRINGER BOEING727 727254 138408LNM WS 629 CRACKED A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 DURING C-CHECK, INSPECTION REVEALED 1 INCH CRACK ON LEFT WING LOWER STRINGER NR 9 AT WS 629. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLERS PER B727 SERVICE BULLETIN 727-57A159 AND BOEING DRAWING 69-72877 FIGURE 18. (M) 2L73 4F A3WE 19960112004761996011200476NM 1996 1 12 TSAA9532187 119951122A3231 RETRACT MECH BOEING737 737297 1384480NM NLG DOORS BROKEN A TSAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 WP13728AL 22629 FLT NR 259 - WHEN LANDING GEAR RAISED AFTER TAKEOFF, A BANG AND VIBRATION HEARD FROM NOSE WHEEL WELL AREA. LOWERED GEAR AND LANDED UNEVENTFULLY. OGG MAINTENANCE FOUND LEFT UPPER ROD OF NLG DOOR MECH BROKEN. REMOVED DOORS AND PINNED ALL THREE LANDING GEARS. AIRCRAFT FERRIED FLIGHT TO HNL FOR REPAIR. REINSTALLED DOORS, REPLACED LT NLG DOOR MECH LINK, AND RT NLG DOOR OPERATING ROD ASSY. OPERATIONS CHECKED IAW BOEING MM 32-22-11. GEAR PINS REMOVED AND AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19960112004771996011200477NM 1996 1 12 TWRA9569 119951208A32321611928 ACTUATOR BOEING747 747136 1384883NM LT MLG DOOR FAILED A TWRAO OTHER J WARNING INDICATION CLCLIMB 1 EA15606FF 20273 DURING CLIMB-OUT AND PASSING THROUGH 250 KNOTS, LEFT WING GEAR DOOR OPEN AND GEAR LIGHT ILLUMINATED. UPON LANDING, MAINTENANCE REPLACED THE DOOR ACTUATOR AND DOOR SEQUENCE VALVE. OPS CHECK OK. (M) 2L74 4F A20WE 19960112004781996011200478NM 1996 1 12 USAA951261 119951211A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 500-520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND THREE 1 TO 2 INCH CRACKS, BL 0 BS 500G TO BS 520, ON INTERCOSTAL. REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD ANGLE. REPAIRED PER DRAWING 65C34688. (M) 2L72 4F RTA16WE 19960112004791996011200479NM 1996 1 12 USAA951282 119951206A5210 ANGLE BOEING737 7372B7 1384560NM FWD ENTRY DOOR CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 24 INCH FORWARD ENTRY DOOR TRANSITION ANGLE. INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004801996011200480NM 1996 1 12 USAA951283 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 1004-1010 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 6 INCH BY 1 INCH S-27 L, BS 1004 TO BS 1010 ON STRINGER. SPLICED IN NEW STRINGER SECTION WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004811996011200481NM 1996 1 12 USAA951284 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 968 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 5 INCH BY 1 INCH S-25 L BS 968 ON STRINGER. INSTALLED DOUBLER WEIGHT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004821996011200482NM 1996 1 12 USAA951285 119951206A53131125652 STRINGER BOEING737 7372B7 1384560NM BS 974-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 12 INCH BY 1 INCH AT S-26 R, BS 974 TO BS 986 ON STRINGER. SPLICED NEW STRINGER SECTION IN, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004831996011200483NM 1996 1 12 USAA951286 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORRODED AREA AROUND NUTPLATE HOLES .25 INCH BY .25 INCH, BS 967 LBL 4, RBL 5, RBL 18 RBL 26, RBL 47, ON FLOOR BEAM. INSTALLED TEE SECTION ANGLES AND STRAPS. REPAIRED PER TR 53-10-05 C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004841996011200484NM 1996 1 12 USAA951308 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 1044 GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH GOUGE IN STRINGER OUTBOARD 'J' SECTION, STATION 1044 STRINGER 27L. INSTALLED REPAIR DOUBLER UNDER 'J' LEG OF STRINGER, AFTER SMOOTHING GOUGE. REPAIRED PER SRM 53-10-3 FIG 1. (M) 2L72 4F A16WE 19960112004851996011200485NM 1996 1 12 USAA951309 119951206A5240 HINGE BOEING737 7372B7 1384560NM SERVICE DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT AFT END OF HINGE, FRONT CABIN SERVICE DOOR LOWER GATE HINGE. REPLACED HINGE, REPAIR PER EA 40350. (M) 2L72 4F A16WE 19960112004861996011200486NM 1996 1 12 USAA951310 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 500/520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35240 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STRINGER 16 L, BETWEEN STATION 500B AND STATION 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M) 2L72 4F A16WE 19960112004871996011200487NM 1996 1 12 USAA951311 119951206A5313 STRINGER BOEING737 7372B7 1384560NM BS 500-520 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK S-16R, BETWEEN STATION 500B AND 520, ON STRINGER. INSTALLED STRINGER REPAIR, REPAIRED PER EO 5393X228. (M) 2L72 4F A16WE 19960112004881996011200488NM 1996 1 12 USAA951312 119951206A5320 ANGLE BOEING737 7372B7 1384560NM BS 540-522 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK RIGHT WING TO BODY SUPPORT ANGLE BS 540-522. REPLACED ANGLE, LESS THAN 1 LB WEIGHT CHANGE, REPAIR PER EA 25375 AND SRM 51-40-3. (M) 2L72 4F A16WE 19960112004891996011200489NM 1996 1 12 USAA951313 119951206A5320 FITTING BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK, BL 0 LONGITUDINAL FLOOR BEAM SUPPORT FITTING FORWARD RADIUS, STATION 727, WL 202.5. INSTALLED REINFORCING ANGLES, RADIUS FILLERS, SHIMS AND SEALED. REPAIRED PER EO 5394G176. (M) 2L72 4F A16WE 19960112004901996011200490NM 1996 1 12 USAA951314 119951206A5230 SKIN BOEING737 7372B7 1384560NM CARGO DOOR GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH GOUGE IN OUTER SKIN OF AFT CARGO DOOR TOP AFT CORNER OF DOOR (6 INCH BY 6 INCH DOUBLER). INSTALLED EXT SKIN DOUBLER, REPAIRED PER SRM 52-00-3. (M) 2L72 4F A16WE 19960112004911996011200491NM 1996 1 12 USAA951315 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 708/710 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BL 0 STATION 708 AND BS 710. INSTALLED WEB REPAIR, REPAIRED PER DWG 65C34537. (M) 2L72 4F A16WE 19960112004921996011200492NM 1996 1 12 USAA951316 119951206A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 707 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM WEB (LOWER) STATION 707, WL 203. INSTALLED WEB REPAIR (WT .3 LBS), REPAIRED PER SRM 51-40-2. (M) 2L72 4F A16WE 19960112004931996011200493NM 1996 1 12 USAA951317 119951206A5347 SEAT TRACK BOEING737 7372B7 1384560NM BS 986.5 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 3 INCH CORRODED AREA BS 986.5 RBL 24. REPLACED SEAT TRACK, WT CHANGE LESS THAN 1 LB. REPAIRED PER SRM 51-10-1 AND SRM 53-10-5. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960112004941996011200494NM 1996 1 12 USAABB95009 119951211A33508731002511 EXIT IDENTIFIER BOEING757 7572B7 1384964NM L4/R4 DOORS INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19621AU 27200 SFO - DURING INSPECTION, FOUND BOTH L4 AND R4 DOOR EXIT IDENTIFIERS INOPERATIVE. REPLACED BOTH EXIT IDENTIFIERS. (M) 2L72 4F RTA2NM 19960112004951996011200495NM 1996 1 12 USAASB95018 119951119A5210 SEAL BOEING737 7373B7 1384580NM L1 DOOR LEAKING A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19371US 22950 BDL - FLT NR 2351 - FLIGHT WAS UNABLE TO PRESSURIZE AFTER TAKEOFF. RETURNED TO BDL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED L1 DOOR SEAL AND TIGHTENED BOLT IN UPPER CAM ASSEMBLY. PRESSURIZATION AND DOOR SEAL CHECKED NORMAL. (M) 2L72 4F RTA16WE 19960112004961996011200496NM 1996 1 12 USAASB95019 119951130A21317638102 CONTROLLER BOEING737 737301 1384611NM E/E BAY FAILED A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19342US13110 23511 PHL - FLT NR 2169 - EN ROUTE LGA TO FLL, PRESSURIZATION FAILED. FLIGHT DESCENDED TO 10,000 FEET AND DIVERTED TO PHL. LANDING WAS WITHOUT INCIDENT. MAINTENANCE REPLACED THE PRESSURIZATION CONTROLLER. BITE AND OPS CHECKED NORMAL. (M) 2L72 4F RTA16WE 19960112004971996011200497NM 1996 1 12 USAASB95020 119951127A5210 DOOR BOEING737 7373B7 1384580NM L1 AIR LEAK A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19511AU27564 23594 IND - FLT NR 2116 - ON CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT CREW REPORTED LEAK AROUND L1 DOOR. RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED L1 DOOR AND SEAL. LUBED ROLLERS. OK FOR SERVICE. (M) 2L72 4F RTA16WE 19960112004981996011200498NM 1996 1 12 USAASB95021 119951202A26136678 DETECTOR BOEING737 7373B7 1384580NM NR 2 ENGINE FAILED A USAAAEF UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CLCLIMB 1 EA19531AU 24478 CLT - FLT NR 0127 - DURING CLIMB-OUT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED HANDBOOK PROCEDURES INCLUDING ENGINE SHUTDOWN. FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE CORE OVERHEAT/FIRE DETECTOR ELEMENT AND REPLACED LEFT AND RIGHT ENGINE FIRE BOTTLES. (M) 2L72 4F RTA16WE 19960112004991996011200499EU 1996 1 12 VTZA96040 119951210A315091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU COCKPIT DIRTY A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27307UE 41021 FLT NR 6501 - IAD-JFK - ABORTED THE TAKEOFF DUE TO THE TAKEOFF CONFIGURATION WARNING SYSTEM ACTIVATING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE CLEANED THE PARKING BRAKE AND FLAP HANDLE MICROSWITCHES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19960112005001996011200500EU 1996 1 12 VTZA96042 119951213A2932S1226142 PRESS TRANS BAG JETSTMJETSTM3201 1500217EU MLG WW BROKEN WIRE A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27487UE 906 FLT NR 6263 - IAD TO EWR - DURING CLIMB-OUT, RETURNED TO IAD DUE TO THE EMERGENCY BRAKE SUPPLY INDICATOR FAILED. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPAIRED WIRE AT PRESSURE TRANSMITTER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19960112005011996011200501NE 1996 1 12 VTZA96043 219951213A732131059003 FUEL CONTL UNIT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE RT ENGINE OUT OF ADJUST A VTZAE ENGINE SHUTDOWN X ENGINE FLAMEOUT APAPPROACH 1 EA27313UE 41026 P76008 PVD-IAD - FLT NR 6416 - DURING APPROACH, THE RIGHT ENGINE FLAMED OUT, APPROXIMATELY 2 MILES OUT OF IAD, WHEN ENGINE SPEEDS WERE SELECTED TO HIGH. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED FLIGHT IDLE FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T4 TRTA41NM E18NE 19960112005021996011200502EU 1996 1 12 VTZA96044 119951206A32336158E ACTUATOR BAG JETSTMJETSTM3201 1500217EU NOSE GEAR LOCKED UP A VTZAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27492UE 790 FLT NR 6237 - IAD-PHL - AIRCRAFT DIVERTED BACK TO IAD DUE TO THE NOSE GEAR NOT EXTENDING WHEN SELECTED DOWN. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED AT IAD WITH NOSE LANDING GEAR RETRACTED. THERE WAS COLLATERAL DAMAGE TO BOTH PROP, ENGINES, NOSE GEAR DOORS AND THE RADOME. MAINTENANCE FOUND THE ACTUATOR LOCKED UP INTERNALLY. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE INTERNAL FILTER SCREEN CAME APART AND A PIECE LODGED IN THE ORIFICE, BLOCKING THE EXIT OF HYDRAULIC FLUID. PLEASE SEE ATTACHED SHEET FOR A COMPLETE LISTING OF PARTS REPLACED AND A FINAL ACCOUNT OF ALL REPAIRS. (M) 2L72 4T RTA56EU 19960112005031996011200503EU 1996 1 12 VTZA96045 119951216A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PAX DOOR OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27317UE 41031 FLT NR 6418 - IAD-BOS - ABORTED TAKEOFF, DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING, ON THE TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 17330 IAW MEL 52-2 ON THE DOOR WARNING SYSTEM. MAINTENANCE LATER CLEARED DMI NR 17330 ON 12-18-95, BY ADJUSTING THE AFT PASSENGER DOOR WARNING MICROSWITH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA41NM 19960112005041996011200504EU 1996 1 12 WTAA950306 119951113A7712310734 TORQUE RING BAG JETSTMJETSTM3101 1500215EU LT ENGINE FALSE INDICATIONA WTAAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 WP17428UE 806 SFO - LEFT ENGINE FAILS TO OBTAIN REQUIRED TAKEOFF TORQUE. SWITCHED TORQUE SIGNAL CONDITIONER TO BRIDGE NR 2 AND ADJUSTED. ENGINE OPERATING PARAMETERS REPORTED NORMAL DURING ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960112005051996011200505EU 1996 1 12 WTAA950309 119951121A32609005EN38 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG BROKEN WIRE A WTAAO OTHER N FALSE WARNING APAPPROACH 1 WP17401UE 729 FAT - NOSE GEAR 'RED' INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE AT NOSE GEAR UPLOCK MICROSWITCH. GEAR INDICATION OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960112005061996011200506SO 1996 1 12 WTAA950311 119951126A32331959520006 ACTUATOR EMB 120 EMB120RT SO RT MLG FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17251YV 120251 SFO - RIGHT MAIN GEAR FAILED TO RETRACT AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. FAT MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR. LANDING GEAR RETRACTION CHECK NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960112005071996011200507NE 1996 1 12 WTAA950312 219951116A7261 OIL SYSTEM EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE REQ'D SERVICE A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17284UE 120145 ACV - RIGHT ENGINE OIL PRESSURE REPORTED LOW ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. SERVICED ENGINE WITH 2 QUARTS OF OIL. OIL PRESSURE INDICATIONS NORMAL ON ENGINE GROUND RUN. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA31SO E20NE 19960112005081996011200508EU 1996 1 12 WTAA950313 119951118A77228974764 EGT RESISTOR BAG JETSTMJETSTM3101 1500215EU LT ENGINE FAILED A WTAAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 WP17422UE 782 BFL - LEFT ENGINE FAILED TO OBTAIN MINIMUM STATIC TORQUE. TAKEOFF ABANDONED WITHOUT INCIDENT. MAINTENANCE REPLACED AND ADJUSTED LEFT ENGINE EGT COMPENSATING RESISTOR. ENGINE GROUND RUNS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960112005091996011200509 1996 1 12 WTAA950314 419951129A34202TW11 SWITCH BAG JETSTMJETSTM3101 1500215EU COCKPIT FAILED A WTAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP17403UE 743 LAX - AFTER TAKEOFF, BOTH COMPASSES AND HSI'S HAD 'RED' FLAGS IN VIEW. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED COMPASS SELECTOR SWITCH. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960112005101996011200510SO 1996 1 12 WTAA950315 119951204A3260922AA2YA6P PROX SENSOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A WTAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP17286UE 120175 SFO - LEFT MAIN LANDING GAER FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE ADJUSTED LEFT MAIN LANDING GEAR UPLOCK PROXIMITY SENSOR. LANDING GEAR EXTENSION AND RETRACTION NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960112005111996011200511EU 1996 1 12 WTAA950316 119951201A261251224127 FIRE LOOP BAG JETSTMJETSTM3101 1500215EU RT ENGINE SHORTED A WTAAO OTHER N FALSE WARNING CRCRUISE 1 WP17418UE 780 SEA - RIGHT ENGINE FIRE DETECTION LIGHT ILLUMINATED INFLIGHT. MAINTENANCE REPLACED RIGHT ENGINE FIRE DETECTION LOOP. DETECTION SYSTEM FUNCTIONAL CHECK NORMAL. AIRCRAFT RETURNED SERVICE. (M) 2L72 4T RTA21EU 19960112005121996011200512EU 1996 1 12 WTAA950317 119951205A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A WTAAK NONE C F.O.D. APAPPROACH 1 WP17418UE 780 SEAT - BIRD STRIKE REPORTED ON FINAL APPROACH FOR LANDING. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO AIRCRAFT DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960112005131996011200513SO 1996 1 12 WTAA950318 119951208A291012039829011 HYDRAULIC LINE EMB 120 EMB120RT SO LT NACELLE CHAFED A WTAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP17120AM 120012 FAT - CREW REPORTED GREEN HYDRAULIC SYSTEM CONTENT LEVEL DROPPING AFTER DEPARTURE FROM STATION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE FOUND AND REPAIRED CHAFED HYDRAULIC LINE IN LEFT NACELLE WHEEL WELL. HYDRAULIC SYSTEM LEAK CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960112005141996011200514WP 1996 1 12 9522169153 119951207A5330 SKIN DOUG DC9 DC914 3022034WP FS 607-609 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL018912E 45829 DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT LONGERON 19L FROM APPROXIMATELY FS 607 - 609. REPLACED SKIN (P/N 5911416-1) PER EA 91-102616. 2L72 4F A6WE 19960112005151996011200515WP 1996 1 12 9522179307 119951213A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FS 208 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01309RC 48088 DURING H-CHECK, FOUND CORROSION ON THE LEFT OUTBOARD SEAT TRACK FS 208, OUTBOARD FLANGE. REPAIRED TRACK (P/N 5930547-3) PER EA 93-103404. 2L72 4F A6WE 19960112005161996011200516WP 1996 1 12 9522189104 119951227A5220 DOOR PANS DOUG DC9 DC915 3022036WP EMER EXITS CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194S 47204 DURING H-CHECK, FOUND CRACKS IN THE LEFT AND RIGHT OVERWING EMERGENCY EXIT DOOR PANS AT THE UPPER STOPS. REPAIRED PANS (P/N 5913195-1) PER EA 91-103350 AND EA 91-103351. 2L72 4F A6WE 19960112005171996011200517WP 1996 1 12 9522199104 119951228A5330 SKIN DOUG DC9 DC915 3022036WP FS 200 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL0194S 47204 DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AFT OF THE MAIN CABIN DOOR FS 200, AT THE 6TH STOP FROM THE TOP. REPAIRED SKIN (P/N 5911406-59) PER EA 91-102632. 2L72 4F A6WE 19960112005621996011200562SO 1996 1 12 96ZZZX201 119951205A213310274642 VALVE GULSTMG1159 G1159 3953505SO OUTFLOW FAILED A IMKAK NONE O OTHER ININSP/MAINT 1 EA252PK 56364 206 INSTALLED OVERHAULED OUTFLOW VALVE IN A/C. UNIT CHECKED NORMAL IAW MAN. CMP. CARDS. PART FAILED WITH LESS THAN 1.5 HOURS IN AUTO AND MANUAL MODE. INSTALLED SERVICEABLE UNIT, SYSTEM CHECKED NORMAL IAW MAN. CMP. CARDS. A/C RETURNED TO SERVICE. SUSPECT CAUSE: IMPROPER OVERHAUL AND QUALITY ASSURANCE. 2L72 4F RTA12EA 19960116000011996011600001NM 1996 1 16 TWRA9560 119950911A2820BACB30NR12 BOLT BOEING747 747259B NM CTR FUEL TANK LOOSE A TWRAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA152FOR 21730 AFTER TAKEOFF ORY-JFK, FUEL FUMES VERY STRONG IN FLIGHT DECK AREA. FUMES DISSIPATED AT 3.0 TO 4.0 FEET DURING CLIMB. DURING INSPECTION FOUND FUEL LEAK AT BOW TIE FITTING. REMOVED AND REPLACED BOLTS, RESEALED FITTING, IAW EA 57-112. LEAK CHECK OK. (M) 2L74 4F RTA20WE 19960116000021996011600002WP 1996 1 16 96ZZZM11 119951116A2913 HYD PUMP BENDIX 55097 DOUG DC8 DC8F54 3021926WP NR 3 ENG INOPERATIVE A BUFAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE05925BV1691 180252K 45885 DSD-MIA - LOST HYD FLUID DOWN TO AUX SYS IN CRUISE. DECLARED AN EMERGENCY INTO MIA. SERVICED AND OPS GOOD ON GROUND IAW MM 29-01 PG 601. R/R SPOILER PUMP ASSY SERV SYS, OPS CK NORMAL, LEAK CK GOOD IAW MM 27-34-6. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAW MM 27-10-LEAK CK GOOD. INSPECTED AND CLEANED DRAIN LINE NR 3 EDHP IAW MM 29-00 LEAK CK GOOD. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAW MM 29-10-15, LEAK CHECK GOOD. INSPECTED CLEANED CASE DRAIN LINE IAW MM 29-00 LEAK CK GOOD. R/R MAIN HYD SYS FILTERS IAW 29-20-5 LEAK CK GOOD. R/R HYD PUMP ASSY SERV SYS RUN UP CK NORMAL, LEAK CK GOOD IAW MM 29-1-7, NR 2 ENG. R/R HYD PUMP ASSY SERV SYS RUN UP CK NORMAL LEAK CK GOOD IAW MM 29-1-7, NR 3 ENG. (M) 2L74 4F 4A25 19960116000031996011600003WP 1996 1 16 BUFA9526 119951116A2913 HYD PUMP BENDIX 55097 DOUG DC8 DC8F54 3021926WP NR 2 ENG INOPERATIVE A BUFAB EMER. DESCENT KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE05925BV1113 163646K 45885 DSD-MIA - LOST HYD FLUID DOWN TO AUX SYS IN CRUISE. DECLARED AN EMERGENCY INTO MIA. SERVICED AND OPS GOOD ON GROUND IAW MM 29-01 PG 601. R/R SPOILER PUMP ASSY SERV SYS, OPS CK NORMAL, LEAK CK GOOD IAW MM 27-34-6. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAW MM 27-10-LEAK CK GOOD. INSPECTED AND CLEANED DRAIN LINE NR 3 EDHP IAW MM 29-00 LEAK CK GOOD. R/R NR 3 EDHP CASE DRAIN FILTER ELEMENT IAW MM 29-10-15, LEAK CHECK GOOD. INSPECTED CLEANED CASE DRAIN LINE IAW MM 29-00 LEAK CK GOOD. R/R MAIN HYD SYS FILTERS IAW 29-20-5 LEAK CK GOOD. R/R HYD PUMP ASSY SERV SYS RUN UP CK NORMAL, LEAK CK GOOD IAW MM 29-1-7, NR 2 ENG. R/R HYD PUMP ASSY SERV SYS RUN UP CK NORMAL LEAK CK GOOD IAW MM 29-1-7, NR 3 ENG. (M) 2L74 4F 4A25 19960119000101996011900010NM 1996 1 19 9600542712 119950107A7711 ERP CONNECTOR BOEING727 7272S7 138407ZNM PWA JT8 JT8D17 52049NE NR 3 ENGINE LOOSE A NWAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL01712RC 22020 689864 NR 3 EPR INDICATION WAS LIMITED TO 1.4 ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPAIRED A LOSE CONNECTOR FOUND ON THE E-6 CARD FILE IN THE E AND E COMPARTMENT. SUBSEQUENT OPERATIONAL CHECKS WERE SATISFACTORY. 2L73 4F4 F A3WE E2EA 19960119000111996011900011NE 1996 1 19 9600559885 219950103A7320 PT2 PROBE DOUG DC9 DC951 3022051WP PWA JT8 JT8D17 52049NE NR 1 ENGINE ICED UP A NWAACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL01401EA 47682 688727 NR 1 ENGINE EPR DID NOT REACH TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND REMOVED ICE OBSTRUCTING THE PT2 PROBE. ENGINE CHECKED OK ON RUNUP. 2L72 4F4 F A6WE E2EA 19960119000351996011900035WP 1996 1 19 ABXA9600009 119950602A27505751152503 DRIVE LINK DOUG DC8 DC861 3021952WP LT FLAP CRACKED A AABXAK NONE O OTHER ININSP/MAINT 1 GL23846AX 46158 DURING COMPLIANCE OF AD 88-10-07, ASB A27-269, FOUND THE LEFT FLAP DRIVE LINK CRACKED AT POINT-J USING ULTRASONIC METHOD OF INSPECTION. REPLACED LEFT FLAP DRIVE LINK IAW DC8 MM. 2L74 4F 4A25 19960119000361996011900036WP 1996 1 19 ABXA9600010 119950816A5321 FLOOR DOUG DC8 DC863 302198AWP FS 67-52 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23821AX 46113 DURING 821AX C-CHECK INSPECTION, FOUND CORROSION IN THE LEFT COCKPIT FLOOR AREA BELOW COCKPIT SEAT AND BETWEEN FINGER DOUBLER. REPAIRED THE CORRODED COCKPIT FLOOR PRESSURE PANEL AT FUSELAGE STATION -67 TO -52 IAW ABX REA D853-12317MR. 2L74 4F 4A25 19960119000371996011900037WP 1996 1 19 ABXA9600011 119950816A5720 FITTING DOUG DC8 DC863 302198AWP LT WING OVERSIZED HOLES A ABXAK NONE O OTHER ININSP/MAINT 1 GL23821AX 46113 DURING 821AX C-CHECK INSPECTION, FOUND THE LEFT WING LOWER SURFACE BELOW NR 1 PYLON, FORWARD T-FITTING AND FORWARD DOUBLER HAS 6 HOLES OVERSIZED FOR BUSHINGS AND SPAR CAP CRACK INDICATIONS. REPAIRED CRACKS ON LEFT WING LOWER SKIN AND FORWARD SPAR CAP, AFT TANG AT NR 1 PYLON IAW ABX REA D857-12344MR. 2L74 4F 4A25 19960119000381996011900038WP 1996 1 19 ABXA9600012 119950816A5313 LONGERON DOUG DC8 DC863 302198AWP BS 1440 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23821AX 46113 DURING 821AX C-CHECK INSPECTION, STATION 1440 LONGERON 29R TO 31R AT C-4 DOOR CUTOUT AFT SECTION HAS SEVERAL CRACKS. REPAIRED STATION 1440 LONGERON 29R TO 31R C-4 DOOR CUTOUT SECTION THAT HAD SEVERAL CRACKS IAW ABX REA D853-12288MR. 2L74 4F 4A25 19960119000401996011900040WP 1996 1 19 ABXA9600014 119950915A27505751152503 DRIVE LINK DOUG DC8 DC863 302198AWP RT FLAP CRACKED A AABXAK NONE O OTHER ININSP/MAINT 1 GL23815AX 46097 DURING COMPLIANCE OF AD 88-10-07, ASB A27-269, FOUND THE RIGHT FLAP DRIVE LINK CRACKED AT POINT-J USING ULTRASONIC METHOD OF INSPECTION. REPLACED RIGHT FLAP DRIVE LINK IAW DC8 MM. 2L74 4F 4A25 19960119000411996011900041WP 1996 1 19 ABXA9600015 119951115A57205692940 TANK LANDING DOUG DC8 DC863 302198AWP WS 22.75 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND RIGHT WING FUEL TANK LANDING AT PANEL 505F CRACKED. REPAIRED RIGHT WING ACCESS DOOR DOUBLER AT XRS=22.750 IAW ABX REA D857-13080MR. 2L74 4F 4A25 19960119000421996011900042WP 1996 1 19 ABXA9600016 119951115A57205642940 TANK LANDING DOUG DC8 DC863 302198AWP XRS 22.75 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND LEFT WING FUEL TANK LANDING PANEL 505F CRACKED. REPAIRED LEFT WING TOP PANEL ACCESS DOOR DOUBLER AT XRS=22.750 IAW ABX REA D857-13018MR. 2L74 4F 4A25 19960119000431996011900043WP 1996 1 19 ABXA9600017 119951115A5330 SKIN DOUG DC8 DC863 302198AWP BS 1620-1640 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND RIGHT HAND LONGERON 32 AND 33 AT STATION 1620 TO 1640 BULGED AND CORRODED BY SEALANT. REPAIRED CUT OUT IN FUSELAGE SKIN AND INNER DOUBLER AT FUSELAGE STATION 1620, LONGERON 32 AND 33, RIGHT HAND IAW ABX REA D853-13083MR. 2L74 4F 4A25 19960119000441996011900044WP 1996 1 19 ABXA9600018 119951115A5311 FRAME DOUG DC8 DC863 302198AWP BS 1040 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND CORROSION ON FRAME AT FUSELAGE STATION 1040, FROM LONGERON 35R TO 33R. REPAIRED FRAME AT FUSELAGE STATION 1040, LONGERON 35R TO 33R IAW ABX REA D853-13088MR. 2L74 4F 4A25 19960119000451996011900045WP 1996 1 19 ABXA9600019 119951115A5210559764611 SKIN DOUG DC8 DC863 302198AWP L 1 DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND CRACK IN THE L-1 DOOR AFT LOWER CORNER SKIN AND DOUBLER. ALSO, A CRACK IN THE FORWARD LOWER CORNER. REPAIRED FORWARD ENTRY DOOR LOWER AFT CORNER AND SKIN IAW ABX REA D853-13085MR. 2L74 4F 4A25 19960119000461996011900046WP 1996 1 19 ABXA9600020 119951115A5711 SPAR DOUG DC8 DC863 302198AWP WS 69.5 LT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23820AX 46155 DURING 820AX C-CHECK INSPECTION, FOUND LEFT HAND WING LOWER AT STATION 69.5, HOLES 2 THROUGH 5 UNDER SKI FITTING HAVE CRACK INDICATIONS BY HFEC INSPECTION. ALL CRACKS ARE IN SPAR AND ALL CRACKS ARE ON OUTBOARD SIDE OF HOLES. REPAIRED LEFT HAND LOWER REAR SPAR CAP AT HOLES 2 THROUGH 5 UNDER SKI FITTING AT STATION 69.5 IAW ABX REA D857-13087MR. 2L74 4F 4A25 19960119000811996011900081EU 1996 1 19 96ZZZX211 119951109A3397 WIRE BRAERODH125 HS125700A 4230170EU CABIN BURNED A AKKYAK NONE O OTHER ININSP/MAINT 1 NE0381KA 9297 NA0227 WHILE PREPARING ACFT TO INSTALL AEROSPACE LIGHTING CORPORATION'S PROTECTED POWER SUPPLIES IN THE CABIN FLUORESCENT LIGHTING SYSTEM, AN INSPECTION OF THE HIGH VOLTAGE WIRING REVEALED A SHORT LENGTH OF WIRE THAT HAD BURNED INSULATION. THERE WAS NO DAMAGE TO ANY EQUIPMENT OR STRUCTURE IN THE AREA. A COMPLETE INSPECTION OF THE HIGH VOLTAGE WIRE SYSTEM UNCOVERED SEVERAL SPOTS WHERE IT APPEARED THAT HIGH VOLTAGE HAD ARCED BETWEEN 2 WIRES (BROWN PIN HOLES). ALL OF THESE SPOTS WERE LOCATED WHERE THE WIRE HAD BEEN TIE-WRAPPED TOGETHER. THE PROTECTED POWER SUPPLIES THAT ARE BEING INSTALLED WOULD HAVE SHUT THE SYSTEM DOWN IN THIS CONDITION. AD 90-14-06 HAD BEEN C/W. MFG P/N, MIL SPEC W-16878. 2L72 4F A3EU 19960119000821996011900082SO 1996 1 19 96ZZZX212 119951215A28201159H40200143 VAPOR VENT LINE SUNDSTRANDEM1159SCP0115 GULSTMG1159 G1159A 3970109SO RT MLG WW LEAKING ASACOZAK NONE K FLUID LOSS ININSP/MAINT 1 WP27492A 428 1944 425 DURING POST-FLIGHT INSPECTION, A HEAVY FUEL SMELL WAS NOTED IN THE RT MLG WHEELWELL. ON INVESTIGATION, FOUND FUEL WEEPING FROM THE RT ALTERNATE BOOST PUMP VAPOR VENT LINE AND COLLECTING IN THE WHEELWELL. FAILED VAPOR VENT LINE, PN 1159H40200-143, WAS INSTALLED IN THIS AIRCRAFT ON 3-8-95 AND WAS A REPLACMENT FOR VENT LINE, PN 661002-6D0150, WHICH HAS AN 8-YEAR SCRAP LIFE DUE TO SIDEWALL WEEPING. (SEE SDR FOR N404CC DATED 11-22-94). TOTAL TIME ON FAILED VENT LINE 428 HOURS, 144 LANDINGS, 9 MONTHS. LINE HAS BEEN SENT TO GULFSTREAM, SAVANNAH FOR EVALUATION. 2L72 4F A12EA 19960119000831996011900083CE 1996 1 19 96ZZZX213 119951208A2820 FUEL BOWL BEECH 99 C99 1154006CE AIRFRAME LEAKING A GUUAK NONE BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS ININSP/MAINT 1 SO19229BH U231 FPO/MIA - FLT 416 - PILOT REPORT: INSIDE AIRCRAFT, SMELLS OF FUEL. MAINTENANCE: DETERMINED AIRFRAME FUEL BOWL TO BE SLIGHTLY LEAKING. RESECURED BOWL, LEAK CHECK GOOD. 1L72 3T A14CE 19960119000851996011900085NE 1996 1 19 96ZZZX215 219951224A73217898426009 ELEC ENG CONT DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 1 ENGINE FAILED A APCAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 EA13825EX1589 91020136 388 121347 LGA - UPON CLIMB-OUT, NR 1 ENGINE EXPERIENCED AN UNSCHEDULED FEATHERING OF THE PROPELLER. MAXIMUM ENGINE TORQUE APPROXIMATELY 109 PERCENT FOR 5 SECONDS. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO THE FIELD. REMOVED AND REPLACED NR 1 TSCU AND NR 1 ECU. CLEANED AND INSPECTED CANNON PLUGS. GROUND RUN CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL NR PCAA9500256. AIRCRAFT TOTAL CYCLES, 3,524. 2H72 4T4 TRTA13NM E20NE 19960119000861996011900086WP 1996 1 19 96ZZZX216 119951227A326010648LD2359 LENS LKHEED1011 10113851 5265010WP LT MLG INOPERATIVE A TWAAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 CE0511003 193B1015 STL - FLT 86 - PRIOR TO LANDING, LT MLG GREEN LIGHT WAS INOPERATIVE RESULTING IN A FLY-BY. REPLACED LENS, MFG PN 10648 LD 2-359. CHECK C-10A - 11-24-95. 2L73 4F A23WE 19960119000871996011900087WP 1996 1 19 96ZZZX217 119951230A3150H05A0035A AURAL WARNING DOUG DC9 DC982 3022082WP COCKPIT FAILED A TWAACD ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE05916TW 49187 STL - FLT 116 - DURING TAKEOFF, AN ELECTRICAL SMELL WAS DETECTED IN THE COCKPIT. TROUBLESHOOTING REVEALED THE AURAL WARNING BOX WAS FAULTY. REMOVED AND REPLACED AURAL WARNING BOX, MFG PN H05A0035-A. OPERATIONAL CHECK NORMAL. CHECK C-1D - FEBRUARY 2, 1995 - MCI. 2L72 4F A6WE 19960119000881996011900088NE 1996 1 19 96ZZZX218 219951231A75327733333 BLEED VALVE BOEING767 767205 1385121NM PWA JT9 JT9D7R4D 52054NE RT ENGINE MALFUNCTIONED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE05650TW 23057 4626 LAX - FLT 8595 - DURING CRUISE, SHUT DOWN NR 2 ENGINE, SN 4626, DUE TO SURGING. REMOVED AND REPLACED RT ENGINE BLEED CONTROL VALVE, MFG PN 773333-3. PERFORMED BORESCOPE INSPECTION OF 5TH, 6TH, 8TH, AND 14TH COMPRESSOR STAGES AND 1ST, 2ND, AND 3RD TURBINE STAGES. NO DISCREPANCIES FOUND. OPERATIONAL CHECK NORMAL. ENGINE TOTAL TIME: 34,097 HOURS; 8,432 CYCLES. CHECK C-4C - 10-25-95 - LAX. 2L72 4F4 FRTA1NM E3NE 19960119000891996011900089EA 1996 1 19 96ZZZX219 119951228A561017180003 WINDOW DHAV DHC8 DHC8311 1386006EA LT COCKPIT CRACKED A MASAK NONE O OTHER CRCRUISE 1 SW01431AW10146 284 DEN - AIRCRAFT WAS IN-FLIGHT EN ROUTE TO DEN WHEN PILOT NOTICED HIS SIDE WINDOW (LEFT) HAD CRACKED. AIRCRAFT PROCEEDED DEN WHERE THE WINDOW WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA13NM 19960119000901996011900090EA 1996 1 19 96ZZZX220 119951228A561017180003 WINDOW DHAV DHC8 DHC8311 1386006EA LT COCKPIT CRACKED A MASAK NONE O OTHER CRCRUISE 1 SW01432AW9472 286 DEN - AIRCRAFT WAS IN-FLIGHT EN ROUTE TO DEN WHEN THE PILOT NOTICED HIS SIDE (LEFT) WINDOW HAD CRACKED, AIRCRAFT PROCEEDED TO DEN WHERE THE WINDOW WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19960119000911996011900091WP 1996 1 19 96ZZZX221 119951212A3310HKXB FUSE HOLDER 57696391 DOUG DC8 DC8F54 3021926WP COCKPIT FAILED A FXLAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO197046H 46011 MIA - ON APPROACH MIA, EXPERIENCED STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. INSPECTION REVEALED A BLOWN 2-AMP FUSE IN THE PILOT'S OVERHEAD PANEL. REPLACED DEFECTIVE FUSE HOLDER AND RETURNED AIRCRAFT TO SERVICE. 2L74 4F 4A25 19960119000921996011900092WP 1996 1 19 96ZZZX222 119951216A291061105340534 HOSE DOUG DC8 DC8F54 3021926WP HYDRAULIC PUMP LEAKING A FXLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO1954FA 45637 SJU - DURING CLIMB, EXPERIENCED LOSS OF HYDRAULIC FLUID AND QUANTITY. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A PIN HOLE IN THE PRESSURE HOSE TO THE RUDDER STANDBY HYDRAULIC PUMP. REPLACED HYDRAULIC PRESSURE HOSE AND RETURNED AIRCRAFT TO SERVICE. 2L74 4F 4A25 19960119000931996011900093NE 1996 1 19 96ZZZX223 219951219A73212436024 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE LT ENGINE FAILED A TWAAE ENGINE SHUTDOWN O OTHER LDLANDING 1 CE05925L 47357 2164 ATL - FLT 605 - DURING LANDING TOUCHDOWN LEFT AND RIGHT ENGINES, 2164-L, 2146-R, SPOOLED DOWN. COMPLETED LANDING PROCEDURES. REPLACED LEFT ENGINE FUEL CONTROL, MFG PN 243602-4, AND RIGHT ENGINE FUEL CONTROL, MFG PN 243602-3. ENGINE OPERATION AND PERFORMANCE CHECKED NORMAL. LEFT ENGINE S/N 2164 - TOTAL TIME: 51,272 HOURS, CYCLES, 60,004. RIGHT ENGINE S/N 2146 - TOTAL TIME: 56,299 HOURS, CYCLES, 66,976. CHECK C-5-14-95 - STL. REFERENCE OPERATOR CONTROL NR 96ZZZX224. 2L72 4F4 F A6WE E2EA 19960119000941996011900094NE 1996 1 19 96ZZZX224 219951219A73212436023 FUEL CONTROL DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE RT ENGINE FAILED A TWAAE ENGINE SHUTDOWN O OTHER LDLANDING 1 CE05925L 47357 2146 ATL - FLT 605 - DURING LANDING TOUCHDOWN LEFT AND RIGHT ENGINES, 2164-L, 2146-R, SPOOLED DOWN. COMPLETED LANDING PROCEDURES. REPLACED LEFT ENGINE FUEL CONTROL, MFG PN 243602-4, AND RIGHT ENGINE FUEL CONTROL, MFG PN 243602-3. ENGINE OPERATION AND PERFORMANCE CHECKED NORMAL. LEFT ENGINE S/N 2164 - TOTAL TIME: 51,272 HOURS, CYCLES, 60,004. RIGHT ENGINE S/N 2146 - TOTAL TIME: 56,299 HOURS, CYCLES, 66,976. CHECK C-5-14-95 - STL. REFERENCE OPERATOR CONTROL NR 96ZZZX223. 2L72 4F4 F A6WE E2EA 19960119000951996011900095WP 1996 1 19 96ZZZX225 119951129A5347 SEAT TRACK DOUG DC9 DC933F 302207AWP BS 234 BS 210 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05937F 47409 DURING OP-15, FOUND CORROSION ON GALLEY FLOOR, RT INBOARD SEAT TRACK, UNDER NR 2 GALLEY, STA 234 AND STA 210. REPLACED SEAT TRACK SECTION PER SRM 53-05. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704, CYCLES. 2L72 4F A6WE 19960119000961996011900096WP 1996 1 19 96ZZZX226 119951124A5315 FLOOR BEAM DOUG DC9 DC933F 302207AWP BS 200 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05937F 47409 STL - DURING OP-15, FOUND A 1.50 INCH CRACK IN FLOOR BEAM STA 200. REPAIRED PER ARA 8794. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704 CYCLES. 2L72 4F A6WE 19960119000971996011900097WP 1996 1 19 96ZZZX227 119951124A5313 LONGERON DOUG DC9 DC933F 302207AWP BS 465 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05937F 47409 STL - DURING OP-15, FOUND A .25 INCH CRACK IN LONGERON 10R, STA 465. REPAIRED PER SRM 53-11-2, FIGURE 2. AIRCRAFT TOTAL TIME: 64,684 HOURS, 61,704 CYCLES. 2L72 4F A6WE 19960119000981996011900098WP 1996 1 19 96ZZZX228 119951122A5530 ANGLE DOUG DC9 DC951 3022051WP VERTICAL STAB CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05416EA 47751 STL - DURING CHECK C, FOUND A 2.50 INCH CRACK AT LEFT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, FS 1292. REPAIRED PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES. 2L72 4F A6WE 19960119000991996011900099WP 1996 1 19 96ZZZX229 119951122A5530 ANGLE DOUG DC9 DC951 3022051WP VERTICAL STAB CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05416EA 47751 STL - DURING CHECK C, FOUND A .3750 INCH CRACK IN RIGHT SIDE OF VERTICAL STABILIZER ATTACH ANGLE, STA 1292. REPAIRED BY INSTALLLING DOUBLER PER SRM 53-05, FIGURE 23. AIRCRAFT TOTAL TIME: 40,618 HOURS, 36,293 CYCLES. 2L72 4F A6WE 19960119001001996011900100NE 1996 1 19 96ZZZX230 219951215A7260467572P3 BUSHING BOEING727 727231 1384079NM PWA JT8 JT8D15 52051NE NR 1 ENG GRBOX FAILED A TWAAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE0554342 21629 4026 ATL- FLT 554 - DURING CRUISE, NR 1 ENGINE, SN 4026, SPUN DOWN. SHUT DOWN ENGINE. FOUND ACCESSORY GEARBOX HAD INTERNAL MALFUNCTION. REPLACED ENGINE AND ENGINE OPERATION CHECK NORMAL. ENGINE TOTAL TIME: 49,589 HOURS, 33,419 CYCLES. CHECK C-1 - 3-7-95 - MCI. INVESTIGATION INTO ENGINE, SN 4026, GEARBOX FAILURE REVEALED A BUSHING, MFG PN 467572P3, ALLOWED GEAR TO MIGRATE CAUSING RAPID TOOTH WEAR RESULTING IN GEARBOX FAILURE. GEARBOX REPAIRED AND RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 19960119001011996011900101WP 1996 1 19 96ZZZX231 119951215A2410696233B CSD DOUG DC9 DC951 3022051WP NR 2 ENGINE FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05410EA 47731 STL - FLT 126 - AFTER TAKEOFF, NR 2 CSD LOW PRESSURE LIGHT CAME ON. NR 2 CSD DISCONNECTED. REMOVED AND REPLACED CSD, MFG PN 696233B, OPERATIONAL AND LEAK CHECK OKAY. ENGINE TOTAL TIME: 34,358 HOURS, 32,155 CYCLES. CHECK C-12 - 1-11-95 - STL. 2L72 4F A6WE 19960119001021996011900102WP 1996 1 19 96ZZZX232 119951211A2170 COALESER SOCK DOUG DC9 DC932 3022066WP LT/RT DIRTY A TWAAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 CE05998R 47030 STL - FLT 363 - FOLLOWING AN ENGINE CHANGE, DURING TAKEOFF, FLIGHT ATTENDANTS REPORTED A BURNING SMELL AT MID-CABIN. REMOVED AND REPLACED RIGHT AND LEFT WATER SEPARATORS. OPERATIONAL CHECK NORMAL. CHECK C - 12-19-94 - STL. 2L72 4F A6WE 19960119001031996011900103NM 1996 1 19 96ZZZX233 119951210A731270034115A HEAT VALVE BOEING727 727231 1384079NM PWA JT8 JT8D5 52046NE NR 1 ENGINE FAILED A TWAAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE0584355 21987 STL - FLT 192 - DURING CLIMB, NR 1 ENGINE FUEL HEAT VALVE INTRANSIT LIGHT STAYED ON WITH SWITCH IN THE OFF POSITION. SHUT DOWN NR 1 ENGINE AND RETURNED FROM FLIGHT. REMOVED AND REPLACED NR 1 ENGINE FUEL HEAT VALVE, MFG PN 700341-15A. OPERATIONAL CHECK NORMAL. OP-17 - 1-8-95 - MCI. 2L73 4F4 F A3WE E2EA 19960119001041996011900104NM 1996 1 19 96ZZZX234 119951117A5320 BEARSTRAP BOEING727 727231 1384079NM DOOR CUTOUT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING CHECK C, FOUND CRACK IN BEARSTRAP, FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER. REPAIRED PER SSRM 53-30-206, PAGES 201-213, FIGURE 202. AIRCRAFT TOTAL TIME: 63,044 HOURS, 42,507 CYCLES. 2L73 4F A3WE 19960119001051996011900105WP 1996 1 19 96ZZZX235 119951205A3260 TARGET ASSY DOUG DC9 DC982 3022082WP RT MLG LOOSE A TWAAO OTHER N FALSE WARNING CLCLIMB 1 CE05955U 49427 STL - FLT 159 - AFTER TAKEOFF, THE RT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED WITH GEAR HANDLE IN THE UP POSITION. FOUND RT GEAR TARGET ASSEMBLY LOOSE. SECURED TARGET ASSEMBLY WITH BELT, MFG PN NAS6203-2H. PERFORMED MM SENSOR CHECK, OPERATIONAL CHECK NORMAL. CHECK C-2D - 10-17-95 - MCI. 2L72 4F A6WE 19960119001061996011900106NM 1996 1 19 96ZZZX236 119951117A5320 FORMER BOEING727 727231 1384079NM FS 1030 DENTED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING CHECK C, FOUND .3750 INCH DENT ON TOP SIDE OF AFT CARGO FORMER RING, FS 1030. REPAIRED PER SSRM 53-60-202, PAGE 201. AIRCRAFT TOTAL TIME: 63,044 HOURS, 42,507 CYCLES. 2L73 4F A3WE 19960119001071996011900107NM 1996 1 19 96ZZZX237 119951118A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564315 20048 DURING CHECK C, FOUND CORROSION AT BOTTOM EDGE OF AFT LAV SERVICE COMPARTMENT SKIN, LT SIDE OF FUSELAGE. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, FIGURE 3-5-3A. AIRCRAFT TOTAL TIME: 66,911 HOURS, 45,166 CYCLES. 2L73 4F A3WE 19960119001081996011900108NM 1996 1 19 96ZZZX238 119951118A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564315 20048 JFK - DURING CHECK C, FOUND CORROSION IN AFT LAV SERVICE COMPARTMENT PRODUCTION EDGE AFT EDGE, AND DISTRESSED RIVET HEAD LT SIDE OF FUSELAGE. REMOVED CORROSION AND DAMAGED SKIN AND INSTALLED DOUBLER REPAIRS PER SRM 53-30-03, FIGURE 3-5-3A. AIRCRAFT TOTAL TIME: 66,911 HOURS, 45,166 CYCLES. 2L73 4F A3WE 19960119001091996011900109NM 1996 1 19 96ZZZX239 119951204A339758541 WIRE BOEING767 767231 1385131NM CABIN FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05608TW 22571 LAX - FLT 810 - DURING A TEST OF THE EGRESS LIGHTING SYSTEM, THE AFT COACH SECTION DID NOT ILLUMINATE. REMOVED AND REPLACED ONE EACH FLEX CABLE, MFG PN 5854-1 AND CHECK C-4D - 11-25-95 - LAX. 2L72 4F RTA1NM 19960119001101996011900110NM 1996 1 19 96ZZZX240 119951118A5712 RIB BOEING727 727231 1384079NM WS 738.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564315 20048 JFK - DURING CHECK C, FOUND CRACK IN LOWER EDGE RADIUS, LW RIB STA 738.5, STR 6 AND STR 8, AFT OF ACCESS HOLE. REPAIRED PER SRM 57-10-05. AIRCRAFT TOTAL TIME: 66,911 HOURS, 45,166 CYCLES. 2L73 4F A3WE 19960119001111996011900111NM 1996 1 19 96ZZZX241 119951118A5712 RIB BOEING727 727231 1384079NM WS 686.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564315 20048 JFK - DURING CHECK C, FOUND CRACK IN RIB AT WS 686.5, LT SIDE. REPAIRED BY STOP-DRILLING CRACK AND INSTALLED REPAIRED DOUBLER PER SRM 57-10-05, FIGURE 1. AIRCRAFT TOTAL TIME, 66,911 HOURS, 45,166 CYCLES. 2L73 4F A3WE 19960119001121996011900112NM 1996 1 19 96ZZZX242 119951118A5313 STRINGER BOEING727 727231 1384079NM BS 601.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564315 20048 JFK - DURING CHECK C, FOUND CRACK EXTENDING BEYOND BOLT HOLE ON STR 13R, STA 601.5. STOP DRILLED AND REPAIRED PER SB 727-57A-159. AIRCRAFT TOTAL TIME: 66,911 HOURS, 45,166 CYCLES. 2L73 4F A3WE 19960119001131996011900113WP 1996 1 19 ASAA9580276 119951124A5210 HANDLE DOUG DC9 DC983 3022083WP L1 DOOR LACK OF LUBE A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01977AS 53453 LAX - FLT 257 - ON ARRIVAL, CREW REPORTED THE L1 DOOR HANDLE RELEASE STICKS. LUBRICATED HANDLE ASSEMBLY AND OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19960119001141996011900114WP 1996 1 19 ASAA9580292 119951212A5347TMS6019609 CARGO TRACK DOUG DC9 DC982 3022082WP BS 427-BS 637 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS28126 49364 PAE - DURING 30K CHECK, CORROSION FOUND ON CARGO TRACK AT Y427 TO Y637, X-17, Z-44.5. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9, SRM 51-10-03 AND SRM 51-30-01, SRM 51-30-02 AND SRM 53-05. PART TAC, 19,401. (X) 2L72 4F A6WE 19960119001151996011900115WP 1996 1 19 ASAA9580293 119951216A5210 LOCKWASHER DOUG DC9 DC982 3022082WP L1 DOOR BROKEN A ASAAK NONE O OTHER ININSP/MAINT 1 NM01937AS 49364 OAK - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO CLOSE. FOUND LOCKWASHER TAB BROKEN ON DOOR ROTATION ADJUSTMENT ROD. REPLACED LOCKWASHER AND CHECKED ADJUSTMENT AND DOOR OPERATED NORMALLY. (X) 2L72 4F A6WE 19960119001161996011900116SO 1996 1 19 ASOA95026 119951210A3150992161H111791 SWITCH EMB 120 EMB120RT SO COCKPIT DEFECTIVE A ASOAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO11242AS 120069 ATL/DHN - FLT 7104 - AFTER TAKEOFF, CREW NOTICED WHITE SMOKE COMING FROM UNDER THE FIRST OFFICER'S GLARESHIELD PANEL AROUND THE ALARM CANCEL BUTTON. THE CAPTAIN DECIDED TO RETURN TO ATL WITH EMERGENCY VEHICLES STANDING BY. LANDING WAS MADE SAFELY WITHOUT INCIDENT, NO ASSISTANCE REQUIRED. REMOVED AND REPLACED FIRST OFFICER'S ALARM CANCEL SWITCH. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. TAT: 20,377.6 HOURS. (X) 2L72 4T RTA31SO 19960119001171996011900117NM 1996 1 19 CAL950910 119951010A304069345111 RESERVOIR BOEING737 737524 1384721NM RAIN REPELLENT LEAKING A CALAA UNSCHED LANDING BG SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CRCRUISE 1 SW0916632 27900 CLE - FLT 1219 - TOXIC FUMES WERE SMELLED IN COCKPIT & CABIN WHILE EN ROUTE FROM DTW TO EWR. THE OXYGEN MASKS WERE DEPLOYED AND ACFT DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MX FOUND RAIN REPELLANT RESERVOIR LEAKING FLUID. RAIN REPELLANT RESERVOIR WAS REMOVED AND REPLACED. LEAK & OPERATIONAL CHECKS WERE GOOD. IN ADDITION, RT ACM WAS REMOVED AND REPLACED DUE TO EVIDENCE OF OIL LEAKAGE. AN INSP OF LT & RT COALESCER BAGS FOUND NO EVIDENCE OF CONTAMINATION, BUT RT BAG FOUND FROZEN DUE TO FAULTY 35 DEGREE TEMP CONTROLLER. TEMP CONTROLLER REPLACED. MX REPORTED ALL OXY MASKS HAD DEPLOYED. EXPENDED OXY GENERATORS REPLACED & OXY MASKS STOWED IAW MM 35-22-31, PAGE 201. (X) 2L72 4F RTA16WE 19960119001181996011900118NM 1996 1 19 CAL951046 119951113A575465C26602312SP SKIN BOEING737 737524 1384721NM NR 5 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09336085087 27321 IAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT INBOARD END OF NR 5 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02394. (X) 2L72 4F RTA16WE 19960119001191996011900119NM 1996 1 19 CAL951047 119951113A575465C26603202SP SKIN BOEING737 737524 1384721NM NR 4 LE SLAT CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09336085087 27321 IAH - FLT 1879 - INSPECTION FOUND A 3 INCH CRACK IN LOWER SKIN AT OUTBOARD END OF NR 4 LEADING EDGE SLAT. A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW ECRA 5750-02393. (X) 2L72 4F RTA16WE 19960119001201996011900120NM 1996 1 19 CAL951059 119951108A3350 FUSE BOEING737 7373Q8 1384670NM CABIN FAILED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0914381 26310 CLE - FLT 1549 - THE LT OVERWING INTERIOR EXIT LIGHT FAILED TO ILLUMINATE ON TEST. MAINTENANCE FOUND A BAD FUSE IN THE BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (X) 2L72 4F RTA16WE 19960119001211996011900121WP 1996 1 19 GRAA9558 119951212A335060030431 POWER SUPPLY DOUG DC9 DC982 3022082WP CABIN INOPERATIVE A GRAAK NONE L NO TEST ININSP/MAINT 1 WP11500TR 49144 AFT OVERWING LIGHTS WOULD NOT SHUT OFF AFTER PERFORMING AN OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY AND OPERATIONALLY CHECKED LIGHTS WITH SATISFACTORY RESULTS. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A6WE 19960119001221996011900122EA 1996 1 19 MESA310901 119951220A3230 RETRACT MECH DHAV DHC8 DHC8311 1386006EA RT MLG MALFUNCTIONED A MASAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW01436AW 336 GJT - AIRCRAFT TOOK OFF FROM GJT, PILOT RADIOED THAT HIS RIGHT GEAR DOOR AMBER ANNUNCIATOR HAD REMAINED ILLUMINATED AFTER GEAR RETRACTION, PILOT THEN CYCLED GEAR AND RECEIVED A RED RIGHT GEAR UNSAFE INDICATION, HE THEN ALTERNATELY EXTENDED THE RIGHT GEAR AND RETURNED TO GJT. GJT MAINTENANCE JACKED AIRCRAFT, CLEARED PSEU MEMORY TO BEGIN TROUBLESHOOTING, PERFORMED NUMEROUS RETRACTIONS AND EXTENSIONS WITHOUT BEING ABLE TO DUPLICATE DISCREPANCY. AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19960119001231996011900123NM 1996 1 19 PCAA9500256 119951224A7712311836502 SIG COND UNIT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE FAILED A APCAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA13825EX3064 MM4520 388 LGA - UPON CLIMB-OUT, NR 1 ENGINE EXPERIENCED AN UNSCHEDULED FEATHERING OF THE PROPELLER. MAXIMUM ENGINE TORQUE APPROXIMATELY 109 PERCENT FOR 5 SECONDS. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO THE FIELD. REMOVED AND REPLACED NR 1 TSCU AND NR 1 ECU. CLEANED AND INSPECTED CANNON PLUGS. GROUND RUN CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE: OPERATOR CONTROL 96ZZZX215. AIRCRAFT TOTAL CYCLES, 3,524. (X) 2H72 4T RTA13NM 19960119001241996011900124NM 1996 1 19 PCAA9500259 119951226A792128E997 OIL COOLER DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE LEAKING A PCAAE ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS NRNOT REPORTED 1 EA13800MX16376551 850654 007 NR 1 ENGINE OIL PRESSURE DROPPED TO 30 PSI. SHUT DOWN NR 1 ENGINE, ASSOCIATED WARNING LIGHT ALSO ILLUMINATED. COMPLETED PRATT AND WHITNEY MM 03-50-00, LOW OIL PRESSURE INSPECTION. REPLACED SCAVENGE FILTER. FOUND NR 1 ENGINE OIL COOLER LEAKING THROUGH FINS, REMOVED AND REPLACED OIL COOLER. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA13NM 19960119001251996011900125EU 1996 1 19 REXA95071 119951217A2120 AIR DISTRIBUTOR BAG JETSTMJETSTM3101 1500215EU CABIN FOG A REXAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO25304PX 663 PASSENGER REPORTS SMOKE IN CABIN. PERFORMED GROUND RUN OF BOTH ENGINES. DID DUPLICATE SMOKE IN CABIN BY SELECTING RT ACM FLOW TO COLD POSITION DUE TO ATMOSPHERIC CONDITIONS INSIDE AND OUTSIDE THE AIRCRAFT - IT WAS FOG INSIDE THE CABIN (APPEARING TO BE SMOKE). NO DEFECTS NOTED, OK FOR SERVICE. (X) 2L72 4T RTA21EU 19960119001261996011900126NE 1996 1 19 REXA95072 219951218A7200 ENGINE SAAB SF340 SF340A 7850100EU GE CT7TP CT75A2 30030NE LEFT FLAMED OUT A REXAO OTHER X ENGINE FLAMEOUT CRCRUISE 1 SO25344AM19613 340A030 GEE367241KU LEFT ENGINE FLAME-OUT. AUTO RE-START, TEMP RISE LEFT SIDE, PLUS 20 DEGREES CELSIUS. NO FURTHER PROBLEM NOTED, OAT MINUS 7 DEGREES CELSIUS, ENGINE ANTI-ICE AND PROPELLER HEAT ON. SUSPECT LEFT ENGINE INGESTED ICE. BRIGHT LIGHT INSPECTED, LEFT ENGINE, STAGE 1 COMPRESSOR BLADES. NO DAMAGE NOTED. PERFORMED GPA RUNS. ALL PARAMETERS WITHIN LIMITS. AIRCRAFT OK FOR SERVICE. (X) 2L72 4T4 TRTA52EU E8NE6 19960119001271996011900127EU 1996 1 19 REXA95073 119951218A2612899253 FIRE LOOP SAAB SF340 SF340A 7850100EU LT ENGINE DAMAGED A REXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25404BH 340A061 JAN - WHILE EN ROUTE TO JAN, L-FIRE DETECT CWP ILLUMINATED. RAN CHECKS AND CALLED DISPATCH. RT BASE. REMOVED AND REPLACED LEFT ENGINE FIRE DETECTION LOOP. OPERATIONAL CHECK GOOD. (X) 2L72 4T RTA52EU 19960119001281996011900128SO 1996 1 19 SRAA129504 119951225A3260 SWITCH LKHEED382 382G 526414USO RT MLG OUT OF ADJUST A SRAAK NONE N FALSE WARNING DEDESCENT 1 SO19920SJ 4561 PILOT REPORT DURING LANDING APPROACH, RT MLG WOULD NOT EXTEND WITHOUT G-FORCE. SUPPORT AIRCRAFT ON JACKS, INSPECT MAIN LANDING GEAR RETRACTION MECHANISM, FOUND SWITCH OUT OF ADJUSTMENT, ADJUSTED POSITION INDICATOR IAW CH 32, OPS CHECKED GOOD. (X) 2H74 4T A1SO 19960119001291996011900129NE 1996 1 19 TWRA9571 219951216A75307479958 EVC BOEING747 747282B 1384860NM PWA JT9 JT9D7A 52054NE NR 2 ENGINE WORN A TWRAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15611FF 20502 662934 DURING CLIMB-OUT, FLIGHT CREW EXPERIENCED AN OIL SMELL IN THE COCKPIT AND CABIN. SMELL CLEARED AFTER POWER WAS REDUCED. REPLACED NR 2 ENGINE'S ENGINE VANE CONTROL. (X) 2L74 4F4 F A20WE E20EA 19960119001301996011900130NM 1996 1 19 USAA951214 119951109A5330 SKIN BOEING757 7572B7 1384964NM FS 1310 PITTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19617AU8535 27148 CLT - DURING CMV-2 CHECK INSPECTION, FOUND LIGHTNING STRIKE ON SKIN AT FS 1310 BETWEEN S27L AND S28L. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-00-01, FIGURE 203 AND USAIR EA 40270. (X) 2L72 4F RTA2NM 19960119001311996011900131EU 1996 1 19 VTZA96050 219951227A7310HTE400064 NON-RETURN VALVE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE331* 01514WP RT WING FAILED A AVTZAA UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 EA27496UE 4987 900 P66203 IAD/PIT - FLT 6332 - DURING CRUISE AT 1830 HOURS ON 12-27-95, RETURNED TO IAD DUE TO THE RT ENGINE ALMOST FLAMING OUT WHEN CROSSFEED WAS SELECTED OFF. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT BOOST PUMP NON-RETURN VALVE. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E2WE 19960119001321996011900132EU 1996 1 19 VTZA96052 119951228A3060660712263 SLIP RING BAG JETSTMJETSTM3201 1500217EU RT ENGINE WORN A VTZAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA27484UE 899 IAD/CMH - FLT 6286 - DURING CRUISE AT 0900 HOURS ON 12-28-95, RETURNED TO IAD DUE TO THE RT PROPELLER DEICE BOOTS DRAWING TOO LITTLE AMPERAGE. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE RT PROPELLER SLIP RING. OPS CHECK GOOD. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19960119001331996011900133EU 1996 1 19 VTZA96053 119951229A527091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR LACK OF LUBE A VTZAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 EA27488UE 907 IAD/RDU - FLT 6590 - DURING CRUISE AT 1851 HOURS ON 12-29-95, RETURNED TO IAD DUE TO THE PASSENGER DOOR WARNING LIGHT ILLUMINATING. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE LUBRICATED MICROSWITCH ASSEMBLY. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA56EU 19960119001341996011900134NE 1996 1 19 VTZA96054 219951229A7321310590U6 FUEL CONTL UNIT JETAIRJETSTMJETSTM4101 1500501EU GARRTTTPE331TPE33114 01514NE LT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27305UE282 41019 P75098 IAD/RDU - FLT 6576 - DURING TAKEOFF AT 0855 HOURS ON 12-29-95, ABORTED TAKEOFF DUE TO LEFT IEC CAP LIGHT ILLUMINATING DURING TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED THE FLIGHT IDLE FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T4 TRTA41NM E18NE 19960119001351996011900135EU 1996 1 19 VTZA96055 119951223A5270SF4594 SWITCH JETAIRJETSTMJETSTM4101 1500501EU BAGGAGE DOOR LACK OF LUBE A VTZACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA27320UE 41043 IAD/MHT - FLT 6203 - DURING TAKEOFF AT 1210 HOURS ON 12-23-95, ABORTED TAKEOFF DUE TO BAGGAGE DOOR LIGHT CAME ON. AICRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED AND LUBED MICROSWITCHES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA41NM 19960119001361996011900136WP 1996 1 19 VTZA96056 219951228A732189778025 FUEL CONTL UNIT BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE331* 01514WP RT ENGINE OUT OF ADJUST A VTZACD ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA27487UE8223 1965 906 P66008 MDT/IAD - FLT 6196 - DURING TAKEOFF AT 0955 HOURS ON 12-28-95, ABORTED TAKEOFF DUE TO THE RT ENGINE NOT DEVELOPING TARGET TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED MAXIMUM FUEL FLOW. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T3 TRTA56EU E2WE 19960119001391996011900139NM 1996 1 19 W8PA9491 119951221A32301030874 SOLENOID BOEING737 737301 1384611NM GEAR HANDLE FAILED A W8PAA UNSCHED LANDING O OTHER CLCLIMB 1 WP05949WP 23230 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE UP PAST THE OFF POSITION. AIRCRAFT RETURNED TO COS. FOUND M-241 LEVER LATCH SOLENOID DEFECTIVE. REMOVED AND REPLACED SOLENOID. (X) 2L72 4F RTA16WE 19960119001401996011900140NM 1996 1 19 W8PA9601 119951228A3397 WIRE BOEING737 7373L9 1384470NM CABIN BROKEN A W8PAK NONE L NO TEST ININSP/MAINT 1 NM03960WP 23331 EXPOSED WIRING AT ROW 12 ON EMERGENCY TRACK LIGHTING. SPLICED EMERGENCY TRACK WIRING TOGETHER. REINSTALLED TRACK. (X) 2L72 4F RTA16WE 19960119001411996011900141 1996 1 19 WRLA95046 419951127A34426225136001 ANTENNA PEDESTAL DOUG MD11 MD11 3023602NM RADAR SYSTEM FAILED A WRLAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27271WA 48518 WMKK - DURING CLIMB-0UT AFTER TAKEOFF WHEN FLIGHT CREW SWITCHED RADAR FROM STANDBY TO 'ON' MODE, BOTH SYSTEMS FAILED. AIRCRAFT LANDED AT WMKK WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE RADAR SYSTEMS AND REPLACED A FAILED ANTENNA PEDESTAL. THE SYSTEM TESTED NORMAL AND AIRCRAFT RETURNED TO SERVICE. (X) 2L73 4F RTA22WE 19960119001421996011900142WP 1996 1 19 96ZZZX243 119951227A56105912290505 WINDSHIELD DOUG DC9 DC983 3022083WP LT COCKPIT CRACKED A TWAAA UNSCHED LANDING O OTHER CRCRUISE 1 CE052FOR 49785 JFK - FLT 730 - IN CRUISE, L-1 WINDSHIELD OUTER PANE CRACKED RESULTING IN AN UNSCHEDULED LANDING AT ABQ. REPLACED L-2 WINDSHIELD, MFG PN 5912290505. CHECK C-1 - 6-27-95. 2L72 4F RTA6WE 19960119001431996011900143WP 1996 1 19 96ZZZX244 119951231A3397 WIRE DOUG DC9 DC983 3022083WP CABIN FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE052FOR 49575 STL - FLT 136 - DURING THE COURSE OF AN INSPECTION, IT WAS DISCOVERED THE EGRESS LIGHTING WAS INOPERATIVE. REPAIRED WIRING HARNESS TO THE EGRESS LIGHTING, OPERATION NORMAL. CHECK C-2D - 6-29-95 - MCI. 2L72 4F RTA6WE 19960119001531996011900153CE 1996 1 19 96ZZZX254 119951014A321007416396 FAIRING CESSNA182 182Q 2072732CE RT GEAR LEG DEFECTIVE A C6PAK NONE O OTHER ININSP/MAINT 1 NM0194803 18266514 RECEIVED NEW GEAR LEG FAIRINGS (FORMS 8130-3 WERE INCLUDED) FOR INSTALLATION ON A 182Q. FOR SHIPPING, THE FAIRINGS HAD THE SCREWS IN PLACE INTO THE TINNERMAN STYLE NUTPLATES, HOLDING THE SEAM TOGETHER. WHILE REMOVING THE SCREWS TO PERFORM THE INSTALLATION, SEVERAL OF THE NUTPLATES SNAPPED APART. SUBMITTER STATED IT APPEARS THERE WAS TOO MUCH TEMPER CAUSING THE NUTPLATES TO BE OVERLY BRITTLE. THESE PARTS CAME DIRECT FROM CESSNA. 1H71 3O NT3A13 19960119001541996011900154CE 1996 1 19 96ZZZX255 119951014A321007416395 FAIRING CESSNA182 182Q 2072732CE LT GEAR LEG DEFECTIVE A C6PAK NONE O OTHER ININSP/MAINT 1 NM0194803 18266514 RECEIVED NEW GEAR LEG FAIRINGS (FORMS 8130-3 WERE INCLUDED) FOR INSTALLATION ON A 182Q. FOR SHIPPING, THE FAIRINGS HAD THE SCREWS IN PLACE INTO THE TINNERMAN STYLE NUTPLATES, HOLDING THE SEAM TOGETHER. WHILE REMOVING THE SCREWS TO PERFORM THE INSTALLATION, SEVERAL OF THE NUTPLATES SNAPPED APART. SUBMITTER STATED IT APPEARS THERE WAS TOO MUCH TEMPER CAUSING THE NUTPLATES TO BE OVERLY BRITTLE. THESE PARTS CAME DIRECT FROM CESSNA. 1H71 3O NT3A13 19960119001681996011900168NE 1996 1 19 96ZZZX269 219951222A72604002T02P03 BEARING 5001T90G06 SKRSKYS61 S61A 814210CNE GE CT58 CT581401 30011NE ASSORY DR GRBOX FAILED A JYEAO OTHER Y ENGINE STOPPAGE CRCRUISE 1 NM091043T5209 4115 00165 61083 280316A THE ENGINE LOST FUEL AND OIL PRESSURE IN-FLIGHT AND QUIT. THE ACCESSORY DRIVE GEARBOX PINION SHAFT BEARINGS FAILED AND ALLOWED GEAR DISSENGAGEMENT TO FAILURE POINT. SUBMITTER RECOMMENDS REPLACING BEARINGS AT 3,600 HOURS TT. 2G72 4U4 U H2EA 1E3 19960119001731996011900173WP 1996 1 19 9522201154 119951227A5320 DOOR JAMB DOUG DC10 DC1040 3023508WP BS 1035-1039 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01154US 46763 DURING T-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB LOWER OUTBOARD SILL BEAM BELOW LONGERON 43R FROM FS 1035 TO 1039. REPAIRED THE BEAM (P/N ADA 0250-1) PER EA 11-104446. 2L73 4F A22WE 19960119001741996011900174WP 1996 1 19 9522219754 119951228A5220 DOOR PAN DOUG DC9 DC941 302207NWP LT EMER EXIT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01754NW 47178 DURING H-CHECK, FOUND CRACKS IN BOTH THE LEFT FORWARD AND AFT EMERGENCY OVERWING EXIT DOOR PANS AT THE UPPER FORWARD AND AFT STOPS, RESPECTIVELY. REPAIRED PANS (P/N 5913195-1) PER EA 97-102013 AND 97-102014. 2L72 4F A6WE 19960119001751996011900175WP 1996 1 19 9522221154 119951228A5315 BEAM DOUG DC10 DC1040 3023508WP FS 761 CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01154US 46763 DURING T-CHECK, FOUND A CRACK IN THE FS 761 FLOORBEAM AT LBL 8, SEAT TRACK ATTACH HOLE. REPAIRED BEAM (P/N ADA 7226-505) PER EA 11-99295. 2L73 4F A22WE 19960119001761996011900176WP 1996 1 19 9522231154 119951229A5320 DOUBLER DOUG DC10 DC1040 3023508WP FS 1177 CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01154US 46763 DURING T-CHECK, FOUND CORROSION ON THE NR 1 RADIO ALTIMETER DOUBLERS AT FS 1177. REPAIRED THE DOUBLERS PER EA 11-104443. 2L73 4F A22WE 19960119002491996011900249CE 1996 1 19 96ZZZX274 119951229A3260571812041 LOGIC BOX CESSNA441 441 2076020CE MLG ANNUNCIATOR MALFUNCTION A DJFAO OTHER N FALSE WARNING APAPPROACH 1 EA23410MA4528 4410254 UPON APPROACH, PILOT SELECTED GEAR DOWN. GEAR CAME DOWN, THREE GREEN LIGHTS CAME ON, RED GEAR UNSAFE LIGHT ILLUMINATED AND MANY ANNUNCIATOR WARNING LIGHTS CAME ON. PILOT ELECTED TO BLOW GEAR DOWN, AND AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOT MALFUNCTION TO ANNOUNCE LOGIC BOX RESISTOR R26 WAS FOUND OPEN. IT IS SUSPECTED THAT THE RESISTOR WENT TO LOW OHMS BEFORE GOING OPEN CAUSING ALL NEGATIVE SEEKING LIGHTS TO ILLUMINATE, INCLUDING GEAR UNSAFE LIGHT. 1L72 3T RTA28CE 19960119003081996011900308NE 1996 1 19 95UAL900354 219951227A7230704523 NR 3 BEARING BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE RT ENGINE FAILED A AUALAO OTHER J WARNING INDICATION CRCRUISE 1 WP299061U183616638 19942 655925 AT 29,000 FEET HEARD A BANG FROM RIGHT HAND SIDE OF AIRCRAFT. EPR DROPPED AND CAPTAIN REDUCED ENGINE TO FLIGHT IDLE. FOUND NUMBER THREE BEARING CAGE FAILURE. SUSPECT IT WAS DUE TO EXCESSIVE POCKET WEAR. FAILURE OCCURRED MIDWAY BETWEEN THE CAGE RIVET HOLES. 2L72 4F4 F A16WE E2EA 19960119003091996011900309NM 1996 1 19 95UAL900359 119951227A32601EN161RB1 SWITCH BOEING727 727222 1384073NM RT MLG DOOR STUCK A UALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP297261U 21408 ON GEAR RETRACTION RT MAIN GEAR DOOR LIGHT REMAINED ON. AIRCRAFT RETURNED TO DEN. FOUND RIGHT MLG DOOR SWITCH STICKING AND REPLACED SWITCH. 2L73 4F A3WE 19960119003231996011900323WP 1996 1 19 ABXA9600021 119951205A5730575178478 SKIN DOUG DC8 DC863 302198AWP WS 107 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 DURING 816AX C-CHECK, DISCOVERED CORROSION ON RIGHT WING LEADING EDGE, LOWER AFT ATTACH EDGE AT FASTENER LOCATION XFS 107. REPAIRED RIGHT WING LEADING EDGE LOWER SURFACE THAT WAS CORRODED AT STATION XFS 107 IAW ABX REA D857-13106MR. 2L74 4F 4A25 19960119003241996011900324WP 1996 1 19 ABXA9600022 119951205A5311 FRAME DOUG DC8 DC863 302198AWP BS 1120 CORRISION A ABXAK NONE O OTHER ININSP/MAINT 1 GL23816AX 46093 DURING 816AX C-CHECK, DISCOVERED CORRISION ON FRAME AROUND NUTPLATES AT FUSELAGE STATION 1120, ABOVE L33R. REPAIRED UPPER FRAME CAP BLEND OUT AT FUSELAGE STATION 1120 AT LONGERON 33R IAW ABX REA D853-13599MR. 2L74 4F 4A25 19960119003251996011900325WP 1996 1 19 ABXA9600023 119950829A5753 HINGE DOUG DC8 DC863 302198AWP LT TE FLAP CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND LEFT HAND INBOARD FLAP, INBOARD HINGE ARM CHAFED. REPAIRED INBOARD FLAP INBOARD HINGE IAW ABX REA D857-12329MR. 2L74 4F 4A25 19960119003261996011900326WP 1996 1 19 ABXA9600024 119950829A532056138595 SILL DOUG DC8 DC863 302198AWP PAX DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, FOUND LEFT FORWARD ENTRY DOOR THRESHOLD AREA HAS CORRODED FASTENERS AND DOUBLER DRILLED HOLES. REPAIRED LEFT FORWARD ENTRY DOOR SILL IAW ABX REA D853-12484MR. 2L74 4F 4A25 19960119003271996011900327WP 1996 1 19 ABXA9600025 119951205A5730 SKIN DOUG DC8 DC863 302198AWP WS 257 LE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED THE CENTER LEADING EDGE SKIN CRACKED BETWEEN ATTACH HOLES ON INBOARD END LEADING AREA. REPAIRED LEFT HAND WING CENTER CRACKED LEADING EDGE AT STATION XW=257 IAW ABX REA D857-13077MR. 2L74 4F 4A25 19960119003331996011900333WP 1996 1 19 ABXA9600031 119951205A5400580273659 TEE DOUBLER DOUG DC8 DC863 302198AWP NR 1 PYLON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED NR 1 PYLON TEE DOUBLER LEAKS FUEL. REPAIRED NR 1 TEE DOUBLER THAT WAS CRACKED IAW ABX REA D854-13070MR. 2L74 4F 4A25 19960119003341996011900334WP 1996 1 19 ABXA9600032 119951205A531356153739 LONGERON DOUG DC8 DC863 302198AWP BS 1580 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED THE LONGERON 1 AT STATION 1615 CORRODED. REPAIRED CORRODED LONGERON 1 AT STATION 1615 IAW ABX REA D853-13069MR. 2L74 4F 4A25 19960119003351996011900335WP 1996 1 19 ABXA9600033 119951205A531357797725 LONGERON DOUG DC8 DC863 302198AWP BS 1020 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED FUSELAGE FRAME 1020 CORRODED ON UPPER FLANGE BETWEEN LONGERON 28L AND 29L. REPAIRED CORRODED FUSELAGE STATION 1020 FRAME AT LONGERON 28L, UPPER FRAME IAW ABX REA D853-13068MR. 2L74 4F 4A25 19960119003381996011900338NM 1996 1 19 DL72E960073 119950927A5754651622199 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272829W 21481 UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON THE 17TH RIB FROM O/B END OF NR 4 L/E SLAT. REPAIRED AS PER MM 57-54-0, FIG 805. 2L73 4F A3WE 19960119003391996011900339NM 1996 1 19 DL72E960074 119950927A5754651622199 RIB BOEING727 727247 138408FNM NR 4 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272829W 21481 UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON THE 5TH RIB FROM THE O/B END NR 4 L/E SLAT. REPAIRED AS PER 57-54-0, FIG 805. 2L73 4F A3WE 19960119003431996011900343NM 1996 1 19 DL72S960061 119951002A5754651622295 FAIRING BOEING727 727232 1384082NM NR 3 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27518DA 21469 THE O/B TRACK FAIRING WAS CRACKED. REPAIRED AS PER MM 57-54-0 FOR NR 3 L/E SLAT. 2L73 4F A3WE 19960119003511996011900351NM 1996 1 19 DL73E960091 119950115A33501619 BULB BOEING737 737247 138448DNM LT LOWER BODY FAILED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27236WA 23184 AFT LOWER BODY EMERGENCY LIGHT INOP. RELAMPED SAME, OPS CHECK GOOD. 2L72 4F A16WE 19960119003681996011900368NM 1996 1 19 DLM11960077 119950110A3350 PIN DOUG MD11 MD11 3023602NM CABIN BENT A DALAK NONE L NO TEST ININSP/MAINT 1 SO27811DE 48566 MCO511390001, FOUND EMERGENCY LIGHTS TEST INOP. FOUND NO 28 VOLTS AT RELAY R2-5699, GOOD VOLTS AT SWITCH PINS 1 AND 2 OF S1-402 AND BENT PIN AT P1 203. REPAIRED PIN AND OPS CK EMERGENCY LIGHTS IS NORMAL PER M/M. 2L73 4F RTA22WE 19960119003801996011900380WP 1996 1 19 96ZZZM31 219951024A72618971973 GEAR SHAFT BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP SCAVANGE PUMP SHEARED A ASABAK NONE O OTHER ININSP/MAINT 1 SO05170PC 717 P63222 THE ENGINE WAS DISASSEMBLIED AND INSPECTED BY GARRETT AVIATION SERVICES IN AUGUSTA, GA. THEY FOUND THAT THE SCAVANGE PUMP GEAR SHAFT HAD SHEARED AND THAT THERE WAS A SLIGHT BINDING IN THE SCAVANGE PUMP WHEN ROTATED BY HAND. THE PUMP WAS DISASSEMBLIED AND INSPECTED AND NO APPARENT DAMAGE WAS FOUND, BUT THE PUMP ROTORS WERE REPLACED AS A PRECAUTIONARY MEASURE. 2L72 4T4 TRTA21EU E4WE 19960119003811996011900381EU 1996 1 19 96ZZZM32 119951102A7712 CONNECTOR BAG JETSTMJETSTM3101 1500215EU LT TQ RING DIRTY A SABAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO05190PC 750 FLT NR 5164 WAS TWENTY MINUTES INTO THE FLIGHT TO HTS WHEN THE LEFT ENGINE TORQUE INDICATION STARTED TO FLUCTUATE. THE CAPTAIN SELECTED THE SRL/TTL COMPUTERS BUT THE FLUCTUATIONS CONTINUED. THE CAPTAIN CONTACTED MAINTENANCE CONTROL AND DISCUSSED THE PROBLEM. THE CAPTAIN DECIDED TO RETURN TO CLT BUT, DID NOT DECLARE AN EMERGENCY. THE AIRCRAFT MADE A SAFE AN UNEVENTFUL LANDING IN CLT. MAINTENANCE PERSONNEL WERE DISPATCHED TO TROUBLESHOOT THE PROBLEM. OIL WAS FOUND IN THE LEFT ENGINE TORQUE RING CANNON PLUG. THE OIL WAS REMOVED FROM THE CANNON PLUG THE AIRCRAFT WAS GROUND RAN AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4T RTA21EU 19960119003821996011900382NE 1996 1 19 96ZZZM33 219951124A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE RIGHT FAILED A SABAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 SO05722PC SH3722 106115 FLT NR 5097 - DESCENDING THROUGH 5,000 FEET FOR LANDING IN RWI WHEN THE RIGHT ENGINE SHUT ITSELF DOWN. THE CAPTAIN DECLARED AN EMERGENCY AND MADE AN UNEVENTFUL LANDING RWI. MAINTENANCE PERSONNEL WERE DISPATCHED TO RWI TO INVESTIGATE THE PROBLEM. THE RIGHT ENGINE OIL FILTER WAS REMOVED TO CHECK FOR METAL CONTAMINATION AND NONE WAS FOUND. THE OIL FILTER WAS REINSTALLED AND THE OIL LEVEL WAS TOPPED OFF. THE ENGINE WAS THEN GROUND RAN FOR APPROXIMATELY FOUR HOURS WITH ALL INDICATIONS NORMAL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2H72 4T4 T A41EU E26NE 19960119003831996011900383SO 1996 1 19 96ZZZM34 119951207A27503069001017 ANNUNCIATOR UNIT EMB 120 EMB120RT SO COCKPIT FAILED A MASAD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SW01221YV 120221 DURING FIRST FLIGHT RUN UP, CREW EXPERIENCED A FLAP CONTROL FAULT THAT WOULD NOT RESET. MAINTENANCE TROUBLESHOT SYSTEM TO BAD ANNUNCIATOR UNIT AND REPLACED SAME. SYSTEM OPS CHECKED GOOD AND WAS RELEASED FOR SERVICE. ANNUNCIATOR UNIT S/N 229 MANUFACTURED BY PARKER. 2L72 4T RTA31SO 19960119003841996011900384WP 1996 1 19 96ZZZM35 119951209A3246GYS1810C49 BOLT GOODYEAR 95608597 DOUG DC9 DC951 3022051WP WHEEL ASSY BROKEN A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING ROUTINE SERVICE, FOUND NR 1 MAIN WHEEL ASSY TIE BOLT BROKEN. WHEEL ASSY SENT TO WHEEL SHOP FOR OVERHAUL. 2L72 4F A6WE 19960119003851996011900385EU 1996 1 19 96ZZZM36 119951204A2710S0001003400000 ROD ASSY AEROSPATR42 ATR42300 8680920EU RT WING RIB 20 WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 ORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY. ROD ASSY AT RIB NR 20 HAS BINDING. RIB NR 9 CRANK ASSY FOUND EXCESSIVE PLAY. REMOVED AND REPLACED BELL CRANK AT RIB NR 24 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED ROD ASSY AT RIB NR 20 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED CRANK ASSY AT RIB NR 9 ON RIGHT WING IAW ATR MAINTENANCE MANUAL. RETURNED AIRCRAFT TO SERVICE. REFERENCE SIMA953363. 2H72 4T RTA53EU 19960119003861996011900386EU 1996 1 19 96ZZZM37 119951204A2710S2711009100000 BELL CRANK AEROSPATR42 ATR42300 8680920EU RT WING RIB 24 WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 ORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY. ROD ASSY AT RIB NR 20 HAS BINDING. RIB NR 9 CRANK ASSY FOUND EXCESSIVE PLAY. REMOVED AND REPLACED BELL CRANK AT RIB NR 24 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED ROD ASSY AT RIB NR 20 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED CRANK ASSY AT RIB NR 9 ON RIGHT WING IAW ATR MAINTENANCE MANUAL. RETURNED AIRCRAFT TO SERVICE. REFERENCE SIMA953363. 2H72 4T RTA53EU 19960119003871996011900387EU 1996 1 19 96ZZZM38 119951204A2710S2711001400100 CRANK ASSY AEROSPATR42 ATR42300 8680920EU RT WING RIB 9 WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 ORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY. ROD ASSY AT RIB NR 20 HAS BINDING. RIB NR 9 CRANK ASSY FOUND EXCESSIVE PLAY. REMOVED AND REPLACED BELL CRANK AT RIB NR 24 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED ROD ASSY AT RIB NR 20 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED CRANK ASSY AT RIB NR 9 ON RIGHT WING IAW ATR MAINTENANCE MANUAL. RETURNED AIRCRAFT TO SERVICE. REFERENCE SIMA953363. 2H72 4T RTA53EU 19960119003881996011900388EU 1996 1 19 96ZZZM39 119951204A2710S2711009100000 BELL CRANK AEROSPATR42 ATR42300 8680920EU LT WING RIB 24 WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 ORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY. ROD ASSY AT RIB NR 20 HAS BINDING. RIB NR 9 CRANK ASSY FOUND EXCESSIVE PLAY. REMOVED AND REPLACED BELL CRANK AT RIB NR 24 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED ROD ASSY AT RIB NR 20 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED CRANK ASSY AT RIB NR 9 ON RIGHT WING IAW ATR MAINTENANCE MANUAL. RETURNED AIRCRAFT TO SERVICE. REFERENCE SIMA953363. 2H72 4T RTA53EU 19960119003891996011900389NM 1996 1 19 AALA951972 119951116A5315111T5007 FLOOR BEAM BOEING767 767223 1385123NM BS 955 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07327AA 22327 AFW - FLOOR BEAM AT RBL 11.06 STATION 955 HAD CORROSION REMOVED BEYOND SRM LIMITS. BLENDED CORROSION. CHECKED, NO CRACKS. REFINISHED AREA CONTINUED IN SERVICE. (M) 2L72 4F RTA1NM 19960119003901996011900390NM 1996 1 19 AALA951973 119951116A5315141T5111 FLOOR BEAM BOEING767 767223 1385123NM BS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07327AA 22327 AFW - FLOOR BEAM AT STATION 287 RBL 30 TO RBL 64 HAD CORROSION BLENDED BEYOND SRM LIMITS. REMOVED CORROSION, PRIMED. FILLED WITH BMS 5-95, FABRICATED AND INSTALLED REPAIR STRAP. (M) 2L72 4F RTA1NM 19960119003911996011900391NM 1996 1 19 AALA951974 119951113A5730111T3013 SKIN BOEING767 767223 1385123NM BS 957 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07327AA 22327 AFW - HEAVY CORROSION REMOVED ON CENTER WING UPPER SKIN AT AFT DRAIN LOWER CHORD TO FLOOR BEAM T-EXTRUSION WAS CUT AND REMOVED. BLENDED AREAS OF CORROSION AND TREATED, PRIMED AND PAINTED. FABRICATED T-EXTRUSION REPAIR. (M) 2L72 4F RTA1NM 19960119003921996011900392NM 1996 1 19 AALA951975 119951116A5315141T5114 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07327AA 22327 AFW - FLOOR BEAM FOUND CORRODED, BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP, USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB 767-1064. (M) 2L72 4F RTA1NM 19960119003931996011900393NM 1996 1 19 AALA951976 119951116A5315146T5141 FLOOR BEAM BOEING767 767223 1385123NM BS 1480 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07327AA 22327 AFW - FOUND FLOOR BEAM CORRODED BEYOND SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301 HALF HARD STAINLESS STEEL. APPROVED BY ENGINEERING EPR MRB 767-1067. (M) 2L72 4F RTA1NM 19960119003941996011900394NM 1996 1 19 AALA951993 119951115A5315146N5089 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07646AA 24604 AFW - FLOOR BEAM AT STATION 1640 FOUND CORRODED. FLOOR BEAM AT STATION 1640 CORROSION REMOVED. ALODINED ALL BLENDED AREAS, FABRICATED STRAPS FROM .050 301 HALF HARD STAINLESS STEEL. APPLIED TWO COATS PRIMED CPN5518489 TO THE STRAPS AND FLOOR BEAM, FILLED ALL BLENDED AREAS WITH BMS 5-92 TYPE 1 OR 2, CPN 5996516 INSTALLED STRAPS WET WITH BMS 5-95 SEALANT USING BACB30NW6 HI-LOCKS PER MRB 757-663. (M) 2L72 4F RTA2NM 19960119003951996011900395NM 1996 1 19 AALA951995 119951113A5311141N8B15 FRAME BOEING757 757223 1384957NM BS 388 GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - FRAME AT FORWARD UPPER CORNER OF L-1 DOOR STAB FRAME, AT 388 WL 277, HAD GOUGE. AFTER BLENDING IS BEYOND SRM LIMITS. PER MRB 757-659. (M) 2L72 4F RTA2NM 19960119003961996011900396NM 1996 1 19 AALA951997 119951111A5311146N1008 FRAME BOEING757 757223 1384957NM BS 1340 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - FRAME CRACKED ON FREE FLANGE AT STATION 1340 STRINGER 26R. PER MRB 757-658. (M) 2L72 4F RTA2NM 19960119003971996011900397NM 1996 1 19 AALA951999 119951108A5210146N6302 PAN BOEING757 757223 1384957NM L1 DOOR GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - L-1 DOOR PANEL HAS SMALL GOUGE. AFTER BLENDING IS BEYOND SRM LIMITS. PER MRB 757-657. (M) 2L72 4F RTA2NM 19960119003981996011900398NM 1996 1 19 AALA952001 119951108A5210146N2101 PAN BOEING757 757223 1384957NM L4 DOOR GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - L-4 DOOR HANDLE PANEL HAS SMALL GOUGE. AFTER BLENDING IS BEYOND SRM LIMITS. PER MRB 757-656. (M0 2L72 4F RTA2NM 19960119003991996011900399NM 1996 1 19 AALA952003 119951109A5315141N2930 FLOOR BEAM BOEING757 757223 1384957NM BS 324 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - FLOOR BEAM AT STATION 324, RBL 60, HAD CORROSION REMOVED BEYOND SRM LIMITS. PER MRB 757-654. (M) 2L72 4F RTA2NM 19960119004001996011900400NM 1996 1 19 AALA952005 119951108A5315141N5112 FLOOR BEAM BOEING757 757223 1384957NM BS 365 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - FLOOR BEAM HAS CORROSION BLENDED BEYOND SRM LIMITS STATION 365, RBL 10, RBL 18 AND RBL 59. PER MRB 757-652. (M) 2L72 4F RTA2NM 19960119004011996011900401NM 1996 1 19 AALA952007 119951113A5321146N5300 DECK BOEING757 757223 1384957NM BS 1681 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07636AM 24594 AFW - DECK PLATE HAD CORROSION BLENDED BEYOND SRM LIMITS. PER MRB 757-651. (M) 2L72 4F RTA2NM 19960119004021996011900402SO 1996 1 19 C2XA95IA363 119951128A3260922AA2YA6PZ722 PROX SWITCH EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0916710 120106 CLL - FLT NR 2627 - PILOT REPORTED THAT AFTER TAKEOFF, THE LEFT MAIN GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD. THE AIRCRAFT WAS THEN FERRIED TO IAH WHERE MAINTENANCE ADJUSTED THE LEFT GEAR UPLOCK PROXIMITY SWITCH. THE AIRCRAFT THEN AIR RETURNED ON THE NEXT FLIGHT, DUE TO THE LEFT GEAR NOT RETRACTING. MAINTENANCE THEN CLEANED THE LEFT GEAR UPLOCK BOX CANNON PLUG, AND THE AIRCRAFT WAS RELEASED ON A TEST FLIGHT. THE TEST FLIGHT PROVED SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960119004031996011900403SO 1996 1 19 C2XA95IA364 119951204A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF.EMB FAX EST435/95. (M) 2L72 4T RTA31SO 19960119004041996011900404SO 1996 1 19 C2XA95IA365 119951205A534712026864007 SEAT TRACK EMB 120 EMB120RT SO LT CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004051996011900405SO 1996 1 19 C2XA95IA366 119951205A532012006159501 FLOOR SUPPORT EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SUPPORT CORRODED FROM FRAME 38.5 TO 40. MAINTENANCE REMOVED AND REPLACED THE SECTION OF FLOOR SUPPORT. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004061996011900406SO 1996 1 19 C2XA95IA367 119951205A534712015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004071996011900407SO 1996 1 19 C2XA95IA368 119951205A534712015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND LEFT LOWER FORWARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004081996011900408SO 1996 1 19 C2XA95IA369 119951205A534712015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT UPPER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004091996011900409SO 1996 1 19 C2XA95IA370 119951205A534712015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT FORWARD LOWER SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004101996011900410SO 1996 1 19 C2XA95IA371 119951205A532012004449001 PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004111996011900411SO 1996 1 19 C2XA95IA372 119951205A523012020235005 MOUNT EMB 120 EMB120RT SO CARGO DOOR CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, FOUND THE CARGO DOOR TORSION BAR FORWARD MOUNT TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE MOUNT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004121996011900412EU 1996 1 19 C2XA95IA373 119951205A33503101210 BULB AEROSPATR42 ATR42300 8680920EU PAX DOOR FAILED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW0916824 166 IAH - DURING A 4A INSPECTION, THE PASSENGER DOOR EMERGENCY STEP LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE BULB AND CLEANED THE BULB SOCKET, REINSTALLED THE BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2H72 4T RTA53EU 19960119004131996011900413SO 1996 1 19 C2XA95IA374 119951205A572012004357019 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 23, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004141996011900414SO 1996 1 19 C2XA95IA375 119951205A572012017057005 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, LOWER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004151996011900415SO 1996 1 19 C2XA95IA376 119951205A572012017062013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004161996011900416SO 1996 1 19 C2XA95IA377 119951205A572012017060011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 19, LOWER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004171996011900417SO 1996 1 19 C2XA95IA378 119951205A572012017057015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004181996011900418SO 1996 1 19 C2XA95IA379 119951205A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004191996011900419SO 1996 1 19 C2XA95IA380 119951205A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 16, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004201996011900420SO 1996 1 19 C2XA95IA381 119951205A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004211996011900421SO 1996 1 19 C2XA95IA382 119951205A572012017056007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 15, UPPER NR 3 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004221996011900422SO 1996 1 19 C2XA95IA383 119951205A571212017061005 RIB EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916702 120078 IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 20 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED NOSE RIB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960119004231996011900423NE 1996 1 19 CAL951038 219951112A7313 NOZ GUIDE VANE BOEING727 727243 138408DNM PWA JT8 JT8D9 52048NE NR 3 ENGINE SEPARATED A CALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION TOTAKEOFF 1 SW09578PE489977879 21661 666978 MSY - FLT 1528 - THE NR 3 ENGINE FAILED ON TAKEOFF FROM MSY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO MSY WHERE IT LANDED WITHOUT INCIDENT. THE NR 3 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THIS WAS A FIRST STAGE TURBINE FAILURE DUE TO BURN-THROUGH AND SEPARATION OF A FIRST STAGE NOZZLE GUIDE VANE. (X) 2L73 4F4 FRTA3WE E2EA 19960119004241996011900424NM 1996 1 19 CKSA95142 119951201A331016419 TRANSFORMER BOEING747 747132 1384882NM PILOTS PANEL BURNED A CKSAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23625PL75157 20247 KLAX - ELECTRICAL SMOKE ODOR IN AREA OF PILOTS MAIN PANEL BACK GROUND RHEOSTAT. PULLED CIRCUIT BREAKER FOR PILOTS BACKGROUND LIGHTING, ODOR DISSIPATED. REMOVED AND REPLACED PILOTS BACKGROUND LIGHT TRANSFORMER. OPS CHECK GOOD IAW 33-10-00. (M) 2L74 4F A20WE 19960119004251996011900425EA 1996 1 19 HNAA9590520 119951130A3230155507 UPLOCK ACTUATOR DHAV DHC7 DHC7102 2802708EA LT MLG FAILED A HNAAO OTHER J WARNING INDICATION APAPPROACH 1 EA07905HA31868 MC335 070 FLT NR 3055 - ORF-DCA - ON APPROACH INTO DCA, THE LEFT MAIN GEAR WOULD NOT INITIALLY EXTEND. WHEN GEAR WAS SELECTED DOWN, GOT TWO GREEN ON NOSE AND RIGHT GEAR FOR APPROXIMATELY 30 SECONDS WHEN THE LEFT GEAR DOORS AND RED LIGHT ILLUMINATED. THE LEFT GEAR THEN EXTENDED AND LOCKED GREEN. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. BLED AIR FROM NR 2 HYDRAULIC SYSTEM. FLT 3144 - ORF-DCA - LATER IN THE DAY, ON APPROACH INTO DCA, WHEN GEAR WAS SELECTED DOWN, THE GEAR REMAINED UP FOR TEN SECONDS BEFORE GOING RED THEN GREEN. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MAIN UPLOCK ACTUATOR. (M) 2H74 4T A20EA 19960119004261996011900426NE 1996 1 19 IXKA900033 219951201A7200 ENGINE BOEING727 727224 1384076NM PWA JT8 JT8D9A 52048NE NR 2 FAILED A IXKAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA2532719294735882 20388 687807 FLT NR 9 - EWR-MCO - DIVERTED TO ATL AFTER OIL FILTER BYPASS LIGHT FOR NR 2 ENGINE ILLUMINATED IN FLIGHT, OPERATED AT REDUCED POWER. ALL OTHER INDICATIONS NORMAL. REPLACED MOS BYPASS SWITCH, OIL PRESS RELIEF VALVE PER MM 79-33-0. ON HIGH POWER ENG RUN, VIBRATION OCCURRED, FOLLOWED BY FAILURE. REMOVED AND REPLACED NR 2 ENGINE PER MM 72-00. OPS CHECK OK. REASON FOR FAILURE OF ENG AWAITING TEAR DOWN REPORT. (M) 2L73 4F4 F A3WE E2EA 19960119004271996011900427SW 1996 1 19 MALA954656 119951006A325035021502 STEER MANIFOLD SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER O OTHER LDLANDING 1 GL1560NE AC760B FLT NR 3350 - DURING THE LANDING ROLL IN EVV, THE AIRCRAFT VEERED TO THE RIGHT BELOW 60 KTS PRIOR TO ENGAGING THE STEERING BUTTON. THE CREW APPLIED THE LEFT BRAKE AND FULL REVERSE TO ASSIST IN STOPPING THE AIRCRAFT. MAINTENANCE REPLACED THE NOSE WHEEL STEERING MANIFOLD. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004281996011900428NM 1996 1 19 MALA954657 119951007A3397 WIRE DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15824MA 327 FLT R 3157 - DURING THE POST FLIGHT INSPECTION IN DTW, THE CREW NOTED THAT THE AFT CEILING LIGHT AND THE RIGHT FORWARD EXIT LIGHT WERE INOPERATIVE. MAINTENANCE RESECURED A LOOSE GROUND WIRE. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004291996011900429SW 1996 1 19 MALA954658 119951006A2841 FULE GAUGE SWRNGNSA227 SA227AC 8780603SW LT/RT FUEL SYS MALFUNCTIONED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1526906 AC654B FLT NR 3301 - ON CLIMB-OUT FROM DTW, THE LEFT FUEL QUANTITY GAUGE DROPPED TO 300 LBS. THE RIGHT GAUGE THEN DROPPED FROM 800 LBS TO 600 LBS. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GAUGE WAS REPLACED AS A PRECAUTION. THE SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004301996011900430 1996 1 19 MALA954659 319951005A6112 DE-ICE BOOT DHAV DHC8 DHC8102 2809003NM LT PROP FAILED A MALAK NONE O OTHER ININSP/MAINT 1 GL15819MA 251 DURING A DAILY WALKAROUND INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE LEFT PROPELLER NR 1 BLADE DE-ICE BOOT WAS BURNED AT THE ROOT. THE MAINTENANCE PERSONNEL REPLACED THE NR 1 BLADE ON THE LEFT PROPELLER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004311996011900431SW 1996 1 19 MALA954663 119951012A5753 RIB SWRNGNSA227 SA227AC 8780603SW LT TE FLAP CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15160MC AC733B DURING A SCHEDULED INSPECTION IN MSP, THE LEFT FLAP INBOARD ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING DOUBLER IAW FAC SRM 51-00-00, 57-90-10, REPAIR NR 11, AND LAR 95-MALA-254. (M) 1L72 4T A8SW 19960119004321996011900432SW 1996 1 19 MALA954664 119951014A52102724044010 CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15421MA AC634 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE NOTED A CRACK IN THE PASSENGER DOOR AT THE LEFT CORNER AT THE NUT PLATE FOR THE HAND RAIL BRACKET. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-010 IAW FAC SRM 51-00-00 PG 4 AND 51-40-01. (M) 1L72 4T A8SW 19960119004331996011900433NM 1996 1 19 MALA954665 119951016A3350 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN SEAT 1C MALFUNCTIONED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15852MA 349 FLT NR 3017 - DURING THE POST FLIGHT IN DTW, THE CREW NOTED THAT THE RED FLOOR LIGHT AT SEAT 1C WAS INOP. UPON MAINTENANCE INSPECTION, THE LIGHT WAS FOUND TO OPERATE AS REQUIRED. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004341996011900434WP 1996 1 19 MALA954666 219951016A723031070511 SEAL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP RT COMPRESSOR FAILED A MALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL15159MC AC728B FLT NR 3487 - IN CRUISE FLIGHT TO MSP, THE CREW NOTED THAT SMOKE WAS NOTED WITH THE BLEED AIR ON. THE CREW TURNED OFF THE BLEED AIR SYSTEMS AND CONTINUED TO MSP. MAINTENANCE REPLACED THE RIGHT COMPRESSOR SEAL. ALL CHECKS WERE SATISFACTORILY. (M) 1L72 4T4 T A8SW E4WE 19960119004351996011900435SW 1996 1 19 MALA954667 119951019A53202722085 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 491.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT CARGO DOOR FRAME, P/N 27-22085, AFT FS 491.060 TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE IAW ARP 53-20-9503. (M) 1L72 4T A8SW 19960119004361996011900436SW 1996 1 19 MALA954668 119951019A52102724044101 CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR CORNER CRACKED AT THE FORWARD HANDLE ATTACH POINT FORWARD CORNER. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-010, IN ACCORDANCE WITH SA227 SRM 51-00-00 AND 51-04-01. (M) 1L72 4T A8SW 19960119004371996011900437SW 1996 1 19 MALA954669 119951019A5311 BELT FRAME SWRNGNSA227 SA227AC 8780603SW BS 174 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER LEFT BELT FRAME RELIEF RADIUS CRACKED AT FS 174. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK, FABRICATING AND INSTALLING A REPAIR DOUBLER IAW FAC ARP 53-20-9148. (M) 1L72 4T A8SW 19960119004381996011900438 1996 1 19 MALA954670 419951019A236015401 STATIC WICK BASE SWRNGNSA227 SA227AC 8780603SW RT ELEVATOR NOT BONDED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT ELEVATOR MIDDLE STATIC WICK BASE NOT SECURELY BONDED. REPAIRS WERE COMPLETED BY REPLACING THE STATIC WICK BASE, P/N 15401, AND PERFORMED A SKIN REPAIR IAW SRM 51-90-04. (M) 1L72 4T A8SW 19960119004391996011900439SW 1996 1 19 MALA954671 119951019A57532731141 DOUBLER SWRNGNSA227 SA227AC 8780603SW LT TE FLAP WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP ROLLER DOUBLER, P/N 27-31141, NEARING WEAR LIMITS. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER IAW FAC SRM 57-90-10 AND ARP 57-20-9424. (M) 1L72 4T A8SW 19960119004401996011900440NM 1996 1 19 MALA954672 119951021A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15846MA 344 DURING THE POST FLIGHT IN DTW, THE EMERGENCY LIGHT ASSEMBLY IN THE COCKPIT ILLUMINATED INTERMITTENTLY. MAINTENANCE REPLACED THE EMERGENCY LIGHT. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004411996011900441SW 1996 1 19 MALA954673 119951021A29102781032081 HYD LINE SWRNGNSA227 SA227AC 8780603SW FWD PRESS BLKHD CRACKED A MALAO OTHER KJBFLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 GL15438MA AC721B FLT NR 3019 - ON THE SHORT FINAL APPROACH INTO DTW, BOTH HYDRAULIC LIGHTS ILLUMINATED AND THE HYDRAULIC GAUGE WENT TO ZERO. THE CREW PERFORMED QUICK REFERENCE PROCEDURES FOR THE HYDRAULIC AND LANDING GEAR PROCEDURES, THEN IN LANDING FLAIR, SMOKE ENTERED THE CABIN. THE CREW PERFORMED QUICK REFERENCE SMOKE REMOVAL AND EMERGENCY SHUTDOWN PROCEDURES. MAINTENANCE REPLACED A LEAKING HYDRAULIC LINE. ALL SYSTEM CHECKS SATISFACTORY. (M) 1L72 4T A8SW 19960119004421996011900442 1996 1 19 MALA954674 419951020A3442066311400 RADAR SCREEN SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL1560NE AC760B FLT NR 3018 - IN CRUISE FLIGHT, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE WEATHER RADAR INDICATOR. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004431996011900443 1996 1 19 MALA954675 419951023A3442071137800 RADAR TR UNIT SWRNGNSA227 SA227AC 8780603SW COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL1563NE AC763B FLT NR 3208 - ON CLIMB-OUT FROM MSP, THE WEATHER RADAR BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER. SYSTEM OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960119004441996011900444WP 1996 1 19 MALA954676 219951023A7320 FUEL CONTROL SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE OUT OF ADJUST A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15446MA AC693 FLIGHT 3485 - DURING THE TAKEOFF ROLL IN DTW, THE LEFT ENGINE WAS SLOW TO MAKE STANDARD POWER. AFTER V, POWER DROPPED TO 80 PERCENT. WHEN SPEEDS WERE BROUGHT BACK TO 100 PERCENT ON THE LEFT ENGINE, THE TORQUE JUMPED TO 105 PERCENT AND THE BYPASS LIGHT CAME ON. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE ADJUSTED THE LEFT ENGINES SCREW X TO RELIEVE OVERSPEED GOVERNOR INTERFERENCE IAW FAC MM 71-00-30. (M) 1L72 4T4 T A8SW E4WE 19960119004451996011900445SW 1996 1 19 MALA954677 119951021A32601EN516 POSITION SW SWRNGNSA227 SA227AC 8780603SW LT MLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15434MA AC717 FLT NR 3087 - ON APPROACH IN MSP, THE LEFT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR INDICATOR SHOWED IT TO BE DOWN AND LOCKED. THE CREW CYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LEFT INBOARD POSITION SWITCH, P/N 1EN51-6. THE LANDING GEAR POSITION INDICATOR WAS REPLACED AS A PRECAUTION. SYSTEM OPERATED SATISFACTORILY DURING A TEST FLIGHT. (M) 1L72 4T A8SW 19960119004461996011900446NM 1996 1 19 MALA954678 119951022A3397 WIRE DHAV DHC8 DHC8102 2809003NM PANEL 143CZ BROKEN A MALAK NONE L NO TEST ININSP/MAINT 1 GL15827MA 331 DURING A INSPECTION IN BNA, MAINTENANCE FOUND A BROKEN WIRE IN THE FLOOR PATH LIGHTING LOCATED AT FLOOR PANEL 143CZ. THE WIRE WAS REPAIRED IAW WM 33-51-00. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004471996011900447 1996 1 19 MALA954679 419951027A341628702502 ALTIMETER SWRNGNSA227 SA227AC 8780603SW LT COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15434MA AC717 FLT NR 3046 - ON CLIMB-OUT FROM DTW, THE CAPTAINS ALTIMETER BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER AND PURGED THE NR 1 AND NR 2 STATIC SYSTEMS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004481996011900448 1996 1 19 MALA954680 419951027A3425 HSI/HDG WARNING DHAV DHC8 DHC8102 2809003NM COCKPIT ACTIVATED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15854MA 357 FLT NR 3396 - EN ROUTE TO YXU, THE CREW RECEIVED A HSI HDG MISMATCH ADVISORY. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE CYCLED THE POWER AND WAS UNABLE TO DUPLICATE THE DISCREPANCY. (M) 2H72 4T RTA13NM 19960119004491996011900449SW 1996 1 19 MALA954681 119951029A32302752004045 RT UPLOCK SWRNGNSA227 SA227AC 8780603SW NLG LACK OF LUBE A MALAO OTHER J WARNING INDICATION CLCLIMB 1 GL152692P AC658B FLT NR 3349 - ON CLIMB-OUT FROM CWA, THE NOSE GEAR WOULDN'T STAY UP AND LOCKED. THE AIRCRAFT CONTINUED, WITH THE GEAR DOWN, TO MSP. MAINTENANCE CLEANED AND LUBRICATED THE RIGHT UPLOCK HOOK ASSY. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004501996011900450SW 1996 1 19 MALA954682 119951029A5210 SKIN SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR AFT LOWER SKIN CRACKED NEAR THE HINGE. REPAIRS WERE COMPLETED BY REPLACING THE SKIN SEGMENT IAW FAC SRM 51-90-10, PAGES 12-14. (M) 1L72 4T A8SW 19960119004511996011900451SW 1996 1 19 MALA954683 119951029A5210 STAIRS SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR STAIR ASSEMBLY CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE STAIR ASSEMBLY, P/N 27-24150-297. (M) 1L72 4T A8SW 19960119004521996011900452SW 1996 1 19 MALA954684 119951029A52102724044009 DOOR CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-009, IAW FAC SRM 51-00-00 PAGE 4. (M) 1L72 4T A8SW 19960119004531996011900453SW 1996 1 19 MALA954685 119951029A52102724044010 DOOR CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-010, IAW FAC SRM 51-00-00 PAGE 4. (M) 1L72 4T A8SW 19960119004541996011900454SW 1996 1 19 MALA954686 119951029A55202744001161 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RT ELEVATOR CORROSION A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT ELEVATOR TORQUE TUBE WELDMENT TO HAVE SIGNS OF CORROSION. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT ELEVATOR ASSEMBLY. (M) 1L72 4T A8SW 19960119004551996011900455SW 1996 1 19 MALA954687 119951029A5347 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 107 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK AT THE NUT PLATES FOR THE PILOTS OUTBOARD SEAT TRACK ATTACHMENT JUST AFT OF FS 107. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 53-10-9322. (M) 1L72 4T A8SW 19960119004561996011900456SW 1996 1 19 MALA954688 119951029A5347 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 107 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PILOTS SEAT TRACK ATTACH POINTS AT FS 107 TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR FLAGNE IAW ARP 53-10-8913. (M) 1L72 4T A8SW 19960119004571996011900457SW 1996 1 19 MALA954689 119951029A5280 SKIN PATCH SWRNGNSA227 SA227AC 8780603SW RT MLG DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15430MA AC710 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT OUTBOARD GEAR DOOR FLUSH PATCH DOOR SKIN REPAIR DAMAGED. REPAIRS WERE COMPLETED BY REPLACING THE FILLER IAW FAC SRM 52-90-30. (M) 1L72 4T A8SW 19960119004581996011900458SW 1996 1 19 MALA954690 119951028A5712 RIB SWRNGNSA227 SA227AC 8780603SW WS 51 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1526863 AC650B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT WING RIB, AT WS 51.0, TO BE CRACKED AT THE HYDRAULIC LINE PASS THROUGH HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING AN ANGLE DOUBLER IAW FAC SRM 57-90-10. (M) 1L72 4T A8SW 19960119004591996011900459SW 1996 1 19 MALA954691 119951031A5730 SKIN SWRNGNSA227 SA227AC 8780603SW WS 113 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15423MA AC636 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE NOTED THAT THE RIGHT LOWER WING HAD A CRACK AROUND THE RIVET HOLE AT WS 113. REPAIRS WERE COMPLETED BY INSTALLING A SURFACE DOUBLER IAW FAC LAR 95-MALA-280 AND INSTALLING STRINGER REPAIR DOUBLERS IAW FAC SRM 51-90-05 PAGES 1-3. (M) 1L72 4T A8SW 19960119004601996011900460SW 1996 1 19 MALA954714 119951116A5330 SKIN SWRNGNSA227 SA227AC 8780603SW FS 512.8 OIL CANNING A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A MAINTENANCE WALKAROUND IN MSP, A MECHANIC NOTED OIL CANNING ON THE LEFT SIDE OF THE FUSELAGE AFT OF THE CARGO DOOR AT FS 512.8. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING AN EXTERNAL DOUBLER IAW FAC SRM 53-90-20. (M) 1L72 4T A8SW 19960119004611996011900461SW 1996 1 19 MALA954715 119951119A2435230790001 STARTER/GEN SWRNGNSA227 SA227AC 8780603SW LT ENGINE INTERNAL FAULT A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15439MA AC722 FLT NR 3272 - ON CLIMB-OUT FROM MSP, THE LEFT GENERATOR FAIL LIGHT ILLUMINATED, AND THE GENERATOR WOULDN'T COME ON LINE. THE AIRCRAFT RETURNED TO MSP. REPAIRS WERE COMPLETED BY REPLACING THE LEFT STARTER/GENERATOR. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004621996011900462NM 1996 1 19 MALA954716 119951121A5541855400266101 RIB DHAV DHC8 DHC8102 2809003NM RUDDER CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15854MA 357 DURING A WALKAROUND INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER END RIB OF THE FORE RUDDER. THEY REPLACED RIB IAW SRM 51-40-00. (M) 2H72 4T RTA13NM 19960119004631996011900463WP 1996 1 19 MALA954717 219951122A7260 CHIP DETECTOR SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE ACTIVATED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15426MA AC645 FLT NR 3330 - DTW-SBN - EN ROUTE, THE LEFT CHIP DETECTOR LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REMOVED A SMALL FLAKE FROM THE CHIP DETECTOR, TOOK AN OIL SAMPLE, AND PLACED A RESAMPLE WATCH ITEM ON THE ENGINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T4 T A8SW E4WE 19960119004641996011900464SW 1996 1 19 MALA954718 119951123A3240 BRAKE SYSTEM SWRNGNSA227 SA227AC 8780603SW MLG REQ'D SERVICE A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15445MA AC687 FLT NR 3141 - DURING TAXI AT DTW, THE CREW HAD TO PUMP THE BRAKE PEDALS TO GET ANY BRAKE EFFECTIVENESS. MAINTENANCE PERSONNEL BLED THE BRAKES AND SERVICED THE BRAKE RESERVOIR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004651996011900465NM 1996 1 19 MALA954719 119951123A335010005511 BATTERY DHAV DHC8 DHC8102 2809003NM COCKPIT DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15829MA 335 FLT NR 3032 - DURING PREFLIGHT IN DTW, THE CREW NOTED THE COCKPIT PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE LIGHT. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004661996011900466SW 1996 1 19 MALA954720 119951122A32347092011 SELECTOR SWRNGNSA227 SA227AC 8780603SW LANDING GEAR MALFUNCTIONED A MALAO OTHER O OTHER APAPPROACH 1 GL1527465 AC755B FLT NR 3379 - ON APPROACH TO DTW, THE GEAR WOULD NOT EXTEND ON COMMAND. THE GEAR EXTENDED NORMALLY AFTER THE CREW RESET THE LANDING GEAR CONTROL CIRCUIT BREAKER. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE GEAR SELECTOR CONTROL, P/N 709201-1, WAS REPLACED. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004671996011900467SW 1996 1 19 MALA954721 119951124A3020 INTAKE HEAT WIRE SWRNGNSA227 SA227AC 8780603SW LT ENGINE FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15422MA AC635 FLT NR 3277 - EN ROUTE, THE LEFT ENGINE INTAKE LIGHT AND VALVE CYCLED ON AND OFF. THE AIRCRAFT RETURNED TO MSP DUE TO EN ROUTE WEATHER. MAINTENANCE REPAIRED A BROKEN WIRE AT THE CTM CONNECTOR FOR THE INTAKE HEAT VALVE. THE INTAKE HEAT VALVE WAS ALSO REPLACED AS A PRECAUTION. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004681996011900468SW 1996 1 19 MALA954722 119951124A5720 STIFFENER SWRNGNSA227 SA227AC 8780603SW BS 254.52 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15434MA AC717 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE CENTER CHANNEL AT BL 0.00 AND FS 254.52. THE CRACK WAS REPAIRED BY REPLACING THE CENTER STIFFENER (P/N 27-31110-031, 032) IAW SRM 157-90-30, REPAIRS NR 1 AND NR 2. (M) 1L72 4T A8SW 19960119004691996011900469NM 1996 1 19 MALA954726 119951127A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT LOOSE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15816MA 231 FLT NR 3469 - DURING PREFLIGHT IN DTW, THE CREW NOTED THE FLIGHT DECK EMERGENCY LIGHT HAD COME LOOSE FROM THE OVERHEAD PANEL. MAINTENANCE PERSONNEL REPLACED THE LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004701996011900470NM 1996 1 19 MALA954730 119951204A3230 UPLOCK ROLLERS DHAV DHC8 DHC8102 2809003NM LT MLG LACK OF LUBE A MALAO OTHER O OTHER APAPPROACH 1 GL15827MA 331 FLT NR 3133 - ON APPROACH TO DTW, THE LEFT LANDING GEAR TOOK LONGER TO EXTEND THAN THE OTHER GEAR. MAINTENANCE INSPECTED AND CLEANED THE LEFT LANDING GEAR UPLOCK AND ROLLERS. NO DEFECTS WERE NOTED. GEAR SWINGS WERE PERFORMED AND ALL CHECKS WERE FOUND TO BE WITHIN LIMITS. (M) 2H72 4T RTA13NM 19960119004711996011900471SW 1996 1 19 MALA954731 119951206A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL152692P AC658B FLT NR 3253 - ON CLIMB-OUT FROM GFK, THE NOSE GEAR INTRANSIT LIGHT ILLUMINATED AFTER THE GEAR WAS SELECTED UP. THE CREW CYCLED THE GEAR AND THE PROBLEM RECURRED. ON THE THIRD ATTEMPT, THE GREEN LIGHT ILLUMINATED AFTER THE INTRANSIT LIGHT EXTINGUISHED. ON APPROACH TO MSP, NORMAL INDICATIONS WERE RECEIVED UPON GEAR EXTENSION. MAINTENANCE ADJUSTED THE RIGHT NOSE GEAR UPLIMIT SWITCH. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004721996011900472SW 1996 1 19 MALA954732 119951206A32602782186057 GEAR POS IND SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15446MA AC693 FLT NR 3214 - ON APPROACH TO MSP, THE NOSE GEAR GREEN LIGHT DIDN'T ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. THE CREW CYCLED THE GEAR BUT THE LIGHT FAILED TO ILLUMINATE. MAINTENANCE REPLACED THE LANDING GEAR POSITION INDICATOR AND THE NOSE GEAR DOWNLOCK SWITCHES AS A PRECAUTION. ALL SYSTEMS OPERATED SATISFACTORILY DURING A TEST FLIGHT. (M) 1L72 4T A8SW 19960119004731996011900473NM 1996 1 19 MALA954733 119951205A3260 CONTL UNIT DHAV DHC8 DHC8102 2809003NM RT MLG MALFUNCTIONED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15865MA 364 FLT NR 3136 - IN CRUISE FLIGHT, THE RIGHT GEAR DOWN AND LOCKED INDICATOR LIGHT ILLUMINATED AND THEN, WHILE PERFORMING AN ADVISORY LIGHT TEST, THE CAUTION LIGHT WOULD NOT TEST. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCIES. DUE TO THE NATURE OF THE DISCREPANCIES, THE PANEL ANNUNCIATOR WARNING CONTROL UNIT WAS REPLACED AS A PRECAUTION. SYSTEMS OPERATED SATISFACTORILY DURING A TEST FLIGHT. (M) 2H72 4T RTA13NM 19960119004741996011900474NM 1996 1 19 MALA954734 119951205A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15827MA 331 FLT NR 3172 - ON APPROACH TO DTW, THE LEFT GEAR GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. THE CREW PERFORMED AN ALTERNATE EXTENSION AND ALL INDICATIONS WERE SATISFACTORY. MAINTENANCE REPLACED THE LEFT UPLOCK ACTUATOR. SYSTEM OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004751996011900475SW 1996 1 19 MALA954735 119951205A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15446MA AC693 FLT RN 3214 - ON APPROACH TO MSP, NO GEAR DOWN AND LOCKED INDICATION WAS RECEIVED FROM THE NOSE GEAR POSITION AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPOSITIONED THE DOWN AND LOCKED SWITCH ON THE NOSE GEAR. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004761996011900476SW 1996 1 19 MALA954748 119951209A5347 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 116.56 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PILOTS INBOARD SEAT TRACK ATTACH POINT AT FS 116.56 TO BE CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE CRACK AND INSTALLING A REPAIR DOUBLER IAW FAC LAR 95-MALA-306. (M) 1L72 4T A8SW 19960119004771996011900477NM 1996 1 19 MALA954751 119951212A2520 INTERIOR PNL DHAV DHC8 DHC8102 2809003NM CABIN OUT OF POSITION A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15859MA 361 FLT NR 3399 - DURING TAXI AT DTW, THE CREW REPORTED THE BRAKES REQUIRED A LOT OF PRESSURE TO ENGAGE AND WOULD THEN LOCK UP. MAINTENANCE PERSONNEL FOUND THE BRAKE CABLE CHAFING AGAINST A CABIN INTERIOR PANEL. THEY REPOSITIONED THE PANEL AND FUNCTIONALLY TESTED THE BRAKE SYSTEM. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960119004781996011900478SW 1996 1 19 MALA954752 119951204A27302743027041 BUSHINGS SWRNGNSA227 SA227AC 8780603SW ELEVATOR WORN A MALAK NONE F FLT CONT AFFECTED CRCRUISE 1 GL15426MA AC645 FLT NR 3357 - EN ROUTE TO DTW, THE ELEVATOR WOULD OCCASIONALLY PITCH UP OR DOWN ABRUPTLY, GIVING UP TO AN 800 FPM VERTICAL SPEED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED BUSHINGS AT THE LOWER PITCH TRIM ACTUATOR MOUNT LUGS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004791996011900479SW 1996 1 19 MALA954754 119951215A5730 SKIN SWRNGNSA227 SA227AC 8780603SW WS 66.584 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL1563NE AC763B DURING A SCHEDULED INSPECTION IN MSP, INSPECTORS NOTED A CRACK IN THE RIGHT WING SKIN AT WS 66.584. MAINTENANCE PERSONNEL FABRICATED AND INSTALLED AN EXTERNAL DOUBLER OVER THE CRACK. (M) 1L72 4T A8SW 19960119004801996011900480SW 1996 1 19 MALA954755 119951215A32302719248001 DNLOCK SPRING SWRNGNSA227 SA227AC 8780603SW RT MLG WORN A MALAK NONE J WARNING INDICATION APAPPROACH 1 GL15421MA AC634 FLT NR 3236 - DURING APPROACH TO MSP, THE RIGHT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE FOR 30 SECONDS AFTER THE GEAR WAS SELECTED DOWN. MAINTENANCE PERSONNEL WERE UNABLE TO DUPLICATE THE DISCREPANCY, BUT REPLACED THE DOWNLOCK SPRINGS AS A PRECAUTION. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960119004811996011900481WP 1996 1 19 ORJA95127 119951115A5320 SUPPORT DOUG DC9 DC982 3022082WP LT MLG WW CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 CORROSION ON AFT SIDE OF FIRST SUPPORT FRAME FORWARD OF LEFT W/W OPENING ON WING TO BODY LOWER FILLET FAIRING SUPPORT (MARKED). REMOVED LIGHT SURFACE CORROSION BY BUFFING. NEGLIGIBLE MATERIAL REMOVED, IAW MD80 SRM 53-04, 53-11-4, 51-10-3. REMOVED AND REPLACED NUTPLATES, ALSO, SRM 51-30-0. REINSTALLED FAIRING. (M) 2L72 4F A6WE 19960119004821996011900482WP 1996 1 19 ORJA95128 119951114A2731 CONTROL ROD DOUG DC9 DC982 3022082WP LT ELEV TAB CORRODED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11843RA 49615 LEFT ELEVATOR OUTBOARD TAB CONTROL ROD UPPER COVER/FAIRING IS CORRODED (HORIZONTAL STAB TO ELEVATOR). REMOVED LIGHT SURFACE CORROSION. TREATED AND PRIMED PER SRM 51-10-3. (M) 2L72 4F A6WE 19960119004831996011900483EU 1996 1 19 PLG111395E1 119951109A243523080031 STARTER/GEN SAAB SF340 340B 7860101EU LT ENGINE INOP A PLGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE05348BE3953 831 92057 340B190 FLT NR 4310 - BOS - ON CLIMB-OUT, THE LEFT GENERATOR DROPPED OFF LINE. THE CREW RESET THE GENERATOR, BUT IT DID NOT COME BACK ON LINE. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. THE GENERATOR WAS REMOVED AND REPLACED. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19960119004841996011900484CE 1996 1 19 PLG111395E2 119951108A76031143890501 CONTROL CABLE BEECH 1900 1900C 1154161CE LT PWR LEVER FROZEN A APLGAA UNSCHED LANDING O OTHER CRCRUISE 1 NE056929M 16909 UB27 FLT NR 4864 - BDL-YUL - EN ROUTE EXPERIENCED A FROZEN LT POWER LEVER CABLE, FROZEN ELEVATOR TRIM, NR 1 COMM SYS FAILURE AND LT ENVIRONMENTAL FAIL LIGHT ILLUMINATED. THE A/C DIVERTED INTO ALB AND LANDED WITHOUT INCIDENT. MX WAS DISPATCHED TO THE A/C. THE POWER LEVER CABLE WAS REPLACED AND THE POWER LEVER OPS CHECKED GOOD. THE ELEVATOR JACK SCREWS AND PULLEYS WERE LUBED AND SYS INSPECTED, SYS OPS CHECKED GOOD. REMOVAL AND REPLACEMENT OF NR 1 COMM HEAD CLEARED DISCREPANCY ON NR 1 COMM SYS, OPS CHECKED GOOD. TO CLEAR ENVIRONMENTAL FAILURE, THE PC BOARD AND CONNECTOR WERE CLEANED AND WATER WAS DRIED FROM WITHIN THE OVERPRESSURE SWITCH, OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE (M) 2L72 4T RTA24CE 19960119004851996011900485EU 1996 1 19 PLG111795E1 119951116A5270 DOOR WARNING SAAB SF340 SF340A 7850100EU PAX DOOR ILLUMINATED A PLGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE05340BE 340A062 DURING DEPARTURE FROM BOS, FLT NR 4414, HAD A FORWARD CABIN DOOR WARNING LIGHT ILLUMINATE. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR WARNING SYSTEM AND FOUND NO FAULT. THE SYSTEM WAS OPS CHECKED AND ALL INDICATIONS WERE NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19960119004861996011900486EU 1996 1 19 PLG11595G1 119951105A2710 ROLL TRIM TAB SAAB SF340 SF340A 7850100EU AILERON SYSTEM OUT OF ADJUST A PLGAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 NE05745BA 340A111 FLT NR 4743 - PSM - AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT REQUIRING STANDBY TRIM TO MAINTAIN STRAIGHT AND LEVEL FLT. THE AIRCRAFT DIVERTED TO MHT LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND RERIGGED THE MAIN ROLL TURN TAB IAW THE SAAB MM AND RETURNED TO SERVICE. THE ROLL TRIM SYSTEM HAD BEEN ON MEL AND 'M' FUNCTION PROCEDURES OF THE MEL HAD NOT BEEN CORRECTED. (M) 2L72 4T RTA52EU 19960119004871996011900487NE 1996 1 19 REXA950066 219951105A7200 ENGINE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE LEFT FAILED A REXAA UNSCHED LANDING BF SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED CLCLIMB 1 SO25362PX6620 GRE785440 340B258 GEE785440 DURING CLIMB, NOTED HIGH OIL TEMP ON LEFT ENGINE AND LOW OIL PRESS. ELECTED TO RETURN TO AIRPORT. THE FLIGHT ATTENDANT INFORMED US THERE WAS FUMES IN THE CABIN. CALLED CFRS AND DECLARED AN EMERGENCY. AFTER LANDING AND CLEARING RUNWAY THE CFRS NOTIFIED US OF A POSSIBLE FIRE ON THE LEFT SIDE. PROCEEDED WITH ENGINE FIRE PROCEDURES AND EVACUATED THE PAX FROM RIGHT SIDE. LEFT T-HANDLE WAS PULLED LEFT EXTINGUISHER ACTIVATED. REMOVED AND REPLACED LEFT ENGINE IAW AMM 71-00-00. PERFORMED ENGINE BREAK IN RUNS AND CHECKS. GROUND RUNS GOOD. NO LEAKS NOTED, OK FOR CONTINUED SERVICE. (M) 2L72 4T4 TRTA52EU E8NE 19960119004881996011900488EU 1996 1 19 REXA95067 119951113A261172111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100EU CARGO COMPT FALSE WARNING A REXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SO25329PX 340A076 CARGO SMOKE 'CWP' WARNING ILLUMINATED IN FLIGHT, STAYED ON, DISCHARGED CARGO FIRE EXTINGUISHER. REMOVED AND REPLACED CARGO FIRE BOTTLE AND CARTRIDGE. OPS CHECKED SMOKE DETECTOR IAW AMM. CHECKED GOOD, OK FOR SERVICE. NO EVIDENCE OF FIRE. (M) 2L72 4T RTA52EU 19960119004891996011900489EU 1996 1 19 SIMA953363 119951204A2710S0001003400000 ROD ASSY AEROSPATR42 ATR42300 8680920EU LT WING RIB 20 WORN A SIMAK NONE O OTHER ININSP/MAINT 1 SW21266AT 266 ORD - WHILE PERFORMING INSPECTION FOR EO E9-2700-001 (INSPECTION OF AILERON CONTROL SYSTEM). FOUND LEFT WING RIB NR 24 BELL CRANK ASSY TO HAVE EXCESSIVE PLAY. LEFT WING AT RIB NR 20 ROD ASSEMBLY WAS BINDING. RIGHT WING AT RIB NR 24 BELL CRANK ASSY HAS PLAY. ROD ASSY AT RIB NR 20 HAS BINDING. RIB NR 9 CRANK ASSY FOUND EXCESSIVE PLAY. REMOVED AND REPLACED BELL CRANK AT RIB NR 24 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED ROD ASSY AT RIB NR 20 ON BOTH LEFT AND RIGHT WINGS. REMOVED AND REPLACED CRANK ASSY AT RIB NR 9 ON RIGHT WING IAW ATR MAINTENANCE MANUAL. RETURNED AIRCRAFT TO SERVICE. (M) 2H72 4T RTA53EU 19960119004901996011900490EU 1996 1 19 SIMA953381 119951204A2121011232100 FAN AEROSPATR72 ATR72212 EU NR 1 FAILED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21270AT7495 S01285 270 DFW - FLT NR 3816 - INBOUND INTO DFW, CREW SMELLED SMOKE IN THE COCKPIT, COMPLIED WITH EMERGENCY PROCEDURES AND NOTIFIED CFT. LANDED WITHOUT FURTHER INCIDENT. RAN ALL SYSTEMS AND FOUND FAULT ON THE NR 1 RECIRC FAN. REMOVED AND REPLACED NR 1 RECIRC FAN. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19960119004911996011900491EU 1996 1 19 SIMA953411 119951207A2910M52191206 FITTING AEROSPATR42 ATR42300 8680920EU GREEN HYD SYSTEMCRACKED A SIMAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21428MQ 0128 ORD - FLT 4094 - DURING CLIMB-OUT, AIRCRAFT LOST GREEN SYSTEM HYD PRESSURE. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED ACCUMULATOR T-FITTING. SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA53EU 19960119004921996011900492WP 1996 1 19 SRAA129501 119951202A3231 RETRACT MECH DOUG DC8 DC873F 302199FWP RT MLG DOOR OUT OF ADJUST A SRAAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO19874SJ 46149 LAX - FLT QFA 7580 - ON CLIMB-OUT, CREW NOTICED AIRCRAFT HAD SEVERE VIBRATION DURING AND AFTER GEAR RETRACTION, CYCLED GEAR AND FOUND VIBRATION LESSENED, BUT DID NOT STOP, ACCOMPLISHED AIR TURN BACK TO LAX. JACKED AIRCRAFT AND PERFORMED GEAR SWING. FOUND RT MLG DOOR FOLLOW UP SYSTEM OUT OF RIG, RERIGGED RT MLG. FOLLOW UP DOOR SYSTEM AND PERFORMED GEAR SWING UPLATCH CHECK PER MM CH 32-31-5. (M) 2L74 4F RT4A25 19960119004931996011900493NM 1996 1 19 TWRA9564 119951025A3150 WARNING HORN BOEING747 747212B 1384886NM COCKPIT SOUNDED A TWRACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 EA15618FF 21937 DURING TAKEOFF ROLL, WARNING HORN SOUNDED. AIRCRAFT RETURNED TO GATE. ALL SYSTEMS CHECKED, NO DEFECTS FOUND. (M) 2L74 4F A20WE 19960119004941996011900494NM 1996 1 19 USAA951235 119951122A5313 STRINGER BOEING737 737201 1384454NM BS 947-977 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19224US45101 21666 ROA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND 30 INCH BY 2 INCH CORROSION AT STRINGER 27 LEFT BS 947 TO 977. REMOVED DAMAGE AND INSTALLED STRINGER SPLICE. (M) 2L72 4F A16WE 19960119004951996011900495EU 1996 1 19 USAA951248 119951206A5315 FLOOR BEAM FOKKERF28 F28MK0100 4990807EU BS 4830-5305 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19863US13264 11303 PIT - DURING APU MODIFICATION TRACK, FOUND CORROSION ON FLOOR BEAM, BETWEEN STATION 4850 AND 5305 AND BL 0. CUT OUT CORRODED SECTION OF BEAM AND SPLICED IN NEW 'T' EXTENSION PER SRM 51-70-06. (M) 2L72 4F RT 19960119004961996011900496NM 1996 1 19 USAA951252 119951211A532065C80735159 ANGLE BOEING737 737401 1384701NM BS 302-362 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE, Z-ANGLE. REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION. REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119004971996011900497NM 1996 1 19 USAA951253 119951211A53206545834256 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES, RBL 11 BS 312 TO BS 328, ON INTERCOSTAL. REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119004981996011900498NM 1996 1 19 USAA951254 119951211A53206545834260 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 312 TO BS 328, ON INTERCOSTAL. REPAIRED PER SRM 51-10-2, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119004991996011900499NM 1996 1 19 USAA951255 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 328 LBL 13 TO RIGHT END OF FLOOR BEAM. REPLACED T-CAP. REPAIRED PER TR 53-10-03 SRM 51-70-12 SRM 51-70-11, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005001996011900500NM 1996 1 19 USAA951256 119951211A5347 SEAT TRACKS BOEING737 737401 1384701NM BS 344-369 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 25 INCH BY .5 INCH CORRODED AREA LBL 22 BS 344-369, ON SEAT TRACKS. FABRICATED SEAT TRACKS AND INSTALLED. REPAIRED PER SRM 53-00-52, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005011996011900501NM 1996 1 19 USAA951257 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 947 LBL 4 AND RBL 4, ON FLOOR BEAM. INSTALLED T-CAP, REPAIR ANGLES AND STRAPS, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005021996011900502NM 1996 1 19 USAA951258 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 74 INCHES BY .5 INCHES CORRODED AREA BS 344 LBL 55 - RBL 21, ON FLOOR BEAM. FABRICATED T-CAP AND REPAIR ANGLE AND INSTALLED. REPAIRED PER TR 53-10-3, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005031996011900503NM 1996 1 19 USAA951259 119951211A5320654587512 ANGLE BOEING737 737401 1384701NM BS 277/344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 30 PERCENT CORRODED 'Z' ANGLE FORWARD GALLEY ENTRANCE, STATION 277 AND STATION 344. REMOVED AND REPLACED NR ME-32 REQUIRED. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005041996011900504NM 1996 1 19 USAA951260 119951211A53206545834259 INTERCOSTAL BOEING737 737401 1384701NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 328 TO BS 344, ON INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005051996011900505NM 1996 1 19 USAA951318 119951211A532065C80735116 Z-ANGLE BOEING737 737401 1384701NM BS 955-992 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 37 INCH CORRODED AREA BS 955 TO BS 992 AT LEFT AFT ENTRY DOOR, Z-ANGLE. REMOVED CORRODED Z-ANGLE AND INSTALLED NEW Z-ANGLE. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005061996011900506NM 1996 1 19 USAA951319 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 312 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 1 INCH CORRODED AREA BS 312, BL 0 (CABIN FLOOR BEAM UPPER FLANGE). CUTOUT CORRODED AREA, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER. REPAIRED PER SRM 53-10-51 AND FIG 206, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005071996011900507NM 1996 1 19 USAA951320 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 987 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH TO 2 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 987 LBL 45 TO RBL 45 ON FLOOR BEAM. SPLICED IN T-CAP. REPAIRED PER EA 40379, CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960119005081996011900508NM 1996 1 19 USAA951331 119951215A5313 STRINGER BOEING737 737201 1384454NM BS 947 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19226US43785 21815 ROA - DURING 'CX-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED STRINGER CAUSED BY LAVATORY SPILL, STRINGER 27L AT BS 947. REMOVED CORRODED STRINGER SECTION AND SPLICED IN NEW SECTION. REPAIRED PER SRM 53-10-3 FIG 1. (M) 2L72 4F A16WE 19960119005091996011900509NM 1996 1 19 USAA951332 119951215A5330 SKIN BOEING737 737201 1384454NM BS 360-540 DELAMINATION A USAAK NONE O OTHER ININSP/MAINT 1 EA19228US43618 21817 INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 360-540 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M) 2L72 4F A16WE 19960119005101996011900510NM 1996 1 19 USAA951333 119951215A5330 SKIN BOEING737 737201 1384454NM BS 727-908 DELAMINATION A USAAK NONE O OTHER ININSP/MAINT 1 EA19228US43618 21817 INT - DURING 'TRANS CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 LHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M) 2L72 4F A16WE 19960119005111996011900511NM 1996 1 19 USAA951334 119951215A5330 SKIN BOEING737 737201 1384454NM BS 727-908 DELAMINATION A USAAK NONE O OTHER ININSP/MAINT 1 EA19228US43618 21817 INT - DURING 'TRANSIT CHECK' ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES, BS 727-908 BETWEEN STRINGER 10 AND 14 RHS, ON FUSELAGE SKIN. REPLACED UPPER ROW OF RIVETS AT STRINGER 14. REPAIRED PER EA 3177A. (M) 2L72 4F A16WE 19960119005121996011900512NM 1996 1 19 USAA951335 119951215A5330 SKIN BOEING737 737201 1384454NM BS 727-908 DELAMINATION A USAAK NONE O OTHER ININSP/MAINT 1 EA19225US45495 21667 INT - DURING 'DROP IN-AV' VISUAL/ULTRASONIC INSPECTION, FOUND DELAMINATION VARIOUS SIZES AND LOCATIONS, FROM BS 727-908 LEFT WINDOW BELT PANEL BS 727-908 LEFT SIDE. REPLACED UPPER ROW OF FASTENERS BS 727-908 S-14 L. REPAIRED PER EA 31780. (M) 2L72 4F A16WE 19960119005131996011900513EU 1996 1 19 USAA951336 119951212A5320 WINDOW POST FOKKERF28 F28MK4000 4990810EU RT NR 2 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19475AU23021 11222 ROA - DURING 'TRANSIT CHECK' EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK RIGHT NR 2 WINDOW POST. STOP DRILLED AND PRIMED. REPAIRED PER TYPICAL REPAIR 53-10-01 REV A PAGE 3. (M) 2L72 4F RTA20EU 19960119005141996011900514NM 1996 1 19 USAA951337 119951206A5330 SKIN BOEING737 737201 1384454NM BS 303.37 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19241US37860 22443 ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK FORWARD ENTRY DOOR UPPER HINGE CUTOUT, STATION 303.37 STRINGER 10-L, IN FUSELAGE SKIN. REMOVED DAMAGE AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3, FIG 21 DETAIL 1. (M) 2L72 4F A16WE 19960119005151996011900515NM 1996 1 19 USAA951338 119951212A53131712450 STRINGER BOEING737 737201 1384454NM BS 948-993 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19244US36610 22752 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND 45 INCHES OF STRINGER 27L CORRODED, STRINGER 27L BETWEEN STATION 948 TO 993. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M) 2L72 4F A16WE 19960119005161996011900516NM 1996 1 19 USAA951339 119951212A53131712450 STRINGER BOEING737 737201 1384454NM BS 965 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19244US36610 22752 ROA - DURING 'CX-6' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 6 INCHES OF STRINGER CORRODED STRINGER 27R AT STATION 965. REMOVED CORROSION AND INSTALLED STRINGER SPLICE. (M) 2L72 4F A16WE 19960119005171996011900517NM 1996 1 19 USAASB95017 119951119A5210 DOOR BOEING737 7373B7 1384580NM L1 NOT LOCKED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19371US 22950 MSP - FLT NR 1090 - AIRCRAFT WOULD NOT PRESSURE AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND L1 DOOR NOT CLOSED PROPERLY. RECLOSED DOOR, PRESSURIZATION CHECKED NORMAL. (M) 2L72 4F RTA16WE 19960122000011996012200001NM 1996 1 22 W8PA9611 119951118A21317102047 CONTROLLER BOEING737 7373L9 1384470NM CABIN FAILED A W8PAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NM03961WP 6690 DA3385 23332 COS - FLT 243 - UNABLE TO CONTROL CABIN PRESSURIZATION. REPLACED CABIN PRESSURE CONTROLLER. (X) 2L72 4F RTA16WE 19960122000021996012200002EU 1996 1 22 SIMA953231 119951119A33503011210 LIGHT AEROSPATR42 ATR42300 8680920EU PASSENGER DOOR FAILED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21351AT 350 354 ORD - STA 4065 - WHILE MAINTENANCE WAS PERFORMING A PERIODIC CHECK, THE PASSENGER STAIR DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19960124000011996012400001NM 1996 1 24 TWRA9572 119951206A53478128757 SEAT TRACK BOEING747 747130 1384880NM LT COCKPIT CRACKED A TWRAK NONE O OTHER ININSP/MAINT 1 EA15603FF 19746 DURING B-CHECK SERVICE INSPECTION, PERFORMED A SPECIAL INSPECTION ON THE CAPTAINS SEAT TRACK AND FOUND A 3 INCH CRACK AT THE FORWARD OUTBOARD RAIL FWD END. SEAT TRACK WAS REPLACED. OPS CHECK OK. (M) 2L74 4F A20WE 19960126000011996012600001WP 1996 1 26 USAA951340 119951214A5311 BELT FRAME DOUG DC9 DC982 3022082WP BS 1309 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5/C-1 INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON BELT FRAME, STA 1309, BETWEEN LONGERON 28R AND LONGERON 28L. CORROSION TASK NR C57-53300. ACCOMPLISHED SPLICE REPAIR PER SRM 53-03, FIGURE 2A. (X) 2L72 4F A6WE 19960126000021996012600002WP 1996 1 26 USAA951341 119951218A5320 CLIP DOUG DC9 DC931 3022065WP BS 1019 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19914VJ66346 47068 PIT - DURING C-6 INSPECTION, FOUND 2 CRACKS APPROXIMATELY 2.25 INCHES IN LENGTH IN SHEAR CLIP AND PREVIOUS REPAIR DOUBLER AT FRAME STA 1019, LONGERON 14L. REMOVED DAMAGED AREA AND INSTALLED FILLER, REPAIR ANGLES, AND NEW SHEAR CLIP PER USAIR E.A. NR 31774. (X) 2L72 4F A6WE 19960126000031996012600003WP 1996 1 26 USAA951352 119951227A5531991183381 SPAR DOUG DC9 DC981 3022081WP VERT STABILIZER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US37750 48099 PIT - DURING Q-1/C-3 INSPECTION, FOUND A 3 INCH CRACK, VERTICAL STABILIZER FRONT SPAR AFT OF CANTED FRAME 1388. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER SRM 55-02-26. (X) 2L72 4F A6WE 19960126000041996012600004WP 1996 1 26 USAA951357 119951227A5313 LONGERON DOUG DC9 DC981 3022081WP BS 1418 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 1 INCH CRACK AT RIVET HOLE IN LONGERON 2R AT STA 1418, OUTBOARD LEG. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 5. (X) 2L72 4F A6WE 19960126000051996012600005WP 1996 1 26 USAA951358 119951227A531199155613 FRAME DOUG DC9 DC981 3022081WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 2 INCH BY 5 INCH LEVEL 1 CORROSION PREVIOUSLY REWORKED AFT SIDE OF FRAME WEB, STA 1338, BETWEEN LONGERONS 28R AND 28L. REMOVED CORRODED AREA OF WEB AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-16. (X) 2L72 4F A6WE 19960126000061996012600006WP 1996 1 26 USAA951359 119951227A5311993636827 FRAME DOUG DC9 DC981 3022081WP BS 937 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND 4 INCH CRACK IN FRAME MLG JAMB KEEL AREA, STA 937, CENTER SECTION. MANUFACTURED DOUBLER AND ANGLE REPAIR PER SRM 53-05. (X) 2L72 4F A6WE 19960126000071996012600007WP 1996 1 26 USAA951360 119951227A5312 BULKHEAD WEB DOUG DC9 DC981 3022081WP AFT PRESS BLKHD GOUGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND TOOLING MARKS (GOUGES), 6 INCH BY 4 INCH AREA BETWEEN LONGERON 27L AT BOTTOM LT SIDE OF AFT PRESSURE BULKHEAD. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 20. (X) 2L72 4F A6WE 19960126000081996012600008WP 1996 1 26 USAA951361 119951227A5230 PAN DOUG DC9 DC981 3022081WP CARGO DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND LOWER FORWARD CARGO DOOR PAN CORRODED/CRACKED IN 2 PLACES APPROXIMATELY .50 INCH IN LENGTH EACH. ACCOMPLISHED SPLICE REPAIR PER SRM 53-05, FIGURE 44. (X) 2L72 4F A6WE 19960126000091996012600009WP 1996 1 26 USAA951362 119951227A5530 ANGLE DOUG DC9 DC981 3022081WP VERT STABILIZER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19819US34764 48099 PIT - DURING Q-1/C-3 CHECK INSPECTION, FOUND .75 INCH VERTICAL CRACK AFT SIDE OF STA 1388, CANTED FRAME, IN ANGLE ON LEFT FRONT SPAR OF VERTICAL STABILIZER. INSTALLED ANGLE REPAIR PER SRM 55-02, FIGURE 26. (X) 2L72 4F A6WE 19960126000101996012600010WP 1996 1 26 USAA951363 119951226A5414 SKIN DOUG DC9 DC931 3022065WP BS 965 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19922VJ34880 48142 PIT - WHILE ACCOMPLISHING X-RAY INSPECTION OF PYLON AREA IN BOS, MAINTENANCE DISCOVERED A .25 INCH CRACK IN SKIN AT STA 965, LONGERON 14L. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIR. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED PER USAIR EA NR 31838. AIRCRAFT RELEASED TO SERVICE. (X) 2L72 4F A6WE 19960126000111996012600011NM 1996 1 26 USAA951373 119951222A5320654587545 ANGLE BOEING737 7372B7 1384560NM BS 294-360 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION .50 INCH BY 66 INCHES AT Z-ANGLE AT FORWARD SERVICE DOOR AREA STA 294 TO STA 360. REPLACED Z-ANGLE. REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000121996012600012NM 1996 1 26 USAA951374 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH BY .50 INCH HOLE AT WEB OF FLOOR BEAM, STA 1016 PLUS 6 INCHES, RBL 6. INSTALLED DOUBLER. REPAIRED PER SRM 51-40-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000131996012600013NM 1996 1 26 USAA951375 119951222A5347 SEAT TRACKS BOEING737 7372B7 1384560NM BS 986-1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT SEAT TRACKS 1 INCH BY 1 INCH, RBL 8, RBL 24, AND RBL 36 AT STA 986 - STA 1016. REPLACED THREE SEAT TRACKS. REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000141996012600014NM 1996 1 26 USAA951377 119951222A5320 FLOOR WEB BOEING737 7372B7 1384560NM BS 1016 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH ROUND AREA AT NUTPLATE CORRODED, FLOOR WEB 10 INCHES AFT OF FLOOR BEAM, BS 1016, BL ZERO. CUT OUT CORROSION, INSTALLED DOUBLER. REPAIRED PER SRM 51-40-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000151996012600015NM 1996 1 26 USAA951378 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 957 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL CLIP NUT HOLES, STA 957. MANUFACTURED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000161996012600016NM 1996 1 26 USAA951379 119951222A5311 FRAME BOEING737 7372B7 1384560NM BS 992 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.50 INCH BY 1 INCH CORROSION AT FRAME BS 992. MANUFACTURED FRAME REPAIR, HEAT TREATED, AND INSTALLED. REPAIRED PER SRM 51-40-3, SPM 20-30-06. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000171996012600017NM 1996 1 26 USAA951382 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 294-312 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 12, STA 294 - STA 312. INTERCOSTAL REPLACED. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000181996012600018NM 1996 1 26 USAA951383 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 316 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORRODED INTERCOSTAL RBL 11, STA 316. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C52-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000191996012600019NM 1996 1 26 USAA951384 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 328-344 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP FLANGE OF INTERCOSTAL, RBL 11, STA 328 TO STA 344. INSTALLED NEW PART ON AIRCRAFT. REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000201996012600020NM 1996 1 26 USAA951385 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 296 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35996 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION ON INTERCOSTAL, LBL 10, STA 296. INSTALLED NEW INTERCOSTAL. REPAIRED PER SRM 51-10-1, RESTORED TO ORIGINAL. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000211996012600021NM 1996 1 26 USAA951386 119951222A5320654587512 ANGLE BOEING737 7372B7 1384560NM DOOR SILL CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND CORROSION .50 INCH BY 1 INCH FORWARD SERVICE DOOR SILL PLATE SUPPORT ANGLE. REPLACED ANGLE, REPAIRED PER SRM 51-10-01. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000221996012600022NM 1996 1 26 USAA951387 119951222A5320 TEE CAP BOEING737 7372B7 1384560NM FS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 3 INCH BY 8 FEET CORROSION FS 328, RBL 10 INCHES, RBL 58 INCHES, TEE CAP. INSTALLED LOCAL MANUFACTURED TEE CAP AND SPLICED ANGLES. REPAIRED PER T.R. 53-10-13, EA 40349. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000231996012600023NM 1996 1 26 USAA951388 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 328 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH BY 48 INCH CORRODED CABIN FLOOR BEAM, BS 328 AT RBL 10 INCHES - RBL 58 INCHES. REMOVED CORRODED SECTION OF T-CAP AND SPLICED IN NEW SECTION. REPAIRED PER TR 53-10-13. CORRISION TASK NR C53-107-02. CORROSION LEVEL 2. (X) 2L72 4F A16WE 19960126000241996012600024NM 1996 1 26 USAA951389 119951222A532065C10592 ANGLE BOEING737 7372B7 1384560NM BS 947-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH FLOOR SUPPORT ANGLE CORRODED AT CLIP NUT HOLES, STA 947 - STA 986, BL ZERO, WL 208.1. INSTALLED NEW PRE-FAB ANGLE. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED SRM 51-10-1, PAGE 5. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000251996012600025NM 1996 1 26 USAA951390 119951222A5347 SEAT TRACK BOEING737 7372B7 1384560NM BS 986-1016 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIP NUT HOLES, STA 986 - STA 1016, RBL 24 AND RBL 26, WL 208.1 SEAT TRACK. REPLACED SEAT TRACKS, REPAIRED PER SRM 51-10-01. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000261996012600026NM 1996 1 26 USAA951391 119951222A53201124784 ANGLE BOEING737 7372B7 1384560NM BS 947-986 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORRODED Z-ANGLE AT LEFT REAR CABIN ENTRY DOOR, STA 947 - STA 986, LBL 50, WL 208.1. INSTALL NEW PREFABRICATED Z-ANGLE. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER SRM 510-10-1, PAGE 5, ITEM 4. (X) 2L72 4F A16WE 19960126000271996012600027NM 1996 1 26 USAA951392 119951222A5320 ANGLE BOEING737 7372B7 1384560NM BS 947-1006 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 36 INCH AREA OF SURFACE CORROSION, 1 INCH CIRCLE OF EXFOLIATION AT RIGHT REAR CABIN DOOR Z-ANGLE, STA 947 - STA 1006, RBL 50, WL 208.1. REPLACED Z-ANGLE. REPAIRED PER SM 51-10-01. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000281996012600028NM 1996 1 26 USAA951393 119951222A5330 SKIN BOEING737 7372B7 1384560NM BS 500 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 4.5 INCH BY 6.5 INCH CORROSION, BS 550A PLUS 10 INCHES, STRINGER 28 RIGHT, FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER EA 40449. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000291996012600029NM 1996 1 26 USAA951394 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CLIP-NUT HOLES CORRODED ENTIRE LENGTH OF FLOOR BEAM STA 986.5, RBL 70 - LBL 70 FLOOR BEAM WL 208.1. REPLACED T-CAP OF BEAM. REPAIRED PER TR 53-10-05 C. CORROSION LEVEL 1. (X) 2L72 4F A16WE 19960126000301996012600030NM 1996 1 26 USAA951395 119951222A5230 SKIN BOEING737 7372B7 1384560NM CARGO DOOR DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 36 INCH BY 22 INCH DOUBLER PREVIOUSLY INSTALLED EXTERNAL SKIN OF AFT CARGO DOOR FUSELAGE SKIN. DOUBLER INSTALLED, REPAIRED PER 737-200, SRM 52-00-3, FIGURE 5. (X) 2L72 4F A16WE 19960126000311996012600031NM 1996 1 26 USAA951396 119951222A5330 SKIN BOEING737 7372B7 1384560NM BS 847 DAMAGED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 9 INCH BY 5.50 INCH DOUBLER PREVIOUSLY INSTALLED FUSELAGE SKIN, BS 847, S22R. REPAIR IS PER SRM, DOUBLER INSTALLED, REPAIRED PER SRM 737-200, SRM 53-30-3, FIGURE 1. (X) 2L72 4F A16WE 19960126000321996012600032NM 1996 1 26 USAA951397 119951222A5311 FRAME BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU 22882 INT - DURING 'Q-2' CHECK EDDY CURRENT, FOUND CRACKED FRAME .5 INCH LONG AT STA 727, S18R. REPLACED FRAME SECTION, EO 5394G068. (X) 2L72 4F A16WE 19960126000331996012600033NM 1996 1 26 USAA951398 119951222A5320 INTERCOSTAL BOEING737 7372B7 1384560NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT LBL 25 INTERCOSTAL 1 INCH FORWARD OF BS 520, FLOOR BEAM WL 206 (UPPER CHORD). REPLACED INTERCOSTAL PER SRM 51-10-2. (X) 2L72 4F A16WE 19960126000341996012600034NM 1996 1 26 USAA951399 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 707-713 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SIX, .25 INCH CRACKS, BL ZERO, LONGITUDINAL FLOOR BEAM WEB BETWEEN STA 707 - STA 713, WL 203. INSTALLED REPAIR DOUBLER, REPAIRED PER BOEING DRAWING NR 65C34537. (X) 2L72 4F A16WE 19960126000351996012600035NM 1996 1 26 USAA951400 119951222A5330 SKIN BOEING737 7372B7 1384560NM BS 907 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1 INCH BY 1 INCH DENT STA 907, S17L, SKIN. INSTALLED 1.50 INCH BY 1.50 INCH FILLER 2024-T3 .080, AND 7 INCH BY 8 INCH DOUBLER 2024-T3 .090. REPAIRED PER SRM 53-30-3, FIGURE 28. (X) 2L72 4F A16WE 19960126000361996012600036NM 1996 1 26 USAA951401 119951222A5311 FRAME BOEING737 7372B7 1384560NM BS 460 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND SEVERAL CRACKS IN HOLES BETWEEN S20L AND S21L, ONE, .50 INCH CRACK AT ATTACH HOLE FOR TRANSITION ANGLE FRAME, BS 460, LEFT SIDE. CUT OUT CRACK AT TRANSITION AREA OF FRAME AND BETWEEN S20L AND S21L. MANUFACTURED, HEAT TREATED, AND INSTALLED REPAIR AND FILLER. REPAIRED PER SRM 20-30-06, SRM 53-10-4. (X) 2L72 4F A16WE 19960126000371996012600037NM 1996 1 26 USAA951402 119951222A5313 STRINGER BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 IINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK APPROXIMATELY .1850 INCH, BS 727, S18A, LEFT SIDE. INSTALLED SPLICE STRAPS, REPAIRED PER EA 40542. (X) 2L72 4F A16WE 19960126000381996012600038NM 1996 1 26 USAA951403 119951222A532069353521 CLIP BOEING737 7372B7 1384560NM BS 707 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S4R TIE CLIP STA 707. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X) 2L72 4F A16WE 19960126000391996012600039NM 1996 1 26 USAA951407 119951222A5320693535214 CLIP BOEING737 7372B7 1384560NM BS 767 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .25 INCH LONG CRACK STA 767 AT STRINGER 10 RIGHT, TIE CLIP. REPLACED TIE CLIP PER EO 5393G227. (X) 2L72 4F A16WE 19960126000401996012600040NM 1996 1 26 USAA951408 119951222A532069353214 CLIP BOEING737 7372B7 1384560NM BS 747 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG STA 747 AT STRINGER 6 RIGHT, TIE CLIP. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X) 2L72 4F A16WE 19960126000411996012600041NM 1996 1 26 USAA951409 119951222A5320693535214 CLIP BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT TIE CLIP, STA 727, STRINGER 5 RIGHT. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (X) 2L72 4F A16WE 19960126000421996012600042NM 1996 1 26 USAA951410 119951222A5320 CHORD BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURNG 'Q-2' CHECK EDDY CURRENT INSPECTION, FOUND 2 CRACKS IN AFT OPEN FASTENER HOLE BS 727, OUTBOARD CHORD, BS 727, STRINGER 18L, IN OUTBOARD CHORD. INSTALLED LEFT 727 OUTBOARD CHORD, REPAIRED PER EO 5394G068 AND 262-21-93828. (X) 2L72 4F A16WE 19960126000431996012600043NM 1996 1 26 USAA951411 119951222A5312 BULKHEAD BOEING737 7372B7 1384560NM BS 727 DENTED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INIT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH BY 3 INCH DENTED AREA PRESSURE BULKHEAD, STA 727, BULKHEAD RBL 40. REPAIRED OVERSIZED FASTENER HOLES AND INSTALLED REPAIR PER EO. WEIGHT CHANGE LESS THAN 1 POUND. REPAIRED PER EO 5394G068 AND BOEING DRAWING 65C33722. (X) 2L72 4F A16WE 19960126000441996012600044NM 1996 1 26 USAA951412 119951222A5320 WEB BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG AT WEB, STRINGER 18A RIGHT, STA 727. INSTALLED DOUBLER, REPAIRED PER EA 40452. (X) 2L72 4F A16WE 19960126000451996012600045NM 1996 1 26 USAA951413 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION ON FLOOR BEAM BS 344, LBBL 15. INSTALLED NEW T-CAP REPAIRED PER TR 53-10-13. (X) 2L72 4F A16WE 19960126000461996012600046NM 1996 1 26 USAA951414 119951222A524165C340689 GATE HINGE BOEING737 7372B7 1384560NM GALLEY DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 15 INCH CRACK IN HINGE AT LOWER GATE, LOWER GATE HINGE OF FORWARD GALLEY DOOR. INSTALLED IMPROVED PART, REPAIRED PER EA 40349. (X) 2L72 4F A16WE 19960126000471996012600047NM 1996 1 26 USAA951415 119951222A5313 STRINGER BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK .25 INCH LONG IN STRINGER 18A LEFT, STA 727. INSTALLED DOUBLERS, REPAIRED PER EA 40452. (X) 2L72 4F A16WE 19960126000481996012600048NM 1996 1 26 USAA951416 119951222A532065C8073584 T-SPLICE BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .3750 INCH CRACK S27L (KEEL BEAM) TO BS 727 BULKHEAD ATTACH ANGLE 1 INCH AFT OF BULKHEAD PLUS 5 INCHES ABOVE LOWER SKIN T-SPLICE. INSTALLED PREFABRICATED T-SPLICE, REPAIRED PER BOEING DRAWING 69-41460. (X) 2L72 4F A16WE 19960126000491996012600049NM 1996 1 26 USAA951417 119951222A53126938933503 BLKHD STIFFENER BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK STA 727 BULKHEAD STIFFENER FITTING LBL 25, WL 202.5. REPLACED FITTING. REPAIRED PER SRM 5-10-1. (X) 2L72 4F A16WE 19960126000501996012600050NM 1996 1 26 USAA951418 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 676 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING 'Q-2' CHECK VISUAL INSPECTION FOUND 1.25 INCH CRACK LBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STA 676. WL 206.5. INSTALLED DOUBLER, REPAIRED PER EA 40395, EO 5791G632. (X) 2L72 4F A16WE 19960126000521996012600052WP 1996 1 26 USAAD9500A 119951229A30406171 HEAT CONTROLLER DOUG DC9 DC931 3022065WP LT WINDSHIELD FAILED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19921VJ32589 48141 BOS - FLT 1204 - EN ROUTE PHL-PWM, THE OUTER PANE OF THE CAPTAIN'S WINDSHIELD BEGAN TO ARC AND CRACK. FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE WINDSHIELD HEAT CONTROLLER. (X) 2L72 4F A6WE 19960126000531996012600053 1996 1 26 USAAD9500B 419951231A3421258733513 VERTICAL GYRO DOUG DC9 DC981 3022081WP E/E BAY FAULTY A USAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA19828US286903029 48028 GSO - FLT 667 - EN ROUTE PIT-RDU, CREW RECEIVED 'HORIZON' ALERT. FLIGHT DIVERTED TO GSO DUE TO WEATHER AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 VERTICAL GYRO. (X) 2L72 4F A6WE 19960126000541996012600054 1996 1 26 USAAD9500C 419951230A2350G3737 AUDIO SELECT DOUG DC9 DC981 3022081WP LT COCKPIT INTERMITTENT A USAAA UNSCHED LANDING O OTHER CLCLIMB 1 EA19809US9551 48041 PIT - FLT 987 - AFTER TAKEOFF FROM PIT, CREW EXPERIENCED LOSS OF RADIO COMMUNCIATIONS. SHORTLY THEREAFTER, ONE RADIO BEGAN TO WORK. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAIN'S AUDIO SELECTOR PANEL AND MICROPHONE. (X) 2L72 4F A6WE 19960126000551996012600055NM 1996 1 26 USAASB95027 119951217A2130 PRESSURIZATION BOEING737 7373B7 1384580NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19520AU 23706 FLT NR 263 - ATL - CABIN PRESSURIZATION STARTED TO INCREASE AT 1K FEET PER MINUTE. FLT DIVERTED TO ATL DUE TO HIGH FUEL CONSUMPTION AT LOWER FLIGHT LEVEL THAT THE A/C WAS REQUIRED TO FLY AT. NO EMERGENCY WAS DECLARED AND THE OXYGEN MASKS WERE NOT DEPLOYED. (M) 2L72 4F RTA16WE 19960126000561996012600056NM 1996 1 26 USAASB95028 119951217A2130 PRESSURIZATION BOEING737 7373B7 1384580NM CABIN MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19385US 22958 FLT 2301 - SYR - ON TAKEOFF, AUTO PRESSURIZATION FAILED. STANDBY WOULD NOT PRESSURIZE THE AIRCRAFT. LEVELED OFF AT 8000 FEET AND RETURNED TO SYR. (M) 2L72 4F RTA16WE 19960126000571996012600057NM 1996 1 26 USAASB95029 119951216A49303609150 FUEL CONTROL BOEING737 737201 1384454NM APU FAILED A USAAB EMER. DESCENT J WARNING INDICATION NRNOT REPORTED 1 EA19234US 22274 FLT NR 8582 - RSW - AFTER SECOND APU START ATTEMPT APU FIRE LIGHT ILLUMINATED APU FIRE SWITCH PULLED AND BOTTLE DISCHARGED. REMOVED AND REPLACED THE APU FCU. ADJUSTED CRACK PRESSURE. CLEANED SHROUD DRAINS. REPLACED IGNITOR LEADS. APU OPS NORMALLY. (M) 2L72 4F A16WE 19960126000581996012600058NM 1996 1 26 USAASB95030 119951217A5210 PASSENGER DOOR BOEING737 737301 1384611NM CABIN NOT CLOSED A AUSAAA UNSCHED LANDING O OTHER NRNOT REPORTED 1 EA19350US 23553 PHL - FLT 451 - UNABLE TO PRESSURIZE AIRCRAFT. FOLLOWED ALL USAIR PROCEDURES, NO HELP. F/A ADVISED IN PHL THAT THE DOOR WAS HARD TO SHUT. ALSO, HAD TO SHUT DOWN AND RESTART LEAVING DCA PRIOR TO STARTING ENGINE. THERE WAS A PRESSURE BUMP. FOUND CABIN DOOR NOT PROPERLY CLOSED. FALSE LOCK INDICATION. OPS CHECK DOOR OPERATION. OPS CHECK GOOD. PRESSURIZED AIRCRAFT AND INSPECTED DOOR. OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19960126000591996012600059NM 1996 1 26 USAASB95032 119951225A3230 RETRACT MECH BOEING737 737201 1384454NM LANDING GEAR MALFUNCTIONED A USAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA19243US 22445 FLT NR 1177 - BWI - RETURN TO FIELD, UNABLE TO RETRACT LANDING GEAR. GEAR HANDLE WOULD NOT GO TO UP, DID NOT ATTEMPT TO OVERRIDE. (M) 2L72 4F A16WE 19960126000611996012600061NM 1996 1 26 95UAL900351 119951227A3231652676134 ACTUATING ARM BOEING727 727222 1384073NM PWA JT8 JT8D15 52051NE RT MLG DOOR FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP297251U 21398 RIGHT MAIN GEAR FAILED TO RETRACT. RT GEAR INTRANSIT LIGHT ON DURING FIRST ATTEMPT. CYCLED GEAR AND RT GEAR LIGHT AND RT GEAR DOOR LIGHT ON. FLIGHT RETURNED TO ORD. REMOVED, INSPECTED AND REINSTALLED RIGHT MLG OUTER DOOR ACTUATION ARM. JACKED AIRCRAFT AND PERFORMED OPERATIONAL AND FREE FALL TESTS. ALSO, DID FUNCTIONAL TEST OF MLG SENORS, ALL NORMAL. 2L73 4F4 F A3WE E2EA 19960126001311996012600131WP 1996 1 26 96ZZZX303 119951204A5347 SEAT TRACK DOUG DC9 DC983 3022083WP BS 200-232 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, RBL 22, STA 200 - STA 232. INSTALLED NEW SECTION OF TRACK PER SRM 51-01 AND SPLICED PER SRM 53-05, FIGURE 4I. AIRCRAFT TOTAL TIME: 25,931 HOURS; 13,041 CYCLES. 2L72 4F RTA6WE 19960126001321996012600132WP 1996 1 26 96ZZZX304 119951204A5347 SEAT TRACK DOUG DC9 DC983 3022083WP NR 3 TRACK CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 DURING OP-16, FOUND CORROSION ON FORWARD END OF NR 3 FLOOR TRACK. INSTALLED NEW SECTION OF TRACK PER SRM 51-01, AND SPLICED PER SRM 53-05, FIGURE 4F. AIRCRAFT TOTAL TIME: 25,931 HOURS; 13,041 CYCLES. 2L72 4F RTA6WE 19960126001401996012600140WP 1996 1 26 96ZZZX312 119951215A3260833703 UPLOCK SENSOR 593535450113DOUG DC9 DC981 3022081WP RT MLG INTERMITTENT A A4JAO OTHER N FALSE WARNING CLCLIMB 1 SO15817SJ 48051 LGB/DFW - FLT 619 - AFTER TAKEOFF FROM LGB, THE RIGHT MLG UNSAFE LIGHT (RETRACT) REMAINED ON. RE-CYCLED LANDING GEAR, AND LIGHT WENT OUT. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MLG UPLOCK SENSOR. OPERATIONAL TEST SATISFACTORY. 2L72 4F A6WE 19960126001411996012600141WP 1996 1 26 96ZZZX313 119951222A3260801801 DOWNLOCK SWITCH 59104475041 DOUG DC9 DC951 3022051WP NLG INOPERATIVE A A4JAO OTHER N FALSE WARNING APAPPROACH 1 SO15919PJ 47663 NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO AIR NOISE, NO VIBRATION. HYDRAULIC PUMP TO 'HIGH' HAD NO AFFECT. WHEN GEAR EXTENDED FOR LANDING, UNSAFE LIGHT STAYED ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND WIRE BROKEN IN NOSE GEAR AT DOWNLOCK PROXIMITY SWITCH, AND DOWNLOCK PROXIMITY SWITCH INOPERABLE. REPLACED DOWNLOCK PROXIMITY SWITCH, REPAIRED WIRE. PERFORMED GEAR SWING - OPS CHECKED GOOD. (X) 2L72 4F A6WE 19960126001421996012600142WP 1996 1 26 96ZZZX314 119951220A361057077356 BRACKET DOUG DC8 DC862 3021970WP NLG WW BROKEN A ARWAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SO19802BN 45909 KOAK/KLSC - FLT 518 - EN ROUTE KOAK, DIVERTED TO KLSC WITHOUT FURTHER INCIDENT. AT FL 370, AFTER LOUD NOISE, EXPERIENCED RAPID DEPRESSURIZATION. MAINTENANCE FOUND SLEEVE OFF OF SLIP JOINT ON SUPPLY DUCT IN RIGHT TUNNEL IN NLG WHEELWELL WITH DUCT SUPPORT BRACKET BROKEN. INSTALLED NEW BRACKET AND RECONNECTED DUCT. OPS CHECK OK IAW MM 21-10-0. 2L74 4F 4A25 19960126001431996012600143WP 1996 1 26 96ZZZX315 119951220A242051508000 GEN CONTROL PNL DOUG DC8 DC862 3021970WP COCKPIT FAILED A ARWAA UNSCHED LANDING H ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 SO19810BN 45905 KBOG - FLT 239 - AFTER APPROXIMATELY ONE HOUR INTO FLIGHT WITH ALL GENERATORS IN PARALLEL MODE, ALL LIGHTS IN AIRCRAFT WENT ON AND OFF SEVERAL TIMES. OPERATED GENERATORS IN ISOLATED MODE. AFTER APPROXIMATELY TWO MINUTES, NR 1 GENERATOR TRIPPED OFF-LINE WHEN IN PARALLEL, ALL LOAD METERS FLUCTUATED. WHEN IN ISOLATED MODE, ALL LOADMETERS NORMAL. TRIED TO RESET NR 1 GENERATOR, NO HELP. FLIGHT RETURNED TO KMIA. ACCOMPLISHED PHYSICAL CHECK OF POWER CENTER AND NR 1 GENERATOR WIRING. ACCOMPLISHED RUN-UP AND ELECTRICAL SYSTEMS CHECK. REMOVED AND REPLACED NR 1 GENERATOR. OPS NORMAL PER MM 24-20-6. 2L74 4F 4A25 19960126001441996012600144NE 1996 1 26 96ZZZX316 219951223A73106667621 FILTER UA5296051 DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 1,4 ENGINES CLOGGED A ARWAA UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 SO19810BN 45905 MAO - ON FLIGHT TO MAO, AIRCRAFT DIVERTED TO SJU DUE TO EXCESSIVELY HIGH ENGINE FUEL PRESSURE ON NR 1 AND NR 4 ENGINES. REMOVED NR 1 AND NR 4 ENGINE FUEL TEMP REGULATOR FILTERS. FOUND TO BE CLOGGED. INSTALLED NEW FILTERS AND ENGINE RUN-UP CHECKED NORMAL. AIRCRAFT CONTINUED TO MAO WITHOUT INCIDENT. UPON RETURN TO MIAMI, ALL 4 FUEL TEMP REGULATOR FILTERS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2L74 4F4 F 4A25 1E8 19960126001451996012600145NM 1996 1 26 96ZZZX317 119951220A3350900835A BATTERY PACK BOEING737 7372T4 1384492NM CABIN DISCHARGED A SPAAK NONE L NO TEST ININSP/MAINT 1 WP07703S 22529 DURING SCHEDULED CHECK, THE FORWARD 'AREA LIGHT/LIGHTED EXIT' INTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE ASSOCIATED BATTERY PACK WAS REPLACED. SUBSEQUENT OPS CHECKS WERE SATISFACTORY PER THE BOEING MM 33-51-11. 2L72 4F A16WE 19960126001461996012600146WP 1996 1 26 96ZZZX318 119951224A32105925306501 TORQUE LINK DOUG DC9 DC932 3022066WP RT MLG FAILED A VJ6AO OTHER O OTHER LDLANDING 1 SO11903VJ 47261 ATL/RDU - FLT 292 - ON LANDING ROLL-OUT, CREW REPORTED BOTH MAIN TIRES ON RT SIDE BLOWN. AIRCRAFT NOT ABLE TO CLEAR RUNWAY. MAINTENANCE FOUND THE RT MAIN GEAR TORQUE LINKS HAD FAILED ALLOWING WHEELS/AXLES TO ROTATE HORIZONTALLY. AIRCRAFT FERRIED TO MIA FOR FURTHER EVALUATION. REPLACED RT MLG ANTI-SKID TRANSDUCER HARNESS PER DC9 MM 32-43-2. REMOVED RT MAIN GEAR PISTON ASSY. INSPECTED RT MLG STRUT INTERNAL SURFACES, NO DEFECTS NOTED. INSTALLED RT MLG PISTON ASSY PER DC9 MM 32-11. 2L72 4F A6WE 19960126001481996012600148WP 1996 1 26 96ZZZX320 119951224A2913AS66411LS666 HYDRAULIC PUMP DOUG DC9 DC932 3022066WP NR 1 ENGINE FAILED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11940VV 47523 IAD/RDU - FLT 295-1 - PILOT REPORTED LEFT HYDRAULIC PUMP FAILURE. DIVERTED FLIGHT TO ATL FROM RDU. REMOVED AND REPLACED LEFT ENGINE HYDRAULIC PUMP. OPS CHECK NORMAL. PER MM 29-10. 2L72 4F A6WE 19960126001491996012600149WP 1996 1 26 96ZZZX321 119951220A32306F2382 VALVE DOUG DC9 DC932 3022066WP NLG MALFUNCTIONED A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11945ML 47168 FLT 543 - AIR RETURN, NOSE GEAR UNSAFE LIGHT ON WHEN GEAR WAS RETRACTED. LOWERED GEAR AND GOT 3 EACH GREEN LIGHTS AND LANDED. REMOVED AND REPLACED DOWN LINE CHECK VALVE, PERFORMED SEVERAL GEAR SWINGS AND UPLATCH CHECKS. OPS CHECK NORMAL PER MM 32-10. 2L72 4F A6WE 19960126001501996012600150NM 1996 1 26 96ZZZX323 119951230A612030005000024 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07912HA14346 40 CHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR HNAA9591231. 2H72 4T RTA13NM 19960126001511996012600151SW 1996 1 26 BDHA9600001 119951228A29102781006117 HYDRAULIC LINE SWRNGNSA226 SA226TC 8780404SW RT FLAP WELL CHAFED A BDHAD RETURN TO BLOCK K FLUID LOSS TXTAXI/GRND HDL 1 GL15328BA TC253 MSP - FLT 421 - WHILE TAXIING, THE PILOT NOTICED RAPID LOSS OF HYDRAULIC PRESSURE AND THE NOSEWHEEL STEERING BECAME STIFF. AFTER RETURNING TO HANGAR, MAINTENANCE FOUND A LINE CHAFED BY A CLAMP IN THE RIGHT FLAP WELL. THE FAULTY LINE WAS REPLACED AND LEAK CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 1L72 4T A8SW 19960126001531996012600153WP 1996 1 26 GRAA9559 119950103A3350P4010021 POWER SUPPLY DOUG DC9 DC987 3022087WP CABIN INOPERATIVE A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111074T 49727 WHILE PERFORMING T/O INSPECTION ON DECEMBER 15, 1995, MAINTENANCE PERSONNEL NOTICED EMERGENCY FLASHLIGHT INDICATOR LIGHT BLINKING SLOWLY. MX REMOVED AND REPLACED BATTERY POWER SUPPLY WITH SERVICEABLE PART. FLASHLIGHT INDICATOR LIGHT BLINKS NORMALLY. (M) 2L72 4F RTA6WE 19960126001551996012600155NM 1996 1 26 HNAA9591231 119951230A612030005000024 CONTROL UNIT SIMMONDS DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07912HA14346 2156 40 CHO/CLT - FLT 3156 - DURING PRE-FLIGHT CHECKS, THE AUTOFEATHER TEST WAS FOUND INOPERATIVE. COULD NOT DUPLICATE. REMOVED AND REPLACED THE NR 1 AND NR 2 TORQUE SENSOR CONTROL UNITS. REFERENCE CONTROL NR 96ZZZX323. (X) 2H72 4T RTA13NM 19960126001561996012600156NM 1996 1 26 HNAA9592429 119951229A612030005000046 CONTROL UNIT DHAV DHC8 DHC8102 2809003NM NR 1 ENGINE FAILED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07924HA 105 BWI/RDU - FLT 3393 - THE AUTOFEATHER WOULD NOT ARM ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 1 TORQUE SENSOR CONTROL UNIT. (X) 2H72 4T RTA13NM 19960126001571996012600157NM 1996 1 26 HNAA9597832 119951230A335082410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003NM CABIN FAILED A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07978HA13203 226 CHO/PIT - FLT 3014 - DURING PREFLIGHT WALKAROUND, DISCOVERED THE EMERGENCY LIGHTS REMAINED DIM ON ARM POSITION AND WILL NOT SHUT OFF. REMOVED AND REPLACED THE CONTROL BOX FOR THE EMERGENCY LIGHTS. (X) 2H72 4T RTA13NM 19960126001581996012600158NM 1996 1 26 HNAA9597930 119951231A3350 CONNECTOR DHAV DHC8 DHC8102 2809003NM CABIN LOOSE A HNAAK NONE L NO TEST ININSP/MAINT 1 EA07979HA 373 RDU/BWI - FLT 3345 - DURING PREFLIGHT WALKAROUND, FOUND THE EMERGENCY EXIT LIGHT OVER THE PASSENGER DOOR INOPERATIVE. SECURED A LOOSE PIN ON THE CONNECTOR. (X) 2H72 4T RTA13NM 19960126001591996012600159NM 1996 1 26 MZZA95051 119951208A2782651781822 ACTUATOR BOEING727 727232 1384082NM NR 5 L/E SLAT LEAKING A MZZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP1315781 20636 AFTER TAKEOFF ON CLIMB-OUT FROM SPN, LOST ALL A-SYSTEM HYDRAULIC QUANTITY. FLIGHT CONTINUED TO GUM AND GEARS EXTENDED MANUALLY FOR LANDING. MAINTENANCE FOUND NR 5 L/E SLAT ACTUATOR LEAKING EXCESSIVELY. REMOVED AND REPLACED ACTUATOR ASSY. ALSO REPLACED BOTH A-SYSTEM HYDRAULIC PUMPS AND FILTER ASSEMBLIES. SLAT SYSTEM OPERATION CHECK GOOD. HYDRAULIC SYSTEM OPERATION CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED BACK TO SERVICE. (X) 2L73 4F A3WE 19960126001601996012600160WP 1996 1 26 ORJA95138 119951214A32462601483 BOLT BENDIX 26088911 DOUG DC9 DC982 3022082WP NR 2 WHEEL ASSY BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11822RA 2958 49932 NR 2 WHEEL THROUGH-BOLT SHEARED. REPLACED NR 4 WHEEL ASSY. (X) 2L72 4F A6WE 19960126001611996012600161WP 1996 1 26 ORJA95139 119951222A32462601483 BOLT BENDIX 26088911 DOUG DC9 DC983 3022083WP NR 2 WHEEL ASSY MISSING A ORJAK NONE O OTHER ININSP/MAINT 1 WP11872RA 1456 49793 FOUND NR 3 MAIN WHEEL MISSING LEA. TY-BOLT. REMOVED AND REPLACED MAIN WHEEL ASSY PER MM 32-40-01. (X) 2L72 4F RTA6WE 19960126001621996012600162WP 1996 1 26 ORJA95140 119951228A335041B994AD073 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ORJAK NONE L NO TEST ININSP/MAINT 1 WP11821RA 49931 EMERGENCY FLOOR LIGHT DOES NOT WORK FROM GALLEY TO ROW 2R. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD. (X) 2L72 4F A6WE 19960126001641996012600164EU 1996 1 26 P2RA950026 119951231A5330202473 SKIN AIRBUS300 A300B4203 3930306EU BS 1964 PUNCTURED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314975 261 DURING SERVICE CHECK, FOUND PUNCTURE DAMAGE TO LEFT FUSELAGE STA 1694, BETWEEN STRINGERS 27L AND 28L. REPAIRED DAMAGE PER AIRBUS ENGINEERING TEMPORARY REPAIR. APPROVED TO NEXT 'C' CHECK, MARCH 17, 1996, PER AIRBUS DOCUMENT 94A-1810/95/AG, DECEMBER 31, 1995. (X) 2L72 4F A35EU 19960126002781996012600278CE 1996 1 26 96ZZZX325 119951024A243503600918 BEARING BEECH 1900 1900 1154160CE LT START/GEN FAILED A HSYAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 NM057254R 390 UB22 DEN - FLT 7536 - DURING CLIMB-OUT, LEFT GENERATOR FAILED. PILOT RETURNED TO BASE WITH NO FURTHER INCIDENT. AFT BEARING, PN 03-6009-18, WAS FOUND TO HAVE FAILED. REMOVED AND REPLACED START/GENERATOR WITH OVERHAULED UNITS. SYSTEM OPS CHECK COMPLETED WITH NO FURTHER DEFECTS. 2L72 4T RTA24CE 19960126002791996012600279NE 1996 1 26 96ZZZX326 219951205A73145009986B HP FUEL PUMP LUCAS 31170952 DORNERDO32 DO328100 2996000NM PWA 119 PW119B NE RT ENGINE CONTAMINATED A VNAAA UNSCHED LANDING J WARNING INDICATION NRNOT REPORTED 1 GL07433JS 2801 3047 PHL/CVG - FLT 4010 - EN ROUTE, APPROXIMATELY 80 MILES EAST OF CVG, FLIGHT CREW WAS ALERTED BY A FUEL FILTER BYPASS CAS MESSAGE. CREW WAS ADVISED TO DIVERT TO DAY. AIRCRAFT LANDED IN DAY WITHOUT FURTHER INCIDENT. DAY MAINTENANCE INSPECTED THE RT ENGINE HP FUEL PUMP FILTER AND FOUND IT WAS CONTAMINATED. DAY MAINTENANCE REMOVED AND REPLACED HP FUEL PUMP FILTER AND FOUND IT WAS CONTAMINATED. DAY MAINTENANCE REMOVED AND REPLACED RT ENGINE HP FUEL PUMP IAW MM 73-11-03. GROUND RUNS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T4 TRTA45NM E20NE 19960126002801996012600280NM 1996 1 26 96ZZZX327 119950928A55406549837503 FITTING BOEING737 737284 138448RNM RUDDER CRACKED B IX3RK NONE O OTHER ININSP/MAINT 1 WP07310VA 21501 ON AM OF SEPTEMBER 28, 1995, MX REPORT OF RUDDER ATTACH POINT WEB ASSY BEING CRACKED UPON INSPECTION FOR RUDDER INSTALLATION. (RUDDER ATTACH POINT NR 2). UPON FURTHER INVESTIGATION, FOUND MX PROCEDURES FOR REMOVAL OF RUDDER WERE NOT STRICTLY ADHERED TO. THE REMOVAL CALLS FOR THE LOCK-OUT OF THE MANUAL OVERRIDE LEVER ON THE STANDBY AND HYDRAULIC MODULAR PACKAGES IN THE OFF POSITION, AND THE DISCONNECTION OF ELECTRICAL CONNECTORS FROM FLIGHT CONTROLS A AND B SHUT-OFF VALVES. AIRCRAFT TOTAL TIME, 37,835.5 HOURS. TOTAL CYCLES, 52,921. 2L72 4F A16WE 19960126002811996012600281NE 1996 1 26 96ZZZX328 219951212A7250 TURBINE BLADE DOUG DC9 DC932 3022066WP PWA JT8 JT8D9A 52048NE NR 2 ENGINE FAILED A AVJ6AEA ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO11930VV 47723 667136 DFW/DFW - FLT 224 - ON CLIMB-OUT AT APPROXIMATELY 5,000 FEET, THE CREW HEARD A LOUD BANG, MODERATE VIBRATION WAS FELT AND N1 READING DROPPED TO APPROXIMATELY 60 PERCENT. CREW SHUT DOWN NR 2 ENGINE. SUBSEQUENT TO ENGINE REMOVAL, ENGINE WAS BORESCOPED TO DETERMINE THE CAUSE OF FAILURE AND EXTENT OF DAMAGE. BORESCOPE FINDINGS REVEALED 1ST STAGE TURBINE BLADE FAILURE WITH RESULTANT LPT TURBINE BLADE AND VANE DAMAGE (FAILURE WAS CONTAINED). BORESCOPE FINDING OF THE HPC 6TH STAGE AND HPC 7TH AND 13TH STAGES WERE NORMAL. ENGINE CHANGE IN PROCESS. 2L72 4F4 F A6WE E2EA 19960126002821996012600282NE 1996 1 26 96ZZZX329 119951129A7931 OIL PRESS TRANS SKRSKYS76 S76 8143010NE NR 1 ENGINE MALFUNCTIONED A AMPAE ENGINE SHUTDOWN N FALSE WARNING CRCRUISE 1 WP0983T 760117 WHILE INFLIGHT, THE PILOT OBSERVED THAT THE NO 1 ENGINE OIL PRESSURE DECREASED INTO THE YELLOW PRECAUTIONARY RANGE. THE NO 1 ENGINE WAS SHUT DOWN AS A PRECAUTION TO PREVENT POSSIBLE ENGINE DAMAGE. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. NO DAMAGE OR INJURY. MAINTENANCE PERSONNEL PERFORMED MAINTENANCE ON THE AIRCRAFT OIL SYSTEM AND FOUND A DEFECTIVE OIL PRESSURE TRANSMITTER. REPLACED SAME. AIRCRAFT WAS OPERATIONAL CHECKED AND LEAK CHECKED AND FOUND TO BE ACCEPTABLE. 1G72 3U H1NE 19960126002831996012600283EU 1996 1 26 96ZZZX330 119951210A32605EN16N95 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG STICKING A ECAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA11223JL 764 FRG - AFTER TAKEOFF DURING CLIMB-OUT WHEN LANDING GEAR RETRACTED, NOSE WHEEL LIGHT REMAINED ON (DOWN AND LOCKED). PILOT CYCLED GEAR DOWN AND RETURNED TO FRG. MADE UNEVENTFUL LANDING. RETURNED AIRCRAFT TO MAINTENANCE FACILITY. JACKED AIRCRAFT. CYCLED LANDING GEAR UP. NOSE DOWN AND LOCKED LIGHT REMAINED ILLUMINATED WITH GEAR UP AND LOCKED. LIGHT EXTINGUISHED SELF AFTER 20 SECONDS. CLEANED AND LUBRICATED SWITCH PLUNGER. CYCLED GEAR FIVE TIMES. ALL INDICATIONS WERE NORMAL, OPS CHECKED OK. REMOVED AIRCRAFT FROM JACKS. 2L72 4T RTA21EU 19960126002841996012600284NE 1996 1 26 96ZZZX331 219951108A8520 ROD BEARING CVAC 240 24013 2422626WP PWA R2800 CA3 52026NE NR 2 ENGINE FAILED A TFAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SO1591237 1062 140 P32011 NR 2 ENGINE HAD INCREASING OIL TEMPERATURE AND DECREASING OIL PRESSURE. THIS STABILIZED, BUT OIL QUANTITY CONTINUED TO DECREASE AND SMOKE WAS OBSERVED COMING OUT OF THE OUTBOARD AUGMENTOR TUBE. ENGINE SHUT DOWN AND SECURED, AND RETURNED TO SDQ. FOUND MASTER ROD BEARING FAILURE. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2L72 4R4 R A793 E231 19960126002851996012600285CE 1996 1 26 96ZZZX332 119951121A2910 B-NUT LEAR 35 36A 5170603CE LT MLG ACTUATOR LOOSE A NADAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NE0570UP 040 BTV/PWA - FLT 1121 - CHARTER FLIGHT FAR 135. AIRCRAFT DEVELOPED A TOTAL LOSS OF HYDRAULIC PRESSURE AND FLUID QUANTITY. AIRCRAFT DIVERTED TO FWA AND PRIORITY HANDLING WAS REQUESTED. AN UNEVENTFUL LANDING WAS MADE FOLLOWING EMERGENCY GEAR EXTENSION. C/A FOUND LINE, PN 2307006131, B-NUT LOOSE ON LT MLG ACTUATOR RETRACT PORT. TIGHTENED. CHECKED HYDRAULIC FILTERS, SERVICED HYDRAULIC SYSTEM. SERVICED EMERGENCY AIR SYSTEM. OPS AND LEAK CHECKED OK. 2L72 4F A10CE 19960126002861996012600286SO 1996 1 26 96ZZZX333 119951021A2910HP985100S11 SHUTOFF VALVE GULSTMG1159 G1159 3953505SO AFT EQUIP BAY LEAKING APACOZAO OTHER K FLUID LOSS ININSP/MAINT 1 WP27400CC10884 102 SCHEDULED MAINTENANCE CHECKS WERE BEING CONDUCTED THAT REQUIRED OPERATION OF THE UTILITY HYDRAULIC PUMP. A HEAVY SKYDROL MIST WAS NOTED COMING FROM THE AFT EQUIPMENT BAY. INSPECTION FOUND THE UTILITY HYDRAULIC PUMP SHUT-OFF VALVE HAD RUPTURED AND WAS SPRAYING FLIGHT HYDRAULIC FLUID FROM AN AREA THAT HAD BEEN STAMPED BY THE MANUFACTURER. SHUT-OFF VALVE MANUFACTURED BY HYDRA-POWER, MANUFACTURE PN HP985100S1-1, GAC PN 1159SCH217-1, SN 1127. 2L72 4F RTA12EA 19960126002881996012600288NM 1996 1 26 96ZZZX335 119951223A32302240500003 UPLOCK ROLLERS DORNERDO32 DO328100 2996000NM MLG DIRTY A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07328JS 3030 FLT 4014 - AFTER TAKEOFF WHILE RETRACTING LANDING GEAR, RIGHT MLG INTRANSIT LIGHT WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO FIELD, AND LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED BOTH RIGHT AND LEFT MLG WHEELWELLS AND DISCOVERED GEAR UPLOCK ROLLERS WERE CONTAMINATED WITH SLUSH AND SAND. CLEANED AND LUBRICATED UPLOCK ROLLERS IAW MM 32-10-00, AND STANDARD MAINTENANCE PRACTICES. GEAR SWING CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960126002891996012600289NM 1996 1 26 96ZZZX336 119951230A32402610799 BRK TEMP SENSOR DORNERDO32 DO328100 2996000NM MLG BRAKES DEFECTIVE A VNAAA UNSCHED LANDING N FALSE WARNING NRNOT REPORTED 1 GL07433JS 00485 3047 FLT 4166 - CREW REPORTED A BRAKE OVER TEMP IN-FLIGHT. CREW ADVISED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED LT BRAKE TEMPERATURE SENSOR IAW MM 32-42-09. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960126002901996012600290NM 1996 1 26 96ZZZX337 119951228A32302240500003 ROLLER MESSIER DORNERDO32 DO328100 2996000NM MLG LACK OF LUBE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07429JS 3043 FLT 4014 - AFTER TAKEOFF, RIGHT MAIN LANDING INTRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED LANDING GEAR SEVERAL TIMES IN AN ATTEMPT TO EXTINGUISH THE INTRANSIT LIGHT, WITHOUT SUCCESS. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE LUBRICATED MAIN LANDING UPLOCK ROLLERS IAW MM 32-10-00, AND STANDARD MAINTENANCE PRACTICES. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960126002911996012600291 1996 1 26 96ZZZX338 419951214A3418693733921 STALL WARN PNL BOEING737 737277 1384570NM COCKPIT FAILED A AWXAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 WP28180AW 22647 LAS - FLT 0131 - AIR TURNBACK; STICK SHAKER ACTIVATED AT ROTATION (139K) AND CONTINUED THROUGH 240K, THEN OFF. ON AGAIN AT 280K, THEN INTERMITTENT. ON RETURN TO LAS, STALL WARNING SWITCH WOULD SOMETIMES STOP SHAKER. REMOVED AND REPLACED LT ANGLE OF ATTACK SENSOR. ALL FLAP SETTINGS WITHIN TOLERANCE, SYSTEM TESTS NORMAL. REMOVED AND REPLACED P5-18 STALL WARNING PANEL. STALL WARNING TESTED GOOD. REFERENCE CONTROL NR AWXA9500815. 2L72 4F RTA16WE 19960126002921996012600292NM 1996 1 26 96ZZZX339 119951216A3244314392 TIRE BOEING737 7373G7 1384595NM NR 4 FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28160AW 14771477 23782 IND/LAS - FLT 0146 - AIR TURNBACK; RIGHT MAIN TIRE BLOWN AFTER ROTATION. MLG WOULD NOT RETRACT. CREW DECLARED EMERGENCY AND RETURNED TO IND, LANDING WITHOUT INCIDENT. UPON LANDING, CREW FOUND TIRE BLOWN. REMOVED AND REPLACED NR 3 AND NR 4 TIRES. REMOVED AND REPLACED AFT T/E RT FLAP, 65C26311-927A, SN 1485. AIRCRAFT RETURNED TO SERVICE. REFERENCE OPERATOR CONTROL NR AWXA9500817. 2L72 4F RTA16WE 19960126002951996012600295WP 1996 1 26 96ZZZX342 119951222A3230 RETRACT MECH 59104475041 DOUG DC9 DC951 3022051WP NLG VIBRATION A A4JAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 SO15920PJ 47677 UPON GEAR RETRACTION A VIBRATION STARTED. GEAR WAS EXTENDED AND VIBRATION CONTINUED. ALL GEAR INDICATIONS NORMAL EXCEPT VIBRATION - AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. 2L72 4F A6WE 19960126002961996012600296NM 1996 1 26 96ZZZX343 119951226A335088320031 BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROWS 12 THROUGH 14. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR ASAA9510117, AND NR 96ZZZX344. 2L72 4F RTA16WE 19960126002971996012600297NM 1996 1 26 96ZZZX344 119951226A33508821004 BATTERY PACK BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROWS 12 THROUGH 14. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. REFERENCE OPERATOR CONTROL NR ASAA9510117, AND NR 96ZZZX343. 2L72 4F RTA16WE 19960126002981996012600298NM 1996 1 26 ASAA9510117 119951225A3350RPS1B BATTERY PACK BOEING737 7372X6C 1384552NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ON THE NR 1 PALLET WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19960126002991996012600299NM 1996 1 26 ASAA9540112 119951228A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01782AS 25113 SNA - FLT 489 - CREW REPORTED THE AFT 6 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RESECURED LOOSE CONNECTION AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA16WE 19960126003001996012600300WP 1996 1 26 ASAA9580286 119951202A3350S103 BATTERIES DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01977AS 53453 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 30 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND LIGHTS OPERATED NORMALLY. (X) 2L72 4F RTA6WE 19960126003011996012600301WP 1996 1 26 ASAA9580295 119951222A33504TL1110B SWITCH DOUG DC9 DC982 3022082WP COCKPIT DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01930AS 49231 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS' SWITCH IN COCKPIT FOUND INOPERATIVE. REPLACED THE SWITCH AND OPERATED NORMALLY. (X) 2L72 4F A6WE 19960126003021996012600302NE 1996 1 26 AWXA9500814 219951213A72309527M99P09 FAN BLADES BOEING737 7373S3 1384711NM GE CFM56 CFM563B1 13802NE ENGINES 1/2 CURLED A AAWXAO OTHER C F.O.D. CRCRUISE 1 WP28314AW 23733 SMF-PHX - FLT NR 555 - CREW REPORTED, ICE INGESTED INTO BOTH ENGINES AT CRUISE, 19,000 FEET. CONTRACT MX REPORTED NR 1 ENGINE WITH 8 FAN BLADES CURLED 2 TO 3 INCHES IN LENGTH WITH MID-ACOUSTIC PANELS DAMAGED MESH APPROX 80 PERCENT WITH DEEP GOUGES. NR 2 ENGINE HAD 13 FAN BLADES CURLED 2 TO 3 INCHES AND SEVERAL BLADES WITH MINOR DAMAGE. MID-ACOUSTICS PANELS MINOR DAMAGE APPROX 75 PERCENT. CONTRACT MX PERFORMED AVM INTERROGATION AND FAXED RESULTS. MAINTENANCE TECHNICIANS SENT OUT TO REPLACE FAN BLADES AND ACOUSTIC PANELS PER POWERPLANT ENGINEERING. BORESCOPED BOTH NR 1 AND NR 2 ENGINES, BOOSTER AND HPC. NO DEFECTS NOTED. COMPLIED MPA RUNS ON BOTH ENGINES AND TRIM BALANCE. (M) 2L72 4F4 FRTA16WE E2GL 19960126003031996012600303 1996 1 26 AWXA9500815 419951214A3418BCREFX087 AOA SENSOR BOEING737 737277 1384570NM STALL WARN SYST FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28180AW 254 22647 LAS - FLT 131 - AIR-TURN-BACK, STICK SHAKER ACTIVATED AT ROTATION (139K) AND CONTINUED THROUGH 240K, THEN OFF. ON AGAIN AT 280K, THEN INTERMITTENT. ON RETURN TO LAS, STALL WARNING SWITCH WOULD SOMETIMES STOP SHAKER. REMOVED AND REPLACED LEFT ANGLE OF ATTACK SENSOR. ALL FLAP SETTINGS WITHIN TOLERANCE, SYSTEM TESTS NORMAL. REMOVED AND REPLACED P5-18 STALL WARNING PANEL. STALL WARNING TESTED GOOD. (M) 2L72 4F RTA16WE 19960126003041996012600304 1996 1 26 AWXA9500816 419951213A3441HG1050AD04 IRU BOEING737 7373G7 1384595NM NR 1 FAILED A AWXAA UNSCHED LANDING O OTHER UKUNKNOWN 1 WP28309AW 2434 24711 PHX/SFO - FLT 0602 - AIR TURN BACK. INERTIAL REFERENCE UNIT (I.R.U.) DATA LOST ON BOTH CAPTAIN AND FIRST OFFICER'S SIDES. REPLACED NR 1 I.R.U. PER MM 34-28-01 AND TESTED BOTH I.R.U.'S PER MM 34-28-01, PAGE 501. NO FAULTS NOTED. (X) 2L72 4F RTA16WE 19960126003051996012600305NM 1996 1 26 AWXA9500817 119951216A3244314392 TIRES BOEING737 7373G7 1384595NM NR 3 FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28160AW 14371437 23782 IND-LAS - FLT NR 146 - AIR-TURN-BACK, RIGHT MAIN TIRE BLOWN AFTER ROTATION. MLG WOULD NOT RETRACT. CREW DECLARED EMERGENCY AND RETURNED TO IND, LANDING WITHOUT INCIDENT. UPON LANDING, CREW FOUND TIRE BLOWN. REMOVED AND REPLACED NR 3 AND NR 4 TIRES. REMOVED AND REPLACED AFT TE RIGHT FLAP. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960126003061996012600306NM 1996 1 26 AWXA9500819 119951220A3397 WIRE BOEING757 7572G7 1384963NM CABIN DISCONNECTED A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28909AW 24522 PHX - FLT 0020 - DURING ROUTINE MAINTENANCE CHECK, FOUND RT OVERHEAD EMERGENCY LIGHTS INOP AT R2 AND R3 DOORS. RESECURED CONNECTOR ON POWER SUPPLY AT 23 D, E, F, OVERHEAD. SYSTEM OPS CHECK NORMAL. STC SA3432NM. (X) 2L72 4F RTA2NM 19960126003071996012600307NM 1996 1 26 AWXA9500830 119951228A5315 FLOOR BEAM BOEING757 757225 1384959NM BS 1640 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28913AW 22207 PAE - FLT 3872 - DURING SCHEDULED C-CHECK INSPECTION, FOUND CORROSION ON FLOOR BEAM BS 1640, LBL 4 - RBL 14, LBL 52 - LBL 56, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED 1640 FLOOR BEAM PER E.W.O. NR 95-4075, SRM 53-00-51. MRR NR 951181. (X) 2L72 4F RTA2NM 19960126003091996012600309 1996 1 26 BUFA9527 419951215A3421 CONNECTOR DOUG DC8 DC861 3021952WP RT COCKPIT LOOSE A BUFAK NONE L NO TEST ININSP/MAINT 1 CE05161DB 45980 FLT MIA/CAE (MIA/MIA) - F/O ART. HORIZ FAILED. TEST CAUSES NO REACTION EXCEPT RANDOM ATTITUDES. FOUND LOOSE CANNON PLUG AND RESET BREAKER, TIGHTEN CANNON PLUG. OPS CHK NORMAL IAW MM 34-23-0. (X) 2L74 4F 4A25 19960126003101996012600310WP 1996 1 26 CAL951111 119951110A5311995823879 BELT FRAME DOUG DC9 DC932 3022066WP BS 1109 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A .75 INCH CRACK IN BELT FRAME AT STA 1109, LONGERON 1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-11-4, FIGURE 4. (X) 2L72 4F A6WE 19960126003111996012600311WP 1996 1 26 CAL951112 119951110A5313 LONGERON DOUG DC9 DC932 3022066WP BS 1076 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A 1.25 INCH CRACK AT FORWARD END OF LONGERON 13R. A NEW SPLICE AND LONGERON WAS INSTALLED IAW SRM 51-10-3. (X) 2L72 4F A6WE 19960126003121996012600312WP 1996 1 26 CAL951113 119951114A5312 BLKHD STIFFENER DOUG DC9 DC932 3022066WP FWD BULKHEAD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A 1 INCH CRACK ON FORWARD BULKHEAD VERTICAL STIFFENER. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 4. (X) 2L72 4F A6WE 19960126003131996012600313WP 1996 1 26 CAL951114 119951116A5313 LONGERON DOUG DC9 DC932 3022066WP BS 980 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 17 AT RIGHT AFT LAV, STA 980. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2A, SRM 51-30-2, AND SRM 51-30-5. (X) 2L72 4F A6WE 19960126003141996012600314WP 1996 1 26 CAL951115 119951114A5330 SKIN DOUG DC9 DC932 3022066WP FUSELAGE CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB UPPER FORWARD CORNER AND A .25 INCH CRACK AT THE LOWER AFT CORNER. DOUBLER REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 38. (X) 2L72 4F A6WE 19960126003151996012600315WP 1996 1 26 CAL951116 119951114A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 617 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A 1 INCH CRACK IN RIGHT SIDE FLOOR BEAM WEB AT STA 617. THE END OF WEB WAS CUT OFF AND A NEW WEB WAS SPLICED IAW SRM 53-01, FIGURE 4. (X) 2L72 4F A6WE 19960126003161996012600316WP 1996 1 26 CAL951117 119951112A5320 ANGLE DOUG DC9 DC932 3022066WP BS 160-200 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT STA 160 - STA 200. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. (X) 2L72 4F A6WE 19960126003171996012600317WP 1996 1 26 CAL951118 119951114A531327779223 LONGERON DOUG DC9 DC932 3022066WP BS 965 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A .50 INCH CRACK IN LONGERON 14L AT STA 965 BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 2. (X) 2L72 4F A6WE 19960126003181996012600318WP 1996 1 26 CAL951119 119951114A5312 BLKHD ANGLE DOUG DC9 DC932 3022066WP AFT PRESS BLKHD CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091753366763 47281 HOU - INSPECTION FOUND A .50 INCH CRACK IN OUTBOARD AFT PRESSURE BULKHEAD FORMER ATTACH ANGLE AT TEE CAP. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (X) 2L72 4F A6WE 19960126003191996012600319WP 1996 1 26 CKSA95144 119951208A2120 AIR DISTRIBUTOR DOUG DC8 DC8F55 3021928WP COCKPIT ODOR A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23809CK64285 45803 KHUF - NOXIOUS SMELL IN COCKPIT, UNABLE TO LOCALIZE OR DETERMINE ORIGIN. SELECTIVELY ELIMINATED COCKPIT LIGHTING, TC'S AND AVIONICS WITH NO APPRECIABLE CHANGE. RAN ENGINES AND PRESSURIZED AIRCRAFT. ATTEMPTED NUMEROUS ELECTRICAL AND ENGINE BLEED CONFIGURATIONS. COULD NOT DUPLICATE SMELL IN COCKPIT. (X) 2L74 4F 4A25 19960126003201996012600320NM 1996 1 26 IXKA950034 119951212A326011010153 LOCK SWITCH BOEING727 727225 1384077NM NLG DEFECTIVE A IXKAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 EA25361KP S1020 20627 FLT 18 - UPON GEAR EXTENSION, NOSE GEAR GREEN LIGHT ILLUMINATED. RED NOSE GEAR LIGHT ALSO REMAINED ILLUMINATED. FOLLOWED AIRCRAFT MANUAL PROCEDURES AND RECEIVED VISUAL FROM TOWER. BOTH INDICATED DOWN AND LOCKED. REMOVED AND REPLACED NOSE LOCK SWITCH IAW 32-61-71. OPERATIONAL CHECK NORMAL. (X) 2L73 4F A3WE 19960126003231996012600323CE 1996 1 26 PLG103195G3 119951031A5270 WARNING LIGHT BEECH 1900 1900C 1154161CE CABIN DOOR ILLUMINATED A PLGAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 NE0576YV UC76 SYR - FLT 4372 - AFTER TAKEOFF, THE FORWARD CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO SYR LANDING WITHOUT INCIDENT. THE DOOR WARNING SYSTEM WAS MEL'D AND THE AIRCRAFT RETURNED TO SERVICE. THIS WAS THE LAST DAY OF SERVICE FOR THE AIRCRAFT. THE AIRCRAFT WAS RETURNED TO BEECH WITH THE DOOR WARNING SYSTEM DEFERRED. (X) 2L72 4T RTA24CE 19960126003241996012600324EU 1996 1 26 SIMA953401 119951206A33503012001 BATTERY PACK BARFIELD 3012000 AEROSPATR72 ATR72202 8680940EU AFT GALLEY DISCHARGED A SIMAK NONE L NO TEST ININSP/MAINT 1 SW21252AM 98 685 253 FA REPORT LAST 4 EMERGENCY FLOOR PROXIMITY LIGHTS STAYED ILLUMINATED WHEN POWER WAS SHUT OFF. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PACK, SYSTEM OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE. (X) 2H72 4T RTA53EU 19960126003271996012600327SO 1996 1 26 SRAA129502 119951208A61207143253 VALVE HOUSING HAMSTD 54H60117 LKHEED382 382E 526413USO NR 3 PROP INOPERATIVE A SRAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 SO19923SJ 237034 4301 DURING FLIGHT MAD08 TO MHZ, NR 3 ENGINE RPM DECAYED TO 97 PERCENT AND TORQUE WAS 5,000-10,000 INCHES/POUNDS AT FLIGHT IDLE (DEPENDING ON ALTITUDE), SHUT DOWN ENGINE AND LANDED SAFELY AT MHZ. REPLACED NR 3 ENGINE PROP VALVE HOUSING, PROP RIGGED AND PERFORMED ENGINE RUN-UP, OPS CHECKED GOOD PER MM CHAPTER 61. (X) 2H74 4T A1SO 19960126003281996012600328NM 1996 1 26 TWRA9567 119951204A575365B155542 FAIRING BOEING747 747121 1384871NM NR 5 FLAP TRACK MISSING A ATWRAK NONE D INFLIGHT SEPARATION LDLANDING 1 EA15617FF 19650 DURING APPROACH INTO MIA, NR 5 FLAP TRACK FAIRING SEPARATED FROM AIRCRAFT. UPON LANDING, INSPECTION FOUND FORWARD ATTACH HINGE BOLTS (2) MISSING. H-FITTING BROKEN, DRIVE ROD AND ATTACH FITTING BROKEN. ALSO, A 32 INCH CRACK IN THE AFT FLAP (BOTTOM T/E). THE CANOE AND H-FITTING WERE REPLACED, ALSO, DRIVE ROD AND ATTACH FITTING. AFT TRAILING EDGE OF AFT FLAP WAS REPAIRED. OPERATIONAL CHECK OF FLAPS WAS PERFORMED. AIRCRAFT RETURNED TO SERVICE 12-06-95. (X) 2L74 4F A20WE 19960126003881996012600388NM 1996 1 26 DL73E960114 119951020A3260 BULB BOEING737 737247 138448DNM NLG FAILED A DALAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 SO27376DL 23603 ON APPROACH TO ATL, LANDING GEAR EXTENDED, NOSE GEAR DID NOT HAVE GREEN LIGHT. CYCLED GEAR, NO CHANGE. ACCOMPLISHED MISSED APPROACH. REPLACED BOTH INDICATOR BULBS, LOWERED GEAR GOT GREEN LIGHT AND LANDED NORMALLY. 2L72 4F A16WE 19960126004101996012600410NE 1996 1 26 DLM88960131 219951227A731350043082 FUEL NOZZLE DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE LOOSE A ADALAK NONE O OTHER ININSP/MAINT 1 SO27992DL 53344 726031 ENGINE WAS REMOVED FOR 7TH STAGE COMPRESSOR BLADES DAMAGED BEYOND LIMITS. ENGINE WAS DISASSEMBLED IN ENGINE SHOP AND NR 3 FUEL NOZZLE WAS FOUND TO HAVE DAMAGE. FUEL NOZZLE SCOOP BECAME LOOSE, ROTATED AND CUT INTO FUEL NOZZLE SUPPORT CAUSING FUEL NOZZLE TO LEAK. FUEL NOZZLE SCOOP CAME OFF AND BECAME LODGED IN NR 2 BURNER CAN. FINDINGS HAVE BEEN REPORTED TO THE LOCAL PRATT AND WHITNEY OFFICE. 2L72 4F4 FRTA6WE E9NE 19960126004181996012600418WP 1996 1 26 UPS805275 119951227A5320 ANGLE DOUG DC8 DC873F 302199FWP LT VERT STAB CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01807UP 46007 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION CRK AT LT VERT STAB TO FUSELAGE ATTACH ANGLE. REPAIRED PER UPS EO. 2L74 4F RT4A25 19960126004551996012600455CE 1996 1 26 96ZZZX379 119951219A2750556517531 GEARBOX CESSNA500 500CESSNA 2076602CE FLAP FAILED A MDGAK NONE O OTHER ININSP/MAINT 1 SO0910UH 1650 A22385 5000304 FLAP GEARBOX HAS AN OVERHAUL TIME OF 3,000 HOURS. SUBMITTER RECOMMENDS 1,000-HOUR OVERHAUL BE REQUIRED. THIS UNIT FAILED AT 1,650 HOURS. 1L72 4F A22CE 19960126004821996012600482NM 1996 1 26 DL72E960064 119951128A5754651622199 RIB BOEING727 727247 138408FNM NR 4 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272829W 21481 DURING SHOP INSPECTION, NR 4 L/E SLAT WAS FOUND WITH RIB NR 12 CRACKED PAST PREVIOUS STOP DRILL. REPAIRED PER MM 57-54-00. 2L73 4F A3WE 19960126004871996012600487NM 1996 1 26 DL72S960175 119951121A575465162249092 RIB BOEING727 727232 1384082NM NR 8 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27406DA 21150 DURING INSPECTION, NR 8 LE SLAT WAS FOUND WITH INTERNAL RIB NR 3 AND NR 2 CRACKED. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19960126005661996012600566NE 1996 1 26 96ZZZM40 219951224A73143782017 SEAL BOEING727 727231 1384079NM PWA JT8 JT8D9 52048NE NR 1 FUEL PUMP FAILED A TWAAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0552313 19832 3962 JFK - DURING CRUISE, NR 1 ENGINE LOST OIL. ENGINE FUEL PUMP SEAL, TW 25052 MFG 378201-7, WAS WORN. REPLACED MFG A03128CHGA. LEAK CHECK OF FUEL PUMP GARLOCK SEAL WAS NORMAL. 2L73 4F4 F A3WE E2EA 19960126005671996012600567NM 1996 1 26 96ZZZM41 119951223A3232731414 ACTUATOR BOEING727 727231 1384079NM RT MLG DOOR FAILED A TWAAO OTHER J WARNING INDICATION LDLANDING 1 CE0552312 19831 STL - DURING LANDING, CREW RECEIVED AN UNSAFE GEAR INDICATION. REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR. TW P/N 10395 MFG 7-3141-4. PERFORMED GEAR SWING ALL THREE OPERATIONS CHECK NORMAL. 2L73 4F A3WE 19960126005681996012600568WP 1996 1 26 96ZZZM42 119951225A3810 WATER LINE DOUG DC9 DC982 3022082WP CARGO COMPT FAILED A TWAAE ENGINE SHUTDOWN K FLUID LOSS LDLANDING 1 CE05904TW 49156 FLT NR 167 - SFO - DURING LANDING, NR 2 ENGINE THROTTLE STUCK MID POSITION. ENGINE SHUT DOWN. APPARENT CAUSE OF TROUBLE, PORTABLE WATER SUPPLY LINE FROZE AND RUPTURED. REPAIRED WATER LINE IN CEILING OF AFT CARGO PIT. 2L72 4F A6WE 19960126005691996012600569WP 1996 1 26 96ZZZM43 119951225A2497 WIRE HARNESS DOUG DC9 DC932 3022066WP COCKPIT OUT OF POSITION A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05921L 47107 FLT NR 471 - STL - DURING CLIMB, MAIN LANDING GEAR HANDLE WOULD NOT TRAVEL BEYOND ONE-THIRD OF TRAVEL. SPOILERS WOULD NOT ARM FOR LANDING. FOUND WIRE BUNDLE BLOCKING GEAR CONTROL LEVER. REPOSITIONED TO CLEAR AND SECURED WIRE BUNDLE. GEAR SWING OPERATIONS NORMAL. 2L72 4F A6WE 19960126005701996012600570WP 1996 1 26 96ZZZM44 119951222A3222MS287787 SCHRADER VLV DOUG DC9 DC983 3022083WP NLG STRUT FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE059307R 49663 PHX - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. FOUND NOSE STRUT FLAT. REPLACED SCHRADER VALVE O-RING, MFG P/N MS28778-7, AND SERVICED STRUT WITH OIL AND AIR. EXTENDED NOSE STRUT TO FULL EXTENSION AND BACK DOWN WITH NO FINDING. NOSE LANDING GEAR CHECKS NORMAL. 2L72 4F RTA6WE 19960126005711996012600571WP 1996 1 26 96ZZZM45 119951223A2913314195 HYD PUMP DOUG DC9 DC982 3022082WP RT ENGINE MALFUNCTIONED A TWAAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE05916TW 49187 JFK - FLT NR 881 - DURING TAKEOFF, EXPERIENCED LOSS OF HYDRAULIC FLUID. RETURNED FOR LANDING. REMOVED AND REPLACED RIGHT AUX AND RIGHT ENGINE DRIVEN PUMPS AND FILTERS. TW 92190 MFG 428177 S/N 407390 AND TW 800877 MFG 314195 S/N 388244 RESPECTIVELY. PRESSURIZE AND LEAK CHECK. NO LEAKS. 2L72 4F A6WE 19960126005721996012600572WP 1996 1 26 96ZZZM46 119951223A3222 STRUT SEALS DOUG DC9 DC982 3022082WP NLG FAILED A TWAAO OTHER J WARNING INDICATION LDLANDING 1 CE05914TW 49185 TPA - DURING LANDING, UNABLE TO LOWER NOSE GEAR. CYCLED LANDING GEAR. NOSE STRUT SEALS REPLACED, REPACKED NOSE STRUT. CYCLED GEAR AND OPERATIONS ARE NORMAL. 2L72 4F A6WE 19960126005731996012600573WP 1996 1 26 96ZZZM47 119951223A21216054577 FAN DOUG DC9 DC983 3022083WP CABIN FAILED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059303K 49529 STL - FLT NR 202 - DURING CRUISE, THERE WAS AN ELECTRICAL SMELL COMING FROM THE RECIRCULATING FAN, P/N 605457-7 TWPN 12801. CIRCUIT BREAKER PULLED AND PLACARDED. DECEMBER 24, 1995, MSP REPLACED RECIRCULATION FAN. OPERATIONS CHECK NORMAL. 2L72 4F RTA6WE 19960126005741996012600574NE 1996 1 26 96ZZZM48 219951222A726029136 GEAR BOX LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122* 54555NE ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE057036T 193B1232 MIA - FLT 149 - DURING CRUISE, LOST OIL RESULTING IN AN ENGINE SHUTDOWN AND DETERMINED HIGH SPEED. MAIN GEAR BOX 29136, S/N 610200 FAILED. REMOVED AND INSTALLED NEW GEAR BOX. LEAK CHECK AND OPERATIONS NORMAL. 2L73 4F4 F A23WE A12EU 19960126005751996012600575NE 1996 1 26 96ZZZM49 219951221A7250 TURBINE BLADE DOUG DC9 DC951 3022051WP PWA JT8 JT8D9A 52048NE NR 1 ENG FAILED A TWAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 CE05409EA 47728 1702 IND - FLT NR 275 - DURING CLIMB, SHUT DOWN NR 1 ENGINE. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE. ENGINE OPERATION CHECKS NORMAL. INVESTIGATION OF METAL PARTICLES IN TAILPIPE AFTER SHUTDOWN OF NR 1 ENGINE, REVEALED THAT A FIRST STAGE TURBINE BLADE FAILED DUE TO FATIGUE CRACKS AT INNER RADIUS. REMOVED AND REPLACED FAILED TURBINE BLADE. ALL SUBSEQUENT DAMAGE WAS ALSO REPAIRED. ENGINE RETURNED TO SERVICE. (M) 2L72 4F4 F A6WE E2EA 19960126005761996012600576NE 1996 1 26 96ZZZM50 219951221A7261 OIL CAP DOUG DC9 DC951 3022051WP PWA JT8 JT8D9A 52048NE NR 2 ENGINE MISSING A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE05409EA 47728 STL - DURING CRUISE, SHUTDOWN NR 2 ENGINE, S/N 1526, DUE TO DECREASING OIL PRESSURE AND OIL QUANTITY. FOUND OIL CAP MISSING, REPLACED OIL CAP, INSPECTED OIL SCREEN, SERVICED OIL, RAN AND LEAK CHECKED ENGINE. OPERATIONS CHECKED NORMAL. (M) 2L72 4F4 F A6WE E2EA 19960126005771996012600577WP 1996 1 26 96ZZZM51 119951228A3230 CONTROL VLV DOUG DC9 DC951 3022051WP LANDING GEAR LACK OF LUBE A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05416EA 47751 OKC - FLT NR 265 - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR VALVE. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19960126005781996012600578WP 1996 1 26 96ZZZM52 119951128A3820 WATER HEATER LKHEED1011 10113851 5265010WP AFT LAV SMOKING A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CE0531013 193B1035 MCO - FLT NR 265 - DURING DESCENT, SMOKE WAS DETECTED IN AFT LAVATORIES. LAVATORY CIRCUIT BREAKERS WERE PULLED, SMOKE IMMEDIATELY CEASED AND DISSIPATED. THE LAVATORY WATER HEATERS WERE FOUND WITH NO WATER IN THEM. HEATERS WERE PURGED AND OPERATIONIONALLY CHECKED. OPERATIONAL CHECK NORMAL. 2L73 4F A23WE 19960126005791996012600579WP 1996 1 26 96ZZZM53 119951129A2781 LOCK OUT LIGHT LKHEED1011 1011385115 5265015WP LE SLAT ILLUMINATED A TWAAO OTHER N FALSE WARNING DEDESCENT 1 CE0531029 193B1109 FLT NR 741 - SEA - DURING DESCENT, THE LEADING EDGE FLAP/SLAT LOCKOUT LIGHT ILLUMINATED. RESET BOTH ASYMMETRICAL BRAKES, FLAP/SLAT OPERATION CHECKED NORMAL. 2L73 4F A23WE 19960126005801996012600580WP 1996 1 26 96ZZZM54 119951202A3350 BULB DOUG DC9 DC951 3022051WP CABIN FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE05410EA 47731 STL - FLT 124 - DURING LAYOVER, MAINTENANCE FOUND RIGHT AFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPERATIONAL CHECK NORMAL. 2L72 4F A6WE 19960126005811996012600581WP 1996 1 26 96ZZZM55 119951226A3222325315 SHRADER VLV DOUG DC9 DC951 3022051WP NLG STRUT FAILED A TWAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE05408EA 47693 JFK - FLT NR 227 - AFTER TAKEOFF, THE NOSE LANDING GEAR UNSAFE LIGHT CAME ON. RETURNED TO JFK. NOSE STRUT FLAT. CHANGED SHRADER VALVE, TWA 32-5315 MFG MS28778-7. SERVICED NOSE STRUT WITH HYDRAULIC FLUID AND DRY NITROGEN. LEAK CHECK OK. 2L72 4F A6WE 19960126005821996012600582NE 1996 1 26 96ZZZM56 219951204A7200 ENGINE DOUG DC9 DC983 3022083WP PWA JT8 JT8D217C 52053NE RIGHT BIRD STRIKE A TWAAA UNSCHED LANDING CB F.O.D. SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CE059409F 53121 FLT NR 312 - SMF - AFTER TAKEOFF, SMOKE EMITTED INTO CABIN. FLIGHT RETURNED. FOUND RIGHT ENGINE HAD INGESTED A BIRD. REPLACED RIGHT ENGINE, S/N 3256. ENGINE OPERATION AND AIR CONDITIONING SYSTEMS OPERATION CHECKED NORMAL. 2L72 4F4 FRTA6WE E9NE 19960126005831996012600583NM 1996 1 26 96ZZZM57 119951213A2410705117E CSD BOEING747 747131 1384881NM NR 2 ENGINE FAILED A TWAAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CE0593104 19670 STL - FLT NR 2 - DURING CRUISE, NR 2 ENGINE CSD FAILED. NR 2 CSD WOULD NOT DISCONNECT. SHUT DOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE CSD, MFG P/N 705117E, AND REPAIRED CSD SOLENOID GROUND WIRE. OPERATIONAL CHECK NORMAL. 2L74 4F A20WE 19960126005841996012600584NM 1996 1 26 96ZZZM58 119951213A2410705117E CSD BOEING747 747284B 1384862NM NR 2 ENGINE FAILED A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE05305TW 20742 FCO - DURING CRUISE, SHUT DOWN NR 2 ENGINE, S/N 4181, DUE TO DECREASING OIL QUANTITY. FOUND OIL LEAKING FROM INTEGRATED DRIVE GENERATOR DRIVE CAVITY DRAIN. CAPPED DRAIN LINE. ENGINE LEAK CHECK WAS NORMAL. 2L74 4F RTA20WE 19960126005851996012600585NM 1996 1 26 96ZZZM59 119951208A5315 FLOOR BEAM BOEING727 72731 1384010NM FWD BAG BIN CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 FORWARD CARGO COMPARTMENT FLOOR BEAM LOWER CHORD HAS CORROSION, BTW BL-0 AND RBL 34. CUT OUT AFFECTED AREA FABRICATED REPAIR PARTS PER 53-10-8, INSTALLED REPAIR PARTS PER SRM 51-10-2. (M) 2L73 4F A3WE 19960126005861996012600586EU 1996 1 26 96ZZZM60 119951114A2730S2738196320000 TQ TUBE FLANGE AEROSPATR72 ATR72211 EU ELEVATOR CRACKED APTTRBAK NONE O OTHER ININSP/MAINT 1 SO212FOR 12527 147 TORQUE TUBE FLANGE FOUND CRACKED DURING INSPECTION AFTER PILOT REPORT. PART REPLACED WITH NEW ASSEMBLY. 2H72 4T RTA53EU 19960126005871996012600587NM 1996 1 26 96ZZZM61 119951126A535065B0672335 FAIRING BOEING747 747124 1384874NM LT WING/FUS MISSING A ATWRAK NONE D INFLIGHT SEPARATION CRCRUISE 1 EA15602FF 19734 DURING CRUISE APPROXIMATELY 160NM W OF HUNTER AFB, A LOUD THUMP WAS FELT AND HEARD. UPON LANDING, MAINTENANCE FOUND LARGE PIECE OF FUSELAGE FAIRING MISSING ON LEFT SIDE BELOW NR 3 MED. AIRCRAFT WAS INSPECTED AND FOUND OK FOR FERRY FLIGHT TO JFK. FUSELAGE FAIRING WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE NOV 31, 1995. REFERENCE NR TWRA9565. 2L74 4F A20WE 19960126005881996012600588NM 1996 1 26 96ZZZM62 119951204A21503964421 FLOW VALVE BOEING737 7373G7 1384595NM LT PACK MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28302AW 914 24009 LAS/BUR - PRESSURIZATION WAS INADEQUATE DURING INITIAL CLIMB. FLIGHT WAS ABORTED. AIRCRAFT RETURNED TO LAS LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PACK FLOW CONTROL VALVE AND THE LEFT AIR CYCLE MACHINE PER BMM CHAPTER 21. BOTH OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REFERENCE AWXA9500795. 2L72 4F RTA16WE 19960126005891996012600589NM 1996 1 26 96ZZZM63 119951216A3244314392 TIRES BOEING737 7373G7 1384595NM NR 3 FAILED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28160AW 14371477 23782 IND-LAS - FLT NR 146 - AIR-TURN-BACK, RIGHT MAIN TIRE BLOWN AFTER ROTATION. MLG WOULD NOT RETRACT. CREW DECLARED EMERGENCY AND RETURNED TO IND, LANDING WITHOUT INCIDENT. UPON LANDING, CREW FOUND TIRE BLOWN. REMOVED AND REPLACED NR 3 AND NR 4 TIRES. REMOVED AND REPLACED AFT TE RIGHT FLAP. AIRCRAFT RETURNED TO SERVICE. REFERENCE NR AWXA9500817. 2L72 4F RTA16WE 19960126005901996012600590 1996 1 26 96ZZZM64 419951214A3418693733921 STALL WARN PNL BOEING737 737277 1384570NM STALL WARN SYST FAILED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28180AW 22647 LAS - FLT 131 - AIR-TURN-BACK, STICK SHAKER ACTIVATED AT ROTATION (139K) AND CONTINUED THROUGH 240K, THEN OFF. ON AGAIN AT 280K, THEN INTERMITTENT. ON RETURN TO LAS, STALL WARNING SWITCH WOULD SOMETIMES STOP SHAKER. REMOVED AND REPLACED LEFT ANGLE OF ATTACK SENSOR. ALL FLAP SETTINGS WITHIN TOLERANCE, SYSTEM TESTS NORMAL. REMOVED AND REPLACED P5-18 STALL WARNING PANEL. STALL WARNING TESTED GOOD. REFERENCE AWXA9500815. 2L72 4F RTA16WE 19960126005911996012600591 1996 1 26 96ZZZM65 419951211A3454127865001 SWITCH UNIT DOUG DC9 DC932 3022066WP NAV SYSTEM FAILED A VJ6AA UNSCHED LANDING O OTHER CLCLIMB 1 SO11930VV 47723 FLT NR 444 - ATL- AIR RETURN - ON TAKEOFF BOTH NAV SYSTEMS WERE INOP. NAV TRANSFER CIRCUIT BREAKER WOULD NOT RESET. REMOVED AND REPLACED NAV SWITCHING UNIT. OPS CHECK WITH T/C-30 IAW 34-10. (M) 2L72 4F A6WE 19960126005921996012600592WP 1996 1 26 96ZZZM66 119951214A2810 SCREWS DOUG DC9 DC932 3022066WP NR 3 PROBE STRIPPED A VJ6AA UNSCHED LANDING K FLUID LOSS CLCLIMB 1 SO11940VV 47523 FLT 496 - ATL - AIR RETURN - THE CREW REPORTED FUEL VENTING FROM THE RIGHT WING. MAINTENANCE FOUND 2 SCREWS ON NR 3 PROBE WOULD NOT TIGHTEN. REPLACED 2 NUT PLATES AND 2 SCREWS. LEAK CHECKED OK PER MM 28-15. (M) 2L72 4F A6WE 19960126005931996012600593WP 1996 1 26 96ZZZM67 119951210A2150 DUCTS DOUG DC9 DC932 3022066WP LT/RT PACKS BLOWN OFF A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11917VV 47323 FLT NR 515 - ATL - WHEN THE AIRCRAFT WAS PASSING THROUGH 17,000 FEET WHEN IT LOST CABIN PRESSURE AND WAS UNABLE TO CONTROL MANUALLY. AIR RETURN. FOUND LEFT AND RIGHT PACK DUCTS BLOWN OFF AT WATER SEPARATORS, REINSTALLED LEFT AND RIGHT DUCTS AND REPLACED LEFT COALESTER BAG. PRESSURIZED AIRCRAFT OPS CHECKED GOOD. (M) 2L72 4F A6WE 19960126005941996012600594WP 1996 1 26 96ZZZM68 119951124A5242 DDOR DOUG DC9 DC932 3022066WP E/E COMPT NOT LATCHED A VJ6AA UNSCHED LANDING P NO WARNING INDICATION CLCLIMB 1 SO11930VV 47723 FLT NR 580 - ATL - AIRCRAFT RETURNED, WAS UNABLE TO PRESSURIZE AFTER TAKEOFF. NO DOOR LIGHTS ON AIRCRAFT. AIRCRAFT RETURNED TO GATE FOUND E/E DOOR OPEN. FOUND DOOR LIGHT SWITCH INOP. DEFERRED DOOR SWITCH FOR REPAIR, CLOSED DOOR DISPATCHED AIRCRAFT. CONTROL NR DM05712, SEQ 33-17. (M) 2L72 4F A6WE 19960126005951996012600595WP 1996 1 26 96ZZZM69 119951107A2150 CLAMPS DOUG DC9 DC932 3022066WP LT PACK LOOSE A VJ6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO11933VV 47489 FLT NR 278 - ATL-CMH - THE AIRCRAFT EXPERIENCED A TAIL COMPARTMENT HIGH TEMP INDICATION, THE FLIGHT DIVERTED TO CHA. FOUND SEVERAL LOOSE CLAMPS ON LEFT PACK AND FLOW CONTROL VALVE TIGHTENED SAME. RAN TO 1.9 EPR, NO LEAKS NOTED. (M) 2L72 4F A6WE 19960126005961996012600596WP 1996 1 26 96ZZZM70 119951218A3260H146 DOOR SWITCH DOUG DC9 DC932 3022066WP LT MLG DOOR FAILED A VJ6AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO11909VJ 47322 FLT NR 231 - ATL - AIRCRAFT RETURNED AFTER TAKEOFF AND GEAR RETRACTION LEFT GEAR DOOR OPEN LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LEFT LANDING GEAR DOOR SWITCH IAW MM 32-10, OPS CHECK GOOD. (M) 2L72 4F A6WE 19960126005971996012600597WP 1996 1 26 96ZZZM71 119951124A3260 CONNECTOR DOUG DC9 DC932 3022066WP LT MLG DOOR LOOSE A VJ6AO OTHER N FALSE WARNING APAPPROACH 1 SO11938VV 47442 FLT NR 229 - ATL-DFW - UPON GEAR EXTENSION LEFT MAIN GEAR DOOR UNSAFE LIGHT AND GREEN DOWNLOCK LIGHTS WERE INTERMITTENT. FOUND CANNON PLUG ON LEFT DOWN LOCK SWITCH LOOSE. SECURED CANNON PLUG AND SAFTIED IAW VALUJET MAINTENANCE MANUAL. (M) 2L72 4F A6WE 19960126005981996012600598EU 1996 1 26 96ZZZM72 119951221A21332647A000 OUTFLOW VALVE BAG JETSTMJETSTM3201 1500217EU CABIN DIRTY A VTZAGH O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 EA27494UE 810 FLT NR 6586 - IAD-ISP - DURING CRUISE, DECLARED AN EMERGENCY AND LANDED AT ISP DUE TO THE PRESSURIZATION DUMPING AT 15,000 FT, THE 'CABIN' CAPTION ILLUMINATED, AND THE CABIN OXYGEN MASKS DEPLOYED. THE A/C LANDED AT ISP WITH NO FURTHER INCIDENT. HOWEVER, THE OXYGEN SYSTEM WAS READING 0. MX OPENED DMI NR 42402 IAW MEL 21-14 ON THE PRESS SYSTEM, AND DMI NR 42403 IAW MEL 35-1 ON THE OXYGEN SYSTEM. MX LATER CLEARED DMI NR 42403 ON 12-22-95, BY CLEANING THE OUTFLOW VALVE AND ALSO SECURING LOOSE SENSE LINE. OPS CHECK GOOD. CLEARED DMI NR 42403 ON 12-22-95, BY REPLACING SEAT 3BC STOWAGE OXYGEN MASK AND STOWED REMAINING OXYGEN MASKS. OPS CHECK GOOD. A/C WAS RELEASED AND RETURNED TO SERV. REF VTZA96051. 2L72 4T RTA56EU 19960126005991996012600599EU 1996 1 26 96ZZZM73 119951221A21301370955L403 SENSE LINE BAG JETSTMJETSTM3201 1500217EU CABIN LOOSE A VTZAGH O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 EA27494UE 810 FLT NR 6586 - IAD-ISP - DURING CRUISE, DECLARED AN EMERGENCY AND LANDED AT ISP DUE TO THE PRESSURIZATION DUMPING AT 15,000 FT, THE 'CABIN' CAPTION ILLUMINATED, AND THE CABIN OXYGEN MASKS DEPLOYED. THE A/C LANDED AT ISP WITH NO FURTHER INCIDENT. HOWEVER, THE OXYGEN SYSTEM WAS READING 0. MX OPENED DMI NR 42402 IAW MEL 21-14 ON THE PRESS SYSTEM, AND DMI NR 42403 IAW MEL 35-1 ON THE OXYGEN SYSTEM. MX LATER CLEARED DMI NR 42403 ON 12-22-95, BY CLEANING THE OUTFLOW VALVE AND ALSO SECURING LOOSE SENSE LINE. OPS CHECK GOOD. CLEARED DMI RN 42403 ON 12-22-95, BY REPLACING SEAT 3BC STOWAGE OXYGEN MASK AND STOWED REMAINING OXYGEN MASKS. OPS CHECK GOOD. A/C WAS RELEASED AND RETURNED TO SERV. REF VTZA96051. 2L72 4T RTA56EU 19960126006001996012600600NM 1996 1 26 AALA951989 119951130A253046700011 COFFEE MAKER DOUG MD11 MD11 3023602NM B-C GALLEY DEFECTIVE A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW071764B 0580 48554 LHR - FLT NR 86 - EN ROUTE ORD/LHR DURING CRUISE, SPARKS NOTED COMING FROM TOP OF NR 4 COFFEE MAKER IN B-C GALLEY. AIRCRAFT PROCEEDED LHR AND LANDED WITHOUT INCIDENT. REPLACED NR 4 COFFEE MAKER IN B-C GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F RTA22WE 19960126006011996012600601EU 1996 1 26 AALA952066 119951210A3230 RETRACT MECH FOKKERF28 F28MK0100 4990807EU RT MAIN LACK OF LUBE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071451N 11460 ORD - FLT NR 81 - AFTER TAKEOFF, WHEN LANDING GEAR RETRACTED, RECEIVED MULTIPLE WARNING MESSAGES ON MFDU ASSOCIATED WITH GROUND/FLIGHT CONTROL AND PRESSURIZATION. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. PSEU BITE CHECK ACCOMPLISHED INDICATING RIGHT MAIN LANDING GEAR SENSOR FAULT. CHECKED SENSORS, TARGET AND RIGHT MAIN LANDING GEAR HARNESS WITH NO DEFECTS FOUND. SUSPECTED PROBLEM WAS WITH GEAR POSITION. LUBRICATED RIGHT MAIN LANDING GEAR GLAND NUT AND SCISSORS AND SERVICED STRUT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19960126006021996012600602NM 1996 1 26 AWXA9500788 119951127A5330 SKIN BOEING737 737277 1384570NM BS 727 CRACKED A AWXAO OTHER O OTHER ININSP/MAINT 1 WP28189AW 22656 PHX - FLT NR 2632 - DURING MAINTENANCE WALK AROUND, FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN AT STATION 727 STRINGER 17L. CONFIRMED CRACK WITH EDDY CURRENT. REPAIRED PER SRM 53-30-3, FIGURE 25. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960126006031996012600603NM 1996 1 26 AWXA9500790 119951129A57546546422208 TRACK BOEING737 737297 1384480NM NR 5 LE FLAP WORN A AAWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28147AW BN162 22630 PHX - FLT NR 417 - PHX/COS - AIR TURN BACK - AIRCRAFT ROLLED TO THE LEFT AND REQUIRED 15 TO 20 DEGREE RIGHT AILERON TO CORRECT. SITUATION CORRECTED AFTER FLAPS RETRACTED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 5 LEADING EDGE SLAT AUXILLIARY TRACK FITTING MOUNT HOLES TO BE ELONGATED. REMOVED AND REPLACED NR 5 SLAT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19960126006041996012600604NM 1996 1 26 AWXA9500795 119951204A215020405010 ACM BOEING737 7373G7 1384595NM LT PACK MALFUNCTIONED A AWXAA UNSCHED LANDING O OTHER CLCLIMB 1 WP28302AW 37623 24009 LAS/BUR - PRESSURIZATION WAS INADEQUATE DURING INITIAL CLIMB. FLIGHT WAS ABORTED. AIRCRAFT RETURNED TO LAS LANDING WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED PACK FLOW CONTROL VALVE AND THE LEFT AIR CYCLE MACHINE PER BMM CHAPTER 21. BOTH OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960126006051996012600605NM 1996 1 26 AWXA9500797 119951205A2750 RETRACT MECH BOEING737 737277 1384570NM TE FLAPS LACK OF LUBE A AAWXAO OTHER O OTHER TOTAKEOFF 1 WP28182AW 22649 LAS - FLT NR 934 - AIRCRAFT ROLLS SHARPLY TO THE RIGHT AT LIFT OFF AND REQUIRES A LOT OF LEFT AILERON ON LANDING. INSPECTED AND OPERATED FLAPS, AILERONS, SPOILERS AND SLATS ON GROUND. NO DEFECTS NOTED. LUBED FLAP GIMBLES AND TRACKS. OK FOR SERVICE. A/C HAS FLOWN ELEVEN FLIGHTS WITHOUT INCIDENT. (M) 2L72 4F RTA16WE 19960126006061996012600606NM 1996 1 26 AWXA9500822 119951223A5320 TEAR STRAP BOEING737 7373G7 1384595NM BS 294 DAMAGED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28307AW 24634 PAE - FLT NR 3694 - TEMPORARY PATCH AT BS 294, WL 156 HAS WORKING FASTENERS BETWEEN STRINGER 22-24 RIGHT HAND. REMOVED EXISTING SKIN PATCH, REPAIRED TEAR STRAP AND INSTALLED EXTERNAL DOUBLER IAW SRM 53-00-01 FIGURE 202 AND 225. (M) 2L72 4F RTA16WE 19960126006071996012600607SO 1996 1 26 C2XA95IA415 119951226A553012015374002 ANGLE EMB 120 EMB120RT SO RT VERT STAB CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006081996012600608SO 1996 1 26 C2XA95IA416 119951226A553012015374001 ANGLE EMB 120 EMB120RT SO LT VERT STAB CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT DRAG ANGLE CRACKED NEAR FORWARD END. MAINTENANCE REMOVED AND REPLACED THE DRAG ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006091996012600609SO 1996 1 26 C2XA95IA417 119951226A534712016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006101996012600610SO 1996 1 26 C2XA95IA418 119951226A534712026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006111996012600611SO 1996 1 26 C2XA95IA419 119951226A534712015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD OUTBOARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006121996012600612SO 1996 1 26 C2XA95IA420 119951226A534712015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FWD OUTBOARD SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006131996012600613SO 1996 1 26 C2XA95IA421 119951226A540012030995001 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE FRAME NR 2 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006141996012600614SO 1996 1 26 C2XA95IA422 119951226A532012004149001 T-PROFILE EMB 120 EMB120RT SO AFT CABIN CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND T-PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE T-PROFILE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006151996012600615SO 1996 1 26 C2XA95IA423 119951226A273012010841001 SPRING EMB 120 EMB120RT SO LT CONTL COLUMN BROKEN A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND SPRING ON CAPTAINS CONTROL COLUMN BROKEN. MAINTENANCE REMOVED AND REPLACED THE SPRING, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006161996012600616SO 1996 1 26 C2XA95IA424 119951226A572012017060007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 1, SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006171996012600617SO 1996 1 26 C2XA95IA425 119951226A572012017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 2, SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006181996012600618SO 1996 1 26 C2XA95IA426 119951226A572012017064009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN NR 4, SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006191996012600619SO 1996 1 26 C2XA95IA427 119951226A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN NR 2, NR 3 SKIN SUPPORTS CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006201996012600620SO 1996 1 26 C2XA95IA428 119951226A572012017056015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, FOUND RT WING LOWER SKIN NR 3 SKIN SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006211996012600621SO 1996 1 26 C2XA95IA429 119951228A572012017062013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006221996012600622SO 1996 1 26 C2XA95IA430 119951228A572012017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENACNE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006231996012600623SO 1996 1 26 C2XA95IA431 119951228A572012017063009 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB NR 22, UPPER NR 4 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006241996012600624SO 1996 1 26 C2XA95IA432 119951228A572012017063007 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE LEFT WING RIB 22, LOWER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006251996012600625SO 1996 1 26 C2XA95IA433 119951228A572012017057015 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 1 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006261996012600626SO 1996 1 26 C2XA95IA434 119951228A572012017056007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB NR 16, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006271996012600627SO 1996 1 26 C2XA95IA435 119951228A572012017063009 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0916729 120185 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 21, UPPER NR 2 SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006321996012600632SO 1996 1 26 C2XA96IA005 119951224A540012030995002 ANGLE EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0931711 120107 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME 2 ATTACH ANGLE CRACKED ON OUTBOARD END. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006331996012600633SO 1996 1 26 C2XA96IA006 119951224A540012030995001 ANGLE EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XAK NONE O OTHER ININSP/MAINT 1 SW0931711 120107 IAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE NACELLE FRAME 2 ATTACH ANGLE INBOARD SIDE CRACKED AT RIVETS. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA31SO 19960126006411996012600641WP 1996 1 26 CKSA95148 119951217A575457695842 PANEL DOUG DC8 DC855 3021927WP RT LE FLAP CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT OUTBOARD PANEL 1 SPOT CORROSION, 1 SCREW MISSING. INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0 AND MM 27-41-2. (M) 2L74 4F 4A25 19960126006421996012600642WP 1996 1 26 CKSA95149 119951217A575457695822 PANEL DOUG DC8 DC855 3021927WP RT LE FLAP CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND OUTBOARD SLOT INBOARD PANEL CORRODED AT LEADING EDGE. INSTALLED NEW OUTBOARD SLOT INBOARD PANEL IAW DC-8 SRM 57-2-0, 51-3-0 AND MM 27-41-2. (M) 2L74 4F 4A25 19960126006431996012600643WP 1996 1 26 CKSA95150 119951217A532036469712 ANGLE DOUG DC8 DC855 3021927WP RT MLG WW CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT WHEEL WELL DOGHOUSE FORWARD LOWER CORRODED. REMOVED AND REPLACED LOWER ANGLE, INSTALLED FASTENERS IAW 51-1-20D. (M) 2L74 4F 4A25 19960126006441996012600644WP 1996 1 26 CKSA95151 119951217A532036469711 ANGLE DOUG DC8 DC855 3021927WP LT MLG WW CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND LEFT WHEEL WELL DOGHOUSE FORWARD LOWER CORRODED. REMOVED ANGLE AND INSTALLED NEW ANGLE PER 51-1-20D. (M) 2L74 4F 4A25 19960126006451996012600645WP 1996 1 26 CKSA95152 119951217A57205614933 FLANGE DOUG DC8 DC855 3021927WP WING TE CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND UPPER TRAILING EDGE PANEL PULLING LOOSE AND POPPED RIVETS JUST OUTBOARD OF MAIN LANDING GEAR TRUNNION. FOUND LOWER FLANGE CORRODED BEYOND LIMITS. INSTALLED NEW FLANGE IAW DC-8 SRM 57-2-0. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. REPLACED RIVETS IAW DC-8 SRM 51-1-21. (M) 2L74 4F 4A25 19960126006461996012600646WP 1996 1 26 CKSA95153 119951217A53205643623511 FITTING DOUG DC8 DC855 3021927WP BS 1320 CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND AFT PIT STATION 1320 CABIN FLOOR SUPPORT AT CENTER SEAT TRACK CRACKED. REMOVED AND INSTALLED NEW FLOOR SUPPORT FITTING AS REQUIRED AS PER 53-2-0. (M) 2L74 4F 4A25 19960126006471996012600647WP 1996 1 26 CKSA95154 119951217A53135615328 LONGERON DOUG DC8 DC855 3021927WP LT MLG WW CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND LEFT LONGERON 24 CRACKED IN FORWARD BOLT CUTOUT. REPAIRED CRACK PER DC-8 SRM 53-2-2 FIGURE 6, SHEET 1. INSTALLED HI-LOCK FASTENERS PER 51-1-20D. (M) 2L74 4F 4A25 19960126006481996012600648WP 1996 1 26 CKSA95155 119951217A53135615328 LONGERON DOUG DC8 DC855 3021927WP RT MLG WW CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT WHEEL WELL LONGERON 24 CRACKED AT FORWARD VERTICAL FITTING STATION 879.325. REPAIRED RIGHT WHEEL WELL LONGERON 24 IAW DC-8 SRM 53-2-2 FIGURE 9, SHEET 1 AND 53-2-2 FIGURE 9, SHEET 2. (M) 2L74 4F 4A25 19960126006491996012600649WP 1996 1 26 CKSA95156 119951217A55125640808507 PANEL DOUG DC8 DC855 3021927WP HORIZ STAB CRACKED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK 45816 KOSC - DURING C-CHECK INSPECTION, FOUND REF R/O 801-363 CRACK INDICATION HORIZONTAL STABILIZER CONSTANT SECTION UPPER FORWARD PANEL RIGHT SIDE BOLT HOLE NR 4 TO NEXT HOLE FORWARD TO FORWARD END OF PANEL. REMOVED AND REPLACED FORWARD UPPER PANEL IAW REFERENCE BULLETIN 55-15 (DC-8 S/B). (M) 2L74 4F 4A25 19960126006501996012600650WP 1996 1 26 CKSA95157 119951217A53124597643 BLKHD ANGLE DOUG DC8 DC855 3021927WP AFT PRESS BLKHD CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND APB LEFT SIDE FLOOR TO BULKHEAD ANGLE CORRODED. REMOVED AND INSTALLED NEW ANGLE AS IT REQUIRED AS PER IAW DC-8 SRM 53-2-0. (M) 2L74 4F 4A25 19960126006511996012600651WP 1996 1 26 CKSA95158 119951217A571155978312 SPAR CAP DOUG DC8 DC855 3021927WP WS 86 CRACK A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND LEADING EDGE STATION XFS 86 (APPROX) TOP SPAR CAP CRACKED AND CORRODED. INSTALLED REPAIR AS IT REQUIRED IAW AIA/E2119 AND DC-8 SRM 51-1-20D. (M) 2L74 4F 4A25 19960126006521996012600652WP 1996 1 26 CKSA95159 119951217A53135615328 LONGERON DOUG DC8 DC855 3021927WP RT MLG WW CORROSION A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 KOSC - DURING C-CHECK INSPECTION, FOUND RIGHT LONGERON 24 AT AFT END CORROSION EXCEEDS 20 PERCENT MATERIAL THICKNESS, APPROXIMATE 2 INCH CRACK COMING OUT OF CORRODED AREA ON HORIZONTAL WEB FORWARD AND AFT DIRECTION. REPAIRED RIGHT LONGERON 24 IAW DC-8 SRM 53-2-2 FIGURE 5 AND 51-1-20D AND 51-1-21. (M) 2L74 4F 4A25 19960126006531996012600653WP 1996 1 26 CKSA95160 119951217A57112700627 SPAR CAP DOUG DC8 DC855 3021927WP WS 410 CORRODED A CKSAK NONE O OTHER ININSP/MAINT 1 GL23801CK59357 45816 DURING C-CHECK INSPECTION, FOUND OUTBOARD FLAP TOP SPAR CAP AT STATION 410 CORRODED. REPAIRED SPAR CAP IAW DC-8 SRM 57-2-0 FIGURE 2. ALODINED AND PRIMED IAW DC-8 SRM 51-1-21. INSTALLED HI-LOCKS IAW DC-8 SRM 51-1-20. REPAIRED LOWER FLAP SKIN IAW DRAWING SKA95224-2. (M) 2L74 4F 4A25 19960126006541996012600654NE 1996 1 26 EIAA9569 219951218A7261 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 OIL LEAK A AEIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 NM09479EV 19898 662747 DURING CRUISE, NR 2 ENGINE OIL QUANTITY BEGAN DECREASING AT MODERATE RATE. WHEN QTY REACHED EMPTY PULLED POWER BACK TO IDLE. AFTER A FEW MINUTES QTY ROSE A LITTLE THEN BELOW EMPTY MARK. AS PRECAUTIONARY SHUT DOWN ENGINE. DURING WINDMILLING MAINTAINED POS OIL PRESSURE. CLEANED ENGINE OF ALL GREASE AND OIL, RAN NR 2 ENGINE FOR 5 MINUTES AT IDLE POWER, OIL PRESS AND QUANTITY NORMAL. SHUT DOWN ENGINE AND REMOVED COWLING NR 2 ENGINE. INSPECTED FOR LEAKS, NO LEAKS FOUND AT THIS TIME. (M) 2L74 4F4 F A20WE E20EA 19960126006551996012600655WP 1996 1 26 EIAA9570 119951222A3260 LATCH LIGHT DOUG DC8 DC862F 3021972WP GEAR DOORS ILLUMINATED A EIAAO OTHER N FALSE WARNING CLCLIMB 1 NM09817EV 46022 DOORS NOT LATCHED INDICATION ILLUMINATED AFTER GEAR RETRACTION. AFTER UPLATCH CHECK, LIGHT OUT AND ALL INDICATIONS NORMAL. TEST DOOR CLOSED SWITCH MECHANISM. NO DEFECTS NOTED. OPS NORMAL IAW DC8 MM 32-12-1. (M) 2L74 4F 4A25 19960126006561996012600656NE 1996 1 26 EIAA9571 219951224A7261 ENGINE BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 REQ'D OIL A EIAAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 NM09479EV 19898 662747 PRECAUTIONARY NR 2 ENGINE SHUTDOWN AT TOP OF DESCENT FOR LOW ENGINE OIL QTY. ENGINE OIL TEMP AND PRESSURE NORMAL. ENGINE NR 2 COWLING OPENED AND INSPECTED/CLEANED NR 2 ENGINE OF ALL GREASE AND OIL. ENGINE RUN PERFORMED AT IDLE POWER. FOUND NO SIGN OF OIL LEAKAGE. RESERVICED ENGINE WITH 20 QTS TO REQUIRED LEVEL, OIL LEVEL DURING ENGINE RUN FOUND SATISFACTORY. (M) 2L74 4F4 F A20WE E20EA 19960126006571996012600657NE 1996 1 26 EIAA9572 219951224A7230 NR 2 BEARING BOEING747 747132 1384882NM PWA JT9 JT9D7F 52054NE NR 2 ENGINE OIL LEAK A EIAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 NM09479EV 19898 662747 HKG - NR 2 ENGINE OIL QTY DROPPED BELOW ONE-QUARTER, PRECAUTIONARY SHUTDOWN, RESTARTED FOR LANDING, ENGINE OIL TEMP AND PRESSURE NORMAL. FOUND OIL LEAKING FROM NR 2 BEARING BREATHER TUBES (AT ELBOW) WHEN ENGINE NR 2 WAS RUN AT HIGH POWER SETTINGS. REPLACED SEAL, SERVICED 22 QTS OIL, LEAK CHECK SATISFACTORY. ADDITIONAL LEAK CHECK ON OIL SYSTEM CARRIED OUT, CHECKED INLET, EXHAUST, NR 2 BEARING WEEP TUBE, OILCOOLER AREA, FRONT AND REAR DRAINS AND ALL OIL SYSTEM LINES. FOUND ALL OK, CARRIED OUT HIGH POWER RUN. NO FURTHER LEAKAGE NOTED. (M) 2L74 4F4 F A20WE E20EA 19960126006581996012600658NE 1996 1 26 EIAA9573 219951223A7200 ENGINE DOUG DC9 DC932F 3022067WP PWA JT8 JT8D9A 52048NE LEFT MALFUNCTIONED A EIAAO OTHER EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 NM09935F 4548 47220 654403 KTN - LEFT ENGINE EPR ABRUPTLY DROPPED TO 1.4 AND EGT PEGGED, CLIMB AT FL 260 ACCOMPANIED BY STRONG VIBRATION, REDUCING THRUST LEVER TO IDLE LESSENED VIBRATION AND EGT CAME DOWN TO 500 DEGREES. WHEN EPR INITIALLY DROPPED TO 1.4, N1 DROPPED TO 38 PERCENT AND N2 DROPPED TO 62 PERCENT. (M) 2L72 4F4 F A6WE E2EA 19960126006591996012600659NM 1996 1 26 EISA95391 119951017A323077GE0761 RETRACT MECH BOEING727 72725 1384006NM NLG LACK OF LUBE A EISAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW07290NE14523 18972 NOSE GEAR FAILED TO EXTEND NORMALLY, RECYCLED SEVERAL TIMES WITH NO GREEN LIGHT, AFTER THIRD TRY NOSE GEAR EXTENDED OK. INSPECTED AND LUBED NOSE GEAR AND ASSOCIATED LINKAGE, RAN EXTENSION AND RETRACTION PER MM 32-33-0. NO DEFECTS NOTED. (M) 2L73 4F A3WE 19960126006601996012600660NM 1996 1 26 EISA95446 119951203A5321 FLOOR BOEING727 72731 1384010NM BS 290-300 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CORROSION AT FORWARD LAV FLOOR PANEL BETWEEN STATION 290-300. REMOVED BAD PART OF FLOOR, FABRICATED NEW PIECE AND DOUBLER PER SRM 57-10-6. INSTALLED FABRICATED PANEL AND DOUBLER PER SRM 51-10-1. 2L73 4F A3WE 19960126006611996012600661NM 1996 1 26 EISA95447 119951129A5347 SEAT TRACK BOEING727 72731 1384010NM BS 825 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CORROSION EXISTS AT SEAT TRACK, STATION 825-830 LEFT. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960126006621996012600662NM 1996 1 26 EISA95450 119951201A5230 HINGE BOEING727 72731 1384010NM MAIN CARGO DOOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 MAIN CARGO DOOR AFT HINGE CORNER APPEARS TO BE CRACKED. INSTALLED NEW HINGE IAW SRM 51-30-2. (M) 2L73 4F A3WE 19960126006631996012600663NM 1996 1 26 EISA95452 119951108A5754 RIB BOEING727 72731 1384010NM NR 5 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 RT WING NR 5 SLAT OUTBOARD NOSE RIB CRACKED WHERE ROD END ATTACHES. REMOVED AND REPLACED RIB IAW SRM 51-10-4. (M) 2L73 4F A3WE 19960126006641996012600664NM 1996 1 26 EISA95454 119951201A5315 FLOOR BEAM BOEING727 72731 1384010NM BS 560 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 FORWARD CARGO COMPARTMENT CORROSION AT FLOOR BEAM STATION 560 RIGHT SIDE. REMOVED CORROSION AND FABRICATED DOUBLER AND INSTALLED PER SRM 51-10-8. (M) 2L73 4F A3WE 19960126006651996012600665NM 1996 1 26 EISA95459 119951201A5522 SKIN BOEING727 72731 1384010NM RT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK IN ELEVATOR INTERNAL STRUCTURE AT APPROXIMATELY ELEVATOR STATION 69 RIGHT, 6 INCHES AFT OF LEADING EDGE. STOP DRILLED CRACK, FABRICATED REPAIR PER SRM 55-20-02 AND INSTALLED REPAIR PER SRM 51-10-2. (M) 2L73 4F A3WE 19960126006661996012600666NM 1996 1 26 EISA95460 119951201A5315 FLOOR BEAM BOEING727 72731 1384010NM FWD LAV CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 FOUND CORROSION AT CABIN INTERIOR, FORWARD LAVATORY FLOOR SUPPORT. REMOVED CORROSION AND FABRICATED DOUBLER PER SRM 51-40-3. (M) 2L73 4F A3WE 19960126006671996012600667NM 1996 1 26 EISA95468 119951201A5522 SKIN BOEING727 72731 1384010NM LT ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 CRACK IN LEFT ELEVATOR STRUCTURE AT APPROXIMATELY STATION 102 LEFT, 2 INCHES AFT OF FLUSH PANEL. STOP DRILLED CRACK AND FABRICATED DOUBLER PER SRM 56-20-3. INSTALLED DOUBLER PER SRM 55-20-3. (M) 2L73 4F A3WE 19960126006681996012600668NM 1996 1 26 EISA95473 119951108A5754 BRACKET BOEING727 72731 1384010NM NR 7 SPOILER CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 LEFT BRACKET FOUND CRACKED AT OUTBOARD SIDE OF NR 7 SPOILER ACTUATOR CASTING. FABRICATED AND INSTALLED WEB REPAIR IAW SRM 51-40-2. (M) 2L73 4F A3WE 19960126006691996012600669NM 1996 1 26 EISA95484 119951130A5754 RIB BOEING727 72731 1384010NM NR 6 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07240NE 18906 NR 6 SLAT OUTBOARD NOSE RIB FOUND CRACKED AT PREVIOUS REPAIR, WHERE ACTUATOR ROD END ATTACHES. INSTALLED NEW NOSE RIB PER SRM 51-10-4. (M) 2L73 4F A3WE 19960126006711996012600671WP 1996 1 26 IXXA9572 119950103A21105614845517 TURBO COMPRESSOR DOUG DC8 DC863F 302198FWP NR 2 ENG FAILED A IXXAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23906R 46087 BETWEEN IAH AND BRO, THE NR 2 CABIN TURBO COMPRESSOR STALLED AND CREATED A LOUD NOISE AND OILY FUMES IN THE COCKPIT. MAINTENANCE DETERMINED THAT THE CABIN TURBO COMPRESSOR HAD SEIZED. THE NR 2 TC WAS DEFERRED AND SCHEDULED FOR REPLACEMENT. (M) 2L74 4F 4A25 19960126006731996012600673NE 1996 1 26 IXXA9596 219950103A7230591168 DIFFUSER DOUG DC8 DC862 3021970WP PWA JT3D JT3D7 52039NE NR 3 ENG CRACKED A AIXXAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL2331CX 932 45911 670973 EN ROUTE FROM OEDR TO ETAR, NR 3 ENGINE WAS NOTED TO BE LOOSING OIL QUANTITY. THE ENGINE WAS PRECAUTIONARILY SHUT DOWN, AND THE AIRCRAFT DIVERTED TO LIPA FOR MAINTENANCE. ON THE GROUND IN LIPA, MAINTENANCE DETERMINED THAT OIL WAS BEING LOST IN THE GAS PATH, POOLING IN THE TURBINE EXHAUST CASE. THE ENGINE WAS REMOVED FROM SERVICE AND SENT TO THE SHOP. TEARDOWN INSPECTION REVEALED A CRACK IN THE DIFFUSER CASE, CAUSING BEARING SUMP AREAS TO PRESSURIZE, PUSHING OIL INTO THE GASPATH. THE ENGINE WAS REPAIRED, TESTED, AND RETURNED TO SERVICE. (M) 2L74 4F4 F 4A25 1E8 19960126006741996012600674SW 1996 1 26 MALA954728 119951202A2612 FIRE WIRE SWRNGNSA227 SA227AC 8780603SW RT ENGINE SHORTED A MALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL15446MA AC693 FLT NR 3334 - EN ROUTE, THE RIGHT ENGINE FIRE LIGHT BECAME DIMLY VISIBLE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPAIRED A SHORTED WIRE TO THE SIDE FIRE DETECTOR. ALL SYSTEMS OPERATED SATISFACTORILY DURING GROUD RUNS. (M) 1L72 4T A8SW 19960126006751996012600675SW 1996 1 26 MALA954736 119951209A3260 SWITCHES SWRNGNSA227 SA227AC 8780603SW NLG DIRTY A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL152692P AC658B FLT NR 3233 - ON CLIMB-OUT FROM MSP, THE NOSE GEAR INTRANSIT LIGHT WOULD NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND THE PROBLEM REMAINED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE GEAR POSITION SWITCHES WERE CLEANED. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006761996012600676SW 1996 1 26 MALA954737 119951209A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL152692P AC658B FLT NR 3235 - ON APPROACH TO MSP, THE NOSE GEAR INTRANSIT LIGHT DIDN'T ILLUMINATE DURING GEAR EXTENSION. ALL OTHER GEAR INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE UPLIMIT AND POSITION SWITCHES IN THE NOSE LANDING GEAR BAY. SYSTEM OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006771996012600677SW 1996 1 26 MALA954738 119951208A3260 POSITION SW SWRNGNSA227 SA227AC 8780603SW LT/RT MLG OUT OF ADJUST A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL1560NE AC760B FLT NR 3226 - AFTER DEPARTURE FROM MSP, THE NOSE GEAR CYCLED IN THE WHEEL WELL. THE CREW ELECTED TO RETURN TO MSP, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL ADJUSTED THE RIGGING ON THE LEFT AND RIGHT MAIN GEAR UP POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006781996012600678SW 1996 1 26 MALA954739 119951208A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15426MA AC645 FLT NR 3065 - INBOUND TO DTW, THE CREW HAD TO CYCLE THE LANDING GEAR THREE TIMES IN ORDER TO GET A GREEN LIGHT FOR THE RIGHT MAIN GEAR. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT INBOARD GEAR POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006791996012600679 1996 1 26 MALA954740 419951208A341427193027 AIRSPEED IND SWRNGNSA227 SA227AC 8780603SW LT/RT COCKPIT FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15422MA AC635 DURING A DEADHEAD FLIGHT FROM GRB TO MSP, THE CREW NOTED UNRELIABLE INDICATIONS FROM THE CAPTAINS AND FLIGHT OFFICERS AIRSPEED INDICATORS. DUE TO WEATHER, THE AIRCRAFT DIVERTED TO CWA AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 AND NR 2 AIRSPEED INDICATORS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006801996012600680SW 1996 1 26 MALA954741 119951209A57532731141001 DOUBLERS SWRNGNSA227 SA227AC 8780603SW TE FLAPS WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING MAINTENANCE IN MSP, THE LEFT AND RIGHT FLAP ROLLER DOUBLERS WERE FOUND TO BE WORN. REPAIRS WERE COMPLETED BY REPLACING THE ROLLER DOUBLERS, P/N 27-31141-001, IAW FAC ARP 57-10-9513 AND ARP 57-20-9424. (M) 1L72 4T A8SW 19960126006811996012600681SW 1996 1 26 MALA954742 119951210A5320 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 149.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15422MA AC635 DURING SCHEDULED MAINTENANCE IN MSP, THE AFT CARGO FUSELAGE DOOR FRAME, FS 491.060 WAS FOUND TO BE CRACKED AT THE DOOR SNUBBER ATTACH POINT. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE AND DOUBLER IAW FAC ARP 53-20-9503. (M) 1L72 4T A8SW 19960126006821996012600682SW 1996 1 26 MALA954743 119951209A5347 SEAT CHANNEL SWRNGNSA227 SA227AC 8780603SW FS 107 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CRACKS AT THE NUT PLATE ATTACH RIVET HOLES ON THE RIGHT INBOARD SEAT CHANNEL LOCATED APPROXIMATELY 4 INCHES AFT OF FS 107. REPAIRS WERE COMPLETED BY INSTALLING A DOUBLER IAW FAC ARP 53-10-9322. (M) 1L72 4T A8SW 19960126006831996012600683SW 1996 1 26 MALA954744 119951209A5347 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 116.56 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND CRACKS AT THE LEFT OUTBOARD SEAT TRACK ATTACH HOLES ON FS 116.56. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW AERO TECH DESIGNS EA 01-95032. (M) 1L72 4T A8SW 19960126006841996012600684SW 1996 1 26 MALA954745 119951209A27302744026007 TQ TUBE ARM SWRNGNSA227 SA227AC 8780603SW LT ELEVATOR CORRODED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING SCHEDULED INSPECTION IN MSP, THE LEFT ELEVATOR TORQUE TUBE ARM, P/N 27-44-026-007, WAS FOUND TO BE CORRODED. REPAIRS WERE COMPLETED TO THE ARM IAW FAC MM 27-30-00 PAGES 202 AND 203 AND SRM 51-40-01 AND 51-40-02. (M) 1L72 4T A8SW 19960126006851996012600685SW 1996 1 26 MALA954746 119951209A575327311141003 DOUBLER SWRNGNSA227 SA227AC 8780603SW WS 27.103 WORN A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT WING TRAILING EDGE RIB AT WS 27.103 TO HAVE THE FLAP WALKING BEAM DOUBLER WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER, P/N 27-311141-003, IAW FAC ARP 57-109513. (M) 1L72 4T A8SW 19960126006861996012600686SW 1996 1 26 MALA954747 119951207A5230 CARGO DOOR SWRNGNSA227 SA227AC 8780603SW FS 438.06 DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15442MA AC725 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR SNUBBER ATTACH POINT AT FS 438.060 TO BE DAMAGED. REPAIRS WERE COMPLETED BY INSTALLING FILLER, DOUBLER AND REPAIR ANGLE IAW FAC ARP 53-20-9503. (M) 1L72 4T A8SW 19960126006871996012600687SW 1996 1 26 MALA954749 119951209A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG DIRTY A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15445MA AC687 FLT NR 3065 - INBOUND TO DTW, THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN THE GEAR HANDLE WAS SELECTED DOWN. THE CREW RECYCLED THE GEAR AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED THE DOWN POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006881996012600688 1996 1 26 MALA954750 419951211A3418 SAS LIGHT SWRNGNSA227 SA227AC 8780603SW COCKPIT ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL152693C AC659B FLT NR 3453 - AFTER TAKEOFF FROM DTW, THE SAS FAULT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED A FUNCTIONAL CHECK OF THE SAS SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006891996012600689SW 1996 1 26 MALA954753 119951213A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER P NO WARNING INDICATION APAPPROACH 1 GL15426MA AC645 FLT NR 3359 - INBOUND TO DTW, WHEN THE CREW SELECTED GEAR DOWN, THE RIGHT MAIN GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AND THE GREEN LIGHT DID NOT ILLUMINATE. THE CREW RECYCLED THE GEAR, ALL INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LOWER OUTBOARD DOWN AND LOCKED POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006901996012600690SW 1996 1 26 MALA954756 119951216A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG FAILED A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL152692P AC658B FLT NR 3049 - ON APPROACH TO MSP, THE RIGHT GEAR INTRANSIT LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR WAS EXTENDED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT INBOARD AND OUTBOARD MAIN LANDING GEAR UP POSITION SWITCHES. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006911996012600691SW 1996 1 26 MALA954757 119951218A29102719154001 TRANSDUCER SWRNGNSA227 SA227AC 8780603SW HYD SYSTEM LEAKING A MALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL152693C AC659B FLT NR 3401 - DURING TAXI INTO GATE AT DTW, THE AIRCRAFT LOST ALL HYDRAULIC PRESSURE RESULTING IN LOSS OF NOSE WHEEL STEERING AND FLAP SYSTEMS. MAINTENANCE PERSONNEL REPLACED THE HYDRAULIC PRESSURE TRANSDUCER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006921996012600692WP 1996 1 26 MALA954758 219951223A7200 ENGINE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE331* 01514WP RIGHT MALFUNCTIONED A AMALAA UNSCHED LANDING O OTHER CLCLIMB 1 GL15446MA AC693 FLIGHT NR 3213 - ON CLIMB-OUT FROM MSP, THE RIGHT ENGINE TORQUE BEGAN TO INDICATE IN EXCESS OF 120 PERCENT. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE ENGINE. INVESTIGATION IS CONTINUING. (M) 1L72 4T3 T A8SW E2WE 19960126006931996012600693NM 1996 1 26 MALA954759 119951223A5230 SKIN DHAV DHC8 DHC8102 2809003NM BAGG DOOR DAMAGED A MALAK NONE O OTHER ININSP/MAINT 1 GL15802MA 245 DURING A SHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED DAMAGE TO THE BAGGAGE DOOR SKIN. THEY REPAIRED THE DAMAGE BY FABRICATING AND INSTALLING AN EXTERNAL DOUBLER IAW DHC RD8-52-207. (M) 2H72 4T RTA13NM 19960126006941996012600694NM 1996 1 26 MALA954760 119951222A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM RT MLG FAILED A MALAO OTHER J WARNING INDICATION APAPPROACH 1 GL15830MA 337 FLT NR 3028 - ON APPROACH TO DTW, THE RIGHT MAIN GEAR DID NOT EXTEND. THE CREW PERFORMED AN EMERGENCY EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE UPLOCK ACTUATOR. SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126006951996012600695NM 1996 1 26 MALA954761 119951216A3350 LIGHTS DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15852MA 349 DURING A MAINTENANCE WALKAROUND INSPECTION IN DTW, A MECHANIC NOTED THE FIRST TWO FLOOR TRACK EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL FOUND CONNECTOR 3352-J3 TO BE LOOSE AND SECURED IT. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126006961996012600696NM 1996 1 26 MALA954762 119951225A3260 WARNING HORN DHAV DHC8 DHC8102 2809003NM LANDING GEAR SOUNDED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15817MA 249 FLT NR 3099 - AFTER DEPARTURE FROM CWA, THE GEAR WARNING HORN SOUNDED AFTER THE GEAR WAS SELECTED UP AND REMAINED ON UNTIL AFTER 130 KNOTS. MAINTENANCE PERSONNEL FUNCTIONALLY TESTED THE LANDING GEAR WARNING HORN, BUT WAS UNABLE TO DUPLICATE THIS DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126006971996012600697SW 1996 1 26 MALA954763 119951225A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW RT MLG DIRTY A MALAO OTHER N FALSE WARNING APAPPROACH 1 GL15426MA AC645 FLT NR 3409 - ON APPROACH TO DTW, THE CREW DID NOT GET A GREEN DOWN AND LOCKED LIGHT FROM THE RIGHT MAIN GEAR. THEY RECYCLED THE GEAR TWICE AND THE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL CLEANED AND LUBRICATED THE RIGHT INBOARD MLG POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006981996012600698SW 1996 1 26 MALA954764 119951225A3340 CONNECTOR SWRNGNSA227 SA227AC 8780603SW NAV LIGHT SHORTED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15442MA AC725 FLT NR 3197 - EN ROUTE FROM DTW TO TVC, THE NAV LIGHT CIRCUIT BREAKER TRIPPED. THE CREW RESET THE CB BUT IT TRIPPED AGAIN. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPAIRED A SHORTED CONNECTION AT THE NAV LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126006991996012600699SW 1996 1 26 MALA954765 119951226A324631418 WHEEL SWRNGNSA227 SA227AC 8780603SW RT NLG OUT OF BALANCE A MALAA UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 GL15424MA AC639 FLT NR 3453 - AFTER TAKEOFF FROM DTW, CREW NOTED A VIBRATION FROM THE NOSE LANDING GEAR. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT NOSE WHEEL ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126007001996012600700SW 1996 1 26 MALA954766 119951226A27202742051037 TORQUE TUBE SWRNGNSA227 SA227AC 8780603SW RUDDER TWISTED A AMALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE RUDDER TORQUE TUBE, P/N 27-42051-037, WAS TWISTED. REPLACED THE TORQUE TUB IAW MM 27-20-20 AND THE SRM. (M) 1L72 4T A8SW 19960126007011996012600701SW 1996 1 26 MALA954767 119951226A52102724044012 CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED THE PASSENGER DOOR UPPER FORWARD CORNER, P/N 27-24044-012, WAS CRACKED. REPLACED THE CORNER IAW THE FAC SRM. (M) 1L72 4T A8SW 19960126007021996012600702SW 1996 1 26 MALA954768 119951226A5320 CHANNEL SWRNGNSA227 SA227AC 8780603SW FUSELAGE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE FORWARD BELLY FAIRING CENTER CHANNEL. REPAIRED THE CRACK BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW THE FAC SRM. (M) 1L72 4T A8SW 19960126007031996012600703SW 1996 1 26 MALA954769 119951226A5311 BELT FRAME SWRNGNSA227 SA227AC 8780603SW FS 174.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME FLANGE AT FS 174.06. STOP DRILLED THE CRACK AND FABRICATED AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 53-90-20. (M) 1L72 4T A8SW 19960126007041996012600704SW 1996 1 26 MALA954770 119951226A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE. REPLACED THE FORWARD 12 INCHES OF THE ATTACH ANGLE IAW SRM 51-00-00. (M) 1L72 4T A8SW 19960126007051996012600705SW 1996 1 26 MALA954771 119951226A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE OUTBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP. (M) 1L72 4T A8SW 19960126007061996012600706SW 1996 1 26 MALA954772 119951226A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP. (M) 1L72 4T A8SW 19960126007071996012600707SW 1996 1 26 MALA954773 119951226A54002735112 ANGLE SWRNGNSA227 SA227AC 8780603SW LT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15439MA AC722 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT UPPER INBOARD NACELLE TO WING SKIN ATTACH ANGLE. THEY REPLACED THE ATTACH ANGLE IAW FAC SRM 51-00-00. (M) 1L72 4T A8SW 19960126007081996012600708SW 1996 1 26 MALA954774 119951226A32312751042179 SHEAR BOLT SWRNGNSA227 SA227AC 8780603SW RT MLG DOOR SHEARED A AMALAO OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 GL15430MA AC710 FLT NR 3250 - DURING LANDING AT GFK, THE RIGHT GEAR DOOR POSITION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED THE LANDING WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RIGHT GEAR DOOR ROLLER SHEAR BOLT. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 1L72 4T A8SW 19960126007091996012600709NM 1996 1 26 MALA954775 119951227A3260864202 UPLOCK SW DHAV DHC8 DHC8102 2809003NM LT MLG FAILED A MALAO OTHER N FALSE WARNING CLCLIMB 1 GL15849MA 347 FLT NR 3166 - AFTER DEPARTURE FROM FNT, CREW RECEIVED A FLASHING GEAR UNSAFE LIGHT FROM THE LEFT MAIN GEAR. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT UPLOCK PROXIMITY SWITCH, P/N 8-642-02, AND THE PROXIMITY SWITCH ELECTRONICS UNIT, P/N 8-410-05. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007101996012600710NM 1996 1 26 MALA954776 119951227A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM RT MLG BINDING A MALAO OTHER O OTHER APAPPROACH 1 GL15817MA 249 FLIGHT NR 3171 - DURING APPROACH TO FNT, THE CREW NOTED RIGHT MAIN GEAR WAS SLOW TO EXTEND. THE AIRCRAFT CONTINUED TO FNT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RT MLG UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007111996012600711NM 1996 1 26 MALA954777 119951227A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG WORN A MALAO OTHER O OTHER APAPPROACH 1 GL15819MA 251 FLT NR 3341 - DURING APPROACH TO DTW, THE LEFT MAIN GEAR WAS SLOW TO EXTEND. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT MLG UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007121996012600712NM 1996 1 26 MALA954778 119951227A323010800113 UPLOCK ACT DHAV DHC8 DHC8102 2809003NM LT MLG WORN A MALAO OTHER O OTHER APAPPROACH 1 GL15826MA 330 FLT NR 3005 - DURING APPROACH TO BMI, THE LEFT MAIN GEAR WAS SLOW TO EXTEND. THE AIRCRAFT CONTINUED TO BMI AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT MLG UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007131996012600713NM 1996 1 26 MALA954779 119951110A3350 LIGHTS DHAV DHC8 DHC8102 2809003NM CABIN INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15816MA 231 DURING A MAINTENANCE GATE WALKAROUND INSPECTION, THE MECHANICS NOTED FOUR RED FLOOR TRACK EMERGENCY LIGHTS WERE OUT OF THEIR POSITIONS IN THE TRACK. MAINTENANCE PERSONNEL REPOSITIONED THE FLOOR TRACK LIGHTS IAW DH8 MM. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007141996012600714NM 1996 1 26 MALA954780 119951115A33506104789 BATTERY PACK DHAV DHC8 DHC8102 2809003NM LT EXTERIOR DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15828MA 333 DURING MAINTENANCE GATE WALKAROUND INSPECTION, THE MECHANIC NOTED THE EXTERIOR LEFT FWD EMERGENCY LIGHT WAS INOP. MAINTENANCE PERSONNEL REPLACED THE TOP WARDROBE BATTERY PACK. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007151996012600715NM 1996 1 26 MALA954781 119951101A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT INOPERATIVE A MALAK NONE L NO TEST ININSP/MAINT 1 GL15833MA 343 DURING A MAINTENANCE GATE WALKAROUND INSPECTION, THE MECHANIC NOTED THE COCKPIT OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE OVERHEAD LIGHT ASSEMBLY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007161996012600716NM 1996 1 26 MALA954782 119951203A3397 WIRE DHAV DHC8 DHC8102 2809003NM CABIN BROKEN A MALAK NONE L NO TEST ININSP/MAINT 1 GL15852MA 349 DURING PREFLIGHT INSPECTION IN DTW, THE CREW NOTED THE FIRST TWO LIGHTS IN THE FLOOR TRACK ESCAPE PATH LIGHTING SYSTEM WERE INOPERATIVE. MAINTENANCE PERSONNEL REPAIRED A BROKEN WIRE BETWEEN THE POWER SUPPLY AND CONNECTOR. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960126007171996012600717SW 1996 1 26 MALA954783 119951226A5532 SKIN SWRNGNSA227 SA227AC 8780603SW LT VERT STAB CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15159MC AC728B DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT VERTICAL STABILIZER SKIN. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC SRM 55-90-30. (M) 1L72 4T A8SW 19960126007181996012600718NM 1996 1 26 MALA954784 119951228A2422DH103024600CSIIBINVERTER DHAV DHC8 DHC8102 2809003NM AVIONICS RACK FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15819MA 251 FLT NR 3157 - AFTER TAKEOFF FROM DTW, THE SECONDARY INVERTER CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE SECONDARY INVERTER. (M) 2H72 4T RTA13NM 19960126007191996012600719EU 1996 1 26 P2RA950035 119951208A5320 INTERCOSTAL AIRBUS300 A300B4203 3930306EU CABIN CORRODED A P2RAK NONE O OTHER ININSP/MAINT 1 WP23149773259913354 274 PHX - DURING B-CHECK, FLOOR PANELS UNDER AFT LAVATORY AND GALLEY SPOTTED WITH CORROSION. REMOVED PANELS AND FOUND TWO FLOOR INTERCOSTAL BEAMS CORRODED AT STATION C72-C75, RBL 48-66. REPLACED FLOOR INTERCOSTAL BEAMS PER SRM 51-10-10 AND TREATED AREA AND PANELS PER SRM 53-10-10, 51-10-30. (M) 2L72 4F A35EU 19960126007201996012600720EU 1996 1 26 P2RA950036 119951207A5414 PANEL AIRBUS300 A300B4203 3930306EU NR 1 PYLON CRACKED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 483DL WAS CRACKED AND BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M) 2L72 4F A35EU 19960126007211996012600721EU 1996 1 26 P2RA950037 119951207A5414 PANEL AIRBUS300 A300B4203 3930306EU NR 1 PYLON CRACKED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURNG B-CHECK, NR 1 ENGINE PYLON PANLE NR 475CL HAS LOOSE FASTENERS AND CRACK PROGRESSING TOWARD FASTENERS HOLE. REMOVED AND REPLACED LOOSE FASTENERS PER SRM 51-30-1. INSTALLED DOUBLER OVER CRACK CONDITION PER SRM 51-30-1. (M) 2L72 4F A35EU 19960126007221996012600722EU 1996 1 26 P2RA950038 119951209A5414 PANEL AIRBUS300 A300B4203 3930306EU NR 1 PYLON CRACKED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING C-CHECK, NR 1 PYLON HAS A CRACK AND MISSING MATERIAL FROM INTERNAL WEB ON LOWER AFT PANEL. MAINTENANCE REMOVED AND REPLACED DAMAGED AREA PER SRM 54-00-00. (M) 2L72 4F A35EU 19960126007231996012600723EU 1996 1 26 P2RA950039 119951208A5320 INTERCOSTALS AIRBUS300 A300B4203 3930306EU BS 1163-1238 CORRODED A P2RAK NONE O OTHER ININSP/MAINT 1 WP23149773259913354 274 PHX - DURING B-CHECK, INTERCOSTALS UNDER FORWARD LAVATORY AND GALLEY FROM STATION 1163 TO STATION 1238 (FRAME 14 AND FRAME 15A), BOTH 1 AND 2 LEFT AND RIGHT OF CENTER LINE, ARE CORRODED. RIGHT FRAME HAS 2.5 INCH DIAMETER WITH 15 PERCENT OF TOTAL THICKNESS AND LEFT FRAME HAS 2.5 INCH DIAMETER 10 PERCENT OF TOTAL THICKNESS. CORROSION CONDITIONS ON INTERCOSTALS BETWEEN FRAMES 14 AND 15A WAS DEFERRED BY AIRBUS INDUSTRIES LETTER DATED 12/9/95 UNITL AIRCRAFT NEXT C(2-8-96) FOR FINAL REPAIRS. PRESIDENTIAL AIR HAS ISSUED A MAINTENANCE CARRY OVER ITEM UNTIL FINAL REPAIRS COMPLETED. (M) 2L72 4F A35EU 19960126007241996012600724EU 1996 1 26 P2RA950040 119951207A5414 PANEL AIRBUS300 A300B4203 3930306EU NR 1 ENG PYLON BUCKLED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 474CR BUCKLED ON LOWER TRAILING EDGE. REPAIRED PANEL PER SRM 51-42-20. (M) 2L72 4F A35EU 19960126007251996012600725EU 1996 1 26 P2RA950041 119951207A5414 PANEL AIRBUS300 A300B4203 3930306EU NR 1 ENG PYLON BUCKLED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING B-CHECK, NR 1 PYLON PANEL NR 474DR HAS LOWER LEADING EDGE AND TRAILING EDGE BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M) 2L72 4F A35EU 19960126007261996012600726EU 1996 1 26 P2RA950042 119951207A5350 TAILCONE AIRBUS300 A300B4203 3930306EU NR 1 ENGINE CRACKED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING B-CHECK, NR 1 ENGINE TAILCONE HAS CRACK ON AFT LOWER END OF TAILCONE. REPAIRED TAILCONE BY WELDING CRACK CONDITION PER AC 43-13-1A. (M) 2L72 4F A35EU 19960126007271996012600727EU 1996 1 26 P2RA950043 119951209A5400 RIB AIRBUS300 A300B4203 3930306EU NR 2 PYLON CRACKED A P2RAK NONE O OTHER ININSP/MAINT 1 WP2314977 274 PHX - DURING B-CHECK, NR 2 ENGINE PYLON AFT FAIRING SUPPORT STRUCTURES INNER RIB CRACKED ENTIRE LENGTH OF THE RIB. REPAIRED PANEL RIB PER SRM 54-50-00 AND 51-30-2. (M) 2L72 4F A35EU 19960126007281996012600728EU 1996 1 26 RAIA951206 119951207A3411137391L401 PITOT BAG JETSTMJETSTM3201 1500217EU LEFT CONTAMINATED A RAIAO OTHER O OTHER CLCLIMB 1 CE03337TE 929 PAH - NR 7365 - CAPTAINS AIRSPEED INDICATOR STUCK AT 80 KNOTS. MAINTENANCE DRAINED WATER FROM PITOT SYSTEM. PERFORMED PITOT/STATIC TEST LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19960126007291996012600729EU 1996 1 26 RAIA951208 119951205A3350OL60424P BULB AEROSPATR72 ATR72202 8680940EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03723TE7735 283 STL - FLT NR 7162 - EMERGENCY LIGHT AT SERVICE DOOR INOP. MAINTENANCE REPLACED LIGHT BULB. (M) 2H72 4T RTA53EU 19960126007301996012600730EU 1996 1 26 RAIA951209 119951209A3222109A703056A STRUT BAG JETSTMJETSTM3201 1500217EU NLG REQ'D SERVICE A RAIAD RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03429AM 879 STL - FLT NR 7067 - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE SERVICED NOSE LANDING GEAR STRUT. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19960126007311996012600731EU 1996 1 26 RAIA951210 119951210A2912QA03043 FILTER BAG JETSTMJETSTM3201 1500217EU HYD SYSTEM DIRTY A RAIAK NONE J WARNING INDICATION APAPPROACH 1 CE03422AM900 856 STL - NR 7088 - NOSE GEAR TOOK TWO ATTEMPTS TO GEN DOWN AND LOCKED. MAINTENANCE REPLACED HYDRAULICS CASE DRAIN FILTER AND PRESSURE FILTER. GEAR SWINGS NORMAL AND LEAK CHECK GOOD. PRESSURE FILTER P/N QA03043, CASE DRAIN P/N QA03044. (M) 2L72 4T RTA56EU 19960126007321996012600732EU 1996 1 26 RAIA951211 119951211A2910HTE4005 CHECK VLV BAG JETSTMJETSTM3201 1500217EU HYD SYSTEM CRACKED A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION LDLANDING 1 CE03872AE5028 872 SAN - FLT 4795 - HYDRAULIC FAILURE IN FLIGHT. MAINTENANCE REPLACED HDRAULIC SYSTEM CHECK VALVE AT MAIN HYDRAULIC SYSTEM UNDER BAGGAGE POD. SYSTEM LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19960126007331996012600733EU 1996 1 26 RAIA951212 119951212A3411137391L401 PITOT DRAIN BAG JETSTMJETSTM3201 1500217EU LEFT MOISTURE A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03428AM10286 877 COU - FLT NR 7036 - CAPTAINS AIRSPEED STUCK AT 90 KNOTS. MAINTENANCE DRAINED CAPTAINS PITOT DRAIN FROM MOISTURE. PITOT/STATIC SYSTEM CHECK GOOD. (M) 2L72 4T RTA56EU 19960126007341996012600734EU 1996 1 26 RAIA951213 119951211A32609EN1C11HB2BB2 DNLOCK SW BAG JETSTMJETSTM3201 1500217EU NLG FAILED A RAIAO OTHER N FALSE WARNING LDLANDING 1 CE03422AM15000 856 STL - FLT NR 7320 - NOSE GEAR TOOK THREE ATTEMPTS TO SHOW DOWN AND LOCKED. MAINTENANCE REPLACED DOWNLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19960126007351996012600735EU 1996 1 26 RAIA951215 119951208A33503011151 BATTERY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE032FOR 121802973 199 EMERGENCY TRACKING LIGHTING INOP. MAINTENANCE REPLACED EMERGENCY BATTERY. (M) 2H72 4T RTA53EU 19960126007361996012600736EU 1996 1 26 RAIA951216 119951214A3242215221 BRAKE BAG JETSTMJETSTM3201 1500217EU LT MLG STICKY A RAIAC ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CE03342TE3548 954 STL - 7450 - BRAKES SEEMED TO CATCH AT 60 KNOTS ON TAKEOFF. MAINTENANCE REPLACED LEFT BRAKE ASSEMBLY. TAXI CHECK GOOD. (M) 2L72 4T RTA56EU 19960126007371996012600737EU 1996 1 26 RAIA951217 119951213A28417485222 FUEL QTY IND AEROSPATR42 ATR42300 8680920EU LEFT FAILED A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03421TE8032 6424 102 STL - FLT NR 7211 - LEFT FUEL QUANTITY GAUGE FLUX, BOOST PUMP CAME ON AND WOULD NOT SHUT. MAINTENANCE REPLACED FUEL QTY INDICATOR. OPS CHECK GOOD. (M) 2H72 4T RTA53EU 19960126007381996012600738EU 1996 1 26 RAIA951218 119951213A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RIGHT ENG OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03422AM106496674 856 JLN - FLT NR 7072 - TORQUE WOULD ONLY REACH 95 PERCENT ON TAKEOFF ON RIGHT SIDE. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUNS CHECK GOOD. (M) 2L72 4T RTA56EU 19960126007391996012600739EU 1996 1 26 RAIA951220 119951215A29101373HD1575 TUBE BAG JETSTMJETSTM3201 1500217EU LT MLG WW LEAKING A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03339TE7652 935 CMI - FLT NR 7439 - LANDING GEAR WOULD NOT RETRACT. REPLACED HYDRAULIC TUBE IN LEFT WHEEL WELL. (M) 2L72 4T RTA56EU 19960126007401996012600740EU 1996 1 26 RAIA951221 119951216A7712310703411 TQ BRIDGE BAG JETSTMJETSTM3201 1500217EU NR 1 ENG INOPERATIVE A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03435AM6883 1503 889 STL - 7492 - LEFT TORQUE DROPPED TO ZERO IN FLIGHT. MAINTENANCE CHANGED BRIDGES ON TORQUE RING. (M) 2L72 4T RTA56EU 19960126007411996012600741EU 1996 1 26 RAIA951222 119951218A33500341516 FUSE AEROSPATR42 ATR42300 8680920EU CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE15799 119 ENTRANCE DOOR EMERGENCY LIGHTS INOP. REPLACED FUSE IN POWER SUPPLY. (M) 2H72 4T RTA53EU 19960126007421996012600742EU 1996 1 26 RAIA951223 119951218A7722CA06RQ89SF80 CONNECTOR BAG JETSTMJETSTM3201 1500217EU NR 1 ENGINE LOOSE PIN A RAIAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03340TE7637 939 STL - FLT 7454 - NR 1 ENGINE EGT WENT TO ZERO. SECURED LOOSE PIN AT CANNON PLUG ON EGT COMP. (M) 2L72 4T RTA56EU 19960126007431996012600743EU 1996 1 26 RAIA951224 119951219A56101379628C402 WINDSCREEN BAG JETSTMJETSTM3201 1500217EU RT COCKPIT CRACKED A RAIAA UNSCHED LANDING O OTHER CRCRUISE 1 CE03872AE10253 872 FAT - FLT 4766 - RIGHT WINDSHIELD CRACKED. REPLACED WINDSCREEN. (M) 2L72 4T RTA56EU 19960126007451996012600745NM 1996 1 26 TAOA129509 119951221A3350079123 LENS BOEING727 727254 138408LNM CABIN MISSING A TAOAK NONE O OTHER ININSP/MAINT 1 EA15912TS 20438 RED ESCAPE PATH LIGHTING LENS MISSING NEXT TO FWD COAT CLOSET. REPLACED MISSING RED LENS COVER. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19960126007461996012600746NM 1996 1 26 TAOA129510 119951221A3350100679 LIGHT BOEING727 727254 138408LNM COCKPIT INOPERATIVE A TAOAK NONE L NO TEST ININSP/MAINT 1 EA15915TS 20252 COCKPIT EMERGENCY LIGHT INOP. REPLACED COCKPIT EMERGENCY LIGHT BASE ASSEMBLY. OPERATIONAL CHECK OK. (M) 2L73 4F A3WE 19960126007471996012600747EU 1996 1 26 VTZA96051 119951221A2520K386371 OXYGEN MASK CLIP BAG JETSTMJETSTM3201 1500217EU CABIN BROKEN A VTZAGH O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 EA27494UE 810 FLT NR 6586 - IAD-ISP - DURING CRUISE, DECLARED AN EMERGENCY AND LANDED AT ISP DUE TO THE PRESSURIZATION DUMPING AT 15,000 FT, THE 'CABIN' CAPTION ILLUMINATED, AND THE CABIN OXYGEN MASKS DEPLOYED. THE A/C LANDED AT ISP WITH NO FURTHER INCIDENT. HOWEVER, THE OXYGEN SYSTEM WAS READING 0. MX OPENED DMI NR 42402 IAW MEL 21-14 ON THE PRESSURIZATION SYSTEM, AND DMI NR 42403 IAW MEL 35-1 ON THE OXYGEN SYSTEM. MX LATER CLEARED DMI NR 42403 ON 12-22-95, BY CLEANING THE OUTFLOW VALVE AND ALSO SECURING LOOSE SENSE LINE. OPS CHECK GOOD. CLEARED DMI RN 42403 ON 12-22-95, BY REPLACING SEAT 3BC STOWAGE OXYGEN MASK AND STOWED REMAINING OXYGEN MASKS. OPS CHECK GOOD. A/C WAS RELEASED AND APPROVED FOR RETURN TO SERV. (M)2L72 4T RTA56EU 19960126007481996012600748EU 1996 1 26 WTAA950319 119951211A261251653151 CONTROL UNIT BAG JETSTMJETSTM3101 1500215EU LT ENGINE SHORTED A WTAAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP17403UE 743 SMF - LEFT ENGINE FIRE DETECTION LIGHT REMAINS ILLUMINATED. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT ENGINE FIRE DETECTION CONTROL UNIT. SYSTEM OPERATIONAL CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960126007491996012600749EU 1996 1 26 WTAA950320 119951215A5730 SKIN BAG JETSTMJETSTM3101 1500215EU LT WING LE BIRD STRIKE A WTAAK NONE C F.O.D. NRNOT REPORTED 1 WP17425UE 798 SJC - BIRD STRIKE REPORTED ON LEFT WING LEADING EDGE OF AIRCRAFT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960126007501996012600750SO 1996 1 26 WTAA950321 119951215A7712300054000019 TQ SIG COND EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17280UE 120090 LAX - CREW REPORTED, UNABLE TO OBTAIN MORE THAN 65 PERCENT NP AT 80 PERCENT TORQUE ON LEFT ENGINE AND LEFT ENGINE AUTOFEATHER SYSTEM FAILED TO INDICATE ARMED, DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITION UNIT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960126007511996012600751SO 1996 1 26 WTAA950322 119951212A2731 TRIM CABLE EMB 120 EMB120RT SO AFT FUSELAGE FROZEN A AWTAAO OTHER F FLT CONT AFFECTED CLCLIMB 1 WP17280UE 120090 SFO - CREW REPORTED, ELEVATOR TRIM WOULD NOT MOVE FORWARD OF INDEX NR 1 AT TOP OF CLIMB (22,000 FEET AND OAT-30C). ELEVATOR TRIM OPERATION REPORTED NORMAL AT LOWER ALTITUDES AND ON LANDING (OAT PLUS 15 C). MAINTENANCE FOUND WATER ACCUMULATION AROUND ELEVATOR TRIM CABLES AFT OF PRESSURE BULKHEAD. CLEARED OBSTRUCTION FROM WATER DRAIN, P/N PE9150421, IN AREA AND DRAINED WATER. ELEVATOR TRIM SYSTEM OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960126007521996012600752WP 1996 1 26 WTAA950323 219951223A73208974575 BYPASS VALVE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP RIGHT ENG FUEL FAILED A WTAAA UNSCHED LANDING O OTHER CLCLIMB 1 WP17403UE 743 BFL - RIGHT ENGINE ERRATIC TORQUE INDICATION. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE DETERMINED RIGHT TTL TO BE INOPERATIVE AND DEFERRED PER MEL 76-2. OPENED DMI 81184. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLLY CLEARED DEFERRAL BY REPLACING THE FUEL BYPASS VALVE. (M) 2L72 4T4 TRTA21EU E4WE 19960126007531996012600753EU 1996 1 26 WTAA950324 119951223A56101379141C427 DV WINDOW BAG JETSTMJETSTM3101 1500215EU LT COCKPIT BIRD STRIKE A WTAAK NONE C F.O.D. LDLANDING 1 WP17425UE 798 SFO - BIRD STRIKE REPORTED ON CAPTAINS DV WINDOW ON LANDING. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION AND FOUND CAPTAINS DV WINDOW SCRATCHED. NO OTHER DAMAGE TO AIRCRAFT. REPLACED CAPTAINS DV WINDOW. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960126007541996012600754EU 1996 1 26 WTAA950326 119951229A5101 STRUCTURE BAG JETSTMJETSTM3101 1500215EU AIRFRAME BIRD STRIKE A WTAAK NONE C F.O.D. TOTAKEOFF 1 WP17402UE 734 ACV - BIRD STRIKE REPORTED ON TAKEOFF ROLL AT CEC. AIRCRAFT CONTINUED TO STATION. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960126007741996012600774WP 1996 1 26 ABXA9600037 119951205A57205614759504 BLIND HUCK DOUG DC8 DC863 302198AWP BS 851 IMPROPER INSTL A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED RBL 42, STATION 851 BLIND HUCK IMPROPERLY PULLED. REPAIRED CENTER WING , AFT STRINGER RBL 40.00, BLIND HUCK THAT WAS IMPROPERLY PULLED IAW ABX REA D857-13071MR. 2L74 4F 4A25 19960126007751996012600775WP 1996 1 26 ABXA9600038 119951205A5315 FLOOR BEAM DOUG DC8 DC863 302198AWP BS 824 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED FLOOR BEAM AT STATION 824 AT APPROXIMATELY RBL 36 CORRODED. REPAIRED CORRODED FLOOR BEAM AT STATION 822 AT RBL 36 IAW ABX REA D853-13076MR. 2L74 4F 4A25 19960126007761996012600776WP 1996 1 26 ABXA9600039 119951205A53309754944 SKIN DOUG DC8 DC863 302198AWP BS 1160-1180 IMPROPER REPAIR A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATIONS 1160-1180, LONGERONS 32R-34R, FUSELAGE SKIN HAS A 5.5 INCH BY 3.5 INCH CUT-OUT FROM PREVIOUS REPAIR. REPAIRED STATIONS 1160-1180 FUSELAGE SKIN AND TITANIUM DOUBLER CUT-OUT AT THE AFT LOWER CARGO COMPARTMENT FORWARD DOOR AREA IAW ABX REA D853-12875MR. 2L74 4F 4A25 19960126007771996012600777WP 1996 1 26 ABXA9600040 119951205A5313 LONGERON DOUG DC8 DC863 302198AWP BS 360-420 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED LONGERON 27L, FUSELAGE STATIONS 360-420 HAVE SEVERAL SPOTS OF CORROSION. REPAIRED LONGERON 27L UPPER FLANGE AT FUSELAGE STATION 360 J-420 THAT WAS CORRODED IAW ABX REA D853-12871MR. 2L74 4F 4A25 19960126007781996012600778WP 1996 1 26 ABXA9600041 119951205A5313 LONGERONS DOUG DC8 DC863 302198AWP BS 160/280/1320 DOUBLE DRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED FRAME AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND STATION 1320, LONGERON 7-10L IS DOUBLE DRILLED. REPAIRED FUSELAGE FRAMES WITH DOUBLE DRILLED HOLES AT STATION 160, LONGERON 6-9R, STATION 280, LONGERON 7-10R AND STATION 1320, LONGERON 7-10 IAW ABX REA D853-12862MR. 2L74 4F 4A25 19960126007791996012600779WP 1996 1 26 ABXA9600042 119951205A533057799383 SKIN DOUG DC8 DC863 302198AWP BS 980 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED CORROSION ON SKIN AND FITTING CRACKED OVER LONGERON 24 IN THE LEFT WHEELWELL AT STATION 980. REPAIRED FUSELAGE STATION 980 FITTING AND SKIN THAT WAS CRACKED IN THE LEFT WHEELWELL IAW ABX REA D853-12861MR. 2L74 4F 4A25 19960126007801996012600780WP 1996 1 26 ABXA9600043 119951205A5347 SEAT TRACKS DOUG DC8 DC863 302198AWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED SEAT TRACK ROW 'B' AT STATION 270, MAIN CABIN SEAT TRACK 'F', STATIONS 1590-1630 AND MAIN CABIN SEAT TRACK 'B', STATIONS 1470-1500 CORRODED AND SCALLOPS WORN. FABRICATED TRIPLE SEAT TRACKS FOR STATIONS 270, 1590-1630, AND 1470-1500 THAT WERE CORRODED AND HAD WORN SCALLOPS IAW ABX REA D853-12706MR. 2L74 4F 4A25 19960126007811996012600781WP 1996 1 26 ABXA9600044 119951205A531557735521 FLOORBEAM DOUG DC8 DC863 302198AWP BS 834 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED FLOORBEAM AT STATION 834, LEFT, CORRODED THROUGH AND AROUND 'B' NUT. REPAIRED FUSELAGE STATION 834 FLOORBEAM THAT WAS CORRODED IAW ABX REA D853-12853MR. 2L74 4F 4A25 19960126007821996012600782WP 1996 1 26 ABXA9600045 119951205A5311564101545 FRAME DOUG DC8 DC863 302198AWP BS 1400 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED CORROSION ON FRAME AT STATION 1400, LONGERON 31L TO LONGERON 33R AT AFT CARGO. REPAIRED CORRODED FRAME SPLICE AT FUSELAGE STATION 1400 IAW ABX REA D853-12854MR. 2L74 4F 4A25 19960126007831996012600783WP 1996 1 26 ABXA9600046 119951205A53205641006501 FITTING DOUG DC8 DC863 302198AWP BS 759 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 759, LONGERON 22L, FRAME END FITTING HAS CRACKED. REPAIRED FUSELAGE STATION 759 FRAME END FITTING THAT WAS CRACKED IAW ABX REA D853-12851MR. 2L74 4F 4A25 19960126007841996012600784WP 1996 1 26 ABXA9600047 119951205A78306AL2V2SNTI SKIN DOUG DC8 DC863 302198AWP NR 3 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED NR 3 ENGINE THRUST REVERSER INBOARD SKIN CRACKED AT YN 232. REPAIRED NR 3 THRUST REVERSER INNER SKIN AND FRAME THAT WAS CRACKED AT YN 232 IAW ABX REA D878-12841MR. 2L74 4F 4A25 19960126007851996012600785WP 1996 1 26 ABXA9600048 119951205A573057583826 SKIN DOUG DC8 DC863 302198AWP CTR WING CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 857, RBL 46 HAS PREVIOUS GRIND-OUT FROM CORROSION REMOVAL, APPROXIMATELY 4 INCHES BY 6 INCHES. REPAIRED CENTER WING, UPPER SKIN AT AFT SPAR RBL 46.000 THAT HAD A PREVIOUS GRIND OUT IAW ABX REA D857-12854MR. 2L74 4F 4A25 19960126007861996012600786WP 1996 1 26 ABXA9600049 119951205A5751576313369 SKIN DOUG DC8 DC863 302198AWP RT AILERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED RIGHT OUTBOARD AILERON SKIN AND DOUBLER CRACKED. REPAIRED RIGHT OUTBOARD AILERON NOSE SKIN AND DOUBLER CRACK IAW ABX REA D857-12844MR. 2L74 4F 4A25 19960126007871996012600787WP 1996 1 26 ABXA9600050 119951205A533057503223 SKIN DOUG DC8 DC863 302198AWP BS 1055 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED BLEND-OUT IN BELLY SKIN AT STATION 1055, BETWEEN LONGERON 34L-35L. REPAIRED EXTERIOR BELLY SKIN THAT WAS DAMAGED AT FUSELAGE STATION 1050, LONGERON 34L-35L IAW ABX REA D853-12838MR. 2L74 4F 4A25 19960126007881996012600788WP 1996 1 26 ABXA9600051 119951205A53153774609503 FLOORBEAM DOUG DC8 DC863 302198AWP BS 55 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED MAIN CABIN FLOORBEAMS, ATTACH FITTINGS, GUSSETS AND BRACKETS HAVE CORROSION FROM BL ZERO TO RIGHT CUSP BS 55.000 IN MAIN CABIN. REPAIRED FUSELAGE STATION 55.000 FLOORBEAM THAT HAD AREAS OF CORROSION IN THE MAIN CABIN IAW ABX REA D853-12718MR. 2L74 4F 4A25 19960126007891996012600789WP 1996 1 26 ABXA9600052 119951227A532097596111 CUSP DOUG DC8 DC863 302198AWP BS 1050 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED CUSP AT STATION 1050 LEFT SIDE HAS A DEEP MACHINE GOUGE. REPAIRED CUSP AT FUSELAGE STATION 1050 LEFT SIDE THAT WAS GOUGED IAW ABX REA D853-12141MR. 2L74 4F 4A25 19960126007901996012600790WP 1996 1 26 ABXA9600053 119951227A5311577977211 FRAME DOUG DC8 DC863 302198AWP BS 1060/1100 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 1060 AND 1100 FRAME AT CUSP HAS DOUBLE DRILLED HOLES, ALSO, FRAME END FITTING HAS CORROSION. REPAIRED FUSELAGE FRAMES AT STATION 1060 AND 1100 THAT WERE MISDRILLED IAW ABX REA D853-12715MR. 2L74 4F 4A25 19960126007911996012600791WP 1996 1 26 ABXA9600054 119951227A532056453323 PRESSURE PANEL DOUG DC8 DC863 302198AWP BS 920-940 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATIONS 920-940 AREA BELOW CENTER FLOOR TRACK HAS CORROSION. REPAIRED PRESSURE PANEL AT XCW 0.0, FUSELAGE STATIONS 920-940 IAW ABX REA D853-12711MR. 2L74 4F 4A25 19960126007921996012600792WP 1996 1 26 ABXA9600055 119951227A53115642857511 FRAME DOUG DC8 DC863 302198AWP BS 742 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 742, LONGERON 1-21 RIGHT AND LONGERON 21 LEFT, HAVE DRILLED HOLES AND CORROSION ON FRAMES. REPAIRED FUSELAGE FRAMES AT STATION 742 IAW ABX REA D853-12707MR. 2L74 4F 4A25 19960126007931996012600793WP 1996 1 26 ABXA9600056 119951227A5312 BLKHD STIFFENER DOUG DC8 DC863 302198AWP BS 1766 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED CRACK ON CENTER STIFFENER AT STATION 1766. REPAIRED HORIZONTAL STIFFENER AT AFT PRESSURE BULKHEAD IAW ABX REA D853-12702MR. 2L74 4F 4A25 19960126007941996012600794WP 1996 1 26 ABXA9600057 119951227A5330 WINDOW CUTOUT DOUG DC8 DC863 302198AWP BS 940 ILLEGAL REPAIR A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED AT STATION 940 RIGHT, WINDOW CUT-OUT HAS QUESTIONABLE REPAIR. REPAIRED WINDOW CUT-OUT AT FUSELAGE STATION 940 RIGHT IAW ABX REA D853-12603MR. 2L74 4F 4A25 19960126007951996012600795WP 1996 1 26 ABXA9600058 119951227A53115642500505 FRAME DOUG DC8 DC863 302198AWP BS 702 MISDRILLED HOLESA ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 702, LONGERON 1-21 RIGHT FRAME HAS NUMEROUS DRILLED HOLES AND CORROSION. REPAIRED FUSELAGE STATION 702, LONGERONS 1-21 RIGHT FRAMES THAT HAD NUMEROUS MISDRILLED HOLES AND CORROSION. 2L74 4F 4A25 19960126007961996012600796WP 1996 1 26 ABXA9600059 119951227A5347 SEAT TRACKS DOUG DC8 DC863 302198AWP CABIN CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED SEAT TRACK ROW 'F', STATION 857 ROW 'B', STATION 420, STATION 500, ROW 'C', STATIONS 1470-1490, ROW 'F', STATION 950 AND STATIONS 990-1300 HAVE CORROSION, ARE CHAFED, AND HAVE WORN SCALLOPS. FABRICATED DUAL SEAT TRACKS AT NUMEROUS ROWS AND STATIONS IAW ABX REA D853-12705MR. 2L74 4F 4A25 19960126007971996012600797WP 1996 1 26 ABXA9600060 119951227A5347 SEAT TRACKS DOUG DC8 DC863 302198AWP CABIN WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED MAIN CABIN SEAT TRACK ROW 'F', STATIONS 1590-1630, STATION 270, AND STATIONS 1540-1580, ROW 'B', STATIONS 1470-1500, AND AT STATIONS 45-70, SCALLOPS WORN, NICKS, GOUGES, BULDGE AREAS AROUND FASTENERS. FABRICATED TRIPLE SEAT TRACK AT VARIOUS ROWS AND STATIONS IAW ABX REA D853-12706MR. 2L74 4F 4A25 19960126007981996012600798WP 1996 1 26 ABXA9600061 119951227A532057549240505 DOUBLER DOUG DC8 DC863 302198AWP BS 1050-1350 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED INTERNAL DOUBLER AT STATIONS 1120 TO 1260 HAVE BARE METAL AND CORROSION, ALSO A CUT-OUT AREA OF PREVIOUS REPAIR AT STATION 1170. REPAIRED INTERNAL DOUBLER AT FUSELAGE STATIONS 1050-1350 THAT WAS CORRODED IAW ABX REA D853-12704MR. 2L74 4F 4A25 19960126007991996012600799WP 1996 1 26 ABXA9600062 119951227A53115612142101 FRAME DOUG DC8 DC863 302198AWP BS 1700 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED FRAME AND GUSSET CRACKED AND CORRODED AT STATION 1700 AT LONGERON 21L. REPAIRED CRACKED AND CORRODED FRAMES AND GUSSETS AT LONGERON 21L, STATION 1700 IAW ABX REA D853-12697MR. 2L74 4F 4A25 19960126008001996012600800WP 1996 1 26 ABXA9600063 119951227A53115612142102 FRAME DOUG DC8 DC863 302198AWP BS 1700 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED FRAME REPAIR AT STATION 1700, LONGERON 16R TO LONGERON 21R NOT PER SRM, WRONG HARDWARE, AND EDGE DISTANCE, ALSO, CORROSION AND BARE METAL IN UPPER CARGO AREA. REPAIRED FUSELAGE FRAME AT STATION 1700, LONGERON 21 RIGHT IAW ABX REA D853-12696MR. 2L74 4F 4A25 19960126008011996012600801WP 1996 1 26 ABXA9600064 119951227A57205769759502 DOUBLER DOUG DC8 DC863 302198AWP WS 527 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED RIGHT WING LEADING EDGE INTERIOR DOUBLER CRACKED AT STATION 527, OUTBOARD END OF CENTER LEADING EDGE SECTION. REPAIRED INTERNAL DOUBLER ON RIGHT WING LEADING EDGE AT STATION XRS 527 IAW ABX REA D853-12692MR. 2L74 4F 4A25 19960126008021996012600802WP 1996 1 26 ABXA9600065 119951227A5311 FRAMES DOUG DC8 DC863 302198AWP BS 600-660 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED CIRCUMFERENTIAL FRAMES FROM STATIONS 600 TO 680, FROM CUSP TO LONGERON 1-21 LEFT/RIGHT HAVE SEVERAL MIS-DRILLED HOLES AND FASTENERS WITH DRILLED OFF HEADS. REPAIRED FUSELAGE FRAMES AT STATIONS 600-660, LONGERONS 1-21 LEFT/RIGHT IAW ABX REA D853-12694MR. 2L74 4F 4A25 19960126008031996012600803WP 1996 1 26 ABXA9600066 119951227A57205770138 ANGLE DOUG DC8 DC863 302198AWP WS 207.5 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED LEFT WING STATION 207.500 INBOARD OF STUB WING ANGLE AND NR 3 LEADING EDGE SLAT INBOARD INTERIOR END CRACKED. REPAIRED FORMER ATTACH ANGLE, PYLON STUB WING AT STATION 207.500 IAW ABX REA D857-12693MR. 2L74 4F 4A25 19960202000541996020200054NE 1996 2 2 96ZZZX389 219951218A853055226 VALVE 114649 DOUG DC3 DC3C 3021457WP PWA R1830 R183092 52020NE RT ENG CYL NR 10BROKEN A VLLAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 GL0536AP 846 AR10633 13439 CP352830 ON CLIMB-OUT OF EOK, RT ENGINE STARTED RUNNING ROUGH. DIRECTED TO SPI. FOUND NR 10 CYLINDER, RT ENGINE, WITH BROKEN EXHAUST VALVE. 2L72 4R4 R A669 5E4 19960202000641996020200064NE 1996 2 2 96ZZZX430 219951201A7532 BLEED VALVE DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 3 ENGINE LACK OF LUBE A TC8AC ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL23803MG 45910 SCDA\SCDA - REJECTED TAKEOFF AT 110 KNOTS DUE TO INSUFFICIENT POWER ON NR 3 ENGINE. (1.55 EPR, 96 PERCENT N1). LUBED INTERSTAGE BLEED VALVE, PERFORMED STATIC POWER RUN, ALL ENGINE PARAMETERS NORMAL. BLEED OPS CHECKS NORMAL IAW 75-6-0. 2L74 4F4 F 4A25 1E8 19960202000851996020200085EU 1996 2 2 96ZZZX452 119951024A32405003340 ROTOR DISC 50028053 ISRAEL1124 1124 4500102EU RT MLG CRACKED AP FUBAK NONE O OTHER ININSP/MAINT 1 NE0398WW 167 30521 398 HEAT CRACKS FOUND ON ROTOR DISC OF MAIN LANDING GEAR BRAKE ASSEMBLY IN THE AREA OF THE LIGHTENING HOLES ON THE DISC'S EXTENDED OUT. 2M72 4F A2SW 19960202000861996020200086WP 1996 2 2 96ZZZX453 119951204A5313 STRINGER LKHEED1011 10113851 5265010WP AFT PRESS BLKHD BROKEN A TWAAK NONE O OTHER ININSP/MAINT 1 CE0511006 193B1018 LAX - DURING CHECK C-9C, FOUND AT AFT PRESSURE BULKHEAD, STR 56 SEVERED. REPAIRED BY FITTING/FASTENERS INSTALLATION PER SB 093-53-105. AIRCRAFT TOTAL TIME: 63,490 HOUS; 23,355 CYCLES. 2L73 4F A23WE 19960202000931996020200093SO 1996 2 2 96ZZZX460 119951204A5330 SKIN EMB 120 EMB120RT SO BELLY CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01267UE17279 120071 SPW - DURING REMOVAL OF THE NR 2 NAVIGATOR BELLY ANTENNA, MAINTENANCE FOUND 2 SKIN CRACKS CONCEALED UNDER THE ANTENNA. THE CRACKS WERE REPAIRED IAW EMBRAER SRM 53-20-01. 2L72 4T RTA31SO 19960202001091996020200109EU 1996 2 2 REXA95068 119951130A3233 ACTUATOR BAG JETSTMJETSTM3101 1500215EU RT MLG FAILED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO25300PX 652 RIGHT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED RT ACTUATOR IAW AMM 32-10-3. PERFORMED GEAR SWING, OPS CHECK GOOD. OK FOR SERVICE. (X) 2L72 4T RTA21EU 19960202001101996020200110EU 1996 2 2 REXA95070 119951122A52101371072C DOOR BAG JETSTMJETSTM3101 1500215EU CABIN DAMAGED A REXACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 SO25316PX 687 MAIN PASSENGER DOOR CAME OPEN ON TAKEOFF ROLL. REMOVED AND REPLACED MAIN CABIN DOOR ASSY IAW JS MM 52-10-00. OPS CHECK GOOD. (X) 2L72 4T RTA21EU 19960202001111996020200111EU 1996 2 2 VTZA86039 119951210A326091SE16 SWITCH BAG JETSTMJETSTM3101 1500215EU NLG DIRTY A VTZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA27473UE 828 SWF/BOS - FLT 6174 - DURING TAKEOFF AT 10:00 HOURS ON 12-10-95, RETURNED TO SWF DUE TO THE NOSE GEAR RED INSTRANSIT LIGHT WILL NOT EXTINGUISH WHEN GEAR IS UP AND LOCKED. AIRCRAFT LANDED AT SWF WITH NO FURTHER INCIDENTS. AIRCRAFT WAS THEN FERRIED TO IAD WHERE IT LANDED WITH NO INCIDENTS. MAINTENANCE CLEANED THE UPLOCK MICROSWITCH. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2L72 4T RTA21EU 19960202001121996020200112EU 1996 2 2 VTZA96041 119951214A3260ATG1066 SWITCH BAG JETSTMJETSTM3101 1500215EU NOSE GEAR OUT OF ADJUST A VTZAO OTHER N FALSE WARNING APAPPROACH 1 EA27473UE 828 LYH/IAD - FLT 6186 - DURING APPROACH AT 11:30 HOURS ON 12-14-95, DECLARED AN EMERGENCY DUE TO THE NOSE GEAR RED INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR WAS SELECTED DOWN. AIRCRAFT LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE ADJUSTED NOSE GEAR DOWN MICROSWITCH. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. 2L72 4T RTA21EU 19960202001281996020200128WP 1996 2 2 ABXA9600067 119951227A53115615718505 FRAME DOUG DC8 DC863 302198AWP FS 680 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 680 LONGERON 1 TO 21 LEFT, STATION 600 TO 680 FROM CUSP TO LONGERON 5R HAVE DRILLED HOLES, CORROSION AND FASTENERS WITH DRILLED OFF HEADS. REPAIRED FUSELAGE STATION 680 FRAME IAW ABX REA D853-12695MR. 2L74 4F 4A25 19960202001331996020200133WP 1996 2 2 ABXA9600076 119951029A3231NAS110312 BOLT DOUG DC9 DC931 3022065WP LT MLG DOOR DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND BOLT CAUSING CHAFING ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED BOLT IAW DC-9 SRM 53-01. 2L72 4F A6WE 19960202001341996020200134WP 1996 2 2 ABXA9600077 119951029A5280AZ8625 PLATE DOUG DC9 DC931 3022065WP LT MLG DOOR MISSING A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND CHAFE STRIP MISSING ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR. REPLACED CHAFE STRIP IAW DC-9 SRM 51-20-00. 2L72 4F A6WE 19960202001351996020200135WP 1996 2 2 ABXA9600078 119951029A5280591055725 SEAL DOUG DC9 DC931 3022065WP LT MLG DOOR TORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE OUTBOARD TRAILING EDGE SEAL ON THE LEFT OUTBOARD MAIN LANDING GEAR DOOR TORN. REPLACED SEAL IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19960202001361996020200136WP 1996 2 2 ABXA9600079 119951031A5320575468828 DOUBLER DOUG DC9 DC932 3022066WP RT EYEBROW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47352 DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE RIGHT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-5 AND 51-30-2. 2L72 4F A6WE 19960202001371996020200137WP 1996 2 2 ABXA9600080 119951031A5320575468827 DOUBLER DOUG DC9 DC932 3022066WP LT EYEBROW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23928AX 47392 DURING COMPLIANCE OF AD 90-18-03; SB 56-11 REV 3, FOUND CRACKS AROUND FASTENER HOLES ON THE LEFT OVERHEAD EYEBROW WINDOW CORNER, LEFT SIDE DOUBLER. REPLACED DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202001381996020200138WP 1996 2 2 ABXA9600081 119951018A53205644324 RETAINER DOUG DC9 DC932F 3022067WP BS 110 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23904AX 47040 DURING COMPLIANCE OF AD 90-18-03, FOUND THAT THE LEFT OVERHEAD WINDOW RETAINER WAS CRACKED. REPAIRED WINDOW RETAINER IAW ABX REA D956-13175-MR. 2L72 4F A6WE 19960202001391996020200139WP 1996 2 2 ABXA9600082 119951025A3231NAS130520D BOLT DOUG DC9 DC931 3022065WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE DRIVER ROD END HAD EXCESSIVE PLAY AT THE MAIN LANDING GEAR STRUT. REPLACED ATTACH BOLT IAW DC-9 MM 20-10-0. 2L72 4F A6WE 19960202001401996020200140WP 1996 2 2 ABXA9600083 119951025A52805933787504 HINGE DOUG DC9 DC931 3022065WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED ARTICULATING DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19960202001411996020200141WP 1996 2 2 ABXA9600084 119951025A32315933787502 HINGE DOUG DC9 DC931 3022065WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED ARTICULATING DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19960202001421996020200142WP 1996 2 2 ABXA9600085 119951025A528059338781 HINGE DOUG DC9 DC931 3022065WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED ARTICULATING DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19960202001431996020200143WP 1996 2 2 ABXA9600086 119951025A52805933787506 HINGE DOUG DC9 DC931 3022065WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED ARTICULATING DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19960202001441996020200144WP 1996 2 2 ABXA9600087 119951025A52805910557136 DOOR DOUG DC9 DC931 3022065WP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23944AX 47550 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED ARTICULATING DOOR IAW DC-9 SRM 51-30-2 AND 51-30-1. 2L72 4F A6WE 19960202001451996020200145WP 1996 2 2 ABXA9600088 119951016A5753995760020 ANGLE DOUG DC9 DC932 3022066WP WS 383 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 DURING C-CHECK INSPECTION AND COMPLIANCE OF AD 92-22-08, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202001461996020200146WP 1996 2 2 ABXA9600089 119951016A5753995760016 ANGLE DOUG DC9 DC932 3022066WP WS 383 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE RIGHT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202001471996020200147WP 1996 2 2 ABXA9600090 119951016A5753995760019 ANGLE DOUG DC9 DC932 3022066WP WS 383 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE THE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202001481996020200148WP 1996 2 2 ABXA9600091 119951016A5753995760015 ANGLE DOUG DC9 DC932 3022066WP WS 383 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23986AX 47543 DURING C-CHECK INSPECTION, FOUND BOTH OUTBOARD FLAP HINGE ATTACH BRACKETS CRACKED INSIDE LEFT FLAP. REPLACED BRACKETS IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202001491996020200149WP 1996 2 2 ABXA9600092 119950914A32313923161503 LINKAGE DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 DURING C-CHECK INSPECTION, WHILE ACCOMPLISHING AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ASSEMBLY WORN. REPLACED IAW DC-9 MM 20-10-1 AND DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19960202001501996020200150WP 1996 2 2 ABXA9600093 119950919A57555910055514 PANEL DOUG DC9 DC941 302207NWP RT SPOILER DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD SPOILER PANEL UPPER SURFACE DELAMINATED. REPLACED PANEL IAW DC-9 MM 27-61-1. 2L72 4F A6WE 19960202001511996020200151WP 1996 2 2 ABXA9600094 119950919A573099574992 TE PANEL DOUG DC9 DC941 302207NWP RT WING DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING TRAILING EDGE PANEL DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960202001521996020200152WP 1996 2 2 ABXA9600095 119950109A532059197415 INTERCOSTAL DOUG DC9 DC941 302207NWP BS 503-522 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23952AX 47615 DURING C-CHECK INSPECTION, A FLOOR INTERCOSTAL WAS FOUND CRACKED BETWEEN STR 503 AND 522R. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19960202001541996020200154WP 1996 2 2 ABXA9600097 119951222A57115911301 SPAR CAP DOUG DC9 DC932 3022066WP WS 164 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING C-CHECK INSPECTION, FOUND LEFT WING REAR SPAR LOWER CAP CRACKED AT THE INBOARD FLAP HINGE STA XRS 164. REPAIRED IAW ABX EA NR AD-57-03901-MR. 2L72 4F A6WE 19960202001591996020200159WP 1996 2 2 ABXA9600102 119951222A5720591000643 ANGLE DOUG DC9 DC932 3022066WP WS 48 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING C-CHECK INSPECTION, FOUND LOWER WING TO FUSELAGE ATTACH ANGLE CRACKED, LEFT WING. REPAIRED IAW DC-9 SB 57-103. 2L72 4F A6WE 19960202001601996020200160WP 1996 2 2 ABXA9600103 119951228A57525910051501 TAB DOUG DC9 DC932 3022066WP LT AILERON DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING C-CHECK INSPECTION, FOUND LEFT WING TRIM TAB DENTED. REPLACED TRIM TAB IAW DC-9 MM 27-10-5. 2L72 4F A6WE 19960202001611996020200161WP 1996 2 2 ABXA9600104 119951220A5313591140617 LONGERON DOUG DC9 DC932 3022066WP BS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING C-CHECK INSPECTION, FOUND LONGERON 4L CRACKED AT STA 160. REPAIRED IAW DC-9 SRM 53-02 FIG 2. 2L72 4F A6WE 19960202001621996020200162WP 1996 2 2 ABXA9600105 119951219A5720991932317 ANGLE DOUG DC9 DC932 3022066WP WS 164 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23900AX 47380 DURING C-CHECK INSPECTION, FOUND LOWER LEADING EDGE SKIN SPLICE AT XRS 164 CLIP CRACKED. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960202002001996020200200WP 1996 2 2 UPS805337 119951229A5320459764320 FITTING DOUG DC8 DC873F 302199FWP FS 260 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MAIN CABIN BELT FRAME END FITTING CRACKED AT FS 260 LONG 21R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19960202002011996020200201WP 1996 2 2 UPS805338 119951228A2560459764320 SLIDE DOUG DC8 DC873F 302199FWP PAX DOOR DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, FWD ENT DOOR SLIDE PACK CANVAS GIRT BAR IS TORN AND FRAYED. REPLACED SLIDE ASSY PER MM 25-62-00. 2L74 4F RT4A25 19960202002081996020200208WP 1996 2 2 UPS805346 119951229A57533775904 FLAP TRACKS DOUG DC8 DC873F 302199FWP WS 97 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION PITS ON FLAP TRACKS RT WING STA 97. REPLACED TRACKS PER MM 27-50-03. 2L74 4F RT4A25 19960202002431996020200243NM 1996 2 2 DL72S960162 119951111A57546516221100 RIB BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27408DA 21152 NR 5 RIB CRACKED ON FORWARD FLANGE. REPAIRED PER M/M 57-54-0 FIGURE 809. FOUND DURING SHOP INSPECTION OF NR 5 L/E SLAT. 2L73 4F A3WE 19960202002501996020200250NM 1996 2 2 DL72S960200 119951209A5754651622369 BAFFLE BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27543DA 22392 DURING ROUTINE SHOP INSPECTION, A CRACK WAS FOUND IN THE ANTI-ICE BAFFLE BETWEEN THE 11TH AND 12TH RIB FROM THE I/B END. BAFFLE WAS REPAIRED AS PER MM 57-57-0 FIG 8103A FOR NR 2 L/E SLAT. 2L73 4F A3WE 19960202002571996020200257NM 1996 2 2 DL757960201 119951202A5754 SLAT BOEING757 757232 1384965NM NR 4 LE FLAP DELAMINATION A DALAK NONE O OTHER ININSP/MAINT 1 SO27637DL 23760 DURING INSPECTION OF THE NR 4 SLAT, THE TRAILING EDGE WAS FOUND DAMAGED WITH A DENT AND DELAMINATION OF THE UPPER TRAILING EDGE WEDGE SKIN, DAMAGE MEASURED 6 INCHES FORE/AFT AND 3 INCHES WIDE. ACCOMPLISHED REPAIRS PER DL ERA 302840-14 AD. 2L72 4F RTA2NM 19960202003441996020200344EU 1996 2 2 96ZZZM100 119951204A2731 BUSHINGS SAAB SF340 340B 7860101EU ELEV TAB WORN A NVEAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET CLCLIMB 1 SO03266AE 340B266 FLT NR 5824 - TPA - VIBRATIONS IN CONTROLS DURING CLIMB AND DESCENT, DEACTIVATED YAW DAMPER. REPLACED ELEVATOR TAB BUSHINGS. FUNCTIONAL TEST FLT PASSED. (M) 2L72 4T RTA52EU 19960202003451996020200345EU 1996 2 2 96ZZZM101 119951130A32301859E DNLOCK ACTUATOR 107A703056A BAG JETSTMJETSTM3201 1500217EU NLG FAILED A NVEAABL UNSCHED LANDING EMER. DESCENT ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SO03927AE23 BADL351L 927 FLT NR 4675 - CHA - CREW REPORTED, NOSE GEAR WILL NOT LOCK DOWN AND NOSE INTRANSIT LIGHT REMAINS ON. NO (GREEN) DOWN AND LOCK INDICATION. REPLACED NOSE GEAR DOWNLOCK ACTUATOR S/N LK8201350. (M) 2L72 4T RTA56EU 19960202003471996020200347NM 1996 2 2 96ZZZM103 119951010A33503322037 BATTERY BOEING727 727227 1384078NM CABIN DISCHARGED A AMTAK NONE L NO TEST CRCRUISE 1 GL11767AT 20035 22001 FORWARD SECTION EGRESS LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY, OPS CHECKS NORMAL. (M) 2L73 4F A3WE 19960202003481996020200348NM 1996 2 2 96ZZZM104 119951221A32302240500003 UPLOCK ACT DORNERDO32 DO328100 2996000NM LT MLG DEFECTIVE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07423JS 3032 FLT NR 4118 - SHORTLY AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED 'UP', GEAR INTRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEAR TWICE, INTRANSIT LIGHT STILL REMAINED ILLUMINATED. CREW THEN ELECTED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. CAK MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED A FAULTY LEFT MAIN LANDING GEAR UPLOCK ACTUATOR. REPLACED FAULTY ACTUATOR IAW MM 32-00-00. FUNCTION CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960202003491996020200349EU 1996 2 2 96ZZZM105 119951229A3234 SWITCH ACT BAG JETSTMJETSTM3101 1500215EU CONTROL HANDLE DIRTY A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07853JS 730 LANDING GEAR WARNING HORN CONTINUED TO SOUND AFTER LANDING GEAR WAS RETRACTED, WOULD NOT CANCEL. CREW ELECTED TO RETURN TO FIELD. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED A DIRTY MICROSWITCH ACTUATOR ON THE LANDING CONTROL HANDLE. CLEANED THE MICROSWITCH ACTUATOR IAW MM 32-00-00 AND STD MX PRACTICES. LANDING GEAR SWING CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19960202003511996020200351CE 1996 2 2 96ZZZM107 119951225A3230 RETRACT MECH BEECH 99 C99 1154006CE LANDING GEAR MALFUNCTIONED A GUUAA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 SO19232BH U232 FLT 481 - MIA-FLL - LEFT NOSE GEAR FAILED TO EXTEND MANUALLY. EXTENDED THE GEAR AFTER THREE FAILED ATTEMPTS. AIRCRAFT RETURNED TO MIA. TROUBLESHOT, FOUND NO DEFECTS, SERVICED HYDRAULIC RESERVOIR, CYCLED GEAR 5 TIMES ON JACK. 1L72 3T A14CE 19960202003521996020200352CE 1996 2 2 96ZZZM74 119951209A79104041898051 OIL TANK BEECH 18 G18S 1151010CE LT NACELLE CORRODED A GGPAE ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 NM019210 19206 BA472 AIRCRAFT GOING FROM MWH TO BFI, PILOT NOTICED PROPELLER STARTED TO WANDER AND OIL PRESSURE DROPPED SLIGHTLY, PILOT SHUT DOWN LEFT ENGINE 30 MILES FROM BFI. AIRCRAFT LANDED AT BFI. MECHANIC FOUND LEFT WHEEL WELL FULL OF OIL. MECHANIC FOUND OIL TANK HAD TWO SMALL HOLES IN IT FROM CORROSION. OIL TANK WAS CHANGED AND AIRCRAFT RETURNED TO SERVICE. (M) 1L72 3R A765 19960202003531996020200353CE 1996 2 2 96ZZZM75 119951109A2497 WIRE BEECH 1900 1900C 1154161CE CONSOLE BROKEN A GLBAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE01104GL UC104 ORD - CREW ELECTED AN AIR TURN BACK AFTER MOMENTARY FLASHING AND SPARKING UNDER THE CONSOLE BY PILOTS LEFT FOOT. A BURNED SMELL OF SHORT DURATION FOLLOWED THE FLASHING. MAINTENANCE REPAIRED BROKEN WIRES BEHIND THE GENERATOR SWITCHES. 2L72 4T RTA24CE 19960202003541996020200354CE 1996 2 2 96ZZZM76 119951115A712012991003279 TRUSS BEECH 1900 1900C 1154161CE RT ENGINE CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01159GL1284 1028 UC159 SPW - DURING ROUTINE INSPECTION (REQUIRED BY AD95-02-18), MAINTENANCE FOUND THE ENGINE TRUSS CRACKED ON THE RIGHT SIDE NEAR THE LOWER BOLT HOLE. THE ENGINE TRUSS WAS REPLACED. (M) 2L72 4T RTA24CE 19960202003551996020200355CE 1996 2 2 96ZZZM77 119951114A5520101610000613 ELEVATOR BEECH 1900 1900C 1154161CE LT DAMAGED A GLBAK NONE O OTHER TXTAXI/GRND HDL 1 CE01159GL10432 UC159 DEN - AIRCRAFT NR 159GL AND NR 122GL, CONTACTED ELEVATORS ON THE GROUND. MAINTENANCE REPLACED THE LEFT ELEVATOR DUE TO TIP DAMAGE. 2L72 4T RTA24CE 19960202003561996020200356CE 1996 2 2 96ZZZM78 119951114A5520101610000614 ELEVATOR BEECH 1900 1900C 1154161CE RIGHT DAMAGED A GLBAK NONE O OTHER ININSP/MAINT 1 CE01122GL14362 UC122 DEN - AIRCRAFT NR 159GL AND N122GL, CONTACTED ELEVATORS ON THE GROUND. MAINTENANCE REPLACED THE RIGHT ELEVATOR DUE TO TIP DAMAGE. (M) 2L72 4T RTA24CE 19960202003571996020200357CE 1996 2 2 96ZZZM79 119951129A3230 RETRACT MECH BEECH 1900 1900 1154160CE NLG MALFUNCTIONED A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01719GL UB19 TUS - CREW ELECTED AN AIR TURN BACK AFTER DETERMINING THAT THE NOSE GEAR WOULD NOT RETRACT. MAINTENANCE TROUBLE SHOT AND SERVICED THE GEAR SYSTEM. PERFORMED RETRACTION TESTS WHICH SHOWED NO BINDING, HESITATION, OR OTHER FAULTS. NO FAULT FOUND. 2L72 4T RTA24CE 19960202003581996020200358CE 1996 2 2 96ZZZM80 119951201A32301018100891 BOLT BEECH 1900 1900C 1154161CE RT MLG BROKEN A AGLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE0167UE 4985 UC67 CIU - UPON DEPARTURE FROM APN EN ROUTE TO DTW, THE CREW NOTED THAT THE GEAR HANDLE LIGHT WAS STILL ON. THE GEAR WAS RECYCLED AND THE RIGHT MAIN INDICATION WAS UNSAFE. THE CREW ELECTED TO DIVERT TO CIU. AN EMERENCY WAS DECLARED AND UPON LANDING THE RIGHT MAIN GEAR FAILED TO STAY EXTENDED AND ROTATED TO THE TRAILING POSITION. NO INJURIES OCCURRED. MAINTENANCE SUSPECTS UPPER DRAG BOLT AND DEPARTED. (M) 2L72 4T RTA24CE 19960202003591996020200359CE 1996 2 2 96ZZZM81 119951204A575335165050259 FLAP BEECH 1900 1900C 1154161CE RT WING BIRD STRIKE A GLBAK NONE C F.O.D. CRCRUISE 1 CE01167GL10387 UC167 GBC - WHILE INBOUND TO GBC, THE CREW REPORTED BIRD STRIKES TO THE RHOB WING LEADING EDGE AND THE RHOB FLAP. THE FLAP WAS REPLACED AND THE WING LEADING EDGE WAS REPAIRED IAW BEECH 1900 STRUCTURAL REPAIR MANUAL. 2L72 4T RTA24CE 19960202003601996020200360NM 1996 2 2 96ZZZM82 119951216A33508821004 BATTERY BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 5 WERE FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9510114. 2L72 4F A16WE 19960202003611996020200361NM 1996 2 2 96ZZZM83 119951126A33503322044 CHARGER BOEING757 7572Q8 1384972NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11755AT 025340 24965 BOS - EGRESS LIGHTING SYSTEM INOPERATIVE, ROWS 11-19 AND 24-26. REPLACED BATTERY CHARGER ASSEMBLY FOR EGRESS LIGHTING SYSTEM ROW 11-19 AND 24-26. OPS CHECK NORMAL. (M) 2L72 4F RTA2NM 19960202003621996020200362NE 1996 2 2 96ZZZM84 219951005A7530 BLEED LINKAGE BOEING757 757212 NM RROYCERB211 RB211* 54555NE LT ENGINE WORN A AMTAK NONE O OTHER CRCRUISE 1 GL11750AT 23126 IND - LEFT ENGINE POWER FLUCTUATES AT 9 CONSTANT POWER SETTINGS. FL 27,000, OAT -29, MACH .80, N1 77.8 TO 78.3, EPR 1.03 TO 1.04 EGT 415 TO 418. PERFORMED FIM PROCEDURES PER FIM 73-21-00 FIG 107. FOUND 2.5 BLEED LINKAGE WORN TO .125 INCH ITEM PLACED ON MCI AEE 1400/375. (M) 2L72 4F4 FRTA2NM A12EU 19960202003631996020200363WP 1996 2 2 96ZZZM85 119951214A33503350221 POWER PACK LKHEED1011 10113851 5265010WP CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11192AT 054057 193C1057 MCI - EMERGENCY LIGHTING AT L1 EXTERIOR AND COCKPIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 1L IAW MM 33-51-03, OPS CHECK NORMAL. (M) 2L73 4F A23WE 19960202003641996020200364WP 1996 2 2 96ZZZM86 119950912A25602552032 CLIP LKHEED1011 10113851 5265010WP CABIN BROKEN A AMTAK NONE O OTHER ININSP/MAINT 1 GL11193AT 001906 193C1017 BOS - L-1 GIRT BAR CLIP BROKEN. REPLACED L-1 SLIDE PER M/M 25-61-01, OPS CHECKS NORMAL. (M) 2L73 4F A23WE 19960202003651996020200365WP 1996 2 2 96ZZZM87 119951120A3260 SENSOR LKHEED1011 10113851 5265010WP RT MLG DOOR FAILED A AMTAO OTHER N FALSE WARNING CLCLIMB 1 GL11197AT 193P1082 LAS - RIGHT GEAR, INTRANSIT DOOR/FE ANNUNCIATOR DOOR LIGHT ON. GEAR RETRACTED, GEAR CYCLED ONCE THEN NORMAL INDICATION. TROUBLESHOT IAW FIM 32-61-00. FOUND RIGHT MLG DOOR UPLOCK SENSOR .200 OUT OF LIMITS. ADJUSTED SENSOR IAW MM CHAPTER 32-61-07, OPS CHECK, NORMAL. (M) 2L73 4F A23WE 19960202003661996020200366WP 1996 2 2 96ZZZM88 119951119A3230 RETRACT MECH LKHEED1011 10113851 5265010WP LANDING GEAR MALFUNCTIONED A AMTAO OTHER J WARNING INDICATION CLCLIMB 1 GL11197AT 193P1082 DTW - AFTER TAKEOFF FROM POB GEAR WOULD NOT RETRACT AUTO GROUND SPOILER LIGHT ON AND INTRANSIT LIGHT ON, PERFORMED ABNORMAL SEC 16P13 AND GEAR RETRACT BUT RT GEAR DOOR OPEN. PERFORMED FIM 32-30-00 PG 118, STEP NR 8 SYSTEM CHECKED GOOD. PERFORMED TEST OF FOUR WAY THREE POSITION SOLENOID VALVE SYSTEM CHECKS GOOD IAW 32-31-02, PG 501. (M) 2L73 4F A23WE 19960202003671996020200367NM 1996 2 2 96ZZZM89 119951220A33503322037 BATTERY BOEING727 727264 138408MNM CABIN DISCHARGED A AMTAK NONE L NO TEST TXTAXI/GRND HDL 1 GL11763AT 010303 22983 MDW - EMERGENCY EXIT LIGHTS ROW 11 FORWARD INOPERATIVE. REPLACED BATTERY FOR FLOOR LIGHTING IAW MM 33-50-10. OPS CHECK OK. (M) 2L73 4F A3WE 19960202003681996020200368NM 1996 2 2 96ZZZM90 119951205A33503315086 BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11768AT 21996 DTW - FORWARD EVACUATION SLIDE EMERGENCY LIGHTS INOPERATIVE. REMOVED ADN REPLACED FORWARD EVACUATION SLIDE EMERGENCY LIGHTS BATTERY CHARGER, OPS CHECK GOOD IAW MM CH 33-50-51. (M) 2L73 4F A3WE 19960202003691996020200369NM 1996 2 2 96ZZZM91 119951201A33503322037 BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11772AT 010353 22003 IND - FIVE RED EGRESS LIGHTS AT AFT EXIT DOOR INOPERATIVE. REMOVED AND REPLACED EGRESS LIGHTS BATTERY PACK PER MM 33-50-01, OPS CHECK GOOD. BATTERY PACK BETWEEN AFT LAVS OVERHEAD PANEL. (M) 2L73 4F A3WE 19960202003701996020200370NE 1996 2 2 96ZZZM92 219951128A7261 OIL SYSTEM BOEING727 727227 1384078NM PWA JT8 JT8D7B 52053NE 1/2/3 ENGINES OVERSERVICED A AAMTAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 GL11778AT 22005 IND - FERRY FLIGHT - DURING TAKEOFF, AIRCRAFT FILLED WITH SMOKE, SOURCE UNKNOWN. FOUND ENGINES OVERSERVICED, REFER TO ITEM 7910/665 FOR CORRECT SERVICING, RAN ENGINES, AT TAKEOFF POWER NO SMOKE NOTICED. 2L73 4F4 F A3WE E2EA 19960202003711996020200371NM 1996 2 2 96ZZZM93 119951123A33502410070 BATTERY CHARGER BOEING727 727227 1384078NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11768AT 024731 21996 IND - ON PREFLIGHT, FOUND OVERWING EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER AS REQUIRED, OPS CHECK NORMAL. (M) 2L73 4F A3WE 19960202003721996020200372NM 1996 2 2 96ZZZM94 119951122A33503314024 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11769AT 21998 IND - CABIN EXIT IDENTIFIER INOPERATIVE OVERHEAD ABOVE SEAT. REPLACED EMERGENCY EXIT IDENTIFIER ASSEMBLY, OPS CHECK NORMAL. (M) 2L73 4F A3WE 19960202003731996020200373NM 1996 2 2 96ZZZM95 119951122A33503314030 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11769AT 21998 IND - COCKPIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL. (M) 2L73 4F A3WE 19960202003741996020200374NM 1996 2 2 96ZZZM96 119951123A33503314024 LIGHT BOEING727 727227 1384078NM CABIN INOPERATIVE A AMTAK NONE L NO TEST ININSP/MAINT 1 GL11768AT10845 21996 IND - EMERGENCY LIGHT ASSY INOPERATIVE AT ROW 24. REMOVED AND REPLACED AS REQUIRED, OPS CHECK NORMAL. (M) 2L73 4F A3WE 19960202003751996020200375EU 1996 2 2 96ZZZM97 119951130A3230 DNLOCK ACTUATOR BAG JETSTMJETSTM3201 1500217EU NLG FAILED A NVEAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SO03927AE 927 FLT NR 4675 - CHA - NOSE GEAR WILL NOT LOCK DOWN. NOSE GEAR INTRANSIT LIGHT ON AND NO GREEN INDICATION. REPLACED NOSE GEAR DOWNLOCK ACTUATOR AND HOOK ASSY. (M) 2L72 4T RTA56EU 19960202003761996020200376EU 1996 2 2 96ZZZM98 119951209A3230 UPLOCK ACTUATOR BAG JETSTMJETSTM3201 1500217EU NLG LACK OF LUBE A NVEAO OTHER J WARNING INDICATION APAPPROACH 1 SO03930AE 930 FLT NR 4566 - CMH - CREW REPORTED, WHEN GEAR EXTENDED THEY HAD THREE GREEN DOWN AND LOCK, BUT HAD NO INTRANSIT. LANDED WITH NO INCIDENT. CLEANED AND LUBED NOSE GEAR UPLOCK ACTUATOR. PERFORMED GEAR SWING, ALL GEAR INDICATIONS INDICATE NORMAL. 2L72 4T RTA56EU 19960202003771996020200377EU 1996 2 2 96ZZZM99 119951230A3230 RETRACT MECH SAAB SF340 340B 7860101EU LANDING GEAR MALFUNCTIONED A NVEAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO03269AE 340B269 FLT NR 4804 - YQB - AFTER TAKEOFF SELECTED GEAR UP INTRANSIT LIGHTS ILLUMINATED, BUT GEAR DID NOT COME UP. RETURNED TO YQB. MX FERRIED TO ALB WITH GEAR PINNED FOR REPAIR. COULD NOT DUPLICATE PROBLEM. REPLACED HDYARULIC PUMP AS A PRECAUTIONARY. (M) 2L72 4T RTA52EU 19960202003781996020200378EU 1996 2 2 AALA951992 119951121A5400 RIB FOKKERF28 F28MK0100 4990807EU LT PYLON CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW071447L 11456 TUL - FOUND VERTICLE STRUCTURE RIB CRACKED APPROXIMATELY 1 INCH FROM FORWARD EDGE AFT, NEAR TOP OF RIB. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SRM 51-70-07-R1, PG 201, 202 AND 203. (M) 2L72 4F RT 19960202003791996020200379NM 1996 2 2 AALA952009 119951213A3350 CONNECTOR BOEING767 767323 1385205NM CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07357AA 24038 SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT AT 24H INOPERATIVE. REPAIRED CONNECTOR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960202003801996020200380EU 1996 2 2 AALA952025 119951202A323071540 VALVE HYDROAIRE FOKKERF28 F28MK0100 4990807EU NLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW071400H 1282G 11340 DFW - FLT 1958 - AFTER TAKEOFF FROM DFW, THE NOSE LANDING GEAR WOULD NOT RETRACT. LOWERED LANDING GEAR HANDLE AND RECEIVED THREE GREEN DOWN AND LOCKED LIGHTS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR CONTROL VALVE. ACCOMPLISHED GEAR SWING, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19960202003811996020200381WP 1996 2 2 AALA952027 119951202A3350A3030398101 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07221AA 49172 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202003821996020200382NM 1996 2 2 AALA952043 119951207A5315141T5113 FLOOR BEAM BOEING767 767223 1385123NM BS 325 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07338AA 22335 FOUND FLOOR BEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED AND INSTALLED REPAIR STRAP USING .050 INCH 301.5 HARD STAINLESS STEEL. PRIMED REPAIR STRAP AND FLOOR BEAM APPROVED BY ENGINEERING PER MRB 767-1081. (M) 2L72 4F RTA1NM 19960202003831996020200383NM 1996 2 2 AALA952044 119951207A5730111T3013 SKIN BOEING767 767223 1385123NM CTR WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07338AA 22335 AFW - FOUND UPPER SKIN CORRODED. AFTER BLENDING, FOUND BEYOND LIMITS OF SRM 57-10-01 FIG 101, SQUARE NOTE A. PEENED BLENDED AREAS AND REFINISHED. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1085. (M) 2L72 4F RTA1NM 19960202003841996020200384NM 1996 2 2 AALA952045 119951207A5315141T5114 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07338AA 22335 AFW - FOUND FLOOR BEAM CORRODED. FOUND BEYOND SRM LIMITS AFTER BLENDING. ALODINED AND FILLED BLENDED AREAS. FABRICATED, PRIMED AND INSTALLED REPAIR STRAP USING .063 INCH 7095T6 ALUMINUM. APPROVED BY ENGINEERING AND INSTALLED PER MRB 767-1082. (M) 2L72 4F RTA1NM 19960202003851996020200385NM 1996 2 2 AALA952046 119951207A5315141T5114 FLOOR BEAM BOEING767 767223 1385123NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07338AA 22335 AFW - FOUND CORROSION IN THE VERTICAL FLANGE OF THE FLOOR BEAM. ALODINED ALUMINUM SURFACES. FABRICATED, INSTALLED AND PRIMED REPAIR PARTS. ACCOMPLISHED AND APPROVED BY ENGINEERING PER MRB 767-1084 2L72 4F RTA1NM 19960202003861996020200386NM 1996 2 2 AALA952048 119951206A5522183T3003 SKIN BOEING767 767223 1385123NM RT ELEV DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - ULTRA SOUND INSPECTION INDICATES INTERNAL DELAMINATION 1.7 INCH LONG AND .75 INCH WIDE ON RT ELEVATOR LEADING EDGE LOWER SKIN. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1069. FOLLOW UP INSPECTION AT NEXT MBV. (M) 2L72 4F RTA1NM 19960202003871996020200387NM 1996 2 2 AALA952049 119951206A5315111T5007 FLOOR BEAM BOEING767 767223 1385123NM BS 870 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 FOUND THREE SPOTS OF CORROSION ON FLOOR BEAM TOP CHORD. HOLES WERE DRILLED TO REMOVE THE DEEP CORROSION PER SRM. TWO HOLES ARE 0.090 INCH TOO CLOSE PER SRM. FLOOR BEAM APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1071. (M) 2L72 4F RTA1NM 19960202003881996020200388NM 1996 2 2 AALA952050 119951206A5315141T511 FLOOR BEAM BOEING767 767223 1385123NM BS 287 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - FLOOR BEAM HAS CORROSION ON UPPER SURFACE. ALODINED BLENDED AREA, FILLED BLENDOUT. FABRICATED AND INSTALLED REPAIR STRAP WING .050 INCH 301.5 HARD STAINLESS STEEL. APPLIED PRIMER, APPROVED BY ENGINEERING AND ACCOMPLISHED PER MRB 767-1073. (M) 2L72 4F RTA1NM 19960202003891996020200389NM 1996 2 2 AALA952051 119951206A5320146T80482 DOOR SILL BOEING767 767223 1385123NM BS 1272 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - FOUND AND BLENDED OUT CORROSION ON THE AFT CARGO DOOR OPENING LOWER MAIN SILL UPPER CHORD. FOUND BEYOND SRM LIMITS AFTER BLENDING. INSURED THAT NO FASTENER OR FASTENER HOLE WAS PRESENT. INSURED THAT NO FURTHER CORROSION OR CRACKING WAS PRESENT. REFINISHED AREA PER SRM. APPROVED FOR CONTINUED SERVICE BY ENGINEERING PER MRB 767-1075. (M) 2L72 4F RTA1NM 19960202003901996020200390NM 1996 2 2 AALA952052 119951206A5522183T3002 SKIN BOEING767 767223 1385123NM RT ELEV DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - ULTRASOUND INSPECTION INDICATES .5 INCH DIAMETER INTERPLY DELAMINATION APPROX 50 PERCENT OF ORIGINAL THICKNESS ON THE SKIN APPROX 1 INCH FROM THE LEADING EDGE OF THE RT ELEVATOR. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1068. (M) 2L72 4F RTA1NM 19960202003911996020200391NM 1996 2 2 AALA952053 119951206A5522183T3003 SKIN BOEING767 767223 1385123NM LT ELEV DELAMINATED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - ULTRASOUND INSPECTION INDICATES .5 INCH INTERPLY DELAMINATION IN SKIN APPROX 1 INCH FROM THE L/E OF THE LEFT ELEVATOR. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1070. REINSPECTION AT NEXT MBV. (M) 2L72 4F RTA1NM 19960202003921996020200392NM 1996 2 2 AALA952054 119951206A5330 SKIN BOEING767 767223 1385123NM BS 740 GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - FOUND AND BLENDED SMALL GOUGE IN THE EXTERNAL SURFACE OF THE FUSELAGE SKIN. AFTER BLENDING FOUND THE BLENDOUT EXCEEDS SRM MAX ALLOWABLE LIMITS. INSURED NO FASTENER OR FASTENER HOLE DAMAGE WAS PRESENT. INSURED NO CORROSION OR CRACKING WAS PRESENT. REFINISHED BLENDOUT PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1074. (M) 2L72 4F RTA1NM 19960202003931996020200393NM 1996 2 2 AALA952055 119951206A573011T3013 SKIN BOEING767 767223 1385123NM CTR WING CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07316AA 22318 AFW - WING BOX UPPER SKIN FOUND CORRODED AT AFT DRAIN LOCATION. REMOVED FASTENERS IN CORRODED AREA. REMOVED CORROSION, EDDY CHECKED FOR CRACKS. SPOT FACED FLAP PEENED AREA AND ALODINED. REINSTALLED FASTENER, APPLIED FUEL BARRIER PER AA SPEC P5-54. APPLIED CORROSION INHIBITING COMPOUND PER SRM. APPROVED BY ENGINEERING PER MRB 767-1072. (M) 2L72 4F RTA1NM 19960202003941996020200394NM 1996 2 2 AALA952057 119951207A3397 WIRE BOEING757 757223 1384957NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07613AA 24489 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPAIRED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRING IN FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA2NM 19960202003951996020200395NM 1996 2 2 AALA952061 119951208A3350A3030398101 CONNECTOR BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07701AA 22459 RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960202003961996020200396WP 1996 2 2 AALA952062 119951208A3350A3030398101 CONNECTOR DOUG DC9 DC982 3022082WP CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07207AA 49158 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 4 AND 21 INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202003971996020200397NM 1996 2 2 AALA952063 119951209A3350A3030398101 CONNECTOR BOEING727 727223 1384074NM CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07892AA 22008 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 6 AND 16 INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960202003981996020200398WP 1996 2 2 AALA952064 119951209A3350A3030398101 CONNECTOR DOUG DC9 DC982 3022082WP CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW07429AA 49341 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY FORWARD GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT CONNECTOR BY FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202003991996020200399NM 1996 2 2 AALA952065 119951209A33507024092007 LIGHT BOEING727 727223 1384074NM R1 DOOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07701AA 22459 DFW - DURING OVERNIGHT CHECK, R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R1 DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960202004001996020200400WP 1996 2 2 AALA952079 119951212A5320CPN5468004 SUPPORT DOUG DC10 DC1010 3022110WP BS 1908 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TULE - FOUND CORROSION ON TOP OF SUPPORT, STATION 1908. FABRICATE A U-CHANNEL FROM 2024 T-3, INSTALL UNDER SUPPORT ATTACH WITH .1875 INCH FASTENERS (HI-LOCKS), WITH PR-1422 SEALANT PER ESO-2349, DATED 12-11-95. (M) 2L73 4F A22WE 19960202004011996020200401WP 1996 2 2 AALA952080 119951211A53205468004 SUPPORT DOUG DC10 DC1010 3022110WP BS 1908 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TULE - FOUND CORROSION ON TOP OF FLOOR SUPPORT, BETWEEN NR 7 AND NR 8 SEAT TRACK, STATION 1908. REMOVED DAMAGED FLOOR SUPPORT AND REPLACED WITH NEW PER AARD 51-01-00-05 PG 1. (M) 2L73 4F A22WE 19960202004021996020200402WP 1996 2 2 AALA952084 119951211A2410976J2526 CSD DOUG DC9 DC982 3022082WP LT ENG DEFECTIVE A AALAO OTHER J WARNING INDICATION CRCRUISE 1 SW07468AA 49598 OAK - FLT 1769 - DURING CRUISE, THE LEFT ENGINE FIRE WARNING CAME ON. LEFT THROTTLE WAS RETARDED AND FIRE WARNING EXTINGUISHED. LANDED OAK WITHOUT INCIDENT. REPLACED LEFT CSD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202004031996020200403WP 1996 2 2 AALA952088 119951214A3350A3030398101 CONNECTOR DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07271AA 49293 SFO - DURING OVERNIGHT CHECK, FOUND RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHTS AT 22F INOPERATIVE. REPLACED CONNECTOR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202004041996020200404WP 1996 2 2 AALA952089 119951213A5320 SUPPORT DOUG DC10 DC1010 3022110WP BS 1099 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TULE - FOUND CORROSION ON FLOOR SUPPORT BETWEEN STRINGER 49L AND 49R, STATION 1099. REMOVED AND REPLACED FLOOR SUPPORT PER AARD 51-01-00-5, TREAT AND PAINT. (M) 2L73 4F A22WE 19960202004051996020200405WP 1996 2 2 AALA952090 119951214A5240 SERVICE DOOR DOUG DC10 DC1010 3022110WP BS 795 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TULE - FOUND MID LAVATORY SERVICE DOOR CORRODED ON INSIDE SURFACE. INSTALLED NEW LAVATORY SERVICE DOOR. (M) 2L73 4F A22WE 19960202004061996020200406NM 1996 2 2 AALA952092 119951218A3350A3060819104 STRIP BOEING727 727227 1384078NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07716AA 20608 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960202004071996020200407WP 1996 2 2 AALA952093 119951216A3350P6010006 CHARGER DOUG DC9 DC982 3022082WP CABIN DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07403A 49314 DFW - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT SIDE LIGHTS ABOVE FORWARD LEFT AND RIGHT ESCAPE HATCHES INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202004081996020200408NM 1996 2 2 AALA952096 119951201A5315141T12121 FLOOR BEAM BOEING767 767323 1385205NM BS 347 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07368AA 25195 AFW - FLOOR BEAM AT STATION 347 HAS CORROSION. REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS. MATERIAL REMOVED IS BEYOND SRM LIMITS, PER MRG 767-1069. (M) 2L72 4F RTA1NM 19960202004091996020200409EU 1996 2 2 AALA952100 119951218A3397 WIRE AIRBUS AIRBUS300 A300B4605R 3930308EU CABIN DAMAGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW0725071 514 JFK - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHTING IN CROSS AISLE BETWEEN DOORS 3L AND 3R INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE BETWEEN SEATS 24C AND 27C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960202004101996020200410WP 1996 2 2 AALA952101 119951214A5313 STRINGER DOUG DC10 DC1010 3022110WP BS 1098 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TUL - FOUND CORROSION ON STRINGER 43L, STATION 1098 TO 1110. REMOVED AND REPLACED STRINGER SECTION PER FSO 7349, DATED 12-12-95 AND SRM 51-21-01. (M) 2L73 4F A22WE 19960202004111996020200411WP 1996 2 2 AALA952102 119951215A5720 FITTING DOUG DC10 DC1010 3022110WP LT WS 130 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07151AA 46706 TULE - FOUND CORROSION ON FITTING OUTBOARD OF LEFT GEAR, ATTACHED TO TRUNNION. REMOVED CORRODED FITTING AND REPLACED WITH NEW PART. (M) 2L73 4F A22WE 19960202004121996020200412 1996 2 2 AALA952108 419951220A2565ADH4087 SLIDE BFGOODRICH DOUG DC10 DC1010 3022110WP PAX DOOR FAILED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A4155 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDE HAD POROSITY LEAKS. EMERGENCY EVACUATION SLIDE SCRAPPED. (M) 2L73 4F A22WE 19960202004131996020200413 1996 2 2 AALA952109 419951220A2565ADH4088 SLIDERAFT DOUG DC10 DC1030 3023501WP NR 2 DOOR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07 A2723 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION SLIDERAFT FABRIC BLISTERING. SCRAPPED EMERGENCY EVACUATION SLIDERAFT. (M) 2L73 4F A22WE 19960202004141996020200414NM 1996 2 2 AALA952110 119951220A3350 FUSE BOEING767 767323 1385205NM POWER SUPPLY FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07387AM 27184 MAI - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR LIGHTS AT SEAT ROW 1J TO 9J INOPERATIVE. REPLACED FUSE IN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960202004151996020200415NM 1996 2 2 AALA952111 119951219A3350 FUSE BOEING767 767323 1385205NM POWER SUPPLY FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07380AN 25449 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR LIGHTS INOP, BETWEEN BUSINESS AND COACH. REPLACED FUSE IN EMERGENCY POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960202004161996020200416NM 1996 2 2 AALA952112 119951219A25308609010000 OVEN BOEING767 767223 1385123NM NR 6 OVEN DIRTY A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07329AA 22329 LHR - FLT 156 - DURING CRUISE, THE NR 6 OVEN STARTED TO EMIT SMOKE WHEN IT WAS TURNED ON. TURNED OVEN OFF AND SMOKE DISSIPATED. LANDED WITHOUT INCIDENT. CLEANED DEBRIS FROM BOTTOM OF OVEN, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA1NM 19960202004171996020200417EU 1996 2 2 AALA952116 119951219A2910 SEAL FOKKERF28 F28MK0100 4990807EU RUDDER PACK BLOWN A AALAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW071447L 11456 DFW - FLT NR 1388 - DURING CRUISE, THE HYDRAULIC PRESSURE AND HYDRAULIC QUANTITY WENT TO ZERO. AIRCRAFT MADE AN EMERGENCY LANDING. LANDING WAS OVERWEIGHT BUT LANDED WITHOUT INCIDENT. REPLACED RUDDER HYDRAULIC PACK SEAL AND SERVICED SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19960202004181996020200418WP 1996 2 2 AALA952118 119951220A3350 MODULE DOUG DC9 DC982 3022082WP CABIN FAILED A AALAK NONE L NO TEST ININSP/MAINT 1 SW07485AA 49678 SFO - DURING OVERNIGHT CHECK, FOUND THE EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 22 AND AFT WILL NOT GO OUT. REPAIRED PUSHED BACK PIN AT AB5-4MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F A6WE 19960202004191996020200419EU 1996 2 2 AALA952119 119951220A3350A3060819104 STRIP AIRBUS300 A300B4605R 3930308EU CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW0790070 513 MAI - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT FLOOR PATH LIGHTING AFT OF SEAT ROW 22 ABC INOPERATIVE. RECONNECTED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960202004201996020200420WP 1996 2 2 AALA952125 119951223A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP BS 757-760 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07161AA 46942 TULE - FOUND CORROSION AT STATION 757 TO STATION 760, SEAT TRACK NR 6, UNDER CENTER GALLEY. INSTALLED STRAP DOUBLER PER SRM 53-70-00. (M) 2L73 4F A22WE 19960202004211996020200421WP 1996 2 2 AALA952126 119951223A5347 SEAT TRACK DOUG DC10 DC1010 3022110WP BS 757-760 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07161AA 46942 FOUND CORROSION AT STATION 757 TO STATION 760, NR 5 SEAT TRACK, BELOW MID GALLEY. REPAIRED PER SRM 53-70-00 FIG 2A. (M) 2L73 4F A22WE 19960202004221996020200422NM 1996 2 2 AALA952135 119951223A33501000679 LIGHT GRIMES BOEING727 727223 1384074NM COCKPIT DOR DEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07868AA 21373 BWI - FLT NR 1736 - DURING OVERNIGHT CHECK, COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT INOPERATIVE. REPLACED COCKPIT DOOR EMERGENCY EXIT SIGN/LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A3WE 19960202004231996020200423NM 1996 2 2 AALA952136 119951224A331010614671216 LIGHT PLATE BOEING727 727227 1384078NM F/E PANEL SHORTED A AALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07717AA 20610 MIA-MSY - FLT 1060 - DURING CRUISE, SMOKE NOTED COMING FROM AC POWER SELECTOR LIGHT PLATE PANEL. AIRCRAFT PROCEEDED TO MSY AND LANDED WITHOUT INCIDENT. PLACARDED AC POWER SELECTOR LIGHT PLATE INOPERATIVE. SUBSEQUENTLY, REPLACED AC POWER SELECTOR LIGHT PLATE PANEL AT ORD/24. SYSTEM GROUND CHECKED NORMAL OPERATION AND PLACARD REMOVED. (M) 2L73 4F A3WE 19960202004241996020200424EU 1996 2 2 AALA952137 119951225A3350A3030398101 CONNECTOR AIRBUS300 A300B4605R 3930308EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW0780057 465 MAI - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS INOPERATIVE BETWEEN PAX SEAT ROWS 23 AND 27. REPLACED BROKEN EMERENCY FLOOR LIGHT CONNECTOR BY PAX SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RTA35EU 19960202004251996020200425NM 1996 2 2 AALA952148 119951227A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 824-879 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071754 48489 TULE - FOUND CORROSION ON SEAT TRACK AT STATION 824-879. REPLACED SEAT TRACK FROM STATION 824-879 WITH NEW TRACK PER SRM 53-70-00, PAGES 344, FIG 1 SHEETS 1 AND 2. (M) 2L73 4F RTA22WE 19960202004261996020200426WP 1996 2 2 AALA952152 119951227A5320ADA34123 ANGLE DOUG DC10 DC1010 3022110WP BS 865 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07161AA 46942 TULE - FOUND CORRODED ANGLE AT FWD LOWER CARGO DOOR CUTOUT (AT SLIDING DOOR TRACK). INSTALLED NEW GUSSET AND SPLICED TO THE END OF ANGLE FABRICATED USING ORIGINAL AS TEMPLATE. INSTALLED REPAIR SPLICE ANGLE PER ESO7349, DATED 12-27-95. (M) 2L73 4F A22WE 19960202004271996020200427EU 1996 2 2 AALA952155 119951231A3397 WIRE FOKKERF28 F28MK0100 4990807EU CABIN BROKEN A AALAK NONE L NO TEST ININSP/MAINT 1 SW071413A 11376 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PAX SEAT ROW 21B INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE BY PAX SEAT ROW 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2L72 4F RT 19960202004321996020200432NM 1996 2 2 ASAA9510111 119951214A33501060091102 LIGHT ASSY BOEING737 737210C 1384459NM AIRSTAIR DOOR DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01744AS 21822 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT OVER THE AIRSTAIR DOOR WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A16WE 19960202004331996020200433NM 1996 2 2 ASAA9510113 119951215A33508821004 BATTERY PACK BOEING737 737290C 138448VNM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01740AS 22578 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 5-6 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY (M) 2L72 4F A16WE 19960202004341996020200434NM 1996 2 2 ASAA9510114 119951216A3350883200312 RECEIVER BOEING737 737210C 1384459NM CABIN DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 5 WERE FOUND INOPERATIVE. REPLACED RECEIVER AND BATTERY, LIGHTS OPERATED NORMALLY. (M) 2L72 4F A16WE 19960202004351996020200435 1996 2 2 ASAA9510118 419951228A25651161131 SLIDE BOEING737 737298C 1384490NM L-1 DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS170813110 0765 20794 DURING A-CHECK, THE L-1 EMERGENCY EVACUATION SLIDE PACK PRESSURE WAS FOUND LOW. REPLACED SLIDE ASSEMBLY. VENDOR TEAR DOWN REVEALED LOW BOTTLE PRESSURE. OVERHAULED, HYDROSTATIC TESTED, AND REFILLED BOTTLE. REFERENCE: OPERATOR CONTROL NR 96ZZZX633. (X) 2L72 4F RTA16WE 19960202004361996020200436NM 1996 2 2 ASAA9540108 119951214A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01779AS 25111 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 26 AFT. RECONNECTED TRACK WIRING AT ROW 26 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960202004371996020200437NM 1996 2 2 ASAA9540109 119951215A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 JNU - DURING MAINTENANCE CHECK, TWO SECTIONS OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 1-2 AND 14-15. RECONNECTED LOOSE TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960202004381996020200438NM 1996 2 2 ASAA9540110 119951215A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01776AS 25109 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 18 AND AFT. RECONNECTED LOOSE TRACK WIRING AT ROW 18 AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960202004391996020200439NM 1996 2 2 ASAA9540111 119951222A3244314393 TIRE ASSY BOEING737 7374Q8 NM NR 1 MLG LOST TREAD A ASAAA UNSCHED LANDING D INFLIGHT SEPARATION TOTAKEOFF 1 NM01776AS 5617 25109 SEA - AIR TURN BACK OF FLIGHT 468 - CREW REPORTED, NR 1 MAIN LANDING GEAR TIRE BLEW TREAD ON TAKEOFF. LANDED WITHOUT INCIDENT. REPLACED NR 1 AND NR 2 MAIN LANDING GEAR TIRE AND WHEEL ASSEMBLIES. REPLACED DAMAGED LEFT INBOARD TRAILING EDGE FLAP. REMOVED LEFT MAIN LANDING GEAR INNER DOOR FOR REPAIRS PER CDL 32-10-4, AND PERFORMED INTERIM REPAIR TO LEFT STRUT PER EA 5720-01085. (M) 2L72 4F RTA16WE 19960202004401996020200440WP 1996 2 2 ASAA9580291 119951214A3350 GROUND STUD DOUG DC9 DC982 3022082WP CABIN LOOSE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01951AS 49111 SEA - DURING MAINTENANCE CHECK, BOTH AFT OVERWING EMERGENCY EXIT SIGNS WERE FOUND INOPERATIVE. TIGHTENED LOOSE GROUND STUD AT STATION 965 AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960202004411996020200441WP 1996 2 2 ASAA9680002 119950102A5210 TRIM DOUG DC9 DC983 3022083WP L1 DOOR DETACHED A ASAAK NONE O OTHER TXTAXI/GRND HDL 1 NM01960AS 53074 LAX - AFTER ARRIVAL OF FLT 534 - FLIGHT ATTENDANT REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. FOUND DOOR TRIM DISPLACED AND LOWER INSERT DETACHED. REATTACHED INSERT AND REPOSITIONED TRIM AND OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19960202004421996020200442NE 1996 2 2 C2XA96CL001 219951230A7200 ENGINE AEROSPATR42 ATR42320 8680930EU PWA PW121 PW121 52124NE NR 1 ENG DAMAGED A C2XAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW09198126748 99 121063 GSO - FLT NR 3484 - THE CREW REPORTED WHILE IN CLIMB, THE OIL AND ITT TEMPERATURES BEGAN TO RISE, POWER WAS REDUCED FOLLOWED BY THE NR 1 ENGINE FIRE WARNING. THE NR 1 ENGINE WAS SHUT DOWN AND THE NR 1 FIRE AGENT WAS USED, FIRE WARNING STOPPED WITHIN 30 SECONDS. AIRCRAFT RETURNED TO GSO. MX INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE IAW ATR 42 MM 72-00-00. ALL OPERATIONAL AND LEAKS CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T4 TRTA53EU E20NE 19960202004571996020200457NM 1996 2 2 CAL951064 119951121A326065448105 DNLOCK ACTUATOR BOEING737 737214 138446RNM RT MLG BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0914239 19920 FLT NR 1249 - EWR - THE RIGHT MLG WOULD NOT RETRACT AFTER DEPARTING BDL FOR CLE. THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG DOWNLOCK ACTUATOR BROKEN. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-51. AN ADJUSTMENT/TEST WAS PERFORMED IAW MM 32-32-00, PAGE 501. SYSTEM OPERATION CHECKED GOOD WITH NO LEAKS NOTED. (M) 2L72 4F A16WE 19960202004581996020200458NM 1996 2 2 CAL951120 119951209A3231 MOUNT BOLT BOEING737 7372C0 1384488NM LT MLG DOOR BACKED OUT A ACALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0910242 20071 FLT NR 1727 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND GEAR DOOR FORWARD TOP MOUNT BOLT ON LEFT GEAR BACKED OUT OF HOLE. THE BOLT, NUT, AND WASHER WERE INSTALLED. THE LANDING GEAR WAS SWUNG AND OPERATION CHECKED GOOD. (M) 2L72 4F A16WE 19960202004591996020200459NM 1996 2 2 CAL951142 119951213A3350 BATTERY PACK BOEING737 737130 1384435NM EXTERIOR DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916201 19018 GSO - INSPECTION FOUND BOTH RT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERATION OF THE LIGHTS WAS RESTORED. (M) 2L72 4F A16WE 19960202004601996020200460NM 1996 2 2 CAL951143 119951213A3350 LIGHT BOEING737 737130 1384435NM CABIN INOPERATIVE A CALAK NONE C F.O.D. ININSP/MAINT 1 SW0916201 19018 GSO - INSPECTION FOUND THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED AND REPLACED. (M) 2L72 4F A16WE 19960202004611996020200461NM 1996 2 2 CAL951144 119951213A3350 BATTERY PACK BOEING737 737130 1384435NM CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916201 19018 GSO - INSPECTION FOUND THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 23 INOPERATIVE. THE EMERGENCY EXIT LIGHT BATTERY PACK WAS REMOVED AND REPLACED. (M) 2L72 4F A16WE 19960202004621996020200462NM 1996 2 2 CAL951145 119951213A3350 LIGHT BOEING737 737130 1384435NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0916201 19018 GSO - INSPECTION FOUND THE LEFT OVERWING INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REMOVED, RECHARGED, AND INSTALLED. (M) 2L72 4F A16WE 19960202004631996020200463NM 1996 2 2 CAL951161 119951128A5313 STRINGER BOEING727 727227 1384078NM BS 620 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND A 3 INCH CRACK IN STRINGER 26L IN FORWARD CARGO PIT AT STATION 620. THE CORROSION WAS REMOVED AND THE CRACK WAS STOP DRILLED. REPAIRS WERE DONE IAW SRM 51-40-1, 51-10-6, AND 51-10-3. (M) 2L73 4F A3WE 19960202004641996020200464NM 1996 2 2 CAL951162 119951128A5313 STRINGER BOEING727 727227 1384078NM BS 720 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION ON STRINGER 29R AT STATION 720G. THE CORROSION WAS REMOVED. A REPAIR SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-00 AND 51-20-2. (M) 2L73 4F A3WE 19960202004651996020200465NM 1996 2 2 CAL951163 119951121A5320 STRINGER TIE BOEING727 727227 1384078NM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND STRINGER TIE CORRODED AT BS 740, S28L. A STRINGER HAT CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2, AND 51-30-2. (M) 2L73 4F A3WE 19960202004661996020200466NM 1996 2 2 CAL951165 119951130A5311 FRAME BOEING727 727227 1384078NM BS 1010 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION ON BOTTOM FORWARD SIDE OF FRAME AT BS 1010 AND OUTBOARD SIDE OF S28R. THE CORROSION WAS REMOVED IAW SRM 53-10-1. (M) 2L73 4F A3WE 19960202004671996020200467NM 1996 2 2 CAL951166 119951128A5321 FLOOR BOEING727 727227 1384078NM AFT LAV CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION ON LEFT SIDE OF FLOOR IN AFT LAV AT DUMP TUBE. THE CORRODED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-0. (M) 2L73 4F A3WE 19960202004681996020200468NM 1996 2 2 CAL951167 119951128A5320 INTERCOSTAL BOEING727 727227 1384078NM BS 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION ON LOWER SIDE OF INTERCOSTAL AT FRAME STATION 1130, RBL 25. THE CORODED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-20-2, AND 51-10-2. (M) 2L73 4F A3WE 19960202004691996020200469NM 1996 2 2 CAL951168 119951128A5320 NUT PLATES BOEING727 727227 1384078NM BS 560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION AROUND NUT PLATES IN FORWARD CARGO PIT AT STATION 560, S26R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-1. (M) 2L73 4F A3WE 19960202004701996020200470NM 1996 2 2 CAL951169 119951128A5313 STRINGER BOEING727 727227 1384078NM BS 1148 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION ON STRINGER 26R AT SHEAR TIE ON FORWARD SIDE OF BS 1148 FRAME IN AFT PIT. THE CORRODED SECTION OF STRINGER WAS CUT OUT. A NEW STRINGER SECTION AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-30-2, 51-30-1, AND 51-20-4. (M) 2L73 4F A3WE 19960202004711996020200471NM 1996 2 2 CAL951170 119951130A5330 SKIN BOEING727 727227 1384078NM BS 950 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND SKIN CORRODED AND FOUND POPPED FASTENERS AT BS 950E, WL 138. THE AREA WAS REPAIRED IAW SRM 51-10-1, 51-10-6, AND 51-30-2. (M) 2L73 4F A3WE 19960202004721996020200472NM 1996 2 2 CAL951171 119951128A5330 SKIN BOEING727 727227 1384078NM BS 1052 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION BETWEEN TWO DISHED RIVETS IN LOWER LEFT FUSELAGE SKIN AT BS 1052, S27L. THE CORRODED SECTION OF SKIN WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-10-3. (M) 2L73 4F A3WE 19960202004731996020200473NM 1996 2 2 CAL951173 119951219A3260 CIRCUIT CARD BOEING727 727227 1384078NM E/E COMPT INOPERATIVE A CALAO OTHER N FALSE WARNING APAPPROACH 1 SW0979754 21363 FLT NR 1834 - TPA - THE LEFT AND RIGHT MLG GREEN DOWN AND LOCKED INDICATION LIGHTS DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION ON APPROACH TO TPA. A VISUAL INSPECTION CONFIRMED THE GEAR WAS DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A FAILED MASTER DIM AND TEST MODULE CIRCUIT CARD. THE MASTER DIM AND TEST MODULE CIRCUIT CARD WAS REMOVED AND REPLACED IAW MM 33-15-11. ALL GEAR INDICATIONS CHECKED NORMAL. (M) 2L73 4F A3WE 19960202004741996020200474NM 1996 2 2 CAL951174 119951223A3350 BATTERY BOEING727 727232 1384082NM CABIN INOPERATIVE A CALAK NONE L NO TEST ININSP/MAINT 1 SW0945793 20647 FLT NR 293 - EWR - THE OVERHEAD EMEGENCY EXIT LIGHT AT AFT GALLEY WOULD NOT ILLUMINATE. THE EMERGENCY EXIT LIGHT BATTERY WAS REPLACED AND OPERATION OF THE LIGHT WAS RESTORED. (M) 2L73 4F A3WE 19960202004751996020200475NM 1996 2 2 CAL951175 119951224A2910BACH88B04NN0202 HYD LINE BOEING737 737217 1384464NM NLG LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW0912231 19885 FLT NR 1084 - EWR - THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. MAINTENANCE FOUND THE HYDRAULIC RETURN LINE ON NLG UPLOCK ACTUATOR LEAKING. THE HYDRAULIC LINE WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. THE GEAR WAS SWUNG WITH OPERATION AND INDICATIONS CHECKING GOOD. (M) 2L72 4F A16WE 19960202004761996020200476 1996 2 2 CAL951176 419951223A22104030952906 COUPLER BOEING737 7373T0 1384582NM YAW DAMPER INOPERATIVE A CALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW091333132042 23569 FLT NR 716 - IAH - THE AIRCRAFT WAS EXHIBITING DUTCH ROLL TENDENCY, ESPECIALLY AT ALTITUDE. THERE WAS NO MOVEMENT OF YAW DAMPER INDICATOR NOTED IN FLIGHT. THE FLIGHT WAS UNEVENTFUL. THE YAW DAMPER COUPLER WAS REMOVED AND REPLACED AND THE SYSTEM CHECKED GOOD PER MM 22-12-31. THE FAILURE HAS BEEN CONFIRMED. TEARDOWN FINDINGS REVEALED THE RATE GYRO WAS AT FAULT. (M) 2L72 4F RTA16WE 19960202004771996020200477NM 1996 2 2 CAL951177 119951227A3232731414 DOOR ACTUATOR BOEING727 727224 1384076NM RT MLG INOPERATIVE A CALAO OTHER J WARNING INDICATION CLCLIMB 1 SW09697366199613335 69736 FLT NR 475 - MCO - THE RIGHT GEAR DOOR LIGHT, ON SECOND OFFICERS PANEL AND RED GEAR DOORS LIGHT ON FORWARD PANEL, ILLUMINATED WHEN MOVING THE LANDING GEAR HANDLE FROM UP TO OFF AFTER TAKEOFF. WHEN MOVING THE HANDLE BACK TO UP THE LIGHT EXTINGUISHED AND THE SOUND OF A DOOR CLOSING COULD BE HEARD. MAINTENANCE FOUND THE RIGHT MLG DOOR ACTUATOR AT FAULT. THE DOOR ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-81. OPERATIONAL AND LEAK CHECKS WERE GOOD. (M) 2L73 4F A3WE 19960202004781996020200478WP 1996 2 2 CAL951178 119951228A323359370365501 ACTUATOR DOUG DC9 DC982 3022082WP LT MLG LEAKING A CALAO OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW091481626577 49370 FLT NR 1078 - IAH - THE RIGHT HYDRAULIC QUANTITY DROPPED WITH PRESSURE DROPPING TO ZERO WHILE EN ROUTE FROM COS TO IAH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG RETRACT ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-32-02 AND LEAK CHECK WAS GOOD. (M) 2L72 4F A6WE 19960202004791996020200479WP 1996 2 2 CAL951180 119951228A335041B004AD073 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A CALAK NONE L NO TEST ININSP/MAINT 1 SW09477AC 48062 EWR - INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. THE BATTERIES FOR THE EMERENCY LIGHTS IN FIRST CLASS CABIN WERE REMOVED AND REPLACED AND OPERATION WAS RESTORED. (M) 2L72 4F A6WE 19960202004801996020200480WP 1996 2 2 CAL951181 119951228A361014J93350 CLAMP DOUG DC9 DC982 3022082WP NR 2 ENGINE BROKEN A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0916808 49262 FLT 1263 - CLE - THE NR 2 ENG FIRE WARN LIGHT ILLUMINATED DURING CLIMB-OUT OF CLE. THE FIRE LIGHT WENT OUT FOR ABOUT 1 MIN AFTER LEVELING OFF, AND CAME ON AGAIN FOR ABOUT 15 SEC. THE FIRE WARN WAS ACCOMPANIED BY NR 2 ENG OIL QTY LOSS AND THE CABIN WOULD NOT PRESS. THE A/C WAS RETURNED TO CLE, LANDED W/O INCIDENT. MX FOUND NO EVIDENCE OF FIRE. THE NR 2 ENG 13TH STAGE DUCT CLAMP WAS FOUND BROKEN WITH RESULTANT DAMAGE TO THE NR 2 ENG NOSE COWL AND UPPER COWL, AND THE 13TH STAGE DUCT WAS DENTED. THE NR 2 ENG LOW OIL PRESS SWITCH WAS ALSO DAMAGED AND LEAKING. THE CLAMP, DUCT, NOSE COWL, UPPER COWL, AND OIL PRESS SWITCH WERE R/R. ENG WAS SERVICED WITH OIL AND LK CK WAS GOOD. FIRE DET SYS CHECKED GOOD. (M) 2L72 4F A6WE 19960202004811996020200481NM 1996 2 2 CAL951182 119951230A3260 UPLOCK SENSOR BOEING737 7373T0 1384582NM RT MLG INOPERATIVE A CALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW0947332 23570 FLT NR 0789 - IAH - THE RIGHT MLG RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING IAH. CYCLING THE GEAR DID NOT HELP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MLG UPLOCK SENSOR INOPERATIVE. THE RIGHT MLG UPLOCK SENSOR WAS REMOVED AND REPLACED IAW MM 32-61-21. THE GEAR WAS RETRACTED AND GEAR INDICATION WAS VERIFIED NORMAL. (M) 2L72 4F RTA16WE 19960202004821996020200482NM 1996 2 2 CAL951183 119951128A5313 STRINGER BOEING727 727227 1384078NM BS 500 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND STRINGER 29L CORRODED AT STATION 500. THE STRINGER WAS REPAIRED IAW SRM 53-10-1. (M) 2L73 4F A3WE 19960202004831996020200483NM 1996 2 2 CAL951184 119951125A5311 FRAME BOEING727 727227 1384078NM BS 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND FRAME CORRODED AT LOWER SIDE OF INTERCOSTAL, STATION 1130, RBL 25. THE AREA WAS REPAIRED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960202004841996020200484NM 1996 2 2 CAL951185 119951125A5311 FRAME BOEING727 727227 1384078NM BS 1110 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND UPPER AND LOWER SIDE OF FRAME CORRODED AT FASTENER HOLES, STATION 1110, RBL 14. THE AREA WAS REPAIRED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960202004851996020200485NM 1996 2 2 CAL951186 119951121A5313 STRINGER BOEING727 727227 1384078NM FS 660/680 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND STRINGER CORRODED AT FS 660 AND 680. THE CORROSION WAS REMOVED AND A REPAIR SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-00, 53-10-2, AND 51-10-2. (M) 2L73 4F A3WE 19960202004861996020200486NM 1996 2 2 CAL951187 119951121A5320 BRACKET BOEING727 727227 1384078NM BS 990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND ATTACH BRACKET CORRODED AT STATION 990, STRINGER 30. THE AREA WAS REPAIRED IAW SRM 51-30-2, 51-10-2, AND 51-10-6. (M) 2L73 4F A3WE 19960202004871996020200487NM 1996 2 2 CAL951188 119951126A5311 FRAME BOEING727 727227 1384078NM BS 1130 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION AT BOTTOM FORWARD SIDE OF BS 1130 FRAME, OUTBOARD OF STRINGER 29R IN AFT PIT. THE AREA WAS REPAIRED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960202004881996020200488NM 1996 2 2 CAL951189 119951128A5320 INTERCOSTAL BOEING727 727227 1384078NM BS 950 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND CORROSION AT BOTTOM OUTBOARD SIDE OF INTERCOSTAL, AFT OF BS 950E, STRINGER 28R, IN AFT PIT. THE AREA WAS REPAIRED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960202004891996020200489NM 1996 2 2 CAL951190 119951128A5320 SUPPORT PANEL BOEING727 727227 1384078NM AFT PIT CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW097675248055 21248 INSPECTION FOUND SUPPORT PANEL IN AFT PIT, NR 2 RIGHT. THE AREA WAS REPAIRED IAW SRM 51-10-6. (M) 2L73 4F A3WE 19960202004911996020200491NM 1996 2 2 CAL960002 119950102A3610 8TH STAGE DUCT BOEING727 727224 1384076NM NR 3 ENG RUPTURED A CALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW0993738 20666 FLT NR 680 - MCO - THE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF FROM MLG. THE NR 3 ENGINE THROTTLE WAS REDUCED TO IDLE AND THE FIRE LIGHT EXTINGUISHED. THE AIRCRAFT WAS DIVERTED TO MCO, AS A PRECAUTIONARY MEASURE, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 3 ENGINE 8TH STAGE SADDLE DUCT WAS FOUND RUPTURED. THE 8TH STAGE DUCT WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND OPERATION CHECKED GOOD. (M) 2L73 4F A3WE 19960202004921996020200492NM 1996 2 2 EISA95531 119951213A5311 FRAME BOEING727 72781 1384025NM BS 760.95 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CORROSION, FORWARD SIDE OF CABIN FLOOR BEAM VERTICAL WEB, BS 760.95 LBL 70.5. CUT OUT CORRODED SECTION OF FRAME INSTALLED FRAME KIT PER BOEING DRAWING 65C 36279-36. (M) 2L73 4F A3WE 19960202004931996020200493NM 1996 2 2 EISA95533 119951107A5320 ANGLE BOEING727 72781 1384025NM BS 760 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 HFEC INSPECTION INDICATES CRACKS IN FWD 2 FASTENER HOLES STATION 760, LT. STOP DRILLED CRACKS, HFEC VERIFIES CRACKS CONTAINED. INSTALLED REPAIR PER BOEING DRAWING 65C 33202 AND SB 57-112. (M) 2L73 4F A3WE 19960202004941996020200494NM 1996 2 2 GAIA9525 119951211A323165267616 ACTUATOR ROD BOEING727 727223 1384074NM RT MLG DOOR CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW076827 24092 20180 DURING 'B' CHECK, INSPECTION REVEALED A CRACK ON THE RIGHT MAIN LANDING GEAR DOOR ACTUATOR ROD AT THE ROD END ATTACHMENT. REMOVED AND REPLACED THE ACTUATOR ROD IAW THE BOEING MM CHAPTER 32-12. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L73 4F A3WE 19960202004951996020200495WP 1996 2 2 GAIA9526 119951215A5711 SPAR CVAC 340 34031 2422704WP WS 29 CRACKED A GAIAK NONE O OTHER ININSP/MAINT 1 SW073412 58787 32 DURING C-CHECK INSPECTION, AN 4.5 INCH LONG CRACK WAS FOUND IN THE LT TOP OUTBOARD SPAR RAIL. THE CRACKED SPAR WAS REPAIRED IAW TRACOR SERVICE ENGINEERING REPORT CODE 340/440-57-50 DATED 12/11/95 AND KHAC EA CV-57-25, DATED 12-9-95. AIRCRAFT RETURNED TO SERVICE AFTER C-CHECK INSPECTION. (M) 2L72 4R 6A6 19960202004961996020200496WP 1996 2 2 GAIA9528 119951219A3230 RETRACT MECH DOUG DC9 DC915F 3022037WP LANDING GEAR LACK OF LUBE A GAIAO OTHER J WARNING INDICATION APAPPROACH 1 SW07564PC49750 47062 FLT NR 9535 - PHL-FSD-SEA - ON APPROACH TO FSD, AFTER EXTENDING THE LANDING GEAR THE 'LANDING GEAR DOOR' LIGHT STAYED ON. THE FLIGHT CREW CYCLED THE LANDING GEAR THREE TIMES BEFORE THE GEAR DOOR LIGHT WENT OUT. THE LANDING GEAR DOORS AND THE LANDING GEAR WERE INSPECTED NO DEFECTS NOTED. LUBRICATED LANDING GEAR HINGE POINTS WHERE MOISTURE WAS PRESENT. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A6WE 19960202004971996020200497WP 1996 2 2 IXXA95135 119951221A6120179893 ACTUATOR DOUG DC8 DC863F 302198FWP PITCH TRIM COMP FAILED A IXXAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL23906R 46087 EN ROUTE FROM KLCK TO TJSJ, THE FLIGHT CREW SMELLED THE STRONG ODOR OF ELECTRICAL SMOKE, AND OBSERVED THAT THE PITCH TRIM COMPENSATION LIGHT FLICKERED SEVERAL TIMES. THE PTC WAS TURNED OFF AND ITS CIRCUIT BREAKER PULLED, AT WHICH TIME THE FUMES STOPPED. INSPECTION ON THE GROUND IN TJSJ REVEALED THAT THE PTC ACTUATOR HAD FAILED ELECTRICALLY, PRODUCING THE ELECTRICAL SMELL. THE ACTUATOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4F 4A25 19960202005011996020200501NM 1996 2 2 USAA951356 119951211A5320 INTERCOSTAL BOEING737 737401 1384701NM BS 500/520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND THREE 1-2 INCH CRACKS, BL 0 BS 500 G TO BS 520 INTERCOSTAL. REMOVED, FABRICATED AND INSTALLED NEW UPPER CHORD ANGLE. REPAIRED PER DRAWING 65C34688. (M) 2L72 4F RTA16WE 19960202005021996020200502NM 1996 2 2 USAA951371 119951211A53206545834260 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 312 TO BS 328 INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960202005031996020200503NM 1996 2 2 USAA951404 119951222A532069353521 CLIP BOEING737 7372B7 1384560NM BS 747 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK S-10 L TIE CLIP STATION 747. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M) 2L72 4F A16WE 19960202005041996020200504NM 1996 2 2 USAA951405 119951222A5320 FITTING BOEING737 7372B7 1384560NM BS 727 CRACK A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 727 BULKHEAD STIFFENER ATTACH FITTING BL 0, WL 202.5. REPLACED FITTING. REPAIRED PER EO 5394G176. (M) 2L72 4F A16WE 19960202005051996020200505NM 1996 2 2 USAA951406 119951222A532069353521 CLIP BOEING737 7372B7 1384560NM BS 707 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 3L TIE CLIP STATION 707. REPLACED TIE CLIP, REPAIRED PER EO 5393G227. (M) 2L72 4F A16WE 19960202005711996020200571WP 1996 2 2 UPS805347 119951229A5310 TORQUE BOX DOUG DC8 DC873F 302199FWP FS 1660 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01810UP 46001 MAINTENANCE REPORTED, HEAVY CORROSION MAIN CABIN AT LOWER AFT TORQUE BOX AFT ENTRY DOOR FS 1660, LONG 21L. REPAIRED PER SRM 53-2-0 AND SRM 51-1-20D. 2L74 4F RT4A25 19960202006051996020200605WP 1996 2 2 ABXA9600069 119951227A5311 FRAME DOUG DC8 DC863 302198AWP BS 260 DAMAGED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED STATION 260 FRAME FROM LONGERON 30 LEFT TO LONGERON 35 LEFT FRAME HAS PREVIOUS REPAIR NOT PER SRM. REPAIRED FUSELAGE FRAME AT STATION 260 BETWEEN LONGERON 30 LEFT TO LONGERON 35 LEFT IAW ABX REA D853-12698MR. 2L74 4F 4A25 19960202006061996020200606WP 1996 2 2 ABXA9600070 119951227A5311 FRAME DOUG DC8 DC863 302198AWP BS 1040 ELONGATED HOLE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD-DISCOVERED THAT STATION 1040 HAS OBLONG HOLE, ABOVE LONGERON 29R AFT CARGO PIT. REPAIRED FUSELAGE FRAME 1040 AT LONGERON 29R IAW ABX REA D853-12678MR. 2L74 4F 4A25 19960202006221996020200622WP 1996 2 2 UPS805360 119951229A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1560 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION, CRACK AT FRAME FITTING F.S. 1560, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19960202006231996020200623WP 1996 2 2 UPS805361 119951229A5320 FITTING DOUG DC8 DC871F 302199DWP FS 1580 CORRODED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, CORROSION IN FRAME FITTING F.S. 1580, LONGERON 21R. REPLACED FITTING PER SRM 51-1-20D. 2L74 4F RT4A25 19960209000081996020900008EU 1996 2 9 96ZZZX543 119951207A79200210145040 VALVE AEROSPSA365 SA365N 8680669EU OIL CHECK LEAKING A ZYWAK NONE K FLUID LOSS ININSP/MAINT 1 GL09365SJ K971B 6018 OIL CHECK VALVE BODY LEAKING. REMOVED AND REPLACED CHECK VALVE. 1G72 3U H10EU 19960209000091996020900009EU 1996 2 9 96ZZZX544 119951223A7920365A53131803 LINE AEROSPSA365 SA365N 8680669EU OIL LEAK A ZYWAK NONE K FLUID LOSS ININSP/MAINT 1 GL09365SJ2963 6018 OIL LINE LEAKING THROUGH BRAID. REMOVED AND REPLACED OIL LINE. 1G72 3U H10EU 19960209000271996020900027NE 1996 2 9 96ZZZX562 219950117A73210164248670 FUEL CONTROL AEROSPSA365 SA365N 8680669EU TMECA ARRIELARRIEL1C 60030NE ENGINE FAIL TEST A BTEAK NONE L NO TEST ININSP/MAINT 1 GL09801BA A669B 6008 2158 FCU FAILED MAXIMUM NG CHECK BY MINIMUM OF .8 PERCENT. MINIMUM CHECK OF 101.8 PERCENT MINUS NG EQUALS 101.0 PERCENT. REMOVED FCU FOR REPAIR. 1G72 3U3 U H10EU E19EU 19960209000581996020900058WP 1996 2 9 96ZZZX567 219950726A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LEFT SEIZED A ANVEACEF ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. AJYFLAME/FIRE WARNING INDICATION ENGINE STOPPAGE TOTAKEOFF 1 SO03942AE6830 1036 942 P66258 BNA - FLT 4539 - PILOT REPORTS: ON TAKEOFF, THE LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED FOLLOWED BY A LOUD NOISE FROM THE LEFT ENGINE. DISCHARGED ENGINE FIRE BOTTLES AS A PRECAUTIONARY MEASURE. CREW ABORTED TAKEOFF. AS THEY WERE RETURNING TO THE GATE, THE CFR STOPPED THE A/C AND TOLD CREW THAT THERE WAS RESIDUAL FLAMES. PASSENGERS WERE DEPLANED ON THE RAMP WITH NO INJURIES. C/A - VERIFIED THERE WERE NO FLAMES IN THE ENGINE NACELLE, REPLACED ENGINE FIRE BOTTLES AND LEFT ENGINE. 2L72 4T4 TRTA56EU E4WE 19960209000591996020900059WP 1996 2 9 96ZZZX568 219950726A7200 ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LEFT FAILED A ANVEACEF ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. AJYFLAME/FIRE WARNING INDICATION ENGINE STOPPAGE TOTAKEOFF 1 SO03931AE6830 1036 931 P66258 BNA - FLT 4539 - PILOT REPORTS: ON TAKEOFF, THE LEFT ENGINE FAILED, CAPTAIN LOOKED OUT THE WINDOW AND VERIFIED FLAMES. CREW ABORTED TAKEOFF AND FIRED BOTTLES. UPON TAXIING BACK IN, CFR STOPPED THE A/C AND TOLD THEM THERE WERE STILL RESIDUAL FLAMES. PASSENGER DEPLANED ON THE RAMP WITH NO INJURIES. 2L72 4T4 TRTA56EU E4WE 19960209000631996020900063NM 1996 2 9 AWXA9500820 119951222A3350 COVER BOEING737 7373G7 1384595NM GALLEY LOOSE A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28304AW 24011 LAS - FLT 1512 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHT COVER IN FORWARD GALLEY LOOSE. REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (X) 2L72 4F RTA16WE 19960209000641996020900064NM 1996 2 9 AWXA9500821 119951222A2450 AC POWER BOEING737 7373S3 1384711NM COCKPIT MALFUNCTIONED A AWXAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP28314AW 23733 SNA/SMF - FLT 0230 - AIR TURN BACK. POWER LOSS OF I.R.U., F.M.C.S., AND SYMBOL GENERATOR. RAW NAVIGATION INFORMATION WAS ALSO LOST. CONTRACT MAINTENANCE AND A.W.A. TECHNICIAN SENT TO T/S. DID BITE CHECK ON ALL FAILED COMPONENTS, NO HARD FAULTS. RESET A/C POWER AND ALL SYSTEMS OPS NORMAL. T/S IN AIR MODE AND ENGINES RUNNING. A/C RETURNED TO SERVICE. (X) 2L72 4F RTA16WE 19960209000651996020900065NM 1996 2 9 AWXA9500831 119951230A5330 SKIN BOEING737 7373Y0 1384671NM BS 315-333 DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PAE - FLT 3853 - DURING SCHEDULED C-CHECK INSPECTION, FOUND DENT/SCRATCH 7 INCHES LONG BY .125 INCH DEEP, BELOW AND AFT OF FIRST OFFICER'S SLIDING WINDOW. CUT OUT DAMAGE AND REPAIRED PER SRM AT 53-00-01, 51-40-02, 51-20-05, 51-20-01, BS 315 - BS 333, WL 191, RBL 65. MRR NR 951184. (X) 2L72 4F RTA16WE 19960209000661996020900066NM 1996 2 9 AWXA9500832 119951231A5315BAC1505100617 FLOORBEAM BOEING737 7373Y0 1384671NM BS 986.5 CORRODED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28323AW 23684 PAE - FLT 3853 - DURING SCHEDULED C-CHECK INSPECTION, FOUND CORROSION IN NUTPLATE HOLE AT BS 986.5 BELOW FLOORBEAM. REMOVED DAMAGE ON TOP CORD FROM RBL 26 TO LBL 26 AT BS 986.5 AND REPAIRED PER SRM 53-00-51, FIGURE 202. MRR NR 951186. (X) 2L72 4F RTA16WE 19960209000671996020900067NM 1996 2 9 AWXA95828 119951229A3350831143 INSERT ASSY BOEING757 75723A 1384967NM CABIN BROKEN A AWXAK NONE L NO TEST ININSP/MAINT 1 WP28916AW 24291 ATL/LAS - FLT 0739 - SEAT ROW 34 EMERGENCY FLOOR PROXIMITY LIGHTING INOPERATIVE. INSTALLED MEL 33-51-01 AND AIRCRAFT ROUTED FOR T/S. EMERGENCY LIGHT AT 34C INOPERABLE DUE TO BROKEN ARMREST. INSTALLED ARMREST AND RECONNECTED EMERGENCY LIGHT. OPS CHECK GOOD. MEL REMOVED. (X) 2L72 4F RTA2NM 19960209000771996020900077NM 1996 2 9 CAL951147 119951213A5330 SKIN BOEING737 737130 1384435NM FUSELAGE CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091620165008 19018 GSO - INSPECTION FOUND THE FUSELAGE SKIN AND DOUBLERS CORRODED AT AFT LOWER CORNER OF C-1 DOORWAY. THE CORROSION WAS REMOVED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND ECRA 5330-02343. (X) 2L72 4F A16WE 19960209000831996020900083NM 1996 2 9 IXKA950036 119951220A215039854021 SHUT-OFF VALVE AIRESRCH 3985421 BOEING727 727251 138408HNM LT PACK FAILED A IXKAA UNSCHED LANDING O OTHER CRCRUISE 1 EA25258US P1581 19977 TPA/MDW - FLT 42 - DIVERTED TO ATL WHEN CABIN RATE OF CLIMB WENT TO 1,000 FPM UP, COULD NOT CONTROL RATE IN AUTO OR MANUAL. FOUND LEFT PACK VALVE NOT OPENING. REMOVED AND REPLACED LEFT PACK VALVE, PRESSURIZATION AND OPS CHECK OK PER MM 21-30-0. (X) 2L73 4F A3WE 19960209002161996020900216NM 1996 2 9 DL72S960251 119951128A575465162222 RIB BOEING727 727232 1384082NM NR 6 LE FLAP CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECTION FOR LEADING EDGE SLAT NR 6, RIBS NR 5 AND NR 13 FOUND TO BE CRACKED. REPAIRED RIBS PER M/M 57-54-0 FIG 805. 2L73 4F A3WE 19960209002171996020900217NM 1996 2 9 DL72S960253 119951128A575465162222 RIB BOEING727 727232 1384082NM NR 6 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING SHOP INSPECTION FOR NR 6 LEADING EDGE SLAT, RIBS NR 16 AND NR 18 WERE FOUND TO BE CRACKED. REPAIRED PER MM 57-54-0 FIG 809. 2L73 4F A3WE 19960209003131996020900313EA 1996 2 9 96ZZZX603 219951207A8530 VALVE CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA CYLINDER 1-2 EXHSTICKING A BJFAA UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 EA2355479755 17275191 L1176939A DURING TAKEOFF, AIRCRAFT ENGINE BECAME VERY ROUGH. PILOT COULD NOT DUPLICATE ON GROUND. FURTHER INVESTIGATION FOUND NR 1 AND NR 2 CYLINDER EXHAUST VALVES STICKING. REMOVED AND CLEANED ALL FOUR CYLINDER EXHAUST VALVES AND GUIDES. THIS IS SECOND OCCURRENCE WITH THIS ENGINE. 1H71 3O3 ONT3A12 E274 19960209003391996020900339NM 1996 2 9 DL72S954636 119951206A5520 ELEVATOR BOEING727 727232 1384082NM RIGHT DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27484DA 20864 DURING SHOP INSPECTION, RT ELEVATOR WAS RESTORED PER SRM 55-20-3. 2L73 4F A3WE 19960209003431996020900343NM 1996 2 9 DL757960034 119951118A5754114N4005183A TE WEDGE BOEING757 757232 1384965NM LT LE FLAP WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27683DA 27103 DURING SHOP INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH TRAILING EDGE WEDGE WORN AND GOUGED. REPAIRED WEDGE PER SRM 51-70-10. 2L72 4F RTA2NM 19960209003471996020900347WP 1996 2 9 DLL13960047 119951202A57111527093 REAR SPAR LKHEED1011 10113851 5265010WP WING CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27788DL 193A1141 CRACKS WERE FOUND ON THE REAR SPAR UPPER CAP AND THE UPPER WING-S IN EMANATING FROM THE BAY 8 ROW 6B FATSENER. DAMAGE FOUND WHILE ACCOMPLISHING ME-04 OF SI 7-63370-12AD. 2L73 4F A23WE 19960209003931996020900393NM 1996 2 9 DL72S960277 119950601A5751657273411W SKIN BOEING727 727232 1384082NM RT AILERON DENTED A DALAK NONE O OTHER ININSP/MAINT 1 SO27477DA 20754 DURING SHOP INSPECTION OF THE RT O/B AILERON, FOUND NR 0244, LOWER I/B SKIN BENT AND OVERSIZED HOLES. REPAIRED PER SRM 57-51-0. NR 9588, TOP SKIN HAS NUMEROUS OVERSIZED HOLES AND DENT. REPAIRED BY REPLACING SKIN. NR 9587, LOWER SKIN O/B 24 HAS MANY OVERSIZED HOLES. REPAIRED PER SRM 57-50-0. 2L73 4F A3WE 19960209004221996020900422NM 1996 2 9 96ZZZM108 119951211A532065317876 ANGLE BOEING737 737401 1384701NM BS 302-362 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE Z-ANGLE. REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. REFERENCE USAA951365. 2L72 4F RTA16WE 19960209004301996020900430WP 1996 2 9 96ZZZM116 119951017A5713 STRINGER DOUG DC8 DC863 302198AWP BS 1190-1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT STRINGER 34R BETWEEN STATION 1190 AND 1200 INSIDE OF C-3 CARGO. REMOVED CORROSION TREATED AND PRIMED AREA. INSTALLED NEW FITTING PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004311996020900431WP 1996 2 9 96ZZZM117 119951226A5320 CHANNEL DOUG DC8 DC863 302198AWP BS 1600 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1600 RIGHT FROM FUSELAGE TO INBOARD TRACK 3 CHANNELS WITH CORROSION AT CLIP NUTS. REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED REPAIR PER SRM 53-2-3. (M) 2L74 4F 4A25 19960209004321996020900432WP 1996 2 9 96ZZZM118 119951226A5320 FRAME DOUG DC8 DC863 302198AWP WINDOW FRAME CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT AFT EMERGENCY EXIT DOOR WINDOW HAS HEAVY SCRATCHES. FOUND CORROSION UNDER WINDOW. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER DRAWING 085330-5115, AND INSTALLED WINDOW. (M) 2L74 4F 4A25 19960209004331996020900433WP 1996 2 9 96ZZZM119 119951226A5311 FRAME DOUG DC8 DC863 302198AWP BS 1338 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1338 LEFT SIDE AFT OF EMERGENCY CIRCUMFERENTIALS, FRAMES AND CUSP HAVE CORROSION. REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED REPAIR PER RIA DRAWING 45931-2. (M) 2L74 4F 4A25 19960209004341996020900434WP 1996 2 9 96ZZZM120 119951226A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1746-1700 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1746 RIGHT TO 1700 RIGHT STRINGER 22, HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 535-20-0. (M) 2L74 4F 4A25 19960209004351996020900435WP 1996 2 9 96ZZZM121 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 727 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SURFACE STATION XRS 727 AT STRINGER 5 HAD CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-7. (M) 2L74 4F 4A25 19960209004361996020900436WP 1996 2 9 96ZZZM122 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 693 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SURFACE HAS CORROSION AT STATION 693 STRINGER 3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-7. (M) 2L74 4F 4A25 19960209004371996020900437WP 1996 2 9 96ZZZM123 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 106 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SURFACE AT XW 106 NEAR AFT SPAR HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-1. (M) 2L74 4F 4A25 19960209004381996020900438WP 1996 2 9 96ZZZM124 119951226A5330 SKIN DOUG DC8 DC863 302198AWP BS 680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, FOUND CORROSION ALONG SKIN JOINT STATION 680 TOP OF FUSELAGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. (M) 2L74 4F 4A25 19960209004391996020900439WP 1996 2 9 96ZZZM125 119951226A5320 SUPPORT DOUG DC8 DC863 302198AWP BS 1680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, FOUND CORROSION AT CABIN FLOOR STATION 1680 RT SUPPORT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004401996020900440WP 1996 2 9 96ZZZM126 119951226A5347 FLOOR TRACK DOUG DC8 DC863 302198AWP FS 1240-1380 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT NR 3 RIGHT SIDE FLOOR TRACK ABOVE STRINGER 33R HAS CORROSION FROM FS 1240 TO FS 1380. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW FLOOR TRACK PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004411996020900441WP 1996 2 9 96ZZZM127 119951227A5347 SEAT TRACK DOUG DC8 DC863 302198AWP BS 1620-1580 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR INBOARD SEAT TRACK STATION 1620 - STATION 1580 RIGHT HAS CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-3. (M) 2L74 4F 4A25 19960209004421996020900442WP 1996 2 9 96ZZZM128 119951227A5320 HAT CHANNEL DOUG DC8 DC863 302198AWP BS 1600-1500 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1600 RIGHT TO 1500 RIGHT HAT CHANNEL HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-01-8. (M) 2L74 4F 4A25 19960209004431996020900443WP 1996 2 9 96ZZZM129 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP BS 1490 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION ON ATTACH FINGER DOUBLER BETWEEN STRINGERS 34L AND 36 AT STATION 1490. REMOVED DOUBLER, CLEANED AND TREATED AREA, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004441996020900444WP 1996 2 9 96ZZZM130 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP BS 1350 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, SEVERAL SPOTS OF CORROSION AND TORN METAL AT FASTENER HOLES ON SKIN ATTACH FINGER DOUBLER AT STATION 1350 BETWEEN STRINGERS 31L AND 31R. REMOVED DOUBLER CLEANED AND TREATED AREA, FABRICATED AND INSTALLED NEW DOUBLER. (M) 2L74 4F 4A25 19960209004451996020900445WP 1996 2 9 96ZZZM131 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP NR 4 CARGO DOOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION ON DOUBLER SKIN AROUND NR 4 CARGO DOOR OPENING. REMOVED AND REPLACED DOUBLER PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004461996020900446WP 1996 2 9 96ZZZM132 119951227A5522565497047 SKIN DOUG DC8 DC863 302198AWP LT ELEVATOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LEFT ELEVATOR LOWER SKIN SURFACE PANELS PITTED AND CORRODED FROM INBOARD TO OUTBOARD END. REMOVED, REPAIRED AND REINSTALLED PANELS PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004471996020900447WP 1996 2 9 96ZZZM133 119951227A5311 CIRCUMFERENTIAL DOUG DC8 DC863 302198AWP BS 980 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT CIRCUMFERENTIAL AT STATION 980 FROM 32L TO 32R INSIDE C3 CARGO COMPARTMENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5. (M) 2L74 4F 4A25 19960209004481996020900448WP 1996 2 9 96ZZZM134 119951227A5320 SUPPORT DOUG DC8 DC863 302198AWP BS 1680-1660 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR SUPPORT FROM STATION 1680 RT TO 1660 RT NEXT TO DOOR FRAME LOWER END HAS CORROSION. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (M) 2L74 4F 4A25 19960209004491996020900449WP 1996 2 9 96ZZZM135 119951227A5330 SKIN DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT AFT GALLEY DOOR CUT OUT LOWER AREA SKIN CORRODED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER RICH DRAWING NR 45931-4. (M) 2L74 4F 4A25 19960209004501996020900450WP 1996 2 9 96ZZZM136 119951227A5753 SKIN DOUG DC8 DC863 302198AWP LT TE FLAP CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LEFT WING FLAP INBOARD LOWER SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-21. (M) 2L74 4F 4A25 19960209004511996020900451WP 1996 2 9 96ZZZM137 119951228A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1230 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT STRINGER 22R STATION 1230. REMOVED STRINGER TIE, REMOVED CORROSION, FABRICATED AND INSTALLED ANGLE REPAIR, REINSTALLED STRINGER TIE. (M) 2L74 4F 4A25 19960209004521996020900452WP 1996 2 9 96ZZZM138 119951228A5320 SILL DOUG DC8 DC863 302198AWP CARGO DOOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, SECOND FORWARD CARGO DOOR FRAME LOWER SILL PLATE SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 51-1-8. (M) 2L74 4F 4A25 19960209004531996020900453WP 1996 2 9 96ZZZM139 119951228A5330 SKIN DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, SKIN PLATE BULGED BELOW NR 2 CARGO DOOR. REMOVED SKIN PLATE. REMOVED DAMAGED AREA UNDER SKIN PLATE, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1 AND REINSTALLED PLATE. (M) 2L74 4F 4A25 19960209004541996020900454WP 1996 2 9 96ZZZM140 119951229A5320 HAT CHANNEL DOUG DC8 DC863 302198AWP BS 1680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR AT STATION 1680L INBOARD HAT CHANNEL HAS CORROSION. REMOVED, REPAIRED AND REINSTALLED HAT CHANNEL SECTION PER SRM 51-1-19. (M) 2L74 4F 4A25 19960209004551996020900455WP 1996 2 9 96ZZZM141 119951229A5320 SILL DOUG DC8 DC863 302198AWP BS 1660 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN AREA STATION 1660 LEFT AFT PASSENGER DOOR FRAME LOWER AREA OF SILL PLATE HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-10-01. (M) 2L74 4F 4A25 19960209004561996020900456WP 1996 2 9 96ZZZM142 119951229A5330 SKIN DOUG DC8 DC863 302198AWP BS 1762 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION ON SKIN ALONG STRINGER 28L AT STATION 1762. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004571996020900457WP 1996 2 9 96ZZZM143 119951229A5520 STRUCTURE DOUG DC8 DC863 302198AWP LT ELEVATOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LEFT ELEVATOR LOWER SURFACE FRAME STRUCTURE IS CORRODED. REMOVED FABRICATED AND INSTALLED BRACKET PER SRM 51-1-0. (M) 2L74 4F 4A25 19960209004581996020900458WP 1996 2 9 96ZZZM144 119951229A5532 SKIN DOUG DC8 DC863 302198AWP VERT STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, VERTICAL STABILIZER LEADING EDGE SEGMENT NR 1 UPPER END HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M) 2L74 4F 4A25 19960209004591996020900459WP 1996 2 9 96ZZZM145 119951229A5532 LE CAP DOUG DC8 DC863 302198AWP VERT STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LOWER END OF NR 2 VERTICAL STABILIZER LEADING EDGE CAP IS CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M) 2L74 4F 4A25 19960209004601996020900460WP 1996 2 9 96ZZZM146 119951229A5321 FLOOR DOUG DC8 DC863 302198AWP BS 1260-1280 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR AT STATION 1260R TO 1280R CUSP HAS CORROSION. REMOVED DAMAGED AREA, INSTALLED NEW FITTING (P/N 464016501N) PER SRM 53-1-0. (M) 2L74 4F 4A25 19960209004611996020900461WP 1996 2 9 96ZZZM147 119951229A5311 CIRCUMFERENTIAL DOUG DC8 DC863 302198AWP BS 1140 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION ON CIRCUMFERENTIAL AT STATION 1140 FROM 32L TO 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-02-0. (M) 2L74 4F 4A25 19960209004621996020900462WP 1996 2 9 96ZZZM148 119951229A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1190-1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT STRINGER 34R BETWEEN STATION 1190 AND 1200 INSIDE C3 CARGO. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE FITTING PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004631996020900463WP 1996 2 9 96ZZZM149 119951229A2550 NET TRACK DOUG DC8 DC863 302198AWP BS 980-1170 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, C-3 CARGO RIGHT SIDE BARRIER NET TRACK HAS CORROSION FROM STATION 980 TO 1170 BETWEEN STRINGER 32R AND 33R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR. (M) 2L74 4F 4A25 19960209004641996020900464WP 1996 2 9 96ZZZM150 119951229A5320 CHANNEL DOUG DC8 DC863 302198AWP BS 1338-1390 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, NR 3 CARGO COMPARTMENT FLOOR CHANNEL HAS CORROSION BETWEEN STRINGER 30 AND 31 AT STATIONS 1338 TO 1390. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-0. (M) 2L74 4F 4A25 19960209004651996020900465WP 1996 2 9 96ZZZM151 119951229A5330 SKIN DOUG DC8 DC863 302198AWP BS 438/456 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, SKIN BULGED ALONG STRINGER 31L BETWEEN STATIONS 438 AND 456. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. (M) 2L74 4F 4A25 19960209004661996020900466WP 1996 2 9 96ZZZM152 119951229A5512 SKIN DOUG DC8 DC863 302198AWP LT HORIZ STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LEADING EDGE SKIN IS CORRODED AROUND FASTENERS 144 INCHES OUTBOARD OF INBOARD END. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. (M) 2L74 4F 4A25 19960209004671996020900467WP 1996 2 9 96ZZZM153 119951229A5730 PANEL DOUG DC8 DC863 302198AWP RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER LEADING EDGE PANEL AFT OF NR 3 PYLON HAS CORROSION AT ATTACH POINTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. (M) 2L74 4F 4A25 19960209004681996020900468WP 1996 2 9 96ZZZM154 119951229A5730 PANEL DOUG DC8 DC863 302198AWP WS 585-659 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER LEADING EDGE OUTBOARD OF NR 4 PYLON HAS SURFACE CORROSION AT ATTACH POINT XFS STATION 585-659. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. (M) 2L74 4F 4A25 19960209004691996020900469WP 1996 2 9 96ZZZM155 119951229A5730 SKIN DOUG DC8 DC863 302198AWP WS 659-993 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING OUTBOARD LEADING EDGE UPPER SURFACE AT ATTACH POINTS HAS SURFACE CORROSION AT STATION XFS 659-993. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. (M) 2L74 4F 4A25 19960209004701996020900470WP 1996 2 9 96ZZZM156 119951229A5313 STRINGER DOUG DC8 DC863 302198AWP BS 438-456 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, SKIN BULGED ALONG STRINGER 31L BETWEEN STATIONS 438 AND 456. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED STRINGER SPLICE PER SRM 53-4-1. (M) 2L74 4F 4A25 19960209004711996020900471WP 1996 2 9 96ZZZM157 119951229A5320 ANGLE DOUG DC8 DC863 302198AWP BS 1600 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1600 LEFT SUPPORT CHANNEL BETWEEN INBOARD LEFT SEAT TRACK AND HAT HAS CORROSION. REMOVED AND REPLACED Z-ANGLE SUPPORT SECTION BETWEEN INBOARD SEAT TRACK AND HAT SECTION PER SRM 51-1-8. (M) 2L74 4F 4A25 19960209004721996020900472WP 1996 2 9 96ZZZM158 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1440 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1440 LEFT CIRCUMFERENTIAL FRAME HAS CORROSION AROUND CUSP AREA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004731996020900473WP 1996 2 9 96ZZZM159 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1360 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, LEFT SIDE OF FUSELAGE CIRCUMFERENTIAL AT STATION 1360 STRINGER 26L HAS CORROSION ON FRAME. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004741996020900474WP 1996 2 9 96ZZZM160 119951229A5320 DOUBLER DOUG DC8 DC863 302198AWP BS 1186 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT STRINGER 36 AT STATION 1186 INSIDE C3 CARGO. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5. (M) 2L74 4F 4A25 19960209004751996020900475WP 1996 2 9 96ZZZM161 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1200 LEFT CIRCUMFERENTIAL FRAME AND CUSP HAVE CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. (M) 2L74 4F 4A25 19960209004761996020900476WP 1996 2 9 96ZZZM162 119951229A5730 SKIN DOUG DC8 DC863 302198AWP WS 763 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SKIN CORROSION BLENDED OUT OF LIMITS AT XRS 763 STRINGER 4. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING NR RGH459318. (M) 2L74 4F 4A25 19960209004771996020900477WP 1996 2 9 96ZZZM163 119951229A5347 TRACK DOUG DC8 DC863 302198AWP FS 1240 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT PIT NR 3 LEFT SIDE FLOOR TRACK ABOVE STRINGER 33L HAS CORROSION FROM FS 1240 TO 1380. REMOVED DAMAGED SECTION OF TRACK AND REPLACED. (M) 2L74 4F 4A25 19960209004791996020900479WP 1996 2 9 ASAA9580296 119951222A3350L201913 LIGHT DOUG DC9 DC982 3022082WP CATWALK DEFECTIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01955AS 48080 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT IN THE CATWALK WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960209004801996020900480WP 1996 2 9 ASAA9580297 119951226A335041B004AD07G3 BATTERY DOUG DC9 DC983 3022083WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01945AS 49643 SEA - DURING MAINTENANCE CHECK, THE AFT TWO OVERHEAD EMERGENCY EXIT LIGHTS AND ONE OF THE EMERGENCY TAIL CONE LIGHTS WERE FOUND INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA6WE 19960209004811996020900481WP 1996 2 9 ASAA9580298 119951228A3350S103 BATTERY DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01954AS 49387 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHT AT ROWS 29-31 WERE FOUND INOPERATIVE. REPLACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F A6WE 19960209004821996020900482WP 1996 2 9 ASAA9580299 119951230A335041B004AD07G3 BATTERIES DOUG DC9 DC982 3022082WP CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01937AS 49364 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) 2L72 4F A6WE 19960209004901996020900490WP 1996 2 9 CKSA95166 119951220A3260189915 PROX SWITCH DOUG DC8 DC863F 302198FWP GEAR DOORS DIRTY A CKSAO OTHER N FALSE WARNING CLCLIMB 1 GL23815CK33877 46151 KORD-KLAX - LANDING GEAR WAS SELECTED UP AFTER TAKEOFF, THE DOORS LIGHT CAME ON. CYCLED GEAR, LIGHT WENT OUT. GOOD UPLATCH CHECK. CLEANED PROXIMITY SWITCHES FOR DOORS. CHECKED CONNECTIONS, NO DISCREPANCIES NOTED AT THIS TIME. CHECKS NORMAL IAW MM 32-12-1. (M) 2L74 4F 4A25 19960209004911996020900491NM 1996 2 9 EISA95507 119951213A5311 FRAME BOEING727 72781 1384025NM BS 620 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FRAME STATION 620 HAS DRILLED HOLES DAMAGE AT RADIUS OF THE FRAME, STRINGER 8R. FABRICATED DOUBLER AND INSTALLED PER SRM 51-40-03. (M) 2L73 4F A3WE 19960209004921996020900492NM 1996 2 9 EISA95508 119951213A5712 RIB BOEING727 72781 1384025NM WS 486.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 RIGHT WING RIB CRACKED WHERE IT ATTACHES TO LOWER STRINGER AT WS 486.5. FABRICATED REPAIR CHANNEL AND INSTALLED PER SRM 51-10-05. (M) 2L73 4F A3WE 19960209004931996020900493NM 1996 2 9 EISA95509 119951213A5311 FRAME BOEING727 72781 1384025NM BS 950-1160 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 UPPER FLANGES OF FRAMES ARE CORRODED WHERE SIDEWALL LOWER ATTACH STRIP BOLTS TO TOP OF FRAMES RIGHT SIDE, FROM STATION 950 TO STATION 1160. REMOVED CORROSION, FABRICATED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER PER SRM 51-10-07. (M) 2L73 4F A3WE 19960209004941996020900494NM 1996 2 9 EISA95510 119951213A5311 FRAME BOEING727 72781 1384025NM BS 1070 CRACKED A EISAO OTHER Z SIGNIFICANT FAILURE REPORT ININSP/MAINT 1 SW07110NE 18952 AT STATION 1070 ABOVE STRINGER 27L, UPPER FLANGE OF FRAME IS CRACKED AT BOLT HOLE. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER. INSTALLED REPAIR PER SRM 53-10-04. (M) 2L73 4F A3WE 19960209004951996020900495NM 1996 2 9 EISA95511 119951213A5712 RIB BOEING727 72781 1384025NM WS 656.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 TWO INCH CRACK IN RIGHT WING RIB NEAR LOWER FASTENER HOLE WS 656.5 AND SECOND STRINGER AFT OF FRONT SPAR. FABRICATED REPAIR CHANNEL AND INSTALLED CHANNEL AND SHIM PER SRM 53-10-5. (M) 2L73 4F A3WE 19960209004961996020900496NM 1996 2 9 EISA95512 119951213A5320 STRAP BOEING727 72781 1384025NM BS 1080 BROKEN A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 STRINGER STRAP AT 3R STATION 1080 IS BROKEN. FABRICATED NEW STRAP AND INSTALLED PER SRM 51-30-02. (M) 2L73 4F A3WE 19960209004971996020900497NM 1996 2 9 EISA95513 119951213A5330 DOUBLER BOEING727 72781 1384025NM BS 1080 NON-CONFORMING A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 CROWN SKIN BONDED DOUBLER AT STATION 1080, DOES NOT CONFORM TO S/B 727-53-0109 AND BOEING DRAWING 69-62161. REMOVED CROWN SKIN DOUBLER AND INSTALLED NEW REPAIR PER BOEING DRAWING 69-62161. (M) 2L73 4F A3WE 19960209004981996020900498NM 1996 2 9 EISA95514 119951213A5313 STRINGER BOEING727 72781 1384025NM BS 312 CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CORROSION AT STRINGER 241, BS 312. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-03. (M) 2L73 4F A3WE 19960209004991996020900499NM 1996 2 9 EISA95515 119951213A5522 SKIN BOEING727 72781 1384025NM RT ELEV CORRODED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND RIGHT ELEVATOR LOWER SKIN CORRODED AT EXISTING DOUBLER AND INBOARD BETWEEN ELEVATOR STATION 158-170. REMOVED CORROSION. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) 2L73 4F A3WE 19960209005001996020900500NM 1996 2 9 EISA95516 119951213A5754 SKIN BOEING727 72781 1384025NM NR 1 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND LEFT WING NR 1 SLAT UPPER TRAILING EDGE SKIN CRACKED ABOVE OUTBOARD HOOK. FABRICATED AND INSTALLED DOUBLER PER SRM. (M) 2L73 4F A3WE 19960209005011996020900501NM 1996 2 9 EISA95517 119951213A5720 SHEAR TIE BOEING727 72781 1384025NM FRONT SPAR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND FRONT SPAR UPPER CHORD SHEAR TIE CRACKED AT STIFFENER MARKED 3. FABRICATED AND INSTALLED SHEAR TIE PER SRM 51-10-1. (M) 2L73 4F A3WE 19960209005021996020900502NM 1996 2 9 EISA95518 119951213A5720 SHEAR TIE BOEING727 72781 1384025NM FRONT SPAR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FRONT SPAR SHEAR TIE CRACKED AT STIFFENER MARKED G-8. FABRICATED AND INSTALLED SHEAR TIE PER SRM 51-10-01. (M) 2L73 4F A3WE 19960209005031996020900503NM 1996 2 9 EISA95519 119951213A5712 RIB BOEING727 72781 1384025NM WS 546.5 CRACKS A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 HFEC INDICATES TWO CRACKS AT LEFT WING RIB AT WS 546.5 LOWER FASTENER HOLE SECOND STRINGER FORWARD OF REAR SPAR. REPLACED RIB ASSY PER SRM 51-10-01 AND 51-30-02. (M) 2L73 4F A3WE 19960209005041996020900504NM 1996 2 9 EISA95520 119951213A5520 STRUCTURE BOEING727 72781 1384025NM ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CRACK IN RIGHT ELEVATOR STRUCTURE AT ELEVATOR STATION 160 RIGHT, 19 INCHES FORWARD OF TRAILING EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 55-2-03. (M) 2L73 4F A3WE 19960209005051996020900505NM 1996 2 9 EISA95521 119951213A5520 STRUCTURE BOEING727 72781 1384025NM ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CRACK IN RIGHT ELEVATOR INTERNAL STRUCTURE AT ELEVATOR STATION 170 RT, 12 INCHES FORWARD OF TRAILING EDGE. FABRICATED REPAIR DOUBLER PER SRM 55-20-03. (M) 2L73 4F A3WE 19960209005061996020900506NM 1996 2 9 EISA95522 119951213A5520 STRUCTURE BOEING727 72781 1384025NM ELEVATOR CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CRACKS IN ELEVATOR INTERNAL STRUCTURE AT APPROX ELEVATOR STATION 1251, 4 INCHES FORWARD OF TRAILING EDGE. STOP DRILLED CRACKS IN HAT CHANNELS HFEC CONFIRMS CRACKS CONTAINED FABRICATED AND INSTALLED DOUBLER PER SRM 55-20-03. (M) 2L73 4F A3WE 19960209005071996020900507NM 1996 2 9 EISA95523 119951213A5330 SKIN BOEING727 72781 1384025NM WS 280-320 DAMAGED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND, FS 280-320 STRINGER 10R, OVERSIZED FASTENER HOLES HAVE KNIFE EDGE CONDITION. REMOVED DAMAGED AREA PER SRM 53-30-03. FABRICATED AND INSTALLED DOUBLER AND FILLERS PER SRM 53-30-03. (M) 2L73 4F A3WE 19960209005081996020900508NM 1996 2 9 EISA95524 119951213A5712 RIB BOEING727 72781 1384025NM WS 738.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND 1 INCH CRACK IN LEFT WING RIB NEAR LOWER FASTENER HOLE AT WS 738.5 AND FIRST STRINGER AFT OF FRONT SPAR. FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-10-05 AND 51-30-01. (M) 2L73 4F A3WE 19960209005091996020900509NM 1996 2 9 EISA95525 119951213A5320 SHEAR TIE BOEING727 72781 1384025NM BS 294.5 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CRACK IN SHEAR TIE BS 294.5 AFT ROW OF FASTENERS ONE FASTENER ABOVE, STRINGER 14L. REPAIRED PER SRM 53-10-04. (M) 2L73 4F A3WE 19960209005101996020900510NM 1996 2 9 EISA95526 119951213A5330 SKIN BOEING727 72781 1384025NM BS 350 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 HFEC INSPECTION REVEALS THREE OUTER SKIN CRACKS AT FASTENER HOLES AT LAP JOINT STRINGER 24R, BS 350 RIGHT SIDE. FABRICATED AND INSTALLED LAP SEAT REPAIR PER SRM 53-30-03. (M) 2L73 4F A3WE 19960209005111996020900511NM 1996 2 9 EISA95527 119951214A5754 RIB BOEING727 72781 1384025NM NR 8 SLAT CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND NR 8 SLAT OUTBOARD TRACK, OUTBOARD RIB SKIN BULGED AND CRACKED. FABRICATED REPAIR PER SRM 57-50-03. INSTALLED REPAIR PER SRM 51-30-02. (M) 2L73 4F A3WE 19960209005121996020900512NM 1996 2 9 EISA95528 119951213A5543 TAB BOEING727 72781 1384025NM RUDDER CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND TWO CRACKS ON RUDDER AT APPROXIMATELY FILL STATION 87, WL 280, 15 INCHES AND 19 INCHES FORWARD OF TRAILING EDGE. REPLACED RUDDER TAB PER MM 27-31-0. (M) 2L73 4F A3WE 19960209005131996020900513NM 1996 2 9 EISA95529 119951213A5320 FITTING BOEING727 72781 1384025NM BS 870 SEPARATED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND 2 INCH BY 4 INCH AREA OF BS 870 RIGHT TERMINAL FITTING WEB, SEPARATED BELOW STRINGER 10R. REPAIRED FITTING AS PER SB 727-53-194 AND BOEING DRAWING 65C35250. (M) 2L73 4F A3WE 19960209005141996020900514NM 1996 2 9 EISA95530 119951213A5311 FRAME BOEING727 72781 1384025NM BS 760.95 CORROSION A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 FOUND CORROSION ON FRAME INBOARD FLANGE, BS 760.95 RIGHT BETWEEN STRINGER 16R AND 17R. REMOVED CORRODED AREA FABRICATED FILLER AND DOUBLER AND INSTALLED PER DRAWING 65C 36279-36. (M) 2L73 4F A3WE 19960209005151996020900515NM 1996 2 9 EISA95532 119951107A5320 ANGLE BOEING727 72781 1384025NM BS 760 CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07110NE 18952 HFEC INSPECTION INDICATES CRACKS IN FORWARD 2 FASTENER HOLES, BS 760 RIGHT SIDE. STOP DRILLED CRACKS. HFEC VERIFIES CRACKS CONTAINED. INSTALLED REPAIR PER BOEING DRAWING 65C33202 AND SB 57-112. (M) 2L73 4F A3WE 19960209005171996020900517NM 1996 2 9 USAA951342 119951212A5330 SKIN BOEING737 737201 1384454NM BS 780 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19244US36610 22752 ROA - DURING CX-6 CHECK VISUAL INSPECTION, CONFIRMED WITH HFEC FOUND FUSELAGE SKIN CRACK, 4.25 INCH LONG, STRINGER 18L, STATION 780. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2L72 4F A16WE 19960209005181996020900518NM 1996 2 9 USAA951343 119951110A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT 3 NUTPLATE HOLES, .075 INCH AT EACH HOLE AFT UPPER SIDE OF STATION 344 FLOOR BEAM, BL 9R TO BL 9L. T-CAP REPAIR AT FLOOR BEAM LBL 24 TO RBL 24 AS PER BOEING SRM 53-10-03. (M) 2L72 4F RTA16WE 19960209005191996020900519NM 1996 2 9 USAA951345 119951113A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION FOUND BY EDDY CURRENT, A 2 INCH CRACK LOCATED AT FLOOR BEAM AT STATION 520 EXTENDING 1 INCH OUTBOARD AND 1 INCH INBOARD OF LBL 24. INSTALLED REPAIR DOUBLER AS PER USAIR EA NR 40294. (M) 2L72 4F RTA16WE 19960209005201996020900520NM 1996 2 9 USAA951347 119951120A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION FOUND LEVEL 2 CORROSION TOP AND BOTTOM OF UPPER CHORD, T-CAP 986.5 FLOOR BEAM LBL 45.5 TO RBL 45.5. INSTALLED T-CAP REPLACEMENT PER BOEING SRM 53-10-05 AND USAIR TYPICAL REPAIR 53-10-05. (M) 2L72 4F RTA16WE 19960209005211996020900521NM 1996 2 9 USAA951348 119951111A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 986.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION VISUALLY FOUND A 1 INCH BY .75 INCH AREA OF LEVEL 2 CORROSION ON 986.5 FLOOR BEAM FWD SIDE OF 986.5 FLOOR BEAM LBL 45.5. INSTALLED UPPER T-CAP REPLACEMENT PER BOEING SRM 53-10-05 AND USAIR TYPICAL REPAIR 53-10-05. (M) 2L72 4F RTA16WE 19960209005221996020900522NM 1996 2 9 USAA951349 119951114A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - INSPECTION VISUALLY FOUND LEVEL 2 CORROSION AT CLIP UNIT LOCATOR ON FLOOR BEAM TOP SURFACE BS 328 RBL12-RBL22. ADDED CERAMIC STRAPS TO FLOOR BEAM UPPER CHORD AS PER USAIR TYPICAL REPAIR 53-10-01A. (M) 2L72 4F RTA16WE 19960209005231996020900523NM 1996 2 9 USAA951350 119951113A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION FOUND BY EDDY CURRENT, A 1.2 INCH FLOOR BEAM CRACK LOCATED AT STATION 520 EXTENDING .7 INCH INBOARD AND .5 INCH OUTBOARD OF RBL 45.5. INSTALLED REPAIR DOUBLER AS PER USAIR EA NR 40294. (M) 2L72 4F RTA16WE 19960209005241996020900524NM 1996 2 9 USAA951351 119951115A5315 FLOOR BEAM BOEING737 737401 1384701NM FS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION VISUALLY FOUND LEVEL 2 CORROSION UPPER CHORD OF FLOOR BEAM AT NUTPLATE HOLES, 48 INCH TOTAL LENGTH BETWEEN FS 344 BETWEEN LBL 24 AND RBL 24. INSTALLED FLOOR BEAM T-CAP REPAIR 48 INCHES TOTAL LENGTH AS PER USAIR TYPICAL REPAIR 53-10-05 AND BOEING SRM 53-10-03. (M) 2L72 4F RTA16WE 19960209005251996020900525NM 1996 2 9 USAA951353 119951207A5330 SKIN BOEING737 7372B7 1384560NM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19285AU31298 23132 CLT - CLT INSPECTION FOUND A FUSELAGE SKIN CRACK 2 INCHES LONG, LOCATED AT STATION 727, STRINGER 17L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 6. (M) 2L72 4F A16WE 19960209005261996020900526EU 1996 2 9 USAA951354 119951227A5313 STRINGER FOKKERF28 F28MK0100 4990807EU BS 12791-13851 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19856US14405 11286 PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 AT STATION 12791 TO STATION 13851. SPLICED IN NEW SECTION OF STRINGER NR 3 PER SRM 51-70-06 REPAIR NR 5. (M) 2L72 4F RT 19960209005271996020900527EU 1996 2 9 USAA951355 119951227A5313 STRINGER FOKKERF28 F28MK0100 4990807EU BS 11257 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19856US14405 11286 PIT - Q1/C2 INSPECTION, FOUND CORROSION ON STRINGER NR 3 STATION 11257. SPLICED IN NEW SECTION OF STRINGER PER SRM 51-70-06 REPAIR NR 5. (M) 2L72 4F RT 19960209005281996020900528NM 1996 2 9 USAA951364 119951211A53206545834256 INTERCOSTAL BOEING737 737401 1384701NM BS 312-328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES, RBL 11 BS 312 TO BS 328 INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005291996020900529NM 1996 2 9 USAA951365 119951211A532065C80735159 ANGLE BOEING737 737401 1384701NM BS 302-362 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 60 INCHES IN SEVERAL AREAS, BS 302 TO BS 362 LEFT SIDE Z-ANGLE. REMOVED CORRODED Z-ANGLE, REPLACED AND COMPLETED INSTALLATION. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005301996020900530NM 1996 2 9 USAA951366 119951211A53206545834259 INTERCOSTAL BOEING737 737401 1384701NM BS 328-344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER CORROSION AT SCREW HOLES LBL 11 BS 328 TO BS 344 INTERCOSTAL. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005311996020900531NM 1996 2 9 USAA951367 119951211A5320654587512 ANGLE BOEING737 737401 1384701NM BS 277/344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 30 PERCENT CORRODED Z-ANGLE FORWARD GALLEY ENTRANCE, STATION 277 AND STATION 344. REMOVED AND REPLACED NR ME-32 REQUIRED. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005321996020900532NM 1996 2 9 USAA951368 119951211A5320 BEAM BOEING737 737401 1384701NM BS 344 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 74 INCHES BY .5 INCH CORRODED AREA BS 344 LBL 55 THROUGH RBL 21 BEAM. FABRICATED T-CAP AND REPAIR ANGLE AND INSTALLED. REPAIRED PER TR 53-10-3. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005331996020900533NM 1996 2 9 USAA951369 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND ONE .5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 947 LBL 4 AND RBL 4 FLOOR BEAM. INSTALLED T-CAP, REPAIR ANGLES AND STRAPS. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005341996020900534NM 1996 2 9 USAA951370 119951211A5347 SEAT TRACKS BOEING737 737401 1384701NM BS 344-369 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 25 INCHES BY .5 INCH CORRODED AREA LBL 22 BS 344-369 SEAT TRACKS. FABRICATED SEAT TRACKS AND INSTALLED. REPAIRED PER SRM 53-00-52. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005351996020900535NM 1996 2 9 USAA951372 119951206A532065C10592906 INTERCOSTAL BOEING737 7372B7 1384560NM BS 947-967 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19272AU35420 22884 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1.5 INCH BY 1 INCH, BY STATION 947 TO STATION 967, RBL 45 INTERCOSTAL. REPLACED INTERCOSTAL, REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960209005361996020900536NM 1996 2 9 USAA951376 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 947 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 SQUARE INCHES OF CORROSION AT T-CAP FLOOR BEAM STATION 947 RBL 9. REMOVED CORRODED SECTION OF T-CAP. SPLICED IN NEW SECTION OF T-CAP. REPAIRED PER SRM 53-10-9. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960209005371996020900537NM 1996 2 9 USAA951380 119951222A5313 STRINGER BOEING737 7372B7 1384560NM BS 947.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH CORRODED AREA ON STRINGER S-27L AT STATION 947.5. REMOVED CORRODED SECTION OF STRINGER AND REPLACED. REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960209005381996020900538NM 1996 2 9 USAA951381 119951222A5320654656010 ANGLE BOEING737 7372B7 1384560NM BS 947.5 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 3 INCH AT ATTACH ANGLE STATION 947.5 BETWEEN STRINGER 26L AND 27L. REPLACED ANGLE WITH NEW ONE FROM STOCK. REPAIRED PER SRM 51-10-2. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960209005391996020900539NM 1996 2 9 USAA951419 119951222A5315 FLOOR BEAM BOEING737 7372B7 1384560NM BS 676 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK RBL 25 LONGITUDINAL FLOOR BEAM AT AILERON QUADRANT STATION 676, WL 206.5. INSTALLED DOUBLER, REPAIRED PER EA 40395 AND EO 5791G632. (M) 2L72 4F A16WE 19960209005401996020900540NM 1996 2 9 USAA951420 119951222A5311 FRAME BOEING737 7372B7 1384560NM BS 616L CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 LEFT FRAME INBOARD CHORD FIRST FASTENER ABOVE CENTER WING. INSTALLED DOUBLER, REPAIRED PER EO 40390. (M) 2L72 4F A16WE 19960209005411996020900541NM 1996 2 9 USAA951421 119951222A5311 FRAME BOEING737 7372B7 1384560NM BS 616 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 616 RIGHT FRAME INBOARD CHORD AT FIRST FASTENER ABOVE CENTER WING. INSTALLED DOUBLER, REPAIRED EPR EA 40390. (M) 2L72 4F A16WE 19960209005421996020900542NM 1996 2 9 USAA951422 119951222A531165C335763 FRAME BOEING737 7372B7 1384560NM BS 597 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.5 INCHES LONG STATION 597 ABOVE WING CENTER SECTION LEFT FRAME. REPLACED FRAME SECTION. REPAIRED PER SRM 51-10-01. (M) 2L72 4F A16WE 19960209005431996020900543NM 1996 2 9 USAA951423 119951222A531165C335264 FRAME BOEING737 7372B7 1384560NM BS 597 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG STATION 597 ABOVE WING CENTER FRAME SECTION RIGHT SIDE. REPLACED FRAME SECTION. REPAIRED PER SRM 51-10-01. (M) 2L72 4F A16WE 19960209005441996020900544NM 1996 2 9 USAA951424 119951222A532066221871 CHANNEL BOEING737 7372B7 1384560NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK LBL 25 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-1. (M) 2L72 4F A16WE 19960209005451996020900545NM 1996 2 9 USAA951425 119951222A532066221871 CHANNEL BOEING737 7372B7 1384560NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FouND .75 INCH CRACK LBL 45 SEAT TRACK SUPPORT CHANNEL STATION 520, WL 207.5. REPLACED SUPPORT CHANNEL, REPAIRED PER SRM 51-10-01. (M) 2L72 4F A16WE 19960209005461996020900546NM 1996 2 9 USAA951426 119951222A5330 SKIN BOEING737 7372B7 1384560NM FS 328 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19270AU35896 22882 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO CRACKS (LIGHTNING STRIKE) ON SKIN S-19R FS 328. INSTALLED DOUBLER AND FILLER. REPAIRED PER EO 40393 EA 40393. (M) 2L72 4F A16WE 19960209005471996020900547NM 1996 2 9 USAA951427 119951211A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 328 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US19951 23989 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1.5 INCH DIAMETER SPOTS OF CORROSION AT SCREW HOLES BS 328 LBL 13 TO RIGHT END OF FLOOR BEAM. REPLACED T-CAP. REPAIRED PER TR 53-10-03 SRM 51-70-12 SRM 51-70-11. CORROSION TASK NR C53-107-02. CORROSION LEVEL 2. (M) 2L72 4F RTA16WE 19960209005481996020900548NM 1996 2 9 USAA951428 119951230A5330 SKIN BOEING737 737201 1384454NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19237US39529 22353 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK SHEET METAL AT LOWER CORNER MED. INSTALLED INTERIM REPAIR PER EA 31854 AND TBC. REPAIRED PER EA 31854SB 737-53-1083. (M) 2L72 4F A16WE 19960209005671996020900567NM 1996 2 9 USAABB95010 119951229A5270834503 SENSOR BOEING767 7672B7 1385107NM CARGO DOOR DAMAGED A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19655US 25257 PHL - FL 194 - AFTER TAKEOFF FROM BWI, AIRCRAFT ENCOUNTERED LIGHT WAKE TURBULENCE. CREW RECEIVED BULK CARGO DOOR WARNING LIGHT AND REPORTED THAT THE AIRCRAFT WOULD NOT HOLD PRESSURIZATION. FLIGHT DIVERTED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PRESSURIZED THE AIRCRAFT AND COULD NOT DUPLICATE THE CONDITION. UPON OPENING THE REAR BULK BIN DOOR, THEY FOUND THAT A BAG HAD FALLEN AGAINST THE DOOR BENDING THE DOOR SENSOR (S211). SENSOR WAS SUBSEQUENTLY REPLACED. (M) 2L72 4F RTA1NM 19960209005731996020900573EU 1996 2 9 USAAF95008 119951228A215022034802 PACK FOKKERF28 F28MK0100 4990807EU RIGHT FAILED A USAAA UNSCHED LANDING O OTHER CRCRUISE 1 EA19886US 11346 FLT NR 689 - PIT - WHILE AT FL 350 THE AIRCRAFT PRESSURIZATION STARTED TO CLIMB TO 10K FEET. THE CAPTAIN REQUESTED DESCENT TO FL 100 AND RECEIVED SAME FROM ATC. THE FLT WAS DIVERTED TO PIT. NO EMERGENCY WAS DECLARED. THE FLT LANDED IN AT PIT WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THAT THE RIGHT AIRCO PACK WAS AT FAULT AND REPLACED SAME. (M) 2L72 4F RT 19960209005741996020900574EU 1996 2 9 USAAF95009 219951231A7200 ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515P 54521EU RIGHT VIBRATING A USAAAE UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 EA19480AU16242 11229 9796 CRW - FL 551 - EN ROUTE CLE-CLT, CREW EXPERIENCED VIBRATION FROM RIGHT ENGINE. UPON POWER REDUCTION, THE VIBRATION BECAME SEVERE. CREW SHUT DOWN ENGINE (SET 12 MINUTES), DECLARED AN EMERGENCY DIVERTED TO CRW. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) 2L72 4F4 FRTA20EU E2EU 19960209005821996020900582NM 1996 2 9 USAASB95026 119951222A24332299 TRNSFRMR RCTFR BOEING737 7374B7 1384702NM NR 1 OVERHEATED A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19780AU 24997 SJU - FL 7010 - ON CLIMB-OUT, FLIGHT ATTENDANT NOTIFIED CAPTAIN OF BURNING SMELL IN CABIN. PUT PRESSURIZATION SYSTEM INTO STANDBY AND RETURNED TO SJU. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR ONE TRANSFORMER RECTIFIER. (M) 2L72 4F RTA16WE 19960209005831996020900583NM 1996 2 9 USAASB95033 119951230A7722 EGT IND BOEING737 737401 1384701NM NR 1 ENGINE HIGH A USAAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA19408US 23878 FLT 818 - PIT - FLIGHT DIVERTED TO PIT DUE TO NR 1 ENGINE HIGH EGT. (M) 2L72 4F RTA16WE 19960209005891996020900589SO 1996 2 9 WTAA950325 119951224A771230005000052 TQ COND UNIT EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17280UE 120090 SMF - CREW REPORTED AUTOFEATHER WARNING DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. SYSTEM WAS ARMED AND TESTED NORMAL EXCEPT GREEN AUTOFEATHER LIGHT DID NOT ILLUMINATE. AIRCRAFT WAS FERRIED TO SFO AND MAINTENANCE REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITIONER UNIT. AUTOFEATHER SYSTEM OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960209006261996020900626EU 1996 2 9 96ZZZX610 119950914A6320FS72B TRANSMISSION BOLKMS105 BO105C 5626005EU M/R FAILED A AGVNAR AUTOROTATION EJYVIBRATION/BUFFET WARNING INDICATION ENGINE STOPPAGE NRNOT REPORTED 1 SW09650MS6124 715 1111 S650 PILOT REPORTED WHINE IN TRANSMISSION FOLLOWED BY LOUD BANG, SEVERE VIBRATIONS, ENGINE NR 1 FIRE WARNING LIGHT, LOSS OF BOTH ENGINES. AUTO-ROTATED SAFELY. AIRCRAFT SEVERELY DAMAGED BY FIRE AFTER LANDING. TEAR-DOWN INSPECTION REVEALED CONTAMINATION BLOCKING OIL PASSAGES TO NR 1 INPUT QUILL OF MAIN TRANSMISSION. INPUT SHAFT HEATED UP AND FAILED CAUSING BENDIX DRIVE SHAFT TO FAIL. THE FAILED DRIVE SHAFT CREATED FOD WHICH WAS INJESTED BY BOTH ENGINES, NO FOD SCREENS. THE DRIVE SHAFT ALSO STRUCK THE TRANSMISSION OIL INLET LINE AND RUPTURED IT. THE OIL WAS IGNITED BY THE HOT QUILL. RECOMMEND REMOVAL OF ALL PLUGS AND MACHINING SCREWS FOR A THOROUGH CLEANING OF TRANSMISSION OIL PASSAGES DURING OVERHAUL. 1G72 3U H3EU 19960209006421996020900642WP 1996 2 9 96ZZZX623 119951225A33507732 BULB DOUG DC9 DC983 3022083WP CABIN FAILED A TWAAK NONE L NO TEST ININSP/MAINT 1 CE059413T 53188 STL - FLT 401 - DURING INSPECTION, FOUND ROW 2 AND ROW 3 EGRESS LIGHTS NOT OPERATING. REPLACE BULBS TW NR 93-2832, MFG 7732. OPERATIONAL CHECK OF EGRESS LIGHTS, CHECK NORMAL. NEW AIRCRAFT 8-25-95. 2L72 4F RTA6WE 19960209006431996020900643NE 1996 2 9 96ZZZX624 219951204A7321 FUEL CONTROL DOUG DC8 DC862 3021970WP PWA JT3D JT3D3B 52039NE NR 3 ENGINE OUT OF ADJUST A TC8ACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 GL23803MG 45910 SCEL/SCEL - NR 3 ENGINE UNABLE TO PRODUCE TAKEOFF POWER. ABORTED TAKEOFF, RETURNED TO RAMP. INCREASE FUEL IN FUEL CONTROL UNIT 3 CLICKS. 2L74 4F4 F 4A25 1E8 19960209006491996020900649NM 1996 2 9 CAL960015 119951228A5210 SKIN BOEING727 727243 138408DNM L-1 DOOR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .50 INCH CRACK IN L-1 DOOR INTERNAL SKIN AT TORQUE BOX CUT OUT. THE CRACKED AREA WAS BLENDED OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-2, SRM 51-10-1, AND SRM 51-20-4. (X) 2L73 4F RTA3WE 19960209006501996020900650NM 1996 2 9 CAL960016 119951214A5315 FLOOR BEAM BOEING727 727243 138408DNM BS 344 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND CABIN FLOOR BEAM CORRODED FROM LBL 20 TO LBL 60, STA 344. THE CORRODED SECTION OF FLOOR BEAM WAS CUT OUT. REPAIR PARTS WERE FABRICATED, TREATED, AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10-2. (X) 2L73 4F RTA3WE 19960209006511996020900651NM 1996 2 9 CAL960017 119951214A5311 FRAME BOEING727 727243 138408DNM BS 720 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A 2.5 INCH CRACK IN FORWARD CARGO FRAME AT STA 720, LBL 6. THE CRACKED SECTION OF FRAME WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006521996020900652NM 1996 2 9 CAL960018 119951214A5311 FRAME BOEING727 727243 138408DNM BS 600 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 600 AND CENTER FLOOR STRUCTURE. THE CRACKED SECTION OF FRAME WAS CUT OUT IAW SRM 51-40-3. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006531996020900653NM 1996 2 9 CAL960019 119951213A5311 FRAME BOEING727 727243 138408DNM BS 660 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, LBL 24. THE CORRODED SECTION OF FRAME WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-40-2, SRM 51-30-1, SRM 51-20-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006541996020900654NM 1996 2 9 CAL960020 119951214A5311 FRAME BOEING727 727243 138408DNM BS 660 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .3750 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, STR 28R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006551996020900655NM 1996 2 9 CAL960021 119951213A5311 FRAME BOEING727 727243 138408DNM BS 680 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT BS 680, LBL 6. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS FABRICATED, TREATED, AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006561996020900656NM 1996 2 9 CAL960022 119951218A5320 SUPPORT BOEING727 727243 138408DNM BS 640 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT STRUCTURE AT STA 640 CENTER SECTION CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6, AN 'L' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND SRM 53-10-8. (X) 2L73 4F RTA3WE 19960209006571996020900657NM 1996 2 9 CAL960023 119951214A5311 FRAME BOEING727 727243 138408DNM BS 640 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND FORWARD CARGO FRAME STA 640 CRACKED AT S29R (.50 INCH), S29L (1.5 INCHES), AND S28L (.25 INCH). A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006581996020900658NM 1996 2 9 CAL960024 119951214A5320 SUPPORT BOEING727 727243 138408DNM BS 480-560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND FORWARD CARGO RIGHT FLOOR SUPPORT STRUCTURE CORRODED AT BS 480 - BS 560. A REPAIR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006591996020900659NM 1996 2 9 CAL960025 119951214A5311 FRAME BOEING727 727243 138408DNM BS 580 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO FRAME AT STA 580 AND CENTER OF FLOOR STRUCTURE. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006601996020900660NM 1996 2 9 CAL960027 119951218A5320 STRAP BOEING727 727243 138408DNM BS 560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND DOUBLER STRAP CORRODED AROUND C-1 ENTRANCE AT STA 560 ABOVE STR 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230-01298 AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006611996020900661NM 1996 2 9 CAL960028 119951214A5313 STRINGER BOEING727 727243 138408DNM BS 1166 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STRINGER 26R CORRODED AT STA 1166. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X) 2L73 4F RTA3WE 19960209006621996020900662NM 1996 2 9 CAL960029 119951214A5320 SHEAR TIE BOEING727 727243 138408DNM BS 1010 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND SHEAR TIE CORRODED BETWEEN S27R AND S28R AND STA 1010. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, SRM 51-10-2, AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006631996020900663NM 1996 2 9 CAL960030 119951214A5313 STRINGER BOEING727 727243 138408DNM BS 1015 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STR 27L CORRODED IN AFT CARGO COMPARTMENT AT BS 1015. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-30-2. A STRINGER REPAIR AND HAT SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X) 2L73 4F RTA3WE 19960209006641996020900664NM 1996 2 9 CAL960034 119951226A5313 STRINGER BOEING727 727243 138408DNM BS 1000 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STR 29R CORRODED AT SPLICE AND UNDER LEVELING COMPOUND AT CENTER OF STRINGER IN AFT CARGO BIN BS 1000. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A STRINGER SPLICE AND REPAIR DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SRM 51-10-2. (X) 2L73 4F RTA3WE 19960209006651996020900665NM 1996 2 9 CAL960035 119951218A5313 STRINGER BOEING727 727243 138408DNM BS 972 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STR 29L CORRODED AT STA 972 IN AFT PIT. THE CORROSION WAS BLENDED OUT IAW SRM 51-10-6. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW ECRA 5310-03205. (X) 2L73 4F RTA3WE 19960209006661996020900666NM 1996 2 9 CAL960036 119951215A5313 STRINGER BOEING727 727243 138408DNM BS 985-994 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STR 28L CORRODED BETWEEN STA 985 AND STA 994, IN THE AFT PIT. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND MM 51-40-5. (X) 2L73 4F RTA3WE 19960209006671996020900667NM 1996 2 9 CAL960037 119951214A5320 SHEAR TIE BOEING727 727243 138408DNM FS 990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND SHEAR TIE CORRODED AT FS 990 BETWEEN STR 28L AND STR 29L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 53-10-4, 51-10-1, 51-10-2, AND 51-30-2. (X) 2L73 4F RTA3WE 19960209006681996020900668NM 1996 2 9 CAL960038 119951214A5311 FRAME BOEING727 727243 138408DNM BS 990 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND UPPER SURFACE OF BELT FRAME LOWER FLANGE IN AFT CARGO BIN CORRODED AT BS 990, LBL 16. THE CORROSION WAS REMOVED IAW SRM 51-10-6. (X) 2L73 4F RTA3WE 19960209006691996020900669NM 1996 2 9 CAL960039 119951214A5312 BULKHEAD FITTING BOEING727 727243 138408DNM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD CORNER FITTING AT S28R. A NEW STRINGER SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, SRM 53-10-3, AND ECRA 5340-01256. (X) 2L73 4F RTA3WE 19960209006701996020900670NM 1996 2 9 CAL960040 119951214A5312 BULKHEAD FITTING BOEING727 727243 138408DNM BS 740 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD FITTING AT S28L. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-2. L-ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM'S 51-30-2, 53-10-3, 51-10-2, AND 51-20-4. (X) 2L73 4F RTA3WE 19960209006711996020900671NM 1996 2 9 CAL9690026 119951214A5313 STRINGER BOEING727 727243 138408DNM BS 520-560 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW09578PE42453 21661 INSPECTION FOUND STR 26R CORRODED AT STA 520 - STA 560. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-10-2, SRM 51-30-2, AND SRM 51-40-5. (X) 2L73 4F RTA3WE 19960209006991996020900699WP 1996 2 9 UPS805375 119951231A5230 FITTING DOUG DC8 DC871F 302199DWP CARGO DOOR CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2ND DR. LATCH FITTING FROM FORWARD LOWER SIDE OF A B/B DR. HAS CORROSION AND CRACKS. REPLACED FITTING PER SRM 50-1-20. 2L74 4F RT4A25 19960209007171996020900717WP 1996 2 9 UPS805398 119951226A5320 TRAP FITTING DOUG DC8 DC871F 302199DWP FS 879 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701UP 45938 WHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT TRAPEZODIAL FITTING CRACKED PAST STOP DRILL. REPLACED FITTING PER UPS E.O. 2L74 4F RT4A25 19960212000011996021200001SW 1996 2 12 MEJA1104 119951129A243035721 TERMINAL SWRNGNSA227 SA227AT 8780610SW RT GENERATOR BROKEN E AMEJAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC APAPPROACH 1 SW17561UP AT561 ON APPROACH TO BIS, THE RIGHT GENERATOR LIGHT CAME ON, UNABLE TO RESET GENERATOR. THE FLIGHT CREW CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND TERMINAL ON WIRE BROKEN AT GENERATOR. REMOVED AND REPLACED TERMINAL IN ACCORDANCE WITH FAIRCHILD AIRCRAFT WIRING MANUAL 24-30-21. FUNCTIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19960212000021996021200002SW 1996 2 12 MEJA1201 119951208A32302751000291 UPLOCK BEARING SWRNGNSA227 SA227AT 8780610SW RT MLG FAILED E AMEJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW17560UP AT560 MFE-SAT - FLT 1851 - AFTER TAKEOFF, THE RIGHT MAIN GEAR SHOWED INTRANSIT LIGHT REMAINED ON. FLIGHT CREW CYCLED GEAR WITH NO CHANGE IN INDICATION. AIRCRAFT RETURNED TO MFE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND UPLOCK ROLLER BEARING FROZEN. REMOVED AND REPLACED UPLOCK ROLLER IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT MAINTENANCE MANUAL. FUNCTIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19960212000031996021200003SW 1996 2 12 MEJA1202 119951206A56102621383006 WINDOW SWRNGNSA227 SA227AT 8780610SW RT COCKPIT CRACKED E AMEJABHI EMER. DESCENT DEACTIVATE SYST/CIRCUITSCABIN DEPRESSURIZATION O OTHER CLCLIMB 1 SW17569UP AT569 MOT-FSD - FLT 1585 - WHILE CLIMBING THROUGH 17,000 FEET THE FLIGHT CREW HEARD A LOUD POP AND HISSING SOUND AND AIRCRAFT STARTED TO DEPRESSURIZE. THE FLIGHT CREW FOUND THE RIGHT SIDE COCKPIT WINDOW CRACKED. DESCENDED, DEPRESSURIZED AND CONTINUED TO FSD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. WINDOW WAS REPLACED IN ACCORDANCE WITH FAIRCHILD AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19960212000041996021200004SW 1996 2 12 MEJA1203 119951209A26121734361600F FIRE DETECTOR SWRNGNSA227 SA227AC 8780603SW RT ENGINE DEFECTIVE E AMEJAEFA ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW17787C AC550 SVMI-TJSF - FLT 9800 - ABOUT ONE HOUR OUT IN CRUISE THE RIGHT ENGINE FIRE LIGHT CAME ON. PERFORMED SHUTDOWN AND DISCHARGED FIRE BOTTLE. AIRCRAFT RETURNED TO SVMI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND A DEFECTIVE 600 DEGREE DETECTOR. REMOVED AND REPLACED DETECTOR, INSTALLED NEW FIRE BOTTLE. PERFORMED FUNCTIONAL CHECK OF THE FIRE DETECTOR SYSTEM, NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A8SW 19960212000051996021200005SW 1996 2 12 MEJA1205 119951218A32322751042189A DOOR ACTUATOR SWRNGNSA227 SA227AT 8780610SW LT MLG WORN E AMEJAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW17807M AT454B FLT 8078 - AFTER TAKEOFF, THE LEFT GEAR DID NOT INDICATE UP AND LOCKED. CYCLED GEAR WITH SAME RESULTS. AIRCRAFT RETURNED AND LANDED AT MIA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND DEFECTIVE DOOR ACTUATOR. REMOVED AND REPLACED ACTUATOR IN ACCORDANCE WITH THE FAIRCHILD AIRCRAFT MAINTENANCE MANUAL. FUNCTIONAL CHECK AND FLIGHT CHECK WAS PERFORMED, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 1L72 4T A5SW 19960213000051996021300005NM 1996 2 13 USAA951346 119951130A5315 FLOOR BEAM BOEING737 737401 1384701NM BS 520 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19421US19854 23988 CLT - CLT INSPECTION FOUND BY EDDY CURRENT A 1.7 INCH FLOOR BEAM CRACK LOCATED AT STATION 520 EXTENDING 6 INCHES INBOARD OF RBL 24.75. INSTALLED REPAIR DOUBLERS AS PER USAIR EA NR 40294. (M) 2L72 4F RTA16WE 19960216000061996021600006NM 1996 2 16 96ZZZX633 119951228A2560104343 BOTTLE BOEING737 737298C 1384490NM L-1 DOOR LOW PRESSURE A ASAAK NONE O OTHER ININSP/MAINT 1 NM01745AS2850 2784 20794 DURING A-CHECK, THE L-1 EMERGENCY EVACUATION SLIDE PACK PRESSURE WAS FOUND LOW. REPLACED SLIDE ASSEMBLY. VENDOR TEAR DOWN REVEALED LOW BOTTLE PRESSURE. OVERHAULED, HYDROSTATIC TESTED, AND REFILLED BOTTLE. REFERENCE: OPERATOR CONTROL NR ASAA9510118. 2L72 4F RTA16WE 19960216000141996021600014NM 1996 2 16 MALA954785 119951227A2460AJA4N176 START RELAY DHAV DHC8 DHC8102 2809003NM NR 2 ENGINE FAILED A MALAE ENGINE SHUTDOWN HJ ELECT. POWER LOSS-50 PC WARNING INDICATION TXTAXI/GRND HDL 1 GL15861MA 362 TYS - FLT 3343 - AFTER ENGINE START IN TYS, THE NR 2 DC GENERATOR WOULD NOT COME ON-LINE AND THE 'DC BUS' LIGHT ILLUMINATED. THE CREW IMMEDIATELY SHUT DOWN THE NR 2 ENGINE. MAINTENANCE PERSONNEL REPLACED THE NR 2 START CONTACTOR RELAY. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19960216000151996021600015NM 1996 2 16 MALA954787 119951228A335061D4781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST ININSP/MAINT 1 GL15861MA 362 MSP - FLT 3288 - DURING PRE-FLIGHT, CREW NOTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPLACED ALL SIX EMERGENCY LIGHT BATTERY PACKS. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19960216000161996021600016NM 1996 2 16 MALA954788 119951229A323010800113 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003NM LT MLG MALFUNCTIONED A MALAK NONE O OTHER APAPPROACH 1 GL15830MA 337 DTW - FLT 3341 - DURING APPROACH TO DTW, THE LT MAIN GEAR WAS VERY SLOW TO EXTEND. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT MLG UPLOCK ACTUATOR. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2H72 4T RTA13NM 19960216000171996021600017NM 1996 2 16 MALA954789 119951231A3230 RETRACT MECH DHAV DHC8 DHC8102 2809003NM RT MLG MALFUNCTIONED A MALAK NONE O OTHER APAPPROACH 1 GL15802MA 245 MSP - FLT 3375 - DURING APPROACH TO MSP, THE RT MAIN GEAR TOOK ABNORMALLY LONG TO INDICATE DOWN AND LOCKED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED TROUBLESHOOTING AND TEST FLEW THE AIRCRAFT, BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. (X) 2H72 4T RTA13NM 19960216000281996021600028EU 1996 2 16 RAIA951132 119951129A21201379221L401 AIR DUCT BAG JETSTMJETSTM3201 1500217EU COCKPIT LOOSE A RAIAK NONE O OTHER NRNOT REPORTED 1 CE03426AM9900 874 STL - FLT 7306 - BOTH FLOWS INOPERATIVE. MAINTENANCE SECURED DUCTS TO CAPTAIN AND FO'S AIR EYEBALL. SYSTEM CHECK GOOD. (X) 2L72 4T RTA56EU 19960216000731996021600073WP 1996 2 16 ABXA9600117 119950822A5330 SKIN DOUG DC9 DC932 3022066WP FS 889 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND FUSELAGE EXTERIOR SKIN BULGING AFT OF FS 889 AT LONGERON 29R. REPLACED SKIN IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216000741996021600074WP 1996 2 16 ABXA9600118 119950801A53135920319 LONGERON DOUG DC9 DC932 3022066WP BS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 4L AT STA 160 CRACKED. REPAIRED LONGERON IAW DC-9 SRM 53-02. 2L72 4F A6WE 19960216000751996021600075WP 1996 2 16 ABXA9600120 119951011A56105644324501 RETAINER DOUG DC9 DC932 3022066WP FS 120 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 56-11 REV 3, FOUND THE LEFT SLIDING WINDOW FRAME CRACKED IN THE UPPER AFT CORNER. REPLACED DOUBLERS IAW DC-9 SRM 56-01 AND ABX REA D956-13036-SB. 2L72 4F A6WE 19960216000761996021600076WP 1996 2 16 ABXA9600122 119951113A5320591015839 JAMB DOUG DC9 DC932 3022066WP FS 897-937 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL 2 CORROSION ON THE AFT BAG BIN DOOR JAMB. REPAIRED AFT BAG BIN DOOR JAMB IAW DC-9 SRM 53-05 FIG 44 SHEET 4. 2L72 4F A6WE 19960216000771996021600077WP 1996 2 16 ABXA9600123 119951114A5320591015835 WEB DOUG DC9 DC932 3022066WP FS 897-937 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL 2 CORROSION ON THE WEBS AROUND THE AFT BAG BIN DOOR JAMB. REPLACED ALL WEBS AROUND AFT BAG BIN DOOR JAMB IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216000781996021600078WP 1996 2 16 ABXA9600124 119950921A52805910557159 DOOR DOUG DC9 DC932 3022066WP LT MLG DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD FLYING DOOR DELAMINATED. REPLACED LEFT FLYING DOOR IAW DC-9 MM 32-12-1. 2L72 4F A6WE 19960216000791996021600079WP 1996 2 16 ABXA9600125 119950921A32313923167501 ROD DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR CONNECTING ROD FROM THE GEAR TO DOOR ROD ENDS WORN. REPLACED ROD ENDS IAW DC-9 OVERHAUL MANUAL 20-10 AND MM 32-12-1. 2L72 4F A6WE 19960216000801996021600080WP 1996 2 16 ABXA9600126 119950921A5280SS2210370P4109 BUSHING DOUG DC9 DC932 3022066WP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR INTERCONNECT LINK WORN. REPLACED BUSHING AND SLEEVE ON LINK IAW DC-9 OVERHAUL MANUAL 20-10-7. 2L72 4F A6WE 19960216000811996021600081WP 1996 2 16 ABXA9600127 119950914A5280591055726 SEAL DOUG DC9 DC932 3022066WP RT MLG DOOR BENT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR AFT METAL SEAL BENT AT THE BOTTOM OF DOOR. REPAIRED SEAL IAW DC-9 SRM 51-01. 2L72 4F A6WE 19960216000821996021600082WP 1996 2 16 ABXA9600128 119951003A32313923167501 LINKAGE DOUG DC9 DC932 3022066WP RT MLG DOOR BROKEN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE BROKEN. REPLACED ROD ASSEMBLY IAW DC-9 MM 21-10-6. 2L72 4F A6WE 19960216000831996021600083WP 1996 2 16 ABXA9600129 119951016A5312 BLKHD WEB DOUG DC9 DC932 3022066WP FS 1038 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 HAD A SMALL CRACK RADIATING FROM LIGHTENING HOLE BETWEEN LONGERON 12R AND 13R. REPAIRED CRACK IAW DC-9 SRM 53-01 FIGURE 2. 2L72 4F A6WE 19960216000841996021600084WP 1996 2 16 ABXA9600130 119951016A5312 BLKHD WEB DOUG DC9 DC932 3022066WP FS 1038 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE BULKHEAD WEB AT FS 1038 CRACKED AT LONGERON 11R. REPAIRED IAW DC-9 SRM 53-01 FIGURE 2. 2L72 4F A6WE 19960216000851996021600085WP 1996 2 16 ABXA9600131 119951010A531127779305 FRAME DOUG DC9 DC932 3022066WP FS 1076 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUS REPAIR ON FUSELAGE FRAME AT FS 1076 CRACKED BETWEEN LONGERONS 12R AND 13R. REPLACED FUSELAGE FRAME AT FS 1076 IAW DC-9 SRM 51-10-2, 51-10-5 AND 51-30-1. 2L72 4F A6WE 19960216000861996021600086WP 1996 2 16 ABXA9600132 119951025A53125910130387N BLKHD TEE CAP DOUG DC9 DC932 3022066WP FS 996 DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION HAD TWO DRILL STARTS. REPLACED LOWER TEE CAP IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216000871996021600087WP 1996 2 16 ABXA9600133 119951017A531359203192 LONGERON DOUG DC9 DC932 3022066WP FS 237 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON NR 30 CRACKED AT FS 237. REPLACED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216000881996021600088WP 1996 2 16 ABXA9600134 119950823A5321 FLOOR DOUG DC9 DC932 3022066WP FS 160-218 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD CABIN SUBFLOOR WEBS CORRODED FROM FS 218 TO FS 160. REPLACED FORWARD CABIN FLOOR WEBS IAW EA FS 53-03748-MA. 2L72 4F A6WE 19960216000891996021600089WP 1996 2 16 ABXA9600135 119951020A57305919573501 DOOR DOUG DC9 DC932 3022066WP XRS 267 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1053 DELAMINATED. REPLACED LEFT BUTE DOOR NR 1503 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19960216000901996021600090WP 1996 2 16 ABXA9600136 119951006A53305911408125 SKIN DOUG DC9 DC932 3022066WP FS 218-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD UPPER FUSELAGE SKIN HAD CORROSION UNDER THE NR 1 AND NR 2 ADF ANTENNAS. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12833-MR. 2L72 4F A6WE 19960216000911996021600091WP 1996 2 16 ABXA9600137 119951020A572059195721 DOOR DOUG DC9 DC932 3022066WP XRS 353 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT BUTE DOOR NR 1502 BROKEN AND DELAMINATED. REPLACED LEFT BUTE DOOR NR 1502 IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19960216000921996021600092WP 1996 2 16 ABXA9600138 119951024A5320991951725 JAMB DOUG DC9 DC932 3022066WP FS 996 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APU CUTOUT FORWARD JAMB CRACKED IN THREE PLACES BETWEEN LONGERON 24L TO 24R. REPAIRED IAW ABX REA D953-13027. REINSTALLED JAMB IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216000931996021600093WP 1996 2 16 ABXA9600139 119951003A541549198641AX FITTING DOUG DC9 DC932 3022066WP FS 1038 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT ENGINE PYLON INTERIOR FITTING CRACKED AT FS 1038 ABOVE THE ELECTRICAL CONNECTORS. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5. 2L72 4F A6WE 19960216000941996021600094WP 1996 2 16 ABXA9600140 119950920A532099100789 ANGLE DOUG DC9 DC932 3022066WP FS 229-180 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CUSP WEB ANGLE CRACKED FORWARD OF FS 218. REPAIRED CUSP WEB ANGLE IAW ABX REA D-953-12721-MR. 2L72 4F A6WE 19960216000951996021600095WP 1996 2 16 ABXA9600141 119950911A531599115937 FLOORBEAM DOUG DC9 DC932 3022066WP FS 160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FLOORBEAM AT FS 160 HEAVILY CORRODED AT RBL 44 AND HAD A RIVET HOLE ELONGATED AT BL 22R. REPAIRED FLOORBEAM IAW ABX REA D953-12722-MR. 2L72 4F A6WE 19960216000961996021600096WP 1996 2 16 ABXA9600142 119951114A53119919614501 FRAME DOUG DC9 DC932 3022066WP FS 639 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A SPLICE REPAIR AT LONGERON 17L WITH A GAP AT THE LEFT FUSELAGE FRAME AT FS 639. REPAIRED FRAME IAW ABX REA D953-12780-MR. 2L72 4F A6WE 19960216000971996021600097WP 1996 2 16 ABXA9600143 119951111A573059104819 SKIN DOUG DC9 DC932 3022066WP FS 658 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR ON THE LOWER CENTER WING SKIN AT FS 658 BETWEEN BL 4.0 AND 24.0 THAT WAS NOT PER THE DC-9 SRM. REPAIRED LOWER WING CENTER SKIN IAW ABX REA D957-12798-MR. 2L72 4F A6WE 19960216000981996021600098WP 1996 2 16 ABXA9600144 119951019A5330591142485 SKIN DOUG DC9 DC932 3022066WP FS 965-979 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE AFT FUSELAGE SKIN DENTED AFT OF FS 965 ABOVE LONGERON 22R. REPAIRED SKIN IAW ABX REA D953-12800-MR. 2L72 4F A6WE 19960216000991996021600099WP 1996 2 16 ABXA9600145 119951109A533059114003 SKIN DOUG DC9 DC932 3022066WP FS 89 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR AT THE EXTERNAL POWER DOOR CUTOUT AT STATION 89L NOT PER THE SRM. REPAIRED SKIN IAW ABX REA D953-12801-MR. 2L72 4F A6WE 19960216001001996021600100WP 1996 2 16 ABXA9600146 119950919A57115911301502 SPAR DOUG DC9 DC932 3022066WP XRS 416-531 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON A REPAIR ON THE RIGHT WING LOWER TEE CAP AT XRS 531. REPAIRED RIGHT WING LOWER SPAR IAW ABX REA D957-12806-MR. 2L72 4F A6WE 19960216001011996021600101WP 1996 2 16 ABXA9600147 119951006A5330591140885 SKIN DOUG DC9 DC932 3022066WP FS 218-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD UPPER FUSELAGE SKIN HAD CORROSION UNDER THE NR 1 AND NR 2 ADF ANTENNAS. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12833-MR. 2L72 4F A6WE 19960216001021996021600102WP 1996 2 16 ABXA9600148 119950921A5330591140940 SKIN DOUG DC9 DC932 3022066WP FS 237 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD FUSELAGE SKIN DENTED AT FS 237 ABOVE LONGERON 17R. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12906-MR. 2L72 4F A6WE 19960216001031996021600103WP 1996 2 16 ABXA9600149 119951102A53159911544507 FLOORBEAM DOUG DC9 DC932 3022066WP FS 389 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CABIN FLOORBEAM GOUGED ON THE LOWER FLANGE AT FS 389 BL 2 R. REPAIRED FLOORBEAM IAW ABX REA D953-12915-MR. 2L72 4F A6WE 19960216001041996021600104WP 1996 2 16 ABXA9600150 119951030A533059114194 SKIN DOUG DC9 DC932 3022066WP FS 935 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A REPAIR ON THE RIGHT AFT FUSELAGE SKIN AT FS 935 AND LONGERON 15R HAD CRACKED. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12916-MR. 2L72 4F A6WE 19960216001051996021600105WP 1996 2 16 ABXA9600151 119950927A53145911418121 KEEL BEAM DOUG DC9 DC932 3022066WP FS 622 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT CANTED KEEL OUTBOARD RAIL CORRODED. REPAIRED CANTED KEEL IAW ABX REA D953-12923-MR. 2L72 4F A6WE 19960216001061996021600106WP 1996 2 16 ABXA9600152 119951031A57305912156191 PANEL DOUG DC9 DC932 3022066WP XRS 137-164 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A SPLICED AREA OF THE UPPER WING TRAILING EDGE SKIN ON THE LEFT HAND WING HAD CORROSION ALONG SPLICE AND RIBS. REPAIRED LEFT WING TRAILING EDGE IAW ABX REA D957-12958-MR AND SERVICE REWORK DRAWING 5928669. 2L72 4F A6WE 19960216001071996021600107WP 1996 2 16 ABXA9600153 119951005A5711991001011 SPAR WEB DOUG DC9 DC932 3022066WP XRS 353 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR SPAR LOWER VERTICAL LEG CORRODED JUST INBOARD OF THE OUTBOARD FLAP HINGE FITTING. REPAIRED LEFT WING REAR SPAR IAW ABX REA D957-13003-MR. 2L72 4F A6WE 19960216001081996021600108WP 1996 2 16 ABXA9600154 119951110A5330592032393 SKIN DOUG DC9 DC932 3022066WP FS 229-588 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT FUSELAGE SKIN DENTED, GOUGED AND CORRODED FROM FS 289 TO FS 588R, BETWEEN LONGERONS 18 AND 26R. REPLACED SKIN PANEL IAW DC-9 SRM 51-30-2, 51-30-5 AND ABX REA D953-13035-MR. 2L72 4F A6WE 19960216001091996021600109WP 1996 2 16 ABXA9600155 119951025A5313591142917 LONGERON DOUG DC9 DC932 3022066WP FS 996 SPLICED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND WHILE REPLACING THE AFT PRESSURE BULKHEAD LOWER TEE SECTION AT FS 996, LONGERON 25L, HAD TO BE CUT AND REPAIRED. REPAIRED LONGERON IAW ABX REA D953-13040-MR. 2L72 4F A6WE 19960216001101996021600110WP 1996 2 16 ABXA9600156 119951018A5312991556141 BLKHD WEB DOUG DC9 DC932 3022066WP FS 996 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE APB WEB CORRODED JUST BELOW FLOOR LEVEL AT FS 996 AND BETWEEN LBL 10 AND LBL 20. REPAIRED WEB IAW ABX REA D953-13041-MR. 2L72 4F A6WE 19960216001111996021600111WP 1996 2 16 ABXA9600157 119951009A57115911301501 SPAR DOUG DC9 DC932 3022066WP XRS 509-531 RT DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING LOWER REAR SPAR HAD A PREVIOUS REPAIR BETWEEN XRS 509 AND XRS 531 WITH FURTHER DAMAGE. REPAIRED REAR SPAR IAW DC-9 SRM 57-09 FIG 11 AND ABX REA D957-13115-MR. 2L72 4F A6WE 19960216001121996021600112WP 1996 2 16 ABXA9600158 119951016A53209919402506 TRAP PANEL DOUG DC9 DC932 3022066WP FS 718 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT TRAPEZIODAL PANEL HAD CORROSION INSIDE THE BOLT HOLES ABOVE THE FIXED SIDE BRACE. REPAIRED PANEL IAW ABX REA D953-13155-MR. 2L72 4F A6WE 19960216001131996021600113WP 1996 2 16 ABXA9600159 119951013A5330591141626 SKIN DOUG DC9 DC932 3022066WP FS 658-680 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE INTERIOR FUSELAGE SKIN CORRODED AT LONGERON 17R BETWEEN FS 658 AND 680. REPAIRED SKIN IAW ABX REA D953-13156-MR. 2L72 4F A6WE 19960216001141996021600114WP 1996 2 16 ABXA9600160 119951110A532099100733 PRESS PANEL DOUG DC9 DC932 3022066WP FS 80 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A CRACK IN AN EXISTING REPAIR ON THE UPPER PRESSURE PANEL LEFT SIDE AT FS 80. REPAIRED PRESSURE PANEL IAW ABX REA D953-13160-MR. 2L72 4F A6WE 19960216001151996021600115WP 1996 2 16 ABXA9600161 119951023A5311995821429 FRAME DOUG DC9 DC932 3022066WP FS 897 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CORROSION BLEND OUT AT LONGERON 29R AT FS 897 BEYOND LIMITS. REPAIRED FRAME IAW ABX REA D953-13169-MR. 2L72 4F A6WE 19960216001161996021600116WP 1996 2 16 ABXA9600162 119951023A5330591142641 SKIN DOUG DC9 DC932 3022066WP FS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN EXISTING REPAIR ON THE FUSELAGE EXTERIOR SKIN AT FS 965 AND LONGERON 14L CRACKED. REPAIRED SKIN IAW ABX REA D953-13181-MR. 2L72 4F A6WE 19960216001171996021600117WP 1996 2 16 ABXA9600163 119951112A53209912455501 DOUBLER DOUG DC9 DC932 3022066WP FS 370-427 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LOWER FORWARD CARGO COMPARTMENT DOOR JAMB LOWER DOUBLER CORRODED. REPAIRED DOOR JAMB DOUBLER IAW ABX REA D953-13204-MR. 2L72 4F A6WE 19960216001181996021600118WP 1996 2 16 ABXA9600164 119951116A533059114063 SKIN DOUG DC9 DC932 3022066WP FS 160 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE EXTERIOR SKIN CRACKED AT FS 160 AT THE MAIN ENTRY DOOR OPENING. REPAIRED FUSELAGE SKIN AT FS 160 IAW ABX REA D953-13277-MR. 2L72 4F A6WE 19960216001191996021600119WP 1996 2 16 ABXA9600165 119951117A532099196505 INTERCOSTAL DOUG DC9 DC932 3022066WP FS 420 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN EXISTING REPAIR ON THE INTERCOSTAL AT FS 420, L19R CRACKED. REPAIRED IAW ABX REA D953-13439-MR. 2L72 4F A6WE 19960216001201996021600120WP 1996 2 16 ABXA9600166 119951111A57205910465501 DOUBLER DOUG DC9 DC932 3022066WP XRS 58 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND A DOUBLER AT XRS 58.0 ON THE LEFT WING LOWER SURFACE CORRODED AND BLENDED OUT OF SRM LIMITS. REPLACED DOUBLER IAW DC-9 SRM 51-30-4, 51-30-5 AND REPAIRED FASTENER HOLES IAW ABX REA D957-12559. 2L72 4F A6WE 19960216001211996021600121WP 1996 2 16 ABXA9600167 119950925A531199196181N FRAME DOUG DC9 DC932 3022066WP FS 718 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE FRAME AT FS 718 CRACKED FROM THE FORWARD BOLT HOLE UP TO AND BEYOND A PREVIOUS REPAIR. REPLACED FUSELAGE FRAME IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-3 AND 51-30-5. 2L72 4F A6WE 19960216001221996021600122WP 1996 2 16 ABXA9600168 119950914A27205616067501 BRACKET DOUG DC9 DC932 3022066WP FS 9 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 89-14-02; ASB 27-307, FOUND A PREVIOUS WELD REPAIR ON THE LEFT RUDDER PEDAL BRACKET NOT IAW THE SERVICE BULLETIN. REPLACED THE LEFT RUDDER PEDAL BRACKET IAW DC-9 MM 27-20-12. 2L72 4F A6WE 19960216001231996021600123WP 1996 2 16 ABXA9600169 119950828A53202913044501 TIE STRAP DOUG DC9 DC932 3022066WP FS 465 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND MAIN CABIN INTERCOSTAL TIE STRAP AT FS 465 AND LONGERON 6R CORRODED AND BLENDED. REPLACED TIE STRAP IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001241996021600124WP 1996 2 16 ABXA9600170 119950912A57309919376503AX SKIN DOUG DC9 DC932 3022066WP WS 164 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING LEADING EDGE SKIN SPLICE BETWEEN NR 3 AND NR 4 SLAT TRACKS CRACKED. REPLACED LEFT WING LEADING EDGE SKIN SPLICE IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001251996021600125WP 1996 2 16 ABXA9600171 119950906A5312595606527AX BLKHD PANEL DOUG DC9 DC932 3022066WP FS 699 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT SLANT PRESSURE PANEL CORRODED AT FS 699. REPLACED THE RIGHT SLANT PRESSURE PANEL IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960216001261996021600126WP 1996 2 16 ABXA9600172 119951101A5320991555351 INTERCOSTAL DOUG DC9 DC932 3022066WP FS 579-598 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN INTERCOSTAL BETWEEN LONGERONS 27L AND 28L CORRODED FROM FS 579 TO FS 598. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001271996021600127WP 1996 2 16 ABXA9600173 119951101A57535912168503 VANE DOUG DC9 DC932 3022066WP LT TE FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FLAP FORWARD MOVEABLE VANE DELAMINATED. REPLACED IAW DC-9 MM 27-51-1. 2L72 4F A6WE 19960216001281996021600128WP 1996 2 16 ABXA9600175 119950928A5320991007813 DOOR JAMB DOUG DC9 DC932 3022066WP FS 160-200 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FORWARD SERVICE DOOR JAMB INTERIOR LOWER AFT CORNER. REPLACED UPPER CUSP IAW DC-9 SRM 53-05 FIG 55. 2L72 4F A6WE 19960216001291996021600129WP 1996 2 16 ABXA9600176 119950921A53135914258503 L0NGERON DOUG DC9 DC932 3022066WP FS 737 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 20 CORRODED AT THE LEFT TRAPEZOIDAL PANEL JUST FORWARD OF FS 737. REPLACED LONGERON 20L IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001301996021600130WP 1996 2 16 ABXA9600177 119951017A531359203192 LONGERON DOUG DC9 DC932 3022066WP FS 237 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED AT FS 237. REPLACED LONGERON 30 IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001311996021600131WP 1996 2 16 ABXA9600178 119951014A53135920319504 LONGERON DOUG DC9 DC932 3022066WP FS 560-579 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED BETWEEN FS 560 AND FS 579. REPLACED LONGERON 30 IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001321996021600132WP 1996 2 16 ABXA9600179 119950901A5320DO489824 WEB DOUG DC9 DC932 3022066WP FS 658 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT CUSP WEB CRACKED AT FS 658. REPLACED RIGHT CUSP WEB IAW DC-9 SRM 51-30-2 AND ABX EA NR FS-53-3689. 2L72 4F A6WE 19960216001331996021600133WP 1996 2 16 ABXA9600180 119951014A573059121341 PANEL DOUG DC9 DC932 3022066WP XRS 531 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING UPPER TRAILING EDGE PANEL AT XRS 531 DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2. 2L72 4F A6WE 19960216001341996021600134WP 1996 2 16 ABXA9600181 119951030A53305911412113 SKIN DOUG DC9 DC932 3022066WP FS 427 DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD FUSELAGE EXTERIOR SKIN DENTED FORWARD OF FS 427, BELOW LONGERON 28R. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5 AND ABX REA D953-13306. 2L72 4F A6WE 19960216001351996021600135WP 1996 2 16 ABXA9600182 119951107A532059203321 FITTING DOUG DC9 DC932 3022066WP FS 579-598 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29R END FITTING CRACKED BETWEEN FS 579 AND 598. REPLACED END FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001361996021600136WP 1996 2 16 ABXA9600183 119951107A532059203321 FITTING DOUG DC9 DC932 3022066WP FS 579-598 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 29L END FITTING CRACKED BETWEEN FS 579 AND 598. REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001371996021600137WP 1996 2 16 ABXA9600184 119951018A572059134384 PANEL DOUG DC9 DC932 3022066WP XRS 69 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT LOWER TRAILING EDGE PANEL INBOARD OF THE MAIN LANDING GEAR DELAMINATED. REPLACED PANEL ASSEMBLY IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960216001591996021600159WP 1996 2 16 DLL10954211 119950612A5711 REAR SPAR LKHEED1011 10113851 5265010WP WS 346 OVERSIZED HOLES A DALAK NONE O OTHER ININSP/MAINT 1 SO27721DA 193C1139 DURING ACCOMPLISHMENT OF PART 5 OF EO 7-56199-3AD, HOLES WERE OVERSIZED IN SEVERAL LOCATIONS, DUE TO REMOVAL OF EXISTING LOOSE FORCE MATE BUSHINGS. WING REAR SPAR IWS 346 MLG ATTACH FITTING INBD, OUTBD, UPPER AND LOWER 1.125 INCH HOLES. REPAIRED PER DL ERA 271059-14. 2L73 4F A23WE 19960216001601996021600160WP 1996 2 16 DLL17954179 119951003A32331591922 ACTUATOR FITIING LKHEED1011 10113853 5265020WP LT/RT MLG DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27765DA 193H1206 THE LT AND RT WING MLG ACTUATOR SUPPORT FITTING HAD THREE FASTENERS, IPC 57-14-0 FIG 1 ITEMS 280, 285, 300 ENT. THESE VERE REPLACED WITH HLT 104 BOLTS PER SRM 57-14-00 FIG 803. 2L73 4F A23WE 19960216001611996021600161NM 1996 2 16 DLM11954180 119951003A5720 DOUBLER DOUG MD11 MD11 3023602NM LT WING DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27802DE 48473 THE LT LOWER WING SPLICE DOUBLER WAS FOUND WITH A GROOVE IN THE TYPICAL LOCATION WITH THE MAX DEPTH BEYOND CONDITION 2 LIMITS STATED IN THE SERVICE BULLETIN MD11-53-048. ACCOMPLISHED REPAIRS PER DL ERA 271998-14. 2L73 4F RTA22WE 19960216001801996021600180NM 1996 2 16 96ZZZX634 119951218A7700 CONNECTORS DORNERDO32 DO328100 2996000NM RT ENGINE DIRTY A VNAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 GL07422JS 3018 FLT 4008 - SHORTLY AFTER TAKEOFF AT APPROXIMATELY 12,000 FEET MGL, RIGHT ENGINE BEGAN TO SURGE (ALL PARAMETERS). CREW ELECTED TO SHUT DOWN RIGHT ENGINE AND RETURN TO FIELD. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OUT-STATION MAINTENANCE REMOVED, CLEANED, AND RE-INSTALLED ENGINE ELECTRICAL HARNESS CANNON CONNECTORS FROM THE FOLLOWING ENGINE SENSORS, ECU, NP, NH AND TQ IAW MM 71-10-00. ENGINE GROUND RUNS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960216001831996021600183NM 1996 2 16 96ZZZX637 119951228A32302240500003 ROLLER MESSIER DORNERDO32 DO328100 2996000NM MLG LACK OF LUBE A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07434JS 3051 FLT 4022 - AFTER TAKEOFF, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. CREW CYCLED GEAR SEVERAL TIMES WITH NO SUCCESS. AIRCRAFT RETURNED TO FIELD, LANDED WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED LANDING GEAR SYSTEM, FOUND RT MAIN GEAR UPLOCK ROLLER IN NEED OF LUBRICATION. LUBRICATED RT AND LT MAIN GEAR UPLOCK ROLLERS IAW MM 32-10-00 AND STANDARD MAINTENANCE PRACTICES. FUNCTION CHECK FLIGHT (FCF) CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. 2H72 4T RTA45NM 19960216001861996021600186NM 1996 2 16 96ZZZX640 119951121A5315 FLOOR BEAM BOEING767 767205 1385121NM BS 1518 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05651TW 23058 MCI - DURING OP-16, FOUND CORROSION ON FLOOR BEAM CAP, STA 1518, RBL 18. REMOVED CORROSION AND REPAIRED PER SRM 53-00-51. AIRCRAFT TOTAL TIME: 38,181 HOURS; 13,720 CYCLES. 2L72 4F RTA1NM 19960216001871996021600187WP 1996 2 16 96ZZZX641 119951229A32603260001483 PROX BOX DOUG DC9 DC982 3022082WP LT MLG FAILED A TWAAO OTHER N FALSE WARNING APAPPROACH 1 CE05917TW 49366 LAX - FLT 39 - ON APPROACH DURING GEAR EXTENSION, LEFT MAIN RED GEAR LIGHT CAME ON. THE ALTERNATE GEAR EXTENSION METHOD WAS USED AND ALL LIGHTS FUNCTIONED PROPERLY. REMOVED AND REPLACED PROXIMITY BOX, MFG PN 3260-0014-83. OPERATIONAL CHECK NORMAL. CHECK C-2D 7-19-95 - MCI. 2L72 4F A6WE 19960216001881996021600188WP 1996 2 16 96ZZZX642 119951208A3222 STRUT DOUG DC9 DC983 3022083WP NLG REQUIRED SERVICEA TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE059404V 53140 STL - FLT 39 - AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT ON LANDING GEAR RETRACTION. CYCLED LANDING GEAR. FOUND NLG AIR CHARGE DEPLETED. SERVICED NLG WITH OIL AND NITROGEN. NLG LEAK CHECKED AND OPERATION CHECKED NORMAL. CHECK C-2D - 12-4-95 - JFK. 2L72 4F RTA6WE 19960216001891996021600189WP 1996 2 16 96ZZZX643 119951223A27611040T1005 ACTUATOR DOUG DC9 DC915 3022036WP SPOILER FAILED A TWAAO OTHER J WARNING INDICATION DEDESCENT 1 CE05975Z 47035 FSD - FLT 0663 - DURING DESCENT, AUTO GROUND SPOILER ACTUATOR FAILED. MFG PN 1040T100-5. PULLED CIRCUIT BREAKER AND PLACARDED. CHECKS MADE TO ASSURE NORMAL PERFORMANCE. POWERED AIRCRAFT, NO FURTHER. ELECTRICAL PROBLEM EXISTS. CHECK C 1-12-95 - STL. 2L72 4F A6WE 19960216001901996021600190WP 1996 2 16 96ZZZX644 119951220A3222A00314 SCHRADER VALVE DOUG DC9 DC982 3022082WP NLG STRUT FAILED A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05959U 49704 STL - FLT 255 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. CYCLED LANDING GEAR. FOUND NLG STRUT LOW ON AIR PRESSURE. REPLACED SCHRADER VALVE, MFG PN A00314. SERVICED NLG STRUT. LANDING GEAR OPERATION CHECKED NORMAL. CHECK C-1D - 7-28-95 - MCI. 2L72 4F A6WE 19960216001921996021600192WP 1996 2 16 96ZZZX646 119951210A253050198A COFFEEMAKER DOUG DC9 DC915 3022036WP GALLEY FAILED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE05490SA 45798 CID - FLT 64 - DURING CRUISE, FIRST CLASS COFFEEMAKER EMITTED SMOKE. TURNED OFF COFFEEMAKER AND OPENED CIRCUIT BREAKER. FOUND INTERNAL MALFUNCTION IN COFFEEMAKER. REPLACED COFFEEMAKER, MFG PN 50198A, AND OPERATION CHECKED NORMAL. CHECK C - 2-17-95 - MCI. 2L72 4F A6WE 19960216001931996021600193WP 1996 2 16 96ZZZX647 119951225A5220 SEAL DOUG DC9 DC932 3022066WP EMERGENCY EXIT FOD A VJ6AAB UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CLCLIMB 1 SO11904VJ 47377 IAD/MCO - FLT 467 - AFT AIRSTAIR LIGHT CAME ON AND CREW COULD NOT HOLD CABIN ALTITUDE. CABIN ROSE TO 8,000 FEET, DESCENDED AND RETURNED TO IAD. LANDED 3,000 POUNDS OVERWEIGHT. INSPECTED ALL AIRCRAFT DOORS AND SEALS. FOUND FOD ON RT FORWARD EMERGECY EXIT DOOR SEAL. REMOVED FOD. NO OTHER DEFECTS. PERFORMED PRESSURIZATION FUNCTIONAL CHECK IAW MM 21-30. PERFORMED OVERWEIGHT LANDING CHECK. 2L72 4F A6WE 19960216001951996021600195 1996 2 16 96ZZZX649 419951223A341651816007163 ALTIMETER DOUG DC9 DC932 3022066WP LEFT MALFUNCTIONED A VJ6AA UNSCHED LANDING O OTHER CRCRUISE 1 SO11967VV 47170 FLT 591 - AIR RETURN, ALTIMETER OFF 200 FEET AT ALTITUDE AND 120 FEET OFF ON ALTERNATE STATIC SOURCE. REMOVED AND REPLACED CAPTAIN'S AND FIRST OFFICER'S ALTIMETER. ACCOMPLISHED LEAK AND OPS CHECK GOOD. 2L72 4F A6WE 19960216001961996021600196 1996 2 16 96ZZZX650 419951223A341651816007163 ALTIMETER DOUG DC9 DC932 3022066WP RIGHT MALFUNCTIONED A VJ6AA UNSCHED LANDING O OTHER CRCRUISE 1 SO11967VV 47170 FLT 591 - AIR RETURN, ALTIMETER OFF 200 FEET AT ALTITUDE AND 120 FEET OFF ON ALTERNATE STATIC SOURCE. REMOVED AND REPLACED CAPTAIN'S AND FIRST OFFICER'S ALTIMETER. ACCOMPLISHED LEAK AND OPS CHECK GOOD. 2L72 4F A6WE 19960216001971996021600197EU 1996 2 16 96ZZZX651 119951213A3242AH52591 BRAKE AC036510 BAG JETSTMJETSTM3201 1500217EU RT MLG OUT OF ADJUST AS S4XAO OTHER O OTHER LDLANDING 1 WP27844JX 844 MFR - ON LANDING, RIGHT TOE PEDAL WAS NOT APPLYING PRESSURE TO RIGHT BRAKE. USED EMERGENCY BRAKE TO COME TO COMPLETE STOP ON RUNWAY WITHOUT INCIDENT. CHECKED RIGHT BRAKE MAXARET, FOUND TO BE CONTACTING MAIN WHEEL HUB. NUT RETAINING BOLT ADJUSTED. OPERATIONAL CHECK OF BRAKE SYSTEM GOOD. NO OTHER BRAKE PROBLEMS NOTED. 2L72 4T RTA56EU 19960216001981996021600198WP 1996 2 16 96ZZZX652 219951224A7250 TURBINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UAR 01514WP LT ENGINE DAMAGED A AS4XAF ACTIVATE FIRE EXT. A FLAME/FIRE ININSP/MAINT 1 WP27848JX 848 P66053C CREW WHILE PERFORMING FIRST FLIGHT OF DAY CHECKS (ON GROUND, TTL PORTION OF CHK), NOTED A LOUD POP FROM LT ENGINE FOLLOWED BY SMOKE FROM ENG COWLS. STOP & FEATHER LEVER PULLED. CREW NOTED FLAMES EMANATING FROM ENG INLET PRIOR TO PROP ROTATION STOPPING. NR 1 FIRE BOTTLE DISCHARGED. CREW NOTED NO FLAME OR SMOKE AFTER ENG SHUT-DOWN. PAX EVACUATED WITHOUT INCIDENT. PRELIMINARY INSPECT OF ENG REVEALED NR 3 TURBINE WHEEL OUTER ONE-THIRD OF BLADES CHIPPED/MISSING DUE TO IMPACT/RUBBING DAMAGE. DEBRIS FLOW ABRADED THROUGH AFT TURB BEARING OIL LINE SHROUD AND OIL LINE CAUSING OIL LEAKAGE INTO EXH DUCT. AWAITING ENG TEAR-DOWN FINDINGS FOR CAUSE OF ENG FAILURE. ENG: TSN 8138.9, CSN 9910, TSO 2961.2, CSO 3581. 2L72 4T4 TRTA56EU E4WE 19960216001991996021600199NE 1996 2 16 96ZZZX653 219951014A7530 STATOR VANES BOEING757 7572Q8 1384972NM PWA 2037 PW2040 NE LT ENGINE CRACKED A AMTAK NONE O OTHER CRCRUISE 1 GL11756AT4016 1317 27351 MDW - LEFT ENGINE SURGE DURING DECELERATION. ENGINE PARAMETERS NORMAL AFTER SURGE. REMOVED AND REPLACED LEFT ENGINE. FOUND CRACKED STATOR VANES. 2L72 4F4 FRTA2NM E17NE 19960216002011996021600201NM 1996 2 16 AALA951890 119951105A3350A3030398101 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07693AA 26973 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS IN FORWARD PART OF MAIN CABIN FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT FORWARD PART OF MAIN CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA2NM 19960216002021996021600202EU 1996 2 16 AALA951932 219951110A7230JR29549 HPC BLADE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAYMK65015 EU NR 2 ENGINE FAILED A AAALAO OTHER E VIBRATION/BUFFET CRCRUISE 1 SW071434A7575 11419 17410 MSP - FLT 0080 - EN ROUTE DFW/MSP, THE NR 2 ENGINE HAD HIGH N2 VIBRATIONS, PERFORMED ICE SHEDDING PROCEDURES AND NR 2 ENGINE FLAMED OUT. DESCENDED FROM 35,000 FEET TO 24,000 FEET AND ACCOMPLISHED SUCCESSFUL WINDMILL START, NR 2 ENGINE STILL HAD N2 VIBRATIONS. KEPT NR 2 ENGINE AT 50 PERCENT THROTTLE, LANDED MSP WITHOUT INCIDENT. NO OTHER ABNORMAL INDICATIONS OCCURRED. REPLACED NR 2 ENGINE IAW 72-00-00-5 AND 71-00-00-4, RUN-UP OK. SHOP FINDINGS: ONE EACH HPC STAGE 1 BLADE FAILED AT MID-SPAN DUE TO POSSIBLE IMPACT DAMAGE AT LEADING EDGE RESULTING IN EXTENSIVE SECONDARY DAMAGE DOWNSTREAM IN HPC. ENGINE PROCESSED THROUGH SHOP AND RETURNED TO SERVICE. (X) 2L72 4F4 FRT 19960216002031996021600203EU 1996 2 16 AALA952122 119951221A7931 OIL PRESS TRANS FOKKERF28 F28MK0100 4990807EU NR 2 ENGINE DIRTY A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW071434A 11419 YYZ - FLT 1049 - EN ROUTE YYZ/LGA, THE NR 2 ENGINE LOW PRESSURE LIGHT ILLUMINATED ALONG WITH THE RED MASTER WARNING ALERT. RETARDED NR 2 ENGINE THROTTLE AND ALERT EXTINGUISHED. ADVANCED NR 2 ENGINE THROTTLE AGAIN, CAUSED ALERT TO RECUR. EMERGENCY DECLARED AND AIRCRAFT RETURNED TO YYZ AND LANDED WITHOUT INCIDENT. ACCOMPLISHED HIGH POWER ENGINE RUN, LOW POWER ENGINE RUN CARRIED OUT, OIL PRESSURE TRANS. CHECKED AND CLEARED. ALL INDICATIONS NORMAL. NO SAP INDICATIONS. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RT 19960216002131996021600213NM 1996 2 16 CAL960010 119951218A575365464321 SKIN BOEING737 737130 1384435NM LT TE MID-FLAP GOUGED A CALAK NONE O OTHER ININSP/MAINT 1 SW091421265664 19029 HOU - INSPECTION FOUND THE LEFT WING INBOARD MID-FLAP UPPER SKIN GOUGED AT INBOARD END. THE GOUGE APPROXIMATED AN AREA OF 1.7 INCH BY 3 INCHES. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5750-02421. (X) 2L72 4F A16WE 19960216002151996021600215NM 1996 2 16 CAL960012 119951224A5330 SKIN BOEING737 737130 1384435NM BS 235 PUNCTURED A CALAK NONE O OTHER ININSP/MAINT 1 SW091421265664 19029 HOU - INSPECTION FOUND A .25 INCH DENT WITH A .1250 INCH HOLE IN RT FUSELAGE SKIN AFT OF EXTERNAL POWER PANEL AT STA 235. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02346. (X) 2L72 4F A16WE 19960216002161996021600216NM 1996 2 16 CAL960013 119951215A5330 SKIN BOEING737 737130 1384435NM E E BAY CUTOUT CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091421265664 19029 HOU - INSPECTION FOUND CORROSION IN E AND E BAY CUTOUT SKIN AT STR 27R. DOUBLERS WERE INSTALLED IAW ECRA 5330-02350. (X) 2L72 4F A16WE 19960216002181996021600218NM 1996 2 16 CAL960044 119951219A57116545409 WEB BOEING737 737130 1384435NM REAR SPAR CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW091421265664 19029 HOU - INSPECTION FOUND 2 CRACKS ON REAR SPAR WEB AT RBL 54.21. ONE CRACK WAS 1.5 INCHES LONG AT UPPER PANEL, AND THE OTHER CRACK WAS 2.3 INCHES LONG AT LOWER PANEL. A REPAIR WAS INSTALLED IAW ECRA 5750-02420. (X) 2L72 4F A16WE 19960216002191996021600219WP 1996 2 16 CKSA95143 119951207A261289492603 CONTROL UNIT LKHEED1011 1011385115 5265015WP NR 2 ENGINE MALFUNCTIONED A CKSAOE OTHER ENGINE SHUTDOWN N FALSE WARNING DEDESCENT 1 GL23102CK38350 193N1198 KHUF - FLT 69407 - ON TOP OF DESCENT 'A' FIRE DETECTOR LOOP ILLUMINATED, 'B' WOULD NOT TEST. SECURED NR 2 ENGINE IAW SHUT DOWN PROCEDURES. RESET FAULT ISOLATION CONTROL UNIT TO BOTH POSITIONS. SYSTEM TESTS GOOD. (X) 2L73 4F A23WE 19960216002201996021600220WP 1996 2 16 CKSA95145 119951208A21105614845513 TURBO COMPRESSOR DOUG DC8 DC8F55 3021928WP NR 2 SEIZED A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23811TC59388 45883 KFWA - FUMES IN COCKPIT DURING CRUISE, SUSPECT NR 2 TURBO COMPRESSOR. FOUND NR 2 TURBO COMPRESSOR TO BE CAUSING FUMES. DMI NR 2 TURBO COMPRESSOR IAW ZIA MEL 21-1, LOG NR 22361 PLACARDS INSTALLED. REFERENCE MRR 95-145 OPEN/ORIG - FUMES IN COCKPIT DURING CRUISE, SUSPECT NR 2 COMPRESSOR. REMOVED AND REPLACED NR 2 TURBO COMPRESSOR SYSTEM. OPS AND LEAK CHECKS NORMAL IAW DC-8MM, PLACARD REMOVED. (X) 2L74 4F 4A25 19960216002211996021600221WP 1996 2 16 CKSA95161 119951215A3310BA170 BALLAST DOUG DC8 DC8F55 3021928WP RT COCKPIT FAILED A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23809CK64312 45803 KSFO/KLAX - FLT 69975 - FIRST OFFICER'S INSTRUMENT PANEL INTEGRAL LIGHTS' CIRCUIT BREAKER OPENED DUE TO SHORT (SMOKE IN COCKPIT). REPLACED BALLAST TRANSFORMER ON FIRST OFFICER'S INSTRUMENT PANEL. OPS CHECKS NORMAL. (X) 2L74 4F 4A25 19960216002221996021600222WP 1996 2 16 CKSA95164 119951218A2751 INDICATION LKHEED1011 1011385115 5265015WP FLAP/SLAT MALFUNCTIONED A CKSAO OTHER FN FLT CONT AFFECTED FALSE WARNING CLCLIMB 1 GL23102CK38461 193N1198 KSEA/KBYH - FLT 70083 - AFTER TAKEOFF ON FLAP RETRACT, 'FLAP/SLAT' LIGHT ON F/E ANNUNCIATOR PANEL ILLUMINATED AND SLATS REMAINED FULL EXTENDED. FLAPS CAME UP NORMAL. SLAT MONITOR SHOWED SLAT FULL 30 DEGREES AND 14 DEGREES GREEN. FORM 27-28-23-00. RESET SLAT LOCKS AND ASYMMETRY DETECTOR SYSTEM. SLATS OPS CHECK NORMAL, DURING SEVERAL CYCLES IAW MM 27-51-00. (X) 2L73 4F A23WE 19960216002231996021600223NM 1996 2 16 EISA95534 119951230A5210 DOOR BOEING727 727223 1384074NM FWD ENTRY CRACKED A EISAK NONE O OTHER ININSP/MAINT 1 SW07312NE 20193 FOUND 1 INCH CRACK IN TOP AFT CORNER OF MAIN ENTRY DOOR SKIN. REPAIRED PER SRM 52-00-3. (X) 2L73 4F A3WE 19960216002241996021600224NM 1996 2 16 PCAA9500254 119951214A2910DSCD40130180 TUBE ASSY DHAV DHC8 DHC8102 2809003NM NR 1 HYD SYST CRACKED A PCAAO OTHER KJ FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 EA13831EX 160 NR 1 HYDRAULIC SYSTEM CONTENTS WENT TO ZERO IN-FLIGHT. TROUBLESHOT, FOUND LINE AT PRESSURE MANIFOLD CRACKED, INSTALLED FLEX LINE IAW MM. RAN AIRCRAFT, OPERATIONAL AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 14,446. (X) 2H72 4T RTA13NM 19960216002251996021600225NM 1996 2 16 PCAA9500255 119951215A335010005511 LIGHT DHAV DHC8 DHC8102 2809003NM COCKPIT OUT OF POSITION A PCAAK NONE L NO TEST ININSP/MAINT 1 EA13829EX7831 060551 146 COCKPIT EMERGENCY LIGHT COMES ON INTERMITTENTLY. WHEN REMOVED FROM SOCKET LIGHT, OPERATES NORMALLY. REPOSITIONED LIGHT IN SOCKET, SAFTIED WITH BREAKAWAY WIRE, CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL CYCLES, 15,115. (X) 2H72 4T RTA13NM 19960216002261996021600226EU 1996 2 16 RAIA951131 119951126A3246AH52688 WHEEL JETAIRJETSTMJETSTM4101 1500501EU NLG OUT OF BALANCE A RAIAA UNSCHED LANDING E VIBRATION/BUFFET LDLANDING 1 CE03556HK142 41073 JFK - FLT 7735 - NOSE WHEEL VIBRATION, AIRCRAFT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE WHEEL ASSEMBLIES. (X) 2L72 4T RTA41NM 19960216002271996021600227EU 1996 2 16 RAIA951134 119951130A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU PASSENGER DOOR OUT OF ADJUST A RAIAK NONE N FALSE WARNING CRCRUISE 1 CE03434JX2242 41034 STL - FLT 7514 - PASSENGER DOOR ALIGNMENT MARK IS NOT ALIGNED. MAINTENANCE ADJUSTED PASSENGER DOOR FORWARD AND AFT WARNING SWITCHES. SYSTEM CHECK GOOD. (X) 2L72 4T RTA41NM 19960216002281996021600228EU 1996 2 16 RAIA951137 119951129A273114127176419 CONTROL CABLE JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR TRIM OUT OF ADJ A RAIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 CE03558HK120 41071 DCA - MAINTENANCE - ELEVATOR TRIM HARD TO OPERATE MANUALLY. MAINTENANCE ADJUSTED CABLE TENSION ON ELEVATOR TRIM PER J4101 MM 273500, PAGE 563. FUNCTIONAL CHECK GOOD PER J4101 MM 273500, PAGE 526. (X) 2L72 4T RTA41NM 19960216002291996021600229EU 1996 2 16 RAIA951207 119951204A3397LE146N WIRE JETAIRJETSTMJETSTM4101 1500501EU CABIN LOOSE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03552HK1491 41057 STL - FLT 7460 - EMERGENCY LIGHTS NOT ILLUMINATING WHEN FLIGHT ATTENDANT'S SWITCH TURNED ON, AND NO POWER SUPPLIED TO AIRCRAFT. (X) 2L72 4T RTA41NM 19960216002301996021600230EU 1996 2 16 RAIA951214 119951210A27317005383921 SERVO MOTOR JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR TRIM FAILED A RAIAO OTHER F FLT CONT AFFECTED CRCRUISE 1 CE03558HK154 41071 JFK - FLT 7740 - ELEVATOR TRIM WHEEL BINDS AT TIMES. OTHER TIMES, IT IS OK. MAINTENANCE REPLACED ELEVATOR TRIM SERVO MOTOR. OPERATIONAL CHECK GOOD OF THE SYSTEM PER J4101 MM 271025. (X) 2L72 4T RTA41NM 19960216002311996021600231EU 1996 2 16 RAIA951219 119951212A527091SE16 SWITCH JETAIRJETSTMJETSTM4101 1500501EU CARGO DOOR OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03556HK598 41073 STL/ORF - CARGO DOOR WARNING ILLUMINATED ON TAKEOFF. MAINTENANCE ADJUSTED MICROSWITCH SYSTEM, CHECK GOOD. (X) 2L72 4T RTA41NM 19960216002321996021600232EU 1996 2 16 RAIA951225 119951219A27317005383921 TRIM SERVO JETAIRJETSTMJETSTM4101 1500501EU ELEVATOR TRIM STICKING A RAIAK NONE O OTHER ININSP/MAINT 1 CE03557HK397 41074 DCA - MAINTEANNCE - ELEVATOR TRIM STIFF. REPLACED ELEVATOR TRIM SERVO. (X) 2L72 4T RTA41NM 19960216003061996021600306WP 1996 2 16 ABXA9600174 119950907A532059560655 PRESS PANEL DOUG DC9 DC932 3022066WP FS 699 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23989AX 47314 DURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT SLANT PRESSURE PANEL AT FS 699. REPLACED THE LEFT SLANT PRESSURE PANEL IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960216003311996021600331NE 1996 2 16 96ZZZX655 219951212A7230 COMP BLADE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE LT ENGINE FAILED A AGUUAE ENGINE SHUTDOWN O OTHER APAPPROACH 1 SO19826BE1312 SH3745 MIA/MIA - FLT 104 (TRAINING) PILOT REPORT: ON SIMULATED MISSED APPROACH (TRANING), HEARD A LOUD BANG FROM LEFT ENGINE. ENGINE SHUT DOWN BY ITSELF, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE: LEFT ENGINE CHANGE IN PROGRESS FOR EVALUATION BY MANUFACTURER. PRATT AND WHITNEY HAS DETERMINED THE CAUSE TO BE CT BLADE FAILURE. 2H72 4T4 T A41EU E26NE 19960216003321996021600332SW 1996 2 16 96ZZZX656 119951218A291027810322684 HYDRAULIC LINE FRCHLDSA227 SA227DC 3377521SW RT NACELLE CRACKED A EQGAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 SW19847LS4749 DC847B HOT/STL - AFTER GAINING CRUISE ALTITUDE EN ROUTE, THE PILOT NOTICED THAT HYDRAULIC PRESSURE WAS FALLING AND DID FALL OFF COMPLETELY. THE PILOT THEN DIVERTED AND RETURNED TO HOT, LANDING WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THE RIGHT ENGINE MAIN HYDRAULIC LINE HAD CRACKED ALLOWING ALL FLUID TO BE DUMPED OVERBOARD. MAINTENANCE REPLACED THE LINE, CLEANED ENGINE AND WHEELWELL AREA, GROUND RAN AND ALL SYSTEMS CHECKED NORMAL. 1L72 4T RTA18SW 19960216003521996021600352WP 1996 2 16 ORJA95141 119951228A3350 COVER DOUG DC9 DC982 3022082WP CABIN BROKEN A ORJAK NONE O OTHER ININSP/MAINT 1 WP11821RA 49931 FLOOR LIGHT COVER BROKEN ON ROW 3. REMOVED AND REPLACED ROW 3 FLOOR LIGHT COVER. (X) 2L72 4F A6WE 19960216003561996021600356EU 1996 2 16 RAIA951226 119951220A521091SE16 HANDLE SWITCH BAG JETSTMJETSTM3201 1500217EU PASSENGER DOOR LACK OF LUBE A RAIAA UNSCHED LANDING ON OTHER FALSE WARNING CLCLIMB 1 CE03340TE7642 939 STL 7418 - PASSENGER DOOR LIGHT ILLUMINATES IN-FLIGHT. SYSTEM DEFERRED PER MEL 52-2. SUPPLEMENT - PASSENGER DOOR LIGHT ILLUMINATES IN-FLIGHT. MAINTENANCE LUBRICATED DOOR HANDLE. SYSTEM CHECK GOOD. AIRCRAFT TT, 7,642.0 HOURS. (X) 2L72 4T RTA56EU 19960216003571996021600357EU 1996 2 16 RAIA951227 119951224A77128972605 TRANSDUCER BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER O OTHER CLCLIMB 1 CE03971JX5308 971 FAT - FLT 4732 - LEFT ENGINE TORQUE DROPPED TO 25 PERCENT. MAINTENANCE REPLACED LEFT DELTA P/P TRANSDUCER. GROUND RUNS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19960216003581996021600358EU 1996 2 16 RAIA951228 119951222A32305EN16N95 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG DIRTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03434AM14447 887 COU - FLT 7042 - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE CLEANED AND LUBED NOSE GEAR SQUAT SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (X) 2L72 4T RTA56EU 19960216003941996021600394NM 1996 2 16 DL72E960315 119951009A5754 RIB BOEING727 727247 138408FNM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27283WA 21485 DURING SHOP INSPECTION, RIBS NR 2 AND NR 3 WERE FOUND TO BE CRACKED. REPAIRS WERE MADE AS PER M/M 57-54-0. ALSO, THE LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0, FOR NR 7 L/E SLAT. 2L73 4F A3WE 19960216004411996021600441WP 1996 2 16 UPS805446 119951229A5320 DOUBLER DOUG DC8 DC871F 302199DWP FS 35-55 CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01701 45938 WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 1 INCH LONG CRACK AT FUSELAGE DOUBLER FS 35 TO 55 LONGERONS 28L TO 30L. REPAIRED PER UPS EO. 2L74 4F RT4A25 19960216004981996021600498NE 1996 2 16 96ZZZM165 219951226A73103035681 FILTER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 CLOGGED AL SABAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO05881CC 294 121097 FLT NR 5052 HAD JUST ROTATED, WHEN THE NR 2 FUEL BYPASS CAPTION ILLUMINATED. THE FLIGHT CREW COMPLETED THE AIRCRAFT CHECKLIST AND RETURNED TO THE FIELD WHERE THEY MADE AN UNEVENTFUL LANDING. ONCE ON THE GROUND IT WAS NOTICED THAT THE BYPASS LIGHT HAD EXTINGUISHED. MAINTENANCE CONTROL WAS CONTACTED AND MECHANICS WERE DISPATCHED TO COLUMBUS, GA TO INVESTIGATE THE PROBLEM. MAINTENANCE PERFORMED A GROUND POWER RUN WITH NO DISCREPANCIES FOUND. AS A PRECAUTIONARY MEASURE THE HIGH PRESSURE FILTER ELEMENT WAS REPLACED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2H72 4T4 TRTA13NM E20NE 19960216005041996021600504EA 1996 2 16 96ZZZM171 119951222A3230LA11A21132 LINEAR ACTUATOR DHAV DHC7 DHC7102 2802708EA NOSE GEAR FAILED A HNAAK NONE J WARNING INDICATION TOTAKEOFF 1 EA07901HA19028 AL34836 042 FLT NR 3030 - DCA-ORF - AFTER TAKEOFF, WITH GEAR HANDLE UP, HANDLE GEAR TRANSIT LIGHT AND RED LIGHT STAYED ON FOR NOSE GEAR. THE AIRCRAFT CONTINUED ON TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG GROUND LOCK CABLE. LATER IN THE DAY, FLIGHT 3082, ORF-DCA, THE NOSE GAER WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SHUTTLE VALVE AND LINEAR ACTUATOR. (M) 2H74 4T A20EA 19960216005051996021600505EU 1996 2 16 96ZZZM172 119951231A3297 WIRE BAG JETSTMJETSTM3101 1500215EU LT MLG BROKEN A VNAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07836JS 732 FLT NR 4139 - GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. PIT - MAINTENANCE INSPECTED THE AIRCRAFT AND DISCOVERED A BROKEN WIRE IN THE LEFT MAIN LANDING GEAR WHEEL WELL. REPAIRED THE BROKEN WIRE IAW SID MX PRACTICES. RETURNED THE AIRCRAFT TO SERVICE. (M) 2L72 4T RTA21EU 19960216005081996021600508NM 1996 2 16 AALA951008 119950530A5754 SKIN BOEING767 767223 1385123NM NR 4 LE SLAT DAMAGED A AAALAO OTHER O OTHER CRCRUISE 1 SW07317AA 22319 SFO - FLT NR 682 - NR 4 SLAT LEADING EDGE HAS LARGE HOLE, NOTICED BY PASSENGER AFTER TAKEOFF AND CLIMB. NOTIFIED COCKPIT OF HOLE IN LEFT SLAT AND WAS CONFIRMED BY FLIGHT OFFICER. NO VIBRATION OR UNUSUAL FLIGHT CONTROL PRESSURE WAS FELT. ON LANDING WHEN FLAPS WERE EXTENDED BEYOND 1 DEGREE TO 5 DEGREE, VIBRATION WAS FELT. ELECTED TO LAND WITH 1 DEGREE FLAP. REMOVED AND REPLACED THE NR 4 LEADING SLAT PER MM, FUNCTIONAL CHECKS OK. NO DEFECTS NOTED, MM 27-B1-02-04. (M) 2L72 4F RTA1NM 19960216005091996021600509NM 1996 2 16 ASAA9540113 119951230A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01763AS 25100 SEA - FLT NR 54 - EMERGENCY EXIT FLOOR TRACK LIGHTS INOPERATIVE AT ROWS 15 AND 16. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960216005101996021600510NM 1996 2 16 ASAA9540114 119951230A3397 WIRE BOEING737 7374Q8 138447QNM CABIN DISCONNECTED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01765AS 25102 JNU - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED TRACK WIRING AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960216005111996021600511NM 1996 2 16 ASAA9540115 119951231A3350S417N5048 LIGHT BOEING737 7374Q8 NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01775AS 25108 ANC - DURING MAINTENANCE CHECK, THE FIRST EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND INOPERATIVE. REPLACED FORWARD LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960216005121996021600512NM 1996 2 16 ASAA9610001 119950103A21506068502 FAN BOEING737 737290C 138448VNM AIR COND SYS INOPERATIVE A ASAAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM01730AS8161 22577 JNU - ON ARRIVAL OF FLIGHT 66 - CREW REPORTED, BURNING ODOR IN COCKPIT AND AIR CONDITIONING FAN CIRCUIT BREAKER TRIPPED. ODOR DISSIPATED. RELEASED PER MINIMUM EQUIPMENT LIST ITEM 21-30. SUBSEQUENTLY CONFIRMED ABNORMAL NOISE AND A BURNING ODOR WHEN FAN WAS OPERATED. REPLACED AIR CONDITIONING FAN AND OPERATED NORMALLY. (M) 2L72 4F A16WE 19960216005501996021600550NM 1996 2 16 CKSA95165 119951218A32601361 BULB BOEING727 72722C 138400FNM NLG FAILED A CKSAO OTHER N FALSE WARNING CRCRUISE 1 GL23727CK54692 19195 BYH-EWR - NOSE GEAR LIGHT WENT OUT, CYCLED GEAR, LIGHT CAME ON NORMALLY. THEN WENT OUT AGAIN TURNING SWITCH TO BRIGHT LIGHT CAME ON AGAIN. CHECKED NOSE GEAR DOWNLOCK SWITCH FOR CONDITION/SECURITY, FOUND OK. RELAMPED NOSE GEAR INDICATION LIGHT CAPSULE. OPS CHECKS GOOD. (M) 2L73 4F A3WE 19960216005511996021600551WP 1996 2 16 CKSA95167 119951229A3310BA170 BALLAST DOUG DC8 DC863F 302198FWP COCKPIT FAILED A CKSAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL23867BX75855 46049 KTOL-KPHL - ELECTRICAL SMELL IN FRONT RIGHT SIDE OF COCKPIT. SUBMITTER STATES, SUSPECT RIGHT GLARESHIELD LIGHT, PULLED BREAKER. NO MORE SMELL, DEFERRED PER MEL 33-1 CAT C DMI NR 654. REPLACED LIGHT BALLAST TRANSFORMER ASSEMBLY. OPS CHECKED GOOD IAW DC-8 MM 33-12-0, DMI NR 654 CLEARED. (M) 2L74 4F 4A25 19960216005531996021600553WP 1996 2 16 GRAA9560 119951212A3350P4010021 BATTERY PACK DOUG DC9 DC915 3022036WP CABIN DISCHARGED A GRAAK NONE L NO TEST ININSP/MAINT 1 WP111064T 45778 DURING C-CHECK AT SOUTHWEST AERO TECHNOLOGIES, IN ROSWELL, NW, THE FORWARD EMERGENCY FLASHLIGHT WAS DISCOVERED TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLASHLIGHT. THE EMERGENCY FLASHLIGHT OPERATIONALLY CHECKED NORMAL. (M) 2L72 4F A6WE 19960216005561996021600556EA 1996 2 16 HNAA9590125 119951222A323050841 SHUTTLE VALVE DHAV DHC7 DHC7102 2802708EA NOSE GEAR FAILED A HNAAK NONE J WARNING INDICATION TOTAKEOFF 1 EA07901HA19028 0056 042 FLT NR 3030 - DCA-ORF - AFTER TAKEOFF, WITH GEAR HANDLE UP, HANDLE GEAR TRANSIT LIGHT AND RED LIGHT STAY ON FOR NOSE GEAR. THE AIRCRAFT CONTINUED ON TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG GROUND LOCK CABLE. LATER IN THE DAY, FLIGHT 3082, ORF-DCA, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LANDING GEAR SHUTTLE VALVE AND LINEAR ACTUATOR. (M) 2H74 4T A20EA 19960216005571996021600557NM 1996 2 16 HNAA9594226 119951222A2721682015 TRIM SW DHAV DHC8 DHC8102 2809003NM RUDDER FAILED A AHNAAO OTHER O OTHER CRCRUISE 1 EA07942HA17806 163 FLT NR 3064 - PBI-TPA - DURING FLIGHT, THE RUDDER TRIM MADE AN UNCOMMANDED RIGHT TRIM. THE PILOT RETURNED THE SWITCH TO CENTER MANUALLY AND CONTINUED ON TO TPA WITHOUT INCIDENT. REMOVED AND REPLACED THE RUDDER TRIM SWITCH. (M) 2H72 4T RTA13NM 19960216005591996021600559NM 1996 2 16 MZZA95057 119951231A2782269002911 ACTUATOR BOEING727 727224 1384076NM NR 5 LE SLAT FAILED A MZZAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 WP1369742 16050 1396 22251 GUM - FLT NR 981 - AIRCRAFT DIVERTED BACK TO GUAM DUE TO LOSS OF 'A' SYSTEM HYDRAULIC QUANTITY. MAINTENANCE DISCOVERED THAT NR 5 LEADING EDGE SLAT ACTUATOR FAILED AND LEAKS. MECHANIC REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR ASSY, SERVICED HYDRAULIC SYSTEM AND OPERATION CHECKED SYSTEM. AIRCRAFT RETURN BACK IN SERVICE. (M) 2L73 4F A3WE 19960216005601996021600560NM 1996 2 16 MZZA95058 119951230A3350900835A BATTERY BOEING727 727212 138407GNM CABIN DISCHARGED A MZZAK NONE L NO TEST ININSP/MAINT 1 WP13296AS 21459 GUM - ON SERVICE CHECK, FOUND AFT EXTERNAL EMERGENCY LIGHT AFT OF LEFT INBOARD FLAP INOP. MECHANIC REPLACED BATTERY PACK ASSY AND SYSTEM FUNCTION CHECK GOOD. (M) 2L73 4F A3WE 19960216005611996021600561NM 1996 2 16 MZZA9555 119951208A3350 COVER BOEING727 727224 1384076NM DOOR EXIT SIGN BROKEN A MZZAK NONE O OTHER ININSP/MAINT 1 WP1369741 22250 TNN - DURING 1/2 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON RIGHT FORWARD EMERGENCY EXIT DOOR 'EXIT' SIGN COVER. THE DAMAGED EXIT SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-10 ASSY PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTORY. HANGAR NON ROUTINE REPAIR ITEM CARD NR 832332 (SEQ NR 02142). (M) 2L73 4F A3WE 19960216005621996021600562NM 1996 2 16 MZZA9556 119951205A339769459345 WIRE BOEING727 727224 1384076NM EMER EXIT DOOR BROKEN A MZZAK NONE L NO TEST ININSP/MAINT 1 WP1369741 22250 TNN - DURING 1/2 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRE WERE FOUND ON RIGHT FORWARD OVERWING EMERGENCY ESCAPE HATCH STEP FORWARD CABLE. THE DAMAGED CABLE ASSY WAS REMOVED AND REPLACED PER B727 MM 52-21-0. HANGAR NON ROUTINE REPAIR ITEM CARD NR 832312 (SEQ NR 02092). (M) 2L73 4F A3WE 19960216005651996021600565EU 1996 2 16 PLG122795E1 119951223A3020ND00752200 THERM CONTROLLER SAAB SF340 SF340A 7850100EU RIGHT FAILED A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05741BA L243655 340A090 FLT NR 4959 - JFK-BWI - DURING CLIMB-OUT, THE RIGHT INTAKE HEAT FAILED. DUE TO EXISTING WEATHER CONDITIONS, THE AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO PSM FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED THE THERMAL CONTROLLER AND THE SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19960216005661996021600566EU 1996 2 16 PLG122795E2 319951219A6112660714246 LEAD SAAB SF340 340B 7860101EU LT PROP CHAFED A PLGAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 NE05352BE 340B239 FLT NR 4909 - BOS-BUF - DURING CLIMB-OUT, THE LEFT PROP DE-ICE FAILED. DUE TO EXISTING WEATHER CONDITIONS THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A CHAFED DE-ICE LEAD AND PERFORMED OPS CHECK OF THE SYSTEM. NO FAULT WAS FOUND. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA52EU 19960216005971996021600597WP 1996 2 16 WTAA950327 219951228A732189737526 FCU BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LT ENGINE FAILED A AWTAAAE UNSCHED LANDING ENGINE SHUTDOWN O OTHER CLCLIMB 1 WP17103XV 747 SEA - LEFT ENGINE POWER SURGE PLUS AND MINUS 20 TO 30 PERCENT REPORTED AFTER DEPARTURE. CREW SECURED LEFT ENGINE AND RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE FUEL CONTROL UNIT. ENGINE GROUND RUNS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19960216005981996021600598WP 1996 2 16 WTAA950328 219951228A732089737526 FCU BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LEFT ENGINE OUT OF ADJUST A WTAACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 WP17331CA 793 LAX - LEFT ENGINE FAILED TO DEVELOP REQUIRED TAKEOFF POWER. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT ENGINE FUEL CONTROL UNIT RIGGING. ENGINE GROUND RUN NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T4 TRTA21EU E4WE 19960216005991996021600599SO 1996 2 16 WTAA950330 119951229A524612016900010 FUEL SERV DOOR EMB 120 EMB120RT SO RT WING UNSECURED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP17280UE 120090 LAX - TAKEOFF ABORTED WITHOUT INCIDENT. SERVICE DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. MAINTENANCE RESECURED FUEL SERVICE DOOR CAM LOCK. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA31SO 19960216006051996021600605SO 1996 2 16 WTAA960006 119951226A3150MS33202 CIRCUIT BREAKER EMB 120 EMB120RT SO COCKPIT TRIPPED A WTAACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 WP17280UE 120090 FAT - TAKEOFF ABORTED WITHOUT INCIDENT. ELEVATOR TRIM WARNING ACTIVATED DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE. RESET AURAL WARNING SYSTEM CIRCUIT BREAKER. (M) 2L72 4T RTA31SO 19960216006511996021600651CE 1996 2 16 96ZZZX664 119950912A3222 STRUT LEAR 35 35A 5170602CE NLG REQUIRED SERVICEA JIKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP01128CA 248 AIRCRAFT RETURNED TO BASE AFTER GEAR INDICATED UNSAFE FOLLOWING RETRACTION. SAFE INDICATION ACHIEVED UPON GEAR EXTENSION. NOSE STRUT PRESSURE WAS LOW, SO STRUT DID NOT FULLY EXTEND AFTER ROTATION, THUS, WOULD NOT PROPERLY ACTIVATE UP-LIMIT SWITCH. SERVICED STRUT, PERFORMED GEAR RETRACTION TEST WITHOUT FURTHER FAULT. 2L72 4F A10CE 19960216006521996021600652EA 1996 2 16 96ZZZX665 219950930A8500 ENGINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE MALFUNCTION A JIKAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP013BT AFTER TAKEOFF, RT ENGINE SURGED AND PILOT NOTICED A DROP IN FUEL FLOW. PILOT ELECTED TO RETURN TO BUR. PERFORMED COMPRESSION CHECK, CHECKED PROP DOME PRESSURE, CHECKED SPARK PLUGS AND MAG TIMING, CHECKED FUEL INJECTOR FLOW, AND CHECKED DENSITY CONTROLLER CONDITION AND ADJUSTMENT. NO DISCREPANCIES FOUND. PERFORMED ENGINE GROUND RUNS WITH NO DEFECTS NOTED. SUBSEQUENT FLIGHT HAD NO DIFFICULTIES. 1L72 3O3 O A20SO E14EA 19960216006531996021600653SO 1996 2 16 96ZZZX666 119950915A28424064803 SENDER 40518XX PIPER PA31 PA31310 7103103SO MAIN OTBD WRONG PART A AJIKAK NONE W INADEQUATE Q C ININSP/MAINT 1 WP019132Y 31178 A MECHANIC WAS PERFORMING MX RUN-UP ON A STRAIGHT NAVAJO, WHEN BOTH ENGINES QUIT DUE TO FUEL STARVATION. PRIOR TO THE RUN, HE HAD CHECKED FUEL QUANTITY INDICATORS, WHICH SHOWED ONE-FOURTH TANK IN EACH MAIN TANK. THE MAIN (INBOARD) TANK HAS 2 SENDERS, AN INBOARD (40648-03) AND AN OUTBOARD (40648-02); INBOARD SENDER IS LONGER THAN OUTBOARD. INVESTIGATION SHOWED THAT IN THIS ACFT, THE 2 SENDERS HAD BEEN SWITCHED. WHEN LONGER SENDER IS PUT IN OUTBOARD LOCATION, IT WILL HIT BOTTOM OF TANK, GIVING A FALSE ONE-FOURTH FULL INDICATION. THIS IS SECOND TIME THIS CONDITION HAS BEEN FOUND IN THE LAST 6 WEEKS. WHILE BOTH INCIDENTS INVOLVED 31-310'S, PARTS, & POTENTIAL FOR PROBLEM, IS SAME IN PA31350 CHIEFTANS. 1L71 3O RTA20SO 19960216006541996021600654SO 1996 2 16 96ZZZX667 119951120A52804752932 HINGE 4752930 PIPER PA31 PA31350 7103110SO LT INBD GR DOOR CRACKED A JIKAK NONE O OTHER ININSP/MAINT 1 WP01600TS 317305047 MAINTENANCE FOUND LT GR DOOR HINGE CRACKED AT CASTING'S 90 DEGREE BEND INNER RADIUS. PART HAD NOT YET FAILED -- CRACK WAS VISIBLE TO THE EYE, AND WAS THROUGH ABOUT 20 PERCENT OF THE MATERIAL. M OR D WAS FILED IN JULY FOR THE CORRESPONDING HINGE ON THE RT GR DOOR. 1L72 3O A20SO 19960216006551996021600655CE 1996 2 16 96ZZZX668 119951018A272050600016 TUBE COLLAR BEECH 99 C99 1154006CE RUD TORQUE SHEARED A AJIKAK NONE O OTHER ININSP/MAINT 1 WP01113GP U211 THIS REPORT FULFILLS REQUIREMENTS OF 14CFR135.415(C). ACFT PURCHASED, USED, FROM BEECH FACTORY & FERRIED TO WEST COAST MX BASE FOR FULL INSP PRIOR TO PLACEMENT ON PART 135 CERTIFICATE. UPON ARRIVAL IN MX HANGAR, FOUND RUDDER MOVED FREELY, INDEPENDENT OF RUDDER CONTROL SYS. SKIN AT HINGE POINTS TORN & PEELED BACK, INDICATING DAMAGE FROM MOVEMENT BEYOND STOPS. FOUND THE TEN AN470AD RIVETS & ONE AN23-42A BOLT WHICH ATTACH PN 50-600016 COLLAR (IPC NOMENCLATURE "FITTING, BELLCRANK") TO PN 96-630000-179 RUDDER TORQUE TUBE (IPC NOMENCLATURE 'WELD ASSEMBLY') SHEARED. OTHER EXCESSIVE WEAR IN EMPENNAGE FLT CONTROL SYSTS INDICATED AREA HAD NOT BEEN PROPERLY INSPECTED FOR SOME TIME. A/C TT 19,120 HRS. 1L72 3T A14CE 19960216006561996021600656SO 1996 2 16 96ZZZX669 119950928A214065D792 HEATER JANITROL PIPER PA31 PA31350 7103110SO CABIN LEAKAGE A JIKAK NONE O OTHER ININSP/MAINT 1 WP0162858 41 1801305 317652115 THIS REPORT IS SUBMITTED IAW 14CFR135.415(A)(5). PILOT REPORTED THE CARBON MONOXIDE INDICATOR TURNED DARK WITH THE HEATER ON. MAINTENANCE PERFORMED DECAY TEST PER JANITROL MANUAL, WITH NO DEFECTS FOUND. HOWEVER, IT WAS FOUND THE GROUND VENTILATION FAN WAS INOPERATIVE. SUSPECT THAT OVERHEAT CONDITION DURING GROUND OPERATIONS WITH FAN INOP CAUSED POSSIBLE CRACKING IN COMBUSTION LINER WHICH FAILS TO INDICATE DECAY TEST AS DECAY TEST IS PERFORMED WHEN HEATER IS COLD. HEATER REMOVED FOR RETURN TO VENDOR. 1L72 3O A20SO 19960216006591996021600659SO 1996 2 16 96ZZZX672 119951107A32606775300 BRACKET 6792604 PIPER PA32 PA32R300 7103213SO LT MLG DNLOCK BROKEN AS JIKAK NONE O OTHER ININSP/MAINT 1 WP011333H 32R7780154 PILOT REPORTED LT MAIN GEAR GREEN LIGHT WOULD INTERMITTENTLY GO OUT WHILE TAXIING. MAINTENANCE FOUND THE SPRING ATTACH BRACKET WAS BROKEN RESULTING IN THE MAIN GEAR DOWNLOCK SPRING (PN 67203-00) NOT BEING ATTACHED TO THE TRUNNION. THE BRACKET (ITEM 14, FIG 55, PA 32R-300 PARTS CATALOG) IS MOUNTED TO THE TRUNNION UNDER THE SQUAT SWITCH, AND IS ATTACHED BY TWO BOLTS. THE EAR WHERE THE SPRING ATTACHES HAD BROKEN OFF, AND INDICATIONS ARE THAT IT WAS PREVIOUSLY CRACKED. A FLEET CAMPAIGN WILL BE INSTIGATED TO CHECK ALL 21 AIRCRAFT FOR CRACKS IN THIS LOCATION. 1L71 3O A3SO 19960216007261996021600726NM 1996 2 16 DL72K960333 119951205A575465162249092 RIB BOEING727 727232 1384082NM NR 8 SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27480DA 20860 DURING INSPECTION, FOUND NR 8 L/E SLAT WITH CRACKED SUPPORT RIB. REPAIRED PER MM 57-54-0. 2L73 4F A3WE 19960223001211996022300121NE 1996 2 23 96ZZZX737 119951227A2420 WIRE SKRSKYS76 S76A 8143006NE DL SW BOX CHAFED AS ALGAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW03768AL 760031 DURING FLIGHT, A ELECTRICAL SPARK WAS SEEN IN THE VICINITY OF THE OVERHEAD CIRCUIT BREAKER PANEL. REMOVED OVERHEAD ON PILOT'S SIDE AND FOUND A WIRE CHAFED AGAINST THE AFT RIGHT CORNER OF THE DL SWITCH BOX. CHAFE WAS REPAIRED. 1G72 3U H1NE 19960223001261996022300126SW 1996 2 23 96ZZZX742 119950825A6230206010443001 BEARING SET 206010450113BELL 206 206L1 1182107SW SWASHPLATE FAILED B ALGRK NONE O OTHER ININSP/MAINT 1 SW032025G1528 17512 45690 AT FIELD BASE FOUND SWASHPLATE BEARING BALLS WERE BREAKING DOWN. 1G71 3U H2SW 19960223001281996022300128GL 1996 2 23 96ZZZX744 219951117A7323355A5747221 SPRING AEROSPAS355 AS355F1 8680810EU ALLSN 250C 250C20 03013GL NR 2 ENG GOV BROKEN A ALGAO OTHER R PARTIAL RPM/PWR LOSS CRCRUISE 1 SW03372AL 5208 DURNG CRUISE FLIGHT, NR 2 ENGINE DROPPED TO FLIGHT IDLE. GOVERNOR SPRING ON NR 2 ENGINE WAS FOUND BROKEN. 1G72 3U3 U H11EU E4CE 19960223001311996022300131NM 1996 2 23 AALA951982 119951120A2810 SCREWS BOEING727 727223 1384074NM RT WING WORN A AALAAJ UNSCHED LANDING DUMP FUEL K FLUID LOSS CRCRUISE 1 SW07892AA 22008 SJU - FLT 0212 - AIRCRAFT WAS EN ROUTE STX/MIA, DUMPED FUEL AND DIVERTED TO SJU. EN ROUTE DURING CRUISE, FUEL SEEPAGE NOTED FROM AREA OF RT OUTBOARD AILERON. AIRCRAFT PROCEEDED SJU AND LANDED WITHOUT INCIDENT. REPLACED SCREWS IN FUEL TANK PANEL NR 4 INBOARD OF RT WING TIP. SYSTEM LEAK AND GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19960223001321996022300132NM 1996 2 23 AALA952010 119951128A3020 ANTIICE DUCT BOEING727 727223 1384074NM NR 1 ENGINE DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07883AA 21522 DFW - FLT 1264 - AFTER TAKEOFF DFW DURING CLIMB-OUT, LOWER AFT BODY OVERHEAT LIGHT CAME ON. CLOSED NR 1 BLEED AND LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NR 1 INLET COWL ANTI-ICE DUCT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L73 4F A3WE 19960223001331996022300133NM 1996 2 23 AALA952056 119951205A302065222723 DUCT BOEING727 727223 1384074NM NR 2 ENGINE RUPTURED A AALAO OTHER J WARNING INDICATION TOTAKEOFF 1 SW07865AA 21370 DFW - FLT 0471 - DURING MAXIMUM POWER TAKEOFF FROM ATL, AFT BODY OVERHEAT LIGHT ILLUMINATED. WHEN POWER WAS REDUCED, LIGHT EXTINGUISHED. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED DFW AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE NOSE COWL ANTI-ICE DUCT. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19960223001341996022300134EU 1996 2 23 AALA952058 119951205A361034H40600 COUPLING JANITROL AIRBUS300 A300B4605R 3930308EU NR 2 ENGINE BROKEN A AALAAE UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 SW0719059 469 SJU - FLT 0678 - AFTER TAKEOFF SJU DURING CLIMB-OUT, NR 2 ENGINE FIRE WARNING ILLUMINATED AND NR 2 ENGINE POWER LEVER BINDING NEAR TAKEOFF POWER SETTING. ACCOMPLISHED SHUT DOWN OF NR 2 ENGINE AND AIRCRAFT RETURNED SJU, LANDING WITHOUT INCIDENT. REPLACED NR 2 ENGINE LPT COOLING MANIFOLD AND BROKEN COUPLING. ACCOMPLISHED GROUND ENGINE RUN WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2L72 4F RTA35EU 19960223001351996022300135EU 1996 2 23 AALA952059 119951208A2932647520201 TRANSMITTER LUCAS AIRBUS300 A300B4605R 3930308EU GREEN HYD SYST DEFECTIVE A AALAO OTHER N FALSE WARNING LDLANDING 1 SW0780057 465 MIA - FLT 0095 - DURING DESCENT INTO MIA, GREEN HYDRAULIC SYSTEM RESERVOIR LOW LEVEL INDICATION AND RESERVOIR GAUGE DROPPED TO RED DOT. ACCOMPLISHED ALTERNATE LANDING GEAR EXTENSION AND AIRCRAFT LANDED MIA WITHOUT INCIDENT. GAUGE READING RETURNED TO NORMAL AFTER LANDING. REPLACED GREEN HYDRAULIC SYSTEM QUANTITY TRANSMITTER. ACCOMPLISHED LEAK AND SYSTEM GROUND CHECKS WITH NO DEFECTS FOUND. RETURNED LANDING GEAR SYSTEM TO NORMAL CONFIGURATION. (X) 2L72 4F RTA35EU 19960223001361996022300136NM 1996 2 23 AALA952060 119951208A3231651781915 LOCK ACTUATOR BOEING727 727223 1384074NM RT MLG DOOR DEFECTIVE A AALAO OTHER J WARNING INDICATION APAPPROACH 1 SW07862AA 21089 IAD - FLT 1654 - DURING APPROACH TO IAD WHEN LANDING GEAR EXTENDED, RT MLG DID NOT EXTEND. RECYCLED LANDING GEAR WITH SAME RESULTS. MANUALLY EXTENDED LANDING GEAR AND AIRCRAFT LANDED IAD WITHOUT INCIDENT. REPLACED RT MLG SEQUENCE DOOR LOCK ACTUATOR. ACCOMPLISHED GEAR DOWN MAINTENANCE FERRY IAD/DCA. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19960223001371996022300137NM 1996 2 23 AALA952091 119951215A3233657276235 ACTUATOR BOEING727 727223 1384074NM NLG DEFECTIVE A AALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW07869AA 21374 TUL - FLT 1923 - AFTER TAKEOFF TUL DURING GEAR RETRACTION, THE GEAR DOOR LIGHT STAYED ON AS WELL AS THE RED NOSE GEAR LIGHT. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR RETRACT ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L73 4F A3WE 19960223001381996022300138 1996 2 23 AALA952107 419951220A2564D23835203 RAFT BOEING727 727227 1384078NM FWD STORAGE COMPDEFECTIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07716AA A530 20608 LAX - DURING SHOP TEST DEPLOYMENT, EMERGENCY EVACUATION RAFT HAD SEAM SEPARATION. EMERGENCY EVACUATION RAFT SCRAPPED. (X) 2L73 4F A3WE 19960223001391996022300139NM 1996 2 23 AALA952121 119951221A32341U13021 SELECTOR VALVE RONSON BOEING767 767223 1385123NM LT MLG DEFECTIVE A AALAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 SW07303AA 22309 MIA - FLT 1165 - DURING APPROACH WHEN EXTENDING THE LANDING GEAR, THE GEAR DID NOT EXTEND. DID GO-AROUND AND CYCLED GEAR WITH SAME RESULT. ACCOMPLISHED ALTERNATE GEAR EXTENSION, DID FLYBY TO CONFIRM GEAR EXTENSION, AND LANDED MIA WITHOUT INCIDENT. REPLACED MAIN GEAR SELECTOR VALVE, ACCOMPLISHED GEAR SWING, AND REPLACED RT MLG FORWARD DRAG BRAKE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA1NM 19960223001401996022300140NM 1996 2 23 AALA952138 119951227A25308609010000 OVEN BOEING767 767223 1385123NM NR 1 DEFECTIVE A AALAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SW07325AA 22326 LHR - FLT 0116 - EN ROUTE JFK/LHR DURING CRUISE, ELECTRICAL SMOKE ODOR NOTED EITHER FROM OVENS 1 OR 2 IN FIRST CLASS GALLEY. PULLED CIRCUIT BREAKERS TO OVENS 1 AND 2 AND AIRCRAFT PROCEEDED TO LHR LANDING WITHOUT INCIDENT. CLEANED NR 2 OVEN IN FIRST CLASS GALLEY AND RESET CIRCUIT BREAKER. OVEN GROUND CHECKED NORMAL OPERATION. DEFERRED OVEN NR 1 IN FIRST CLASS GALLEY DUE TO FAILED COOLING FAN. SUBSEQUENTLY. REPLACED NR 1 OVEN IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERTION. (X) 2L72 4F RTA1NM 19960223001411996022300141EU 1996 2 23 AALA952144 119951227A2912695501AA000PC0A FILTER ASSY AIRBUS300 A300B4605R 3930308EU TAIL SECTION DEFECTIVE A AALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0711060 470 SJU - FLT 1170 - AFTER TAKEOFF, AIRCRAFT FILLED WITH SMOKE AND HYDRAULIC ODOR. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED HIGH PRESSURE FILTER ASSEMBLY FOR THE BLUE HYDRAULIC SYSTEM AND YELLOW HYDRAULIC SYSTEM RESERVOIR PRESSURE RELIEF VALVE. ACCOMPLISHED FUNCTIONAL CHECK FLIGHT AND BURNED OFF REMAINING ODOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA35EU 19960223001421996022300142NE 1996 2 23 AALA952162 219951016A7314 FUEL PUMP DOUG DC9 DC982 3022082WP PWA JT8 JT8D217A 52053NE RT ENGINE FAILED A AALAEA ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SW07418AA 49329 ABQ - FLT 1262 - AFTER TAKEOFF ABQ DURING CLIMB-OUT, RT ENGINE FLAMED OUT. ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE AND AIRCRAFT RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. CHECKED ENGINE INLET, EXHAUST AND FUEL PUMP FILTER WITH NO DEFECTS OR DISCREPANIES NOTED. REPLACED RT ENGINE DRIVEN FUEL PUMP AND FUEL CONTROL. ACCOMPLISHED LEAK CHECK AND GROUND ENGINE RUN WITH NO DEFECTS FOUND. (X) 2L72 4F4 F A6WE E9NE 19960223001851996022300185NM 1996 2 23 DL72S960376 119951201A53306554590 SKIN BOEING727 727232 1384082NM FS 680-720 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 DURING INSPECTION, CORROSION WAS FOUND IN SCATTERED LOCATIONS FROM STA 680 TO 720, BETWEEN S-26L AND 26R. ALSO, THERE WERE THREE EXISTING REPAIR DOUBLERS ON THE LOWER SKIN IN THE SAME AREA. IN ACCORDANCE WITH BAC/O S/B 727-53A203, RV 2, THE EXISTING EXTERNAL REPAIR DOUBLER AND THE DAMAGED SECTIONS OF SKIN WERE REPAIRED WITH A SKIN SPLICE, PER DL ERA 302834-14. 2L73 4F A3WE 19960223001861996022300186NM 1996 2 23 DL72S960377 119951203A5330 SKIN BOEING727 727232 1384082NM FS 700-706 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 DURING INSPECTION, MAINTENANCE FOUND THE UPPER SKIN AT THE S-26L LAP JOINT CORRODED BETWEEN STA 700 AND STA 706. DAMAGE REMOVAL RESULTED IN A 3 INCH BY 6 INCH CUT OUT AREA OF THE UPPER SKIN. ALSO, THE 0.020 2024-T3 CLAD BONDED DOUBLER BETWEEN THE UPPER AND LOWER SKINS IN THE LAP, WAS REMOVED FROM APPROXIMATELY BS 680 TO 712 TO REMOVE CORROSION. IN ACCORDANCE WITH B727 SRM 53-30-3, FIG 14, A DOUBLER WAS INSTALLED, REF DL ERA 302842-14. 2L73 4F A3WE 19960223001871996022300187NM 1996 2 23 DL72S960380 119951201A53306554590 SKIN BOEING727 727232 1384082NM FS-700 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27470DA 20747 DURING INSPECTION, CORROSION WAS FOUND IN THREE LOCATIONS BETWEEN STA 700 AND STA 720, S-27R AND S-28L. DAMAGE WAS MACHINED TO LEAVE A MAXIMUM THICKNESS OF 0.063 IN THE CLAD 2024-T3 SKIN. ALSO, THERE IS AN EXISTING EXTERNAL REPAIR DOUBLER, INSTALLED PER ER/A 208573-14 ON THE LOWER SKIN JUST AFT OF STA 720, ON S-28R. DOUBLER AND DAMGED SKIN WAS REMOVED AND A SKIN SPLICE WAS INSTALLED PER THE BOEING S/B 727-53A203, REV 2, REF DL ERA 302829-14AD. 2L73 4F A3WE 19960223001971996022300197NM 1996 2 23 DL767960375 119951231A5320146T802212 FAIL-SAFE CHORD BOEING767 767232 1385132NM FS 1540 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27106DA 22218 THE FUSELAGE RT SIDE AFT PASSENGER DOOR LOWER SILL INNER CHORD WAS FOUND WITH DEEP CORROSION ON THE ATTACHED FAIL-SAFE CHORD AT FS 1540. THE CORROSION IS OF DEPTH REQUIRING CUT OUT. THE CORROSION WILL BE REPAIRED IN ACCORDANCE WITH REF ER/A272246 REV C. 2L72 4F RTA1NM 19960223004361996022300436NM 1996 2 23 DL72S960392 119951202A5320 WEB BOEING727 727232 1384082NM FS 1273 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA 21153 DURING INSPECTION PER S/B 727-53-0129 IN ACCORDANCE WITH AD 94-07-08, THE INBD WEB WAS CUT TO THE BOTTOM EDGE OF THE WEB, THUS SEVERING. ALSO, SEVERAL OBLONG HOLES IN THE WEB WERE FOUND. ACCOMPLISHED REPAIRS PER FORM 8110-3, DATED 12-02-92, BACP TWX DA; -AT; 95-1303RR, REF DL ERA 302811 RC. 2L73 4F A3WE 19960223004371996022300437NM 1996 2 23 DL72S960393 119951220A5531 RIB TAB BOEING727 727232 1384082NM VERT STAB CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27493DA 21062 DURING INSPECTION, STRINGER 8R OF THE VERTICAL STAB. HAS A CRACK ON THE FIN STA. 157.2 RIB ATTACHMENT TAB. THE SUBJECT CRACK RUNS FROM FASTENER HOLE TO EDGE OF TAB. A REPAIR ANGLE WAS INSTALLED IN ACCORDANCE WITH B727 S/B 55-0075. 2L73 4F A3WE 19960223004381996022300438NM 1996 2 23 DL72S960394 119950316A5320651841483 WEB BOEING727 727232 1384082NM FS 294.5/285.5 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27468DA 20745 DURING INSPECTION, FOUND THE LT SIDEWALL WEB OF THE NOSE WHEEL WELL CRACKED BETWEEN STA 294.5 AND 285.5 APPROXIMATELY AT WL 170. THE CRACK IS APPROXIMATELY 1.75 INCH IN LENGTH. IN ACCORDANCE WITH S/B 727-53-145, THE WEB WAS TRIMMED OUT AND A REPAIR DOUBLER AND TWO STRAPS WERE INSTALLED. 2L73 4F A3WE 19960223004751996022300475NE 1996 2 23 96ZZZM175 219950116A7261 OIL LINE BOEING707 707323C 138367DNM PWA JT3D JT3D3B 52039NE NR 1 ENGINE FAILED A MIRAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19751MA 19582 645202 KMIA - SHUTDOWN NR 1 ENGINE AT 4:15 DUE TO LOSS OF OIL QUANTITY AND PRESSURE. FOUND HEAVY LEAK AT NOSE COWLING 4 O'CLOCK POSITION ON OIL PRESSURE LINE TO NR 1 BEARING DUE TO BROKEN O-RING. REMOVED AND REPLACED O-RING, SERVICED ENGINE AS REQUIRED, PERFORMING ENGINE RUNUP, NO LEAKS OBSERVED. OIL PRESSURE AND TEMPERATURE NORMAL IAW MM 71-00-00. (M) 2L74 4F4 F 4A26 1E8 19960223004761996022300476CE 1996 2 23 96ZZZM176 119951218A3260404EN1 SWITCH BEECH 1900 1900C 1154161CE LANDING GEAR LACK OF LUBE A GPPAO OTHER N FALSE WARNING CRCRUISE 1 CE0933014 UC13 EN ROUTE TO DEN ON FLIGHT 2110, LANDING GEAR INTRANSIT LIGHT ILLUMINATED WHEN GEAR WAS UP. FERRIED AIRCRAFT FROM DEN TO GRI. MAINTENANCE INSPECTED, CLEANED AND LUBED LANDING GEAR SWITCHES. AIRCRAFT PERFORMED A TEST FLIGHT. TEST FLIGHT WAS SATISFACTORY. 2L72 4T RTA24CE 19960223004771996022300477CE 1996 2 23 96ZZZM177 119951204A61235038912129 SWITCH BEECH 1900 1900C 1154161CE RT ENGINE INOPERATIVE A GPPAK NONE L NO TEST ININSP/MAINT 1 CE09129GP UC114 RIGHT AUTO FEATHER NOT TESTING PROPERLY ON GROUND. REMOVED AND RETURNED LOW PRESSURE SWITCH. OPS GOOD. (M) 2L72 4T RTA24CE 19960223004801996022300480NM 1996 2 23 96ZZZM180 119951215A2120 AIR DISTR BOEING727 727225 1384077NM CABIN SMOKE A UHVAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO17355PA 20625 SMOKE IN CABIN RIGHT PACK TURNED OFF, SMOKE CLEARED. ENGINES CHECK OK PER MM 72 PACK CHECK OK PER MM 21. UNABLE TO LOCATE SOURCE. CREW REPORTED OIL SMELL IN CABIN, NOT NOTICED IN COCKPIT. UNABLE TO LOCATE SOURCE THROUGH EXTENSIVE TROUBLESHOOTING. (M) 2L73 4F A3WE 19960223004811996022300481WP 1996 2 23 96ZZZM181 119951230A5312 BULKHEAD DOUG DC9 DC931 3022065WP LAVATORY FWD CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05987Z 47137 STL - DURING OP-15, FOUND .25 INCH CRACK IN AFT RIGHT LAVATORY FORWARD BULKHEAD, AT OUTBOARD CORNER AT FLOOR LINE. REPAIRED LAVATORY BULKHEAD PER SRM 53-03, FIGURE 31. 2L72 4F A6WE 19960223004831996022300483NM 1996 2 23 96ZZZM183 119951211A5712 RIB BOEING727 727231 1384079NM WS 629 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING C-CHECK, FOUND RIGHT WING TANK RIB CRACKED, LOWER STRINGER, 2ND STRINGER, STATION 629, FROM REAR. STOP DRILLED AND INSTALLED REPAIR PER SRM 57-10-5. 2L73 4F A3WE 19960223004841996022300484NM 1996 2 23 96ZZZM184 119951211A5320 PRESS DECK BOEING727 727231 1384079NM FS 948 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING C-CHECK, FOUND A .5 INCH CRACK IN LEFT WHEELWELL PRESSURE DECK, LBL 55, STATION 938, AND A .25 INCH CRACK, STATION 948. STOP DRILLED AND REPAIRED BY INSTALLING DOUBLER PER BOEING DWG 6589360. (M) 2L73 4F A3WE 19960223004851996022300485NM 1996 2 23 96ZZZM185 119951211A5712 RIB BOEING727 727231 1384079NM STA 601.5 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING C-CHECK, FOUND BOTTOM LEG OF RIB CRACKED ABOVE STRINGER 6, STATION 601.5. STOP DRILLED PER SRM 51-10-1 AND REPAIRED PER SRM 57-10-5. 2L73 4F A3WE 19960223004861996022300486NM 1996 2 23 96ZZZM186 119951211A5712 RIB BOEING727 727231 1384079NM ST 6865 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554330 20308 MCI - DURING C-CHECK, FOUND BOTTOM FLANGE OF RIB CRACKED ABOVE STRINGER 5, STATION 6865. STOPPED DRILLED CRACKS PER SRM 51-10-01 AND REPAIRED PER SRM 57-10-15, FIGURE 2 SHEET, 1 AND FIGURE 1, SHEET 3. (M) 2L73 4F A3WE 19960223004871996022300487NM 1996 2 23 96ZZZM187 119951211A5330 SKIN BOEING727 727231 1384079NM FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564319 20052 MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN FUSELAGE SKIN AT STRINGER 1, STRINGER BOX 1090, INSIDE CENTER ENGINE INLET HOUSING THROUGH BOTH SIDES OF RIVET HOLE, EXTENDING UNDER FAIRING HOUSING HATCH ANGLE. REPAIRED PER SERVICE BULLETIN 727-53A-0204. (M) 2L73 4F A3WE 19960223004881996022300488WP 1996 2 23 96ZZZM188 119951230A5330 SKIN DOUG DC9 DC983 3022083WP FS 740-750 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059304C 49530 MCI - DURING OP-16, FOUND CORROION LOWER FUSELAGE SKIN BETWEEN LONGERONS 27R AND 28R, STATION 740 TO STATION 750. REMOVED CORROSION PER SRM 51-10-3, INSTALLED REPAIR PER SRM 53-04, FIGURE 53. (M) 2L72 4F RTA6WE 19960223004891996022300489WP 1996 2 23 96ZZZM189 119951230A5330 SKIN DOUG DC9 DC915 3022036WP FS 817 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05969Z 47001 STL - DURING SPECIAL CHECK, FOUND ONE AND TWO INCH CRACKS IN FUSELAGE SKIN BETWEEN RIVETS AT STATION 817, LONGERON R9, AND A 1 INCH FUSELAGE SKIN CRACK AT STATION 817, LONGERONS R7-R8. REPAIRED PER SERVICE BULLETIN A53-147, AND DRAWING J060143. (M) 2L72 4F A6WE 19960223004901996022300490NM 1996 2 23 96ZZZM190 119950105A5320 DOOR FRAME BOEING727 727231 1384079NM CABIN DOOR CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0564319 20052 MCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN CABIN FORWARD DOOR FRAME RIGHT SIDE. REPAIRED PER SRM 51-40-3, FIGURE 1 AND TWA STANDARD PRACTICES. (M) 2L73 4F A3WE 19960223004911996022300491WP 1996 2 23 96ZZZM191 119951230A5330 SKIN DOUG DC9 DC931 3022065WP FWD FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05987Z 47137 STL - DURING OP-15, FOUND A TWO INCH CRACK IN FUSELAGE SKIN, FORWARD OF FIRST OFFICERS WIPER BLADE POST. REPAIRED PER ARA 10023. (M) 2L72 4F A6WE 19960223004941996022300494WP 1996 2 23 96ZZZM194 119951230A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 980 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05987Z 47137 STL - DURING OP-15, FOUND CORROSION AT TOP OF SCREW HOLE ON FLOOR BEAM OUTBOARD WALL OF RIGHT LAV, STATION 980. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ARA 10024. 2L72 4F A6WE 19960223004971996022300497WP 1996 2 23 96ZZZM197 119951228A5220 DOOR PAN DOUG DC9 DC931 3022065WP EMER EXIT CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05987Z 47137 DURING OP-15, FOUND THREE CRACKS, 1.5 INCH EACH, IN RIGHT FORWARD OVERWING EXIT DOOR PAN, UPPER AFT AND BOTH TOP CLIPS. INSTALLED DOUBLERS AND REPAIRED PER SRM 52-05, FIGURE 51 AND ARA 8897. (M) 2L72 4F A6WE 19960223005121996022300512WP 1996 2 23 96ZZZM212 119951211A5230 SEAL DOUG DC9 DC983 3022083WP CARGO DOOR CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CRACK AT AFT LATCH AREA OF MID CARGO DOOR SEAL RETAINER AND DOOR FRAME. REPAIRED PER SRM 52-05, PAGE 110A, FIGURE 26A. 2L72 4F RTA6WE 19960223005131996022300513NM 1996 2 23 96ZZZM213 119951220A5311 FRAME BOEING727 727231 1384079NM FUSELAGE CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0554332 20310 MCI - DURING C-CHECK, FOUND CRACK IN LEFT FUSELAGE FRAME AT 5TH HOLE FROME BOTTOM OF FUSELAGE FRAME. REPAIRED PER DWG NR 65C36280, SHEET 1. 2L73 4F A3WE 19960223005181996022300518WP 1996 2 23 USAA951327 119951215A5311 BELTFRAME DOUG DC9 DC982 3022082WP BS 408 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND .375 INCH CRACK AT STATION 408 LONGERON 17R BELTFRAME. SPLICED IN NEW SECTION OF BELTFRAME PER SRM 53-03 FIG 32. (M) 2L72 4F A6WE 19960223005191996022300519WP 1996 2 23 USAA951328 119951215A5315 FLOOR BEAM DOUG DC9 DC982 3022082WP BS 1322 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION ON UPPER AND LOWER HORIZONTAL FLANGE AND FWD FACE OF WEB AT STATION 1322 RIGHT SIDE FLOOR BEAM. CORROSION TASK C5853300. CLEANED OUT CORRODED AREA AND REPAIRED PER SRM 53-05 FIG 73A AND 79 AND USAIR EA 31736. (M) 2L72 4F A6WE 19960223005201996022300520WP 1996 2 23 USAA951329 119951215A5315 FLOOR BEAM DOUG DC9 DC982 3022082WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED AT STATION 1338 RIGHT AFT LAV FLOOR BEAM CAP. CORROSION TASK REF C58-53300. CUT OUT CORRODED AREA AND ACCOMPLISHED SPLICE REPAIR OF BEAM SECTION PER SRM 53-10-14. (M) 2L72 4F A6WE 19960223005211996022300521WP 1996 2 23 USAA951330 119951215A5313 LONGERON DOUG DC9 DC982 3022082WP BS 1338 CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19818US37663 48098 PIT - DURING Q-5 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED FROM LONGERON 28R-29R AT STATION 1338 T-CAP ANGLES AND WEB. CORROSION TASK REF C50-53300. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-10. (M) 2L72 4F A6WE 19960223005251996022300525NM 1996 2 23 USAA960016 119950105A5320 BEAM BOEING737 7372B7 1384560NM BS 297 CORROSION A USAAK NONE O OTHER ININSP/MAINT 1 EA19276AU34396 22888 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CORROSION NUT PLATE HOLE BEAM BS 297 LBL 10 INCH. REMOVED CORROSION AND INSTALLED STRAP. REPAIRED PER TR 53-10-01A. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2L72 4F A16WE 19960301000011996030100001NM 1996 3 1 AALA951971 119951120A5330 SKIN BOEING727 727227 1384078NM FS 590 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07726AA 20733 TUL - FUSELAGE SKIN CRACKED AT STA 590 AND STR 27L. CUT OUT CRACKED AREA AND INSTALLED DOUBLER PER SRM 53-30-3, PAGE 154, FIGURE 24, SHEET 1-4. TST 62,695 HOURS, CYCLES, 41,603. (X) 2L73 4F A3WE 19960301000021996030100002EU 1996 3 1 AALA952015 119951130A5320 SEAL SECTION AIRBUS300 A300B4605R 3930308EU PAX DOOR CUT OUTCORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - LOWER R-4 DOOR CUT OUT SEALING SECTION HAS CORROSION. INSTALLED NEW SEALING SECTION PER SRM 51-72-10. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000031996030100003EU 1996 3 1 AALA952022 119951130A5320A5398019520351 SEAL SECTION AIRBUS300 A300B4605R 3930308EU PAX DOOR CUT OUTCORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION ON SEALING SECTION AT RT MID-PASSENGER DOORWAY. INSTALLED NEW FACTORY SEALING SECTION PER SRM 53-10-72. TST: 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000041996030100004EU 1996 3 1 AALA952024 119951204A57204014285 ANGLE AIRBUS300 A300B4605R 3930308EU LT WING CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - LOWER WING PICKUP ANGLE AFT OF FRONT SPAR AT ROOT CRACKED FROM EDGE INTO FASTENER HOLE. REMOVED AND REPLACED PICKUP ANGLE WITH NEW PART. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000051996030100005EU 1996 3 1 AALA952034 119951204A5320A53981929203 ATTACH SECTION AIRBUS300 A300B4605R 3930308EU FUS CROWN CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION ALONG LENGTH OF ATTACH SECTION. REPLACED ATTACH SECTION PER SRM 51-70-00. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000061996030100006EU 1996 3 1 AALA952035 119951204A5320A53981929202 ATTACH SECTION AIRBUS300 A300B4605R 3930308EU FUS CROWN CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - DEEP CORROSION ALONG LENGTH OF ATTACH SECTION. REPLACED ATTACH SECTION PER SRM 51-70-00. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000071996030100007EU 1996 3 1 AALA952036 119951205A5712A5724199320020 RIBLET AIRBUS300 A300B4605R 3930308EU LT WING CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CRACK IN LOWER ANGLE OF LEADING EDGE FORMER/RIBLET OUTBOARD OF KRUEGER FLAP ACTUATOR BAY. STOP DRILLED CRACK AND INSTALLED REINFORCING ANGLE PER SRM 57-41-11 AND ESO 30595, DATED 10-5-95. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000081996030100008NM 1996 3 1 AALA952037 119951205A575165217097 CASTING BOEING727 727223 1384074NM LT AILERON CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07873AA 21385 TUL - CORROSION ON LOWER FACE OF CASTING UNDER NUT. REMOVED CORROSION FROM CASTING 65-21709-7 AND REPAIRED PER ESO 11697, DATE 11-27-95. TST, 49,577 HOURS. CYCLES, 30,842. (X) 2L73 4F A3WE 19960301000091996030100009EU 1996 3 1 AALA952038 119951205A5320 SEAL STRIP AIRBUS300 A300B4605R 3930308EU PAX DOORWAY CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION ON AFT SEAL STRIP RT MID-PASSENGER DOORWAY. REPLACED PART PER SRM 51-72-10. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000101996030100010EU 1996 3 1 AALA952039 119951205A5540A55471611000 FITTING AIRBUS300 A300B4605R 3930308EU RUDDER CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION AROUND LOWER CLEVIS BOLT (HINGE) HOLE. REPLACED RUDDER FITTING A5547161100 PER SRM 51-70-00. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000111996030100011EU 1996 3 1 AALA952040 119951206A5320 SEALING SECTION AIRBUS300 A300B4605R 3930308EU L-2 DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - AFT SEALING SECTION OF DOOR FRAME AT L-2 DOOR HAS CORROSION. INSTALLED NEW SEALING SECTION AT AFT SIDE OF L-2 DOOR FRAME PER SRM 51-74-00, PAGES 1-3. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000121996030100012EU 1996 3 1 AALA952041 119951206A5320 SEALING SECTION AIRBUS300 A300B4605R 3930308EU L-2 DOOR CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - AT FORWARD END OF L-2 DOOR FRAME, SEALING SECTION HAS CORROSION. INSTALLED NEW SEALING SECTION AT L-2 DOOR FRAME. PER SRM 51-74-00, PAGES 1-3. TST, 21,241.57 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000131996030100013EU 1996 3 1 AALA952042 119951206A5313 STRINGER AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION ON STRINGER AND FLANGE SUPPORT FOR DUCT. STR 45R AND FR 33-34. REMOVED CORROSION AND INSTALLED STRINGER DOUBLER REPAIR PER A300 SRM 53-10-14, PP 202. TREATED, PRIMED, AND PAINTED. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000141996030100014EU 1996 3 1 AALA952068 119951211A5400 LUG AIRBUS300 A300B4605R 3930308EU LT PYLON CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - CORROSION IN BORE OF LUG OF PYLON. LUG BORED AND RE-BUSHED ON SHOP HAND-WRITE C8HF. CORROSION REMOVED. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000151996030100015EU 1996 3 1 AALA952069 119951210A5542 SKIN AIRBUS300 A300B4605R 3930308EU RUDDER TE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - LOWER TRAILING EDGE HAS CORROSION. REPAIRED LOWER TRAILING EDGE PER SRM 55-41-12, PAGE 221M. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000161996030100016EU 1996 3 1 AALA952070 119951211A5320F53270510224 SPLICE AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - SPLICE PLATE HAS CORROSION ON TOP OF PLATE. INSTALLED EXTERNAL DOUBLER PER ESO 30595, DATED 12-7-95. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000171996030100017EU 1996 3 1 AALA952071 119951211A5311A53611499203 FRAME AIRBUS300 A300B4605R 3930308EU FRAME 18 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - BOTTOM OF FRAME HAS CORROSION ON FRAME FOOT. REPAIRED FRAME FOOT EPR ESO 30595, DATED 12-11-95. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000181996030100018EU 1996 3 1 AALA952072 119951211A5311A53611663200 FRAME AIRBUS300 A300B4605R 3930308EU FRAME NR 19 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - BOTTOM OF FRAME HAS CORROSION ON FRAME FOOT. REPAIRED FRAME PER ESO 30595, DATED 12-7-95. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000191996030100019EU 1996 3 1 AALA952077 119951212A5330A53773487200 SKI AIRBUS300 A300B4605R 3930308EU FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW0791050 423 TUL - AREA OF SKIN HAS CORROSION FROM STR 53L TO STR 54L. INSTALLED EXTERNAL DOUBLER PER ESO 30595, DATED 12-12-95. TST, 21,241.75 HOURS. CYCLES, 8,851. (X) 2L72 4F RTA35EU 19960301000491996030100049NM 1996 3 1 95UAL900358 119951227A2410699647 CSD BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 1 ENGINE FAILED A UALAO OTHER J WARNING INDICATION CRCRUISE 1 WP299012U 19050 IN CRUISE WHEN THROTTLES WERE RETARDED, NR1 CSD LOW OIL PRESSURE LIGHT CAME ON AND THEN WENT OFF, OCCURRED REPEATEDLY. ALSO, AUTOPILOT DISENGAGED MANY TIMES FOR NO REASON. REPLACED NUMBER ONE ENGINE CONSTANT SPEED DRIVE, OIL COOLER AND OIL FILTER. RAN ENGINE, SYSTEM CHECKS OK. SHOP FINDINGS FOUND CONSTANT SPEED DRIVE HAD INTERNAL FAILURE CAUSING THE LOW PRESSURE. 2L72 4F4 F A16WE E2EA 19960301000961996030100096NM 1996 3 1 DL72K960413 119950718A5754 SKIN 651622373 BOEING727 727232 1384082NM NR 2 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27481DA BN1037 20861 INNER TAI SKIN CRACKED BETWEEN RIBS 11 AND 12 AFT RIVET TAIL. REPAIRED PER MM 57-54-0 FIG 803A, FOR NR 2 L/E SLAT. FOUND DURING SHOP INSPECTION. 2L73 4F A3WE 19960301001111996030100111NM 1996 3 1 DL73S960415 119950925A575565C2524216A SKIN BOEING737 737232 1384475NM SPOILER TORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27322DL 23094 DUE TO THE FATIGUE FAILURE OF THE O/B ACTUATOR FITTING, THE FRONT SPAR AND THE UPPER SKIN OF THE SUBJECT SPOILER WERE TORN. IN ACCORDANCE WITH BACO S/B 737-57-1207, THE SKIN AND SPOILER WERE REPAIRED. 2L72 4F RTA16WE 19960301002011996030100201NM 1996 3 1 DL72S960426 119951103A5240 FRAME BOEING727 727232 1384082NM LT SERVICE DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27490DA 21020 DURING INSPECTION, A 2 INCH CRACK WAS FOUND EMANATING FROM THE CORNER OF THE UPPER HINGE CUTOUT ON THE FWD FRAME OF THE LT AFT SERVICE DOOR. IN ACCORDANCE WITH B727 SRM 52-40-2 FIG 4, A DOUBLER WAS INSTALLED AROUND THE DAMAGE. 2L73 4F A3WE 19960301002471996030100247WP 1996 3 1 96ZZZM215 119951211A5311 FRAME LKHEED1011 1011385115 5265015WP FS 689 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE0531031 193B1115 MCI - DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED RIGHT SIDE WL 280.6, STATION 689. INSTALLED REPAIR PER ARA 9471 AND TWA STANDARD PRACTICES. 2L73 4F A23WE 19960301002501996030100250WP 1996 3 1 96ZZZM218 119951211A5320 MEMBRANE DOUG DC9 DC983 3022083WP FS 1280 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND A 3 INCH CRACK LEFT SIDE AT SIDEWALL UNDER FLOOR MEMBRANE, FS 1280. REPAIRED PER SRM 53-05-96. 2L72 4F RTA6WE 19960301002521996030100252WP 1996 3 1 96ZZZM220 119951211A5347 SEAT TRACK DOUG DC9 DC983 3022083WP FS 1130/1142 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION ON NR 2 CHAIR TRACK, FS 1130 AND FS 1142. INSTALLED NEW TRACK PER SRM 51-01, PAGE 1. 2L72 4F RTA6WE 19960301002541996030100254WP 1996 3 1 96ZZZM222 119951220A5315 FLOOR BEAM DOUG DC9 DC983 3022083WP FS 1309 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND FLOOR BEAM CORROSION, FS 1309, LBL 45. REMOVED CORROSION PER SRM 51-10-3, REPAIRED BEAM PER SRM 53-05, FIGURE 20A. 2L72 4F RTA6WE 19960301002551996030100255WP 1996 3 1 96ZZZM223 119951220A5330 SKIN DOUG DC9 DC983 3022083WP BS 775-827 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND LOWER FUSELAGE SKIN CORROSION, STATION 775 TO 827, RB 273. REPAIRED EPR SRM 53-04, PAGE 321. 2L72 4F RTA6WE 19960301002561996030100256WP 1996 3 1 96ZZZM224 119951220A5315 FLOOR BEAM DOUG DC9 DC983 3022083WP FS 1211 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND FLOOR BEAM CORROSION BETWEEN FLOOR TRACKS, FS 1211. REPAIRED PER SRM 51-01, PAGE 1 AND TWA STANDARDS PRACTICES. 2L72 4F RTA6WE 19960301002571996030100257WP 1996 3 1 96ZZZM225 119951220A5330 SKIN DOUG DC9 DC983 3022083WP FS 1155-1212 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON FUSELAGE SKIN BELOW AFT CARGO BIN DOORWAY UNDER COVER PLATE, STATION 1155-1212. REMOVED CORROSION PER SRM 51-10-3. 2L72 4F RTA6WE 19960301002581996030100258WP 1996 3 1 96ZZZM226 119951220A5347 FLOOR TRACK DOUG DC9 DC983 3022083WP BS 200-240 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK NR 3, RBL 20, STATION 200-240. REPLACED TRACK PER SRM 53-05, PAGE 10G AND SRM 51-01, ITEM C. 2L72 4F RTA6WE 19960301002621996030100262WP 1996 3 1 96ZZZM230 119951220A5347 FLOOR TRACK DOUG DC9 DC983 3022083WP BS 1136 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK FORWARD OF AFT END OF TRACK AT SCREWS, LBL 36, STATION 1136. REMOVED CORROSION PER SRM 51-10-3, AND REPLACED TRACK PER SRM 51-10-1C. 2L72 4F RTA6WE 19960301002631996030100263WP 1996 3 1 96ZZZM231 119951220A5347 HOLD DOWN TRACK DOUG DC9 DC983 3022083WP FS 1302-1281 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON 'E' GALLEY AFT INBOARD HOLD DOWN TRACK, STATION 1302 TO STATION 1281. REPLACED TRACK PER SRM 53-03, PAGE 10G. 2L72 4F RTA6WE 19960301002641996030100264WP 1996 3 1 96ZZZM232 119951220A5311 FRAME DOUG DC9 DC983 3022083WP FS 1322 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND FORMER FRAME CORROSION BETWEEN LONGERONS 29L TO 29R, FS 1322. REPAIRED PER SRM 53-03, PAGE 4E AND SSRM 51-40-501. 2L72 4F RTA6WE 19960301002651996030100265WP 1996 3 1 96ZZZM233 119951220A5312 BLKHD SUPPORT DOUG DC9 DC983 3022083WP FS 1320 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON BULKHEAD SUPPORT MEMBER, FS 1320, LBL 25L TO LBL 31L. REPAIRED PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES. (M) 2L72 4F RTA6WE 19960301002661996030100266WP 1996 3 1 96ZZZM234 119951220A5320 SUPPORT BEAM DOUG DC9 DC983 3022083WP FS 1155 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON FLOOR PANEL SUPPORT BEAM BL, FS 1155. INSTALLED NEW BEAM PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES. 2L72 4F RTA6WE 19960301002671996030100267WP 1996 3 1 96ZZZM235 119951220A5320 FLOOR SUPPORT DOUG DC9 DC983 3022083WP FS 1155 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON RIGHT FLOOR SUPPORT, FS 1155. INSTALLED NEW FLOOR SUPPORT PER SRM 51-01, PAGE 1C AND TWA STANDARD PRACTICES. 2L72 4F RTA6WE 19960301002681996030100268WP 1996 3 1 96ZZZM236 119951220A5315 FLOOR BEAM DOUG DC9 DC983 3022083WP AFT LAV CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION AT FLOOR BEAM, LEFT AFT LAVATORY FORWARD BULKHEAD LOWER END. REPAIRED PER SRM 53-01, FIGURE 4, SHEET 3. 2L72 4F RTA6WE 19960301002691996030100269WP 1996 3 1 96ZZZM237 119951220A5321 FLOOR PANEL DOUG DC9 DC983 3022083WP FS 1305-1309 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CABIN FLOOR PANEL CORROSION, STATION 1305 TO STATION 1309. REPLACED FLOOR PAN PER SRM 51-10-01. 2L72 4F RTA6WE 19960301002701996030100270WP 1996 3 1 96ZZZM238 119951220A5347 CARGO TRACK DOUG DC9 DC983 3022083WP FS 1079-1222 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION ON LEFT FLOOR CARGO TRACK, FS 1079 TO FS 1222. INSTALLED NEW TRACK PER SRM 51-10, ITEM 1, FIGURE C AND INSTALLED SPLICE PER SRM 53-03, FIGURE 4G. 2L72 4F RTA6WE 19960301002711996030100271WP 1996 3 1 96ZZZM239 119951220A5320 ATTACH BRACKET DOUG DC9 DC983 3022083WP FS 1155 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION BOTTOM SIDE IN FORMER ATTACH BRACKET, FS 1155, LBL 7. REPAIRED PER SRM 51-01, PAGE 1, ITEM C AND TWA STANDARD PRACTICES. 2L72 4F RTA6WE 19960301002761996030100276WP 1996 3 1 96ZZZM244 119951220A5313 STRINGER DOUG DC9 DC983 3022083WP FS 1155 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION AT STRINGER WEB OF STRINGER 29L, FS 1155. REPAIRED PER SRM 51-10-3 AND TWA STANDARD PRACTICES. 2L72 4F RTA6WE 19960301002771996030100277WP 1996 3 1 96ZZZM245 119951220A5347 FLOOR TRACK DOUG DC9 DC983 3022083WP BS 160-200 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION ON FLOOR TRACK, STATION 160 TO STATION 200, RBL 53. REPLACED TRACK PER SSRM 51-10-01. 2L72 4F RTA6WE 19960301002781996030100278WP 1996 3 1 96ZZZM246 119951220A5320 ANGLE DOUG DC9 DC983 3022083WP FS 1155 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05931TW 49527 MCI - DURING OP-16, FOUND CORROSION ON FORMER TO STRINGER ATTACH ANGLE OF STRINGER 29L, FS 1155. REPAIRED PER SRM 51-01, PAGE 1, ITEM C AND TWA STANDARD PRACTICES. 2L72 4F RTA6WE 19960301002791996030100279WP 1996 3 1 96ZZZM247 119951220A5347 TIEDOWN TRACK DOUG DC9 DC983 3022083WP FS 1079-1109 CORRODED A TWAAK NONE O OTHER ININSP/MAINT 1 CE059303K 49529 MCI - DURING OP-16, FOUND CORROSION IN LEFT TIEDOWN TRACK, STATION 1079 TO STATION 1109. REPAIRED PER SRM 53-05, FIGURE 4G AND ARA 9859. 2L72 4F RTA6WE 19960301002821996030100282NM 1996 3 1 AALA952017 119951130A5315 FLOOR BEAM BOEING727 727223 1384074NM BS 1110 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07870AA 21382 TUL - FOUND CORROSION ON TOP OF FLOOR BEAM AT FASTENER HOLE STATION 1110 LBL 28 INCHES. CUT OUT DAMAGED AREA INSTALLED FILLER AND DOUBLER PER SRM 53-10-8 PG 9C 9D. (M) 2L73 4F A3WE 19960301002831996030100283NM 1996 3 1 AALA952019 119951130A5320 BEAM BOEING727 727223 1384074NM BS 1183 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW07870AA 21382 TULE - FOUND 1183 VERTICAL BEAM CRACKED IN OUTBOARD RADIUS LBL 8 LOWER END ONE INCH LONG. INSTALLED VERTICAL BEAM REPAIR PER SB 727-53-0175. 2L73 4F A3WE 19960301002841996030100284NM 1996 3 1 AALA952021 119951130A5512 SKIN BOEING727 727223 1384074NM LT ELEVATOR DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07870AA 21382 TULE - FOUND LEFT LOWER SURFACE OF ELEVATOR DAMAGED. REMOVED LOWER LEFT ELEVATOR SKIN AND REPLACED WITH NEW SKIN. (M) 2L73 4F A3WE 19960301002851996030100285NM 1996 3 1 AALA952073 119951212A5320657527259 INTERCOSTAL BOEING727 727223 1384074NM FS 990 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07891AA 22007 TULE - FOUND CORROSION ON LOWER INTERCOSTAL JUST AFT OF STATION 990 ABOVE STRINGER 30. REMOVED CORRODED INTERCOSTAL AND REPLACED WITH NEWLY MANUFACTURED INTERCOSTAL. (M) 2L73 4F A3WE 19960301002861996030100286NM 1996 3 1 AALA952074 119951212A5330 SKIN BOEING727 727223 1384074NM FS 720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07891AA 22007 TULE - FOUND CORROSION ON BELLY SKIN STATION 720B BETWEEN STATIONS 28 LT AND 28 RT. FABRICATED NEW PANEL AS PER SRM 51-20-1, PAGES 8-11. TREATED AND PRIMED. (M) 2L73 4F A3WE 19960301002871996030100287NM 1996 3 1 AALA952075 119951212A5330 SKIN BOEING727 727223 1384074NM FS 480-490 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07891AA 22007 TULE - HEAVY CORROSION ON INNER SKIN STRINGER 27L, STATION 480-490. CUT OUT DAMAGED AREA INSTALLED DOUBLER PER BOEING SRM 53-30-3 PG 12-14A. (M) 2L73 4F A3WE 19960301002881996030100288NM 1996 3 1 AALA952076 119951212A5330 SKIN BOEING727 727223 1384074NM FS 720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07891AA 22007 TULE - FOUND CORROSION ON SKIN AROUND PANEL MOUNTING FLANGE AT RAM AIR DOOR ACTUATOR JACKSCREWS. INSTALLED DOUBLER AND TRIPLER, PER ESO 11697. (M) 2L73 4F A3WE 19960301002891996030100289NM 1996 3 1 AALA952078 119951212A5330144N3140 SKIN BOEING757 757223 1384957NM BS 1094 GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07648AA 24606 AFW - FOUND FUSELAGE SKIN HAS A SMALL BUT DEEP GOUGE AT STATION 1094 AT S10R. PER MRB 757-673, BLENDED PER MRB. PERMANENT REPAIR REQUIRED AT NEXT 'C' CHECK. (M) 2L72 4F RTA2NM 19960301002901996030100290NM 1996 3 1 AALA952081 119951213A5315 FLOOR BEAM BOEING727 727223 1384074NM FS 380 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07869AA 21374 TULE - FOUND CORROSION ON UPPER FLANGE OF FLOOR BEAM STATION 380 RIGHT SIDE, APPROX 12 INCHES INBOARD OF INBOARD SEAT TRACK OUTBOARD TO THE DOOR CUTOUT. REPAIRED FLOOR BEAM PER SRM 53-10-8 AT STATION 380 RIGHT SIDE. (M) 2L73 4F A3WE 19960301002911996030100291NM 1996 3 1 AALA952082 119951213A5532 SKIN BOEING727 727223 1384074NM VERT STAB CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07869AA 21374 TUL - FOUND 1 INCH CRACK IN LEFT SIDE OF VERTICAL STABILIZER SKIN EXTENDING FROM FASTENER HOLE, FS 1212. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO11697 DATED 6-23-95. (M) 2L73 4F A3WE 19960301002921996030100292NM 1996 3 1 AALA952083 119951213A5730 SKIN BOEING727 727223 1384074NM FS 836 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07869AA 21374 TUL - FOUND CORROSION ON LOWER SKIN OF CENTER WING SECTION ABOVE LEFT PRIMARY HEAT EXCHANGER FS 836 AND LBL 31. SMOOTH BLEND CORROSION, EDDY CURRENT THICKNESS CHECK, FLAP/SHOT PEN, ALODINE, LPS-3/AV8 PER ESO 11697 DATED 12/5/95. (M) 2L73 4F A3WE 19960301002931996030100293NM 1996 3 1 AALA952139 119951222A2910BACH8A04EE0232K HOSE BOEING757 757223 1384957NM LT MLG LEAKING A AALAO OTHER JK WARNING INDICATION FLUID LOSS APAPPROACH 1 SW07627AA 24585 LAX - FLT NR 41 - DURING APPROACH TO LAX WHEN LANDING GEAR LOWERED AND FLAPS EXTENDED, LEFT HYDRAULIC QUANTITY WENT TO ZERO AND LOST ALL LEFT HYDRAULIC PRESSURE. ACCOMPLISHED QRH PROCEDURE AND AIRCRAFT LANDED LAX WITHOUT INCIDENT. INSTALLED LANDING GEAR PINS AND AIRCRAFT TOWED TO GATE. REPLACED HYDRAULIC PRESSURE HOSE TO LEFT MAIN LANDING GEAR DOWNLOCK ACTUATOR. SERVICED HYDRAULIC SYSTEM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. REMOVED LANDING GEAR PINS. (M) 2L72 4F RTA2NM 19960301002941996030100294NM 1996 3 1 AALA952142 119951226A5314 KEEL BEAM BOEING727 727227 1384078NM FS 740-770 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07725AA 20732 TULE - FOUND CORROSION ON BOTTOM OF KEEL BEAM WEB AND FASTENERS STATION 740 TO STATION 770. REMOVED CORROSION, INSTALLED DOUBLER PER SRM 53-10-2 PG 26F. (M) 2L73 4F A3WE 19960301002951996030100295NM 1996 3 1 AALA952143 119951226A5315 FLOOR BEAM BOEING727 727227 1384078NM FS 380 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07725AA 20732 TULE - FOUND CORROSION ON CAP OF FLOOR BEAM STATION 380 BETWEEN SEAT TRACKS OUTBOARD RIGHT SIDE. REMOVED TOP CAP AND INSTALLED REPAIR AS PER SRM 53-10-8 PG 8-9. (M) 2L73 4F A3WE 19960301002961996030100296WP 1996 3 1 AALA952149 119951228A5320 CUSP DOUG DC9 DC982 3022082WP BS 1155 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07450AA 49476 TULE - FOUND CORROSION ON BOTTOM OF FLOOR PAN AROUND AFT SERVICE DOOR. AFT DRAIN PAN. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M) 2L72 4F A6WE 19960301002971996030100297WP 1996 3 1 AALA952150 119951228A53475936663501 TIED DOWN TRACK DOUG DC9 DC982 3022082WP BS 1045-1155 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07450AA 49476 TULE - FOUND HEAVY CORROSION ON RIGHT TIEDOWN TRACK STATION 1045-1136, 1141, AND 1155. REPLACED SECTION OF TIEDOWN TRACK STATION 1007-1155. (M) 2L72 4F A6WE 19960301002981996030100298NM 1996 3 1 AALA952151 119951222A5414311T1400 SKIN BOEING767 767223 1385123NM LT PYLON DAMAGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07336AA 22334 AFW - FOUND SIDE SKIN DAMAGE IS BEYOND SRM LIMITS AFTER BLEND OUT. SIDE SKIN BLENDED AND FINISHED PER MRB 767-1098. SIDE SKIN IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1098. (M) 2L72 4F RTA1NM 19960301002991996030100299NM 1996 3 1 AALA952157 119951226A5315141N5112 FLOOR BEAM BOEING757 757223 1384957NM BS 365.5 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07638AA 24596 AFW - FLOOR BEAM AT STATION 365.5 HAS CORROSION REMOVED ON UPPER SURFACE. MATERIAL REMOVED IS BEYOND SRM LIMITS. PER MRB 757-676. (M) 2L72 4F RTA2NM 19960301003001996030100300NM 1996 3 1 AALA952158 119951226A5315141N5113 FLOOR BEAM BOEING757 757223 1384957NM BS 377.7 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07638AA 24596 AFW - FOUND FLOOR BEAM AT STATION 377.7 HAS CORROSION REMOVED BEYOND SRM LIMITS ON UPPER SURFACE. PER MRB 757-678. (M) 2L72 4F RTA2NM 19960301003011996030100301NM 1996 3 1 AALA952159 119951226A5321146N5300 DECK PLATE BOEING757 757223 1384957NM BS 1681.5 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07638AA 24596 AFW - FOUND DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACES AT VARIOUS LOCATIONS. CORROSION REMOVED IS BEYOND SRM LIMITS. PER MRB 757-677. (M) 2L72 4F RTA2NM 19960301003021996030100302NM 1996 3 1 AALA952160 119951220A5315146N5089 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07638AA 24596 AFW - FOUND FLOOR BEAM AT STATION 1640 HAS CORROSION REMOVED ON UPPER SURFACE. CORROSION DEPTH IS BEYOND SRM LIMITS. PER MRB 757-679. (M) 2L72 4F RTA2NM 19960301003031996030100303NM 1996 3 1 AALA952161 119951226A5210146N6201 DOOR PAN BOEING757 757223 1384957NM L-4 DOOR GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07638AA 24596 AFW - FOUND L-4 DOOR EXTERNAL HANDLE PAN HAS GOUGE BLENDED OUT BEYOND SRM LIMITS. PER MRB 757-681. (M) 2L72 4F RTA2NM 19960301003041996030100304NM 1996 3 1 AALA952163 119951213A5330143N3420 SKIN BOEING757 757223 1384957NM BS 580 GOUGED A AALAK NONE O OTHER ININSP/MAINT 1 SW07614AA 24490 AFW - FOUND FUSELAGE SKIN HAS GOUGE BLENDED BEYOND SRM LIMITS AT STATION 580, STRINGER 26R. PER MRG 757-680. (M) 2L72 4F RTA2NM 19960301003061996030100306WP 1996 3 1 AALA960004 119951227A5311 FRAME DOUG DC9 DC982 3022082WP BS 1322 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07276AA 49273 TULE - FOUND CORROSION AT STATION 1322 LONGERON NR 30 AND 29R. INSTALLED DOUBLER PER SRM 53-03 FIG 2A. (M) 2L72 4F A6WE 19960301003071996030100307WP 1996 3 1 AALA960005 119951227A5320 DOOR JAMB DOUG DC9 DC982 3022082WP BS 1155-1212 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07276AA 49273 TULE - FOUND LOWER DOOR JAMB BEAM CORRODED SEVERAL PLACES. SMOOTHLY BLENDED OUT CORROSION IN THE VERTICAL LEG TO A MINIMUM THICKNESS OF .0210 INCHES AS SHOWN IN FIG. REWORK BLEND OUT PER AARD 53-10-00-3 CONDITION 2 (ESO 80559 DATED 12-22-95). (M) 2L72 4F A6WE 19960301003101996030100310WP 1996 3 1 AALA960008 119951231A5311 FRAME DOUG DC9 DC982 3022082WP BS 1309 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07276AA 49273 TULE - FOUND FRAME AT STATION 1309 CORRODED FROM LONGERON 29L TO 29R. SPLICED IN NEW SECTION OF FRAME 1309 FROM LONGERON 29L TO 29R PER SRM 5303 FIG 2A SHEET 1. (M) 2L72 4F A6WE 19960301003141996030100314NM 1996 3 1 AALA960014 119951229A5347 SEAT TRACK DOUG MD11 MD11 3023602NM BS 1351-1352 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW071754 48489 TULE - FOUND CORROSION IN SEAT TRACK NR 2. INSTALLED PLUG REPAIR PER SRM 53070-00 FIG 4 VOL 1. (M) 2L73 4F RTA22WE 19960301003151996030100315WP 1996 3 1 AALA960015 119951229A5751 RIBS DOUG DC10 DC1010 3022110WP AILERON CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07161AA 46942 TULE - FOUND LOWER LEADING EDGE SKIN OF OUTBOARD AILERON AT LEFT AND RIGHT RIBS OF ACTUATOR ATTACH POINT RAISED AND BULGED. INSTALLED SERVICEABLE AILERON FROM SHOP. (M) 2L73 4F A22WE 19960301003211996030100321NM 1996 3 1 AALA960034 119951230A3211161T0000 TRUNNION BOEING767 767223 1385123NM LT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - FOUND LOCAL CORROSION IN AFT TRUNNION BORE. BLENDED AREA PER BOEING SB 767-3240148 AND ENGINEERING MRB 767-100. (M) 2L72 4F RTA1NM 19960301003221996030100322NM 1996 3 1 AALA960035 119951230A5730111T3013 WING SKIN BOEING767 767223 1385123NM FS 955 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - FOUND WING BOX SKIN UPPER SURFACE HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. REPAIRED 'T' CHORD USING SRM 51-70-12 AS A GUIDE PER ENGINEERING MRB 767-1027. (M) 2L72 4F RTA1NM 19960301003231996030100323NM 1996 3 1 AALA960036 119951230A3211161T0000 TRUNNION BOEING767 767223 1385123NM RT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - BLENDED LOCAL CORROSION IN AFT TRUNNION BORE PER BOEING SB 767-3240148. BLENDED AREA PER BOEING SB 767-3740148 AND ENGINEERING MRB 767-1099. (M) 2L72 4F RTA1NM 19960301003241996030100324NM 1996 3 1 AALA960037 119951230A5315143T5120 FLOOR BEAM BOEING767 767223 1385123NM BS 478 DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - FOUND FLOOR BEAM LOWER FLANGE AND BOTTOM OF WEB ARE DENTED. INSTALLED 0.080 BY 2.5 BY 13 INCH 7075-0 REPAIR ANGLE PER ENGINEERING MRB 767-1025. (M) 2L72 4F RTA1NM 19960301003251996030100325NM 1996 3 1 AALA960038 119951230A5315111T5007 FLOOR BEAM BOEING767 767223 1385123NM BS 950 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS AFTER BLEND OUT. FLOOR BEAM IS ACCEPTABLE FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1093. (M) 2L72 4F RTA1NM 19960301003261996030100326NM 1996 3 1 AALA960039 119951230A5311143T10601 FRAME BOEING767 767223 1385123NM BS 676 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07321AA 22322 AFW - FOUND AREA ON FORWARD CARGO FRAME UPPER CHORD BEYOND SRM LIMITS AFTER BLEND OUT. VOIDS FILLED WITH BMS5-25. CHORD IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION PER ENGINEERING MRB 767-1092. (M) 2L72 4F RTA1NM 19960301003401996030100340WP 1996 3 1 AALA960086 119950117A5311 FRAME DOUG DC9 DC982 3022082WP BS 1320 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07258AA 49288 TULE - FOUND BELT FRAME AT STATION 1320 HAS CORROSION AT L30 LOWER ATTACH POINT. INSTALLED REPAIR PER SRM 53-03 FIG 2A. (M) 2L72 4F A6WE 19960301004281996030100428NM 1996 3 1 TSAA9521205 119951128A2121 FAN BOEING737 7372Q9 138448MNM CABIN FAILED A TSAAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP13804AL 21719 ELECTRICAL BURNING SMELL IN CABIN COMING FROM GASPERS. DEFERRED GASPER FAN IAW MEL 21-24. AIRCRAFT PLACARDED. REPLACED GASPER FAN. PLACARD REMOVED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F A16WE 19960301004291996030100429NM 1996 3 1 TSAA9553192 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 520 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 520 EXFOLIATION CORROSION NOTED THIRD RIGHT TRACK FROM THE WALL. REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004301996030100430NM 1996 3 1 TSAA9553193 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 747 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 747 EXFOLIATION CORROSION NOTED ON THE SECOND RIGHT TRACK FROM THE WALL. REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004311996030100431NM 1996 3 1 TSAA9553194 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 747 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 747 EXFOLIATION CORROSION NOTED ON THE SECOND LEFT TRACK FROM THE WALL. REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004321996030100432NM 1996 3 1 TSAA9553195 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 747 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 747 EXFOLIATION CORROSION NOTED ON THE THIRD LEFT TRACK FROM THE WALL. REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004331996030100433NM 1996 3 1 TSAA9553196 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 706 WORN A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 706, SECOND TRACK FROM THE RIGHT SIDE (SLOT WORN). REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004341996030100434NM 1996 3 1 TSAA9553197 119951124A5347 SEAT TRACK BOEING737 7372M6C 1384708NM BS 910 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN SEAT TRACK AT STATION 910 RIGHT SECOND TRACK FROM THE WALL CRACKED. REPAIRED PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004351996030100435NM 1996 3 1 TSAA9553198 119951124A5320 CHORD BOEING737 7372M6C 1384708NM BS 727 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, BS 727 COMPRESSION CHORD CRACKED APPROXIMATELY 1.5 INCHES AT LBL 25. REPAIRED PER ECO 1528R2, PART III. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004361996030100436NM 1996 3 1 TSAA9553199 119951124A5320 INTERCOSTAL BOEING737 7372M6C 1384708NM BS 727 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, EXFOLIATION ON INTERCOSTAL BETWEEN 727A AND 727B ABOVE STRINGER 25L. REPLACED INTERCOSTAL PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004371996030100437NM 1996 3 1 TSAA9553200 119951124A5311 FRAME BOEING737 7372M6C 1384708NM BS 807 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, FOUND CORROSION ON FRAME LOWER FLANGE AT BS 807, STRINGER 27R. CLEANED AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004381996030100438NM 1996 3 1 TSAA9553201 119951124A5311 FRAME BOEING737 7372M6C 1384708NM BS 480 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, CRACK FOUND ON FRAME AT BS 480 BETWEEN STRINGER 21L AND 22L, LOWER LOBE COMPARTMENT AS EVIDENT. REPAIRED PER ECO 2275. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004391996030100439NM 1996 3 1 TSAA9553202 119951124A5320 BEAM BOEING737 7372M6C 1384708NM BS 630 CRACKED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, FUSELAGE BS 639 FLOOR STUB VERTICAL BEAM LOWER CHORD CRACKED LEFT SIDE. REPAIRED PER ECO1567. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004401996030100440NM 1996 3 1 TSAA9553204 119951124A5315 FLOOR BEAM BOEING737 7372M6C 1384708NM BS 520 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, PASSENGER CABIN FLOOR BEAM CORRODED AT BS 520, LBL 4, 16, 21. REPAIRED PER ECO2641. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004411996030100441NM 1996 3 1 TSAA9557203 119951124A5754 STOP BOEING737 7372M6C 1384708NM LE SLAT CRACKED A TSAAK NONE L NO TEST ININSP/MAINT 1 WP13805AL 21809 DURING HEAVY MAINTENANCE VISIT, NR 3 LEADING EDGE SLAT, CENTER UP STOP, AREA ON BOTH INBOARD AND OUTBOARD OF UP STOP CRACKED. REPAIRED PER ECO 2159R4, PT VI. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960301004431996030100443EU 1996 3 1 VTZA96066 119951220A21501379211L401 COLD AIR UNIT BAG JETSTMJETSTM3201 1500217EU LT WING ROOT OVERSERVICED A VTZAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA27495UE 818 FLT NR 6423 - IAD-ROC - DURING CLIMB-OUT AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO IAD DUE TO THERE BEING SMOKE IN THE CABIN. AIRCRAFT LANDED AT IAS WITH NO FURTHER INCIDENT. MAINTENANCE DRAINED A SMALL AMOUNT OF OIL FROM THE LEFT COLD AIR UNIT. PERFORMED MAINTENANCE RUNS, BUT COULD NOT DUPLICATE DISCREPANCIES. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2L72 4T RTA56EU 19960301004661996030100466EU 1996 3 1 96ZZZX828 119951213A3242AH52591 MAXARET ACO36510 BAG JETSTMJETSTM3201 1500217EU RT MLG OUT OF ADJUST AS S4XAO OTHER O OTHER LDLANDING 1 WP27844JX 844 ON LANDING IN MFR, RIGHT TOE PEDAL WAS NOT APPLYING PRESSURE TO RIGHT BRAKE. USED EMERGENCY BRAKE TO COME TO COMPLETE STOP ON RUNWAY WITHOUT INCIDENT. CHECKED RIGHT BRAKE MAXARET, FOUND CONTACTING MAIN WHEEL HUB. NUT RETAINING BOLT ADJUSTED. OPERATIONAL CHECK OF BRAKE SYSTEM GOOD. NO OTHER BRAKE PROBLEMS NOTED. 2L72 4T RTA56EU 19960301004671996030100467WP 1996 3 1 GAIA9527 119951227A3260 DOWNLOCK SWITCH DOUG DC9 DC915F 3022037WP LT MLG ICED UP A GAIAL ABORTED APPROACH P NO WARNING INDICATION APAPPROACH 1 SW07563PC 47055 KHA - FLT 290 - TRI/ROC - ON APPROACH TO ROC, LT MLG DID NOT INDICATE DOWN AND LOCKED. GREEN LIGHT DID NOT ILLUMINATE. FLIGHT CREW DECLARED AN EMERGENCY, A NORMAL UNEVENTFUL LANDING WAS MADE IN ROC. ON TAXI TO RAMP, GROUND PERSONNEL NOTED LT INBOARD MAIN WHEEL WAS NOT ROTATING. MAINTENANCE FOUND LT DOWNLOCK SCISSOR LINKAGE ENCASED IN ICE, AND NR 2 MLG TIRE FLAT (FROM SKIDDING). THAWED SCISSOR LINKAGE AND CLEANED LT DOWNLOCK SWITCH CONNECTOR. DOWNLOCK INDICATION FUNCTIONALLY CHECKED NORMAL. REPLACED BOTH LT MLG WHEEL ASSEMBLIES. AIRCRAFT RELEASED FOR FLIGHT. (X) 2L72 4F A6WE 19960301004901996030100490EU 1996 3 1 96ZZZX849 119950725A2731SD3456030XA CABLE ASSY STBROSSD3 SD360 8100606EU ELEVATOR TRIM BROKEN AS PIVAO OTHER O OTHER APAPPROACH 1 WP13711PM 3715 ON 7-25-95, FLT 3801, INBOUND FROM ROTA TO GUAM, APPROXIMATELY 50 FEET OVER THE RUNWAY, ELEVATOR TRIM WAS APPLIED WHEN THE CABLE SNAPPED. THE TRIM WHEEL WAS ROTATING, BUT WAS NOT HOLDING THE 'TRIM SET'. THE AIRCRAFT WAS LANDED SAFELY. MAINTENANCE WAS NOTIFIED. AIRCRAFT WAS OPENED UP AND A TRIM CABLE WAS FOUND BROKEN (P/N SD3 45 6030XA). CABLE WAS REPLACED AND RIGGED PER SHORT MM 27-32-30, PAGE 201. 2H72 4T A41EU 19960301004911996030100491SO 1996 3 1 96ZZZX850 119950724A27316270142 CONTROL CABLE PIPER PA32 PA32300 7103212SO ELEV TRIM BROKEN A PIVAK NONE O OTHER ININSP/MAINT 1 WP134509T2421 327240083 PILOT REPORT STABILATOR TRIM INOPERATIVE. TROUBLESHOT AND FOUND STABILATOR TRIM CABLE BROKEN IN TWO PIECES IN AREA WHERE IT WRAPS AROUND ELECTRIC TRIMS SERVO. REPLACED CABLE. 1L71 3O A3SO 19960301005321996030100532NM 1996 3 1 95UAL900357 119951227A32419561006 ANTI-SKID MODULE BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE E/E COMPT INOPERATIVE A UALACD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 WP299016U 19054 OUTBOARD ANTI-SKID WARNING LIGHT ILLUMINATED AT 100 KNOTS ON TAKEOFF ROLL. TAKEOFF WAS ABORTED WITH VERY LITTLE BRAKING USED. REPLACED ANTI-SKID CONTROL MODULE, CHECKS OK. 2L72 4F4 F A16WE E2EA 19960301005331996030100533NM 1996 3 1 95UAL900360 119951227A26121705 SENSING ELEMENT BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE NR 2 ENGINE INOPERATIVE A UALAE ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 WP299018U 19056 CREW REPORTED, NR 2 ENGINE FIRE WARNING INDICATION ILLUMINATED IN FLIGHT. DISCHARGED BOTTLES AND SHUTDOWN ENGINE. REPLACED NUMBER TWO ENGINE FIRE DETECTION SENSING ELEMENT, CHECKS OK. 2L72 4F4 F A16WE E2EA 19960301005991996030100599NM 1996 3 1 DL72S960432 119951201A5242650216340 BEAM BOEING727 727232 1384082NM E/E COMPT DOOR CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27404DA 21148 DURING INSPECTION, FOUND A 2 INCH CRACK IN THE E/E COMPARTMENT DOOR AFT TRANSVERSE BEAM AFT LOWER ATTACH ANGLE. THE CRACK IS LOCATED IN THE RADIUS OF THE L-ANGLE AND RUNS BETWEEN 2 EXISTING ADJACENT FASTENERS. AN EXISTING REPAIR IS INSTALLED ON THE FWD FACE OF THE VERTICAL WEB AND EXTENDS 3 FASTENER ROWS UP FROM THE ANGLE RADIUS. IN ACCORDANCE WITH B727 SRM 51-40-03, A TIME LIMITED REPAIR OF STOP DRILLING THE REPAIR AND ADDING A REPAIR ANGLE WAS INSTALLED. THE PERMANENT REPAIR WILL BE ACCOMPLISHED PER B727 SRM 52-40-2 FIG 3. 2L73 4F A3WE 19960308000251996030800025NE 1996 3 8 AWXA9500834 219951229A7532 BLEED VALVE BOEING737 737277 1384570NM PWA JT8 JT8D15 52051NE NR 1 ENGINE LACK OF LUBE A AWXAD RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 WP28185AW 22652 PHX/IAH - FLT 0276 - GATE TURNBACK FOR NR 1 ENGINE COMPRESSOR STALLS. LUBED BLEED VALVES PER E.R. (X) 2L72 4F4 FRTA16WE E2EA 19960308000261996030800026NE 1996 3 8 AWXA95829 219951228A726071700 GEARBOX BOEING737 7372E3 NM PWA JT8 JT8D15 52051NE NR 1 ENGINE LEAKING A AWXAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 WP28138AW GT4419 22792 PHX/LAS - FLT 0024 - NR 1 ENGINE OIL LEAK ON GROUND. REMOVED AND REPLACED NR 1 ENGINE GEARBOX FOR OIL LEAK AT PS5 DRAIN BOSS. (X) 2L72 4F4 FRTA16WE E2EA 19960308001271996030800127NM 1996 3 8 96ZZZX906 119951123A5753CCN5711556 FAIRING BOEING727 727264 138408MNM RT TE FLAP DAMAGED A AMTAK NONE O OTHER ININSP/MAINT 1 GL11765AT 23014 MCO - ON FLAP RETRACTION, INBOARD FLAPS STUCK AT 2 DEGREES, VISUALLY SHOWED 2 DEGREES, SWAPPED GAUGES WITH NEW ONE FROM DESK, NO HELP. CYCLED FLAPS AND STILL OFF 2 DEGREES. REMOVED AND REPLACED RT INBD FLAP INBD TRANSMISSION FAIRING. 2L73 4F A3WE 19960308001281996030800128SO 1996 3 8 96ZZZX907 119950102A2434ALX8421 ALTERNATOR PIPER PA23 PA23250 7102308SO LEFT FAILED A C2TAH DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC CRCRUISE 1 SO056975Y 274342 THE LOSS OF THE LEFT ALTERNATOR FIELD CAUSED LEFT ALTERNATOR TO GO OFF-LINE AND TRIPPED THE REGULATOR WHICH CAUSED THE RIGHT ALTERNATOR TO GO OFF-LINE. SUBSEQUENTLY, BATTERY WAS DEPLETED AND LOSS OF ELECTRICAL POWER OCCURRED. WHEN PILOT SWITCHED REGULATORS, THE LEFT ALTERNATOR WAS NOT ALLOWING EITHER REGULATOR TO FUNCTION PROPERLY. PILOT WAS ABLE TO ISOLATE THE LEFT ALTERNATOR AND RESET THE REGULATOR AND POWER WAS RESTORED. 1L72 3O 1A10 19960308001291996030800129EU 1996 3 8 96ZZZX908 119951127A323085106R106S81 CONNECTOR AMD FALC20FALCON 2720302EU NLG LOOSE A DKAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23950RA 95 YIP - GEAR WOULD NOT RETRACT AFTER TAKEOFF. YIP FOUND CANNON PLUG TO 9G NOT COMPLETELY SECURE - SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F A7EU 19960308001341996030800134SO 1996 3 8 96ZZZX913 119951207A27523203001005 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP FAILED A MASAO OTHER J WARNING INDICATION LDLANDING 1 SW01270YV1495 67 1150 120270 AIRCRAFT EXPERIENCED AN IN-FLIGHT CONTROL FAULT OF THE FLAP SYSTEM. MAINTENANCE INSPECTED SYSTEM AND RE-RACKED FCU, TEST FLOWN WITH SAME RESULTS. AIRCRAFT FERRIED TO MAINTENANCE BASE. SYSTEM TROUBLESHOT TO FAILED INBOARD RIGHT FLAP ACTUATOR. ACTUATOR REPLACED, FLAP TRACKS CLEANED, HYDRAULIC SYSTEM FLUSHED AND REPLENISHED. HYDRO SAMPLES TAKEN. AIRCRAFT TEST FLOWN WITH NO FURTHER DISCREPANCIES AND RETURNED TO SERVICE. 2L72 4T RTA31SO 19960308001361996030800136NE 1996 3 8 96ZZZX915 219951030A7200 ENGINE LEAR 24 24D 5170311CE GE CJ610 CJ610* 30006NE NR 2 FLAMED OUT A BSMAA UNSCHED LANDING X ENGINE FLAMEOUT CLCLIMB 1 SO17470TR 298 222ZA086A DURING CLIMB AT 450 FEET, NR 2 ENGINE FLAMED OUT. DESCENDED TO RESTART ALTITUDE, RESTARTED WITH NO APPARENT PROBLEM. LANDED AT NEAREST SUITABLE AIRPORT. INSPECTED ENGINE, FOUND NO IRREGULARITIES. OPERATOR SUSPECTED TURBULENCE AND HIGH ANGLE OF ATTACK DURING CLIMB. ENGINE TSN, 2,667.3 HOURS. ENGINE CSN 1,682. 2L72 4J4 J A10CE 1E16 19960308001391996030800139WP 1996 3 8 96ZZZX918 119951015A78303640085501 CONTROL CABLE DOUG DC9 DC932 3022066WP LT TR UNIT MISROUTED B SH6YK NONE O OTHER ININSP/MAINT 1 EU038270A 47037 DUE TO CABLE MISRIGGING, LEFT THRUST REVERSER CABLE CHAFED THROUGH THE FORWARD PULLEY MOUNTING BRACKET UNDER THE COCKPIT PEDESTAL. 2L72 4F A6WE 19960308001401996030800140EU 1996 3 8 96ZZZX919 119951202A2840710920 INDICATOR STBROSSD3 SD330 8100602EU AFT FUEL TANK MALFUNCTIONED A DATAEA ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL13336MV SH3018 AT CRP, AIRCRAFT WAS FUELED TO 3,840 POUNDS. EN ROUTE FROM CRP TO TUL, CREW OBSERVED LT FUEL LOW PRESSURE LIGHT. THE CREW FOLLOWED CROSSFEED PROCEDURE, THEN BOTH FUEL LOW PRESSURE LIGHTS CAME ON, CREW THEN CLOSED CROSSFEED AND BOTH LIGHTS WENT OUT. MOMENTS LATER, LT LOW PRESS LIGHT CAME BACK ON AND LT ENG BEGAN TO SURGE. AFTER ENG SHUT DOWN, CREW DIVERTED TO MLC ON SINGLE ENG AND NO EMERGENCY DECLARED. ONCE ON GROUND, CREW PUT ON FUEL AND COMPARED FUEL TANK DIP STICKS WITH FUEL QTY INDICATOR AND BOTH AGREED WITH EACH OTHER. CREW THEN CONTINUED TO TUL WITHOUT PROBLEMS. MX CHECKED FUEL QTY INDICATING SYSTEM CALIBRATION AND FUEL SYSTEM, NO ABSOLUTE REASON FOR DIFFICULTY DETERMINED. 2H72 4T A41EU 19960308001441996030800144SO 1996 3 8 96ZZZX923 119951110A3231 PROX SENSOR EMB 120 EMB120ER 3260203SO LT MLG OUT OF ADJUST A GLBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE01297UX 120297 MDT - AFTER TAKEOFF, CREW ELECTED AN AIR TURN-BACK DUE TO THE LT MLG DOOR NOT CLOSING. MAINTENANCE ADJUSTED THE LT MAIN GEAR UP AND LOCK PROXIMITY SENSOR. SEVERAL SUCCESSFSUL GEAR SWINGS WERE ACCOMPLISHED. 2L72 4T RTA31SO 19960308001451996030800145EU 1996 3 8 96ZZZX924 119951230A32425012589 BRAKE ASSY SAAB SF340 340B 7860101EU LT MLG FAILED A NVEAK NONE O OTHER ININSP/MAINT 1 SO03264AE275 JAN910617 340B264 RFD - MECHANIC REPORTS DURING INSPECTION, NR 2 BRAKE INNER STATOR FAILED. SPINS FREELY WITH BRAKE ROTORS. MAINTENANCE REPLACED BRAKE ASSEMBLY. 2L72 4T RTA52EU 19960308001461996030800146NM 1996 3 8 AALA952103 119951208A5320146N5300 DECK PLATE BOEING757 757223 1384957NM BS 1681.8 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07639AA 24597 AFW - DECK PLATE HAS CORROSION REMOVED ON UPPER SURFACE AT VARIOUS LOCATIONS BEYOND SRM LIMITS PER MRB 757-668. TST, 15,327.4 HOURS, CYCLES, 5,762. (X) 2L72 4F RTA2NM 19960308001471996030800147NM 1996 3 8 AALA952104 119951208A5315146N5089 FLOOR BEAM BOEING757 757223 1384957NM BS 1640 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07639AA 24597 AFW - FLOOR BEAM AT STA 1640, RBL 50 AND RBL 53 HAD CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-667. TST, 15,327.4 HOURS. CYCLES, 5,762. (X) 2L72 4F RTA2NM 19960308001481996030800148NM 1996 3 8 AALA952105 119951208A5315141N5113 FLOOR BEAM BOEING757 757223 1384957NM FS 317 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07639AA 24597 AFW - FLOOR BEAM AT STA 377, LBL 57, 55, 51, 35, 22, 18, AND RBL 10 HAD CORROSION BLENDED BEYOND SRM LIMITS, PER MRB 757-666. TST, 15,327.4 HOURS. CYCLES, 5,762. (X) 2L72 4F RTA2NM 19960308001491996030800149NM 1996 3 8 AALA952106 119951208A5330143N3340 SKIN BOEING757 757223 1384957NM BS 502 DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW07639AA 24597 AT STA 502 AND BETWEEN S29L AND S28L, THE LOWER FUSELAGE SKIN HAS A DENT AND GOUGE 20 INCHES AFT OF MAIN E/E DOOR. THE PARENT MATERIAL REMAINING IN THE BLEND AREA OF GOUGE, 0.033 INCH. DAMAGE IS BEYOND SRM LIMITS, PER MRB 757-671. TST, 15,327.4 HOURS. CYCLES, 5,762. (X) 2L72 4F RTA2NM 19960308001501996030800150NM 1996 3 8 AALA952113 119951219A532069436835 SHEAR TIE BOEING727 727223 1384074NM BS 1166 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07899AA 22015 TUL - CORROSION ON SHEAR TIE AFT SIDE OF FRAME 1166 BETWEEN STR 29L AND STR 30. INSTALLED SERVICEABLE SHEAR TIE PER SRM 53-10-4, FIGURE 12. TST, 39,560 HOURS. CYCLES, 23,346. (X) 2L73 4F A3WE 19960308001511996030800151NM 1996 3 8 AALA952114 119951219A5313655624538 STRINGER BOEING727 727223 1384074NM BS 620 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07899AA 22015 CORROSION ON STR 27R, STA 620. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PER SRM 51-10-3, PAGES 3-4B. TST, 42,286. CYCLES, 23,346. (X) 2L73 4F A3WE 19960308001521996030800152NM 1996 3 8 AALA952115 119951219A5313651822026 STRINGER BOEING727 727223 1384074NM BS 950 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW07899AA 22015 TUL - STR 29R HAS CORROSION. INSTALLED REPAIR PER ESO 11697, DATED 12-18-95. TST, 42,286. CYCLES, 23,346. (X) 2L73 4F A3WE 19960308001841996030800184NM 1996 3 8 UIEA9602 119951220A36109068M40G01 STAGE 14 DUCT BOEING747 747243B 1384830NM NR 4 ENGINE CRACKED A UIEACD ABORTED TAKEOFF RETURN TO BLOCK MJ OVER TEMP WARNING INDICATION TOTAKEOFF 1 EA15516MC 22507 LGW/LGW - FLT BA3571/20 - AIRCRAFT ABORTED TAKEOFF, APPROXIMATELY 140 KNOTS, GROSS WEIGHT 365,000 KGS DUE MASTER FIRE WARNING AND BELL SOUND. CREW EVACUATED AIRCRAFT PER FIRE CHIEF INSTRUCTIONS DUE TO BRAKE FIRE. AIRCRAFT INSPECTION REVEALED 8 BLOWN MAIN GEAR TIRES, NR 4 ENGINE REVERSER DOORS DAMAGED. FIRE WARNING ATTRIBUTED TO RUPTURED STAGE 14 PNEUMATIC ENGINE DUCT, NR 4 ENGINE POSITION. REPLACED STAGE 14 DUCT ASSEMBLY, LT AND RT REVERSER HALVES, ALL WHEEL AND BRAKE ASSEMBLIES, 2 FIRE WARNING CARDS. AIRCRAFT OPS CHECKS OK. (X) 2L74 4F A20WE 19960308003541996030800354WP 1996 3 8 DLL10960486 119950512A5312 BLKHD CAP LKHEED1011 10113851 5265010WP FS 1363 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27718DA 193C1097 TWO CRACKS WERE FOUND IN BLKHD CAP AT LBL 42.5 AND 74.5. THE CRACKS ARE LOCATED IN THE VERTICAL BLKH ATTACH FLANGE AND EMANATES FROM FASTENER HOLES. THE CRACKS HAVE BEEN REMOVED BY OVERSIZING THE SUBJECT FASTENER HOLES. ALSO, THE BLKHD WAS FOUND CRACKED AT WEB-TO-CAP ATTACHMENT AT LBL 82 AND AT LBL 64. THESE CRACKS WERE REPAIRED BY FABRICATING AND INSTALLING NEW WEBS PER DL ERA 270871-14A. 2L73 4F A23WE 19960308003831996030800383NM 1996 3 8 96ZZZM253 119951231A3350883200312 RECEIVER BOEING737 737298C 1384490NM CABIN INOPERATIVE A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 5 AND 6. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. REFERENCE ASAA9510119. 2L72 4F RTA16WE 19960308003881996030800388WP 1996 3 8 96ZZZM258 119951117A53209919402503 TRAP FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15913VV 47318 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY FL, FOUND CRACK AT BS 718 LEFT UPPER TRAPEZOIDAL FRAME. FAB AND INSTALLED PLATE IAW DC-9 SC 53-100 REV 5 AND DC-9 SRM 51-10-3. (M) 2L72 4F A6WE 19960308003931996030800393CE 1996 3 8 96ZZZM263 119951225A2730MS27039C128 SCREW BEECH 10161002621 BEECH 1900 1900C 1154161CE LT ELEVATOR LOOSE A GPPAO OTHER F FLT CONT AFFECTED LDLANDING 1 CE0939019 UC39 UPON LANDING FLARE INTO DENVER, ELEVATOR CONTROL WAS LIMITED TO 2 TO 3 INCHES. ELEVATOR TRIM WAS USED TO COMPLETE LANDING. UPON INSPECTION THE COVER OVER THE LEFT ELEVATOR COUNTER BALANCE WEIGHTS WAS FOUND TO BE MISSING ONE SCREW AND THE REMAINING SCREW HAD BACKED OUT AND WAS BINDING ON THE HORIZONTAL STABILIZER. THE COVER WAS RESECURED AND AIRCRAFT REPOSITIONED TO GRAND ISLAND. 2L72 4T RTA24CE 19960308003951996030800395WP 1996 3 8 96ZZZM265 119951203A32305616554 BOGIE ACTUATOR 57783155538RDOUG DC8 DC861 3021952WP RT MLG LEAKING A FXLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO1927UA R950 45942 IN CLIMB BAQ, RIGHT MAIN LANDING GEAR DOOR UNLATCHED LIGHT ON AND UNSAFE LIGHT ON RIGHT MAIN LANDING GEAR. RETURNED TO BAQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC FLUID LEAKAGE AT THE BOGIE TRIM ACTUATOR. REPLACED TRIM ACTUATOR AND RETURNED AIRCRAFT TO SERVICE. 2L74 4F 4A25 19960308003961996030800396WP 1996 3 8 96ZZZM266 119951205A29101445TS1001 SWITCH ABEX 55097 DOUG DC8 DC8F55 3021928WP NR 2 HYD PUMP LEAKING A FXLAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO1955FB MS356666Y 45678 IN CLIMB FROM MIA, EXPERIENCED HYDRAULIC FLUID LOSS. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. GROUND INSPECTION REVEALED NR 2 HYD PUMP LEAKING AT THE BYPASS SOLENOID. REPLACED BOTH PUMPS AS PRECAUTION AND RETURNED AIRCRAFT TO SERVICE. (M) 2L74 4F 4A25 19960308003971996030800397NM 1996 3 8 ASAA9510119 119951231A3350882104 BATTERY BOEING737 737298C 1384490NM CABIN DISCHARGED A ASAAK NONE L NO TEST ININSP/MAINT 1 NM01745AS 20794 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 5 AND 6. REPLACED BATTERY AND RECEIVER, LIGHTS OPERATED NORMALLY. (M) 2L72 4F RTA16WE 19960308004131996030800413NM 1996 3 8 AWXA9500836 119951231A2840 CLOSED LIGHT BOEING737 737277 1384570NM RT FUEL VALVE ILLUMINATED A AWXAO OTHER N FALSE WARNING CRCRUISE 1 WP28189AW 22656 SFO - FLT NR 456 - RIGHT FUEL VALVE CLOSED LIGHT ILLUMINATED IN FLIGHT, CAME ON DIM AND WENT TO BRIGHT AND STAYED BRIGHT. UPON DESCENT, LIGHT OPERATED NORMAL. MAINTENANCE CHECKED FUEL SHUTOFF VALVE (P/N 61185 S/N B5923) MANUALLY AND ELECTRICALLY OPERATED VALVE. CHECKED PINS ON OVERHEAD AND VALVE. NO DEFECTS FOUND. CHECK VALVE OPERATION IN OPEN AND CLOSED POSITION CHECKED GOOD. (M) 2L72 4F RTA16WE 19960308004141996030800414NM 1996 3 8 AWXA9500838 119951231A5330 SKIN BOEING737 7372E3 NM BS 727 CRACKED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28138AW 22792 PHX - FLT NR 550 - DURING REGULAR MAINTENANCE CHECK, DISCOVERED 3 CRACKS IN THE FUSELAGE SKIN AFT OF THE WING TO BODY FAIRING AT BS 727D, STRINGER 18L. REPAIRED CRACKS PER SRM 53-30-3, FIGURE 6 AND 25. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4F RTA16WE 19960308004151996030800415EU 1996 3 8 AWXA95827 119951227A4990 B-NUT AIRBUS320 A320231 3930325EU APU LOOSE A AWXAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 WP28626AW 65 PHX - APU INOP, CAUSES SMELL IN CABIN. CLEANED APU AREA OF OIL LEAKS. ROUTED A/C FOR PHX RON TO INVESTIGATE POSSIBLE OIL LEAKS AND REMOVED AND REPLACED OIL TUBING O-RINGS. INSTALLED MEL 49-10-01. CLEANED APU COMPARTMENT AND TIGHTENED ALL B-NUTS, OIL LINES. CLEANED PLENUM AREA. LEAK CHECK AND OPS CHECK GOOD WITH BOTH PACKS RUNNING. MEL CLEARED. (M) 2L72 4F RTA28NM 19960308004471996030800447WP 1996 3 8 EIAA9602 119950131A2130 PRESSURIZATION DOUG DC9 DC933F 302207AWP CABIN MALFUNCTIONED A EIAAO OTHER O OTHER DEDESCENT 1 NM09944F 47194 OAK - DESCENT INTO SLC TURNED ON AIRFOIL A/I AT APPROXIMATELY FL 23.0, CABIN RATE OF CLIMB WENT APPROX FULL UP WITH OUTFLOW VALVE FULL CLOSED. TURNED OFF WING A/I AND CABIN PRESSURE RETURNED TO NORMAL. (M) 2L72 4F A6WE 19960308006141996030800614WP 1996 3 8 ABXA9600198 119951208A5321592240035 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 237-294 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FLOOR PANELS AT RBL 8.5 TO 22 STA 237 AND 256, LBL 0 TO 16.25 STA 237 AND 294. REPAIRED IAW ABX REA D953-13739-MR. 2L72 4F A6WE 19960308006151996030800615WP 1996 3 8 ABXA9600199 119951208A5321592240047 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 237-294 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FLOOR PANELS AT RBL 8.5 TO 22 STA 237 AND 256, LBL 0 TO 16.25 STA 237 AND 294. REPAIRED IAW ABX REA D953-13739-MR. 2L72 4F A6WE 19960308006161996030800616WP 1996 3 8 ABXA9600200 119951208A5321592240073 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 237-294 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FLOOR PANELS AT RBL 8.5 TO 22, STA 237 AND 256, LBL 0 TO 16.25 STA 237 AND 294. REPAIRED IAW ABX REA D953-13739-MR. 2L72 4F A6WE 19960308006171996030800617WP 1996 3 8 ABXA9600201 119951208A5321592240079 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 237-294 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORROSION ON THE FLOOR PANELS AT RBL 8.5 TO 22 STA 237 AND 256, LBL 0 TO 16.25 STA 237 AND 294. REPAIRED IAW ABX REA D953-13739-MR. 2L72 4F A6WE 19960308006181996030800618WP 1996 3 8 ABXA9600202 119951208A53135924878501 LONGERON DOUG DC9 DC933F 302207AWP BS 756 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND LONGERON 30 CORRODED AT STA 752 TO 756. REPAIRED IAW ABX REA D953-13747-MR. 2L72 4F A6WE 19960308006191996030800619WP 1996 3 8 ABXA9600203 119951206A532099107349 CUSP DOUG DC9 DC933F 302207AWP BS 218-290 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND EXCESSIVE CORROSION ON CUSP BETWEEN STA 218 TO 290 LBL 54. REPAIRED IAW ABX REA D953-13758-MR. 2L72 4F A6WE 19960308006201996030800620WP 1996 3 8 ABXA9600204 119951207A532159224303 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 193 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 193. REPAIRED IAW ABX REA D953-13771-MR. 2L72 4F A6WE 19960308006211996030800621WP 1996 3 8 ABXA9600205 119951207A532159224305 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 193 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 193. REPAIRED IAW ABX REA D953-13771-MR. 2L72 4F A6WE 19960308006221996030800622WP 1996 3 8 ABXA9600206 119951211A531599223961 FLOOR BEAM DOUG DC9 DC933F 302207AWP BS 897 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR BEAM AT STA 897. REPAIRED IAW ABX REA D953-13781-MR. 2L72 4F A6WE 19960308006231996030800623WP 1996 3 8 ABXA9600207 119951207A5321592243019 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 160. REPAIRED IAW ABX REA D953-13783-MR. 2L72 4F A6WE 19960308006241996030800624WP 1996 3 8 ABXA9600208 119951207A5321592243029 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANELS AT STA 160. REPAIRED IAW ABX REA D953-13783-MR. 2L72 4F A6WE 19960308006251996030800625WP 1996 3 8 ABXA9600209 119951207A5321592243063 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 160 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANELS AT STA 160. REPAIRED IAW ABX REA D953-13783-MR. 2L72 4F A6WE 19960308006261996030800626WP 1996 3 8 ABXA9600210 119951211A5321592243059 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 180 TO 237. REPAIRED IAW ABX REA D953-13784-MR. 2L72 4F A6WE 19960308006271996030800627WP 1996 3 8 ABXA9600211 119951211A5321592243023 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 180 TO 237. REPAIRED IAW ABX REA D953-13784-MR. 2L72 4F A6WE 19960308006281996030800628WP 1996 3 8 ABXA9600212 119951211A5321592243025 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FLOOR PANEL CORRODED AT STA 180 TO 237. REPAIRED IAW ABX REA D953-13784-MR. 2L72 4F A6WE 19960308006291996030800629WP 1996 3 8 ABXA9600213 119951208A53115911448527 FRAME DOUG DC9 DC933F 302207AWP BS 522 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND FRAME AT STA 522 CORRODED. REPAIRED IAW ABX REA D953-13780-MR. 2L72 4F A6WE 19960315000091996031500009WP 1996 3 15 ABXA9600214 119951211A5321592243067 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13795-MR. 2L72 4F A6WE 19960315000101996031500010WP 1996 3 15 ABXA9600215 119951211A5321592243065 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13795-MR. 2L72 4F A6WE 19960315000111996031500011WP 1996 3 15 ABXA9600216 119951211A5321592243013 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13795-MR. 2L72 4F A6WE 19960315000121996031500012WP 1996 3 15 ABXA9600217 119951209A5321592243019 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13796-MR. 2L72 4F A6WE 19960315000131996031500013WP 1996 3 15 ABXA9600218 119951209A5321592243057 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13796-MR. 2L72 4F A6WE 19960315000141996031500014WP 1996 3 15 ABXA9600219 119951209A5321592243069 FLOOR PANEL DOUG DC9 DC933F 302207AWP BS 180-237 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CORRODED FLOOR PANEL AT STA 180 - STA 237. REPAIRED IAW ABX REA D953-13796-MR. 2L72 4F A6WE 19960315000151996031500015WP 1996 3 15 ABXA9600220 119951212A5320992240589 CHANNEL DOUG DC9 DC933F 302207AWP BS 163 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND H-CHANNEL CORRODED AT STA 163. REPAIRED IAW ABX REA D953-13801-MR. 2L72 4F A6WE 19960315000161996031500016WP 1996 3 15 ABXA9600221 119951204A5312991150983 BLKHD WEB DOUG DC9 DC933F 302207AWP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND BULKHEAD WEB AT STA 110 CORRODED AT LONGERONS 27R AND 25R. REPAIRED IAW ABX REA D953-13722-MR. 2L72 4F A6WE 19960315000171996031500017WP 1996 3 15 ABXA9600222 119951209A5320991150985 TEE CAP DOUG DC9 DC933F 302207AWP BS 110 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND STA 110 TEE CAP CORRODED AT LONGERONS 27R AND 25R. REPAIRED IAW ABX REA D953-13722-MR. 2L72 4F A6WE 19960315000181996031500018WP 1996 3 15 ABXA9600223 119951130A531327779225 LONGERON DOUG DC9 DC933F 302207AWP BS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND LONGERON 16L CRACKED AT STA 965. REPAIRED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960315000191996031500019WP 1996 3 15 ABXA9600224 119951129A531327779224 LONGERON DOUG DC9 DC933F 302207AWP BS 965/980 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND LONGERON 17L CRACKED AT STA 980 AND STA 965. REPAIRED IAW DC-9 SRM 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960315000201996031500020WP 1996 3 15 ABXA9600225 119951129A531327779224 LONGERON DOUG DC9 DC933F 302207AWP BS 980 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C - CHECK INSPECTION, FOUND LONGERON 17R CRACKED AT STA 980. REPAIRED LONGERON IAW DC-9 SRM 53-03, FIGURE 2. 2L72 4F A6WE 19960315000211996031500021WP 1996 3 15 ABXA9600226 119951128A5240991158113N FITTING DOUG DC9 DC933F 302207AWP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND THIRD BEAM ON SERVICE DOOR AFT END FITTING CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19960315000221996031500022WP 1996 3 15 ABXA9600227 119951210A524099115809 FITTING DOUG DC9 DC933F 302207AWP SERVICE DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND CRACKED END FITTING AT FORWARD END OF SECOND BEAM IN SERVICE DOOR. REPAIRED IAW DC-9 SRM 52-05, PAGE 91. 2L72 4F A6WE 19960315000231996031500023WP 1996 3 15 ABXA9600228 119951207A5347593008413 SEAT TRACK DOUG DC9 DC933F 302207AWP BS 180-218 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE SEAT TRACK AT LBL 24 AT STA 180 - STA 218. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960315000241996031500024WP 1996 3 15 ABXA9600229 119951211A5347593008413 SEAT TRACK DOUG DC9 DC933F 302207AWP BS 180-218 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON THE SEAT TRACK AT RBL 24 AT STA 180, STA 210, AND STA 218. INSTALLED NEW SEAT TRACK IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960315000251996031500025WP 1996 3 15 ABXA9600230 119951130A53209919661 STIFFENER DOUG DC9 DC933F 302207AWP BS 1040 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION, FOUND STIFFENER JUST RIGHT OF AUXILIARY LANDING GEAR STRUCTURE CRACKED. REPAIRED IAW ABX DRAWING K05159. 2L72 4F A6WE 19960315000261996031500026WP 1996 3 15 ABXA9600231 119951205A53205956026175 SUPPORT DOUG DC9 DC933F 302207AWP BS 332-351 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX 47384 DURING C-CHECK INSPECTION FOUND LEVEL 2 CORROSION ON THE LONGITUDINAL FLOOR SUPPORT BETWEEN LONGERONS 27R AND 28R, BETWEEN STA 332 AND STA 351. MANUFACTURED FLOOR SUPPORT IAW ABX DRAWING K05554 AND INSTALLED IAW DC-9 SRM 51-30-2. 2L72 4F A6WE 19960315000271996031500027WP 1996 3 15 ABXA9600233 119951115A532059248976 PANEL DOUG DC9 DC941 302207NWP BS 772 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND RIGHT WHEELWELL PANEL ABOVE HYDRAULIC OVERFLOW BOTTLE CRACKED. REPAIRED IAW DC-9 SRM 53-01, SHEET 3. 2L72 4F A6WE 19960315000281996031500028WP 1996 3 15 ABXA9600234 119951116A55309911834197 ANGLE DOUG DC9 DC941 302207NWP VERT STAB CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER REAR SPAR, RIGHT SUPPORT FOR PANEL 60407 CORRODED. REPAIRED IAW ABX REA D955-13589-MR. 2L72 4F A6WE 19960315000291996031500029WP 1996 3 15 ABXA9600235 119951120A57535910041503 VANE DOUG DC9 DC941 302207NWP LT TE FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND LEFT WING INBOARD FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 M.M. 27-51-3. 2L72 4F A6WE 19960315000301996031500030WP 1996 3 15 ABXA9600236 119951120A57525910047501 TAB DOUG DC9 DC941 302207NWP LT AILERON DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND AILERON CONTROL TAB DELAMINATED ON THE LEFT WING. REPLACED IAW DC-9 M.M. 27-10-2. 2L72 4F A6WE 19960315000311996031500031WP 1996 3 15 ABXA9600237 119951120A573059134384 PANEL DOUG DC9 DC941 302207NWP RT WING DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND RIGHT WHEELWELL AREA UNDERSIDE PANEL FORWARD AND INBOARD OF GEAR DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1. 2L72 4F A6WE 19960315000321996031500032WP 1996 3 15 ABXA9600238 119951120A5320992344510 WEB DOUG DC9 DC941 302207NWP RT MLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE RADIUS OF LOWER FORMED FLANGE OF BRACKET IN THE RIGHT WHEELWELL. REPAIRED IAW ABX REA D953-13703-MR. 2L72 4F A6WE 19960315000331996031500033WP 1996 3 15 ABXA9600239 119951121A57133911238512 STRINGER DOUG DC9 DC941 302207NWP WS 111 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND RIGHT WING STRINGER 18 CORRODED AND GOUGED AT STA 111. REMOVED CORROSION IAW DC-9 SRM 51-10-3, REMOVED GOUGE IAW DC-9 SRM 51-22-1. 2L72 4F A6WE 19960315000341996031500034WP 1996 3 15 ABXA9600240 119951121A57204912005511 FITTING DOUG DC9 DC941 302207NWP WS 111 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND CRACKED FITTING AT STA 111 AT STRINGER 11 IN LEFT WING. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2L72 4F A6WE 19960315000351996031500035WP 1996 3 15 ABXA9600241 119951024A528059337871 HINGE DOUG DC9 DC941 302207NWP LT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 91-22-07; A.S.B. 32-244, FOUND LEFT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED DOOR IAW DC-9 M.M. 32-10-0. 2L72 4F A6WE 19960315000631996031500063 1996 3 15 96ZZZX1011 419950330A2330M4000 PA SYSTEM BELL 214 214ST 1182106SW CABIN DEFECTIVE C K NONE O OTHER ININSP/MAINT 1 EU01745H 1033 9201196 28197 PA ADDRESS SYSTEM TRIPS CIRCUIT BREAKER. 2G72 4U H10SW 19960315001631996031500163SW 1996 3 15 96ZZZX1025 119951226A3212 FLOAT BELL 214 214ST 1182106SW SKID INFLATED A HEEAA UNSCHED LANDING O OTHER CRCRUISE 1 SW038045T 28101 DURING CRUISE FLIGHT, FLOATS INFLATED. PILOT LANDED ON OFFSHORE PLATFORM WITHOUT INCIDENT. INCIDENT STILL UNDER INVESTIGATION. 2G72 4U H10SW 19960315001831996031500183WP 1996 3 15 96ZZZX1046 119951206A6710A1217 PP TUBE ROBSINR22 R22 7640102WP CONTROL TUBE CHAFE A ABXOAK NONE O OTHER ININSP/MAINT 1 EA092362E701 2351 GUIDE ASSY, PN A432-1, INSTALLED IMPROPERLY WHICH RESULTED IN P/P TUBE TO CHAFE THROUGH CONTROL TUBE AT LOWER END. LOCATED IN HORIZONTAL FIREWALL B238-1 BOLTS. SUBMITTER STATED TO INSPECT INSTALLATION OF GUIDE ASSY FOR FULL ADJUSTMENT BEFORE INSTALLING P/P TUBES. 1G71 3O H10WE 19960315002471996031500247NM 1996 3 15 DL72S960540 119951010A52416556150137 SKIN BOEING727 727232 1384082NM R 1 DOOR. CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 UPON SHOP INSPECTION, FOUND OUTER SKIN AND FRAME CRACKED AT UPPER FORWARD CORNER. REPAIRED SKIN PER SRM 52-00-3, FIG 4 AND REPAIRED FRAME PER MM 52-12-0, FIG 805, FOR R-1 SERVICE DOOR. 2L73 4F A3WE 19960315004021996031500402NM 1996 3 15 95UAL900352 119951227A21317638101 CONTROLLER BOEING737 737322 1384676NM E/E COMPT MALFUNCTIONED A UALAK NONE O OTHER CRCRUISE 1 WP29359UA 24452 DURING CRUISE AT 330 FEET, HEARD A THUMP, FELT PRESSURE ON EARS AND THE CABIN WAS DESCENDING AT 900 FEET PER MINUTE. SWITCHED TO STANDBY MODE AND WORKED NORMALLY. ON DESCENT THROUGH LANDING ALTITUDE, CONTINUED TO DESCEND AT 500 FEET PER MINUTE. THE CABIN PRESSURE CONTROLLER WAS REPLACED AND SYSTEM CHECKS OK. SHOP FOUND THAT THE STANDBY AND AUTO TRANSDUCER CIRCUITS NEEDED ADJUSTMENT. 2L72 4F RTA16WE 19960315004221996031500422NM 1996 3 15 96ZZZM267 119951114A571165810811 SPAR CHORD BOEING707 707330C 138367GNM RT WING DEFECTIVE A CLCAK NONE K FLUID LOSS ININSP/MAINT 1 SO19707HE81771 20124 FLT NR 52 - SVMI-MDSD - THE FLIGHT ENGINEER FOUND A FUEL LEAK FROM NR 3 MAIN TANK AT THE LOWER AFT SECTION OF THE BEAVER TAIL. THE A/C WAS INSPECTED, TANK DRAINED COMPLETELY OF FUEL AND FERRIED TO MIAMI, FL. DYNAIR TECH OF FLORIDA REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING AND THE UPPER REAR SPAR CHORD IAW BOEING DRAWINGS. THE A/C WAS RETURNED TO SERVICE ON 02/12/96. 2L74 4F 4A26 19960315004231996031500423NM 1996 3 15 96ZZZM268 119951114A5720659595050 FITTING BOEING707 707330C 138367GNM RT WING CRACKED A CLCAK NONE K FLUID LOSS ININSP/MAINT 1 SO19707HE81771 20124 FLT NR 52 - SVMI-MDSD - THE FLIGHT ENGINEER FOUND A FUEL LEAK FROM NR 3 MAIN TANK AT THE LOWER AFT SECTION OF THE BEAVER TAIL. THE A/C WAS INSPECTED, TANK DRAINED COMPLETELY OF FUEL AND FERRIED TO MIAMI, FL. DYNAIR TECH OF FLORIDA REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING AND THE UPPER REAR SPAR CHORD IAW BOEING DRAWINGS. THE A/C WAS RETURNED TO SERVICE ON 02/12/96. 2L74 4F 4A26 19960315004391996031500439NM 1996 3 15 96ZZZM284 119951229A5320 CHANNEL BOEING727 727232 1384082NM BS 380-420 CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 LEVEL 2 SURFACE CORROSION WIDE SPREAD ON R-1 DOOR THRESHOLD Z-CHANNEL FROM STATION 380-420 RBL 53. REMOVED AND REPLACED 2 CHANNEL PER LIMITS PER SRM 51-40-2. (M) 2L73 4F A3WE 19960315004581996031500458NM 1996 3 15 96ZZZM303 119951229A5320 ANGLE BOEING727 727232 1384082NM BS 1130 CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 MAIN CABIN CRACK IN FLOOR BOARD ATTACH ANGLE AT STATION 1130 RBL 64. ALSO, SMALL AREA OF LEVEL 1 CORROSION 6 INCHES FARTHER AFT FROM CRACK. REMOVED CORROSION, MATERIAL LOSS WITHIN ACCEPTABLE LIMITS PER SRM 51-10-6, 51-10-3 AND FABRICATED ANGLE DOUBLERS, ALODINE AND PRIMED PER SRM 51-10-2 AND 51-40-4. INSTALLED ANGLE DOUBLERS PER SRM 51-40-4 FIG 3. (M) 2L73 4F A3WE 19960315006501996031500650EA 1996 3 15 96ZZZX1101 219951223A7314 PUMP BNORM BN2 BN2A3 1520215EU LYC O540 O540E4C5 41532EA AFT ENGINE FAILED A VLIAO OTHER ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 SO21901TA1927 22393A 1003 L2231840A DURING SCHEDULED FLIGHT AFTER TAKEOFF CLIMB AT 700 MSL, THE REAR ENGINE STARTED DECREASING RPM'S, AND INCREASING MANIFOLD ON REAR ENGINE. VIBRATION FELT ON AIRCRAFT RETURN AND LANDING WITHOUT ANY FURTHER INCIDENT. REAR ENGINE RUN-UP AND FOUND DEFECTIVE MECHANICAL FUEL PUMP. REPLACED BY NEW ONE. ENGINE RUN-UP AND FOUND AIRWORTHY. THE AIRCRAFT WAS RETURNED TO SERVICE. 1H72 3O3 O A17EU E295 19960315006511996031500651 1996 3 15 96ZZZX1102 419951220A6122G210659 GOVERNOR WOODWARD BNORM BN2 BN2A3 1520215EU AFT ENGINE PROP SHAFT FAILED A VLIAE ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 SO21901TA3900 1917 2249112M 1003 DURING TAKEOFF, REAR ENGINE LOST POWER AND PROPELLER FEATHER. REAR GOVERNOR REMOVED AND FOUND BROKEN SHAFT. GOVERNOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1H72 3O A17EU 19960321000021996032100002NM 1996 3 21 AALA951906 119951108A3350A3030398101 CONNECTOR BOEING757 757223 1384957NM CABIN LOOSE A AALAK NONE L NO TEST ININSP/MAINT 1 SW07654A 24612 SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BY PASSENGER SEAT ROW 35D FOUND INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR BY PASSENGER SEAT ROW 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2L72 4F RTA2NM 19960322000671996032200067WP 1996 3 22 ABXA9600270 119951120A57535910043510 VANE DOUG DC9 DC941 302207NWP RT TE FLAP DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND THE RIGHT FLAP OUTBOARD FIXED VANE DELAMINATED. REPLACED VANE IAW DC-9 MM 27-51-3. 2L72 4F A6WE 19960322000681996032200068WP 1996 3 22 ABXA9600271 119951024A528059337871 HINGE DOUG DC9 DC941 302207NWP RT MLG DOOR WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT MAIN LANDING GEAR ARTICULATING DOOR HINGE WORN. REPLACED DOOR IAW DC-9 MM 32-10-0. 2L72 4F A6WE 19960322000691996032200069WP 1996 3 22 ABXA9600273 119951116A53129915558155 BLKHD STIFFENER DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 12L. REPAIRED IAW DC-9 SUPP SRM K05159. 2L72 4F A6WE 19960322000701996032200070WP 1996 3 22 ABXA9600274 119951117A53129915558135 BLKHD STIFFENER DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND AFT PRESSURED BULKHEAD STIFFENER CRACKED AT STA 1072 BETWEEN LONGERON 16L AND 17L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159. 2L72 4F A6WE 19960322000711996032200071WP 1996 3 22 ABXA9600275 119951117A53129915558141 BLKHD STIFFENER DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 15L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159. 2L72 4F A6WE 19960322000721996032200072WP 1996 3 22 ABXA9600276 119951117A53129915558145 STIFFENER DOUG DC9 DC941 302207NWP BS 1072 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23955AX 47619 DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD STIFFENER CRACKED AT STA 1072 AT LONGERON 14L. REPAIRED IAW DC-9 SUPPLEMENTAL SRM K05159. 2L72 4F A6WE 19960322000771996032200077WP 1996 3 22 ABXA9600281 119950929A5330592032339 SKIN DOUG DC9 DC931 3022065WP BS 332 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, A PRIOR REPAIR ACCOMPLISHED IAW ABX REA D953-07841-MR REQUIRED INSPECTION. INSPECTED AND REPAIRED IAW ABX REA D953-12979-MR. 2L72 4F A6WE 19960322000781996032200078WP 1996 3 22 ABXA9600282 119951009A531599115451 FLOORBEAM DOUG DC9 DC931 3022065WP BS 389 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE LOWER FLANGES OF THE FLOOR BEAM AT STA 389 WERE FOUND GOUGED. REPAIRED IAW ABX REA D953-13021-MR. 2L72 4F A6WE 19960322000791996032200079WP 1996 3 22 ABXA9600283 119951009A531599115441 FLOORBEAM DOUG DC9 DC931 3022065WP BS 408 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE LOWER FLANGES OF THE FLOOR BEAM AT STA 408 WERE FOUND GOUGED. REPAIRED IAW ABX REA D953-13021-MR. 2L72 4F A6WE 19960322000801996032200080WP 1996 3 22 ABXA9600284 119951006A53305919707 SKIN DOUG DC9 DC931 3022065WP BS 794-813 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, DAMAGE WAS FOUND ON THE SKIN IN THE AFT LOWER CARGO AREA BETWEEN STA 794 AND 813 JUST OUTBOARD OF LONGERON 30. REPAIRED SKIN IAW ABX REA D953-13022-MR. 2L72 4F A6WE 19960322000811996032200081WP 1996 3 22 ABXA9600285 119951009A53203616987501 BRACKET DOUG DC9 DC931 3022065WP BS 110 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE PULLEY BRACKET WAS FOUND CUT BY CABLE RUN 47 JUST FORWARD OF STA 110. REPAIRED IAW ABX REA D953-13111-MR. 2L72 4F A6WE 19960322000821996032200082WP 1996 3 22 ABXA9600286 119951009A53203640085501 BRACKET DOUG DC9 DC931 3022065WP BS 110 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE PULLEY BRACKET WAS FOUND CUT BY CABLE RUN 47 JUST FORWARD OF STA 110. REPAIRED IAW ABX REA D953-13111-MR. 2L72 4F A6WE 19960322000831996032200083WP 1996 3 22 ABXA9600287 119951010A53135920319508 LONGERON DOUG DC9 DC931 3022065WP BS 456-503 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, FOUND CORROSION ON LONGERON 30 BETWEEN STA 456 AND 503. REPAIRED IAW ABX REA D953-13133-MR. 2L72 4F A6WE 19960322000841996032200084WP 1996 3 22 ABXA9600288 119951010A53115911448519 FRAME DOUG DC9 DC931 3022065WP BS 484 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, A GOUGE WAS BLENDED BEYOND LIMITS ON A FRAME AT STA 484 AND LONGERON 29L. REPAIRED IAW ABX REA D953-13140-MR. 2L72 4F A6WE 19960322000851996032200085WP 1996 3 22 ABXA9600289 119950925A57209910010155 DOUBLER DOUG DC9 DC931 3022065WP WS 58.7 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF AD 90-18-03, SB 57-129: REV 4, FOUND CRACK INDICATION PER STEP 2B, ON THE RIGHT WING DOUBLER. REPLACED RIGHT WING DOUBLER IAW EA AD-57-03636-MA. 2L72 4F A6WE 19960322000861996032200086WP 1996 3 22 ABXA9600290 119950925A57119910010153 SPAR WEB DOUG DC9 DC931 3022065WP WS 58.7 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING COMPLIANCE OF AD 90-18-03; SB 57-129: REV 4, FOUND CRACK INDICATION PER STEP 2B, ON THE RIGHT WING WEB. REPLACED SPAR WEB IAW EA AD-57-03636-MA. 2L72 4F A6WE 19960322000871996032200087WP 1996 3 22 ABXA9600291 119951002A532049125401 ANGLE DOUG DC9 DC931 3022065WP BS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE VERTICAL FLOOR SUPPORT ATTACH ANGLE WAS FOUND CRACKED AT STA 965L. REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 19960322000881996032200088WP 1996 3 22 ABXA9600292 119951002A532049125402 ANGLE DOUG DC9 DC931 3022065WP BS 965 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE VERTICAL FLOOR SUPPORT ATTACH ANGLE WAS FOUND CRACKED AT STA 965R. REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-1. 2L72 4F A6WE 19960322000891996032200089WP 1996 3 22 ABXA9600293 119950927A5230591015825 DOUBLER DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE DOUBLER AT THE LOWER CENTER OF THE AFT LOWER CARGO DOOR WAS FOUND CORRODED. REPAIRED THE DOUBLER IAW ABX REA D953-12971-MR. 2L72 4F A6WE 19960322000901996032200090WP 1996 3 22 ABXA9600294 119950927A5230591970731 SKIN DOUG DC9 DC931 3022065WP CARGO DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23907AX 47203 DURING C-CHECK INSPECTION, THE SKIN AT THE LOWER CENTER OF THE AFT LOWER CARGO DOOR WAS FOUND CORRODED. REPAIRED IAW ABX REA D953-12971-MR. 2L72 4F A6WE 19960322001451996032200145WP 1996 3 22 96ZZZX1184 119951017A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1190-1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION AT STR 34R BETWEEN STA 1190 AND STA 1200, INSIDE OF C-3 CARGO. REMOVED CORROSION, TREATED AND PRIMED AREA, AND INSTALLED NEW FITTING PER SRM 53-2-0. 2L74 4F 4A25 19960322001461996032200146WP 1996 3 22 96ZZZX1185 119951226A5320 CHANNEL DOUG DC8 DC863 302198AWP BS 1600 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STA 1600 RT, FROM FUSELAGE TO INBD TRACK, 3 CHANNELS WITH CORROSION AT CLIP NUTS. REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED REPAIR PER SRM 53-2-3. 2L74 4F 4A25 19960322001471996032200147WP 1996 3 22 96ZZZX1186 119951226A5220 WINDOW FRAME DOUG DC8 DC863 302198AWP EMER EXIT DOOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RT AFT EMERGENCY EXIT DOOR WINDOW HAS HEAVY SCRATCHES (FOUND CORROSION UNDER WINDOW). REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER DRAWING 085330-5115, AND INSTALLED WINDOW. 2L74 4F 4A25 19960322001481996032200148WP 1996 3 22 96ZZZX1187 119951226A5321 FLOOR DOUG DC8 DC863 302198AWP BS 1338 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STA 1338, LT SIDE AFT OF EMERGENCY CIRCUMFERENTIALS, FRAMES AND CUSP HAVE CORROSION. REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED REPAIR PER RIA DRAWING 45931-2. 2L74 4F 4A25 19960322001491996032200149WP 1996 3 22 96ZZZX1188 119951226A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1746 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STA 1746R TO 1700R, STR 22 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 535-20-0. 2L74 4F 4A25 19960322001501996032200150WP 1996 3 22 96ZZZX1189 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 727, RT WING CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RT WING UPPER SURFACE, STA XRS 727 AT STR 5 HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-7. 2L74 4F 4A25 19960322001511996032200151WP 1996 3 22 96ZZZX1190 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 693 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RT WING UPPER SURFACE HAS CORROSION AT STA 693, STR 3. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-7. 2L74 4F 4A25 19960322002721996032200272WP 1996 3 22 96ZZZW1 119951227A5347 SEAT TRACK DOUG DC8 DC863 302198AWP BS 1580-1620 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR INBOARD SEAT TRACK STATION 1620 TO 1580 RT HAS CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-3. 2L74 4F 4A25 19960322002731996032200273WP 1996 3 22 96ZZZW10 119951228A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1230 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION AT STRINGER 22R STATION 1230. REMOVED STRINGER TIE, REMOVED CORROSION, FABRICATED AND INSTALLED ANGLE REPAIR, REINSTALLED STRINGER TIE. 2L74 4F 4A25 19960322002741996032200274WP 1996 3 22 96ZZZW11 119951228A5320 SUPPORT DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SECOND FORWARD CARGO DOOR FRAME LOWER SILL PLATE SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-8. 2L74 4F 4A25 19960322002751996032200275WP 1996 3 22 96ZZZW12 119951228A5320 DOUBLER DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SKIN PLATE BULGED BELOW NR 2 CARGO DOOR. REMOVED SKIN PLATE, REMOVED DAMAGED AREA UNDER SKIN PLATE, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1 AND REINSTALLED PLATE. 2L74 4F 4A25 19960322002761996032200276WP 1996 3 22 96ZZZW13 119951229A5320 HAT CHANNEL DOUG DC8 DC863 302198AWP BS 1680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR AT STATION 1680 INBOARD HAT CHANNEL HAS CORROSION. REMOVED, REPAIRED AND REINSTALLED HAT CHANNEL SECTION PER SRM 51-1-19. 2L74 4F 4A25 19960322002771996032200277WP 1996 3 22 96ZZZW14 119951229A5320 ANGLE DOUG DC8 DC863 302198AWP BS 1660 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN AREA STATION 1660 LEFT AFT PASSENGER DOOR FRAME LOWER AREA OF SILL PLATE HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 51-1-01. 2L74 4F 4A25 19960322002781996032200278WP 1996 3 22 96ZZZW15 119951229A5330 SKIN DOUG DC8 DC863 302198AWP BS 1762 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION ON SKIN ALONG STRINGER 28L AT STATION 1762. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SMR 53-2-0. 2L74 4F 4A25 19960322002791996032200279WP 1996 3 22 96ZZZW16 119951229A5520 BRACKET DOUG DC8 DC863 302198AWP LT ELEVATOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - LEFT ELEVATOR LOWER SURFACE FRAME STRUCTURE IS CORRODED. REMOVED, FABRICATED AND INSTALLED BRACKET PER SRM 51-1-0. 2L74 4F 4A25 19960322002801996032200280WP 1996 3 22 96ZZZW17 119951227A5311 CIRCUM DOUG DC8 DC863 302198AWP BS 980 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION AT CIRCUMFERENTIAL AT STATION 980 FROM 32L TO 32R INSIDE C3 CARGO COMPARTMENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F 4A25 19960322002811996032200281WP 1996 3 22 96ZZZW18 119951229A5512 SKIN DOUG DC8 DC863 302198AWP VERT STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - VERTICAL STABILIZER LEADING EDGE SEGMENT NR 1 UPPER END HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. 2L74 4F 4A25 19960322002821996032200282WP 1996 3 22 96ZZZW19 119951229A5530 CAP DOUG DC8 DC863 302198AWP VERT STAB LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - LOWER END OF NR 2 VERTICAL STABILIZER LEADING EDGE CAP IS CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 55-2-1. 2L74 4F 4A25 19960322002831996032200283WP 1996 3 22 96ZZZW2 119951227A5320 HAT CHANNEL DOUG DC8 DC863 302198AWP BS 1500-1600 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1600 RT TO 1500 RT HAT CHANNEL HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-01-8. 2L74 4F 4A25 19960322002841996032200284WP 1996 3 22 96ZZZW20 119951229A5320464016501N FITTING DOUG DC8 DC863 302198AWP BS 1260-1280 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR AT STATION 1260R TO 1280R CUSP HAS CORROSION. REMOVED DAMAGED AREA, INSTALLED NEW FITTING PER SRM 53-1-0. 2L74 4F 4A25 19960322002851996032200285WP 1996 3 22 96ZZZW21 119951229A5311 CIRCUM DOUG DC8 DC863 302198AWP BS 1140 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION ON CIRCUMFERENTIAL AT STATION 1140 FROM 32L TO 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19960322002861996032200286WP 1996 3 22 96ZZZW22 119951229A5320 FITTING DOUG DC8 DC863 302198AWP BS 1190-1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION AT STRINGER 34R BETWEEN STATION 1190 AND 1200 INSIDE C3 CARGO. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE FITTING PER SRM 53-2-0. 2L74 4F 4A25 19960322002871996032200287WP 1996 3 22 96ZZZW23 119951229A5320 NET TRACK DOUG DC8 DC863 302198AWP BS 980-1170 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - C-3 CARGO RIGHT SIDE BARRIER NET TRACK HAS CORROSION FROM STATION 980 TO 1170 BETWEEN STRINGER 32R AND 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR. 2L74 4F 4A25 19960322002881996032200288WP 1996 3 22 96ZZZW24 119951229A5320 CHANNEL DOUG DC8 DC863 302198AWP BS 1338-1390 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - NR 3 CARGO COMPARTMENT FLOOR CHANNEL HAS CORROSION BETWEEN STRINGER 30 AND 31 AT STATIONS 1338 TO 1390. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0. 2L74 4F 4A25 19960322002891996032200289WP 1996 3 22 96ZZZW25 119951229A5330 SKIN DOUG DC8 DC863 302198AWP BS 438-456 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SKIN BULGED ALONG STRINGER 32L BETWEEN STATIONS 438 AND 456. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. 2L74 4F 4A25 19960322002901996032200290WP 1996 3 22 96ZZZW26 119951229A5330 SKIN DOUG DC8 DC863 302198AWP LT HORIZ STAB CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SKIN BULGED ALONG STRINGER 32L BETWEEN STATIONS 438 AND 456. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. 2L74 4F 4A25 19960322002911996032200291WP 1996 3 22 96ZZZW27 119951229A5730 PANEL DOUG DC8 DC863 302198AWP WS 585-659 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - RIGHT WING UPPER LEADING EDGE OUTBOARD OF THE NR 4 PYLON HAS SURFACE CORROSION AT ATTACH POINT XFS STATION 585 TO 659. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19960322002921996032200292WP 1996 3 22 96ZZZW28 119951229A5730 PANEL DOUG DC8 DC863 302198AWP RT WING LE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - RIGHT WING UPPER LEADING EDGE PANEL AFT OF NR 3 PYLON HAS CORROSION AT ATTACH POINTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19960322002931996032200293WP 1996 3 22 96ZZZW29 119951229A5730 SKIN DOUG DC8 DC863 302198AWP WS 659-993 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - RT WING OUTBOARD LEADING EDGE UPPER SURFACE AT ATTACH POINTS HAS SURFACE CORROSION AT STATION XFS 659-993. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1. 2L74 4F 4A25 19960322002941996032200294WP 1996 3 22 96ZZZW3 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP BS 1490 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION ON ATTACH FINGER DOUBLER BETWEEN STRINGERS 34L AND 36 AT STATION 1490. REMOVED DOUBLER, CLEANED AND TREATED AREA, FABRICATED AND INSTALLED NEW DOUBLER PER SRM 51-1-0. 2L74 4F 4A25 19960322002951996032200295WP 1996 3 22 96ZZZW30 119951229A5313 STRINGER DOUG DC8 DC863 302198AWP BS 438 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SKIN BULGED ALONG STRINGER 31L BETWEEN STATIONS 438 AND 456. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED STRINGER SPLICE PER SRM 53-4-1. 2L74 4F 4A25 19960322002961996032200296WP 1996 3 22 96ZZZW31 119951229A5320 Z-ANGLE DOUG DC8 DC863 302198AWP BS 1600 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1600 LT SUPPORT CHANNEL BETWEEN INBOARD LEFT SEAT TRACK AND HAT HAS CORROSION. REMOVED AND REPLACED Z-ANGLE SUPPORT SECTION BETWEEN INBOARD SEAT TRACK AND HAT SECTION PER SRM 51-1-8. 2L74 4F 4A25 19960322002971996032200297WP 1996 3 22 96ZZZW32 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1440 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1440 LT CIRCUMFERENTIAL FRAME HAS CORROSION AROUND CUSP AREA. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19960322002981996032200298WP 1996 3 22 96ZZZW33 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1360 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - LEFT SIDE OF FUSELAGE CIRCUMFERENTIAL AT STATION 1360 STRINGER 26L HAS CORROSION ON FRAME. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19960322002991996032200299WP 1996 3 22 96ZZZW34 119951229A5730 SKIN DOUG DC8 DC863 302198AWP WS 763 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - RIGHT WING UPPER SKIN CORROSION BLENDED OUT OF LIMITS AT XRS 763 STRINGER 4. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING NR RGH459319. 2L74 4F 4A25 19960322003001996032200300WP 1996 3 22 96ZZZW35 119951229A5311 FRAME DOUG DC8 DC863 302198AWP BS 1200 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR STATION 1200 LT CIRCUMFERENTIAL FRAME AND CUSP HAD CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-0. 2L74 4F 4A25 19960322003011996032200301WP 1996 3 22 96ZZZW36 119951229A5313 STRINGER DOUG DC8 DC863 302198AWP BS 1186 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION AT STRINGER 36, STATION 1186 INSIDE C3 CARGO. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-5. 2L74 4F 4A25 19960322003021996032200302WP 1996 3 22 96ZZZW37 119951229A5347 TRACK DOUG DC8 DC863 302198AWP FS 1240-1380 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - AFT CARGO COMPARTMENT PIT NR 3 LEFT SIDE FLOOR TRACK ABOVE STRINGER 33L HAS CORROSION FROM FS 1240 TO 1380. REMOVED DAMAGED SECTION OF TRACK AND REPLACED. 2L74 4F 4A25 19960322003051996032200305WP 1996 3 22 96ZZZW4 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP BS 1350 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - SEVERAL SPOTS OF CORROSION AND TORN METAL AT FASTENER HOLES ON SKIN ATTACH DOUBLER AT STATION 1350 BETWEEN STRINGERS 31L AND 31R. REMOVED DOUBLER, CLEANED AND TREATED AREA, FABRICATED AND INSTALLED NEW DOUBLER. 2L74 4F 4A25 19960322003071996032200307WP 1996 3 22 96ZZZW5 119951227A5320 DOUBLER DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CORROSION ON DOUBLER SKIN AROUND NR 4 CARGO DOOR OPENING. REMOVED AND REPLACED DOUBLER PER SRM 51-1-0. 2L74 4F 4A25 19960322003081996032200308WP 1996 3 22 96ZZZW6 119951227A5522565497047 PANEL DOUG DC8 DC863 302198AWP LT ELEVATOR CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - LEFT ELEVATOR LOWER SKIN SURFACE PANELS PITTED AND CORRODED FROM INBOARD END. REMOVED, REPAIRED AND INSTALLED PANELS PER SRM 51-1-0. 2L74 4F 4A25 19960322003091996032200309WP 1996 3 22 96ZZZW7 119951227A5320 SUPPORT DOUG DC8 DC863 302198AWP BS 1680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - CABIN FLOOR SUPPORT FROM STATION 1680 RT TO 1660 RT NEXT TO DOOR FRAME LOWER END HAD CORROSION. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. 2L74 4F 4A25 19960322003101996032200310WP 1996 3 22 96ZZZW8 119951227A5330 SKIN DOUG DC8 DC863 302198AWP FUSELAGE CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - RIGHT AFT GALLEY DOOR CUTOUT LOWER AREA SKIN CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING NR 45931-4. 2L74 4F 4A25 19960322003111996032200311WP 1996 3 22 96ZZZW9 119951227A5753 SKIN DOUG DC8 DC863 302198AWP LT TE FLAP CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION - LEFT WING FLAP INBOARD LOWER SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-21. 2L74 4F 4A25 19960322004461996032200446CE 1996 3 22 96ZZZX1256 119951129A531207126261 BULKHEAD CESSNA182 182N 2072730CE FS 230.187 CRACKED A GGSAK NONE O OTHER ININSP/MAINT 1 NM13925195093 18260241 CRACK IN THE RT RUDDER CABLE CUT-OUT HOLE AT THE RT UPPER OUTBOARD RADIUS. ALSO, CRACK FROM RT RUDDER STOP BOLT HOLE UPWARD TO BULKHEAD BEND RADIUS, THEN ALONG BEND RADIUS FOR .3750 INCH. SUSPECT CAUSED BY RUDDER SLAMMING AGAINST STOPS IN GUSTY WIND. SUBMITTER RECOMMENDS USE OF RUDDER LOCKS AND/OR SECURING AIRCRAFT IN DIRECTION TO MINIMIZE MOVEMENT IN GUSTY CONDITIONS. 1H71 3O NT3A13 19960322006001996032200600NE 1996 3 22 96ZZZM327 219951130A7321 FUEL CONTROL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 ENGINE MALFUNCTIONED A A6WAE ENGINE SHUTDOWN J WARNING INDICATION DEDESCENT 1 GL31610AW E2082 WITH ENGINES AT FLIGHT IDLE, AND IN CLEAR (VFR CONDITION) NR 1 ENGINE N1 PLUS N2 ROLLED BACK TO APPROXIMATELY 30 PERCENT. PRECAUTIONARY SHUT DOWN OF NR 1 ENGINE EMERGENCY CHECK LIST COMPLETED. (M) 2H74 4F4 FRTA49EU E6NE 19960322006011996032200601EU 1996 3 22 96ZZZM328 119951021A5320 ANGLE BAG BAE146BAE146200A 1500266EU FRAME 36 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FREIGHT ANGLE FOR FRAME 36, LOWER CENTER AREA CRACKED. REPAIRED FREIGHT ANGLE AS PER 146 SRM. 2H74 4F RTA49EU 19960322006021996032200602EU 1996 3 22 96ZZZM329 119951020A5260 TRACK BAG BAE146BAE146200A 1500266EU AIRSTAIR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 AFT AIRSTAIR INBOARD TRACK IS CORRODED AT VERY AFT END, CORROSION IS GREATER THAN .005 INCH REF SRM 51-10-02. RAIL ALREADY REMOVED. INSTALLED AFT AIRSTAIR INBOARD TRACK ASSY AND APPLIED PRC TO PROTECT RAIL. 2H74 4F RTA49EU 19960322006031996032200603EU 1996 3 22 96ZZZM330 119951020A5400 ATTACH STRUCT BAG BAE146BAE146200A 1500266EU NR 3 PYLON DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 NR 3 MOTOR (PYLON) AFT MOUNT FOR SHOULDER COWL HAS MOUNTING HOLES ENLONGATED WHERE SHOULDER COWL ATTACHES TO LORD MOUNT, SEE REPAIR HC710H9003 FOR FIX. REPAIRED NR 3 ENGINE SHOULDER COWL AFT DOOR LORD MOUNT ATTACH STRUCTURE IAW BAE FAX PJN/1954-91. (M) 2H74 4F RTA49EU 19960322006041996032200604EU 1996 3 22 96ZZZM331 119951019A5320 REINFORCE PLATE BAG BAE146BAE146200A 1500266EU FUSELAGE DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 CHAFING DISCOVERED ON FUSELAGE REINFORCING PLATE BELOW RIGHT FORWARD FUSELAGE WING, LUG DAMAGE TYPICALLY CAUSED BY ARMPIT FAIRING. MEASURES .010 INCH - .014 INCH DEEP. PERFORMED EDDY CURRENT INSPECTION AFTER BLENDING AS PER FAX DJH/RJ1230-95. NO CRACK INDICATIONS WERE EVIDENT AT EITHER DAMAGED AREA. BLENDING, ALODINED, PRIMED AND PAINTED CHAFED AREA RIGHT FUSELAGE APPLIED TEMP RUB STRIP WITH SEALANT. 2H74 4F RTA49EU 19960322006051996032200605EU 1996 3 22 96ZZZM332 119951018A5311 FASTENER BAG BAE146BAE146200A 1500266EU FRAME 32 MISSING A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FRAME 32 IN CABIN APPROXIMATELY 9 INCHES ABOVE FLOOR LINE ON RIGHT SIDE, IS MISSING A HI-LOK FASTENER. INSTALLED MISSING HI-LOK FASTENER. 2H74 4F RTA49EU 19960322006061996032200606EU 1996 3 22 96ZZZM333 119951018A5753 SKIN BAG BAE146BAE146200A 1500266EU LT TE FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT INBOARD TRAIL FLAP TOP SIDE HAS 2 SPOTS OF WEAR THROUGH PAINT, NEED FURTHER INVESTIGATION FOR LIMITS. BLENDED DAMAGED AREA TO A SMOOTH DEPRESSION. PERFORMED ET TO BLENDED AREA. NO DEFECTS FOUND. INSPECTION RIVET NO DAMAGE NOTED, TREATED PRIMED AND TOP COATED. REPROTECTED WITH ALOCROM FOLLOWED BY PRIMER AND TOPCOAT ALL IAW DJH/RJ1301-95. 2H74 4F RTA49EU 19960322006071996032200607EU 1996 3 22 96ZZZM334 119951018A5753 CARRIAGE BAG BAE146BAE146200A 1500266EU NR 2 TE FLAP WORN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 RIGHT NR 2 UPPER FLAP CARRIAGE HAS A WEAR MARK APPROXIMATELY .040 INCH TO .050 INCH DEEP IN THE VERY UPPER INBOARD EDGE ADJACENT TO THE BONDING LEAD ATTACHMENT TO THE FLAP. BLENDED WEAR MARK TO A SMOOTH DEPRESSION AS PER AVRO FAX. PERFORMED EDDY CURRENT TO BLENDED AREA AND FOUND TO BE CRACK FREE. REPROTECTED THE DAMAGED AREA W/ALOCROM, PRIMED, TOPCOATED AND REPOSITIONED BONDING. 2H74 4F RTA49EU 19960322006081996032200608EU 1996 3 22 96ZZZM335 119951017A5530 TERMINAL BLOCK BAG BAE146BAE146200A 1500266EU HORIZ STAB CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FOUND CORRODED TERMINAL BLOCK AFT OF HORIZONTAL STABILIZER REAR SPAR RIGHT SIDE INBOARD AT VERTICLE FIN TERMINAL BLOCK LABELED UB25. LOCATED ON ELEVATOR CONTROL BOX STRUCTURE. REMOVED AND REPLACED TERMINAL BLOCK UB25 AND REPLACED WIRE LUGS TO UB25. ELEVATOR FDR INDICATION, OPS CHECK OK. 2H74 4F RTA49EU 19960322006091996032200609EU 1996 3 22 96ZZZM336 119951017A5753 BOLT BAG BAE146BAE146200A 1500266EU NR 3 FLAP TRACK CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FORWARD FLAP ATTACH BOLT AT LEFT FLAP TRACK NR 3 IS CORRODED. REMOVED, CLEANED AND INSPECTED BOLT, REINSTALLED BOLT. NO CORROSION FOUND. 2H74 4F RTA49EU 19960322006101996032200610EU 1996 3 22 96ZZZM337 119951016A5753 BOLT BAG BAE146BAE146200A 1500266EU NR 3 FLAP TRACK FAILED TEST A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT NR 3 FLAP TRACK CARRIAGE TO FLAP ATTACH BOLT HAS FAILED UT INSPECTION AND NEEDS NEW BOLT INSTALLED. REMOVED AND REPLACED FLAP ATTACH BOLT. 2H74 4F RTA49EU 19960322006111996032200611EU 1996 3 22 96ZZZM338 119951004A5755 BOLTS BAG BAE146BAE146200A 1500266EU LT SPOILER CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT WING OUTBOARD LIFT SPOILER FOUND BOTH FORWARD AND AFT JACK BOLTS HAVE PLATING MISSING ON BOLT SHANK. REPLACED FWD AND AFT JACK BOLTS. (M) 2H74 4F RTA49EU 19960322006121996032200612EU 1996 3 22 96ZZZM339 119951003A5720 JO-BOLTS BAG BAE146BAE146200A 1500266EU CTR WING LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 CENTER WING SECTION LEFT SIDE AT RIB 2 HAS 2 JO-BOLT FASTENERS ON TOP SKIN STRINGER JOINT FITTINGS THAT ARE LOOSE AND WILL NOT TORQUE UP. SSI 57-10-117. REMOVED 2 JO-BOLT FASTENERS AND INSTALLED OVERSIZE MEL FASTENERS PER RIL NR HC571H9033 AND AVRO FAX'S GCB/RJ1186-95 PG 1/2;GCB/RJ1179-95. 2H74 4F RTA49EU 19960322006131996032200613EU 1996 3 22 96ZZZM340 119951002A5320 RIVETS BAG BAE146BAE146200A 1500266EU FRAME NR 19 MISSING A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FRAME 19 RIGHT SIDE BELOW THE 3RD ABUTMENT DIAPHRAM THERE ARE 2 RIVETS MISSING IN STRUCTURE. INSTALLED ABOVE RIVETS. 2H74 4F RTA49EU 19960322006141996032200614EU 1996 3 22 96ZZZM341 119951002A5753 BOLT BAG BAE146BAE146200A 1500266EU NR 2 TE FLAP CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 RIGHT NR 2 FLAP CARRIAGE UPPER CARRIAGE TO FLAP BOLT HAS FLAKING PROTECTIVE COATING AND IS CORRODED. REMOVED AND REPLACED CARRIAGE TO FLAP BOLT NR 2 POS. 2H74 4F RTA49EU 19960322006151996032200615EU 1996 3 22 96ZZZM342 119950929A5755 TERM BLOCK BAG BAE146BAE146200A 1500266EU NR 3 SPOILER CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 TERMINAL BLOCK AT RIGHT NR 3 LIFT SPOILER JACK IS CORRODED. REPLACED TERMINAL BLOCK 'M' AT RIGHT OUTER SPOILER JACK. W/C GENERATED FOR OP CHECK. (M) 2H74 4F RTA49EU 19960322006161996032200616EU 1996 3 22 96ZZZM343 119950924A5520 BOLT BAG BAE146BAE146200A 1500266EU LT ELEVATOR FAILED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT ELEVATOR NR 4 HINGE, LOWER 'A' FRAME BOLT FAILED NDT INSPECTION. INSTALLED NEW LOWER LEFT NR 4 'A' FRAME BOLT AND SAFETIED. 2H74 4F RTA49EU 19960322006171996032200617EU 1996 3 22 96ZZZM344 119950919A5751 BOLT BAG BAE146BAE146200A 1500266EU LT AILERON BROKEN A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT AILERON RIB 18 UPPER 'A' FRAME FAIL/SAFE BOLT BROKEN. REMOVED AND REPLACED RIB 18 UPPER 'A' FRAME FAIL/SAFE BOLT. 2H74 4F RTA49EU 19960322006181996032200618EU 1996 3 22 96ZZZM345 119950918A5753 PIVOT PIN BAG BAE146BAE146200A 1500266EU NR 4 FLAP TRACK DEFECTIVE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 RIGHT WING OUTER FLAP TRACK NR 4 INSPECTION OF FLAP TRACK PIVOT PIN, LOWER CARRIAGE TO INTERCARRIAGE LEVER FOUND DEFECT ALONG SHANK OF BOLT FROM BOLT HEAD TO THREADS. INSPECTION CARD NR 267 SSI NR 57-55-127. INSTALLED NEW PIVOT PIN ASSY AT RIGHT OUTBOARD NR 4 FLAP TRACK LOWER CARRIAGE ON INBOARD INNER CARRIAGE LEVER. 2H74 4F RTA49EU 19960322006191996032200619EU 1996 3 22 96ZZZM346 119950918A5755HC5724H09909204 BOLTS BAG BAE146BAE146200A 1500266EU RT SPOILER CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 RIGHT WING ROLL SPOILER INBOARD HINGE BOLT P/N HC72H0909-204 HAS CORROSION IN THREADS, CLEANED AND FOUND DEEP PIT IN THREAD AREA. SCRAP BOLT. INSTALLED NEW BOLT ASSY ON RIGHT ROLL SPOILER INBD HINGE. 2H74 4F RTA49EU 19960322006201996032200620NE 1996 3 22 96ZZZM347 219951111A7200 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 3 MALFUNCTIONED A A6WAE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 GL31610AW E2082 NR 3 ENGINE VIBRATION WENT TO 1.5, RETARDED THRUST LEVER AND IT STAYED AT 1.5. NO VIBES FELT OR ABNORMAL INDICATIONS. 10 MINUTES LATER TGT WENT TO 1000 DEGREES, CREW SHUT DOWN ENGINE. DIVERTED TO ATW. REMOVED AND REPLACED NR 3 ENGINE. 2H74 4F4 FRTA49EU E6NE 19960322006211996032200621EU 1996 3 22 96ZZZM348 119951214A5720 JO-BOLTS BAG BAE146BAE146100A 1500260EU CTR TANK RIB LOOSE A A6WAK NONE O OTHER ININSP/MAINT 1 GL31463AP E1063 LOOSE JO-BOLTS REQUIRE REPLACEMENT IN CENTER TANK RIB 0 AND RIB 2 LEFT AND RIGHT. REPLACED JO-BOLTS. 2H74 4F RTA49EU 19960322006221996032200622NE 1996 3 22 96ZZZM349 219951114A7200 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 1 MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31609AW E2070 AIRCRAFT RETURNED TO DEN NR 1 ENGINE TGT IND FULL SCALE AND FLAGGED. N1 WNET TO 60 PERCENT AND WF WENT TO 600 LBS. TMS WAS ON AT THE TIME. LOCKED DOWN ENGINE AND FERRIED TO ATW FOR REPAIR. BUSBAR BROKE. 2H74 4F4 FRTA49EU E6NE 19960322006231996032200623EU 1996 3 22 96ZZZM350 119951115A5350 RIB BAG BAE146BAE146300A 1500267EU RADOME DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 REF AVRO FAX DJR/RJ0379-95, RIGHT FUSELAGE NOSE DAMAGE AT RIB NR 1 BETWEEN UPPER 'E' LAP JOINT AND LOWER RADOME LATCH IS TO BE REASSESSED FOR REPAIR OR FURTHER SERVICE AT NEXT 'C' CHECK OR COMPLETION OF 3000 FLTS WHICHEVER IS SOONER. CURRENT CYCLES 16,863. 2H74 4F RTA49EU 19960322006241996032200624EU 1996 3 22 96ZZZM351 119951113A5320 STIFFENERS BAG BAE146BAE146300A 1500267EU FS 25.94 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 WHILE COMPLIED WITH ITEM 3 OF EO E95/003/653 2 CRACKS WERE DISCOVERED AT FRAME 29 IN HYDRAULIC BAY. CRACKS WERE LOCATED AT BOLT HOLES OF STIFFENER 25.94 LEFT AND 25.94 RIGHT. REPAIRED FRAME 29 STIFFENERS AT 25.94 LEFT AND RIGHT SIDES IAW EO E95/003/653 REV ORIG. 2H74 4F RTA49EU 19960322006251996032200625EU 1996 3 22 96ZZZM352 119951114A2710 CABLE BAG BAE146BAE146300A 1500267EU AILERON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 AILERON INTERCONNECT CABLE HAS CORROSION AT WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTIONS OF AILERON INTERCONNECT CABLE IAW MM 27-11-44. REF W/C 6004 FOR FUNCTIONAL TEST OF AILERON CONTROLS. 2H74 4F RTA49EU 19960322006261996032200626EU 1996 3 22 96ZZZM353 119951110A5320 GUSSET BAG BAE146BAE146300A 1500267EU FRAME 42-43 CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 SURFACE CORROSION ON GUSSET PLATES FRAME 42 TO 43 RIGHT INTERCOSTAL FLOOR SUPPORT STRUCTURE. REMOVED AND REPLACED GUSSET PLATES. ALODINE, PRIME AND PAINT COVERED AREA WITH PRC PER SRM. 2H74 4F RTA49EU 19960322006271996032200627EU 1996 3 22 96ZZZM354 119951110A5320 GUSSET BAG BAE146BAE146300A 1500267EU FRAME 15 CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 ONE GUSSET PLATE CORRODED ON FORWARD VESTIBULE INTERCOSTALS JUST LEFT OF FUSELAGE CENTER LINE AT FRAME 15. FOUND CORROSION BAD ENOUGH TO REPLACE GUSSET PLATE, REPLACED, TREATED AND APPLIED PROTECTIVE FINISH. 2H74 4F RTA49EU 19960322006281996032200628EU 1996 3 22 96ZZZM355 119951109A5320 SILL BAG BAE146BAE146300A 1500267EU PAX DOOR CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 FORWARD PASSENGER DOOR SILL PLATE HAS AREAS OF CORROSION NOTED. UNDER AFT GIRT BAR BRACKET. UNDER SPACER FOR TREAD PLATE, AND IN BEND RADIUS OF THE FLANGE. FOUND ALL CORROSION TO BE MINOR SURFACE CORROSION. CLEANED, TREATED AND REAPPLIED PROTECTIVE FINISH. ONLY EXCEPTION WAS CORROSION IN RADIUS. REMOVED DAMAGE, TREATED ADN REAPPLIED FINISH IAW FAX JM/RJ0711-95 AND ROB. 2H74 4F RTA49EU 19960322006291996032200629NE 1996 3 22 96ZZZM356 219951128A7200 ENGINE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE NR 4 MALFUNCTIONED A A6WAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31608AW E2049 PACK NR 2 EMITS A BLUE HAZE IN THE CABIN. AIRCRAFT FERRY TO ATW FOR TROUBLESHOOTING DUE TO HISTORY. REPLACED THE NR 4 ENGINE. 2H74 4F4 FRTA49EU E6NE 19960322006301996032200630EU 1996 3 22 96ZZZM357 119951127A2120 AIR DISTR BAG BAE146BAE146200A 1500266EU CABIN SMOKE A A6WAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 GL31608AW E2049 FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. WITH NR 1 A/C OFF SMOKE DISSIPATED, UNABLE TO DUP SMELL IN NR 1 OR NR 2 PACKS WITH APU OR ENGINE AIR AT THIS TIME. 2H74 4F RTA49EU 19960322006311996032200631 1996 3 22 96ZZZM358 419951114A2565 ESCAPE SLIDE BAG BAE146BAE146300A 1500267EU CABIN INOP A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31615AW E3141 RIGHT AFT ESCAPE SLIDE LIGHTING INOP. REPLACED SLIDE. 2H74 4F RTA49EU 19960322006321996032200632EU 1996 3 22 96ZZZM359 119951016A3230200915248 CRANK BAG BAE146BAE146200A 1500266EU RT MLG CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW HSA163 E2082 RIGHT MLG DIRECTIONAL CRANK AFT BUSHING SURFACE SHOWS SIGNS OF CORROSION. TRANSFER TO W/O BT4300, GEN W/C TO INSTALL SERVICEABLE CRANK, NR 7021. 2H74 4F RTA49EU 19960322006331996032200633EU 1996 3 22 96ZZZM360 119950921A5320 INTERCOSTAL BAG BAE146BAE146200A 1500266EU FUSELAGE CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 ZONE 100, INTERNAL, BETWEEN FRAMES 14 AND 15 INTERCOSTAL IS CRACKED AT FUSELAGE CENTER LINE. SSI 53-10-127. REPLACED INTERCOSTAL. 2H74 4F RTA49EU 19960322006451996032200645WP 1996 3 22 AALA960285 119951224A783012636622 TR DRIVE DOUG DC10 DC1010 3022110WP NR 2 ENG DEFECTIVE A AALAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 SW07132AA 47827 HNL - FLT NR 14 - DURING CLIMB-OUT, FLT CREW NOTED IMPAIRED CLIMB PERFORMANCE AND SOME AILERON AND RUDDER TRIM REQUIRED TO MAINTAIN WINGS LEVEL. A/C RETURNED TO HNL AND LANDED W/O INCIDENT. AFTER ARRIVAL, NR 2 ENG RT TRANSLATOR COWL NOTED PARTIALLY DEPLOYED. COWL MANUALLY STOWED AND NR 2 REVERSER PLACARDED INOP. SUBSEQUENTLY AT LAX/26, REPLACED NR 2 ENG RT REVERSER HALF AND REPLACED CORE HOUSING AND DRIVE CABLE ON LT REVERSER HALF. ACCOMPLISHED THRUST REVERSER RIGGING BUT CONTINUED PLACARD. SUBSEQUENTLY AT JFK/28, REPLACED NR 2 ENG LT REVERSER HALF, NR 2 ENG THRUST REVERSER DRIVE AND SHUTOFF VLV. ACCOMP LEAK AND GROUND CHECK WITH NO DEFECTS FOUND. SYS GROUND CHECKED NORMAL OPERATION. (M) 2L73 4F A22WE 19960322007571996032200757WP 1996 3 22 CAL960215 119951229A5313 LONGERON DOUG DC10 DC1030 3023501WP BS 1536/1545 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW091306777547 47866 KUL - INSPECTION FOUND LONGERON 37R SPLICE CORRODED AT STATION 1536 AND 1545. THE AREA WAS REPAIRED IAW ECRA 5310-03223. (M) 2L73 4F A22WE 19960322007621996032200762WP 1996 3 22 CAL960220 119951212A5313 STRINGER DOUG DC10 DC1030 3023501WP BS 1501 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW094106866458 47867 KUL - INSPECTION FOUND CORROSION ON STRINGER 30R AT STATION 1501. THE STRINGER WAS REPAIRED IAW SRM 53-10-00. (M) 2L73 4F A22WE 19960322007631996032200763WP 1996 3 22 CAL960221 119951101A5512NLC6041506L SKIN DOUG DC10 DC1030 3023501WP RT ELEVATOR WARPED A CALAK NONE O OTHER ININSP/MAINT 1 SW094106866458 47867 KUL - INSPECTION FOUND THE RIGHT OUTBOARD ELEVATOR UPPER SKIN WARPED. THE SKIN WAS REPAIRED IAW SRM 55-10-00, PAGE 15, FIGURE 8. (M) 2L73 4F A22WE 19960322007641996032200764WP 1996 3 22 CAL960222 119951108A5320 SUPPORT DOUG DC10 DC1030 3023501WP CABIN CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW094106866458 47867 KUL - INSPECTION FOUND THE FLOOR BOARD SUPPORT CHANNEL CORRODED AT AFT SIDE BETWEEN G6 AND G7 AISLE. THE SUPPORT WAS REPLACED IAW SRM 53-16-01, FIGURE 10, SHEET 2, ITEM 6. (M) 2L73 4F A22WE 19960322007651996032200765WP 1996 3 22 CAL960223 119951028A5320 SUPPORT DOUG DC10 DC1030 3023501WP BS 1887 CORRODED A CALAK NONE O OTHER ININSP/MAINT 1 SW094106866458 47867 KUL - INSPECTION FOUND FLOOR BOARD SUPPORT CORRODED AT STATION 1887. THE SUPPORT WAS REPLACED IAW SRM 53-16-01, FIGURE 10, ITEM 6. (M) 2L73 4F A22WE 19960322007661996032200766WP 1996 3 22 CAL960224 119951014A5320 ATTACHMENT DOUG DC10 DC1030 3023501WP BS 1967 CRACKED A CALAK NONE O OTHER ININSP/MAINT 1 SW094106866458 47867 KUL - INSPECTION FOUND A 2 INCH CRACK IN STATION 1967 FRAME ATTACHMENT TO STRINGER 51R. A REPAIR WAS CARRIED OUT IAW SRM 53-16-01, FIGURE 17, ITEM 42G. (M) 2L73 4F A22WE 19960322008211996032200821EU 1996 3 22 RF6A951111 119951129A335010620BAC6 SWITCH BAG ATP ATP EU COCKPIT FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31853AW9587 2022 SBN - DURING POWER DOWN OF AIRCRAFT THE EMERGENCY LIGHTS CAME, REGARDLESS OF SWITCH POSITION. MAINTENANCE REPAIRED WIRES ON SWITCH. (M) 2L72 4T RTA27NM 19960322008241996032200824EU 1996 3 22 UF6A950801 119950826A335010620BAC6 SWITCH BAG ATP ATP EU COCKPIT INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31857AW7506 2034 ORD - FLT NR 5090 - OFF INDICATOR, CABIN EMERGENCY LIGHT PBSI INOPERABLE. MAINTENANCE REPLACED THE SWITCH. (M) 2L72 4T RTA27NM 19960322008251996032200825EU 1996 3 22 UF6A950802 119950827A33504197195086035 SWITCH BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31860AW6247 2037 ORD - FLT NR 5065 - FORWARD EMERGENCY LIGHT SWITCH INOPERABLE. MAINTENANCE REPLACED SWITCH. (M) 2L72 4T RTA27NM 19960322008261996032200826EU 1996 3 22 UF6A950901 119950902A3350JD922J01001553 DIODE CARD BAG ATP ATP EU COCKPIT FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31854AW8552 2028 ORD - FLT 5063 - EMERGENCY LIGHTS ILLUMINATE WHEN CWP LEGEND TEST IS PRESSED. MAINTENANCE REPLACED DIODE CARD. (M) 2L72 4T RTA27NM 19960322008271996032200827EU 1996 3 22 UF6A950902 119950903A5270 WIRE BAG ATP ATP EU PAX DOOR CHAFED A UF6AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31856AW7996 2032 ORD - FLT NR 5045 - DOOR WARNING LIGHT ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPAIRED CHAFED WIRE ON DOOR MICROSWITCH, P/N 9EN4D81BT1BB2. (M) 2L72 4T RTA27NM 19960322008281996032200828EU 1996 3 22 UF6A950903 119950912A33506013211 BATTERY PACK BAG ATP ATP EU CABIN DISCHARGED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31851AW2814 560 2020 CWA - FLT NR 5026 - EMERGENCY LIGHTS SECTION INOPERABLE. MAINTENANCE REPLACED BATTERY PACK. (M) 2L72 4T RTA27NM 19960322008291996032200829EU 1996 3 22 UF6A951008 119951020A52709EN4D83DB1BS SWITCH BAG ATP ATP EU CABIN DOOR DIRTY A UF6AK NONE N FALSE WARNING LDLANDING 1 GL31859AW7531 2036 ORD - FLT NR 5064 - REAR CABIN DOOR EXIT WARNING ILLUMINATED ON LANDING. MAINTENANCE CLEANED ROLLERS ON THE DOOR SWITCHES. (M) 2L72 4T RTA27NM 19960322008301996032200830EU 1996 3 22 UF6A951009 119951021A2611CG7PT2 SMOKE ALARM BAG ATP ATP EU LAVATORY FAILED A UF6AK NONE N FALSE WARNING TXTAXI/GRND HDL 1 GL31855AW8337 2029 ORD - FLT NR 5104 - LAVATORY SMOKE ALARM GOES OFF WHEN STARTING ENGINE. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE ALARM. (M) 2L72 4T RTA27NM 19960322008311996032200831EU 1996 3 22 UF6A951010 119951023A760391SEI6 SWITCH BAG ATP ATP EU NR 1 PWR LEVER OUT OF ADJUST A UF6AK NONE P NO WARNING INDICATION DEDESCENT 1 GL31856AW8264 2032 SBN - FLT NR 5105 - WHEN NR 1 POWER LEVER IS RETARDED THERE IS NO GEAR WARNING HORN. MAINTENANCE ADJUSTED THE MICROSWITCH ON THE THROTTLE SERVO UNIT AND PERFORMED A FUNCTION TEST. OPS CHECK GOOD. (M) 2L72 4T RTA27NM 19960322008321996032200832EU 1996 3 22 UF6A951011 119951027A2120 AIR DISTR BAG ATP ATP EU CABIN ODOR A UF6AK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31854AW 2028 ORD - FLT NR 5065 - ELECTRICAL BURN SMELL IN CABIN. MAINTENANCE INSPECTED NR 2 RECIRC FAN, NO DEFECTS NOTED. MAINTENANCE OPERATED NR 2 PACK, OPS CHECK GOOD. (M) 2L72 4T RTA27NM 19960322008331996032200833EU 1996 3 22 UF6A951012 119951030A33506013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31858AW7331 2035 SBN - MAINTENANCE FORWARD DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER SUPPLY. (M) 2L72 4T RTA27NM 19960322008341996032200834EU 1996 3 22 UF6A951013 119951027A3350362624 STRIP BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31860AW6567 2037 ORD - MAINTENANCE FORWARD SECTION EMERGENCY TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP. (M) 2L72 4T RTA27NM 19960322008351996032200835EU 1996 3 22 UF6A951014 119951031A335058786 POWER RIBBON BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31854AW8871 2028 ORD - MAINTENANCE FRONT EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED POWER RIBBON. (M) 2L72 4T RTA27NM 19960322008361996032200836EU 1996 3 22 UF6A951101 119951101A33506013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31860AW6596 2037 SBN - MAINTENANCE FOUND OVERWING EMERGENCY EXIT LIGHT EXTINGUISH AFTER 1 MINUTE OF TEST. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT POWER SUPPLY. (M) 2L72 4T RTA27NM 19960322008371996032200837EU 1996 3 22 UF6A951102 119951104A3350362634 STRIP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31853AW9458 2022 ORD - FLT NR 5015 - TWO STRIPS OF FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP. (M) 2L72 4T RTA27NM 19960322008381996032200838EU 1996 3 22 UF6A951103 119951106A33506013211 BATTERY PACK BAG ATP ATP EU COCKPIT DISCHARGED A UF6AK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL31859AW7594 2036 CWA - FLT NR 5028 - BURNING SMELL IN COCKPIT AND EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POSITION 5 EMERGENCY BATTERY PACK. (M) 2L72 4T RTA27NM 19960322008391996032200839 1996 3 22 UF6A951104 319951106A6140S5600045N CONNECTOR BAG ATP ATP EU RT ENGINE DIRTY A UF6AK NONE N FALSE WARNING CRCRUISE 1 GL31857AW7836 2034 ORD - FLT NR 5114 - RIGHT PROP OIL PRESSURE CWP WARNING OCCURED FOR 2-3 SECONDS THEN EXTINGUISHED. MAINTENANCE INSPECTED AND CLEANED CANNON PLUG B. (M) 2L72 4T RTA27NM 19960322008401996032200840EU 1996 3 22 UF6A951106 119951108A7931TP0751010 PRESS SWITCH BAG ATP ATP EU RT ENGINE FAILED A UF6AK NONE N FALSE WARNING DEDESCENT 1 GL31857AW6177 2034 ORD - FLT NR 5106 - NR 2 PROP OIL PRESSURE CWP ILLUMINATED ON SHORT FINAL. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH ON THE NR 2 RBG. (M) 2L72 4T RTA27NM 19960322008411996032200841EU 1996 3 22 UF6A951107 119951110A2421BA03304 GENERATOR BAG ATP ATP EU RT ENGINE FAILED A UF6AO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC TOTAKEOFF 1 GL31860AW6580 1710 2037 CWA - FLT NR 5026 - RIGHT GENERATOR FAILED AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED GENERATOR. (M) 2L72 4T RTA27NM 19960322008421996032200842EU 1996 3 22 UF6A951108 119951118A5270JD920J069200 CABLE BAG ATP ATP EU EMER EXIT BROKEN A UF6AO OTHER N FALSE WARNING LDLANDING 1 GL31854AW8975 2028 ORD - FLT NR 5066 - EXIT CWP AND RIGHT EMERGENCY EXIT ILLUMINATED ON FINAL. MAINTENANCE REMOVED AND REPLACED EXIT WARNING CABLE, EXIT DOOR OPS CHECKED GOOD. (M) 2L72 4T RTA27NM 19960322008431996032200843EU 1996 3 22 UF6A951109 119951126A527014XE112 SWITCH BAG ATP ATP EU RT EMER EXIT FAILED A UF6AK NONE N FALSE WARNING DEDESCENT 1 GL31855AW8520 2029 GRB - FLT NR 5067 - ON SHORT FINAL, 'EXITS' CWP ILLUMINATED FOR 1-2 SECONDS. MAINTENANCE ADJUSTED THE RIGHT OVERWING EXIT DOOR MICROSWITCH. (M) 2L72 4T RTA27NM 19960322008441996032200844EU 1996 3 22 UF6A951110 119951126A3020MT37K1914SN CONNECTOR BAG ATP ATP EU RT ENG DE-ICE BROKEN WIRE A UF6AO OTHER J WARNING INDICATION CRCRUISE 1 GL31851AW 2020 ORD - FLT NR 5029 - RIGHT ENGINE DE-ICE FAILED. MAINTENANCE REPAIRED 2 BROKEN WIRES, 1246A AND 1248C, IN MOD 3, TO CANNON PLUG 'B'. (M) 2L72 4T RTA27NM 19960322008951996032200895NM 1996 3 22 96ZZZX1292 119950309A5711 SPAR BOEING727 72722C 138400FNM FS 870 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, CORROSION ON AFT UPPER SPAR CAP CENTER WING TANK AT FS 870, LBL 33 TO LBL 48. CUT WEB FROM LBL 33 TO LBL 48, CUT SPAR CAP, 1 INCH BY 4 INCHES. INSTALLED WEB AND ANGLES FOR SPAR REPAIR PER SRM 57-10-6 (WEB REPAIR), 51-40-4 AND AERO NR 95PMSI.053R0-1, DATED 2-18-95 (SPAR REPAIR). TAT: 53,881.4 HOURS. TAC: 36,380. 2L73 4F A3WE 19960322008961996032200896NM 1996 3 22 96ZZZX1293 119950309A5320 CORD BOEING727 72722C 138400FNM BS 312 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, LOWER RT CORD ANGLE CORRODED ON VERTICAL LEG, STA 312, STR 27R. REMOVED AND REPLACED RT NOSE CORD ANGLE WITH NEW ONE PER SRM 51-10-1, PARAGRAPH 4. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322008971996032200897NM 1996 3 22 96ZZZX1294 119950309A5320 SUBFLOOR BOEING727 72722C 138400FNM BS 1160 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, CORROSION ON SUB-FLOOR, STA 1160, BLL 23. CUT 10 INCH BY 7 INCH CORRODED AREA AND INSTALLED 12 INCH BY 10 INCH .063 INCH 7075-T6 DOUBLER PER SRM 51-40-2. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322008981996032200898NM 1996 3 22 96ZZZX1295 119950309A5320 SUBFLOOR BOEING727 72722C 138400FNM BS 1130-1136 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING C-CHECK, CORROSION CABIN SUB-FLOOR, STA 1130 TO STA 1136, STR 48 TO STR 58. FOUND CORROSION OUT OF LIMITS, REPAIRED PER SRM 51-40-4, FIGURE 1, MATERIALS USED: ALCLAD 7075-T6.050, 22 INCH BY 2.5 INCH, 7075-T6.90, 18 INCH BY 4 INCH EXTRUSION, 7075-T6.90, 3.5 INCH BY 1.25 INCH BY 36 INCH WEB REPAIR PER SRM 51-40-2. MAINTENANCE USED ALCLAD 7075-T6.063, 12 INCH BY 6 INCH. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322008991996032200899NM 1996 3 22 96ZZZX1296 119950309A5321 FLOOR PANEL BOEING727 72722C 138400FNM BS 1030-1110 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, CORROSION AND CRACK ON CABIN FLOOR PANEL, STA 1030 TO STA 1110, STR 48 TO STR 60. FABRICATED NEW FLOOR PANEL, STA 1030 - STA 1110, STR 48 TO STR 60 PER SRM 51-10-1 AND SRM 53-20-2. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322009001996032200900NM 1996 3 22 96ZZZX1297 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 780-800 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, CORROSION, NR 7 SEAT TRACK, STA 780 TO STA 800. REMOVED CORRODED SEAT TRACK, MADE NEW SEAT TRACK, ALODINED AND PRIMED AND INSTALLED PER SRM 51-10-1. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322009011996032200901NM 1996 3 22 96ZZZX1298 119950309A5315 FLOOR BEAMS BOEING727 72722C 138400FNM BS 400-480 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, LIGHT CORROSION CABIN FLOOR BEAMS, STA 480 AND STA 400, AND SEAT TRACK LIPS. CUT OUT DAMAGED AREA, BS 400, LBL 27, AND REPAIR PER SRM 51-40-4 7075-T6.063, 12 INCH LONG DOUBLER INSTALLED. REMOVED LIGHT CORROSION, BS 400 TO BS 480 PER SRM 51-10-6 MAT. LOSS .003 INCH. TREATED AND PRIMED PER SRM 51-10-2. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322009021996032200902NM 1996 3 22 96ZZZX1299 119950309A5313 STRINGER BOEING727 72722C 138400FNM FS 265 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FS 265, STR 9R, HAS SEVEN CRACKED RIVET HOLES. FS 265, STR 10R, HAS BURNISHED SKIN OUT OF LIMITS PER SRM 53-30-01. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED PARTS PER SRM 53-30-3, FILLER MATERIAL .040 INCH, 2024T3, 12 INCH BY 16 INCH DOUBLER MATERIAL, .050 INCH, 2024-T3 15 .50 INCH BY 16 INCH. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322009031996032200903NM 1996 3 22 96ZZZX1300 119950309A5711 SPAR BOEING727 72722C 138400FNM BS 870 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, WING, CENTER SECTION, INTERIOR REAR SPAR WEB, BLR 48, BULGING. POP RIVET HEADS. CORROSION STA 870. CUT OUT 2 INCH BY 6 INCH BULGED AREA AND INSTALLED DOUBLER 10 INCH BY 12 INCH, .200 INCH 2024T3 PER SRM 57-10-6. REPLACED STIFFENER PER SRM 51-10-1, PARAGRAPH 4, AND FASTENERS PER SR 51-30-2. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009041996032200904NM 1996 3 22 96ZZZX1301 119950309A2820 VENT LINE BOEING727 72722C 138400FNM BS 580 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, VENT TURBINE AT STA 580 HAS IMPROPER REPAIR. INSTALLED PROPER REPAIR PER AVITAS ENGINEERING NR 95PMSI.049 RO-1. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009051996032200905NM 1996 3 22 96ZZZX1302 119950309A2820 FUEL VENT LINE BOEING727 72722C 138400FNM WS 629/601 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FUEL VENT LINE AT WS 629 AND WS 601, CHECK THAT REPAIR IS IN C/W E.O. REPAIR. BLENDED OUT PER SRM 51-40-1. MATERIAL LOOSE .002 INCH. INSTALLED REPAIR PER AVITAS ENGINEERING NR 95PMSI.049RO-0 IN BOTH LOCATIONS. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009061996032200906NM 1996 3 22 96ZZZX1303 119950309A5754 SKIN BOEING727 72722C 138400FNM NR 2 SLAT GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING C-CHECK, NR 4 RIB FROM INBD END OF STAT NR 2 LEADING EDGE IS GOUGED. TRIMMED OUT DAMAGED AREA PER SRM 51-10-1. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009071996032200907NM 1996 3 22 96ZZZX1304 119950309A5711 SPAR BOEING727 72722C 138400FNM BS 870 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH5388153881 19191 DURING D-CHECK, WING, CENTER SECTION, INTERNAL REAR SPAR WEB BLR 24 BULGING, POP RIVET HEADS, CORROSION STA 870. CUT OUT DAMAGED WEB PER SRM 57-10-6. INSTALLED NEW STIFFENER PER SRM 51-10-1, PARAGRAPH 4. INSTALLED WEB REPAIR PER SRM 57-10-6. FILLER 3 INCH BY 10 INCH .063 INCH 2024T3 DOUBLER 2024T3 10 INCH BY 14 INCH BY .200 INCH. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009081996032200908NM 1996 3 22 96ZZZX1305 119950309A5754 SKIN BOEING727 72722C 138400FNM NR 2 SLAT CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, NR 10 RIB FROM OUTBOARD END OF SLAT NR 2 LEADING EDGE IS CRACKED AT LOWER FWD CORNER. INSTALLED TYPICAL RIB REPAIR PER SRM 57-50-3. REPLACED FASTENERS PER SRM 51-30-3. TAT: 53,882.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009091996032200909NM 1996 3 22 96ZZZX1306 119950309A5320 VERTICAL SUPPORT BOEING727 72722C 138400FNM BS 920 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, STA 920, LT VERTICAL SUPPORT AT STR 15 IS CRACKED AT FASTENER LOCATION. STOP-DRILLED CRACK PER SRM 51-10-01. FABRICATED DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER PER SRM 51-40-21, 5 INCH BY 2 INCH, 2024T3.071. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009101996032200910NM 1996 3 22 96ZZZX1307 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM FS 850 BROKEN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, CABIN, SEAT TRACK BROKEN AT FS 850, RBL 45. CUT OUT BROKEN SECTION OF SEAT TRACK. MADE REPAIR PER SRM 53-10-5, PAGE 4A. DRILLED HOLES, ALODINED AND PRIMED. INSTALLED REPAIR PER SRM 53-10-5, PAGES 4A AND 4B. TAT: 53,881.4 HRS. TAC: 36,380 2L73 4F A3WE 19960322009111996032200911NM 1996 3 22 96ZZZX1308 119950309A5321 PANELS BOEING727 72722C 138400FNM BS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, CABIN, FWD OF BS 1183 RT, LT OF FLOOR LEVEL FLOTATION PANELS ARE CRACKED. ROUTED OUT CRACK AREAS PER SRM 51-40-2. FABRICATED DOUBLER 2024T3.025, 6 INCH BY 72 INCH, AND INSTALLED PER SRM 51-40-2, AND SRM 51-30-2. SEALED WITH PRC PER SRM 51-20-4. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009121996032200912NM 1996 3 22 96ZZZX1309 119950309A5320 CHANNEL BOEING727 72722C 138400FNM FS 850-870 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, CABIN, FLOOR SUPPORT CHANNEL, FS 850-FS 870, RBL 62, HAS CORROSION ON UNDERSIDE OF CHANNEL. REMOVED CORROSION UNDERSIDE OF CHANNEL PER SRM 51-10-6. TREAT AND ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED U-CHANNEL REPAIR 15 INCHES LONG AND MATERIAL 2024-T3.080 PER SRM 51-40-4. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009131996032200913NM 1996 3 22 96ZZZX1310 119950309A5720 VERTICAL SUPPORT BOEING727 72722C 138400FNM FS 106.8 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, LT WING LEADING EDGE FS 106.8 VERTICAL SUPPORT LOWER END IS CRACKED AT FASTENER ATTACH POINT. FAB NEW ANGLE MATERIAL .050 INCH 2024-T3 LENGTH = 17 INCH BY 2 INCH. INSTALLED PER SRM 51-10-1, PAR 4 AND SRM 51-30-2. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009141996032200914NM 1996 3 22 96ZZZX1311 119950309A5311 FRAME BOEING727 72722C 138400FNM FS 500 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING C-CHECK, CABIN FS 500 FRAME CRACKED JUST ABOVE FLOOR LEVEL, 3.8125 INCHES ABOVE FLOOR LEVEL BETWEEN STR 17R - STR 18R. CUT OUT DAMAGED AREA PER SRM 51-40-3. FABRICATED DOUBLER 7075-T6.063 BY 10.50 INCH BY 4.50 BY 1 INCH PER SRM 51-40-3, AND INSTALLED IT AT FS 500 3.8125 INCHES ABOVE FLOOR LEVEL BETWEEN STR 17R AND STR 18R PER SRM 51-40-3 AND SRM 51-30-2. TAT: 53,881.4 HRS. TAC: 36.380. 2L73 4F A3WE 19960322009151996032200915NM 1996 3 22 96ZZZX1312 119950309A5330 SKIN BOEING727 72722C 138400FNM BS 400-420 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FUSELAGE SKIN AT STR 4L FROM STA 400 TO STA 420 IS DAMAGED. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER 2024-T3.050 13 INCH BY 9 INCH PER SRM 53-30-3, FIGURE 14, PRC EDGES PER SRM 51-20-4. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009161996032200916NM 1996 3 22 96ZZZX1313 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 360 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FUSELAGE EXTERIOR, EVIDENCE OF CORROSION AT FS 360 AT LAP SEAM STR 10R. REMOVED FASTENERS PER SRM 51-30-2, CLEANED CORROSION PER SRM 51-10-6, ALODINE AND PRIMED PER SRM 51-10-2, AND REINSTALLED FASTENERS PER SRM 51-30-2. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009171996032200917NM 1996 3 22 96ZZZX1314 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 650 GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FUSELAGE EXTERIOR, RT GALLEY SERVICE DOOR EXTERIOR SKIN CORRODED AND GOUGED JUST FORWARD OF DOOR WINDOW AT FS 650. INSTALLED EXTERNAL REPAIR PER SRM 52-00-3, FIGURE 3. TAT: 53,881.4. TAC: 36,380. 2L73 4F A3WE 19960322009181996032200918NM 1996 3 22 96ZZZX1315 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 700/740 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, CORROSION ON FLOOR BEAM SEAT TRACK NR 7 APPROXIMATELY RBL 60 BETWEEN BS 700 AND BS 740, BOTTOM SIDE. CORROSION BEYOND LIMITS, REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK PER SRM 53-10-5 AND SRM 51-10-1, 44 INCHES LONG. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009191996032200919NM 1996 3 22 96ZZZX1316 119950309A5350 FAIRING BOEING727 72722C 138400FNM NR 3329 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FAIRING NR 3329 HAS A 2 INCH CRACK IN THE END RADIUS. STOP DRILLED AT ENDS OF CRACK. ROUNDED OUT CRACK. FABRICATED DOUBLER 2024-T3.040, 4 INCH BY 4 INCH. INSTALLED DOUBLER PER SRM 51-10-1, 51-10-2 AND 51-40-3. TAT: 53,881.4 HRS. TAC: 36,380. 2L73 4F A3WE 19960322009201996032200920NM 1996 3 22 96ZZZX1317 119950309A5320 ANGLE BOEING727 72722C 138400FNM FS 1343 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, INSIDE VERTICAL FIN THROUGH ACCESS PANEL 9504, CORROSION ON HORIZONTAL LEG OF HORIZONTAL L-ANGLE (CHORD) APPROXIMATELY FS 1343, LEFT SIDE. INSTALLED REPAIR S/S 301 1/2 HARD ANGLE PER SRM 51-40-4 AND 51-30-2, 6 INCH BY 10 INCH, .125 INCH. TAT: 53,881.4 HRS. TAC 36,380. 2L73 4F A3WE 19960322009311996032200931NM 1996 3 22 AWXA9500835 119951230A5512657378337 SKIN BOEING737 73733A 1384673NM LT HORIZ STAB DENTED A AWXAK NONE O OTHER ININSP/MAINT 1 WP28509DC 23636 PHX/SNA - FLT 0661 - DENT FOUND IN LT HORIZONTAL STABILIZER 8 FEET INBOARD OF TIP. PERFORMED INTERIM REPAIR PER SRM 55-10-01. (X) 2L72 4F RTA16WE 19960322009541996032200954NM 1996 3 22 95UAL900356 119951227A5220 LATCH MECH BOEING737 737222 1384473NM PWA JT8 JT8D7B 52053NE EMER EXIT OUT OF ADJUST A UALAK NONE O OTHER CRCRUISE 1 WP299062U 19943 HANDLE AT DOOR 2 LEFT KEEPS MOVING TOWARD THE OPEN POSITION IN-FLIGHT. SUPPLEMENTAL DATA UPDATE: CHECKED LATCH TORQUE TUBES FOR PROPER ADJUSTMENT PER MM. DOOR CHECKS O.K. 2L72 4F4 F A16WE E2EA 19960327000011996032700001NE 1996 3 27 UF6A951016 219951025A732060750032155 TRIM SWITCH BAG ATP ATP EU PWA PW120 PW126A NE RT ENGINE STUCK A UF6ACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 GL31851AW7607 2020 124241 SBN - FLT NR 5102 - WHEN ADVANCING POWER LEVER FOR TAKEOFF THE NR 2 ENGNE CONTROL ILLUMINATED. MAINTENANCE FOUND ENGINE TRIM SWITCH STUCK IN, FREED SWITCH AND OPS CHECK GOOD. (M) 2L72 4T4 TRTA27NM E2ONE 19960329000011996032900001WP 1996 3 29 9522249610 119951027A5753 SKIN DOUG DC9 DC932 3022066WP TE FLAP CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING TRAILING EDGE FLAP OUTBOARD AFT LOWER SPAR CAP STA 335. REPAIRED CAP (P/N 5912125-1) PER EA 12-5750-9-C0618. 2L72 4F A6WE 19960329000021996032900002WP 1996 3 29 9522259610 119951226A5720 DOUBLER DOUG DC9 DC932 3022066WP LT WING CORRODED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01610NW 47432 DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING LANDING GEAR SUPPORT UPPER DOUBLER. REPAIRED DOUBLER (P/N 5912438) PER EA 12-5730-9-C0654. 2L72 4F A6WE 19960329000751996032900075WP 1996 3 29 ABXA9600360 119951227A5320561494351 WEB DOUG DC8 DC863 302198AWP BS 834-857 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED CORROSION ON STATION 857 AT LOWER SPAR CAP RIGHT WHEEL WELL FORWARD BULKHEAD AND BL 0 ATTACH ANGLE CORRODED UNDER KEEL WEB. REPAIRED WEB AND TEE AT BL 0, STATION 834 TO 857 THAT WERE CORRODED IAW ABX REA D853-12674MR. 2L74 4F 4A25 19960329000761996032900076WP 1996 3 29 ABXA9600361 119951227A5315 FLOOR BEAM DOUG DC8 DC863 302198AWP BS 1320 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED CABIN FLOOR PANEL SUPPORT FRAME CRACKED AND DENTED AT STATION 1320, 30 RIGHT FROM CENTERLINE ABOVE LONGERON 29R AFT CARGO PIT. REPAIRED FUSELAGE STATION 1320 FLOOR BEAM AT RBL 30 THAT WAS CRACKED IAW ABX REA D853-12676MR. 2L74 4F 4A25 19960329000771996032900077WP 1996 3 29 ABXA9600362 119951227A5311 FRAME DOUG DC8 DC863 302198AWP BS 1260 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED FRAME CRACKED AT STATION 1260 BETWEEN LONGERON 4 RIGHT AND LONGERON 5 RIGHT. REPAIRED FRAME AT FUSELAGE STATION 1260, LONGERON 4 RIGHT AND LONGERON 5 RIGHT IAW ABX REA D853-12675MR. 2L74 4F 4A25 19960329000781996032900078WP 1996 3 29 ABXA9600363 119951227A5330 SKIN DOUG DC8 DC863 302198AWP BS 1440-1460 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED SKIN CORRODED ON INNER SURFACE BETWEEN LONGERON 31 RIGHT AND 29 RIGHT AT STATION 1440 TO 1460. REPAIRED UPPER FUSELAGE SKIN AT C-4 DOOR THAT WAS CORRODED ON INNER SURFACE IAW ABX REA D853-12672MR. 2L74 4F 4A25 19960329000791996032900079WP 1996 3 29 ABXA9600364 119951227A53205597646321 DOOR JAMB DOUG DC8 DC863 302198AWP BS 70-80 MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING MODIFICATION, DISCOVERED L-1 DOOR JAM AFT TORQUE BOX COVER HAS TORN HOLES, DOUBLE DRILLED HOLES AND HOLES IN RADIUS. REPAIRED FORWARD ENTRANCE DOOR JAMB STRUCTURE AT FUSELAGE STATION 70 TO 80 IAW ABX REA D853-12671MR. 2L74 4F 4A25 19960329000801996032900080WP 1996 3 29 ABXA9600365 119951227A53203773077510 SUPPORT DOUG DC8 DC863 302198AWP BS 140 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING MODIFICATION, DISCOVERED FLOOR BEAM AT VERTICAL SUPPORT FRAME AT FUSELAGE STATION 140, LONGERON 27R WAS CORRODED AT SEVERAL LOCATIONS. REPAIRED FLOOR BEAM SUPPORT AT FUSELAGE STATION 140 IAW ABX REA D853-12609MR. 2L74 4F 4A25 19960329003911996032900391WP 1996 3 29 ABXA9600354 119951003A78305958782503 TR DRIVE LINK DOUG DC9 DC931 3022065WP NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23947AX 47004 DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND A CRACK INDICATION ON THE NR 2 ENGINE UPPER OUTBOARD THRUST REVERSER DRIVER LINK. REMOVED LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK. 2L72 4F A6WE 19960329003921996032900392WP 1996 3 29 ABXA9600355 119950220A78305958782503 TR DRIVE LINK PWA 591029415 DOUG DC9 DC933F 302207AWP NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23931AX2058 AZ78100 47384 DURING COMPLIANCE OF AD 75-14-06, AD 90-18-03; SB'S 78-36, 78-38, 78-40 AND 78-66, FOUND THE NR 2 THRUST REVERSER OUTBOARD UPPER DRIVER LINK HAD A CRACK INDICATION. REPLACED THE NR 2 THRUST REVERSER OUTBOARD UPPER DRIVER LINK IAW DC-9 MM 78-31-5. LINK CRACKED, SCRAPPED LINK. 2L72 4F A6WE 19960329003951996032900395NE 1996 3 29 ABXA9600358 219950618A7240 DRAIN BOSS DOUG DC9 DC941 302207NWP PWA JT8 JT8D15 52051NE NR 1 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23966AX 47510 686296 DURING COMPLIANCE OF AD 87-11-07; PRATT AND WHITNEY ASB 5676, FOUND THE NR 1 ENGINE AFT DRAIN BOSS HAD A CRACK INDICATION. REPLACED THE NR 1 ENGINE IAW ABX J7001 CARD. REPAIRED ENGINE IAW PRATT AND WHITNEY OVERHAUL MANUAL AND ABX GMM, CHAPTER 4. 2L72 4F4 F A6WE E2EA 19960329003961996032900396WP 1996 3 29 ABXA9600373 119951219A532059197073 JAMB DOUG DC9 DC931 3022065WP FS 889-945 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT LOWER CARGO DOOR JAMB HAD A PREVIOUS REPAIR THAT WAS NOT IAW THE DC-9 SRM. REPAIRED THE AFT LOWER CARGO DOOR JAMB IAW ABX REA D953-13587-MR. 2L72 4F A6WE 19960329003991996032900399WP 1996 3 29 ABXA9600376 119951228A53159911544505 FLOOR BEAM DOUG DC9 DC931 3022065WP FS 313 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR BEAM AT FS 313 CORRODED AND BLENDED BEYOND LIMITS. REPAIRED FLOOR BEAM IAW ABX REA D953-13766-MR. 2L72 4F A6WE 19960329004001996032900400WP 1996 3 29 ABXA9600377 119951206A531239164101 BLKHD FITTING DOUG DC9 DC931 3022065WP FS 699 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND CORROSION ON THE UPSTANDING LEG OF THE SLANT PRESSURE PANEL FITTING AT FS 699. REPAIRED SLANT PRESSURE PANEL FITTING IAW ABX REA D953-13779-MR. 2L72 4F A6WE 19960329004011996032900401WP 1996 3 29 ABXA9600378 119951226A5320995821429 FRAME DOUG DC9 DC931 3022065WP FS 897-935 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE AFT LOWER CARGO DOOR JAMB PAN THAT WAS NOT IAW THE DC-9 SRM. REPAIRED AFT LOWER CARGO DOOR JAMB PAN IAW ABX REA D953-13785-MR. 2L72 4F A6WE 19960329004021996032900402WP 1996 3 29 ABXA9600379 119951226A5320995791739 DOOR JAMB DOUG DC9 DC931 3022065WP FS 897-935 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE AFT LOWER CARGO DOOR JAMB PAN THAT WAS NOT IAW THE DC-9 SRM. REPAIRED IAW ABX REA D953-13785-MR. 2L72 4F A6WE 19960329004051996032900405WP 1996 3 29 ABXA9600382 119951229A53305911409503 SKIN DOUG DC9 DC931 3022065WP FS 229 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FORWARD FUSELAGE SKIN PANEL CREASED, DENTED AND GOUGED AT FS 229 AND LONGERON 19L. REPAIRED LEFT FORWARD FUSELAGE SKIN PANEL IAW ABX REA D953-13827-MR. 2L72 4F A6WE 19960329004061996032900406WP 1996 3 29 ABXA9600383 119951228A53305911408125 SKIN DOUG DC9 DC931 3022065WP FS 250-319 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE FORWARD UPPER FUSELAGE SKIN AT LONGERON 1 FROM FS 250.0 TO 319.0 THAT WAS NOT PER THE DC-9 SRM. REPAIRED FUSELAGE SKIN IAW ABX REA D953-13828-MR. 2L72 4F A6WE 19960329004081996032900408WP 1996 3 29 ABXA9600385 119951226A57209919369501 T-CAP DOUG DC9 DC931 3022065WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-18-03 AND SB 57-98 ON THE LEFT WING, FOUND CORROSION INSIDE BARREL NUT HOLE NR 14 AT THE MAIN FRAME T-CAP AT STA XCW 58.5. REPAIRED LEFT WING T-CAP IAW ABX REA D957-13835-MR. 2L72 4F A6WE 19960329004111996032900411WP 1996 3 29 ABXA9600388 119951229A55125922578512 SKIN DOUG DC9 DC931 3022065WP LT HORIZ STAB DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL THAT WAS NOT IAW THE DC-9 SRM. REPAIRED LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL IAW ABX REA D955-13859-MR. 2L72 4F A6WE 19960329004131996032900413WP 1996 3 29 ABXA9600390 119951227A5312591142717 BLKHD TEE DOUG DC9 DC931 3022065WP FS 996 REQD TRIM A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THAT WHEN REPLACING THE AFT PRESSURE BULKHEAD LOWER TEE, THERE WAS A REQUIREMENT TO TRIM 1.0 INCH FROM THE TEE SECTION VERTICAL LEG. REPAIRED THE AFT PRESSURE BULKHEAD LOWER TEE IAW ABX REA D953-13901-MR. 2L72 4F A6WE 19960329004281996032900428WP 1996 3 29 ABXA9600405 119951226A57209919369501 T-CAP DOUG DC9 DC931 3022065WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-18-03; SB 57-98 OF THE LEFT WING MAIN FRAME T-CAP, FOUND NUMEROUS CORRODED FASTENERS, GOUGES AND CORROSION ON THE T-CAP BETWEEN AND UNDER STRINGERS 11 THROUGH 15, 16 TO 17, 19 TO 20, 20 TO 21 AND 21 TO 22. CLEANED AND TREATED CORROSION AND REPLACED FASTENERS IAW SB 57-98. CORROSION IN STRINGER NR 14 REPAIRED PER ABX REA D957-13835-MR. COMPLIED WITH ULTRASONIC INSPECTION PER SB 57-98. NO WING SKIN THINNING NOTED. 2L72 4F A6WE 19960329004291996032900429WP 1996 3 29 ABXA9600406 119951122A57209919369502 T-CAP DOUG DC9 DC931 3022065WP WS 58.5 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-18-03; SB 57-98 OF THE RIGHT WING MAIN FRAME T-CAP, FOUND NUMEROUS CORRODED FASTENERS, GOUGES AND CORROSION ON THE T-CAP BETWEEN STRINGERS 11 THROUGH 19 AND 21 TO 22. CLEANED AND TREATED CORROSION ON THE T-CAP IAW SB 57-98 AND DC-9 SRM 51-30-5. COMPLIED WITH ULTRASONIC INSPECTION OF WING PLANKS PER SB 57-98. NO CORROSION THINNING OF WING SKIN NOTED. 2L72 4F A6WE 19960329004321996032900432WP 1996 3 29 ABXA9600409 119951123A53119919617502 FRAME DOUG DC9 DC931 3022065WP FS 699 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05; SB 53-131 VISUAL INSPECTION OF THE LEFT AND RIGHT FUSELAGE FRAMES, FOUND THE FRAME AT FS 699R CRACKED. REPLACED FRAME AT FS 699 IAW SB 53-131 AND DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5. 2L72 4F A6WE 19960329004351996032900435WP 1996 3 29 ABXA9600412 119951220A532049568771 ANGLE DOUG DC9 DC931 3022065WP FS 69 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM ATTACH ANGLE AT FS 69L CRACKED. REPLACED THE ATTACH ANGLE AT FS 69 IAW DC-9 SRM CHAPTER 51-30-5. 2L72 4F A6WE 19960329004361996032900436WP 1996 3 29 ABXA9600413 119951202A574338134352 HINGE DOUG DC9 DC931 3022065WP WS 91 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR DOOR WING MOUNTED HINGE WORN. REPLACED HINGE HALF IAW SB 32-244 AND DC-9 SRM CHAPTER 51-30-5. 2L72 4F A6WE 19960329004371996032900437WP 1996 3 29 ABXA9600414 119951218A52803923159505 DOOR LINK DOUG DC9 DC931 3022065WP WS 91 WORN A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR LINK AND CLEVIS WORN. REBUSHED CLEVIS AND REPLACED LINK ARM, BASE AND ALL HARDWARE IAW SB 32-244 AND DC-9 OVERHAUL MANUAL 32-10-6. 2L72 4F A6WE 19960329004381996032900438WP 1996 3 29 ABXA9600415 119951218A52805910557136 DOOR DOUG DC9 DC931 3022065WP RT MLG DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR ARTICULATING DOOR PREVIOUSLY REPAIRED AND FILLER COMING OUT. REPLACED ARTICULATING DOOR IAW DC-9 OVERHAUL MANUAL 32-10-6 AND SB 32-244. 2L72 4F A6WE 19960329004391996032900439WP 1996 3 29 ABXA9600416 119951122A5280591055725 SEAL DOUG DC9 DC931 3022065WP LT MLG DOOR CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 91-22-07; ASB 32-244, FOUND THE LEFT MAIN LANDING GEAR DOOR TRAILING EDGE SEAL CRACKED. REPLACED SEAL IAW DC-9 SRM CHAPTER 51-30-2. 2L72 4F A6WE 19960329004401996032900440WP 1996 3 29 ABXA9600417 119951208A57305912737502 TE PANEL DOUG DC9 DC931 3022065WP WS 353-445 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING TRAILING EDGE PANEL DELAMINATED AND CORRODED FROM XRS 353 TO XRS 445. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2L72 4F A6WE 19960329004411996032900441WP 1996 3 29 ABXA9600418 119951207A573059127352 TE PANEL DOUG DC9 DC931 3022065WP WS 445-509 DELAMINATED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23936AX 47269 DURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING TRAILING EDGE PANEL DELAMINATED AND CORRODED BETWEEN XRS 445 AND 509. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2L72 4F A6WE 19960329004831996032900483EU 1996 3 29 96ZZZM361 119951004A5755 BOLT BAG BAE146BAE146200A 1500266EU RT SPOILER DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 RIGHT WING INNER LIFT SPOILER FORWARD JACK BOLT HAS DAMAGED THREADS. INSTALLED NEW BOLT. 2H74 4F RTA49EU 19960329004841996032900484EU 1996 3 29 96ZZZM362 119951016A5755 BOLT BAG BAE146BAE146200A 1500266EU RT SPOILER CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 AFT JACK BOLT FOR RIGHT MID LIFT SPOILER CRACKED UNDER HEAD. REMOVED AND REPLACED AFT JACK BOLT FOR RIGHT MID LIFT SPOILER. 2H74 4F RTA49EU 19960329004851996032900485EU 1996 3 29 96ZZZM363 119951015A5753 BUSHINGS BAG BAE146BAE146200A 1500266EU NR 3 TE FLAP DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 PIN ASSY FLAP UPPER CARRIAGE TO LEVER FOUND BUSHING WITH PLATING LOSS SCRAPED. SSI NR 57-55-129, NR 3 RIGHT FLAP. REMOVED AND REPLACED FLAP UPPER CARRIAGE TO LEVER BUSHING, NR 3 RIGHT FLAP. 2H74 4F RTA49EU 19960329004861996032900486 1996 3 29 96ZZZM364 419951101A2565D3100201 SLIDE BAG BAE146BAE146200A 1500266EU NR 3 FAILED CHECK A A6WAK NONE O OTHER ININSP/MAINT 1 GL31606AW74620 0123 E2033 THE NR 3 EMERGENCY SLIDE FAILED THE POWER PACK EFFICIENCY CHECK. REPLACED THE SLIDE. 2H74 4F RTA49EU 19960329004871996032900487 1996 3 29 96ZZZM365 419951031A2565625601102 SLIDE BAG BAE146BAE146300A 1500267EU CABIN DAMAGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31612AW 6121 E3122 DEPLOYED THE LEFT FORWARD ESCAPE SLIDE S/N 0548, PER MM 25-60-11 PAGE 501 APRA 1A, 1C, AND ZW CHECK LIST 25-60-36-06. THEN REMOVED THE SLIDE FOR A DETAILED VISUAL INSPECTION, FORWARDED THE CHECK LIST WITH THE SLIDE TO THE SHOP. UPDATE TASK P/N 625601102, S/N 612-1. DEPLOYED SLIDE, VISUALLY INSPECTED AND UNCOVERED A SMALL HOLE IN SLIDE AFTER DEPLOYMENT. SLIDE DEPLOYED NORMALLY AND INFLATED WELL ABOVE PRESSURE MINIMUMS. INSTALLED SLIDE. 2H74 4F RTA49EU 19960329004881996032900488EU 1996 3 29 96ZZZM366 119951030A5350 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 SKIN AROUND FRONT CARGO DOOR, FORWARD LOWER SECTION ABOUT 13 INCHES UP FROM CORNER, HAS A .016 INCH DEEP GOUGE APPROXIMATELY .25 INCH BY .375 INCH IN SIZE WITH METAL ROLLED UP AT BOTTOM. BLENDED REPAIRED AREA AT FORWARD CARGO BAY AS DESCRIBED ABOVE IAW AVRO FAX DJH/RJ1304-95. PERFORMED ET ON THE ABOVE BLENDED AREA AND FOUND TO BE CRACK FREE NOW 10/20/95. REPRO WITH ALOCROM 1200. FOLLOWED BY EPOXIDE PRIME. 2H74 4F RTA49EU 19960329004891996032900489EU 1996 3 29 96ZZZM367 119951030A5320 STIFFENERS BAG BAE146BAE146200A 1500266EU FRAME NR 29 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 DURING STEP 3 INSPECTION FOR CRACKS AT STIFFENERS ON FRAME 29, REF EO E95/003/653, 3 CRACKED STIFFENERS WERE DISCOVERED, 25.94 RIGHT, AND 25.94 LEFT AND 31.13 LEFT. REPAIRED CRACKS IAW EO NR E95/005/653 ORIG PER NOTE NR 1 OF REPAIR DRAWING AW-53-20-9506-06, ET CUT AWAY FLANGE OF STIFFENERS COMPLIED WITH, NO CRACKS. 2H74 4F RTA49EU 19960329004901996032900490EU 1996 3 29 96ZZZM368 119951021A5330 SKIN BAG BAE146BAE146200A 1500266EU FUSELAGE GOUGED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 SKIN AROUND REAR CARGO BAY DOOR FORWARD LOWER SECTION ABOUT 10 INCHES UP FROM CORNER HAS A .013 INCH DEEP GOUGE APPROXIMATELY .125 INCH BY .5 INCH INSIDE WITH METAL ROLLED UP AT BOTTOM OF GOUGE MARKED WITH PINK MARKER. BLEND REPAIRED AREA AFT CARGO BAY AS DESCRIBED ABOVE IAW AVRO FAX DJH/RJ1304-95. PERFORMED ET ON ABOVE AREA. FOUND CRACK FREE 10/20/95. 2H74 4F RTA49EU 19960329004911996032900491EU 1996 3 29 96ZZZM369 119951021A5320 ANGLE BAG BAE146BAE146200A 1500266EU FRAME NR 35 CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 FREIGHT ANGLE FOR FRAME 35 (LOWER) CENTER AREA CRACKED. REPLACED FREIGHT ANGLE. 2H74 4F RTA49EU 19960329004951996032900495NM 1996 3 29 96ZZZM373 119951205A3350 BATTERY CHARGER BOEING727 727227 1384078NM CABIN INOPERATIVE A AMTAK NONE L NO TEST TXTAXI/GRND HDL 1 GL11768AT 21996 FORWARD EVAC SLIDE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUTATION SLIDE EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK GOOD IAW MM CH 33-50-51. (M) 2L73 4F A3WE 19960329004961996032900496NM 1996 3 29 96ZZZM374 119951221A3350 CONNECTOR BOEING727 727227 1384078NM CABIN SHORTED A AMTAK NONE L NO TEST TXTAXI/GRND HDL 1 GL11772AT 22003 EMERGENCY EXIT PATH LIGHTING (FLOOR LIGHTS LAST 6 LIGHTS OF STRINGER) ARE INOP (AFT 6) FROM AFT EXIT BACK 5 RED, 1 WHITE. FOUND BAD WIRE CONNECTOR FOR LIGHTS STRIP AT ROW 31C SECURED CONNECTOR, OPS CHECK NORMAL. (M) 2L73 4F A3WE 19960329004971996032900497NM 1996 3 29 96ZZZM375 119951201A3350 BATTERY PACK BOEING727 727227 1384078NM CABIN DISCHARGED A AMTAK NONE L NO TEST TXTAXI/GRND HDL 1 GL11772AT 22003 FIVE RED EGRESS LIGHTS AT AFT EXIT DOOR INOPERATIVE. REMOVED AND REPLACED EGRESS LIGHT BATTERY PACK PER MM 33-50-01, OPS CHECK GOOD. (M) 2L73 4F A3WE 19960329005031996032900503CE 1996 3 29 96ZZZM381 119951219A30201189100383 ICE VANE BEECH 1900 1900D 1154162CE RT ENG COWL CRACKED A AMWAO OTHER O OTHER ININSP/MAINT 1 CE07178YV314 UE178 DURING ROUTINE MAINTENANCE, THE RIGHT FIXED ICE VALVE WAS FOUND TO TO HAVE SEVERAL CRACKS. 2L72 4T RTA24CE 19960329005041996032900504NM 1996 3 29 96ZZZM382 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 211.8 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FUSELAGE EXTERIOR SKIN DENTED BELOW LOWER FORWARD CORNER OF L2 WINDOW CUTOUT AT FS 211.8 BETWEEN STRINGER 12L AND STRINGER 13L APPROXIMATELY. REMOVED FASTENERS, FABRICATED AND INSTALLED 11 INCHES BY 9 INCHES .050 DOUBLER PER SRM 53-30-3 FIG 1. 2L73 4F A3WE 19960329005051996032900505NM 1996 3 29 96ZZZM383 119950309A5320 INTERCOSTAL BOEING727 72722C 138400FNM BS 227.8 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND NOSE COMPARTMENT AT BS 227.8 BL 0 HAD CORROSION AT INTERCOSTAL LOWER FLANGE. INSTALLED NEW INTERCOSTAL AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960329005061996032900506NM 1996 3 29 96ZZZM384 119950309A5320 INTERCOSTAL BOEING727 72722C 138400FNM BS 211.8-219.8 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND NOSE COMPARTMENT BETWEEN BS 211.8-219.8 APPROXIMATELY BLR 20-35 CORROSION AT INTERCOSTAL FRAME. CORROSION BEYOND LIMITS, REMOVED INTERCOSTAL FRAME AS PER SRM 51-30-2. FABRICATED NEW FRAME AS PER SRM 51-40-3 AND INSTALLED AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960329005071996032900507NM 1996 3 29 96ZZZM385 119950309A5320 INTERCOSTAL BOEING727 72722C 138400FNM BS 211.8-219.8 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND FORWARD NOSE COMPARTMENT BETWEEN BS 211.8-219.8 APPROXIMATELY BLL 30, CORROSION AT INTERCOSTAL AND AT FRAME. REMOVED DAMAGED AREA PER SRM 51-30-2. FABRICATED AND INSTALLED NEW PART AS PER SRM 51-40-3. 2L73 4F A3WE 19960329005081996032900508NM 1996 3 29 96ZZZM386 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 385 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND TOP SKIN IS CRACKED AT ONE FASTENER HOLE AT FS 385 STRINGER 4R. CUT OUT DAMAGE AREA PER SRM 53-30-3 FIG 4 AND INSTALLED DOUBLER 9 INCHES BY 8 INCHES 2024-T3 .050 PER SRM 53-30-3 FIG 4. 2L73 4F A3WE 19960329005091996032900509NM 1996 3 29 96ZZZM387 119950309A5311 FRAME BOEING727 72722C 138400FNM BS 520/540 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, FOUND FUSELAGE FRAMES DENTED AT INNER ANGLE STATION 520 AND STATION 540 JUST ABOVE STRINGER 6R. CUT OUT DENTED AREA AT STRINGER 520 AND STRINGER 540. FOUND OUT OF LIMITS. REPAIRED AS PER SRM 53-10-4. TWO REPAIRS 12 INCHES BY 3 INCHES 7075-T6 .071. 2L73 4F A3WE 19960329005101996032900510NM 1996 3 29 96ZZZM388 119950309A5230 SKIN BOEING727 72722C 138400FNM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURNG D-CHECK, FOUND AFT CARGO COMPARTMENT DOOR EXTERIOR SKIN 2 EACH SMALL CRACKS AT LOWER AND FORWARD EDGE CORNER. CUT OUT DAMAGE AREA AND INSTALLED DOUBLER 2024-T3 .063 14 INCHES BY 12.5 INCHES AS PER SRM 52-20-2. SEALED EDGE WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329005111996032900511NM 1996 3 29 96ZZZM389 119950309A5720 ANGLE BOEING727 72722C 138400FNM WS 130.7 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND LOWER SUPPORT ANGLE CRACKED IN TWO PLACES FORWARD OF LOWER SPAR LE SPAR LE STATION 130.7. REMOVED FASTENERS PER SRM 51-30-2. REMOVED DAMAGED AREA AT SUPPORT ANGLE PER SRM 51-40-2. FABRICATED NEW SECTION OF SUPPORT ANGLE 17 INCH BY 1 INCH 2024-T3 .050. FABRICATED SPLICE .063 2024-T3 8 INCHES BY 1 INCH BY 1 INCH PER SRM 51-40-3. TREATED AND PRIMED PER SRM 51-10-2. (M) 2L73 4F A3WE 19960329005121996032900512NM 1996 3 29 96ZZZM390 119950309A5720 ANGLE BOEING727 72722C 138400FNM FSS 106.8 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, VERTICAL LEADING EDGE SUPPORT ANGLE, SECOND FROM AFT END IS CRACKED AT LOWER FASTENER FSS 106.8 SEEN THROUGH ACCESS PANEL 6402. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .050 PER SRM 51-40-3. ALODINED AND PRIMED, DOUBLER 4 INCH BY 3 INCH PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 51-10-3. 2L73 4F A3WE 19960329005131996032900513NM 1996 3 29 96ZZZM391 119950309A5711 SPAR WEB BOEING727 72722C 138400FNM FS 106.8 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND VERTICAL WEB ATTACHED TO FRONT SPAR FSS 106.8 CRACKED AT 3 PLACES, SEEN THROUGH ACCESS PANEL 6402. RENIVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACKS PER SRM 51-10-1. INSTALLED WEB REPAIR PER SRM 51-10-1. INSTALLED WEB REPAIR PER SRM 51-40-2. (M) 2L73 4F A3WE 19960329005141996032900514NM 1996 3 29 96ZZZM392 119950309A5321 FLOOR BOEING727 72722C 138400FNM AFT LAV CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, MANY SPOTS OF HEAVY CORROSION ON SUB FLOOR AROUND RIGHT AFT LAV DRAIN FITTING. CUT OUT CORRODED AREA, CLEANED AREA, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED DOUBLER 2024-T3 .063 29 INCHES BY 13.5 INCHES AND INSTALLED PER SRM 51-40-2. REPLACED SEAT TRACK 36 INCHES PER SRM 51-10-1 PAR 4, SEALED WITH PRC PER SRM 51-20-4. (M) 2L73 4F A3WE 19960329005151996032900515NM 1996 3 29 96ZZZM393 119950309A5730 SKIN BOEING727 72722C 138400FNM WING CTR SECTIONCORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND WING CENTER SECTION LOWER SKIN HAS EXTERIOR CORROSION BULGE/CRACK AT RT EDGE BOLTS BL 70 INCHES R AT 38 INCHES AFT OF FRONT SPAR. REMOVED CORROSION AS PER SRM 51-10-6. ULTRASONIC INSPECTED TO DETERMINE MATERIAL REMOVED. HFEC INSPECTION FASTERNER HOLES, NO CRACKS NOTED. COLD WORKED HOLES AND INSTALLED DOUBLER PER BOEING DRAWING 65C36586 DIM 16 INCHES BY 7 INCHES 2024-T3 .125. 2L73 4F A3WE 19960329005161996032900516NM 1996 3 29 96ZZZM394 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 1025-1035 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1025 TO STATION 1035. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4 (WIDTH 3.25 INCH) AND SRM 51-30-2. 2L73 4F A3WE 19960329005171996032900517NM 1996 3 29 96ZZZM395 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 1045-1055 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1045 TO STATION 1055. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4, (WIDTH 3.25 INCH) AND SRM 51-30-2. (M) 2L73 4F A3WE 19960329005181996032900518NM 1996 3 29 96ZZZM396 119950309A5230 SUPPORT ANGLE BOEING727 72722C 138400FNM FWD CARGO DR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND SUPPORT ANGLE CRACKED INSIDE FORWARD CARGO DOOR AT FORWARD EDGE BY THIRD STOP FITTING FROM BOTTOM. REMOVED SUPPORT ANGLE, FABRICATED SUPPORT ANGLE. INSTALLED SUPPORT ANGLE PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2. 2L73 4F A3WE 19960329005191996032900519NM 1996 3 29 96ZZZM397 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 1131-1135 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 2 STATION 1131 TO 1135. REMOVED FASTENER PER SRM 51-30-2 AND REMOVED CORROSION PER SRM 51-10-6 MAT LOSS .003. ALODINED AND PRIMED AS PER SRM 51-10-2. 2L73 4F A3WE 19960329005201996032900520NM 1996 3 29 96ZZZM398 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 950 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH 19191 DURING D-CHECK, FOUND CORROSION SEAT TRACK NR 1 STATION 950. TWO FASTENERS REMOVED PER SRM 51-30-2. FOUND CORROSION OUT OF LIMITS PER SRM 51-10-6. REPLACEMENT OF SEAT TRACT SECTION 107 AND INSTALLED FASTENERS AS PER SRM 51-10-1 AND 51-30-2. 2L73 4F A3WE 19960329005211996032900521NM 1996 3 29 96ZZZM399 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 660-740 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND CORROSION NR 1 CABIN SEAT TRACK STATION 700. REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM STATION 660-740. 2L73 4F A3WE 19960329005221996032900522NM 1996 3 29 96ZZZM400 119950309A5321 FLOOR BOEING727 72722C 138400FNM BS 1110-1183 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND CORROSION ON CABIN FLOOR STATION 1110 TO 1183 ROW 4. REMOVED CORROSION PER SRM 51-10-6. CUT OUT CORROSION PER SRM 51-10-2. INSTALLED DOUBLER .040 12 INCH BY 5 INCH AND FILLER PER SRM 51-40-1. 2L73 4F A3WE 19960329005231996032900523NM 1996 3 29 96ZZZM401 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 1030 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND CORROSION CABIN SEAT TRACK NR 7 STATION 1030. FABRICATED NEW SEAT TRACK FS 870-1070. INSTALLED TRACK PER SRM 51-10-1 PAR 4 WIDTH 3.25 INCH AND SRM 51-30-2. 2L73 4F A3WE 19960329005241996032900524NM 1996 3 29 96ZZZM402 119950309A5347 SEAT TRACK BOEING727 72722C 138400FNM BS 870-950 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND CORROSION ON CABIN FILLER SEAM NR 7 STATION 870 TO STATION 950 SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK FS 870-1070 WIDTH 3.25 INCH, INSTALLED PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. 2L73 4F A3WE 19960329005251996032900525NM 1996 3 29 96ZZZM403 119950309A5330 SKIN BOEING727 72722C 138400FNM BS 1343-1353 MISSING FASTENERA DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND EXT FUSELAGE BETWEEN BS 1343-1353 BETWEEN STRINGER 8R-13R MISSING FASTENER, LOOSE FASTENERS, RUST ON WASHERS/FASTENERS, BUCKLED SKIN. FABRICATED AND INSTALLED DOUBLER AS PER SRM 54-30-3 15 INCHES BY 10 INCHES 2024-T3 .063 AND INSTALLED PER SRM 51-30-2. 2L73 4F A3WE 19960329005261996032900526NM 1996 3 29 96ZZZM404 119950309A5330 SKIN BOEING727 72722C 138400FNM BS 1233 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND EXT FUSELAGE, APPROXIMATELY BS 1233 JUST UNDER LAP SEAT 20R, DENTED. FOUND OUT OF LIMITS PER SRM 53-30-1 PAGE 1 PAR B. REMOVE DAMAGED AREA AND FABRICATED FILLER FROM 2024-T3 .050 14.5 INCHES BY 6.5 INCHES AND DOUBLER FROM 2024-T3 .063 12.5 INCHES BY 10.5 INCHES PER SRM 53-30-3. ALODINED AND PRIMED REPAIR PARTS AND AREA PER SRM 51-10-2. 2L73 4F A3WE 19960329005271996032900527NM 1996 3 29 96ZZZM405 119950309A5230 CARGO DOOR BOEING727 72722C 138400FNM BS 500 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND MCD, BOTTOM OF DOOR INBOARD STRUCTURE JUST BELOW STATION 500 RIB, HAS CRACK INDICATION. REMOVED RIB AND ALUMINUM BLOCK. FABRICATED NEW ALUMINUM BLOCK 7075-T6 .250 3.5 INCHES BY 5.5 INCHES AND INSTALLED. REPLACED SEAL RETAINER 1 INCH BY 12 INCH 2024-T3 .032 AS PER SRM 51-10-1 PAR 4 AND 51-30-2. 2L73 4F A3WE 19960329005281996032900528NM 1996 3 29 96ZZZM406 119950309A5230 CARGO DOOR BOEING727 72722C 138400FNM BS 600 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND MCD, BOTTOM OF DOOR INBOARD STRUCTURE JUST BELOW STATION 600, RIB HAS CRACK INDICATION. REMOVED AND REPLACED ALUMINUM SUPPORT BLOCK 7075-T6 .250 5.5 INCH BY 3.5 INCH AS PER SRM 51-10-1 PAR 4 AND 51-30-2. 2L73 4F A3WE 19960329005291996032900529NM 1996 3 29 96ZZZM407 119950309A5320 WEB BOEING727 72722C 138400FNM STA 940/950 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND APPROXIMATELY 3 INCH CRACK IN WEB BETWEEN RIGHT 940 AND 950 FITTINGS AT STRINGER 180 IN R/W/W. REMOVED EXISTING WEB AND TWO ANGLES PER S/B 727-53-140. ALODINED AND PRIMED AREA PER SRM 51-10-2. REPLACED WITH NEW 'T' CHORD PER S/B 727-53-140. 2L73 4F A3WE 19960329005301996032900530NM 1996 3 29 96ZZZM408 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 267/282 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND ON FUSELAGE EXTERIOR, FOUR RUSTED FASTENERS AND FUSELAGE SKIN DENTED BETWEEN FS 267 AND FS 282 APPROXIMATELY AT STRINGER 23L. REMOVED DAMAGED AREA PER SRM 53-30-3. FABRICATED DOUBLER 10 INCHES BY 8 INCHES 2024-T3 .063 PER SRM 53-30-3 AND INSTALLED DOUBLER PER SRM 53-30-3. 2L73 4F A3WE 19960329005311996032900531NM 1996 3 29 96ZZZM409 119950309A5320 ANGLE BOEING727 72722C 138400FNM FS 312 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND FUSELAGE EXTERIOR EVIDENCE OF CORROSION AT AFT SIDE OF EXTERNAL DOUBLER AND TWO BLIND FASTENERS AT FS 312 APPROXIATELY BETWEEN STRINGER 26R AND STRINGER 27R. REMOVED DOUBLER, CORROSION FOUND ON NOSE CHORD ANGLE. REPLACED DOUBLER AS PER SRM 53-30-3 FIG 1. MATERIAL .021 INCH SIZE 10 INCHES BY 24 INCHES 2024-T3. 2L73 4F A3WE 19960329005321996032900532NM 1996 3 29 96ZZZM410 119950309A5330 SKIN BOEING727 72722C 138400FNM FS 188 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND ON FUSELAGE EXTERIOR, FUSELAGE SKIN AND EXTERNAL DOUBLER DENTED AT FS 188 APPROXIMATELY AT STRINGER 26R AREA. REMOVED OLD DOUBLER PER SRM 51-30-2. CUT OUT DAMAGE AREA PER SRM 53-30-3. INSTALLED DOUBLER 14.5 INCHES BY 17 INCHES 2024-T3 .50 AND FILLER PER SRM 53-30-3. 2L73 4F A3WE 19960329005331996032900533NM 1996 3 29 96ZZZM411 119950309A5330 SKIN BOEING727 72722C 138400FNM BS 880 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND ON RT W/W, CORROSION ON LOWER SURFACE OF RT W/W PRESSURE DECK AT FS 880 RBL 12 AND 20. REMOVED FLAP CTL VALVE, REMOVED FASTENERS, REMOVED CORROSION, STOP DRILLED CRACK, INSTALLED DOUBLER .080 2024-T3 21 INCHES BY 12 INCHES AND REINSTALLED FLAP CTL VALVE IAW B727 MM 27-51-51 AND SRM 51-30-2, 51-10-6 AND SB 727-53-149 DWG 65-89360. 2L73 4F A3WE 19960329005341996032900534NM 1996 3 29 96ZZZM412 119950309A5312 BLKHD SKIN BOEING727 72722C 138400FNM BS 870 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, FOUND ON RT W/W, CORROSION AT BULKHEAD 870 RBL 4 FORWARD OF APU CUT OUT. REMOVED OLD REPAIR, CLEANED AREA AND INSTALLED NEW DOUBLER 2024-T3 .050 2 INCHES BY 4 INCHES AS PER SRM 51-40-2. (M) 2L73 4F A3WE 19960329005351996032900535NM 1996 3 29 96ZZZM413 119950906A5400 'S' DUCT BOEING727 72730C 1384009NM BS 1332 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT STATION 1332 TO 1342 RIB 35 AT 6 O'CLOCK (BOTTOM) SKIN BULGED AND CRACKED. REMOVED CORROSION AS PER SRM 51-10-6 AND CUT DAMAGED SECTIONS 4 INCHES BY 5 INCHES AND 1 INCH BY 1 INCH TREATED AND PAINTED PER SRM 51-10-2, FABRICATED NEW DOUBLERS 9 INCHES BY 3.75 INCHES .50, 5 INCH BY 2.75 INCHES .05 AND 1.5 INCH BY .75 .50 PER SRM 51-40-2. INSTALLED DOUBLERS AND FILLERS AS PER SRM 51-40-2. 2L73 4F A3WE 19960329005361996032900536NM 1996 3 29 96ZZZM414 119950906A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 890/920 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND SEAT TRACK CORRODED RBL 62 AT STATION 890 AND STATION 920. REMOVED SECTION OF SEAT TRACK FROM STATION 870 TO STATION 970 RBL 62. INSTALLED NEW TRACK MADE OF BACK 1520 1430 - TMS 60 5030 FROM STATION 870-970. 2L73 4F A3WE 19960329005371996032900537NM 1996 3 29 96ZZZM415 119950906A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 760 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND STATION 760 RBL 65 FRAME AND SUPPORT ANGLE IS CORRODED LOCATED JUST BELOW FLOOR LEVEL. REMOVED AND REPLACED SUPPORT ANGLE STATION 760 RBL 65 7075 T-6 .100 1 INCH BY 1 INCH BY 3.5 INCH AS PER SRM 51-10-1. 2L73 4F A3WE 19960329005381996032900538NM 1996 3 29 96ZZZM416 119950906A5312 BLKHD BEAM BOEING727 72730C 1384009NM FS 1183 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND CABIN FS 1183 RBL 37 BULKHEAD VERTICAL BEAM HAS CRACK INDICATION AFT INBOARD FLANGE IN RADIUS 29 INCHES ABOVE FLOOR LEVEL. STOP DRILLED CRACK PER SB 727-53-0192. HFEC INSPECTED STOP DRILL HOLES AND NO FURTHER CRACK PROGRESSION NOTED IAW PART G51-00-00. INSTALLED REPAIR PER SB 727-53-0192 AND SEALED PER SRM 51-20-4. 2L73 4F A3WE 19960329005391996032900539NM 1996 3 29 96ZZZM417 119950906A5312 BLKHD BEAM BOEING727 72730C 1384009NM BS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH 19793 DURING C-CHECK, FOUND CABIN STATION 1183 BULKHEAD VERTICAL BEAM HAS 4 INCH LONG CRACK COMING FROM FLOOR AT LBL 37. DRILLED .25 IN DIAMETER STOP HOLE AT CRACK END PER SRM 51-10-1 REF S/B 727-53A-0173. INSTALLED REPAIR PER SB 727-53-0173 AND BOEING DRAWING 65C31492. 2L73 4F A3WE 19960329005401996032900540NM 1996 3 29 96ZZZM418 119950906A5522 SKIN BOEING727 72730C 1384009NM RT ELEVATOR PUNCTURED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND RIGHT ELEVATOR BOTTOM SKIN HAS 1.5 INCH BY .5 INCH HOLE AFT OF NR 4 BALANCE BAY. REMOVED SMALL ACCESS PANEL IAW SRM 51-30-2. ROUNDED OUT HOLE IAW SRM 51-10-1. MADE DOUBLER 2024 T-3 0.032 3.5 INCH BY 2.5 INCH LOT 750761 PO 9319067 PER SRM 51-20-3. INSTALLED DOUBLER PER SRM 55-20-2. INSTALLED ACCESS PANEL IAW SRM 51-30-2. 2L73 4F A3WE 19960329005411996032900541NM 1996 3 29 96ZZZM419 119950906A5330 SKIN BOEING727 72730C 1384009NM BS 178 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FUSELAGE STATION 178 SKIN DOUBLER BETWEEN WINDSHIELD CENTER POST RADOME DAMAGED AND PULLED LOOSE AT FWD END. REMOVED DAMAGE AREA ON FUS STATION 178 SKIN DOUBLER BETWEEN WINDSHIELD CENTER POST AND RADOME. FABRICATED FILLER 1.5 INCH BY 10 INCH 2024 T-3 .63 PER SRM 53-30-3. FABRICATED DOUBLER 4 INCH BY 10 INCH 2024 T-3 .063 AS PER SRM 53-30-3. INSTALLED DOUBLER AND FILLER PER SRM 53-30-1. SEALED PER SRM 51-20-4. 2L73 4F A3WE 19960329005421996032900542NM 1996 3 29 96ZZZM420 119950906A5312 BLKHD BEAM BOEING727 72730C 1384009NM FS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND CABIN FS 1183 LBL 27 VERTICAL BEAM HAS APPROXIMATELY 10 INCH CRACK STARTING APPROXIMATELY 48 INCHES ABOVE FLOOR LEVEL. STOPPED DRILL .25 DIAMETER HOLES STATION 1183 LBL 27 IAW REF SRM 51-10-1 AND S/B 727-53-0182. NDT CHECKED STOP DRILLED HOLES OK. INSTALLED BOEING REPAIR KIT 65L33556-1 AS PER SB 727-53-0182 AND DRAWING NR 65C33556. 2L73 4F A3WE 19960329005431996032900543NM 1996 3 29 96ZZZM421 119950906A5230 SKIN BOEING727 72730C 1384009NM CARGO DOOR CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND AFT CARGO DOOR SKIN CRACKED BS 1070 STRINGER 22R. REMOVED AFT CARGO DOOR. CUT OUT CRACKED AREA AS PER SRM 52-00-3 FIG 3 5.25 INCH BY 4 INCH. FABRICATED EXTERNAL DOUBLER 2024 T-3 .063 10.25 INCH BY 11.75 INCH PO 766422. INSTALLED DOUBLER PER SRM 51-40-2. 2L73 4F A3WE 19960329005441996032900544NM 1996 3 29 96ZZZM422 119950906A5230 SKIN BOEING727 72730C 1384009NM CARGO DOOR DENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND LARGE DENT ON AFT CARGO DOOR SKIN BS 1090 STRINGER 22R. STRAIGHTEND OUT DENT PER SRM 51-40-1. CUT OUT DAMAGED AREA 3 INCH BY 4 INCH PER SRM 52-00-3 PAGE 6. FABRICATED DOUBLER 2024 T-3 .063 11 INCH BY 9 INCH PER SRM 52-00-3. INSTALLED DOUBLER PER SRM 52-00-3 FIG 3 AT AFT CARGO DOOR BS 1090 STRINGER 22R. INSTALLED FASTENERS PER SRM 51-30-2. 2L73 4F A3WE 19960329005451996032900545NM 1996 3 29 96ZZZM423 119950906A5330 SKIN BOEING727 72730C 1384009NM BS 312 CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED STATION 312 STRINGER 23L. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF STRINGER 23L AT FS 312 AS PER SRM 53-10-3. FABRICATED DOUBLER AS PER SRM 53-10-3. FABRICATED DOUBLER AS PER SRM 53-30-3 2024-T-3 15 INCH BY 10 INCH LOT NR 766422. INSTALLED REPAIR PART (DOUBLER) PER SRM 53-10-3. INSTALLED FASTENERS PER SRM 51-30-2. (M) 2L73 4F A3WE 19960329005461996032900546NM 1996 3 29 96ZZZM424 119950906A5313 STRINGER BOEING727 72730C 1384009NM FS 312 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FORWARD E/E COMPARTMENT, STRINGER 22L IS CRACKED IN TWO PLACES JUST AFT OF FUSELAGE FRAME AT FS 312. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF STRINGER 22L AT FS 312 AS PER SRM 53-10-3 16 INCHES APPROXIMATELY. FABRICATED STRINGER 22L 7075 T-6 24 INCHES LARGE PER SRM 53-10-3. INSTALLED STRINGER REPAIR ON STATION 312 STRINGER 22L AS PER SRM 53-10-3 STATION 304 TO 320. 2L73 4F A3WE 19960329005471996032900547NM 1996 3 29 96ZZZM425 119950906A5311 FRAME BOEING727 72730C 1384009NM FS 870 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FS 870 RIGHT FRAME HAS CRACK INDICATION AT ROW 2 BETWEEN 3RD AND 4TH FASTENERS FROM TOP VERIFIED BY EDDY CURRENT AND UT. REMOVED FORWARD SPLICE ANGLE PER SRM 51-30-2. ACCOMPLISHED HFEC AS PER PART G NDT MANUAL 51-00-00 FIG 4. ACCOMPLISHED HFEC OF HOLES COMMON TO FITTING, AND NO CRACKS NOTED. INSTALLED REPAIR PER SB 727-53-0194, MATERIAL 2024 T-3 .125 15.5 INCH BY 20 INCH LOT NR 672-773 PO 9318078. 2L73 4F A3WE 19960329005481996032900548NM 1996 3 29 96ZZZM426 119950906A5330 SKIN BOEING727 72730C 1384009NM FS 760 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND CABIN FS 760 RIGHT SIDE BETWEEN WING CENTER TANK AND FLOOR LEVEL RBL 67, HEAVY CORROSION ON FRAME AND PRESS PAN WEB. REMOVED OUTSIDE FAIRING FOR S/M ACCESS AND REMOVED FASTENERS PER SRM 51-30-2. REMOVED CORROSION ON FRAME PER SRM 51-10-6 MATERIAL LOSS .005. REMOVED PRESS PAN WEB FOUND CORROSION OUT OF LIMITS. ALODINE AND PRIMED PER SRM 51-10-2. FABRICATED AND INSTALLED NEW PRESS PAN WEB 2024 T-3 .040 2 INCH BY 8 INCH PER SRM 51-10-1. INSTALLED PRESS BOX PER SRM 51-30-2. 2L73 4F A3WE 19960329005491996032900549NM 1996 3 29 96ZZZM427 119950906A5311 FRAME BOEING727 72730C 1384009NM BS 304 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FRAME CORROSION ON FORWARD SIDE AT PREVIOUS REPAIR, STATION 304 STRINGER 21-22 LEFT. REMOVED FASTENERS AND OLD REPAIR PER SRM 51-30-2. CUT OUT DAMAGE AREA PER SRM 51-40-4 3 INCHES BY 4 INCHES. CLEANED ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER REPAIR 2024 T3 .080 AND .063 16 INCHES BY 5 INCHES PO NR 766422-44611 AS PER SRM 51-40-4. 2L73 4F A3WE 19960329005501996032900550NM 1996 3 29 96ZZZM428 119950906A5313 STRINGER BOEING727 72730C 1384009NM BS 740 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH 19793 DURING C-CHECK, FOUND FUSELAGE BULGE STATION 740 STRINGER 25L AND CLIP HAVE CORROSION. CLIP WAS REMOVED AND CUT OUT DAMAGED AREA OF STRINGER 25L BS 740 7 INCHES APPROXIMATELY AS PER SRM 53-10-3. REPLACED CLIP PER SRM 51-10-1 PAGE 4. INSTALLED STRINGER REPAIR AS PER SRM 53-10-3 FIG 1 ABOUT 12 INCHES LONG. MATERIAL USED BAC 1498-145 LOT NR 464951. 2L73 4F A3WE 19960329005511996032900551NM 1996 3 29 96ZZZM429 119950906A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 540/560/580 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH 19793 DURING C-CHECK, FOUND FORWARD PIT BULGE RIGHT SEAT TRACK CRACKED AT RADIUS CUT OUTS AT STATION 540, 560, AND 580. REMOVED SECTION OF TRACK PER SRM 51-30-2. CUT OUT DAMAGED AREA OF SEAT TRACK STATION 520 TO STATION 600 AS PER SRM 53-10-5. INSTALLED SEAT TRACK STATION 520 TO STATION 600 AS PER SRM 53-10-5. DRILL SPLICE FOR FLOOR PANELS. DRILL HOLES FOR PANELS IAW SRM 53-10-5. DRILLED SPLICES .250 7075 T-6 15 INCHES BY 1 INCH THREE EACH. 2L73 4F A3WE 19960329005521996032900552NM 1996 3 29 96ZZZM430 119950906A5320 FITTING BOEING727 72730C 1384009NM BS 940 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH 19793 DURING C-CHECK, FOUND BS 940 FITTING LEFT SIDE CRACK AT REPAIR BETWEEN TWO FASTENERS FWD SIDE UNDER CABIN FLOOR PANEL (VISUAL PER SB 727-53-190 INSP). REMOVED FAST FOR ACCESS FOR HFEC PER SRM 51-30-2. ACCOMPLISHED HFEC INSPECTION OF SUSPECTED CRACK AREA, FOUND CRACK RUNNING FROM LOWER FASTENER HOLES UP TO MORE FASTENERS, CRACK STOPPED AT HOLE. FABRICATED AND INSTALLED REPAIR ANGLE PER BOEING REPAIR SKETCH DHL-MIA-95-0016TR ANGLE 5 INCHES BY 1.5 INCH BY 1.5 INCH BY .100 15-5 STEEL ANGLE 4 INCH BY 4 INCH BY 4 INCH BY 1 INCH .250 STEEL 15-5 STEEL. 2L73 4F A3WE 19960329005531996032900553NM 1996 3 29 96ZZZM431 119950906A5330 SKIN BOEING727 72730C 1384009NM BS 1223 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FUSELAGE SKIN CRACKED AT TAIL SKID CUTOUT STATION 1223. STOP DRILL PER SRM 51-10-1. ZYGLO CHECKED END OF CRACK, FOUND ADDITIONAL CRACK EMMINATING FROM HOLE. CUT OUT AREA DAMAGED PER SRM 51-10-1. FABRICATED DOUBLER AND INSTALLED DOUBLER. MATERIAL USED 2024 T-3 .050 8 INCH BY 5 INCH AS PER SRM 51-40-1. 2L73 4F A3WE 19960329005541996032900554NM 1996 3 29 96ZZZM432 119950906A5330 SKIN BOEING727 72730C 1384009NM BS 141 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND FUSELAGE SKIN BULGED BETWEEN STRINGER 25L AND 26L STATION 141. LFEC INSPECTED C/W PER NDT MANUAL 51-00-00 PART 6 FIG 5 MORE THAN 10 PERCENT NOTED. REMOVED FASTENERS AROUND DAMAGED AREA IAW SRM 51-30-2. CUT OUT DAMAGED AREA 4 INCH BY 4 INCH IAW SRM 51-10-1. FABRICATED 14 INCH BY 4 INCH FILLER PART 2024 T-3 .050 PO 9319522 LOT NR 766-541 PER SB 53-0084. FABRICATED 21 INCH BY 6.5 INCH DOUBLER REPAIR 2024 T-3 .063 PER SB 53-0034. INSTALLED DOUBLER REPAIR PER SRM 53-0034. 2L73 4F A3WE 19960329005551996032900555NM 1996 3 29 96ZZZM433 119950906A5330 SKIN BOEING727 72730C 1384009NM FS 178 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND MSI 702-0119-1002 DENT AT STATION 178 RIGHT SIDE FORWARD OF WINDOW POST E-F. REWORKED DENT ON STATION 178 RIGHT SIDE FORWARD WINDOW POST, FOUND OUT OF LIMITS AS PER SRM 51-40-1. FABRICATED DOUBLER AS PER SRM 53-30-3 10 INCHES BY 13 INCHES .050 2024-T3 LOT NR 495092. INSTALLED DOUBLER AS PER SRM 53-30-3 AT STATION 178 RT SIDE FWD OF WINDOW POST E-F. 2L73 4F A3WE 19960329005561996032900556NM 1996 3 29 96ZZZM434 119950906A5754 SKIN BOEING727 72730C 1384009NM RT LE SLAT DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH44571 19793 DURING C-CHECK, FOUND MSI 702-0125-1003, DENT AT RW SLAT STATION 193.5. CUT OUT DENTED (DAMAGED) AREA. INSTALLED FLUSH REPAIR PER SRM 57-50-3 FIG 1 (REPAIR II). INSTALLED DOUBLER .080 2024-0 4.5 INCH BY 7.25 INCH FILLER .063 2024-T3 2.75 INCH BY 5 INCH. FASTENERS AND PRC INSTALLED PER SRM 57-50-3. 2L73 4F A3WE 19960329005571996032900557NM 1996 3 29 96ZZZM435 119950906A5730 SKIN BOEING727 72730C 1384009NM LT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01702DH 19793 DURING C-CHECK, FOUND LEFT WING UPPER SURFACE, NR 3 SPOILER NR 3 HINGE CUTOUT IS CRACKED. REMOVED NR 3 SPOILER PANEL. STOP DRILLED AS PER SRM 51-10-1. FABRICATED 2024 PLUS 3 .050 4 INCH BY 4 INCH DOUBLER AS PER SRM 57-30-4. INSTALLED FASTENERS ON UPPER SURFACE CUT OUT HINGE REPAIR AS PER SRM 51-30-2 AND 57-30-4. INSTALLED NR 3 SPOILER IAW MM CHAP 27-51-1. 2L73 4F A3WE 19960329005581996032900558NM 1996 3 29 96ZZZM436 119950808A5320 AIRSTAIR WALL BOEING727 72730C 1384009NM BS 1300 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH 19010 DURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1300 AIR STAIR LEFT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .040 5 INCH BY 3 INCH. TREATED AND PRIMED PER SRM 51-10-2. 2L73 4F A3WE 19960329005591996032900559NM 1996 3 29 96ZZZM437 119950808A5320 AIRSTAIR WALL BOEING727 72730C 1384009NM BS 1300 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH 19010 DURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1300 AIR STAIR LEFT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .040 5 INCH BY 3 INCH. TREATED AND PRIMED PER SRM 51-10-2. 2L73 4F A3WE 19960329005601996032900560NM 1996 3 29 96ZZZM438 119950808A5320 AIRSTAIR WALL BOEING727 72730C 1384009NM BS 1305 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND LIGHTNING HOLE EDGE CRACKED AT BS 1305 AIR STAIR RIGHT SIDE WALL. STOP DRILLED CRACK. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALL REPAIR PER SRM 51-40-2 2024-T3 .040 8 INCH BY 4 INCH. TREATED AND PRIMED PER SRM 51-10-2. 2L73 4F A3WE 19960329005611996032900561NM 1996 3 29 96ZZZM439 119950808A5313 STRINGER BOEING727 72730C 1384009NM BS 1210 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND STRINGER CORRODED SECOND STRINGER BELOW VERTICAL FIN FRONT SPAR FORGING IN STAIRWELL STATION 1210. VERT FIN STRINGER 2 LEFT. REMOVED CORROSION FROM SECOND STRINGER BELOW VERTICAL FIN STATION 1210 PER SRM 51-10-2. MATERIAL LOSS .010, CORROSION BEYOND LIMITS. INSTALLED TYPICAL ANGLE REPAIR PER SRM 51-40-4. ALODINE AND PRIME PER SRM 51-10-2. FABRICATED REPAIR PER SRM 55-30-4. INSTALLED DOUBLER REPAIR PER SRM 55-30-4 MATERIAL 7075-T6 .0631 1.25 INCH BY 1 INCH BY 7 INCH. 2L73 4F A3WE 19960329005621996032900562NM 1996 3 29 96ZZZM440 119950808A5730 SKIN BOEING727 72730C 1384009NM WING LE DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH 19010 DURING C-CHECK, FOUND THE OVERWING LEADING EDGE CUTOUT FOR THE NR 2 SLAT OUTBOARD TRACK DENTED. ROUTED OUT DAMAGED SKIN PER SRM 51-10-1. FABRICATED DOUBLER .063, 2024-T3, 7 INCH BY 4 INCH PER SRM 57-30-4. INSTALLED REPAIR DOUBLER PER SRM 57-30-4. INSTALLED HOOK SEAL PREVIOUSLY REMOVED (TO FACILITATE REPAIR) PER SRM 51-10-1. 2L73 4F A3WE 19960329005631996032900563NM 1996 3 29 96ZZZM441 119950808A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 850-870 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FLOOR PANEL SUPPORT CORRODED STATION 850-870 RBL 64. REPLACEMENT OF SUPPORT ANGLE AT STATION 850 TO 870 RBL 64 AS PER SRM 51-10-1 PAR 4. INSTALLATION AS PER SRM 51-30-2. 2L73 4F A3WE 19960329005641996032900564NM 1996 3 29 96ZZZM442 119950808A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM FS 330-344 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FORWARD LAV FLOOR SUPPORT CORRODED FS 330 TO 344 RBL 51. REMOVED CORROSION PER SRM 51-10-6, MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED ANGLE 2024-T3 .080 FILLER .080 PER SRM 51-40-3. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR ANGLE AND FILLER AT FWD LAV FLOOR SUPPORT FS 330 TO 344 RBL 51 PER SRM 51-40-1 AND FASTENER HL18 5-3 PNAS 1097 5-4 PER SRM 51-30-2. 2L73 4F A3WE 19960329005651996032900565NM 1996 3 29 96ZZZM443 119950808A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM FS 414 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FORWARD LAV FLOOR SUPPORT CORRODED ON TOP AND BOTTOM FS 314 RBL 13 TO 42. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED FWD LAV FLOOR SUPPORT FS 314 RBL 13 TO 42 WITH NAS 5176-3 AN960D10 PER SRM 51-10-1 AND SRM 51-30-2. FLOOR SUPPORT FIMALCO 130158-4-1A 7075-T6 BAC 1505-100617. 2L73 4F A3WE 19960329005661996032900566NM 1996 3 29 96ZZZM444 119950808A5320 SUPPORT BOEING727 72730C 1384009NM FS 344 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FORWARD LAV LIGHT CORROSION ON AFT WALL SUPPORT FS 344 RBL 25 TO 55. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS .005 FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED DOUBLER 5 INCH BY 1 INCH 7075-T6 .080 SHIM 4 INCH BY 1 INCH 7075-T6 .050 PER SRM 51-40-3. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER AND SKIN AT FWD LAV AFT WALL PER SRM 51-40-3. 2L73 4F A3WE 19960329005671996032900567NM 1996 3 29 96ZZZM445 119950808A5347 SEAT TRACK BOEING727 72730C 1384009NM FS 380-390 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND CENTER SEAT TRACK CORRODED, GOUGED AND BROKEN OUT FS 380-390. REMOVED SEAT TRACK AS PER SRM 51-30-2. INSTALLED NEW SECTION PER SRM 53-10-5. TREATED AND PRIMED PER SRM 51-10-2. REINSTALLED FLOOR PANELS PER SRM 51-30-2. 2L73 4F A3WE 19960329005681996032900568NM 1996 3 29 96ZZZM446 119950808A5510 FITTING BOEING727 72730C 1384009NM HORIZ STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND HORIZONTAL STABILIZER FRONT SPAR RIGHT UPPER OUTBOARD FITTING INDICATES CRACK AT LUG HOLE. REMOVED BUSHING AT RIGHT UPPER OUTBOARD LUG. ACCOMPLISHED HFEC INSPECTION OF LUG HOLE, CRACK NOTED AT 7 O'CLOCK POSITION. REAMED LUG TO .8125 INCH AS PER SB 727-53-A69. ACCOMPLISHED HFEC INSPECTION OF LUG HOLE, NO CRACKS NOTED THIS TIME. REAMED LUG HOLE TO .875 INCH FOR ADDITIONAL CLEARANCE AS PER SB 727-55-A0069. INSTALLED BUSHING AT RIGHT UPPER AS PER SB 727-55-A69. 2L73 4F A3WE 19960329005691996032900569NM 1996 3 29 96ZZZM447 119950808A5531 SPAR WEB BOEING727 72730C 1384009NM VERT STAB CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND VERTICAL STABILIZER FORWARD SPAR WEB HAS CRACK AT EXISTING REP OUTBOARD SIDE OF FWD TERMINAL FITTING LEFT AT TOP OUTBOARD LEFT SIDE CABLE PULLEY CASTING UNDER PNL 9707. TWO CRACKS FOUND UPPER CRACK ROUTED OUT PER SRM 51-10-1, LOWER CRACK TERMINATES AT EXISTING HOLE. MFG REPAIR PER SRM 51-40-2. INSTALLED WEB REPAIR PER SRM 51-30-2 LOT NR 165573 .040 2024-T3 8.5 INCH BY 5.75 INCH. 2L73 4F A3WE 19960329005701996032900570NM 1996 3 29 96ZZZM448 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 259 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FUSELAGE EXTERIOR GREATER THAN 10 PERCENT LOSS MATERIAL NOTED AT FWD SIDE OF FS 259 IN AREA OF LAP SEAM COMMON TO BUTT SEAM AT STRINGER 19R. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 4 INCH PER SB 727-53-0084. FABRICATED FILLERS AND DOUBLER PER SB 53-0084. FILLER DIM 4 INCH BY 4 INCH AND 6 INCH BY 4.5 INCH. DOUBLER DIM 11 INCH BY 6 INCH MATERIAL USED FOR FILLERS 2024-T3 .050 LOT NR 766-541, FOR DOUBLER 2024-T3 .063 P/O 9319645. INSTALLED REPAIR PER SB 727-53-0084 AND SEALED AREA PER SRM 51-20-4. 2L73 4F A3WE 19960329005711996032900571NM 1996 3 29 96ZZZM449 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 441 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGER 22L AND 26L HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 37 INCH PER S/B 727-53-0084. REMOVED CORROSION PER SRM 51-10-6, FABRICATED .016 37 INCH BY 1.875 FILLER PER SB 53-0084, FABRICATED .050 37 INCH BY 4 INCH FILLER PER SB 53-0084. FABRICATED DOUBLER 2024-T3 .063 44 INCH BY 6.5 INCH PER SB 727-53-0084. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PER SB 727-53-0084. 2L73 4F A3WE 19960329005721996032900572NM 1996 3 29 96ZZZM450 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 441 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGER 17L AND 19L HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4.5 INCH BY 22 INCH PER SB 727-53-0084. REMOVED CORROSION PER SRM 51-10-6. FABRICATED DOUBLER REPAIR PER SB 727-53-0084. MATERIAL USED 2024-T3 .063 P/O 9319 645 LOT MRS 766-422 6 INCH BY 24 INCH APPROXIMATELY 2024-T3 .071 P/O 9319719 LOT 768-651 10 INCH BY 30 INCH APPROXIMATELY INSTALLED REPAIR PER SB 727-53-0084. 2L73 4F A3WE 19960329005731996032900573NM 1996 3 29 96ZZZM451 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 441 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE BUTT SEAM AT FS 441 BETWEEN STRINGER 24R AND 26R HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS FROM SKIN PANEL. REMOVED FASTENERS AND CUT OUT DAMAGED AREA 4 INCH BY 16 INCH PER SB 727-53-0084. REMOVED CORROSION PER SRM 51-10-6 MATERIAL LOSS .002. FABRICATED .016 2024-T3 16 INCH BY 1 INCH .375 INCH FILLER PER SB 53-0084, FABRICATED .050 2024-T6 16 INCH BY 4 INCH FILLER PER SB 53-0084. FABRICATED DOUBLER 2024-T6 .063 24 INCH BY 6 INCH PER SB 727-53-0084. TREATED AND PRIMED PER SRM 51-10-2. 2L73 4F A3WE 19960329005741996032900574NM 1996 3 29 96ZZZM452 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 441 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 BETWEEN STRINGERS 20R AND 23R SKIN PANEL HAS 10 PERCENT TO 15 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA 22.5 INCH BY 4.5 INCH APPROXIMATELY PER SB 727-53-0084. FABRICATED FILLER AND DOUBLER REPAIR PER SB 727-53-0084. REMOVED CORROSION PER SRM 51-10-6. MATERIAL REMOVED .003. TREATED AFFECTED AREA WITH ALODINE AND PRIMER PER SRM 51-10-2. MATERIAL USED ON FILLER 2024-T3 .050 LOT NR 766-541 22.5 INCH BY 4.5 INCH APPROXIMATELY ON DOUBLER 2024-T3 .063 DOUBLER 2024-T3 .063 29 INCH BY 8 INCH PER SB 727-53-0084. INSTALLED REPAIR SRM 53-30-3. 2L73 4F A3WE 19960329005751996032900575NM 1996 3 29 96ZZZM453 119950808A5330 SKIN BOEING727 72730C 1384009NM FS 441 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND ON FUSELAGE EXTERIOR, FORWARD SIDE OF BUTT SEAM AT FS 441 MATERIAL LOSS NOTED BETWEEN 10 PERCENT TO 20 PERCENT BETWEEN STRINGER 14R AND 15R. REMOVED FASTENERS. CUT OUT DAMAGED AREA BETWEEN STRINGER 14 AND 15R 4 INCH BY 11 INCH APPROX PER SB 53-0084. CLEANED ADJACENT AREA ALODINED AND PRIMED PER SRM 51-10-1. FABRICATED PARTS 2024-T3 16 INCH BY 8 INCH APPROX FILLER 2024-T3 4 INCH BY 11 INCH. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED REPAIR AND DOUBLER AS PER SB 727-53-0084. SEALED AFFECTED AREA AS PER SRM 51-20-4. 2L73 4F A3WE 19960329005761996032900576NM 1996 3 29 96ZZZM454 119950808A5711 SPAR WEB BOEING727 72730C 1384009NM WS 870 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND WING CENTER SECTION, AFT LOWER SPAR WEB EXTERIOR HAS CORROSION, STATION 870 LBL 0 TO 14 INCHES (SEVERAL AREAS) BULDGING FROM AROUND FASTENERS. CUT OUT DAMAGE AREA AS PER SRM 51-40-2 25 INCH BY 3 INCH. INSTALLED WEB REPAIR AS PER SRM 51-10-6 LOT NR 165373 DOUBLER 2024-T3 .063 33 INCH BY 10 INCH AND FILLER LOT NR 165573 2024-T3 .040 25 INCH BY 3 INCH. 2L73 4F A3WE 19960329005771996032900577NM 1996 3 29 96ZZZM455 119950808A5320 DOOR FRAME BOEING727 72730C 1384009NM BS 540 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND MCD FRAME CRACKED AT STATION 540 ABOVE WINDOW FRAME MKD PER SSID D6-48040-1 F-3A. INSTALLED TYPICAL ANGLE REPAIR PER SRM 51-40-3. MATERIAL USED 7075-T6. SIZE OF REPAIR 10 INCH BY 4 INCH .050 THICKNESS. 2L73 4F A3WE 19960329005781996032900578NM 1996 3 29 96ZZZM456 119950808A5320 ANGLE BOEING727 72730C 1384009NM FWD ENTRY DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01703DH46863 19010 DURING C-CHECK, FOUND FORWARD ENTRY DOOR CUTOUT AT BOTTOM LATCH ANGLE IS CRACKED AT SEVERAL PLACES. STOP DRILLED CRACK PER SRM 51-10-1. PENETRANT INSPECTED PER OHM 20-20-2. CRACK TERMINATES AT STOP DRILL. INSTALLED REPAIR PER SRM 51-40-2 2024-T3 .050 3 INCH BY 18 INCH. 2L73 4F A3WE 19960329005791996032900579NM 1996 3 29 96ZZZM457 119950516A5311 FRAME BOEING727 72729 1384007NM BS 600 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 600 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19960329005801996032900580NM 1996 3 29 96ZZZM458 119950516A5311 FRAME BOEING727 72729 1384007NM BS 580 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 580 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 6 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19960329005811996032900581NM 1996 3 29 96ZZZM459 119950516A5311 FRAME BOEING727 72729 1384007NM BS 560 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 560 RT SIDE. CUT OUT DAMAGED AREA. INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-4 AND 51-30-2. 2L73 4F A3WE 19960329005821996032900582NM 1996 3 29 96ZZZM460 119950516A5311 FRAME BOEING727 72729 1384007NM BS 540 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT INBOARD ANGLE 4 INCHES ABOVE CABIN FLOOR STATION 540 RT SIDE. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER 7075-T6 .070 6 INCH BY 8 INCH BY 1 INCH AS PER SRM 51-40-3 AND 51-30-2. 2L73 4F A3WE 19960329005831996032900583NM 1996 3 29 96ZZZM461 119950516A5730 SKIN BOEING727 72729 1384007NM LT WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND LEFT WING LEADING EDGE OUTBOARD OF LANDING LIGHT DENTED. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR 7075-T6 .071 AND .063 9 INCH BY 9 INCH. FILLER 2 INCH BY 4 INCH AS PER SRM 57-30-4. SEALED WITH RTV PER SRM 51-20-4. 2L73 4F A3WE 19960329005841996032900584NM 1996 3 29 96ZZZM462 119950516A5321 FLOOR PANEL BOEING727 72729 1384007NM COCKPIT CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND CORROSION ON AND UNDER COCKPIT FLOOR PANEL AT F/E RT SEAT TRACK. REPLACED SEAT TRACK SUPPORT ANGLE AND CORRODED FLOOR PANEL PER SRM 51-10-1 PAR 4 AND SRM 51-30-2. 2L73 4F A3WE 19960329005851996032900585NM 1996 3 29 96ZZZM463 119950516A5320 ANGLE BOEING727 72729 1384007NM PAX DOOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FORWARD EXTERIOR DOOR UNDER THRESHOLD 'U' ANGLE HAS CORROSION SEVERAL PLACES. REMOVED PANEL PER MM 53-20-11. CUT OUT DAMAGED SECTION AND REMOVED CORROSION PER SRM 51-10-6. REMOVED AND REPLACED U-CHANNEL PER SRM 51-10-1 PAGE 4 AND INSTALLED ANGLE REPAIR PER SRM 51-40-3 40 INCH BY 2.5 INCH 2024-T3 .090 INCH. INSTALLED FLOOR PANEL PER MM 20-80-1. 2L73 4F A3WE 19960329005861996032900586NM 1996 3 29 96ZZZM464 119950516A5320 ANGLE BOEING727 72729 1384007NM BS 1273 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, AFT STAIRWELL LOWER RT TORQUE BOX INBOARD CHORD ANGLE CRACKED 6 INCHES IN RADIUS RUNNING AFT FROM UNDER STAIR ACTUATOR BRACKET AT APPROX STA 1273. REPAIRED ANGLE AS PER SRM 51-40-3. RE-ASSEMBLED AFT AIRSTAIR ACTUATOR AND STRUTS IAW MM 52-62-71. 2L73 4F A3WE 19960329005871996032900587NM 1996 3 29 96ZZZM465 119950516A5320 FRAME BOEING727 72729 1384007NM CARGO DOOR BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, AFT LOWER DOUBLER DAMAGED/BENT MCD FRAME OPENING. REPLACED DAMAGED DOUBLER WITH 7075-T6 .063 4 INCH BY 6 INCH AS PER SRM 51-40-2 AND 51-30-2. SEALED WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329005881996032900588NM 1996 3 29 96ZZZM466 119950516A5230 SKIN BOEING727 72729 1384007NM MAIN CARGO DR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND MCD INNER SKIN CRACKED UNDER PRESSURE SEAL AT FWD AND AFT UPPER CORNERS. REMOVED FWD AND AFT CORNERS. INSTALLED NEW CORNER AT FWD AND AFT POSITION AS PER SRM 51-10-1 PAR 4. CLOSED INNER SKIN PER SRM 51-30-2. 2L73 4F A3WE 19960329005891996032900589NM 1996 3 29 96ZZZM467 119950516A5314 KEEL BEAM BOEING727 72729 1384007NM LEFT W/W CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND LEFT W/W KEEL BEAM WEB CRACKED FWD OF APU CUTOUT. CUT OUT DAMAGED AREA AND INSTALLED WEB REPAIR AS PER SRM 51-40-2 .063 7075-T6 4 INCH BY 13 INCH. 2L73 4F A3WE 19960329005901996032900590NM 1996 3 29 96ZZZM468 119950516A5320 ANGLE BOEING727 72729 1384007NM BS 910 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND LEFT MAIN GEAR UPLOCK SUPPORT FITTING SUPPORT ANGLE CRACKED BS 910 BETWEEN STRINGER 18 AND 18R. COMPLIED WITH BOEING SERVICE BULLETIN 727-53-165 INSTALLED FRAME MODIFICATION AT BS 910 AND 913.5 BETWEEN STRINGER 18A AND 18, LEFT MAIN W/W. 2L73 4F A3WE 19960329005911996032900591NM 1996 3 29 96ZZZM469 119950516A5720 BRACKET BOEING727 72729 1384007NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND RT WING NR 7 LEADING EDGE SLAT ACTUATOR INBOARD VERTICAL MOUNT BRACKET CRACKED AT UPPER END. REPLACED MOUNT BRACKET DOUBLER PER SRM 51-40-2 7075-T6 7 INCH BY 3 INCH .100 AND SRM 51-30-2. 2L73 4F A3WE 19960329005921996032900592NM 1996 3 29 96ZZZM470 119950516A5320 FLOOR WEB BOEING727 72729 1384007NM FS 1176.9-1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND AFT CABIN, CURVED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 BULKHEAD CRACKED, JUST FORWARD OF WIRE BUNDLE CONDUIT AT RBL 31. STOP DRILL CURVED FLOOR PER SRM 51-10-1 AND INSTALLED DOUBLER PER SRM 51-40-2, 3 INCH BY 2 INCH 2024-T3 .032. 2L73 4F A3WE 19960329005931996032900593NM 1996 3 29 96ZZZM471 119950916A5320 FLOOR WEB BOEING727 72729 1384007NM FS 1176.9-1183 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND AFT CABIN, CURVED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 BULKHEAD IS CRACKED AROUND LIGHTENING HOLE AT LBL 60. INSTALLED DOUBLER CRACKED FLOOR WEB BETWEEN FS 1176.9 CHORD AND FS 1183 PER SRM 51-40-2, 5 INCHES BY 6 INCHES 2024-T3 .032 INCH. 2L73 4F A3WE 19960329005941996032900594NM 1996 3 29 96ZZZM472 119950516A5320 CHORD BOEING727 72729 1384007NM FS 1176.9 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND AFT CABIN, REINFORCEMENT CHORD IS HEAVILY CORRODED AT FS 1176.9 AT LBL 63 UPPER SIDE OF CHORD. CUT OUT DAMAGED AREA AT LBL 50.5 AND INSTALLED NEW CHORD ANGLE AND SPLICE AS PER 95PMSI067D-1. 2L73 4F A3WE 19960329005951996032900595NM 1996 3 29 96ZZZM473 119950516A5320 BEAM BOEING727 72729 1384007NM BS 1273 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND RIGHT AFT STAIRWELL AREA APPROX .25 INCH CRACK RUNNING FROM UNDER DOUBLER ON UPPER FRAME BEAM OF LOWER RIGHT TORQUE BOX, JUST BELOW ACTUATOR BRACKET AT APPROX STATION 1273. INSTALLED DOUBLER OVER STOP DRILL HOLE. DOUBLER 7075-T6 .063 PER SRM 51-30-3, 4 INCH BY 3 INCH 1422 SEALANT USED ALODINE AND PRIMED PER SRM 51-10-6. 2L73 4F A3WE 19960329005961996032900596NM 1996 3 29 96ZZZM474 119950516A5320 WEB BOEING727 72729 1384007NM BS 1263 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND RIGHT AFT STAIRWELL AREA, VERTICAL WEB OF LOWER TORQUE BOX CRACKED APPROX .75 INCH FROM OUTBOARD TO INBOARD AT STATION 1263. INSTALLED TYPICAL WEB REPAIR AS PER SRM 51-40-2 AT VERTICAL WEB OF LOWER TORQUE BOX STATION 1263. MATERIAL 7075-T6 .063 3 INCH BY 6 INCH. 2L73 4F A3WE 19960329005971996032900597NM 1996 3 29 96ZZZM475 119950516A5320 ANGLE BOEING727 72729 1384007NM BS 870 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND SUPPORT ANGLE FOR KEEL BEAM TO BS 870 WEB CRACKED. REMOVED AND REPLACED SUPPORT ANGLE FOR KEEL BEAM RT SIDE TO BS 870 AS PER SRM 51-10-1 PAR 4 AND 51-30-2. REINSTALLED PANELS PER SRM 51-30-2. 2L73 4F A3WE 19960329005981996032900598NM 1996 3 29 96ZZZM476 119950516A5230 ANGLES BOEING727 72729 1384007NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND MCD FORWARD AND AFT SUPPORT ANGLES CRACKED IN AFT ACT, CUT OUT AREA NEAR HINGE. REMOVED CRACKED ANGLES FWD AND AFT PER SRM 51-30-2. FABRICATED AND INSTALLED NEW ANGLE SUPPORT AT FWD AND AFT POSITION 4 INCH BY 2 INCH BY 1 INCH, 7075-T6 P/N 60358 EXTRUSION PER SRM 51-10-1 PAR 4 AND 51-30-2. 2L73 4F A3WE 19960329005991996032900599NM 1996 3 29 96ZZZM477 119950516A5230 DOOR FRAME BOEING727 72729 1384007NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND MCD SUPPORT ANGLE AND DOOR FRAME CRACKED AT FWD ACTUATOR AREA NEAR HINGE. REMOVED SUPPORT ANGLE AND DOOR FRAME PER SRM 51-30-2. INSTALLED NEW ANGLE PER SRM 51-10-1 PAGE 4 AND FABRICATED AND INSTALLED NEW FRAME SECTION PER SRM 51-40-3. SIZE 4 INCH BY 3 INCH BY 1 INCH 2024-T3 .080 INCH, INSTALLED PER SRM 51-30-2 AND 51-20-4. 2L73 4F A3WE 19960329006001996032900600NM 1996 3 29 96ZZZM478 119950516A5320 ANGLE BOEING727 72729 1384007NM SERVICE DR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FORWARD SERVICE DOOR 'Z' ANGLE UNDER THRESHOLD HAS CORROSION FULL LENGTH. CUT OUT DAMAGED AREA OF 'Z' ANGLE 26 INCHES APPROX, ALODINED AND PRIMED AREA PER SRM 51-10-6. INSTALLED NEW ANGLE 7075-T6 .080 1.25 INCH BY 1 INCH BY 26 INCH PER SRM 51-40-3, SEALED AREA WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329006011996032900601NM 1996 3 29 96ZZZM479 119950916A5230 SKIN BOEING727 72729 1384007NM CARGO DOOR DENTS A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND NR 2 CARGO DOOR EXTERIOR STATION 1070 ABOVE HANDLE HAS DENTS AND GOUGES. CUT OUT DAMAGED 5 INCH BY 7 INCH APPROX, FABRICATED AND INSTALLED DOUBLER 7075-T6 .050 12 INCH BY 15 INCH APPROX AS PER SRM 52-00-3 FIG 3. SEALED EDGE WITH PRC PER SRM 51-20-4, SMOOTH OUT GOUGES PER SRM 51-10-1 MATERIAL LOSS .001. 2L73 4F A3WE 19960329006021996032900602NM 1996 3 29 96ZZZM480 119950516A5330 SKIN BOEING727 72729 1384007NM BS 270 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND SKIN HAS DENT AT APPROX STATION 270 STRINGER 20R ABOVE EXTERIOR POWER DOOR. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER 2024-T3 .050 3 INCH BY 13 INCH, REPAIR FILLER 3 INCH BY 3 INCH 2024-T3 .040 IAW SRM 53-30-3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED WET WITH SEALANT IAW SRM 53-30-3. FAY SEALED IAW SRM 51-20-4. 2L73 4F A3WE 19960329006031996032900603NM 1996 3 29 96ZZZM481 119950516A5330 SKIN BOEING727 72729 1384007NM BS 203.8 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND SKIN DENTED BELOW LAP SEAM STRINGER 18L, STATION 203.8. CUT OUT DAMAGED AREA 3 INCH BY 4 INCH, INSTALLED EXTERNAL DOUBLER 2024-T3 .050 11 INCH BY 11 INCH AS PER SRM 53-30-3, SEALED EDGE WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329006041996032900604NM 1996 3 29 96ZZZM482 119950516A5347 SEAT TRACK BOEING727 72729 1384007NM BS 480/600 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND SEAT TRACK EXTRUSION AT RBL 45.5 CORRODED BETWEEN STATION 480 AND STATION 600. REMOVED DAMAGED SEAT TRACK AND REPLACED SEAT TRACK IAW SRM 51-10-1 PAR 4 AND SRM 51-30-2. 2L73 4F A3WE 19960329006051996032900605NM 1996 3 29 96ZZZM483 119950516A5320 ANGLE BOEING727 72729 1384007NM BS 836-850 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND CABIN FLOOR PANEL SUPPORT ANGLE CORRODED, ATTACHED TO CREASE BEAM WEB BS 836 TO BS 850 RBL 65. CUT OUT DAMAGE AREA PER SRM 51-10-1 AND INSTALLED NEW ANGLE PER SRM 51-10-1 PAGE 4 ON BS 836 AND BS 850 RBL 65 27.5 INCH BY 2 INCH BY 2 INCH 7075-T6 .063. 2L73 4F A3WE 19960329006061996032900606NM 1996 3 29 96ZZZM484 119950516A5330 SKIN BOEING727 72729 1384007NM BS 178 WORN A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND AT STATION 178 TOP SKIN DOUBLER JUST AFT OF RADOME HINGES, DOUBLER L/E IS BENT UP AND WORN THIN AT EDGES ONLY. REPLACED SKIN DOUBLER AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960329006071996032900607NM 1996 3 29 96ZZZM485 119950516A5330 SKIN BOEING727 72729 1384007NM AFT STAIRWELL MISSING A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND SECTION OF FUSELAGE SKIN MISSING APPROX 3 SQUARE INCHES AT AFT AIRSTAIR CUT OUT FWD LEFT CORNER. REMOVED FASTENERS PER SRM 51-30-2, CUT OUT PER SRM 51-10-1, INSTALLED FILLER REPAIR PER SRM 53-30-3 4.5 INCH BY 1.75 INCH 2024-T3 .40 INCH. 2L73 4F A3WE 19960329006081996032900608NM 1996 3 29 96ZZZM486 119950516A5315 FLOOR BEAM BOEING727 72729 1384007NM BS 560 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT STATION 560 BETWEEN RBL 45.5 AND RBL 24.75. REMOVED DAMAGED AREA PER SRM 53-10-8 AND INSTALLED REPAIR PER SRM 53-10-8 FIG 3. ALODINED AND PRIMED AREA PER SRM 52-10-2. SIZE 27 INCH 7075-T6 AND SIZE 27 INCH BY 2 INCH BY 1.25 INCH. 2L73 4F A3WE 19960329006091996032900609NM 1996 3 29 96ZZZM487 119950516A5314 KEEL BEAM BOEING727 72729 1384007NM BS 872 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND RIGHT W/W KEEL BEAM WEB CRACKED TWO PLACES FORWARD OF APU CUTOUT BS 872. CUT OUT DAMAGE AREA AND INSTALLED WEB REPAIR AS PER SRM 51-40-2 .063 7075-T6 3 INCH BY 13 INCH. 2L73 4F A3WE 19960329006101996032900610NM 1996 3 29 96ZZZM488 119950516A5320 DOUBLER BOEING727 72729 1384007NM WINDSHIELD POST CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01712DH45184 19401 DURING C-CHECK, FOUND CRACK INDICATION ON WINDSHIELD CENTER POST, OUTSIDE DOUBLER ON LOWER END. COMPLIED WITH BOEING SERVICE BULLETIN NR 727-53-160 AND REPLACED SKIN PANEL. 2L73 4F A3WE 19960329006381996032900638WP 1996 3 29 96ZZZM516 119951226A5730 SKIN DOUG DC8 DC863 302198AWP WS 106 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, RIGHT WING UPPER SURFACE AT XW 106 NEAR AFT SPAR HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH DRAWING 45931-1. 2L74 4F 4A25 19960329006391996032900639WP 1996 3 29 96ZZZM517 119951226A5330 SKIN DOUG DC8 DC863 302198AWP BS 680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CORROSION ALONG SKIN JOINT STATION 680 TOP OF FUSELAGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SRM 53-2-1. 2L74 4F 4A25 19960329006401996032900640WP 1996 3 29 96ZZZM518 119951226A5320 SUPPORT DOUG DC8 DC863 302198AWP BS 1680 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, CABIN FLOOR STATION 1680 RT SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0. 2L74 4F 4A25 19960329006411996032900641WP 1996 3 29 96ZZZM519 119951226A5347 FLOOR TRACK DOUG DC8 DC863 302198AWP BS 1240-1380 CORRODED A RIAAK NONE O OTHER ININSP/MAINT 1 SO194935C 45931 LEVEL 2 CORROSION, AFT CARGO COMPARTMENT NR 3 RIGHT SIDE FLOOR TRACK ABOVE STRINGER 33R HAS CORROSION FROM FS 1240 TO FS 1380. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW FLOOR TRACK PER SRM 51-1-0. 2L74 4F 4A25 19960329006431996032900643WP 1996 3 29 96ZZZM521 119950829A57445751183506N FLAP ATTACH FTG DOUG DC8 DC873F 302199FWP WS 97 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, FOUND BOTH STATION 97 FLAP ATTACH FITTINGS ON RIGHT SIDE CRACKED. REPLACED BOTH FITTINGS PER DOUGLAS SRM AND STANDARD PRACTICES. 2L74 4F RT4A25 19960329006441996032900644WP 1996 3 29 96ZZZM522 119950829A57445751182506N FLAP ATTACH FTG DOUG DC8 DC873F 302199FWP WS 97 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, FOUND BOTH STATION 97 FLAP ATTACH FITTINGS ON RIGHT SIDE CRACKED. REPLACED BOTH FITTINGS PER DOUGLAS SRM AND STANDARD PRACTICES. 2L74 4F RT4A25 19960329006451996032900645WP 1996 3 29 96ZZZM523 119950829A5312 PRESS BLKHD DOUG DC8 DC873F 302199FWP AFT FUS CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, FOUND 5 INCH BY 2 INCH LONG CRACKS IN AFT PRESSURE BLKHD. REPAIRED PER DOUGLAS SRM 53-2-5. 2L74 4F RT4A25 19960329006461996032900646WP 1996 3 29 96ZZZM524 119950829A323357740355506 ACTUATOR DOUG DC8 DC873F 302199FWP RT MLG CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, RIGHT MLG RETRACT CYL FOUND TO HAVE CORRODED THREADS. REPLACED ACTUATOR. 2L74 4F RT4A25 19960329006471996032900647WP 1996 3 29 96ZZZM525 119950829A5330 SKIN DOUG DC8 DC873F 302199FWP FUSELAGE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, FOUND TWO SKIN CRACKS AT EXTERIOR POWER RECEPTICLE. REPAIRED PER JOSSAIR DWG NR. 2L74 4F RT4A25 19960329006481996032900648WP 1996 3 29 96ZZZM526 119950829A57425753064501N FITTING DOUG DC8 DC873F 302199FWP NR 2 PYLON CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01803DH64239 46123 DURING C-CHECK, DURING COMPLIANCE OF AD 93-21-08, FOUND NR 2 PYLON SUPT FITTING CRACKED. REPLACED NR 2 PYLON SUPPORT FITTING PER DHL J/C 4525. 2L74 4F RT4A25 19960329006491996032900649NM 1996 3 29 96ZZZM527 119950303A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 848.95 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, FLOOR SUPPORT AT SEAT TRACK NR 6 STATION 848.95 RBL 48 INCHES PREVIOUS REPAIR IS CRACKED. REPLACED PREVIOUS REPAIR PER SRM 51-40-3 2024-T3 .040 2 INCH BY 4 INCH AND SRM 51-30-2. 2L73 4F A3WE 19960329006501996032900650NM 1996 3 29 96ZZZM528 119950303A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 804.5 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, FLOOR SUPPORT BEAM AT STATION 804.5 RIGHT BL 49 INCHES. WEB IS CRACKED AT TWO PLACES BELOW AND ABOVE WHERE TURBINE GOES THROUGH WEB. REMOVED DAMAGE WEB SECTION PER SRM 51-30-2. FABRICATED AND INSTALLED NEW SECTION AS PER SRM 51-10-1 P4 AND SRM 51-30-2 8 INCH BY 13 INCH .050 INCH 7075-T6. 2L73 4F A3WE 19960329006511996032900651NM 1996 3 29 96ZZZM529 119950303A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 848.95 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, FLOOR SUPPORT BETWEEN NR 3 AND NR 4 SEAT TRACK IS BROKEN OFF AT ENDS, STATION 848.95. CLEANED FLOOR SUPPORT, TREATED AND PRIMED PER SRM 51-10-6. INSTALLED DOUBLER AT DAMAGED AREA 2024-T3 .032 2 INCH BY 4 INCH AS PER SRM 51-40-3. 2L73 4F A3WE 19960329006521996032900652NM 1996 3 29 96ZZZM530 119950303A5320 FLOOR SUPPORT BOEING727 72730C 1384009NM BS 848.95 CRACKED A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, FLOOR SUPPORT HAS A CRACK AT PREVIOUS REPAIR STATION 848.95 RBL 27 INCHES (SEAT TRACK NR 5). REMOVED OLD REPAIR AND INSTALLED NEW DOUBLER 2024-T3 .040 5.5 INCH BY 1.5 INCH AS PER SRM 51-40-2. 2L73 4F A3WE 19960329006531996032900653NM 1996 3 29 96ZZZM531 119950303A5230 DOOR BOEING727 72730C 1384009NM NR 2 CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, AFT INTERIOR CORNER IS BENT OUT AND HAS TWO CRACKS AT BEND. STOP DRILLED PER SRM 51-10-1. INSTALLED DOUBLER 2024-T3 .063 9 INCH BY 4 INCH AS PER SRM 51-40-2. 2L73 4F A3WE 19960329006541996032900654NM 1996 3 29 96ZZZM532 119950303A5400 S-DUCT BOEING727 72730C 1384009NM NR 2 ENG CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, NR 2 ENGINE S-DUCT INTERIOR AT STATION 1203, SKIN IS BULGING AT SPLICE JUST FWD OF PREVIOUS REPAIR. REMOVED CORROSION PER SRM 51-10-6. CUT OUT DAMAGE AREA PER SRM 51-10-3 AND INSTALLED REPAIR AS PER SRM 54-10-3 AND SRM 51-30-2 12 INCH BY 3 INCH 7075-T6 .050 INCH. 2L73 4F A3WE 19960329006551996032900655NM 1996 3 29 96ZZZM533 119950303A5330 SKIN BOEING727 72730C 1384009NM BS 1148 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, CORROSION ON FWD FACE AT STATION 1148, STRINGER 27L. CUT OUT DAMAGED AREA PER SRM 51-40-3. FABRICATED FILLER 7075-T6 .091 1 INCH BY 2.5 INCH DOUBLER 7075-T6 .063 6 INCH BY 18 INCH, INSTALLED AS PER SRM 51-40-3. ALODINED AND PRIMED PER SRM 51-10-6. 2L73 4F A3WE 19960329006561996032900656NM 1996 3 29 96ZZZM534 119950303A5320 ANGLE BOEING727 72730C 1384009NM BS 540/560 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, FOUND FORWARD BAG FLOOR TO SIDE WALL ATTACH ANGLE CRACKED AT STATION 540 AND 560 LT. CUT OUT DAMAGED AREA AT STATION 560 AND INSTALLED DOUBLER PER SRM 51-40-2, 6 INCH BY 4 INCH 2024-T3 .063 INCH AND STOP DRILLED CRACK AT STATION 540 AND INSTALLED DOUBLER PER SRM 51-40-2 6 INCH BY 4 INCH 2024-T3 .063 INCH. 2L73 4F A3WE 19960329006571996032900657NM 1996 3 29 96ZZZM535 119950303A5330 SKIN BOEING727 72730C 1384009NM BS 570-600 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, FOUND MAIN CARGO DOOR CUTOUT EXTERIOR SKIN DENTED AND WORN FROM STATION 570 TO 600 BOTTOM EDGE. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER PER SRM 53-30-3. DOUBLER SIZE 5.5 INCH BY 30 INCH 7075-T6 1.0. 2L73 4F A3WE 19960329006581996032900658NM 1996 3 29 96ZZZM536 119950303A5347 SEAT TRACK BOEING727 72730C 1384009NM STA 480-580 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, RIGHT SEAT TRACK HAS SURFACE CORROSION FROM STATION 480 TO 580. CUT OUT DAMAGED TRACK FROM BS 520 TO 580. INSTALLED NEW TRACK AS PER SRM 53-10-5. 2L73 4F A3WE 19960329006591996032900659NM 1996 3 29 96ZZZM537 119950303A5347 SEAT TRACK BOEING727 72730C 1384009NM BS 480-500 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH 19011 DURING C-CHECK, FORWARD BAG LEFT SEAT TRACK AT STATION 480 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT FWD BAG FROM BS 480 TO 500 LBL 30 INCH, 22 INCH APPROX AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960329006601996032900660NM 1996 3 29 96ZZZM538 119950303A5330 SKIN BOEING727 72730C 1384009NM BS 420 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01701DH32259 19011 DURING C-CHECK, FOUND SKIN BULGING AT STATION 420 BELOW STRINGER 25R. SKIN REPAIRED AS PER SRM 53-30-3 7075-T6 .063 18 INCH BY 10 INCH. SEALED EDGE WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329006611996032900661NM 1996 3 29 96ZZZM539 119950709A5730 SKIN BOEING727 727228 NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, RIGHT WING UPPER SURFACE NR 1 HINGE CUT OUT FOR THE NR 13 SPOILER IS CRACKED. INSTALLED STOP DRILL, FABRICATED REPAIR DOUBLER AS PER SRM 57-30-4. INSTALLED REPAIR AND REPLACED FASTENERS AT RT WING UPPER SURFACE NR 1 HINGE CUT OUT FOR THE NR 13 SPOILER. 2L73 4F A3WE 19960329006621996032900662NM 1996 3 29 96ZZZM540 119950709A5730 SKIN BOEING727 727228 NM RT WING CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, NR 3 HINGE CUTOUT FOR THE NR 13 SPOILER IS CRACKED AT FWD END. RIGHT WING UPPER SURFACE. REMOVED FASTENERS, LAY OUT REPAIR CRACK ENDS AT EDGE OF METAL, FABRICATED REPAIR DOUBLER AS PER SRM 57-30-4 7075-T6 .071 5 INCH BY 3 INCH. INSTALLED REPAIR AND FASTENERS AS PER SRM 57-30-4 AT NR 3 HINGE CUT OUT FOR THE NR 13 SPOILER RIGHT WING UPPER SURFACE. 2L73 4F A3WE 19960329006631996032900663NM 1996 3 29 96ZZZM541 119950709A5712 RIB BOEING727 727228 NM WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FIXED WING LEADING EDGE AT WBL 92.8 INNER VERTICAL SUPPORT 2ND FROM AFT END IS CRACKED AT TOP FASTENER. STOP DRILLED CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER AND FILLER 2024-T3 .050 5 INCH BY 5 INCH AND INSTALLED PER SRM 51-40-2. 2L73 4F A3WE 19960329006641996032900664NM 1996 3 29 96ZZZM542 119950709A5712 RIB BOEING727 727228 NM WS 130.7 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FIXED WING LEADING EDGE STATION 130.7 INNER RIB HAS LOWER INBD INNER REPAIR ANGLE CRACKED 5 INCHES FROM FWD END. REMOVED FASTENERS FROM REPAIR ANGLE. REMOVED FASTENERS FROM ANGLE AND CUT OUT ANGLE PER SRM 51-40-4. FABRICATED ANGLE 2024-T3 .063 1 INCH BY 1 INCH BY 24 INCH, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED SPLICE ANGLE PER SRM 51-40-3 5 INCH BY 2 INCH ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED NEW ANGLE AND SPLICE ANGLE PER SRM 51-10-1. INSTALLED NUT PLATES PER SRM 51-10-1. 2L73 4F A3WE 19960329006651996032900665NM 1996 3 29 96ZZZM543 119950709A5712 RIB BOEING727 727228 NM WS 349.6 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND WING LEADING EDGE INTERIOR UPPER RIB REPAIR ANGLE IS CRACKED AT AFT END STATION 349.6 OUTBOARD SIDE. INSTALLED FAB CHANNEL 2024-T3 .040 INCH 14 INCHES LONG BY 3 INCHES WIDE PER SRM 51-40-3. LOCATION, WING L/E STATION 349.6 OUTBOARD SIDE. 2L73 4F A3WE 19960329006661996032900666NM 1996 3 29 96ZZZM544 119950709A5712 RIB BOEING727 727228 NM RT WING CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, RIB INSIDE RIGHT WING HAS 5 INCH CRACK AS SEEN THROUGH ACCESS HOLE NR 8811. REMOVED FASTENERS AND OPENED LOWER SKIN FOR ACCESS PER SRM 51-30-2. STOP DRILLED AT END OF CRACKS PER SRM 51-10-1. FABRICATED ANGLE REPAIR 2024-T3 .063 12 INCH BY 1 INCH BY 1.5 INCH. INSTALLED REPAIR AS PER SRM 51-40-2. REINSTALLED FASTENERS AT LOWER SKIN PER SRM 51-30-2. 2L73 4F A3WE 19960329006671996032900667NM 1996 3 29 96ZZZM545 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 480-490 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND STATION 480-490 STRINGER 17L SIDEWALL ANGLE LOWER SIDE HAS NUMEROUS OPEN HOLES, CORROSION ON LOWER RANGE AND LOWER FLANGE DAMAGED. REMOVED ANGLE FLOOR SUPPORT PER SRM 51-30-2. INSTALLED NEW ANGLE SUPPORT FROM BS 480 TO BS 500 AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960329006681996032900668NM 1996 3 29 96ZZZM546 119950709A5320 INTERCOSTAL BOEING727 727228 NM FS 211.8-229.8 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND CORROSION AND BULGE ON INTERCOSTAL FS 211.8-229.8 LEFT SIDE 12 ABOVE ACCESS DOOR. REMOVED CORROSION WITHIN LIMITS PER SRM 51-10-6. TREATED WITH ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED NEW INTERCOSTAL OF 2024-T3 .040 9 INCH BY 6 INCH TRIMMED TO FIT PER SRM 51-10-1. INSTALLED WITH NEW HARDWARE PER SRM 51-30-2. 2L73 4F A3WE 19960329006691996032900669NM 1996 3 29 96ZZZM547 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 640-700 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND FWD CARGO COMPARTMENT, CORROSION UNDER FLOOR PANEL SUPPORT AT BS 640 TO BS 700 AND RBL 7. REMOVED CORROSION AS PER SRM 51-10-6. ALODINED AND PRIMED AS PER SRM 51-10-2. FABRICATED WEB 7075-T6 .032 55.5 INCH BY 2.5 INCH AT BS 640 TO BS 700 AND RBL 7. 2L73 4F A3WE 19960329006701996032900670NM 1996 3 29 96ZZZM548 119950709A5347 SEAT TRACK BOEING727 727228 NM BS 1130/1136 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, NR 5 TRACK LOWER SURFACE CORRODED AROUND FASTENERS BETWEEN STATION 1130 AND STATION 1136 RBL 24.75. REMOVED FASTENERS AS PER SRM 51-30-2. REMOVED CORROSION FOUND OUT OF LIMIT. CUT OUT DAMAGE SECTION SEAT TRACK FOR REPAIR. FABRICATED SEAT TRACK SECTION 24 INCHES LENGTH PER SRM 51-10-1. ALODINED AND PRIMED SEAT TRACK SECTION PER SRM 51-10-2. INSTALLED NEW SEAT TRACK PER SRM 51-30-2. 2L73 4F A3WE 19960329006711996032900671NM 1996 3 29 96ZZZM549 119950709A5347 SEAT TRACK BOEING727 727228 NM BS 1164-1173 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND NR 6 CABIN FLOOR TRACK LIP DAMAGED BETWEEN STATION 1164 AND STATION 1173 RBL 45.50. REMOVED SLAT TRACK NR 6 FROM STATION 1164 TO 1178 PER SRM 53-10-5. INSTALLED SEAT TRACK NR 6 FROM STATION 1164 TO 1173 PER SRM 53-10-5. 2L73 4F A3WE 19960329006721996032900672NM 1996 3 29 96ZZZM550 119950709A5320 WEB BOEING727 727228 NM FS 990-1010 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND AFT CARGO, CRACK AND BULGE IN WEB FS 990-1010 STRINGER 30. CUT OUT DAMAGED AREA. ALODINED AND PRIMED AREA. INSTALLED FILLER 2024-T3. INSTALL DOUBLER AS PER SRM 51-40-2, SIZE 5 INCH BY 4 INCH AND 5 INCH BY 3 INCH .050 2024-T3. 2L73 4F A3WE 19960329006731996032900673NM 1996 3 29 96ZZZM551 119950709A5347 TRACK BOEING727 727228 NM BS 760-754 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND NR 4 CABIN FLOOR TRACK UPPER SURFACE AND LIPS DAMAGED AND WORN AT APPROX STATION 764. REPLACED UPPER SURFACE DAMAGED LIPS WITH SEAT TRACK REPAIR AS PER SRM 53-10-5 APPROX 6 INCHES FROM STATION 760 TO 754. TREATED AND ALODINED AND PRIMER ON BOTTOM AS PER SRM 51-10-2. SEALED WITH PRC/SELASTIC AS PER SRM 51-20-4. 2L73 4F A3WE 19960329006741996032900674NM 1996 3 29 96ZZZM552 119950709A5330 SKIN BOEING727 727228 NM RAM AIR PLENUM CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND CORROSION ON UPPER SURFACE OF LEFT RAM AIR PLENUM ABOVE SECONDARY HEAT EXCHANGER. REMOVED CORROSION AS PER SRM 51-10-6. REMOVED FASTENERS PER SRM 51-30-2. NDT CHECK LOSS MATERIAL .090. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED TWO EXTERNAL DOUBLER AS PER SRM 57-30-3 FIG 8 2024-T3 3.75 BY 13 INCH .080 AND INSTALLED FASTENERS. 2L73 4F A3WE 19960329006751996032900675NM 1996 3 29 96ZZZM553 119950709A5330 SKIN BOEING727 727228 NM RAM AIR PLENUM CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND CORROSION ON UPPER SURFACE OF RIGHT RAM AIR PLENUM ABOVE RIGHT SECONDARY HEAT EXCHANGER. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT 'L' ANGLE SUPPORT FOR ACCESS. REMOVED CORROSION PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED TWO DOUBLERS 2024-T3 .080 3.75 INCH BY 13 INCH AND FILLER 3.75 BY 9 INCH. INSTALLED REPAIR AS PER SRM 57-30-3. 2L73 4F A3WE 19960329006761996032900676NM 1996 3 29 96ZZZM554 119950709A5320 ANGLE BOEING727 727228 NM BS 950 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, EXTERIOR FUSELAGE VERTICAL STIFFENER ANGLE CRACKED AT LOWER END STATION 950 AFT SIDE OF RIGHT WHEEL WELL AFT BULKHEAD RBL 54 INCHES. STOP DRILLED AS PER SRM 51-10-1. INSTALLED TYPICAL WEB REPAIR AS PER SRM 51-40-2 AT STATION 950 AFT SIDE OF RIGHT WHEEL WELL WITH 2024-T3 MATERIAL .050 5 INCH BY 2 INCH. 2L73 4F A3WE 19960329006771996032900677NM 1996 3 29 96ZZZM555 119950709A5330 DITCHING PLATE BOEING727 727228 NM BS 1180 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND MAIN CABIN STATION 1180 RBL 28, DITCHING PLATE IS CRACKED. FABRICATED NEW DITCHING PLATE PER SRM 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER 2024-T3 .025 6 INCH BY 3 INCH PER SRM 51-10-1. 2L73 4F A3WE 19960329006781996032900678NM 1996 3 29 96ZZZM556 119950709A5330 SKIN BOEING727 727228 NM BS 1260 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND AFT AIR STAIR COMPARTMENT WEB CRACKED AT LIGHTENING HOLE STATION 1260 LEFT. INSTALLED REPAIR ON WEB AT LIGHTENING HOLE STATION 1260 LEFT. REPAIR DIMENSIONS 3 INCH BY 4 INCH 2024-T3 AS PER SRM 51-40-2. 2L73 4F A3WE 19960329006791996032900679NM 1996 3 29 96ZZZM557 119950709A5313 STRINGER BOEING727 727228 NM BS 736 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, LOWER FORWARD AIR COND BAY INT'R BS 736F STRINGER 26R CENTER BOTTOM STRINGER TO TIE CLIP CORROSION LEVEL 1. REMOVED FASTENERS BS 725F TO 740 STR 26R AS PER SRM 51-30-2. CUT OUT 9 INCHES OF STRINGER 26R BS 729F TO 738F. REMOVED TIE CLIP FOR CORROSION. CLEANED AREA, NO CORROSION. REINSTALLED NEW SECTION OF STRINGER 9 INCHES AND STRINGER SPLICE 12 INCHES LONG AS PER SRM 53-10-3 FIG 1. 2L73 4F A3WE 19960329006801996032900680NM 1996 3 29 96ZZZM558 119950709A5330 SKIN BOEING727 727228 NM BS 723E CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND FORWARD LOWER C/C AND AIR COND BAY INT'R BS 723E STRINGER 26R LAP SEAM UPPER SIDE CORROSION LEVEL 1. REMOVED RIGHT RAM AIR DUCT FOR S/M ACCESS. REMOVE HI-LOKS PER SRM 51-30-2. CUT OUT DAMAGED SKIN CORROSION OUT OF LIMITS AS PER SRM 53-30-3. FABRICATED FILLER .090 10 INCHES BY 10 INCHES AND DOUBLER 2024-T3 .0100 14 INCHES BY 10 INCHES. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3. SEALED EDGE WITH PRC PER SRM 51-20-4. 2L73 4F A3WE 19960329006811996032900681NM 1996 3 29 96ZZZM559 119950907A5320 SUPPORT BEAM BOEING727 727228 NM BS 1183 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND MAIN CABIN STATION 1183 LBL 35 VERTICAL SUPPORT BEAM IS CRACKED 28 INCHES ABOVE FLOOR AT ATTACH BOLTS. STOP DRILLED CRACK AS PER SRM 51-10-1. INSTALLED REPAIR AS PER DRAWING 65C34406 AT STATION 1183 LBL 35 FROM WL 23 TO WL 242. 2L73 4F A3WE 19960329006821996032900682NM 1996 3 29 96ZZZM560 119950709A5330 PLATE BOEING727 727228 NM BS 1180 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20204 DURING D-CHECK, FOUND MAIN CABIN STATION 1180 LBL 60, DITCHING PLATE HAS 1 INCH HOLE THAT IS NOT COVERED. STOP DRILLED AT THE END OF CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2. 2L73 4F A3WE 19960329006931996032900693SW 1996 3 29 MALA954692 119951104A5210 SEAL SWRNGNSA227 SA227AC 8780603SW PAX DOOR DAMAGED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15424MA AC639 FLT NR 3453 - IN CRUISE FLIGHT, A LOUD SQUEAL WAS NOTED FROM THE PASSENGER DOOR. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE FOUND THAT THE PASSENGER DOOR FRAME FORWARD UPPER SCUFF REPAIR PLATE CAUGHT ONTO THE DOOR ALIGNMENT TEFLON BLOCK, WHICH IN TURN TORE THE DOOR SEAL. REPAIRS TO THE DOOR FRAME WERE COMPLETED BY INSTALLING A NEW SCUFF PLATE PER ARP 53-20-9116 AND BY REPLACING THE UPPER TEFLON BLOCK. THE DOOR SEAL SYSTEM WAS DEFERRED. (M) 2L72 4T RTA8SW 19960329006941996032900694SW 1996 3 29 MALA954693 119951106A27302782168007 CONTROL BOX FRCHLDSA227 SA227DC 3377521SW PITCH TRIM FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL15452LA DC848B FLT NR 3224 - ON CLIMB-OUT FROM MSP, WITH THE GEAR UP, THE OUT OF TRIM FOR TAKEOFF WARNING HORN SOUNDED. WHEN THE PITCH TRIM WAS PUT IN THE GREEN ARC, THE HORN STOPPED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE PITCH TRIM WARNING CONTROL BOX, P/N 27-82168-007, AND ADJUSTED THE POTENTIOMETER IAW SA227 MM 27-40-10. (M) 1L72 4T RTA18SW 19960329006951996032900695SW 1996 3 29 MALA954694 119951105A215020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW LT WING ROOT SEIZED A MALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL152692P AC658B FLT NR 3265 - DURING TAXI FROM GATE IN FSD, THE CREW NOTED A SMOKEY ODOR IN THE AIRCRAFT ALONG WITH A SMALL AMOUNT OF VISIBLE SMOKE. THE CREW SHUT DOWN THE LEFT BLEED AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT COOLING TURBINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329006961996032900696SW 1996 3 29 MALA954695 119951108A2435230790001 STARTER/GEN SWRNGNSA227 SA227AC 8780603SW LT ENGINE FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15160MC AC733B DURING A TRAINING FLIGHT IN FAR, THE LEFT ESSENTIAL BUS AND LEFT GENERATOR FAILED. THE AIRCRAFT RETUREND TO FAR WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT STARTER GENERATOR AND A P/N ANL 325 CURRENT LIMITER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329006971996032900697NM 1996 3 29 MALA954696 119951108A33506104781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST CRCRUISE 1 GL15849MA 347 FLT NR 3432 - DURING PREFLIGHT INSPECTION IN DTW, THE CREW NOTED SEVERAL WHITE FLOOR TRACK EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE. MAINTENANCE PERSONNEL REPLACED THE EMERGENCY BATTERY PACKS AT THE LEFT FORWARD AND LEFT AFT POSITIONS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329006981996032900698NM 1996 3 29 MALA954697 119951108A3260 GEAR LIGHT DHAV DHC8 DHC8102 2809003NM LT MLG ILLUMINATED A MALAK NONE N FALSE WARNING CRCRUISE 1 GL15849MA 347 FLT NR 3432 - EN ROUTE TO MDT, THE LEFT MAIN GEAR UNSAFE LIGHT AND INTRANSIT LIGHT ILLUMINATED. THE FLIGHT CONTINUED TO MDT, WHERE THE GEAR WAS EXTENDED NORMALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED THE GEAR AND PERFORMED A TEST FLIGHT BUT WERE UNABLE TO DUPLICATE THIS DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329006991996032900699NM 1996 3 29 MALA954698 119951108A3234574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003NM LANDING GEAR FAILED A MALAK NONE J WARNING INDICATION CRCRUISE 1 GL15849MA 347 FLT NR 3383 - EN ROUTE FROM MDT TO DTW, THE LEFT MAIN GEAR UNSAFE LIGHT AND GEAR INTRANSIT LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LANDING GEAR SELECTOR VALVE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329007001996032900700SW 1996 3 29 MALA954699 119951108A3260 GEAR LIGHT SWRNGNSA227 SA227AC 8780603SW NLG MALFUNCTIONED A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL1527465 AC755B FLT NR 3463 - EN ROUTE TO DTW, THE CREW NOTED GEAR INTRANSIT INDICATIONS FROM THE NOSE GEAR. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL INSPECTED AND FUNCTIONALLY TESTED THE GEAR INDICATION SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPANCY. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329007011996032900701SW 1996 3 29 MALA954700 119951112A5414 SKIN SWRNGNSA227 SA227AC 8780603SW RT NACELLE CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, INSPECTORS NOTICED A CRACK IN THE RIGHT LOWER INBOARD NACELLE SKIN TO LOWER WING SKIN ATTACH ANGLE. MAINTENANCE PERSONNEL REMOVED THE CRACKED ATTACH ANGLE AND REPLACED IT WITH A NEW ANGLE IAW ARP 54-20-9101. (M) 2L72 4T RTA8SW 19960329007021996032900702SW 1996 3 29 MALA954701 119951112A5210 DOOR FRAME SWRNGNSA227 SA227AC 8780603SW FS 438.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE CARGO DOOR FRAME TO BE CRACKED AT FS 438.060. THEY FABRICATED A REPAIR FILLER, DOUBLER AND ATTACH ANGLE AND INSTALLED THEM IAW ARP 53-20-9503. (M) 2L72 4T RTA8SW 19960329007031996032900703SW 1996 3 29 MALA954702 119951112A5320 SUPPORT SWRNGNSA227 SA227AC 8780603SW FS 347.241 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE RIGHT FS 347.241 FLOOR SUPPORT FLANGE AT APPROXIMATELY BL 8.0. THEY REPAIRED THE CRACK BY STOP DRILLING IT AND FABRICATING AND INSTALLING A REPAIR DOUBLER IAW SRM 53-90-20. (M) 2L72 4T RTA8SW 19960329007041996032900704SW 1996 3 29 MALA954703 119951111A5347 SEAT TRACK SWRNGNSA227 SA227AC 8780603SW FS 107.06 CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE SEAT TRACK UPPER FLANGE AT FS 107.06. THE POINT HAD BEEN PREVIOUSLY REPAIRED. MECHANICS REMOVED THE PREVIOUS REPAIR AND FABRICATED AND INSTALLED A NEW REPAIR. (M) 2L72 4T RTA8SW 19960329007051996032900705SW 1996 3 29 MALA954704 119951111A5210 FRAME SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER AFT CORNER OF THE PASSENGER DOOR FRAME. THEY REPLACED THE LOWER AFT PASSENGER DOOR FRAME CORNER, P/N 27-24044-010, IAW SRM 54-40-01 AND 02. (M) 2L72 4T RTA8SW 19960329007061996032900706SW 1996 3 29 MALA954705 119951109A216020475546 COOLING TURBINE SWRNGNSA227 SA227AC 8780603SW LT WING ROOT SEIZED A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 GL15434MA AC717 FLT NR 3434 - DURING TAXI AFTER LANDING, THE CREW NOTED SMOKE IN THE CABIN AND COCKPIT. THE CREW SHUT DOWN BOTH BLEEDS AND PROCEEDED TO THE GATE. MAINTENANCE PERSONNEL REPLACED THE LEFT COOLING TURBINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329007071996032900707SW 1996 3 29 MALA954706 119951112A32601EN516 SWITCH SWRNGNSA227 SA227AC 8780603SW NLG OUT OF ADJUST A MALAO OTHER N FALSE WARNING CRCRUISE 1 GL1527465 AC755B FLT NR 3360 - AFTER THE LANDING GEAR WAS RETRACTED ON TAKEOFF FROM DTW, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL ADJUSTED THE NOSE GEAR UP POSITION SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329007081996032900708SW 1996 3 29 MALA954707 119951112A5320 CHANNEL SWRNGNSA227 SA227AC 8780603SW BELLY FAIRING CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE CENTER CHANNEL FOR THE FORWARD WING TO FUSELAGE BELLY FAIRING. THEY REPLACED THE CENTER CHANNEL AND INSTALLED A STIFFENER IAW SRM 57-90-30. (M) 2L72 4T RTA8SW 19960329007091996032900709NM 1996 3 29 MALA954708 119951112A33506104781 BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A MALAK NONE L NO TEST CRCRUISE 1 GL15827MA 331 FLT NR 3032 - DURING PREFLIGHT IN DTW, THE CREW NOTED SEVERAL FLOOR TRACK EMERGENCY LIGHTS INOP. MAINTENANCE PERSONNEL REPLACED THE LEFT HAND AND RIGHT HAND FORWARD BATTERY PACKS. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329007101996032900710NM 1996 3 29 MALA954709 119951112A3040SYLZ50970 HEAT CONTROLLER DHAV DHC8 DHC8102 2809003NM LT WINDSHIELD FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15826MA 330 FLT NR 3302 - EN ROUTE FROM DTW TO AZO, THE LEFT WINDSHIELD HOT LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE CAPTAINS WINDSHIELD HEAT CONTROLLER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329007111996032900711SW 1996 3 29 MALA954710 119951114A52102724044009 FRAME CORNER SWRNGNSA227 SA227AC 8780603SW PAX DOOR CRACKED A MALAK NONE O OTHER ININSP/MAINT 1 GL15433MA AC714 DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER FORWARD PASSENGER DOOR CORNER. THEY REPLACED THE CORNER IAW FAIRCHILD SRM 51-40-01 AND 02. (M) 2L72 4T RTA8SW 19960329007121996032900712SW 1996 3 29 MALA954711 119951114A2422PC350 INVERTER SWRNGNSA227 SA227AC 8780603SW NR 2 FAILED A MALAA UNSCHED LANDING O OTHER CRCRUISE 1 GL15428MA AC646 FLT NR 3237 - EN ROUTE FROM MSP TO BJI, THE NR 2 INVERTER DROPPED OFF LINE. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 2 INVERTER. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329007131996032900713SW 1996 3 29 MALA954712 119951115A302031998061 SOLENOID VALVE SWRNGNSA227 SA227AC 8780603SW LT INTAKE HEAT FAILED A MALAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL15423MA AC636 FLT NR 3345 - EN ROUTE FROM DTW TO CVG, THE LEFT INTAKE HEAT WOULD NOT FUNCTION WHEN SELECTED ON. THE AIRCRAFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT INTAKE HEAT VALVE AND REPAIRED BROKEN WIRES AT THE INTAKE HEAT VALVE CANNON PLUG. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2L72 4T RTA8SW 19960329007141996032900714NM 1996 3 29 MALA954713 119951116A3240 BRAKE SYSTEM DHAV DHC8 DHC8102 2809003NM MLG REQ'D SERVICE A MALAO OTHER O OTHER TXTAXI/GRND HDL 1 GL15864MA 363 FLT NR 3309 - AFTER LANDING IN DTW, THE CREW NOTED THE FIRST OFFICERS BRAKES REQUIRED EXCESSIVE PRESSURE BEFORE BRAKING ACTION WOULD OCCUR. MAINTENANCE PERSONNEL BLED THE BRAKE SYSTEM IAW DHC-8 MM 32-42-00. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960329007151996032900715NM 1996 3 29 MALA954729 119951203A3150 WARNING LIGHT DHAV DHC8 DHC8102 2809003NM SPOILER SYSTEM ILLUMINATED A MALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL15864MA 363 FLT NR 3410 - ON CLIMB-OUT, THE GROUND SPOILER ADVISORY LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE LEFT INBOARD AND OUTBOARD GROUND SPOILER TARGETS WERE REPLACED AS A PRECAUTION. ALL SYSTEMS OPERATED SATISFACTORILY. (M) 2H72 4T RTA13NM 19960405000041996040500004NM 1996 4 5 96ZZZX1393 119951221A5347 SEAT TRACK BOEING727 727232 1384082NM BS 340-380 CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 SEAT TRACK, RBL 13, STA 340 - STA 380, HAS LEVEL 2 CORROSION AT SEVERAL AREAS ALONG FLANGES AND FLOOR BEAM ATTACH POINTS. REMOVED DAMAGED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK SECTION PER SRM 51-10-1 AND SRM 51-30-2. 2L73 4F A3WE 19960405000051996040500005NM 1996 4 5 96ZZZX1394 119951229A5320 DOUBLER BOEING727 727232 1384082NM RT AFT LAV CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 AFT RT LAV, APPROXIMATELY 6 INCHES DIAMETER AREA OF BULGING ON SUB-FLOOR AROUND PLUMBING LINES. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2. 2L73 4F A3WE 19960405000061996040500006NM 1996 4 5 96ZZZX1395 119951229A5320 DOUBLER BOEING727 727232 1384082NM BS 546 CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 BRACKET CRACKED IN FORWARD CARGO BETWEEN STR 26R AND STR 27R AT STA 546. STOP DRILLED CRACK, FABBED DOUBLER AND INSTALLED PER SRM 51-20-2. 2L73 4F A3WE 19960405000071996040500007NM 1996 4 5 96ZZZX1396 119951227A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 380R CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 STA 380.0 FLOOR BEAM UPPER CORD HAS LEVEL 2 CORROSION ACROSS IT FROM RBL 13 TO RBL 60. REMOVED AREA OUT OF LIMITS AND REPAIRED PER SRM 53-10-8, FIGURE 3. 2L73 4F A3WE 19960405000081996040500008NM 1996 4 5 96ZZZX1397 119950102A5315 FLOOR BEAM BOEING727 727232 1384082NM BS 420 CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP0118786 20641 STA 420.0 FLOOR BEAM UPPER CHORD HAS LEVEL 2 CORROSION AT SEVERAL AREAS FROM RBL 10 TO RBL 60. REMOVED CORROSION PER SRM 51-10-6. WITHIN LIMITS PER SRM 53-10-1 EXCEPT AT RBL 14. REPAIRED WITH NESTED ANGLES PER SRM 51-40-4. 2L73 4F A3WE 19960405000241996040500024EA 1996 4 5 96ZZZX1413 119950514A79337645000906101 GAUGE DHAV DHC7 DHC7102 2802708EA ENG OIL TEMP FLUCTUATION A BTEAK NONE O OTHER ININSP/MAINT 1 GL09176RA 102 76 REMOVED GAUGE FOR NEEDLE RAPID FLUCTUATION - 20-50 DEGREES, SPIKING WILDLY OCCASIONALLY. 2H74 4T A20EA 19960405000541996040500054EU 1996 4 5 96ZZZX1443 119951204A5523 BUSHINGS SAAB SF340 340B 7860101EU ELEV TAB FAILED A NVEAAH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET CLCLIMB 1 SO03266AE 340B266 TPA - FLT 5824 - VIBRATIONS IN CONTROLS DURING CLIMB AND DESCENT, DEACTIVATED YAW DAMPER. REPLACED ELEVATOR TAB BUSHINGS. FUNCTIONAL TEST FLT PASSED. 2L72 4T RTA52EU 19960405000551996040500055EU 1996 4 5 96ZZZX1444 119951221A3260M3001264 RELAY BAG JETSTMJETSTM3201 1500217EU LNDG GEAR HORN FAILED A NVEAB EMER. DESCENT J WARNING INDICATION APAPPROACH 1 SO03930AE 930 CVG - FLT 4509 - CREW REPORTED WITH GEAR DOWN AND LOCKED AND FLAPS AT 20 DEGREES, THEY HAD A GEAR HORN. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED GEAR HORN INHIBIT RELAY. TEST FLEW, OPS CHECK GOOD. 2L72 4T RTA56EU 19960405000761996040500076SW 1996 4 5 MALA954786 119951228A2730MS210424 NUT SWRNGNSA227 SA227AC 8780603SW VERTICAL STAB MALFUNCTIONED A MALAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 GL15159MC AC728B FLT 3237 - DURING APPROACH TO BJI, CREW NOTED AN EXCESSIVE PITCH DOWN WHEN POWER WAS REDUCED. AFTER PERFORMING A GO-AROUND, ACFT RETURNED TO BJI AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND UPPER ELEVATOR STOP BOLT HAD MIGRATED OUT RESULTING IN INTERFERENCE WITH VERTICAL STAB STRUCTURE. MAINTENANCE PERSONNEL REPLACED UPPER ELEVATOR STOP HARDWARE. ALL SYSTEMS OPERATED SATISFACTORILY. (X) 2L72 4T RTA8SW 19960405001791996040500179EU 1996 4 5 96ZZZX1459 119951013A2612D2370120 FIRE LOOP BAG JETSTMJETSTM3101 1500215EU LEFT MALFUNCTIONED A REXAO OTHER N FALSE WARNING CLCLIMB 1 SO25317PX 688 LEFT DETECT LIGHT ON TWICE DURING FLIGHT. STAYED ON FOR A FEW MINUTES. REMOVED AND REPLACED LT FIRE CONTROL UNIT IAW JSMM 2610. REMOVED AND REPLACED FORWARD FIRE LOOP IAW JSMM 2610. REFERENCE CONTROL NR REXA95-065. 2L72 4T RTA21EU 19960405001961996040500196EU 1996 4 5 REXA95065 119951013A261251653120 CONTROL UNIT BAG JETSTMJETSTM3101 1500215EU LEFT MALFUNCTIONED A REXAO OTHER N FALSE WARNING CLCLIMB 1 SO25317PX 688 LEFT DETECT LIGHT ON TWICE DURING FLIGHT. STAYED ON FOR A FEW MINUTES. REMOVED AND REPLACED LT FIRE CONTROL UNIT IAW JSMM 2610. REMOVED AND REPLACED FORWARD FIRE LOOP IAW JSMM 2610. REFERENCE CONTROL NR 96ZZZX1459. (X) 2L72 4T RTA21EU 19960405001971996040500197EU 1996 4 5 REXA95069 119951217A78107271899731 MIXER DUCT SAAB SF340 SF340A 7850100EU LT ENGINE MISSING A REXAO OTHER D INFLIGHT SEPARATION CRCRUISE 1 SO25404BH 340A061 MIXER DUCT MISSING ON LT ENGINE. PASSENGER REPORTS SEEING SOMETHING FALL OUT OF THE REAR OF ENGINE. REPLACED LT MIXER DUCT AND COUPLING IAW AMM 78-10-05. PERFORMED GROUND RUN. NO DEFECTS. OK FOR SERVICE. (X) 2L72 4T RTA52EU 19960405001981996040500198EU 1996 4 5 REXA95074 119951218A2460A2042C43C PWR DISTR UNIT SAAB SF340 SF340A 7850100EU RIGHT FAILED A REXAL ABORTED APPROACH HJ ELECT. POWER LOSS-50 PC WARNING INDICATION APAPPROACH 1 SO25402BH 340A058 LOST RT MAIN BUS AND ALL ASSOCIATE FLEET EQUIPMENT ON APPROACH. REMOVED AND REPLACED SHORTED WIRE AC225. REMOVED AND REPLACED LT AND RT PDU'S AND TIME DELAY RELAY PC12. SYSTEM OPERATION CHECKED GOOD. ACFT OK FOR CONTINUED SERVICE. (X) 2L72 4T RTA52EU 19960405002071996040500207NM 1996 4 5 TSAA9557206 119951218A5744 FITTING BOEING737 7372Q9 138448MNM FSS 422 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND INTERGRANULAR CORROSION NEAR NR 5 L/E SLAT ACTUATOR ATTACH FITTING (FRONT SPAR) APPROXIMATELY FSS-422. REPAIRED PER ECO 2659. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405002081996040500208NM 1996 4 5 TSAA9557207 119951218A5711NRTC10726 SPAR BOEING737 7372Q9 138448MNM FSS 286-321 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, NUMEROUS SPAR CORROSION NOTED BETWEEN FSS 286.9 - SS 45.9, AND FSS 321 - SS 80.1. REPAIRED PER ECO 2646. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405002441996040500244WP 1996 4 5 ABXA9600424 119951227A53203773077510 SUPPORT BEAM DOUG DC8 DC863 302198AWP BS 180 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED THE FLOOR BEAM VERTICAL SUPPORT AT FUSELAGE STATION 180, 50 INCHES INBOARD OF CENTER LINE HAS CORROSION WHERE GILLINER SUPPORT ANGLE ATTACHES. REPAIRED THE FLOOR BEAM VERTICAL SUPPORT BEAM AT STATION 180 THAT WAS CORRODED IAW ABX REA D853-12608MR. 2L74 4F 4A25 19960405002451996040500245WP 1996 4 5 ABXA9600425 119951227A7800 ATTACH CHANNEL DOUG DC8 DC863 302198AWP NR 2 ENGINE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED NR 2 ENGINE RIGHT HAND AFT TRANSITION ATTACHMENT ASSEMBLY DUCT STRIP IS CRACKED ON BOTH ENDS. REPAIRED NR 2 ENGINE RIGHT HAND AFT TRANSITION BI-DUCT ATTACH CHANNEL IAW ABX REA D878-12614MR. 2L74 4F 4A25 19960405002461996040500246WP 1996 4 5 ABXA9600426 119951227A533057503223 SKIN DOUG DC8 DC863 302198AWP BS 1050-1150 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED BELLY SKIN AT STATION 1050 TO 1150 HAS BARE METAL AND CORROSION ON ENTIRE UNDERSIDE OF SKIN. REPAIRED CORRODED BELLY SKIN AT FUSELAGE STATION 1050 TO 1150, LONGERON 33L AND 33R IAW ABX REA D853-12613MR. 2L74 4F 4A25 19960405002471996040500247WP 1996 4 5 ABXA9600427 119951227A5414 SKIN DOUG DC8 DC863 302198AWP NR 3 PYLON DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED A DENT AT NR 3 ENGINE PYLON, STATION YN 141.00, PYLON LOWER SURFACE. REPAIRED NR 3 ENGINE PYLON THAT WAS DENTED ON THE LOWER SURFACE AT STATION YN 141.00 IAW ABX REA D854-12587MR. 2L74 4F 4A25 19960405002481996040500248WP 1996 4 5 ABXA9600428 119951227A57303757852 SKIN DOUG DC8 DC863 302198AWP WS 451 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LEFT HAND UPPER WING AT NR 1 ENGINE BETWEEN FRONT AND MID SPAR SKIN REPAIR HAS CORRODED FASTENERS AND CORROSION BETWEEN REPAIR AND SKIN. REPAIRED LEFT HAND WING TOP PANEL PLATING THAT WAS CORRODED AT STATION XW 451 IAW ABX REA D857-12592MR. 2L74 4F 4A25 19960405002491996040500249WP 1996 4 5 ABXA9600429 119951227A5330 SKIN DOUG DC8 DC863 302198AWP BS 340 DAMAGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 340 LONGERON 17R, BOTH WINDOW CUTOUTS HAVE QUESTIONABLE REPAIRS. REPAIRED WINDOW CUTOUTS AT FUSELAGE STATION 340, LONGERON 17R IAW ABX REA D853-12604. 2L74 4F 4A25 19960405002501996040500250WP 1996 4 5 ABXA9600430 119951227A5320577278711 DOOR JAMB DOUG DC8 DC863 302198AWP BS 120 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 120 FOWARD SIDE OF MAIN CARGO DOOR SEAL RETAINER CRACKED AND BENT IN SEVERAL PLACES. REPAIRED MAIN CARGO DOOR FORWARD JAMB STRUCTURE AND WEB THAT WAS CRACKED AND BENT IN SEVERAL PLACES IAW ABX REA D853-12597MR. 2L74 4F 4A25 19960405003691996040500369NM 1996 4 5 TSAA9553210 119951218A5280 DOOR HINGE BOEING737 7372Q9 138448MNM LT MLG CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, INTERGRANULAR CORROSION NOTED ON FIXED DOOR HINGE AREA, LT GEAR. CLEANED AND TREATED PER SRM 51-10-6. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003701996040500370NM 1996 4 5 TSAA9553214 119951218A5313 STRINGER BOEING737 7372Q9 138448MNM BS 907 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, AFT CARGO COMPARTMENT, CORROSION NOTED ON S27R AT BS 907. REPAIRED PER ECO 2599. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003711996040500371NM 1996 4 5 TSAA9553215 119951218A5313 STRINGER BOEING737 7372Q9 138448MNM BS 907-927 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, AFT CARGO COMPARTMENT, CORROSION NOTED ON S27L BETWEEN BS 907 AND BS 927. REPAIRED PER ECO 2599. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003721996040500372NM 1996 4 5 TSAA9553216 119951218A5320 PANEL RECESS BOEING737 7372Q9 138448MNM AFT LAVATORY CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND AFT LAVATORY SERVICE PANEL HAS INTERGRANULAR CORROSION AROUND PANEL RECESS. REPAIRED PER ECO 1998, OPTION II. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003731996040500373NM 1996 4 5 TSAA9555209 119951218A5532 SKIN BOEING737 7372Q9 138448MNM VERT STAB CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND VERTICAL STABILIZER, LT SKIN EXFOLIATED APPROXIMATELY 2 INCHES BY .50 INCH JUST ABOVE AFT FUSELAGE TO STABILIZER MOUNT BOLT. REPAIRED PER ECO 2649. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003741996040500374NM 1996 4 5 TSAA9557208 119951218A5711 SPAR BOEING737 7372Q9 138448MNM FSS 286-321 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, OUTBOARD OF NR 3 ACTUATOR ATTACH POINT HAS SPAR CORROSION NEXT TO RIVET BETWEEN FSS 286.9 AND FSS 321.1. REPAIRED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003751996040500375NM 1996 4 5 TSAA9557211 119951218A5711 SPAR BOEING737 7372Q9 138448MNM FSS 326-359 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND RT LOWER FRONT SPAR HAS CORROSION AT FSS 321.6 INCH, FSS 359-3.5 INCH AND FSS 359 PLUS 18 INCH. REPAIRED PER ECO 2645. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003761996040500376NM 1996 4 5 TSAA9557212 119951218A5730 SKIN BOEING737 7372Q9 138448MNM WS 499.9 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND RT WING LOWER SURFACE HAS CORROSION AT WS 499.9 PLUS 11.50 INCH, AND WS 499.9 PLUS 17 INCH. REPAIRED PER ECO 2648. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405003771996040500377NM 1996 4 5 TSAA9557213 119951218A5730 SKIN BOEING737 7372Q9 138448MNM WS 461 CORRODED A TSAAK NONE O OTHER ININSP/MAINT 1 WP13809AL 21720 DURING HEAVY MAINTENANCE VISIT, FOUND RT WING, TOP SURFACE, HAS SURFACE CORROSION. CLEANED AND TREATED PER SRM 51-10-6 AT FSS 461 PLUS 17 INCH AFT OF FRONT SPAR. REPAIRED PER ECO 1722R5. AIRCRAFT RETURNED TO SERVICE. (X) 2L72 4F A16WE 19960405005341996040500534WP 1996 4 5 ABXA9600432 119951227A5320577278515 DOOR JAMB DOUG DC8 DC863 302198AWP BS 240-280 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, UPPER AFT TORQUE BOX WEB GOUGED WITH NUMEROUS MISDRILLED HOLES AT STATION 240 T0 280. REPAIRED MAIN CARGO DOOR AFT UPPER JAMB WEB AND PAN THAT WAS GOUGED WITH NUMEROUS MISDRILLED HOLES AT STATION 240 TO 280 IAW ABX REA D853-12593. 2L74 4F 4A25 19960405005351996040500535WP 1996 4 5 ABXA9600433 119951227A5320577278513 DOOR JAMB DOUG DC8 DC863 302198AWP BS 160-180 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, STATION 160 TO 180, UPPER TORQUE BOX WEB REPAIR DOUBLER GOUGED. REPAIRED MAIN CARGO DOOR UPPER JAMB WEB DOUBLER AT STATION 160 IAW ABX REA D853-12590MR. 2L74 4F 4A25 19960405005361996040500536WP 1996 4 5 ABXA9600434 119951227A5320577278712 DOOR JAMB DOUG DC8 DC863 302198AWP BS 280 MISDRILLED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED MAIN CARGO DOOR, AFT SIDE TORQUE BOX WEB AT STATION 280 THAT HAD NUMEROUS DRILL MARKS AND MISDRILLED HOLES. REPAIRED MAIN CARGO DOOR AFT JAMB STRUCTURE AND WEB AT STATION 280 THAT HAD NUMEROUS MISDRILLED HOLES IAW ABX REA D853-12582MR. 2L74 4F 4A25 19960405005371996040500537WP 1996 4 5 ABXA9600435 119951227A533056493283 SKIN DOUG DC8 DC863 302198AWP BS 1746-1766 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED SKIN BULGING AND CRACKS AROUND RIVET HEADS AT LONGERON 28L, STATION 1746 TO 1766. REPAIRED FUSELAGE SKIN IAW ABX REA D853-12584MR. 2L74 4F 4A25 19960405005381996040500538WP 1996 4 5 ABXA9600436 119951227A531156119433 FRAME DOUG DC8 DC863 302198AWP BS 70 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED PRODUCTION SPLICE FRAME AT STATION 70 FORWARD SIDE CORRODED. ALSO, LONGERON END FITTING AT LONGERON 32R CORRODED. REPAIRED FUSELAGE STATION 70 LOWER FORWARD FRAME AND END FITTING IAW ABX REA D853-12580MR. 2L74 4F 4A25 19960405005571996040500557NE 1996 4 5 DL72W960701 219951107A7250 TURB BLADES BOEING727 7272Q8 138407WNM PWA JT8 JT8D15A 52051NE NR 3 ENGINE FAILED A DALAE ENGINE SHUTDOWN X ENGINE FLAMEOUT TOTAKEOFF 1 SO27831L 21826 700235 ON ENGINE DISASSY, FOUND ALL 4TH STG TURB BLADES FRACTURED NEAR PLATFORM. UNKNOWN BMOD/FOD NOTED ON 3RD STG TURB BLADE LEADING EDGES. EVIDENCE SUGGESTS THAT THE OBJECT(S) CAUSING THIS DAMAGE, ALSO CAUSED THE 4TH STAGE BLADE FRACTURE. 2L73 4F4 F A3WE E2EA 19960405006031996040500603EU 1996 4 5 95UAL900349 119951227A4900 APU SUNSTRAND AIRBUS320 A320232 3930326EU APU COMPT SMOKING A UALAD RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP29410UA 1025 463 SMOKE IN CABIN AFTER ENGINE START, RETURNED TO GATE. REPLACED APU AND OPERATIONALLY CHECKED NORMAL WITH NO ODOR IN CABIN. 2L72 4F RTA28NM 19960405006701996040500670 1996 4 5 96ZZZX1547 419950116A6122G210659 GOVERNOR WOODWARD BNORM BN2MK3BN2AMK32 1520208EU RT ENGINE SHAFT FAILED A AVLIAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 SO21906GD2700 504 1444822K 1060 DURING CRUISE FLIGHT, RIGHT ENGINE QUIT AND PROPELLER FEATHERED. RIGHT GOVERNOR REMOVED AND FOUND BROKEN SHAFT. GOVERNOR REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1H73 3O A29EU 19960405006861996040500686NM 1996 4 5 96ZZZM561 119950709A5312 BULKHEAD BOEING727 727228 NM BS 126.3 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, BULKHEAD HAS TWO CRACKS AT STATION 126.3 RIGHT JUST UNDER AFT STAIR ACTUATOR ATTACH FITTING. REMOVED FASTENERS FROM INBOARD VERTICAL WEB ON RIGHT SIDE TORQUE BOX. REMOVED FASTENERS AND VERTICAL STIFFENER, CUT OUT CRACKED AREA OF WEB STATION 126.3. INSTALLED FILLER WITH NEW HARDWARE, REINSTALLED VERTICAL STIFFENER WITH NEW HARDWARE, REINSTALLED INBOARD VERTICAL WEB RIGHT SIDE OF TORQUE BOX WITH NEW FASTENERS, FILLER MADE OF 2024-T3 .040 1.5 INCH BY 3 INCH. ALODINED AND PRIMED PER SRM 51-10-2. 2L73 4F A3WE 19960405006871996040500687NM 1996 4 5 96ZZZM562 119950709A5720 WING TIP WEB BOEING727 727228 NM RT WING CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, HEAVY CORROSION ON WEB INTERIOR OF WING TIP. CUT OUT DAMAGED AREAS WITH CORROSION OUT OF LIMITS PER SRM 51-40-2. CLEANED AREA PER SRM 51-10-6. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED DOUBLER 2024-T3 .040 7.5 INCH BY 4 INCH. INSTALLED DOUBLER AT WEB AS PER SRM 51-40-2 AT WING TIP ASSY. 2L73 4F A3WE 19960405006881996040500688NM 1996 4 5 96ZZZM563 119950709A5330 SKIN BOEING727 727228 NM BS 1183-1203 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, STATION 1183 TO 1203 BETWEEN STRINGER 25R AND 24R, HAS DENT FILLED WITH BONDO AND HAS A GOUGE JUST AFT OF 1183 BUTT SEAM. REMOVED FILLER MATERIAL PER SRM 51-40-1. FOUND DENT TO BE BEYOND LIMITS PER SRM 53-30-1. CUT OUT DAMAGED AREA AS PER SRM 53-30-3. FABRICATED DOUBLER .080 2024-T3 20 INCH BY 11 INCH PER SRM 53-30-3. INSTALLED DOUBLER PER SRM 53-30-3. 2L73 4F A3WE 19960405006891996040500689NM 1996 4 5 96ZZZM564 119950709A5313 STRINGER BOEING727 727228 NM BS 852 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN AT STATION 852 STRINGER 16L HAS CRACK IN STRINGER. INSTALLED NEW STRINGER PER SRM 51-10-1. 2L73 4F A3WE 19960405006901996040500690NM 1996 4 5 96ZZZM565 119950709A5320 SILL BOEING727 727228 NM AFT GALLEY DR CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, CORROSION UNDER FORWARD TO CENTER NUT PLATES OF INBOARD LOWER SILL ATTACH FLANGE AT RIGHT AFT GALLEY DOOR. REMOVED CORROSION, CORROSION BEYOND LIMIT, MADE TYPICAL ANGLE REPAIR PER SRM 51-40-3. CUT OUT DAMAGED AREA PER SRM 51-40-3. REPAIRED AND INSTALLED TYPICAL ANGLE REPAIR AS PER SRM 51-40-3. SIZE OF REPAIR 15 INCH BY 1 INCH BY 1 INCH MATERIAL USED 2024-T3. 2L73 4F A3WE 19960405006911996040500691NM 1996 4 5 96ZZZM566 119950709A5312 BULKHEAD BOEING727 727228 NM BS 1183 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, CORROSION AFT SIDE OF BS 1183 ABOVE NR 1 PYLON (2 INCH). REMOVED DOUBLER AND REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER SRM 51-10-2. FABRICATED NEW DOUBLER AND INSTALLED PER SRM 51-30-2 (2024-T3 .040 2.5 INCH BY 3 INCH). 2L73 4F A3WE 19960405006921996040500692NM 1996 4 5 96ZZZM567 119950709A5320 INTERCOSTAL BOEING727 727228 NM FS 290 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, NLG W/W LT SIDE FS 290 INTERCOSTAL WEB CRACKED TWO PLACES AROUND LIGHTENING HOLES. FABRICATED WEB LEFT SIDE FS 290 NLG W/W AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960405006931996040500693NM 1996 4 5 96ZZZM568 119950709A5320 INTERCOSTAL BOEING727 727228 NM BS 1070-1077 CRACKS A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FUSELAGE STATION 1070-1077 TWO EACH CRACKS AT INTERCOSTAL FASTENER STRINGER 6R. REMOVED INTERCOSTAL STATION 1070-1077 STRINGER 6R PER SRM 51-10-1 PAR 4 AND 51-30-2. FABRICATED INTERCOSTAL PER SRM 51-10-1 PAR 4. INSTALLED INTERCOSTAL PER SRM 51-10-1 PAR 4 AND 51-30-1. 2L73 4F A3WE 19960405006941996040500694NM 1996 4 5 96ZZZM569 119950709A5311 FRAME BOEING727 727228 NM BS 1166 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FUSELAGE FRAME 1166 STRINGER 17R HEAVY CORROSION. REMOVED FASTENERS AS PER SRM 51-30-2. CUT OUT DAMAGE AREA AS PER SRM 51-40-3. FABRICATED FRAME REPAIR AS PER SRM 51-40-3 MATERIAL 7075-T6 ,090 11 INCH BY 1 INCH BY 9 INCH FILLER 7075-T6 .100 11 INCH BY 1 INCH BY 19 INCH DOUBLER. INSTALLED FRAME REPAIR AS PER SRM 51-40-3. 2L73 4F A3WE 19960405006951996040500695NM 1996 4 5 96ZZZM570 119950709A5230 BRACKET BOEING727 727228 NM CARGO DOOR CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, LOWER CARGO DOOR NR 2 AFT VERTICAL SUPPORT BRACKET FOR EXTERNAL DOOR HANDLE IS CORRODED AT BOTTOM. REMOVED FASTENERS ON VERTICAL SUPPORT BRACKET PER SRM 51-30-2. REMOVED CORRODED VERTICAL SPACER AND FABRICATED 2024-T3 .050 5 INCH BY 5 INCH PER SRM 51-10-1 PAR 4. ALODINE AND PRIMED SPACER PER SRM 51-10-2. INSTALLED WITH NEW FASTENERS PER SRM 51-30-2. 2L73 4F A3WE 19960405006961996040500696NM 1996 4 5 96ZZZM571 119950709A5330 PLATE BOEING727 727228 NM BS 1180 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN STATION 1180 LBL 30, DITCHING PLATE IS CRACKED. STOP DRILLED AT THE END OF CRACK PER SRM 51-10-1. FABRICATED DOUBLER REPAIR 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER AS PER SRM 51-40-2. 2L73 4F A3WE 19960405006971996040500697NM 1996 4 5 96ZZZM572 119950709A5330 PLATE BOEING727 727228 NM BS 1180 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN STATION 1180 LBL 27, DITCHING PLATE CRACKED. STOP DRILLED AT THE END OF CRACK PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 4 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2. 2L73 4F A3WE 19960405006981996040500698NM 1996 4 5 96ZZZM573 119950709A5530 T-ANGLE BOEING727 727228 NM VERT STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, EMPANNAGE, T-ANGLE CRACKED AT FORWARD SIDE OF VERTICAL STABILIZER FORWARD SPAR (L/E PANEL NR 9707 ATTACH ANGLE) AT LEFT SIDE UPPER END, JUST OUTBOARD OF LEFT VERTICAL FIN UPPER TERMINAL FITTING. REMOVED T-ANGLE FOR REPAIR. STOPPED DRILLED CRACK, FABRICATED ANGLE REPAIR 1 INCH BY 1 INCH BY 4 INCH AS PER SRM 51-40-4 7075-T6. TREATED AND PRIME AS PER SRM 51-10-2 AND 51-40-5. INSTALLED PER SRM 51-40-4. INSTALLED ANGLE REPAIR 1 INCH BY 1 INCH BY 7 INCH 7075-T6 PER SRM 51-40-4 AT FWD SPAR OF L/E PANEL 9707. 2L73 4F A3WE 19960405006991996040500699NM 1996 4 5 96ZZZM574 119950709A5530 ANGLE BOEING727 727228 NM VERT STAB CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, EMPANNAGE, LEADING PANEL NR 9707 FOR VERTICAL STABILIZER, HAS CRACKED ATTACHING ANGLE ON RIGHT SIDE OF VERTICAL STABILIZER FORWARD SPAR JUST OUTBOARD OF RIGHT VERTICAL FIN UPPER TERMINAL FITTING, AT UPPER END OF ANGLE. REMOVED T-ANGLE FOR REPAIR. CUT OUT CRACKED AREA. FABRICATED ANGLE REPAIR OUT OF 7075-T6 1 INCH BY 1 INCH BY 7 INCH AS PER SRM 51-40-4. TREATED AND PRIMED AS PER SRM 51-10-2 AND 51-40-5. INSTALLED ANGLE REPAIR AS PER SRM 51-40-4. 2L73 4F A3WE 19960405007001996040500700NM 1996 4 5 96ZZZM575 119950709A5330 SKIN BOEING727 727228 NM BS 1334-1346 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, LEFT VERTICAL EXTERNAL SKIN AT LBL 19 INSIDE TORQUE BOX IS HEAVILY CORRODED FROM BS 1334 TO BS 1346 AND S-10 TO LOWER TORQUE BOX CHORD ANGLE. REMOVED SURFACE CORROSION PER SRM 51-10-6. CUT OUT DAMAGED AREA PER SRM 55-30-3 AND ALODINE AND PRIMED PART PER SRM 51-10-2. FABRICATED 24 INCH BY 18 INCH .063 2024-T3 STRAPS DOUBLER 4 INCH BY 24 INCH AND 4 INCH BY 18 INCH .071 2024-T3. INSTALLED PARTS PER SRM 55-30-3. 2L73 4F A3WE 19960405007011996040500701NM 1996 4 5 96ZZZM576 119950709A5330 SKIN BOEING727 727228 NM BS 1342.4-1345 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, LEFT HORIZONTAL RIB INNER CHORD AND ADJACENT SKIN IS CORRODED FROM BS 1342.4 TO BS 1345. CUT OUT DAMAGED AREA OF SKIN 8 INCH BY 7 INCH .063, REMOVED FASTENERS, REMOVED CORROSION ON CHORD ANGLE, MATERIAL LOSS .004 AS PER SRM 51-10-6. ALODINED AND PRIMED AS PER SRM 51-10-2. INSTALLED WEB REPAIR AS PER SRM 51-40-2, MATERIAL USED 7075-T6 8 INCH BY 7 INCH .063 AND 7075-T6 .071 8 INCH BY 4 INCH WEB SPLICE. 2L73 4F A3WE 19960405007021996040500702NM 1996 4 5 96ZZZM577 119950709A5510 RIB BOEING727 727228 NM STA 1354 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, RIB LEFT SIDE STATION 1354 INSIDE TORQUE BOX LOWER SURFACE OF LOWER ANGLE HAS CORROSION ON HORIZ STAB. REMOVED CORROSION AS PER SRM 51-10-6 MATERIAL LOSS .005. INSTALLED ANGLE REPAIR 2024-T3 .063 2 INCH BY 10 INCH AS PER SRM 51-40-3. 2L73 4F A3WE 19960405007031996040500703NM 1996 4 5 96ZZZM578 119950709A5320 WEB BOEING727 727228 NM BS 760-783 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN WEB IS CORRODED AT UNDER SIDE STATION 760-783 LBL 68 INCHES. REPLACEMENT OF WEB AT STATION 760-783 LBL 68 INCHES 7075-T6 .071 AS PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960405007041996040500704NM 1996 4 5 96ZZZM579 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 745 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT STATION 745 LBL 65 INCHES. REMOVED FLOOR SUPPORT ANGLE PER SRM 51-30-2. INSTALLED NEW FLOOR ANGLE SUPPORT PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2, SIZE 107 INCHES BY 1.5 INCH BY 1.25 INCH BAC 1515-532 T-6 .071 INCH. 2L73 4F A3WE 19960405007051996040500705NM 1996 4 5 96ZZZM580 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 760-849 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT SEVERAL AREAS AT STATION 760-849 LBL 65 INCHES. REMOVED FLOOR SUPPORT ANGLE AS PER SRM 51-30-2. INSTALLED NEW FLOOR SUPPORT ANGLE AS PER SRM 51-10-1 PAGE 4 AND SRM 51-30-2. SIZE 107 INCH BY 1.25 INCH BY 1.25 INCH BAC 1515-532 T6 .071 INCH. 2L73 4F A3WE 19960405007061996040500706NM 1996 4 5 96ZZZM581 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 923 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN FLOOR SUPPORT ANGLE IS CORRODED AT SPLICE AT STATION 923 RBL 65 INCHES. REPLACED ANGLE SPLICE PER SRM 51-10-1 AND SRM 51-30-2 AT STATION 923 RBL 65 INCHES. 2L73 4F A3WE 19960405007071996040500707NM 1996 4 5 96ZZZM582 119950709A5320 CHORD BOEING727 727228 NM BS 1176.9 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, CORROSION ON FLOOR REINFORCEMENT CHORD BOTTOM SIDE AT STATION 1176.9 LBL 37 INCH AND 48 INCH. REMOVED FASTENERS AND CHORD ANGLE AT STATION 1176.9 PER SRM 51-30-2. CUT OUT FLOOR LBL 26 INCH, CORROSION BEYOND LIMITS 20 INCH BY 15 INCH APPROX CLEANED AREA, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED DOUBLER 2024-T3 .050 24 INCH BY 18 INCH. INSTALLED FLOOR REPAIR PER SRM 51-40-2. 2L73 4F A3WE 19960405007081996040500708NM 1996 4 5 96ZZZM583 119950709A5320 ANGLE BOEING727 727228 NM BS 1176.9 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN FLOOR HAS CORROSION AN ANGLE AT STATION 1176.9 RBL 61-66. REMOVED FASTENERS AND CHORD ANGLE AT STATION 1176.9. FOUND CORROSION BEYOND LIMITS. CLEANED AREA AND PRIMED PER SRM 51-10-2. REPLACED CHORD ANGLE PER SRM 51-10-1 PAR 4. 2L73 4F A3WE 19960405007091996040500709NM 1996 4 5 96ZZZM584 119950709A5313 STRINGER BOEING727 727228 NM BS 420 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, STATION 420 AFT SIDE OF RIB STRINGER 3L HAS CORROSION THROUGH STRINGER TOP FLANGE. CUT OUT DAMAGED SECTION AS PER SRM 53-10-3. INSTALLED 1 INCH BY .5 INCH REPAIR AS PER SRM 53-10-3 FIG 2 PART 1 10 INCH J-ANGLE BAC 1493-508. 2L73 4F A3WE 19960405007101996040500710NM 1996 4 5 96ZZZM585 119950709A5313 STRINGER BOEING727 727228 NM BS 460 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, JUST FORWARD OF STATION 460 STRINGER 3R HAS HEAVY CORROSION. REMOVED CORROSION FORWARD STATION 460 STRINGER 3R PER SRM 51-10-6, OUT OF LIMITS. INSTALLED STRINGER REPAIR PER SRM 53-10-3 7075-T6 .040 10 INCH BY 1 INCH BY 1 INCH. ALODINED AND PRIMED STRINGER 3R. 2L73 4F A3WE 19960405007111996040500711NM 1996 4 5 96ZZZM586 119950709A5320 DITCHING WEB BOEING727 727228 NM FS 1180 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH 20404 DURING D-CHECK, AFT BAGGAGE DITCHING WEB IS TORN AND CRACKED FS 1180 RBL 55. STOP DRILLED AT END OF CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER 2024-T3 .025 6 INCH BY 3 INCH. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2. 2L73 4F A3WE 19960405007121996040500712NM 1996 4 5 96ZZZM587 119950709A5311 FRAME BOEING727 727228 NM BS 930 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH 20404 DURING D-CHECK, MAIN CABIN FRAME CRACKED STATION 930 STRINGER 14R UNDER STUB FRAME SUPPORT FITTING. CRACK GOES FROM HOLE TO HOLE. FABRICATED PARTS PER STEP ONE ON DHL/BOEING FAX 95-14TR DATED MAY 26, 1995. OVERSIZE HOLES.03125 FRAME ONLY PER STEP TWO OF DHL/BOEING FAX 95-14TR DATE MAY 26, 1995. INSTALLED DOUBLER REPAIR AS PER STEP ONE OF DHL/BOEING FAX 95-14TR DATED MAY 26, 1995. 2L73 4F A3WE 19960405007131996040500713NM 1996 4 5 96ZZZM588 119950709A5311 FRAME BOEING727 727228 NM STA 930 CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH 20404 DURING D-CHECK, MAIN CARGO LEFT FRAME CRACKED STATION 930 STRINGER 14-15L AT STUB FRAME ATTACHMENT FITTING. STOP DRILLED CRACK AS PER SRM 51-10-1. FABRICATED PARTS PER STEP ON OF DHL/BOEING FAX 95 14TR DATED MAY 26, 1995. INSTALLED REPAIR PARTS PER DHL FAC 95-0014TR AND SB 727-53-0162. 2L73 4F A3WE 19960405007141996040500714NM 1996 4 5 96ZZZM589 119950709A5330 SKIN BOEING727 727228 NM FS 1152 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FUSELAGE EXTERIOR SKIN DOUBLER REPAIR FS 1152 STRINGER 27L UPGRADE PER SRM. REMOVED DOUBLER. REMOVED CORROSION, FOUND GRINDOUT TO BE BEYOND LIMITS AS PER SRM 51-10-6. FILLED GRINDOUT PER SRM 51-40-1. FABRICATED .125 2024-T3 8 INCH BY 11 INCH DOUBLER PER SRM 53-30-3. INSTALLED DOUBLER PER SRM 53-30-3. 2L73 4F A3WE 19960405007151996040500715NM 1996 4 5 96ZZZM590 119950709A5321 FLOOR BOEING727 727228 NM FS 1176 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, MAIN CABIN FLOOR, CORROSION UNDER REINFORCEMENT CHORD AT FS 1176 RBL 20 BETWEEN SUB FLOOR AND CHORD. REMOVED FASTENERS AND REMOVED CHORD ANGLE AT STATION 1176.9 PER SRM 51-30-2. CUT OUT DAMAGED AREA OF SUB FLOOR 15 INCHES BY 20 INCHES AND CLEANED AREA. ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED FLOOR REPAIR 2024-T3 .050 18 INCHES BY 24 INCHES. INSTALLED REPAIR DOUBLER PER SRM 51-40-2 2024-T3 .050 18 INCHES BY 24 INCHES. 2L73 4F A3WE 19960405007161996040500716NM 1996 4 5 96ZZZM591 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM FS 283 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND COCKPIT FLOOR SUPPORT IS CRACKED FS 283 RBL 7. STOP DRILLED CRACK .25 INCH PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 FIG 1 8 INCHES 2024-T3 .050. 2L73 4F A3WE 19960405007171996040500717NM 1996 4 5 96ZZZM592 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM STA 1070 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND CRACK AND CORROSION BY NR 2 RIGHT SERVICE DOOR FLOOR SUPPORT BEAM STATION 1070 RRBL 57 TO 64. CRACK IS BOTTOM SIDE OF BEAM SUPPORT. CUT OUT CORRODED AREA AND STARTED FABRICATING REPAIR AS PER SRM 53-10-8. FABRICATED T-ANGLE OUT OF 7075-T73 22 INCHES LONG, STRAPS .080 AND .050 OUT OF 7075-T6 22 INCHES LONG, SUPPORT ANGLES .080 AND .050 OUT OF 7075-T73 AS PER SRM 53-10-8. INSTALLED REPAIR PER SRM 53-10-8. 2L73 4F A3WE 19960405007181996040500718NM 1996 4 5 96ZZZM593 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 1130 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND FLOOR SUPPORT BEAM HAS CORROSION AT STATION 1130 RCL 31-45. REMOVED CORROSION PER SRM 51-10-6. MATERIAL LOST .100 BEYOND LIMITS. FABRICATED ANGLES 7075-T6 .100 1 INCH BY 2O INCH. INSTALLED ANGLE REPAIR PER SRM 51-40-4. 2L73 4F A3WE 19960405007191996040500719NM 1996 4 5 96ZZZM594 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 950 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND NR 2 SEAT TRACK CHANNEL SUPPORT HAS BARE METAL AND SURFACE CORROSION AT STATION 950A-950B AND LCL 25. FABRICATED AND INSTALLED NEW SEAT TRACK ANGLE SUPPORT PER SRM 51-10-1 PAR 4 19.75 INCH BY .75 INCH BY .75 INCH 2024T-3 .040 ANGLE. 2L73 4F A3WE 19960405007201996040500720NM 1996 4 5 96ZZZM595 119950709A5315 FLOOR BEAM BOEING727 727228 NM BS 400 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND FLOOR BEAM STATION 400 TOP FLANGE BL 0 TO LBL 25 CORROSION. REMOVED CORROSION AS PER 51-10-6. OUT OF LIMITS SEVERAL SPOTS BETWEEN RBL 3 THROUGH LBL 33. ALODINE AND PRIME PER SRM 51-10-2. CUT UPPER CHORD OF FLOOR BEAM FROM RBL 5 THROUGH LBL 33 PER SRM 53-10-8. INSTALLED FLOOR BEAM REPAIR PER SRM 53-10-8 FROM RBL 3 TO LBL 33. 2L73 4F A3WE 19960405007211996040500721NM 1996 4 5 96ZZZM596 119950709A7110 SKIN BOEING727 727228 NM NR 2 ENG INLET CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, NR 2 ENGINE INLET INNER SKIN BULGE AND CRACKED JUST BELOW PRODUCTION JOINT 7 O'CLOCK. REMOVED FASTENERS PER SRM 51-30-2. REMOVED ALL DAMAGED AREA PER SRM 54-10-3. FABRICATED DOUBLER AND FILLER AS 7075-T6 (DOUBLER .050 AND FILLER .040) PER SRM 54-10-3. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED PER SRM 51-30-2. INSTALLED PER SRM 54-10-3 IN THE NR 2 ENGINE INLET INNER SKIN BULGED JUST BELOW PRODUCTION JOINT AT 7 O'CLOCK. 2L73 4F A3WE 19960405007221996040500722NM 1996 4 5 96ZZZM597 119950709A5400 S-DUCT BOEING727 727228 NM NR 2 ENG CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH 20404 DURING D-CHECK, FOUND NR 2 ENGINE INLET 'S' DUCT HAS INNER SKIN BULGE AT 6 O'CLOCK BETWEEN 10-21 INCH FORWARD OF LOWER AFT EDGE. REMOVED FASTENERS PER SRM 51-30-2. CLEANED CORROSION INNER SKIN PER SRM 51-10-6 MATERIAL LOSS .003. FOUND CRACK AT BETWEEN 10-21 INCH AT 6 O'CLOCK. CUT OUT DAMAGED AREA AS PER SRM 54-10-3. FABRICATED NEW FLUSH PATCH 7075-T6 16 INCH BY 5 INCH .050. INSTALLED NEW FLUSH PATCH AS PER SRM 54-10-3. 2L73 4F A3WE 19960405007231996040500723NM 1996 4 5 96ZZZM598 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 460/420 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND BETWEEN STATION 460 AND 420 FLOOR SUPPORT ANGLE RBL 10 HAS CORROSION. REMOVED FLOOR SUPPORT 400 TO 420 CORROSION EXCEED SRM LIMITS 51-10-6. FABRICATED NEW FLOOR SUPPORT ANGLE 20 INCH BY 2 INCH BY 2.5 INCH 7075 T-6 .125 PER SRM 51-40-3. REMOVED FLOOR SUPPORT 420 TO 440, CORROSION EXCEED SRM LIMITS 51-10-6. FABRICATED NEW FLOOR SUPPORT ANGLE 20 INCH BY 2 INCH BY 2.5 INCH 7075 T-6 .125 PER SRM 51-40-3. INSTALLED FLOOR SUPPORT PER SRM 51-10-1. 2L73 4F A3WE 19960405007241996040500724NM 1996 4 5 96ZZZM599 119950709A5320 ANGLE BOEING727 727228 NM BS 480/500 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND BETWEEN STATION 480 AND 500 LEFT SIDE ANGLE AT LBL 62, CORROSION. REMOVED CORROSION LEFT SIDE STATION 480 TO 460 .001 MATERIAL LOSS PER SRM 51-10-6. REMOVED 20 INCH 7075-T6 511 A200/U PER SRM 51-10-1 PAR 4. INSTALLED NEW ANGLE 20 INCH 7075-T6 511 A200/U PER SRM 51-40-3. 2L73 4F A3WE 19960405007251996040500725NM 1996 4 5 96ZZZM600 119950709A5320 FLOOR SUPPORT BOEING727 727228 NM BS 400 DAMAGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND STATION 400 FLOOR BEAM APPROX RBL 60 HAS HOLE IN TOP CHORD TO CLOSE TO EDGE, BAD E/D. CUT OUT DAMAGE SECTION UPPER CHORD PER SRM 53-108. INSTALLED UPPER FLOOR BEAM REPAIR PER SRM 53-10-8 3 INCH BY 8 INCH. 2L73 4F A3WE 19960405007261996040500726NM 1996 4 5 96ZZZM601 119950709A5315 FLOOR BEAM BOEING727 727228 NM BS 380 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FOUND FLOOR BEAM TOP FLANGE RBL 42 TO RBL 64 STATION 380 HAS CORROSION. CUT OUT DAMAGED AREA OF FLOOR BEAM BS 380 LBL 52 10 INCHES APPROX CLEANED AREA, NO MORE CORROSION FOUND. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED FLOOR BEAM REPAIR AS PER SRM 53-10-8. 2L73 4F A3WE 19960405007271996040500727NM 1996 4 5 96ZZZM602 119950709A5315 FLOOR BEAM BOEING727 727228 NM BS 716 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01727DH45615 20404 DURING D-CHECK, FORWARD CARGO COMPARTMENT FLOOR BEAMS HAVE ANCHOR NUTS CORRODED AND CORROSION UNDER ANCHOR NUTS FROM LEFT AND RIGHT LINER ATTACH WEB AT STATION 716. CUT DAMAGE AREA AS PER SRM 53-10-8 AND INSTALLED REPAIR AS PER SRM 53-10-8, 51-30-2 AND 51-40-3, SIZE 10 INCH BY 1 INCH 7075-T6. 2L73 4F A3WE 19960405007311996040500731EU 1996 4 5 96ZZZM606 119951115A3230SD3406016XA RETAINING PIN STBROSSD3 SD360 8100606EU LT MLG WORN A TRBAO OTHER J WARNING INDICATION LDLANDING 1 SO21360MQ23679 SH3602 NO DOWNLOCK INDICATION IN LEFT MAIN GEAR ON LANDING. REPAIRED, LEFT AND RIGHT SHEAR DECK. INSTALLED BUSHINGS IAW SHORTS REPAIR MANUAL. REPLACED RETAINING PIN. 2H72 4T A41EU 19960405007321996040500732EU 1996 4 5 96ZZZM607 119951201A32601HE2412 SWITCH STBROSSD3 SD360 8100606EU RT MLG INTERMITTENT A TRBAO OTHER N FALSE WARNING LDLANDING 1 SO21360MQ23708 SH3602 LANDING GEAR CYCLED TWICE BEFORE RIGHT MAIN WOULD INDICATE DOWN AND LOCKED. REMOVED AND REPLACED DOWN LOCK SWITCH. 2H72 4T A41EU 19960405007331996040500733EU 1996 4 5 96ZZZM608 119950127A5415S5421039420000 FITTING AEROSPATR42 ATR42300 8680920EU NR 2 ENGINE CRACKED AS TRBAK NONE O OTHER ININSP/MAINT 1 SO21973NA13534 065 DURING PHASE NR 4 INSPECTION, FOUND NR 2 ENGINE LEFT AFT LATERAL ENGINE MOUNT ATTACHMENT FITTING CRACKED WITH NO VIBRATION OR DISCREPANCY REPORTED DURING FLIGHT. MOUNT ATTACHMENT FITTING WAS REMOVED AND REPLACED. 2H72 4T RTA53EU 19960405007341996040500734EU 1996 4 5 96ZZZM609 119951109A3211D56801 BUSHING D22686040 AEROSPATR42 ATR42300 8680920EU RT MLG BROKEN A TRBAK NONE O OTHER ININSP/MAINT 1 SO21143DD7154 MN176 056 DURING RIGHT MAIN LANDING GEAR REPLACEMENT, FOUND INNER BUSHING ON LEG STRUCTURE TRUNNION DAMAGED WITH ONE SECTION MISSING ON THE OUTER BORDER. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR LEG STRUCTURE TRUNNION AS PER MAINTENANCE MANUAL. 2H72 4T RTA53EU 19960405007351996040500735EU 1996 4 5 96ZZZM610 119950703A5720MS2125007026 ATTACH BOLT AEROSPATR42 ATR42300 8680920EU WING FITTING LOOSE ASATRBAK NONE O OTHER ININSP/MAINT 1 SO21971NA8384 017 FUEL SEEPAGE FOUND AT LEFT REAR WING ATTACHMENT BOLT AT RIB NR 4 LOCATED AT LEFT AFT INSTALLATION FITTING. FOUND LEFT WING ATTACHMENT AFT FITTING BOLT LOOSE. NEW BOLT WAS INSTALLED AND AREA INSIDE THE FUEL TANK WAS SEALED AS PER STRUCTURAL REPAIR MANUAL CHAPTER 517120. 2H72 4T RTA53EU 19960405007371996040500737EU 1996 4 5 96ZZZM612 119951106A2822CM17MQ0010 FEED JET PUMP AEROSPATR42 ATR42300 8680920EU WING FUEL TANK CLOGGED ASATRBAO OTHER X ENGINE FLAMEOUT ININSP/MAINT 1 SO21140DD1822424776 009 AIRCRAFT REPORTED HEAVY FLUCTUATIONS ON ALL PARAMETERS OF ENGINE NR 1. AFTER REPLACING VARIOUS ENGINE FUEL AND IGNITION COMPONENTS, ENGINE FLAMED OUT DURING GROUND RUNUP. FOUND DRY PRC RESIDUE IN DROPLET FORM CLOGGED IN FEEDER TANK JET PUMP. BOTH AIRFRAME FEEDER JET PUMPS WERE REMOVED, CLEANED AND REINSTALLED. 2H72 4T RTA53EU 19960405007491996040500749EU 1996 4 5 96ZZZM624 119951003A2710 CONTROL CABLE BAG BAE146BAE146200A 1500266EU LT AILERON CORRODED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31610AW E2082 LEFT AILERON INTERCONNECT CABLE C2C-D IS CORRODED BEYOND MAINTENANCE MANUAL LIMITS, CABLE 63C AND 63B TURN BUCKLE HAS BARREL UNSAFETIED AND SLACKENED. REMOVED AND REPLACED LEFT AILERON INTERCONNECT CABLE IAW 146 MM 27-11-44 THROUGH STEP N6 PG 414. GENERATED W/C FOR COMPLETION. 2H74 4F RTA49EU 19960405007501996040500750EU 1996 4 5 96ZZZM625 119951016A3233104796004 ACTUATOR STBROSSD3 SD360 8100606EU LT MLG DAMAGED A TRBAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO21380MQ4879 DRG99290 SH3702 CREW REPORTED 'UNLOCK' INDICATION ON LEFT MAIN GEAR. GEARS WERE RECYCLED BUT PROBLEM PERSISTED. REMOVED AND REPLACED LEFT LANDING GEAR ACTUATOR AS PER COMPONENT MAINTENANCE MANUAL CHAPTER 3230. RETRACTION CHECK PERFORMED WITH SATISFACTORY RESULTS AS PER MAINTENANCE MANUAL CHAPTER 3200. (M) 2H72 4T A41EU 19960405007511996040500751EU 1996 4 5 96ZZZM626 119950404A32132009920604 GLAND NUT 200920003 STBROSSD3 SD360 8100606EU LANDING GEAR CRACKED A TRBAK NONE O OTHER ININSP/MAINT 1 SO21374MQ230948207 DRG155584 SH3683 DURING FLEET CAMPAIGN INSPECTION OF SHOCK ABSORBER GLAND NUT FOR CRACKS CORROSION, CRACK WAS FOUND ON NUT LOWER SECTION .25 INCH FROM THE RADIUS 1.5 INCH LONG. (PRC SEALEANT WAS MISSING SINCE LAST OVERHAUL). NUT WAS REPLACED BY NEW ONE, REST OF THE FLEED INSPECTION UNDER PROGRESS ON FLEET CAMPAIGN. 2H72 4T A41EU 19960405007521996040500752EU 1996 4 5 96ZZZM627 119951022A7603SD3476010KA POWER CABLE STBROSSD3 SD360 8100606EU RT ENGINE BROKEN A TRBAED ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 SO21377MQ167377602 SH3699 CAPTAIN SHUT OFF RIGHT ENGINE DURING TAXI DUE TO RIGHT ENGINE POWER CABLE BROKEN. REMOVED AND REPLACED RIGHT ENGINE POWER CABLE AS PER MAINTENANCE MANUAL CHAPTER 76-10. RUN UP PERFORMED WITH SATISFACTORY RESULTS AS PER MM CHAPTER 7200. 2H72 4T A41EU 19960405007531996040500753NE 1996 4 5 96ZZZM628 219951114A7230310468201 COMPRESSOR CASE STBROSSD3 SD360 8100606EU PWA PT6 PT6A65AR 52043NE LT ENG CORRODED A TRBAK NONE O OTHER ININSP/MAINT 1 SO21374MQ157021015 SH3683 97163 DURING DECONFORMITY INSPECTION, FOUND SEVERE COMPRESSOR INLET CASE FLANGE CORROSION AND EXFOLIATION. REMOVED AND REPLACED LEFT ENGINE AS PER MM CHAPTER 7200. 2H72 4T4 T A41EU E4EA 19960405008451996040500845NM 1996 4 5 PCAA9500266 119950801A5347 SEAT TRACK DHAV DHC8 DHC8102 2809003NM COCKPIT WORN A PCAAK NONE O OTHER ININSP/MAINT 1 EA13800MX19859 007 PILOTS AND CO-PILOTS SEAT RAILS WERE FOUND WORN WHILE PERFORMING TASK 2510/01. PERFORMED MODIFICATION 8/2168, INSTALLATION OF STAINLESS STEEL WEAR STRIPS. MODIFICATION WAS ACCOMPLISHED IAW DHC S/B 8-53-53. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960405008461996040500846NM 1996 4 5 PCAA9500270 119950811A534785320490 SEAT TRACK DHAV DHC8 DHC8102 2809003NM CABIN CORRODED A PCAAK NONE O OTHER ININSP/MAINT 1 EA13800MX1989621333 007 RIGHT FORWARD CABIN SEAT RAIL FOUND CORRODED BEYOND LIMITS WHERE GALLEY AND LAVATORY REST UPON IT. REMOVED AND REPLACED CABIN SEAT RAIL PART NR 85320490 IAW DEHAVILLAND DRAWING 85320019 AND STRUCTURAL REPAIR MANUAL PRACTICES. AIRCRAFT RETURNED TO SERVICE. (M) 2H72 4T RTA13NM 19960405009221996040500922WP 1996 4 5 ABXA9600438 119951227A5311 FRAME DOUG DC8 DC863 302198AWP FUSELAGE MISDRILLED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED FROM STATION 25 TO AFT PRESSURE BULKHEAD FRAMES GREATER THAN .100 INCH THICKNESS, HAVE NUMEROUS MISDRILLED HOLES. REPAIRED FUSELAGE FRAMES .080TO .125 INCH THICK THAT WERE MISDRILLED IAW ABX REA D853-12547MR. 2L74 4F 4A25 19960405009231996040500923WP 1996 4 5 ABXA9600439 119951227A5320 DOOR FRAME DOUG DC8 DC863 302198AWP R 1 DOOR DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED R-1 DOOR JAMB LOWER AFT CORNER, ANGLE CORRODED AND FRAME AND COVER DENTED. REPAIRED FRAME AT FUSELAGE STATION 200 RIGHT AT FLOOR LEVEL THAT WAS CORRODED AND COVER DENTED IAW ABX REA D853-12568MR. 2L74 4F 4A25 19960405009241996040500924WP 1996 4 5 ABXA9600440 119951227A5751 RIB DOUG DC8 DC863 302198AWP LT AILERON CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LEFT HAND INBOARD AILERON, LIGHTING HOLE COVER, FRAME AND BULKHEAD WORN, CRACKED AND BROKEN. REPAIRED END RIB, LEFT HAND INBOARD AILERON, LIGHTING HOLE COVER THAT WAS WORN, CRACKED AND BROKEN IAW ABX REA D857-12485. 2L74 4F 4A25 19960412000011996041200001NE 1996 4 12 96ZZZX1563 219951124A7230430135703 SEAL BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE O OTHER ININSP/MAINT 1 NM0717SJ 813 665 7230 LE45756EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19960412000021996041200002NE 1996 4 12 96ZZZX1564 219951124A7250411100720 SHROUD LEARSIEGLER BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE GAS PROD BLADE RUB A R7MAK NONE O OTHER ININSP/MAINT 1 NM0717SJ 813 097E 7230 LE45756EF EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19960412000081996041200008NE 1996 4 12 96ZZZX1570 219951229A7250414129001 ROTOR ASSY BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BY683 70 SC17095 7127 LE45134E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 2 PLUS 0.013 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 979.4. 1G72 3U3 U H13EU E5NE 19960412000091996041200009NE 1996 4 12 96ZZZX1571 219951229A7250430144801 SEAL BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07911BY156 0129070 7127 LE45134E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000101996041200010NE 1996 4 12 96ZZZX1572 219951018A7250411105056 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE GAS PROD CRACKS A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 1333 90A031 7231 LE45807F DUE SB LT101-72-10-0150. REQUIRES DISASSEMBLY AND INSPECTION OF THE ROTOR BROACH SLOTS FOR POSSIBLE CRACKS IN THE DISC/TENON AREA. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 2,641.6. 1G72 3U3 U H13EU E5NE10 19960412000111996041200011NE 1996 4 12 96ZZZX1573 219950518A7230430135703 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07428MB745 703 7088 LE45033E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000121996041200012NE 1996 4 12 96ZZZX1574 219950518A7250430144801 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07428MB745 0492587 7088 LE45033E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000131996041200013NE 1996 4 12 96ZZZX1575 219951129A725041016701 SEAL RING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE 1ST TURB SHROUD WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07158BK 7058 LE45166E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000141996041200014NE 1996 4 12 96ZZZX1576 219951129A7230430135703 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07158BK86 745 7058 LE45166E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000151996041200015NE 1996 4 12 96ZZZX1577 219950712A7250410106701 SEAL RING BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE 1ST TURB SHROUD WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07586BH386 7129 LE45254E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. (X) 1G72 3U3 U H13EU E5NE 19960412000161996041200016NE 1996 4 12 96ZZZX1578 219950712A7230430125302 BEARING BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE COMP WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07586BH567 7129 LE45254E BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000171996041200017NE 1996 4 12 96ZZZX1579 219950712A7230430135703 SEAL BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07586BH567 465 7129 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000181996041200018NE 1996 4 12 96ZZZX1580 219950712A7250430144801 SEAL BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07586BH567 1290744 7129 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000191996041200019NE 1996 4 12 96ZZZX1581 219950712A7250430144801 SEAL BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07586BH567 1290744 7129 LE45254E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000201996041200020SW 1996 4 12 96ZZZX1582 119951226A7712222375020103 INDICATOR BELL 222 222 1182122SW TRIPLE TORQUE INOPERATIVE A R7MAK NONE W INADEQUATE Q C ININSP/MAINT 1 NM0730SV 47044 INDICATOR UNIT INOPERATIVE ON INSTALL. NR 1 INDICATOR NEEDLE STUCK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H9SW 19960412000231996041200023NE 1996 4 12 96ZZZX1585 219951106A7250411105056 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE GAS PRODUCER DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 7231 LE45806F DUE SB LT101-72-10-0150. REQUIRES DISASSEMBLY AND INSPECTION OF THE ROTOR BROACH SLOTS FOR POSSIBLE CRACKS IN THE DISC/TENON AREA. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19960412000241996041200024NE 1996 4 12 96ZZZX1586 219951116A7250430144801 SEAL BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM077059N209 RE8I940632 7154 LE45540EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19960412000251996041200025NE 1996 4 12 96ZZZX1587 219951116A7230430135703 SEAL BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM077059N209 388 7154 LE45540EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE10 19960412000321996041200032EU 1996 4 12 96ZZZX1594 119951027A62201051410157 BOLT BOLKMS117 BK117B1 5626012EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM075188B310 7163 M/R BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000331996041200033EU 1996 4 12 96ZZZX1595 119951027A62201051410157 BOLT BOLKMS117 BK117B1 5626012EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM075188B859 7163 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000341996041200034EU 1996 4 12 96ZZZX1596 119950710A62301051011305 BELLOWS BOLKMS117 BK117B1 5626012EU MAST TORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM075188B433 7163 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000351996041200035EU 1996 4 12 96ZZZX1597 119951028A6410134617P BUSHING BOLKMS117 BK117B1 5626012EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07417BK606 7143 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000361996041200036EU 1996 4 12 96ZZZX1598 119951028A6410134616P BUSHING BOLKMS117 BK117B1 5626012EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07417BK606 7143 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000371996041200037EU 1996 4 12 96ZZZX1599 119951028A64201053170018 BOLT BOLKMS117 BK117B1 5626012EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07417BK606 7143 FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000381996041200038EU 1996 4 12 96ZZZX1600 119950925A52101172428111 CATCHER BOLKMS117 BK117B1 5626012EU LT DOOR WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 7231 LEFT CATCHER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000391996041200039EU 1996 4 12 96ZZZX1601 119951204A642010531717 BOLT BOLKMS117 BK117B1 5626012EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 653 7231 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000401996041200040EU 1996 4 12 96ZZZX1602 119951205A64201053170023 BEARING BOLKMS117 BK117B1 5626012EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM0710UM 596 7231 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000411996041200041EU 1996 4 12 96ZZZX1603 119950711A5210T669503 STRIKER BOLKMS117 BK117B1 5626012EU DOOR WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM0771703491 7227 STRIKER WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000421996041200042EU 1996 4 12 96ZZZX1604 119950830A7712G555674 TRANSDUCER BOLKMS117 BK117B1 5626012EU ENGINE TORQUE ERROR A R7MAK NONE O OTHER ININSP/MAINT 1 NM077060G18 269 7173 INACCURATE READINGS. REPLACED WITH NEW TRANSDUCER UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412000431996041200043EU 1996 4 12 96ZZZX1605 119950920A62201051410110 BOLT BOLKMS117 BK117B1 5626012EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM075194C635 7169 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRRECTED PROBLEM. 1G72 3U H13EU 19960412000441996041200044EU 1996 4 12 96ZZZX1606 119950624A7931DK040 TRANSMITTER BOLKMS105 BO105CBS 5626008EU NR 1 ENGINE OIL READS HIGH A R7MAK NONE O OTHER ININSP/MAINT 1 NM07105NC484 7101 790 NR 1 ENGINE OIL PRESSURE INDICATES HIGH. REPLACED WITH NEW TRANSMITTER UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960412000451996041200045EU 1996 4 12 96ZZZX1607 119950823A2840DK042 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL SYSTEM READS HIGH A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB69 10761 S754 HIGH PRESSURE READINGS. REPLACED WITH NEW UNIT, CORRECTED UNIT. 1G72 3U H3EU 19960412000461996041200046EU 1996 4 12 96ZZZX1608 119950728A2840DK042 TRANSMITTER BOLKMS105 BO105S 5626006EU FUEL SYSTEM READS HIGH A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB734 10756 S754 HIGH PRESSURE READINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000471996041200047EU 1996 4 12 96ZZZX1609 119950904A7931DK040 TRANSMITTER BOLKMS105 BO105S 5626006EU ENGINE OIL HIGH READING A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB490 7231 S754 HIGH RPESSURE READINGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000481996041200048EU 1996 4 12 96ZZZX1610 119950726A7931DK040 TRANSMITTER BOLKMS105 BO105S 5626006EU ENG OIL ERROR A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB151 7067 S754 PRESSURE INDICATED IN YELLOW BAND ON GROUND AND WHILE IN CRUISE FLIGHT. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000491996041200049EU 1996 4 12 96ZZZX1611 119951024A64201053170023 BEARING BOLKMS105 BO105S 5626006EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB154 S754 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000501996041200050EU 1996 4 12 96ZZZX1612 119950803A64201053170023 BEARING BOLKMS105 BO105S 5626006EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB297 S754 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000511996041200051EU 1996 4 12 96ZZZX1613 119951024A64201053170018 BOLT BOLKMS105 BO105S 5626006EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07722MB607 S754 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H3EU 19960412000521996041200052NE 1996 4 12 96ZZZX1614 219951112A7250414129001 ROTOR ASSY BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BY2518 86 SC04245 7127 LE45134E ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000531996041200053NM 1996 4 12 96ZZZX1615 119951209A7931900P3650009101 SENSOR DOUG MD900 MD900 3027375NM EGINE OIL DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM07901CF248 46133324 90000012 SENSOR UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960412000541996041200054NE 1996 4 12 96ZZZX1616 219951005A7250410106701 SEAL RING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE 1ST TURB SHROUD WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07127HH538 7060 LE45083E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000551996041200055NE 1996 4 12 96ZZZX1617 219950531A7250430144801 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07202HN531 11902397 7115 LE45071 SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000561996041200056NE 1996 4 12 96ZZZX1618 219950531A7230430135703 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM07202HN531 825 7115 LE45071 SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000571996041200057NE 1996 4 12 96ZZZX1619 219950531A7250410106701 SEAL RING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE 1ST TURB SHROUD WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07202HN531 7115 LE45071 SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960412000581996041200058NE 1996 4 12 96ZZZX1620 219950531A7250414129001 ROTOR ASSY BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM07202HN2241 1714 SC12199 7115 LE45071 ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 15 PLUS 0.0105 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 5749.2. 1G72 3U3 U H13EU E5NE 19960412000591996041200059NE 1996 4 12 96ZZZX1621 219951124A7250414129001 ROTOR ASSY BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE POWER TURBINE BLADE SHIFT A R7MAK NONE O OTHER ININSP/MAINT 1 NM0717SJ 1180 SC14540 7230 LE45756EF ROTOR ASSY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 10 PLUS 0.024 INCH, NR 11 PLUS 0.012 INCH. REPLACED WTIH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 2410.2. 1G72 3U3 U H13EU E5NE10 19960412000761996041200076WP 1996 4 12 ABXA9600442 119951227A532056138595 THRESHOLD DOUG DC8 DC863 302198AWP FWD ENTRY DOOR CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LEFT FWD ENTRY DOOR THRESHOLD AREA HAS CORRODED FASTENERS AND DOUBLE DRILLED HOLES. REPAIRED LEFT FORWARD ENTRY DOOR THRESHOLD/SILL THAT WAS CORRODED AND HAD DOUBLE DRILLED HOLES IAW ABX REA D853-12484MR. 2L74 4F 4A25 19960412000771996041200077WP 1996 4 12 ABXA9600443 119951227A5313 LONGERONS DOUG DC8 DC863 302198AWP BS 130-270 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 130 TO 270, LONGERON 16L TO 23L MAIN CARGO DOOR CUTOUT BOTTOM SECTION FUSELAGE SKIN HAS CRACKS, GOUGED, DENTS AND QUESTIONABLE REPAIRS. REPAIRED MAIN CARGO DOOR AT STATION 130 TO 270, LONGERON 16L TO 23L, BOTTOM SECTION OF FUSELAGE SKIN THAT WAS CRACKED, GOUGED AND DENTED IAW ABX REA D853-12483MR. 2L74 4F 4A25 19960412000781996041200078WP 1996 4 12 ABXA9600444 119951227A25505704461 BARRIER DOOR DOUG DC8 DC863 302198AWP AFT PIT CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED THAT THE AFT ACCESSORY COMPARTMENT DOOR WAS CRACKED AT BOTH LEFT HAND AND RIGHT HAND SIDES. REPAIRED AFT LOWER PIT, AFT BARRIER COMPARTMENT DOOR THAT WAS CRACKED ON BOTH LEFT HAND AND RIGHT HAND SIDES IAW ABX REA D853-12475MR. 2L74 4F 4A25 19960412000791996041200079WP 1996 4 12 ABXA9600445 119951227A5313 LONGERON DOUG DC8 DC863 302198AWP BS 1070-1085 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LONGERON 27L WAS CORRODED AT STATION 1070 TO 1085 AT AFT CARGO PIT. REPAIRED CORRODED LONGERON 27L AT STATION 1070 TO 1085 IAW ABX REA D853-12471MR. 2L74 4F 4A25 19960412000801996041200080WP 1996 4 12 ABXA9600446 119951227A5330 SKIN DOUG DC8 DC863 302198AWP BS 1400 CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED AT STATION 1400, LONGERON 29R TO 33R, C-4 DOOR CUTOUT HAS CRACKS. REPAIRED LOWER FUSELAGE EXTERIOR SKIN AT C-4 DOOR, STATION 1400, LONGERON 29R TO 33R IAW ABX REA D853-12449MR. 2L74 4F 4A25 19960412003651996041200365WP 1996 4 12 9522269750 119951228A5240 SKIN DOUG DC9 DC941 302207NWP DOOR CUTOUT CRACKED A NWAAK NONE O OTHER ININSP/MAINT 1 GL01750NW 47114 DURING LINE CHECK, FOUND A 1.7 INCH CRACK IN THE FORWARD SERVICE DOOR EXTERNAL SKIN LOWER AFT CORNER. REPAIRED SKIN PER EA 97-103395. 2L72 4F A6WE 19960412004101996041200410EU 1996 4 12 96ZZZX1658 119951108A622010513103505 BOLT BOLKMS117 BK117A4 5626017EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07117CW299 181005 7125 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004111996041200411EU 1996 4 12 96ZZZX1659 119951108A622010513103505 BOLT BOLKMS117 BK117A4 5626017EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07117CW120 181529 7125 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004121996041200412EU 1996 4 12 96ZZZX1660 119950916A6420ABWT82008 BEARING BOLKMS117 BK117A3 5626015EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07117NY251 7110 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004131996041200413EU 1996 4 12 96ZZZX1661 119951120A671010513142 ROD END BOLKMS117 BK117A3 5626015EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07127HH431 7060 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004141996041200414EU 1996 4 12 96ZZZX1662 119950601A622010513103505 BOLT BOLKMS117 BK117A1 5626010EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07128HH398 18588 7036 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004151996041200415EU 1996 4 12 96ZZZX1663 119950730A334011796135 LIGHT GRIMES BOLKMS117 BK117A1 5626010EU ANTI COLL INOPERATIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM07128HH85 7036 ANTI-COLLISION LIGHT UNIT INOPERATIVE. REPLACED WTIH NEW UNIT FROM GRIMES, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004161996041200416EU 1996 4 12 96ZZZX1664 119951101A64201053170018 BOLT BOLKMS117 BK117A3 5626015EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07202HN295 7115 FITTED BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004171996041200417EU 1996 4 12 96ZZZX1665 119950606A62101051585403 BUSHING BOLKMS117 BK117A3 5626015EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07424MB58 7082 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 8 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004181996041200418EU 1996 4 12 96ZZZX1666 119950623A642010531717 BOLT BOLKMS117 BK117A3 5626015EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07424MB130 7082 BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004191996041200419EU 1996 4 12 96ZZZX1667 119950707A62301051011305 BELLOWS BOLKMS117 BK117A3 5626015EU MAST TORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07428MB422 7088 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004201996041200420EU 1996 4 12 96ZZZX1668 119950810A64201053170023 BEARING BOLKMS117 BK117A3 5626015EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07527SF355 7111 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004211996041200421EU 1996 4 12 96ZZZX1669 119950810A2930APT10010002030SGTRANSDUCER BOLKMS117 BK117A4 5626017EU HYD SYSTEM SHORTED A R7MAK NONE O OTHER ININSP/MAINT 1 NM07586BH11 45472257 7129 TRANSDUCER HAS INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004221996041200422EU 1996 4 12 96ZZZX1670 119951130A62201051310114 SHIM BOLKMS117 BK117A4 5626017EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07586BH420 7129 SHIM WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004231996041200423EU 1996 4 12 96ZZZX1671 119951026A561004011340990 WINDOW SNIAS 350 AS350B2 8680813EU RT SLIDER CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM076099P326 2818 SLIDING WINDOW CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004241996041200424EU 1996 4 12 96ZZZX1672 119951128A6710CN6MEGR ROD END SNIAS 350 AS350B2 8680813EU M/R BEARING WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM076099P392 2818 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004251996041200425EU 1996 4 12 96ZZZX1673 119951109A6320704A34621004 OIL FILTER SNIAS 350 AS350B2 8680813EU M/R TRANSMISSIONLEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM076099P343 2818 OIL FILTER LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004261996041200426NE 1996 4 12 96ZZZX1674 219951228A7310571712A BYPASS VALVE SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE FUEL DEFECTIVE A R7MAK NONE N FALSE WARNING ININSP/MAINT 1 NM076099P458 2818 BYPASS VALVE CAUSES FALSE FILTER CLOG INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U3 U H9EU E19EU 19960412004271996041200427EU 1996 4 12 96ZZZX1675 119950914A334031031 LIGHT SNIAS 350 AS350B2 8680813EU GREEN SIDE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM076099P217 2818 WORN BEYOND SERVICEABLE LIMITS. BULB FITS LOOSE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004291996041200429EU 1996 4 12 96ZZZX1677 119951127A6410704A33633171 HINGE SNIAS 350 AS350B2 8680813EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM076099P392 2818 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004301996041200430EU 1996 4 12 96ZZZX1678 119950922A6220117775P BALL JOINT SNIAS 350 AS350B2 8680813EU STARFLEX WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM0793LG 606 2654 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004321996041200432EU 1996 4 12 96ZZZX1680 119951214A7931642790041 TRANSMITTER SNIAS 350 AS350B2 8680813EU ENGINE OIL DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM0796LG 374 2817 ENGINE OIL PRESSURE READS .5 TO .75 HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412004331996041200433EU 1996 4 12 96ZZZX1681 119950730A62301051011305 BELLOWS BOLKMS117 BK117A4 5626017EU MAST TORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BY299 7127 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004341996041200434EU 1996 4 12 96ZZZX1682 119950828A64201053170023 BEARING BOLKMS117 BK117A4 5626017EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BY280 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004351996041200435EU 1996 4 12 96ZZZX1683 119951204A2840DK042 TRANSMITTER BOLKMS105 BO105CBS 5626008EU FUEL SYSTEM DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BH206 10773 685 INDICATES PRESSURE TOO HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960412004361996041200436EU 1996 4 12 96ZZZX1684 119950904A62301051011305 BELLOWS BOLKMS105 BO105CBS 5626008EU MAST TORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911BH496 685 BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960412004371996041200437EU 1996 4 12 96ZZZX1685 119950609A33402LA00162500 LIGHT BOLKMS117 BK117B1 5626012EU TAIL DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM07911VU215 7141 LIGHT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960412004381996041200438EU 1996 4 12 96ZZZX1686 119951117A561004011340990 WINDOW SNIAS 350 AS350B2 8680813EU RT SLIDER CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM0796LG 2817 SLIDING WINDOW CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960412006151996041200615EU 1996 4 12 UF6A951204 119951223A3250JD325J0033002 CONTROL CABLE BAG ATP ATP EU NLG STEERING FAILED A AUF6AD RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 GL31856AW8525 2032 SBN - NOSE WHEEL STEERING FAILED, FOUND STEERING CABLE BROKEN. MAINTENANCE REMOVED AND REPLACED CABLE. (M) 2L72 4T RTA27NM 19960412006161996041200616EU 1996 4 12 UF6A951205 119951225A3250JD325J0033002 CONTROL CABLE BAG ATP ATP EU NLG STEERING FRAYED A UF6AK NONE O OTHER ININSP/MAINT 1 GL31851AW9945 2020 SBN - NOSE WHEEL STEERING CABLE FRAYED. MAINTENANCE REMOVED AND REPLACED CABLE. (M) 2L72 4T RTA27NM 19960412006171996041200617EU 1996 4 12 UF6A951206 119951224A30407CZ1068008 CONTROLLER BAG ATP ATP EU RT WINDSHIELD FAILED A UF6AA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL31856AW8532 2032 CWA - FLT NR 5032 - RIGHT WINDSCREEN HEAT OVERHEATED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED WINDSHIELD CONTROLLER. (M) 2L72 4T RTA27NM 19960418000131996041800013WP 1996 4 18 ABXA9600450 119951227A5330 SKIN DOUG DC8 DC863 302198AWP BS 360 MISREPAIRED A ABXAK NONE W INADEQUATE Q C ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 360, LONGERON 27R-29R, BOTH REPAIRS HAVE NO FINGER DOUBLERS. REPAIRED FUSELAGE SKIN AT FUSELAGE STATION 360, LONGERON 27R-29R, THAT HAD NO FINGER DOUBLERS IAW ABX REA D853-12442MR. 2L74 4F 4A25 19960418000141996041800014WP 1996 4 18 ABXA9600451 119951227A53309754028501 SKIN DOUG DC8 DC863 302198AWP BS 340 GOUGED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R FUSELAGE SKIN, STATION 180 LONGEON 25R C1 DOOR AFT BOTTOM CUTOUT HAS GOUGE. REPAIRED FUSELAGE SKIN AT STATION 340, LONGERON 31R, LONGERON 24R-25R, LONGERON 27R AND STATION 180, LONGERON 25R IAW ABX REA D853-12441MR. 2L74 4F 4A25 19960418000151996041800015WP 1996 4 18 ABXA9600452 119951227A5311 FRAME DOUG DC8 DC863 302198AWP BS 460 CORRODED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME AT STATION 460 BETWEEN LONGERON 27R AND LONGERON 25R HAS AREAS ON CORROSION. REPAIRED FUSELAGE STATION 460 FRAME SECTION, GUSSET PLATE AND VERTICAL FLOOR SUPPORT FRAME AT LONGERON 26R THAT HAS AREAS OF CORROSION IAW ABX REA D853-12361MR. 2L74 4F 4A25 19960418000161996041800016WP 1996 4 18 ABXA9600453 119951227A5311 FRAME DOUG DC8 DC863 302198AWP FUSELAGE CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED STATION 1580 AT APPROXIMATELY LONGERON 8L, FROM STATION 25 TO AFT PRESSURE BULKHEAD, STATION 1580 AT CUSP AREA FRAMES OF .100 INCH THICKNESS OR LESS, HAVE NUMEROUS DRILLED HOLES, FRAME END IS CRACKED AND CORRODED. REPAIRED FUSELAGE FRAMES LESS THAN .080 INCH THICK AT STATIONS 25 TO AFT PRESSURE BULKHEAD, STATION 1580 AT CUSP AREA, AND STATION 1580, LONGERON 8L, IAW ABX REA D853-12348MR. 2L74 4F 4A25 19960418000171996041800017WP 1996 4 18 ABXA9600454 119951227A5311 FRAME DOUG DC8 DC863 302198AWP BS 1613 BENT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED L-2 DOOR JAMB LOWER TORQUE BOX FRAME IS BENT AT FUSELAGE STATION 1613. REPAIRED FUSELAGE STATION 1613 FRAME ON L-2 DOOR THAT WAS BENT IAW ABX REA D853-12374MR. 2L74 4F 4A25 19960418000951996041800095WP 1996 4 18 ABXA9600458 119951227A5320 DOOR JAMB DOUG DC8 DC863 302198AWP BS 1620 BENT A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED R-2 DOOR JAMB LOWER FOWARD CORNER AT FUSELAGE STATION 1620, STRUCTURE IS BENT. REPAIRED R-2 DOOR JAMB FORWARD CORNER FRAME AT FUSELAGE STATION 1620 THAT WAS BENT IAW ABX REA D853-12345MR. 2L74 4F 4A25 19960418000961996041800096WP 1996 4 18 ABXA9600459 119951227A552056550151 TIP CAP DOUG DC8 DC863 302198AWP LT ELEVATOR DENTED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LEFT HAND ELEVATOR OUTBOARD TIP CAP DENTED. REPAIRED LEFT HAND ELEVATOR OUTBOARD TIP CAP THAT WAS DENTED IAW ABX REA D853-12346MR. 2L74 4F 4A25 19960418000971996041800097WP 1996 4 18 ABXA9600460 119951227A5753 HINGE FITTING DOUG DC8 DC863 302198AWP LT TE FLAP CHAFED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23826AX 46061 DURING 826AX MOD, DISCOVERED LEFT HAND INBOARD FLAP INBOARD HINGE ARM CHAFED. REPAIRED HINGE FITTING ON INBOARD FLAP, INBOARD HINGE THAT WAS CHAFED IAW ABX REA D857-12329MR. 2L74 4F 4A25 19960418001021996041800102NM 1996 4 18 96ZZZX1734 119951004A5730 SKIN BOEING727 727225 1384077NM WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, WING LEADING EDGE CUT-OUT FOR THE NR 7 SLAT OUTBOARD HOOK FOUND CRACKED AT THE AFT OUTBOARD CORNER. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 57-30-4 FROM 301 1/2 HARD 7.5 INCH BY 7.5 INCH DOUBLER. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001031996041800103NM 1996 4 18 96ZZZX1735 119951004A5730 SKIN BOEING727 727225 1384077NM WING LE CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, NR 3 SLAT OUTBOARD SLAT HOOK WING LEADING EDGE CUT-OUT FOUND CRACKED AT AFT END. STOP DRILLED CRACK PER SRM 51-10-1. INSTALL DOUBLER REPAIR LEADING EDGE CUT-OUT PER SRM 57-30-4. SIZE OF REPAIR 6 INCHES BY 5 INCHES. MATERIAL USED 0.020 INCH CRES AISI 301 1/2 HARD, 0.063 INCH CLAD 2024-T3 AND 0.032 INCH CRES AISI 301 1/2 HARD. TAT: 45,788.3. TAC: 29,959. 2L73 4F A3WE 19960418001041996041800104NM 1996 4 18 96ZZZX1736 119951004A5730 SKIN BOEING727 727225 1384077NM WING LE GAP A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FOUND THE WING LEADING EDGE CUT-OUT FOR THE NR 4 SLAT ACTUATOR HAS A LARGE GAP AT THE AFT END. FABRICATED DOUBLER 5.5 INCH BY 5.5 INCH 2024-T3 .080 INCH ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER AT WING L/E CUT-OUT NR 7 SLAT PER SRM 57-30-4 SEALED AREA PER MM 51-20-4. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001051996041800105NM 1996 4 18 96ZZZX1737 119951004A5730 SKIN BOEING727 727225 1384077NM WING LE CRACK A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, WING LEADING EDGE CUT-OUT FOR THE NR 6 SLAT OUTBOARD SLAT HOOK FOUND CRACKED AT THE AFT END. REMOVED ALL ATTACHING HARDWARE PER SRM 51-30-2. CUT FILLER STRIP PER SRM 57-30-4. STOP DRILLED CRACK PER SRM 51-10-1. ALODINE AND PRIMED PER SRM 51-10-2. FABRICATED REPAIR 6 INCHES BY 5 INCHES. MATERIAL USED 0.020 INCH CRES AISI 301 1/2 HARD 0.063 INCH CLAD 2024-T3 AND 0.032 INCH RES AISI 301 1/2 HARD PER SRM 57-30-4. INSTALLED REPAIR PER SRM 51-30-2. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001061996041800106NM 1996 4 18 96ZZZX1738 119951004A5330 SKIN BOEING727 727225 1384077NM BS 325 GOUGED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FUSE EXT SKIN STA 325 STR 18-STR 19R - 2 EA GOUGES/DENTS. BURNISH OUT GOUGES, FORWARD GOUGE BEYOND LIMITS. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER REPAIR 8 INCHES BY 9 INCHES .050 INCH PER SRM 51-40-1. SEALED EDGES AND TAILS PER 51-20-4. AFT GOUGE BURNISHED, WITHIN LIMITS. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001071996041800107NM 1996 4 18 96ZZZX1739 119951004A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, AFT LOWER CARGO DOOR AFT UPPER PRESSURE RELEASE, PREVIOUS STOP DRILL NEEDS REPAIR ON CUT-OUT. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 57-40-2, 4 INCHES BY 6 INCHES, .050 INCH 2024-T3. TAT: 45,788.3. TAC: 29,959. 2L73 4F A3WE 19960418001081996041800108NM 1996 4 18 96ZZZX1740 119951004A5230 SKIN BOEING727 727225 1384077NM CARGO DOOR GOUGE A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FORWARD CARGO DOOR EXT STA 604 AT BOTTOM - SMALL GOUGE. CUT OUT DAMAGE AREA PER SRM 53-30-3, FIGURE 13. FABRICATED DOUBLER AND INSTALLED REPAIR PER SRM 53-30-3, FIGURE 13. SIZE 4.25 INCH DIA .063 INCH 7075-T6. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001091996041800109NM 1996 4 18 96ZZZX1741 119951004A5320 DOOR FRAME BOEING727 727225 1384077NM BS 950 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING C-CHECK, LOWER AFT CARGO BENT FRAME STA 950, STR 26R. ROUTED OUT CRACK FOUND ON FRAME 950C, STR 26R, PER SRM 51-10-1. ALODINED AND PRIMED AREA PER SRM 51-10-6. FABRICATED AND INSTALLED FRAME REPAIR 11 INCHES BY 3.5 INCHES .071 7075-T6 PER SRM 53-10-4 AND SRM 51-30-2. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001101996041800110NM 1996 4 18 96ZZZX1742 119951004A5320 DOOR FRAME BOEING727 727225 1384077NM BS 950 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, LOWER AFT CARGO BENT FRAME STA 950 AT STR 26L. FABRICATED AND INSTALLED FRAME REPAIR PER SRM 53-10-4 AND SRM 51-30-2, 10 INCHES BY 3.5 INCHES, 7075-T6 .071 INCH. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001111996041800111NM 1996 4 18 96ZZZX1743 119951004A5320 SPLICE BOEING727 727225 1384077NM FS 680 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FORWARD BAGG COMPT - FS 680 STR 26L SPLICE HAS CORROSION FWD AND AFT OF CIRCUMFERENTIAL FRAME. REMOVED SPLICE PER SRM 53-10-3. MADE NEW SPLICE PER SRM 51-10-1 P.4 10 INCHES 7075-T6. INSTALLED SPLICE AT STA 680 STR 26L PER SRM 53-10-3 AND SRM SRM 51-30-2. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001121996041800112NM 1996 4 18 96ZZZX1744 119951004A5313 STRINGER BOEING727 727225 1384077NM BS 985-990 CORROSION A DHLAO OTHER O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, AFT B/B BS 985 - BS 990 STR 29R CORR LEVEL 2. REMOVED CORROSION ON STR 29R OUT OF LIMITS. ORIGINAL THICKNESS .185 INCH AFTER CORROSION REMOVAL THICKNESS .071 INCH AT LOWEST POINT PER SRM 51-10-6 BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER AVITAS PER NR 95 PMSI .075 INCH D-1, 3 INCHES BY 18 INCHES. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001131996041800113NM 1996 4 18 96ZZZX1745 119951004A5330 SKIN BOEING727 727225 1384077NM BS 251.6 DENTED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FUSE EXT SKIN IS DENTED AT STA 251.6 STR 15 AND STR 16L. CUT OUT DAMAGED AREA FOUND OUT OF LIMITS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR 15 INCHES BY 12 INCHES 2024-T3 .063 INCH ON FUS EXT SKIN STA 251.6, STR 15 AND STR 16L PER SRM 5330-3, PAGE 1, FIGURE 1. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001141996041800114NM 1996 4 18 96ZZZX1746 119951004A5311 FRAME BOEING727 727225 1384077NM BS 500 BENT A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, FWD BAGG COMPT FRAME IS DAMAGED AT SPLICE DOUBLER AT STA 500 STR 25R. REMOVED DOUBLER AND STRAIGHTENED FRAME PER SRM 51-10-1. FABRICATED DOUBLER AND ALODINED AND PRIMED PER SRM 51-40-2 AND SRM 51-10-2, 7075-T6, 6.5 INCHES BY 4 INCHES, .071 INCH. INSTALLED DOUBLER PER SRM 51-30-2. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001151996041800115NM 1996 4 18 96ZZZX1747 119951004A5320 ANGLE BOEING727 727225 1384077NM BS 277-303.9 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, COCKPIT LT SIDEWALL FLOOR SUPPORT ANGLE CORRODED BETWEEN STA 277 AND STA 303.9. REMOVED CORROSION AND Z-ANGLE BRACKET PER SRM 51-10-2. INSTALLED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1 P.4, SIZE 8 INCHES BY 6 INCHES .050 INCH 2024-T3. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001161996041800116NM 1996 4 18 96ZZZX1748 119951004A5347 SEAT TRACK BOEING727 727225 1384077NM BS 1030-1130 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, SEAT TRACK NR 2 LBL 24 IS CORRODED FROM BS 1030 TO BS 1130. REMOVED FASTENERS FOR REMOVAL OF SEAT TRACK PER SRM 51-30-2. FABRICATED TO FIT IN PLACE. NEW SEAT TRACK BS 1030 TO BS 1130 OF 7075-T6. ALODINED AND PRIMED PER 51-10-2. INSTALLED SEAT TRACK WITH NEW FASTENERS PER SRM 51-10-1, PARAGRAPH 4. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001171996041800117NM 1996 4 18 96ZZZX1749 119951004A5315 FLOOR BEAM BOEING727 727225 1384077NM BS 1030 CORROSION A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, BS 1030 FLOOR BEAM CAP IS CORRODED AT LBL 9 FLOOR PANEL ATTACH HOLES. REMOVED DAMAGED AREA BS 1030 FLOOR BEAM CAP AT LBL 9 PER SRM 51-10-6 AND INSTALLED UPPER CHORD BEAM REPAIR PER SRM 53-10-8 P.18 FIG. 3. SIZE OF REPAIR 14 INCH BY 2 INCH BY 2 INCH CHORD BAC 1505-100617 PLUS 22120 7075-T73 SUPPORT ANGLE BAC 1490-2837 7075-T6. REINFORCEMENT STRAP BAC 1512-3396 AND BAC 1512-3353 7075-T6. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001181996041800118NM 1996 4 18 96ZZZX1750 119951004A5347 SEAT TRACK BOEING727 727225 1384077NM BS 1058-1075 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, SEAT TRACK NR 1 LBL 45 IS CORRODED FROM BS 1058 TO BS 1075. REMOVED TRACK STA 1050 TO STA 1090 PER SRM 51-30-2. FABRICATED NEW TRACK PER SRM 51-10-1. ALODINED AND PRIMED NEW TRACK PER SRM 51-10-2. INSTALLED NEW TRACK PER SRM 51-30-2. 2L73 4F A3WE 19960418001191996041800119NM 1996 4 18 96ZZZX1751 119951004A5315 FLOOR BEAM BOEING727 727225 1384077NM BS 480 CORRODED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01742DH 21290 DURING D-CHECK, BS 480 FLOOR BEAM CAP IS CORRODED AT TWO NUT-CLIP LOCATIONS, BL ZERO AND RBL 10. CUT OUT DAMAGED AREA PER SRM 53-10-8, 13 INCH LENGTH OF CUT-OUT ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED REPAIR PARTS PER SRM 53-10-3. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS T-CHORD, 19 INCHES BY 2 INCHES BY 2 INCHES (BAC 1505-100617) ANGLE AND 7075-T6, .080 INCH AND .050 INCH 7075-T6 STRAP AND .080 INCH 7075-T6 AND .050 INCH 7075-T6. TAT: 45,788.3 HRS. TAC: 29,959. 2L73 4F A3WE 19960418001251996041800125EU 1996 4 18 96ZZZX1757 119951229A5230S5237900100600 STRUCTURE AEROSPATR72 ATR72211 EU RT CARGO DOOR CRACKED A TRBAK NONE O OTHER ININSP/MAINT 1 SO21EICBD R0002 150 DURING ROUTINE OVERNIGHT MAINTENANCE CHECK ON AIRCRAFT, A CRACK WAS FOUND AT UPPER INTERNAL STRUCTURE OF RIGHT FORWARD CARGO DOOR. REMOVED AND REPLACED RIGHT FORWARD CARGO DOOR PER MM CHAPTER 52-31-00. PRESSURIZATION CHECK PERFORMED PER 05-53-00 WITH SATISFACTORY RESULTS. (IRELAND) 2H72 4T RTA53EU 19960418001931996041800193WP 1996 4 18 ABXA9600461 119951028A27603923251501 DRIVE LINK DOUG DC9 DC931 3022065WP LT SPOILER CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23945AX 47551 DURING COMPLIANCE OF AD 85-01-03 AND SB'S 27-228, 27-229 AND 27-240, FOUND THE LEFT WING OUTBOARD SPOILER DRIVE LINK HAD A CRACK INDICATION. REPLACED THE LEFT WING OUTBOARD SPOILER DRIVE LINK IAW DC-9 MM 27-61-01. 2L72 4F A6WE 19960418002761996041800276WP 1996 4 18 96ZZZX1841 119950925A57535910041501 END RIB DOUG DC9 DC931 3022065WP RT TE FLAP CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT MOVEABLE FLAP VANE END RIB CRACKED. REPLACED VANE, PN 5910041-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002771996041800277WP 1996 4 18 96ZZZX1842 119950925A55435910257 SKIN DOUG DC9 DC931 3022065WP RUDDER TAB DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB, PN 5910257. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002781996041800278WP 1996 4 18 96ZZZX1843 119950925A57535910042503 VANE DOUG DC9 DC931 3022065WP LT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WING FLAP CENTER MOVEABLE VANE IS DELAMINATED. REPLACED VANE, PN 5910042-503. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002791996041800279WP 1996 4 18 96ZZZX1844 119950925A57535910043509 VANE DOUG DC9 DC931 3022065WP LT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WING FLAP OUTBOARD MOVEABLE VANES DELAMINATED. REPLACED VANE, PN 5910043-509. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002801996041800280WP 1996 4 18 96ZZZX1845 119950925A524059195723 BUTT DOOR DOUG DC9 DC931 3022065WP LT WING DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WING NR 2 BUTT DOOR DELAMINATED. REPLACED DOOR, PN 59195723. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002811996041800281WP 1996 4 18 96ZZZX1846 119950925A57525910051501 SKIN DOUG DC9 DC931 3022065WP AILERON TRIM TABDELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WING AILERON TRIM TAB DELAMINTED. REPLACED TAB, PN 5910051-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002821996041800282WP 1996 4 18 96ZZZX1847 119950925A57525910051502 SKIN DOUG DC9 DC931 3022065WP AILERON TRIM TABDELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT WING AILERON OUTBOARD TAB DELAMINATED. REPLACED TAB, PN 5910051-502. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002831996041800283WP 1996 4 18 96ZZZX1848 119950925A5744 HINGE FITTING DOUG DC9 DC931 3022065WP RT AILERON CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT WING/AILERON OUTBOARD HINGE FITTING CRACKED. REPLACED FITTING. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002841996041800284WP 1996 4 18 96ZZZX1849 119950925A575559100532 SKIN DOUG DC9 DC931 3022065WP RT SPOILER DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD SPOILER DELAMINATED. REPLACED SPILER, PN 5910053-2. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002851996041800285WP 1996 4 18 96ZZZX1850 119950925A5315 FLOOR BEAM DOUG DC9 DC931 3022065WP BS 965 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND FLOOR BEAM CORRODED, STA 965. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002861996041800286WP 1996 4 18 96ZZZX1851 119950925A57535912168506 VANE DOUG DC9 DC931 3022065WP RT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD MOVEABLE FLAP VANE DELAMINATED. REPLACED VANE, PN 5912168-506. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002871996041800287WP 1996 4 18 96ZZZX1852 119950925A575359100401 VANE DOUG DC9 DC931 3022065WP RT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD MOVEABLE FLAP VANE DELAMINATED. REPLACED VANE, PN 5910040-1. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002881996041800288WP 1996 4 18 96ZZZX1853 119950925A5321 FLOOR DOUG DC9 DC931 3022065WP CABIN DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND E AND E COMPARTMENT, CABIN FLOOR AREA JUST ABOVE SERVO DRIVE UNIT CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002891996041800289WP 1996 4 18 96ZZZX1854 119950925A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 598-617 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D- CHECKS, FOUND LONGERON 11L AND INTERCOSTAL AT STA 598-617 CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002901996041800290WP 1996 4 18 96ZZZX1855 119950925A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 579-598 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND INTERCOSTAL CORRODED, FORWARD CARGO COMPARTMENT, STA 579 - STA 598. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002911996041800291WP 1996 4 18 96ZZZX1856 119950925A57535912068501 VANE DOUG DC9 DC931 3022065WP LT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WING MOST INBOARD UPPER MOVEABLE FLAP VANE IS DELAMINATED. REPLACED VANE, PN 5912068-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002921996041800292WP 1996 4 18 96ZZZX1857 119950925A5310 STRUCTURE DOUG DC9 DC931 3022065WP FUSELAGE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND INTERCOSTAL, SKIN, AND LONGERON CORRODED AT AFT CARGO COMPARTMENT LONGERON 29R. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002931996041800293WP 1996 4 18 96ZZZX1858 119950925A5320 ANGLE DOUG DC9 DC931 3022065WP BS 917-956 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND FLOOR ATTACH ANGLE CORRODED, AFT CARGO COMPARTMENT, STA 917 - STA 956, LONGERON 27L. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002941996041800294WP 1996 4 18 96ZZZX1859 119950925A5320 ANGLE DOUG DC9 DC931 3022065WP BS 956-996 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND AFT CARGO COMPARTMENT FLOOR ATTACH ANGLE AND SUPPORT BEAM CORRODED, FS 956 - FS 996. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002951996041800295WP 1996 4 18 96ZZZX1860 119950925A5311 FRAME DOUG DC9 DC931 3022065WP BS 714 CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECKS, FOUND LEFT WHEELWELL SUPPORT FRAME CRACKED, STA 714. REPAIRED IAW DC9 SB 53-100. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002961996041800296WP 1996 4 18 96ZZZX1861 119950925A5313 LONGERON DOUG DC9 DC931 3022065WP BS 996 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158924E 45839 DURING C- AND D-CHECK, FOUND LONGERON 24L AT STA 996, AFT SIDE OF PRESSURE BULKHEAD IS CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610. 2L72 4F A6WE 19960418002971996041800297WP 1996 4 18 96ZZZX1862 119950630A5400 APRON DOUG DC9 DC951 3022051WP NR 2 ENGINE CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING C-CHECK, FOUND NR 2 ENGINE UPPER APRON STRUCTURE CRACKED APPROXIMATELY 14 INCHES AFT OF UPPER ISOLATOR. REPAIRED IAW DC9 SRM CH 54. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897. 2L72 4F A6WE 19960418002981996041800298WP 1996 4 18 96ZZZX1863 119950630A5720 FILLET DOUG DC9 DC951 3022051WP LT WING DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING C-CHECK, FOUND LEFT WING AFT ADF FILLET PANEL DELAMINATED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897. 2L72 4F A6WE 19960418002991996041800299WP 1996 4 18 96ZZZX1864 119950630A5531 SPAR DOUG DC9 DC951 3022051WP VERTICAL STAB CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING C-CHECK, FOUND VERTICAL STABILIZER REAR SPAR CORRODED ABOVE UPPER RUDDER HINGE FITTING. REPAIRED IAW DC9 SRM CH 55. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897. 2L72 4F A6WE 19960418003001996041800300WP 1996 4 18 96ZZZX1865 119950630A5530 ANGLE DOUG DC9 DC951 3022051WP LT VERT STAB CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING C-CHECK, LEFT VERTICAL STABILIZER STIFFENER ATTACH ANGLE CORRODED ABOVE UPPER RUDDER HINGE. REPAIRED IAW DC9 SRM CH 55. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897. 2L72 4F A6WE 19960418003011996041800301WP 1996 4 18 96ZZZX1866 119950630A553199118819 RIB DOUG DC9 DC951 3022051WP VERT STABILIZER CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15919PJ 47663 DURING C-CHECK, FOUND FIXED VERTICAL STABILIZER LEADING EDGE RIB CRACKED. REPLACED RIB, PN 9911881-9. AIRCRAFT TT: 35,252. AIRCRAFT TC: 51,897. 2L72 4F A6WE 19960418003621996041800362WP 1996 4 18 96ZZZM674 119951128A3231 CONTL VALVE DOUG DC9 DC951 3022051WP GEAR DOOR LACK OF LUBE A TWAAO OTHER J WARNING INDICATION CLCLIMB 1 CE05416EA 47751 FLT NR 430 - OKC - AFTER TAKEOFF, FOLLOWING GEAR RETRACTION, GEAR DOOR LIGHT STAYED ON. CHECKED AND LUBRICATED LANDING GEAR CONTROL VALVE. OPERATIONAL CHECK NORMAL. (M) 2L72 4F A6WE 19960418003651996041800365EU 1996 4 18 96ZZZM677 119950926A33503012000 POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN MISMANUFACTURED AL TRBAK NONE W INADEQUATE Q C ININSP/MAINT 1 SO21432MQ9249 1554 228 144 DURING AN INTERNAL PART INSPECTION DUE TO RECHARGING OF THE BATTERY, FOUND LEADS SOLDERED DIRECTLY TO THE PC BOARD. THIS EMERGENCY LIGHT POWER SUPPLY WAS REMOVED FROM THE AIRPLANE AND RETURNED TO THE STOCKROOM. UNIT WAS REPLACED WITH A NEW ONE FROM STOCKROOM. SUBMITTER STATES, 'INSPECTED THE PART IN QUESTION AND THE DISCREPANCIES NOTED ARE, THE REPLACEMENT BATTERY HAS THE LEADS SOLDERED DIRECTLY TO THE PC BOARD. THESE BATTERIES SHOULD HAVE A PUSH ON CARD EDGE CONNECTOR INSTALLED ON THE WIRES TO FACILITATE REMOVAL. VISUALLY COULD NOT FIND ANY OTHER CAUSE FOR REJECTION'. 2H72 4T RTA53EU 19960425000011996042500001WP 1996 4 25 96ZZZX1867 119950611A5311591555965 FRAME WEB DOUG DC9 DC951 3022051WP BS 1230 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPLACED STA 1230 FRAME WEB BELOW CUSP LINE, PN 5915559-65. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000021996042500002WP 1996 4 25 96ZZZX1868 119950611A5311591555969 FRAME CHORD DOUG DC9 DC951 3022051WP BS 1230 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPLACED STA 1230 FRAME LOWER CHORD BELOW CUSP LINE, PN 5915559-69. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000031996042500003WP 1996 4 25 96ZZZX1869 119950911A5311591555967 FRAME CHORD DOUG DC9 DC951 3022051WP BS 1230 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPLACED STA 1230 FRAME UPPER CHORD BELOW CUSP LINE, PN 5915559-967. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000041996042500004WP 1996 4 25 96ZZZX1870 119950611A531159155565 FRAME DOUG DC9 DC951 3022051WP BS 1230 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPLACED STA 1230 FRAME BELOW CUSP LINE, PN 5915556-5. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000051996042500005WP 1996 4 25 96ZZZX1871 119950611A5311 FRAME DOUG DC9 DC951 3022051WP BS 1209 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPAIRED FRAME AT STA 1209 BELOW CUSP LINE (CRACKED). ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000061996042500006WP 1996 4 25 96ZZZX1872 119950611A53125910130279 BLKHD SKIN DOUG DC9 DC951 3022051WP BS 1167 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, REPLACED LOWER HALF OF STA 1167 (AFT PRESSURE BULKHEAD CONSISTING OF PN 5910130-279 BULKHEAD SKIN. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000071996042500007WP 1996 4 25 96ZZZX1873 119950611A5312591013045 BLKHD T-CHORD DOUG DC9 DC951 3022051WP BS 1167 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 REPLACED LOWER HALF OF STA 1167 (AFT PRESSURE BULKHEAD) CONSISTING OF PN 5910130-45, T-CHORD. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000081996042500008WP 1996 4 25 96ZZZX1874 119950611A53125910130387 BLKHD Y-CHORD DOUG DC9 DC951 3022051WP BS 1167 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 REPLACED LOWER HALF OF STA 1167 (AFT PRESSURE BULKHEAD) CONSISTING OF PN 5910130-387, Y-CHORD. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000091996042500009WP 1996 4 25 96ZZZX1875 119950611A5330 SKIN DOUG DC9 DC951 3022051WP CARGO DR CUTOUT DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, FOUND FORWARD CARGO DOOR CUTOUT, FUSELAGE SKIN DAMAGED FORWARD CENTER AREA. REPAIRED IAW DC9 SRM CH 53. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000101996042500010WP 1996 4 25 96ZZZX1876 119950611A5315 FLOOR BEAM DOUG DC9 DC951 3022051WP BS 1167 DAMAGED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15920PJ 47677 DURING C-CHECK, FOUND FLOOR BEAM AT STA 1167, RBL 45, DAMAGED AT LOWER CHORD AND CRACKED AT WEB. REPAIRED IAW DC9 SRM CH 53. ACFT TT: 35,951 HRS. ACFT TC: 49,919. 2L72 4F A6WE 19960425000111996042500011WP 1996 4 25 96ZZZX1877 119951011A5280 SKIN DOUG DC9 DC981 3022081WP LT MLG DOOR CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, LT MLG DOOR SKIN FOUND CRACKED. REPAIRED IAW DC9 SRM CH 52. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000121996042500012WP 1996 4 25 96ZZZX1878 119951011A5730 PANEL DOUG DC9 DC981 3022081WP RT WING LE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING LOWER SURFACE LEADING EDGE PANEL CORRODED ON EXTERIOR SURFACE. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000131996042500013WP 1996 4 25 96ZZZX1879 119951011A5730 PANEL DOUG DC9 DC981 3022081WP RT WING LE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING L/E PANEL 1235C CORRODED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000141996042500014WP 1996 4 25 96ZZZX1880 119951011A5730 PANEL DOUG DC9 DC981 3022081WP RT WING LE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING L/E PANEL 1215C CORRODED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000151996042500015WP 1996 4 25 96ZZZX1881 119951011A57305912737502 TE PANEL DOUG DC9 DC981 3022081WP WS 375 DISBONDED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING UPPER SURFACE T/E PANEL FWD OF AILERON DISBONDED, XW 375. REPLACED PANEL, PN 5912737-502. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000161996042500016WP 1996 4 25 96ZZZX1882 119951011A5730 PANEL DOUG DC9 DC981 3022081WP WS 198-205 LE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND LT WING LE PANEL AT STA XIS 198-205 CORRODED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000171996042500017WP 1996 4 25 96ZZZX1883 119951011A5730 SKIN DOUG DC9 DC981 3022081WP WS 383 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, LT WING, STA XRS 383 LOWER AFT SKIN CORRODED. REPAIRED IAW DC9 SR CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000181996042500018WP 1996 4 25 96ZZZX1884 119951011A5730 SKIN DOUG DC9 DC981 3022081WP WS 295 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND LT WING, STA XRS 295, LOWER AFT SKIN CORRODED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000191996042500019WP 1996 4 25 96ZZZX1885 119951011A5730 SKIN DOUG DC9 DC981 3022081WP WS 250 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, LT WING, STA XRS 250, LOWER AFT SKIN CORRODED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000201996042500020WP 1996 4 25 96ZZZX1886 119951011A535059100913 RADOME DOUG DC9 DC981 3022081WP FWD FUSELAGE DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RADOME INTERIOR DELAMINATED. REPLACED RADOME, PN 59100913. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000211996042500021WP 1996 4 25 96ZZZX1887 119951011A71105930649508 COWL DOUG DC9 DC981 3022081WP NR 3 ENGINE DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND NR 2 ENGINE UPPER COWL DELAMINATED. REPLACED COWL, PN 5930649-508. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000221996042500022WP 1996 4 25 96ZZZX1888 119951011A5320 DOOR FRAME DOUG DC9 DC981 3022081WP CARGO COMPT CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND FORWARD CARGO DOOR FRAME CORRODED, INBOARD AREA. REPAIRED IAW DC9 SRM CH 53. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000231996042500023WP 1996 4 25 96ZZZX1889 119951011A575359304961 VANE DOUG DC9 DC981 3022081WP LT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND LT WING, NR 3 FLAP VANE DELAMINATED. REPLACED VANE, PN 5930496-1. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000241996042500024WP 1996 4 25 96ZZZX1890 119951011A57535930495504 VANE DOUG DC9 DC981 3022081WP RT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING, INBOARD FLAP OUTBOARD VANE DELAMINATED. REPLACED VANE, PN 5930495-504. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000251996042500025WP 1996 4 25 96ZZZX1891 119951011A575359304961 VANE DOUG DC9 DC981 3022081WP RT TE FLAP DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING, OUTBOARD FLAP VANE DELAMINATED. REPLACED VANE, PN 593496-1. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000261996042500026WP 1996 4 25 96ZZZX1892 119951011A553059201032 FITTING DOUG DC9 DC981 3022081WP VERT STABILIZER CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND VERTICAL STABILIZER, FORWARD RT FUSELAGE TO STABILIZER ATTACH FITTING CRACKED. REPLACED FITTING, PN 5920103-2. ACFT TT: 22,675 HRS. ACFT TC: 41,431. 2L72 4F A6WE 19960425000271996042500027WP 1996 4 25 96ZZZX1893 119951011A5240 BUTE DOOR DOUG DC9 DC981 3022081WP RT WING CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15817SJ 48051 DURING C-CHECK, FOUND RT WING NR 4 BUTE DOOR CRACKED. REPAIRED IAW DC9 SRM CH 57. ACFT TT: 22,675 HRS. ACFT TC: 41.431. 2L72 4F A6WE 19960425000281996042500028WP 1996 4 25 96ZZZX1894 119951112A5230 FITTINGS DOUG DC9 DC931 3022065WP TE FLAP VANE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND FORWARD CARGO DOOR OUTER PAN CRACKED IN RADIUS WHERE PAN ATTACHES TOP OUTER SKIN UNDER PRESSURE SEAL. REPAIRED IAW DC9 SRM. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000291996042500029WP 1996 4 25 96ZZZX1895 119951112A523039260461 PIN DOUG DC9 DC931 3022065WP CARGO DOOR CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND CARGO DOOR LOWER INTERIOR, FITTING, PN 3926046-1, CRACKED. REPLACED. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000301996042500030WP 1996 4 25 96ZZZX1896 119951112A5320 ANGLE DOUG DC9 DC931 3022065WP BS 889 CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND CRACKED LONGERON ATTACH ANGLE, STA 889, BETWEEN LONGERON 28R AND LONGERON 29R. REPAIRED ATTACH ANGLE IAW DPS 10.225. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000311996042500031WP 1996 4 25 96ZZZX1897 119951112A5320 ANGLE DOUG DC9 DC931 3022065WP BS 660 CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND FLOOR BEAM ANGLE CORRODED, LT CENTER AT STA 660. REPLACED ANGLE. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000321996042500032WP 1996 4 25 96ZZZX1898 119951112A575349148141 FITTING DOUG DC9 DC931 3022065WP TE FLAP VANE CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RT INBOARD FIXED FLAP VANE CENTER ATTACH FITTINGS CORRODED. REPLACED FITTINGS, PN 4914814-1. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000331996042500033WP 1996 4 25 96ZZZX1899 119951112A575349148141 FITTINGS DOUG DC9 DC931 3022065WP TE FLAP VANE CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RT CENTER FIXED FLAP VANE ATTACH FITTINGS CORRODED. REPLACED FITTINGS, PN 4914814-1. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000341996042500034WP 1996 4 25 96ZZZX1900 119951112A57535910042506 VANE DOUG DC9 DC931 3022065WP LT WING CORRODED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT WING NR 2 FLAP VANE TO OUTBOARD END IS CORRODED. REPLACED VANE, PN 5910042-506. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000351996042500035WP 1996 4 25 96ZZZX1901 119951112A55235910414503 TAB DOUG DC9 DC931 3022065WP LT ELEVATOR DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT ELEVATOR GEARED TAB TRAILING EDGE DELAMINATED. REPLACED TAB, PN 5910414-503. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000361996042500036WP 1996 4 25 96ZZZX1902 119951112A57555910055511 SKIN DOUG DC9 DC931 3022065WP NR 3 SPOILER DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT WING, NR 3 SPOILER, DELAMINATED AT CENTER LOWER SURFACE. REPLACED SPOILER, PN 5910055-511. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000371996042500037WP 1996 4 25 96ZZZX1903 119951112A57555910053501 SKIN DOUG DC9 DC931 3022065WP NR 1 SPOILER DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT WING, NR 1 SPOILER, DELAMINATED AT INBD AND OUTBD ENDS. REPLACED SPOILER, PN 5910053501. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000381996042500038WP 1996 4 25 96ZZZX1904 119951112A52405919586501 BUTE DOOR DOUG DC9 DC931 3022065WP LT WING DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT WING, NR 2 BUTE DOOR, DELAMINATED. REPLACED BUTE DOOR, PN 5919586-501. ACFT TT: 64,568 HRS. ACFT TC: 60,367. 2L72 4F A6WE 19960425000391996042500039WP 1996 4 25 96ZZZX1905 119951112A52405919573502 BUTE DOOR DOUG DC9 DC931 3022065WP RT WING DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RIGHT WING NR 3 BUTE DOOR DELAMINATED. REPLACED BUTE DOOR, PN 5919573502. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960425000401996042500040WP 1996 4 25 96ZZZX1906 119951112A53305914221506 PANEL DOUG DC9 DC931 3022065WP FUSELAGE DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK - FOUND RT ADF FWD SENSE ANTENNA PANEL DELAMINATED. REPLACED PANEL, PN 5914221-506. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960425000411996042500041WP 1996 4 25 96ZZZX1907 119951112A573059127372 PANEL DOUG DC9 DC931 3022065WP LT WING DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND LT WING UPPER TRAILING EDGE PANEL ABOVE OTBD FLAP HINGE DELAMINATED. REPLACED PANEL, PN 59127372. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960425000421996042500042WP 1996 4 25 96ZZZX1908 119951112A57535910043510 VANE DOUG DC9 DC931 3022065WP NR 3 DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RT WING NR 3 FLAP VANE DELAMINATED. REPLACED FLAP VANE, PN 5910043-510. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960425000431996042500043WP 1996 4 25 96ZZZX1909 119951112A57535910042506 VANE DOUG DC9 DC931 3022065WP NR 2 DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RT WING NR 2 FLAP VANE DELAMINATED. REPLACED VANE, PN 5910042-506. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960425000441996042500044WP 1996 4 25 96ZZZX1910 119951112A57535910041505 VANE DOUG DC9 DC931 3022065WP NR 1 DELAMINATED A A4JAK NONE O OTHER ININSP/MAINT 1 SO158931E 47140 DURING C-CHECK AND D-CHECK, FOUND RT WING NR 1 FLAP VANE DELAMINATED. REPLACED FLAP VANE, PN 5910041-505. ACFT TT: 64,568 HRS. ACFT TOTAL CYCLES: 60,367. 2L72 4F A6WE 19960502000011996050200001GL 1996 5 2 95UAL900242 219951101A72309661M85PO7 HPC ROTOR DOUG DC10 DC1010 3022110WP GE CF6 CF66D 30020GL NR 1 ENGINE WORN SPLINES A UALAA UNSCHED LANDING JX WARNING INDICATION ENGINE FLAMEOUT CLCLIMB 1 WP291831U 3029 46630 RETURNED TO LAX UNDER AMBER ALERT DUE TO NR 1 ENGINE FLAMEOUT. SUPPLEMENTAL DATA UPDATE: CAUSE WAS FAILURE OF THE H.P.C. ROTOR SPLINE ADAPTER DUE TO OIL STARVATION. ONE OF THE FOUR OIL DRAIN HOLES BLOCKED BY NORMAL SPLINE OPERATION WEAR DEBRIS. UAL MAINTAINS AN ISOTOPE INSPECTION OF UNEXPOSED SPLINE ADAPTERS FOR SPLINE WEAR. AT PART LEVEL, UAL INSPECTION CRITERIA FOR SPLINE WEAR IS TIGHTER THAN G. E.'s. 2L73 4F4 F A22WE E23EA 19960502002021996050200202NM 1996 5 2 96ZZZX2119 119950914A5313 STRINGER BOEING737 7372P6 NM BS 503 RT CRACKED A A6XAK NONE O OTHER ININSP/MAINT 1 SO13CICKL38000 21356 CLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET IN STR STA 503, S15R. STRINGER CHANNEL AND TIE REPAIR PER BOEING 737-53-1145. 2L72 4F RTA16WE 19960502002031996050200203NM 1996 5 2 96ZZZX2120 119950914A5313 STRINGER BOEING737 7372P6 NM BS 516 LT CRACKED A A6XAK NONE O OTHER ININSP/MAINT 1 SO13CICKL38000 21356 CLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET HOLE IN STR STA 516, S15L. INSTALLED DOUBLER PER IAW SB 737-53-1145. 2L72 4F RTA16WE 19960502002041996050200204NM 1996 5 2 96ZZZX2121 119950914A5313 STRINGER BOEING737 7372P6 NM BS 503 LT CRACKED A A6XAK NONE O OTHER ININSP/MAINT 1 SO13CICKL 21356 CLT - DURING A C-2 CHECK INSPECTION, VISUALLY FOUND A 1 INCH CRACK AROUND RIVET HOLE IN STR STA 503, S15L. REPAIRED PER SB. INSTALLED DOUBLER. BOEING SB 737-53-1145. 2L72 4F RTA16WE 19960502002051996050200205NM 1996 5 2 96ZZZX2122 119951018A5330 SKIN BOEING737 7372P6 NM BS 875 LIGHTNING STRIKEA A6XAK NONE O OTHER ININSP/MAINT 1 SO13EICKK 21612 CLT - CLT INSPECTION VISUALLY LOCATED A LIGHTNING STRIKE LOCATED ON SKIN AT STA 875, S28R. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. 2L72 4F RTA16WE 19960502002061996050200206NM 1996 5 2 96ZZZX2123 119951018A5311 FRAME BOEING737 7372P6 NM BS 807 DENTED A A6XAK NONE O OTHER ININSP/MAINT 1 SO13EICKK37228 21612 CLT - CLT INSPECTION VISUALLY FOUND A 6 INCH BY 12 INCH DENT CAUSING INTERNAL DAMAGE TO FRAME LOCATED STA 807, BL ZERO, BETWEEN S27L AND BL ZERO. INSTALLED REPAIR ANGLES PER SRM 51-40-3. 2L72 4F RTA16WE 19960502002101996050200210EU 1996 5 2 96ZZZX2127 119951120A6410704A33633171 HINGE SNIAS 350 AS350B 8680801EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 116 1065 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM. 1G71 3U H9EU 19960502002111996050200211EU 1996 5 2 96ZZZX2128 119950925A6410704A33633171 HINGE SNIAS 350 AS350B 8680801EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 463 1065 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00, CORRECTED PROBLEM. 1G71 3U H9EU 19960502002191996050200219 1996 5 2 96ZZZX2136 419951230A2565D31050103 SLIDE BAG BAE146BAE146100A 1500260EU CABIN MALFUNCTIONED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31246SS 12974 0571 E1003 DURING SCHEDULED DEPLOYMENT, SLIDE DEPLOYED UNDER THE AIRCRAFT. 2H74 4F RTA49EU 19960502004431996050200443EU 1996 5 2 96ZZZM746 119951229A3350 LIGHTS BAG BAE146BAE146100A 1500260EU CABIN INOPERATIVE A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31463AP E1063 EMERGENCY LIGHT INOP IN LAVATORY. RESET SWITCHES, OPS CHECKED GOOD. 2H74 4F RTA49EU 19960502004441996050200444EU 1996 5 2 96ZZZM747 119951230A3350 SLIDE LIGHT BAG BAE146BAE146100A 1500260EU CABIN INOPERATIVE A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31246SS E1003 DURING SCHEDULED DEPLOYMENT, SLIDE LIGHTING WAS INOPERATIVE. 2H74 4F RTA49EU 19960502004451996050200445EU 1996 5 2 96ZZZM748 119951117A3350 TRACK LIGHT BAG BAE146BAE146300A 1500267EU CABIN INOPERATIVE A A6WAK NONE L NO TEST ININSP/MAINT 1 GL31615AW E3141 FLOOR TRACK LIGHT INOP AT FR32-FR33B. REMOVED AND REPLACED NR 4 BATTERY (POWER) SUPPLY, CHECKS OK. 2H74 4F RTA49EU 19960502004471996050200447EU 1996 5 2 96ZZZM750 119950902A2761D15850 POSITION TRANS BAG BAE146BAE146200A 1500266EU AIR BRAKES FAILED A AA6WAO OTHER J WARNING INDICATION CRCRUISE 1 GL31606AW E2033 UNCOMMANDED AIRBRAKE OPERATION. CREW COMPLIED WITH 'M' MEL PULLED AND COLLORED CIRCUIT BREAKER. REMOVED AND REPLACED AIRBRAKE FEEDBACK POSITION POTENTIOMETER IAW AC MM. OP CHECK SATISFACTORY. MEL 27-60-1 REM. 2H74 4F RTA49EU 19960502004481996050200448EU 1996 5 2 96ZZZM751 119950827A27603799H1 VALVE BAG BAE146BAE146200A 1500266EU AIR BRAKES FAILED A AA6WAO OTHER J WARNING INDICATION APAPPROACH 1 GL31606AW E2033 UNCOMMANDED OPENING OF THE AIRBRAKE ON APPROACH INTO ORD. COMPLIED WITH M ACTION OF THE MEL. REMOVED AND REPLACED AIR BRAKE VALVE IAW MM. OPS CHECK OK. REMOVED FROM MEL. 2H74 4F RTA49EU 19960502004511996050200451EU 1996 5 2 96ZZZM754 119951108A5541 RIB BAG BAE146BAE146300A 1500267EU RUDDER CRACKED A A6WAK NONE O OTHER ININSP/MAINT 1 GL31615AW E3141 RUDDER LOWER RIB IS CRACKED UP AND LOOSE SECTION. REMOVED AND REPLACED LOWER RUDDER RIB PER SRM STANDARD PRACTICES. PRIMED AND PAINTED RIB AND RIVETS. 2H74 4F RTA49EU 19960502006191996050200619CE 1996 5 2 CA951103008 119951028A273004102021 SUPPORT CESSNA150 150L 2071826CE ELEV BELLCRANK CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6224 (CAN)SUPPORT FOUND CRACKED DURING A 200 HOUR INSPECTION. THIS SUPPORT HOLDS THE ELEVATOR BELLCRANK ASSEMBLY IN THE FUSELAGE FRONT AND CENTRE SECTION ASSEMBLY. SUBMITTER STATED THAT THIS AREA IS HARD TO INS PECT WITHOUT A MIRROR. 1H71 3O 3A19 19960509002521996050900252WP 1996 5 9 96ZZZX2262 219951024A7200 ENGINE BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110U 01514WP LEFT FAILED A SABAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO33170PC 717 P63222 BWI/SHD - FLT 5116 - FLT DEPARTED, LT ENG OIL PRESS LIGHT ILLUMINATED. PRESS GAUGE DROPPED TO ZERO & ENG STARTED TO SHUT DOWN. FLT CREW MANUALLY SHUT ENG DOWN. CREW DECLARED EMERG & RETND TO BWI, MADE SAFE LANDING. MX DISPATCHED FROM CLT. UPON ARRIVAL IN BWI, EXAMINED ENG & FND OIL LEAK IN NOSE CASE AREA. SEVERAL BOLTS ON NOSE CASE LOOSE & RETORQUED. ENG SERVICED WITH OIL & DRY MOTORING RUN PERFORMED. NO LEAKS FND. ENG OIL RESERVICED & ENG START ATTEMPTED. ENG DID NOT START. GRBOX DRAIN PLUG REMOVED & APPROX 5 GALLONS OF OIL DRAINED FROM GRBOX. T/S REVEALED DRV GEAR FOR SCAVENGE PUMP TURNING ONE-THIRD OF TIME. ENG REMOVED & REPLACED, A/C RETURNED TO SERVICE. ENG SENT TO GARRETT FOR REPAIR. 2L72 4T4 TRTA21EU E4WE 19960509002531996050900253EU 1996 5 9 96ZZZX2263 119951011A2400 ELECTRICAL SYST STBROSSD3 SD360 8100606EU LT/RT MALFUNCTIONED A SABAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SO33121PC SH3721 CLT - FLT 5087 - FLIGHT HAD JUST DEPARTED WHEN THE AIRCRAFT EXPERIENCED A PARTIAL ELECTRICAL FAILURE. GROUND SERVICES BUS DROPPED OFF-LINE, LT AND RT SHEDDING BUSSES DROPPED OFF-LINE, PANEL 9P WENT BLANK, EMERGENCY LIGHTS CIRCUIT BREAKER TRIPPED AND EMERGENCY LIGHTS CAME ON, AND CAPTAIN'S EHSI INDICATED FAIL. AFTER CAPTAIN HAD TALKED TO MAINTENANCE CONTROL AND TRIED TO RESET ESSENTIAL SERVICES TRANSFER RELAYS, HE RETURNED TO CLT, MADE SAFE UNEVENTFUL LANDING. UPON LANDING, ALL EFFECTED SYSTEMS RETURNED TO NORMAL. MX WAS DISPATCHED TO T/S PROBLEMS. A COMPLETE TEST OF THE ELECTRICAL SYSTEMS INVOLVED FOUND NO PROBLEMS. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2H72 4T A41EU 19960509002541996050900254NE 1996 5 9 96ZZZX2264 219951124A7200 ENGINE STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE RIGHT MALFUNCTIONED A SABAE ENGINE SHUTDOWN XJ ENGINE FLAMEOUT WARNING INDICATION DEDESCENT 1 SO33722PC SH3722 106115 FLT 5097 - FLIGHT WAS DESCENDING THROUGH 5,000 FEET FOR LANDING IN RWI WHEN THE RT ENGINE SHUT ITSELF DOWN. CAPTAIN DECLARED AN EMERGENCY AND MADE UNEVENTFUL LANDING IN RWI. MAINTENANCE PERSONNEL DISPATCHED. THE RT ENGINE OIL FILTER REMOVED TO CHECK FOR METAL CONTAMINATION AND NONE WAS FOUND. THE OIL FILTER WAS REINSTALLED AND THE OIL LEVEL WAS TOPPED OFF. THE ENGINE WAS THEN GROUND RUN FOR APPROXIMATELY 4 HOURS WITH ALL INDICATIONS NORMAL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2H72 4T4 T A41EU E26NE 19960516006401996051600640WP 1996 5 16 96ZZZM790 119950314A5313 LONGERON DOUG DC9 DC931 3022065WP BS 794 CRACKED A TWAAK NONE O OTHER ININSP/MAINT 1 CE05981Z 47345 DURING OP-15, FOUND LONGERON 30 CRACKED APPROXIMATELY 10 INCHES FROM STATION 794, AFT TO SPLICE. REPLACED LONGERON 30 FROM STATION 756 TO 813 PER SRM 51-30 AND TWA STANDARD PRACTICES. 2L72 4F A6WE 19960516007121996051600712EU 1996 5 16 UF6A951201 119951204A33506013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE O OTHER ININSP/MAINT 1 GL31859AW2757 55 2036 ORD - MX FORWARD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY. (M) 2L72 4T RTA27NM 19960516007131996051600713EU 1996 5 16 UF6A951202 119951206A3350362624 LAMP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31851AW9890 2020 SBN - EMERGENCY FLOOR PROXIMITY LIGHT INOP, ROW 1. MAINTENANCE REMOVED AND REPLACED NR 2 LAMP. (M) 2L72 4T RTA27NM 19960516007141996051600714EU 1996 5 16 UF6A951203 119951210A33506013210 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31858AW3141 191 2035 SNB - EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 POWER SUPPLY. (M) 2L72 4T RTA27NM 19960523000851996052300085EU 1996 5 23 96ZZZX2525 119951222A6410704A33633171 HINGE SNIAS 350 AS350B 8680801EU TAIL ROTOR WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 63 1065 TAIL ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153-00. CORRECTED PROBLEM. 1G71 3U H9EU 19960523000871996052300087EU 1996 5 23 96ZZZX2527 119951017A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 533 4099 1065 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523000881996052300088EU 1996 5 23 96ZZZX2528 119951017A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 533 4116 1065 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523000891996052300089EU 1996 5 23 96ZZZX2529 119951017A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM1122UM 533 4150 1065 MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523000901996052300090EU 1996 5 23 96ZZZX2530 119950731A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11792LF526 3768 1035 OCCURRENCE DATE IS 7-31-95. MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523000911996052300091EU 1996 5 23 96ZZZX2531 119950731A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11792LF604 2477 1035 OCCURRENCE DATE IS 7-31-95. MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523000921996052300092EU 1996 5 23 96ZZZX2532 119950731A6220704A33633156 SPHERICAL STOP SNIAS 350 AS350B 8680801EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11792LF604 2573 1035 OCCURRENCE DATE IS 7-31-95. MAIN ROTOR ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G71 3U H9EU 19960523002411996052300241EA 1996 5 23 CA950621021 119950619A32461015071 WHEEL BFGOODRICH 314801 DHAV DHC8 DHC8311 1386006EA MLG NR 2 EXPLODED W K NONE O OTHER TXTAXI/GRND HDL 1 CA 5689 1287 (CAN)#2 MAIN WHEEL ASSEMBLY OUTER RIM EXPLODED DURING TAXI. APPROXIMATELY 1/2 OF OUTSIDE LIP 1 INCH WIDE PIECE, IMPACTED AND PUNCTURED FUSELAGE SKIN. SENT WHEEL HALF TO DEHAVILLAND FOR ANALYSIS. GOODRICH HAS CHANGED OVERHAUL MANUAL PROCEDURE TIMES FROM 30 TO 10 OVERHAUL FOR NDT CHECK. 2H72 4T RTA13NM 19960523002431996052300243SO 1996 5 23 CA950817029 119950805A3213 BOLT PIPER PIPER PA23 PA23250 7102308SO MLG SCISSORS MISSING W O OTHER O OTHER LDLANDING 1 CA 0 (CAN)THE BOLT OF THE RIGHT SCISSORS SEEMS TO HAVE BECOME UNDONE OR BROKEN OFF, WHICH LED TO AN APPROXIMATE 90 DEGREE TURN OF THE RIGHT WHEEL DURING DECELERATION OF THE AIRCRAFT. THE PILOT APPLIED LEFT BRAKE TO KEEP THE AIRCRAFT ON THE RUNWAY. THE BOLT WAS NOT RECOVERED. 1L72 3O 1A10 19960523002441996052300244SW 1996 5 23 CA950824204 119950817A3230EA1570501 DRAG BRACE GULSTM690TP 690A 0141722SW L/H GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5009 (CAN)UPPER DRAG BRACE FOUND CRACKED IN TOP WEB DURING PRE-FLIGHT INSPECTION. LOCTION WAS AT UPPER EYEBOLT ATTACH HOLE. 1H72 3T 2A4 19960523002721996052300272NM 1996 5 23 SWAA960390 119950516A5320 CHANNEL BOEING737 7373G7 1384595NM FWD CARGO CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW07691WN 23781 DURING SCHEDULED 1/4 D-CHECK, FOUND CHANNEL CRACKED ABOVE VHF ANTENNA, IN FWD CARGO BIN. REPLACED CHANNEL PER BOEING SRM. 2L72 4F RTA16WE 19960523005771996052300577NM 1996 5 23 96ZZZM858 119951130A5320 SEAT TRACKS BOEING727 727290 138408WNM CABIN CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01294AS 22146 FOUND RBL 24 AND 48, STATION 370-390 HAS LEVEL 2 CORROSION ON SEAT TRACK FLANGES. REMOVED SEAT TRACK AND FABRICATED NEW TRACKS PER SRM 51-30-2 DRILLED OUT AND ALODINED AND PRIMED PER SRM 51-10-2. REINSTALLED PER SRM 51-10-2 AND 51-30-2 STATION 340 TO 490. 2L73 4F A3WE 19960523005781996052300578NM 1996 5 23 96ZZZM859 119951231A532069477952 CHANNEL BOEING727 727290 138408WNM CABIN CORRODED C S3BMK NONE O OTHER ININSP/MAINT 1 WP01294AS 22146 FOUND FORWARD LAVATORY COMPARTMENT STATION 346, RBL 12 WL 208, HAS LEVEL 2 CORROSION ALONG THE UPPER SURFACE OF THE FLOOR CHANNEL. REMOVED AND INSTALLED NEW FLOOR SUPPORT P/N 69-47795-2 PER SRM 51-10-1 STATION 346 TO 260 RBL 12 WL 208. 2L73 4F A3WE 19960523005791996052300579NM 1996 5 23 96ZZZM860 119951128A5320 CHANNEL BOEING727 727290 138408WNM FWD LAV CORRODED C S3BMK NONE O OTHER ININSP/MAINT 1 WP01294AS 22146 FOUND FORWARD LAVATORY COMPARTMENT, STATION 315-342, RBL 38 WL 208, HAS LEVEL 2 CORROSION ALONG THE UPPER SURFACE OF FLOOR 'T' CHANNEL. FABRICATED NEW PAINT, TREATED, PAINTED AND INSTALLED PER SRM 51-20-1, 51-10-2. 2L73 4F A3WE 19960523005811996052300581NM 1996 5 23 96ZZZM862 119951130A5347 SEAT TRACK BOEING727 727290 138408WNM CABIN CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01294AS 22146 FOUND STATION 346-370 WL 208 RBL 40H, HAS LEVEL 2 CORROSION ON THE SEAT TRACK OUTBOARD FLANGE UPPER SURFACE. REMOVED SEAT TRACK AND FABRICATED NEW TRACK PER SRM 51-30-2. DRILLED OUT AND ALODINED AND PRIMED PER SRM 51-10-2. REINSTALLED FOR SRM 51-10-2 AND 51-30-2 STATION 340 TO STATION 490. 2L73 4F A3WE 19960530002821996053000282WP 1996 5 30 96ZZZX2749 219951127A7200 ENGINE AMD FALC20FALCON20FS 2730105EU GARRTTTFE731TFE731* 01518WP RT ENGINE MAKING METAL A AOSAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 EA11212PB 313 P103114C APPROXIMATELY 45 MINUTES AFTER TAKEOFF, RIGHT OIL PRESSURE ANNUNCIATOR ILLUMINATED. NOTE: OIL PRESSURE AND OIL TEMPERATURE GAUGES WERE NORMAL. TRIP DIVERTED TO IND TO AN APPROVED GARRETT FACILITY. INVESTIGATION REVEALED METAL CONTAMINATION IN OIL SYSTEM FILTER. ENGINE TSO 1,118 HOURS. AIRCRAFT TT, 7,265 HOURS. 2L72 4F4 FRTA7EU E6WE 19960530003401996053000340NM 1996 5 30 96ZZZM878 119951030A276069268661 ROD END BOEING727 727212 138407GNM NR 5 SPOILER CORRODED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01293AS 21348 LEFT WING INBOARD FLIGHT SPOILER NR 5 ACTUATOR INPUT ROD END BEARING CORRODED. REPLACED ACTUATOR ROD PER MM 27-61-9 AND OPS CHECKED SPOILERS PER MM 27-61-00 PQ 530 TO 531 FIG 515, NR 5 PANEL OPS CHECKED GOOD. (M) 2L73 4F A3WE 19960531000021996053100002NM 1996 5 31 96ZZZM99999 119950309A5720 ANGLE BOEING727 72722C 138400FNM FSS 337 CRACKED A DHLAK NONE O OTHER ININSP/MAINT 1 SO01705DH53881 19191 DURING D-CHECK, LEADING EDGE SUPPORT ANGLE CRACKED AT UPPER AFT CORNER ALONG RADIUS FSS 337. REMOVED AND REPLACED ANGLE PER SRM 51-10-1 15 INCHES BY 2 INCHES 2024-T3 .040. 2L73 4F A3WE 19960531000041996053100004GL 1996 5 31 CA950828004 219950706A732123034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILURE W K NONE O OTHER ININSP/MAINT 1 CA 1645 CAE820733 (CAN)INCONSISTENT STARTS AND UNABLE TO SHUT DOWN ENGINE ON ONE OCCASION. FCU REPLACED, HELICOPTER RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 19960531000051996053100005GL 1996 5 31 CA950828012 219950805A732123034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILURE W O OTHER X ENGINE FLAMEOUT LDLANDING 1 CA 242 801246BA (CAN)ENGINE FLAMED OUT WHEN THROTTLE WAS ROLLED BACK TO IDLE AFTER LANDING. DURING THE TWO PREVIOUS DAYS LEADING TO THE INCIDENT, THE IDLE HAD TO BE ADJUSTED THREE TIMES AND WOULD NOT STABILIZE. UNIT REPLACED, AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 19960531000061996053100006SW 1996 5 31 CA950828013 119950822A28407G547 SWITCH BELL 206 206B 1181511SW FUEL SYS PRESS CORROSION W K NONE O OTHER ININSP/MAINT 1 CA (CAN)ELECTRICAL TERMINAL STUD CORRODED, BROKE OFF WHEN NUTS WERE TIGHTENED. 1G71 3U H2SW 19960531000071996053100007CE 1996 5 31 CA950828028 119950322A3233AA5C ACTUATOR MTSBSIMU2 MU2B60 5780460CE MAIN GEAR WATER CONTAM W O OTHER J WARNING INDICATION APAPPROACH 1 CA 2617 (CAN)LANDING GEAR WOULD NOT EXTEND WITH NORMAL SYSTEM. EMERGENCY GEAR EXTENSION CARRIED OUT AND AIRCRAFT LANDED SAFELY. MOISTURE FOUND IN MAIN GEAR ACTUATOR. UNIT RESEALED BUT WAS EVENTUALLY REPLACED AFTERSUBSEQUENT FAILURE. 1H72 3T RTA10SW 19960531000091996053100009WP 1996 5 31 CA950912019 119950831A6720C1281 BEARING ROBSINR44 R44 7640120WP T/R FLAPPING CRACKED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN)DURING FACTORY ACCEPTANCE THE PILOT/OWNER REPORTED THAT THE FORCE REQUIRED FOR FLAPPING THE TAIL ROTOR WAS EXCESSIVE. COMPANY FLIGHT TEST RESPONDED THAT THIS WAS NORMAL FOR A NEW AIRCRAFT. DURING THE IMPORT INSPECTION THE FLAPPING BEARING INNER RACE WAS FOUND CRACKED, WHICH WAS CAUSING EXCESSIVE STIFFNESS. 1G71 3O H11NM 19960606001621996060600162EU 1996 6 6 96ZZZX2795 119950512A6720A6898764 SEAL BOLKMS105 BO105CBS 5626008EU OIL BELLOWS LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11105NC53 396 790 OIL BELLOWS SEAL LEAKING BEYOND SERVICEABLE LIMITS. TURBINE SMOKING CAT-40356 TT 3606.6. TC 9835. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960606001731996060600173 1996 6 6 CAL950996 419951030A3417HG480B20 AIR DATA COMP BOEING737 7372C0 1384488NM E/E COMPT INOPERATIVE A CALAO OTHER F FLT CONT AFFECTED CRCRUISE 1 SW091424110391 20070 CLE - FLT 1255 - WHILE CRUISING AT FL 220 EN ROUTE FROM BDL TO CLE AND WITH AUTOPILOT ENGAGED IN 'B' MODE, THE AIRCRAFT MADE AN ABRUPT BANK TO THE RIGHT. THE AUTOPILOT WAS DISCONNECTED AND THE AIRCRAFT FLEW NORMAL FOR REMAINDER OF FLIGHT. THE 'B' AUTOPILOT WAS PLACARDED INOPERATIVE. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING CORRECTIVE ACTION/INVESTIGATION. SUPPLEMENT - INVESTIGATION REVEALED THE AIR DATA COMPUTER WAS AT FAULT. SHOP TEAR DOWN REVEALED WINDINGS IN TRANSFORMER HAD OPENED UP. (X) 2L72 4F A16WE 19960606004121996060600412NM 1996 6 6 96ZZZX2836 119951030A524165C1917614 DOOR BOEING727 72777 1384018NM GALLEY SERVICE CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 GALLEY SERVICE DOOR IS CRACKED APPROXIMATELY 1 INCH AT THE INNER RADIUS OF THE INSIDE UPPER AFT CORNER. CUT OUT DAMAGED AREA. INSTALLED NEW FRAME SECTION PN 65C19176-14 AND SPLICE CHANNEL PN 65C19176-15 PER 727 SB 72752-116, FIGURES 4, 6, 8, AND 9. 2L73 4F A3WE 19960606004131996060600413NM 1996 6 6 96ZZZX2837 119951026A5753692289411 BRACKET BOEING727 72777 1384018NM NR 2 TE FLAP CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 NR 2 FLAP TRACK, INBOARD ATTACH BRACKET (TO AUXILIARY LOWER T/E STRUCTURE) HAS A CRACK APPROXIMATELY 1 INCH LONG. REMOVED AND REPLACED BRACKET WITH NEW BRACKET PER SRM 51-20-1. 2L73 4F A3WE 19960606004141996060600414NM 1996 6 6 96ZZZX2838 119951026A5720 ANGLE BOEING727 72777 1384018NM RT WING T/E CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 RIGHT WING T/E CAVITY INTERIOR HAS CRACKED (APPROXIMATELY 1 INCH LONG) SUPPORT ANGLE FOR ACCESS PANEL NR 8611 (WS 383.5). REMOVED AND FABBED NEW SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-10-01 AND SRM 51-20-01. 2L73 4F A3WE 19960606004151996060600415NM 1996 6 6 96ZZZX2839 119951026A5754 BRACKET BOEING727 72777 1384018NM NR 2 LE FLAP CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 CRACKED DOUBLER INSIDE NR 2 L/E SLAT AT BASE OF INBOARD TRACK OUTBOARD RIB. REMOVED CRACKED BRACKET, STOP DRILLED RIB, FABBED AND INSTALLED NEW L-ANGLE BRACKET PER SRM 5750-3, FIGURE 9. 2L73 4F A3WE 19960606004161996060600416NM 1996 6 6 96ZZZX2840 119951026A5320 BRACKET BOEING727 72777 1384018NM LT MLG CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 LEFT MLG SUPPORT BEAM, AFT FACE, APPROXIMATELY 4 INCHES OUTBOARD OF MAIN TRUNNION, THERE IS A SUPPORT BRACKET FOR AUXILIARY T/E STRUCTURE WITH A .50 INCH LONG CRACK IN BRACKET. REMOVED BRACKET, FABBED NEW BRACKET, TREATED, AND INSTALLED PER SRM 51-10-1. 2L73 4F A3WE 19960606004171996060600417NM 1996 6 6 96ZZZX2841 119951024A5210 BRACKET BOEING727 72777 1384018NM L-1 DOOR CRACKED B S3BRK NONE O OTHER ININSP/MAINT 1 WP01720DC 19253 L-1 DOOR LOWER LINER ATTACH PLATE BRACKET 3RD HOLE IS CRACKED AT LOWER AFT CORNER OF DOOR. FABBED AND INSTALLED DOUBLER PER SRM 51-20-2 AND REINSTALLED BRACKET. 2L73 4F A3WE 19960606008521996060600852SO 1996 6 6 CA950515033 119950409A291641300201 TRANSMISSION CAMAIR480 480 1890102SO SIGHT GLASS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 584 (CAN)GLASS IN SIGHT INDICATOR LEAKING SLOWLY. LEAK ENOUGH TO MAKE A MESS BUT NOT ENOUGH TO REQUIRE ADDITION OF OIL BETWEEN OIL CHANGES. 1L72 3O 2A2 19960606008531996060600853SO 1996 6 6 CA950515034 119950411A327041740071 WEAR PLATE CAMAIR480 480 1890102SO MID POINT WORN W R AUTOROTATION O OTHER DEDESCENT 1 CA 595 (CAN)WEAR PLATE TABS BROKEN OFF WHERE TABS ATTACH TO PLATE. TABS BROKE DURING PRACTICE RUN ON AUTO ROTATION. 1L72 3O 2A2 19960606008541996060600854GL 1996 6 6 CA950913202 119950830A55205221019 BRACKET ? 772100122 NAMER T6 HARVARD4 6400430GL ELEV HINGE BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 0 (CAN)DURING PREFLIGHT OF THE AIRCRAFT THE PILOT NOTICED THE OUTBOARD ELEVATOR HINGE BRACKET WAS BORKEN AND THE HEAD OF THE BOLT WAS FOUND MISSING. SUBMITTER BELIEVES THAT THE BRACKET FAILED AND SUBSEQUENTL Y THE LOAD ON THE BOLT CAUSE IT TO FAIL. SUBMITTER IS ALSO SEEKING INSTALLATION APPROVAL OF P/N 88-21019 WHICH IS USED ON THE AMERICAN T6 VERION OF THIS AIRCRAFT. 1L71 3R EXPA1L71 19960606008571996060600857EA 1996 6 6 CA950926002 119950901A554285540001005 RUDDER DHAV DHAV DHC8 DHC8311 1386006EA LEFT SIDE SKIN TEAR W K NONE O OTHER ININSP/MAINT 1 CA CAP0249 (CAN)HOLE NOTED ON LEFT SIDE OF FORE RUDDER. APPROXIMATELY 1 INCH FROM TOP OF RUDDER ALONG TOP RIB. IT SEEMS A CRACK HAD STARTED ALONG THE ROW OF RIVETS ON THE RIB AND THE AIRFLOW TORE THE SKIN BACK LEAVIN G A 6 INCH HOLE. CRACK APPEARS TO BE FATIGUE RELATED CAUSED BY OIL CANNING.CRACKING DUE TO STIFFENE R. GENERIC REPAIR RD 8-55-335 DEVELOPED FEBRUARY 1996. LIKELY PROBLEM CAUSED BY VIBRATION BUFFETING. SERIES 400 AIRCRAFT TO BE MODIFIED. 2H72 4T RTA13NM 19960606008581996060600858SO 1996 6 6 CA950929002 119950917A24212CM353C1H GENERATOR LKHEED382 382G 526414USO NR 2 ENG BEARING FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA 4895 235867 (CAN) GENERATOR FAIL LIGHT ILLUMINATED. SHUT ENG DOWN. 2H74 4T A1SO 19960606008591996060600859SW 1996 6 6 CA951027008 119951012A7920MS51830202L INSERT GARRTT 8974072 SWRNGNSA227 SA227AC 8780603SW OIL FILTER STRIPPED W AE UNSCHED LANDING ENGINE SHUTDOWN JK WARNING INDICATION FLUID LOSS TOTAKEOFF 1 CA 0 (CAN)L/H ENGINE OIL LOW PRESSURE LIGHT ILLUMINATED WITH CORRESONDING LOW OIL PRESSURE INDICATION ON GAUGE DURING TAKEOFF AND CLIMB. L/H ENGINE SHUTDOWN AND ONE ENGINE OUT LANDING MADE WITHOUT INCIDENT. L/HGEARBOX OIL BYPASS PIN ASSEMBLY LOCK/ATTACH BOLT HOLE THREADS WOULD NOT HOLD PIN/BOLT TORQUED IN PLACE. HELI-COIL INSTALLED. 2L72 4T RTA8SW 19960606008601996060600860NM 1996 6 6 CA951030003 119951028A7810 CLAMP DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE EXHAUST MIS INSTALLED W E ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP TXTAXI/GRND HDL 1 CA 120164 (CAN)ON TAXI TO RUNWAY, #2 FIRE WARNING LIGHT CAME ON. WHEN PROP FEATHERED, LIGHT WENT OUT. TAIL PIPE CLAMP NOT INSTALLED CORRECTLY ALLOWING AN EXHAUST LEAK INTO THE REAR COWL AREA ALLOWING WARNING LIGHT T O GO OFF. 2H72 4T4 TRTA13NM E20NE 19960613000951996061300095WP 1996 6 13 ABXA9600503 119950531A33504TL111013 SWITCH DOUG DC9 DC931 3022065WP COCKPIT DEFECTIVE A ABXAK NONE O OTHER ININSP/MAINT 1 GL23946AX 47003 DURING SERVICE CHECK, WHEN SELECTING EMERGENCY LIGHTS TO OFF, THE LIGHTS REMAINED ILLUMINATED. REPLACED THE EMERGENCY LIGHT SWITCH. 2L72 4F A6WE 19960613001331996061300133NM 1996 6 13 SWAA960486 119950625A33506128251 CHARGER BOEING737 7373Y0 1384671NM CABIN INOP A SWAAK NONE L NO TEST ININSP/MAINT 1 SW07682SW 23496 DURING SCHEDULED SERVICE CHECK, FOUND FORWARD DOOR LOWER EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK CHARGER PER BOEING M/M. 2L72 4F RTA16WE 19960613001471996061300147SO 1996 6 13 96ZZZX2924 119950904A5414 SKIN LKHEED188 188C 5262604SO LT NACELLE DAMAGED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING RETRACTION TEST OF LANDING GEAR, THE LEFT INBOARD AFT GEAR DOOR CAUGHT ON THE LOWER EDGE OF NACELLE SKIN. REPAIRED PER SRM 54-2-1, FIGURE 3. 2L74 4T 4A22 19960613001481996061300148SO 1996 6 13 RAAA995069 119951223A33508621014 BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 LT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001491996061300149NM 1996 6 13 RAAAB295002 119950308A5315 FLOORBEAM BOEING727 72722C 138400FNM BS 294.5 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK PER CARD 51004, FOUND TRANSVERSE FLOOR BEAM WEB CRACKED AT BS 294.5, LBL 55 AND WL 208. REPAIRED PER SRM 53-10-2, FIGURE 1. (X) 2L73 4F A3WE 19960613001501996061300150NM 1996 6 13 RAAAB295003 119950308A5730 SKIN BOEING727 72722C 138400FNM RT WING CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK PER CARD 22004, FOUND RT WING UPPER SKIN CRACKED AT INBOARD GUIDE PIN ATTACH POINT NR 8, LE SLAT. REPAIRED PER SRM 57-50-3, FIGURE 10, PAGES 27 AND 28. (X) 2L73 4F A3WE 19960613001511996061300151NM 1996 6 13 RAAAB295004 119950308A5720 ANGLE BOEING727 72722C 138400FNM RT WING CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK PER CARD 22004, FOUND RT WING UPPER SPAR ANGLE TO LEADING EDGE RIB BRACKET CRACKED. REPAIRED ANGLE PER SRM 51-40-3. (X) 2L73 4F A3WE 19960613001521996061300152NM 1996 6 13 RAAAB295005 119950308A5330 SKIN BOEING727 72722C 138400FNM BS 290 DAMAGED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK, FOUND STR 24R CORRODED AT BS 290. REMOVED CORROSION PER SRM 53-10-1, REPAIRED SKIN PER SRM 53-30-1 AND SKIN DAMAGE DUE TO CORROSION REMOVAL PER SRM 53-30-1. (X) 2L73 4F A3WE 19960613001531996061300153NM 1996 6 13 RAAAB295006 119950308A5754 RIB BOEING727 72722C 138400FNM NR 3 LE FLAP CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK, FOUND LT WING NR 3 LE SLAT RIBS CRACKED AT SLAT STA'S 121, 122, AND 128. REPAIRED CRACKED RIBS PER SRM 57-50-3. (X) 2L73 4F A3WE 19960613001541996061300154NM 1996 6 13 RAAAB295007 119950308A5754 SKIN BOEING727 72722C 138400FNM NR 3 LE FLAP CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK, FOUND LT WING NR 3 LE SLAT SKIN CORRODED AT SLAT STA 121. REMOVED CORROSION (BEYOND LIMITS) TREATED AND PRIMED INSTALLED DOUBLER PER SRM 57-50-3, FIGURE 1, SHEET 1. (X) 2L73 4F A3WE 19960613001551996061300155NM 1996 6 13 RAAAB295008 119950308A5543 TE SKIN BOEING727 72722C 138400FNM RUDDER TAB DAMAGED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK PER CARD S2-33101, FOUND UPPER RUDDER TAB TRAILING EDGE DENTED AND GOUGED NEAR TIP. REPAIRED PER SRM 51-40-6, FIGURE 1, SHEETS 4 AND 5. (X) 2L73 4F A3WE 19960613001561996061300156NM 1996 6 13 RAAAB295009 119950308A5400 COWL BOEING727 72722C 138400FNM NR 3 ENGINE CHAFED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV 19098 DURING SCHEDULED 6C CHECK, FOUND NR 3 ENGINE UPPER COWL CHAFED BETWEEN 3RD AND 4TH CIRCUMFERENTIAL. REPAIRED PER SRM 54-10-3. (X) 2L73 4F A3WE 19960613001571996061300157NM 1996 6 13 RAAAB295010 119950308A5411 CIRCUMFERENTIAL BOEING727 72722C 138400FNM NR 3 ENGINE CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV 19098 DURING SCHEDULED 6C CHECK, FOUND NR 3 ENGINE UPPER COWL FORWARD CIRCUMFERENTIAL FLANGE CRACKED ON INBOARD SIDE. REPAIRED PER SRM 51-40-3, FIGURE 1. (X) 2L73 4F A3WE 19960613001581996061300158NM 1996 6 13 RAAAB295011 119950308A5411 CIRCUMFERENTIAL BOEING727 72722C 138400FNM NR 3 ENGINE CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV 19098 DURING SCHEDULED 6C CHECK, FOUND NR 3 ENGINE LOWER COWL L/E CIRCUMFERENTIAL CRACKED. REPAIRED PER SRM 51-40-3. (X) 2L73 4F A3WE 19960613001591996061300159NM 1996 6 13 RAAAB295012 119950308A5320 WEB BOEING727 72722C 138400FNM BS 280 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV3928 19098 DURING SCHEDULED 6C CHECK, FOUND NOSE WHEELWELL PRESSURE WEB CORRODED AT BS 280, RBL 3 OUTER SURFACE. REMOVED DAMAGED AREA PER SRM 51-10-6, FABRICATED FILLER AND DOUBLER PER SRM 51-40-2 AND INSTALLED PER SRM 51-40-2. (X) 2L73 4F A3WE 19960613001601996061300160NM 1996 6 13 RAAAB295013 119950308A5711 SPAR CAP BOEING727 72722C 138400FNM WS 290 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV53928 19098 DURING SCHEDULED 6C CHECK PER CARD 22004, FOUND RT WING CORRODED ON FORWARD SPAR UPPER CAP AT WS 290. REPAIRED IAW BOECOM MSG 7272-95-0834, DATED FEBRUARY 13, 1995. (X) 2L73 4F A3WE 19960613001611996061300161NM 1996 6 13 RAAAB295014 119950308A534365176768 TRUNNION BOEING727 72722C 138400FNM RT NLG DAMAGED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03832RV 19098 DURING SCHEDULED 6C CHECK, FOUND RT NLG TRUNNION MATING SURFACE DAMAGED. REPLACED LT AND RT TRUNNIONS PER SB 727-53-0119, REV 2, PART III. (X) 2L73 4F A3WE 19960613001621996061300162NM 1996 6 13 RAAAB295025 119951028A3350900833A TRANSMITTER BOEING727 72722C 138400FNM CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 AFT PASSENGER CABIN EGRESS TRANSMITTER FAILED SERVICE CHECK. CHANGED UNIT. (X) 2L73 4F A3WE 19960613001631996061300163NM 1996 6 13 RAAAB295030 119950628A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 LEFT FORWARD OVERWING EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960613001641996061300164SO 1996 6 13 RAAAE8950 119950904A5320 FIRE SHIELD LKHEED188 188C 5262604SO LT MLG WW CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND CRACK IN THE LT WHEELWELL FIRE SHIELD, LOWER EDGE FOR THE NR 1 MAIN WHEEL AND TIRE ASSY. REPAIRED PER SRM 51-3-7, FIGURE 1, SHEET 1. (X) 2L74 4T 4A22 19960613001651996061300165SO 1996 6 13 RAAAE895004 119950227A32308304435 FULCRUM 8304441 LKHEED188 188C 5262604SO NLG CRACKED A ARAAAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AL03178RV 13 188C2010 DIVERTED TO CDB DUE ON TAKEOFF FROM DUT, NLG FAILED TO FULLY RETRACT AND MADE A LOUD BANGING NOISE. AIRCRAFT FERRIED TO ANCH. ANCH MAINTENANCE FOUND LEFT AFT SIDE OF CROSS HEAD FULCRUM CRACKED APPROXIMATELY ONE INCH FROM INBOARD END OF PREVIOUSLY INSTALLED REPAIR FITTINGS. CHANGED NLG ASSY. (X) 2L74 4T 4A22 19960613001661996061300166SO 1996 6 13 RAAAE895005 119950301A33508621006 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001671996061300167SO 1996 6 13 RAAAE895006 119950301A33508621014 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 MAIN CABIN DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001681996061300168SO 1996 6 13 RAAAE895007 119950310A3350S102 BATTERIES GRIMES 1000553 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 LEFT AFT OVERWING EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED BATTERIES DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001691996061300169SO 1996 6 13 RAAAE895008 119950426A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 RIGHT AFT OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (X) 2L74 4T 4A22 19960613001701996061300170SO 1996 6 13 RAAAE895009 119950426A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN FAILED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 LEFT AFT OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (X) 2L74 4T 4A22 19960613001711996061300171SO 1996 6 13 RAAAE895012 119950506A33508621006 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 SEAT ROW 15 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001721996061300172SO 1996 6 13 RAAAE895013 119950527A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN FAILED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 LEFT AFT OVERWING EXIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (X) 2L74 4T 4A22 19960613001731996061300173SO 1996 6 13 RAAAE895014 119950607A27508247615 CONTROL CABLE 8247428 LKHEED188 188C 5262604SO RT TE FLAP BROKEN A RAAAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AL03178RV 188C2010 MADE ZERO FLAP LANDING AT ANCH DUE FLAP ASYMMETRY ANNUNCIATOR ILLUMINATED ON CLIMB-OUT FROM CDB DURING RETRACTION. FLAP INDICATOR READS ZERO DEGREES AND CORRELATES WITH HANDLE. REPLACED BROKEN RT ASYMMETRY DETECTOR CABLE PER L-188MM 27-6-13. LUBED TENSION REGULATOR. OPS CHECK NORMAL. (X) 2L74 4T 4A22 19960613001741996061300174SO 1996 6 13 RAAAE895015 119950629A33508621014 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 RIGHT AFT OVERWING EGRESS IDENTIFIER LIGHT ASSY FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001751996061300175SO 1996 6 13 RAAAE895016 119950629A33508621015 BATTERY PACK 8631003 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 MID-PASSENGER COMPARTMENT EGRESS TRANSMITTER FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001761996061300176SO 1996 6 13 RAAAE895017 119950629A33508621015 BATTERY PACK 8631003 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 FORWARD PASSENGER COMPARTMENT EGRESS TRANSMITTER FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. 2L74 4T 4A22 19960613001771996061300177SO 1996 6 13 RAAAE895018 119950904A5320 DOUBLER LKHEED188 188C 5262604SO BS 549 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND RIVET HEAD MISSING AND REPAIR DOUBLER BULGING AROUND FASTENERS AT FS 549 AND STR 39. REPAIRED PER LAC DWG 841500 NOTE NR 30. (X) 2L74 4T 4A22 19960613001781996061300178SO 1996 6 13 RAAAE895019 119950904A5320 DOUBLER LKHEED188 188C 5262604SO BS 255-321.5 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND CORROSION EMANATING FROM AFT EDGE OF ANTENNA DOUBLER AND BULGING AROUND MOST FASTENERS FS 255 - FS 321.5 AND STR 34 TO STR 39. REMOVED AND REPLACED DOUBLER PER SRM 51-2-9. (X) 2L74 4T 4A22 19960613001791996061300179SO 1996 6 13 RAAAE895020 119950904A5320 SPLICE LKHEED188 188C 5262604SO WS 170-172.5 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND CRACK IN LOWER LT WING 3 TO 4 WING PANEL SPLICE WS 170 TO WS 172.5. REPAIRED PER LUMBY DESIGN SERVICE DWG 188285. (X) 2L74 4T 4A22 19960613001801996061300180SO 1996 6 13 RAAAE895021 119950904A5313 STRINGER LKHEED188 188C 5262604SO BS 68 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND STR 19 CRACKED AT FS 68. REPLACED STRINGER PER SRM 51-2-9. (X) 2L74 4T 4A22 19960613001811996061300181SO 1996 6 13 RAAAE895022 119950904A5320 DOUBLER LKHEED188 188C 5262604SO BS 730 MISREPAIRED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND PREVIOUS REPAIR AT FS 730 AND STR 3 NOT PER SRM. REMOVED AND INSTALLED NEW REPAIR DOUBLER PER SRM 53-2-1, PAGE 10, FIGURE 2, SHEET 3. (PARAGRAPH C/II) 2L74 4T 4A22 19960613001821996061300182SO 1996 6 13 RAAAE895023 119950904A5312 BULKHEAD LKHEED188 188C 5262604SO BS 200 DAMAGED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS -200 PRESSURE BULKHEAD DENTED, GOUGED AND RIVET HEAD DAMAGED AT RBL 34. REMOVED DAMAGED AREA INSTALLED DOUBLER PER SRM 51-31-1, FIGURE 1, SHEET 2. (X) 2L74 4T 4A22 19960613001831996061300183SO 1996 6 13 RAAAE895024 119950904A5311 FRAME LKHEED188 188C 5262604SO BS 262 HOLED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 262 STUB FRAME - MULTIPLE HOLES DRILLED IN RADIUS STR 35 - STR 37. INSTALLED REPAIR DOUBLER PER SRM 53-2-3, PAGE 9. (X) 2L74 4T 4A22 19960613001841996061300184SO 1996 6 13 RAAAE895025 119950904A5311 FRAME LKHEED188 188C 5262604SO BS 283.5 HOLED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 283.5 STUB FRAME PREVIOUS REPAIR HOLED IN RADIUS AND FASTENERS STR 35 - STR 37. REPAIRED PER SRM 53-2-3, PAGE 9. (X) 2L74 4T 4A22 19960613001851996061300185SO 1996 6 13 RAAAE895026 119950904A5313 STRINGER LKHEED188 188C 5262604SO BS 306 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND STR 37 CORRODED AT FS 306. REPAIRED PER SRM 53-2-2, FIGURE 2, SHEET 3. (X) 2L74 4T 4A22 19960613001861996061300186SO 1996 6 13 RAAAE895027 119950904A5330 SKIN LKHEED188 188C 5262604SO BS 236-371 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FUSELAGE SKIN BULGED AND CORRODED THROUGH FS 309 TO FS 333 AND STR 35 TO STR 37. CLEANED ALL CORROSION FROM FRAMES AND STRINGERS, REMOVED AND REPLACED SKIN PANEL AND DOUBLERS FS 236 TO FS 371, AND STR 34 TO STR 38 PER SRM 51-2-9. (X) 2L74 4T 4A22 19960613001871996061300187SO 1996 6 13 RAAAE895028 119950904A5414 SKIN LKHEED188 188C 5262604SO NR 1 NACELLE CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND NR 1 NACELLE LOWER INBOARD AFT NACELLE SKIN CRACKED AT NACELLE STA 43.0, LOWER. REPAIRED PER SRM 54-2-1, FIGURE 3. (X) 2L74 4T 4A22 19960613001881996061300188SO 1996 6 13 RAAAE895029 119950904A5320 SHEAR TIE LKHEED188 188C 5262604SO BS 1133 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND CRACKED SHEAR TIE BETWEEN STR 1 AND STR 2 AT FS 1133. INSTALLED REPAIRED DOUBLER PER SRM 53-3-3, FIGURE 2, PAGE 1. (X) 2L74 4T 4A22 19960613001891996061300189SO 1996 6 13 RAAAE895030 119950904A5320 SUPPORT LKHEED188 188C 5262604SO BS 863 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 863 TRANSVERSE FLOOR SUPPORT CORRODED LBL 24 - LBL 41. REPAIRED PER SRM 53-2-4, FIGURE 1, SHEET 1. (X) 2L74 4T 4A22 19960613001901996061300190SO 1996 6 13 RAAAE895031 119950904A5311 FRAME LKHEED188 188C 5262604SO BS 958 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 958 FRAME CORRODED STR 29 TO STR 30. REMOVED CORROSION, INSTALLED REPAIR PER SRM 53-2-3, FIGURE 2. (X) 2L74 4T 4A22 19960613001911996061300191SO 1996 6 13 RAAAE895032 119950904A5320 SUPPORT LKHEED188 188C 5262604SO BS 635 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 635 TRANSVERSE SUPPORT UPPER CHORD CORRODED AT RBL 50. REPAIRED PER SRM 53-2-4, FIGURE 2, SHEET 1. (X) 2L74 4T 4A22 19960613001921996061300192SO 1996 6 13 RAAAE895033 119950904A322180099412 TRUSS RIB LKHEED188 188C 5262604SO NLG WW LOOSE BEARINGS A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71688 188C2010 DURING SCHEDULED INSPECTION PER SB 701, FOUND BOTH NLG TRUSS LUG BEARINGS LOOSE IN BORE. REPAIRED PER LUNDBY DESIGN DWG 188273. (X) 2L74 4T 4A22 19960613001931996061300193SO 1996 6 13 RAAAE895034 119950904A5313 STRINGER LKHEED188 188C 5262604SO BS 260 BROKEN A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND STRINGER 36 BROKEN AT FS 260. REPAIRED PER SRM 53-2-2, FIGURE 2, SHT 3. (X) 2L74 4T 4A22 19960613001941996061300194SO 1996 6 13 RAAAE895035 119950904A5220807079 DOOR STOPS LKHEED188 188C 5262604SO BS 674.6 CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND RT FORWARD OVERWING EMERGENCY EXIT AFT FRAME UPPER AND LOWER DOOR STOPS CRACKED. INSTALLED NEW STOP FITTINGS. (X) 2L74 4T 4A22 19960613001951996061300195SO 1996 6 13 RAAAE895036 119950904A5320 SUPPORT LKHEED188 188C 5262604SO BS 352 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 352 CARGO FLOOR TRANSVERSE SUPPORT CORRODED AT BL 18L TO BL 36L. REPAIRED PER SRM 53-2-4, PAGES 8 AND 9. (X) 2L74 4T 4A22 19960613001961996061300196SO 1996 6 13 RAAAE895037 119950904A5320 SUPPORT LKHEED188 188C 5262604SO BS 863 CORRODED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND FS 863 TRANSVERSE FLOOR SUPPORT UPPER CHORD, UPPER AND LOWER SURFACE CORRODED LBL 23 TO LBL 42. REPAIRED PER SRM 53-2-4, PAGES 8 AND 9. (X) 2L74 4T 4A22 19960613001971996061300197SO 1996 6 13 RAAAE895038 119950904A5320 FIRE SHIELD LKHEED188 188C 5262604SO LT MLG WW CRACKED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03178RV71656 188C2010 DURING SCHEDULED NR 4 CHECK, FOUND CRACK IN THE LT WHEELWELL FIRE SHIELD, LOWER EDGE FOR THE NR 1 MAIN WHEEL AND TIRE ASSY. REPAIRED PER SRM 51-3-7, FIGURE 1, SHT 1. (X) 2L74 4T 4A22 19960613001981996061300198SO 1996 6 13 RAAAE895039 119950920A33508621006 BATTERY PACK 763199212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 SEAT ROW 16 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613001991996061300199SO 1996 6 13 RAAAE895040 119950920A33508621006 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 SEAT ROW 11 EGRESS FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002001996061300200SO 1996 6 13 RAAAE895041 119950920A33508621014 BATTERY PACK 873100212 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 AFT PASSENGER CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002011996061300201SO 1996 6 13 RAAAE895042 119951104A33501102832 LIGHT LKHEED188 188C 5262604SO CABIN FAILED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 MID-PASSENGER CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSY. (X) 2L74 4T 4A22 19960613002041996061300204SO 1996 6 13 RAAAE905011 119950506A3350S106 BATTERY PACK GRIMES 1102832 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03178RV 188C2010 AFT PASSENGER CABIN OVERHEAD EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002061996061300206SO 1996 6 13 RAAAE995069 119951223A33508621014 BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 RIGHT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002531996061300253GL 1996 6 13 RAAAE495026 219951010A72506844936 BEARING SUPPORT LKHEED188 188A 5262602WP ALLSN 501D 501D13 03004GL TURBINE SEPARATED A RAAAE ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 AL039744C350065891 188A1140 500943 NR 2 ENGINE 'E' HANDLED WHILE CLIMBING OUT OF SDP DUE TO LOW OIL QUANTITY AND FLUCTUATING ENGINE AND RGB OIL PRESSURE. REPLACED ENGINE ASSY DUE REAR TURBINE BEARING SUPPORT OUTER CONE 95 PERCENT SEPARATED AT WELD .5 INCH AFT OF HUB ASSY. ALSO, HUB STRUTS CRACKED AT 6 AND 8 O'CLOCK POSITIONS. (X) 2L74 4T4 TRT4A22 E282 19960613002571996061300257SO 1996 6 13 RAAAE995059 119950718A33508612006 BATTERY PACK 873100112 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 EGRESS FLOOR PROXIMITY LIGHT PASSENGER ROW 15 FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002581996061300258SO 1996 6 13 RAAAE995060 119950718A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 RIGHT AFT OVERWING EMERGENCY EXIT PULL DOWN LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSY. (X) 2L74 4T 4A22 19960613002591996061300259SO 1996 6 13 RAAAE995061 119950718A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 AFT PASSENGER ENTRY EMERGENCY PULL DOWN LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSY. (X) 2L74 4T 4A22 19960613002601996061300260SO 1996 6 13 RAAAE995062 119950718A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 REAR EMERGENCY EXIT EMERGENCY PULL DOWN LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSY. (X) 2L74 4T 4A22 19960613002611996061300261SO 1996 6 13 RAAAE995064 119950901A3350821015 BATTERY PACK 8631003 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 MID-PASSENGER COMPARTMENT EGRESS TRANSMITTER FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002621996061300262SO 1996 6 13 RAAAE995065 119950901A3350821015 BATTERY PACK 8631003 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 AFT PASSENGER COMPARTMENT EGRESS TRANSMITTER FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002631996061300263SO 1996 6 13 RAAAE995066 119950901A33501000553 LIGHT LKHEED188 188C 5262604SO CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 AFT PASSENGER COMPARTMENT OVERHEAD EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY. (X) 2L74 4T 4A22 19960613002641996061300264SO 1996 6 13 RAAAE995067 119950928A3350S102 BATTERY 1000553 LKHEED188 188C 5262604SO CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 LEFT OVERWING EMERGENCY EXIT PULL DOWN LIGHT WOULD NOT TEST ON SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L74 4T 4A22 19960613002651996061300265SO 1996 6 13 RAAAE995068 119951117A33501000553 LIGHT LKHEED188 188C 5262604SO COCKPIT FAILED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL031968R 188C2007 COCKPIT EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. (X) 2L74 4T 4A22 19960613004771996061300477WP 1996 6 13 96ZZZM930 219951227A73218070256 FUEL CONTL UNIT SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP LT ENGINE FAILED A ABSAAAE UNSCHED LANDING ENGINE SHUTDOWN Y ENGINE STOPPAGE CLCLIMB 1 NM05115BS TC324 LEFT ENGINE POWER BEGAN CLIMBING UNCOMMANDED DURING CLIMB-OUT AT APPROX 500 FEET AGL. POWER LEVER (FCU) MOVEMENT UNRESPONSIVE. ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO LWT AND LANDED UNEVENTFULLY. INTERNAL FCU FAILURE. IT WAS DETERMINED THAT INTERNAL FCU FAILURE WAS INDEED THE CAUSE OF TROUBLE AS A NEW FCU WAS INSTALLED AND THE ENGINE WAS GROUND RUN AND POWER CHECKED NORMAL AFTER INSTALLATION. A 25 HR SOAP SAMPLE HAS BEEN REQUESTED ON ENGINE P54159 PER GARRETT MM. AIRCRAFT HAS BEEN RELEASED FOR SERVICE. (M) 2L72 4T4 TRTA8SW E4WE 19960613006041996061300604NM 1996 6 13 USAA960435 119950514A5311 FRAME BOEING737 7372Q9 138448MNM BS 727 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19230AU43662 21975 INT - DURING Q-4 CHECK EDDY CURRENT, FOUND TWO CRACKS .125 INCH LONG, STATION 727 STRINGER 18A RIGHT. REPLACED FRAME SECTION AND REPAIRED PER EO 5394G068. (M) 2L72 4F A16WE 19960619000011996061900001NM 1996 6 19 CA951108024 119951112A801138315212 STARTER BOEING727 727217 NM NR 2 ENG FAILURE W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 2346 (CAN) AFTER TAKEOFF, NR 2 FIRE WARNING ILLUMINATED. FIRE DRILL COMPLETED AND NR 2 ENGINE FIRE WARNING LIGHT EXTINGUISHED PRIOR TO FIRE BOTTLE DISCHARGE. AIRC RAFT RETURNED. NR 2 STARTER DISINTEGRATED. STARTER CHANGED. 2L73 4F RTA3WE 19960619000021996061900002NM 1996 6 19 CA951110001 119951104A2460 RELAY BOEING737 737217 1384464NM R4 TRANSFER FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA (CAN)ON CLIMB FLIGHT ATTENDANT NOTICED SMOKE IN CABIN, #2 FUEL BOOST PUMP CIRCUIT BREAKER POPPED. GALLEY POWER OFF, GASPER FAN OFF, AIR CONDITIONING SMOKE CHECKLIST ACCOMPLISHED AND SMOKE DISPATCHED. REPLA CED R4 TRANSFER RELAY DUE PHASE C UNSERVICEABLE, HIGH VOLTAGE ACROSS CONTACT. 2L72 4F A16WE 19960619000031996061900003NM 1996 6 19 CA951120011 219951103A7510577957 DUCT BOEING727 727212 138407GNM VALVE FLANGE RUPTURED W A AEJ UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL JK WARNING INDICATION FLUID LOSS CLCLIMB 1 CA 79 (CAN)DURING CLIMB OUT CREW OBSERVED A FIRE INDICATION ON #2 ENGINE. ENGINE SHUTDOWN AND FUEL DUMPED PRIOR TO LANDING. MAINTENANCE DISCOVERED THE FUEL HEATER SUPPLY LINE RUPTURED AT THE SHUT OFF VALVE INLETFLANGE. REPLACED. 2L73 4F A3WE 19960619000041996061900004NM 1996 6 19 CA951122006 119951117A56105893572 WINDOW PPG 5893572 BOEING737 737210C 1384459NM INNER PANE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 16487 86H110366 (CAN)DURING MAINTENANCE CAPTAINS #4 EYEBROWN WINDOW INNER PANE FOUND CRACKED. REPLACED. 2L72 4F A16WE 19960619000051996061900005NM 1996 6 19 CA951122021 119951109A26121825280037525 FIRE WIRE BOEING727 727212 138407GNM NR 2 ENG BROKEN W AE UNSCHED LANDING ENGINE SHUTDOWN JM WARNING INDICATION OVER TEMP CRCRUISE 1 CA (CAN)AFTER DEPARTURE THE CREW OBSERVED #2 ENGINE HAD A FIRE INDICATION AND HIGH OIL TEMPERATURE. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO BLOCKS. FIRE WIRE FOUND BROKEN, REPLACED. 2L73 4F A3WE 19960619000071996061900007NM 1996 6 19 CA951122028 119951109A7830 SWITCH BOEING727 727212 138407GNM NR 2 ENG TR INTERMITTENT W CD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CA (CAN)#2 ENGINE REVERSER LIGHT ILLUMINATED ON TAKEOFF ROLL. REJECTED. REVERSER LOCKED IN FORWARD AND LOCKED POSITION AND DEFERRED TO MEL 78.02. REVERSER POSITION SWITCH REPLACED. 2L73 4F A3WE 19960619000081996061900008WP 1996 6 19 CA951123104 119951031A2710 CABLE DOUG DC10 DC1030 3023501WP AILERON BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)AILERON LOCKOUT CABLE WAS FOUND BROKEN ON "A" CHECK. IT APPEARS THE CABLE JUMPED THE PULLEY AND OPERATED IN THIS STATE UNTIL IT FAILED. BROKEN CABLE WAS REPLACED AS PER MM 27-11-04. 2L73 4F A22WE 19960619000091996061900009NM 1996 6 19 CA951123105 119951027A2731654997013 JACK SCREW BOEING 654997013 BOEING737 737275C NM STAB TRIM CORRODED W O OTHER F FLT CONT AFFECTED DEDESCENT 1 CA 39960 00133 (CAN)ON DESCENT WITH AUTOPILOT ON, THE STAB OUT OF TRIM LIGHT CAME ON. DISCONNECTED AUTOPILOT AND ATTEMPTED TO RETRIM. POSSIBLE TO TRIM NOSE UP BUT NOT POSSIBLE TO TRIM NOSE DOWN ELECTRICALLY OR MANUALLY. CORROSION IN AUXILIARY BRAKE HOUSING AND BRAKE ARMS BINDING - STAB TRIM JACK SCREW REPLACED. 2L72 4F A16WE 19960619000101996061900010NM 1996 6 19 CA951123106 119951021A3010 CIRCUIT BREAKER BOEING737 737275 1384485NM NR 2 ENG AI MALFUNCTION W A UNSCHED LANDING O OTHER CLCLIMB 1 CA (CAN)CIRCUIT BREAKER #2 ENGINE AND WING ANTI-ICE POPPED AFTER USING ENGINE ANTI-ICE. ON ARRIVAL CIRCUIT BREAKER RESET AND VALVE OPERATION CHECKED NORMAL. CONNECTORS REMOVED FROM THREE VALVES AND INSPECTED.NO EVIDENCE OF ARCING. CIRCUIT BREAKER REPLACED ON SPEC. 2L72 4F A16WE 19960620001011996062000101NM 1996 6 20 RAAAB195009 119950223A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 LEFT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001021996062000102NM 1996 6 20 RAAAB195010 119950223A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001031996062000103NM 1996 6 20 RAAAB195012 119950223A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 RIGHT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001041996062000104NM 1996 6 20 RAAAB195013 119950916A35304566M37B042NM PBE BOEING727 72722C 138400FNM CABIN INFLATED A RAAAK NONE O OTHER ININSP/MAINT 1 AL03831RV 19093 DURING SERVICE CHECK, FOUND BULKHEAD P.B.E. GREEN SEAL MISSING AND LOSS OF VACUUM. CHANGED P.B.E. (X) 2L73 4F A3WE 19960620001051996062000105NM 1996 6 20 RAAAB195014 119950927A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 LEFT FORWARD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001061996062000106NM 1996 6 20 RAAAB195015 119951103A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 LEFT FORWARD ENTRANCE DOOR EGRESS LIGHT INOPERATIVE. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001071996062000107NM 1996 6 20 RAAAB195016 119951103A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 RIGHT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001081996062000108NM 1996 6 20 RAAAB195017 119951103A33508621006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 ROW 14 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001091996062000109NM 1996 6 20 RAAAB195018 119951103A33508621006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001101996062000110NM 1996 6 20 RAAAB195019 119951118A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 LEFT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001111996062000111NM 1996 6 20 RAAAB195020 119951118A33508621006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620001131996062000113NM 1996 6 20 RAAAE196001 119951115A335086821006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03831RV 19093 ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (X) 2L73 4F A3WE 19960620007801996062000780CE 1996 6 20 CA951010023 119950829A551112320005 SPAR CESSNA185 A185F 2072821CE L/H STAB INB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 8406 (CAN)THE LEFT HAND STABILIZER REINFORCEMENT BRACKET P/N 6732101-4 WAS FOUND TO BE CRACKED. IT WAS REMOVED AND REPLACED. UPON REMOVAL THE AFT SPAR WAS ALSO FOUND TO BE CRACKED. 1H71 3O 3A24 19960620007811996062000781CE 1996 6 20 CA951010024 119950911A551007321014 STABILIZER CESSNA185 A185F 2072821CE R/H INBOARD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4015 (CAN)THE RIGHT HAND REINFORCEMENT BRACKET WAS FOUND TO BE CRACKED. REPLACED. 1H71 3O 3A24 19960620007821996062000782CE 1996 6 20 CA951018022 119951004A32135012020258 ANGLE BEECH BEECH 100 A100 1152915CE DRAG LEG SUPP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 0 (CAN)DURING A DETAILED 150 HOUR INSPECTION OF THE DRAG LEG ATTACHED SUPPORT, A CRACK WAS FOUND AT THE BEND RADIUS. THE SUPPORTING STRUCTURE WAS FURTHER INSPECTED AND NO DAMAGE WAS FOUND. THE ANGLE WAS REPL ACED. SUBMITTER STATES THAT THIS IS THE FIRTST TIME A CRACK HAS BEEN FOUND IN THIS LOCATION. 1L72 3T A14CE 19960620007831996062000783CE 1996 6 20 CA951018027 119951010A553107310271 DOUBLER CESSNA 07310294 CESSNA185 A185F 2072821CE LH SIDE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3190 0 (CAN)CRACK FOUND DURING INSPECTION ON THE LEFT HAND SIDE OF THE RECESS FOR THE TORQUE TUBE. REFERENCE SB 95-2. 1H71 3O 3A24 19960620007841996062000784EA 1996 6 20 CA951027003 119951025A8000AA4N103YCD4N RELAY DHAV DHC8 DHC8311 1386006EA START CONTACTOR STUCK CLOSED W H DEACTIVATE SYST/CIRCUITS O OTHER TXTAXI/GRND HDL 1 CA (CAN)STARTER CONTACTOR STUCK CLOSED. 2H72 4T RTA13NM 19960620007851996062000785NM 1996 6 20 CA951027004 119951025A731210718D FUEL HEATER DHAV DHC8 DHC8102 2809003NM FUEL SYS FAILED W O OTHER M OVER TEMP CLCLIMB 1 CA 8707 (CAN)#2 FUEL TEMP AT RED LINE DURING CLIMB. FUEL/OIL HEAT EXCHANGER REPLACED. 2H72 4T RTA13NM 19960620007861996062000786NE 1996 6 20 CA951027005 219951026A7313 FUEL NOZZLE DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE RESTRICTORS DEFECTIVE W A CD ABORTED TAKEOFF RETURN TO BLOCK RK PARTIAL RPM/PWR LOSS FLUID LOSS TOTAKEOFF 1 CA 123049 (CAN)#2 ENGINE TORQUE WOULD NOT EXCEED 60 PERCENT ON TAKEOFF. INSPECTION NOTED A MAJOR FUEL LEAK. FUEL NOZZLE AT THE 9 O'CLOCK POSITION WAS FOUND TO HAVE RESTRICTORS MISSING FROM THE FUEL FEED TUBE SOCKETS ALLOWING THE TUBES TO SLIDE FAR ENOUGH INTO THE SOCKETS SO THEY DISENGAGED THE ADJACENT NOZZLE CAUSING A MASSIVE FUEL LEAK. THE NOZZLE HAD APPROXIMATELY 25 HOURS SINCE OVERHAUL. 2H72 4T4 TRTA13NM E20NE 19960620007871996062000787NE 1996 6 20 CA951102008 219951030A7230LK58499 PIN RROYCE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE COMP CASE LUGS MIGRATED W A K NONE O OTHER ININSP/MAINT 1 CA 0 10233 (CAN)ON ROUTINE INSPECTION OF #3 ENGINE LOW PRESSURE COMPRESSOR SUPPORT STRUCTURE, THE LEFT HAND LOWER ROD END LUG PIN WAS FOUND MIGRATED BY 2.0" AND THE RETAINING BOLT MISSING. THE RETAINING BOLT HAD BEEN FITTED AS WITNESS MARKS OF BOLT WERE IDENTIFIED ON TWO SEPARATE AREAS AT BASE OF TRANSFER DRIVE SHAFT L.P. CASE, ON REMOVAL OF TRANSFER DRIVE FAIRINGS. THE RETAINING BOLT WAS NOT RECOVERED. VISUAL INSPECTION OF THE AREA WAS CARRIED OUT SATISFACTORILY AND PIN + REPLACEMENT RETAINING BOLT WERE REFITTED. 2L73 4F4 F A23WE E12EU 19960620007881996062000788NM 1996 6 20 CA951103010 119951026A271082700521001 CONTROL CABLE DHAV DHC8 DHC8102 2809003NM RT AILERON WORN W O OTHER O OTHER NRNOT REPORTED 1 CA 16636 (CAN) AILERON CONTROL CABLE IN RIGHT HAND WING ROOT WORN DIRECTLY OUTBOARD OF SPLITTER QUADRANT. 2H72 4T RTA13NM 19960620007891996062000789EU 1996 6 20 CA951103103 119951012A21339023157038 OUTLFOW VALVE AIRBUS320 A320211 3930320EU CABIN PRESS INOPERATIVE W IBA CABIN DEPRESSURIZATION EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 1422 1352 (CAN)CABIN PRESSURE 1 & 2 FAULT IN CRUISE AT FL350, UNABLE TO CONTROL MANUALLY. FLIGHT CREW REPORTED EAR PAIN FOLLOWED BY ECAM WARNING, CABIN ALTITUDE AT 8500 FEET AND CLIMBING, OUTFLOW VALVE INDICATING FU LL OPEN. NO APPRECIABLE POSITION CHANGE WHEN STANDBY SYSTEM TOGGLED TO CLOSED. EMERGENCY DESCENT INITIATED. STANDBY CONTROL OF THE OUTFLOW VALVE WAS LATER CONFIRMED AND THE CABIN PRESSURE WAS MANUALLY CONTROLLED DURING DESCENT. OUTFLOW VALVE WAS REPLACED AND TESTED SERVICEABLE. 2L72 4F RTA28NM 19960627003081996062700308NM 1996 6 27 96ZZZX3122 119950110A2133 OUTFLOW VALVE BOEING767 767259 1385136NM CABIN MALFUNCTIONED W ANCFG O2 MASK DEPLOYED J WARNING INDICATION NRNOT REPORTED 1 SO23985AN 24618 PAR/BOG - FLT 015 - AUTO INOP LIGHT ILLUMINATED. EICAS MESSAGE, CABIN AUTO INOP AND CABIN ALT AUTO 1 AND DISPLAYED. OPERATION IN MANUAL MODE WAS OK. CABIN ALTITUDE WARNING AND MESSAGE CAME ON. OXYGEN MASKS WERE DROPPED BY PILOTS. PERFORMED BITE PROCEDURE IAW FIM 21-30-00, PAGE 109. OUTFLOW VALVE CHANGED. CYCLES, 4,953. HOURS, 23,854. 2L72 4F RTA1NM 19960627003151996062700315NM 1996 6 27 96ZZZX3129 119951101A6230900CF010210101 LINK DOUG MD900 MD900 3027375NM M/R MAST WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11901CF173 90000012 LINK WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003161996062700316NM 1996 6 27 96ZZZX3130 119951103A3210900F2361503101 PAD DOUG MD900 MD900 3027375NM MLG WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11901CF178 90000012 PAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS 4 EACH, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003171996062700317NM 1996 6 27 96ZZZX3131 119951202A5210683733 HANDLE DOUG MD900 MD900 3027375NM DOOR WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11901CF230 90000012 DOOR HANDLE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003181996062700318NM 1996 6 27 96ZZZX3132 119951225A6230900C2010184103 SCISSORS DOUG MD900 MD900 3027375NM M/R WORN A R7MAK NONE E VIBRATION/BUFFET ININSP/MAINT 1 NM11901CF294 90000012 SCISSORS WORN BEYOND SERVICEABLE LIMITS. CAUSING MR VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003201996062700320NM 1996 6 27 96ZZZX3134 119951223A2510900N3201141103 SEAT ASSY DOUG MD900 MD900 3027375NM CREW WILL NOT ADJ A R7MAK NONE O OTHER ININSP/MAINT 1 NM1191CF 287 90000012 PILOT SEAT WILL NOT ADJUST FORE OR AFT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003211996062700321NM 1996 6 27 96ZZZX3135 119950928A7810900D2630103101 EXHAUST STACK DOUG MD900 MD900 3027375NM ENGINE CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM11901CF100 90000012 EXHAUST STACK CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627003291996062700329NM 1996 6 27 96ZZZX3143 119951126A7931900P365000101 SENSOR DOUG MD900 MD900 3027375NM ENGINE OIL FLUCTUATES A R7MAK NONE O OTHER ININSP/MAINT 1 NM11901CF217 90000012 PRESSURE SENSOR CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH19NM 19960627005601996062700560NM 1996 6 27 RAAAB295017 119950628A33508621006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 ROW 22 FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (M) 2L73 4F A3WE 19960627005611996062700561NM 1996 6 27 RAAAB295018 119950628A335086210144 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 LEFT FWD OVERWING EXIT EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M) 2L73 4F A3WE 19960627005621996062700562NM 1996 6 27 RAAAB295019 119950714A33501000679 LIGHT BOEING727 72722C 138400FNM CABIN FAILED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 MID CABIN SERVICE DOOR EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY. (M) 2L73 4F A3WE 19960627005631996062700563NM 1996 6 27 RAAAB295020 119950714A33508621014 BATTERY PACK 873100212 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 MID CABIN DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M) 2L73 4F A3WE 19960627005641996062700564NM 1996 6 27 RAAAB295021 119950714A33508621014 BATTERY PACK 873100212 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 AFT CABIN DOOR EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE TO LOW CHARGE. (M) 2L73 4F A3WE 19960627005651996062700565NM 1996 6 27 RAAAB295022 119951015A3350873100112 LIGHT BOEING727 72722C 138400FNM CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 ROW 22 FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. (M) 2L73 4F A3WE 19960627005661996062700566NM 1996 6 27 RAAAB295023 119951015A3350873100212 LIGHT BOEING727 72722C 138400FNM CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 RIGHT FORWARD OVERWING EXIT EGRESS LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. (M) 2L73 4F A3WE 19960627005671996062700567NM 1996 6 27 RAAAB295024 119951022A3350873100112 LIGHT BOEING727 72722C 138400FNM CABIN INOPERATIVE A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 ROW 22 FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. REPLACED LIGHT ASSEMBLY. (M) 2L73 4F A3WE 19960627005681996062700568NM 1996 6 27 RAAAB295029 119950628A33508621006 BATTERY PACK 873100112 BOEING727 72722C 138400FNM CABIN DISCHARGED A RAAAK NONE L NO TEST ININSP/MAINT 1 AL03832RV 19098 ROW 22 FLOOR PROXIMITY LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE TO LOW CHARGE. (M) 2L73 4F A3WE 19960627006271996062700627NM 1996 6 27 CA951030004 119951005A5300 FUSELAGE DHAV DHC8 DHC8102 2809003NM NOSE LIGHTNING STRIKEW A UNSCHED LANDING C F.O.D. CRCRUISE 1 CA (CAN)AIRCRAFT STRUCK BY LIGHTNING. DAMAGE TO NOSE AREA REPORTED BY PILOT. OTHER DAMAGE FOUND INCLUDED DAMAGE TO #3 BLADE OF L/H PROP, R/H AILERON ASSEMBLY, AND STRUCTURAL DAMAGE TO NOSE AREA. 2H72 4T RTA13NM 19960627006281996062700628NM 1996 6 27 CA951102005 119951029A760287600518001 CABLE 85410010001 DHAV DHC8 DHC8102 2809003NM CONDITION LEVER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 17047 0 (CAN)20 TO 30 STRANDS OF CONDITION LEVER CABLE FOUND BROKEN IN AREA THAT GOES OVER FIRE WALL PULLEY 2H72 4T RTA13NM 19960627006291996062700629NM 1996 6 27 CA951103011 119951026A271082700522001 CONTROL CABLE DHAV DHC8 DHC8102 2809003NM RT AILERON WORN W O OTHER O OTHER NRNOT REPORTED 1 CA 16636 (CAN) AILERON CONTROL CABLE IN RIGHT HAND WING ROOT WORN DIRECTLY OUTBOARD OF SPLITTER QUADRANT. 2H72 4T RTA13NM 19960627006301996062700630NE 1996 6 27 CA951108002 219951103A7421CH34687A IGNITER PLUG CHAMPION DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE ENGINE INSERT LOOSE W K NONE O OTHER ININSP/MAINT 1 CA 0 120056 (CAN)PORCELAIN INSERT FELL OUT OF THE IGNITER PLUG AND JAMMED IN THE HIGH PRESSURE TURBINE. THE ENGINE WAS REPLACED AS IT WAS NEARING A HOT SECTION INSPECTION (HSI). 2H72 4T4 TRTA13NM E20NE 19960627006311996062700631NM 1996 6 27 CA951108003 119951103A792128E997 OIL COOLER JANITROL DHAV DHC8 DHC8102 2809003NM ENG OIL LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 5612 0 (CAN)OIL COOLER LEAKING ON WELD. 2H72 4T RTA13NM 19960627006321996062700632NM 1996 6 27 CA951108012 119951027A5330 SKIN DHAV DHC8 DHC8102 2809003NM BEHIND NLG LIGHTNING STRIKEW K NONE C F.O.D. CRCRUISE 1 CA (CAN)HILE CRUISING AT 16,000 FEET AIRCRAFT STRUCK BY LIGHTNING. MOSTLY COSMETIC DAMAGE TO RADOME AND SEVERAL EXIT POINTS ALONG BELLY BEHIND NOSE LANDING GEAR. NO CRACKING OR DISBONDING NOTED. 2H72 4T RTA13NM 19960627006331996062700633NM 1996 6 27 CA951114004 119951111A323182910010175 LINE DHAV DHC8 DHC8301 NM NLG LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN)HYDRAULIC LEAK FROUND IN NOSE LANDING GEAR BAY FROM GEAR EXTEND RETRACT LINE TO NLG DOOR. 2H72 4T RTA13NM 19960627006341996062700634NM 1996 6 27 CA951116015 119951105A575469378451 HINGES BOEING737 7372A9C 1384495NM OUTB FLAP NR 2-3CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING ROUTINE INSPECTION THE #2 AND #3 OUTER KRUEGER FLAP HINGES SIGNIFICANTLY CORRODED, EXFOLIATION, AT THE TOP END PIVOT. REPLACED. 2L72 4F A16WE 19960627006351996062700635NE 1996 6 27 CA951116017 219951103A7260UL29500 DRIVE SHAFT RROYCE BOEING757 75728A 1384976NM RROYCERB211 RB211535E4 54555NE ACCESS GEARBOX BEARING WORN W K NONE O OTHER ININSP/MAINT 1 CA 0 30779 (CAN)WHILE DOING SCHEDULED MAINTENANCE BRONZE METAL CONTAMINATION WAS FOUND IN THE SCAVENGE OIL FILTER. INSPECTION REVEALED THE INNER BEARING ON THE RADIAL DRIVE SHAFT, IN THE ACCESSORY GEARBOX, HAD EXCESSIVE PLAY DUE TO WEAR OF THE BRONZE BEARING CAGE. THE RADIAL DRIVE SHAFT AND THE INNER BEARING WERE REPLACED. 2L72 4F4 FRTA2NM E12EU 19960627006361996062700636NE 1996 6 27 CA951122030 219951116A7230 FAN BLADES RROYCE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE ENG COMPRESSOR FOD ICE DAMAGE W CD ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TOTAKEOFF 1 CA 10145 (CAN)TAKEOFF REJECTED DUE TO ENGINE PARAMETERS BELOW REQUIREMENTS. HIGH N1 AND LOW EPR. DURING RUN-UP PARAMETERS WERE FOUND NORMAL AT LOW POWER SETTINGS. CREW DID NOT BRING TO HIGHER POWER DUE TO HEAVY ENG INE RUMBLE HEARD IN THE COCKPIT. DURING VISUAL INSPECTION 7 FAN BLADES WERE FOUND BENT AND THE ACCOUSTIC LINING DAMAGE AROUND THE BLADES DUE TO ICE INGESTION. ACCOUSTIC LINING REPAIRED AND FAN BLADES REPLACED. 2L73 4F4 F A23WE E12EU 19960627006371996062700637WP 1996 6 27 CA951123101 119951113A3411 PITOT HEAD PQH4S1M1 DOUG DC10 DC1030 3023501WP 1ST OFF AIR SPD FOD BLOCKAGE W A CD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CA 0 (CAN)ON TAKEOFF ROLL, 1ST OFFICER ASI REMAINED AT ZERO, TAKEOFF ABORTED1ST OFFICER'S ASI REPLACED MAINTENANCE INVESTIGATION REVEALED A CLEVIS SCREW (FOD) WAS FOUND INSERTED IN THE PITOT INLET OPENING P RIOR TO DEPARTURE, THE AUTO THROTTLE SYSTEM WAS TESTED AND A LEAK CHECK OF THE F/O'S PITOT WAS CARRIED OUT. THE FOD ITEM WAS IDENTIFIED AS AN AN24-14A CLEVIS BOLT, THE SAME TYPE AS SOCK SECURING BRACKET PIVOT BOLT. APPARENTLY THE SCREW WAS INADVERTENTLY LEFT IN THE PITOT HEAD INLET WHEN THE SOCK WAS REMOVED. IT IS RECOMMENDED THE SOCKS BE STORED WITH DUMMY PITOT HEADS INSTALLED. 2L73 4F A22WE 19960627006381996062700638NM 1996 6 27 CA951129502 119950929A3244 TIRE BOEING747 747133 138448BNM NR 4 MAIN BLOWN W O OTHER O OTHER LDLANDING 1 CA (CAN)AFTER TOUCHDOWN THE #4 MAIN WHEEL TIRE, LHR BLEW. DENT UNDER #6 SPOILER. 2L74 4F A20WE 19960627006391996062700639WP 1996 6 27 CA951129503 119950929A2530CA167072 RECEPTACLE DOUG DC9 DC932 3022066WP NR 1 OVEN BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN)A BURNING ELECTRICAL SMELL WAS DETECTED IN THE GALLEY AREA. INVESTIGATION REVEALED #1 OVEN RECEPTACLE WAS BURNT. DEFECTIVE ELECTRICAL RECEPTACLE REPLACED. 2L72 4F A6WE 19960703001181996070300118NM 1996 7 3 96ZZZX3277 119950915A71106553553152 COWLING 6585278388 BOEING737 737247 138448DNM NR 2 ENGINE WORN A VSTAK NONE O OTHER ININSP/MAINT 1 WP07302VA 0302 20126 TUS - MAINTENANCE REPORT NR 2 ENGINE NOSE COWL WORN 50 PERCENT OF DEPTH IN .040 INCH, 2024T3 SKIN UNDER MATING SURFACE OF FORWARD WING TO NACELLE FAIRING. FABRICATED DOUBLER .040 INCH, 2024T3, 2 FASTENER ROWS WIDER THAN EXISTING DAMAGE AND REPAIRED PER SHIVA ENT., INC., E.O. 354E004 AND APPROVED FAA FORM 8110-3, REPORT 95-9, DATED 9-14-95. ACFT TT: 51,945.9 HOURS. TOTAL CYCLES, 60,051. 2L72 4F A16WE 19960703001191996070300119NM 1996 7 3 96ZZZX3278 119950622A5270188929 POS SWITCH BOEING737 737247 138448DNM AFT ENTRY DOOR INOPERATIVE A VSTAO OTHER P NO WARNING INDICATION NRNOT REPORTED 1 WP07302VA 20126 RNO - FLT 2302 - AFT ENTRY DOOR OPEN. INDICATION IN COCKPIT INOPERATIVE. TROUBLESHOT IAW CHAPTER 52, PER DOOR POSITION SWITCH. OPS CHECK GOOD. 2L72 4F A16WE 19960703001201996070300120NM 1996 7 3 96ZZZX3279 119950721A324426015711 TIRE BOEING737 737247 138448DNM NR 2 MAIN FAILED A VSTAK NONE O OTHER ININSP/MAINT 1 WP07302VA 20126 PIT - FLT 2302 - UPON ARRIVAL AT GATE, GROUND CREW INFORMED PILOTS NR 2 MAIN TIRE BLOWN. DEBRIS ON RUNWAY SLASHED NR 2 MAIN TIRE ON LANDING ROLL-OUT. REPLACED NR 1 AND NR 2 MAIN WHEEL ASSYS AND NR 2 BRAKE ASSY AS PRECAUTIONARY. 2L72 4F A16WE 19960703001211996070300121NM 1996 7 3 96ZZZX3280 119950806A3350 BULB BOEING737 737247 138448DNM CABIN FAILED A VSTAK NONE L NO TEST ININSP/MAINT 1 WP07302VA 20126 ACY - FLT 2302 - EMERGENCY TRACK LIGHTS INOPERATIVE. RED LENS MISSING. REPLAMPED AND REPLACED MISSING LENS AS REQUIRED. 2L72 4F A16WE 19960703001221996070300122NM 1996 7 3 96ZZZX3281 119950731A3350 BULB BOEING737 737247 138448DNM CABIN FAILED A VSTAK NONE L NO TEST ININSP/MAINT 1 WP07302VA 20126 ACY - FORWARD EMERGENCY LIGHTS, ROW 15, INOPERATIVE. T/S SYSTEM. REPAIRED BROKEN WIRE FROM SIDEWALL TO TRACK. RELAMPED ALL BULBS BLOWN AND RETORQUED SCREW AND NUT ON GROUND CAUSING SHORT GROUND. 2L72 4F A16WE 19960703001231996070300123NM 1996 7 3 96ZZZX3282 119950817A3397 WIRE BOEING737 737247 138448DNM CABIN BROKEN A VSTAK NONE L NO TEST ININSP/MAINT 1 WP07302VA 20126 ACY - ROWS 11 TO 17 EMERGENCY TRACK LIGHTS INOPERATIVE. TROUBLESHOT, REPAIRED BROKEN WIRE. OPS CHECKED GOOD. 2L72 4F A16WE 19960703001241996070300124NM 1996 7 3 96ZZZX3283 119950816A2560 SLIDE BOTTLE BOEING737 737247 138448DNM L1 DOOR LOW PRESSURE A VSTAK NONE O OTHER ININSP/MAINT 1 WP07303VA 20125 MEM - SLIDE PRESSURE LOW. REMOVED L1 SLIDE, SERVICED BOTTLE IAW CMM 25-60-10. REINSTALLED L1 SLIDE IAW MM 25-61-311. 2L72 4F A16WE 19960703001251996070300125NM 1996 7 3 96ZZZX3284 119950528A27505701801 BALLSCREW ASSY BOEING737 737247 138448DNM TE FLAP INOPERATIVE A AVSTAK NONE O OTHER ININSP/MAINT 1 WP07303VA 3298R 20125 MEM - FLT 8303 - FLAPS WILL NOT EXTEND BELOW 15 DEGREES IN-FLIGHT. OPERATES NORMALLY ON GROUND. REMOVED AND REPLACED NR 1 BALLSCREW ASSY IAW MM REF 27-51-281. 2L72 4F A16WE 19960703001261996070300126NM 1996 7 3 96ZZZX3285 119950525A2750 BRACKET BOEING737 737247 138448DNM NR 1 FLAP FRNG OUT OF POSITION A AVSTAO OTHER J WARNING INDICATION APAPPROACH 1 WP07303VA 20125 MSY - FLT 8303 - FLAPS FAILED TO EXTEND ON APPROACH TO MSY. FOUND FORWARD BRACKET ON RETRACTABLE LANDING LT CONTROL ARM IN NR 1 FLAP FAIRING LOOSE AND MIGRATED UPWARDS BLOCKING 360 DEGREE ROTATION OF THE NR 1 BALL NUT. BRACKET RESTORED TO NORMAL POSITION. TURN BOLTS TIGHTENED AND SAFETIED. OPERATION OF FLAPS SATISFACTORY. 2L72 4F A16WE 19960703001271996070300127NM 1996 7 3 96ZZZX3286 119950915A5330 SKIN BOEING737 737247 138448DNM BS 257-277 CORRODED A VSTAK NONE O OTHER ININSP/MAINT 1 WP07309VA 19614 TUS - MAINTENANCE REPORT OF CORROSION AT FORWARD LAVATORY SERVICE PANEL SKIN AND REINFORCING DOUBLER, STA 257 TO STA 277, BETWEEN STR 23R AND STR 24R. AFTER CORROSION REMOVAL, FOUND REMAINING SKIN TO BE WITHIN LIMITS, IAW 737 SRM 53-30-1. FABBED SKIN AND REINFORCING DOUBLER IAW 737 SRM 51-10-1 AND SRM 53-30-3, AND REPAIRED SAME IAW SHIVA ENT., E.O. 353E021, REPORT 95-8 DATE 9-14-95 ON FAA FORM 8110-3. ACFT TOTAL TIME, 58,386.8 HOURS. TOTAL CYCLES, 65,586. 2L72 4F A16WE 19960703001281996070300128NM 1996 7 3 96ZZZX3287 119950928A55406549837503 FITTING BOEING737 737284 138448RNM RUDDER CRACKED A AVSTAK NONE O OTHER ININSP/MAINT 1 WP07310VA 001 21501 TUS - MAINTENANCE REPORT OF RUDDER ATTACH POINT WEB ASSEMBLY BEING CRACKED UPON INSPECTION FOR RUDDER INSTALLATION (RUDDER ATTACH POINT NR 2). UPON INSPECTION, FOUND MAINTENANCE PROCEDURES FOR REMOVAL OF RUDDER WERE NOT STRICTLY ADHERED TO. THE REMOVAL CALLS FOR THE LOCK OUT OF THE MANUAL OVERRIDE LEVER ON THE STANDBY AND HYDRAULIC MODULAR PACKAGES IN THE OFF POSITION, AND THE DISCONNECTION OF ELECTRICAL CONNECTORS FROM FLIGHT CONTROL A AND B SHUT-OFF VALVES. AIRCRAFT TOTAL TIME, 37,835.5 HOURS. TOTAL CYCLES, 52,921. 2L72 4F A16WE 19960703001291996070300129NE 1996 7 3 96ZZZX3288 219950901A7230845601 C-1 BLADE BOEING737 737247 138448DNM PWA JT8 JT8D9A 52048NE ENG COMPRESSOR DAMAGED A VSTAK NONE C F.O.D. ININSP/MAINT 1 WP07309VA 19614 IFP - FLT 3225 - EN ROUTE IFP - NR 2 ENGINE ENCOUNTERED A BIRD STRIKE. UPON INSPECTION, FOUND BIRD STRIKE DAMAGED, 3 EACH N1 FAN BLADES. REPLACED NOTED BLADES. BORESCOPE LP COMPRESSOR. NO DAMAGE FOUND. ENGINE RUN AND ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 F A16WE E2EA 19960703001301996070300130NM 1996 7 3 96ZZZX3289 119950712A523065479521 LOWER CORNER BOEING737 737247 138448DNM CARGO DOOR CRACKED AS VSTAK NONE O OTHER ININSP/MAINT 1 WP074501W 19598 LAS - FLT 430 - AIRCRAFT HAD DIFFICULTY MAINTAINING CABIN PRESSURE. CRACK IN UPPER CORNER OF FORWARD GALLEY DOOR AFT FRAME, AND CRACK IN LOWER CORNER OF AFT CARGO DOOR FORWARD FRAME. REPLACED CRACKED DOORS WITH SERVICEABLE DOORS. AIRCRAFT TOTAL TIME, 50,727.9 HRS. AIRCRAFT CYCLES, 59,847. 2L72 4F A16WE 19960703001311996070300131NM 1996 7 3 96ZZZX3290 119950712A524065458712 UPPER CORNER BOEING737 737247 138448DNM SERVICE DOOR CRACKED A VSTAK NONE O OTHER ININSP/MAINT 1 WP074501W 19598 LAS - FLT 430 - AIRCRAFT HAD DIFFICULTY MAINTAINING CABIN PRESSURE. CRACK IN UPPER CORNER OF FORWARD GALLEY DOOR AFT FRAME, AND CRACK IN LOWER CORNER OF AFT CARGO DOOR FORWARD FRAME. REPLACED CRACKED DOORS WITH SERVICEABLE DOORS. AIRCRAFT TOTAL TIME, 50,727.9 HRS. AIRCRAFT CYCLES, 59,847. 2L72 4F A16WE 19960703001321996070300132NM 1996 7 3 96ZZZX3291 119950712A523065479521 AFT CORNER BOEING737 737247 138448DNM CARGO DOOR CRACKED A VSTAK NONE O OTHER ININSP/MAINT 1 WP074501W 19598 LAS - FLT 430 - AIRCRAFT CABIN PRESSURE WAS DIFFICULT TO MAINTAIN. CRACK IN LOWER CORNER OF AFT CARGO DOOR FORWARD FRAME. AIRCRAFT TOTAL TIME: 50,727.9 HOURS. AIRCRAFT TOTAL CYCLES, 59,847. 2L72 4F A16WE 19960703001331996070300133NM 1996 7 3 96ZZZX3292 119950712A524165458712 CORNER BOEING737 737247 138448DNM GALLEY DOOR CRACKED A VSTAK NONE O OTHER ININSP/MAINT 1 WP074501W 19598 LAS - FLT 430 - AIRCRAFT CABIN PRESSURE WAS DIFFICULT TO MAINTAIN. CRACK IN UPPER CORNER OF FORWARD GALLEY DOOR AFT FRAME. AIRCRAFT TOTAL TIME, 50,727.9 HOURS. AIRCRAFT TOTAL CYCLES, 59,847. 2L72 4F A16WE 19960703001341996070300134NM 1996 7 3 96ZZZX3293 119950726A7931 PRESS SW TUBE BOEING737 737247 138448DNM NR 2 ENG LEAKING A VSTAE ENGINE SHUTDOWN K FLUID LOSS NRNOT REPORTED 1 WP074501W 19598 FAT - FLT 433 - NR 2 ENGINE LOST OIL PRESSURE. CREW SHUT DOWN ENGINE IN-FLIGHT. OIL LEAKING OUT THROUGH OIL PRESSURE SWITCH TUBE, 'BANJO' FITTING. 2L72 4F A16WE 19960703001351996070300135NM 1996 7 3 96ZZZX3294 119950219A3397 WIRE BOEING737 737247 138448DNM CABIN FAILED A VSTAK NONE L NO TEST ININSP/MAINT 1 WP074501W 19598 ROW 7, FLOOR TRACK LIGHTING INOPERATIVE. REPAIRED WIRING IAW MM STANDARD PRACTICES. OPS CHECKED GOOD. 2L72 4F A16WE 19960703001361996070300136NM 1996 7 3 96ZZZX3295 119950123A3397 WIRE BOEING737 737247 138448DNM CABIN FAILED A VSTAK NONE L NO TEST ININSP/MAINT 1 WP074501W 19598 TRACK LIGHTS DIM AT FORWARD CABIN. REPAIRED FAULTY WIRING IAW MM 33-51-01. OPS CHECK GOOD. 2L72 4F A16WE 19960703001371996070300137NE 1996 7 3 96ZZZX3296 219950828A7261 OIL SYSTEM BOEING737 737247 138448DNM PWA JT8 JT8D9A 52048NE ENGINE LEAKING A VSTAO OTHER K FLUID LOSS ININSP/MAINT 1 WP074501W 19598 LAS - FLT 432 - UPON ARRIVAL LAS, POST-FLIGHT INSPECTION, MAINTENANCE FOUND OIL ACCUMULATION IN TAILPIPE AREA BELOW TURBINE EXHAUST CONE. INSPECTED CSD OIL COOLER, NO LEAKS FOUND. INSPECTED NR 4, NR 5, AND NR 6 PRESSURE TUBES, AND NR 6 BEARING COMPARTMENT FOR LEAKS. NONE FOUND. REMOVED NR 6 BEARING SCAVENGE PUMP PER MM 72-50, NO CARBON FOUND COLD STREAM DRY. 2L72 4F4 F A16WE E2EA 19960703002971996070300297WP 1996 7 3 AALA950787 119950518A2722 B-NUT DOUG DC9 DC982 3022082WP RUDDER ACTUATOR LOOSE A AALAK NONE B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW0770425 49337 DFW - FLT 1532 - AFTER TAKEOFF ABQ, DURING INITIAL CLIMB-OUT, STRONG BURNING ODOR BRIEFLY NOTED IN CABIN. NO OTHER ABNORMAL INDICATIONS AND AIRCRAFT PROCEEDED DFW, LANDING WITHOUT INCIDENT. RESECURED B-NUT FOUND LEAKING ON RUDDER ACTUATOR. REPLACED ALL AIR CYCLE MACHINE COALESCER BAGS AND ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO ODOR NOTED. (M) 2L72 4F A6WE 19960708000021996070800002NM 1996 7 8 CA951012002 119951004A2760 ACTUATOR DHAV DHAV DHC8 DHC8102 2809003NM SPOILER QUAD JAMMED W A O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 15729 0 (CAN)ROLL CONTROL JAMMED DURING APPROACH AT 50 FEET. CREW WERE TRYING TO INPUT RIGHT ROLL. A FORCE OF 10 LBS WAS APPLIED TO CONTROL AND CONTROL CAME FREE. AIRCRAFT LANDED OK. LH AND RH ROLL SPOILER QUADRANT, LOWER JAM SWITCH WIRE CLAMP RUBBING ON ACCESS PANELS 532DB (LH) AND 632DB (RH). GROOVES HAVE BEEN WORN IN PANELS AND WIRE CLAMP WAS CATCHING IN GROOVE AND JAMMING CONTROL. 2H72 4T RTA13NM 19960708000031996070800003SO 1996 7 8 CA951018201 119950903A78206689403 MUFFLER PIPER 6689403 PIPER PA28 PA28140 7102802SO ENG EXH FAILED W A A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 0 (CAN)THE PILOT WAS EXPERIENCING ENGINE DEGRADATION AND DECIDED TO LAND. THE AME WITH A PILOTS LICENCE, ARRIVED & INSPECTED THE AIRCRAFT AND HE DECIDED TO PROCEED BASE. WHILE IN CRUISE HE EXPERIENCED LOWER THAN NORMAL ENGINE RPM. UPON ARRIVAL AT BASE THE INSPECTION WAS STARTED AND SEVERAL ITEMS WERE FOUND. THE SPARK PLUGS WERE CHANGED AND THE CARBURETOR WAS CHANGED DUE TO A POROUS FLOAT, ALSO THE RPM GAUGE WAS FOUND TO BE READING LOW BY APPROXIMATELY 100 RPM. THESE REPAIRS PROVED TO BE ACCEPTABLE ON GROUND RUN BUT THE RPM WOULD DECAY IN FLIGHT. AN AUDIBLE RATTLE WAS PRESENT AT IDLE. THIS WAS FOUND TO BE CAUSED BY A BREAKDOWN INSIDE THE EXHAUST PIPE. THE BROKEN PIECES WERE BLOCKING EXHAUST FLOW INTERMITTENTLY. 1L71 3O 2A13 19960708000041996070800004EA 1996 7 8 CA951026015 219950829A8530 CYLINDER PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA NR 5 CYL DISINTEGRATED W A AE UNSCHED LANDING ENGINE SHUTDOWN EKYVIBRATION/BUFFET FLUID LOSS ENGINE STOPPAGE CRCRUISE 1 CA 1523 L1659248 (CAN)THE #5 CYLINDER WAS TORN OFF THE ENGINE BLOCK. THE PISTON BROKE INTO A THOUSAND PIECES AND ALL THE REST OF THE CENTRAL PARTS WHICH KEEP THE ENGINE TOGETHER WERE CRACKED. IT IS THOUGHT THAT EITHER THE #5 CYLINDER PISTON OR PISTON PIN FAILED AND THE RESULT WAS A DESTROYED ENGINE. 1L72 3O3 O 1A10 1E4 19960708000051996070800005WP 1996 7 8 CA951116001 119951027A7603580291751 CABLE ASSY DOUG DC10 DC1030 3023501WP OUTER SLEEVE BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)THE CONTROLEX CABLE FOR THRUST CONTROL OF #2 ENGINE WHICH RUNS FROM THE THRUST DRUM (PYLON AREA) TO THE THRUST QUADRANT ON THE ENGINE HAD A BROKEN OUTER SLEEVE. PROBLEM WAS FOUND DURING ROUTINE INSPECTION AT THE #14 CHECK. DEFECTIVE CONTROL ASSEMBLY REPLACED. 2L73 4F A22WE 19960708000061996070800006EA 1996 7 8 CA951129501 119950807A322016400103 DRAG BRACE CNDAIRCL600 CL6002B19 EA NOSE GEAR FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN)NOSE LANDING GEAR DID NOT RETRACT. CHANGED NLG DRAG BRACE ASSEMBLY. 2L72 4F RTA21EA 19960708000071996070800007EU 1996 7 8 CA951129504 119950928A2752791A000003 ACTUATOR AIRBUS320 A320211 3930320EU NR 1 INB FLAP FAILED W O OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 CA (CAN)DURING APPROACH FLAPS LOCKED OUT AT FLAP 2 SELECTION. MAINTENANCE REPLACED #1 INBOARD LEFT FLAP ACTUATOR. 2L72 4F RTA28NM 19960708000081996070800008WP 1996 7 8 CA951129505 119951001A5240 OIL PANEL DOUG DC9 DC932 3022066WP RH ENGINE MISSING W K NONE O OTHER UKUNKNOWN 1 CA (CAN)RIGHT ENGINE OIL ACCESS PANEL FOUND MISSING. NEW PANEL INSTALLED. 2L72 4F A6WE 19960708000121996070800012EU 1996 7 8 CA951027002 119951025A5610NF20216245 WINDSHIELD BAG BAE146BAE146200A 1500266EU OUTERPLY CRACKED W O OTHER O OTHER CRCRUISE 1 CA 9112 (CAN)LEFT OUTER 'A' SCREEN BADLY CRACKED IN FLIGHT AT 31,000 FEET. 2H74 4F RTA49EU 19960710004221996071000422NM 1996 7 10 CA951114002 119951111A3412 WIRE DHAV DHAV DHC8 DHC8101 2809002NM TEMP BULB BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 22621 0 (CAN)OUTSIDE AIR TEMP INDICATOR NOT INDICATING CORRECTLY. DIGITAL AIR DATA COMPUTER (DADC) INVALID. AUTOPILOT AND YAW DAMPER FAILED. BROKEN WIRE FOUND AT TEMPERATURE BULB CONNECTOR. 2H72 4T RTA13NM 19960710004231996071000423EU 1996 7 10 CA951114003 119951104A750032829703 STOP VBV 301774705 AIRBUS320 A320211 3930320EU GE CFM56 CFM565A 13802NE NR 1 ENG SEIZED W A A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 11511 5303 731623 (CAN)ON CLIMB AT APPROXIMATELY 1500 FEET THE #1 EGT WAS OBSERVED TO BE IN THE CAUTION RANGE. THE POWER WAS REDUCED MANUALLY ON MAINTENANCE INPUT THEN TRIED AGAIN WITH ANTI-ICE ON, THEN WITH #1 ENGINE BLEEDAIR OFF, PROBLEM REMAINED. SUBSEQUENT MAINTENANCE ACTION FOUND VBV FUEL GEAR MOTOR, STOP SEIZED. DEFECTIVE VALVE REPLACED. 2L72 4F4 FRTA28NM E29NE 19960710004241996071000424WP 1996 7 10 CA951129507 119951006A792079589011 OIL LINE DOUG DC9 DC932 3022066WP LT ENG FILTER LEAKING W E ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CA (CAN)ON CLIMB OUT, LEFT ENGINE OIL PRESSURE FLICKERED & OIL QUANTITY LOST. LEFT ENGINE SHUT DOWN. AIRCRAFT RETURNED TO DEPARTURE TERMINAL. MAINTENANCE ACTION INVOLVED CHANGING OIL LINE AT OIL FILTER DIFFER ENTIAL PRESSURE SWITCH. AIRCRAFT CHECKED FOR LEAKS ON GROUND RUN. 2L72 4F A6WE 19960710004251996071000425WP 1996 7 10 CA951129519 119951018A3246 WHEEL ASSEMBLY DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE MLG & NLG SEIZED W C ABORTED TAKEOFF E VIBRATION/BUFFET TOTAKEOFF 1 CA (CAN)A LOUD RATTLING NOISE WAS HEARD COMING FROM NOSE WHEEL WELL AREA ON TAKEOFF. REJECTED TAKEOFF AT 80 KNOTS. A 180 DEGREE TURN WAS EXECUTED, AIRCRAFT TAXIED 100 FEET AND STOPPED. A LOUD WINDING DOWN NOI SE WAS HEARD IN NOSE WHEEL WELL AREA AS BRAKE SET. UNABLE TO MOVE AFTER BRAKES SET. MAINTENANCE INSPECTION FOUND #1 & #2 BRAKE CARRIERS SEIZED. MAINTENANCE ACTION INVOLVED REPLACING BRAKE CARRIERS, #1 & #2 MAIN WHEEL AND NOSE WHEEL ASSEMBLIES. 2L72 4F4 F A6WE E2EA 19960710004261996071000426WP 1996 7 10 CA951129523 119951028A2120 DUCT DOUG DC9 DC932 3022066WP CABIN PRESS DISCONNECTED W B EMER. DESCENT J WARNING INDICATION CLCLIMB 1 CA (CAN)PRESSURIZATION UNCONTROLLABLE GOING THROUGH FL200, EMERGENCY DESCENT CARRIED OUT. MAINTENANCE INVESTIGATION REVEALED DUCT CONNECTOR DISCONNECTED AT OUTLET OF LEFT AIR CYCLE MACHINE (ACM). DUCT CONNECT OR REINSTALLED. 2L72 4F A6WE 19960710004791996071000479NM 1996 7 10 DL72L961620 119951213A5330 SKIN BOEING727 727232 1384082NM BS 480-520 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO27504DA 21306 THE SKIN AND STRINGER AT FS 480 TO 520 AND STR 26R WERE FOUND CORRODED. THE SKIN CORROSION REQUIRED A 3.25 BY 2.75 CUTOUT IN THE UPPER AND LOWER SKINS OF THE STR 26R LAP JOINT. THE STRINGER CORROSION REQUIRED A CUTOUT IN THE STRINGER FROM THE EXISTING FACTORY SPLICE AT FS 480 RUNNING AFT TO FS 500 TO 520. MAINTENANCE REPORTS THE STRINGER TO BE 0.050 THICK. THE SKIN DAMAGE WILL BE REPAIRED PER THE SRM WITH A MINOR DEVIATION TO EXTEND THE FILLER TO THE STA 480 BUTT JOINT. 2L73 4F A3WE 19960710004971996071000497NM 1996 7 10 DL72W961618 119951221A5330 SKIN BOEING727 727247 138408FNM BS 690 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO272817W 20873 THE SKIN AT FS 680 CL AND FS 690 STR 26R WAS FOUND TO HAVE CORROSION DAMAGE. THE DAMAGE CUTOUT AT STA 680 CL IS APPROXIMATELY 2 BY 3, LOCAL SKIN THICKNESS IS 0.050. THE DAMAGE CUTOUT AT FS 690 IS APPROXIMATELY 2 BY 2, WITH A LOCAL SKIN THICKNESS OF 0.050. THERE IS A PREVIOUS INTERNAL REPAIR AT FS 680 TO 710, STR 26R TO STR 27R REFERENCE ER/A 232661-14 AND A PREVIOUS EXTERNAL REPAIR AT FS 703 STR 28L AND STR 28R, REFERENCE ER/A 216859-14. THIS ER/A IS CLASSIFIED AS AN RII DUE TO THE SIZE OF THE REPAIR AT STATION 690. 2L73 4F A3WE 19960710004981996071000498NM 1996 7 10 DL72W961619 119951220A5330 SKIN BOEING727 727247 138408FNM BS 500-570 CORROSION A DALAK NONE O OTHER ININSP/MAINT 1 SO272817W 20873 THE SUBJECT FUSELAGE SKIN WAS FOUND WITH CORROSION DAMAGE AT STR 26L LAP JOINT, FS 500, 520 TO 540 AND 560 TO 570. AT FS 500, THE DAMAGE CUTOUT IS APPROXIMATELY 8 BY 2 IN THE LOWER SKIN. AT FS 520 TO 540, THE DAMAGE CUTOUT IS APPROXIMATELY 7.75 BY 2 IN THE UPPER SKIN AND 14.5 BY 2.75 IN THE LOWER SKIN. AT STA 560 TO 570, THE DAMAGE CUTOUT IS APPROXIMATELY 9 BY 2.5 IN THE UPPER SKIN. 2L73 4F A3WE 19960711000021996071100002NM 1996 7 11 CA951116002 119951107A3213161T111026 OUTER CYLINDER BOEING767 767375 NM TRUNNION RT MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 2448724487 (CAN)THE RH MAIN LANDING GEAR INSPECTED AS PER AD 95-19-10, FOUND VISIBLE EVIDENCE OF CORROSION AT THE UPPER TRUNNION AFT BUSHING TO THE CYLINDER SURFACE. CORROSION CONFIRMED BY CHEMICAL SPOT TEST. CYLINDE R REPLACED. 2L72 4F RTA1NM 19960711000031996071100003NM 1996 7 11 CA951123110 119951105A3244468K221 TIRE BOEING767 767375 NM #7 WHEEL CAP MISSING W K NONE O OTHER TOTAKEOFF 1 CA (CAN)ON ARRIVAL #7 MAIN WHEEL CAP WAS FOUND THROWN. DAMAGE TO 7 SPOILER RHS INBOARD MAIN FLAP, TWO UNDERWING PANELS, AND THE SPOILER SUPPORT BEAM LOWER CORD. #7 SPOILER REPLACED, FLAPS AND PANELS REPAIRED AND #7 AND #8 WHEELS REPLACED. 2L72 4F RTA1NM 19960718000021996071800002EA 1996 7 18 CA951130009 219951128A7322233700 VALVE ASSEMBLY CESSNA182 TR182 2072735CE LYC O540 O540L3C5 41532EA MCAULY2D34C B2D34C219 GL CARBURETOR MALFUNCTIONED W A O OTHER Y ENGINE STOPPAGE CRCRUISE 1 CA 2574 401 L2237140A 815040 (CAN)PILOT REPORTED ENGINE STOPPAGE (2-3 SECONDS) DURING TURBULANCE; THEN RETURNED TO NORMAL THERE HAVE BEEN 3 OR 4 OF THESE OCCURRENCES OF THIS TYPE IN THE LAST 100 HOURS, THESE HAPPENED DURING BOTH SMOO TH AND ROUGH AIR. DURING TROUBLESHOOTING THE PROBLEM LYCOMING SERVICE INSTRUCTION 1398A SURFACED AND IT INDICATES A MODIFICATION TO THE CARBURETOR DURING ROUGH AIR. THE S/I INVOLVES THE CHANGE OF THE VALVE ASSEMBLY. THE AIRCRAFT IS CURRENTLY UNDERGOING TESTS TO DETERMINE IF THE PROBLEM HAS BEEN RECTIFIED. 1H71 3O3 O 3A13 E295 5 CP7EA 19960718000511996071800051EU 1996 7 18 96ZZZX3462 119950918A291310545028 PACK ASSY BOLKMS105 BO105C 5626005EU HYD SYSTEM DEFECTIVE A AHEEAA UNSCHED LANDING FJ FLT CONT AFFECTED WARNING INDICATION CRCRUISE 1 SW0391070 052377 S145 DURING CRUISE FLIGHT, NOSE OF AIRCRAFT SUDDENLY PITCHED NOSE DOWN, HYDRAULIC BLOCK LIGHT ILLUMINATED, MAST MOMENT INDICATOR LIGHT ILLUMINATED. AFTER RECOVERY TO LEVEL ATTITUDE, AIRCRAFT LANDED WITHOUT INCIDENT. 1G72 3U H3EU 19960718000881996071800088EU 1996 7 18 96ZZZX3466 119951121A6410134617P BUSHING BOLKMS117 BK117A4 5626017EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BY522 7127 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960718000891996071800089EU 1996 7 18 96ZZZX3467 119951121A6410134616P BUSHING BOLKMS117 BK117A4 5626017EU T/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BY522 7127 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW 2 EACH UNITS, CORRECTED PROBLEM. 1G72 3U H13EU 19960718000941996071800094EU 1996 7 18 96ZZZX3472 119951231A6510BB1B649616B BEARING BOLKMS105 BO105CBS 5626008EU T/R DRIVE WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BH192 7743 685 WORN BEYOND SERVICEABLE LIMITS CAUSING VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960718000951996071800095EU 1996 7 18 96ZZZX3473 119951231A6510BB1B649616B BEARING BOLKMS105 BO105CBS 5626008EU T/R DRIVE WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BH192 7760 685 BEARING WORN BEYOND SERVICEABLE LIMITS CAUSING VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960718000961996071800096EU 1996 7 18 96ZZZX3474 119951231A6510BB1B649616B BEARING BOLKMS105 BO105CBS 5626008EU T/R DRIVE WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BH192 7706 685 WORN BEYOND SERVICEABLE LIMITS CAUSING VIBRATION. REPALCED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960718000971996071800097EU 1996 7 18 96ZZZX3475 119951231A6510BB1B649616B BEARING BOLKMS105 BO105CBS 5626008EU T/R DRIVE WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911BH192 7777 685 BEARING WORN BEYOND SERVICEABLE LIMITS CAUSING VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U NCH3EU 19960718003001996071800300NM 1996 7 18 DL72E961586 119951120A53206517518 BEAM BOEING727 727247 138408FNM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272829W 21481 THERE IS A 1 INCH CRACK IN THE FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273 AND A 3 INCH CRACK IN THE AFT SIDE GUSSET. THE INBD UPPER CHORD HAS A 4 INCH LONGITUDINAL CRACK. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE/REPAIR THE DAMAGED PARTS IN ACCORDANCE WITH THE S/B. IN ADDITION, THE INBD WEB WILL BE CUT TO FACILITATE PART REPLACEMENT. 2L73 4F A3WE 19960718003011996071800301NM 1996 7 18 DL72K961587 119951128A532065175186 ANGLE BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27480DA 20860 THERE IS A 2.5 CRACK IN THE ANGLE OF BOTH THE FWD AND AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PARTS IN ACCORDANCE WITH THE S/B. 2L73 4F A3WE 19960718003021996071800302NM 1996 7 18 DL72K961588 119951201A532065175186 ANGLE BOEING727 727232 1384082NM FS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27471DA 20748 THERE IS A 3 INCH CRACK IN THE ANGLE OF THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B. 2L73 4F A3WE 19960718003041996071800304NM 1996 7 18 DL72K961608 119951102A5320651751738 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27474DA 20751 CRACKS ON THE LOWER TORQUE BOX AT FS 1263. THE CRACKS ARE ON THE FORWARD RT SIDE TRANSVERSE BEAM AND THE RT VERTICAL WEB. THE RT VERTICAL WEB HAS A 1 INCH CRACK AT THE FUEL LINE CUTOUT. NORMALLY, THE FUEL LINE IS REMOVED AND THE REPAIR DOUBLER (65-17517-31, 0.032 CLAD 2024-T3) IS INSTALLED IN ONE PIECE. HOWEVER, DUE TO SCHEDULING REQUIREMENTS, IT IS DESIRABLE TO CUT THE DOUBLER AND INSTALL IT WITH THE FUEL LINE IN PLACE IN ACCORDANCE WITH FAA ALTERNATE MEANS OF COMPLIANCE LETTER DATED 19 OCTOBER 1994. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08. 2L73 4F A3WE 19960718003051996071800305NM 1996 7 18 DL72K961612 119951223A532065175186 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27417DA 21259 THERE IS A 1.5 INCH CRACK IN THE AFT GUSSET AND FWD TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTS. TERMINATING ACTION WILL BE PROVIDED BY EO 4-61071-3. 2L73 4F A3WE 19960718003061996071800306NM 1996 7 18 DL72L961610 119951003A5320651751738 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27501DA 21303 A CRACK IN THE ANGLE ON THE LOWER TORQUE BOX FS 1263 TRANSVERSE BEAM FORWARD RIGHT HAND SIDE. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTS. TERMINATING ACTION WILL BE PROVIDED BY EO 4-61071-3. 2L73 4F A3WE 19960718003141996071800314NM 1996 7 18 DL72S961609 119951017A532065175186 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1273 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27482DA 20862 THERE IS A CRACK IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1273. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. 2L73 4F A3WE 19960718003151996071800315NM 1996 7 18 DL72S961611 119951018A5320651751737 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27522DA 21582 THERE IS A CRACK IN THE AFT TRANSVERSE BEAM OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTS. TERMINAING ACTION WILL BE PROVIDED BY EO 4-61071-3. 2L73 4F A3WE 19960718003181996071800318NM 1996 7 18 DL72S961617 119950829A5320651751738 TRANSVERSE BEAM BOEING727 727232 1384082NM BS 1263 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27535DA 22048 THERE IS DAMAGE TO THE LOWER TORQUE BOX STATION 1263 TRANSVERSE BEAM FWD SIDE. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AD 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS REPLACEMENT DOES NOT TERMINATE THE REPETITIVE INSPECTION REQUIREMENTS. TERMINATING ACTION WILL BE PROVIDED BY EO 4-61071-3. 2L73 4F A3WE 19960718003421996071800342WP 1996 7 18 DLL10961591 119951018A5320 STIFFENER LKHEED1011 10113851 5265010WP BS 445 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27718DA 193C1097 DURING HMV, THE NLG PRESSURE DECK INTEGRAL STIFFENER ALONG RBL 40 WAS FOUND CRACKED. THE CRACK WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. 2L73 4F A23WE 19960718003431996071800343WP 1996 7 18 DLL10961592 119950906A5320 STIFFENER LKHEED1011 10113851 5265010WP BS 445 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27714DA 193C1090 THE NLG PRESSURE DECK RISER ALONG RBL 66 WAS FOUND CRACKED AT FS 445 DURING LTR CHECK IN ATL. THE CRACKED WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED. 2L73 4F A23WE 19960718006451996071800645EU 1996 7 18 96ZZZX3578 119951108A621010513103505 BLADE PIN BOLKMS117 BK117A4 5626017EU M/R WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11117CW299 18638 7125 BLADE PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960718006461996071800646EU 1996 7 18 96ZZZX3579 119951228A63206607A2114 SWITCH BOLKMS105 BO105LSA3 5626020EU NR 1 MGB FAILED A R7MAK NONE P NO WARNING INDICATION ININSP/MAINT 1 NM11203LF116 T16984 2015 GEARBOX OIL PRESSURE SWITCH INOPERATIVE. NR 1 MGB PRESSURE LIGHT WILL NOT ILLUMINATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H3AU 19960718006651996071800665EU 1996 7 18 96ZZZX3598 119951026A33402LA00162500 LIGHT BOLKMS117 BK117B1 5626012EU TAIL CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911VU352 7141 TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960718006661996071800666EU 1996 7 18 96ZZZX3599 119951208A33402LA00162500 LIGHT BOLKMS117 BK117B1 5626012EU TAIL CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911VU101 7141 TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960718006671996071800667EU 1996 7 18 96ZZZX3600 119951228A33402LA00162500 LIGHT BOLKMS117 BK117B1 5626012EU TAIL CRACKED A R7MAK NONE O OTHER ININSP/MAINT 1 NM11911VU43 7141 TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U H13EU 19960718006921996071800692NM 1996 7 18 CA951020016 119951012A2760 ACTUATOR DHAV DHAV DHC8 DHC8102 2809003NM SPOILER CLUTCH STUCK W A CD ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA 15707 0 (CAN)DURING PRE-FLIGHT ROLL CONTROL CHECK, PILOT REPORTED THAT RH OUTBOARD ROLL SPOILER WOULD ONLY EXTEND HALFWAY. IN GROUND MODE IT WAS OK. INSPECTION OF RH WING SPOILER CLUTCH AT PANEL 632DB LOCATED AT R H LOWER WING WAS FOUND RUBBING AGAINST LOWER MICROSWITCH CABLE CLAMP. THE CLAMP WORE A GROOVE INTO PANEL AND IT EVENTUALLY DUG IN PREVENTING ACTUATOR ARM FROM OUTBOARD ROLL SPOILER FROM MOVING TO FULL TRAVEL. CLAMP REPLACED. FLEET CHECK BEING CARRIED OUT. 2H72 4T RTA13NM 19960718006931996071800693EA 1996 7 18 CA951026016 219950802A8530 TOP RING LYC PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA ALL CYLINDERS BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 753 0 L758148 (CAN)DURING 100 HOUR INSPECTION #1, #5 & #6 CYLINDERS WERE FOUND WITH VERY LOW COMPRESSION AND IT WAS DECIDED TO REPLACE THE CYLINDERS. SHORTLY BEFORE THIS THE ENGINE HAD HIGH OIL COMSUMPTION AND #2, #3 & #4 CYLINDERS HAD TO BE REPLACED. ON ALL CYLINDERS THE TOP PISTON RING WAS BROKEN. 1L72 3O3 O 1A10 1E4 19960718006961996071800696CE 1996 7 18 CA951027001 119951023A575350160018 FLAP TRACK BEECH BEECH 99 99 1154002CE R/H OUTBD TRACK CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 21890 0 (CAN)DETAILED INSPECTION FOUND THE RIGHT HAND FLAP SEEMED TO HAVE EXCESSIVE PLAY. ON CLOSER EXAMINATION IT WAS FOUND THAT THE FLAP TRACK WAS CRACKED. TRACK REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1L72 3T A14CE 19960718006981996071800698EU 1996 7 18 CA951027009 119951018A6410112131746 BLADE BOLKMS105 BO105C 5626005EU T/R DEBONDED LE W K NONE O OTHER ININSP/MAINT 1 CA 1202 (CAN)TAIL ROTOR BLADE LEADING EDGE EROSION STRIP DEBONDING TO A POINT 50 MM ALONG LEADING EDGE. 1G72 3U H3EU 19960718007001996071800700EA 1996 7 18 CA951030002 119950501A324695443821 WHEEL HALF DHAV DHC6 DHC6300 EA TIRE BEAD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WHEEL HALF FOUND CRACKED 5 INCHES ALONG THE TIRE BEAD FLANGE. 1H72 3T A9EA 19960718007011996071800701EU 1996 7 18 CA951108036 119951028A3242AHO89455 HEAT PACK DUNLOP AHA1413 BAG BAE146BAE146200A 1500266EU BRAKE SEPARATION W K NONE O OTHER ININSP/MAINT 1 CA 1178 MT011 (CAN)DURING WALKAROUND, PILOT NOTICED THAT BRAKE WEAR INDICATOR PIN HAD BENT, AND THE STATOR APPEARED TO HAVE SHIFTED. INVESTIGATION FOUND THAT THE STATOR LOBES HAD SEPARATED AND THE STATOR HAD SHIFTED CAU SING THE BRAKE INDICATOR TO BEND. 2H74 4F RTA49EU 19960718007031996071800703NE 1996 7 18 CA951109005 219951031A7414SF14LN3 MAGNETO BENDIX DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183092 52020NE CAM DRIVE STRIPPED GEAR W A A UNSCHED LANDING ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CLCLIMB 1 CA 50523 303774 (CAN)SHORTLY AFTER TAKEOFF THE #1 ENGINE BACKFIRED AND RAN ROUGH. AIRCRAFT RETURNED AND LANDED. MAINTENANCE FOUND LEFT HAND MAGNETO DEAD. INVESTIGATION REVEALED THAT THE PHENOLIC CAM DRIVE GEAR HAD ALL THE TEETH STRIPPED BY THE STEEL GEAR IT MESHES WITH. CAUSE COULD NOT BE DETERMINED AS SHAFT AND GEAR TURN FREELY. 2L72 4R4 R A669 5E4 19960718007041996071800704GL 1996 7 18 CA951114011 319951023A6114B30012 BETA RING DHAV DHC6 DHC6300 EA HARTZLHCB3T HCB3TN3 GL PROP HUB GROOVED W K NONE O OTHER ININSP/MAINT 1 CA 3590 BU4915 (CAN)PROPELLER BETA RING WAS FOUND GROOVED DURING INSPECTION. THE GROOVING WAS CAUSED BY THE ENGINE NOSE CASE BOLTS LOCKWIRE TAILS. THE TAILS (ENDS) OF THE LOCKWIRE WERE CUTTING INTO THE BETA RING DURING E NGINE/PROPELLER OPERATION. HARTZELL SERVICE INSTRUCTION #166 AND MCCAULEY SERVICE LETTER 1992-11 ADDRESSES THIS PROBLEM. 1H72 3T A9EA 6 CP15EA 19960718007101996071800710EA 1996 7 18 CA951120009 119951113A575360014546 VANE CNDAIR CNDAIRCL600 CL6002A12 1900304EA FLAP CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 8058 0 (CAN)DURING ROUTINE NDT CHECK OF ADJOINING STRUCTURE, CORROSION WAS NOTICED AT POINT WHERE BUTE DOOR ROLLER RESTS IN FLIGHT ON THE CENTRE SUPPORT BRACKET. CORROSION TO A DEPTH OF .017". 2L72 4F RTA21EA 19960718007111996071800711EA 1996 7 18 CA951120015 119951109A5311C2FS3203H FRAME DHAV C2F1A DHAV DHC2 DHC2MK1 2800102EA FORWARD FUSE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 22656 (CAN)FUSELAGE FRONT SECTION TUBE FOUND CORRODED. 1H71 3R A806 19960718007121996071800712NM 1996 7 18 CA951120016 119951102A760387600520001 CABLE DHAV DHC8 DHC8102 2809003NM L/H COND. LEVER CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)#1 ENGINE CONDITION LEVER CABLE ASSEMBLY WAS FOUND WORN ON INSPECTION. THE WORN SECTION OF THE CABLE WAS AT THE FIREWALL. 2H72 4T RTA13NM 19960718007131996071800713EU 1996 7 18 CA951129520 119951019A2140 HEAT EXCHANGER AIRBUS320 A320211 3930320EU CABIN STRONG ODOR W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA (CAN)A VERY NOTICEABLE SMOKE ODOR WAS DETECTED AFTER TAKEOFF. AIRCRAFT RETURNED TO BASE. INVESTIGATION REVEALED PACK #1 PRIMARY HEAT EXCHANGER REPLACED PRIOR TO FLIGHT. SUSPECT PAINT OR SEALANT EMITTING ODOR WHEN FIRST HEATED. BOTH PACKS OPERATED, NO ODOR DETECTED. 2L72 4F RTA28NM 19960718007141996071800714WP 1996 7 18 CA951129521 119951021A324432500201 TIRE TREAD LKHEED1011 10113851 5265010WP NLG MISSING W O OTHER E VIBRATION/BUFFET CLCLIMB 1 CA (CAN)SEVERE NOSE WHEEL VIBRATION AFTER ROTATION, DELAYED RAISING LANDING GEAR UP UNTIL WHEEL ROTATION STOPPED. LEFT NOSE MISSING 1/8 OF RUBBER TREAD. 2L73 4F A23WE 19960718007151996071800715SO 1996 7 18 CA951204003 119951127A531337397913 STRINGER LKHEED382 382G 526414USO LT WHEEL WELL CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH WHEEL WELL PANEL STRINGER AT STA 610 WL 140 BL 68 CORRODED. REPLACED. 2H74 4T A1SO 19960718007161996071800716SO 1996 7 18 CA951204004 119951127A5320345751R WEB LKHEED382 382G 526414USO FS 477-517 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23425 (CAN)FUSELAGE PRESSURE WEB ATTACH AT BL 61 STA 477-517 WL 275 CRACKED. REPLACED. 2H74 4T A1SO 19960718007171996071800717SO 1996 7 18 CA951204005 119951127A532034575L WEB LKHEED382 382G 526414USO FS477 BL61L CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)FUSELAGE PRESSURE WEB ATTACH AT BL61L, STA 477-517, WL275 CRACKED. REPLACED. 2H74 4T A1SO 19960718007181996071800718SO 1996 7 18 CA951204006 119951127A53113898793 FRAME LKHEED382 382G 526414USO FS511 CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH WHEEL WELL FAIRING STRUCTURE AT STA 511 FRAME CORRODED. REPLACED. 2H74 4T A1SO 19960718007191996071800719SO 1996 7 18 CA951204007 119951127A531235361232L STIFFENER LKHEED382 382G 526414USO FS 10 BL45 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)RAMP STA 10 BL45 BULKHEAD STIFFENER CRACKED. REPLACED. 2H74 4T A1SO 19960718007201996071800720SO 1996 7 18 CA951204008 119951127A53303536175 SKIN LKHEED382 382G 526414USO RAMP STA 0 LE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RAMP STA O LEADING EDGE CRACKED. REPLACED. 2H74 4T A1SO 19960718007211996071800721SO 1996 7 18 CA951204009 119951127A53303717927 PANEL LKHEED382 382G 526414USO FS596-617 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH ATTIC WEB PANEL STA 596-617 BL61.6 WL270-284 CRACKED. REPAIRED IN ACCORDANCE WITH TRANSPORT CANADA APPROVAL W-RA95-106 ISSUE 1. 2H74 4T A1SO 19960718007221996071800722SO 1996 7 18 CA951204010 119951127A5320LS5145 CLINE CAP LKHEED382 382G 526414USO FS 697-737 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)BL61 LH AND RH STA 697-737 WL146 CLINE CAP FLOOR "Z" CRACKED REPLACED. 2H74 4T A1SO 19960718007231996071800723SO 1996 7 18 CA951204011 119951127A532033914949 PANEL LKHEED382 382G 526414USO FS617 WL170 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH WHEEL WELL STA 617 WL170-195 BL61-82 PANEL CRACKED. REPLACED. 2H74 4T A1SO 19960718007241996071800724SO 1996 7 18 CA951204012 119951127A533033110224 SKIN LKHEED382 382G 526414USO FS437-477 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH SIDE FUSELAGE SKIN STA 437-477 WL200 DOUBLER CHANNEL CRACKED. REPLACED. 2H74 4T A1SO 19960718007251996071800725SO 1996 7 18 CA951204013 119951127A5512 SKIN LKHEED382 382G 526414USO H STAB STA 219 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH HORIZONTAL STABILIZER STA 219 UPPER SKIN CRACKED. REPAIRED DWG #SK382-55-024. 2H74 4T A1SO 19960718007261996071800726SO 1996 7 18 CA951204014 119951127A5510 MOUNTS LKHEED382 382G 526414USO H STAB LE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH HORIZONTAL STABILIZER LEADING EDGE ASSEMBLY STA 156 AND STA 162 COMPENSATOR MOUNTS CRACKED. REPAIRED SRM 51-140-20. 2H74 4T A1SO 19960718007271996071800727SO 1996 7 18 CA951204015 119951127A5512370019 SKIN LKHEED382 382G 526414USO H STAB LE STA 89CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH HORIZONTAL STABILIZER LEADING EDGE OUTER SKIN AT STA 89 CRACKED. REPAIRED SRM 51-140-14. 2H74 4T A1SO 19960718007281996071800728SO 1996 7 18 CA951204016 119951127A55213726112R RIB LKHEED382 382G 526414USO RT ELEV LE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH ELEVATOR LEADING EDGE HSS.58 CRACKED. REPLACED. 2H74 4T A1SO 19960718007291996071800729SO 1996 7 18 CA951204017 119951127A5520 DOUBLER LKHEED382 382G 526414USO LT ELEV TE BEAM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH ELEVATOR TRAILING EDGE BEAM ASSEMBLY CRACKED. REPLACED. 2H74 4T A1SO 19960718007301996071800730SO 1996 7 18 CA951204018 119951127A5753 SKIN LKHEED382 382G 526414USO RT INB FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH INBOARD FLAP CRACKED IN THREE LOCATIONS. REPAIRED IN ACCORDANCE WITH SRM 51-140-10. 2H74 4T A1SO 19960718007311996071800731SO 1996 7 18 CA951204019 119951127A5753344007L END RIB LKHEED382 382G 526414USO LT OUTB FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH OUTBOARD FLAP INBOARD END RIB STA.0 CRACKED. REPLACED. 2H74 4T A1SO 19960718007321996071800732SO 1996 7 18 CA951204020 119951127A575334007R END RIB LKHEED382 382G 526414USO RT OUTB FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH OUTBOARD FLAP INBOARD END RIB STA.0 CRACKED. REPLACED. 2H74 4T A1SO 19960718007331996071800733SO 1996 7 18 CA951204021 119951127A5712 RIB CAP LKHEED382 382G 526414USO RT OUTB WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH OUTER WING LOWER RIB CAP CRACKED. REPAIRED SRM 57-50-38. 2H74 4T A1SO 19960718007341996071800734SO 1996 7 18 CA951204022 119951127A571238940523 RIB BRACE LKHEED382 382G 526414USO LT WS 90 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH WING OWS.90 RIB BRACE CRACKED. REPLACED. 2H74 4T A1SO 19960718007351996071800735SO 1996 7 18 CA951204023 119951127A571238940527 RIB BRACE LKHEED382 382G 526414USO WS 108 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH WING OWS.108 RIB BRACE CRACKED. REPLACED. 2H74 4T A1SO 19960718007361996071800736SO 1996 7 18 CA951204024 119951127A5330 SKIN LKHEED382 382G 526414USO STA 695 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)RH SIDE FUSELAGE SKIN STA 695 BL62.5 WL256 CRACKED. REPAIRED DWG SK 382-53-274. 2H74 4T A1SO 19960718007371996071800737SO 1996 7 18 CA951204025 119951127A5350 FORMER LKHEED382 382G 526414USO LT WHEEL WELL CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH WHEEL WELL FAIRING STRUCTURE STA 497 WL165 CRACKED. REPAIRED SRM 51-140-20. 2H74 4T A1SO 19960718007381996071800738SO 1996 7 18 CA951204026 119951127A5343388493 BEAM LKHEED382 382G 526414USO LT MLG STA 528 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 23435 (CAN)LH MAIN LANDING GEAR BEAM STA 528 WL220 CRACKED. REPAIRED SRM 53-40-20. 2H74 4T A1SO 19960718008221996071800822WP 1996 7 18 96ZZZM1098 119951124A5315 FLOOR BEAM DOUG DC8 DC8F54 3021926WP BS 920 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION FOUND ON THE WEB OF THE FLOOR BEAM AT FS 920 UNDER OUTBOARD TRACK. DAMAGED AREA WAS CUT OUT AND INSTALLED 14 BY 7 INCHES .063 301 1/2H MIL-S-5059 DOUBLER WITH A 2 INCH .188 7075-T6 FILLER IAW EO 9508221, 8110-3 ISSUED BY DER SW-713. 2L74 4F 4A25 19960718008231996071800823WP 1996 7 18 96ZZZM1099 119951124A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 430-610 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 430 TO 610 AND FROM LONGERON 31 RIGHT TO LONGERON 31 LEFT. REMOVED AND REPLACED LOWER FUSELAGE SKIN FROM FS 430 TO 610 AND FROM L31 RIGHT TO L31 LEFT IAW SRM 51-1-21. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M) 2L74 4F 4A25 19960718008241996071800824WP 1996 7 18 96ZZZM1100 119951124A5522 SKIN DOUG DC8 DC8F54 3021926WP LT ELEVATOR CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER INBOARD SKIN PANELS OF THE LEFT ELEVATOR FROM STATION XE 32 TO STATION XE 133. REMOVED EACH DAMAGED SKIN PANEL FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAW EO 9502283. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960718008251996071800825WP 1996 7 18 96ZZZM1101 119951124A5522 SKIN DOUG DC8 DC8F54 3021926WP LT ELEVATOR CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER SKIN CENTER PANELS OF THE LEFT ELEVATOR FROM STATION XE 133 TO STATION XE 246. REMOVED THE DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKINS PANEL OF .040 2024-T3 IAW EO 9502083. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960718008261996071800826WP 1996 7 18 96ZZZM1102 119951124A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 610-670 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 610 TO 670 AND FROM L31 RT TO L31 LT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-1-21. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M) 2L74 4F 4A25 19960718008271996071800827WP 1996 7 18 96ZZZM1103 119951124A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 1384-1449 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION AND DENTS WERE FOUND BELOW THE AFT PASSENGER DOOR FUSELAGE SKIN. CUT OUT ALL CORROSION AND DENTS ON DAMAGED SKIN. INSTALLED A 36.5 BY 6.5 INCH .090 7075-T6 FILLER WITH A 66 INCH BY 24.5 INCH .100 7075-T6 QQ-A-250/13 REPAIR DOUBLER FROM STATION FS 1384 TO FS 1449 IAW EO 9509121. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960723000031996072300003NM 1996 7 23 CA951129509 119951010A324226088126 BRAKE BENDIX 26088126 BOEING767 767333 NM ML BROKEN CLIPS W O OTHER E VIBRATION/BUFFET LDLANDING 1 CA UFB3967 (CAN)HIGH LANDING GEAR VIBRATION DURING LANDING. VIBRATION RESULTS OF DETERIORATION OF BRAKES. 12 CLIPS BROKEN, DAMAGED CARBON ROTORS. 2L72 4F RTA1NM 19960725003531996072500353SW 1996 7 25 CA951010036 119950927A2820 FUEL DIST. BELL 212 212 1181420SW LT FUEL TRAPPED AIR W A UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 CA (CAN)#1 ENGINE FLAME OUT. FUEL GAUGE SHOWED 280 LBS, #1 FUEL LOW LIGHT ON #2 LIGHT OFF. FUEL QUANTITY SELECTOR SHOWED L/H TANK AT 0 LBS & R/H TANK 280 LBS. SELECTED INTERCONNECT OPEN UNTIL FUEL EQUALED IN BOTH TANKS. FUEL SAMPLES TAKEN THEN FUEL FILTERS DRAINED #2 DRAINED NORMALLY BUT #1 HAD SOUNDS OF AIR PASSING THROUGH. AIRCRAFT GROUND RUN, NO FURTHER INCIDENT. CONCLUDED THAT FLAMEOUT OCCURRED DUE TO FUEL STARVATION DUE TO AIR IN SYSTEM. 1G71 4U H4SW 19960725003541996072500354SW 1996 7 25 CA951027006 119950922A6510206040352001 SPRING BELL 206040338009BELL 206 206B 1181511SW T/R DRIVE HANGERBROKEN W K NONE O OTHER ININSP/MAINT 1 CA 0 (CAN)DURING COMPLIANCE WITH BELL ASB 206-95-86 THE AME REMOVED SPRING FOR DIMENSIONAL INSPECTION FOUND SPRING BROKEN ON STUD WITH HARDWARE STILL IN PLACE. SPRING LOCATION WAS THE FIFTH HANGER FROM FRONT, O VER HORIZONTAL STABILIZERS. 1G71 3U H2SW 19960725003551996072500355EA 1996 7 25 CA951030005 219951020A72613027254 CHIP DETECTOR SWRNGNSA226 SA226T 8780122SW PWA PT6 PT6A28 EA NOSE CASE FAILED W E ENGINE SHUTDOWN BK SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CRCRUISE 1 CA PCE52148 (CAN)SMOKE IN AIRCRAFT CABIN. REDUCTION OF OIL PRESSURE AND TORQUE RESULTING IN SHUT DOWN OF ENGINE. FOUND CHIP DETECTOR BROKEN AND THREADS STILL IN ENGINE NOSE CASE. 2L72 4T4 TRTA5SW E4EA 19960725003561996072500356CE 1996 7 25 CA951030007 119951019A311099364022601 PANEL BEECH 99 99 1154002CE RT AVIONICS SHORTED W AH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 17766 (CAN)RIGHT HAND AVIONICS LIGHTED "WHEAT" PANEL SHORTED AND HEATED TO THE POINT OF SMOKING. 1L72 3T A14CE 19960725003571996072500357EA 1996 7 25 CA951030008 119951012A5711C2W1008ND SPAR DHAV DHAV DHC2 DHC2MK1 2800102EA WS 123.5 RH CRACKED W K NONE O OTHER NRNOT REPORTED 1 CA 14751 0 (CAN)REAR WING SPAR FOUND CRACKED AT WING STA. 123.5, AT THE OUTBOARD FLAP HANGAR. 1H71 3R A806 19960725003581996072500358CE 1996 7 25 CA951030009 119951019A35205056000975 FITTING BEECH 5056000963 BEECH 90 B90 1152912CE FS 176.5 CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 0 (CAN)DURING THE ROUTINE INSPECTION AND TEST OF THE OXYGEN SYSTEM A HISSING NOISE WAS DETECTED EMANATING FROM BEHIND THE LEFT SIDE PANEL OF THE CABIN. UPON FURTHER INVESTIGATION THE UNION FITTING IN THE OXY GEN LINE AT FUSELAGE STA. 176.5 BETWEEN LINE P/N 50560009-63 AND P/N 50560009-75 AND EACH "B" NUT ATTACHED TO THE LINES WERE FOUND TO BE CORRODED TO THE POINT OF DISINTEGRATION. 1L72 3T 3A20 19960725003591996072500359SO 1996 7 25 CA951030010 119951023A79218530016 OIL COOLER HARRISON PIPER PA23 PA23250 7102308SO NR 1 ENGINE CRACKED W AE UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CRCRUISE 1 CA 119 0 (CAN)#1 ENGINE OIL COOLER CRACKED IN FLIGHT. AIRCRFT RETURNED TO BASE WITH #1 ENGINE FEATHERED. SLIGHT OIL PRESSURE LOSS, 3 LITERS REMAINING ON SHUTDOWN. 1L72 3O 1A10 19960725003601996072500360CE 1996 7 25 CA951031202 119951019A2434510098 RETAINING RING BENDIX 30B1077B LEAR 35 35LEAR 5170600CE ROTOR BEARING CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 80UI (CAN)INCORRECTLY INSTALLED RETAINING NUTS CAUSED DAMAGE TO BEARING SHIELD/SEAL AND RESULTING IN POSSIBLE BEARING CONTAMINATION WITH FRAGMENTS OF METAL THAT SEPARATED FROM THE SHIELD. 2L72 4F A10CE 19960725003611996072500361CE 1996 7 25 CA951101202 119950921A282010192000015 FUEL LINE BEECH 200 200BEECH 1152920CE WHEEL WELL WORN W O OTHER K FLUID LOSS TXTAXI/GRND HDL 1 CA 14417 (CAN)FUEL WAS FOUND LEAKING FROM THE LEFT HAND WHEEL WELL AFTER FLIGHT. THE MOTIVE LINE FROM THE AUXILIARY TANK WAS FOUND CHAFED ON A WIRE BUNDLE TO THE POINT WHERE IT BEGAN TO LEAK. THE WIRE BUNDLE WAS UN TOUCHED. 1L72 4T A24CE 19960725003621996072500362EA 1996 7 25 CA951101203 119951004A5413C6W1512S141 LONGERON DHAV DHC6 DHC6300 EA NACELLE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 21768 (CAN)CRACK FOUND IN THE LEFT NACELLE OUTBOARD LONGERON. INSPECTION IN THIS AREA REQUIRED BY AD CF-85-12R3. IT WAS NOTED THAT DURING REPLACEMENT THE SCREWS SECURINGTHE REINFORCING STRAP OF MOD 6/1655 HAD BEEN LOST AND WITH IT CLAMPING FORCE ON THE STRAP. 1H72 3T A9EA 19960725003631996072500363EU 1996 7 25 CA951129508 119951009A2780 LIMITER AIRBUS320 A320211 3930320EU SL;AT ACTUATOR TRIPPED W K NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN)PRIOR TO ARRIVAL, WHEN FLAPS INITIALLY SELECTED TO FLAP 1, SLATS DID NOT MOVE & SHOWED ZERO DEGREES RANGE. MAINTENANCE FOUND OUTBOARD TORQUE LIMITER TRIPPED ON #2 RIGHT SLAT ACTUATOR. THE OUTBOARD TOR QUE LIMITER WAS RESET. ACTUATOR CHECKED, WING TIP BRAKE & SLAT SYSTEM OPERATIONALLY CHECKED. 2L72 4F RTA28NM 19960725003641996072500364 1996 7 25 CA951129511 419951011A2565D311517105 SLIDE CABLE AIRBUS320 A320211 3930320EU L2 ESCAPE SLIDE ROUTING WRONG W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING INSPECTION OF L2 DOOR ESCAPE SLIDE, MAINTENANCE FOUND ACKBOARD RELEASE MECHANISM INSTALLED INCORRECTLY BY MANUFACTURER. AS A RESULT SLIDE WOULD NOT DEPLOY PROPERLY. UNIT REMOVED TO SAFETY SHOP FOR OVERHAUL. 2L72 4F RTA28NM 19960725003651996072500365EA 1996 7 25 CA951129512 119951011A2750855D1005 BPSU EEMCO CNDAIRCL600 CL6002B19 EA FLAPS FAILED W O OTHER JF WARNING INDICATION FLT CONT AFFECTED APAPPROACH 1 CA 0 (CAN)FLAPS JAMMED AT 20 DEGREES. INSPECTION FOUND THAT WHEN CIRCUIT BREAKERS RESET AND FLAP LEVER REPOSITIOINED MESSAGE WOULD NOT GO OUT TEMPORARILY AND REAPPEAR AS SOON AS FLAPS REACHED SELECTED POSITION.RH BRAKE POSITION SENSOR UNIT AT FAULT. ALSO REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU). 2L72 4F RTA21EA 19960725003661996072500366WP 1996 7 25 CA951214101 119951205A7603580291751 THROTTLE CABLE DOUG DC10 DC1030 3023501WP NR 2 ENG SEPARATED W A K NONE O OTHER ININSP/MAINT 1 CA (CAN)#2 ENGINE THRUST LEVER WAS FOUND DIFFICULT TO MOVE. MAINTENANCE INVESTIGATION REVEALED THE THRUST CONTROL LEVER CABLE WAS SEPARATED AT ONE END, THE OUTER SLEEVE HAD SEPARATED FROM THE END FITTING. THECABLE WAS REPLACED. THREE PREVIOUS FAILURES OF THIS CABLE HAD BEEN REPORTED IN THE SDR DATA BASE. 2L73 4F A22WE 19960725003671996072500367NM 1996 7 25 CA951214103 119951206A5523767379914 TAB BOEING 657379914 BOEING737 737217 1384464NM RT ELEV BROKEN W A UNSCHED LANDING EFDVIBRATION/BUFFET FLT CONT AFFECTED INFLIGHT SEPARATION CLCLIMB 1 CA 4025426754 9999 (CAN)WHILE IN FLIGHT THE RH ELEVATOR TAB BROKE 10 INCHES FROM THE INBOARD END, A PIECE 24 INCHES LONG IS MISSING FROM THE TAB. THE PILOT REPORTED AT APPROXIMATELY FL330 IN THE CLIMB TO 370. SEVERE AIRFRAMEVIBRATION. DESCEND AND RETURN TO BLOCKS. 2L72 4F A16WE 19960725003681996072500368NM 1996 7 25 CA951219102 119951130A324269627231 STUD BOEING737 737217 1384464NM BRAKE SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING BRAKE CHANGE FOUND BRAKE STUD SHEARED. 2L72 4F A16WE 19960725003711996072500371WP 1996 7 25 CA951229001 119951226A2824197303 VALVE DOUG DC10 DC1030 3023501WP MOTIVE XSFER FAILED CLOSED W E ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 CA 49102 (CAN)DURING APPROACH THE #3 SCHEDULE LIGHT CAME ON. QRH CARRIED OUT. THE #3 FUEL TANK FORWARD AND AFT LOW PRESSURE LIGHTS ILLUMINATED AND THE #3 ENGINE FLAMED OUT AT 1,000 FEET. ENGINE CROSSFEED VALVE OPEN ED AND TRANSFER PUMPS ON, ENGINE RELIGHT AT 200 FEET. SUBSEQUENT MAINTENANCE TROUBLESHOOTING FOUND GRAVITY SYSTEM TRANSFER NORMAL BUT NO CHANGE USING MOTIVE TRANSFER SYSTEM. FURTHER INVESTIGATION REVEALED THE INBOARD MOTIVE TRANSFER SHUT-OFF VALVE HAD FAILED INTERNALLY, INTERNAL GATE CLOSE, VALVE WAS REPLACED AS PER MAINTENANCE MANUAL 28-21-13. 2L73 4F A22WE 19960725003721996072500372NM 1996 7 25 CA951229002 119951223A2130 VALVE BOEING737 737275 1384485NM CABIN PRESS INTERMITTENT W A UNSCHED LANDING G MULTIPLE FAILURE CRCRUISE 1 CA (CAN)AIRCRAFT RETURNED TWICE DUE TO PRESSURIZATION PROBLEMS, OUTFLOW AND CONTROLLER REPLACED. NEXT FLIGHT PRESSURIZATION FAILED, REPLACED PRESSURE CONTROL PANEL AND COOLING EQUIPMENT FAN EXHAUST VALVE. NEX T FLIGHT UNABLE TO CONTROL PRESSURIZATION AT FL310 AND 7.6 PSI DIFFERENTIAL. REPLACED UPPER AND LOWER PRESSURE RELIEF VALVES. TEST FLOWN TO FL370 OK. 2L72 4F A16WE 19960725003731996072500373NM 1996 7 25 CA951229003 119951219A80121G38616927 SWITCH BOEING737 737217 1384464NM PWA JT8 JT8D17 52049NE START VALVE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA 451392089 702657 (CAN)THE #1 ENGINE START VALVE OPEN LIGHT CAME ON IN FLIGHT. THE #1 ENGINE WAS SHUTDOWN AS PER THE CHECKLIST. POST FLIGHT THE #1 ENGINE START VALVE AND THE PRESSURE SWITCH WERE REPLACED. 2L72 4F4 F A16WE E2EA 19960725003741996072500374NE 1996 7 25 CA960102101 219951210A7250 TURBINE BOEING737 737275 1384485NM PWA JT8 JT8D17 52049NE NR 1 ENGINE DAMAGED W EA ENGINE SHUTDOWN UNSCHED LANDING EX VIBRATION/BUFFET ENGINE FLAMEOUT CLCLIMB 1 CA 385443577 702735B (CAN)WHILE CLIMBING THROUGH 18,000 FEET A LOUD BANG WAS HEARD AND #1 ENGINE SPOOLED DOWN WITH VIBRATIONS AT 5.0 PLUS. #1 ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION FOUND EXTENSIVE TURBINE DAMAGE AND 6 SMA LL PUNCTURES IN TAILPIPE THE LARGEST BEING 3/8 INCH. ENGINE, TAILPIPE AND REVERSER WERE REPLACED. 2L72 4F4 F A16WE E2EA 19960725003751996072500375NM 1996 7 25 CA960103010 119951216A3411271N64611220 TUBE BOEING757 75728A 1384976NM LEFT STATIC CHAFED W O OTHER J WARNING INDICATION ININSP/MAINT 1 CA (CAN)STATUS MESSAGE "ELEV FEEL" FOUND LEFT STATIC TUBE CHAFING ON DUCT. 2L72 4F RTA2NM 19960725004071996072500407WP 1996 7 25 96ZZZM1104 119951124A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 1140-1340 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FOUND CORROSION ON SEVERAL AREAS OF FUSELAGE SKIN FROM FS 1140 TO 1340 FROM L31 LEFT TO L31 RIGHT. REMOVED AND REPLACED LOWER FUSELAGE SKIN IAW SRM 51-21-1. ALSO, TREATED AND PRIMED ALL AREAS IAW SRM 51-1-8. (M) 2L74 4F 4A25 19960725004081996072500408WP 1996 7 25 96ZZZM1105 119951124A5330 SKIN DOUG DC8 DC8F54 3021926WP BS 850 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FOUND CORROSION DAMAGE ON THE LOWER EDGE OF THE FUSELAGE SKIN PANEL JUST FORWARD OF LONGERON 24 CLEVIS AND RUNNING FORWARD FOR ABOUT 32 INCHES AT STATION 850. CORROSION WAS CUT OUT AND INSTALLED TWO 40 BY 8.5 INCHES .100 AISI 3011/2H MIL-S-5059 DOUBLERS. ALSO, INSTALLED A 33.2 BY 2.0 INCH .200 2024-T3 FILLER IAW EO 9510061. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004091996072500409WP 1996 7 25 96ZZZM1106 119951124A5311 FRAME DOUG DC8 DC8F54 3021926WP BS 540/560/580 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FUSELAGE FRAME AT FUSELAGE STATION 540, 560 AND 580 WERE FOUND WITH CORROSION DAMAGE ALONG THE LOWER SEVERAL INCHES WHERE THEY JOIN THE FLOOR ATTACH FITTING. CUT EACH OF THE 3 FRAMES AT A LOCATION 19 INCHES ABOVE THE FLOOR LEVEL AND REPLACED WITH IDENTICAL FRAME SEGMENTS 7075-T6. SPLICED THE REPLACEMENT FRAMES SEGMENT TO EXISTING FRAME WITH TWO .050 AISI 301 1/2H REPAIR DOUBLERS IAW EO 9508231. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004101996072500410WP 1996 7 25 96ZZZM1107 119951124A5311 FRAME DOUG DC8 DC8F54 3021926WP BS 500 CORRODED A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FUSELAGE FRAME AT FS 500 IN THE CABIN BETWEEN LONGERONS 9 AND 10 RIGHT FOUND CRACK. CUT OUT THE DAMAGED MATERIAL. INSTALLED A 2.25 FILLER FROM AN IDENTICAL FRAME SECTION AND INSTALLED TWO 11.0 INCH .050 AISI 301 1/2H REPAIR DOUBLERS IAW EO 9509141. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004111996072500411WP 1996 7 25 96ZZZM1108 119951124A5753 SKIN DOUG DC8 DC8F54 3021926WP TE FLAP CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, RT WING AT THE OUTBOARD END OF THE UPPER AND LOWER SKIN OF THE OUTBOARD FLAP CORROSION DAMAGE WAS FOUND. CUT AND REMOVED THE AREA OF CORRODED SKIN AND INSTALLED A .050 2924-T3 MATERIAL DOUBLER WITH A .063 2024-T3 SPLICE PLATE IAW EO 9508092. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004121996072500412WP 1996 7 25 96ZZZM1109 119951124A5730 PLATING DOUG DC8 DC8F54 3021926WP WS 600 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FOUND CORROSION ON THE UPPER PLATING OF THE RIGHT WING UPPER SURFACE AT STATION XRS 600. CUT AND REMOVED CORRODED PLATING AND INSTALLED A 2 INCH BY 80 INCH .100 7075-T3 FILLER WITH 47 BY 84 INCH .100 7075-T6 DOUBLER IAW EO 9510181. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004131996072500413WP 1996 7 25 96ZZZM1110 119951124A5751 SKIN DOUG DC8 DC8F54 3021926WP RT OUTBD AILERONCORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF OUTBOARD AILERON HAD CORROSION AT LOWER OUTBOARD SKIN PANEL. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL IAW EO 9507251. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004141996072500414WP 1996 7 25 96ZZZM1111 119951124A5751 SKIN DOUG DC8 DC8F54 3021926WP RT INBD AILERON CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, RIGHT WING LOWER SKIN OF INBOARD AILERON HAD CORROSION AT OUTBOARD END OF AILERON SKIN. CUT AND REMOVED CORRODED SKIN PANEL AND INSTALLED NEW IDENTICAL REPLACEMENT PANEL OF .050 2024-T3 MATERIAL WITH A .063 2024-T3 SPLICE PLATE IAW EO 9508091. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004151996072500415WP 1996 7 25 96ZZZM1112 119951124A5730 SKIN DOUG DC8 DC8F54 3021926WP WS 554/659 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, LEFT WING UPPER SKIN CORROSION WAS FOUND IN VARIOUS PLACES BETWEEN WING STATION 554 AND 659. REMOVED ALL CORROSION DAMAGE AND BLENDED THE AREA OUT TO A 63 MICRO INCH FINISH. INSTALLED 35 INCH BY 63.5 INCH .100 7075-T6 DOUBLER IAW EO 9509221. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004161996072500416WP 1996 7 25 96ZZZM1113 119951124A5512 SKIN DOUG DC8 DC8F54 3021926WP LT HORIZ STAB CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON LEFT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .080 7075-T6 MATERIAL. ALSO, REPLACED EACH BEAD WITH A HAT CHANNEL REINFORCEMENT OF SAME LENGTH OF .050 7075-T6 MATERIAL AND INSTALLED PANELS ON HORIZONTAL STABILIZER. ALL WORK ACCOMPLISHED IAW EO 9507232. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004171996072500417WP 1996 7 25 96ZZZM1114 119951124A5512 SKIN DOUG DC8 DC8F54 3021926WP RT HORIZ STAB CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AND LOWER SURFACES OF SKIN FROM STATION XE 221 TO XE 272. REMOVED THE DAMAGED UPPER AND LOWER SKIN PANELS AND FABRICATED PANELS OF .808 7075-T6 MATERIAL. ALSO, REPLACED EACH BEAD WITH A HAT CHANNEL REINFORCEMENT OF SAME LENGTH OF .050 7075-T6 MATERIAL AND INSTALLED PANEL ON HORIZONTAL STABILIZER. ALL WORK ACCOMPLISHED IAW EO 9507231. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004181996072500418WP 1996 7 25 96ZZZM1115 119951124A5522 SKIN DOUG DC8 DC8F54 3021926WP RT ELEV CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER INBOARD SKIN PANELS OF THE RT ELEVATOR FROM STATION XE 32 TO STATION XE 133. REMOVED EACH DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAE EO 9502284. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004191996072500419WP 1996 7 25 96ZZZM1116 119951124A5522 SKIN DOUG DC8 DC8F54 3021926WP RT ELEV CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE UPPER AND LOWER SKIN CENTER SKIN PANELS OF THE RT ELEVATOR FROM STATION XE 133 TO STATION XE 246. REMOVED THE DAMAGED SKIN PANELS FROM THE ELEVATOR AND INSTALLED A NEW IDENTICAL SKIN PANEL OF .040 2024-T3 IAW EO 9502084. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004201996072500420WP 1996 7 25 96ZZZM1117 119951124A5315 FLOOR BEAM DOUG DC8 DC8F54 3021926WP BS 877 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, CORROSION WAS FOUND ON THE LOWER FORWARD AND AFT FLANGES OF THE FLOOR BEAM AT STATION 877. REMOVED ALL CORROSION AND BLENDED TO A 63 MICRO INCH FINISH. INSTALLED TWO 24.0 INCH .063 AISI 301 1/2H DOUBLER IAW EO 9503211. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004211996072500421WP 1996 7 25 96ZZZM1118 119951124A5320 ANGLE DOUG DC8 DC8F54 3021926WP BS 700 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FOUND CORROSION ON THE CENTER TANK LOWER END ANGLE AT FS 700 LEFT. CUT OFF THE LOWER 9 INCHES OF MATERIAL FROM THE ANGLE AND INSTALLED A SPLICE ANGLE OF .125 17-7PH TH1050 MATERIAL IAW EO 9508081. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004221996072500422WP 1996 7 25 96ZZZM1119 119951124A5311 FRAME DOUG DC8 DC8F54 3021926WP BS 310 CORROSION A FXLAK NONE O OTHER ININSP/MAINT 1 SO1954FA 45637 DURING D-CHECK INSPECTION, FOUND CORROSION WAS FOUND ON THE FORWARD CIRCUMFERENCIAL FRAME AT FS 310 BETWEEN LONGERON 29L AND 34L. CUT OUT THE DAMAGED FRAME BY CUTTING MIDWAY BETWEEN LONGERON 28L AND 29L AND BETWEEN LONGERON 34L AND 35L. REPLACED WITH AN IDENTICAL SEGMENT OF LIKE MATERIAL AND INSTALLED TWO SPLICE STRAP .10 BY 5.0 AISI 301 1/2 AND INSTALLED EIGHT .100 BY 1.25 BY 5.0 AISI 301 1/2H IAW EO 9508284. 8110-3 ISSUED BY DER SW-713. (M) 2L74 4F 4A25 19960725004281996072500428NE 1996 7 25 96ZZZM1125 219951222A8530327627 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 CB3 52026NE NR 1 ENGINE CRACKED A NACAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 AL0343872 533294 27393 FLT 20 - SHUT DOWN NR 1 ENGINE AT 2029Z. MAINTENANCE REPLACED NR 18 CYLINDER ASSEMBLY ON NR 1 ENGINE DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R4 R A781 E264 19960725004291996072500429NE 1996 7 25 96ZZZM1126 219951219A8530327627 CYLINDER DOUG DC6 DC6B 3021712WP PWA R2800 CB3 52026NE NR 4 ENGINE CRACKED A NACAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 AL03867TA 45202 36781 FLT 70 - SHUT DOWN NR 4 ENGINE AT 2340Z DUE TO RAPID BACKFIRING AND ROUGH RUNNING. MAINTENANCE REPLACED NR 8 CYLINDER ASSEMBLY ON NR 4 ENGINE DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R4 R 6A4 E264 19960725004301996072500430WP 1996 7 25 96ZZZM1127 119951208A6120 WIRE DOUG DC6 DC6B 3021712WP NR 3 ENGINE BROKEN A NACAA UNSCHED LANDING O OTHER CLCLIMB 1 AL03867TA 2342 45202 FLT 731 - RETURNED TO ANC DUE TO LOSS OF CONTROL ON NR 3 PROPELLER. MAINTENANCE REPAIRED PROP GOVERNOR WIRING FROM GOVERNOR TO NOSE CASE J-BOX. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R 6A4 19960725004311996072500431NE 1996 7 25 96ZZZM1128 219951229A8530327627 CYLINDER DOUG DC6 DC6 3021702WP PWA R2800 CB3 52026NE NR 3 ENGINE CRACKED A NACAE ENGINE SHUTDOWN E VIBRATION/BUFFET CRCRUISE 1 AL0343872 622 533294 P33603 FLT 43 - SHUT DOWN NR 3 ENGINE AT 1910Z DUE TO BACKFIRING IN CRUISE. MAINTENANCE REPLACED NR 18 CYLINDER ASSEMBLY ON NR 3 ENIGNE DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R4 R A781 E264 19960725004321996072500432NE 1996 7 25 96ZZZM1129 219951208A852083477 INTAKE VALVE DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 ENGINE STUCK OPEN A NACAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 AL034213X 44605 P36421 FLT NR 9013 - RETURNED TO ANC DUE TO BACKFIRING ON TAKEOFF. MAINTENANCE REPLACED NR 3 CYLINDER ASSEMBLY ON NR 3 ENGINE DUE TO DAMAGED INTAKE VALVE AND PISTON. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R4 R 6A3 E264 19960725004331996072500433NE 1996 7 25 96ZZZM1130 219951213A8530327627 CYLINDER DOUG DC6 DC6A 3021706WP PWA R2800 CB3 52026NE NR 3 ENGINE CRACKED A NACAE ENGINE SHUTDOWN EK VIBRATION/BUFFET FLUID LOSS CRCRUISE 1 AL034213X 44605 P36421 FLT 43 - SHUT DOWN NR 3 ENGINE AT 2050Z DUE TO BACKFIRING AND OIL LOSS. MAINTENANCE REPLACED NR 18 CYLINDER ASSEMBLY ON NR 3 ENGINE DUE TO CRACKED HEAD. AIRCRAFT RETURNED TO SERVICE. (M) 2L74 4R4 R 6A3 E264 19960802004811996080200481CE 1996 8 2 CA951102001 119951025A2121C4140070102RX BEARING CESSNA208 208B 2073701CE AVIONICS BLOWER SPALLED W K NONE O OTHER CRCRUISE 1 CA (CAN)THE PILOT REPORTED HEAVY STATIC ON THE COMM AND VOR FLUCTUATION OF UP TO 5 DEGREES. AVIONICS TRACED THE PROBLEM TO THE AVIONICS COOLING FAN MOTOR WHOS BEARINGS HAD WORN OUT AND WERE BEGINNING TO DRAG THE MOTOR ROTATION DOWN. A CHECK WITH THE HISTORY OF THE AIRCRAFT REVEALED NAV FLUCTATIONS AND DECREASED VOR RANGE COINCIDING WITH REPORTS OF A NOISY FAN MOTOR. 1H71 3T A37CE 19960802004821996080200482EA 1996 8 2 CA951102003 219950728A85205015 STUD LYC LW15631 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA NR1 CYLINDER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 438 L47861A (CAN)ON INSPECTION FOUND #1 CYLINDER AFT BOTTOM HOLD DOWN STUD BROKEN. CYLINDER WAS REMOVED AND ALL HOLD DOWN NUTS REPLACED. NO RECORD OF NUT REPLACEMENT AT ENGINE OVERHAUL OR CRANKCASE REPAIR FACILITY . 1L72 3O3 O A20SO E14EA 19960802004831996080200483EA 1996 8 2 CA951102004 219951030A721050990118 QUILL SHAFT BEECH 5099011535 BEECH 90 65A90 1152908CE PWA PT6 PT6A20 52043EA BEARING JOURNAL OVERHEATED W A K NONE O OTHER ININSP/MAINT 1 CA S0856 PCE21003 (CAN)GEAR BOX REMOVED FOR SCHEDULED INSPECTION WITH 96.0 HOURS REMAINING. CURSORY INSPECTION OF THE GEAR BOX INDICATED NO DEFECTS UNTIL THE QUILL SHAFT WAS TURNED BY HAND. DURING THIS INSPECTION THE QUILL SHAFT AND BEARINGS SHOWED SIGNS OF OVER-HEATING. THE BEARING WAS ROUGH AND SIGNS OF SLIPPAGE WERE INDICATED BETWEEN BEARINGS AND THE QUILL SHAFT. A SAMPLE OF OIL SHOWED TRACES OF METAL. SUBMITTER STATES THAT FURTHER TIME IN USE MAY HAVE RESULTED IN A FAILURE OF THE GEAR BOX. 1L72 3T3 T 3A20 E4EA 19960802004851996080200485EA 1996 8 2 CA951102009 219951027A8520 CRANKSHAFT LYC PIPER PA31 PA31 7103102SO LYC O540 LTIO540J2BD 41533EA NR 1&3 CYLS BROKEN W K NONE O OTHER NRNOT REPORTED 1 CA 1909 0 L611361A (CAN)ENGINE CRANKSHAFT BROKEN BETWEEN #1 AND #3 CYLINDERS. 1L72 3O3 O A20SO E14EA 19960802004861996080200486SW 1996 8 2 CA951103002 119951026A3213 YOKE SWRNGNSA226 SA226TC 8780404SW RH MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)ULTRASONIC INSPECTION CARRIED OUT AS PER AD 95-19-07R1, AND SB 226-32-065. CRACK 1 INCH LONG. 2L72 4T RTA8SW 19960802004871996080200487EU 1996 8 2 CA951103003 119951021A71200301042710 BRACKET SNIAS 350 AS350B 8680801EU EDGE OF MOUNT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 540 (CAN)UPON REMOVAL OF BRACKET TO COMPLY WITH SL 1656/95/ARL/27, THE BRACKET WAS FOUND TO BE CRACKED 1/2 WAY THROUGH. THE CRACK RUNS UP AND DOWN AND IS DIRECTLY IN CONTACT WITH THE SHARP SQUARE EDGE OF THE G EARBOX. 1G71 3U H9EU 19960802004881996080200488EU 1996 8 2 CA951103004 119951009A7120350A21106606 MOUNT SNIAS 350 AS350D 8680803EU INTERIOR RIB CRACKED W A K NONE O OTHER ININSP/MAINT 1 CA (CAN)BOTH R/H MOUNT P/N 350A21-1066-05 AND L/H MOUNT P/N 350A21-1066-06 WERE FOUND CRACKED. 1G71 3U H9EU 19960802004891996080200489CE 1996 8 2 CA951103006 119951027A55419763000023 SPAR BEECH BEECH 100 A100 1152915CE RUDDER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 17299 0 (CAN)RUDDER WAS REMOVED BY MAINTENANCE TO SERVICE ANOTHER AIRCRAFT. THEY FOUND CRACKING OF THE SPAR BY THE HINGE ATTACH POINTS. A FLEET INSPECTION CAMPAIGN WAS INITIATED AND SDR 951103007 HIGHLIGHTS ANOTHER FINDING OF THE SAME NATURE. 1L72 3T A14CE 19960802004901996080200490CE 1996 8 2 CA951103007 119951023A55419763000023 SPAR BEECH 100 A100 1152915CE RUD UPPER HINGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13015 (CAN)DURING INSPECTION THE UPPER RIGHT HINGE WAS FOUND TO BE WORN. UPON REMOVAL A CRACK WAS FOUND ON THE SPAR SIMILAR TO THAT OF SDR 951103006. 1L72 3T A14CE 19960802004911996080200491SW 1996 8 2 CA951103101 119951004A7120204060157001 TRIPOD MOUNT BELL BELL 204 204B 1181404SW TOP INSIDE LEG CRACKED W A K NONE O OTHER ININSP/MAINT 1 CA 0 (CAN)TRIPOD ENGINE MOUNT INSIDE LEG BROKEN WHERE LEG IS WELDED TO THE UPPER BEARING MOUNT. REPLACEMENT TRIPOD INSTALLED AND A MISALIGNMENT WAS NOTED AT THE ATTACHMENT POINT CAUSING A PRELOAD ON THE MOUNT. 1G71 4U H1SW 19960802004921996080200492WP 1996 8 2 CA951103102 119951013A2910 LINE CVAC 340 340CVAC 242270AWP NLG WHEEL WELL BROKEN W A UNSCHED LANDING K FLUID LOSS CRCRUISE 1 CA (CAN)HYDRAULIC PRESSURE LINE LOCATED IN NOSE WHEEL WELL LOST SWAGED END FITTING CAUSING LOSS OF MAIN HYDRAULIC SYSTEM. MAINTENANCE INVESTIGATION REVEALED THAT THE LINE SLEEVE WAS NOT COMPLETELY COMPRESSED ALTHOUGH THE ASSEMBLY WAS CORRECT. 2L72 4R 6A6 19960802004931996080200493CE 1996 8 2 CA951106202 119951025A5720082340063 BULKHEAD CESSNA402 402B 207590PCE TIP TANK AFT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7534 (CAN)A 2 CM CRACK WAS DETECTED DURING A ROUTINE INSPECTION ON THE LEFT HAND MAIN FUEL TIP TANK REAR BULKHEAD ASSEMBLY ADJACENT TO WHERE IT ATTACHES TO THE MAIN WING REAR SPAR. SUBMITTER SUGGESTS THAT OTHER OPERATORS OF TWIN ENGINE CESSNA AIRCRAFT EQUIPPED WITH TIP TANKS SHOULD PAY PARTICULAR ATTENTION TO POTENTIAL CRACKS IN THIS AREA. 1L72 3O A7CE 19960802004951996080200495CE 1996 8 2 CA951108001 119951030A324441020990 TIRE GOODYEAR 22X6075X10 BEECH 200 200BEECH 1152920CE SIDEWALL FAILED W K NONE O OTHER ININSP/MAINT 1 CA 310 41020990 (CAN)THIS IS THE SECOND INSTANCE OF CASE FAILURE IN THE PAST TWO YEARS. SUBMITTER STATES THAT THE TIRE PRESSURE WAS PROPERLY MAINTAINED. 1L72 4T A24CE 19960802004961996080200496NE 1996 8 2 CA951108005 119951027A2497M813811106C WIRE SKRSKY P206A06 SKRSKYS76 S76A 8143006NE STA 210 CHAFED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA 0 (CAN)EVIDENCE OF ARCING BETWEEN #2 DC PRIMARY BUS WIRE AND FUSELAGE FORMER AT STA 210, WHERE CABLE FEEDS THROUGH. SOOT AND ASH INDICATE GROMMET FAILURE AND CHAFING. THE CURRENT LIMITER CL2 P/N MS28936-130 HAD NOT BLOWN. 1G72 3U H1NE 19960802004981996080200498WP 1996 8 2 CA951108008 119951014A6420369D216009 TAIL ROTOR ASSY HUGHES369 369D 4470706WP FLAPPING BEARINGDELAMINATED W A E ENGINE SHUTDOWN E VIBRATION/BUFFET APAPPROACH 1 CA 6850 (CAN)SEVERE VIBRATION ON FINAL APPROACH. INSPECTION REVEALED THAT ELASTOMERIC CONICAL BEARINGS WERE DELAMINATED WHICH CAUSED VIBRATION. 1G71 3U H3WE 19960802004991996080200499WP 1996 8 2 CA951108009 119951015A6210369D21100517 BLADE HUGHES369 369D 4470706WP LEADING EDGE DEBONDING W K NONE O OTHER ININSP/MAINT 1 CA 1760 (CAN)M/R BLADE LEADING EDGE ABRASION STRIP DEBONDED. 1G71 3U H3WE 19960802005021996080200502SW 1996 8 2 CA951108014 119951103A3230 BEARINGS SWRNGNSA226 SA226AT 8780405SW NLG DRAG BRACE DIRTY W A D RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CA (CAN)NLG NOT LOCK, AND IN TRANSIT LIGHT STAYED ON. THIS WAS 4TH INCIDENT THIS ACFT IN PAST MONTH. IN PREVIOUS INCIDENTS, GEAR RIGGED, LUBED ETC. AND NIL FOUND. IN THIS CASE FURTHER INSP FOUND UPLOCK SHAFT BEARINGS WERE STICKY AND DIRTY DESPITE FACT THAT GEAR DRAG BRACE WAS OVERHAULED IN MID 1994. DRAG BRACE HAD LATEST BUSHINGS INSTALLED AS PER SB 226-32-060. SB HAS NOT ALWAYS BEEN SUCCESSFUL. COLDER THAN NORMAL TEMPS MAY HAVE CONTRIBUTED TO STIFFNESS OF GEAR UPLOCK SHAFT AND MASKED THE PROBLEM AT AMBIENT TEMP. 2L72 4T RTA5SW 19960802005031996080200503NE 1996 8 2 CA951108015 219951026A8520 CRANKSHAFT BEECH 18 G18S 1151010CE PWA R985 R985AN14B 52008NE THRUST BEARING CRACKED W A K NONE K FLUID LOSS ININSP/MAINT 1 CA 1031 16218 (CAN)INVESTIGATION OF #1 ENGINE OIL LEAK FOUND OIL FLOW AT THRUST BEARING (CRANKSHAFT). ENGINE MOTORING INDICATED NO CYLINDER BLOW BY. PROPELLER REMOVED AND CRANKSHAFT CAPPED, ACTUATION OF FEATHERING PUMP INDICATED LOSS OF OIL THROUGH AN ANNULAR CRACK STARTING IN THE THRUST BEARING NUT RETENTION THREADS AND COMING FORWARD UNDER THE PROP CONE AREA. THE SHAFT WAS CRACKED MORE THAN 270 DEGREES OF THE CRANKSHAFT CIRCUMFERENCE. 1L72 3R3 R A765 5E1 19960802005041996080200504CE 1996 8 2 CA951108016 119951022A733312281301 TRANSMITTER BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE FUEL FLOW INTERMITTENT W K NONE P NO WARNING INDICATION CRCRUISE 1 CA 14 (CAN) FUEL FLOW STARTS TO WORK INTERMITTENTLY AND THEN FAILS. FUEL FLOW (FF) TRANSMITTER INSTALLED ON OTHER ENGINE AND SNAG FOLLOWED TRANSMITTER. THIS IS THE FOURTH FF TRANSMITTER REPLACED ON A NEW AIRCRAFT. SUSPECT POOR QUALITY OF UNIT. 2L72 4T4 TRTA24CE E26NE 19960802005061996080200506EA 1996 8 2 CA951129515 119951015A2750860D10018 FECU CNDAIRCL600 CL6002B19 EA FLAPS CONTROL FAILED W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 CA 1541 (CAN)FLAP FAIL MESSAGE ON WHEN FLAPS SELECTED ON APPROACH. FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) AT FAULT. 2L72 4F RTA21EA 19960802005071996080200507EA 1996 8 2 CA951129522 119951023A5620NP1393221 WINDSHIELD PPG CNDAIRCL600 CL6002B19 EA PILOT SHATTERED W O OTHER O OTHER NRNOT REPORTED 1 CA 0 (CAN)CAPTAINS WINDSHIELD SHATTERED. EMERGENCY DECLARED. 2L72 4F RTA21EA 19960802005081996080200508EA 1996 8 2 CA951129524 119951029A2752852D1007 ACTUATOR EEMCO CNDAIRCL600 CL6002B19 EA LH INBD FLAP FAILED W O OTHER FJ FLT CONT AFFECTED WARNING INDICATION APAPPROACH 1 CA 1640 0 (CAN)DURING APPROACH, FLAP FAIL MESSAGE. ZERO DEGREE FLAP LANDING. LEFT INBOARD FLAP, INBOARD ACTUATOR REPLACED. 2L72 4F RTA21EA 19960802005091996080200509NM 1996 8 2 CA951130013 119951117A276082950010277 PIPE DHAV DHAV DHC8 DHC8102 2809003NM PRESSURE LINE CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 13366 0 (CAN)CREW NOTICED FLUID LEAK IN AREA OF LEFT OUTBOARD ROLL SPOILER. PRESSURE LINE TO SPOILER FOUND CRACKED. 2H72 4T RTA13NM 19960802005101996080200510NM 1996 8 2 CA951206002 119951205A2710532AD ACCESS PANEL DHAV DHAV DHC8 DHC8102 2809003NM ROLL SPOILER FOULED W K NONE O OTHER ININSP/MAINT 1 CA 22991 0 (CAN)INSPECTION AS PER AL-95-06 FOUND LH ROLL SPOILER CLAMP FOULING AGAINST PANEL. CLAMP REPOSITIONED AND PANEL REPAIRED. 2H72 4T RTA13NM 19960802005111996080200511NM 1996 8 2 CA951206003 119951205A2710532DB PANELS DHAV DHAV DHC8 DHC8102 2809003NM ROLL SPOILERS GOUGED W K NONE O OTHER ININSP/MAINT 1 CA 19102 0 (CAN)DURING INSPECTION FO SDA AL-95-06 BOTH LH AND RH ACCESS PANELS WERE WORN DUE TO FOULING OF ROLL SPOILER CLAMP. CLAMPS REPOSITIONED AND PANELS REPAIRED. 2H72 4T RTA13NM 19960802005121996080200512NM 1996 8 2 CA951206009 119951127A5310 AIRFRAME DHAV DHAV DHC8 DHC8102 2809003NM FUSELAGE LIGHTNING STRIKEW A UNSCHED LANDING C F.O.D. CRCRUISE 1 CA 0 (CAN)LIGHTNING STRIKE TO AIRCRAFT AT 11,000 FEET. BOTH DC GENERATORS KICKED OFF LINE AND LANDING GEAR DOORS OPENED. AIRCRAFT LANDED OKAY. 2H72 4T RTA13NM 19960802005131996080200513SW 1996 8 2 CA951206013 119951127A2742DL5040MS ACTUATOR FCDINDUS SWRNGNSA226 SA226TC 8780404SW HORIZ STAB FAILED W K NONE O OTHER ININSP/MAINT 1 CA M0404 (CAN)INBOARD TRIM SWITCH WHICH SHOULD OPERATE ORAL TRIM ALARM, ALLOWED ACTUATOR TO RUN, BUT THE STABILIZER DID NOT MOVE. ACTUATOR REPLACED. 2L72 4T RTA8SW 19960802005141996080200514SW 1996 8 2 CA951209102 119951114A3231 DOOR LINKAGE OZONE OAS545 SWRNGNSA226 SA226AT 8780405SW RH MLG OUT OF ADJUST W AEH UNSCHED LANDING ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS J WARNING INDICATION APAPPROACH 1 CA 0 (CAN)AN INTRANSIT LIGHT NOTED ON FIRST FLIGHT BUT ACFT LEFT GROUND FOR NEXT FLT BEFORE CHECK. GEAR WOULD NOT EXTEND. AFTER ALL ATTEMPTS TO LOWER ACFT LANDED GEAR UP. ACFT JACKED AND RH GEAR HAD TO BE FORCED DOWN, OTHERS OK. DOOR ACTUATOR PICK UP BEARING WAS BROKEN ALLOWING DOORS TO OPERATE OUT OF SEQUENCE. LIKELY DOOR LINKAGE CAME OUT OF OVER CENTRE CAUSING DOOR ACTUATOR PICK UP BEARING P/N DW4K TO STRIKE LOWER PART OF FORK ON DOOR ACTUATOR ASSEMBLY P/N 27-55001009,INSTEAD OF INTO FORK, BRINGING DOORS TO CLOSE TOO SOON DURING MOVEMENT OF GEAR CAUSING DOORS TO JAMB AGAINST WHEELS. 2L72 4T RTA5SW 19960802005151996080200515 1996 8 2 CA951211014 419951201A34161367 KNOB DYNAMICAIR 57024929001 FOKKERF28 F28MK1000 4990808EU NR 2 ALTIMETER SEIZED W K NONE O OTHER ININSP/MAINT 1 CA 39526 1367 (CAN)ALTIMETER #2 SETTING KNOB WAS SEIZED. REPLACED. 2L72 4F RTA20EU 19960802005161996080200516EA 1996 8 2 CA951215005 119951214A3030 PITOT TUBE DHAV DHC8 DHC8311 1386006EA LEFT PITOT ICED W CD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CA (CAN)ON TAKEOFF ROLL PILOTS AIRSPEED STUCK AT 25 KNOTS. TAKEOFF REJECTED. ICE FOUND IN PITOT TUBE. 2H72 4T RTA13NM 19960802005171996080200517NE 1996 8 2 CA951218019 319951207A61117854031 BORE PLUG HAMSTD SFA13E1OA DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE PROP BLADE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 287 857643 880133 (CAN)DURING INSPECTION A CRACK WAS FOUND ON A PROPELLER BLADE BORE PLUG OUTER SIDE NEAR THE THREAD. 2H72 4T RTA13NM 6 CP7NE 19960802005181996080200518NE 1996 8 2 CA951221004 319951219A6112SFA13G1OA BLADE HAMSTD DHAV DHC8 DHC8102 2809003NM HAMSTD14SF 14SF7 NE NR 4 BLADE BURNT BOOT W O OTHER O OTHER ININSP/MAINT 1 CA 116542912 8623577 860711 (CAN)INSPECTION FOUND A HOLE BURNT THROUGH THE LEADING EDGE DE-ICER BOOT, CAUSED BY A SHORT CIRCUIT IN THE ELECTRIC DE-ICE SYSTEM, ON THE #4 BLADE ON THE #2 PROPELLER. THE PROPELLER BLADE WAS REPLACED. 2H72 4T RTA13NM 6 CP7NE 19960802005191996080200519NM 1996 8 2 CA951221005 119951219A2923731840 PUMP VICKERS DHAV DHC8 DHC8102 2809003NM NR2 STANDBY LOW OUTPUT W O OTHER J WARNING INDICATION CRCRUISE 1 CA 13029 MX424071X (CAN)#2 STANDBY HYDRAULIC PUMP OUTPUT ONLY 1,600 PSI. PUMP REPLACED. 2H72 4T RTA13NM 19960802005201996080200520EA 1996 8 2 CA951221006 119951219A2923731840 PUMP VICKERS DHAV DHC8 DHC8311 1386006EA NR2 STANDBY FAILED W O OTHER J WARNING INDICATION CRCRUISE 1 CA 12721 MX438431 (CAN)NO PRESSURE INDICATION FROM #2 STANDBY HYDRAULIC PUMP. PUMP REPLACED. 2H72 4T RTA13NM 19960802005211996080200521NM 1996 8 2 CA951221007 119951220A2450 CONNECTOR DHAV DHC8 DHC8101 2809002NM NR1 AC CONT BOX CONTAMINATED W O OTHER GJ MULTIPLE FAILURE WARNING INDICATION TXTAXI/GRND HDL 1 CA 22900 (CAN)AFTER START #2 AUXILIARY FUEL PUMP AND #1 STANDBY HYDRAULIC PUMP WOULD NOT WORK. RH AC BUSS FAIL LIGHT ILLUMINATED. CB RESET, BUT DID NOT WORK. PLUG ON #1 AC CONTACTOR BOX CLEANED. THIS FIXED PROBLEM. 2H72 4T RTA13NM 19960802005221996080200522EA 1996 8 2 CA951221008 119951220A2920170K0036CR0280 LINE DHAV DHC8 DHC8311 1386006EA STANDBY HYD LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN)HYDRAULIC LEAK IN #2 WHEEL WELL. LEAK FROM HYDRAULIC PUMP PRESSURE LINE. 2H72 4T RTA13NM 19960802005231996080200523EA 1996 8 2 CA951221009 119951220A243168001008010 MONITOR DHAV DHC8 DHC8311 1386006EA BATTERY TEMP FAILED W O OTHER N FALSE WARNING TXTAXI/GRND HDL 1 CA 4825 (CAN)BATTERY TEMPERATURE SENSOR FLASHING FULL SCALE DEFLECTION CONTINUOUSLY. MONITOR PANEL FAILED. 2H72 4T RTA13NM 19960802005241996080200524EA 1996 8 2 CA951221010 119951220A2923731840 PUMP VICKERS DHAV DHC8 DHC8311 1386006EA NR1 STANDBY HYD OVERHEATED W H DEACTIVATE SYST/CIRCUITS JM WARNING INDICATION OVER TEMP CRCRUISE 1 CA 10207 MX487811 (CAN)#1 STANDBY HYDRAULIC PUMP HOT CAUTION LIGHT CAME ON AND CB POPPED. HYDRAULIC PUMP AND PRESSURE SWITCH REPLACED. ALSO FILTERS INSPECTED. 2H72 4T RTA13NM 19960802005271996080200527CE 1996 8 2 CA951228005 119951211A2750DT2RA7 SWITCH BEECH 1900 1900D 1154162CE FLAP LIMIT FROZEN W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 1414 (CAN)JUST AFTER TAKEOFF THE CREW SELECTED FLAPS UP WITH NO CORRESPONDING MOVEMENT. AIRCRAFT RETURNED TO BASE AND INVESTIGATION FOUND THE MICRO SWITCHES FROZEN, PROBABLY FROM THE PREVIOUS NIGHTS WASHING OF THE AIRCRAFT. SWITCHES CLEANED, DRIED AND SYSTEM CHECKED OUT SERVICEABLE. 2L72 4T RTA24CE 19960802005281996080200528SW 1996 8 2 CA951228007 119951218A29102781032756 LINE SWRNGNSA226 SA226TC 8780404SW RH NACELLE PIERCED W K NONE JK WARNING INDICATION FLUID LOSS LDLANDING 1 CA (CAN)LOW PRESSURE WARNING ON AFTER LANDING. ALL HYDRAULIC POWER LOST. SYSTEM CHECKED AND LEAK FOUND ON A LINE IN RH NACELLE. LINE HAD BEEN PIERCED BY A HARD OBJECT. 2L72 4T RTA8SW 19960806000021996080600002NM 1996 8 6 CA951129516 119951016A25308650010000 OVEN BOEING767 767233 NM NR 3 GALLEY BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN)PRIOR TO DEPARTURE SMOKE IN #3 GALLEY OVEN CAVITY. CHANGED #3 OVEN AND CONTROLLER. 2L72 4F RTA1NM 19960806000061996080600006NM 1996 8 6 96ZZZX3663 119951009A5510 CHORD BOEING727 7272J7 138400ENM LT HORIZ STAB CORRODED AS ULHFK NONE O OTHER ININSP/MAINT 1 SO23552NA 20706 WHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 3 ELEVATOR HINGE FITTING AT STABILIZER STA 151, ELEVATOR STA 136.30, AREA 3-91 EFFECTED. CLEANED UP WITHIN SRM LIMITS 55-10-01, FIGURE 1, SHEET 1. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL MODIFICATION SVCS INC. 2L73 4F A3WE 19960806000071996080600007NM 1996 8 6 96ZZZX3664 119951009A5510 CHORD BOEING727 7272J7 138400ENM HORZ STAB CORRODED AS ULHFK NONE O OTHER ININSP/MAINT 1 SO23552NA 20706 WHILE PERFORMING CPCP TASK CARD NR C55-300-10.01, FOUND INDICATION OF LEVEL 2 CORROSION. THIS CORROSION EFFECTED THE LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE CHORD AROUND FASTENERS FOR THE NR 2 ELEVATOR HINGE FITTING AT STABILIZER STA 118.65, ELEVATOR STA 173.21, ZONE 3-91. THE EFFECTED AREA CLEANED UP WITHIN SRM LIMITS 55-10-01, FIGURE 1, SHEET 1. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL MODIFICATION SVCS INC. 2L73 4F A3WE 19960806000081996080600008NM 1996 8 6 96ZZZX3665 119951009A57116516201188 SPAR FITTING BOEING727 7272J7 138400ENM RT WING CORRODED AS ULHFK NONE O OTHER ININSP/MAINT 1 SO23552NA 20706 FOUND LEVEL 2 CORROSION WHILE PERFORMING TASK NR C57-581-03. THE CORROSION EFFECTED A FITTING ON THE RIGHT WING REAR SPAR LOWER CHORD AT WBL 94 INCHES, AT ZONE 6-85. REPLACED FITTING AND CLEANED CHORD PER SRM 51-10. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL MODIFICATION SVCS INC. 2L73 4F A3WE 19960806000091996080600009NM 1996 8 6 96ZZZX3666 119951204A5313BAC1498137 STRINGER BOEING727 7272J7 138400ENM BS 500-520 CORRODED AS ULHFK NONE O OTHER ININSP/MAINT 1 SO23553NA 20707 WHILE PERFORMING CPCP TASK CARD NR C53-113-01.01, FOUND CORROSION BLEEDING FROM FASTENERS ON STR 26L BETWEEN STA 500 - STA 520 IN ZONE 1-13. OPEN AREA FOUND LEVEL 2 CORROSION ON STRINGER. REPLACED SECTION OF STRINGER FROM STA 480 TO STA 515. THE REMAINDER OF STR 26L CLEANED UP WITHIN SRM LIMITS 53-10-1. MAINTENANCE ACCOMPLISHED BY PROFESSIONAL MODIFICATION SVCS INC. 2L73 4F A3WE 19960806000161996080600016EU 1996 8 6 CA951204001 119951130A2913520696 PUMP BAG BAE146BAE146200A 1500266EU YELLOW HYD SYS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN)HYDRAULIC LEAK NOTED FROM HYDRAULIC BAY. FOUND PTU (PUMP) LEAKING. 2H74 4F RTA49EU 19960806000171996080600017EU 1996 8 6 CA951221002 119951219A2913716853 PUMP VICKERS BAG BAE146BAE146200A 1500266EU HYDRAULIC PTU LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 727 F7837130 (CAN)HYDRAULIC POWER TRANSFER UNIT PUMP LEAKING. 2H74 4F RTA49EU 19960806000181996080600018EU 1996 8 6 CA951221003 119951219A2910520696 PTU VICKERS BAG BAE146BAE146200A 1500266EU HYDRAULIC SYS FAILED W K NONE J WARNING INDICATION ININSP/MAINT 1 CA 9974 266 F8910747 (CAN)PTU FAILED DURING COCKPIT CHECK, POWER TRANSFER UNIT REPLACED. 2H74 4F RTA49EU 19960808007581996080800758CE 1996 8 8 CA951108018 119951101A324422X675108190 TIRE GOODYEAR BEECH 200 200BEECH 1152920CE TREAD SIDEWALL BULGED TREAD W K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA 362 42940926 (CAN)WHILE CARRYING OUT DAILY INSPECTION NOTICED INBOARD TIRE DID NOT APPEAR NORMAL. THERE WAS BULGING OF THE SIDEWALL AND TREAD ON SOME PORTIONS OF THE TIRE. THE TREAD IN THESE AREAS WAS FOUND TO BE SOFT WHEN DEPRESSED. THE TIRE TREAD ALIGNMENT ALSO APPEARED TO BE OFF CENTRE IN THE BULGED AREAS. 1L72 4T A24CE 19960808007591996080800759NM 1996 8 8 CA951108020 119951029A276082950010137 LINE DHAV DHC8 DHC8102 2809003NM LH OB SPOILER HOLED W O OTHER K FLUID LOSS CRCRUISE 1 CA 13263 (CAN)PILOT NOTICED RH HYDRAULIC GAUGE LOOSING QUANTITY. FLUID TRANSFERRED FROM LEFT SIDE. MAINTENANCE FOUND A LEAK IN LH OUTBOARD GROUND SPOILER PRESSURE LINE. 2H72 4T RTA13NM 19960808007601996080800760EA 1996 8 8 CA951108021 119951021A2913601751005 PUMP SPERRYVICRS CNDAIRCL600 CL6002A12 1900304EA HYDRAULIC FAILED W K NONE O OTHER ININSP/MAINT 1 CA 4752 (CAN)HYDRAULIC PUMP FOUND WITH METAL PARTICLES IN CASE DRAIN FILTER. 2L72 4F RTA21EA 19960808007611996080800761CE 1996 8 8 CA951108022 119951023A27106565007144 CABLE ASSEMBLY CESSNA500 550 2076604CE AIL R/H UPPER WORN W K NONE O OTHER ININSP/MAINT 1 CA 2000 (CAN)DURING A DAILY INSPECTION, THE R/H AILERON WAS MOVED AT THE WING WHERE A RUBBING SOUND WAS HEARD. UPON INVESTIGATION, IT WAS DISCOVERED SEVERAL CABLE PASS THROUGH HOLES IN THE WING RIB WERE RUBBED BY THE CABLE. VERY LITTLE WEAR COULD BE SEEN ON THE CABLE AT THIS POINT. LATER IT WAS DISCOVERED THAT AT R.W.S. 36, THERE WAS SEVERE WEAR AND A FEW BROKEN STRANDS. 1L72 4F A22CE 19960808007621996080800762EU 1996 8 8 CA951108023 119951023A5230350A2100321001 DOOR ASSEMBLY SNIAS 350 AS350D 8680803EU L/H CARGO MISRIGGED W O OTHER JEDWARNING INDICATION VIBRATION/BUFFET INFLIGHT SEPARATION DEDESCENT 1 CA (CAN)SHORTLY AFTER TAKEOFF, PILOT NOTICED THE DOOR CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BASE AND DOOR OPENED AND THEN CLOSED FIRMLY. THE LIGHT WENT OUT. PILOT SET OUT ON SECOND LEG AND UPON LAND ING CHECKED DOOR AND FOUND SECURE. ON THIRD LEG DOOR LIGHT CAME ON AGAIN AND AS PILOT REDUCED SPEED FOR DESCENT SHE HEARD A THUMP AND FELT VIBRATION. UPON LANDING SHE FOUND THE L/H CARGO DOOR HAD COME OFF IN FLIGHT PUNCTURING ONE MAIN ROTOR BLADE. IT APPEARS THAT THE WARNING LIGHT WAS RIGGED TO INDICATE THAT THE DOOR WAS FULLY LATCHED WHEN IN FACT IT WAS NOT. VISUALLY THE DOOR APPEARED CLOSED PROPERLY. 1G71 3U H9EU 19960808007711996080800771SW 1996 8 8 CA951108037 119951026A3222 YOKE SWRNGNSA226 SA226TC 8780404SW LH MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)ULTRASONIC INSPECTION CARRIED OUT AS PER AD 95-19-07R1 AND SB 226-32-065 CRACK .500 INCH LONG IN LEFT MAIN LANDING GEAR YOKE. LH GEAR REPLACED. 2L72 4T RTA8SW 19960808007721996080800772SW 1996 8 8 CA951108038 119951026A3222 YOKE SWRNGNSA226 SA226TC 8780404SW NOSE GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)ULTRASONIC INSPECTION CARRIED OUT AS PER AD 95-19-07R1 AND SB 226-32-065. CRACK .500 INCH LONG IN NOSE YOKE 2L72 4T RTA8SW 19960808007731996080800773EA 1996 8 8 CA951109001 119951108A306078926511 BRACKET DHAV DHC8 DHC8311 1386006EA BRUSH BLOCK BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)#2 PROP BRUSH BLOCK MOUNTING BRACKET BROKEN. 2H72 4T RTA13NM 19960808007741996080800774EA 1996 8 8 CA951109002 119951108A323182910010175 LINE DHAV DHC8 DHC8311 1386006EA NLG DR ACTUATOR CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN)HYDRAULIC LINE ON NOSE GEAR DOOR ACTUATOR LEAKING. 2H72 4T RTA13NM 19960808007761996080800776EA 1996 8 8 CA951110004 119951030A3234555404 VALVE CNDAIRCL600 CL6002A12 1900304EA LANDING GEAR SHORTED W K NONE O OTHER TXTAXI/GRND HDL 1 CA 8259 (CAN)NOSE LANDING GEAR CONTROL CIRCUIT BREAKER POPPED ON APPLICATION OF GROUND POWER. SELECTOR VALVE FOUND INTERNALLY SHORTED. 2L72 4F RTA21EA 19960808007771996080800777EA 1996 8 8 CA951110005 119951031A2432600591407 CHARGER CNDAIRCL600 CL6002A12 1900304EA BATTERY FAILED W K NONE J WARNING INDICATION CRCRUISE 1 CA 4408 (CAN)BATTERY CHARGER FAIL LIGHT ON DURING FLIGHT. BATTERY CHARGER FOUND FAILED. 2L72 4F RTA21EA 19960808007801996080800780CE 1996 8 8 CA951110008 119951102A3246300257 WHEEL BFGOODRICH 50300010133 BEECH 90 65A90 1152908CE BOLT HOLE BORE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7 B887 (CAN)WHEEL CRACKED AT BOLT HOLE COUNTERBORE BASE, CIRCUMFERENTIALLY TOWARDS THE INSIDE SURFACE OF THE WHEEL. 1L72 3T 3A20 19960808007811996080800781SW 1996 8 8 CA951114001 119950928A29102781032793 LINE FRCHLDSA227 SA227CC SW HYD SHUT OFF CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)HYDRAULIC LINE CHAFED BY ENGINE RPM SPEED LEVER CABLE NEAR HYDRAULIC SHUT OFF. 2L72 4T RTA18SW 19960808007821996080800782EA 1996 8 8 CA951114005 119951111A731210718G HEAT EXCHANGER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE FUEL/OIL FAILED W O OTHER J WARNING INDICATION CRCRUISE 1 CA 9115 507 123150 (CAN)#2 ENGINE FUEL TEMP AT REDLINE IN CRUISE AND ON GROUND. OIL/FUEL HEAT EXCHANGER REPLACED. 2H72 4T4 TRTA13NM E20NE 19960808007831996080800783NM 1996 8 8 CA951114006 119951111A8010YD4N RELAY DHAV DHC8 DHC8102 2809003NM STARTER FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER ININSP/MAINT 1 CA (CAN)#2 ENGINE IGNITORS ON CONTINUOUSLY AND STARTER SWITCH WILL NOT AUTO DISENGAGE. START RELAY FOUND FAILED. 2H72 4T RTA13NM 19960808007841996080800784SW 1996 8 8 CA951114008 119951108A29102781006137 LINE SWRNGNSA226 SA226TC 8780404SW RH WING ROOT CRACKED W O OTHER G MULTIPLE FAILURE CLCLIMB 1 CA (CAN)LOW PRESS LIGHT FLICKERED DURING GEAR RETRACT & THEN CAME ON STEADY. HYD PRESS TO ZERO & NLG UNSAFE LIGHT ON. ALTHOUGH NLG INDICATED DOWN & LOCKED. TOTAL HYD FAILURE . MLG WAS RETRACTED. CRACKED HYD LINE IN THE RH WING ROOT FOUND. FOLLOWING REPLACEMENT OF LINE, AIR WAS IN HYD SYSTEM & THE ACCUM CONTAINED NIL AIR PRESSURE & HYD FLUID HAD MIGRATED PAST THE PISTON. FAILURE MAY HAVE BEEN CAUSED BY FLAT ACCUM. POWERFUL & RAPID OSCILLATION OF HYD PRESS IS CAUSED BY THE ACTION OF PUMPS ALLOWING A "BORDEN TUBE EFFECT" & HYD TUBES ARE STRESSED AT ANY BENDS. NO PRESSGAUGE ON ACCUMULATOR, 2L72 4T RTA8SW 19960808007851996080800785GL 1996 8 8 CA951114009 319950829A6114D4720 HUB CESSNA206 U206F 2073333CE CONT MCAULY3A32C D3A32C90 GL THREADS CRACKED W O OTHER K FLUID LOSS ININSP/MAINT 1 CA 501 765747 (CAN)PROPELLER HAD PERSISTENT "RED DYE" OIL LEAKS SINCE SEPTEMBER 1989, PROPELLER REMOVED SIX TIMES FOR LEAKS. LAST REMOVAL/INSPECTION HUB THREADS FOUND CRACKED AND PROPELLER REMOVED FROM SERVICE. 1H71 3O A4CE 5 CP21EA 19960808007871996080800787SO 1996 8 8 CA951114013 119951103A3710441CC7 VACUUM PUMP RAPCO 441CC7 PIPER PA31 PA31 7103102SO VALVE BLOCKAGE W K NONE O OTHER ININSP/MAINT 1 CA 55654 (CAN)BEFORE TAKEOFF, DURING GROUND RUNS THE TWO WARNING LIGHTS "VACUUM PUMP INOP." LIGHT UP TOGETHER. INSPECTION FOUND THE RIGHT HAND PUMP SEIZED AND THE ONEWAY VALVE HALF BLOCKED BY A PIECE OF RUBBER. SOU RCE OF THE RUBBER IS UNKNOWN. FILTERS CHECKED AND CHANGED. 1L72 3O A20SO 19960808007881996080800788SO 1996 8 8 CA951116003 119950903A7810 MUFFLER CONE PIPER PA28 PA28140 7102802SO EXHAUST SYSTEM BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)EXHAUST CONE BROKE OFF INSIDE THE MUFFLER ASSEMBLY CAUSING A PARTIAL OBSTRUCTION TO THE EXHAUST PATHS OF #2 & #4 CYLINDERS. BECAUSE THE ENGINE CONTINUED TO RUN SMOOTH THE ONLY INDICATION OF A PROBLEM WAS A SHORTFALL OF THE FULL STATIC R.P.M. THE NEWER MUFFLERS HAVE A CONTINUOUS PIPE THROUGH THE RESONATOR, UNLIKE THIS FAILED ITEM WHICH IS ORIGINAL PIPER EQUIPMENT AND IS JOINED INTERNALLY WHICH CAN LEAD TO COLLAPSE. 1L71 3O 2A13 19960808007911996080800791CE 1996 8 8 CA951116006 119951106A3230508103385 HOOK DOWNLOCK BEECH 200 200BEECH 1152920CE RT MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 14466 (CAN)DURING INSPECTION OF THE RIGHT HAND GEAR A CRACK WAS FOUND IN THE DOWNLOCK HOOK. THE HOOK WAS REPLACED AND GEAR SWINGS PROVED ACCEPTABLE. 1L72 4T A24CE 19960808007921996080800792CE 1996 8 8 CA951116007 119951107A3260 SWITCH BEECH 200 200BEECH 1152920CE LT MLG DWNLOCK BROKEN WIRE W E ENGINE SHUTDOWN J WARNING INDICATION APAPPROACH 1 CA 14466 (CAN)L/H GEAR LIGHT DID NOT COME ON WHEN GEAR SELECTED. EMERGENCY EXTENSION AND LEFT HAND ENGINE SHUTDOWN AS A PRECAUTION. AIRCRAFT LANDED SAFELY. INSPECTION REVEALED A BROKEN WIRE ON THE DOWNLOCK SWITCH A T THE DRAG BRACE GEAR ATTACH POINT. 1L72 4T A24CE 19960808007941996080800794SW 1996 8 8 CA951116010 119951108A322060NBC2074YZP BEARING SWRNGNSA226 SA226TC 8780404SW NLG RUSTY W O OTHER G MULTIPLE FAILURE TXTAXI/GRND HDL 1 CA (CAN)AFTER LANDING CREW UNABLE TO TAXI OFF RUNWAY BECAUSE NOSE WHEEL WOULD NOT RESPOND. NOSE GEAR AND STEERING ACTUATOR REPLACED TO NO AVAIL. HYDRAULIC SYSTEM THEN FLUSHED. BOTH NOSE STEERING FILTER AND MA IN HYDRAULIC FILTERS REPLACED, STEERING THEN OKAY. THIS AIRCRAFT HAD PREVIOUS HISTORY OF NOSE LANDING GEAR AND STEERING PROBLEMS. DURING DISASSEMBLY OF NLG BOTTOM BEARING WAS FOUND TO BE WATER CONTAIMINATED AND VERY RUSTY. THIS BEARING PROBABLY FROZE AT EACH NOSE STEERING FAILURE. 2L72 4T RTA8SW 19960808007951996080800795CE 1996 8 8 CA951116012 119951108A301015323 DE-ICE VALVE ? 15323 BEECH 200 200BEECH 1152920CE SOLENOID PORT B INOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 CA 4914 43490U (CAN)MALFUNCTION OF THE HORIZ STAB SURFACE DE-ICERS WAS SUSPECTED DUE TO FAILURE TO RECOGNIZE A THIRD BUMP AS SHOULD BE INDICATED ON THE PNEUMATIC PRESS GAUGE. FURTHER INVEST REVEALED THAT THE SOLENOID FOR PORT B, WHICH SUPPLIES PRESSURE TO THE HORIZ STAB BOOTS, LOCATED INTERNALLY IN THE DISTRIBUTOR VALVE, WAS NOT BEING ACTIVATED. REPLACEMENT PART WAS SUBSEQUENTLY INSTALLED AND SYS CHECKED OK. 1L72 4T A24CE 19960808007961996080800796EA 1996 8 8 CA951116013 219950613A72613022374 SEAL PWA 310019601 BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA MAIN OIL PUMP CUT W K NONE K FLUID LOSS ININSP/MAINT 1 CA PCE80879 (CAN)AFTER ENGINE INSTALLATION THE OIL TANK WAS FILLED WITH 10 LITERS OF OIL. THE FOLLOWING DAY AN OIL SPILL WAS NOTICED BENEATH THE ENGINE. THE OIL LEAK WAS FOUND TO ORIGINATE FROM THE COMPRESSOR INLET CA SE. INSPECTION REVEALED NO OIL IN THE OIL TANK. REMOVAL OF THE ACCESSORY GEARBOX DRAIN PLUG REVEALED THE OIL WAS TRANSFERRING FROM THE OIL TANK TO THE ACCESSORY GEARBOX (AGB). REMOVAL OF THE AGB REVEALED THE MAIN OIL PRESSURE PUMP SEAL WAS CUT. THE SEAL WAS REPLACED. 1L72 4T4 T A24CE E4EA 19960808007971996080800797CE 1996 8 8 CA951116014 119951101A7714EM8001 TACHOMETER BEECH 200 200BEECH 1152920CE DRIVE SHAFT ERRATIC W K NONE P NO WARNING INDICATION CRCRUISE 1 CA 4890 (CAN)PILOT REPORTED THAT N1 TACHOMETER INDICATOR FLUCTUATES ERRATICALLY, APPROXIMATELY 1 OR 2 PERCENT IN CRUISE. TACHOMETER REMOVED FROM THE ENGINE. INSPECTION REVEALED THE DRIVE SHAFT WAS STIFF TO TURN AN D GRINDING COULD BE HEARD FROM INSIDE THE UNIT. TACHOMETER REPLACED AND ENGINE GROUND RUN SERVICEABLE. 1L72 4T A24CE 19960808007981996080800798WP 1996 8 8 CA951116016 219951019A7240310166812 COMB CHAMBER SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP LT ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 5338 P44144C (CAN)DURING A ROUTINE 'A' CHECK, MAINTENANCE PERSONNEL FOUND THE LEFT HAND ENGINE COMBUSTION CHAMBER CRACKED WHICH WAS 1 3/4" LONG IN THE AREA OF THE WELD FOR THE PLENUM DRAIN VALVE BOSS. RECTIFICATION INV OLVED REPLACING THE ENGINE FOR REPAIR. 2L72 4T4 TRTA8SW E4WE 19960808007991996080800799NM 1996 8 8 CA951116018 119951104A573085350599005 PANEL DHAV DHC8 DHC8102 2809003NM WING 262DT DEPARTED W O OTHER D INFLIGHT SEPARATION TOTAKEOFF 1 CA 18002 (CAN)PANEL 262DT OVERWING WAS NOT INSTALLED CORRECTLY AND WAS BLOWN OFF DURING TAKEOFF. 2H72 4T RTA13NM 19960808008001996080800800NM 1996 8 8 CA951116019 119951104A2750745581 SHAFT ASSEMBLY DHAV DHC8 DHC8102 2809003NM FLAP DRIVE SHEARED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 22187 (CAN)ON APPROACH FLAP SELECTION RESULTED IN FLAP DRIVE CAUTION LIGHT ILLUMINATING, AND REMAINING ON AFTER LANDING. INSPECTION REVEALED FLAP SECONDARY DRIVE HAD SHEARED AT THE COUPLING. SUSPECT IMPROPER MAI NTENANCE DURING INSTALLATION FOLLOWING DRIVE COUPLING INSPECTION. 2H72 4T RTA13NM 19960808008011996080800801EU 1996 8 8 CA951116020 119951108A3242MT011 HEAT PACK DUNLOP AHA1413 BAG BAE146BAE146200A 1500266EU MLG BRAKE SEPARATING W K NONE O OTHER ININSP/MAINT 1 CA 115131179 MT011 (CAN)HEAT PACK ASSEMBLY SEPARATING FROM BRAKE ASSEMBLY. 2H74 4F RTA49EU 19960808008021996080800802NM 1996 8 8 CA951116021 119951108A2932APT7510004000SW SWITCH KULITE DHAV DHC8 DHC8102 2809003NM HYDRAULIC BROKEN BODY W K NONE K FLUID LOSS NRNOT REPORTED 1 CA 16951 (CAN)HYDRAULIC LEAK FOUND IN #2 NACELLE. #2 HYDRAULIC SYSTEM PRESSURE TRANSDUCER ON THE PRESSURE MANIFOLD FOUND DAMAGED. TOP OF SWITCH HAD COME APART. 2H72 4T RTA13NM 19960815002661996081500266EA 1996 8 15 96ZZZX3971 219951230A7200 ENGINE BAC 146 AVRO146RJ1001500096EU LYC ALF502ALF502* 41580EA NR 4 MALFUNCTIONED W ANCFCD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 SO23504MM E3221 RNG - FLT 160 - ABORTED TAKEOFF DUE TO N1 ENGINE NR 4 FALL 3 PERCENT OF N1 TARGET 96.8 OAT REPORTED 12 OC. ENGINE NR 4 WAS CHECKED AND PERFORMED SEQUENCE OF MAINTENANCE CONTROL CENTER EDR NR 086. TEST ON GROUND IS OK. MODE AUTO AND MANUAL. HOURS, 2,912. CYCLES, 2,780. 2H74 4F4 FRTA49EU E6NE 19960815002681996081500268NE 1996 8 15 96ZZZX3973 219951222A7200 ENGINE BAC 146 AVRO146RJ1001500096EU LYC LF507 LF5071F NE NR 3 FAILED W AANCFE ENGINE SHUTDOWN EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 SO23506MM E3244 FLT 180 - EXCESSIVE ENGINE VIBRATION. ENGINE NR 3 (3.0 OF VIBRATION). ENGINE SHUT DOWN IN-FLIGHT. ENGINE NR 3 WAS REPLACED. RUN-UP TEST NORMAL. PERFORMED FUNCTIONAL TEST, OK. ENGINE S/N OFF: LF07305, S/N ON: LF07201. 2H74 4F4 FRTA49EU E6NE 19960815002711996081500271EU 1996 8 15 96ZZZX3976 119951120A61215485020 SYNC ACTUATOR STBROSSD3 SD360 8100606EU LT ENGINE FAILED AL PIVAK NONE O OTHER ININSP/MAINT 1 WP13711PK 2007527MUW SH3696 PROPELLER SYNCHRONIZATION INOPERABLE. PROPELLER SYNCHRONIZATION ACTUATOR NOT RETURNING THE PROPELLER GOVERNOR INPUT DRIVE TO THE CENTER WHEN PROPELLER SYNC WAS SWITCHED OFF. 2H72 4T A41EU 19960815006881996081500688NE 1996 8 15 CA951120001 119951105A6410S6111730101045 BLADE SKRSKYS61 S61N 8142104NE T/R CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 10159 (CAN)TAIL ROTOR BLADE WAS FOUND TO HAVE A SKIN CRACK. 2G72 4U 1H15 19960815006891996081500689NE 1996 8 15 CA951120002 119951001A6310S6135206073 SPUR GEAR SKRSKYS61 S61N 8142104NE R/H SPUR GEAR PLATING FLAKING W K NONE O OTHER ININSP/MAINT 1 CA 558 (CAN)DURING ROUTINE INPUT FREEWHEEL CHANGE, R/H SPUR GEAR AFT BEARING SURFACE HAD AN AREA APPROXIMATELY 3/16" X 1/2" OF SURFACE PEELED OFF. 2G72 4U 1H15 19960815006901996081500690CE 1996 8 15 CA951120008 119951107A7830V315 SWITCH CESSNA 55652249 CESSNA500 550 2076604CE L/H THRUST REV BROKEN WIRING W O OTHER F FLT CONT AFFECTED LDLANDING 1 CA 1671 (CAN)AFTER LANDING,THRUST REV LIGHTS SHOWED NORMAL DEPLOYMENT,BUT AFTER SELECTING STOW,THEY REMAINED DEPLOYED & THE UNLOCK LIGHTS REMAINED ON.SELECTING THE EMERGENCY STOW SWITCH STOWED THE THRUST REV. TROUBLESHOOTING, FOUND THAT SWITCHES S153 & S161, IN THE PEDESTAL,HAD BROKEN WIRING.THE SWITCHES ARE ATTACHED TO THE RESPECTIVE POWER LEVER ASSY & THE WIRING LEADING AWAY IS HEAT SHRINK WRAPPED & POTTED IN THE VICINITY OF THE SWITCHES. IT IS IN THE IMMEDIATE AREA OF THE SWITCHES THAT ALL OF THE FAILURES HAVE OCCURRED.BOTH THE LT & RT SWITCHES ARE ROUTED IN THE SAME MANNER,BUT IT IS ONLY THE LEFT SWITCHES THAT ARE CAUSING PROBLEM. 1L72 4F A22CE 19960815006911996081500691CE 1996 8 15 CA951120012 119951020A2720040010749 CONTROL CABLE CESSNA150 150L 2071826CE PULLEY FS 173 FRAYED W K NONE O OTHER ININSP/MAINT 1 CA 1288 (CAN)DURING SCHEDULED INSPECTION FRAYED RUDDER CABLES WERE FOUND WHERE THE CABLES RIDE THROUGH THE PULLEYS AT STA. 173.41 THROUGH 200.37. THE CABLES WERE REMOVED AND REPLACED. 1H71 3O 3A19 19960815006931996081500693CE 1996 8 15 CA951120014 119951110A21202297009 SOLENOID BEECH 200 200BEECH 1152920CE AMBIENT AIR BURNT OUT W A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA 4929 (CAN) WHILE PERFORMING MAINTENANCE, GROUND POWER WAS USED FOR TESTING. SMOKE WAS OBSERVED EXITING THE TOP OF THE RIGHT HAND ENGINE COWL. ELECTRICAL POWER WAS SHUT OFF. INVESTIGATION FOUND SMOKE COMING FROM THE AMBIENT AIR SHUTOFF VALVE SOLENOID, LOCATED INLINE BETWEEN THE PNEUMOSTAT AND THE BUTTERFLY AIR VALVE OF THE RIGHT SIDE FLO-PACK ASSEMBLY. THE SOLENOID IS POWERED TO CLOSE. IT IS NORMALLY OPEN AND IS THEREFORE POWERED UP WHILE THE AIRCRAFT IS ON THE GROUND WITH POWER TO THE BUS. 1L72 4T A24CE 19960815006941996081500694NE 1996 8 15 CA951122001 219951115A73228070434 FCU MTSBSIMU2 MU2B35 5780411CE GARRTTTPE331TPE3316252M 01514NE RT ENG FAILED W A E ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 CA 311 P33087C (CAN) DURING TAXI FOR TAKEOFF, THE RIGHT HAND ENGINE EXPERIENCED AN UNCOMMANDED INCREASE IN POWER OUTPUT TOWARD MAXIMUM. THE CREW SHUTDOWN THE ENGINE WITH EMERGENCY STOP/FEATHER LEVER. THE ENGINE WAS REMOVED, A NEW FCU WAS INSTALLED, AND THE ENGINE RE-INSTALLED. GROUND RUN AIRCRAFT AND RETURNED TO SERVICE. FCU SENT TO MANUFACTURER FOR REPAIR AND INVESTIGATION. SUBMITTER SUSPECTS INTERNAL FAILURE. 1H72 3T RTA10SW E2WE 19960815006961996081500696NM 1996 8 15 CA951122003 119951121A276082950010271 LINE DHAV DHC8 DHC8102 2809003NM SPOILER ACT CRACKED W O OTHER K FLUID LOSS NRNOT REPORTED 1 CA (CAN)LOSS OF ALL #1 HYDRAULIC FLUID. RH INBOARD ROLLL SPOILER ACTUATOR LINE FOUND CRACKED. 2H72 4T RTA13NM 19960815006971996081500697NM 1996 8 15 CA951122004 119951117A71208DK1763001 STRUT DHAV DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE REAR ENG MOUNT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA PCE120369 (CAN)REAR ENGINE MOUNT STRUT #2 ENGINE INBOARD FOUND CRACKED JUST BELOW MID POINT CROSSBRACE BOLT HOLE. STRUT WAS MODIFIED AS PER MOD 8/1763 AND AD CF-92-14. 2H72 4T4 TRTA13NM E20NE 19960815006981996081500698EA 1996 8 15 CA951122005 119951121A243141307 SENSOR SAFT 20412 DHAV DHC8 DHC8311 1386006EA BATTERY TEMP FAILED W K NONE N FALSE WARNING NRNOT REPORTED 1 CA 9065 41307 (CAN)MAIN BATTERY INDICATOR IN THE RED. NO OVER TEMP INDICATED. BATTERY AT NORMAL TEMP TO TOUCH. BATTERY REPLACED DUE TO SENSOR FAILURE. 2H72 4T RTA13NM 19960815006991996081500699EU 1996 8 15 CA951122007 119951024A6230350A37118322 BEARING LOCK SNIAS 350 AS350BA 8680817EU MAST SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)MAST BEARING CHIP PLUG WAS SHEARED. INVESTIGATION FOUND THAT THE BEARING LOCK HAD SEPARATED AT THE WEAKEST POINT NEAR THE BEARING KEYWAY AND WAS PULLED OUTBOARD WHICH SHEARED THE MAGNETIC CHIP PLUG. 1G71 3U NCH9EU 19960815007001996081500700SW 1996 8 15 CA951122008 119951114A6220206011100021 M/R HEAD BELL 206 206B 1181511SW STATIC STOPS INCORRECT SHIMS W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 6677 (CAN)WHILE ATTEMPTING TO TRACK AND BALANCE ROTOR ASSEMBLY AFTER A HEAD CHANGE, THE VERTICAL VIBRATION COULD NOT BE REMOVED. DETAILED INVESTIGATION FOUND THE STATIC STOP SHIMMING WAS INCORRECT, THIS ALLOWEDTHE INBOARD FITTINGS TO MOVE WITHIN THE YOKE ASSEMBLY (0.030" SHIM HAD TO BE REMOVED). 1G71 3U H2SW 19960815007011996081500701GL 1996 8 15 CA951122009 219951103A72506898735 NOZZLE BELL 206 206L 1181522SW ALLSN 250C 250C20B 03013GL TURBINE ASSEMBLYBELOW SPECFS W K NONE O OTHER ININSP/MAINT 1 CA 6152 900 CAE802430BA (CAN)POWER CHECKS BELOW SPECS. TURBINE ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 19960815007021996081500702EU 1996 8 15 CA951122010 119951109A2842647510032 TRANSMITTER SNIAS 350 AS350B 8680801EU FUEL QTY FAILED W K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA (CAN)LOW FUEL LIGHT DOES NOT ILLUMINATE, FUEL QUANTITY TRANSMITER ASSEMBLY REPLACED. 1G71 3U H9EU 19960815007031996081500703SW 1996 8 15 CA951122011 119951106A6710206001342001 CYCLIC TUBE BELL 206 206B 1181511SW BOLT SLOTS CRACKED W K NONE F FLT CONT AFFECTED ININSP/MAINT 1 CA 11369 (CAN)TWO CRACKS FOUND IN UPPER ATTACHMENT SLOT STARTING FROM INSIDE AND PROGRESSING OUTWARD. CRACKS WERE STILL WITHIN THE BEVELLED SLOT OF THE UPPER MOUNTING BOLT AREA. 1G71 3U H2SW 19960815007041996081500704EU 1996 8 15 CA951122012 119951110A6520350A33215300 HINGE SNIAS 350 AS350B 8680801EU T/R GR BOX SEPARATING W K NONE E VIBRATION/BUFFET ININSP/MAINT 1 CA 270 (CAN)TAIL ROTOR VIBRATION. FOUND ELASTOMERIC TO BE SEPARATING. 1G71 3U H9EU 19960815007051996081500705CE 1996 8 15 CA951122013 119951113A553007120013 FITTING CESSNA 0712055201 CESSNA185 A185F 2072821CE VERT STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3815 (CAN)MIDDLE FITTING FOR THE VERTICAL SABILIZER FOUND CRACKED ON REMOVAL. 1H71 3O 3A24 19960815007061996081500706CE 1996 8 15 CA951122014 119951113A551007120487 HORIZONTAL STAB CESSNA 0712055201 CESSNA185 A185F 2072821CE L/H SIDE CRACKED W A K NONE O OTHER ININSP/MAINT 1 CA 8058 (CAN) LEFT HAND ATTACH POINT FOR HORIZONTAL STABILIZER FOUND CRACKED. REINFORCEMENT P/N 0712048-7 IS PART OF THE STABILIZER ATTACHMENT. SUBMITTER STATES THAT SUSPECT CAUSE IS USING THE HORIZONTAL STABILIZER TO PUSH THE AIRCRAFT. 1H71 3O 3A24 19960815007071996081500707CE 1996 8 15 CA951122015 119951113A2742071250011 ACTUATOR SCREW CESSNA 07125001 CESSNA185 A185F 2072821CE L/H & R/H SIDE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)LEFT AND RIGHT HAND TRIM ACTUATOR SCEWS WORN WHERE THEY SIT IN THE BEARING. SUBMITTER SUGGESTS INSTALLING KIT P/N SK 185-27 WHICH INCLUDES AN INSPECITON PANEL AND LUBRICATION PROVISIONS. 1H71 3O 3A24 19960815007091996081500709WP 1996 8 15 CA951122018 219951111A726031033541 IDLER GEAR SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP ACCESS GEARBOX EXCESSIVE WEAR W A O OTHER O OTHER ININSP/MAINT 1 CA 14380 9P3268 P54219 (CAN) IMMEDIATELY AFTER AN OIL SAMPLE, THE CHIP DETECTOR LIGHT ILLUMINATED. MAINT INVEST REVEALED A SMALL AMOUNT OF UNIDENTIFIED METAL ACROSS THE CHIP DET CONTACTS. THE ACFT WAS CLEARED TO CONTINUE IN SERVICE. SEVERAL WEEKS LATER THE CHIP DET LIGHT AGAIN ILLUMINATED, IN FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. EXAM OF THE ENG & CHIP DET LED TO DISASSEMBLY OF THE ENG. DISASSEMBLY REVEALED EXCESS WEAR OF THE IDLER GEAR FACE & WEAR TO THE IDLER GEAR BEARINGS, P/NS 9AA11SOCN & AA11SOCN. THE CLOSE PROXIMITY OF THE IDLER GEAR TO THE BEARINGS MAY HAVE CONTRIBUTED TO THEIR SUBSEQUENT FAILURE. 2L72 4T4 TRTA8SW E4WE 19960815007101996081500710CE 1996 8 15 CA951122019 119951121A324006111800 BRAKE CALIPER 06111800 CESSNA208 208B 2073701CE BOLT HOLES CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6554 (CAN)DURING A COMPANY REFIT PROGRAM CRACKS WERE FOUND BY SEVERAL BOLT HOLES THAT ATTACH THE PAD ASSEMBLIES TO THE MAIN BODY ALSO AREAS OF CORROSION WERE FOUND 1H71 3T A37CE 19960815007111996081500711CE 1996 8 15 CA951122020 119951109A325026430533 RING BOLT CESSNA 26430533 CESSNA208 208B 2073701CE STEERING RING WORN W K NONE O OTHER ININSP/MAINT 1 CA 6277 (CAN)DURING MAINTENANCE THE STEERING RING WAS FOUND TO BE LOOSE. FURTHER INVESTIGATION REVEALED THE BOLT THAT ATTACHES THE STEERING RING TO THE GEAR WAS LOOSE. THE BOLT WAS REMOVED AND FOUND TO BE WORN. A NEW BOLT WAS INSTALLED AND THE SYSTEM CHECKED OUT, OK. 1H71 3T A37CE 19960815007121996081500712NM 1996 8 15 CA951122022 119951116A77003038579 WIRING HARNESS DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR 2 ENGINE FAULTY W E ENGINE SHUTDOWN O OTHER APAPPROACH 1 CA 8T841 RH120824 (CAN)MOMENTARY TORQUE EXCURSION ON APPROACH, FOLLOWED SHORTLY AFTER BY OVERTORQUE ON #2 ENGINE ENGINE WAS SHUTDOWN ON SHORT FINAL. OVERTORQUE WAS WITHIN LIMITS FROM FDR READOUT#2 ENGINE HARNESS WAS REPLACED AND PROBLEM RECTIFIED. 2H72 4T4 TRTA13NM E20NE 19960815007141996081500714CE 1996 8 15 CA951122026 119951116A7830V315 SWITCH CESSNA500 550 2076604CE THRUST REV SW BROKEN WIRE W K NONE L NO TEST TXTAXI/GRND HDL 1 CA 1809 (CAN)WHILE CONDUCTING GROUND TEST, L/H THRUST REVERSER DID NOT DEPLOY. TECHNICIAN FOUND WIRE #K106C20 BROKEN AT THE MICROSWITCH P/N V3 15. 1L72 4F A22CE 19960815007151996081500715CE 1996 8 15 CA951122027 119951116A7897 WIRE CESSNA500 550 2076604CE THRUST REV SW DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WHILE TROUBLESHOOTING SNAG, TECHNICIAN FOUND WIRE GOING AROUND L/H THRUST REVERSER SWITCH WAS BEING DAMAGED BY A COTTER PIN. WIRE REPAIRED. 1L72 4F A22CE 19960815007181996081500718EA 1996 8 15 CA951123108 119950906A2842 TRANSMITTER DHAV DHC3 DHC3 2800202EA FUEL QTY FAULTY W A A UNSCHED LANDING X ENGINE FLAMEOUT CRCRUISE 1 CA (CAN)AN UNSCHEDULED LANDING WAS CARRIED OUT AFTER THE ENGINE FLAMED OUT IN CRUISE. THE ENGINE FLAMED OUT DUE TO FUEL STARVATION. FUEL WAS ADDED AND THE FLIGHT CONTINUED. SUBSEQUENT INVESTIGATION TO THE FUEL QUANTITY INDICATOR SYSTEM REVEALED A BUILD-UP OF SALT CRYSTALS IN THE CENTER TANK TRANSMITTER UNIT CAUSING THE UNIT TO REMAIN AT 60 GALLONS INDICATED. THE INDICATOR UNIT WAS CLEANED, THE CALIBRATION CHECKED AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3R A815 19960815007191996081500719CE 1996 8 15 CA951124001 119951104A523099430062612 FAIRING 994300621 BEECH 99 99 1154002CE CARGO POD DEPARTED W A K NONE D INFLIGHT SEPARATION CRCRUISE 1 CA (CAN) BOTTOM PANEL OF CARGO POD AFT FAIRING DEPARTED AIRCRAFT IN FLIGHT. UPON WALK AROUND AFTER LANDING THE LOSS WAS IDENTIFIED 1L72 3T A14CE 19960815007231996081500723EA 1996 8 15 CA951127004 119951116A78103022254 INNER CONE DHAV DHC6 DHC6 2802606EA NR3 BRG COVER SHIFTED POSITIONW A K NONE O OTHER ININSP/MAINT 1 CA 1550 (CAN) DURING AN INSPECTION THE #3 BEARING COVER WAS FOUND TO HAVE SHIFTED POSITION, THIS CONDITION IF NOT RECTIFIED WOULD ALLOW THE PART TO ROTATE AND CAUSE WEAR LEADING TO SEPARATION AND RUBBING ON THE TURBINE WHEEL. 1H72 3T RTA9EA 19960815007241996081500724EA 1996 8 15 CA951127005 119951116A78103022254 INNER CONE DHAV DHC6 DHC6 2802606EA NR3 BRG COVER DAMAGED W A K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA 3025 (CAN) DURING A ROUTINE HOT SECTION INSPECTION (HSI), THE #3 BEARING COVER WAS FOUND TO BE WEARING AND IF NOT REPAIRED IT WOULD CAUSE SEPARATION FROM ITS LOCATION AND RUB ON THE TURBINE WHEEL. 1H72 3T RTA9EA 19960815007251996081500725EA 1996 8 15 CA951127006 119951115A78103022254 INNER CONE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043EA NR3 BRG COVER SEPARATED W A K NONE O OTHER ININSP/MAINT 1 CA 2950 PCE42463 (CAN) A PIECE OF METAL WAS FOUND ON THE APRON WHERE MANY AIRCRAFT HAD BEEN MOVING. AFTER THE RETURN AN INSPECTION OF THE ENGINE FOUND THE #3 BEARING COVER TO HAVE ROTATED CAUSING WEAR ON THE INNER CONE DUCT ASSEMBLY, ALLOWING IT TO SEPARATE FROM THE DUCT AND DAMAGE THE POWER TURBINE WHEEL. 1H72 3T4 T A9EA E4EA 19960815007261996081500726 1996 8 15 CA951127008 119951122A5413HS5722545 STRINGER CVAC STC STC340CVAC ALLSN 501D 501D13 03004GL OUTBD NACELLE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 26267 500816 (CAN)DURING INSPECTION PHASE A SLIGHT BULGE IN THE SKIN ON THE OUTBOARD ENGINE NACELLE AT STN 135.O TO 171.0, WATER LINE 0.0 TO 111.0 BETWEEN RIVETS WAS DETECTED. AN NDT X-RAY REVEALED SLIGHT CORRO SION IN THE AREA OF THE RIVETS AND EXTENSIVE CORROSION ON A STRINGER REMOVED FROM THIS AREA. REPAIRS TO THIS AREA OF CORROSION CARRIED OUT. 2L72 4R4 TT 6A6 E282 19960815007271996081500727SO 1996 8 15 CA951127009 119951015A32306751000 DOWNLOCK BEARINGPIPER PIPER PA28 PA28R200 7102811SO MLG DOWNLOCK WORN W L ABORTED APPROACH O OTHER APAPPROACH 1 CA 9149 (CAN)PILOT FAILED TO GET AN INDICATION WHEN THE GEAR WAS SELECTED DOWN. EMERGENCY SELECTION WAS MADE AND THE AIRCRAFT LANDED SAFELY. INVESTIGATION FOUND THE DOWNLOCK BEARING HAD WORN TO THE POINT WHERE THE MICRO SWITCH TAB WAS ACTUALLY MISSING ITS CONTACT POINT. 1L71 3O 2A13 19960815007281996081500728CE 1996 8 15 CA951127201 119951102A325012606311 TRIM ROD END CESSNA CESSNA206 U206G 2073356CE STEERING MIS REPAIRED W A K NONE O OTHER ININSP/MAINT 1 CA 7536 (CAN) PILOTS REPORTED THAT THE AIRCRAFT HAD POOR STEERING ON THE GROUND. MAINTENANCE FOUND THE RUDDER CONTROL CABLE TENSION LOW. AN UNAUTHORIZED REPAIR WAS MADE TO THE TRIM BUNGEE ROD END BY WAY OF WELDING WHICH SHORTENED THE THREADED PORTION AND THUS THE ADJUSTMENT CAPABILITY. 1H71 3O A4CE 19960822002291996082200229EA 1996 8 22 CA951127003 119951120A2460 CIRCUIT BREAKER DHAV DHC6 DHC6 2802606EA PWA AVIONICS IMPROPER WIRED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)AVIONICS BREAKER FOUND FED WITH INDIVIDUAL #18 GAUGE WIRE RATHER THAN THE NORMAL BUSS BAR ARRANGEMENT. IN ADDITION, SEVERAL OF THE CIRCUIT BREAKERS WERE IMPROPERLY LABELLED AND CONNECTED TO MORE THAN ONE SYSTEM. FOR EXAMPLE, THE BREAKER LABELLED "RNAV", ALSO FED THE RAD ALT., PILOT'S HORIZON AND PILOTS DG. 1H72 3T RTA9EA 19960822002311996082200231SO 1996 8 22 CA951127204 119951025A3260487862 SWITCH PIPER PA31 PA31350 7103110SO MAIN GEAR STUCK W O OTHER P NO WARNING INDICATION APAPPROACH 1 CA 7961 (CAN)PILOT SELECTED GEAR DOWN AND RECEIVED NO INDICATION FROM THE LEFT MAIN GEAR. PILOT RAN THE RED PAGES AND EVENTUALLY MADE A SUCCESSFUL LANDING. MAINTENANCE FOUND THE MICRO-SWITCH WAS STUCK. SUSPECT POSSIBLE ICE AS THE AIRCRAFT HAD BEEN CLEANED RECENTLY. 1L72 3O A20SO 19960822002351996082200235NE 1996 8 22 CA951130001 219950912A73220164448330 FCU SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE OSCILLATING W K NONE O OTHER ININSP/MAINT 1 CA 818 303 (CAN)FCU OSCILLATING. REMOVED AND REPLACED. 1G71 3U3 U H9EU E19EU 19960822002361996082200236NE 1996 8 22 CA951130002 219950619A73220164448160 FCU SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE ENGINE FAULTY W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CLCLIMB 1 CA 2239 2239 303 (CAN)ENGINE DECELERATED CAUSING LOSS OF RPM. FUEL FLOW LEVER WAS REMOVED TO EMERGENCY GATE BY THE PILOT WITH NO RESULTS. 1G71 3U3 U H9EU E19EU 19960822002371996082200237EU 1996 8 22 CA951130007 119951127A6220350A312005 EXTERNAL STOP SNIAS 350 AS350B 8680801EU TMECA M/R HEAD CORROSION W K NONE O OTHER ININSP/MAINT 1 CA (CAN)EXFOLIATION CORROSION ON OUTBOARD SIDE OF STOP. 1G71 3U H9EU 19960822002381996082200238EU 1996 8 22 CA951130008 119951127A6720350A27191004 CONTROL TUBE SNIAS 350 AS350B 8680801EU TMECA T/R BEARING LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN)SPHERICAL BEARING FOUND LOOSE IN CONTROL TUBE. 1G71 3U H9EU 19960822002391996082200239EA 1996 8 22 CA951130010 219951128A741462224 GASKET BENDIX D3000 CESSNA182 TR182 2072735CE LYC O540 O540L3C5 41532EA MMAG MOUNTING STRESSED W K NONE O OTHER ININSP/MAINT 1 CA 236 L2237140A (CAN)REPORT OF A ROUGH RUNNING ENG, LED TO FINDING A MAG LOOSE ON FLANGE & THAT THE HOLD DOWN NUTS HAD BACKED OFF & MT FLANGE WAS SEVERELY WORN.MAG CASE WAS REPLACED. REPAIRED MAG WAS RETURNED WITH A P/N 62224 GASKET THAT HAS THE MOUNT EARS INCORPORATED.SUBMITTER BELIEVES THAT DUE TO THE TYPE OF MOUNTING CONFIGURATION,WITH THE HOLD DOWN CLAMPS,THE PROPER GASKET SHOULD BE P/N LW 12681 WITHOUT THE EARS.THE EARS ON THE P/N 62224 GASKET WAS COMPRESSING & THE RESULTING STRESS FAILURE RELAXED THE TORQUE ON THE MOUNTING NUTS ALLOWING THE MAG TO ROTATE. THE GASKET WAS REPLACED WITH A 12681 MOUNTING GASKET,AFTER THE MAG WAS FOUND LOOSE WITH THE 62224 GASKET INSTALLED. 1H71 3O3 O 3A13 E295 19960822002401996082200240 1996 8 22 CA951130011 419951116A341846001SA04 STALL WARN LEAR 25 25B 5170511CE COCKPIT FAULTY CARD W H DEACTIVATE SYST/CIRCUITS FN FLT CONT AFFECTED FALSE WARNING CRCRUISE 1 CA 89 (CAN)FLIGHT CREW REPORTED DURING FLIGHT THAT WHILE IN CRUISE, STICK PUSHER CAME ON. THEY MANUALLY SELECTED L/H STALL WARNING SWITCH OFF. STICK PUSHER RELEASED, NO FURTHER INCIDENT. STALL WARNING CARD FOUND DEFECTIVE, PUSHER REMAINED ON AT ALL TIMES. DEFECTIVE CARD REPLACED. 2L72 4J A10CE 19960822002411996082200241SW 1996 8 22 CA951130012 119951109A2823206031117033 PAN ASSEMBLY BELL 206 206B 1181511SW ALLSN FUEL SOV BLOCKED DRAIN W K NONE O OTHER ININSP/MAINT 1 CA 8296 (CAN)DURING PRE-FLIGHT, PILOT CYCLED THE FUEL SHUT OFF SYSTEM AND NOTICED A DIFFERENT NOISE THAN NORMAL. FUEL VALVE ACCESS PANEL REMOVED AND PAN AREA WAS FOUND 2/3RDS FULL OF ICE WHICH HAD TOTALLY ENCASED THE FUEL SHUT OFF VALVE. THE PAN DRAIN WAS CLOGGED WHICH ALLOWED WATER TO BACK UP DURING SEVERE RAIN STORM THE PREVIOUS NIGHT AND DUE TO A DRASTIC TEMPERATURE CHANGE BECAME ICE. 1G71 3U H2SW 19960822002441996082200244CE 1996 8 22 CA951130018 119951121A56101013840258 WINDSHIELD BEECH 1013840258 BEECH 200 200BEECH 1152920CE PWA WINDOW RT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7363 88H09420 (CAN)DURING RUN-UP WINDSHIELD HEAT WAS APPLIED. RIGHT HAND WINDSHIELD CRACKED FROM THE BOTTOM APPROXIMATELY FOUR INCHES FROM THE LEFT HAND EDGE. 1L72 4T A24CE 19960822002491996082200249EA 1996 8 22 CA951204002 119951115A7922721648 THERMOSTAT STWARNER 10528A DHAV DHC6 DHC6300 EA ENG OIL FAILED W E ENGINE SHUTDOWN M OVER TEMP CRCRUISE 1 CA 27 386 (CAN)THERMOSTAT FAILED TO OPEN WHICH DID NOT ALLOW OIL TO PASS THROUGH COOLER. OIL TEMPERATURE EXCEEDED LIMITS AND ENGINE WAS SHUT DOWN. 1H72 3T A9EA 19960822002501996082200250EU 1996 8 22 CA951204027 119951031A7120350A21106605 MOUNT SNIAS 350 AS350D 8680803EU LYC INBOARD BRACKET CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)L/H MOUNT ASSEMBLY CRACKED. 1G71 3U H9EU 19960822002511996082200251EU 1996 8 22 CA951204028 119951015A7120350A21106606 MOUNT SNIAS 350 AS350D 8680803EU LYC RT LT ENG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)BOTH R/H AND L/H ENGINE MOUNTS FOUND CRACKED. 1G71 3U H9EU 19960822002541996082200254SO 1996 8 22 CA951206006 119951202A2435 STARTER LKHEED382 382G 526414USO ALLSN HAMSTD NR 1 GR BOX WORN DRIVE W E ENGINE SHUTDOWN J WARNING INDICATION CRCRUISE 1 CA 13205 (CAN)DURING CRUISE, THE #1 ENGINE REDUCTION GERABOX CHIP DETECTOR LIGHT ILLUMINATED AND THE ENGINE WAS SHUT DOWN AS A PRECAUTION. MAINTENANCE INVESTIGATION REVEALED THAT THE DRIVE TEETH ON THE STARTER WERE WORN OUT. THE DRIVE WAS REPLACED AND THE OIL SYSTEM FLUSHED. 2H74 4T A1SO 19960822002551996082200255GL 1996 8 22 CA951206007 219951203A7250 BLADES LKHEED382 382G 526414USO ALLSN 501D 501D22A 03006GL TURBINE SECTION DAMAGED W A O OTHER O OTHER TOTAKEOFF 1 CA 4401 4401 500706 (CAN)DURING A THREE ENGINE FERRY FLIGHT ON TAKEOFF, A LOUD BANG WAS HEARD, FOLLOWED BY 1000 DEGREES C TIT INDICATION. THE THROTTLE WAS PULLED BACK AND NO OTHER INDICATIONS WERE NOTED. ON DESCENT, WHEN POWER WAS PULLED BACK, AN NTS OCCURRED WITH HIGH FUEL FLOW AND HIGH TIT. THE ENGINE WAS SHUT DOWN ON THE GROUND. MAINTENANCE FOUND DAMAGE TO THE TURBINE BLADES. 2H74 4T4 T A1SO E282 19960822002571996082200257EU 1996 8 22 CA951206010 119951127A3020 INTAKE LIP BRAERO748 HS7482A 4231001EU NR 1 ENG FAILED HEAT W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA (CAN)IN CRUISE CREW OBSERVED #1 ENGINE INTAKE LIP TO BE GLOWING AND SPARKING. DE-ICE TURNED OFF. AIRCRAFT RETURNED. LIP ASSEMBLY REPLACED. 2L72 3T A24EU 19960822002581996082200258EA 1996 8 22 CA951209101 219951107A73223010466 FCU ARM BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA FUEL CONTRL UNITDISCONNECTED W A EA ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CLCLIMB 1 CA PCE80606 (CAN)ON CLIMB OUT SHORTLY AFTER TAKEOFF THE #2 ENGINE LOST TORQUE AND AUTOFEATHERED. THE ENGINE WAS SECURED AND A SINGLE ENGINE LANDING WAS CARRIED OUT. INSPECTION FOUND THE FUEL CONTROL UNIT (FCU) ARM WAS ROTATING FREELY ON THE SERRATED WASHER THAT CONNECTS IT TO THE FCU INPUT SHAFT. THE ENGINE WAS REPLACED 76.5 HOURS EARLIER. THE ARM WAS FOUND "NOT" SECURED WITH LOCKWIRE TO THE ATTACHING NUT. THE ENGINE WAS RERIGGED AND SAFETYED AND GROUND RUN SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A24CE E4EA 19960822002591996082200259NE 1996 8 22 CA951211002 219951208A731110718T HEAT EXCHANGER STWARNER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE OIL FUEL FAILED W O OTHER M OVER TEMP CRCRUISE 1 CA 1163 120164 (CAN)#2 ENGINE FUEL TEMPERATURE TOO HIGH. FUEL TEMPERATURE PROBE REPLACED. STILL NO GOOD. OIL FUEL HEAT EXCHANGER REPLACED. 2H72 4T4 TRTA13NM E20NE 19960822002601996082200260CE 1996 8 22 CA951211003 119951207A3222MS28775328 O-RING MITSUELECT 010A39190 MTSBSIMU2 MU2B36 5780412CE NLG STRUT CHAFED W A OH OTHER DEACTIVATE SYST/CIRCUITS G MULTIPLE FAILURE APAPPROACH 1 CA 1410 1410 (CAN)THE CREW MADE AN UNEVENTFUL SHORT TURN AROUND AT DAWSON CREEK (-35C),THEN PROCEEDED TO FT. ST. JOHN (-41C). DURING THE APP A LOUD BANG WAS HEARD DURING GEAR EXTENSION. ALL ATTEMPTS TO LOWER THE GEAR WERE UNSUCCESSFUL. THE ACFT MADE A SUCCESSFUL GEAR-UP LANDING ON AN ICE COVERED RUNWAY. THERE WERE NO INJURIES & VERY LITTLE DAMAGE TO THE AIRCRAFT. INVEST FOUND THE GEAR DOORS TIGHT AGAINST THE MAIN TIRES. THE GEAR WAS EXTENDED & THE NOSE STRUT FOUND FLAT. SUBMITTER STATES THAT THE NOSE GEAR STRUT WENT FLAT ON TAKEOFF FROM DAWSON DUE TO THE COLD & A "CHAFED" 'O'RING. THIS ALLOWED THE DOORS TO CLOSE APPROX. 95 PERCENT, EN OUGH TO SIGNAL GEAR-UP, BUT ALSO JAMMING THE GEAR IN THE UP POSITION. 1H72 3T RTA10SW 19960822002611996082200261CE 1996 8 22 CA951211010 119951205A324422X675108190 TIRE PARKER HANNI04020300 BEECH 200 200BEECH 1152920CE PWA LT OUTB MAIN BULGED W K NONE O OTHER ININSP/MAINT 1 CA 468 1477 (CAN)BULGE ON THE LEFT OUTBOARD MAIN TIRE, NOTICED WHILE PERFORMING DAILY INSPECTION. SEEMS TO INDICATE A SEPARATION IN THE INBOARD TREAD AREA. REFERENCES: SDRS 951108018, 951222004 AND 951108001. 1L72 4T A24CE 19960822002621996082200262CE 1996 8 22 CA951211011 119951204A272024670011 TORQUE TUBE CESSNA CESSNA172 172RG 2072438CE LYC RUDDER BROKEN W A A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 6345 (CAN)SHORTLY AFTER TAKEOFF THE PILOT HEARD A LOUD BANG, AFTER WHICH RUDDER AUTHORITY WAS LOST. AIRCRAFT LANDED SAFELY AND INVESTIGATION FOUND THE FORWARD RUDDER PEDAL TORQUE TUBE HAD CRACKED APPROXIMATELY 3/4 OF THE WAY AROUND. THIS ALLOWED THE TORQUE TUBE TO BEND AND TWIST AND LOSS OF RUDDER CABLE TENSION. THE BREAK OCCURRED IN THE CENTRE STRUCTURE AREA BETWEEN THE RUDDER PEDALS. SUBMITTER STATES THAT THIS AREA IS DIFFICULT TO INSPECT. 1H71 3O 3A17 19960822002641996082200264SW 1996 8 22 CA951211018 119951021A561036004312 WINDSHIELD GULSTM690TP 690D 3970405SW ARSRCH COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA 8379 (CAN)THE WINDSHIELD OUTER GLASS CRACKED WHEN ON DESCENT TO AIRPORT. 1H72 3T 2A4 19960822002661996082200266SO 1996 8 22 CA951212002 119951211A2430 WIRE PRESTOLITE ALU8421 PIPER PA31 PA31 7103102SO ALTERNATOR CHAFED W AH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CLCLIMB 1 CA 2K000007 (CAN)DURING CLIMB OUT THE CREW NOTICED A LOW VOLTAGE WARNING LIGHT. THEY SELECTED AUX REGULATOR AND SHORTLY AFTER AGAIN GOT A LOW VOLTAGE WARNING LIGHT. AIRCRAFT DIVERTED TO MAINTENANCE BASE. INVESTIGATION REVEALED AN OVERVOLTAGE CONDITION WHICH WAS TRACED TO A CHAFED WIRE. WIRE REPAIRED. 1L72 3O A20SO 19960822002701996082200270CE 1996 8 22 CA951212007 119951125A321308412121 O-RING CESSNA421 421C 2076016CE MLG STRUT WORN W K NONE O OTHER ININSP/MAINT 1 CA 4147 4147 (CAN)WHILE COMPLYING WITH AD 90-02-13, THE L/H AND R/H PIN SUPPORT RINGS (SEAL SUPPORTS) WERE REMOVED AND FOUND TO HAVE RIPPED AND MISSING PHENOLIC TAPE ON THE INNER SURFACE. FOUR NEW PIN SUPPORT RINGS WER E INSTALLED IN BOTH GEAR. 1L72 3O A7CE 19960822002721996082200272GL 1996 8 22 CA951215001 319951204A6111R1015255 BLADE DHAV DHC2 DHC2EVANS 2801832EA PWA HARTZLHCB3R HCB3R304 GL NR 1 BLADE TIP SEPARATION W BE EMER. DESCENT ENGINE SHUTDOWN DE INFLIGHT SEPARATION VIBRATION/BUFFET CRCRUISE 1 CA 191 EM93 (CAN)THE PROPELLER BLADE SEPARATED 6 INCHES FROM THE TIP DURING CRUISE FLIGHT. THE PROPELLER HAS BEEN RETURNED TO THE OVERHAULER. 1H71 3O A806 5 CP28EA 19960822002731996082200273NM 1996 8 22 CA951215002 119951213A5610NP1579014 WINDSHIELD PPG DHAV DHC8 DHC8101 2809002NM PWA RH OUTER LAYER SHATTERED W O OTHER O OTHER CRCRUISE 1 CA 222734782 (CAN)RH WINDSHIELD OUTER LAYER SHATTERED INFLIGHT. NO APPARENT REASON POSSIBLE HEAT OR STATIC CAUSE. 2H72 4T RTA13NM 19960822002741996082200274NE 1996 8 22 CA951215003 219951213A731110718K HEAT EXCHANGER STWARNER DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE NR1 FUEL OIL FAILED W K NONE JM WARNING INDICATION OVER TEMP CRCRUISE 1 CA 5606 556 608 120083 (CAN)#1 ENGINE FUEL TEMPERATURE NEARING MAXIMUM. FUEL OIL EXCHANGER REPLACED. 2H72 4T4 TRTA13NM E20NE 19960822002811996082200281CE 1996 8 22 CA951215011 119951206A261224418922 FIRE WIRE CESSNA CESSNA208 208B 2073701CE PWA FIREWALL SHORTED W H DEACTIVATE SYST/CIRCUITS N FALSE WARNING DEDESCENT 1 CA CAN)PILOTS REPORTED FIRE WARNING ACTIVATED & LASTED ABOUT 20 SECONDS THEN DEACT IVATED. NORMAL LANDING WAS CARRIED OUT BUT SYSTEM ACTIVATED AGAIN ON TAXIING & REMAINED ON. MAINTENANCE TROUBLE SHOT THE FAULT TO THE FIREWALL CONNECTION BEHIND THE INERTIAL SEPARATOR & THE UPPER STANBY SIDE OF THE FIREWALL. CONNECTIONS WERE CLEANED & DRIED & REINSTALLED. APPROXIMATELY 2.5 HOURS INTO SERVICE THE FAULT REAPPEARED. AIRCRAFT GROUNDED FOR FURTHER INVESTIGATION. INVESTIGATION REVEALED THAT BOTH ENDS OF THE FIRE WIRE, ON THE INERTIAL SEPARATOR & ONE UPPER STANDBY SIDE FIREWALL WERE LOOSE CAUSING AN INTERMITTENT CIRCUIT. THE FIRE WIRE WAS REPLACED & NO FURTHER FAULTS WERE OCCURRED. 1H71 3T A37CE 19960822002831996082200283SO 1996 8 22 CA951215013 219951207A7414107902010 MAGNETO BENDIX CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO INTERNAL GEAR FAILURE W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 513 175034R (CAN)THE MAGNETO INTERNAL DRIVE GEAR FAILED. THERE WAS NO APPARENT REASON. 1H71 3O3 O 3A24 E5CE 19960822002841996082200284CE 1996 8 22 CA951215014 119951113A2752503801535 DRIVE BEECH 1295210511 BEECH 90 C90 1152913CE PWA LT FLAP INB ACT BROKEN TOOTH W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 30 511B95 (CAN)ON APPROACH, FLAP WAS SELECTED AND IT WAS IMMEDIATELY NOTICED THAT THE LEFT INBOARD FLAP DID NOT EXTEND. AIRCRAFT EXHIBITED A SLIGHT ROLL TO THE LEFT, BUT WAS LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LACK OF CONTINUITY THROUGH THE 90 DEGREE DRIVE OF THE LEFT INBOARD ACTUATOR. 1L72 3T 3A20 19960822002851996082200285NM 1996 8 22 CA951215015 119951212A2710DB532 PANEL DHAV DHAV DHC8 DHC8102 2809003NM PWA ROLL SPOILER GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)IN ACCORDANCE WITH SDA AL-95-06 AND AOM 369 MINOR INTERFERENCE AND CHAFING FOUND ON EXISTING PANEL. 2H72 4T RTA13NM 19960822002861996082200286CE 1996 8 22 CA951215016 119951207A3222SK15011 FORK CESSNA 0442504201 CESSNA150 152 2071835CE NLG LEFT ARM CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7885 (CAN)NOSE GEAR FORK FOUND CRACKED DURING INSPECTION. NO CORROSION FOUND. CRACK MEASURED 1.25 INCHES IN LENGTH. 1H71 3O NT3A19 19960822002881996082200288EA 1996 8 22 CA951215018 119951008A2710NAS5411 BOLT DHAV C2CF161A DHAV DHC2 DHC2MK1 2800102EA PWA AILERON CONT WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)AT THE AILERON CABLES CONNECTION IN THE FUSELAGE AT THE FORWARD EXTREMITY OF LEVER ASSEMBLY P/N C2CF161A BOLT SHOWED SIGNS OF WEAR BY THE LINK CONTROL CABLE P/N C2CF307. 1H71 3R A806 19960822002901996082200290NM 1996 8 22 CA951215020 119951116A2710532DB PANELS DHAV DHAV DHC8 DHC8102 2809003NM PWA ROLL SPOILER GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WITH REFERENCE TO SDA AL-95-06, INSPECTION OF LOWER JAM QUADRANT PANELS CLAMP FOUND RUBBING ON ACCESS PANELS 532DB (LH) AND 632DB (RH). 2H72 4T RTA13NM 19960822002911996082200291NM 1996 8 22 CA951215021 119951116A2710532DB PANEL DHAV DHAV DHC8 DHC8102 2809003NM PWA ROLL SPOILER GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WITH REFERENCE TO AL-95-06, INSPECTION OF LOWER JAM QUADRANT PANELS, PANEL 532DB (LH) AND 632DB (RH) FOUND GOUGED. 2H72 4T RTA13NM 19960822002921996082200292NM 1996 8 22 CA951215022 119951116A2710532DB PANEL DHAV DHAV DHC8 DHC8102 2809003NM PWA ROLL SPOILER GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WITH REFERENCE TO AL-95-06, INSPECTION OF LOWER JAM QUADRANT, PANELS IN ROLL SPOILER 532DB (LH) AND 632DB (RH) AND FOUND GOUGED. 2H72 4T RTA13NM 19960822002931996082200293WP 1996 8 22 CA951215201 119951117A6720369A75058 BRACKET HUGHES369 369D 4470706WP ALLSN ROTOR PEDAL CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 7424 (CAN)TAIL ROTOR PEDAL BRACKET BROKE AWAY FROM AIRFRAME. PILOT PERFORMING PRE-FLIGHT CONTROL CHECK. 1G71 3U H3WE 19960822002941996082200294CE 1996 8 22 CA951215202 119951205A323108411066 BELLCRANK CESSNA402 402B 207590PCE R/H GEAR DOOR BROKEN W K NONE O OTHER LDLANDING 1 CA 9561 (CAN)R/H LANDING GEAR BELLCRANK BROKEN ON END THAT ACTUATES GEAR DOOR MECHANISM. NO APPARENT CAUSE, SUSPECT CYCLIC FATIGUE. FAILURE ALLOWED INBOARD GEAR DOOR TO FALL OPEN. 1L72 3O A7CE 19960822002951996082200295CE 1996 8 22 CA951218001 119951206A2913AN33701 RELAY BEECH 90 C90 1152913CE PWA HYD PUMP CONTACTS FAILED W H DEACTIVATE SYST/CIRCUITS L NO TEST TXTAXI/GRND HDL 1 CA 227 (CAN)AFTER LANDING THE HYDRAULIC PUMP WOULD CYCLE OFF. CONTACTS IN THE RELAY WERE FOUND WELDED SHUT. 1L72 3T 3A20 19960822002961996082200296WP 1996 8 22 CA951218003 119951211A6720369D21800501 PITCH CHANGE HUGHES369 369D 4470706WP ALLSN T/R DRY REQ LUBE W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 1285 (CAN)TIME EXPIRED FOR REGREASE, COMPONENT APPEARS TO HAVE NO GREASE LEFT IN ASSEMBLY. TIME THIS INSTALLATION 23 MONTHS. 1G71 3U H3WE 19960822002971996082200297GL 1996 8 22 CA951218004 219951206A732223034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL LT SIDE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA 388 CAE820289 (CAN)FUEL CONTROL LEAKING FROM ALLEN KEY, L/H SIDE OF FCU BELOW 'FROM PTG FITTING' WITH BOOST PUMP ON. 1G71 3U3 U H2SW E4CE 19960822002981996082200298WP 1996 8 22 CA951218005 119951213A6720369D21800501 LINK HUGHES369 369D 4470706WP ALLSN T/R PITCH ROUGH BEARING W K NONE O OTHER ININSP/MAINT 1 CA 347 (CAN)DURING INSPECTION FOR ABNORMAL NOISE, THE T/R PITCH CONTROL BEARING WAS FOUND TO BE ROUGH. 1G71 3U H3WE 19960822002991996082200299 1996 8 22 CA951218006 419951130A3422200DC GYRO BELL 206 206B 1181511SW ALLSN COCKPIT DG SHORTED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA 979 (CAN)DIRECTIONAL GYRO MOTOR SHORTED OUT AND EMITTED SMOKE INTO THE CABIN. 1G71 3U H2SW 19960822003001996082200300EU 1996 8 22 CA951218007 119951106A77140177555170 TACH BOX SNIAS 350 AS350BA 8680817EU TMECA ENG LOOSE PARTS W O OTHER J WARNING INDICATION CLCLIMB 1 CA 1 (CAN)TIME SINCE OVERHAUL, 0.7 HOURS. BLEED VALVE FUNCTIONED CORRECTLY ON TEST FLIGHT BUT PART WAY THROUGH NEXT FLIGHT, BLEED VALVE WOULD NO LONGER CLOSE. TACH BOX REMOVED, LOOSE PARTS FOUND INSIDE. ASSEMBLY REPLACED. AIRCRAFT RETURNED TO SERVICE. 1G71 3U NCH9EU 19960822003011996082200301SO 1996 8 22 CA951218008 119951214A3240500190025001 BRAKE DISC ASSY PLESSEY 500100925001GULSTMG159 G159 3952202SO MOTOR DRIVE END SEIZED W K NONE O OTHER ININSP/MAINT 1 CA 1285J (CAN)UNIT WAS SENT FOR REPAIR. INVESTIGATION FOUND INTERNAL CORROSION, WITH THE HEAVIEST CORROSION ON THE INTERNAL BRAKE END OF THE MOTOR. SUBMITTER STATES THAT THIS UNIT SHOULD BE INSPECTED MORE FREQUENTLY. 2L72 4T 1A17 19960822003031996082200303EA 1996 8 22 CA951218013 219951207A7200 ENGINE BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA NR 1 POSITION FAILURE W E ENGINE SHUTDOWN Y ENGINE STOPPAGE CRCRUISE 1 CA 2591 PCE50673 (CAN) BANG HEARD FROM NR 1 ENGINE DURING CRUISE FLIGHT, FOLLOWED BY IMMEDIATE POWER LOSS. ENGINE SHUTDOWN/FEATHERED AND AIRCRAFT RETURNED TO BASE. ENGINE REMOVED AND RETURNED TO PRATT & WHITNEY FOR INVESTIGATION AND REPAIR. 1L72 3T4 T A14CE E4EA 19960822003051996082200305SO 1996 8 22 CA951218018 219951211A73146493683 FUEL PUMP PIPER PA34 PA34200 7103405SO CONT O360 TSIO360E 17025SO NR 2 ENGINE FAULTY W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 747 307278 (CAN)DURING A TRAINING FLIGHT,AT 5,000 FEET,THE #2 ENGINE HAD A LOSS OF POWER & THE LOWERING OF PRESSURE ON THE FUEL FLOW INDICATOR.THE #2 ENGINE WAS SHUTDOWN & THE AIRCRAFT LANDED.AFTER ARRIVAL THE #2 ENG INE WAS RUN UP,THREE TIMES IT FAILED TO EXCEED 2,000 RPM WITH LESS THAN 10 GPH (GALLONS PER HOUR) ON THE FUEL FLOW INDICATOR.ON THE FOURTH RUN UP THE #2 ENGINE WAS NORMAL.THE PROBLEM WAS BELIEVED TO BE AN INTERMITTENT FUEL PUMP,WHICH WILL BE REPLACED.AFTER RECEIPT & INSTALLATION OF A NEW FUEL PUMP A TEST FLIGHT WILL BE DONE & IF SUCCESSFUL, THE AIRCRAFT WILL BE RETURNED TO SERVICE. 1L72 3O3 O A7SO E9CE 19960822003071996082200307NM 1996 8 22 CA951218022 119951212A2710DB532 PANEL DHAV DHAV DHC8 DHC8102 2809003NM PWA ROLL SPOILER GOUGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)IN ACCORDANCE WITH SDA AL-95-06 AND AOM 369 MINOR INTERFERENCE FOUND ON PANELS. 2H72 4T RTA13NM 19960822003091996082200309NM 1996 8 22 CA951219101 119951123A273065B848545 BRACKET BOEING747 747475 NM ELEV CABLE WORN W K NONE O OTHER ININSP/MAINT 1 CA 22462 (CAN)DURING "D" CHECK FOUND THE PRIMARY ELEVATOR CABLE E1A NOT FITTED TO ITS PULLEY AT STN 1310. CABLE HAS CUT ITS WAY THROUGH THE PULLEY FRAME ASSEMBLY BOTH FORWARD AND AFT OF THE PULLEY. BOTH PULLEY AXLEBOLT AND CABLE GUIDE BOLT FITTED AND STILL SEALED WITH THE BOEING PRODUCTION SEAL. PARTS REPLACED. 2L74 4F RTA20WE 19960822003101996082200310NM 1996 8 22 CA951219103 119951227A575369B112566 BOLT BOEING747 747475 NM FLAP CARRIAGE SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING ROUTINE INSPECITON AND RETORQUE OF THE MAIN FLAP CARRIAGE SPINDLE RETAINING NUTS, THE #1 T.E. FLAP SPINDLE NUT RETAINER HAD FALLEN OUT OF POSITION AND DAMAGED THE STRUCTURE. INSPECTION REVEALED THAT THE RETAINER NUT LOCK BOLT HAD SHEARED DUE TO HYDROGEN EMBRITTLEMENT OF THE BOLT. REPLACED. 2L74 4F RTA20WE 19960822003121996082200312SW 1996 8 22 CA951219105 119950118A6320204040353023 MAIN CASE BELL 205 205A1 1181414SW GR BOX CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 721 (CAN) CRACK FOUND ON WEB ABOVE INPUT BORE. 1G71 4U H1SW 19960822003131996082200313CE 1996 8 22 CA951219107 119951208A56101013840258 WINDSHIELD BEECH 200 B200 1152922CE PWA INNER PANE CRACKED W BI EMER. DESCENT CABIN DEPRESSURIZATION O OTHER CRCRUISE 1 CA (CAN)INNER PANE OF THE WINDSHIELD SHATTERED AT 29,000 FEET AT MAX. PRESSURE DIFFERENTIAL. EMERGENCY DESCENT TO 16,000 FEET WAS INITIATED AND PRESSURE REDUCED. 1L72 4T A24CE 19960822003141996082200314CE 1996 8 22 CA951219108 119951205A323108411066 BELLCRANK ASSY CESSNA402 402B 207590PCE RT WING DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9561 (CAN)AFTER LANDING THE PILOT NOTICED THE RIGHT HAND WING DOOR HANGING DOWN AS THE AIRCRAFT WAS BEING POSITIONED IN THE HANGAR. MAINTENANCE FOUND THE BELLCRANK WAS BROKEN ON THE END THAT ACTUATES THE GEAR DOOR MECHANISM. PART REPLACED AND GEAR CHECKS COMPLETED AND AIRCRAFT RETURNED TO SERVICE. 1L72 3O A7CE 19960822003161996082200316CE 1996 8 22 CA951221011 119951211A551107326114 RIB CESSNA CESSNA207 207A 2073604CE CONT HORIZ STAB LT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING INSPECTION OF THE AIRCRAFT, CRACKS WERE FOUND ON VARIOUS PORTIONS OF THE FLIGHT CONTROL SURFACES AND STABILIZERS. CRACKS ALL REPAIRED AND AIRCRAFT RETURNED TO SERVICE. 1H71 3O A16CE 19960822003181996082200318CE 1996 8 22 CA951221013 119951130A7120121343316 MOUNT CESSNA 12134334 CESSNA206 U206F 2073333CE CONT ENG AFT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9338 N3N (CAN)WHILE CARRYING OUT ROUTINE INSPECTION, BOTH REAR ENGINE MOUNTS WERE FOUND CRACKED. CRACKS WERE APPROXIMATELY ONE INCH LONG. NEW MOUNTS INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 1H71 3O A4CE 19960822003191996082200319SO 1996 8 22 CA951221014 119951208A275174243002 POTENTIOMETER PIPER PA31T PA31T2 7103127SO PWA FLAP IND DEFECTIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 4397 (CAN)FLAP SYSTEM GIVING FALSE INDICATION ON PANEL. RIGGING PERFORMED AND ELECTRICAL ADJUSTED. DURING FLIGHT IN COLD CONDITIONS -20 DEGREES C OAT, THE SAME LIGHT ILLUMINATED. LEFT AND RIGHT HAND POTENTIOMETERS TESTED AND THE LEFT HAND POTENTIOMETERS WAS FOUND DEFECTIVE. PARTS REPLACED AND RETURNED TO SERVICE. 1L72 3T RTA8EA 19960822003201996082200320CE 1996 8 22 CA951221015 119951209A53505042002338 FAIRING BEECH 100 100BEECH 1152916CE PWA WING TO FUSE WORN/LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN)LEFT AND RIGHT HAND WING TO FUSELAGE FAIRING RIVETS FOUND LOOSE. FILLET ABRAIDED THE SKIN TO A MAX .009". SKIN REPAIR DOUBLER FABRICATED AND INSTALLED. 1L72 3T A14CE 19960822003211996082200321SW 1996 8 22 CA951221016 119951214A2910212076146001 ELBOW BELL 212 212 1181420SW PWA HYD SYS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9487 (CAN)HYDRAULIC FITTING REMOVED, INSPECTION REVEALED CRACK ON THREADED MALE NIPPLE END. 1G71 4U H4SW 19960822003221996082200322SW 1996 8 22 CA951221017 119951207A2821MS295284 DRAIN VALVE BELL 206 206B 1181511SW ALLSN FUEL SYS LEAKING W K NONE O OTHER ININSP/MAINT 1 CA (CAN)AFTER LANDING A SMELL OF FUEL WAS PRESENT. FOUND AIRFRAME FUEL FILTER DRIPPING, REPLACED 'O' RING IN DRIAN VALVE. 1G71 3U H2SW 19960822003231996082200323SW 1996 8 22 CA951221018 119951110A6700206001343001 ELBOW BELL 206 206B 1181511SW ALLSN CYCLIC CORRODED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)FLAKING PAINT FOUND ON THE ELBOW AT UPPER END OF CYCLIC STICK. EXAMINATION REVEALED CORROSION PITTING BEYOND SERVICEABLE LIMITS. 1G71 3U H2SW 19960822003241996082200324SW 1996 8 22 CA951221019 119951025A2844206061535007 TRANSDUCER BELL 206 206L 1181522SW FUEL PRESS FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)UNSTABLE FUEL PRESSURE READINGS FOUND DURING MAINTENANCE. 1G71 3U H2SW 19960822003251996082200325GL 1996 8 22 CA951221020 219951124A732223034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE MALFUNCTION W O OTHER O OTHER LDLANDING 1 CA 3653 CAE802180BA (CAN)FCU WOULD NOT RETURN TO FLIGHT IDLE WHEN THROTTLE WAS ROLLED OFF. THROTTLE CYCLED SEVERAL TIMES BEFORE ENGINE RETURNED TO IDLE. ASSEMBLY REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 19960822003281996082200328CE 1996 8 22 CA951221029 119951214A282110192002949 FUEL STRAINER BEECH 200 B200C 1152924CE PWA INTERNAL CORRODED W K NONE K FLUID LOSS ININSP/MAINT 1 CA 13479 (CAN)DURING MAINTENANCE A LEAKING FUEL STRAINER WAS INSPECTED AND FOUND TO BE CORRODED ABOUT 3/4 OF THE WAY THROUGH THE FLANGE WHICH IN TURN CAUSED THE LEAK. THE FUEL STRAINER WAS REPLACED. 1L72 4T A24CE 19960829000021996082900002CE 1996 8 29 CA951221030 119951128A325007430118 COLLAR CESSNA CESSNA172 172N 2072434CE LYC NLG STEERING BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 5767 (CAN)DURING ROUTINE MAINTENANCE FOUND CRACKED COLLAR ON THE NOSE GEAR. REMOVED STEERING COLLAR AND FOUND BROKEN BEARING. REPLACED PARTS AND RETURNED AIRCRAFT TO SERVICE. 1H71 3O NT3A12 19960829000031996082900003GL 1996 8 29 CA951221032 319951215A6114 PROPELLER CESSNA150 152 2071835CE LYC MCAULY1A103 1A103TCM GL MOUNTING BOLTS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 775267 (CAN)DURING INSPECTION 3 CRACKS WERE SUSPECTED IN THE PROPELLER. AT THE MOUNTING BOLTS, THIS COULD NOT BE CONFIRMED BY DYE PENETRANT INSPECTION. THE PROPELLER WAS SENT TO A PROPELLER OVERHAUL SHOP AND A ZY GLO INSPECTION CONFIRMED THE CRACKS. 1H71 3O NT3A19 5 NP50GL 19960829000041996082900004EU 1996 8 29 CA951221033 119951212A3251NB41099 STEERING RING BNORM BNORM BN2 BN2B27 7080227EU LYC LH CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1025 (CAN)FOUND STEERING RING CRACKED ON TOP OF RING LEFT SIDE. FOUND IN ACCORDANCE WITH SB 214. CAA AD 005-09-93. 1H72 3O A17EU 19960829000091996082900009SO 1996 8 29 CA951222002 219951211A7414107902010 MAGNETO BENDIX CESSNA180 180J 2072622CE CONT O470 O470S 17026SO DISTRIBUTOR GEARTEETH STRIPPED W O OTHER O OTHER NRNOT REPORTED 1 CA 917 A202874 463652 (CAN)COMPLETE MAGNETO FAILURE (RIGHT HAND) REPORTED BY PILOT. INSPECTION REVEALED STRIPPED GEAR TEETH FOR ONE-HALF OF THE DISTRIBUTOR GEAR. 1H71 3O3 O 5A6 E273 19960829000111996082900011CE 1996 8 29 CA951222004 119951213A324422X675108190 TIRE GOODYEAR BEECH 200 200BEECH 1152920CE TREAD GROOVE BULGED W K NONE O OTHER ININSP/MAINT 1 CA 260 31472574 (CAN)WHILE PERFORMING DAILY INSPECTION ON THE MAIN LANDING GEAR, WHEELS AND TIRES, BULGING WAS NOTICED IN THE TREAD GROOVE OF THE FIRST INBOARD TREAD. CLOSER EXAMINATION REVEALED EXPOSED PORTIONS OF INNER CORDS ON TWO AREAS OF TREAD ABOUT 8 INCHES APART. SUBMITTER REPORTS THE 80 PERCENT OF THE TREAD WAS REMAINING ON THE TIRE - VIRTUALLY NEW. 1L72 4T A24CE 19960829000121996082900012CE 1996 8 29 CA951222005 119951212A325250420041 SHIMMY BRACKET CESSNA414 414 2075908CE NLG STRUT PIVOTED 90 DEG W O OTHER O OTHER TOTAKEOFF 1 CA 2913 (CAN)THE PILOT NOTICED THAT THE PEDALS FELT LIKE SOMETHING HOOKED THEM DURING RETRACTION OF THE GEAR. ON EXAMINATION AFTER LANDING, IT WAS DISCOVERED THAT THE STEERING CABLE HAD BEEN BENT AT THE TURNBUCKLE .THE SHIMMY DAMPER HAD ROTATED 90 DEGREES FROM IT'S POSITION AND STRUCK THE CABLE WHEN THE GEAR HAD RETRACTED. IT IS SUSPECTED THAT THIS DISPLACEMENT OF THE SHIMMY BRACKET WAS CAUSED BY AN OVERSTEERING CONDITION. THE SUBMITTER SUGGESTS THAT BY PAINTING A WITNESS MARK ON THE STRUT AND BRACKET, EARLY DETECTION OF AN OVERSTEERING CONDITION WILL BE VERY NOTICEABLE. 1L72 3O RTA7CE 19960829000131996082900013CE 1996 8 29 CA951222007 119951204A7722AN55342 BALANCE RESISTOR BEECH 200 200BEECH 1152920CE L/H ENGINE MOUNTGROUNDED W K NONE O OTHER ININSP/MAINT 1 CA 7085 (CAN)WHILE PERFORMING ENGINE RUN-UP, NOTICED A LOW ITT ON THE LEFT ENGINE. FURTHER INVESTIGATION REVEALED THE LOCKWIRE SECURING THE BALANCE RESISTOR BOX WAS TOUCHING A CONTROL CABLE AND THUS GROUNDING OUT GIVING THE SYSTEM A FALSE INDICATION. SUBMITTER SUSPECTS THE BOX WAS PROBABLY MOVED WHILE WORKING IN THE AREA OF THE ENGINE. BALANCE RESISTOR WAS SECURED. 1L72 4T A24CE 19960829000181996082900018CE 1996 8 29 CA951228002 119950620A2752C3010020104 ACTUATOR 99105861 CESSNA208 208B 2073701CE FLAP MOTOR SHORTED W O OTHER O OTHER APAPPROACH 1 CA (CAN)MULTIPLE CIRCUIT BREAKER TRIPPINGS ON DIFFERENT OCCASIONS PROMPTED THE REPLACEMENT OF THE FLAP MOTOR THREE TIMES. THE THREE MOTORS WERE SERVICEABLE AS RECEIVED FROM THE MANUFACTURER, HOWEVER THE SUBMITTER STATES THAT THERE APPEARED TO BE IMPROPER SOLDER JOINTS OF THE WIRES ON THE BRUSH HOLDER BOARD. THE WIRES HAD COME LOOSE AND MOVED TO SHORT AGAINST THE BOLT WHICH SECURE THE END CAP TO THE HOUSING. THE MOTOR WILL OPERATE IN ONE DIRECTION BUT WILL POP THE CIRCUIT BREAKER WHEN MOVED IN THE OTHER DIRECTION. 1H71 3T A37CE 19960829000191996082900019SO 1996 8 29 CA951228003 219951211A8520 BEARING CESSNA401 401A 207590DCE CONT O520 TSIO520E 17040SO CONNECTING ROD FAILED W E ENGINE SHUTDOWN EKRVIBRATION/BUFFET FLUID LOSS PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 271189R (CAN)DURING FLIGHT THE OIL PRESSURE ON THE #2 ENGINE BEGAN TO DROP SO THE ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION OF THE ENGINE REVEALED THE OIL BREATHER LINE HAD FROZEN AND CREATED A PRESSURE BUILD THAT CAUSED ONE OF THE PUSH RODS SEAL TO BLOW OUT RESULTING IN THE LOSS OF ENGINE OIL. THE OIL FILTER WAS CUT OPEN AND INSPECTED AND ALTHOUGH THERE WAS SOME EVIDENCE OF METAL CONTAMINATION IT WAS DECIDED, FOLLOWING AN ENGINE RUN-UP, TO RELEASE THE AIRCRAFT FOR A FERRY FLIGHT. THE #2 ENGINE FAILED ENROUTE DUE TO THE FAILURE OF A CONNECTING ROD BEARING. 1L72 3O3 O A7CE E8CE 19960829000201996082900020CE 1996 8 29 CA951228004 119951201A32311008100191 WELD ASSEMBLY BEECH 100 100BEECH 1152916CE MLG DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WHILE REFUELING THE AIRCRAFT, IT WAS NOTICED THAT THE RIGHT HAND INNER MAIN GEAR DOOR WAS HANGING DOWN. THE ASSEMBLY THAT HOLDS THE GEAR DOOR ATTACHMENT ARM WAS FOUND CRACKED. 1L72 3T A14CE 19960829000211996082900021CE 1996 8 29 CA951228006 119951220A7603 LOCKOUT CABLE CESSNA500 550 2076604CE THROTTLE BROKEN ROD END W K NONE O OTHER ININSP/MAINT 1 CA 1842 (CAN)DUE TO THE SEPARATION OF THE THROTTLE LOCKOUT CABLE ROD END, THE ENGINES CAN BE STARTED AND OPERATED THROUGHOUT THEIR FULL RANGE WHILE THE FLIGHT CONTROLS WERE IN THE LOCKED POSITION. 1L72 4F A22CE 19960829000221996082900022 1996 8 29 CA960102001 419951218A3452 COAX DHAV DHC3 DHC3 2800202EA TRANSPONDER DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)TRANSPONDER COAX DAMAGED BY TY-RAPS ALL ALONG ITS LENGTH CAUSING TRANSPONDER TO BE PULLED OFF FREQUENCY. IN ADDITION, THE ANTENNA WAS FOUND DAMAGED CAUSING FURTHER TRANSPONDER PROBLEMS. IN ADDITION, ANUMBER OF INSTRUMENT HOSES WERE FOUND CRACKED AND BRITTLE, INCLUDING THE ENCODER STATIC HOSE. ALSO THE AIRCRAFT HAD NO STATIC WICKS. 1H71 3R A815 19960829000231996082900023EA 1996 8 29 CA960102002 119951218A2400 ELECTRICAL SYSTM DHAV DHC3 DHC3 2800202EA PWA P3 HEAT MIS WIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN)THE AIRCRAFT ELECTRICAL SYSTEM HAS BOTH DESIGN PROBLEMS AND FAILED ITEMS. P3 HEAT CIRCUIT INCORRECT. DUCT OVERHEAT WIRED INCORRECTLY. HOBBS METER NOT WIRED CORRECTLY. INLET DEICE NOT WORKING. STARTER CB U/S. #2 JB WIRES FOUND CHAFED AND BURNED. MAIN JB WIRES ALSO FOUND CHAFED AND BURNT. BEACON IMPROPERLY WIRED. FOUR CB'S UNLABELLED. FMS WARNING PLACARD MISSING. TURBINE CONVERSION DOES NOT TIE SHUNT INTO ELECTRICAL SYSTEM CORRECTLY. THE ENGINE ELECTRICAL LOADS ARE ON THE BATTERY SIDE OF THE SHUNT, WHILE THE AIRFRAME LOADS ARE ON THE GENERATOR SIDE. STC HOLDER CONTACTED. 1H71 3R A815 19960829000241996082900024NM 1996 8 29 CA960102003 119951020A6123MS3476L2255P CONNECTOR CANNON DHAV DHC8 DHC8301 NM AUTO FEATHER CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 11752 (CAN)DURING SIO 8-61-03 INSPECTION, THE LEFT HAND CONNECTOR (9811-P13) WAS FOUND HEAVILY CORRODED. BACKSHELL AND CANNONN PLUG SHOWING SEVERE 'POWDERING' DUE TO EXCESSIVE CORROSION. THIS CORROSION POSSIBLY CAUSING LOSS OF CIRCUIT INTEGRITY IN AUTO-FEATHER SYSTEM. 2H72 4T RTA13NM 19960829000251996082900025WP 1996 8 29 CA960102004 219951219A73228070425 FCU SWRNGNSA226 SA226TC 8780404SW GARRTTTPE331TPE33110UA 01514WP ENGINE OVER ADJUSTED W E ENGINE SHUTDOWN O OTHER APAPPROACH 1 CA 648 P54214 (CAN)INSTALLED NEWLY OVERHAULED FCU. HAD TO ADJUST MAX FUEL TWICE AT 1/2 CW TURN EACH TIME. 5 MONTHS LATER, ADJUSTED ANOTHER 30 POUNDS PER HOUR. ENGINE WAS NOW UNABLE TO GO BELOW 95 PERCENT, REPLACED FCU. SUBMITTER SUGGESTS THAT THE FCUS ARE BEING RECEIVED FROM MANUFACTURER INDEXED TO THE LOW SIDE. 2L72 4T4 TRTA8SW E4WE 19960829000261996082900026EA 1996 8 29 CA960102005 119951213A7160 SNOW DEFLECTOR DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043EA NR 1 ENGINE NOT LOCKED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 6269 PCE22436 (CAN) PILOT REPORTED THAT IN CRUISE FLIGHT, IN MODERATE SNOW AND PRECIPITATION, THE NR 2 ENGINE BEGAN TO LOSE POWER. A PRECAUTIONARY ENGINE SHUTDOWN WAS CARRIED OUT. POST-FLIGHT INSPECTION REVEALED THAT THE NR 2 ENGINE SNOW DEFLECTOR WAS IN THE RETRACTED POSITION AND AS NO OTHER DISCREPANCIES WERE FOUND THIS WAS THE LIKELY CAUSE OF THE NR 2 ENGINE SHUTDOWN. THE SNOW DEFLECTOR WAS LOCKED IN THE DOWN POSITION AND THE AIRCRAFT WAS RELEASED FOR TEST FLIGHT. THE TEST FLIGHT WAS FLOWN SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1H72 3T3 T A9EA E4EA 19960829000271996082900027SO 1996 8 29 CA960102006 119951201A57514019017 SPAR PIPER 4020043 PIPER PA31 PA31350 7103110SO AIL HINGE ATTACHCRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7341 315537 (CAN)IN CARRYING OUT PIPER SERVICE BULLETIN 974 ON THE AILERON HINGE BRACKET ATTACH POINTS, THE SPAR WAS FOUND CRACKED ON THE RIGHT AILERON. UPON INSPECTION OF A REPLACEMENT PART, IT TOO, WAS DISCOVERED TO BE CRACKED IN THE SAME LOCATION. THE ORIGINAL PART WAS REPAIRED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE SUBMITTER HIGHLY RECOMMENDS COMPLYING WITH PIPER SERVICE BULLETIN #974. 1L72 3O A20SO 19960829000281996082900028 1996 8 29 CA960102102 419951120A6113D1870 SPINNER DHAV DHC2 DHC2EVANS 2801832EA HARTZLHCB3R HCB3R304 GL PROPELLER CRACKED W O OTHER O OTHER NRNOT REPORTED 1 CA EM93 (CAN) RIM ON PROPELLER BACK PLATE CRACKED CAUSING SPINNER TO FAIL. FAILED PIECE OF SPINNER HIT PROPELLER NR 1 BLADE AT LEADING EDGE APPROXIMATELY 8 INCHES FROM THE PROP GRIP. THE DAMAGE ON THE NR 1 BLADE WAS DRESSED OUT. 1H71 3O A806 5 CP28EA 19960829000301996082900030NE 1996 8 29 CA960103001 119951215A261130231R7B SMOKE DETECTOR SKRSKYS76 S76A 8143006NE BAG COMPT LAMP BURNT W K NONE O OTHER ININSP/MAINT 1 CA (CAN)BAGGAGE COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. DETECTOR CHANGED AND FOUND BEACON LIGHT BURNT OUT. BULB REPLACED. 1G72 3U H1NE 19960829000341996082900034EU 1996 8 29 CA960103006 119951213A2910 HYDRAULIC SYSTEM BRAERO748 HS7482A 4231001EU HYD SYS CONTAMINATED W A UNSCHED LANDING OJ OTHER WARNING INDICATION CRCRUISE 1 CA 27712 (CAN)AIRCRAFT HAD PARTIAL HYDRAULIC PRESSURE LOSS. AIRCRAFT DIVERTED. HYDRAULIC SYSTEM CONTAINED AIR, WITH OAT AT -44 C AND AIRCRAFT HAD COLD SOAKED FOR A NUMBER OF HOURS PREVIOUS TO TAKEOFF. 2L72 3T A24EU 19960829000351996082900035EA 1996 8 29 CA960103007 219951214A855048103 OIL FILTER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENG OIL COLLAPSED W K NONE P NO WARNING INDICATION ININSP/MAINT 1 CA 50 L679761A (CAN)DURING INSPECTION THE ENGINE OIL FILTER WAS FOUND COLLAPSED ON ONE SIDE. THIS WAS DISCOVERED WHEN THE OUTER CASE/CAN WAS CUT OPEN FOR INSPECTION. THE FILTER WAS CODED FO3F13-1. 1L72 3O3 O A20SO E14EA 19960829000371996082900037SW 1996 8 29 CA960103009 119951212A2821 FUEL SYSTEM BELL 206 206L1 1182107SW ALLSN FILTERS CLOGGING W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN)BOOST PUMP LOW PRESSURE WARNING LIGHT ON, FUEL FILTERS CHECKED FOUND SCREENS COATED IN WAX VISCOUS SUBSTANCE. ENGINE RUN, BOOST PUMP PRESSURE DROPPED TO ZERO AND #2 PUMP WARNING LIGHT ON. AIRCRAFT TAKEN INTO HANGAR TO WARM UP. PROBLEM DISAPPEARED. FUEL SAMPLE TAKEN AND SENT FOR ANALYSIS. 1G71 3U H2SW 19960829000381996082900038SO 1996 8 29 CA960103011 119950327A52464341300 ACCESS PANEL PIPER 4183405 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2B 41532EA OIL DIPSTICK LATCH FAILED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA RL13361 (CAN)AFTER TAKEOFF THE ACCESS PANEL FOR THE OIL LEVEL DIPSTICK ON THE LEFT HAND ENGINE COWLING OPENED. THE PILOT RETURNED TO BASE WHERE MAINTENANCE REPAIRED THE LATCH AND RETURNED THE AIRCRAFT TO SERVICE. 1L72 3O3 O A20SO E14EA 19960829000391996082900039WP 1996 8 29 CA960103013 119951216A5280 DOOR LKHEED1011 1011385114 WP RROYCE RT MLG DOOR DAMAGED W K NONE E VIBRATION/BUFFET CRCRUISE 1 CA (CAN)DURING CRUISE VIBRATION FELT. RH MAIN LANDING GEAR FIXED DOOR FOUND DAMAGED. REPLACED. 2L73 4F A23WE 19960829000411996082900041NE 1996 8 29 CA960103501 219951102A7320 FUEL SHUTOFF DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE ENG FUEL SEIZED W E ENGINE SHUTDOWN P NO WARNING INDICATION TXTAXI/GRND HDL 1 CA P656975D (CAN)ON ENGINE SHUTDOWN, THE RIGHT ENGINE FUEL CONTROL LEVER WOULD NOT MOVE TO THE FUEL OFF POSITION. ENGINE WAS SHUTDOWN USING FIRE SHUT OFF HANDLE. SEVERAL MINUTES LATER THE FUEL SHUT OFF LEVER COULD BE MOVED EASILY. MAINTENANCE ACTION INVOLVED LUBRICATING THE FUEL SHUT OFF EANCO CABLE. 2L72 4F4 F A6WE E2EA 19960829000421996082900042EA 1996 8 29 CA960103502 119951103A2752853D1007 ACTUATOR CNDAIRCL600 CL6002B19 EA GE LEFT OUTB FLAP FROZEN W O OTHER F FLT CONT AFFECTED LDLANDING 1 CA 1667 (CAN)UNABLE TO EXTEND FLAPS FOR LANDING. FLAPLESS LANDING CARRIED OUT. SUSPECT FLAP ACTUATOR FREEZING AT ALTITUDE. 2L72 4F RTA21EA 19960829000431996082900043EA 1996 8 29 CA960103503 119951103A2750 BPSU CNDAIRCL600 CL6002B19 EA LEFT BRAKE OUT OF ADJUST W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 1293 (CAN)FLAPS FAIL MESSAGE ON WHEN SELECTING FLAPS ON APPROACH. FLAPLESS LANDING CARRIED OUT. LEFT BRAKE POSITION SENSING UNIT (BPSU) ADJUSTED. 2L72 4F RTA21EA 19960829000441996082900044EA 1996 8 29 CA960103504 119951104A2752852D1005 ACTUATOR CNDAIR CNDAIRCL600 CL6002B19 EA RH OUTB FLAP FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 1298 (CAN)FLAPS FAIL MESSAGE ON WHEN SELECTING FLAPS. FLAPLESS LANDING CARRIED OUT. RIGHT OUTBOARD FLAP INBOARD ACTUATOR REPLACED. 2L72 4F RTA21EA 19960829000451996082900045EU 1996 8 29 CA960103505 119951104A3230664700500A4B LGCU AIRBUS320 A320211 3930320EU GEAR DOORS FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN)ON CLIMB OUT THROUGH 15,000 FEET ALL 3 LANDING GEAR DOORS BECAME UNLOCKED. SPEED REDUCED TO 240 KNOTS AND AIRCRAFT RETURNED TO BASE. MAINTENANCE ACTION INVOLVED CHANGING L.G.C.I.U. #1 & #2 (LANDING GE AR CONTROL INTERFACE UNIT). 2L72 4F RTA28NM 19960829000461996082900046EU 1996 8 29 CA960103506 119951104A2752 GEARBOX AIRBUS320 A320211 3930320EU FLAP WATER INGRESS W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)ON APPROACH, FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION. FLAPS RECYCLED, NO CHANGE. FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED CHECKING FLAP SYSTEM, REMOVING PLUGS ON EACH ACTUATOR & GEAR BOX. WATER WAS FOUND PRESENT ON EACH GEARBOX 6259 CM & ACTUATOR ASSEMBLY #36271 CM, WATER DRAINED AND PLUGS REINSTALLED. 2L72 4F RTA28NM 19960829000471996082900047EA 1996 8 29 CA960103507 119951104A2750 FECU CNDAIR CNDAIRCL600 CL6002B19 EA FLAP FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 2388 (CAN)FLAPS FAIL MESSAGE AT 20 DEGREES. FECU RESET SYSTEM OKAY. 2L72 4F RTA21EA 19960829000481996082900048EU 1996 8 29 CA960103508 119951104A2750 WING TIP BRAKE AIRBUS320 A320211 3930320EU FLAPS REQ RESET W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)ON APPROACH FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION, FLAPS RECYCLED, NO CHANGE. FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED RESETTING WING TIP BRAKE ON S.F.C.C. #1 & #2. OPERATIONALCHECK CARRIED OUT. 2L72 4F RTA28NM 19960829000491996082900049EU 1996 8 29 CA960103509 119951105A2750 TORQUE LIMITERS AIRBUS320 A320211 3930320EU FLAP CONTROL TRIPPED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION. PERFORMED ECAM, NO CHANGE, FLAPS LOCKED AT ZERO. MAINTENANCE CHECK FOUND LEFT INBOARD FLAP INBOARD ACTUATOR & LEFT OUTBOARD FLAP OUTBOARD ACTUATOR TORQUE LIMITERS TRIPPED. FLAP TORQUE LIMITERS RESET AND FLAPS OPERATIONALLY CHECKED. SLAT FLAP CONTROL COMPUTER (S.F.C.C.) #1 & #2 TEST CARRIED OUT. 2L72 4F RTA28NM 19960829000501996082900050EA 1996 8 29 CA960103510 119951105A2752852D1007 ACTUATOR CNDAIR CNDAIRCL600 CL6002B19 EA GE LH INB FLAP FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 2388 (CAN)FLAPS FAIL MESSAGE AT '0' DEGREES. FLAPLESS LANDING CARRIED OUT. LEFT INBOARD FLAP, INBOARD ACTUATOR REPLACED. 2L72 4F RTA21EA 19960829000511996082900051EA 1996 8 29 CA960103511 119951105A2750 FLAPS CNDAIR CNDAIRCL600 CL6002B19 EA FECU SYS FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 1300 (CAN)FLAPS FAIL MESSAGE ON WHEN SELECTING FLAPS ON APPROACH. FECU SYSTEM TESTED. SB 601R-27-052 INCORPORATED. 2L72 4F RTA21EA 19960829000521996082900052EU 1996 8 29 CA960103512 119951108A2750780A000001 SENSOR AIRBUS320 A320211 3930320EU FLAP INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)ECAM MESSAGE, "FLAPS LOCKED", FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED REPLACING FLAP SELECTOR SENSOR AND RIGHT INBOARD FLAP ACTUATOR P/N 791A000003. FLAP SYSTEM FUNCTIONALLY CHECKED. 2L72 4F RTA28NM 19960829000531996082900053EA 1996 8 29 CA960103513 119951108A2750865D1007 MOTOR CNDAIR CNDAIRCL600 CL6002B19 EA GE FLAP MOTOR FAILED W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 2414 (CAN)FLAP FAIL MESSAGE AT 'O' DEGREES INDICATED ON ADI. FLAPLESS LANDING CARRIED OUT. FLAP MOTOR REPLACED. 2L72 4F RTA21EA 19960829000541996082900054EA 1996 8 29 CA960103514 119951111A5610601R330332 WINDSHIELD CNDAIRCL600 CL6002B19 EA FIRST OFFICER SHATTERED W O OTHER O OTHER CRCRUISE 1 CA 138 (CAN)FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT. 2L72 4F RTA21EA 19960829000551996082900055EA 1996 8 29 CA960103515 119951111A2750855D1007 BPSU CNDAIR CNDAIRCL600 CL6002B19 EA FLAP FAILED W O OTHER F FLT CONT AFFECTED CRCRUISE 1 CA 1339 (CAN)FLAPS FAIL MESSAGE ON AT FL330 IN CRUISE. FLAPLESS LANDING CARRIED OUT. NEW BRAKE POSITION SENSING UNIT INSTALLED. 2L72 4F RTA21EA 19960829000561996082900056EA 1996 8 29 CA960103516 119951113A2750855D1005 BPSU CNDAIR CNDAIRCL600 CL6002B19 EA RIGHT FLAP FAULTY W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA 218 (CAN)FLAP FAIL MESSAGE ON APPROACH. FLAPLESS LANDING CARRIED OUT. CHANGED RIGHT BRAKE POSITION SENSING UNIT (BPSU), AND SYSTEM RIGGED. 2L72 4F RTA21EA 19960829000571996082900057EA 1996 8 29 CA960103517 119951113A2750 HARNESS CNDAIR CNDAIRCL600 CL6002B19 EA LEFT BPSU SHORTING W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA 991 (CAN)FLAPS FAILED TO RETRACT FROM 20 DEGREES AT TAKEOFF. FOUND LEFT BRAKE POSITION SENSING UNIT (BPSU) ELECTRICAL HARNESS ISOLATION BROKEN AND SHORTING. BPSU HARNESS REPLACED. 2L72 4F RTA21EA 19960829000581996082900058NE 1996 8 29 CA960103518 219951115A7250 LP TURBINE AIRBUS320 A320211 3930320EU GE CFM56 CFM565A 13802NE ENGINE NR 2 DAMAGED W EF ENGINE SHUTDOWN ACTIVATE FIRE EXT. JR WARNING INDICATION PARTIAL RPM/PWR LOSS CLCLIMB 1 CA 145528456 (CAN)WHILE CLIMBING THROUGH FL280 AFTER TAKEOFF, THE #2 ENGINE HAD AN IMMEDIATE POWER LOSS ACCOMPANIED BY A LOUD BANG AND HIGH EXHAUST GAS TEMPERATURE. THE CREW SHUT DOWN THE ENGINE AND THE #2 ENGINE FIRE BUTTON WAS PUSHED. INITIAL MAINTENANCE INVESTIGATION FOUND INTERNAL ENGINE DAMAGE AND THE LOW PRESSURE TURBINE CASE WAS WORN THROUGH. 2L72 4F4 FRTA28NM E29NE 19960829000591996082900059WP 1996 8 29 CA960103519 119951115A2530CA167072 RECEPTACLE DOUG DC9 DC932 3022066WP GALLEY OVEN BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN)PRIOR TO DEPARTURE, BURNING SMELL DETECTED IN GALLEY AREA. CHECK OF AREA FOUND #18 OVEN RECEPTACLE BURNT. RECEPTACLE REPLACED. 2L72 4F A6WE 19960829000601996082900060EU 1996 8 29 CA960103520 119951115A2750 WING TIP BRAKE AIRBUS320 A320211 3930320EU FLAPS INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLAPS FAULT INDICATION FLIGHT CONTROL PAGE, FLAPS LOCKED DURING APPROACH. THE S.F.C.C. #1 & #2 RESET, WING TIP BRAKE RESET. FLAPS OPERATED SEVERAL TIMES. 2L72 4F RTA28NM 19960829000611996082900061WP 1996 8 29 CA960103521 119951121A3320 ELECT SOCKET DOUG DC9 DC932 3022066WP LIGHTING SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 CA (CAN)STRONG ELECTRICAL BURNING ODOR DETECTED IN CABIN. INVESTIGATION REVEALED FLOURESCENT LIGHT SOCKET AT 1AB SIDEWALL HAD SHORTED. DEFECTIVE SOCKET REPLACED. 2L72 4F A6WE 19960829000621996082900062EU 1996 8 29 CA960103522 119951122A2750 WING TIP BRAKE AIRBUS320 A320211 3930320EU FLAPS INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLAPS LOCKED ON APPROACH. FLAP WING TIP BRAKE RESET. 2L72 4F RTA28NM 19960829000631996082900063EU 1996 8 29 CA960103524 119951123A2752793A000003 ACTUATOR AIRBUS320 A320211 3930320EU FLAP INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)ON APPROACH, E.C.A.M. MESSAGE FLAPS FAIL. AIRCRAFT LANDED FLAPLESS. FLAP ACTUATORS 6271 CM AND 6259 CM CHANGED. FLAPS FUNCTIONALLY CHECKED. 2L72 4F RTA28NM 19960829000641996082900064WP 1996 8 29 CA960103525 119951123A5240 ACCESS PANEL DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE RT ENG CSD MISSING W K NONE O OTHER ININSP/MAINT 1 CA P657409D (CAN)DURING WALK AROUND, RIGHT ENGINE CSD SERVICE DOOR WAS FOUND MISSING. NEW DOOR INSTALLED. 2L72 4F4 F A6WE E2EA 19960829000651996082900065WP 1996 8 29 CA960103526 119951123A5240 SERVICE DOOR DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE NR 2 ENG OIL MISSING W K NONE O OTHER ININSP/MAINT 1 CA P657386D (CAN)ON WALK AROUND, FOUND #2 ENGINE OIL SERVICING DOOR MISSING. NEW DOOR FITTED. 2L72 4F4 F A6WE E2EA 19960829000661996082900066EU 1996 8 29 CA960103527 119951124A5610STA320241 WINDSHIELD AIRBUS320 A320211 3930320EU 1ST OFFICER SHATTERED W O OTHER O OTHER CRCRUISE 1 CA (CAN)DURING CRUISE, 1ST OFFICERS WINDSHIELD SHATTERED. NEW WINDSHIELD INSTALLED. 2L72 4F RTA28NM 19960829000671996082900067WP 1996 8 29 CA960103528 119951126A5240 ACCESS PANEL DOUG DC9 DC932 3022066WP RIGHT WING TIP MISSING W K NONE O OTHER ININSP/MAINT 1 CA (CAN)DURING WALK AROUND, FOUND THE RIGHT WING TIP NAVIGATION LIGHT ACCESS PANEL MISSING. NEW PANEL FITTED. 2L72 4F A6WE 19960829000681996082900068NM 1996 8 29 CA960103529 119951126A2121 FAN BOEING747 747433 NM CABIN AIR BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN)DURING DEPARTURE, BURNING SMELLL IN AFT CABIN. REPLACED AIR CIRCULATION FAN. 2L74 4F RTA20WE 19960829000691996082900069EA 1996 8 29 CA960103530 119951128A324632100011 WHEEL ASSEMBLY CNDAIRCL600 CL6002B19 EA NOSE WHEEL FAILED W O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA 2157 (CAN)AFTER LANDING GEAR RETRACTION CONTINUOUS THUMPING HEARD AND FELT UNDER THE COCKPIT FLOOR. THUMPING OCCURRED ON ONE SECOND INTERVALS AND CONTINUED UNTIL LANDING GEAR SELECTED DOWN NINE MINUTES LATER. BOTH NOSE WHEEL ASSEMBLIES CHANGED. 2L72 4F RTA21EA 19960829000701996082900070SO 1996 8 29 CA960103531 119951127A5743 TRUSS BRACKET PIPER PA28 PA28R200 7102811SO WHEEL WELL CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9162 (CAN)WHILE INSPECTING THE MAIN GEAR TRUSS BRACKET, REMOVED THE BRACKET ON THE LEFT HAND SIDE AND FOUND THE ANGLE BEHIND THE BRACKET WAS CRACKED. ANGLE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE. 1L71 3O 2A13 19960829000751996082900075EU 1996 8 29 CA960109002 219951223A7322995736R CARBURETOR DIAMONDA20A1DA20A1 05626UXGL ROTAX 912 ROTAX912 55555EU ENG FAULTY W CD ABORTED TAKEOFF RETURN TO BLOCK ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS TOTAKEOFF 1 CA 698 4076240 (CAN)DURING TAKEOFF ROLL THE AIRCRAFT EXPERIENCED A 300 RPM POWER LOSS ALONG WITH ENGINE VIBRATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE RAMP. NO FAULT WAS FOUND ON INSPECTION OR GROUND RUNUP. FAULT WAS THOUGHT TO BE DUE TO CARBURETOR ICING DUE TO LONG DELAY PRIOR TO TAKEOFF, SO AIRCRAFT WAS RELEASED FOR SERVICE. AFTER TWO FLIGHTS THE SYMPTOMS RETURNED AND THIS TIME THE FAULT COULD BE DUPLICATED ON GROUND. THE CARBURETOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1L71 3O3 INTTA4CH EXPE3I 19960829000771996082900077CE 1996 8 29 CA960109004 119951229A32222342003 O-RING LEAR 35 35LEAR 5170600CE NLG OLEO PINCHED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 321 321 (CAN)OLEO WOULD LOSE AIR AND WOULD FAIL TO EXTEND, NOT LOCKING UP. HYDRAULIC FLUID FOUND IN NOSE WHEEL STEERING GEARBOX. 'O' RING FOR OLEO METERING VALVE FOUND PINCHED. 'O' RING REPLACED AND TESTED SERVICE ABLE. 2L72 4F A10CE 19960829000811996082900081CE 1996 8 29 CA960110001 119951203A56101013840257 WINDOW BEECH 1013840257 BEECH 200 200BEECH 1152920CE LEFT WINDOW CRACKED W GI O2 MASK DEPLOYED CABIN DEPRESSURIZATION O OTHER CLCLIMB 1 CA 5845 (CAN)ON CLIMB OUT A LOUD BANG WAS HEARD AND EASILY DISCOVERED AS THE FRONT WINDOW ON THE PILOTS SIDE WHICH HAD CRACKED APPROXIMATELY 90 PERCENT ACROSS. PRIOR TO THIS OCCURRENCE THE AIRCRAFT HAD FLOWN THROUGH HEAVY RIME ICING CONDITIONS, DURING WHICH HIGH HEAT HAD BEEN APPLIED TO MELT THE ICE. THE WINDOW WAS ALSO NOTED TO HAVE DELAMINATED TO CERTAIN PORTIONS AROUND THE EDGES. PRESSURIZATION WAS REDUCED TO 4 PSI AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DESTINATION. 1L72 4T A24CE 19960829000821996082900082CE 1996 8 29 CA960110002 119951222A2752C1450046 TRANSMISSION CESSNA 99105861 CESSNA208 208 2073702CE STDBY FLAP MOTORSHEARED DRIVE W K NONE O OTHER ININSP/MAINT 1 CA 2415 (CAN)DURING INSPECTION THE STANDBY FLAP MOTOR SYSTEM WAS TESTED IN ACCORDANCE WITH THE ENGINE NOT RUNNING CHECK. IT WAS NOTED THAT THE STANDBY FLAP MOTOR WAS HEARD TO BE RUNNING BUT THE FLAPS WERE NOT MOVI NG. THE FLAP MOTOR AND TRANSMISSION ASSEMBLY WERE REMOVED AND THE TRANSMISSION DRIVE SHAFT ASSEMBLY WAS FOUND TO BE SHEARED. SUBMITTER STATES THAT THE FLAP SYSTEM TESTED OK IN THE NORMAL TEST MODE. 1H71 3T NTA37CE 19960829000861996082900086SO 1996 8 29 CA960110007 119951130A32133182402 AXLE YOKE PIPER PIPER PA23 PA23250 7102308SO L/H & R/H GEAR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 7023 (CAN)CRACKS FOUND RUNNING PERPENDICULAR ON THE YOKE ASSEMBLY STARTING FROM THE LIGHTENING HOLE. L/H GEAR CRACK WAS VISIBLE WHILE THE R/H GEAR REQUIRED THE USE OF DYE PENETRANT. 1L72 3O 1A10 19960829000871996082900087EA 1996 8 29 CA960110008 119951221A2710MS245664B PULLEY DHAV DHAV DHC6 DHC6300 EA R/H AILERON SEIZED W K NONE F FLT CONT AFFECTED ININSP/MAINT 1 CA 12146 (CAN)AILERON PULLEY IN RIGHT HAND WING AT STA. 247.5 FOUND WITH BEARING SEIZED TO STUD AND SEVERAL BALLS MISSING. CABLE WAS WEARING INTO ONE SIDE OF GROOVE FLANGE. 1H72 3T A9EA 19960829000881996082900088EA 1996 8 29 CA960110009 119951221A2730C6TE1059S103 TORQUE TUBE DHAV C6TE10007 DHAV DHC6 DHC6300 EA ELEVATOR GOUGED W K NONE F FLT CONT AFFECTED ININSP/MAINT 1 CA 12146 258L18 (CAN)ELEVATOR PUSHROD ATTACH POINTS ON RIGHT HAND ELEVATOR TORQUE TUBE DAMAGED BEYOND SRM LIMITS. TORQUE TUBE REPLACED. 1H72 3T A9EA 19960829000891996082900089NE 1996 8 29 CA960110201 219951207A8530 VALVE SEAT DOUG DC4 C54A 3021512WP PWA R2000 R20007M2 52023NE NR 8 CYLINDER LOOSE W E ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 200 BP701714 (CAN)IN CRUISE FLIGHT #4 ENGINE BEGAN TO RUN ROUGH ACCOMPANIED BY BACKFIRING THROUGH THE INDUCTION SYSTEM. THE ENGINE WAS SHUTDOWN. POST FLIGHT INSPECTION DISCLOSED THE #8 CYLINDER INTAKE VALVE SEAT HAD CA ME ADRIFT, PREVENTING THE INTAKE VALVE FROM CLOSING. 2L74 4R4 R A762 5E5 19960829000901996082900090WP 1996 8 29 CA960110501 119950921A793042D1091 SWITCH DOUG DC9 DC932 3022066WP PWA JT8 JT8D7A 52053NE ENG OIL INOPERATIVE W E ENGINE SHUTDOWN J WARNING INDICATION CLCLIMB 1 CA P657715D (CAN)DURING CLIMB, RIGHT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON. RIGHT ENGINE SHUTDOWN. MAINTENANCE CHECK FOUND 13TH STAGE AIR ANTI-ICE DUCT UNDONE AT ENGINE LOW OIL PRESSURE AND OIL FILTER DIFFERENTIA L PRESSURE SWITCHES. THE 13TH STAGE AIR CAUSED DAMAGE TO BOTH SWITCHES. MAINTENANCE ACTION INVOLVED REPLACING BOTH SWITCHES AND OIL FILTER. AIRCRAFT GROUND RUN. 2L72 4F4 F A6WE E2EA 19960829000911996082900091EU 1996 8 29 CA960110502 119951207A5210 DOOR AIRBUS320 A320211 3930320EU RT PAX FROZEN CLOSED W K NONE O OTHER TXTAXI/GRND HDL 1 CA (CAN)ON ARRIVAL FOUND R1 DOOR FROZEN. UNABLE TO OPEN. OAT -27 DEGREES. DOOR THAWED USING HEATER. 2L72 4F RTA28NM 19960829000921996082900092EU 1996 8 29 CA960110503 119951207A5210 DOOR AIRBUS320 A320211 3930320EU CABIN L2 FROZEN W K NONE O OTHER TXTAXI/GRND HDL 1 CA (CAN)AFTER LANDING, FOUND L2 DOOR & EMERGENCY SLIDE MECHANISM FROZEN. DOOR THAWED USING HEATER FOLLOWED BY LUBRICATION. 2L72 4F RTA28NM 19960829000931996082900093EU 1996 8 29 CA960110504 119951208A2121767A000004 FAN AIRBUS320 A320211 3930320EU EQUIP COOLING FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 CA (CAN)A LOUD SCREECHING SOUND WAS HEARD ON DESCENT FOLLOWED BY ELECTRICAL BURNING ODOR AND SMOKE IN CABIN. MAINTENANCE CHECK FOUND AVIONICS COOLING FAN GRINDING & RIGHT PACK AIR CYCLE MACHINE COOLING BLADE S FAILED. AVIONICS COOLING FAN REPLACED, RIGHT PACK AIR CYCLE MACHINE P/N 757A0000-09 REPLACED AND GALLEY AREA INSPECTED FOR EVIDENCE OF OTHER ELECTRICAL FAULTS. 2L72 4F RTA28NM 19960829000941996082900094EA 1996 8 29 CA960110505 119951209A2170 COALESCER BAG CNDAIRCL600 CL6002B19 EA AIR COND PACK CONTAMINATED W AH UNSCHED LANDING DEACTIVATE SYST/CIRCUITS BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 CA 2811 (CAN)AFTER TAKEOFF COCKPIT FILLED WITH SMOKE. LEFT AIR CONDITIONING PACK SHUT DOWN WITH OVER PRESSURE EICAS MESSAGE. BOTH AIR CONDITIONING PACK COALESCER BAGS REMOVED AND FOUND CONTAMINATED WITH GLYCOL. 2L72 4F RTA21EA 19960829000951996082900095WP 1996 8 29 CA960110506 119951210A2530 OVEN DOUG DC9 DC932 3022066WP GALLEY ELECT FAULT W O OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 CA (CAN)AISLE TROLLEY (MEAL) POPPED CIRCUIT BREAKER & GAVE AN ELECTRICAL SHOCK TO FLIGHT ATTENDANT. MAINTENANCE ACTION INVOLVED CHECKING THREE PHASE POWER & GROUND RETURN, AIRCRAFT OVEN OUTLET. OVEN REPLACED. 2L72 4F A6WE 19960829000961996082900096EU 1996 8 29 CA960110507 119951211A5210 DOOR AIRBUS320 A320211 3930320EU CABIN FROZEN W K NONE O OTHER TXTAXI/GRND HDL 1 CA (CAN)ON ARRIVAL, FOUND DOOR & EMERGENCY ARMING LEVER MECHANISM FROZEN. O.A.T. -10 DEGREES. DOOR THAWED AND OPERATIONALLY CHECKED. 2L72 4F RTA28NM 19960829000971996082900097WP 1996 8 29 CA960110508 119951212A3222 STRUT DOUG DC9 DC932 3022066WP NLG REQ SERVICE W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN)UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK FOUND NOSE OLEO PRESSURE LOW. NOSE OLEO SERVICED WITH NITROGEN. 2L72 4F A6WE 19960829000981996082900098NM 1996 8 29 CA960110509 119951212A2710252T12001 ACTUATOR BOEING767 767233 NM AILERON FAILURE W O OTHER F FLT CONT AFFECTED CRCRUISE 1 CA (CAN)DURING FLIGHT - AILERON LOCKOUT - HARD FAULT. AILERON ACTUATOR CHANGED. 2L72 4F RTA1NM 19960829000991996082900099WP 1996 8 29 CA960110510 119951215A2150 AIR COND PACK DOUG DC9 DC932 3022066WP LEFT PACK CABIN SMOKE W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN)DURING PASSENGER DISEMBARKATION, SMOKE FUMES DETECTED IN CABIN WHILE APU RUNNING AND LEFT PACK ON. BOTH ENGINES GROUND RUN & BOTH PACKS OPERATED. SMOKE ONLY WAS EVIDENT WHEN LEFT PACK WAS OPERATED FROM APU. SUSPECT RESIDUE OF DE-ICEING FLUID INJECTED ACCIDENTLY. 2L72 4F A6WE 19960829001001996082900100EU 1996 8 29 CA960110511 119951220A2752791A000003 ACTUATOR AIRBUS320 A320211 3930320EU FLAP INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLIGHT CONTROL MESSAGE, FLAP SYSTEM 2 FAULT ON APPROACH, FLAP LOCKED, WING TIP BRAKE ON. R.M.A. 27-50-123 CARRIED OUT. MAINTENANCE INSTALLED NEW FLAP ACTUATOR AT #1 POSITION. 2L72 4F RTA28NM 19960829001011996082900101EA 1996 8 29 CA960110512 119951217A5610NP1393222 WINDSHIELD CNDAIRCL600 CL6002B19 EA CAPTAINS SHATTERED W O OTHER O OTHER CLCLIMB 1 CA 2867 (CAN)CAPTAINS WINDSHIELD SHATTERED AT 27,000 FEET. 2L72 4F RTA21EA 19960905002261996090500226EU 1996 9 5 CA960110513 119951220A5753 TAIL CONE AIRBUS320 A320211 3930320EU RT INB FLAP DAMAGED W K NONE F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN)AFTER ARRIVAL, THE RIGHT INBOARD FLAP TRACK TAIL CONE WAS FOUND DAMAGED. CONE REPAIRED AND FITTED. 2L72 4F RTA28NM 19960905002271996090500227WP 1996 9 5 CA960110514 119951220A3244 TIRE DOUG DC9 DC932 3022066WP NR 2 BLOWN W K NONE O OTHER LDLANDING 1 CA (CAN)#2 TIRE BLEW ON LANDING. MAINTENANCE CHECKED AIRCRAFT FOR DAMAGE. REPLACED #1 AND #3 MAIN WHEEL ASSEMBLIES. 2L72 4F A6WE 19960905002281996090500228EU 1996 9 5 CA960110515 119951220A5610STA320261 WINDSHIELD AIRBUS320 A320211 3930320EU 1ST OFFICER SHATTERED W A UNSCHED LANDING O OTHER UKUNKNOWN 1 CA (CAN)AIRCRAFT RETURNED TO AIRPORT DUE TO SHATTERING OF 1ST OFFICERS WINDSHIELD. #2 WINDSHIELD AND HEAT COMPUTER (P/N 6664287-0) CHANGED. 2L72 4F RTA28NM 19960905002291996090500229WP 1996 9 5 CA960110516 119951220A2750472085117 COMPARATOR LKHEED1011 10113851 5265010WP FLAP ASYMMETRY FAILURE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLAP/SLAT LOCK LIGHT ON DURING APPROACH WITH FLAPS LOCKED AT 10 DEGREES. RESET LH AND RH ASYMMETRY BRAKES. CHANGED FLAP ASYMMETRY COMPARATOR. 2L73 4F A23WE 19960905002301996090500230EU 1996 9 5 CA960110517 119951221A27504911709 COMPUTER AIRBUS320 A320211 3930320EU FLAP CONTROL INOPERATIVE W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN)FLIGHT CONTROL MESSAGE, FLAP SYSTEM 1 FAULT ON APPROACH THEN CLEARED ITSELF, APPEARED AGAIN ON FINAL, FLAPS WERE SLOW TO EXTEND. MAINTENANCE ACTION INVOLVED CHANGING S.F.C.C. (SLAT/FLAP CONTROL COMPUTER. 2L72 4F RTA28NM 19960905002311996090500231NM 1996 9 5 CA960110518 119951225A2497 WIRE HARNESS BOEING747 747133 138448BNM POWER DIST BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 CA 63189 (CAN)ARCING SOUNDS AND SPARKS COMING FROM OVERHEAD PSU AT SEAT 4AB. WIRING HARNESS THAT RUNS PARALLEL WITH SIDEWALL LIGHT ASSEMBLY ABOVE 4AB BURNT THROUGH. REPAIRED. 2L74 4F A20WE 19960905002321996090500232EU 1996 9 5 CA960110519 119951227A4990 APU AIRBUS320 A320211 3930320EU INTAKE OIL LEAK W O OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 CA (CAN)ENROUTE ACRID SMELL DETECTED ALONG WITH LIGHT HAZE IN CABIN. SMOKE SMELL DIMINISHED AFTER 10 MINUTES. MAINTENANCE CHECK REVEALED LOW OIL LEVEL IN APU AND OIL SEEPING INTO INTAKE OF APU. THE APU WAS RE PLACED. 2L72 4F RTA28NM 19960905002331996090500233WP 1996 9 5 CA960110520 119951228A2170 WATER SEPARATOR DOUG DC9 DC932 3022066WP PWA CABIN PRESS LOOSE CLAMP W O OTHER J WARNING INDICATION CLCLIMB 1 CA (CAN)DURING CLIMB, CABIN PRESSURE FLOW LIGHT CAME "ON". CABIN PRESSURIZATION SYSTEM DID NOT MAINTAIN PRESSURE IN AUTO OR MANUAL MODE. MAINTENANCE CHECK FOUND RIGHT AIR CONDITIONING WATER SEPARATOR CLAMP LOOSE. CLAMP RETIGHTENED. 2L72 4F A6WE 19960905002341996090500234EU 1996 9 5 CA960110521 119951229A21502120001 FAN AIRBUS320 A320211 3930320EU COOLING EXTRACT SEIZED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA (CAN)DURING TAXIING, A BURNING SMELL WAS DETECTED AND A LOUD SOUND HEARD IN FLIGHT DECK. MAINTENANCE CHECK FOUND COOLING EXTRACT FAN SEIZED. FAN WAS REPLACED. 2L72 4F RTA28NM 19960905002351996090500235 1996 9 5 CA960110522 419951229A3460B398BAM0205 COMPUTER AIRBUS320 A320211 3930320EU FLT MGMT FAILED W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN)DURING DEPARTURE, AUTO FLIGHT SYSTEM TESTED, FAULTED BOTH FLIGHT MANAGEMENT GUIDANCE COMPUTERS. MAINTENANCE ACTION , #1 FLIGHT MANAGEMENT COMPUTER CHANGED. #2 FLIGHT MANAGEMENT COMPUTER TESTED FOR FUL L 7 MINUTES, CHECKED SERVICEABLE. 2L72 4F RTA28NM 19960905002361996090500236EU 1996 9 5 CA960110523 119951220A5210 DOOR MECHANISM AIRBUS320 A320211 3930320EU SERVICE DR FWD FROZEN W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN)ON ARRIVAL, FOUND FORWARD SERVICE DOOR OPENING MECHANISM FROZEN. MAINTENANCE REMOVED DOOR LINNING, HEAT APPLIED TO DISARM CABLE, CABLE THAWED, MECHANISM LUBRICATED. DOOR OPERATIONALLY CHECKED SERVICEA BLE. 2L72 4F RTA28NM 19960905002481996090500248NM 1996 9 5 CA960111019 119951231A3222883003 PISTON CAP ROTOL 8800121 DHAV DHC8 DHC8102 2809003NM NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 22661 DCL10787 (CAN)ON NOSE LANDING GEAR, THE FLANGE ON PISTON CAP ON LINK COMPLETELY DETACHED FROM PISTON. 2H72 4T RTA13NM 19960905002511996090500251EA 1996 9 5 CA960115001 219951122A7210310063901 BEARING PWA BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA COMBINING GRBOX SPALLED W K NONE O OTHER NRNOT REPORTED 1 CA 1841 CPGB1121 61927 (CAN)"C" BOX WAS GENERATING METAL ON THE #2 SIDE. UPON DISASSEMBLY OF THE GEARBOX IT WAS NOTED THAT THE #5 INNER BEARING HAD ONE OF THE BALLS STARTING TO SPALL. 1G71 4U4 U H4SW E22EA 19960905002631996090500263EA 1996 9 5 CA960115013 219950707A72403024767 DIFFUSER PIPES PWA 3027037 BEECH 100 A100 1152915CE PWA PT6 PT6A28 EA GAS GEN CASE LOOSE IN CASE W K NONE O OTHER ININSP/MAINT 1 CA 1503 PCE50246 (CAN)DURING FIRST HOT SECTION INSPECTION AFTER OVERHAUL THREE (3) DIFFUSER PIPES WERE FOUND LOOSE DUE TO DEFECTIVE WELDS. ENGINE RETURNED FOR REPAIR. 1L72 3T4 T A14CE E4EA 19960905002641996090500264NM 1996 9 5 CA960115014 119951221A323310500103 ACTUATOR ROTOL DHAV DHC8 DHC8102 2809003NM RT MLG LEAKING W HO DEACTIVATE SYST/CIRCUITSOTHER K FLUID LOSS APAPPROACH 1 CA 12916 (CAN)DURING LANDING GEAR EXTENSION, #2 HYDRAULIC QUANTITY WENT TO ZERO. ALTERNATE GEAR EXTENSION CARRIED OUT. RH MAIN LANDING GEAR RETRACTION ACTUATOR FOUND LEAKING. 2H72 4T RTA13NM 19960905002741996090500274CE 1996 9 5 CA960115201 119951229A2810S21061 FUEL DRAINS CESSNA206 U206G 2073356CE RT WING CORRODED STEM W K NONE O OTHER ININSP/MAINT 1 CA 999 (CAN)WHILE COMPLYING WITH CAP 28-30-01 THE FUEL DRAINS ON THE RIGHT HAND WING AND BOTH RESERVE TANKS WERE FOUND TO BE BADLY CORRODED AND THE INTERNAL SPRINGS WERE STICKING. THE FUEL DRAINS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3O A4CE 19960905002821996090500282GL 1996 9 5 CA960116010 219951120A732223034702 FCU HUGHES369 369HS 4470728WP ALLSN 250C 250C20 03013GL ENGINE FAILURE W K NONE O OTHER ININSP/MAINT 1 CA 2356 (CAN)START LAG AT AROUND 28 PERCENT N1 UP TO 38 PERCENT. THEN START RESUMED FOR SECOND PEAK. WOULD NEED HIGH CHARGE BATTERY FOR START-UP. FIRST PEAK 720 DEGREES, THEN WENT BACK DOWN TO 550 DEGREES THROUGH 28 PERCENT N1 TO 38 PERCENT N1. SECOND PEAK AT 38 PERCENT N1 780 DEGREES. 1G71 3U3 U H3WE E4CE 19960905002831996090500283NM 1996 9 5 CA960116011 119951230A783065378518 ACTUATOR BOEING727 727212 138407GNM T/R NR 2 ENG FAILED W CD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TOTAKEOFF 1 CA (CAN)#2 ENGINE THRUST REVERSER LIGHT ILLUMINATED DURING TAKEOFF ROLL. ABLE TO SELECT THRUST REVERSER REGARDLESS OF THRUST LEVER POSITION. REJECTED TAKEOFF BELOW 80 KNOTS. REVERSER LOCKED IN FORWARD THRUST AND DEACTIVATED AS PER MM 78-30-00. LOCKED THRUST REVERSER REPLACED AND TESTED AS PER MM. 2L73 4F A3WE 19960905002851996090500285NM 1996 9 5 CA960118101 119951221A2424915F2125 CONTROL UNIT WESTINGHOUSE915F2125 BOEING737 737275 1384485NM NR 1 BUS INTERMITTENT W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CLCLIMB 1 CA 3075413407 NB26633F (CAN)AFTER TAKEOFF #1 BUS LOST. AIRCRAFT RETURNED TO BLOCKS. BUS PROTECTION PANEL AND GENERATOR CONTROL UNIT REPLACED. 2L72 4F A16WE 19960905002861996090500286NM 1996 9 5 CA960119101 119951228A53306545771 SKIN DOUBLER BOEING737 737217 1384464NM FS 663 CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4834248342 (CAN)FUSELAGE INNER BONDED DOUBLER CRACKED AT BBL 70.85 RH STA. 663. CRACK IS AT THE LOWER AFT FASTENER HOLE. CRACK POSITION 12 O'CLOCK, GOING UPWARDS. REPAIRED AS PER SRM. 2L72 4F A16WE 19960905002921996090500292CE 1996 9 5 CA960122006 119951229A5511123260024 STAB RIB 123260024 CESSNA207 207A 2073604CE MCAULYD3A34 D3A34C404 GL HORIZ STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 805499 (CAN) UPON INVESTIGATION VARIOUS RIBS WERE FOUND CRACKED INSIDE THE HORIZONTAL STABILZER. 0732611-4, 0732611-3, 0732611-2 AND 1232624-1. PARTS REPLACED WITH FACTORY NEW. 1H71 3O A16CE 5 CP47GL 19960905003001996090500300NE 1996 9 5 CA960122015 219950717A7260107006204 SPUR GEAR LYC BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE ACCY DRIVE BROKEN W O OTHER O OTHER NRNOT REPORTED 1 CA LE07672 (CAN)SPUR GEAR BROKEN IN TWO PIECES. 1G71 4U4 U H1SW E17EA 19960905003031996090500303CE 1996 9 5 CA960122020 119951122A7712 CONNECTOR LEAR 35 35LEAR 5170600CE GARRTT P2 SENSOR CONTAMINATED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA (CAN)ON CLIMB, R/H ENGINE HAD ENGINE PARAMETERS FLUCTUATE FOR A FEW SECONDS. MAINTENANCE CLEANED P2 SENSOR CONNECTOR. ENGINE GROUND RUN, NO FURTHER FAULT REPORTED. 2L72 4F A10CE 19960905003081996090500308NE 1996 9 5 CA960123002 119951229A2420 WIRE SKRSKYS76 S76A 8143006NE STA 215 CHAFED W O OTHER J WARNING INDICATION CRCRUISE 1 CA 17394 (CAN)AC GENERATOR WOULD FALL OFF LINE WITHOUT PATTERN OR CONSISTENCY. A, B & C PHASE WIRING FROM AC GENERATOR P702 TO AC GENERATOR CONTACTOR K1 WAS REPLACED. UPON REMOVAL A SMALL CHAFED AREA WAS FOUND ON THE PHASE B WIRING. THE CHAFING OCCURRED AT STATION 215 WL112. 1G72 3U H1NE 19960905003121996090500312EU 1996 9 5 CA960123006 119951128A2910 VALVE FOKKERF28 F28MK1000 4990808EU NR 1 HYD SYS LEAKING W AD UNSCHED LANDING RETURN TO BLOCK K FLUID LOSS CLCLIMB 1 CA (CAN)ON CLIMB #1 SYSTEM HYDRAULIC FLUID QUANTITY INDICATED LOSS OF FLUID. AIRCRAFT RETURNED TO BLOCKS. ALTERNATE GEAR LOWERING USED. EMERGENCY SERVICES CALLED OUT. LEAK CAUSED BY CHECK VALVE NOT SEATED PRO PERLY ON REFILL PANEL. 2L72 4F RTA20EU 19960905003131996090500313EA 1996 9 5 CA960123007 119951229A56105C004307803 WINDSHIELD PPG DHAV DHC8 DHC8311 1386006EA PILOTS SHATTERED W K NONE O OTHER CRCRUISE 1 CA (CAN)AT 21,000 FEET, OUTER PANE OF PILOT'S WINDSHIELD SHATTERED. (POSSIBLE BIRD STRIKE). 2H72 4T RTA13NM 19960905003141996090500314EU 1996 9 5 CA960123008 119951130A2721109901 TRIM CABLE FOKKERF28 F28MK1000 4990808EU RUDDER BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 CA (CAN)AFTER TAKEOFF WHEN TRIMMING AIRCRAFT THE CREW HAD NO RUDDER TRIM IN EITHER DIRECTION. AIRCRAFT RETURNED TO BLOCKS. FEEL TRIM BUNGEE CABLE BROKEN. REPLACED. 2L72 4F RTA20EU 19960905003151996090500315NM 1996 9 5 CA960123009 119951028A7602 TRANSMITTER ARM DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE CONDITION LEVER BROKEN W CD ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 CA PCE120256 (CAN)ON TAKEOFF ROLL TAKEOFF WARNING HORN SOUNDED AT 30-40 KTS. TAKEOFF REJECTED. MAINTENANCE FOUND #2 CONDITION LEVER MICROSWITCH TRANSMITTER ARM BROKEN. 2H72 4T4 TRTA13NM E20NE 19960905003361996090500336NE 1996 9 5 96ZZZX4258 219951208A7250430124202 BEARING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 3 DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11428MB497 3523 7088 LE45155E BEARING DEFECTIVE. REMOVED TO FACILITATE OTHER MAINTENANCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003371996090500337NE 1996 9 5 96ZZZX4259 219951208A7260430101501 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ACC DRIVE LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 7088 LE45155E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003381996090500338NE 1996 9 5 96ZZZX4260 219951208A7260430101501 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ACC DRIVE LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 7088 LE45155E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003391996090500339NE 1996 9 5 96ZZZX4261 219951208A7260430101301 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ACC DRIVE LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 7088 LE45155E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003401996090500340NE 1996 9 5 96ZZZX4262 219951208A7260430101201 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ACC DRIVE LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 7088 LE45155E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003411996090500341NE 1996 9 5 96ZZZX4263 219951208A7250411100720 SHROUD BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE GAS PROD BLADE TIP RUB A R7MAK NONE O OTHER ININSP/MAINT 1 NM11428MB387 7088 LE45155E EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW SHROUD UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003421996090500342NE 1996 9 5 96ZZZX4264 219951208A7250410106701 SEAL RING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE 1ST TURB SHROUD WORN A R7MAK NONE O OTHER ININSP/MAINT 1 NM11428MB387 7088 LE45155E SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003431996090500343NE 1996 9 5 96ZZZX4265 219951208A7250430144801 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 3 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 RE8I940629 7088 LE45155E NR 3 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003441996090500344NE 1996 9 5 96ZZZX4266 219951208A7230430135703 SEAL BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE NR 2 BEARING LEAKING A R7MAK NONE K FLUID LOSS ININSP/MAINT 1 NM11428MB387 039 7088 LE45155E NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960905003491996090500349NE 1996 9 5 96ZZZX4271 219951208A7250430136201 BEARING BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE DEFECTIVE A R7MAK NONE O OTHER ININSP/MAINT 1 NM11428MB497 42392 7088 LE45155E BEARING DEFECTIVE. REMOVED TO FACILITATE OTHER MAINTENANCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 U H13EU E5NE 19960912002731996091200273CE 1996 9 12 96ZZZM1300 119950714A5751MS276434 BEARINGS BEECH 1900 1900D 1154162CE AILERONS WORN A JJBAK NONE O OTHER ININSP/MAINT 1 EA01830CA5391 UE19 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M) 2L72 4T RTA24CE 19960912002771996091200277CE 1996 9 12 96ZZZM1304 119951129A5751MS276434 BEARINGS BEECH 1900 1900D 1154162CE AILERONS WORN A JJBAK NONE O OTHER ININSP/MAINT 1 EA01836CA5863 UE32 DURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WERE FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M) 2L72 4T RTA24CE 19960912003331996091200333WP 1996 9 12 ASAA9680164 119950215A5320 THRESHOLD DOUG DC9 DC982 3022082WP CARGO COMPT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01932AS 49233 PAE - DURING 30K CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1217, LONGERON 29. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01330. (M) 2L72 4F A6WE 19960912003341996091200334WP 1996 9 12 ASAA9680165 119950316A5330 SKIN DOUG DC9 DC983 3022083WP BS 1155-1174 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01942AS 53052 PAE - DURING 15K CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AROUND THE CUTOUT FOR THE NR 3 VHF ANTENNA AT Y1155 TO Y1174, LONGERON 29L AND 30. CORROSION REMOVAL REQUIRED ENLARGING THE EXISTING CUTOUT BY APPROXIMATELY .125 INCH AT EACH EDGE. AN AREA AROUND THE OPENING OF APPROXIMATELY 4 INCHES BY 4 INCHES WAS BLENDED TO A DEPTH OF .017 INCH. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5330-01177. (M) 2L72 4F RTA6WE 19960912003351996091200335WP 1996 9 12 ASAA9680166 119951105A5320 ANGLE DOUG DC9 DC982 3022082WP BS 168.75 CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS 49111 PAE - DURING 15K CHECK, A CRACK WAS FOUND ON THE FUSELAGE CUSP ANGLE AT Y168.75. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01387. (M) 2L72 4F A6WE 19960912003361996091200336WP 1996 9 12 ASAA9680167 119951106A5320 THRESHOLD DOUG DC9 DC982 3022082WP CARGO COMPT CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM01951AS 49111 PAE - DURING 15K CHECK, FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1155, LONGERON 29R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01383. (M) 2L72 4F A6WE 19960912008391996091200839CE 1996 9 12 CA951218017 119951211A574007236006 WING STRUT CESSNA150 152 2071835CE L/H STRUT UPPER LOOSE RIVET W K NONE O OTHER ININSP/MAINT 1 CA 3123 (CAN)DURING INSPECTION UPWARD PRESSURE WAS APPLIED TO THE WING AND A LOUD CRACKING NOISE WAS HEARD. THE SOURCE WAS TRACED TO THE UPPER WING STRUT ATTACH RIVETS WHICH HAD BECOME LOOSE. SUBMITTER REBUCKED TH E RIVETS AND RETURNED THE AIRCRAFT TO SERVICE. 1H71 3O NT3A19 19960912008431996091200843SO 1996 9 12 CA960123017 119951017A2820 FUEL HOSE PIPER PA31 PA31350 7103110SO FUEL SYS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN)NO TEXT. 1L72 3O A20SO 19960912008471996091200847EU 1996 9 12 CA960123024 119951202A2121 BLOWER BRAERO748 HS7482A 4231001EU VENT INOPERATIVE W F ACTIVATE FIRE EXT. J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN)DURING START CYCLE THE FIRE WARNING INDICATION CAME ON. VENT BLOWER INOPERATIVE. BLOWER AND TEMPERATURE PROBES REPLACED. 2L72 3T A24EU 19960912008481996091200848NM 1996 9 12 CA960123025 119951216A243010138A16NA1 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE LT TRU BURNED W K NONE O OTHER NRNOT REPORTED 1 CA 15585 PCE120851 (CAN)PILOT REPORTED TRU CIRCUIT BREAKER HAD POPPED. INSPECTION FOUND THAT CABLE 10138A-16NA-1 OF PIN 'D' ON CONNECTOR 2431P19 (LEFT TRU) TO GROUND GS 13 HAD BURNT ALONG ITS FULL LENGTH REF. WIRING DIAGRAM 24-31-00 (DC GENERATION). 2H72 4T4 TRTA13NM E20NE 19960912008491996091200849NM 1996 9 12 CA960123026 119951222A3040WB1050 BUSHING 83040013102 DHAV DHC8 DHC8102 2809003NM WIPER MOTOR WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN)BUSHING AND WASHER RUB DIRECTLY ON METAL AND WEAR WIPER MOTOR MOUNTING PLATE 2H72 4T RTA13NM 19960912008511996091200851SW 1996 9 12 CA960123028 119951227A7110212060822001 DOOR ASSEMBLY BELL 212060803135BELL 212 212 1181420SW COWL BENT W E ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 CA (CAN)RETENTION SPRING BROKE ON DOOR ASSEMBLY P/N 212-060-803-135 ALLOWING IT TO FLAP AND BREAK OFF, DROPPING DOWN ON THE INPUT SHAFT. IT THEN BOUNCED FORWARD LODGING UNDER THE #2 ENGINE THROTTLE ARM LIMITI NG IT'S TRAVEL. 1G71 4U H4SW 19960912008531996091200853NE 1996 9 12 CA960123101 219951213A7260 DRIVE ALLIED SIGNA103040001 BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE ACCESSORY GEARBXFAILED W G O2 MASK DEPLOYED Y ENGINE STOPPAGE CRCRUISE 1 CA LEO7683 (CAN)ENGINE HAD CATASTROPHIC FAILURE, AIRCRAFT DESTROYED. ACCIDENT HAPPENED IN AUSTRALIA AND IS BEING INVESTIGATED BY BUREAU OF AIR SAFETY INVESTIGATION, FILE #9504205. PRELIMINARY OBSERVATIONS INDICATE FA ILURE OF N2 GEARBOX DRIVE. 1G71 4U4 U H1SW E17EA 19960919005251996091900525SW 1996 9 19 CA960126007 119951206A6320206040002025 TRANSMISSION BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL M/R MAKING METAL W K NONE O OTHER ININSP/MAINT 1 CA 140552907 CAE820651 (CAN)TRANSMISSION REMOVED DUE TO MAKING METAL. TIME THIS INSTALLATION 120.8 HOURS. 1G71 3U3 U H2SW E4CE 19960919005261996091900526GL 1996 9 19 CA960126008 219950805A732223034702 FCU BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL ENGINE FAILURE W E ENGINE SHUTDOWN X ENGINE FLAMEOUT LDLANDING 1 CA 242 801246BA (CAN)ENGINE FLAMED OUT WHEN THROTTLE WAS ROLLED BACK TO IDLE AFTER LANDING. DURING THE TWO PREVIOUS DAYS LEADING TO THE INCIDENT, THE IDLE HAD TO BE ADJUSTED THREE TIMES AND WOULD NOT STABILIZE. FCU REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 19960919005271996091900527WP 1996 9 19 CA960126009 119951117A6322369D25623 BELT HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL OIL COOLER WORN W K NONE O OTHER ININSP/MAINT 1 CA 602 CAE832056 (CAN)BELT WORN BEYOND LIMITS. 1000 HOUR NORMAL RETIREMENT LIFE. 1G71 3U3 U H3WE E4CE 19960919005281996091900528GL 1996 9 19 CA960126010 219951117A732323057870 GOVERNOR HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL ENG FCU LEAKING W K NONE O OTHER ININSP/MAINT 1 CA 403 CAE832056 (CAN)BEARING LEAKING BLUE GREASE AND FEELS ROUGH. 1G71 3U3 U H3WE E4CE 19960919005291996091900529GL 1996 9 19 CA960126011 219951117A732223057344 BEARING HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL FCU LEAKING W K NONE O OTHER ININSP/MAINT 1 CA 1110 CAE832056 (CAN)BEARING LEAKING GREASE AND FEELS ROUGH. FCU REPLACED. 1G71 3U3 U H3WE E4CE 19960919005301996091900530SW 1996 9 19 CA960126012 119951231A5610212030466001 WINDSCREEN BELL 212 212 1181420SW CENTRE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN)WINDSHIELD CRACKED HORIZONTALLY IN CENTER LAYER AND CRACKED VERTICALLY IN INSIDE LAYER. 1G71 4U H4SW 19960919005311996091900531EU 1996 9 19 CA960126013 119951218A24350268980110 CLAMP SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE START/GEN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 416 (CAN)STARTER GENERATOR HALF CLAMPS FOUND TO BE CRACKED. HALF CLAMPS REPLACED. AIRCRAFT RETURNED TO SERVICE. 1G71 3U3 U H9EU E19EU 19960919005321996091900532EU 1996 9 19 CA960126014 119951231A6210350A11001001 BLADE SNIAS 350 AS350B 8680801EU M/R WONT TRACK W K NONE E VIBRATION/BUFFET ININSP/MAINT 1 CA 9269 (CAN)EXTREME DIFFICULTY WITH TRACKING OF MAIN ROTOR BLADE. COULD NOT GET BLADE BALANCED WITH MAXIMUM BALANCE PLATES INSTALLED. 1G71 3U H9EU 19960919005331996091900533EU 1996 9 19 CA960126015 119951231A6220EIT254901 FREQUENCY ADAPTE SNIAS 350 AS350B 8680801EU TMECA ARRIELARRIEL1B 6OO30NE M/R WORN W K NONE E VIBRATION/BUFFET ININSP/MAINT 1 CA 2388 840 (CAN)EXCESSIVE 3 PER VIBRATION CAUSED BY WORN FREQUENCY ADAPTERS. 1G71 3U3 U H9EU E19EU 19960919005531996091900553WP 1996 9 19 CA960126037 119951230A7110 FAIRING PANEL LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122B02 54555NE NR 3 ENG DAMAGED W K NONE D INFLIGHT SEPARATION CRCRUISE 1 CA 10346 (CAN)ON ARRIVAL #3 ENGINE GAS GENERATOR PANEL (FAIRING) WAS FOUND DAMAGED DURING REVERSE. DAMAGE WAS EVALUATED AND PANEL WAS REPLACED. #3 ENGINE REVERSER LOCKED-OUT & AIRCRAFT DISPATCHED AS PER MM 78-03 & MEL 79-31-00. 2L73 4F4 F A23WE E12EU 19960919005661996091900566NM 1996 9 19 CA960129009 119951230A3250 O-RING DHAV DHC8 DHC8102 2809003NM STEER MANIFOLD FAILED W O OTHER JK WARNING INDICATION FLUID LOSS DEDESCENT 1 CA (CAN)ON DESCENT, THROUGH 10,000 FEET, COMPLETE LOSS OF #2 HYDRAULIC SYSTEM. ALTERNATE GEAR EXTENSION CARRIED OUT. AND AIRCRAFT LANDED OK. 'O' RING BETWEEN STEERING MANIFOLD AND CHECK VALVE FOUND LEAKING. # 2 ENGINE DRIVEN PUMP ALSO REPLACED BECAUSE SYSTEM HAD RUN DRY. 2H72 4T RTA13NM 19960919005741996091900574WP 1996 9 19 AENA131C 119950321A57535912149508 BRACKET ASSY DOUG DC9 DC932 3022066WP WS 251.683 CRACKED A AENAK NONE O OTHER ININSP/MAINT 1 WP191271L 47319 INSPECTION FOUND BRACKET ASSY CRACKED AT THE RT CENTER FLAP HINGE, WS 251.683. (X) 2L72 4F A6WE 19960919005751996091900575WP 1996 9 19 AENA131C1 119950321A57535912150508 BRACKET ASSY DOUG DC9 DC932 3022066WP RT INBD FLAP BROKEN A AAENAO OTHER F FLT CONT AFFECTED APAPPROACH 1 WP191271L 47319 ON APPROACH INTO LAS, PILOT SELECTED 40 DEGREE FLAP DOWN AND HAD 30 DEGREE SPLIT ON FLAP INDICATOR L20 DEGREEES, R50 DEGREES. PILOT INDICATED NO CONTROL PROBLEMS AND ACFT LANDED WITHOUT INCIDENT. ON INSPECTION BY MAINTENANCE AT LAS, FOUND RT INBD FLAP HINGE (STA 154.584) SEPARATED IN TWO. UPON FURTHER INSPECTION BY NDT, ALSO FOUND RT CENTER FLAP HINGE (STA 251.683) CRACKED. (X) 2L72 4F A6WE 19960919005771996091900577SW 1996 9 19 96ZZZX4689 119950305A6120C81024 CONTROL CABLE SWRNGNSA226 SA226TC 8780404SW PROPELLER PITCH UNSCREWED AS QTVAK NONE O OTHER ININSP/MAINT 1 NM11341PL204 500 TC334 PILOT WAS UNABLE TO GET PROPELLER ON LOCKS AT ENGINE SHUT-DOWN. INSPECTION REVEALED SEPARATION OF CABLE ASSEMBLY WHERE THE MOUNTING BARREL THREADS INTO OUTER SPIRAL ASSEMBLY. THERE ARE NO PROVISIONS FOR THIS AREA TO BE SAFTIED. PART WAS NOT BROKEN, ONLY UNSCREWED FROM POSITION. 2L72 4T RTA8SW 19960919005991996091900599CE 1996 9 19 96ZZZX4712 119950224A56102311260208 WINDSHIELD LEAR 35 35A 5170602CE COCKPIT RT CRACKED A AGBUAK NONE O OTHER ININSP/MAINT 1 NM1144AB 4382 473 WINDSHIELD CRACKED THROUGH OUTER PLY JUST ABOVE DEFOG NOZZLE OUTLET. DISCREPANCY NOTED ON POST-FLIGHT INSPECTION. BOTH WINDSHIELDS ON THIS AIRCRAFT HAVE BEEN REWORKED I N THIS AREA TO REMOVE CRAZING CAUSED BY WINDSHIELD HEAT. WINDSHIELD MET MINIMUM THICKNESS REQUIREMENTS SPECIFICED BY MANUFACTURER. CRACK ORIGINATED IN RADIUS WHERE REWORKED AREA MEETS UNALTERED WINDSHIELD UNDER DEFOG NOZZLE. SUGGEST USING A LARGER RADIUS TO BLEND IN REWORKED AREA AT NOZZLE EDGE. CRACK APPROXIMATELY 5 INCHES LONG, OUTER PLY ONLY. 2L72 4F A10CE 19960919006121996091900612SO 1996 9 19 96ZZZX4725 219950218A8530641370CP VALVE PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360E 17025SO NR 5, 6 CYL EXH BURNED A OHGAE ENGINE SHUTDOWN ER VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CRCRUISE 1 NM0932959 1275 347570069 304586 PILOT REPORTED ENGINE STARTED MISSING AT 15,000 FEET FOLLOWED BY SURGING THAT MADE IT NECESSARY TO SECURE ENGINE. TROUBLESHOOTING FOUND NR 5, AND NR 6 CYLINDERS HAD 12-18 PSI COMPRESSION. PULLED CYLINDERS AND FOUND EXHAUST VALVE BURNED IN BOTH CYLINDERS. CAUSE IS MOST LIKELY ENGINE HAD BEEN OPERATED AT TOO LEAN A MIXTURE. 1L72 3O3 O A7SO E9CE 19960919006211996091900621SO 1996 9 19 96ZZZX4734 119950215A2434 ALTERNATOR PRESTOLITE PIPER PA31 PA31310 7103103SO LT ENGINE FAILED A OHGAO OTHER H ELECT. POWER LOSS-50 PC CRCRUISE 1 NM0968ST 660 8N000029 31729 PILOT REPORTED ALTERNATOR FAILED EN ROUTE. UPON TROUBLESHOOTING FOUND FORWARD BEARING HAD FAILED. REPLACED WITH OVERHAULED UNIT. 1L71 3O RTA20SO 19960919009221996091900922SO 1996 9 19 96ZZZX4737 219950203A8520643033 CRANKCASE PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360E 17025SO RT ENG NR 3 CYL CRACKED A OHGAK NONE K FLUID LOSS ININSP/MAINT 1 NM09821GS4509 1385 304857 347770419 304857 WHILE TROUBLESHOOTING OIL LEAK, FOUND 3 INCH CRACK RUNNING FROM TOP CENTER BOLT ON CRANKCASE DOWN TO BASE OF NR 3 CYLINDER. 1L72 3O3 O A7SO E9CE 19960919009231996091900923SO 1996 9 19 96ZZZX4738 219950202A8530649484 CYLINDER PIPER PA34 PA34200T 7103406SO CONT O360 LTSIO360E 17025SO NR 3 CYLINDER CRACKED A OHGAK NONE O OTHER TXTAXI/GRND HDL 1 NM09821GS 1351 347770419 304857 AFTER LANDING, PILOT NOTICED NOISE FROM ENGINE, THOUGHT HE HAD EXHAUST LEAK. UPON INSPECTION, FOUND NR 3 CYLINDER HAD CRACKED AT TOP OF BARREL AND BURNED HOLE IN AREA OF CRACK. CRACK PROGRESSED THREE-FOURTHS WAY AROUND HEAD, AT TOP OF BARREL. 1L72 3O3 O A7SO E9CE 19960919009251996091900925SO 1996 9 19 96ZZZX4740 119950215A55234322100 HORN ASSY PIPER PA31 PA31310 7103103SO ELEV TRIM TAB CRACKED AS OHGAK NONE O OTHER ININSP/MAINT 1 NM099111Y 31148 DURING 100-HOUR INSPECTION, FOUND CRACK IN TRIM TAB HORN ASSY FROM FORWARD LOWER CORNER BACK TO SECOND RIVET. ALSO, THE 4 RIVETS HOLDING HORN ASSY TO FORWARD SIDE OF FORWARD SPAR WERE LOOSE AND WORKING. TAB SHOWS EVIDENCE OF POOR REPAIR AT SOME TIME IN ITS LIFE. 1L71 3O RTA20SO 19960926000011996092600001GL 1996 9 26 ERAA9564 219950502A725023031938 NOZZLE 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 2ND STAGE FAILED A ERAAK NONE O OTHER ININSP/MAINT 1 AL03298EH CAT25333 S845 WHILE CUTTING 2ND STG B.T.P. CLEARANCE METAL BEGAN TO FLAKE OFF. 2ND STAGE NOZZLE SENT IN FOR OVERHAUL 1G72 3U3 U H3EU E4CE 19960926000041996092600004GL 1996 9 26 ERAA9567 219950503A7250A6898977 COUPLING BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL N1 COUPLING ROUGH SPLINES A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03298EH S845 SPLINES ARE ROUGH ON N1 COUPLING. 1G72 3U3 U H3EU E4CE 19960926000051996092600005GL 1996 9 26 ERAA9568 219950504A725047089 OUTER SHROUD BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE DEFECTIVE A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03207EH 3296 ALLSN NEW PART WITH -0- HOURS. SHROUD WILL NOT THREAD INTO BODY. 1G71 3U3 U H2SW E4CE 19960926000061996092600006GL 1996 9 26 ERAA9570 219950504A7210A6875035 BEARING BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL ENG GR BOX DEFECTIVE A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03127EH S571 NEW BEARING WITH -0- HRS. ROLLER END RADIUS NOT CONSISTENT. 1G72 3U3 U H3EU E4CE 19960926000071996092600007GL 1996 9 26 ERAA9572 219950511A72506895010 GP SUPPORT 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL GAS PROD MIS OVERHAULED A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03291EH CAT36048 S842 G.P. SUPPORT WAS OVERHAULED BY DALLAS AIRMOTIVE ON W/O C67562 , SENT IN ON ERA P.O.G107056 AND RECEIVED BACK JAN 18, 1995. TANG SLOTS ARE UNDER SIZED. 1G72 3U3 U H3EU E4CE 19960926000081996092600008GL 1996 9 26 ERAA9573 219950512A72506878498 NOZZLE 6898735 BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 2ND STAGE NOT BONDED A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03291EH CAT36048 S842 NOZZLE WAS OVERHAULED BY DALLAS AIRMOTIVE ON W/O C67745, SENT IN ON ERA P.O. G108376 , RECEIVED BACK AT ERA 3/16/95. A VISUAL INSPECTION WAS CONDUCTED AND DISCOVERED THAT THE METALIZED PORTION OF THE 2ND STG BLADE TIP PATH IS NOT BONDED TO THE PARENT MATERIAL. 1G72 3U3 U H3EU E4CE 19960926000091996092600009GL 1996 9 26 ERAA9574 219950512A72506878498 NOZZLE BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL 2ND STAGE TIP DELAMINATED A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03127EH S571 NOZZLE SENT IN EXCHANGE FOR S/N X58872 THAT HAD BEEN OVERHAULED ON D/AIR W/O C67745 AND RETURNED FOR TIP PATH NOT BEING BONDED TO PARENT MATERIAL. THIS NOZZLE REC'D IN EXCHANGE IS ALSO BAD, 2ND STAGE BLADE TIP PATH IS DELAMINATING. 1G72 3U3 U H3EU E4CE 19960926000101996092600010EU 1996 9 26 ERAA9575 119950512A6220A6871259 TIE BOLT BOLKMS105 BO105S 5626006EU M/R WRONG SIZE A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03424EH S548 NEW TIE BOLT THAT WOULD NOT GO INTO ROTOR ASSY. TOP MUTE MICS AT .4433 (MAX IS .4425 AS PER ALLISON L/H & SUPERIOR PRINTS). 1G72 3U H3EU 19960926000111996092600011GL 1996 9 26 ERAA9576 219950512A7250A6898784 ADAPTER BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL SPLINE ADAPTER PLATING FLAKING A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03135EH S675 NEW ADAPTER THAT HAS DAMAGED INTERNAL SPLINES, FLAKING SILVER PLATING. 1G72 3U3 U H3EU E4CE 19960926000121996092600012GL 1996 9 26 ERAA9577 219950517A7250A23037403 INNER SHAFT BOLKMS105 BO105S 5626006EU ALLSN 250C 250C20B 03013GL BEARING RACE PITTED A ERAAK NONE W INADEQUATE Q C ININSP/MAINT 1 AL03124EH S559 NEW INNER SHAFT THAT HAS PITS ON BEARING RACE. 1G72 3U3 U H3EU E4CE 19961003007941996100300794 1996 10 3 CA960103523 419951122A2310A3873 FILTER BOEING767 767233 NM AFT GALLEY LEAKING OIL W O OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 CA (CAN)AT RAMP FLIGHT ATTENDANT REPORTED SMOKE COMING FROM STARBOARD REAR GALLEY. RH HF COMM FILTER LEAKING OIL. 2L72 4F RTA1NM 19961010003971996101000397EU 1996 10 10 CA951130005 219951121A73105500101517002 ACTUATOR PLESSEY 500101517002BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU FUEL TRIM CORROSION W K NONE O OTHER ININSP/MAINT 1 CA 2841 3510J 19413 (CAN)INSPECTION REVEALED RUBBER SEAL MISSING ALLOWING MOISTURE INTO UNIT CAUSING INTERNAL CORROSION. NO INTERNAL CORROSION PROTECTION EVIDENT. SEVERAL UNAUTHORIZED PARTS INSTALLED. 2L72 3T4 T A24EU A196 19961010003981996101000398SW 1996 10 10 CA951209103 119951120A7120111023008 DIFFUSER HOUSING BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE BLEED PAN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2025 LEO7596 (CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT. 1G71 4U4 U H1SW E17EA 19961010003991996101000399SW 1996 10 10 CA951209104 119951120A7120111023008 DIFFUSER HOUSING BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE BLEED PAN CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 1971 LEO7240 (CAN)ON DAILY INSPECTION IT WAS FOUND THAT THE PAN HAD CRACKED AROUND THE INSERT. 1G71 4U4 U H1SW E17EA 19961010004001996101000400EU 1996 10 10 CA951218020 119951205A243594065 BEARING LUCAS 23095002 BAG JETSTMJETSTM4112 EU AFT SHAFT RT GENFAILED W O OTHER EH VIBRATION/BUFFET ELECT. POWER LOSS-50 PC NRNOT REPORTED 1 CA 1042 475 94065 (CAN)RIGHT GENERATOR FAILED IN FLIGHT. RESET, BUT FAILED 10 MINUTES LATER AGAIN. A VIBRATION THEN STARTED AND LASTED ABOUT FIVE MINUTES. RIGHT HAND STARTER GENERATOR REPLACED. 1L72 4T RTA196 19961010004011996101000401EU 1996 10 10 CA951221034 119951212A3260AIR135668 SWITCH BAG JETSTMJETSTM4112 EU MCAULY LH GEAR LOCK FAILED W K NONE O OTHER NRNOT REPORTED 1 CA 1541 NC254394 (CAN)LEFT 'GEAR LOCK' RED LIGHT ON WHEN GEAR SELECTED UP 1L72 4T RTA196 19961010004021996101000402EU 1996 10 10 CA951221036 119951212A2913384925 PUMP VICKERS BAG JETSTMJETSTM4112 EU NR1 HYD LOW PRESSURE W K NONE O OTHER NRNOT REPORTED 1 CA 1885 9433265 (CAN)#1 HYDRAULIC SYSTEM PRESSURE LOW. PUMP REPLACED. 700 VS. 2000 PSI. 1L72 4T RTA196 19961010004031996101000403EU 1996 10 10 CA951221037 119951214A3297NC252994 WIRE BAG JETSTMJETSTM4112 EU LT MLG LIGHT BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 1595 NC252994 (CAN)WIRES FOUND PULLED OUT FROM SWITCH BODY WHILE INVESTIGATING SNAG ON LEFT RED GEAR LIGHT SWITCH ASSEMBLY IS FOR LANDING GEAR HANDLE TRANSIT LIGHT. 1L72 4T RTA196 19961010004041996101000404EU 1996 10 10 CA951221038 119951214A3260AIR135668 SWITCH BAG JETSTMJETSTM4112 EU LH GEAR LIGHT FAILED W K NONE P NO WARNING INDICATION NRNOT REPORTED 1 CA 1595 NC252594 (CAN)LEFT RED GEAR LIGHT WOULD NOT ILLUMINATE. SWITCH FOR LH GEAR LIGHT REPLACED 1L72 4T RTA196 19961010004051996101000405EU 1996 10 10 CA960102007 119951221A2750TY175603C VALVE LUCAS BAG JETSTMJETSTM4112 EU FLAP SELECTOR STUCK W K NONE O OTHER NRNOT REPORTED 1 CA 1597 10046 (CAN)FLAP DOES NOT COME OUT OF 25 DEGREE SETTING. FLAP SELECTOR VALVE REPLACED. 1L72 4T RTA196 19961010004351996101000435CE 1996 10 10 CA960202021 119950912A5510169620009 SPAR BEECH 169620001661BEECH 23 B19 1151215CE LYC O320 O320E3D 41508EA HINGE ATTH POINTCRACKED W K NONE O OTHER ININSP/MAINT 1 CA 6906 MB874 L3885427A (CAN)SUBMITTER FOUND THE BEGINNING OF CRACKS IN THE FILLET OF THE SPAR AT THE STABILATOR HINGE ATTACHMENT POINTS. 1L71 3O3 O A1CE E274 19961010005521996101000552WP 1996 10 10 96ZZZM1404 119950303A57209919369502N TEE CAP DOUG DC9 DC932 3022066WP WS 58.5 CRACKED A VJ6AK NONE O OTHER ININSP/MAINT 1 SO11908VJ65515 47321 RIGHT WING LOWER TEE CAP CRACKED IN THE RADIUS AFT OF STRINGER 16 EXTENDING UNDERNEATH STRINGER 15 (AD90-18-03 UPDATED TO 96-10-11). REMOVED AND REPLACED STA XCW 58.5 RIGHT AND LEFT TEE CAPS IAW MDC SERVICE BULLETING 57-98 REV 8 DATED 3-15-91 AND WORKORDER NR 42523515.1 AND 42523515.2. LEFT TEE CAP CHANGED FOR CONVENIENCE AND GROUND TIME. 2L72 4F A6WE 19961010005651996101000565WP 1996 10 10 GTIA96NK006 119951121A5720 SUPPORT DOUG DC9 DC932 3022066WP RT WING CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT AT XRS324.00 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT IAW COOPESA DWG HSE9-57-242 DATED NOV 14, 1995 AND FAA FORM 8110-3 DATED NOV 14, 1995. (M) 2L72 4F A6WE 19961010005661996101000566WP 1996 10 10 GTIA96NK007 119951121A5753 PANEL DOUG DC9 DC932 3022066WP RT TE FLAP CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING AT XFS187 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING IAW SRM 51-01, PARAGRAPH C AND SRM 51-30-2 AND FAA FORM 8110-3 DATED NOV 9, 1995. (M) 2L72 4F A6WE 19961010005671996101000567WP 1996 10 10 GTIA96NK008 119951121A5711 SPAR DOUG DC9 DC932 3022066WP RSS 129 LT & RT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND LEFT AND RIGHT WING UPPER REAR SPAR CAP FLANGES AT RIGHT STATION XRS129 AND LEFT STATION XRS127.5 CORRODED. REWORKED LEFT AND RIGHT UPPER REAR SPAR CAP FLANGES IAW MCDONNELL DOUGLAS INSTRUCTION ON FILE 95-11-06-014/AJC00146 DATED NOV 8, 1995 AND FAA FORM 8110-3 DATED NOV 10, 1995. (M) 2L72 4F A6WE 19961010005681996101000568WP 1996 10 10 GTIA96NK009 119951121A5311 FRAME DOUG DC9 DC932 3022066WP BS 1104 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104, LONGERON 4 LEFT CRACKED. REPAIRED FUSELAGE CANTED FRAME SECTION IAW SRM 53-01, FIG 2. (M) 2L72 4F A6WE 19961010005691996101000569WP 1996 10 10 GTIA96NK010 119951121A5330 SKIN DOUG DC9 DC932 3022066WP Y1121-1136 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y1121 TO STATION Y1136, LONGERONS 20 RIGHT TO 21 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-01, FIG 2, PAGE 8, SRM 51-30-2. (M) 2L72 4F A6WE 19961010005701996101000570WP 1996 10 10 GTIA96NK011 119951121A5311 FRAME DOUG DC9 DC932 3022066WP BS Y1104.937 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104.937 BETWEEN LONGERON 10 RIGHT TO 16 RIGHT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW SRM 51-01, PARAGRAPH C. (M) 2L72 4F A6WE 19961010005711996101000571WP 1996 10 10 GTIA96NK012 119951121A5311 FRAME DOUG DC9 DC932 3022066WP BS 1104 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104 BETWEEN LONGERONS 10 LEFT TO 23 LEFT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW ARM 51-01, PARAGRAPH C. (M) 2L72 4F A6WE 19961010005721996101000572WP 1996 10 10 GTIA96NK013 119951121A5313 LONGERON DOUG DC9 DC932 3022066WP BS 1109-1114 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE LONGERON 14 LEFT BETWEEN STATION Y1109 TO STATION Y1114 CORRODED. REPAIRED LONGERON 14 LEFT IAW SRM 53-02, FIG 2A. (M) 2L72 4F A6WE 19961010005731996101000573WP 1996 10 10 GTIA96NK014 119951121A5330 SKIN DOUG DC9 DC932 3022066WP BS 451-465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE SKIN SECTION AT PITOT STATIC PORT AREA BETWEEN STATION Y451 TO STATION Y465, LONGERONS 23 LEFT TO 26 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 31, SHEET 1. (M) 2L72 4F A6WE 19961010005741996101000574WP 1996 10 10 GTIA96NK015 119951121A531199196182N FRAME DOUG DC9 DC932 3022066WP BS 718 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND RIGHT CENTER OVER WHEEL FRAME, P/N 9919618-2N, AT STATION Y718, CRACKED. REPLACED RIGHT CENTER FRAME IAW MD S/B 53-131 REV 3, DATED FEB 11, 1988 OPTION 2, GROUP III, FIG 4. (M) 2L72 4F A6WE 19961010005751996101000575WP 1996 10 10 GTIA96NK016 119951121A5313 LONGERON DOUG DC9 DC932 3022066WP BS 356.7-415 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION BETWEEN STATION Y356.7 TO STATION Y415 CORRODED. REPLACED LONGERON 30 SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 53-02 FIG 14, DATED NOV 13, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M) 2L72 4F A6WE 19961010005761996101000576WP 1996 10 10 GTIA96NK017 119951121A5320 FITTING DOUG DC9 DC932 3022066WP BS 996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE LONGERON 20 RIGHT END FITTING AT STATION Y996 CORRODED. REPLACED LONGERON 20 END FITTING IAW SRM 51-01 PARAGRAPH C AND SRM 51-10-2. (M) 2L72 4F A6WE 19961010005771996101000577WP 1996 10 10 GTIA96NK019 119951121A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 965.09 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND THE PAX/FLOOR BEAM LOWER CHORD AT STATION Y965.09 BETWEEN PLUS X6.7 TO PLUS X18 AND BETWEEN PLUS X21.5 TO PLUS 53.5 CORRODED. REPAIRED PAX/FLOOR BEAM LOWER CHORD AT IAW COOPESA DWG NO HSE9-53-140 REV A DATED NOV 12, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M) 2L72 4F A6WE 19961010005781996101000578WP 1996 10 10 GTIA96NK020 119951223A5313 LONGERON DOUG DC9 DC931 3022065WP BS 563-604 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE 30 LONGERON SECTION FROM STATION Y563 TO STATION Y604 CORRODED. REPLACED FUSELAGE 30 LONGERON SECTION IAW COOPESA DWG HSE9-53-247, FAA FORM 8110-3 NR 95113 DATED NOV 30, 1995, AND FAA FORM 8110-3 NR 95112 DATED NOVE 30, 1995. (M) 2L72 4F A6WE 19961010005791996101000579WP 1996 10 10 GTIA96NK021 119951223A5210 DOOR BEAM DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AA-AA PAGE 185. (M) 2L72 4F A6WE 19961010005801996101000580WP 1996 10 10 GTIA96NK022 119951223A5320 FAIRING DOUG DC9 DC931 3022065WP RT ADF ANTENNA DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD RIGHT ADF ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD RIGHT ADF ANTENNA IAW COOPESA DWG HSE9-53-262 DATED DEC 8, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M) 2L72 4F A6WE 19961010005811996101000581WP 1996 10 10 GTIA96NK023 119951223A5311 FRAME DOUG DC9 DC931 3022065WP BS 917 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y917 BETWEEN LONGERONS 26 LEFT AND 29 RIGHT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M) 2L72 4F A6WE 19961010005821996101000582WP 1996 10 10 GTIA96NK024 119951223A5320 FAIRING DOUG DC9 DC931 3022065WP LT ADF ANTENNA DELAMINATED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD ADF LEFT ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD ADF LEFT ANTENNA IAW COOPESA DWG HSE-9-53-270 DATED DEC 15, 1995 AND FAA FORM 8110-3 DATED DEC 15, 1995. (M) 2L72 4F A6WE 19961010005831996101000583WP 1996 10 10 GTIA96NK025 119951223A5311 FRAME DOUG DC9 DC931 3022065WP BS 408 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y408 BETWEEN LONGERONS 25 LEFT AND 30 CRACKED AND CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEETS 1 TO 5. (M) 2L72 4F A6WE 19961010005841996101000584WP 1996 10 10 GTIA96NK026 119951223A5320 JAMB DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER IAW SRM 53-05 FIG 26A PAGE 62A. (M) 2L72 4F A6WE 19961010005851996101000585WP 1996 10 10 GTIA96NK027 119951223A5210 DOOR BEAM DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION IAW SRM 52-05 FIG 31 SHEET 7 SECTION MM PAGE 193. (M) 2L72 4F A6WE 19961010005861996101000586WP 1996 10 10 GTIA96NK028 119951223A5210 DOOR BEAM DOUG DC9 DC931 3022065WP PAX DOOR CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AC-AC PAGE 185. (M) 2L72 4F A6WE 19961010005871996101000587WP 1996 10 10 GTIA96NK029 119951223A5347 SEAT TRACK DOUG DC9 DC931 3022065WP BS 200-256 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX SEAT TRACKS FROM FS Y200 TO FS Y256 AT PLUS X23 AND -X47 CORRODED. REPAIRED PAX SEAT TRACKS IAW SRM 53-05 FIG 4 SHEET 1. (M) 2L72 4F A6WE 19961010005881996101000588WP 1996 10 10 GTIA96NK030 119951223A5311 FRAME DOUG DC9 DC931 3022065WP BS 1132.6 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1132.6 AND LONGERON 16 LEFT CORRODED AND WORN. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 4 PAGE 9. (M) 2L72 4F A6WE 19961010005891996101000589WP 1996 10 10 GTIA96NK031 119951223A5312 BULKHEAD TEE DOUG DC9 DC931 3022065WP BS 604 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE BULKHEAD T-CHORD SECTION AT Y604 BETWEEN LONGERONS 28 RIGHT AND 28 LEFT CORRODED. REPAIRED FUSELAGE T-CHORD SECTION IAW DOUGLAS FAX ACTION NR 284374 DATED DEC 6, 1995 AND MD DWG 5934768 VIEW 'C' ZONE 3 AND VIEW 'B' ZONES 8 AND 9. (M) 2L72 4F A6WE 19961010005901996101000590WP 1996 10 10 GTIA96NK032 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 432-465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y432 AND STATION Y465, LONGERONS 28 LEFT TO 29 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04 FIG 44 SHEET 1. (M) 2L72 4F A6WE 19961010005911996101000591WP 1996 10 10 GTIA96NK033 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 589-607 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y589 AND STATION Y607, LONGERONS 17 RIGHT TO 19 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA HSE9-53-263 DATED DEC 11, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M) 2L72 4F A6WE 19961010005921996101000592WP 1996 10 10 GTIA96NK034 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 667-756 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C AND SRM 51-30-2. (M) 2L72 4F A6WE 19961010005931996101000593WP 1996 10 10 GTIA96NK035 119951223A5311 FRAME DOUG DC9 DC931 3022065WP BS 1038 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1038 AND LONGERON 13 LEFT CRACKED. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 2. (M) 2L72 4F A6WE 19961010005941996101000594WP 1996 10 10 GTIA96NK036 119951223A5312 BULKHEAD WEB DOUG DC9 DC931 3022065WP BS 996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE BULKHEAD WEB AT STATION Y996 FROM LONGERONS 23 RIGHT TO 23 LEFT AND BETWEEN -Z210 AND -Z240 CORRODED. REPLACED FUSELAGE BULKHEAD WEB IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 51-30-5. (M) 2L72 4F A6WE 19961010005951996101000595WP 1996 10 10 GTIA96NK037 119951223A5280 DOOR PAN DOUG DC9 DC931 3022065WP LT MLG CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND LEFT WHEEL WELL DOOR PAN INBOARD AFT SECTION CRACKED. REPAIRED LEFT WHEEL WELL DOOR PAN INBOARD AFT IAW COOPESA DWG HSE9-52-261 DATED DEC 7, 1995. (M) 2L72 4F A6WE 19961010005961996101000596WP 1996 10 10 GTIA96NK038 119951223A5311 FRAME DOUG DC9 DC931 3022065WP BS 579 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y579 BETWEEN LONGERONS 27 RIGHT AND 27 LEFT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M) 2L72 4F A6WE 19961010005971996101000597WP 1996 10 10 GTIA96NK039 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 576-591 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURIGN C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y576 AND STATION Y591, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA DWG HSE9-53-256 DATED DEC 4, 1995 AND FAA FORM DATED DEC 5, 1995. (M) 2L72 4F A6WE 19961010005981996101000598WP 1996 10 10 GTIA96NK040 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 667-756 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURIGN C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 LEFT TO 28 RIGHT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2. (M) 2L72 4F A6WE 19961010005991996101000599WP 1996 10 10 GTIA96NK041 119951223A5330 SKIN DOUG DC9 DC931 3022065WP BS 988-996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y988 AND STATION Y996, LONGERONS 29 RIGHT TO 29 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 9 PAGE 23. (M) 2L72 4F A6WE 19961010006081996101000608WP 1996 10 10 GTIA96NK050 119951125A5313 LONGERON DOUG DC9 DC931 3022065WP BS 813-869 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPT LONGERON 30 WITH CORROSION BETWEEN Y813 AND Y869. REMOVED CORROSION AND TREATED METAL SECTION IAW SRM 51-10-3 AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006091996101000609WP 1996 10 10 GTIA96NK051 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 851 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPT FRAME WITH CORROSION IN BOTH FACE AT Y-851 BETWEEN LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. SECTION WITHIN LIMITS IAW SRM 53-01 FIG 1 SHEET 3. REPLACED RIVETS IAW 51-30-2. (M) 2L72 4F A6WE 19961010006101996101000610WP 1996 10 10 GTIA96NK052 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 832 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPT FRAME WITH CORROSION AT Y832 BETWEEN LONGERONS 28 LT AND 29 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006111996101000611WP 1996 10 10 GTIA96NK053 119951125A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 756-889.5 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPT FLOOR CHANNEL RIGHT WITH CORROSION AND LOOSE RIVETS BETWEEN Y756 AND Y889.5. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1 AND REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006121996101000612WP 1996 10 10 GTIA96NK054 119951125A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 794 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR CHANNEL LEFT WITH CORROSION AND LOOSE RIVETS BETWEEN Y794 AND Y809. ACCOMPLISHED REPAIR AT AFT C/C FLOOR CHANNEL LEFT BETWEEN Y813 AND Y832, Y794 AND Y813 IAW SRM 53-02 FIG 2 SHEET 4. (M) 2L72 4F A6WE 19961010006131996101000613WP 1996 10 10 GTIA96NK055 119950112A5311 FRAME DOUG DC9 DC931 3022065WP BS 813 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE AND FORWARD FACE AT Y813 BETWEEN LONGERON 29LT AND LONGERON 28RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006141996101000614WP 1996 10 10 GTIA96NK056 119951125A5320 SPLICE DOUG DC9 DC931 3022065WP BS 794-813 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 SPLICE WITH CORROSION BETWEEN Y794 AND Y813. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006151996101000615WP 1996 10 10 GTIA96NK057 119951125A5330 SKIN DOUG DC9 DC931 3022065WP BS 794-813 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN LONGERON 30 AND LONGERON 29 LEFT AND BETWEEN Y794 AND Y813. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1 SHEET 3. INSTALLED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006161996101000616WP 1996 10 10 GTIA96NK058 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 794 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE AND FORWARD FACE AT Y794 BETWEEN LONGERON 29 LEFT AND LONGERON 30. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006171996101000617WP 1996 10 10 GTIA96NK059 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 775 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, AFT CARGO COMPARTMENT FRAME WITH CORROSION IN LOWER FLANGE IN Y775 BETWEEN LONGERON 30 AND LONGERON RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006181996101000618WP 1996 10 10 GTIA96NK060 119951125A5330 SKIN DOUG DC9 DC931 3022065WP BS 756 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN LONGERON 29 RIGHT AND 30 AT Y756. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006191996101000619WP 1996 10 10 GTIA96NK061 119951125A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 889-897 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, AFT CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y889 AND Y897 AND BETWEEN LONGERONS 30 AND 29 RT. REPLACED INTERCOSTAL BETWEEN Y889 AND Y897 AND LONGERON 30/29 RIGHT IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. FABRICATED UNIT IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961010006201996101000620WP 1996 10 10 GTIA96NK063 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 869 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION AT Y869 BETWEEN LONGERONS 26 AND 25 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006211996101000621WP 1996 10 10 GTIA96NK064 119951125A5313 LONGERON DOUG DC9 DC931 3022065WP BS 869-945 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y869 AND Y945. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006221996101000622WP 1996 10 10 GTIA96NK065 119951125A5313 LONGERON DOUG DC9 DC931 3022065WP BS 869-889 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29 RIGHT WITH CORROSION BETWEEN Y869 AND Y889. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 53-30-2. (M) 2L72 4F A6WE 19961010006231996101000623WP 1996 10 10 GTIA96NK066 119951125A5311 FRAME DOUG DC9 DC931 3022065WP BS 869 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME WITH CORROSION AT Y869 BETWEEN LONGERON 29 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006241996101000624WP 1996 10 10 GTIA96NK067 119951125A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR CHANNEL RIGHT WITH CORROSION BETWEEN Y945 AND Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006251996101000625WP 1996 10 10 GTIA96NK068 119951126A5311 FRAME DOUG DC9 DC931 3022065WP BS 937 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y937 AFT FACE WITH CORROSION BETWEEN LONGERONS 26 LEFT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006261996101000626WP 1996 10 10 GTIA96NK069 119951126A5311 FRAME DOUG DC9 DC931 3022065WP BS 917 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y917 WITH CORROSION BETWEEN LONGERONS 26 LEFT AND 29 RIGHT. REPAIRED DAMAGED FRAME SECTION AT Y917 BETWEEN LONGERONS 26 LEFT AND 29 RIGHT IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A, FABRICATED SPLICE IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961010006271996101000627WP 1996 10 10 GTIA96NK070 119951126A5311 FRAME DOUG DC9 DC931 3022065WP BS 897 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME STATION Y897 AFT FACE FRAME WITH CORROSION BETWEEN LONGERON 26 LEFT AND 30 FRAME. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006281996101000628WP 1996 10 10 GTIA96NK071 119951125A5313 LONGERON DOUG DC9 DC931 3022065WP BS 897 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 23 LEFT STRAP WITH CORROSION AT Y897. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006291996101000629WP 1996 10 10 GTIA96NK072 119951125A5320 FITTING DOUG DC9 DC931 3022065WP BS 996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, AFT CARGO COMPARTMENT LONGERON 230C END FITTING WITH CORROSION AT STATION Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006301996101000630WP 1996 10 10 GTIA96NK073 119951126A5313 LONGERON DOUG DC9 DC931 3022065WP BS 170 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND E/E COMPARTMENT LONGERON 29 RIGHT WITH LIGHT CORROSION AT STATION Y170. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006311996101000631WP 1996 10 10 GTIA96NK074 119951121A53135920303 LONGERON DOUG DC9 DC932 3022066WP BS 756-802 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION, P/N 592030350, IN BETWEEN STATION Y756 TO STATION Y802 CRACKED. REPLACED LONGERON 30 IAW SRM 51-01 PARA C, SRM 51-30-2. THE FRAMES AT STATION Y775 AND STATION Y794 WERE CUT FOR ACCESS AND REPAIRED IAW SRM 53-03 FIG 2A PAGE 4. (M) 2L72 4F A6WE 19961010006321996101000632WP 1996 10 10 GTIA96NK075 119951126A5311 FRAME DOUG DC9 DC931 3022065WP BS 180 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND E/E COMPARTMENT STATION Y180 FRAME CORRODED BETWEEN LONGERON 29R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006331996101000633WP 1996 10 10 GTIA96NK076 119951126A5311 FRAME DOUG DC9 DC931 3022065WP BS 200 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND E/E COMPARTMENT FRAME CORRODED AT STATION Y200 BETWEEN LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006341996101000634WP 1996 10 10 GTIA96NK077 119951126A5320 ANGLE DOUG DC9 DC931 3022065WP BS 218 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND E/E COMPARTMENT FLOOR SUPPORT ANGLE WITH CORROSION AT STATION Y218 BETWEEN LONGERON 29R AND 29L. REPLACED DAMAGED ANGLE IAW SRM 51-01 PARA C. FABRICATED ANGLE IAW SRM 51-10-2, TREATED METAL IAW SRM 51-10-20. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006351996101000635WP 1996 10 10 GTIA96NK078 119951126A5321 FLOOR DOUG DC9 DC931 3022065WP BS 197 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND E/E COMPARTMENT PAX CABIN FLOOR PANEL WITH CORROSION AT Y197 AND X20. REPLACED SHEET IN FLOOR PANEL IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-70-2. (M) 2L72 4F A6WE 19961010006361996101000636WP 1996 10 10 GTIA96NK079 119951126A5320 BASE DOUG DC9 DC931 3022065WP BS 218 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, E/E COMPARTMENT ANTENNA MOUNTING BASE WITH CORROSION AT STATION Y218 BETWEEN LONGERON 30 AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006371996101000637WP 1996 10 10 GTIA96NK080 119951126A5313 LONGERON DOUG DC9 DC931 3022065WP BS 980-996 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y980 AND Y996. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006381996101000638WP 1996 10 10 GTIA96NK081 119951127A5320 SUPPORT DOUG DC9 DC931 3022065WP BS 590 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT WITH CORROSION AT Y590 BETWEEN LONGERON AND 26R AND 26L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006391996101000639WP 1996 10 10 GTIA96NK082 119951127A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 579-598 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION AND CRACKED BETWEEN Y579 AND Y598 AND BETWEEN LONGERONS 28L AND 27L. REPLACED DAMAGED INTERCOSTAL IAW SRM 51-01 PARA C. TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961010006401996101000640WP 1996 10 10 GTIA96NK083 119951127A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 579-598 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y579 AND Y598 AND BETWEEN LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-01 PARA C AND SRM 51-10-3. INSTALLED RIVETS IAW SRM 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961010006411996101000641WP 1996 10 10 GTIA96NK107 119951128A5320 DOOR FRAME DOUG DC9 DC931 3022065WP BS 427 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT Y427 AFT DOOR CUT OUT FRAME WITH CORROSION, AT ANCHOR NUTS ATTACHMENT POINTS BETWEEN LONGERON 25R AND 28R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01. (M) 2L72 4F A6WE 19961010006421996101000642WP 1996 10 10 GTIA96NK108 119951203A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 237-256 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN INTERCOSTAL WITH CORROSION BETWEEN Y237 TO Y256 CENTER SECTION, FOUND DURING FLOOR PANEL REMOVAL. REPAIRED CHANNEL SUPPORT IAW EO-COO-9-53-165-95. (M) 2L72 4F A6WE 19961010006431996101000643WP 1996 10 10 GTIA96NK109 119951203A5320 SUPPORT DOUG DC9 DC931 3022065WP CABIN CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN FORWARD LAVATORY FORWARD BULKHEAD BASE WITH CORROSION. REPLACED SUPPORTS OF FLOOR IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006441996101000644WP 1996 10 10 GTIA96NK110 119951204A5321 FLOOR DOUG DC9 DC931 3022065WP BS 200-210 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN BETWEEN Y200 TO Y210 AND FROM XX23 TO XX49 PANEL CORRODED. LOCATED UNDER FLOOR PANEL. REPLACED SHEET UNDER FLOOR PANEL IAW SRM 51-0 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006451996101000645WP 1996 10 10 GTIA96NK111 119951207A5321 FLOOR DOUG DC9 DC931 3022065WP BS 237 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND PAX CABIN AT Y237 TO X50 FLOOR OUTBOARD MEMBRANE CORRODED, FOUND DURING FORWARD TOILET FLOOR PANEL. REPLACED SHEET IAW SRM 51-01 PARA C. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006461996101000646WP 1996 10 10 GTIA96NK113 119951121A5315 FLOOR BEAM DOUG DC9 DC932 3022066WP BS 965.09 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM Y965.09 WITH CORROSION BETWEEN XO AND PLUS X58. REPAIRED FLOOR BEAM LOWER CHORD AT Y965.09 BETWEEN PLUS X6.7 TO PLUS X 18 AND BETWEEN PLUS 21.5 TO PLUS X535 IAW EO NR COO-9-53-138-95. (M) 2L72 4F A6WE 19961010006471996101000647WP 1996 10 10 GTIA96NK114 119951121A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 815 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y815 BETWEEN LONGERON 27 RT AND 28 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006481996101000648WP 1996 10 10 GTIA96NK115 119951121A5330 SKIN DOUG DC9 DC932 3022066WP BS 756-775 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH LIGHT CORROSION BETWEEN Y756 AND Y775, LONGERON 26 LEFT AND LONGERON 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19961010006491996101000649WP 1996 10 10 GTIA96NK116 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 775 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FILLING SUPPORT FLOOR PANEL WITH CORROSION IN Y775 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006501996101000650WP 1996 10 10 GTIA96NK117 119951106A5320 CHANNEL DOUG DC9 DC932 3022066WP BS 756-775 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL WITH CORROSION SPOTS BETWEEN Y756 AND Y775 ON LONGERON 26 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006511996101000651WP 1996 10 10 GTIA96NK118 119951106A5311 FRAME DOUG DC9 DC932 3022066WP BS 889 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y889 WITH CORROSION BETWEEN LONGERON 29 RIGHT AND 27 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006521996101000652WP 1996 10 10 GTIA96NK119 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 869 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 29 RIGHT AND FRAME Y869 WITH CORROSION. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006531996101000653WP 1996 10 10 GTIA96NK120 119951106A5311 FRAME DOUG DC9 DC932 3022066WP BS 935 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y935 WITH CORROSION BETWEEN LONGERON 25 LEFT AND 30 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006541996101000654WP 1996 10 10 GTIA96NK121 119951106A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 889 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y889 LONGERON 27 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 51-01, FIG 1. (M) 2L72 4F A6WE 19961010006551996101000655WP 1996 10 10 GTIA96NK122 119951106A5330 SKIN DOUG DC9 DC932 3022066WP BS 889-916 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH CORROSION BETWEEN Y889 AND Y916, LONGERON 28 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 53-04. AREA WITHIN LIMITS IAW SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19961010006561996101000656WP 1996 10 10 GTIA96NK123 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 889-965 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 LEFT WITH CORROSION IN SEVERAL PLACES BETWEEN Y889 AND Y965. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006571996101000657WP 1996 10 10 GTIA96NK124 119951106A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 756-889 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT CHANNEL FLOOR SUPPORT PANELS WITH CORROSION BETWEEN Y 756 AND Y 889, LONGERON 27 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006581996101000658WP 1996 10 10 GTIA96NK125 119951106A5311 FRAME DOUG DC9 DC932 3022066WP BS 980 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y980 WITH CORROSION BETWEEN LONGERON 23 LEFT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006591996101000659WP 1996 10 10 GTIA96NK126 119951106A5311 FRAME DOUG DC9 DC932 3022066WP BS 965 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT FRAME Y965 WITH CORROSION BETWEEN LONGERON 19 LEFT AND 23 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006601996101000660WP 1996 10 10 GTIA96NK127 119951106A5330 SKIN DOUG DC9 DC932 3022066WP BS 945-965 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN AND CHANNELS WITH CORROSION BETWEEN Y945 AND Y965 LONGERON 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1 AND 53-04 FIG 38. (m) 2L72 4F A6WE 19961010006611996101000661WP 1996 10 10 GTIA96NK128 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 945 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT ATTACH FITTINGS ON LONGERONS 25 RIGHT AND 26 RIGHT WITH CORROSION IN Y945. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006621996101000662WP 1996 10 10 GTIA96NK129 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 945-980 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 24 RIGHT WITH CORROSION BETWEEN Y945 AND Y980. REMOVED CORROSION AND TREATED METAL IAW 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006631996101000663WP 1996 10 10 GTIA96NK130 119951106A5320 BEAM DOUG DC9 DC932 3022066WP CARGO COMPT CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT HORIZONTAL BEAM WITH CORROSION BETWEEN LONGERON 22 RIGHT AND 23 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006641996101000664WP 1996 10 10 GTIA96NK131 119951104A5320 FITTING DOUG DC9 DC932 3022066WP BS 996 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT END FITTING, LONGERON 29 RIGHT WITH CRACK AND CORROSION IN Y996. REPLACED END FITTING IN LONGERON 20 RIGHT IAW SRM 51-01 PARA C AND 51-30-2, PART FABRICATED IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961010006651996101000665WP 1996 10 10 GTIA96NK132 119951106A5313 LONGERON DOUG DC9 DC932 3022066WP BS 965-980 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND AFT CARGO COMPARTMENT LONGERON 20, 21, 22 WITH CORROSION BETWEEN Y965 AND Y980 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006661996101000666WP 1996 10 10 GTIA96NK133 119951105A5311 FRAME DOUG DC9 DC932 3022066WP BS 503 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y503 WITH CORROSION BETWEEN LONGERON 28 RIGHT AND 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006671996101000667WP 1996 10 10 GTIA96NK134 119951106A5320 SUPPORT DOUG DC9 DC932 3022066WP BS 503 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CHANNEL WITH CORROSION BETWEEN Y503 AND Y522, LONGERON 21 RIGHT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961010006681996101000668WP 1996 10 10 GTIA96NK135 119951105A5313 LONGERON DOUG DC9 DC932 3022066WP BS 503-522 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 25 RIGHT WITH CORROSION BETWEEN Y503 AND Y522. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006691996101000669WP 1996 10 10 GTIA96NK136 119951105A5313 LONGERON DOUG DC9 DC932 3022066WP BS 484-510 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURIGN C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y484 AND Y510. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006701996101000670WP 1996 10 10 GTIA96NK137 119951105A5311 FRAME DOUG DC9 DC932 3022066WP BS 484 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y484 WITH CORROSION BETWEEN LONGERON 29 LEFT AND 29 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006711996101000671WP 1996 10 10 GTIA96NK138 119951105A5311 FRAME DOUG DC9 DC932 3022066WP BS 465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y465 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006721996101000672WP 1996 10 10 GTIA96NK139 119951116A5313 LONGERON DOUG DC9 DC932 3022066WP BS 359-389 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y359 AND Y389. REPLACED LONGERON 30 FROM Y356.7 TO Y415 IAW SRM 51-01, PARA C. INSTALLED TWO SPLICES IN LONGERON 30 FROM Y 356.7 TO Y415. INSTALLED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961010006731996101000673WP 1996 10 10 GTIA96NK140 119951105A5313 LONGERON DOUG DC9 DC932 3022066WP BS 446-465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y446 AND Y465. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961010006741996101000674WP 1996 10 10 GTIA96NK141 119951105A5311 FRAME DOUG DC9 DC932 3022066WP BS 446 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME Y446 WITH CORROSION BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW 53-01, FIG 1. (M) 2L72 4F A6WE 19961010007261996101000726WP 1996 10 10 GTIANK018 119951121A5313 LONGERON DOUG DC9 DC932 3022066WP BS 446-465 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DURING C-CHECK, FOUND THE FUSELAGE LONGERON 25 LEFT BETWEEN STATION Y446 TO Y465 CRACKED. REPAIRED THE LONGERON 25 IAW SRM 53-02 FIG 2A. (M) 2L72 4F A6WE 19961010008831996101000883SW 1996 10 10 CA960206101 119951229A622020057530D BOLT BELL 205 205A1 1181414SW LYC T53 T5313B 41549NE M/R HEAD SHEARED W K NONE O OTHER ININSP/MAINT 1 CA 239 LEO7506 (CAN)THE DRIVE LINK WAS BEING REMOVED TO REPLACE THE TRUNNION BEARING IN THE SWASHPLATE OUTER RING ASSEMBLY. THE BOLT HEAD SHEARED OFF UPON DISASSEMBLY. 1G71 4U4 U H1SW E17EA 19961010008901996101000890NM 1996 10 10 CA960212006 119951115A5280 ARM DHAV DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE RH NOSE GEAR BROKEN W K NONE O OTHER TXTAXI/GRND HDL 1 CA 120342 (CAN)AFTER ARRIVAL CREW NOTED RIGHT HAND NOSE GEAR DOOR ARM BROKEN AND RH NOSE TIRE SLICED. GEAR DOOR AND BOTH NOSE WHEEL ASSEMBLIES REPLACED. 2H72 4T4 TRTA13NM E20NE 19961010008911996101000891EU 1996 10 10 CA960212007 119951129A2910A71871451 TUBE ASSEMBLY FOKKERF28 F28MK1000 4990808EU LT STUB WING CHAFED W K NONE OJ OTHER WARNING INDICATION CRCRUISE 1 CA (CAN)AFTER TAKEOFF #2 SYSTEM HYDRAULIC QUANTITY DROPPED NOTICEABLY, OFFLOADED PUMPS BUT QUANTITY DROPPED TO ZERO. SUCTION LINE IN THE LH STUB WING CHAFED AND LEAKING. LINE REPLACED. 2L72 4F RTA20EU 19961010008951996101000895CE 1996 10 10 CA960212017 119951111A531226110292 BULKHEAD CESSNA CESSNA208 208B 2073701CE PWA PT6 PT6A114 52043NE UPPER FLANGE DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA 11887 17280 (CAN)BULKHEAD ON LEFT AND RIGHT HAND SIDE FOUND BENT IN THE LOWER FUSELAGE STRUCTURE UNDER THE FLOOR. ALL BULKHEADS BETWEEN STA 319 AND 237 SHOWS SIGNS OF DAMAGE. THE SUBMITER REPORTS PROBLEMS OF A SIMILAR NATURE WITH FOUR OTHER AIRCRAFT IN ITS FLEET. CESSNA CONTACTED AND A REPAIR SCHEME WAS ACCEPTED. SUBMITTER STATES THAT A LOT OF BULKY HEAVY CARGO IS CARRIED DURING ITS OPERATION. 1H71 3T3 T A37CE E4EA 19961010009021996101000902SO 1996 10 10 CA960212024 119951117A24341100717 ALTERNATOR DELCO 1100717 PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA DC SYS FAULTY W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CRCRUISE 1 CA 06931601 L411248 (CAN)INSPECTION REVEALED THE TWO ALTERNATORS TO BE FAULTY. ONE DID NOT FUNCTION AT ALL, AND THE OTHER ONLY VERY WEAKLY. BATTERY 6-35 DID NOT CHARGE FULLY AFTER LONG CHARGING HOURS. THE BATTERY PROBABLY WASNOT AT MAXIMUM CHARGE LEVEL FOR MANY FLIGHT HOURS, THUS CAUSING THE ALTERNATORS TO WORK AT MAXIMUM. WHEN THE FIRST ALTERNATOR FAILED THE SECOND FAILED SOON AFTER UNDER THE ADDITIONAL LOAD. REPLACED THE TWO ALTERNATORS AND BATTERY AND THE SYSTEM FUNCTIONED NORMALLY. 1L72 3O3 O 1A10 1E4 19961010009051996101000905GL 1996 10 10 CA960212027 219950804A7313 NOZZLE BELL 206 206L 1181522SW ALLSN 250C 250C20B 03013GL ENGINE CARBON BUILDUP W AB UNSCHED LANDING EMER. DESCENT OY OTHER ENGINE STOPPAGE CRCRUISE 1 CA 830999 (CAN)DURING FLIGHT, AT ABOUT 150' AGL, THE ENGINE FLAMED OUT AND THEN RELIT, HOWEVER THE ENGINE RPM ONLY REACH 30 PERCENT NG. THE PILOT CARRIED OUT AN AUTOROTATION. THE AIRCRAFT WAS FITTED WITH FLOAT GEAR.DURING THE FLARE AND RUN-ON LANDING, THE TAIL SKID CONTACTED THE GROUND AND THE MAIN ROTOR BLADES SEVERED THE TAIL ROTOR DRIVE SHAFT AND DAMAGED THE TAIL BOOM. THE ENGINE WAS STILL RUNNING AT 30 PERCENT NG WHEN THE AIRCRAFT CAME TO REST. ON SITE INVESTIGATION REVEALED NO APPARENT PROBLEMS EXCEPT THAT THE NOZZLE HAD SIGNIFICANT CARBON BUILD UP. THE FUEL WAS ANALYZED AND THE ENGINE WAS SENT FOR DEPOT LEVEL INSPECTION, WITH NO PROBLEMS FOUND. 1G71 3U3 U H2SW E4CE 19961024000031996102400003CE 1996 10 24 96ZZZX5246 119951227A3710442CW PUMP AIRBORNE CESSNA414 414A 2075907CE LT VACUUM PUMP SHAFT SHEARED A CWNAK NONE O OTHER ININSP/MAINT 1 WP09414RW365 48610 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1L72 3O A7CE 19961024000061996102400006CE 1996 10 24 96ZZZX5249 119950921A3710442CW PUMP AIRBORNE CESSNA414 414A 2075907CE RT VACUUM PUMP SHAFT SHEARED A CWNAK NONE O OTHER ININSP/MAINT 1 WP09414RW561 42161 414A0295 FOLLOWING PUMP REMOVAL FOR FAILURE, FOUND DRIVE SHAFT SHEARED. THIS IS A VACUUM TYPE SYSTEM. 1L72 3O A7CE 19961024000241996102400024SO 1996 10 24 96ZZZX5267 119950703A32314A11364001 ROD ASSY EMB 110 EMB110P1 3260122SO NLG DOOR LINK DETACHED A PIVAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP13216EB 110447 AFTER SELECTING GEAR, GEAR UNSAFE LIGHT REMAINED ON. INSPECTION REVEALED NOSE GEAR DOOR LINKAGE ROD END DETACHED FROM BELLCRANK BALL JOINT. INSPECTED ROD END AND BALL JOINT. NO DEFECTS NOTED. PERFORMED GEAR RETRACTION TEST THROUGH 10 FAULT FREE CYCLES. 1L72 4T A21SO 19961024002561996102400256WP 1996 10 24 RRXA95004 119950830A5330 SKIN DOUG DC8 DC862F 3021972WP BS 1200-1210 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15997CF 46154 CORROSION ON SKIN AND SURROUNDING WINDOW PLUG LAND ON LT AFT TYPE 1 EXIT. REMOVED CORROSION BEYOND LIMITS. FABRICATED AND INSTALLED A REPAIR DOUBLER TO WINDOW PLUG LAND AND SKIN IAW COTNEY ENGINEERING ORDER SKA 95148-2. 2L74 4F 4A25 19961024002571996102400257WP 1996 10 24 RRXA95005 119950830A5312 BULKHEAD DOUBLER DOUG DC8 DC862F 3021972WP BS 680-683 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15997CF 46154 CORROSION ON FRAME AND BULKHEAD AT Y= 680 TO 683 BETWEEN LONGERONS L35L TO L35R. REMOVED FRAME SECTION, SPLICE AND DOUBLERS. FABRICATED AND INSTALLED REPAIR ANGLES TO FRAME AND REPAIR DOUBLER TO BULKHEAD IAW COTNEY ENGINEERING ORDER SKA 95148-3 AND SRM 51-1-8. 2L74 4F 4A25 19961024002581996102400258WP 1996 10 24 RRXA95006 119951230A5330 SKIN DOUG DC8 DC873F 302199FWP BS 25-35 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15791FT 46045 INNER SKIN CORROSION AT Y= 25 AND Y= 35 BETWEEN LONGERONS 33 AND 36. REPAIRED SKIN DAMAGE BY DOUBLER REPAIR IAW SKA 95251-3 AND TREATED AREA IAW SRM 51-1-8. 2L74 4F RT4A25 19961024002591996102400259WP 1996 10 24 RRXA95008 119951230A5330 SKIN DOUG DC8 DC873F 302199FWP BS 1600-1620 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15791FT 46045 SKIN LOWER AFT BELLY AT Y=1600 TO 1620 AND LONGERON 31R. REPAIRED DAMAGED SKIN BY DOUBLER REPAIR IAW SKA 95251-4 SHEET 1 AND 2, TREATED AREA IAW SRM 51-1-8. 2L74 4F RT4A25 19961024002601996102400260WP 1996 10 24 RRXA95009 119951230A5320 DOUBLER DOUG DC8 DC873F 302199FWP BS 12 CORRODED A RRXAK NONE O OTHER ININSP/MAINT 1 WP15791FT 46045 FINGER DOUBLER AT LONGERON 31R AND Y=12 CORRODED PAST LIMITATIONS IAW 53-2-0. REPAIRED FINGER DOUBLER IAW SKA 95251-5 AND TREATED AREA IAW SRM 58-1-8. 2L74 4F RT4A25 19961024007761996102400776WP 1996 10 24 GTIA96NK084 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 541 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FCC FRAME WITH CORROSION ON LOWER FLANGE AT Y541 BETWEEN LONGERONS 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3 PG 20. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961024007771996102400777WP 1996 10 24 GTIA96NK085 119951127A5330 SKIN DOUG DC9 DC931 3022065WP BS 541-560 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FWD CARGO COMPT INTERNAL SKIN WITH CORROSION BETWEEN Y541 AND Y560 AND FROM LONGERON 30 TO 29L. REMOVED CORROSION IN FWD CARGO COMPT INTERNAL SKIN BETWEEN Y541 AND Y560 AND FROM LONGERON 30 TO 29L, MATERIAL TREATED IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-04 FIG 38. (M) 2L72 4F A6WE 19961024007781996102400778WP 1996 10 24 GTIA96NK086 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 503 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURNIG C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y503 BETWEEN LONGERON 29L TO 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961024007791996102400779WP 1996 10 24 GTIA96NK087 119951127A5320 JAMB DOUG DC9 DC931 3022065WP BS 439-362.5 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INNER SKIN OF DOOR JAMB DENTED, CRACKED AND CORRODED BETWEEN Y439 AND Y362.5 FROM LONGERON 29R TO 24R. REPLACED SKIN SECTION IN LOWER DOOR FRAME SECTION OF FWD CARGO COMPT BETWEEN Y439 TO Y362.5, LONGERON 29 AND 24R IAW SRM 51-01 PARA C. INSTALLED RIVETS IAW SRM 51-30-2. FABRICATED MATERIAL IAW SRM 51-10-2. (M) 2L72 4F A6WE 19961024007801996102400780WP 1996 10 24 GTIA96NK088 119951127A5320 JAMB DOUG DC9 DC931 3022065WP BS 427-370 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LOWER DOOR CUT OUT, JAMB WITH CORROSION BETWEEN Y427 AND Y370. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007811996102400781WP 1996 10 24 GTIA96NK089 119951127A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 362.5-218 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR CHANNEL WITH CORROSION BETWEEN Y362.5 AND Y218 AND BETWEEN LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1, BETWEEN Y362.5 AND Y218. REPLACED DAMAGE FLOOR CHANNEL SECTIONS IAW SRM 51-01 PARA C BETWEEN Y363 AND Y304. INSTALLED RIVETS AND ANCHOR NUTS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007821996102400782WP 1996 10 24 GTIA96NK090 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 332 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y332 BETWEEN LONGERON 29R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961024007831996102400783WP 1996 10 24 GTIA96NK091 119951127A5330 SKIN DOUG DC9 DC931 3022065WP BS 332-351 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN AND DOUBLER WITH CORROSION BETWEEN Y332 AND Y351 FROM LONGERON 24R AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW 53-04, FIG 38. (M) 2L72 4F A6WE 19961024007841996102400784WP 1996 10 24 GTIA96NK092 119951127A5313 LONGERON DOUG DC9 DC931 3022065WP BS 351-332 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 29R WITH CORROSION BETWEEN Y351 AND Y332. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1, SHEET 3. (M) 2L72 4F A6WE 19961024007851996102400785WP 1996 10 24 GTIA96NK093 119951127A5320 INTERCOSTAL DOUG DC9 DC931 3022065WP BS 332 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL WITH CORROSION BETWEEN Y351 AND Y332 AT LONGERON 29R. REPLACED INTERCOSTAL IAW SRM 51-01, PARA C. FABRICATED PART IAW SRM 51-10-2. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007861996102400786WP 1996 10 24 GTIA96NK094 119951127A5320 SUPPORT DOUG DC9 DC931 3022065WP BS 362.5 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR SUPPORT CRACKED AT 7362.5 BETWEEN LONGERON 28R AND 27R. REPLACED FLOOR SUPPORT IAW RM 51-01 PARA C. FABRICATED PART IAW SRM 51-10-2. REPLACED HI-LOCKS IAW SRM 51-30-5. (M) 2L72 4F A6WE 19961024007871996102400787WP 1996 10 24 GTIA96NK095 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 389 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y389 BETWEEN 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITH IN LIMITS IAW SRM 53-01 FIG 1. (M) 2L72 4F A6WE 19961024007881996102400788WP 1996 10 24 GTIA96NK096 119951127A5330 SKIN DOUG DC9 DC931 3022065WP BS 362.5 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION AND SCRATCHES BETWEEN Y362.5 AND Y427 FROM LONGERON 29L TO 29R. REMOVED DOUBLER, CORROSION AND SCRATCHES AND TREATED METAL FROM Y362.5 AND Y427, BETWEEN LONGERONS 29L TO 29R IAW 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. REINSTALLED DOUBLERS AND RIVET IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007891996102400789WP 1996 10 24 GTIA96NK097 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 408 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION AND CRACKED ON LOWER FLANGE AT Y408 BETWEEN LONGERON 30 AND 25L. REPAIRED FRAME IAW SRM 53-03, FIG 2A, SHEET 1 OF 5 AT STATION Y408 FROM LONGERON 25L TO 30. (M) 2L72 4F A6WE 19961024007901996102400790WP 1996 10 24 GTIA96NK098 119951127A5313 LONGERON DOUG DC9 DC931 3022065WP BS 389-465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 29L WITH CORROSION AND CRACKED BETWEEN Y389 AND Y465. REPLACED 29L LONGERON SECTION FROM Y389 TO Y465 IAW EO NR 000-9-53-172-95. (M) 2L72 4F A6WE 19961024007911996102400791WP 1996 10 24 GTIA96NK099 119951127A5320 ANGLE DOUG DC9 DC931 3022065WP BS 439 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT ANGLE WITH CORROSION AT Y439 BETWEEN LONGERON 29L AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007921996102400792WP 1996 10 24 GTIA96NK100 119951127A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 598.5 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FLOOR CHANNEL WITH CORROSION BETWEEN Y439 AND Y598.5 FROM LONGERON 28R AND 27R. REMOVED CORROSION AND TREATED METAL IN CHANNEL SECTION BETWEEN Y470 AND Y598.5 LONGERONS 27 AND 28R IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED DAMAGE SECTIONS BETWEEN Y433 AND Y470 IAW SRM 51-01 PARA C. INSTALLED RIVETS AND ANCHOR NUTS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007931996102400793WP 1996 10 24 GTIA96NK101 119951127A5330 SKIN DOUG DC9 DC931 3022065WP BS 446-427 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION BETWEEN Y446 AND Y427 FROM LONGERON 28R AND 29L. REMOVED CORROSION AND TREATED MATERIAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-01 FIG 1. REPLACED RIVETS IAW SRM 51-30-2. (M) 2L72 4F A6WE 19961024007941996102400794WP 1996 10 24 GTIA96NK102 119951127A5330 SKIN DOUG DC9 DC931 3022065WP BS 465-446 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DUIRNG C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL DOUBLER AND SKIN WITH CORROSION BETWEEN Y465 AND Y446 FROM LONGERON 29R TO 30. REPAIRED LOWER SKIN SECTION AND REPLACED DOUBLER BETWEEN Y432 AND Y465, LONGERONS 28L AND 29R IAW SRM 53-04, FIG 44 SHEET 1. (M) 2L72 4F A6WE 19961024007951996102400795WP 1996 10 24 GTIA96NK103 119951127A5320 CHANNEL DOUG DC9 DC931 3022065WP BS 484-465 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD COMPARTMENT CHANNEL WITH CORROSION FROM Y484 TO Y465 BETWEEN LONGERON 30 AND 29L. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961024007961996102400796WP 1996 10 24 GTIA96NK104 119951127A5311 FRAME DOUG DC9 DC931 3022065WP BS 484 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT FRAME WITH CORROSION ON LOWER FLANGE AT Y484 BETWEEN LONGERON 30 AND 29R. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-01, FIG 1. (M) 2L72 4F A6WE 19961024007971996102400797WP 1996 10 24 GTIA96NK105 119951127A5320 SKIN DOUG DC9 DC931 3022065WP BS 503 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT INTERNAL SKIN WITH CORROSION BETWEEN LONGERON 29L AND 29R FROM Y484 TO Y503. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. REPLACED RIVETS IAW SRM 51-30-2. AREA WITHIN LIMITS IAW SRM 53-04, FIG 38 TABLE A. (M) 2L72 4F A6WE 19961024007981996102400798WP 1996 10 24 GTIA96NK106 119951128A5312 BULKHEAD ANGLE DOUG DC9 DC931 3022065WP BS 218 CORRODED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23934ML 47526 DURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT Y218 FORWARD BULKHEAD LOWER ANGLE WITH CORROSION BETWEEN LONGERON 25L AND 25R. REPAIRED ANGLE IAW SRM53-01, FIG 2 SHEET 4. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREA WITHIN LIMITS IAW SRM 53-0, FIG 1. (M) 2L72 4F A6WE 19961024009751996102400975EU 1996 10 24 RAIA950410 319950407A61408659566 BETA SWITCH BAG JETSTMJETSTM3201 1500217EU RT ENGINE FAILED A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03343TE6408 6408 955 STL - FLT 7422 - RIGHT BETA LIGHT CAME ON. MAINTENANCE REPLACED RIGHT BETA LIGHT SWITCH. GROUND RUNS AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19961024009761996102400976EU 1996 10 24 RAIA950406 119950406A243523079009 STARTER/GEN BAG JETSTMJETSTM3201 1500217EU LT ENGINE FAILED A RAIAO OTHER JH WARNING INDICATION ELECT. POWER LOSS-50 PC CLCLIMB 1 CE03341TE 950 STL - FLT 7456 - LEFT ENGINE STARTER/GENERATOR FELL OF LINE. MAINTENANCE REPLACED LEFT STARTER/GENERATOR. GROUND RUN TEST REVEALED NO FAULTS. (M) 2L72 4T RTA56EU 19961024009771996102400977EU 1996 10 24 RAIA950405 119950404A521091SE16 SWITCH BAG JETSTMJETSTM3201 1500217EU PAX DOOR OUT OF ADJUST A RAIAD RETURN TO BLOCK J WARNING INDICATION CRCRUISE 1 CE03339TE6347 935 STL - FLT 7457 - PASSENGER DOOR LIGHT ILLUMINATED. MAINTENANCE ADJUSTED PASSENGER DOOR HANDLE MICROSWITCH. SYSTEM CHECK GOOD. (M) 2L72 4T RTA56EU 19961024009781996102400978SO 1996 10 24 RAIA950417 119950410A3230922FS2AGN2735 PROX SWITCH EMB 120 EMB120RT SO LANDING GEAR INOP A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03131AM 120158 STL - FLT 7148 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE DEFERRED LANDING GEAR HANDLE AS PER MEL 32031-1, CAT A. (M) 2L72 4T RTA31SO 19961024009791996102400979SO 1996 10 24 RAIA950404 119950402A33503071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03125AM19173 120017 STL - FLT 7514 - EMERGENCY LIGHT OVER ROW 8 IS INOP. MAINTENANCE REPLACED LIGHT BULB FOR EMERGENCY LIGHT. (M) 2L72 4T RTA31SO 19961024009801996102400980EU 1996 10 24 RAIA950402 119950402A3260E0052R10B6SNE CONNECTOR AEROSPATR72 ATR72202 8680940EU NLG DIRTY A RAIAO OTHER N FALSE WARNING CLCLIMB 1 CE03722TE8087 220 STL - FLT 7398 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH WHEN SELECTED UP. MAINTENANCE CLEANED NOSE UPLOCK BOX CANNON PLUG. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2H72 4T RTA53EU 19961024009811996102400981EU 1996 10 24 RAIA950346 119950331A3240215221 BRAKE SYSTEM BAG JETSTMJETSTM3201 1500217EU LT MLG REQ'D SERVICE A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03423AM8049 858 STL - LEFT BRAKES ARE MUSHY AND WEAK. MAINTENANCE BLED BRAKE SYSTEM. TAXI CHECK REVEALED NORMAL OPERATION AND LEAK CHECK GOOD. (M) 2L72 4T RTA56EU 19961024009821996102400982EU 1996 10 24 RAIA950401 119950402A32609EN1C11HB2BB2 SWITCH BAG JETSTMJETSTM3201 1500217EU NLG LACK OF LUBE A RAIAD RETURN TO BLOCK N FALSE WARNING CLCLIMB 1 CE03422AM13093 856 STL - FLT 7034 - NOSE GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER GEAR SELECTED UP. MAINTENANCE CLEANED AND LUBED NOSE GEAR UPLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19961024009831996102400983EU 1996 10 24 UF6A950405 119950412A3350362624 LIGHT STRIP BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31851AW8808 2020 FLT 5093 - ORD - FORWARD EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED FORWARD EMERGENCY LIGHT STRIP. (M) 2L72 4T RTA27NM 19961024009841996102400984EU 1996 10 24 RAIA950414 119950407A3350311701 BATTERY BAG JETSTMJETSTM3201 1500217EU AFT CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03871JX5708 871 STL - AFT EMERGENCY BATTERY IS LOW IN VOLTS. MAINTENANCE REPLACED AFT EMERGENCY BATTERY. (M) 2L72 4T RTA56EU 19961024009851996102400985EU 1996 10 24 RAIA950413 119950407A3350311701 BATTERY BAG JETSTMJETSTM3201 1500217EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03871JX1817 871 STL - FORWARD EMERGENCY LIGHTING BATTERY IS LOW. MAINTENANCE REPLACED FORWARD EMERGENCY LIGHTING BATTERY. (M) 2L72 4T RTA56EU 19961024009861996102400986EU 1996 10 24 RAIA950418 119950408A3350OL60424P BULB AEROSPATR42 ATR42300 8680920EU PAX DOOR FAILED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03423TE13886 119 STL - EMERGENCY LIGHT IN THE CABIN DOOR DOES NOT WORK. MAINTENANCE REPLACED EMERGENCY LIGHT BULB. (M) 2H72 4T RTA53EU 19961024009871996102400987EU 1996 10 24 RAIA950416 119950410A261251216090 FIRE LOOP AEROSPATR42 ATR42300 8680920EU RT ENGINE FAILED A RAIAO OTHER N FALSE WARNING CRCRUISE 1 CE03421TE9883 102 MEM - FLT 7149 - RIGHT FIRE DETECTION WARNING INFLIGHT. CREW FIRED BOTH FIRE BOTTLES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH ENGINE FIRE BOTTLES AND REPLACED RIGHT FIRE DETECTION LOOP. TEST REVEALED NORMAL OPERATION. (M) 2H72 4T RTA53EU 19961024009881996102400988EU 1996 10 24 RAIA950415 119950407A33503011151 POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03421TE5018 102 STL - SEVERAL EMERGENCY LIGHTS IN THE CABIN ARE INOP. MAINTENANCE REPLACED EMERGENCY LIGHTING POWER SUPPLIES. (M) 2H72 4T RTA53EU 19961024009891996102400989EU 1996 10 24 RAIA950412 119950407A32609EN1C11HB2BB2 UPLOCK SWITCH BAG JETSTMJETSTM3201 1500217EU NLG LACK OF LUBE A RAIAO OTHER J WARNING INDICATION CLCLIMB 1 CE03422AM 856 STL - FLT 7364 - NOSE GEAR UPLOCK LIGHT CAME ON. MAINTENANCE CLEANED AND LUBED NOSE UPLOCK SWITCH. GEAR SWINGS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19961024009901996102400990WP 1996 10 24 RAIA950411 219950407A75308961153 GASKET BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UA 01514WP LT ENGINE LEAKING A RAIACD ABORTED TAKEOFF RETURN TO BLOCK O OTHER TOTAKEOFF 1 CE03422AM7616 856 66179 STL - FLT 7302 - LEFT ENGINE PRODUCED LOW POWER. MAINTENANCE REPLACED LEFT ENGINE BLEED GASKETS. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T4 TRTA56EU E4WE 19961024009911996102400991EU 1996 10 24 RAIA950403 119950402A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU LT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03436AM8631 8631 891 STL - FLT 7316 - LEFT ENGINE TEMPERATURE LIMITED AND TORQUE FLUCTUATED. MAINTENANCE ADJUSTED LEFT ENGINE TORQUE SIGNAL CONDITIONER AND CLEANED LEFT ENGINE TORQUE STRAIN GAUGE PLUG OF OIL RESIDUE. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19961101000221996110100022CE 1996 11 1 CA960311009 119951130A2720S16751 TORQUE TUBE CESSNA172 172E 2072412CE CONT O300 O300D 17022SO RUDDER BAR CORRODED SADDLE W K NONE O OTHER ININSP/MAINT 1 CA 4884 27692D2D (CAN)DURING A 100 HOUR INSPECTION WHITE RESIDUE WAS NOTED ON THE RIGHT HAND RUDDER BAR SADDLE. UPON REMOVAL THE SADDLE HALVES WERE FOUND TO BE CORRODED. THE SUPPORTING STRUCTURE, FIG. 31 #34 CESSNA 172 PAR TS MANUAL, WAS ALSO FOUND CORRODED. 1H71 3O3 ONT3A12 E253 19961101000231996110100023SO 1996 11 1 CA960311010 119951218A32112082900 STUD PIPER PIPER PA24 PA24250 7102404SO LYC O540 O540A1C5 41532EA MLG BRACE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2248 L353740 (CAN)WHILE COMPLYING WITH AD 95-20-09, BOTH SIDE BRACE STUDS WERE FOUND CRACKED. 1L71 3O3 O 1A15 E295 19961101009131996110100913EU 1996 11 1 RAIA950409 119950409A771231024766 TQ SIGNAL COND BAG JETSTMJETSTM3201 1500217EU RT ENGINE OUT OF ADJUST A RAIACD ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TOTAKEOFF 1 CE03423AM9090 9090 858 STL - FLT 7058 - RIGHT ENGINE TORQUE DROPPED TO 65 PERCENT. MAINTENANCE ADJUSTED RIGHT TORQUE SIGNAL CONDITIONER. GROUND RUNS REVEALED NORMAL OPERATION. (M) 2L72 4T RTA56EU 19961101009141996110100914EU 1996 11 1 RAIA950408 119950404A33503011151 POWER SUPPLY AEROSPATR42 ATR42300 8680920EU CABIN DISCHARGED A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03425TE13314 125 STL - MIDDLE SECTION OF FLOOR ESCAPE PATH LIGHTING AND FRONT AND BACK EMERGENCY EXIT ARE INOP. MAINTENANCE REPLACED BATTERY POWER SUPPLY. (M) 2H72 4T RTA53EU 19961101009151996110100915EU 1996 11 1 UF6A950403 119950411A27511ENN14 SWITCH BAG ATP ATP EU TE FLAPS DIRTY A UF6AA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL31854AW7811 2028 FLT 5112 - SBN - ON CLIMB FLAP CENTRAL WARNING PANEL ILLUMINATED. MAINTENANCE CLEANED BOTH FLAP SIGNALING UNIT SWITCHES CG17, CG18. (M) 2L72 4T RTA27NM 19961101009161996110100916 1996 11 1 UF6A950402 319950411A6112 PROP DE-ICE BAG ATP ATP EU NR 2 PROP FAILED A UF6AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31855AW2274 2029 FLT 5069 - ORD - DE-ICE CENTRAL WARNING PANEL ACTIVATED AFTER TAKEOFF FOUND BURNED SPOT ON ONE PROPELLER BLADE, P/N 7863504. MAINTENANCE REPLACED THE NR 1 BLADE NR 2 SIDE. (M) 2L72 4T RTA27NM 19961101009171996110100917EU 1996 11 1 UF6A950401 119950405A61201SE112 SWITCH BAG ATP ATP EU NR 2 ENGINE FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31858AW6287 2035 FLT 777 - SBN - THE AUTOFEATHER SYSTEM WOULD NOT TEST. MAINTENANCE ADJUSTED CONDITION LEVER MICROSWITCH NR 2 ENGINE. (M) 2L72 4T RTA27NM 19961101009181996110100918EU 1996 11 1 UF6A950404 119950412A3350362624 LIGHT BAG ATP ATP EU CABIN FAILED A UF6AK NONE L NO TEST ININSP/MAINT 1 GL31856AW7302 2032 FLT 5017 - ORD - EMERGENCY LIGHTS INOP, ROW 16. MAINTENANCE REPLACED AFT TWO LIGHT STRIPS. (M) 2L72 4T RTA27NM 19961107002341996110700234EA 1996 11 7 CA960325007 119951215A29111356583314 ACCUMULATOR PARKERHANFIN DHAV DHC6 DHC6300 EA PWA HYDRAULIC FAILED W K NONE O OTHER ININSP/MAINT 1 CA 95 2360 (CAN)ACCUMULATOR WOULD NOT HOLD PRESSURE. FOLLOW-UP NOTED THAT FLUID WAS CONTAMINATED WITH BLACK DIRT. 1H72 3T A9EA 19961114002571996111400257EA 1996 11 14 CA960408501 119951219A5311C2FS1503A FRAME DHAV DHAV DHC2 DHC2MK1 2800102EA LOWER TUBE CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 19001 (CAN)AFTER INSPECTING THE TUBULAR STRUCTURE PER SB 2/49, MANY TUBES FOUND CORRODED. ALSO INSPECTION EXTENDED TO ALL TUBULAR 4130 PARTS AND ONE FRONT DIAGONAL STRUT P/N C2FS210 FOUND CORRODED. 1H71 3R A806 19961114005561996111400556EU 1996 11 14 ABXA9600661 219951105A7240 HOT SECTION NIHON YS11 YS11 6310406WP RROYCEDART DART54210J 54522EU ENGINE OVERHEATED A ABXAEA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL23914AX 2056 21165 AT APPROXIMATELY 700 FEET, ENGINE OVERHEAT INDICATION. ENGINE WAS SECURED IAW EMERGENCY PROCEDURES AND RETURNED TO ROA. PERFORMED HOT SECTION INSPECTION IAW ABX TASK NR 03720. 2L72 4T4 T A1PC E5EU 19961114006141996111400614SW 1996 11 14 CA960418005 119951207A2810 CAP O-RING MOONEYM20 M20K 5870220SW CONT O360 TSIO360GB 17025SO FUEL CAP MECH OUT OF ADJUST W K NONE O OTHER ININSP/MAINT 1 CA 893 309411 (CAN)WATER FOUND IN THE RIGHT HAND FUEL TANK. SUBMITTER BELIEVES THAT RAIN WATER FOUND ITS WAY PAST THE FUEL CAP O-RING DUE TO AN OUT OF ADJUSTMENT IN THE FUEL CAP CENTRE LOCKING MECHANISM. 1L71 3O3 O 2A3 E9CE 19961127000301996112700030GL 1996 11 27 CA960514105 219950510A72306890550 ROTORS BELL 47 47G4 1181030SW ALLSN 250C 250C20B 03013GL 4TH & 5TH STAGESERODED W K NONE O OTHER ININSP/MAINT 1 CA 9304 557 CAE821137 (CAN) HEAVY EROSION OF 4TH AND 5TH STAGE ROTORS AND UNDERCUTTING ON 4TH AND 5TH STAGE STATOR VANES. CORROSION OF COMPRESSOR SCROLL. 1G71 3O3 U 2H3 E4CE 19961127000571996112700057EU 1996 11 27 CA960522003 119951101A3213200556209 TORQUE LINK 200427009 FOKKERF28 F28MK1000 4990808EU LT MLG BROKEN W A K NONE O OTHER LDLANDING 1 CA 4003744131 XC88988 (CAN)ON LANDING ROLL CREW FELT A HEAVY SHIMMY AND VIBRATION FROM THE LANDING GEAR. ON FINAL ROLL OUT, THE AIRCRAFT SETTLED LOWER ON THE L/H SIDE, HOWEVER, DIRECTIONAL CONTROL WAS MAINTAINED AND THE AIRCRAF T CAME TO A STOP IN THE CENTRE OF THE RUNWAY. THE L/H MLG WHEEL ASSEMBLIES AND BRAKE ASSEMBLIES HAD SEPARATED FROM THE STRUT. THE WHEEL ASSEMBLIES HAD IMPACTED THE L/H INBOARD FLAP - TWO LOCATIONS - CAUSING SUBSTANTIAL DAMAGE, AND ON AIRCRAFT STOPPING IMPACTED THE L/H OUTBOARD FLAP BRINGING THE WHEELS TO A HALT. 2L72 4F RTA20EU 19961212005141996121200514NM 1996 12 12 CA960311104 119950823A27221U11501 ACTUATOR DOWTY 1U11501 BOEING737 737296 1384486NM PWA JT8 JT8D9A 52048NE RUDDER INTERNAL LEAK W O OTHER L NO TEST ININSP/MAINT 1 CA 38318 0751 707405 (CAN) DURING HYDRAULIC SYSTEM INTERNAL LEAKAGE CHECK THE STANDBY SYSTEM TEST FAILED. DISPLACEMENT OF INPUT CRANK TO FULL AFT OR INDICATION IS A CURRENT INCREASE PROPORTIONAL TO ACTUATOR LEAKAGE. STANDBY ACTUATOR REPLACED. ON DISMANTLE CORROSION WAS FOUND AT PRESSURE INPUT FITTING CONNECTION, BEYOND ECONOMICAL REPAIR, PISTON SCORED, NEEDS RECHROMING AND STATIC SEALS BEGINNING TO DETERIORATE. 2L72 4F4 FRTA16WE E2EA 19961218000181996121800018GL 1996 12 18 CA960212008 319951223A6111 BLADE PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA HARTZLHCE3Y HCE3YR2A GL PROP #3 TIP BENT W K NONE C F.O.D. ININSP/MAINT 1 CA 936 L593461A DJ8147A (CAN) PROPELLER BLADE DAMAGE NOTICED WHILE AIRCRAFT WAS UNDERGOING MAINTENANCE. SUSPECT CAUSE WAS GROUND DEBRIS CONTACT DURING TAXI. 1L72 3O3 O A20SO E14EA 5 CP33EA 19961219004691996121900469NM 1996 12 19 DL72S954639 119951207A5754651622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27489DA 21019 RIBS MARKED NR 4 AND NR 9 CRACKED. REPAIRED PER M/M 57-54-0 FOR NR 7 L/E SLAT AT SHOP INSPECTION. 2L73 4F A3WE 19961219004701996121900470NM 1996 12 19 DL72S954640 119951207A5754651622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27489DA 21019 RIBS MARKED NR 17 AND NR 18 CRACKED. REPAIRED PER M/M 57-54-0 FOR L/E SLAT NR 7 AT SHOP INSPECTION. 2L73 4F A3WE 19961219004711996121900471NM 1996 12 19 DL72S954641 119951207A575465622374 RIB BOEING727 727232 1384082NM NR 7 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27489DA 21019 RIB MARKED NR 16 CRACKED. REPAIRED PER M/M 57-54-0 FOR NR 7 L/E SLAT DURING SHOP INSPECTION. 2L73 4F A3WE 19961219004721996121900472NM 1996 12 19 DL767954642 119951207A2560 BATTERY BOEING767 767232 1385132NM RT SLIDE DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27113DA 22225 SQUIB TEST 1 THE LEFT LIGHT DOES NOT COME ON FOR SLIDE. SQUIB TEST 2 THE RIGHT LIGHT DOES NOT COME ON FOR SPOLILER. REPLACED RIGHT HAND OVER WING SLIDE BATTERY ASSEMBLY. SYSTEM SQUIB TEST CHECKS AS PER M/M. . 2L72 4F RTA1NM 19961219004731996121900473NM 1996 12 19 DL73S954643 119951207A2910 HYD LINE BACH6P026300BOEING737 737232 1384475NM NLG BROKEN A DALAO OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 SO27318DL 23090 SYS A-HYD QTY LOSS ON APPROACH. FOUND HYD LINE BROKEN AT B-NUT ON NOSE GEAR ACTUATING CYLINDER. INSTALLED TEMP LINE CHANGED A-SYS FILTERS PRESS AND CASE DRAIN, LEAK CHKS OK. 2L72 4F RTA16WE 19961219004741996121900474NM 1996 12 19 DL72S954644 119951208A5210 PASSENGER DOOR BOEING727 727232 1384082NM FWD ENTRY BENT A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27535DA 22048 AC LOG ITEM Z60966002 RT CORNER OF FORWARD ENTRY DOOR IS BENT UP. REPAIRED PER MM 52-11-01 FIG 804. 2L73 4F A3WE 19961219004751996121900475NM 1996 12 19 DL72S954645 119951208A3350S106 BATTERY BOEING727 727232 1384082NM CABIN DISCHARGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27545DA 22494 EMERGENCY EXIT LIGHTS OVER R-1 DOOR ARE INOP. INSTALLED NEW BATTERIES, CKS GOOD. 2L73 4F A3WE 19961219004761996121900476WP 1996 12 19 DLL15954649 119951017A57531529517114 SKIN LKHEED1011 10113853 5265020WP RT TE FLAP VANE WORN A DALAK NONE O OTHER ININSP/MAINT 1 SO27755DL 193Y1184 NR 3 RT FLAP VANE UPPER SKIN HAD A WORN AND SCRATCHED SPOT. REPLACED SKIN SECTION PER SRM 57-53-00. 2L73 4F A23WE 19961219004771996121900477NM 1996 12 19 DL757954651 119951208A3350 POWER SUPPLY BPS73 BOEING757 757232 1384965NM CABIN INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27668DN 10605 25141 ON LAYOVER, L-1 AND R-1 DOOR EMERGENCY EXIT LIGHS FAIL TO TEST. REPLACED POWER SUPPLY, OPERATION NORMAL. 2L72 4F RTA2NM 19961219004781996121900478NM 1996 12 19 DL72S954653 119951208A5320 WEB BOEING727 727232 1384082NM BS 1223 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27519DA 21470 A .25 INCH CRACK LT LWR TORQUE BOX VERTICAL WEB STA 1223 AT TOP ROW OF RIVETS. ALSO, .25 INCH CRACK IN LIGHTENING HOLE BELOW THE TOP ROW OF RIVETS. REPAIRED PER MM 53-11-0. 2L73 4F A3WE 19961219004791996121900479NM 1996 12 19 DLM88954654 119951209A32105935347503 PISTON DOUG MD88 MD88 3023688NM LT MLG CRACKED A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27985DL 53312 WHILE PERFORMING ERA 335832-14, FOUND LEFT MAIN GEAR PISTON CRACKED O/B AND I/B LUG AT TORQUE LINK (S/N MALSS019). 2L72 4F RTA6WE 19961219004801996121900480 1996 12 19 DL73S954655 419951208A2565 SLIDE 1061323184 BOEING737 737232 1384475NM L1 DOOR LOW PRESSURE A DALAK NONE O OTHER TXTAXI/GRND HDL 1 SO27307DL 0028 23079 L1 DOOR SLIDE PRESSURE LOW PILOT REPORT. REPLACED DOOR SLIDE. 2L72 4F RTA16WE 19961219004811996121900481NM 1996 12 19 DL767954656 119951207A2620 EXTINGUISHER 892480 BOEING767 767232 1385132NM CABIN LEAKING A DALAO OTHER K FLUID LOSS TXTAXI/GRND HDL 1 SO27104DA DL1503 22216 VERBAL FROM CREW ON ARRIVAL, AFT CABIN WATER FIRE EXTINGUISHER LEAKING. REPLACED EXTINGUISHER. 2L72 4F RTA1NM 19961219004821996121900482NM 1996 12 19 DL72S954658 119951122A7110 INLET SKIN BOEING727 727232 1384082NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 TIME LIMITED REPAIR INSTALLED AT NR 2 ENGINE INLET DUCT HOUSING RT SKIN AT LOWER AFT CORNER OF ACCESS PLATE 9516 CUTOUT REF NR 86 PER M/M 54-30-0 PG 802. REPAIRED PER M/M 54-30-0 REF NR 861. 2L73 4F A3WE 19961219004831996121900483NM 1996 12 19 DL72S954659 119951127A7110 INLET SKIN BOEING727 727232 1384082NM NR 2 ENGINE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27496DA 21076 NR 2 ENGINE INLET EXT SKIN RIGHT SIDE TEMPORARY REPAIR DOUBLER AT LWR AFT CUTOUT FOR PANEL 9516. MANUFACTURED NEW DOUBLER PER M/M 54-30-0. INSTALLED REPAIR PER M/M 54-30-0. 2L73 4F A3WE 19961219004841996121900484NM 1996 12 19 DL72S954662 119951208A5711 STIFFENER BOEING727 727232 1384082NM WS 588 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27475DA 20752 FRONT SPAR STIFFENER, NOSE RIB ATTACH BRACKET CRACKED BETWEEN TWO LOWER FASTENERS AT NR 7 SLAT INBOARD TRACK AT APPROX IWS 588. REPLACED STIFFENER PER MM 57-20-21. 2L73 4F A3WE 19961219004851996121900485NM 1996 12 19 DLM88954667 119951207A301012911021 THERMOSTAT DOUG MD88 MD88 3023688NM LT ANTI-ICE MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS APAPPROACH 1 SO27945DL 49818 BURNING ODOR, NO VISIBLE SMOKE ON SHORT FINAL. SMOKE ALARMS IN AFT LAVS ACTIVATED. ANTI-ICE IN USE, ODOR DISSIPATED WHEN ANTI-ICE SHUT OFF. REPLACED ANTICIPATORS AND THERMOSTATS L/R SIDE. NO SMOKE OR ODOR NOTED DURING ENGINE RUN WITH ANTI-ICE ON. 2L72 4F RTA6WE 19961219004861996121900486NM 1996 12 19 DL72S954668 119951207A35304566M37B MASK BOEING727 727232 1384082NM CABIN POPPED INDICATORA DALAK NONE O OTHER ININSP/MAINT 1 SO27536DA 22049 DURING INSPECTION, FOUND FWD CABIN PBE WITH POPPED INDICATOR. REPLACED PBE. 2L73 4F A3WE 19961219004871996121900487NM 1996 12 19 DL757954669 119951207A3340233N321422 CONTROL PANEL BOEING757 757232 1384965NM FLT DECK FAILED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SO27625DL 22915 ON TAKOFF ROLL HAD SMELL OF ELECTRICAL BURNING. FOUND LEFT RUNWAY TURNOFF LIGHT SWITCH BAD. REPLACED CONTROL PNL FOR TAXI/RUNWAY TURNOFF AND FLOODLIGHTS, OPERATION NORMAL. 2L72 4F RTA2NM 19961219004881996121900488NM 1996 12 19 DL72S954670 119951208A33501000677 LIGHT BOEING727 727232 1384082NM FLT DECK INOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27531DA 21814 DURING PREFLIGHT, COCKPIT EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL. 2L73 4F A3WE 19961219004891996121900489NM 1996 12 19 DL76L954671 119951208A5620PA140U400515AR PANE BOEING767 767332 1382001NM CABIN CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27181DN 25986 DURING INSPECTION, FOUND CABIN WINDOW OUTER PANE CRACKED, AT SEAT ROW LOCTION LEFT SIDE 27A. REPLACED WINDOW PER MM. 2L72 4F RTA1NM 19961219004901996121900490WP 1996 12 19 DLL10954672 119951209A3234450100109 GEAR SELECTOR LKHEED1011 10113851 5265010WP FLT DECK FAILED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27712DA 193C1088 AFTER TAKOFF, UPON MOVING LDG GEAR HANDLE TO NEUTRAL GOT GEAR IN TRANSIT LIGHT ALONG WITH TAIL SKID AND DOORS. RETURNED, FERRIED AC TO ATL. REPLACED C/P LANDING GEAR CONTROL, SWUNG GEAR AND OPERATION NORMAL. 2L73 4F A23WE 19961219004911996121900491WP 1996 12 19 DLL10954673 119951209A2150B6388011 CONTROLLER LKHEED1011 10113851 5265010WP NR 2 PACK MALFUNCTIONED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27712DA 193C1088 AFTER T/O, SMOKE WAS DETECTED IN AFT LAV AND SMOKE DET WENT OFF. CABIN FILLED WITH SMOKE. PER CK LIST EVENTUALLY NR 2 PACK OVHT LIGHT CAME ON. UNLATCHED PACK, SMOKE STARTED TO CLEAR. REPLACED NR 2 PACK TEMP CONT, RAN ALL ENG TO T/O PWR WITH ALL THREE PACKS, NO SMOKE. NR 2 PACK CKS OK. 2L73 4F A23WE 19961226003791996122600379NM 1996 12 26 DL72W962734 119951218A5754651622296 SKIN BOEING727 727247 138408FNM NR 6 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO272807W 20579 AFT LOWER SKIN CRACKED I/B END. REPAIRED PER M/M 57-54-0. 2L73 4F A3WE 19970116001121997011600112NE 1997 1 16 CA960311003 219950825A7250 GP MODULE BELL 204 204B 1181404SW LYC T53 T5313B 41549NE ENGINE BURNED W A UNSCHED LANDING M OVER TEMP CLCLIMB 1 CA 5276 2551 LE07253X (CAN) ENGINE GP AND POWER TURBINE NOZZLE AND WHEEL BURNED. ALL ACCESSORIES SUCH AS NOZZLES. FCU, GOVERNOR, BLEED BAND, AIR VALVE WERE SENT FOR TEST AND HAVE TESTED SERVICEABLE. NO EROSION OR FOD FOUND ON COMPRESSOR ASSEMBLY. NO DAMAGE OR FAILURE FOUND ON ANY BEARING, GEAR OR GEARBOX. NO INTERNAL OR EXTERNAL MECHANICAL MALFUNCTION WERE FOUND AS A RESULT OF THIS OVERTEMP ON THIS ENGINE. 1G71 4U4 U H1SW E17EA 19970122000031997012200003NE 1997 1 22 CA960311024 219950726A8530 CYLINDER DHAV DHC3 DHC3 2800202EA PWA R1340 R1340* 52016NE ENGINE CRACKED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 25178 (CAN) DURING FLIGHT, ENGINE MALFUNCTIONED. AIRCRAFT LANDED ON FLOATS WITHOUT INCIDENT. CYLINDER FOUND CRACKED. CYLINDER REPLACED. 1H71 3R3 R A815 5E2 19970123004441997012300444WP 1997 1 23 97ZZZM85 119951028A2530 OVEN DOUG DC9 DC983 3022083WP GALLEY MALFUNCTIONED A TWAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE059413T 53188 PDX - DURING CRUISE 'D' GALLEY OVEN, MFG P/N 8203-11-0000 EMITTED SMOKE. OVEN WAS TURNED OFF AND CIRCUIT BREAKER PULLED. TROUBLESHOOTING UNDERWAY TO DETERMINE CAUSE. INVESTIGATION REVEALED OVEN HAD INTERNAL MALFUNTION AND WAS RETURNED TO THE MANUFACTURE. (M) 2L72 4F RTA6WE 19970123004451997012300445NE 1997 1 23 97ZZZM86 219951030A7261699602 BREATHER BOEING747 747131 1384881NM PWA JT9 JT9D7AH 52054NE NR 4 ENGINE OIL LEAK A TWAAE ENGINE SHUTDOWN KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CE0553110 19676 JFK - DURING CRUISE SHUT DOWN NR 4 ENGINE, S/N 4199, DUE TO DECREASING OIL QTY. FOUND OIL LEAKING IN ENGINE CORE. REPLACED NR 4 ENGINE AND ENGINE OPERATION CHECKED NORMAL. INVESTIGATION REVEALED NR 1 AND NR 2 BEARING BREATHER MANIFOLD BELLOWS PROTECTIVE SHIELD, MFG P/N 640640, WORE A SMALL HOLE IN BEARING BREATHER MANIFOLD ASSEMBLY, MFG P/N 699602. REPLACED BREATHER ASSEMBLY AND BREATHER MANIFOLD BELLOWS PROTECTIVE SHIELD. ENGINE S/N 4199 RETURNED TO SERVICE. (M) 2L74 4F4 F A20WE E20EA 19970206006271997020600627NE 1997 2 6 ORJA96114 219951209A7230500091601 LOCK RING DOUG DC9 DC983 3022083WP PWA JT8 JT8D219 52053NE C-1 BLADE CRACKED A ORJAK NONE O OTHER ININSP/MAINT 1 WP11882RA7153 49949 725578 FOUND C-1 BLADE LOCK RING BROKEN AT PULL HOLE APPROXIMATELY TWO INCHES FROM END. REPLACED C-1 BLADE LOCK RING. (M) 2L72 4F4 FRTA6WE E9NE 19970311000071997031100007GL 1997 3 11 CA960502062 219951114A732123059929 FUEL CONTROL BELL 206 206L 1181522SW ALLSN 250C 250C20 03013GL ENGINE CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 CA 458 CAE295257 (CAN) AIRCRAFT HAD TO OVERNIGHT DUE TO POOR WEATHER CONDITIONS. NEXT MORNING HOT STARTS. BATTERY, FUEL NOZZLE CHANGED, NO EFFECT. FINALLY CHANGED FCU, GOOD STARTS. ORIGINAL FCU BACK FROM REPAIR WAS FOUND TO BE OK. SUSPECT MOISTURE OR OTHER CONTAMINANTS. 1G71 3U3 U H2SW E4CE 19970415000211997041500021EU 1997 4 15 CA961112048 219951015A8530R854116 VALVE DIAMONDA20A1DA20A1 05626UXGL ROTAX 912 ROTAX912 55555EU EXHAUST WORN W K NONE O OTHER ININSP/MAINT 1 CA 898 (CAN) EXHAUST VALVE STEM FOUND WORN. SUSPECT BUILD UP OF CARBON POSSIBLY DUE TO A COMBINATION 100 LOW LEAD FUEL AND SYNTHETIC OIL USAGE. TECHNICAL BULLETIN 912-13 ADDRESSES THIS PROBLEM. 1L71 3O3 INTTA4CH EXPE3I 19970424006041997042400604WP 1997 4 24 GTIA9700172 119951028A5320 ANGLE DOUG DC9 DC932 3022066WP BS 832 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y832 BETWEEN LONGERON 29 RT AND LONGERON 26 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M) 2L72 4F A6WE 19970424006051997042400605WP 1997 4 24 GTIA9700173 119951028A5320 ANGLE DOUG DC9 DC932 3022066WP BS 815 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y 815 BETWEEN LONGERON 27 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M) 2L72 4F A6WE 19970424006061997042400606WP 1997 4 24 GTIA9700174 119951028A5320 ANGLE DOUG DC9 DC932 3022066WP BS 816 CRACKED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23941ML 47131 DTW - AFT CARGO COMPARTMENT FLOOR ANGLE WITH CRACKS IN Y816 BETWEEN LONGERON 28 RT AND LONGERON 24 LT. PERFORMED STOP DRILL ON FLOOR SUPPORT ANGLE IAW SRM 53-01. ITEM TO BE REPAIRED AT NEXT C-CHECK. (M) 2L72 4F A6WE 19970619004871997061900487NM 1997 6 19 CA970109015 119951228A56105893543129 WINDSHIELD BOEING737 737248C NM PWA JT8 JT8D9A 52048NE OUTER PANEL SHATTERED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA 90164H1332 674215 (CAN) IN CLIMB SHORTLY AFTER DEPARTURE, CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED EXTENSIVELY. REPLACED. 2L72 4F4 F A16WE E2EA 19970626004921997062600492SW 1997 6 26 CA970311028 119951218A7120206031302 SUPPORT CHANNEL BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL UPPER FLANGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 14319 CAE820733 (CAN) CRACKS FOUND IN UPPER FLANGE BEND RADIUS, FORWARD ENGINE ATTACHMENT. LOWER ROOF BEAM WEB P/N 206-031-200-019 CRACKED. 1G71 3U3 U H2SW E4CE 19970717003671997071700367EU 1997 7 17 CA951122016 119951020A8010F1727 RELAY ROTAX BRAERO748 HS7482A 4231001EU RROYCEDART DART5342 EU STARTER FAULTY W K NONE O OTHER ININSP/MAINT 1 CA 1271 19427 (CAN) STARTER BUTTON KICKS OUT AT 2700 RPM. OVERSPEED RELAY REPLACED WITH NO CHANGE. SEVERAL COMPONENTS REPLACED, NO CHANGE. OVERSPEED RELAY REPLACED AGAIN, NO CHANGE. KNOWN SERVICEABLE RELAY INSTALLED. SYSTEM SERVICEABLE. 2L72 3T4 T A24EU A196 19971218003841997121800384NM 1997 12 18 CA950320101 119950310A3260H1010153 SWITCHES BOEING727 72722C 138400FNM PWA JT8 JT8D7B 52053NE NOSE GEAR INTERMITTENT W K NONE O OTHER APAPPROACH 1 CA 655353 (CAN) ON APPROACH GEAR SELECTED DOWN THREE GREEN LIGHT ON. SHORTLY AFTER NOSE GEAR DOWN LIGHT INDICATOR WENT OUT. GEAR CYCLED ALL INDICATIONS NORMAL AND AIRCRAFT LANDED. NOSE GEAR POSITION AND LOCK SWITCHES REPLACED. 2L73 4F4 F A3WE E2EA 19980211001111998021100111NE 1998 2 11 98ZZZX588 219951114A7310430128601 MANIFOLD BELL 222 222U 1182140SW LYC LTS101LTS101750C1 41560NE ENGINE FUEL LEAKS A RMXAK NONE K FLUID LOSS ININSP/MAINT 1 SW056992 7A365 47521 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. OMNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1G72 3U3 U H9SW E5NE 19980211001121998021100112NE 1998 2 11 98ZZZX589 219950627A731043013761 MANIFOLD BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE FUEL LEAKS A RMXAK NONE K FLUID LOSS ININSP/MAINT 1 SW051140H813 S7078 LE45118 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. OMNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1G72 3U3 U H13EU E5NE 19980211001131998021100113NE 1998 2 11 98ZZZX590 219950616A7310430137601 MANIFOLD BOLKMS117 BK117A3 5626015EU LYC LTS101LTS101650B1 41560NE ENGINE FUEL LEAKS A RMXAK NONE K FLUID LOSS ININSP/MAINT 1 SW051140H1085 1G02322 S7078 LE45042 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. OMNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1G72 3U3 U H13EU E5NE 19980226006651998022600665EU 1998 2 26 WTAA950232 119950718A5330 SKIN BAG JETSTMJETSTM3101 1500215EU FUSELAGE BIRDSTRIKE A WTAAO OTHER C F.O.D. APAPPROACH 1 WP17417UE 794 BFL - BIRD STRIKE REPORTED AT LOWER LEFT SIDE OF FUSELAGE DURING APPROACH TO LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED BIRD STRIKE INSPECTION. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2L72 4T RTA21EU 19980505003171998050500317NM 1998 5 5 DL72S960582 119951125A5754 RIB 6516221100 BOEING727 727232 1384082NM NR 5 LE SLAT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27409DA BN1196 21153 LOWER AFT CORNER OF NR 2 RIB FROM OUTBOARD END CRACKED. REPAIRD PER MM 57 54 0, FIG 814, DURING SHOP INSPECTION FOR NR 5 L/E SLAT. 2L73 4F A3WE 19990226003431999022600343NM 1999 2 26 99ZZZX738 119950716A32602219300000 TARGET DORNERDO32 DO328100 2996000NM RT MLG BENT A EQGAO OTHER J WARNING INDICATION DEDESCENT 1 SW19328LS1376 3025 WHILE IN FLIGHT, PROXIMITY WEIGHT ON WHEEL FAIL MESSAGE ILLUMINATED. LANDED DFW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS INSPECTED FOR FERRY FLIGHT TO MAINTENANCE AND FERRIED TO HOT, GEAR DOWN. REPLACED WEIGHT ON WHEELS PROXIMITY SWITCH TARGET. PERFORMED GEAR RETRACTION AND EXTENSION IAW DORNIER MM, 32-31-00, OPS CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2H72 4T RTA45NM 20000205007662000020500766NE 2000 2 5 CA950711101 219950613A7200 ENGINE BELL 212 212 1181420SW PWA PT6T PT6T3B 52045NE NR 1 FIRE W A UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 CA (CAN) ROTORCRAFT CONDUCTED A NORMAL TAKEOFF, BUT WAS SOON FOLLOWED BY LOSS OF ALTITUDE. PILOT TOOK EVASIVE ACTION TO MISS TREES, BUT A HARD CRASH RESULTED AND ROTORCRAFT ROLLED ONTO RIGHT SIDE. FIRE WAS BURNING ON NR 1 ENGINE AND FIRE WAS THEN EXTINGUISHED. ALL PASSENGERS EVACUTATED WITH NO INJURIES. TSB INVESTIGATIONAT THIS TIME. 1G71 4U4 U H4SW E22EA 19950825005341995082500534 1995 8 25 AALA951232 419950711A3497 WIRE DOUG DC9 DC982 3022082WP E/E COMPT BROKEN A AALAA UNSCHED LANDING G MULTIPLE FAILURE CLCLIMB 1 SW07288AA 49300 ORD - FLT 1155 - AFTER T/O, JUST AFTER SLAT RETRACTION, A/C LOST YAW DAMPER OPERATION AND SIMULTANEOUS COMPUTER FAILURE WITH ALTITUDE IND STUCK AT FL 130, AIRSPEED IND STUCK AT 250 KTS AND FLT GUIDANCE COMPUTER C/B TRIPPED. A/C RETURNED AND LANDED W/O INCIDENT. GRD CHK OF FLT GUIDANCE SYS WAS UNABLE TO DUPLICATE PROBLEM. CHK'D WIRING IN AFT TAIL COMPART WITH NO DEFECTS NOTED. PRECAUTIONARY REPLACED NR 1 AND NR 2 DFGC'S NR 1 AND NR 2 AUTOPILOTS GRD CHK'D NORM OPERATION AND NR 1 AND NR 2 DFGC'S GROUND CHK'D NORM OPERATION. SUBSEQUENTLY, ON FLT 0578 DURING DESCENT IN DCA, PROB REPEATED. A/C LANDED DCA W/O INCIDENT. REPAIRED WIRE 2C610U2ORD BTWN P10-1206 AND S30-5 POST NR 10, WDM REF 22-16-11. OPS CHK OK.(M)2L72 4F A6WE 19960112002711996011200271SW 1996 1 12 QXEA9600009 119950104A3297 WIRE SWRNGNSA227 SA227AC 8780603SW NLG LOOSE A QXEAL ABORTED APPROACH N FALSE WARNING APAPPROACH 1 NM09380PH AC580 HLN - NOSE GEAR INDICATION DIDN'T ILLUMINATE UPON GEAR EXTENSION, BULB TESTED GOOD. ALTERNATE GEAR EXTENSION PERFORMED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT INSPECTED AND FERRIED TO BOI FOR REPAIR. LOOSE WIRES AT TERMINAL STRIP TS114 TIGHTENED. GEAR INDICATION OPS CHECKED GOOD ON GEAR SWING AND AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTA8SW 19950224003491995022400349EA 1995 2 24 COM60426 119950218A2750 WIRE CNDAIRCL600 CL6002B19 1900309EA RT TE FLAP SHORTED A COMAO OTHER O OTHER APAPPROACH 1 SO01937CA1183 7044 FLAPS FAILED AT 20 DEGREES ON APPROACH. REPAIRED SHORTED WIRING AT RT FLAP BRAKE POSITION SENSOR UNIT. 2L72 4F RTA21EA 19960822002331996082200233NE 1996 8 22 CA951129517 219951017A7260736664 ID GENERATOR SUNDSTRANDEM PWA JT9 JT9D7R4D 52054NE NR 2 ENGINE BROKEN CASING W EF ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE CRCRUISE 1 CA P707535 (CAN)#2 ENGINE ON FIRE AT FL410; FIRE EXTINGUISHED AFTER FIRE DRILL COMPLETED. ENGINE SHUTDOWN. GROUND INSPECTION FOUND INTEGRATED DRIVE GENERATOR (I.D.G.) CASING BROKEN. STATOR HOUSING BROKEN. FILTER CONTAMINATED, PIECES OF PISTON BROKEN. THERMO RELIEF VALVE OPEN, OIL DRAINED. UNIT REMOVED & FORWARDED TO MANUFACTURER FOR INSPECTION. 4 F E3NE 19970116001201997011600120 1997 1 16 CA960311031 119950816A7921AS3209219 O-RING PWA PW120 PW123 NE L/H OIL COOLER CUT W K NONE K FLUID LOSS CRCRUISE 1 CA 79 79 109057 (CAN) DURING FLIGHT, CREW NOTICED DROPPING OIL PRESSURE ON L/H ENGINE. THE L/H ENGINE WAS SHUT DOWN AS A PRECAUTIONARY PROCEDURE AND AIRCRAFT RETURNED TO ORIGIN. INVESTIGATION REVEALED A BAD OIL LEAK AT L/H OIL COOLER AREA. THE INLET COUPLING WAS REMOVED AND SHOWED A TORN AND IMPROPERLY INSTALLED 'O' RING. THE SEAL WAS INSTALLED AT THE WELDED JOINT AS OPPOSED TO BEING INSTALLED IN THE BOSS WHICH IS USED FOR THE SEAL. BOTH OIL COOLERS WERE INSEPCTED AND AIRCRAFT RETURNED TO SERVICE. 4 T E20NE 19960822002431996082200243EA 1996 8 22 CA951130016 219951112A8520 SEAL LYC O360 AEIO360A1B6 41514EA CRANKSHAFT DISPLACED W A UNSCHED LANDING K FLUID LOSS CRCRUISE 1 CA 98 L2652551A (CAN)IN CRUISE PILOT NOTICED OIL STREAMING BACK ALONG CANOPY. AN EMERG WAS DECLARED & ACFT LANDED.ENG WAS SHUTDOWN IMMEDIATELY & ACFT TOWED TO MAINT.THE OIL LEVEL PRIOR TO FLT WAS 6 QUARTS AFTER ENG SHUTDWN THE OIL LEVEL WAS CHECKED AT 3.5 QUARTS.POST FLT INSP FOUND THE FRONT CRANKSHAFT SEAL WAS POPPED OUT OF THE CRANKCASE.THE PROPELLER WAS REMOVED FOR INVESTIGATION & NO DEFECTS WERE FOUND.THE ENGINE OIL FILTER & SCREENS SHOWED NO DEFECTS.CRANKSHAFT SEAL WAS INSPECTED & FOUND SERVICEABLE.SEAL REINSTALLED.ENGINE BREATHER LINES LAGGED.IT IS SUSPECTED THAT THE ENG BREATHER LINES FROZE & THE CRANKCASE PRESSURIZED & THE SEAL POPPED OUT.ACFT RETURNED TO SERVICE. 3 O 1E10 19951006003721995100600372 1995 10 6 95UAL900168 419951002A2564D30658123 SLIDE RAFT R2 DOOR TORN A UALAK NONE L NO TEST ININSP/MAINT 1 WP29 DURING TIME CONTROLLED OVERHAUL OF A DOOR NR 2 RIGHT HAND SLIDE/RAFT, THE LOWER LEFT HAND INFLATION TUBE BURST DURING PROOF PRESSURE TEST. INTERNAL BULKHEAD IS SPLIT FOUR FEET AND INFLATION TUBE IS TORN IN TWO PLACES. RETURNED SLIDE/RAFT TO VENDOR FOR REPAIR. 19960815006951996081500695NE 1996 8 15 CA951122002 219951121A72302030371301 SEAL LYC ALF502ALF502R5 41580NE NR 9 BEARING FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CA LF05465A (CAN)FUMES IN THE CABIN WERE CAUSING THE PASSENGERS AND CREW TO BECOME ILL. AN INSPECTION OF THE ENGINE REVEALED #1 ENGINE HAD AN OIL LEAK INTO THE COMPRESSOR SECTION AND THEREFORE INTO THE AIR CYCLE MACHI NE. AIRCRAFT FERRIED BACK TO HOME BASE WITH #1 BLEED SYSTEM TURNED OFF. CAUSE OF OIL LEAK WAS FAULTY #9 BEARING SEAL. 4 F E6NE 19960926001351996092600135 1996 9 26 96ZZZX4798 219950615A7414104DD001678 IMPULSE COUPLINGBENDIX S6LN1227 MAGNETO FAILED DS K NONE O OTHER ININSP/MAINT 1 NM09 A208813FR IMPULSE COUPLING FAILED. 19961010009001996101000900 1996 10 10 CA960212022 119951208A7714333000017 TACHOMETER BFGOODRICH 333000017 LYC O360 AEIO360A1B6 41514EA ENG RPM SEIZED W A DE RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TXTAXI/GRND HDL 1 CA 27 5534 L2662554 (CAN)AFTER START UP THE PILOT OBSERVED NO TACH INDICATION AND THE ENGINE WAS SHUTDOWN. INVESTIGATION FOUND THE TACH HEAD WAS SEIZED INTERNALLY. A NEW MECHANISM WAS INSTALLED. 3 O 1E10 19950609008351995060900835NE 1995 6 9 USAA950462 219950511A7240616315A COMB OUTER CASE PWA JT8 JT8D9A 52048NE ENGINE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19 407324868 5020 667180 DURING ROUTINE SHOP INSPECTION, FOUND 1 INCH CRACK IN OUTER COMBUSTION CHAMBER CASE REAR FLANGE. REPLACED CASE. NOTE: CRACKED CASE SCRAPED. (X) 4 F E2EA 19950804006721995080400672 1995 8 4 95UAL900079 119950803A262180950017 CYLINDER FIRE BOTTLE FAILED A UALAK NONE L NO TEST ININSP/MAINT 1 WP29219 FIRE EXTINGUISHER BOTTLE FAILED HYDROSTATIC TESTING. SENT BOTTLE TO MANUFACTURER FOR DISPOSITION. 19950602004821995060200482NE 1995 6 2 95ZZZW752 219950301A7200 ENGINE PWA JT8 JT8D17R 52049NE NR 3 FAILED A AMTAA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL11779AT 707130 IND - AFTER TAKEOFF NR 3 ENGINE EGT MOMENTARILY REACHED 730 DEGREES CELSIUS. THIS WAS DUE TO THROTTLE CREEPING UP. REMOVED AND REPLACING NR 3 ENGINE. 4 F E2EA 19950414003831995041400383 1995 4 14 VTZA95120 119950329A79311241012 TRANSDUCER LT ENGINE FAILED A VTZAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27321UE 41045 FLT NR 6266 - IAD-BTV - DURING CLIMB-OUT THE LEFT ENGINE OIL PRESSURE FLUCTUATED BETWEEN 20-50 PSI. AIRCRAFT RETURNED TO IAD WITH NO FURTHER INCIDENTS. MAINTENANCE REPLACED THE OIL PRESSURE TRANSDUCER. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (W) 19950602001861995060200186GL 1995 6 2 95ZZZX2552 219950427A72506890040 SHIELD ALLSN 250C 250C20B 03013GL NR 1 NOZZLE DEFECTIVE A RMXAK NONE O OTHER ININSP/MAINT 1 SW05 382248 NOZZLE SHIELD HAS SADDLE PROTRUSIONS, UNDERSIZE. 3 U E4CE 19950526001831995052600183 1995 5 26 CAL950347 119950205A2421976J4981 GENERATOR NR 2 INOP A CALAA UNSCHED LANDING HJ ELECT. POWER LOSS-50 PC WARNING INDICATION CLCLIMB 1 SW09322AS FLT NR 0954 - ROR - NR 1 GENERATOR WAS ON PLACARD NR 2 GEN TRIPPED UNABLE TO RESET RETURNED TO ROR. CHANGED OUT BOTH GENERATORS ALL SYSTEMS CHECKS GOOD. (W) 19960822002751996082200275 1996 8 22 CA951215004 119951214A8011501113775 STARTER PLESSEY LYC ALF502ALF502R5 41580NE ENGINE OVERHEATED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CRCRUISE 1 CA 112191330 TE0967 LF05465A (CAN)STARTER OPERATING LIGHT CAME ON INFLIGHT. WENT OUT ON LANDING. STARTER VERY HOT TO TOUCH. STARTER REPLACED. 4 F E6NE 19960829000081996082900008 1996 8 29 CA951222001 119951209A7603157930 THROTTLE CABLE 157930 ROTAX 912 ROTAX912 55555EU INNER CORE KINKED W C ABORTED TAKEOFF O OTHER TOTAKEOFF 1 CA 447 4076114 (CAN) ENGINE FAILED TO COME UP TO POWER ON TAKEOFF, TAKEOFF ABORTED. RIGHT HAND CARBURETOR STAYING AT IDLE WHILE THE LEFT HAND CARBURETOR WENT TO WIDE OPEN WHEN THE THROTTLE WAS MOVED TO THE FULL THROTTLE POSITION. THE INNER CORE OF THE RIGHT HAND THROTTLE CABLE WAS LOOPED AND KINKED AT THE QUADRANT END. CABLE WAS REPLACED WITH NEW ONE. 3 I EXPE3I 19960105004261996010500426 1996 1 5 96ZZZM1 119951020A32469560892 WHEEL HALF LANDING GEAR CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15 DURING SHOP INSPECTION VISIT BY SUNJET DIRECTOR OF QUALITY CONTROL, FOUND 1 INCH CRACK ON WHEEL, P/N 9560892 S/N FEB71-350, OUTBOARD. CRACK STARTED FROM BOLT HOLE. WHEEL HALF UNSERVICEABLE AND SCRAPPED. 19960822003041996082200304WP 1996 8 22 CA951218015 219951206A732289737526Y FCU GARRTTTPE331TPE33110U 01514WP RT ENG MALFUCNTIONED W E ENGINE SHUTDOWN O OTHER CLCLIMB 1 CA 4347 P633350 (CAN)ON TAKEOFF ROLL, PILOT REPORTED A 50 DEGREES SPLIT IN ENGINE TGTS, ALL OTHER PARAMETERS NORMAL AND TGTS WITHIN LIMITS. DURING CRUISE PILOT NOTICED THAT THE RIGHT HAND ENGINE CONDITION LEVER WAS NOT RESPONSIVE TO POWER REDUCTION AS THE LEFT ENGINE. SUBSEQUENT GROUND RUN AND TEST FLIGHT COULD NOT FIND ANY DISCREPANCIES. 4 T E4WE 19960822002341996082200234NE 1996 8 22 CA951129518 219951018A7322315T304012 FCU BOX PWA JT9 JT9D7R4D 52054NE LT THROTTLE MALFUNCTION W O OTHER P NO WARNING INDICATION DEDESCENT 1 CA P709637 (CAN)AT TOP OF DESCENT THE LEFT THROTTLE JAMMED AT CRUISE POWER. WITH CONSIDERABLE FORCE IT WAS RETARDED ABOUT ONE WIDTH ABOVE RIGHT THROTTLE. POWER COULD NOT BE REDUCED TO IDLE. POST FLIGHT INSPECTION FOUND THE FUEL CONTROL BOX STIFF & RATCHETING. THE FUEL CONTROL BOX WAS REPLACED AND THE ENGINE CHECKED SERVICEABLE. 4 F E3NE 19960105004301996010500430 1996 1 5 96ZZZM2 119951020A3246GY18948 BOLT GOODYEAR 9560892 WHEEL CRACKED A A4JAK NONE O OTHER ININSP/MAINT 1 SO15 DURING SHOP INSPECTION VISIT BY SUNJET DIRECTOR OF QUALITY CONTROL, FOUND ONE CRACKED BOLT (P/N GY18948) ON WHEEL (P/N 9560892 S/N NOV77-5003/OCT90-982). REPLACED BOLT PER MM 32-40-22. 19960829000051996082900005NE 1996 8 29 CA951221035 219951214A72502143030R21 DISC SHAFT LYC ALF502ALF502R5 41580NE 3RD STAGE TURB LOOSE BLADES W K NONE O OTHER ININSP/MAINT 1 CA 110241796 LF05843 (CAN)ENGINE REMOVED DUE TO BOROSCOPE INSPECTION OF THE 2ND STAGE NOZZLE REVEALING CRACKING IN THE INNER SUPPORT, TO THE MAINTENANCE MANUAL LIMITS. DURING THE ENGINE TEARDOWN THE 3RD STAGE NOZZLE DISC BLADE S WERE FOUND LOOSE, DUE TO LOOSE RIVETS. 4 F E6NE 19960808007791996080800779GL 1996 8 8 CA951110007 219951010A73107000F1A16 COUPLING ? 903312 ALLSN 501D 501D13 03004GL FIREWALL MISALIGNED W E ENGINE SHUTDOWN O OTHER ININSP/MAINT 1 CA 501465 (CAN)UNCOMMANDED SHUT-DOWN OF RH ENGINE OCCURRED WHILE IN LOW SPEED GROUND IDLE SUBSEQUENT MAINTENANCE INSPECTION REVEALED ALIGNMENT PINS WITHIN DISCONNECT FITTING COUPLING WERE FOUND TO BE OUT OF ALIGNMENT. FIREWALL WIGGINS FUEL COUPLING FITTING FOR ENGINE FUEL LINE REPLACED. 4 T E282